Boeing 757-24APF
Service difficulty reports · 16,046
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 IPXA2026041803176Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRINGER UPPER FLANGE HAS CORROSION APPROX BTW BS 1460 AND BS 1480, RBL 16.10, ID STICKER NUM, (085-041) ATA 53-10 VERIFIED STEP 6. OK TO INSTALL.SDR IPXA2026050883072Skin · crackedRH WING BETWEEN SLAT# 8 AND #9 ON FIXED LEADING EDGE SKIN IN CRACKED. COMPLIED WITH STEP FOR EO-97223-REQ1 AND VT-MAE EA 757-5741-27-A4443, REV-, PRIOR TO FURTHER FLIGHT IS DOCUMENTED ON T3F18E008PRFYSDR IPXA2026041984059Angle · corrodedRIGHT WTB PANEL LANDING, 2ND FROM FWD, AT UPPER WING ROOT HAS SURFACE CORROSION. 83-021. ATA 53-030 INSTALLED (3EA) NUTPLATES ON FWD SUPPORT ANGLE AND (3EA) NUTPLATES ON AFT SUPPORT ANGLE AT RT WTB UPPER WING ROOT STA-925, WL-208.1. I.A.W. SRM 51-40-02-0G-0 PASDR IPXA2026043078576Angle · crackedAFT CARGO R/H AFT. WALL ANGLE SUPPORT ZONE 164 FOUND CRACK. ES-009. REMOVED CRACKED AFT CARGO RT AFT. WALL ANGLE SUPPORT AT STA 1640 RBL 24.8 IAW SRM 51-40-02-0G-0. INSTALLED FABRICATED SUPPORT ANGLE P/N 453N1809-36SAAU AND REINSTALLED VERTICAL BULKHEAD PANEL SDR IPXA2026042382776Tie Down · corrodedFWD CARGO RH OTBD TRANSITION HAS CORROSION BS 770 - 800. REMOVED CORROSION AT R/H STA. 780 ON TIE DOWN FITTING RBL 20R IAW 51-10-02-0G-0. INSTALLED NEW TIE DOWN FITTING AT FWD CARGO BS 780 RBL 20R IAW SRM 51-40-02-0G-0.SDR IPXA2026042382902Sidewall Support · corrodedFWD CARGO LH LOWER SIDEWALL SUPPORT FRAME CORRODED STA 740 STR. REMOVED CORROSION ON L/H LOWER SIDEWALL SUPPORT AT BS 740 BTW STR 22R-26R IAW B757-200PF SRM 51-10-02-0G-0. CORROSION REMOVAL IS 100% MAT'L LOSS, PART WILL BE REMOVED AND REPLACED. INSTALLED SIDSDR IPXA2026042783844Support Channel · corrodedAFT WTB LOWER FAIRING PANEL LANDING CHORD AT APPROX. BS 1217 HAS EXFOLIATED CORROSION. 83-015. REMOVED 1EA EXFOLIATED CHORD (CHANNEL) AT AFT WTB LOWER FAIRING AREA BTW BS 1180 AND 1220 RBL 7 IAW SRM 51-40-02-0G-0. INSTALLED 1 E/A NEW PART CHANNEL SUPPORT AND RSDR IPXA2026043083949Support Angle · crackedSTR- RH AFT WTB LOWER FAIRING PNL LANDING SUPPORT BRACKET HAS EVIDENCE OF A CRACK. 83-018. REMOVED SUPPORT BRACKET AT RH AFT WTB LOWER FAIRING PNL IAW B757-200PF SRM 51-40-02-0G-0 REV 124- 20 SEP 2025. INSTALLED SUPPORT BRAKET AND ATTACHED BEAM AT STR - RH AFTSDR IPXA2026042884007Angle · corrodedRIGHT WTB FWD PANEL LANDING AT UPPER WING ROOT HAS SURFACE CORROSION. 