# Service difficulty reports: N171UP

A list on [N171UP](https://openairdocs.org/aircraft/N171UP.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 · 187 reports

- [SDR IPXA2025062370033](https://openairdocs.org/sdr/IPXA2025062370033.md): Accumulator · low pressure · Jun 23, 2025 · N171UP · Airbus A300F4622R · Hydraulic Reservoir, Main
  > AFTER TAKEOFF GREEY SYS HYD LOW PRESSURE ECAM AIRCRAFT WAS VIBRATING LANDING GEAR WOULD NOT RETRACT FOLLOWED ECAM PROC AND ATB TO SDF. REMOVED AND REPLACED GREEN HYDRAULIC ACCUMULATOR REF AMM 29-11-56/0401 OPS CHK GOOD. C/W LANDING GEAR NORMAL EXTENSION AND
- [SDR IPXA2025020615290](https://openairdocs.org/sdr/IPXA2025020615290.md): Web · cracked · Jan 27, 2025 · N171UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > R/H ENG, INLET NOSE COWL REAR BULKHEAD, L/H SIDE, PNEUMATIC DUCT CONNECTION SURFACE WITH EVIDENCE OF CRACK. DOT 73-011. INSTALLED PT2 LINE IAW-A300-AMM-73-24-07-0401 TOURQED TO 95 LBF. IN. (T89023). INSTALLED REPAIR IAW-A300-SRM-51-40-21. RETURNED TO NORMAL CO
- [SDR IPXA2025012906803](https://openairdocs.org/sdr/IPXA2025012906803.md): Web · broken · Jan 27, 2025 · N171UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CARGO COMPARTMENT, BTW FR 79 AND FR 80, R/H CORNER, WEB BROKEN. NO DOT. INSTALLED NEW WEB USING EXISTING FASTENERS AND COLLAR P/N NSA5075-6, BATCH 0004148406, P/NNSA5075-5, BATCH 0004148352, IAW A300-600 SRM 51-40-21 AND USING SEALANT P/N 04-001-0114, BAT
- [SDR IPXA2025012906567](https://openairdocs.org/sdr/IPXA2025012906567.md): Web · broken · Jan 27, 2025 · N171UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CARGO COMPARTMENT, BTW FR 79 AND FR 80, L/H CORNER, WEB BROKEN. NO DOT. INSTALLED NEW WEB USING EXISTING FASTENERS AND COLLAR P/N NSA5075-6, BATCH 0004148406, P/NNSA5075-5, BATCH 0004148352, IAW A300-600 SRM 51-40-21 AND USING SEALANT P/N 04-001-0114, BAT
- [SDR IPXA2025012686417](https://openairdocs.org/sdr/IPXA2025012686417.md): Bracket · broken · Jan 19, 2025 · N171UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO FRAME 54.3 STA -450, FLOOR STRUCTURE HAS BROKEN BRACKET FOR BLUE WIRE. INSTALLED NEW BRACKET AT AFT CARGO FRAME 54.3 STA -450, FLOOR STRUCTURE IAW SRM 51-40-21.
- [SDR IPXA2025021444220](https://openairdocs.org/sdr/IPXA2025021444220.md): Seal · broken · Jan 17, 2025 · N171UP · Airbus A300F4622R · Passenger/Crew Doors
  > FWD CREW DOOR, AFT UPPER INNER SEAL BROKEN. DOT 73-009. REMOVED AND REPLACED SEAL AT FWD CREW DOOR AFT UPPER INNER SIDE IAW A300 AMM 12-21-12/001. T95888.
- [SDR IPXA2025021444218](https://openairdocs.org/sdr/IPXA2025021444218.md): Skin · damaged · Jan 17, 2025 · N171UP · Airbus A300F4622R · Passenger/Crew Doors
  > FWD CREW DOOR, UPPER INNER SKIN WITH METAL MARKS. DOT 73-008. RESTORED SURFACE PROTECTION AT UPPER INNER SKIN OF THE FWD CREW DOOR I.A.W. A300-600 S.R.M. 51-21-10 AND 51-75-10. PAUNT CUP #02-012-176.
