# STC SA3593NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Raisbeck Engineering Inc., United States
- Description: Installation of Raisbeck/Hartzell Quiet Turbofan Propellers or Swept Turbofan Propellers, and optional Increased Gross Weight
- Applied: March 11, 1986
- Status date: September 1, 2023
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS 3A20](https://openairdocs.org/tcds/3A20)
- Certificate PDF: https://openairdocs.org/files/sha256/75/fa/75fadfc4704af33806e02109802ecd8f05015b6d04aa97bd5ac9e17b31f3671e
- Approved model list and other attachments: [SA3593NM_AML.pdf](https://openairdocs.org/files/sha256/e9/c5/e9c5c8ab4a9d0803d531ec43b7e3aadb7331241ef049d3385763e68a348ab9c0)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184190257620231003175420.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA3593NM

## ADs that name it (1)

- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005. Cited in the text

## Approved models (7)

- Textron Aviation Inc. 65-A90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Textron Aviation Inc. B90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Textron Aviation Inc. C90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Textron Aviation Inc. C90A ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Textron Aviation Inc. C90GT ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Textron Aviation Inc. C90GTi ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Textron Aviation Inc. E90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))

## 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.

(See Continuation Sheet Page 3 of 4 Pages) SA3593NM 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) SA3593NM for approvedaircraft models and applicable airworthiness regulations.

Installation of Raisbeck/Hartzell Quiet Turbofan Propellers or Swept Turbofan Propellers, and optional Increased Gross Weight in accordance with Raisbeck Engineering Master Drawing List 86-2500, Revision CW, dated February 8, 2017, or later Federal Aviation Administration (FAA) approved revision.

March 11, 1986 September 1, 2023 September 12, 1986 4/1/88; 5/19/88; 6/14/88; 11/21/88; 2/23/89; 9/28/90; 4/29/91; 7/22/94;

8/11/94; 11/8/95; 2/24/06; 5/9/06; 3/15/08; 9/2/08; 9/19/08; 12/9/08;

11/4/09; 11/9/10; 7/27/12; 12/31/13; 8/19/14; 11/10/15; 4/1/16, 4/17/17 for Manager, West Certification Branch Approval of this change in type design applies to the aircraft models listed on the AML only and is subject to the limitation contained in the AML. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

Aircraft must be operated in accordance with the applicable FAA-approved Airplane Flight Manual Supplement (AFMS) listed on the latest amendment of AML SA3593NM, or later FAA-approved AFMS revision. Aircraft must be maintained in accordance with the Raisbeck Engineering Maintenance Manual Document No. 85-120, Revision AC, dated December 7, 2016, or later FAA-approved revision.

SA3593NM

SA3593NM A copy of this Certificate and AML, FAA-approved AFMS, and Maintenance Manual Supplement must be maintained as part of the permanent records for the modified aircraft.

Propellers and Propeller Limitations:

For 2 Hartzell HC-D4N-3C Hubs with Hartzell D9290K Blades in Pairs.

Diameter 93.0 inches (Maximum); Minimum allowable for repair: 92.0 inches No further reduction in diameter permitted.

Pitch Settings:

Low Pitch: +20.1 deg ±0.1 deg Reverse: -9.0 deg ±0.5 deg Feathered: +84.5 deg ±0.5 deg

Stabilized ground operation is prohibited between 400 and 1,100 RPM. Propellers must be feathered for stabilized ground operation at or below 400 RPM.

Auto-feathering system must be installed and operational, except when optional propeller cam is installed.

Optional Propellers and Propeller Limitations:

For C90A Aircraft Models only.

Hartzell Model No. HC-E4N-3N/D8990(K) as listed on and installed in accordance with STC SA00966CH

For C90GT/C90GTi Aircraft Models only.

Hartzell Model No. HC-E4N-3N/D8990SK as listed on and installed in accordance with TCDS 3A20

End Limitations and Conditions continued:

SA3593NM Propellers and Propeller Limitations:

For 2 Hartzell HC-D4N-3C Hubs with Hartzell D9510SK Blades in Pairs.

