N303UP
Service difficulty reports · 191
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 = 'N303UP' 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.
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 = 'N303UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IPXA11667138Floor Panel · puncturedPOSITION 5, CTR MAIN DECK FLOOR PANEL HAS A 3" DENT WITH A 2" HOLE. IDENTIFIED PANEL FROM POS 5 CTR PN145T5876-51 IAW EO B767-5320-9693 HAS REPLACEMENT FLOOR PANEL BY CUTTING OUT NEW PANEL FROM A402H AND MARKING INSERT LOC USING EXISTING FLOOR PANEL AS TEMPLASDR IPXA10660831Switch · looseEMERGENCY DECLARED - EICAS MSG "LE SLAT ASYM" L/E LIGHT ILLUM WITH FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. T/S IAW FIM 27-81-00 BLOCKS 1-3 SUB 9, FOUND NR11 SLAT 301 SWITCH TARGET LOOSE IN MT. SECURED TARGET AND BITE CHECK PSEU WITH NO FAULTS. CYSDR IPXA10659938Stringer · misrepairedINSPECTION TYPE:C, FUSELAGE STA524 STR25L EXISTING REPAIR MUST BE REMOVED AND REACCOMPLISHED IAW SRM. GIVEN IN VALIDATION EO B767-5100-36544 APPENDIX B ITEM 1 FX AT BTN BS511.5 & 532.5 STR25L STR REPAIRED IAW R53-00-36725 & EO B767-5330-37838, ORG MATL 7075T6 SDR IPXA10659893Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD T/E FLAP MID L/E FAIRING INBD AREA DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5C, FIG 2.SDR IPXA10659901Skin · delaminatedINSPECTION TYPE:C, LT WING INBD AFT FLAP UPPER SURFACE INBD AREA FOUND DELAM. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R REPAIR 4, FIG 201 SH.1.SDR IPXA10659846Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBERGLASS FABRIC PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A (1) FIG 5.SDR IPXA10659809Tee Fitting · corrodedINSPECTION TYPE:C, FUS STA955 LT TEE FITTING FWD LOWER HOLE FOUND CORROSION AT MATING SURFACE AS MARKED. FUSELAGE STA955 REAR SPAR BULKHEAD SIDE FITTING AERA TEE FITTING REPLACED IAW SRM 51-10-02, REV 46 AND INSTALLED IAW EO B767-5350-17922, APPENDIX C.SDR IPXA10659961Support · crackedINSPECTION TYPE:8C, NR 1 PYLON MID SPAR WEB RT SUPPORT CLIP FOUND CRACKED JUST AT NAC STA 285.45 CRACK LENGTH 1" NR 1 PYLON MID SPAR WEB RT SUPPORT CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10659916Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD T/E FLAP MID L/E FAIRING OTBD AREA DELAMINAION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5C, FIG 2.SDR IPXA10659903Support · crackedINSPECTION TYPE:C, LT WING FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR SUPPORT CLIP FOUND CRACKED JUST AT OFSS549. LT WING FIXED FAIRING UPPER SUPORT WEB AFT FRONT SPAR SUPPORT CLIP AT OFSS549 AREA REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.SDR IPXA10659941Support Fitting · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT OTBD ROTARY ACTUATOR OTBD SUPPORT FITTING FWD FLANGE FOUND CRACKED JUST AT OSS648.595. RT WING NR 9 SLAT OTBD ROTARY ACT OTBD SUPPORT FITTING AT OSS648.595 FWD FLANGE CRACKED AREA REPAIRED IAW RS R57-00-36731 & B767-5740-SDR IPXA10659902Support · crackedINSPECTION TYPE:C, RT WING FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR SUPPORT CLIP FOUND CRACKED JUST AT OFSS549. RT WING FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR SUPPORT CLIP AT OFSS549 AREA REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.SDR IPXA10659897Seat Track · corrodedINSPECTION TYPE:C, M/DECK STA 742-786 LBL 77.5" SEAT TRACK FLANGE CORROSION M/D AT BTN STA 709.45-789.75 LBL 77.5" SEAT TRACK REPAIRED IAW SRM 53-00-52-2R9 FIG201, ORG MATL IS BAC1520-2772-7150T77511, BLEND OUT DEPTH 0.019" X 0.75" X 1.25" AT STA 742.5 AND 0.0SDR IPXA10659896Seat Track · corrodedINSPECTION TYPE:C, M/DECK STA742 TO 764 RBL11 SEAT TRACK FLANGE CORROSION M/D AT BTN STA 709.45 & 782.5 RBL 11 SEAT TRACK REPAIRED IAW SRM 53-00-52-2R9, FIG 201, ORG MATL IS BAC1520-2772-7150-T77511, CORROSION BLENDED OUT 0.032" X 1" X 3" AT STA 737.5 RBL 11" SDR IPXA10659875Stiffener · crackedINSPECTION TYPE:C, RT WING FRONT SPAR STIFFENER UPPER AREA FOUND CRACKED JUST