# STC SA2698NM-S

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Raisbeck Engineering Inc., United States
- Description: Installation of a set of Hartzell/Raisbeck Quiet Turbofan Propellers or Swept Turbofan Propellers
- Applied: June 27, 1984
- Status date: October 20, 2023
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/01/02/010242558b9aed0868dabd46bef0d6ab16fecf8637fe99493d95595cbf56f792
- Approved model list and other attachments: [SA2698NM-S_AML.pdf](https://openairdocs.org/files/sha256/ea/70/ea7021ec740d0f68800d57d1ba9deaba2f05f421b567ad99a9c4bc7a9b08f795)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199100294820231031173848.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2698NM-S

## ADs that name it (0)

None.

## Approved models (26)

- Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200 (C-12A) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200 (C-12C) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200C (UC-12B) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (C-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (FWC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12G) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12H) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12K) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12P) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12Q) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200C (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200C (C-12R) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200C (UC-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200C (UC-12M) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200CGT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200GT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200T ([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.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

(See Continuation Sheet Page 3 of 4 Pages) SA2698NM-S Raisbeck Engineering Inc.

2811 South 102nd Street, Suite 100 Tukwila, WA 98168 Part* * the Regulations * * * See attached Federal Aviation Administration (FAA)Approved Model List (AML) SA2698NM-S for approved aircraft models and applicable airworthiness regulations.

Installation of a set of Hartzell/Raisbeck Quiet Turbofan Propellers or Swept Turbofan Propellers or Five-Blade Swept Turbofan Propellers in accordance with Raisbeck Engineering Drawing List 85-1500, Revision BV, dated September 13, 2019, or later FAA-approved revision.

This installation consists of Hartzell 4-bladed or 5-bladed propellers and aluminum hubs with spinners, and a propeller de-icing system.

Approval of this change in type design applies to the aircraft listed on AML SA2698NM-S only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

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.

June 27, 1984 September 1, 2023; October 20, 2023 February 7, 1985 4/28/89; 11/15/96; 4/29/09; 12/31/12; 3/27/14;

9/30/14; 1/28/16;11/22/19 For Acting Manager, Seattle ACO Branch 4

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

SA2698NM-S 4

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

(See Continuation Sheet Page 4 of 4 Pages) SA2698NM-S Limitations and Conditions (continued):

Aircraft must be operated in accordance with the applicable FAA-approved Airplane Flight Manual Supplement (AFMS) in accordance with AML SA2698NM-S, or previous versions of this STC. Aircraft must be maintained in accordance with the Raisbeck Engineering Maintenance Manual Document No.

85-120, Revision AK, dated September 18, 2019, or later FAA-approved revision.

Compatibility between this supplemental type certificate (STC) and STCs SA1783NM, SA10737SC, SA00433AT, SA10824SC, and SA10842SC has been demonstrated. A copy of this certificate, and the appropriate AFMS determined from AML SA2698NM-S must be maintained with the permanent records of the modified aircraft.

Propellers and Propeller Limitations:

Two (2) Hartzell HC-D4N-3A hubs with Hartzell D9383K blades in pairs.

Diameter 94.0 in. (maximum); minimum allowable for repair: 93.0 in. No further reduction in diameter permitted.

Pitch Settings: Flight Idle Stop: See Note 1 or 2 Reverse: -10.5 deg.

Feathered: +86 deg.

Stabilized ground operation between 400 and 1,150 propeller RPM is prohibited. Operation between O and 400 propeller RPM is permissible only with propeller feathered.

Beechcraft autofeathering system or Raisbeck Magicam must be installed and operational.

Airspeed Limits: Air minimum control speed VMCA 96 KCAS (91 KIAS)

Note 1: Flight idle propeller low pitch stop is set so that at 1,800 RPM there shall be an indicated 640 ± 60 ft-lb torque corrected to sea level standard day (Beechcraft Autofeather Only)

Note 2: Flight idle propeller low pitch stop set per Magicam Installation and Rigging Procedures (Raisbeck Magicam Only) 3 4

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

End SA2698NM-S Limitations and Conditions (continued):

Propellers and Propeller Limitations:

Two (2) Hartzell HC-D4N-3A hubs with Hartzell D9515K blades in pairs.

