# Kaman Aerospace K-1200 - Type: Aircraft model (FAA registry) - Registry code: 13027LS - Manufacturer (registry): KAMAN AEROSPACE CORP - Model: K-1200 - Aircraft type: Rotorcraft - Category: Rotorcraft - Engines: 1 · Turbo-shaft - Seats: 1 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS TR7BO](https://openairdocs.org/tcds/TR7BO) (OpenAirDocs) - Holder: Kaman Aerospace Corporation - Registered aircraft: 17 - Page: https://openairdocs.org/model/kaman-aerospace-k-1200 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 2016-08-21](https://openairdocs.org/ad/2016-08-21): Main Rotor Control · Kaman Aerospace K-1200. Effective May 31, 2016 - [AD 2015-14-04](https://openairdocs.org/ad/2015-14-04): Main Rotor MRB · Kaman Aerospace K-1200. Effective Aug 17, 2015 - [AD 2010-26-11](https://openairdocs.org/ad/2010-26-11): Main Rotor Blades · Kaman Aerospace K-1200. Effective Jan 5, 2011 - [AD 2004-13-26](https://openairdocs.org/ad/2004-13-26): Main rotor blade (blade) grips · Kaman Aerospace K-1200. Effective Jul 22, 2004 - [AD 2001-13-03 R1](https://openairdocs.org/ad/2001-13-03-R1): Flap clevis · Kaman Aerospace K-1200. Effective May 27, 2003 - [AD 2000-18-10](https://openairdocs.org/ad/2000-18-10): Sprag Clutches · Kaman Aerospace K-1200. Effective Sep 26, 2000 - [AD 99-26-04](https://openairdocs.org/ad/99-26-04): Clutch Assembly · Kaman Aerospace K-1200. Effective Feb 8, 2000 Historical (superseded or no longer in force): - [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021 - [AD 2001-13-03](https://openairdocs.org/ad/2001-13-03) (historical): Rotor Shaft and Teeter Pin Assembly · Kaman Aerospace K-1200. Effective Aug 1, 2001 ## Registered aircraft (17) - [N107MW](https://openairdocs.org/aircraft/N107MW): [Mountain West Helicopters Of Montana LLC](https://openairdocs.org/faa-owner/MOUNTAIN%20WEST%20HELICOPTERS%20OF%20MONTANA%20LLC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), S/N A94-0045 - [N10KA](https://openairdocs.org/aircraft/N10KA): [Kaman Aerospace Corp](https://openairdocs.org/faa-owner/KAMAN%20AEROSPACE%20CORP), [Bloomfield, CT](https://openairdocs.org/faa-place/CT/Bloomfield), built 1997, S/N A94-0021 - [N131KA](https://openairdocs.org/aircraft/N131KA): [Kaman Aerospace Corp](https://openairdocs.org/faa-owner/KAMAN%20AEROSPACE%20CORP), [Bloomfield, CT](https://openairdocs.org/faa-place/CT/Bloomfield), built 1993, S/N A94-0002, Non-citizen corporation, flight hours not reported - [N171PL](https://openairdocs.org/aircraft/N171PL): [Precision Lift LLC](https://openairdocs.org/faa-owner/PRECISION%20LIFT%20LLC), [La Grande, OR](https://openairdocs.org/faa-place/OR/La%20Grande), built 2018, S/N A94-0047 - [N267KA](https://openairdocs.org/aircraft/N267KA): [Timberline Helicopters Inc](https://openairdocs.org/faa-owner/TIMBERLINE%20HELICOPTERS%20INC), [Sandpoint, ID](https://openairdocs.org/faa-place/ID/Sandpoint), built 2003, S/N A94-0037 - [N314](https://openairdocs.org/aircraft/N314): [Central Copters Inc](https://openairdocs.org/faa-owner/CENTRAL%20COPTERS%20INC), [Bozeman, MT](https://openairdocs.org/faa-place/MT/Bozeman), built 2001, S/N A94-0032 - [N319WA](https://openairdocs.org/aircraft/N319WA): [Sky High Leasing LLC](https://openairdocs.org/faa-owner/SKY%20HIGH%20LEASING%20LLC), [Montrose, CO](https://openairdocs.org/faa-place/CO/Montrose), built 2019, S/N A94-0048 - [N357KA](https://openairdocs.org/aircraft/N357KA): [Heli 807 Leasing LLC](https://openairdocs.org/faa-owner/HELI%20807%20LEASING%20LLC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), built 2001, S/N A94-0028 - [N39HX](https://openairdocs.org/aircraft/N39HX): [Helicopter Express LLC](https://openairdocs.org/faa-owner/HELICOPTER%20EXPRESS%20LLC), [Chamblee, GA](https://openairdocs.org/faa-place/GA/Chamblee), built 2017, S/N A94-0042 - [N40HX](https://openairdocs.org/aircraft/N40HX): [Helicopter Express LLC](https://openairdocs.org/faa-owner/HELICOPTER%20EXPRESS%20LLC), [Chamblee, GA](https://openairdocs.org/faa-place/GA/Chamblee), built 2019, S/N A94-0051 - [N43HX](https://openairdocs.org/aircraft/N43HX): [Helicopter Express LLC](https://openairdocs.org/faa-owner/HELICOPTER%20EXPRESS%20LLC), [Chamblee, GA](https://openairdocs.org/faa-place/GA/Chamblee), built 2001, S/N A94-0029 - [N526MW](https://openairdocs.org/aircraft/N526MW): [Mountain West Helicopters LLC](https://openairdocs.org/faa-owner/MOUNTAIN%20WEST%20HELICOPTERS%20LLC), [Saratoga Springs, UT](https://openairdocs.org/faa-place/UT/Saratoga%20Springs), built 1994, S/N 0004 - [N674TH](https://openairdocs.org/aircraft/N674TH): [Timberline Helicopters