# Service difficulty reports: N128UP

A list on [N128UP](https://openairdocs.org/aircraft/N128UP.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 5 · 214 reports

- [SDR IPXA2026020329998](https://openairdocs.org/sdr/IPXA2026020329998.md): Engine · bird ingestion · Jan 29, 2026 · N128UP · Airbus A300F4622R · Engine (Turbine/Turboprop)
  > SUSPECTED BIRD STRIKE DURING TAKE OFF. ENG #2 N1 VIBRATION REACHED 7.5 DURING CLIMBOUT. REPLACED FAN BLADES ON #2 ENG ACCOMPLISHED ENG RUN OPS CK NORMAL.
- [SDR IPXA2026013029998](https://openairdocs.org/sdr/IPXA2026013029998.md): Engine · vibration · Jan 29, 2026 · N128UP · Airbus A300F4622R · Engine (Turbine/Turboprop)
  > AIR TURN BACK. SUSPECTED BIRD STRIKE DURING TAKE OFF. ENG NR 2 N1 VIBRATION REACHED 7.5 DURING CLIMBOUT, C/W BIRDSTRIKE INSPECTION FOR ENGINE IAW AMM 05-51-19/0001 AND 72-00-00/601 PARA. 21. SEE T3F18E0086DCU AND T3F18E0086CV5 FOR FINDINGS.
- [SDR IPXA2025030910596](https://openairdocs.org/sdr/IPXA2025030910596.md): Limiter · faulted · Mar 1, 2025 · N128UP · Airbus A300F4622R · Leading Edge Slat Control System
  > *EMERGENCY DECLARED* SLAT SYS#1 &SLAT SYS #2 FAULT FLAPS OPERATED NORMAL LANDED 0 SLATS 40 FLAPS INSTALLED NEW TORQUE LIMITER PER AMM 27-84-12/401. OP€™S CHECK€™S GOOD.
- [SDR IPXA2024040117865](https://openairdocs.org/sdr/IPXA2024040117865.md): Shear Plate · cracked · Mar 16, 2024 · N128UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CRACK FOUND AT FWD SIDE OF FRAME 65 STR 42 ON INTERCOSTAL. INSTALLED SHEAR PLATE AT FWD SIDE OF FRAME 65 STR 42 IAW A300 SRM 51-40-21 PARAGRAPH 6 AND 7.
- [SDR IPXA2024040221180](https://openairdocs.org/sdr/IPXA2024040221180.md): Rib · cracked · Mar 12, 2024 · N128UP · Airbus A300F4622R · Wing, Rib/Bulkhead
  > ZONE 513 LT WING, FWD WING ROOT STA71/RIB2 LEADING EDGE RIB HAS A CRACK. INSTALLED REINFORCED ANGLE P/N: A5724199320200 AT FWD WING ROOT RH RIB 2. IAW SRM 51-40-21.
- [SDR IPXA2024041502252](https://openairdocs.org/sdr/IPXA2024041502252.md): Frame · damaged · Mar 11, 2024 · N128UP · Airbus A300F4622R · Fuselage Main, Frame
  > HOLES A & S HAVE DAMAGE INDICATIONS. HOLES B, F, AND P HAVE CRACK INDICATIONS ON FR 47 LH HORIZONTAL JUNCTION. COMPLIED WITH UPS EO: EO-90000-REQ1 AND VT MAE FINAL EA 300-5710-27-A3547 REV.
- [SDR IPXA2024041102178](https://openairdocs.org/sdr/IPXA2024041102178.md): Skin · cracked · Mar 11, 2024 · N128UP · Airbus A300F4622R · Horizontal Stabilizer, Plate/Skin
  > HOLES C AND E HAVE DAMAGE INDICATIONS. HOLE B HAS A CRACK AT 5'OCLOCK POSTION FACING FWD ON RH FR47 HORIZONTAL JUNCTION. REVIEWED
- [SDR IPXA2024040178433](https://openairdocs.org/sdr/IPXA2024040178433.md): Floor Panel · cracked · Mar 9, 2024 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCD FLOOR PANEL 251VJ IS DAMAGED. FABBED PANEL 251VJ FROM 5024N40000SS-G,BATCH #40552-B PER SREO -40552-REQ001 (APPX B).
- [SDR IPXA2024040177288](https://openairdocs.org/sdr/IPXA2024040177288.md): Floor Panel · cracked · Mar 9, 2024 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCD FLOOR PANEL 251ZF IS DAMAGED. FABBED PANEL 251ZF FROM 5024N400001SS-G, BATCH # 4055277, PER SREO-40552-REQ001 (APPX B).
