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RECORD OF |
VISIT |
TIME |
DATE: |
NAME(S) OF PERSON(S) CONTACTED OR IN CONFERENCE AND LOCATION |
Robert Cunningham-PMI, Orlando FSDO |
Bill Allen-MTSU Aerospace Facilities Manager |
Paul Jones-SPM, Nashville FSDO, Craig Roberts-ASI, Nashville FSDO |
SUBJECT |
DIGEST |
N52749 of Robert Scovill to determine the egress capability of water in the integral wing fuel tanks. This aircraft |
has Cessna Service Kit SK182-100 installed incorporating 4 additional sump drains in each wing. |
The aircraft was leveled in accordance with the Cessna service manual. The top three access panels are removed |
and 32 ounces of dyed water was introduced through the openings of each wing. |
After 5 minutes, the wings were sumped with the following results: |
|
Left wing |
Right wing |
|
original factory sump |
clear |
clear |
|
aft middle sump |
clear |
clear |
|
aft outboard sump |
negligible |
negligible |
|
forward outboard sump |
clear |
clear |
|
forward inboard sump |
clear |
clear |
|
An additional 20 ounces were introduced into each fuel filer port and the wings were again sumped. No water |
was found in any sample from all 10 sump drains. A total of 52 ounces of water remained in each wing. |
The aircraft was rocked by its wings for 30 seconds and sumped again with the following results. |
|
Left wing |
Right wing |
|
original factory sump |
Clear |
Clear |
|
aft middle sump |
Clear |
Clear |
|
aft outboard sump |
Clear |
Clear |
|
forward outboard sump |
Clear |
Clear |
|
forward inboard sump |
29 ozs. |
18.5 ozs. |
|
|
|
|
|
Water remaining in wing |
23 ozs. |
33.5 ozs. |
|
DATE |
TITLE |
SIGNATURE |
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