AD 2008-16-02

[Federal Register Volume 73, Number 147 (Wednesday, July 30, 2008)]
[Rules and Regulations]
[Pages 44142-44145]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: E8-17329]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-0353; Directorate Identifier 2007-CE-101-AD; 
Amendment 39-15620; AD 2008-16-02]
RIN 2120-AA64


Airworthiness Directives; Hawker Beechcraft Corporation Model 390 
Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for certain 
Hawker Beechcraft Corporation Model 390 airplanes. This AD requires you 
to repetitively do a post-flight check (owner/operator holding at least 
a private pilot certificate checking for residual heat in the angle-of-
attack (AOA) probes or an appropriately-rated mechanic doing a 
maintenance manual operational test of the heat of the AOA probes) 
after every flight and replace or modify (upload software) the stall 
warning AOA transmitters. This AD results from reports of the potential 
for unannunciated loss of the heating function in the left-hand (LH) 
and right-hand (RH) stall warning AOA transmitters of Model 390 
airplanes. We are issuing this AD to correct potentially inadequate 
stall warning with loss of stick pusher function.

DATES: This AD becomes effective on September 3, 2008.
    On September 3, 2008, the Director of the Federal Register approved 
the incorporation by reference of certain publications listed in this 
AD.

ADDRESSES: For service information identified in this AD, contact 
Hawker Beechcraft Corporation, 9709 East Central, Wichita, Kansas 
67291; telephone: (800) 429-5372 or (316) 676-3140.
    To view the AD docket, go to U.S. Department of Transportation, 
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 
New Jersey Avenue, SE., Washington, DC 20590, or on the Internet at 
<a href="http://www.regulations.gov">http://www.regulations.gov</a>. The docket number is FAA-2008-0353; 
Directorate Identifier 2007-CE-101-AD.

FOR FURTHER INFORMATION CONTACT: Philip Petty, Aerospace Engineer, 
Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, 
Wichita, Kansas 67209; telephone: (316) 946-4139; fax: (316) 946-4107.

[[Page 44143]]


SUPPLEMENTARY INFORMATION:

Discussion

    On March 19, 2008, we issued a proposal to amend part 39 of the 
Federal Aviation Regulations (14 CFR part 39) to include an AD that 
would apply to certain Hawker Beechcraft Corporation Model 390 
airplanes. This proposal was published in the Federal Register as a 
notice of proposed rulemaking (NPRM) on March 25, 2008 (73 FR 15678). 
The NPRM proposed to require you to repetitively do a post-flight check 
(owner/operator holding at least a private pilot certificate checking 
for residual heat in the angle-of-attack (AOA) probes or an 
appropriately-rated mechanic doing a maintenance manual operational 
test of the heat of the AOA probes) after every flight and replace or 
modify (upload software) the stall warning AOA transmitters.

Comments

    We provided the public the opportunity to participate in developing 
this AD. We received no comments on the proposal or on the 
determination of the cost to the public.

Conclusion

    We have carefully reviewed the available data and determined that 
air safety and the public interest require adopting the AD as proposed 
except for minor editorial corrections. We have determined that these 
minor corrections:
    <bullet> Are consistent with the intent that was proposed in the 
NPRM for correcting the unsafe condition; and
    <bullet> Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Costs of Compliance

    We estimate that this AD affects 152 airplanes in the U.S. 
registry.
    We estimate the following costs to incorporate and remove the 
temporary change to the AFM.

------------------------------------------------------------------------
                                                         Total cost per
            Labor cost                  Parts cost          airplane
------------------------------------------------------------------------
0.5 work-hour x $80 per hour =     Not Applicable.....               $40
 $40.
------------------------------------------------------------------------

    We estimate that the post-flight residual heat check requires about 
3 minutes to do. We estimate the following costs to do 10 of the post-
flight residual heat checks. We have no way of determining the number 
of airplanes that would have this post-flight residual heat check, or 
how many times this will need to be performed before the terminating 
action is done:

------------------------------------------------------------------------
 Labor cost to do 10 post-flight                         Total cost per
       residual heat checks             Parts cost          airplane
------------------------------------------------------------------------
0.5 work-hour x $80 per hour =     Not Applicable.....               $40
 $40.
------------------------------------------------------------------------

    We estimate the following costs to do the maintenance manual 
operational test of the heat of the AOA probes. We have no way of 
determining the number of airplanes that would have this operational 
test, or how many times this will need to be performed before the 
terminating action is done:

------------------------------------------------------------------------
                                                         Total cost per
            Labor cost                  Parts cost          airplane
------------------------------------------------------------------------
0.5 work-hour x $80 per hour =     Not Applicable.....               $40
 $40.
------------------------------------------------------------------------