- [SDR IPXA2024040177370](https://openairdocs.org/sdr/IPXA2024040177370.md): Floor Panel · cracked · Mar 9, 2024 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCD FLOOR PANEL 242KN IS DAMAGED. FABBED PANEL 242KN FROM 5024N400001SS-G, BATCH # 4055277, PER SREO-40552-REQ001 (APPX B).
- [SDR IPXA2024040169755](https://openairdocs.org/sdr/IPXA2024040169755.md): Floor Panel · cracked · Mar 8, 2024 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCD FLOOR PANEL 232LF IS DAMAGED FABBED PANEL 232LF FROM 5024N400001SS-G, BATCH # 4055277, PER SREO-40552-REQ001 (APPX B).
- [SDR IPXA2024040169921](https://openairdocs.org/sdr/IPXA2024040169921.md): Floor Panel · cracked · Mar 8, 2024 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCDFLOOR PANEL 221E IS DAMAGED FABBED PANEL 221EG FROM 5024N400001SS-G,BATCH #4055277 PER SREO-40552-REQ001 ((APPX B)
- [SDR IPXA2024040846502](https://openairdocs.org/sdr/IPXA2024040846502.md): Frame · damaged · Mar 7, 2024 · N128UP · Airbus A300F4622R · Fuselage Main, Frame
  > DAMAGE FOUND ON BOTTOM HOLE ON FR 40 RH LOWER JUNCTION FASTENERS. COMPLIED WITH UPS EO-89994-REQ1 AND VTMAE FINAL EA 300-5710-27-A3542 REV-.
- [SDR IPXA2024033025126](https://openairdocs.org/sdr/IPXA2024033025126.md): Floor Panel · cracked · Mar 6, 2024 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCD FLOOR PANEL 231MJ IS DAMAGED. FABBED PANEL 231MJ FROM 5024N400001SS-G, BATCH # 4055277 PER SREO-40552-REQ001 (APPX B).
- [SDR IPXA2024040121999](https://openairdocs.org/sdr/IPXA2024040121999.md): Floor Panel · cracked · Mar 6, 2024 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCD FLOOR PANEL 241AQ IS DAMAGED FABBED PANEL 241AQ FROM 5024N400001SS-G, BATCH # 4055277, PER SREO-40552-REQ001 (APPX B).
- [SDR IPXA2024040125736](https://openairdocs.org/sdr/IPXA2024040125736.md): Floor Panel · cracked · Mar 6, 2024 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCD FLOOR PANEL 232QH IS DAMAGED FABBED PANEL 232QH FROM 5024N400001SS-G BATCH#4055277 PER SREO-40552-REQ001 (APPX B).
- [SDR IPXA2024032525309](https://openairdocs.org/sdr/IPXA2024032525309.md): Panel · cracked · Mar 6, 2024 · N128UP · Airbus A300F4622R · Wing, Plate/Skin
  > R/H WING ROOT UNDER PANEL 613AB, SKIN IS CRACKED BY NUTPLATE. INSTALLED DOUBLER AT R/H WING ROOT UNDER PANEL 613AB, IAW SRM 53-15-53 AND SRM 51-40-21. APPLIED TOP COAT AT EXTERNAL DOUBLER AT R/H WING ROOT UNDER PANEL 613AB. IAW SRM 51-23-10.
- [SDR IPXA2024040102721](https://openairdocs.org/sdr/IPXA2024040102721.md): Floor Panel · damaged · Mar 5, 2024 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR MCD FLOOR PANEL 261KF HAS (1EA) BROKEN INSERT. FABBED PANEL 261KF FROM 5024N400001SS-G BATCH # 4055277. PER SREO- 40552-REQ001(APPX B).
- [SDR IPXA2024032064596](https://openairdocs.org/sdr/IPXA2024032064596.md): Floor Support · corroded · Mar 2, 2024 · N128UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT: FLOOR STRUCTURE IN FRONT OF LAV HAS CORROSION ON TOP OF BEAM, BENEATH PANEL 221TF. DOT 60-047 INSTALLED FLOOR BEAM SUPPORT IAW SRM 51-40-21-001
- [SDR IPXA2024040157286](https://openairdocs.org/sdr/IPXA2024040157286.md): Fitting · cracked · Mar 1, 2024 · N128UP · Airbus A300F4622R · Wing Main, Frame Structure
  > *** SUPPLEMENTAL SDR *** FAULT: CRACK FOUND AT 10 O'CLOCK POSITION FACING AFT AT FR40 LOWER JUNCTION RH SIDE. APPLIED PROTECTION SURFACE ON FASTENERS HEAD IAW SRM 51-23-10. (8 OZ PAINT CUP #02-012-176) AND APPLIED CIC IAW EO: M-5100-2780-L ON STIFFENER AT FR 4
- [SDR IPXA2024032057068](https://openairdocs.org/sdr/IPXA2024032057068.md): Support Bracket · cracked · Mar 1, 2024 · N128UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO BULKHEAD FRAME 54 HAS A CRACKED FLOOR SUPPORT BRACKET L/H SIDE. DOT 60-043 INSTALLED BRACKET SUPPORT IAW SRM 51-40-21-001.
