# Service difficulty reports: N157UP

A list on [N157UP](https://openairdocs.org/aircraft/N157UP.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 194 reports

- [SDR IPXA2026081505605](https://openairdocs.org/sdr/IPXA2026081505605.md): Fairing · cracked · Aug 15, 2026 · N157UP · Airbus A300F4622R · Nacelle/Pylon Structure
  > UPON 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.
- [SDR IPXA2026051102957](https://openairdocs.org/sdr/IPXA2026051102957.md): Bulb · burned out · May 9, 2026 · N157UP · Airbus A300F4622R · Passenger Compartment Lighting
  > LAV AUXILIARY LIGHT INOP. RELAMPED LAV AUXILIARY LIGHT REF AMM 33-51-00, OPS CHECK GOOD.
- [SDR IPXA2026012195967](https://openairdocs.org/sdr/IPXA2026012195967.md): Fuel Sys · malfunctioned · Jan 21, 2026 · N157UP · Airbus A300F4622R · Aircraft Fuel Distribution System
  > DURING 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 28-21-09-1
- [SDR IPXA2025091075594](https://openairdocs.org/sdr/IPXA2025091075594.md): Floor Panel · damaged · Sep 8, 2025 · N157UP · Airbus A300F4622R · Fuselage Floor Panel
  > FAULT: 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 53-15-31/401
- [SDR IPXA2025091863260](https://openairdocs.org/sdr/IPXA2025091863260.md): Wedge · damaged · Sep 1, 2025 · N157UP · Airbus A300F4622R · Leading Edge Devices
  > NR 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-S
- [SDR IPXA2025091662656](https://openairdocs.org/sdr/IPXA2025091662656.md): Frame · cracked · Sep 1, 2025 · N157UP · Airbus A300F4622R · Nacelle/Pylon, Plate/Skin
  > NR 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 51-40-21
- [SDR IPXA2025091662750](https://openairdocs.org/sdr/IPXA2025091662750.md): Frame · cracked · Sep 1, 2025 · N157UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > NR 1 ENGINE PPANEL 475AL I/B SIDE #7 STRINGER FROM FRONT CRACKED DT 1/042 INSTALLED FRAME #7 AT 475AL USING FASTNERS IAW SRM-51-40-21
- [SDR IPXA2025091662589](https://openairdocs.org/sdr/IPXA2025091662589.md): Frame · cracked · Sep 1, 2025 · N157UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > NR 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-51-40-21
- [SDR IPXA2025091526093](https://openairdocs.org/sdr/IPXA2025091526093.md): Shear Tie · cracked · Sep 1, 2025 · N157UP · Airbus A300F4622R · Fuselage Internal Mounting Structure
  > FRAME 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 COMPLETE
- [SDR IPXA2025090962357](https://openairdocs.org/sdr/IPXA2025090962357.md): Profile · cracked · Sep 1, 2025 · N157UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.INST
- [SDR IPXA2025090962412](https://openairdocs.org/sdr/IPXA2025090962412.md): Profile · cracked · Sep 1, 2025 · N157UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.INSTALLE
- [SDR IPXA2025091629288](https://openairdocs.org/sdr/IPXA2025091629288.md): Skin · gouged · Aug 29, 2025 · N157UP · Airbus A300F4622R · Leading Edge Devices
  > MAJOR 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. -.
- [SDR IPXA2025091104660](https://openairdocs.org/sdr/IPXA2025091104660.md): Rib · cracked · Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT 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. -.
- [SDR IPXA2025091104681](https://openairdocs.org/sdr/IPXA2025091104681.md): Rib · cracked · Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT 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. -.
- [SDR IPXA2025091104842](https://openairdocs.org/sdr/IPXA2025091104842.md): Rib · cracked · Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT 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. -.
- [SDR IPXA2025091104710](https://openairdocs.org/sdr/IPXA2025091104710.md): Rib · cracked · Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT 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. -.
- [SDR IPXA2025091104697](https://openairdocs.org/sdr/IPXA2025091104697.md): Rib · cracked · Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT 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. -.
- [SDR IPXA2025091104847](https://openairdocs.org/sdr/IPXA2025091104847.md): Rib · cracked · Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT 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. -.
- [SDR IPXA2025091104635](https://openairdocs.org/sdr/IPXA2025091104635.md): Rib · cracked · Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT 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. -.
- [SDR IPXA2025091104804](https://openairdocs.org/sdr/IPXA2025091104804.md): Rib · cracked · Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT 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. -.
