# Service difficulty reports: N164UP

A list on [N164UP](https://openairdocs.org/aircraft/N164UP.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 3 · 137 reports

- [SDR IPXA2026102145646](https://openairdocs.org/sdr/IPXA2026102145646.md): Lamp · inoperative · Oct 20, 2026 · N164UP · Airbus A300F4622R · Emergency Lighting
  > SMALL EMERGENCY LIGHT IN LAV NEAR MIRROR INOP IN LOW ALWAYS ON POSITION. FOUND ON PREFLIGHT. RELAMPED LIGHT IAW CMS 33-24-03. OPS CHKD NORMAL.
- [SDR IPXA2025072127726](https://openairdocs.org/sdr/IPXA2025072127726.md): Lens · broken · Jul 21, 2025 · N164UP · Airbus A300F4622R · Emergency Lighting
  > LAV COMPT EMER LIGHT LENS BROKEN INSTALLED NEW LIGHT LENS IAW AMM 33-51-21/401.
- [SDR IPXA2025011476124](https://openairdocs.org/sdr/IPXA2025011476124.md): Gust Lock · damaged · Jan 14, 2025 · N164UP · Airbus A300F4622R · Passenger/Crew Doors
  > GUST LOCK ON MAIN CABIN WILLL SPRING BACK TO UP POSITON DURING INSPECTION OF THE L1 DOOR GUST LOCK BUTTON FOUND PLASTIC DEBRIS STUCK, REMOVED DEBRIS AND PERFORMED THE OPERATIONAL CHECK OF THE L1 DOOR IAW AMM 52-10-00. NO DEFECTS NOTED, THIS CLEARS DEFERRAL, D
- [SDR IPXA2024091163490](https://openairdocs.org/sdr/IPXA2024091163490.md): Hinge · broken · Sep 6, 2024 · N164UP · Airbus A300F4622R · Fuselage, Door Hinge
  > **SUPPLEMENTAL SDR** FAULT: APG L-1 CREW DOOR LINER ARM HINGE IS BROKEN. INSTALLED PANELS IAW AMM 52-10-13/401. REVIEWED
- [SDR IPXA2024090963490](https://openairdocs.org/sdr/IPXA2024090963490.md): Hinge · broken · Sep 6, 2024 · N164UP · Airbus A300F4622R · Fuselage, Door Hinge
  > L1 CREW DOOR LINER ARM HINGE IS BROKEN.
- [SDR IPXA22512](https://openairdocs.org/sdr/IPXA22512.md): Wire · damaged · Sep 4, 2024 · N164UP · Airbus A300F4622R · Light System Wiring
  > EMERGENCY LIGHTS TEST FAILS, LIGHTS STAY ACTIVATED WHEN TEST IS PREFORMED AT L1 DOOR, THEY DO NOT EXTINGUISH UNTIL PULLING 22VU E28 CB.PERFORMED CONTINUITY CHECK IAW A300 AWM 33-51-03 BETWEEN "TEST EMER" PUSH BUTTON SWITCH 25WL AND 5801VC CONNECTOR LIGHTING CO
- [SDR IPXA2024091723722](https://openairdocs.org/sdr/IPXA2024091723722.md): Warning Buzzer · inoperative · Sep 4, 2024 · N164UP · Airbus A300F4622R · Door Warning System
  > L1 DOOR BUZZER HORN & WARNING LIGHT INOP. PERF T/S IAW AWM 52-73-01 CKD POWER & GROUND ON 6035VT.CK GOOD. CONT CK BETWEEN 6035VT & 11WN BUZZER WARN.CONT CK BETWEEN 6035VT & 7WN IND-WARN CHECK GOOD. IAW AWM 52-73-01 AND ESPM 20-52-21-11. PERFORMED OPS. CHECK GO
- [SDR IPXA2024090522512](https://openairdocs.org/sdr/IPXA2024090522512.md): Light · no test · Sep 4, 2024 · N164UP · Airbus A300F4622R · Emergency Lighting
  > EMERGENCY LIGHTS TEST FAILS, LIGHTS STAY ACTIVATED WHEN TEST IS PREFORMED AT L1 DOOR, THEY DO NOT EXTINGUISH UNTIL PULLING 22VU E28 CB. APPROVED. LATE FIND.
