CAE SimuFlite Citation Bravo, Pilot Training Manual, Page: 128 / 718

CAE SimuFlite
3B-20
Developed for Training Purposes
Citation Bravo
March 2009
The nose wheel must be firmly on the ground before actuation of the
thrust reversers to reduce the possiblity of pitch-up and lift-off; and
to improve directional control steering. Do not exceed
approximately 15 lbs of force on the thrust reverser levers during
deployment because the throttle lock-out cams could jam.
Reverser Indicator Lights . . . . “6 LIGHTS”/ILLUMINATED
The ARM, UNLOCK, and DEPLOY lights should illuminate.
Reverser Power. . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
Do not exceed 76.6% N
1
when OAT is below -18°C or 86% N
1
at or
above -18°C. Once the thrust reversers are deployed, move the
levers aft to a maximum reverser thrust. "Stops" on the levers
provide 80.1% N
1
on a -18°C day at sea level so the pilot can keep
his attention on the landing rollout. The factory setting results in
lower than 80.1% N
1
at warmer temperatures and may be reset for
higher N
1
if temperatures are predominantly warmer. Do not exceed
80.1% N
1
.
At 60 KIAS:
Thrust Reverser Levers . . . . . . . . . . . . . . . . . IDLE REVERSE
With the thrust reverser levers in the IDLE REVERSE detent, the
reversers are left deployed for aerodynamic drag. Thrust reversing
and braking should commence according to runway length. With
excess runway, braking normally is begun after thrust reverser
deceleration is below 60 knots.
Do not use the thrust reversers for touch and go landings; a full stop
landing must be made once the reversers are selected.
Use caution on runways with small loose grit because it may be
ingested in the engine at idle reverse at low taxi speed.
Landing (Without Use of Thrust Reversers)
Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
Eight seconds after touchdown, the engines spool down from flight
idle (approximately 49% N
2
) to ground idle (45% N
2
) if the flight
idle switch is in the NORM position. The GROUND IDLE
annunciator illuminates.
Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY
To obtain maximum braking performance from the antiskid system,
apply continuous maximum effort (no modulation or “pumping”) to
brake pedals.
Speedbrakes . . . . . . . . . . . . . . . . . EXTEND (after touchdown)
CAUTION:
If during, a hard
brake pedal - no breaking condi-
tion is encountered, operate the
emergency brake system. Mainte-
nance is required before next
flight.
CAUTION: If
during landing, a
hard brake pedal-no braking condi-
tion is encountered, operate the
emergency brake system. Mainte-
nance is required before next
flight.