Diameter 96.0 inches (Maximum); Minimum allowable for repair: 95.0 inches No further reduction in diameter permitted.

Pitch Settings:

Low Pitch: +18.6 deg ±0.1 deg Reverse: -10.0 deg ±0.5 deg Feathered: +86.7 deg ±0.5 deg

Stabilized ground operation is prohibited between 500 and 1,100 RPM. Propellers must be feathered for stabilized ground operation at or below 500 RPM.

Auto-feathering system must be installed and operational.

For 2 Hartzell HC-E4W-3 Hubs with Hartzell D9290K Blades in Pairs.

Diameter 93.0 inches (Maximum); Minimum allowable for repair: 92.0 inches No further reduction in diameter permitted.

Pitch Settings:

Low Pitch: +17.1 deg ±0.1 deg Reverse: -9.0 deg ±0.5 deg Feathered: +84.5 deg ±0.5 deg

Stabilized ground operation is prohibited between 400 and 1,100 RPM. Propellers must be feathered for stabilized ground operation at or below 400 RPM.

Auto-feathering system must be installed and operational.

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.

### SA3593NM_AML.pdf

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA3593NM FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: April 17, 2017

Page 1 of 8 Aircraft Make: Beechcraft Corporation Original Product – Type Certificate Number: 3A20 Certification Basis for Alteration: Civil Air Regulations Part 3 & Title 14 Code of Federal Regulations Part 23

Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 1 65-A90 PT6A-20 For aircraft not modified by Notes 17 or 19 of TCDS 3A20 88-205A Revision B, 04/08/16 86-206A Revision B, 08/13/14 HC-D4N-3C/D9290K 2 65-A90 PT6A-281 For aircraft not modified by Notes 17 or 19 of TCDS 3A20 For aircraft Serial Number LJ-286, Reg. No. N37DA 88-205A Revision B, 04/08/16 86-206A/LJ286 Revision IR, 02/14/89 HC-D4N-3C/D9290K 3 65-A90, B90 PT6A-20 For 65-A90 aircraft modified by Notes 17 or 19 of TCDS 3A20 88-205A/B Revision B, 04/08/16 86-206A/B Revision B, 08/13/14 HC-D4N-3C/D9290K 4 65-A90 PT6A-281 88-205A/E Revision A, 04/08/16 86-206A/E

86-206A/E-TFM-1 86-206A/E-TFM-2 Revision IR, 11/21/88 12/12/12 12/12/12 HC-D4N-3C/D9290K 5 B90, C90 PT6A-281 96-205BC/28 Revision IR, 06/21/16 94-206B/C-28 Revision A, 06/28/96 HC-D4N-3C/D9290K 6 C90 PT6A-281 IGW to 10,100 lb., DABS (SA4010NM) 96-205BC/28 Revision IR, 06/21/16 94-206C-28 Revision IR, 06/94 HC-D4N-3C/D9290K

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA3593NM FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: April 17, 2017

Page 2 of 8 Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 7 B90 PT6A-342 88-205BC/34 Revision C, 10/21/16 86-206B/34

86-206B/34-TFM-1 86-206B/34-TFM-2 86-206B/34-TFM-3 Revision IR, 02/23/89 12/12/12 12/12/12 12/12/12 HC-D4N-3C/D9290K 8 C90 PT6A-342 88-205BC/34 Revision C, 10/21/16 86-206C/34 Revision IR, 02/23/89 HC-D4N-3C/D9290K 9 C90 PT6A-6/C20, PT6A -20, PT6A -20A PT6A -21 86-205C Revision Y, 05/02/16 86-206C Revision C, 08/13/14 HC-D4N-3C/D9290K 10 C90A PT6A -21 86-205C Revision Y, 05/02/16 86-206C Revision C, 08/13/14 HC-D4N-3C/D9290K 11 C90 PT6A-6/C20, PT6A -20, PT6A -21 IGW to 10,100 lb., DABS (SA4010NM) 86-205C Revision Y, 05/02/16 90-206CGW

