# N350CF: Beech B300

- Status: Valid registration
- Airframe: [Beech B300](https://openairdocs.org/model/beech-b300) (registry code 1152932, 19 seats)
- Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032)
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (Textron Aviation Inc.) (OpenAirDocs)
- Serial number: FL-57
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: June 12, 1991
- Certificate issued: March 31, 2025
- Expires: March 31, 2032
- Mode S code: A3E505
- Registered owner: [Clemens Aviation LLC](https://openairdocs.org/faa-owner/CLEMENS%20AVIATION%20LLC)
- Location: [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- Owner type: LLC
- Owner's area on the map: 37.7687° N, 97.2202° W: Placed by OpenAirDocs at the center of ZIP code 67226, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=350CF
- Page: https://openairdocs.org/aircraft/N350CF

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included.

## ADs that may apply (OpenAirDocs): 58 in force

### Matched by airframe (Beech B300)

- [AD 2026-15-05](https://openairdocs.org/ad/2026-15-05): Wing Structure · Textron B300 and B300C. Effective Aug 10, 2026
- [AD 2025-20-11](https://openairdocs.org/ad/2025-20-11): Rudder Control System · Textron B200GT, B200CGT, B300 and 1 more. Effective Oct 17, 2025
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2022-03-23](https://openairdocs.org/ad/2022-03-23): Rudder Control System · Garmin G1000 Integrated Avionics System and GFC 700 Automatic… (STC SA01535WI-D). Effective Feb 22, 2022
- [AD 2021-05-17](https://openairdocs.org/ad/2021-05-17): NAVIGATION SYSTEM · Rockwell Collins FDSA-6500, CL-600-2B16 (CL-604), 525B and 7 more. Effective Apr 29, 2021
- [AD 2011-15-05](https://openairdocs.org/ad/2011-15-05): Charts · Textron B300 and B300C (C-12W). Effective Aug 19, 2011
- [AD 2010-26-03](https://openairdocs.org/ad/2010-26-03): Ice and Rain Protection · Textron B200, B200GT, B300 and 1 more. Effective Dec 20, 2010
- [AD 2010-05-10](https://openairdocs.org/ad/2010-05-10): Instruments · Textron B300 and B300C (C-12W). Effective Apr 8, 2010
- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [AD 2007-12-06](https://openairdocs.org/ad/2007-12-06): Flight controls · Textron B200, B200C, B300 and 2 more. Effective Jul 16, 2007
- [AD 2006-19-09](https://openairdocs.org/ad/2006-19-09): Passenger seat mod kit · Textron B300. Effective Oct 24, 2006
- [AD 2005-01-18](https://openairdocs.org/ad/2005-01-18): Fuselage stringers · Textron 200, 200C, 200CT and 24 more. Effective Mar 1, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2005-01-04](https://openairdocs.org/ad/2005-01-04): Fuel hose · Textron 100, 200, 200C and 29 more. Effective Feb 22, 2005
- [AD 2004-17-02](https://openairdocs.org/ad/2004-17-02): Cross shaft attach bolt · Textron 100, 1900, 1900C and 52 more. Effective Oct 4, 2004
- [AD 2003-02-03](https://openairdocs.org/ad/2003-02-03): Airstair door and emergency exits · Textron 100, 200, 2000 and 46 more. Effective Mar 7, 2003
- [AD 2002-23-11](https://openairdocs.org/ad/2002-23-11): Elevator Balance Weight Attachment Screws · Textron 1900, 1900C, 1900C (C-12J) and 30 more. Effective Jan 10, 2003
- [AD 2002-14-19](https://openairdocs.org/ad/2002-14-19): Collins Air Data Computers (ADC) · Boeing DC-8-11, DC-8-12, DC-8-21 and 36 more. Effective Aug 23, 2002
- [AD 99-18-15](https://openairdocs.org/ad/99-18-15): Landing Gear Emergency Hand Pumps · Textron 1900D, B200, B300 and 1 more. Effective Sep 27, 1999
- [AD 99-09-10](https://openairdocs.org/ad/99-09-10): Landing Gear Hand Pump · Textron 200CT, 300, A200CT (C-12D) and 19 more. Effective Jun 7, 1999
- [AD 99-09-15](https://openairdocs.org/ad/99-09-15): Flight Control Mechanism · Textron 1900D, 58, 58A and 5 more. Effective May 18, 1999
- [AD 99-02-16](https://openairdocs.org/ad/99-02-16): Elevator Trim Tab System · Textron B300 and B300C. Effective Mar 12, 1999
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 98-21-35](https://openairdocs.org/ad/98-21-35): Actuator Clevis Assembly in Main Landing Gear · Textron 200T, 300, A200CT (C-12D) and 15 more. Effective Nov 23, 1998
- [AD 98-04-24](https://openairdocs.org/ad/98-04-24): AFM - Limitations Section - Icing · Textron 100, 300, 58 and 13 more. Effective Mar 13, 1998
- [AD 97-25-03](https://openairdocs.org/ad/97-25-03): AFM - Limitations - Power Levers · Textron 100, 1900, 1900C and 44 more. Effective Jan 21, 1998
- [AD 97-25-01](https://openairdocs.org/ad/97-25-01): Outflow/Safety Valve · Textron 100, 200, 2000 and 38 more. Effective Jan 11, 1998
- [AD 97-23-17](https://openairdocs.org/ad/97-23-17): Pneumatic Tubing · Textron 200, 200C, 200CT and 30 more. Effective Dec 29, 1997
- [AD 91-20-14 R1](https://openairdocs.org/ad/91-20-14-R1): Performance Charts and Information · Textron B300 and B300C. Effective Sep 12, 1994
- [AD 94-01-01](https://openairdocs.org/ad/94-01-01): Cabin Seats · Textron B300 and B300C. Effective Feb 11, 1994
- [AD 92-15-01](https://openairdocs.org/ad/92-15-01): Truss-To-Firewall Bolts · Textron 100, 200, 200C and 40 more. Effective Aug 21, 1992
- [AD 92-06-11](https://openairdocs.org/ad/92-06-11): Autopilot/Flight Director System Wiring · Textron 1900C, 300, B200 and 2 more. Effective Mar 30, 1992

