Editing Bell UH-1 Iroquois (section)

==Specifications (UH-1H)==
[[File:Bell UH-1H Iroquois 3-view line drawing.png|thumb|Bell UH-1H Iroquois 3-view drawing]]

{{Aircraft specs
 |ref= ''Jane's All the World's Aircraft 1987-88''<ref>{{cite book |editor1-last= Taylor |editor1-first= John W. R. |title= Jane's All the World's Aircraft 1987-88 |date= 1987 |publisher= Jane's Publishing Company Limited |location= London |isbn= 0 7106-0850-0 |page= 365 |url= https://archive.org/details/janesallworldsai0000unse/page/365/mode/1up |access-date= 8 September 2021}}</ref>
 |prime units?= imp<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->
<!--   General characteristics
-->
 |crew= 1–4
 |capacity= {{convert|3,880|lb|kg}} including 11–14 troops, 6 stretchers and attendant, or equivalent cargo
 |length m=
 |length ft= 57
 |length in= 9+5/8
 |length note= with rotors
 |width m=
 |width ft= 9
 |width in= 6+1/2
 |width note= (over skids)
 |height m=
 |height ft= 14
 |height in= 5+1/2
 |height note= (tail rotor turning)
 |empty weight kg=
 |empty weight lb= 5,210
 |empty weight note=
 |gross weight kg=
 |gross weight lb= 9,039
 |gross weight note= (mission weight)
 |max takeoff weight kg=
 |max takeoff weight lb= 9,500
 |max takeoff weight note=
 |fuel capacity=
 |more general=
<!--   Powerplant
-->
 |eng1 number= 1
 |eng1 name= [[Lycoming T53|Lycoming T53-L-13]]
 |eng1 type= [[turboshaft]]
 |eng1 kw=<!-- prop engines -->
 |eng1 shp= 1,400
 |eng1 note= (limited to {{cvt|1100|shp}} by transmission)
 |power original=
 |thrust original=
 |more power=
 |rot number= 1
 |rot dia ft= 48
 |rot dia in= 0
 |rot area sqm=<!-- helicopters -->
 |rot area sqft= 1,809.56
 |rot area note=
<!--   Performance
-->
 |max speed kmh=
 |max speed mph= 127
 |max speed kts=
 |max speed note= (at maximum takeoff weight; also [[Vne]] at this weight)
 |cruise speed kmh=
 |cruise speed mph= 127
 |cruise speed kts=
 |cruise speed note= (at {{cvt|5700|ft}} at maximum takeoff weight)
 |range km= 511
 |range miles=
 |range nmi=
 |range note= (with maximum fuel, no reserves, at sea level)
 |combat range km=
 |combat range miles=
 |combat range nmi=
 |combat range note=
 |ferry range km=
 |ferry range miles=
 |ferry range nmi=
 |ferry range note=
 |endurance=<!-- if range unknown -->
 |ceiling m=
 |ceiling ft= 12,600
 |ceiling note=(at maximum takeoff weight)
 |g limits=<!-- aerobatic -->
 |roll rate=<!-- aerobatic -->
 |climb rate ms=
 |climb rate ftmin= 1,600
 |climb rate note= at sea level (at maximum takeoff weight)
 |time to altitude=
 |lift to drag=
 |wing loading kg/m2=
 |wing loading lb/sqft=
 |wing loading note=
 |disk loading kg/m2=
 |disk loading lb/sqft= 5.25
 |disk loading note=
 |fuel consumption kg/km=
 |fuel consumption lb/mi=
 |power/mass= {{cvt|0.1159|hp/lb}} <!-- note Jane's 1987-88 kg/kW value is inconsistent with its lb/shp value because the raw engine power value was used for the former -->
 |more performance=
<!--   Armament
-->
 |armament= various including:
* 7.62 mm machine guns
* {{convert|2.75|in|mm|abbr=on}} rocket pods
{{see also|U.S. helicopter armament subsystems}}
 |guns=
 |bombs=
 |rockets=
 |missiles=
 |hardpoints=
 |hardpoint capacity=
 |hardpoint rockets=
 |hardpoint missiles=
 |hardpoint bombs=
 |hardpoint other=
 |avionics=
}}