# Service difficulty reports: N163UP

A list on [N163UP](https://openairdocs.org/aircraft/N163UP.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 · 187 reports

- [SDR IPXA2026100104566](https://openairdocs.org/sdr/IPXA2026100104566.md): Light · no test · Sep 30, 2026 · N163UP · Airbus A300F4622R · Emergency Lighting
  > SUPERNUMERARY AREA EMERGENCY LIGHT SYSTEM TEST FUNCTION INOP. REPLACED THE EMERGENCY LIGHT POWER SUPPLY UNIT REF AMM 33-51-14/0401, OPS CHECK GOOD.
- [SDR IPXA2026060970478](https://openairdocs.org/sdr/IPXA2026060970478.md): Fitting · damaged · Jun 8, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > ACCOMPLISHED REPAIR PER UPS EO-97677-REQ1 AND VT-MAE EA 300- 5710-27-A4483 REV._.
- [SDR IPXA2026061295129](https://openairdocs.org/sdr/IPXA2026061295129.md): Keelbeam · cracked · May 8, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, Keel
  > RT & 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. _.
- [SDR IPXA2026051493816](https://openairdocs.org/sdr/IPXA2026051493816.md): Hinge Fitting · broken · May 8, 2026 · N163UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > NR 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.
- [SDR IPXA2026061253833](https://openairdocs.org/sdr/IPXA2026061253833.md): Keelbeam · cracked · May 6, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, Keel
  > THE 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. _.
- [SDR IPXA2026061253788](https://openairdocs.org/sdr/IPXA2026061253788.md): Keelbeam · cracked · May 6, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, Keel
  > MAJOR 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.
- [SDR IPXA2026061153760](https://openairdocs.org/sdr/IPXA2026061153760.md): Keelbeam · cracked · May 6, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, Keel
  > MAJOR 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.
- [SDR IPXA2026051748003](https://openairdocs.org/sdr/IPXA2026051748003.md): Fitting · damaged · Apr 23, 2026 · N163UP · Airbus A300F4622R · Wing Main, Frame Structure
  > WHILE 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.
- [SDR IPXA2026052712905](https://openairdocs.org/sdr/IPXA2026052712905.md): Sidewall Panel · damaged · Apr 21, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > PANEL EXT SURFACE DAMAGED. 5 ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97691-REQ1 AND VT-MAE EA 300-2555-27-A4503. REV. _.
- [SDR IPXA2026042900034](https://openairdocs.org/sdr/IPXA2026042900034.md): Latch · no test · Apr 21, 2026 · N163UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > ENG #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.
- [SDR IPXA2026043094249](https://openairdocs.org/sdr/IPXA2026043094249.md): Retainer · cracked · Apr 20, 2026 · N163UP · Airbus A300F4622R · Engine Thrust Reverser
  > NR 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.
- [SDR IPXA2026060294870](https://openairdocs.org/sdr/IPXA2026060294870.md): Rub Strip · gouged · Apr 20, 2026 · N163UP · Airbus A300F4622R · Engine Thrust Reverser
  > NR 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. -.
- [SDR IPXA2026050181377](https://openairdocs.org/sdr/IPXA2026050181377.md): Skin · dented · Apr 19, 2026 · N163UP · Airbus A300F4622R · Wing, Plate/Skin
  > RH WING LEADING EDGE WING TIP SKIN COVER WITH DENTED. INSTALLED RH WING LEADING EDGE TIP SKIN IAW SRM 51-40-21-001.
- [SDR IPXA2026051480291](https://openairdocs.org/sdr/IPXA2026051480291.md): Bracket · cracked · Apr 19, 2026 · N163UP · Airbus A300F4622R · Engine Thrust Reverser
  > ENG #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.
- [SDR IPXA2026042970084](https://openairdocs.org/sdr/IPXA2026042970084.md): Profile · cracked · Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > M.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.
- [SDR IPXA2026051567724](https://openairdocs.org/sdr/IPXA2026051567724.md): Structure · corroded · Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, Structure
  > AFT 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
- [SDR IPXA2026050267681](https://openairdocs.org/sdr/IPXA2026050267681.md): Profile · corroded · Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT 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 ST
- [SDR IPXA2026051567636](https://openairdocs.org/sdr/IPXA2026051567636.md): Profile · corroded · Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT 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 PL
- [SDR IPXA2026051167251](https://openairdocs.org/sdr/IPXA2026051167251.md): Cover · broken · Apr 18, 2026 · N163UP · Airbus A300F4622R · Escape Slide
  > FWD 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.
