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2008-10-02: Part number identification placard

FAA order 2008-10-02 is an airworthiness directive in force since May 12, 2008. The FAA's subject line: Part number identification placard. It names Cessna 172 Skyhawk, Cessna 175 Skylark, Cessna 180 Skywagon, Cessna 182 Skylane, Cessna 185 Skywagon, Cessna 206 Stationair, Cessna 207 Skywagon 207, Cessna 208 Caravan, Cessna 210 Centurion, Cessna P172, Cessna P206 Super Skylane, Cessna R172 Hawk XP, Cessna R182 Skylane RG, Cessna T182 Turbo Skylane, Cessna T206 Turbo Stationair, Cessna T210 Turbo Centurion, Cessna T303, Cessna TR182 Turbo Skylane RG, Cessna TU206, Cessna U206 Stationair: about 45,727 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Cessna Aircraft Company
Models
172, 172R, 172RG, 172S, 175, 180, 182, 182S, 182T, 185, 206, 206H, 207, 208, 208B, 210, 210-5 (205), F172D, F172E, F172F, F172G, F172H, F172K, F172L, F172M, F172N, F172P, F182P, F182Q, FR172E, FR172F, FR172G, FR172H, FR172J, FR172K, FR182, P172D, P206, R172E, R172F, R172G, R172H, R172J, R172K, R182, T182, T182T, T206H, T210F, T210G, T210H, T210J, T210K, T210L, T210M, T210N, T210R, T303, TR182, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, U206
On this site
Cessna 172 Skyhawk 20,669 registered
Cessna 175 Skylark 927 registered
Cessna 180 Skywagon 2,606 registered
Cessna 182 Skylane 11,828 registered
Cessna 185 Skywagon 227 registered
Cessna 206 Stationair 213 registered
Cessna 207 Skywagon 207 115 registered
Cessna 208 Caravan 1,022 registered
Cessna 210 Centurion 1,526 registered
Cessna P172 23 registered
Cessna P206 Super Skylane 163 registered
Cessna R172 Hawk XP 758 registered
Cessna R182 Skylane RG 706 registered
Cessna T182 Turbo Skylane 936 registered
Cessna T206 Turbo Stationair 1,058 registered
Cessna T210 Turbo Centurion 1,285 registered
Cessna T303 59 registered
Cessna TR182 Turbo Skylane RG 465 registered
Cessna TU206 343 registered
Cessna U206 Stationair 798 registered

Dates and paperwork

In force since
May 12, 2008
Published
May 2, 2008 (signed April 28, 2008)
Docket
FAA-2008-0471
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 series airplanes. This AD requires you to inspect the alternate static air source selector valve to assure that the part number identification placard does not obstruct the alternate static air source selector valve port. If the part number identification placard obstructs the port, this AD requires you to remove the placard, assure that the port is unobstructed, and report to the FAA if obstruction is found. This AD results from reports of improper installation of the part number identification placard on the alternate static air source selector valve. The actions specified by this AD are intended to prevent erroneous indications from the altimeter, airspeed, and vertical speed indicators, which could cause the pilot to react to incorrect flight information and possibly result in loss of control.

