N144UP

Service difficulty reports · 292

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2026102386192Lens · brokenCREQ REPORTED CABIN PRESSURIZATION LIGHT LENS BROKEN ON L1 DOOR. INSTALLED LENS PER AMM 52-73-15.Oct 23, 2026 · N144UP · Airbus A300F4622R · Cabin Pressure IndicatorSDR IPXA2026101568239Light · inoperativeRED 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 Oct 15, 2026 · N144UP · Airbus A300F4622R · Emergency LightingSDR IPXA2026090492079Hinge · crackedPIANO 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 -.Aug 14, 2026 · N144UP · Airbus A300F4622R · Fuselage, Door HingeSDR IPXA2026090191812Hinge · damagedPIANO 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 -.Aug 14, 2026 · N144UP · Airbus A300F4622R · Fuselage, Door HingeSDR IPXA2026082792079Hinge · crackedPIANO 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.Aug 14, 2026 · N144UP · Airbus A300F4622R · Fuselage, Door HingeSDR IPXA2026082605349Frame · crackedNDT 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.Jul 22, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2026081506117Floor Support · corrodedMAJOR 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.Jul 22, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026080905349Web · crackedMAJOR REPAIR, NDT SUSPECTED CRACKS ON FRAME 40 FUEL TANK SIDE VERTICAL STIFFENERS VERIFIED, SEALING WILL BE COMPLETED UNDER NON-ROUTINE T3F18E009BG1C.Jul 22, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026072804647Angle · crackedANGLE FITTING WITH CRACK AT FR79 -Y1580.5. INSTALLED NEW ANGLE AT FR79 -Y1580.5 IAW A300-600 SRM 51-40-21-001.Jul 22, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026071910870Stiffener · crackedBETWEEN 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.Jul 17, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026073098071Adapter · corrodedCLS ADAPTER WITH CORROSION AT FR62 Y0 RH SIDE. INSTALLED NEW CLS ADAPTER AT MDC FR62 Y0 RH SIDE IAW SRM 51-40-21.Jul 16, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, Longeron/StringerSDR IPXA2026082668019Web · crackedWHILE WORKING T3F18E009437N, LT WING, INBD FLAP, WEB WAS FOUND CRACKED. REMOVED AND REPLACED THE WEB IAW SRM 51-40-21-001.Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026081968144Profile · crackedWHILE WORKING T3F18E00, LT WING INBD FLAP, CLOSING PROFILE WAS FOUND CRACKED. REMOVED AND REPLACED PROFILE CROSSING IAW SRM 51-40-21-001.Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026081967748Web · crackedWHILE WORKING T3F18E009437N, LH WING, INBD FLAP, WEB WAS FOUND CRACKED. REMOVED AND REPLACED WEB IAW SRM 51-40-21-001.Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026081968074Web · crackedWHILE WORKING T3F18E009437N, LT WING, I/B FLAP, WEB WAS FOUND CRACKED. REMOVED AND REPLACED WEB IAW SRM51-40-21-001.Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026081968156Bracket · crackedWHILE WORKING T3F18E009437N, LT WING, INBD FLAP BRACKET WAS FOUND CRACKED. TRAILING EDGE SPLICE BRACKET INSTALLED IAW SRM51-40-21-001.Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026081968019Web · crackedWHILE WORKING T3F18E009437N, LT WING, INBD FLAP, WEB WAS FOUND CRACKED.Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026081967957Web · crackedWHILE WORKING T3F18E009437N, LT WING, INBD FLAP, WEB WAS FOUND CRACKED. REMOVED AND REPLACED WEB IAW A300-600F SKRM51-40-21-001.Jul 15, 2026 · N144UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026082657227Bracket · corrodedHORIZONTAL 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.Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026082657391Bracket · corrodedHORIZONTAL STAB, LT UPPER APRON ATTACH AREA, NR 7 BRACKET WITH CORROSION. INSTALLED A NEW BRACKET NR 7, IAW SRM 51-40-21-001.Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026082657322Bracket · damagedHORIZONTAL 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.Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026073057244Support · corrodedHORIZONTAL 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 55Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026073057393Support · corrodedHORIZONTAL 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 51-75-10-201Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026073057350Support · corrodedHORIZONTAL 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.Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026073057348Support · corrodedHORIZONTAL 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 51-75-10-201Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026072957272Support · corrodedHORIZONTAL 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 51-40-21-001Jul 14, 2026 · N144UP · Airbus A300F4622R · Rudder StructureSDR IPXA2026072157154Bracket · damagedHORIZONTAL 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- 001Jul 14, 2026 · N144UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026082645373Skin · damagedRIGHT 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-.Jul 13, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2026082045373Frame · damagedRH FR58, FWD FASTENER ROW, 6TH HOLE OUTBOARD FROM STRINGER 4 HAS DAMAGE INDICATION OVER 100% FSH.Jul 13, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2026081744849Shear Tie · crackedRIGHT 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.Jul 13, 2026 · N144UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026082702249Frame · crackedRIGHT 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-.Jul 10, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2026082686422Adapter · corrodedMDC CLS FR26 BETWEEN Y1959 AND Y2462 SHOWS EVIDENCE OF CORROSION. ACCOMPLISHED EO-98365-REQ1 SEE T3F18E009DMX5.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026082681011Fitting · crackedCENTER 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.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026082680739Fitting · crackedCENTER 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) .Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082680711Fitting · crackedCENTER 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).Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026080380704Fitting · crackedMAJOR 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. -.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026073085880Seat Track · corrodedMDC CLS AT FR27/Y0 SHOWS EVIDENCE OF CORROSION. INSTALLED CLS TRACK ADAPTER AT Z200 FR27/YO IAW A300-600 SRM 51-40-21-001.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026080786372Seat Track · corrodedMDC 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.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026080981011Shear Tie · crackedCENTER 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.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR IPXA2026080786502Adapter · corrodedFR 32, BTW Y1959 AND Y2462, CLS ADAPTER WITH CORROSION. REPLACED CLS ADAPTER, MDC, FR 32, BTW Y1959 AND Y2462, CLS ADAPTER IAW SRM 51-40-21-001Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026072481022Shear Tie · crackedCENTER 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.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR IPXA2026071185916Adapter · corrodedMDC CLS AT FR28/Y0 SHOWS EVIDENCE OF CORROSION. INSTALLED NEW CLS ADAPTER AT MDC FR28/Y0 IAW SRM 51-40-21.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026072885432Angle · crackedMAIN 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. REVIEWEDJul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026072986100Floor Panel · brokenMAJOR 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 FABRICATIONJul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026072986403Floor Panel · brokenMAJOR REPAIR, MDC, FLOOR PANEL 251XJ BROKEN. FLOOR PANEL 251XJ FABRICATION IS COMPLETED IAW SREO-16407-REQ001 ((APPX B). MAIN DECK CARGO FLOOR PANEL FABRICATION.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026072486375Seat Track · corrodedMDC, 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.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026072386482Adapter · corrodedFR 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 20-54-50-02Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026072185558Profile · crackedMAIN 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.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026071885468Profile · crackedMAIN 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.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026071685417Profile · crackedMAIN 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.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
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