N326UP
Service difficulty reports · 146
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 = 'N326UP' 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 = 'N326UP' 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 IPXA10659128Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A, FIG 5, REV 46.SDR IPXA10659126Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03, PAR 5A (1) FIG 5, REV 46.SDR IPXA10659125Fairing · delaminatedINSPECTION TYPE:C RT WING OTBD T/E FLAP L/E MID FAIRING DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR5A (1) FIG 5, REV 46.SDR IPXA10659124Wedge · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP, T/E WEDGE LWR SURFACE MID AREA DELAMINATION . COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-06 PAR 5A (1) FIG 9. REV 46.SDR IPXA10659163Skin · misrepairedINSP TYPE:C, SURVEY SEQUENCE NR 326-F1-06 FUSELAGE BETWEEN BS 604 TO BS 628 STR 1R TO STR 4R EXISTING REPAIR WAS FOUND. BETWEEN BS604-628 STR1R-4R SKIN IAW R53-31-36683A MAT'L 2024T3 SKIN 0.093"-0.056" AT CUTOUT AREA WITH CUTOUT SIZE 4.18"X5.5". MAJOR REPAIRSDR IPXA10659157Skin · delaminatedINSP TYPE:C, LT OTBD ELEVATOR UPPER SKIN PANEL INBD AFT CORNER DELAMINATION COMPOSITE WET LAY UP. REPAIR CARRIED OUT IAW EO B767-5520-37266-A REFER RS R55-20-36688, REV A.SDR IPXA10659155Spar · crackedINSPECTION TYPE:6C, LT WING L/E LES675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP FOUND CRACK. LT WIING L/E LES675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.SDR IPXA10659145Attach Fitting · crackedINSPECTION TYPE:C AFT CARGO COMPT STA1087 BELOW FLOOR ATT CLIP FOUND CRACKED AT LBL25". AFT CARGO COMPT STA1087 LBL25" BELOW FLOOR ATT CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 46.SDR IPXA10659144Attach Fitting · crackedINSPECTION TYPE:C, AFT CARGO COMPT STA1087 BELOW FLOOR ATT CLIP FOUND CRACKED AT RBL25". AFT CARGO COMPT STA1087 RBL25" BELOW FLOOR ATT CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.SDR IPXA10659123Panel · crackedINSP TYPE:C EMP - LT INBD ELEVATOR T/E AREA CRACK COMPOSITE WET LAY UP. REPAIR CARRIED OUT IAW RS R55-23-36680 REV A.SDR IPXA10659090Floor Panel · gougedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND DEEP AND LONG GOUGE AT STN 731 TO STN 833. RBL 11" TO RBL 33". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659041Hinge · crackedINSPECTION TYPE:C, LT WING INBD MAIN FLAP INBD HINGE FTG FOUND CRACKED LT WING INBD MAIN FLAP INBD HINGE FTG AT IFS 179.75 AREA REPAIRED IAW SRM 57-53-02-2R1, FIG 201. ORG MATL IS FORGING 7075T3 CRK LENGTH IS 1.12" AT INBD FLANGE 0.9" AT OTBD FLANGE DAMAGED CUSDR IPXA10659040Skin · crackedINSPECTION TYPE:C, LTW NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING NR 3 SLAT INBD AREA AT OSS723.9 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.12" DAMAGED CUTOUT IS 8.875" X 7.125" THIS REPASDR IPXA10659039Structure · crackedINSP TYPE:C, LT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT INBD AREA AT OSS572.5 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201. ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.12" DAMAGED CUTOUT IS 8.875" X 7.375" THIS REPAIR ISDR IPXA10659038Structure · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT OTBD AREA AT OSS641.9 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.13" DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPSDR IPXA10659037Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT INBD NOSE SKIN RIVET HOLD FOUND CRACKED. RT WING NR 9 SLAT INBD AREA AT OSS572.5 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.12" DAMAGED CUTOUT IS 8.875" X 7.3" THIS REPASDR IPXA10659036Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT OTBD AREA AT OSS641.9. NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201 ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.16" DAMAGED CUTOUT IS 8.875" X 7.25" THIS RESDR IPXA10659034Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR10 SLAT OTBD AREA AT OSS792.5 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG201. ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.12" DAMAGED CUTOUT IS 8.875" X 7" THIS REPAISDR IPXA10659160Skin · misrepairedINSP TYPE:C, SURVEY SEQUENCE NR 326-F1-02 BULK CARGO DOOR AT BETWEEN STA 1430-1439 STR 26L-27L AREA EXISTING REPAIR DOES NOT CORRELATE TO A SRM. BETWEEN STA 1426-1456 STR 25L-28L AREA SKIN REPAIRED RS R52-00-36681A ORG MAT'L IS 2024T3 .050" CHEM-MILLED SKIN.SDR IPXA10659156Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQUENCE NR 326-F1-01 FUSELAGE BETWEEN BS443-461 & S22R-26R EXISTING REPAIR DOES NOT CORRELATE TO A SRM. SURVEY SEQ NR 326-F1-01 FX BTN BS443-461 & STR22R-26R EXISTING REPAIR ADD FASTENERS ARE ADDED AND INSTALLED COMMON TO REPAIR DOSDR IPXA10659143Floorbeam · crackedINSPECTION TYPE:C FX STA246 MAIN DECK FLOORBEAM ATT CLIP FOUND CRACK AT RBL10". FX STA 246 MAIN DECK FLOORBEAM ATT CLIP AT RBL10" AREA REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 46.SDR IPXA10659142Floorbeam · crackedINSPECTION TYPE:C, AFT BULK CARGO COMPT MAIN DECK FLOORBEAM ATT ANGLE FOUND CRACK AT STA1581 LBL70". AFT BULK CARGO COMPT MAIN DECK FLOORBEAM ATT ANGLE REPLACED AND INSTALLED AT STA1581 LBL70" IAW SRM 51-10-02 AND 51-40-02, REV 46.SDR IPXA10659139Floorbeam · crackedINSP TYPE:6C, AFT BULK CARGO COMPT MAIN DECK FLOORBEAM ATT ANGLE FOUND CRACKED AT STA 1581, RBL70". AFT BULK CARGO COMPT MAIN DECK FLOORBEAM ATT ANGLE REPLACED AND INSTALLED AT STA 1581 RBL 70" IAW SRM 51-10-02 AND 51-40-02 REV46.SDR IPXA10659115Stiffener · crackedINSPECTION TYPE:C WING CTR SECTION FRONT SPAR VERTICAL STIFFENER FOUND CRACKED JUST AT STA785.9 RBL10.94. WING CTR SECT FRONT SPAR AT STA785.9 RBL10.94 VERT STIFFENER REPAIRED IAW RS R57-00-36677 ORG MATL IS BAC1518-749-2024T3511 CRK LENGTH IS 3" CUT OFF LENGSDR IPXA10659101Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 1041 TO STN 1114, RBL 33" TO RBL 55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALL IAW AMM 53-01-01.SDR IPXA10659100Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 540 TO STN 654+22, LBL 11" TO RBL 11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALL IAW AMM 53-01-01.SDR IPXA10659099Floor Panel · gougedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND DEEP GOUGE MARKS AT STN 540 TO STN 654+22, RBL 33" TO RBL 55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALL IAW AMM 53-01-01.SDR IPXA10659098Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 1344 TO STN 1425, RBL 55" TO RBL 77". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659097Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND SEVERAL PUNCTURES AT STN 1370 TO STN 1480, RBL 77" TO RBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALL IAW AMM 53-01-01.SDR IPXA10659091Floor Panel · puncturedINSP TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 833 TO STN 930, LBL 11" TO RBL 11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659083Floor Panel · puncturedINSPECTION TYPE:6C MCD FLOOR PANEL FOUND PUNTURED AT STN 833 TO STN 930, LBL 33" TO LBL 55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659082Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 932 TO STA 985, RBL 77" TO RBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10659035Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACK RT WING NR 10 SLAT INBD AREA AT OSS723.9 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201. ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.14" DAMAGED CUTOUT IS 8.875" X 7.125". THISSDR IPXA09656634Floor Panel · damagedINSPECTION TYPE:N/A FLOORBOARD DAMAGED. FABRICATED FLOOR IAW EO B767-5320-9693.SDR IPXA09656602Floor Panel · puncturedINSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PNL AT POS 10L .5 INCH PUNCTURE. REPAIR PER EO B767-5320-34205-A.SDR IPXA09654967Floor Panel · crackedINSPECTION TYPE:N/A MCD POS NR 8 PANEL CRACKED. CRACK RUNS FROM EDGE TO EDGE. REPAIRED PER EO B767-5320-9693-E.SDR UPS08651708Actuator · leakingINSPECTION TYPE:N/A DIVERSION - LEFT HYD QTY DECREASED TO ZERO AND SYSTEM PRESSURE AND QTY LIGHTS ILLUM, EICAS MSG LEFT HYD SYSTEM PRESS AND LEFT HYD QTY DISPLAYED. COMPLIED WITH QRH PROCEDURES. SERVICED LEFT HYD AND FOUND NR 6 SPOILER ACTUATOR LEAKING. REMSDR UPS08651693Cap · crackedINSPECTION TYPE:N/A ATB - COMPLETE LEFT HYD SYSTEM QTY LOST. AT BLOCK, FLUID REMAINING 0.06. FOUND NR 6 SPOILER ACTUATOR FILTER HOUSING CAP TO BE CRACKED AND LEAKING. INSTALLED INTERIM FITTING AND CAP PER EO B767-2760-28637A. ENTERED IN DMI LOG AS D369563.SDR UPS07650170Oil System · overtempINSPECTION TYPE:ETOP IFSD - LT ENGINE HIGH OIL TEMP IN AMBER A/C IS OOS TAC = 25693; TAT = 5073; ET = 22841; TEC = 6814; TSLV/TSR = 1123. [07-25-07] ALL CHECKS FOUND NORMAL. R & R LT ENG EEC PER AMM 72-21-15-4. ACCOMPLISHED LT ENGINE ADJUSTMENT IAW 71-00-0SDR UPS06646923Skin Panel · brokenTAIL COMPARTMENT RT BS 1788.375, LWR SIDE OF STAB CUTOUT, SKIN PANEL IS BROKEN. REPAIRED PER ERO NR 06-2047.SDR UPS05643639Life Raft · activatedFOUND LIFE RAFT S/N Q47, SELF INFLATED IN STOWAGE CONTAINER. DEFERRED D25-62-1-2 WAITING FOR CLOSING LOG PAGE. LIFE RAFT REMOVED FROM A/C. REPLACED LIFE RAFT, ETOIS SIGN OFF REQUIRED THIS CLEARS DFRL M294789.SDR UPS04643023Control Cable · chafedINSPECTION TYPE: ETOP, RUDDER CONTROL CABLE RB IS MISROUTED AND IS CHAFING AGAINST PULLEY SUPPORT BRACKET AT BS 240, LBL 5, WL 199. REMOVED, INSPECTED TO BE IN SERVICEABLE CONDITION, PROPERLY ROUTED / INSTALLED, RIGGED AND FUNCTIONAL TESTED GOOD.SDR UPS04641796Rib · crackedRIGHT INBOARD TRAILING EDGE FLAP OUTBOARD CLOSURE RIB CRACK. ACCOMPLISHED PERMANENT REPAIR PER EO B767-5750-19900B THIS CLEARS D275 213. REFERENCE LP604020.SDR UPS01635281Window · crackedINSPECTION TYPE:PFLT ON PREFLIGHT WHEN TURNING ON WINDOW HEAT RIGHT SIDE WINDOW CRACKED AND RIGHT SIDE WINDOW HEAT INOP EICAS MESSAGE DISPLAYED. *S/D* REMOVED AND REPLACED THE RT NR 2 WINDOW.SDR UPS00632984Warning Light · intermittentINSPECTION TYPE:N/A, RT ENG INTERMITTENT ENGINE FIRE INDICATION (2 VERY QUICK) ALL OTHER INDICATIONS NORMAL. CHECKED PWER FIM 26-11-00. PERFORMED RESISTANCE CHECK, FOUND CIRCUITS WITHIN LIMITS. CHECKED WIRING AND FIRE LOOPS AT RT ENGINE, NO FAULTS FOUND. SSDR UPS99629479Bulb · failedEXTERIOR EMERGENCY ESCAPE LIGHT BELOW CREW ENTRY DOOR INOP. RELAMPED EXTERIOR ESCAPE LIGHT. OPS CHECK GOOD.
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