# Service difficulty reports: N127UP

A list on [N127UP](https://openairdocs.org/aircraft/N127UP.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 · 194 reports

- [SDR IPXA2026101512243](https://openairdocs.org/sdr/IPXA2026101512243.md): Skin · dented · Oct 6, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE, BTWN FR 51 TO 52, LH SIDE, NEXT TO MLG DOOR CUTOUT, EXTERNAL SURFACE, SKIN HAS A DENT W/ GOUGE. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-98862-REQ1 AND STE PNA EA 300-5315-27-A4660, REV-.
- [SDR IPXA2026102161735](https://openairdocs.org/sdr/IPXA2026102161735.md): Fitting · out of limits · Oct 2, 2026 · N127UP · Airbus A300F4622R · Wing Main, Frame Structure
  > HOLE N HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; FWD FITTING.3780", SPLICE.2840, AFT FITTING.3780". ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.
- [SDR IPXA2026102161645](https://openairdocs.org/sdr/IPXA2026102161645.md): Fitting · out of limits · Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, Structure
  > HOLE M HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; FWD FITTING.4530", SPLICE.3070, AFT FITTING.4580". ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.
- [SDR IPXA2026102161581](https://openairdocs.org/sdr/IPXA2026102161581.md): Fitting · out of limits · Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, Structure
  > HOLE L HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; FWD FITTING.3830", SPLICE.2810, AFT FITTING.3840". ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.
- [SDR IPXA2026102161504](https://openairdocs.org/sdr/IPXA2026102161504.md): Fitting · out of limits · Oct 2, 2026 · N127UP · Airbus A300F4622R · Fuselage Main, Structure
  > HOLE H HOLE SIZES MEASURES DIFFERENT FROM THE EO-90930-REQ2 REV 4; SPLICE.3480, AFT FITTING.4050".ACCOMPLISHED THE REPAIR PER EO-98948-REQ1 AND EA 300-5710-27-A4658, REV. _.
- [SDR IPXA2026082400675](https://openairdocs.org/sdr/IPXA2026082400675.md): Test Unit · faulted · Aug 21, 2026 · N127UP · Airbus A300F4622R · Doors
  > ASPSU TEST UNIT FAULT LIGHT ILLUMINATED WHEN BITE TESTED. REPLACED ASPSU IAW AMM 52-73-18/401. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.
- [SDR IPXA2026081438198](https://openairdocs.org/sdr/IPXA2026081438198.md): Pump · low pressure · Aug 12, 2026 · N127UP · Airbus A300F4622R · Hydraulic Pump (Electric/Engine), Main
  > EMERGENCY DECLARED. GREEN ENG HYD PUMP 2 LO PRESSURE FOLLOWED ECAM,SELECTED OFF, RESULTED IN LOSS OF GREEN HYD FLUID RESULTED IN GREEN HYD FALURE. NUMBER 2 GREEN ENGINE DRIVEN HYDRAULIC PUMP REPLACEMENT COMPLETE IAW AMM 29-11-31. OPS CHECK, LEAK CHECKS GO
- [SDR IPXA2026081238198](https://openairdocs.org/sdr/IPXA2026081238198.md): Pump · low pressure · Aug 12, 2026 · N127UP · Airbus A300F4622R · Hydraulic Pump (Electric/Engine), Main
  > EMERGENCY DECLARED, GREEN ENG HYD PUMP 2 LOW PRESSURE FOLLOWED ECAM,SELECTED OFF, RESULTED IN LOSS OF GREEN HYD FLUID RESULTED IN GREEN HYD FALURE.
