# Agusta 206A - Type: Aircraft model (FAA registry) - Registry code: 0260301 - Manufacturer (registry): AGUSTA SPA - Model: 206A - Aircraft type: Rotorcraft - Category: Rotorcraft - Engines: 1 · Turbo-shaft - Seats: 5 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) (OpenAirDocs) - Holder: Bell Textron Canada Limited - Registered aircraft: 0 - Page: https://openairdocs.org/model/agusta-206a 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 2024-20-07](https://openairdocs.org/ad/2024-20-07): Emergency Equipment; Emergency Flotation Section · Apical Emergency Float Kit, P/N 20498 (STC SR00780LA or 12 others). Effective Dec 5, 2024 - [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023 - [AD 2023-06-05](https://openairdocs.org/ad/2023-06-05): Tail Rotor Drive Shaft · Bell Textron Canada 206A, 206A-1 (OH-58A), 206B and 5 more. Effective May 19, 2023 - [AD 2022-20-04](https://openairdocs.org/ad/2022-20-04): Tail Rotor Drive Shaft · Bell Textron Canada 206, 206A, 206A-1 (OH-58A) and 6 more. Effective Dec 23, 2022 - [AD 2021-19-01](https://openairdocs.org/ad/2021-19-01): Cabin Equipment/Furnishings · Shoulder harness restraint system (Bell Helicopter Textron STC SH2073SO or SH2751SO). Effective Oct 13, 2021 - [AD 2021-15-06](https://openairdocs.org/ad/2021-15-06): Tail Rotor Drive · Bell Textron Canada 206A, 206B, 206L and 3 more. Effective Aug 27, 2021 - [AD 2019-08-10](https://openairdocs.org/ad/2019-08-10): Main Rotor Drive System · Bell Helicopter Textron Canada 206A, 206B, 206L and 4 more. Effective Jun 24, 2019 - [AD 2018-25-17](https://openairdocs.org/ad/2018-25-17): Air Conditioning System Wiring · Airbus Helicopters 206A, 206B, 206L and 13 more. Effective Jan 22, 2019 - [AD 2017-05-04](https://openairdocs.org/ad/2017-05-04): Tension Torsion Strap · Bell Helicopter Textron Canada 206A, 206B, 206L and 3 more. Effective Mar 17, 2017 - [AD 2013-22-21](https://openairdocs.org/ad/2013-22-21): Emergency Flotation Section · Apical Industries, Inc. Emergency Float Kits (Dart Aerospace ULC STC SR01535LA). Effective Dec 13, 2013 - [AD 2013-18-06](https://openairdocs.org/ad/2013-18-06): Main Rotor Control · Bell Helicopter Textron Canada 206A, 206B, 206L and 10 more. Effective Oct 17, 2013 - [AD 2013-18-03](https://openairdocs.org/ad/2013-18-03): Ignition Power Supply · Bell Helicopter Textron Canada 206A, 206B and 206L. Effective Oct 11, 2013 - [AD 2012-12-11](https://openairdocs.org/ad/2012-12-11): Engine EFT/TOT Indicating System · Supplemental lighting system (Aviation Specialties Unlimited STC SR01383SE). Effective Jul 24, 2012 - [AD 2011-25-01](https://openairdocs.org/ad/2011-25-01): Liferafts · Agusta AB412, AB412 EP, 206A and 23 more. Effective Jan 17, 2012 - [AD 2010-26-51](https://openairdocs.org/ad/2010-26-51): Tail rotor blade · Bell Helicopter Textron Canada 206A, 206B, 206L and 10 more. Effective Mar 25, 2011 - [AD 2009-07-52](https://openairdocs.org/ad/2009-07-52): Cyclic control lever assembly · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 7 more. Effective May 1, 2009 - [AD 2008-14-03](https://openairdocs.org/ad/2008-14-03): Tailboom attachment · Bell Helicopter Textron Canada 206A, 206B, 206L and 3 more. Effective Aug 14, 2008 - [AD 