ATTACHMENT_80_-_PWS_Encl_13_T44A_01-50-T44A-600-6-4-2.pdf

NAVAIR (PMA 273) 01-50-T44A-600-6-4.2

U.S. NAVY T-44A

PEGASUS

2nd DETAILED

INSPECTION

January 1, 2013

ATTACHMENT 80

PWS Encl 13 T44A 01-50-T44A-600-6-4-2 N00019-14-R-0018

PAGE EFFECTIVITY LISTING

Summary:

• The original issue of the NAVAIR (PMA 273) 01-50-T44A-600-6-4.2 is dated November 1, 2005.

• The date of this change, which is a complete reissue, is January 1, 2013.

Page (s) Change Number Date Comments Cover NA 1/1/2013 Changes Not Bar Marked i NA 1/1/2013 Changes Not Bar Marked ii NA 1/1/2013 Changes Not Bar Marked iii NA 1/1/2013 Changes Not Bar Marked iv NA 1/1/2013 Changes Not Bar Marked 1 NA 1/1/2013 Changes Not Bar Marked 2 NA 1/1/2013 Changes Not Bar Marked 3 NA 1/1/2013 Changes Not Bar Marked 4 NA 1/1/2013 Changes Not Bar Marked 5 NA 1/1/2013 Changes Not Bar Marked 6 NA 1/1/2013 Changes Not Bar Marked 7 NA 1/1/2013 Changes Not Bar Marked 8 NA 1/1/2013 Changes Not Bar Marked 9 NA 1/1/2013 Changes Not Bar Marked 10 NA 1/1/2013 Changes Not Bar Marked 11 NA 1/1/2013 Changes Not Bar Marked 12 NA 1/1/2013 Changes Not Bar Marked 13 NA 1/1/2013 Changes Not Bar Marked 14 NA 1/1/2013 Changes Not Bar Marked 15 NA 1/1/2013 Changes Not Bar Marked 16 NA 1/1/2013 Changes Not Bar Marked 17 NA 1/1/2013 Changes Not Bar Marked 18 NA 1/1/2013 Changes Not Bar Marked 19 NA 1/1/2013 Changes Not Bar Marked 20 NA 1/1/2013 Changes Not Bar Marked 21 NA 1/1/2013 Changes Not Bar Marked

21.1 NA 1/1/2013 Changes Not Bar Marked

22 NA 1/1/2013 Changes Not Bar Marked 23 NA 1/1/2013 Changes Not Bar Marked

Interim Change Notice information and entry requirements:

Interim Change Notices (ICNs) can be either issued in hard copy, navy message format or via E-Mail. Each ICN will have a unique serial number assigned for tracking purposes.

When an ICN is received/issued holders of the Scheduled Inspection Requirements Guide (SIRG) will be required to enter the data in the above log in the appropriate section of the manual that it applies to; i.e., the NAVAIR (PMA-273) 01-50-T44A-600-6, -600-6-4.1, –600-6-

4.2 or the Corrosion Control Manual.

NOTE: Changes to the Daily/Turnaround and the Seven Day Inspection MRCs will be annotated on Page ii of the applicable MRC package.

Entry information requirements in the above ICN Log are self-explanatory. All ICNs will be incorporated into the appropriate portion of the SIRG package when a formal change is to the document is issued.

Copies of ICNs shall be posted to the applicable document immediately behind the title/cover page and a notation shall be made in the appropriate/referenced area of the affected document to alert the user to the ICN that has modified or amended the requirements.

INTERIM CHANGE NOTICE (ICN) LOG

ICN Number Page/Section/Item Date Comments/Information

TECHNICAL INFORMATION REPORT, DISCRPANCY (TIRD)

CHANGE RECOMMENDATION

(TO BE FILLED IN BY ORIGINATOR)

REPORT DATE: __________________________________

FROM (Originator): ________________________________ ACTIVITY: ________________________________________

ADDRESS AND/OR E-MAIL OF ORIGINATOR:________________________________________________________________

SEND COMPLETED FORM TO:

NAVAIRSYSCOM

ATTENTION: PMA-273, T-34 OR T-44 APMSE

22581 SAUFLEY ROAD, BUILDING 3258

PATUXENT RIVER, MARYLAND 20670

NAME/P/N OF MANUAL CHANGE # CHANGE DATE PAGE/SECTION/PARAGRAPH

DEFICIENCY: ____________________________________________________________________________________________

RECOMMENDATION (Be Specific): __________________________________________________________________________

_________________________________________________________________________ Check if continuation sheets or drawings attached.

IMPACT: _________________________________________________________________________________________________

REPORT BY: _____________________________________________

SIGNATURE:_____________________________________________ TITLE:________________________________________

TO BE FILLED IN BY PMA-273

FROM: __________________________________________________ DATE: ________________________________________

TO: _____________________________________________________

REFERENCE:_______________________________________________________________________________________________

Your change recommendation has been received and is currently in review for possible incorporation.

INSTRUCTIONS FOR COMPLETING THE TIRD

1. REPORT DATE: This identifies the year, month, and day that the report was prepared and consists of six digits, e.g., 050115. The first two digits indicate the year, the second two digits indicate the month, and the remaining two digits specify the day.

