Supplemental Type Certificate for the Cessna 206 Stationair
Cessna 206 Stationair · Supplemental Type Certificate
Overview
This document is a Supplemental Type Certificate (STC) specifically for the Cessna 206 Stationair. It provides detailed information regarding modifications and alterations approved for this aircraft model. The STC is essential for ensuring compliance with aviation regulations and maintaining the airworthiness of the aircraft after modifications. It serves as a reference for maintenance personnel, pilots, and owners who need to understand the implications of the modifications covered under this certificate. The document outlines the approved changes, their installation procedures, and any limitations or operational considerations that must be adhered to following the modifications.
- The STC is specifically for the Cessna 206 Stationair.
- Modifications must be installed according to the specifications outlined in the STC.
- Operational limitations may include weight and performance restrictions post-modification.
- Regular maintenance checks are required to ensure continued compliance with the STC.
- Accurate record-keeping of modifications and inspections is essential for FAA compliance.
Document
Source
Originally published by www.airglas.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Supplemental Type Certificate
- Pages
- 12
- File size
- 487 KB
- Publisher
- www.airglas.com
Common. Rarer than 2% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna 206 Stationair.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Introduction
The introduction section outlines the purpose of the STC, which is to certify specific modifications made to the Cessna 206 Stationair. It emphasizes the importance of adhering to the approved specifications to maintain safety and compliance with FAA regulations.
Modifications Approved
This section lists the specific modifications that have been approved under the STC for the Cessna 206 Stationair. Each modification is described in detail, including the parts involved, installation instructions, and any necessary adjustments to the aircraft systems.
Operational Limitations
The operational limitations section details any restrictions that apply to the Cessna 206 Stationair following the modifications. This includes weight limits, performance changes, and any special operating procedures that must be followed to ensure safe operation.
Maintenance Requirements
This section outlines the maintenance requirements for the modifications approved under the STC. It specifies the intervals for inspections and any special tools or procedures that may be necessary for maintaining the modified aircraft.
Compliance and Record Keeping
The compliance section emphasizes the importance of maintaining accurate records of the modifications and inspections performed on the Cessna 206 Stationair. It provides guidance on how to document compliance with the STC and the importance of keeping these records accessible for FAA inspections.
Safety notes
- Failure to adhere to the approved modifications may result in safety hazards.
- Operational limitations must be strictly followed to ensure safe aircraft operation.
Full document text
: United States Of America Bepartment of Transportation - Federal Aviation Administration Supplemental Type Certificate This Certificate issued to Number SA02069AK Airglas, Inc. P.O. Box 190107 Anchorage, AK 99519-0107 certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part * of the * Regulations. Make: * Original Product Type Certificate Number: Refer to attached FAA Approved Model List (AML) No. SA02069AK Revision F dated June 5 2006, or later FAA approved revision, for approved airplane makes and models corresponding Type Certificate numbers, and applicable airworthiness regulations. Model: