Boeing 757-225
Service difficulty reports · 1,988
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 = '757225' 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 = '757225' 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 FDEA201111164938Crease Beam · corrodedRT CREASE BEAM CORRODED BS 440. REMOVED CORROSION FOUND TOOL MARKS OVER 50 PERCENT OF THE THICKNESS OF THE MATERIAL. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 DETAIL III. REMOVED CREASE BEAM IAW SRM 51-40-02. FABRICATED NEW CREASE BEAM IAW SRM 53-10-13 DSDR FDEA201111164937Crease Beam · gougedRT CREASE BEAM GOUGED BS 374. BLENDED GOUGE IAW SRM 51-10-00. CHECKED LIMITS FOUND DOUBLE DRILLED HOLE OUT OF LIMITS IAW SRM 53-00-51. REMOVED CREASE BEAM IAW SRM 51-40-02. FABRICATED NEW CREASE BEAM AND INSTALLED IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201111164935Crease Beam · gougedRT CREASE BEAM GOUGED AT STA 405. BLENDED GOUGE CHECKED LIMITS IAW SRM 53-00-51. MATERIAL REMOVED EXCEEDS 10 PERCENT, .040 REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, DRAWING III. REMOVED CREASE BEAM IAW 51-40-02 FABRICATED NEW CREASE BEAM IAW SRSDR FDEA201111114881Shear Tie · corrodedRT FRAME SHEAR TIE CORRODED BS 1681.0 S22-23R. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA MAX MATERIAL REMOVED .020 ORIG MAT, .050 REMAINING MAT .030 OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DET II. R & R SHEAR TIE IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201111114878Floorbeam · corrodedR2 DOOR ENTRANCE FLOORBEAM CORRODED, BS 324.0, RBL 30.0-62.0. REMOVED CORROSION, ORIGINAL MATERIAL .125 THICK AFTER REWORK .070 THICK L=5', W=2'D=.055, IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW-SRM-53-00-51. R & R TOP FLOORBEAM TEE IAW SRM-51-40-02. CAT "ASDR FDEA201111104870Skin · dentedFUSELAGE SKIN CREASED BS 1390-1410 S15-16L.SDR FDEA201111104868Frame · misrepairedFRAME AT BS 1400, STR 24-26L MISREPAIRED. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1028. MAJOR REPAIR.SDR FDEA201111084817Crease Beam · damagedMAIN DECK CREASE BEAM BS 900-1040 RT HAS AN ELONGATED HOLE. REMOVED EXISTING CREASEBEAM IAW SRM 51-40-02. . LOCATED, DRILLED AND INSTALLED NEW CREASEBEAM IAW SRM 51-10-02. TREATED AND PRIMED IAW SRM 51-20-01. APPLIED TOP COAT PER AMM 51-00-07. MAJOR REPAIRSDR FDEA201111084806Seat Track · corrodedMAIN CABIN SEAT TRACK, BS 1397-1404, RBL 45.50 UPPER SURFACE CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-02, FIG.101, SHEET 2 OF 6. REMOVED SEAT TRACK IAW SRM 51-40-02. INSTALLED NEW SEAT TRACK, BS 1320-1540, RBL 45.50, PESDR FDEA201111034737Skin · wrinkledFUSELAGE SKIN JUST AFT OF BS 660 TO 675 S20-23L HAS WRINKLING/BUCKLING. REPAIRED IAW SRM 51-40-02 & 53-00-01, REPAIR 16. MAJOR REPAIR.SDR FDEA201111024729Floor Panel · corrodedMAIN CABIN DECK PLATE STA 1681.8 TO STA 1720 BL-0 TO RBL-58 HAS SEVERAL AREAS OF CORROSION. R & R MAIN CABIN DECK PLATE, BS 1681-1720, RBL 58 - LBL 58, IAW SRM 51-40-02.SDR FDEA201111014717Seat Track · corrodedMAIN CABIN SEAT