N163UP

Service difficulty reports · 187

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 = 'N163UP' 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 IPXA2026100104566Light · no testSUPERNUMERARY AREA EMERGENCY LIGHT SYSTEM TEST FUNCTION INOP. REPLACED THE EMERGENCY LIGHT POWER SUPPLY UNIT REF AMM 33-51-14/0401, OPS CHECK GOOD.Sep 30, 2026 · N163UP · Airbus A300F4622R · Emergency LightingSDR IPXA2026060970478Fitting · damagedACCOMPLISHED REPAIR PER UPS EO-97677-REQ1 AND VT-MAE EA 300- 5710-27-A4483 REV._.Jun 8, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026061295129Keelbeam · crackedRT & LT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BTWN FR13A AND 14 REQUIRES MORE CLEANING FOR RE-INSPECTION OF AREA ACCOMPLISHED THE REPAIR PER EO-97712-REQ1 AND EA 300-5312-27-A4495, REV. _.May 8, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026051493816Hinge Fitting · brokenNR 1 ENG I\B FAN COWL INNER SURFACE FWD ATTACH FITTING BROKEN. INSTALLED NEW FWD FITTING AT #1 ENG I\B FAN COWL IAW SRM 51-40-21-001.May 8, 2026 · N163UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026061253833Keelbeam · crackedTHE R/H SIDE, BOTTOM AFT FASTENER HOLE BETWEEN FR13A & 14, IS IN AN OUT OF ROUND CONDITION AND IS GOUGED AROUND THE FASTENER HOLE ON THE BEAM FACE. ACCOMPLISHED THE REPAIR PER EO-97712-REQ1 AND EA 300-5312-27-A4495, REV. _.May 6, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026061253788Keelbeam · crackedMAJOR REPAIR, THE RT SIDE, BOTTOM FWD FASTENER HOLE BETWEEN FR13A & 14, IS IN AN OUT OF ROUND CONDITION AND IS GOUGED AROUND THE FASTENER HOLE ON THE BEAM FACE. ACCOMPLISHED THE REPAIR IAW EO-97712-REQ1 AND EA 300-5312-27-A4495, REV-, & GMM 04.02.May 6, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026061153760Keelbeam · crackedMAJOR REPAIR, THE LT SIDE, FWD BOTTOM KEELBEAM FASTENER HOLE BETWEEN FR13A & 14, HAS A CRACK IND. (1EA) BETWEEN THE 6 & 7 O'CLOCK POSITION. ACCOMPLISHED THE REPAIR PER EO-97711-REQ1 AND EA 300-5312-27-A4494, REV-, & GMM 04.02.May 6, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026051748003Fitting · damagedWHILE ACCOMPLISHING EO#7219-REQ001 REV1, HOLE "A", HOLE DIAMETER WAS FOUND OUT OF TOLERANCES, DWG MAPPING ATTACHED WITH DETAILS OF TOLERANCE. RECEIVED AND ACCOMPLISHED THE REPAIR EO-97617-REQ1 WITH EA# 300-5710-27-A4469 REV.-. MAJOR REPAIR.Apr 23, 2026 · N163UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026052712905Sidewall Panel · damagedPANEL EXT SURFACE DAMAGED. 5 ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97691-REQ1 AND VT-MAE EA 300-2555-27-A4503. REV. _.Apr 21, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042900034Latch · no testENG #2 O/B FAN COWL PRESSURE RELIEF DOOR LATCH TEST FAILED. REPLACED 1EA DOOR LATCH AT ENG. #2 O/B FAN COWL PRESURE RELIEF DOOR IAW A300-600 SRM 51-40-21-001.Apr 21, 2026 · N163UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026043094249Retainer · crackedNR 1 ENG OUTBD T/R LOWER CIRCUMFERENTIAL STRAP RETAINER BRACKET IS CRACKED. INSTALLED NEW BRACKET #1 ENG OUTBD T/R LOWER CIRCUMFERENTIAL STRAP.IAW A300-600 SRM 51-40-21/001.Apr 20, 2026 · N163UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2026060294870Rub Strip · gougedNR 1 ENG INBD T/R UPPER AFT METALLIC STRIP IS GOUGED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97623-REQ1 AND VT-MAE EA 300-5430-27-A4474, REV. -.Apr 20, 2026 · N163UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2026050181377Skin · dentedRH WING LEADING EDGE WING TIP SKIN COVER WITH DENTED. INSTALLED RH WING LEADING EDGE TIP SKIN IAW SRM 51-40-21-001.Apr 19, 2026 · N163UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2026051480291Bracket · crackedENG #2, I/B T/R UPPER AFT BRACKET HAS A CRACK. REMOVED AFT BRACKET (CLOSURE) P/N 221-6546-501 AT ENG #2, I/B T/R UPPER IAW SRM 51-40-21-001. INSTALLED CLOSURE ON ENG #2, I/B T/R UPPER AFT EDGE IAW SRM 51-40-21-001.Apr 19, 2026 · N163UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2026042970084Profile · crackedM.C.DECK LH FR#79 Z-PROFILE CRACKED DOT#58-07. REMOVED CRACKED Z-PROFILE BTW C77 TO C79 LH SIDE MAIN DECK IAW A300-600 SRM 51-40-21-001. INSTALLED NEW Z-PROFILE AT M.C. DECK LH FR#79 IAW A300-600 SRM 51-40-21.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026051567724Structure · corrodedAFT CARGO-FRAME 58 CEILING STRUCTURE FROM LH TO RH SIDE HAS CORROSION AROUND MULTIPLE HOLES. SH 91148554. REMOVED (07 EA) RECEPTACLES FROM ANGLE SUPPORT, CEILING ESTRUCTRURE BETWEEN Y450 AND Y2462 ,FOR ACCESS IAW A300-600 SRM 51-40-21-001. REMOVED DAMAGE (07 Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026050267681Profile · corrodedAFT CARGO-FRAME 57 CEILING STRUCTURE FROM LH TO RH SIDE HAS CORROSION AROUND MULTIPLE HOLES. SH 91148554. REMOVED DAMAGE (02 EA) ON ANGLE SUPPORT, CEILING STRUCTRURE FR-57, BETWEEN Y1959 AND Y450 IAW A300-600 SRM 51-74-10-201. INSTALLED NEW PROFILE (CEILING STApr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026051567636Profile · corrodedAFT CARGO-FRAME 54-54.2 CEILING STRUCTURE RUNNING FWD AND AFT, LH AND RH STRUCTURE HAS CORROSION AROUND MULTIPLE HOLES. REMOVED DAMAGE (01 EA) ON ANGLE SUPPORT, CEILING ESTRUCTRURE BETWEEN CROSS BEAM 54 TO 54.2 , Y-450. IAW SRM 51-74-10-201. INSTALLED NEW PLApr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026051167251Cover · brokenFWD CREW DOOR HAS BROKEN SLIDE ARM/DISARM COVER. REMOVED SLIDE ARM/DISARM COVER IAW AMM 52-10-13/401. INSTALLED SLIDE ARM/DISARM COVER IAW 52-10-13/401.Apr 18, 2026 · N163UP · Airbus A300F4622R · Escape SlideSDR IPXA2026042968001Bracket · crackedAFT CARGO- FRAME 54 RH SIDEWALL BRACKET IS CRACKED. INSTALLED BRACKET AT FRAME 54 RH SIDEWALL, IAW A300-600- SRM 51-40-21-001. NEW PART NUMBER A53410765218PNSU, IAW GMM 09.08.01.04.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050170017Web · crackedMAIN CARGO DECK RT FR 77 OTBD OF SIDEWALL LOWER WEB HAS A CRACK. REMOVED CRACKED WEB BTW C76 TO C77 RT SIDE MAIN DECK IAW SRM 51-40-21-001. INSTALLED NEW WEB 2 ANGLES AND 1 PROFILE ON MAIN CABIN BETWEEN C76 TO C77 SIDEWALL LOWER I.A.W AIRBUS SRM 51-40-21.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050267675Crossbeam · corrodedAFT CARGO-FRAME 54.2 CEILING STRUCTURE FROM LT TO RT SIDE HAS CORROSION AROUND MULTIPLE HOLES. INTALLED NEW PROFILE-CROSS FRAME 54.2 STA Y-450 TO Y450 AND Y-450 TO Y-1959 IAW SRM 51-40-21-001.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026042968063Bracket · crackedAFT CARGO- FRAME 54 LT SIDEWALL BRACKET IS CRACKED. INSTALLED BRACKET AT FRAME 54 LH SIDEWALL, IAW SRM 51-40-21-001.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042969269Attach Bracket · brokenLOWER HALF FUSL TAIL SECTION JACK SUPPORT AREA ATTACH BRACKETS BROKEN 2EA. REMOVED 2(EA) BRACKETS L/H & R/H SIDE AT LWR HALF FUSE TAIL SECTION JACK SUPPORT AREA IAW SRM 51-40-21-001. INSTALLED 2 (E/A) ANGLE IAW SRM 51-40-21.