AD 2010-13-07
Piper PA-32 Saratoga II TC · Systems Description
Overview
This document is a service bulletin for the Piper PA-32R-301T Saratoga II TC, detailing necessary inspections and replacements for various components of the aircraft's exhaust system. It specifically addresses the inspection of engine mounts, transition headers, and tailpipes, emphasizing the importance of regular checks to ensure safety and compliance with airworthiness directives. The bulletin outlines part numbers for replacement components and provides guidance on ensuring proper assembly and integrity of exhaust system parts. This document is intended for maintenance personnel and pilots responsible for the upkeep of the Piper PA-32R-301T and related models.
- Inspect engine mount for cracks every 100 hours until compliance with SB 955 is achieved.
- Check transition header for cracks and tailpipes for internal pitting, especially at thin sections.
- Replace spot welded clamps with riveted types as per AD 2010-13-07.
- Ensure slip fit stacks are ordered as complete assemblies for proper integrity.
- Inspect hot areas of exhaust components for black flaking metal and bulges.
Document
Source
Originally published by www.acornwelding.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Systems Description
- Year
- 2010
- Pages
- 1
- File size
- 154 KB
- Publisher
- www.acornwelding.com
Most owners only have the POH. Here's the essential set for the Piper PA-32 Saratoga II TC.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
More Piper PA-32 Saratoga II TCmanuals & documents
See all 17 →- Airworthiness Directive Schedule Aeroplanes Piper PA-32 Series (Cherokee 6, Saratoga, Lance and Seaplane)Airworthiness Directives
- LAUSANNE AEROCLUB - PA32R-301 PIPER SARATOGA II - HB-PJEChecklist
- AFMS – GFC 500 Piper PA-32(R) SeriesPilot's Operating Handbook
- PA-32R-301/301T, SARATOGA II HP/TC MAINTENANCE MANUALChecklist
- N123AX - Piper Saratoga II HP (PA-32R-301) ChecklistChecklist
- PA32 SpecificationsPerformance Data
- Airworthiness Directives; Piper Aircraft, Inc. Models PA-32R-301T and PA-46-350P AirplanesAirworthiness Directives
- PA-32R-301 / 301T AIRPLANE MAINTENANCE MANUALPilot's Operating Handbook
- PA-32R-301T, SARATOGA II TC EQUIPMENT LISTChecklist
- Performance Data for the Piper PA-32 Saratoga II TCPerformance Data
- Pilot's Operating Handbook and FAA Approved Airplane Flight ManualPilot's Operating Handbook
- PIPER AIRCRAFT PA-32R-301/301T MAINTENANCE MANUALMaintenance Manual
In this document
Inspection Requirements
The document mandates inspections of the engine mount for cracks every 100 hours until compliance with Part 2 of Piper SB 955 is achieved. It also requires checks for cracks in the transition header and internal pitting in the tailpipes, particularly at the outside radius and support brackets.
Exhaust System Components
A detailed list of exhaust system components is provided, including part numbers for exhaust stacks, transition cylinders, and various clamps. The bulletin specifies that slip fit stacks should be ordered as complete assemblies to ensure proper joint integrity.
Compliance with Airworthiness Directives
The bulletin references AD 2010-13-07, which requires the replacement of spot welded clamps with riveted types to ensure durability and safety. It emphasizes the importance of ensuring all slip joints have movement and that flanges align correctly.
Safety notes
- Regular inspections are critical for maintaining airworthiness and safety.
- Failure to comply with inspection requirements may lead to safety hazards.