2. FROM: The reporting activity originating change request. Address and/or e-mail address should be provided.

3. ACTIVITY: The activity reporting the discrepancy, e.g., contractor, NAS Corpus Christi, TX.

4. TECHNICAL MANUAL: Give the complete number assigned to the manual being reported as deficient.

5. CHANGE NUMBER: This appears on the area/page on which the deficiency is located.

6. CHANGE DATE: This appears on the area/page on which the deficiency is located.

7. SECTION/PAGE: Enter the number of the pages of the technical manual on which the deficiency is located.

8. PARAGRAPH: Enter the specific number in which the deficiency is located.

9. DEFICIENCY: Be very specific. Provide complete information regarding discrepancy, including drawings, schematics, sketches, and references. If necessary, attach copies of any reference data.

10. RECOMMENDATION: Be very specific. Provide complete information regarding the corrective action required, including drawings, schematics, sketches, and references. If necessary, attach additional pages.

11. IMPACT: Enter concise statement of the impact of this discrepancy on work load/operational readiness.

12. REPORTED BY: Name and position of person that prepared the TIRD.

SECOND 100-HUNDRED HOUR INTERVAL DETAILED INSPECTION

FORMS REQUIRED: The following forms are required to accommodate the requirements:

• Second 100-Hour Detailed Inspection

• Power Assurance Run Work Sheet

• Continuous Inspection Work Sheet

• VIDS/MAF (OPNAV Form 4790/60)

REFERENCE MATERIAL: The following technical manuals/data may be required to accommodate the requirements:

• BEECHCRAFT Model H90 (T-44A) Maintenance Manual, Part Number 92-38879

• BEECHCRAFT Model H90 (T-44A) Wiring Diagram Manual, Part Number 92-38028

• Pratt & Whitney PT6A-34B Engine Maintenance Manual, Part Number 3021242

• NAVAIR 01-T44AAA-1, NATOPS Manual

• Maintenance Engineering Directives (MED)

• Local Engineering Specification (LES)

INSPECTION PROCEDURES: The following ground rules are to be adhered to by personnel directly involved with the requirements specified for the inspection:

• The Engine Wash and Power Assurance Run (PAR) are to be performed immediately after completion of Detailed Inspection. The PAR Sheet and the associated Sign- Off sheet are contained in the back of this package.

• Fill out heading on each form in its entirety.

• Each item on the inspection form is to be checked/initialed on the form in the spaces provided.

• List all discrepancies found during the inspection on the Continuous Inspection Work Sheet.

• Initiate VIDS/MAFs (OPNAV Form 4790/60) for all discrepancies requiring replacement of repairable components and all discrepancies that are deferred/not completed as part of the inspection.

• Each discrepancy is to be signed off when the discrepancy has been corrected.

• When the inspection has been completed, the Supervisor will sign the “INSPECTION COMPLETED” block at the end of the inspection sheet.

NOTE: In case of conflict, the lubrication data contained in the attached lubrication charts/tables takes precedence over and supercedes the data contained in Section 12-00-00 of the T-44A Maintenance Manual.

NAVAIR (PMA 273) 01 -50-T44A-600-6-4.2

T-44A CONTINUOUS INSPECTION REQUIREMENTS

SECOND 100 HOUR INTERVAL INSPECTION REQUIREMENTS

Inspection Date: _________________________ JCN: ____________________ BUNO: ________________________

Aircraft Time: _________________________ Landings: _________________ Engine Time L/H ______ R/H _____

A. GENERAL AIRCRAFT INTERIOR CORRECTED

BY

INSPECTED

BY

1. Remove life raft, seats, and floorboards.

2. Inspect for, document and correct any corrosion that is detected in the sub floor area.

3. Inspect for and remove any fungus growth detected in the sub floor area.

NOTE

Reinstallation of the floorboards, seats and life raft is contained in Section E of this document.

B. PILOT’S COMPARTMENT CORRECTED

BY

INSPECTED

BY

1. CABLES AND PULLEYS – Check control cables, pulleys and associated equipment for condition, attachment, alignment, clearance, and proper operation.

2. BRAKE SYSTEM – Perform the following:

2.1 Check brake system components for leakage.

2.2 Inspect brake master cylinder for proper operation.

2.3 Check brake line plumbing for condition and attachment.

2.4 Check brake pedals and linkage for condition, attachment and proper operation.

2.5 Check for proper pedal travel and parking brake release.

3. RUDDER PEDALS – Check rudder pedal condition, clearance and attachment.

Visually inspect the rudder pedal bellcrank support beams, (P/N 109-420042-xx) left and right hand for cracks at the mounting holes.

4. INSTRUMENT PLUMBING AND WIRING – Inspect instrument panel, sub-panels, placards, shock mounts, instruments and instrument plumbing, and wiring for condition, attachment, chafing, etc.

5. CONTROL COLUMN – Check condition, attachment and operation. Check flight control lock for condition, positive locking, and alignment.

6. HEATER – Check cabin heat shut-off valve and defroster valve for proper operation. Check all ducts for condition IAW MED -19 Rev A. Check bleed air ducts for condition, insulation and adequate clearance of electrical wiring.