TRACK, BS 1180 TO 1280, RBL 45.50 HAS SEVERAL AREAS OF BARE METAL AND CORROSION. BLENDED CORRODED AREAS PER SRM 51-10-02. FOUND OUT OF LIMITS PER SRM 53-00-52, DETAIL 1, FIG.101, PAGE 102. REMOVED AND INSTALLED NEW SEAT TRACK PER SRM 51-40SDR FDEA201111014716Frame · misrepairedFRAME BS 1500, STR 24-26L MISREPAIRED. REMOVED FRAME IAW SRM 51-40-02. INSTALLED NEW FRAME IAW SRM 51-40-02, AND DWG 146N1030.SDR FDEA201110314696Seat Track · corrodedSEAT TRACK AT STA 440-530, LBL 45 NICKED, GOUGED & HAS SURFACE CORROSION. BLENDED AREAS IAW SRM 51-10-02. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1, FIG 101, PAGE 102. R & R SEAT TRACK AT LBL 45.50, BS 440-680, IAW SRM 51-40-02, 53-30-SDR FDEA201110284680Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 1661 BL 0 CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. R & R FLOORBEAM IAW SRM 53-60-51, AND DWG 146N5180. MAJOR REPAIR.SDR FDEA201110284682Seat Track · gougedMAIN CABIN SEAT TRACK BS 1220, RBL 24.75 UPPER LOBES GOUGED. GOUGE BLENDED IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101, DETAIL I, PG 102. ORIGINAL MATERIAL 0.145 LOSS 0.024 REMAINING 0.021. REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED SDR FDEA201110264658Frame · misrepairedFRAME AT BS 1320 STR 22L- 26L MISREPAIRED. REMOVED & REPLACED FRAME IAW SRM 51-40-02 AND DWG 146N1028.SDR FDEA201110254647Floorbeam · bentFLOORBEAM, STA 879 BL 0, BENT. FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, FIG.101, PAGE 101. REMOVED AND REPLACED FLOORBEAM PER SRM 51-40-02 AND DWG 143N5072.SDR FDEA201110254649Frame · misrepairedFRAME MISREPAIRED REPAIR AT BS 1440, S24-26L. R & R FRAME IAW SRM 51-40-02, AND DWG 146N1028. MAJOR REPAIR.SDR FDEA201110254648Frame · misrepairedFRAME AT BS 1540, STR 24L-26L MISREPAIRED. REMOVED & REPLACED FRAME IAW SRM 51-40-02 AND DWG 146N1030.SDR FDEA201110194587Floorbeam · corrodedFLOORBEAM UPPER TEE IS CORRODED BS 1681.8, LBL 25. CORROSION OUT OF LIMITS PER SRM 53-00-51, FIG.101, DETAIL 3. REMOVED FLOORBEAM IAW SRM 51-40-02. FABRICATED NEW FLOORBEAM IAW SRM 53-60-51 AND DWG 146N5091. INSTALLED IAW SRM 51-40-02 AND DWG 146N5091. MAJSDR FDEA201110194585Seat Track · damagedSEAT TRACK AT BS 365-440, RBL 45.50 HAS NICKS, GOUGES AND CORROSION. REMOVED CORROSION ON SEAT TRACK. ORIGINAL: .080", REMAINING: .062", FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 7, PAGE 104. REMOVED AND REPLACED SEAT TRACK PER SRM 51-40-0SDR FDEA201110194584Seat Track · damagedMDC SEAT TRACK AT BS 365-440 RBL 24.75 HAS SEVERAL NICKS, GOUGES AND CORROSION. REMOVED CORROSION ON SEAT TRACK, ORIGINAL MATERIAL .080", MATERIAL REMOVED .021", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG. 101, DETAIL VII, PAGE 104. REMOVED AND REPLACESDR FDEA201110184572Seat Track · damagedSEAT TRACK BS 879-900 LBL 24 NICKED & GOUGED. BLENDED DAMAGE IAW SRM 51-10-02 AND FOUND OUT OF LIMITS PER SRM 53- 00-52 FIG.101, DETAIL 1, PAGE 102. