# Piper Service Bulletin 1309: SB_1309 - Rights: © Piper. Filed by the FAA in regulations.gov docket FAA-2018-0015; AD 2018-02-05 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. - Document: [Piper Service Bulletin 1309](https://openairdocs.org/service-documents/piper/sb-1309.md) - Title as filed: SB_1309 - Pages: 6 - PDF: https://openairdocs.org/files/sha256/f3/0b/f30b6ff31b2eef3c2abbf502acc962ae0d03a54776140ccf96c7cd8713d8b3d5 - Page: https://openairdocs.org/service-documents/piper/sb-1309/file/f30b6ff31b2e ## Text Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 (OVER) Date: October 10, 2017 (S) SERVICE BULLETIN NO. 1309 PIPER CONSIDERS COMPLIANCE MANDATORY Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, FL, U.S.A. 32960 Subject: Fuel tank Selector PlacardS InSPectIon ModelS aFFected: SerIal nuMberS aFFected: PA-28-140 Cherokee Cruiser 28-20001 through 28-26946; 28-7125001 through 28-7725290 PA-28-150/160 Cherokee 28-03; 28-1 through 28-4377 and 28-1760A PA-28-180 Cherokee 28-03; 28-671 through 28-5859; 28-7105001 through 28-7205318 PA-28-236 Dakota 28-7911001 through 28-8611008; 2811001 through 2811050 PA-28-151 Warrior 28-7415001 through 28-7715314 PA-28-161 Cadet 2841001 through 2841365 PA-28-161 Warrior II 28-7716001 through 28-8216300; 28-8316001 through 28-8616057; 2816001 through 2816109 PA-28-161 Warrior III 2816110 through 2816119; 2842001 through 2842420 PA-28-180 Archer 28-E13; 28-7305001 through 28-7505261 PA-28-181 Archer II 28-7690001 through 28-8690056; 28-8690061; 28-8690062; 2890001 through 2890205 PA-28-181 Archer III 2890206 through 2890231; 2843001 through 2843879 PA-28-201T Turbo Dakota 28-7921001 through 28-7921095 PA-28R-180 Arrow 28R-30002 through 28R-31270; 28R-7130001 through 28R-7130019 PA-28R-200 Arrow 28R-30482; 28R-35001 through 28R-35820; 28R-7135001 through 28R-7135238 PA-28R-200 Arrow II 28R-7235001 through 28R-7635545 PA-28R-201 Arrow III 28R-7737002 through 28R-7837317; 2837001 through 2837061; 2844001 through 2844171 PA-28R-201T Turbo Arrow III 28R-7703001 through 28R-7803374; 2803001 through 2803015 PA-28RT -201 Arrow IV 28R-7918001 through 28R-8218026 PA-28RT -201T Turbo Arrow IV 28R-7931001 through 28R-8631005; 2831001 through 2831038 ATA/JASC: 2822 ### Page 2 SerVIce bulletIn no. 1309 PaGe 2 of 6 coMPlIance tIMe: Part I. Inspection: Prior to next flight Part II. allowance for limited operation: If the inspection provided in Part I of this service bulletin determines that one or more placards must be replaced, an additional 100 hours of operation is permitted, prior to compliance with Part III, so long as the aircraft is in compliance with the requirements in Part II. Part III. Placard replacement: If the inspection provided in Part I determines that one or more placards must be replaced, compliance with Part III is to coincide with the next regularly scheduled maintenance event, but not to exceed the next 100 hours time in service, provided that the aircraft is in compliance with Part II. aPProVal: The engineering aspects of this service document have been shown to comply with the applicable Federal Aviation Regulations and are FAA approved. PurPoSe: Some affected aircraft may have the left and right fuel tank placards improperly installed on the fuel selector cover. This service bulletin mandates a one-time inspection of the fuel selector cover, and, on condition, the replacement of missing, damaged, or mislocated placards. SaFety Intent: The safety intent of this service bulletin is to identify and correct a fuel selector cover that has the left and right fuel tank placards reversed. A fuel selector cover in this condition could cause the pilot to make a fuel management error, leading to loss of engine power while in flight. InStructIonS: NOTE: Some steps in these instructions are identified as “required for compliance” (RC). If this service bulletin is mandated by an airworthiness directive (AD), the steps identified as RC must be done to comply with the AD. Steps not identified as RC are recommended and may be deviated from, done as a part of other actions, or done with accepted methods different from those given in this service bulletin, if the RC steps can be done and the airplane can be put back in a serviceable condition. Part I. Inspection 1. RC – Identifying Fuel Selector Cover Configuration Compare the currently installed fuel selector cover against the one shown in Figure 1, View A–A. • If the currently installed fuel selector cover matches the cover shown in Figure 1, View A–A, then proceed to Step 2. • If the currently installed fuel selector cover does not match the cover shown Figure 1, View A–A, then the instructions in this service bulletin do not apply. Proceed to Part IV, Documentation of Compliance. NOTE: The fuel selector cover that does not match View A–A is a flat round plate without any features that limit the rotational travel of the fuel selector lever. ### Page 3 SerVIce bulletIn no. 1309 PaGe 3 of 6 Figure 1, Sheet 1 of 2 Fuel Selector Cover P/N 99635-800 – Location and Identification FWD UP VIEW A−A PIPER P/N 99635-800 OTHER COMPONENTS OMITTED FOR CLARITY A AB B PLAN VIEW ### Page 4 SerVIce bulletIn no. 1309 PaGe 4 of 6 