Boeing 757-24APF

Service difficulty reports · 16,054

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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.

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. REVIEWEDNov 11, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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. REVIEWEDNov 11, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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.- VNov 11, 2023 · N456UP · Boeing 75724APF · Fuselage Main, StructureSDR 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.Nov 11, 2023 · N459UP · Boeing 75724APF · Aerodynamic FairingsSDR 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 APPRNov 11, 2023 · N459UP · Boeing 75724APF · Aerodynamic FairingsSDR 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.Nov 11, 2023 · N459UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR 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.Nov 10, 2023 · N459UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR 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.Nov 10, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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: MS20Nov 10, 2023 · N456UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2023112919701Tee Angle · corroded*** SUPPLEMENTAL SDR *** FAULT: WTB STRUCTURE - T-CHORD STA 1037.67 IS CORRODED BETWEEN LBL 20 TO LBL 65 REVIEWEDNov 9, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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. REVIEWEDNov 9, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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. REVIEWEDNov 9, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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.- REVIEWEDNov 9, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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. REVIEWEDNov 9, 2023 · N456UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR 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. REVIEWEDNov 9, 2023 · N405UP · Boeing 75724APF · Wing SparSDR 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. REVIEWEDNov 9, 2023 · N405UP · Boeing 75724APF · Wing SparSDR 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.Nov 9, 2023 · N459UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2023111315514Unknown · unknownMAIN CARGO DECK - FLOOR BEAM STA 1057 BL 0 TO RBL 24.75 WITH CORROSION (UNDER FLOOR PANEL 242XGF) .Nov 9, 2023 · N456UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR 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 FINov 9, 2023 · N456UP · Boeing 75724APF · Aerodynamic FairingsSDR 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.Nov 9, 2023 · N456UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR 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.Nov 8, 2023 · N405UP · Boeing 75724APF · DoorsSDR 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 Nov 8, 2023 · N405UP · Boeing 75724APF · Passenger/Crew DoorsSDR 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. REVIEWEDNov 8, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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 51-10-0Nov 8, 2023 · N428UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2023110999411Unknown · unknownCREW ENTRY DOOR LATCHES UPPER AND LOWER 2EA APPEAR TO HAVE GOUGES . OPENNov 8, 2023 · N405UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2023110999488Unknown · unknownFWD EXTERNAL ACCESS DOOR 113 AL ( AREA FWD OF NLG W/W ) BOTH IB AND OB HINGES HAS WEAR BUSHINGS . OPENNov 8, 2023 · N405UP · Boeing 75724APF · Cargo/Baggage DoorsSDR 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.Nov 8, 2023 · N428UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR 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.Nov 8, 2023 · N428UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR 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. REVIEWEDNov 7, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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. REVIEWEDNov 7, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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. REVIEWEDNov 7, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2023112767770Tee Angle · corrodedFAULT: R/H WTB, INTERCOSTAL, FOUND EXFOLIATE CORROSION, BETWEEN STA 1037 TO STA 1060. INSTALLED T-CHORD IAW SRM 51-40-02. REVIEWEDNov 7, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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 COMPLETENov 7, 2023 · N456UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR 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. REVIEWEDNov 7, 2023 · N405UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2023111967834Tee Angle · corrodedR/H WTB, T-CHORD STA 1220, AT RBL 63 FOUND EXFOLIATED CORROSION. INSTALLED T-CHORD IAW SRM 51-40-02-0G. REVIEWEDNov 7, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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.Nov 7, 2023 · N405UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR 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.Nov 7, 2023 · N456UP · Boeing 75724APF · Aerodynamic FairingsSDR 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.Nov 7, 2023 · N456UP · Boeing 75724APF · Aerodynamic FairingsSDR 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.Nov 6, 2023 · N459UP · Boeing 75724APF · Trailing Edge FlapsSDR 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.Nov 6, 2023 · N459UP · Boeing 75724APF · Trailing Edge FlapsSDR 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.Nov 6, 2023 · N459UP · Boeing 75724APF · Trailing Edge FlapsSDR 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.Nov 6, 2023 · N459UP · Boeing 75724APF · Trailing Edge FlapsSDR 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. SRNov 6, 2023 · N456UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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. REVIEWEDNov 6, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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.- REVIEWEDNov 6, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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.- REVIEWEDNov 6, 2023 · N459UP · Boeing 75724APF · Fuselage Structure (General)SDR 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 COMPLETEDNov 6, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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. REVIEWEDNov 6, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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. REVIEWEDNov 6, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR 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 & 1Nov 6, 2023 · N456UP · Boeing 75724APF · Fuselage Main, Structure
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