N157UP

Service difficulty reports · 194

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 = 'N157UP' 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.

SDR IPXA2026081505605Fairing · crackedUPON FURTHER INSPECTION CRACK DEFERRED ON TASK T3F18E0097P77 HAS GROWN TO 5.5€? BEYOND SRM LIMITS ON NR 1 ENGINE LOWER AFT PYLON LOWER SKIN. C/W EO-98354-REQ3.Aug 15, 2026 · N157UP · Airbus A300F4622R · Nacelle/Pylon StructureSDR IPXA2026051102957Bulb · burned outLAV AUXILIARY LIGHT INOP. RELAMPED LAV AUXILIARY LIGHT REF AMM 33-51-00, OPS CHECK GOOD.May 9, 2026 · N157UP · Airbus A300F4622R · Passenger Compartment LightingSDR IPXA2026012195967Fuel Sys · malfunctionedDURING INITIAL CLIMB AN UNENNUNCIATED AUTO FUEL FAULT. FUEL FED FROM OUTER TANKS OUT OF SEQUENCE, PUMP CYCLED OFF THEN ON. AUTO FUEL FEED OPERATION RESTORED. R & R FUEL AMPLIFIER REF AMM 28-46-23 OPS CHECKS GOOD THIS CLEARS MEL 28-21-09-1Jan 21, 2026 · N157UP · Airbus A300F4622R · Aircraft Fuel Distribution SystemSDR IPXA2025091075594Floor Panel · damagedFAULT: APG / Z100 / DURING MAIN WHELL WELL INSPECTION FOR HYDRAULIC SYSTEM LEAK CHECKS A FLOOR PANEL (P/N: A2551027700100) FOUND SOFT AND DELAMINATED INSTALLED MAIN WHELL WELL FLOOR PANEL (P/N: A2551027700100) IAW AMM 53-15-31/401Sep 8, 2025 · N157UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025091863260Wedge · damagedNR 2 SLAT I/B T/E WEDGE LWR SURFACE HAS GOUGE DOT 55-012 REPAIR RH WING #2 SLAT P/N: A57864200173, S/N: FH1636, IAW A300-600F SRM 57-43-11 PARAGRAPH 4.B AND FIGURE 202, APPLICABLE REPAIR PER SRM. REMOVED DAMAGED SKIN AND FABRICATED REPLACEMENT PARTS IAW-A300-SSep 1, 2025 · N157UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2025091662656Frame · crackedNR 2 ENGINE PANEL 485AL O/B SIDE #1 STRINGER CRACKED. INSTALLED PART STRINGER #2 ENGINE PANEL 485AL O/B SIDE #1 IAW A300-600 SRM 51-40-21Sep 1, 2025 · N157UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2025091662750Frame · crackedNR 1 ENGINE PPANEL 475AL I/B SIDE #7 STRINGER FROM FRONT CRACKED DT 1/042 INSTALLED FRAME #7 AT 475AL USING FASTNERS IAW SRM-51-40-21Sep 1, 2025 · N157UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2025091662589Frame · crackedNR 2 ENGINE PANEL 485AL HAS CRACK ON I/B SIDE #7 FRAME FROM FRONT. INSTALLED FRAME #7 AT 485AL USING FASTENERS IAW A300-600-SRM-51-40-21Sep 1, 2025 · N157UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/RibSDR IPXA2025091526093Shear Tie · crackedFRAME BASE FITTING R/H FR45 AREA 1 HAS A CRACK 1.5" LONG.SJ-30 VERIFIED REPAIR PARTS INSTALLED IAW E0-46789-JIC008 REV1(SB A300-57-6177) STEPS 51-68 COMPLETED. JOB COMPLETESep 1, 2025 · N157UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR IPXA2025090962357Profile · crackedMAIN DECK FLOOR STRUCTURE, UNDER PANEL 261PF AT FR 74 AND FR75, LT FLOOR SUPPORT HAVE 2EA CRACKS. DOT 90-095. REMOVED MAIN DECK FLOOR STRUCTURE, UNDER PANEL 261PF AT FR 74 AND FR75 L/H FLOOR SUPPORT IAW SRM 51-40-21.FABRICATED NEW Z-PROFILE, IAW GMM 09-08.INSTSep 1, 2025 · N157UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025090962412Profile · crackedMAIN DECK FLOOR STRUCTURE, UNDER PANEL 262PF AT FR 74 AND FR75, R/H FLOOR SUPPORT HAVE 2EA CRACKS. REMOVED Z-PROFILE