chapter 77 engine indicating - canaero - home 77 . engine . indicating . uncontrolled copy...

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Illustrated Parts Catalog FBA-2C1, FBA-2C2 FBA-2C3, FBA-2C4

77-00 July 14, 2011

CHAPTER 77

ENGINE INDICATING

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77-00 July 14, 2011

List of Effective Pages

Chapter / Section

Page No. Date Chapter /

Section Page No. Date

77-00 1 Jul 14, 2011 2 Jul 14, 2011

77-05 1 Jul 14, 2011 2 Jul 14, 2011 3 Jul 14, 2011 4 Jul 14, 2011

77-13 1 Jul 14, 2011 2 Jul 14, 2011

77-14 1 Jul 14, 2011 2 Jul 14, 2011

77-40 1 Jul 14, 2011 2 Jul 14, 2011 3 Jul 14, 2011 4 Jul 14, 2011 5 Jul 14, 2011 6 Jul 14, 2011 7 Jul 14, 2011 8 Jul 14, 2011 9 Jul 14, 2011 10 Jul 14, 2011 11 Jul 14, 2011 12 Jul 14, 2011

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77-05 Page 1 July 14, 2011

GROUP Engine Indicating MAJOR ASSEMBLY Engine Instrument Cluster (2C1/2C2)

Figure And Index Number PART No. DESCRIPTION

Effect. Vendor Ident.

UnitsPer

Assy

1- -1 -2 -3 -4 -5 -6 -7 -8 -9

-10 -11

-12

-13

No Number 7740-00478 MS3106R-12S-3S MS3320-5 MS24524-23 1U645-001 205839-3 86255 MS24482-1 242PC150G MS28034-1 No Number 342-014 AGC2 No Number 342-014 AGC2 22-370-70

Engine Instrument Cluster & Transducers Fuel Sender Cannon Connector Circuit Breaker DPDT Switch Engine Instrument Cluster Circular Connector EGT Probe CHT Probe Oil Pressure Sender Oil Temperature Sender Fuse Assembly Fuse Holder Fuse, 2 Ampere Fuse Assembly Fuse Holder Fuse, 2 Ampere Shunt, 50mV @ 70 Amps

ROG

TIN

SIG AMP ALC

HON

LTF

LTF

SIG

2 1 1 1 1 1 1 1 1 1

1 1

1 1 1

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9

11,12,13

2,10

8

76

4

3

1 1

To apply parking brake depress brake pedals and pull parking brake handle To release parking brake depress brake pedals and push parking brake handle

Parking Brake Handle

OFF OFF

VOLTAGE

OVER UNDER

MASTERON

ALT.ENABLE

BLINDENC.

HSIDME AUTOPILOT

A PALERT

XPNDR ADF AVNFAN

NO SMOKING FIRE EXTINGUISHER FASTEN SEATBELTS LOCATED UNDER PILOT SEAT

MANPRESS

FLAPIND

INSTR.CLUSTER

TURNCO-OR

PITOTHEAT

FLAPMOTOR

PULSECNTRL

LANDLTS

TAXILTS

INTERLTS

NAV 2GPS 2

COMM2 HOBBSMETER

12VdcAUX.

NAV.LTS

STROBELTS

NAV 1GPS 1

COMM1

TACH

PULSELT

ENGMONITOR

FUELFLOW

PANELLTS

AUDIOINT

ALTFLD

GEARCNTRL

GEARADV.

AUX.FUEL

STALLWARN

GEARMOTOR

VOLT.REG.

IGNSW

The markings and placards installed in this airplane contain operating limitations which must be complied with when

operating this airplane in the Normal Category. Other operatinglimitations which must be complied with when operating this

airplane in this category are contained in the Airplane Flight Manual.

