thrush 510 garret flight manual

Thrush Aircraft Inc Model S2R-G10 TABLE of Albany, GA

AIRPLANE FLIGHT MANUAL CONTENTS

FAA APPROVED: March 25, 2010 Rev. 2 Page i

TABLE of CONTENTS Table of Contents ................................................................................................................................ i Log of Pages....................................................................................................................................... ii Log of Revisions .................................................................................................................................iii

SECTION 1 LIMITATIONS Powerplant .......................................................................................................................................1-1 Instrument Markings ........................................................................................................................1-2 Airspeed Limitations ........................................................................................................................1-3 Altitude Limitations...........................................................................................................................1-3 Flight Load Factors ..........................................................................................................................1-3 Weight and Center of Gravity...........................................................................................................1-4 Maneuvers .......................................................................................................................................1-4 Types of Operation ..........................................................................................................................1-4 Ground Operation ............................................................................................................................1-4 Placards...........................................................................................................................................1-4

SECTION 2 NORMAL PROCEDURES Definitions ........................................................................................................................................2-1 Visual Inspection..............................................................................................................................2-1 Before Starting Engine.....................................................................................................................2-5 Starting Engine ................................................................................................................................2-5 Dry Motoring Run.............................................................................................................................2-7 Pre-Taxi ...........................................................................................................................................2-8 Taxi ..................................................................................................................................................2-8 Before Takeoff .................................................................................................................................2-8 Takeoff .............................................................................................................................................2-9 Climb................................................................................................................................................2-9 Cruise ..............................................................................................................................................2-9 Glide and Approach .......................................................................................................................2-10 Go Around .....................................................................................................................................2-10 Landing ..........................................................................................................................................2-10 After Clearing the Runway.............................................................................................................2-10 Engine Shutdown...........................................................................................................................2-11 Securing the Aircraft ......................................................................................................................2-11

SECTION 3 EMERGENCY PROCEDURES Ground Engine Fire .........................................................................................................................3-1 In-Flight Engine Fire.........................................................................................................................3-1 In-Flight Engine Shutdown...............................................................................................................3-1 Engine Flame-Out............................................................................................................................3-1 Normal Air Starts .............................................................................................................................3-2 Electrical Fire in Flight......................................................................................................................3-2 Emergency Egress ..........................................................................................................................3-3 Generator Failure.............................................................................................................................3-3

SECTION 4 PERFORMANCE Power-off Stall Speeds ....................................................................................................................4-1 Speeds for Best Rate of Climb.........................................................................................................4-1 Torque Vs. PSIG Chart ....................................................................................................................4-2 TPE331-10 Torque Chart.................................................................................................................4-3 TPE331-10 Fuel Flow Chart ............................................................................................................4-4 TPE331-10 EGT Chart.....................................................................................................................4-5

Thrush Aircraft Inc Model S2R-G10 LOG of Albany, GA

AIRPLANE FLIGHT MANUAL PAGES

FAA APPROVED Rev. 3 Page ii

LOG OF PAGES

ONLY THE PAGES LISTED HERE ARE APPLICABLE TO THE THRUSH AIRCRAFT INC. TURBO THRUSH MODEL S2R-G10

SERIAL NUMBER G10-______

PAGE DATE i ...............................................................................................................March 25, 2010 ii .............................................................................................................. iii .............................................................................................................March 25, 2010 iv .............................................................................................................

SECTION 1 LIMITATIONS 1-1...........................................................................................................March 25, 2010 1-2...........................................................................................................March 25, 2010 1-3........................................................................................................... 1-4...........................................................................................................March 25, 2010 1-5...........................................................................................................March 25, 2010 1-6...........................................................................................................March 25, 2010 1-7...........................................................................................................March 25, 2010 1-8...........................................................................................................March 25, 2010

SECTION 2 NORMAL PROCEDURES 2-1...........................................................................................................March 25, 2010 2-2...........................................................................................................March 25, 2010 2-3...........................................................................................................March 25, 2010 2-4...........................................................................................................March 25, 2010 2-5........................................................................................................... 2-6...........................................................................................................March 25, 2010 2-7...........................................................................................................March 25, 2010 2-8........................................................................................................... 2-9...........................................................................................................March 25, 2010 2-10.........................................................................................................March 25, 2010 2-11.........................................................................................................March 25, 2010 2-12.........................................................................................................March 25, 2010

