AD Amdt-39-10042

[Federal Register Volume 62, Number 103 (Thursday, May 29, 1997)]
[Rules and Regulations]
[Pages 28999-29001]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 97-14076]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 95-CE-34-AD; Amendment 39-10042; AD 97-11-13]
RIN 2120-AA64


Airworthiness Directives; Fairchild Aircraft SA226 and SA227 
Series Airplanes

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule.

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SUMMARY: This amendment adopts a new airworthiness directive (AD) that 
applies to certain Fairchild Aircraft SA226 and SA227 series airplanes. 
This AD requires modifying the electrical power generation system. The 
AD results from reports of both generators going off-line during flight 
on three of the affected airplanes. The actions specified by this AD 
are intended to prevent failure of both generators during critical 
phases of flight (such as night operation or while in icing 
conditions), which could result in loss of control of the airplane.

DATES: Effective July 11, 1997.
    The incorporation by reference of certain publications listed in 
the regulations is approved by the Director of the Federal Register as 
of July 11, 1997.

ADDRESSES: Service information that applies to this AD may be obtained 
from Field Support Engineering, Fairchild Aircraft, P.O. Box 790490, 
San Antonio, Texas 78279-0490; telephone (210) 824-9421; facsimile 
(210) 820-8609. This information may also be examined at the Federal 
Aviation Administration (FAA), Central Region, Office of the Assistant 
Chief Counsel, Attention: Rules Docket No. 95-CE-34-AD, Room 1558, 601 
E. 12th Street, Kansas City, Missouri 64106; or at the Office of the 
Federal Register, 800 North Capitol Street, NW., suite 700, Washington, 
DC.

FOR FURTHER INFORMATION CONTACT: Ms. Ingrid D. Knox, Aerospace 
Engineer, FAA, Airplane Certification Office, 2601 Meacham Boulevard, 
Fort Worth, Texas 76193-0150; telephone (817) 222-5190; facsimile (817) 
222-5960.

SUPPLEMENTARY INFORMATION:

Events Leading to the Issuance of This AD

    A proposal to amend part 39 of the Federal Aviation Regulations (14 
CFR part 39) to include an AD that would apply to certain Fairchild 
Aircraft SA226 and SA227 series airplanes was published in the Federal 
Register as a notice of proposed rulemaking (NPRM) on November 4, 1996 
(61 FR 56642 ). The NPRM proposed to require modifying the electrical 
power generation system. Accomplishment of the proposed modifications 
as specified in the NPRM would be in accordance with the following 
service bulletins, as applicable:

--Fairchild Service Bulletin (SB) 226-24-027, Issued: May 19, 1988, 
Revised: February 22, 1989;
--Fairchild SB 227-24-008, Issued: March 18, 1988, Revised: February 
22, 1989;
--Fairchild SB 226-24-023, Issued: October 25, 1985, Revised: January 
23, 1989;
--Fairchild SB 227-24-005, Issued: October 25, 1985, Revised: January 
23, 1989;
--Fairchild SB 226-24-026, Issued: May 27, 1987;
--Fairchild SB 24-018, Issued: October 22, 1980, Revised: January 7, 
1981;
--Fairchild SB 226-24-031, dated July 27, 1989;
--Fairchild SB 227-24-012, Issued: May 4, 1989, Revised: July 27, 1989.

    The NPRM resulted from reports of both generators going off-line 
during flight on three of the affected airplanes.
    Interested persons have been afforded an opportunity to participate 
in the making of this AD. One comment was received in support of the 
proposed AD and no comments were received regarding the FAA's 
determination of the cost to the public.

The FAA's Determination

    After careful review of all available information related to the 
subject presented above, the FAA has determined that air safety and the 
public interest require the adoption of the rule as proposed except for 
minor editorial corrections. The FAA has determined that these minor 
corrections will not change the meaning of the AD and will not add any 
additional burden upon the public than was already proposed.