- [SDR IPXA2024040826401](https://openairdocs.org/sdr/IPXA2024040826401.md): Frame · damaged · Feb 29, 2024 · N128UP · Airbus A300F4622R · Fuselage Main, Frame
  > TOP HOLE RH SIDE ON FR17 HAS DAMAGE THROUGHOUT HOLE. INSTALLED SHACKLE AT FR 17 RH, IAW SRM 51-40-21.
- [SDR IPXA2024032231515](https://openairdocs.org/sdr/IPXA2024032231515.md): Crossbeam · corroded · Feb 29, 2024 · N128UP · Airbus A300F4622R · Fuselage Main, Structure
  > FAULT: AFT CARGO AT FR65, FLOOR BEAM HAS CORROSION. (EXFOLIATION) DOT 60-045 INSTALLED T-PROFILE AND ANGLES REPAIR IAW SRM 51-10-15 PARAGRAPH 11. INSTALLED FILLER BEAM IAW SRM 51-40-21.
- [SDR IPXA2024041663795](https://openairdocs.org/sdr/IPXA2024041663795.md): Frame Splice · damaged · Feb 26, 2024 · N128UP · Airbus A300F4622R · Fuselage Main, Frame
  > MAJOR REPAIR, HOLES A,B,E,F,L,M & N ALL HAVE DAMAGE ON FRAME 47 LH SPLICE FITTING. AREAS MARKED IN RED. VERIFIED INSTALLATION OF FRAME SPLICE AT FR47 FROM S24 TO S26. COMPLIED WITH UPS EO-89765-REQ1 AND VTMAE FINAL EA 300-5315-27-A3531 REV 1
- [SDR IPXA2023100613615](https://openairdocs.org/sdr/IPXA2023100613615.md): Skin · damaged · Oct 5, 2023 · N128UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > STAND IMPACTED AIRCRAFT CREATING HOLE APPROX 4' BEHIND R/H MLG DOOR REMOVED DAMAGE IAW SRM 51-27-00. REPAIRED SKIN IAW EO-88377-REQ1. CW EO
- [SDR IPXA2022122089173](https://openairdocs.org/sdr/IPXA2022122089173.md): Apu · inoperative · Dec 16, 2022 · N128UP · Airbus A300F4622R · APU Cowling/Containment
  > INSPECTION TYPE:NA*EMERGENCY DECLARED* *DIVERSION* *LANDED WITHOUT FURTHER INCIDENT* AT FL360 (WITH GEN 2 DEFERRED)WE LOST APU AND APU GENERATOR,ATTEMTED APU RESTART WITHOUT SUCCESS. DIVERTED DUE TO ONE OPERATING GENERATOR.PERFROMED BITE CHK ON ECB, LOW OIL PR
- [SDR IPXA2022081985397](https://openairdocs.org/sdr/IPXA2022081985397.md): Indicator · inoperative · Aug 18, 2022 · N128UP · Airbus A300F4622R · Landing Gear Brake System
  > INSPECTION TYPE:N/A**ATB** - IMMEDIATELY AFTER TAKE OFF, HOT BRAKE MESSAGE AND LIGHT IN FAN SWITCH. LEFT TRUCK BRAKE TEMP WERE ALL HIGH WITH #5 AND #6 THE HIGHEST. #6 INDICATED 335^ GEAR WAS EXTENDED TO COOL BRAKES WITH VERY LITTLE EFFECT. THE LEFT TRUCK WHEE
- [SDR IPXA2022020478646](https://openairdocs.org/sdr/IPXA2022020478646.md): None · none · Feb 4, 2022 · N128UP · Airbus A300F4622R · Doors
  > INSPECTION TYPE:NA**SUPPLEMENTAL SDR** AIR TURN BACK DUE TO LOWER FWD CARGO DOOR OPEN INDICATION JUST AFTER TAKEOFF. BOTH ECAM AND SYSTEM PAGE CONFIRMED DOOR OPEN CABIN ALT COULD NOT BE VERIFIED DUE TO PHASE OF FLIGHT. DEFERRED CARGO DOOR INDICATION PER MEL 52
- [SDR IPXA2021083173352](https://openairdocs.org/sdr/IPXA2021083173352.md): Web · cracked · Aug 30, 2021 · N128UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:CAFTER PERFORMING ROTO PROBE INSP. PER NTM 57-10-29 FOUND A CRACK INDICATION AT CWB CENTER WEB SPAR REINFORMENT FR 44 LH CUT OUT DOUBLER BOTTOM HOLE AFT LAYER AT 12 O'CLOCK I/B BOTTOM HOLE FWD LAYER.REAMED HOLE TO.262 PER SRM 51-40-40.
