III-8
February 2008
Legacy
III-9
February 2008
Legacy
LANDING GEAR
Your Lancair gear is held up by hydraulic pressure. Pressure switches shut off the
electrical power to the pump in both the up and the down positions. If the gear will
not remain retracted it may be discernable by loss of cruise speed and/or additional
wind noise. Proper actions are:
Airspeed, reduce to .............................
90 KIAS
Gear Circuit Breaker............................
PULL
Gear Switch .........................................
DOWN
Gear DumpValve .................................
OPEN
Gear......................................................
3-LIGHTS
Gear Dump Value ................................
CLOSED
It may be necessary to slip the aircraft allowing airloads to help push gear to full
down. An observer (tower or aircraft) can be used to confirm its full down posi-
tion.
WARNING
Aircraft observers must be used with caution as not
all pilots have the training to safely fly “formation”
and may not be sufficiently familiar with the Lancair
gear to confirm its down and locked configuration.
Once lowered it is not advisable to attempt a retraction prior to landing and deter-
mining the cause of its failure to remain fully up.
UNLATCHED CANOPY IN FLIGHT
The Canopy must not be opened in flight. Doing so may cause it to separate from
the aircraft possibly injuring the occupants in the process.
Should a latch become disengaged from the locked position, slow the aircraft to
approximately 85 kts and attempt to relock. If unable to lock, land as soon as
practical.
Summary of Contents for Legacy
Page 6: ...Legacy ...
Page 8: ...I 2 February 2008 Legacy Intentionally Left Blank ...
Page 20: ...I 14 February 2008 Legacy NOTES ...
Page 21: ...I 15 February 2008 Legacy NOTES ...
Page 22: ...I 16 February 2008 Legacy NOTES ...
Page 24: ...II 2 February 2008 Legacy Intentionally Left Blank ...
Page 34: ...II 12 February 2008 Legacy NOTES ...
Page 35: ...II 13 February 2008 Legacy NOTES ...
Page 36: ...II 14 February 2008 Legacy NOTES ...
Page 38: ...III 2 February 2008 Legacy Intentionally Left Blank ...
Page 47: ...III 11 February 2008 Legacy NOTES ...
Page 48: ...III 12 February 2008 Legacy NOTES ...
Page 50: ...IV 2 February 2008 Legacy Intentionally Left Blank ...
Page 69: ...IV 21 February 2008 Legacy NOTES ...
Page 70: ...IV 22 February 2008 Legacy NOTES ...
Page 72: ...V 2 February 2008 Legacy Intentionally Left Blank ...
Page 90: ...V 20 February 2008 Legacy NOTES ...
Page 91: ...V 21 February 2008 Legacy NOTES ...
Page 92: ...V 22 February 2008 Legacy NOTES ...
Page 94: ...VI 2 February 2008 Legacy Intentionally Left Blank ...
Page 108: ...VI 16 February 2008 Legacy NOTES ...
Page 110: ...VII 2 February 2008 Legacy Intentionally Left Blank ...
Page 134: ...VII 26 February 2008 Legacy NOTES ...
Page 135: ...VII 27 February 2008 Legacy NOTES ...
Page 136: ...VII 28 February 2008 Legacy NOTES ...
Page 138: ...VIII 2 February 2008 Legacy Intentionally Left Blank ...
Page 158: ...VIII 22 February 2008 Legacy NOTES ...
Page 160: ...IX 2 February 2008 Legacy Intentionally Left Blank ...
Page 168: ...IX 10 February 2008 Legacy Emergency Procedures ...
Page 169: ...IX 11 February 2008 Legacy Emergency Procedures ...
Page 170: ...IX 12 February 2008 Legacy Emergency Procedures ...
Page 171: ...IX 13 February 2008 Legacy Emergency Procedures Continued ...
Page 172: ...IX 14 February 2008 Legacy Normal Procedures ...
Page 173: ...IX 15 February 2008 Legacy Normal Procedures Continued ...
Page 174: ...IX 16 February 2008 Legacy Performance System Description ...
Page 176: ...IX 18 February 2008 Legacy NOTES ...
Page 178: ...X 2 February 2008 Legacy Intentionally Left Blank ...