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(OVER) Date: October 16, 2018 (S)
SERVICE
BULLETIN NO. 1332
PIPER CONSIDERS
COMPLIANCE MANDATORY ATA/JASC: 5312 Piper Aircraft, Inc.
2926 Piper Drive Vero Beach, FL, U.S.A. 32960 SUBJECT: BULKHEAD RIVET REPLACEMENT MODELS AFFECTED: SERIAL NUMBERS AFFECTED:
PA-46-600TP M600 4698001, 4698004 through 4698010, 4698012 through 4698016, 4698018 through 4698076 COMPLIANCE TIME:
Part I. Temporary Ground Operating Limitation: Upon receipt, prior to next flight. Part I is to remain in effect until the aircraft is made compliant with Part II of this service bulletin.
Part II. Rework: To coincide with the next regularly scheduled maintenance event, but not to exceed the next 100 hours time in service. Compliance with Part II will remove the temporary operating limitation imposed by Part I of this service bulletin APPROVAL: The engineering aspects of this service document have been shown to comply with the applicable Federal Aviation Regulations and are FAA approved.
PURPOSE: Part I of this service bulletin imposes a temporary ground operating limitation.
Part II mandates the replacement of specific rivets common to the fuselage station (FS) 79.00 bulkhead.
SAFETY INTENT: As delivered from the factory, the FS 79.00 bulkhead on the affected aircraft does not have the required strength. Compliance with this service bulletin will ensure that loading conditions do not exceed the strength capability of the FS 79.00 bulkhead.
Failure of the FS 79.00 bulkhead could result in loss of structural integrity of the airframe.
The safety intent of this service bulletin is to ensure that operating loads do not exceed the airframe capability at the affected area:
• For short-term mitigation, airframe load is limited by completing Part I of this service bulletin.
• For long-term mitigation, the airframe conforms to type design strength by completing Part II of this service bulletin.
CONFIGURATION DESCRIPTION: Part II of this service bulletin mandates the replacement of specific rivets in the FS
79.00 bulkhead.
SERVICE BULLETIN NO. 1332 PAGE 2 of 11 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. Temporary Ground Operating Limitation NOTE: The limitation provided in the attached temporary page for the pilot’s operating handbook (POH), and the related instrument panel placard, are precautionary until the aircraft is made compliant with Part II of this service bulletin.
1. RC – Cut out and insert the temporary page from Figure 1 into the current PA-46-600TP POH VB–2366, after the existing page 2-1
2. RC – Temporary Placard
a. Order one (1) Placard – Ground Limitation, Piper part number (P/N) 46G110013-702, per aircraft.
Alternatively, it is permissible to either 1) fabricate a placard or 2) utilize one of the placards in Figure 2:
1) Fabricate a placard from locally sourced materials, subject to the constraints listed below.
• The size of the placard shall be no greater than 0.75 inch high by 2.66 inches wide (3/4 x 2 1/3).
• The layout of the text shall agree with the example fabricated placard in Figure 2.
• The colors used shall be either white text on a matte black background, or black text on a white background.
• The font size shall be nine points (9 pt.) or larger.
• The text shall be comprised of all upper case (capital) letters.
• The typeface shall be chosen for its legibility. Examples include Alternate Gothic #2, Arial, Calibri, and Helvetica.
2) Print and cut out either of the example placards from Figure 2. Print the placard at the actual size.
For these alternatives, the printing material and adhesive used (e.g.: double-sided tape; clear, single-sided tape; or a suitable adhesive-backed material) is at the discretion of the owner/operator. The placard must be installed securely with none of its text concealed.
b. Install the placard onto the cockpit instrument panel in the location shown in Figure 3.
3. RC – Make a logbook entry documenting compliance with Part I of this service bulletin.
SERVICE BULLETIN NO. 1332 PAGE 3 of 11 ISSUED: June 17, 2016 REPORT: VB-2366 2-1a SECTION 2 PA-46-600TP LIMITATIONS REQUIRED UNTIL SB 1332 PART II COMPLIED WITH.
TEMPORARY GROUND OPERATIONS LIMITATION During ground operations including towing or taxiing, sharp turns are limited to groundspeeds below 10 knots.
For PA-46-600TP airplanes serial numbers 4698001, 4698004 through 4698010, 4698012 through 4698016, and 4698018 through 4698076, the above limitation is imposed by Piper Service Bulletin 1332 Part I (latest revision) and must remain in effect until the airplane is made compliant with Piper Service Bulletin 1332 Part II (latest revision).
When the airplane is compliant with Piper Service Bulletin 1332 Part II (latest revision), this page may be removed.
