# Service difficulty reports: Boeing 747-44AF

A list on [Boeing 747-44AF](https://openairdocs.org/model/boeing-747-44af.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 23 · 1,133 reports

- [SDR IPXA2026102391622](https://openairdocs.org/sdr/IPXA2026102391622.md): Line · loose · Oct 23, 2026 · N577UP · Boeing 74744AF · Pneumatic Distribution System
  > ATB, ENG 3 OVHT/PRV EICAS MSG AFTER TAKE OFF CHECKLIST PROC. FOLLOWED UP WITH MSG RETURNING AT CRUISE POWER RESULTING IN NO NAI OR T/R ENG 3. FOUND PRV PNEUMATIC PRESSURE LINE FITTING LOOSE AND BLEEDING AIR OFF THE BELLOWS. TIGHTENED AS OUTLINED IN AMM 11-19-
- [SDR IPXA2026102389310](https://openairdocs.org/sdr/IPXA2026102389310.md): Life Vest · torn · Oct 23, 2026 · N573UP · Boeing 74744AF · Life Jacket
  > SUPERNUMERARY LIFE VEST EXP TAG TORN. REMOVED AND REPLACED LT OTBD LIFE VEST IAW AMM 25-62-05
- [SDR IPXA2026102153875](https://openairdocs.org/sdr/IPXA2026102153875.md): Window · cracked · Oct 21, 2026 · N575UP · Boeing 74744AF · Flight Compartment Windows
  > ARRIVAL FOUND L1 WINDOW CRACK.
- [SDR IPXA2026101188731](https://openairdocs.org/sdr/IPXA2026101188731.md): Battery Pack · inoperative · Oct 10, 2026 · N573UP · Boeing 74744AF · Emergency Lighting
  > FOUND UPPER DECK EMERGENCY LIGHT M4915, L1533, L5733,5767 INOPERATIVE. IAW AMM 33-51-04-002-009-001, 33-51-04-402-012-001, AND 33-51-04-902-001-001 REV.117 AND SSM 33-51-01 REV.48 REPLACED THE EMERGENCY LIGHT POWER SUPPLY M5169 AND THE BATTERY ASSEMBLY, AND P
- [SDR IPXA2026093003820](https://openairdocs.org/sdr/IPXA2026093003820.md): Handle · binding · Sep 30, 2026 · N573UP · Boeing 74744AF · Passenger/Crew Doors
  > L1 DOOR IS DIFFICULT TO OPEN & CLOSE HANDLE SWINGS VIOLENTLY COULD CAUSE INSURY. LUB THE L1 DOOR HANDLE AS PER B747 AMM 12-21-04 P.301 AND PERFORMED L1 DOOR OPS CHECK FOUNND "SATIS" AS PER B747 AMM 52-11-00 P.201.
- [SDR IPXA2026092951034](https://openairdocs.org/sdr/IPXA2026092951034.md): Door · damaged · Sep 21, 2026 · N570UP · Boeing 74744AF · Cabin Cooling System
  > UNKNOWN NOISE & VIBRATION FROM AIRCRAFT ON CLIMBOUT RESULTED IN AIR TURN BACK. FOUND #2 AIR INLET DOOR DAMAGED. INSTALLED NEW INLET DOOR ASSY IAW AMM 21-62-02.
- [SDR IPXA2026092251034](https://openairdocs.org/sdr/IPXA2026092251034.md): Unknown · vibration · Sep 21, 2026 · N570UP · Boeing 74744AF · Fuselage Structure (General)
  > ATB, UNKNOWN NOISE & VIBRATION FROM AIRCRAFT DURING CLIMBOUT. RESULTED IN AIR TURN BACK.
- [SDR IPXA2026092146237](https://openairdocs.org/sdr/IPXA2026092146237.md): Lamp · inoperative · Sep 21, 2026 · N576UP · Boeing 74744AF · Emergency Lighting
  > MAIN CARGO COMPARTMENT ENTRY, EMERGENCY LIGHTS INOP. RELAMPED AND OPS CHKD IAW AMM 33-51-00.
