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Airworthiness Directives
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Amendment 39-4249; AD 81-12-06 R1
Airworthiness Directives; BENDIX: Applies to Bendix Engine Products Division D-3000 and D-3200 (Blue) series magnetos
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Regulatory Information
81-12-06 R1 BENDIX: Amendment 39-4249. Applies to Bendix
Engine Products Division D-3000 and D-3200 (Blue) series magnetos identified
as follows, unless previously identified by the letter "X", on the upper
left area of magneto data plate:
a. D-3000 series (see models specified under "MAGNETO IDENTIFICATION")
pressurized (dark blue) magnetos with serial numbers below 1423, installed
on AVCO Lycoming TIO, LTIO-540-J2BD engines.
MAGNETO IDENTIFICATION |
| |
MODEL | PART NO. |
D6LN-3200 | 10-682910-13 |
D6RN-3200 | 10-682910-18 |
These magnetos are installed on but not limited to the following aircraft engines or aircraft engine/aircraft combinations:
AVCO LYCOMING ENGINES | AIRCRAFT INSTALLATIONS |
TIO-540-J2BD | Piper PA-31-350; |
LTIO-540-J2BD | STC SA1151SO
and SA970SO Colemill conversion of Piper PA-31, PA-31-325 and PA-31-350;
STC SA980NW Machen Industries conversion of Piper Aerostar 600 STC SA762NW
Machen Industries conversion of Beechcraft Bonanza B35 and A36 series. |
To detect loose distributor gear rotating electrodes on magnetos having
100 hours or more in service since new or overhaul, accomplish paragraph
c, before further flight, unless previously accomplished, and every 50 hours
in service thereafter until the gears are replaced with laser welded gear
assemblies identified by the presence of the letter "Z" or the letters "XO"
on the retaining ring end of the gear axle.
b. All D-3000 and D-3200 series (blue) magnetos with serial numbers
100 through 1968 not covered by paragraph a, unless previously accomplished.
To detect loose distributor gear rotating electrodes on magnetos having
100 hours or more in service since new or overhaul, accomplish paragraph
c, before the expiration of 50 hours in service since new or overhaul after
the effective date of this AD unless previously accomplished and every 50
hours in service thereafter until the gears are replaced with laser welded
gear assemblies identified by the presence of the letter "Z" or the letters
"XO" on the retaining ring end of the gear axle or the letter "L", stamped
on the distributor gear electrode.
c. 1. Remove the distributor block from the magneto and the gears from the block.
2. (A). Inspect distributor gears and block for the presence of bronze
colored particles and for indications of metal to metal contact of electrodes.
(B). Inspect rotating electrode for looseness by holding the gear
in one hand while attempting to move the distributor gear electrode relative
to the axle, clock-wise and vertically. Any looseness of the rotating electrode
is reason for rejection of distributor gear.
3. If the distributor block is contaminated with brass filings or bronze colored dust, inspect the engine as follows:
(A). Observe engine pistons through spark plug hole for evidence of burning.
(B). Check valve dry tappet clearance per engine manufacturer's instructions.
If piston damage or lower than specified dry tappet clearance is present,
the engine must be inspected, in accordance with the engine manufacturer's
instructions, for continued airworthiness.
4. Reinstall serviceable distributor gears into a clean serviceable
distributor block. Reassemble the magneto and check timing as appropriate.
5. (A). Make an engine log entry of compliance, including magneto serial number.
(B). When the laser beam welded distributor gear has been installed
in a D-3000 or D-3200 series magneto, identify that magneto by metal stamping
the letter "X", on the upper left area of magneto data plate and make the
appropriate log entry.
Equivalent inspections and procedures must be approved by the Chief
of the Engineering and Manufacturing Branch, AEA-210, Federal Aviation Administration
(FAA) Eastern Region. As permitted by FAR 21.197, aircraft may be flown
to a base where maintenance required by this AD can be accomplished.
(Bendix Service Bulletins 618 and 619 pertain to paragraphs a and b respectively.)
This Airworthiness Directive is effective November 12, 1981, and paragraph
a. was effective upon receipt for all recipients of airmail letter dated
June 5, 1981, which covered that subject.
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