N469UP
Service difficulty reports · 207
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N469UP' AND registry_match = 'registration' 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 n_number = 'N469UP' AND registry_match = 'registration' 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 IPXA2026010883023Control Unit · faultedAT CRUISE FLT AT FL380. L SIDE WINDOW HAD STARTED TO DELAMINATE THE HEATING ELEMENT. FOLLOWED QRH CHECKLIST & WINDOW WAS EXTREMELY HOT TO TOUCH AND APPROX 5IN AREA IS AFFECTED. REMOVED AND INSTALLED L2 WINDOW IAW AMM 56-11-02/401 UP TO AND INCLUDING STEP C.8. SDR IPXA2026010783023Window · delaminatedAT CRUISE FLT AT FL380. L SIDE WINDOW HAD STARTED TO DELAMINATE THE HEATING ELEMENT. FOLLOWED QRH CHECKLIST & WINDOW WAS EXTREMELY HOT TO TOUCH AND APPROX 5IN AREA IS AFFECTED. UPON INSPECTION OF L2 WINDOW, REF AMM 56-11-00-206-068, FOUND BROWN COLORING, GROUPSDR IPXA2025122247034Engine · vibrationDIVERSION, NR 2 ENG HIGH N1 VIBRATION ON CLIMB AT 36,000. KEPT OUT OF YELLOW BAND BELOW 67% N1 POWER SETTING. POWERPLANT ENGINEERING REVIEWED ECM/OCM DATA. CLE LINE MAINTENANCE REPORTED THAT ICE WAS FOUND ON THE SPINNER AND FAN BLADES. POWERPLANT ENGINEERING SDR IPXA2025111093190Elec Connector · damagedAIR TURN BACK DUE TO RIGHT ENG TAI INOP LIGHT & EICAS MSG. ENG. A/I CHECKLIST WAS RUN W/NO RELIEF. ICING CONDITIONS AT DESTINATION THIS OCCURRED ON CLIMB-OUT. REPLACED CONNECTOR D1318 FOR ENG ANTI-ICE VALVE IRW B757 SWPM 20-60-03. REVERSED DMP 30-21-1-1. PERFSDR IPXA2025081246933Latch · inoperativeCREW ENTRY DOOR UPPER LATCH IS OUT OF LIMITS. INSTALLED CREW ENTRY DOOR UPR LATCH, IAW CMM 52-11-08 AND AMM 20-11-00-912-001.SDR IPXA202508046933Latch · out of limitsCREW ENTRY DOOR UPPER LATCH IS OUT OF LIMITS VERIFIED STEP 6. INSTALLATION OF CREW ENTRY DOOR UPPER LATCH.REMOVED CREW ENTRY DOOR UPPER LATCH, IAW B757-200 AMM 20-11-00-912-001.INSTALLED CREW ENTRY DOOR UPR LATCH, IAW B757-200 CMM 52-11-08 AND AMM 20-11-00-912SDR IPXA2025080310676Frame · crackedDURING OK TO INSTALL, FOUND AT STA 1200, BTW RBL 5 TO RBL 24, INTERCOSTAL DELAMINATED AND WITH CRACK. INSTALLED 1 EA INTERCOSTAL IAW SRM 51-40-02-0G.SDR IPXA2025080308094Floorbeam · corrodedMAIN DECK FLOORBEAM BELOW FLOOR PANEL 242XGF AT BS 1100 RBL 24.75, HAS EXFOLIATED CORROSION, DOT 78-20, FABRICATED 01 EA REPAIR UPPER CHORD SECTION PER E.A.# 757-5340-27-A4084 STEP 8, LETTER A AND B. ACCOMPLISH CATEGORY B REPAIR IN ACCORDANCE WITH EO-94658-REQSDR IPXA2025080303268Tee Angle · corrodedAT STA 1040 TO 1060 LEFT, UNDER THE RAM AIR DOOR ACTUATOR, T-CHORD HAS EXFOLITATION CORROSION ON UPPER FLANGE, DOT 8-018.RECEIVED NEW INTERCOSTAL FROM TRAVELER # T25/1825274, BATCH #0004248846. RESTORED SURFACE IN NEW INTERCOSTAL IAW AMM 51-21-15 ALODINE PAISDR IPXA2025080383490Skin · corrodedCORROSION