83-020. REMOVED (1EA) FWD SUPPORT ANGLE AND (1EA) AFT SUPPORT ANGLE FROM RH WTB UPPER WING ROOT STA-900, WL-208.1 I.A.W. B757-200PF SRM 51-40-02-0G-0 PARAG.7. INSTALLED FWD AND AFT SUPPORT ASDR IPXA2026042982498Strap · corrodedAFT CARGO RT OTBD CEILING PROFILE CORRODED BS 1420 - 1440, REMOVED CORROSION ON CEILING PROFILE STABILIZATION STRAP AT BS1420, RBL 24.75 ON BOTH UPPER AND LOWER SURFACES IAW SRM 53-00-51-1A-1. INSTALLED NEW STABILIZATION STRAP RBL 24.75 BETWEEN BS 1440-1360 SDR IPXA2026041183869Skin · dentedEXTERNAL FUSELAGE BETWEEN BS 1700 - 1720, S16-17L DENTED. COMPLIED WITH EO-97220-REQ1 AND EA 757-5360-27-A4433.SDR IPXA2026041183937Skin · dentedEXTERNAL FUSELAGE SKIN BETWEEN BS 1720 - 1743, S29L - 28L HAS A PROTRUDING DENT. ACCOMPLISH REPAIR PER EO-97221-REQ1 & EA 757-5380-27-A4434.SDR IPXA2026042384007Angle · corrodedRH WTB FWD PANEL LANDING AT UPPER WING ROOT HAS SURFACE CORROSION.SDR IPXA2026042383844Support Channel · corrodedAFT WTB LOWER FAIRING PANEL LANDING CHORD AT APPROX. STA. 1217 HAS EXFOLIATED CORROSION.SDR IPXA2026042383814Tee Angle · corrodedAFT WTB LOWER FAIRING PANEL LANDING CHORD AT STA. 1220 HAS EXFOLIATED CORROSION. REMOVED EXFOLIATED CHORD FROM AFT WTB LOWER FAIRING AREA AT STA 1220 BTW RBL 30 AND LBL 30 REF B757 SRM 51-40-02-0G-0. INSTALLED 1 E/A NEW PART CHORD TEE P/N 149N7701-36 B/N 00SDR IPXA2026042382439Transition Panel · corrodedAFT CARGO RH OTBD TRANSITION PANEL CORRODED STA 1440-1500. REMOVED CORROSION AT RT BS 1440 ON TIE DOWN FITTING RBL 20R IAW 51-10-02-0G-0. INSTALLED NEW RT OTBD TRANSITION PANEL IN AFT CARGO COMPARTMENT BS 1440-1528 IAW SRM 51-40-02-0G-0.SDR IPXA2026042176560Strap · corrodedWHILE EVALUATING CORROSION AT APU INLET SURROUND STRUCTURE FOUND CORROSION AT APU INLET AFT STRAP AT STA 1825 BETWEEN STR 3R-6R. CORROSION FOUND ON MIDDLE STRAP OUTER SURFACE ONLY. REMOVED AND BLENDED SMOOTH THE CORROSION IAW SRM 53-80-15-1A-1 PARA 3. REINSTALSDR IPXA2026042280199Skin · corrodedAFT CARGO DOOR INNER SKIN LOWER WEB CORRODED IN SEVERAL PLACES. REMOVED 36 E/A FASTENERS AND CORROSION ON AFT CARGO DOOR INNER SKIN LOWER WEB BETWEEN BS 1380-1440 AT 11" FROM LOWER EDGE IAW SRM 51-40-02-0G AND 51-10-02-0G. INSTALLED 36 E/A FASTENERS ON AFT CSDR IPXA2026041882776Transition Panel · corrodedFWD CARGO RT OTBD TRANSITION HAS CORROSION STA 770-800.SDR IPXA2026041782902Sidewall Support · corrodedFWD CARGO LH LOWER SIDEWALL SUPPORT FRAME CORRODED STA 740.SDR IPXA2026042865233Floorbeam · corrodedMAJOR REPAIR, FWD CARGO CEILING MAIN CABIN FLOORBEAM UPPER FLANGE LOWER SURFACE EXFOLIATED RT OTBD SIDE BS 879, ACCOMPLISHED REPAIR IAW EO-97324-REQ1 AND