Division Cessna 500 (Citation) Series Aeroplanes - AD/CESSNA 500/29 - Wing Fuel Boost Pump Wiring - Cessna 500 (Citation) Series Aeroplanes

Cessna 500 (Citation) Series Aeroplanes

AD/CESSNA 500/29	Wing Fuel Boost Pump Wiring	8/2007 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>Cessna Model 500 and 501 model aeroplanes with serial numbers 001 through 0689 inclusive.</span></p></td></tr><tr><td style="width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p><span>Requirement:</span></p></td><td colspan="3" style="width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:21.3pt; text-indent:-21.3pt"><span>1.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>If not previously accomplished, </span><span>revise the Limitations Section of the applicable Cessna aircraft flight manual (AFM) to prohibit use of the wing fuel boost pumps for defueling under certain conditions, by inserting the applicable temporary change identified in the following table.</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 style="width:157.7pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:21.3pt; margin-bottom:12pt"><span style="font-weight:bold">AFM Temporary Change</span></p><p style="margin-top:12pt; margin-left:35.45pt"><span>500FM TC-R57-01</span><br><span>500FM TC-R57-02</span><br><span>500FM TC-R57-03</span></p></td><td style="width:104.4pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-bottom:12pt; text-align:center"><span style="font-weight:bold">Dated</span></p><p style="margin-top:12pt; margin-left:15.9pt"><span>5 April 2004</span><br><span>5 April 2004</span><br><span>5 April 2004</span></p></td><td style="width:131.05pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-bottom:12pt; text-align:center"><span style="font-weight:bold">AFM</span></p><p style="margin-top:12pt"><span>Cessna Model 500</span><br><span>Cessna Model 500</span><br><span>Cessna Model 500</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; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:21.3pt; text-indent:-21.3pt"><span>2.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>If not previously accomplished</span><span>, install a placard close to the fuel quantity gauge, in accordance with the Accomplishment Instructions of the Cessna Service Bulletin SB500-28-12 dated 14 June 2004.</span><span> </span><span>In addition to the specifications in the service bulletin, the letters on the placard must be at least 6mm (1/4 inch) tall.</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; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:21.3pt; text-indent:-21.3pt"><span>3.</span><span style="width:12.3pt; text-indent:0pt; display:inline-block"> </span><span>If not previously accomplished, carry out the following actions in accordance with the Accomplishment Instructions of SB500-28-12:</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; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:42.55pt; text-indent:-21.25pt"><span>a.</span><span style="width:12.92pt; text-indent:0pt; display:inline-block"> </span><span>Do a detailed inspection for chafed wiring of the wing fuel boost pumps.</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; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p style="margin-left:42.55pt; text-indent:-21.25pt"><span>b.</span><span style="width:12.25pt; text-indent:0pt; display:inline-block"> </span><span>Modify the wing fuel boost pumps.</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; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span>Note 1</span><span>:</span><span> </span><span>For the purposes of this Directive, a detailed inspection is: "An intensive examination of a specific item, installation or assembly to detect damage, failure or irregularity.</span><span> </span><span>Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate.</span><span> </span><span>Inspection aids such as mirror, magnifying lenses, etc., may be necessary.</span><span> </span><span>Surface cleaning and elaborate procedures may be required.''</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; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top"><p class="Note"><span>Note 2:</span><span> </span><span>Actions required by this Directive may have been previously accomplished in accordance with FAA AD 2006-06-03.</span></p></td></tr></tbody></table>

	4. If as a result of the Requirement 3.a. inspection any discrepancies are detected, accomplish all applicable corrective and other specified actions in accordance with the service bulletin.
	5. Remove the Requirement 1 AFM temporary change and the Requirement 2 placard.
	Later revisions of the above SB(s), approved by the United States Federal Aviation Administration (FAA) as an Alternate Method of Compliance (AMOC) to FAA AD 2006-05-08, are considered acceptable for compliance with the equivalent Requirements of this Directive.
	Note 3: FAA AD 2006-06-03 Amdt 39-14511 refers.
Compliance:	For Requirements 1 and 2 - Within 25 hours time in service (TIS) after the effective date of this Directive.
	For Requirement 3 - Within 300 hours TIS after the effective date of this Directive.
	For Requirement 4 - Before further flight, immediately following the Requirement 3.a. inspection.
	For Requirement 5 - Before further flight after the Requirement 3 inspection and modification are accomplished.
	This Airworthiness Directive becomes effective on 15 June 2007.
Background:	This Directive requires the revision of the AFM to initially prohibit use of the wing fuel boost pumps for defueling under certain conditions and the installation of a placard. The Directive subsequently requires the accomplishment of other specified investigative and corrective actions as necessary. Terminating action for this Directive is the modification of the wing boost pumps together with the removal of the AFM revision and placard.
	The FAA has received a report of a chafed electrical wiring harness, which was arcing inside the fuel tank. This Directive is issued to prevent potential fuel vapour ignition in a fuel tank, which could result in explosion and loss of the aeroplane.

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