- [SDR IPXA2024090523722](https://openairdocs.org/sdr/IPXA2024090523722.md): Warning Buzzer · inoperative · Sep 4, 2024 · N164UP · Airbus A300F4622R · Door Warning System
  > L1 DOOR BUZZER HORN AND WARNING LIGHT INOP APPROVED.
- [SDR IPXA2024090690022](https://openairdocs.org/sdr/IPXA2024090690022.md): Access Panel · corroded · Aug 4, 2024 · N164UP · Airbus A300F4622R · Fuselage Main, Structure
  > WHEEL WELL, FRAME ACCESS PANEL 148ZC CORRODED. DOT 28-97. RO-28. INSTALLED PANEL ASSY P/N: A2551030700701, BATCH: 0004319687, IAW SRM 51-40-21 AT ZONE 100, WHEEL WELL RH SIDE. USED HARDWARE: NSA55184-1 (WASHER RETAINING), NSA55182-1B (GROMMET), NSA55181-22 (ST
- [SDR IPXA2024090677035](https://openairdocs.org/sdr/IPXA2024090677035.md): Rib · cracked · Aug 3, 2024 · N164UP · Airbus A300F4622R · Wing, Rib/Bulkhead
  > LH WING FIXED L/E STRUCTURE HAS CRACKED RIB JUST O/B OF KRUGER FLAP NEAR STA. 142. DOT 142-010. INSTALLED RIB P/N: A572419920200 BATCH: 4282208 WITH RIVET P/N: MS20470AD5-6 BATCH: 4139271, RIVET P/N: MS20470AD4-4 BATCH: 3997710, CHERRY RIVET P/N: CR3213-5-04 B
- [SDR IPXA2024082266971](https://openairdocs.org/sdr/IPXA2024082266971.md): Skin · gouged · Aug 2, 2024 · N164UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > CREW DOOR CUTOUT, AFT MID AREA WITH GOUGE. GIVEN OK TO RESTORE PROTECTIVE COATINGS. RESTORED PROTECTIVE COATING PER SRM 51-21-10.
- [SDR IPXA2024082267429](https://openairdocs.org/sdr/IPXA2024082267429.md): Door · scratched · Aug 2, 2024 · N164UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, UPPER INTERNAL SURFACE WITH SCRATCHES. DOT 73-049. (MOYA-73). PRIMED AND PAINTED AT Z831, CREW DOOR UPPER INTERNAL SURFACE IAW SRM 51-21-10.
- [SDR IPXA2024082267447](https://openairdocs.org/sdr/IPXA2024082267447.md): Door Frame · scratched · Aug 2, 2024 · N164UP · Airbus A300F4622R · Fuselage Main, Structure
  > CREW DOOR FRAME, UPPER EXTERNAL SURFACE WITH SCRATCHES. PRIMED & PAINTED AT Z831, CREW DOOR FRAME, UPPER EXTERNAL SURFACE. IAW 51-21-10 USING 4OZ PRIMER 02-013-8, BATCH # 4263188 AND WHITE PAINT PG6-W2K4Q, BATCH #415963, CUP #02-012-176.
- [SDR IPXA2024081367429](https://openairdocs.org/sdr/IPXA2024081367429.md): Door Frame · damaged · Aug 2, 2024 · N164UP · Airbus A300F4622R · Fuselage Main, Structure
  > **SDR FILED OPEN**FAULT - STR - Z831 - CREW DOOR, UPPER INTERNAL SURFACE WITH SCRATCHES. DOT 73-049. (MOYA-73) APPROVED.
- [SDR IPXA2024081367447](https://openairdocs.org/sdr/IPXA2024081367447.md): Door Frame · damaged · Aug 2, 2024 · N164UP · Airbus A300F4622R · Fuselage Main, Structure
  > **SDR FILED OPEN**FAULT - STR - Z831 - CREW DOOR FRAME, UPPER EXTERNAL SURFACE WITH SCRATCHES. DOT 73-050 (MOYA-73) APPROVED.
- [SDR IPXA2024080566971](https://openairdocs.org/sdr/IPXA2024080566971.md): Door Frame · gouged · Aug 2, 2024 · N164UP · Airbus A300F4622R · Fuselage Main, Structure
  > CREW DOOR CUTOUT, AFT MID AREA WITH GOUGE. DOT 73-045 (MOYA-73) APPROVED.
