U.S. Department of Transportation
Federal Aviation Administration
FEDERAL AVIATION ADMINISTRATION - PARTS MANUFACTURER APPROVAL
PMA No.: _P..:.
Q_38_8_6C_E_ _ _ __
Supplement No.: 13 Rev. 3
Date: ~--~----------December 10, 2012
Aerospace Sealants LLC
4 Plum Ct.
Sleepy Hollow, II 60118
Art icle Name
Sealant
Approved
Replacement For
Part Number Part Number
AS I 06
GE 106,
RTV 106
Approval Basis and
Approved Design Data
Test and Computations per
14 CFR 21.303
Report No:
Aerospace Sealants
Product Analysis Report:
PARI06
Rev: A
Date: 12/18/06 or a later
FAA-approved revi sion
and
Report No:
Flammability and Analytical
Test Report:
FTARI06
Rev: A
Date: 12/24/07 or a later
FAA-approved revision
1/14
Make Eligibility
CFM International,
SA
Model Eligibility
CFM56-2, CFM56-2A,
CFM56-2B, CFM56-3,
CFM56-3B, CFM56-3C,
CFM56-5, CFM56-5-Al/F,
CFM56-5A3, CFM56-5A4,
CFM56-5A4/F,
CFM56-5A5,
CFM56-5A5/F
CFM56-5BI,
CFM56-5Bl/3,
CFM56-5B21P,
CFM56-5B4/3,
CFM56-5B3/2P,
CFM56-5B4/Pl,
CFM56-5B51P,
CFM56-5B7,
CFM56-5B7/3,
CFM56-5C2,
CFM56-5C2/G,
CFM56-5C3/F4,
CFM56-5C4,
CFM56-5B liP,
CFM56-5B2/3,
CFM56-5B2/2P,
CFM56-5B4/3Bl,
CFM56-5B3/2PI ,
CFM56-5B4/2P,
CFM56-5B6,
CFM56-5B7/P,
CFM56-5B8/3,
CFM56-5C2/4,
CFM56-5C2/G4,
CFM56-5C3/G,
CFM56-5C4/P,
CFM56-5B l/2P,
CFM56-5B3/3,
CFM56-5B3/P,
CFM56-585/3,
CFM56-584,
CFM56-5B4/2P I,
CFM56-5B6/P
CFM56-5B8/P,
CFM56-5B9/3,
CFM56-5C2/F,
CFM56-5C2/P,
CFM56-5C3/G4,
CFM56-5C4/l,
FEDERAL AVIATION ADMINISTRATION-PARTS MANUFACTURER APPROVAL
PMA No.: _P~Q-38_8_6_C_
E _ _ _ __
Supplement No.: 13 Rev. 3
Date: ~-~~~~----December 10, 2012
Aerospace Sealants LLC
4 Plum Ct.
Sleepy Hollow, II 60118
Article Name
Sealant
Approved
Replacement For
Part Number Part Number
ASI06
GE 106,
RTV 106
Approval Basis and
Approved Design Data
Test and Computations per
14 CFR 21.303
Report No:
Aerospace Sealants
Product Analysis Report:
PARI06
Rev: A
Date: 12/ 18/06 or a later
FAA-approved revision
and
Reoort No:
Flammability and Analytical
Test Report:
