# STC SA01795CH - Type: Supplemental type certificate - Status: Current, Amended - Holder: Wipaire Inc., United States - Description: For Model AT-802A: Installation of Wipaire Model 10000 Amphibious Floats in accordance with Wipaire, Inc. Installation Drawing No. 7D1-4251, No Revision, dated January 13, 2003, or later FAA approved revisions. Operations with the floats removed are permitted when the aircraft is modified in accordance with Wipaire, Inc. Installation Drawing No. 7D1-4405, No Revision, dated January 13, 2003, or later FAA approved revisions. For Model AT-802: Installation of Wipaire Model 10000 Amphibious Floats in accordance with Wipaire, Inc. Installation Drawing No. 1003231, Revision A, dated June 12, 2008, or later FAA approved revisions. Operations with the floats removed are permitted when the aircraft is modified in accordance with Wipaire, Inc. Installation Drawing No. 1003406, Revision 01, dated July 15, 2008, or later FAA approved revisions. - Applied: May 9, 2001 - Status date: July 15, 2026 - Product: Aircraft, Small Airplane - Certification basis: Part 23 - Data sheets: [TCDS A19SW](https://openairdocs.org/tcds/A19SW) - Certificate PDF: https://openairdocs.org/files/sha256/04/33/043345ebb6b324acc5b97b40d52af0a8f6a5602a707b06c306889e5fffdf2ced - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115860335220260728134650.0001 - DRS record last changed: July 28, 2026 - Page: https://openairdocs.org/stc/SA01795CH ## ADs that name it (3) - [AD 2026-16-12](https://openairdocs.org/ad/2026-16-12): Horizontal stabilizer structure; Horizontal stabilizer miscellaneous structure; Vertical stabilizer structure · Air Tractor AT-802 and AT-802A. Effective Aug 31, 2026. Named in the applicability - [AD 2024-16-06](https://openairdocs.org/ad/2024-16-06) (historical): Horizontal Stabilizer Structure; Horizontal stabilizer, Spar/Rib; Horizontal Stabilizer Miscellaneous Structure; Vertical Stabilizer Structure · Air Tractor AT-802 and AT-802A. Effective Sep 4, 2024. Named in the applicability - [AD 2023-15-07](https://openairdocs.org/ad/2023-15-07) (historical): Horizontal Stabilizer Structure; Horizontal stabilizer, Spar/Rib; Horizontal Stabilizer Miscellaneous Structure; Vertical Stabilizer Structure · Air Tractor AT-802 and AT-802A. Effective Aug 9, 2023. Named in the applicability ## Approved models (2) - Air Tractor Inc. AT-802 ([TCDS A19SW](https://openairdocs.org/tcds/A19SW)) - Air Tractor Inc. AT-802A ([TCDS A19SW](https://openairdocs.org/tcds/A19SW)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number This certificate issued to: SA01795CH Wipaire, Inc. 1700 Henry Avenue - Fleming Field South St. Paul, MN 55075 Part 23 Title 14, Code of Federal Regulations A19SW Air Tractor, Inc. AT-802; AT-802A 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission. (See continuation sheet 3 of 5 for additional Limitations and Conditions) 05/09/2001 03/14/2003 10/08/2003 09/29/2008 04/15/2010 for Jason S. Deutschman Acting Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 5 For Model AT-802A: Installation of Wipaire Model 10000 Amphibious Floats in accordance with Wipaire, Inc. Installation Drawing No. 7D1-4251, No Revision, dated January 13, 2003 or later FAA approved revisions. Operations with the floats removed are permitted when the aircraft is modified in accordance with Wipaire, Inc. Installation Drawing No. 7D1-4405, No Revision, dated January 13, 2003, or later FAA approved revisions. (See continuation sheet 3 of 5 for the remaining Description of Type Design Change) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number Date o transfer: SA01795CH 07/15/2026 5 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA01795CH 07/15/2026 Date Amended (continued): 07/08/2011; 07/15/2026 Description of Type Design Change (continued): For Model AT-802: Installation of Wipaire Model 10000 Amphibious Floats in accordance with Wipaire, Inc. Installation Drawing No. 1003231, Revision A