1982 SIKORSKY UH-60A For Sale in Palm Beach, Florida United States
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1982 Sikorsky Black Hawk UH-60A Empty Weight: 10,387 – 11,253 lbs. | 4,711 – 5,104 kg Max. Operating Weight: 15,976 – 16,803 lbs. | 7,246 – 7,621 kg Max. Take-Off Weight: 22,000 lbs. | 10,000 kg Cruise Speed: 139 – 145 kts at 4,000 ft and 95 F | 257 – 268 kph
1982 Sikorsky Black Hawk UH-60A Empty Weight: 10,387 – 11,253 lbs. | 4,711 – 5,104 kg Max. Operating Weight: 15,976 – 16,803 lbs. | 7,246 – 7,621 kg Max. Take-Off Weight: 22,000 lbs. | 10,000 kg Cruise Speed: 139 – 145 kts at 4,000 ft and 95 F | 257 – 268 kph
Details
- StatusFor Sale
- ConditionUsed
- Year1982
- MakeSIKORSKY
- ModelUH-60A
- Reg #N264P
- Serial #8223722
- Airframe9045 hrs
- LocationPalm Beach, Florida United States
- External URL
See attached Documents for complete details.
- ENGINE 1 / Serial# GE-E-307850 - 5,043 Hours
- ENGINE 2 / Serial# GE-E-306637 - 4,238 Hours
- APU Manufacturer: Model: Honeywell GTCP36-150 [BH]
- 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
- Total hours on other major components ? 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) ? Restricted Type Certificate
- ? See Type Certificate Data Sheet
1982_Sikorsky_Black_Hawk_UH-60A.pdf 