N306UP
Service difficulty reports · 127
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 = 'N306UP' 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 = 'N306UP' 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 IPXA2018070731453Warning System · false activationLEFT SIDE WINDOW EICAS MSG.C/O TECH RECOMMENDATION ALERT H182251, LEFT SIDE WINDOW EICAS MSG, NO PHYSICAL BURNS NOR DAMAGE NOTED ON L2 AND L3 WINDOW. PERFORMED OPS CHECK PER AMM 30-41-00-715-001, NO ABNORMALITIES FOUND. AS PER PRE-CAUTIONARY R&R WHCU PER MM 30SDR IPXA2017121324495Unknown · noneINSPECTION TYPE:N/ADIV - DECENDING THROUGH 20000 FT INTO UIO HEARD A LOUD BANG. LEVELED OFF AT 18000 FT TO COMENCE APPROACH SELECTED FLAPS ONE AND HEARD ANOTHER BANG. DISCONECTED AUTOPILOT SUSPECTING A CARGO SHIFT. DIVERTED GYE AND LANDS A WITH 13 UNITS OF TRISDR IPXA2017040615867Skin · dentedINSPECTION TYPE: C11, DENTS ON THE RT WING INBD AFT FLAP LOWER SKIN AT IFS 194.75. REPAIRED IAW SRM 57-53-01, REPAIR 1, SRM 51-70-10, REPAIR 4, AND SRM 51-70-10, REPAIR GENERAL, REV 67.SDR IPXA2017040615866Skin · dentedINSPECTION TYPE: C11, DENTS ON THE RT WING INBD AFT FLAP LOWER SKIN AT IFS 145.25. REPAIRED IAW SRM 57-53-01, REPAIR 1, SRM 51-70-10, REPAIR 4, AND SRM 51-70-10, REPAIR GENERAL, REV 67.SDR IPXA2017040615865Skin · dentedINSPECTION TYPE: C11, DENTS ON THE RT WING INBD AFT FLAP LOWER SKIN. REPAIRED IAW SRM 57-53-01, REPAIR 1, SRM 51-70-10, REPAIR 3 & 4, AND SRM 51-70-10, REPAIR GENERAL, REV.67.SDR IPXA2017040615864Skin · dentedINSPECTION TYPE: C11, DENTS ON RT WING INBD AFT FLAP LOWER SKIN. REPAIRED IAW SRM 57-53-01, REPAIR 1, SRM 51-70-10, REPAIR 4, AND SRM 51-70-10, REPAIR GENERAL, REV 67.SDR IPXA2017031715269Seal Depressor · dentedMAIN CARGO DOOR SILL AFT SEAL DEPRESSOR DENTED. ABOUT 12 INCHES AFT, UPPER CORNER. DAMAGED AREA REPAIRED IAW EO B767-5230-08088-1.SDR IPXA2016072706377Computer · malfunctionedATB - RUDDER RATION EICAS AT 400' ILLUMINATED THROUGHOUT FLIGHT. AILERON LOCKOUT EICAS AT 400' ILLUMINATED THROUGHOUT FLIGHT. R & R C FCC IAW MM 22-11-1. OPS NORMAL. R & R L ADC IAW MM 34-12-01. OPS NORMAL.SDR IPXA2016071205776Case · crackedPBE CASE CRACKED. REPLACED THE PBE.SDR IPXA2015081392320Pressure Switch · inoperative"C HYD SYS PRESSURE" ALERT AND ASSOCIATED"SYS PRESSURE" LIGHT ILLUMUNATED ON CLIMBOUT AFTER SELECTING ADP PUMP OFF IAW MEL TURNED ADP BACK TO "ON" POSITION IAW QRH PROCEDURE. EICAS MSG AND PRESSURE LIGHT REMAINED. R & R CENTER SYSTEM PRESSURE TRANSMITTER IAWSDR IPXA2015080992176Floor Panel · damagedMCD FLOOR PANEL POS 11-L DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320=9693-H.SDR IPXA2015040887844Stiffener · crackedINSPECTION TYPE:C10, CRACK ON THE CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT STA 785.9, RBL 11. REPAIR IAW SRM 57-10-10, REPAIR 2, REV 61, SRID: 4-2866088213 AND EO: B767-5710-57147-A.SDR IPXA2015040587714Floor Panel · crackedINSPECTION TYPE:C10, FOUND CRACK ON M/D CARGO FLOOR PANEL, 241MFF, AT STA 955, FABRICATE THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.SDR IPXA2014092684399Fire Detector · damagedINSPECTION E, PERFORMED AN AIR TURN BACK DUE TO LT ENGINE FIRE INDICATION. REPLACED UPPER AND LOWER EGT THERMAL COUPLE CABLE ASSY. R & R DAMAGED 7TH STAGE COOLING AIR TEE. REPLACED DAMAGED FIRE LOOP WIRES AND PERFORMED NR 2 ENGINE FIRE DETECTION LOOP TEST. TSDR IPXA2014091584297Floor Panel · damagedMCD FLOOR PANEL BS 412 HAS DAMAGE. REPAIRED IAW SRM 