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 IPXA09656146Skin · crackedINSPECTION TYPE:7C NR 2 PYLON STRUT LT EXT SKIN 425DL CUTOUT CRACKED. NR 2 PYLON STRUT LT EXT SKIN 425DL CUTOUT REPAIRED AS PER HX RS R-54-51-36328 REV A. THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL AMS4911-00901IN AND AIS1-301-00161INFH, REPAIR SIZE SDR IPXA09656143Floor Panel · puncturedINSPECTION TYPE:7C MAIN COMPT FLOOR PANEL AT STN 1576 LBL 11 FOUND PUNCTURE ABOUT 1 INCH DIA. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.SDR IPXA09656142Floor Panel · puncturedINSPECTION TYPE:7C MAIN COMPT FLOOR PANEL AT STN 654+3, RBL 74 FOUND PUNCTURE ABOUT .5 INCH DIA. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R, REV 43, FIG 201.SDR IPXA09656141Floor Panel · puncturedINSPECTION TYPE:7C MAIN COMPT FLOOR PANEL AT STN 326, LBL 6 FOUND PUNCTURE ABOUT .5 INCH DIA. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43, FIG 201.SDR IPXA09656140Skin · crackedINSPECTION TYPE:7C RT WING - NR 9 SLAT I/B UPPER AREA FOUND CRACKED. RT WING - NR 9 SLAT OSS573 SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201, REV 43. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 7075-0-0063IN AND 7075-0-0071IN. REPAIR DOUBLER ANDSDR IPXA09656139Skin · crackedINSPECTION TYPE:7C RT WING - NR 9 SLAT O/B UPPER AREA FOUND CRACKED. RT WING NR 9 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 AS REPAIR DOUBLERS AND REPSDR IPXA09656137Stringer · chafedINSPECTION TYPE:7C M/D STA 1241 - 1263 STR 16R FOUND DEEP CHAFING MARK. MAIN DECK BS 1233 TO 1271 STR 16R STRINGER REPAIR AS PER SRM 53-00-03-2R1 FIG 201 REV 43. THIS REPAIR CLASSIFIED AS A CATEGORY 'A' REPAIR WITH MATERIAL BAC1498-208 7075T62 AND BAC1498-20SDR IPXA09656124Support Bracket · crackedINSPECTION TYPE:7C RT WING - L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT SUPPORT BRACKET FOUND CRACKED. RT WING - L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.SDR IPXA09656123Doubler · delaminatedINSPECTION TYPE:C RT WING I/B AFT FLAP LOWER O/B EXISTING REPAIR FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 202 REV 43. REPAIR DOUBLER MATERIAL 2024T3-0040IN AND ADHESIVE FILM AF163-2K0010IN REPAIR DOUBLER SIZE: 9 XSDR IPXA09656121Hinge Fitting · crackedINSPECTION TYPE:C LT WING I/B MAIN FLAP TO AFT FLAP HINGE ARM FTG FOUND CRACKED 1.5 INCH LENGTH AT I/B FLANGE AND 0.9 INCH LENGTH AT O/B FLANGE. LT WING I/B MAIN FLAP TO AFT FLAP HINGE ARM FTG REPAIRED AS PER SRM 57-53-02-2R1, FIG 201 REV 43.SDR IPXA09656120Skin · misrepairedINSPECTION TYPE:7C SURVEY SEQUENCE 306-F1-02, FX BS 388-400 BETWEEN STR 29L AND 30L, THE SKIN REPAIR CANNOT BE CORRELATED TO SRM. FX REPAIRED AS PER SRM 53-00-01-2R1 FIG 201 REV 43 JUST AT STA 385 - 415 BETWEEN STR 28L AND 31L. THIS IS CLASSIFIED AS A MAJOR SDR IPXA09656145Stiffener · crackedINSPECTION TYPE:7C FWD CARGO COMPT STA 786, WL 196, RBL 33 WING CENTER SECTION FRONT SPAR ATT STIFFENER FOUND CRACKED. FWD CARGO COMPT BS 786 RBL 33 CENTER TANK FRONT SPAR STIFFENER REPAIR AS PER HX RS R57-11-36330 REV A WITH MATERIAL 2024T351.0250 AND 2024T3SDR IPXA09656114Cylinder · corrodedINSPECTION TYPE:7C LT MLG OUTER CYLINDER EXTERIOR SURFACE FRONT SIDE AND O/B SIDE NUMEROUS LOCATIONS FOUND RUSTY ABOVE