Beechcraft King Air C90

TCDS: A24CE Max Weight: 9,650 lbs

Beechcraft Corporation

Certification
Normal

Aircraft Overview

Official TCDS specifications for Beechcraft King Air C90 per Type Certificate A24CE

⚖️ Weight and Balance Specifications

Critical weight and balance data per Type Certificate A24CE. Verify against current aircraft records before flight operations.

Weight Limits

Max Takeoff
9,650 lbs
Max Landing
9,350 lbs
Typical Empty
6,145 lbs
Max Baggage
375 lbs
Useful Load
3,505 lbs

Loading Stations & Arms

Station Arm Description
Fuel Tanks 288.0 in Main fuel tanks (standard configuration)
Baggage Area 378.0 in Primary baggage compartment
Aft Passenger 340.0 in Standard loading position
Fwd Passenger 309.0 in Standard loading position
Pilot Copilot 278.0 in Standard loading position

Center of Gravity Envelope

CG must remain within these limits throughout all phases of flight.

📊 aft limit Category
📊 forward limit Category
🔧 Engine Specifications
Engine Model
Pratt & Whitney PT6A-21 (2x)
Power Output
550 HP
Fuel Type
Jet A
Oil Capacity
7 qt
📋 Key Specifications
TCDS Number A24CE
Max Weight 9,650 lbs
Engine Pratt & Whitney PT6A-21 (2x)
Power 550 HP
Category Normal
🏁 Speed Limits
VNE (Never Exceed) 340 KIAS
VNO (Normal) 266 KIAS
VFE (Flaps) 195 KIAS
VS (Stall Clean) 96 KIAS
VS0 (Stall Landing) 84 KIAS
📈 Performance Notes

The King Air C90 delivers turboprop performance with 245 KTAS cruise speed, pressurized cabin, and exceptional reliability in business aviation.

⚠️ Important Disclaimers

Verification Required

Always verify against current aircraft records and equipment list before flight operations.

TCDS Reference

This summarizes TCDS A24CE but does not replace the official document.

Regulatory Compliance

Calculations must comply with 14 CFR Part 23 and applicable airworthiness directives.

Data Accuracy

Specifications may vary by serial number and modifications. Verify with aircraft documentation.