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 IPXA2023120195921Tee Angle · corroded*SUPPLEMENTAL SDR* FAULT: R/H WTB T-CHORD, RBL 67, FOUND EXFOLIATED CORROSION, BET STA 1037 TO 1060. INSTALLED T- CHORD RBL 67 STA 1037 TO 1060 IAW SRM 51-40-02-OG. REVIEWEDSDR IPXA2023112750267Tee Angle · corrodedFAULT: WTB STRUCTURE - FRAME WTB STRUCTURE STA. 1240 BETWEEN RBL 57 AND RBL 63 IS EXFOLIATED. INSTALLED CHANNEL STA.1240 RBL 63 I.A.W. SRM 51-40-02-0G STEP. 4,7,8 AND SRM 51-70-11-0G-0. REVIEWEDSDR IPXA2023112750323Frame · corrodedFAULT: WTB STRUCTURE - FRAME WTB STRUCTURE BETWEEN STA. 1180 AND 1240. RBL 63 IS EXFOLIATED. INSTALLED WEB STA.1180 TO 1240 RH, 6 EA STIFFENERS BETWEEN STA.1187 TO 1235, ANGLES 1180 RBL 63 AND STA 1200 RBL 63 AND FRAME STA 1220 RBL 63 I.A.W SRM 51-40-02-0G.- VSDR IPXA2023111343755Unknown · unknownR/H WTB, T-CHORD STA 1220, FOUND EXFOLIATED CORROSION. REMOVED T-CHORD STA 1220 IAW SRM 51-40-02-0G. VERIFIED T-CHORD AT STA. 1220 REMOVED.SDR IPXA2023111343694Unknown · unknown*** SDR FILED OPEN *** FAULT: R/H WTB, T-CHORD, RBL 63, FOUND EXFOLIATED CORROSION. REMOVED T-CHORD AT RBL 63.0 BETWEEN FS 1180 TO FS 1240 IAW B757 SRM 51-40-02-0G. REMOVED STRAP FROM T-CHORD AT RBL 63.0 BETWEEN FS 1180 TO FS 1240 IAW B757 SRM 51-40-02-0G APPRSDR IPXA2023111343467Unknown · unknownR/H WTB, T-CHORD, STA 1240, FOUND EXFOLIATED CORROSION, BETWEEN RBL 57.50 T0 RBL 63 PERFORMED CUT OUT AT T-CHORD FROM BL0 TO RBL63 STA 1240 I.A.W SRM 51-70-12-OG AND SRM 51-10-02. VERIFIED T-CHORD AT STA 1240 FROM BL-0 TO RBL-63 HAS BEEN CUT OUT.SDR IPXA2023112740899Skin · corroded*MAJOR REPAIR* FAULT: EVIDENCE OF CORROSION INSIDE #2 PYLON SKIN FWD OF PANEL 443CR. DOT 140-13. ACCOMPLISH EO-88765-REQ1 AND EA 757-5450-27-A3442. SUBTASK UP TO REP REVIEW, JOB COMPLETE, AUDIT COMPLETE. REVIEWED.SDR IPXA2023112533548Tee Angle · corrodedFAULT:LOWER FUSELAGE WEBS BETWEEN BOTH AIR CONDITIONING ACCESS DOOR WITH SURFACE CORROSION.DOT119-065. INSTALLED T-CHORD IN LOWER FUSELAGE BTWN BOTH AIR CONDITIONING IAW SRM 51-40-02-0G.- JOB COMPLETED.SDR IPXA2023112637854Fairing · corrodedFAULT-FUS BELLY FAIRING AFT W/W CUTOUT SUPPORT FITTING WITH CORROSION SEVERAL PLACES. INSTALLED T-CHORD AT LBL 5750 BETWEEN STA 1180 TO 1240 IAW SRM 51-40-02-0G. WORK VERIFIED, NUTPLATES INSTALLED NUTPLATES P/N; BACN11P3A5C, BATCH #0004204060. RIVETS P/N: MS20SDR IPXA2023112919701Tee Angle · corroded*** SUPPLEMENTAL SDR *** FAULT: WTB STRUCTURE - T-CHORD STA 1037.67 IS CORRODED BETWEEN LBL 20 TO LBL 65 REVIEWEDSDR IPXA2023112915514Floor Support · corroded*** SUPPLEMENTAL SDR *** FAULT: MAIN CARGO DECK - FLOOR BEAM STA 1057 BL 0 TO RBL 24.75 WITH CORROSION (UNDER FLOOR PANEL 242XGF) . DOT 07608-026 INSTALLED SUPPORT BEAM IAW SRM 51-40-02-0G. REVIEWEDSDR IPXA2023120119733Tee Angle · corrodedWTB STRUCTURE - T-CHORD STA 1060 IS CORRODED BETWEEN LBL 50 TO LBL 65. INSTALLED NEW T-CHORD STA 1060 IAW SRM 51-40-02, STEP 4. REVIEWEDSDR IPXA2023112718179Tee Angle · corrodedFAULT:WING TO BODY LH STRUCTURE HAS CORROSION AT T CHORD STA 1.040.DOT119-060. INSTALLED NEW T-CHORD IN WING TO BODY LH STRUCTURE STA.1040 IAW SRM 51-40-02-0G.