Joe Deaton's 1952 de Havilland Chipmunk!
Have you ever wanted to own a WWII fighter? Me too!
Has your budget kept you from owning a WWII fighter? Well, unfortunately, me too!
The next best option for those of us who want the thrill of flying a WWII era airplane on a budget are trainers. Yeah, they aren’t as fast or agile as a fighter but, they’re almost as much fun to fly!
The de Havilland Chipmunk was introduced in 1946 to replace the aging biplanes in the British training fleet. The airplane resembles typical fighter aircraft of the time but is much smaller and has considerably less horsepower. While a typical WWII fighter might have 1200HP, the Chipmunk flies behind the 145HP Gipsy Major (Affectionately called the Dripsy Major because they leak oil….a lot of oil!) inline 4 cylinder engine. The engine is canted 4 degrees to the right to mimic the high HP fighters on takeoff. You need to use generous amounts of left rudder when taking off in a Chipmunk. Wait, did I say LEFT rudder?? Yep, the engine turns the opposite direction of most airplanes, so left rudder is required when taking off.
The Chipmunk is a fun airplane. Sitting in the very “cozy” cockpit, it feels very fighter like. Even though it’s rather snug, all of the controls are easily managed.
Designed for +9 and -6 G’s, aerobatics are a delight! Rolls and loops are fun and easy to perform.
Landing the Chipmunk will spoil any tailwheel pilot. At 55kts over the fence with wide, soft landing gear and a very effective rudder, landing this taildragger is a pleasant experience.
If you would like to know more about this airplane, please ask! I am always ready for a little hangar talk!
Specifications: |
Powerplant |
Rolls-Royce Gipsy Major 8 or 10-2, 4-cyl, inverted in-line, 145 hp @ 2,550 rpm |
Recommended TBO |
1,500 hr |
Propeller |
Fairey Reed two-blade, fixed-pitch, 81-in dia |
Length |
25 ft 5 in |
Height |
7 ft |
Wingspan |
34 ft 4 in |
Wing area |
172.5 sq ft |
Wing loading |
12.8 lb/sq ft |
Power loading |
15.2 lb/hp |
Seats |
2 |
Empty weight (as tested) |
1,517 lb |
Max gross weight |
2,200 lb |
Max gross weight (aerobatics) |
2,100 lb |
Max useful load |
683 lb |
Payload w/full fuel |
550 lb |
Fuel capacity, std |
22 gal |
Oil capacity |
8 qt |
Baggage capacity |
40 lb |
PERFORMANCE |
Takeoff distance over 50-ft obstacle |
1,350 ft |
Max demonstrated crosswind component |
10 kt |
Rate of climb, sea level |
800 fpm |
Max level speed, sea level |
120 KIAS |
Cruise speed/range w/45-min rsv, std fuel (fuel consumption)
@ 75% power, 5,000 ft |
95 kt/207 nm (7.5 gph) |
Service ceiling |
15,800 feet |
Glide ratio |
10.5:1 |
Landing distance over 50-ft obstacle |
1,425 ft |
LIMITING AND RECOMMENDED AIRSPEEDS |
Takeoff safety speed |
56 KIAS |
V X (best angle of climb) |
56 KIAS |
V Y (best rate of climb) |
65 KIAS |
V A (design maneuvering) |
117 KIAS |
V FE (max flap extended) |
71 KIAS |
V NO (max structural cruising) |
155 KIAS |
V NE (never exceed) |
155 KIAS |
Best-glide speed |
60 KIAS |
Final approach speed |
60 KIAS |
Max canopy-open speed |
90 KIAS |
V S1 (stall, clean) |
47 KIAS |
V S0 (stall, landing configuration) |
43 KIAS |