Boeing 757-24APF
Service difficulty reports · 16,054
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 = '75724APF' 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 = '75724APF' 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 IPXA2026022030189Unknown · fumesON TAKEOFF ROLL, FUMES WERE OBSERVED WITH AN ACRID WET SOCK ODOR. AT POWER REDUCTION TURNED RIGHT PACK OFF AND FUMES DISSIPATED. RAN NR 2 ENGINE AND PACKS NO FUMES PRESENT COULD NOT DUPLICATE. IAW AMM 71-00-00 BEGINNING FUEL QUANTITY 17.7 ENDING 17.4SDR IPXA2026021610589Line · unsecureAIR TURN BACK, EMERGENCY DECLARED. CLIMBING THROUGH 4000 RT ENG OIL PSI FLUCTUATED FROM 80-5 PSI. STOPPED CLIMB. RAN CK LIST AND SHUTDOWN RT ENG BEFORE LANDING UNEVENTFUL OTHERWISE. RESECURED/TORQUED LOOSE OIL SCAVENGE LINE IAW AMM 79-21-13. PERFORMED WINDMISDR IPXA2026021696516Light · inoperativeEXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS EXTERIOR EMERGENCY LIGHT ASSY IAW AMM 33-51-06-962-001-003. OPS CHECKED NORMAL.SDR IPXA2026021697269Windshield · failedDIVERSION, RT FWD WINDSHIELD STARTED ARCING THEN SHATTERED UPON REACHING TOP OF CLIMB. FL400. COMPLIED WITH QRH. DIVERTED TO SDF PER MOC & DISPATCH. REPLACED R1 WINDOW WITH REF TO MM 56-11-01-401. ACCOMPLISHED CONTINUITY CHECK OF R1 WINDOW HEAT SENSORS WISDR IPXA2026021396516Light · inoperativeEXTERIOR EMERGENCY LIGHT INOPSDR IPXA2026021397269Windshield · arcedRIGHT FWD WINDSHIELD STARTED ARCING THEN SHATTERED UPON REACHING TOP OF CLIMB. FL400. COMPLIED WITH QRH. DIVERTED TO SDF PER MOC & DISPATCH. ACCOMPLISHED SECOND TORQUE AT 1:27 LOCAL PER MM 56-11-01-401.SDR IPXA2026030476823Skin · damagedMAJOR REPAIR, UPPER FUSELAGE EXTERNAL SKIN AT BS 1370, S4L - S5L HAD A LIGHTNING STRIKE. TEMPORARY FASTENER INSTALLED. REMOVED FASTENER IN FUSELAGE FOR LIGTHNING STRIKE IAW SRM 51-40-02. INSTALLED DOUBLER IAW 53-00-01-2R-28, TABLE 205.SDR IPXA2026031739174Crease Beam · corrodedDURING MAIN CABIN BS 1200 FLOORBEAM REPAIR, AFTER REMOVAL OF RT OTBD WEB, BS 1180-1210, RBL 65. CREASE BEAM WAS FOUND WITH CORROSSION. REMOVED ONE CRACKED ANGLE & ONE WEB IAW SRM 51-40-02. INSTALLED NEW CHANNEL AND INSTALLED WEB IN LT MLG WW, BS 1180, THROUGSDR IPXA2026030239174Crease Beam · corrodedMAJOR REPAIR. DURING MAIN CABIN FLOOR BS 1200, FLOORBEAM REPAIR, AFTER REMOVAL OF RT OTBD WEB, BS 1180 - 1210, RBL 65 CREASE BEAM WAS FOUND WITH CORROSSION. WORK ACCOMPLISHED IAW EO-96522-REQ 1, & EA 757-5360-27-A4343 REV-.SDR IPXA2026022820240Tee Fitting · corrodedLOWER FUSELAGE BS 1220 LT SIDE TEE FITTING EXFOLIATED. INSTALLED A NEW TEE FITTING IAW SRM 51-40-02.SDR IPXA2026030318640Skin · dentedMAJOR REPAIR. SEVERAL SMALL DENTS ON TOP SKIN OF RT INBD FLAP. OUTER SKIN OF RT WING INBD MAIN FLAP ASSY WAS FOUND WITH ONE DENT OUT OF SRM 57-53-01-1A-1 