Cost Impact

    The FAA estimates that 34 SA226 series airplanes and 206 SA227 
series airplanes in the U.S. registry will be affected by this AD, that 
it will take approximately 80 workhours per SA226 series airplane and 
50 workhours per SA227 series airplane to accomplish the required 
action, and that the average labor rate is approximately $60 an hour. 
Parts cost approximately $12,400 for SA226 series airplanes and $6,000 
for SA227 series airplanes. Based on these figures, the total cost 
impact of this AD on U.S. operators is estimated to be $584,800 for 
SA226 series airplane operators (or $17,200 per airplane) and 
$1,854,000 for SA227 series airplane operators (or $9,000 per 
airplane). This figure is based on the presumption that no owner/
operator of the affected airplanes has accomplished the required 
modifications. Fairchild Aircraft has informed the FAA that no parts 
have been distributed to any affected airplane owner/operator.
    This AD allows 2,000 hours time-in-service (TIS) after the 
effective date of the AD before mandatory accomplishment of the design 
modifications. The average utilization of the fleet for those airplanes 
in commercial commuter service is approximately 25 to 50 hours TIS per 
week. Based on these figures, operators of commuter-class airplanes 
involved in commercial operation will have to accomplish the required 
modification within 24 to 48 calendar months after the effective date 
of the AD. For private owners, who typically operate between 100 to 200 
hours TIS per year, this allows 24 to 48 years before the required 
modification will be mandatory.

Regulatory Flexibility Determination and Analysis

    The Regulatory Flexibility Act of 1980 (RFA) was enacted by 
Congress to

[[Page 29000]]

ensure that small entities are not unnecessarily or disproportionally 
burdened by government regulations. The RFA requires government 
agencies to determine whether rules could have a ``significant economic 
impact on a substantial number of small entities,'' and, in cases where 
they could, conduct a Regulatory Flexibility Analysis in which 
alternatives to the rule are considered. FAA Order 2100.14A, Regulatory 
Flexibility Criteria and Guidance, outlines FAA procedures and criteria 
for complying with the RFA. Small entities are defined as small 
businesses and small not-for-profit organizations that are 
independently owned and operated or airports operated by small 
governmental jurisdictions. A ``substantial number'' is defined as a 
number that is not less than 11 and that is more than one-third of the 
small entities subject to a proposed rule, or any number of small 
entities judged to be substantial by the rulemaking official. A 
``significant economic impact'' is defined by an annualized net 
compliance cost, adjusted for inflation, which is greater than a 
threshold cost level for defined entity types. FAA Order 2100.14A sets 
the size threshold for small entities operating aircraft for hire at 
nine aircraft owned and the annualized cost thresholds at $69,000 for 
scheduled operators and $5,000 for unscheduled operators.
    The FAA has determined that, for four entities (two nonscheduled 
air carriers and two scheduled air carriers), the compliance costs of 
this AD will impose a significant economic impact. Because at least 11 
small entities are not affected, this AD does not affect a 
``substantial number of small entities'' as defined in Order 2100.14A.
    A copy of the full Cost Analysis and Regulatory Flexibility 
Determination for the required action may be examined at the FAA, 
Central Region, Office of the Assistant Chief Counsel, Attention: Rules 
Docket No. 95-CE-34-AD, Room 1558, 601 E. 12th Street, Kansas City, 
Missouri.

Regulatory Impact

    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 copy of the final evaluation prepared for this 
action is contained in the Rules Docket. A copy of it may be obtained 
by contacting the Rules Docket at the location provided under the 
caption ADDRESSES.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, 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 
(AD) to read as follows:

97-11-13  Fairchild Aircraft: Amendment 39-10042; Docket No. 95-CE-
34-AD.