7. ELECTRICAL EQUIPMENT – Check switches, knobs and circuit breakers for looseness and operation. Check generator control boxes for condition and attachment. Check all wiring and equipment for condition, attachment, chafing, security, etc.

B. PILOT’S COMPARTMENT (Continued) CORRECTED

BY

INSPECTED

BY

8. EMERGENCY STATIC AIR SOURCE – Check for security.

9. ENGINE AND PROPELLER CONTROLS – Check for freedom of movement, full travel and proper friction lock operation.

10. SEATS AND SEAT BELTS – Inspect seats for proper operation and security, determine seat belts are satisfactory and inspect seat tracks for wear. Refer to Chapter 25-10-00 in BEECHCRAFT Model H90 (Navy T-44A) Maintenance Manual.

11. WINDOWS – Inspect windows and associated seals for general condition. Refer to Chapter 56-00-00 in BEECHCRAFT Model H90 (Navy T-44A) Maintenance Manual for permissible window damage.

12 WINDSHIELD - Check for proper heating as specified in Chapter 56-10-00 in

13. STATIC LINE – Open drain and remove moisture.

14. ACCESS DOORS - Check for fit and attachment after installation.

15. CONDITION LEVERS – Inspect condition of fuel cut-off stops.

16. FLAPS - Check that flaps operate to a selected position, indicator reading is proper and handle guide secure.

C. LANDING GEAR/WHEELS AND TIRES

CORRECTED

BY

INSPECTED

BY

L/H R/H L/H R/H

NOTE

Raytheon Aircraft Safety Communiqué Number 239 dated November 2003, which pertains to the main landing gear wheels, provides additional/alternate means for aligning the slot in the castellated nut and the cotter pin hole in the axle to preclude exceeding the maximum torque. In the case of the T-44A that torque is, 120-inch pounds of torque. If the castellated nut and the cotter pin hole can’t be aligned within the specified torque range, remove and replace the axle nut or add an additional adjusting washer P/N NAS1149C1616R, NAS1149F1616P or NAS1149G1616P and re-torque in accordance with the current established guidelines.

1. WHEELS AND TIRES – Check wheels for condition and tires for wear, condition, and proper inflation. (54-60psi) Inflator Kit # ________ Inflator Cal Date # ________ Final Tire Pressure Left ________ Final Tire Pressure Right ________

2. Clean, inspect and/or replace and lubricate the MLG wheel bearings with SHC 100 Mobil Aviation Synthetic Grease. Torque the retainer nut while the wheel is being rotated clockwise to 200-inch pounds to seat the bearings. Back off the torque to zero and re-torque to 60 to 120-inch pounds. Reference MED-106.

Torque Wrench # ___________________ Cal. Date: __________________ Final Torque L/H _____________________ Final Torque R/H _____________

3. Check torque plate mounting bolts for proper torque (130-150 in/lbs).

Torque Wrench # ____________________ Cal Date: ____________________

Torque L/H _________________________ Torque R/H _________________

C. LANDING GEAR/WHEELS AND TIRES (Continued)

CORRECTED

BY

INSPECTED

BY

4. NOSE WHEEL AND TIRE – Check wheel for condition and tire for wear, condition and proper inflation.(50-55psi)

Inflator kit # ________ Inflator Cal Date ________ Final Tire Pressure ________

5. Clean, inspect and/or replace and lubricate the NLG wheel bearings with SHC 100 Mobil Aviation Synthetic Grease. Torque the retainer nut while the wheel is being rotated clockwise to 200-inch pounds to seat the bearings. Back off the torque to zero and re-torque to 30 to 100-inch pounds. Reference MED-106.

Torque Wrench #__________________ Cal. Date: ____________________

Final Torque ______________________

6. NOSE GEAR RETRACT CHAIN – Inspect links for corrosion, dirt and rust. Inspect, clean or lubricate as necessary as outlined in Chapter 32-30-00 of the BEECHCRAFT Model H90 (Navy T-44A) Maintenance Manual.

CAUTION

Since battery voltage is not sufficient to properly cycle the landing gear, use only an external power source capable of delivering and maintaining 28.5 + .25 volts throughout the extension and retraction cycles when performing the landing gear retraction inspection. Jack the aircraft before starting the landing gear retraction inspection.

7. LANDING GEAR GEARBOX AND MOTOR – Inspect for condition, attachment and leakage. Lubricate as necessary.

8. LANDING GEAR TORQUE SHAFTS - Inspect shafts and universal joints inside pressure vessel for condition, attachment and visible damage.

9. POSITION INDICATORS – Check for proper indication.

10. WARNING HORN - Check for proper operation.

11. LIMIT SWITCHES - Check for proper adjustment and attachment. Lube with LPS-1.

CAUTION

DO NOT CONTINUE OPERATION AFTER RECEIVING A GEAR-DOWN INDICATION. FURTHER MOVEMENT OF

THE HANDLE COULD DAMAGE THE DRIVE MECHANISM AND PREVENT SUBSEQUENT ELECTRICAL GEAR

RETRACTION. THE LANDING GEAR CANNOT BE RETRACTED MANUALLY.

