Boeing 747-45E
Service difficulty reports · 711
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 = '74745E' 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 = '74745E' 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 IPXA10B58855Seal · brokenSEAL BROKEN ON EMERGENCY DESCENT DEVICE. REPLACED DESCENT DEVICE IAW MM 25-61-01-2.SDR 2010F00064Power Cable · brokenTHE ELECTRICAL POWER FEEDER CABLE OF NR 4 HYD AUX PUMP IN THE MEC WAS BROKEN, THE MAIN DECK FLOOR BEAM NEXT TO THE BROKEN CABLE WAS DISCOLORED AND HEAT DAMAGED. PERFORMED INSPECTION AND STRUCTURE REPAIR TO MAIN DECK FLOOR BEAM, SPLICE REPAIR ELECTRICAL POWER SDR IPXA10B58186Floor Panel · damagedFLOOR DAMAGED. FABRICATED NEW FLOOR.SDR IPXA10B58185Floorboard · damagedFLOORBOARD DAMAGED. FABRICATED NEW FLOORBOARD.SDR IPXA10B58184Floorboard · damagedFLOORBOARD DAMAGED. FAB NEW FLOORBOARD.SDR IPXA10B58183Floorboard · damagedFLOORBOARD DAMAGED. FABRICATED NEW FLOOR BOARD.SDR IPXA10B58182Floorboard · damagedFLOORBOARD DAMAGED. FABRICATED NEW FLOORBOARD IAW EO B747-5320-36305.SDR IPXA10B58175Floorboard · damagedFLOORBOARD DAMAGED. FABRICATED NEW FLOORBOARD.SDR IPXA09B57871Light · inoperativeUPPER DECK AFT EMERGENCY CEILING LIGHT INOP. RE-LAMPED UPPER DECK AFT EMERGENCY CEILING LIGHT PER MM 33-51-07-2. OPS CK NORMAL.SDR IPXA09B57473Skin · bulgedINSPECTION TYPE:C FUSELAGE STA 1720 TO 1740 STR 42R EXT SKIN BULGED UP. FX BETWEEN BS 1720 TO BS 1741 & STR 41R-43R SKIN REPAIR AS PER SRM 53-00-01 FIG 201 REPAIR 15 REV 12. THIS REPAIR IS CLASSIFIED AS MAJOR CAT B REPAIR REPAIR SIZE 11 X 13.75 INCHES DAMAGESDR IPXA09B57453Frame · crackedINSPECTION TYPE:C NR 3 PYLON INTERIOR AREA STA 346.4 O/B SIDE VERTICAL CHORD FOUND CRACK. NR 3 PYLON INT AREA AT STA 346.4 O/B SIDE VERT FRAME CHORD REPAIRED AS PER HX RS R54-00-36429 REV A. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MAT'L 2024T62 0.090"SDR IPXA09B57417Wedge · delaminatedINSPECTION TYPE:C RIGHT I/B ELEVATOR T/E WEDGE LOWER SURFACE FOUND DELAMINATED FROM I/B 31 INCHES. RIGHT I/B ELEVATOR T/E COMPOSITE REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A REV 12.SDR IPXA09B55829Hinge Fitting · corrodedINSPECTION TYPE:N/A RT WING - NR 14 K/FLAP BULLNOSE FAIRING O/B HINGE FTG CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-02 AND 51-20-01 BLENDING WITHIN LIMIT AND REF UPS EO B747-5740-33385-A.SDR IPXA09B55849Fairing · crackedINSPECTION TYPE:D RT WING - NR 18 VC FLAP BULLNOSE FAIRING SURFACE SKIN FOUND CRACKED. RT WING NR 18 VC FLAP BULLNOSE FAIRING SKIN REPAIRED AS PER SRM 57-43-02 FIG 20 REPAIR 2 REV11, MATERIAL 202473 .056IN & REPAIR SIZE 4 .75 X 10 INCH.SDR IPXA09B55841Fitting · crackedINSPECTION TYPE:D LT WING NR 6 SPOILER LWR 'H' FTG O/B LWR AREA NR 3 HOLE FROM BOTTOM FOUND CRACKED RUNNING UPWARD AND I/B DOWNWARD CRACK LENGTH APPROX 0.040 INCH FOR BOTH