The Lockheed Electra 10-E 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-E
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-E Electra 10-E | — | 4,700 kg | 950 nm | 169 kt | 10 |
Type certification
The FAA paperwork
TCDS TC 590
- MTOW
- 4,763 kg
- Fuel
- 948 L
- Ceiling
- 10,500 ft
Engine
2 P&W Wasps S3H1
Certification basis
Type Certificate No. 590 (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-E — frequently asked
What is the range of the Lockheed Electra 10-E?
The Lockheed Electra 10-E has a maximum range of 950 nautical miles across variants.
How many people can the Lockheed Electra 10-E carry?
The Lockheed Electra 10-E seats up to 10 across its variants.
What is the MTOW of the Lockheed Electra 10-E?
The Lockheed Electra 10-E's maximum take-off weight is 4,700 kg.
How many Lockheed Electra 10-E aircraft are registered worldwide?
Sprinkle tracks 2 registered Lockheed Electra 10-E airframes worldwide.
Registered Electra 10-E aircraft
Individual Electra 10-E airframes by tail number — registration history, operator and lineage.