- [SDR IPXA2026042968001](https://openairdocs.org/sdr/IPXA2026042968001.md): Bracket · cracked · Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR IPXA2026050170017](https://openairdocs.org/sdr/IPXA2026050170017.md): Web · cracked · Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026050267675](https://openairdocs.org/sdr/IPXA2026050267675.md): Crossbeam · corroded · Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, Structure
  > AFT 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.
- [SDR IPXA2026042968063](https://openairdocs.org/sdr/IPXA2026042968063.md): Bracket · cracked · Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO- FRAME 54 LT SIDEWALL BRACKET IS CRACKED. INSTALLED BRACKET AT FRAME 54 LH SIDEWALL, IAW SRM 51-40-21-001.
- [SDR IPXA2026042969269](https://openairdocs.org/sdr/IPXA2026042969269.md): Attach Bracket · broken · Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > LOWER 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.
- [SDR IPXA2026042870068](https://openairdocs.org/sdr/IPXA2026042870068.md): Profile · cracked · Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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 FAST
- [SDR IPXA2026042870092](https://openairdocs.org/sdr/IPXA2026042870092.md): Profile · cracked · Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026042067251](https://openairdocs.org/sdr/IPXA2026042067251.md): Cover · broken · Apr 18, 2026 · N163UP · Airbus A300F4622R · Escape Slide
  > FWD CREW DOOR HAS BROKEN SLIDE ARM/DISARM COVER APPROVED
- [SDR IPXA2026061056763](https://openairdocs.org/sdr/IPXA2026061056763.md): Splice Angle · gouged · Apr 17, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN 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.
- [SDR IPXA2026061056670](https://openairdocs.org/sdr/IPXA2026061056670.md): Fitting · gouged · Apr 17, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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. -.
- [SDR IPXA2025021186763](https://openairdocs.org/sdr/IPXA2025021186763.md): Bottle · low pressure · Feb 11, 2025 · N163UP · Airbus A300F4622R · Escape Slide
  > L1 DOOR SLIDE OF OF GREEN BAND. REMOVED AND REPLACED ESCAPE SLIDE IAW A300 AMM 25-61-21-0401.
- [SDR IPXA2025012423113](https://openairdocs.org/sdr/IPXA2025012423113.md): Bustle · unsecure · Jan 22, 2025 · N163UP · Airbus A300F4622R · Escape Slide
  > *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 25-61-21
- [SDR IPXA2024112699633](https://openairdocs.org/sdr/IPXA2024112699633.md): Warning Light · inoperative · Nov 26, 2024 · N163UP · Airbus A300F4622R · Door Warning System
  > THE 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 GOOD
- [SDR IPXA2023113066828](https://openairdocs.org/sdr/IPXA2023113066828.md): Flap · damaged · Nov 19, 2023 · N163UP · Airbus A300F4622R · Leading Edge Devices
  > *SUPPLEMENTAL SDR* L/H KRUGER FLAP SURROUND HAS DAMAGE STRUCTURE DAMAGE INSTALLED NEW UPPER SKIN RIBS & STRUCTURE REF SRM 51-40-21
- [SDR IPXA2023113072262](https://openairdocs.org/sdr/IPXA2023113072262.md): Slat · damaged · Nov 19, 2023 · N163UP · Airbus A300F4622R · Leading Edge Slat Control System
  > *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.
- [SDR IPXA2023112266828](https://openairdocs.org/sdr/IPXA2023112266828.md): Unknown · unknown · Nov 19, 2023 · N163UP · Airbus A300F4622R · Leading Edge Devices
  > *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 & 51-40-21
- [SDR IPXA2023112272262](https://openairdocs.org/sdr/IPXA2023112272262.md): Unknown · unknown · Nov 19, 2023 · N163UP · Airbus A300F4622R · Leading Edge Devices
  > *SDR FILED OPEN* LEFT WING I/B SLAT I/B EDGE DAMAGE
- [SDR IPXA2023113061044](https://openairdocs.org/sdr/IPXA2023113061044.md): Flap · damaged · Nov 18, 2023 · N163UP · Airbus A300F4622R · Leading Edge Devices
  > DURING 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 PIN
- [SDR IPXA2023112061044](https://openairdocs.org/sdr/IPXA2023112061044.md): Unknown · unknown · Nov 18, 2023 · N163UP · Airbus A300F4622R · Leading Edge Devices
  > *SDR FILED OPEN* DURING WALK AROUND FOUND EXTENSIVE DAMAGE TO LEFT WING KRUEGER FLAP. SEE TASK INFO FOR PHOTOS
- [SDR IPXA2023111500285](https://openairdocs.org/sdr/IPXA2023111500285.md): Unknown · unknown · Nov 15, 2023 · N163UP · Airbus A300F4622R · Landing Gear Retraction/Extension System
  > ATB 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.