SECTION 3 EMERGENCY PROCEDURES 3-1...........................................................................................................March 25, 2010 3-2........................................................................................................... 3-3...........................................................................................................March 25, 2010 3-4...........................................................................................................March 25, 2010

SECTION 4 PERFORMANCE 4-1...........................................................................................................March 25, 2010 4-2...........................................................................................................March 25, 2010 4-3...........................................................................................................March 25, 2010 4-4...........................................................................................................March 25, 2010 4-5...........................................................................................................March 25, 2010 4-6...........................................................................................................March 25, 2010

L.BlomeleyTypewritten Text






L.BlomeleyTypewritten TextDecember 07, 2010



AIRPLANE FLIGHT MANUAL REVISIONS

FAA APPROVED: March 25, 2010 Rev. 2 Page iii

LOG OF REVISIONS Revision Number

Page

Description of Revision

FAA Approved

1

See previous G-10 Single Cockpit AFM dated January 12, 1993 and G-10 Dual cockpit AFM dated May 1, 1996 for Revision 1

Manager, FAA Atlanta Aircraft

Certification Office

2

ALL i

ii & iii 1-1 1-2

1-3

1-4

1-5

1-6

2-1 2-2 2-3

2-4

2-9

Re-formatted entire document to standard Thrush AFM format. Combined SC and DC flight manuals into one. Made the Table of Contents a true one Updated per this revision Moved Table of Contents to page i Corrected EGT instrument markings to what the approved gauges show Corrected torque gauge markings to what is on the instruments Changed engine speed limits to match Production Flight Test Procedure Added Maximum Crosswind Velocity 15 MPH Changed to C.G. Range for Single and Dual Cockpit Placards moved to right instrument panel. Added standard sulfur dusting placard. Placard moved from side panel. Placard now includes fuel tank capacity. Added placards P, Q, R. and S., now standard on production airplanes. Moved Table of Contents to page i. Added placards M, N. and O., now standard on production airplanes. Added placards P, Q and R., now standard on production airplanes. Moved Table of Contents to page i. Added step 12. & step 22 Added steps 25, 26, 27, 30, 44 & 45. Moved step 36 from behind the wing and reworded it for clarity. Added steps 47 & 48, added (Single Cockpit) to 55, and 59 & 60 were a single check. Added Step 10.

David Crew For Manager, FAA

Atlanta Aircraft Certification Office

March 25, 2010


AIRPLANE FLIGHT MANUAL REVISIONS

FAA APPROVED: March 25, 2010 Rev. 2 Page v

THIS PAGE INTENTIONALLY LEFT BLANK

Thrush Aircraft Inc Model S2R-G10 SECTION 1 Albany, GA

AIRPLANE FLIGHT MANUAL LIMITATIONS

FAA APPROVED: March 25, 2010 Rev. 2 Page 1-1

SECTION 1 LIMITATIONS

POWERPLANT ENGINE: Garrett TPE331-10

FUEL: - JET A, JET B, JP-4, or JP-5. If jet fuel is not available, aviation gasoline, MIL-G-5572, all grades, may be used, not in excess of 250 gallons per 100 hours of operation may be used for emergency fuel operation. Total gasoline usage must be limited to 7,000 gallons during any 3,000 hour period. ENGINE LIMITS:

POWER SETTING

SHP

TORQUE

% PSI

EGT C

RPM % (1)

OIL PRESSURE

PSIG

OIL TEMP. C

(2)

Takeoff: 5 Min. Limit 900 100

See Note (4)

See Note (3) 100 70 to 120 55 to 127

Max Continuous 900 100

See Note (4)

See Note (3) 100 70 to 120 55 to 110

Ground Idle

72 to 85 40 to 120 -40 to 110

Starting -40 to 110

NOTES: (1) Avoid operation between 18% and 28% RPM, except for transients during start

(2) limitation for MIL-L-23699 oil (3) EGT Limits: 600C at OAT of 45C to 540 C at -15C, straight line

variation between (set the variable redline on the EGT gauge) (4) Takeoff torque limit is 2972 lb/ft at 100% RPM. See current engine log

book for PSI equivalent. Variable redline to match the torque PSI placard.