Decsription of Type Design Change: Fabrication and installation of the Airglas, Inc., Landes PA32-206LA Nose Fork equipped with Goodyear 8,50 x 6 tire (see Limitations and Conditions) in accordance with Airglas Master ata List Number PA32-206LA, Revision D, dated May 26, 2006, or later FAA approved revision Limitations and Conditions: Airplanes incorporating this design change may be equipped with 6.00-5, 7.00-6, 8.00-6, or Goodyear 8.50 5 pires on the nose and main wheels. The nose tire must be the same size as the main tires in all installations. AMPL An FAA approved Supplemental Flight Manual (SAFM) or Airplane Flight Manual (AFMS) modification. Supplement is a required part of (AML) No. SA02069AK for the require and model. Compatibility of this design determined by the installer. When Cessna models U206F, TU206F, U206 Refer to FAA Approved Model List A FMS document applicable to each approved make hange with previously approved modifications must be tilizing SAFM/AFMS No. AE96-5FM, Revision C, with and TU206G, this STC has been found compatible with STC No. SA4366WE. If the holder agrees to permit another person to use this Certificate to alter a product, then the permission: 14 CFR Part 43 is adequate shall give that person written evidence of such asure continued airworthiness of this modification. This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Date reissued: May 18, 2000 Date amended: May 18, 2000; September 15, 2000; November 30, 2001; January 5, 2004; June 5, 2006 Date of application: May 05, 1995 Date of issuance: .. January 29, 1997 Federal Aviation Podministratio By direction 17. FEDERAL AVIATION TOMINISTRATIO By direction of the Administrator Holt (signature) Gregory J. Holt Manager Anchorage Aircraft Certification office (Title) Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA Form 8110-2 (20-68) Page 1 DE This certificate may be transferred in accordance with FAR 21.47. Airglas, Inc. P. O. Box 190107 Anchorage, AK 99519 FAA Approved Model List (AML) No. SA02069AK Description of Type Design Change: Installation of Airglas, Inc. P/N PA32-206LA Nose Fork Rev Level Original Rev A Rev B Rev C Revision History Date January 29, 1997 May 18, 2000 September 15, 2000 November 30, 2001 Rev D June 18, 2002 Rev E January 5, 2004 Rev F June 5, 2006 Rev G August 22, 2006 TCDS Certification Basis 3A19 CAR 3 Installation Instructions AE06-4IRI Flight Manual Supplement AE00-1FM, Rev B, dated May 26, 2006 or later FAA Approved revision A13CE 3A17 3A12 AMPLI CAR 3 AE06-41RI AE06-41R! AE06-4IRI Make/Model Cessna: 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, A150K, 150L, A150L, 150M, A150M, 152, A152 Cessna: 172, 172A, 172B, 172C, 172D, 172E, 172F,172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S Cessna: 175, 175A, 175B, 175C, Cessna: 177, 177A, 177B Cessna: 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182S, T182 Cessna: 206, P206, P206A, P206B, P206C, P206D, P206E, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, TP206A, TP206B, TP206C, TP206D, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, 206H, T206H, A4CE CAR 3 AE96-1IRI Page 1 of 2 AE00-1FM, Rev B, dated May 26, 2006 or later FAA Approved revision AE00-1FM, Rev B, dated May 26, 2006 or later FAA Approved revision AE00-1FM, Rev B, dated May 26, 2006 or later FAA Approved revision AE00-1FM, Rev A, dated November 30, 2001 or later FAA Approved Revision. AE96-5FM, Rev. C, dated January 4, 2004, or later FAA Approved Revision Airglas, Inc. P. O. Box 190107 Anchorage, AK 99519 FAA Approved Model List (AML) No. SA02069AK Description of Type Design Change: Rev Level Original Installation of Airglas, Inc. P/N PA32-206LA Nose Fork Rev. A Rev. B Rev C Revision History Date : January 29, 1997 May 18, 2000 September 15, 2000 November 30, 2001 Rev D June 