ATT 79 01-50-T44A-600-6-1.pdf

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T-34/T-44/T-6 Aircraft Maintenance and Contractor Logistics Support
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NAVAIR (PMA 273) 01-50-T44A-600-6-1

U.S. NAVY T-44A

PEGASUS

DAILY TURNAROUND

MAINTENANCE

REQUIREMENTS

NAVAIR (PMA 273) 01-50-T44A-600-6-1

January 1, 2013

ATTACHMENT 79

NAVAIR (PMA-273) 01-50-T44A-600-6-1 N61340-18-FOSR-0001

MAINTENANCE REQUIREMENTS CARD

CARD NUMBER

i

DATE

January 1, 2013

CHANGE #

Reissued

CARD NUMBER: NAVAIR (PMA 273) 01-50-T44A-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

WORK AREA TASK DESCRIPTION/REQUIREMENT

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 first flight of the day and are valid for seventy-two (72) hours provided the aircraft has not been flown during that period of time.

The Turnaround Inspection is accomplished prior to the first flight of the day, as part of the Daily Inspection, and between flights on the same day. An asterisk in front of those items requiring inspection indicates the Turnaround Inspection requirements.

A Turnaround Inspection must be accomplished on aircraft that have had a valid Daily Inspection completed but have not been flown and 24 or more but less then 72 clock hours have transpired since the last Daily Inspection was completed.

CAUTION

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

THINK SAFETY

ii

DATE

January 1, 2013

CHANGE

Original

CARD NUMBER: NAVAIR (PMA 273) 01-50-T44A-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

WORK AREA TASK DESCRIPTION/REQUIREMENT

Change Summary:

Card Number Date Revision i January 1, 2013 Original ii January 1, 2013 Original

1 January 1, 2013 Original

2 January 1, 2013 Original

3 January 1, 2013 Original

4 January 1, 2013 Original

5 January 1, 2013 Original

6 January 1, 2013 Original

7 January 1, 2013 Original

8 January 1, 2013 Original

DATE

January 1, 2013

CHANGE

Original

CARD NUMBER: NAVAIR (PMA 273) 01-50-T44A-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

WORK AREA TASK DESCRIPTION/REQUIREMENT

1. Fuel Samples Obtain/Inspect.

Note 1: Aircraft shall not have been operated or refueled within thirty (30) minutes.

Note 2: 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.

2. Remove All Protective Covers Check.

3. Cockpit/Cabin:

a. *Equipment Switches Off/Positioned.

b. Battery Voltage Checked - 20-VDC Minimum.

c. Interior Lights (All) Check On/Off.

d. Fire Warning System Test All Three Positions Both Engines.

e. Battery Switch Off.

f. Stall Warning Switch Off.

g. Stall Warning Heat Switch Off.

h. Standby Gyro Battery Switch Off.

i. Control Lock Stowed.

j. Flight Controls Free Movement.

k. Cockpit/Cabin Interior Cleanliness.

l. *Windshield/Side Windows Damage/Cleanliness.

DATE

January 1, 2013

CHANGE

Original

CARD NUMBER: NAVAIR (PMA 273) 01-50-T44A-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

WORK AREA TASK DESCRIPTION/REQUIREMENT

3. Cockpit/Cabin (Continued):

m. Windshield Wipers Condition.

n. Fire Extinguishers Secured.

o. Seat Belts/Harnesses Condition/Security.

p. Emergency Landing Gear Extension Handle Stowed.

q. First Aid Kit Secured/Seal Intact

r. Relief Tube Stowed.

s. Emergency Exit Door Secured.

t. Air Crew Life Support Equipment Verify Expiration Date.

u. Door Dampener Condition/Operation.

v. Door Steps Operation.

w. *Air stair Door Seal/Wire Bundle Condition.

x. *Air stair Door Latch Mechanism Condition/Operation.

4. Left Wing, Landing Gear and Wheel Wells:

a. *Flaps (Lowered) Damage/Condition/Security.

b. *Aileron Damage/Condition/Security.

c. *Skin Damage.

d. *Wing Tip Damage.

e. *Deicer Boot Damage.

f. Lift Transducer Condition/Security.

g. *Fuel Leakage/Quantity.

DATE

January 1, 2013

CHANGE

Original

CARD NUMBER: NAVAIR (PMA 273) 01-50-T44A-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

WORK AREA TASK DESCRIPTION/REQUIREMENT

4. Left Wing, Landing Gear and Wheel Wells (Continued):

h. Shock Strut Clean/Extension (3.0 inches). Verify

Condition Of All Attaching Hardware.

i. *Wheel Damage.

j. *Brake and Lines Wear/Leakage.

k. *Tire _________________________________Wear/Inflation (Check for proper inflation using a

Certified Tire Gauge. Proper inflation is 54 to 60

PSI.)

l. *Wheel Well and Doors Damage/Security.

m. Fire Bottle Correct Charge.

n. Fuel Vents Clear.

5. Left Side No. 1 Engine:

a. *Oil Tank Quantity.

b. Engine/Accessories Condition/Leakage/Damage.

c. Engine Intake Screen Clear.

d. *Exhaust Stacks Secure/Clear.

6. L/H Propeller Area:

a. *Propeller Damage.

b. *Prop De-ice Boots Damage/Security.

c. *Spinner Damage/Security.

d. *Intake Ducts Clear.

e. *Lip De-Ice Boot Condition.

f. Ice Vane Condition/Security.