- [SDR IPXA2025091104437](https://openairdocs.org/sdr/IPXA2025091104437.md): Skin · cracked · Aug 28, 2025 · N157UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT 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. -.
- [SDR IPXA06201](https://openairdocs.org/sdr/IPXA06201.md): Lock · broken · Feb 28, 2025 · N157UP · Airbus A300F4622R · Passenger/Crew Doors
  > LOCKING 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.
- [SDR IPXA2025022531068](https://openairdocs.org/sdr/IPXA2025022531068.md): Handle · loose · Feb 25, 2025 · N157UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW 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.
- [SDR IPXA2025013190824](https://openairdocs.org/sdr/IPXA2025013190824.md): Lamp · inoperative · Jan 30, 2025 · N157UP · Airbus A300F4622R · Flight Compartment Lighting
  > FLIGHT CREW STOWAGE AREA/LOCKER LIGHT INOP RE-LAMPED STOWAGE AREA LT - OPS CHECK GOOD IAW MM 33-27-00
- [SDR IPXA2025011476968](https://openairdocs.org/sdr/IPXA2025011476968.md): Seal · damaged · Jan 14, 2025 · N157UP · Airbus A300F4622R · Leading Edge Devices
  > SLAT 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 TRACK
- [SDR IPXA2024121620871](https://openairdocs.org/sdr/IPXA2024121620871.md): Door · no discrepancy · Dec 15, 2024 · N157UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW 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.
- [SDR IPXA2024092003708](https://openairdocs.org/sdr/IPXA2024092003708.md): Warning Light · malfunctioned · Sep 19, 2024 · N157UP · Airbus A300F4622R · Escape Slide
  > EMERGENCY 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.
- [SDR IPXA2023110263106](https://openairdocs.org/sdr/IPXA2023110263106.md): Unknown · unknown · Nov 1, 2023 · N157UP · Airbus A300F4622R · Emergency Lighting
  > LIGHT 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 33-21-01-3-0-2
- [SDR IPXA2023110163106](https://openairdocs.org/sdr/IPXA2023110163106.md): Unknown · unknown · Nov 1, 2023 · N157UP · Airbus A300F4622R · Emergency Lighting
  > *** SDR FILED OPEN *** LIGHT OUT IN SUPERNUMERARY COAT CLOSET. DEFERRED COAT CLOSET LIGHT PER MEL 33-21-01-3-0-2. INSTALLED PLACARD.
- [SDR IPXA2023091194135](https://openairdocs.org/sdr/IPXA2023091194135.md): Power Supply · failed · Sep 10, 2023 · N157UP · Airbus A300F4622R · Emergency Lighting
  > INSPECTION 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.
- [SDR IPXA2023071693667](https://openairdocs.org/sdr/IPXA2023071693667.md): Flap System · faulted · Jul 16, 2023 · N157UP · Airbus A300F4622R · Flight Control System
  > INSPECTION 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 NORMA
- [SDR IPXA2023061293423](https://openairdocs.org/sdr/IPXA2023061293423.md): Reservoir · inoperative · Jun 2, 2023 · N157UP · Airbus A300F4622R · Hydraulic System, Main
  > INSPECTION 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 R
- [SDR IPXA2023040392546](https://openairdocs.org/sdr/IPXA2023040392546.md): Flap · chafed · Apr 3, 2023 · N157UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION 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 269862
- [SDR IPXA2023040392564](https://openairdocs.org/sdr/IPXA2023040392564.md): Unknown · unknown · Apr 2, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:CK1C*MAJOR REPAIR* FRAME 12 LAVATORY VENTURI EXTERNAL DOUBLER INSTALLATION FOR RCD PURPOSES ONLYCOMPLIED WITH UPS EO A300-5330-72601-B AND RCD 269970
- [SDR IPXA2023033092446](https://openairdocs.org/sdr/IPXA2023033092446.md): Floor Panel · damaged · Mar 29, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:CK1CPANEL 242CF IS DAMAGEDFABBED PANEL 242CF FROM 5024N400001SS-G, BATCH# 3855547 PER SREO A300-5320-40552
- [SDR IPXA2023033092420](https://openairdocs.org/sdr/IPXA2023033092420.md): Adapter · broken · Mar 29, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION 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.
- [SDR IPXA2023033092419](https://openairdocs.org/sdr/IPXA2023033092419.md): Adapter · broken · Mar 29, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION 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.
