hl9272 aircraft repetitive inspections and servicing

49
HL9272 Aircraft Repetitive Inspections and Servicing HL9272 Aircraft Make Model Aircraft N # Aircraft S/N ACTT Acft reg. due Date WO # Avg Flt Time Airbus EC155B1 N155TD 6664 5245.7 0/0/0 09/22/20 17-903 1.0 Engine Make Model Eng Serial # Engine TT CSN1 CSN2 TC Events Run on LDS Landin gs Sling loads Avg. landings Turbomeca Arriel 2C2 26175 2249.1 2533.13 599.81 16695 16695 N/A 10 Turbomeca Arriel 2C2 26108 1569.4 2739.13 760.56 Airbus EC155, Chapter 04-20-00 Manditory Inspections, Inspection Item ATA code Conditions Interval C/W @ ACTT/Date Next Due ACTT/Date Time Remaining Projected date due Margin NLT ACTT NLT Date Life raft AMM 25 69 01 222 Pre Mod 600 hrs N/A not Xmsn deck - MGB Fwd fitting AMM 53.41.00.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9 Xmsn deck - MGB Aft fitting AMM 53.41.00.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9 M/R blade - Tip cap AMM 62.10.00.223 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9 Spherical thrust AMM 05.22.00.213 N/A 15 hrs See Daily Times Update sheet for current C'd/W time Bearing AMM 62.24.02.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9 Frequency adapter AMM 05.22.00.213 N/A 15 hrs See Daily Times Update sheet for current C'd/W time Blade horn - Attach beam bolt AMM 62.24.03.991 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4 P/C rod - Blade horn bolt AMM 62.26.01.991 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4 Spherical thrust brg - Attach beam bolt AMM 62.24.02.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9 Frequency adapter - Attach beam bolt AMM 62.25.01.991 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4 Swashplate bearing AMM 62.23.02.641 N/A 100 hrs 5224.9 5324.9 79.2 02/12/21 10.0 5334.9 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9 Non-rotating swashplate AMM 62.23.02.991 N/A 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.2 N/A 2 yr 05/21/20 5/21/22 606 07/24/22 0.0 Rotating swashplate AMM 62.23.02.991 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4 Pitch - Change rod AMM 05.22.00.213 N/A 15 hrs See Daily Times Update sheet for current C'd/W time Scissors lower link AMM 62.23.01.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9 Scissors upper link AMM 62.23.01.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9 Flared housing - Fwd bar Attach AMM 62.22.00.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9 Airbus EC155, Chapter 04-20-00 Manditory Inspections, continued ACTT Inspection Item ATA code Conditions Interval C/W @ ACTT/Date Next Due ACTT/Date Time Remaining Projected date due Margin NLT ACTT NLT Date Flared housing - Skin AMM 62.22.00.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9 Page 1 of 49

Upload: others

Post on 06-Feb-2022

3 views

Category:

Documents


0 download

TRANSCRIPT

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

Aircraft Make Model Aircraft N # Aircraft S/N ACTT Acft reg. due Date WO # Avg Flt TimeAirbus EC155B1 N155TD 6664 5245.7 0/0/0 09/22/20 17-903 1.0

Engine Make Model Eng Serial # Engine TT CSN1 CSN2 TC Events Run on LDS

Landings

Sling loads

Avg. landings

Turbomeca Arriel 2C2 26175 2249.1 2533.13 599.81 16695 16695 N/A 10Turbomeca Arriel 2C2 26108 1569.4 2739.13 760.56

Airbus EC155, Chapter 04-20-00 Manditory Inspections,

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

Life raft AMM 25 69 01 222 Pre Mod 600 hrs N/A not Xmsn deck - MGB Fwd fitting AMM 53.41.00.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Xmsn deck - MGB Aft fitting AMM 53.41.00.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

M/R blade - Tip cap AMM 62.10.00.223 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Spherical thrust AMM 05.22.00.213 N/A 15 hrs See Daily Times Update sheet for current C'd/W time

Bearing AMM 62.24.02.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Frequency adapter AMM 05.22.00.213 N/A 15 hrs See Daily Times Update sheet for current C'd/W time

Blade horn - Attach beam bolt AMM 62.24.03.991 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4P/C rod - Blade horn bolt AMM 62.26.01.991 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4

Spherical thrust brg - Attach beam bolt AMM 62.24.02.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Frequency adapter - Attach beam bolt

AMM 62.25.01.991 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4

Swashplate bearing AMM 62.23.02.641 N/A 100 hrs 5224.9 5324.9 79.2 02/12/21 10.0 5334.9N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Non-rotating swashplate AMM 62.23.02.991 N/A 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.2N/A 2 yr 05/21/20 5/21/22 606 07/24/22 0.0

Rotating swashplate AMM 62.23.02.991 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4Pitch - Change rod AMM 05.22.00.213 N/A 15 hrs See Daily Times Update sheet for current C'd/W timeScissors lower link AMM 62.23.01.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Scissors upper link AMM 62.23.01.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Flared housing - Fwd bar Attach

AMM 62.22.00.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Airbus EC155, Chapter 04-20-00 Manditory Inspections, continued ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

Flared housing - Skin AMM 62.22.00.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Page 1 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

Rotor shaft AMM 62.21.00.991 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4Mast and/or hub AMM 62.20.00.291 Pre Mod 0762C42 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Flex Coupling (MGB side) AMM 05.22.00.213 N/A 15 hrs See Daily Times Update sheet for current C'd/W timePlant gear carrier AMM 63.20.00.291 N/A 50 hrs 5224.9 5274.9 29.2 12/24/20 0.0

MGB bottom AMM 63.20.00.212 After 2600 cls 15 hrs See Daily Times Update sheet for current C'd/W timeMGB fwd suspension bar AMM 63.30.01.991 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4

MGB aft RH suspension bar AMM 63.30.01.991 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4MGB aft LH suspension bar AMM 63.30.01.991 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4

T/R blade - SS ring AMM 05.22.00.213 N/A 15 hrsT/R hub AMM 64.20.04.991 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4

Splined flange AMM 64.20.00.992 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4Torsion bar AMM 64.20.00.225 N/A 2000 hrs 2000.0 -3245.7 01/06/12 0.0

T/R hub AMM 64.20.04.211 N/A 50 hrs 5224.9 5274.9 29.2 12/24/20 5.0 5279.9T/R Flexible coupling AMM 05.22.00.213 At MGB 15 hrs See Daily Times Update sheet for current C'd/W timeT/R Flexible coupling AMM 65.10.00.211 All 50 hrs 5224.9 5274.9 29.2 12/24/20 5.0 5279.9

Fwd shaft element AMM 65.10.01.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Center shaft element AMM 65.10.02.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Aft shaft element AMM 65.10.03.991 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9T/R Flexible coupling AMM 65.10.00.211 At TGB 50 hrs 5224.9 5274.9 29.2 12/24/20 5.0 5279.9

Airbus EC155 Chapter 05-20-00 Inspections ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

15 hour check AMM 05.22.00.213 N/A 15 hrs See Daily Times Update sheet for current C'd/W time7 days See Daily Times Update sheet for current C'd/W time

15 hour check AMM 05.22.00.214 N/A 15 hrs See Daily Times Update sheet for current C'd/W timeOptional equipment 7 days See Daily Times Update sheet for current C'd/W timeAdditional check "S" AMM 05.25.00.211 N/A 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

1 yr May-20 May-21 241 07/24/21 36 Jun-21Additional check "F" AMM 05.25.00.212 FAA req'd 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

FAA required with "S" ck 1 yr May-20 May-21 241 07/24/21 36 Jun-21Airbus EC155 Chapter 05-20-00 Inspections ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

Page 2 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

ATA 21P2 air system AMM 21.41.00.221 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4

Ventilation system AMM 21.51.00.221 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4Vent indicating system AMM 21.51.00.722 N/A 6000 hrs 0.0 6000.0 754.3 12/19/22 300.0 6300.0

Heating system AMM 21.41.00.721 N/A 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.21 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18

Heating - FLEXIRAC union seals AMM 21.41.04.211 Post Mod OP21C01 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Air conditioner AMM 21.52.00.211 N/A 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18AC - mechanical AMM 21.52.00.221 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

AC - electrical AMM 21.52.00.221 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Comp. elec.AC - belt AMM 21.52.00.067 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4

Air conditioner AMM 21.52.00.611 N/A 6 yr Nov-15 Nov-21 408 01/07/22 180 May-22Air conditioner system AMM 21.52.00.722 N/A 1 Mon Jan-18 Feb-18 -949 04/21/18 3 Feb-18

ATA 22SAS indicator sys AMM 22.10.00.722 N/A 6000 hrs 0.0 6000.0 754.3 12/19/22 300.0 6300.0

Ball end AMM 22.11.00.211 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9ATA 23

Radio - comm sys AMM 23.00.00.211 N/A 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.22 yr 42789.0 Feb-19 -577 04/28/19 73 May-19

External hailers AMM 23.42.01.221 N/A 600 hrs Not installed 60.0ATA 24

Electrical power sys AMM 24.00.00.211 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Elec pwr sys - bonding AMM 24.00.00.761 N/A 4 yr Feb-17 Feb-21 140 04/14/21 146 Jul-21

10 kVA alternator AMM 24.21.01.221 N/A 100 hrs 10.0AC power system AMM 24.20.00.211 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Main battery 40208-2 CMM 24.30.99 N/A 6 mon Jul-20 Jan-21 117 03/22/21 18 Feb-21Main battery 33490409000 CMM 24 39 91 N/A 6 mon 01/07/00 73

Main battery 40208-2 CMM 24.30.99 N/A 1 yr Jul-20 Jul-21 300 09/21/21 36 Aug-21

Airbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

Page 3 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

Main battery 40208-2 CMM 24.30.99 N/A 2 yr Jul-20 Jul-22 665 09/21/22 73 Sep-22Battery compartment AMM 24.31.01.141 N/A 2 yr Jul-17 Jul-19 -432 09/20/19 73 Sep-19Emergency battery CMM 24.39.38 N/A 2 yr Jul-17 Jul-19 -432 09/20/19 73 Sep-19Emergency battery AMM 24.31.02.741 N/A 1 yr Jul-17 Jul-18 -797 09/20/18 36 Aug-18

Battery circuit AMM 24.30.00.722 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Double power AMM 24.63.01.761 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Generator circuits AMM 24.30.00.722 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9ATA 25

Harness - all AMM 25.00.00.221 Also at install 1 yr Jul-17 Jul-18 -797 09/20/18 36 Aug-18Floats CMM 25.69.35 TSM 6 yr 11/06/15 Nov-21 408 01/07/22 180 May-22

TSM 9 yr 11/06/15 Nov-18 -687 01/08/19 180 May-19TSM 12 yr 11/06/15 Nov-21 408 01/07/22 180 May-22

Cylinder 704A42693007 TSM 3 yr Not installed 0Cylinder 704A42693013 TSM S/N 8107 5 yr May-16 May-21 245 07/28/21 0

TSM S/N 222 5 yr Feb-13 Jan-18 -965 04/05/18 0Cylinder AMM 25.62.01.761 TSM 1 yr Jul-17 Jul-18 -797 09/20/18 0Cylinder CMM 25.69.35 TSM 1 yr 07/18/17 Jul-18 -797 09/20/18 36 Aug-18

