# Service difficulty reports: N170UP

A list on [N170UP](https://openairdocs.org/aircraft/N170UP.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 · 151 reports

- [SDR IPXA2026060113712](https://openairdocs.org/sdr/IPXA2026060113712.md): Cover · missing · May 29, 2026 · N170UP · Airbus A300F4622R · Emergency Lighting
  > CAPT FOUND EMERGENCY LIGHT IN FLIGHT COMPARTMENT MISSING COVER. REMOVED AND RPLACED EMERGENCY WALL MOUNTED LIGHT ASSY IAW AMM 33-51-17/401, OP'S CKS GOOD
- [SDR IPXA2025091060943](https://openairdocs.org/sdr/IPXA2025091060943.md): Wire · detached · Sep 7, 2025 · N170UP · Airbus A300F4622R · Emergency Lighting
  > EMER EXIT SIGN ABOVE MAIN ENTRY DOOR WILL NOT RETAIN WIRING PINS DUE TO BEING RIPPED OUT CONNECTED WIRES IAW AMM 33-51-13. OPS CHECKS GOOD. INSTALLED ENTRY DOOR LINING IAW AMM 25-23-41/401
- [SDR IPXA2025090860943](https://openairdocs.org/sdr/IPXA2025090860943.md): Wire · detached · Sep 7, 2025 · N170UP · Airbus A300F4622R · Light System Wiring
  > EMER EXIT SIGN ABOVE MAIN ENTRY DOOR WILL NOT RETAIN WIRING PINS DUE TO BEING RIPPED OUT REMOVED AND REPLACED EMER EXIT SIGN MODULE ABOVE MAIN ENTRY DOOR REF A300 AMM 33-51-13. REQUIRES ELECTRICAL HOOK UPS AND PANEL INSTALLATION/OPS CK. OPEN
- [SDR IPXA2024120641999](https://openairdocs.org/sdr/IPXA2024120641999.md): Warning Message · illuminated · Dec 5, 2024 · N170UP · Airbus A300F4622R · Trailing Edge Flap Control System
  > FLT CTL FLAPS SYS 1 & SLATS SYS 1 FAULT ON FLAP RETRACTION AFTER T/O. ECAM & AOM PROCEDURE FOLLOWED A/C RETURNED TO NORMAL OPS. PERFORMED FLAPS/SLATS OPS CHECK PER A300 AMM 27-50-00/0301. OPS CHECK GOOD. NO CURRENT FAULTS.
- [SDR IPXA2024103054935](https://openairdocs.org/sdr/IPXA2024103054935.md): Skin · cracked · Oct 25, 2024 · N170UP · Airbus A300F4622R · Wing, Plate/Skin
  > SKIN CRACKED AT NUTPLATE CORNER OF ACCESS PANEL 513AB. MB-60. TREATED AND PRIMED 2 (EA) DOUBLERS WITH ALODINE P/N ALODINE1132, BATCH 0004325097 AND PRIMER P/N 10-P4-2/2TU, BATCH 0004268573, IAW A300-600 SRM 51-21-10.
- [SDR IPXA2024102465947](https://openairdocs.org/sdr/IPXA2024102465947.md): Frame · cracked · Oct 21, 2024 · N170UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > -#1 PYLON- PANEL 475AL I/B 1ST STIFFENER (FWD) HAS 1' CRACK BETWEEN RIVETS- DOT 109-067-VWV.REMOVED FRAME BRACKET BROKEN FROM PYLON #1 475AL I/B IAW A300-600 SRM 51-40-21.INSTALLED NEW FRAME BRACKET P/N 221-0081-192, BATCH 0003973110 IAW A300-600 SRM 51-40-21
- [SDR IPXA2024111369010](https://openairdocs.org/sdr/IPXA2024111369010.md): Skin · debonded · Oct 10, 2024 · N170UP · Airbus A300F4622R · Elevator, Plate/Skin
  > THE L/H SIDE ELEVATOR UPPER SURFACE, HAS A (1EA) DISBOND NEAR THE INBD SIDE. AREA MARKED IN RED. REVIEWED.
