# Service difficulty reports: N144UP

A list on [N144UP](https://openairdocs.org/aircraft/N144UP.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 6 · 292 reports

- [SDR IPXA2026102386192](https://openairdocs.org/sdr/IPXA2026102386192.md): Lens · broken · Oct 23, 2026 · N144UP · Airbus A300F4622R · Cabin Pressure Indicator
  > CREQ REPORTED CABIN PRESSURIZATION LIGHT LENS BROKEN ON L1 DOOR. INSTALLED LENS PER AMM 52-73-15.
- [SDR IPXA2026101568239](https://openairdocs.org/sdr/IPXA2026101568239.md): Light · inoperative · Oct 15, 2026 · N144UP · Airbus A300F4622R · Emergency Lighting
  > RED EMERGENCY LIGHT IN MAIN CABIN DOOR INOP. DEFERRED IAW MEL 52-73-01-1. FOUND LOOSE WIRES ON LIGHT WARNING ASSEMBLY. VERIFIED CORRECT POLARITY OF WIRES RECONNECTED AS REQUIRED REF AMM 52-73-11/401 & ASM 52-73-00 TEST GOOD AT THIS TIME OK FOR SERVICE THIS
- [SDR IPXA2026090492079](https://openairdocs.org/sdr/IPXA2026090492079.md): Hinge · cracked · Aug 14, 2026 · N144UP · Airbus A300F4622R · Fuselage, Door Hinge
  > PIANO HINGE FITTING OF MDC DOOR HOLE 22F HAS INDICATIONS AT 9 O, CLOCK. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-98430-REQ1 AND 300-5236-27-A4604, REV -. ACCOMPLISHED REPAIR IAW EA 300-5236-27-A4604, REV -.
- [SDR IPXA2026090191812](https://openairdocs.org/sdr/IPXA2026090191812.md): Hinge · damaged · Aug 14, 2026 · N144UP · Airbus A300F4622R · Fuselage, Door Hinge
  > PIANO HINGE FITTING OF MDC DOOR HOLE NR 16F HAD TWO INDICATIONS AT 6 & 4 O`CLOCK. ACCOMPLISHED THE REPAIR IAW EO-98430-REQ1, & EA 300-5236-27-A4604, REV -.
- [SDR IPXA2026082792079](https://openairdocs.org/sdr/IPXA2026082792079.md): Hinge · cracked · Aug 14, 2026 · N144UP · Airbus A300F4622R · Fuselage, Door Hinge
  > PIANO HINGE FITTING OF MDC DOOR, HOLE 22F HAS INDICATIONS AT 9 O,CLOCK. STEP 18 OF PRELIMINARY 1, E.A 300-5236-27-A4604, COMPLETED.
- [SDR IPXA2026082605349](https://openairdocs.org/sdr/IPXA2026082605349.md): Frame · cracked · Jul 22, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, Frame
  > NDT SUSPECTED CRACKS ON FRAME 40 FUEL TANK SIDE VERTICAL STIFFENERS. INSTALLED STIFENER REPAIR, DOUBLER AND FRAME STIFENER WAS INSTALLED IAW SRM 51-40-21 AND SRM 57-10-21/201 PER GMM 04-02.
- [SDR IPXA2026081506117](https://openairdocs.org/sdr/IPXA2026081506117.md): Floor Support · corroded · Jul 22, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, AREA BELOW LAVATORY AT FR 11A SHOWS EVIDENCE OF CORROSION. THE FLOOR SUPPORT WAS REMOVED AND REPLACED (STEPS 11 THRU 25) USING RAW MATERIAL IAW SRM 53-12-15-001, FIG 19, ITEM 10, SRM 51-40-44-001, & SRM 51-40-21-00-001.
- [SDR IPXA2026080905349](https://openairdocs.org/sdr/IPXA2026080905349.md): Web · cracked · Jul 22, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, NDT SUSPECTED CRACKS ON FRAME 40 FUEL TANK SIDE VERTICAL STIFFENERS VERIFIED, SEALING WILL BE COMPLETED UNDER NON-ROUTINE T3F18E009BG1C.
- [SDR IPXA2026072804647](https://openairdocs.org/sdr/IPXA2026072804647.md): Angle · cracked · Jul 22, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > ANGLE FITTING WITH CRACK AT FR79 -Y1580.5. INSTALLED NEW ANGLE AT FR79 -Y1580.5 IAW A300-600 SRM 51-40-21-001.