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02, AND DWG 143N5481. MAJOR REPAIR.SDR FDEA201110184573Seat Track · damagedSEAT TRACK BS 440-570 LBL 24.75 NICKED, GOUGED AND CORRODED. REMOVED CORROSION PER SRM 51-10-02. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, DETAIL 1, FIG.101, PAGE 102. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 & 53-00-52. MAJOR SDR FDEA201110144506Floorbeam · corrodedFLOORBEAM BS 1640, BL15L-R CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM 53-60-51, AND DRAWING 146N5180. FOUND TO BE CORRODED OUT OF LIMITS PER SRM 53-00-51, FIG.101, DETAIL 3, PAGE 103. MAJOR REPAIR.SDR FDEA201110144497Gate · gougedL4 DOOR LOWER GATE OTBD FWD AND AFT CORNERS GOUGED. REMOVED DAMAGE AND CHECKED LIMITS OF DAMAGE IAW SRM 52-10-02, SRM 51-10-02. OUT OF LIMITS FOR DAMAGE IAW SRM 52-10-02, FIG 101, DETAIL V. R & R L4 DOOR LOWER GATE AND OPS CHECKED IAW AMM 52-11-38, AMM 52-11SDR FDEA201110134474Seat Track · gougedSEC 41 SEAT TRACK BS 1180-1240, LBL 24.75 GOUGED AND CORRODED. BLENDED AREA ON SEAT TRACK PER SRM 51-10-02. FOUND OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 1, PAGE 102. ORIGINAL MATERIAL: .145", LOSS: .058:, REMAINING: .087". REMOVED SEAT TRACK IAW SSDR FDEA201110134484Seat Track · gougedSEAT TRACK, BS 1320-1540, LBL 45.50 GOUGED AND CORRODED. BLENDED SEAT TRACK IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201110134480Crease Beam · corrodedCREASEBEAM BS 1300-1320 LBL 58.22 CORRODED. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL 8, P 105. R & R CREASEBEAM IAW SRM 51-40-02, AND DWG 146N8322. MAJOR REPAIR.SDR FDEA201110114418Seat Track · corrodedMDC AT STA 377-440 LBL 24.45 SEAT TRACK HAS SEVERAL NICKS, GOUGES & CORROSION. REMOVED AND REPLACED SEAT TRACK PER SRM 51-40-02. REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 7; BEFORE: .050", AFTER: .030", LOSS: .020". MAJORSDR FDEA201110114420Seat Track · damagedMCD STA 377-440 AT LBL 45.50 SEAT TRACK HAS SEVERAL NICKS, GOUGES & CORROSION. R & R SEAT TRACK IAW-SRM-51-40-02. REMOVED CORR0SION FROM SEAT TRACK IAW SRM 51-10-02. CHECKED LIMITS ORIG MATERIAL WAS .070, AFTER REWORK .052, TOTAL MATERIAL LOSS WAS .028, FOUSDR FDEA201110104410Floorbeam · corrodedFLOORBEAM AT STA 365, RBL25 UPPER TEE CORRODED. REMOVED CORROSION ORIG MAT .125, AFTER BLEND .108, TOTAL MAT REMOVED .017, MAT. FOUND TO BE OUT OF LIMITS IAW SRM-53-00-51, FIG 101, DET III, REPAIRED FLOORBEAM IAW-SRM-53-00-51, FIG 201 REPAIR B NR 3. MAJOR SDR FDEA201109103818Fitting · corrodedAFT PRESSURE DECK UPON REMOVAL, FOUND FITTING CORRODED.SDR 22AA201000069AWindow · bindingAFTER LANDING AND ENGINE SHUTDOWN, UNABLE TO OPEN LT COCKPIT WINDOW, CRANK SKIPPING FRM NR 56-11-XA-02.SDR 22AA201000069Flex Line · leakingLT HYD DECREASED TO ZERO. AFTER LANDING AND ENGINE SHUTDOWN UNABLE TO OPEN LT COCKPIT WINDOW. CRANK SKIPPING FRM 56-11-XA-02. R & R DOWNLOCK ACTUATOR FLEXIBLE HOSE IAW AMM 20-10-10/401. SERVICED LT HYD RESERVOIR IAW AMM 12-12-01/301. SYS OPS CHECKED GOOD, NOSDR 22AA201000034Tire · damagedON TAKE OFF, EXCESSIVE N1 VIBRATIONS ON LT ENGINE, RETARDED THRUST LEVER TO