ALLOWABLE LIMITS. THE DENT WAS TRIMMED OUT. CATEGORIZED AS A MAJOR REPAIR.SDR IPXA2026030320044Tee Angle · corrodedRIGHT FUSELAGE BS 1147 TEE ANGLE GOUGED AND CORRODED. INSTALLED A NEW TEE ANGLE, TWO STRAPS, & ONE ANGLE IAW SRM 51-40-02.SDR IPXA2026030320240Tee Angle · corrodedLOWER FUSELAGE BS 1220, LT SIDE TEE ANGLE EXFOLIATED.SDR IPXA2026022786894Skin · delaminatedMAJOR REPAIR, APU COMPT LOWER SKIN BELOW THE EXHAUST DUCT INNER SURFACE DELAMINATED AT BS 1992. THE PROTECTIVE COATING WAS RESTORED IAW AMM 51-21-15-370-802.SDR IPXA2026022486878Skin · delaminatedMAJOR REPAIR APU COMPT LH WALL INNER SKIN DELAMINATED IN AREA ABOVE THE OIL COOLER AIR EXIT DUCT. PREPARED AREA AND FABRICATED REPAIR PARTS IAW B757-200PF SRM 51-70-10-2R-4.SDR IPXA2026030387426Bracket · crackedLEFT MLG WW INBD SEAL RETAINER SUPPORT STRUCTURE BRACKET 6EA, FOUND CRACKED AFTER REMOVAL OF SEAL RETAINER BS 1060. INSTALLED NEW BRACKETS IAW SRM 51-40-02.SDR IPXA2026030291662Strap · corrodedSTR ACCESS DOOR313AL LOWER STRAP HAS CORROSION BETWEEN RBL 9 AND LBL 12. REMOVED COVER STRAP FOR ACCESS AND STRAP CORRODED IAW SRM 51-40-02-0G-0 INSTALLED AND PAINTED LOWER STRAP ACCESS DOOR 313AL BETWEEN RBL 9 AND LBL 12 IAW SRM 51-40-02SDR IPXA2026022593920Support Angle · corrodedFWD CARGO AT STA 863 BULKHEAD PANEL SUPPORT ANGLE LBL 19 - RBL 19 HAS CORROSION DOT 5842-11 REMOVED CORROSION AT THE STA 863 BULKHEAD PANEL SUPPORT ANGLE LBL 19 - RBL 19. I.A.W SRM 51-10-02. AFTER FURTHER EVALUATION IT WAS FOUND OUT OF LIMITS. I.A.W SRM 51-10-SDR IPXA2026021691664Transition Panel · dentedFWD CARGO TRANSITION PANEL AT STA 630 RBL 22 HAS A GOUGE. REMOVED DAMAGE SECTION OF WEB (SIDE PANEL). IAW WITH SREO-3220-REQ003 AND SRM 51-70-13 STEP 1. INSTALLED REPAIR PART ON SIDE PANEL AT STA 630 RBL22. IAW B757-200 WITH SREO-3220-REQ003, SRM 51-70-13 FRSDR IPXA2026030282338Frame · dentedMAJOR REPAIR. FWD CARGO BS 800 RT SIDE FRAME DENTED. WORK ACCOMPLISHED IAW EO-96553-REQ 1 & EA 757-5330-27-A4327, REV-.SDR IPXA2026030267696Bracket · corrodedACCESS DOOR 313AL LT & RT LATCH STOPS AT THE CUT-OUT, TWO BRACKETS ARE CORRODED. REMOVED ADJACENT STRIP AT BS 1885 TO FACILTATE MAINTENANCE, FOR REMOVAL OF ACCESS DOOR 313AL LT & RT LATCH STOPS AT THE CUT-OUT IAW SRM 51-40-02. INSTALLED TWO BRACKETS AND ADSDR IPXA2026022079132Skin · dentedSLAT NR 5 WITH SEVERAL DENTS IN THE UPPER SURFACE. REMOVED DAMAGE AND PREPARED AREA AT SLAT NR 5 2EA DENTS IAW B757-200 SRM 51-70-10-2R-0.SDR IPXA2026021468498Strap · corrodedAPU INLET DOOR FWD OF OPENING HAS CORROSION. REMOVED STRAP IAW SRM 51-40-02. INSTALLED NEW STRAP IAW SRM 51-40-02 IN APU INLET DOOR FWD.SDR IPXA2026020973228Lamp · inoperativeCOCKPIT EMERGENCY LIGHT, 5 LAMPS INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED NORMAL IAW AMM 33-51-00-501.SDR