Boeing 747-44AF
Service difficulty reports · 1,135
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IPXA2026042634350Clamp · crackedCRACKED CLAMP - APU ACOC COOLING DUCT. I.A.W.AMM 49-51-04-004-001 REV116 AND AMM 49-51-04-404-011 REV116 REPLACED THE CLAMP WITH NEW.SDR IPXA2026042119204Skin · damagedLIGHTNING STRIKE- SKIN, RT NOSE AREA (ABOVE UPS LOGO) SUSPECTED LIGHTENING STRIKE ON FASTENER. BLEND OUT THE DAMAGE AREA I.A.W SRM 51-10-02-0G REV.106. ACCOMPLISHMENT LIGHTNING STRIKE REPAIR I.A.W UPS EO-97134-REQ1 REV.1.SDR IPXA2026042072963Ring · crackedCRACKED ACSR-ON ENG-2 , R/H THRUST REVERSER HALF. IAW AMM 78-31-01-004-001-J00 REV 116 REMOVED THE T/R HALF. RII NO.2 ENG R/H THRUST REVERSER HALF OK TO INSTALLED CHECKED OK AND INSTALLED CHECKED OK.SDR IPXA2026042075055Fitting · crackedFND 3L T/R AGB FITTING CRACK AT 7 O'CLOCK POSITION. I.A.W. AMM 78-31-01-004-001-J00 REV116 REMOVED THE T/R HALF. I.A.W SRM 51-40-02-0G REV.106 REMOVE DAMAGE AGB FITTING. RII NO.3 ENG L/H THRUST REVERSER HALF OK TO INSTALLED CHECKED OK AND INSTALLED CHECKED OK.SDR IPXA2026041557453Angle · crackedDURING PERFORMANCE OF EO-95214-JIC2, FOUND RT WING LG SHOCK STRUT DOOR FAIRING SEAL DEPRESSOR. I.A.W SRM 51-40-02-0G REV.106 REMOVED DAMAGE DEPRESSOR. I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO.65B11675 SH. 2 REV. G INSTALLED NEW DEPRESSOR.SDR IPXA2026041557510Angle · crackedDURING PERFORM EO-95214-JIC2, FOUND RT WING SHOCK STRUT DOOR FAIRING CLIP CRACKED. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE CLIP. I.A.W SRM 51-40-02-0G REV. 106 AND BOEING DWG NO: 65B11675 SHEET 1 REV. K INSTALLED FABRICATED CLIP.SDR IPXA2026032784468Ballast · inoperativeALL LIGHTS IN THE LAVATORY FOUND TO BE INOPERATIVE, NOT JUST THE CEILING LIGHT. BALLAST CONNECTION RESET AND LAMPS RESET C/OUT, FOUND OPS NORMAL.SDR IPXA2026032353595Battery · inoperativeFOUND EMERGENCY LIGHT L1853, L1854, L5735 INOP. I.A.W AMM 33-51-04-902-001-001 REV.116 REPLACED POWER SUPPLY BATTERY AND CONDITION CHECK NORMAL. I.A.W AMM 33-51-04-902-001-001 REV.116 PERFORMED THE EMERGENCY LIGHT POWER SUPPLY TEST, RESULT WAS SATISFACTORY.SDR IPXA2026031953595Light · inoperativeFOUND EMERGENCY LIGHT L1853, L1854, L5735 INOP (REPLACE)SDR IPXA2026031710375Skin · erodedERODED SKIN, LT WING UPPER PANEL OLES 1318.65~OLES 1453 P/N:65B10870-39. INSTALL L/H WING LEADING EDGE UPPER FIXED PANEL OLES1318.65 - OLES 1453 I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO.65B14961 SH1 REV.E AND 65B14961 SH2 REV.C AND 65B10652 SH4 REV.F ANSDR IPXA2026031086246Cover · chafedCHAFED COVER, NR 3 ENG R/H CORE COWL INNER AFT LATCH AREA. INSTALL NEW COVER I.A.W SRM 51-40-02-0G REV.106 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-24 REV.50.SDR IPXA2026031886249Bracket · chafedNR 4 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET CHAFING. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.106 AND CMM IPL 71-13-23 REV.47SDR IPXA2026031685821Bracket · gougedGOUGED BRACKET, NR 2 ENGINE LT THRUST REVERSER COWL LOWER FWD FIXED PANEL T/E. REMOVED THE DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 106. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 106, AND ST ENGINEERING IPC 78-32-21 REV 94.SDR IPXA2026031686662Bracket · gougedGOUGED BRACKET, NR 2 ENG RT CORE COWL HOLD- OPEN ROD RECIVER BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G REV.106. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G ,REV.106 AND CMM IPL 71-13-24 REV.50.SDR IPXA2026032076722Retainer · brokenBROKEN RETAINER, RT WING L/G W/W OUTBD DOOR FWD AND AFT SEAL AREA, QTY:2EA INSTALL NEW RETAINERS I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO.65B10907 SH11 REV.-.SDR IPXA2026032076687Retainer · crackedCRACKED RETAINER, LT WLG W/W OUTBD DOOR AFT SEAL .INSTALL NEW RETAINER I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO.65B10907 SH11 REV.-.SDR IPXA2026032176637Bracket · crackedCRACK-BRACKET, R/H BODY L/G W/W FLUID TRANSFER ALTERNATE BRAKE SUPPORT BRACKET, STA 1394 (REPLACE) INSTALLED FABRICATED BRACKET I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO 257U2231 SH1 REV.ASDR IPXA2026031675369Skin · crackedCRACK - SKIN , LOWER FACE OF L/H WING T/E INBD MID FLAP T/E UPPER FIXED PNL , WBL 438. (REPAIR) I.A.W AMM 27-51-03-404-008 REV.115 INSTALL THE PIN BETWEEN NO.5 SWING ARM AND SPINDLE.SDR IPXA2026032075538Latch · deformedDEFORMED SKIN , R1 ENGINGE THRUST REVERSER COWL BLOWOUT DOOR INBD EDGE ADJACENT NR 1 LATCH. INSTALL NEW DOOR I.A.W SRM 51-40-02-0G REV.106 AND IPC 78-31-19-02 REV.60.SDR IPXA2026031977449Bracket · crackedCRACK-BRACKET, NO.2 ENG R/H T/R COWL LOWER LATCH HANDLE (REPLACE) I.A.W. AMM 78-31-02-004-001-J00 REV:116 AND AMM 78-31-02-404-007-J00 REV:116, REPLACED THE BRACKET.SDR IPXA2026031705369Skin · crackedCRACKED SKIN, LOWER FACE OF LT WING T/E INBD MID FLAP T/E UPPER FIXED PANEL , WBL 438. RII COMPLETED FOR THE PIN BETWEEN NR 5 SWING ARM AND SPINDLE OK TO INSTALL.SDR IPXA2026031775549Skin · crackedCRACKED PANEL, RT BODY MLG WW INNER LONGERON BOX AREA ,BS 1372. REPAIRED THE DAMAGE IAW EO-96831,REQ1, REV 1, AND EGAT EI F2026A53M-503, REV 1.SDR IPXA2026031675363Skin · crackedRIGHT WING INBOARD MID FLAP , T/E LOWER SURFACE CRACK. (REPAIR) 3 BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG.SDR IPXA2026031325538Skin · deformedDEFORM - SKIN , NO. 1 ENG R/H T/R COWL BLOWOUT DOOR INBD EDGE ADJACENT NO. 1 LATCH. (REPLACE) CONDITION CHECK NORMAL.SDR IPXA2026030875659Floor Panel · delaminatedFOUND MAIN DECK FLOOR PANEL DELAMINATED. INSTALL THE REPLACEMENT FLOOR PANELSDR IPXA2026032365412Track · brokenBROKEN TRACK, L1 ENTRY DOOR CUTOUT AFTER MID SIDE. IAW AMM 25-59-01-404-176 REV.116, INSTALLED MAIN DECK SIDEWALL PANEL AT L1 DOOR AFT SIDE.SDR IPXA2026032165091Frame · crackedNR 3 PYLON STRUT UPPER FRAME, OUTBOARD SIDE PANEL SUPPORT FRAME CRACK (REPLACE) INSTALLED FABRICATED FRAME I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO 313U2200 SH15 REV.