IDLE ALL ENG PARAMETERS WITHIN LIMITS, ON POST FLIGHT FOUND LT REAR INNER TIRE CAP MISSING WITH EXCESSIVE DAMAGE. R & R NR 6 TIRE IAW MM 32-45-01, ACCOMPLISHED BORESCOPE INSP OF 1P COSDR 22AA200900033Shutoff Valve · malfunctionedRT ENG BLEED OFF LIGHT CAME ON AT FL 340, CABIN CLIMBED RAPIDLY EMERGENCY DESCENT RETURN TO DEPARTURE. LT ENG BLEED VALVE WAS DEFERRED IAW. T/S SYS IAW FIM 36-10-00, FOUND "B" NOT LEAKING AT 490 DEGREE SWITCH, REMOVE LINE CLEAN REINSTALLED, NO LEAKS NOTED, SDR USAA2009121193324Skin · corrodedCLT - RON - SKIN BULGE & POPPED RIVETS AT LOWER SKIN FUSELAGE STA 1450, S29R. A SUPPLEMENT WILL BE SUBMITTED UPON COMPLETION OF REPAIR. REPAIR COMPLETED.SDR 22AA200900027Shaft · sheared"L" OIL FILTER MSG OIL PRESS AND VIBRATION NORMAL 78 PSI, 0.7 N3 RESPECTIVELY, 79-21-06-01. IN CRUISE, PRIOR TO DESCENT, LT ENGINE FAIL. ACCOMPLISHED RB # 026248, REMOVED NR 1 ESN 30595 DUE TO RADIAL GEAR BOX SHAFT SHEARED. INSTALLED ESN 30700 IAW MM 71-00-SDR USAA20090831BB130Lock · missingTHE RT AFT SERVICE DOOR FWD LOCK GIRT BAR IS MISSING. MX REPALCED THE GIRT BAR LOCK ASSY. (K)SDR USAA2009821BB127Battery · dischargedCLT - F/A JUMPSEAT STATION AFT / CENTER EMERGENCY FLASHLIGHT BATTERY INOP. MAINTENANCE REPLACED EMERGENCY FLASHLIGHT BATTERY.SDR USAA20090817BB124Harness · frayedPHL - HARNESS FRAYED. MAINTENANCE REPLACED SLIDE.SDR USAA20090817BB123Light · inoperativeSJU-PHL WHILE INBOUND TO PHL, THE FLIGHT SHOWED A RT MLG UNSAFE LIGHT ON. CAPTAIN USED ALT EXTENSION PROCEDURE AND DID A FLY BY TO CONFIRM GEAR WAS DOWN BECAUSE ALT PROCEDURE DID NOT SHOW GEAR DOWN. FLIGHT LANDED SAFELY. MAINTENANCE PERFORMED BITE TEST ON PSDR USAA20090804BB120Windshield · crackedFLL - FLT 1211 - EN-ROUTE PHL TO SXM. FL370 TAKEOFF PLUS 220 HRS, CAPT'S FORWARD WINDOW TOTALLY SHATTERED. REPLACED CAPT NR 1 WINDOW.SDR USAA20090727BB119Plenum · damagedFLT 1018. F/A REPORTED ODOR IN CABIN ACCOMPANIED BY HAZE, POSSIBLE AIR CONTAMINATION, IN CRUISE & DESCENT. NO CONTAMINATION OR ODOR NOTICED IN COCKPIT. LANDED WITHOUT FURTHER INCIDENT. ACFT INSPECTED & RELEASED FOR A MX FLT. APPROX 2 HOURS INTO FLT, 2L LASDR USAA20090717BB113Retainer · corrodedPHL - L1 SLIDE TIME CHANGE FOUND GIRT BAR RETAINER PLATE CORRODED. REPLACED GIRT BAR RETAINER.SDR USAA20090709BB109Holder · brokenPHL - L2 DOOR HOLD OPEN IS BROKEN. REPLACED L2 DOOR HOLD OPEN ASSEMBLY.SDR 22AA200900004Fire Detector · false indicationDURING CLIMBOUT, PASSING THROUGH 12.000 FT, MAIN CARGO FIRE WARNING INDICATION. NO SMOKE NOR FIRE ON THE MAIN DECK, NOTIFIED ATC AND RETURNED TO DEPARTURE. DURING DESCENT AND APPROACH, THE FIRE WARNING WAS INTERMITTENT. REMOVED AND REPLACED SMOKE DETECTOR USDR USAA20090702BB108Switch · failedFLT 1488 - AFTER TAKEOFF, CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT (GEAR LEVER WOULD NOT GO BEYOND OFF POSITION). CAPTAIN DID NOT DECLARE AN EMERGENCY BUT DID ADVISE ATC THAT ACFT WAS RETURNING TO THE FIELD AND REQUESTED EQUIPMENT TO BE READY. CREW F
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