MANEUVER SPEED = 114 KIAS

Normal Category: No acrobatic maneuversincluding spins, approved. Flight into knownicing conditions prohibited. This airplane iscertified for the following flight operations:

DAY-NIGHT-VFR-IFR(With required equipment)

STALLWARNING

OFF

20°

30°

OFFOFF OFF

10°

0°

OFF OFF OFFOFFOFF

UP

DOWN

FLAPS

LAND.LTS

TAXI LIGHT

AVIONICSMASTER

NAV.LTS

AUX.FUEL

INTERIORLIGHT

PITOTHEAT

STROBELIGHT

BACKUPPOWER

XPZONE1 ZONE2 ZONE3

DIMMER CONTROLS

DO NOT RELY ON FUEL FLOW INSTRUMENTTO DETERMINE FUEL LEVEL IN TANKS

13.75 V.D.C.4 AMP CONT.5 AMP MAX.

5

Figure 1 (Sheet 1)

Engine Instrument Cluster & Transducers (2C1/2C2)

77-05 Page 2 July 14, 2011

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1

9

12

10

11

8

6

4

3

5

7

1

13

2

Figure 1 (Sheet 2)

Engine Instrument Cluster & Transducers (2C1/2C2)

77-05 Page 3 July 14, 2011

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77-05 Page 4 July 14, 2011

INTENTIONALLY LEFT BLANK

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77-13 Page 1 July 14, 2011

GROUP Engine Indicating MAJOR ASSEMBLY Manifold Pressure (2C1/2C2)



Units Per

Assy

1- -1 -2 -3 -4 -5 -6 -7 -8

No Number X113-4 AN924-4D AN960-816 X113-3 AN815-4D X113-2 M-1 MS3320-1

Manifold Pressure System Tube, Gauge to Fire Wall Bulk Head Fitting Washer Hose, Fire Wall to Engine Baffle Union Tube, Engine Baffle to Engine Fitting Manifold Pressure Gauge Circuit Breaker 1 Ampere

1 1 2 1 1 1 1 1

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77-13 Page 2 July 14, 2011

7

8

MASTERON

ALT.ENABLE

VOLTAGE

OFF

OVER

OFF

UNDER



MANPRESS

PULSECNTRL


DMEADF HSIAUTOPILOT

A PALERT

NAV 1GPS 1

COMM2 NAV 2GPS 2

HOBBSMETER

12VdcAUX.

XPNDR

COMM1

INSTR.CLUSTER

GEARMOTOR

STALLWARN

FLAPIND

FLAPMOTOR

ALTFLD

GEARCNTRL

GEARADV.

TURNCO-OR

TAXILTS

STROBELTS

LANDLTS

INTERLTS

NAV.LTS

AUX.FUEL

PITOTHEAT

AVNFAN

BLINDENC.

AUDIOINT

VOLT.REG.

IGNSW

TACH FUELFLOW

PULSELT

PANELLTS

ENGMONITOR

ZONE1 ZONE2 ZONE3DIMMER CONTROLSAUX.

FUEL




STALLWARNING




OFF

BACKUPPOWER

OFF

AVIONICSMASTER

OFF

TAXI LIGHT

OFFOFF

STROBELIGHT

LAND.LTS

OFF

NAV.LTS

UP

DOWN

20°

30°

10°

0°

FLAPS

OFF

PITOTHEAT

OFF

INTERIORLIGHT

OFF



XP

7

8

6

5

42

33

1

Figure 1 Manifold Pressure System (2C1/2C2)

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77-14 Page 1 July 14, 2011

GROUP Engine Indicating MAJOR ASSEMBLY Electric Tachometer (2C1/2C2)



Units Per

Assy

1- -1 -2

No Number MS3320-1 R-1-6

Electric Tachometer Circuit Circuit Breaker 1 Ampere Electric Tachometer

EIT

1 1

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77-14 Page 2 July 14, 2011

2

1

21

MASTERON

ALT.ENABLE

VOLTAGE

OFF

OVER

OFF

UNDER



MANPRESS

PULSECNTRL


DMEADF HSIAUTOPILOT

A PALERT

NAV 1GPS 1

COMM2 NAV 2GPS 2

HOBBSMETER

12VdcAUX.

XPNDR

COMM1

INSTR.CLUSTER

GEARMOTOR

STALLWARN

FLAPIND

FLAPMOTOR

ALTFLD

GEARCNTRL

GEARADV.

TURNCO-OR

TAXILTS

STROBELTS

LANDLTS

INTERLTS

NAV.LTS

AUX.FUEL

PITOTHEAT

AVNFAN

BLINDENC.

AUDIOINT

VOLT.REG.

IGNSW

TACH FUELFLOW

PULSELT

PANELLTS

ENGMONITOR

ZONE1 ZONE2 ZONE3DIMMER CONTROLSAUX.