- [SDR IPXA2026071910870](https://openairdocs.org/sdr/IPXA2026071910870.md): Stiffener · cracked · Jul 17, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > BETWEEN FR 37-FR 38 LT SIDE STIFFENER (DOG BONE) CRACKED. INSTALLED FLOOR CHANNELS BETWEEN FR 37 TO FR 38 LT IAW SRM 51-40-21-001.
- [SDR IPXA2026073098071](https://openairdocs.org/sdr/IPXA2026073098071.md): Adapter · corroded · Jul 16, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, Longeron/Stringer
  > CLS ADAPTER WITH CORROSION AT FR62 Y0 RH SIDE. INSTALLED NEW CLS ADAPTER AT MDC FR62 Y0 RH SIDE IAW SRM 51-40-21.
- [SDR IPXA2026082668019](https://openairdocs.org/sdr/IPXA2026082668019.md): Web · cracked · Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge Flaps
  > WHILE WORKING T3F18E009437N, LT WING, INBD FLAP, WEB WAS FOUND CRACKED. REMOVED AND REPLACED THE WEB IAW SRM 51-40-21-001.
- [SDR IPXA2026081968144](https://openairdocs.org/sdr/IPXA2026081968144.md): Profile · cracked · Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge Flaps
  > WHILE WORKING T3F18E00, LT WING INBD FLAP, CLOSING PROFILE WAS FOUND CRACKED. REMOVED AND REPLACED PROFILE CROSSING IAW SRM 51-40-21-001.
- [SDR IPXA2026081967748](https://openairdocs.org/sdr/IPXA2026081967748.md): Web · cracked · Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge Flaps
  > WHILE WORKING T3F18E009437N, LH WING, INBD FLAP, WEB WAS FOUND CRACKED. REMOVED AND REPLACED WEB IAW SRM 51-40-21-001.
- [SDR IPXA2026081968074](https://openairdocs.org/sdr/IPXA2026081968074.md): Web · cracked · Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge Flaps
  > WHILE WORKING T3F18E009437N, LT WING, I/B FLAP, WEB WAS FOUND CRACKED. REMOVED AND REPLACED WEB IAW SRM51-40-21-001.
- [SDR IPXA2026081968156](https://openairdocs.org/sdr/IPXA2026081968156.md): Bracket · cracked · Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge Flaps
  > WHILE WORKING T3F18E009437N, LT WING, INBD FLAP BRACKET WAS FOUND CRACKED. TRAILING EDGE SPLICE BRACKET INSTALLED IAW SRM51-40-21-001.
- [SDR IPXA2026081968019](https://openairdocs.org/sdr/IPXA2026081968019.md): Web · cracked · Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge Flaps
  > WHILE WORKING T3F18E009437N, LT WING, INBD FLAP, WEB WAS FOUND CRACKED.
- [SDR IPXA2026081967957](https://openairdocs.org/sdr/IPXA2026081967957.md): Web · cracked · Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge Flaps
  > WHILE WORKING T3F18E009437N, LT WING, INBD FLAP, WEB WAS FOUND CRACKED. REMOVED AND REPLACED WEB IAW A300-600F SKRM51-40-21-001.
- [SDR IPXA2026082657227](https://openairdocs.org/sdr/IPXA2026082657227.md): Bracket · corroded · Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB, RT LOWER APRON ATTACH AREA, NR 10 BRACKET, CORROSION AROUND ALL SCREW HOLES. INSTALLED NEW BRACKET HORIZONTAL STAB, RT LOWER NR 10 BRACKET IAW SRM 51-40-21-001.
- [SDR IPXA2026082657391](https://openairdocs.org/sdr/IPXA2026082657391.md): Bracket · corroded · Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB, LT UPPER APRON ATTACH AREA, NR 7 BRACKET WITH CORROSION. INSTALLED A NEW BRACKET NR 7, IAW SRM 51-40-21-001.
- [SDR IPXA2026082657322](https://openairdocs.org/sdr/IPXA2026082657322.md): Bracket · damaged · Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB, LEFT LOWER APRON ATTACH AREA, NR 5 BRACKET, 1 SCREW HOLE WITH DRILL HOLE DAMAGE. INSTALLED BRACKET NR 5 IN HORIZONTAL STAB, LT LOWER APRON. IAW SRM 51-40-21-001 AND SRM 55-11-28, PAGE 2, PAGE 3.