- [SDR IPXA2025012844227](https://openairdocs.org/sdr/IPXA2025012844227.md): Angle · broken · Jan 17, 2025 · N171UP · Airbus A300F4622R · Passenger/Crew Doors
  > FWD CREW DOOR, AFT MID INNER SEAL SUPPORT BROKEN. DOT 73-010. REMOVED AND REPLACED ANGLE P/N A2521328920200 B/N 0004359285 WITH P/N MS20470AD5-6 B/N 0004237215 IAW SRM 51-40-21.
- [SDR IPXA2024012144220](https://openairdocs.org/sdr/IPXA2024012144220.md): Seal · broken · Jan 17, 2025 · N171UP · Airbus A300F4622R · Passenger/Crew Doors
  > FWD CREW DOOR, AFT UPPER INNER SEAL BROKEN. DOT 73-009 VERIFIED REPLACEMENT OF SEAL AT FWD CREW DOOR AFT UPPER INNER SIDE IAW A300 AMM 12-21-12/001
- [SDR IPXA2025011744218](https://openairdocs.org/sdr/IPXA2025011744218.md): Skin · damaged · Jan 17, 2025 · N171UP · Airbus A300F4622R · Passenger/Crew Doors
  > FWD CREW DOOR, UPPER INNER SKIN WITH METAL MARKS. DOT 73-008 APPROVED
- [SDR IPXA2025012634796](https://openairdocs.org/sdr/IPXA2025012634796.md): Angle · broken · Jan 16, 2025 · N171UP · Airbus A300F4622R · Trailing Edge Flaps
  > LEFTO/B FLAP INBD EDGE ANGLE WEB BROKEN DOT# 110-161 JP-110. REMOVED AND REPLACED ANGLE P/N A5796040221400 BATCH # 0004352771. IAW A300-600 SRM 51-40-21. OSD: 1/27/2025
- [SDR IPXA2025012634986](https://openairdocs.org/sdr/IPXA2025012634986.md): Angle · broken · Jan 16, 2025 · N171UP · Airbus A300F4622R · Trailing Edge Flaps
  > LEFT CENTER FLAP IO/B EDGE ANGLE WEB BROKEN DOT# 110-162 JP-110. TECHNICIAN #91195302 (MCCANKIUS HARRIS) REMOVED AND REPLACED ANGLE P/N A5796040221400 BATCH # 0004352771. IAW A300-600 SRM 51-40-21. OSD: 1/27/2025
- [SDR IPXA2025012635000](https://openairdocs.org/sdr/IPXA2025012635000.md): Angle · broken · Jan 16, 2025 · N171UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT CENTER FLAP IO/B EDGE ANGLE WEB BROKEN DOT# 110-163 JP-110. REMOVED AND REPLACED ANGLE P/N A5796040221400 BATCH #004352771 IAW SRM51-40-21.
- [SDR IPXA2025012628014](https://openairdocs.org/sdr/IPXA2025012628014.md): Angle · broken · Jan 16, 2025 · N171UP · Airbus A300F4622R · Leading Edge Devices
  > LEFT WING FLAP KRUEGER INTERNAL UPPER CENTER AREA HAS BEAM STRUCTURE BROKEN. DOT 75-061 HA-75.INSTALLED WEB/ANGEL USING FASTNERS P/N MS20470AD5-5 BATCH #004237215 AND CR2313-5-05 BATCH # 0004287420 IAW SRM 57-41-11 AND SRM 51-40-21.
- [SDR IPXA2025021289146](https://openairdocs.org/sdr/IPXA2025021289146.md): Flange · damaged · Jan 14, 2025 · N171UP · Airbus A300F4622R · Wing Main, Frame Structure
  > DAMAGE FOUND ON LH FR47 HORIZONTAL JUNCTION (HOLES F AND S). ACCOMPLISH THE REPAIR PER EA 300-5710-27-A3766 REV. -.
- [SDR IPXA2025012683972](https://openairdocs.org/sdr/IPXA2025012683972.md): Floor Panel · broken · Jan 14, 2025 · N171UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO PANEL 151CX (F2557610800900) IS BROKE IN HALF NO DOT SH48554. REPAIRED PANEL IAW-A300-AMM-51-77-10/801. P/N- 04-001-0008 BATCH- 4315497. NO FURTHER ACTION REQUIRED.