Emergency floatation gear CMM 25.69.35 TSM 18 mon Dec-00 -43731 03/04/01 36 Feb-01Emergency floatation gear AMM 25.62.01.211 3 yr Dec-00 -43731 03/04/01 54 Feb-01

ELT - Kannad 406 AMM 25.66.06.211 N/A 1 mon Jul-17 Aug-17 -1196 08/17/17 3 Aug-17AMM 25.66.06.721 1 yr Jul-17 Jul-18 -862 07/17/18 3 Jul-18

ELT HR Smith 500 27/ 12 Various N/A Various Not installedAirbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

VIP footsteps 2000 AMM 25.95.01.211 N/A 6000 hrs 0.0 6000.0 754.3 12/19/22 300.0 6300.012 yr Jan-04 Jan-16 -1718 03/13/16 180 Jul-16

ATA 26Eng Fire Ext - Cylinder AMM 26.21.00.222 PO 1 yr Sep-17 Sep-18 -747 11/09/18 36 Oct-18Eng Fire Ext - system AMM 26.21.00.211 N/A 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18Eng Fire Ext - system AMM 26.21.00.721 N/A 2 yr Jul-17 Jul-19 -432 09/20/19 73 Sep-19

Check valve AMM 26.21.00.221 N/A 2 yr Jul-17 Jul-19 -432 09/20/19 73 Sep-19Eng Fire ExT Cylinder P/N Hydro TSM 5 yr Not installed 0Eng Fire ExT - Cylinder P/N Hydro TSM S/N UR73527 7 yr Jul-15 Jul-22 674 09/30/22 0

Page 4 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

704A42820049 TSM S/N UR73486 7 yr May-15 Apr-22 584 07/02/22 0Fire Ext sys - Squib P/N

704A38710040, 041 AMM 26.21.00.761 N/A 2 yr Jul-17 Jul-19 -432 09/20/19 73 Sep-19

Eng Fire Ext - system AMM 26.21.00.721 N/A 2 yr 07/18/17 Jul-19 -432 09/20/19 73 Sep-19Hand fire ext. H1-10AIR CMM 26.24.04 N/A 6 mon Oct-17 Apr-18 -889 06/20/18 18 May-18

Bag. comp. Fire Ext - Cyl. AMM 26.23.01.221 PO 1 yr Jul-17 Jul-18 -797 09/20/18 36 Aug-18704A42820042 Hydro TSM 5 yr Not installed 0704A42820048* Hydro TSM S/N UP628UG 7 yr May-13 May-20 -117 07/31/20 0

Fire Ext sys - Squib P/N 704A38710040, 041 AMM 26.23.01.761 N/A 2 yr Jul-17 Jul-19 -432 09/20/19 73 Sep-19

ATA 28Fuel tank MTC 20.08.06.401 Damp atmos. 3 mon 9

Suplementary fuel tank AMM 28.12.01.221 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4Feeder tank - Bleed valve AMM 28.14.00.721 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4

Tank AMM 28.20.01.141 After install PO 3 hrs 7.0Engine supply line AMM 28.20.00.211 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4

Transfer pump CMM 28.19.03 N/A 2400 hrs 4644.4 7044.4 1798.7 10/28/25 240.0 7284.4Fuel transfer elec. pump AMM 28.20.03.721 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Airbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

Fuel shut-off valves AMM 28.20.02.721 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4Jet pump filter AMM 28.20.01.141 N/A 6000 hrs 0.0 6000.0 754.3 12/19/22 300.0 6300.0

Diodes, fuel manage panel AMM 28.40.00.761 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Fuel quantity indicator AMM 28.41.01.821 N/A 6000 hrs 0.0 6000.0 754.3 12/19/22 300.0 6300.0

Feeder tank low-level sensor AMM 28.41.03.721 N/A 6 yrs Nov-15 Nov-21 408 01/07/22 180 May-22Fuel flowmeter AMM 28.42.00.211 N/A 3000 hrs 3000.0 -2245.7 10/02/14 300.0 3300.0

Fuel anti-icing system AMM 28.93.01.211 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Fuel anti-icing thermal swt AMM 28.93.01.721 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4

ATA 29Hyd power system AMM 29.00.00.211 N/A 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18Hyd reservoir/manifold filter AMM 29.00.00.211 After install PO 2 hrs 5.0MGB comp. hyd pipes AMM 29.10.00.211 Pre mod 0729B68 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Page 5 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

Right hyd system AMM 29.11.00.612 N/A 2400 hrs 4644.4 7044.4 1798.7 10/28/25 240.0 7284.4AMM 29.11.00.612 Salt atmos. 2 yrs Jul-17 Jul-19 -432 09/20/19 73 Sep-19

Right hyd pump AMM 29.11.00.062 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4Left hyd system - hose AMM 29.12.00.211 Pre mod 0779B33 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

Left hyd system AMM 29.12.00.612 N/A 2400 hrs 4644.4 7044.4 1798.7 10/28/25 240.0 7284.4AMM 29.12.00.612 Salt atmos. 2 yrs Jul-17 Jul-19 -432 09/20/19 73 Sep-19

Left hyd pump AMM 29.12.00.062 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4Standby electric pump CMM 29.29.11 N/A 3000 hrs 3000.0 -2245.7 10/02/14 300.0 3300.0

ATA 30Windshield wiper blades Replace 1 yr Jul-17 Jul-18 -797 09/20/18 36 Aug-18

Windshield wiper AMM 30.42.00.721 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4Windshield washer AMM 30.43.01.211 N/A 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4

ATA 31Central panel display sys AMM 31.60.01.721 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Camera cockpit AMM 31.33.00.725 N/A 1 yr Jul-17 Jul-18 -797 09/20/18 36 Aug-18ATA 32

Landing gear AMM 12.30.00.611 Damp/salt atmos 7 days See log book for current times 0

Airbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

AMM 32.10.00.221 Std atmos. 1200 hrs 5233.2 6433.2 1187.5 02/25/24 120.0 6553.24 yrs Feb-17 Feb-21 152 04/26/21 146 Jul-21

Main landing gear AMM 32.10.00.221 Adverse Atmos. 1200hr/2 yrs 120/73AMM 32.10.00.613 N/A 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.2

N/A 1 yr Feb-18 Feb-19 -578 04/27/19 36 Mar-19AMM 32.10.00.611 N/A 2 yrs Jul-17 Jul-19 -432 09/20/19 73 Sep-19AMM 32.10.01.612 N/A 1200 hr 1200.0 -4045.7 10/28/09 120.0 1320.0

N/A 2 yrs Dec-01 -43366 03/04/02 73 Mar-02Main L/G-Shock absorbers AMM 32.10.01.611 Very cold 50 hrs

AMM 32.10.02.611 Std atmos. 1200 hrs 5233.2 6433.2 1187.5 02/25/24 120.0 6553.2Actuating strut 4 yrs Feb-17 Feb-21 152 04/26/21 146 Jul-21

AMM 32.10.02.611 Adverse Atmos. 1200hr/2 yrs 120/73

Page 6 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

AMM 32.20.00.221 Std atmos. 1200 hrs 5233.2 6433.2 1187.5 02/25/24 120.0 6553.24 yrs Feb-17 Feb-21 152 04/26/21 146 Jul-21

AMM 32.20.00.221 Adverse Atmos. 1200hr/2 yrs 120/73Nose landing gear AMM 32.20.00.613 N/A 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.2

N/A 1 yr Feb-18 Feb-19 -578 04/27/19 36 Mar-19AMM 32.20.00.611 N/A 2 yrs Jul-17 Jul-19 -432 09/20/19 73 Sep-19AMM 32.20.03.612 N/A 1200 hr 1200.0 -4045.7 10/28/09 120.0 1320.0

N/A 2 yrs Dec-01 -43366 03/04/02 73 Mar-02AMM 32.20.03.611 Std atmos. 1200 hrs 5233.2 6433.2 1187.5 02/25/24 120.0 6553.2

Actuating strut 4 yrs Feb-17 Feb-21 152 04/26/21 146 Jul-21AMM 32.20.03.611 Adverse Atmos. 1200hr/2 yrs 120/73AMM 32.30.00.221 Std atmos. 1200 hrs 5233.2 6433.2 1187.5 02/25/24 120.0 6553.2

Ext/ret control system 4 yrs Feb-17 Feb-21 152 04/26/21 146 Jul-21AMM 32.30.00.221 Adverse Atmos. 1200hr/2 yrs 120/73AMM 32.30.00.721 Std atmos. 1200 hrs 5233.2 6433.2 1187.5 02/25/24 120.0 6553.2

4 yrs Feb-17 Feb-21 152 04/26/21 146 Jul-21Landing gear AMM 32.30.00.721 Adverse Atmos. 1200hr/2 yrs 120/73

AMM 32.30.00.722 Std atmos. 1200 hrs 5233.2 6433.2 1187.5 02/25/24 120.0 6553.24 yrs Feb-17 Feb-21 152 04/26/21 146 Jul-21

AMM 32.30.00.722 Adverse Atmos. 1200hr/2 yrs 120/73Skis installation AMM 32.40.06.211 PO 45 hrs Not installed 5

Airbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

AMM 32.40.00.211 Std atmos. 600hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.2Wheel and tire 2 yrs Feb-18 Feb-20 -213 04/26/20 73 May-20

AMM 32.40.00.211 Adverse Atmos. 600hrs/1yr 60/36AMM 32.40.00.212 Std atmos. 1200 hrs 5233.2 6433.2 1187.5 02/25/24 120.0 6553.2

Wheel 4 yrs Feb-17 Feb-21 152 04/26/21 146 Jul-21AMM 32.40.00.212 Adverse Atmos. 1200hr/2 yrs 120/73AMM 32.40.00.213 Std atmos. 600hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.2

Page 7 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

Brake system 2 yrs Feb-18 Feb-20 -213 04/26/20 73 May-20AMM 32.40.00.213 Adverse Atmos. 600hrs/1yr 60/36

Ski installation-M/L gear AMM 32.40.06.211 Pre mod 0732B47 25 hrs Not installed 2AMM 32.40.03.721 Std atmos. 1200 hrs 5233.2 6433.2 1187.5 02/25/24 120.0 6553.2

Brake system 4 yrs Feb-17 Feb-21 152 04/26/21 146 Jul-21AMM 32.40.03.721 Adverse Atmos. 1200hr/2 yrs 120/73

Shoe AMM 32.40.05.211 N/A 100hr/1yr Not installed 10/36Ski installation AMM 32.40.06.611 Post mod 600hrs/1yr Not installed 60/36

LG not ext'd audio warning AMM 32.60.00.721 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Tail guard AMM 32.70.01.221 N/A 2 yrs Jul-17 Jul-19 -432 09/20/19 73 Sep-19Tail guard AMM 32.70.01.223 N/A 6000 hrs 0.0 6000.0 754.3 12/19/22 300 6300.0ATA 33Lights AMM 33.00.00.211 N/A 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.2

2 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19Retractable landing lights AMM 33.43.00.610 N/A 1 yr Jul-17 Jul-18 -797 09/20/18 36 Aug-18

Searchlight SX-16 AMM 33.43.07.221 N/A 600 hrs Not installed 60AMM 33.43.07.222 N/A 300 hrs Not installed 30

Searchlight Trakka A800 CMM 32.45.93 N/A 100 hr Not installed 10AMM 33.43.08.721 N/A 600 hrs Not installed 60

