What it approves
Installation of non-hazard ice protection systems kits
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.
FAA Form 8110-2 (5/14) Page 1 of
Part of the
Signature
Title SA09838AC SMR Acquisition LLC dba SMR Technologies, Inc.
93 Nettie Fenwick Rd.
Fenwick, WV 26202 Federal Aviation Regulations.
1. Installation of non-hazard ice protection systems kits SMR9068-20, SMR9068-21, SMR9068-22, SMR9068-23, SMR9068-30, SMR9068-31, SMR9068-40, SMR9068-41, and SMR9068-50, on the Beechcraft Bonanza series aircraft in accordance with Installation Instructions as listed on Master Document List MDL-0069 Revision B dated April 23, 2014, or later FAA approved revision; and maintained in accordance with the Instructions for Continued Airworthiness (ICAs) listed in the Limitations section of this STC.
(See Description of Type Design Change continued on Page 3 of 4)
1. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft.
2. Flight into known icing is prohibited with this STC.
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.
Anthony E. Gallo Manager New York ACO Branch Beechcraft Corporation F33A (S/N CE-748, CE-772 through CE-1791), A36 (S/N E-1111, E-1241 to E-3635, except E-3630), A36TC (EA-1 through EA-272, except EA-242), (See Model continued on Page 3 of 3) May 20, 2014, March 19, 2019 January 18, 2013 May 16, 2014 3A15 4
FAA Form 8110-2 (5/14) Page 2 of
To (Name and address of transferee)
From (Name and address of grantor)
4 SA09838AC
FAA Form 8110-2 (5/14) Page 3 of
4 Date Reissued: March 19, 2019
Model (continued):
B36TC (EA-242, EA-273 through EA-695), G36 (E-3630, E-3636 through current)
Description of Type Design Change (continued):
2. The following Airplane Flight Manual Supplement(s) (AFMS), or later FAA approved revisions must be carried on the airplane when the following kits are installed:
A. The following AFMS are required when SMR kits SMR9068-21 or SMR9068-23 is installed with noncontinuous timer option: 13-33-018, Rev. IR, dated April 30, 2014.
B. The following AFMS are required when SMR kits SMR9068-20 or SMR9068-22 is installed with continuous timer option: 13-33-108, Rev. IR, dated April 30, 2014.
C. The following AFMS are required when SMR kits SMR9068-30 or SMR9068-31 is installed with Electrothermal De-ice System for 3 Blade Propeller: 13-33-109, Rev. IR, dated April 30, 2014.
D. The following AFMS are required when SMR kits SMR9068-40 or SMR9068-41 is installed with Heated Windshield Panel System: 13-33-106, Rev. IR, dated April 30, 2014.
E. The following AFMS are required when SMR kit SMR9068-50 is installed with Ice Viewing Light System:
13-33-107, Rev. IR, dated April 30, 2014.
3. The following Instructions for Continued Airworthiness (ICA), or later revisions, are required for this modification:
A. When kit SMR9068-20 or SMR9068-21 or SMR9068-22 or SMR9068-23 is installed: 13-33-097, Rev. 1, dated February 12, 2014;
B. When kit SMR9068-30 or SMR9068-31 is installed: 13-33-098, Rev. 1, dated February 12, 2014;
C. When kit SMR9068-40 or SMR9068-41 is installed: 13-33-099, Rev. 1, dated February 12, 2014;
D. When kit SMR9068-50 is installed: 13-33-100, Rev. 1, dated February 12, 2014;
Certification Basis:
Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for the Beechcraft Bonanza Series aircraft is as follows:
a. The type certification basis for parts not changed or not affected by the change is shown on TCDS 3A15.
b. The modification certification basis for parts changed or affected by the change since the reference application date, January 18, 2013, is based upon CAR 3 as amended to CAR 3-8 and part 23 as amended by Amendment 23-62 as follows:
Regulations at the latest amendment 23-00 through 23-62
23.21, 23.29, 23.31, 23.301, 23.303, 23.305, 23.561, 23.601, 23.603, 23.605, 23.609, 23.773(a), 23.775(e)(g),
23.1301, 23.1306, 23.1309 (a) (c) (d), 23.1351 (a), 23.1357 (a) (b) (c) (d), 23.1365 (a) (b) (d) (e) (f), 23.1367, (See Certification Basis continued on Page 4 of 4) SA09838AC
FAA Form 8110-2 (5/14) Page 4 of
4 SA09838AC Date Reissued: March 19, 2019
Regulations at the latest amendment 23-00 through 23-62
23.1416 (b) (c), 23.1438 (b), 23.1501 (a) (b), 23.1525, 23.1529, 23.1555 (a), 23.1581 (a) (b) (c) (d),
23.1583 (h) (m), 23.1585 (j)
Regulations at CAR 3-8
3.83, 3.85, 3.106, 3.114, 3.117, 3.118, 3.120, 3.122, 3.159, 3.311, 3.712
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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 · 5
Every issue · 3
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| March 19, 2019 | Reissued, current | Certificate |
| May 20, 2014 | Reissued, earlier issue | Certificate |
| May 16, 2014 | Issued, earlier issue | Certificate |