- REVIEWEDSDR IPXA2023112819755Tee Angle · corrodedFAULT: WTB STRUCTURE - T-CHORD STA 1060 IS CORRODED BETWEEN LBL 20 TO LBL 30. INSTALLED T-CHORD SECTION I.A.W. B757-200 S.R.M. 51-40-02-OG. REVIEWEDSDR IPXA2023112621920Spar · corrodedFAULT-RIGHT WING UPPER EXTEIOR SURFACE STA 150 TO STA 204 SHOWS SPOTS WITH CORROSION. NO DOT. INSTALLED PANEL 196AR IAW SRM 51-40-02. REVIEWEDSDR IPXA2023112621836Spar · corrodedFAULT-LEFT WING UPPER EXTEIOR SURFACE STA 150 TO STA 204 SHOWS SPOTS WITH CORROSION. DOT 68-01. INSTALLED PANEL 195AL PER SRM 51-40-02. REVIEWEDSDR IPXA2023112316833Web · corrodedFAULT:WING TO BODY FAIRING STA 1.200 WEB RH HAS CORROSION.DOT119-048. INSTALLED NEW WEB AT STA 1200 RH WTB IAW SRM 51-40-02-0G. REVIEWED.SDR IPXA2023111315514Unknown · unknownMAIN CARGO DECK - FLOOR BEAM STA 1057 BL 0 TO RBL 24.75 WITH CORROSION (UNDER FLOOR PANEL 242XGF) .SDR IPXA2023111319733Unknown · unknown*** SDR FILED OPEN *** FAULT: WTB STRUCTURE - T-CHORD STA 1060 IS CORRODED BETWEEN LBL 50 TO LBL 65 EVALUATED T-CHORD AT STA 1060 BETWEEN LBL 50 TO LBL 65, EXFOLIATED CORROSION NOTED, AFTER FUTHER INVESTIGATION FOUND TO BE OUT LIMITS I.A.W SRM 53-00-71-1A-1 FISDR IPXA2023111319701Unknown · unknownWTB STRUCTURE - T-CHORD STA 1037.67 IS CORRODED BETWEEN LBL 20 TO LBL 65 REF. STEP 3 , WORK VERIFIED. REMOVED T-CHORD STA 1037.67 BETWEEN LBL 20 TO LBL 65 INSPECTED.SDR IPXA2023113099488Access Door · unknownFWD EXTERNAL ACCESS DOOR 113 AL ( AREA FWD OF NLG W/W ) BOTH IB AND OB HINGES HAS WEAR BUSHINGS . 89-096. UPON FURTHER INVESTIGATION DOOR HINGES FOUND TO BE IN SERVICEABLE CONDITION I.A.W AMM 52-48-01-404-005.SDR IPXA2023113099411Door Latch · gougedCREW ENTRY DOOR LATCHES UPPER AND LOWER 2EA APPEAR TO HAVE GOUGES . 89-095. BLENDED OUT GOUGES ON UPPER AND LOWER LATCHES OF CREW ENTRY DOOR. PER STEP 1 OF SREO-14721-REQ001. PERFORMED SURFACE HFEC INSP. AT CREW ENTRY DOOR LATCHES UPPER AND LOWER IAW NTM PART SDR IPXA2023112989044Tee Angle · corrodedFAULT: L/H WTB T-CHORD AT STA. 1200 HAS EXFOLIATING CORROSION. INSTALLED NEW T-CHORD AT FS 1200 LH IAW B757 SRM 51-40-02-0G. REVIEWEDSDR IPXA2023112189904Skin · damagedFUSELAGE SKIN HAS A BURN HOLE AT B STA 462 APPROX 2" ABOVE S-8R MEASURING 0.011" DEEP AND 0.060" IN DIAMETER. UPON FURTHER INSPECTION FOUND DAMAGE TO WITHIN LIMITS FOR ALLOWABLE DAMAGE IAW SRM 53-30-01. BLENDED OUT DAMAGE AND REFINISHED SURFACE IAW SRM 51-10-0SDR IPXA2023110999411Unknown · unknownCREW ENTRY DOOR LATCHES UPPER AND LOWER 2EA APPEAR TO HAVE GOUGES . OPENSDR