HEEL cabin roof - battery CMM 33.51.93 N/A 18 mon 54HEEL system AMM 33.50.03.721 N/A 18 mon 54

HEEL cabin roof - converter CMM 33.51.92 N/A 18 mon 54ATA 34

Navigation system AMM 34.00.00.211 N/A 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.21 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18

Air data system AMM 34.11.00.221 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9AMM 34.11.02.791 N/A 2 yrs Jul-17 Jul-19 -432 09/20/19 73 Sep-19

Airbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

Radar 1400 AMM 34.42.01.211 N/A 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.22 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19

Radar 1600 AMM 34.42.03.211 N/A 1200 hr / 3 yr Not installed 120/109

Page 8 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

Instrument control AMM 34.70.01.721 N/A 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.21 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18

Instrument control AMM 34.70.03.721 N/A 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.21 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18

Pelican rack fans AMM 34.70.05.721 N/A 600 hrs Apr-14 5824.9 579.2 06/27/22 60.0 5884.9ATA 45

CVR installation AMM 45.11.01.721&722 N/A 6 mon Not installed 18FDR & CVR data control AMM 45.11.01.724 N/A 1 yr Not installed 36

Discrete signals AMM 45.11.01.726 N/A 1 yr Not installed 36Immersion probe AMM 45.11.01.723 N/A 600 hrs Not installed 60

2 yrs Not installed 73CVFDR recorder AMM 45.11.04.724&726 Pre Mod 0731B89 6 mon Not installed 18

L3COM Post mod 6 mon Not installed 0AMM 45.11.04.727 Pre Mod 0731B89 1 yr Not installed 36

Post mod 1 yr Not installed 0RIPS AMM 45.11.04.723 N/A 1 yr Not installed 36

Immersion probe AMM 45.11.04.725 N/A 600 hrs Not installed 0ED55 margin 73H/60D N/A 2 yrs Not installed 0

CVFDR-ELT, L3COM Dukane DK120,120/90 N/A 2 yrs Not installed 0CVFDR recorder AMM 45.11.04.726 N/A 1 yr Not installed 36

ATA 52Doors AMM 52.00.00.211 Insp 100 hrs 5224.9 5324.9 79.2 02/12/21 10.0 5334.9

Crew doors AMM 52.11.00.221 DI 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.22 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19

ASB 52A018 Pre mod 52C23AMM 52.12.00.211 Post mod 52C23 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Sliding doors AMM 52.12.00.221 Post mod 52C23 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.2DI 2 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19

AMM 52.12.00.641 Post mod 52C23 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.2Lube 2 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19

Hinged doors AMM 52.12.01.221 DI 200 hrs Not installed 20VIP Hinged doors SB 52-029 Post mod OP53C80 200 hrs Not installed

ATA 53

Page 9 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

Structure AMM 12.30.00.611 Salt atmos. 7 days 0ALF 0

Structure - Bead AMM 53.00.00.211 Tropical/damp 100 hrs 10.0Salt atmos. 6 mon 18

Airbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

Structure and cowlings AMM 53.00.00.211 N/A 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.21 yr Oct-17 Apr-18 -887 06/22/18 36 May-18

Fwd bottom structure AMM 53.10.00.221 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Fwd bottom struct- Upper flange

longitude beam AMM 53.10.00.223 N/A 2 yrs Jul-17 Jul-19 -432 09/20/19 73 Sep-19

Transmission deck AMM 53.40.00.221 N/A 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Fwd bottom structure AMM 53.10.00.222 Adverse atmos. 10 yrs

Std atmos. 14 yrs Dec-13 -38986 03/01/14 180 Jun-14Engine deck AMM 53.00.00.223 N/A 7200 hrs 7200.0 1954.3 04/02/26 300.0 7500.0

Canopy and nose structure AMM 53.20.00.221 N/A 600 hrs 600.0 -4645.7 03/07/08 60.0 660.0Cabin/carbon structure attach AMM 53.20.00.223 Adverse atmos. 10 yrs

Std atmos. 14 yrs Dec-13 -38986 03/01/14 180 06/25/1425 degree frame AMM 53.20.00.223 Adverse atmos. 10 yrs

Std atmos. 14 yrs Dec-13 -38986 03/01/14 180 06/25/1412 degree frame AMM 53.20.00.223 Adverse atmos. 10 yrs

Std atmos. 14 yrs Dec-13 -38986 03/01/14 180 06/25/14Cabin structure AMM 53.30.00.221 DI 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Transmission deck AMM 53.40.00.222 TRQ ck 6000 hrs 0.0 6000.0 754.3 12/19/22 300.0 6300.0Transmission deck AMM 53.40.00.222 DI 7200 hrs 0.0 7200.0 1954.3 04/02/26 300.0 7500.0Cowlings & fairings AMM 53.50.00.221 DI 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.2

2 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19MGB cowlings AMM 53.50.00.221 Insp 100 hrs 5224.9 5324.9 79.2 02/12/21 10.0 5334.9

Cowling attachments AMM 53.50.00.222 DI 6000 hrs 0.0 6000.0 754.3 12/19/22 300.0 6300.0Aft removable cowling - Heat

shields or M15 protection AMM 53.54.00.211 If defects found do daily 100 hrs 5224.9 5324.9 79.2 02/12/21 10.0 5334.9

Aft structure assm. AMM 53.60.00.221 DI 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Page 10 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

Frame X 4630 AMM 53.60.00.222 DI 7200 hrs 0.0 7200.0 1954.3 04/02/26 300.0 7500.09 degree frame AMM 53.60.00.222 DI 7200 hrs 0.0 7200.0 1954.3 04/02/26 300.0 7500.0

Feeder tank AMM 53.60.00.222 Adverse atmos. 10 yrsmounting plate assm. Std atmos. 14 yrs Dec-13 -38986 03/01/14 180 06/25/14

Frame X 4630 AMM 53.60.00.222 Adverse atmos. 10 yrsStd atmos. 14 yrs Dec-13 -38986 03/01/14 180 06/25/14

Airbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

Main landing gear AMM 53.60.00.223 Adverse atmos. 10 yrsleg fittings Std atmos. 14 yrs Dec-13 -38986 03/01/14 180 06/25/14

Main landing gear brace AMM 53.60.00.223 Adverse atmos. 10 yrsstrut actuator fittings Std atmos. 14 yrs Dec-13 -38986 03/01/14 180 06/25/14Aft floatability cradles AMM 53.60.00.225 Adverse atmos. 8 yrs

Std atmos. 14 yrs Dec-13 -38986 03/01/14 180 06/25/14Cabin & baggage compt floor AMM 53.70.00.221 DI 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Chords of forward AMM 53.70.00.222a Pre mod 0753C71 8 yrs Dec-07 -41176 03/02/08 180 Jun-08Chords of forward AMM 53.70.00.222b Adverse atmos. 10 yrs

Post mod 0753C71 Std atmos. 14 yrsTail boom AMM 53.80.00.221 DI 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Structure to tail boom AMM 53.80.00.211 Adverse atmos. 8 yrsto fenestron junctions Std atmos. 14 yrs Dec-13 -38986 03/01/14 180 06/25/14

Structure to tail boom to fenestron junctions

AMM 53.80.00.222 DI 6000 hrs 0.0 6000.0 754.3 12/19/22 300.0 6300.0

Structure to tail boom to fenestron junctions

AMM 53.80.00.222 DI 7200 hrs 0.0 7200.0 1954.3 04/02/26 300.0 7500.0

Tail boom AMM 53.80.00.222 Adverse atmos. 8 yrsStd atmos. 14 yrs Apr-04 Apr-18 -902 06/07/18 180 10/01/18

Fenestron AMM 53.90.00.221 DI 600 hrs 5296.1 5896.1 650.4 09/06/22 60.0 5956.1Shrouded fenestron AMM 53.90.00.222 DI 8 yrs Apr-04 Apr-12 -3092 06/08/12 180 Oct-12

Carbon tube - TGB mount AMM 53.92.00.221 DI 7200 hrs 0.0 7200.0 1954.3 04/02/26 300.0 7500.0TGB flared coupling tube AMM 53.93.00.221 DI 7200 hrs 0.0 7200.0 1954.3 04/02/26 300.0 7500.0

8 yrs Apr-04 Apr-12 -3092 06/08/12 180 Oct-12ATA 55

Page 11 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

Horizontal stabilizer AMM 55.10.00.221 DI 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.22 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19

Out board fins AMM 55.30.00.221 DI 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.22 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19

ATA 56Jettisonable windows AMM 56.00.00.721 Jet ck 2 yrs Jul-17 Jul-19 -432 09/20/19 73 Sep-19

Sliding doors AMM 56.00.00.211 Post mod 52C23 100 hrs 5224.9 5324.9 79.2 02/12/21 10.0 5334.9Airbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

ATA 60MRH - Engine/MGB

coupling - T/R D/S - TRHAMM 05.39.00.221 Tropical/dampSalt

atmos.Initial 8 yrs

4 yrs after that 180

MRH - Engine/MGB coupling - T/R D/S - TRH

AMM 05.39.00.221 Standard conditions Initial 12 yrs 6 yrs after that Dec-11 -39716 03/01/12 180 Jun-12

MGB - TGB AMM 05.39.00.221 Tropical/dampSalt atmos.

Initial 8 yrs 4 yrs after that 146

MGB - TGB AMM 05.39.00.221 Standard conditions Initial 12 yrs 6 yrs after that Dec-11 -39716 03/01/12 180 Jun-12

ATA 62PO on New 90 hrs

Main rotor blade AMM 62.10.00.221 overhauled 180 hrsor repaired 360 hrs

Main rotor blade AMM 62.10.00.211 Sand/dust 15 hrsMain rotor blade AMM 62.10.00.211 Visual 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

ck 1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18Main rotor blade AMM 62.10.00.221 Tap ck 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.2

add insp. ck 2 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19Main rotor blade - Tip cap AMM 62.10.00.221 Tap ck 2 yrs Jul-17 Jul-19 -432 09/20/19 73 Sep-19

Main rotor blade AMM 60.00.00.101 Tropical/damp Salt atmos. 50 hrs 5.0

MRH or MRH component AMM 62.20.00.222 TRQ ck PO 3 hrs See log book for current times 7.0MRH AMM 12.20.00.211 Ck mag plug PO 3 hrs See log book for current times 7.0

Rotor blade pin AMM 62.10.00.061 Lube 300 hrs 5233.2 5533.2 287.5 09/08/21 30.0 5563.2

Page 12 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18MRH AMM 62.20.00.211 Insp 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18Frequency adapter AMM 62.20.00.211 Ck axial play 50 hrs 5224.9 5274.9 29.2 12/24/20 5.0 5279.9

MRH AMM 62.20.00.224 DI 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4MRH AMM 62.20.00.221 DI 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Airbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

MRH AMM 62.20.00.223 DI 3000 hrs 3000.0 -2245.7 10/02/14 300.0 3300.0NR mag speed sensor AMM 62.40.01.721 Func test 3000 hrs 3000.0 -2245.7 10/02/14 300.0 3300.0

Flared housing elec mag plug AMM 12.20.00.211 Insp 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.21 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18

Flared housing elec mag plug AMM 62.40.03.721 Func test 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9ATA 63

