STC SA02846NY

United States of America Project #ST6728 NY-A Department of Transportation Federal Aviation Administration Supplemental Type Certificate IMPORT Number: SA02846NY This certificate issued to: MT- Propeller Entwicklung GmbH FlugplatzstraBe 1 94348 Atting. Germany furt 23 of the Federal Regulations.

Original Product -- Type Certificate Number: No. A4CE Cessna Aircraft Corporation Model: 206H. T206H Description of Type Design Change:

Installation of 5-blade propeller MTV-5-1-D-C-F-R(A)/CFR210-56 propeller in accordance with MT Propeller Installation Instruction Doc. No. E-1831, Original Issued, December 1, 2009. The following MT Propeller documents are required with this installation:

1831, Original Issued, December 1, 2009. Airplane Flight Manual Supplement Doc. No. E-1830, Original Issued, December 1. 2009 and Installation Instruction Doc. No. E- Simituticas und Conditions:

1. The Installer must determine whether this design change is compatible with previously approved modifications. 2. 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.

3. This STC modification can only be installed on Cessna 206H and T206H that have incorporated FAA STC No. SA01878SE (Soloy Mark II Turbine Conversion).

(See Continuation Sheet 2 of 2) balministrater of the Federal Aviation Administration .

Date of Application: June 28, 2010 Date Reissued:

Date of Issuance: September 16, 2010 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Franco Piera (Signature) TOMINISTRATO Manager Anthony Socias PoN New York Aircraft Certification Office (Title) FAA Form 8110-2(10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA02846NY Issuance date: September 29, 2010 Certificutica Busis:

Based on 14 CFR $§ 21.115 and 21.101, and the FAA policy for changes that are not significant in FAA Order 8110.48. the certification basis for this modification are as follows:

• The type certification basis for the Cessna Models 206H and T206H Aircraft are Type Certified under TCDS NO. A4CE for parts not changed or not affected by the change.

• The type certification basis for the Cessna Models 206H and T206H Aircraft are Type Certified under TCDS NO. A4CE for parts changed or affected by the change with the following 14 CFR exceptions:

23.29 23.21 23.1 Amendment 23-21 Amendment 23-34 Amendment 23-45 23.1041 23.1043 Amendment 23-51 Amendment 23-51

23.45 23.33 Amendment 23-50 Amendment 23-50 23.1155 23.1045 Amendment 23-7 Amendment 23-51

23.49 23.51 Amendment 23-50 Amendment 23-50 23.1501 23.1305 Amendment 23-21 Amendment 23-52

23.53 Amendment 23-50 23.1521 Amendment 23-50

23.73 23.75 23.65 23.69 23.71 23.77 23.63 Amendment 23-50 Amendment 23-50 Amendment 23-50 Amendment 23-50 Amendment 23-50 Amendment 23-50 Amendment 23-50 23.1587 23.1559 23.1581 23.1583 23.1541 23.1529 23.1549 Amendment 23-50 Amendment 23-50 Amendment 23-50 Amendment 23-50 Amendment 23-21 Amendment 23-45 Amendment 23-26

23.201 Amendment 23-50

23.207 Amendment 23-50 14 CFR Section 36 Amendment 36-28

23.251 Amendment 23-50

23.629 Amendment 23-48

23.901 Amendment 23-53

23.905 Amendment 23-43

23.907 Amendment 23-51

23.925 Amendment 23-51

23.929 Amendment 23-51

23.933 Amendment 23-51

23.937 Amendment 23-43 END FAA Form 8110-2-1(10-69) Page 2 of 2

United States of America Profect #ST6729NY-T Department of Transportation Federal Aviation Administration Supplemental Type Certificate IMPORT Number: ST02852NY This certificate issued to: Bombardier Aerospace Dorval. Québec H4S 1Y9, Canada as specified hereen meets the airverthiness requirements of : Purt 25 of the Federal. brialion Regulations. Certifies that the change in the type design for the following product with the limitations and conditions therefore Original Product - Type Certificute Number: T00005NY Malco: Bombardier Model: BD-100-1A10 Description of Type Design Change:

Data Summary Number G573000 Revision N/C, Transport Canada approved May 19 2010 or later Transport Canada approved revision. Aircell Air-to-Ground Communication System and Inmarsat Satcom System Installation in accordance with ACS-NAI Ltd. Modification Limitations and Conditions:

2. The installer must determine whether this design change is compatible with previously approved modifications. 1. Maintenance must be in accordance with Instruction for Continued Airworthiness Bombardier documents BAS68058000-ICA and If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person BAS68050007-ICA Revision F1 dated January 27 2010, or later Transport Canada accepted revision. written evidence of that permission.

