Boeing 757-204
Service difficulty reports · 676
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 = '757204' 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 = '757204' 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 FDEA202502060189Floor Panel · damagedFLOOR PANEL 222MEF HAS FRAYED DAMAGE FABRICATED FLOOR PANEL 222MEF ZONE 220 ON VTMAE TRAVELER #T24/1796467 IAW MAE DWG PL11861182-1 REV G. MAJOR REPAIRSDR FDEA202502060190Floor Panel · frayedFLOOR PANEL 221 BF HAS FRAYED DAMAGE FABRICATED FLOOR PANEL 221 BF ZONE 220 ON VTMAE TRAVELER # T25/1796462 IAW BOEING DWG PL141N5370 REV CY MAJOR REPAIRSDR FDEA202502050181Floor Panel · damagedFLOOR PANEL 222MBF HAS FRAYED DAMAGE FABRICATED FLOOR PANEL 222MBF ZONE 220 ON VTMAE TRAVELER #T25/1796466 IAW MAE DWG PL11861182-14 REV G. MAJOR REPAIRSDR FDEA202502050180Floor Panel · damagedFLOOR PANEL 221 MBF HAS FRAYED DAMAGE. FABRICATED FLOOR PANEL 221MBF ZONE 220 ON VTMAE TRAVELER #T25/1796463 IAW MAE DWG PL11861182-16 REV G, MAJOR REPAIR.SDR FDEA202502040173Seat Track · corrodedSEAT TRACK AT STA 348 LBL 8 HAS CORROSION-DOT 45-012 REMOVED AND REPLACED SEAT TRACK AT BS 348 LBL 8 IAW SRM 51-40-02 AND SRM 53-10-52-01, PART MARK IAW GMM 07-0-1001, MAJOR REPAIRSDR FDEA202501310163Intercostal · crackedMAIN DECK FLOOR AREA LOWER INTERCOSTAL EDGE SKIN HAS PUNCTURED @ STA.1680 RBL 25. 16-46 REMOVED SPLICE IAW SRM 51-40-02, CUTOUT DAMAGE AREA IAW SRM 53-00-21-2R, PERFORMED HFEC SURFACE INSPECTION, NO CRACK NOTED IAW NTM 51-00-19, FABRICATED NEW REPAIR PARSDR FDEA202501310162Intercostal · crackedMAIN DECK FLOOR AREA LH SIDE @ STA 16-61 LOWER BEAM INTERCOSTAL HAS CRACK. CUTOUT AND REMOVED DAMAGE AREA (1.65") IAW SRM 53-00-51-2R PERFORMED HFEC SURFACE INSPECTION IAW NTM 51-00-19, NO CRACK NOTED. FABRICATED 01 EA STRAP AND 01 EA FILLER IAW SRM 53-00-SDR FDEA202412161810None · no discrepancyGROUNDING NOTICE RECEIVED FOR A PREVIOUS REPAIR NEEDING RII BUYBACK AND SDR. CONFIRMITY INSPECTION AND HFEC OF PREVIUS REPAIR (W/O# 00079725, N/R 272 HAS BEEN COMPLIED WITH. NO DEFECTS NOTED. REF SRM 53-00-07, EA F-5310-T0381469 AND NDTM PT6. AMM 25-50-02SDR FDEA202411261739Flap System · malfunctionedSELECTING FLAPS 25 GOT TE FLAPS DISAGREE WITH FLAPS 20. AMM: 27-51-00-5 PERFORMED OPERATIONAL TEST OF FLAP SYSTEM IRW AMM 27-51-00-5. CYCLED THROUGH ALL POSITIONS TWICE. OPS CHECK GOODSDR FDEA202410281596Skin · crackedFREIGHT ULD HIT AIRCRAFT AND CREATED A HOLE ON R/H OF A/C AFT OF AFT CARGO DOOR UPDT 25OCT24 08:28 EWR SRM 53-00-00-0G DAMAGE FOUND AROUND STATION 1608 (SECTION 46) . DAMAGE DIMENSIONS ARE 10 FROM FWD TO AFT AND 9 FROM TOP TO BOTTOM WHILE BEING 2 1/SDR FDEA202410021413Connector · damagedR FWD ENTRY DOOR ON EICAS AT TOUCHDOWN. REPEAT WRITE UP. RELEASED FOR SERVICE PER MEL : 52-71-01-A. R CREW ENTRY DOOR INDICATION SYSTEM - INOP. VERIFY THATCREW ENTRY DOOR IS CLOSED, LATCHED, AND LOCKED BEFORE EACH DEPARTURE. USE HAND SIGNALS OR VERBAL COMSDR FDEA202409261382Warning Message · illuminatedON SHORT FINAL, ONCE THE GEAR WAS EXTENDED, WE RECEIVED R FWD ENT DOOR EICAS MESSAGE ACCOMPANIED BY THE OVERHEAD ENTRY DOORS DISCRETE LIGHT. THE ACARS BLOCKED THE FLIGHT IN ON TOUCHDOWN, AND THEN THE LIGHT WENT OUT. FACT 27SEP24 00:19 CDG AMM: 52-71-0SDR FDEA202409261372Plunger · looseON FINAL APPROACH AROUND 2500 AGL, RECEIVED RT ENTRY DOOR EICAS. MESSAGE WENT AWAY ON TOUCHDOWN. CREW ENTRY DOOR INDICATION SYSTEM INOP. VERIFY THAT CREW DOOR IS CLOSED, LATCHED & LOCKED BEFORE EACH DEPARTURE. USE HAND SIGNALS OR VERBAL COMMUNICATIONS TOSDR FDEA202409041227Battery Pack · inoperativeDURING MX PRE-FLIGHT CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT SIGN (L31), AND L1 SLIDE LIGHT (L25)WILL ONLY STAY ILLUMINATED FOR APPROX 2 SECONDS. FACT 03SEP24 22:20 SWF AMM: 33-51-07-2 KEPT A/C POWERED UP FOR 3 HOURS AND ATTEMPTED EMERGENCY EXITSDR FDEA202408161131Actuator · failedRUDDER TRIM OPERATES EXTREMELY SLOW TO NOSE LEFT AND NOT AT ALL NOSE RIGHT. FOUND RUDDER TRIM ACTUATOR U/S AMM 27-21-06-2. REPLACED RUDDER TRIM ACTUATOR IAW AMM 27-21-06-2. OPERATIONAL TEST OK. A/C OK FOR SERVICE.SDR FDEA202408011119Handle · unsecureMDIS 927 52-10 0097 01AUG24 15:54 AMS FACT DURING LAYOVER FOUND L1 ENTRY DOOR OUTSIDE HANDLE NOT CLOSING PROPERLY FACT 02AUG24 09:03 CDG AMM: 52-11-00-2 AMM: 52-11-00-6 PERFORMED L1 DOOR INSPECTION CHECK AS PER AMM 52-11-00-6. NO DEFECT SDR FDEA202403230357Door · malfunctionedL1 DOOR NOT FUNCTIONING PROPERLY, UNABLE TO OPEN FROM OUTSIDE RELEASED FOR SERVICE PER MEL : 52-11-01-A: L1 DOOR INOP AMM: 52-11-01-A L1 DOOR INOP C/7391449. OPERATED L1 DOOR FROM BOTH INSIDE AND OUTSIDE USING ONE AMT, OPENED AND CLOSED WITH NO ISSUSDR FDEA2023012380154Floor Panel · wornDURING REMOVAL, FOUND FLOOR PANEL WORN. REPLACED THE FLOOR PANEL IAW DWG SRZ-25-005.SDR FDEA2023012380153Floor Panel · wornDURING REMOVAL FOUND FLOOR PANEL WORN. REPLACED THE FLOOR PANEL IAW DWG SRZ-25-005.SDR FDEA202211272849Fseu · failedTE FLAP DISAGREE ON FINAL. EXECUTED GO AROUND. RAN TE FLAP DISAGREE PROCEDURE IAW QRH. LANDED UNEVENTFULLY. EMERGENCY DECLARED. PERFORMED FSEU BITE