18, 2002 Rev E January 5, 2004 Rev F June 5, 2006 Rev G August 22, 2006 Make/Model TCDS Cessna: A16CE 207, 207A, T207, T207A Cessna: 3A21 CAR 3 AE06 4IRI 210-5 (205), 210-5A (205A) Certification Basis 14 CFR 23 FAA Approved: Manager, Anchorage Aircraft Certification Office Federal Aviation Administration- Anchorage, Alask Date: SAMPLE Installation Instructions AE00-21RI Flight Manual Supplement AE00-4FM; Rev. A, dated November 30, 2001 or latter FAA Approved Revision. AE00-1FM, Rev B, dated May 26, 2006 or later FAA Approved revision Page 2 of 2 Airglas, Inc. PO Box 190107 Anchorage, AK 99519 Phone 907-344-1450 Fax 907-349-4938 DOCUMENT AE00-1FM FAA-APPROVED SUPPLEMENTAL AIRPLANE FLIGHT MANUAL OR AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR CESSNA MODELS: Registration Numbers Serial Number: EQUIPPED WITH AN AIRGLAS PA32-206LA NOSE FORK MPLE Model Number: This document must be carried in the airplane at all times when the Airglas PA32-206LA Nose Fork Assembly is installed in accordance Supplemental Type Certificate Number SA02069AK. The information contained in this document supplements or supersedes the
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information made available to the operator by the manufacturer in the form of clearly stated placards, markings, or manuals as required by CAR 3.777(b), or in the form of an FAA approved Airplane Flight Manual as required by FAR 21.5, only in those areas listed herein. For limitations, procedures, and performance information not contained in this document, consult the basic placards, markings, or manuals, or the basic FAA approved Airplane Flight Manual. FAA Approved: Manager, Anchorage Aircraft Certification Office Federal Aviation Administration Anchorage, Alaska FAA Approved DATE: JUN 5 2006 Page 1 of 5 Airglas, Inc. 3500 O'Malley Rd Anchorage, AK 99516 Revision No. Pages Affected Initial Rel. 1-5 A 1-5 B 1-5 FAA Approved 5 2006 DATE: .............. Airglas, Inc. PO Box 190107 Anchorage, AK 99519 Phone 907-344-1450 Fax 907-349-4938 AFM Supplement for Cessna 150, 152, 172, 175, 177, 182, 205 LOG OF REVISIONS Ser. # Reg. # Description Original Added other tire sizes Added 150,152,172,175,107,205 SAMP FAA Approved Date 09-03-00 11-30-01 GJH JUN 5 2006 Page 2 of 5 ................. Airglas, Inc. 3500 O'Malley Rd Anchorage, AK 99516 Airglas, Inc. PO Box 190107 Anchorage, AK 99519 Phone 907-344-1450 Fax 907-349-4938 AFM Supplement for Cessna 150, 152, 172, 175, 177, 182, 205 Ser. # Reg. # SECTION I. General This aircraft is equipped with an Airglas PA32-206LA Nose Fork. This Nose Fork replaces the previous Nose Fork and allows an 8.50-6 tire to be used (other size tires are acceptable). The Nose Fork is made out of 4130 chromoly steel that is heat treated. The tire inflation pressure is unchanged from the manufacturer's recommendations. SECTION III. Limitations 1. 2. Nose wheel tire - A tire clearance of at least 1/2 inch from the four (4) bolts on the Nose Fork is required. SAMPL Tire size on the main gear: The main gear tires must be the same size as the nose gear tire (8.50-6 maximum). SECTION III. Emergency Procedu No Change SECTION IV. Normal Procedures 1. PREFLIGHT INSPECTION A. Nose Fork wheel & tire attaching hardware -- Secure B. Nose Fork block attaching hardware -- Secure C. Nose Fork tire -- Proper Inflation FAA Approved DATE: JUN 5 2006 Page 3 of 5 .................. Airglas, Inc. 3500 O'Malley Rd Anchorage, AK 99516 Airglas, Inc. PO Box 190107 Anchorage, AK 99519 Phone 907-344-1450 Fax 907-349-4938 AFM Supplement for Cessna 150, 152, 172, 175, 177, 182, 205 Ser. # Reg. # ............. 