Boeing 757-24APF

Service difficulty reports · 16,054

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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"

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SDR IPXA2025022192637Filler · corrodedNR 1 PYLON HAS SURFACE CORROSION AROUND FASTENER HOLES FOR PANEL 433CL. DOT 142-22.REMOVED CRACKED AND CORRODED STRAP (OUT OF LIMITS WITH EXFOLIATED CORROSION VISIBLE IAW SRM 51-10-08) IAW B757-200-51-40-02-OG.Feb 5, 2025 · N439UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2025021994372Frame · dentedDENT FOUND AT AFT CARGO COMPARTMENT FRAME STA 1540 R/H BETWEEN STR 22 AND STR 23.SURFACE HFEC PERFORMED ON CUT OUT ON AFT CARGO FRAME STA 1540 RH BETWEEN STR22-23. NO DEFECTS FOUND IAW NTM 51-00-19.Feb 5, 2025 · N439UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025021195005Skin · corroded#2 ENGINE OUTBD PYLON INNER SKIN AFT OF THE MID SPAR FITTING HAS CORROSION. DOT 8-002. RESTORED SURFACE PROTECTION IN #2 ENG, OUTBD PYLON INNER SKIN IAW SRM 51-20-01 P/N ALODINE1132 BTCH 0004336881 PRIME P/N 02-013-8 BTCH 4263196.Feb 5, 2025 · N439UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2025021194979Skin · corrodedNR 2 ENGINE OUTBD PYLON INNER SKIN FWD OF VENT PANEL OPENING HAS SURFACE CORROSION AND PROTECTIVE COATING DETERIOATED. DOT 8-001. RESTORED SURFACE PROTECTION IN #2 ENG, OUTBD PYLON INNER SKIN IAW SRM 51-20-01 P/N ALODINE1132 BTCH 0004336881 PRIME P/N 02-013-8Feb 5, 2025 · N439UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2025021192630Skin · corrodedPYLON #1 INNER SURFACE, JUST FWD OF 433CL HAS AREA OF CORROSION. DOT IS ON OUTSIDE OF PYLON. DOT 142-15.SURFACE HFEC PERFORMED ON BLENDED AREA OF #1 PYLON INNER SURFACE JUST FWD OF 433CL PANEL. NO DEFECTS FOUND IAW NTM 51-00-19.Feb 5, 2025 · N439UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2025020576230Flap System · faulted*EMERGENCY DECLARED* TE DISAGREE ICAS MSG PERFORMED FIM TASK 27-51 FAULT TREE 808. NO FAULTS ON FSEU 1, 2 , & 3. OPERATED FLAPS AND SLATS SYS MULITPLE TIMES. COULD NOT DUPLICATE FAULT. NO HISTORY NOTED. OPS CK GOOD.Feb 5, 2025 · N461UP · Boeing 75724APF · Trailing Edge Flap Control SystemSDR IPXA2025020870377Angle · corrodedAPU INLET DOOR STRUCTURE LOWER ANGLE PN: 148N3152-1 CORRODED.REMOVED AND REPLACED 1 EACH S-6R SUPPORT ANGLE (P/N: 148N3152-1) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SRM CHAPTER 51 REQUIREMENTS.Feb 4, 2025 · N439UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA2025022643278Door · damaged**SUPPLEMENTAL SDR**FAULT: ZONE 800, STR, RH FUSELAGE, AFT CARGO DOOR CUTOUT, INNER/LOWER SIDE, HAS SEAL RETAINER DAMAGED. DOT 103-20.INSPECTED AND VERIFIED REMOVAL OF LOWER DOOR SILL AND DISPLACEMENT OF LOWER SEAL ON AFT CARGO DOOR.CLEANED AREA PER SOPM 20-30Feb 3, 2025 · N439UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA2025022150787Plate · damagedNR 2 ENG, INB T/R INSIDE AREA HAS PLATE DAMAGED (ASSY LJ76605-0-01). DOT 34-007.REMOVED PLATE DAMAGE ON ENG# 2, INB T/R INSIDE AREA IAW SRM 51-40-02.INSTALLED NEW