90-206CGW-TFM-1 90-206CGW-TFM-3 Revision G, 01/05 12/12/12 08/13/14 HC-D4N-3C/D9290K 12 C90A PT6A -21 IGW to 10,100 lb., DABS (SA4010NM) 86-205C Revision Y, 05/02/16 90-206CGW

90-206CGW-TFM-1 90-206CGW-TFM-3 Revision G, 01/05 12/12/12 08/13/14 HC-D4N-3C/D9290K 13 C90 PT6A-6/C20, PT6A -20, PT6A -21 IGW to 10,100 lb., DABS (SA4010NM) 86-205C Revision Y, 05/02/16 05-206CGW Revision D, 06/07/16 HC-D4N-3C/D9290K 14 C90A PT6A -21 IGW to 10,100 lb., DABS (SA4010NM) 86-205C Revision Y, 05/02/16 05-206CGW Revision D, 06/07/16 HC-D4N-3C/D9290K

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA3593NM FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: April 17, 2017

Page 3 of 8 Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 15 C90 PT6A-6/C20, PT6A -20, PT6A -21 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM) 86-205C Revision Y, 05/02/16 05-206CGW Revision D, 06/07/16 HC-D4N-3C/D9290K 16 C90A PT6A -21 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM) 86-205C Revision Y, 05/02/16 05-206CGW Revision D, 06/07/16 HC-D4N-3C/D9290K 17 C90A PT6A -21 Dual VMO indicator per SB- 20-31-1, 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM) 86-205C Revision Y, 05/02/16 20-206CGW Revision D, 06/07/16 HC-D4N-3C/D9290K 18 C90, C90A PT6A-135A5 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM) C90-135A-IM Revision J, 05/02/16 C90-135A-1900 Revision D, 06/07/16 HC-D4N-3C/D9290K 19 E90 PT6A-28 86-205E Revision M, 06/17/16 86-206E Revision C, 08/13/14 HC-D4N-3C/D9290K 20 E90 PT6A-28 IGW to 10,500 lb., DABS (SA4010NM) 86-205E Revision M, 06/17/16 91-206EGW

91-206EGW-TFM-1 91-206EGW-TFM-2 Revision A, 05/94 08/13/14 08/13/14 HC-D4N-3C/D9290K 21 E90 PT6A-343 PT6A-354 IGW to 10,500 lb., DABS (SA4010NM) E90-34-IM Revision C, 06/17/16 E90-34-1900 Revision A, 11/09/10 HC-D4N-3C/D9290K

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA3593NM FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: April 17, 2017

Page 4 of 8 Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 22 E90 PT6A-135A5 IGW to 10,500 lb., DABS (SA4010NM) E90-135A-IM Revision E, 06/21/16 E90-135A-1900 Revision B, 10/20/16 HC-D4N-3C/D9290K 23 E90 PT6A-1356 PT6A-135A6 IGW to 10,500 lb., DABS (SA4010NM) C90/E90-135A-IM-SH Revision H, 05/02/16 E90-135A-1900SH Revision A, 12/09/10 HC-D4N-3C/D9290K 24 C90GT, C90GTi PT6A-135A 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM) C90GT-IM Revision P, 05/02/16 C90GT-1900 Revision G, 06/07/16 HC-D4N-3C/D9290K 25 C90, C90A PT6A-1356 PT6A-135A6 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM) C90/E90-135A-IM-SH Revision H, 05/02/16 C90-135A-1900SH Revision D, 06/07/16 HC-D4N-3C/D9290K 26 C90, C90A PT6A-354 10-PR main tires, IGW to 10,350 lb., DABS (SA4010NM) C90-35-IM Revision B, 06/17/16 C90-35-1900,

