ATT 74 01-50-T34C-600-6-1.pdf

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DEPARTMENT OF THE NA\ry

PROGRAM EXECUTIVE OFFICER

TACTICAL AI RCRAFT PROGRAMS

47123 BUSE ROAD BLDG 2272

PATUXENT RIVER MARYIAND 20670-1 547

ser PW\ -273 / rO7 9

AU6 | 2 2013

Program Executive Officer, Tact,ical Aircraft Programs, Naval Undergraduate Flight Training (PMA-273 )

Chief of Naval Air Training, Corpus Christi, TX

NAVATR (PMA 273)01-50-T34C-600-6-r U.S. NAVY T-34C TURBO MENToR oeTT,y/TURNARoUND MAINTENANCE REQUIREMENTS

Encl: (1) NAVAIR (pue 273 ) Or-50-T3 4C-500-5-1

1 . Enclosure ( 1 ) is forwarded for action.

2. PI"IA-273 point of contact is Mr. Tim Quinn, PMA-273 Assistant Program Manager for Systems Engineering (apt'!Se), DSN 757-5181 or Commercial (301) 757-5181.

BACON

USN

Distribution:

CNAF Norfol-k, VA (Attn: Code N42LS) NASA Dryden, Edwards AFB, CA (Attn: Maria E1ena Nichols) NASA Cleveland, Cleveland, OH (attn: Geral-d Anschuetz M/S 4-2) AATD Ft Eustis, VA (Attn: Wayne Waersch) USAOTC, Ft. Bragg, NC (Attn: Rj-chard Dolan) AAFTD, FT. Rucker, AL (Attn: Frank Gonzal-ez) FST, Jacksonville, FL (Attn: David pfeffer)

ATTACHMENT 74

NAVAIR (PMA 273) 01-50-T34C-600-6-1 N61340-18-FOSR-0001

NAVAIR (PMA 273) 01-50-T34C-600-6-1

TECHNICAL MANUAL

T-34C TURBO MENTOR

DAILY/TURNAROUND MAINTENANCE REQUIREMENTS

1 AUGUST 2013

MAINTENANCE REQUIREMENT CARD

CARD NUMBER

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DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

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WORK AREA WUC ITEM TASK DESCRIPTION/REQUIREMENT HYD PWR

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INTRODUCTION

This checklist contains abbreviated inspection requirements that are necessary to determine the need for servicing and ensure the integrity of the aircraft for flight.

APPLICATION

Daily Inspection requirements shall be accomplished prior to the aircraft being released safe for flight. The Daily Inspection is valid for a period of 72 hours commencing from the date and time the inspection is completed, provided no flight occurs during this period and no maintenance other than servicing has been performed. Aircraft may be flown for 24 hours without another daily. This 24 hour period begins with the first launch following accomplishment of the daily inspection. The 24 hours cannot exceed the 72 hour expiration of the daily unless the expiration occurs during a mission.

A Turnaround Inspection shall be accomplished between flights and when more than 24 hours has elapsed since completion of the Daily Inspection on aircraft that have not been flown. The turnaround inspection is considered to be valid for a period of 24 hours commencing from the date and time the inspection is completed, provided that no flight and no maintenance other than servicing occurs during this period.

An asterisk (*) in front of those items requiring inspection indicates the Turnaround Inspection requirements.

Note: Turnaround Inspection may be waived on US Naval Training Command and Test Pilot School aircraft when cold refueling between flight evolutions if pilot in command stays the same.

CAUTION

Ensure area around aircraft is free of foreign objects and all safety items are properly positioned, removed or installed, as applicable.

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DATE

August 1, 2013

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CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

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Insert latest changed cards; dispose of superseded cards in accordance with applicable regulations.

NOTE: The portion of text affected by the change is indicated by a vertical line or other change symbol in the outer margin of the card.

Dates of issue for original and changed cards.

