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Boone, Edney Sterling CD (Corporal)

Killed in Flying Accident 1977-April-06

Birth Date: 1936-April-09 (age 40)

Born: Aroostook Junction, New Brunswick

Son of George Ellis and Rose (nee Balch) Boone of Aroostook, New Brunswick.

Home: Aroostook Junction, New Brunswick

Enlistment: Edmonton, Alberta

Enlistment Date: 1967-05-29

Decorations: CD


Canadian Forces Decoration
Service
RCAF
Unit
Aerospace Engineering and Test Establishment 
Rank
Corporal
Marshal
Air Chief MarshalA/C/M
Air MarshalA/M
Air Vice MarshalA/V/M
Air CommodoreA/C
Group CaptainG/C
Wing CommanderW/C
Squadron LeaderS/L
Flight LieutenantF/L
Flying OfficerF/O
Pilot OfficerP/O
Warrant Officer 1st ClassWO1
Warrant Officer 2nd ClassWO2
Flight SergeantFS
SergeantSGT
CorporalCPL
Senior AircraftmanSAC
Leading AircraftmanLAC
Aircraftman 1st ClassAC1
Aircraftman 2nd ClassAC2
Position
Service Numbers
220504
Two other personnel from AETE were also killed in this accident.

Canada Source Canadian Virtual War Memorial

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Crew on Twin Huey 135101

Bell CH-135 Twin Huey

Source: Harold A Skaarup Web Page (Bill Cummings Photo)
Bell CH-135 Twin Huey Helicopter (Serial No. 135115)

The Bell UH-1N Twin Huey is a medium military helicopter. A member of the extensive Huey family, it first flew in 1969. The CUH-1N Twin Huey (later CH-135 Twin Huey) was the original version, first ordered by the Canadian Forces. The UH-1N has a 15-seat configuration, with one pilot and 14 passengers. In cargo configuration, it has an internal capacity of 220 ft³ (6.23 m³). An external load up to 5,000 lb (2,268 kg) can be carried. The UH-1N was later developed into the civilian Bell 212.

Based on the stretched-fuselage Bell 205, the Bell 212 was originally developed for the Canadian Forces (CF) under the designation CUH-1N Twin Huey. Later, the CF adopted a new designation system and the aircraft was redesignated CH-135 Twin Huey. The CF approved the development of the aircraft on 1 May 1968 and purchased 50 aircraft, with deliveries commencing in May 1971.

The UH-1N's main rotor is powered by a PT6T-3/T400 Turbo Twin Pac made up of two Pratt & Whitney Canada PT6 power sections that drive a single output shaft. They are capable of producing up to 1,342 kW (1,800 shp). Should one power section fail, the remaining section can deliver 671 kW (900 shp) for 30 minutes or 571 kW (765 shp), enabling the UH-1N to maintain cruise performance at maximum weight.

The aircraft were retired from the Canadian Forces starting in 1996 and struck off strength in December 1999. Two CH-135s are on display in museums, one at the Canada Aviation Museum in Ottawa and one at the National Air Force Museum of Canada at CFB Trenton. Wikipedia (with revisions)

Wkikpedia Wikipedia Bell CH-135 Twin Huey

General Harold A Skaarup Web Page

General Canada Aviation and Space Museum

General Helis Web Page

CASPIR Aircraft Groups:
RCAF On Strength (50), Canadian Aircraft Losses (3)
last update: 2021-11-01 18:48:41

Twin Huey 135101

US UH-1N 70-15650, serial and designation used for book keeping, never marked. With Aerospace Engineering Test Establshment at CFB Cold Lake, Alberta, when it crashed on 6 April 1977, near Cold Lake.
1971-10-19 Taken on Strength 2019-08-20
1979-03-20 Struck off Strength Struck off after crash. 2019-08-20

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