2. INFLIGHT PROCEDURES A. Landing: The Nose Fork and 8.50-6 tire increase the length of the nose gear by approximately 4". Pilots should ensure that all landings are accomplished in a nose high attitude similar to the soft field approach attitude. CAUTION During landing there is an increased possibility of wheelbarrowing or porpoising during landing. Pilots should ensure that all landings are accomplished in a nose high attitude similar to the soft field approach attitude. SAMP E SECTION V. 1. Performance Information Cruise: Cruise speeds are reduced up to 8 mph True Airspeed due to the increased size of the 8.50-6 tires. Pilots should reduce maximum range data by 5%. SECTION VI. Weight and Balance/Equipment List 1. Aircraft weight and balance records and equipment list have been updated to reflect this installation. SECTION VII. Systems Descriptions This airplane is equipped with an Airglas, Inc., PA32-206LA Nose Fork Assembly. The tire inflation pressure is unchanged from the manufacturer's recommendations. The tire and wheel are unchanged and wear indications should follow that specific manufacturer's recommendations. FAA Approved DATE: JUN 5 2006. Page 4 of 5 Airglas, Inc. 3500 O'Malley Rd Anchorage, AK 99516 Airglas, Inc. PO Box 190107 Anchorage, AK 99519 Phone 907-344-1450 Fax 907-349-4938 AFM Supplement for Cessna 150, 152, 172, 175, 177, 182, 205 Ser. # Reg. # SECTION VIII. Handling, Servicing and Maintenance All handling procedures for this modification are standard. The PA32-206LA Nose Fork Assembly may be serviced and maintained in accordance with Part 43 of the Federal Aviation Regulations (FAR 43). Servicing and maintenance in accordance with FAR 43 is adequate to insure the continued airworthiness of this modification. Information on installing the PA32- 206LA Nose Fork Assembly can be found in the Landes Nose Fork Installation Instructions, original issue dated November 5, 1996 or later FAA approved revision. SAMP FAA Approved DATE: JUN 5 2006 Page 5 of 5 Airglas, Inc. PO Box 190107 Anchorage, AK 99519 Phone 907-344-1450 Fax 907-349-4938 www.airglas.com AE06-4IRI LANDES Nose Fork Installation/Removal Instructions Cessna 150, 152, 172, 175, 177, 182, 205 Series Page 1 of 3 Original Issue: 09-03-00 Revision A: 11-20-01 Revision B: 05-11-06 Registration Number_ 1. 2. 3. 1. 2. 3. Aircraft Model WHEEL REMOVAL, LANDES NOSE FORK Weight or tie down tail of aircraft to raise nose wheel off of the ground. Remove axle rod (Part No. PA32-206L-4) using Airglas drawing PA32-206LA as a reference. Use a rod or long punch inserted through one bucket (Part No. PA32-206L-6) to tap the opposite bucket out of the axle. Remove both buckets and pull nose wheel from fork. AMPL If speed fairing is installed, it may be necessary to loosen the wheel scraper to remove the wheel. WHEEL INSTALLATION, LANDES NOSE FORK Install nose wheel in fork and install the two buckets (Part No. PA32-206L-6) using Airglas drawing PA82-206LA as a reference. Install axle rod (Part No. PA32-206L-4) using Airglas drawing PA32-206LA as a reference. Tighten axle rod (Part No. PA32-206L-4) until a slight bearing drag is obvious when the wheel is turned. Back off 1/4 turn so that wheel turns freely. WEIGHT AND BALANCE/EQUIPMENT LIST 1. PA32-206LA Nose Fork Assembly: Cleveland 40-76A Wheel Assembly: 13.5 lbs 4.0 lbs Nose Tire (use actual weight of tire): Total Weight Ibs lbs @ C-150 Station. -11.00 in. C-152 Station. -10.80 in. C-172 thru K -7.50 in. Page 2 of 3 Airglas, Inc. PO Box 190107 Anchorage, AK 99519 Phone 907-344-1450 Fax 907-349-4938 www.airglas.com LANDES Nose Fork Installation/Removal Instructions Cessna 150, 152, 172, 175, 177, 182, 205 Series WEIGHT AND BALANCE/EQUIPMENT LIST (CONTINUED) PA32-206LA Nose Fork Assembly: Cleveland 40-76A Wheel Assembly: Nose Tire (use actual weight of tire): 13.5 lbs 4.0 lbs Total Weight Ibs lbs @ C-172L thru S -6.80 in. C-P172D R172E,F,G,H,J,K -7.00 in. C-175 thru C -7.00 in. C177 thru B -6.80 in. C-182 thru S, T182 -7.50 in. C-205, 205A -7.50 in. ARI RLE LANDES Block Installation/Removal Instructions 1. Remove lower nose strut using procedures outlined in the appropriate Cessna Maintenance Manual for that model of aircraft. 