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Sikorsky MH-53M Pave Low IV

1998 · Three-engine heavy turbine helicopter

Factory at US Stratford

History News
USAF MH-53J upgraded by the Pave Low IV program. Introduced in 1998, aircraft received the IDAS/MATT (Interactive Defensive Avionics System/Multi-Mission Advanced Tactical Terminal) which provide real-time access to the total battlefield situation. A color, multifunctional, night-vision compatible digital map screen is the most visible hardware in the system. Located on the helicopter instrument panel, the display gives an MH-53 crew a clearer situation awareness. They were retired in 2008.

Specifications

Engine2 x General Electric T64-GE-100 4330 shp
Capacity6 + 37
Length (m)28
Height (m)7.6
Blades6
Rotor diam. (m)21.9
Disc area (m2)216
Weight (kgs)Empty: 14500 Max: 21000
Speed (km/h)Cruise: 278 Max: 315
Range (km)1100
Ceiling (m)4900
blueprints MH-53M Pave Low IV

Airframes (26)

C/NModelBuiltReg
65-142hh-53cUS 67-14993w/o 2003
65-143hh-53cUS 67-14994
65-144hh-53cUS 67-14995
65-147hh-53cUS 68-8284
65-149hh-53cUS 68-8286w/o 2002
65-199hh-53cUS 68-10369
65-253ch-53cUS 68-10924
65-257ch-53cUS 68-10928
65-259ch-53cUS 68-10930
65-263hh-53cUS 69-5784
65-264hh-53cUS 69-5785
65-269hh-53cUS 69-5790
65-270hh-53cUS 69-5791w/o 2001
65-272hh-53cUS 69-5793
65-273hh-53cUS 69-5794w/o 2007
65-274hh-53cUS 69-5795
65-275hh-53cUS 69-5796
65-276hh-53cUS 69-5797w/o 2004
65-335ch-53cUS 70-1625w/o 2003
65-336ch-53cUS 70-1626
65-339ch-53cUS 70-1629
65-340ch-53cUS 70-1630
65-341ch-53cUS 70-1631
65-387hh-53c1974US 73-1649
65-388hh-53c1974US 73-1650w/o 1984
65-390hh-53c1974US 73-1652

Operators

1968-2008 US US Air Force S-65 H-53