EA 757-5310-01-B0710, REV IR, PRIOR TO FURTHER FLIGHT.SDR IPXA2026042965161Crease Beam · damagedFWD CARGO COMP RT LOWER CUSP FITTING BS 760 HAS TOOL MARKS. REMOVED FWD CARGO COMP RT LOWER AFT CUSP FITTING AT BS 760 IAW SRM 51-40-02-0G-0. LOCATED, DRILLED AND INSTALLED CUPS TIE (FITTING) AT FWD CARGO COMP R/H LOWER AFT BS 760 IAW SRM 51-40-02.SDR IPXA2026042265976Angle · corrodedAFT CARGO RT AFT BULKHEAD PANEL STA. 1640 SUPPORT FOUND CORROSION. AFTER FURTHER EVALUATION REPORTED CORROSION FOUND ON AFT CARGO R/H AFT UPPER BULKHEAD PANEL LANDING AT STA 1640 FROM LBL45.50 TO RBL 60 IS 50% MATERIAL LOSS FOUND TO BE OUT OF 10% REWORK LIMITSDR IPXA2026042265216Transition Panel · corrodedFWD CARGO RH OTBD TRANSITION PANEL CORRED AT STA 620 STR ATA 53-00 GM028. REMOVED CORROSION ON FWD CARGO RH OTBD TRANSITION PANEL AT STA 620, ORIGINIGINAL THICHINESS 0.063" ALLOWABLE MAT. REMAINING 10% = .006" LOSS MATERIAL .002" AREA FOUND WITHIN LIMITS IASDR IPXA2026042065233Floorbeam · corrodedFWD CARGO CEILING MAIN CABIN FLOOR BEAM UPPER FLANGE LOWER SURFACE EXFOLIATED RH OTBD SIDE STA 879. FABRICATED REPAIR PARTS AS SHOWN IN FIG. 2, -1 ANGLE (2 EACH) -2 FILLER (1 EA) AND -4 FILLER (2 EA) IAW 757-5310-01-B0710 REV P2 STEP 9.SDR IPXA2026042153361Strap · corrodedAPU INLET SURROUND STRUCTURE FWD STRAP O/B CORNER HAS CORROSION. REMOVED 1EA FWD STRAP, 1EA UPPER SUPPORT ANGLE, 1EA UPPER CORNER ANGLE, 1EA LOWER SUPPORT ANGLE ON APU INLET SURROUND STRUCTURE BETWEEN STA 1787.45- 1825 AND BETWEEN STR 3R-6R REF B757-200PF SRSDR IPXA2026050134931Retainer · corrodedAPU COMPARTMENT FWD BULKHEAD STA 1885 HORZ STRIFFENER JUST BELOW LIGHT SWITCH ASSY HAS AREAS OF LITE CORROSION, BENT AND DOOR HOOK DAMAGED WITH SEVERAL SHEARED FASTENERS. REMOVED 01EA DAMAGED HOOK (RETAINER) FROM APU COMPARTMENT FWD BULKHEAD STA 1885.20 IAW B7SDR IPXA2026043035211Bracket · corrodedAPU COMPARTMENT FWD BULKHEAD STA 1885 CEILING WIRE HARNESS CLAMP SUPPORT BRACKETS 6 EACH UPPER AND LOWER SIDES HAVE LITE CORROSION AND MISSING PROTECTIVE FINISH. REMOVED CORROSION ON 6EA BRACKETS AT APU COMPARTMENT FWD BULKHEAD STA 1885 CEILING WIRE HARNESS MASDR IPXA2026041134931Stiffener · inoperativeAPU COMPARTMENT FWD BULKHEAD STA 1885 HORZ STRIFFENER JUST BELOW LIGHT SWITCH ASSY HAS AREAS OF LITE CORROSION, BENT AND DOOR HOOK DAMAGED WITH SEVERAL SHEARED FASTENERS. RLOO7 PROD AUDIT C/WSDR IPXA2026042143555Clamp · crackedFWD CARGO O2 BOTTLE RETAINER IS CRACKED AND TENSION STRAP IS SECURED CORRECTLY. REMOVED FWD CARGO CRACKED O2 BOTTLE RETAINER FRONT HALF ASSY