Inc](https://openairdocs.org/faa-owner/TIMBERLINE%20HELICOPTERS%20INC), [Sandpoint, ID](https://openairdocs.org/faa-place/ID/Sandpoint), built 2004, S/N A94-0035 - [N675TH](https://openairdocs.org/aircraft/N675TH): [Timberline Helicopters Inc](https://openairdocs.org/faa-owner/TIMBERLINE%20HELICOPTERS%20INC), [Sandpoint, ID](https://openairdocs.org/faa-place/ID/Sandpoint), built 1998, S/N A94-0025 - [N767NA](https://openairdocs.org/aircraft/N767NA): [Dh Helicopter Inc](https://openairdocs.org/faa-owner/DH%20HELICOPTER%20INC), [Whitefield, ME](https://openairdocs.org/faa-place/ME/Whitefield), built 2022, S/N A94-0049 - [N88HX](https://openairdocs.org/aircraft/N88HX): [Helicopter Express LLC](https://openairdocs.org/faa-owner/HELICOPTER%20EXPRESS%20LLC), [Chamblee, GA](https://openairdocs.org/faa-place/GA/Chamblee), S/N A94-0054 - [N970MB](https://openairdocs.org/aircraft/N970MB): [Sky High Leasing LLC](https://openairdocs.org/faa-owner/SKY%20HIGH%20LEASING%20LLC), [Montrose, CO](https://openairdocs.org/faa-place/CO/Montrose), built 2021, S/N A94-0057 ## NTSB investigations (14) 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 CEN26FA247](https://openairdocs.org/ntsb/CEN26FA247), Jul 12, 2026: Kaman Aerospace K-1200 (N40HX), Silver Jack Reservoir, CO, substantial damage, 1 fatal, investigation ongoing - [NTSB CEN25LA334](https://openairdocs.org/ntsb/CEN25LA334), Aug 22, 2025: Kaman Aerospace K-1200 (N171PL), Eagle, CO, substantial damage. Probable cause: The pilot’s failure to maintain helicopter control which resulted in an uncontrolled descent and impact with terrain. - [NTSB WPR23LA097](https://openairdocs.org/ntsb/WPR23LA097), Jan 24, 2023: Kaman Aerospace K-1200 (N202WM), Sweet Home, OR, substantial damage. Probable cause: Improper installation of the hardware retaining the adjustment screw in the N2 topping governor lever and roller assembly, which resulted in a partial loss of engine power. - [NTSB WPR20LA283](https://openairdocs.org/ntsb/WPR20LA283), Aug 25, 2020: Kaman K 1200 (N314), Pine Grove, OR, substantial damage, 1 fatal. Probable cause: An in-flight breakup resulting from contact of the left rotor system with the right rotor system after an in-flight failure of a servo flap from a left rotor blade. - [NTSB GAA17CA146](https://openairdocs.org/ntsb/GAA17CA146), Mar 13, 2017: Kaman Aerospace K 1200 (N675TH), Julian, CA, substantial damage. Probable cause: The pilot’s failure to conduct a thru-flight walkaround inspection, which resulted in the engine cowling remaining open and subsequently separating from the helicopter and striking the main rotor… - [NTSB WPR10FA295](https://openairdocs.org/ntsb/WPR10FA295), Jun 16, 2010: Kaman Aerospace K-1200 (N134WC), Donnelly, ID, substantial damage, 1 fatal. Probable cause: The collision of two counter-rotating main rotor blades for undetermined reasons, which resulted in a loss of control. - [NTSB WPR09LA057](https://openairdocs.org/ntsb/WPR09LA057), Dec 17, 2008: Kaman K-1200 (N267KA), Santa Clarita, CA, substantial damage, 1 fatal. Probable cause: The helicopter's encounter with a gusty crosswind condition during engine start that exceeded the helicopter's demonstrated wind envelope. - [NTSB SEA06FA067](https://openairdocs.org/ntsb/SEA06FA067), Mar 17, 2006: Kaman K-1200 (N263KA), Dayville, OR, substantial damage, 1 fatal. Probable cause: The improper overhaul of the reduction gear box assembly and improper installation of the N1 seal and nut assembly lockcup by maintenance personnel, which resulted in failure of the reduction gear… - [NTSB SEA04LA082](https://openairdocs.org/ntsb/SEA04LA082), May 12, 2004: Kaman K-1200 (N162KA), West Fork, OR, substantial damage, 1 fatal. Probable cause: The pilot's failure to maintain adequate clearance with trees during logging operations. Contributing factors were the trees, mountainous (steeply sloped) terrain, and the pilot's decision to conduct… - [NTSB SEA03GA153](https://openairdocs.org/ntsb/SEA03GA153), Jul 26, 2003: Kaman K-1200 (N314KA), Keller, WA, destroyed, 1 fatal. Probable cause: Corrosion fatigue within the blade retention bolt bushing(s) of the main rotor blade grip resulting in fatigue, cracking and ultimate separation of the upper grip plate. The separation of the upper… - [NTSB SEA00LA129](https://openairdocs.org/ntsb/SEA00LA129), Jul 11, 2000: Kaman K-1200 (N311KA), Cusick, WA, substantial damage. Probable cause: The termination of power to the main rotor system as a result of the malfunction of the free-wheeling sprag clutch assembly, followed by the torsional overload separation of the engine adapter shaft.