Aquila AT01-100 Manuel utilisateur

POH / AFM

AQUILA AT01-100/200 POH-Supplement

AS-18

Document Nr.: Issue: supersedes Issue: Date: Page:

FM-AT01-1010-257 A.02A.01 (15.10.2013) 02.03.2020 AS-18-1

SECTION 9

Pilot's Operating Handbook Supplement AS-18

GARMIN GNC 255A / 255B (COM/NAV)

This supplement is applicable and must be inserted into Section 9 of the POH when the

Garmin GNC 255A or 255B COM/NAV is installed in the AQUILA AT01-100/200. The

information in this supplement adds to or replaces information in the basic POH.

Revision A.02 of AFM Supplement AS-18 ref. FM-AT01-1010-257 is approved under the authority

of DOA ref. EASA.21J.025.

POH / AFM

AQUILA AT01-100/200 POH-Supplement

AS-18

Document Nr.: Issue: supersedes Issue: Date: Page:

FM-AT01-1010-257 A.02 A.01 (15.10.2013) 02.03.2020 AS-18-2

0.1 RECORD OF REVISIONS

Issue Reason for Change Effected Pages Date of Issue

A.01 Initial Issue All 15.10.2013

A.02 also valid for AT01-200 All 02.03.2020

0.2 LIST OF CURRENT PAGES

Page Issue Date

1 - 6 A.02 02.03.2020

0.3 TABLE OF CONTENTS

1. GENERAL...............................................................................................................3

2. OPERATING LIMITATIONS...................................................................................4

3. EMERGENCY PROCEDURES...............................................................................5

4. NORMAL PROCEDURES ......................................................................................5

5. PERFORMANCE....................................................................................................5

6. WEIGHT AND BALANCE.......................................................................................6

7. SYSTEM DESCRIPTION........................................................................................6

8. HANDLING, SERVICE AND MAINTENANCE .......................................................6

POH / AFM

AQUILA AT01-100/200 POH-Supplement

AS-18

Document Nr.: Issue: supersedes Issue: Date: Page:

FM-AT01-1010-257 A.01 - 15.10.2013 AS-18-3

1. GENERAL

The Garmin GNC 255A/255B combines a VHF communications transceiver with 200

channel VOR, Localizer and Glideslope receivers. Besides traditional Nav/Com

features, the GNC 255 also incorporates workload-reducing functions such as automatic

decoding of the Morse code station identifier for VOR/LOC, most-used frequency

storage in memory and more.

The GNC 255A/255B has the ability to monitor the standby COM frequencies. The GNC

255’s Com radio operates in the aviation voice band, from 118.000 to 136.975 MHz, in

25 kHz steps (default). For European operations, a Com radio configuration of 8.33 kHz

steps is also available. The GNC 255 VHF Nav receiver operates from 108 MHz to

117.95 MHz decoding both the VHF Omni Range and Localizer navigation signals. The

built-in Glideslope receiver will automatically tune the corresponding glideslope paired

frequencies (328 MHz to 335 MHz) when the localizer is tuned. The GNC 255A is

available with a 10 watt com transmitter. The GNC 255B is available with a 16 watt com

transmitter.

GNC 255A / 255B Front Panel:

Photo

Sensor

Frequency Transfer

(FLIP/FLOP) Key

USB

Port

LARGE and

SMALL Knobs

(Frequency

Adjust)

Power On/Off,

Com Volume,

Squelch On/Off

Nav (VLOC)

Volume, Nav ID

On/Off

Frequency

Monitor Key

Com or Nav

Frequency Selection

OBS

Selection

To/From

Selection

Function

Selection

Clear Data

Key

Enter Key

POH / AFM

AQUILA AT01-100/200 POH-Supplement

AS-18

Document Nr.: Issue: supersedes Issue: Date: Page:

FM-AT01-1010-257 A.01 - 15.10.2013 AS-18-4

2. LIMITATIONS

The information contained in this supplement must be used in conjunction with the basic

POH.

