Rockwell Commander 111 / 112 / 114

Touring Aircraft

Rockwell Commander 114B © Karsten Palt
Photo ©: Karsten Palt
The Rockwell Commander 112 and Commander 114 are single-engine four-seat light touring aircraft with retractable landing gear produced by the US-American manufacturer North American Rockwell, later Rockwell International and later by Commander Aircraft Corporation.
The prototypes Commander 111 had a fixed landing gear.
Crew1
Passengers3
Propulsion1 Piston Engine
Engine ModelLycoming IO-360-C1D6
Engine Power149 kW200 hp
alternative Engine Variant
Engine ModelLycoming IO-540-T4B5D
Engine Power194 kW260 hp
Speed265 (274) km/h 143 (148) kts
165 (170) mph
Service Ceiling4.633 (5.304) m15.200 (17.400) ft
Range1.085 (1.356) km586 (732) NM
674 (842) mi.
Empty Weight804 (855) kg1.773 (1.885) lbs
max. Takeoff Weight1.270 (1.424) kg2.800 (3.140) lbs
Wing Span10,85 (9,98) m35 ft 7 in (32 ft 9 in)
Wing Area15,2 (14,1) m164 (152) ft
Length7,63 m25 ft 0 in
Height2,57 m8 ft 5 in
First Flight04.12.1970
Production Statusout of production
Total Production>1000
ICAO CodeAC11
IATA CodeACP
FAA TCDSA11SO, A12SO
Data for (Version)Rockwell Commander 112B (114)
VariantsCommander 111, 112, 112A, 112B, 112TC, 112TCA Alpine Commander, 114, 114A Grand Turismo, 114B, 114TC

[Photo-ID: 1794] Karsten Palt 2009-04-03
Rockwell Commander 114, , HB-NDE, c/n 14150, Karsten Palt, 2009Rockwell
Commander 114
Reg.: HB-NDE
c/n: 14150
 
[Friedrichshafen (EDNY / FDH)]
[Photo-ID: 795] Karsten Palt 2008-04-09
Rockwell Commander 114B, , D-EQCA, c/n 14565, Karsten Palt, 2008Rockwell
Commander 114B
Reg.: D-EQCA
c/n: 14565
 
[Wilhelmshaven-Mariensiel (EDWI / WVN)]