Aveo Engineering Mooney M20 Installation Instruction

Installation Instruction

Mooney M20
Series

www.aveoengineering.com

Mooney M20 series Installation Instruction s

AVE-MOD-012-INS

Issue 02

__________________________________________________________________________________

Aveo Engineering Group, s.r.o.

Drasov 202, 261 01 Drasov

Czech Republic

Issue of form 01

Page 2 of 21

Table of Contents

PART 0

MANUAL ADMINISTRATION 3

0.1 DOCUMENT APPROVAL 3

0.2 AMENDMENT RECORD PROCEDURE 4

0.3 AFFECTED PAGES PROCEDURE 4

PART 1 INSTALLATION INSTRUCTION 5

1.1 GENERAL 5

1.2 CONTINUED AIRWORTHINESS 5

1.3 DESCRIPTION 6

1.3.1 Wingtip lights 6

1.3.2 Aft position light 7

1.3.3 Anti-collision lights 7

1.3.4 Taxi- and landing lights 7

1.4 WINGTIP MODIFICATION 8

1.4.1 Option A - Replacement of Light Unit 8

1.4.2 Option B - Wingtip Replacement 11

1.5 REAR POSITION LIGHT INSTALLATION 13

1.6 ANTI-COLLLISION LIGHTS INSTALLATION 15

1.7 TAXI AND LANDING LIGHTS INSTALLATION 16

1.7.1 Wing inst allation 16

1.7.2 Cowling installation 19

PART 2 COMPLIANCE DEMONSTRATION 21

Mooney M20 series Installation Instruction s

AVE-MOD-012-INS

Issue 02

__________________________________________________________________________________

Aveo Engineering Group, s.r.o.

Drasov 202, 261 01 Drasov

Czech Republic

Issue of form 01

Page 3 of 21

Part 0 Manual Administration

0.1 Document approval

This document has been established in accordance with an alternative procedure to
DOA approved under EASA AP429.
This ins t allatio n Instruction is applicable for the Mooney models M20J, M20K, M20L
and M20S.

Compiled by: 19. – Dec. - 2018

Petr Jaroš

Engineer, Aveo Engineering Group, s.r.o.

Approved by: 19. – Dec. - 2018

Georg Hartl

Head of DO, Aveo Engineering Group, s.r.o.

Mooney M20 series Installation Instruction s

AVE-MOD-012-INS

Issue 02

__________________________________________________________________________________

Aveo Engineering Group, s.r.o.

Drasov 202, 261 01 Drasov

Czech Republic

Issue of form 01

Page 4 of 21

0.2 Amendment Record procedure

The master copy of this document shall be kept electronically as a read only
document under the control of Aveo Engineering Group, s.r.o. as Master Copy.

ALL amendments to this manual will initiate a raise of Issue
ALL raises of issue will be given a sequential Alphabetic Issue Ident sequentially

from 01 to 99 in Table 01 - Issue No: Column– Initial Issue of Document will be

“01”
ALL Issues of this document will be approved by Head of DO

0.3 Affected Pages Procedur e

ALL pages affected by ANY raise of issue of this document will be listed in Table 01 ­Affected Pages Column.
The reason(s) for ALL ra ise of issu e and desc ripti on of change du e to raise of issue will be
provided for ALL raises of issu e in Table 01 - Details Column.
Changes from the previous issue are highlighted by YELLOW HIGHLIGHTING over new
content. AND YELLOW HIGHLIGHTING AND CROSSING OUT of deleted content.
Example (CROSSING OUT)

Issue

No.

Details Date

Affected

Pages

01 Initial Issue 28.Aug.2018 ALL

02

Remove models M20M, M20R, M20TN , M20U,

M20V(not marked)

Correct references to installation manuals and

AMM SUP

Add remark

Add standard for wire

Correct instruction for tip installation, add EN 2267

reference, remove preheating (not marked)

Add balancing of rudder

19.Dec.2018

3

5

10

12

14

Table 01: Document Amendment Record Table

Mooney M20 series Installation Instruction s

AVE-MOD-012-INS

Issue 02

__________________________________________________________________________________

Aveo Engineering Group, s.r.o.

