Rockwell Commander 111 / 112 / 114
Touring Aircraft
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.
| Crew | 1 | |
| Passengers | 3 | |
| Propulsion | 1 Piston Engine | |
| Engine Model | Lycoming IO-360-C1D6 | |
| Engine Power | 149 kW | 200 hp |
| alternative Engine Variant | ||
| Engine Model | Lycoming IO-540-T4B5D | |
| Engine Power | 194 kW | 260 hp |
| Speed | 265 (274) km/h | 143 (148) kts 165 (170) mph |
| Service Ceiling | 4.633 (5.304) m | 15.200 (17.400) ft |
| Range | 1.085 (1.356) km | 586 (732) NM 674 (842) mi. |
| Empty Weight | 804 (855) kg | 1.773 (1.885) lbs |
| max. Takeoff Weight | 1.270 (1.424) kg | 2.800 (3.140) lbs |
| Wing Span | 10,85 (9,98) m | 35 ft 7 in (32 ft 9 in) |
| Wing Area | 15,2 (14,1) m² | 164 (152) ft² |
| Length | 7,63 m | 25 ft 0 in |
| Height | 2,57 m | 8 ft 5 in |
| First Flight | 04.12.1970 | |
| Production Status | out of production | |
| Total Production | >1000 | |
| ICAO Code | AC11 | |
| IATA Code | ACP | |
| FAA TCDS | A11SO, A12SO | |
| Data for (Version) | Rockwell Commander 112B (114) | |
| Variants | Commander 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 Reg.: HB-NDE c/n: 14150 |
| [Friedrichshafen (EDNY / FDH)] | |
| [Photo-ID: 795] © Karsten Palt 2008-04-09 | |
 | Rockwell Commander 114B Reg.: D-EQCA c/n: 14565 |
| [Wilhelmshaven-Mariensiel (EDWI / WVN)] | |