# Service difficulty reports: N154UP A list on [N154UP](https://openairdocs.org/aircraft/N154UP.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 5 · 223 reports - [SDR IPXA2026082388187](https://openairdocs.org/sdr/IPXA2026082388187.md): Controller · faulted · Aug 23, 2026 · N154UP · Airbus A300F4622R · Cabin Pressure Controller > AIR TURN BACK, DURING CLIMB OUT CAB PRESSURE ECAM ADVISORY DISPLAY V/S AT 0. THEREAFTER ECAM CABIN PRESS REG 1 FAULT. FOLLOWED ECAM AND TURNED NR 1 OFF. LEVELED OFF AT 14,000 AND CABIN ALTITUDE OF 14000'. ECAM SHOWED FWD. PERFORMED TECH RECOMMENDED FUNCTIONAL - [SDR IPXA2025030196232](https://openairdocs.org/sdr/IPXA2025030196232.md): Light · intermittent · Feb 28, 2025 · N154UP · Airbus A300F4622R · Emergency Lighting > LT OTBD CEILING LIGHT OUT SUPERNUMERARY AREA. PERFORMED OPS CK IAW AMM 33-21-00-501. TESTS GOOD. - [SDR IPXA2025022048585](https://openairdocs.org/sdr/IPXA2025022048585.md): Control Handle · inoperative · Feb 20, 2025 · N154UP · Airbus A300F4622R · Landing Gear Selector > AFTER T/O GEAR HANDLE SELECTED UP-GEAR DID NOT RETRACT. PER ECAM PLACED TO SYS#2 AND GEAR RETRACTED NORMALLY. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW AMM 32-31-11/401. OPS TEST GOOD. QA REPORTED GEAR SWING IS BEST PRACTICE BUT NOT REQUIRED. SUPERVI - [SDR IPXA2024121611147](https://openairdocs.org/sdr/IPXA2024121611147.md): Windshield · delaminated · Dec 14, 2024 · N154UP · Airbus A300F4622R · Flight Compartment Windows > SERIOUS DELIMITATION ON CAPT SIDE FRONT WINDSHIELD DELIMITATION INDICATES POSSIBLE EVIDENCE OF ARCING DELAMINATION ON CAPTAIN WINDSHIELD WAS FOUND TO BE WITHIN LIMITS IAW AMM 56-11-11/601 - [SDR IPXA2024101139400](https://openairdocs.org/sdr/IPXA2024101139400.md): Ground Wire · unlocked · Oct 3, 2024 · N154UP · Airbus A300F4622R · Equipment/Furnishings Wiring > DURING OPERATIONAL CHECK OF ESCAPE SLIDE WARNING LIGHT AND ANNUNCIATOR, BOTH THE LIGHT AND ANNUNCIATOR ARE NOT WORKING. PERFORMED FAULT ISOLATION IAW AMM 52-73-01 PAGE 5, DURING THE WIRING CHECK THE GROUND LINE IN THE TERMINAL BLOCK 6035VT CONTACT "B" FOUND UN - [SDR IPXA2024100439400](https://openairdocs.org/sdr/IPXA2024100439400.md): Annunciator · inoperative · Oct 3, 2024 · N154UP · Airbus A300F4622R · Door Warning System > DURING OPERATIONAL CHECK OF ESCAPE SLIDE WARNING LIGHT AND ANNUNCIATOR, BOTH THE LIGHT AND ANNUNCIATOR ARE NOT WORKING. - [SDR IPXA2024092741847](https://openairdocs.org/sdr/IPXA2024092741847.md): Floorbeam · cracked · Sep 27, 2024 · N154UP · Airbus A300F4622R · Fuselage Main, Floor Beam > AFT CARGO FR 54 RH SIDE HAS A CRACKED FLOOR SUPPORT ANGLE DOT 07586-02. INSTALLED FLOOR SUPPORT ANGLE AT AFT CARGO FR54 RH SIDE IAW A300-600 SRM 51-40-21. FASTENERS P/N:DAN5-6-6, BATCH:0004085822, P/N:BACC30M5, BATCH:0004143638, P/N:MS21060-3, BATCH:0004201914 - [SDR IPXA2024092620567](https://openairdocs.org/sdr/IPXA2024092620567.md): Web · cracked · Sep 26, 2024 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > LH