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/A Predicted 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