# N71: 1988 Beech 300

- Status: Valid registration
- Airframe: [Beech 300](https://openairdocs.org/model/beech-300) (registry code 1152930, 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: FF-6
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: December 30, 1994
- Certificate issued: September 1, 1988
- Expires: April 30, 2028
- Mode S code: A979B3
- Registered owner: [Federal Aviation Administration](https://openairdocs.org/faa-owner/FEDERAL%20AVIATION%20ADMINISTRATION)
- Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)
- Owner type: Government
- Owner's area on the map: 35.3806° N, 97.6484° W: Placed by OpenAirDocs at the center of ZIP code 73169, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=71
- Page: https://openairdocs.org/aircraft/N71

From the FAA registry file of October 21, 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): 59 in force

### Matched by airframe (Beech 300)

- [AD 2025-07-01](https://openairdocs.org/ad/2025-07-01): Air Data Computer · Synthetic Vision Electronic Flight Information System (Arrow STC SR09595RC or ST01523WI). Effective May 15, 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 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 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005
- [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 2004-23-02](https://openairdocs.org/ad/2004-23-02): Nose Landing Gear (NLG) Fork · Textron 100, 1900, 1900C and 50 more. Effective Dec 23, 2004
- [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 2004-08-15](https://openairdocs.org/ad/2004-08-15): TAWS8000 terrain awareness warning systems (TAWS) · Cessna 421, 500, 501 and 18 more. Effective Jun 7, 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 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 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 98-08-20](https://openairdocs.org/ad/98-08-20): Autopilot Servo Actuators · Alliedsignal Avionics Autopilot Servo Actuators, Mystere-Falcon 20 - C5, Mystere-Falcon 20 - D5 and 17 more. Effective Jun 2, 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 94-01-06](https://openairdocs.org/ad/94-01-06): Traffic Alert and Collision Avoidance System II Processors · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 176 more. Effective Feb 4, 1994
- [AD 93-04-02](https://openairdocs.org/ad/93-04-02): Transponders · BAE Systems ATP, CL-600-2A12 (CL-601), DHC-8-101 and 23 more. Effective Mar 26, 1993
- [AD 93-01-20](https://openairdocs.org/ad/93-01-20): Aft Cowling Doors · Textron 300. Effective Mar 10, 1993
- [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
- [AD 91-12-11](https://openairdocs.org/ad/91-12-11): Side Windows · Textron 200, 200C, 200CT and 7 more. Effective Jul 15, 1991
- [AD 91-12-10](https://openairdocs.org/ad/91-12-10): Wing Spar Attachment · Textron 300, 300LW, B200 and 2 more. Effective Jul 15, 1991
- [AD 89-19-04 R1](https://openairdocs.org/ad/89-19-04-R1): Wing Fuel Bay Skin Panels · Textron 200, 200C, 200CT and 6 more. Effective Jul 9, 1990
- [AD 90-08-17](https://openairdocs.org/ad/90-08-17): Fuselage Moisture Drain System · Textron 100, 200, 200C and 32 more. Effective May 7, 1990
- [AD 90-06-13](https://openairdocs.org/ad/90-06-13): Vertical Gyro · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 14 more. Effective Mar 30, 1990
- [AD 89-22-14](https://openairdocs.org/ad/89-22-14): Aileron Flutter · Textron 200, 200C, 200CT and 9 more. Effective Nov 17, 1989
- [AD 87-04-24](https://openairdocs.org/ad/87-04-24): Elevator Trim Cable System · Textron 1900, 1900C, 200 and 28 more. Effective Apr 14, 1987

### 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 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 87-22-01 R1](https://openairdocs.org/ad/87-22-01-R1) (historical): Nose Landing Gear Fork · Raytheon 100 Model or Series (all), 1900, 1900C and 50 more. Effective Sep 30, 1989
- [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) (13 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 CE-06-27](https://openairdocs.org/saib/CE-06-27): . Issued Jan 30, 2006
- [SAIB CE-03-43R1](https://openairdocs.org/saib/CE-03-43R1): . Issued Sep 23, 2003
- [SAIB CE-02-19](https://openairdocs.org/saib/CE-02-19): . Issued Mar 11, 2002
- [SAIB CE-02-11R1](https://openairdocs.org/saib/CE-02-11R1): . Issued Feb 22, 2002
- [SAIB CE-00-16](https://openairdocs.org/saib/CE-00-16): . Issued Feb 4, 2000
- [SAIB ACE-96-15](https://openairdocs.org/saib/ACE-96-15): . Issued Dec 20, 1996
- [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
- [SAIB CE-03-43](https://openairdocs.org/saib/CE-03-43) (historical): . Issued Jun 27, 2003
- [SAIB CE-02-11](https://openairdocs.org/saib/CE-02-11) (historical): . Issued Jan 4, 2002