… - [NTSB SEA00FA015](https://openairdocs.org/ntsb/SEA00FA015), Nov 4, 1999: Kaman K-1200 (N164KA), Emida, ID, substantial damage. Probable cause: Failure of the splined engine adaptor as a result of torsional overstress. Factors include a worn freewheeling clutch assembly. - [NTSB SEA98LA065](https://openairdocs.org/ntsb/SEA98LA065), Apr 21, 1998: Kaman K-1200 (N224GM), La Grande, OR, substantial damage. Probable cause: The pilot's inadvertent shutdown of the engine with the FUEL/OIL shutoff switch. Contributing to the accident were: the manufacturer's inadequate location and design of the FUEL/OIL shutoff switch;… - [NTSB IAD98LA024](https://openairdocs.org/ntsb/IAD98LA024), Jan 27, 1998: Kaman K-1200 (N135KA), Bloomfield, CT, substantial damage. Probable cause: The pilot's failure to maintain control during autorotation, which resulted in an unleveled attitude touchdown, roll over, and collision with the ground. ## FAA accident and incident reports (21) 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 20260712008179A](https://openairdocs.org/incident/20260712008179A), Jul 12, 2026: Kaman Aerospace Corp K-1200 (N40HX), Gunnison, CO, Destroyed, 1 fatal. On July 12, 2026, about 1705 mountain daylight time, a Kaman aerospace corporation K-1200 (k-max) helicopter, [privacy data omitted], was substantially damaged… - [Accident 20250822011389A](https://openairdocs.org/incident/20250822011389A), Aug 22, 2025: Kaman Aerospace Corp K-1200 (N171PL), Eagle, CO, Substantial damage. On August 22nd 2025 a k-max helicopter that was participating in firefighting operations approached a position above a pond to fill up the external bucket.… - [Accident 20230124001399A](https://openairdocs.org/incident/20230124001399A), Jan 24, 2023: Kaman Aerospace Corp K-1200 (N202WM), Sweet Home, OR, Substantial damage. During an approach to a log landing insuffecient power was avaiable to arrest descent. Pilot commanded the release of the load form the hook. Aircraft settled… - [Accident 20200824014239A](https://openairdocs.org/incident/20200824014239A), Aug 24, 2020: Kaman Aerospace Corp K-1200 (N314), Pine Grove, OR, Destroyed, 1 fatal. During a fire-fighting bucket operation for the ?white river? Wildfire, the aircraft went down approximately 14 NM se of Mt. Hood into the white river. Records… - [Incident 20190607006079I](https://openairdocs.org/incident/20190607006079I), Jun 7, 2019: Kaman Aerospace Corp K-1200 (N805RA), Aniak, AK, Minor damage. The rotak K-1200 was dispatched to a landing zone with out prior confirmation the landing zone was safe to land on. While landing the blades struck a new roof… - [Accident 20170312002059A](https://openairdocs.org/incident/20170312002059A), Mar 12, 2017: Kaman Aerospace Corp K-1200 (N675TH), Julian, CA, Substantial damage. After landing and engine shutdown the pilot- in- command slid open the engine cowling to allow the engine to cool down for a quicker turn time.… - [Incident 20141105019449I](https://openairdocs.org/incident/20141105019449I), Nov 5, 2014: Kaman Aerospace Corp K-1200 (N674TH), White Salmon, WA, Minor damage. Pilot was conducting long line operations at a logging site. Dropped a load of logs and backed out of site, with aft cyclic at 40 PSI torque and allowed… - [Incident 20140810013209I](https://openairdocs.org/incident/20140810013209I), Aug 10, 2014: Kaman Aerospace Corp K-1200 (N674TH), Wenanchee, WA, Minor damage. Helicopter experienced an unknon annomilay with the rotor track, pilot landed helicopter without further incident. No injuries. - [Incident 20130630010869I](https://openairdocs.org/incident/20130630010869I), Jun 30, 2013: Kaman Aerospace Corp K-1200 (N674TH), Wenatchee, WA, Minor damage. Pilot initiated intentional autorotation but added power too late, too close to the ground. Aircraft landed "three point" hitting the tailboom and landing gear… - [Incident 20110804018829I](https://openairdocs.org/incident/20110804018829I), Aug 4, 2011: Kaman Aerospace Corp K-1200 (N675TH), Plaster City, CA, No damage. N675TH was conducting FAR 133 flight operations from Plaster City fly yard on 8-4-11. The first flight of the day consisted of an external load lift of an air… - [Accident 20100616035869A](https://openairdocs.org/incident/20100616035869A), Jun 16, 2010: Kaman Aeros K-1200 (N134WC), Donnelly, ID, Destroyed, 1 fatal. The pilot was manuevering after lifting a load during helicopter logging operations. During the manuever the rotor blades came apart and the lf pylon came off… - [Accident 20081217853909A](https://openairdocs.org/incident/20081217853909A), Dec 17, 2008: Kaman K1200 (N267KA), Santa Clarita, CA, Substantial damage, 1 