This document contains performance specifications for an aircraft including: 1) Maximum takeoff weight of 7905 lbs with a zero fuel weight of 6100 lbs and fuel weight of 1100 lbs. 2) Maximum allowable gross weights for various conditions ranging from 6851 lbs to 7905 lbs. 3) Fuel quantities including a maximum range of 281 nm and maximum endurance of 2.7 hours with 164.2 gallons of fuel. 4) Performance data for takeoff, landing, and cruise specifications including airspeeds, torque, and fuel flow.

1. A/C GWT: 6500 lbs 2948 kg PA: 3500 ft FAT: 30 C
A/C GWT: 7200 lbs 3265 kg PA max: ft FATmax: 14 C 92.7% AV 46.3% CT AV
Fuel Weight: 1100 lbs 499 kg PA @ T/O: ft FAT T/O: 8 C 7905 lbs 3585 kg
Zero Fuel Weight: 6100 lbs 2766 kg Max allowable GWT OGE: 7784 lbs 3530 kg
117.7% AV 58.8% CT AV 78.7% IGE 76.9% OGE
Max allowable GWT IGE: 7905 lbs 3585 kg 6851 lbs 3107 kg
Max allowable GWT OGE: 7905 lbs 3585 kg
73.0% IGE 73.0% OGE 126 ft AGL
7146 lbs 3241 kg Remarks:
Predicted Hover Torque @ 3 ft:
74 ft AGL
Remarks: bleed air: off skid hover height: 3 ft
OGE Hover TQ @ T/O:
Fuel on board @ cruise:* 2.2 hrs or 2 hrs 15 mins -------------
Fuel on board lbs to gls: 164.2 gls Prepared:
Max Range* 281.0 nm IFR reserve = 245 lbs VFR reserve = 163 lbs
Max Endurance* 2.7 hrs or 2 hrs 41 mins
* does not include any reserve
A/C GWT: 7150 lbs 3243 kg PA: ft FAT: 10 C Take Off 4404 6873 600
TQ Fuel Flow Zero Fuel 4424 5905 600
115.0 kts 118.4 kts 54.3% 490 lb/hr Landing 4394 6128 600
65.5 kts 67.4 kts 37.4% 409 lb/hr 2/27/15 trial start
121.8 kts 125.4 kts 59.7% 491 lb/hr 5/28/15 today
Trial Days Remaining: 0 of 90
MIN/MAX- S.E. IAS min kts max 110 kts © 2011 Robert Arthur Walters
DA FORM 5701-72E 5 Jan 2012 Previous editions obsolete page 1 of 2 DA FORM 5701-72E 5 Jan 2012 Previous editions obsolete page 2 of 2
64.6%
CG (mm)
Max Allowable GWT OGE w/ MCP:
H/V Altitude
GM (kg)
GM
(lbs)
2779
2000
SINGLE ENGINE
25.1
IAS
3117
2678
CRUISE
MAX ENDURANCE
MAX RANGE
TAS
H/V Altitude
71.4%
CRUISE
N/APredicted Hover Torque:
Go/No Go Torque:
Max Allowable GWT OGE w/ MCP:
ARRIVAL
AEO Dual Engine OEI Single Engine
92.7%Max Torque Available/Critical:
Max Hoist
Load (lbs)
N/A
61.1%
UH-72 Performance Planning Card
For use of this form, see TC 1-272 and Flight Manual; the proponent agency is TRADOC
DEPARTURE
0
Max Torque Available/Critical:
AEO OEI
100
117.7%
Max allowable GWT IGE:
Go/No Go Torque:
5/28/2015

2. HV Departure HV Arrival

3. 4000 lbf 5000 lbf 6000 lbf 7000 lbf 7904 lbf GW Actual
Max S.E. A/S Min S.E. A/S Cruise AEO <55 KIAS >=55 KIAS

4. Max TQ Departure Max TQ Arrival