- [SDR IPXA2026081096634](https://openairdocs.org/sdr/IPXA2026081096634.md): Light · inoperative · Aug 9, 2026 · N573UP · Boeing 74744AF · Emergency Lighting
  > DOOR 1L, EMERGENCY EXIT SIGN LIGHT INOPERATIVE. C/W AMM33-51-05-962-031, REV. 137, OPC O.K.
- [SDR IPXA2026080575871](https://openairdocs.org/sdr/IPXA2026080575871.md): Battery · inoperative · Aug 2, 2026 · N572UP · Boeing 74744AF · Emergency Lighting
  > FOUND THE UPPER DECK AISLE EMERGENCY LIGHT INOP. IAW SSM 33-51-01 REV.47 PERFORMED THE UPPER DECK AISLE EMERGENCY LIGHT SYSTEM CHECK, FOUND THE EMERGENCY LIGHT BATTERY M5168 FUNCTION FAIL. IAW AMM 33-51-04-902-001-001, REV.117. REPLACED THE EMERGENCY LIGH
- [SDR IPXA2026080575748](https://openairdocs.org/sdr/IPXA2026080575748.md): Battery · inoperative · Aug 2, 2026 · N572UP · Boeing 74744AF · Emergency Lighting
  > FOUND THE UPPER DECK EMERGENCY EXIT SIGN LIGHT INOP. I.A.W SSM 33-51-01 REV.47 PERFORMED THE UPPER DECK EMERGENCY EXIT SIGN LIGHT SYSTEM CHECK, FOUND THE EMERGENCY LIGHT BATTERY M5169 FUNCTION FAIL. I.A.W AMM 33-51-04-902-001-001 REV.117 REPLACED THE EMERGEN
- [SDR IPXA2026080375748](https://openairdocs.org/sdr/IPXA2026080375748.md): Light · inoperative · Aug 2, 2026 · N572UP · Boeing 74744AF · Emergency Lighting
  > FOUND THE UPPER DECK EMERGENCY EXIT SIGN LIGHT INOP. (REPLACE)
- [SDR IPXA2026080375871](https://openairdocs.org/sdr/IPXA2026080375871.md): Light · inoperative · Aug 2, 2026 · N572UP · Boeing 74744AF · Emergency Lighting
  > FOUND THE UPPER DECK AISLE EMERGENCY LIGHT INOPERATIVE. (REPLACE)
- [SDR IPXA2026082710827](https://openairdocs.org/sdr/IPXA2026082710827.md): Doubler · ground damage · Jul 5, 2026 · N576UP · Boeing 74744AF · Fuselage Main, Structure
  > UPON REMOVAL, TAILSTAND CONTACTED STANCHION DOUBLER. ACCOMPLISHED ALL REQUIRED AMT STEPS AND VERIFIED ALL OTHER STEPS HAVE BEEN ACCOMPLISHED PER EO-97949-REQ1. THIS REPAIR IS NOW PERMANENT PER EO-97949-REQ3. MAJOR REPAIR.
- [SDR IPXA2026070878270](https://openairdocs.org/sdr/IPXA2026070878270.md): Flap · cracked · Jul 3, 2026 · N572UP · Boeing 74744AF · Trailing Edge Flaps
  > FOUND RT WING OUTBD AFT FLAP INBD SIDE BOTTOM SURFACE CRACK. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2 INCHES AROUND HEATED AREA,PER 747 NDT MANUAL PART 1 51-01-01 REV:183 RESULT:NO DEFECT WAS FOUND. IAW AMM 51-24-11-477-083, REV 116, REPAINT PEEL OFF
- [SDR IPXA2026071560216](https://openairdocs.org/sdr/IPXA2026071560216.md): Skin · cracked · Jul 2, 2026 · N572UP · Boeing 74744AF · Nacelle/Pylon, Plate/Skin
  > CRACKED SKIN, NR 4 PYLON R/H FAIRING DOOR L/E AREA. I.A.W.AMM 54-62-03-404-005 REV117 INSTALLED NO.4 PYLON R/H FAIRING DOOR.
