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Piper Service Bulletin No. 1041

Piper PA-42 Cheyenne III · Service Bulletins

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Overview

This document is a Service Bulletin issued by The New Piper Aircraft, Inc. on September 25, 2000, concerning the inspection and cleaning of Airborne Air Filter Elements. It specifically addresses potential contamination of the gyro vacuum/pressure system due to loose particles from the air filter. The bulletin outlines compliance requirements based on Airborne Service Letter Number 56 and emphasizes the importance of inspecting and cleaning the air filter elements to maintain the reliability of the gyro system. It is applicable to various Piper models, including the Cheyenne III, and provides guidance on compliance procedures and logbook entries.

  • This Service Bulletin is effective upon receipt and requires compliance with Airborne Service Letter Number 56.
  • Failure to comply may result in contamination of the gyro vacuum/pressure system, affecting reliability.
  • Affected models include the PA-31T1, PA-31T2, PA-31T3, and PA-42/42-720 (Cheyenne III/IIIA).
  • Operators must inspect and clean the air filter elements as detailed in the service letter.
  • A logbook entry must be made after compliance with the Service Bulletin.

Document

Source

Originally published by www.univair.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Service Bulletins
Year
2000
Pages
8
File size
406 KB
Publisher
www.univair.com
How rare is it?
24Piper PA-42 Cheyenne III registered worldwide · 0 active

Common. Rarer than 4% of the aircraft models we track.

Documentation completeness
5/7

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In this document

Purpose

The purpose of this Service Bulletin is to inform aircraft owners and operators about the potential contamination of the gyro vacuum/pressure system due to loose particles from the air filter element. It highlights the need for inspection and cleaning as outlined in Airborne Service Letter Number 56.

Compliance Time

Compliance with the instructions in Airborne Service Letter Number 56 is required to prevent contamination of the gyro vacuum/pressure system. Failure to comply may compromise system reliability.

Instructions

Operators are instructed to refer to the attached Airborne Service Letter Number 56 for detailed inspection and cleaning procedures. If loose particles are found, further inspection of the gyro vacuum/pressure system may be necessary.

Models Affected

The bulletin lists several affected models, including the PA-31T1, PA-31T2, PA-31T3, and PA-42/42-720 (Cheyenne III/IIIA). A comprehensive list of serial numbers for affected models is also provided.

Logbook Entry

Upon successful completion of the inspection and cleaning as per the service letter, operators must make an appropriate logbook entry to document compliance with this Service Bulletin.

Safety notes

  • Failure to comply with Airborne Service Letter Number 56 may result in loose particles contaminating the gyro vacuum/pressure system.

