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Military


T-41A/C Mescalero

Specifications
Span 35 ft. 10 in.
Length 26 ft. 11 in.
Height 8 ft. 10 in.
Weight 2,300 lbs. loaded [T-41A]
2550 lbs (1,135 kg) [T-41C/D]
Armament None
EngineOne Continental O-300-C six-cylinder piston engine of 145 hp [T-41A]
one Continental piston engine (IO-360-DB) 210 horsepower [T-41C/D]
Maximum speed 139 mph [T-41A]
182 mph [T-41C/D]
Cruising speed 117 mph.
Range 720 miles [T-41A]
690 miles (600 nautical miles/1,104 km) at 10,000 feet (3,000 meters) [T-41C/D]
Service Ceiling 13,100 ft. [T-41A]
16,000 feet (4,850 meters) [T-41C/D]
Cost $13,465
INVENTORY 50 at Hondo, Texas, 50 at the U.S. Air Force Academy at Colorado Springs, Colo.
AIRCRAFT
MODEL
C-172 K C-172 M C-172 M C-172 N C-172 P C-172 S T-41 C T-41 B C-182 RG
AIRSPEED MPH MPH KTS KTS KTS KTS MPH MPH KTS
ROTATION 60 60 55 55 55 55 60 60 55
NORMAL CLIMB 80 80 70 70 70 70 100 85 80
Vx (SL-10K) 68-74 75 64-62 59-61 60-65 62-67 85 75 72-74
Vy (SL-10K) 82-79 91-80 78-68 73-68 76-71 74-72 100-91 95-87 88-86
SHORT FIELD T/O 68 68 59 59 56 56 71 60 59
Va
(Weight)
122
(2300)
112
(2300)
97
(2300)
89
(1950)
80
(1600)
97
(2300)
89
(1950)
80
(1600)
99
(2400)
92
(2000)
82
(1600)
105
(2550)
98
(2200)
90
(1900)
125
(2500)
127
(2500)
112
(3100)
102
(2600)
91
(2100)
BEST GLIDE 80 80 65 65 65 68 85 85 75
DOWNWIND 95 95 85 85 85 85 95 95 85
BASE 85 85 75 75 75 75 85 85 75
FINAL 75 75 65 65 65 70 75 75 70
SHORT FINAL
FLAPS UP
FLAPS DOWN

70
65

70
65

60
55

60
55

65
60

65
60

75
70

70
65

70
65
SHORT FIELD LDG 69 69 60 60 61 61 75 60 64
Vno 140 145 128 128 127 129 146 145 157
Vne 174 182 160 160 158 163 185 182 179
Vfe 100 100 85 85 85 85 100 100 95
Vs 57 61 47 47 44 48 64 64 43
Vso 49 54 42 42 33 40 53 56 43
USABLE FUEL(GAL) 38 38
48 (9621V)
38 38 40
50
(6601K)
53 51 51 88
MAX WEIGHT(lbs) 2300 2300 2300 2300 2400 2550 2500 2500 3100



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