- [SDR IPXA2024090918006](https://openairdocs.org/sdr/IPXA2024090918006.md): Seat Track · corroded · Jul 31, 2024 · N164UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MCD SEAT TRACK Y450 AT FR 75 SHOWS EVIDENCE OF CORROSION. 72-024. INSTALLED SEAT TRACK AT MCD Y450 FR80 IAW A300-600 SRM 53-10-16 P/N HL18PB8-5 BATCH 0003725375 P/N HL70-8 BATCH 0004286662 P/N NAS 1097DD6-10 BATCH 0004244840.
- [SDR IPXA2024091273020](https://openairdocs.org/sdr/IPXA2024091273020.md): Intercostal · bent · Jul 29, 2024 · N164UP · Airbus A300F4622R · Fuselage Main, Bulkhead
  > FAULT: STR-Z30 THS BAY AFT PRESSURE BULKHEAD BETWEEN FR86 AND FR87 R/H SIDE, INTERCOSTAL IS BENT. MB-60-029. INSTALLED INTERCOSTAL RH BETWEEN FR86 AND FR87 IAW A300-600 SRM 51-40-21 RIVETS PN: MS20470AD5-5, BATCH: 0004301662 AND PN: MS20470AD4-6 BATCH: 0004304
- [SDR IPXA2024091269244](https://openairdocs.org/sdr/IPXA2024091269244.md): Static Wick · corroded · Jul 29, 2024 · N164UP · Airbus A300F4622R · Wing Main, Frame Structure
  > FAULT STR Z600 R/WING TIP WINGLET, STATIC WICK BASES (2EA) ARE CORRODED. 72-012 INSTALLED WING TIP WINGLET R/H SIDE(2EA) STATIC WICK BASES. IAW SRM 51-40-21. REVIEWED
- [SDR IPXA2024091069202](https://openairdocs.org/sdr/IPXA2024091069202.md): Doubler · corroded · Jul 29, 2024 · N164UP · Airbus A300F4622R · Wing Main, Frame Structure
  > FAULT STR Z600 R/WING TIP, UPPER SURFACE STATIC WICK BASE IS CORRODED. 72-011 INSTALLED FILLER PLATE, DOUBLER AND STATIC WICK BASE AT R/H WING TIP, UPPER SURFACE I.A.W. A300-600 S.R.M. 57-30-11, FIGURE 214 (SHEET 4) AND S.R.M. 51-40-21.
- [SDR IPXA2024082670943](https://openairdocs.org/sdr/IPXA2024082670943.md): Doubler · corroded · Jul 29, 2024 · N164UP · Airbus A300F4622R · Wing Structure
  > R/WING OUT BOARD FLAP, STATIC WICK BASE IS CORRODED. 72-013. ACCOMPLISHED WORK PER EO: EO-91267-REQ 1 AND VTMAE EA 300-5750-27-A3672 REV.-.
- [SDR IPXA2023031691890](https://openairdocs.org/sdr/IPXA2023031691890.md): Door · inoperative · Mar 16, 2023 · N164UP · Airbus A300F4622R · Passenger/Crew Doors
  > AFT CLS CONTROL PANEL DOOR (152JR) SHOWS SIGNS OF DENT. PLACED CLS CONTROL PANEL DOOR 152JR ON DEFERRAL IAW A300 CDL 52-10 DOOR REMOVED PLACARD INSTALLED REFERENCE C805009REMOVED AND REPLACED DOOR IAW AMM 52-42-19.
