Description
AIRCRAFT MAINTENANCE MANUAL SUPPLEMENT
FOR
CONTINUED AIRWORTHINESS
OF THE
DE HAVILLAND MODEL DHC-2 MK I BEAVER
MODIFIED WITH
WIPAIRE STCSA01186CH
TURBINE ENGINE POWERPLANT
has 62 pages
TABLE OF CONTENTS:
I. LOG OF REVISIONS
II. INTRODUCTION
III. DESCRIPTION OF AIRFRAME MODIFICIATIONS – Figure 1
Figure 2-5 – Fuel System
Figure 6 – Heater Installation (Optional)
Figure 7,8 – Fuselage and Wing Reinforcements
Figure 9 – Horizontal Tailplace Modification
Figure 10 – Finlet and Strake Installation
Figure 11 – Engine Installation
Figure 12 – Battery Box Installation
Figure 13 – Cowling Installation
Figure 14 – Oil Cooler Installation
Figure 15 – Oil Cooler Duct Installation
Figure 16-18 – Wing Installation
Figure 19 – Airspeed Warning System
Figure 20 – Aileron Balancing Weights and Data
Figure 21 – Firewall Installation
Figure 22-23 – Rudder/Aileron Interconnect and Elevator Down Spring Inst
Figure 24 – Flap Limiter Spacer Installation
Figure 25 – Auxiliary Rudder Tab Installation
Figure 26 – Wing Fence, Flow Energizer, and Aileron Trim System
Figure 27 – Checkvalves and Filling Baffles Wing
Figure 28-49 – Electrical Schematics
IV. TIME LIFE COMPONENTS
1. Airframe
2. Engine
3. Propeller
V. CONTINUED AIRWORTHINESS INSPECTION CRITERIA
