Boeing 757-2B7
Service difficulty reports · 3,730
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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 = '7572B7' 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 = '7572B7' 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 USAABB08136Light · inoperativeBOS - THE EMERGENCY ESCAPE SLIDE LIGHT WAS INOPERATIVE AT THE R4 DOOR. MAINTENANCE REPLACED THE R4 DOOR EMERGENCY ESCAPE SLIDE LIGHT ASSEMBLY. OPERATIONALLY CHECKS OK. (S)SDR USAABB08134Slide · malfunctionedCLT - THE CABIN CREW FAILED TO DISARM THE L2 DOOR, RESULTING IN A PARTIAL EMERGENCY ESCAPE SLIDE DEPLOYMENT. MAINTENANCE REPLACED THE L2 DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. (S)SDR 08FDEA03427Seat Track · damagedUPON REMOVAL OF SEAT TRACK AT LBL 24, BS 540-640, MAIN CABIN, IT WAS DISCOVERED THAT THERE WERE SEVERAL EXISTING ELONGATED FASTENER HOLES. TWO EACH AT BS 540-620 AND ONE EACH ON THE FOWARD SIDE OF BS 640. REPAIRED SEAT TRACK PER MAE EA 757-5335-16-F0975, REVSDR USAABB08132Slide · failedPHL - WHILE PARKED AT A REMOTE GATE, THE L1 DOOR WAS ACCIDENTALLY OPENED WHILE THE EMERGENCY EVACUATION SLIDE WAS STILL ARMED. THE SLIDE DEPLOYED, BUT DID NOT INFLATE. MAINTENANCE REPLACED THE EMERGENCY EVACUATION SLIDE AT THE L1 DOOR. OK FOR SERVICE. (S)SDR USAABB08145Inverter · inoperativePHL FLT 798 ENROUTE PHL TO AMS. THE STANDBY ATTITUDE INDICATOR FAILED ABOUT 45 MINUTES AFTER DEPARTURE. THE DECISION WAS MADE TO RETURN TO PHL. THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. MX REPLACED THE STANDBY HORIZON INVERTER. OPS CHECKS OK.SDR FDEA200808073305Seat Track · corrodedSEAT TRACK LBL 45 STA 440-680 CORRODED AND SCALLOPS DAMAGED IN NUMEROUS LOCATIONS. FABRICATED SEAT TRACK FROM STA 440 TO 680 LBL 45.5 IAW MAE TRAV NR T8/739184 AND IAW SRM 53-00-52, INSTALLED SEAT TRACK IAW SRM 51-40-02, MAJOR REPAIR.SDR 08FDEA03305Seat Track · corrodedSEAT TRACK LBL 45 STA 440-680 CORRODED AND SCALLOPS DAMAGED IN NUMEROUS LOCATIONS. FABRICATED SEAT TRACK FROM STA 440 TO 680 LBL 45.5 PER MAE TRAV NR T8/739184 AND IAW SRM 53-00-52. INSTALLED SEAT TRACK IAW SRM 51-40-02, MAYOR REPAIR.SDR USAABB08125Connector · damagedPHL FLT 1209 PHL TO SXM - DURING TAKEOFF ROLL, TNE NR 2 ENG WOULD NOT DEVELOP TAKEOFF POWER. THE CREW ABORTED THE TAKEOFF AT 60 KNOTS AND RETURNED TO THE GATE. MAINTENANCE REPAIRED THE CONNECTOR ON THE FUEL FLOW GOVERNOR SOLENOID. OPERATIONALLY CHECKS OK. SDR FDEA200807303180Seat Track · corrodedMAIN CARGO DECK SEAT TRACK STA 1540-1640 LBL 24 CORRODED REMOVED SEAT TRACK IAW SRM 51-41-02. RECEIVED AND FABRICATED NEW SET TRACK ON M.A.E TRAV NR T8/746699, MAT