AT OFSS532. RT WING FRONT SPAR STIFFENER JUST AT OFSS532 AREA FABRICATED WITH MATL AND10133-2403 7075T6511 EXTRUSION, REPLACED AND INSTALLED IAW RS R57-21-36728 & EO B767-5710-37790SDR IPXA10659833Panel · delaminatedINSPECTION TYPE:C, LT WING NR 5 SPOILER UPPER SURFACE INBD AREA EXISTING REPAIR DELAMINATION. GRAPHITE FABRIC PRE PREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-04 PAR 5A (1) FIG 5.SDR IPXA10659767Fitting · crackedINSPECTION TYPE:C, RT WING INBD FLAP INBD HINGE FTG FLANGE AREA FOUND CRACKED. RT WING INBD MAIN FLAP HINGE FTG AT IFS179.75 REPAIRED IAW SRM 57-53-02-2R1, FIG 201, ORG MATL IS 7075T73 FORGING, CRK LENGTH AT INBD FLANGE IS 0.875" AND OTBD FLANGE IS 1" DAMAGEDSDR IPXA10659937Attach Fitting · crackedINSPECTION TYPE:C, FUS MEC COMPT STA 246 FLOORBEAM ATT CLIP FOUND CRACKED AT RBL10". FUS MEC COMPT STA 246 FLOORBEAM ATT CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.SDR IPXA10659894Longeron Splice · wornINSPECTION TYPE:C, FUSELAGE SECTION 45 RT STA955 REAR SPAR BULKHEAD FITTING HOLE WORN AT LONGERON SPLICE AREA. FUSELAGE SECTION 45 RT STA955 REAR SPAR BULKHEAD FITTING LONGERON SPLICE HOLE WORN AREA REPAIRED IAW RS R53-50-36729 & EO B767-5310-37821. ORG MATL SDR IPXA10659880Floor Panel · groovedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND DEEP AND LONG GROOVE RUN THROUGH AT BS 985 TO 1087 LBL 77" TO LBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659878Floor Panel · groovedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND DEEP AND LONG GROOVE RUN THROUGH AT BS 764 TO 873 LBL 77" TO LBL 88". FLOOR PANEL FABRICATE IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659845Floor Panel · groovedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND DEEP AND LONG GROOVE RUN THROUGH WITH PUNCTURE HOLE AT BS 873 TO 933 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659844Floor Panel · groovedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND DEEP AND LONG GROOVE RUN THROUGH WITH PUNCTURE HOLE AT BS 933 TO 985 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659817Failsafe · crackedINSPECTION TYPE:C, CRACKS WERE FOUND AT BS 955 BULKHEAD RT SIDE LOWER BOLT HOLE AT FAIL SAFE STRAP RUNNING 4 AND 9 O'CLOCK POSITION WITH THROUGH THICKNESS INDICATION. FUSELAGE STA 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP REPAIRED IAW UPS EO B767-53SDR IPXA10659816Failsafe · crackedINSP TYPE:C, CRACKS WERE FOUND AT BS 955 BULKHEAD LT SIDE AT LOWER BOLT HOLE OF FAIL SAFE STRAP CRACK RUNNING FWD & AFT WITH THROUGH THICKNESS INDICATION. FUSELAGE STA 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP REPAIRED IAWUPS EO B767-5350-17922 APPESDR IPXA10659814Floor Panel · groovedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND DEEP AND LONG GROOVE RUN THROUGH AT BS 1087 TO 1197+22 LBL77" TO LBL88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01SDR IPXA10659813Panel · groovedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND DEEP AND LONG GROOVE RUN THROUGH AT STN1197+22 TO 1207 LBL77" TO LBL88". FLOOR PANEL FABRICATED AS IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659811Floor Panel · groovedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND DEEP AND LONG GROOVE RUN THROUGH AT STN 1207 TO 1351 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659810Tee Fitting · crackedINSPECTION TYPE:C, CRACK WAS FOUND AT BS 955 BULKHEAD TEE FITTING LOWER BOLT HOLE OTBD SURFACE RUNNING 7 O'CLOCK WITH .0652" DEPTH APPROX BS 955 REAR SPAR BULKHEAD SIDE FITTING AREA TEE FITTING REPLACED IAW SRM 51-10-02, REV 46. AND INSTALLED IAW UPS EO B767-SDR IPXA10659798Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT L/E OTBD NOSE SKIN AT OSS792.5 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.1" DAMAGED CUTOUT IS 8.875" X 7" SDR IPXA10659793Skin · crackedINSPECTION TYPE:C, LT WING NR4 SLAT L/E INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/E INBD NOSE SKIN AT OSS572.5 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG, 