    We estimate the following costs to do any upload of software to the 
AOA transmitters. We have no way of determining the number of airplanes 
that would have this modification:

------------------------------------------------------------------------
                                                         Total cost per
            Labor cost                  Parts cost          airplane
------------------------------------------------------------------------
4 work-hours x $80 per hour =      Not Applicable.....              $320
 $320.
------------------------------------------------------------------------

    We estimate the following costs to do any replacement of 2 stall 
warning AOA transmitters. We have no way of determining the number of 
airplanes that would have this replacement:

------------------------------------------------------------------------
                                                         Total cost per
            Labor cost                  Parts cost          airplane
------------------------------------------------------------------------
2 work-hours x $80 per hour =      $18,600............           $18,760
 $160.
------------------------------------------------------------------------

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to 
issue rules on aviation safety. Subtitle I, Section 106 describes the 
authority of the FAA Administrator. Subtitle VII, Aviation Programs, 
describes in more detail the scope of the agency's authority.
    We are issuing this rulemaking under the authority described in 
Subtitle VII,

[[Page 44144]]

Part A, Subpart III, Section 44701, ``General requirements.'' Under 
that section, Congress charges the FAA with promoting safe flight of 
civil aircraft in air commerce by prescribing regulations for 
practices, methods, and procedures the Administrator finds necessary 
for safety in air commerce. This regulation is within the scope of that 
authority because it addresses an unsafe condition that is likely to 
exist or develop on products identified in this AD.

Regulatory Findings

    We have determined that this AD will not have federalism 
implications under Executive Order 13132. This AD will not have a 
substantial direct effect 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.
    For the reasons discussed above, I certify that this AD:
    1. Is not a ``significant regulatory action'' under Executive Order 
12866;
    2. Is not a ``significant rule'' under the 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.
    We prepared a summary of the costs to comply with this AD (and 
other information as included in the Regulatory Evaluation) and placed 
it in the AD Docket. You may get a copy of this summary by sending a 
request to us at the address listed under ADDRESSES. Include ``Docket 
No. FAA-2008-0353; Directorate Identifier 2007-CE-101-AD'' in your 
request.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

0
Accordingly, under 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

0
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]

0
2. FAA amends Sec.  39.13 by adding the following new AD:

2008-16-02 Hawker Beechcraft Corporation: Amendment 39-15620; Docket 
No. FAA-2008-0353; Directorate Identifier 2007-CE-101-AD.

Effective Date

    (a) This AD becomes effective on September 3, 2008.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Model 390 airplanes, serial numbers RB-4 
through RB-204, that are certificated in any category.

Unsafe Condition

    (d) This AD results from reports of the potential for 
unannunciated loss of the heating function in the left-hand (LH) and 
right-hand (RH) stall warning angle-of-attack (AOA) transmitters of 
Model 390 airplanes. We are issuing this AD to correct potentially 
inadequate stall warning with loss of stick pusher function.

Compliance

    (e) To address this problem, you must do the following, unless 
already done:

----------------------------------------------------------------------------------------------------------------
               Actions                             Compliance                            Procedures
----------------------------------------------------------------------------------------------------------------
(1) Incorporate Raytheon Aircraft     Within 15 hours time-in-service       Not Applicable.
 Company Temporary Change to the FAA   (TIS) after September 3, 2008 (the
 Approved Airplane Flight Manual P/N   effective date of the AD) or within
 390-590001-0003CTC7, issued: March    30 days after September 3, 2008
 15, 2007, into the airplane flight    (the effective date of the AD),
 manual (AFM).                         whichever occurs first.
(2) After every flight do the         Begin the post-flight checks within   (A) For the post-flight check for
 following:                            15 hours TIS after September 3,       residual heat in the AOA probes:
(i) Do a post-flight check for         2008 (the effective date of the AD)   Follow Raytheon Aircraft Company
 residual heat in the AOA probes.      or within 30 days after September     Temporary Change to the FAA
 CAUTION: TO PREVENT POSSIBLE BURNS,   3, 2008 (the effective date of the    Approved Airplane Flight Manual
 USE EXTREME CAUTION TOUCHING HEATED   AD), whichever occurs first.          Temporary Change P/N 390-590001-
 AREAS. TO CHECK HEATING AND AVOID     Completion of paragraph (e)(3)(i)     0003CTC7, issued: March 15, 2007.
 BURNS, HOLD HAND NEAR HEATED AREA     or (e)(3)(ii) of this AD terminates   The owner/operator holding at least
 OR MOVE HAND GRADUALLY FROM AMBIENT   the required repetitive post-flight   a private pilot certificate as
 AREA TOWARD HEATED AREA UNTIL         checks of this AD. Replace any AOA    authorized by section 43.7 of the
 WARMTH CAN BE FELT. If you do not     probe that fails the operational      Federal Aviation Regulations (14
 feel heat in the AOA probes, then     test before further flight.           CFR 43.7) may do this post-flight
 do paragraph (e)(2)(ii) of this AD;                                         check required by paragraph
 or                                                                          (e)(2)(i) of this AD. Make an entry
(ii) Do a post-flight maintenance                                            into the aircraft records showing
 manual operational test of the heat                                         compliance with this AD following
 of the AOA probes. If the AOA probe                                         section 43.9 of the Federal
 fails the operational test, replace                                         Aviation Regulations (14 CFR 43.9).
 the AOA probe.                                                             (B) For the post-flight maintenance
                                                                             manual operational test of the heat
                                                                             of the AOA probes: Follow Raytheon
                                                                             Aircraft Company Temporary Change
                                                                             to the FAA Approved Airplane Flight
                                                                             Manual Temporary Change P/N 390-
                                                                             590001-0003CTC7, issued: March 15,
                                                                             2007, and Hawker Beechcraft
                                                                             Mandatory Service Bulletin No. SB
                                                                             27-3787, issued: May 2007. The
                                                                             maintenance manual operational test
                                                                             must be done by an appropriately
                                                                             rated mechanic.
                                      ....................................  (C) For AOA probe replacement:
                                                                             Follow Hawker Beechcraft Mandatory
                                                                             Service Bulletin No. SB 27-3787,
                                                                             issued: May 2007.

