Learjet
Learjet 24A
The Learjet 24A is an early certification variant of the original Model 24. It preserves the early Learjet layout of two rear-mounted engines, a narrow executive cabin and wingtip fuel tanks, making it a distinct historical model within the wider Learjet family.
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Aircraft profile
Development and lineage
- Manufacturer
- Learjet
- Family
- Learjet 24A
- Aircraft category
- Business aircraft
- Propulsion
- Jet
Aircraft data
Key specifications
- PAX
- 6
- Crew
- 2
- Range
- 880 nm
- Max operating speed
- 300 KIAS
- Max ceiling
- 41,000 ft
- Engines
- 2
- Engine model
- General Electric CJ610-4
- Thrust per engine
- 2,850 lbf
- MTOW
- 12,499 lbs
- Cabin height
- 52 in
- Cabin width
- 57 in
- Cabin length
- 108 in
- Cabin volume
- 170 cu ft
- Baggage volume
- 40 cu ft
- Overall length
- 43.3 ft
- Wingspan
- 35.6 ft
Overview
Program history
The 24A belongs to the first Model 24 approval group, before the later B through F developments. The aircraft retained the compact business-travel role of the original Learjet, with individual equipment and approved weight configuration distinguishing specific examples. For an individual aircraft, engine installation, operating limitations and modifications must be matched to its approved flight manual.