[Federal Register Volume 63, Number 111 (Wednesday, June 10, 1998)]
[Rules and Regulations]
[Pages 31616-31617]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-15443]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 98-SW-04-AD; Amendment 39-10583; AD 98-12-29]
RIN 2120-AA64
Airworthiness Directives; Lucas Air Equipment Electric Hoists
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
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SUMMARY: This amendment adopts a new airworthiness directive (AD),
applicable to Lucas Air Equipment electric hoists (hoists) installed
on, but not limited to, all models of Eurocopter France SA-360 and SA-
365 helicopters that requires visually inspecting the cable for damage
before the next hoist operation, blanking (plugging) the electronic
control box upper vent, and performing an end-of-travel procedure
before each hoist operation. This amendment is prompted by several
incidents of cable failures caused by dynamic overload on the winding-
up limit due to uncontrolled excessive speed of the cable, which is
normally regulated by the automatic speed-reducing mechanism or the
operator. The actions specified by this AD are intended to prevent
breaking of the cable, which could become entangled with a main rotor
or tail rotor blade, and result in damage or separation of a rotor
blade, and subsequent loss of control of the helicopter.
EFFECTIVE DATE: July 15, 1998.
FOR FURTHER INFORMATION CONTACT: Mr. Carroll Wright, Aerospace
Engineer, FAA, Rotorcraft Directorate, Rotorcraft Standards Staff, 2601
Meacham Blvd., Fort Worth, Texas 76137, phone (817) 222-5120, fax (817)
222-5961.
SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) to include an airworthiness
directive (AD) that is applicable to Lucas Air Equipment hoists
installed on, but not limited to, all models of Eurocopter France SA-
360 and SA-365 helicopters was published in the Federal Register on
April 10, 1998 (63 FR 17738). That action proposed to require visually
inspecting the cable for damage before the next hoist operation,
plugging the electronic control box upper vent, and performing an end-
of-travel procedure before each hoist operation.
Interested persons have been afforded an opportunity to participate
in the making of this amendment. No
[[Page 31617]]
comments were received on the proposal or the FAA's determination of
the cost to the public. The FAA has determined that air safety and the
public interest require the adoption of the rule as proposed except for
an editorial change in the ``Applicability'' section of the AD where
the word ``and'' has been changed to ``or.'' The FAA has determined
that this change will neither increase the economic burden on an
operator nor increase the scope of the AD.
The FAA estimates that 1 helicopter of U.S. registry will be
affected by this proposed AD, that it will take approximately 2 work
hours per helicopter to accomplish the proposed actions, and that the
average labor rate is $60 per work hour. Required parts will cost
approximately $775. Based on these figures, the total cost impact of
the AD on U.S. operators is estimated to be $895 to replace the hoist
and electronic control box.
The regulations adopted herein will not have substantial direct
effects on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government. Therefore, in
accordance with Executive Order 12612, it is determined that this final
rule does not have sufficient federalism implications to warrant the
preparation of a Federalism Assessment.
For the reasons discussed above, I certify that this action (1) is
not a ``significant regulatory action'' under Executive Order 12866;
(2) is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979); and (3) will not have a
significant economic impact, positive or negative, on a substantial
number of small entities under the criteria of the Regulatory
Flexibility Act. A final evaluation has been prepared for this action
and it is contained in the Rules Docket. A copy of it may be obtained
from the Rules Docket at the FAA, Office of the Regional Counsel,
Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas
76137.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety. Adoption of
the Amendment.
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration amends part 39 of
the Federal Aviation Regulations (14 CFR part 39) as follows:
PART 39--AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
2. Section 39.13 is amended by adding a new airworthiness directive
to read as follows:
AD 98-12-29 Lucas Air Equipment: Amendment 39-10583. Docket No. 98-
SW-04-AD.
Applicability: Electric hoists, part numbers (P/N) 76375-030,
76375-130, 76378, or 76378-100, equipped with electronic control
boxes, P/N 61148-001, 002, or 006, installed on, but not limited to
all models of Eurocopter France SA-360 and SA-365 helicopters,
certificated in any category.