Original . . . . . . . . . . . . . . . . . . . . . . . . August 1, 2013 (this issue supersedes all previous editions)

Total number of pages in this manual is 15 consisting of the following:

Card Number Change Number Date Card Number Change Number Date

i. 0 4. 0

ii. 0 5. 0

iii. 0 6. 0

iv. 0 7. 0

v. 0 8. 0

vi. 0 9. 0

vii. 0 10. 0

viii. 0 11. 0

ix. 0 12. 0

1. 0 13. 0

2. 0 14. 0

3. 0 15. 0 iii

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

ELEC PWR

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Figure 1. T34C Front Cockpit

1. Emergency Locator Transmitter (ELT)

2. Fuel Shut Off Handle “T” Handle

3. UHF Radio

4. Flap Handle

5. Aileron Trim Wheel

6. Elevator Trim Wheel

7. Rudder Trim Wheel

8. Engine Controls

9. Environmental Control Handle

10. Landing Gear Handle

11. Battery Switch

12. Generator Switch

13. O2 Regulator Panel

14. TACAN

15. VOR

16. Audio Panel

17. Master Avionics Switch

18. Attitude Gyro Switch

19. RMI Switch

20. Exterior Lights and Strobe Lights

21. Pitot Heat

22. Fuel Pump

23. Inverter Select Switch

24. Avionics Command Transfer Switch

1 2 3 7

14 15 16

UTILITY

LIGHT

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DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

ELEC PWR

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1. LANDING GEAR POSITION Indicators (28 VDC)

2. Flap Position Indicator (28 VDC)

3. Angle-of-Attack (AOA) Indicator (28 VDC)

4. Landing Gear Warning Light — (28 VDC)

5. GPS/NAV Annunciator/Control Panel - (28 VDC)

6. Airspeed Indicator - (Pitot-Static)

7. MASTER CAUTION Light - (23 VDC, Flashing - Amber)

8. Altimeter - (Mode C 28 VDC, 28 VDC, Vibrator, Static)

9. AlTITUDE GYRO PAST ERECT Switch - (1 per minute)

10. Attitude Gyro Indicator - (115 VAC)

11. FIRE Warning Light - (28 VDC- Red)

12. Radio Magnetic Indicator (RMI) - (28 VDC & 26 VAC)

13. NACWS - C28 VD.C. & 26 VAC)

14. VHF/UHF Radio Transmit Switch (28 VDC)

15. VHF Receive Switch (28 VDC)

16. Course Deviation Indicator- (Repeat VOR/TACAN Info from RMI)

17. Clock - (8 Day & Elapsed Time, Self Powered)

18. Torque meter - (26 VAC)

19. VOLT/AMMETER - (Reads Minus Amps on GPU)

20. Interstage Turbine Temperature Gauge - (Self Powered)

21. Fuel Flow Indicator - (26 VAC)

22. FIRE Warning Teat Switch - (1. Low ACC. 2. Upper ACC. 3. Engine)

23. Oil Temperature and Pressure Gauge - (28 VDC)

24. Fuel Quantity Gauge - (28 VDC)

25. Propeller Tachometer - (Self Powered)

26. Fuel Quantity Gauge - (28 VDC)

27. Turbine Tachometer - (Self Powered)

28. PROP OVSP TEST Switch - (1950 - 2150 Prop RPM)

29. Annunciator Panel - (28 VDC)

30. Annunciator Panel Test Switch - (28 VDC)

31. A.O.A. Test Switch - (28 VDC - App. 20 Units - Stall Warning 26.5 Units)

32. Accelerometer - (Self Powered By Acceleration Forces)

33. Turn-and-Slip Indicator - (115 VAC)

34. Vertical Speed Indicator - (Static) 35, COMPASS SLAVE Switch - (MANUAL Control in D.G. Position)

38. COMPASS FAST SLAVE Switch - (SLAVE - Auto Align, FAST - Quick Align Card to Flux Det, D.G. - Disconnects Card from Flux Det.)

