# Service difficulty reports: N162UP A list on [N162UP](https://openairdocs.org/aircraft/N162UP.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 · 162 reports - [SDR IPXA2026032099651](https://openairdocs.org/sdr/IPXA2026032099651.md): Warning Buzzer · inoperative · Mar 16, 2026 · N162UP · Airbus A300F4622R · Door Warning System > BUZZER AND RED LIGHT TO L1 DOOR ESCAPE SLIDE IS INOPERATIVE. PERFORMED OPS CHECK OF L1 DOOR BUZZER AND WARNING LIGHT IAW AMM 52-73-12-0401 AND 52-73-11-0401, OPS CHECKED GOOD. PERFORMED BITE CHECK OF 70WN AUTONOMOUS STANDBY POWER SUPPLY UNIT IAW 52-73-00-05 - [SDR IPXA2026031799651](https://openairdocs.org/sdr/IPXA2026031799651.md): Slide · inoperative · Mar 16, 2026 · N162UP · Airbus A300F4622R · Escape Slide > BUZZER AND RED LIGHT TO L1 DOOR, ESCAPE SLIDE IS INOPERATIVE. PANELS 831FZ, 831DZ, 831CZ, & 831BZ REMOVED IAW AMM 52-10-13-0401. - [SDR IPXA2026031861571](https://openairdocs.org/sdr/IPXA2026031861571.md): Plate · damaged · Mar 13, 2026 · N162UP · Airbus A300F4622R · Wing Structure > HOLES IN REINFORCING PLATE P/N: A57244651203 UNDERLYING STRUCTURE LOOKING FWD FOUND HOLE DIAMETER TO BE AT 0.250" 35(EA) WITH SHORT EDGE DISTANCE (1.5D). IT WAS FOUND OUT OF LIMITS. INSTALLED NEW REINFORCING PLATE P/N A57244651203 IAW SRM 51-40-21-001 AND S - [SDR IPXA2026031493952](https://openairdocs.org/sdr/IPXA2026031493952.md): Bracket · cracked · Mar 9, 2026 · N162UP · Airbus A300F4622R · Leading Edge Devices > LEFT WING, KRUEGER AREA, OTBD INNER BRACKET HAS A CRACK. INSTALLED NEW ANGLE IAW SRM51-40-21-001. - [SDR IPXA2026031987548](https://openairdocs.org/sdr/IPXA2026031987548.md): Pressure Blkhd · dented · Mar 3, 2026 · N162UP · Airbus A300F4622R · Fuselage Main, Bulkhead > MAJOR REPAIR, THROUGH RADOME 110AL, FWD PRESSURE BULKHEAD, ABOVE LOCALIZER ANTENNA RH ATTACHMENT HAS BULGE. DOT 103-25 ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96865-REQ1 AND VT-MAE EA 300-5311-27-A4387, REV. -. - [SDR IPXA2026031781646](https://openairdocs.org/sdr/IPXA2026031781646.md): Bracket · cracked · Mar 2, 2026 · N162UP · Airbus A300F4622R · Wing, Attach Fittings > LH WING, KRUEGER AREA, I/B INNER BRACKET HAS A CRACK. DOT 90-04 VERIFIEDÂ NEW BRACKET AT LH WING KRUEGER AREA INSTLLED IAW A300-600 SRM 51-40-21, JOB COMPLETED. - [SDR IPXA2026031781689](https://openairdocs.org/sdr/IPXA2026031781689.md): Bracket · cracked · Mar 2, 2026 · N162UP · Airbus A300F4622R · Wing, Attach Fittings > LH WING, KRUEGER AREA, I/B BRACKET HAS A CRACK. DOT 90-05 VERIFIED NEW BRAKET INSTALLATION IAW SRM 51-40-21 ON LH WING, KRUEGER I/B AREA. - [SDR IPXA2026031475852](https://openairdocs.org/sdr/IPXA2026031475852.md): Web · cracked · Mar 2, 2026 · N162UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure > NR 1 ENG, AFT PYLON, INNER BOX, BTWN RIB 19 TO RIB 20, PLATE STRUCTURE AT HYD PRESSURIZATION LINE FITTING CUTOUT HAS A