N314UP
Service difficulty reports · 137
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 = 'N314UP' 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 = 'N314UP' 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 IPXA2017051617193Floorboard · damagedFLOORBOARD AT POS 2/3 LBL 49 DAMAGED. REMOVED THE FLOORBOARD. MAJOR REPAIR. FABRICATED A NEW FLOORBOARD.SDR IPXA2017051617170Floor Panel · wornMAIN CABIN FLOOR PANEL WORN BY BALL MAT ROLLER HOUSING. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I.SDR IPXA2017051617169Floor Panel · wornFLOOR PANEL WORN THROUGH BY BALL MAT ROLLER HOUSINGS. FABRICATE A NEW FLOOR PANEL IAWEO B767-5320-9693-1SDR IPXA2017051417084Floor Panel · puncturedMAIN CARGO DECK FLOOR PANEL POSITION 3L PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I.SDR IPXA2017051417083Floorboard · damagedMAIN CARGO DECK FLOORBOARD POSITION 3L HAS MULTIPLE AREAS OF DAMAGE. MANUFACTURED A NEW FLOORBOARD IAW EO B767-5320-9693-I, APPX B.SDR IPXA2017051417081Floorboard · dentedMAIN CAGRO DECK FLOORBOARD, POSITION 3L HAS MULTIPLE DENTS. MANUFACTURED A NEW FLOORBOARD IAW EO B767-5320-9693-I, APPX B.SDR IPXA2017032615521Floor Panel · damagedFLOOR PANEL IS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I.SDR IPXA2016121511757Warning Light · false activationNO LANDING RECEIVED A RT THRUST REVERSER ISOLATION VALVE EICAS MESSAGE. TROUBLESHOT IAW FIM 78-34-00-990-813. NO FAULTS FOUND. SYSTEM TESTED IAW AMM 78-31-00 FOUND OPS NORMAL.SDR IPXA2016072206155Transceiver · malfunctionedRIGHT HF WOULD NOT RECEIVE. PERFORMED AN AIR TURNBACK BEFORE ETOPS ENTRY POINT. RERACKED THE RT HF TRANSCEIVER IAW MM 23-11-03-401. OPS TEST PASSED IAW MM 23-11-00-501-2.SDR IPXA2015082092529Skin · crackedINSPECTION TYPE:C10, CRACK INDICATION WAS FOUND ON RT WING LOWER SKIN, FASTENER HOLE AT STR L-9.5, NEAR WING STA 995. REPAIR IAW SR 3-3334851482 AND EO B767-5730-58408-A.SDR IPXA2015081992501Floor Panel · crackedINSPECTION TYPE:C10, FOUND CRACK ON CARGO FLOOR PANEL, 242VFF AT BS 985-BS 1087, RBL 78-RBL 88. FABRICATED THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.SDR IPXA2015082092530Stiffener · crackedINSPECTION TYPE:C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9 , LBL 11. REPAIR IAW SRM 57-10-10, REPAIR 2, REV 63 , SRID:3-3334935982 AND EO: B767-5710-58407-A.SDR IPXA2015082092528Stiffener · crackedINSPECTION TYPE:C10, CRACK ON THE CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, RBL 11. REPAIR IAW SRM 57-10-10, REPAIR 2, REV.63 , SRID:3-3334935982 AND EO: B767-5710-58407-A.SDR IPXA2015071491128Light · crackedEMERGENCY EXIT LIGHT CASE NEAR ENTRY DOOR CAME OUT OF WALL MOUNT. EMERGENCY EXIT LIGHT WORKS. REPAIRED IAW EO B767-2510-58066-A.SDR