### Matched by engine (Pratt & Whitney PT6A series)

- [AD 2024-04-51](https://openairdocs.org/ad/2024-04-51): Turbine Section · Pratt & Whitney Canada PT6A-64, PT6A-66, PT6A-66A and 17 more. Effective Mar 28, 2024
- [AD 2022-08-13](https://openairdocs.org/ad/2022-08-13): Turbine Section · Pratt & Whitney Canada PT6A-34, PT6A-34B, PT6A-34AG and 2 more. Effective May 27, 2022
- [AD 2016-05-13](https://openairdocs.org/ad/2016-05-13): Corrosion and perforation of the two-ply Cu-Be bellows in Woodward FCUs. · Pratt & Whitney Canada PT6A-60AG, PT6A-65AG, PT6A-67AF and 1 more. Effective Apr 22, 2016
- [AD 2014-17-08 R1](https://openairdocs.org/ad/2014-17-08-R1): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Jun 5, 2015
- [AD 2014-11-05](https://openairdocs.org/ad/2014-11-05): Reinforcement liner to the power turbine (PT) containment   
  ring and, for certain PT containment rings, adding scallops · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 18 more. Effective Aug 5, 2014
- [AD 2012-09-10](https://openairdocs.org/ad/2012-09-10): First stage sun gears · Pratt & Whitney Canada PT6A-110, PT6A-112, PT6A-114 and 12 more. Effective May 23, 2012
- [AD 2011-25-12](https://openairdocs.org/ad/2011-25-12): Sun gear · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 4 more. Effective Dec 28, 2011
- [AD 2011-20-51](https://openairdocs.org/ad/2011-20-51): Gears · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 4 more. Effective Nov 1, 2011
- [AD 2004-25-18](https://openairdocs.org/ad/2004-25-18): Propeller governor assemblies · Pratt & Whitney Canada PT6A-60A and PT6A-65B. Effective Jan 18, 2005
- [AD 2002-23-13](https://openairdocs.org/ad/2002-23-13): Turbine Exhaust Ducts · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 20 more. Effective Dec 31, 2002
- [AD 2001-20-01](https://openairdocs.org/ad/2001-20-01): Compressor Bleed Valve Assembly · Pratt & Whitney Canada PT6A-114A and PT6A-25C. Effective Nov 5, 2001
- [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997
- [AD 95-13-08](https://openairdocs.org/ad/95-13-08): Compressor Turbine Disk · Pratt & Whitney Canada PT6A-67D. Effective Jul 12, 1995
- [AD 93-23-06](https://openairdocs.org/ad/93-23-06): Airframe Chip Detector Flag System · Pratt & Whitney Canada PT6A-50. Effective Jan 26, 1994
- [AD 92-15-11](https://openairdocs.org/ad/92-15-11): Compressor Delivery Air Line (P3) Filter Assembly · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-21 and 7 more. Effective Aug 17, 1992
- [AD 90-12-05](https://openairdocs.org/ad/90-12-05): Engine Overhaul · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 3 more. Effective May 30, 1990
- [AD 86-10-05](https://openairdocs.org/ad/86-10-05): First Stage Compressor Hub · Pratt & Whitney Canada PT6A-42. Effective Jun 5, 1986