2. Remove torque link fitting bolt and fork bolt as required. Note: Heavy duty and late model combine fork and link fitting. (See special instruction #1 3. Drive fork and link from lower strut tube using hydraulic press. Do not push on base plug, press on tube periphery only. 4. Heat Landes Block with electric heat gun or oven to a maximum of 200° Fahrenheit. 5. Mark strut tube holes with magic marker lines extending upward approximately 2". This will aid in aligning block bolt holes with the holes in strut tube. Some models have a 3/8" hole. (See special instruction #2.) · 6. After block temperature has stabilized, quickly slide block onto tube. (Hydraulic press will often be needed to accomplish this operation.) Use magic marker guides to help align the bolt holes. Drive a 5/16” bullet through hole to ensure final alignment while still hot. 7. Assemble strut with new seals using appropriate Cessna Maintenance Manual for the particular aircraft model. Page 3 of 3 Airglas, Inc. PO Box 190107 Anchorage, AK 99519 Phone 907-344-1450 Fax 907-349-4938 www.airglas.com LANDES Nose Fork Installation/Removal Instructions Cessna 150, 152, 172, 175, 177, 182, 205 Series SPECIAL INSTRUCTIONS: #1. On Standard nose struts the lower hole must be removed by cutting approximately 1" off of the lower portion of the tube. Alternately the tube may be replaced with a heavy duty model. #2. Some models use a 3/8" hole in the block and tube combined with a bushing. The bushing must be cut and ground to fide flush with the outside diameter of the strut tube. This installation requires the disassembly of the block and tube to replace o-ring seal on base plug. SAMP Cessna AVALASKA, INC. 4340 Postmark Drive, Anchorage, AK 99502 (907) 248-7070 FAX (907) 248-7771 Mr. Gary Landes Airglas Engineering Box 190107 Anchorage, AK 99519 January 24, 2002 Gary, REFERENCE ONLY SERIAL BLOCK In researching the different part numbers for nose wheel barrels we have come up with the following: MODEL FORK AND BARREL YOUR COST 206/207 HD ALL 206/207 STD ALL 206H STD ALL ASSEMBLY P/N 1243610-28 SK205-3 1243610-7 BARREL " ONLY P/N LIST PRICE 1242003-5 $524 $497.8 4300304 5539 $431.2 43003-4 $539 $431.2 182 53-62 33000-53007 0594300-206 0543006-6 $744 $669.6 182 53-62 53008 AND ON 0543039-20 0543040-2 NLA 182 62-73 STD 53599-57625 0743600 4 0543006-5 $379 $360.05 182 62-73 HD 53599-57625 0743600-201 0743611-3 NLA 182 62-73 STD 57626-62465 0743624 0543006-5 $379 $360.05 182 62-73 HD 57626-60825 074362 201 0743611-3 NLA 182 74-86 62466 AND ON 0543006-5 $379 $360.05 182 96 AND ON ALL 14361-4 0543006-5 $379 $360.05 172 56-62 2800-47746 0543000-212 0543006-6 $744 $669.6 175 56-62 55001-56238 0543000-212 0543006-6 $744 $669.6 172 47747-49544 0543039-201 0543040-2 NLA 175 56239 71 0543039-201 0543040-2 NLA 172 63-74 STD 49545-54892 0543039-201 0543040-2 NLA 172 63-74 STD 54893-63458 0543062-201 0543040-2 NLA. 172 63-74 HD 172 63-74 HD 172 75-86 49545-54892 54893-63458 0543062-200 0543031-2 NLA 0543062-203 0543040-2 NLA 63459 AND ON 0543062-201 0543040-2 NLA 172 96 AND ON ALL 0543062-201 0543040-2 NLA The items marked NLA are no longer available from Cessna, we must purchase the next higher assembly number. Mark is talking to Cessna about making the NLA barrels available for retail sale. We can install your blocks on the barrels for $35.00 each if you will do it in a quantity of two or more at a time. Sincerely Belleau REFERENCE ONLY Alaska's Cessna Source! CESSNA STAR
What's in the Cessna 206 Stationair TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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