# Service difficulty reports: N173UP

A list on [N173UP](https://openairdocs.org/aircraft/N173UP.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 · 215 reports

- [SDR IPXA2026052693472](https://openairdocs.org/sdr/IPXA2026052693472.md): Door · noise · May 21, 2026 · N173UP · Airbus A300F4622R · Passenger/Crew Doors
  > EXTREMELY LOUD SQUEAL EMANATING FROM MAIN DOOR ON AIRCRAFT. SOUND IS COMING FROM AREA OF LOWER DOOR HINGE OR FLOOR. INSTALLED NEW ENTRY DOOR SEAL PER AMM 52-10-18. AWAITING SEALANT CURE TIME AND PRESSURIZATION LEAK CHECK. PERFORMED PRESSURIZATION OF ACFT PER
- [SDR IPXA2026052293472](https://openairdocs.org/sdr/IPXA2026052293472.md): Seal · leaking · May 21, 2026 · N173UP · Airbus A300F4622R · Passenger/Crew Doors
  > EXTREMELY LOUD SQUEAL EMANATING FROM MAIN DOOR ON AIRCRAFT. SOUND IS COMING FROM AREA OF LOWER DOOR HINGE OR FLOOR. INSTALLED NEW ENTRY DOOR SEAL PER AMM 52-10-18.
- [SDR IPXA2026011039757](https://openairdocs.org/sdr/IPXA2026011039757.md): Skin · ground damage · Jan 10, 2026 · N173UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > FUSELAGE DAMAGE FROM PACKAGE CONTAINER AT FRAME 54 STATION 3354 LEFT SIDE PAST HYD. SERVICE DOOR. REF[T3F18E0080U8N]. REQUESTED FAULT BE DERRERD FOR 6 MONTHS IAW EO 96143 REQ1
- [SDR IPXA2026010969701](https://openairdocs.org/sdr/IPXA2026010969701.md): Skin Panel · damaged · Dec 29, 2025 · N173UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > FUSELAGE DAMAGE FROM PACKAGE CONTAINER AT FRAME 54 STATION 3354 LEFT SIDE PAST HYD. SERVICE DOOR. REPLACEMENT STRINGER WAS FABRICATED IAW SRM 53-10-14 AND EO-96143-PRELIM4 STEP 6.
- [SDR IPXA2025123069701](https://openairdocs.org/sdr/IPXA2025123069701.md): Skin · damaged · Dec 29, 2025 · N173UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > FUSELAGE DAMAGE FROM PACKAGE CONTAINER AT FRAME 54 STATION 3354 LEFT SIDE PAST HYD. SERVICE DOOR. VERIFY DAMAGE AND REPORT FINDINGS TO SDF LIAISON ENGINEERING PRIOR TO STARTING INITIAL CUTOUT. FOUND 24€? LONG DENT FWD AND AFT OF FRAME 54.2. WIDTH OF DENT MEAS
- [SDR IPXA2025101112350](https://openairdocs.org/sdr/IPXA2025101112350.md): Adapter · cracked · Oct 11, 2025 · N173UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN DECK-CLS ADAPTER CRACKED FR38.1 BETWEEN -Y1959 AND -Y2462-RT SIDE-109. REMOVED 01 CLS ADAPTER. IAW SRM 51-40-21. INSTALLED CLS ADAPTER. IAW SRM 51-40-21.