IPXA2014112684945Unknown · odorDURING CLIMBOUT, ODOR LIKE BURNED FOOD. SUSPECT RT ENGINE BIRDSTRIKE SINCE ONLY HAD ODOR IF RIGHT PACK WAS ON AND ONLY FOR A FEW MINUTES. RT FAN VIBRATION WAS 3.5 IN CLIMB. ALL OTHER INDICATIONS NORMAL. INSPECTON IAW FIM 71-05-00-815-872-H01 SHOWS ENGINE SDR IPXA2014090284150Battery Pack · inoperativeEMERGENCY LIGHTS INADVERTANTLY IN THE ARMED WITH SHIPS POWER. R & R EMERGENCY BATTERY IAW AMM 33-51-07-022-001 AND 33-51-07-422-012. OPS CK GOOD.SDR IPXA2014051282927Radome · damagedNOSE RADOME DAMAGED DUE TO BIRD STRIKE DURING LANDING. R & R RADOME IAW AMM 53-12-01-902-038 AND AMM 53-12-01-402-059.SDR IPXA2014021081839Switch · failedEMERGENCY LIGHTS FAILED TEST, FOUND SWITCH BAD. R & R EMERGENCY CONTROL PANEL IAW AMM 33-51-08-401. OPS CHECKED GOOD.SDR IPXA3677672Unknown · odorINSPECTION TYPE:ETOP ELECTRICAL BURNING ODOR NOTED IN FLIGHT. BOTH PACKS RUNNING. ODOR DISSIPATED THEN NOTICED MORE STRONGLY UPON BLOCK IN. AFTER BLOCK IN, ODOR WAS STRONGER IN AFT RT TUNNEL OF E/E BAY. COULD NOT PIN POINT SOURCE. RAN BOTH ENGINES, PACKS. APSDR IPXA12675819Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL AT POS NR 6L HAS 1" HOLE. REPAIRED IAW SRM 53-00-50-2R.SDR IPXA2673114Skin · puncturedLT FUSELAGE SKIN PUNCTURE AT STA 1919 TOP OF FUSELAGE LBL 4. HOLE IS . 95". REPAIRED IAW EO B767-5330-46446-B.SDR IPXA2672447Skin · damagedFUSELAGE CROWN IS DAMAGED JUST FORWARD OF APU EXHAUST. REPAIRED IAW EO B767-5330-46446-A.SDR IPXA11669993Failsafe · unknownINSPECTION TYPE:8C INSTALLED A PROTECTIVE SHIM BETWEEN THE SKIN AND THE FAILSAFE STRAP ON RT SIDE IAW EO B767-5350-17922-J APPENDIX 'D' FIG 6, REPAIR IS CLASSIFIED AS A MAJOR.SDR IPXA11669791Battery Pack · inoperativeINSPECTION TYPE:8C, EMERGENCY LIGHTS DID NOT STAY FOR 15 MINUTES. EMERGENCY LIGHTS BATTERY PACK REPLACED AND OPS TEST CARRIED OUT NORMAL. REF AMM 33-51-07.SDR IPXA11669994Tee Fitting · corrodedINSPECTION TYPE:8C, FRETTING FOUND AT TEE FITTING FWD LOWER HOLE MATING SURFACE AREA, TEE FITTING REPLACED IAW EO B767-5350-17922-J, APPENDIX 'D' FIG 6. REPAIR IS CLASSIFIED AS A MAJOR.SDR IPXA11669985Floorbeam · corrodedINSPECTION TYPE:8C, M/D STA 1540 LBL 75.25" TO LBL 78" FLOORBEAM FWD FACE UPPER CHORD FOUND CORROSION. REPAIRED IAW HX RS NR R-53-65-37243 REV A & EO B767-5310-44767-A, ORIGINAL THICKNESS IS 0.150", CORROSION BLENDED OUT AREA IS DEPTH 0.084" X WIDTH 2" X LENGSDR IPXA11669984Floorbeam · corrodedINSPECTION TYPE:8C, M/D STA 1518 LBL 80.75, FLOORBEAM AFT FACE UPPER TEE FOUND CORRODED. REPAIRED IAW HX RS NR R53-65-37241 REV A & EO B767-5310-44765-A, ORIGINAL THICKNESS AT FWD FLANGE IS 0.150" & AFT FLANGE IS 0.180", CORROSION BLENDED OUT AREA AT FWD FLSDR IPXA11669862Floor Panel · damagedINSPECTION TYPE:C, MCD FLOOR PANEL FOUND 2 DAMAGED AND 8 DENTS AT STA 1540 TO STA 1598 LBL 55 TO LBL 80. