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2014-03-03: Placards and Markings

FAA order 2014-03-03 is an airworthiness directive in force since April 7, 2014. The FAA's subject line: Placards and Markings. It names Cessna 310, Cessna 320, Cessna 340, Cessna 401, Cessna 402, Cessna 411, Cessna 414 Chancellor, Cessna 421 Golden Eagle: about 3,862 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Cessna Aircraft Company; Textron Aviation Inc.
Models
310, 310A, 310B, 310C, 310D, 310E, 310F, 310G, 310H, 310I, 310J, 310J-1, 310K, 310L, 310N, 310P, 310Q, 310R, 320, 320-1, 320A, 320B, 320C, 320D, 320E, 320F, 340, 340A, 401, 401A, 401B, 402, 402A, 402B, 411, 411A, 414, 421, 421A, 421B
On this site
Cessna 310 1,410 registered
Cessna 320 137 registered
Cessna 340 707 registered
Cessna 401 51 registered
Cessna 402 174 registered
Cessna 411 10 registered
Cessna 414 Chancellor 605 registered
Cessna 421 Golden Eagle 768 registered

Dates and paperwork

In force since
April 7, 2014
Published
March 3, 2014 (signed January 31, 2014)
Docket
FAA-2011-0562
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 310, 320, 340, 401, 402, 411, 414, and 421 airplanes. This AD was prompted by an investigation of recent and historical icing-related accidents and incidents for the products listed above. This AD requires either having the supplemental airplane flight manual/airplane flight manual supplement (SAFM/AFMS) inside the airplane and accessible to the pilot during the airplane's operation or installing a placard that prohibits flight into known icing conditions and installing a placard that increases published airspeed on approach at least 17 mph (15 knots) in case of an inadvertent encounter with icing. We are issuing this AD to correct the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (6,704 characters)
Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 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. The FAA amends Sec. 39.13 by adding an airworthiness directive (AD): 2014-03-03 Cessna Aircraft Company: Amendment 39-17740; Docket No. FAA-2011-0562; Directorate Identifier 2011-CE-015-AD. (a) Effective Date This AD is effective April 7, 2014. (b) Affected ADs None. (c) Applicability This AD applies to Cessna Aircraft Company Models 310, 320, 340, 401, 402, 411, 414, and 421 airplanes identified in Cessna Aircraft Company Service Bulletin MEB97-4, dated March 24, 1997, certificated in any category. (d) Subject Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code: 11, Placards and Markings. (e) Unsafe Condition This AD was prompted by an investigation of recent and historical icing-related accidents and incidents for the products listed above. We are issuing this AD to prohibit flight into known icing conditions as well as increase the approach speed in case of an inadvertent encounter with icing. This condition, if not corrected, could result in unusual flight characteristics that could lead to loss of control after flight into known icing conditions or an inadvertent encounter with icing conditions. Based on the data, an example of the unusual flight characteristics seen in many of the accidents is high sink speeds that resulted in a hard landing. (f) Compliance Comply with the actions specified in paragraphs (g) through (i) of this AD, to [[Page 11689]] include all subparagraphs, unless already done. (g) Incorporate Operational Limitations Within 100 hours time-in-service (TIS) after April 7, 2014 (the effective date of this AD) or within 3 calendar months after April 7, 2014 (the effective date of this AD), whichever occurs first, incorporate the operational limitations by accomplishing either paragraph (g)(1) or (g)(2) of this AD, to include all subparagraphs: (1) Incorporate the limitations identified in Appendix 1 of this AD into your airplane maintenance records and install a copy of the approved supplemental airplane flight manual/airplane flight manual supplement (SAFM/AFMS) in Appendix 1 of this AD in the airplane accessible to the pilot; or (2) Install the following placards: (i) Cessna placard part number (P/N) DP0500-13 or a placard that states: ``This airplane is prohibited from flight into known icing conditions.'' If installing the Cessna placard P/N DP0500-13, obtain the placard following Cessna Aircraft Company Service Bulletin MEB97-4, dated March 24, 1997; and (ii) An additional placard for the applicable airspeed indicator readings listed in paragraph (g)(2)(A) or (g)(2)(B) below, as applicable: (A) If Airspeed Indicator Reads in MPH. Placard states: ``For inadvertent encounters with icing conditions, increase published airspeed on approach at least 17 mph.'' (B) If Airspeed Indicator Reads in Knots. Placard states: ``For inadvertent encounters with icing conditions, increase published airspeed on approach at least 15 KIAS.'' (h) Placard Installation Install the placards on the instrument panel in clear view of the pilot using 1/8-inch black lettering on a white background. (i) Pilot Authorization In addition to the provisions of 14 CFR 43.3 and 43.7, the actions required by paragraphs (g)(1) and (g)(2) of this AD, to include all subparagraphs, may be performed by the owner/operator (pilot) holding at least a private pilot certificate and must be entered into the airplane records showing compliance with this AD in accordance with 14 CFR 43.9 (a)(1)-(4) and 14 CFR 91.417(a)(2)(v). The record must be maintained as required by 14 CFR 91.417. This authority is not applicable to aircraft being operated under 14 CFR part 119. (j) Special Flight Permit Special flight permits are permitted with the following limitation: flight into known icing is prohibited. (k) Alternative Methods of Compliance (AMOCs) (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. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office.(l) Related Information For more information about this AD, contact Dan Withers, Program Manager, FAA, Wichita ACO, 1801 S. Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946-4137; fax: (316) 946-4107; email: [email protected]. (m) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) Cessna Aircraft Company Service Bulletin MEB97-4, dated March 24, 1997. (ii) Reserved. (3) For Cessna Aircraft Company service information identified in this AD, contact Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, KS 67277; telephone: (316) 517-5800; fax: (316) 517-7271; email: [email protected]; Internet: http://www.cessna.com/.(4) You may view this service information at FAA, FAA, Small Airplane Directorate, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (816) 329-4148. (5) You may view this service information that is incorporated by reference 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: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Appendix 1 to Airworthiness Directive 2014-03-03 Supplemental Airplane Flight Manual (SAFM) for Airplanes Without an Approved AFM or Airplane Flight Manual Supplement (AFMS) For Airplanes With an FAA-Approved AFM or POH/AM BILLING CODE 4910-13-P [[Page 11690]] [GRAPHIC] [TIFF OMITTED] TR03MR14.000

Related safety bulletins advice on the same designs, not orders

2015-09-23CE-14-11R1 · Landing Gear; Nose Landing Gear Trunnions
2014-05-30CE-14-19 · Landing Gear; Main Landing Gear (MLG) Torque Link
2014-02-25CE-14-11 · Landing Gear; Nose Landing Gear Trunnions
2013-03-13CE-13-22 · Electrical Power System Circuit Breaker Switch
2011-09-27CE-11-29R1 · Flight Control System

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 26, 2026. Connections as data: /graph/directive/2014-03-03.json · aircraft systems.