- [SDR IPXA2025101448379](https://openairdocs.org/sdr/IPXA2025101448379.md): Skin · cracked · Oct 8, 2025 · N173UP · Airbus A300F4622R · Nacelle/Pylon, Plate/Skin
  > FAULT-STR-Z400- #2 ENG PYLON LOWER SPAR LOWER SURFACE LH/RH ANGLE CRACKED PROJECTION RIB 18. DOT 139-2. REMOVED 02 EA ANGLE CRAKED AT #2 ENG PYLON LOWER SPAR LOWER SURFACE LH/RH, IAW A300-600 SRM 51-40-21. INSTALLED NEW 01EA ANGLE SECTION LH P/N A545150632040
- [SDR IPXA2025102037512](https://openairdocs.org/sdr/IPXA2025102037512.md): Thrust Reverser · cracked · Oct 7, 2025 · N173UP · Airbus A300F4622R · Engine Thrust Reverser
  > ENGINE NR 1 OTBD THRUST REVERSER INTERNAL STRUCTURE, AFT UPPER CORNER HAD A CRACK. PERFORMED SURFACE HFEC INSPECTION IN THE CRACKED AREA TO THE NR 1 THRUST REVERSER INTERNAL STRUCTURE AFT UPPER CORNER. FOUND AND VERIFIED CRACK WITH AN EST. LENGTH OF 31.75MM (1
- [SDR IPXA2025100313786](https://openairdocs.org/sdr/IPXA2025100313786.md): Stiffener · cracked · Sep 30, 2025 · N173UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC FLOOR, R/H SIDE, BTW FR 38.1 AND FR 38.2, DOG BONE SUPPORT BROKEN. REMOVED AND REPLACED THE DOG BONE SUPPORT BTW FR 38.1 AND FR 38.2 R/H SIDE IAW SRM 51-40-21.
- [SDR IPXA2025100313780](https://openairdocs.org/sdr/IPXA2025100313780.md): Stiffener · cracked · Sep 30, 2025 · N173UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC FLOOR, R/H SIDE, BTW FR 37 AND FR 38, DOG BONE SUPPORT BROKEN. REMOVED AND REPLACED THE DOG BONE SUPPORT BTW FR 37 AND FR 38 R/H SIDE IAW A300-600 SRM 51-40-21.
- [SDR IPXA2025102300439](https://openairdocs.org/sdr/IPXA2025102300439.md): Floor Panel · damaged · Sep 29, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC FLOOR PANEL 251 LJ IS DAMAGED. FABRICATION OF PANEL 251LJ IS COMPLETE IAW SREO-16407-REQ001((APPX B) A300 MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)). VERIFIED FABRICATION 251LJ
- [SDR IPXA2025101600754](https://openairdocs.org/sdr/IPXA2025101600754.md): Floor Panel · damaged · Sep 29, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > FLOOR PANEL 252 PG IS DAMAGED. FLOOR PANEL 252PG FABRICATION COMPLETED IAW SREO-16407-REQ001.
- [SDR IPXA2025101389818](https://openairdocs.org/sdr/IPXA2025101389818.md): Bracket · gouged · Sep 29, 2025 · N173UP · Airbus A300F4622R · Aerodynamic Fairings
  > LH WING, UPPER SURFACE, WTB, THROUGH FAIRING 577DT, CLOSE TO FALSE REAR SPAR, BRACKET SUPPORT HAS GOUGE. REMOVED BRACKET SUPPORT AT LH WING, UPPER SURFACE, WTB IAW A300-600 SRM 51-40-21. ++INSTALLED NEW BRACKET IAW A300-600 SRM 51-40-21.
- [SDR IPXA2025100383584](https://openairdocs.org/sdr/IPXA2025100383584.md): Fairing · damaged · Sep 28, 2025 · N173UP · Airbus A300F4622R · Leading Edge Devices
  > R/H WING, KRUEGER MOVABLE VANE, EXTERNAL LOWER O/B SKIN WITH GOUGE. REMOVED GAUGE ON EXTERNAL SKIN R/H KRUEGER IAW SRM 51-73-10, ORIGINAL THICKNESS.090", REMAINING THICKNESS.065", MAX MATERIAL LOSS.025" FOUND OUT OF LIMITS IAW A300-600 SRM 51-73-11. REMOVE
- [SDR IPXA2025100383586](https://openairdocs.org/sdr/IPXA2025100383586.md): Fairing · gouged · Sep 28, 2025 · N173UP · Airbus A300F4622R · Leading Edge Devices