- [AD 80-08-12](https://openairdocs.org/ad/80-08-12): Fuel Pump Drive Coupling Splines · Pratt & Whitney Canada PT6A-11, PT6A-112, PT6A-135 and 24 more. Effective Apr 18, 1980
- [AD 80-04-02](https://openairdocs.org/ad/80-04-02): Push-Pull Control Terminal · Pratt & Whitney Canada PT6A-20, PT6A-6A, PT6A-6B and 1 more. Effective Feb 8, 1980
- [AD 78-17-07](https://openairdocs.org/ad/78-17-07): Fuel Control Unit · Pratt & Whitney Canada PT6A-38, PT6A-41 and PT6A-45A. Effective Aug 31, 1978
- [AD 78-12-04](https://openairdocs.org/ad/78-12-04): No. 2 Bearing Pressure Oil Transfer Tube Assembly · Pratt & Whitney Canada PT6A-38, PT6A-41 and PT6A-45A. Effective Jun 19, 1978
- [AD 75-06-01](https://openairdocs.org/ad/75-06-01): Gearbox Deterioration · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-20B and 11 more. Effective Apr 1, 1977
- [AD 75-11-04](https://openairdocs.org/ad/75-11-04): Reduction Gearbox Engine Distress · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-20B and 8 more. Effective May 20, 1975
- [AD 70-16-01](https://openairdocs.org/ad/70-16-01): Turbo Propeller Governors · Pratt & Whitney Canada PT6A-11, PT6A-11AG, PT6A-15AG and 5 more. Effective Aug 4, 1970
- [AD 69-23-06](https://openairdocs.org/ad/69-23-06): Fuel Pumps · Pratt & Whitney Canada PT6A-20, PT6A-27, PT6A-28 and 4 more. Effective Nov 15, 1969
- [AD 68-05-03](https://openairdocs.org/ad/68-05-03): Reverse Mode · Pratt & Whitney Canada PT6A-20 and PT6A-6B. Effective Feb 28, 1968

### Historical (superseded or no longer in force)

- [AD 2019-12-09](https://openairdocs.org/ad/2019-12-09) (historical): Navigation · Bombardier CL-600-2B16 (CL-604), Flight Display System Application FDSA-6500, 525B and 13 more. Effective Jul 23, 2019
- [AD 2008-07-10](https://openairdocs.org/ad/2008-07-10) (historical): Pneumatic supply tube · Hawker Beechcraft B200, B200GT, B300 and 1 more. Effective Apr 10, 2008
- [AD 2006-23-02](https://openairdocs.org/ad/2006-23-02) (historical): Flight controls for improper assembly or damage · Raytheon B200, B200C, B300 and 2 more. Effective Dec 13, 2006
- [AD 98-15-13](https://openairdocs.org/ad/98-15-13) (historical): Fuel Hose · Raytheon 100 Model or Series (all), 200 Model or Series (all), 200C and 32 more. Effective Aug 28, 1998
- [AD 96-17-10](https://openairdocs.org/ad/96-17-10) (historical): Outflow/Safety Valve · Raytheon 200 Model or Series (all), 2000, 300 and 5 more. Effective Sep 24, 1996
- [AD 93-25-07](https://openairdocs.org/ad/93-25-07) (historical): Fuselage Stringers · Raytheon 200 Model or Series (all), 200C, 200CT and 22 more. Effective Feb 15, 1994
- [AD 2014-17-08](https://openairdocs.org/ad/2014-17-08) (historical): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Oct 8, 2014
- [AD 88-24-02](https://openairdocs.org/ad/88-24-02) (historical): Airframe Chip Detector Flag System · Pratt & Whitney Canada PT6A-50