Flex coupling attach bolt on MGB side

AMM 63.10.02.221 After install PO 5 hrs See log book for current times 7.0

Eng/MGB coupling - Gimbals pins

AMM 63.10.00.221 Ck / lube 100 hrs 5224.9 5324.9 79.2 02/12/21 10.0 5334.9

Eng - MGB coupling AMM 63.10.00.221 DI 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Flex coupling (eng side) AMM 63.10.02.211 DI 50 hrs 5224.9 5274.9 29.2 12/24/20 5.0 5279.9

Flexible coupling AMM 63.10.02.221 DI 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9AMM 63.20.00.611 After install PO 45 hrs See log book for current times 5.0

MGB AMM 63.20.00.211 Insp 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.21 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18

AMM 63.20.00.221 DI 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Attach bolt MGB/servo-control AMM 63.20.00.222 Ck 4 yrs Feb-17 Feb-21 140 04/14/21 146 Jul-21

MGB - Mineral oil AMM 63.20.00.611 Drain 400 hrs 5233.2 5633.2 387.5 12/17/21 40.0 5673.22 yrs Oct-17 Oct-19 -339 12/22/19 73 Dec-19

MGB AMM 63.21.02.221 Ck oil filter PO 3 hrs See log book for current times 7.0Oil filter AMM 63.21.02.221 Insp 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18AMM 05.21.00.216 Ck ALF See log book for current times 0.0AMM 63.23.00.211 Insp 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

Page 13 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

Rotor brake 1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18AMM 63.23.00.221 DI 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9AMM 63.23.00.221 Adverse atmos. 600 hrs N/A 60.0

2 yrs N/A 73AMM 63.24.01.221 After install PO 100 hrs See log book for current times 10.0

MGB TDS flange AMM 63.24.01.221 Ck 300 hrs 5159.3 5459.3 213.6 06/26/21 30.0 5489.3AMM 63.24.01.221 Ck 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Airbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

AMM 63.30.00.222 TRQ ck PO 3 hrs See log book for current times 7.0Support Assembly AMM 63.30.00.211 Insp 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18AMM 63.30.00.221 DI 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4AMM 12.20.00.211 Insp 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

MGB - Elec mag plug 1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18AMM 63.40.02.721 Func test 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Oil temp warning system AMM 63.40.03.721 Func test 6 yrs Nov-15 Nov-21 408 01/07/22 180 May-22ATA 64

P/N 365A12-0060-01 AMM 64.10.00.211A PO 5 hrsAMM64.20.00.222&224 Install of & 25 hrs

P/N 365A12-0070-00 AMM 64.10.00.211B new, ovhl'd PO 5 hrs 10.0P/N 365A12-0070-01 AMM64.20.00.222&224 or repaired & 25 hrs 5.0P/N 365A12-0060-01 AMM 64.10.00.221A blade 90 hrs

P/N 365A12-0070-00/-01 AMM 64.10.00.221B 90 hrs 10.0P/N 365A12-0060-01 AMM 64.10.00.211A PO Install of 5 hrsP/N 365A12-0070-00 AMM 64.10.00.211B serviceable 5 hrs See log book for current times 10.0P/N 365A12-0070-01 AMM 64.20.00.222 blade

T/R blade-Protect from erosion AMM 64.10.00.065 Post mod OP61B33 100 hrs 5224.9 5324.9 79.2 02/12/21 10.0 5334.9P/N 365A12-0060-01 AMM 64.10.00.211A Visual 100 hrs 10.0

P/N 365A12-0070-00/-01 AMM 64.10.00.211B insp 100 hrs 5224.9 5324.9 79.2 02/12/21 10.0 5334.9

Page 14 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

T/R blade - ALL AMM 64.10.00.101 Salt atmos. 50 hrs 5224.9 5274.9 29.2 12/24/20 5.0 5279.9P/N 365A12-0060-01 AMM 64.10.00.211A Sand/dust 15 hrs

P/N 365A12-0070-00/-01 AMM 64.10.00.211B atmos. 15 hrsP/N 365A12-0060-01 AMM 64.10.00.221A Visual 600 hrsP/N 365A12-0060-01 AMM 64.10.00.211A Tap ck 2 yrs

P/N 365A12-0070-00/-01 AMM 64.10.00.221B Visual 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4P/N 365A12-0070-00/-01 AMM 64.10.00.211B Tap ck 2 yrs Jul-17 Jul-19 -432 09/20/19 73 Sep-19

AMM 64.20.00.222 Install PO 3 hrs 07/22/10 7.0Tail rotor head AMM 64.20.00.211 Insp 100 hrs 5224.9 5324.9 79.2 02/12/21 10.0 5334.9

AMM 64.20.00.225 DI 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4Airbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

ATA 65Bearing AMM 65.10.00.211 After lube PO 3 hrs See log book for current times 7.0

Tubes and bearings AMM 65.10.00.211 Ck 50 hrs 5224.9 5274.9 29.2 12/24/20 5.0 5279.9Tail rotor drive shaft AMM 65.10.00.222 DI 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Brg mounts T/R D/S sys AMM 65.10.00.225 Adverse atmos. 8 yrs N/A 180Std atmos. 14 yrs

Tail rotor drive shaft AMM 65.10.00.641 Lube 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.26 mon Oct-17 Apr-18 -889 06/20/18 18 May-18

AMM 65.20.01.611 Drain PO 45 hrs See log book for current times 5.0AMM 65.20.02.061 TRQ ck PO 3 hrs See log book for current times 7.0AMM 65.20.00.211 Insp 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

TGB 1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18AMM 65.20.00.221 Ck corrosion 1200 hrs 5233.2 6433.2 1187.5 02/25/24 120.0 6553.2

4 yrs Feb-17 Feb-21 152 04/26/21 146 Jul-21AMM 65.20.00.221 DI 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

TGB - Mineral oil AMM 65.20.01.611 Drain 400 hrs 5233.2 5633.2 387.5 12/17/21 40.0 5673.22 yrs Oct-17 Oct-19 -339 12/22/19 73 Dec-19

AMM 12.20.00.211 Insp 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2TGB - Elec mag plug 1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18

AMM 65.40.01.721 Func test 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Page 15 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

ATA 67Rotor controls AMM 67.00.00.221 Advers atmos 2 yrs N/A 73

AMM 67.00.00.212 ALL 7200 hrs 0.0 7200.0 1954.3 04/02/26 300.0 7500.0Flight control systems Advers atmos 10 yrs N/A 180

Std atmos. 14 yrsAMM 67.10.00.223 Mag ck PO 12 yrs Dec-11 -39716 03/01/12 180 Jun-12AMM 67.10.00.621 Advers atmos 100 yrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2

Main rotor controls 1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18AMM 67.10.00.221 Insp 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.2

2 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19

Airbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

AMM 67.10.00.224 Tropical/damp 6 mon N/A 18.0Ball control AMM 67.10.00.224 Salt atmos. 1 yr N/A 36

AMM 67.10.00.224 Std atmos. 2 yrs Jul-17 Jul-19 -432 09/20/19 73 Sep-19Collective lever AMM 67.12.01.822 Ck 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

AMM 67.20.00.621 Tropical/damp 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.2Tail rotor controls Salt atmos. 1 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18

AMM 67.20.00.221 Insp 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.22 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19

AMM 67.20.00.222 Tropical/damp 6 mon N/ABall control AMM 67.20.00.222 Salt atmos. 1 yr N/A 36

AMM 67.20.00.222 Std atmos. 2 yrs Jul-17 Jul-19 -432 09/20/19 73 Sep-19Main rotor servo-control AMM 67.30.01.061 After install PO 3 hrs See log book for current times 7.0T/R servo-control-input lever AMM 67.30.02.222 Ck 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Servo-controls AMM 67.30.00.221 Insp 1200 hrs 4644.4 5844.4 598.7 07/16/22 120.0 5964.4Main rotor servo-control AMM 67.30.01.061 TRQ ck 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.2

2 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19Hyd power assistance AMM 67.30.01.721 Test 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Servo-control - Test AMM 67.30.00.711 Cold temp 15 hrs Check forcast for applicability

Post Mod 0739C30 & Pre Mod 0739C37 7 days

Page 16 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

ATA 71Engine bay fan AMM 71.00.00.211 Ck 50 hr 5

Power plant installation AMM 71.00.00.211 DI 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.22 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19

Engine mounts AMM 71.20.00.221 DI 6000 hrs 0.0 6000.0 754.3 12/19/22 300.0 6300.0Fire walls AMM 71.30.00.221 DI 7200 hrs 0.0 7200.0 1954.3 04/02/26 300.0 7500.0

Engine flushing system AMM 71.60.20.221 DI 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9Sand filter AMM 71.61.01.221 Insp 600 hrs

ATA 73AMM 73.20.00.761 Test 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

FADEC unit AMM 73.20.00.762 Ck 100 hrs 5233.2 5333.2 87.5 02/20/21 10.0 5343.21 yr Oct-17 Oct-18 -704 12/22/18 36 Nov-18

Airbus EC155 Chapter 05-20-00 Inspections, (Continued) ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

ATA 77Emer cntrl op "EBCAU" FLM Sec. 8.3 Ck 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Fuzz burner AMM 77.30.00.721 Func test 600 hrs2 yrs

ATA 79Engine AMM 79.00.00.211 After install PO 3 hrs See log book for current times 7.0

Eng/MGB oil cooling sys Pre mod 0779B33 100 hrs 5224.9 5324.9 79.2 02/12/21 10.0 5334.9Pre mod 0750B32 // Pre mod 0771C26 100 hr 5224.9 5324.9 79.2 02/12/21 10.0 5334.9

External oil system AMM 79.00.00.211B Insp 6 yr Nov-15 Nov-21 408 01/07/22 36 Dec-21Elec mag plug-eng oil tank AMM 79.20.00.721 FT 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Eng oil temp switch AMM 79.30.00.721 Insp/tst 6000 hrs 0.0 6000.0 754.3 12/19/22 300.0 6300.06 yrs Nov-15 Nov-21 408 01/07/22 180 May-22

Eng oil temp probe AMM 79.30.00.722 Insp/tst 6 yrs Nov-15 Nov-21 408 01/07/22 180 May-22ATA 80

CMM 80.19.02 S/N 1500 hrs 4484.7 5984.7 739.0 12/04/22 150.0 6134.7Starter generator Rpl brgs PO S/N 1500 hrs 4441.7 5941.7 696.0 10/22/22 150.0 6091.7

AMM 80.10.00.211 Sys insp 600 hrs 5224.9 5824.9 579.2 06/27/22 60.0 5884.9

Page 17 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

Ck brushesATA 88

Connection and wiring AMM 88.00.00.211 Insp 600 hrs 5233.2 5833.2 587.5 07/05/22 60.0 5893.22 yrs Feb-17 Feb-19 -577 04/28/19 73 May-19

ATA 93FLIR installation Wescam AMM 93.51.01.221 DI 600 hrs N/A not installedFLIR installation U7000 AMM 93.51.02.211 Insp/tst 100 hr/1 yr N/A not installedFLIR installation U7000 AMM 93.51.02.721 FT 100 hr/1 yr N/A not installed

FLIR installation UF350EP AMM 93.51.04.221 Insp/tst 100 hr N/A not installed

Airbus Chapter 05-50-00 Inspections further to an event ACTT

Inspection Item ATA code Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due Margin NLT