- [SDR IPXA2026062307338](https://openairdocs.org/sdr/IPXA2026062307338.md): Door · binding · Jun 23, 2026 · N127UP · Airbus A300F4622R · Passenger/Crew Doors
  > MAIN CABIN DOOR HARD TO CLOSE. FLIGHT CREW NOTED TO MX UPON ARRIVAL THAT THE L1 DOOR FUNCTIONS NORMALLY. OPENED & CLOSED L1 DOOR NUMEROUS TIMES PER A300 AMM 52-10-00. NO ABNORMAL RESISTANCE NOTED. ARMED & DISARMED SLIDE MULTIPLE TIMES PER A300 AMM 52-73-00. NO
- [SDR IPXA2026061720384](https://openairdocs.org/sdr/IPXA2026061720384.md): Computer · faulted · Jun 17, 2026 · N127UP · Airbus A300F4622R · Landing Gear System
  > DURING GEAR EXTENSION ECAM FWS-CRT AMBER CAUTION NOT AVAIL, ENG 1, LG WHEEL, ATS FUEL AFT TRANSFER NA, LEFT BRAKES KEEP SHOOTING UP TO ABOVE 300 C. A/C NORMAL WITH HANDLING SO LANDED. AIRCRAFT RETURNED TO FULL CAT STATUS.
- [SDR IPXA2025072931607](https://openairdocs.org/sdr/IPXA2025072931607.md): Slide · ruptured · Jul 26, 2025 · N127UP · Airbus A300F4622R · Escape Slide
  > WHILE WORKING D/D MEL-L1 DOOR SLIDE, FOUND DOOR DAMPER PRESS LOW, AND DIAPHRAGM RUPTURED. VERIFIED ALL LOCKOUT PINS REMOVED FROM DOOR DAMPNER AND ALL OPS CHECKS GOOD IAW AMM 52-10-14
- [SDR IPXA2025072252379](https://openairdocs.org/sdr/IPXA2025072252379.md): Arming Lever · faulted · Jul 22, 2025 · N127UP · Airbus A300F4622R · Passenger/Crew Doors
  > UNABLE TO ARM DOOR. DMP C/W.
- [SDR IPXA2025070105651](https://openairdocs.org/sdr/IPXA2025070105651.md): Slide · no discrepancy · Jul 1, 2025 · N127UP · Airbus A300F4622R · Escape Slide
  > UNABLE TO ARM SLIDE AFTER CLOSING DOOR ADJUSTED GIRT BAR ASSEMBLY REF AMM 25-61-21. DOOR OPERATES CORRECTLY AT THIS TIME. DEFERRAL CLEARED PLACARDS REMOVED.
- [SDR IPXA2025052074149](https://openairdocs.org/sdr/IPXA2025052074149.md): Fitting · dirty · May 20, 2025 · N127UP · Airbus A300F4622R · Emergency Equipment
  > PILOT REPORTS L1 DOOR SLIDE WOULD NOT ARM AT DEPARTURE. INSPECTED DOOR, CLEANED GIRT BAR FLOOR ATTACHMENT POINTS, OPS CHECK GOOD W/ SLIDE INDICATION ON ECAM. AMM 52-10-11
- [SDR IPXA2025021322729](https://openairdocs.org/sdr/IPXA2025021322729.md): Bottle · low pressure · Feb 13, 2025 · N127UP · Airbus A300F4622R · Escape Slide
  > L1 DOOR SLIDE LOW PRESSURE. REVERSED DMP 52-11-01-2-3, REPLACED DOOR SLIDE ASSEMBLY IAW AMM 25-61-21-401 DEFERRAL CLEARED PLACARD REMOVED. ACCOMPLISHED RII STEPS PER GMM 04-02.
- [SDR IPXA2024072637979](https://openairdocs.org/sdr/IPXA2024072637979.md): Rib · cracked · Jun 13, 2024 · N127UP · Airbus A300F4622R · Trailing Edge Flaps
  > LH CENTER FLAP CRACK RIB 25 ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -. REVIEWED
- [SDR IPXA2024061737979](https://openairdocs.org/sdr/IPXA2024061737979.md): Rib · cracked · Jun 13, 2024 · N127UP · Airbus A300F4622R · Trailing Edge Flaps
  > LEFTCENTER FLAP CRACKED RIB 25.
