N911TG
Service difficulty reports not matched to an aircraft · 27
They name N911TG, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N911TG' AND registry_match IS NULL 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 = 'N911TG' AND registry_match IS NULL 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 QMLA2013062413089Shaft · wornDURING THE DAILY AIRWORTHINESS CHECK, A MISSING RIVET WAS FOUND IN THE AREA OF THE TAIL GEARBOX. AFTER A CLOSER INSPECTION, NUMEROUS RIVETS WERE FOUND TO HAVE THE APPEARANCE OF STARTING TO BE "WORKING". THE TAIL ROTOR HEAD/BLADE ASSY WAS REMOVED ALONG WITH TSDR QMLA2013021313026Gearbox · making metalTAIL ROTOR GEARBOX CHIP LIGHT OCCURED DURING ENGINE SHUTDOWN. A VISUAL INSPECTION FOUND A CHIP OUT OF LIMITS. REMOVED FAILED GEARBOX. GEARBOX AND SHAFT ASSY, ASSEMBLED AND INSTALLED ON ACFT, PERFORMED VIBRATION & BALANCE CHECK AND RETURNED ACFT TO SERVICE.SDR BAQA200700032Fitting · crackedTAILROTOR GEAR BOX MOUNT FITTING AT TOP OF VERTICAL FIN CRACKED AND TAIL ROTOR GEAR BOX MOUNTING STUD ROSSET FITTING LOOSE.SDR BAQA2007005Skin · crackedA CRACK WAS FOUND AT THE TOP OF THE TAILBOOM VERTICAL FIN WHILE TROUBLESHOOTING A TAIL ROTOR VIBRATION ISSUE. THE CRACK WAS FOUND ON THE LT SIDE OF THE ACCESS SIDE OF THE OPENING FOR ACCESS TO THE TAILROTOR GEARBOX MOUNTING HARDWARE.SDR BAQA094843Indicator · failedNR 2 ENG N1 IND LED DIGITAL DISPLAY DIM/BRITE BULB BURNED OUT. REPLACED WITH SERVICABLE UNIT. 06/04/2004SDR BAQA094415Control Unit · inoperativeSTRONG LAT. INPUTS WITH YAW CSAS IN ON POSITON OR STANDBY POSITION, GOES AWAY WHEN SYSTEM IS TURNED OFF. UNIT LASTED 83.6 HOURS SINCE LAST REPAIR. LAST REPAIR, CJ RO 9-090006-17 ; INVOICE NR S29024201.SDR BAQA094402Indicator · inoperativeWHEN FLOWN WITH INDICATOR. WINGS LEVEL IN TRIM A/C MAKES SLOW RT TURN, INDICATOR IS DRIFTING. REPLACED WITH SERVICABLE UNIT. 05/05/2004SDR BAQA093829Control Unit · failedYAW CSAS MADE UNCOMMANDED YAW OSCILLATIONS IN NORMAL AND STANDBY MODE AT APPROX. TWO SECOND INTERVALS. UNIT WAS INSTALLED 02/16/2004 AT A/C TT 5145.8 AND WAS REMOVED 03/12/2004 AT A/C TT 5172.2 FOR A TOTAL OF 26.4 HOURS. LAST REPAIR REF RO 9-090006-18 MMIR CLSDR BAQA093635Blade · damagedWARRANTY REPAIR/EXCHANGE : SINCE JULY 2, 1996 BLADE HAS FLOWN ONLY 346.1 HOURS. BLADE HAS ZERO HOURS AFTER BEING REMOVED FOR SUSPECTED COWLING STRIKE ON JULY 9, 1998 (A/C 7109). BLADE REPAIRED THREE TIMES SINCE 1998 AND BLADE IS STILL UNABLE TO FLY. LAST REPSDR BAQA092751Blade · out of trackRENTAL 117-151451V001 S/N 2622 RENTAL CHARGE 36.75 HR REPLACEMENT VALVE RETURN OF RENTAL BLADE AFTER .4 HOURS OF USE, WOULD NOT TRACK REPLACED WITH ANOTHER RENTAL BLADE (S/N 2419)SDR BAQA092750Blade · out of trackRETURN OF RENTAL BLADE AFTER .4 HOURS OF USE, BLADE WOULD NOT TRACK. REPLACED WITH ANOTHER RENTAL BLADE (S/N 2413)SDR BAQA093649Blade · damagedLEAD/LAG IN EXCESS OF 20MM, INSTALLED A/C TT 5145.8, REMOVED AC TT 5146.2 FOR A TOTAL .4 HOURS. RECEIVED BLADE ON EXCHANGE FROM AEC UNDER OUR PO 8-080114-36. WOULD LIKE TO HAVE THIS BLADE BACK AFTER REPAIR, SEEMS TO HAVE A GOOD HISTORY OF BEING ABLE TO STASDR BAQA093648Blade · out of trackBLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. BLADE WAS INSTALLED ON A/C N911TG/7506 FOR A TOTAL OF 2.4 HOURS. BLADE WAS RECEIVED AS AN EXCHANGE, UNDER OUR PO 8-080114-36.SDR BAQA093639Blade · out of trackBLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. BLADE WAS INSTALLED ON A/C N911TG/7506 FOR A TOTAL OF 2.4 HOURS. LAST REPAIR WAS A INSURANCE CLAIM, REF. PO 1-010199-41.SDR BAQA093638Blade · damagedBLADE DIVES IN FORWARD FLIGHT. BLADE WAS INSTALLED .2 HOURS SINCE WE HAD RECEIVED AS AN EXCHANGE UNDER OUR PO 8-080114-10. BLADE HAS ACCUMULATED 106.1 HOURS SINCE 10/23/2001 AND HAS BEEN REPAIRED THREE TIMES IN THAT TIME SPAN WITH THIS BEING THE FOURTH. AIR MESDR BAQA093636Blade · out of trackWARRANTY REPAIR/EXCHANGE : S/N 198 ; BLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. SINCE FEBRUARY 21,200 BLADE HAS ACCUMULATED ONLY 279.8 HOURS BUT HAS BEEN REMOVED FROM SIX DIFFERENT AIRCRAFT FOR REPAIR WITH THIS BEING THE SEVENTH TIMSDR BAQA092782Gyro · inoperativeSTANDBY GYRO CARD SLIPS IN DISPLAY. REPLACED WITH SERVICABLE UNIT. 02/20/2004SDR BAQA093650Blade · damagedEXCESSIVE BLADE LAG, BLADE WAS INSTALLED BUT NEVER FLOWN DUE TO EXCESSIVE LAG. RECEIVED BLADE ON EXCHANGE FROM AEC UNDER OUR PO 8-080103-07, BLADE IS UNSERVICABLE WITH ZERO HOURS ON IT. BLADE HAS ACCUMULATED ONLY 733.4 HOURS ON IT SINCE 09/15/1997 BUT HAS BEENSDR BAQA088806Bolt · mismanufacturedBOLTS JUST PURCHASED, BUT THE COTTER PINS HOLES ARE DRILLED WRONG, MAKING THE BOLTS UNUSEABLE. REQUEST WARRANTY CREDIT ON THESE BOLTS.SDR BAQA088681Blade · damagedMAIN ROTOR BLADE HAS MINOR LEAD LAG PLAY. BLADE LASTED ONLY 421.6 HOURS SINCE LAST REPAIR. PART IS ALSO DUE LOOP INSPECTION.SDR BAQA093003Igniter Box · failedIGNITOR BOX NOT FIRING. IGNITOR BOX IS ORIGINAL EQUIPMENT. REPLACED WITH SERVICABLE UNIT. 02/27/2004SDR BAQA081591Starter Gen · failedBELIEVE INTERNAL MALFUNCTION. BRUSHES LOOK GOOD. NO GENERATION. THIS STARTER GENERATOR WAS INSTALLED 7/1/02 AND ONLY HAS 168.5 HOURS. REPLACED WITH SERVICEABLE UNIT.SDR BAQA081575Pump · intermittentFUEL BOOST PUMP INTERMITTENT OPERATION. REPLACED WITH SERVICEABLE UNIT.SDR 98ZZZX1704Blade · crackedDURING A PRE-FLIGHT INSPECTION, THE MECHANIC FOUND A 3 INCH CRACK AT THE ROOT END OF TAIL ROTOR BLADE. THIS IS THE THIRD EVENT. 11-18-94, 198.4 HRS, S/N 116/118. 5-3-96, 1,050.1 HRS, S/N 103/104. 858.5 HOURS ON THE BLADES, SAME P/N.SDR 96ZZZX2602Mount · flange crackedFORWARD AND REAR MOUNT BRACKETS CRACKED DUE TO VIBRATION AND SB 133-1 HAD NOT BEEN ISSUED YET AND HAD NOT BEEN C/W AT THE TIME. INSTALLED NEW COIL ASSY, PN JBS3001-3, AND C/W SIB 133-1.SDR 95ZZZX6211Fcu · defectiveIN CRUISE FLIGHT, 60 PERCENT TORQUE WHEN ENGINE IS BEEPED TO 100 PERCENT, N2 TORQUE DROPS OFF 40 PERCENT, AND N1 DROPS OFF 10-15 PERCENT. SEEMS TO OPERATE NORMALLY WHEN N2 IS AT 98-99 PERCENT.SDR 95ZZZX5102Evaporator Mount · crackedDURING ROUTINE BATTERY CHANGE, MECH NOTICED 3 OUT OF 4 MOUNTS ON A/C EVAPORATOR ASSY CRACKED. UNIT JUST INSPECTED 5 DAYS PRIOR WITH NO DEFECTS. UNIT LOCATED BETWEEN ENG EXHAUST EJECTORS. THESE AFT COWLING ARE NOT NORMALLY REMOVED BETWEEN ENG CHANGES OR MAJO
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