# Service difficulty reports: N122UP A list on [N122UP](https://openairdocs.org/aircraft/N122UP.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 6 · 274 reports - [SDR IPXA2026062992527](https://openairdocs.org/sdr/IPXA2026062992527.md): Lamp · inoperative · Jun 27, 2026 · N122UP · Airbus A300F4622R · Emergency Lighting > SMALL EMERGENCY EXIT LIGHT IN LAV INOP IN THE ALWAYS ON LOW POSITION. SMALL RECTANGLE LIGHT. RELAMPED LAV AUX/MIRROR LIGHT PER 33-51-21. OPS CHECK GOOD - [SDR IPXA2026051480941](https://openairdocs.org/sdr/IPXA2026051480941.md): Warning Light · failed · May 14, 2026 · N122UP · Airbus A300F4622R · Passenger/Crew Doors > WHEN I OPENED THE MAIN ENTRY DOOR THE PRESS WARNING LT UNIT FELL OUT. REMOVED AND REPLACED ESCAPE SLIDE LIGHT AND RECESSED PANEL ASSY. IAW AMM 57-73-11 AND 52-10-13 OPS CHECK GOOD - [SDR IPXA2026050716996](https://openairdocs.org/sdr/IPXA2026050716996.md): Skin · damaged · May 4, 2026 · N122UP · Airbus A300F4622R · Fuselage Main, Plate/Skin > *** MAJOR REPAIR *** TO LINK AND ACCOMPLISH EO-97088-REQ1 (N122UP: FUSELAGE SKIN LEFT AND RIGHT SIDE EXTERNAL DOUBLER REPAIRS AT FR7 AND FR8) REVIEWED - [SDR IPXA2026050177952](https://openairdocs.org/sdr/IPXA2026050177952.md): Skin Panel · damaged · May 1, 2026 · N122UP · Airbus A300F4622R · Fuselage Main, Plate/Skin > IN ORDER TO COMPLETE STEP 142 OF EA 300-5311-27-A4409, PRELIMINARY 5. ACCOMPLISHED PER STEP 142 OF EA 300-5311-27-A4409 PRELIMINARY 5. ACCOMPLISHED PER STEP 142 OF E.A.#: 300-5311-27-A4409 PRELIMINARY 5 AS A REQUIREMENT OF THE T3F18E008CUAT REPAIR. - [SDR IPXA2026042665993](https://openairdocs.org/sdr/IPXA2026042665993.md): Panel · cracked · Apr 24, 2026 · N122UP · Airbus A300F4622R · Wing Main, Frame Structure > DURING OK TO INSTALL PANEL 623BB, FOUND CRACK AT THE FWD UPPER RADIUS OF PANEL CUTOUT, DOT 55-006. INSTALLED REFORCING PLATE IAW SRM 57-41-12-227. - [SDR IPXA2026050281677](https://openairdocs.org/sdr/IPXA2026050281677.md): Fitting · damaged · Apr 1, 2026 · N122UP · Airbus A300F4622R · Wing Main, Frame Structure > THE R/H SIDE MIDDLE FASTENER HOLE INSIDE FR40 LWR JUNCTION, HAS ABRASION DAMAGE TO ALL LAYERS. INSTALLED PANELS (4 E/A) AT RH WING FRAME 40 LWR JUNTION IAW A300-600 SRM 51-40-21 - [SDR IPXA2026043082382](https://openairdocs.org/sdr/IPXA2026043082382.md): Fitting · corroded · Apr 1, 2026 · N122UP · Airbus A300F4622R · Wing Main, Frame Structure > THE RT SIDE TOP FASTENER HOLE INSIDE FR40 LWR JUNCTION, HAS PITTING CORROSION TO ALL LAYERS. INSTALLED PANELS (4 E/A) AT RH WING FRAME 40 LWR JUNTION IAW A300-600 SRM 51-40-21. THIS TASK CARD WAS WORKED IN CONJUNCTION WITH TASK CARD T3F18E008KY8Y. PRELIMINAR - [SDR IPXA2026040684589](https://openairdocs.org/sdr/IPXA2026040684589.md): Bracket · cracked · Apr 1, 2026 · N122UP · Airbus A300F4622R · Engine Thrust Reverser > ENG #1, I/B T/R UPPER