# STC SA11136SC

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: BHE & Associates LTD, United States
- Description: Installation of a Rockwell Collins Pro Line Fusion ® embedded display system (EDS) and optional TCAS II
- Applied: December 30, 2014
- Status date: February 8, 2023
- Product: Aircraft, Small/Large Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/ad/d6/add630da3a24ef00b54e2fa9072ba6600935093c2d45e271999281655fb51874
- Approved model list and other attachments: [SA11136SC_AML.pdf](https://openairdocs.org/files/sha256/d4/1d/d41d7c8429daca959826ed976ee32dc1ff46c4459d5ecda96b2c5efbc5df33e8)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127918458820230222133327.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA11136SC

## ADs that name it (0)

None.

## Approved models (4)

- Textron Aviation Inc. B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. B300C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## 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.

SA11136SC BHE & Associates, Ltd.

12002 Warfield St.

Suite 250 San Antonio, TX. 78216 Part 23 Code of Federal Regulations See attached AML See attached AML See attached AML Installation of a Rockwell Collins Pro Line Fusion ® embedded display system (EDS) and optional TCAS II including updating the existing Collins Aerospace Pro Line II system to a Pro Line 21 backbone or updating the existing Collins Aerospace Pro Line 21 in accordance with Master Data List, Instructions for Continued Airworthiness and Airplane Flight Manual Supplement referenced on the attached AML or later FAA-approved revisions.

1. The installer must determine whether this design change is compatible with previously approved modifications.

(See continuation sheet 3 of 3) December 30, 2014 December 24, 2015 October 15, 2016, July 18, 2018, December 08,2021 February 8, 2023 VT DRB Aviation Lead ODA Administrator ODA-831473-SW 3

SA11136SC 3

SA11136SC Limitations and Conditions (continued):

2. See attached FAA Approved Model List ( AML) for applicable serial numbers.

3. 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.

4. Flight data recorder( FDR) interface has not been validated for this STC, installer must determine compatibility.

...........END...........

### SA11136SC_AML.pdf

Approved Model List For:

Rockwell Collins Pro Line Fusion embedded display system (EDS) with optional TCAS II

BHE & Associates, Ltd.

STC Number SA11136SC Revision C

FAA Approved:

VT DRB Aviation Project ODA Administrator ODA-831473-SW

BHE & Associates, Ltd.

STC Number:

SA11136SC Revision C Date 2018-07-18 Page 2 of 6 Document Title:

FAA Approved Model List ( AML) STC Number SA11136SC

1. AML Revision Log

Revision Section Description FAA Approval Date IR All Initial Release Robert Hurley December 24, 2015 A 2

3 4

2,3,4

Add APC-65, APC-65H (B200/B200C) and APC-65J (B300/B300C) and TCAS I to “Important Notes” Add B300/B300C engine and propeller.

Add missing rules to cert basis - B300 Changed Master Drawing List to Master Data List.

Add model B200/B200C

Darryl Seow October 15, 2016 B 2 Administrative change Corrected Auto pilot number for B300/B300C should be APC-65J Updated -added TCAS numbers to B300/B300C Updated –added TCAS numbers to B200/B200C Added propeller numbers HC-B4MP-3C/M10476NSK and HC-E4P- 3K/E10479S Melissa Sandow October 11, 2017 C 2

3 Updated- added TCAS numbers to B200/B200C Added propeller numbers Corrected certification basis for B200/B200C July 18, 2018

BHE & Associates, Ltd.

STC Number:

SA11136SC Revision C Date 2018-07-18 Page 3 of 6 Document Title:

FAA Approved Model List ( AML) STC Number SA11136SC

2. Introduction

This document is the FAA AML for STC Number SA11136SC for installing a Rockwell Collins Pro Line Fusion EDS and optional TCAS II into eligible aircraft.

Revisions to the AML must be coordinated between the STC holder and the responsible ODA/ACO and require FAA approval.