CRACKS (2EA). REMOVED WEB FROM #1 PYLON LOWER SPAR EXTENTION MEMBER UNDER AFT FAIRING IAW SRM 51-40-21-001. INSTALLED SPAR EXTENTION MEMBER A - [SDR IPXA2026031281768](https://openairdocs.org/sdr/IPXA2026031281768.md): Bracket · cracked · Mar 2, 2026 · N162UP · Airbus A300F4622R · Wing Miscellaneous Structure > LEFT WING, ACCESS PANEL 575AB AREA, INNER TOP BRACKET HAS A CRACK. REMOVED BRACKET AT LT WING, ACCESS PANEL 575AB AREA, INNER TOP. IAW SRM-51-40-21. INSTALLED PLATE MOUNTING USING EXISTING FASTENERS, IAW SRM 51-40-21. - [SDR IPXA2026031383459](https://openairdocs.org/sdr/IPXA2026031383459.md): Bracket · cracked · Mar 2, 2026 · N162UP · Airbus A300F4622R · Wing Miscellaneous Structure > RIGHT WING LEADING EDGE INSIDE THE ACCES PANEL 675AB HYD LNES SUPPORT BRACKET BROKEN. INSTALLED NEW BRACKET-MOUNTING AT RT WING LEADING EDGE INSIDE THE ACCES PANEL 675AB, IAW SRM 51-40-21. - [SDR IPXA2026032467813](https://openairdocs.org/sdr/IPXA2026032467813.md): Bracket · cracked · Mar 1, 2026 · N162UP · Airbus A300F4622R · Wing, Attach Fittings > UPPER I/B ATTACH ANGLE FITTING CRACKED FROM HOLE TO EDGE-109-028-VWV INSTALLED NEW BRACKET IAW A300-600 SRM 51-40-21-001 AT ZONE 600-632BB UPPER I/B - [SDR IPXA2026030469211](https://openairdocs.org/sdr/IPXA2026030469211.md): Gimbal Joint · cracked · Mar 1, 2026 · N162UP · Airbus A300F4622R · Stabilizer Control System > THS ACTUATOR UPPER GIMBAL IS CRACKED. INSTALLED TAB WASHER IN HINGE ARMS SECTION B-B ITEM (27) IAW AMM 55-16-36-401. - [SDR IPXA2026031166900](https://openairdocs.org/sdr/IPXA2026031166900.md): Profile · cracked · Mar 1, 2026 · N162UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > LEFT BTW FR73-76 Z-PROFILE HAS A CRACK. REMOVED Z-PROFILE BTW FR73- FR76 IN ZONE 200 L/H SIDE IAW SRM 53-18-18 AND SRM 51-40-21. INSTALLED L/H BTW FR73-76 Z PROFILE MDC AFT SECTION IAW SRM 51-40-21-001. - [SDR IPXA2026031170844](https://openairdocs.org/sdr/IPXA2026031170844.md): Profile · cracked · Mar 1, 2026 · N162UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > MDC AFT SECTION RH SIDE, Z PROFILE CRACKED AT FR 74. REMOVED Z-PROFILE BTW FR73- FR76 IN MDC AFT SECTION RT SIDE IAW SRM 53-18-18 AND SRM 51-40-21. INSTALLED RT Z PROFILE MDC AFT SECTION IAW SRM 51-40-21-001. - [SDR IPXA2026031170858](https://openairdocs.org/sdr/IPXA2026031170858.md): Profile · cracked · Mar 1, 2026 · N162UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > MDC AFT SECTION LT SIDE, Z PROFILE CRACKED AT FR 79. REMOVED Z-PROFILE IN MDC AFT SECTION IAW SRM 53-18-18, AND SRM 51-40-21. INSTALLED THE PROFILE MDC AFT SECTION IAW SRM 51-40-21-001. - [SDR IPXA2026012041694](https://openairdocs.org/sdr/IPXA2026012041694.md): Unknown · odor · Jan 16, 2026 · N162UP · Airbus A300F4622R · Air Distribution System > IN DESCENT, BOTH PACKS ON AND ENGINE & WING ANTI ICE ON, AIR FLOW THRU DUCTS WAS VERY LOUD. PACK FLOW