IPXA2023110999488Unknown · unknownFWD EXTERNAL ACCESS DOOR 113 AL ( AREA FWD OF NLG W/W ) BOTH IB AND OB HINGES HAS WEAR BUSHINGS . OPENSDR IPXA2023110889941Unknown · unknownFUSELAGE SKIN HAS A BURN HOLE AT B STA 488 APPROX 4" ABOVE S-14R MEASURING 0.047" DEEP AND 0.084" IN DIAMETER.SDR IPXA2023110889904Unknown · unknown*SDR FILED OPEN* FUSELAGE SKIN HAS A BURN HOLE AT B STA 462 APPROX 2" ABOVE S-14R MEASURING 0.011" DEEP AND 0.060" IN DIAMETER.SDR IPXA2023112984644Angle · corroded*** SUPPLEMENTAL SDR *** FAULT RT WING TO BODY AREA ABOVE RAT DOOR INTERIOR AREA SHOWS EVIDENCE OF CORROSION DOT 47-09 INSTALLED T-CHORD I.A.W SRM 51-40-02-0G INSTALLED HINGE ASSY (4EA) AND GAUSSET ASSY 5(EA) I.A.W SRM 51-40-02-0G. REVIEWEDSDR IPXA2023112984377Angle · corroded*** SUPPLEMENTAL SDR *** FAULT LEFT WING TO BODY SUPPORT AREA FWD OF W/W SHOWS EVIDENCE OF CORROSION DOT 47-05 INSTALLED T-CHORD STA 1037,67 TO 1060 LH SIDE IAW SRM 51-40-02, STEP 4. REVIEWEDSDR IPXA2023112867666Tee Angle · corrodedFAULT: R/H WTB T-CHORD STA 1037, FOUND EXFOLIATED CORROSION AT NUT PLATE HOLES. INSTALLED T-CHORD AT STA 1037RH WTB IAW SRM 51-40-02-0G. REVIEWEDSDR IPXA2023112767770Tee Angle · corrodedFAULT: R/H WTB, INTERCOSTAL, FOUND EXFOLIATE CORROSION, BETWEEN STA 1037 TO STA 1060. INSTALLED T-CHORD IAW SRM 51-40-02. REVIEWEDSDR IPXA2023112486155Skin · corroded*MAJOR REPAIR* FAULT: #1 ENGINE PYLON I/B AFT. SKIN HAS CORROSION AT INNER SKIN APP. STA 154 . DOT 07308-005 (PLACED AT EXTERNAL SKIN) VERIFIED COMPLIED WITH EO 88741-REQ1 AND EA 757-5450-27-A3437 REV. -. JOB COMPLETESDR IPXA2023112475686Frame · none*MAJOR REPAIR* FAULT : EXISTING FRAME REPAIR FOUND AT AFT CARGO COMPARTMENT STA 1240 R/H. VERIFIED ALL WORK ACCOMPLISHED IAW EO-87166-REQ1 AND VTMAE EA 757-5360-27-A3424 REV. JOB COMPLETE. AUDIT COMPLETE. REVIEWEDSDR IPXA2023111967834Tee Angle · corrodedR/H WTB, T-CHORD STA 1220, AT RBL 63 FOUND EXFOLIATED CORROSION. INSTALLED T-CHORD IAW SRM 51-40-02-0G. REVIEWEDSDR IPXA2023111979160Skin · out of limits*SDR FILED OPEN* FAULT: PUNCTURE BETWEEN STA 1400- 1420. STR 24-25 L/H. GIVEN THE OK TO APPLY TOP COAT. SUPPLEMENTAL INSPECTIONS DEFERRED IAW B757-200PF REV 118.00 SRM CHAPTER 53-00-01-2R-29, TABLE 206, FOR ZONE A.SDR IPXA2023111384377Unknown · unknownLEFT WING TO BODY SUPPORT AREA FWD OF W/W SHOWS EVIDENCE OF CORROSION DOT 47-05 REMOVED T-CHORD FROM STA 1037.67 TO 1060 LH SIDE LBL 67 IAW SRM 51-40-02-0G. VERIFIED T-CHORD AT STA 1037.67 TO 1060 LH SIDE REMOVED.SDR IPXA2023111384644Unknown · unknown*** SDR FILED OPEN *** FAULT RT WING TO BODY AREA ABOVE RAT DOOR INTERIOR AREA SHOWS EVIDENCE OF CORROSION DOT 47-09 REMOVED T-CHORD AT AREA INTERIOR DOOR RAT I.A.W SRM 51-40-02-0G.