NOE-001-11 C90-35-1900-TFM-1 C90-35-1900-TFM-2 Revision IR, 09/19/08 06/02/11 07/23/10 07/21/10 HC-D4N-3C/D9290K 27 C90, C90A PT6A-135A5 C90-135A-IM Revision J, 05/02/16 09-135-206 Revision B, 01/25/16 HC-D4N-3C/D9290K 28 C90GT, C90GTi PT6A-135A C90GT-IM Revision P, 05/02/16 09-135-206 Revision B, 01/25/16 HC-D4N-3C/D9290K 29 C90, C90A PT6A-1356 PT6A-135A6 C90/E90-135A-IM-SH Revision H, 05/02/16 09-135-206 Revision B, 01/25/16 HC-D4N-3C/D9290K 30 C90A PT6A-21 10-PR main tires, IGW to 10,500 lb.

N/A 10-206CGW Revision B, 06/07/16 HC-E4N-3N/D8990K 31 C90GT, C90GTi PT6A-135A 10-PR main tires, IGW to 10,500 lb.

N/A 10-135A-206CGW Revision B, 06/07/16 HC-E4N-3N/D8990SK

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA3593NM FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: April 17, 2017

Page 5 of 8 Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 32 E90 PT6A-28 86-205E Revision M, 06/17/16 13-206E Revision A, 09/17/14 HC-D4N-3C/D9510SK 33 E90 PT6A-28 IGW to 10,500 lb., DABS (SA4010NM) 86-205E Revision M, 06/17/16 13-206EGW Revision A, 09/17/14 HC-D4N-3C/D9510SK 34 E90 PT6A-135A5 IGW to 10,500 lb., DABS (SA4010NM) E90-135A-IM Revision E, 06/21/16 13-E90-135A-1900 Revision A, 09/17/14 HC-D4N-3C/D9510SK 35 E90 PT6A-1356 PT6A-135A6 IGW to 10,500 lb., DABS (SA4010NM) C90/E90-135A-IM-SH Revision H, 05/02/16 13-E90-135A-1900SH Revision A, 09/17/14 HC-D4N-3C/D9510SK 36 C90 PT6A-6/C20, PT6A -20, PT6A -20A, PT6A -21 86-205C Revision Y, 05/02/16 13-206C Revision A, 09/17/14 HC-D4N-3C/D9510SK 37 C90A PT6A -21 86-205C Revision Y, 05/02/16 13-206C Revision A, 09/17/14 HC-D4N-3C/D9510SK 38 C90 PT6A-6/C20, PT6A -20, PT6A -21 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM) 86-205C Revision Y, 05/02/16 13-206CGW Revision B, 06/07/16 HC-D4N-3C/D9510SK 39 C90A PT6A -21 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM) 86-205C Revision Y, 05/02/16 13-206CGW Revision B, 06/07/16 HC-D4N-3C/D9510SK

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA3593NM FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: April 17, 2017

Page 6 of 8 Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 40 C90A PT6A-21 Dual VMO indicator per SB- 20-31-1, 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM) 86-205C Revision Y, 05/02/16 13-206CGW-VMO Revision B, 06/07/16 HC-D4N-3C/D9510SK 41 C90, C90A PT6A-135A5 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM) C90-135A-IM Revision J, 05/02/16 13-C90-135A-1900 Revision B, 06/07/16 HC-D4N-3C/D9510SK 42 C90, C90A PT6A-1356 PT6A-135A6 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM) C90/E90-135A-IM-SH Revision H, 05/02/16 13-C90-135A- 1900SH Revision B, 06/07/16 HC-D4N-3C/D9510SK 43 C90GT, C90GTi PT6A-135A 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM) C90GT-IM Revision P, 05/02/16 13-C90GT-1900 Revision B, 06/07/16 HC-D4N-3C/D9510SK 44 C90, C90A PT6A-135A5 C90-135A-IM Revision J, 05/02/16 13-135-206 Revision B, 07/26/16 HC-D4N-3C/D9510SK 45 C90GT, C90GTi PT6A-135A C90GT-IM Revision P, 05/02/16 13-135-206 Revision B, 07/26/16 HC-D4N-3C/D9510SK 46 C90, C90A PT6A-1356 PT6A-135A6 C90/E90-135A-IM-SH Revision H, 05/02/16 13-135-206 Revision B, 07/26/16 HC-D4N-3C/D9510SK 47 C90GTi PT6A-135A DABS (SA4010NM), BLR Winglets (SA02054SE), Beechcraft IMOW (SA10747SC) 214-6112 Revision B, 02/05/16 14-C90GTx Revision C, 07/26/16 HC-D4N-3C/D9510SK

