Learjet 60 User Manual

PILOT'S MANUAL
Learjet
60
This Pilot's Manual provides information
supplemental
to
the Learjet 60 FAA Approved
Airplane Flight Manual . In
the event
any information herein conflicts with informa-
tion in the FAA Approved Airplane Flight Manual, the
FAA Approved Airplane Flight Manual shall take prece-
dence .
Learjet
PM -123

July 1993

Learjet 60 Specifications

General

Manufacturer	Bombardier Aerospace
Crew	2
Max Takeoff Weight	23, 500 lb (10, 659 kg)
Engines	2 × Pratt & Whitney Canada PW305A turbofans
Thrust per engine	4, 600 lbf (20.5 kN)
Service Ceiling	51, 000 ft (15, 545 m)
Rate of Climb	4, 500 ft/min (22.9 m/s)
Length	58 ft 8 in (17.88 m)
Maximum Speed	848 km/h
Cruise Speed	747 km/h
Range	4, 454 km