fatal. On 12/17/2008 at 0930 after starting the helicopter the pilot reported that while at ground idle he felt a strong gust of wind. This lifted the rear and right… - [Accident 20060317008649A](https://openairdocs.org/incident/20060317008649A), Mar 17, 2006: Kaman K1200 (N263KA), Dayville, OR, Substantial damage, 1 fatal. (-23) During logging operations the pilot dropped the load and notified ground crew that he needed to go to service and would be right back. Witnesses stated… - [Accident 20040512021969A](https://openairdocs.org/incident/20040512021969A), May 12, 2004: Kaman K1200 (N162KA), Glendale, OR, Destroyed, 1 fatal. (-23) Pilot was logging trees, hit a tree with the main rotor blade. - [Accident 20030725017499A](https://openairdocs.org/incident/20030725017499A), Jul 25, 2003: Kaman K1200 (N314KA), Keller, WA, Destroyed, 1 fatal. (-23) N314KA/K-1200/SN: A940015 had been contracted by the united states department of the interior, bureau of indian affairs and was being operated as public… - [Accident 20000711007229A](https://openairdocs.org/incident/20000711007229A), Jul 11, 2000: Kaman K1200 (N311KA), Cusick, WA, No damage. (-23) Arrived on scene at approximately 0800. Took photos of accident site. With the assistance of roger wassman, Kaman aerospace, the k-flex input shaft was… - [Accident 19991104040849A](https://openairdocs.org/incident/19991104040849A), Nov 4, 1999: Kaman K1200 (N164KA), Emida, ID, No damage. (-23) There are no recommendations or corrective actions to be submitted at this time. However, when the test results for the engine adapter, engine test cell… - [Accident 19980421013329A](https://openairdocs.org/incident/19980421013329A), Apr 21, 1998: Kaman K1200 (N224GM), La Grande, OR, Substantial damage. Accidently turned off fuel switch instead of particle seperator on climbout. Switches close together. Poor design. (.4)the pilot reported that after takeoff,… - [Accident 19980127000649A](https://openairdocs.org/incident/19980127000649A), Jan 27, 1998: Kaman K1200 (N135KA), Bloomfield, CT, Substantial damage. FAA on familerization flight. During hovering autorotation drifted. Touched down left main gear and rolled over. (.19) on January 27, 1998, at 1150 eastern… - [Incident 19950910037919I](https://openairdocs.org/incident/19950910037919I), Sep 10, 1995: Kaman K1200 (N163KA), Atlantic Ocean, Minor damage. Landing on usns in Ocean. Deck moving on swells. Rotors struck pallets during hover landing. - [Incident 19950411016449I](https://openairdocs.org/incident/19950411016449I), Apr 11, 1995: Kaman K1200 (N135KA), Ukiah, CA, Minor damage. Narrative: on Tuesday, April 11, 1995, at approximately 1315 hrs. PST, Mr. Robert g. fulton, pilot in command of Kaman K-1200, N135KA, operated by Louisiana… ## Service difficulty reports (68, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2023F00178](https://openairdocs.org/sdr/2023F00178), May 22, 2023: SERVO. BROKEN. THERE WAS A CATASTROPHIC FAILURE OF THE LEFT HAND MAIN ROTOR SYSTEM CAUSING THE AIRCRAFT TO CRASH. A SERVO FLAP BROKE OFF WHILE THE PILOT WAS LIFTING AN EXTERNA - [SDR CA150410018](https://openairdocs.org/sdr/CA150410018), Apr 7, 2015: PIN. FAILED. (CAN) LT TEETER PIN SLIDING BEARING KARON BEARING SURFACE FAILURE CAUSE METAL TO METAL CONTACT WITH THE ROTOR HUB TEETER PIN BORE. THE RESULT WAS HEAVY WEAR TO - [SDR CA130116020](https://openairdocs.org/sdr/CA130116020), Jan 16, 2013: PANEL. INOPERATIVE. (CAN) DURING TROUBLESHOOTING OF THE FUEL QTY INDICATING SYS FOR A CALIBRATION DEFECT. THE ACFT WAS SUBSEQUENTLY DEFUELED AND THE AME NOTICED THAT THERE WAS NO L - [SDR CA081120004](https://openairdocs.org/sdr/CA081120004), Nov 16, 2008: MOUNT. CRACKED. (CAN) CRACK DISCOVERED ON LT FWD STRUT MOUNT FITTING. - [SDR CA070411003](https://openairdocs.org/sdr/CA070411003), Mar 17, 2007: DRIVE GEAR. DAMAGED. (CAN) DURING THE INITIAL START UP OF THE DAY, AT APPROX 10 PERCENT ROTOR RPM, AN ABNORMAL NOISE WAS HEARD COMING FROM THE POWER TRAIN AND A TRANSMISSION CHIP WA - [SDR CA050707005](https://openairdocs.org/sdr/CA050707005), Jun 24, 2005: HUB. WORN. (CAN) DURING LAG PIN REPLACEMENT BLADE WAS REMOVED. UPON REMOVAL OF BLADE HUB WAS INSPECTED AND THE PROBLEM WAS FOUND. THE UPPER SURFACE OF THE LOWER HUB HALF K - [SDR CA051115006](https://openairdocs.org/sdr/CA051115006), Jul 5, 2004: STRUCTURE. CRACKED. ON MAINTENANCE SHUTDOWN DURING A NORMAL HELI LOGGING DAY, DURING INSP OF FLIGHT CONTROLS THE APPRENTICE NOTICED SOME SMOKING COMING FROM THE BOTTOM CORNER OF TH - [SDR 2004FA0000423](https://openairdocs.org/sdr/2004FA0000423), Mar 25, 2004: PIN. UNSERVICEABLE. THE LEADING EDGE