STC SA00332BO

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SA00332BO SMR Acquisition LLC dba SMR Technologies, Inc.

93 Nettie Fenwick Rd.

Fenwick, WV 26202 Federal Aviation Regulations.

1. Installation of non-hazard ice protection system kits SMR9065-11, SMR9065-12, SMR9065-14, SMR9065-15, SMR9065-16, SMR9065-17, SMR9065-24, SMR9065-25, SMR9065-30, SMR9065-31, SMR9065-40, SMR9065-60, SMR9065-61, SMR9065-62, SMR9065-63, SMR9065-64, SMR9065-65, SMR9065-66, SMR9065-67, SMR9065-68, SMR9065-69, SMR9065-70, SMR9065-71, SMR9065-72, SMR9065-80, SMR9065-81, SMR9065-82, SMR9065-83, SMR9065-84, SMR9065-85, and SMR9065-86, in accordance with Installation Instructions as listed on MDL-0065, Revision H, dated September 12, 2014, or later FAA approved revisions.

(See Description of Type Design Change continued on Page 3 of 3)

1. 14 Volt System aircraft must upgrade to a National AirParts Inc. P/N P312RN, 120 Amp Alternator. This can be installed via its PMA, but a separate logbook entry must be made if this alternator is installed.

2. 14 Volt System PA-32R-301 and PA-32R-301T aircraft must have an Oildyne hydraulic pump, Piper P/N 481-879, installed.

Prestolite hydraulic pumps must be replaced with Oildyne hydraulic pumps using Piper kit P/N 764-785. A separate logbook entry must be made if the Oildyne pump is installed, as it is not part of this STC.

3. Flight into known icing prohibited with this STC.

(See Limitations and Conditions continued on Page 3 of 3) Anthony E. Gallo Manager New York ACO Branch Piper Aircraft Corporation PA-32R-301T, PA-32R-301 (HP), PA-32R-301 (SP), PA-32-301, PA-32-301T, PA-32-301FT, PA-32-301XTC March 19, 2019 October 28, 2014 March 9, 2012 June 18, 2013 A3SO 4

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

4 SA00332BO

FAA Form 8110-2 (5/14) Page 3 of

4 Date Reissued: March 19, 2019

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 SMR9065-11, SMR9065-12, SMR9065-61, SMR9065-63, SMR9065-64, or SMR9065-65, are installed: 12-33-126, Rev. IR, dated June 18, 2013; 13-33-067, Rev. IR, dated June 18, 2013; 12-33-123, Rev. IR, dated June 18, 2013; 12-33-124, Rev. IR, dated June 18, 2013.

b. The following AFMS are required when SMR kit SMR9065-60, SMR9065-62, SMR9065-66, SMR9065-67, SMR9065-68, or SMR9065-69, are installed: 12-33-126, Rev. IR, dated June 18, 2013; 12-33-125, Rev. IR, dated June 18, 2013; 12-33-123, Rev. IR, dated June 18, 2013; 12-33-124, Rev. IR, dated June 18, 2013.

c. The following AFMS are required when SMR kits SMR9065-14, SMR9065-15, SMR9065-70, SMR9065-71 or SMR9065-72 are installed: 12-33-126, Rev. IR, dated June 18, 2013.

d. The following AFMS are required when SMR kits SMR9065-16, SMR9065-40, SMR9065-81, SMR9065-83 or SMR9065-84, are installed: 13-33-067, Rev. IR, dated June 18, 2013.

e. The following AFMS are required when SMR kit SMR9065-17, SMR9065-80, SMR9065-82, SMR9065-85, or SMR9065-86, are installed: 12-33-125, Rev. IR, dated June 18, 2013.

f. The following AFMS are required when kits SMR9065-30 or SMR9065-31 is installed: 12-33-123, Rev. IR.

dated June 18, 2013.

g. The following AFMS are required when kits SMR9065-24 or SMR9065-25 is installed: 12-33-124, Rev. IR.

dated June 18, 2013.

3. The following Maintenance Instructions for Continued Airworthiness (ICA), or later FAA accepted revisions, are required for this modification:

a. When kit SMR9065-11, SMR9065-12, SMR9065-60, SMR9065-61, SMR9065-62, SMR9065-63, SMR9065-64, SMR9065-65, SMR9065-66, SMR9065-67, SMR9065-68 or SMR9065-69 is installed:

12-33-129, Rev. 7, dated June 4, 2014; 12-33-119, Rev. 5, dated February 28, 2014; 12-33-128, Rev. 4, dated October 30, 2013; 12-33-117, Rev. 5 dated October 30, 2013.

b. When kit SMR9065-14, SMR9065-15, SMR9065-70, SMR9065-71 or SMR9065-72 is installed: 12-33-129, Rev. 7, dated June 4, 2014.

c. When kit SMR9065-16, SMR9065-17, SMR9065-40, SMR9065-80, SMR9065-81, SMR9065-82, SMR9065-83, SMR9065-84, SMR9065-85 or SMR9065-86 is installed: 12-33-119, Rev. 5, dated February 28, 2014.

d. When kit SMR9065-24 or SMR9065-25 is installed: 12-33-128, Rev. 4, dated October 30, 2013.

e. When kit SMR9065-30 or SMR9065-31 is installed: 12-33-117, Rev. 5, dated October 30, 2013.

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 this certificate to alter a product, the holder must give the other person written evidence of that permission.

SA00332BO

FAA Form 8110-2 (5/14) Page 4 of

4 SA00332BO Date Reissued: March 19, 2019

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 this modification to the Piper PA-32 is as follows:

a. The type certification basis for the Piper PA-32 as shown on the TCDS A3SO for parts not changed or not affected by the change.

b. The modification certification basis for parts changed or affected by the change since the reference application date, March 9, 2012, is based upon CAR 3 as amended to CAR 3-8 and part 23 as amended by Amendment 23-62 as follows:

Regulation at the latest amendment 23-00 through 23-62

23.21, 23.23, 23.25, 23.29, 23.31, 23.201, 23.203, 23.207, 23.605, 23.1301, 23.1309 (a) (c) (d), 23.1351 (a),

23.1357 (a) (b) (c) (d), 23.1365 (a) (b) (d) (e) (f), 23.1367, 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).

Regulation at CAR 3-8

3.83, 3.85, 3.106, 3.114, 3.117, 3.118, 3.159, 3.171, 3.172, 3.173, 3.291, 3.292, 3.311, 3.712 ----------END----------