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Robin DR400/180R User Manual

Robin DR400/180R
104 pages
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PILOT’S OPERATING HANDBOOK
SUPPLEMENT
DR400/135CDI
Document n° 1001639
GB

Table of Contents

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Robin DR400/180R Specifications

General IconGeneral
ManufacturerRobin Aircraft
ModelDR400/180R
TypeLight Aircraft
Horsepower180 hp
Wingspan8.72 m (28 ft 7 in)
Seating Capacity4
EngineLycoming O-360
Range1, 200 km
Rate of climb4.5 m/s
Fuel capacity120 L

Summary

SECTION 2 LIMITATIONS

APPROVED OPERATION

Defines approved operating parameters for the aircraft.

MAXIMUM ALTITUDE

Specifies the maximum altitude the aircraft is qualified for.

FLIGHT LOAD FACTOR LIMITS AT MAXIMUM WEIGHT

Outlines load factor limits for different weights and configurations.

MAXIMUM AUTHORIZED WEIGHTS

Lists the maximum takeoff and landing weights.

ENGINE OPERATING LIMITS

Specifies limits for engine operation.

PERMISSIBLE FUEL GRADES

Lists approved fuel grades for the aircraft.

MAXIMUM FUEL QUANTITIES

Details the fuel capacity of the standard and optional tanks.

PERMISSIBLE OIL GRADES

Lists approved oil grades for the engine and gearbox.

SECTION 3 EMERGENCY PROCEDURES

ENGINE FAILURE OR LOSS OF POWER

Procedures for engine failure during various flight phases.

LANDING WITHOUT ENGINE POWER

Steps for landing the aircraft without engine power.

FADEC malfunction in flight

Actions to take for FADEC system malfunctions in flight.

ENGINE SHUT-DOWN IN FLIGHT

Steps for shutting down the engine while in flight.

FIRE

Procedures for dealing with engine or electrical fires.

ROUGH ENGINE OPERATION

Steps for handling abnormal engine operation conditions.

ICING

Procedures for encountering icing conditions.

ELECTRICAL POWER SUPPLY MALFUNCTION

Actions for electrical system power failures.

INADVERTENT SPIN

Procedure for recovering from an inadvertent spin.

LOSS OF ELEVATOR CONTROL

Guidance for loss of elevator control.

SECTION 4 NORMAL PROCEDURES

SECTION 5 PERFORMANCE

SECTION 6 WEIGHT AND BALANCE

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