# Service difficulty reports: N160UP

A list on [N160UP](https://openairdocs.org/aircraft/N160UP.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 · 181 reports

- [SDR IPXA2026080420489](https://openairdocs.org/sdr/IPXA2026080420489.md): Controller · unserviceable · Aug 4, 2026 · N160UP · Airbus A300F4622R · Overheat Detection
  > AIR TURN BACK, ENG 1 BLEED LEAK RESULTING IN AIR TURN BACK FOUND LT WING MFA ILLUMINATED ON MX PANEL. INSPECTED WING PNEUMATIC JOINTS FROM PACK BAY OUT TO LT WING TIP. NO LEAKS NOTED IAW TSM 36-22-00/401. RAN NR 1 ENGINE, NO LEAK INDICATIONS. CHANGED NR 2 OVE
- [SDR IPXA2025031741931](https://openairdocs.org/sdr/IPXA2025031741931.md): Door · damaged · Mar 14, 2025 · N160UP · Airbus A300F4622R · Door Warning System
  > LIGHTNING STRIKE DAMAGE ON RIGHT NOSE GEAR DOOR 2€?AFT OF LE, 6€? OF OUTBD EDGE ADDRESSED AREA AS PER AMM 12-21-11.
- [SDR IPXA2025031742006](https://openairdocs.org/sdr/IPXA2025031742006.md): Skin · damaged · Mar 14, 2025 · N160UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE ON FUSELAGE BETWEEN FR 23 AND 24, 37 INCHES BELOW LWR FWD CARGO DOOR. BLENDED AREA WITHIN ALLOWABLE LIMITS AND RESTORED FINISHED TO THE REQUIREMENTS OF SRM 53-10-12 REPAIR 6.
- [SDR IPXA2025031741968](https://openairdocs.org/sdr/IPXA2025031741968.md): Door · damaged · Mar 14, 2025 · N160UP · Airbus A300F4622R · Door Warning System
  > LIGHTNING STRIKE DAMAGE ON RIGHT NOSE GEAR DOOR 1€?FWD OF AFT EDGE, 10€? FROM OUTBD EDGE. REPAIRED IAW SRM 53-10-12.
- [SDR IPXA2025031741956](https://openairdocs.org/sdr/IPXA2025031741956.md): Skin · damaged · Mar 14, 2025 · N160UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE ON FUSELAGE RT SIDE AT 2410 35€? BELOW WING. PERFORMED A DVI AT STATION 2410 35 INCHES BELOW WING RIGHT HAND SIDE. AT ORANGE TAPE THERE WAS A BLACK SPECK ON FUSELAGE. WIPED ENTIRE AREA DOWN WITH ACETONE. NO LIGHTNING STRIKE NOTED I
- [SDR IPXA2025031441931](https://openairdocs.org/sdr/IPXA2025031441931.md): Skin · damaged · Mar 14, 2025 · N160UP · Airbus A300F4622R · Landing Gear Doors
  > LIGHTNING STRIKE DAMAGE ON RIGHT NOSE GEAR DOOR 2€?AFT OF LE, 6€? OF OUTBD EDGE
- [SDR IPXA2025031442006](https://openairdocs.org/sdr/IPXA2025031442006.md): Skin · damaged · Mar 14, 2025 · N160UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE ON FUSELAGE BETWEEN FR 23 AND 24, 37 INCHES BELOW LWR FWD CARGO DOOR.
- [SDR IPXA2025031441968](https://openairdocs.org/sdr/IPXA2025031441968.md): Skin · damaged · Mar 14, 2025 · N160UP · Airbus A300F4622R · Landing Gear Doors
  > LIGHTNING STRIKE DAMAGE ON RIGHT NOSE GEAR DOOR 1€?FWD OF AFT EDGE, 10€? FROM OUTBD EDGE.
- [SDR IPXA2025031441956](https://openairdocs.org/sdr/IPXA2025031441956.md): Skin · damaged · Mar 14, 2025 · N160UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE ON FUSELAGE RT SIDE AT 2410 35€? BELOW WING.
