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Military


AB139

AW139

Specifications
PROPULSION

Powerplants (2):

 

 

Pratt & Whitney PT6C-67C
with FADEC

 

ENGINE RATINGS:
HP
KW
     
Take off Power
2 x 1679
2 x 1252
Max Continuous Power
2 x 1531
2 x 1142
OEI max contingency 2 min.
1x 1725
1x 1286
OEI max continuous power
1x 1679
1 x 1252

 

 

    

PERFORMANCE (ISA, MTOW):

    
     
Max. Cruise Speed 157 KTAS 290 Km/hr
Vne 167 KTAS 310 Km/hr
Rate of Climb TOP AEO >2000 ft/min > 10 m/sec
HOGE TOP AEO >12000 ft > 3600/m
Max. Range - No reserve > 400 NM > 750 Km
Max. Endurance - No reserve 3.9 hrs 3.9 hrs

 

 

    
ft
m
Internal cabin size (L x W x H) 8.86 x 6.56 x 4.66 2.7 x 2.0 x 1.42
Sliding and plug-in cabin door (L x H) 5.51 x 4.43 1.68 x 1.35
Length overall* 54.63 16.65
Height overall* 16.24 4.95

Rotor diameter

*Rotors turning

 45.28 13.80

 

Back to top

 

    
WEIGHTS:
Lb
Kg
Max. Take-off
13,227
6,000
Useful load (external) 6,000 2,700

 

 

    
CAPACITIES:    
Required Crew
1-2
  
Seating
 up to 15  
Stretchers
up to 6
(with 4 attendants)
Baggage compartment
120 cu ft
3.4 cu m

 

 

    
FEATURES:
(Category "A" at MTOW)		    
  • Four (4) blade canted tail rotor
  • High tail rotor ground clearance
  • Five (5) blade fully articulated main rotor
  • Excellent visibility
  • Honeywell Primus Epic modular/intergrated
    glass cockpit
  • Ice detection & protection option
  • Refueling either side
  • Large baggage compartment
    (Accessible from the cabin and externally, both sides)
  • Large unobstructed cabin
  • Two large "plug-in" type sliding doors
  • Crashworthy crew/passenger seats
  • Day/night single pilot IFR
  • All Weather Operations (AWO)
    
   
     



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