N1805D - 1981 BEECH A36TC - Complete Aircraft History & Registry Information

Quick Facts & Current Owner

Current Owner
DODSON INTERNATIONAL PARTS INC
Location
RANTOUL, Kansas
Registration Status
Active until 01-31-2030
Serial Number
EA-233
Last Seen on Market
Never Listed
Last Seen Airborne
No Recent Activity
Last FAA Action Date
February 2023
Owned Since
January 2023
Location of N1805D in RANTOUL, Kansas

About the BEECH A36TC

The Beechcraft A36TC, a variant of the highly respected Bonanza series, holds a significant place in general aviation history for its combination of performance, reliability, and versatility. Introduced by Beech Aircraft Corporation, now a part of Textron Aviation, the A36TC first took to the skies in the late 1970s. It was developed to address the market demand for a high-performance, turbocharged version of the already popular Beechcraft A36 Bonanza, enhancing its capability to operate from high-altitude airports and in hot weather conditions without sacrificing performance. This model primarily targets private pilots, aviation enthusiasts, and small business owners who require efficient and reliable transportation over varying distances and terrain conditions. Production of the A36TC began in 1979 and continued until 1981, during which a relatively small number of units were produced, making this model somewhat of a collector's item today. The aircraft is powered by a turbocharged Continental TSIO-520-UB engine, generating 300 horsepower and enabling a maximum cruise speed of approximately 197 knots. Its range is roughly 836 nautical miles, with fuel consumption managed economically due to the efficient powerplant. One of the standout features of the A36TC is its cabin comfort, a significant factor in its niche appeal. It offers club seating for up to six passengers, with large windows providing an airy feel and excellent visibility. The aircraft also includes advanced navigation and autopilot systems for its time, enhancing safety and ease of flight, especially on long journeys. Despite its relatively short production run, the Beechcraft A36TC remains a beloved model in the general aviation community, lauded for its robust build, impressive performance, and the luxurious comfort it offers, making it an attractive choice for those seeking a blend of practicality and sophistication in their flying endeavors.



Flight History and Activity for N1805D

No flight activity has been observed for this aircraft since 2022.

This could indicate the aircraft is in storage, undergoing maintenance, or operating in areas without flight tracking coverage.

Maintenance and Safety Records

Safety Record Summary

  • 2 accident/incident report(s) on file

Accident and Incident Reports

November 15, 2021 - ROCKPORT, Texas

Damage Level
Substantial
Description
DURING PREFLIGHT PILOT VERIFIED FUEL QUANTITY VIA COCKPIT INSTRUMENTS ONLY AND DID NOT OPEN A WING TANK TO PHYSICALLY VERIFY FUEL QUANTITY. PILOT STATED FUEL QUANTITY ON THE LEFT WING TANK INDICATED BETWEEN 1/4 TO 1/2 ON THE FUEL GAUGE. PILOT STATED HE ESTIMATED THAT THE LEFT TANK HAD APPROXIMATELY 15 GALLONS OF FUEL. PILOT USED LEFT WING TANK FOR TAXI, TAKEOFF AND CLIMB TO CRUISING ALTITUDE OF 3500 FEET. PILOT STATED HE SWITCHED TO THE LEFT WING TIP TANK AFTER REACHING CRUISING ALTITUDE. PILOT STATED HE OBSERVED FUEL STREAMING FROM THE FUEL CAP OF BOTH WING TANKS DURING THE FLIGHT. PILOT SWITCHED FROM THE LEFT WING TIP TANK TO THE LEFT WING TANK APPROXIMATELY 15 MINUTES PRIOR TO LANDING. PILOT STATED AT THE FINAL APPROACH FIX TO RNAV 14 KRPK HE CONFIGURED THE AIRPLANE FOR LANDING AND LOWERED THE GEAR. PILOT STATED THE ENGINE SPUTTERED A FEW TIMES AND QUIT SHORTLY AFTER LOWERING THE GEAR. PILOT STATED HE SWITCHED TO THE RIGHT WING TANK IN AN ATTEMPT TO RESTART THE ENGINE. PILOT STATED HE DID NOT VERIFY FUEL FLOW OR ACTIVATE THE AUXILIARY FUEL BOOST PUMP AS RECOMMENDED IN THE AIRCRAFT'S PILOT OPERATOR HANDBOOK. PILOT STATED WHEN THE ENGINE FAILED TO RESTART HE SWITCHED BACK TO THE LEFT WING TANK, RAISED THE LANDING AND DITCHED THE AIRCRAFT IN THE COPANO BAY APPROXIMATELY 2NM SHORT OF RWY 14.