FOUND AT SKIN AREA STA 1885.20 S-17L JUST ABOVE APU LEFT DOOR. PERFORMED EO-94659-REQ1 AND VT-MAE EA 757-5380-27-A4073, REV -.SDR IPXA2025080708252Tee Angle · corrodedAT STA 1200 LOWER T-CHORD SUUPORT CLIP HAS CORROSION ON INNER FLANGE. DOT 8-015.CLEANED INTRECOSTAL AT STA 1200 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 P/N 02-00SDR 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 PRISDR 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.SDR 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.SDR 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-.SDR 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-.SDR 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 51-21-15-370-801SDR 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.SDR 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.SDR 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-,SDR 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.SDR 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.SDR 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 RSDR 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 1220SDR 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%. LOCATEDSDR 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%. TREATSDR 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 PERCESDR 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 SRSDR 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 757-200PSDR 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))SDR IPXA202507214120Cam · gougedCREW DOOR LOWER LATACH CAM HAS A GOUGE ON OUTER SIDE.SDR IPXA2025072113981Cam · gougedCREW DOOR UPPER LATACH CAM HAS A GOUGE ON OUTER SIDE. ACCOMPLISHMENT OF SREO-14721-REQ001.SDR IPXA2025071153206Indicator · inoperativeAIR TURN BACK DUE TO RIGHT SIDE FUEL QTY INDICATION INOP REMOVED AND REPLACED ON R/H WING TANK: FUEL PROBES: #1, #2, #3, #4, #5, #7, #8, #9, #10, #11 AND 12, AND PERFORMED LEAK CHECK ON THOSE FUEL ACCESS PANEL, WHERE FUEL PROBES INSTALLED BY A UPS VENDOR. ACCOSDR IPXA2025070753206Indicator · inoperativeAIR TURN BACK DUE TO RIGHT SIDE FUEL QTY INDICATION INOP ACCOMPLISHED DRY CAPACITANCE TEST PER AMM 28-41-00-735-080-002.<BR>RM TU 10 AND 11 CAPACITANCES WITHIN LIMITS.SDR IPXA2025040792925Indicator · inoperative**SUPPLEMENTAL SDR** DURING CLIMBOUT LEFT MAIN FUEL QTY AND TOTAL FUEL QTY BLANKED OUT. DEFUELED LH MAIN TANK AND PERFORMED FQIS DRY CAPACITANCE TEST PER FIM 28-41 AND FOUND VALUES WITHIN LIMITS. PERFORMED FQIS BITE TEST PER FIM 28-41 AND FOUND NO FAULTS AT THSDR IPXA2025040792867Indicator · inoperative**SUPPLEMENTAL SDR** DURING CLIMBOUT RT MAIN FUEL QTY GAUGE BLANKED OUT TECH SUSPECTED POSSIBLE RH MAIN TANK HARNESS, REFERENCE BARCODE T3F18E006DBEX FOR RH MAIN TANK HARNESS REPLACEMENT. AFTER REPLACEMENT PERFORMED FQIS DRY CAPACITANCE