IMPORTANT NOTES:

This STC assumes the following equipment is already installed on each airplane eligible for the proposed modification (all models):

Rockwell Collins APC-65 or APC-65H (B200/B200C) and APC-65J (B300/B300C) Autopilot Rockwell Collins Pro Line II radios Honeywell KGP-860 TAWS

MODEL SPECIFIC LIMITATIONS AND CONDITIONS (continued from sheet 1 of the certificate):

Beechcraft B300 and B300C:

1. Serial numbers FL-120, FL-122 thru FL-380, FL-382; FM-9 thru FM-11.

2. Equivalent Level of Safety Findings has been made for the following regulations:

14 CFR §23.1305(a)(2), (a)(3), c(2) and (c)(5), Amendment 23-52 14 CFR §23.1311 (a)(6) and (a)(7), Amendment 23-62 14 CFR §23.1549(a), (b) and (c) Amendment 23-45 (Documented in ELOS Memo ST1933DRB-A-F-1)

3. Aircraft must have two of the same propeller part numbers from the list below:

a. HC-B4MP-3C/M10476K

b. HC-B4MP-3C/M10476NK

c. HC-B4MP-3C/M10476NSK

d. HC-E4P-3K/E10479S

4. Pratt & Whitney PT6A-60A engine

5. The TCAS interfaces are limited to the following:

Rockwell Collins TCAS-4000, TCAS-4100 or TTR-920

Beechcraft B200 and B200C:

BHE & Associates, Ltd.

STC Number:

SA11136SC Revision C Date 2018-07-18 Page 4 of 6 Document Title:

FAA Approved Model List ( AML) STC Number SA11136SC

1. Equivalent Level of Safety Findings has been made for the following regulations:

14 CFR §23.1305(a)(2), (a)(3), c(2) and (c)(5), Amendment 23-52 14 CFR §23.1311 (a)(6)(7) Amendment 23-62 14 CFR §23.1549(a), (b) and (c) Amendment 23-45 (Documented in ELOS Memo SA1967DRB-A-P-1)

Beechcraft B200 and B200C (cont):

2. Aircraft must have two of the same propeller part numbers from the list below:

a. HC-B3TN-3G/TI0178B-3R

b. HC-B3TN-3N/TI0178B-3R

c. HC-B3TN-3G/TI0178K-3R

d. HC-B3TN-3N/TI0178K-3R

e. 3GFR34C702--100LA

f. HC-E4N-3G/D9390SK-1R

g. HC-D4N-3A/D9383K

h. HC-D4N-3A/D9515K

3. Pratt & Whitney PT6A-42 engine

4. The TCAS interfaces are limited to the following:

Rockwell Collins TCAS-4000, TCAS-4100, TTR-920 or Extant Aerospace/L3 TCAS TRC-899

BHE & Associates, Ltd.

STC Number:

SA11136SC Revision C Date 2018-07-18 Page 5 of 6 Document Title:

FAA Approved Model List ( AML) STC Number SA11136SC

3. Certification Basis

The certification basis for each model qualified for this modification is detailed below.

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 the AML modified by installing a Rockwell Collins Pro Line Fusion EDS and optional TCAS II is as follows:

a. The type certification basis for the approved model list for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application for the B300/B300, 30 December 2014 and B200/B200C, 14 April 2016, is based upon part 23 as amended by amendment 23-62:

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 this modification were determined to be:

Aircraft Make Aircraft Model Type Data Sheet Certification Basis Beechcraft B300 B300C A24CE Regulations at the latest amendment 23-0 through 23-62 14 CFR § 23.1, 23.23 (b), 23.25 (a1ii), 23.301 (a)(b), 23.305,

23.561 (a)(b)(e), 23.574 (a), 23.575, 23.773 (a2), 23.777

(a)(b), 23.853 (a), 23.901 (a)(b1)(b2)(e1), 23.903(b2),

23.937(a), 23.1141(g2), 23.1203(a)(d), 23.1301, 23.1303

(a)(b)(c)(e)(g), 23.1306, 23.1308 (a)(b)(c), 23.1309, 23.1311,

23.1321,23.1322, 23.1323 (a)(c), 23.1331, 23.1353(h),

23.1357(a)(b)(c)(d), 23.1361(a)(b), 23.1431 (a)(b)(d)(e),

23.1521(a)(b)(c), 23.1525, 23.1543(b)(c), 23.1545(c),

23.1549, 23.1555 (a), 23.1583(h)(m), 23.1585 (a)(j).

