# Service difficulty reports: N99GH A list on [N99GH](https://openairdocs.org/aircraft/N99GH.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR TIMA2024021614005](https://openairdocs.org/sdr/TIMA2024021614005.md): Indication Sys · false indication · Feb 14, 2024 · N99GH · Beech 99 · Landing Gear Position and Warning > ON 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 ILLUMINAT - [SDR TIMA2018102500001](https://openairdocs.org/sdr/TIMA2018102500001.md): Oil System · low pressure · Oct 22, 2018 · N99GH · Beech 99A · Turbine Engine Oil System > DURING 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 TO - [SDR TIMA20140127001](https://openairdocs.org/sdr/TIMA20140127001.md): Rib · broken · Jan 27, 2014 · N99GH · Beech 99A · Elevator, Spar/Rib > ON 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 TIMA20131030011](https://openairdocs.org/sdr/TIMA20131030011.md): Engine · overtemp · Oct 30, 2013 · N99GH · Beech 99A · Engine (Turbine/Turboprop) > DURING 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 A - [SDR TIMA20130510003](https://openairdocs.org/sdr/TIMA20130510003.md): Hinge Bracket · broken · May 10, 2013 · N99GH · Beech 99A · Elevator Structure > LEFT ELEVATOR OTBD HINGE BRACKET WAS FOUND TO BE BROKEN. REMOVED THE BROKEN ELEVATOR HINGE AND INSTALLED A NEW HINGE. - [SDR TIMA201000009](https://openairdocs.org/sdr/TIMA201000009.md): Blade · broken · Jan 28, 2010 · N99GH · Beech 99A · Turbine Engine Compressor Section > LEFT ENGINE FAILED IN FLIGHT. - [SDR TIM2005F00004](https://openairdocs.org/sdr/TIM2005F00004.md): Fire Detector · contaminated · Apr 20, 2005 · N99GH · Beech 99A · Fire Detection > THE 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 YDA2005F00000](https://openairdocs.org/sdr/YDA2005F00000.md): Hinge · damaged · Oct 18, 2004 · N99GH · Beech 99A · Landing Gear Doors > THE 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 INSPECTIO - [SDR VDA2004F00000](https://openairdocs.org/sdr/VDA2004F00000.md): Fan · failed · Jun 25, 2004 · N99GH · Beech 99A · Air Distribution Fan > THE 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 TIM2001F00005](https://openairdocs.org/sdr/TIM2001F00005.md): Warning Light · illuminated · Jul 18, 2001 · N99GH · Beech 99A · Landing Gear Position and Warning > GEAR INTRANSIT LIGHT STAYED ON, AFTER GEAR RERACK. - [SDR TIM2001F00004](https://openairdocs.org/sdr/TIM2001F00004.md): Arm · worn · Jun 18, 2001 · N99GH · Beech 99 · Rudder Control System > DURING 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 TIM2001F00000](https://openairdocs.org/sdr/TIM2001F00000.md): Control Cable · frayed · May 16, 2001 · N99GH · Beech 99A · Rudder Control System > DURING 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 DAMAG - [SDR 20001019SH033](https://openairdocs.org/sdr/20001019SH033.md): Torque Tube · cracked · Sep 27, 2000 · N99GH · Beech 99A · Elevator Control System > DURING 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 20000620SH007](https://openairdocs.org/sdr/20000620SH007.md): Harness · shorted · May 28, 2000 · N99GH · Beech 99A · Engine EGT/TIT Indicating System > RIGHT 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 ENG - [SDR 20000601SH018](https://openairdocs.org/sdr/20000601SH018.md): Fuel Cell · punctured · Apr 25, 2000 · N99GH · Beech 99A · Fuel Storage > RIGHT 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 TAN - [SDR 99ZZZX4112](https://openairdocs.org/sdr/99ZZZX4112.md): Beacon · inoperable · Sep 27, 1999 · N99GH · Beech 99A · Exterior Lighting > UPPER BEACON INOPERABLE. MOTOR THAT ROTATES BULBS SHORTED OUT. RESULT OF BLOWN CIRCUIT BREAKER. - [SDR 99ZZZX4111](https://openairdocs.org/sdr/99ZZZX4111.md): Relay · inoperable · Sep 27, 1999 · N99GH · Beech 99A · DC Generating System > RIGHT GENERATOR WOULD NOT COME ON LINE. FOUND REVERSE CURRENT RELAY INOPERABLE. - [SDR 98ZZZX3882](https://openairdocs.org/sdr/98ZZZX3882.md): Pedal Arm · worn · Sep 30, 1998 · N99GH · Beech 99A · Rudder Control System > HINGE POINT FROM RUDDER PEDALS TO RUDDDER ARM BUSHING IS WEARING DEEP GROOVES INTO TANGS ON RUDDER PEDAL ARMS. - [SDR 98ZZZX3881](https://openairdocs.org/sdr/98ZZZX3881.md): Pedal Arm · worn · Sep 30, 1998 · N99GH · Beech 99A · Rudder Control System > HINGE POINT FROM RUDDER PEDAL TO RUDDER ARM BUSHING IS WEARING DEEP GROOVES INTO TANGS ON RUDDER PEDAL ARMS. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N99GH/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.