## Information bulletins (advisory) (7 in force)

- [SAIB CE-15-15](https://openairdocs.org/saib/CE-15-15): Empennage  Horizontal & Vertical Stabilizer Structure. Issued Apr 20, 2015
- [SAIB CE-12-36](https://openairdocs.org/saib/CE-12-36): Flight Controls: Aileron. Issued Jun 19, 2012
- [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015
- [SAIB NE-12-04](https://openairdocs.org/saib/NE-12-04): Turbine/ Turboprop Engine: Reduction Gearbox. Issued Nov 1, 2011
- [SAIB NE-10-47](https://openairdocs.org/saib/NE-10-47): Turbine Engine Compressor Section. Issued Aug 30, 2010
- [SAIB NE-06-34](https://openairdocs.org/saib/NE-06-34): . Issued Mar 21, 2006
- [SAIB CE-03-24](https://openairdocs.org/saib/CE-03-24): . Issued Feb 19, 2003

## NTSB investigations

None matched to N350CF.

## FAA accident and incident reports

None matched to N350CF.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N350CF not matched to an aircraft (30)

They name N350CF, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 254041](https://openairdocs.org/sdr/254041), Sep 10, 2004: WIRE. BROKEN. LEFT ENGINE FIRE TEST WILL NOT TEST PROPERLY NO CHIME. REPAIRED BROKEN WIRE AT LT FIRE WARNING CIRCUIT BREAKER IAW MM 31-50-05, OP CHECKED GOOD.
- [SDR SIMA200416003](https://openairdocs.org/sdr/SIMA200416003), Jun 2, 2004: FRAME. CORRODED. ABI - DURING AN MBV INSPECTION, THE AFT FLANGE OF FRAME 258 WAS FOUND CORRODED BEYOND SRM LIMITS. COMPLETELY REMOVED THE CORRODED AREA BY CREATING A 2 INCH BY .
- [SDR SIMA200416002](https://openairdocs.org/sdr/SIMA200416002), Jun 1, 2004: SKIN. DENTED. DURING AN MBV INSPECTION OF THE FUSELAGE A DENT AFT OF FRAME 363 ON THE LEFT SIDE, WAS FOUND TO BE BEYOND SRM LIMITS. COMPLETELY REMOVED THE DAMAGED BY CREATING
- [SDR SIMA200416004](https://openairdocs.org/sdr/SIMA200416004), May 31, 2004: FRAME. BENT. DURING A MBV INSPECTION, FOUND CARGO FRAME AT STATION 677 WAS FOUND BENT. RECONTOURED CARGO FRAME AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR 
- [SDR SIMA200311103](https://openairdocs.org/sdr/SIMA200311103), Apr 19, 2003: ACTUATOR. BROKEN. SGF - FLT 3617 - DURING APPROACH THE RIGHT ENGINE STARTED TO VIBRATE SEVERLY. CREW SHUT DOWN THE ENGINE AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH N
- [SDR SIMA200228702](https://openairdocs.org/sdr/SIMA200228702), Oct 12, 2002: CONTROL VALVE. MALFUNCTIONED. CREW REPORTED UNCOMMANDED PITCH CHANGES IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL VALVE AND FLAP CONTROL VALVE AND FLAP CONTROL BOX IAW MM. O
- [SDR SIMA200224201](https://openairdocs.org/sdr/SIMA200224201), Aug 29, 2002: CONNECTOR. DISCONNECTED. FSM - FLT 3535 - RIGHT MLG SAFE LIGHT FAILED TO ILLUMINATE. LAMP TEST GOOD. EMERGENCY WAS DECLARED. LANDING WAS NORMAL. FOUND CANNON PLUG ON RIGHT MLG NOT CONNE