+

STARTER: Maximum starter duration is three minutes. Allow a five minute cooling off period for the starter between starting attempts.

AIRSTARTS: Normal airstarts are approved for sea level to 12,000 feet altitude and from 100 mph to 159 mph airspeed. (See Emergency Procedures, Section 3)




PROPELLER: Hartzell 4-blade McCauley 4-blade

McCauley 4-blade

Model Number HCB4TN-5NL-LT10890N 4HFR34C653-[X]

[X]-L106FA-0 X4HFR34C662-[X] [X]-L108FA-0

Used on Engine Type TPE331-10 TPE331-10 TPE331-10

Diameter (inches) max. 109.5 106.0 108.0

Diameter (inches) min. 107.5 105.0 105.0

Measurement Station (inches) 42 30 30

Start Lock Blade Angle (degrees) -1.4 0.1 6.0 0.2 6.0 .0.2

Flight Idle Blade Angle (degrees) 4.5 0.2 12.0 0.5 12.0 0.5

Feathered Angle (degrees) 81.2 0.5 87.4 0.2 87.4 0.2

Reverse Angle (degrees) -6.0 0.5 -4.0 0.2 -4.0 0.2

REVERSE POWER: Do not use in flight

INSTRUMENT MARKINGS: Limits Features Meaning

OIL TEMP (C)

-40 -40 to 55 55 to 110 110 to 127

127

Red Radial Yellow Arc Green Arc Yellow Arc Red Radial

Minimum Caution Range Normal Range Caution Range

Maximum

OIL PRESSURE (PSI)

40 40 to 70

70 to 120 120

Red Radial Yellow Arc Green Arc Red Radial

Minimum Caution Range Normal Range

Maximum

FUEL PRESSURE (PSI)

8 8 to 20 80 to 90 20 to 80

90

Red Radial Yellow Arc Yellow Arc Green Arc Red Radial

Minimum Caution Range Caution Range Normal Range

Maximum

EGT (C) Variable 770 Red Bug

Red Graphic Maximum T.O.

Maximum Starting




WEIGHT AND CENTER OF GRAVITY

NOTE Datum is the leading edge of the wing.

Maximum Weight 6,000 pounds

C.G. Range for SINGLE and DUAL COCKPIT: Forward Limit at 6,000 pounds is 26.5 inches AFT of Datum. Forward Limit at 4,000 pounds is 24.0 inches AFT of Datum. (Straight line variation between 4,000 and 6,000 #) AFT Limit at all weights is 30.0 inches AFT of Datum.

NOTE It is the responsibility of the airplane owner and the pilot to insure that the airplane is properly loaded. See the Weight and Balance Section for loading information.

MANEUVERS RESTRICTED CATEGORY

Restricted Category flight maneuvers shall be limited to those normally performed in special purpose operations and approved by Administrator.

TYPES OF OPERATION The Model S2R-G10 aircraft is approved for day and night VFR flight conditions. Flight into known icing conditions is PROHIBITED.

GROUND OPERATION The Pilot should monitor the engine instruments for operation within limits during all ground operations.

PLACARDS A. Located on right hand instrument panel:

THE FLIGHT OPERATION OF THIS AIRPLANE IS LIMITED TO DAY AND NIGHT VFR CONDITIONS. FLIGHT INTO KNOWN ICING CONDITIONS IS PROHIBITED SULFUR DUSTING IS PROHIBITED UNLESS SPECIAL FIRE PREVENTION MEASURES HAVE BEEN INCORPORATED IN AIRCRAFT TAKING OFF IN VISIBLE MOISTURE BELOW 40F IS PROHIBITED




