Lateral Mixer Assemblies Found Cracked
Editor's Note: MD
Helicopters, Inc. (MDHI) told ANN this weekend it has been working
closely with the FAA Rotorcraft Directorate to identify and resolve
a discovered issue with the lateral mixer on the MD600N helicopter.
MDHI states it worked closely with the FAA to initiate an emergency
airworthiness directive for this issue, presented unedited
below.
The requirements of the AD are interim actions, in response
to the MDHI Service Bulletin SB600N-044 Lateral Mixer Output Link
Assembly, One Time Inspection, issued February 16.
DATE: February 17, 2007
AD#: 2007-05-51
This Emergency Airworthiness Directive (AD) is prompted by the
discovery of a cracked lateral mixer output link assembly (mixer
link), part number (P/N) 600N7636-1, on an in-service MDHI Model
MD600N helicopter. Cracks were also found on two additional mixer
links, P/N 600N7636-3, which were being held as spares. The cracks
on all three mixer links run through the bearing end area of the
mixer link and emanate from staking marks in the mixer link. Cracks
in the mixer link, if not detected, could result in failure of the
mixer link and subsequent loss of control of the helicopter. The
requirements of this AD are interim actions; the manufacturer
continues to investigate the cause of the cracks and, based on that
investigation, we will determine either follow-on actions or a
terminating action for the requirements of this AD.
The FAA has reviewed MDHI Service Bulletin No. SB600N-044, dated
February 16, 2007 (SB), which describes procedures for a one-time
visual inspection and an eddy current inspection of the mixer link.
The SB includes only P/Ns 600N7636-1, and -3 in its effectivity,
however, because the exact cause of the cracks is unknown, and the
-9 and -11 are similar designs, we have included them in the
applicability of this AD. We are also requiring an eddy current
inspection of each affected mixer link before installing it on any
helicopter.
A one-time flight permit is allowed for flying the helicopter to
an approved maintenance facility to perform the eddy current
inspection, provided that no crack is found during the visual
inspection required in paragraph (a) of this AD and that the
helicopter’s airspeed does not exceed 100 knots. This unsafe
condition is likely to exist or develop on other helicopters of the
same type design. Therefore, this AD requires, before further
flight, the following for each mixer link, P/N 600N7636-1, -3, -9,
and -11:
Removing each mixer link, and visually inspecting, with a bright
light and a 10x or higher magnifying glass, the shaded areas on
both sides around the bearing bore for any crack; and Performing an
eddy current inspection of each mixer link in the bearing end
areas. Replacing any cracked mixer link with an airworthy mixer
link on which an eddy current inspection has been performed.
This AD also requires
performing an eddy current inspection on each mixer link before
installing it on any helicopter.
This rule is issued under 49 U.S.C. Section 44701 pursuant to
the authority delegated to me by the Administrator, and is
effective immediately upon receipt of this emergency AD. 2007-05-51
MD Helicopters Inc. (MDHI): Directorate Identifier
2007-SW-05-AD.
Applicability: Model MD600N helicopters, with a
lateral mixer output link assembly (mixer link), part number (P/N)
600N7636-1, -3, -9, or -11 installed, certificated in any category.
Compliance: Required as indicated, unless accomplished
previously.
To detect a crack in the mixer link, which could result in
failure of the mixer link and subsequent loss of control of the
helicopter, accomplish the following:
- Before further flight:
-
- Remove each mixer link and visually inspect, with a bright
light and a 10x or higher magnifying glass, the shaded areas around
the bearing bore for any crack as depicted in the following
- Perform an eddy current inspection of each mixer link in the
bearing end areas.
- Replace any cracked mixer link with an airworthy mixer link on
which an eddy current inspection has been performed.
-
- Note: MDHI Service Bulletin No. SB600N-044,
dated February 16, 2007, pertains to the subject of this AD.
- Perform an eddy current inspection on each mixer link before
installing it on any helicopter.
- To request a different method of compliance or a different
compliance time for this AD, follow the procedures in 14 CFR 39.19.
Contact the Manager, Los Angeles Aircraft Certification Office,
FAA, ATTN: Jon Mowery, Aviation Safety Engineer, Airframe Branch,
3960 Paramount Blvd., Lakewood, California 90712, telephone (562)
627-5322, fax (562) 627-5210, for information about previously
approved alternative methods of compliance.
- A one-time special flight permit may be issued in accordance
with 14 CFR 21.197 and 21.199 to operate the helicopter to a
location where the eddy current inspection requirements of this AD
can be accomplished provided that no crack is found during the
visual inspection required in paragraph (a) of this AD and that the
helicopter’s airspeed does not exceed 100 knots.
- Copies of the applicable service information may be obtained
from MD Helicopters Inc. Attn: Customer Support Division, 4555 E.
McDowell Rd., Mail Stop M615, Mesa, Arizona 85215-9734, telephone
1-800-388-3378, fax 480-346-6813, or on the web at www.mdhelicopters.com.
- Emergency AD 2007-05-51, issued February 17, 2007, becomes
effective upon receipt.