SIDE OF THE E&E BAY HAS A CRACKED WEB BETWEEN FR 11 - 12 DOT 07586-01. INSTALLED WEB NEW P/N: UP513100-1.IAW A300-600 SRM 51-40-21. - [SDR IPXA2024091841773](https://openairdocs.org/sdr/IPXA2024091841773.md): Unknown · noise · Sep 17, 2024 · N154UP · Airbus A300F4622R · Standard Practices/Structures > DURING CLIMB THROUGH 10,000 EXPERIENCED A VERY LOUD NOISE AND VIBRATION WITH A TEMPORARY BURNING SMELL THAT LASTED APPROX TWO MINUTES. SUSPECT NOSE WHEEL ROTATION. EMERGENCY DECLARED, PERFORMED GVI OF AIRFRAME, NOSE WHEEL AND WHEEL WELL, FLIGHT BRAKE BAND. TI - [SDR IPXA2024022728743](https://openairdocs.org/sdr/IPXA2024022728743.md): Relay · faulted · Feb 23, 2024 · N154UP · Airbus A300F4622R · Engine Oil Pressure > ENG 1 OIL LO PR ECAM WARNING IMMEDIATELY AFTER LIFT OFF. DETERMINED IT WAS AN ERRONEOUS MESSAGE BASED ON ECAM AND ANALOGUE OIL PRESSURE GAUGES. DIVERT TO CAE WITH BOTH ENGINES OPERATING NORMALLY. OPS CHECKED LOW OIL PRESSURE SWITCH REF AMM 71-00-00, REPLACED - [SDR IPXA2024022628743](https://openairdocs.org/sdr/IPXA2024022628743.md): Oil System · low pressure · Feb 23, 2024 · N154UP · Airbus A300F4622R · Engine Oil Temperature > *** DIVERSION *** ENG 1 OIL LO PR ECAM WARNING IMMEDIATELY AFTER LIFT OFF. DETERMINED IT WAS AN ERRONEOUS MESSAGE BASED ON ECAM AND ANALOGUE OIL PRESSURE GAUGES. DIVERT TO CAE WITH BOTH ENGINES OPERATING NORMALLY. OPS CHECKED LOW OIL PRESSURE SWITCH REF AMM 7 - [SDR IPXA2022122889349](https://openairdocs.org/sdr/IPXA2022122889349.md): Slide · low pressure · Dec 28, 2022 · N154UP · Airbus A300F4622R · Escape Slide > SLIDE PRESSURE IN RED ZONE. R&R L1 DOOR ESCAPE SLIDE IAW AMM 25-61-21-0401, NO DEFECTS NOTED. PRESSURE GAUGE IS IN THE GREEN. - [SDR IPXA2022052582499](https://openairdocs.org/sdr/IPXA2022052582499.md): Ceiling Panel · cracked · May 25, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:C FWD CARGO COMP CEILING SUPPORT STRUCTURE AT FRAME 20 -Y2462 HAS CRACK.REMOVED, REPAIRED, AND INSTALLED IAW SRM 51-40-21. - [SDR IPXA2022052482448](https://openairdocs.org/sdr/IPXA2022052482448.md): Adapter · delaminated · May 24, 2022 · N154UP · Airbus A300F4622R · Fuselage Main, Structure > INSPECTION TYPE:C AFT CABIN SEAT TRACK ADAPTER AT FR 72 BETWEEN Y1456 AND Y1959 EXFOLIATED.REMOVED AND REPLACED CLS ADAPTER IAW-SRM 51-40-21. - [SDR IPXA2022052482447](https://openairdocs.org/sdr/IPXA2022052482447.md): Support Web · cracked · May 24, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:C L/H MAIN CABIN COMPARTMENT BEHIND LOWER SIDEWALL PANEL BETWEEN FR 38.1 AND FR 38.2 SUPPORT WEB CRACKED.INSTALLED SIDEWALL SUPPORT WEB IAW-SRM 51-40-21. - [SDR IPXA2022052582483](https://openairdocs.org/sdr/IPXA2022052582483.md): Crossbeam · bent · May 24, 2022 · N154UP · Airbus A300F4622R · Fuselage Main, Structure > INSPECTION TYPE:C CROSSBEAM AT FR48 -Y450 AND -Y953 IS BENT REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-21 - [SDR