- [SDR IPXA2024101591523](https://openairdocs.org/sdr/IPXA2024101591523.md): Rib · cracked · Oct 6, 2024 · N170UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR REPAIR, AGING ACFT INSP- STRUCT-500- LEFT WING INBD FLAP HAS DEEP GUOGING WITH A DENT DAMAGE IN THE UPPER SKIN SURFACE AT THE #7 TRACK POSITION. DOT AA-001 INSTALLED EXTERNAL PLATE AND SHIM ON INBOARD FLAP AT #17 RIB IAW A300-600 SRM 57-50-00 AND SRM 51
- [SDR IPXA2024110433253](https://openairdocs.org/sdr/IPXA2024110433253.md): Floor Panel · damaged · Oct 3, 2024 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR. FLOOR PANEL 147EF, 2 CORNERS DAMAGED.
- [SDR IPXA2024103079756](https://openairdocs.org/sdr/IPXA2024103079756.md): Tension Tie · cracked · Sep 30, 2024 · N170UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > *SDR FILED OPEN* CRACKS FOUND IN TOP AND MIDDLE HOLES ON FR40 RH UPPER TENSION. VERIFIED LINE 26
- [SDR IPXA2024103079737](https://openairdocs.org/sdr/IPXA2024103079737.md): Frame · cracked · Sep 30, 2024 · N170UP · Airbus A300F4622R · Fuselage Main, Frame
  > CRACKS FOUND IN TOP AND MIDDLE HOLES ON LH FR40 UPPER TENSION. ACCOMPLISED REPAIR IN ACCORDANCE VT-MAE EA 300-5710-27-A3702, REV -.
- [SDR IPXA2024101472885](https://openairdocs.org/sdr/IPXA2024101472885.md): Seat Track · corroded · Sep 30, 2024 · N170UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > BTW FR 73 AND 74, CORROSION ON R/H OF SEAT TRACK -Y2462 (UNDER FLOOR 262JM). INSTALLED NEW SEAT TRACK IAW A300-600 SRM 53-10-16 AND SRM 51-40-21, MATERIAL USED: SEALANT P/N: 04-001-0114, BATCH: 0004301149, SOLID RIVETS P/N: MS20426AD5-4, BATCH: #0004289747,
- [SDR IPXA2024101472878](https://openairdocs.org/sdr/IPXA2024101472878.md): Seat Track · corroded · Sep 30, 2024 · N170UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > BTW FR 73 AND 74, CORROSION ON L/H OF SEAT TRACK Y2462 (UNDER FLOOR 261JM). DOT 73-011 (MOYA-73). INSTALLED NEW SEAT TRACK IAW A300-600 SRM 53-10-16 AND SRM 51-40-21 WITH P/N MS20426AD5-4 BATCH #0004289747, P/N HL10VF8-5 BATCH #0004322830, P/N HL10VF6-3 BATCH
- [SDR IPXA2024101716614](https://openairdocs.org/sdr/IPXA2024101716614.md): Support Bracket · cracked · Sep 26, 2024 · N170UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO AT PRESSURE BULKHEAD FR 54 FOUND 6EA FLOOR SUPPORT BRAKETS CRACKED. DOT 60-006. INSTALLED 6EA BRACKET AT AFT CARGO PRESSURE BULKHEAD FR54 RIVET PN: MS20470AD5-8 BATCH: 0004235393 IAW A300 SRM 51-40-21.
- [SDR IPXA2024102800031](https://openairdocs.org/sdr/IPXA2024102800031.md): Floor Panel · broken · Sep 25, 2024 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO LH SIDE FLOOR PANEL 132MG IS BROKEN. NO DOT. FABRICATED FLOOR PANEL 132MG I.A.W. SREO 16407-REQOO2 USING MATERIALS P/N:5024N400001SS-G BATCH#:0004055277 P/N:SLS5182A3-400-2 BATCH#:0004291041 P/N:SLP5182A3-1 BATCH#:0004305624
- [SDR IPXA2024102800004](https://openairdocs.org/sdr/IPXA2024102800004.md): Floor Panel · broken · Sep 25, 2024 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO LH SIDE FLOOR PANEL 131SG IS BROKEN. NO DOT. FABRICATED FLOOR PANEL 131SG I.A.W. SREO 16407-REQ002 USING MATERIALS P/N: 5024N400001SS-G BATCH#:0004055277 P/N:SLS5182A3-400-2 BATCH#:0004291041 P/N:SLP5182A3-1 BATCH#:0004305624.
