# Arrow Falcon Exporters UH-1H - Type: Aircraft model (FAA registry) - Registry code: 1500001 - Manufacturer (registry): ARROW FALCON EXPORTERS INC - Model: UH-1H - Aircraft type: Rotorcraft - Category: Rotorcraft - Engines: 1 · Turbo-shaft - Seats: 15 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS R00007DE](https://openairdocs.org/tcds/R00007DE) (OpenAirDocs) - Holder: Arrow Falcon Exporters Inc. - Registered aircraft: 2 - Page: https://openairdocs.org/model/arrow-falcon-exporters-uh-1h Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2024-19-17](https://openairdocs.org/ad/2024-19-17): Rotorcraft flight control · Airwolf Aerospace, LLC Tension-Torsion Strap Assemblies, P/N… (STC SR03408CH). Effective Oct 11, 2024 - [AD 2022-20-14](https://openairdocs.org/ad/2022-20-14): Main Rotor Gearbox · Bell Textron 204B, 205A, 205A-1 and 20 more. Effective Dec 27, 2022 - [AD 2022-22-12](https://openairdocs.org/ad/2022-22-12): Nose/Tail Landing Gear Structure/Axle · Replacement crosstubes P/N D212-664 (Dart Aerospace STC SR01298NY). Effective Nov 22, 2022 - [AD 2022-21-11](https://openairdocs.org/ad/2022-21-11): Main rotor blades · Bell Textron 204B, 205A, 205A-1 and 11 more. Effective Nov 16, 2022 - [AD 2022-05-10](https://openairdocs.org/ad/2022-05-10): Cabin Equipment/Furnishings · Airbus Helicopters AS332L, AS332L1, AS332L2 and 57 more. Effective Apr 20, 2022 - [AD 2022-06-05](https://openairdocs.org/ad/2022-06-05): Main Rotor System · WSH HH-1K, TH-1F, TH-1L and 11 more. Effective Mar 16, 2022 - [AD 2021-26-16](https://openairdocs.org/ad/2021-26-16): Engine/Transmission Coupling · Arrow Falcon Exporters UH-1H and SW205 (UH-1H). Effective Feb 25, 2022 - [AD 2021-15-14](https://openairdocs.org/ad/2021-15-14): Rotorcraft Tail Boom · California Department of Forestry UH-1H, UH-1F, TH-1L and 39 more. Effective Aug 30, 2021 - [AD 2018-02-07](https://openairdocs.org/ad/2018-02-07): Main Rotor Blades · California Department of Forestry UH-1H, UH-1F, UH-1F and 24 more. Effective Feb 1, 2018 - [AD 2016-23-09](https://openairdocs.org/ad/2016-23-09): Main Rotor Blades · California Department of Forestry UH-1H, UH-1F, UH-1F and 24 more. Effective Dec 27, 2016 - [AD 2014-03-10](https://openairdocs.org/ad/2014-03-10): Tail Rotor Control System · JJASPP Engineering Services UH-1H, UH-1F, TH-1L and 35 more. Effective Mar 26, 2014 - [AD 2013-13-06](https://openairdocs.org/ad/2013-13-06): Main rotor head · California Department of Forestry UH-1H, UH-1F, TH-1L and 36 more. Effective Sep 10, 2013 - [AD 2013-13-14](https://openairdocs.org/ad/2013-13-14): Main Rotor Head · JJASPP Engineering Services UH-1H, UH-1F, TH-1L and 33 more. Effective Jul 24, 2013 - [AD 2012-17-10](https://openairdocs.org/ad/2012-17-10): Main Rotor Blades · California Department of Forestry UH-1H, UH-1F, TH-1L and 36 more. Effective Sep 28, 2012 - [AD 2012-14-12](https://openairdocs.org/ad/2012-14-12): Tail Rotor Blades · California Department of Forestry UH-1H, UH-1F, TH-1L and 36 more. Effective Sep 4, 2012 - [AD 2010-14-12](https://openairdocs.org/ad/2010-14-12): Landing Gear System · Overseas Aircraft Support UH-1H, UH-1F, UH-1H and 40 more. Effective Jul 23, 2010 - [AD 2006-19-05](https://openairdocs.org/ad/2006-19-05): Tail rotor (T/R) slider · California Department of Forestry UH-1H, UH-1F, TH-1L and 36 more. Effective Oct 16, 2006 - [AD 2002-20-01](https://openairdocs.org/ad/2002-20-01): TT strap · Overseas Aircraft Support UH-1H, UH-1F, TH-1L and 34 more. Effective Nov 6, 2002 - [AD 2002-13-51](https://openairdocs.org/ad/2002-13-51): Tail Rotor (T/R) Grip · Overseas Aircraft Support UH-1H, UH-1F, TH-1L and 34 more. Effective Aug 19, 2002 - [AD 2002-01-31](https://openairdocs.org/ad/2002-01-31): Retirement Index Number (RIN) for Masts · Overseas Aircraft Support UH-1H, UH-1F, TH-1L and 36 more. Effective Mar 8, 2002 - [AD 2000-15-21 R1](https://openairdocs.org/ad/2000-15-21-R1): Main Rotor Mast Assemblies · Overseas Aircraft Support UH-1H, UH-1F, TH-1L and 33 more. Effective Nov 22, 2000 - [AD 99-25-12](https://openairdocs.org/ad/99-25-12): Tailboom Vertical Fin Spar · California Department of Forestry UH-1H, UH-1F, TH-1L and 31 more. Effective Jan 11, 2000 - [AD 99-07-15](https://openairdocs.org/ad/99-07-15): Tail Rotor Yoke · Arrow Falcon Exporters UH-1H, UH-1F, TH-1L and 33 more. Effective May 3, 1999 - [AD 97-01-06](https://openairdocs.org/ad/97-01-06): Tail Rotor Slider · Arrow Falcon Exporters UH-1H, UH-1F, TH-1L and 32 more. Effective Feb 13, 1997 - [AD 96-12-26](https://openairdocs.org/ad/96-12-26): Clean and Inspect Tail Rotor Blade · Arrow Falcon Exporters UH-1H, UH-1F, TH-1L and 36 more. Effective Sep 23, 1996 - [AD 95-10-08](https://openairdocs.org/ad/95-10-08): Tail Rotor Control System · Arrow Falcon Exporters UH-1H, UH-1F, TH-1L and 34 more. Effective May 26, 1995 - [AD 94-22-09](https://openairdocs.org/ad/94-22-09): Tail Rotor Driveshaft · Arrow Falcon Exporters UH-1H, UH-1F, TH-1L and 34 more. Effective Nov 22, 1994 - [AD 90-03-10](https://openairdocs.org/ad/90-03-10): Tail Rotor Grips · Arrow Falcon Exporters UH-1H, UH-1F, 204B and 33 more. Effective Oct 18, 1991 Historical (superseded or no longer in force): - [AD 2021-15-52](https://openairdocs.org/ad/2021-15-52) (historical): Main Rotor System · Arrow Falcon Exporters UH-1H, UH-1F, TH-1L and 39 more. Effective Aug 13, 2021 - [AD 2000-22-51](https://openairdocs.org/ad/2000-22-51) (historical): Main Rotor Mast or Trunnion · Arrow Falcon Exporters UH-1H, UH-1F, HH-1K and 33 more. Effective Dec 26, 2000 - [AD 2000-08-53](https://openairdocs.org/ad/2000-08-53) (historical): Main Rotor System · AST UH-1F, HH-1K, TH-1F and 32 more - [AD 97-20-09](https://openairdocs.org/ad/97-20-09) (historical): Vertical fin spar · Arrow Falcon Exporters UH-1H, UH-1F, UH-1F and 33 more. Effective May 28, 1998 ## Information bulletins (advisory) (3) - [SAIB SW-18-29R1](https://openairdocs.org/saib/SW-18-29R1): Rotorcraft Tail Boom, Attach Structure Failure. Issued Feb 19, 2019 - [SAIB SW-18-29](https://openairdocs.org/saib/SW-18-29) (historical): Rotorcraft Tail Boom, Attach Structure Failure. Issued Oct 1, 2018 - [SAIB SW-12-38](https://openairdocs.org/saib/SW-12-38): Emergency Push Out Window Retention. Issued Jul 30, 2012 ## Registered aircraft (2) - [N16TV](https://openairdocs.org/aircraft/N16TV): [Sei Holdings LLC](https://openairdocs.org/faa-owner/SEI%20HOLDINGS%20LLC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 1969, S/N 69-15455 - [N194BP](https://openairdocs.org/aircraft/N194BP): [Jones Aviation Inc](https://openairdocs.org/faa-owner/JONES%20AVIATION%20INC), [Biggs, CA](https://openairdocs.org/faa-place/CA/Biggs), built 1967, S/N 67-17420 ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB WPR11LA423](https://openairdocs.org/ntsb/WPR11LA423), Sep 2, 2011: Arrow Falcon Exporters UH-1H (N205PJ), Stockton, CA, substantial damage. Probable cause: A total loss of engine power due to the separation of a tooth from the starter-generator drive gear, which resulted in failure of the engine oil pump and subsequent oil starvation. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20110901022849A](https://openairdocs.org/incident/20110901022849A), Sep 1, 2011: Arrow Falcon Exporters Inc UH-1H (N205PJ), Trull, CA, Substantial damage. The pilot reported that while in cruise flight he noted a low oil indication to the engine. As pilot was performing a precautionary landing, the engine had a… ## Service difficulty reports (93, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2020FA0000296](https://openairdocs.org/sdr/2020FA0000296), Feb 12, 2020: PIN. DISLODGED. PRIMARY CAUSE OF DAMAGE TO ACCESSORY DRIVE, PIN CAME OUT OF SLEEVE BUSHING AND DAMAGED ADJOINING COMPONENTS. ENGINE IS STILL UNDER TEARDOWN AND INSPECTION. - [SDR 2018FA0000537](https://openairdocs.org/sdr/2018FA0000537), Jul 24, 2018: SUPPORT. INFLT SEPARATION. THE SWASHPLATE SUPPORT FAILED AT 1916 HOURS IN SERVICE, PRIOR TO ITS SCHEDULED RETIREMENT LIFE OF 3600 HOURS, FOR UNKNOWN REASONS. TOTAL TIME TRACKING ERRORS WE - [SDR 2018FA0000193](https://openairdocs.org/sdr/2018FA0000193), Jun 20, 2018: QUILL. DISCONNECTED. AIRCRAFT EXPERIENCED A LOSS OF TAIL ROTOR CONTROL DURING