- [SDR SIMA200219201](https://openairdocs.org/sdr/SIMA200219201), Jul 11, 2002: PUMP. FAILED. DISC LOST ALL HYDRAULIC POWER INBOARD, OUTBOARD, MAIN INDICATOR SHOWS ZERO ON TAXI OUT. REMOVED AND REPLACED HYDRAULIC MOTOR DRIVEN PUMP IAW MM. OPS CHECK AND L
- [SDR SIMA200203703](https://openairdocs.org/sdr/SIMA200203703), Feb 3, 2002: SWITCH. DEFECTIVE. DFW - FLT 3818 - FOUND INTERIOR EMERGENCY LIGHTS CAN'T BE CONTROLLED FROM THE COCKPIT. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT SWITCH. (M)
- [SDR 2001F00670](https://openairdocs.org/sdr/2001F00670), Oct 25, 2001: SEAT TRACK. CORRODED. ABI - DURING MBV INSPECTION, FOUND CORROSION ON SEAT TRACK AT BL 18.3L, BETWEEN STATIONS 297 TO 348 TO BE OUT OF SRM LIMITS. CUT OUT A 56 INCH SECTION OF EXISTI
- [SDR SIMA200130302](https://openairdocs.org/sdr/SIMA200130302), Oct 25, 2001: SEAT TRACK. CORRODED. ABI - DURING MBV INSPECTION, FOUND CORROSION ON SEAT TRACK AT BL 18.3L, BETWEEN STATIONS 297 TO 348 TO BE OUT OF SRM LIMITS. CUT OUT A 56 INCH SECTION OF EXISTI
- [SDR SIMA200115619](https://openairdocs.org/sdr/SIMA200115619), Jun 5, 2001: POWER SUPPLY. DISCHARGED. SBA - FLT 3037 - FORWARD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWERS SUPPLY AT 20LN AND 21LN (S/N 18524, 18070) IAW AMM. OPS CHECK GOOD. (M)
- [SDR 20000612SH001](https://openairdocs.org/sdr/20000612SH001), May 12, 2000: SMOKE DETECTOR. MALFUNCTIONED. OC - FLT 5102 - CARGO SMOKE LIGHT CAME ON AFTER TAKEOFF. REMOVED AND REPLACED FIRE BOTTLES AND SMOKE DETECTORS IAW SAAB 340B AMM 26-13-15. OPS CHECK IAW SAAB 34
- [SDR SIMA1336](https://openairdocs.org/sdr/SIMA1336), May 12, 2000: SMOKE DETECTOR. MALFUNCTIONED. ROC - FLT 5102 - CARGO SMOKE LIGHT CAME ON AFTER TAKEOFF. REMOVED AND REPLACED FIRE BOTTLES AND SMOKE DETECTORS IAW SAAB 340B AMM 26-13-15. OPS CHECK IAW SAAB 3
- [SDR SIMA993432](https://openairdocs.org/sdr/SIMA993432), Dec 9, 1999: SMOKE DETECTOR. MALFUNCTIONED. ISP - FLT 5153 - AVIONIC SMOKE MASTER WARNING ACTIVATED. COULD NOT DUPLICATE DISCREPANCY. REMOVED AND REPLACED AVIONICS RACK SMOKE DETECTOR FOR SUSPECTED INTERM
- [SDR SIMA992992](https://openairdocs.org/sdr/SIMA992992), Oct 26, 1999: SKIN. DENTED. ABI - DEN IN RIGHT SIDE OF FUSELAGE SKIN BETWEEN FRAMES AT STATION 363 AND 376 AND BETWEEN SL 1617 AND SL 1618. PERFORMED A 1 INCH CUTOUT OF DAMAGED SKIN. PERFO
- [SDR SIMA991821](https://openairdocs.org/sdr/SIMA991821), Jul 1, 1999: BULB. FAILED. LAX - FLT 3265 - FLOOR PROXIMITY LIGHT AT SEAT 12 B/C DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. (X)
- [SDR SIMA991033](https://openairdocs.org/sdr/SIMA991033), Apr 13, 1999: WEU. MALFUNCTIONED. LAX - FLT 3449 - AFTE DEPARTURE, THE RIGHT ENGINE FIRE WARNING SYSTEM ACTIVATED. CREW DISCHARGED FIRE EXTINGUISHER AND RETURNED TO LAX. AFTER LANDING CREW PERFO