THIS AIRPLANE MUST BE OPERATED AS A RESTRICTED CATEGORY AIRPLANE IN ACCORDANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS AND THE AIRPLANE FLIGHT MANUAL. NO ACROBATIC MANEUVERS, INCLUDING SPINS APPROVED. DESIGN MANEUVERING SPEED: 126 MPH. MAX. FLAP-DOWN SPEED: 123 MPH. MAX. CROSSWIND VELOCITY, LANDING-15 MPH. USABLE TANK CAPACITY 114 GALLONS EACH SIDE. PUSH STICK FORWARD TO UNLOCK TAILWHEEL NO SMOKING

B. Located near Park Brake Valves:

PARK BRAKE ON. DEPRESS PEDALS AND PULL LEVER. OFF, DEPRESS PEDALS

C. Located on Forward Lower Corner of Each Door Side Window: DO NOT OPEN DOOR IN FLIGHT

D. Located adjacent to the torque meter:

MAXIMUM TORQUE IS 100% Or MAXIMUM TORQUE IS XX.X PSI (Note: value is determined from engine log

book) For aircraft equipped with any McCauley Propeller: CONTINUOUS GROUND OPERATION WITH BRAKES LOCKED ABOVE 70% TORQUE IN REAR QUARTERING WINDS GREATER THAN 20 KNOTS PROHIBITED

E. At both fuel filler caps:

FUEL 115 GAL. CAP. JET A, JET B, JP-4, JP-5 F. Located on glareshield directly in front of pilot:

WARNING DO NOT MOVE POWER LEVER BELOW FLIGHT IDLE IN FLIGHT. AT HIGH TAXI SPEEDS USE REVERSE POWER ONLY IF THE TAIL WHEEL IS LOCKED AND FIRMLY ON THE GROUND

G. Located on top of hopper:




HOPPER CAPACITY 4000 LBS

H. Located on the instrument panel next to the engine tachometer AVOID ENGINE OPERATION BETWEEN 18 and 28 PERCENT RPM EXCEPT DURING START AND SHUTDOWN

I. Located adjacent to the engine fuel switch:

CAUTION: HOLD FUEL SWITCH FOR FIVE SECONDS IN THE OFF POSITION DURING SHUTDOWN

J. Located near the pilots door:

RESTRICTED

K. Located near the EGT gauge:

EGT LIMIT

OAT, C EGT, C

45 35 25 15 5 -5 -15

600 590 580 570 560 550 540

L. On airplanes equipped with the Hartzell HC-B4TN-5NL/LT 10890 propeller,

located near the tachometer:

STABILIZED GROUND OPERATION IS PROHIBITED BETWEEN 85% and 92% RPM

M. Located on the fuel gauge:

USABLE FUEL 114 U.S. GAL. FUEL ABOVE 82 GAL. IS UNGAGEABLE

N. Located at each door latch:

OPEN or OPEN O. Located at each door knockout panel:

PUSH OUT AND LIFT HINGE PIN FOR EMERGENCY EXIT




P. Located (external, inverted) at each door hinge pin:

PULL HINGE PIN FOR EMERGENCY EXIT

Q. Located on inside of baggage door: (Single Cockpit Only)

60 LBS. MAXIMUM BAGGAGE

R. On the right hand side panel:(Dual Cockpit Only)

Passenger or cargo 200 LBS MAXIMUM




This Page Intentionally Left Blank

Thrush Aircraft Inc Model S2R-G10 NORMAL Albany, GA

AIRPLANE FLIGHT MANUALPROCEDURES


SECTION 2 NORMAL PROCEDURES

DEFINITIONS

WARNING Personal injury or loss of life could result if the operating procedures and techniques are not followed carefully.

CAUTION Damage to equipment could result if the operating procedures and techniques are not followed carefully.

NOTE This is used when it is essential to emphasize an operating procedure or technique.

Airspeeds: All airspeeds in this Section are Indicated Airspeeds (IAS) in Miles per Hour (MPH), unless otherwise noted.

VISUAL INSPECTION

NOTE Visually check aircraft for general condition during walk-around inspection. Verify that all skin panel Cam-Locs are fastened. In cold weather, remove all accumulations of frost, ice, or snow from wing, tail and control surfaces. Check that control surfaces contain no internal accumulations of ice. If a night flight is planned, check operation of all lights and assure a flashlight is available.