37. Global Positioning System Unit - (28 VDC/25 VAC)

38. Inboard Gear Door Position Indicator (28 VDC)

Figure 2. T34C Front Cockpit Instrument Panel v

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

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1. AOA Indexer

2. Standby Magnetic Compass

3. Free Air Temperature Gauge

4. Rudder Pedals

5. Emergency Canopy Open Handle

6. Starter/Ignition Control Panel

7. Parking Brake Handle

8. Control Stick

9. Engine Air Inlet Bypass

10. Oxygen Control Handle

11. Alternate Static Air Control

12. Electrical Control Command Panel

13. Emergency Landing Gear Extension Handle

14. Landing Gear Hand Crank Clutch Knob

15. Cockpit Flood Lights

16. Cockpit Utility Light

17. Circuit Breaker Panel

18. VHF Radio

19. Map Case

20. Flight Controls Lock Frame

21. Emergency Locator Transmitter (ELT)

22. Emergency Fuel Shutoff Handle

23. Aileron Trim Wheel 24, Elevator Trim Wheel

25. Rudder Trim Knob

26. Flap Switch

27. Evaporator Unit

28. Engine/Propeller Control Quadrant

29. Rudder Pedal Adjustment Control

30. Left Subpanel

31. Cockpit Environmental Control

32. Windshield Defogger Control

Figure 3. T34C Front Cockpit Arrangement vi

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

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Figure 4. T34C AFT Cockpit

UTILITY

LIGHT

1. Vertical Gyro

2. Flap Lever

3. Aileron Trim Wheel

4. Engine Controls

5. Rudder Trim Wheel

6. Elevator Trim Wheel

7. UHF Radio

8. Inverter Select Switch

9. Generator

10. Battery

11. O2 Regulator

12. TACAN

13. VOR

14. Audio Panel

15. Interior Lights

12 13 14 15 vii

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

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1. LANDING GEAR POSITION Indicators (28 VDC)

2. Flap Position Indicator (28 VDC)

3. Angle of Attack (AOA) Indicator (28 VDC)

4. Landing Gear Warning Light (28 VDC)

5. GPS/NAV Annunciator/Control Panel - (28 VDC)

6. Airspeed Indicator Pitot.-Static)

7. MASTER CAUTION Light - (28 VDC, Flashing Amber)

8. Altimeter (Mode C 28 VDC, 28 VDC, Vibrator, Static)

9. ATTITUDE GYRO FAST ERECT Switch (1 per minute)

10. Attitude Gyro Indicator (115 VAC)

11. FIRE Warning Light - (28 VDC, Red)

12. Radio Magnetic Indicator (RMI) (28 VDC & 26 VAC)

13. NACWS- (28 VDC & 26 VAC)

14. VHF/UHF Radio Transmit Switch (28 VDC)

15. VHF Receive Switch (28 VDC)

16. Course Deviation Indicator (Repeat VOR Tacan Info from RMI)

17. Clock - (8 Day & Elapsed Time, Self Powered)

18. Torque meter (26 VAC)

19. VOLT/AMMETER (Reads Minus Amps on GRU)

20. lnterstage Turbine Temperature Gauge (Self Powered)

21. Fuel Flow Indicator- (23 VAC)

22. Solo Flight Placard (Aft Cockpit Only)

23. Oil Temperature and Pressure Gauge (28 VDC)

24. Fuel Quantity Gauge (28 VDC)

25. Propeller Tachometer - (Self Powered)

26. Fuel Quantity Gauge - (28 VDC)

27. Turbine Tachometer - (Self Powered)

28. PROP OVSP TEST Switch (1950.. 2150 Prop R.P.M.>

29. Annunciator Panel (28 VDC)

30. Annunciator Panel Test Switch - (28 VDC)

31. A.O.A. Test Switch - (28 VDC. App. 20 Units.. Stall Warning 26.5 Units)

32. Accelerometer (Self Powered By Acceleration Forces)

33. Turn-and-Slip Indicator.. (115 VAC)

34. Vertical Speed Indicator- (Static)

35. COMPASS SLAVE Switch.. (MANUAL Control in D.G. Position)

36. COMPASS FAST SLAVE Switch.. (SLAVE - Auto Align, FAST Quick Align Card to Flux Oat, D.G.. Disconnects Card from Flux Det.)