Full document text
Exhaust Systems Engine Mounts Carb Air Boxes Shrouds Seats Piston Turbine Radial Vintage And More... L E L N E C C E X E 1 AD 93-05-10 Piper PA-32R-301T Applies to S/N's 32R-8029001 thru 32R-8629006, 3229001 thru 3229003. Inspect engine mount for cracks. Inspection required every 100 hrs until compliance with Part 2 of Piper SB 955 accomplished. Inspect transition header for cracks Inspect tail pipes for internal pitting and wall thickness especially at the outside radius, which is the thin section, and at support bracket. Slip fit stacks should be ordered as a complete assembly to ensure good joint integrity with smooth slip fits. This part has a hot area at the elbow. Inspect this area for black flaking metal and bulges. PIPER PA-32R-301T Saratoga II TC SN 3255001 and on SN 3257001 and on With Lycoming TIO-540-AH1A Engine PIPER PA-32-301 XTC 7 8 2 3 4 5 7 7 9 11 12 13 14 10 6 AD 2010-13-07 Replace all spot welded clamps (40D21162-340M and LW-12093-8) with riveted type (40D23255-340M). Ensure all slip joints have movement and flanges line up correctly. Item Part Number Description 40B22315 EXHAUST STACK CYL #1 40B22304 EXHAUST STACK CYL #2 40B22303 EXHAUST STACK CYL #3 40B21921 EXHAUST STACK CYL #4 47C21912 TRANSITION CYL #5 40B21919 EXHAUST STACK CYL #6 40B19840 EXHAUST PIPE ADAPTER 40B22317 WASTEGATE PIPE 40B22316 TAILPIPE 40C19819 SLIP FLANGE, V-BAND LW-12125-3 CLAMP FORWARD OF WASTEGATE LW-12093-6 CLAMP AFT OF WASTEGATE LW-12093-5 CLAMP FORWARD OF TRANSITION CLAMP TAILPIPE 104697-002 SHROUD 77611 GASKET 78084 GASKET FORWARD OF TRANSITION 75845 GASKET WASTEGATE 07A22530 BRACKET TURBO MOUNT RIGHT 07F19871 STRUT TURBO RIGHT 38080-022 INDUCTION AIR BOX 100923-002 ALTERNATE AIR BOX ASSY 69768-000 HORN ASSY STREERING 38729-021 ENGINE MOUNT 38727-022 ENGINE MOUNT J-9613-55/19 SHOCK MOUNT VARIOUS SEAT BASE 40B22315 EXHAUST STACK CYL #1 40B22304 EXHAUST STACK CYL #2 40B22303 EXHAUST STACK CYL #3 40B21921 EXHAUST STACK CYL #4 47C21912 TRANSITION CYL #5 40B21919 EXHAUST STACK CYL #6 40B19840 EXHAUST PIPE ADAPTER 40B22317 WASTEGATE PIPE 40B22316 TAILPIPE 40C19819 SLIP FLANGE, V-BAND LW-12125-3 CLAMP FORWARD OF WASTEGATE LW-12093-6 CLAMP AFT OF WASTEGATE LW-12093-5 CLAMP FORWARD OF TRANSITION CLAMP TAILPIPE 104697-002 SHROUD 77611 GASKET 78084 GASKET FORWARD OF TRANSITION 75845 GASKET WASTEGATE 07A22530 BRACKET TURBO MOUNT RIGHT 07F19871 STRUT TURBO RIGHT 38080-022 INDUCTION AIR BOX 100923-002 ALTERNATE AIR BOX ASSY 69768-000 HORN ASSY STREERING 38729-021 ENGINE MOUNT 38727-022 ENGINE MOUNT J-9613-55/19 SHOCK MOUNT VARIOUS SEAT BASE 1 2 3 4 5 6 7 8 9 10 11 12 13 14 - - - - - - - - - - - - - SN 3246001 and on SN 3255001 and on (XTC) SN 3255001 and on (XTC) SN 3257001 and on 40D23255-340M SB1092 (Inconel) AD 2010-13-07 Compliant (toll free) 1-888-388-8803 1-780-447-5955 Fax: 1-780-447-5980 sales@acornwelding.com parts@acornwelding.com www.acornwelding.com (toll free) 1-888-388-8803 1-780-447-5955 Fax: 1-780-447-5980 sales@acornwelding.com parts@acornwelding.com www.acornwelding.com ©2010 Acorn Welding Ltd.