- [SDR IPXA2026070759188](https://openairdocs.org/sdr/IPXA2026070759188.md): Cowling · dented · Jul 2, 2026 · N572UP · Boeing 74744AF · Nacelle/Pylon, Main Frame
  > DENTED SKIN, NR 2 ENG NOSE COWL INLET AT 10 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA: 0.5", 12.8" FROM AFT EDGE, 51.7" FROM LWR EDGE, AT 10 O'CLOCK ON THE ACOUSTIC PNL OF NO.2 ENG INLET COWL). FILL THE CUT OUT WITH ADHESIVE C
- [SDR IPXA2026070724623](https://openairdocs.org/sdr/IPXA2026070724623.md): Seal · broken · Jun 30, 2026 · N572UP · Boeing 74744AF · Leading Edge Devices
  > BROKEN MOLDING SEAL, LT WING NR 11 KRUEGER FLAP INBD SIDE MOLDING. CHECKED OK.
- [SDR IPXA2026070921962](https://openairdocs.org/sdr/IPXA2026070921962.md): Web · corroded · Jun 30, 2026 · N572UP · Boeing 74744AF · Fuselage Miscellaneous Structure
  > CORRODED UPPER DECK FLOOR PNL WEB AT BS 480 - 520, LBL 10 - RBL 40 CORRODED. INSTALLED A NEW WEB IAW SRM 51-40-02-0G, REV 107.
- [SDR IPXA2026070724617](https://openairdocs.org/sdr/IPXA2026070724617.md): Seal · broken · Jun 30, 2026 · N572UP · Boeing 74744AF · Leading Edge Devices
  > BROKEN MOLDING SEAL, LT WING NR 6 VC FLAP INBD SIDE MOLDING. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 160 PERFORM REPAIR
- [SDR IPXA2026070624604](https://openairdocs.org/sdr/IPXA2026070624604.md): Seal · broken · Jun 30, 2026 · N572UP · Boeing 74744AF · Leading Edge Devices
  > BROKEN MOLDING SEAL, LT WING NR 3 VC FLAP INBD SIDE, IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 160 PERFORM REPAIR.
- [SDR IPXA2026070624589](https://openairdocs.org/sdr/IPXA2026070624589.md): Seal · broken · Jun 30, 2026 · N572UP · Boeing 74744AF · Trailing Edge Flaps
  > BROKEN MOLDING SEAL, LT WING NR 2 VC FLAP INBD SIDE. REMOVED THE RAIN EROSION SHIELDS AND CLEANED. APPLY THE SEALANT TO REPAIR AREA.
- [SDR IPXA2026070324858](https://openairdocs.org/sdr/IPXA2026070324858.md): Skin · damaged · Jun 30, 2026 · N572UP · Boeing 74744AF · Wing, Plate/Skin
  > ABRADED SKIN, UPPER FACE OF LT WING INBD L/E REFUELING STATION LOWER DOOR, PANEL 521BB, IAW AMM 52-49-09-402-003, REV 116. INSTALLED REFUELING PANEL 521BB. CONDITION CHECKED NORMAL.
- [SDR IPXA2026070420634](https://openairdocs.org/sdr/IPXA2026070420634.md): Fairing · debonded · Jun 30, 2026 · N572UP · Boeing 74744AF · Aerodynamic Fairings
  > DEBONDED PANEL, AFT WING TO BODY FAIRING PANEL 193CL EXTERNAL SURFACE. IAW AMM 20-51-01-912-008 REV.116 INSTALL PANEL 193CL. CONDITION CHECK NORMAL.
- [SDR IPXA2026070524776](https://openairdocs.org/sdr/IPXA2026070524776.md): Skin · cracked · Jun 30, 2026 · N572UP · Boeing 74744AF · Wing, Plate/Skin
  > CRACKED SKIN, RT WING T/E NEAR INBD AILERON PANEL 673AB. IAW SRM 57-51-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.107 PERFORM REPAIR AS BELOW STEP: REMOVE THE DAMAGE MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA (L:0.38", W:0.28", 11" FROM INBD EDGE,AT PNL AFT ED
- [SDR IPXA2026070324807](https://openairdocs.org/sdr/IPXA2026070324807.md): Skin · cracked · Jun 30, 2026 · N572UP · Boeing 74744AF · Wing, Plate/Skin
  > CRACKED SKIN, RT WING T/E NEAR INBD AILERON 673CB. IAW AMM 20-51-01-912-008 REV. 116 INSTALLED THE ACCESS PANEL 673CB. CONDITION CHECKED NORMAL.