TEST AND FOUND CODE 305 IAW FIM 27-51, TREE 805, PERFORMED TREE 805 AND OPS NORMAL, NO FAULTS FOUND IAW MSDR FDEA202211022709Fseu · failedGOING FROM FLAPS 0 TO 1 RECEIVED A TE FLAP DISAGREE. INDICATOR FROZEN BETWEEN 0 & 1. ACCOMPLISHED QRH & LANDED CDG. EMERGENCY DECLARED. AMM 27-51-01-2 NO HISTORY FOR TE DISAGREE ALERT, NO EXISTING FAULT & NO PREVIOUS FLIGHT FAULT IN ALL THREE FSEU'S, T/S SDR FDEA202210112537Engine · power lossON TAKEOFF ROLL, F/O FLYING, ACFT TOOK A LOT OF RT RUDDER AT CLIMB OUT, LT ENG 5-10% LOWER N1 & SLIGHTLY LOWER EPR. INCREASED POWER ON LT ENG TO MATCH RT. RT ENG INCREASED SLIGHTLY ON IT`S OWN & GOT A COMPRESSOR STALL, 2 QUICK BANGS. RETARDED RT ENG POWER & SDR FDEA202210072519Skin · debondedRH AFT FLAP IN INBD UPPER TRAILING EDGE DISBONDED REPAIRED TRAILING EDGE FLAP AS REQUIRED PER 757 SRM 57-53-01-2R (REPAIR 1, FIG 201, SHEET 5)AND SRM 51-70-05.SDR FDEA202210072518Skin · debondedLH AFT FLAP IN INBD UPPER TRAILING EDGE DISBONDED REPAIRED TRAILING EDGE FLAP AS REQUIRED PER 757 SRM 57-53-01-2R (REPAIR 1, FIG 201, SHEET 5)AND SRM 51-70-05.SDR FDEA202209202348Line · leakingTAXING IN AFTER LANDING, WHILE MAKING THE LEFT TURN FROM TAXIWAY C ONTO C8, THE TILLER LOST RESPONSIVENESS FOLLOWED BY A MASTER CAUTION ALERT AND L HYD SYS PRESS EICAS MESSAGE. VERIFIED ZERO HYD QUANTITY AND PRESSURE. COORDINATED A MX TOW IN WITH COMPANSDR FDEA202207261802Slide Raft · deployedPDIS 927 25-60 8270 23JUL22 TLV FACT U INADVERTENT SLIDE DEPLOYMENT. HANDLE WAS IN THE ARMED POSITION AND SLIDE DEPLOYED BUT DID NOT INFLATE. IDENTIFIED PARTSSLIDE/RAFT MPN: D30654-131 CPN: 2520951 QTY: 1 ***L1 ESCAPE SLIDE MISSINSDR FDEA202206271601Switch · inoperativePDIS 927 33-20 8208 27JUN22 CGN FACT U L1 SLIDE DISARM LIGHT IS INOP. FACT 27JUN22 20:28 CGN U ADJUSTED GIRT BAR PROXIMITY SWITCHES I.A.W. 25-66-11-2. CHECKED OK. A/C GOOD FOR SERVICE.SDR FDEA202204170980Tube · crackedON CLIMB OUT AT APPROX 4000 R ENG STARTED A SLOW ROLLED BACK. 2000 POUND FF LESS THAN L ENG WITH CORRESPONDING ENG PERFORMANCE. WE WATCHED IT AND CLIMBED TO 16K WHERE ENGINE FF HAD FALLEN TO 4000ILB. LOWER THAN THE LEFT AND NO PERFORMANCE FROM R ENG. SDR FDEA202202070240Seat Track · corrodedMAIN CABIN SEAT TRACK HAS CORROSION ON SEVERAL NUT PLATE HOLES LOCATED BET STA 1140 AND STA 1200 LBL 45. REMOVED AND REPLACED SEAT TRACK FROM STA 1180-1240 LBL 45 IAW SRM 51-40-02, MAJOR REPAIR.SDR FDEA202202010172Seat Track · corrodedMAIN CABIN SEAT TRACK HAS CORROSION ON SEVERAL NUT PLATE HOLES LOCATED BET STA 1100 AND STA 1180 RBL 