- [SDR IPXA2024102930903](https://openairdocs.org/sdr/IPXA2024102930903.md): Adc · faulted · Oct 29, 2024 · N160UP · Airbus A300F4622R · Autopilot System
  > ECAM: NAV ADC FAULT 2 FAULT WAS INTERMITTENT EVERY 30 SECONDS / USE EMERGENCY CANCEL TO STOP AUDIO ALERT TROUBLESHOT PER TSM CH 34-10-00-101 FIGURE 103. PERFORMED BITE TEST OF ADC #2 BOX. NO FAULTS FOUND. PERFORMED BITE TEST OF ADC #2 SYSTEM PER AMM CH 34-10-0
- [SDR IPXA2024081222135](https://openairdocs.org/sdr/IPXA2024081222135.md): Hydraulic System · leaking · Aug 12, 2024 · N160UP · Airbus A300F4622R · Hydraulic System, Main
  > **EMERGENCY DECLARED**ECAM GREEN HYD RES LO, FLUID QTY INDICATION LOSS OF FLUID. COMPLIED WITH ECAM / ARCH PROCEDURES SERVICED GREEN HYDRAULIC WITH 2 GALLONS REF AMM 12-12-29/0001
- [SDR IPXA2024052191808](https://openairdocs.org/sdr/IPXA2024052191808.md): Adapter · broken · May 15, 2024 · N160UP · Airbus A300F4622R · Fuselage Main, Structure
  > FOUND BROKEN "CLS" ADAPTOR, RH FR19 BETWEEN MCD FLOOR PANELS 222DG AND 232EF REMOVED AND REPLACED CLS ADAPTER IN R/H FR 19 IAW A300 SRM 51-40-21 PARAGRAPH 7. P/N: B5377413820200 S/N: TAG 02036446. INSTALLED MCD FLOOR PANELS 222DE AND 232EF. IAW AMM 53-10-23-
- [SDR IPXA2024052144309](https://openairdocs.org/sdr/IPXA2024052144309.md): Support Angle · cracked · May 13, 2024 · N160UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT -A300 OPEN Z200 - RH FR 37 MAIN CARGO DECK SUPPORT ANGLE IS CRACKED. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-21 P/N HL11VF6-3 BATCH# 0004186230 P/N 3D0006-3 BATCH# 0004273630 REVIEWED.
- [SDR IPXA2024052144327](https://openairdocs.org/sdr/IPXA2024052144327.md): Support Angle · cracked · May 13, 2024 · N160UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT -A300 OPEN Z200 - RH FR 38.1 MAIN CARGO DECK SUPPORT ANGLE IS CRACKED. INSTALLED STIFFENER AT FRAME 38.1 R/H TO 38.2 R/H IAW SRM 51-40-21 P/N HL11VF6-3 BATCH #0004186230 P/N HL116-6 BATCH# 4279917 P/N 3D0006-3 BATCH# 0004273630 REVIEWED.
- [SDR IPXA2024052844359](https://openairdocs.org/sdr/IPXA2024052844359.md): Support Angle · cracked · May 13, 2024 · N160UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > RH FR 38.2 MAIN CARGO DECK SUPPORT ANGLE IS CRACKED TREATED AND PRIMED NEW CUSP WEB IAW A300 SRM 51-21-10 PRIMER PN: 10P4-2NF BATCH: 8473297014 ALODINE1132 BATCH: 1445846. APPLIED TOPCOAT IAW A300 SRM 51-75-10-201 P/N ECL-G-101
- [SDR IPXA2024052523679](https://openairdocs.org/sdr/IPXA2024052523679.md): Cusp Web · broken · May 11, 2024 · N160UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > BROKEN CUSP WEB AT MCD LH FR 38.2 TREATED AND PRIMED NEW CUSP WEB IAW A300 SRM 51-21-10 PRIMER PN: 10P4-2NF BATCH: 8473297014 ALODINE1132 BATCH: 1445846. APPLIED TOPCOAT IAW A300 SRM 51-75-10-201 P/N ECL-G-101 BATCH: 4266626
- [SDR IPXA2024052183546](https://openairdocs.org/sdr/IPXA2024052183546.md): Floor Panel · damaged · May 2, 2024 · N160UP · Airbus A300F4622R · Fuselage Main, Keel
  > FWD CARGO FLOOR PANEL 131AH IS DAMAGED.