ID BAC1520-792, 7178T6511 IAW SRM 53-00-52 FIG. 201, BATCH NR 00013400254 AND LOCATED, TRIMED, SDR 08FDEA03180Seat Track · corrodedMAIN CARGO DECK SEAT TRACK STA 1540-1640 LBL 24 CORRODED REMOVED SEAT TRACK IAW SRM 51-41-02. RECEIVED AND FABRICATED NEW SEAT TRACK ON MAE TRAV NR T8/746699, MAT ID BAC1520-792, 7178T6511 IAW SRM 53-00-52 FIG 201, BATCH NR 00013400254 AND LOCATED, TRIMMED, ASDR USAA920081426Skin · debondedCLT - IRAN - MAJOR REPAIR - NR 10 SLAT HAS DISBONDING AT INBOARD AFT CORNER OF THE UPPER SKIN. REPAIRED NR 10 SLAT AT INBOARD AFT CORNER OF THE UPPER SKIN IAW US AIRWAYS EA NR100580. (S)SDR USAABB124Fan · failedMCO FLT 816 EN-ROUTE CUN TO CLT. CREW RECEIVED NUMEROUS LAVATORY SMOKE DETECTOR WARNINGS, AND AN ODOR OF SMOKE IN BOTH THE COCKPIT AND CABIN. ALSO RECEIVED AN APU OVERHEAT MESSAGE. THE FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANSDR USA2008F00018Apu · malfunctionedMCO FLT 816 EN ROUTE CUN TO CLT. CREW RECEIVED NUMEROUS LAVATORY SMOKE DETECTOR WARNINGS, AND AN ODOR OF SMOKE IN BOTH THE COCKPIT AND CABIN. ALSO RECEIVED AN APU OVERHEAT MESSAGE. THE FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCESDR USAABB08127Duct · leakingLAS FLT 790 LAS-CLT - THE CREW RECEIVED A RT ENG OVERHEAT WARNING ON TAKEOFF, RESULTING IN AN IN-FLIGHT SHUTDOWN. THE FLIGHT RETURNED TO FIELD LAS AND LANDED WITHOUT FURTHER INCIDENT. THERE WAS 30 MINUTES SINGLE ENG TIME. MAINTENANCE REPLACED A LEAKING RT ESDR USAABB08122Circuit Breaker · malfunctionedFLL FLT 811 EN ROUTE PHL TO CUN. DURING CRUISE, RECEIVED A LT UTILITY BUS OFF MESSAGE. ATTEMPTS TO RESET WERE UNSUCCESSFUL. THE CREW DECIDED TO STOP IN FLL TO HAVE MAINTENANCE REPAIR THE ACFT. THE FLIGHT DIVERTED TO FLL WITHOUT FURTHER INCIDENT. MAINTENANSDR USA2008F00008Fan · out of balancePHL - FLT 722 EN ROUTE (PHL TO DUB). DURING CLIMBOUT FROM PHL THE RT ENGINE INDICATED VIBRATION OF 2.5 WITH SPIKES UP TO 2.8. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A FAN TRIM BALANCE. VIBRATION LEVELS WITHISDR USA2008F00007Flashlight · defectivePHL - THE FORWARD FLIGHT ATTENDANT FLASHLIGHT STATUS LIGHT DID NOT BLINK, BUT WAS OTHERWISE OPERATIONAL. MAINTENANCE REPLACED THE FLASHLIGHT. OPERATIONALLY CHECKS OK. (A)SDR USAABB08117Drain Line · crackedPLEASE REVISE RECORD FROM USAABB08116 TO USAABB08117. PHL FLT 723 EN-ROUTE DUB TO PHL. DURING DESCENT INTO PHL, THE LEFT HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO AND THE SYSTEM PRESSURE LIGHT ILLUMINATED. ALSO, EICAS MESSAGE "G L HYD SYS PRESS" DISPLAYSDR USA2008F00010Drain · crackedPHL FLT 723 - EN ROUTE DUB TO PHL. DURING DESCENT INTO PHL, THE LT HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO AND THE SYSTEM PRESSURE LIGHT ILLUMINATED. ALSO, EICAS MESSAGE "G L HYD SYS PRESS" DISPLAYED. THE FLIGHT LANDED SAFELY AND WAS ABLE TO TAXI OFF THSDR USA2008F00009Drain · crackedPHL FLT 723 EN ROUTE DUB TO PHL. DURING DESCENT INTO PHL, THE LT HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO AND THE SYSTEM PRESSURE LIGHT ILLUMINATED. ALSO, EICAS MESSAGE "G L HYD SYS PRESS" DISPLAYED. THE FLIGHT LANDED SAFELY AND WAS ABLE TO TAXI OFF THE SDR 08FDEA02580Floorbeam · corrodedCABIN FLOORBEAM, HAS CORROSION, BS 1640, LBL 6 - RBL 6. COMPLIED WITH EA F-5310-110867, REV -, DATED 05/20/2008. EA CLASSIFIED REPAIR AS A MAJOR REPAIR.SDR 08FDEA02486Seat Track · damagedBS 440-640, LBL 24, SEAT TRACK HAS DOUBLE DRILLED HOLES AND GOUGES AROUND CLIPNUT HOLES. REMOVED DAMAGE SEAT TRACK IAW SRM 51-40-02. ALL DAMAGE TO SEAT TRACK IS OUT OF LIMITS PER SRM 53-00-52. FABRICATED A NEW SEAT TRACK, ON TRAVELER NR T8/741233, AND INSSDR 08FDEA02389Frame · dentedAFT CARGO COMPARTMENT, LT SIDE, STA 1340, S026L, FRAME IS DENTED. REPAIRED DENTED FRAME BY INSTALLING A FABRICATED DOUBLER REPAIR, ON MAE TRAVELER NR T8/741854, IAW SRM 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED AS A CATAGORY "A" MAJOR REPAIR.SDR 08FDEA02388Frame · dentedAFT CARGO COMPARTMENT LT STA 1460 S-26L, FRAME IS DENTED. CUT OUT DAMAGED AREA IAW SRM 53-00-01, FIG 201. NDT, HFEC IAW NTM 51-00-00, FIG 6, OF CUT OUT AREA. FABRICATED SPLICE ANGLE IAW SRM 53-00-07, MAT. 7075T6, .071 INCH C, BATCH NR 532681, PO NR MST 0023SDR USAA920081262Flap · delaminatedCLT - C-22 - MAJOR REPAIR - FOUND DELAMINATION ON LEFT OUTBOARD AFT FLAP MEASURES 4"X4.5", 5.5" FORWARD OF TRAILING EDGE. REPAIRED DELAMINATION ON LEFT OUTBOARD AFT FLAP 4"X4.5" AREA., 5.5" FORWARD OF TRAILING EDGE IAW B757 SRM 57-53-01. (S)SDR USAA920081251Angle · corrodedCLT - RON - MAJOR REPAIR - CORROSION FOUND ON ANGLE IN BOTTOM OF R2 DOOR AT BS 710. REPAIRED CORROSION FOUND ON ANGLE IN BOTTOM OF R2 DOOR AT BS 710 IAW BOEING B757 DRAWING 143N6100. (S)SDR USAA920081244Skin · crackedBFM - C2 - MAJOR REPAIR - LT WING LEADING SLAT NR 2 COVE PANEL SKIN ALONG OUTBOARD TRACK HINGE FITTING HAS A CRACK. REPAIRED LT WING LEADING EDGE SLAT NR 1 COVE PANEL SKIN ALONG OUTBOARD TRACK HINGE FITTING IAW B737 SRM 51-20-05. (S)SDR 08FDEA02346None · noneACCOMPLISHED BOEING SB 757-54-0035, R2, PARA. 3, PART 3, STRUCTURE CHANGES FOR THE NR 2 STRUT, EXCEPT STEO Q, PANEL 5, PER FEDEX EA F-5450-108907, DATED 11 OCT 2007. COMPLIED WITH FEDEX EA F-5450-108907A, DATED 28 MAY 2008 ON W/C T F-5450-108907A, WRI 5450017SDR 08FDEA02345None · noneACCOMPLISH SB 