Reference Material

Please refer to the Pilot’s Operating Handbook and Rotorcraft Flight Manual for specific reference and information.
The POH contains all aircraft operating specifications, limitations, and performance charts.

 

1.WEIGHTS

Empty 7,341 lbs
Fuel 1,600 lbs (242 US Gal)
Flight Crew 200 lbs (x4)
Bagage 205 lbs
Patient >350lbs (not incl stretcher)
Stretcher 151 lbs
Maximum T/O 10,500 lbs
Maximum Landing 10,300 lbs
Max. Vertical T/O 9,500 lbs

NOTE:

Due to FS2004 limitations, A/C will be loaded with maximum (1600 lbs) fuel. The pilot should off-load required fuel for mission requirements.

By default, A/C loads with Captain, First Officer, Medic 1 & Medic 2 and Baggage weights. For realism, add Patient & stretcher (151 lbs) weight after scene arrival.

 [Go to Top]

2. DIMENSIONS  

Length 52' 7"
Width 9' 6"
Height 11' 10"
Main Rotor Diameter 44' 0"
Tail Rotor Diameter 8' 0"
Powerplant Allison 250-C30 Turboshaft (650 SHP)

 [Go to Top]

3.   SPEEDS & CEILINGS

Vne 155 KIAS
Vcruise 130-145 KIAS
Vmax range 115 KIAS
Vclimb 90 KIAS
V ifr approach 110 KIAS
Landing Approach (VFR) 35 KIAS @ 100ft AGL
   
Service Ceiling 15,00ft MSL
Hover Ceiling  
-In Ground Effect 5,650ft MSL
-Out of Ground Effect 1,800ft MSL
   
Max Rate of Climb 2,200ft / min
Vertical Max Climb 1,625ft / min

 [Go to Top]

4. RANGE  

Full, @ 610lb/hr 2.9 hrs
(1800 lbs) 395 NM (@140 KTAS)
Half, @ 610lb/hr 1.90 hrs
(800 lbs) 275 NM (@140 KTAS)
Full, @ 580lb/hr 3.25 hrs
  374 NM (@115 KTAS)

Fuel ranges do not include Taxi allowance (50-80 lbs), VFR or IFR reserves ( 300-450 lbs).

 [Go to Top]

5. TORQUE LIMITS  

Max Continuous 101.2%
Max 2 1/2 min 114.5%
Max T5 temperature (cont) 684 Deg. F
High Speed Cruise 95% (15 min. max)
One Engine Inop 155%
(no flight after until maint. inspection completed.)

 [Go to Top]

6. CREDITS & NOTES

[© November 2006, Nemeth Designs & Ed Easterbrook]

These checklists modified from Sikorsky S-76A Pilot's Operating Handbook. Intended for FS 2004 use only. Not intended for real-world flight operations. It is the pilot's responsability to aquaint themselves with all rotorcraft tendencies and operational limitations. The author assumes NO liability for any damages & injuries occured through inappropriate use of this information.

 [Go to Top]