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Piper Service Bulletin No. 1041

Piper PA-20 Pacer · Service Bulletins

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Overview

This document is a service bulletin for the Piper PA-20 Pacer, detailing the inspection and cleaning of Airborne air filter elements to prevent contamination of the gyro vacuum/pressure system. It outlines compliance requirements, affected models, and necessary actions to ensure safety and reliability.

  • Compliance with Airborne Service Letter Number 56 is required.
  • Inspection and cleaning of air filter elements are necessary to prevent gyro system contamination.
  • Affected models include PA-20/20S (Pacer) serial numbers 20-1 through 20-1121.
  • Failure to comply may compromise gyro system reliability.
  • Logbook entries are required after compliance.
  • Factory participation is limited to new aircraft in warranty.
  • Contact a Factory Authorized Piper Service Facility for compliance arrangements.
  • The document is effective upon receipt.

Document

Source

Originally published by barteltaviation.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
File size
·
309 KB
Publisher
·
barteltaviation.com
Language
·
en
About this document
What is the Piper Service Bulletin No. 1041?

The Piper Service Bulletin No. 1041 is a service bulletins for the Piper PA-20 Pacer, dated 2000.

Where does the Piper Service Bulletin No. 1041 come from?

This copy of the Piper Service Bulletin No. 1041 was originally published by barteltaviation.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the Piper Service Bulletin No. 1041 published?

The Piper Service Bulletin No. 1041 — the Piper PA-20 Pacer service bulletins on file — is dated 2000.

Documentation completeness
1/7

Most owners only have the POH. Here's the essential set for the Piper PA-20 Pacer.

  • Pilot's Operating Handbook / AFM
  • Checklist
  • Maintenance Manual
  • Parts Catalog (IPC)
  • Systems & Wiring
  • Service Bulletins on file
  • Type Certificate (TCDS)

More Piper PA-20 Pacermanuals & documents

In this document

Models Affected

The PA-20/20S (Pacer) is affected, with serial numbers ranging from 20-1 to 20-1121.

Compliance Time

Compliance must be in accordance with the attached Airborne Service Letter Number 56.

Caution

Failure to comply may result in contamination of the gyro vacuum/pressure system.

Instructions

Follow the instructions in Airborne Service Letter Number 56 for inspection and cleaning.

Factory Participation

Limited to new aircraft in warranty at the time of compliance, effective for 180 days.

Contact Information

For compliance arrangements, contact The New Piper Aircraft, Inc. Customer Services.

Safety notes

  • Failure to comply with Airborne Service Letter Number 56 may result in gyro system contamination.
  • Inspect the entire gyro vacuum/pressure system if loose particles are found.
  • Do not cut the paper filter portion of the air filter element during inspection.
  • Mark the air filter element to indicate it has been inspected per the service letter.

Full document text

1041 Date: September 25, 2000 (S/M) SUBJECT: 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 numbers 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 The New Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida, U.S.A. 32960 TM PAGE 2 of 4 SERVICE BULLETIN NO. 1041 Effectivity Reference Guide MODELS AFFECTED: SERIAL NUMBERS AFFECTED: PA-18/18A/18S (Super Cub) 18-1 through 18-9004, 18-7309016 through 18-8309025 1809001 through 1809113 PA-20/20S (Pacer) 20-1 through 20-1121 PA-22/22S (Tripacer/Caribbean/Colt) 22-1 through 22-9848 PA-23/23-160 (Apache) 23-1 through 23-2046 PA-23 235 (Apache) 27-505 through 27-622 PA-23-250/E23-250 (Aztec) 27-1 through 27-4866, 27-7304917 through 27-8154030 PA-24-180/250 (Comanche) 24-1 through 24-3687 PA-24-260 (Comanche) 24-3642, 24-4000 through 24-5028 PA-24-400 (Comanche) 26-2 through 26-148 PA-28-140 (Cherokee) 28-20000 through 28-7725290 PA-28-150/160/180/28S-160/180 (Cherokee) 28-1 through 28-7505259 & 28-E13 PA-28-151 (Warrior) 28-7415001 through 28-7715314 PA-28-161 (Warrior II) 28-7716002 through 28-8616057, 2816001 through 2816109 PA-28-161 (Warrior III) 2816110 through 2816119, 2842001 through 2842083 PA-28-161 (Cadet) 2841001 through 2841365 PA-28-181 (Archer II) 28-7690001 through 28-8690056, 2890001 through 2890205 PA-28-181 (Archer III) 2890206 through 2890231, 2843001 through 2843346 PA-28-235 (Cherokee) 28-10001 through 28-7710089 & 28-E11 PA-28-201T (Turbo Dakota) 28-7921001 through 28-7921091 PA-28-236 (Dakota) 28-7911001 through 28-8611008, 2811001 through 2811050 PA-28R-180 (Arrow) 28R-30001 through 28R-7130013 PA-28R-200 (Arrow/Arrow II) 28R-35001 through 28R-7635545 PA-28R-201 (Arrow III) 28R-7737002 through 28R-7837317 PA-28R-201 (Arrow) 2837001 through 2837061, 2844001 through 2844031 PA-28R-201T (Turbo Arrow III) 28R-7703002 through 28R-7803372, 2803001 through 2803015 PA-28RT-201 (Arrow IV) 28R-7918001 through 28R-8218026 PA-28RT-201T (Turbo Arrow IV) 28R-7931002 through 28R-8631005, 2831001 through 2131038 PA-30 (Twin Comanche) 30-1 through 30-2000 PA-31/300/325 (Navajo/Navajo CR) 31-2 through 31-861, 31-7300901 through 31-8312019 PA-31-350 (Chieftain) 31-5001 through 31-5004, 31-7305005 through 31-8452021 PA-31-350 (T1020) 31-8253001 through 31-8553002 PA-31P (Pressurized Navajo) 31P-3 through 31P-80, 31P-7300110 through 31P-7400230, 31P-7530001 through 31P-7730012 PA-31P-350 (Mojave) 31P-8414001 through 31P-8414050 PA-31T (Cheyenne/Cheyenne II) 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: SERIAL NUMBERS AFFECTED: PA-31T1 (Cheyenne I/IA) 31T-7804001 through 31T-8104101 31T-8304001 through 31T-8304003, 31T-1104004 through 31T-1104017 PA-31T2 (Cheyenne IIXL) 31T-8166001 through 31T-8166076, 31T-1166001 through 31T-1166008 PA-31T3 (T1040) 31T-8275001 through 31T-8475001, 31T-5575001 PA-32-260 (Cherokee Six) 32-1 through 32-7800008 PA-32-300/32S-300 (Cherokee Six) 32-40000 through 32-7940290 PA-32-301 (Saratoga) 32-8006001 through 32-8606023, 3206001 through 3206019 PA-32-301T (Turbo Saratoga) 32-8024001 through 32-8424002 PA-32RT-300T (Turbo Lance II) 32R-7787001 through 32R-7987126 PA-32R-300 (Lance) 32R-7680001 through 32R-7880068 PA-32RT-300 (Lance II) 32R-7885001 through 32R-7985105 PA-32R-301 (Saratoga SP) 32R-8013001 through 32R-8613006, 3213001 through 3213041 PA-32R-301 (Saratoga II HP) 3213029, 3213042 through 3213103, 3246001 through 3246160 PA-32R-301T (Turbo Saratoga SP) 32R-8029001 through 32R-8629006, 3229001 through 3229003 PA-32R-301T (Saratoga II TC) 3257001 through 3257145 PA-34-200 (Seneca) 34-7250001 through 34-7450220 PA-34-200T (Seneca II) 34-7570001 through 34-8170092 PA-34-220T (Seneca III) 34-8133001 through 34-8633031, 3433001 through 3433216, 3448001 through 3448035