The order itself the regulatory text, as published

Show the full text (6,158 characters)
2008-10-02 Cessna Aircraft Company: Amendment 39-15508; Docket No. FAA-2008-0471; Directorate Identifier 2008-CE-025-AD. \n\nEffective Date \n\n\t(a) This AD becomes effective on May 12, 2008. \n\nAffected ADs \n\n\t(b) None. \n\nApplicability \n\n\t(c) This AD applies to airplanes listed in Table 1 and Table 2 of this AD that: \n\n\t(1) Have a part number (P/N) 2013142-18 alternate static air source selector valve installed after November 19, 2007; and \n\n\t(2) Are certificated in any category: \n\n\tTable 1.--Applicability for Airplanes That Had the Affected Part Installed at Manufacture\n\nModel \nSerial Nos. (S/Ns) \n172S \n172S10672 through 172S10674, 172S10676, 172S10678 through 172S10680, 172S10682, 172S10683, and 172S10685. \n182T \n18282062 and 18282065. \nT182T \nT18208822 and T18208828. \n208 \n20800417, 20800418, and 20800419. \n208B \n208B1294 through 208B1310. \n\n\n\tNote 1: Airplanes listed in Table 1 may have also had the affected part installed as a replacement part.Table 2.--Applicability for Airplanes That Could Have Had the Affected \n\tPart Installed as a Replacement Part or From Parts Held as Spares\n\n\nModel \nS/Ns \n172\nAll S/Ns. \n172R\nAll S/Ns beginning with 17280001. \n172S\n172S8001 through 172S10671. \nF172D\nAll S/Ns. \nF172E\nAll S/Ns. \nF172F\nAll S/Ns. \nF172G\nAll S/Ns. \nF172H\nAll S/Ns. \nF172K\nAll S/Ns. \nF172L\nAll S/Ns. \nF172M\nAll S/Ns. \nF172N\nAll S/Ns. \nF172P\nAll S/Ns. \nFR172E\nAll S/Ns. \nFR172F\nAll S/Ns. \nFR172G\nAll S/Ns. \nFR172H\nAll S/Ns. \nFR172J\nAll S/Ns. \nFR172K\nAll S/Ns. \nP172D\nAll S/Ns. \nR172E (USAF T-41B) (USAF T-41C and D). \nAll S/Ns. \nR172F (USAF T-41). \nAll S/Ns. \nR172G (USAF T-41C or D). \nAll S/Ns. \nR172H (USAF T-41D). \nAll S/Ns. \nR172J\nAll S/Ns. \nR172K\nAll S/Ns. \n172RG\nAll S/Ns. \n175\nAll S/Ns. \n180\nAll S/Ns. \n182\nAll S/Ns. \n182S\n18280001 through 18280944. \n182T\n18280945 through 18282061. \nR182\nAll S/Ns. \nT182\nAll S/Ns. \nTR182\nAll S/Ns. \nT182T\nT18208001 through T18208821. \nF182P\nAll S/Ns. \nF182Q\nAll S/Ns. \nFR182\nAll S/Ns. \n185\nAll S/Ns. \n206\nAll S/Ns. \n206H\nAll S/Ns beginning with 20608001. \nP206\nAll S/Ns. \nU206\nAll S/Ns. \nT206H\nAll S/Ns beginning with T20608001. \nTU206A\nAll S/Ns. \nTU206B\nAll S/Ns. \nTU206C\nAll S/Ns. \nTU206D\nAll S/Ns. \nTU206E\nAll S/Ns. \nTU206F\nAll S/Ns. \nTU206G\nAll S/Ns \n207\nAll S/Ns. \n208\n20800001 through 20800416. \n208B\n208B0001 through 208B1293. \n210\nAll S/Ns. \n210-5 (205). \nAll S/Ns. \nT210F\nAll S/Ns. \nT210G\nAll S/Ns. \nT210H\nAll S/Ns. \nT210J \nAll S/Ns. \nT210K\nAll S/Ns. \nT210L\nAll S/Ns. \nT210M\nAll S/Ns. \nT210N\nAll S/Ns. \nT210R\nAll S/Ns. \nT303\nAll S/Ns. \n\n\n\tNote 2: P/N 2013142-18 replaced P/Ns 2013142-9, -13, and -17. \n\nUnsafe Condition \n\n\t(d) This AD is the result of reports of improper installation of the part number identification placard on the alternate static air source selector valve. We are issuing this AD to prevent erroneous indications from thealtimeter, airspeed, and vertical speed indicators, which could cause the pilot to react to incorrect flight information and possibly result in loss of control. \n\nCompliance \n\n\t(e) For all affected airplanes, to address this problem, you must do the following, unless already done: \n\n\nActions \nCompliance \nProcedures \n(1) Inspect the alternate static air source selector valve to assure that the part number identification placard is not obstructing the port. \n(i) For static air source selector valves installed before May 12, 2008 (The effective date of this AD): Before further flight after May 12, 2008 (the effective date of this AD), and \n(ii) For static air source selector valves installed as modification or replacement parts on or after May 12, 2008 (the effective date of this AD): Before further flight after installation of a P/N 2013142-18 alternate static air source selector valve. Inspection of the part before installation is acceptable. \n(A) Adjust the pilot and copilot seats as far aft as possible. \n(B) Use a flashlight and mirror to inspect the alternate static air source selector valve to assure the port on the forward end of the valve is clearly visible and not covered by the part number identification placard. \n(2) If the alternate static air source selector valve port is found obstructed by the part number identification placard during any inspection required by paragraph (e)(1) of this AD, remove the placard from the valve body, discard the placard, and assure that the port is open and unobstructed. \nBefore further flight after any inspection required in paragraph (e)(1) of this AD where the port is found obstructed. \nMake an entry in the aircraft records showing compliance with this portion of the AD following 14 CFR 43.9. \n\n\n\t(f) Report the results of the inspection required by this AD where an obstruction was found to the FAA. \n\n\t(1) Submit this report within 10 days after the inspection or 10 days after the effective date of this AD, whichever occurs later. \n\n\t(2) Use the form in Figure 1 of this AD and submit it to FAA, Manufacturing Inspection District Office, Mid-Continent Airport, 1804 Airport Road, Room 101, Wichita, Kansas, 67209; or fax to (316) 946-4189. \n\n\t(3) The Office of Management and Budget (OMB) approved the information collection requirements contained in this regulation under the provisions of the Paperwork Reduction Act of 1980 (44 U.S.C. 3501 et seq.) and assigned OMB Control Number 2120-0056. \n\n\n\nAlternative Methods of Compliance (AMOCs) \n\n\t(g) 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: David Fairback, Aerospace Engineer, FAA, Wichita ACO, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: 316-946- 4154; fax: 316-946-4107; e-mail address: david.fairback@faa.gov. 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.

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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 5, 2026. Connections as data: /graph/directive/2008-10-02.json · aircraft systems.