  > FAULT - STR - Z600 - R/H WING, KRUEGER MOVABLE VANE, EXTERNAL LOWER CENTER SKIN WITH GOUGE.REMOVED GAUGE ON EXTERNAL SKIN R/H KRUEGER IAW A300-600 SRM 51-73-10.RECEIVED SERVICEABLE RH KRUEGER FLAP FOLDING FAIRING P/N: A5351028500500 AND IT IS APPLICABLE TO USE
- [SDR IPXA2025100383592](https://openairdocs.org/sdr/IPXA2025100383592.md): Skin · gouged · Sep 28, 2025 · N173UP · Airbus A300F4622R · Leading Edge Devices
  > R/H WING, KRUEGER MOVABLE VANE, INTERNAL STRUCTURE, INBOARD LOWER SECTION WITH GOUGE.REMOVED GOUGE ON INTERNAL STRUCTURE SKIN R/H KRUEGER IAW A300-600 SRM 51-73-10.RECEIVED SERVICEABLE RH KRUEGER FLAP FOLDING FAIRING P/N: A5351028500500 AND IT IS APPLICABLE TO
- [SDR IPXA2025100383981](https://openairdocs.org/sdr/IPXA2025100383981.md): Skin · damaged · Sep 28, 2025 · N173UP · Airbus A300F4622R · Leading Edge Devices
  > RIGHT KRUEGER MOVABLE VANE, EXTERNAL SKIN WITH SCRATCH.EMOVED SCRATCH ON EXTERNAL SKIN R/H KRUEGER IAW A300-600 SRM 51-73-10.RECEIVED SERVICEABLE RH KRUEGER FLAP FOLDING FAIRING.INSTALLED R/H WING, KRUEGER FLAP MOVABLE VANE I.A.W. A300 AMM 27-87-12/401
- [SDR IPXA2025101047419](https://openairdocs.org/sdr/IPXA2025101047419.md): Floor Panel · broken · Sep 26, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC, LT SIDE, FLOOR PANEL 241EF, LOWER SURFACE HAS AFT EDGE DAMAGED. FLOOR PANEL 241EF FABRICATION COMPLETE IAW SREO-16407-REQ001.
- [SDR IPXA2025101546777](https://openairdocs.org/sdr/IPXA2025101546777.md): Bracket · cracked · Sep 26, 2025 · N173UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > FWD CARGO, FR 38.2, BULKHEAD PANEL UPPER SUPPORT HAS BRACKETS CRACKED (6EA). SAW THROUGH FLOOR PANELS). REMOVED (6EA) BRACKETS SUPPORT I.A.W SRM 51-40-21. INSTALLED 6 EA NEW BRACKETS IAW A300-600 SRM 51-40-21.
- [SDR IPXA2025101647392](https://openairdocs.org/sdr/IPXA2025101647392.md): Floor Panel · damaged · Sep 26, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC, LH SIDE, FLOOR PANEL 241HF HAS INSERT OUT OFF POSITION AND LOWER SURFACE DAMAGED. FLOOR PANEL 241HF FAB COMPLETED IAW SREO-16407-REQ001.
- [SDR IPXA2025101046801](https://openairdocs.org/sdr/IPXA2025101046801.md): Adapter · corroded · Sep 26, 2025 · N173UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC, LH SIDE, FLOOR AREA, FR36 HAS CLS ADAPTER BROKEN (BY CORROSION). DOT 103-41. REMOVED 01 CLS ADAPTER. IAW SRM 51-40-21. IAW STEP 9. INSTALLED CLS ADAPTER. IAW SRM 51-40-21.
- [SDR IPXA2025100848616](https://openairdocs.org/sdr/IPXA2025100848616.md): Floor Panel · damaged · Sep 26, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC, LH SIDE, FLOOR PANEL241BF, LOWER SURFACE HAS A PUCTURE AND MATERIAL DAMAGED. DOT 103-52 JOB COMPLETED
- [SDR IPXA2025100847419](https://openairdocs.org/sdr/IPXA2025100847419.md): Floor Panel · damaged · Sep 26, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC, LH SIDE, FLOOR PANEL 241EF, LOWER SURFACE HAS AFT EDGE DAMAGED. DOT 103-48 APPROVED
- [SDR IPXA2025100251097](https://openairdocs.org/sdr/IPXA2025100251097.md): Support · broken · Sep 26, 2025 · N173UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > MDC, LH SIDE, FLOOR PANEL241BF, LOWER SURFACE HAS A PUCTURE AND MATERIAL DAMAGED. FLOOR PANEL 241BF FABRICATION COMPLETE IAW SREO-16407-REQ001.