OF THE LT SIDE TEETER PIN WAS DAMAGED (MUSHROOMED). FURTHER INSPECTION SHOWED THAT THE HEAD SIDE OF THE INSIDE DIAMETER OF THE LINER THAT THE T - [SDR CA021120008](https://openairdocs.org/sdr/CA021120008), Nov 4, 2002: CLUTCH. FAILED. (CAN) PILOT HEARD A LOUD BANG AS HE WAS LOWERING A LOG ONTO LANDING WITH A SLIGHT DROP IN ALTITUDE. THE AIRCRAFT WAS LANDED AND THE MAIN DRIVE SHAFT BETWEEN ENG - [SDR CA021113004](https://openairdocs.org/sdr/CA021113004), Oct 31, 2002: NOZZLE. UNAPPROVED PART. (CAN) MILITARY PART FOUND INSTALLED ON ENGINE S/N LE-81004. INSTALLED PART MANUFACTURER CODE NUMBER IS 81996, (US MILITARY) IT SHOULD BE 91547. (HONEYWELL OEM) - [SDR 20010124CW005](https://openairdocs.org/sdr/20010124CW005), Dec 11, 2000: PUMP. SEIZED. O.O TIME SINCE OVERHAUL, TRANSMISSION OIL PUMP SEIZED MOMENTARILY, ON FIRST STARTUP AFTER INSTALLATION. DAMAGING TRANSMISSION INTERNAL OIL PUMP DRIVE GEAR. NO S - [SDR CA991027035](https://openairdocs.org/sdr/CA991027035), Sep 30, 1999: SKIN. CRACKED. (CAN) CIRCUMFERENTIAL CRACK ON FIRST PANEL AFT OF MOUNTING BRACKET. LEFT SIDE CRACK APPROXIMATELY 1 INCH LONG. MANUFACTURER CONTACTED AND REPAIR IMPLEMENTED. - [SDR CA981022003](https://openairdocs.org/sdr/CA981022003), Oct 7, 1998: BLADE. CRACKED. (CAN) ON SCHEDULED MAINT, CRACK ON TOP OF BLADE, 10.25 INCHES LONG FROM TRAILING EDGE FORWARD, 1/3 DISTANCE FROM HUB TO TIP, NEAR 'YELLOW' CENTER OF BALANCE STR - [SDR 98ZZZX3153](https://openairdocs.org/sdr/98ZZZX3153), Jul 12, 1998: PIN. DETACHED. AFTER PERFORMING ENGINE VIBRATION CHECK, PILOT LANDED AND NOTICED PIN ROLLING AROUND ON FLOOR. SHOWED PIN TO MECHANIC AND WAS IMMEDIATELY IDENTIFIED AS THE PIN - [SDR 98ZZZX1398](https://openairdocs.org/sdr/98ZZZX1398), Jan 29, 1998: CONTROL VALVE. FAILED. PARTICAL SEPARATOR PURGE VALVE INOPERABLE. INSTALLED NEW VALVE. - [SDR 98ZZZX1396](https://openairdocs.org/sdr/98ZZZX1396), Jan 16, 1998: GCU. FAILED. PILOT REPORTED GENENRATOR WILL NOT COME ON-LINE. REPLACED GENERATOR CONTROL UNIT. OPERATIONS NORMAL. - [SDR CA980302005](https://openairdocs.org/sdr/CA980302005), Jan 15, 1998: BOLT. WORN. (CAN) PLAY IN RUDDER CONTROL SYSTEM TRACED TO THE CONTROL BOLT CONNECTING THE CONTROL SPRING STRUT ASSY. TO THE PEDAL SYSTEM CONTROL TUBE. BOLT FOUND TO HAVE DE - [SDR 98ZZZX1411](https://openairdocs.org/sdr/98ZZZX1411), Jan 15, 1998: BLADE. DELAMINATED. NORMAL INSPECTION OF MAIN ROTOR BLADES FOUND DELAMINATED LOWER SURFACE INBOARD AT TIP. NO BLADE STRIKE. - [SDR 98ZZZX1410](https://openairdocs.org/sdr/98ZZZX1410), Jan 15, 1998: BLADE. DELAMINATED. NORMAL INSPECTION OF MAIN ROTOR BLADES FOUND DELAMINATED LOWER SURFACE INBOARD AT TIP. NO BLADE STRIKE. - [SDR 98ZZZX1408](https://openairdocs.org/sdr/98ZZZX1408), Jan 14, 1998: LIMITER. BINDING. PILOT REPORTED COLLECTIVE LIMITER BINDING HARD TO MOVE UP OR DOWN: 12 EACH LIMITERS WERE INSTALLED. AFTER EACH INSTALL, AIRCRAFT OPERATIONS REPORTED NORMAL. 12- - [SDR 98ZZZX1417](https://openairdocs.org/sdr/98ZZZX1417), Dec 30, 1997: INDICATOR. ERRATIC. LOAD ON HOOK INDICATOR ERRATIC. TT: 1,165 HOURS. - [SDR 98ZZZX1413](https://openairdocs.org/sdr/98ZZZX1413), Dec 30, 1997: TRANSMITTER. FLUCTUATIONS. PILOT REPORTED TORQUE INDICATOR FLUCTUATIONS 1.0 PSI TO 2.0 PSI. REMOVED S/N 4990-4-109. TOTAL TIME 517.8 HOURS. - [SDR 98ZZZX1406](https://openairdocs.org/sdr/98ZZZX1406), Dec 18, 1997: DAMPER. FAILED. STABILIZER DAMPER LEAKING AT SHAFT SEAL. RECOMMENDATIONS: ENGINE EXHAUST DIRECTED DOWN ON TAIL BOOM. EXCESSIVE HEAT BUILD UP CAUSING EXCESSIVE PRESSURE IN DAMPE - [SDR 97ZZZX4859](https://openairdocs.org/sdr/97ZZZX4859), Nov 6, 1997: OIL PUMP. DAMAGED. OIL PUMP SEIZED ON START-UP. NO SHEAR SHAFT WAS INCORPORATED IN OIL PUMP. SEIZURE CAUSED DAMAGE TO PUMP DRIVE RING GEAR TEETH INSIDE TRANSMISSION ASSY AS WELL A - [SDR 97ZZZX4858](https://openairdocs.org/sdr/97ZZZX4858), Nov 6, 1997: OIL PUMP. SEIZED. OIL PUMP SEIZED ON START-UP. NO SHEAR SHAFT WAS INCORPORATED IN OIL PUMP. SEIZURE CAUSED DAMAGE TO PUMP DRIVE RING GEAR TEETH INSIDE TRANSMISSION ASSY AS WELL A - [SDR 98ZZZX1409](https://openairdocs.org/sdr/98ZZZX1409), Nov 4, 1997: LOAD LINK. ERRATIC. EXTERNAL LOADS READING LIGHT ERRATIC. - [SDR 98ZZZX1405](https://openairdocs.org/sdr/98ZZZX1405), Sep 30, 1997: DAMPER. FAILED. STABILIZER DAMPER LEAKING AT SHAFT SEAL. RECOMMENDATIONS: ENGINE EXHAUST DIRECTED DOWN ON TAIL BOOM. EXCESSIVE HEAT BUILD UP CAUSING EXCESSIVE PRESSURE IN DAMPE - [SDR 98ZZZX1403](https://openairdocs.org/sdr/98ZZZX1403), Sep 18, 1997: GPS. DEFECTIVE. GPS LT CONTROL ROTOR KNOB STICKING. - [SDR 98ZZZX1407](https://openairdocs.org/sdr/98ZZZX1407), Sep 10, 1997: DUAL TACH. FAILED. DUAL