AT MAIN DECK FLOOR STRUCTURE, UNDER PANEL 262PF BTW FR 74 AND FR75, IAW A300-600 SRM 51-40-21.FABRICATED NEW Z-PROFILE, IAW GMM 09-08.INSTALLESep 1, 2025 · N157UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025091629288Skin · gougedMAJOR REPAIR. LEFT WING SLAT #1 WITH 2EA GOUGES AND PERFORATED DAMAGE AT LOWER SKIN, O/B SIDE. ACCOMPLISHED PERMANENT REPAIR IR ACCORDANCE WITH EO-95028-REQ1 AND VT-MAE EA 300-5742-27-A4127, REV. -.Aug 29, 2025 · N157UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2025091104660Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 2 AREAS AT RIB12. CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025091104681Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACK NOTED IN 1 AREA AT RIB15.CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025091104842Rib · crackedRIGHT WING,CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 3 AREAS AT RIB26. ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025091104710Rib · crackedRIGHT WING,CENTER FLAP, TOP SKIN RIB FLANGE. CRACK NOTED IN 1 AREA AT RIB16. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025091104697Rib · crackedRIGHT WING,CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 2 AREAS AT RIB19. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025091104847Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 3 AREAS AT RIB27. CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025091104635Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 3 AREAS AT RIB13. CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025091104804Rib · crackedRIGHT WING,CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 2 AREAS AT RIB25. ACCOMPLISHED REPAIR IR ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4127, REV. -.Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025091104437Skin · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 2 AREAS AT RIB11. CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA06201Lock · brokenLOCKING DEVICE BROKEN ON CREW ENTRY DOOR OUTER HANDLE. ORDERED FROM A300 IPC 52-11-11-09B ITEM 630. HARDWARE IN PARTS BAG HANGING FROM HANDLE. REMOVED AND REPLACED EXTERIOR CONTROL HANDLE PER AMM 52-11-21. OPS CHECK GOOD.Feb 28, 2025 · N157UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025022531068Handle · looseCREW ENTRY DOOR EXTERIOR DOOR HANDLE LOSES TENSION AND CANNOT LOWER AND LATCH DOOR. REMOVED AND REPLACED EXTERIOR CONTROL HANDLE PER AMM 52-11-21. OPS CHECK GOOD. STICKER REMOVED. DMP REVERSED.Feb 25, 2025 · N157UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025013190824Lamp · inoperativeFLIGHT CREW STOWAGE AREA/LOCKER LIGHT INOP RE-LAMPED STOWAGE AREA LT - OPS CHECK GOOD IAW MM 33-27-00Jan 30, 2025 · N157UP · Airbus A300F4622R · Flight Compartment LightingSDR IPXA2025011476968Seal · damagedSLAT JACK SEAL RIPPED LT WING RIB 27. LOWERED SLAT AND INSPECTED RIB 27 SLAT SEAL, REPOSITIONED CORNER OF SEAL IAW M/M 27-81-41-0601. RAISED SLATS AND SEAL LOOKS NORMAL IN TRACKJan 14, 2025 · N157UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2024121620871Door · no discrepancyCREW ENTRY DOOR WILL NOT CLOSE FROM THE OUTSIDE. PERFORMED INSPECTION AND CHECK OF CREW ENTRY DOOR IAW AMM 52-00-00/601 