Full document text

~-.i~TM r-'lper SERVICE BULLETIN No. 1041 The New Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida, U.S.A. 32960 SUBJECT: PIPER CONSIDERS Date: September 25, 2000 (S/M) Distribution of Airborne Service Letter Number 56, "Inspection and Cleaning of Airborne Air Filter Elements" MODELS AFFECTED: SERIAL NUMBERS AFFECTED: A guide to Models and Serial Numbers Affected is listed on pages 2 and 3. Because of the possibility of service spares installations, all models and serial r.umbers must be checked for applicability. Note: Many of the Piper models listed use the Airborne Air Filter Element, Part Number D9-18-1 (Piper Code 757-899). See the current Piper Parts Catalog for parts applications and locations of Airborne Air Filter Elements used on your particular Piper model. COMPLIANCE TIME: In accordance with the attached Airborne Service Letter Number 56. Caution: Failure to comply with Airborne Service Letter Number 56 may result in loose particles contaminating the gyro vacuum/pressure system. Left uncorrected, reliability of the gyro vacuum/pressure system may be compromised. PURPOSE: We have been notified by Parker Hannifin Corporation, Airborne Division, that the possibility exists where the airplane's gyro vacuum/pressure system may become contaminated by loose particles originating from the air filter element. To remedy this condition, Airborne has issued Service Letter Number 56, "Inspection and Cleaning of Airborne Air Filter Elements," which requires inspection and cleaning of the air filter elements and associated gyro vacuum/pressure system plumbing. Left uncorrected, reliability of the gyro vacuum/pressure system may be compromised. APPROVAL: The technical contents of this Service Bulletin have been approved by the FAA. INSTRUCTIONS: 1. Refer to the attached Airborne Service Letter Number 56, "Inspection and Cleaning of Airborne Air Filter Elements," and follow the instructions listed under Recommendation. Note: If there is evidence of loose particles in the air filter element, the possibility exists that particles may have entered the gyro vacuum/pressure system, and therefore the entire gyro vacuum/pressure system and components may require inspection. 2. Upon successful completion of Airborne Service Letter Number 56, make an appropriate logbook entry of compliance with this Service Bulletin. (OVER) ATA:3714 PAGE 2 of 4 SERVICE BULLETIN NO. 1041 Effectivity Reference Guide MODELS AFFECTED: PA-18118N18S (Super Cub) PA-20/20S (Pacer) PA-22/22S (Tripacer/Caribbean/Colt) PA-23/23-160 (Apache) PA-23 235 (Apache) PA-23-250/E23-250 (Aztec) PA-24-180/250 (Comanche) PA-24-260 (Comanche) PA-24-400 (Comanche) PA-28-140 (Cherokee) PA-28-150/160/180/288-160/180 (Cherokee) PA-28-151 (Warrior) PA-28-161 (Warrior II) PA-28-161 (Warrior Ill) PA-28-161 (Cadet) PA-28-181 (Archer II) PA-28-181 (Archer Ill) PA-28-235 (Cherokee) PA-28-201T (Turbo Dakota) PA-28-236 (Dakota) PA-28R-180 (Arrow) PA-28R-200 (Arrow/Arrow II) PA-28R-201 (Arrow Ill) PA-28R-201 (Arrow) PA-28R-201T (Turbo Arrow Ill) PA-28RT-201 (Arrcw IV) PA-28RT-201T (Turbo Arrow IV) PA-30 (Twin Comanche) PA-31/300/325 (Navajo/Navajo CR) PA-31-350 (Chieftain) PA-31-350 (T1 020) PA-31 P (Pressurized Navajo) PA-31 P-350 (Mojave) PA-31T (Cheyenne/Cheyenne II) SERIAL NUMBERS AFFECTED: 18-1 through 18-9004, 18-7309016 through 18-8309025 1809001 through 1809113 20-1 through 20-1121 22-1 through 22-9848 23-1 through 23-2046 27-505 through 27-622 27-1 through 27-4866, 27-7304917 through 27-8154030 24-1 through 24-3687 24-3642, 24-4000 through 24-5028 26-2 through 26-148 28-20000 through 28-7725290 28-1 through 28-7505259 & 28-E13 28-7415001 through 28-7715314 28-7716002 through 28-8616057, 2816001 through 2816109 2816110 through 2816119, 2842001 through 2842083 2841001 through 2841365 28-7690001 through 28-8690056, 2890001 through 2890205 2890206 through 2890231, 2843001 through 2843346 28-10001 through 28-7710089 & 28-E11 28-7921001 through 28-7921091 28-7911001 through 28-8611008, 2811001 through 2811050 28R-30001 through 28R-7130013 28R-35001 through 28R-7635545 28R-7737002 through 28R-7837317 2837001 through 2837061 , 2844001 through 2844031 28R-7703002 through 28R-7803372, 2803001 through 2803015 28R-7918001 through 28R-8218026 28R-7931002 through 28R-8631005, 2831001 through 2131038 30-1 through 30-2000 31-2 through 31-861, 31-7300901 through 31-8312019 31-5001 through 31-5004, 31-7305005 through 31-8452021 31-8253001 through 31-8553002 31 P-3 through 31 P-80, 31P-7300110 through 31P-7400230, 31 P-7530001 through 31 P-7730012 31 P-8414001 through 31 P-8414050 31T-7400002 through 31T-7400009, 31T-7520001 through 31T-8120104 SERVICE BULLETIN NO. 1041 PAGE 3 OF 4 Effectivity Reference Guide (Cont'd) MODELS AFFECTED: PA·31T1 (Cheyenne 1/IA) PA-31T2 (Cheyenne IIXL) PA-31T3 (T1 040) PA-32-260 (Cherokee Six) PA-32-300/32S-300 (Cherokee Six) PA-32-301 (Saratoga) PA-32-301T (Turbo Saratoga) PA-32RT-300T (Turbo Lance II) PA-32R-300 (Lance) PA-32RT-300 (Lance II) PA-32R-301 (Saratoga SP) PA-32R-301 (Saratoga II HP) PA-32R-301T (Turbo Saratoga SP) PA-32R-301T (Saratoga II TC) PA-34·200 (Seneca) PA-34·200T (Seneca II) PA·34·220T (Seneca Ill) PA·34·220T (Seneca IV) PA-34-220T (Seneca V) PA-36·285 (Pawnee Brave) PA-36·300 (Pawnee Brave) PA-36·375 (Pawnee Brave) PA-38-112 (Tomahawk) PA-39 (Twin Comanche) PA-40 (Arapaho) PA-42/42-720 (Cheyenne 111/IIIA) PA-42·1000 (Cheyenne 400LS) PA-44·180 (Seminole) PA-44-180T (Seminole) PA-46-31 OP (Malibu) PA-46·350P (Malibu Mirage) SERIAL NUMBERS AFFECTED: 31T-7804001 through 31T-8104101 31T-8304001 through 31T-8304003, 31T-1104004 through 31T-1104017 31T-8166001 through 31T-8166076, 31T-1166001 through 31T-1166008 31T-8275001 through 31T-8475001, 31T-5575001 32-1 through 32-7800008 32-40000 through 32-7940290 32-8006001 through 32-8606023, 3206001 through 3206019 32-8024001 through 32-8424002 32R-7787001 through 32R-7987126 32R-7680001 through 32R-7880068 32R-7885001 through 32R-7985105