- [SDR IPXA2026073057244](https://openairdocs.org/sdr/IPXA2026073057244.md): Support · corroded · Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB, R/H LOWER APRON ATTACH AREA, NR 4 BRACKET, CORROSION AROUND 4 SCREW HOLES. LOCATED AND DRILL NEW SUPPORT RT HORIZONTAL STAB LOWER APRON ATTACH AREA, NR 4 BRACKET IAW SRM 51-40-44-001. INSTALLED HORIZONTAL STAB, RT APRON PANEL 343AR IAW AMM 55
- [SDR IPXA2026073057393](https://openairdocs.org/sdr/IPXA2026073057393.md): Support · corroded · Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB, L/H UPPER APRON ATTACH AREA, NR 8 BRACKET WITH CORROSION. RESTORED SURFACE PROTECTION.APPLIED TREATMENT AND PRIMER IAW SRM 51-21-10-001.APPLIED TOPCOAT IAW SRM 51-75-10-201
- [SDR IPXA2026073057350](https://openairdocs.org/sdr/IPXA2026073057350.md): Support · corroded · Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB, L/H UPPER APRON ATTACH AREA, #10 BRACKET WITH CORROSION. RESTORED SURFACE PROTECTION.APPLIED TREATMENT AND PRIMER IAW SRM 51-21-10-001.APPLIED TOPCOAT IAW SRM 51-75-10-201.
- [SDR IPXA2026073057348](https://openairdocs.org/sdr/IPXA2026073057348.md): Support · corroded · Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB, L/H UPPER APRON ATTACH AREA, NR 9 BRACKET WITH CORROSION. RESTORED SURFACE PROTECTION.APPLIED TREATMENT AND PRIMER IAW SRM 51-21-10-001.APPLIED TOPCOAT IAW SRM 51-75-10-201
- [SDR IPXA2026072957272](https://openairdocs.org/sdr/IPXA2026072957272.md): Support · corroded · Jul 14, 2026 · N144UP · Airbus A300F4622R · Rudder Structure
  > HORIZONTAL STAB, R/H UPPER APRON ATTACH AREA, ONE BRACKET WITH CORROSION. OUT OF SEQUENCE: STEP 2. INSTALLED SUPPORT, USING 04 BOLTS P/N EN611V3-7, BCH 4491492 AND 04 COLLARS. IAW SRM 51-40-21-001
- [SDR IPXA2026072157154](https://openairdocs.org/sdr/IPXA2026072157154.md): Bracket · damaged · Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB, RT LOWER APRON ATTACH AREA, #11 BRACKET SCREW HOLE WITH DRILLED DAMAGE. INSTALLED NEW BRACKET AT STR-Z300-HORIZONTAL STAB, R/H LOWER APRON I.A.W. A300-600 SRM 51-40-21- 001
- [SDR IPXA2026082645373](https://openairdocs.org/sdr/IPXA2026082645373.md): Skin · damaged · Jul 13, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > RIGHT FR 58, FWD FASTENER ROW, 6TH HOLE OTBD FROM STRINGER 4R HAD DAMAGE INDICATION OVER 100% FSH. ACCOMPLISH THE REPAIR IAW EO-98380-REQ1 AND EA 300-5316-27-A4573, REV-.
- [SDR IPXA2026082045373](https://openairdocs.org/sdr/IPXA2026082045373.md): Frame · damaged · Jul 13, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, Frame
  > RH FR58, FWD FASTENER ROW, 6TH HOLE OUTBOARD FROM STRINGER 4 HAS DAMAGE INDICATION OVER 100% FSH.
- [SDR IPXA2026081744849](https://openairdocs.org/sdr/IPXA2026081744849.md): Shear Tie · cracked · Jul 13, 2026 · N144UP · Airbus A300F4622R · Wing Main, Frame Structure
  > RIGHT WING, NEXT TO NR 4 SPOILER OTBD HINGE, WEB CRACKED. INSTALLED NEW SKIN SUPPORT AT R/H WING NEXT TO SPOILER #4 O/B. HINGE. IAW SRM 51-40-21.
