Aérospatiale N 262
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Original source: Own work Author MilborneOne [edit] Licensing I, the copyright holder of this work, hereby publish it under the following licenses: Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled GNU Free Documentation License. www.gnu.org/copyleft/fdl.htmlGFDLGNU Free Documentation Licensetruetrue
Author: MilborneOne [edit] Licensing I, the copyright holder of this work, hereby publish it under the following licenses: Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled GNU Free Documentation License. www.gnu.org/copyleft/fdl.htmlGFDLGNU Free Documentation Licensetruetrue

The Aérospatiale N 262 was a French twin-prop high-wing airliner built first by Nord Aviation.

* Aérospatiale N 262 & Mohawk 298 máy bay dân dụng tuabin cánh quạt tầm gần * Aerospatiale SA-330 Puma trực thăng hai động cơ nâng cỡ trung bình 1
L'application principale du moteur était Aérospatiale N 262 avion de ligne. Références - * Gunston, Bill (1986).2

Made by Aérospatiale.

The Aérospatiale N 262 was a French twin-prop high-wing airliner built first by Nord Aviation.3
More Users
Allegheny Airlines
French Navy
Height Main
6.21 m
Height Alt
619.76
Stall Speed Main
128.0
Length Alt
1927.86
Max Takeoff Weight Main
10300.0
Jet Or Prop
prop
Lists
* List of airliners
Range Main
1110.0
Max Speed Alt
14340.0
Type Of Prop
turboprops
Never Exceed Speed Alt
18540.0
Max Speed Main
385.0
Introduction
1964
Capacity
29
Airfoil
NACA 23016 at root
NACA 23012 at tip
Cruise Speed Main
360.0
Max Takeoff Weight Alt
22710.0
Ceiling Main
7
300 m
Number Built
110
Crew
2
Never Exceed Speed Main
498.0
Span Main
21.90 m
Cruise Speed Alt
13380.0
Area Main
55.0 m²
Primary user
Span Alt
2189.48
Plane Or Copter?
Power Alt
1065
Engine(prop)
Turbomeca
Turbomeca Bastan
Manufacturer
Number Of Props
2
First Flight
--05-20
--12-24
Production End Year
1976
Origin
France
National Origin
France
Climb Rate Main
6.3 m-s
Power Main
794.0
Production Start Year
1962
Stall Speed Alt
4740.0
Climb Rate Alt
1250.0
Length Main
19.28 m
Area Alt
592.0
Range Alt
41400.0
Similar Aircraft
* Fokker F27* ATR 42* Let L-410 Turbolet
Empty Weight Main
6654.0
Ceiling Alt
24000.0
Produced
1962
Empty Weight Alt
14669.0
Category

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