- [SDR SIMA990095](https://openairdocs.org/sdr/SIMA990095), Jan 9, 1999: PANEL. FAILED. LAX - FLT 3227 - FLIGHT ATTENDANT PANEL EMERGENCY ARM LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED COCKPIT EMERGENCY ARM SWITCH PANE. OPERATIONAL CHECK GOOD.
- [SDR SIMA982592](https://openairdocs.org/sdr/SIMA982592), Sep 16, 1998: SMOKE DETECTOR. FAILED. SBP - DURING PS-2 INSPECTION, THE AVIONICS SMOKE DETECTOR WOULD NOT TEST. FOUND BAD GROUND AT GROUNDING BLOCK 203VNGA. REMOVED BLOCK, CLEANED INSULATION MATERIA
- [SDR SIMA982513](https://openairdocs.org/sdr/SIMA982513), Sep 8, 1998: MFD. MALFUNCTIONED. LAX - FLT 3281 - CREW REPORTED SMOKE ODOR IN THE COCKPIT. REMOVED AND REPLACED MULTI-FUNCTION DISPLAY UNIT. OPERATIONAL CHECK GOOD. (M)
- [SDR SIMA982301](https://openairdocs.org/sdr/SIMA982301), Aug 18, 1998: VALVE. FAILED. LAX - FLT 3313 - LANDING GEAR WOULD NOT EXTEND NORMALLY. CREW SUCCESSFULLY PERFORMED EMERGENCY GEAR EXTENSION PROCEDURE. AIRCRAFT LANDED WITHOUT INCIDENT. REMOV
- [SDR WWMA9800080](https://openairdocs.org/sdr/WWMA9800080), Apr 17, 1998: PANEL. INOPERATIVE. FLIGHT 3235, LAX, EMERGENCY ARM LIGHT ON F/A'S PANEL INOP. REPLACED FLT ATT PANEL.
- [SDR WWMA9800010](https://openairdocs.org/sdr/WWMA9800010), Jan 12, 1998: SMOKE LIGHT. ILLUMINATED. DURING PREFLIGHT, THE CARGO SMOKE LIGHT ON THE CWP ILLUMINATED. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE CARGO SMOKE DETECTION SYSTEM AND COULD NOT DUPLIC
- [SDR WWMA9800008](https://openairdocs.org/sdr/WWMA9800008), Jan 9, 1998: SMOKE DETECTOR. DEFECTIVE. CARGO SMOKE LIGHT ON THE CWP ILLUMINATED DURING PREFLIGHT. REPLACED FORWARD SMOKE DETECTOR, DETECTOR WAS OEM.
- [SDR WWMA9800002](https://openairdocs.org/sdr/WWMA9800002), Jan 4, 1998: SMOKE DETECTOR. DIRTY. CARGO SMOKE LIGHT ILLUMINATED INTERMITTENTLY EVERY 15 TO 18 SECONDS DURING PREFLIGHT. MAINTENANCE CLEANED SMOKE DETECTOR AND RESECURED LOOSE CANNON PLUG.
- [SDR WWMA9700188](https://openairdocs.org/sdr/WWMA9700188), Nov 26, 1997: BULB. LOOSE. RIGHT FIRE HANDLE LIGHT WILL NOT ILLUMINATE DURING PREFLIGHT CHECKS. MAINTENANCE FOUND LOOSE BULB IN THE RIGHT FIRE HANDLE, TIGHTENED BULB.
- [SDR WWMA9700144](https://openairdocs.org/sdr/WWMA9700144), Sep 13, 1997: WHEEL ASSEMBLY. CRACKED. CREW REPORTED, THE RIGHT OUTBOARD MAIN LANDING GEAR TIRE WAS FLAT. MAINTENANCE FOUND A SECTION OF THE WHEEL RIM AT THE INBOARD BEAD APPROXIMATELY 6 INCHES LONG 
- [SDR WWMA9700102](https://openairdocs.org/sdr/WWMA9700102), Jul 24, 1997: BATTERIES. DISCHARGED. EMERGENCY LIGHT, OVER 8 A-B SEATS, COMES ON THEN GOES OUT. REPLACED ALL EMERGENCY BATTERIES, OP CK OKAY.
- [SDR WWMA9700072](https://openairdocs.org/sdr/WWMA9700072), May 14, 1997: SMOKE DETECTOR. INTERMITTENT. LAVATORY SMOKE DETECTOR LIGHT CAME ON INTERMITTENTLY IN FLIGHT. REPLACED THE LAVATORY SMOKE DETECTOR.

