AD 2011-06-02

We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires installing a full authority digital engine control (FADEC) backup battery, replacing the supplement pilot's operating handbook and FAA approved airplane flight manual, and replacing the FADEC backup battery every 12 calendar months. This AD was prompted by an incident where an airplane experienced an in-flight engine shutdown caused by a momentary loss of electrical power to the FADEC. We are issuing this AD to prevent interruption of electrical power to the FADEC, which could result in an uncommanded engine shutdown. This failure could lead to a loss of engine power.

Final rule.

Adoption of the Amendment \n\n\n\tAccordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: \n\nPART 39--AIRWORTHINESS DIRECTIVES \n\n0 1. The authority citation for part 39 continues to read as follows: \n\n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701. \n\n\n\nSec. 39.13 (Amended) \n\n0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): \n\n2011-06-02 Cessna Aircraft Company: Amendment 39-16626; Docket No. FAA-2010-1243; Directorate Identifier 2010-CE-058-AD. \n\nEffective Date \n\n\n\t(a) This AD is effective May 26, 2011. \n\nAffected ADs \n\n\n\t(b) None. \n\nApplicability \n\n\n\t(c) This AD applies to all serial numbers of the following airplanes, certified in any category, that are modified by Supplemental Type Certificate (STC) SA01303WI, as identified in Table 1 of this AD: \n\n\n\tTable 1 ------------------------------------------------------------------------ \n\tModelEngine Group ------------------------------------------------------------------------ (1) 172F, 172G, 172H, 172I, 172K, TAE 125-01............ 1 \n\t172L, 172M, F172F, F172G, F172H, \n\tF172K, F172L, and F172M. (2) 172F, 172G, 172H, 172I, 172K, TAE 125-02-99......... 2 \n\t172L, 172M, F172F, F172G, F172H, \n\tF172K, F172L, and F172M. (3) 172N, 172P, F172N, and F172P... TAE 125-01............ 3 (4) 172N, 172P, F172N, and F172P... TAE 125-02-99......... 4 (5) 172R and 172S.................. TAE 125-01............ 5 (6) 172R and 172S.................. TAE 125-02-99......... 6 ------------------------------------------------------------------------ \n\nSubject \n\n\n\t(d) Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 72: Engine. \n\nUnsafe Condition \n\n\n\t(e) This AD was prompted by an incident where an airplane experienced an in-flight engine shutdown caused bya momentary loss of electrical power to the FADEC. We are issuing this AD to prevent interruption of electrical power to the FADEC, which could result in an uncommanded engine shutdown. This failure could lead to a loss of engine power. \n\nCompliance \n\n\n\t(f) Comply with this AD within the compliance times specified, unless already done. \n\n---------------------------------------------------------------------------------------------------------------- \n\tActions Compliance Procedures ---------------------------------------------------------------------------------------------------------------- (1) For all airplanes: Modify the Within the next 100 hours time-in- (i) For groups 1, 3, and 5 \n\tengine electrical system by service after May 26, 2011 (the airplanes: Follow Thielert Aircraft \n\tinstalling a backup battery system effective date of this AD) or Engines GmbH Service Bulletin TM \n\tand associated wiring and within 30 days after May 26, 2011 TAE 601-0007, Revision 8, dated \n\tcircuitry. (the effective date of this AD), October 14, 2010. \n\twhichever occurs first. (ii) For groups 2, 4, and 6 \n\tairplanes: Follow Thielert Aircraft \n\tEngines GmbH Service Bulletin TM \n\tTAE 601-1001 P1, Revision 8, dated \n\tOctober 14, 2010. (2) For all airplanes: Replace the Within 12 calendar months after (i) For groups 1, 3, and 5 \n\tFADEC backup battery. doing the modification required in airplanes: Follow Page 8, Revison \n\tparagraph (f)(1) of this AD and 2, dated October 8, 2010, from \n\trepetitively thereafter within 12 Chapter 24 ''Electrical Power'' \n\tcalendar months after the previous (Chapter 20-AMM-24-01-US) of \n\treplacement. Thielert Aircraft Engines GmbH \n\tSupplement Airplane Maintenance \n\tManual Cessna 172 & Reims F172 TAE \n\t125-01, Doc. No.: AMM-20-01 (US- \n\tVersion) Version: 2/4. \n\t(ii) For groups 2, 4, and 6 \n\tairplanes: Follow page 7, Revision \n\t1, dated October 8, 2010, from \n\tChapter 24 ''Electrical Power'' \n\t(Chapter 20-AMM-24-02-US) of \n\tThielert Aircraft Engines GmbH \n\tSupplement Airplane Maintenance \n\tManual Cessna 172 & Reims F172 \n\tCENTURION 2.0 (TAE 125-02-99), Doc. \n\tNo.: AMM-20-02 (US-Version) \n\tVersion: 1/1. \n\n((Page 22301)) \n\n\n\n(3) For groups 1 and 2 airplanes: Before further flight after doing Not applicable. \n\tIncorporate Thielert Aircraft the modification required in \n\tEngines GmbH ''Supplemental paragraph (f)(1) of this AD. \n\tAirplane Flight Manual or Pilot's \n\tOperating Handbook and FAA Approved \n\tAirplane Flight Manual Supplement \n\t(as applicable) for the Cessna 172 \n\tF, G, H, I, K, L, M, Reims Cessna \n\tF172 F, G, H, K, L, M, Equipped \n\twith TAE 125-01 or TAE 125-02-99 \n\tInstallation,'' Issue 2-1, TAE-Nr.: \n\t20-0310-21042, dated October 4, \n\t2010,into the pilot's operating \n\thandbook. (4) For groups 3 and 4 airplanes: Before further flight after doing Not applicable. \n\tIncorporate Thielert Aircraft the modification required in \n\tEngines GmbH ''Supplemental paragraph (f)(1) of this AD. \n\tAirplane Flight Manual or Pilot's \n\tOperating Handbook and FAA Approved \n\tAirplane Flight Manual Supplement \n\t(as applicable) for the Cessna 172 \n\tN & P, Reims Cessna F172 N & P, \n\tEquipped with TAE 125-01 or TAE 125- \n\t02-99 Installation,'' Issue 2-1, \n\tTAE-Nr.: 20-0310-20042, dated \n\tOctober 4, 2010, into the pilot's \n\toperating handbook. (5) For groups 5 and 6 airplanes: Before further flight after doing Not applicable. \n\tIncorporate Thielert Aircraft the modification required in \n\tEngines GmbH ''Supplemental Pilot's paragraph (f)(1) of this AD. \n\tOperating Handbook and FAA Approved \n\tAirplane Flight Manual Supplement \n\tfor the Cessna 172 R & S, Equipped \n\twith TAE 125-01 or TAE125-02-99 \n\tInstallation,'' Issue 2-1, TAE-Nr.: \n\t20-0310-22042, dated October 4, \n\t2010, into the pilot's operating \n\thandbook. ---------------------------------------------------------------------------------------------------------------- \n\nAlternative Methods of Compliance (AMOCs) \n\n\n\t(g)(1) 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. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the ACO, send it to the attention of the person identified in the Related Information section of this AD. \n\t(2) Before using any approved AMOC, notify your Principal Maintenance Inspector or Principal Avionics Inspector, as appropriate, or lacking a principal inspector, your local Flight Standards District Office. \n\nRelated Information \n\n\n\t(h) For more information about this AD, contact Richard Rejniak, Aerospace Engineer, Wichita ACO, FAA, 1801 Airport Road, Room 100; phone: (316) 946-4128; fax: (316) 946-4107; e-mail: richard.rejniak@faa.gov. \n\nMaterial Incorporated by Reference \n\n\n\t(i) You must use the following information to do the actions required by this AD, unless the AD specifies otherwise: \n\t(1) Thielert Aircraft Engines GmbH Service Bulletin TM TAE 601- 0007, Revision 8, dated October 14, 2010; \n\t(2) Thielert Aircraft Engines GmbH Service Bulletin TM TAE 601- 1001 P1, Revision 8, dated October 14, 2010; \n\t(3) Chapter 24 ''Electrical Power'' (Chapter 20-AMM-24-01-US), Issue 2, Revision No.: 2, dated October 8, 2010, of Thielert Aircraft Engines GmbH Supplement Airplane Maintenance Manual Cessna 172 & Reims F172 TAE 125-01, Doc. No.: AMM-20-01 (US-Version) Version: 2/4; \n\t(4) Chapter 24 ''Electrical Power'' (Chapter 20-AMM-24-02-US), Issue: 1, Rev. No: 1, dated October 8, 2010, of Thielert Aircraft Engines GmbH Supplement Airplane Maintenance Manual Cessna 172 & Reims F172 CENTURION 2.0 (TAE 125-02-99), Doc. No.: AMM-20-02 (US- Version) Version: 1/1; \n\t(5) Thielert Aircraft Engines GmbH ''Supplemental Airplane Flight Manual or Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement (as applicable) for the Cessna 172 F, G, H, I, K, L, M, Reims Cessna F172 F, G, H, K, L, M, Equipped with TAE 125-01 or TAE 125-02-99 Installation,'' Issue 2-1, TAE-Nr.: 20-0310-21042, dated October 4, 2010; and \n\t(6) Thielert Aircraft Engines GmbH ''Supplemental Airplane Flight Manual or Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement (as applicable) for the Cessna 172 N & P, Reims Cessna F172 N & P, Equipped with TAE 125-01 or TAE 125- 02-99 Installation,'' Issue 2-1, TAE-Nr.: 20-0310-20042, dated October 4, 2010; and \n\t(7) Thielert Aircraft Engines GmbH ''Supplemental Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement for the Cessna 172 R & S, Equipped with TAE 125-01 or TAE 125-02-99 Installation,'' Issue 2-1, TAE-Nr.: 20-0310-22042, dated October 4, 2010. \n\t(j) 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. \n \t(1) For service information identified in this AD, contact Thielert Aircraft Engines Service GmbH, Platanenstra(szlig)e 14, D-09350 Lichtenstein, Deutschland; telephone: +49 (37204) 696-1474; fax: +49 (37204) 696-1910; Internet: http://www.thielert.com/.