PLATE IN #2 ENG, T/R I/B, IAW SRM 51-40-02-0G-0 CHERRY MAX P/N CR3523-4-02 BTCH 0004348973 RTV106Feb 3, 2025 · N439UP · Boeing 75724APF · Engine Thrust ReverserSDR IPXA2025022443278Retainer · damagedRH FUSELAGE, AFT CARGO DOOR CUTOUT, INNER/LOWER SIDE, HAS SEAL RETAINER DAMAGED.Feb 3, 2025 · N439UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025022042790Fitting · gougedLH FUSELAGE, CREW DOOR FWD EDGE, LOWER AND UPPER ROD BEARING FITTINGS HAVE GOUGES. DOT 103-05. BLENDED OUT GAUGES AT LOWER AND UPPER LH CREW DOOR LATCH CAM IAW STEP 1 SREO-14721-REQ001. ACOMPLISHED WORK PER SREO-14721-REQ001.Feb 3, 2025 · N439UP · Boeing 75724APF · Fuselage, Door HingeSDR IPXA2025021543109Plate · crackedRH FUSELAGE, FWD CARGO DOOR CUTOUT, LOWER SIDE, SILL PLATE HAS DENT WITH CRACK. DOT 103-10. INSTALLED SCUFF PLATE IAW AMM 53-13-02-4 PER SREO-36318-REQOO4 REV1.Feb 3, 2025 · N439UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA2025020342790Fitting · gougedLH FUSELAGE, CREW DOOR FWD EDGE, LOWER AND UPPER ROD BEARING FITTINGS HAVE GOUGES.Feb 3, 2025 · N439UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2025020635608Pseu · faultedAIR TURN BACK* FAULT- BTW ON 2-2-25 @ 1430Z, BACK TO PNS BROUGHT A/C OUT OF MTC FOR GEAR CHANGE. ON CLIMBOUT WITH GEAR HANDLE IN OFF POSITION, HAD HALF OF LEFT GEAR LIGHT ILLUMINATED, LE. INSTALLED ROBED PSEU OPS CHECK GOOD IAW AMM 32-09-04-404-009. INSTALLED Feb 2, 2025 · N420UP · Boeing 75724APF · Landing Gear Position and WarningSDR IPXA2025020774817Compressor · stalledON CLIMB OUT AFTER V NAV SELECTED R ENGINE COMPRESSOR STALLED AND MAX EGT WAS 892. RAN CHECKLIST AND RETURNED TO SJO PERFORMED ENGINE HOROSCOPE PER AMM 72-00-00/101, FOUND DAMAGE TO THE COMPRESSOR PATH LINER OUT OF LIMITS PER TASK 72-00-726-202-R04. ENGINE INSJan 30, 2025 · N455UP · Boeing 75724APF · Turbine Engine Compressor SectionSDR IPXA2025013074817Compressor · stalled**EMERGENCY DECLARED. ATB, ON CLIMB OUT AFTER V NAV SELECTED R ENGINE COMPRESSOR STALLED AND MAX EGT WAS 892. RAN CHECKLIST AND RETURNED TO SJO OVERTEMPERATURE IS ZONE A PER FIM TASK 71-05 FAULT TREE 824, PERFORM FIM TASK 71-06 FAULT TREE 812 AND REPORT RESULJan 30, 2025 · N455UP · Boeing 75724APF · Turbine Engine Compressor SectionSDR IPXA2025013162143Warning Message · false activationL FWD ENT DOOR EICAS WITH DOOR CLOSED. REVERSED DMP. TROUBLESHOT IAW 757 FIM 52-71 FAULT TREE 802. ADJUSTED THE SENSOR FOR THE CREW ENTRY DOOR. CREW ENTRY DOOR EICAS INDICATION AND ANNUNCIATOR LIGHT OPERATE CORRECTLY WITH DOOR IN THE OPEN AND CLOSED POSITIONJan 29, 2025 · N440UP · Boeing 75724APF · Door Warning SystemSDR IPXA2025012962143Warning Message · false indicationL FWD ENT DOOR EICAS WITH DOOR CLOSED DEFERRED CREW ENTRY DOOR IND SYS IAW MEL 52-71-1. DMP CW. PLACARD INSTALLED. OPENJan 29, 2025 · N440UP · Boeing 75724APF · Door Warning SystemSDR IPXA2025020571335Angle · corrodedAPU DOOR SURROUND BETWEEN FS 1790 - FS 1810 STR 6R ANGLE HAS SURFACE CORROSION ALL NUTPLATES ARE CORRODED WITH SCREW SHANKS STILL INSIDE. INSTALLED ANGLE LOWER