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB OPS10IA155](https://openairdocs.org/ntsb/OPS10IA155), Apr 22, 2010: Beech 300 (N71), Chicago, IL, incident, no damage. Probable cause: The air traffic controller's issuance of an improper takeoff clearance to the pilot of the Embraer. Contributing to the incident was the instructor’s inadequate monitoring of the trainee local…

## FAA accident and incident reports

None matched to N71.

## Service difficulty reports (18)

As reported by operators and repair stations. Reports filed since May 4, 1964, when the mark's previous registration was cancelled.

- [SDR RU3A2021100600014](https://openairdocs.org/sdr/RU3A2021100600014), Oct 5, 2021: BLADDER. LEAKING. DEFECT: STRONG FUEL SMELL/ODOR AFTER TAKE-OFF, ACFT DECLARED IFE AND RETURNED BACK TO DEPARTURE AIRPORT (BNA). MXC PLAN: N71’S RT AUX FUEL BLADDER WAS JUST REPL
- [SDR RU3A2020100500032](https://openairdocs.org/sdr/RU3A2020100500032), Oct 5, 2020: LANDING GEAR. COLLAPSED. RIGHT MAIN LANDING GEAR COLLAPSED ON LANDING ROLLOUT.
- [SDR RU3A201912163074](https://openairdocs.org/sdr/RU3A201912163074), Dec 13, 2019: STRINGER. DAMAGED. MAJOR REPAIR ENGINEERING ORDER TO REPAIR DAMAGE FOUND DURING INSPECTION IN THE WEB OF STRINGER CAUSED BY SCREW THREADS, WHICH IMPINGED ON THE STRINGER WEB DUE T
- [SDR RU3A201910218053](https://openairdocs.org/sdr/RU3A201910218053), Oct 18, 2019: PRESSURE SWITCH. MALFUNCTIONED. RT FUEL XFER AMBER LIGHT CAME ON IN FLIGHT LONG WITH LOW PRESSURE LIGHT. MAINTENANCE REPLACED RIGHT ENGINE LOW FUEL PRESSURE SWITCH.
- [SDR RU3A2018053029023](https://openairdocs.org/sdr/RU3A2018053029023), May 29, 2018: TUBE. CHAFED. RIGHT BLEED AIR FAIL ILLUMINATED IN FLIGHT, WENT OUT DURING DESCENT. FOUND EVA TUBING CHAFED ON THE METAL TAPE AROUND BLEED LINE, OTBD OF RT INBD WING. NO EVIDE
- [SDR RU3A20170907028](https://openairdocs.org/sdr/RU3A20170907028), Sep 7, 2017: PRESSURE BLKHD. GOUGED. MID RIGHT ZONE OF THE AFT PRESSURE BULKHEAD IS GOUGED. REPAIRED IAW EO 15-28-10.
- [SDR RU3A20170907027](https://openairdocs.org/sdr/RU3A20170907027), Sep 7, 2017: PRESSURE BLKHD. GOUGED. UPPER LEFT ZONE OF AFT PRESSURE BULKHEAD IS GOUGED. REPAIRED IAW EO 15-28-10.
- [SDR RU3A20170907026](https://openairdocs.org/sdr/RU3A20170907026), Sep 6, 2017: BULKHEAD WEB. GOUGED. UPPER RIGHT ZONE OF THE AFT PRESSURE BULKHEAD IS GOUGED. REPAIRED IAW EO 15-28-10.
- [SDR RU3A20150925018](https://openairdocs.org/sdr/RU3A20150925018), Sep 25, 2015: TUBE. DAMAGED. LEFT BLEED AIR FAIL & MASTER CAUTION ILLUMINATED. WARNING LIGHT EXTINGUISHED AFTER COMPLETING IMMEDIATE ACTION ITEMS. FOUND EVA TUBING IN NEED OF REPAIR. REPAIR
- [SDR RU3A20150918019](https://openairdocs.org/sdr/RU3A20150918019), Sep 18, 2015: SENSE LINE. DAMAGED. RIGHT BLEED AIR FAIL & MC ILLUMINATED. A HOLE WAS DISCOVERED IN THE EVA SENSE LINE IN RT NACELLE LE. LINE WAS REPLACED WITH NO DEFECTS NOTED.