ACTTNLT Date

Aft removable cowling - Heat shields or M15 protection AMM 53.54.00.211 Until replaced Ater last flt of the

day See log book for current times

Lower attach beam - Adapter plastic bunches AMM 62.24.05.991 Until replaced 15 hrs See log book for current times

Upper attach beam - Adapter plastic bunches AMM 62.24.05.991 Until replaced 15 hrs See log book for current times

Blade horn - Stop ring AMM 62.24.03.991 Until replaced 15 hrs See log book for current timesPitch change rod - Swivel brg AMM 62.26.01.991 Until replaced 15 hrs See log book for current times

Rotor mast - Elec mag plug AMM 12.20.00.211 Metal on plug Ater each flt for 25 hrs See log book for current times

AMM 63.21.02.221 Ck filter every 5 hrs for 25 hrs See log book for current times

MGB suspension bars - AMM 63.30.00.991 Until replaced 100 hrs 5233.2 5333.2 87.5 02/20/21 Bars: swivel bearings 1 yr Oct-17 Oct-18 -704 12/22/18

MGB - Elec mag plug AMM 12.20.00.211 Metal on plug Ater each flt for 25 hrs See log book for current times

AMM 63.21.02.221 Ck filter every 5 hrs for 25 hrs See log book for current times

Page 18 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

Tail rotor blade See log book for applicablityP/N 365-A12-0060-01 AMM 64.10.00.221A If fault found 50, 100, 150

P/N 365A12-0070-00/-01 AMM 64.10.00.221B If fault found & 300 hrs

TGB - Elec mag plug AMM 12.20.00.211 Metal on plug Ater each flt for 25 hrs See log book for current times

Turbomeca Arriel Scheduled Inspections, Chapter 05-20-10 ACTTTurbomeca Arriel 2C2 #1 engine

ATA Task code Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due

05-20-10-201-810-A01 15 hr or See Daily Times Update sheet for current C'd/W time7 days See Daily Times Update sheet for current C'd/W time

05-20-10-201-812-A01 25 hrs See Daily Times Update sheet for current C'd/W time05-20-10-201-815-A01 30 hrs See Daily Times Update sheet for current C'd/W time05-20-10-201-817-A01 50 hrs 5226.2 5276.2 30.5 12/25/2005-20-10-201-835-A01 300 hrs 5226.2 5526.2 280.5 09/01/2105-20-10-201-850-A01 600 hrs 5226.2 5826.2 580.5 06/28/2205-20-10-201-880-A01 3000 hrs 2996.6 5996.6 750.9 12/15/22

Turbomeca Arriel 2C2 #2 engine

ATA Task code Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due

05-20-10-201-810-A01 15 hr or See Daily Times Update sheet for current C'd/W time7 days See Daily Times Update sheet for current C'd/W time

05-20-10-201-812-A01 25 hrs See Daily Times Update sheet for current C'd/W time05-20-10-201-815-A01 30 hrs See Daily Times Update sheet for current C'd/W time

Page 19 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

05-20-10-201-817-A01 50 hrs 5226.2 5276.2 30.5 12/25/2005-20-10-201-835-A01 300 hrs 5226.2 5526.2 280.5 09/01/2105-20-10-201-850-A01 600 hrs 5226.2 5826.2 580.5 06/28/2205-20-10-201-880-A01 3000 hrs 3676.3 6676.3 1430.6 10/25/24

FAR & Ops Manual Required Inspections

Inspection Item Requirement Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due

Altimeters FAR 91.411 N/A 24 months Dec-01 -43366 03/04/02Transponder FAR 91.413(a) N/A 24 months Mar-20 Mar-22 536 05/15/22 X

ELT FAR 91.207(d) N/A 12 months May-20 May-21 241 07/24/21Avionics Ops Manual N/A 12 months No longer required

Weighting FAR 135.185 N/A 36 months Mar-20 Mar-23 914 05/28/23ELT installed Kannad

Model 406 AF P/N S1821502-02 S/N L0746-0096Battery P/N S1820516-99 S/N UNK Retire due Nov-23

Location LH Aft Baggage Compartment overheadRepetitive AD's Airframe ACTT

Inspection Item Part Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due

AD2004-12-06 (b)(2) M/R blades Daily / 10 hrs See AMOC dated 02/19/13ASB 62A006 2.B.1 & 2.B.5 660 hrs 5233.2 5893.2 647.5 09/03/22

AD2004-16-15R1 (b) MGB base plate 15 hrs See HFS 108 form for current timeASB 05A005

AD2010-19-05 (e)(2) T/R Blades 15 hrs N/A by the P/N of the T/R blades installedEASB 05A011AD2010-20-20 (a) MGB carrier 50 hrs 5233.2 5283.2 37.5 01/01/21

EASB 05A007R2AD2013-03-02 (f)(1) T/R hub 55 hrs 5233.2 5288.2 42.5 01/06/21

ASB EC155-05A021R1AD2014-02-04 (e)(1)(i) Vertical 55 hrs N/A by P/N of fittings installedASB 05A017 Stabilizer

AD2016-23-05 (1)(iii) & (2) T/R G/B oil level 15 hrs See HFS 108 form for current time

Page 20 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

AD2018-19-01 ( e )(1)(i) Outer Skin 660 hrs 5233.2 5893.2 647.5 09/03/22ASB 05A033 ( e )(2) X4630 thru X6630 110 hrs 5233.2 5343.2 97.5 03/02/21

Repetitive AD's Engine

Inspection Item Part Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due

FAA AD2016-03-02 MSB 292.72.2860 See AMOC dated 08/08/17 for accomplishment

TCB resistance ck #1 engine 600 hrs 5233.2 5833.2 587.5 07/05/22 xFAA AD2016-03-02 MSB 292.72.2860 See AMOC dated 08/08/17 for accomplishment

TCB resistance ck #2 engine 600 hrs 5233.2 5833.2 587.5 07/05/22 x

FAA AD2016-25-13 MSB 292.72.2861AGB wear ck #1 engine 600 hrs N/A by AGB P/N

FAA AD2016-25-13 MSB 292.72.2861AGB wear ck #2 engine 600 hrs N/A by AGB P/N

Repetitive Airframe Bulletins

Inspection Item Part Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due

ASB EC155-04A014 Rev 3TGB - Control rod 1.E.2.a.1. 15 hr / 7 day See Daily Times Update sheet for current C'd/w time

Double bearing 1.E.2.a.2. 25 hrs See HFS 108 form for current time Brg replc'd 09/24/16EC155 05-012

Ck for corrosion MRH beams 1.E.2.b 36 months Dec-02 -43001 03/04/03ASB EC155 05A021 Rev 1 FAA AD2013-03-02

TR blade insp. 1.E.2. 55 hrs 5233.2 5288.2 42.5 01/06/21EC155-05-032 Rev 1

Landing gear No longer applicable SB incorporated into the manual

Page 21 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

Corrosion checkASB EC155-05A033

Baggage Compartment 1.E.2.a. Visual 110 hrs 5233.2 5343.2 97.5 03/02/21 xSkin Tap 660 hrs 5233.2 5893.2 647.5 09/03/22

ASB EC155-05A034 Rev 5Periodic check for metal 3.B.2.a Ck mag plugs 10 hrs See HFS 108 form for current timePlanetary gears replaced 3.B.2.c Ck filter 25 hrs 25.0 -5220.7 08/10/06

After 400 hrs 3.B.2.b & .c Insp bottom 55 hrs 55.0 -5190.7 09/09/06ASB EC155-52A018Cabin sliding door See the ASB ALF & 15 hr See Daily Times Update sheet for current C'd/W time

maintenance for details 100 hr 100.0 -5145.7 10/24/06600 hr or 660.0 -4585.7 05/06/0824 month 12/30/01 -43366 03/04/021200 hr 1200.0 -4045.7 10/28/09

Non Repetitive Bulletins Coming dueASB EC155-34A033

AHRS wiring mod. Due by -44160 01/00/00ASB EC155-63A013

T/R drive flange Issue date As of issue 600 hrs 600.0 -4645.7 03/07/08Install of rear stop 01/22/18 date of ASB 24 months 12/30/01 -43366 03/04/02

ASB EC155-53A038Mod of MGB cowling As of the issue date 110 hrs 5233.2 5333.2 87.5 44247.5

Repetitive Engine Bulletins ACTT

Inspection Item Part Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Projected date due

MSB 292.72.2860 FAA AD2016-03-02TCB resistance ck #1 engine 600 hrs 5233.2 5833.2 587.5 07/05/22MSB 292.72.2860 FAA AD2016-03-02TCB resistance ck #2 engine 600 hrs 5233.2 5833.2 587.5 07/05/22

MSB 292.72.2861 FAA AD2016-25-13AGB wear ck #1 engine 600 hrs N/A by AGB P/N x

Page 22 of 49

HL9272 Aircraft Repetitive Inspectionsand Servicing

HL9272

MSB 292.72.2861 FAA AD2016-25-13AGB wear ck #2 engine 600 hrs N/A by AGB P/N x

Repetitive Vendor Bullentins

Inspection Item Part Conditions Interval C/W @ ACTT/Date

Next Due ACTT/Date

Time Remaining

Percent Remaining Margin NLT

ACTTNLT Date

NoneTurbomeca Engine Servicing, Note for both engines ACTT

Servicing or Lube Item Chapter Conditions IntervalC/W @

ACTT/Date

@

ACTT/DateTime

Remaining Projected date due

Oil service 05-20-10-201- Oil & filter 600 hrs 600.0 -4645.7 03/07/08850-A01 Replace 12 mon Dec-00 -43731 03/04/01

Fuel filter Same Replace 600 hrs 600.0 -4645.7 03/07/08Service with Engine

Misc. Servicing

Servicing Item Requirement Conditions IntervalC/W @

ACTT/DateNext Due

ACTT/DateTime

Remaining Percent

RemainingC/W Initial

C/W at ACTT

C/W on Date

NiCad battery Top Chg/Water N/A 6 months Jul-20 -65 -36%S/N MO0192 Deep Cycle N/A 12 months Jul-20 -65 -18%ELT Battery Retire N/A I/A/W Manu Nov-23 Oct-29 3325 152%

Fire Visual insp. N/A 1 month See Flight log 108 form for current dateExtinguisher Weight Ck N/A 12 months Dec-00 -43731 -11981%

S/N C-32532084 Replace N/A 10 year Dec-09 -40446 -1108%Life Vest Recert. N/A 12 months Jul-20 Jul-21 282 77%

First Aid Kit Out of date items N/A 12 months Dec-00 -43731 -11981%

Davtron clock Battery replacement 12 months Dec-00 -43731 12/30/00Data Base Updates

Item Requirement Conditions IntervalC/W @

ACTT/DateNext Due

ACTT/DateTime

Remaining Percent

RemainingC/W Initial

C/W at ACTT

C/W on Date

Garmin Nav. Data Update N/A 28 days 01/28/00 -44068 ########

Page 23 of 49

N155WH N155WH

Aircraft Make Model Aircraft N # ACFT S/N ACTT TC Events Run on

LDSDaily

Landings Date

Airbus EC155B1 N155TD 6664 5245.7 16695 N/A 16695 12/06/17

Engine Make Model Eng Serial # Eng. TT CSN1 CSN2

Turbomeca Arriel 2C2 26175 2249.1 2533.13 599.81

Turbomeca Arriel 2C2 26108 1569.4 2739.13 760.56 * indicates installed P/N

Airbus EC155B, Chapter 04-10-00, Airworthiness Limitations Section RT(P) Possible extention