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.SDR IPXA11669861Floorbeam · corrodedINSPECTION TYPE: C, MAIN DECK BS 1540 RBL 71.25" FLOORBEAM FWD FACE UPPER CHORD FOUND CORROSION. FLOORBEAM REPAIRED IAW RS R53-65-37244, REV A & EO B767-5310-44764-A, ORG MATERIAL IS BAC1506-4177-7075T6511 EXTRUSION, ORG THICKNESS 0.150" CORROSION BLEND OUT SDR IPXA11669821Wedge · delaminatedINSPECTION TYPE: 8C, LT WING OTBD T/E FLAP, T/E WEDGE MID AREA LWR SURFACE DELAMINATION. FIBERGLASS PREPERG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR5 A (1), FIG 9, REV 50.SDR IPXA11669991Tee Fitting · crackedINSPECTION TYPE:8C, FUSELAGE BS 955 LT REAR SPAR BULKHEAD FITTING AREA WAS FOUND 1 EA FASTENER HOLE CRACKED ON 6 O/C POSITION AT TEE FITTING APPROX .1250" IN LENGTH. TEE FITTING REPLACED IAW EO NR B767-5350-17922-J APPENDIX 'C', FIG 6, CRACK APPROX .1250" IN SDR IPXA11669989Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING WAS FOUND 1EA FASTENER HOLE CRACKED AT FAILSAFE STRAP ON 2 O/C AND 4 O/C POSITION THROUGH THICKNESS AND .1250" IN LENGTH. REPAIRED IAW EO B767-5350-17922-J APPENDIX 'C', REPAIR IS CLASSISDR IPXA11669992Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE RT BS 955 FAILSAFE STRAP FOUND CRACKED. REPAIRED IAW EO B767-5350-17922-J APPENDIX 'D'. REPAIR IS CLASSIFIED AS A MAJOR.SDR IPXA11669990Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING FAILSAFE STRAP AREA CRACK FOUND, REMOVE FASTENER FOR NDT CONFIRMATION. R & R IAW EO B767-5350-17922-J APPENDIX 'D' FIG 6. REPAIR IS CLASSIFIED AS A MAJOR.SDR IPXA11669988Failsafe · crackedINSPECTION TYPE:8C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING FAILSAFE STRAP AREA, CRACK FOUND, REMOVE FASTENER FOR NDT CONFIRMATION. REMOVED AND REINSTALLED IAW EO NR B767-5350-17922-J APPENDIX 'C' FIG 6. REPAIR IS CLASSIFIED AS A MAJOR.SDR IPXA1668634Floorboard · damagedFLOORBOARD DAMAGED FED OF MAIN CARGO DOOR. FABRICATED IAW EO B767-5320-9693-H.SDR IPXA1668633Floorboard · damagedFLOORBOARD DAMAGED AFT OF MAIN CARGO DOOR LT SIDE. FABRICATED IAW EO.SDR IPXA11667535Floor Panel · damagedNUMEROUS HOLES IN MAIN CARGO FLOOR PANEL, POS 2L, JUST FWD OF MAIN CARGO DOOR OPENING. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.SDR IPXA10663155Compressor · stalledINSPECTION TYPE:ETOP, RT ENGINE HAD 4 COMPRESSOR STALLS AT 200 FT, NO HIGH EGT OR ENGINE EXCEEDENCE. CHECKLIST WAS ACCOMPLISHED, TRIED ONE MORE RECOVERY, HOWEVER ENGINE STALLED AGAIN. ENGINE WAS SHUTDOWN, LANDING WEIGHT WAS 320.00. R & R ENGINE.SDR IPXA10662886Pressure Switch · inoperativeE-TOP DIVERSION LT ENGINE ANTI-ICE DISPLAYED AND ENGINE ANTI ICE VALVE REMAINED ILLUMINATED WITH SWITCH ON. REPLACED LT ENG ANTI ICE VALVE IAW MM 30-21-03-4 AND THERM A/I PRESS SWITCH IAW MM 30-21-04-4. OPS CHECK NORMAL.SDR IPXA10662654Floor Panel · damagedD424528 MAIN CARGO POS 4 L FLOOR PANEL 2ND FR PM OTBD HAS .5" HOLE. REMOVED AND MFG NEW FLOOR PANEL IAW B767-5320-9693G.SDR IPXA10662653Floor Panel · damagedD424529 MAIN CARGO POS 5 L FLOOR PANEL 2ND FROM OTBD HAS .5" HOLE. REMOVED AND MFG NEW FLOOR PANEL IAW B767-5320-9693G.SDR IPXA10658126Floor Support · crackedSTA 246 CABIN FLOOR STRUCTURE ATT CLIP FOUND CRACKED JUST AT RBL10". AV COMPT STA 246 CABIN FLOOR STRUCTURE ATTACH CLIP AT RBL10" REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45.SDR IPXA10658113Skin · misrepairedSURVEY SEQUENCE NR 314-F1-06 BULK CARGO DOOR FWD LWR STA1423.5 TO 1431 THE EXISTING REPAIR DOES NOT CORRELATED TO A SRM DUE NO CUTOUT FOUND. FX SURVEY SEQUENCE NR 314-F1-06 BULK CARGO DOOR FWD LWR EDGE AT STA 1423.5 TO 1431 AREA SKIN REPAIRED IAW RS R52-36-36SDR IPXA10658112Skin · misrepairedFX - SURVEY SEQUENCE NR 314-F1-04 STA382 TO 398 BETWEEN STR33L TO 35L THE EXISTING REPAIR NOT CORRELATE TO SRM DUE TOO CLOSE OF 314-F1-03 EXISTING REPAIR DOUBLER. FX SURVEY SEQUENCE NR 314-F1-04 STA382 TO 398 BTN STR33L-35L SKIN REPAIRED IAW RS R53-11-36575 OSDR IPXA10658111Skin · misrepairedSURVEY SEQUENCE NR 314-F1-03 STA 362 TO 374 BETWEEN STR31L AND 33L EXISTING REPAIR NOT CORRELATED TO SRM DUE TOO CLOSE OF 314-F1-04 EXISTING REPAIR DOUBLER. FX SURVEY SEQUENCE NR 314-F1-03 STA362 TO 374 BTN STR31L-33L SKIN REPAIRED IAW RS R53-11-36575 ORG MATSDR IPXA10658109Spar · crackedRT WING L/E LES675 FIXED FAIRING SUPPORT RIB AFT FRONT SPAR ANGLE FOUND CRACKED. RT WING L/E LES675 FIXED FAIRING SUPPORT RIB AFT FRONT SPAR ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 45.SDR IPXA10658082Skin · delaminatedINSPECTION TYPE:SPV-RT WING INBD AFT FLAP LOWER SURFACE INBD T/E FOUND DELAMINATED ON THE EXISTING REPAIR PATCH OTBD EDGE. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10 REPAIR 4, FIG 202, SHEET 1 REV 45.SDR IPXA10658081Support Fitting · crackedINSPECTION TYPE:SPV-RT WING INBD MAIN FLAP, INBD AFT FLAP SUPPORT FITTING FOUND CRACKED. RT INBD MAIN FLAP AFT FLAP SUPPORT FITTING REPAIRED IAW SRM 57-53-02-2R1 FIG201, REV45. INBD FLANGE CRACK LENGTH 1.25". OTBD FLANGE CRACK LENGTH 1.5" BOTH INBD & OTBD CUSDR IPXA10658074Attach Fitting · crackedINSPECTION TYPE:C-AFT CARGO STA 1087 FWD PARTITION BELOW FLOOR LBL 25 CLIP FOUND CRACKED. AFT CARGO STA 1087 LBL 25 FWD PARTITION BELOW FLOOR ATTACH CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV45.
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