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Cessna T206/T207/T210/P206 Systems Description

CESSNA T206 · Systems Description

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Overview

This document provides a comprehensive systems description for the Cessna T206, T207, T210, and P206 aircraft models. It includes detailed information on the exhaust systems, engine mounts, carburetor air boxes, and other critical components. The document is intended for maintenance personnel and pilots who require in-depth knowledge of the aircraft systems for operational and safety purposes. It outlines specific inspection requirements, part numbers, and applicable airworthiness directives (ADs) for various serial number ranges, ensuring that users can maintain compliance and safety in their operations.

  • Inspect exhaust outlet stack for chaffing from the shroud.
  • Inspect muffler for blisters or bulges under heat shroud.
  • Inspect joints for freedom of movement and distortion.
  • AD 85-10-02 applies to S/N's P206-0001 thru P20600647 with Continental IO-520 engines.
  • Inspection of the exhaust system is required every 50 hours of operation for certain models.

Document

Source

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

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Document details

Type
Systems Description
Pages
1
File size
247 KB
Publisher
www.acornwelding.com
How rare is it?
1CESSNA T206 registered worldwide

Common. Rarer than 24% of the aircraft models we track.

Documentation completeness
6/7

Most owners only have the POH. Here's the essential set for the CESSNA T206.

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In this document

Exhaust System Inspection

The document emphasizes the importance of inspecting the exhaust system for potential issues such as chaffing from the shroud, blisters or bulges on the muffler, and ensuring joints are free of distortion. Regular inspections are mandated to maintain system integrity.

Airworthiness Directives (ADs)

Several ADs are applicable to the Cessna T206 and related models. For instance, AD 85-10-02 requires inspections of the engine induction air box duct for cracks every 100 hours of operation. AD 83-23-03 R2 mandates exhaust system inspections every 50 hours for the P210N model.

Part Numbers and Descriptions

The document lists various part numbers related to the exhaust and induction systems, including components like exhaust ends, risers, tailpipes, and induction air boxes. Each part is identified with a specific code for easy reference.

Safety notes

  • Regular inspections are critical for maintaining safety and compliance with ADs.
  • Failure to inspect exhaust systems can lead to serious operational 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 CESSNA T206/T207/T210/P206 Usable on Codes A: SN U20600487 to 02199, SN 207-00001 to 00788 SN 210-00001 to 59199, P206-0161 to P206-0647 B: SN U20602200 to U20607020, SN 210-59200 to 64897 C: SN U2060276 to 0914, SN P2060001 to 0419 D: SN P2060420 to 0647 E: SN 20700001 and on, SN U2060438 to 2199 SN TP2060161 to 0647, SN T21000001 to 64136 F: SN 210-00001 to 64897, SN 207 00001 to 00788 G: SN 210-00001 to 64897, SN U20602200 to 07020 H: SN 210-00001 to 60089, SN 20700001 to 00788 SN TP206161 to 0647 I: SN 21060090 to 64135, SN U20602200 to 07020 J: SN 21063700 to 64535 with air conditioning K: SN 210-64136 and on, SN 21064136-64535 with air conditioning L: SN 210-64136 and on, SN 21064136-64535 with air conditioning M: SN 210-64136 and on, SN 21064136-64535 with air conditioning Inspect outlet stack for chaffing from the shroud. Inspect muffler for blisters or bulges under heat shroud. Inspect joints for freedom of movement and distortion. Cessna P206 AD 85-10-02 Applies S/N's P206-0001 thru P20600647 with Continental IO-520 engines. Inspect engine induction air box outboard duct for cracks. Inspection required for each 100 hrs of operation till repaired or replaced. Cessna P210N AD 83-23-03 R2 Applies to S/N's P21000001 thru P21000811 Inspect exhaust system for cracks. Inspection required for each 50 hrs of operation. AD does not apply when Inconel exhaust system installed. Cessna TP206 AD 71-09-07 R1 Applies to all S/N's Pressure test exhaust manifold in heat exchanger area, replace if leaks are found. Inspection required for each 50 hrs of operation. 11 10 8 13 12 6 6 12 12 12 12 12 11 22 14 3 4 7 9 5 Item Part Number Description Code 1250860-104 EXHAUST RIGHT FRONT RND END 1250860-203 EXHAUST LEFT SIDE RND END 1250860-72 EXHAUST RIGHT FRONT SQ END 1250860-201 EXHAUST LEFT SIDE SQ END 1250860-90 CROSSOVER RISER 1250860-100 RISER 1250860-110 TAILPIPE 1250860-109 TAILPIPE 1250860-78 TAILPIPE ADAPTER 1250860-105 TURBO INLET 1250860-150 SHROUD INBOARD 1250860-151 SHROUD OUTBOARD 1250860-156 EXHAUST RIGHT FRONT 1250860-157 EXHAUST LEFT SIDE 1250860-121 CROSSOVER RISER 1250860-117 RISER 1250860-164 TAILPIPE 1250860-163 TAILPIPE 1250860-168 TAILPIPE ADAPTER 1250860-122 TURBO INLET 1250860-29 CLAMP HALF 1250860-28 TAILPIPE ADAPTER CLAMP HALF 628260 GASKET 1250700-5 INDUCTION BOX ASSY 1250830-10 INDUCTION AIR BOX 1250700-7 INDUCTION AIR BOX 1250839-1 INDUCTION BOX ASSY AFT 1250830-37 INDUCTION BOX DUCT CTR 1250830-5 INDUCTION BOX DUCT FRT 1250830-29 INDUCTION BOX DUCT FRT 1250830-48 INDUCTION BOX DUCT FRT 1250735-1 INDUCTION BOX AFT 1250734-1 INDUCTION BOX CTR 1250830-42 INDUCTION BOX FRT VARIOUS SEAT BASE 1 2 3 4 5 6 7 7 8 9 10 11 1 2 5 6 7 7 8 9 12 13 - 14 - - - - - - - - - - - B B A A B A B A C D E F G H I J K L M INCONEL INCONEL