Component Part Number Serial Number SLL Date of Install

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining

ATA 53Trans deck - 365A21-8117-00 VAI82 Ret 16100 01/01/03 0.0 0.0 16100.0 10854.3

MGB fwd fitting 365A21-8117-01 VAI87 Ret 16100 01/01/03 0.0 0.0 16100.0 10854.3Trans deck - 365A21-8201-00 SD078 Ret 20000 02/01/03 0.0 0.0 20000.0 14754.3

MGB fitting assy SD096 Ret 20000 02/01/03 0.0 0.0 20000.0 14754.3Trans deck - 365A21-3355-04 S1056 Ret 3200 10/12/09 0.0 3189.0 6389.0 1143.3

MGB aft fitting 365A21-3355-05 S1117 Ret 3200 10/12/09 0.0 3189.0 6389.0 1143.3Carbon tube - TGB mount 365A23-4211-00/-02 Ret 30000 Not installedCarbon tube - TGB mount 365A23-4210-02 M1779 Ret 20000 04/01/03 0.0 0.0 20000.0 14754.3

365A23-4213-00 Ret 20000 Not installedATA 62

365A11-0080-00 390 Ret 10000 08/01/03 0.0 0.0 10000.0 4754.3404 Ret 10000 07/01/03 0.0 0.0 10000.0 4754.3

Main rotor blade 414 Ret 10000 07/01/03 0.0 0.0 10000.0 4754.3423 Ret 10000 07/01/03 0.0 0.0 10000.0 4754.3424 Ret 10000 07/01/03 0.0 0.0 10000.0 4754.3

365A11-0080-01 Ret 20000 Not installedDe-iced Main rotor blade 365A11-0082-00 Ret 1000 Not installed

Lower attach beam 365A31-4596-00* M749 Ret 5350 05/01/03 0.0 0.0 5350.0 104.3365A31-4596-01 M751 Ret 5350 05/01/03 0.0 0.0 5350.0 104.3

M768 Ret 5350 05/01/03 0.0 0.0 5350.0 104.3M829 Ret 5350 05/01/03 0.0 0.0 5350.0 104.3M844 Ret 5350 05/01/03 0.0 0.0 5350.0 104.3

Page 24 of 49

N155WH N155WH

Airbus EC155B, Chapter 04-10-00, Airworthiness Limitations Section RT(P) Possible extention

Component Part Number Serial Number SLL Date of Install

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining Upper attach beam 365A31-4597-01 M830 Ret 5350 05/01/03 0.0 0.0 5350.0 104.3

M832 Ret 5350 05/01/03 0.0 0.0 5350.0 104.3M833 Ret 5350 05/01/03 0.0 0.0 5350.0 104.3

365A31-4706-00* M837 Ret 5350 05/01/03 0.0 0.0 5350.0 104.3365A31-4706-01 M849 Ret 5350 05/01/03 0.0 0.0 5350.0 104.3

Spherical thrust bearing 704A33633213 0512 Ret 4300 06/21/11 0.0 4046.8 8346.8 3101.10514 Ret 4300 06/21/11 0.0 4046.8 8346.8 3101.10507 Ret 4300 06/21/11 0.0 4046.8 8346.8 3101.10518 Ret 4300 06/21/11 0.0 4046.8 8346.8 3101.10513 Ret 4300 06/21/11 0.0 4046.8 8346.8 3101.1C249 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4

704A33633218 C346 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.412-11505P C353 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4

C358 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4Frequency adapter C399 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4

end-fitting C666 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4704A33633217 C754 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4

12-11506P C473 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4C476 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4C659 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.41571 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.41572 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4

Frequency adapter 704A33640090 1573 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4F4T410001 1587 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4

1593 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4

Page 25 of 49

N155WH N155WH

Airbus EC155B, Chapter 04-10-00, Airworthiness Limitations Section RT(P) Possible extention

Component Part Number Serial Number SLL Date of Install

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining M14952 Ret 2800 07/19/20 0.0 5245.7 8045.7 2800.0M14999 Ret 2800 07/19/20 0.0 5245.7 8045.7 2800.0M15001 Ret 2800 07/19/20 0.0 5245.7 8045.7 2800.0M14863 Ret 2800 07/19/20 0.0 5245.7 8045.7 2800.0

Unequipped rotor 365A31-2031-20 M15005 Ret 2800 07/19/20 0.0 5245.7 8045.7 2800.0blade pin M14886 Ret 2800 07/19/20 0.0 5245.7 8045.7 2800.0

M15004 Ret 2800 07/19/20 0.0 5245.7 8045.7 2800.0M14880 Ret 2800 07/19/20 0.0 5245.7 8045.7 2800.0M14679 Ret 2800 07/19/20 0.0 5245.7 8045.7 2800.0M14857 Ret 2800 07/19/20 0.0 5245.7 8045.7 2800.0MAP237 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3MAP245 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

Blade horn 365A31-4561-00* MAP247 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3365A31-4561-01 MAP248 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

MAP253 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3783 Ret 8000 05/01/03 0.0 0.0 8000.0 2754.3792 Ret 8000 05/01/03 0.0 0.0 8000.0 2754.3793 Ret 8000 05/01/03 0.0 0.0 8000.0 2754.3794 Ret 8000 05/01/03 0.0 0.0 8000.0 2754.3

Spherical thrust bearing 704A33-6332-24 797 Ret 8000 05/01/03 0.0 0.0 8000.0 2754.3Attach beam bolt 798 Ret 8000 05/01/03 0.0 0.0 8000.0 2754.3

800 Ret 8000 05/01/03 0.0 0.0 8000.0 -8695.0807 Ret 8000 05/01/03 0.0 0.0 8000.0 2754.3809 Ret 8000 05/01/03 0.0 0.0 8000.0 2754.3810 Ret 8000 05/01/03 0.0 0.0 8000.0 -8695.0

704A33-6332-42 755 Ret 8050 05/01/03 0.0 0.0 8050.0 2804.3758 Ret 8050 05/01/03 0.0 0.0 8050.0 2804.3

Page 26 of 49

N155WH N155WH768 Ret 8050 05/01/03 0.0 0.0 8050.0 2804.3

Frequency adapter 777 Ret 8050 05/01/03 0.0 0.0 8050.0 2804.3Attach beam bolt 782 Ret 8050 05/01/03 0.0 0.0 8050.0 2804.3

787 Ret 8050 05/01/03 0.0 0.0 8050.0 2804.3788 Ret 8050 05/01/03 0.0 0.0 8050.0 2804.3791 Ret 8050 05/01/03 0.0 0.0 8050.0 2804.3793 Ret 8050 05/01/03 0.0 0.0 8050.0 2804.3797 Ret 8050 05/01/03 0.0 0.0 8050.0 2804.3

Airbus EC155B, Chapter 04-10-00, Airworthiness Limitations Section RT(P) Possible extention

Component Part Number Serial Number SLL Date of Install

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining Scissors drive adapter 365A31-1171-00 S 971 Ret 5000 01/08/14 0.0 4986.8 9986.8 4741.1

Non-rotating swashplate 365A31-4531-01/02* M96 Ret 3800 05/01/03 0.0 0.0 3800.0 -1445.7Rotating swashplate 365A31-4541-01/02* M74 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

704A33633216 Ret 1000 Not installed704A33633259* 307 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

Pitch - Change rod body 704A33633268 323 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3331 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3333 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3337 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

704A33633220 A030 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4A038 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4A042 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4A058 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4

Pitch - Change A085 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4rod end-fitting 704A33633221 A361 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4

A364 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4A374 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4A376 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4A380 Ret 20000 03/01/13 0.0 4644.1 24644.1 19398.4

704A33633222 Ret 20000 Not installed704A33633219 Ret 20000 Not installed

365A31-1116-03* S 1493 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3Scissors lower link 365A31-1116-04 S 1535 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

S 1547 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

Page 27 of 49

N155WH N155WH365A31-1115-03* S 402 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

Scissors upper link 365A31-1115-04 S 411 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3SD 13179 Ret 20000 06/21/11 0.0 4046.8 24046.8 18801.1

Flared housing 365A31-4591-00,01*,02,03 FR032 Ret 6400 05/01/03 0.0 0.0 6400.0 1154.3Rotor mast bearing spacer 365A31-4527-00 Ret 1300 Not installed

365A31-4527-01* M86 Ret 13700 05/01/03 0.0 0.0 13700.0 8454.3365A31-4521-00,02,03,04,05 Ret 2470/25795 Not installed

Rotor shaft 365A31-4521-06,07* M92 Ret 7850 05/01/03 0.0 0.0 7850.0 2604.3Ret 30637 05/01/03 0 0 30637 13942

Airbus EC155B, Chapter 04-10-00, Airworthiness Limitations Section RT(P) Possible extention

Component Part Number Serial Number SLL Date of Install

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining Scissors upper link 365A31-1115-05 Ret 10900 Not installed

Mast and/or hub nut 365A31-2060-20 Ret 6200hr/31100tc Not installed365A31-2060-21 Ret 13800 hr/69400 TC Not installed

ATA 63Coupling shaft fwd 365A35-1010-24 M495 Ret 6500 05/01/03 0.0 0.0 6500.0 1254.3

flared housing 365A35-1010-25 DUC295 Ret 6500 05/01/03 0.0 0.0 6500.0 1254.3Coupling shaft 365A35-1011-28 MA12243 Ret 2900 04/02/09 0.0 2852.8 5752.8 507.1

aft flared housing MA16365 Ret 2900 04/02/09 0.0 2852.8 5752.8 507.1Coupling shaft 365A35-1067-00/01* S362 Ret 56400 05/01/03 0 0 56400 39705

S365 Ret 56400 05/01/03 0 0 56400 39705365A35-1064-00/01 Ret 56400 Not installed

Eng-MGB coupling flange 365A35-1073-00/01* MA01232 Ret 56400 05/01/03 0 0 56400 39705MA01320 Ret 56400 05/01/03 0 0 56400 39705

MGB input flange 365A32-5427-21/22 Ret 49400 49400 32705Ret 49400 49400 32705

Servo-control 360A32-1163-03 Ret 20000 20000.0 14754.3attachment fitting 360A32-1163-04 Ret 20000 20000.0 14754.3

Ret 20000 20000.0 14754.3Housing 365A32-2046-15 Ret 10000 10000.0 4754.3

Ret 29300 29300 12605Planetary gear carrier 360A32-3036-20/21/22 Ret 25900 25900 9205

Page 28 of 49

N155WH N155WHT/R D/S bevel gear wheel 365A32-1058-22 Ret 12500 12500.0 7254.3

Main bevel gear wheel 360A32-3256-25/26 Ret 20000 20000.0 14754.3T/R D/S bevel pinion 360A32-1029-26/29 Ret 2800 2800.0 -2445.7

Not installedFirst reduction pinion 365A32-4129-03 Ret 20000 20000.0 14754.3

Ret 20000 20000.0 14754.3Double pinion 365A32-7100-20 Ret 20000 20000.0 14754.3

Ret 20000 20000.0 14754.3Fixed ring gear 365A32-7035-21 Ret 20000 20000.0 14754.3

Ret 64900 64900 48205Sun gear vertical shaft 365A32-7021-23 Ret 20000 20000.0 14754.3