INDICATION ON ECAM, BOTH AMBER AND LOW FLOW POSITION. CONDITIONED AIR SMELLED HOT. BOTH TAKEOFF AND LANDING. PERFORMED OPS TEST OF PACKS IAW AMM 21-51-00. NO - [SDR IPXA2025120116797](https://openairdocs.org/sdr/IPXA2025120116797.md): Skin · cracked · Dec 1, 2025 · N162UP · Airbus A300F4622R · Fuselage Main, Plate/Skin > SECTION 18 LOWER SHELL REPLACEMENT AND INTERNAL STRUCTURE REPAIR. VERIFIED THAT REPAIR FOR SECTION 18 DAMAGE DUE TO TAILSTRIKE WAS REPAIRED ACCOMPLISHED ON AIRBUS WORK CARD 7086382 AND AIRBUS REPAIR DRAWING R53970080 ISSUE B. REPAIR THRESHOLD IS TO BE TRACKE - [SDR IPXA2025112536730](https://openairdocs.org/sdr/IPXA2025112536730.md): Skin · cracked · Nov 25, 2025 · N162UP · Airbus A300F4622R · Fuselage Main, Plate/Skin > SECTION 17 LOWER SKIN SPLICE REPAIR/REPLACEMENT AND INTERNAL STRUCTURE REPAIR. VERIFIED THAT THE DAMAGE TO SECTION 17 DUE TO THE TAIL STRIKE WAS REPAIRED IN ACCORDANCE WITH AIRBUS WORK CARD 7086383 AND AIRBUS REPAIR DRAWINGS R53970076 ISSUE B AND R53970056 I - [SDR IPXA2025112426003](https://openairdocs.org/sdr/IPXA2025112426003.md): Crossbeam · cracked · Nov 24, 2025 · N162UP · Airbus A300F4622R · Fuselage Main, Structure > SECTION 18 MAIN DECK FLOOR CROSSBEAM REPAIR AT FRAME 76 VERIFIED REPAIR ACCOMPLISHED ON AIRBUS WORK CARD 7086591 PER AIRBUS REPAIR DRAWING R53970070 ISSUE A. REPAIR THRESHOLD IS TO BE TRACKED ON EO-95628-REQ2. - [SDR IPXA2025112189231](https://openairdocs.org/sdr/IPXA2025112189231.md): Crossbeam · cracked · Nov 21, 2025 · N162UP · Airbus A300F4622R · Fuselage Main, Structure > SECTION 18 MAIN DECK CROSS BEAM DAMAGED AT FRAME 77 VERIFIED THAT THE DAMAGE DUE TO THE TAIL STRIKE WAS REPAIRED IN ACCORDANCE WITH UPS EO-95641-REQ1, AIRBUS WORK CARD 7088148 AND AIRBUS REPAIR DRAWING R53970074 ISSUE B. REPAIR THRESHOLD IS TO BE TRACKED ON EO - [SDR IPXA2025112068723](https://openairdocs.org/sdr/IPXA2025112068723.md): Skin · damaged · Nov 20, 2025 · N162UP · Airbus A300F4622R · Fuselage Main, Plate/Skin > FUSELAGE SKIN DAMAGE AT FR80/82 BETWEEN STR44LH AND STR 44RH VERIFIED THAT THE DAMAGE DUE TO THE TAIL STRIKE WAS REPAIRED IN ACCORDANCE WITH UPS EO-95523-REQ1, AIRBUS WORK CARD 7086636 AND AIRBUS REPAIR DRAWING R53970081 ISSUE B. REPAIR THRESHOLD IS TO BE TRAC - [SDR IPXA2025112401030](https://openairdocs.org/sdr/IPXA2025112401030.md): Skin · pilot error · Nov 16, 2025 · N162UP · Airbus A300F4622R · Fuselage Main, Plate/Skin > TAIL STRIKE EVENT - FUSELAGE AFT INTERMEDIATE SECTION SKIN/STRUCTURE REPLACEMENT/REPAIRS - [SDR IPXA2025120364540](https://openairdocs.org/sdr/IPXA2025120364540.md): Strut · cracked · Oct 31, 2024 · N162UP · Airbus A300F4622R · Fuselage Main, Floor Beam > )FLOOR BEAM STRUTS BROKEN AT FR 76 THESE ITEMS WERE REPLACED UNDER AIRBUS WORKCARD 7086382-20 AND TIED TO BARCODE T3F18E007T13S WHICH IS THE REPLACEMENT OF THE SECTION 18. ALL WORK CAN BE FOUND ON