WARNING Figure 1 POH VB-2366 Temporary Page
SERVICE BULLETIN NO. 1332 PAGE 4 of 11 TEMP. GROUND OPS. LIMITATION REF SB1332 LATEST REV. 46G110013-702 SHARP TURNS LIMITED TO 10 KTS GS P/N 46G110013-702
2.40
0.625 P/N 46G110013-702 TEMP. GROUND OPS. LIMITATION REF SB1332 LATEST REV. 46G110013-702 SHARP TURNS LIMITED TO 10 KTS GS TEMP. GROUND OPS. LIMITATION REF SB1332 LATEST REV.
SHARP TURNS LIMITED TO 10 KTS GS 0.625 APPROX. 2.50 TEMP. GROUND OPS. LIMITATION REF SB1332 LATEST REV.
SHARP TURNS LIMITED TO 10 KTS GS 0.625
EXAMPLE FABRICATED PLACARD
EXAMPLE FABRICATED PLACARD Figure 2 P/N 46G110013-702 and an Example of a Fabricated Temporary Placard 46F24A001 46F24A016-A 46G11A001-F Sh5
NXXXXX
STALL WARN
ICE SCHEDULE (PRESS OFF)
SEE DETAIL B
PLACARD P/N 46G110013-702
DETAIL B
PLACARD P/N 46G110013-702 Figure 3 Instrument Panel – Temporary Placard Installation
SERVICE BULLETIN NO. 1332 PAGE 5 of 11 Part II. Rework
1. RC – Remove the main battery per Piper PA-46-600TP M600 Airplane Maintenance Manual (AMM), part number (P/N) 767-617, Section 24-30-00.
NOTE: At the discretion of the technician, the engine and engine mount may be removed as one assembly, rather than separately as the following two steps state.
2. Remove the engine per Piper PA-46-600TP AMM P/N 767-617, Section 71-00-00.
3. Remove the engine mount assembly per Piper AMM P/N 767-617, Section 71-20-00.
4. Remove the fuel filter assembly per Piper AMM P/N 767-617, Section 28-20-00.
5. Remove heat blankets, as necessary.
6. Examine the entire surface of the bulkhead for damage. Any discovery of cracks, wrinkling, or missing rivets must be reported to Piper before proceeding. Contact Piper Customer Service to request the development of a suitable repair at (+1) 772-299-2141 or CustomerService@piper.com. Piper’s normal business hours are Monday through Friday, 7:30 a.m. to 4:30 p.m. (Eastern).
7. RC – Identify and remove all rivets within the highlighted areas in Figure 4, View B–B.
To replace the single rivet identified in Figure 4, View C–C, it may be necessary to remove some or all of the rivets retaining two (2) Upper Tunnel Support Channels, P/N 103142-002 and 103144-002, which are identified in View C–C. View D–D shows the channel rivet locations and types.
8. RC – Install the rivets shown in Table 1, as depicted in View B–B and, if necessary, View D–D, as replacements.
Ensure that a minimum edge distance of 0.32 inches is maintained for all rivets.
Wet install all rivets with primer that conforms to MIL-PRF-85582D Type 1 Class C2, or, any one of the primers listed in Table 2.
TABLE 1
REPLACEMENT RIVETS
QUANTITY PART NUMBER
BASIC CODE (per NAS523) A/R MS20613-4P (See Note 1) LL 21 NAS1738M AAR 13 CR3523-5 (See Note 2) ASC 12 MS20613-5C LM A/R MS20613-4C (See Note 3) LM NOTE 1: Where MS20613-4P (LL) fasteners are specified, it is permissible to install oversize repair rivets MS20613-5P (LL), provided that a minimum edge distance of 0.32 inches is maintained.
NOTE 2: Optionally, NAS9307M-5 (AYS) rivets may be installed in place of CR3523-5 rivets.
NOTE 3: Where MS20613-4C (LM) fasteners are specified, it is permissible to install oversize repair rivets MS20613-5C (LM), provided that a minimum edge distance of 0.32 inches is maintained.
TABLE 2
ACCEPTABLE PRIMERS Piper P/N Vendor Name Vendor Product No./Description 279-179 PPG Aerospace PRC-DeSoto EWDE072A/B 279-506 Akzo Nobel Aerospace Coatings 10P8-10NF/EC-283 279-108 Akzo Nobel Aerospace Coatings 10P30-5/EC-275 N/A Deft (PPG Industries) 44GN036 279-240 Axalta Coating Systems 13550S Epoxy Primer
SERVICE BULLETIN NO. 1332 PAGE 6 of 11
9. Reinstall the fuel filter assembly per Piper AMM P/N 767-617, Section 28-20-00. Reinstall all heat blankets that were removed.
NOTE: At the discretion of the technician, the engine and engine mount may be reinstalled as one assembly, rather than separately as the following two steps state.
10. Reinstall the engine mount assembly per Piper AMM P/N 767-617, Section 71-20-00.
11. Reinstall the engine per Piper AMM P/N 767-617, Section 71-00-00.
12. Reinstall the battery per Piper AMM P/N 767-617, Section 24-30-00.
13. Remove the temporary page that was placed in the current PA-46-600TP POH, VB–2366, and the temporary placard that was installed on the instrument panel, as part of compliance with Part I of this service bulletin.
