1982 SIKORSKY UH-60A For Sale in Palm Beach, Florida United States

      owner says "sell my blackhawk"
      For Sale$3,250,000
      Posted by JetLease Palm Beach Updated 4/8/2021

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      For Sale$3,250,000

      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

      Posted by JetLease Palm Beach Updated 4/8/2021

      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

      • Status
        For Sale
      • Condition
        Used
      • Year
        1982
      • Make
        SIKORSKY
      • Model
        UH-60A
      • Reg #
        N264P
      • Serial #
        8223722
      • Airframe
        9045 hrs
      • Location
        Palm 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
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      Seller Information

      Seller Logo
      Name: Russ Dise
      Company: Jetlease
      Address: 1515 Perimeter Road
       T-101
       Palm Beach, FL 33406
       United States
      Website: www.jetlease.com

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