-SDR IPXA2026032366783Attach Fitting · crackedRIGHT WING INBOARD L/E NOSE WEB ATTACH ANGLE CRACK, ILES 635.4 (REPLACE) INSTALLED NEW FITTING I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO: 65B15696 SH 7 REV.DSDR IPXA2026032166896Splice Plate · crackedFAULT - RIGHT WING OUTBOARD L/E CAVITY INSE, PANEL SPLICE PLATE CRACK (REPLACE) INSTALLED FABRICATED FRAME I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO 65B11862 SH2 REV.FSDR IPXA2026031066913Bracket · chafedCHAFED BRACKET, NT3 ENG R/H T/R FWD LWR FAIRING T/E AREA (REPLACE) INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.106 AND ST ENGINEERING AEROSPACE IPC 78-32-22 REV.94.SDR IPXA2026031266432Bracket · chafedCHAFED BRACKET, NR 4 ENG L/H T/R FWD LWR FAIRING T/E AREA INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.106 AND ST ENGINEERING IPC 78-32-21 REV.94SDR IPXA2026040554363Fairing · puncturedPUNCTURE IN FWD OTBD AREA OF #1 MOVEABLE FLAP TRACK FAIRING. I.A.W. 747-400F SRM 57-53-70-2R-1 REFER TO SRM 51-70-07-0G-0 REV.106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE PUNCTURE MATERIALS AND CLEAN. 1.2 MEASURE THE DAMAGE AREA (DIA:1", 2.5" FROM THE PASDR IPXA2026031148678Bracket · chafedCHAFED BRACKET, NR 4 ENG R/H T/R FWD LWR FAIRING T/E AREA. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.106 AND ST ENGINEERING IPC 78-32-22 REV.94SDR IPXA2026030919342Floorboard · wornMAJOR REPAIR, FLOORBOARD INSIDE L1 DOOR THRESHOLD IS WORN AND IS SHOWING CORE MATERIAL. INSTALLED NEW FLOORBOARD INSIDE L1 DOOR THRESHOLD IAW AMM 53-21-02.SDR IPXA2026030908993Door Frame · damagedFOUND DAMAGE ON UNDERLYING STRUCTURE BEHIND SEAL DEPRESSOR SPLICE AT FS 615 APPROX WL 170. ALL STEPS ARE COMPLETE EO-96726-REQ1.SDR IPXA2026031672729Frame · crackedLEFT WING SHOCK STRUT DOOR FAIRING RUB CRACK FRAME. (REPLACE) INSTALLED NEW FRAME I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO: 65B11675 SH 1 REV.K AND 65B11675 SH2 REV.G AND 65B11675 SH3 REV.KSDR IPXA2026031702729Frame · crackedCRACKED LT WING SHOCK STRUT DOOR FAIRING RUB, CRACKED FRAME.SDR IPXA2026041369914Skin · dentedNR 25 VCF HAS DENT ON LEADING INB END RII COMPLETED STEP 13 I.A.W AMM 27-81-02-404-010 REV.116 ASSEMBLY THE NR 26 FOLDING NOSE AND INSTALLED THE NR 26 V.C FLAP CHECK OK. ACCOMPLISHED REPAIR I.A.W EGAT WORK SHEET NO.60222 AND SRM 57-43-02-2R-2 REPAIR2 REV.106SDR IPXA2026020652253Antenna · faultedAIR TURN BACK, TCAS SYSTEM ADVISORY MESSAGE CHECK CMC PRESENT LEG FAULT.FND TCAS LOWER ANTENNA FAIL. REPLACED LOWER TACAS ANTENNA .PFM GOUND TEST PASS.PER AMM34-45-02.SYS BACK TO NML.SDR IPXA2026012682273Start Valve · faultedAIR TURN BACK, NR 3 STARTER CUTOUT EICAS MESSAGE IN CLIMB, CONTINUED