CRACKS. LT WING NR 6 SPOILER LWR 'H' FTG O/B LOWER LUG REPAIRED AS PER RS R57-51-36307 SDR IPXA09B55785Fitting · crackedINSPECTION TYPE:D FWD CARGO COMPT DOOR AFT UPPER CORNER CLIP FOUND CRACKED. FWD CARGO COMPT DOOR AFT UPPER CORNER CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.SDR IPXA09B55784Fitting · crackedINSPECTION TYPE:D FWD CARGO COMPT DOOR FWD UPPER CORNER CLIP FOUND CRACKED. FWD CARGO COMPT DOOR FWD UPPER CORNER CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.SDR IPXA09B55783Fitting · crackedINSPECTION TYPE:D AFT CARGO DOOR FWD HINGE DOOR SIDE FWD UPPER CORNER CLIP FOUND CRACKED. AFT CARGO DOOR FWD HINGE DOOR SIDE FWD UPPER CORNER CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.SDR IPXA09B55845Web · crackedINSPECTION TYPE:D LT WING - ILES 1185 L/E NOSE FAIRING AFT WEB FOUND CRACKED. LT WING OLES 1185 L/E NOSE FAIRING AFT WEB REPAIRED AS PER RS R57-00-36311 REV A. REPAIR WITH MATERIAL 7075T6.063" SPLICE, REPAIR SIZE 5" X 6.25". UPS EO B747-5720-33425-A.SDR IPXA09B55844Web · crackedINSPECTION TYPE:D RT WING - ILES 1185 L/E NOSE FAIRING AFT WEB FOUND CRACKED. RT WING OLES 1185 L/E NOSE FAIRING AFT WEB REPAIRED AS PER RS R53-00-36311 REV A. REPAIR WITH MATERIAL 7075T6.063" REPAIR SIZE 5" X 6.25". UPS EO B747-5720-33425-A.SDR IPXA09B55815Cargo Track · crackedINSPECTION TYPE:D FWD CARGO RBL 45 STA 570 PALLET LOCK TRACK FOUND CRACKED. FWD CARGO COMPT BS 570 TO BS 590-875 RBL 45 TIE DOWN TRACK REPAIRED AS PER SRM 53-00-52 FIG 201 REPAIR 10 REV 11.SDR IPXA09B55782Floor Support · crackedINSPECTION TYPE:D FWD CARGO RBL 45" STA 570 FLOOR SUPPORT FOUND CRACKED. FWD CARGO COMPT BS 570 RBL 34.25" TO RBL 58.25" FORMER SUPPORT REPAIRED AS PER SRM 51-70-11 FIG 1 REV 11.SDR IPXA09B55756Flap · delaminatedINSPECTION TYPE:C RIGHT - I/B FOREFLAP TE LWR I/B AREA DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 11.SDR IPXA09B55836Support · damagedINSPECTION TYPE:D LT WING - NR 13 K/FLAP SUPPORT FRAME LWR CHORD MID AREA FOUND CORROSION CRACKED. LT WING - NR 13 K/FLAP SUPPORT FRAME LWR CHORD REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.SDR IPXA09B55834Mount Bracket · crackedINSPECTION TYPE:D RT WING - ILES 344 L/E FAIRING UPPER SUPPORT RIB AFT MOUNT BRACKET FOUND CRACKED. RT WING - ILES 344 L/E FAIRING UPPER SUPPORT RIB AFT MOUNT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.SDR IPXA09B55833Support · crackedINSPECTION TYPE:D LT WING - ILES 344 L/E FAIRING UPPER SUPPORT RIB AFT MOUNT BRACKET FOUND CRACKED. LT WING - ILES 344 L/E FAIRING UPPER SUPPORT RIB AFT MOUNT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.SDR IPXA09B55757Skin · delaminatedINSPECTION TYPE:C LEFT WING - O/B FORE FLAP T/E LWR SURFACE DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 11.SDR IPXA09B55755Skin · delaminatedINSPECTION TYPE:C RT WING O/B FORE FLAP T/E UPPER