IAW BOEING 757-200PF SRM 51-40-02-0G-0. INSTALLED NEW FWD CARGO O2 BOTTLE RETAINER FRONT AND REAR HALF ASSY, AND TORQUSDR IPXA2026042142345Angle · corrodedAFT CARGO. CORROSION ON 2 EA NUT PLATES AND STIFFNER BTWN STA 1715 AND AFT PRESS BULHEAD. BTWN 12 RBL AND 24 RBL. 61. REMOVED 2EA STIFFENER AT AFT CARGO BTW STA 1701 AND PRESS BULKHEAD, BTW 24RBL AND 12RBL IAW B757-200PF SRM 51-40-02-OG-0 ,PAR-4 REV 124 -20SDR IPXA2026042142289Angle · corrodedAFT CARGO. CORROSION ON NUT PLATE AND STIFFNER. BTWN STA 1715 AND AFT PRESS. BULKHEAD BTWN. 33 RBL AND 39 RBL. 61. REMOVED 1EA STIFFENER AT AFT CARGO BTWN STA 1701 AND AFT PRESS. BULKHEAD BTW 62RBL TO 45RBL IAW SRM 51-40-02-OG-0, PAR 4 REV 124-20 SEP 2025. ISDR IPXA2026042142204Angle · corrodedAFT CARGO. CORROSION ON NUT PLATE AND STIFFNER BTWN BS 1715 AND AFT PRESS. BULKHEAD 45LBL - 24.74 LBL 61. REMOVED DAMAGED NUTPLATE ASSY FROM STIFFNER PER B757-200PF SRM 51-40-02. OK TO FABRICATE REPLACEMENT NUTPLATE ASSY FROM SHT-7075T6- .063" BATCH 00029SDR IPXA2026041735211Support Bracket · corrodedAPU COMPARTMENT FWD BULKHEAD STA 1885 CEILING WIRE HARNESS CLAMP SUPPORT BRACKETS 6 EACH UPPER AND LOWER SIDES HAVE LIGHT CORROSION AND MISSING PROTECTIVE FINISH. RL014 VERIFIED STEP #18 C/W INSTALLATION.SDR IPXA2026042143284Doubler · corrodedRT FWD LAV DUMP VALVE ADAPTER PLATE CORRODED. REMOVED PLATE FOR ACCESS FROM R/H FWD LAV DUMP VALVE ADAPTER REF. B757-200PF SRM 51-40-02-OG-0, UPON FURTHER EVALUATION FOUND 100% OF MAT. LOSS. USED CALIPER ID#23-2023 DATE DUE 10-MAY-2026. INSTALLED REPLACEMENT SDR IPXA2026040311723Overheat Sys · false activationEMERGENCY DECLARED, EQUIP OVRHT MSG @ FL 390. DID QRH CHECKLIST YET MSG REMAINED. WENT AWAY @ 1200" AGL. ALSO REF 21-58-00-710-802-011 STEP D. AND STEP E. NO OVER HEAT NOTED. INSTALLED FWD AIR FILTER REF AMM 21-58-21-201 OPS CHECK GOOD SEE ATTACHED PICTURE FSDR IPXA2026040487396Support Bracket · corrodedWING TO BODY FAIRING STR, RH FWD UPPER WING, BTW STA 1080-1100, 1EA PANEL SUPPORT BRACKET HAS CORROSION. REMOVED CORROSION FROM WING TO BODY FAIRING STR, RH FWD UPPER WING, BTW STA 1080-1100. EVALUATED, TOTAL THICKNESS: 0.080, MATERIAL LOSS:0.003IN (4%), MATESDR IPXA2026041587231Angle · corrodedWING TO BODY FAIRING RH, FWD UPPER WING, BTW STA 900-920, 2EA PANEL SUPPORTS CORRODED. DOT 23-077. INSTALLED 2 NEW BRACKETS I.A.W. B757-200PF SRM 51-40-02. REVIEWEDSDR IPXA2026041367944Holder · crackedACCESS DOOR 435AL, HOLD OPEN ROD HOLDER IS CRACKED. INSTALLED 1EA NEW SPRING CLIP IAW SRM 51-40-02-0G-0.SDR IPXA2026041765252Tee