2007-25-07](https://openairdocs.org/ad/2007-25-07): Fin support · Bell Helicopter Textron Canada 206A and 206B. Effective Jan 14, 2008 - [AD 2007-23-17](https://openairdocs.org/ad/2007-23-17): Main rotor latch bolts · Bell Helicopter Textron Canada 206A and 206B. Effective Dec 6, 2007 - [AD 2007-22-01](https://openairdocs.org/ad/2007-22-01): Spindle · Bell Helicopter Textron Canada 206A and 206B. Effective Nov 6, 2007 - [AD 2007-01-06](https://openairdocs.org/ad/2007-01-06): Tail rotor blade (blade) · Bell Helicopter Textron Canada 206A, 206B, 206L and 3 more. Effective Feb 13, 2007 - [AD 2005-21-03](https://openairdocs.org/ad/2005-21-03): Tail rotor blade (blade) root doublers (doublers) · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 5 more. Effective Nov 21, 2005 - [AD 2005-16-04](https://openairdocs.org/ad/2005-16-04): High forward crosstube · Bell Helicopter Textron Canada 206A and 206B with STC SH1392SO. Effective Sep 12, 2005 - [AD 2003-13-14](https://openairdocs.org/ad/2003-13-14): Chip detector · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 5 more. Effective Aug 12, 2003 - [AD 2002-20-05](https://openairdocs.org/ad/2002-20-05): Rescue hoists · Agusta A109, A109A, A109A II and 31 more. Effective Nov 7, 2002 - [AD 81-18-01 R1](https://openairdocs.org/ad/81-18-01-R1): Trunnion · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 3 more. Effective Jan 15, 2002 - [AD 2001-02-03](https://openairdocs.org/ad/2001-02-03): Raised Forging Boss · Bell Helicopter Textron Canada 206A, 206B, 206L and 2 more. Effective Mar 9, 2001 - [AD 96-06-04](https://openairdocs.org/ad/96-06-04): Driveshaft Assembly Inspection · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 1 more. Effective Apr 25, 1996 - [AD 95-11-14](https://openairdocs.org/ad/95-11-14): Crosstubes · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 5 more. Effective Jun 30, 1995 - [AD 95-09-06](https://openairdocs.org/ad/95-09-06): Fuel Valve Switch · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 4 more. Effective Jun 8, 1995 - [AD 94-24-11](https://openairdocs.org/ad/94-24-11): Tail Rotor Drive Shaft · Bell Helicopter Textron Canada 206A, 206B, 206L and 2 more. Effective Jan 6, 1995 - [AD 94-20-03](https://openairdocs.org/ad/94-20-03): Main Rotor Hub Trunnion · Bell Helicopter Textron Canada 206A, 206B, 206B-1 and 4 more. Effective Oct 11, 1994 - [AD 94-19-02](https://openairdocs.org/ad/94-19-02): Swashplate Support Assembly · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 4 more. Effective Sep 28, 1994 - [AD 94-15-07](https://openairdocs.org/ad/94-15-07): Main Rotor Blades · Bell Helicopter Textron Canada 206A, 206B, 206L and 3 more. Effective Aug 26, 1994 - [AD 92-09-07](https://openairdocs.org/ad/92-09-07): Vertical Fin Supports · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 1 more. Effective Jun 29, 1992 - [AD 92-06-12](https://openairdocs.org/ad/92-06-12): Transmission Failure · Bell Helicopter Textron Canada 206A, 206B, 206L and 2 more. Effective Apr 13, 1992 - [AD 92-01-05](https://openairdocs.org/ad/92-01-05): Main Rotor Blades · Bell Helicopter Textron Canada 206A, 206B, 206L and 2 more. Effective Feb 5, 1992 - [AD 90-21-03](https://openairdocs.org/ad/90-21-03): Tail Rotor Blade