N99GH
Service difficulty reports · 19
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 = 'N99GH' 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 = 'N99GH' 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 TIMA2024021614005Indication Sys · false indicationON APPROACH TO 16L SLC, EXTENDED GEAR AND CONFIGURED FOR LANDING. NEGATIVE GEAR INDICATION FOR THE NOSE GEAR, WENT AROUND AND REQUESTED DELAY VECTORS TO TROUBLE SHOOT. CYCLED THE GEAR WITH NO CHANGE TO NOSE GEAR INDICATION. TESTED THE BULBS, WITH NO ILLUMINATSDR TIMA2018102500001Oil System · low pressureDURING CRUISE, PILOT NOTED LEFT ENGINE LOW OIL PRESSURE WARNING ILLUMINATED, AND VERIFIED WITH LOW OIL PRESSURE ON THE GAUGE. PILOT SHUT DOWN THE ENGINE AND RETURNED SAFELY WITH NO FURTHER INCIDENT TO SLC, THE ORIGINAL DEPARTURE POINT. FURTHER INVESTIGATION TOSDR TIMA20140127001Rib · brokenON POST FLIGHT INSPECTION THE LT ELEVATOR OTBD LE RIB WAS FOUND TO BE BROKEN OFF ALLOWING THE LT ELEVATOR BALANCE WEIGHT TO SEPARATE FROM THE ELEVATOR.SDR TIMA20131030011Engine · overtempDURING AN ILS APPROACH. A MISSED APPROACH WAS EXECUTED. WHEN POWER WAS ADVANCED TO COMMENCE THE MISSED APPROACH, NR 2 ENGINE EXHIBITED HIGH ITT (1100 DEG C), TORQUE FLUCTUATED FROM 200 TO 1500 LBS. AND RPM FLUCTUATED FROM 0 TO 2200. AFTER THE ACFT WAS AT ASDR TIMA20130510003Hinge Bracket · brokenLEFT ELEVATOR OTBD HINGE BRACKET WAS FOUND TO BE BROKEN. REMOVED THE BROKEN ELEVATOR HINGE AND INSTALLED A NEW HINGE.SDR TIMA201000009Blade · brokenLEFT ENGINE FAILED IN FLIGHT.SDR TIM2005F00004Fire Detector · contaminatedTHE FIRE DETECTOR WARNING LIGHT ILLUMINATED IN FLIGHT. MOISTURE WAS THE PROBABLE PROBLEM. AFTER TAXI THE LIGHT EXTINGUISHED. NOT OTHER PROBLEM WITH FIRE DETECTION SYSTEM WAS FOUND. (K)SDR YDA2005F00000Hinge · damagedTHE LT NOSE GEAR DOOR CENTER HINGE AND NOSE GEAR DOOR ACTUATOR LINK QUIDE, BENT. THE NOSE GEAR DOORS WERE DISCONNECTED FOR AN INSPECTION. THE LT MAIN GEAR DOORS WERE RIGGED AND A RETRACTION TEST WAS PERFORMED. A LOAD POPPING NOISE WAS HEARD. UPON INSPECTIOSDR VDA2004F00000Fan · failedTHE CENTRIFUGAL FAN ASSY CAME APART, SHED ALL THE BLADES. POSSIBLE THAT THE FAN WAS OUT OF BALANCE. POSSIBLE THAT THE FAN WAS THROWN OUT OF BALANCE BY INGESTION OF MATERIAL THROUGH THE AIR RETURN SYSTEM OF THE AIRCRAFT. INSPECTION OF THE VENT RETURN SYSTEM SDR TIM2001F00005Warning Light · illuminatedGEAR INTRANSIT LIGHT STAYED ON, AFTER GEAR RERACK.SDR TIM2001F00004Arm · wornDURING INSPECTION, THE RUDDER PEDAL PIVOT HOLES WERE FOUND TO BE ELONGATED. THE WEAR APPEARS TO BE NORMAL. THE RUDDER PEDAL ARM WAS REPLACED WITH A SERVICEABLE ARM AND SAFTIED AND LUBED. SINCE THE RUDDER PEDAL IS A HIGH USE ASSEMBLY, A HEAVIER LUBRICATING SDR TIM2001F00000Control Cable · frayedDURING A DETAILED INSPECTION OF THE CONTROL CABLES, THE RUDDER CABLE WAS FOUND TO BE FRAYED ABOUT 3 INCHES AFT OF A PULLEY IN THE BILGE JUST AFT OF THE AIR STAIR DOOR. THE AFFECTED RUDDER CABLE WAS REMOVED AND THE OTHER INSPECTED FOR SIMILAR DAMAGE. NO DAMAGSDR 20001019SH033Torque Tube · crackedDURING A SCHEDULED TAIL INSPECTION, DISCOVERED THE ELEVATOR TORQUE TUBE/CASTING HAD CRACKS. DEFECTIVE TORQUE TUBE ASSY REPLACED WITH SERVICEABLE PART. THIS CONDITION MOST LIKELY OCCURRED AS A RESULT OF NORMAL OPERATION. NO OTHER DISCREPANCIES NOTED. (X)SDR 20000620SH007Harness · shortedRIGHT ENGINE ITT READING LOW IN ALL CONDITIONS OF OPERATION. DETERMINED PROBLEM TO BE AN INTERNAL SHORT IN THE TRIM HARNESS ON THE RIGHT ENGINE. REPLACED TRIM HARNESS WITH SERVICEABLE TRIM HARNESS AND CALIBRATED ITT AIRFRAME SYSTEM RESISTANCE. INSPECTED ENGSDR 20000601SH018Fuel Cell · puncturedRIGHT NACELLE FUEL CELL FOUND LEAKING FUEL. INSPECTION REVEALED A PUNCTURE IN THE SIDE OF THE CELL CAUSED BY A TANK HANGER THAT HAD BECOME DISLODGED FROM ITS ORIGINAL LOCATION. THE HANGER PROTRUDING CLIP HAD REPOSITIONED TOWARD THE TANK LINER CAUSING THE TANSDR 99ZZZX4112Beacon · inoperableUPPER BEACON INOPERABLE. MOTOR THAT ROTATES BULBS SHORTED OUT. RESULT OF BLOWN CIRCUIT BREAKER.SDR 99ZZZX4111Relay · inoperableRIGHT GENERATOR WOULD NOT COME ON LINE. FOUND REVERSE CURRENT RELAY INOPERABLE.SDR 98ZZZX3882Pedal Arm · wornHINGE POINT FROM RUDDER PEDALS TO RUDDDER ARM BUSHING IS WEARING DEEP GROOVES INTO TANGS ON RUDDER PEDAL ARMS.SDR 98ZZZX3881Pedal Arm · wornHINGE POINT FROM RUDDER PEDAL TO RUDDER ARM BUSHING IS WEARING DEEP GROOVES INTO TANGS ON RUDDER PEDAL ARMS.
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