- [SDR IPXA2025012689498](https://openairdocs.org/sdr/IPXA2025012689498.md): Web · cracked · Jan 14, 2025 · N171UP · Airbus A300F4622R · Wing Main, Frame Structure
  > WEB O/B OF LH KRUEGER FLAP P/N A5724199320200 CRACKED. DOT# 110-136 JP-110. INSTALLED WEB/ANGEL USING FASTNERS P/N MS20470AD5-5 BATCH #004237215 AND CR2313-5-05 BATCH # 0004287420 IAW SRM 57-41-11 AND SRM 51-40-21.
- [SDR IPXA2025021841197](https://openairdocs.org/sdr/IPXA2025021841197.md): Hose · damaged · Jan 11, 2025 · N171UP · Airbus A300F4622R · Life Raft
  > LIFE RAFT BOX HAS DAMAGED HOSE. VERIFIED STEP 2 AFTER FURTHER INSPECTION, IT WAS DEEMED THAT IT CAN BE REPAIRED WITHOUT AFFECTING OPTIMAL OPERATION. REPAIR COMPLETED IAW AMM 25-00-00/801. REVIEWED
- [SDR IPXA2025012043476](https://openairdocs.org/sdr/IPXA2025012043476.md): Web · bent · Jan 11, 2025 · N171UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > THS COMPARTMENT ACCESS THROUGH 312AL LH WEB BETWEEN FR86 AND FR87 BENT DOT# 110-133 JP-110. COMPLIED WITH SREO 410097 REQ 002 (APPX A). STEPS 1 THRU 12. COLD WORKED WEB AT FR 86 TO FR 87. REQUEST NDT FOR HFEC OF REWORKED AREA.
- [SDR IPXA2025012739972](https://openairdocs.org/sdr/IPXA2025012739972.md): Door · out of limits · Jan 11, 2025 · N171UP · Airbus A300F4622R · Engine Thrust Reverser
  > NR 2 PYLON OUTBD. T/R AFT LATCH DOOR CHAFED INSIDE. INSTALLED NEW DOOR ASSY WITH FASTENERS P/NCR3213-5-04, BATCH 0004188901 IAW A300-600 SRM 51-40-21. REVIEWED
- [SDR IPXA2025011341197](https://openairdocs.org/sdr/IPXA2025011341197.md): Life Raft · damaged · Jan 11, 2025 · N171UP · Airbus A300F4622R · Life Raft
  > **SDR FILED OPEN** FAULT: INT Z200 LIFE RAFT BOX HAS DAMAGED HOSE APPROVED.
- [SDR IPXA2025012677901](https://openairdocs.org/sdr/IPXA2025012677901.md): Web · punctured · Jan 8, 2025 · N171UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > WEB 9, FLOOR LEVEL, WEB UNDERNEATH FLOOR PANEL HAD A PUNCTURE. OSD:1/27/2025
- [SDR IPXA2025011691240](https://openairdocs.org/sdr/IPXA2025011691240.md): Floor Panel · damaged · Jan 8, 2025 · N171UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152VF HAS EDGE HONEYCOMB DAMAGE DOT SH-79 SH48554. REPAIRED FLOOR PANEL 152VF EDGE DAMAGE IAW A300 SREO-42721-REQ001. P/N 04-009-0145 BATCH # 0004354693 NO FURTHER ACTION REQUIRED. ORIGINAL SUBMISSION DATE; 1/16/2025
- [SDR IPXA2025011691270](https://openairdocs.org/sdr/IPXA2025011691270.md): Floor Panel · damaged · Jan 8, 2025 · N171UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151VF HAS EDGE HONEYCOMB DAMAGE SH-80 SH48554. REPAIRED FLOOR PANEL 151VF EDGE DAMAGE IAW A300 SREO-42721-REQ001. P/N 04-009-0145 BATCH # 0004354693 NO FURTHER ACTION REQUIRED. ORIGINAL SUBMISSION DATE: 1/16/2025
- [SDR IPXA2025012681763](https://openairdocs.org/sdr/IPXA2025012681763.md): Floor Support · cracked · Jan 8, 2025 · N171UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FR 10 BELOW FLIGHT DECK IN AVIONICS BAY HAS A CRACKED FLOOR SUPPORT BRACKET ON R/H SIDE. DOT 60-001. VERIFIED INSTALLATION OF NEW FLOOR SUPPORT BRACKET WITH FASTENERS P/N HL10VF5-2, BATCH 0004262584 AND P/N NSA5075-5, BATCH 0004178418 IAW A300-600 SRM 51-40-
- [SDR IPXA2025012681517](https://openairdocs.org/sdr/IPXA2025012681517.md): Bracket · broken · Jan 8, 2025 · N171UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > FWD LWR CARGO FR38.2 HAS TWO BROKEN BRACKET ON L/H SIDE FOR FLOOR SUPPORT BEAM. INSTALLED 2EA BRACKETS IAW-A300-SRM-51-40-21.
