STC SA1038SO

SA1038SO Outpost X Aviation, Inc.

111 E. Seminole Ave.

Bushnell, FL 33513 * * * * See attached FAA Approved Model List (AML) No. SA1038SO for list of approved airplane models and applicable airworthiness regulations.

Installation of Aqua Model 1500 floats in accordance with CAPRE, Inc. Drawing List No. P-1, Revision B, dated December 15, 1978, or later FAA approved revision for J3C-65 or J3C-65S. Installation of Aqua Model 1500 floats in accordance with CAPRE, Inc. Drawing List No. P-1, Revison D, dated December 3, 1980 or later FAA approved revision for PA-11, PA-11S, J3F-65, and J3F-65S. Note that additional placards are required to be installed.

(See Continuation Sheet 3 of 11) April 1, 1978 11/15/2023; 04/30/90; 02/10/1988; 08/21/1984 December 20, 1978 12/17/1980; 06/22/1982; 03/21/1994 for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 11

SA1038SO 11

SA1038SO Date of Issuance: 12/20/1978 Date Amended: 12/17/1980; 06/22/1982; 03/21/1994 Date Reissued: 11/15/2023; 04/30/90; 02/10/1988; 08/21/1984

This approval should not be extended to other specific aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage.

Models J3C-65, J3C-65S

Engines: 1. With STC SA338CE installed. (Continental C-90-12F engine - 90 HP = T.O. - 80 HP = ALL OTHER OPS.)

2. C-85-8, -12 Engine limits: Takeoff, 2575 r.p.m. (85 h.p.)

All other operations, 2525 r.p.m. (80 h.p.)

Fuel: 80 min. octane aviation gasoline Oil capacity: 4 1/2 qts.

Note: C-85 engine installation may be accomplished using original engine installation components or in accordance with Kit and Dwg. P4-400 by 0ng Aircraft Corporation, P.O. Box 214, Kansas City, Missouri.

PROPELLERS: For C-85-8, -12

(a) Propeller - Wood (fixed or adjustable pitch).

(continued on page 4) 3 11

SA1038SO Date of Issuance: 12/20/1978 Date Amended: 12/17/1980; 06/22/1982; 03/21/1994 Date Reissued: 11/15/2023; 04/30/90; 02/10/1988; 08/21/1984

Limitations and Conditions (continued from page 3 of 11):

Models J3C-65, J3C-65S continued:

(b) Propeller - McCauley 1A90CF or 1B90CM.

Limits:

Static r.p.m. at maximum permissible throttle setting:

Not over 2550, not under 1950.

No additional tolerance permitted.

Diameter: Not over 71 in., not under 68.5 in.

Propeller - Hartzell ground adjustable hub HA12U, blades 7414 to 6814 or 7214M to 6814M, eligible on all models and all engines at diameter and static r.p.m. limits shown on specification for fixed pitch wood propellers. Where no limits are specified use those of the propeller being replaced.

3. C-90-8F Engine limits: Takeoff 2475 r.p.m. (90 h.p.)

All other operations, 2375 r.p.m. (80 h.p.)

Fuel: 80 min. octane aviation gasoline Oil capacity: 5 qt.

Propeller limits:

Static r.p.m. (with Item 101, 5 or 6 propellers) Reference Aircraft Specification No. A-691.

Not over 2300, not under 2100 (seaplane).

No additional tolerance permitted.

Carburetor heat systems must be modified to provide required heat (continued on page 5) 4 11

SA1038SO Date of Issuance: 12/20/1978 Date Amended: 12/17/1980; 06/22/1982; 03/21/1994 Date Reissued: 11/15/2023; 04/30/90; 02/10/1988; 08/21/1984

Limitations and Conditions (continued from page 4 of 11):

Models J3C-65, J3C-65S continued:

rise. Approved modification made by M. Mullis, York, South Carolina.

Propellers: For C-90-8F Engines

(a) Propeller - McCauley 1B90 or 1A90 Diameter: Not over 71 in., not under 69.5 in.