- [SDR IPXA2024052183493](https://openairdocs.org/sdr/IPXA2024052183493.md): Floor Panel · damaged · May 2, 2024 · N160UP · Airbus A300F4622R · Fuselage Floor Panel
  > - FWD CARGO FLOOR PANEL 131RG IS DAMAGED. COMPLETED SREO-16407-REQ002 ((APPX C). JOB IS NOW COMPLETE.
- [SDR IPXA2024052183513](https://openairdocs.org/sdr/IPXA2024052183513.md): Floorboard · broken · May 2, 2024 · N160UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131FE IS DAMAGED FABRICATED FWD CARGO FLOOR PANEL 131FE P/N B5327052700000 USING MATERIAL P/N 5024N400001SS-G BATCH:0004055277 I.A.W. SREO A300-5320-16407-E.
- [SDR IPXA2024050283493](https://openairdocs.org/sdr/IPXA2024050283493.md): Floor Panel · damaged · May 2, 2024 · N160UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131RG IS DAMAGED APPROVED.
- [SDR IPXA2024050283546](https://openairdocs.org/sdr/IPXA2024050283546.md): Floor Panel · damaged · May 2, 2024 · N160UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131AH IS DAMAGED REVIEWED.
- [SDR IPXA2024050283513](https://openairdocs.org/sdr/IPXA2024050283513.md): Floor Panel · damaged · May 2, 2024 · N160UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131FE IS DAMAGED APPROVED.
- [SDR IPXA2024061056443](https://openairdocs.org/sdr/IPXA2024061056443.md): Repair · damaged · Apr 24, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT WING INNER FLAP HAS A DAMAGED EXISTING REPAIR DOUBLER. INSTALLED REPAIR DOUBLER AT INNER FLAP IAW SRM 57-50-00-201. APPLIED TOP COAT AT REPAIR DOUBLER ON INNER FLAP IAW SRM 51-23-10-001. ACCOMPLISH A PERMANENT REPAIR PER SRM REV. 40, 57-50-00-201 PARAGR
- [SDR IPXA2024050754126](https://openairdocs.org/sdr/IPXA2024050754126.md): Floor Panel · cracked · Apr 24, 2024 · N160UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 231LG HAS A CRACK UNDER PANEL.DOT 135/057 FABRICATED M.D.C. FLOOR PANEL 231LG PN: B5327073500000 USING MATERIAL PN:5024N400001SS-G BTCH: 0004055277 I.A.W. S.R.O.A300-5320-40552.
- [SDR IPXA2024043056443](https://openairdocs.org/sdr/IPXA2024043056443.md): Repair · damaged · Apr 24, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > OPEN, RW INNER FLAP HAS A DAMAGED EXISTING REPAIR DOUBLER AND FILLED OUT MEASUREMENTS
- [SDR IPXA2024042766820](https://openairdocs.org/sdr/IPXA2024042766820.md): Floor Panel · broken · Apr 18, 2024 · N160UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 232WG FOUND TO BE CRACKED ON BOTTOM FABRICATED M.D.C. FLOOR PANEL 232WG PN: B5327074600400 USING MATERIAL PN:5024N400001SS-G BTCH: 0004055277 I.A.W. S.R.O.A300-5320-40552. INSTALLED FLOOR PANEL 232WG IAW A300 AMM 53-10-23-0401.
- [SDR IPXA2024061087686](https://openairdocs.org/sdr/IPXA2024061087686.md): Support Angle · corroded · Apr 13, 2024 · N160UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT - MXP-531535-01-1-151- AFT CARGO FR54 BLKHD RH UPPER ANGLE IS CORRODED DOT 5612-1 INSTALLED NEW AFT CARGO BLKH RIGHT UPPER ANGLE IAW SRM 51-40-21 REVIEWED
- [SDR IPXA2024042753612](https://openairdocs.org/sdr/IPXA2024042753612.md): Support · corroded · Apr 11, 2024 · N160UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO CEILING SUPPORT AT FR58 IS CORRODED. VERIFIED APPLICATION OF TOPCOAT ON CEILING SUPPORT AND OK TO INSTALL CEILING SUPPORT GIVEN INSP ONLY. INSTALLED CEILING SUPPORT IAW A300 SRM 51-40-21.