- [SDR IPXA2023100950591](https://openairdocs.org/sdr/IPXA2023100950591.md): Battery · no test · Oct 2, 2023 · N163UP · Airbus A300F4622R · Emergency Lighting
  > *** SUPPLEMENTAL SDR *** FAULT: CABIN EMERGENCY LIGHTIING SYSTEM FAILS OPS CHECK REVIEWED
- [SDR IPXA2023100650591](https://openairdocs.org/sdr/IPXA2023100650591.md): Unknown · unknown · Oct 2, 2023 · N163UP · Airbus A300F4622R · Emergency Lighting
  > *** 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 GOOD
- [SDR IPXA2023100926600](https://openairdocs.org/sdr/IPXA2023100926600.md): Rudder · unknown · Sep 30, 2023 · N163UP · Airbus A300F4622R · Rudder Structure
  > *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 INSPECTIONS
- [SDR IPXA2023100710211](https://openairdocs.org/sdr/IPXA2023100710211.md): Adapter · corroded · Sep 30, 2023 · N163UP · Airbus A300F4622R · Fuselage Main, Structure
  > FAULT-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. REVIEWED
- [SDR IPXA2023092894287](https://openairdocs.org/sdr/IPXA2023092894287.md): Rudder · delaminated · Sep 21, 2023 · N163UP · Airbus A300F4622R · Rudder Structure
  > INSPECTION 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.
- [SDR IPXA2023091894189](https://openairdocs.org/sdr/IPXA2023091894189.md): Bracket · cracked · Sep 18, 2023 · N163UP · Airbus A300F4622R · Engine Mount Section
  > INSPECTION TYPE:1CENG 1 PYLON FWD BRACKET UNDERNEATH BUTTERFLY PANEL HAS A CRACKREMOVED, FABRICATED AND INSTALLED IAW SRM 51-40-21
- [SDR IPXA2023091894188](https://openairdocs.org/sdr/IPXA2023091894188.md): Adapter · cracked · Sep 18, 2023 · N163UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:1CCRACK ON SEAT TRACK AROUND FLOOR PNL 241TK BETWEEN FT 37 AND FR 38REMOVED AND REPLACED IAW SRM 51-40-21
- [SDR IPXA2023091894187](https://openairdocs.org/sdr/IPXA2023091894187.md): Bracket · cracked · Sep 18, 2023 · N163UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:1CBRACKET BROKEN ON LH SIDEWALL BELOW FLOOR BETWEEN FR 39 AND FR 40REMOVED AND REPLACED IAW SRM 51-40-21
- [SDR IPXA2023091894186](https://openairdocs.org/sdr/IPXA2023091894186.md): Plate · cracked · Sep 18, 2023 · N163UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > INSPECTION TYPE:1CRH PYLON ACCESS PANEL 424CR UPPER FWD CORNER SUPPORT PLATE HAS CRACKREMOVED, FABRICATED AND REPLACED IAW SRM 15-40-21
- [SDR IPXA2023091894185](https://openairdocs.org/sdr/IPXA2023091894185.md): Crossbeam · bent · Sep 18, 2023 · N163UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:1CCROSSBEAM P/N A5381337900040 AT FRAM 51 BETWEEN Y450 TO Y953 IS BENTREMOVED AND REPLACED IAW SRM 51-40-21
- [SDR IPXA2023091894184](https://openairdocs.org/sdr/IPXA2023091894184.md): Bracket · cracked · Sep 18, 2023 · N163UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:1CAFT CARGO COMPARTMENT FWD BULKHEAD AT FRAM 54 HAS A CRACKED SUPPORT BRACKETREMOVED AND REPLACED IAW SRM 51-40-21

Next page: https://openairdocs.org/aircraft/N163UP/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 = 'N163UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N163UP/reports

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