N142UP

Service difficulty reports · 287

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 = 'N142UP' 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 IPXA2026090755372Skin · dentedMAJOR REPAIR. DENT ON LEFT SIDE OF FUSELAGE JUST AFT OF LAV SERVICE DOOR REPAIRED IAW EO-98195-REQ2.Jul 31, 2026 · N142UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2026011406798Warning Light · inoperativeON PREFLIGHT, L1 RED WARNING LIGHT DOES NOT ILLUMINATE WHEN TESTED. BUZZER DOES SOUND. FOUND ASPSU WITH RED LIGHT DISPLAYED ON UNIT POSITION. REMOVED AND REPLACED APSU 70WN AND OPERATION CHECKS GOOD IAW AMM 52-73-18/401. THIS CLEARS DMI, PLACARD REMOVED. NO DMJan 14, 2026 · N142UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2026011546798Indicator · no testON PREFLIGHT, L1 RED WARNING LIGHT DOES NOT ILLUMINATE WHEN TESTED. BUZZER DOES SOUND. DEFERRED AS PER MEL 52-73-01-1. PLACARD INSTALLED. NO DMP REQ.Jan 14, 2026 · N142UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2025093098082Bracket · crackedDURING ACCOMPLISHING OF T.C T3F18E007GZC1 FOUND 1EA HYDRAULIC CASE DRAIN LINES SUPPORT BRACKET CRACKED INSIDE ACCESS PANEL 675AB. REMOVED SUPPORT BRACKET IAW SRM 51-40-21. FABRICATED NEW PPORT BRACKET I.A.W A300-600 SRM 57-51-11.INSTALLED NEW BRACKET IAWSep 29, 2025 · N142UP · Airbus A300F4622R · Wing, Attach FittingsSDR IPXA2025092036861Skin Panel · crackedRIGHT WING INBD FIXED T/E IS CRACKED AT FASTNER HOLE. INSTALLED SKIN PANEL AT UPEER AND LOWER R/H WING T/E FIXED INBD USING FASTNERS P/N CR3212-4-03 B# 0004279987 150 EA AND P/N MS20426AD4 B# 0004361884 10 EA IAW A300-600-SRM-51-40-21 AND A300-600-IPC-75-51-1Sep 16, 2025 · N142UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2025092043577Support Bracket · damagedFAULT-Z600-APG-RH WING ACCESS PANEL 672PB CHAFFING ON VERTICAL SUPPORT BRACKET DOT 55-060. INSTALLED RIB ATTACHMENT ON RH WING ACCESS PANEL 672PB IAW A300-600 SRM 51-40-21. REVIEWEDAug 30, 2025 · N142UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2025091706569Attach Bracket · crackedRIGHT HORIZONTAL STAB UPPER CLOSE OUT ATTACH BRACKET IS CRACKED, INSTALLED R/H HORIZONTAL STABILIZER FRONT APRON IAW AMM 55-15-11/401.Aug 28, 2025 · N142UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2025092275064Retainer · gougedLEFT WING FAIRING 533AT SEAL RETAINER HAS A GOUGE. 33-009. INSTALLED NEW SEAL RETAINER ON FAIRING 533AT IAW SRM 51-40-21 AND SRM 51-40-23. REVIEWEDAug 27, 2025 · N142UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2025091978349Floor Panel · damagedFWD. CARGO PIT FLOORBOARD PANEL#132MG RT. CENTER EDGE DAMAGE. VERIFIED FABRICATIN OF FLOOR PANEL 132MG. IAW SREO-16407-REQ002 ((APPX C).Aug 27, 2025 · N142UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025091978207Floor Panel · damagedFWD. CARGO PIT FLOORBOARD PANEL #131DE LH. CORNERS DAMAGED DOT#58-20 DARRYL FORD 91102506. FABRICATED/ INSTALL FLOOR PANEL 131DE, P/N B5327052700000 IAW A300 SREO-16407-REQ002 ((APPX C).Aug 27, 2025 · N142UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025090682238Floorbeam · crackedMDC FLOOR, FR 80, BTW -Y1221.2 AND -Y1580.5, CORNER FLOOR SUPPORT CRACKED. INSTALLED NEW PART IAW SRM 51-40-21 WITH FASTENERS.Aug 27, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2025090682210Floorbeam · crackedMDC FLOOR, FR 80, BTW Y1221.2 AND