757-54-0035, R2, PARA 3, PART 2; WING STRUCTURE CHANGES FOR THE NR 2 STRUT AND RT WING PER EA F-5450-108907, DATED 11 OCT 2007. ACCOMPLISHED SB 757-54-0035, PART 2, ON NR 2 STRUT, AS PER EA F-5450-108907A, DATED 28 MAY 2008. PER EA, SCHEDULE EOSDR FDEA200806172288Skin · corrodedSTRUT NR 2 INBD SIDE OF SKIN AT APPROX PPS 200.50 HAS EXFLOIATED CORROSION (APPEARS TO BE TRAVELING UNDER FRAME/CORD ALSO). REMOVED SKIN IAW SRM 51-40-02. REMOVED CORROSION AT STA 157, ORIGINAL MATERIAL THICKNESS .090", REMAINING THICKNESS .062", OUT OF LIMITSDR USAA920081245Skin · delaminatedBFM - C2 - MAJOR REPAIR - LT WING LEADING EDGE SLAT NR 3 AFT WEDGE UPPER AND LOWER SKIN APPROX 28 INCHES FROM INBOARD AND 8 INCHES FROM AFT EDGE HAS DELAMINATION. REPAIRED LT WING LEADING EDGE SLAT NR 3 AFT WEDGE UPPER AND LOWER SKIN IAW B757 SRM 57-43-02 & 5SDR 08FDEA02288Skin · corrodedSTRUT NR 2 INBOARD SIDE OF SKIN AT APPROX PPS 200.50 HAS EXFOLIATED CORROSION (APPEARS TO BE TRAVELING UNDER FRAME/CORD ALSO). REMOVED SKIN IAW SRM 51-40-02. REMOVED CORROSION AT STA 157, ORIGINAL MATERIAL THICKNESS .090 INCH, REMAINING THICKNESS .062 INCH, SDR USAABB08106Bellows · blownCUN - FLT 808 EN-ROUTE CUN TO CLT. ON CLIMBOUT, AT FL290, THE RIGHT ENGINE INDICATED AN OVERHEAT CONDITION. THE CREW REDUCED THE THRUST SETTING. HOWEVER, THE INDICATION DID NOT GO OUT. THE CREW SHUT DOWN THE RIGHT ENGINE AS REQUIRED PER PROCEDURES, AND RESDR USA2008F00005Slide · low pressurePHL - THE R4 DOOR EMERGENCY ESCAPE SLIDE PRESSURE WAS IN THE RED ZONE. MAINTENANCE REPLACED THE R4 DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. (K)SDR USA2008F00004Engine · overheatedCUN FLT 808, ENROUTE CUN TO CLT. ON CLIMB-OUT, AT FL290, THE RIGHT ENGINE INDICATED AN OVERHEAT CONDITION. THE CREW REDUCED THE THRUST SETTING HOWEVER, THE INIDCATION DID NOT GO OUT. THE CREW SHUTDOWN THE RIGHT ENGINE AS REQURIED IAW PROCEDURES, AND RETURNED TSDR FDEA200806122246Stringer · corrodedBS 1440, STRINGER 28R, AFT CARGO DOOR LOWER SILL AREA, IS CORRODED. REMOVED CORROSION IAW SRM 53-00-03, FIG 1, DETAIL 3. CORROSION REMOVAK WAS 100% THROUGH MATERIAL. REMOVED AND REPLACED STRINGER 28R, FROM BS 1380 - 1457 IAW SRM 53-00-03 AND 51-40-02. THISSDR USAA920081214Skin · delaminatedBFM - C2-MAJOR REPAIR - TAXK CARD NR JL-900-09000 - RIGHT WING NR 6 SLAT HAS AREA OF DELAMINATION. REPAIRED RIGHT WING NR 6 SLAT IAW SRM 57-43-01 AND 51-70-10. (K)SDR USAA920081213Strap · crackedBFM - C-2 - MAJOR REPAIR - NR 6051543 - FLOORBEAM STRAP CRACKED AT BS 1300 RBL 25. REPAIRED FLOORBEAM STRAP AT BS 1300 RBL25 IAW SRM 51-70-11. (K)SDR BB08104Megaphone · damagedMCO - THE AFT MEGAPHONE WAS FOUND DAMAGED