Arintion Administration suspended, revcked or a termination date is otherwise estublished by the Administruter of the Federal.

Date of Application: June 10 2010 Date Reissued:

Date of Issuance: September 28. 2010 Date Amended:

FEDERAL AVIATION By Direction of the Administrator TOMINSTRATO Anthony Socias (Signature) Manager New York Aircraft Certification Office

47.

United States of America Project #-ST6632NY-A Department of Transportation Federal Aviation Administration Supplemental Type Certificate IMPORT Number: SA02854NY This certificate issued to: Seaplanes West Inc.

Hangar 36, 51401 RR 221 Sherwood Park, Alberta T8E IH1 Canada :Purt. 3 of the Civil Aviation Bequlations.

Original Product - Type Cerlificate Number: 3A13 Abater: Cessna

•Abedel: 182P, 182Q, and 182R Description of Type Design Change:

Engineering Order EO354301, Revision 2, dated June 4, 2010, or later approved Transport Canada revision. Gross weight increase for use with floats to be accomplished in accordance with Transport Canada approved Seaplanes West (SPW) Limitations and Conditions:

3. 1. Operate in accordance with SPW Flight Manual Supplements FMS354301, Revision 1, FMS 354302, Revision 2, FMS354311, Maintain in accordance with SPW Maintenance Manual Supplement and Instructions for Continued Airworthiness MMS354301, Revision 2, dated August 16. 2010, or later Transport Canada approved revisions. This STC does not approve the use of the 3500 Aerocet floats for use on model 182R Revision 1 or FMS354312, Revision 2, all dated July 16, 2010, all TCCA approved September 22, 2010, or later approved Transport Canada revision as applicable to the aircraft model and gross weight configuration installed.

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

5. If the holder agrees to permit another person to use the certificate to alter the product, the holder must give the other person

10225 Ryan Avenue Dorval, Quebec Canada H9P 1A2 Purt 25 o/ the Federal Aviation Pegulations.

Original Product - Type Lerlificate Number: T00005NY Make: Bombardier Inc.

Model: BD-700-1A10, Serial No. 9036 Description of Type Design Change:

The modification of Passenger Cabin Entertainment System to be done in accordance with Innotech Aviation Master Drawing List MDL30107002 Revision NC, dated March 5, 2010, or later Transport Canada approved revision.

1. Maintenance must be in accordance with Kmlex Aviation Inc. TL30107-004 Time Limits and Maintenance Checks, Cabin Entertainment System Upgrade, A/C BD-700-1A10, SN 9036, Revision NC, dated March 5, 2010.

2. Descriptive data pertaining to this design change are considered inadequate for duplication in other product. This approval is limited to only the installation made in airplane Serial Number 9036 only.

Administration suspended, revsked or a terminution date is elherwise estublishet ly the Administrator of the Federal Aviation Date of Application: June June 2010 Date Reissued:

Date of Issuance: October 5, 2010 Date Amended:

FEDERAL AVIATION By djection of the Adduvinistrater aus E Deline * foR Anthony Socias (Signature) TOMINISTRATIO Manager New York Aircraft Certification Office (Title) FAA Form 8110-2(10 punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

Project # St c38ONY-T United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate IMPORT Number: ST0285TNY This certificate issued to: Aero Consulting Services Limited 25 Dunlop Avenue Winnipeg, Manitoba Canada R2X 2V2 Purt 25 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: A21EA Make: Bombardier, Inc.

Model: CL-600-2B16 Description of Type Design Change:

Modification to be completed in accordance with Aero Consulting Services Ltd. Modification Data Summary F418000 Revision F dated May 05, 2010 or later Transport Canada approved revision.