TACH FAILED. ROTOR NEEDLE INOPERATIVE. - [SDR 98ZZZX1402](https://openairdocs.org/sdr/98ZZZX1402), Aug 27, 1997: IDLERCRANK BRG. FAILED. IDLERCRANK BEARING FAILURES FOUND DURING NORMAL INSPECTION. - [SDR 98ZZZX1401](https://openairdocs.org/sdr/98ZZZX1401), Aug 27, 1997: IDLERCRANK BRG. FAILED. IDLERCRANK BEARING FAILURES FOUND DURING NORMAL INSPECTION. - [SDR 97ZZZX3979](https://openairdocs.org/sdr/97ZZZX3979), Aug 26, 1997: BLADE. CRACKED. WHILE PERFORMING POST-FLIGHT INSPECTION, MECHANIC SAW WHAT APPEARED TO BE A CRACK IN THE UPPER SURFACE OF M/R BLADE SKIN. UPON FURTHER INSPECTION, FOUND THE SKI - [SDR 98ZZZX1400](https://openairdocs.org/sdr/98ZZZX1400), Aug 21, 1997: IDLERCRANK BRG. FAILED. IDLERCRANK BEARING FAILURES FOUND DURING NORMAL INSPECTION. - [SDR 98ZZZX1399](https://openairdocs.org/sdr/98ZZZX1399), Aug 21, 1997: IDLERCRANK BRG. FAILED. IDLERCRANK BEARING FAILURES FOUND DURING NORMAL INSPECTION. - [SDR 98ZZZX1412](https://openairdocs.org/sdr/98ZZZX1412), Aug 20, 1997: TRANSMITTER. FLUCTUATIONS. PILOT REPORTED TORQUE INDICATOR FLUCTUATIONS 1.0 PSI TO 2.0 PSI. RMEOVED S/N 4755-4-260. TOTAL TIME 912.0 HOURS. - [SDR 98ZZZX1404](https://openairdocs.org/sdr/98ZZZX1404), Aug 4, 1997: DAMPER. FAILED. STABILIZER DAMPER LEAKING AT SHAFT SEAL. RECOMMENDATIONS: ENGINE EXHAUST DIRECTED DOWN ON TAIL BOOM. EXCESSIVE HEAT BUILD UP CAUSING EXCESSIVE PRESSURE IN DAMPE - [SDR 98ZZZX1397](https://openairdocs.org/sdr/98ZZZX1397), Jul 8, 1997: OIL TANK. CRACKED. TRANSMISSON OIL TANK CRACK ON TOP AT VENT LINE FITTING. - [SDR 98ZZZX1414](https://openairdocs.org/sdr/98ZZZX1414), Jun 21, 1997: INDICATOR. FAILED. PILOT REPORTED ENGINE OIL PRESSURE DROPPED TO ZERO. NO CAUTION LIGHT. INSTALLED NEW INDICATOR, OPERATION NORMAL. - [SDR 98ZZZX1394](https://openairdocs.org/sdr/98ZZZX1394), Jun 17, 1997: FAN ASSY. FAILED. CABIN HEAT FAN ASSY HOT AND VIBRATION. BEARING FAILURE. PART TT: 257.8 HOURS. SUSPECT CAUSE: ENGINE BLEED AIR PASSES THROUGH FAN ASSY TRANSFERRING HEAT TO BEARI - [SDR 98ZZZX1395](https://openairdocs.org/sdr/98ZZZX1395), Jun 4, 1997: CHIP DETECTOR. DEFECTIVE. REMOVAL FOR NORMAL INSPECTION FOUND PHENOLIC RING MISSING FROM TIP. TT: 456.9 HOURS. - [SDR 98ZZZX1391](https://openairdocs.org/sdr/98ZZZX1391), Jun 2, 1997: INDICATOR. FAILED. TORQUE INDICATOR'S FIRST LED SEGMENT WILL NOT ILLUMINATE. - [SDR 98ZZZX1393](https://openairdocs.org/sdr/98ZZZX1393), May 8, 1997: FAN ASSY. FAILED. CABIN HEAT FAN ASSY HOT AND VIBRATION. PART TT: 47.3 HOURS. BEARING FAILURE. SUSPECT CAUSE: ENGINE BLEED AIR PASSES THROUGH FAN ASSY TRANSFERRING HEAT TO BEARIN - [SDR 98ZZZX1416](https://openairdocs.org/sdr/98ZZZX1416), May 7, 1997: INDICATOR. ERRATIC. LOAD ON HOOK INDICATOR ERRATIC. - [SDR 98ZZZX1392](https://openairdocs.org/sdr/98ZZZX1392), Apr 29, 1997: FAN ASSY. FAILED. CABIN HEAT FAN ASSY INOPERABLE. PART TT: 233.8 HOURS. SUSPECT CAUSE: ENGINE BLEED AIR PASSES THROUGH FAN ASSY TRANSFERRING HEAT TO BEARINGS. - [SDR CA970430001](https://openairdocs.org/sdr/CA970430001), Apr 22, 1997: SKIN. CRACKED. (CAN) FUSELAGE SKIN AT STA 183.0, LBL 24.75 - 28.0 FOUND CRACKED. THE CRACK APPEARS TO HAVE ORIGINATED ON THE LEFT HAND EDGE OF THE SKIN AND PROPAGATED INBOARD - [SDR 98ZZZX1415](https://openairdocs.org/sdr/98ZZZX1415), Mar 27, 1997: INDICATOR. ERRATIC. LOAD ON HOOK INDICATOR ERRATIC. TT 71 HOURS. - [SDR 98ZZZX1016](https://openairdocs.org/sdr/98ZZZX1016), Jan 20, 1997: OIL PUMP. FAILED. HAD TO REMOVE TRANSMISSION FOR DAMAGED OIL PUMP DRIVE GEAR CAUSED FROM OIL PUMP SEIZURE (NO SHEAR SHAFT ON OIL PUMP). DATE OF INCIDENT 1-20-97. - [SDR 97ZZZX213](https://openairdocs.org/sdr/97ZZZX213), Dec 20, 1996: GEAR. PIN FAILED. N2 FAILURE OCCURRED. UPON ENGINE DISASSEMBLY AND INSP, FAILURE WAS CAUSED BY LOCK PIN AN 122683 HOLDING BEARING SLEEVE IN GEAR 1-070-062-04 FALLING OUT ALLOWING - [SDR 97ZZZX347](https://openairdocs.org/sdr/97ZZZX347), Dec 15, 1996: GOVERNOR. FAILED. OVERSPEED GOVERNOR FAILED. PILOT WAS FORCED TO JETTISON LONG LINE, HOOKS, AND LOGS. PILOT AUTOROTATED TOWARDS SERVICE LANDING, WENT T EMERGENCY GOVERNOR SETTIN - [SDR CA961112049](https://openairdocs.org/sdr/CA961112049), Oct 25, 1996: FRAME. CRACKED. (CAN) DURING A ROUTINE INSPECTION THE AME DISCOVERED 2 HORIZONTAL CRACKS AT STA.115.0, WL 85.0, LBL 15 INCHES. BOTH CRACKS ORIGINATE AT BOLT HOLE AND PROPAGATE All 68: https://openairdocs.org/model/kaman-aerospace-k-1200/reports.md ## STCs that may be installed (OpenAirDocs) (11) 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 SR04464NY](https://openairdocs.org/stc/SR04464NY): Installation of the iPad Mount. Avio Design Group Inc - [STC