Diameter 96.0 in. (maximum); minimum allowable for repair: 95.0 in. No further reduction in diameter permitted.

Pitch Settings: Flight Idle Stop: See Note 1 Reverse: -10.3 deg.

Feathered: +84.2 deg.

Stabilized ground operation between 450 and 1,150 propeller RPM is prohibited. Operation between O and 450 propeller RPM is permissible only with propeller feathered.

Beechcraft autofeathering system must be installed and operational.

Airspeed Limits: Air minimum control speed VMCA 96 KCAS (91 KIAS)

Note 1: Flight idle propeller low pitch stop is set so that at 1,800 RPM there shall be an indicated 640 ± 60 ft-lb torque corrected to sea level standard day

Propellers and Propeller Limitations:

Two (2) Hartzell 5D3-NK366A1 hubs with 5 Hartzell 91D15B blades each.

Diameter 96.0 in. No further reduction in diameter permitted.

Pitch Settings: Flight Idle Stop: See Note 1 Reverse: -8.0 deg.

Feathered: +85.7 deg.

Stabilized ground operation between 700 and 1,150 propeller RPM is prohibited. Operation between O and 700 propeller RPM is permissible only with propeller feathered.

Beechcraft autofeathering system must be installed and operational.

Airspeed Limits: Air minimum control speed VMCA 96 KCAS (91 KIAS)

Note 1: Flight idle propeller low pitch stop is set so that at 1,800 RPM there shall be an indicated 640 ± 60 ft-lb torque corrected to sea level standard day

Certification Basis: As listed on AML SA2698NM-S 4 4

### SA2698NM-S_AML.pdf

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2698NM-S FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: November 22, 2019 Page 1 of 9 Aircraft Make: Beechcraft Corporation Original Product – Type Certificate Data Sheet (TCDS) Number: A24CE Certification Basis: 1. Items 1-70 as listed on TCDS A24CE;

2. Items 71-79, 5D3-NK366A1/91D15B propellers, as listed on TCDS A24CE except for:

14 CFR 23 Paragraph 23.201, 23.203, 23.205 and 23.613 at Amendment 23-45 14 CFR 23 Paragraph 23.607 and 23.611 at Amendment 23-48 14 CFR 23 Paragraph 23.907 at Amendment 23-59 14 CFR 36 at Amendment 36-31

Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 1 200, 200C, 200T, 200CT, A200, A200C, A200CT, B200, B200C, B200T, B200CT PT6A-616 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 07BM-116 Revision B, 05/03/19 HC-D4N-3A/D9383K 2 200, 200C, 200T, 200CT, A200, A200C, A200CT, B200, B200C, B200T, B200CT PT6A -616 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 07BM-116 Revision B, 05/03/19 HC-D4N-3A/D9383K 3 200, 200C, A200, B200, B200C PT6A -523 85-105 Revision AG, 07/01/19 09-52-106 Revision A, 07/13/11 HC-D4N-3A/D9383K 4 200, 200C, B200, B200C PT6A -524, 5 85-105 Revision AG, 07/01/19 09-52-106 Revision A, 07/13/11 HC-D4N-3A/D9383K 5 B200GT, B200CGT PT6A -52 85-105 Revision AG, 07/01/19 09-52-106 Revision A, 07/13/11 HC-D4N-3A/D9383K 6 200, 200C, A200, B200, B200C PT6A -616 85-105 Revision AG, 07/01/19 09-52-106 Revision A, 07/13/11 HC-D4N-3A/D9383K 7 200, 200C, B200, B200C, B200T, B200CT PT6A -523 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09BM-52-116 Superseded by 09-B200GT-116 Revision C, 07/01/19 HC-D4N-3A/D9383K 8 200, 200C, B200, B200C, B200T, B200CT PT6A -523 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09BM-52-116 Superseded by 09-B200GT-116 Revision C, 07/01/19 HC-D4N-3A/D9383K