## STCs that may be installed (OpenAirDocs) (479, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Beech B300)

- [STC SA03025CH](https://openairdocs.org/stc/SA03025CH): Installation of weather research equipment and weather modification equipment for the purpose of modifying weather conditions. 3S Certification, LLC
- [STC SA04617NY](https://openairdocs.org/stc/SA04617NY): Installation of the Medivac Audio System. Avmax Aviation Services Inc
- [STC SA04218NY](https://openairdocs.org/stc/SA04218NY): Installation of Wing Tip Low Profile Pylons with Pods, Underwing Wiring Tunnel and Optional Underwing Antenna Provisions and Antennas. Aerospace Design & Compliance LLC
- [STC SA4175NM](https://openairdocs.org/stc/SA4175NM): Installation of fully enclosed main landing gear door system for high-flotation- gear-equipped aircraft. Raisbeck Engineering Inc
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA02658LA](https://openairdocs.org/stc/SA02658LA): Replacement of the original Pratt and Whitney PT6A-60A engines and propellers with Pratt and Whitney PT6A-67A engines and MT Propeller MTV-27-1-N-C-F-R(P)/CFR260-65b propellers. Blackhawk Modifications LLC
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA04221CH](https://openairdocs.org/stc/SA04221CH): Installation of Thermal Acoustic Kit. Skandia Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA04808NY](https://openairdocs.org/stc/SA04808NY): Installation of Mission Systems for Flight Inspection. Delta Engineering Corporation
- [STC SA03204CH](https://openairdocs.org/stc/SA03204CH): Installation of an RF Transparent Pod. DS Technologies LLC D/B/A DST
- [STC SA02133SE](https://openairdocs.org/stc/SA02133SE): Installation of a Luma Technologies LT-4500 Series Integrated Light\Emitting Diode (LED) Display Panel and LT-3500 LED light modules. Luma Technologies LLC
- [STC SA12345IB](https://openairdocs.org/stc/SA12345IB): Replacement of the Halon Type 1211 portable fire extinguisher with the Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC SA11302DS](https://openairdocs.org/stc/SA11302DS): Installation of the Pro Line Fusion embedded display system (EDS) latest version 3.7 software upgrade and additional factory options. BHE & Associates Ltd
- [STC SA03930NY](https://openairdocs.org/stc/SA03930NY): Installation of King Air Belly Payload Mount. Icarus Aero Inc
- [STC SA02017WI](https://openairdocs.org/stc/SA02017WI): The Installation of the Parker-Meggitt iPRESS™ System. 3S Certification LLC
- [STC SA03275CH](https://openairdocs.org/stc/SA03275CH): Installation of an antiskid brake system. Lee Air Inc
- [STC SA01638WI](https://openairdocs.org/stc/SA01638WI): Part Fabrication and Installation of Arm Ledge System and Table Assembly for aircraft cabin interior. Aviation Fabricators Inc
- [STC SA12242IB](https://openairdocs.org/stc/SA12242IB): Manufacturing and Installation of King Air Equipment. ICARUS AERO INC
- [STC ST04442CH](https://openairdocs.org/stc/ST04442CH): Installation of SmartSky LiTE System. Apcela IFC JV, LLC dba Apcela ATG
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA04757NY](https://openairdocs.org/stc/SA04757NY): Installation of a Lower-Fuselage Radome with Extended Nose & updated ECS. Metrea Special Aerospace, ISR Inc. (an Arizona Corporation)
- [STC SA12202IB](https://openairdocs.org/stc/SA12202IB): Installation of Garmin GWX Weather Radar System. Maxcraft Avionics Ltd
- [STC SA10800SC](https://openairdocs.org/stc/SA10800SC): Installation of a 3-tube Rockwell Collins IDS-3000 Electronic Flight Instrument System with File Server Unit (FSU). BHE & Associates LTD
- [STC SA01535WI-D](https://openairdocs.org/stc/SA01535WI-D): Installation of the Garmin G1000 Integrated Avionics System and GFC 700 Automatic Flight Control System and optional Electronic Stability and Protection (ESP). Garmin International Inc
- [STC SA10965SC](https://openairdocs.org/stc/SA10965SC): Installation of upgraded hardware to the Rockwell Collins Pro Line 21 FMS-3000 to provide Localizer Performance with Vertical Guidance (LPV). BHE & Associates LTD
