AD 80-10-01

Superseded

Placard - Airspeed

Key Information
80-10-01
Superseded
May 12, 1980
Not specified
Unknown
39-3762
Applicability
["Aircraft"]
["Small Airplane"]
Not specified
180 180A 180B 180C 180D 180E 180F 180G 180H 180J 185 185A 185B 185C 185D 185E A185E A185F
Regulatory Text

80-10-01 CESSNA: Amendment 39-3762. Applies to Cessna Models 180 through 180J, 185 through 185E, A185E, and A185F airplanes equipped with Airglas Engineering Company, Inc., LW3600-180 or LW3600-180A ski installations in accordance with STC SA213AL.

Compliance required as indicated, unless already accomplished.

To preclude the possibility of a ski rotating tip-down in flight, with resulting adverse flight and landing characteristics, accomplish the following:

(a) Operation of airplanes equipped with Airglas Engineering Company, Inc., LW3600-180 or LW3600-180A ski installations, in excess of 160 KT IAS is prohibited.

(b) Prior to further flight, on airplanes equipped with Airglas Engineering Company, Inc., LW3600-180 or LW3600-180A ski installation, install a placard on the instrument panel immediately adjacent to the airspeed indicator and in plain view of the pilot to read as follows:

DO NOT EXCEED 160 KTS IAS
WITH AIRGLAS LW3600-180
SKIS INSTALLED
or
DO NOTEXCEED 160 KTS IAS
WITH AIRGLAS LW3600-180A
SKIS INSTALLED

whichever is appropriate.

(c) Within the next 50 hours time in service after the effective date of this AD, and thereafter at any time the skis are installed, rig and modify the LW3600-180 or LW3600-180A ski check, safety, and bungee cables in accordance with Airglas Engineering Company, Inc. Service Bulletin No. LW3600-3, dated September 21, 1979, or an FAA-approved equivalent.

This amendment supersedes Amendment 39-1218 (36 FR 9860) AD 71-11-06.

This amendment becomes effective May 12, 1980.

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Related ADs
98-23-02 Replaced by the above
References
This information is not available.
--- - Part 39
FAA Documents