N8974U, cancelled Jul 11, 2005
Service difficulty reports · 23
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 = 'N8974U' AND deregistration_id = 'N8974U-2005-07-11' 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 = 'N8974U' AND deregistration_id = 'N8974U-2005-07-11' 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 ARWA20040105Attach Fitting · looseDURING PREFLIGHT FOUND ELEVATOR STARBOARD SIDE UP SLIGHTLY AND PORT SIDE SLIGHTLY DOWN, SLIGHT DIFFERENCE IN TRAVEL BETWEEN PORT AND STARBOARD SIDE ELEVATORS. FOUND LOOSE ATTACHMENT AT PORT SIDE ELEVATOR ATTACHMENT TO TORQUE TUBE. PERFORMED ELEVATOR INSPECTISDR ARWA20030702Skin · crackedNR 34M. DURING "A" CHECK NON-ROUTINE INSPECTION, THE FOLLOWING WAS FOUND- NLG WW LT SIDE, STA. 208 L-33L CORNER WITH .2500 INCH CRACK. TRIMMED OUT CRACK ON EDGE OF NOSE SKIN AT NOSE LANDING GEAR DOOR LEFT AFT CORNER AND FABRICATED FILLER FROM 707STG.O50 AND SDR ARWA20030206Line · leakingIN FLIGHT ABOUT ONE HOUR OUT OF VTBU AFTER TAKE-OFF AIRCRAFT WAS LOSING HYDRAULIC FLUID. DID IN-FLIGHT TURNBACK, DUMPED FUEL AND LANDED BACK AT VTBU. RAN ALL APPROPIATE CHECK LISTS. FOUND NR 3 ENGINE HYDRAULIC PUMP SUPPLY LINE LEAKING. REMOVED AND REPLACESDR ARWA20021205O-Ring · leakingON FINAL APPROACH LOSS OF HYDRAULIC FLUID TO THE STAND PIPE. FOUND EMPENNAGE FILTER BOWL LEAKING AT MAGNETIC PLUG. REMOVED AND REPLACED O-RING LEAK CHECK NORMAL IAW MM.SDR IXXA0000021Seal · leakingEN ROUTE FROM QPG TO OKO, WHEN THE FLIGHT CREW TURNED ON THE NUMBER ONE TURBO COMPRESSOR A SQUEAL WAS HEARD AND AN ODOR WAS SENSED IN THE COCKPIT. THE FLIGHT CREW SECURED THE TURBO COMPRESSOR, THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO OKO FOR AN UNEVENTFUL SDR IXXA0000018Line · defectiveEN ROUTE FROM KWI TO HIK, THE FLIGHT CREW NOTICED THE MAIN HYDRAULIC SYSTEM FLUID QUANTITY DECLINING. THE FLIGHT CREW FOLLOWED COMPANY EMERGENCY PROCEDURES, DECLAIRED AN EMERGENCY, AND CONTINUED TO HIK FOR AN UNEVENFUL LANDING. MAINTENANCE INSPECTED THE AIRCSDR IXXA0000013Uplock · malfunctionedHIK - FLT JZ43 - EN ROUTE TO KWA, THE LANDING GEAR FAILED THE GEAR UPLATCH CHECK, ACCOMPANIED BY GEAR AND DOOR WARNING LIGHTS ILLUMINATING. THE FLIGHT CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO HIK FOR AN UNEVENSDR IXXA9800058Pumps · defectiveEN ROUTE, THE MAIN HYDRAULIC SYSTEM FAILED AND HYDRAULIC PRESSURE DROPPED TO ZERO. THE FLIGHT CONTROL MANUAL REVERSION LIGHTS ILLUMINATED CONFIRMING THE FAILURE. THE FLIGHT WAS DIVERTED TO DNA FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT ANSDR IXXA9700119Actuator · failedAFTER TAKEOFF UPON GEAR RETRACTION, THE DOORS LIGHT REMAINED ILLUMININATED AFTER THE UPLATCH CHECK. THE GEAR WAS RECYCLED SEVERAL TIMES WITH NO CHANGE IN WARNING STATUS. THE FLIGHT RETURNED TO HIK. MAINTENANCE REPLACED THE MAIN GEAR CONTROL VALVE, THE HYDRASDR 96ZZZM272Unsafe Light · illuminatedRIA FLT NR 7700 MIA - DOVER AIRCRAFT RETURNED TO MIA AFTER TAKEOFF WHEN MLG DOOR UNSAFE LIGHT ILLUMINATED. IN MIA, AIRCRAFT JACKED AND RIGGED LEFT DOOR ACTUATOR. OPS CHECK OK, AIRCRAFT RETURNED TO SERVICE. (M)SDR 96ZZZX905Skin · corrodedLEVEL 2 CORROSION/AFT CARGO COMPARTMENT LOWER AREA, STR 34R BETWEEN STA 1220 AND STA 1240, FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER SRM 51-1-0. (X)SDR 96ZZZX904Doubler · corrodedLEVEL 2 CORROSION/AFT CARGO COMPARTMENT, STR 21R BETWEEN STA 1160 AND STA 1180, FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER RICH E.O. NR RCH D85310-6124. (X)SDR 96ZZZX903Doubler · corrodedLEVEL 2 CORROSION/AFT CARGO COMPARTMENT STR 21R BETWEEN STA 1160 AND STA 1180, FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER SRM 53-2-5. (X)SDR 96ZZZX902Doubler · corrodedLEVEL 2 CORROSION/AFT CARGO COMPARTMENT, LT SIDE STR 21L BETWEEN STA 1240 AND STA 1260, FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER RICH E.O. D85310-6124, REV 1.SDR 96ZZZX901Doubler · corrodedLEVEL 2 CORROSION/AFT CARGO COMPARTMENT, LT SIDE STR 21L, BETWEEN STA 1240 AND STA 1260, FLOOR SUPPORT CORRODED. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER RICH DRAWING D85310-6124. (X)SDR 96ZZZX900Skin · corrodedLEVEL 2 CORROSION/LOWER FUSELAGE IS BULGED WITH CORROSION AT FS 540R BETWEEN LONGERONS 35R AND 34R BELOW FORWARD CARGO DOOR SILL PLATE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 52-2-1.SDR 96ZZZX899Skin · corrodedLEVEL 2 CORROSION/2 SMALL SKIN BULGES JUST AFT OF NR 4 PIT DOOR FS 1290, STR 28R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1.SDR 96ZZZW49Skin · corrodedLEVEL 2 CORROSION, AFT CARGO COMPARTMENT LOWER AREA STRINGER 34R BETWEEN STA 1220 AND 1240 FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-0.SDR 96ZZZW48Stringer · corrodedLEVEL 2 CORROSION, AFT CARGO COMPARTMENT STRINGER 21R BETWEEN STA 1160 AND 1180 FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PER SMR 53-2-5.SDR 96ZZZW47Stringer · corrodedLEVEL 2 CORROSION, AFT CARGO COMPARTMENT LEFT SIDE STRINGER 21L BETWEEN STA 1240 AND 1260 FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH EO D85310-6124 REV 1.SDR 96ZZZW46Skin · corrodedLEVEL 2 CORROSION, LOWER FUSELAGE IS BULGED WITH CORROSION AT FS 540R BETWEEN LONGERONS 35R AND 34R BELOW FORWARD CARGO DOOR SILL PLATE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PER SRM 52-2-1.SDR 96ZZZW45Skin · corrodedLEVEL 2 CORROSION, TWO SMALL SKIN BULGES JUST AFT OF NR 4 PIT DOOR FS 1290 STRINGER 28R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1.SDR 95ZZZX6787Fire Loop · brokenLICZ/ETAR - FLT BEHF800 - FIRE INDICATION DURING FLIGHT AT CRUISE ON NR 2 ENGINE. SHUT DOWN ENGINE, AND FIRED BOTH FIRE BOTTLES. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND FIRE LOOP BROKEN AND SHORTED. REPLACED LOOP AND BOTH FIRE BOTTLES. SYSTEM OPERATED GOO
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