- VERIFIED REMOVAL OF T-CHORD INTERIOR RAT DOOR AREA.SDR IPXA2025022649962Skin · corrodedWING RH I/B FLAP SURFACE CORROSION AT LOWER SURFACE. DOT119-029 PLEASE REF BARCODE T3F18E0039JV1 FOR CORRECTIVE ACTION AND INSTALLATION OF NEW FLAP.SDR IPXA2025022651282Skin · corrodedWING RH I/B TRAILING EDGE FLAP SURFACE CORROSION AT LOWER SKIN. DOT119-031 INSTALLED RH IB TRAILING EDGE MAIN FLAP PER AMM 27-51-02-424-021. COMPLETED INSTALLATION AS OUTLINED IN AMM 27-51-12.SDR IPXA2023112049962Skin · corroded*SDR FILED OPEN* FAULT:WING RH I/B FLAP SURFACE CORROSION AT LOWER SURFACE. DOT119-029 PARTS ON ORDER IN BARCODE T3F18E0039JV1. 3 MECHANICS REQUIRED FOR 4 SHIFTS ESTIMATED, CRANE REQUIRED, HANGER RECOMMENDED. WORK WITH BARCODE T2F18E0039JV1.SDR IPXA2023112051282Skin · corroded*SDR FILED OPEN* FAULT:WING RH I/B TRAILING EDGE FLAP SURFACE CORROSION AT LOWER SKIN. DOT119-031 PARTS ON ORDER. 3 MECHANICS REQUIRED FOR 4 SHIFTS ESTIMATED, CRANE REQUIRED, HANGER RECOMMENDED. WORK WITH BARCODE T2F18E0039HSE.SDR IPXA2023112956677Tee Angle · corroded*** SUPPLEMENTAL SDR *** FAULT: WTB STRUCTURE - WEB FOR T-CHORD STA 900 HAS CORROSION AT APROX LBL 10 - DOT 07608-002 INSTALLED WEB AT STA 900 I.A.W. SRM 51-40-02-0G. INSTALLED SECTION T-CHORD I.A.W. SRM 51-40-02-0G. INSTALLED INTERCOSTAL AT STA 900 I.A.W. SRSDR IPXA2023112865059Tee Angle · corrodedFAULT: R/H WTB T-CHORD, RBL 57.50, FOUND EXFOLIATED CORROSION, BET STA 1180 TO STA 1240. INSTALLED T-CHORD I.A.W. B757-200 S.R.M. 51-40-02-OG. REVIEWEDSDR IPXA2023112759219Tee Angle · corrodedFAULT: LH AFT WTB STRUCTURE T-CHORD AT STA 1220, UNDER PANEL 195CL HAS CORROSION. INSTALLED NUT PLATE 17 E/A IAW SRM 51-40-02-0G. INSTALLED T-CHORD AT STA 1220 UNDER PANEL 145CL IAW SRM 51-40-02-0G.- REVIEWEDSDR IPXA2023112758827Unknown · corrodedFAULT: WTB STRUCTURE UNDER PANEL 198MR, FROM STA 1180-1240 ON TH RH SIDE HAS SEVERAL AREAS WITH CORROSION. INSTALLED T-CHORD UNDER PANEL 198MRFROM STA.1180 TO 1240 ON THE RH SIDE IAW SRM 51-40-02-0G.- REVIEWEDSDR IPXA2023112265202Tee Angle · corrodedFULT: R/H WTB T-CHORD STA 1240, FOUND EXFOLIATED CORROSION, BET RBL 57.50 TO RBL 63.0 INSTALLED T-CHORD I.A.W. SRM 51-40-02-0G. INSTALLED 4 E/A SPLICES AT R/H WTB T-CHORD STA 1240 I.A.W. SRM 51-40-02-0G. JOB COMPLETEDSDR IPXA2023111958867Tee Angle · corrodedFAULT: RH WTB STRUCTURE UNDER PANEL 198AR, STA 1040-1060 HAS CORROSION. INSTALLED T- CHORD STA. 1040 TO STA.1060 IAW SRM 51-40-02-0G. REVIEWEDSDR IPXA2023111959108Tee Angle · corrodedFAULT: RH WTB STRUCTURE T-CHORD AT STA 1060 HAS CORROSION. INSTALLED T-CHORD I.A.W. B757-200 S.R.M. 51-40-02-OG. REVIEWEDSDR IPXA2023111360602Unknown · unknown*** SDR FILED OPEN *** FAULT: RH RAM AIR INLET STRUCTURE AT APROX STA 880 HAS 2 ANGLES WITH CORROSION. DOT 07608-006 REMOVED RAM AIR INLET ASSY P/N: 149N7160-31 IAW AMM 21-53-01-004-001 AND LIP P/N: 149N7160-24 AND 2 CHANNELS WITH CORROSION P/N: 149N7160-8 & 1
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