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2698NM-S FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: November 22, 2019 Page 2 of 9 Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 9 200, 200C, B200, B200C PT6A -524 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09EA-52-116 Superseded by 09-B200GT-116 Revision B, 07/01/19 HC-D4N-3A/D9383K 10 200, 200C, B200, B200C PT6A -524 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09EA-52-116 Superseded by 09-B200GT-116 Revision B, 07/01/19 HC-D4N-3A/D9383K 11 200, 200C, B200, B200C PT6A -525 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09SA-52-116 Superseded by 09-B200GT-116 Revision C, 07/01/19 HC-D4N-3A/D9383K 12 200, 200C, B200, B200C PT6A -525 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09SA-52-116 Superseded by 09-B200GT-116 Revision C, 07/01/19 HC-D4N-3A/D9383K 13 200, 200C, 200T, 200CT, B200, B200C, B200T, B200CT PT6A -523 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09-B200GT-116 Revision C, 05/03/19 HC-D4N-3A/D9383K 14 200, 200C, 200T, 200CT, B200, B200C, B200T, B200CT PT6A -523 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09-B200GT-116 Revision C, 05/03/19 HC-D4N-3A/D9383K 15 200, 200C, B200, B200C PT6A -524, 5 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09-B200GT-116 Revision C, 05/03/19 HC-D4N-3A/D9383K 16 200, 200C, B200, B200C PT6A -524, 5 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09-B200GT-116 Revision C, 05/03/19 HC-D4N-3A/D9383K 17 B200GT, B200CGT PT6A -52 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09-B200GT-116 Revision C, 05/03/19 HC-D4N-3A/D9383K 18 B200GT, B200CGT PT6A -52 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09-B200GT-116 Revision C, 05/03/19 HC-D4N-3A/D9383K

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2698NM-S FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: November 22, 2019 Page 3 of 9 Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 19 200, 200C, A200 PT6A -41 85-105 Revision AG, 07/01/19 85-106

85-106UK Revision E, 12/15/05 Revision E, 10/20/16 HC-D4N-3A/D9383K 20 B200, B200C PT6A -42 85-105 Revision AG, 07/01/19 85-106

85-106UK Revision E, 12/15/05 Revision E, 10/20/16 HC-D4N-3A/D9383K 21 200, 200C PT6A -41 SA1783NM (Mark VI) 85-105 Revision AG, 07/01/19 85-107 Revision IR, 06/01/86 HC-D4N-3A/D9383K 22 B200, B200C PT6A -42 SA1783NM (Mark VI) 85-105 Revision AG, 07/01/19 85-108 Revision C, 06/12/87 HC-D4N-3A/D9383K 23 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -41 SA3831NM (EPLE) 85-105 Revision AG, 07/01/19 85-109 Revision A, 12/93 HC-D4N-3A/D9383K 24 B200, B200C, B200T, B200CT PT6A -42 SA3831NM (EPLE) 85-105 Revision AG, 07/01/19 85-110 Revision A, 12/93 HC-D4N-3A/D9383K 25 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -41 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 85-115 Revision J, 05/03/19 HC-D4N-3A/D9383K 26 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -41 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 85-115 Revision J, 05/03/19 HC-D4N-3A/D9383K 27 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -421, 2 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 85-116H Revision D, 05/03/19 HC-D4N-3A/D9383K 28 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -421, 2 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 85-116H Revision D, 05/03/19 HC-D4N-3A/D9383K

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2698NM-S FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: November 22, 2019 Page 4 of 9 Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 29 B200, B200C, B200T, B200CT PT6A -42 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 85-116H Revision D, 05/03/19 HC-D4N-3A/D9383K 30 B200, B200C, B200T, B200CT PT6A -42 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 85-116H Revision D, 05/03/19 HC-D4N-3A/D9383K 31 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -421 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 85-116 Superseded by 85-116H Revision L, 07/01/19 HC-D4N-3A/D9383K 32 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -421 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 85-116 Superseded by 85-116H Revision L, 07/01/19 HC-D4N-3A/D9383K 33 B200, B200C, B200T, B200CT PT6A -42 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 85-116 Superseded by 85-116H Revision L, 07/01/19 HC-D4N-3A/D9383K 34 B200, B200C, B200T, B200CT PT6A -42 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 85-116 Superseded by 85-116H Revision L, 07/01/19 HC-D4N-3A/D9383K 35 200, 200C, 200T, 200CT PT6A -422 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09SA-42-116 Superseded by 85-116H Revision B, 07/01/19 HC-D4N-3A/D9383K 36 200, 200C, 200T, 200CT PT6A -422 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 09SA-42-116 Superseded by 85-116H Revision B, 07/01/19 HC-D4N-3A/D9383K 37 200, 200C, 200T, 200CT PT6A -41 89-105 Revision IR, 03/01/89 89-118 Revision IR, 04/28/89 HC-D4N-3A/D9383K 38 B200, B200C, B200T, B200CT PT6A -42 89-105 Revision IR, 03/01/89 89-118 Revision IR, 04/28/89 HC-D4N-3A/D9383K 39 200, 200C, 200T, 200CT, A200, A200C, A200CT, B200, B200C, B200T, B200CT PT6A -616 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11BM-116 Revision B, 05/03/19 HC-D4N-3A/D9515K