- [SDR IPXA2023071093633](https://openairdocs.org/sdr/IPXA2023071093633.md): Warning Light · inoperative · Jul 7, 2023 · N170UP · Airbus A300F4622R · Escape Slide
  > INSPECTION TYPE:NAEVACUATION SLIDE RELEASE WARNING LIGHT INOP. DEFERRED IAW MEL # 52-73-01-1 NO DMP REQUIRED.ACCOMPLISHED RESET TEST OF AUTONOMOUS STDBY PWR UPPLY UNIT IAW AMM 52-73-00 AND CHECKS OK. VERIFIED EVAC/SLIDE RELEASE WARNING LIGHT WHEN COMES ON AND
- [SDR IPXA2022051882217](https://openairdocs.org/sdr/IPXA2022051882217.md): None · inoperative · May 18, 2022 · N170UP · Airbus A300* · Passenger/Crew Doors
  > INSPECTION TYPE:N/ATOOK SEVERAL TIRES TO DISARM SLIDE ON CREW ENTRY DOOR DISARM HANDLE WAS GETTING STUCK ABOUT 3/4" PRIOR TO DISARMED EVENTUALLY HANDLE MOVED TO DISARMED POSITIONLUBRICATED GIRT BAR & GIRT BAR ACTUATING MECHANISM OPS CHECKED ARM & DISARM FUNCTI
- [SDR IPXA2022050681822](https://openairdocs.org/sdr/IPXA2022050681822.md): Bracket · broken · May 6, 2022 · N170UP · Airbus A300* · Aerodynamic Fairings
  > INSPECTION TYPE:SEGFUSELAGE TAIL CONE 317AL HOLD OPEN ROD ATTACHMENT BRACKET WORN.REMOVED AND REPLACED IAW SRM 54-42-21
- [SDR IPXA2021102775386](https://openairdocs.org/sdr/IPXA2021102775386.md): None · none · Oct 27, 2021 · N170UP · Airbus A300F4622R · Passenger/Crew Doors
  > INSPECTION TYPE:NADOOR SLIDE PIN WIRE IS NIOT CONNECTED TO DOORREPAIRED LANYARD AS REQUIRED PER EO A300 5210 72239B
- [SDR IPXA2020102861778](https://openairdocs.org/sdr/IPXA2020102861778.md): Fitting · dirty · Oct 27, 2020 · N170UP · Airbus A300F4622R · Emergency Equipment
  > INSPECTION TYPE: N/A CAPT REPORTED SLIDE HARD TO DISARM. CLEANED DEBRIS FROM FWD GIRT BAR FLOOR FITTING, IAW 52-10-00. OPERATIONS CHECK GOOD.