- [SDR IPXA2022041481157](https://openairdocs.org/sdr/IPXA2022041481157.md): None · none · Apr 14, 2022 · N164UP · Airbus A300* · Passenger/Crew Doors
  > INSPECTION TYPE:NAPASSING FL330 WE GOT A LOUD AUDIBLE WHINE AROUND THE MAIN DOOR AREA. I THINK THERE IS AN AIR LEAK AROUND THE MAIN DOOR SEAL? CABIN PRESSURE WAS NORMAL. THE NOISE STOPPED AT FL230 IN THE DESCENT.INSPECTED AND CLEANED FWD MAIN DOOR SEAL IAW AMM
- [SDR IPXA2022040780949](https://openairdocs.org/sdr/IPXA2022040780949.md): None · cracked · Apr 7, 2022 · N164UP · Airbus A300* · Wing Main, Frame Structure
  > INSPECTION TYPE:SEGFRAME 40 LEFT HAND SIDE TOP, MIDDLE AND BOTTOM HOLES ALL HAVE REJECTABLE CRACK INDICATIONS.ACCOMPLISHED REPAIR PER SRM 57-10-24 TABLE 202 AND 206
- [SDR IPXA2022040780948](https://openairdocs.org/sdr/IPXA2022040780948.md): None · cracked · Apr 7, 2022 · N164UP · Airbus A300F4622R · Wing Main, Frame Structure
  > INSPECTION TYPE:SEGFRAME 40 RIGHT HAND SIDE TOP AND MIDDLE HOLES HAVE REJECTABLE CRACK INDICATIONS.ACCOMPLISHED REPAIR PER SRM 57-10-24 TABLE 202 AND 206
- [SDR IPXA2022040780942](https://openairdocs.org/sdr/IPXA2022040780942.md): None · cracked · Apr 7, 2022 · N164UP · Airbus A300F4622R · Wing, Plate/Skin
  > INSPECTION TYPE:SEGLEFT WING LOWER SKIN OVERSIZE HOLE REPAIR AT ACCESS PANEL 550QB BTWN RIB 26 AND 27 HAS A CRACL INDICATION AT 8'O CLOCK LOOKING UPACCOMPLISHED REPAIR PER FINAL EA 300-5720-A2886 AND FINAL UPS EO A300-5730-83369-A
- [SDR IPXA2022011978030](https://openairdocs.org/sdr/IPXA2022011978030.md): None · none · Jan 19, 2022 · N164UP · Airbus A300F4622R · Emergency Exits
  > INSPECTION TYPE:N/ASHORTLY AFTER LEVELING AT FL340 SLIDE WARNING BUZZER SOUNDED AND CONTINUED TO SOUND UNTIL THE SLIDE WAS DIS ARMEDFOUND TEST SWITCH FOR SLIDE WARNING PUSHED THROUGH DOOR LINING. INSTALLED NEW HARDWARE ON BUTTON PER AMM 52-73-14-0401,OPS CHECK
- [SDR IPXA2021100974771](https://openairdocs.org/sdr/IPXA2021100974771.md): None · none · Oct 9, 2021 · N164UP · Airbus A300F4622R · Passenger/Crew Doors
  > INSPECTION TYPE:N/AREF M759060: MAIN ENTRY DOOR/ SLIDES - ARMING LEVER WILL NOT ARM. REF: WAN 3441133 BH1231641UPON ARRIVAL NUMEROUS OPERATION IAW AMM 52-10-30-0501. NO DEFECT NOTED. NO DMI REVERSAL REQUIRED. M759060 CLEARED.
- [SDR IPXA2021101274866](https://openairdocs.org/sdr/IPXA2021101274866.md): None · none · Oct 7, 2021 · N164UP · Airbus A300F4622R · Passenger/Crew Doors
  > INSPECTION TYPE:N/ADOOR SLIDE WILL NOT ARM. DOOR OPS NORMALUPON ARRIVAL NUMBEOUS OPERATION IAW AMM 52-10-30-0501. NO DEFECTS NOTED. NO DMI REVERSAL REQUIRED. THIS CLEARS M759060
- [SDR IPXA2020090439829](https://openairdocs.org/sdr/IPXA2020090439829.md): Warning Light · inoperative · Sep 3, 2020 · N164UP · Airbus A300F4622R · Emergency Equipment
  > INSPECTION TYPE:N/A. SLIDE WARNING LIGHT DOES NOT ILLUMINATE WHEN TESTED. DEFERRED PER MEL 52-73-01-1, M718952 CREATED. NO DMP, STICKER INSTALLED. ACCOMPLISHED TEST OF WARNING LIGHT WRT AMM 52-73-11-0401. OPS CK GOOD, NO FAULTS NOTED. THIS CLEARS M718952,
- [SDR IPXA2020042954759](https://openairdocs.org/sdr/IPXA2020042954759.md): Fdu · faulty · Apr 28, 2020 · N164UP · Airbus A300F4622R · Fire Detection
  > INSPECTION TYPE:NA DIVERSION, SUPPLEMENTAL SDR. NO EMERG DECLARED, ENG 2 LOOP B IN FLT PERF ECAM INSTRUCT (ENG & WING A/I ON) THEN SEVERAL INTERMIT ENG 2 LOOP ECAM MSG & NO ENG FIRE DET MSG. SWAPPED FD CONT UNITS (11WD &12WD T/S - NO FAULTS ON LOOP B DURING E
- [SDR IPXA2019092247066](https://openairdocs.org/sdr/IPXA2019092247066.md): Actuator · faulty · Sep 22, 2019 · N164UP · Airbus A300F4622R · Aileron Control System
  > INSPECTION TYPE:12YR DURING ENG RUN GREEN SYS SERVO CONTROL JAM LIGHT ILLUMINATES WHEN #1 ENG STARTS. ICAC MSG "LEFT AILERON SERVO CONTROL JAM" REMOVED AND REPLACED LEFT AILERON CENTER SERVO ACTUATOR.