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA3593NM FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: April 17, 2017

Page 7 of 8 Item Model Engine* Configuration Installation Instructions AFMS Turbofan Propeller System*** AML Amdt Date Doc. No. Revision** Doc. No. Revision** 48 C90GT, C90GTi PT6A-135A DABS (SA4010NM), BLR Winglets (SA02054SE), Beechcraft IMOW (SA10747SC) C90GT-IM Revision P, 05/02/16 14-C90GTRx Revision B, 07/26/16 HC-D4N-3C/D9510SK 49 C90A PT6A-135A5 DABS (SA4010NM), BLR Winglets (SA02054SE), Beechcraft IMOW (SA10747SC) C90-135A-IM Revision J, 05/02/16 14-C90GTRx Revision B, 07/26/16 HC-D4N-3C/D9510SK 50 C90A PT6A-135A6 DABS (SA4010NM), BLR Winglets (SA02054SE), Beechcraft IMOW (SA10747SC) C90/E90-135A-IM-SH Revision H, 05/02/16 14-C90GTRx Revision B, 07/26/16 HC-D4N-3C/D9510SK 51 C90A GE H75-1007 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM), CWLS (SA2939NM) C90-GEH75-100-IM Revision C, 10/21/16 14-NX-206CGW Revision B, 07/26/16 HC-E4W-3/D9290K 52 C90 PT6A-281 10-PR main tires, IGW to 10,500 lb., DABS (SA4010NM) 96-205BC/28 Revision A, 05/24/17 16-206CGW-28 Revision IR, 08/15/17 HC-D4N-3C/D9510SK 8/25/17 53 C90 PT6A-342 IGW to 10,100 lb., DABS (SA4010NM) 88-205BC/34 Revision D, 02/13/18 94-206C-34 Revision B, 02/13/18 HC-D4N-3C/D9290K 3/15/18 * Unless otherwise noted, Pratt & Whitney Canada.

** Or later FAA Approved revision.

*** Hartzell hub/blade part number.

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA3593NM FOR**

INSTALLATION OF TURBOFAN PROPELLER SYSTEM ISSUE DATE: April 17, 2017

Page 8 of 8

Limitations:

1. Installation of the Pratt and Whitney PT6A-28 engines on Models 65-A90, B90, and C90 aircraft must be accomplished in accordance with West Tennessee Aviation STC SA1206SO (B90 and C90), West Tennessee Aviation STC SA822SO (60-A90), or Frakes Aviation STC SA2837SW (applicable to airplane S/N LJ-286 only) as applicable, refer to the appropriate FAA approved type design change and Flight Manual Supplement.

2. Installation of the Pratt and Whitney PT6A-34 engines on Models B90 and C90 aircraft must be accomplished in accordance with Frakes Aviation STC SA3501SW, refer to the appropriate FAA approved type design change and Flight Manual Supplement.

3. Installation of the Pratt and Whitney PT6A-34 engines on Model E90 aircraft must be accomplished in accordance with Blue Aviation STC SA02238AT, refer to the appropriate FAA approved type design change and Flight Manual Supplement.