12. EMERGENCY EXTENSION – Check system for freedom of operation and positive engagement of down-locks.

13. RETRACT MECHANISM – Check retraction system for proper operation of all components inside pressure vessel through at least two complete cycles. Check for unusual noises and evidence of binding.

D. CABIN SECTION

CORRECTED

BY

INSPECTED

BY

1. SKIN - Inspect visible internal skin for condition and loose or missing rivets. If damage is found, check adjacent structure.

2. STRUCTURE - Check for cracks, loose or missing rivets and concealed damage. Check pressure seals for condition and attachment.

3. CABLES AND PULLEYS- Check control cables, pulleys and associated equipment for condition, attachment, alignment, clearance and proper operation.

4. FLAP MOTOR AND DRIVES – Inspect for condition and attachment and lubricate as necessary.

5. AILERON QUADRANT – Check for security, attachment, operation and proper travel.

6. WINDOWS – Inspect windows and window seals for general condition. Refer to Chapter 56- 00-00 in BEECHCRAFT Model H90 (Navy T-44A) Maintenance Manual for permissible window damage.

7. EMERGENCY EXIT DOOR – Inspect door, seal, and latching mechanism for condition and security of attachment.

8. AIRSTAIR DOOR – Inspect cabin door hinge for cracks, corrosion. Apply torque to hinge by moving airstair door BY HAND to check for security of hinge. Looseness of hinge suggests oversized holes or cracks in hinge.

9. ELECTRICAL WIRING AND EQUIPMENT – Perform the following:

9.1 Check cabin and compartment lights for condition and attachment.

9.2 Inspect wiring and equipment for condition and attachment.

9.3 Check generator control boxes for condition and attachment.

9.4 Check the electrical panel under the aisle floorboards for chafing and security of attachment of all components.

9.5 Check cockpit observer audio control panel on right cabin wall for chafing and security of attachment of all components.

9.6 Check avionics fault insertion system on right armrest for chafing and security and attachment of all components.

10. HEATER DUCTS – Perform the following:

10.1 Check the cabin hot and cold air outlets and valves for condition, obstructions and proper

10.2 Inspect heating and cooling ducts for condition and attachment.

10.3 Check bleed air ducts for condition, insulation and adequate clearance from electrical wiring.

T-44A CONTINUOUS INSPECTION REQUIREMENT

D. CABIN SECTION (Continued)

CORRECTED

BY

INSPECTED

BY

11. PRESSURE REGULATOR, EJECTOR AND DEICER DISTRIBUTOR VALVE – Check equipment and plumbing for security and condition.

12. SEATS AND SEAT BELTS – Check seat and seat belts for condition and attachment. Inspect seat tracks for wear and condition refer to Chapter 25-20-00 in BEECHCRAFT Model H90

13. ACCESS DOORS – Check for fit and attachment after installation.

14. OUTFLOW VALVE VACUUM LINE – Open drain and remove moisture.

15. OUTFLOW AND SAFETY VALVES – Check for condition and attachment. Check safety valve screen for obstruction. Clean as outlined in Chapter 12-10-00 of BEECHCRAFT Model H90 (Navy T-44A) Maintenance Manual if required.

16. CONTROL CABLE SEALS – Check for condition, security and cleanliness.

17. BELLY DRAINS – Inspect for corrosion and possible obstruction(s).

18. AUTOPILOT – Check components for damaged cases, bent or broken pins on electrical connectors, damaged seals, poor soldering connections and damaged wiring.

19. OXYGEN MASK HOLDER – Inspect oxygen mask holder to insure proper attachment and

E. GENERAL AIRCRAFT INTERIOR FINAL

BY

INSPECTED

BY

1. Thoroughly clean and vacuum any dirt or loose objects from the sub floor are immediately prior to the reinstallation of the floorboards.

NOTE

A THOROUGH FOD INSPECTION SHALL BE PERFORMED OF THE SUB FLOOR AREA PRIOR TO PROCEEDING TO

THE NEXT STEP.

2. Reinstall floorboards, seats and life raft.

F. FIRE DETECTOR/SUPRESSION

CORRECTED

BY

INSPECTED

BY

1. FIRE DETECTORS – Check all detectors for sensitivity as outlined in MED 26-10-00/PR-56.

CAUTION

DISCONNECT THE GROUND AND POWER WIRES PRIOR TO TESTING THE FIRE EXTINGUISHING SYSTEM.

2. FIRE BOTTLE – Inspect the firing circuits for proper operation.

3. FIRE DETECTOR – Check control amplifier input circuits.

NAVAIR (PMA 273) 01 -50-T44A-600-6-4.2

January 1, 2013

G. NOSE SECTION

CORRECTED

BY

INSPECTED

BY

1. SKIN – Inspect skins and structure for condition and loose or missing rivets.

2. STRUCTURE – Check for cracks, loose rivets and concealed damage.

3. ELECTRICAL/ELECTRONIC EQUIPMENT – Inspect radio rack structure and security of units in their mounts.

4. BRAKE RESERVOIR – Inspect reservoir and fill as needed.

5. INSTRUMENT AIR FILTER – Inspect for condition. Replace every 500 hours or sooner if conditions warrant; e.g., operation in heavy smoke and/or dust.