SR01767SE](https://openairdocs.org/stc/SR01767SE): Manufacture of Isolair Eliminator Model 4600-K1200 Fire Fighting System. Isolair Inc - [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc - [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC - [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SR02394AK](https://openairdocs.org/stc/SR02394AK): Replacement of existing landing and/or hover light bulbs with Light Emitting Diode (LED) lighting system. Seaplanes North LLC - [STC SR00103SE](https://openairdocs.org/stc/SR00103SE): Installation of Aviation Development Corporation oil filter. Aviation Development Corporation - [STC SR01561SE](https://openairdocs.org/stc/SR01561SE): Installation of the Model 36300 Auxiliary Hydraulic System. Kawak Aviation Technologies Inc - [STC SR01587SE](https://openairdocs.org/stc/SR01587SE): Installation of the Model 36400 Fire Tank System. Kawak Aviation Technologies Inc - [STC SR00811NY](https://openairdocs.org/stc/SR00811NY): Installation of Technisonic Industries Limited TFM-138 series transceiver models. Technisonic Industries Limited - [STC SR01834NY](https://openairdocs.org/stc/SR01834NY): Installation of Globalstar Satellite Telephone System. Atlantic Avionics Inc ## PMA parts (OpenAirDocs) (36) 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. - [01-0790906-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177448894920220610124311.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Jun 6, 2022 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115107808220210622142452.0001): AeroLEDs LLC · PMA PQ5259NM · Jan 13, 2021 - [87-05208-001](https://drs.faa.gov/browse/excelExternalWindow/C4B8A8A2B2422B728625822E007853B6.0001): Assembly, Light, PAR 46 Landing. Astronics Luminescent Systems Inc · PMA PQ0786NE · Replaces 01-0790750-20 · Jan 23, 2018 - [3038-8](https://drs.faa.gov/browse/excelExternalWindow/C1AC1632FE672797862581DA0064BAF0.0001): Pump Assembly. Meggitt Safety Systems Inc · PMA PQ0303NM · Replaces K974120-109 · Oct 18, 2017 - [ADB47412Y6](https://drs.faa.gov/browse/excelExternalWindow/540131F0E58EEA1486257A610055E857.0001): Fuel Filter Assembly. Pall Aeropower Corporation · PMA PQ1063CE · Replaces AD-B474-12Y6 · May 15, 2012 - [ADB24512Y5](https://drs.faa.gov/browse/excelExternalWindow/2744A8268281C1FC86257A610055E853.0001): Oil Filter Assembly. Pall Aeropower Corporation · PMA PQ1063CE · Replaces AD-B245-12Y5 · May 15, 2012 - [AD32558Y67](https://drs.faa.gov/browse/excelExternalWindow/09EF38DB1A171A6786257A610055E854.0001): Lube Filter Assembly. Pall Aeropower Corporation · PMA PQ1063CE · Replaces AD-3255-8Y67 · May 15, 2012 - [RA2C27-3](https://drs.faa.gov/browse/excelExternalWindow/493595C8AB346D3C862579A5005D5716.0001): Electric Fuel Boost Pump. Rapco Inc · PMA PQ2101CE · Replaces Airborne P/N 2C27-3 · Feb 9, 2012 - [RA2C27-3](https://drs.faa.gov/browse/excelExternalWindow/A9394D308C95BADB862579640059F6C0.0001): Electric Fuel Boost Pump. Rapco Inc · PMA PQ2101CE · Replaces Airborne P/N 2C27-3 · Nov 13, 2011 - [AYLC-52301](https://drs.faa.gov/browse/excelExternalWindow/8FE3B214264025E68625744B006E32DF.0001): ACTUATOR, ROTARY CYCLIC TRIM. GE Aviation Systems LLC (formerly Smiths and Barbar Coleman) · PMA PQ2047CE · Replaces K983162-001 · Apr 21, 2008 - [SYLC-52285](https://drs.faa.gov/browse/excelExternalWindow/791EA043CA9477098625744B006E331E.0001): ACTUATOR. GE Aviation Systems LLC (formerly Smiths and Barbar Coleman) · PMA PQ2047CE · Replaces K983160-3 · Apr 21, 2008 - [SYLC-52286](https://drs.faa.gov/browse/excelExternalWindow/39B05B81BAB427508625744B006E3334.0001): LINEAR ACTUATOR, RPM CONTROL. GE Aviation Systems LLC (formerly Smiths and Barbar Coleman) · PMA PQ2047CE · Replaces K983161-1 · Apr 21, 2008 - [AYLC-52306](https://drs.faa.gov/browse/excelExternalWindow/31632088093E635F8625744B006E32FD.0001): ACTUATOR, ROTARY CYCLIC TRIM. GE Aviation Systems LLC (formerly Smiths and Barbar Coleman) · PMA PQ2047CE · Replaces K983179-001 · Apr 21, 2008 - [SYLC-52285](https://drs.faa.gov/browse/excelExternalWindow/ED62E8195087F38C8625738D00706BA7.0001): ACTUATOR. GE Aviation Systems LLC (formerly Smiths and Barbar Coleman) · PMA PQ2047CE · Replaces K983160-3 · Nov 4, 2007 - [AYLC-52306](https://drs.faa.gov/browse/excelExternalWindow/E42D9978CDA4383F8625738D00706B7D.0001): ACTUATOR, ROTARY CYCLIC TRIM. GE Aviation Systems LLC (formerly Smiths and Barbar Coleman) · PMA PQ2047CE · Replaces K983179-001 · Nov 4, 2007 - [AYLC-52301](https://drs.faa.gov/browse/excelExternalWindow/D31EF3412004B6C58625738D00706B47.0001): ACTUATOR, ROTARY CYCLIC TRIM. GE Aviation Systems LLC (formerly Smiths