- [SDR IPXA2026082702249](https://openairdocs.org/sdr/IPXA2026082702249.md): Frame · cracked · Jul 10, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, Frame
  > RIGHT FR 47 VERTICAL JUNCTION AREA. CRACK INDICATION NOTED AT HOLE N IN ALL LAYERS AT 6 O' CLOCK POSITION. ACCOMPLISHED THE REPAIR PER EO-98116-REQ1 AND EA 300-5710-27-A4553, REV-.
- [SDR IPXA2026082686422](https://openairdocs.org/sdr/IPXA2026082686422.md): Adapter · corroded · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC CLS FR26 BETWEEN Y1959 AND Y2462 SHOWS EVIDENCE OF CORROSION. ACCOMPLISHED EO-98365-REQ1 SEE T3F18E009DMX5.
- [SDR IPXA2026082681011](https://openairdocs.org/sdr/IPXA2026082681011.md): Fitting · cracked · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, Structure
  > CENTER FUSELAGE BASE FRAME FITTING C45 LT SIDE HAS A CRACK. ACCOMPLISHED A REPLACEMENT OF THE BASE FRAME FITTING FR 45 LT IAW EO-46789-JIC003, REV 1, REPLACEMENT-BASE FRAME FITTINGS, FR41 AND FR46, LT. REPAIR PERFORMED IAW EO-46789-JIC003.
- [SDR IPXA2026082680739](https://openairdocs.org/sdr/IPXA2026082680739.md): Fitting · cracked · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE BASE FRAME FITTING FR 44 RH SIDE HAS A CRACK. ACCOMPLISHED EO-46789-JIC008 REV2 REPAIR-BASE FRAME FITTING, FR 41 TO FR 46, RH SIDE (SB A300-57-6177).
- [SDR IPXA2026082680711](https://openairdocs.org/sdr/IPXA2026082680711.md): Fitting · cracked · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE BASE FRAME FITTING FR 46 RH SIDE HAS A CRACK. ACCOMPLISHED EO-46789-JIC008 REV2 REPAIR-BASE FRAME FITTING, FR 41 TO FR 46 (FR46), RH SIDE (SB A300-57-6177).
- [SDR IPXA2026080380704](https://openairdocs.org/sdr/IPXA2026080380704.md): Fitting · cracked · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CENTER FUSELAGE BASE FRAME FITTING FR 45 RT SIDE HAS A CRACK. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-98327-REQ1 AND VT-MAE EA 300-5710-27-A4570, REV. -.
- [SDR IPXA2026073085880](https://openairdocs.org/sdr/IPXA2026073085880.md): Seat Track · corroded · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC CLS AT FR27/Y0 SHOWS EVIDENCE OF CORROSION. INSTALLED CLS TRACK ADAPTER AT Z200 FR27/YO IAW A300-600 SRM 51-40-21-001.
- [SDR IPXA2026080786372](https://openairdocs.org/sdr/IPXA2026080786372.md): Seat Track · corroded · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC SEAT TRACK BETWEEN FR27 AND FR28/ Y1959 SHOWS EVIDENCE OF CORROSION. INSTALLED NEW SEAT TRACK AND 2 EA SPLICE ON MDC AT FR27 TO FR32 Y1959 L/H SIDE IAW A300-600 SRM 53-10-16-201.
- [SDR IPXA2026080981011](https://openairdocs.org/sdr/IPXA2026080981011.md): Shear Tie · cracked · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Internal Mounting Structure
  > CENTER FUSELAGE BASE FRAME FITTING C45 LH SIDE HAS A CRACK. VERIFIED, BASE FRAME FITTING FR45 LT REPLACED IAW EO-46789-JIC003 REV1, STEP 69 TO STEP 84.
- [SDR IPXA2026080786502](https://openairdocs.org/sdr/IPXA2026080786502.md): Adapter · corroded · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > FR 32, BTW Y1959 AND Y2462, CLS ADAPTER WITH CORROSION. REPLACED CLS ADAPTER, MDC, FR 32, BTW Y1959 AND Y2462, CLS ADAPTER IAW SRM 51-40-21-001
- [SDR IPXA2026072481022](https://openairdocs.org/sdr/IPXA2026072481022.md): Shear Tie · cracked · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Internal Mounting Structure
  > CENTER FUSELAGE BASE FRAME FITTING C46 LH SIDE HAS A CRACK. ACCOMPLISHED IAW EO-46789-JIC007 REV2 REPAIR-BASE FRAME FITTING, FR46 TO FR 46 (FR46),LH SIDE (SB A300-57-6177) T3F18E0095MF8 STEP 54 - 64.
