When the mission is critical, and the performance of your aircraft is on the line, the DA Form 5701-228-R, or the OH-58A/C and TH-67 Performance Planning Card, becomes an indispensable tool. Designed under the guidance of TC 3-04.43 and backed by TRADOC, this form serves as a comprehensive planning card that meticulously outlines every aspect necessary for flight preparation and performance evaluation. Covering hover data including gross weight, fuel specifics, torque availability, and safe pedal margin, to cruise and arrival intricacies such as altitude, speed, and fuel management, each section of the form is meticulously crafted to ensure pilots have accurate and immediate access to crucial information. On top of performance insights, it provides a detailed look into weight and balance departure data, thereby ensuring every flight operates within safe and efficient parameters. Whether it’s managing the operational weight or calculating the center of gravity (CG) for both departure and arrival, this form is tailored to foster a culture of precision and safety. With the inclusion of hover in-ground effect (IGE) and out-of-ground effect (OGE) torque metrics, alongside maximum allowable gross weight and pedal margin safety checks, the DA Form 5701-228-R equips crews with the knowledge needed to make informed decisions for a wide array of flight conditions. Through its detailed sections, this form not only guides in performance planning but also stands as a critical component in the pursuit of aviation excellence.
Question | Answer |
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Form Name | Da Form 5701 228 R |
Form Length | 2 pages |
Fillable? | No |
Fillable fields | 0 |
Avg. time to fill out | 30 sec |
Other names | a5701_228_r da form 5701 228r |
For use of this form, see TC
HOVER DATA
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AIRCRAFT GWT |
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FUEL |
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lbs |
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lbs/gal |
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PA CUR |
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PA MAX |
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FAT CUR |
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FAT MAX |
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LOAD AVAIL CUR PA/FAT |
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IGE |
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OGE |
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LOAD AVAIL MAX PA/FAT |
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IGE |
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OGE |
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MAX TORQUE AVAIL (CURR/MAX) |
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CONT TORQUE AVAIL (CURR/MAX) |
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HOVER IGE TORQUE (CURR/MAX) |
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HOVER OGE TORQUE (CURR/MAX) |
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MAX ALLOW GWT IGE (CURR/MAX) |
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MAX ALLOW GWT OGE (CURR/MAX) |
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SAFE PEDAL MARGIN |
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YES |
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NO |
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CRUISE DATA |
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ALT |
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FAT (C) |
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GWT |
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VNE |
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IAS |
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IAS |
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TAS |
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FUEL |
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TORQUE |
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MAX R/C/ENDURANCE |
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IAS |
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FUEL |
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TORQUE |
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MAX RANGE |
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IAS |
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FUEL |
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TORQUE |
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FUEL MANAGEMENT |
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START(TIME lbs/gal) |
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STOP (TIME lbs/gal) |
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RESERVE (TIME) |
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FUEL FLOW |
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BURNOUT (TIME) |
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BINGO/RESERVE |
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PPH/GPH lbs/gal
ARRIVAL DATA
PA MAX FAT MAX LANDING GWT
MAX TORQUE AVAIL (MAX)
CONT TORQUE AVAIL (MAX)
HOVER IGE TORQUE (MAX)
HOVER OGE TORQUE (MAX)
MAX ALLOWABLE GWT IGE (MAX)
MAX ALLOWABLE GWT OGE (MAX)
REMARKS
DA FORM |
PREVIOUS EDITIONS ARE OBSOLETE |
Page 1 of 2 |
APD LF v1.00
WEIGHT AND BALANCE
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DEPARTURE DATA |
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WEIGHT |
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BASIC WEIGHT (OIL INCLUDED): |
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CREW AND FLIGHT EQUIPMENT FORWARD (F.S. 65): |
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OPERATION WEIGHT: |
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CREW/PAX/CARGO AFT (F.S. 104): |
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BAGGAGE/CARGO (F.S. 148): |
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ZERO FUEL WEIGHT: |
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TAKEOFF FUEL GALLONS/POUNDS: |
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EXTERNAL LOAD: |
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DEPARTURE GROSS WEIGHT: |
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DEPARTURE CG: |
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ALLOWABLE CG RANGE |
VMC: |
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LANDING DATA |
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WEIGHT |
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OPERATING WEIGHT: |
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ARRIVAL FUEL GALLONS/POUNDS: |
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CREW/PAX/CARGO AFT (F.S. 104): |
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BAGGAGE/CARGO (F.S. 148): |
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EXTERNAL LOAD: |
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ARRIVAL GROSS WEIGHT: |
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ARRIVAL CG: |
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ALLOWABLE CG RANGE |
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REMARKS |
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DA FORM |
Page 2 of 2 |
APD LF v1.00