1. Refer to Aero Consulting Services Ltd. Airplane Flight Manual Supplement 41-299M003 Revision A dated October 14, 2009 or later Transport Canada approved revision.

2. Maintenance must be performed in accordance with Aero Consulting Services Ltd. Mandatory Maintenance Manual Supplement

3. Maintenance must be performed in accordance with Aero Consulting Services Ltd. Mandatory Maintenance Manual Supplement F230070 Revision A dated September 23, 2008 or later Transport Canada approved revision.

F418070 Revision NC dated June 11, 2009 or later Transport Canada approved revision.

4. Maintenance must be performed in accordance with Aero Consulting Services Ltd. Mandatory Maintenance Manual Supplement F418071 Revision NC dated June 11, 2009 or later Transport Canada approved revision.

5. For Instructions for Continued Airworthiness refer to "Instructions for Continued Airworthiness for the Installation, Complete Custom Aircraft Interior" 41-027E075 Revision A dated June 16, 2009 or later Transport Canada accepted revision.

6. Descriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in Bombardier CL-600-2B16, Serial Number 5717. This STC does not permit manufacturing of parts for multiple installations.

Bute of uppliention: June 16, 2009 Date Reissued:

Dule of issuunce: October 14.2010 Lute umended:

FEDERAL AVIATION By Direction of the Administrator F6F- Anthony Socias (Signature) TOMINISTRATO Manager New York Aircraft Certification Office (Title) 47

United States of America Project # 5T6738NY-R Department of Transportation Federal Aviation Administration Supplemental Type Certificate IMPORT Number: SR02843N% This certificate issued to: Canadian Heli-Structures Ltd.

9-5225- 216th Street Langley, British Columbia Canada V2Y 2N3 Surt 29 of the Federal Aviation Regulutions.

Original Product Type Cerlificate Number: * See attached FAA Approved Model List (AML) No. SR02843NY for a list of approved models and applicable airworthiness regulations Make: * Model:

Installation of Sliding Door Pop Out Windows in accordance with ICE Designs Co. Drawing Package 07002DP-L, Revision 1, Dated December 02, 2009, approved by Transport Canada Civil Aviation (TCAA) on April 13, 2010, or later TCCA approved revisions.

1. This modification is to be maintained in accordance with the Instructions for Continued Airworthiness document specified in AML SR02843NY or later TCCA accepted revisions.

Date of Application: April 14,2010 Date Reissued:

Dule of issmunce: September 9, 2010 Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signature) TOMINISTRATO Anthony Socias Manager New York Aircraft Certification Office (Title) te is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both ificate may be transferred in accordance with FAR 21.47

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR02843NY Date of Issuance: September 9, 2010 Limitations and Conditions: (Continued).

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

3. If the holder agrees to permit another person to use the certificate to alter a product, the holder must give the other person written evidence of that permission.

4. A copy of this certificate and the FAA AML No. SR02843NY, Issued September 9, 2010, must be maintained as part of the permanent records of this modified aircraft.

Busis of Cerlificution:

FAR Part 29 Dated February 1, 1965, (Transport Category A& B) Including Amendments 29-1 thru 29-9 FAR 29.801 Dated February 1, 1977 (Ditching) Amendment 29-12 FAR 29.853 Dated November 26, 1984 (Compartment Interiors) Amendment 29-23 ...........END.........

FAA Form 8110-2-1(10-69) Page 2 of 2

APPROVED MODEL LIST (AML) NO. SR02843NY CANADIAN HELI-STRUCTURES LTD. INSTALLATION OF SLIDING DOOR POP OUT WINDOWS Issue Date: September 9, 2010 INSTRUCTION FOR CONTINUED AML AMENDMENT DATE AIRWORTHINESS ICE Designs Co. Component Maintenance Manual No. 07002CMM-L, Revision 1, December 12, 2009 accepted by TCAA April 13, 2010, or later TCCA accepted revisions FAA Approved: Jun Anthony Socias Manager, New York Aircraft Certification Office FOR TCDS H4SW H6SW H10SW Page 1 of 1 MODEL 212, 412, 412CF, 412EP 214B, 214B-1 214ST MAKE Bell Helicopter Textron, Inc. Bell Helicopter Textron, Inc. Bell Helicopter Textron, Inc.