AFT BRACKET HAS A CRACK. INSTALLED NEW BRAKET IN ENG #1, I/B T/R UPPER AFT PER SRM 51-40-21-001. - [SDR IPXA2026040286416](https://openairdocs.org/sdr/IPXA2026040286416.md): Ceiling Panel · corroded · Apr 1, 2026 · N122UP · Airbus A300F4622R · Passenger Compartment Equipment > FWD CARGO- PANEL 132LC HAS CORROSION AROUND 16EA HOLES. SH91148554. REMOVED CEILING STRUCTURE AT CROSS BEAM 54 STA Y-450 BTW Y+450 IAW SRM 51-40-21-001. INSTALLED NEW CEILING SUPPORT AT FRAME 54 IAW SRM 51-40-21-001. - [SDR IPXA2026033149250](https://openairdocs.org/sdr/IPXA2026033149250.md): Seat Track · corroded · Mar 30, 2026 · N122UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings > MDC SEAT TRACK ON -Y1221.2 AT FR 80 RH SIDE, CORRODED DOT 31-039. REMOVED CORROSION BY TOOL FROM SEAT TRACK -Y1221.2 AT FR 80 RH SIDE AND AFTER MESUARED FOUND WITHIN LIMITS. IAW A300-600 SRM 53-10-16. RESTORED SURFACE PROTECTION AT MDC SEAT TRACK ON -Y1221.2 - [SDR IPXA2026040347629](https://openairdocs.org/sdr/IPXA2026040347629.md): Intercostal · cracked · Mar 30, 2026 · N122UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > EMPENNAGE TAIL SECTION, INSIDE OF ACCESS DOOR 312AR R/SIDE LOWER AREA BTWN FR 85/86 INTERCOSTAL UPPER CHORD IS CRACKED AND BENTED. DOT 34-002 INSTALLED NEW INTERCOSTAL UPPER CHORD I.A.W A300-600 SRM 51-40-21 - [SDR IPXA2026040449560](https://openairdocs.org/sdr/IPXA2026040449560.md): Profile · cracked · Mar 30, 2026 · N122UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > MDC Z PROFILE BROKEN AT FR80 RH SIDE DOT 31-044 INSTALLED NEW Z PROFILE (PROFILE-T) I.A.W. SRM 51-40-21 - [SDR IPXA2026040549573](https://openairdocs.org/sdr/IPXA2026040549573.md): Profile · cracked · Mar 30, 2026 · N122UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > MDC Z PROFILE BROKEN AT FR80 LH SIDE. INSTALLED NEW PROFILE AT FR80 LH SIDE IAW SRM 51-40-21-001. - [SDR IPXA2026040649374](https://openairdocs.org/sdr/IPXA2026040649374.md): Profile · cracked · Mar 30, 2026 · N122UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > MDC Z PROFILE AT FR74 LH SIDE HAS A CRACK. VERIFIED INSTALLATION OF Z-PROFILE AT MDC LH FR 74-75 IAW SRM 51-40-21-001. - [SDR IPXA2026042734147](https://openairdocs.org/sdr/IPXA2026042734147.md): Longeron · gouged · Mar 29, 2026 · N122UP · Airbus A300F4622R · Engine Thrust Reverser > FAULT - STR Z400 - ENG #1, I/B T/R, INTERNAL STRUCTURE UPPER STRIP HAS GOUGES. DOT 90-24. REMOVED STRIP AT ENG #1, I/B T/R, INTERNAL STRUCTURE UPPER IAW A300-600 SRM 51-40-21-001 WIL BE REPLACE (BROKEN PART). ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97062-RE - [SDR IPXA2026042435568](https://openairdocs.org/sdr/IPXA2026042435568.md): Plate · cracked · Mar 29, 2026 · N122UP · Airbus A300F4622R · Engine Thrust Reverser > NR 1 PYLON, OTBD SIDE RIB 3, BRACKET HAS A CRACK. NEW FISHPLATE (BRACKET) AT PYLON #1, O/B SIDE RIB 3, INSTALLED IAW A300-600 SRM 51-40-21, JOB COMPLETED. REVIEWED - [SDR IPXA2026042434161](https://openairdocs.org/sdr/IPXA2026042434161.md): Bracket · damaged · Mar 29, 2026 · N122UP · Airbus A300F4622R · Engine Thrust Reverser > ENG #1, I/B T/R, INTERNAL STRUCTURE UPPER MIDDLE BRACKET DAMAGED. DOT 90-25. INSTALLED MIDDLE BRACKET IN ENG #1, I/B T/R, INTERNAL STRUCTURE UPPER. IAW P&W SRM 54-30-00, PAGE 98.138, ITEM 52 AND SRM 51-40-21. - [SDR IPXA2026040434749](https://openairdocs.org/sdr/IPXA2026040434749.md): Cleat · gouged · Mar 29, 2026 · N122UP · Airbus A300F4622R · Leading Edge Devices > RIGHT WING, KRUEGER BOX AREA, AFT STR, BTW RIB 1 AND 2, STRUCTURE WITH 4 GOUGE AND 4 RIVETS HEADS DAMAGE. INSTALLED NEW STRAP AT R/H WING, KRUEGER BOX AREA, AFT STR, BTW RIB 1 AND 2 IAW A300-600 SRM 51-40-21. - [SDR IPXA2026040835520](https://openairdocs.org/sdr/IPXA2026040835520.md): Plate · cracked · Mar 29, 2026 · N122UP · Airbus A300F4622R · Engine Thrust Reverser > NR 1 PYLON, INBD SIDE RIB 3, BRACKET HAS A CRACK. REMOVED 1EA BRACKET AT NR 1 PYLON, INBD SIDE RIB 3 IAW SRM 51-40-21. INSTALLED NEW FISHPLATE AT NR 1 PYLON, INBD SIDE RIB 3 IAW SRM 51-40-21. - [SDR IPXA2026040935958](https://openairdocs.org/sdr/IPXA2026040935958.md): Web · cracked · Mar 29, 2026 · N122UP · Airbus A300F4622R · Engine Thrust Reverser > NR 1 ENG AFT FAIRING LOWER SURFACE HAS A CRACK AND ELONGATED HOLE. INSTALLED NEW FAIRING LOWER, IAW SRM 51-40-21-001. - [SDR IPXA2026040234747](https://openairdocs.org/sdr/IPXA2026040234747.md): Bracket · cracked · Mar 29, 2026 · N122UP · Airbus A300F4622R · Wing, Attach Fittings > RIGHT WING, KRUEGER BOX AREA, FWD STR AT RIB 1, ATTACH BRACKET WITH CRACK. DOT 73-004 INSTALLED NEW BRACKET AT R/H WING, KRUEGER BOX AREA, FWD STR AT RIB 1:I.A.W. A300-600 SRM 51-40-21: - [SDR IPXA2026033134161](https://openairdocs.org/sdr/IPXA2026033134161.md): Bracket · damaged · Mar 29, 2026 · N122UP · Airbus A300F4622R · Engine Thrust Reverser > NR 1 ENG, INBD THRUST REVERSER, INTERNAL STRUCTURE UPPER MIDDLE BRACKET DAMAGED. - [SDR IPXA2026041403483](https://openairdocs.org/sdr/IPXA2026041403483.md): Flap · cracked · Mar 27, 2026 · N122UP · Airbus A300F4622R · Trailing Edge Flaps > *** MAJOR REPAIR *** FAULT: 1EA CRACKS FOUND AT R/H RIB 15 CENTER WING FLAP TOP SKIN AND RIB FLANGES BETWEEN THE TRACKS. MARKED IN RED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96975-REQ1 AND VT-MAE EA 300-5753-27-A4410, REV. -. - [SDR IPXA2026033103502](https://openairdocs.org/sdr/IPXA2026033103502.md): Skin · cracked · Mar 27, 2026 · N122UP · Airbus A300F4622R · Trailing Edge Flaps > MAJOR RPAIR, 1EA CRACKS FOUND AT RT RIB 26 CENTER WING FLAP TOP SKIN AND RIB FLANGES BETWEEN THE TRACKS. ACCOMPLISHED PERMANTENT REPAIR IN ACCORDANCE WITH EO-96969-REQ1 AND VT-MAE EA 300-5753-27-A4408, REV. -. - [SDR