- [SDR IPXA2026070624831](https://openairdocs.org/sdr/IPXA2026070624831.md): Skin · cracked · Jun 30, 2026 · N572UP · Boeing 74744AF · Wing, Plate/Skin
  > CRACKED SKIN, LOWER FACE OF LT WING INBD L/E REFUELING STATION LOWER DOOR CUTOUT, ILES 845. IAW AMM 52-49-09-402-003, REV. 116. INSTALLED REFUELING PANEL NO. 521CB. 2. CONDITION CHECK NORMAL. ATTACHMENT ARE UPLOADED.
- [SDR IPXA2026063024905](https://openairdocs.org/sdr/IPXA2026063024905.md): Crash Axe · damaged · Jun 30, 2026 · N576UP · Boeing 74744AF · Emergency Equipment
  > MAIN DECK CRASH AXE FOUND DAMAGED/CORRODED REINSTALLED CRASH AXE INTO HOLDER ON MAIN CARGO DECK IAW AMM 25-60-00.
- [SDR IPXA2026073009895](https://openairdocs.org/sdr/IPXA2026073009895.md): Web · cracked · Jun 29, 2026 · N572UP · Boeing 74744AF · Wing Miscellaneous Structure
  > SURFACE & HOLE CRACK INDICATION, DURING PFM SB 747-57A2357 FND SURFACE & HOLE CRACK. ACCOMPLISHED REPAIR IAW EO-98227-REQ1, REV 1, & EGAT EI F2026A57M-1427, REV 4.
- [SDR IPXA2026072111084](https://openairdocs.org/sdr/IPXA2026072111084.md): Panel · debonded · Jun 29, 2026 · N572UP · Boeing 74744AF · Vertical Stabilizer, Plate/Skin
  > DEBONDED PANEL, VERTICAL STABILIZER LOWER PANEL 322BL. REPAIR DISBOND ON PANEL ASSY OF VST FWD TORQUE BOX BETWEEN STA 2365 AND STA 2413 I.A.W. EGAT EI F2026A55M-1378 REV.1 AND UPS EO-98179-REQ1 REV.1 2. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2026072111043](https://openairdocs.org/sdr/IPXA2026072111043.md): Panel · debonded · Jun 29, 2026 · N572UP · Boeing 74744AF · Vertical Stabilizer, Plate/Skin
  > DISBONDED PANEL, VERTICAL STABILIZER LOWER PANEL 322CL. REPAIR DISBOND DAMAGE ON LH FWD LWR VST FORWARD TORQUE BOX PANEL BETWEEN STA 2285 AND 2365 AND BETWEEN FIN WL10 AND 25 I.A.W. EGAT EI NO. F2026A55M-1379 REV. 1 AND UPS EO-98180-REQ1 REV. 2
- [SDR IPXA2026070697892](https://openairdocs.org/sdr/IPXA2026070697892.md): Seal · broken · Jun 28, 2026 · N572UP · Boeing 74744AF · Leading Edge Devices
  > BROKEN MOLDING SEAL, L/H WING NR 4 VC FLAP INBD SIDE MOLDING. IAW SRM 57-43-02-2R-5, REV 107, REFER TO SOPM 20-50-12 REV 160. PERFORMED A REPAIR, REMOVED THE RAIN EROSION SHIELDS AND CLEANED.APPLY THE SEALANT TO REPAIR AREA. CONDITION CHECKED SATISFACTORY.
- [SDR IPXA2026070697902](https://openairdocs.org/sdr/IPXA2026070697902.md): Seal · broken · Jun 28, 2026 · N572UP · Boeing 74744AF · Leading Edge Devices
  > BROKEN MOLDING SEAL, LT WING NR 5 VC FLAP INBD SIDE. IAW SRM 57-43-02-2R-5, REV 107, REFER TO SOPM 20-50-12, REV 160. PERFORMED A REPAIR, REMOVED THE RAIN EROSION SHIELDS AND CLEANED, APPLY THE SEALANT TO REPAIR AREA. CONDITION CHECKED SATISFACTORY.
- [SDR IPXA2026072186856](https://openairdocs.org/sdr/IPXA2026072186856.md): Seal · damaged · Jun 27, 2026 · N572UP · Boeing 74744AF · Passenger/Crew Doors
  > FOUND NR 1 ENTRY DOOR LOWER SEAL DAMAGED. IAW AMM 52-09-00-308-001, REV.116. REPLACED NR 1 ENTRY DOOR LOWER SEAL. CONDITION CHECK NORMAL.