- [SDR IPXA2021083173351](https://openairdocs.org/sdr/IPXA2021083173351.md): Web · cracked · Aug 30, 2021 · N128UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:CAFTER PERFORMING ROTO PROBE INSP. PER NTM 57-10-29 FOUND A CRACK INDICATION AT CWB CENTER WEB SPAR REINFORMENT FR 44 LH CUT OUT DOUBLER BOTTOM HOLE AFT LAYER AT 6 O'CLOCK O/B BOTTOM HOLE FWD LAYER.REAMED HOLE TO.262 PER SRM 51-40-40.
- [SDR IPXA2021083173350](https://openairdocs.org/sdr/IPXA2021083173350.md): Spar · cracked · Aug 30, 2021 · N128UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:CAFTER PERFORMING ROTO PROBE INSP. PER NTM 57-10-29 FOUND A CRACK INDICATION AT CWB CENTER WEB SPAR REINFORMENT FR 44 RH CUT OUT DOUBLER O/B BOTTOM HOLE FWD AND AFT LAYER AT 9 O'CLOCK.REAMED HOLE TO.276 PER SRM 51-40-40.
- [SDR IPXA2021082873240](https://openairdocs.org/sdr/IPXA2021082873240.md): Shear Tie · cracked · Aug 28, 2021 · N128UP · Airbus A300F4622R · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:A300RH FR44 FRAME FOOT FITTING HAS A CRACKACCOMPLISHED REPAIR PER EO A300-5310-46789-G APPENDIX K
- [SDR IPXA2021082773198](https://openairdocs.org/sdr/IPXA2021082773198.md): Bracket · cracked · Aug 26, 2021 · N128UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:CAFT CARGO COMP. AT FWD BULHEAD FR54 FOUND 2EA BRACKETS CRACKED.REMOVED AND REPLACED 2EA BRACKETS PER SRM 51-40-21.
- [SDR IPXA2021082873241](https://openairdocs.org/sdr/IPXA2021082873241.md): Shear Tie · cracked · Aug 23, 2021 · N128UP · Airbus A300F4622R · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:A300LH FR44 FRAME FOOT FITTING HAS A SIGN OF CRACKACCOMPLISHED REPAIR PER EO A300-5310-46789-G APPENDIX J
- [SDR IPXA2021082773197](https://openairdocs.org/sdr/IPXA2021082773197.md): Bracket · cracked · Aug 21, 2021 · N128UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:CAFT CARGO COMP. AT FWD BULHEAD FR54 FOUND 2EA BRACKETS CRACKED.REMOVED AND REPLACED 2EA BRACKETS PER SRM 51-40-21.
- [SDR IPXA2021012864998](https://openairdocs.org/sdr/IPXA2021012864998.md): Switch · failed · Jan 28, 2021 · N128UP · Airbus A300F4622R · Cargo/Baggage Doors
  > INSPECTION TYPE: NA ATB-NO EMERGENCY DECLARED-LANDING UNEVENTFUL. ON CLIMB ECAM LOWER FWD CARGO DOOR OPEN MESSAGE. ACCOMPLISHED AIR TURN BACK ON INSPECTION FOUND AFT DOOR SILL MICRO SWITCH 14WS COVERED IN ICE, CLEANED MICRO SWITCH. REMOVED ALL ICE DEBRIS C/
- [SDR IPXA2020071767840](https://openairdocs.org/sdr/IPXA2020071767840.md): Stiffener · cracked · Jul 7, 2020 · N128UP · Airbus A300F4622R · Spoilers
  > LEFT WING TE STIFFENER CRACKED OUTBOARD OF NR 6 SPOILER. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-21 AND SRM 51-40-44.