Regulations at an intermediate amendment

23.1545(d) 23-50 Beechcraft B200 B200C A24CE Regulations at the latest amendment 23-0 through 23-62 14 CFR § 23.1, 23.25 (a1ii), 23.301 (a)(b), 23.305, 23.561

(a)(b)(e), 23.574 (a), 23.575, 23.773 (a2), 23.777 (a)(b),

23.901 (a)(b1)(e1), 23.903(b2), 23.937(a)(b), 23.1141(g2),

23.1203(a)(d), 23.1301, 23.1303 (a)(b)(c)(e)(g), 23.1309,

23.1311, 23.1323 (a)(c), 23.1331, 23.1361(a)(b), 23.1431

(a)(b)(d)(e), 23.1525, 23.1543(b)(c), 23.1545(c), 23.1549,

23.1555(a), 23.1583(h)(m), 23.1585 (a)(j).

Regulations at an intermediate amendment None

BHE & Associates, Ltd.

STC Number:

SA11136SC Revision C Date 2018-07-18 Page 6 of 6 Document Title:

FAA Approved Model List ( AML) STC Number SA11136SC

Approved Model List Aircraft Make Aircraft Model Type Certificate Number Required Approved Data and Added Model Specific Limitations AML Amendment Date Beechcraft B300 B300C A24CE Master Data List:

522-00-0001, Rev. H dated 24 December 2015 Airplane Flight Manual Supplement:

522-00-0097, Rev IR, dated December 24, 2015 Instructions for Continued Airworthiness:

522-00-0098, Rev B, dated November 11, 2015

IR 24 December 2015 Beech B200 B200C A24CE Master Data List:

548-00-0001 Rev. A dated October 14, 2016 Airplane Flight Manual Supplement:

548-00-0097, Rev A, dated October 12 2016 Instructions for Continued Airworthiness:

548-00-0098, Rev A, dated September 22, 2016

A 15 October 2016

## Every issue (5)

- February 8, 2023: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ad/d6/add630da3a24ef00b54e2fa9072ba6600935093c2d45e271999281655fb51874), [SA11136SC_AML.pdf](https://openairdocs.org/files/sha256/d4/1d/d41d7c8429daca959826ed976ee32dc1ff46c4459d5ecda96b2c5efbc5df33e8)
- December 8, 2021: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/80/fe/80fee6c7dcb699a7b1ec0163050e18d440e3d94bec853eb688499557841b3761), [SA11136SC_AML.pdf](https://openairdocs.org/files/sha256/d4/1d/d41d7c8429daca959826ed976ee32dc1ff46c4459d5ecda96b2c5efbc5df33e8)
- July 18, 2018: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/6b/33/6b33b014aadbf4e2d5fbb0f47bfdbb96049aa6480e9c0a213b2fc833ef0308e0), [SA11136SC_AML.pdf](https://openairdocs.org/files/sha256/05/cf/05cf1ced81febbc2cc5034afc81f6eca2b1485b9ff209867836cf71fe42222f4)
- October 15, 2016: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/c3/1b/c31b3d62cdaf3deb7fd6ebbd7f23dab897924062837cc7ac5cd016df7d9e3cb1), [SA11136SC_AML.pdf](https://openairdocs.org/files/sha256/80/8b/808b6282f2209cd2c1c94740ba6acf0e8808b3ca0dee3e86e781fbcea2154e3d)
- December 24, 2015: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/5f/31/5f31322b3f224db4a7a2c52b21f921ff60e13a44ba18fd9f17ada40e14a526be), [SA11136SC_AML.pdf](https://openairdocs.org/files/sha256/c9/54/c9541732c735a69178102724e25aa123964a7d9e86bb2888f82f164dfed2a10c)

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