REGULATION Federal Aviation Federal Aviation Federal Aviation PART 29 29 29

troject # St4+74N4-T United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate NumberST02856NY This certificate issued to: Monogram Systems- TIA Division 44931 Falcon Place Sterling, VA 20166 Certifies that the change in the type design for the fellowing preduct with the limitations and cenditicas therefer as specified hereen meets the nirverthiness requirement's of Purt 25 of the Federal Aviation ¿Regulutions.

Original Product - Type Certificate umber: AINM The Boeing Company Model: 767-200, -300, -300F, -400ER Description of Type Design Change:

Installation of a TIA Model 1547 Convection Oven, part number 400-2286-01, in accordance with Monogram Systems TIA Division Master Drawing List ST-OV-007, Revision B, dated October 14, 2010, or later FAA approved revision.

1. Monogram Systems TIA Division Instructions for Continued Airworthiness, document number ST-OV-013, Revision IR, dated August 26, 2010, or later FAA accepted revision, is required for this installation.

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

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.

Lute c/ applicution: July 30,2009 Date Reissued:

Lute c/ issunce: October 14, 2010 Date Amended:

By Direction of the Administrator FEDERAL AVIATION Anthony Socias (Signature) O. shhel Manager TOMINSTRATIO New York Aircraft Certification Office (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST02856NY Certification Basis:

STC holder for the modification to the Bocing 767 series aircraft modified by this change is as follows: Based on 14 CFR §§ 21.115 and 21.101, for non-significant changes to type design, the certification basis elected by the

a. The type certification basis for Boeing 767 series airplanes is shown on TCDS AINM 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, July 30, 2009, is based upon part 25 as amended by Amendment 25-128, and 14 CFR part 26. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for non-significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be as shown in the TCDS AINM except the regulations listed below:

Section Title Amendment $25.29 Empty Weight and 25-72 Corresponding Center of Gravity $25.305 Strength and Deformation 25-86 $25.307 Proof of Structure 25-72 $25.561 Emergency Landing Conditions 25-64 $25.603 Materials 25-46 $25.605 Fabrication Methods 25-46 §25.613 Material Strength Properties and 25-72 Material Design Values $25.1316 System Lightning Protection 25-80

825.1351 Electrical Systems and 25-72 Equipment 14 CFR Part 26 regulations Based on 14 CFR § 21.101(g), applicable provisions of 14 CFR part 26 are included in the certification basis. For any future STC amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of the issuance date of this STC, compliance has been found for the following regulation: 14CFR § 26.11, amendment 26-0 through 26-3.

---END---

FAA Form 8110-2-1(10-69) Page 2 of 2

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST02659NY-D This certificate issued to: Delta Engineering 13 DRBA Way New Castle County Airport New Castle, Delaware 19720 Certifies that the change in the type design fox the following product with the limitations and conditions therefon as specified hexcon meets the airwonthiness requirement's of Part 25 of the Federal Svintion Regulations.

Original Product - Type Certificate Numben: AINM Make: Boeing Model: 767-300 Series Description of Type Design Change:

dated Oct. 7, 2010 or later FAA approved revisions to Delta Engineering Master Data List previously listed. Instructions for Continued Airworthiness as listed on the Master Data List required for this alteration. Update of Cabin Crew Rest in accordance with Delta Engineering Master Data List 0144-06658-2214 Revision C Limitations and Conditions:

1. If the holder agrees to permit another person to use the certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of Application: September 24, 2009 Date Reissued:

Date of Issuance: October 8, 2010 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Lotte TO MINISTRATO Jonathan E. Meritz ODA Administrator Delta Engineering, ODA-800728-NE FAA Form 8110-2 (10-68) Page 1 of 2 Pages

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST02659NY-D Date of Issuance: October 8, 2010 Limitations and Conditions: (continued):

3. The Cabin Crew Rest must interface with the following listed required existing components/systems, which must 2. Compatibility of this design change with previously approved modifications must be determined by the installer. be installed in a manner acceptable to the FAA Administrator, The below listed required existing components/systems are not approved by this STC.

