XtremeAIR XA41 User Manual

Maintenance Manual XA41/XA42
AMM-XA42-0040-001 C.00
Page date: 25.09.2018 I
Aircraft Maintenance Manual
XA41 / XA42
S/N:
_________________
Registration:
_____________________
Document Number:
AMM-XA42-0040-001
Manufacturer:
XtremeAir GmbH
Harzstraße 2
Am Flughafen Cochstedt
39444 Hecklingen
Germany
This Manual includes the material required to be furnished to the maintenance
personal by EASA regulations, additional information provided by the manufacturer,
and in Chapter 4 the EASA approved Airworthiness Limitations.
The present revision C replaces the previous revision B.
The technical information contained in this document has been approved under the authority of EASA
Design Organization Approval no. EASA.21J.360

XtremeAIR XA41 Specifications

General

Brand	XtremeAIR
Model	XA41
Category	Aircrafts
Language	English

Summary

LOG OF REVISIONS

LOG OF EFFECTIVE PAGES

Chapter 01 Introduction

01-10-00 SAFETY

Outlines essential safety precautions for maintenance procedures.

Chapter 03 General Description of the Aircraft

03-10-04 Powerplant

Provides specifications for the engine, propeller, and related systems.

Chapter 04 Airworthiness Limitations

04-10-02 Replacement Time

Specifies items requiring replacement during regular maintenance periods.

Chapter 05 Time Limits and Maintenance Checks

05-10-02 Overhaul Schedule

Lists overhaul time limits for major aircraft components and systems.

05-20-00 SCHEDULED MAINTENANCE CHECKS

Details mandatory scheduled inspection tasks and intervals.

Chapter 08 Leveling and Weighing

08-20-01 Weighing

Chapter 12 Servicing

12-10-00 REPLENISHING

Chapter 20 Standard Practices - Airframe

20-10-02 Standard Torque Values

Chapter 24 Electrical Power

Chapter 25 Equipment and Furnishing

Chapter 27 Flight Controls

27-10-00 AILERONS

Details the mechanical connection and adjustment of the aileron control system.

27-20-00 RUDDER

Describes the rudder's operation and adjustment procedures.

27-30-00 ELEVATOR AND TRIM TAB

Procedures for adjusting the elevator's neutral position and trim tab operation.

Chapter 28 Fuel

28-20-01 Fuel Selector Valve and Fuel Selector Switch

28-40-00 INDICATING

Chapter 32 Landing Gear

32-10-00 MAIN LANDING GEAR

Procedures for removing and installing the main landing gear struts.

32-40-02 Brakes

Inspection, removal, and assembly procedures for the aircraft's brakes.

Chapter 34 Navigation and Pitot Static System

34-10-01 Pitot Static System

Chapter 39 Electric/Electronic Panels & Multipurpose Parts

39-30-00 THROTTLE AND TRIM CONTROL

Chapter 51 Standard Practices and Structures - General

51-70-00 REPAIRS

Outlines standard practices for repairing composite structures, including damage inspection.

Chapter 55 Stabilizers

55-10-00 HORIZONTAL STABILIZER

55-20-00 ELEVATOR

Chapter 57 Wing

57-10-00 WING

57-60-00 AILERONS

Procedures for removing, installing, and adjusting the ailerons.

Chapter 61 Propeller

61-10-00 PROPELLER

General information on the propeller, its construction, and operation.

Chapter 71 Power Plant

71-20-00 ENGINE MOUNT

Chapter 72 Engine

72-10-00 ENGINE

General information about the engine and procedures for its removal and installation.

Chapter 76 Engine Controls

76-10-00 THROTTLE CONTROL

Describes the throttle control operation, adjustment, and removal.

Chapter 79 Oil System

79-00-01 Christen Inverted Oil System