STC SA876CE

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 3 5 SA876CE Civil Air Regulations.

Remove Continental 0-470-13 or 0-470-13A engine and propeller. Install Continental I0-470-N engine and Hartzell BHC-L2YF-4F/FC8468AR propeller in accordance with drawings listed in PDA 4479 drawing list dated October 6, 1972.

United Beechcraft FAA approved Airplane Flight Manual Supplement dated October 5, 1972 is required.

Beech A-45 (Military T-34A, B-45) This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. 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.

(See Continuation Sheets) November 15, 1972; April 15, 1996; March 26, 2007; April 12, 2013; November 16, 2016 April 6, 1972 October 5, 1972 5A3 Mark Fuller STC ODA administrator ODA-100129-CE

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 3 of

Date of Issuance: October 5, 1972 Date Reissued: November 16, 2016

The conditions and limitations of Aircraft Specification No. 5A3 apply except as follows:

A copy of this addendum and the STC are required to be maintained as part of the modified aircraft permanent records.

1. Model A45 (Military T-34A, B-45), approved October 5, 1972

Engine: Continental I0-470-N

*Fuel: 100/130 min. grade aviation gasoline

Engine Limits: For all operations 2625 rpm (260 hp)

Propeller and Propeller Limits: Hartzell BHC-L2YF-4F/FC8468AR Diameter: Not over 84 inches, not under 84 inches.

No cutoff allowed.

Pitch settings at 30 in. sta.: low 13.5°, high 30°

Powerplant Instrument Markings:

*Oil Temperature Gage: 107°C (225°F) Red Radial (Maximum) 24°C to 107°C (75°F to 225°F) Green Arc (Normal) 24°C (75°F) Red Radial (Minimum)

*Oil Pressure Gage: 100 PSI Red Radial (Maximum) 30 to 60 PSI Green Arc (Normal) 30 PSI Red Radial (Minimum)

*Fuel Pressure Gage: 19 PSI Red Radial (Maximum) 6 to 22 GPH Green Arc (Normal)

1.5 PSI Red Radial (Minimum)

*Fuel Capacity: 44 gal. (two 22-gal. wing tanks, 22 gal. usable in each tank at +80) 3 gal. unusable in each tank

Oil Capacity: 12 qts. (10 qts. usable) SA876CE 5

FAA Form 8110-2 (5/14) Page 4 of

SA876CE Date of Issuance: October 5, 1972 Date Reissued: November 16, 2016

*Cylinder Head Temp: 107°C to 238°C (225°F to 460°F) Green Arc (Normal) 238°C (460°F) Red Radial (Maximum)

*Tachometer: 1500 to 2625 RPM Green Arc (Normal) 2625 RPM Red Radial (Maximum)

*Manifold Pressure: 15 to 29.6 in. Hg. Green Arc (Normal)

29.6 in. Hg. Red Radial (Maximum)

Maneuvers: Recommended Entry Speeds

1. Stalls (except whip stalls) Use slow deceleration

2. Steep Turns Maximum - 150 knots (CAS)

3. Spins Use slow deceleration

4. Lazy Eights 115 knots (CAS)

5. Chandelle 130 knots (CAS)

6. Snap Rolls 95 knots (CAS)

7. Vertical Reversements 95 knots (CAS)

8. Loops, Cuban Eights & Immelmanns 150 knots (CAS)

9. Slow Rolls 115 knots (CAS)

Placards:

On instrument panel, front and rear: "ACROBATIC CATEGORY AIRPLANE, OPERATE IN ACCORDANCE WITH CAA APPROVED FLIGHT MANUAL. Do not lower landing gear or flaps above 109 knots TIAS. For recommended entry speeds, see Approved Acrobatic Maneuvering Placard and Airplane Flight Manual."

On right side panel, front and rear cockpit: "APPROVED ACROBATIC MANEUVERS (1) STALLS (EXCEPT WHIP STALLS) - USE SLOW DECELERATION (2) STEEP TURNS - MAXIMUM 150 KNOTS (3) SPINS - USE SLOW DECELERATION (4) LAZY EIGHTS - 115 KNOTS (5) CHANDELLE - 130 KNOTS (6) SNAP ROLLS - 95 KNOTS

(7) VERTICAL REVERSES - 95 KNOTS (8) LOOPS, CUBAN EIGHT AND IMMELMANNS - 150 KNOTS (9) SLOW ROLLS - 115 KNOTS"

On Fuel Selector: "22 GAL. L.H. - 22 GAL. R.H.

On fuel filler caps: "22 US GAL. CAP - 100/130 OCTANE"

FAA Form 8110-2 (5/14) Page 5 of

SA876CE Date of Issuance: October 5, 1972 Date Reissued: November 16, 2016

Limitation and Conditions (continued):

Near fuel selector: "USE BOOST PUMP DURING RE-START AND AFTER SWITCHING TANKS". "USE LEFT TANK FOR TAKE-OFF AND FIRST 30 MINUTES OF FLIGHT".

On right hand front side panel: "ON BATT ALTERNATOR" OFF

"ALT FAIL LIGHT"

On right hand side of instrument panel: "ALTERNATOR MUST BE OFF WHEN USING GND POWER CART".

On left hand side of cockpit rail: "DO NOT TAKE-OFF IF FUEL GAGES INDICATE IN YELLOW BAND OR WITH LESS THAN 13 GAL. IN EACH MAIN TANK". "DO NOT PERFORM APPROVED MANEUVERS WITH LESS FUEL THAN REQUIRED FOR TAKE-OFF".

On upper left hand side of instrument panel: "INVERTED FLIGHT PROHIBITED".

On lower left hand side of instrument panel: "ALTERNATE INDUCTION AIR PULL AND RELEASE".

In addition to the placards specified above, the prescribed operating limitations indicated by an asterisk (*) in this addendum must be displayed by permanent markings.

Required Equipment: 201(b) or (c), 202, 205, 206, 301(b), 302(b), 303(b), 305 or 402(b), 601, all airplanes must be equipped with a United Beechcraft , Inc. FAA approved Airplane Flight Manual Supplement dated October 5, 1972.

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