IPXA2022052582484](https://openairdocs.org/sdr/IPXA2022052582484.md): Rib · cracked · May 23, 2022 · N154UP · Airbus A300F4622R · Horizontal Stabilizer Structure > INSPECTION TYPE:C L/H HORIZONTAL STAB LEADING EDGE PANEL 331CB O/B RIB CRACKED INSTALLED RIB PANEL 331CB IAW SRM 51-40-21 - [SDR IPXA2022052382426](https://openairdocs.org/sdr/IPXA2022052382426.md): None · cracked · May 23, 2022 · N154UP · Airbus A300* · Fuselage Main, Structure > INSPECTION TYPE:CCLS ADAPTER AT FRAME 20 FRAME 20 APPROX -Y1959 BROKEN.INSTALLED NEW CLS ADAPTER IAW-SRM 51-40-21. - [SDR IPXA2022052182321](https://openairdocs.org/sdr/IPXA2022052182321.md): Plate · cracked · May 21, 2022 · N154UP · Airbus A300* · Wing, Plate/Skin > INSPECTION TYPE:1CLEFT KRUGER FLAP WING ACCESS PANEL HAS A CRACK ON PANEL PLATE. DOT A-13REMOVED AND REPLACED IAW SRM 51-40-21. - [SDR IPXA2022052182313](https://openairdocs.org/sdr/IPXA2022052182313.md): None · damaged · May 18, 2022 · N154UP · Airbus A300* · Fuselage Miscellaneous Structure > INSPECTION TYPE:CE/E FLOOR PANEL 122LF FOUND DAMAGEREPAIR IAW SREO A300-5320-42722F - [SDR IPXA2022051882233](https://openairdocs.org/sdr/IPXA2022051882233.md): Plate · elongated · May 18, 2022 · N154UP · Airbus A300* · Nacelle/Pylon Structure > INSPECTION TYPE:CL/H PYLON FAIRING PANEL 475AL LH SIDE UPPER EDGE 35EA ELONGATED FASTENER HOLES FWD TO AFT EDGES AS MARKED.INSTALLED NEW PLATE IAW-SRM 5-40-21. - [SDR IPXA2022051882204](https://openairdocs.org/sdr/IPXA2022051882204.md): Bracket · broken · May 17, 2022 · N154UP · Airbus A300F4622R · Engine Thrust Reverser > INSPECTION TYPE:C#1 ENG I/B T/R COWL CIRCUMFERENTIAL LATCH UPPER BRACKET BROKENREMOVED AND REPLACED BRACKET #1 ENG I/B T/R IAW SRM 51-40-21 - [SDR IPXA2022051882203](https://openairdocs.org/sdr/IPXA2022051882203.md): Support · bent · May 17, 2022 · N154UP · Airbus A300F4622R · Fuselage Main, Structure > INSPECTION TYPE:CW/W REAR ZONE FLOOR PANEL SUPPORT MIDDLE WEB IS BENTREFORMED SUPPORT WEB 2EA IAW SREO M-5100-41097-41097-E APPENDIX A STEP 11 - [SDR IPXA2022051882202](https://openairdocs.org/sdr/IPXA2022051882202.md): Plate · elongated · May 17, 2022 · N154UP · Airbus A300* · Nacelle/Pylon Structure > INSPECTION TYPE:CL/H PYLON FAIRING PANEL 475AL R/H SIDE UPPER EDGE 34EA ELONGATED HOLES FWD TO AFT EDGESINSTALLED NEW PLATE IAW SRM 51-40-21 - [SDR IPXA2022051882201](https://openairdocs.org/sdr/IPXA2022051882201.md): Longeron · none · May 17, 2022 · N154UP · Airbus A300* · Fuselage Structure (General) > INSPECTION TYPE:C#1 PYLON FAIRING PANEL 475AL R/H SIDE UPPER EDGE 34EA ELONGATED HOLES FWD TO AFT EDGESINSTALLED NEW LONGERON IAW SRM 51-40-21 - [SDR IPXA2022051882200](https://openairdocs.org/sdr/IPXA2022051882200.md): Longeron · none · May 17, 2022 · N154UP · Airbus A300* · Fuselage Structure (General) > INSPECTION TYPE:CR/H PYLON FAIRING PANEL 485AL L/H SIDE UPPER EDGE 35EA ELONGATED FASTENER HOLES FWD TO AFT EDGESINSTALLED NEW LONGERON IAW SRM 51-40-21 - [SDR IPXA2022051882199](https://openairdocs.org/sdr/IPXA2022051882199.md): Plate · none · May 17, 2022 · N154UP · Airbus A300* · Fuselage Structure (General) > INSPECTION TYPE:CR/H PYLON FAIRING PANEL 485AL L/H SIDE UPPER EDGE 35EA ELONGATED FASTENER HOLES FWD TO AFT EDGESINSTALLED NEW PLATE IAW SRM 51-40-21 - [SDR IPXA2022051882198](https://openairdocs.org/sdr/IPXA2022051882198.md): Longeron · none · May 17, 2022 · N154UP · Airbus A300* · Fuselage Structure (General) > INSPECTION TYPE:CR/H PYLON FAIRING PANEL 485AL R/H SIDE UPPER EDGE 35EA ELONGATED FASTENER HOLES FWD TO AFT EDGESINSTALLED NEW LONGERON IAW SRM 51-40-21 - [SDR IPXA2022051882197](https://openairdocs.org/sdr/IPXA2022051882197.md): Plate · none · May 17, 2022 · N154UP · Airbus A300* · Fuselage Structure (General) > INSPECTION TYPE:CR/H PYLON FAIRING PANEL 485AL R/H SIDE UPPER EDGE 35EA ELONGATED FASTENER HOLES FWD TO AFT EDGESINSTALLED NEW PLATE IAW SRM 51-40-21 - [SDR IPXA2022051882194](https://openairdocs.org/sdr/IPXA2022051882194.md): Support · broken · May 17, 2022 · N154UP · Airbus A300* · Fuselage Structure (General) > INSPECTION TYPE:CENG 2 PYLON SUPPORT WEB BTW PANEL 423AL/424AR AND 423BL CRACKEDINSTALLED SUPPORT WEB IAW SRM 51-40-21 - [SDR IPXA2022052482453](https://openairdocs.org/sdr/IPXA2022052482453.md): Floor Panel · damaged · Apr 26, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:A300PNL 152NG DAMAGED FABBED PER SREO A300-5320-16407-E - [SDR IPXA2022052482452](https://openairdocs.org/sdr/IPXA2022052482452.md): Floor Panel · damaged · Apr 26, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:A300PNL 151VF DAMAGEDFABBED PER SREO A300-5320-16407-E - [SDR IPXA2022052582476](https://openairdocs.org/sdr/IPXA2022052582476.md): Floor Panel · damaged · Apr 26, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:CPNL 252FK IS DAMAGED FABBED IAW SREO A300-5320-40552-B - [SDR IPXA2022052582475](https://openairdocs.org/sdr/IPXA2022052582475.md): Floor Panel · cracked · Apr 26, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:CPNL 152VF CRACKED FABBED PER SREO A00-5320-16407-E - [SDR IPXA2022052582474](https://openairdocs.org/sdr/IPXA2022052582474.md): Floor Panel · damaged · Apr 26, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:C PNL 132SG DAMAGED FABBED PER SREO A3005320-16407-E - [SDR IPXA2022052582472](https://openairdocs.org/sdr/IPXA2022052582472.md): Floor Panel · damaged · Apr 26, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:CPNL 132PG DAMAGEDFABBED PER SREO A300-5320-16407-E - [SDR IPXA2022052582471](https://openairdocs.org/sdr/IPXA2022052582471.md): Floor Panel · broken · Apr 26, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:C PNL 131 RG BROKENFABBED PER SREO A300-5320-16407-E - [SDR IPXA2022052582470](https://openairdocs.org/sdr/IPXA2022052582470.md): Floor Panel · damaged · Apr 26, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:CPNL 151KG DAMAGEDFABBED PER SREO A300-5320-16407-E - [SDR IPXA2022052582468](https://openairdocs.org/sdr/IPXA2022052582468.md): Floor