Note 1: This AD applies to each electric hoist (hoist) equipped
with an electronic control box (control box) identified in the
preceding applicability provision, regardless of whether it has been
modified, altered, or repaired in the area subject to the
requirements of this AD. For hoists that have been modified,
altered, or repaired so that the performance of the requirements of
this AD is affected, the owner/operator must use the authority
provided in paragraph (e) to request approval from the FAA. This
approval may address either no action, if the current configuration
eliminates the unsafe condition, or different actions necessary to
address the unsafe condition described in this AD. Such a request
should include an assessment of the effect of the changed
configuration on the unsafe condition addressed by this AD. In no
case does the presence of any modification, alteration, or repair
remove any hoist or control box from the applicability of this AD.
Compliance: Required as indicated, unless accomplished
previously.
To prevent breaking of the cable, which could become entangled
with a main rotor or tail rotor blade, and result in damage or
separation of a rotor blade, and subsequent loss of control of the
helicopter, accomplish the following:
(a) Before the next hoist operation, visually inspect the cable
for damage in accordance with the applicable maintenance manual, and
blank (plug) the electronic control box upper vent with a potting
compound. If the control box has only one vent, install it with the
vent hole in the lowest position.
(b) Apply red paint to the hoist cable starting at 0.8 meter (m)
and extending to the 3m point (31.5 inches to 118 inches) from the
upper plate of the hook assembly.
Note 2: Lucas Air Equipment Service Telex 61148-25-CW-01,
Revision 01, dated April 26, 1994, pertains to the subject of this
AD.
(c) Thereafter, before each hoist operation, perform the end-of-
travel procedure as follows:
(1) With approximately 3m of cable remaining before the hook
assembly reaches the up-limit switch operating lever (upper end of
red-painted cable), reduce the cable speed to approximately one-
third of the normal speed with the control knob. Release the control
knob to the neutral position to stop the hook at a distance
approximately 0.8m from the hoist up-limit switch operating lever
(lower end of red-painted cable). Continue controlling the cable
speed by exclusive use of the control on the pendant, making short
and repetitive inputs until the hook reaches a position with 5 to 10
centimeters (2 to 4 inches) between the upper plate of the hook
assembly and the up-limit switch operating lever. After stopping the
cable at that point, place the hook against the up-limit switch
operating lever. The procedure required by this paragraph may be
accomplished by an owner/operator (pilot) holding at least a private
pilot certificate, and must be entered into the aircraft records
showing compliance with this paragraph in accordance with sections
43.11 and 91.417(a)(2)(v) of the Federal Aviation Regulations.
(2) If the hook comes fully home at an uncontrolled speed, or
the hoist exhibits uncontrolled speed variation or absence of
automatic speed reduction, remove the hoist assembly (hoist and
control box) and replace it with an airworthy hoist assembly before
any further hoist operation.
(d) Installation of an electronic control box, P/N 61148-016 or
P/N 61148-012, as applicable, with installation of a hoist, P/N
76375-060, 76375-160, 76378-060, or 76378-160, is a terminating
action for the requirements of this AD.
(e) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be
used if approved by the Manager, Rotorcraft Standards Staff,
Rotorcraft Directorate, FAA. Operators shall submit their requests
through an FAA Principal Maintenance Inspector, who may concur or
comment and then send it to the Manager, Rotorcraft Standards Staff.
Note 3: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Rotorcraft Standards Staff.
(f) Special flight permits may be issued in accordance with
sections 21.197 and 21.199 of the Federal Aviation Regulations (14
CFR 21.197 and 21.199) to operate the helicopter to a location where
the requirements of this AD can be accomplished.
(g) This amendment becomes effective on July 15, 1998.
Note 4: The subject of this AD is addressed in Direction
Generale De L'Aviation Civile (France) AD 94-116(AB)R1, dated May
21, 1997.
Issued in Fort Worth, Texas, on June 3, 1998.
Larry M. Kelly,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 98-15443 Filed 6-9-98; 8:45 am]
BILLING CODE 4910-13-U