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The North American A-36A is an aircraft of United States origin. It has a maximum take-off weight of 5,000 kg. It offers a maximum range of 700 nm, a cruise speed of 250 knots, a service ceiling of 46,000 ft and seating for up to 1 across its variants.

North American A-36A

North American A-36A
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Photo via Wikipedia: North American A-36
Year
—
Owner
—
Last seen
—
MTOW
5,000 kg
Range
700 nm
Seats
1
A-36A
North American · A-36A
Model overview

Fleet & certification

Built
2
Active
2
Origin
United States
Certifying authorities
FAA
Market

Comparable listings

N257DB · 1952 · 6,875 hrs
$219,000
VH-NAG · 1942 · 4,004 hrs
$255,000
N25KP · 1951 · 13,030 hrs
$257,500
N584M · 8,628 hrs
$259,000
Variants

Per-variant specifications

VariantEngineMTOWRangeCruisePax
A-36A
A-36A
—5,000 kg700 nm250 kt1
Type certification

The FAA paperwork

TCDS LTC-15 · Rev 2

The FAA-issued Type Certificate for this model is on file (TCDS LTC-15), but we haven't yet extracted the structured spec values.

Read the TCDS (PDF) →
Safety & ops history

Where to look next

Detailed safety & ops history coming soon — view this model's FAA Airworthiness Directives at FAA.gov.
A-36A — frequently asked
What is the range of the North American A-36A?

The North American A-36A has a maximum range of 700 nautical miles across variants.

How many people can the North American A-36A carry?

The North American A-36A seats up to 1 across its variants.

What is the MTOW of the North American A-36A?

The North American A-36A's maximum take-off weight is 5,000 kg.

How many North American A-36A aircraft are registered worldwide?

Sprinkle tracks 2 registered North American A-36A airframes worldwide.

Registered A-36A aircraft

Individual A-36A airframes by tail number — registration history, operator and lineage.