SURFACE I/B AREA DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 11.SDR IPXA09B55847Access Panel · wornINSPECTION TYPE:D NR 4 ENG - RT C-DUCT LWR FWD LATCH ACCESS PANEL FWD AND AFT EDGE WORN. NR 4 ENG RT C-DUCT LOWER FWD LATCH ACCESS PANEL FWD AND AFT EDGE REPAIRED AS PER UPS EO NO B747-7830-33315-A AND CMM 78-32-09 REPAIR 005. MATERIAL 17-7PH 0.085" AS REPAISDR IPXA09B55848Panel · corrodedINSPECTION TYPE:D LT WING I/B TRAILING EDGE MID FLAP I/B LOWER FWD PANEL AFT 82 INCHES FOUND CORRODED. LT WING I/B TRAILING EDGE MID FLAP I/B LOWER FWD PANEL AFT 82 INCH AREA REPAIRED AS PER HX RS NO R57-55-36310 REV A & UPS EO B747-5750-33412-A.SDR IPXA09B55843Panel · corrodedINSPECTION TYPE:D LT WING I/B TRAILING EDGE MID FLAP I/B LOWER AFT PANEL AFT 82 INCHES FOUND CORRODED. LT WING I/B TRAILING EDGE MID FLAP I/B LOWER AFT PANEL AFT 83 INCHES AREA REPAIRED AS PER HX RS R57-55-36310 REV A AND UPS EO B747-5750-33412-A.SDR IPXA09B55837Skin · delaminatedINSPECTION TYPE:D RT WING - NR 7 SPOILER LWR SURFACE FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED AS PER SRM REV 11 51-70-10 REPAIR 4 FIG 201.SDR IPXA09B55835Stiffener · crackedINSPECTION TYPE:D FUSELAGE AREA STA 1232 RBL 104 STIFFENER FOUND CRACKED. FUSELAGE BS 1152 TO BS 1232 RBL 104 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 11.SDR IPXA09B55851Fitting · crackedINSPECTION TYPE:D LHW - NR 6 SPOILER LWR 'H' FTG O/B LWR LUG FOUND CRACKED. LHW NR 6 SPOILER LOWER 'H' FTG OTBD LOWER LUG REPAIRED AS PER RS NR R 57-51-36307 REV A REPEAT INSPECTIONS IN REQUIRE AS PER RS NO R 57-51-36037 REV A REPAIR WITH MATERIAL 707576 .100SDR IPXA09B55850Fitting · crackedINSPECTION TYPE:D RT WING - NR 8 SPOILER 'H' FTG I/B LWR LUG FOUND CRACKED. RT WING NR 8 SPOILER 'H' FTG I/B LOWER LUG REPAIRED AS PER RS R-57-51-36307 REV A REPEAT DETAILED VISUAL INSPECTIONS IS REQUIRED AS PER RS R 57-51-36307 REV A REPAIR WITH MATERIAL 707SDR IPXA09B55832Rib · crackedINSPECTION TYPE:D RT WING GEAR W/W TRIANGLE PANEL I/B RIB FWD BRACKET FOUND CRACKED. RT WING GEAR W/W TRIANGLE PANEL I/B RIB FWD BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.SDR IPXA09B55781Skin · delaminatedINSPECTION TYPE:D RT WING - I/B FORE FLAP TRAILING EDGE I/B LWR SURFACE DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 11.SDR IPXA09B55842Seal · damagedINSPECTION TYPE:D DMI C397322 RT WING MISSING MID - FLAP T/E FLAP TO FUSELAGE SEAL. ORIGINAL COMPRESSION SEAL ASSY BETWEEN FROM CUSTOMER. VISUAL INSP PERFORMED SUPPORT TUBES FOUND WORN AND SUPPORT WEB CRACK FOUND. SUPPORT TUBES REPLACED AS PER SRM 57-52-01.SDR UPS08B54086Skin · damagedINSPECTION TYPE:N/A HOLE IN FUSELAGE 40 INCHES FWD OF LWR AFT CARGO DOOR BS 1770, BETWEEN STRINGERS 28R & 29R. FABRICATED PATCH PER EO B747-5330-31394A, AND SRM 53-00-01 OUT OF 2024 -T-3 .125 CLEANED DAMAGE ON A/C REPAIRS MATERIAL AND