US Air Force Contract
Find out more about our contract with the US Air Force.
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Specifications and Performance: Mitsubishi Short Body
View Long Body
| Model | MU-2F | MU-2K | MU-2M | MU-2P | Solitaire |
| Year of Mfg. | 1968-1972 | 1972-1974 | 1975-1976 | 1977-1978 | 1979-1985 |
| Engines | TPE331-1 | TPE331-6 | TPE331-6 | TPE3331-5 | TPE331-10 |
| Manufacture | Garrett | Garrett | Garrett | Garrett | Garrett |
| SHP | 705 | 724 | 724 | 724 | 727 |
| TBO (hrs) | 5400 | 5400 | 5400 | 5400 | 5400 |
| Dimensions | |||||
| Exterior (ft.-in.) -- Length -- Wing Span -- Height |
33'3" 39'2" 12'11" |
33'3" 39'2" 12'11" |
33'3" 39'2" 12'11" |
33'3" 39'2" 12'11" |
33'3" 39'2" 12'11" |
| Interior (ft.-in.) -- Length (Overall) -- (Excl. Cockpit) -- Height -- Width |
13'5" 8'0" 4'3" 4'11" |
13'5" 8'0" 4'3" 4'11" |
13'5" 8'0" 4'3" 4'11" |
13'5" 8'0" 4'3" 4'11" |
13'5" 8'0" 4'3" 4'11" |
| Volume (cu. ft.) -- Total pressurized -- Excluding Cockpit |
245 168 |
245 168 |
245 168 |
245 168 |
245 168 |
| Accomodations | |||||
| Crew Seats | 2 | 2 | 2 | 2 | 2 |
| Passenger -- Maximum -- Typical |
7 6 |
7 6 |
7 6 |
7 6 |
7 6 |
| Baggage Vol. -- cu. ft. -- wt. lbs. |
31 574 |
31 574 |
43 574 |
43 574 |
43 574 |
| Pressurization | |||||
| psi | 5.0 | 5.0 | 6.0 | 6.0 | 6.0 |
| S.L. Cabin to ft. | 12,000 | 12,000 | 14,000 | 14,000 | 14,000 |
| 8000 Cabin to ft. | 23,000 | 23,000 | 27,000 | 27,000 | 27,000 |
| Speeds (ktas) | |||||
| VMO | 250 | 250 | 250 | 250 | 250 |
| Cruise Speeds -- Maximum -- Normal |
296 270 |
317 270 |
317 283 |
316 283 |
321 313 |
| Minimum Control | 93 | 93 | 99 | 93 | 93 |
| Stall Speed - dirty | 71 | 71 | 76 | 76 | 73 |
| Maneuvering Speed | 181 | 181 | 191 | 182 | 182 |
| Gross Wt. Performance | |||||
| Takeoff Distance Over 50ft. | 1,700 | 1,700 | 1,800 | 1,800 | 1,800 |
| Accelerate-Stop Distance | 2,675 | 2,650 | 2,770 | 2,750 | 2,750 |
| Landing Distance (ft) Maximum Landing wt. |
1,550 | 1,800 | 1,960 | 1,950 | 1,950 |
| Rate of Climb (fpm) -- Two-Engine -- One-Engine |
2,875 920 |
3,100 920 |
2,350 760 |
2,350 760 |
2,350 475 |
| Service Ceiling (ft) -- Two-Engine -- One-Engine |
30,400 14,800 |
33,200 19,800 |
32,200 18,000 |
32,200 18,000 |
33,500 16,900 |
| Max Wt. Limits (lbs) | |||||
| Ramp Weight | 9,920 | 9,920 | 10,520 | 10,520 | 10,520 |
| Takeoff Weight | 9,920 | 9,920 | 10,470 | 10,470 | 10,470 |
| Landing Weight | 9,435 | 9,435 | 9,955 | 9,955 | 9,955 |
| Zero Fuel Weight | N/A | N/A | ------ | ------ | 9,700 |
| Usable Fuel Capacity (gal) | 336 | 366 | 366 | 364 | 403 |
| -- (6.7 lb/gal.) - lbs | 2,452 | 2,452 | 2,452 | 2,439 | 2,700 |
| Useful Load & Ramp (lbs) | |||||
| Useful Payload | 3,420 | 3,370 | 3,428 | 3,422 | 3,510 |
| Payload w/ Full Fuel | 968 | 918 | 976 | 983 | 810 |
| Maximum Payload (2FW less OWE) |
N/A | N/A | ------ | ------ | 2,490 |
| Range 2/Four Pax--nm (NBAA VFR reserve ISA-0 Wind Max. recommended cruise power) | 1,358 | 1,391 | ------ | ------ | 1,455 |
| Maximum Range--nm | 1,428 | 1,461 | 1,330 | 1,461 | 1,600 |