- [SDR IPXA2025101631355](https://openairdocs.org/sdr/IPXA2025101631355.md): Floor Panel · damaged · Sep 25, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > FAULT: INT-200- MCC FLOORBOARD 232SG HAS DAMAGE. 33-035. FLOOR PANEL 232SG FAB COMPLETED IAW SREO-16407-REQ001 FLOOR PANEL MATERIAL P/N 5024N400001SS-G B/N 0004055277 QTY-1 TOP INSERTS P/N G2001B-3P B/N 0004418941 QTY-50 BOTTOM INSERTS P/N PG2002B-3S B/N 0004
- [SDR IPXA2025101631583](https://openairdocs.org/sdr/IPXA2025101631583.md): Floor Panel · damaged · Sep 25, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > FAULT: INT-200- MCC FLOORBOARD 232WG HAS AN OVERSIZE SCREW HOLE. 33-038. FLOOR PANEL 232WG FAB COMPLETED IAW SREO-16407-REQ001 FLOOR PANEL MATERIAL P/N 5024N400001SS-G B/N 0004055277 QTY-1 TOP INSERTS P/N G2001B-3P B/N 0004418941 QTY-50 BOTTOM INSERTS P/N PG
- [SDR IPXA2025101539416](https://openairdocs.org/sdr/IPXA2025101539416.md): Bracket · cracked · Sep 25, 2025 · N173UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > FAULT-STR-ZONE 300. VERTICAL STAB, FIN TO FUSELAGE FAIRING AREA, LH #2 UPPER PANEL SUPPORT BRACKET (1EA) BROKEN. REMOVED THE BROKE UPPER BRACKET AT 300. VERTICAL STAB, FIN TO FUSELAGE FAIRING AREA, LH IAW A300-600 SRM 51-40-21 IT. ++INSTALLED SUPPORT BRACKE
- [SDR IPXA2025101339189](https://openairdocs.org/sdr/IPXA2025101339189.md): Bracket · cracked · Sep 25, 2025 · N173UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > VERTICAL STAB, FIN TO FUSELAGE FAIRING AREA, RH #3 PANEL SUPPORT BRACKET (1EA) BROKEN. REMOVED SUPPORT BRACKET (1EA)I.A.W A300-600 SRM 51-40-21. ++INSTALLED NEW PART IAW A300-600 SRM 51-40-21. RIVET P/N CR3213-4-06, BATCH #0004279158, QTY 2EA
- [SDR IPXA2025101046481](https://openairdocs.org/sdr/IPXA2025101046481.md): Adapter · broken · Sep 25, 2025 · N173UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC, LH SIDE, FLOOR AREA, THROUGH PANEL 241YK, BTWN FR38.1 TO 38.2 HAS CLS ADAPTER BROKEN (BY CORROSION). REMOVED 02 EA CLS ADAPTER LOCATED IN FR38.1 AND FR38.2. IAW SRM 51-40-21. IAW STEP 9. INSTALLED 02 EA CLS ADAPTERS. IAW SRM 51-40-21.
- [SDR IPXA2025101031266](https://openairdocs.org/sdr/IPXA2025101031266.md): Floorboard · broken · Sep 25, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCC FLOOR BOARD 231MJ IS BROKEN. 33-033. FLOOR BOARD 231MJ FABRICATION COMPLETE IAW SREO-16407-REQ 001 INSERT QUANTITY 40 INSERT, EDGE FILL, KIT INSERT GLUE. MAJOR.
- [SDR IPXA2025100931224](https://openairdocs.org/sdr/IPXA2025100931224.md): Floor Panel · damaged · Sep 25, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > MCC FWD FLOORBOARD 221CG HAS FWD EDGE DAMAGE. 33-032. FLOOR PANEL FABRICATION COMPLETE IAW SREO-16407-REQ001.