IPXA2026020673228Lamp · inoperativeCOCKPIT EMERGENCY LIGHT- 5 LAMPS INOPERATIVE. OPENSDR IPXA2026030360879Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL, BS 1040 - 1060, RBL 60 CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02-0G.SDR IPXA2026030359670Tee Angle · corrodedRIGHT WING TO BODY TEE ANGLE AT BS 1040 - 1059, RBL 40, INLET STRUCTURE CORRODED.SDR IPXA2026022760898Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL, BS 1040.2, RBL 40 - 60 CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02-OG.SDR IPXA2026022860882Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL AT BS 1040 - 1060, RBL 65 CORRODED. APPLICATION OF CIC ON INTERCOSTAL.SDR IPXA2026030360752Tee Angle · corrodedLEFT WING TO BODY, BS 1030 BEHIND PANEL 197AL TEE ANGLE CORRODED AT LBL 26. INSTALLED A NEW TEE ANGLE IAW SRM 51-40-02.SDR IPXA2026021949700Angle · puncturedCREW ENTRY DOOR, INNER SIDE, LOWER SILL, CLOSE TO LT STA 297, ANGLE SUPPORT HAS A HOLE. REMOVED FROM CREW ENTRY DOOR, INNER SIDE, LOWER SILL, BETWEEN LH STA 297 TO 333.45, ANGLE SUPPORT WITH A HOLE (MISDRILLED HOLE) IAW SRM 51-40-02 INSTALLED NEW ANGLE SUPPOSDR IPXA2026021950684Channel · crackedLH WW MLG, BULKHEAD 1180, UNDER PANEL 143XAL, VERTICAL BRACKET SUPPORT AT JOGGLE AREA HAS A CRACK. REMOVED LH WW MLG, BULKHEAD 1180, UNDER PANEL 143XAL, VERTICAL BRACKET SUPPORT IAW SRM 51-40-02-0G-0 INSTALLED NEW BRACKET SUPPORT LH WW MLG, BULKHEAD 1180, UNDSDR IPXA2026022350890Channel · crackedRH WW MLG, BULKHEAD 1180, UNDER PANEL 144XAR, VERTICAL BRACKET SUPPORT AT JOGGLE AREA HAS A CRACK. REMOVED RH W/W MLG BULKHEAD 1180 UNDER PANEL 144XAR ANGLE SUPPORT TO GAIN ACCESS IAW SRM 51-40-02-0G-0 INSTALLED NEW BRACKET SUPPORT ON RH WW MLG, BULKHEAD 118SDR IPXA2026021961043Shim · corrodedFAULT/STR/ZONE 100 EXTERIOR RIGHT SIDE. WINGB / BODY PANEL 198KR STRUCTURE HAS CORROSION. REMOVED 01 EA SHIM LOCATED BTW STA 1180 TO STA 1240 AND RBL57. IAW B757-200 SRM 51-40-02 INSTALLED SPACER SHIM IAW SRM B757-200 TASK: 51-40-02SDR IPXA2026020956799Warning Message · illuminatedEMERGENCY DECLARED. MOMENTARY CABIN ALTITUDE ALERTS IN FLIGHT FL 320 WITH RIGHT PACK ON, LEFT PACK OFF, RESTORED LT PACK IAW QRH CHECK LIST. CABIN CONTROLLABLE, NORMAL, PERFORMED MANUAL MODE CONTROL TEST OF CABIN PRESSURE CONTROL SYSTEM IAW AMM 21-31-00. OSDR IPXA2026030841896Tee Angle · corrodedRIGHT WING TO BODY TEE ANGLE AT BS 1060, RBL 10 - 40 HAS CORROSION AT NUTPLATE HOLES. INSTALLED TEE-ANGLE AND PLATES AT RT WING TO BODY IAW SRM 51-40-02.SDR IPXA2026030243996Panel · crackedNR 2 PYLON GAP PANEL HAS A CRACK IN LOWER SURFACE. INSTALLED ONE DOUBLER & FILLER WASHERS IAW SRM 51-40-02, AND SRM 57-41-01-2R-3, REPAIR 3.SDR IPXA2026022839378Frame · dentedAFT CARGO FRAME AT BS 1500 RT, DENTED. VERIFIED ACCOMPLISHMENT OF