\n\t(2) You may review copies of the service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call 816-329-4148.\n\t(3) You may also review copies of the service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at an NARA facility, call 202-741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

Discussion \n\n\n\tWe issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an airworthiness directive (AD) that would apply to the specified products. That NPRM published in the Federal Register on December 15, 2010 (75 FR 78177). That NPRM proposed to require installing a FADEC backup battery, replacing the supplement pilot's operating handbook and FAA approved airplane flight manual, and replacing the FADEC backup battery every 12 calendar months. \n\nComments \n\n\n\tWe gave the public the opportunity to participate in developing this AD. The following presents the comment received on the proposal and the FAA's response to the comment. \n\nRequest \n\n\n\tRob van den Bosch, Thielert Aircraft Engines GmbH, when referring to the airplane maintenance manual (AMM) and airplane flight manual (AFM) supplement, recommended adding ''or later approved issue or revision.'' The commenter reasoned that future changes to the AMM or AFM would require additional work by the FAA to update the AD. \n\tWe disagree with the recommendation. If we would include such language, it would violate regulation, specifically 1 CFR 51.1, paragraph (f), which states ''Incorporation by reference of a publication is limited to the edition of the publication that is approved. Future amendments or revisions of the publication are not included.''. Service information that we incorporate by reference in an AD is often revised after we issue the AD. We can approve later revisions of service information as an alternative method of compliance (AMOC). \n\tThe FAA is not changing this AD as a result of this comment. \n\nConclusion \n\n\n\tWe reviewed the relevant data, considered the comment received, and determined that air safety and the public interest require adopting the AD as proposed except for minor editorial changes. We have determined that these minor changes: \n\tAre consistent with the intent that was proposed in the NPRM for correcting theunsafe condition; and \n\tDo not add any additional burden upon the public than was already proposed in the NPRM. \n\nCosts of Compliance \n\n\n\tWe estimate that this AD affects 14 airplanes of U.S. registry. \n\tWe estimate the following costs to comply with this AD: \n\n\n\tEstimated Costs ---------------------------------------------------------------------------------------------------------------- \n\tCost per Cost on U.S. \n\tAction Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- For airplanes with a 14-volt battery 24 work-hours x $85 per $820 $2,860 $14,300 \n\tsystem; installation of a 14-volt hour = $2,040. \n\tFADEC backup battery. For airplanes with a 28-volt battery 24 work-hours x $85 per 1,160 3,200 28,800 \n\tsystem; installation of a 28-volt hour =$2,040. \n\tFADEC backup battery. ---------------------------------------------------------------------------------------------------------------- \n\nAuthority for This Rulemaking \n\n\n\tTitle 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. \n\tWe are issuing this rulemaking under the authority described in subtitle VII, 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 rulemaking action. \n\nRegulatory Findings \n\n\n\tThis AD will not have federalism implications under Executive Order 13132. This AD will not have a \n\n((Page 22300)) \n\nsubstantial 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. \n\tFor the reasons discussed above, I certify that this AD: \n\t(1) Is not a ''significant regulatory action'' under Executive Order 12866, \n\t(2) Is not a ''significant rule'' under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), \n\t(3) Will not affect intrastate aviation in Alaska, and \n\t(4) 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. \n\nList of Subjects in 14 CFR Part 39 \n\n\n\tAir transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.