4. Installation of the Pratt and Whitney PT6A-35 engines on Models C90, C90A, and E90 aircraft must be accomplished in accordance with Blue Aviation STC SA02238AT, refer to the appropriate FAA approved type design change and Flight Manual Supplement.

5. Installation of the Pratt and Whitney PT6A-135A engines on Models C90, C90A, and E90 aircraft must be accomplished in accordance with Blackhawk Modifications STC SA10341SC, refer to the appropriate FAA approved type design change and Flight Manual Supplement.

6. Installation of the Pratt and Whitney PT6A-135/-135A engines on Models C90, C90A, and E90 aircraft must be accomplished in accordance with Silverhawk Aviation STC SA10741SC, refer to the appropriate FAA approved type design change and Flight Manual Supplement.

7. Installation of the General Electric H75-100 engines on Model C90A aircraft must be accomplished in accordance with Nextant Aerospace STC SA01902CH, refer to the appropriate FAA approved type design change and Flight Manual Supplement.

FAA Approved:

for Manager, West Certification Branch AMENDED: March 15, 2018 REISSUED: September 1, 2023

## Every issue (15)

- September 1, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/75/fa/75fadfc4704af33806e02109802ecd8f05015b6d04aa97bd5ac9e17b31f3671e), [SA3593NM_AML.pdf](https://openairdocs.org/files/sha256/e9/c5/e9c5c8ab4a9d0803d531ec43b7e3aadb7331241ef049d3385763e68a348ab9c0)
- March 15, 2018: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/a2/5c/a25c9c7b3f53e4cfd722d85377cec9e8c3e556cc8b3c47b03db02a10a26e325f), [SA3593NM_AML.pdf](https://openairdocs.org/files/sha256/43/81/438137e6daf4d486e5ecf85268f71bbca6c4a8635dc8a8902b154b17241a8b41)
- April 17, 2017: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/a2/5c/a25c9c7b3f53e4cfd722d85377cec9e8c3e556cc8b3c47b03db02a10a26e325f), [SA3593NM_AML.pdf](https://openairdocs.org/files/sha256/43/4e/434eb871a3bb82043f327c1617ff6e58459fcc5b28630ceb1c64b1fd44fdb0e2)
- April 1, 2016: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/f1/c5/f1c5d2d4626d06e724181d2024c5d98120389467f01cf7f386f076f6e83996b8)
- November 10, 2015: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/f1/06/f106d051c7f6d8bad4e989ebb71375afc78f728cbeee203e3883c07e7d50d04c)
- August 19, 2014: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/53/86/5386aa150361d30aef2c418591c96cd4c56d3710a3c3664666afa2d5f55a7030)
- December 31, 2013: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/23/60/236034d68a3c8a0fa231464e3ea1d5979ce580ff88a893f894927ab2005c391f)
- July 27, 2012: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/a0/ac/a0acf9575cab7463310634a335f32f1ee628a60a189e38a1a7ee710dd0aec3c2)
- November 9, 2010: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/77/47/77479daaa9dfb312866a9b2a5c3f367c01fdb7bb6892ff1a0cc14722d1065596)
- November 4, 2009: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/8f/11/8f11c3f5d063bbd36765c116a4c0de46430fd3115004f66fd6fd4b7a49da2c3d)
- March 25, 2009: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/c8/94/c894953846542950663d29169c3fa2b241060cd868781fca6b08a47bdf042faf)
- December 9, 2008: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/d1/d0/d1d014d7ca9c48b53f6acce52bdc0bb0be503a1c5897edda9f6dc2d0074da3bf)
- September 2, 2008: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/9c/8e/9c8e705fdf9081e2a89b5a81571d32e85ba11466071e97c7df31521bbca7f3f6)
- March 15, 2008: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/1b/51/1b518db8ae7aded411bcec0e0d501acefd3486037583fd1c900fcfe8d29a9c34)
- May 9, 2006: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/64/2b/642b92fc4a2cf640149eaff201a2d12c8f67e153a03ffa586c16859677a1e725)

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