37. Global Positioning System Unit (28 VDC/25 VAC)

38. Inboard Gear Door Position Indicator (28 VDC)

Figure 5. T34C AFT Cockpit Instrument Panel viii

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

ELEC PWR

N/A

1. AOA Indexer

2. Standby Magnetic Compass

3. Emergency Canopy Open Handle

4. Starter/Ignition Control Panel 5, Electrical Command Control Panel

6. Circuit Breaker Panel

7. Cockpit Flood Lights

8. Cockpit Utility Light

9. Instrument Flight Hood

10. Map Case

11. Vertical Gyro

12. Aileron Trim Wheel

13. Flap Switch

14. Elevator Trim Wheel

15. Rudder Trim Knob

16. Evaporator Unit

17. Engine/Propeller Control Quadrant

18. Rudder Pedal Adjustment Control

19. Left Subpanel

Figure 6. T34C AFT Cockpit Arrangement ix

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

ELEC PWR

N/A

1. Strobe Light

2. Navigation Light

3. Instrument Hood

4. First Aid Kit

5. GPS Antenna

6. NACWS GPS Antenna

7. UHF Antenna

8. ELT Antenna

9. VOR Antenna

10. Ventral Fin (RH Not Shown)

11. TACAN Antenna

12. Strake (RH Not Shown)

13. Static Air Source (RH Not Shown)

14. NACWS Antenna Lower

15. Avionics Compartment

16. AFT Transponder Antenna

17. AFT Cockpit Assist Step

18. Assist Handle 18a. VHF Antenna 19, Wing Walkway (RN Not Shown I

20. Angle of Attack Probe 21, Pitot Tube

22. Landing Light

23. External Landing Gear Position Indicator Light

24. Forward Transponder Antenna

25. Cooling Air Outlet (RH Not Shown)

26. Oil Cooler Air Intake

27. Engine Air Intake

28. Exhaust Stacks

29. NACWS Antenna, Upper

Figure 7. T34C General Aircraft Arrangement

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

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THINK SAFETY

“Any discrepancies found or noted during this inspection shall be documented and reported to Maintenance Control”

1. Review ADB for completed maintenance actions and outstanding discrepancies.

2. Remove all protective covers________________________________ Check

Note

Aircraft shall not have been operated or refueled within thirty (30) minutes.

The fuel sample shall be obtained prior to the first flight of the day for an aircraft that is intended to be flown that day. A fuel sample is considered valid for the day or a flight if the sample was obtained within twenty-four (24) hours prior to the flight.

3. Fuel Samples____________________________________________ Obtain/Inspect

Refer to figures 1 thru 6 for cards 1, 2, 3, and 4.

4. Cockpit (F/C & R/C, As Applicable):

* a. Canopy/Windscreen___________________________________ Damage/Cleanliness

* b. Canopy Latches______________________________________ Proper Operation

* c. Canopy Rail Screws___________________________________ Flush with Rail

d. Center Canopy Drain__________________________________ Condition/Blockage

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

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4. Cockpit (Continued):

Check cockpit and floorboards for pooled water or excessive moisture. Document discrepancies, notify maintenance control

* e. Cockpit Interior______________________________________ FOD Free/Water intrusion

f. First Aid Kit_________________________________________ Date/Seal Intact

g. Outside Air Temperature gauge and probe (OAT)___________ Damage/Condition/Security

* h. Wet Compass________________________________________ Damage/Leakage/Security

* i. Relief Tubes_________________________________________ Condition and Stowed

WARNING

Failure to check the Inertial Reel locking function could result in serious injury or death.

* j. Seat Belt/Inertial Harness_______________________________ Operation/Condition/Straps Fully Extended

* k. Seats_______________________________________________ Check for freedom of movement, operation, Bungee

Cord for security and condition

If lumbar support is attached to the parachute, remove and return it to Maintenance Control.