A/C ETCHED, ALODINE & PRSDR UPS08B53921Hmu · malfunctionedINSPECTION TYPE:N/A ENG NR 1 FAILURE ON FINAL WITH SUCCESSFUL AUTO RELIGHT. NR 1 FAILED AGAIN ON GROUND WITH ENG 1 CONTROL MESSAGE. WIND ON FINAL APPROACH TO 26L WAS OUT OF NORTH UP TO 50 KNOTS. REMOVED AND REPLACED NR 1 ENG HMU IAW MM 73-21-14, REMOVED ANDSDR EVA96001Flap Track · fracturedB-16407. DURING C01 CHECK, FRACTURE WAS DETECTED ON NR 5 FLAP TRACK (PN 65B17064-78) FWD END CLEVIS. THE FLAP TRACK HAD PERFORMED THE AD 2003-14-15 REQUIRED SB 747-57-2307 ACTION. THE DAMAGE PART HAD SENT TO MFG FOR ANALYSIS.SDR EVAS092018Door · damagedDURING CARGO LOADING, THE MAIN DECK CARGO DAMAGED BY THE LATCH/HOOK ACTUATOR. AIRCRAFT REPAIR PER SRM 52-00-01 FIGURE 204. THE REPAIR DOUBLER MADE FROM 0.125, 2024-T3 CLAD ALUMINUM SHEET, LOCATED ON MAIN DECK SIDE CARGO DOOR EXTERNAL SKIN (P/N:65B17701-1) ATSDR EVAS092016Hmu · failedDURING PUSHBACK, ENGINE FAILED TO START. CHECK SYSTEM, FOUND NO POWER TO ENGINE,TRY TO REPLACE HMU ON HELP,KEEP TROUBLESHOOTING FOUND THE FIRE HANDLE SWITCH OPERATION WAS NOT WELL,REPLACED THE SWITCH AND SYSTEM OPERATION CHECK NORMAL.SDR EVAE092014Actuator · leakingCAPTAIN REPORT: (GEAR TILT) MESSAGE,LANDING GEAR CANNOT RETRACT,AIRCRAFT AIR TURN BACK TO TPE. MAINTENANCE CHECK, FOUND THE HYDRAULIC TUBE OF RIGHT BODY GEAR TRUCK POSITION ACTUATOR LEAKING AND HYDRAULIC FUSE ACTIVED. REPLACED THE HYDRAULIC TUBE AND LEAK CHESDR EVAS092011Skin · corrodedDURING C08 CHECK, FOUND CORROSION ON RT WING EXTENTION LOWER SKIN UPPER SURFACE AT ERSS STA 1635. REMOVE THE CORROSION AND PERFORM NDI INSPECTION, ON FURTHER DEFECTS FOUNDSDR EVAS092009Skin · dentedDURING D02 CHECK FOUND A DENT IN THE LOWER EXTERIOR SURFACE OF FUSELAGE SKIN OF STA 528 STRINGER S-45L.DENT DIMENSION WAS 3"X1"X0.114".REFORM THE DENT IN SKIN WITH STANDARD PRACTICE.FABRICATE A REIN FORCED INNER DOUBLER FROM TI-6A1-4V 8.75"X5.25"X0.04".INSTALSDR EVAS092008Filter · cloggedDURING CRUISE FOUND NR 3 ENGINE OIL QUANTITY DROP TO ZERO & IN-FLIGHT SHUT DONE ENGINE. PERFORM ENGINE CHANGE. AFTER REMOVE GEARBOX FOUND OIL SCAVENGE FILTER WAS CLOGGED BY OBJECTS. SUSPECT IT IS TEFLON SEALSDR EVAS091024Bear Strap · corrodedCORROSION FOUND ON BEAR STRAP OF R3 DOOR CUTOUT 13191 LONG 16 RT. BLEND OUT THE CORROSION DAMAGE PORTION & PERFORM EXTERNAL REPAIR BY USING TWO DOUBLERS ON FUSELAGE SKIN PANEL.SDR E220405Module · failedSTS MAG "GEAR MOMNITOR" REPLACED GEAR CONTROL HANDLE MODULE PERFORM ALL LANDING GEAR ALTE EXTENSIN SYS TEST NML.SDR EVA200202Light · burned1.DURING DES (ABOUT 7,000') C/PURSER SMELT SMOKE/OVHT WIRE(ELECT) AT R1 DR. SELECT UTILITY BUS OFF, DECLARE EMERGENCY LANDING. UNEVENTFUL LANDING.2.ON GND CHECK FOUND 24/25 HK INDIRECT CEILING LIGHT FWD CONNECTOR DAMAGED.3.PER MM REPLACE THE FLOUSCENT LIGHT AN
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