DOOR STR 6 RH PER B757 SRM 51-40-02. REVIEWED.Jan 24, 2025 · N401UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA2025020471181Angle · corrodedAPU DOOR SURROUND PN 148N3152-2 BETWEEN FS 1790 - 1810 STR 3R ANGLE HAS INTERGRANULAR CORROSION. INSTALLED ANGLE UPPER STR 3 RH SIDE PER B757 SRM 51-40-02. AUDIT COMPLETE.Jan 24, 2025 · N401UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA2025012108882Hinge Fitting · wornAPU SHUTDOWN IN FLIGHT, DOWN TO SINGLE GEN DUE TO MEL. ATB PER QRH AND FLIGHT CONTROL. REMOVED AND REPLACED APU INLET DOOR INBOARD HINGE BEARING ASSY AND BOTH DOOR HINGE BOLTS. REF AMM 49-15-05. REVERSED DPM AND OPERATED APU PER AMM 49-11-00 WITH NO FAULTS. Jan 21, 2025 · N470UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA2025020495767Strap · corrodedCLEAN CORROSION OFF OF STRAP AT FS 1825 S3R - S6R. ACCOMPLISH REPAIR PER 757-200PF SRM REV 122 CHAPTER 53-80-15-2R-1, DETAIL I ON FIGURE 202 (SHEET 2).Jan 20, 2025 · N401UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025012994882Door Frame · corrodedSEVERE CORROSION FOUND ON APU AIR INLET DOOR FRAME. INSTALLED NEW STRAP IAW B757-200, SRM 51-40-02. REVIEWEDJan 20, 2025 · N401UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2025012426474Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QEH, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5360-01-B0334 IR. OSD: 1/24/2025Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025012326458Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QE4, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5360-01-B0331 IR.Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025012426435Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QE6, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5360-01-B0330 IR. OSD: 1/24/2025Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025012326400Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QC2, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0328 IR. OSD: 1/24/2025Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025012326442Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QCU, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0337 IR. OSD: 1/24/2025Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025012326367Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QBG, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0326 IR. OSD: 1/24/2025Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025012326402Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QCB, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0329 IR. OSD: 1/24/2025Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025012326492Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QFY, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5360-01-B0335 IR. OSD: 1/24/2025Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2025011826131None · noneREF HEAVY CHECK REPAIR T3F18E0056FMQ, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. VERIFIED ACCOMPLISHMENT OF REPAIR PER EA 757-5360-27-A3769, REV- COMPLETED.COMPLIED WITH