Required existing components/systems:

Component/System Manufacture Boeing Model Additional Requirements Cabin Configuration Or Boeing TC Heath Tecna or FAA STC ST02214NY-D Seat Change Weber FAA TSO Service Bulletin 866139-25-3120 Bertification Bassis:

certification basis for the Boeing 767-300 Series aircraft with this STC is as follows: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the The type certification basis for Boeing 767-300 Series airplanes is shown on TCDS AINM for parts not changed or not affected by the change.

The certification basis for parts changed or affected by the change since the reference date of application, Sep. 24, 2009 is based upon part 25 as amended by Amendment 25-122. Based on 14 CFR $§ 21.115 and 21.101, and the FAA policy for TCDS AINM except the regulations listed below: significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be as shown on the Additionally 14 CFR Part 26 is applicable to this STC This STC does not require a revised Electrical Wiring Interconnection System (EWIS) Instructions for Continued Airworthiness (ICA).

Section $25.785 $25.831 Seats, berths, safety belts, and harnesses Ventilation Title At Amendment 25-88 $25.1431 §25.1529 $25.1353 $25.1351 $25.1307 $25.981 $26.47 $25.853 $25.869 $26.11 Instructions for Continued Airworthiness Electrical equipment and installations Aging Aircraft Safety Rule Miscellaneous Equipment Electronic equipment Fire protection: systems Fuel tank temperature Compartment interiors General EWIS 25-113 25-113 25-102 25-116 25-113 25-54 25-72 26-1 25-72 25-89 26-0 -END- FAA Form 8110-2 (10-68) Page 2 of 2 Pages

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST02660NY-D This certificate issued to: Delta Engineering 13 DRBA Way New Castle County Airport New Castle, Delaware 19720 Part 25 of the Federal Ilviation Regulations.

Original Product - Type Certificate Numben: A31SO Make: Embraer Model: EMB-120ER Description of Type Design Change:

Installation of a Rockwell Collins TCAS-94 in accordance with Delta Engineering Master Data List 0166-07020- 2229 Revision B dated October 01, 2010 or later FAA approved revisions to Delta Engineering Master Data List previously listed. Instructions for Continued Airworthiness and Airplane Flight Manual Supplement as listed on the Master Data List required for this alteration.

1. If the holder agrees to permit another person to use the certificate to alter the product, the holder shall give the other person written evidence of that permission.

2. Compatibility of this design change with previously approved modifications must be determined by the installer.

Date of Application: June 30, 2010 Date Reissued:

Date of Issuance: October 01, 2010 Date Amended:

FEDERAL AVIATION By Direction of the Administrator TOMNSTRATC John A. Moritz cad ODA Administrator ohn A. Morik gnature/ Delta Engineering, ODA-800728-NE Nito FAA Form 8110-2 (10-68) Page 1 of 2 Pages

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number STO2660NY-D Issuance Date: October 1, 2010 Limitations and Conditions: (continued):

3. If an Avidyne FLIGHTMAX display had TCAS (TRAFFIC) display enabled the system must be updated to the FLIGHTMAX is not approved by this STC. disable the TCAS (TRAFIC) display. This is also required for any other display system showing TCAS except for the TVI/VSI installed by this STC. The approval to remove display from other systems such as

4. The Rockwell Collins TCAS-94 must interface with the following listed required existing listed required existing systems are not approved by this STC. systems/components, which must be installed in a manner acceptable to the FAA Administrator, The below Required existing systems/components:

System/Component Transponder Rockwell Collins Manufacture TDR-94 Model Additional Requirements Certification Basis:

certification basis for the EMB-120ER aircraft with this STC is as follows: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the

a. The type certification basis for EMB-120ER airplanes is shown on TCDS A31SO 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 regulations listed below: §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the application, June 30, 2010 is based upon part 25 as amended by Amendment 25-122. Based on 14 CFR certification basis for this modification was determined to be as shown on the TCDS A20WE except the

c. Additional CFR 14 Part 26 is applicable to this STC Instructions for Continued Airworthiness (ICA). This STC does not require a revised Electrical Wiring Interconnection System (EWIS) Section 25.1307 25.1351 25.831 25.853 25.869 25.981 Fuel tank ignition prevention Miscellaneous equipment Fire protection: systems Compartment interiors Ventilation General Title At Amendment 25-113 25-102 25-116 25-72 25-89