365A32-7021-24 Ret 7200

Airbus EC155B, Chapter 04-10-00, Airworthiness Limitations Section RT(P) Possible extention

Component Part Number Serial Number SLL Date of Install

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining Freewheel shaft 365A32-5424-01 Ret 101600 101600 84905

Ret 101600 101600 84905Freewheel driven 365A32-5422-20 Ret 18300 18300 1605

head shaft Ret 18300 18300 1605365A32-7023-21 Ret 5000 5000.0 -245.7

Ret 5000 5000.0 -245.7Plant gear Assm# 365A32-9011-00 Ret 5000 5000.0 -245.7

Assm# 365A32-9013-00 Ret 5000 5000.0 -245.7Ret 5000 5000.0 -245.7

First reduction 365A32-7108-00 Ret 20000 20000.0 14754.3gear housing Ret 20000 20000.0 14754.3

365A32-7110-00 Ret 20000 20000.0 14754.3Half-gimbal joint Ret 20000 20000.0 14754.3

365A32-7112-00 Ret 20000 20000.0 14754.3Ret 20000 20000.0 14754.3

Upper cover 365A32-7102-00/7824-00 Ret 20000 20000.0 14754.3Gimbal ring /-00 365A32-7113-20 Ret 20000 20000.0 14754.3

Assm 365A7114-00/-01 /-01 365A32-7113-21 Ret 20000 20000.0 14754.3MGB bottom 366A32-1060-26 Ret 526000 526000 509305

Page 29 of 49

N155WH N155WHAssm 366A32-1062-06 366A32-1060-29 Ret 17000

366A32-1062-09/10 366A32-1060-30 Ret 17000Fixed flange (T/R drive) 360A32-2034-20/21/22/23 Ret 2800 2800.0 -2445.7

T/R D/S flange 360A32-1035-20/21 Ret 20000 20000.0 14754.3Accessory drive pinion 365A32-4059-20 Ret 10600

MGB fwd suspension bar 365A38-4520-01 FR150 Ret 5560 04/01/03 0.0 0.0 5560.0 314.3FR155 Ret 5560 04/01/03 0.0 0.0 5560.0 314.3

MGB aft RH suspension bar 365A38-4521-02 FR109 Ret 8600 04/01/03 0.0 0.0 8600.0 3354.3MGB aft LH suspension bar 365A38-4521-03 FR103 Ret 8600 04/01/03 0.0 0.0 8600.0 3354.3Suspension bar/fitting bolt 704A33-633-233 139 Ret 20000 04/01/03 0.0 0.0 20000.0 14754.3

141 Ret 20000 04/01/03 0.0 0.0 20000.0 14754.3

Airbus EC155B, Chapter 04-10-00, Airworthiness Limitations Section RT(P) Possible extention

Component Part Number Serial Number SLL Date of Install

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining ATA 64

365A12-0060-01 Ret 1500 Not installed365A12-0070-00 Ret 5000 Not installed

14508 Ret 5000 09/28/06 0.0 1487.0 6487.0 1241.314494 Ret 5000 09/28/06 0.0 1487.0 6487.0 1241.314483 Ret 5000 09/28/06 0.0 1487.0 6487.0 1241.3

Tail rotor blade 14535 Ret 5000 09/28/06 0.0 1487.0 6487.0 1241.314531 Ret 5000 09/28/06 0.0 1487.0 6487.0 1241.3

365A12-0070-01 14518 Ret 5000 09/28/06 0.0 1487.0 6487.0 1241.314569 Ret 5000 09/28/06 0.0 1487.0 6487.0 1241.314566 Ret 5000 09/28/06 0.0 1487.0 6487.0 1241.314540 Ret 5000 09/28/06 0.0 1487.0 6487.0 1241.314597 Ret 5000 09/28/06 0.0 1487.0 6487.0 1241.3

T/R hub 365A33-3511-00/01/02*/03 CUR00105 Ret 13000 05/01/03 0.0 0.0 13000.0 7754.3Plate 365A33-3522-20 S136 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

Splined flange 365A33-3523-00 MA01118 Ret 16000 05/01/03 0.0 0.0 16000.0 10754.31468 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31470 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

Page 30 of 49

N155WH N155WH1471 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31477 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

Torsion bar bolt 365A33-3525-20 1479 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31484 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31492 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31500 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31504 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31506 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

Battery 40208-2 MO0192 7/19/2020 0 5245.7

Airbus EC155B, Chapter 04-10-00, Airworthiness Limitations Section RT(P) Possible extention

Component Part Number Serial Number SLL Date of Install

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining 1409 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31412 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31433 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31449 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

Blade attaching bolt 365A33-3535-20 1454 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31480 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31481 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31487 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31501 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.31509 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3

ATA 65Flexible coupling 365A34-1033-01 M9966 Ret 20000 01/06/14 0.0 4986.8 24986.8 19741.1

M5646 Ret 20000 05/01/03 0.0 0.0 20000.0 14754.3Forward shaft element 365A34-4510-00 FR070 Ret 6300 06/01/03 0.0 0.0 6300.0 1054.3Center shaft element 365A34-4520-00 FR0309 Ret 6300 01/06/14 0.0 4986.8 11286.8 6041.1

Page 31 of 49

N155WH N155WHAft shaft element 365A34-4530-00 FR0251 Ret 10000 07/11/13 0.0 4829.7 14829.7 9584.0

Input Pinion 365A33-6123-22/24* M1118 Ret 11700 08/01/08 0.0 4644.1 16344.1 11098.4Bevel gear wheel 365A33-6104-00/01/02*/03/04/05 M958 Ret 20000 08/01/08 0.0 4644.1 24644.1 19398.4

Sliding flange 365A33-6197-21/22* PRD305 Ret 8400 08/01/08 0.0 4644.1 13044.1 7798.4Input flange 365A33-6196-21/22/23/24* FR203 Ret 11700 08/01/08 0.0 4644.1 16344.1 11098.4Control shaft 365A33-6214-20*/21/22/23 S128 Ret 20000 08/01/08 0.0 4644.1 24644.1 19398.4Control rod 365A33-6145-21 PRD373 Ret 20000 08/01/08 0.0 4644.1 24644.1 19398.4

Input housing 365A33-6128-00/01* S284 Ret 20000 08/01/08 0.0 4644.1 24644.1 19398.4Housing 365A33-6137-02/03* 57 Ret 20000 08/01/08 0.0 4644.1 24644.1 19398.4

Flared coupling tube 365A33-6141-20/21*/22/23 SE163 Ret 20000 04/01/03 0.0 0.0 20000.0 14754.3ATA 67

Tail rotor servo-control 704A44831153 (SC7291) 105 Ret 9000 03/09/20 3749.7 5233.2 10483.5 5237.8704A44831149 (SC8037) Ret 8000 Not installed

Main rotor servo-control 704A44831155 (SC8037-1) 110 Ret 8000 08/12/09 2996.0 3085.4 8089.4 2843.777 Ret 8000 06/01/09 2942.0 2996.5 8054.5 2808.873 Ret 8000 06/01/09 2942.0 2996.5 8054.5 2808.8

Airbus EC155B, Chapter 04-10-00, Airworthiness Limitations Section RT(P) Possible extention

Component Part Number Serial Number SLL Date of Install

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining 704A33632062 (1211350P) A226 Ret 3400 01/28/10 0.0 3400.6 6800.6 1554.9

A419 Ret 3400 01/28/10 0.0 3400.6 6800.6 1554.9Servo-control end-fitting A427 Ret 3400 01/28/10 0.0 3400.6 6800.6 1554.9

7041A33632061 (1211351P) A454 Ret 3400 01/28/10 0.0 3400.6 6800.6 1554.9A512 Ret 3400 01/28/10 0.0 3400.6 6800.6 1554.9A256 Ret 3400 01/28/10 0.0 3400.6 6800.6 1554.9

Airbus EC155, Chapter 05-10-00, Component Subject to TBO, OTL, OC

Component Part Number Serial Number Limit Date of Install/Man

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining

Chapter 24 Electrical Power10-kVA alternator ALT3577 (704A46220036) 1099 TBO 3000 07/14/14 0.0 5127.9 8127.9 2882.2

Main Battery 33490409000 (704A46130049) OC N/APage 32 of 49

N155WH N155WHChapter 25 Equipment / FurnishingsHarness-all All MP/N OC N/A

Cylinder (floats) 216122-1 (704A42693013) 8107 OTL 15 Y TSM 03/01/10 0.0 4784.9 02/25/25 1553216122-1 (704A42693013) 222 OTL 15 Y TSM 02/01/13 0.0 4692.4 01/29/28 2621216064-0 (NR101500123) 36 OTL 15 Y TSM 09/01/03 0.0 5.4 08/28/18 -820

Floats 216166-0 (NR101500125) 31 OTL 15 Y TSM 06/01/03 0.0 5.4 05/28/18 -912216167-0 (NR101500124) 33 OTL 15 Y TSM 09/01/03 0.0 5.4 08/28/18 -820216280-0 (NR101500126) 30 OTL 15 Y TSM 06/01/03 0.0 5.4 05/28/18 -912

Electric hoist 90m 76378 260 (704A41815065) TBO 10 Y Not installed

Component Part Number Serial Number Limit Date of Install/Man

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining ELT - Battery pack S1820516-99 OTL ED Due retire 11/2023

Kannad 406-AF &-AP 1 OPH

Component Part Number Serial Number Limit Date of Install/Man

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining

Chapter 26 Fire ProtectionEngine fire ext. - Squib 863080-00 (704A38710040) 3728 OTL 5 Y TSI 06/05/13 0.0 4784.9 06/04/18 -905

LH 7 Y TSM 07/30/12 0.0 4784.9 07/29/19 -485863085-00 (704A38710041) 4175 OTL 5 Y TSI 06/05/13 0.0 4784.9 06/04/18 -905

7 Y TSM 05/30/13 0.0 4784.9 05/28/20 -181Engine fire ext. - Squib 863080-00 (704A38710040) 3727 OTL 5 Y TSI 06/05/13 0.0 4784.9 06/04/18 -905

RH 7 Y TSM 07/30/12 0.0 4784.9 07/29/19 -485863085-00 (704A38710041) 4174 OTL 5 Y TSI 06/05/13 0.0 4784.9 06/04/18 -905

7 Y TSM 05/30/13 0.0 4784.9 05/28/20 -181Engine fire ext. - Cylinder 10230-1 (704A42820049) UR73527 OC 06/01/11 0.0 5233.2

UR73486 05/11/11 0.0 5226.9Engine fire ext. - Cylinder 1023000 (704A42820043 OC Not installed

Hand fire ext - Cylinder 12085-01 (S262A10T1001) 1254772 OTL 10 Y TSM Nov-12 0.0 4599.0 11/17/22 722H1-10AIR (704A32810008)* 1357109 10 Y TSM Oct-13 0.0 5081.1 10/20/23 1059

Hand fire extinguisher 74-00 (800G6799980) OC Not installedBaggage Comp. - Squib 863080.00 (704A38710040) 4226 OTL 5 Y TSI 06/05/13 0.0 4784.9 06/04/18 -905

7 Y TSM 04/30/13 0.0 4784.9 04/28/20 -211863085-00 (704A38710041) 4173 OTL 5 Y TSI 06/05/13 0.0 4784.9 06/04/18 -905

7 Y TSM 05/30/13 0.0 4784.9 05/28/20 -181Page 33 of 49

N155WH N155WHBaggage Comp. - Fire Ext. 864250-00 (704A42820042)

