80-19-08: Fuel/Air Mixture
FAA order 80-19-08 is an airworthiness directive in force since September 15, 1980. The FAA's subject line: Fuel/Air Mixture. It names Cessna 172 Skyhawk: about 20,670 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- Cessna Aircraft Company
- Models
- 172RG
- On this site
- Cessna 172 Skyhawk 20,670 registered
Dates and paperwork
- In force since
- September 15, 1980
- Docket
- Unknown
- Status
- Current
- The FAA's document
- Read the order on the FAA's site
The order itself the regulatory text, as published
Show the full text (2,119 characters)
80-19-08 CESSNA: Amendment 39-3902. Applies to Model 172RG (S/N 172RG0001 through 172RG0573) airplanes certificated in all categories.
COMPLIANCE: Required as indicated unless already accomplished.
To preclude slippage of the mixture control wire at the carburetor fuel mixture control arm and resultant power loss due to a lean fuel/air mixture, within the next 25 hours time-in-service after the effective date of this AD, accomplish the following:
A) Visually inspect the mixture control connection on the right side of the carburetor for correct assembly. Assure that (1) Cessna Part Number (P/N) 9862010-9 mixture control assembly wire is secured to the Cessna P/N S2323-11 clamp at the carburetor mixture control arm with an AN960-10 (approximately .063 inch thick) washer installed between the mixture control wire and the MS20365-1032C nut and (2) an AN960-10L (approximately .032 inch thick) washer is installed between the mixture control wire and the mixture controlarm.
B) If the parts are assembled per Paragraph A), check to assure that the minimum torque on the MS20365-1032C nut is 15 inch-pounds and that the Cessna P/N S2323-11 clamp will swivel in the mixture control arm. Make the prescribed entry in the aircraft maintenance records indicating compliance with this AD and no further action is required.
C) If the parts are not assembled per Paragraph A) remove and discard the MS20365-1032C nut. Install washers in the positions specified by Paragraph A) and install a new MS20365-1032C nut. Torque the nut to 15 inch-pounds minimum and assure that the Cessna P/N S2323-11 clamp will swivel in the mixture control arm.
D) Airplanes may be flown in accordance with FAR 21.197 to a location where the inspection required by Paragraph A) may be accomplished.
E) Any equivalent method of compliance with this AD must be approved by the Chief, Aircraft Certification Program, Federal Aviation Administration, Room 238, Terminal Building No. 2299, Mid-Continent Airport, Wichita, Kansas 67209; Telephone (316) 942-4285.
This amendment becomes effective September 15, 1980.
Related safety bulletins advice on the same designs, not orders
2022-12-06CE-19-01 R1 · Engine Oil and Airplane Hour Meter; Pressure Switch Failure
2021-08-26AIR-21-16 · FLIGHT COMPARTMENT EQUIPMENT, Cessna Seat Back Attachment Bolt Inspection
2019-02-12CE-19-01 · Engine Oil and Airplane Hour Meter; Pressure Switch Failure
2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2018-07-19CE-18-23 · Passenger Compartment Equipment - Installation of F. Atlee Dodge Aircraft Services LLC. Folding Jump Seats
Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 8, 2026. Connections as data: /graph/directive/80-19-08.json · aircraft systems.