- [SDR IPXA2025011691198](https://openairdocs.org/sdr/IPXA2025011691198.md): Floor Panel · damaged · Jan 8, 2025 · N171UP · Airbus A300F4622R · Fuselage Floor Panel
  > FAULT- STR- ZONE 100- AFT CARGO FLOOR PANEL 152QF HAS EDGE HONEYCOMB DAMAGE DOT SH-78 SH48554. REPAIRED FLOOR PANEL 152QF DAMAGE IAW A300 SREO-42721-REQ001. P/N 04-009-0145 BATCH # 0004354693 NO FURTHER ACTION REQUIRED.
- [SDR IPXA2025011691166](https://openairdocs.org/sdr/IPXA2025011691166.md): Floor Panel · damaged · Jan 8, 2025 · N171UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 152MG HAS EDGE HONEYCOMB DAMAGE DOT SH-77 SH48554. REPAIRED FLOOR PANEL 152MG DAMAGE IAW A300 SREO-42721-REQ001. P/N 04-009-0145 BATCH # 0004354693 NO FURTHER ACTION REQUIRED. REVIEWED
- [SDR IPXA2025013160750](https://openairdocs.org/sdr/IPXA2025013160750.md): Hinge Fitting · damaged · Jan 7, 2025 · N171UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > #1 ENG INBD FAN COWL AFT HINGE ARM CHAFFED. VERIFIED INSTALLATION OF NEW HINGE FITTING USING EXISTING FASTENERS IAW A300-600 SRM 51-40-21 WITH SEALANT P/N 04-001-0114, BATCH 0004321398 IAW A300-600 SRM 51-76-10.
- [SDR IPXA2025012660053](https://openairdocs.org/sdr/IPXA2025012660053.md): Fitting · cracked · Jan 7, 2025 · N171UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > FITTING AT FR54, YO AFT CARGO COMPT CRACKED DOT# 110-63 JP-110. INSTALLED THE NEW BRACKET AT FR-54 Y0 IAW SRM 51-40-21. HI-LO P/N: HL18PB5-5, B/N: 0004211840, NUT PLATE P/N: ABS0337-01A, B/N: 0004352855, RIVET BLIND P/N: CCP264SS3-03, B/N: 0004336657, COLLAR
- [SDR IPXA2025012950933](https://openairdocs.org/sdr/IPXA2025012950933.md): Seat Track · corroded · Jan 6, 2025 · N171UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC, FRAME 80, Y450. SEAT TRACK CORRODED DOT 3325-6. LL07167. ACCOMPLISH CAT A PERMANENT REPAIR PER A300-600 SRM REV 41 CHAPTER 53-10-16-201 PARAGRAPH 4 FIGURE 201B.
- [SDR IPXA2025020649678](https://openairdocs.org/sdr/IPXA2025020649678.md): Duct · cracked · Jan 6, 2025 · N171UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > FAULT: STR-540-#2 ENGINE PRECOOLER AIR DUCT CRACKED DOT# 110-71 JP-110. ACCOMPLISHED PERMANENT REPAIR PER EO-92575-REQ1 AND VTMAE EA 300-3611-27-A3759 REV-. REVIEWED
- [SDR IPXA2025012550933](https://openairdocs.org/sdr/IPXA2025012550933.md): Seat Track · corroded · Jan 6, 2025 · N171UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > -MDC, FRAME 80, Y450. SEAT TRACK CORRODED.
