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