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PA-34-220T (Seneca IV) 3448038 through 3448079, 3447001 through 3447029 PA-34-220T (Seneca V) 3449001 through 3449168 PA-36-285 (Pawnee Brave) 36-7360001 through 36-7660135, PA-36-300 (Pawnee Brave) 36-7760001 through 36-8160023 PA-36-375 (Pawnee Brave) 36-7802001 through 36-8302025 PA-38-112 (Tomahawk) 38-78A0002 through 38-82A0124 PA-39 (Twin Comanche) 39-1 through 39-155 PA-40 (Arapaho) 40-7400002 PA-42/42-720 (Cheyenne III/IIIA) 42-7800001 through 42-7800002, 42-7801003 through 42-8301002, 42-5501003 through 42-5501060 PA-42-1000 (Cheyenne 400LS) 42-5527001 through 42-5527044 PA-44-180 (Seminole) 44-7995001 through 44-8195026, 4495001 through 4495013, 4496001 through 4496036 PA-44-180T (Seminole) 44-8107001 through 44-8207020 PA-46-310P (Malibu) 46-8408002 through 46-8608088, 4608001 through 4608140 PA-46-350P (Malibu Mirage) 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. NOTE: 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 Vero Beach, FL 32960 AirborneAir & Fuel Products Service Letter Service Letter Number: 56 Date: 4/19/00 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. from Airborne between l/l/99 and 3/31/00. These components were shipped Item Part Number (P/N) Air Filter Element D9-14-3 (See Note) Date Code IAR thru 12AR and IAT thru 3AT Air Filter Element Air Filter Element D9-14-5 (See Note 2) D9-18-1 (See Note 3) IAR thru 12AR and IAT thru 3AT IAR thru 12AR and IAT thru 3AT Note 1: The D9-14-3 is used in the 1J2-2 Air Filter Assembly. Note 2: The D9-14-5 is used in the 1J2-1, 1J2-5 and 1J2-6 Air Filter Assemblies. Note 3: The D9-18-I 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, inspect/clean 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) Aerospace Parker Hannifin Corporation . Airborne Division 711 Taylor Street l Elyria, Ohio 44035 l 440 284-6300 . Fax: 440 322-5625 Technical Service Hotline: l-800-382-8422 l E-mail: techhelp@parker.com l 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 outlined 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 Direct Phone Number: 440-937-I 315 Fax Number: 440-937-5409 E-Mail: techhelp@parker.com (Page 2 of 4) Aerospace AirborneAir & Fuel Products REMOVE ANY FLASHING REMOVE ANY PARTICLES FROM BETWEEN PLEATS FIGURE 2 (Page 3 of 4) Aerospace Airborne Air & Fuel Products ,REMOVE LOOSE RESIDUE ON PLEAT TIPS FIGURE 3 WICKING OF POTTING ONTO PLEATS IS ACCEPTABLE FIGURE 4 (Page 4 of 4) Aerospace