EO-96676-REQ1, AND EA 757-5360-27-A4324, REV- AS RII IAW UPS GMM 04-02-01-15.SDR IPXA2026030443086Tee Fitting · gougedFAULT - STR - Z100 - LH UPPER WING TO BODY T-CHORD AT STA 1147 HAS GOUGE ON EDGE DOT 5698-08 INSTALLED T-CHORD AT LH WING STA 1147 I.A.W. B757 SRM 51-40-02.SDR IPXA2026020942975Support · crackedLEFT MLG I/B SEAL RETAINER SUPPORT STRUCTURE HAS A CRACK IN THE CORNER AT BS 1060 VERIFIED INSTALLED SEAL RETAINER SUPPORT STRUCTURE AT LT MLG INBD BS 1060 IAW SRM 51-40-02.SDR IPXA2026022139192Frame · dentedMAJOR REPAIR, AFT CARGO FRAME AT STA 1300 RH IS DENTED. VERIFIED STEP 47. COMPLIED WITH EO-96677-REQ1, AND EA 757-5360-27-A4325, REV-.SDR IPXA2026030342999Tee Angle · corrodedLEFT WING TO BODY TEE ANGLE, BS 1260, BEHIND PANEL 197LL, CORRODED.SDR IPXA2026030340724Tee Angle · corrodedLEFT WING UNDER UPPER WING TO BODY PANEL 195BL HAD CORROSION. INSTALLED A TEE ANGLE IAW SRM 51-40-02.SDR IPXA2026030341147Doubler · corrodedRIGHT WING TO BODY TEE ANGLE, BS 1040 - 1059, RBL 40 - 60, INLET STRUCTURE HAD CORROSION. INSTALLED RAMP EXHAUST DOUBLER & PAX EXHAUST ASSY AT RT WING TO BODY TEE ANGLE IAW SRM 51-40-02-OG.SDR IPXA2026030244157Floorbeam · corrodedMAJOR REPAIR. MAIN CABIN FLOORBEAM, STA 1200 RBL 45-65 CORRODED. WORK ACCOMPLISHED IAW EO-96554-REQ 1, & EA 757-5360-27-A4326, REV-.SDR IPXA2026021744310Seat Track · corrodedMAJOR REPAIR. MAIN CABIN FLOOR STRUCTURE, STA 1160-1200 BL 0 SEAT TRACK CORRODED. DOT 28-28 REMOVED CORROSION IN SEAT TRACK I.A.W. B757-200 SRM 51-10-02 INSTALLED REPAIR PARTS IAW B757-200PF SRM 53-00-52-2R-7 STEP 10 AND B757-200PF SRM 51-40-02-0G-0SDR IPXA2026022243116Skin · corrodedMAJOR REPAIR, L/H PYLON INBD INNER SKIN BETWEEN BETWEEN PANELS 433JR ANS 433HR HAS EVIDENCE OF CORROSION AT LOWER AREA. MARKED IN RED PERFORMED BLENDOUT OF DAMAGE ON L/H PYLON INBD INNER SKIN BETWEEN PANELS 433JR AND 433HR, IAW 757-200PF SRM 51-10-02. ACCOMPSDR IPXA2026021734376Floorbeam · corrodedMAIN CABIN FLOOR STRUCTURE, FLOOR BEAM STA 1680 RBL 25-65 HAS (3EA) AREAS WITH EXFOLIATION. REMOVED DAMAGE IAW SRM 51-10-02. REQUEST NDT TO VERIFY DAMAGE FREE. HEFC AND ROTO. RE-ACCOMPLISHED DECK PLATE REPAIR USING SRM REV 124 CHAPTER 53-60-51-2R-8 REPAIR 8.SDR IPXA2026022344163Seat Track · corrodedF MAIN CABIN FLOOR STRUCTURE, STA 1160-1200 LBL 45 SEAT TRACK CORRODED. REMOVED CORROSION IN SEAT TRACK I.A.W. B757-200 SRM 51-10-02 AND EVALUATED I.A.W. B757-200 SRM 53-00-52-1A-1. REMOVED SEAT TRACK FROM LBL 45 STA 1180 TO STA 1320 IAW B757 SRM 51-40-02. SDR IPXA2026021927248Bracket · crackedFAULT-STR-ZONE 200: AIR COND. DUCT AT CABIN CEILING STA 1680 SUPPORT BRACKET IS CRACKED. REMOVED MAIN CABIN SUPPORT BRACKET IAW B757-200PF SRM 51-40-02 INSTALLED NEW BRACKET IAW SRM 51-40-02
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