Drasov 202, 261 01 Drasov

Czech Republic

Issue of form 01

Page 5 of 21

Part 1 Installation Instruction

1.1 General

This ins t allatio n is to be performed in accordance to common practice as described in
FAR AC 43.13-2B Chapter 4 and in FAR AC 43.13 1B Chapter 11 Section 15 (Bonding)
as published by FAA.

The installer is responsible to follow the installation instructions in the latest revision
of:

• FAR AC 43.13-2B Chapter 4

• FAR AC 43.13 1B Chapter 11 Section 15

• AVE-WPS-64G-IM

• AVE-PSPSYW-IM

• AVE-RBXP-001-IM

• AVE-CCPS-IM

• AVE-H30-002-IM

• AVE-SDD45-IM

All drawings applicable for this change are listed in the Drawing List:

• AVE-MOD-012-DL, issue 01

The following appliances carry an ETSO authorization:

• AVE-WPSR-64G & AVE-WPSG-64G – ETSOA 210.10053936

• AVE-RBXPR-001 – ETSOA 210.10055069

The change is to be performed using the document AVE-MOD-012-MCS in the latest
issue.

The aircraft modified according to this instruction may not be released back to service
without the EASA design approval certificate being provided.

1.2 Continued Airworthiness

The aircraft manuals remain fully valid. The inspection intervals and the procedures of
the aircraft override the general statements in the component manuals as listed under

§1.1.
For inspection of the new lights themsel ves follow the procedure of the AMM

supplement AVE-MOD-012-SUP-AMM.

Mooney M20 series Installation Instruction s

AVE-MOD-012-INS

Issue 02

__________________________________________________________________________________

Aveo Engineering Group, s.r.o.

Drasov 202, 261 01 Drasov

Czech Republic

Issue of form 01

Page 6 of 21

1.3 Description

This modification is the replacement or new installation of the composite wingtip
segment and of position, anti-collision, taxi- and landing lights by LED type lights.

1.3.1 Wingtip lights

This modification allows on aircraft which already have a composite wingtip to replace
either the complete wingtip or only the light unit inside or outside the original
composite wingtip. The Mooney also exists in versions without a composite wingtip at
all. For those aircraft the light unit can be replaced. Aircraft which originally have no
composite wingtip cannot be equipped with the Aveo wingtip.

Aveo designed a new wingtip with integrated position lights type I and II including the
strobe function.
Alternatively the originally wingtip lights on aircraft with or without wingtip can be
replaced by the Aveo Ultra Galactica embedded without installation or replacement of
the conformal wingtip. The Ultra Galactica e mbedded also fulfills the requirement for
position lights type I and II plus the strobe function.

1. Light assembly navigation &
strobe

2. Wingtip

3. Landing / Taxi light installation
LH, RH and cowling

4. Recognition light installation

5. Beacon installation

6. Strobe assembly tail

7. Ice retrofit

Synchronization:
The strobe lights may be synchronized but the frequency of the strobes is so low that
synchronization of the lights is not required.

For the synchronization function the blue wires of each light to be synchronized have
to be connected. If for this function additional wires are to be installed then these
must be installed along the wire bundle in which the lights power wires run. If the
function is not used the blue wire at each light is to be capped and stowed.

Mooney M20 series Installation Instruction s

AVE-MOD-012-INS

Issue 02

__________________________________________________________________________________

Aveo Engineering Group, s.r.o.

Drasov 202, 261 01 Drasov

Czech Republic

Issue of form 01

Page 7 of 21

1.3.2 Aft position light

The aft position light can be replaced by Aveo PosiStrobe CP. The light is a direct
replacement. For synchronization applies description under section 1.3.1.

1.3.3 Anti-collision lights

The originally installed anticollision light can be replaced by Aveo RedBaron XP red
including the adapter.

1.3.4 Taxi- and landing lights

The M20 can be equipped with a taxi light (wide angle lens) and a landing light
(narrow angle). This modification allows replacing all insta lled taxi and landing lights
with the same configuration as installed before the modification. A configuration
change is not allowed.