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 IPXA2025072588319Paint · damagedINTRECOSTAL AT BS 1090, RBL 50 HAS SURFACE CORROSION ON INNER SURFACES. CLEANED INTRECOSTAL AT BS 1190, NO CORROSION NOTED FOUND TO BE PAINT DAMAGED ONLY IAW B757-200 SOPM 20-30-03 ACETONEQT P/N ACETONEQT BATCH#0004346929 1QT, MAROON HAND PAD. TREATED AND PRIJul 23, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025080560795Skin · corrodedNUMBER 2 PYLON INBD SIDE, FWD INNER SKIN HAS CORROSION AROUND CUTOUT OF PANEL 443GL. INSTALLED PYLON #2 I/B FWD FAIRING IAW B757-200PF SRM 51-40-02-0G-0.Jul 22, 2025 · N469UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2025080265076Tee Angle · corrodedTEE CHORD BS 900 RBL 0 HAVE CORROSION. INSTALLED TEE CHORD AND 8 PLATES, IAW SRM 51-70-12-0G-0, SRM 51-40-02.Jul 22, 2025 · N469UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2025080366377Skin · dentedEXTERNAL FUSELAGE SKIN BETWEEN STA 560 TO 580 AND S-27R TO S-28R HAS A DENT. ACCOMPLISH REPAIR PER EO-94639-REQ1 AND VT-MAE EA 757-5330-27-A4080, REV-.Jul 22, 2025 · N469UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2025080361106Skin · corrodedNR 2 PYLON INBD SIDE, AFT INNER SKIN HAS CORROSION BETWEEN PANELS 443HL AND 443JL AT LOWER AREA. ACCOMPLISH REPAIR PER EO-94655-REQ1 AND VT-MAE EA 757-5450-27-A4075, REV-.Jul 22, 2025 · N469UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2025080706343Support Bracket · corrodedBETWEEN T-CHORD 860 AND LOWER SKIN OF FUSELAGE, LOWER SUPPORT BRACKET HAS CORROSION.REMOVED CORROSION T-CHORD 860 RBL 0 IAW B757-200PF SRM 51-10-02.TREATED AND PRIMED AREA IAW B757-200PF SRM 51-20-01.APPLIED TOP COAT AT AREA IAW B757-200PF AMM 51-21-15-370-801Jul 22, 2025 · N469UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2025080766917Support Angle · corrodedEVIDENCE CORROSION PANEL 192 DR UPPER SUPPORT R/H SIDE. CLEANED AREA AT PANEL 192 DR UPPER SUPPORT R/H SIDE IAW SOPM 20-30-03.TREATED AND PRIMED AREA IAW SRM 51-20-01.APPLIED TOP COAT AT AREA IAW AMM 51-21-15-370-801.Jul 22, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025080234385Strap · corrodedAPU INLET DOOR FWD STRAP AT STA 1787.45 FROM STR 3R TO STR 6R HAS EXFOLIATION. INSTALLED NEW FWD STRAP IAW SRM 51-40-02-0G-0.Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025080534561Skin · corrodedAPU INLET DOOR AFT STRAP AT STA 1826 FROM STR 3R TO STR 6R HAS EXFOLIATION CORROSION. ACCOMPLISH REPAIR PER EO-94632-REQ1 AND VT-MAE EA 757-5380-27-A4072, REV-,Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2025080234761Angle · corrodedAPU INLET DOOR UPPER ANGLE FROM STA 1787.45 TO STA 1826 AT STR 3R HAS CORROSION. INSTALLED NEW UPPER ANGLE IAW B757-200PF SRM 51-40-02-0G-0.Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025080234656Angle · corrodedAPU INLET DOOR LOWER ANGLE FROM STA 1787.45 TO STA 1826 AT STR 6R HAS EXFOLIATION CORROSION. INSTALLED 1EA LOWER ANGLE IAW B757-200PF SRM 51-40-02-0G-0.Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025080337337Tee Angle · corrodedEVIDENCE OF CORROSION ON T-CHORD UPPER R/H SECTION STA 1200. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.063''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:2.5, W:1.4, DEPTH: 0.018'', REMAINING MAT.: 0.045'', %DAMAGE:28.6%. REMOVED UPPER RJul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025080700384Stiffener · corrodedEVIDENCE OF CORROSION ON CHANNEL UPPER L/H STA 1120. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.050''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:2.1, W:1.2, DEPTH: 0.007'', REMAINING MAT.: 0.043'', %DAMAGE:14%. REMOVED STIFFENER STA 1220Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025080237575Tee Angle · corrodedEVIDENCE OF CORROSION ON T-CHORD NEAR TO RAM AIR R/H STA 1220 RBL50. .REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.071''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:2.2, W:1.1, DEPTH: 0.020'', REMAINING MAT.: 0.051'', %DAMAGE:28.1%. LOCATEDJul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025080737989Tee Angle · corrodedEVIDENCE OF CORROSION ON T-CHORD L/H STA 1180 TO 1240 LBL50.DOT 5846-12. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.080''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:1.9, W:1.4, DEPTH: 0.006'', REMAINING MAT.: 0.074'', %DAMAGE:7.5%. TREATJul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025080738248Tee Angle · corrodedEVIDENCE OF CORROSION ON T-CHORD NEAR TO RAM AIR LT STA 1220 LBL50. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.071''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:2.1, W:1.4, DEPTH: 0.031'', REMAINING MAT.: 0.040'' PERCENT, DAMAGE:43.7 PERCEJul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025080239097Support Angle · corrodedAPU INLET DOOR UPPER CORNER ANGLE AT STA 1787.45 S3R HAS CORROSION. REMOVED UPPER CORNER ANGLE WITH CORROSION IAW B757-200 SRM 51-40-02-0G.REMOVED AND REPLACED ONE S3R CORNER SUPPORT ANGLE (P/N: 148N3141-6) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SRJul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025080239271Angle · corrodedAPU INLET DOOR LOWER CORNER ANGLE AT BS 1787.45 STR 6R HAS CORROSION.REMOVED LOWER CORNER ANGLE WITH CORROSION IAW B757-200 SRM 51-40-02-0G.REMOVED AND REPLACED 1 EACH S-6R CORNER SUPPORT ANGLE (P/N: 148N3141-5) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PJul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025081314120Cam · damagedCREW DOOR LOWER LATCH CAM HAS A GOUGE ON OUTER SIDE. ACCOMPLISHED JOB IN SREO-14721-REQ001 ((APPX A) CREW ENTRY DOOR UPPER AND LOWER LATCH CAMS REWORK INSTRUCTIONS (SREO))Jul 19, 2025 · N469UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2025081112145Skin · dentedL/H LWR FUSELAGE SKIN PROTRUDING AT STA 1400. INSTALLED -1 DOUBLER REPAIR AND -2 REPLACEMENT SPLICE STRAP SEGMENT AT STA 1400 BTW S-27L AND 28L IAW EA 757-5360-01-B0545 REV. P2 PAR.D STEP 18. ACCOMPLISH REPAIR PER EO-94648-REQ1 AND VT-SAA EA 757-5360-01-B054Jul 19, 2025 · N433UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2025072313969Stringer · dentedMAJOR REPAIR, STRINGER 25L DENTED AT STA 1340. DISPLACED FRAME AT STATION 1340, STRINGER 25L FOR FOM. EO-94445-REQ1Jul 19, 2025 · N425UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR IPXA202507214120Cam · gougedCREW DOOR LOWER LATACH CAM HAS A GOUGE ON OUTER SIDE.Jul 19, 2025 · N469UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2025072113981Cam · gougedCREW DOOR UPPER LATACH CAM HAS A GOUGE ON OUTER SIDE. ACCOMPLISHMENT OF SREO-14721-REQ001.Jul 19, 2025 · N469UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2025071881182Sign · inoperativeEMERGENCY EXIT SIGN HAS 7 EACH LIGHTS INOP. ++REPLACED 7 EACH BULBS IN EMERGENCY EXIT SIGN IAW AMM 33-51-01 OPS CHECK GOODJul 17, 2025 · N422UP · Boeing 75724APF · Emergency LightingSDR IPXA2025071398635Heat Exchanger · inoperativeDURING CLIMB LEFT ENG OIL TEMP IN AMBER BAND. QRH PROCEDURE WITH THROTTLE ALMOST IDLE LOWERED TEMP TO NORMAL RANGE. COMPLETED K ALERT ON BAR CODE T3F18E0071FDT. PERFORMED