Posts Tagged ‘Cessna 172’

Special Airworthiness Bulletin on Cessna 172 Aircraft

Monday, December 1st, 2014

Special Airworthiness Information Bulletin (SAIB) is written to inform the public about an approved alternative method of compliance (AMOC) to an airworthiness directive (AD) and how to obtain a copy of the Cessna global AMOC (aka; AMOC of general applicability) to AD 2001-06-07 against 1996 and after Cessna Models 172R and 172S airplanes pdf icon CE-12-02R1.pdf
pdf icon Cessna-Global-AMOC-2001-06-17.pdf

AD on Aircraft Fuel Distribution System for Cessna 172R and 172S Aircraft

Wednesday, February 13th, 2013

The FAA is adopting a new airworthiness directive (AD) 2013-03-15 for certain Cessna Aircraft Company Models 172R and 172S airplanes. This AD was prompted by reports of chafing of a new configuration of the fuel return line assembly, which was caused by the fuel return line assembly rubbing against the right steering tube assembly during rudder pedal actuation. This AD requires you to install the forward and aft fuel return line support clamps and brackets; inspect for a minimum clearance between the fuel return line assembly and the steering tube assembly and clearance between the fuel return line assembly and the airplane structure; and, if any damage is found, replace the fuel return line assembly. They are issuing this AD to correct the unsafe condition on these products.

DATES: This AD is effective March 19, 2013.

Estimate of $223-$248 to inspect and fix ($53 to $78 for part and 2 hours of labor at $85/hour)

default icon2013-03-15.pdf

FAA Bulletin on Cessna 172, 182, 210 and Crusader Landing Gear

Friday, February 8th, 2013

This Special Airworthiness Information Bulletin (SAIB) CE-13-16 advises owners and operators of Cessna Aircraft Company Models 172RG, R182, TR182, FR182, 210N, T210N, 210R, T210R, P210N, P210R, and T303 airplanes, of an airworthiness concern, regarding landing gear hydraulic power pack systems.

At this time, the airworthiness concern is not considered an unsafe condition that would warrant airworthiness directive (AD) action under Title 14 of the Code of Federal Aviation Regulations (14 CFR) part 39.

Cessna 303 Crusader, Landing Gear

default iconCE-13-16.pdf

FAA Bulletin on Alternative Method of Compliance to AD 20010617 on Cessna 172 Aircraft

Tuesday, November 1st, 2011

This Special Airworthiness Information Bulletin (SAIB) CE-12-02 is written to inform the public about an approved alternative method of compliance (AMOC) to an airworthiness directive (AD) and how to obtain a copy of the Cessna global AMOC (aka; AMOC of general applicability) to AD 2001-06-17 against 1996 and after Cessna Model 172R and 172S airplanes.

pdf iconce-12-02.pdf pdf iconglobal_amoc_2001-06-17.pdf

AD on Alternate static air source selector valve for Cessna Aircraft

Thursday, December 16th, 2010

Airworthiness Directive 2008-26-10 for Cessna Aircraft 172, 175, 177, 180,
182, 185, 206, 207, 208, 210, 303, 336, and 337 Model Airplanes

pdf icon2008-26-10_correction.pdf