45. REMOVED CORROSION IAW SRM 51-10-02, ORIGINAL MATERIAL 0.080", MATERIAL LOSS 0.018", REMAIN 0.062", FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FABRICATED SDR FDEA202109302436Transmitter · faultedTE FLAP ASYM ON EXTENSION BETWEEN 0 AND 1 DEGREES. FOLLOWED QRH PROCEDURE AND DECLARED EMERGENCY. UNEVENTFUL LANDING. FIM 27-51 FAULT TREE 809 FOLLOWED: - FSEU #1 READOUT AT FLAPS 20 POSN RH 274.13 LH 253.59 - LT FLAP POSITION TRANSMITTER REQUIRES REPSDR FDEA202107261867Indicator · malfunctionedGEAR LIGHT IN THE COCKPIT TO THE RIGHT OF THE GEAR INDICATORS DID NOT ILLUMINATE DURING THE GEAR DOWN PROCESS. THE BULB CHECKS GOOD. ANNUNCIATOR LIGHTS TEST PFD IAW AMM 33-16-00. FOUND ALL BULS ATIS. LDG GEAR POS IND AND WARNING SYS TEST PFD IAW AMM 32-61SDR FDEA202106101522Seat Track · corrodedCORROSION FOUND ON SEAT TRACK LOCATED BETWEEN STATION 1020 AND 1060 RBL 58.22 REPLACED SEAT TRACK AT RBL 58.22 STATION 1020 TO 1080 BY SPLICING IN NEW SECTION OF BAC 1520-792 PER SRM 53-00-52-2R REPAIR 1 OPTION 1 PER EA F-5320=T0361821SDR FDEA202106101487Frame · crackedCRACK COMES OUT FROM RIVET HOLE ON THE FRAME WEB BS 1240 BETWEEN STR 9R TO 8R PERFORMED FUSELAGE FORMED ZEE FRAME REPAIR PER SRM 53-00-07, REPAIR 3, FIG 201, DETAIL 1 DEFERRED ITEM NO 2. THIS REPAIR IS A CAT B PERMANENT REPAIR.SDR FDEA202105311423Skin · damagedDOT(137-05) LH WING I/B MAIN FLAP UPPER SURFACE HAS SEVERAL HAIL DAMAGED. REPAIRED L/H WING I/B MAIN FLAP UPPER SURFACE IAW SRM 57-53-01-1A AND 51-70-07, MAJOR REPAIR.SDR FDEA202105291421Floor Panel · delaminatedMAIN CARGO COMPARTMENT FLOOR PANEL 231MGF IS DELAMINATED AND DAMAGED. FABRICATED FLOOR PANEL 231MGF ON VT MAE TRAVELER T21/1551858 IAW DWG SRZ-25-005 REV R. MAJOR REPAIRSDR FDEA202105291420Floor Panel · delaminatedLH MAIN CARGO COMPT FLOOR PANEL 231MCF IS DELAMINATED AND DAMAGED. FABRICATED FLOOR PANEL 231MCF ON VT MAE TRAVELER T21/1551856 IAW DWG SRZ-25-005 REV R. MAJOR REPAIRSDR FDEA202105271413Drag Fitting · cracked#1 PYLON INBD DRAG FITTING HAS A CRACK INDICATION AT #3 HOLE. ACCOMPLISHED EA #F-5740-T0361812, TITLE: WINGS-ATTACH FITTINGS-DRAG FITTING #3 CRACKED HOLE-FEDEX EO F-5730-E0340076 PART 1 REV B- BOEING SB757-57A0073 STEPS 1 AND 2, MAJOR REPAIR.SDR FDEA202105261406Floor Panel · delaminatedCOURIER FLOOR PANEL 221MBF DELAMINATED. FABRICATED ZONE 220 COURIER FLOOR PANEL 221MBF ON VTMAE TRAVELER #T21/1550764 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.SDR FDEA202105261405Floor Panel · delaminatedCOURIER FLOOR PANEL 222MAF DELAMINATED. FABRICATED ZONE 220 