HIGH POWER ENG RUN RFEF 757 M/M 71-00-00- 501. LEFT ENG OIL TEMP CHKED WITHIN LIMITS.Jul 12, 2025 · N434UP · Boeing 75724APF · Turbine Engine Oil SystemSDR IPXA2025072576091Strap · corrodedMAJOR REPAIR, CORROSION FOUND ON STRAP AT AUXILARY POWER UNIT AIR INLET DOOR SURROUND STRUCTURE STA Y=1825 AND BETWEEN S-3R AND S-6R INSTALLED REPAIR PARTS, STRAP (1), STRAP (2), STRAP (7), FILLER (3) AND FILLER (4) AT AUXILARY POWER UNIT AIR INLET DOOR SURRJul 11, 2025 · N471UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025071670051Unknown · noiseLOUD NOISE SHORTLY AFTER LIFT OFF STARTED AT A LOW FREQUENCY THEN SLOWLY INCREASED IN PITCH, SOUNDED LIKE AN ENGINE SLOWLY REVING TO REDLINE. NOISE ENDED AT 5000€™. SUSPECT CREW ENTRY DOOR SEAL PRESSURIZED AIRCRAFT PER MM 21-30-00, NO LEAKS OR KOOKY NOISES NJul 11, 2025 · N434UP · Boeing 75724APF · Fuselage Structure (General)SDR IPXA2025071170051Unknown · noiseLOUD NOISE SHORTLY AFTER LIFT OFF STARTED AT A LOW FREQUENCY THEN SLOWLY INCREASED IN PITCH, SOUNDED LIKE AN ENGINE SLOWLY REVING TO REDLINE. NOISE ENDED @ 5000€™. SUSPECT CREW ENTRY DOOR SEAL PRESSURIZED AIRCRAFT PER MM 21-30-00, NO LEAKS OR KOOKY NOISES NOJul 11, 2025 · N434UP · Boeing 75724APF · Standard Practices/StructuresSDR IPXA2025073057913Plate · corrodedAGING FINDING - LEFT ELEVATOR TIP STATIC WIC CONDUCTIVE PLATE HAS EVIDENCE OF CORROSION. AA026 INSTALLED SERVICEABLE L/H ELEVATOR IN REF TO B757 AMM 27-31-01-424-028Jul 10, 2025 · N449UP · Boeing 75724APF · Elevator StructureSDR IPXA2025072257913Static Wick · corrodedLEFT ELEVATOR TIP STATIC WIC CONDUCTIVE PLATE HAS EVIDENCE OF CORROSION. AA026 INSP VERIFIED STEP 14 ADJUSTMENT OF THE ELEVATOR POSITION INDICATING SYSTEM IN REF B757 AMM 27-38-00-825-009. ADJUSTMENT GOOD. PERFORMED ELEVATOR POSITION INDICATING SYSTEM OPERATIOJul 10, 2025 · N449UP · Boeing 75724APF · Pitot/Static SystemSDR IPXA2025072442329Strap · corrodedMAJOR REPAIR, CORROSION ON APU INLET FWD NUT PLATE STRAP INSTALLED STRAP P/N: 148N3138-20, BTCH NO. 0004410942 AT APU INLET DOOR SURROUNDING STRUCTURE IAW B757-200PF SRM 51-40-02-0G-0.Jul 9, 2025 · N471UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA2025071845628Angle · corrodedAGING FINDING - MAIN DECK FLOOR STRUCTURE LOCATED APPROX STA 1715 RBL 12" AS SEEN FROM THE AFT PIT AFT ELEC BAY IS CORRODED AND EXFOLIATED. AA025 AUDIT C/W. VERIFIED REMOVE AND REPLACE SUPPORT ANGLE REF P/N: 146N5240-21 PER BOEING DWG 146N5240 IAW 757-200PF SRJul 9, 2025 · N449UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025071820838Angle · corrodedAFTER REMOVING THE APU DOOR SURROUND FOUND THE ANGLE HAS SURFACE CORROSION. INSTALLED ANGLE IAW SRM 51-40-02.Jul 8, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025071821035Angle · corrodedAFTER REMOVING THE APU DOOR SHROUD FOUND THE ANGLE HAS SURFACE CORROSION. INSTALLED ANGLE IAW SRM 51-40-02.Jul 8, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025071819525Bracket · corrodedAFTER REMOVAL OF THE APU DOOR SHROUD FOUND THE 148N3141-6 BRACKET HAS SURFACE CORROSION. INSTALLED ANGLE 148N3141-6 IAW SRM 51-40-02.Jul 8, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025071820911Angle · corrodedAFTER REMOVING APU DOOR SHROUD FOUND THE 148N3152-2 ANGLE HAS SURFACE CORROSION INSTALLED ANGLE 148N3152-2 IAW SRM 51-40-02.Jul 8, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025071919982Floorbeam · corrodedMAJOR REPAIR, CORROSION ON FLOORBEAM IN MAIN CABIN AT APPROX FS 1200 LBL3 TO LBL 18. ACCOMPLISHED REPAIR PER EO-94406-REQ1 AND VT-SAA