THAT BARCODE. - [SDR IPXA2025120364549](https://openairdocs.org/sdr/IPXA2025120364549.md): Strut · cracked · Oct 31, 2024 · N162UP · Airbus A300F4622R · Fuselage Main, Floor Beam > FLOOR BEAM STRUTS BROKEN AT FR 77 THESE ITEMS WERE REPLACED UNDER AIRBUS WORKCARD 7086382-020 AND TIED TO BARCODE T3F18E007T13S WHICH IS THE REPLACEMENT OF THE SECTION 18. ALL WORK CAN BE FOUND ON THAT BARCODE. - [SDR IPXA2024110727032](https://openairdocs.org/sdr/IPXA2024110727032.md): Skid · pilot error · Oct 29, 2024 · N162UP · Airbus A300F4622R · Fuselage Main, Structure > TAIL STRIKE C/W TAIL SKID INSPECTION PER AMM 05-51-21/001. FOUND EXTENSIVE DAMAGE TO LOWER FUSELAGE FROM FR70 THROUGH FR80. VERIFIED DFDR DATA WAS ROUTED TO APPROPRIATE PERSONEL. REFERENCE WORK PACKAGE NUMBER 13026706 FOR DOCUMENTED FAULT'S REQUIRING REPAIR. - [SDR IPXA2024103027032](https://openairdocs.org/sdr/IPXA2024103027032.md): Skin · pilot error · Oct 29, 2024 · N162UP · Airbus A300F4622R · Fuselage Main, Plate/Skin > SDR FILED OPEN, TAIL STRIKE. - [SDR IPXA2024102238823](https://openairdocs.org/sdr/IPXA2024102238823.md): Warning Message · false activation · Oct 20, 2024 · N162UP · Airbus A300F4622R · Cabin Pressure Control System > **EMERGENCY DECLARED**AT FL370 GOT EMERGENCY DESCENT ECAM CAB ALT ON OVERHEAD AND ECAM INDICATED 9800, CAB RATE APPROX 1000 FPM. PACK 2 WAS THE PACK OPERATING AT THAT TIME. DESCENDED TO 10000, (CONT IN FAULT DESCRIPTION) PERFORMED CABIN PRESSURIZATION AND CONT - [SDR IPXA2024042280142](https://openairdocs.org/sdr/IPXA2024042280142.md): Trim Panel · detached · Apr 19, 2024 · N162UP · Airbus A300F4622R · Passenger/Crew Doors > CREW ENTRY DOOR MOULDING HANDLE FELL OFF FOUND CREW ENTRY DOOR ASSIST HANDLE TOP SECTION AND SNAPPED BACK INTO PLACE IAW AMM 52-10-13. - [SDR IPXA85949](https://openairdocs.org/sdr/IPXA85949.md): Unknown · unknown · Dec 4, 2023 · N162UP · Airbus A300F4622R · Aircraft Fuel Distribution System > FUEL LEAK AT LOWER SURFACE OF L/H WING INBOARD OF ENGINE. POSSIBLE PRIOR CLICK PATCH INSTALL. ISOLATED LEAKING BOLT, INBOARD OF RIB 1 IN CENTER TANK AFT SECTION. PERFORMED REAPAIR INSIDE THE FUEL TANK. DESEALED, CLEANED AND RESEALED I.A.W SRM 51-76-20. FUELED - [SDR IPXA2023120585949](https://openairdocs.org/sdr/IPXA2023120585949.md): Unknown · unknown · Dec 4, 2023 · N162UP · Airbus A300F4622R · Aircraft Fuel Distribution System > FUEL LEAK AT LOWER SURFACE OF L/H WING INBOARD OF ENGINE. POSSIBLE PRIOR CLICK PATCH INSTALL. FOUND CLICK PATCH CURRENTLY INSTALLED AND FUEL LEAKING PAST IT. FUEL TANK PERMANENT REPAIR REQUIRED PER AMM 28-11-00-801 PARA 2.D.(I). - [SDR IPXA2023101164157](https://openairdocs.org/sdr/IPXA2023101164157.md): Unknown · unknown · Oct 7, 2023 · N162UP · Airbus A300F4622R · Leading Edge Slat Control System > *SUPPLEMENTAL SDR* L/H NOTCH FLAP FRAME CRACKED. REMOVED NOTCH FLAP UP TO AND INCLUDING AMM 27-87-13 PAGEBLOCK 0401 STEP B.