6. VACUUM REGULATOR VALVE FILTER – Replace or clean in accordance with, Chapter 37-00-00, BEECHCRAFT Model H90 (Navy T-44A) Maintenance Manual.

H. FORWARD SPARS CORRECTED

BY

INSPECTED

BY

1. FORWARD WING SPARS - Thoroughly inspect the upper and lower spar caps and hinge lobe areas for signs of buckling, loose or raised paint and other evidence of corrosion.

Using A strong light source, inspect visible internal structure of wing spar via already opened wing access panels for corrosion, i.e. grayish/white powder and or flaking substance on or around spar area.

2. FORWARD WING SPARS SEALENT- Thoroughly inspect the condition of the sealant used to seal the hinge lobe areas of both the upper and lower spar caps.

I. POWER PLANT

BY

INSPECTED

BY

L/H R/H L/H R/H

1. COWLING – Perform the following:

1.1 Check adjustment of all latches prior to removing cowling.

1.2 Remove upper cowling and clean.

1.3 Inspect removed cowling for cracks and repair as necessary.

2. ENGINE OIL FILTER – Remove and inspect for condition and foreign matter. Replace with clean filter received from supply. Torque to 32 – 36-inch pounds.

Torque Wrench #____________________ Cal Date ____________________________ Torque L/H ________________________ Torque R/H __________________________

3. CHIP DETECTOR – Inspect for metal accumulation prior to performing circuit test.

Reinstall and torque to 45 – 55-inch pounds.

Torque Wrench #____________________ Cal Date ____________________________ Torque L/H ________________________ Torque R/H __________________________

I. POWER PLANT (Continued)

CORRECTED

BY

INSPECTED

BY

L/H R/H L/H R/H

4. DRAIN PLUGS – Check all drain plugs for security.

5. OIL QUANTITY – Check oil level and service as required.

6. FUEL FILTERS AND SCREENS – Inspect all fuel filters and screens for evidence of foreign matter, corrosion or microbiological growth in the fuel system.

6.1 Firewall Filter – Check for foreign matter and condition. Replace with filter that has been ultrasonically cleaned. Torque the Air Maze type filter assembly to 80 – 180-inch pounds. Torque the Purolator type filter assembly to 30 – 50-inch pounds. Leak-check the filter assembly after installation using the electric boost pumps.

Torque Wrench #__________________ Cal Date ______________________

Torque L/H ____________________ Torque R/H ______________________

6.2 Fuel Pump Inlet Filter (Screen Filter) – Check for foreign matter or distortion.

Clean and reinstall or replace as necessary. Torque cap to 180 – 220-inch pounds.

Torque Wrench #__________________ Cal Date _________________________

Torque L/H _____________________ Torque R/H ________________________

6.3 Fuel Pump Outlet Filter (Paper Filter) – Check for condition and foreign matter.

Install new filter. Torque cover to 180 – 220-inch pounds.

7. IGNITER PLUGS – Inspect the igniter plugs as described in the P&WC Engine Maintenance Manual. Torque Igniters to 300 – 360-inch pounds.

8. OIL COOLER – Check the cooler and plumbing for condition, blockage of air passage and attachment.

9. ENGINE EXHAUST SYSTEM – Examine the exhaust section and visible portions of the power turbine for burning, distortion, damage and cracks. If any damage is noted, refer to the engine maintenance manual for corrective action.

10. INDUCTION SYSTEM – Check the air intake duct and engine inlet screen for obstructions and damage.

I. Power Plant (Continued)

CORRECTED

BY

INSPECTED

BY

L/H R/H L/H R/H

11. PLUMBING – Inspect plumbing and associated equipment and accessories for condition and attachment.

12. ENGINE AND PROPELLER CONTROLS – Check controls and associated equipment for condition, attachment and proper rigging.

13. ENGINE ACCESSORIES – Inspect all accessories for condition, attachment and leakage.

14. ENGINE MOUNTS – Inspect for condition and attachment. Replace the vibration isolator mount as required. All mounts on an aircraft must be of the same manufacturer. Refer to Chapter 71-20-00 in the BEECHCRAFT Model H90 (Navy T-44A) Maintenance Manual.

15. ELECTRICAL WIRING AND EQUIPMENT – Inspect wiring and associated equipment and accessories for condition and attachment.

16. STARTER GENERATOR – Perform the following:

16.1 Inspect one set of brushes for an indication of excessive wear or damage. Determine wear by observing the diagonal groove on the brush. Refer to Chapter 24-30-00 in the

16.2 Inspect inlet duct and blast cap for cracks or obstructions.

16.3 Inspect quick disconnect attachment flange.

17. FUEL CONTROL SENSE LINE HEATERS – Check operation and security of attachment.

18. INERTIAL ANTI-ICE – Check vane for freedom of movement and proper travel.

19. DEICER BOOTS – Check propeller and engine air inlet boots for condition and security of attachment. Check propeller deicer slip rings for gouges, cracks, burned or discolored areas and deposits of grease, oil or dirt. Clean contaminated slip rings.

