|This section of the site is devoted to technical
data related to Cessna Skymaster and O-2 aircraft. If you have something
you would like to share, please email
P337H Checklist and Training Book
Contributed by Willem C.J.M. Van Genk CFII-ATP
(Use this material at your own risk. Always follow manufacturer's recommendations.)
P337H Checklist (click for document)
P337H Training Book (click for document)
Airworthiness Concern Sheet for 336/337
flap cable failure
for document. Airworthiness Concern Sheets (ACS) are distributed
to the user community to collect information that may or may not
lead to further action by the FAA, such as Airworthiness Directives
(AD). Your answers to the questions in this document and other comments
are solicited by the FAA. Please comment using the message
thread in the Messages section of the Message Board titled Flap
Cable ACS. The FAA engineer who issued the ACS, as well as Tom Carr
at CPA, will receive and are interested in your comments.
FAA Maintenance Alert on 336/337
for document. The artwork referred to in this document is
missing, but it is the figure from AC43-13 that shows inspecting
the cable by looping to
check for broken strands internal to the cable. DOC and PDF versions
of this section are available below.
Cessna Service Bulletin MEB02-7 Main
Landing Gear Actuator Inspection
This service bulletin is no longer available on this site, see
below for explanation.
We initially received permission to post Service Bulletins on this
site from Cessna's public relations department. A week or so after
we ordered the service bulletin subscription, we received email
from Tom Wakefield, Cessna VP and General Counsel informing us that
the person who gave us permission did not have the authority to
do so, and that we did not have permission to post Cessna's copyrighted
service bulletin material. Accordingly, the material has been removed
from the site. We obviously are disappointed by this decision. We
emailed Mr. Wakefield asking him to reconsider his decision (begged
him, actually), and copied his boss, Russ Meyer, CEO of Cessna.
In that email, we also asked if Cessna would like to provide a statement
for this site, explaining their actions. Mr. Wakefield's response
is shown in quotes below.
"Cessna does not and it does not allow others to post its
service letters and
bulletins on websites. Cessna has a full range of copyrighted service
publications available for owners, including subscriptions to Service
letters and bulletins. Cessna directly distributes such publications
ensure that accurate, correct, and complete service information
to individual owners for their specific aircraft. If you would like
information about Cessna copyrighted service publications, please
Cessna Customer Services, Telephone No. 316/517-5800 or Facsimile
Tom Wakefield (firstname.lastname@example.org)
Mr. Wakefield copied his boss, Russ Meyer, CEO of Cessna, using
this email address (DDrinkwater@cessna.textron.com)
which shows in the email as Russ Meyer (Chairman).
FAA AC 43-13 Acceptable Methods...Aircraft Inspection and Repair
Note: The 43-13 files in this section are
big. Gmas file is 1.4 Mb. First link in list of files contributed
by Bob Cook (control cable inspection) is the same as Gmas document,
but only 435K in PDF format. Other Cook files are as much as 400K.
So if you download these files via a dialup connection, please be
prepared to be patient...
to FAA web site with entire Advisory Circular
Contributed by Gmas
version of cable inspection and repair section
FAA document contributed by Gmas
||PDF versions of various section of AC 43-13
FAA documents converted and contributed by Bob Cook
and maintenance of landing gear
Human factors as they
relate to maintenance
Shadin Digiflo Fuel Flow Indicator Wiring Diagrams
Shadin documents scanned and contributed by Rick
Sorry, these scans are not the best resolution.
||Page 1, Page
2, Page 3, Page
Mitchell Instrument Cluster
Replacement in 1967 C337
Contributed by Jim Stack.
Description of instrument cluster (oil pressure, temp, fuel qty,
etc.) replacement on C337. From the FAA 337 form. 337 available
from FAA records, but cannot be provided here.
Description (Word document) This is a 10
MB file, it may take some time to download or open, depending on your
System Schematic (PCX format).
||Cluster Schematic (PCX
||Cluster Shematic (Visio
format). Same as PCX drawing above.