- [SDR IPXA2019110848771](https://openairdocs.org/sdr/IPXA2019110848771.md): Floor Panel · damaged · Nov 4, 2019 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YRMAIN CABIN FLOOR PANEL 241LJ IS DAMAGED.FABRICATED REPLACEMENT MAIN CABIN FLOOR PANEL 241LJ IAW UPS EO A300-5320-40552-B. (MAJOR)
- [SDR IPXA2019111148810](https://openairdocs.org/sdr/IPXA2019111148810.md): Floor Panel · damaged · Oct 27, 2019 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YRFWD. CARGO FLOOR PANEL # 131BH IS DAMAGED.FABRICATED AND REPLACED FWD. LOWER CARGO FLOOR PANEL # 131BH IAW UPS EO A300-5320-16407-E APPX.C. (MJOR)
- [SDR IPXA2019111148809](https://openairdocs.org/sdr/IPXA2019111148809.md): Floor Panel · damaged · Oct 27, 2019 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YRFWD. CARGO FLOOP PANEL # 131MG IS DAMAGED.FABRICATED AND REPLACED FLOOR PANEL # 131MG IAW UPS EO A300-5320-16407-E APPX.C (MAJOR)
- [SDR IPXA2019111188776](https://openairdocs.org/sdr/IPXA2019111188776.md): Floor Support · cracked · Oct 27, 2019 · N170UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:12YRMAIN CABIN L/H MOST O/B FLOOR SUPPORT IS CRACKED BETWEEN FR 38.1 & 38.12.REMOVED AND REPLACED CRACKED MAIN CABIN L/H MOST O/B FLOOR SUPPORT BETWEEN FR 38.1 & 38.2 IAW A300 SRM 51-40-21. (MINOR)
- [SDR IPXA2019111188775](https://openairdocs.org/sdr/IPXA2019111188775.md): Floor Support · cracked · Oct 27, 2019 · N170UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:12YRMAIN CABIN R/H FLOOR SUPPORT MOST O/B BETWEEN FR 38.1 & 38.2 IS CRACKED.REMOVED AND REPLACED CRACKED MAIN CABIN R/H MOST O/B FLOOR SUPPORT BETWEEN FR 38.1 & 38.2 IAW A300 SRM 51-40-44 AND 51-40-21. (MINOR)
- [SDR IPXA2019110648704](https://openairdocs.org/sdr/IPXA2019110648704.md): Floor Panel · damaged · Oct 27, 2019 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YRFWD CARGO FLOOR PANEL 132SG IS DAMAGED.FABRICATED REPLACEMENT FWD CARGO FLOOR PANEL 132SG IAW UPS EO A300-5320-16407-E APPENDIX C. (MAJOR)
- [SDR IPXA2019110648703](https://openairdocs.org/sdr/IPXA2019110648703.md): Floor Panel · damaged · Oct 27, 2019 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YRFWD CARGO FLOOR PANEL 132MG IS DAMAGED.FABRICATED REPLACEMENT FWD CARGO FLOOR PANEL 132MG IAW UPS EO A300-5320-16407-E APPENDIX C. (MAJOR)
- [SDR IPXA2019110648702](https://openairdocs.org/sdr/IPXA2019110648702.md): Floor Panel · damaged · Oct 27, 2019 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YRFWD CARGO FLOOR PANEL 131DE IS DAMAGED.FABRICATED REPLACEMENT FWD CARGO FLOOR PANEL 131DE IAW UPS EO A300-5320-16407-E APPENDIX C. (MAJOR)
- [SDR IPXA2019110448641](https://openairdocs.org/sdr/IPXA2019110448641.md): Floor Panel · damaged · Oct 27, 2019 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YRMAIN CABIN FLOOR PANEL # 241LH IS DAMAGED.REMOVED, FABRICATED AND REPLACED FLOOR PANEL # 241LH IAW UPS EO A300-5320-40552-B. (MAJOR)
- [SDR IPXA2019111148808](https://openairdocs.org/sdr/IPXA2019111148808.md): Web · cracked · Oct 26, 2019 · N170UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:12YRMAIN CABIN AT FRAME 47, CENTER LINE RIGHT WEB BELOW PANEL 242YH IS CRACKED.REMOVED AND REPLACED WEB IAW SRM 51-40-21. (MINOR)
- [SDR IPXA2019111148801](https://openairdocs.org/sdr/IPXA2019111148801.md): Web · cracked · Oct 26, 2019 · N170UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:12YRFRAME 47 CENTER LINE L/H WEB IS CRACKED.REMOVED AND REPLACED WEB IAW SRM 51-40-21.