- [SDR IPXA2024042753647](https://openairdocs.org/sdr/IPXA2024042753647.md): Support · corroded · Apr 11, 2024 · N160UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO CEILING SUPPORT AT FR54.2 IS CORRODED. TREATED AND PRIMED NEW CEILING SUPPPORTS (2EA) IAW SRM 51-21-10. INSTALLED 2EA CEILING SUPPORTS IAW SRM 51-40-21.
- [SDR IPXA2024042753575](https://openairdocs.org/sdr/IPXA2024042753575.md): Support · corroded · Apr 11, 2024 · N160UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO CEILING SUPPORT AT FR57 IS CORRODED. TREATED AND PRIMED SUPPORTS IAW A300 SRM 51-21-10. INSTALLED 2EA CEILING SUPPORTS IAW SRM 51-40-21.
- [SDR IPXA2024042753524](https://openairdocs.org/sdr/IPXA2024042753524.md): Support · corroded · Apr 11, 2024 · N160UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO CEILING SUPPORT AT FR62 IS CORRODED. TREATED AND PRIMED SUPPORT IAW SRM 51-21-10. INSTALLED CELING SUPPORT IAW SRM 51-40-21.
- [SDR IPXA2024042937639](https://openairdocs.org/sdr/IPXA2024042937639.md): Floor Panel · broken · Apr 10, 2024 · N160UP · Airbus A300F4622R · Fuselage Floor Panel
  > **SDR FILED OPEN** FAULT- MCD FLOOR PANEL 231WG IS BROKEN INSTALLED FLOOR PANEL 231WG IAW A300 AMM 53-10-23-0401.
- [SDR IPXA2024042993716](https://openairdocs.org/sdr/IPXA2024042993716.md): Angle · cracked · Apr 8, 2024 · N160UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > ACCESS AVIONICS AREA FRAME 10 Y-953 INTERCOASTAL HAS PREVIUOS REPAIR CRACKED 3 INCHS LONG IN THE CORNER NO DOT. INSTALLED 1EA. ANGLE P/N UPA53610270522 AND 1EA. WEB P/N UPA5361197720201 IAW SRM 51-40-21.
- [SDR IPXA2024061071382](https://openairdocs.org/sdr/IPXA2024061071382.md): Rib · cracked · Apr 6, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > ONE CRACK FOUND ON RIB FLANGE 17 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.
- [SDR IPXA2024051575400](https://openairdocs.org/sdr/IPXA2024051575400.md): Shroud · gouged · Apr 6, 2024 · N160UP · Airbus A300F4622R · Wing Main, Frame Structure
  > LEFT WINGTIP LE HAS A DENT FRONT INBD SIDE. APPLIED TREAT AND PRIMER IAW SRM 51-21-10 PARAGRAPH 2. INSTALLED NEW SHROUD ASSY IAW SRM 51-40-21, PARAGRAPH 13. INSTALLED STRIP IAW IAW SRM 51-40-21 PARAGRAPH 5. APPLIED TOP COAT IN AREA IAW SRM 51-75-10, PARAGRAPH
- [SDR IPXA2024050271382](https://openairdocs.org/sdr/IPXA2024050271382.md): Rib · cracked · Apr 6, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > **SDR FILED OPEN** FAULT: 1 CRACK FOUND ON RIB FLANGE 17A RIGHT WING FLAP. VERIFIED STEP # 31 COMPLETED.
- [SDR IPXA2024050271374](https://openairdocs.org/sdr/IPXA2024050271374.md): Rib · cracked · Apr 6, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > TWO CRACKS FOUND ON RIB FLANGE 18 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.
- [SDR IPXA2024050271247](https://openairdocs.org/sdr/IPXA2024050271247.md): Rib · cracked · Apr 6, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > TWO CRACKS FOUND ON RIB FLANGE 27 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.
- [SDR IPXA2024050271299](https://openairdocs.org/sdr/IPXA2024050271299.md): Rib · cracked · Apr 6, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > TWO CRACKS FOUND ON RIB FLANGE 25 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.