- [SDR IPXA2019092047017](https://openairdocs.org/sdr/IPXA2019092047017.md): Bushing · gouged · Sep 13, 2019 · N164UP · Airbus A300F4622R · Main Landing Gear Strut/Axle/Truck
  > INSPECTION TYPE:12YR RT MLG SHOCK ABSORBER P/N D22485020 S/N B483 ON O/B LEG AT BOGIE ALIGNMENT PIN I/B BUSHING IS GOUGED. REPAIRED GOUGED RT MLG SHOCK ABSORBER O/B LEG AT BOGIE ALIGNMENT PIN I/B BUSHING IAW EO A300-3210-73966-A SECTION 6A. (MINOR)
- [SDR IPXA2019091846973](https://openairdocs.org/sdr/IPXA2019091846973.md): Panel Support · damaged · Aug 30, 2019 · N164UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:12YR MAIN CABIN FLOOR PANEL SUPPORT PROFILE IS DAMAGED AT FR 80/82. REMOVED AND REPLACED DAMAGED MAIN CABIN FLOOR PANEL SUPPORT PROFILE AT FR 80/82 IAW SRM 51-40-21. (MINOR)
- [SDR IPXA2019091846969](https://openairdocs.org/sdr/IPXA2019091846969.md): Adapter · corroded · Aug 30, 2019 · N164UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:12YR MAIN CABIN CLS ADAPTER AT FR 20 AND RBL 75 IS CORRODED. REMOVED AND REPLACED CORRODED MAIN CABIN CLS ADAPTER AT FR 20 & RBL 75 IAW EA 300-5310-01-A7890 REV IR AND EO A300-5310-73885-A. (MAJOR)
- [SDR IPXA2019091446748](https://openairdocs.org/sdr/IPXA2019091446748.md): Floor Panel · damaged · Aug 30, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YR MAIN CABIN FLOOR PANEL 231NJ IS DAMAGED. FABRICATED REPLACEMENT DAMAGED MAIN CABIN FLOOR PANEL 231NJ IAW EO A300-5320-40552-B APPENDIX B. (MAJOR)
- [SDR IPXA2019091446747](https://openairdocs.org/sdr/IPXA2019091446747.md): Floor Panel · damaged · Aug 30, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YR MAIN CABIN FLOOR PANEL 231RG IS DAMAGED. FABRICATED REPLACEMENT DAMAGED MAIN CABIN FLOOR PANEL IAW EO A300-5320-40552-B APPENDIX B. (MAJOR)
- [SDR IPXA2019091446746](https://openairdocs.org/sdr/IPXA2019091446746.md): Floor Panel · damaged · Aug 30, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YR MAIN CABIN FLOOR PANEL 231SG IS DAMAGED. FABRICATED REPLACEMENT DAMAGED MAIN CABIN FLOOR PANEL 231SG IAW EO A300-5320-40552-B APPENDIX B. (MAJOR)
- [SDR IPXA2019091046588](https://openairdocs.org/sdr/IPXA2019091046588.md): Floor Panel · damaged · Aug 30, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YR MAIN CABIN FLOOR PANEL 232WG IS CRACKED. FABRICATED REPLACEMENT MAIN CABIN FLOOR PANEL 232WG IAW EO A300-5320-40552-B APPENDIX B. (MAJOR)
- [SDR IPXA2019091046586](https://openairdocs.org/sdr/IPXA2019091046586.md): Floor Panel · damaged · Aug 30, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YR MAIN CABIN FLOOR PANEL 231PJ IS DAMAGED. FABRICATED REPLACEMENT MAIN CABIN FLOOR PANEL 231PJ IAW EO A300-5320-40552-B APPENDIX B. (MAJOR)
- [SDR IPXA2019091046585](https://openairdocs.org/sdr/IPXA2019091046585.md): Floor Panel · damaged · Aug 30, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YR MAIN CABIN FLOOR PANEL 231TC IS DAMAGED. FABRICATED REPLACEMENT MAIN CABIN FLOOR PANEL 231TC IAW EO A300-5320-40552-B APPENDIX B. (MAJOR)