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, Attach FittingsSDR IPXA2026042870068Profile · crackedMAIN CARGO DECK RH FR 74 Z PROFILE CRACKED. REMOVED CRACKED Z-PROFILE BTW C73 TO C76 RH SIDE MAIN DECK IAW SRM 51-40-21-001. INSTALLED NEW Z-PROFILE TRAVELER NUMBER:T26/1862656 BTW C73 TO C76 RH SIDE MAIN DECK IAW SRM 51-40-21-001. OK TO TOP COAT HEAD OF FASTApr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042870092Profile · crackedMAIN CARGO DECK LT FR 74 Z-PROFILE CRACKED. REMOVED CRACKED Z-PROFILE BTW C73 TO C76 LH SIDE MAIN DECK IAW SRM 51-40-21-001. INSTALLED NEW Z-PROFILE AT MAIN CABIN L/H C73 TO C76 IAW SRM 51-40-21-001.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042067251Cover · brokenFWD CREW DOOR HAS BROKEN SLIDE ARM/DISARM COVER APPROVEDApr 18, 2026 · N163UP · Airbus A300F4622R · Escape SlideSDR IPXA2026061056763Splice Angle · gougedMAIN CARGO DECK RT FRAME 47 SPLICE FITTING BETWEEN STRG 24 AND STRG 26 HAS (2 EA) SPOTS OF TOOLING DAMAGE ON AFT FACE ON SPLICE FITTING. ACCOMPLISHED PERMANENT REPAIR PER EO-97689-REQ1 AND EA 300-5236-27-A4484 REV.Apr 17, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026061056670Fitting · gougedMAIN CARGO DECK RH FRAME 47 SPLICE FITTING BETWEEN STRG 24 AND STRG 26 HAS GOUGES ON FWD FACE OF SPLICE FITTING. ACCOMPLISHED PERMANENT REPAIR PER EO-97689-REQ1 AND EA 300-5236-27-A4484 REV. -.Apr 17, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025021186763Bottle · low pressureL1 DOOR SLIDE OF OF GREEN BAND. REMOVED AND REPLACED ESCAPE SLIDE IAW A300 AMM 25-61-21-0401.Feb 11, 2025 · N163UP · Airbus A300F4622R · Escape SlideSDR IPXA2025012423113Bustle · unsecure*EMERGENCY SLIDE BUSTLE ON CREW DOOR NOT SECURED TO DOOR AND DAMAGED. REMOVED AND REPLACED EMERGENCY SLIDE DECORATIVE COVER AND SECURED SAME DOOR CKS GOOD REF A300 AMM 25-61-21Jan 22, 2025 · N163UP · Airbus A300F4622R · Escape SlideSDR IPXA2024112699633Warning Light · inoperativeTHE WARNING LIGHT ON THE CREW ENTRY DOOR IS INOPERATIVE. WARNING LIGHT FOR THE ESCAPE SLIDE . BUZZER IS OPERATIVE PERFORMED OPS CK OF DOOR WARNING LT REF AMM 52-73-11 . OPS CK GOODNov 26, 2024 · N163UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2023113066828Flap · damaged*SUPPLEMENTAL SDR* L/H KRUGER FLAP SURROUND HAS DAMAGE STRUCTURE DAMAGE INSTALLED NEW UPPER SKIN RIBS & STRUCTURE REF SRM 51-40-21Nov 19, 2023 · N163UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2023113072262Slat · damaged*SUPPLEMENTAL SDR* LEFT WING I/B SLAT I/B EDGE DAMAGE. COMPLETED INSTALLATION OF LH #1 SLAT IAW AMM 27-80-11/401. OPS AND FIT CHECK GOOD.Nov 19, 2023 · N163UP · Airbus A300F4622R · Leading Edge Slat Control SystemSDR IPXA2023112266828Unknown · unknown*SDR FILED OPEN* L/H KRUGER FLAP SURROUND HAS DAMAGE STRUCTURE DAMAGE REMOVED DAMAGED UPPER SKIN .RIBS & STRUCTURE FROM L/H KARMAN FAIRING REF SRM 53-15-63 & 51-40-21Nov 19, 2023 · N163UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2023112272262Unknown · unknown*SDR FILED OPEN* LEFT WING I/B SLAT I/B EDGE DAMAGENov 19, 2023 · N163UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2023113061044Flap · damagedDURING WALK AROUND FOUND EXTENSIVE DAMAGE TO LEFT WING KRUEGER FLAP. SEE TASK INFO FOR PHOTOS. ACCOMPLISHED AMM 27-88-11-0401 2C THRU END. ACCOMPLISHED AMM 27-87-11-0401 2D THRU END. ACCOMPLISHED AMM 27-87-14-0401 2E (4) THRU END. WITNESSED OPS CHECKS. RIG PINNov 18, 2023 · N163UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2023112061044Unknown · unknown*SDR FILED OPEN* DURING WALK AROUND FOUND EXTENSIVE DAMAGE TO LEFT WING KRUEGER FLAP. SEE TASK INFO FOR PHOTOSNov 18, 2023 · N163UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2023111500285Unknown · unknownATB AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. ECAM PROCEDURES FOLLOWED. RETURNED TO PHL WITH GEAR DOWN. WHEN TRYING TO RAISE GEAR HANDLE IT WOULD NOT RAISE ABOVE CENTER POSITION. ECAM STATED €ŒL/G NOT UP LOCKED" C/W SPACER ASSY. INSTALL IAW AMM 32-00-00. Nov 15, 2023 · N163UP · Airbus A300F4622R · Landing Gear Retraction/Extension SystemSDR IPXA2023100950591Battery · no test*** SUPPLEMENTAL SDR *** FAULT: CABIN EMERGENCY LIGHTIING SYSTEM FAILS OPS CHECK REVIEWEDOct 2, 2023 · N163UP · Airbus A300F4622R · Emergency LightingSDR IPXA2023100650591Unknown · unknown*** SDF FILED OPEN *** FAULT: CABIN EMERGENCY LIGHTIING SYSTEM FAILS OPS CHECK INSTALLED BATTERY EMERGENCY PWR SUPPLY UNIT IAW A300-600 AMM 33-51-14-0401. VERIFIED, OPS CHK GOODOct 2, 2023 · N163UP · Airbus A300F4622R · Emergency LightingSDR IPXA2023100926600Rudder · unknown*MAJOR REPAIR* FAULT: 554007-01-1-326/ RH RUDDER SKIN HAS WATER INGRESSION AT TE FASTENER LOCATION 3RD FROM THE TOP CIRCLED IN RED. ALL WORK ACCOMPLISHED PER RCD 298944. PER A300-6-- SRM 55-41-12-201 PARA 23 FIG 223A. SRI 55-41-2-006-00 FOR FUTURE INSPECTIONSSep 30, 2023 · N163UP · Airbus A300F4622R · Rudder StructureSDR IPXA2023100710211Adapter · corrodedFAULT-531388-01-1-231 MDC SEAT TRACK ADAPTERS AT LH AND RH OF Y0 HAVE LIGHT SURFACE CORROSION BETWEEN FR55 AND FR66 NO DOT INSTALLED CLS ADAPTER IAW SRM 51-40-21. REVIEWEDSep 30, 2023 · N163UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2023092894287Rudder · delaminatedINSPECTION TYPE:1C*MAJOR REPAIR* R/H RUDDER SKIN HAS WATER INGRESSION AT THE FASTENER LOCATION 3RD FROM THE TOP.REPAIRED PANEL IAW SRM 55-41-12-201 PAR. 23A. REFER TO SRI 55-41-12-2-006-00 FOR INSPECTION CRITERIA.Sep 21, 2023 · N163UP · Airbus A300F4622R · Rudder StructureSDR IPXA2023091894189Bracket · crackedINSPECTION TYPE:1CENG 1 PYLON FWD BRACKET UNDERNEATH BUTTERFLY PANEL HAS A CRACKREMOVED, FABRICATED AND INSTALLED IAW SRM 51-40-21Sep 18, 2023 · N163UP · Airbus A300F4622R · Engine Mount SectionSDR IPXA2023091894188Adapter · crackedINSPECTION TYPE:1CCRACK ON SEAT TRACK AROUND FLOOR PNL 241TK BETWEEN FT 37 AND FR 38REMOVED AND REPLACED IAW SRM 51-40-21Sep 18, 2023 · N163UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2023091894187Bracket · crackedINSPECTION TYPE:1CBRACKET BROKEN ON LH SIDEWALL BELOW FLOOR BETWEEN FR 39 AND FR 40REMOVED AND REPLACED IAW SRM 51-40-21Sep 18, 2023 · N163UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2023091894186Plate · crackedINSPECTION TYPE:1CRH PYLON ACCESS PANEL 424CR UPPER FWD CORNER SUPPORT PLATE HAS CRACKREMOVED, FABRICATED AND REPLACED IAW SRM 15-40-21Sep 18, 2023 · N163UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2023091894185Crossbeam · bentINSPECTION TYPE:1CCROSSBEAM P/N A5381337900040 AT FRAM 51 BETWEEN Y450 TO Y953 IS BENTREMOVED AND REPLACED IAW SRM 51-40-21Sep 18, 2023 · N163UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2023091894184Bracket · crackedINSPECTION TYPE:1CAFT CARGO COMPARTMENT FWD BULKHEAD AT FRAM 54 HAS A CRACKED SUPPORT BRACKETREMOVED AND REPLACED IAW SRM 51-40-21Sep 18, 2023 · N163UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
Back to N163UP