| AD Number | 77-08-05 | Status | Active |
| Effective Date | April 28, 1977 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-2876 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Cessna Aircraft Company |
| Model(s) | 337 337A 337B 337C 337D 337E 337F 337G 337H M337B T337B T337C T337D T337E T337F T337G T337H T337H-SP |
77-08-05 CESSNA: Amendment 39-2876. Applies to 337 Series (Serial Numbers 337-0002 thru 33701783), T337 Series (Serial Numbers 337-0001, 337-0526 thru 33701398 and P3370001 thru P3370271) and M337 Series (Serial Numbers 337-M0001 thru 337-M0467) airplanes.
Compliance: Required as indicated, unless already accomplished.
To prevent single engine takeoffs, within the next 25 hours' time in service after the effective date of this AD, accomplish the following:
A) Install a Cessna P/N 1400019-77 placard right of the tachometer instrument which reads as follows:
"DO NOT INITIATE SINGLE ENGINE TAKEOFF"
and operate the aircraft in accordance with this limitation.
B) Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
C) Cessna Service Letter ME77-8, dated March 28, 1977, or later approved revisions pertains to the subject matter of this AD.
This amendment becomes effective April 28, 1977.