Sikorsky UH-60A Black Hawk

Aircraft Information

Category:
Turbine Military
Manufacturer:
Sikorsky
Condition:
Pre-Owned
Year:
2007
TTAF:
9045hrs.
Serial Number:
8223722
Registration:
N264P
Price:
Call For Price
Location:
Florida, United States

Seller Information

West Palm Beach, Florida, United States
Contact Name:
Russell Dise
(561) 242-4393
Contact This Seller
Sikorsky UH-60A Black Hawk
Sikorsky UH-60A Black Hawk
Sikorsky UH-60A Black Hawk
Sikorsky UH-60A Black Hawk
Sikorsky UH-60A Black Hawk
Sikorsky UH-60A Black Hawk
Aircraft Description: 

TTAF: 9045

Engine Information: 

Left: GE-E-307850
5043 HSN

Right: GE-E-306637
4238 HSN

Engine #1
HMU Replacement Due 30 Nov 18
Cold Section Module Repl in 880 Hours

Engine #2
Power Turbine Module Due in <90 Hours
Cold Section in < 423 Hours
Rotor/Stator in 946 Hours
Main Transmission: 727 Hours
Crossfeed Valve Due in Approx. 93 Hours
M/R Blade Cuff (Blade Repl; Cuff is not field replaceable)
Due in 286 Hours. (only one of them due for replacement)
Main Rotor Shaft Repl Due in 314 Hours.
T/R Pitch Change Shaft and Bearings Due in 397 Hours

Time to Next Major Inspection (i.e. next Phase 1 inspection)
PMI 1: 113.4 Hours. Out
PMI 2: 373.4 Hours. Out
PNs and/or Descriptions of any “After-market” Parts that have been Added to the a/c
Transponder (GTX-327) and TransCal Encoder (SSD120-30N)

Additional Information: 

Construction: Aluminum Monocoque Structure; Conventional, Non-retractable, Main Landing Gear and Tail-wheel Assemblies

Main Rotor: Articulated, Main Rotor Head Consisting of Titanium Hub, Elastomeric Bearings, Lead-lag Dampers, and Passive Vibration Absorbers; Ballistically Tolerant, Main Rotor Blades (4) Constructed from Titanium and Composite Materials

Tail Rotor: Tail Rotor Head Consisting of Flex Beams, and Elastomeric Bearings; Ballistically Tolerant, Tail Rotor Blades (4) Constructed from Titanium and Composite Materials

Main Gearbox: Transmission Consisting of Main Module (1), Input Modules (2), and Accessory Modules (2); Rated to 2,828 SHP

Engines: General Electric T700-GE-700 (2); Max. Continuous Power 1,318 SHP per Engine

Aux. Power Unit (APU): Honeywell GTCP36-150[BH]

Standard Fuel Capacity: 360 Gals / 1,363 l Total

Empty Weight: 22,000 Lbs. I 10,000 Kg
Max. Operating Weight: 15,976 - 16,803 Lbs. I 7,246 - 7,621 Kg
Max. Take-Off Weight: 22,000 Lbs. I 10,000 Kg
Cruise Speed: 139 - 145 Kts at 4,000 Ft and 95 F I 257 - 268 Kph
VNE Speed: 193 Kts
Vertical Rate of Climb: 390 - 1,000 Fpm I 119 - 305 Mpm
Service Ceiling: 19,000 Ft I 5,971 M
HIGE: 18,000 Ft MSL at 25 C at 18,000 Lbs.
HOGE: 18,000 Ft MSL at 25 C at 16,400 Lbs.
Range: 300 Nautical Miles with 30 Min. Reserve I 555 Km with 30 Min. Reserve
Endurance: >3 Hours