- [SDR IPXA2025011950782](https://openairdocs.org/sdr/IPXA2025011950782.md): Frame · broken · Jan 6, 2025 · N171UP · Airbus A300F4622R · Fuselage Main, Frame
  > MDC, FRAME 38.1 R/H. P/N B53781038215, BROKEN. DOT 3325-1. LL07167. REMOVED AND REPLACED SUPPORT ON FRAME RH 38.1 PN#53781038215, IAW SRM 51-40-21 USED THE SAME FASTNERS, PAINT PN#ECL-G-101 BATCH:4340756 APPLIED TOP COAT IAW SRM 51-75-10 CUP PN# 02-012-176.
- [SDR IPXA2024123176779](https://openairdocs.org/sdr/IPXA2024123176779.md): Bracket · cracked · Dec 31, 2024 · N171UP · Airbus A300F4622R · Fuselage Main, Frame
  > AFT CARGO FRAME 54 AT Y0 HAS 1EA CRACKED BRACKET- NO DOT- SH48554 INSTALLED THE NEW BRACKET AT FR-54 Y0 IAW SRM 51-40-21. HI-LO P/N: HL18PB5-5, B/N: 0004211840, NUT PLATE P/N: ABS0337-01A, B/N: 0004352855, RIVET BLIND P/N: CCP264SS3-03, B/N: 0004336657, COLLAR
- [SDR IPXA2024123176810](https://openairdocs.org/sdr/IPXA2024123176810.md): Bracket · cracked · Dec 31, 2024 · N171UP · Airbus A300F4622R · Fuselage Main, Frame
  > AFT CARGO FRAME 54 AT -Y1959 HAS 1EA CRACKED BRACKET- NO DOT- SH48554 INSTALLED BRACKET AT AFT CARGO FRAME 54 AT -Y1959IAW A300 SRM 51-40-21.
- [SDR IPXA2024123176873](https://openairdocs.org/sdr/IPXA2024123176873.md): Bracket · cracked · Dec 31, 2024 · N171UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FWD CARGO FRAME 54 AT Y1959 HAS 1EA CRACKED BRACKET- NO DOT- SH48554. REMOVED AND REPLACED BRACKET AT AFT CARGO FRAME 54 AT Y1959 IAW SRM 51-40-21 SRM 51-76-00.
- [SDR IPXA2024123176805](https://openairdocs.org/sdr/IPXA2024123176805.md): Bracket · cracked · Dec 31, 2024 · N171UP · Airbus A300F4622R · Fuselage Main, Frame
  > AFT CARGO FRAME 54 AT Y953 HAS 2EA CRACKED BRACKETS- NO DOT- SH48554 INSTALLED BRACKET AT AFT CARGO FRAME 54 AT -Y1959 IAW A300 SRM 51-40-21.
- [SDR IPXA2025011768891](https://openairdocs.org/sdr/IPXA2025011768891.md): Striker · cracked · Dec 6, 2024 · N171UP · Airbus A300F4622R · Fuselage Main, Structure
  > DEFERRAL:AFT CARGO UPPER AFT SEAL STRIKER DAMAGED BY GROUND CREW DURING LOAD. VERIFIED REPLACEMENT OF SEAL DEPRESSOR SUPPORT ANGLE AT FR65 IAW SRM 51-40-21.
