STC SA58NE

Par t 25 of the Federal Aviation R egulations.

Original Product Type Certificate N umber:

M ake:

M odel:

Description of Type Desig n Change:

Passenger interior and supplementary avionics installations in accordance with I.A.L. Drawing List:

Configuration 1: ML 9830 Revision G, dated January 24, 1982, and Report No. TM-600-571 Rev. B, dated April 23, 1982.

OR

1. The Following Canadian Department of Transport approved flight manual supplements are required as indicated:

a. For Configuration 1 & 2: FMS CL-600-IAL-1 Passenger Oxygen System, Rev. D, dated April 13, 1982.

Bombardier Completion Center Inc.

200 Cote Vertu West Dorval, Quebec H4S 2A3 Canada

A21EA Bombardier, Inc.

CL-600-1A11 Date reis sued : May 23, 1988, February 4, 2000

Date amended : 8/26/82, 9/21/82, 6/22/83, 7/12/83, 9/21/83, 12/22/83, 5/16/84, 8/21/86, 9/18/86, 5/23/88

B y direction of the A dministrator

(Signature) Gaetano Sciortino Manager New York Aircraft Certification Office

(Title)

Date of application : August 12, 1983

Date of issuance : March 29, 1982

FAA Form 8110-2-1(10-69) Page 4 of 4

N umber SA58NE Date Reissued: February 4, 2000

Description of Type Design Change (Continued):

Configuration 2: ML9830-3 Revision G, dated September 15, 1982, and Report No. TM-600-610 Rev. D, dated April 10, 1984.

OR Configuration 3: ML9830-9 Revision C, dated May 13, 1983.

OR Configuration 4: ML9830-8 Revision D, dated September 4, 1983.

OR Configuration 5: ML9830-10 Revision E, dated December 2, 1983 (amends and supplements Configuration 4).

OR Configuration 6: ML 9128 Revision M, dated August 14, 1986, and amendment Innotech Aviation Report No. TM-600-1018, dated August 27, 1986.

OR Configuration 7: ML9830-2 Revision G, dated January 14, 1983.

b. For Configuration 3: FMS CL-600-IAL-1 Passenger Oxygen System, Rev. E, dated March 16, 1983.

c. For Configuration 4 and 5: FMS CL-600-IAL-1A Passenger Oxygen System, original issue dated June 7, 1983.

d. For Configuration 1: FMS CL-600-IAL-9 CMA 771 Omega/VLF Navigation System, Rev. C, dated April 20, 1982.

e. For Configuration 2: FMS CL-600-IAL-17 GNS 500A III Omega/VLF Navigation System, original issue dated September 16, 1982.

f. For Configurations 1 and 2: FMS CL-600-IAL-10 Single Litton 72RL INS, original issue, dated February 18, 1982.

g. For Configuration 3: FMS CL-600-IAL-31 Global GNS 500A Series 3 System Rev. B, dated July 12, 1983.

h. For Configuration 3: FMS CL-600-IAL-43 Delco C-6 I.N.S. original issue dated May 27, 1983.

i. For Configurations 1 and 2: FMS CL-600-IAL-11 Sperry Voice Advisory System Model VA-100, Rev. A, dated March 9, 1982.

j. For Configurations 3, 4, and 5: FMS CL-600-IAL-11 Sperry Voice Advisory System Model VA-100, Rev. B, dated May 26, 1983.

k. For Configurations 1, 2, and 3: FMS CL-600-IAL-12 Sperry Air Data Command Indicator Model CD 125, original issue, dated 2/18/82.

l. For Configurations 2 and 3: FMS CL-600-IAL-22 Fairchild Model A-100 Cockpit Voice Recorder System, original issue dated November 17, 1982.

m. For Configurations 2 and 3: FMS CL-600-IAL-41 Fairchild Model 5425 Flight Data Recorder System, original issue dated April 8, 1983.

n. For Configuration 2: FMS CL-600-IAL-14 Sperry A.D.C. #2 System, original issue dated March 29, 1983.

o. For Configuration 5: FMS CL-600-IAL-14 Sperry A.D.C. #2 System, Revision A, dated November 29, 1983.

p. For Configurations 3 and 4: FMS CL-600-IAL-30 Sperry A.D.C. #2 System, Revision A, dated July 12, 1983.

q. For Configuration 5: FMS CL-600-IAL-53 Ryan WX-10 Stormscope System, original issue dated November 29, 1983.

r. For Configuration 2: FMS CL-600-IAL-33 Sperry Data Nav III System, original issue dated January 12, 1983.

s. For Configuration 4: FMS CL-600-IAL-56 Sperry Data Nav III System, Rev. B, dated September 21, 1983.

t. For Configuration 5: FMS CL-600-IAL-56 Sperry Data Nav III System, Rev. C, dated December 2, 1983.

u. For Configuration 4: FMS CL-600-IAL-47 Single Global GNS-500A Series 3C and Vandling NDB-2 System dated September 16, 1983.

v. For Configuration 5: FMS CL-600-IAL-57 Single Global GNS-500A Series 3C original issue dated November 29, 1983.

w. For Configuration 4: FMS CL-600-IAL-48 Dual Delco C-6 Inertial Navigation System with Vandling NDB-2 dated September 16, 1983.

x. For Configuration 5: FMS CL-600-IAL-55 Honeywell NAV Inertial Navigation System Model YG1761, original issue dated November 29, 1983.

FAA Form 8110-2-1(10-69) Page 4 of 4

N umber SA58NE Date Reissued: February 4, 2000

y. For Configuration 4: FMS CL-600-IAL-49 Sperry EFIS System Rev. B, dated September 21, 1983.

z. For Configuration 5: FMS CL-600-IAL-58 Dual Sperry Electronic Flight Instrument System Model EDZ-800 Rev. A, dated December 2, 1983.

aa. For Configuration 6: FMS CL-600-IAL-1B Passenger Oxygen System, Rev. A, dated September 8, 1986.

bb. For Configuration 6: FMS CL-600-IAL-4B Dual Litton 72 RL Inertial Navigation System, Rev. B, dated September 8, 1986.

cc. For Configuration 6: FMS CL-600-IAL-5B Single CMA 771 OMEGA/VLF Navigation System, Rev. B, dated September 8, 1986.

dd. For Configuration 6: FMS CL-600-IAL-88B Sperry A.D.C. #2 System Model AZ-242, Rev. A, dated September 8, 1986.

ee. For Configuration 7: FMS CL-600-IAL-1 Passenger Oxygen System, Rev. E, dated March 16, 1983.

ff. For Configuration 7: FMS CL-600-IAL-12 Sperry CD125 Air Data Command, original issue, dated February 18, 1982.

gg. For Configuration 7: FMS CL-600-IAL-14 No. 2 Sperry AZ 242 Air Data Computer, Rev. A dated November 29, 1983.

hh. For Configuration 7: FMS CL-600-IAL-31 Single Global GNS 500A Series 3 Nav System, Rev. B, dated July 12, 1983.

ii. For Configuration 7: FMS CL-600-IAL-32 Single Delco MK IV AX I.N.S., Rev. B, dated May 18, 1988.

jj. For Configuration 7: FMS CL-600-IAL-33 Sperry Data III System, original issue, dated January 12, 1983.

2. For Configurations 3, 4, and 5: That portion of the data pertaining to the Sperry A.D.C. #2 System and the FMS specified in Limitation 1.o. and 1.p. are eligible only on 40,400 lb MTOW aircraft.

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

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.

……….END……….