20. REVERSING PROPELLER – Perform the following:

20.1 Check propellers for condition and attachment.

20.2 Check condition of the mechanical feedback ring, stop rods and springs.

20.3 Inspect the carbon block pin for freedom of movement. The end float can be observed without disassembly. Refer to Chapter 61-11-00 in the BEECHCRAFT Model H90

I. POWER PLANT (Continued)

CORRECTED

BY

INSPECTED

BY

L/H R/H L/H R/H

20.4 Check for no metal-to-metal contact between the brass ring and the reversing lever.

20.5 Check the reversing linkage for proper adjustment, static operation and evidence of binding and security of attachment.

21. PROPELLER SYNCHROPHASER – Perform the following:

21.1 Check drive unit for condition, security, wear, rigging and electrical connection.

21.2 Check flexible shaft and trimmer for security of attachment, wear and rigging.

21.3 Inspect rod end bearing for condition and lubrication.

21.4 Check for proper gap between sensors and slip rings.

22. AUTOFEATHER RELAYS, DUMP SOLENOIDS AND PRESSURE SWITCHES –

Check for condition, security of attachment and proper electrical connections.

23. AUTO-IGNITION PRESSURE SWITCHES – Check for condition, security of attachment and proper electrical connection.

24. FUEL DRAIN COLLECTOR SYSTEM (EPA PUMP) – Perform the following:

24.1 Check for security of attachment of tank and pump.

24.2 Check hoses for cracks, deterioration and proper attachment.

24.3 Inspect pump screen/filter for condition. Clean and/or replace as required.

24.4 Install screen/filter and reassemble and secure the assembly.

J. GENERAL SERVICE ITEMS CORRECTED

BY

INSPECTED

BY

1. CLEANING – Vacuum and clean aircraft interior. Clean windshields and windows.

NOTE

Aircraft are washed every fourteen (14) days IAW the provisions of the NAVAIR T-44A Corrosion Control Plan.

2. SERVICING – Aircraft and systems serviced in accordance with applicable technical data.

3. LUBRICATION – Aircraft lubricated as specified in the attached lubrication charts/tables.

K. ENGINE WASH AND POWER ASSURANCE RUN

CORRECTED

BY

INSPECTED

BY

L/H R/H L/H R/H

1. Check the physical condition and alignment of the wash rings and all associated plumbing.

2. Perform engine wash in accordance with the Pratt and Whitney Maintenance Manual.

3. During the engine rinse evolution visually check the spray ring for proper operation to ensure a good full spray pattern is being delivered to the engine and that none of the nozzles/orifices are clogged.

4. Perform Power Assurance Run and record the results on the form provided in the back of the Detail Inspection package.

5. Inspect engine after ground run. Check for oil and fuel leaks security, and attachment of external components.

6. Check engine oil level after ground run. Service as required.

7. Install all cowling removed during the phase inspection.

L. OPERATIONAL INSPECTION

CORRECTED

BY

INSPECTED

BY

1. PITOT HEAT – Check amperage drawn on ammeter and for proper heating at unit.

2. FUEL VENTS – Check for heat at vents.

3. FUEL CONTROL SENSE LINE HEATER – Check operation.

4. AOA TRANSDUCER – Check for operation and heating.

5. ALL LIGHTS – Check for operation and replace defective bulbs as required.

6. FUEL GAGES – Check operation.

7. FLAPS – Check for noisy or erratic operation.

8. Perform pre-start, engine start and ground run-up in accordance with the NAVAIR 01-T-

44AAA-1.

L. OPERATIONAL INSPECTION (Continued) CORRECTED

BY

INSPECTED

BY

9. ENGINE INERTIAL ANTI-ICE VANES – Check for proper operation and rigging.

10. PROP DEICER – Check for proper operation and cycling.

11. WINDSHIELD AND SURFACE DEICER – Check for proper operation and cycling.

12. STARTERS – Check for proper operation.

13. IGNITION – Check for light illumination.

14. INTERSTAGE TURBINE TEMPERATURE – Check for proper limits.

15. BOOST PUMPS, CROSSFEED VALVE AND FIREWALL SHUTOFF VALVES – Check for proper operation with the battery switch in the off position. If any unit fails to operate, check fuses located beneath battery box.

16. OIL – Check for proper pressure and temperature limits.

17. FUEL TRANSFER PUMPS – Check for operation.

18. GENERATOR – Check output.

19. VACUUM SYSTEM – Check for proper limits.

20. GYRO INSTRUMENTS – Check for erratic or noisy operation.

21. ENGINE AND PROPELLER CONTROLS – Check for proper adjustment and freedom of movement.

22. EMERGENCY BUSS- Check emergency bus fuel boost pumps, fuel crossfeed and fuel firewall shutoff valves. If any unit fails to operate, check fuses beneath battery box.

23. POWER CHECK – Check in accordance with the engine maintenance manual.

24. BRAKES, Toe and Parking – Check for proper travel, ease of operation and proper release of parking brake.

25. PRESSURIZATION SYSTEM – Check for proper operation.

L. OPERATIONAL INSPECTION (Continued) CORRECTED

BY

INSPECTED

BY

26. AIR CONDITIONING SYSTEM – Check for proper operation in manual heat, manual cool and automatic modes. Check operation of all outlets and ease of operation of all controls.

