# STC SA4300WE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Flint Aero Inc, United States - Description: Installation of a 16.25 gallon usable fuel-containing wing tips. - Applied: February 6, 1981 - Status date: February 25, 2000 - Product: Aircraft, Single-Engine - Certification basis: Part 21 - Data sheets: [TCDS 3A21](https://openairdocs.org/tcds/3A21) - Certificate PDF: https://openairdocs.org/files/sha256/ad/23/ad2350c4bec737ff3f7ec00eed0af746b27ed9592ed6aab5580f6512da14268a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1A420DAD0F98E84785256CC2000E3B65.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA4300WE ## ADs that name it (0) None. ## Approved models (18) - The Cessna Aircraft Company 210G ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company 210H ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company 210J ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company 210K ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company 210L ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company 210M ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company 210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company 210R ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company P210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company P210R ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company T210G ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company T210H ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company T210J ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company T210K ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company T210L ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company T210M ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company T210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) - The Cessna Aircraft Company T210R ([TCDS 3A21](https://openairdocs.org/tcds/3A21)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA4300WE This certificate issued to: FLINT AERO, INC. 1942 Joe Crosson Drive El Cajon, California 92020-1236 Part 3 of the Civil Air Poegulations, Effective May 15, 1956 Original Product Type Certificate Number: 3A21 Make: CESSNA Model: See Page 3 of this STC Description of Type Design Change: Installation of 16.25 gallon usable fuel-containing wing tips in accordance with FAA sealed Flint Aero Master Drawing List MDL FA2101 revision N, dated January 21, 1987, or later approved FAA revisions. For 210G thru T210N Flint Aero, Inc., FAA approved Airplane Flight Manual Supplement dated January 16, 1984 or later FAA approved revisions is required as part of this installation. For 210R, T210R and P210R (See page 5). Limitations and Conditions: The limitations and conditions of Data Sheet 3A21 apply except as outlined on Page 3 of the STC. A copy of this STC must be included in the permanent records of each airplane modified in accordance with this STC. Models 210R, T210R and P210R limited to standard tank airplanes only. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. Date of Application: February 6, 1981 Date Reissued: Jan. 21, 1987, June 15, 1990, Feb. 25, 2000 Bute of isseunce: March 20, 1981 Date Amended: Jan. 20, 1984, Feb. 12, 1987 FEDERAL AVIATION By Direction of the Administrator Michael A Murphy (Signature TOMINISTRATO Manager, Technical & Administrative Suppor Staff, Los Angeles Aircraft Certification Office (Title) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA4300WE (A) 02/06/81 (I) 03/20/81 (A) 01/20/87, 06/15/90 (R) 01/21/87, 07/13/90, 02/25/2000 Models 210G T210G 210H T210H 210J T210J 210K T210K 210L T210L 210M T210M P210N 210N T210N 210R T210R P210R Limitations and Conditions: Fuel Capacity 123 gal. (121.5 gal. usable); two 45 gal. main tanks in wings at (+43) and two 16.5 gal. (16.25 gal. usable) aux. tank in wings at (+49.5). Placards The following placards are required in the locations noted: Adjacent to each auxiliary tank shut-off valve: 'Total Aux. fuel 33 U.S. Gals. (32.5 Gals. usable).Auxiliary fuel must be off during take-off, landing refueling, and when auxiliary is empty. Monitor main fuel tank gauge while transferring auxiliary fuel to prevent overfilling." Adjacent to each auxiliary tank filler: 16.5 U.S. Gal. *Min Grade Av. gasoline. Aux. Fuel switch must be off before filling.i *Insert grade number on placards for main tanks. Adjacent to the airspeed indicator (Models T210G, T210H, T210J, T210K, T210L, T210M, P210N, T210N, T210R and P210R only): Reduce Vne 5Knots per 1,000 feet above 18,000 feet maximum altitude 25,000 feet." In full view of the pilot: (a) For Models 210G, T210G, 210H, T210H, 210J, and T210J: "Design weights 3400 Ibs. max. provided each wing tip contains 7 gals. or more fuel. 3240 Ibs. max. with no fuel in wing tips" (b) For Models 210K T210K, 210L, T210L, 210M, T210M, and 210N: iDesign weights 3800 Ibs. max. provided each wing tip contains 7 gals. or more fuel and main tanks are 2/3 full or more. 3530 Ibs. max. with no fuel in wing tips." United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA4300WE (A) 02/06/81 (I) 03/20/81 (A) 01/20/87, 06/15/90 (R) 01/21/87, 07/13/90, 02/25/2000 Limitations and Conditions: (cont'd) (c) For Models P210N and T210N: Wing Tip Aux. Tank Weight Limits Aux. Fuel Tank Max. T. O. Weight Max. Ldg. Weight Either is less 3730 Ibs. 3530 Ibs. than 7 gals. Both are 7 gals. 4000 Ibs. 3800 Ibs. or more (d) For Models T210R and P210R: Wing Tip Aux. Tank Weight Limits Aux. Fuel Tank Max. T. O. Weight Either is less 3830 Ibs. than 7 gal. Both are 7 gal. 4100 Ibs. or more (e) For Model 210R: Wing Tip Aux. Tank Weight Limits Aux. Fuel Tank Max. T. O. Weight Either is less 3580 Ibs. than 7 gals. Both are 7 gals. 3850 Ibs. or more United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA3400WE (A) 02/06/81 (I) 03/20/81 (A) 01/20/87, 06/15/90 (R) 01/21/87, 07/13/90, 02/25/2000 Flight Manual (cont'd) For 210R, T210R and P210R Flint Aero, Inc., FAA Approved Airplane Flight Manual Supplement No. 210R(3) to applicable Cessna FAA Approved AFM/POH documents, dated February 12, 1987 or later FAA approved revisions is required as part of this installation. Limitation of The approval of this change in type design applies to the above noted Applicability Cessna models that are otherwise unmodified and should not be extended to other aircraft of these models on which other aircraft of these models on which other modifications are incorporated unless it is determined that the interrelationship between this change and any previously approved modification will introduce no adverse effect on the airworthiness of these aircraft. - END - ## Every issue (1) - February 25, 2000: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ad/23/ad2350c4bec737ff3f7ec00eed0af746b27ed9592ed6aab5580f6512da14268a) --- 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.