Assembly · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 4 more. Effective Aug 14, 1991 - [AD 91-03-12](https://openairdocs.org/ad/91-03-12): Emergency Float Bags · Bell Helicopter Textron Canada 206A, 206B, 206L and 2 more. Effective Feb 28, 1991 - [AD 89-10-11 R1](https://openairdocs.org/ad/89-10-11-R1): Rfm Limitations · Bell Helicopter Textron Canada 206A and 206B. Effective Jul 31, 1989 - [AD 88-23-03](https://openairdocs.org/ad/88-23-03): Tail Rotor Yoke Assembly · Bell Helicopter Textron Canada 206A, 206B, 206B-1 and 3 more. Effective Jul 25, 1989 - [AD 78-11-02 R1](https://openairdocs.org/ad/78-11-02-R1): Rotor Blade Straps · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 4 more. Effective Dec 15, 1988 - [AD 87-10-11](https://openairdocs.org/ad/87-10-11): Main Rotor Mast Assemblies · Bell Helicopter Textron Canada 206A, 206B, 206L and 2 more. Effective Aug 8, 1988 - [AD 86-24-01](https://openairdocs.org/ad/86-24-01): T/R Assembly · Bell Helicopter Textron Canada 206A, 206B and 206L. Effective Dec 15, 1986 - [AD 85-26-06](https://openairdocs.org/ad/85-26-06): Tail Rotor Blades · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 4 more. Effective Jan 31, 1986 - [AD 85-25-01](https://openairdocs.org/ad/85-25-01): Cyclic Control Stick · Bell Helicopter Textron Canada 206A, 206B, 206L and 2 more. Effective Dec 30, 1985 - [AD 80-18-04 R1](https://openairdocs.org/ad/80-18-04-R1): Main Rotor Trunnion · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 3 more. Effective Nov 24, 1980 - [AD 80-17-05](https://openairdocs.org/ad/80-17-05): Tail Rotor Blades · Bell Helicopter Textron Canada 206A, 206A-1 (OH-58A), 206B and 2 more. Effective Sep 10, 1980 - [AD 80-08-04](https://openairdocs.org/ad/80-08-04): Auxiliary Fuel System · Chadwick C-20 auxiliary fuel system (Phoenix Air-Atlanta STC SH129WE or SH139WE). Effective Apr 17, 1980 - [AD 79-10-01](https://openairdocs.org/ad/79-10-01): External Load Carrying Devices · Bell Helicopter Textron Canada 206A and 206B with STC SH474AL or SH515AL. Effective May 14, 1979 Historical (superseded or no longer in force): - [AD 2021-26-08](https://openairdocs.org/ad/2021-26-08) (historical): Tail Rotor Drive Shaft · Bell Textron Canada 206, 206A, 206A-1 and 7 more. Effective Jan 27, 2022 - [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 2013-20-13](https://openairdocs.org/ad/2013-20-13) (historical): Turbine Section · Bell Helicopter Textron Canada 206A, 206B and 206L. Effective Dec 10, 2013 - [AD 2009-08-03](https://openairdocs.org/ad/2009-08-03) (historical): Tail rotor blade (blade) · Bell Helicopter Textron 206A, 206B, 206L and 10 more. Effective Apr 24, 2009 - [AD 2009-07-51](https://openairdocs.org/ad/2009-07-51) (historical): Lever assembly bearing · Bell Helicopter Textron 206A, 206A-1 (OH-58A), 206B and 7 more - [AD 2007-19-52](https://openairdocs.org/ad/2007-19-52) (historical): Tail rotor blade (blade) · Bell Helicopter Textron 206A, 206B, 206L and 10 more. Effective Dec 5, 2007 - [AD 2004-24-08](https://openairdocs.org/ad/2004-24-08) (historical): Tail rotor blade (blade) · Bell Helicopter Textron 206A, 206B, 206L and 3 more. Effective Dec 16, 2004 - [AD 81-18-01](https://openairdocs.org/ad/81-18-01) (historical): Main