EO-92552. REVIEWED.Jan 16, 2025 · N419UP · Boeing 75724APF · Standard Practices/StructuresSDR IPXA2025011826183None · noneREF HEAVY CHECK REPAIR T3F18E0056FHS, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. VERIFIED ACCOMPLISHMENT OF REPAIR PER EA 757-5360-27-A3770, REV- COMPLETED.COMPLIED WITH EO-92553. REVIEWED.Jan 16, 2025 · N419UP · Boeing 75724APF · Standard Practices/StructuresSDR IPXA2025012126292None · noneREF HEAVY CHECK REPAIR T3F18E004J5QK, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. VERIFIED ACCOMPLISHMENT OF REPAIR PER EA 757-5360-27-A3771, REV- COMPLETED.COMPLIED WITH EO-92554. REVIEWED.Jan 16, 2025 · N422UP · Boeing 75724APF · Standard Practices/StructuresSDR IPXA2025011826274Frame · no discrepancyREF HEAVY CHECK REPAIR T3F18E004SYHW, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. COMPLIED WITH EO-92551. REVIEWED.Jan 16, 2025 · N418UP · Boeing 75724APF · Standard Practices/StructuresSDR IPXA2025011724182Slat System · warning message**EMERGENCY DECLARED**ON DOWNWIND MOVED FLAP LEVER TO POSITION 1 AND RECEIVED LE FLAP DISAGREE MSG AND LIGHT. PERFORMED QRH PROCEDURE AND LOWERED FLAPS WITH ALTERNATE METHOD LANDED FLAPS 20 NON-NORMAL LEFT FLAPS DOWN RAISED FLAPS W/ALT METHOD. PLACED FLAPS TO Jan 16, 2025 · N415UP · Boeing 75724APF · Trailing Edge Flap Control SystemSDR IPXA2025012222873Window · scratched**SUPPLEMENTAL SDR**FIRST OFFICERS #2 WINDOW SCRATCHED TO THE POINT THAT VISIBILITY IS COMPROMISED OUT THAT WINDOW. VERIFIED PROPER INSTALLATION AND TORQUE OF ELECTRICAL CONNECTIONS AS REQUIRED. <BR>INSPECTION PERFORMED BY RII CERTIFIED TECHNICIAN IAW GMM 04-0Jan 15, 2025 · N422UP · Boeing 75724APF · Flight Compartment WindowsSDR IPXA2025011622873Window · scratchedFIRST OFFICERS #2 WINDOW SCRATCHED TO THE POINT THAT VISIBILITY IS COMPROMISED OUT THAT WINDOW. VERIFIED PROPER INSTALLATION AND TORQUE OF ELECTRICAL CONNECTIONS AS REQUIRED. INSPECTION PERFORMED BY RII CERTIFIED TECHNICIAN IAW GMM 04-02.Jan 15, 2025 · N422UP · Boeing 75724APF · Flight Compartment WindowsSDR IPXA2025011604140Warning Message · false activationAIR TURNBACK, APU FAULT CLIMBING THROUGH 15,000€™. DID NOT RESTART PER QRH PROCEDURE. ACCOMPLISHED APU BITE REF 757 FIM 49-11-875. NO FAULTS FOUND ON ECU. INSPECTED APU REF FOUND NO DEFECTS. OPERATED APU REF 757 M/M CHAP 49- 11-00- 802-00. APU STARTED ANJan 15, 2025 · N470UP · Boeing 75724APF · Airborne Auxiliary Power Unit (APU) SystemSDR IPXA202501154140Apu · faulted**ATB** **SDR FILED OPEN** APU FAULT CLIMBING THROUGH 15,000€™. DID NOT RESTART PER QRH PROCEDURE.Jan 15, 2025 · N470UP · Boeing 75724APF · APU Core EngineSDR IPXA2025013172057Transition Panel · corrodedAFT CARGO TRANSITION PANEL (CURRENTLY ON PANEL RACK) HAS CORROSION ON LOWER SURFACE AROUND 24 EA. NUTPLATES. (AREAS CIRCLED IN RED) DOT 142-366. CORROSION WAS REMOVED BY HAND IN 13 AREAS OF THE NUT PLATE.CHECK THE BOUNDARIES IN THE AFFECTED AREAS.DEEPEST THICKJan 13, 2025 · N420UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025013155554Bracket · crackedNR 1 ENG PYLON NAC