Schempp-Hirth Flugzeugbau ARCUS M - User Manual

SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK
P R O V I S I O N A L
FLIGHT MANUAL
for Powered Sailplane
Model: A R C U S M
Serial-No.:
Registr.-No.:
Date of issue:
O c t o b e r 2 0 1 1
Pages as indicated by „
appr.“ are approved by
This powered sailplane is to be operated in compliance with information and limitations
contained herein.
Approval of translation has been done by best knowledge and judgement.
In any case the original text in German language is authoritative.

Summary

Section 1

1. General

Provides an overview of general information for the Arcus M aircraft.

1.2 Certification basis

Details the aircraft's certification and approval by EASA.

1.4 Descriptive data

Describes the physical characteristics and construction of the aircraft.

Section 2

2. Limitations

Outlines crucial operating limits and restrictions for safe flight.

2.2 Airspeed

Details airspeed limitations and their operational significance.

2.7 Centre of gravity

Defines CG limits and calculation methods for safe operation.

2.12 Minimum equipment

Lists essential instruments and equipment required for normal operations.

Section 3

3. Emergency procedures

Provides guidance on handling various in-flight emergencies.

3.4 Stall recovery

Explains methods for recovering from stalls in different configurations.

3.7 Engine failure

Covers procedures for engine failure during takeoff and flight.

Section 4

4. Normal operating procedures

Guides pilots through standard flight operations.

4.3 Inspections

Outlines daily and pre-flight inspection procedures.

4.4 Pre-flight inspection

Provides pre-takeoff and self-launch checklists.

Section 5

5. Performance

Presents data on the aircraft's performance characteristics.

5.2 Approved data

Details approved data for airspeed calibration and stall speeds.

5.2.2 Stall speeds

Lists stall speeds at various flap settings and configurations.

Section 6

6. Weight (mass) and balance

Covers weight and balance procedures and permitted load ranges.

6.2 Weight and balance record; Permitted seat load range

Details loading charts and seat load limits.

Section 7

7. Description of the aircraft and its system

Describes the aircraft's components and systems.

7.2 Cockpit-Description

Provides a detailed description and labeling of the cockpit layout.

7.3 Instrument panels

Explains the front and rear instrument panels and their components.

7.10 Power plant system

Describes the engine, propeller, and associated control systems.

7.11 Fuel system

Details the aircraft's fuel system, including tank capacities and refueling.

Section 8

8. Handling, care and maintenance

Covers procedures for ground handling, servicing, and care.

8.2 Powered sailplane inspection periods

Details maintenance schedules for airframe, cables, and power plant.

8.3 Alterations or repairs

Outlines procedures for modifications, repairs, and abbreviations.

Section 9

9. Supplements

Contains supplementary information for optional systems and equipment.

9.1 Introduction

Introduces the supplements for optional systems and equipment.

Schempp-Hirth Flugzeugbau ARCUS M Specifications

General

Category	Sailplane
Manufacturer	Schempp-Hirth Flugzeugbau
First Flight	2009
Maximum Glide Ratio	50:1
Wingspan	20.0 m (65 ft 7 in)
Maximum Takeoff Weight	850 kg
Maximum Speed	280 km/h
Cockpit	Two seats in tandem