- [SDR IPXA2023033092439](https://openairdocs.org/sdr/IPXA2023033092439.md): Floor Panel · damaged · Mar 29, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:CK1CPANEL 242BJ IS CRACKEDFABBED 242BJ FROM 5024N400001SS-G, BATCH# 3855547 PER SREO A300-5320-40552
- [SDR IPXA2023032892371](https://openairdocs.org/sdr/IPXA2023032892371.md): Pylon · cracked · Mar 28, 2023 · N157UP · Airbus A300F4622R · Nacelle/Pylon Structure
  > INSPECTION TYPE:CK1C#1 PYLON RIB FWD OF PRE-COOLER CRACKED, (RIB 3)REMOVED AND INSTALLED RIB ARCH IAW SRM 51-40-21.
- [SDR IPXA2023032892358](https://openairdocs.org/sdr/IPXA2023032892358.md): Bracket · broken · Mar 28, 2023 · N157UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:CK1CR/H WING CENTER FLAP O/B EDGE HAS BROKEN BRACKET.REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.
- [SDR IPXA2023032892357](https://openairdocs.org/sdr/IPXA2023032892357.md): Stiffener · cracked · Mar 28, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:CK1CAFT PIT FWD BULKHEAD STIFFENER P/N A5341076521700 IS CRACKED.REMOVED AND REPLACED STIFFENER IAW SRM 51-40-21.
- [SDR IPXA2023032992416](https://openairdocs.org/sdr/IPXA2023032992416.md): Adapter · broken · Mar 25, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:CK1CCLS ADAPTER BROKEN AT FRAME 32-Y2200 P/N B5377413620490.REMOVED AND REPLACED CLS ADAPTER AT FR32-Y2200 IAW SRM 51-40-21.
- [SDR IPXA2023032992414](https://openairdocs.org/sdr/IPXA2023032992414.md): Adapter · broken · Mar 25, 2023 · N157UP · Airbus A300F4622R · Standard Practices/Structures
  > INSPECTION TYPE:CK1CCLS ADAPTER AT FRAME 33-Y2200 P/N B53774136204 IS BROKENREMOVED AND REPLACED, CLS ADAPTER AT FR33-Y2200 IAW SRM 51-40-21.
- [SDR IPXA2023032492225](https://openairdocs.org/sdr/IPXA2023032492225.md): Stiffener · cracked · Mar 24, 2023 · N157UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:1CAFT PIT FWD BULKHEAD STIFFNER IS CRACKEDREMOVED AND REPLACED IAW SRM 51-40-21
- [SDR IPXA2023040692672](https://openairdocs.org/sdr/IPXA2023040692672.md): Universal Joint · cracked · Mar 17, 2023 · N157UP · Airbus A300F4622R · Trailing Edge Flap Control System
  > INSPECTION 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 RCD
- [SDR IPXA2023040392542](https://openairdocs.org/sdr/IPXA2023040392542.md): Doubler · damaged · Mar 14, 2023 · N157UP · Airbus A300F4622R · Rudder Control System
  > INSPECTION TYPE:SEGRUDDER R/H SIDE UPPER T/E HAS LIGHTENING STRIKEFABRICATED DOUBLER IAW SRM-44-11
- [SDR IPXA2023040692663](https://openairdocs.org/sdr/IPXA2023040692663.md): Floor Panel · damaged · Mar 8, 2023 · N157UP · Airbus A300F4622R · Standard Practices/Structures
  > INSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 132FE DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E
- [SDR IPXA2023040692657](https://openairdocs.org/sdr/IPXA2023040692657.md): Floor Panel · damaged · Mar 8, 2023 · N157UP · Airbus A300F4622R · Standard Practices/Structures
  > INSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 132SG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E
- [SDR IPXA2023040692656](https://openairdocs.org/sdr/IPXA2023040692656.md): Floor Panel · damaged · Mar 8, 2023 · N157UP · Airbus A300F4622R · Standard Practices/Structures
  > INSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 131FE DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E
- [SDR IPXA2023040692655](https://openairdocs.org/sdr/IPXA2023040692655.md): Floor Panel · damaged · Mar 8, 2023 · N157UP · Airbus A300F4622R · Standard Practices/Structures
  > INSPECTION TYPE:CK1C*MAJOR REPAIR* PANEL 131SG DAMAGEDFABRICATED NEW PANEL PER SREO A300-5320-16407 REV. E.

Next page: https://openairdocs.org/aircraft/N157UP/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N157UP/reports

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