FLIGHT REQUIRING THE PILOT TO CONDUCT A HOVERING AUTOROTATION THAT DAMAGED THE LANDING GEAR AND BELLY O - [SDR 2018FA0000086](https://openairdocs.org/sdr/2018FA0000086), Jan 18, 2018: GRIP. CRACKED. LOWER TANG LEADING EDGE HAS A CRACK EXTENDING THRU GRIP TANG TO BLADE BOLT BUSHING. FOUND DURING PREFLIGHT INSPECTION. - [SDR 2017FA0000601](https://openairdocs.org/sdr/2017FA0000601), Jul 25, 2017: LINE. RUPTURED. ONE REPORT DESCRIBING LOSS OF HYDRAULIC FLUID AND SYS PRESSURE. MECHANICS NOTED A HIGH FREQUENCY VIBRATION IN THE HYDRAULIC SYS SPECIFIC TO TUBE WHICH CAN LEAD - [SDR 2017FA0000035](https://openairdocs.org/sdr/2017FA0000035), Jan 27, 2017: BOLT. LOOSE. DURING INSPECTION, FOUND THE ENGINE COMPRESSOR STATOR VANE RETAINING BOLT HANGING OUT OF IT'S RECESSED MOUNT HOLE. ENGINE BLEED BAND WAS PREVENTING BOLT FROM FA - [SDR 2014FA0000320](https://openairdocs.org/sdr/2014FA0000320), May 14, 2014: LONGERON. CRACKED. DURING HOVER, PILOT HEARD A BANG FROM THE REAR OF THE ACFT. PILOT LANDED BACK AT STAGING AREA. DURING INVESTIGATION, DETERMINED THE TAILBOOM JUST AFT OF THE UPP - [SDR 2012FA0000656](https://openairdocs.org/sdr/2012FA0000656), Sep 17, 2012: BLADE. MISINSTALLED. DURING A PHASE 1 INSPECTION, TAIL ROTOR BLADE CLEARANCE FROM VERTICAL STABILIZER WAS INSUFFICIENT AS IT HAD BEEN IMPROPERLY SHIMMED AND INSTALLED ON THE 90 DEGR - [SDR 2012FA0000655](https://openairdocs.org/sdr/2012FA0000655), Sep 17, 2012: SCISSORS. MISINSTALLED. DURING A PHASE 1 INSPECTION, SCISSOR HAD BEEN IMPROPERLY ASSEMBLED AND INSTALLED ON THE SLEEVE CAUSING DAMAGE TO THE SLEEVE. - [SDR 2012FA0000654](https://openairdocs.org/sdr/2012FA0000654), Sep 17, 2012: GRIP. MISINSTALLED. DURING A PHASE 1 INSPECTION, MAIN ROTOR GRIP HAD BEEN IMPROPERLY ASSEMBLED AND INSTALLED ON THE MAIN ROTOR YOKE CAUSING DAMAGE TO THE NEEDLE BEARING AND RACE. - [SDR 2012FA0000308](https://openairdocs.org/sdr/2012FA0000308), Apr 24, 2012: CAP. BROKEN. CAP BROKEN AT BS 238, LBL 14. - [SDR 2011FA0000657](https://openairdocs.org/sdr/2011FA0000657), Oct 3, 2011: BLADE. CRACKED. PILOT NOTED A VERTICAL VIBRATION DURING FLIGHT. UPON VISUAL INSPECTION, IT WAS FOUND THAT MAIN ROTOR BLADE HAD CRACKED 90 INCHES FROM BLADE TIP THROUGH THE T/E - [SDR 2011FA0000518](https://openairdocs.org/sdr/2011FA0000518), Aug 2, 2011: PINION GEAR. FAILED. GEARBOX WAS O/H AS PART OF AN AIRFRAME REFURBISHMENT PROJECT. THE INPUT QUILL SEAL HAD DEVELOPED AN OIL LEAK AND UPON INVESTIGATION IT WAS FOUND THAT THE INPUT - [SDR 2007FA0000812](https://openairdocs.org/sdr/2007FA0000812), Sep 19, 2007: QUILL ASSY. WORN. QUILL INTERNAL SPLINES WORN AND DAMAGED IN QUILL TUBE CONTACT AREA - [SDR 2006FA0001017](https://openairdocs.org/sdr/2006FA0001017), Oct 20, 2006: SUPPORT BRACKET. LOOSE. TAIL BOOM ELEVATOR SUPPORT BRACKET LOOSE. (WORKING RIVETS/SITE OF PREVIOUS REPAIR WITH PULL TYPE RIVETS). - [SDR 2006FA0000530](https://openairdocs.org/sdr/2006FA0000530), May 18, 2006: FITTING. CRACKED. TAIL BOOM ATTACH FITTING CRACKED UPPER LEFT [TAIL BOOM SIDE] - [SDR 2006FA0000529](https://openairdocs.org/sdr/2006FA0000529), May 18, 2006: FITTING. CRACKED. TAIL BOOM ATTACH FITTING CRACKED UPPER LEFT [TAIL BOOM SIDE] - [SDR 2006FA0000528](https://openairdocs.org/sdr/2006FA0000528), May 18, 2006: FITTING. CRACKED. TAIL BOOM ATTACH FITTING CRACKED UPPER LEFT [TAIL BOOM SIDE] - [SDR 2006FA0000231](https://openairdocs.org/sdr/2006FA0000231), Feb 27, 2006: FITTING. FRACTURED. AC LANDED FOR SHUTDOWN AFTER OPERATING FOR APPROX 3 FLIGHT HOURS, AC WAS SHAKING DURING SHUTDOWN. DURING POST FLIGHT INSP IT WAS FOUND THAT UPPER LT MOUNT HARD - [SDR ASI200501A](https://openairdocs.org/sdr/ASI200501A), Jul 15, 2005: PIN. FAILED. DURING 1200 OVERHAUL OUTBOARD FITTING/STRAP PIN P/N 204-012-104-005, S/N DIFS12334 WAS FOUND BROKEN IN HALF. PIN HAD 1085.1 HOURS SINCE NEW. DISCOLORATION AND C - [SDR ASI200501](https://openairdocs.org/sdr/ASI200501), Jul 15, 2005: PIN. FAILED. DURING 1200 OVERHAUL OUTBOARD FITTING/STRAP PIN WAS FOUND BROKEN IN HALF. PIN HAD 1085.1 HOURS SINCE NEW. DISCOLORATION AND CONDITION OF BREAK INDICATES THE BRE - [SDR 