- [SDR IPXA2026071085535](https://openairdocs.org/sdr/IPXA2026071085535.md): Skin · broken · Jun 27, 2026 · N572UP · Boeing 74744AF · Wing, Plate/Skin
  > CRACKED SKIN, RT WING L/E NR 23 V.C FLAP INBD LWR. ACCOMPLISHED JOB IAW EO-97981-REQ1, REV1 AND EGAT EI F2026A57M-1340. ACCOMPLISHED JOB I.A.W UPS EO-97981-REQ1 REV2 AND EGAT EI NO. F2026A57M-1340, REV.0 AND REV.1.
- [SDR IPXA2026062986856](https://openairdocs.org/sdr/IPXA2026062986856.md): Seal · damaged · Jun 27, 2026 · N572UP · Boeing 74744AF · Passenger/Crew Doors
  > FOUND NO.1 ENTRY DOOR LOWER SEAL DAMAGED
- [SDR IPXA2026061359943](https://openairdocs.org/sdr/IPXA2026061359943.md): Duct · damaged · Jun 8, 2026 · N577UP · Boeing 74744AF · Wing Main, Frame Structure
  > FOUND R/H WING FUEL VENT DUCT FWD SIDE HAS ENLARGE HOLE. PERFORMED NDT/UT FOR REWORKED AREA PLUS 6'' AROUND HEATED AREA I.A.W 747 NTM PART1 51-01-01 REV:182. FOUND R/H WING FUEL VENT DUCT FWD SIDE HAS ENLARGE HOLE. I.A.W. 747-400F SRM 57-51-01-2R-1 REFER TO
- [SDR IPXA2026061160591](https://openairdocs.org/sdr/IPXA2026061160591.md): Floor Panel · damaged · Jun 8, 2026 · N577UP · Boeing 74744AF · Fuselage Floor Panel
  > FOUND MAIN DECK CARGO FLOOR PANEL DAMAGE. IAW SREO-42648-REQ1, REV 3 FABRICATED A NEW FLOOR PANEL. CONDITION CHECK IS SATISFACTORY. IAW AMM 53-21-02-404-006 REV.116 INSTALLED MAIN DECK CARGO FLOOR PANEL.
- [SDR IPXA2026061021955](https://openairdocs.org/sdr/IPXA2026061021955.md): Floor Panel · damaged · Jun 5, 2026 · N577UP · Boeing 74744AF · Fuselage Floor Panel
  > MAJOR REPAIR. FOUND MAIN DECK CARGO FLOOR PANEL DAMAGE I.A.W. SREO-42648-REQ1 REV. 3 FABRICATE A NEW FLOOR PANEL. CONDITION CHECK IS SATISFACTORY
- [SDR IPXA2026060698163](https://openairdocs.org/sdr/IPXA2026060698163.md): Bracket · chafed · Jun 4, 2026 · N577UP · Boeing 74744AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 4 ENG RT T/R FWD LWR CLOSURE DOOR T/E AREA. IAW SRM 51-40-02-0G REV. 106 AND ST ENGINEERING IPC 78-32-22 REV. 96 INSTALLED NEW BRACKET.
- [SDR IPXA2026060899517](https://openairdocs.org/sdr/IPXA2026060899517.md): Bracket · chafed · Jun 4, 2026 · N577UP · Boeing 74744AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 4 ENG L/H T/R FWD LWR CLOSURE DOOR T/E AREA. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE BRACKET. I.A.W SRM 51-40-02-0G REV. 106 AND ST ENGINEERING IPC 78-32-21 REV. 96 INSTALLED NEW BRACKET.