Rotor Trunnions · Bell Helicopter Textron 206A, 206A-1 (OH-58A), 206B and 3 more. Effective Sep 22, 1981 All 91: https://openairdocs.org/model/agusta-206a/ads.md ## Information bulletins (advisory) (7) - [SAIB SW-18-02](https://openairdocs.org/saib/SW-18-02): Loss of Hardware Tail Rotor Drive Shaft Couplings. Issued Nov 2, 2017 - [SAIB SW-12-45](https://openairdocs.org/saib/SW-12-45): Garmin Model 400W/500W Series GPS-WAAS Navigation System. Issued Oct 3, 2012 - [SAIB SW-10-42R1](https://openairdocs.org/saib/SW-10-42R1): Emergency Float Kits. Issued Aug 11, 2010 - [SAIB SW-10-42](https://openairdocs.org/saib/SW-10-42) (historical): Emergency Float Kits. Issued Aug 5, 2010 - [SAIB SW-08-42](https://openairdocs.org/saib/SW-08-42): Emergency Float with Liferaft Kits (kits). Issued Aug 27, 2008 - [SAIB SW-05-24](https://openairdocs.org/saib/SW-05-24): . Issued Dec 22, 2004 - [SAIB SW-04-92](https://openairdocs.org/saib/SW-04-92): . Issued Sep 30, 2004 ## Registered aircraft None registered with this model now. ## STCs approved for it (423, first 50) - [STC SA00475SE](https://openairdocs.org/stc/SA00475SE): Replacement of the original land gear skid tubes and saddles with DART Aerospace Model D206-642 skid tubes and saddles.. Dart Aerospace USA Inc. - [STC SA00500SE](https://openairdocs.org/stc/SA00500SE): Installation of DART Heli-Access-Steps on the skid landing gear cross tubes.. Dart Aerospace USA Inc. - [STC SA00680SE (2 OF 6](https://openairdocs.org/stc/SA00680SE%20(2%20OF%206): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.. Electronics International - [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC - [STC SA00944CH](https://openairdocs.org/stc/SA00944CH): Replace Janitrol combustion heater Model 81D94-X (XX) with C&D Associates combustion heater Model CD25K, CD35K, and CD45K. Hartzell Engine Technologies, LLC - [STC SA116WE](https://openairdocs.org/stc/SA116WE): Installation of Nightsun SX-16C Searchlight.. Spectrolab, Inc - [STC SA1609SO](https://openairdocs.org/stc/SA1609SO): Installation of a spacer block assembly on helicopters equipped with high skid gear. Bell Helicopter Textron Inc. - [STC SA1626NM PAGE 1](https://openairdocs.org/stc/SA1626NM%20PAGE%201): Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series). Electronics International - [STC SA244NW](https://openairdocs.org/stc/SA244NW): Installation of HE-206-010 bleed air heater system.. Flippo J E - [STC SA2511CE](https://openairdocs.org/stc/SA2511CE): Installation of Phoenix Aerospace, Inc. (PAI) Model VR-1010-24-1A or Model VR-1010-24-2A silicon, solid-state, DC voltage regulator units.. Phoenix Aerospace, Inc - [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories.. Electronics International Inc. - [STC SA2844CE (1 OF 2)](https://openairdocs.org/stc/SA2844CE%20(1%20OF%202)): Installation of a plastic cap enclosure over the anti-collision strobe light system.. Air Transport Inc - [STC SA4173NM](https://openairdocs.org/stc/SA4173NM): Installation of Simplex Model 7600 modular electrical system. (47G-5 WITH 12 VOLT SYSTEM). Simplex Manufacturing Company - [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer.. Electronics International - [STC