* l. Parachutes___________________________________________ Condition/Security/Tacking Thread

* m. Landing Gear Handle_________________________________ Check In Down Position

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

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Maximum limits are +4.5 Gs and –2.3 Gs as indicated in either/both cockpits. Notify Maintenance Control to initiate a VIDS/MAF for performance of appropriate “Over G”

Inspection if maximum limits have been exceeded. Also notify Maintenance Control to initiate a VIDS/MAF if the “Tie Wrap” is missing or broken.

* n. “G” Meter___________________________________________ Check Within Limits/Tie Wrap Installed On Reset

Knob Shaft

If Emergency Landing Gear Handle Crank Clutch is engaged notify Maintenance Control

o. Emergency Landing Gear Hand Crank Clutch_______________ Disengaged

* p. Equipment Switches___________________________________ Off/Positioned/Damage/Condition

* q. NACWS CDU_______________________________________ Off (Both Cockpits),

* r. GPS________________________________________________ Off (Both Cockpits)

* s. Starter/Auto-Ignition Switches___________________________ Off (Both Cockpits)

* t. Inverters_____________________________________________ Off (Both Cockpits)

* u. Generator Switch______________________________________ Positioned GEN (Both Cockpits)

If Circuit Breakers are found popped/pulled out notify Maintenance Control

* v. Circuit Breakers______________________________________ Set

w. Flap Lever__________________________________________ Off

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

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If the indicated battery voltage is less than twenty-two (22) volts, plan for a GPU assisted start.

If the indicated battery voltage is less than eighteen (18) volts, the battery must be replaced.

Notify Maintenance Control so a VIDS/MAF can be initiated to replace the battery.

* x. Battery_____________________________________________ On/Check Voltage

* y. Fuel Quantity Indication_______________________________ Check

z. Landing Gear Position Indicators_________________________ Three Down & Locked

aa. Interior Lights (All)___________________________________ Check On/Off

ab. Fire Warning System__________________________________ Test All Three Positions

ac. Pitot Heat___________________________________________ Test (Amp Drop)/Off

ad. Standby Fuel Pump___________________________________ Test (Annunciation Light Out) Off

ae. Emergency Locator Transmitter_________________________ Check (Arm Position) Do Not Move Switch

CAUTION

Do not move engine power lever into BETA range

af. Engine Controls______________________________________ Operation/Binding/Position

ag. Fuel Shut Off “T” Handle______________________________ Check Down and Lock

5. Cockpit:

* a. Control Locks________________________________________ Remove/Stow As Required

b. Rudder Pedal Adjustment_______________________________ Freedom Of Movement

* c. Flight Controls (Including Tabs)__________________________ Binding/Free Movement

d. Trim Tabs (All)_______________________________________ Set Zero (0)

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

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N/A

5. Cockpit (Continued):

e. UHF________________________________________________ Preset/Both/Squelch-On

f. VHF (if installed)______________________________________ Off

g. Annunciator System, Both Cockpits_______________________ Test and Check

h. Inboard Door Indication System, Both Cockpits______________ Test and Check

* i. Oxygen System_______________________________________ T-Handle Pulled

* j. Oxygen System_______________________________________ Quantity (1,000 psi minimum and

1,500 psi minimum for cross-country flights.

Maximum 1800)

* k. Oxygen Regulator_____________________________________ On (Shear Wire Not Broken) 100% Oxygen, Normal/Switch Integrity

l. Oxygen Hose_________________________________________ Looseness/Condition/Security

m. TACAN____________________________________________ T/R

n. VOR________________________________________________ On

o. Transponder__________________________________________ Off

p. Audio Panel:

1. VOR_____________________________________________ Off

2. TACAN__________________________________________ Off

3. UHF_____________________________________________ Normal

4. ICS______________________________________________ Cold Microphone (CM)

q. Master Avionics______________________________________ Off

r. Attitude Gyro/RMI Switches (For R/C)____________________ On

s. Instrument Panels, Both Cockpits_________________________ Properly Secured

Ensure flaps are clear. Observe flap movement corresponding with the flap indicator

