Lockheed 300-50A-01
Model overview
Fleet & certification
- Origin
- United States
Certifying authorities
FAA
Variants
Per-variant specifications
| Variant | Engine | MTOW | Range | Cruise | Pax |
|---|---|---|---|---|---|
| 300-50A-01 300-50A-01 | — | — | — | — | — |
Type certification
The FAA paperwork
TCDS A2SO · Rev 4 · issued 2001-10-25
- Category
- Cargo transport aircraft
- MTOW
- 143,657 kg
- MZFW
- 92,856 kg
- Seats
- 3 crew · 79 passengers
- Fuel
- 89,304 L
- Ceiling
- 40,000 ft
Approved fuelJP-4JP-5
Engine
4 Pratt and Whitney turbofan TF33-P-7 with anti-icing regulator assembly, P/N 476015GI, and heated PT2 probes
Certification basis
CAR 1 dated October 1, 1955, including Amendments through 1-4 effective December 31, 1960. CAR 4b dated December 31, 1953, including Amendments through 4b-11 effective October 1, 1…
Safety & ops history
Where to look next
Detailed safety & ops history coming soon — view this model's FAA Airworthiness Directives at FAA.gov.
This aircraft
Tools
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