Division Cessna 170, 172, F172, FR172 and 175 Ser - AD/CESSNA 170/83 - Alternate Static Air Source Valve - Cessna 170, 172, F172, FR172 and 175 Series Aeroplanes

Cessna 170, 172, F172, FR172 and 175 Series Aeroplanes

AD/CESSNA 170/83	Alternate Static Air Source Valve	7/2008 TX

<table cellspacing="0" cellpadding="0" style="width:510.3pt; margin-top:0pt; margin-bottom:0pt; border-collapse:collapse"><tbody><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Applicability:</span></p></td><td colspan="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Aeroplanes models listed in Table 1 and Table 2 that have an alternate static air source selector valve, part number (P/N) 2013142-18, installed after 19</span><span> </span><span>November</span><span> </span><span>2007.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span></span></p></td><td colspan="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span>Note 1:</span><span> </span><span>Aircraft listed in Table 1 had an </span><span>alternate static air source selector valve, P/N 2013142-18, installed during manufacture but may have also had the affected part installed as a replacement part.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="3" style="width:414.55pt; border-bottom:0.75pt solid #000000; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">Table 1 - Applicability for Aeroplanes that Had</span><br><span style="font-weight:bold">the Affected Part Installed at Manufacture</span></p></td></tr><tr><td style="width:74.35pt; border-right:0.75pt solid #000000; padding-right:4.97pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td style="width:164.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span style="font-weight:bold">Model</span></p></td><td colspan="2" style="width:239.1pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">Serial Numbers</span></p></td></tr><tr><td style="width:74.35pt; border-right:0.75pt solid #000000; padding-right:4.97pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td style="width:164.75pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>172S</span></p></td><td colspan="2" style="width:239.1pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>172S10672 through 172S10674, 172S10676, 172S10678 through 172S10680, 172S10682, 172S10683 and 172S10685</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="3" style="width:414.55pt; border-top:0.75pt solid #000000; border-bottom:0.75pt solid #000000; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">Table 2 - Applicability for Aeroplanes that Could Have Had the Affected</span><br><span style="font-weight:bold">Part Installed as a Replacement Part or From Parts Held as Spares</span></p></td></tr><tr><td style="width:74.35pt; border-right:0.75pt solid #000000; padding-right:4.97pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="2" style="width:221.45pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span style="font-weight:bold">Model</span></p></td><td style="width:182.4pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span style="font-weight:bold">Serial Numbers (S/N)</span></p></td></tr><tr><td style="width:74.35pt; border-right:0.75pt solid #000000; padding-right:4.97pt; padding-left:5.35pt; vertical-align:top"><p><span></span></p></td><td colspan="2" style="width:221.45pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p><span>172</span><br><span>172R</span><br><span>172S</span><br><span>F172D</span><br><span>F172E</span><br><span>F172F</span><br><span>F172G</span><br><span>F172H</span><br><span>F172K</span><br><span>F172L</span><br><span>F172M</span><br><span>F172N</span><br><span>F172P</span><br><span>FR172E</span><br><span>FR172F</span></p></td><td style="width:182.4pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top"><p style="text-align:center"><span>All S/Ns</span><br><span>All S/Ns beginning with 17280001</span><br><span>172S8001 through 172S10671</span><br><span>All S/Ns</span><br><span>All S/Ns</span><br><span>All S/Ns</span><br><span>All S/Ns</span><br><span>All S/Ns</span><br><span>All S/Ns</span><br><span>All S/Ns</span><br><span>All S/Ns</span><br><span>All S/Ns</span><br><span>All S/Ns</span><br><span>All S/Ns</span><br><span>All S/Ns</span></p></td></tr><tr style="height:0pt"><td style="width:85.05pt"></td><td style="width:175.45pt"></td><td style="width:56.7pt"></td><td style="width:193.1pt"></td></tr></tbody></table>

	4. If, during any requirement 1 inspection, the alternate static air source selector valve port is found obstructed by the part number identification placard, remove the placard from the valve body, discard the placard and assure that the port is open and unobstructed.
	5. Static air source selector valves P/N 2013142-18 installed as modification or replacement parts on or after the effective date of this Directive must be inspected in accordance with Requirement 1 prior to installation.
	Note 4: FAA AD 2008-10-02 Amdt 39-15508, which becomes effective on 12 May 2008, refers.
Compliance:	For Requirements 1, 2 and 3 - Before further flight after the effective date of this Directive.
	For Requirement 4 - Before further flight after the Requirement 1 inspection.
	For Requirement 5 - As of the effective date of this Directive.
	This Airworthiness Directive becomes effective on 13 May 2008.
Background:	The United States Federal Aviation Administration (FAA) has received reports of improper installation of the part number identification placard on alternate static air source selector valves of certain Cessna 172, 175, 180, 182, 185, 206, 207, 208, 210 and 303 series aeroplanes. The part number identification placard refers to alternative air source selector valves, part number 2013142-18 that were manufactured between 20 November 2007 and 18 February 2008. The part number identification placard was installed on the valve body in a location that covers the port, which is the inlet for static air reference into the valve. The problem was discovered during a quality control check.
	The FAA has advised that all parts held in stock at Cessna have been corrected and that Cessna has no way of verifying how many of these assemblies were manufactured and sent to the field with the part number identification placard installed over the alternate static air source selector valve port. The Civil Aviation Safety Authority (CASA) has no way of determining which aeroplanes have the remaining problem alternate static air source selector valve assemblies installed without having all of the affected aeroplanes and spares stock inspected.
	This condition, if not corrected, could result in the altimeter, airspeed and vertical speed indicators displaying erroneous indications. This could cause the pilot to react to incorrect flight information and possibly result in loss of control.

Cessna 170, 172, F172, FR172 and 175 SerCessna 170, 172, F172, FR172 and 175 Series Aeroplanes

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Cessna 170, 172, F172, FR172 and 175 Series Aeroplanes