Technical Specifications
C212-200 Technical Specifications.
| Spec | Value |
|---|---|
| Engines | 2 × Garrett TPE331-10R-513C |
| Power | 900 SHP each (925 SHP with APR) |
| Propellers | 4-blade Dowty Rotol constant-speed, feathering & reverse |
| Maximum Takeoff Weight | 7,700 kg (16,975 lb) |
| Seating | Up to 26 passengers or military transport configuration |
Limitations
Weight Limitations
| Parameter | Limit | Remarks |
|---|---|---|
| Maximum Ramp Weight | 7,700 kg (16,976 lb) | |
| Maximum Takeoff Weight | 7,650 kg (16,865 lb) | |
| Maximum Landing Weight | 7,400 kg (16,314 lb) | |
| Maximum Zero Fuel Weight | 7,100 kg (15,653 lb) | |
| Minimum Flight Weight | 4,300 kg (9,481 lb) |
Powerplant Limitations
| Parameter | Limit | Remarks |
|---|---|---|
| Takeoff Power | 900 SHP / 100% RPM | 5 minutes max |
| Maximum Continuous Power | 900 SHP / 100% RPM | 925 SHP with APR Activated |
| Maximum Indicated EGT | 650°C | SRL system ON |
| Maximum Torque | 100% TQ continuous | |
| Starting EGT limit | 770°C | 1 second max |
Airspeed Limitations
| Parameter | Limit | Remarks |
|---|---|---|
| Maximum Operating Speed (VMO) | 200 KIAS | |
| Maximum Maneuvering Speed (VA) | 146 KIAS | |
| Maximum Flap Extended Speed (25%) | 135 KIAS | |
| Maximum Flap Extended Speed (100% / DOWN) | 115 KIAS | |
| Minimum Control Speed, Air (VMCA) | 76 KIAS | |
| Minimum Control Speed, Ground (VMCG) | 69 KIAS |