The Lockheed Electra 10-A is an aircraft of United States origin. It has a maximum take-off weight of 4,700 kg. It offers a maximum range of 950 nm, a cruise speed of 169 knots, a service ceiling of 20,000 ft and seating for up to 10 across its variants.
Lockheed Electra 10-A
Model overview
Fleet & certification
- Built
- 2
- Active
- 2
- Origin
- United States
Certifying authorities
FAA
Variants
Per-variant specifications
| Variant | Engine | MTOW | Range | Cruise | Pax |
|---|---|---|---|---|---|
| Electra 10-A (Army UC-36A; Navy R-20; and XR-20-1) Electra 10-A (Army UC-36A; Navy R-20; and XR-20-1) | — | 4,700 kg | 950 nm | 169 kt | 10 |
Type certification
The FAA paperwork
TCDS TC 551 · issued 1951-01-31
- MTOW
- 4,763 kg
- OEW
- 4,763 kg
- Seats
- 10 passengers
- Fuel
- 735 L
- Ceiling
- 8,600 ft
Approved fuel87 minimum octane fuel80 minimum octane fuel
Engine
2 Pratt & Whitney Wasp Jr. SB
Certification basis
Type Certificate No. 551 (Aero. Bulletin 7A requirements)
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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Electra 10-A — frequently asked
What is the range of the Lockheed Electra 10-A?
The Lockheed Electra 10-A has a maximum range of 950 nautical miles across variants.
How many people can the Lockheed Electra 10-A carry?
The Lockheed Electra 10-A seats up to 10 across its variants.
What is the MTOW of the Lockheed Electra 10-A?
The Lockheed Electra 10-A's maximum take-off weight is 4,700 kg.
How many Lockheed Electra 10-A aircraft are registered worldwide?
Sprinkle tracks 2 registered Lockheed Electra 10-A airframes worldwide.
Registered Electra 10-A aircraft
Individual Electra 10-A airframes by tail number — registration history, operator and lineage.