FTARI06
Rev: A
Date: 12/24/07 or a later
FAA-approved revision
2114
Make Eligibility
Model Eligibility
CFM International,
SA
CFM56-5B2,
CFM56-583/3BI,
CFM56-5B3/P I,
CFM56-586/3,
CFM56-5B4/P,
CFM56-585,
CFM56-5B6nP,
CFM56-5B9/P,
CFM56-589/2P,
CFM56-5C2/F4,
CFM56-5C3/F,
CFM56-5C3/P,
CFM56-5C4/ I P,
CFM56-7B20,
CFM56-7B22,
CFM56-7822/3,
CFM56-7824,
CFM56-7B24/3,
CFM56-7B26,
CFM56-7826/3B I,
CFM56-7B27,
CFM56-7B27/3,
CFM56-7827/B I,
CFM56-7B27/3B I,
CFM56-7B27/3B IF,
CFM56-7820/3,
CFM56-7B20n,
CFM56-7822/2,
CFM56-7B22/3BI ,
CFM56-7824/2,
CFM56-7B24/3B I,
CFM56-7B26n,
CFM56-7B26/382F,
CFM56-7827 A,
CFM56-7827/3 F,
CFM56-7B27/B3,
CFM56-7827/3 83,
CFM56-7B22/B I,
CFM56-7824/B I,
CFM56-7B26/3,
CFM56-7B26/B I,
CFM56-7B26/3F,
CFM56-7826/B2,
CFM56-7B26/3B2,
CFM56-7B27/2,
CFM56-7B27A/3,
CFM56-7B27EIF
CFM56-5C2,
CFM56-5C2/G,
CFM56-5C3/F4
FEDERAL AVIATION ADMINISTRATION-PARTS MANUFACTURER APPROVAL
PMA No.: _P~
Q_
38_8_6C
_E_ _ _ __
Supplement No.: 13 Rev. 3
Date: ~------~------December 10,2012
Aerospace Sealants LLC
4 Plwn Ct.
Sleepy Hollow, II 60118
Article Name
Sealant
Same as above
Approved
Replacement For
Part Number Part Number
Approval Basis and
Approved Design Data
ASI06
GE 106,
RTV 106
Test and Computations per
14 CFR 21.303
Report No:
Aerospace Sealants
Product Analysis Report:
PAR106
Rev: A
Date: 12118/06 or a later
FAA-approved revision
and
Report No:
Flammability and Analytical
Test Report:
FfARI06
Rev: A
Date: 12/24/07 or a later
FAA-approved revision
Same as above
Same as above
Same as above
3/14
Make Eligibility
Boeing
Bombardier Inc
Model Eligibility
727 Series, 727-100 Series,
727C Series,
727-IOOC Series,
727-200 Series,
727-200F Series,
737-100 Series,
737-200 Series,
737-200C Series,
737-300 Series,
737-400 Series,
737-500 Series,
737-600 Series,
737-700 Series,
737-800 Series,
737-900 Series,
737-900ER Series,
747-lOO Series,
747-2008 Series,
747-200F Series,
747-200C Series,
747SR Series,
747SP Series,
747-1 008 Series,
747-300 Series,
747-1008 SUD Series,
747-400 Series,
747-400D Series,
747-400F Series,
757-200 Series,
757-200PF Series.
757-200CB Series,
757-300 Series,
767-200 Series,
767-300 Series,
767-300F Series,
767-400ER Series,
777-200 Series,
777-300 Series,
777-300ER Series,
777-200LR Series,
777F Series
BD-100-IAIO,
BD-700-IA IO,
BD-700-IAI1,
CL-215-6A I 0,
CL-21 5-6811 (CL-215T
Variant),
CL-2 15-68 11 (CL-415
Variant),
CL-600-1-A I l (CL-600),
CL-600-2A12 (CL-60l-3A
Variant),
CL-600-28 16 (CL-600-3R
FEDERAL AVIATION ADMINISTRATION - PARTS MANUFACTURER APPROVAL
PMA No.:
Supplement No.:
Date:
Aerospace Sealants LLC
4 Plwn Ct.
Sleepy Hollow, 11 60118
Article Name
Sealant
Same as above
Approved
Replacement For
Part Number Part Number
Approval Basis and
Approved Design Data
AS I06
GE 106,
RTV 106
Test and Computations per
14 CFR 21.303
Report No:
Aerospace Sealants
Product Analysis Report:
PARI06
Rev: A
Date: 12/18/06 or a later
FAA-approved revision
and
Report No:
Flammability and Analytical
Test Report:
FTAR I06
Rev: A
Date: 12/24/07 or a later
FAA-approved revision
Same as above
Same as above
Same as above
4/14
Make Eligibility
Bombardier Inc
Pratt & Whitney
..;.P..;:,
Q;;..
38.;..;8;..;.
6..;.
C;;;.
