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| Technical
Specifications |
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The
Magister was a single engine two-seat low-wing
cantilever monoplane with a fixed tricycle
undercarriage. The aircraft was of wooden
construction with magnesium alloy castings
used for stressted parts. It was designed
for elementary training, including aerobatics
and also as a communications aircraft.
Also known as the M.14
Hawk Trainer (civilian role) the Miles Magister
was designed and constructed by Philips
& Powis Aircraft Company. |
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Length |
24'7.5" (7.510mm)
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| Wing span/wing chord,
max |
33'10"/6'3"
(10,310/1.910mm) |
| Centre plane span |
7'11.625" (2,430mm) |
| Tailplane span/tailplane
chord, max. |
9'0"/3'7.125"
(2.740/1.100mm) |
| Height |
9'9" (2.970mm) |
| Wheel track |
7'4.5" (2,250mm) |
| Dihedral, centre
plane/outer wings/tailplane |
0o/6o +15/0o |
| Incidence, centre
plane/2/3 of outer wings/tailplane |
1o30+5'/1o7.5' +30'/0o38'+20' |
| Sweepback angle,
at wing leading edge |
3o30' |
| Aileron deflection
angle, up/down |
+23.5o + 0.5o/-9.5o-0.5o |
| Flaps fully down,
fuselage.main plane |
-71o _ 10o.78o_10o |
| Elevator deflection
angle up/down |
+31o + 0.5o/-24o-0.5o |
| Rudder deflection
angle |
+30o |
| Wing area total |
224.96 sq ft (20.90m2) |
| Horizontal.vertical
tail surface area, total |
28.50/12.64 sq ft
(2.65/1.17m2 |
| Loading, max power |
14.6 ib/hp (8.9 kg
kW1) |
| Loading max wing |
8.4ib/sq ft (41.3
kg m2) |
| Weight, empty |
1,286ib (583 kg) |
| Max take-off weight |
1,900ib (862 kg) |
| Max aerobatics |
1,845ib (837 kg) |
| Max, speed, at sea
level |
142mph (229 km h-1) |
| Max, speed, at 5,000
ft |
130 mph (209 km h-1) |
| Max, speed, at 10,000
ft |
125 mph (201 km h-1) |
| Take-off speed |
55 mph (88/69 km
h-1) |
| Landing speed, flaps
up/down |
52/43 mph (84/69
km h-1) |
| Cruising speed/initial
climbing speed |
124/70mph (200/113
km h-1) |
| Rate of climb, initial
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750 ft/min (3.8 m
s-1) |
| Climbing time to
5,000 ft (1,525 m) |
7.6 min |
| Climbing time to 10,000 ft (3,050
m) |
18.8min |
| Service/max, ceiling |
16,500/19,000 ft (5,029/5,791 m) |
| Take-off/landing run |
630/420 ft (192/128 m) |
| Take-off/landing run to/from 50 ft
(15 m) |
1,200/975 ft (366/297 m) |
| Range |
367 miles (591 km) |
| Duration, max, fuel capacity |
3hr |
| Engine |
1 x Gipsy Major I |
| Engine Power |
2,350 rpm |
| Propeller |
two-bladed wooden propeller |
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