- [SDR IPXA2024072376565](https://openairdocs.org/sdr/IPXA2024072376565.md): Fitting · cracked · Jun 3, 2024 · N127UP · Airbus A300F4622R · Passenger/Crew Doors
  > *SUPPLEMENTAL SDR* FAULT: FWD CREW DOOR AFT LOWER FITTING HAS A CRACK REMOVED AND REPLACED LOWER FITTING CRACK FWD CREW DOOR IAW AMM 52-10-31/401 P/N A5211038420401 BATCH 0004293554. REVIEWED
- [SDR IPXA2024060476565](https://openairdocs.org/sdr/IPXA2024060476565.md): Stop Fitting · cracked · Jun 3, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, Structure
  > FWD CREW DOOR AFT LOWER FITTING STOP CRACKED. OPEN
- [SDR IPXA2024062873248](https://openairdocs.org/sdr/IPXA2024062873248.md): Bulkhead · damaged · May 27, 2024 · N127UP · Airbus A300F4622R · APU Cowling/Containment
  > 8 HOLES ON REAR PRESSURE BULKHEAD APU BLEED AIR CUT OUT HAVE DAMAGE. CLEANED 3 EA HOLES IAW SRM 51-40-44 ON APU BLEED AIR CUT OUT. ROTO PERFORMED ON 1 HOLE AT BOTTOM OF THE APU BLEED AIR CUTOUT. NO INDICATIONS FOUND. IAW NTM 51-10-01.
- [SDR IPXA2024062345856](https://openairdocs.org/sdr/IPXA2024062345856.md): Frame · cracked · May 24, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, Frame
  > DAMAGE FOUND IN TOP HOLE, & CRACK FOUND IN MIDDLE HOLE ON FR40 LH UPPER TENSION BOLTS. CLEANED HOLES TOP HOLE AND MIDDLE HOLE ON FR 40 UPPER TENSION BOLT LH SIDE I.A.W. A300-600 SRM 51-73-10.
- [SDR IPXA2024072208143](https://openairdocs.org/sdr/IPXA2024072208143.md): Frame · damaged · May 22, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, Frame
  > DAMAGE FOUND IN HOLES (A, B, C, D, E, F, P) ON FR47 RH HORIZONTAL JUNCTION. AREAS MARKED IN RED. ACCOMPLISHED THE REPAIR PER UPS EO: EO-90872-REQ1 AND VT MAE FINAL EA 300-5710-27-A3621 REV. -.
- [SDR IPXA2024061365489](https://openairdocs.org/sdr/IPXA2024061365489.md): Rib · cracked · May 20, 2024 · N127UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE R/H CENTER FLAP ASSY, HAS A CRACK (1EA) AT RIB LOCATION 26, AFT SIDE. INSTALLED DOUBLER. IAW A300-600 SRM 51-40-21 AND SRM 57-50-00 REVIEWED
- [SDR IPXA2024061336460](https://openairdocs.org/sdr/IPXA2024061336460.md): Structure · cracked · May 17, 2024 · N127UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE L/H CENTER FLAP ASSY, HAS MULTIPLE CRACKS (2EA) AT RIB LOCATION 27, AFT SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -. JOB COMPLETE. VERIFIED. REVIEWED
- [SDR IPXA2024061336422](https://openairdocs.org/sdr/IPXA2024061336422.md): Rib · cracked · May 17, 2024 · N127UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE L/H CENTER FLAP ASSY, HAS A CRACK (1EA) AT RIB LOCATION 26, AFT SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -. JOB COMPLETE. VERIFIED. REVIEWED
- [SDR IPXA2024061336403](https://openairdocs.org/sdr/IPXA2024061336403.md): Rib · cracked · May 17, 2024 · N127UP · Airbus A300F4622R · Trailing Edge Flaps
  > THE L/H CENTER FLAP ASSY, HAS A CRACK (1EA) AT RIB LOCATION 25, AFT SIDE. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -.
