Aeronautica

Sandel Avionics Inc. 2401 Dogwood Way Vista, CA 92081 USA Supplement No. ST12361 LA-T-1 0

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT TO THE

Make and Model Airplane (per AML # ST12361LA-T-16)

Aircraft SIN ~

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Aircraft Reg. No. ~

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This document must be attached to the FAA Approved Airplane Flight Manual, when the aircraft is modified by the installation of SandelAvionics SA4550 Primary Attitude Display in accordance with STC no. ST01930LA. The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitation,procedures, and performance information not contained in this supplement, consult the basic Airplane Flight Manual

FAA APPROVED:

Manager~Ch, ANM-160L Federal AviaY9rl Administration LosAngeleslAircraft Certification Office Transport Airplane Directorate

L///--L-4

DATE:

~

Sandel Avionics Inc. 2401 Dogwood Way Vista, CA 92081 USA Supplement No. ST12361LA-T-10

AFM SUPPLEMENTfor Models as listed in AML ST12361LA-T-16 Sandel Avionics SA4550 ADI STC No. ST01930LA

LOG OF PAGES PAGE
Rev

No. Original

No. Title Log Contents 1 of 4 2 of 4 30f4 4 of 4

Date 06/04/0706/04/07 06/04/07 06/04/07 06/04/07 06/04/07 06/04/07

DESCRIPTION Complete Supplement

FAA APPROVED

Mgr::Fii~ANM=160L FAA, Los ngeles ACO Transport Airplane Directorate

A~

Date

tf--1-

07

Pagei

Sandel Avionics Inc. 2401 Dogwood Way Vista, CA 92081 USA Supplement No. ST12361LA-T-10

AFM SUPPLEMENT for Models as listed in AML ST12361LA-T-16 Sandel Avionics SA4550 ADISTC No. ST01930LA

TABLE OF CONTENTS

SECTION

PAGE

SECTION 1: GENERAL

1

SECTION 2: LIMITATIONS

2

SECTION 3: EMERGENCY PROCEDURES

3

SECTION 4: NORMAL PROCEDURES

3SECTION 5: ABNORMAL PROCEDURES

4

SECTION 6: PERFORMANCE

DATA

4

SECTION 7: WEIGHT AND BALANCE DATA

4

SECTION 8: SYSTEM DESCRIPTIONS

4

FAA Approved Date June 4.2007

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