25.1585 25.1353 25.1557 25.1581 25.1583 25.1431 26.11 26.47 Miscellaneous markings and placards Electrical equipment and installations Electronic equipment Operating limitations Operating procedures General EWIS AASR 25-105 25-105 25-113 25-72 25-113 25-72 25-72 26-0 26-1 ---END FAA Form 8110-2 (10-68) Page 2 of 2 Pages

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate IMPORT Number: ST02828NY This certificate issued to: Jazz Air LP (Air Canada Jazz) 310 Goudey Drive Halifax International Airport Enfield, Nova Scotia Canada B2T 1E4 Purt 25 of the Federal Aviation

• Requlutions.

Original Product - Type Certificate Number: A21EA Make: Bombardier Aerospace Model: CL-600-2B19 Description of Type Design Change:

Modification of Data Summary report No. A0304000, Rev A, Transport Canada approved October 26, 2005, or later Transport Installation an Aircraft Communications Addressing & Recording System (ACARS) printer in accordance with Air Canada Jazz Canada approved revision.

2. Installation of Aircraft Communications Addressing & Recording System (ACARS) STC ST01000LA-D must be incorporated 1. Maintenance must be in accordance with Air Canada Jazz Maintenance and Engineering Substantiation Report A0304020 Rev A, Transport Canada approved October 26, 2005, or later Transport Canada approved revision. prior to completion of this modification.

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

Administration suspended, reecked or a terination date is otherrise established by the Administrator of the Federal Aviation Date of Application: October 21, 2009 Date Reissued:

Date of Issuance: July 21, 2010 Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signature) No prei Anthony Socias TOMINISTRATO Manager New York Aircraft Certification Office (Title) FAA Form 8110-2(10-68) Page 1 of 1

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST02828NY Date of Issuance: July 21, 2010 Limitations and Conditions: (Continued)

4. 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.

Note: Compliance with 14 CFR § 26.11 was shown as no impact to existing EWIS ICA.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101 and FAA Order 8110.48, the type certification basis for the CL-600-2B19 is as shown on TCDS A21EA for parts changed or affected by the change. Based on 14 CFR §21.101(g), applicable provisions of 14 CFR part 26 are included in the certification basis. For any future 14 CFR part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of the issuance date of this STC, compliance has been found for the following regulations: 14 CFR § 26.11, § 26.35 and § 26.47 (amendment 26-0 through 26-3).

..END....

FAA Form 8110-2-1 (10-69) Page 2 of 2

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate IMPORT Number: ST02829NY This certificate issued to: Bombardier Inc 200 Cote Vertu West Dorval, Quebec Canada H4S 2A3 Surt 25 of the Federal Aviation Original Product - Type Certificute Number : T00003NY Make: Bombardier Model: BD-700-1A10 Description of Type Design Change:

Number G541000 Revision N/C approved February 8, 2010 or later Transport Canada approved revision. Upgrade the Swift64 system to Swiftbroadband system, installed in accordance with Bombardier Inc Modification Data Summary Limitations and Conditions:

3. If the holder agrees to permit another person to use the certificate to alter the product, the holder must give the other person 2. The installer must determine whether this design change is compatible with previously approved modifications. 1. Maintenance must be in accordance with Bombardier Inc. Instructions for Continued Airworthiness document number G541071 Revision N/C, approved January 27, 2010 or later Transport Canada approved revisions. written evidence of that permission.

Date of Application: March March 2010 Date Reissued:

Dule of issuence: July 23, 2010 Bute umended :

By Direction of the Administrator (Signature) O Anthony Socias TOMINSTRATO Manager New York Aircraft Certification Office (Title) FAA Form 8110-2(10-68) Page 1 of 1 ate may be transferred in accordance with FAR 21.47