- [SDR RU3A20140205007](https://openairdocs.org/sdr/RU3A20140205007), Feb 5, 2015: SWITCH. OUT OF ADJUST. CABIN DOOR ANNUNCIATOR ILLUMINATED DURING FLIGHT. ADJUSTED CABIN DOOR LOCK SWITCH.
- [SDR RU3A20140204006](https://openairdocs.org/sdr/RU3A20140204006), Feb 4, 2015: TUBE. RUPTURED. WITH RT BLEED AIR PNEUMATIC ENV OFF, RT BLEED FAIL LIGHT INTERMITTENT ON & OFF. FOUND & REPLACED RUPTURED EVA TUBE.
- [SDR RU3A20140401037](https://openairdocs.org/sdr/RU3A20140401037), Apr 1, 2014: SKIN. CRACKED. CRACKS SUSPECTED IN FUSELAGE SKIN VERIFIED BY NDT. THE DAMAGED AREA IS LOCATED INBD OF STRINGER 14L & NEAR FRAME 177.5. THE TWO FORE AFT CRACKS IN THE BELLY SKI
- [SDR RU3A1101](https://openairdocs.org/sdr/RU3A1101), Jan 20, 2011: LIGHT. INOPERATIVE. ON APPROACH, LANDING GEAR EXTENDED. LANDING GEAR APPEARED TO EXTEND NORMALLY, HOWEVER RIGHT MAIN GEAR INDICATED UNSAFE (GREEN DOWN AND LOCKED LIGHT NOT ILLUMINA
- [SDR RU3A0706](https://openairdocs.org/sdr/RU3A0706), Jul 18, 2007: UNKNOWN. WARNING LIGHT. DURING FLARE FOR LANDING, THE AIRCRAFT ABRUPTLY AND WITHOUT WARNING YAWED HARD RIGHT. TOUCHDOWN OCCURRED DURING THE GO-AROUND. THE PILOT NOT FLYING REPORTED THA
- [SDR RU3A0702](https://openairdocs.org/sdr/RU3A0702), May 16, 2007: PROPELLER. OUT OF ADJUST. RT PROP PITCH LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT YAWED RIGHT. POWER INCREASED TO MAINTAIN CONTROL. WHEN RETURNED TO IDLE FOR LANDING IT WAS OK. TROUBLESHOT A
- [SDR RU3A99014](https://openairdocs.org/sdr/RU3A99014), Dec 10, 1999: SWITCH. STICKING. LANDING GEAR FAILED TO EXTEND WHEN 'GEAR DOWN' SELECTED.. RESULTED IN EMERGENCY EXTENSION OF LANDING GEAR. THE MICRO-SWITCH IN THE LANDING GEAR CONTROL SWITCH A
- [SDR RU3A95005](https://openairdocs.org/sdr/RU3A95005), Mar 28, 1995: BULB. FAILED. PRECAUTIONARY LANDING WAS MADE AFTER NOSE AND RT MLG LIGHTS FAILED TO LIGHT DURING MANUAL EXTENSION. LIGHT BULBS IN GEAR LIGHTS WERE FOUND BURNED OUT. LIGHT BUL

## Earlier aircraft with N71

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N71 before.

- [Cancelled 1964-05-04](https://openairdocs.org/deregistered/N71-1964-05-04): Douglas DC3C-S1C3G, S/N 9005. Owner: [Federal Aviation Agency](https://openairdocs.org/faa-owner/FEDERAL%20AVIATION%20AGENCY), [Washington, DC](https://openairdocs.org/faa-place/DC/Washington)
- [Cancelled 1930-04-29](https://openairdocs.org/deregistered/N71-1930-04-29): Lincoln Standard LINCOLN STANDARD, S/N 0001. Owner: [Sagmiller J S](https://openairdocs.org/faa-owner/SAGMILLER%20J%20S), [Bowman, ND](https://openairdocs.org/faa-place/ND/Bowman)

## Related

- Other Beech 300 aircraft: https://openairdocs.org/model/beech-300/aircraft.md
- STCs for the Beech 300: https://openairdocs.org/model/beech-300/stcs.md
- The Pratt & Whitney PT6A series engine: https://openairdocs.org/engine/pratt-whitney-pt6a-series.md

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