TORSION LINK UPPER FTG UP TO 56 INCHES TOP AREA HAND BLEND AREA 50" X 14" REWORK DEPTH 0.001". LT MLG OUTER CYLINDER EXTERIOR SURFACE FRONT SDR IPXA09656147Skin · misrepairedINSPECTION TYPE:7C SURVEY SEQUENCE 306-F1-05 FUSELAGE BS 1241 - 1263 STR 15R - 17R DOUBLER AND TRIPLER FOUND IDENTIFY REQUIRE. SKIN REPAIR AS PER SRM 53-00-01-2R1 FIG 201 REV 43. SUBSEQUENT INSP ARE NECESSARY AS PER SRM 53-00-01-2R1 FIG 201 SHT 9 TABLE V. TSDR IPXA09655002Shunt · inoperativeINSPECTION TYPE:ETOP ATB - LT ENG PRI AND STBY EGT INOP. EPER FIM 77-21-00 PIMU BITE SHOWS 352 16A EGT SENSOR AND 352 16B EGT SEN PER PIMU MESS INDEX. REMOVED AND REPLACED SHUNT JUNCTION BOX IAW 77-21-53-4 UP TO OPS CK. SHUNT BOX CKS J131 PIN B TO J3 PIN E SDR UPS08653308Bracket · crackedINSPECTION TYPE:N/A R2 WINDOW CARRIAGE ASSEMBLY BRACKET CRACKED. REMOVED AND REPLACED BALL SCREW ASSEMBLY AND CARRIAGE ASSEMBLY PER MM 56-11-04-4.SDR UPS08652951Pseu · faulted2ND ATB - LE FLAP ASSYMETRY. REF FIM 27-81-00 FIG 107 PSEU FAULTED S280. INSPECTED TARGET AND AFFECTED SLAT. NO DAMAGE FOUND. CLEARANCE WITHIN LIMITS AT .111 INCH. TESTED INDUCTANCE IAW FIM 32-09-03 FIG 108. FOUND S280 OUT OF LIMITS READING 5.8 MILLIHENRYS. RSDR UPS08652923Indicator · malfunctionedATB - RECEIVED MESSAGE AND FLAP INDICATOR SHOWED LE FLAPS NOT UP. RAN CHECKLISTS. REMOVED AND REPLACED IAW 27-58-02-4 FLAP POSITION INDICATOR OPERATION CHECKED SATISFACTORY IAW 27-58-00-5.SDR UPS07650485Warning System · malfunctionedINSPECTION TYPE:ETOP BTB - RIGHT PRV MSG ON START. PERFORMED ENGINE START AND EICAS MESSAGE WENT AWAY. OK FOR AIRCRAFT TO CONTINUE PER FIM 36-10-00.SDR UPS07650479Connector · dirtyINSPECTION TYPE:ETOP RT ENG PRV EICAS MSG WITH STATUS MSG AND BLEED LIGHT ON RIGHT SIDE. REMOVED AND CLEANED CONNECTOR ON RT PRSOV. CYCLED VALVE MANUALLY. RAN ENGINE, NO MSG OR BLEED LIGHT. OPERATES NORMAL PER MM 36-11-00.SDR UPS07649969Seat Track · corrodedINSPECTION TYPE:2C SEAT TRACK CORRODED. REPAIRED IAW SRM 53-00-52-2R REPAIR 9.SDR UPS07649916Seat Track · corrodedINSPECTION TYPE:2C SEAT TRACK CORRODED. REPAIRED IAW SRM 53-00-52-2R REPAIR 9.SDR UPS07649915Seat Track · corrodedINSPECTION TYPE:2C SEAT TRACK CORRODED. REPAIRED IAW SRM 53-00-52-2R REPAIR 9.SDR UPS07649917Skin · crackedINSPECTION TYPE:2C CRACKS IN SKIN AT UPPER GPS ANTENNA DOUBLER. REPAIRED IAW EO B767-5330-26944-A, ER 07-2324. CUT OUT DAMAGED AND INSTALLED DOUBLER.SDR UPS07649926Case · corrodedINSPECTION TYPE:C2 NR 1 ENGINE CORROSION ON AFT FAN CASE AT 5-6:30 POS AT NUT PLATES 8 INCHES FROM AFT END OF CASE. REPAIRED PER UPS ENGINEERING FILE NUMBER 80C2-72-20000.SDR UPS06647836Servo · malfunctionedUNCOMMANDED RUDDER YAW TWICE IN FLIGHT. R & R LT & RT YAW DAMPER SERVO IAW MM 22-21-02-4. LEAK CHECK RIGHT & LEFT YAW DAMPER SERVO PER TECH SERVICES. R&R RIGHT YAW DAMPER MODULE ASSY IAW MM 22-21-04-2. ALSO R&R LEFT YAW DAMPER MODULE ASSY AS PRECAUTIONARY. PSDR UPS01636828Valve · malfunctionedINSPECTION TYPE:ETOP LEFT DUCT PRESSURE FLUCTUATES W/ENGINE RUNNING AND BLEED SWITCH ON. AFTER TAKEOFF PRESSURE DROPPED BELOW 20 PSI & ROSE ABOVE 60 PSI. TURNED LEFT PACK OFF AND LEFT ENG BLEED SWITCH OFF. DEF LEFT ENG PRSOV PER MEL 36-11-1-1. C/W DMP 36-11-1.
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