AND INOPERATIVE. MAINTENANCE REPLACED THE AFT MEGAPHONE. OPERATIONALLY CHECKS OK.SDR USAA920081175Skin · debondedMCN - MAJOR REPAIR - A CHECK WINGLET MOD - RT WING NR 10 SLAT TRAILING EDGE HAS 2 AREAS THAT ARE DEBONDED, SS 790 AND SS 802. REPAIRED RT WING NR 10 SLAT TRAILING EDGE, SS 790 AND SS 802 IAW B757 SRM 51-70-10 REPAIR 2 AND 4. (S)SDR 08FDEA02077Skin Panel · gougedRIGHT WING T/E O/B FLAP NOSE SKIN TOP SIDE HAS GOUGE. REMOVED RIGHT WING T/E FLAP NOSE SKIN IAW SRM 51-40-02. RECEIVED NEW PART P/N 113N3500Y28. INSTALLED NEW SKIN IAW SRM 51-40-02.SDR BB08103Power Supply · no testCLT - THE EMERGENCY LIGHT POWER SUPPLY OVER L3 DOOR WILL NOT TEST. MAINTENANCE REPLACED THE POWER SUPPLY UNIT FOR THE L3 DOOR. OPERATIONALLY CHECKS OK.SDR 08FDEA02070Seat Track · gougedSTA 440-640 RBL 24 SEAT TRACK HAS HOLE AND GOUGES AROUND CLIPNUTS HOLE. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK ON MAE TRAVELER T8/741234 MAT BAC1520-792-7178-T6511. INSTALLED NEW SEAT TRACK AND SPLICE REPAIR ON STA 440-530 IASDR USAA920081215Strap · crackedBFM - C2 - MAJOR REPAIR - TASK CARD 19C11053005 -FLOOR SUPPORT STABILIZER STRAP CRACKED AT BS 365.25 - 377.7, LBL 25. REPAIRED FLOOR SUPPORT STABILIZER STRAP AT BS 365.25 - BS 377.7, LBL 25 IAW SRM 51-40-02 AND 53-35-01. (K)SDR USAA920081225Fitting · crackedWINGLET MOD/ ETOPS MOD - NR 6110937, LEFT WING RIB 22 LOWER FITTING CRACKED, WS 681.5. REPLACED LEFT WING RIB 22 LOWER FITTING, WS 681.5 IAW DWG 112N5136. (K)SDR 08FDEA02000Skin · dentedEXTERNAL FUSELAGE LOWER SKIN, APPROX BS 255, STR 27L, DENT WITH GOUGE. ACCOMPLISHED A MAJOR REPAIR IAW EA F-5330-110861, WITH A RELEASE DATE OF 5/9/08. THERE IS NO FOLLOW UP TRACKING OR REPETITIVE INSPECTIONS REQUIRED FROM THIS REPAIR.SDR USAA920081173Battery · dischargedMCN - EMERGENCY EQUIPMENT - ETOPS WINGLET MOD - MAIN CABIN FLASHLIGHT INOPERATIVE WHEN BATTERY LEADS ARE CONNECTED. REMOVED AND REPLACED BATTERY ON MAIN CABIN FLASHLIGHT. (S)SDR BB08094Fuse · blownCLT - THE EXTERIOR EMERGENCY LIGHTS AT L2, L3 & R3 WERE FOUND INOPERATIVE. MAINTENANCE REPLACED A BLOWN FUSE AT POWER SUPPLY UNIT M733. OPERATIONALLY CHECKS OK.SDR BB08095Link · bindingCLT - DURING THE R2 DOOR EMERGENCY EVACUATION SLIDE OPERATIONAL TEST, THE R2 DOOR DID NOT OPEN, AND THE DOOR ASSIST BOTTLE DID NOT DISCHARGE DUE TO A BINDING LINK. MAINTENANCE REPLACED DOOR ASSIST BOTTLE LINK. SYSTEM OPERATIONALLY CHECKS OK.SDR BB08093Slide · low pressureMCO - THE R-2 DOOR EMERGENCY ESCAPE SLIDE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE R-2 DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE.
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