53-00-50-2R.SDR IPXA2014091584296Floor Panel · damagedFLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50-2R.SDR IPXA2014091584294Floor Panel · cutMAIN CARGO DECK FLOOR PANEL CENTER HAS A ONE INCH CUT UNDER NR 3 LATERAL CAN GUIDE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA13677574Seat Track · corrodedINSPECTION TYPE:C09 FOUND CORROSION ON RBL 88 SEAT TRACK AT BS 522 AND 566. REPAIRED IAW EO NR B767-5310-50212-A.SDR IPXA13677237Floor Panel · damagedHOLE IN FLOOR PANEL POS 9L FWD SECOND FLOOR PANEL FROM OTBD OF MAIN CARGO DECK. FABRICATED NEW FLOOR PANEL REF EO B767-5320-9693-H.SDR IPXA2675472Floor Panel · tornTWO SMALL UPPER SURFACE TEARS ON FLOOR PANEL, POS 8 FWD JUST AFT OF CENTERLINE FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H. TSDR IPXA2673997Fseu · inoperativeFLAP T/E DISAGREE LIGHT AT FLAPS 5 POSITION WHEN RETRACTING AFTER TAKE OFF. HAD TO USE ALTERNAT FLAP SWITCH LAND FLAPS 20. R & R FSEU IN REF TO MM 27-51-01-4. PERFORMED BITE CK IN REF TO FIM 27-51-00. SYS CKS GOOD. FSEU ALSO TESTS GOOD IAW MM 27-51-01-4. OSDR IPXA2673103Floor Panel · puncturedDAMAGED FLOOR PANEL AT POS 2L OTBD. REPAIRED IAW SRM 53-00-50-2R, PARA 4C.SDR IPXA2673102Floor Panel · puncturedDAMAGED FLOOR PANEL POS 4L OTBD. REPAIRED IAW SRM 53-00-50-2R.SDR IPXA2672221Floor Panel · damagedFLOOR PANEL POS 6R HAS HOLE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA2672220Floor Panel · damagedTWO HOLES IN FLOOR PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA2672219Floor Panel · damagedFLOOR PANEL HAS TWO HOLES. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.SDR IPXA2672218Floor Panel · damagedTWO HOLES FLOOR PANEL. FABRICATED FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA2672213Floor Panel · damagedHOLE IN FLOOR PANEL. FABRICATED NEW FLOOR PANEL IAW B767-5320-9693-H.SDR IPXA2672212Floor Panel · damagedDAMAGE IN FLOOR PANEL 145T5876-73 FWD CTR PANEL 6" LEFT OF CTR, FABRICATED PANEL REF EO B767-5020-9693-H.SDR IPXA11670596Skin · dentedRT WING OTBD FLAP T/E WEDGE DENTED. REPAIRED IAW EO B767-5750-44843-B.SDR IPXA1668564Adi · failedAT FLT LEVEL 340, CAPTAINS ADI CRT CB POPPED. SCREEN WENT BLANK FOLLOWED BY AN ELECTRICAL BURNING ODOR. CHECKED EADI CONNECTOR FOR BURN, FOUND OK. REPLACED EADI LT SIDE IAW 34-22-03-4, OPS CHECK COMPLETE.SDR IPXA1666338Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND SEVERAL DENTS AND PUNCTURES AT STA 654+22 TO STA 690 LBL 11 TO RBL 11. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.SDR IPXA1666337Floor Panel · dentedINSPECTION TYPE:C, FLOOR PANEL FOUND SEVERAL DENTS AND PUNCTURES AT STA 930 TO 975 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.SDR IPXA1666380Strap · crackedINSPECTION TYPE: C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING AREA CORROSION CRACK FOUND AT FAILSAFE STRAP FROM 5 O/C TO 7 O/C POSITION APPROX .1250" IN DEPTH FUS BS 955 LT SIDE REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP REPAIR IAW EO B767-5350-17922-H APPSDR IPXA1666379Strap · crackedINSPECTION TYPE:C, FUSELAGE RT BS 955, REAR SPAR BULKHEAD FITTING AREA CRACK FOUND AT FAIL SAFE STRAP ON 4 O/C AND 10 O/C POSITION APPROX .1875" AND THROUGH THICKNESS FUS BS 955 RT SIDE REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922SDR IPXA1666378Fitting · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING AREA CRACK FOUND AT T-FITTING INBD LAYER APPROX 0.040" IN LENGTH. FUSELAGE LT BS 955 REAR SPAR BULKHEAD AREA