    Applicability: The following model and serial number airplanes, 
certificated in any category:

------------------------------------------------------------------------
              Model                             Serial Nos.             
------------------------------------------------------------------------
SA226-T..........................  T201 through T275 and T277 through   
                                    T291.                               
SA226-T(B).......................  T(B)276 and T(B)292 through T(B)417. 
SA226-AT.........................  AT001 through AT074.                 
SA226-TC.........................  TC201 through TC419.                 
SA227-TT.........................  TT421 through TT541.                 
SA227-AT.........................  AT423 through AT631.                 
SA227-AC.........................  AC406, AC415, AC416, AC420 through   
                                    AC705, and AC707 through AC733.     
------------------------------------------------------------------------

    Note 1: This AD applies to each airplane 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 airplanes that have been modified, 
altered, or repaired so that the performance of the requirements of 
this AD is affected, the owner/operator must request approval for an 
alternative method of compliance in accordance with paragraph (g) of 
this AD. The request should include an assessment of the effect of 
the modification, alteration, or repair on the unsafe condition 
addressed by this AD; and, if the unsafe condition has not been 
eliminated, the request should include specific proposed actions to 
address it.

    Compliance: Required within the next 2,000 hours time-in-service 
after the effective date of this AD, unless already accomplished.
    To prevent failure of both generators during critical phases of 
flight (such as night operation or while in icing conditions), which 
could result in loss of control of the airplane, accomplish the 
following:
    (a) For the model and serial number airplanes presented below, 
replace the existing generator fault transformer wiring with new 
dual conductor shielded wire in accordance with Fairchild Service 
Bulletin (SB) 226-24-027, Issued: May 19, 1988, Revised: February 
22, 1989, or Fairchild SB 227-24-008, Issued: October 25, 1985, 
Revised: January 23, 1989, as applicable.
    (1) Model SA226-T airplanes, serial numbers T201 through T275 
and T277 through T291; Model SA226-T(B) airplanes, serial numbers 
T(B)276 and T(B)292 through T(B)417; Model SA226-AT airplanes, 
serial numbers AT001 through AT074; and Model SA226-TC airplanes, 
serial numbers TC201 through TC419.
    (2) Model SA227-TT airplanes, serial numbers TT421 through 
TT541; Model SA227-AT airplanes, serial numbers AT423 through AT631; 
and Model SA227-AC airplanes, serial numbers AC406, AC415, AC416, 
and AC420 through AC683.
    (b) For the model and serial number airplanes presented below, 
rewire the electrical power generation system to reduce the 
possibility of 325-amp current limiter failure in accordance with 
Fairchild SB 226-24-023, Issued: October 25, 1985, Revised: January 
23, 1989, or Fairchild SB 227-24-005, Issued: October 25, 1985, 
Revised: January 23, 1989, as applicable.
    (1) Model SA226-T airplanes, serial numbers T249 through T275 
and T277 through T291; Model SA226-T(B) airplanes, serial numbers 
T(B)276 and T(B)292 through T(B)417; Model SA226-AT airplanes, 
serial numbers AT025 through AT074; and Model SA226-TC airplanes, 
serial numbers TC209 through TC419.
    (2) Model SA227-TT airplanes, serial numbers TT421 through 
TT541; Models SA227-AT airplanes, serial numbers AT423 through 
AT591; and SA227-AC airplanes, serial numbers AC420 through AC594.
    (c) For Model SA226-T airplanes, serial numbers T249 through 
T275 and T277 through T291; Model SA226-T(B) airplanes, serial 
numbers T(B)276 and T(B)292 through T(B)417; Model SA226-AT 
airplanes, serial numbers AT025 through AT074; and Model SA226-TC 
airplanes, serial numbers TC209 through TC419, modify the voltage 
regulator access panel and install a connector in the wire bundle in 
accordance with Fairchild SB 226-24-026, Issued: May 27, 1987.
    (d) For Model SA226-T airplanes, serial numbers T201 through 
T275 and T277 through T291; Model SA226-T(B) airplanes, serial 
numbers T(B)276 and T(B)292 through T(B)347; Model SA226-AT 
airplanes, serial numbers AT001 through AT074; and Model SA226-TC 
airplanes, serial numbers TC201