* t. Flap Lever___________________________________________ Full Down

* u. Battery Switch_______________________________________ Off

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

ELEC PWR

OFF

WORK AREA WUC ITEM TASK DESCRIPTION/REQUIREMENT HYD PWR

6. Left Hand Wing, Main Landing Gear and Wheel Well

Inspect Aileron for freedom of movement. Inspect flap and aileron attaching hardware including the bonding wire for security and “safety” of locking devices

* a. Flaps_______________________________________________ Damage/Condition/Security

* b. Aileron (Including Tabs)_______________________________ Damage/Condition/Security

* c. Static Wicks_________________________________________ Damage/Condition/Security

* d. Wing Skin___________________________________________ Damage

* e. Wing Tip____________________________________________ Damage/Security

* f. Navigation/Strobe Light lenses___________________________ Cracks, distortion, security.

* g. AOA Sensor_________________________________________ Condition/Security

Visually check fuel level through filler neck. During Daily Inspection ensure visual fuel level corresponds with indicated fuel quantity. Ensure the fuel cap is properly secured and aligned with arrow.

* h. Fuel:

1. Fuel______________________________________________ Leakage/Visual Quantity

2. Fuel Anti-Siphon Valve/Gasket________________________ Damage/Condition/Security

3. Fuel Cap__________________________________________ Damage/Condition

* i. Pitot Tube___________________________________________ Damage/Condition/Clear of obstructions

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

ELEC PWR

OFF

WORK AREA WUC ITEM TASK DESCRIPTION/REQUIREMENT HYD PWR

6. Left Hand Wing, Main Landing Gear and Wheel Well (Continued):

Check to ensure presence of corrosion preventative compound (CPC) on flight control cables in the wheel well area.

* j. Landing Gear Light___________________________________ Damage/Condition/Security

* k. Landing Gear Shock Strut______________________________ Clean/Extension

Main Landing Gear Strut extension is minimum 3 inches

* l. Torque Knees________________________________________ Damage/Condition/Security

* m. Brake and Brake Lines________________________________ Wear/Leakage

* n. Brake Bolts_________________________________________ Safety Wired

* o. Tire and Wheel_______________________________________ Damage/Wear/Slippage Marks

Main Landing Gear Tire pressure is 90 psi plus or minus 2 psi.

p. Tire_________________________________________________ Check Tire Pressure

q. Wheel Retaining_______________________________________ Nut Cotter Keyed

r. Wheel Well and Doors__________________________________ Damage/Condition/Security

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

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6. Left Hand Wing, Main Landing Gear and Wheel Well (Continued):

Do not pull on the down lock assembly, serious injury will occur

* s. Down Lock Block Assembly (Including Cables)____________ Damage/Condition/Security

* t. Fuel Vents__________________________________________ Clear of obstructions

7. Left Side Engine:

* a. Left Side Engine Compartment__________________________ FOD Free

* b. Oil Cap_____________________________________________ Quantity/Secured/Locking Tab Aft

* c. Engine and Accessories________________________________ Damage/Condition/Security/Leakage/Chafing

* d. Oil Cooler Intake Screen and Plenum_____________________ Clear of obstructions

* e. A/C Compressor Drive Belt ____________________________ Condition/Tension/Safety Stripes

* f. Cowling____________________________________________ Damage/Condition/Security

* g. Exhaust Stack and fairing______________________________ Condition/Security/Clear of obstruction and cracks.