November 15, 2021 - Rockport, Texas

Damage Level
Substantial
Description
The private pilot stated that, before departure for the 45-minute flight, the airplane contained 70 total gallons of fuel: 20 gallons in each wing tip tank and about 15 gallons in each main tank. Shortly after departure, the pilot switched the fuel selector from a main tank to the left tip tank. About 20 minutes into the flight, the pilot noticed β€œa trail of fuel being sucked out of both the left and right main [tank] gas caps.” The pilot decided to continue the flight because, at that time, the airplane was about halfway to the destination airport and the weather was favorable. In preparation for the visual approach, the pilot switched the fuel selector to the left main fuel tank. When the airplane was at an altitude of 1,200 ft and was about 4 miles from the runway, the engine β€œsputtered a couple of times and quit completely.” The pilot switched to the right main fuel tank, which indicated 1/2 fuel and attempted an engine restart that was unsuccessful. The pilot switched back to the left main fuel tank, which also indicated 1/2 fuel. The pilot recognized that the airplane was not going to make it to the runway, so he ditched the airplane into the water about 1.5 miles short of the runway. The airplane sustained substantial damage to the fuselage, both wings and ailerons. Postaccident examination of the airframe revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. The fuel selector was found in the left main fuel tank position. The engine and magnetos could not be functionally tested due to water immersion/damage. The enginedriven fuel pump was removed; residual fuel, consistent with aviation gasoline, drained from the fuel pump, and the drive spline was intact. Application of compressed air to the fuel system revealed the venting of air from the left and right fuel caps; no additional anomalies were noted with the fuel system. Both the left and right fuel caps showed evidence of water corrosion, and the cap O-rings appeared dry and pliable. Although the pilot reported observing fuel draining from the fuel caps, he also reported the airplane fuel tank indicators showed about one-half of the fuel capacity in each main fuel tank when the engine lost power. As a result, the reason for the total loss of engine power could not be determined based on the available evidence for this investigation.

Complete History Timeline

πŸ“‹

Feb 2023

Registration

Registered to DODSON INTERNATIONAL PARTS INC in RANTOUL, KS




πŸ“‹

Jan 2023

Registration

Registered to DODSON INTERNATION PARTS INC in RANTOUL, KS




⚠️

Nov 2021

Accident/Incident

Accident with substantial damage




⚠️

Nov 2021

Accident/Incident

Accident with substantial damage




πŸ“‹

Apr 2021

Registration

Registered to MCTEE CLIFFORD R III in AUSTIN, TX




πŸ“‹

Dec 2019

Registration

Registered to RICHARD D MARTIN INSURANCE SERVICES INC in WOODLAND HILLS, CA




πŸ“‹

Oct 2016

Registration

Registered to RICHARD D MARTIN INSURANCE SERVICES INC in LOS ANGELES, CA




πŸ“‹

Dec 2013

Registration

Registered to RICHARD D MARTIN INSURANCE SERVICES INC in LOS ANGELES, CA




πŸ“‹

Sep 2012

Registration

Registered to RICHARD D MARTIN INSURANCE SERVICES INC in LOS ANGELES, CA




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Frequently Asked Questions

Who owns N1805D?

N1805D is currently registered to DODSON INTERNATIONAL PARTS INC in RANTOUL, Kansas.

What type of aircraft is N1805D?

N1805D is a 1981 BEECH A36TC with serial number EA-233.

Has N1805D been in any accidents?

Yes, N1805D has 2 accident/incident report(s) on file with the FAA/NTSB.