- [SDR IPXA2023083194063](https://openairdocs.org/sdr/IPXA2023083194063.md): Panel · cracked · Aug 31, 2023 · N171UP · Airbus A300F4622R · Spoilers
  > DEFLECTOR PANEL ABOVE #5 SPOILER LH WING PN A5724077000206 HAS CRACK 2.5 IN LONGREMOVED, FABRICATED AND INSTALLED PANEL IAW EO A300-5750-88043-A AND EA 300-5772-27-A3338
- [SDR IPXA2023083194062](https://openairdocs.org/sdr/IPXA2023083194062.md): Skin · cracked · Aug 31, 2023 · N171UP · Airbus A300F4622R · Spoilers
  > LH WING FIXED TRAILING EDGE SKIN HAS A CRACK AT #5 SPOILER CUTOUTREMOVED FABRICATED AND INSTALLED SKIN IAW SRM 51-40-21
- [SDR IPXA2023083194061](https://openairdocs.org/sdr/IPXA2023083194061.md): Rib · cracked · Aug 31, 2023 · N171UP · Airbus A300F4622R · Spoilers
  > D811439 D/D 08/25/23 EA FLT REINSPECT LEFT WING #5 SPOILER CENTER HINGE SUPPORT JACK RIB DAMAGED REPAIR AT ABX 184-625 (M811438)REMOVED AND REPLACED IAW SRM 51-40-21
- [SDR IPXA2022111488098](https://openairdocs.org/sdr/IPXA2022111488098.md): Wire · damaged · Nov 14, 2022 · N171UP · Airbus A300F4622R · Door System Wiring
  > FWD PAX DOOR FWD LIGHT ASSY PUSH BUTTON WIRES (3LZ) STRIPPED, CRIMPED, AND INSTALLED NEW TERMINALS INTO NEW SOCKET AT FWD LIGHT, FWD PAX DOOR, AS PER SRM 20-48-14. OPS TEST OK
- [SDR IPXA2022111088029](https://openairdocs.org/sdr/IPXA2022111088029.md): Handle · inoperative · Nov 10, 2022 · N171UP · Airbus A300F4622R · Passenger/Crew Doors
  > L1 ENTRY DOOR HANDLE DOES NOT GO ALL THE WAY UP. FOUND COMPENSATION MECHANISM OUT OF ADJUSTMENT, ADJUSTED COMPENSATION MECHANISM TO HANDLE MAX FORCE OF 361. OPERATES W/LIMITS PER AMM 52-10-11. REQUIRES LINING AND SLIDE INSTALLATION.INSTALLED DOOR LINING IAW
- [SDR IPXA2022092386534](https://openairdocs.org/sdr/IPXA2022092386534.md): A/C Pack · odor · Sep 23, 2022 · N171UP · Airbus A300F4622R · Cabin Cooling System
  > PACK 2 HAD A BURNING SMELL ON TAKEOFF AND CRUISE. SWITCHED TO PACK 1 AND SMELL WENT AWAY. PLACED ON MEL IAW A300 MEL 21-51-01-0-1. M791784 ASSIGNED PLACARD INSTALLED. REPLACED AIR COND PACK WATER SOP COURIER BAGS 0868726, OPS CHECK GOOD REF MM 21-51-16. THIS C
- [SDR IPXA2022091986431](https://openairdocs.org/sdr/IPXA2022091986431.md): Warning System · inoperative · Sep 19, 2022 · N171UP · Airbus A300F4622R · Emergency Equipment
  > CREW ENTRY DOOR EVACUATION SLIDE WARNING SYSTEM LIGHT INOP. DEFERRED IAW MEL 52-73-01-1. C/N M791468 ASSIGNED. PLACARD INSTALLED, NIL DMP.ACCOMPLISHED WARNING LIGHT TEST W/R/T AMM 52-73-11-401. OPS CHECK GOOD. NO FAULT NOTED. THIS CLEARS M791468 PLACARD REM
- [SDR IPXA2022070883967](https://openairdocs.org/sdr/IPXA2022070883967.md): Web · cracked · Jul 8, 2022 · N171UP · Airbus A300F4622R · Nacelle/Pylon Structure
  > INSPECTION TYPE:SEGPYLON 1 WEB BEHIND BUTTERFLY PANELS 413 AL AND 414 AR IS CRACKED.ACCOMPLISHED WELD REPAIR PER SRM 54-50-00.
- [SDR IPXA2022070883966](https://openairdocs.org/sdr/IPXA2022070883966.md): Web · cracked · Jul 8, 2022 · N171UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:SEGPYLON 2 WEB BEHIND BUTTERFLY PANELS423AL AND 424AR IS CRACKED.ACCOMPLISHED WELD REPAIR PER SRM 54-50-00
- [SDR IPXA2022070883965](https://openairdocs.org/sdr/IPXA2022070883965.md): Panel · cracked · Jul 8, 2022 · N171UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:SEG#2 ENG PYLON GRILL PANEL O/B HAS A CRACK.ACCOMPLISHED WELD REPAIR PER SRM 54-50-00
- [SDR IPXA2022070883960](https://openairdocs.org/sdr/IPXA2022070883960.md): Panel · cracked · Jul 8, 2022 · N171UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:SEGPANEL 423BL HAS 3 EA CRACK EXTERIOR AT VENT GRILLS.ACCOMPLISHED WELD REPAIR PER SRM 54-52-51

Next page: https://openairdocs.org/aircraft/N171UP/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 = 'N171UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N171UP/reports

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