- [SDR IPXA2019110848770](https://openairdocs.org/sdr/IPXA2019110848770.md): Floorbeam · cracked · Oct 26, 2019 · N170UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > INSPECTION TYPE:12YRMAIN CABIN FLOOR SUPPORT ANGLE UNDER C.L.S. ADAPTER IS CRACKED AT FR 50 FUSELAGE CENTERLINE.REMOVED AND REPLACE CRACKED MAIN CABIN FLOOR SUPPORT ANGLE UNDER C.L.S. ADAPTER AT FR 50 FUSELAGE CENTERLINE IAW A300SRM 51-40-44 AND 51-40-21. (MIN
- [SDR IPXA2019110848769](https://openairdocs.org/sdr/IPXA2019110848769.md): Floor Support · cracked · Oct 26, 2019 · N170UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:12YRMAIN CABIN FLOOR SUPPORT (PROFILE) IS CRACKED AT R/H SIDE FR 80/82.REMOVED AND REPLACED CRACKED MAIN CABIN FLOOR SUPPORT (PROFILE) AT RT SIDE FR 80/82 IAW A300 SRM 51-40-21. (MINOR)
- [SDR IPXA2019110448638](https://openairdocs.org/sdr/IPXA2019110448638.md): Floor Panel · cracked · Oct 26, 2019 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YRMAIN CABIN FLOOE PANEL #251WG IS CRACKED.REMOVED, FABRICATED AND REPLACED MAIN CABIN FLOOR PANEL # 251WG IAW UPS EO A300-5320-40552-B.
- [SDR IPXA2019110848768](https://openairdocs.org/sdr/IPXA2019110848768.md): Web · cracked · Oct 25, 2019 · N170UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE:12YR#1 PYLON RIB 8 WEB LT SIDE IS CRACKED.REPAIRED CRACKED #1 PYLON RIB 8 WEB AT LT SIDE IAW UPS EO A300-5450-51643-A. (MINOR)
- [SDR IPXA2019110848774](https://openairdocs.org/sdr/IPXA2019110848774.md): Floor Support · cracked · Oct 25, 2019 · N170UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:12YRMAIN CABIN FLOOR SUPPORT PROFILE IS CRACKED AT FR 80/82 L/H SIDE.REMOVED AND REPLACED CRACKED MAIN CABIN FLOOR SUPPORT PROFILE AT FR 80/82 L/H SIDE IAW A300 SRM 51-40-21. (MINOR)
- [SDR IPXA2019110448640](https://openairdocs.org/sdr/IPXA2019110448640.md): Floor Panel · broken · Oct 25, 2019 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YRMAIN CABIN FLOOR PANEL # 261GM HAS A BROKEN OFF CORNER.REMOVED, FABRICATED AND REPLACED FLOOR PANEL # 261GM IAW UPS EO A300-5320-40552-B. (MAJOR)
- [SDR IPXA2019110448639](https://openairdocs.org/sdr/IPXA2019110448639.md): Floor Panel · punctured · Oct 25, 2019 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:12YRMAIN CABIN FLOOR PANEL # 251AN HAS LOWER SKIN PUNCTURE.REMOVED, FABRICATED AND REPLACED FLOOR PANEL # 251AN IAW UPS EO A300-5320-40552-B. (MAJOR)
- [SDR IPXA2019111148807](https://openairdocs.org/sdr/IPXA2019111148807.md): Landing · cracked · Oct 24, 2019 · N170UP · Airbus A300F4622R · Wing Main, Frame Structure
  > INSPECTION TYPE:12YRL/H WING FIXED T/E UPPER PNL. INTERCOSTAL/SUPPORT IS CRACKED ABOVE CENTER FLAP O/B FLAP TRACK.REMOVED AND REPLACED INTERCOSTAL/SUPPORT IAW SRM 51-40-21.(MINOR)
- [SDR IPXA2019110848773](https://openairdocs.org/sdr/IPXA2019110848773.md): Skin · gouged · Oct 24, 2019 · N170UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:12YRRT WING I/B FLAP UPPER SKIN IS GOUGED AT RIB 12 AND BETWEEN STRINGERS 2.1 & 2.2.REPAIRED GOUGED RT WING I/B FLAP UPPER SKIN AT RIB 12 AND BETWEEN STRINGER 2.1 & 2.2 IAW A300 SRM 57-50-00 PAR. E, FIG. 205. (MAJOR)