VISUAL INSPECTION (Continued)

23. Fuel quantity CHECK, visually and secure cap. 24. Left Wing Sump DRAIN 25. Header Tank Sump DRAIN 26. Left Fuel Vent Sump DRAIN 27. Firewall Fuel Filter DRAIN, check bypass indicator. 28. Fuel Vent Pressure Inlet CHECK for obstruction. 29. Battery Vent Inlet, CHECK for obstruction. 30. Main Wheel Tire CHECK for inflation, damage and wear. 31. Wheel Brake CHECK condition

32. Propeller CHECK for spinner damage or oil leaks. 33. Propeller CHECK the propeller blades for nicks, cracks, or excessive

erosion of the leading edge and on start locks.

CAUTION

DO NOT ROTATE PROPELLER BACKWARDS. IT WILL CAUSE DAMAGE TO THE STARTER GENERATOR.

34. Engine Inlet CHECK for condition of first stage centrifugal compressor. 35. P2T2 Sensor Probe CHECK for general condition. 36. Oil Cooler CHECK for leaks and stoppage. 37. Battery Vent Outlet CHECK, for obstruction 38. Dispersal Equipment (if installed) CHECK the windmill, the pump, the

hose, the spreader, the mounting, and so forth. 39. Engine CHECK for oil leaks, fuel leaks, loose fittings, cracked exhaust

stacks and excessive dirt or corrosion. 40. Oil Quantity CHECK dipstick and secure cap. 41. Oil By-Pass Indicator CHECK.

42. Wheel Chocks REMOVE. 43. Fuel Quantity CHECK, visually and secure the cap. 44. Main Wheel Tire CHECK for inflation, damage and wear. 45. Right Fuel Vent Sump DRAIN.




VISUAL INSPECTION (Continued)

46. Right Wing Sump DRAIN. 47. Wing Leading Edge CHECK for damage.

NOTE Keep the wing leading edge clean. An excessive build-up of dirt, bugs, and chemicals can have the same negative

effect on lift as an accumulation of ice or frost.

48. Pitot Mast CHECK, for blockage of opening. 49. Wing Tie Down REMOVE. 50. Wing Tip CHECK for damage.

51. Aileron CHECK for free and correct movement. 52. Aileron Hinges CHECK, for looseness. Use a brisk UP and DOWN

motion, but use caution so as not to damage control or stops. 53. Spray Boom (if installed) CHECK, for leaks and security. 54. Wing Flap CHECK, for security. 55. Baggage Compartment (Single Cockpit) - CHECK and secure area.

56. Rudder Gust lock (if installed) REMOVE 57. Empennage CHECK, for Condition 58. Tail Struts CHECK, for tension and security. 59. Tail Wheel Tire CHECK, for inflation, damage and wear. 60. Tail Wheel Spring CHECK for condition and security. 61. Tail Wheel Assembly and locking mechanism CHECK, for condition

and security. 62. Rudder and Elevator CHECK, for freedom of movement and security. 63. Elevator Trim Tabs CHECK, for near neutral (takeoff) position and

excessive play. 64. Tail Tie down REMOVE 65. Static Port Openings CHECK for blockage




STARTING ENGINE (Continued)

CAUTION

DO NOT ATTEMPT AN ENGINE START WITHOUT PROPELLER ON START LOCKS

NOTE Engine starts can be made with the aircraft battery power, or with auxiliary electrical power. However, it is recommended that an auxiliary power unit be used when ambient air temperature is ten degrees F. or below. Ensure that ground power unit (aux power) is regulated to 28 volts dc, and is capable of providing a minimum of 24 volts dc, 800 amperes during start cycle.