Pilot´s Guide

The Garmin GNC 255A / 255B Pilot´s Guide, p/n 190-01182-01, Rev. A (or later

revisions), must be immediately available to the flight crew.

WARNING

For safety reasons, GNC 255´s operational procedures must be learned on the ground.

NOTE

The Garmin GNC 255A / 255B must be switched off during engine start-up and shut-

down. Non-compliance could destroy the equipment. All warranty and guarantee claims

will become void!

NOTE

Do not use outdated database information. Databases used in the system must be

updated regularly in order to ensure that the information remains current. Pilots using an

outdated database do so entirely at their own risk.

NOTE

Transmit Duty Cycle: 10W: 100%

16W: Recommended 25% (5 seconds on/15 seconds off,

15 seconds on/45 seconds off, etc.)

POH / AFM

AQUILA AT01-100/200 POH-Supplement

AS-18

Document Nr.: Issue: supersedes Issue: Date: Page:

FM-AT01-1010-257 A.01 - 15.10.2013 AS-18-5

3. EMERGENCY PROCEDURES

LOSS OF COM RADIO TUNING FUNCTIONS

•If alternate COM is available:

Communications USE ALTERNATE COM

•If no alternate COM is available:

FLIP/FLOP key PRESS AND HOLD FOR 2 SECONDS

NOTE

This procedure will tune the COM radio to the

emergency frequency 121.5. Certain failures of the tuning system

will automatically tune 121.5, regardless of what frequency is

displayed on the GNC, without flight crew action.

NOTE

The GNC 255 helps protect you from a situation where the microphone may get stuck

in the ON or Transmit position. If the microphone is keyed for longer than 35 seconds,

the GNC 255 will return to the receive mode on the selected frequency.

A “Stuck Mic” message will display until the transmit key is released. Alerts will

display until the error clears or the user acknowledges it.

LOSS OF NAVIGATION FUNCTIONS

Use alternative Navigation

4. NORMAL PROCEDURES

Refer to the Pilot´s Guide defined in Section 2 of this document for normal operating

procedures and a complete list of system messages and associated flight crew actions.

5. PERFORMANCE

No change to the basic POH.

POH / AFM

AQUILA AT01-100/200 POH-Supplement

AS-18

Document Nr.: Issue: supersedes Issue: Date: Page:

FM-AT01-1010-257 A.01 - 15.10.2013 AS-18-6

6. WEIGHT AND BALANCE

Changes to Weight and Balance due to Installation/Removal of the GNC 255A/255B

must be considered in accordance with chapter 6 of the Basic POH.

7. SYSTEM DESCRIPTION

Pilot’s Guide

The Garmin GNC 255A / 255B Pilot´s Guide, defined in Section 2 of this document,

contains information regarding GNC system description, control and function. This

Pilot’s Guide must be immediately available to the flight crew.

Power

Power to the Garmin GNC 255A / 255B is provided through a circuit breaker labeled

COM 1 or COM 2. Power to the NAV Unit is provided through a circuit breaker labeled

NAV/GPS 1 or NAV/GPS 2.

Database

Instructions for updating the Frequency Database can be found in the Garmin GNC

255A / 255B Pilot´s Guide, defined in Section 2 of this document.

8. HANDLING, SERVICE AND MAINTENANCE

CAUTION

The Garmin GNC 255A/255B must be switched off during engine start-up and shut-

down. Otherwise it could be seriously damaged or destroyed. All warranty and

guarantee claims will become void!

CAUTION

The GNC 255´s display uses a lens coated with a special anti-reflective coating that is

very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING

AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to

clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is

specified as safe for anti-reflective coatings.

MALFUNCTION OF THE GNC 255A / 255B:

The Garmin GNC 255 does not contain any user-serviceable parts. Repairs should only

be made by an authorized Garmin service center. Unauthorized repairs or modifications

could void both the warranty and the pilot’s authority to operate this device under local

authority regulations.

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