5-13
VELIS Electro
Pilot's Operating Handbook
POH
-
128
-
00
-
40
-
001
PAGE REV. 0
PAGE
SECTION
5
PERFORMANCE DATA
APPROVED
5.9 ENDURANCE AND RANGE
CAUTION:
The available battery energy is a function of SOC and SOH.
Both parameters must be considered for a correct endurance estimation.
Reduction of SOH (usually due to aging/use) reduces the batteries' energy
storage capability and, therefore, also endurance.
CAUTION:
Always consider that battery temperature >40 °C at take o
ff
may
a
ff
ect the duration of flight, as the mission must be aborted when the in-flight
battery temperature exceeds the caution threshold (50 °C).
The following tables present expected endurance for local flights (A-A flight)
and endurance/range for cross country flights (A-B flight). VFR reserve is
di
ff
erent for the two situations, 10 min or 30 min, in accordance with Ops.125.
Endurance and range
typical flight profile
Summary of Contents for VELIS Electro
Page 9: ...SECTION 1...
Page 21: ...SECTION 2...
Page 36: ...This page is intentionally left blank...
Page 37: ...SECTION 3...
Page 40: ...This page is intentionally left blank...
Page 86: ...This page is intentionally left blank...
Page 108: ...This page is intentionally left blank...
Page 109: ...SECTION 4...
Page 126: ...This page is intentionally left blank...
Page 128: ...This page is intentionally left blank...
Page 140: ...This page is intentionally left blank...
Page 141: ...SECTION 5...
Page 167: ...SECTION 6...
Page 172: ...This page is intentionally left blank...
Page 173: ...SECTION 7...
Page 176: ...This page is intentionally left blank...
Page 209: ...SECTION 8...
Page 225: ...SECTION 9...
Page 227: ...APPENDIX 9 A1...