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2698NM-S FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: November 22, 2019 Page 5 of 9 Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 40 200, 200C, 200T, 200CT, A200, A200C, A200CT, B200, B200C, B200T, B200CT PT6A -616 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11BM-116 Revision B, 05/03/19 HC-D4N-3A/D9515K 41 200, 200C, A200, B200, B200C PT6A -523 85-105 Revision AG, 07/01/19 11-52-106

11-52-106-TFM-1 Revision B, 06/27/2016 Revision --, 01/24/2017 HC-D4N-3A/D9515K 42 200, 200C, B200, B200C PT6A -524, 5 85-105 Revision AG, 07/01/19 11-52-106

11-52-106-TFM-1 Revision B, 06/27/2016 Revision --, 01/24/2017 HC-D4N-3A/D9515K 43 B200GT, B200CGT PT6A -52 85-105 Revision AG, 07/01/19 11-52-106

11-52-106-TFM-1 Revision B, 06/27/2016 Revision --, 01/24/2017 HC-D4N-3A/D9515K 44 200, 200C, A200, B200, B200C PT6A -616 85-105 Revision AG, 07/01/19 11-52-106

11-52-106-TFM-1 Revision B, 06/27/2016 Revision --, 01/24/2017 HC-D4N-3A/D9515K 45 200, 200C, B200, B200C, B200T, B200CT PT6A -523 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11BM-52-116 Superseded by 11-B200GT-116 Revision B, 07/01/19 HC-D4N-3A/D9515K 46 200, 200C, B200, B200C, B200T, B200CT PT6A -523 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11BM-52-116 Superseded by 11-B200GT-116 Revision B, 07/01/19 HC-D4N-3A/D9515K 47 200, 200C, B200, B200C PT6A -524 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11EA-52-116 Superseded by 11-B200GT-116 Revision B, 07/01/19 HC-D4N-3A/D9515K 48 200, 200C, B200, B200C PT6A -524 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11EA-52-116 Superseded by 11-B200GT-116 Revision B, 07/01/19 HC-D4N-3A/D9515K

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2698NM-S FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: November 22, 2019 Page 6 of 9 Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 49 200, 200C, B200, B200C PT6A -525 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11SA-52-116 Superseded by 11-B200GT-116 Revision B, 07/01/19 HC-D4N-3A/D9515K 50 200, 200C, B200, B200C PT6A -525 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11SA-52-116 Superseded by 11-B200GT-116 Revision B, 07/01/19 HC-D4N-3A/D9515K 51 200, 200C, 200T, 200CT, B200, B200C, B200T, B200CT PT6A -523 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-B200GT-116 Revision C, 05/03/19 HC-D4N-3A/D9515K 52 200, 200C, 200T, 200CT, B200, B200C, B200T, B200CT PT6A -523 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-B200GT-116 Revision C, 05/03/19 HC-D4N-3A/D9515K 53 200, 200C, B200, B200C PT6A -524, 5 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-B200GT-116 Revision C, 05/03/19 HC-D4N-3A/D9515K 54 200, 200C, B200, B200C PT6A -524, 5 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-B200GT-116 Revision C, 05/03/19 HC-D4N-3A/D9515K 55 B200GT, B200CGT PT6A -52 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-B200GT-116 Revision C, 05/03/19 HC-D4N-3A/D9515K 56 B200GT, B200CGT PT6A -52 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-B200GT-116 Revision C, 05/03/19 HC-D4N-3A/D9515K 57 200, 200C, A200 PT6A -41 85-105 Revision AG, 07/01/19 11-106 Revision A, 03/27/2014 HC-D4N-3A/D9515K 58 B200, B200C PT6A -42 85-105 Revision AG, 07/01/19 11-106 Revision A, 03/27/2014 HC-D4N-3A/D9515K 59 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -41 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-115 Revision B, 05/03/19 HC-D4N-3A/D9515K