SA615EA](https://openairdocs.org/stc/SA615EA): Installation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision lights.. Whelen Aerospace Technologies - [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [STC SA848NW](https://openairdocs.org/stc/SA848NW): Fabrication and installation of Simplex 4900 spray tank system.. Simplex Manufacturing Co - [STC SA86GL](https://openairdocs.org/stc/SA86GL): Installation of Marathon CA1700 nickel cadmium storage battery.. Aero Quality Sales Co, Inc - [STC SH1008NE](https://openairdocs.org/stc/SH1008NE): Installation of nose mounted camera pod 104/12 Wescam or 116 series Wescam or Model 12 Series Wescam.. 1592686 Ontario Inc - [STC SH1018EA](https://openairdocs.org/stc/SH1018EA): Installation of Casey shroud type heater.. Rilpa Enterprises, Ltd - [STC SH1031NE](https://openairdocs.org/stc/SH1031NE): Installation of utility equipment kit, consisting of Sling Mirror(s), bear paws and maintenance steps.. Dart Aerospace Limited - [STC SH1032GL](https://openairdocs.org/stc/SH1032GL): Install SMR Technologies/BF Goodrich Emergency Float Assemblies, P/N 7MA1042-1, 7MA1043-1, and 7MA1044-1.. SMR Technologies - [STC SH1057NE](https://openairdocs.org/stc/SH1057NE): Installation of Kwik float emergency flotation system.. Dart Aero Accessories, Inc - [STC SH1062SO](https://openairdocs.org/stc/SH1062SO): Installation of fuel tank filler extension (increased fuel capacity).. Thoroughbred Helicopter Service Inc - [STC SH10CE](https://openairdocs.org/stc/SH10CE): Install Hoskins Twilighter Mk II supplementary lighting system consisting of P/N 60-0032-31 power supply and two Model 2(P/N 30-0021-11) lights.. BF Goodrich Aerospace - [STC SH1125EA](https://openairdocs.org/stc/SH1125EA): Installation of Aircraft Parts Corp. starter-generator, P/N 150SG111Q, 150SG117Q, 150SG121Q.. Shurka Aerospace Inc - [STC SH1134SO](https://openairdocs.org/stc/SH1134SO): Installation of one-piece entrance step.. Bell Helicopter Textron Inc. - [STC SH1147SO](https://openairdocs.org/stc/SH1147SO): Installation of baggage floor protector.. Bell Helicopter Textron Inc. - [STC SH1148EA](https://openairdocs.org/stc/SH1148EA): Installation of a modified Lear-Siegler starter-generator, P/N 23032-010.. Shurka Aerospace Inc - [STC SH1148SO](https://openairdocs.org/stc/SH1148SO): Installation of a raingutter. Bell Helicopter Textron Inc. - [STC SH1152NW](https://openairdocs.org/stc/SH1152NW): Installation of the Automatic Flagman Model 135 Control Stick Grip. Air Products & Parts LLC - [STC SH1163SO](https://openairdocs.org/stc/SH1163SO): Installation of an entrance step on high skid gear with emergency floatation system (pop-outs).. Bell Helicopter Textron Inc. - [STC SH1164SW](https://openairdocs.org/stc/SH1164SW): Installation of dual battery system using the ship's original battery and one installed by Bell Service Instructions and Qualitron Aero.. Tiger Air Svc Center, Inc - [STC SH117WE](https://openairdocs.org/stc/SH117WE): Installation of cargo rack on one side or on both sides of skid gear.. USDA Forest Service - [STC SH1214EA](https://openairdocs.org/stc/SH1214EA): Installation of Field Aviation moveable window panel(s) in aft door(s) only.. Eagle Reach, Inc - [STC