EA 757-5300-01-B0535, REV. I/R.Jul 8, 2025 · N449UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2025071891774Channel · crackedFOUND ROD STRUCTURE CHANNEL (313N3022-102) HAS A .60 LONG CRACK ON PANEL 445BL RUNNING FROM EDGE OF FASTENER HOLE TO EDGE OF PART. INSTALLED 1 EA CHANNEL IAW B757-200-SRM-51-40-02.Jul 6, 2025 · N407UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2025080177856Tee Angle · corroded*** SUPPLEMENTAL SDR *** FAULT- Z100- STR: RH WTB T-CHORD BETWEEN STA 1037 - STA 1060 RBL 65 HAS EXFOLIATION ON UPPER SURFACE. INSTALLED T-CHORD P/N UP-149N7553-28, BETWEEN STA 1037 - STA 1060 RBL 65IAW B757-200PF, SRM 51-40-02Jul 5, 2025 · N407UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2025071179209Stringer · corrodedMAJOR REPAIR, LOWER AFT FUSELAGE, BS 1460 HAS EXFOLIATION CORROSION BETWEEN SKIN INNER AREA AND STRINGERS 29 AND 30. INSTALLED STRINGER 23 CLIPS. INSTALLED 2 SUPPORT CHANNELS. INSTALLED 8 FLOOR SUPPORT BRACKETS. INSTALLED 6 STRINGER SPLICES. INSTALLED ONE ANTJul 5, 2025 · N407UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR IPXA2025072377856Tee Angle · corrodedSTRINGER RT WTB TEE-CHORD BETWEEN BS 1037 - 1060, RBL 65, HAS EXFOLIATION ON UPPER SURFACE.Jul 5, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025070677817Intercostal · corrodedRIGHT PACK EXHAUST INTERCOSTAL FRAME SUPPORT AT FWD AREA HAS CORROSION INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02. VERIFIED INSTALLATION OF RT PACK EXHAUST INTERCOSTAL FRAME FWD SUPPORT.Jul 5, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025070677685Tee Angle · corrodedLOWER FUSELAGE INTERCOSTAL T-CHORD BETWEEN STA 1037-STA 1060 RBL 7 HAS CORROSION. INSTALLED T-CHORD P/N: UP-144N8180-48, STA 1037-STA 1060 RBL 7 IAW B757-200PF, SRM 51-40-02Jul 5, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025070677526Tee Angle · corrodedWTB T-CHORD BETWEEN STA 1037 - STA 1060 LBL 65 HAS EXFOLIATION ON UPPER SURFACE. INSTALLED NEW WTB T-CHORD BETWEEN STA 1037 - STA 1060 LBL 65 IAW B757-200PF, SRM 51-40-02.Jul 5, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025070770161Panel · crackedNUMBER 6 SLAT O/B END LWR LEADING EDGE LWR SURFACE CLOSING PLIE HAS A CRACK AS MARKED. INSTALLED CLOSING PLIE IAW SRM 51-40-02.Jul 4, 2025 · N407UP · Boeing 75724APF · Leading Edge DevicesSDR IPXA2025071169520Floor Panel · corrodedFWD CARGO COMPT FLOOR PANEL 121DF HAS SURFACE CORROSION. INSTALLATION OF ROLLER TRAY, PN- 81658-1. INSTALLED FWD CARGO PIT MBA SYSTEM IAW 757-200 SRM 51-40-02-0G-0 AND AMM 25-57-01-404-003-001.Jul 4, 2025 · N407UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025080155352Intercostal · corrodedFS 1037 - FS 1060 LBL 37 THE PAX EXHAUST INTERCOSTAL 149N7559-1 HAS EXFOLIATION ON UPPER FWD SURFACE INSTALLED PAX EXHAUST INTERCOSTAL OF FS 1037-1060 LBL 37 IAW SRM 51-40-02.Jul 3, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025071644664Strap · corrodedAPU INLET FWD STRAP HAS CORROSION UNDERNEATH. INSTALLED NEW STRAP IAW SRM 51-40-02Jul 3, 2025 · N407UP · Boeing 75724APF · APU Core EngineSDR IPXA2025070751400Strip · corrodedMETAL STRIP AT BS 1180, BL 5.5 IS CORRODED. INSTALLED METAL TRIP IAW B757-200 SRM 51-40-02 USING SAME HARDWARE.Jul 3, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025072355352Intercostal · corrodedFS 1037 - FS 1060 LBL 37 THE PAX EXHAUST INTERCOSTAL 149N7559-1 HAS EXFOLIATION ON UPPER FWD SURFACEJul 3, 2025 · N407UP · Boeing 75724APF · Fuselage Miscellaneous Structure
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