Fitting · corrodedLOWER FUSELAGE THROUGH ACCESS PANEL 198BR STRUCTURE FAIRING SUPPORT BS 1040 RBL 0 TO RBL 65 TIEH CORROSION DOT 07-106. INSTALLED 1 TEE FITTINGIAW SRM 51-40-02.SDR IPXA2026041565071Intercostal · corrodedLOWER FUSELAGE AT STA 1045 RBL 45 INTERCOSTAL WITH CORROSION. INSTALLED NEW PART AT OWER FUSELAGE AT BS 1045 RBL 45 IAW SRM 51-40-02-0G-0.SDR IPXA2026041454777Angle · crackedNR 1 ENG O/B T/R INNER TOP MIDDLE BRACKET NEXT TO HOLD-OPEN ACTUATOR ATTACHMENTS IS CRACKED. INSTALLED NEW BRACKET ON #1 ENG O/B T/R INNER TOP MIDDLE. IAW B757-200PF, SRM 51-40-02.SDR IPXA2026041365276Web · corrodedLOWER FUSELAGE STA 1180 TO 1240 RBL 59 WEB WITH CORROSION DOT 07-107. INSTALLED NEW WEB (1 EA) LOWER FUSELAGE STA 1180 TO 1240 RBL 59 IAW B757-200 SRM 51-20-01. REVIEWED.SDR IPXA2026041365017Floor Support · corrodedBULK CARGO COMP, FLOOR SUPPORT HAS 2EA SHIMS CORRODED, BTW BS 1701-1720, LBL 9.20. REMOVED 2EA NUTPLATES SUPPORT (SHIMS) AND 1EA ANGLE SUPPORT CORRODED IAW SRM 51-40-02-0G-0. INSTALLED NUTPLATE SUPPORT SHIM & 1EA ANGLE SUPPORT AT BULK CARGO COMP, FLOOR SUPPOSDR IPXA2026040965063Intercostal · corrodedTHROUGH ACCESS PANEL 198BR FAIRING STRUCTURE AT STA 1040 TO 1060 RBL 65 WITH CORROSION. REMOVED FAIRING STRUCTURE AT STA 1040 TO 1060 RBL 65 OUT OF LIMITS IAW SRM 53-00-71-1A-1. INSTALLED NEW INTERCOSTAL AT BS 1040 - 1060, RBL 65, IAW SRM 51-40-02.SDR IPXA2026040163446Unknown · odorOILY SMELL START UP AND TAKEOFF REPLACED NR 2 ENG. ACCOMPLISHED HIGH POWER RUNS ON LT AND RT ENGINES WITH ALL BLEED SOURCES ISOLATED AND PACKS SELECTED ON. CONFIRMED ODOR IS COMING FROM R/H ENGINE AT HIGH POWER SETTING WITH L/H BLEED OFF. FOUND WITH LT ENGINSDR IPXA2026041150506Tee Fitting · corrodedCORROSION FOUND AT STA 1180 TO STA 1240 L/H TEE CHORD. WTB SUPPORT AFT FUSELAGE. INSTALLED NEW T-CHORD.IAW B757-200PF, SRM 51-40-02. REVIEWEDSDR IPXA2026033150838Lamp · inoperativeEMERGENCY LIGHT SWITCH KORRY DRAWER ASSEMBLY BROKEN AND LAMPS INOPERATIVE. PERFORMED PERMANENT REPAIR IAW EO-96965-REQ1. OK FOR SERVICE.SDR IPXA2026033140569Ecs · odorSTRONG WET SOCK ODOR EMANATED FROM ECS SYSTEM AT V1 SPEED TAKEOFF. ODOR INCREASED EVEN GREATER AT 10K ACCELERATION. (SEE ATTACHMENT FOR THE REST OF THE WRITE UP) ACCOMPLISHED FIM 21-00-00/301. INSPECTED APU, LEFT AND RIGHT PACK BLEED DUCTS FOR POSSIBLE OIL CONSDR IPXA2026033040569Ecs · odorSTRONG, ALMOST OVERWHELMING WET SOCK ODOR EMANATED FROM ECS SYSTEM AT V1 SPEED TAKEOFF. ODOR INCREASED AT 10K ACCELERATION.
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