2005FA0000785](https://openairdocs.org/sdr/2005FA0000785), May 11, 2005: DRIVE SHAFT. VIBRATION. ( 2005-5-1) PILOT NOTICED VIBRATION AND RUMBLE COMING FROM THE MAIN TRANSMISSION AREA ON TAKEOFF. MECHANIC DID TROUBLE TROUBLESHOOTING PROCEDURES AND NOTICED ON - [SDR 2004FA0000333](https://openairdocs.org/sdr/2004FA0000333), Mar 25, 2004: STRAP. CRACKED. AIRCRAFT WAS EXPERIENCING VIBRATIONS DURING FLIGHT, MAINTENANCE WAS UNABLE TO REMOVE THE VIBRATION THROUGH TRACK AND BALANCE PROCEDURES. THE MAIN ROTOR ASSEMBLY - [SDR AGQA088876](https://openairdocs.org/sdr/AGQA088876), Aug 12, 2003: PUMP. BROKEN. PUMP PRODUCING FLUXUATING OIL PRESSURE - [SDR LS12003F00000](https://openairdocs.org/sdr/LS12003F00000), Jun 6, 2003: SKIN. CRACKED. THE TAILBOOM FIRST 2 UPPER SKINS HAD NUMEROUS CRACKS. UNDER NORMAL OPERATIONS THESE CRACKS WOULD NEVER MATERIALIZE. THE AIRCRAFT HAS BEEN DOING LIFTING WORK. MU - [SDR CDFROTW1](https://openairdocs.org/sdr/CDFROTW1), Apr 25, 2003: BATTERY. LEAKING. AT REMOVAL OF ELT BATTERY AT POSTED REMOVAL DATE IT WAS DISCOVERED THE BATTERY PACK HAD LEAKED AND CORRODED COMPONENTS WITHIN THE CASE. THERE WAS ALSO A CRACK N - [SDR AUS20021231](https://openairdocs.org/sdr/AUS20021231), Oct 15, 2002: FITTING. FAULTY. (AUS) TAILBOOM LH LOWER ATTACHMENT FITTING ON FUSELAGE HAD OVERSIZE HOLES ALLOWING THE HILOK' PINS TO LOOSEN. SUSPECT CAUSED BY POOR REPAIR WORK. - [SDR XVI2002F00000](https://openairdocs.org/sdr/XVI2002F00000), Apr 11, 2002: FRAME. CRACKED. X-RAY INSPECTION REVEALED A CRACK IN THE FRAME FLANGE APPROXIMATELY .1250 INCH LONG CONTAINED BY ADJACENT FASTENER HOLE. THE CRACK IS LOCTED IN THE 3 OCLOCK POS - [SDR LS1R074932](https://openairdocs.org/sdr/LS1R074932), Jul 20, 2001: CYLINDER. WORN. PART IS WORN EXCESSIVELY. - [SDR LS1R074916](https://openairdocs.org/sdr/LS1R074916), Jul 20, 2001: BATTERY. WEAK. PART IS WEAK. - [SDR LS1R072592](https://openairdocs.org/sdr/LS1R072592), Apr 16, 2001: REGULATOR. OUT OF ADJ. REGULATOR UNABLE TO HOLD ADJUSTMENT. - [SDR LS1R072590](https://openairdocs.org/sdr/LS1R072590), Apr 16, 2001: CONTROL PANEL. INOPERATIVE. LIGHTS WILL NOT COME ON. CONTROL PANEL INOPERATIVE. - [SDR LS1R072190](https://openairdocs.org/sdr/LS1R072190), Apr 10, 2001: CABLE DRUM. STRETCHED. CABLE DRUM STRETCHED. - [SDR LS1R071917](https://openairdocs.org/sdr/LS1R071917), Apr 6, 2001: SHAFT. WORN. PART IS WORN EXCESSIVELY. - [SDR LS1R071916](https://openairdocs.org/sdr/LS1R071916), Apr 6, 2001: SHAFT. WORN. PART IS WORN EXCESSIVELY. - [SDR 20010502CW005](https://openairdocs.org/sdr/20010502CW005), Apr 2, 2001: BLADE. CRACKED. A CRACK WAS NOTICED INSIDE DENT AFT OF THE SPAR ON THE TOP OF THE MAIN ROTOR BLADE. REMOVAL OF PAINT DETERMINED THE CRACK TO BE IN EXCESS OF 6 INCHES LONG. THE - [SDR 20001017SH029](https://openairdocs.org/sdr/20001017SH029), Sep 19, 2000: CROSSTUBE. CRACKED. DURING REFUEL, FOUND FORWARD CROSSTUBE AT RIGHT SADDLE CRACKED. POSSIBLE CAUSE, WEAR. (X) - [SDR 20001017SH030](https://openairdocs.org/sdr/20001017SH030), Sep 1, 2000: ANGLE. CRACKED. FOUND ANGLE CRACKED AT LEFT LOWER TAILBOOM MOUNT. POSSIBLE CAUSE IS STRESS TORQUE OF TAILBOOM TO FUSELAGE. (X) - [SDR LS1R066445](https://openairdocs.org/sdr/LS1R066445), Feb 29, 2000: BEARING. ROUGH. BEARING EXTREMELY ROUGH, AND RATCHETY. - [SDR LS1R066421](https://openairdocs.org/sdr/LS1R066421), Feb 23, 2000: BEARING. DAMAGED. BEARING SLINGING GREASE. - [SDR LS1R066420](https://openairdocs.org/sdr/LS1R066420), Feb 23, 2000: BEARING. DAMAGED. BEARING SLINGING GREASE. - [SDR LS1R066419](https://openairdocs.org/sdr/LS1R066419), Feb 23, 2000: BEARING. DAMAGED. BEARING SLINGING GREASE. - [SDR LS1R066011](https://openairdocs.org/sdr/LS1R066011), Feb 17, 2000: AUDIO PANEL. FAILED. ICS BOX DOES NOT TRANSMIT. - [SDR LS1R066010](https://openairdocs.org/sdr/LS1R066010), Feb 17, 2000: AUDIO PANEL. FAILED. ICS BOX DOES NOT TRANSMIT. - [SDR LS1R065962](https://openairdocs.org/sdr/LS1R065962), Feb 15, 2000: LINEAR ACTUATOR. INOP. LINEAR ACTUATOR IS INOPERATIVE. - [SDR LS1R065943](https://openairdocs.org/sdr/LS1R065943), Feb 11, 2000: VOLT REGULATOR. SHORTED. VOLTAGE REGULATOR SHORTED