[[Page 29001]]

through TC348, install new voltage regulators, reroute certain 
wires, and replace the entire voltage regulator panel assembly in 
accordance with Fairchild SB 24-018, Issued: October 22, 1980, 
Revised: January 7, 1981.
    (e) For the model and serial number airplanes presented below, 
modify the direct current (DC) generator control system so that it 
will operate off its respective generator output in accordance with 
Fairchild SB 226-24-031, dated July 27, 1989, or Fairchild SB 227-
24-012, Issued: May 4, 1989; Revised: July 27, 1989, as applicable. 
This includes removing field current and reset resistors, removing 
the reset and generator relays and associated diodes, installing a 
10-amp generator control circuit breaker to the left-hand and right-
hand essential bus panels, and replacing the 10-amp generator 
control circuit breakers in the left-hand and right-hand wheelwells 
with 15-amp circuit breakers that are wired in series with the 
generator control circuit breakers.
    (1) Model SA226-T airplanes, serial numbers T249 through T275 
and T277 through T291; Model SA226-T(B) airplanes, serial numbers 
T(B)276 and T(B)292 through T(B)417; Model SA226-AT airplanes, 
serial numbers AT025 through AT074; and Model SA226-TC airplanes, 
serial numbers TC209 through TC419.
    (2) Model SA227-TT airplanes, serial numbers TT421 through 
TT541; Model SA227-AT airplanes, serial numbers AT423 through AT695; 
and Model SA227-AC airplanes, serial numbers AC406, AC415, AC416, 
AC420 through AC556, AC558 through AC705, and AC707 through AC733.
    (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 airplane to a location where 
the requirements of this AD can be accomplished.
    (g) An alternative method of compliance or adjustment of the 
compliance time that provides an equivalent level of safety may be 
approved by the Manager, Fort Worth Airplane Certification Office 
(ACO), FAA, 2601 Meacham Boulevard, Fort Worth, Texas 76193-0150. 
The request shall be forwarded through an appropriate FAA 
Maintenance Inspector, who may add comments and then send it to the 
Manager, Fort Worth ACO.

    Note 2: Information concerning the existence of approved 
alternative methods of compliance with this AD, if any, may be 
obtained from the Fort Worth ACO.
    (h) The modifications required by this AD shall be done in 
accordance with the following service bulletins, as applicable:
--Fairchild Service Bulletin 226-24-027, Issued: May 19, 1988, 
Revised: February 22, 1989;
--Fairchild Service Bulletin 227-24-008, Issued: March 18, 1988, 
Revised: February 22, 1989;
--Fairchild Service Bulletin 226-24-023, Issued: October 25, 1985, 
Revised: January 23, 1989;
--Fairchild Service Bulletin 227-24-005, Issued: October 25, 1985, 
Revised: January 23, 1989;
--Fairchild Service Bulletin 226-24-026, Issued: May 27, 1987;
--Fairchild Service Bulletin 24-018, Issued: October 22, 1980, 
Revised: January 7, 1981;
--Fairchild Service Bulletin 226-24-031, dated July 27, 1989; and
--Fairchild Service Bulletin 227-24-012, Issued: May 4, 1989, 
Revised: July 27, 1989.

    This incorporation by reference was approved by the Director of 
the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR 
part 51. Copies may be obtained from Fairchild Aircraft, P.O. Box 
790490, San Antonio, Texas 78279-0490. Copies may be inspected at 
the FAA, Central Region, Office of the Assistant Chief Counsel, Room 
1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of 
the Federal Register, 800 North Capitol Street, NW., suite 700, 
Washington, DC.
    (i) This amendment (39-10042) becomes effective on July 11, 
1997.

    Issued in Kansas City, Missouri, on May 22, 1997.
Henry A. Armstrong,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 97-14076 Filed 5-28-97; 8:45 am]
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