T-FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-H APPENDIX 'C' ORIGINAL MATERSDR IPXA1666361Fitting · corrodedINSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING AREA CORROSION CRACK FOUND ON 6 O/C POSITION AT TEE FITTING OUTBOARD LAYER APPROX .1250" IN DEPTH. FUSELAGE RT BS 955 REAR SPAR BULKHEAD AREA TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-SDR IPXA1666382Strap · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FAIL SAFE STRAP CRACK SUSPECT FOUND, REMOVED AND REINSTALLED IAW EO B767-5350-17922-H, APPENDIX 'C' FIG 6 FOR FURTHER CONFIRMATION BY NDT INSP, THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.SDR IPXA1666381Strap · crackedINSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FAILSAFE STRAP CRACK SUSPECT FOUND, PLS REMOVE BOLT FOR NDT CRACK CONFIRMATION. FUS RT BS 955 REAR SPAR BULKHEAD FAILSAFE STRAP ATT MOST LOWER BOLT REMOVED AND REINSTALLED IAW EO B767-5350-17922-H, APPSDR IPXA11666204Stiffener · crackedINSPECTION TYPE:C, FX MAIN EQUIPMENT CTR STA 246 LBL40 FLOORBEAM VERTICAL STIFFENER FOUND CRACKED. FX MEC STA246 LBL40 FLOORBEAM VERT STIFFENER REPAIRED IAW SRM 53-10-51-2R4, REPAIR 4 FIG 201. CRACKED LENGTH 0.75" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.SDR IPXA1666339Floor Panel · dentedINSPECTION TYPE:C, DMI NR D442907 MAIN CARGO DECK POSITION 11R FLOOR PANEL INTERIM REPAIR DUE TO DENT AT STA 1340. MCD FLOOR PANEL AT STA 1263 TO 1370, RBL 88 FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.SDR IPXA11665166Floor Panel · damagedMCD POS 14L STATION 1490 FLOOR PANEL HAS 3 HOLES. FAB NEW FLOOR PANEL REF EO B767-5300-9693-H.SDR IPXA2675473Floor Panel · damagedHOLE IN MAIN CARGO DECK FLOOR PANEL POS 7R THIRD FLOOR PANEL FROM OTBD. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA09656144Attach Fitting · crackedINSPECTION TYPE:7C MAIN E/E COMPT STA 246 RBL 10 FLOOR SUPPORT ATT CLIP CRACKED. MAIN E/E COMPT STA 246 RBL 10 FLOOR SUPPORT ATT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.SDR IPXA09656113Attach Angle · crackedINSPECTION TYPE:C MAIN E/E COMPT STA 246 LBL 25 FLOOR SUPPORT ATT ANGLE CRACKED. CRACKED 0.75 INCH LENGTH. MAIN E/E COMPT STA 246 LBL 25 FLOOR SUPPORT ATT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.SDR IPXA09656138Skin · crackedINSPECTION TYPE:7C LT WING - NR 4 SLAT EXT SKIN FOUND CRACK AT O/B STRINGER FASTENER AREA. LT WING NR 4 SLAT OSS641-74 SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 43. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 7075T6.071" AND 7075T6.063" ASSDR IPXA09656122Panel · delaminatedINSPECTION TYPE:C EMP VERTICAL STAB RT LWR FWD EXTERNAL FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM REV 43, 51-70-10 REPAIR 4 FIG 201, DOUBLER MATERIAL 7075T6BARE0025IN, REPAIR DOUBLER SIZE: 16.125 X 13 INCHES.SDR IPXA09656117Stiffener · crackedINSPECTION TYPE:7C AFT CARGO COMPT STA 1087 LBL 26 BILGE AREA STIFFENER FOUND CRACKED. AFT CARGO COMPT BS 1087 LBL 26 BILGE AREA STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 43.SDR IPXA09656116Fairing · delaminatedINSPECTION TYPE:7C LT WING - I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05, PAR 5A (1), FIG 5, REV 43.SDR IPXA09656115Stiffener · crackedINSPECTION TYPE:7C AFT CARGO COMPT STA 1087 RBL 26 BILGE AREA STIFFENER FOUND CRACKED. AFT CARGO COMPT BS 1087 RBL 26 BILGE AREA STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 43.
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