AD 76-07-09

Active

Radio Magnetic Indicator

Key Information
76-07-09
Active
April 19, 1976
Not specified
Unknown
39-2570
Applicability
["Appliance"]
Not specified
Collins
Radio Magnetic Indicator
Regulatory Text

76-07-09 COLLINS: Amendment 39-2570. Applies to Collins Model 332C-10 Radio Magnetic Indicator (part numbers and serial numbers listed below) installed on various aircraft makes and models equipped with 24 V electrical systems:

Collins Part No.
Serial No.
622-0555-001
729 and below
622-0555-002
963 and below
622-0555-003
3593 and below, 3595 thru 3600,

3602 thru 3611, 3613 thru 3628
622-0555-004
3693 and below, 3695 thru 3706
622-0555-005
3252 and below
622-0555-006
4156 and below
622-0555-007
3208 and below, 3210 thru 3231,

3233 thru 3239
622-0555-008
2805 and below

Compliance: Required as indicated, unless already accomplished.

To preclude possible erroneous VOR bearing information presentation, with no flag warning, when 26 VAC input power is lost, accomplish the following:

A) Within 50 hours" time in service in service after the effective date of this AD, determine if the 332C-10 Radio Magnetic Indicator(s) is (are) installed, and if so, whether modified in accordance with Collins 332C-10 Radio Magnetic Indicator (622-0555-XXX) Service Bulletin No. 6, dated February 16, 1976, or later approved revision. On those units not modified in accordance with Service Bulletin No. 6, prior to further flight, install a placard on glass face of the magnetic indicator which reads:

"USE ADF MODE ONLY"

and operate the unit in accordance with this limitation.

NOTE: Indicators which have been modified in accordance with Service Bulletin No. 6 will have the No. 6 removed from the modification plate attached to the unit.

B) On or before January 1, 1977, modify the 332C-10 indicators(s) in accordance with Collins 332C-10 Radio Magnetic Indicator (622-0555-XXX) Service Bulletin No. 6, dated February 16, 1976, or later approved revisions.

C) When Paragraph B has been accomplished, compliance with Paragraph A is no longer required.

D) Any alternate method of compliance with this AD must be approvedby the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

This amendment becomes effective April 19, 1976.

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References
This information is not available.
--- - Part 39
FAA Documents