EasyManua.ls Logo

Learjet 35 - Page 227

Learjet 35
482 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
Leerjet 35/36 Developed for Training Purposes 3-43
February 1998
Limitations
Dee Howard TR4000 Thrust Reversers
Maximum Demonstrated Crosswind Velocity . . . . . . . . 20 KTS
Minimum Airspeed with Full Reverse Thrust . . . . . . . . . 50 KTS
Maximum Fan Speed (N
1) in Reverse . . . . . . . . . . . . . . . . 75%
Deployment restricted to ground operation only.
Disarm reversers immediately after takeoff; leave disarmed
until final approach to landing.
Do not use the reversers to back up the aircraft.
Simultaneous use of reverse thrust and a drag chute (if
installed) is prohibited.
Thrust reversers are limited to ground operations on paved sur-
faces.
Engine starts with reversers deployed are prohibited.
Time limit in reverse thrust is 30 seconds for each deployment.
WARNING: When landing on snow-covered runways, apply
reverse thrust with caution because visibility may be
impaired.
CAUTION: Operation under OAT conditions below 20°F can
cause N
1 speeds in excess of 75% limit. Observe N1 when
operating thrust reversers in cold temperatures to ensure that
the 75% limit is not exceeded.

Table of Contents

Related product manuals