IPXA2026042710419](https://openairdocs.org/sdr/IPXA2026042710419.md): Skin · cracked · Mar 27, 2026 · N122UP · Airbus A300F4622R · Trailing Edge Flaps > LEFT WING I/B FLAP UPPER SURFACE I/B RUB STRIP HAS A CRACK AND ARROUN IT SKIN TOO, ALSO NEEDS A INPECTION UNDER IT TO RULE OUT DAMAGE TO THE RIB DOT 31-015 ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97032-REQ1 AND VT-MAE EA 300-5752-27-A4416, REV. _. - [SDR IPXA2026040303576](https://openairdocs.org/sdr/IPXA2026040303576.md): Skin · cracked · Mar 27, 2026 · N122UP · Airbus A300F4622R · Trailing Edge Flaps > TWO CRACKS FOUND AT LT RIB 26 CENTER WING FLAP TOP SKIN AND RIB FLANGES BETWEEN THE TRACKS. PERFORMED CUTOUT OF CRACKED FLANGE ON RIB 26 STR 2.2 - 2.3 IAW SRM 57-50-00. INSTALLED REPAIR DOUBLER AT RIB 26 TO RIB 27 STR 2.1 TO STR 2.3 IAW SRM 51-40-21. - [SDR IPXA2026021846164](https://openairdocs.org/sdr/IPXA2026021846164.md): Skin · punctured · Oct 19, 2025 · N122UP · Airbus A300F4622R · Fuselage Main, Plate/Skin > MAJOR REPAIR, DURING JACKING OF AIRCRAFT, AIRCRAFT FELL OFF ALL THREE JACKS. ACCOMPLISH THE CATEGORY C MAJOR REPAIR PER EO-96552-REQ1. - [SDR IPXA2024092766148](https://openairdocs.org/sdr/IPXA2024092766148.md): Valve · faulted · Sep 24, 2024 · N122UP · Airbus A300F4622R · Fuel Transfer Valve > UNCOMMANDED FUEL MIGRATION RIGHT OUTER TANK REMOVED AND REPLACED RT INBD FILL VALVE. REF AMM 28-25-12 LEAK CK AND OPS CK GOOD. NO MIGRATION OF NOTED. OK FOR SERVICE. - [SDR IPXA2024092466148](https://openairdocs.org/sdr/IPXA2024092466148.md): Fuel Sys · malfunctioned · Sep 24, 2024 · N122UP · Airbus A300F4622R · Fuel Storage > UNCOMMANDED FUEL MIGRATION RIGHT OUTER TANK - [SDR IPXA2024022619351](https://openairdocs.org/sdr/IPXA2024022619351.md): Actuator · malfunctioned · Feb 22, 2024 · N122UP · Airbus A300F4622R · Autopilot System > *** ATB *** FAULT: PILOT REPORT AP 1 WOULD NOT COUPLE IN FLIGHT PERFORMED OPS CHECK OF YAW DAMPER ACTUATOR. OPS CHECK GOOD IAW AMM 22-26-00/501. PERFORMED AFS TEST. AFS TEST GOOD. IAW AMM 22-40-00/501 AC STILL CAT DOWNGRADED - [SDR IPXA2024022619435](https://openairdocs.org/sdr/IPXA2024022619435.md): Wire · broken · Feb 22, 2024 · N122UP · Airbus A300F4622R · Instrument System Wiring > FAULT: PILOT REPORT EMERGENCY CANCEL BUTTON SAFETY WIRE BROKEN. SAFETY WIRE INSTALLED ON EMERGENCY CANCEL BUTTON IAW AMM 20-11-11/001. - [SDR IPXA2024020837884](https://openairdocs.org/sdr/IPXA2024020837884.md): Adapter · broken · Feb 6, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, Structure > O/B L/H CLS ADAPTER AT FR37 IS BROKEN REMOVED AND REPLACED CLS ADAPTER IAW A300-600 SRM 51-40-21. INSTALLED SIDEWALL PANEL 131PW AND CEILING PANELS 131UC AND 131WC IAW A300-600 SRM 51-40-21 - [SDR IPXA2024020737884](https://openairdocs.org/sdr/IPXA2024020737884.md): Adapter · broken · Feb 6, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, Structure > O/B L/H CLS ADAPTER AT FR37 IS BROKEN REMOVED SIDEWALL PANEL 131PW AND CEILING PANELS 131UC AND 131WC FOR ACCESS IAW A300-600 SRM 51-41-21 - [SDR IPXA2024020150456](https://openairdocs.org/sdr/IPXA2024020150456.md): Floor Panel · cracked · Feb 1, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor Panel > FRAME 38.1 R/H SIDE HAS DOGBONE CRACKED O/B EDGE OF FLOOR PANEL. REMOVED AND REPLACED DOGBONE ON FRAME 38.1 RH SIDE O/B EDGE OF FLOOR PANEL IAW A300 SRM 51-40-21 REVIEWED - [SDR IPXA2024013116972](https://openairdocs.org/sdr/IPXA2024013116972.md): Access Panel · damaged · Jan 24, 2024 · N122UP · Airbus A300F4622R · Wing, Plate/Skin > ALL FASTENER HOLES IN THE LWR SIDE OUTER WING SKIN, FOR FUEL TANK ACCESS PANEL 550MB (NEAR RIB 24), HAVE CORROSION INDICATIONS INSIDE THE HOLES AND SURROUNDING OUTER SURFACE. REMOVED LIGHT CORROSION BY HAND IN HOLE AND SURROUNDING OUTER SURFACE IN PANEL 550MB, - [SDR IPXA2024013017376](https://openairdocs.org/sdr/IPXA2024013017376.md): Access Panel · corroded · Jan 24, 2024 · N122UP · Airbus A300F4622R · Wing, Plate/Skin > 13EA FASTENER HOLES IN THE LWR SIDE OUTER WING SKIN, FOR FUEL TANK ACCESS PNL 650LB (NEAR RIB 23), HAVE CORROSION INDICATIONS INSIDE THE HOLES AND 1EA OUT OF ROUND. ROTO PERFORMED ON FASTENER HOLES. NO DEFECTS FOUND IAW 51-10-01. - [SDR IPXA2024012493601](https://openairdocs.org/sdr/IPXA2024012493601.md): Deflector · broken · Jan 23, 2024 · N122UP · Airbus A300F4622R · Trailing Edge Flaps > RH WING CENTER FLAP OTBD END DEFLECTOR PLATE BROKEN REMOVED AND REPLACED DEFLECTOR PLATE ANGLE P/N A5796040221500 BATCH # 0004185041 IAW SRM 57-53-11 FIG 2. - [SDR IPXA2024020876679](https://openairdocs.org/sdr/IPXA2024020876679.md): Floorboard · cracked · Jan 22, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor Panel > *MAJOR REPAIR* FAULT-FLOOR PANEL 151NG CRACKED FABBED PNL 151NG FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED - [SDR IPXA2024013077745](https://openairdocs.org/sdr/IPXA2024013077745.md): Bracket · cracked · Jan 22, 2024 · N122UP · Airbus A300F4622R · Fuselage Main, Attach Fittings > AFT CARGO COMP FR54 Y -1959 BRACKET CRACKED INSTALLED AFT. CARGO COMP BRACKET AT FR54 -Y 1959 P/N A5341076521900 BATCH #0004158669 AND MS20470AD5-6 IAW SRM 51-40-21. - [SDR IPXA2024022236204](https://openairdocs.org/sdr/IPXA2024022236204.md): Skin · contaminated · Jan 19, 2024 · N122UP · Airbus A300F4622R · Elevator, Plate/Skin > FOUND WATER INTRUSION ON THE UPPER SURFACE OF THE R/H ELEVATOR. AREA MARKED IN RED VERIFIED INSTALLED R/H ELEVATOR I.A.W A300 AMM 27-31-24/401 REVIEWED - [SDR IPXA2024012536204](https://openairdocs.org/sdr/IPXA2024012536204.md): Skin · contaminated · Jan 19, 2024 · N122UP · Airbus A300F4622R · Elevator, Plate/Skin > *SDR FILED OPEN* FAULT: FOUND WATER INTRUSION ON THE UPPER SURFACE OF THE R/H