- [SDR IPXA2025100236550](https://openairdocs.org/sdr/IPXA2025100236550.md): Angle · cracked · Sep 25, 2025 · N173UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FR 80, BTW -Y1137.1 AND -Y1580.5, Z ANGLE WITH CRACK.REMOVED AND REPLACED PROFILE-T P/N A53988140120100 BATCH 0004429452, AT MDC, FR 80, BTW -Y1137.1 AND -Y1580.5, IAW A300-600 SRM 51-40-21
- [SDR IPXA2025100638930](https://openairdocs.org/sdr/IPXA2025100638930.md): Fitting · cracked · Sep 25, 2025 · N173UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE, FR 10, -Y1456, FITTING PICK-UP WITH CRACK.REMOVED FITTING IN MAIN DECK FLOOR STRUCTURE, FR 10, -Y1456. IAW AIRBUS A300-600 SRM 51-40-21.FABRICATED, LOCATED AND DRILL NEW FITTING PICK-UP P/N: 2024-T3.063, BATCH: 0004410262 IAWAIRBUSA
- [SDR IPXA2025100346608](https://openairdocs.org/sdr/IPXA2025100346608.md): Support · cracked · Sep 25, 2025 · N173UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC, LH SIDE, FLOOR AREA, FR38.1 TO FR38.2 HAS CROSS WEB (DOG BONE) BROKEN. DOT 103-39.REMOVED SUPPORT CROOS WEB (DOG BONE) LOCATED AT Z200, MDC, LH SIDE, FLOOR AREA, FR38.1 TO FR38.2 IAW A300-600 SRM 51-40-21.RECEIVED NEW CROSS WEB (DOG BONE) IAW A300-600 SRM
- [SDR IPXA2025100431410](https://openairdocs.org/sdr/IPXA2025100431410.md): Stiffener · cracked · Sep 25, 2025 · N173UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > RIGHT MAIN DECK DOG BONE IS LOOSE BETWEEN FR 37-38. REPLACED DOG BONE BETWEEN FR 37-38 IAW SRM 51-40-21.
- [SDR IPXA2025100431378](https://openairdocs.org/sdr/IPXA2025100431378.md): Stiffener · cracked · Sep 25, 2025 · N173UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > RIGHT MAIN DECK DOGBONE BROKEN AT FR 38.1 - 38.2. REPLACED DOG BONE BETWEEN FR 38.1 - 38.2 IAW SRM 51-40-21.
- [SDR IPXA2025102108625](https://openairdocs.org/sdr/IPXA2025102108625.md): Door · damaged · Sep 24, 2025 · N173UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, EXTERNAL HANDLE INNER SIDE, LOWER EDGE HAS A GOUGE. REMOVED MINOR GOUGE AT CREW DOOR, EXTERNAL HANDLE INNER SIDE, LOWER IAW SRM 51-73-10 AND ORIGINAL THICKNESS IS 0.135" AND MATERIAL LOSS IS 0.001 AND REMAINING THICKNESS IS 0.134" AND FOUND WITH I
- [SDR IPXA2025102125858](https://openairdocs.org/sdr/IPXA2025102125858.md): Skin · damaged · Sep 24, 2025 · N173UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR, EXTERNAL SURFACE, ALONG OF THE FWD EDGE HAS BARE METAL. PREPPED AND PAINTED CREW DOOR EXTERNAL SURFACE,ALONG OF THE FWD EDGE IAW SRM 51-75 10.
- [SDR IPXA2025102126197](https://openairdocs.org/sdr/IPXA2025102126197.md): Rail · damaged · Sep 24, 2025 · N173UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR CUT-OUT, FWD AND AFT FRAMES, ROLLER RAILS (4EA) HAVE GOUGES. REMOVED MINOR GOUDES AT FWD AND AFT FRAMES, ROLLER RAILS (4EA) IAW SRM 51-73-10 AND THE ORIGINAL THICKNESS IS 0.095" AND MATERIAL LOSS 0.002 AND REMAINING THICKESS IS 0.093" AND FOUND WITH
- [SDR IPXA2025101613715](https://openairdocs.org/sdr/IPXA2025101613715.md): Floor Panel · damaged · Sep 24, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 251DN, CORNER DAMAGED. FLOOR PANEL 251CN FAB COMPLETED IAW SREO-16407-REQ001 FLOOR PANEL MATERIAL P/N 5024N400001SS-G B/N 0004055277 QTY-1 TOP INSERTS P/N G2001B-3P B/N 0004418941 QTY-50 BOTTOM INSERTS P/N PG2002B-3S B/N 0004392380 QTY-5
- [SDR IPXA2025101622483](https://openairdocs.org/sdr/IPXA2025101622483.md): Floor Panel · damaged · Sep 24, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 251CN HAS COMPOSITE DAMAGE. PANEL 251CN FABRICATION COMPLETED IAW SREO-16407-REQ001 FLOOR PANEL MATERIAL P/N 5024N400001SS-G B/N 0004055277 QTY1 TOP INSERT P/N G2001B-3P B/N 0004418941 QTY 50 BOTTOM INSERT P/N G2002B-3S B/N 0004392380 QT
- [SDR IPXA2025101522450](https://openairdocs.org/sdr/IPXA2025101522450.md): Adapter · broken · Sep 24, 2025 · N173UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC FLOOR STRUCTURE, FR 63, -Y1959 HAS CLS ADAPTER BROKEN.. REMOVED CLS ADAPTER AT MDC FLOOR STRUCTURE, FR 63, -Y1959, IAW SRM 51-40-21. ACCOMPLISH PERMANENT REPAIR IAW EO-95271-REQ1 AND VT-MAE EA 300-5317-27-A4164.