Y1580.5, CORNER FLOORBEAM CRACKED. PROFILE T WAS INSTALLED IAW SRM 51-40-21.Aug 27, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2025092671560Adapter · corrodedCORROSION FOUND ON SEAT TRACK ADAPTER BTW FR 21 AND FR 27 AT 4 PLACES, NEXT TO ADAPTERS CLS, Y0 -2". INSTALLED NEW SEAT TRACK ADAPTER BETWEEN FR 21 TO FR 27 AND Y-2 IAW SRM 51-20-21.Aug 26, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025092671370Adapter · corrodedCORROSION FOUND ON SEAT TRACK ADAPTER BTW FR 21 AND FR 27 AT 4 PLACES, NEXT TO ADAPTERS CLS. Y0 +2". INSTALLED A NEW SEAT TRACK ADAPTER BETWEEN FR 21 TO FR 27 AND Y+2 IAW SRM 51-20-21.Aug 26, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025092565497Profile · chafedLEFT WING FAIRING 34AT HAS CHAFING ON FWD ATTACH ANGLE 109, INSTALLED NEW PROFILE ON FAIRING 534AT IAW AIRBUS SRM 51-40-21 & SRM 51- 40-23.Aug 26, 2025 · N142UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2025092358524Support Plate · crackedPANEL 575AB SUPPORT PLATE CRACKED. DOT NO. 17-48.INSTALLED SUPPORT PLATE, IAW SRM 51-40-21. VERIFIED ACCOMPLISHMENT OF REPAIR IAW EO-95135-REQ1 AND VT-MAE EA 300-5751-27-A4146, REV.Aug 26, 2025 · N142UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2025091964060Floor Panel · damagedAFT CARGO FLOOR PANEL 151QF HAS DAMAGED EDGES . FABRICATION OF FLOOR PANEL 151QF, IAW SREO-16407-REQ002 ((APPX C). PANEL WILL BE INSTALLED ACCORDING TO CARD NO T3F18E006P978.Aug 26, 2025 · N142UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025091970836Floor Panel · damagedFWD CARGO FLOOR PANEL 132MG HAS DAMAGE IN 10 PLACES. SH 91148554 VERIFIED FABRICATION OF FLOOR PANEL 132MG, IAW SREO-16407-REQ002 ((APPX C).Aug 26, 2025 · N142UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025090663534Bracket · crackedAFT CARGO COMPARTMENT WEB AT FR54, Y0, CRACKED. JP-110. INSTALLED NEW BRACKET IN STR-ZONE 150- AFT CARGO COMPARTMENT WEB AT FR54, Y0, I.A.W. SRM 51-40-21 WITH SEALANT,Aug 26, 2025 · N142UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025090663530Bracket · crackedAFT CARGO WEB AT FR54, Y1959, CRACKED. JP-110. INSTALLED NEW BRACKET IN STR-ZONE 150-AFT CARGO WEB AT FR54, Y1959, I.A.W. A300-600 SRM 51-40-21 WITH SEALANT.Aug 26, 2025 · N142UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025090657922Skin · corrodedLEFT WING TIP UPPER SURFACE BONDING STRIP AFT END CORRODED. DOT NO. 17-35. INSTALLED 1 EA FILLER 1 EA DOUBLER 1 MOUNTING STATIC DISCHARGE IAW SRM 51-40-21.Aug 26, 2025 · N142UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2025091850638Bracket · cracked-EXT TAIL-L/H SIDE WHERE FUSELAGE AND TAIL MEET-ANGLE CRACKED FOR UPPER APRON(333AT)-109 VWV 91195430. INSTALLED L/H HORIZONTAL STABILIZER LEADING EDGE 331AB IAW A300-600 AMM 55-12-11/401. REVIEWEDAug 25, 2025 · N142UP · Airbus A300F4622R · Fuselage, Stabilizer Attach FittingsSDR IPXA2025091739173Bracket · crackedE&E COMPARTMENT, RIB 10, -Y953, SUPPORT ANGLE WITH EVIDENCE OF CRACK. INSTALLED NEW SUPPORT ANGLE AT Z100 E&E COMPARTMENT, RIB 10, -Y953. IAW SRM 51-75-10. REVIEWEDAug 24, 2025 · N142UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025091739164Bracket · crackedE&E COMPARTMENT, RIB 10, Y953, SUPPORT ANGLE CRACK. INSTALLED NEW SUPPORT ANGLE AT E&E COMPARTMENT, RIB 10, Y953. IAW A300-600 SRM 51-75-10.Aug 24, 2025 · N142UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA202509025671Hinge Fitting · crackedPIANO HINGE FITTING OF MDC DOOR HAS CRACK/DAMAGE IN HOLE [19F] BOTTOM LAYERS, 5`CLOCK POSITION. FASTENER IS INSTALLED IAW TASK CARD MXP-531355-02-1-233-JIC (SDI - PIANO HINGE FITTINGS OF MDC DOOR ON FUSELAGE AND DOOR INCLUDING SURROUNDING STRUCTURE) REVIEWEDAug 23, 2025 · N142UP · Airbus A300F4622R · Fuselage, Door HingeSDR IPXA2025082925599Hinge · crackedPIANO HINGE FITTING OF MDC DOOR HAS CRACK IN HOLE [10D] BOTTOM LAYER. FASTENER IS INSTALLED IAW TASK CARD MXP-531355-02-1-233-JIC. SDI - PIANO HINGE FITTINGS OF MDC DOOR ON FUSELAGE AND DOOR INCLUDING SURROUNDING STRUCTURE.Aug 23, 2025 · N142UP · Airbus A300F4622R · Fuselage, Door HingeSDR IPXA2025092606949Rib · crackedLEFT WING CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACKS NOTED AT RIB11. CIRCLED IN RED.ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-94890-REQ1 AND VT-MAE EA 300-5750-27-A4108.Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025092607053Rib · crackedLEFT WING CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK NOTED AT RIB15. CIRCLED IN RED.ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-94890-REQ1 AND VT-MAE EA 300-5750-27-A4108.Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025092607057Rib · crackedLEFT WING CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK NOTED AT RIB19. CIRCLED IN RED.ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-94890-REQ1 AND VT-MAE EA 300-5750-27-A4108.Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025092607061Rib · crackedLEFT WING CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK NOTED AT RIB25. CIRCLED IN RED.ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-94890-REQ1 AND VT-MAE EA 300-5750-27-A4108.Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025092607301Rib · crackedRIGHT WING CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACKS NOTED AT RIB 25. ACCOMPLISHED PERMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV -.Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025101307330Rib · crackedRIGHT WING CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACKS NOTED AT RIB 27. ACCOMPLISHED PERMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV -.Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025092607320Rib · crackedMAJOR REPAIR, RT WING CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACKS NOTED AT RIB 26. ACCOMPLISHED PERMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV. -.Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025092607221Rib · crackedMAJOR REPAIR, RT WING CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACKS NOTED AT RIB 13. ACCOMPLISHED PERMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV. -.Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025092607255Rib · crackedMAJOR REPAIR. RT WING CENTER FLAP, TOP SKIN RIB FLANGE, ONE CRACK NOTED AT RIB18. ACCOMPLISHED PRMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV. -.Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025091909183Floor Panel · damagedFWD CARGO FLOOR PANEL 131DE HAS EDGE DAMAGE 4". SH 91148554. FABRICATED/ INSTALLED FLOOR PANEL 131DE, P/N B5327052700000 IAW A300 SREO-16407-REQ002 ((APPX C).Aug 22, 2025 · N142UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025091908647Floor Panel · damagedAFT CARGO FLOOR PANEL 151QF HAS 2 PLACES 5" OF EDGE DAMAGE. SH 91148554 VERIFIED FABRICATION OF FLOOR PANEL 151QF, P/N B5327053100000<BR>IAW A300 SREO-16407-REQ002 ((APPX C) PANEL WILL BE INSTALLED ACCORDING TO CARD NO T3F18E006P978.Aug 22, 2025 · N142UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025091007301Rib · crackedMAJOR REPAIR. RT WING CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACKS NOTED AT RIB25. CIRCLED IN RED. REVIEWEDAug 22, 2025 · N142UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2025091007330Rib · crackedMAJOR REPAIR, RT WING CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACKS NOTED AT RIB27.Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025091907221Rib · crackedMAJOR REPAIR, RT WING CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACKS NOTED AT RIB13.Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025091507320Rib · crackedRIGHT WING CENTER FLAP, TOP SKIN RIB FLANGE, HAD 2 CRACKS AT RIB 26. COMPLIED WITH STEP 33 OF EA 300-5750-27-A4107, PRELIMINARY 1.Aug 22, 2025 · N142UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025090913704Floorbeam · damagedMAIN DECK-RT SIDE FR51 CROSSBEAM BENT (Y-953 TO Y-450)-109 VWV 91195430 ACCOMPLISHED JOB IAW SREO-75878-REQ001 ((APPX B) TASK CARD:T3F18E007A68T.Aug 22, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2025092089259Adapter · corrodedMAJOR REPAIR, CORROSION ON CLS ADAPTER FR76 Y1580.5. ACCOMPLISHED A PERMANENT REPAIR IAW EO-95063-REQ1 AND EA 300-5318-27-A4106 REV. - .Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025092090275Adapter · corrodedMAJOR REPAIR, CORROSION FOUND ON CLS FR60 Y0 + 3" LT, ACCOMPLISHED REPAIR IAW EO-95062-REQ1 AND EA 300-5317-27-A4104 REV. - .Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025092090261Adapter · corrodedMAJOR REPAIR, CORROSION FOUND ON CLS FR63 Y0 + 3", LT. ACCOMPLISHED PERMANENT REPAIR IAW EO-95062-REQ1 AND EA 300-5317-27-A4104 REV. -..Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025091990000Seat Track · corrodedMAJOR REPAIR, CORROSION FOUND ON SEAT TRACK FLANGE FR 30, Y2462, TWO LOCATIONS. INSTALLED A NEW SEAT TRACK SECTION Y2462 TO FR 30 IAW SRM 51-40-21 AND SRM 53-10-16 PARAGRAPH 4 (FIGURE 201) PAGE 205/206.Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025091789967Seat Track · corrodedMAJOR REPAIR, CORROSION FOUND ON SEAT TRACK FLANGE FR 30 Y1959, TWO LOCATIONS. SEAT TRACK WAS INSTALLED IAW SRM 51-40-21 AND SRM 53-10-16.Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025092090347Adapter · corrodedMAJOR REPAIR, CORROSION FOUND ON CLS FR 33 Y0 + 3" RT, ACCOMPLISHED PERMANENT REPAIR IAWEO-95061-REQ1 AND EA 300-5314-27-A4103 REV. - .Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025083089022Seat Track · corrodedMAJOR REPAIR, CORROSION ON SEAT TRACK Y0 BTW FR79 AND FR80/82 NEW SEAT TRACK SECTION Y0 BTW FR79-FR80 HAS BEEN INSTALLED IAW SRM 53-10-16 PARAGRAPH 4 PAGE 204 FIGURE 201 AND SRM 51-40-21.Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025090289057Seat Track · corrodedMAJOR REPAIR, CORROSION ON SEAT TRACK Y794.3 BTW FR 79 AND FR 80- 82, NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 51-40-21 AND SRM 53-10-16 PARAGRAPH 4 FIGURE 201.Aug 21, 2025 · N142UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
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