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2698NM-S FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: November 22, 2019 Page 7 of 9 Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 60 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -41 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-115 Revision B, 05/03/19 HC-D4N-3A/D9515K 61 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -421, 2 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-116H Revision B, 05/03/19 HC-D4N-3A/D9515K 62 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -421, 2 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-116H Revision B, 05/03/19 HC-D4N-3A/D9515K 63 B200, B200C, B200T, B200CT PT6A -42 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-116H Revision B, 05/03/19 HC-D4N-3A/D9515K 64 B200, B200C, B200T, B200CT PT6A -42 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-116H Revision B, 05/03/19 HC-D4N-3A/D9515K 65 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -421 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-116 Superseded by 11-116H Revision B, 07/01/19 HC-D4N-3A/D9515K 66 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -421 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-116 Superseded by 11-116H Revision B, 07/01/19 HC-D4N-3A/D9515K 67 B200, B200C, B200T, B200CT PT6A -42 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-116 Superseded by 11-116H Revision B, 07/01/19 HC-D4N-3A/D9515K 68 B200, B200C, B200T, B200CT PT6A -42 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11-116 Superseded by 11-116H Revision B, 07/01/19 HC-D4N-3A/D9515K 69 200, 200C, 200T, 200CT PT6A -422 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11SA-42-116 Superseded by 11-116H Revision B, 07/01/19 HC-D4N-3A/D9515K

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2698NM-S FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: November 22, 2019 Page 8 of 9 Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 70 200, 200C, 200T, 200CT PT6A -422 SA1783NM (Mark VI) SA4175NM (HFGD)7 85-105 Revision AG, 07/01/19 11SA-42-116 Superseded by 11-116H Revision B, 07/01/19 HC-D4N-3A/D9515K 71 200, A200, 200C PT6A -41 19BC-61-003 Revision IR, 09/13/19 19-106 Revision IR, 10/22/2019 5D3-NK366A1/91D15B 72 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -41 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 19BC-61-003 Revision IR, 09/13/19 19-115 Revision IR, 10/22/2019 5D3-NK366A1/91D15B 73 200, 200C, 200T, 200CT, A200, A200C, A200CT PT6A -41 SA1783NM (Mark VI) SA4175NM (HFGD)7 19BC-61-003 Revision IR, 09/13/19 19-115 Revision IR, 10/22/2019 5D3-NK366A1/91D15B 74 B200, B200C PT6A -42 19BC-61-003 Revision IR, 09/13/19 19-106 Revision IR, 10/22/2019 5D3-NK366A1/91D15B 75 B200, B200C, B200T, B200CT PT6A -42 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 19BC-61-003 Revision IR, 09/13/19 19-116H Revision IR, 10/22/2019 5D3-NK366A1/91D15B 76 B200, B200C, B200T, B200CT PT6A -42 SA1783NM (Mark VI) SA4175NM (HFGD)7 19BC-61-003 Revision IR, 09/13/19 19-116H Revision IR, 10/22/2019 5D3-NK366A1/91D15B 77 B200GT, B200CGT PT6A -52 19BC-61-003 Revision IR, 09/13/19 19-52-106 Revision IR, 10/22/2019 5D3-NK366A1/91D15B 78 B200GT, B200CGT PT6A -52 SA3366NM (RARS) SA3831NM (EPLE) SA3591NM (DABS) SA4175NM (HFGD)7 19BC-61-003 Revision IR, 09/13/19 19-B200GT-116 Revision IR, 10/22/2019 5D3-NK366A1/91D15B 79 B200GT, B200CGT PT6A -52 SA1783NM (Mark VI) SA4175NM (HFGD)7 19BC-61-003 Revision IR, 09/13/19 19-B200GT-116 Revision IR, 10/22/2019 5D3-NK366A1/91D15B * Unless otherwise noted, Pratt & Whitney Canada engines installed by Textron Aviation.