- [SDR IPXA2025101513883](https://openairdocs.org/sdr/IPXA2025101513883.md): Adapter · corroded · Sep 24, 2025 · N173UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC FLOOR, FR 59, BTW Y0 AND -Y450, CLS ADAPTER CORRODED. REWORKED CLS ADAPTER AT FR59 BTW Y0 AND Y-450 BY TOOL AND IS OUT OF LIMITS. ACCOMPLISHED STEP 11 EA#300-5317-27-A4163 PRELIMINARY 1. INSTALL CLS ADAPTER PER DRAWING A53275514.
- [SDR IPXA2025101022102](https://openairdocs.org/sdr/IPXA2025101022102.md): Crossbeam · bent · Sep 24, 2025 · N173UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC, FR 48, BTW -Y450 AND -Y953, CROSSBEAM BENT. CROSSBEAM REMOVED AND REPLACED IAW A300-600 SRM51-72-10, SRM51-40-21.
- [SDR IPXA2025101022100](https://openairdocs.org/sdr/IPXA2025101022100.md): Crossbeam · bent · Sep 24, 2025 · N173UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC, FR 49, BTW -Y450 AND -Y953, CROSSBEAM BENT. CROSSBEAM REMOVED AND REPLACED IAW A300-600 SRM51-72-10, SRM51-40-21.
- [SDR IPXA2025101022072](https://openairdocs.org/sdr/IPXA2025101022072.md): Crossbeam · bent · Sep 24, 2025 · N173UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC, FR 50, BTW -Y450 AND -Y953, CROSSBEAM BENT. CROSSBEAM REMOVED AND REPLACED IAW A300-600 SRM51-72-10, SRM51-40-21.
- [SDR IPXA2025101021115](https://openairdocs.org/sdr/IPXA2025101021115.md): Crossbeam · cracked · Sep 24, 2025 · N173UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC, FR 51, BTW -Y450 AND -Y953, CROSSBEAM CRACKED. CROSSBEAM REMOVED AND REPLACED IAW A300-600 SRM51-72-10, SRM51-40-21.
- [SDR IPXA2025101023459](https://openairdocs.org/sdr/IPXA2025101023459.md): Floorboard · delaminated · Sep 24, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 241JN DELAMINATED. FLOOR BOARD 231MJ FABRICATION COMPLETE IAW SREO-16407-REQ00.
- [SDR IPXA2025101022355](https://openairdocs.org/sdr/IPXA2025101022355.md): Floorboard · damaged · Sep 24, 2025 · N173UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN DECK FOOR PANEL 262GH EDGE DAMAGED. FLOOR BOARD 262GH FABRICATION COMPLETE IAW SREO-16407-REQ001. MAJOR REPAIR.
- [SDR IPXA2025100122455](https://openairdocs.org/sdr/IPXA2025100122455.md): Floor Support · cracked · Sep 24, 2025 · N173UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT - STR - Z200 - MDC FLOOR STRUCTURE, FR 74, -Y2127.5 Z ANGLE CRACKED DOT 1/026.REMOVED Z-PROFILE AT MDC FLOOR STRUCTURE, FR 74, -Y2127.5, IAW A300-600 SRM 51-40-21.FABRICATED NEW Z-PROFILE, IAW A300-600 SRM 53-18-18 AND GMM 09-08-01-04.INATALLED NEW Z-PRO

Next page: https://openairdocs.org/aircraft/N173UP/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 = 'N173UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N173UP/reports

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