What it approves
Installation of Honeywell EGPWS Software -218-218 with optional Runway Awareness and Advisory System (RAAS) in Honeywell MK V EGPWS Computer in accordance with the -1 Configuration of Bombardier Aerospace Business Aviation Services Master Document List, Document Number BAS63017003, Revision NC, dated September 7, 2004, or later FAA-approved revision.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Part 25 of the Federal Aviation Regulations.
Installation of Master Document List (MDL):
MDL -1 Configuration: Honeywell EGPWS Software -218-218 or later FAA approved version.
MDL -2 Configuration: optional Runway Awareness and Advisory System (RAAS).
MDL -3 Configuration: Honeywell EGPWS Software -230 Mod 1-230 Mod 1 or later FAA approved version.
MDL -4 Configuration: optional SmartRunway RAAS.
MDL -5 Configuration: optional SmartLanding Monitor.
MDL -6 Configuration: optional Inhibit Switch.
in a Honeywell MK V EGPWS Computer in accordance with Bombardier Aerospace Business Aviation Services Master Document List, Document Number BAS63017003, Revision A, dated July 01, 2010, or later FAA-approved revision.
1. MDL -1 Configuration and MDL -3 Configuration require that the aircraft be equipped with a previously approved installation of a Honeywell MK V EGPWS Computer with version -212-212 software or later FAA approved version.
(Limitations and Conditions continued on Page 3 of 4)
Learjet, Inc.
85-173 Bradley International Airport Windsor Locks, CT 06096 A21EA Make : Bombardier, Inc.
Model : CL-600-2B16 (CL-601-3A, CL-601-3R, CL-604 Variants)
Date of application : September 3, 2004
Date of issuance : September 16, 2004
Date amended : November 30, 2004; July 08, 2010
( Signature) Robert G. Mann Manager Boston Aircraft Certification Office
( Title)
United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number ST00205BO July 08, 2010
FAA Form 8110-2-1(10-69) Page 2 of 4
Transfer the ownership of Supplemental Type Certificate Number
to (Name of transferee)
(Address of transferee) (Number and street)
( City, State, and ZIP code)
from (Name of grantor)(Print or type)
(Address of grantor) (Number & street)
(City, State, and ZIP code)
Signature of grantor ( In ink):
United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number ST00205BO July 08, 2010
FAA Form 8110-2-1(10-69) Page 3 of 4
Limitations and Conditions: (continued from Page 1 of 4)
2. MDL -1 Configuration is a prerequisite for MDL -2 Configuration.
3. MDL -3 Configuration is a prerequisite for MDL -4 Configuration and/or MDL -5 Configuration.
4. MDL -2 Configuration or MDL -4 Configuration or MDL -5 Configuration is a prerequisite for MDL -6 Configuration.
5. MDL -4 Configuration does not include the Takeoff Flap Configuration Monitor Non-Routine Advisory/Caution of ‘Flaps, Flaps’.
6. MDL -5 Configuration does not include the Stabilized Approach Monitor Non-Routine Advisory/Caution of ‘Excessive Approach Speed’.
7. MDL -4 Configuration approved aural alert volume levels are documented in Bombardier Aerospace Business Aviation Services Installation Instruction SmartRunway/RAAS Document No. BAS63247003, Revision NC, dated May 11, 2010, later FAA approved revision.
8. MDL -5 Configuration approved aural alert volume levels are documented in Bombardier Aerospace Business Aviation Services Installation Instruction SmartLanding Monitor Document No. BAS63247002, Revision NC, dated May 11, 2010, later FAA approved revision
9. Operation must be in accordance with Bombardier Aerospace Business Aviation Services Airplane Flight Manual Supplement (AFMS) as follows:
MDL -1 Configuration or MDL -3 Configuration: No change to the existing AFM.
MDL -2 Configuration: Document No. BAS63047006, Revision NC, approved November 30, 2004, or later FAA approved revision.
MDL -4 Configuration through MDL -6 Configuration: Document No. BAS63047006, Revision A, approved July 08, 2010, or later FAA approved revision.
The applicable AFMS must be carried in the aircraft during all flights.
10. Maintenance must be in accordance with Bombardier Aerospace Business Aviation Services Instructions for Continued Airworthiness (ICA) as follows:
MDL -1 Configuration: No change to the existing Instructions for Continued Airworthiness (ICA’s).
MDL -2 Configuration: Document BAS63017003-IFCA-2, Revision NC, dated October 20, 2004 or later FAA accepted revision.
MDL -3 Configuration: Document BAS63017003-ICA-3, Revision NC, dated May 7, 2010 or later FAA accepted revision.
MDL -4 Configuration: Document BAS63017003-ICA-4, Revision NC, dated May 13, 2010 or later FAA accepted revision.
MDL -5 Configuration: Document BAS63017003-ICA-5, Revision NC, dated May 13, 2010 or later FAA accepted revision.
MDL -6 Configuration: Document BAS63017003-ICA-6, Revision NC, dated May 13, 2010 or later FAA accepted revision.
The applicable ICA must be made available to the operator at the time of installation.
11. Compatibility of this design with previously approved modifications must be determined by the installer.
United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number ST00205BO July 08, 2010
FAA Form 8110-2-1(10-69) Page 4 of 4
Certification Basis:
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 Bombardier, Inc. CL-600-2B16 (CL-601-3A, CL-601-3R, CL-604 Variants) aircraft is as follows:
a. The type certification basis for Bombardier, Inc. CL-600-2B16 (CL-601-3A, CL-601-3R, CL-604 Variants is shown on TCDS A21EA for parts not changed or not affected by the change.
b. The certification for parts changed or affected by the change since the reference date of application, September 3, 2004, is based upon part 25 as amended by Amendment 25-115. 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 was determined to be:
Regulations at the latest amendment 25-0 through 25-115
25.1, 25.29, 25.301, 25.303, 25.307, 25.601, 25.603, 25.771, 25.777, 25.1322, 25.1351, 25.1381, 25.1529,
25.1581
Regulations at the amendment level in TCDS A21EA
25.305, 25.341, 25.561, 25.613, 25.773, 25.869, 25.1301, 25.1309, 25.1353, 25.1431
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.
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ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 3
Every issue · 3
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| July 8, 2010 | Amended, current | Certificate |
| November 30, 2004 | Amended, earlier issue | Certificate |
| September 16, 2004 | Issued, earlier issue | Certificate |