- [SDR IPXA2024050271412](https://openairdocs.org/sdr/IPXA2024050271412.md): Rib · cracked · Apr 6, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > TWO CRACKS FOUND ON RIB FLANGE 11 RIGHT WING FLAP. COMPLIED WITH UPS EO-90101 AND VTMAE FINAL EA 300-5750-27-A3570 REV-.
- [SDR IPXA2024050271410](https://openairdocs.org/sdr/IPXA2024050271410.md): Rib · cracked · Apr 6, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > ONE CRACK FOUND ON RIB FLANGE 12 RT WING FLAP. COMPLIED WITH UPS EO-90101 AND VTMAE FINAL EA 300-5750-27-A3570 REV-.
- [SDR IPXA2024050271406](https://openairdocs.org/sdr/IPXA2024050271406.md): Rib · cracked · Apr 6, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > TWO CRACKS FOUND ON RIB FLANGE 13 RT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.
- [SDR IPXA2024050271311](https://openairdocs.org/sdr/IPXA2024050271311.md): Rib · cracked · Apr 6, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > CRACK FOUND ON RIB FLANGE 19 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.
- [SDR IPXA2024050271279](https://openairdocs.org/sdr/IPXA2024050271279.md): Rib · cracked · Apr 6, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > ONE CRACK FOUND ON RIB FLANGE 26 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.
- [SDR IPXA2024050271249](https://openairdocs.org/sdr/IPXA2024050271249.md): Rib · cracked · Apr 6, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > TWO CRACKS FOUND ON RIB FLANGE 26 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV-.
- [SDR IPXA2024050271400](https://openairdocs.org/sdr/IPXA2024050271400.md): Rib · cracked · Apr 6, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > ONE CRACK FOUND ON RIB FLANGE 15 RIGHT WING FLAP. ACCOMPLISH PERMANENT REPAIR PER EO-90101-REQ1 AND EA 300-5750-27-A3570 REV -.
- [SDR IPXA2024041371234](https://openairdocs.org/sdr/IPXA2024041371234.md): Skin · cracked · Apr 6, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > CRACK FOUND RIB FLANGE 27A LEFT FLAP TOP SKIN. ACCOMPLISH PERMANENT REPAIR PER EO-90102-REQ1 AND EA 300-5750-27-A3568 REV -.
- [SDR IPXA2024052145562](https://openairdocs.org/sdr/IPXA2024052145562.md): Cover Plate · cracked · Apr 4, 2024 · N160UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT: CRACK FOUND ON FR40 R/W LOWER CORNER RADIUS AT 6 O'CLOCK POSITION FACING FORWARD. INSTALLEED REPAIR PARTS IAW DRAWING R53810798 REV C AND SRM 51-40-21 AND EO 64579-JIC004 REV 1. INSTALLED RIB AND INTERCOSTAL AT FR 40 L/E IAW SRM 51-40-21 AND EO 64579-JI
- [SDR IPXA2024052145527](https://openairdocs.org/sdr/IPXA2024052145527.md): Cover Plate · cracked · Apr 4, 2024 · N160UP · Airbus A300F4622R · Wing Miscellaneous Structure
  > FAULT: MULTIPLE CRACKS FOUND ON F40 L/W LOWER RADIUS HOLE AROUND 9-11 O'CLOCK FACING FOWARD. INSTALLED REPAIR PARTS IAW DRAWING R53810798 REV C AND SRM 51-40-21 AND EO 64579-JIC003 REV 1. RE-INSTALLED RIB AND INTERCOSTAL AT FR 40 L/E IAW SRM 51-40-21 AND EO 64
- [SDR IPXA2024042701079](https://openairdocs.org/sdr/IPXA2024042701079.md): Skin · dented · Apr 2, 2024 · N160UP · Airbus A300F4622R · Trailing Edge Flaps
  > **SDR FILED OPEN**FAULT - LH OUTBOARD FLAP HAS DENT IN LEADING EDGE VERIFIED TOP COAT APPLICATION STEP 49.

Next page: https://openairdocs.org/aircraft/N160UP/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 = 'N160UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N160UP/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.