Panel · damaged · Apr 26, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:CPNL 152 SF DAMAGEDFABBED PER SERO A300-5320-6407-E - [SDR IPXA2022052582467](https://openairdocs.org/sdr/IPXA2022052582467.md): Floor Panel · damaged · Apr 26, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:CPNL 132MG DAMAGEDFABBED PER SREO A300-5320-16407-E - [SDR IPXA2022052582466](https://openairdocs.org/sdr/IPXA2022052582466.md): Floor Panel · damaged · Apr 26, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:CPNL 13ZRG BROKENFABBED PER SREO A300-532-16407-E - [SDR IPXA2022052582465](https://openairdocs.org/sdr/IPXA2022052582465.md): Floor Panel · damaged · Apr 26, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:C PN 15ZLG DAMAGE FABBED PER SREO A300-5320-16407-E - [SDR IPXA2022051081918](https://openairdocs.org/sdr/IPXA2022051081918.md): Bracket · cracked · Apr 26, 2022 · N154UP · Airbus A300F4622R · Wing, Plate/Skin > INSPECTION TYPE:CLT WING KRUGER FLAP BOX BEHIND WEB PIN LOWER CHORD HAS 3EA BRACKET CRACKEDREMOVED, FABRICATED AND INSTALLED NEW BRACKETS IAW SRM 57-40-11 AND SRM 51-40-21 - [SDR IPXA2022052582524](https://openairdocs.org/sdr/IPXA2022052582524.md): Floor Panel · broken · Apr 25, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:A300MDC FLOOR PANEL 241FN IS BROKENREPAIRED MDC FLOOR PANEL 241FN AS NEEDED IAW EO NO A300-5320-42722-F - [SDR IPXA2022052582523](https://openairdocs.org/sdr/IPXA2022052582523.md): Floor Panel · broken · Apr 25, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:A300MDC FLOOR PANEL 231RG IS BROKENREPAIRED MDC FLOOR PANEL 231RG AS NEEDED IAW EO NO A300-5320-42722-F - [SDR IPXA2022052582482](https://openairdocs.org/sdr/IPXA2022052582482.md): Floor Panel · damaged · Apr 25, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:C PNL 252BN BROKEN FABBED IAW SREO A300-5320-40552-B - [SDR IPXA2022052582481](https://openairdocs.org/sdr/IPXA2022052582481.md): Floor Panel · damaged · Apr 25, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:C PNL 251VJ BROKEN FABBED IAW SREO A300-5320-40552-B - [SDR IPXA2022052582480](https://openairdocs.org/sdr/IPXA2022052582480.md): Floor Panel · damaged · Apr 25, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:C PNL 252LJ BROKEN FABBED IAW SREO A300-5320-40552-B - [SDR IPXA2022052582479](https://openairdocs.org/sdr/IPXA2022052582479.md): Floor Panel · damaged · Apr 25, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:CPNL 242LH CRACKED FABBED IAW SREO A300-5320-40552-B - [SDR IPXA2022052582478](https://openairdocs.org/sdr/IPXA2022052582478.md): Floor Panel · damaged · Apr 25, 2022 · N154UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:C PNL 241GN BROKEN FABBED IAW SREO A300-5320-40552-B Next page: https://openairdocs.org/aircraft/N154UP/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 = 'N154UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N154UP/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.