(b) Propeller - McCauley 1A90 or 1B90 Diameter: Not over 71 in., not under 69.5 in.

(c) Propeller - Wood (fixed or adjustable pitch) Diameter: not over 76 in., not under 70 in.

C. G. Limits: See Aircraft Specification No. A-691.

1. For all airplanes modified per Specification No. A-691 to meet 1220 lbs. maximum weight - the seaplane modification C.G. Limits are as follows:

+10.6" to +18.5" at 1300 lbs or less

2. For airplanes not modified per Specification No. A691, C.G. limits are:

+10.6" to 18.5" at weights listed in the Specification.

(continued on page 6) 5 11

SA1038SO Date of Issuance: 12/20/1978 Date Amended: 12/17/1980; 06/22/1982; 03/21/1994 Date Reissued: 11/15/2023; 04/30/90; 02/10/1988; 08/21/1984

Limitations and Conditions (continued from page 5 of 11):

Models J3C-65, J3C-65S continued:

Maximum Weight: See data included in C.G. Limits above.

Placards: In addition to those in the basic Airplane Flight Manual, the following placards must be displayed on the instrument panel in full view of the pilot:

"SEAPLANE IS APPROVED FOR NORMAL CATEGORY ONLY"

"CAUTION RETRACT WATER RUDDER FOR FAST TAXIING, TAKEOFF, AND LANDINGS"

"SALT WATER OPERATION PROHIBITED" (*)

(*) NOTE: Placard is not applicable if corrosion-proofing has been accomplished.

Weight and Balance: Airplane Weighing Diagram

Models PA-11, PA-11S

Engines: (1) Continental C-90-12-F installed per STC SA338CE

(2) C-90-8F (Bendix-Stromberg carburetor, Continental Part No. 530726 and engine cooling baffles per Piper Dwg. 11258 change E are required with this engine.)

(continued on page 7) 6 11

SA1038SO Date of Issuance: 12/20/1978 Date Amended: 12/17/1980; 06/22/1982; 03/21/1994 Date Reissued: 11/15/2023; 04/30/90; 02/10/1988; 08/21/1984

Limitations and Conditions (continued from page 6 of 11):

Models PA-11, PA-11S continued:

(3) Continental O-200 (with McCauley 1B90 propeller installed per STC SA1436SW for PA-11, Serial No. 11-1364 only.)

Engine limits: Static r.p.m. 2300-2400.

Propeller diameter limits: 69.75 - 71.25 in.

Propellers: (for C-90-8F)

Propeller - McCauley 1B90 or 1A90 Diameter - Not over 71 in., not under 69.5 in.

Propeller - McCauley 1A90 or 1B90

Propeller - Koppers F200/00-73E Parts List Assembly No. 4348 Low pitch setting 12.5˚ measured at 24 in. sta.

Static r.p.m. at maximum permissible throttle setting;

Not over 2425, not under 2375. No additional tolerance permitted.

Diameter: Not over 73 in., not under 71.5 in.

Installation and operation must be accomplished in accordance with Koppers "Installation Procedure and Operating Limitation" No. 33.

Propeller - Sensenich fixed pitch metal Model M76AS-2 Eligible with Items 311D(5) AND 311C(9) engines only.

Static r.p.m. at maximum permissible throttle setting (No additional tolerance permitted):

(continued on page 8) 7 11

SA1038SO Date of Issuance: 12/20/19 Date Amended: 12/17/1980; 06/22/1982; 03/21/1994 Date Reissued: 11/15/2023; 04/30/90; 02/10/1988; 08/21/1984

Limitations and Conditions (continued from page 7 of 11):

Models PA-11, PA-11S continued:

Not over 2425, not under 1950 Diameter: Not over 74 in., not under 70 in.

C.G. Limits: C.G. + 12.9 to 18.5" at all weights

Maximum Weight: PA-11 = 1220 lbs.

PA-11S = 1350 lbs.