2. RC – Identifying Placard Configuration Compare the currently installed fuel selector cover to the illustration in Figure 1, View B–B. Examine all placards for condition and proper placement, with specific emphasis on the location of placards labeled L TANK and R TANK. Replace placards on condition. The proper placard locations are as follows: Placard label Placard PoSItIon OFF Aft (9:00 position) L TANK Up (12:00 position) R TANK Forward (3:00 position) • If the placards are in the proper locations and in good condition, then no replacement is required. Proceed to Part IV, Documentation of Compliance. • If replacement is required, proceed to either Part II or Part III, at owner/operator discretion and as specified under Compliance Time, above. Figure 1, Sheet 2 of 2 Fuel Selector Cover P/N 99635-800 – Showing Placard Locations NOTE: Shown is the proper installation of P/N 99635-800, Fuel Selector Cover, and its placards. NOTE: Clock face graphic is provided to clarify the correct location of the placards. NOTE: The fuel tank capacity stated on the L TANK and R TANK placards will vary by aircraft model, but the location of these placards with respect to the fuel selector cover must all conform to View B–B. SPRING-LOADED METAL STOP, PROTRUDING THROUGH AN OPENING IN THE COVER RIGHT TANK PLACARD (3:00 POSITION) LEFT TANK PLACARD (12:00 POSITION) FUEL OFF PLACARD (9:00 POSITION) FWD UP 9 12 1 2 6 3 VIEW B−B ### Page 5 SerVIce bulletIn no. 1309 PaGe 5 of 6 Part II. allowance for limited operation RC – If the inspection provided in Part I determines that one or more placards must be replaced, an additional 100 hours of operation is permitted prior to complying with Part III, Placard Replacement. The aircraft must maintain compliance with the following requirements in order to operate: a. RC – Fabricate temporary placards, as required, with text (all capital letters) L, R, and/or OFF , using locally sourced materials. Text shall be black in color on a white background, or white on a black background, at the operator’s discretion. Font size shall be 28 points or larger. b. RC – Install each placard at the appropriate location, as shown in Figure 1, View B–B. c. RC – Proceed to Part IV, Documentation of Compliance. Part III. Placard replacement RC – Order replacement placards, as required, as specified in Table 2. Install the replacement placards as follows. For the proper adhesion of the decals, apply them when the ambient temperature is between 55° and 90° F . a. RC – Prepare the surface of the fuel selector cover: 1) Remove the old placards, or temporary placards that were installed in Part II, as applicable. 2) Wipe the area where each new placard is to be installed, using a clean cloth soaked with isopropyl alcohol. 3) Dry with a clean, dry cloth before the alcohol evaporates to avoid discoloration and deposits at the edges of the wetted area. b. RC – Lift a corner or edge of the backing from the new placard. Do not touch the adhesive. c. RC – Position the new placard as shown in Figure 1, View B–B, and secure the free corner or edge. d. RC – Use finger pressure to hold down the secured corner or edge. Remove the rest of the backing from the new placard. e. RC – Firmly press the new placard onto the fuel selector cover to ensure adhesion. f. RC – Proceed to Part IV, Documentation of Compliance. Part IV. documentation of compliance RC – Make a logbook entry documenting compliance with the applicable part(s) of this service bulletin. table 2 rePlaceMent PlacardS – Fuel tank Selector aIrcraFt ModelS Placard Part nuMber leFt tank rIGHt tank oFF PA-28-140/150/160/180 Cherokee 581-686 (99184-003, 25-gallon) 581-687 (99184-004, 25-gallon) 581-685 (99184-002) PA-28R-180 Arrow PA-28R-200 Arrow / II PA-28-151/161 Warrior / II / III 581-890 (99184-007, 24-gallon) 581-891 (99184-008, 24-gallon) PA-28-161 Cadet PA-28-181 Archer II / III (incl. LX and TX) PA-28-201T Turbo Dakota 582-694 (69669-170, 36-gallon) 582-693 (69669-169, 36-gallon) PA-28-236 Dakota PA-28R-201/201T Arrow / Turbo Arrow III PA-28R-201 Arrow III PA-28RT -201/201T Arrow IV / Turbo Arrow IV IF THIS TABLE CHANGES, THEN TABLE UNDER SUPPLEMENT MUST CHANGE TO MATCH ### Page 6 SerVIce bulletIn no. 1309 PaGe 6 of 6 MaterIal reQuIred: On condition, Placards, one each per Table 2 in Instructions, per aircraft aVaIlabIlIty oF PartS: Y our Piper Approved Service Center eFFectIVIty date: This service bulletin is effective upon receipt. SuMMary: Applicable factory participation is limited to new aircraft in warranty at the time of compliance. Factory participation will remain in effect for a period of time not to exceed 180 days from the date of this service bulletin. Please contact your Piper Approved Service Center to make arrangements for compliance with this service bulletin in accordance with the compliance time indicated. note: Please notify the factory of any address/ownership corrections. Changes should include aircraft model, serial number, and current owner’s name and address. Corrections and/or changes should be directed to: PIPER AIRCRAFT, INC. Attn: Customer Service 2926 Piper Drive Vero Beach, FL 32960 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.