DHC-6-200HG 12,500 lbs (5670 KG) MTOW

DHC-6-200HG ™ 12,500 LBS (5670 KG) MTOW

APPLICABILITY De Havilland DHC-6-100/-200 Twin Otter Airplanes AUTHORIZATIONS United States FAA STC No. SA02252LA

Canada STC No. SA09-94 EASA STC. No. 10051900 DESCRIPTION

MINIMUM REQUIREMENTS • PWC PT6A-27/-34 engines • Hartzell HC-B3TN-3D propellers • Structural components with time/cycles not exceeding the requirements for a DHC-6-300 airplane in accordance with DHC PSM 1-6-11, Rev. 6 • DHC modification status and implementation as required NOTE: DHC-6-100 aircraft can be converted to DHC-6-200 and be eligible for the DHC-6-200HG ™ STC. Inquire about applicability. OPERATING REQUIREMENTS • Airplane Flight Manual Supplement, Document No. HG-62-1A • Weight and Balance Supplement, Document No. HG-62-8 MAINTENANCE/INSPECTION REQUIREMENTS • Instructions for Continued Airworthiness, Document No. HG-62-1 • Maintenance Manual Supplement, Document No. HG-62-2

Provides increased capabilities for a DHC-6-200 series Twin Otter with PT6A-27/-34 powerplants approved for operation at 620 Shaft HP with Hartzell HC-B3TN-3D three bladed propellers. Maximum Takeoff Weight (MTOW) is increased from 11,579 (5252 Kg) pounds to 12,500 pounds (5670 Kg). Effectively upgrades a DHC-6-200 with DHC-6-300 characteristics. • Increase MTOW/Payload by 921 pounds (11,579 + 921=12,500 lbs.) • Increase profitability • DHC-6-300 performance with 620 SHP • Empty weights of typical DHC-6-200HG ™ aircraft are a proximately 300-400 pounds lighter than similarly equipped DHC-6-300 series aircraft

Information subject to change without notice

AEVEX.com

AEVEX Aerospace | 37260 Sky Canyon Dr., Hangar 20, Murrieta, California 92563 | T: 951-600-0009 | E-mail: aircraftservices@AEVEX.com

Page 1

Made with FlippingBook - Share PDF online