Placards: In Addition to those in the basic Airplane Flight Manual, the following placards must be in full view of the pilot:

"SEAPLANE IS APPROVED FOR NORMAL CATEGORY ONLY"

"CAUTION RETRACT WATER RUDDER FOR FAST TAXIING, TAKEOFF, AND LANDINGS"

"SALT WATER OPERATION PROHIBITED" (*)

(*) NOTE: Placard is not applicable if corrosion-proofing has been accomplished.

Weight and Balance: Airplane weight diagram.

(continued on page 9) 8 11

Date of Issuance: 12/20/1978 Date Amended: 12/17/1980; 06/22/1982; 03/21/1994 Date Reissued: 11/15/2023; 04/30/90; 02/10/1988; 08/21/1984

Limitations and Conditions (continued from page 8 of 11):

Models J3C-65, J3C-65S, PA-11, PA-11S

For aircraft with 65 h.p. or 75 h.p. Continental engines installed per Aircraft Specification No. A-691, the limitations and conditions for seaplanes identified therein are applicable.

Models J3F-65, J3F-65S

Engines: With STC SA338CE installed [Continental C-90-12F engine (90 HP = T.O.

and 80 HP= ALL other ops)]

Propellers: With Continental C-90 Series engines only

(a) Propeller - Sensenich 72GK50 or any other fixed pitch wood propeller which is rated for the engine power and speed, and which meets the following limits:

Static r.p.m. at maximum permissible throttle setting (No additional tolerance permitted):

(Seaplane) Not over 2350, not under 2300 Diameter: Not over 72 in., not under 70.5 in.

(b) Propeller - Sensenich M76AM-2 fixed pitch metal Static r.p.m. at maximum permissible throttle setting (No additional tolerance permitted):

(Seaplane) Not over 2350, not under 2200 Diameter: Not over 74 in., not under 72.5 in.

(continued on page 10) 9 11 SA1038SO

SA1038SO Date of Issuance: 12/20/1978 Date Amended: 12/17/1980; 06/22/1982; 03/21/1994 Date Reissued: 11/15/2023; 04/30/90; 02/10/1988; 08/21/1984

Limitations and Conditions (continued from page 9 of 11):

Models J3F-65, J3F-65S continued:

C.G. Limitations: C.G. = 12.0" to 17.0" at all weights.

If placard "SOLO FLYING IN REAR SEATS ONLY" is installed:

C.G. = 10.0' to 14.5" at all weights.

NOTE 1. Current weight and balance report including list of equipment included in certificated weight empty, and loading instructions when necessary, must be in each aircraft at the time of original certification and at all times thereafter (except in the case of air carrier operators having an approved weight control system).

NOTE 2. Placard front cockpit, "SOLO FLYING FROM REAR SEAT ONLY". Placard may be removed if individual aircraft actual weight and balance shows that the approved C.G.

limits will not be exceeded under any loading condition.

Manufacturer recommends that all J-3 airplanes be flown solo from the rear seat.

Maximum Weight: 1200 lbs.

Placards: In Addition to those in the basic Airplane Flight Manual, the following placards must be in full view of the pilot:

(continued on page 11) 10 11

FAA Form 8110-2 (03/21) Page _ __ of United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

SA1038SO 11 11 Date of Issuance: 12/20/1978 Date Amended: 12/17/1980; 06/22/1982; 03/21/1994 Date Reissued: 11/15/2023; 04/30/90; 02/10/1988; 08/21/1984

Limitations and Conditions (continued from page 10 of 11):

Models J3F-65, J3F-65S continued:

"SEAPLANE IS APPROVED FOR NORMAL CATEGORY ONLY"

"CAUTION RETRACT WATER RUDDER FOR FAST TAXIING, TAKEOFF, AND LANDINGS"

"SALT WATER OPERATION PROHIBITED" (*)

(*) NOTE: Placard is not applicable if corrosion-proofing has been accomplished.

Weight and Balance: Airplane weight diagram.

ALL MODELS

A copy of this Certificate and FAA Approved Model List No. SA1038SO, issued March 21, 1994, or later FAA Approved revision, must be maintained as part of the permanent records for the modified aircraft.

The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

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