* h. Brake Fluid Reservoir_________________________________ Quantity and Cap Security

Refer to Figure 7 for NACWS Antenna location

* i. NACWS Antenna, Upper_______________________________ Damage / Condition/Security / Antenna Cable

Attachment

8. Nose Area:

* a. Propeller____________________________________________ Damage/Condition/Security

1. Propeller Retaining Bolts (8)__________________________ Security/Safety Wire Intact

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

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8. Nose Area (Continued)

* b. Spinner and Screws___________________________________ Damage/Condition/Security

* c. Intake Ducts_________________________________________ Clear of obstruction

* d. Wheel Wells and Doors________________________________ Damage/Condition/Security

Nose Landing Gear Strut extension is minimum 5 inches

* e. Landing Gear Shock Strut______________________________ Clean/Extension

f. Torque Knees________________________________________ Damage/Condition/Security

* g. Tire and Wheel_______________________________________ Damage/Wear/Slippage Marks / Cotter Pin

Nose Landing Gear Tire pressure is 70 psi plus or minus 2 psi.

h. Tire________________________________________________ Check Tire Pressure

* i. Shimmy Dampener____________________________________ Condition/Security/Fluid Leakage

* j. Ground Blower Inlet___________________________________ Condition/Security

The side and lower aft right hand portion of the “V” Brace in and around the area where the preservative filler is located shall be visually inspected for cracks and signs of leakage/weeping.

* k. Nose Landing Gear “V” Brace___________________________ Condition/Security

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

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WORK AREA WUC ITEM TASK DESCRIPTION/REQUIREMENT HYD PWR

9. Right Side Engine:

Open both left and right hand aft cowl doors and reach inside the upper forward cowling and physically lift the aft corners of the upper forward cowling to determine it is secure. Ensure all four latch pins are flush.

* a. Right Side Engine Compartment_________________________ FOD Free

* b. Exhaust Stack and Fairing______________________________ Condition/Security/ Clear of obstructions and cracks.

* c. Engine and Accessories________________________________ Damage/Condition/Security /Leakage/Chafing

* d. Engine Intake and Plenum______________________________ Clear of obstructions

* e. Air Inlet Bypass Door_________________________________ Condition/Security

* f. Cowling____________________________________________ Secured

* g. Manifold Drain______________________________________ Leakage

* h. Battery / Tray Pin and Vent Tube________________________ Condition/Security/Leakage

10. Right Hand Wing, Landing Gear and Wheel Well:

Inspect Aileron for freedom of movement. Inspect flap and aileron attaching hardware including the bonding wire for security and “safety” of locking devices

* a. Flaps_______________________________________________ Damage/Condition/Security

* b. Aileron (Including Tabs)_______________________________ Damage/Condition/Security

* c. Static Wicks_________________________________________ Damage/Condition/Security

* d. Wing Skin__________________________________________ Damage

* e. Wing Tip ___________________________________________ Damage/Security

* f. Navigation/Strobe Light lenses___________________________ Cracks/Distortion/Security

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

ELEC PWR

OFF

WORK AREA WUC ITEM TASK DESCRIPTION/REQUIREMENT HYD PWR

10. Right Hand Wing, Main Landing Gear and Wheel Well (Continued):

Visually check fuel level through filler neck. During Daily Inspection ensure visual fuel level corresponds with indicated fuel quantity. Ensure the fuel cap is properly secured and aligned with arrow.

* g. Fuel:

1. Fuel______________________________________________ Leakage/Visual Quantity

2. Fuel Anti-Siphon Valve/Gasket________________________ Damage/Condition/Security

3. Fuel Cap__________________________________________ Damage/Condition

Check to ensure presence of corrosion preventative compound (CPC) on flight control cables in the right-hand wheel well area.

* h. Landing Gear Light___________________________________ Damage/Condition/Security

Main Landing Gear Strut extension is minimum 3 inches

* i. Landing Gear Shock Strut______________________________ Clean/Extension

* j. Torque Knees________________________________________ Damage/Condition/Security

* k. Brake and Brake Lines________________________________ Wear/Leakage

* l. Brake Bolts__________________________________________ Safety Wired

* m. Tire and Wheel______________________________________ Damage/Wear/Slippage Marks

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

ELEC PWR

OFF

WORK AREA WUC ITEM TASK DESCRIPTION/REQUIREMENT HYD PWR

10. Right Hand Wing, Main Landing Gear and Wheel Well (Continued):

Main Landing Gear Tire pressure is 90 psi plus or minus 2 psi.