(10). ROUTED TO SHEET METAL FOR DRILLING OF NEW NOTCH FLAP. COMPLETED REMAINING STEPS OF LEFT NOTCH FLAP REF AMM. 27-87-13-401 AND REINS - [SDR IPXA2023100964157](https://openairdocs.org/sdr/IPXA2023100964157.md): Unknown · unknown · Oct 7, 2023 · N162UP · Airbus A300F4622R · Trailing Edge Flaps > L/H NOTCH FLAP FRAME CRACKED REMOVED NOTCH FLAP UP TO AND INCLUDING AMM 27-87-13 PAGEBLOCK 0401 STEP B.(10). ROUTED TO SHEET METAL FOR DRILLING OF NEW NOTCH FLAP. QC MATCH DRILLED NEW PART IAW A300 SRM 51-00-00. FAILED NOTCH FLAP HANGER INSPECTION DURING RII - [SDR IPXA2023081493898](https://openairdocs.org/sdr/IPXA2023081493898.md): Web · dented · Aug 13, 2023 · N162UP · Airbus A300F4622R · Horizontal Stabilizer Structure > INSPECTION TYPE:CRH HORIZ. STAB BOX BETWEEN F87-88 STGR R33 WEB HAS A DENT.REPLACED IAW 51-31-00. - [SDR IPXA2023081493897](https://openairdocs.org/sdr/IPXA2023081493897.md): Web · dented · Aug 13, 2023 · N162UP · Airbus A300F4622R · Horizontal Stabilizer Structure > INSPECTION TYPE:CLH HORZ STAB BOX FRAME F86 WEB HAS A DENT.REPLACED IAW 51-31-00. - [SDR IPXA2023081493896](https://openairdocs.org/sdr/IPXA2023081493896.md): Web · dented · Aug 13, 2023 · N162UP · Airbus A300F4622R · Horizontal Stabilizer Structure > INSPECTION TYPE:CRH HORIZ. STAB BOX BETWEEN F85-86 STGR R33 WEB HAS A DENT.REPLACED IAW 51-31-00. - [SDR IPXA2023081293881](https://openairdocs.org/sdr/IPXA2023081293881.md): Frame · cracked · Aug 12, 2023 · N162UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib > INSPECTION TYPE:CPANEL 485AL HAS A CRACKED FRAME FLANGE.FABRICATED NEW FLANGE IAW SRM 55-55-51. - [SDR IPXA2023081493909](https://openairdocs.org/sdr/IPXA2023081493909.md): Floor Panel · damaged · Aug 7, 2023 · N162UP · Airbus A300F4622R · Fuselage Floor Panel > INSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131BH IS DAMAGED.FABBED PNL 131BH PER SREO A300-5320-16407. - [SDR IPXA2023081493910](https://openairdocs.org/sdr/IPXA2023081493910.md): Floor Panel · damaged · Aug 7, 2023 · N162UP · Airbus A300F4622R · Fuselage Floor Panel > INSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131GE IS DAMAGED.FABBED PNL 131GE PER SREO A300-5320-16407. - [SDR IPXA2023081493908](https://openairdocs.org/sdr/IPXA2023081493908.md): Floor Panel · damaged · Aug 7, 2023 · N162UP · Airbus A300F4622R · Fuselage Floor Panel > INSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131MG IS DAMAGED.FABBED PNL 131MG PER SREO A300-5320-16407. - [SDR IPXA2023081493907](https://openairdocs.org/sdr/IPXA2023081493907.md): Floor Panel · damaged · Aug 7, 2023 · N162UP · Airbus A300F4622R · Fuselage Floor Panel > INSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131AH IS DAMAGED.FABBED PNL 131AH PER SREO A300-5320-16407. - [SDR IPXA2023081493906](https://openairdocs.org/sdr/IPXA2023081493906.md): Floor Panel · damaged · Aug 7, 2023 · N162UP · Airbus A300F4622R · Fuselage Main, Plate/Skin > INSPECTION TYPE:C*** MAJOR REPAIR *** PNL 132MG IS DAMAGED.FABBED PNL 132MG PER SREO A300-5320-16407. - [SDR IPXA2023081493905](https://openairdocs.org/sdr/IPXA2023081493905.md): Floor Panel · damaged · Aug 7, 2023 · N162UP · Airbus A300F4622R · Fuselage Floor Panel > INSPECTION TYPE:C*** MAJOR REPAIR *** PANEL 132DE IS DAMAGED.FABBED PNL 132DE PER SREO A300-5320-16407. - [SDR IPXA2023081493904](https://openairdocs.org/sdr/IPXA2023081493904.md): Floor Panel · damaged · Aug 7, 2023 · N162UP · Airbus A300F4622R · Fuselage Floor Panel > INSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131SG IS DAMAGED.FABBED PNL 131SG PER SREO A300-5320-16407. - [SDR IPXA2023072893758](https://openairdocs.org/sdr/IPXA2023072893758.md): Fairing · cracked · Jul 28, 2023 · N162UP · Airbus A300F4622R · Nacelle/Pylon Structure > INSPECTION TYPE:CPANEL 413BL HAS A CRACK IN CORNER UNDER THE SEAL.REPAIRED CRACK IAW SRM 54-52-51. - [SDR IPXA2023081793947](https://openairdocs.org/sdr/IPXA2023081793947.md): Seat Track · gouged · Jul 21, 2023 · N162UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings > INSPECTION TYPE:1C*** MAJOR REPAIR *** SEAT TRACK IS GOUGED AT FRAME 80 BL - Y450.REPAIRED PER RCD 278425. - [SDR IPXA2023081793946](https://openairdocs.org/sdr/IPXA2023081793946.md): Seat Track · gouged · Jul 21, 2023 · N162UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings > INSPECTION TYPE:1C*** MAJOR REPAIR *** SEAT TRACK IS GOUGED AT FRAME 80 BL Y450.REPAIRED PER RCD 278423. - [SDR IPXA2023081793943](https://openairdocs.org/sdr/IPXA2023081793943.md): Seat Track · gouged · Jul 21, 2023 · N162UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings > INSPECTION TYPE:1C*** MAJOR REPAIR *** SEAT TRACK IS GOUGED AT FRAME 80 BL Y794.3.REPAIRED PER RCD 278424. - [SDR IPXA2023081693930](https://openairdocs.org/sdr/IPXA2023081693930.md): Support · cracked · Jul 21, 2023 · N162UP · Airbus A300F4622R · Fuselage Miscellaneous Structure > INSPECTION TYPE:1CSEAT TRACK WALL SUPPORT IS CRACKED AT FR 80 BL 1173.REMOVED, FABRICATED AND REPLACED IAW SRM 51-40-21. - [SDR IPXA2023082293986](https://openairdocs.org/sdr/IPXA2023082293986.md): Unknown · broken · Jul 19, 2023 · N162UP · Airbus A300F4622R · Wing, Plate/Skin > INSPECTION TYPE:1CPANEL 672GB HAS 2 BROKEN CLIPS.REMOVE AND INSTALLED IAW SRM 51-40-21. - [SDR IPXA2023082293985](https://openairdocs.org/sdr/IPXA2023082293985.md): Unknown · broken · Jul 19, 2023 · N162UP · Airbus A300F4622R · Wing, Plate/Skin > INSPECTION TYPE:1CPANEL 672LB HAS 2 BROKEN CLIPS.REMOVE AND INSTALLED IAW SRM 51-40-21. Next page: https://openairdocs.org/aircraft/N162UP/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 = 'N162UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N162UP/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.