- [SDR IPXA2024062810799](https://openairdocs.org/sdr/IPXA2024062810799.md): Skin · damaged · May 16, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > MDC DOOR AFT MIDDLE FUSELAGE SKIN WITH DAMAGE REMOVED NEGLIGIBLE SURFACE DISCREPANCY BY HAND WITH SCOTCH BRITE THAT WAS NOTED IN PAINT SURFACE ONLY IAW SRM 51-73-11 AND NO MATERIAL LOSS WAS NOTED. OK TO TREAT AND PRIME. RESTORED SURFACE PROTECTION IAW SRM 51-2
- [SDR IPXA2024062860200](https://openairdocs.org/sdr/IPXA2024062860200.md): Hinge · damaged · May 14, 2024 · N127UP · Airbus A300F4622R · Fuselage, Door Hinge
  > DAMAGE FOUND IN HOLES ON MIDDLE HINGE. STEEL (14D) ALUMINIUM (12F, 13F, 15F). CLEANED HOLE (14D AND 15F) IAW SRM 51-73-10 AND REAMING HOLES (12F AND 13F) SIZE.281 IAW SRM 51-40-21. ROTO INSPECTION PERFORMED IAW NTM 51-10-01 PT 6. ALL HOLES ARE DEFECT FREE.
- [SDR IPXA2024062760200](https://openairdocs.org/sdr/IPXA2024062760200.md): Hinge · damaged · May 14, 2024 · N127UP · Airbus A300F4622R · Fuselage Structure (General)
  > DAMAGE FOUND IN HOLES ON MIDDLE HINGE. STEEL (14D) ALUMINIUM (12F, 13F, 15F). OPEN
- [SDR IPXA2024062742586](https://openairdocs.org/sdr/IPXA2024062742586.md): Web · cracked · May 13, 2024 · N127UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AGING ACFT INSP.- FRAME WEB BETWEEN FRAME 86L AND 87L IN AFT ACCESORY COMPT. ARE BENT AND CRACKED. DOT AA025. INSTALLED FRAME WEB BETWEEN FRAME 86 & 87 LH STGR 34 IAW SRM 51-40-21 P/N:CR3213-5-02, BTCH:0004070310. APPLIED CIC AT FRAME WEB BETWEEN FR 86 & 87 LH
- [SDR IPXA2024070830033](https://openairdocs.org/sdr/IPXA2024070830033.md): Floorbeam · cracked · May 12, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > FAULT STR FUSELAGE RH SIDE BETWEEN (Y= -450 TO Y= -953) FR 50 CROOSBEAM CROKED DOT 108-120. INSTALLED NEW CROSSBEAN IAW SRM 51-40-21 AND APPLIED CIC IAW EO NO:M-5100-2780-L. REVIEWED
- [SDR IPXA2024070830019](https://openairdocs.org/sdr/IPXA2024070830019.md): Floorbeam · cracked · May 12, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > FAULT STR FUSELAGE RH SIDE BETWEEN (Y= -450 TO Y= -953 FR 51 CROOSBEAM BROKEN DOT 108-119. VERIFIED CROSSBEAM REPLACEMENT AND INSTALLATION PER IAW A300-600 SRM 51-40-21. REVIEWED
- [SDR IPXA2024072425041](https://openairdocs.org/sdr/IPXA2024072425041.md): Splice · cracked · May 11, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, Structure
  > DAMAGE FOUND IN HOLES (A, E, L, M, AND N) CRACK/DAMAGE FOUND IN HOLE (H) ON FR47 LH SPLICE FITTING. AREAS MARKED IN RED. ACCOMPLISHED THE REPAIR PER EO-90930-REQ1 AND EA 300-5315-27-A3616 REV. -. JOB COMPLETE. REVIEWED
- [SDR IPXA2024062923528](https://openairdocs.org/sdr/IPXA2024062923528.md): Access Panel · cracked · May 11, 2024 · N127UP · Airbus A300F4622R · Wing, Plate/Skin
  > L/H WING ACCESS PANEL 577DT HAS A COMPOSITE CRACK ON THE INNER SIDE. DOT 110/01. REPAIRED CRACKED AREA IAW AMM A300 53-15-63/801 PARA C.2.A-F. 08-010 (EA 934) BATCH 4271892.