Cylinder 864250-01 (704A42820048)* UP628UG OC 07/01/04 0.0 5175.7

Component Part Number Serial Number Limit Date of Install/Man

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining

Chapter 28 FuelFuel tank All MP/N OC

Booster pump C11BC0080 TBO 1800 FH Not installedC11BC0081 (704A44510024)

Booster pump P94C16-606 (704A44510022) 21278 TBO 2000 FH 05/29/14 0.0 5115.8 7115.8 1870.122376 TBO 2000 FH 05/29/14 0.0 5115.8 7115.8 1870.1

C03608 TBO 2000 FH 10/17/11 0.0 4212.6 6212.6 966.9A61415 TBO 2000 FH 07/26/12 0.0 4424.8 6424.8 1179.1

Chapter 29 Hydraulic PowerHydraulic pump C24999010 (704A44320032)* H0129 TBO 3600 FH 10/09/10 0.0 3686.8 7286.8 2041.1

C24999010-1 (704A44320038) H0210 TBO 3600 FH 05/26/08 0.0 2324.2 5924.2 678.5Standby electric pump A5029190 (704A44310025) 01269494 OC 03/15/05 3077.3 618.7

Chapter 31 Ind./Recording SystemsClock CH97-10 - Battery CMM 31.21.97 OTL 2 Y

Chapter 32 Landing GearMain landing gear All MP/N B246 LH OC 02/01/05 403.0 570.9

B214 RH OC 02/01/05 414.0 570.9Nose landing gear All MP/N B211 OC 02/01/03 0.0 0.0

Anti-sinking shoes - 355090001 TBO 8 Y TSM Not installedMechanical actuator 704A41450036

Chapter 33 LightsSearchlight Gimbal arm ALUM 019058 / 019058 21 / 021715 OTL 7 Y Not installedChapter 34 Navigation

Radar 1400 & 1600 antenna 4000504-0301* (N6707152800) T2241 TBO 3000 05/07/15 0.0 5226.9 8226.9 2981.2Slaving unit 4000504-0303 (N6707154000) 3 Y TSI 05/07/15 0.0 5226.9 05/06/18 -934Chapter 62 Main Rotor Head

Pitch-change rod body 704A33633216 OTL 2 Y Not installedSwashplate bearing 121620 (704A33651157) OTL

Y51BB10843S2M74 (704A33651158*) NR10624 OTL 5000 FH 01/08/14 0.0 4986.8 9986.8 4741.1Mast bearing Y45CB10700S7M74 / 704A33651119 NR8279 OTL 2500 FH 06/29/13 0.0 4823.5 7323.5 2077.8

MRH All MP/N M 167 OC 05/01/03 0.0 0.0Page 34 of 49

N155WH N155WHChapter 63 Main Rotor Drive

Engine-MGB coupling All MP/N OCMGB 365A32-9001-00 TBO 1800 FH 1800.0 -3445.7

24 Y 12/25/23 -35400MGB supports & attachments - All MP/N OC

Suspension assy

Chapter 64 Tail RotorTRH 365A33-3501-03 OC

365A33-3502-01* 05/01/03 0.0 0.0Chapter 65 Tail Rotor Drive

Tail rotor drive shaft All MP/N OCBearing 593364 (704A33651180) OTL 6000 FH Not installed

83A904D-1C3 (704A33651142) 10 Y83A904DC3 (704A33651142)

TGB 365A33-6005-06,-08*,-09 M849 TBO 2400 FH 02/28/13 0.0 4644.1 7044.1 1798.424 Y 02/28/13 0.0 4644.1 02/25/25 1553

Chapter 67 Main Rotor ControlsM/R Ball control 82CF9242 (704A34130197) 2 ea. OTL 2300 FH Not installed

82CF9243 (704A34130198) 256 OTL 2300 FH 03/01/13 0.0 4644.1 6944.1 1698.4M/R Ball control 82CF-10307*(704A34130228) 106 OTL 6000 FH 03/01/13 0.0 4644.1 10644.1 5398.4

82CF-10308 (704A34130229) 102 OTL 6000 FH 03/01/13 0.0 4644.1 10644.1 5398.4

Component Part Number Serial Number Limit Date of Install/Man

Comp TT /TSO TSI

Installed @ ACTT/RINS

ACTT/RINS/ CYC Due

Time/RINS/CYC

Remaining

T/R Ball control 82CF9240 (704A34130196) OTL 2300 FH Not installed82CF9241 (704A34130195)

T/R Ball control 82CF-10305 (704A34130226) 38 OTL 20000 FH 03/01/13 0.0 4644.1 24644.1 19398.482CF-10306 (704A34130227) 47 20000 FH 03/01/13 0.0 4644.1 24644.1 19398.4

Tail rotor servo-control SC7291 (704A44831153) 105 TBO 3000 FH 03/09/20 712.7 5233.2 8233.2 2987.520 Y TSM 09/29/11 0.0 5233.2 09/24/31 3955

Main rotor servo-control SC8037 (704A44831149) TBO 1000 FH Not20 Y TSM installed

Main rotor servo-control SC8037-1 (704A44831155) 110 TBO 3000 FH 08/12/09 0.0 3085.4 6085.4 839.720 Y TSM 04/01/03 0.0 0.0 03/27/23 852

Page 35 of 49

N155WH N155WH77 TBO 3000 FH 06/01/09 0.0 2996.5 5996.5 750.8

20 Y TSM 12/01/02 0.0 0.0 11/26/22 73173 TBO 3000 FH 06/01/09 0.0 2996.5 5996.5 750.8

20 Y TSM 12/01/02 0.0 0.0 11/26/22 731Chapter 71 Power Plant

Engine bay fan VCT1518D (704A43691028) 00386 TBO 1200 FH 03/08/13 0.0 4664.1 5864.1 618.4Technofan 00366 TBO 1200 FH 03/08/13 0.0 4664.1 5864.1 618.4

Chapter 79 Oil Cooling SystemEngine/MGB 34774 (704A33220037) OC

oil cooler 53139 (704A33220038)Chapter 80 Engine Starting

Starter generator 524-031 (704A46101011) 3615 TBO 3000 FH 08/16/12 0.0 4424.8 7424.8 2179.14451 TBO 3000 FH 08/16/12 0.0 4424.8 7424.8 2179.1

Chapter 93 Monitoring System

Page 36 of 49

N155WH N155WH

Manual

Chap 4 Rev 00 Chap 5 Rev 00

Avg Flt Time

1.0

Proj'd date due

08/14/5008/14/5004/18/6104/18/6101/12/2401/12/24

04/18/61

12/01/3312/01/3312/01/3312/01/3312/01/33

03/09/2103/09/2103/09/2103/09/2103/09/21

Page 37 of 49

N155WH N155WH

Proj'd date due

03/09/2103/09/2103/09/2103/09/2103/09/2105/23/2905/23/2905/23/2905/23/2905/23/2901/04/7401/04/7401/04/7401/04/7401/04/7401/04/7401/04/7401/04/7401/04/7401/04/7401/04/7401/04/7401/04/7401/04/7401/04/74

Page 38 of 49

N155WH N155WH

Proj'd date due

07/26/2807/26/2807/26/2807/26/2807/26/2807/26/2807/26/2807/26/2807/26/2807/26/2804/18/6104/18/6104/18/6104/18/6104/18/6106/10/2806/10/2806/10/2806/10/2806/10/2806/10/2802/04/9706/10/2806/10/2802/04/9707/30/2807/30/28

Page 39 of 49

N155WH N155WH07/30/2807/30/2807/30/2807/30/2807/30/2807/30/2807/30/2807/30/28

Proj'd date due

11/18/3312/10/1604/18/61

04/18/6104/18/6104/18/6104/18/6104/18/6101/04/7401/04/7401/04/7401/04/7401/04/7401/04/7401/04/7401/04/7401/04/7401/04/74

04/18/6104/18/6104/18/61

Page 40 of 49

N155WH N155WH04/18/6104/18/6105/17/7201/23/24

01/18/44

01/12/28N/A

Proj'd date due

05/02/2405/02/2404/16/2204/16/22

N/AN/A

N/AN/AN/AN/A

04/18/6104/18/6104/18/6112/01/33

N/AN/A

Page 41 of 49

N155WH N155WH10/05/4004/18/6103/16/14

04/18/6104/18/6104/18/6104/18/6104/18/61

N/A04/18/61

Proj'd date due

N/AN/AN/AN/A

03/24/2003/24/2003/24/2003/24/2003/24/2004/18/6104/18/6104/18/6104/18/6104/18/6104/18/6104/18/6104/18/6104/18/61

N/A

Page 42 of 49

N155WH N155WH

03/16/1404/18/61

10/05/2110/05/2101/31/3001/31/3004/18/6104/18/61

Proj'd date due

04/19/2404/19/2404/19/2404/19/2404/19/2404/19/2404/19/2404/19/2404/19/2404/19/2402/17/4204/18/6105/06/5004/18/6104/18/61

Page 43 of 49

N155WH N155WH04/18/6104/18/6104/18/6104/18/6104/18/6104/18/6104/18/6104/18/61

Proj'd date due

04/18/6104/18/6104/18/6104/18/6104/18/6104/18/6104/18/6104/18/6104/18/6104/18/61

12/13/7404/18/6110/15/2306/10/37

Page 44 of 49

N155WH N155WH02/21/4704/15/5101/04/7404/02/4204/15/5101/04/7401/04/7401/04/7401/04/7404/18/61 Ck mod.

03/29/35

09/07/2808/03/2808/03/28

Proj'd date due

02/26/2502/26/2502/26/2502/26/2502/26/2502/26/25

Proj'd date due Margin

10/16/28 300

Page 45 of 49

N155WH N155WH

02/25/25 0

01/29/28 0

08/28/18 180

05/28/18 180

08/28/18 180

05/28/18 180180

Proj'd date due Margin

0

0

Proj'd date due Margin

06/04/18 0

07/29/19 0

06/04/18 0

05/28/20 0

06/04/18 0

07/29/19 0

06/04/18 0

05/28/20 0

11/17/22 0

10/20/23

06/04/18 0

04/28/20 0

06/04/18 0

05/28/20 0

Page 46 of 49

N155WH N155WH

Proj'd date due Margin

01/08/26 0

01/08/26 0

07/19/23 0

02/17/24 0

06/28/26 200 FH

10/04/22 200 FH

73 D

0

180 D

01/23/29 300 FH

05/06/18 109 D

73 D

0

11/18/33 0

08/03/26 0

Page 47 of 49

N155WH N155WH

06/20/11 0

12/25/23 0

0

180D

10/28/25 240 FH

02/25/25 180 D

07/20/2509/06/35 300 FH

09/06/35 300 FH

Proj'd date due Margin

01/04/74 300 FH

01/04/74 300 FH

01/29/29 300 FH

09/24/31 180 D

100 FH

180 D

03/14/23 300 FH

03/27/23 180 D

Page 48 of 49

N155WH N155WH12/15/22 300 FH

11/26/22 180 D

12/15/22 300 FH

11/26/22 180 D

08/05/22 120

08/05/22 120

11/13/26 300 FH

11/13/26 300 FH

Page 49 of 49