- [STC SA04749NY](https://openairdocs.org/stc/SA04749NY): Atmospheric Research Aircraft Modification. Avcon Industries, Inc
- [STC SA04797NY](https://openairdocs.org/stc/SA04797NY): Atmospheric Research Aircraft Modification. Avcon Industries Inc
- [STC SA11300DS](https://openairdocs.org/stc/SA11300DS): Upgrade previously installed Collins Aerospace Radar Altimeter. BHE & Associates Ltd
- [STC SA2300CE](https://openairdocs.org/stc/SA2300CE): Installation of Removable External Baggage Compartment. Avcon Industries Inc
- [STC SA00263WI](https://openairdocs.org/stc/SA00263WI): Installation of 60 cubic foot cargo compartment on fuselage lower surface. Metrea Special Aerospace ISR Inc
- [STC SA01936LA](https://openairdocs.org/stc/SA01936LA): Installation of a Wescam FLIR unit into an extended fuselage nose (STC SA00367SE). Metrea Special Aerospace ISR Inc
- [STC SA03343CH](https://openairdocs.org/stc/SA03343CH): Extended Range Fuel Tanks. Metrea Special Aerospace ISR Inc
- [STC SA2794NM](https://openairdocs.org/stc/SA2794NM): Installation of Flight Equipment and Engineer Corp. passenger seats. Metrea Special Aerospace ISR Inc
- [STC SA6078NM](https://openairdocs.org/stc/SA6078NM): Installation of forward facing two-passenger seat. Metrea Special Aerospace ISR Inc
- [STC SA03342CH](https://openairdocs.org/stc/SA03342CH): Operating Weight Increase. Metrea Special Aerospace ISR Inc
- [STC SA00400BO](https://openairdocs.org/stc/SA00400BO): Installation of an Autothrottle System (ATS). Innovative Solutions & Support Inc
- [STC SA156CH](https://openairdocs.org/stc/SA156CH): Installation of a TCAS I. Acron Aviation Inc
- [STC SA9210SC-D](https://openairdocs.org/stc/SA9210SC-D): Installation of the L-3 Communications Avionics Systems Infrared Imaging System (IRIS). Acron Aviation Inc
- [STC SA04191NY](https://openairdocs.org/stc/SA04191NY): Installation of Underwing Pylons with a Pod and Underwing Wiring Tunnel. Aerospace Design & Compliance LLC
- [STC SA00225MC](https://openairdocs.org/stc/SA00225MC): Project 10684-1 Installation of Mission System Modifications for a MX-15/MX-20 Sensor System. L3Harris Technologies Integrated Systems L.P
- [STC SA11914IB](https://openairdocs.org/stc/SA11914IB): Installation of the MT-Propeller Entwicklung GmbH MTV-47-1-()-C-F-R(P)/CFR260-361(). MT-Propeller Entwicklung GmbH
- [STC SA11133SC](https://openairdocs.org/stc/SA11133SC): Installation of a Rockwell Collins Pro Line 21 update to include optional TAWS mode 5 warnings during LPV approaches, optional ADS-B Out, optional synthetic vision system (SVS), optional Communication Management Unit (CMU) and 3rd VHF to support Controller Pilot Data Link. BHE & Associates LTD
- [STC SA00416BO](https://openairdocs.org/stc/SA00416BO): Installation of an Outerlink Satellite Communications System (Satcom) and Flight Data Monitoring System Kit. Outerlink Corporation
- [STC SA11855IB](https://openairdocs.org/stc/SA11855IB): Installation of the Flap Roller Bearing Assembly. Marsh Brothers Aviation Inc
- [STC SA01101DE](https://openairdocs.org/stc/SA01101DE): Installation of Gogo AVANCE L5/LX5 System. Aviation Fabricators Inc
- [STC SA11301DS](https://openairdocs.org/stc/SA11301DS): Installation of an AirSync flight data monitoring system. BHE & Associates Ltd
- [STC SA02038WI](https://openairdocs.org/stc/SA02038WI): Installation of the Universal Avionics ClearVision and Enhanced Vision System (EVS) equipment. Global Aviation Tech LLC

All 479: https://openairdocs.org/aircraft/N350CF/stcs.md

## Earlier aircraft with N350CF

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N350CF before.

- [Cancelled 2018-09-18](https://openairdocs.org/deregistered/N350CF-2018-09-18): Eurocopter AS 350 B2, S/N 4159, built 2007. Exported to New Zealand. Owner: [Tri-State Care Flight LLC](https://openairdocs.org/faa-owner/TRI-STATE%20CARE%20FLIGHT%20LLC), [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village)

## Related

- Other Beech B300 aircraft: https://openairdocs.org/model/beech-b300/aircraft.md
- The Pratt & Whitney PT6A series engine: https://openairdocs.org/engine/pratt-whitney-pt6a-series.md

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