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Military


C-26 Metroliner

Specifications
MODEL C-26A
Metro III
Model SA227-AC
C-26B
Metro 23
Model SA227-DC
UC-26C
Merlin IV-C
Engines - number 2
Engines -Type
  • TPE331-llU-601G or -611G
  • (with Dowty Rotol propellers)
  • TPE331-llU-602G or -612G

  • (with McCauley propellers)
  • TPE331-12UA-701G
  • TPE331-12UAR-701G
  • TPE331-12UHR-701G
  • TPE331-3U-303G
Engine Mfg. Garrett (AiResearch)
SHP 11001100840
Length 42.17 ft59.33 ft
Wing Span 46.25 ft57.0 ft
Height 16.83 ft16.67 ft
Crew Seats 222
Passengers 221914
Ramp Weight 14,110 lbs16,600 lbs12,560 lbs
Takeoff Weight 14,000 lbs16,500 lbs12,500 lbs
Landing Weight 14,000 lbs15,675 lbs12,500 lbs
Zero Fuel Weight 13,13014,500 lbs8,320 lbs
Usable Fuel 652 gal652 gal544 gal
Usable Fuel
(@ 6.7 lb/gal.)
3,480 lbs3,480 lbs3,645 lbs
Max Range
(NBAA IFR reserves)
2,025 nm2040 nm1,580 nm
SPEED Max Oper 248 (ktas) 248 (ktas) 248 (ktas)
Ceiling 31,000 ft25,000 ft30,000 ft



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