COURIER FLOOR PANEL 222MAF ON VTMAE TRAVELER # T21/1550761 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.SDR FDEA202105261404Floor Panel · delaminatedLAVATORY FLOOR PANEL 221BF DELAMINATED. FABRICATED FLOOR PANEL 221BF ON VTMAE TRAVELER #T21/1550763 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.SDR FDEA202105211336Floor Panel · damagedMAIN CARGO COMPT FLOOR PANEL 231MSF HAS A DAMAGED AREA LOCATED AT FWD LH EDGE . FABRICATED FLOOR PANEL 231 MSF ON TRAVELER T21/1551857 IAW SRZ-25-005 REVISION R MAJOR REPAIRSDR FDEA202105211337Floorboard · damagedMCD FLOORBOARD PNL 232 MTF HAS DAMAGE. FABRICATED MCD FLOORBOARD 232 MTF ON TRAVELER # T21/1551859 IAW DWG SRZ-25-005 REVESION R MAJOR REPAIRSDR FDEA202105181285Warning Message · false activationTE FLAP DISAGREE EICAS MESSAGE ON APPROACH. COMPLIED WITH QRH PROCEDURES, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. T/ S PER 757 F.I.M. 27-51 TREE 808. ALSO PERFORMED FSEU BITE TEST PER AMM 27-51-01-2. NO CURRENT FAULTS. OPERATED FLAPS FULL TRAVEL SDR FDEA202103230757Shoulder Belt · wornPDIS 927 25-20 7038 23MAR21 HEL FACT U LOGPAGES:3300263 CA S SHOULDER HARNESS QUICK RELEASE TAB DOES NOT WORK LAP BELT 2 EA AND LOCK REPLACED ACC TO AMM 25-11-04-4SDR FDEA202103160796Skin · dentedFOUND A DENT ON SLAT #6 O/B TRAILING EDGE 10.5" FROM O/B TO 3.8" FROM TOP REPAIRED #6 SLAT UPPER T/E WEDGE 9.752 FROM OUTBOARD EDGE AND 4.5" FROM UPPER IAW IAW SRM 57-43-02-2R REPAIR 4 FIG 201 THIS IA A CAT A MAJOR REPAIRSDR FDEA202103030546Flap Track · looseR/H O/B MAIN FLAP TRACKS #7 AND #8 ARE LOOSE AT AFT ATTACH POINTS REPLACED AFT ATTACH POINTS HARDWARE ON R/H O/B MAIN FLAP TRACKS #7 AND #8 IAW AMM 27-51-15SDR FDEA202103030544Flap Track · looseL/H O/B MAIN FLAP TRACKS #1 AND #2 ARE LOOSE AT AFT ATTACH POINTS. REPLACED AFT ATTACH POINTS HARDWARE ON L/H O/B MAIN FLAP TRACKS #1 AND #2 IAW AMM 27-51-15SDR FDEA202102190761Drag Fitting · corrodedCORROSION FOUND DURING NOT INSPECTION ON L/H ENG #1 DRAG AND DIALONAL BRACE IN THE FOLLOWING HOLES 2,3,6,8,9,10,14,16 REMOVED CORROSION FROM HOLES #2,3,6,8,9,10,14,16, AND 16. CRACKS FOUND AT HOLES #3 AND #9. REPLACED INBOARD AND OUTBOARD DRAG BRACE FITTING ISDR FDEA202102180762Drag Fitting · corrodedCORROSION FOUND DURING NDT INSPECTION ON RH ENG #2 DRAG FITTING DIAGONAL BRACE HOLES #1, 2, 3, 5, 6, 8, 10, 11, 13, 14, 15, 16, 17, AND 18. REMOVED CORROSION FROM HOLES #1, 2, 3, 5, 6, 8, 10, 11, 13, 14, 15, 16, 17, AND 18. CRACKS FOUND AT HOLES #4 AND #9. REP
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