dated June 12, 2008, or later FAA approved revisions. Operations with the floats removed are permitted when the aircraft is modified in accordance with Wipaire, Inc. Installation Drawing No. 1003406, Revision A, dated March 11, 2009, or later FAA approved revisions. Limitation and Conditions (continued): 3. The following FAA approved Airplane Flight Manual Supplements (AFMS), or later FAA approved revision, are required with this installation: Document No. A/C Model & Operation Type Approval Date POHSA01795CH-A-1 AT-802A Amphibian March 13, 2003 POHSA01795CH-A-5 AT-802A Landplane October 7, 2003 POHSA01795CH-A-3 AT-802 Amphibian September 29, 2008 POHSA01795CH-A-4 AT-802 Landplane September 29, 2008 POHSA01795CH-A-2 AT-802A Amphibian* June 9, 2009 POHSA01795CH-A-6 AT-802 & AT-802A Amphibian** June 4, 2026 *with PWC PT6A-67F Engine (1600 SHP) **with Wipaire Scoop Position Monitor 4. For Model AT-802, Amphibious Operation: Airspeed, Maximum Weight, and C.G.Range are limited to the following: a. AIRSPEED LIMITS: Never Exceed (VNE) 160 KCAS (158 KIAS) Maximum Structural Cruising (VNO) 145 KCAS (143 KIAS) Maneuvering (VA) at 11,500 lbs. 123 KCAS (123 KIAS) Maximum Flap Extended (VFE) 123 KCAS (122 KIAS) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA01795CH 07/15/2026 Limitation and Conditions (continued): b. MAXIMUM WEIGHT: Takeoff from Land 16,000 lbs. Takeoff from Water 11,500 lbs. Landing on Land or Water 11,500 lbs. Scooping Operations 16,000 lbs. c. C.G. RANGE: (+24.5) to (+27.0) at 16,000 lbs. (+24.5) to (+28.1) at 14,000 lbs. (+26.0) to (+29.5) at 11,500 lbs. or less. Straight line variation between points given. 5. For Model AT-802A, Amphibious Operation: Airspeed, Maximum Weight, and C.G.Range are limited to the following: a. AIRSPEED LIMITS: Never Exceed (VNE) 160 KCAS (155 KIAS) Maximum Structural Cruising (VNO) 145 KCAS (140 KIAS) Maneuvering (VA) at 11,500 lbs. 126 KCAS (121 KIAS) Maximum Flap Extended (VFE) 123 KCAS (125 KIAS) b. MAXIMUM WEIGHT: Takeoff from Land 16,000 lbs. Takeoff from Water 11,500 lbs. Landing on Land or Water 11,500 lbs. Scooping Operations 16,000 lbs. c. C.G. RANGE: (+24.5) to (+27.0) at 16,000 lbs. (+24.5) to (+28.1) at 14,000 lbs. (+26.0) to (+29.5) at 11,500 lbs. or less. Straight line variation between points given. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA01795CH 07/15/2026 Limitations and Conditions (continued): 6. For Landplane Operation: Airspeed, Maximum Weight, and C.G.Range are limited to that of the standard Air Tractor Models AT-802 and AT-802A in the fire bomber configuration. Models AT-802 & AT-802A, Certification Basis: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for Make: Air Tractor, Inc. Models: AT-802 & AT-802A Aircraft is as follows: (1) The type certification basis for Make: Air Tractor, Inc. Models: AT-802 & AT-802A aircraft is shown on TCDS A19SW for parts not changed or not affected by the change. (2) The certification basis for parts changed or affected by the change since the reference date of application 05/09/2001, is based upon Part 23 as amended by Amendment 23-42 with the exception of those above amendment 23-42 listed below. Regulations at later amendment than 23-42: 14 CFR Part 23.201 amdt 23-50 14 CFR Part 23.203 amdt 23-50 14 CFR Part 23.207 amdt 23-50 - END - ## Every issue (4) - July 15, 2026: Amended, Current. [certificate](https://openairdocs.org/files/sha256/04/33/043345ebb6b324acc5b97b40d52af0a8f6a5602a707b06c306889e5fffdf2ced) - July 8, 2011: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/23/19/2319fd146316600f10107642f959ce12facf0450e5b63065c782ec05b0e5485a) - April 15, 2010: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/ec/d1/ecd19dd3b9dcb5b04eebe6b7da99e1b0566b47f37fd520d669091ec88df09805) - September 29, 2008: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/3e/a7/3ea7876b5afc35a2f5072d08e4386c1aa2a62abc358e5846eb1891be87727c6c) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.