- [SDR IPXA2024062707930](https://openairdocs.org/sdr/IPXA2024062707930.md): Structure · cracked · May 10, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, Structure
  > CRACKS/DAMAGE FOUND IN ALL 3 HOLES ON FR40 RH UPPER TENSION BOLTS. TOP HOLE (3 SMALL CRACKS IN 1ST LAYER) MIDDLE HOLE (PITTED CORROSION AT START OF HOLE) BOTTOM HOLE (CRACK AT START OF HOLE). ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-90914-REQ1 AND VT-MAE EA 3
- [SDR IPXA2024062789486](https://openairdocs.org/sdr/IPXA2024062789486.md): Floor Support · cracked · May 9, 2024 · N127UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO FR 54 L/H O/B HAS A CRACKED FLOOR SUPPORT BRACKET. INSTALLED FLOOR SUPPORT FR 54/LH IAW 51-40-21 A300-600. REVIEWED
- [SDR IPXA2024062788979](https://openairdocs.org/sdr/IPXA2024062788979.md): Floor Support · cracked · May 9, 2024 · N127UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT R/H MIDDLE AT FR 54 IS CRACKED. APPLIED TOP COAT ON FLOOR SUPPORT I.A.W. SRM 51-75-10, AND INSTALLED FLOOR SUPPORT I.A.W. SRM 51-40-20. REVIEWED
- [SDR IPXA2024072669041](https://openairdocs.org/sdr/IPXA2024072669041.md): Seal · torn · May 8, 2024 · N127UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW ENTRY DOOR SEAL AFT MIDDLE AREA HAS TORN COVERING IN SEVERAL PLACES DOT47-03 REMOVED AND REPLACED MAIN ENTRY DOOR SEAL IAW AMM 52-10-18/401 T95749. P/N F521813562000. BATCH 0004290380. REVIEWED
- [SDR IPXA2024050969041](https://openairdocs.org/sdr/IPXA2024050969041.md): Seal · torn · May 8, 2024 · N127UP · Airbus A300F4622R · Passenger/Crew Doors
  > **SDR FILED OPEN**FAULT CREW ENTRY DOOR SEAL AFT MIDDLE AREA HAS TORN COVERING IN SEVERAL PLACES DOT47-03
- [SDR IPXA2024070855351](https://openairdocs.org/sdr/IPXA2024070855351.md): Nose Cowl · cracked · May 7, 2024 · N127UP · Airbus A300F4622R · Turbine Engine Air Inlet Section
  > ENGINE #2 NOSE COWL FRON SIDE, LIP WITH CRACK IN POSITION 10 HRS, APROX 0,5 INCH DOT 108-110. INSTALLED DOUBLER AND FILLER ON AREA OF #2 NOSE COWL FRONT SIDE, I.A.W. PWA SRM 54-10-00, FIGURE 204.
- [SDR IPXA2024072335114](https://openairdocs.org/sdr/IPXA2024072335114.md): Bulkhead · corroded · May 6, 2024 · N127UP · Airbus A300F4622R · Fuselage Main, Bulkhead
  > FAULT FWD CARGO COMPT AFT BULKHEAD FR39 UPPER TOP AREAS HAS 3 AREAS OF EXFOLIATING CORROSION MARKED WITH RED TAPE DOT 47-01 ACCOMPLISHED PERMANENT REPAIR PER EO-90839-REQ1 AND EA 300-5315-27-A3601 REV. -. JOB COMPLETE. REVIEWED
- [SDR IPXA2023071793669](https://openairdocs.org/sdr/IPXA2023071793669.md): Apu · inoperative · Jul 14, 2023 · N127UP · Airbus A300F4622R · Airborne Auxiliary Power Unit (APU) System
  > INSPECTION TYPE:NA*DIVERSION* DURING CRUISE APU AUTO SHUTDOWN APU OIL QTY BELOW MIN INDICATED. DIVERT TO BIL DUE ENG 2 B SYSTEM IGN DIVERT 1205Z AND APU REQ PER MELFOUND LOOSE B NUT ON LINE FOM OIL PUMP OUTLET. TIGHTENED PER AMM 49-90-00. LINE NUT OPS CHECKED
