Leerjet 35/36 Developed for Training Purposes 3-45
February 1998
Limitations
AFM Supplement Limitations
The following items originate in selected AFM supplements.
For the supplements applicable to a specific aircraft, refer to
the Supplements section in the AFM for that aircraft.
Pointer Emergency Locator Transmitter (ELT)
Model 3000-1 with 3004-1 HV Dual Antenna Array: As plac-
arded, operation of the ELT system in the RESET position is
not to exceed five (5) seconds.
Landing Gear Tire Substitution
When 10-ply tires are substituted for 12-ply tires on the main
landing gear, refer to Figure 3-5 (page 3-47) for takeoff weight
limits. In no case is takeoff weight to exceed that as listed in
AFM Section I.
Electrically Heated Windshield
350-Knot (ECR 2498)
V
MO, Maximum Operating Speed . . . . . . . . . . . . . . . 350 KIAS
. . . . . . . . . . . . . . . . . . . .(Figure 3-6, page 3-49)
Information shown in italics is not included in the AFM Limitations chapter.
To Next Page
Loading...