THROUGH FLIGHT. QRH PROCEDURE FOLLOWED. R & R NR 3 ENG START VALVE IAW AMM 80-11-02/401 & OPS CHECKED NORMAL.SDR IPXA2026020211187Skin · gougedON ARRIVAL DAMAGE TO SKIN FOUND JUST AFT OF AFT CARGO DOOR. REMOVED STRINGER CLIPS IN COMMON TO REPAIR REF SRM 51-40-02. COMPLETED REPAIR IAW EO-96145.SDR IPXA2025120545461Warning Message · false activationEICAS GEAR DOOR. ? QRH PG 14.13 STS MSG GEAR DOOR & GEAR MONITOR. R&R RH BODY GEAR DOOR ACTUATOR IAW AMM 32-33-27 UP TO AND INCLUDING STEP D.17. WITNESSED THE FINAL GEAR SWING PER GMM 04-02. OPS CHECK GOOD. ACCOMPLISHED REMAINING STEPS TO COMPLETE RH BODY SDR IPXA2025120345461Door · faultedATB AT 1058Z FOR EICAS GEAR DOOR. QRH PG 14.13 STS MSG GEAR DOOR & GEAR MONITOR DEBRIEF WITH CREW CAPTAIN REFERENCED HEARING A LOUD WIND NOISE WHEN GEAR HANDLE WAS MOVED TO THE OFF POSITION. WITH HANDLE IN UP POSITION NO WIND NOISE.SDR IPXA2025111479619Spoiler Sys · inoperative**ATB** HYD QUAN 2 LOW - EICAS. R&R SPOILER CONTROL PACKAGE ASSEMBLY PER AMM 27-61-05-402-012. LEAK AND OPS CHECK OK. NO FAULTS NOTED AT THIS TIME.SDR IPXA2025111341703Engine · oil consumptionINFLIGHT SHUTDOWN, EMERGENCY DECLARED. DURING CRUISE AT APPROX 3.5 HRS INTO FLT. ENG 4 OIL QTY BEGAN TO DROP FROM 5 QT TO ZERO IN 25 MINS. OIL PRESS WAS NORMAL UNITL AT REACHED ZERO. WHEN OIL PRESS INDICATED RED LINE. ENG WAS SHUT DOWN. PERFORMED ENG RUN CHSDR IPXA2025101684764Pump · bypassingFUEL IMBALANCE, 2-3.C/W WITH QRH, NO FUEL LEAK SUSPECTED, BALANCED FUEL. MAIN TANK 2 IS CONSISTENTLY LOWER THAN MAIN TANK 3 CMC MSG 28798. VERIFIED DEFUEL VALVE POSITION PER IFIM 28-22 TASK 925. PRESSURIZED FUEL MANIFOLD. FOUND FUEL FLOW RATE IS 400LBS LESS USSDR IPXA2025100885263Floor Panel · crackedCRACK- FLOOR PANEL, MAIN DECK COMPARTMENT FLOOR PNL (P/N: 144U5803-98). MAIN DECK COMPARTMENT FLOOR PNL (P/N: 144U5803-98).I.A.W AMM 25-59-01-004-175 REV.114 REMOVE MAIN DECK CARGO FLOOR PANEL/SEALANT AND PERFORM G.V.I CHECK RESULT WAS NORMAL. IAW AMM 53-21-02SDR IPXA2025100965035Skin · gougedGOUGE - SKIN, RT WING OUTBOARD AFT FLAP AT WS900 - WS920. REPAIRED GOUGE DAMAGE RT WING OUTBD T/E FLAP AFT FLAP UPPER PANEL BETWEEN WBL 747.7 AND WBL 822.0 IAW EI F 2025A57M-2243, REV 2 AND EO-95508-REQ1 REV 1.SDR IPXA2025101564861Skin · gougedGOUGE - SKIN - RT WING OUTBOARD FLAP AFT FLAP AT WS 880 - 890. REFER TO 747 NDT MANUAL, PART 6,51-00-00, FIGURE 1,11OR 16 FOR HFEC PROCEDURE. IAW EGAT EI F 2025A57M-2243 SEQUENCE A STEP 3. REQUEST RII VERIFY VALIDATE SPECIALIZED PROCESS IN REPAIR INSTRUCTIONS SDR IPXA2025101564889Skin · gougedGOUGE - SKIN - RT WING OUTBOARD FLAP AFT FLAP AT STA WS 862-870. RT WING OUTBD AFT FLAP T. REFER TO 747 NDT MANUAL, PART 6,51-00-00, FIGURE 1,11OR 16 FOR HFEC PROCEDURE. IAW EGAT EI F 2025A57M-2243 SEQUENCE A STEP 3. REQUEST RII VERIFY VALIDATE SPECIALIZED P
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