ELEVATOR. AREA MARKED IN RED VERIFIED SAFETY LOCK WASHERS INSTALLED - [SDR IPXA2024012319999](https://openairdocs.org/sdr/IPXA2024012319999.md): Shear Web · cracked · Jan 18, 2024 · N122UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > FAULT AT FRAME 75-76 HAS A CRACKED ON WEB ON R/H SIDE INSTALLED NEW SHEER WEB AT FRAME 67 TO FRAME 77 R/H IAW SRM 51-40-21 (P/N HL18PB6-3). - [SDR IPXA2024020801253](https://openairdocs.org/sdr/IPXA2024020801253.md): Floor Panel · cracked · Jan 17, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor Panel > FWD CARGO FLOOR PNL 131GE CRACKED DOT 146-162 FABBED PNL 131GE FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED - [SDR IPXA2024020801348](https://openairdocs.org/sdr/IPXA2024020801348.md): Floorboard · cracked · Jan 17, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor Panel > FWD CARGO FLOOR PNL 131RG CRACKED DOT 146-165 FABBED PNL 131RG FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED - [SDR IPXA2024020801293](https://openairdocs.org/sdr/IPXA2024020801293.md): Floor Panel · cracked · Jan 17, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor Panel > FWD CARGO FLOOR PNL 132MG CRACKED DOT 146-163 VERIFIED. FABBED PNL 132MG FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED - [SDR IPXA2024020801181](https://openairdocs.org/sdr/IPXA2024020801181.md): Floor Panel · cracked · Jan 17, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor Panel > FWD CARGO FLOOR PNL 131DE CRACKED DOT 146-160 VERIFIED FABBED PNL 131DE FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED - [SDR IPXA2024020981253](https://openairdocs.org/sdr/IPXA2024020981253.md): Floor Panel · cracked · Jan 17, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor Panel > *SDR FILED OPEN* FAULT-FWD CARGO FLOOR PNL 131GE CRACKED DOT 146-162 VERIFIED - [SDR IPXA2024020804223](https://openairdocs.org/sdr/IPXA2024020804223.md): Floorboard · cracked · Jan 17, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor Panel > AFT CARGO FLOOR PANEL 152VF CRACKED. FABBED PNL 152VF FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED - [SDR IPXA2024020901348](https://openairdocs.org/sdr/IPXA2024020901348.md): Floor Panel · cracked · Jan 17, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor Panel > *OPEN* FWD CARGO FLOOR PNL 131RG CRACKED. - [SDR IPXA2024020801315](https://openairdocs.org/sdr/IPXA2024020801315.md): Floor Panel · cracked · Jan 17, 2024 · N122UP · Airbus A300F4622R · Fuselage Floor Panel > FWD CARGO FLOOR PNL 131FE CRACKED DOT 146-164 FABBED PNL 131FE FROM 4522-374001CB-8 BAT# 3996294 PER SREO A300-5320-16407-E REVIEWED Next page: https://openairdocs.org/aircraft/N122UP/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 = 'N122UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N122UP/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.