DATE

January 1, 2013

CHANGE

Original

CARD NUMBER: NAVAIR (PMA 273) 01-50-T44A-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

WORK AREA TASK DESCRIPTION/REQUIREMENT

7. Right Side No. 1 Engine:

a. *Exhaust Stack Secure & Clear.

b. Engine & Accessories Condition/Leakage/Damage

c. Engine Intake Screen Clear.

d. Cowling Secured.

e. Wash Ring Provisions Secured.

f. Manifold Drain Leakage.

g. Bleed Air Intercooler Duct Obstruction.

8. Nose Area:

a. Avionics Equipment Bay Secure.

b. Standby Gyro Battery Perform Test Function To Determine Battery Condition

c. *Avionics Bay Door (LH) Secured.

d. Ram Air Duct Obstruction.

e. Condenser Air Outlet Obstruction.

f. Pitot Tubes Clear.

g. *Radome Condition/Damage

h. *Wheel Well and Doors Damage/Security.

i. Shock Strut Clean/Extension (3.0 - 3.5 inch).

j. Shimmy Dampener Condition/Security.

k. *Tire _________________________________Wear/Inflation (Check for proper inflation using a

Certified Tire Gauge. Proper inflation is 50 to 55 PSI.)

DATE

January 1, 2013

CHANGE

Original

CARD NUMBER: NAVAIR (PMA 273) 01-50-T44A-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

WORK AREA TASK DESCRIPTION/REQUIREMENT

8. Nose Area (Continued):

l. Landing and Taxi Lights Cleanliness/Damage.

m. Condenser Air Inlet Obstruction.

n. *Avionics Bay Door (RH) Secured.

9. Left Side No. 2 Engine:

a. Bleed Air Intercooler Duct Obstruction.

b. Battery Compartment Cover Security.

c. *Oil Tank Quantity.

d. Engine & Accessories Condition/Leakage/Damage.

e. Engine Intake Screen Clear.

f. *Exhaust Stacks Secure & Clear.

10. R/H Propeller Area:

a. *Propeller Damage.

b. *Prop De-ice Boots Damage.

c. *Spinner Damage/Security.

d. *Intake Ducts Clear.

e. *Lip De-Ice Boot Condition.

f. Ice Vane Condition/Security.

11. Right Side No. 2 Engine.

a. *Exhaust Stack Secure & Clear.

b. Engine & Accessories Condition/Leakage/Damage.

DATE

January 1, 2013

CHANGE

Original

CARD NUMBER: NAVAIR (PMA 273) 01-50-T44A-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

WORK AREA TASK DESCRIPTION/REQUIREMENT

11. Right Side No. 2 Engine (Continued).

c. Engine Intake Screen Clear.

d. *Cowling Secured.

e. Wash Ring Provisions Secured.

f. *Manifold Drain Leakage.

12. Right Wing, Landing Gear and Wheel Well:

a. *Flaps (Lowered) Damage/Condition/Security.

b. *Aileron Damage/Condition/Security.

c. *Skin Damage.

d. *Wing Tip Damage.

e. *Deicer Boot Damage.

f. *Fuel Leakage/Quantity.

g. Shock Strut Clean/Extension (3.0 inches). Verify Condition

Of All Attaching Hardware.

h. *Wheel Damage.

i. *Brake and Lines Wear/Leakage.

j. *Tire Wear/Inflation (Check for proper

Inflation using a Certified Tire Gauge.

Proper inflation is 54 to 60 PSI.)

k. *Wheel Well & Doors Damage/Security.

l. Fire Bottle Correct Charge.

m. Fuel Vents Clear.

DATE

January 1, 2013

CHANGE

Original

CARD NUMBER: NAVAIR (PMA 273) 01-50-T44A-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

WORK AREA TASK DESCRIPTION/REQUIREMENT

12. Fuselage, Right Side:

a. *Skin Damage.

b. Static Ports Clear.

c. *Oxygen Quantity (1,000 PSI Local, 1,500 PSI When

Cross Country).

d. Aft Fuselage Compartment Condition/Security.

e. *ELT Switch Armed Position.

f. *Aft Fuselage Compartment Door Secured.

14. Empennage:

a. Antennas Security.

b. *Control Surfaces Damage/Condition/Security.

c. Taillight Damage.

d. Strobe Beacon Damage.

15. Fuselage, Left Side:

a. *Skin Damage.

b. Static Ports Clear.

16. Fuselage, Underside:

a. *Skin Damage.

b. Antennas Damage/Security.

c. Strobe Beacon Damage.

DATE

January 1, 2013

CHANGE

Original

CARD NUMBER: NAVAIR (PMA 273) 01-50-T44A-600-6-1

TITLE: DAILY/TURNAROUND INSPECTION CHECKLIST

WORK AREA TASK DESCRIPTION/REQUIREMENT

17. Last Flight of the Day:

a. Protective Covers As Required.

b. Prop Restraints As Required.

18. Last Flight of the Day (Continued):

c. Tie Downs As Required.

d. Cabin Door Closed.

e. Storm Windows Closed.

f. Control Locks Installed.

g. Chocks In Place.

h. Parking Brake Released.

Note: If no wheel chocks and/or tie downs are immediately available or heavy weather is expected, SET the Parking Brake.

No Further Entries On This Card/End Of Card Set

DATE
CARD NUMBER
January 1, 2013
CHANGE #
TASK DESCRIPTION/REQUIREMENT
INTRODUCTION
APPLICATION
CAUTION
THINK SAFETY

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