STA.149.5 FRAME I/B HAS ELONGATED HOLES AND 0,5 CRACK. EA-62. INSTALLED NEW FRAME ANGLE ON #1 PYLON. IAW SRM 51-40-02-0G. INSTALLED NEW BRACKET ON FRAME ANGLE OF PYLON #1. IAW SRM 51-40-02-0G.Jan 12, 2025 · N401UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2025013142659Skin · crackedRH WING, FIXED L/E UPPER SKIN, UNDER SLAT #7 O/B, HAS 2,5 IN CRACK AFT PREVIOUS . EA-62. VERIFIED FINAL EA # 757-5741-27-A3772 REV WAS RECEIVED ACCOMPLISHED WITHOUT DEVIATIONS AND EO-92568-REQ1 WAS ACCOMPLISHED WITHOUT DEVIATIONS. OSD: 2/4/2025Jan 11, 2025 · N401UP · Boeing 75724APF · Wing, Plate/SkinSDR IPXA2025020543514Tee Angle · corrodedFAULT-STR-ZONE 100. LH MID WING TO BODY STRUCTURE, T-CHORD AT STA 1080-1200, LBL 60 HAS CORROSION. DOT 28-01. INSTALLED NEW T-CHORD AT STA 1080-1200, LBL 60 IAW B757-200 SRM 51-40-02. REVIEWED.Jan 11, 2025 · N401UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2025020543758Tee Angle · corrodedRH WING TO BODY STRUCTURE, T-CHORD AT STA 1260, RBL 10 HAS LIGHT CORROSION. DOT 28-05. NEW T-CHORD IT IS FOUND TO BE INSTALLED IAW B757-200 SRM 51-40-02-0G-0.Jan 11, 2025 · N401UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2025012041574Seat Track · corrodedSEAT TRACK AT STA 520 LBL 24.75 HAS CORROSION. DOT 142-319. CLEANED AREA IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS OF SEAT TRACK CROWN IS, 0.130". A MATERIAL LOSS OF 0.006" WAS NOTED USING ULTRA SONIC, T93968. MAX LOSS ALLOWED IS 0.020". REMAINING THICKNESJan 11, 2025 · N420UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025012041608Floor Panel · corrodedMAIN CABIN FLOOR DECKING UNDER FLOOR PANEL 231XJF STA 560 TO 620 BTWN LBL 64 AND 45.50 HAS AREAS OF CORROSION. CIRCLED IN RED. DOT 142-320. CLEANED MULTIPLE AREAS IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS FOR ALL AREAS IS 0.100". ALL FOUND TO BE IN LIMITS Jan 11, 2025 · N420UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025012845154Cover Plate · corrodedFLOOR BRACKET BTWN BL-0 AND LBL 8 DENTED AND HAS 8 EA DOME NUTS WITH CORROSION IN AND AROUND HOLES. INSTALLED COVER PLATE IN STA 900 BL, 0 AND 8 E/A DOME NUTS IAW SRM 51-40-02, GOOD ISSUE VOUCHER, DOME NUTS. OSD: 1/29/2025Jan 11, 2025 · N420UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025012042686Seat Track · corrodedCORROSION AROUND 2 EA RIVETS STA 680 LBL 45.5 SEAT TRACK. REMOVED CORROSION IN TWO POINTS AFTER REWORK:P1) ORIGINAL THICKNESS 0.070'' MATERIAL LOSS 0.003'' MATERIAL REMAINING 0.067''.P2) ORIGINAL THICKNESS 0.070'' MATERIAL LOSS 0.002''MATERIAL TEMAINING 0.068'Jan 11, 2025 · N420UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025012844732Seat Track · corrodedMAIN CABIN FLOOR STRUCTURE AT STA 1020 TO STA 1040 RBL 45.5 HAS CORROSION AROUND 5 EA. FASTENER HOLES. DOT 142-328. EVALUATED REWORK FIVE PAINTS IN MAIN CABIN FLOOR STRUCTURE AT STA 1020 TO STA 1040 RBL 45.5. MATERIAL THICKNESS 0.090''AFTER REWORK, P1) MATERIAJan 11, 2025 · N420UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings
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