- [SDR IPXA2023011289822](https://openairdocs.org/sdr/IPXA2023011289822.md): Lamp · inoperative · Jan 11, 2023 · N127UP · Airbus A300F4622R · Emergency Lighting
  > EMERGENCY "EXIT" SIGN HAS 3 EA LAMPS INOPRELAMPED & OPS NORMAL W/REF TO MM 33-51-00 PB 0501
- [SDR IPXA2023010389546](https://openairdocs.org/sdr/IPXA2023010389546.md): Brake Assy · malfunctioned · Dec 27, 2022 · N127UP · Airbus A300F4622R · Landing Gear Brake System
  > BTB: 1250 PULSATING BRAKES AT VARIOUS TAXI SPEED. BRAKES HIGHER THAN NORMAL TEMPPILOTS NOTED BRAKES 5 AND 6 TEMP HIGH. INSPECTED BRAKES 5 AND 6. NO DISCREPANCIES NOTED WHEN JACKED AND OPS CHECKED FOIUND 040 FAULT ON BSCU. REMOVED AND REPLACED BSCU IAW A300 AMM
- [SDR IPXA2022110487837](https://openairdocs.org/sdr/IPXA2022110487837.md): Warning Light · inoperative · Nov 3, 2022 · N127UP · Airbus A300* · Door Warning System
  > INSPECTION TYPE:NA*SUPPLEMENTAL SDR* EVACUATION SLIDE WARNING SYSTEM LIGHT INOP. DEFERRED WARNING LIGHT IAW MEL 52-73-01-1. PLACARD INSTALLED. NIL DMP. C/N M794640 ASSIGNED.R/R ASPSU OUTBD BATTERY & INBD BATTERY REF AMM 52-73-11 PB 0401. SYSTEM OPS NORMAL. THI
- [SDR IPXA2021112076176](https://openairdocs.org/sdr/IPXA2021112076176.md): None · none · Nov 20, 2021 · N127UP · Airbus A300F4622R · Emergency Exits
  > INSPECTION TYPE:NACANNOT PREFLIGHT THE ESCAPE SLIDE, PRESSURE GAUGE IS NOT VISIBLE IN THE SLIDE PACK HOUSING WINDOW.R/R DOOR SLIDE PER MM 25-61-21-0401. THIS CLEARS M763622.
- [SDR IPXA2021110475596](https://openairdocs.org/sdr/IPXA2021110475596.md): None · none · Nov 2, 2021 · N127UP · Airbus A300F4622R · Passenger/Crew Doors
  > INSPECTION TYPE:NA** SUPPLEMENTAL SDR ** THE DOOR SLIDE DOES NOT SHOW ARMED ON ECAM WITH DOOR CLOSED AND SLIDE IN ARMED POSITION. DEFERED PER MEL 52-30-04, PLACARD INSTALLED.FOUND CONNECTOR 13WN-A UNPLUGGED. RECONNECTED PLUG OPS CHECK PER 52-73-00-0001 PARA8.
- [SDR IPXA2021102975450](https://openairdocs.org/sdr/IPXA2021102975450.md): Frame · cracked · Oct 29, 2021 · N127UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:SEGFUSELAGE FRAME FOOT FITTING LH SIDE FRAME 44, IS CRACKED AT AREA 1.ACCOMPLISHED REPAIR PER APPENDIX J OF EO A300-5310-46789-G
- [SDR IPXA2021102975449](https://openairdocs.org/sdr/IPXA2021102975449.md): Frame · cracked · Oct 29, 2021 · N127UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:SEGFUSELAGE FRAME FOOTING AT LH SIDE FRAME 45, IS CRACKED AT AREA 1ACCOMPLISHED REPAIR PER APPENDIX J OF EO. A300-5310-46789-G
- [SDR IPXA2021102975448](https://openairdocs.org/sdr/IPXA2021102975448.md): Frame · cracked · Oct 29, 2021 · N127UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:SEGFUSELAGE FRAME FOOT FITTING AT LH SIDE FRAME 46 IS CRACKED AT AREA 1.ACCOMPLISHED REPAIR PER APPENDIX K OF EO. A600-5310-46789-G.

Next page: https://openairdocs.org/aircraft/N127UP/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 = 'N127UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N127UP/reports

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