SH1216EA](https://openairdocs.org/stc/SH1216EA): Installation of Wescam camera pod.. 1592686 Ontario Inc - [STC SH122WE](https://openairdocs.org/stc/SH122WE): Installation of Freon air conditioning system.. Parker Hannifin Corp - Airborne Division - [STC SH1244SO](https://openairdocs.org/stc/SH1244SO): Fabrication and installation of camera mount and photographer's seat.. Ephraim Nowak - [STC SH124NW](https://openairdocs.org/stc/SH124NW): Installation of Simplex 2700 and2700A spray system tank assembly.. Simplex Manufacturing Co - [STC SH1250EA](https://openairdocs.org/stc/SH1250EA): Installation of 'zapper' electric chip detector system.. Vickers Inc - [STC SH1269SO](https://openairdocs.org/stc/SH1269SO): Installation of safety step.. Vanic, Inc - [STC SH126WE](https://openairdocs.org/stc/SH126WE): Installation of cartridge boost electrical starter system.. Talley Industries, Inc - [STC SH1281SO](https://openairdocs.org/stc/SH1281SO): Installation of a maintenance step.. Bell Helicopter Textron Inc. - [STC SH1282SO](https://openairdocs.org/stc/SH1282SO): Installation of a preflight step/access handle.. Bell Helicopter Textron Inc. - [STC SH1286SO](https://openairdocs.org/stc/SH1286SO): Installation of a cargo frame assembly. Bell Helicopter Textron Inc. - [STC SH1312SO](https://openairdocs.org/stc/SH1312SO): Installation of nightscanner belly mounted searchlight.. Bell Helicopter Textron Inc. - [STC SH1321SO](https://openairdocs.org/stc/SH1321SO): Installation of a sunvisor kit in cockpit of helicopters.. Bell Helicopter Textron Inc. - [STC SH1322SO](https://openairdocs.org/stc/SH1322SO): Manufacture of aluminum entrance step in accordance with Aeronautical Accessories, Inc. Drawing List Report No. KR-175, Revision E , dated July 8, 1982, or later FAA approved revisions, and installation per Installation Instructions listed therein on helicopters equipped with high skid gear.. Bell Helicopter Textron Inc. - [STC SH1385SO](https://openairdocs.org/stc/SH1385SO): Installation of a cargo viewing mirror on Bell helicopters in accordance with Aeronautical Accessories, Inc. Report KR-198, Revision A , dated July 6, 1982, or later FAA approved revisions.. Bell Helicopter Textron Inc. - [STC SH138WE](https://openairdocs.org/stc/SH138WE): Installation of Chadwick cargo rack C-72.. Isolair All 423: https://openairdocs.org/model/agusta-206a/stcs.md ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (16) As reported by operators and repair stations, by the model named in the report. - [SDR 2017FA0000367](https://openairdocs.org/sdr/2017FA0000367), Apr 6, 2017: CAGE. BENT. FOUND FREE WHEELING ASSY SEIZED AT ACFT SHUTDOWN. DISASSEMBLY OF FWU, FOUND CAGE BENT BETWEEN SPRAG. - [SDR XJ2R20160414001](https://openairdocs.org/sdr/XJ2R20160414001), Apr 14, 2016: DRIVE SHAFT. SHEARED. HYDRAULIC PUMP DRIVE SHAFT 20546AA SHEARED DURING RUN UP AFTER INSTALLATION OF REPLACEMENT PUMP. - [SDR 2014FA0000669](https://openairdocs.org/sdr/2014FA0000669), Nov 14, 2014: NUT. CORRODED. CORROSION EXCESSIVE IN THE MAST BEARING RETAINING NUT AREA. AREA J IN THE MFG CR&O MANUAL. - [SDR SD72005F00000](https://openairdocs.org/sdr/SD72005F00000), Feb 28, 2005: FUEL CONTROL. FAILED. PILOT REPORTED DECAY OF N2 RPM WHEN ATTEMPTING TO REAPPLY