# Sievers Kelly 206A - Type: Aircraft model (FAA registry) - Registry code: 05605QE - Manufacturer (registry): SIEVERS KELLY - Model: 206A - Aircraft type: Rotorcraft - Category: Rotorcraft - Engines: 1 ยท Reciprocating - Seats: 4 - Weight class: Up to 12,499 lb - Certification: Not type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/sievers-kelly-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. None matched. ## Registered aircraft None registered with this model now. ## 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 206A](https://openairdocs.org/model/agusta-206a): 0 registered aircraft, registry code 0260301 - [Agusta Bell AB 206A](https://openairdocs.org/model/agusta-bell-ab-206a): 0 registered aircraft, registry code 0260304 --- 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.