3. B. 3. INSPECTION AND CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. DOOR CLOSED SEVERAL TIMES WITH NO ISSUES.Dec 15, 2024 · N157UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2024092003708Warning Light · malfunctionedEMERGENCY EVACUATION SLIDE ASSEMBLY WARNING LIGHT INOPERATIVE-BUZZER OPERATIVE PERFORMED OPS CHECK OF SLIDE TEST SWITCH PER AMM 52-73-14/401. OPS CHECK NORMAL. LIGHT AND HORN FUNCTION NORMAL.Sep 19, 2024 · N157UP · Airbus A300F4622R · Escape SlideSDR IPXA2023110263106Unknown · unknownLIGHT OUT IN SUPERNUMERARY COAT CLOSET. RELAMPED LIGHT AND FOUND THAT DOOR SWITCH WAS OUT OF ADJUSTMENT, ADJUSTED SWITCH OPS CK GOOD , PLACARD REMOVED. THIS CLEARS THE DEFERRAL PER MEL 33-21-01-3-0-2Nov 1, 2023 · N157UP · Airbus A300F4622R · Emergency LightingSDR IPXA2023110163106Unknown · unknown*** SDR FILED OPEN *** LIGHT OUT IN SUPERNUMERARY COAT CLOSET. DEFERRED COAT CLOSET LIGHT PER MEL 33-21-01-3-0-2. INSTALLED PLACARD.Nov 1, 2023 · N157UP · Airbus A300F4622R · Emergency LightingSDR IPXA2023091194135Power Supply · failedINSPECTION TYPE: NA AUTONOMOUS POWER SUPPLY DOES NOT BITE TEST.R&R BOTH EMERGENCY PWR SUPPLY BATTERIES PER AMM 52-73-18 BITE TEST WORKS BUT NO GOOD. FAULTS THE UNIT AND NO OUTPUT SINGAL. R&R APSU PER AMM 52-73-18. BITE TEST GOOD. NO FAULTS NOTED. OK FOR SVC.Sep 10, 2023 · N157UP · Airbus A300F4622R · Emergency LightingSDR IPXA2023071693667Flap System · faultedINSPECTION TYPE:NA*EMERGENCY DECLARED* CONFIGURING FOR LANDING, UPON SELECTION OF FLAP 15Ï¿½. ECAM "FLAPS SYS 2 FAULT" APPEARED. RAN QRH PROCEDURE FOR FLAPS FAULT. PER PROCEDURE FLAPS EXTENDED TO 30/40 FOR APPROACH AND LANDING. FLAPS EXTENDED SLOWER THAN NORMAJul 16, 2023 · N157UP · Airbus A300F4622R · Flight Control SystemSDR IPXA2023061293423Reservoir · inoperativeINSPECTION TYPE:NA*EMERGENCY DECLARED* HYD-GREEN RSVR LOW LEVEL-COMPLIED WITH QRH.RESERVOIR INDICATOR SHOWED COMPLETELY DELETEDFOUND #2 ENGINE PYLON GREEN HYD.PIPELINE WITH PIN HOLE MID SECTION OF PYLON.REMOVED & REPLACED PIPELINE IAW AMM.29-11-69-0401 & IPC RJun 2, 2023 · N157UP · Airbus A300F4622R · Hydraulic System, MainSDR IPXA2023040392546Flap · chafedINSPECTION TYPE:1C*MAJOR REPAIR* L/H WING INNER FLAP P/N A57960000010 S/N FH1297 O/B EDGE HAS A REPAIR DOUBLER WITH 2 EACH CHAFE DAMAGESWORKED PER UPS EO A300-5750-86183-A AND UPS RCD 269862Apr 3, 2023 · N157UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2023040392564Unknown · unknownINSPECTION TYPE:CK1C*MAJOR REPAIR* FRAME 12 LAVATORY VENTURI EXTERNAL DOUBLER INSTALLATION FOR RCD PURPOSES ONLYCOMPLIED WITH UPS EO A300-5330-72601-B AND RCD 269970Apr 2, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2023033092446Floor Panel · damagedINSPECTION TYPE:CK1CPANEL 242CF IS DAMAGEDFABBED PANEL 242CF FROM 5024N400001SS-G, BATCH# 3855547 PER SREO A300-5320-40552Mar 29, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2023033092420Adapter · brokenINSPECTION TYPE:1CR/H MAIN CARGO COMP-Y1959 FRAME19 FLOOR TIEDOWN (CLS ADAPTER) IS BROKEN P/N B5377413820200.REMOVED AND REPLACED CLS ADAPTER IAW-SRM 51-40-21.Mar 29, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2023033092419Adapter · brokenINSPECTION TYPE:1CR/H MAIN CARGO COMP - Y1959 FRAME 20 FLOOR TIEDOWN (CLS ADAPTER) IS BROKEN, P/NB53774133820200.REMOVED AND REPLACED CLS ADAPTER IAW-SRM 51-40-21.Mar 29, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2023033092439Floor Panel · damagedINSPECTION TYPE:CK1CPANEL 242BJ IS CRACKEDFABBED 242BJ FROM 5024N400001SS-G, BATCH# 3855547 PER SREO A300-5320-40552Mar 29, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2023032892371Pylon · crackedINSPECTION TYPE:CK1C#1 PYLON RIB FWD OF PRE-COOLER CRACKED, (RIB 3)REMOVED AND INSTALLED RIB ARCH IAW SRM 51-40-21.Mar 28, 2023 · N157UP · Airbus A300F4622R · Nacelle/Pylon StructureSDR IPXA2023032892358Bracket · brokenINSPECTION TYPE:CK1CR/H WING CENTER FLAP O/B EDGE HAS BROKEN BRACKET.REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.Mar 28, 2023 · N157UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2023032892357Stiffener · crackedINSPECTION TYPE:CK1CAFT PIT FWD BULKHEAD STIFFENER P/N A5341076521700 IS CRACKED.REMOVED AND REPLACED STIFFENER IAW SRM 51-40-21.Mar 28, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2023032992416Adapter · brokenINSPECTION TYPE:CK1CCLS ADAPTER BROKEN AT FRAME 32-Y2200 P/N B5377413620490.REMOVED AND REPLACED CLS ADAPTER AT FR32-Y2200 IAW SRM 51-40-21.Mar 25, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2023032992414Adapter · brokenINSPECTION TYPE:CK1CCLS ADAPTER AT FRAME 33-Y2200 P/N B53774136204 IS BROKENREMOVED AND REPLACED, CLS ADAPTER AT FR33-Y2200 IAW SRM 51-40-21.Mar 25, 2023 · N157UP · Airbus A300F4622R · Standard Practices/StructuresSDR IPXA2023032492225Stiffener · crackedINSPECTION TYPE:1CAFT PIT FWD BULKHEAD STIFFNER IS CRACKEDREMOVED AND REPLACED IAW SRM 51-40-21Mar 24, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2023040692672Universal Joint · crackedINSPECTION TYPE:1C*MAJOR REPAIR* RH WING FLAP DRIVE UNIVERSAL JOINT O/B FITTING BRACKET CRACKEDREMOVED, FABRICATED, AND INSTALLED PER UPS EO A300-5750-86448-A AND RCDMar 17, 2023 · N157UP · Airbus A300F4622R · Trailing Edge Flap Control SystemSDR IPXA2023040392542Doubler · damagedINSPECTION TYPE:SEGRUDDER R/H SIDE UPPER T/E HAS LIGHTENING STRIKEFABRICATED DOUBLER IAW SRM-44-11Mar 14, 2023 · N157UP · Airbus A300F4622R · Rudder Control SystemSDR IPXA2023040692663Floor Panel · damagedINSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 132FE DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. EMar 8, 2023 · N157UP · Airbus A300F4622R · Standard Practices/StructuresSDR IPXA2023040692657Floor Panel · damagedINSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 132SG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. EMar 8, 2023 · N157UP · Airbus A300F4622R · Standard Practices/StructuresSDR IPXA2023040692656Floor Panel · damagedINSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 131FE DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. EMar 8, 2023 · N157UP · Airbus A300F4622R · Standard Practices/StructuresSDR IPXA2023040692655Floor Panel · damagedINSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 131SG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E.Mar 8, 2023 · N157UP · Airbus A300F4622R · Standard Practices/Structures
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