- [SDR IPXA2019110848772](https://openairdocs.org/sdr/IPXA2019110848772.md): Web · cracked · Oct 24, 2019 · N170UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE:12YR#2 PYLON RIB 8A WEB IS CRACKED AT R/H CORNER.REPAIRED CRACKED #2 PYLON RIB 8A WEB AT R/H CORNER IAW UPS EO A300-5450-51643-A. (MINOR)
- [SDR IPXA2019111198791](https://openairdocs.org/sdr/IPXA2019111198791.md): Spar · cracked · Oct 23, 2019 · N170UP · Airbus A300F4622R · Wing Spar
  > INSPECTION TYPE:12YRL/T WING FIXED L/E SUB-SPAR BOTTOM ANGLE IS CRACKED BETWEEN STN 409.3832 & STN 455.233.REPAIRED CRACKED LT WING FIXED L/E SUB-SPAR BOTTOM ANGLE BETWEEN STN 409.3832 & STN 455.233 IAW VT-SAA EA 300-5740-01-A7938 REV. IR AND UPS EO A300-5740-
- [SDR IPXA2019111148802](https://openairdocs.org/sdr/IPXA2019111148802.md): Web · cracked · Oct 22, 2019 · N170UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:121YAFT FUSELAGE LOWER R/H SIDE INTERCOSTAL/WEB IS BENT BETWEEN FRAME 86-87.REMOVED AND REPLACED INTERCOSTAL/WEB IAW SRM 51-40-21. (MINOR)
- [SDR IPXA2019071344394](https://openairdocs.org/sdr/IPXA2019071344394.md): Warning System · malfunctioned · Jul 12, 2019 · N170UP · Airbus A300F4622R · Door Warning System
  > INSPECTION TYPE:N/A MAIN ENTRY DOOR SLIDE WARNING RED LIGHT DOES NOT ILLUMINATE WHEN TEST BUTTON PRESSED. RESET SLIDE WARNING C/B ARM & WORNING BRAKER SLIDE LIGHT OPS CHECKS NORMAL AT THIS TIME.
- [SDR IPXA2018091984144](https://openairdocs.org/sdr/IPXA2018091984144.md): Proximity Sensor · out of limits · Sep 18, 2018 · N170UP · Airbus A300F4622R · Landing Gear Position and Warning
  > AFTER SETTING 1.5 EPR FOR ENGINE STABILIZATION AND PRIOR TO SETTING TAKEOFF THRUST, THE MASTER WARNING WITH ECAM GEAR NOT DOWN. TAKEOFF REJECTED WITH TWO MORE MASTER WARNINGS WITH THROTTLES AT IDLE, POSITION DET SYS 2. FOUND THE PROXIMITY SENSOR 81GB CLEARANC
- [SDR IPXA2018040528212](https://openairdocs.org/sdr/IPXA2018040528212.md): Lens · broken · Apr 4, 2018 · N170UP · Airbus A300F4622R · Emergency Lighting
  > EMERGENCY LIGHT LENS BROKEN, REPLACED THE LENS.
- [SDR IPXA2017112623890](https://openairdocs.org/sdr/IPXA2017112623890.md): Seal · missing · Nov 25, 2017 · N170UP · Airbus A300F4622R · Electrical/Electronic Compartment Doors
  > AVIONIC COMPARTMENT HINGED ACCESS DOOR SMOKE BARRIOR SEAL MISSING ON ALL SIDES. DOOR SEALS REPLACED IAW SREO A300-2510-66517-B.
- [SDR IPXA2017053017700](https://openairdocs.org/sdr/IPXA2017053017700.md): Angle · cracked · May 23, 2017 · N170UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: 1C, FUSELAGE EXTERIOR LT A/C BAY FAIRING ATTACH ANGLE CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-21
- [SDR IPXA2017053017692](https://openairdocs.org/sdr/IPXA2017053017692.md): Plate · cracked · May 19, 2017 · N170UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > INSPECTION TYPE: 1C, NR 1 PYLON HAS A CRACKED FISH PLATE AT THE INBD PANELS 414CR & 412DR. REMOVED AND REPLACED THE PLATE IAW SRM 54-52-21, AND 54-40-21.

Next page: https://openairdocs.org/aircraft/N170UP/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 = 'N170UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N170UP/reports

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