- [SDR IPXA2019090546381](https://openairdocs.org/sdr/IPXA2019090546381.md): Floor Panel · damaged · Aug 30, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YR MAIN CARGO COMPARTMENT FLOOR PANEL 231KJ IS DAMAGED. REPAIRED DAMAGED MAIN CARGO COMPARTMENT FLOOR PANEL 231KJ IAW EO A300-5320-42721-F APPENDIX A. (MAJOR)
- [SDR IPXA2019091446745](https://openairdocs.org/sdr/IPXA2019091446745.md): Floor Panel · damaged · Aug 29, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YR MAIN CABIN FLOOR PANEL 242BJ IS DAMAGED. FABRICATED REPLACEMENT DAMAGED MAIN CABIN FLOOR PANEL 242BJ IAW EO A300-5320-40552-B APPENDIX B. (MAJOR)
- [SDR IPXA2019091446744](https://openairdocs.org/sdr/IPXA2019091446744.md): Floor Panel · damaged · Aug 29, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YR MAIN CABIN FLOOR PANEL 242LJ LOWER SKIN IS DAMAGED. FABRICATED REPLACEMENT DAMAGED MAIN CABIN FLOOR PANEL 242LJ IAW EO A300-5320-40552-B APPENDIX B. (MAJOR)
- [SDR IPXA2019091446743](https://openairdocs.org/sdr/IPXA2019091446743.md): Floor Panel · damaged · Aug 29, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YR MAIN CABIN FLOOR PANEL 251DN LOWER SKIN IS DAMAGED. FABRICATED REPLACEMENT DAMAGED MAIN CABIN FLOOR PANEL 251DN IAW EO A300-5320-40552-B APPENDIX B. (MAJOR)
- [SDR IPXA2019091446742](https://openairdocs.org/sdr/IPXA2019091446742.md): Floor Panel · damaged · Aug 29, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YR MAIN CABIN FLOOR PANEL 251ZF LOWER SKIN IS DAMAGED. FABRICATED REPLACEMENT DAMAGED MAIN CABIN FLOOR PANEL 251ZF IAW EO A3005320-40552-B APPENDIX B. (MAJOR)
- [SDR IPXA2019091046584](https://openairdocs.org/sdr/IPXA2019091046584.md): Floor Panel · damaged · Aug 29, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YR MAIN CABIN FLOOR PANEL 241ZG IS DAMAGED. FABRICATED REPLACEMENT MAIN CABIN FLOOR PANEL 241ZG IAW EO A300-5320-40552-B APPENDIX B. (MAJOR)
- [SDR IPXA2019090646417](https://openairdocs.org/sdr/IPXA2019090646417.md): Floor Panel · cracked · Aug 29, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12Y MAIN CABIN FLOOR PANEL #261DM LOWER SKIN IS CRACKED. REMOVED, FABRICATED AND REPLACED FLOOR PANEL #261DM IAW EO A3005320-40552-B APPX. B. (MAJOR)
- [SDR IPXA2019092247071](https://openairdocs.org/sdr/IPXA2019092247071.md): Floor Panel · broken · Aug 28, 2019 · N164UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YR BULK CARGO COMPT FLOOR PANEL 162F HAS BROKEN CORNER. FABRICATED NEW FLOOR PANEL 162F PER EO - A300-5320-16407-E AND EO - A300-5320-73956-A. REF: FAB/PROCESS TRAVELER 70019668150001.

Next page: https://openairdocs.org/aircraft/N164UP/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 = 'N164UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N164UP/reports

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