** Or later FAA approved revision.

*** Hartzell hub/blade part number.

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA2698NM-S FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: November 22, 2019 Page 9 of 9 Limitations:

1. Installation of the Pratt and Whitney PT6A-42 engines on King Air model 200, 200C, 200CT, 200T, A200, A200C, or A200CT aircraft must be accomplished in accordance with Blackhawk Modifications, Inc. STC SA00433AT; refer to the appropriate FAA approved type design change and Flight Manual Supplement.

2. Installation of the Pratt and Whitney PT6A-42 engines on King Air model 200, 200C, 200CT, 200T, A200, A200C, or A200CT aircraft must be accomplished in accordance with Standard Aero STC SA02603CH-D; refer to the appropriate FAA approved type design change and Flight Manual Supplement.

3. Installation of the Pratt and Whitney PT6A-52 engines on King Air model 200, 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200T, or B200CT aircraft must be accomplished in accordance with Blackhawk Modifications, Inc. STC SA10824SC; refer to the appropriate FAA approved type design change and Flight Manual Supplement.

4. Installation of the Pratt and Whitney PT6A-52 engines on King Air model 200, 200C, B200, or B200C aircraft must be accomplished in accordance with Enhanced Aero, LLC STC SA10842SC; refer to the appropriate FAA approved type design change and Flight Manual Supplement.

5. Installation of the Pratt and Whitney PT6A-52 engines on King Air model 200, 200C, B200, or B200C aircraft must be accomplished in accordance with Standard Aero STC SA02715CH-D; refer to the appropriate FAA approved type design change and Flight Manual Supplement.

6. Installation of the Pratt and Whitney PT6A-61 engines on King Air model 200, 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200T, or B200CT aircraft must be accomplished in accordance with Blackhawk Modifications STC SA10737SC; refer to the appropriate FAA approved type design change and Flight Manual Supplement.

7. When aircraft are High Float Gear equipped, STC SA1668NM installs Fully-Enclosed Main Landing Gear Doors.

FAA APPROVED: ____________________________________________ for Manager, West Certification Branch

AMENDED: December 18, 2019; April 29, 2021 REISSUED: September 1, 2023

## Every issue (10)

- October 20, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/01/02/010242558b9aed0868dabd46bef0d6ab16fecf8637fe99493d95595cbf56f792), [SA2698NM-S_AML.pdf](https://openairdocs.org/files/sha256/ea/70/ea7021ec740d0f68800d57d1ba9deaba2f05f421b567ad99a9c4bc7a9b08f795)
- September 1, 2023: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/65/d5/65d58093de39516905d0ed875aeb775e1a8fe7d2d01c1b9102373abf20045f8c), [SA2698NM-S_AML.pdf](https://openairdocs.org/files/sha256/a0/f2/a0f275b610078164dd627cf6ccf8b8f8a2d38d7b85ed974c71da3a543e8aadc8)
- April 29, 2021: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/53/3c/533ce8ff77cf09c40cd046c73ee79048c2cfc4d4df2216fa725f6b4a81ca8f21), [AML_SA2698NM-S.pdf](https://openairdocs.org/files/sha256/29/4e/294e2f19a89f42e7ba6d8151d934c12f74026995d9a487d45baa3339fae89f2f)
- November 22, 2019: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/53/3c/533ce8ff77cf09c40cd046c73ee79048c2cfc4d4df2216fa725f6b4a81ca8f21)
- January 28, 2016: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/8b/f1/8bf102626846478dadd84d9e9b865704fc64b30b0c90a8ac8ca2b3bdef3fa11b)
- September 30, 2014: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/e7/a2/e7a29374a0c63e7ddadb25123a0cc0fa8a227d4770715d17965a8a04ff2daacf)
- March 27, 2014: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/63/e8/63e826e600c764a9785db35eb142c6b3b568a5754fa9111dcf2e0e563f77679e)
- December 31, 2012: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/aa/07/aa0722851cbccd207a2affdc1315ab0d23bb3364250c365c7e42056623fc84ea)
- October 15, 2009: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/b7/7f/b77f8b16ee6e820672fe8aac8136532f95c794687f767d4f014162909944a6d6)
- April 29, 2009: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/e3/44/e34463f2bc9ef059221a61ea036865d96d32008622a8b004226e96dd1eff39d8)

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