7. Negative Torque System Check The NTS System should be checked during the first start of the day or if a malfunction of the system is suspected. To accomplishes the check, do the following during starting: A. NTS Light PRESS to test. B. Unfeathering Pump Switch ON C. NTS Check Switch ON D. NTS Light CHECK ON E. Engine Starter Ground position (Carry out normal start) F. NTS Light OUT when starter is engaged G. NTS Light On at 10 to 30 percent RPM

8. Engine Starter Ground position 9. Ignition Switch ON at 10% RPM minimum

CHECK IGNITION LIGHT ON PRIOR TO OPERATING FUEL SWITCH.

CAUTION

10. Engine Fuel Switch ON at 10% RPM minimum.




STARTING ENGINE (Continued)

CAUTION

IF LIGHT OFF IS NOT INDICATED WITHIN TEN SECONDS OR 20% RPM, REJECT THE START BY

ACTIVATING THE EMERGENCY SHUT-OFF LEVER.

11. Fuel Enrichment Switch ON until approximately 680 degrees EGT (maximum during start is 770 degrees). Then regulate enrichment switch to obtain satisfactory rpm increase and temperature.

CAUTION

IF RPM STOPS INCREASING PRIOR TO 40%, OR IF EGT IS APPROACHING LIMITS (770 DEGREES C.) AND RISING

RAPIDLY, ACTIVATE THE EMERGENCY SHUT OFF LEVER. 12. Engine Instruments CHECK

A. RPM 72% Minimum B. Fuel Pressure 8 PSIG Minimum C. Oil Pressure 40 PSIG Minimum

CAUTION

IF OIL PRESSURE IS NOT INDICATED WITHIN TEN SECONDS AFTER LIGHT-OFF, SHUT DOWN ENGINE AND DETERMINE CAUSE.

13. Starter OFF 14. Generator ON and charging normally 15. Warning Lights CHECK and consider 16. If NTS check was accomplished:

A. Unfeathering Pump Switch OFF B. NTS Check Switch OFF

DRY MOTORING RUN 1. Allow three minutes for fuel and vapors to drain from the engine before

attempting re-start. 2. Motor the engine with the starter (prop on locks) with fuel and ignition

off.




NOTE The ground idle region of the throttle quadrant

may be utilized for taxiing. Push the stick forward to unlock tail wheel.

3. Brakes CHECK

BEFORE TAKE OFF 1. Flight Controls CHECK free and full travel 2. Instruments NORMAL 3. Fuel Valve ON

BEFORE TAKE OFF (Continued) 4. Flaps 15 Degree or as required 5. Auxiliary Fuel Pump ON 6. Ignition Switch ON 7. Speed Lever HI RPM 8. Strobe Lights ON 9. Torque PSI Limits Set (Airplanes with P.S.I. Gauge) 10. Elevator tab SET for Take-off

TAKE-OFF 1. Brakes Release 2. Power Lever- Advance. Do not exceed engine operational limitations.

(See Limitations Section).

MAXIMUM TORQUE FOR TAKE OFF IS 100% or XX.XPSI (see engine log book)(900SHP). AS AIRCRAFT ACCELERATES, TORQUE AND EGT WILL INCREASE.

CAUTION

3. After breaking ground, allow air speed to build up to best rate-of-climb speed, 85 MPH.

CLIMB 1. Established best-rate-of-climb speed, 85 MPH. 2. Reduce power as necessary. 3. Flaps RETRACT. 4. Fuel Aux. Pump OFF 5. Ignition Switch OFF




SECURING THE AIRCRAFT 1. Parking Brake RELEASE and INSTALL wheel chocks. 2. Control Lock ENGAGE 3. Wing and Tail Tie-downs SECURE.

Thrush Aircraft Inc Model S2R-G10 EMERGENCY Albany, GA


FAA APPROVED: March 25, 2010 Rev. 2 page 3-1

SECTION 3

EMERGENCY PROCEDURES GROUND ENGINE FIRE See DRY MOTORING RUN under Ground Operation, Section 2.

IN-FLIGHT ENGINE FIRE In case of an in-flight fire, the following procedures should be used:

1. Emergency Cut-Off Lever CUT OFF 2. Engine Fuel Switch OFF 3. Fuel Auxiliary Pump Switch OFF 4. Fuel Valve OFF

IN-FLIGHT ENGINE SHUT DOWN The following procedure should be used to shut down the engine in flight:

NOTE In the unlikely event of a shutdown in flight due to fuel starvation or an engine problem, the negative torque sensing system will increase propeller blade angle toward feather at the optimum rate to reduce drag. This decreases the urgency of feathering the engine and allows the pilot to concentrate on control of the aircraft.