27. IDLE RPM – Check for correct rpm at high and low idle.

28. REVERSIG PROPELLER – Perform flight idle torque checks as indicated in Chapter 76- 00-00 in the BEECHCRAFT Model H90 (Navy T-44A) Maintenance Manual.

29. PROPELLER GOVERNOR – Check for proper governing operation, feathering and ease of control movement.

30. PROPELLER SYNCHROPHASER – Check for proper operation.

31. FUEL CROSSFEED VALVE – Check for proper operation.

32. OVER VOLTAGE RELAYS – Functionally test as specified in Chapter 24-30-00 in the BEECHCRAFT Model H-90 (Navy T-44A) Maintenance Manual.

33. CUT-OFF - Check for a clean shutdown and no dump valve discharge.

34. Inspect engine after ground run. Check for oil and fuel leaks security, and attachment of external components.

35. Check engine oil level after ground run. Service as required.

36. Install all cowling removed during the phase inspection.

M. CDI FINAL CORRECTED

BY

INSPECTED

BY

1. Comply with final closure inspection and FOD check.

N. SCHEDULE REMOVAL COMPONENT INVENTORY CORRECTED

BY

INSPECTED

BY

1. Comply with serial number verification sheet, Page 24.

NAVAIR (PMA 273) 01 -50-T44A-600-6-4.2

January 1, 2013

SECOND 100 HOUR DETAILED INSPECTION LUBRICATION CHART

RUDDER AND ELEVATOR TABS, AND WIPER ARMS

Index No Location Lubricant Interval Accomplished

By Inspected

By 1 Rudder Trim Tab

Tube VV-L-800 Oil 1/100 and 2/100 Detail

2 Rudder Trim Tab

Hinge

3 Elevator Trim Tab

Actuator (2 Places) MIL-G-23827 Grease 1/100 and 2/100 Detail

4 Elevator Trim Tab Control Tubes (4 Places)

VV-L-800 Oil 1/100 and 2/100 Detail

5 Elevator Trim Tab Hinges

VV-L-800 Oil 1/100 and 2/100 Detail

6 Windshield Wiper Hinges

3 4 5

NOTE: Index numbers may not match T-44A Maintenance Manual lube chart index numbers.

NOSE LANDING GEAR

Index

No Location Lubricant Interval Accomplished By

Inspected By

1 Door Hinges and Retract Linkage

VV-L-800 General Purpose Oil

1/100 and 2/100 Detail

2 Grease Fittings MIL-G-81322 Grease 1/100 and 2/100 Detail

3 Reserved

4 Nose Wheel Steering Mechanism

MIL-G-81322 Grease 1/100 and 2/100 Detail

5 Top Brace Assembly, Grease Fittings

Aeroshell Grease 17 (Do Not Substitute)

1/100 and 2/100 Detail

6 Grease Fittings MIL-G-81322 Grease 1/100 and 2/100 Detail

7 Drag Leg Stop Bolt Grease Fitting

MIL-G-81322 Grease 1/100 and 2/100 Detail

MAIN LANDING GEAR

Index No Location Lubricant Interval

Accomplished By

Inspected By

L/H R/H L/H R/H

1 Grease Fittings MIL-G-81322 Grease 1/100 and 2/100 Detail

2 Reserved

3 Retract Grease Fittings (10 Places) MIL-G-81322 Grease 1/100 and 2/100 Detail

Door Hinges and Retract Linkage (12 Places)

VV-L-800 General Purpose Oil 1/100 and 2/100 Detail

5 Yoke Assembly, Drag Brace M77 Graphite Paste 1/100 and 2/100 Detail

1 1 6

4 5

NOTE: Index numbers may not match T-44A Maintenance Manual lube chart index numbers.

NOTE: Index numbers may not match T-44A Maintenance Manual lube chart index numbers.

LANDING GEAR RETRACT SYSTEM

Index No Location Lubricant Interval Accomplished

By Inspected

By

1 Emergency Extension Mechanism

VV-L-800 General Purpose Oil 1/100 and 2/100 Detail

2 Limit Switch Screw and Nut

M77 Graphite Paste.

Wipe off All Excess. 1/100 and 2/100 Detail

3 Shaft Bearings MIL-G-81322 Grease 1/100 and 2/100 Detail

4 Landing Gear Clutch Fingers M77 Graphite Paste 1/100 and 2/100 Detail

5 Nose Gear Retract Chains SAE 30 W Oil 1/100 and 2/100 Detail

NOTE: Index numbers may not match T-44A Maintenance Manual lube chart index numbers.

ENGINE CONTROLS AND PROPELLER

Index No Location Lubricant Interval

Accomplished By

Inspected By

L/H R/H L/H R/H 1 Control Rod Ends MIL-G-23827 Grease 1/100 and 2/100 Detail

2 Cam Plates and Pins Lubriplate No. 130A 1/100 and 2/100 Detail

3 Propeller Hub Aeroshell 6 1/100 and 2/100 Detail

4 Low Pitch Stop Rods Marvel Mystery Oil 1/100 and 2/100 Detail

NOTE: Index numbers may not match T-44A Maintenance Manual lube chart index numbers.