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32R-8013001 through 32R-8613006, 3213001 through 3213041 3213029, 3213042 through 3213103, 3246001 through 3246160 32R-8029001 through 32R-8629006, 3229001 through 3229003 3257001 through 3257145 34-7250001 through 34-7450220 34-7570001 through 34-8170092 34-8133001 through 34-8633031, 3433001 through 3433216, 3448001 through 3448035 3448038 through 3448079, 3447001 through 3447029 3449001 through 3449168 36-7360001 through 36-7660135, 36-7760001 through 36-8160023 36-7802001 through 36-8302025 38-78A0002 through 38-82A0124 39-1 through 39-155 40-7400002 42-7800001 through 42-7800002, 42-7801003 through 42-8301002, 42-5501003 through 42-5501060 42-5527001 through 42-5527044 44-7995001 through 44-8195026, 4495001 through 4495013, 4496001 through 4496036 44-8107001 through 44-8207020 46-8408002 through 46-8608088, 4608001 through 4608140 4622001 through 4622200, 4636001 through 4636284 PAGE 4 of 4 SERVICE BULLETIN NO. 1041 MATERIAL REQUIRED: N/A AVAILABILITY OF PARTS: N/A EFFECTIVE 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 Factory Authorized Piper Service Facility to make arrangements for compliance with this Service Bulletin in accordance with the compliance time indicated. Please contact your Factory Authorized Piper Service Facility to make arrangements for compliance with this Service Bulletin in accordance with the compliance time indicated. If you are no longer in possession of this aircraft, please forward this information to the present owner/operator and notify the factory of address/ownership corrections. Changes should include aircraft model, serial number, current owner's name and address. Corrections/changes should be directed to: THE NEW PIPER AIRCRAFT, INC. Attn: Customer Services 2926 Piper Drive Vera Beach, FL 32960 AirborneAir & Fuel Products Service Letter Number: 56 Date: 4/19/00 Service Letter Subject: Inspection and Cleaning of Airborne Air Filter Elements. Applicability: Airborne Air Filter Elements with the following part numbers/date codes which have not been inspected per this service letter as identified in step number seven (7) of the procedure listed below. These components were shipped from Airborne between 1/1/99 and 3/31/00. Item Date Code Air Filter Element Air Filter Element Air Filter Element Part Number !P/Nl 09-14-3 (See Note1) 09-14-5 (See Note 2) 09-18-1 (See Note 3) 1AR thru 12AR and 1AT thru 3AT 1AR thru 12AR and 1AT thru 3AT 1AR thru 12AR and 1AT thru 3AT Note 1: The 09-14-3 is used in the 1J2-2 Air Filter Assembly. Note 2: The 09-14-5 is used in the 1J2-1, 1J2-5 and 1J2-6 Air Filter Assemblies. Note 3: The 09-18-1 is used in the 1J7-1 and 1J7-2 Air Filter Assemblies. Background: Field reports indicate the possibility that loose particles of a black elastomeric compound may not have been completely removed from these air filter elements during the manufacturing process. Recommendation: Within the next thirty days, inspecUclean the air filter elements listed above and also the associated pneumatic system plumbing per the following procedure: 1) Remove the affected air filter element from aircraft per the instructions outlined in the appropriate maintenance/service manual provided by the airframe manufacturer. 2) Inspect the inner diameter of the black end piece(s) of these elements for flashing (Figure 1). Remove all flashing using a sharp knife. Caution: Do not cut the paper filter portion of the element. (Page 1 of 4) Parker Aerospace Parker Hannifin Corporation • Airborne Division 711 Taylor Street • Elyria, Ohio 44035 • 440 284-6300 • Fax: 440 322-5625 Technical Service Hotline: 1-800-382-8422 • E-mail: techhelp@parker.com • www.parker.com/airborne Airborne Air & Fuel Products Service Letter Number: 56 (Continued) 3) Tap the element lightly on a clean work surface in order to remove any loose particles from between the pleat tips on the inside of the paper filter (Figure 2). 4) Inspect the inner diameter (pleat tips) of the paper filter for black residue (Figure 3). Remove all loose residue using the "sticky side" of a strip of masking tape attached to the end of a blunt instrument. 5) Seal one end of the element using a plug. Then, use a heavy-duty vacuum cleaner (e.g. shop vac) to remove all loose particles from inside the element. 6) Thoroughly inspect all internal surfaces of the element for any loose particles. Remove any remaining loose particles using any combination of the above steps. Note: The wicking of black potting material onto pleats of paper filter is acceptable (Figure 4). 7) Identify the element as having been inspected per this service letter by permanently marking (ink stamp, magic marker, etc.) the number of this service letter ("56") on an exterior surface of the element. Note: This marking should be clearly visible once the element is installed back into the aircraft. 8) Remove the applicable pneumatic system hoses/lines as outlined below: Vacuum System: Hoses/lines between system inlet filter and gyro instruments. Pressure System: Hoses/lines between system inlet filter and dry air pump. 9) Clean hoses/lines using a heavy-duty vacuum cleaner (e.g. shop vac) and then reinstall. 10) Reinstall the clean air filter element per the instructions ou!Hned in the appropriate maintenance/service manual provided by the airframe manufacturer. 11) Perform an operational check of the complete pneumatic system per the instructions outlined in the appropriate maintenance/service manual provided by the airframe manufacturer. 12) Any questions regarding this service letter should be directed to Airborne's Customer Support Team as follows: Toll Free Phone Number: 800-382-8422 440-937-1315 440-937-5409 Direct Phone Number: Fax Number: E-Mail: techhelp@parker.com (Page 2 of 4) Parker Aerospace AirborneAir & Fuel Products REMOVE ANY FLASHING FIGURE 1 FIGURE 2 (Page 3 of 4) REMOVE ANY PARTICLES FROM BEIWEEN PLEATS Parker Aerospace Airborne Air & Fuel Products FIGURE 3 REMOVE LOOSE RESIDUE FOUND ON PLEAT TIPS .--WICKING OF POTTING ONTO -----1 PLEATS IS ACCEPTABLE FIGURE 4 (Page 4 of 4) Parker Aerospace

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