COLLECTIVE FOLLOWING GRADUAL DECENT IN LOW ALTITUDE CRUISE FLIGHT. PRECAUTIONARY LANDING ACCOMPLISHED. - [SDR CA030409013](https://openairdocs.org/sdr/CA030409013), Mar 28, 2003: STRUCTURE. CRACKED. (CAN) WHILE IN CRUISE FLIGHT THE PILOT NOTICED A YAW TO THE RIGHT. UPON LANDING HE NOTICED THAT THE TAIL FELT TWITCHY AND SHUTDOWN TO INVESTIGATE. WHEN HE GOT O - [SDR CA021129009](https://openairdocs.org/sdr/CA021129009), Oct 17, 2002: SEAL. WARPED. (CAN) AME INSTALLED TURBINE ASSEMBLY FOLLOWING REPAIR. ON GROUND RUN, OIL LEAK WAS OBSERVED BETWEEN PT SUPPORT AND THE EXTERNAL OIL SUMP. SUMP WAS REMOVED AND S - [SDR JJWA080369](https://openairdocs.org/sdr/JJWA080369), Jul 15, 2002: STIFFENER. CRACKED. FOUND STIFFNER CRACKED DURING INSPECTION - CRACK ORIGINATED IN LOWEST HI-LOCK FASTNER POSITION 2.875 - [SDR HEEA080096](https://openairdocs.org/sdr/HEEA080096), Jun 11, 2002: SLEEVE. LEAKING. VENDOR REWORKED SLIDE AND SLEEVE ASSY CAUSES SERVO TO HAVE EXCESSIVE INTERNAL LEAKAGE DURING FINAL TEST. - [SDR HEEA076525](https://openairdocs.org/sdr/HEEA076525), Oct 9, 2001: CAP. CRACKED. RECEIVED DENTED AND CRACK AT LEADING EDGE. - [SDR CA000419006](https://openairdocs.org/sdr/CA000419006), Apr 10, 2000: BOLT. CRACKED. (CAN) DURING O/H OF MAAIN ROTOR HEAD, ONE OF THE BLADE BOLTS WAS FOUND TO BE CRACKED BY NON DESTRUCTIVE TESTING. BLADE BOLT P/N 206-101-152-1 CAN HAVE EIHTER NU - [SDR CA000404017](https://openairdocs.org/sdr/CA000404017), Apr 4, 2000: WIRE. BROKEN. (CAN) BROKEN WIRE FOUND ON GOVERNOR BEEP SWITCH. WIRE RE-SOLDERED AND AIRCRAFT RETURNED TO SERVICE. - [SDR 98ZZZX4203](https://openairdocs.org/sdr/98ZZZX4203), Nov 5, 1998: DRIVE COLLAR. FAILED. 'BELL HELICOPTER TEXTRON HAS ISSUED OPERATION SAFETY NOTICE OSN 206-98-34 AND 206L-98-40 DATED 11-2-98.' BELL HELICOPTER HAS LEARNED OF A RECENT HARD-FOULING CO - [SDR AU980839](https://openairdocs.org/sdr/AU980839), Jul 21, 1998: TRUNNION. CRACKED. (AUS) MAIN ROTOR TRUNNION CRACKED IN TWO PLACES. FOUND DURING MAGNETIC PARTICLE INSPECTION FOLLOWING HEAVY LANDING. - [SDR CA970904029](https://openairdocs.org/sdr/CA970904029), Jul 21, 1997: FUEL CONTROL. FAULTY. (CAN) ENGINE SHUTS OFF WHEN THROTTLE IS RETARDED TO 25 DEGREES ON FCU QUADRANT. WHEN THROTTLE IS RIGGED TO IDLE AT 30 DEGREES, IT WILL GO BELOW 30 DEGREES IF TH - [SDR GCHA959](https://openairdocs.org/sdr/GCHA959), Apr 20, 1995: YOKE. CORRODED. M/R YOKE P/N 206-010-101-129 S/N A2744 WAS EVALUATED , CPR # 064540, AND WAS FOUND TO HAVE CORROSION ON BEARING JOURNALS BEYOND ACCEPTABLE LIMITS. THE YOKE WAS - [SDR 95ZZZX1689](https://openairdocs.org/sdr/95ZZZX1689), Mar 17, 1995: SPRING. BROKEN. DURING 100-HOUR INSPECTION, MECHANIC FOUND GREASE LEAKAGE FROM THE FORWARD COUPLING OF MAIN DRIVE SHAFT. AT DISASSEMBLY FOR REPAIR, THE COUPLING SPRING WAS FOUN ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Bell 206A](https://openairdocs.org/model/bell-206a): 23 registered aircraft, registry code 1181508 - [Agusta Bell AB 206A](https://openairdocs.org/model/agusta-bell-ab-206a): 0 registered aircraft, registry code 0260304 - [Sievers Kelly 206A](https://openairdocs.org/model/sievers-kelly-206a): 0 registered aircraft, registry code 05605QE --- 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.