OUT. - [SDR LS1R065941](https://openairdocs.org/sdr/LS1R065941), Feb 11, 2000: CONTROLLER. FAILED. INTERPHONE DOES NOT TRANSMIT. - [SDR LS1R065936](https://openairdocs.org/sdr/LS1R065936), Feb 11, 2000: VOLT REGULATOR. SHORTED. VOLTAGE REGULATOR SHORTED OUT. - [SDR AGQA065942](https://openairdocs.org/sdr/AGQA065942), Feb 11, 2000: VOLT REGULATOR. INOPERATIVE. VOLTAGE REGULATOR INOPERABLE. WILL NOT REGULATE. - [SDR AGQA065935](https://openairdocs.org/sdr/AGQA065935), Feb 11, 2000: VOLT REGULATOR. INOPERATIVE. VOLTAGE REGULATOR INOPERABLE, WILL NOT REGULATE. All 93: https://openairdocs.org/model/arrow-falcon-exporters-uh-1h/reports.md ## STCs that may be installed (OpenAirDocs) (22) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SR12332SE](https://openairdocs.org/stc/SR12332SE): Installation of Mechanical Specialties, LLC Human External Cargo (HEC) and non-HEC Hook System. Mechanical Specialties, LLC - [STC SR02796SE](https://openairdocs.org/stc/SR02796SE): Installation of Human External Cargo (HEC) system. Boost Systems LLC - [STC SH8609SW](https://openairdocs.org/stc/SH8609SW): Fabrication of Isolair Eliminator II Model 4600-205 fire fighting system. Isolair Inc - [STC SR01776SE](https://openairdocs.org/stc/SR01776SE): Fabrication, installation, and maintenance of the Isolair Helicopters, Inc., Model 9002 High Cross tubes. Isolair Inc - [STC SR00143DE](https://openairdocs.org/stc/SR00143DE): Installation of an upgraded 42 degree Tail Rotor gearbox, P/N 212-040-003. Midwest Aerospace TC LLC - [STC SR02492LA](https://openairdocs.org/stc/SR02492LA): Installation of a Helicopter Technology Company main rotor blade assembly. Helicopter Technology Co - [STC SR02641SE](https://openairdocs.org/stc/SR02641SE): Installation of a Service Deck. Northwest Heli-Structures Inc - [STC SR02070SE](https://openairdocs.org/stc/SR02070SE): Fabrication of Dart D205-770-011 Replacement Engine Mount Kit. Dart Aerospace USA Inc - [STC SR00929SE](https://openairdocs.org/stc/SR00929SE): Fabrication of tail boom mounted strakes. BLR Aerospace LLC - [STC SR01470SE](https://openairdocs.org/stc/SR01470SE): Fabrication and Installation of Fast Fin System. BLR Aerospace LLC - [STC SR03408CH](https://openairdocs.org/stc/SR03408CH): Install Airwolf Aerospace, LLC Tension-Torsion Strap Assemblies, P/N AA-204-310-101-101 or AA-204-310-101-103. Airwolf Aerospace LLC - [STC SR02413LA](https://openairdocs.org/stc/SR02413LA): Installation of an AKV, Inc Exceedence and Trend Monitoring System kit P/N ETM1000. AKV Inc - [STC ST04270AT](https://openairdocs.org/stc/ST04270AT): Install the VTOL ASSALT V3 Windscreen Laminate Kit. VTOL LLC - [STC SR01742NY](https://openairdocs.org/stc/SR01742NY): Installation of extended height landing gear. Dart Aerospace Limited - [STC SR01196LA](https://openairdocs.org/stc/SR01196LA): Installation of Honeywell (Lycoming) T53-L-703 engine to replace Honeywell (Lycoming) T53-L-13/13B/-13BA engine. Responsible ACO is Los Angeles, NM-L. Minuteman Aviation Inc - [STC SR02051LA](https://openairdocs.org/stc/SR02051LA): Installation of a VAn Horn Aviation Tail Rotor Blade. Van Horn Aviation LLC - [STC SR01946SE](https://openairdocs.org/stc/SR01946SE): Installation of the Mechanical Specialties, Model UH606. Mechanical Specialties Inc - [STC SR09257RC](https://openairdocs.org/stc/SR09257RC): Fabrication, modification, and installation of a new vertical fin spar in accordance with Global Helicopter Technology, Inc., Drawing number VTF-030-800, Revision D, dated March 26, 2001, or later FAA approved revision. Global Spar LLC - [STC SR00103SE](https://openairdocs.org/stc/SR00103SE): Installation of Aviation Development Corporation oil filter. Aviation Development Corporation - [STC SR01298NY](https://openairdocs.org/stc/SR01298NY): Installation of replacement crosstubes P/N D212-664. Dart Aerospace Limited - [STC SR00563NY](https://openairdocs.org/stc/SR00563NY): Installation of Skidtubes and associated saddles. Dart Aerospace Limited - [STC SR01395NY](https://openairdocs.org/stc/SR01395NY): Installation of adjustable engine mount. Dart Aerospace Limited ## PMA parts (OpenAirDocs) (69, first 50) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first. - [650-430-100-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117790220120260512112134.0001): MECHANICAL SPECIALTIES, LLC MODEL 650-430-100-100ADVANCED DUEL EXTERNAL CARGO HOOK /ADEC™HOOK SYSTEM. Mechanical Specialties LLC · PMA PQ2180NM · Modification part · Apr 29, 2026 - [AG627000-13](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134320260320220809130828.0001): Gasket – Marker Beacon. Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Modification part · May 10, 2022 - [AG844000-23](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195221458420220809102505.0001): Gasket – UHF/VHF Antenna. Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Modification part · Apr 18, 2022 - [AG844000-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191230361020220408135722.0001): Gasket – UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Feb 8, 2022 - [AG728000-52](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162191710020220408135657.0001): Gasket – Satcom Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jan 26, 2022 - [AG627000-23](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158717923620220408135621.0001): Gasket – Marker Beacon. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 15, 2021 - [AG627000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138464412620220408140210.0001): Gasket – Marker Beacon Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021 - [AG358000-08](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125087130720220408135734.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021 - [“](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID341325238120210603195421.0001): “. Van Horn Aviation · PMA PQ2454NM · Mar 23, 2021 - [AG358000-07](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID357403392120210727195115.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 11, 2020 - [Master Document List (MDL) 204-MDL-001](https://drs.faa.gov/browse/excelExternalWindow/B7B368AF5851BC1E862582F9006A34CA.0001): Tail Rotor Blade. Van Horn Aviation · PMA PQ2454NM · Modification part · Jul 2, 2018 - [TAI-4010-481-001](https://drs.faa.gov/browse/excelExternalWindow/F807326BE4235B85862582DB00565953.0001): Nut, Mast, Main Rotor. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-010-481-001 · Jun 4, 2018 - [TAI-4010-720-003](https://drs.faa.gov/browse/excelExternalWindow/F6C009903E010FCC862582DB00565906.0001): Slider -Tail Rotor Assembly. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-010-720-003 · Jun 4, 2018 - [TAI-4040-306-011](https://drs.faa.gov/browse/excelExternalWindow/F20C400159BFD59C862582DB0056597B.0001): Sleeve Assembly, Spiral Bevel Gear, Hydraulic, Pump & Tachometer Drive, Transmission. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-040-306-011 · Jun 4, 2018 - [TAI-4012-107-1](https://drs.faa.gov/browse/excelExternalWindow/E74F5A5BCFF81E15862582DB00565962.0001): Sleeve, Seal, Strap Fitting Outboard M/R. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-012-107-1 · Jun 4, 2018 - [ASI-5011-711-101](https://drs.faa.gov/browse/excelExternalWindow/DF3DBD707008996A862582DB00565901.0001): Grip Assembly. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 205-011-711-101 · Jun 4, 2018 - [TAI-4040-815-001](https://drs.faa.gov/browse/excelExternalWindow/D9E505652B43F8B5862582DB00565927.0001): Bolt, Lift Link. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-040-815-1 · Jun 4, 2018 - [TAI-4040-514-001](https://drs.faa.gov/browse/excelExternalWindow/D2A9FC0640E2918A862582DB0056590B.0001): Glass, Sight Gage, Oil Gearbox. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-040-514-001 · Jun 4, 2018 - [TAI-4011-443-001](https://drs.faa.gov/browse/excelExternalWindow/C43F1B7A11B1A41F862582DB0056595F.0001): Bearing & Liner, Assembly. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-443-001 · Jun 4, 2018 - [TAI-4010-433-1](https://drs.faa.gov/browse/excelExternalWindow/C36E0968D0B2B979862582DB0056594D.0001): Bearing & Liner, Assembly. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-010-433-1 · Jun 4, 2018 - [ASI-4011-120-5](https://drs.faa.gov/browse/excelExternalWindow/BA88D40ADF39D435862582DB005658BB.0001): Pitch Horn Assembly, Main Rotor. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-120-5 · Jun 4, 2018 - [TAI-4040-386-001](https://drs.faa.gov/browse/excelExternalWindow/AE70D63859B86050862582DB00565981.0001): Case-Support, Bevel Gear, Transmission, Assembly of. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-040-386-1 · Jun 4, 2018 - [ASI-4011-403-1](https://drs.faa.gov/browse/excelExternalWindow/AA0201AAB98214FE862582DB005658E1.0001): Ring Assembly, Outer Swashplate. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-403-1 · Jun 4, 2018 - [TAISGT-522-002](https://drs.faa.gov/browse/excelExternalWindow/A9A7B9F55360FFAA862582DB00565929.0001): Wingshaft. Extex Engineered Products Inc · PMA PQ2203NM · Replaces SGT-522-2 · Jun 4, 2018 - [ASI-4011-151-1](https://drs.faa.gov/browse/excelExternalWindow/A721D48DB30AF69C862582DB005658D6.0001): Bolt - Blade, Main Rotor Assembly. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-151-1 · Jun 4, 2018 - [ASI-4011-180-1](https://drs.faa.gov/browse/excelExternalWindow/A4B2F3CEAD3AACA7862582DB005658DF.0001): Fitting, Drag Brace Assembly. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-180-1 · Jun 4, 2018 - [ASI-4040-811-1](https://drs.faa.gov/browse/excelExternalWindow/A45495326BB2DA22862582DB005658F3.0001): Clamp Assembly, Curvic Coupling, Tail Rotor Driveshaft. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-040-811-1 · Jun 4, 2018 - [TAISGT528-1](https://drs.faa.gov/browse/excelExternalWindow/9E75E4E7D3EE5AF9862582DB00565997.0001): Transparent Window. Extex Engineered Products Inc · PMA PQ2203NM · Replaces SGT528-1 · Jun 4, 2018 - [TAI-4040-359-1](https://drs.faa.gov/browse/excelExternalWindow/96DFEE8A38E9FBED862582DB00565909.0001): Case-Top, Transmission Assembly. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-040-359-1 · Jun 4, 2018 - [ASI-4011-121-113](https://drs.faa.gov/browse/excelExternalWindow/91FEDEAC4ACE2BD2862582DB005658C8.0001): Grip Assembly, Main Rotor. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-121-113 · Jun 4, 2018 - [204-011-409-1AL](https://drs.faa.gov/browse/excelExternalWindow/8A86E20A202CA199862582DB00565933.0001): Bearing Set, Ball. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-409-1 · Jun 4, 2018 - [TAI-4012-118-1](https://drs.faa.gov/browse/excelExternalWindow/889970960DCE6A63862582DB00565968.0001): Shield, Assembly, M/R. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-012-118-1 · Jun 4, 2018 - [ASI-4012-103-001](https://drs.faa.gov/browse/excelExternalWindow/83D8AE6F8CFFDDCE862582DB005658EC.0001): Fitting, Retention Strap, Outboard, Main Rotor. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-012-103-1 · Jun 4, 2018 - [ASI-4011-136-103](https://drs.faa.gov/browse/excelExternalWindow/809C7F48A370A3A4862582DB005658D4.0001): Clevis, Pitch Change, Main Rotor. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-136-103 · Jun 4, 2018 - [ASI-4011-171-3](https://drs.faa.gov/browse/excelExternalWindow/80211E740A2458B3862582DB005658DE.0001): Bolt, Pillow Block. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-171-3 · Jun 4, 2018 - [TAI-4011-122-001](https://drs.faa.gov/browse/excelExternalWindow/7B37C3E562A1271C862582DB00565954.0001): Liner Assembly, Trunnion Bearing, Main Rotor. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-122-001 · Jun 4, 2018 - [TAI-4012-106-1](https://drs.faa.gov/browse/excelExternalWindow/7601E818D6284F39862582DB00565961.0001): Nut, Yoke M/R. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-012-106-1 · Jun 4, 2018 - [ASI-4040-313-001](https://drs.faa.gov/browse/excelExternalWindow/6F6817CE65B03A89862582DB005658EF.0001): Spacer, Tail Rotor Drive Quill. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-040-313-1 · Jun 4, 2018 - [TAI-4011-425-1](https://drs.faa.gov/browse/excelExternalWindow/6F541843976D1DA0862582DB0056595E.0001): Liner, Outer Ring. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-425-1 · Jun 4, 2018 - [TAI-5011-711-101](https://drs.faa.gov/browse/excelExternalWindow/6218D42E894DA1B8862582DB00565928.0001): Grip Assembly - Steel, Tail Rotor. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 205-011-711-101 · Jun 4, 2018 - [TAI-4011-153-001](https://drs.faa.gov/browse/excelExternalWindow/5DD60C874EC5B949862582DB0056595A.0001): Nut, Blade Main Rotor. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-153-1 · Jun 4, 2018 - [TAI-4011-144-001](https://drs.faa.gov/browse/excelExternalWindow/5B1503ABCE77DE67862582DB00565959.0001): Nut, Drag Brace. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-144-001 · Jun 4, 2018 - [ASI-4010-404-1](https://drs.faa.gov/browse/excelExternalWindow/504EA5498A693738862582DB005658B3.0001): Ring Assembly Swashplate Gimbal. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-010-404-1 · Jun 4, 2018 - [204-011-430-1T](https://drs.faa.gov/browse/excelExternalWindow/4E8CAC2605B03DCE862582DB0056593A.0001): Bearing Ball, Thrust Swashplate. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-430-1 · Jun 4, 2018 - [TAI-4031-244-005](https://drs.faa.gov/browse/excelExternalWindow/4AFCFC91BCC5F720862582DB00565908.0001): Bolt, 5th Mount Assembly of. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-031-244-5 · Jun 4, 2018 - [ASI-4011-116-1](https://drs.faa.gov/browse/excelExternalWindow/4850B9B20E45A7D6862582DB005658B7.0001): Nut Retention Strap, Main Rotor. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-116-1 · Jun 4, 2018 - [TAI-2040-136-001](https://drs.faa.gov/browse/excelExternalWindow/4473953C854028FC862582DB0056594C.0001): Bearing. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 212-040-136-001 · Jun 4, 2018 - [TAI-4011-423-1](https://drs.faa.gov/browse/excelExternalWindow/43AEA9C9699CE28E862582DB0056595C.0001): Sleeve, Bearing Inner Race S/P Inner Ring. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-423-1 · Jun 4, 2018 - [TAI-5030-517-001](https://drs.faa.gov/browse/excelExternalWindow/39BBECB417A39BC9862582DB00565988.0001): Pin, Lower, Latch. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 205-030-517-001 · Jun 4, 2018 - [TAI-4011-130-1](https://drs.faa.gov/browse/excelExternalWindow/37EA743353239854862582DB00565955.0001): Liner, Outboard Bearing. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 204-011-130-1 · Jun 4, 2018 All of them: https://openairdocs.org/model/arrow-falcon-exporters-uh-1h/pma.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Bell UH-1H](https://openairdocs.org/model/bell-uh-1h): 289 registered aircraft, registry code 1181407 - [Garlick Helicopters UH-1H](https://openairdocs.org/model/garlick-helicopters-uh-1h): 7 registered aircraft, registry code 3740005 - [Northwest Rotorcraft UH-1H](https://openairdocs.org/model/northwest-rotorcraft-uh-1h): 6 registered aircraft, registry code 9640002 - [Williams Helicopter UH-1H](https://openairdocs.org/model/williams-helicopter-uh-1h): 6 registered aircraft, registry code 9790870 - [Southwest Florida UH-1H](https://openairdocs.org/model/southwest-florida-uh-1h): 3 registered aircraft, registry code 118141C - [Bell Helicopter UH-1H (205)](https://openairdocs.org/model/bell-helicopter-uh-1h-205): 3 registered aircraft, registry code 1181430 - [Richards Heavylift Helo UH-1H](https://openairdocs.org/model/richards-heavylift-helo-uh-1h): 2 registered aircraft, registry code 118142G - [Rotorcraft Development UH-1H](https://openairdocs.org/model/rotorcraft-development-uh-1h): 2 registered aircraft, registry code 3741202 - [Western International Avia UH-1H](https://openairdocs.org/model/western-international-avia-uh-1h): 2 registered aircraft, registry code 9640001 - [Precision Helicopters UH-1H](https://openairdocs.org/model/precision-helicopters-uh-1h): 1 registered aircraft, registry code 1181429 - [Lillquist Brien UH-1H](https://openairdocs.org/model/lillquist-brien-uh-1h): 0 registered aircraft, registry code 056244L - [Bell/Southern Aero UH-1H](https://openairdocs.org/model/bell-southern-aero-uh-1h): 0 registered aircraft, registry code 118141E --- 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.