TEST PER FIM 28-41SDR IPXA2025040292925Indicator · inoperative**SDR FILED OPEN** **DIVERSION** DURING CLIMBOUT LEFT MAIN FUEL QTY AND TOTAL FUEL QTY BLANKED OUT.SDR IPXA2025040292867Indicator · failed**SDR FILED OPEN** **DIVERSION** DURING CLIMBOUT RT MAIN FUEL QTY GAUGE BLANKED OUTSDR IPXA2025030526691Light · inoperative*SUPPLEMENTAL SDR* INTERIOR EMERGENCY LIGHT INOP ACCOMPLISHED OPS CK OF INTERIOR EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CK GOOD. THIS CLEARS ITEM. PLACARD REMOVEDSDR IPXA2025022426691Light · inoperative**SDR FILED OPEN**INTERIOR EMERGENCY LIGHT INOP DEFERRED PER MEL 33-51-1-1. NO DMP, PLACARED INSTALLED.SDR IPXA2024052305539Processor · failed*** ATB *** ON CLIMB OUT LEFT MAIN TANK FUEL BLANK, INDICATION CAME BACK 90 MINUTES INTO FLIGHT R/R FQIS PROCESSOR IAW AMM 28-41-08 . OPS CHECK GOOD.SDR IPXA2024032045317Engine · slowLEFT ENGINE SLOW TO SPOOL WHEN POWER PUSHED UP ON TAKEOFF AND IN THE AIR. SLOW ENOUGH TO YAW AIRCRAFT IN THE AIR. ONCE CAUGHT UP ALL PARAMETERS APPEAR NORMAL + MATCH RIGHT ENGINE. REMOVED AND REPLACED LH ENG FUEL FLOW GOVERNOR REF B757 AMM 73-21-01. PERFORMED SDR IPXA2024031545317Governor · slowLEFT ENGINE SLOW TO SPOOL WHEN POWER PUSHED UP ON TAKEOFF AND IN THE AIR. SLOW ENOUGH TO YAW AIRCRAFT IN THE AIR. ONCE CAUGHT UP ALL PARAMETERS APPEAR NORMAL + MATCH RIGHT ENGINE. REMOVED AND REPLACED LH ENG FUEL FLOW GOVERNOR REF B757 AMM 73-21-01. PERFORMED SDR IPXA2024040259120Panel · damagedDAMAGE RUDDER HINGE PANEL VERY MOST TOP PANEL DEFERED PER EO-89694 CORRECTIVE ACTION. SPEED TAPE APPLIED TO THE AREA. ITEM CLOSED AND FAULT TRANSFERRED TO BARCODE T3F18E0047VUR FOR REPAIR AND DEADLINE EXTENSION.SDR IPXA2024030459120Hinge · damaged*SDR FILED OPEN* DAMAGE RUDDER HINGE PANEL VERY MOST TOP PANEL DAMAGED BONDED PANEL REMOVED. WAITING ON NEW PANELSDR IPXA2023120557614Door Sill · damaged*** SUPPLEMENTAL SDR *** AFT LOWER CARGO COMP. HAS DAMAGE TO INNER SILL PROTECTOR AND UNDERLYING FITTINGS. INSTALLLED AFT LWR SILL PLATE AS REQUIRED REF AMM 20-00-00SDR IPXA2023112057614Unknown · unknown*SDR FILED OPEN* *MAJOR REPAIR* AFT LOWER CARGO COMP. HAS DAMAGE TO INNER SILL PROTECTOR AND UNDERLYING FITTINGS. REMOVED CLOSEOUT ZEE ANGLE FROM STA 1380 TO STA 1440 TO GAIN ACCESS TO THE TEE CHORD SPLICE REPAIR. REF SRM 51-40-02SDR IPXA61502Unknown · unknown*SDR FILED OPEN* GEAR DISAGREE EICAS WITH NO RIGHT MAIN GEAR DOWNSDR IPXA2023090693849Skin · crackedLEFT WING FIXED LEADING EDGE HAS CRACK BEHIND SLAT#4 OUTBOARD END REPAIR ACCOMPLISHED ON FAULT: T3F18E002792J. INSTALLED REPAIR PARTS I.A.W. B757-200 S.R.M. 51-40-02-OG REVIEWED T3F18E002792J.SDR IPXA202308230001Unknown · unknown*** SDR FILED OPEN *** FAULT: LEFT WING FIXED LEADING EDGE HAS CRACK BEHIND SLAT#4 OUTBOARD END
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