201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.11" DAMAGED CUTOUT IS 8.875" X SDR IPXA10659940Skin · misrepairedINSPECTION TYPE:C SURVEY SEQUENCE NR 303-F1-04 FUSELAGE SKIN AT BETWEEN STA 1600 TO STA 1623 AND STR34L - 36L AREA EXISTING REPAIR WAS FOUND AND DOES NOT CORRELATED TO A SRM. SURVEY SEQ NR 303-F1-04 FX SKIN AT BTN STA1600-1623 & STR34L-36L AREA REPAIRED IAW RSDR IPXA10659895Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQUENCE NO 303-F1-09 FUSELAGE SKIN AT BETWEEN STA 434-453 AND S25R - 26R AREA EXISTING REPAIR PATCH WAS FOUND AND DOES NOT CORRELATE TO A SRM. SURVEY SEQ NO 303-F1-09 FX SKIN AT BTN STA434-453 & STR25R-26R AREA SKIN REPAIRED IAW RS SDR IPXA10659879Floor Panel · puncturedINSPECTION TYPE:C, DMI D423102 HOLE REPAIR MCD POS 7, RT 25 INCHES FROM AFT EDGE & 4.5" INBD LT SIDE. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659877Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE HOLE 2" X 2.5" AT BS 985 TO 1087 RBL 77" TO RBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659869Floor Panel · groovedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND LONG AND DEEP GROOVE RUN THROUGH THE PANEL AT BS 540 TO 654+22 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659868Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 3 PUNCTURE HOLES 1.75" X 1.5" AND 1" X 1.25" AT BS 412 TO 540 LBL 11" TO RBL 11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED AMM 53-01-01.SDR IPXA10659867Floor Panel · gougedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND LONG DEEP GOUGE AND TEAR AT BS 412 TO 540 RBL 55" TO RBL 77". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659866Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE HOLE 1.5" X 2.5" AT BS 412 TO 540 RBL 33" TO RBL 55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659865Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 2 PUNCTURE HOLE 1.2" X 1.5" AND 1.2" X 1.8" AT BS 1480 TO 1598 RBL 33" TO RBL 55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659864Floor Panel · groovedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND LONG AND DEEP GROOVE RUN THROUGH THE PANEL AT BS 690 TO 764 LBL 77" TO LBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659863Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE HOLE 1.5" X 1.75" AT STN1480 TO 1598 LBL33" TO LBL55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659843Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE HOLE 1.5" X 2" AT BS 764 TO 873 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659842Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND (2) PUNCTURE HOLES 1.5" X 2" AND 1.75" X 2" AT BS 873 TO 935 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659841Floor Panel · groovedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND LONG AND DEEP GROOVE RUN THROUGH THE PANEL AT BS 654+22 TO 690 LBL 77 OT LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659818Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE HOLE 1.5" X 1.75" AT STN731 TO 833 RBL33" TO RBL55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659815Failsafe · crackedINSPECTION TYPE:C, BS 955 WL 200 SUSPECTED CRACK INDICATIONS WERE FOUND AT BOTH LT AND RT OF BS 955 FAILSAFE STRAP. FUSELAGE BS 955 REAR SPAR BULKHEAD SIDE FITTINGS FAILSAFE STRAPS REPAIRED IAW UPS EO B767-5350-17922 APPENDIX C & D.SDR IPXA10659812Floor Panel · puncturedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE HOLE 1.2" X 1.5" AT BS 1351 TO 1480 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659797Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT L/E INBD NOSE SKIN AT OSS723.9 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.13" DAMAGED CUTOUT IS 8.875" X 7"SDR IPXA10659796Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT OTBD SE SKIN RIVET HOLE FOUND CRACKED RT WING NR9 SLAT L/E OTBD NOSE SKIN AT OSS641.9 AREA SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH IS 0.2" DAMAGED CUTOUT IS 8.875" X 7.125"
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