n. Tire________________________________________________ Check Tire Pressure

* o. Wheel Retaining Nut__________________________________ Nut Cotter Keyed

* p. Wheel Well and Doors_________________________________ Damage/Condition/Security

Do not pull on the down lock assembly, serious injury will occur

* q. Down Lock Block Assembly (Including Cables)_____________ Damage/Condition/Security

* r. Fuel Vents___________________________________________ Clear of Obstructions

11. Fuselage, Right Side:

* a. Skin________________________________________________ Damage

b. Static Port___________________________________________ Clear of Obstructions

c. Oxygen Blow-Out Plug_________________________________ Intact

* d. Canopy N2 Bottle Pressure ______________________________ Needle in Green Band vs. Ambient Air Temperature

12. Empennage:

Refer to Figure 7 for Empennage Antenna location

* a. Antennas____________________________________________ Damage/Condition/Security

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

ELEC PWR

ON

WORK AREA WUC ITEM TASK DESCRIPTION/REQUIREMENT HYD PWR

12. Empennage (Continued):

Inspect Rudder and Elevator for freedom of movement and attaching hardware including the bonding wires for security and “safety” of locking devices “as visible from the ground”

* b. Vertical Stabilizer (Including Rudder and Tab)______________ Damage/Condition/Security

* c. Horizontal Stabilizer (Including Elevator and Tabs)__________ Damage/Condition/Security

* d. Static Wicks_________________________________________ Damage/Condition/Security

e. Aft Navigation and Strobe Light__________________________ Damage

* f. Tail Skid____________________________________________ Damage/Condition/Security

13. Fuselage, Left Side:

* a. Skin________________________________________________ Damage

b. Static Port___________________________________________ Clear of Obstructions

Ensure Safety pin for Canopy emergency Blow-back System N2 Bottle is not installed.

* c. Avionics Equipment___________________________________ Secure

Check avionics bay for pooled water or excessive moisture. Document discrepancies, notify maintenance control

* d. Avionics Bay________________________________________ FOD/Water Intrusion/Condition/Security

* e. Avionics Bay Door___________________________________ Secure/Latched

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

ELEC PWR

OFF

WORK AREA WUC ITEM TASK DESCRIPTION/REQUIREMENT HYD PWR

N/A

14. Fuselage, Underside:

* a. Skin_______________________________________________ Damage

Refer to Figure 7 for Fuselage Antennas location

* b. Antennas___________________________________________ Damage/Condition/Security

c. Air Scoop___________________________________________ Clear of Obstruction

d. Fuel Vent___________________________________________ Clear of Obstruction/Secured

15. Exterior light / Flap Operation Check:

* a. Battery_____________________________________________ On/Check Voltage

* b. Exterior Lights (All)__________________________________ On/Operation/Off

Ensure flaps are clear. Observe flap movement corresponding with the flap indicator

* c. Flaps______________________________________________ Full Up

* d. Battery_____________________________________________ Off

16. Securing of Aircraft, Following the Last Flight of the Day (Optional):

Installation of canopy covers subject to local policy.

a. Protective Covers_____________________________________ As Required

b. Propeller Restraints___________________________________ Installed As Required

DATE

August 1, 2013

CHANGE #

CARD NUMBER: NAVAIR (PMA 273) 01-50-T34C-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

ELEC PWR

OFF

WORK AREA WUC ITEM TASK DESCRIPTION/REQUIREMENT HYD PWR

N/A

16. Securing of Aircraft, Following the Last Flight of the Day (Optional):

c. Control Locks________________________________________ Installed/Pedals Adjusted Forward

d. Tie Downs___________________________________________ As Required

Possible system leakage can occur when parking brake is set for extended period. Release parking brake if aircraft is chocked.

e. Chocks______________________________________________ In Place

f. Parking Brake_________________________________________ Released

g. Canopy______________________________________________ Closed

END OF REQUIREMENTS