[[Page 44145]]

 
(3) Replace or modify (upload         Within 250 hours TIS after September  Follow Hawker Beechcraft Mandatory
 software) the stall warning AOA       3, 2008 (the effective date of this   Service Bulletin No. SB 27-3787,
 transmitters by doing one of the      AD) or within 12 months after         issued: May 2007.
 following:                            September 3, 2008 (the effective
(i) Upload new software Kit No. 123-   date of this AD), whichever occurs
 3436 (Field Software Upload SLZ8060-  first.
 3,-4) to the AOA transmitters; or    Completion of either paragraph
(ii) Replace any part number (P/N)     (e)(3)(i) or (e)(3)(ii) of this AD
 SLZ8060-3 and/or P/N SLZ8060-4 AOA    terminates the required repetitive
 transmitters with new P/N SLZ8060-5   post-flight check of this AD.
 AOA transmitters.
(4) Remove Raytheon Aircraft Company  Before further flight after doing     Follow Hawker Beechcraft Mandatory
 Temporary Change to the FAA           the actions required by paragraph     Service Bulletin No. SB 27-3787,
 Approved Airplane Flight Manual P/N   (e)(3)(i) or paragraph (e)(3)(ii)     issued: May 2007.
 390-590001-0003CTC7, issued: March    of this AD.
 15, 2007, from the AFM.
(5) Do not install any P/N SLZ8060-3  As of September 3, 2008 (the          Not Applicable.
 or P/N SLZ8060-4 AOA transmitter      effective date of this AD).
 that does not have the new upgraded
 software required by paragraph
 (e)(3)(i) of this AD.
----------------------------------------------------------------------------------------------------------------

Alternative Methods of Compliance (AMOCs)

    (f) The Manager, Wichita Aircraft Certification Office (ACO), 
FAA, has the authority to approve AMOCs for this AD, if requested 
using the procedures found in 14 CFR 39.19. Send information to 
ATTN: Philip Petty, Aerospace Engineer, Wichita ACO, 1801 Airport 
Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946-4139; 
fax: (316) 946-4107. Before using any approved AMOC on any airplane 
to which the AMOC applies, notify your appropriate principal 
inspector (PI) in the FAA Flight Standards District Office (FSDO), 
or lacking a PI, your local FSDO.

Material Incorporated by Reference

    (g) You must use Raytheon Aircraft Company Temporary Change to 
the FAA Approved Airplane Flight Manual P/N 390-590001-0003CTC7, 
issued: March 15, 2007, and Hawker Beechcraft Mandatory Service 
Bulletin No. SB 27-3787, issued: May 2007, to do the actions 
required by this AD, unless the AD specifies otherwise.
    (1) The Director of the Federal Register approved the 
incorporation by reference of this service information under 5 
U.S.C. 552(a) and 1 CFR part 51.
    (2) For service information identified in this AD, contact 
Hawker Beechcraft Corporation, 9709 East Central, Wichita, Kansas 
67291; telephone: (800) 429-5372 or (316) 676-3140.
    (3) You may review copies at the FAA, Central Region, Office of 
the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; or at 
the National Archives and Records Administration (NARA). For 
information on the availability of this material at NARA, call 202-
741-6030, or go to: <a href="http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html">http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html</a>.

    Issued in Kansas City, Missouri, on July 23, 2008.
John Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E8-17329 Filed 7-29-08; 8:45 am]
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