14. RC – Make a logbook entry documenting compliance with Part II of this service bulletin.
SERVICE BULLETIN NO. 1332 PAGE 7 of 11 Figure 4, Sheet 1 of 4 Fastener Replacements FS
132.00 FS
124.125 FS
117.00 FS
108.00 FS
100.00 FS
95.00 FS
53.75 FS
66.375 FS
79.00
FIREWALL (REF)
SEE VIEW A B B
VIEW A ISOMETRIC VIEW SHOWING FS 79.00 (COMPONENTS REMOVED FOR CLARITY) FWD UP FS
79.00 B B
SERVICE BULLETIN NO. 1332 PAGE 8 of 11 Figure 4, Sheet 2 of 4 Fastener Replacements
DOUBLER P/N 102172-003
(2) (See Note 2, Table 1) 9X ASC 5 (See Note 2, Table 1) 4X ASC 5
ACCEPTABLE AS IS
ACCEPTABLE AS IS P/N 102173-003 (REF) P/N 102174-002 (REF) 6X LM 5 6X LM 5 C C (See Note 3, Table 1) A/R LM 4 A/R LM 4 (See Note 3, Table 1) BL
0.00 BL
0.00
DOUBLER P/N 102172-004
(1)
DOUBLER P/N 46F531237-001
(2) RIVET (See View C–C) A Fig 4 Sh 2 A Fig 4 Sh 3 B Fig 4 Sh 2 B Fig 4 Sh 3 VIEW B−B (SECTION 1 OF 2) LOOKING AFT AT F.S. 79.00
BULKHEAD ASSEMBLY VIEW B−B (SECTION 2 OF 2) LOOKING AFT AT F.S. 79.00
BULKHEAD ASSEMBLY NOTE: All fasteners (rivets) in the highlighted areas are affected.
SERVICE BULLETIN NO. 1332 PAGE 9 of 11 Figure 4, Sheet 3 of 4 Fastener Replacements
DOUBLER P/N 102172-003
(2) (See Note 2, Table 1) 9X ASC 5 (See Note 2, Table 1) 4X ASC 5
ACCEPTABLE AS IS
ACCEPTABLE AS IS P/N 102173-003 (REF) P/N 102174-002 (REF) 6X LM 5 6X LM 5 C C (See Note 3, Table 1) A/R LM 4 A/R LM 4 (See Note 3, Table 1) BL
0.00 BL
0.00
DOUBLER P/N 102172-004
(1)
DOUBLER P/N 46F531237-001
(2) RIVET (See View C–C) A Fig 4 Sh 2 A Fig 4 Sh 3 B Fig 4 Sh 2 B Fig 4 Sh 3 VIEW B−B (SECTION 1 OF 2) LOOKING AFT AT F.S. 79.00
BULKHEAD ASSEMBLY VIEW B−B (SECTION 2 OF 2) LOOKING AFT AT F.S. 79.00
BULKHEAD ASSEMBLY NOTE: All fasteners (rivets) in the highlighted areas are affected.
SERVICE BULLETIN NO. 1332 PAGE 10 of 11 Figure 4, Sheet 4 of 4 Fastener Replacements VIEW C−C
LOOKING UP AND AFT
CHANNELS TO REMOVE TO REPLACE
THE IDENTIFIED RIVET
CHANNEL P/N 103144-002
CHANNEL P/N 103142-002 RIVET FWD D D FWD VIEW D−D
LOOKING UP
CHANNELS THAT MAY REQUIRE REMOVAL
OR SOME RIVETS REMOVED
TO COMPLY WITH PART II A/R LL 4 (See Note 1, Table 1) A/R LL 4 (See Note 1, Table 1) AAR 4F
CHANNEL P/N 103144-002
CHANNEL P/N 103142-002
SERVICE BULLETIN NO. 1332 PAGE 11 of 11 MATERIAL REQUIRED: Per aircraft:
For Part I:
• One (1) Placard – Ground Limitation, Piper P/N 46G110013-702, or equivalent
• Attached, POH VB-2366 Temporary Page, Figure 1 For Part II, sufficient amounts (refer to Table 1):
• Rivet, P/N MS20613-4P (LL), or, as required, P/N MS20613-5P (LL)
• Rivet, P/N MS20613-4C (LM), or, as required, P/N MS20613-5C (LM)
• Rivet, P/N MS20613-5C (LM)
• Rivet, P/N CR3523-5 (ASC), or P/N NAS1738M (AAR) AVAILABILITY OF PARTS: Y our Piper Approved Service Center, or, procure locally 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.
Att’n: Customer Service 2926 Piper Drive Vero Beach, FL 32960 or:
CustomerService@piper.com Please include in subject line: “Aircraft ownership update”