and Barbar Coleman) · PMA PQ2047CE · Replaces K983162-001 · Nov 4, 2007 - [SYLC-52286](https://drs.faa.gov/browse/excelExternalWindow/9186D7E874D736F88625738D00706BD3.0001): LINEAR ACTUATOR, RPM CONTROL. GE Aviation Systems LLC (formerly Smiths and Barbar Coleman) · PMA PQ2047CE · Replaces K983161-1 · Nov 4, 2007 - [AYLC-52301](https://drs.faa.gov/browse/excelExternalWindow/D47F51BE3B479A2A86257292006AC857.0001): Actuator, Rotary Cyclic Trim. GE Aviation Systems LLC (formerly Smiths and Barbar Coleman) · PMA PQ2047CE · Replaces K983162-001 · Feb 5, 2007 - [AYLC-52306](https://drs.faa.gov/browse/excelExternalWindow/B1DB372980F4DE4A86257292006AC88C.0001): Actuator, Rotary Cyclic Trim. GE Aviation Systems LLC (formerly Smiths and Barbar Coleman) · PMA PQ2047CE · Replaces K983179-001 · Feb 5, 2007 - [SYLC-52285](https://drs.faa.gov/browse/excelExternalWindow/96A7701915D8155B86257292006AC7F5.0001): Actuator, Linear. GE Aviation Systems LLC (formerly Smiths and Barbar Coleman) · PMA PQ2047CE · Replaces K983160-3 · Feb 5, 2007 - [SYLC-52286](https://drs.faa.gov/browse/excelExternalWindow/1BA5E0C12A56D97286257292006AC827.0001): Actuator, Linear. GE Aviation Systems LLC (formerly Smiths and Barbar Coleman) · PMA PQ2047CE · Replaces K983161-1 · Feb 5, 2007 - [36300-401](https://drs.faa.gov/browse/excelExternalWindow/75D6F33571C68459862572A500623BE7.0001): Auxiliary Hydraulic System Kit, K-Max K1200 Helicopter. Kawak Aviation Technologies Inc · PMA PQ1998NM · Modification part · Aug 24, 2006 - [36300-402](https://drs.faa.gov/browse/excelExternalWindow/421C99A0ADF7F52F862572A500623C19.0001): Auxiliary Hydraulic System Kit, K-Max K1200 Helicopter. Kawak Aviation Technologies Inc · PMA PQ1998NM · Modification part · Aug 24, 2006 - [36400-401](https://drs.faa.gov/browse/excelExternalWindow/2B6D5B360BE40245862572A500623BB9.0001): K-Max K-1200 Helicopter Fire Tank System. Kawak Aviation Technologies Inc · PMA PQ1998NM · Modification part · Aug 24, 2006 - [9750W0538](https://drs.faa.gov/browse/excelExternalWindow/0F669128083B2005862570670060CF94.0001): Sealed Lead-Acid Battery, 24V/40Ah. EnerSys Energy Products Inc · PMA PQ3810CE-D · Replaces Concorde RG380E/40B · Apr 4, 2005 - [9750W0538](https://drs.faa.gov/browse/excelExternalWindow/DEC502F7873D09388525704200515948.0001): Sealed Lead-Acid Battery, 24V/40Ah. EnerSys Energy Products Inc · Replaces Concorde RG380E/40B · Nov 14, 2004 - [3038-7](https://drs.faa.gov/browse/excelExternalWindow/445D226CD33BF19985257046005D6CEC.0001): Pump Assembly, lube, scavenge & hydraulic. Mewggitt Airdynamics Inc · Replaces K974120-107 · May 2, 2004 - [3038-8](https://drs.faa.gov/browse/excelExternalWindow/13FC3A7808877E9285257046005D6CED.0001): Pump Assembly, lube, scavenge & hydraulic. Mewggitt Airdynamics Inc · Replaces K974120-109 · May 2, 2004 - [9750W0538](https://drs.faa.gov/browse/excelExternalWindow/5BCEB609EB56B42F8525704200515571.0001): Sealed Lead-Acid Battery, 24V/40Ah. EnerSys Energy Products Inc · Replaces Concorde RG380E/40B · Nov 28, 2001 - [3038-7](https://drs.faa.gov/browse/excelExternalWindow/B9E0805424F3C371852570440054EE9D.0001): Pump Assembly, lube, scavenge & hydraulic. Howden Airdynamics · Replaces K974120 · Jun 4, 2000 - [3038-7](https://drs.faa.gov/browse/excelExternalWindow/CB570C068BEAE51B852570440054ED75.0001): Pump Assembly. Howden Fluid Systems · Replaces Kaman K974120-107 · Sep 30, 1996 - [2C27-3FR](https://drs.faa.gov/browse/excelExternalWindow/34CC8E37512F15858525704A0053D219.0001): Factory Rebuilt Fuel Pump. Parker Hannifin Corp, Nichols Airborne Division · Replaces Airborne 2C27-3 · Aug 26, 1996 - [AD-B245-12Y5](https://drs.faa.gov/browse/excelExternalWindow/979CBA53516E3DB2852570460060DCB9.0001): PAC/APM Oil Filter Assembly (Lube). Pall Aeropower Corp · Replaces AD-B245-12Y5 · Jul 25, 1996 - [AD-B474-12Y6](https://drs.faa.gov/browse/excelExternalWindow/6AB9C9BF0D164367852570460060DCBA.0001): PAC/APM Filter Assembly (Fuel). Pall Aeropower Corp · Replaces AD-B474-12Y6 · Jul 25, 1996 - [AD-3255-8Y67](https://drs.faa.gov/browse/excelExternalWindow/3F41DD054C7868BE852570460060DCB3.0001): PAC/APM Filter Assembly (Lube). Pall Aeropower Corp · Replaces AD-3255-8Y67 · Jul 25, 1996 - [RG380E/40B](https://drs.faa.gov/browse/excelExternalWindow/FEA80BE23A04C0108525703F004DD18D.0001): Battery. Concorde Battery Corp · PMA PQ1174NM · Modification part · Jun 20, 1996 ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Kiwi Technologies K1200](https://openairdocs.org/model/kiwi-technologies-k1200): 0 registered aircraft, registry code 061014U --- 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.