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Garmin MX20 Capstone System Instructions for Continued Airworthiness
Capstone System
Instructions for Continued Airworthiness
Document Number: 560-1040-00 Rev B
19 April 2013
Garmin International, Inc.
1200 E. 151st Street
Olathe, Kansas 66062 USA
 Copyright 2000 to 2013 Garmin AT, Inc. All rights reserved.
Garmin AT, Inc.
Instructions for Continued Airworthiness
560-1040-00 Rev B
Revision Log
Rev
A
B
Date Description
12/11/00 Initial release, Word 6.0
7-Nov-03 Change company name from UPS AT to Garmin
AT. Add CAGE code to signature block.
19-Apr-13 Correct Section 2.2 step 2 to use local altimeter
setting. Update address and Confidential notice.
EN
By Auth Chk
CWH
7718 MAK
A
9096 MAK
Company Proprietary Information
This drawing and the specifications contained herein are the property of Garmin International or its subsidiaries and
may not be reproduced or used in whole or in part as the basis for manufacture or sale of products without written
permission.
Garmin International, Inc.
1200 E. 151st Street
Olathe, Kansas 66062 U.S.A.
Garmin AT, Inc.
Cage Code
0XCJ6
P. O. Box 13549
Salem, Oregon USA
Title:
Prepared By:
Capstone Instructions for Continued Airworthiness
Craig Hudson
Number:
Date:
560-1040-00
December 11, 2000
Approved By:
Craig Hudson
Date:
12/12/00
Date:
12/12/00
Date:
12/13/00
Craig Hudson, Capstone Program Manager
Approved By:
Jeff Bethel
Jeff Bethel, MX20 Project Manager
Approved By:
Chris Schulte
Chris Schulte, Systems Engineer, DER
19-Apr-2013
Page 2 of 4
Garmin AT, Inc.
Instructions for Continued Airworthiness
560-1040-00 Rev B
Table of Contents
1. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR THE
CAPSTONE SYSTEM ............................................................................................ 4
1.1
INTRODUCTION .....................................................................................................................4
2. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS ........................ 4
2.1
2.2
FOR AIRCRAFT UTILIZING ADS-B IFR SERVICES ...............................................................4
FOR ALL OTHER AIRCRAFT .................................................................................................4
3. IMPLEMENTATION AND RECORD KEEPING ........................................ 4
19-Apr-2013
Page 3 of 4
Garmin AT, Inc.
Instructions for Continued Airworthiness
560-1040-00 Rev B
1. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR THE CAPSTONE
SYSTEM
1.1 INTRODUCTION
This document is designed to assist the installing agency of the Capstone system in preparing
Instructions for Continued Airworthiness in response to Federal Aviation Regulation (CFR 14)
Part 23.1529, Appendix G. This includes information for aircraft modified with the Capstone
STC to adequately maintain the Capstone system.
2. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
2.1 FOR AIRCRAFT UTILIZING ADS-B IFR SERVICES
Altimeter system and altitude reporting equipment tests and inspections:
1. Within the preceding 24 calendar months, each static pressure system, each altimeter
instrument, and each automatic pressure altitude reporting system must be tested and
inspected and found to comply CFR 14 part 43 appendix E.
This will entail a pitot-static check with ramp test equipment. The MX20 altitude readout can be
used to verify that the encoder is within tolerance.
2.2 FOR ALL OTHER AIRCRAFT
Altimeter system and altitude reporting equipment tests and inspections:
1. Within the preceding 24 calendar months, each static pressure system, each altimeter
instrument, and each automatic pressure altitude reporting system must be tested and
inspected and found to comply with CFR 14 part 43 appendix E; OR
2. Has been operationally checked within the preceding 90 days, and was found to be within the
limits of the permissible indicated altitude error set forth below:
 Cross check the field elevation against the altimeter and MX20 readout, when both have
been set to the known local altimeter setting. Verify both the altimeter and the MX20
display are within +/-125 feet of the field elevation; or
 While in flight, contact ATC to cross check radar surveillance altitude and
altimeter/MX20 readout. Verify both the altimeter and the MX20 readout are within +/125 feet of the ATC information.
3. Each person making the Altimeter system check, as specified above shall enter the date,
place, error, and sign the aircraft log or other record.
4. Should the altitude encoder fail the above tests, the operators must set the Capstone system
to STBY on the MX20 traffic page.
3. IMPLEMENTATION AND RECORD KEEPING
For operators under FAR 91, the owner/operator is responsible for ensuring the Instructions for
Continued Airworthiness are made part of the applicable section 91.409 inspection program for
their aircraft.
For operators under FAR 121/135, the Instructions for Continued Airworthiness must be
incorporated into the operator’s approved maintenance program through coordination and
approval with the certificate holder’s PMI/POI as applicable.
19-Apr-2013
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