EASA Regulations for Cessna 172R

5 airworthiness directives and regulations affecting Cessna 172R.

EASA SIB CE-12-02R1

Cessna 172R/172S- Alternative Methods of Compliance (AMOC) for FAA AD 2001-06-17

The Cessna 172R/172S- Alternative Methods of Compliance (AMOC) for FAA AD 2001-06-17 is a Safety Information Bulletin addressing alternative compliance options for the FAA Airworthiness Directive 2001-06-17. It specifically concerns the Cessna 172R and 172S aircraft models. The bulletin provides guidance on acceptable alternative methods to meet the safety requirements outlined in the original AD.

Nov 14, 2014

Safety Information BulletinMaintenanceSafety MgmtCessna 172RCessna 172S

EASA SIB CE-12-15

Cessna 172R/S, (T)182T and (T)206H Aeroplanes with Garmin G1000 Avionics - Master Switch Failure

The Special Airworthiness Information Bulletin SAIB: CE-12-15 is an FAA informational bulletin addressing a potential failure of the avionics master switch on Cessna 172R, 172S, 182T, T182T, 206H, and T206H airplanes equipped with Garmin G1000 avionics. The bulletin highlights a risk of accelerated switch failure that could lead to loss of avionics equipment, though essential flight and landing systems remain powered through alternate electrical sources.

Feb 1, 2012

Safety Information BulletinMaintenanceSafety MgmtCessna 172RCessna 172SCessna 182TCessna T182TCessna 206HCessna T206H

EASA SIB CE-12-03

Cessna Model 172R and 172S Fuel Control; Engine Performance with the Throttle Control at Idle

The Special Airworthiness Information Bulletin SAIB: CE-12-03 is an informational document issued by the FAA regarding fuel control and engine performance at idle throttle settings for 1996 and later Cessna Model 172R and 172S reciprocating engine airplanes. It addresses concerns about proper engine operation when the throttle is at idle and clarifies what constitutes idle engine performance. The bulletin is not an airworthiness directive and does not impose mandatory requirements.

Nov 2, 2011

Safety Information BulletinMaintenanceSafety MgmtCessna 172RCessna 172S

EASA SIB CE-11-37

Piper PA-44-180 & Cessna 172R and S Aeroplanes - Engine Oil Filter Interference

The Special Airworthiness Information Bulletin SAIB: CE-11-37 is an FAA informational bulletin addressing engine oil filter interference issues in Piper PA-44-180 aircraft with Lycoming O-360-A1H6 and LO-360-A1H6 engines, and Cessna 172R and S aircraft with Lycoming IO-360-L2A engines. The bulletin highlights potential interference between oil cooler hose fittings and the oil filter that could lead to improper installation and oil system problems. Other engines and aircraft models may also be affected.

Jun 6, 2011

Safety Information BulletinMaintenanceSafety MgmtPiper PA-44-180Cessna 172RCessna 172S

EASA SIB CE-09-12

Garmin G1000, G900X and G950 units - CRS/BARO Knob Interference

Special Airworthiness Information Bulletin SAIB: CE-09-12 is an FAA informational bulletin addressing a potential interference issue between the CRS and BARO knobs in some Garmin G1000, G900X, and G950 avionics installations. This issue affects aircraft equipped with certain 10-inch GDU 104X displays, including models such as Cessna 172R/172S/182T, Columbia 350/400, Diamond DA40/DA42, Mooney M20 series, Piper PA 32 Saratoga, Quest Kodiak 100, and Hawker Beechcraft G36 Bonanza and G58 Baron. The bulletin provides awareness of the concern but does not mandate corrective action.

Feb 17, 2009

Safety Information BulletinMaintenanceSafety MgmtCessna 172RCessna 172SCessna 182TColumbia 350Columbia 400Diamond DA40Diamond DA42Mooney M20Piper PA 32 SaratogaQuest Kodiak 100Hawker Beechcraft G36 BonanzaHawker Beechcraft G58 Baron