STC SA2862WE

SHOOCO / WE Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA28621E This certificate issued to: Flint Aero Certifies that the change in the type design for the fellowing product with the limitations and conditions thereforusspecified heronmelethe virearhiness requirementif Puri 3 eftle CIVil Air Regulalions, effective May 15, 1956 and Paragraph 3.112 effective October 1, 1959.

Original Product - Typeterificate Numben: 3A21 Make: Cessna Mutei:

210G, T210G, 210H, 1210H, 2100, 12100, 210K, Description of Type Design Change: T210N T210K, 210L, T21OL, 210M, T210M, P21ON, 210N, Installation of larger fuel-containing wing tips in accordance with FAA sealed Flint Aero Data List No. DL FA2101.

Limitations and Conditions: of Data Sheet 3A21 apply, except as outlined on Page 3 of this STC. A copy of this SiC must be included in the permanent records of each airplane modified in accordance with this STC.

Date of Application: August 7; 1973 Jule missued: March 8, 1976 Date of Issuance: Date Amended: 9/26/75, 3/8/76, 3/11/77, March 22, 1974 4/28/77, 5/3/78, 3/27/79; 7/23/73 FEDERAL AVIATION Bry direction ¿ The j. Adminiatrater Lammata ( Signature ) TOMINISTRA ON •Chiel Aircraft Engineering Division (Title) 47 FAA FoRM 8110-2 (10-68)

mied Starte of Scrice 03/22/74 (1) Department of Transportation Federal Aviation Administration 09/26/75 (A) 03/08/76 (R) Supplemental Type Certificate 03/11/77 (A) 04/28/77 (A) 05/03/78 (A) (Continuation Sheet) 03/27/79 (A) 07/23/79 (A) Number: SA2862WE Limitations and Conditions:

Fuel Capacity 118 gal. (117 gal. usable); two 45 gal. main tanks in wings at (+43) and two 14 gal. aux. tanks in wings at (+49.5).

Placards The following placards are required in locations noted:

Adjacent to each auxiliary tank shutoff valve:

'Aux. fuel 14 U.S. Gal. Transfer aux. fuel only in level flight when main tank is half empty and when main tank is not supplying engine. Aux. fuel switch must be off during take-off, landing, filling and when empty."

Adjacent to each auxiliary tank filler: '14 U.S. Gal.

before rilling gasoline. Aux. Fuel switch must be off *Insert grade number on placards for main tanks.

Adjacent to the airspeed indicator (Models T210G, 1210H, 721N, T2he 3 MPH per 1,000 feet above 18,000 feet." "Reduce V 1210L, T210M, P2ION, and 1210N only):

In full view of the pilot:

(a) For Models 210G, T210G, 210H, T210H, 210J and T2100:

"Design weights 3400 lbs. max. provided each wing tip contains 7 gals. or more fuel. 3240 1bs. max.

with no fuel in wings tips."

(b) For Models 210K, T210K, 210L, T210L, 210M, T210M, and 210N:

"Design weights 3800 lbs, max. provided each wing tip contains 7 gals. or more fuel and main tanks are 2/3 full or more. 3530 lbs. max. with no fuel in wing tips."

FAA FORM 8110-2-1 (10-69) PAGE 3 OF 4 PAGES C FAA AC 73-2651

*nicol Statos of Surica 03/22/74 (1) Department of Transportation Federal Aviation Administration 09/26/75 (A) Supplemental Type Certificate 03/08/76 (R) 03/11/77 (A) 04/28/77 (A) (Continuation Sheet) 05/03/78 (A) 03/27/79 (A) 07/23/79 (A) Number: SA282WE Limitations and Conditions: (continued)

(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 1bs.

than 7 gals.

Both are 7 gals. 4000 1bs. 3800 1bs.

or more Limitation of The approval of this change in type design applies to the Applicability above noted Cessna models that are otherwise unmodified and should not be extended to other aircraft of these models on which other modifications are incorporated unless it is determined ihat the interrelationship between this change and any previously approved modification will introduce no adverse effect on the airworthiness of these aircraft.

END 47 PAGE 4 OF 4 PAGES C FAA AC 73-2631