1. Emergency Cut Off Lever CUT OFF 2. Power Lever FULL FORWARD

NOTE Moving the power lever fully forward drives the propeller blade to the lowest angle of attack in the event the feather valve or NTS system has not functioned properly.

3. Fuel Aux. Pump Switch OFF 4. Engine Fuel Switch OFF 5. Fuel Valve OFF

ENGINE FLAME-OUT The symptoms of an engine flame-out will be a drop in the exhaust gas temperature, torque meter pressure and RPM. The flame-out may result from the engine running out of fuel, or possibly may be caused by unstable engine operation. Once the fuel supply has been restored to the engine or the cause of the unstable operation eliminated, the engine may be restarted in the manner described under Air Starts, following.




ELECTRICAL FIRE IN FLIGHT (Continued) If electrical power is essential for the flight, attempt to identify and isolate the faulty circuit as follows:

1. Generator Switch ON 2. If Generator Circuit is Defective, Generator Switch OFF, then Battery

Switch ON. 3. Turn on each circuit individually. Allow a short period of time before

proceeding from one circuit to the next until the defective circuit is identified.

4. Defective Circuit OFF.

EMERGENCY EGRESS If it if necessary to remove the cockpit door from its hinges, do the following:

1. KNOCK OUT the oval panel below the window. 2. REACH through the hole and PULL UP the flexible hinge pin. This

releases the door at the hinge. 3. PUSH the door clear of the aircraft and EXIT.

FOR DUAL COCKPIT AIRCRAFT: If it if not desired to release the door from its hinges, but it is desired to exit the aircraft in the normal manner, do the following:

1. The front cockpit door must be closed in order for the rear occupant to deplane.

2. The rear occupant can deplane by using the step in the left side of the fuselage below the front door.

GENERATOR FAILURE 1. RESET Generator 2. If Generator is not restored, accomplish the following:

a. All nonessential electrical equipment OFF. NOTE

If Generator Fails, Air conditioner will not work because it is powered directly off the generator.

Thrush Aircraft Inc Model S2R-G10 PERFORMANCE Albany, GA

AIRPLANE FLIGHT MANUAL


SECTION 4 PERFORMANCE

POWER OFF STALL SPEEDS The variation of power-off stall speeds with bank angle, flight configuration and airplane weight is shown below for the flaps up and flaps 15 degrees configurations.

ASSOCIATED CONDITIONS

Configurations Clean T.O/Landing Wing Flaps 0 degrees 15 degrees

Dispersal Equipment none none

Stall Entry Rate Uniformly Decreasing Gross Weight 6,000 pounds

POWER OFF STALL SPEEDS MPH (CAS)

WING FLAPS 0 degrees 15 degrees GROSS WEIGHT

(pounds) 6,000 6,000

0 70 66 30 75.2 70.9 BLANK ANGLES (degrees) 60 99.0 93.3

NOTE: Altitude loss for stall recovery is 300 fee.

SPEED FOR BEST-RATE-OF-CLIMB

Configuration 6,000 pounds

Flaps 0 degrees 85 MPH (CAS)

Flaps 15 degrees 81 MPH (CAS)

NOTE The S2RHG-G10 may be operated at cruise up to and including 100% torque, provided that airspeed and EGT limits are not exceeded. Use the chart below (pg 4-2) to determine the PSI settings for a given percent of torque, after entering the engine torque pressure characteristics.




Torque Vs. PSIG Chart





G10 AFM Cover Rev. 3G10 AFM ppi Rev. 2G10 AFM ppii Rev. 3G10 AFM ppiii Rev. 3G10 AFM SEC 1 Rev. 3G10 AFM SEC 2 Rev. 3G10 FM SEC 3 Rev. 3G10 FM SEC 4 Rev. 3

thrush 510 garret flight manual

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