- [SDR IPXA2026061583676](https://openairdocs.org/sdr/IPXA2026061583676.md): Duct · damaged · Jun 3, 2026 · N577UP · Boeing 74744AF · Wing Main, Frame Structure
  > ENLARGE - HOLE, RT WING T/E OUTBD FUEL TANK VENT SCOOP AND DUCT ASSY. I.A.W. 747-400F SRM 57-51-01-2R-1 REFER TO SRM 51-70-17-0G-0 REV.106. REMOVE THE DAMAGED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM V
- [SDR IPXA2026060878687](https://openairdocs.org/sdr/IPXA2026060878687.md): Bracket · broken · Jun 3, 2026 · N577UP · Boeing 74744AF · Fuel Storage
  > FOUND FUEL LINE TUBE SUPPORT BRACKET BROKEN, ACCESS DOOR: 652DB, AT WS 1056RIB. I.A.W SRM 51-40-02-0G REV. 106 AND BOEING DWG NO: 65B01076 SHEET 5 REV. B INSTALLED FABRICATED BRACKET.
- [SDR IPXA2026061762754](https://openairdocs.org/sdr/IPXA2026061762754.md): Angle · broken · Jun 2, 2026 · N577UP · Boeing 74744AF · Landing Gear Doors
  > LEFT BODY GEAR S/S INBOARD DOOR, DOOR SEAL ANGLE DAMAGE. INSTALLED NEW SEAL GAP IAW SRM 51-40-02-0G REV.106 AND BOEING DWG 65B10920, SH19, REV-.
- [SDR IPXA2026061862990](https://openairdocs.org/sdr/IPXA2026061862990.md): Bracket · cracked · Jun 2, 2026 · N577UP · Boeing 74744AF · Fuselage Miscellaneous Structure
  > FOUND MAIN DECK CREW ACCESS LADDER BRACKET CRACK. REPAIR CRACK AREA IAW EO-97678-REQ1, REV 2.
- [SDR IPXA2026061762524](https://openairdocs.org/sdr/IPXA2026061762524.md): Strip · broken · Jun 2, 2026 · N577UP · Boeing 74744AF · Fuselage Miscellaneous Structure
  > RIGHT BODY GEAR S/S OUTBOARD DOOR, LOWER SEAL DAMAGE GAP STRIP. REMOVED DAMAGE GAP STRIP I.A.W SRM 51-40-02-0G REV.106. INSTALLED NEW GAP STRIP I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO: 65B10920 SH13 REV.A.
- [SDR IPXA2026061565577](https://openairdocs.org/sdr/IPXA2026061565577.md): Fitting · damaged · Jun 2, 2026 · N577UP · Boeing 74744AF · Engine Thrust Reverser
  > ENLARGED HOLE, NR 3 ENG RT T/R INNER UPPER POD AREA. REPAIR DAMAGE POD AREA IAW CMM 78-32-02 REPAIR 020 REV 71.
- [SDR IPXA2026061562566](https://openairdocs.org/sdr/IPXA2026061562566.md): Fitting · cracked · Jun 2, 2026 · N577UP · Boeing 74744AF · Wing Miscellaneous Structure
  > CRACKED BRACKET, LT WING T/E INBD SECTION UPPER FIXED PANEL LOWER SUPPORT AT WBL 255.692, ADJACENT NR 6 SPOILER INBD SIDE. IAW SRM 51-40-02-0G REV 106, AND DWG:65B11544, SHEET 1, REV G. INSTALL NEW FITTING ASSY.
- [SDR IPXA2026061563360](https://openairdocs.org/sdr/IPXA2026061563360.md): Bracket · cracked · Jun 2, 2026 · N577UP · Boeing 74744AF · Fuselage Miscellaneous Structure
  > LEFT BODY GEAR WW, AFT HYD SUPPORT BRACKET CRACKED. IAW SRM 51-40-02-0G, REV 106. REMOVED DAMAGE BRACKET. IAW SRM 51-40-02-0G REV. 106, & DWG:65B80259, SHEET 4, REV-. INSTALLED NEW BRACKET.
- [SDR IPXA2026061565907](https://openairdocs.org/sdr/IPXA2026061565907.md): Seal · worn · Jun 2, 2026 · N577UP · Boeing 74744AF · Fuselage Main, Structure
  > RIGHT WING GEAR W/W, FWD CUTOUT FAIRING FWD LOWER SEAL WORN. REVIEWED TASK PER GMM-MTX 09.05.01.09.I.A.W SRM 51-40-02-0G REV. 106 AND DWG:65B10555 SHEET 3 REV.G INSTALL NEW SEAL.

Next page: https://openairdocs.org/model/boeing-747-44af/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '74744AF'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-747-44af/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.