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General| Horsepower | 260 hp each |
|---|---|
| Wingspan | 37 ft 10 in (11.53 m) |
| Seating | 6 |
| Manufacturer | Raytheon |
| Model | Baron D55 |
| Type | Twin-engine piston aircraft |
| Engine | 2 x Continental IO-470-L |
| Range | 1, 200 miles (1, 931 km) |
Procedures for safe ground handling to avoid damage, including towing and jacking instructions.
Instructions for checking refrigerant level, changing air filters, and charging the system.
Step-by-step procedure for removing the wing, including fuel lines, wiring, and hydraulic connections.
Instructions for removing and installing cabin doors, including handle and latch adjustments.
General information on control surfaces, travel stops, and rigging illustrations.
Procedures for removing, installing, and rigging ailerons and trim tabs.
Details on elevator removal, installation, trim tab actuator procedures, and free play checks.
Step-by-step instructions for overhauling the main landing gear, including disassembly and cleaning.
Details on engine types, ratings, magneto timing, spark plugs, oil pressure, and oil capacity.
Description of fuel system components, fuel selector valve operation, and fuel quantity indicators.
Details the heater control system, including thermostats, iris valve, and safety switch.
Information on the oxygen system, including cylinder removal, installation, and low pressure testing.
Procedures for servicing, charging, and troubleshooting the air conditioning system.
Details on lead-acid battery installation, maintenance, cleaning, and troubleshooting.
Procedures for obtaining optimum service from nickel-cadmium batteries, including maintenance and reconditioning.
Information on alternator removal, installation, and voltage regulator adjustment.
Information on the stall warning system, including adjustment procedures.
Overhaul and replacement intervals for landing gear components.
Overhaul and replacement intervals for engine components, including propellers and pumps.
General maintenance practices and compliance with Airworthiness Directives.
Detailed inspection procedures for the 100-hour service interval.
Procedures for first and second level inspections after a hard landing.
Procedures for inspecting the airframe components after encountering turbulent air.
Procedures for inspecting components for damage after a lightning strike.
