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21 September 2000 IN REPLY,REFER TO: Federal Aviation Administration |
ATTENTION: |
Mr. C. Dale Bleakney |
SUBJECT: |
Cessna/FAA Integral Tank Water Contamination Test Action Plan: 09/20/00 |
Dear Mr. Bleakney: On 20 September 2000, Steve Copeland and Doug Bassett of Cessna's DOA-100129-CE DOA met with As A result of this meeting Cessna is working to revise the plan and incorporate the following items not 6.0 Flight Testing |
Additional Items: |
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Add coordinated flight pushover maneuvers to simulate moderate turbulence for 15 seconds to include |
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Add rough field takeoffs and landings from a minimum 3000' unimproved airport with minimum |
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The auxiliary tank is to be filled to capacity prior to each flight test. |
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A burn limit of 50% capacity will be observed for the auxiliary tank to allow an assured amount of fuel |
Modifications to 13 September 2000 Instructions: |
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The flight test water charge volume determined by saturation testing would remain unchanged, but for |
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The 1 1/2 ball sideslip described in condition C of the Descent and Approach profile will be replaced |
Cessna is working to have all of the latest modifications incorporated into Revision A in FT172R-15, The FAA's expedited review of and concurrence with the above items is hereby requested.
Very Truly Yours,
Mike McClary
cc: Mike Kiesov, Small Aircraft Directorate |
L417-02-00-175 |
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