FUEL




STALLWARNING




OFF

BACKUPPOWER

OFF

AVIONICSMASTER

OFF

TAXI LIGHT

OFFOFF

STROBELIGHT

LAND.LTS

OFF

NAV.LTS

UP

DOWN

20°

30°

10°

0°

FLAPS

OFF

PITOTHEAT

OFF

INTERIORLIGHT

OFF



XP

Figure 1

Electric Tachometer Circuit (2C1/2C2)

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77-40 Page 1 July 14, 2011

GROUP Engine Indicating MAJOR ASSEMBLY Engine Integrated Instrument System

(2C3 & 2C4)



Units Per

Assy

1- -1 -2

No Number MVP 50P-6 MS35214-31

Engine Monitor Display Head MVP 50-P Display Head Screws

1 4

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77-40 Page 2 July 14, 2011

2

1

Figure 1 Engine Monitor Display Head Installation (2C3/2C4)

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77-40 Page 3 July 14, 2011


(2C3 & 2C4)



Units Per

Assy

2- -1 -2 -3 -4 -5 -6

-7 -8

No Number PT-30ALT PT-05DIFF PT-30ABS RFLM-4-24 EDC-33P 3060-1 MS35206-228 MS24693S50

EDC Panel Assembly Altitude Pressure Transducer Differential Pressure Transducer Absolute Pressure Transducer Resistive Level Fuel Module Electronic Data Converter 1/4 x 1/8 Straight Reduction Connector Screw Screw

1 1 1 1 1 4

8 2

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4 PLACES6

8 PLACES

2 PLACES

5

4

1

2

3

7

8

Figure 2

EDC Panel Assembly (2C3/2C4) 77-40 Page 4 July 14, 2011

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77-40 Page 5 July 14, 2011

FBA 2C3 Models GROUP Engine Indicating MAJOR ASSEMBLY Engine Integrated Instrument System

(2C3 & 2C4)



Units Per

Assy

3- -1 -2 -3 -4 -5 -6 -7 -8 -9

No Number AN924-4 AN960-716L AE3660000E0234 AN816-4D AN837-4 X2095 AN910-1D 1860-1 05-00659

Manifold Pressure System Nut Washer Flex Line Fitting Bulkhead Fitting Rigid Line Coupling Fitting Hose

1 2 1 2 1 1 1 1

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77-40 Page 6 July 14, 2011

5, 264

78

9

FIREWALL

Manifold Pressure System

EDC Panel to Firewall

Manifold Pressure System Firewall To Engine

1, 2

3

4

Figure 3 Manifold Pressure System (2C3/2C4)

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77-40 Page 7 July 14, 2011


(2C3 & 2C4)



Units Per

Assy

4- -1 -2 -3 -4 -5 -6 -7

No Number AN924-4 P-110 Hose Clamp, Type K P-100 3/8-24, Type K FT-90 P-120 PT-100GA P-128 3/8x28, Type K

Engine Sensor Locations Fuel Sender EGT Probe CHT Probe Fuel Flow Transducer Oil Temp Probe Oil Pressure Transducer OAT Probe

2 6 6 1 1 1 1

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7

77-40 Page 8 July 14, 2011

1

1

6

234

5

Figure 4 Engine Sensor Locations (2C3/2C4)

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77-40 Page 9 July 14, 2011


(2C3 & 2C4)



Units Per

Assy

5- -1 -2 -3 -4 -5 -6

No Number MS35206-228 PT-05Diff 4060-1 X2093 MS21047L06 QS200M-60H

Vacuum Pressure Transducer Screw Transducer Fitting Mounting Bracket Nutplate Hose Clamp

2 1 2 1 2 1

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77-40 Page 10 July 14, 2011

Attitude Gyro(1U149-010-5)

2

1

1

5

5

6 43

Figure 5 Vacuum Pressure Transducer Installation

(2C3/2C4)

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77-40 Page 11 July 14, 2011


(2C3 & 2C4)

Figure

r PART No. DESCRIPTION

Effect. Vendor Units And IndexNumbe

Ident. Per Assy

6- -1

P

YZQE

Engine Monitor Switch Panel

itch t

-2 -3 -4 -5

No NumberAL-1R X2159 AV-17CL933 7201S

Check Engine Light Placard Voice Alarm Sw Attenuated Post Ligh Switch

1 1 1 1 1

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77-40 Page 12 July 14, 2011

2 3

1

45

(Flight Panel)

Figure 6 Engine Monitor Switch Panel

(2C3/2C4)

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