AILERON CONTROL SYSTEM AND FLAP TRACKS

Index No Location Lubricant Interval Accomplished

By Inspected By

1 Aileron Quadrant VV-L-800 General Purpose Oil

2/100 Detail

2 Aileron Bell Cranks (2 Places)

VV-L-800 General

3 Flap Roller Tracks (8 Places Per Side)

Dry Slide, Synthetic Molybdenum (Spray) 1/100 and 2/100 Detail

1 2

NOTE: Index numbers may not match T-44A Maintenance Manual lube chart index numbers.

CONTROL COLUMN AND RUDDER PEDAL LINKAGE

Index No Location Lubricant Interval Accomplished By Inspected By

1 Control Column Linkage

VV-L-800 General

2 Rudder Pedals and Bell Crank Linkage

VV-L-800 General

NOTE: Index numbers may not match T-44A Maintenance Manual lube chart index numbers.

T44A CONTINUOUS INSPECTION DISCREPANCEY RECORD WORK SHEET

AIRCRAFT BUNO:________________ JCN: ________________ DATE: _______________

ITEM STATUS DISCEPANCY CORRECTIVE ACTION MECH CDI QA M/H

1. ↑↓

2. ↑↓

3. ↑↓

4. ↑↓

5. ↑↓

6. ↑↓

7. ↑↓

8. ↑↓

9. ↑↓

DETAIL INSPECTION SIGN-OFF SIGNATURE AND INITIAL RECORD

INSPECTION COMPLETED

DATE: _____ /_____ / _____ AIRCRAFT BUNO: __________MODEX: ________________

I certify that a Detailed Inspection was performed in accordance with the Continuous Inspection Program and that the aircraft is approved for return to service.

COMPLETED BY: _________________________________

QUALITY ASSURANCE REPRESENTATIVE: _____________________________

DATE: _____/_____ /_____

ALL EMPLOYEES PERFORMING TASKS ON THIS INSPECTION MUST ENTER THEIR NAMES,

SIGNATURE AND INITIALS.

EMPLOYEE NAME (PRINT) EMPLOYEE SIGNATURE EMPLOYEE

INITIALS

INSPECTION COMPLETED (Continued)

ALL EMPLOYEES PERFORMING TASKS ON THIS INSPECTION MUST ENTER THEIR NAMES,

SIGNATURE AND INITIALS.

Page 21.1

T-44A POWER ASSURANCE RUN WORKSHEET/RECORD

Aircraft BUNO

Date Purpose Of Run Outside Air Temp Altimeter in Ft

Aircraft Hours Left Engine Time, Since Overhaul

Right Engine, Time Since Overhaul

Low Pitch Torque Check

L/H Engine Target Torque

R/H Engine Target Torque

L/H Engine Observed Torque

R/H Engine Observed Torque Torque Difference in Foot Pounds

TREND MONITORING CHECK

Engine Inlet Temp in Degrees C (O.A.T) + 4.5 = ° C

Observed L/H Engine Observed R/H Engine

Torque (Target) 1315 Ft. Lbs. 1315 Ft. Lbs.

Prop Speed (N2) 2200 RPM 2200 RPM

Interstage Turbine Temperature (ITT)

Gas Generator Speed (N1)

Fuel Flow (WF)

Oil Pressure

Oil Temperature

L/H Engine

Target

Observed

Difference

Allowable Difference

N1 ± 1%

ITT + 15 / -75 ° C

WF (Fuel Flow) + 15 / -75 PPH

R/H Engine

Target

Difference

Allowable Difference

N1 ± 1%

ITT + 15 / -75 ° C

WF (Fuel Flow) + 15 / -75 PPH Inspection Completed: Time: Date: Name:

(Printed) Signature:

POWER ASSURANCE RUN SIGN-OFF SIGNATURE AND INITIALS RECORD

T-44 Scheduled Removal Component Inventory To be verified during 2nd 100 hour detail

Aircraft ____________________ Modex ___________________

Nomenclature Serial Number Mechanic Initials L&R Clerk Initials Retract Motor Retract Gearbox Flap Motor LH INBD Flap Actuator RH INBD Flap Actuator LH OTBD Flap Actuator RH OTBD Flap Actuator LH Engine LH Fuel Control Unit LH Fuel Pump LH Start Control LH Bleed Valve LH Starter Generator LH Overspeed Governor LH Primary Prop Governor RH Engine RH Fuel Control Unit RH Fuel Pump RH Start Control RH Bleed Valve RH Starter Generator RH Overspeed Governor RH Primary Prop Governor LH Prop RH Prop Scheduled Maintenance Mechanic: ________________________________ Date: _________

Scheduled Maintenance Crew Leader / CDI: ________________________ Date: _________

Logs and Records Clerk: _______________________________________ Date: _________

Aircraft Hours and Landings this Detail:

Hours: ________________ Landings: ______________

NAVAIR (PMA 273) 01 -50-T44A-600-6-4.2

January 1, 2013

TREND MONITORING CHECK