- [SDR IPXA2026071185916](https://openairdocs.org/sdr/IPXA2026071185916.md): Adapter · corroded · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC CLS AT FR28/Y0 SHOWS EVIDENCE OF CORROSION. INSTALLED NEW CLS ADAPTER AT MDC FR28/Y0 IAW SRM 51-40-21.
- [SDR IPXA2026072885432](https://openairdocs.org/sdr/IPXA2026072885432.md): Angle · cracked · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO, BRACKET HAS A CRACK AT FRAME 79 AND Y1580.5 (DOT 64-086). INSTALLED NEW ANGLE AT MAIN DECK CARGO, FRAME 79 AND Y1580.5 IAW A300-600 SRM 51-40-21-001. REVIEWED
- [SDR IPXA2026072986100](https://openairdocs.org/sdr/IPXA2026072986100.md): Floor Panel · broken · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, MAIN CABIN FLOOR STRUCTURE, FLOOR PANEL 262JM CORNER IS BROKEN. VERIFIED FABRICATION OF FLOOR PANEL 262JM IAW SREO-16407-REQ001 (APPX B). MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATION
- [SDR IPXA2026072986403](https://openairdocs.org/sdr/IPXA2026072986403.md): Floor Panel · broken · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, MDC, FLOOR PANEL 251XJ BROKEN. FLOOR PANEL 251XJ FABRICATION IS COMPLETED IAW SREO-16407-REQ001 ((APPX B). MAIN DECK CARGO FLOOR PANEL FABRICATION.
- [SDR IPXA2026072486375](https://openairdocs.org/sdr/IPXA2026072486375.md): Seat Track · corroded · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC, FR 62, Y953, SEAT TRACK CORRODED. VERIFIED AS RII ITEM IAW GMM 04-02, MAJOR REPAIR, A NEW SEAT TRACK SECTION AT MDC, FR 62, Y953 WAS INSTALLED IAW SRM 53-10-16-201, PARAGRAPH 4 FIGURE 201. SURFACE PROTECTION RESTORED AFTER INSTALLATION.
- [SDR IPXA2026072386482](https://openairdocs.org/sdr/IPXA2026072386482.md): Adapter · corroded · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > FR 34, BTW Y1959 AND Y2462, CLS ADAPTER BASE WITH CORROSION. DOT 73-121 VERIFIED STEP 11 INSTALLED NEW CLS ADAPTER ON MDC AT FR34 BTW Y1959 AND Y2462 IAW SRM 51-40-21 AND REMOVED PROTECTION ELECTRICAL (EWIS) IAW ESPM 20-54-50-02
- [SDR IPXA2026072185558](https://openairdocs.org/sdr/IPXA2026072185558.md): Profile · cracked · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO, Z PROFILE HAS A CRACK BETWEEN FR74 & 75 UNDERNEATH RH AIR GRILL (DOT 64-091) Z PROFILE INSTALLED ON MAIN CABIN FR74 AND FR75 R/H SIDE. IAW A300-600 SRM 51-40-21-001.
- [SDR IPXA2026071885468](https://openairdocs.org/sdr/IPXA2026071885468.md): Profile · cracked · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO, Z PROFILE HAS A CRACK AT Y2127.5, BETWEEN FR73 & 74. VERIFIED REMOVAL OF EWIS PROTECTION AT MAIN DECK CABIN FR73 AND FR74. IAW ESPM UPS D4-UPS-A300 20-54-50-02. Z PROFILE INSTALLED AT FR73 AND FR74. IAW SRM 51-40-21-001.
- [SDR IPXA2026071685417](https://openairdocs.org/sdr/IPXA2026071685417.md): Profile · cracked · Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO, ZEE PROFILE HAS A CRACK AT FR 80 - 82 BETWEEN Y1221.2 & Y1580.5. MAIN DECK CARGO, FR 80 - 82 BETWEEN Y1221.2 & Y1580.5. INSTALLED ZEE PROFILE, USING SOLID RIVETS IAW SRM 51-40-21-001.

Next page: https://openairdocs.org/aircraft/N144UP/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 = 'N144UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N144UP/reports

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