US Air Force Contract
Find out more about our contract with the US Air Force.
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Specifications and Performance: Mitsubishi Long Body
View Short Body
| Model | MU-2G | MU-2J | MU-2L | MU-2N | Marquise |
| Year of Mfg. | 1970-1971 | 1972-1976 | 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 | 776 | 776 | 778 |
| TBO (hrs) | 5400 | 5400 | 5400 | 5400 | 5400 |
| Dimensions | |||||
| Exterior (ft.-in.) -- Length -- Wing Span -- Height |
39'5" 39'2" 13'8" |
39'5" 39'2" 13'8" |
39'5" 39'2" 13'8" |
39'5" 39'2" 13'8" |
39'5" 39'2" 13'8" |
| Interior (ft.-in.) -- Length (Overall) -- (Excl. Cockpit) -- Height -- Width |
21'6" 16'0" 4'3" 4'11" |
21'6" 16'0" 4'3" 4'11" |
21'6" 16'0" 4'3" 4'11" |
21'6" 16'0" 4'3" 4'11" |
21'6" 16'0" 4'3" 4'11" |
| Volume (cu. ft.) -- Total pressurized -- Excluding Cockpit |
347 270 |
347 270 |
347 270 |
347 270 |
347 270 |
| Accomodations | |||||
| Crew Seats | 2 | 2 | 2 | 2 | 2 |
| Passenger -- Maximum -- Typical |
9 7 |
9 7 |
9 7 |
9 7 |
9 7 |
| Baggage Vol. -- cu. ft. -- wt. lbs. |
38 60 |
38 60 |
38 60 |
38 60 |
38 60 |
| 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 |
283 261 |
300 265 |
296 276 |
296 276 |
308 295 |
| Minimum Control | 93 | 93 | 99 | 99 | 99 |
| Stall Speed - dirty | 73 | 73 | 76 | 76 | 76 |
| Maneuvering Speed | 188 | 188 | 191 | 191 | 191 |
| Gross Wt. Performance | |||||
| Takeoff Distance Over 50ft. | 1,890 | 1,870 | 2,170 | 2,170 | 2,170 |
| Accelerate-Stop Distance | ------ | 2,625 | 3,400 | 3,300 | 3,300 |
| Landing Distance (ft) Maximum Landing wt. |
2,000 | 2,000 | 2,200 | 2,200 | 2,200 |
| Rate of Climb (fpm) -- Two-Engine -- One-Engine |
2,590 725 |
2,690 845 |
2,630 675 |
2,630 675 |
2,200 410 |
| Service Ceiling (ft) -- Two-Engine -- One-Engine |
27,000 11,600 |
30,800 18,700 |
29,600 15,450 |
29,600 15,450 |
29,750 14,800 |
| Max Wt. Limits (lbs) | |||||
| Ramp Weight | 10,800 | 10,800 | 11,625 | 11,625 | 11,625 |
| Takeoff Weight | 10,800 | 10,800 | 11,575 | 11,575 | 11,575 |
| Landing Weight | 10,260 | 10,260 | 11,025 | 11,025 | 11,025 |
| Zero Fuel Weight | N/A | N/A | 9,950 | 9,950 | 9,950 |
| Usable Fuel Capacity (gal) | 366 | 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 | 3,900 | 3,800 | 3,855 | 3,729 | 3,975 |
| Payload w/ Full Fuel | 1,448 | 1,348 | 1,403 | 1,290 | 1,275 |
| Maximum Payload (2FW less OWE) |
N/A | N/A | ------ | ------ | 2,100 |
| Range 2/Four Pax--nm (NBAA VFR reserve ISA-0 Wind Max. recommended cruise power) | 1,287 | 1,271 | 1,261 | ------ | 1,395 |
| Maximum Range--nm | 1,348 | 1,348 | 1,261 | 1,261 | 1,395 |