- [SDR IPXA2020072087908](https://openairdocs.org/sdr/IPXA2020072087908.md): Floor Panel · canning · Jul 2, 2020 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:A300COCKPIT FLOOR PANEL CO-PILOTS SDE OB BETWEEN SEAT AND CB PANEL HAS PREVIOUS REPAIR OR CANNINGREPAIRED IAW SRM 51-77-12 PAR 2 (2) FIG 202 SHEET 3
- [SDR IPXA2020072087910](https://openairdocs.org/sdr/IPXA2020072087910.md): Panel · chafed · Jun 30, 2020 · N128UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > PANEL 147BZ FLANGE CHAFED. REMOVED AND REPLACED THE PANEL.
- [SDR IPXA2020071757882](https://openairdocs.org/sdr/IPXA2020071757882.md): Support Bracket · cracked · Jun 30, 2020 · N128UP · Airbus A300F4622R · Wing, Attach Fittings
  > RIGHT WING NR 3 SPOILER OTBD HINGE SUPPORT BRACKET WAS CRACKED. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-40-21.
- [SDR IPXA2020050454937](https://openairdocs.org/sdr/IPXA2020050454937.md): Hinge · broken · May 1, 2020 · N128UP · Airbus A300F4622R · Passenger/Crew Doors
  > INSPECTION TYPE:N/A** SUPPLEMENTAL SDR ** FWD PASSENGER/ CREW DOOR PANEL # Z831 UPPER HINGE BROKEN. DEFERRED PER REF NEF 25-70-52-10-02 AMC # M706114 ORDER PARTS REQ # 309055.REMOVED SUPPORT ARM LINING. REPLACED UPPER & LOWER HINGES TO FLAP LINING & REINSTALLE
- [SDR IPXA2019052642494](https://openairdocs.org/sdr/IPXA2019052642494.md): Floor Panel · punctured · May 26, 2019 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12Y MAIN CABIN FLOOR PANEL 242DN HAS A PUNCTURE ON UPPER SKIN. REPAIRED PER UPS REO A300-5320-42721-F.
- [SDR IPXA2019052442432](https://openairdocs.org/sdr/IPXA2019052442432.md): Rib · cracked · May 17, 2019 · N128UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:12YR L/W I/B FLAP NOSE RIB #16 IS CRACKED. REMOVED AND REPLACED RIB PER DWG #A57960058-200.
- [SDR IPXA2019051942259](https://openairdocs.org/sdr/IPXA2019051942259.md): Floor Panel · cracked · May 16, 2019 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:124C CRACKED/DELAMINATEDFABRICATED FLOOR PANEL IAW EO A300-5320-16407-E REV DATE 07/29/2010.
- [SDR IPXA2019051942258](https://openairdocs.org/sdr/IPXA2019051942258.md): Floor Panel · cracked · May 16, 2019 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:124C CRACKED/DELAMINATEDFABRICATED FLOOR PANEL IAW EO A300-5320-16407-E REV DATE 07-29-2010.
- [SDR IPXA2019051942257](https://openairdocs.org/sdr/IPXA2019051942257.md): Floor Panel · cracked · May 16, 2019 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:124C CRACKED / DELAMINATEDFABRICATED FLOOR PANEL IAW EO A300-5320-16407-E REV DATE 07/29/2010.
- [SDR IPXA2019051942256](https://openairdocs.org/sdr/IPXA2019051942256.md): Floor Panel · cracked · May 16, 2019 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:124C CRACKED / DELAMINATED FABRICATED FLOOR PANEL IAW EO A300-5320-16407-E REV DATE 07-29-2010.
- [SDR IPXA2019051942255](https://openairdocs.org/sdr/IPXA2019051942255.md): Floor Panel · cracked · May 16, 2019 · N128UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12C CRACKED/DELAMINATEDFABRICATED FLOOOR PANEL IAW EO A300-5320-16407-E REV DATE 07/29/2010.
- [SDR IPXA2019051342057](https://openairdocs.org/sdr/IPXA2019051342057.md): Seat Track · corroded · May 6, 2019 · N128UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:12YR MAIN CABIN SEAT TRACK AT FR 79-80 -Y450 IS CORRODED. REPAIRED PER SRM 53-10-16.
- [SDR IPXA2019051342056](https://openairdocs.org/sdr/IPXA2019051342056.md): Seat Track · corroded · May 6, 2019 · N128UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:12YR MAIN CABIN SEAT TRACK AT FR 79-80 Y1794 IS CORRODED. REPAIRED PER SRM 53-10-16.

Next page: https://openairdocs.org/aircraft/N128UP/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 = 'N128UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N128UP/reports

---
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