E _ _ _ __
13 Rev. 3
~-~~~~---
D ecember 10,2012
Model Eligibility
Variant),
CL-600-2B I6 (CL-604
Variant),
CL-600-28 19 (Regional Jet
Series 100 & 440),
CL-600-2CJO (Regional Jet
Series 700, 70 1 & 702),
CL-600-2DI5 (Regional Jet
Series 705),
CL-600-2024 (Regional Jet
Series 900),
DHC-8-100 Series,
DHC-8-200 Series,
DHC-8-300 Series,
DHC-8-400 Series
JTI5D-I , JTI5D-I A,
JTI5D-1B, JT15D-4,
JTI5D-4B, JT15D-4C,
JT I5D-4D, JT15D-5,
JTI5D-5A, JTI5D-5B,
JT15D-5C, JTI5D-5F,
JT15D-5R, JT15D-5D,
PT6A-6, PT6A-6A,
PT6A-6B, PT6A-6/C20,
PT6A-ll, PT6A- IIAG,
PT6A-15AG, PT6A-20,
PT6A-20A, PT6A-20B,
PT6A-25, PT6A-25A,
PT6A-25C, PT6A-27, PT6A28, PT6A-29,
PT6A-34, PT6A-34B, PT6A34AG, PT6A-35,
PT6A-36, PT6A-38,
PT6A-40, PT6A-4 1,
PT6A-41AG, PT6A-42,
PT6A-42A, PT6A-45,
PT6A-45A, PT6A-45B,
PT6A-45R, PT6A-50,
PT6A-60, PT6A-60A, PT6A60AG, PT6A-61 ,
PT6A-6 1A, PT6A-65B,
PT6A-65R, PT6A-65AR,
PT6A-65AG, PT6A-110,
PT6A-1 12, PT6A-1 14,
PT6A- 11 4A, PT6A-1 14A,
PT6A-116, PT6A-121 ,
PT6A-135, PT6A-135A,
PT6A-52, PT6A-66,
PT6A-66A, PT6A-67,
PT6A-67A, PT6A-67AF,
PT6A-67P, PT6A-67B,
FEDERAL AVIATION ADMINISTRATION - PARTS MANUFACTURER APPROVAL
PMA No.: _
P~
Q_
38_8_
6C
_E
_ _ _ __
Supplement No. : 13 Rev. 3
Date: December 10,2012
Aerospace Sealants LLC
4 Plum Ct.
Sleepy Hollow, Il 601 18
Article Name
Sealant
-------------------
Approved
Replacement For
Part Number Part Number
AS 106
GE 106,
RTV 106
Approval Basis and
Approved Design Data
Test and Computations per
14 CFR 21.303
Report No:
Aerospace Sealants
Product Analysis Report:
PAR106
Rev: A
Date: 12/18/06 or a later
FAA-approved revision
and
Report No:
Flammability and Analytical
Test Report:
FTARI06
Rev: A
Date: 12/24/07 or a later
FAA-approved revision
5/ 14
Make Eligibility
Pratt & Whitney
Model Eligibility
PT6A-67D, PT6A-64,
PT6A-66B, PT6A-68,
PT6A-67AG, PT6A-67T,
PT6A-66D, PT6A-67F,
PT6B-36, PT6B-36A, PT6B36B, PT6B-37,
PT6B-37A,
PT6C-67D, PT6C-67C,
PT6T-3, PT6T-3A,
PT6T-3B, PT6T-3BG,
PT6T-3BE, PT6T-6,
PT6T-3D, PT6T-9,
PT6T-3DE, PT6T-3DF,
PT6T-3BF,
PW118, PWI18A,
PW1 18B, PWI19B,
PWII9C, PW120,
PW120A, PW121 ,
PW I21A, PW123,
PWI23AF, PW I23B,
PW123C, PWI23D,
PWI23E, PW124B,
PWI25B, PW126A,
PW127, PW127E,
PW127F, PW127G,
PW127M, PW150A,
PW206A, PW206B,
PW206B2, PW206C,
PW206E, PW207C,
PW207D, PW207D1 ,
PW207D2,
PW305, PW305A,
PW305B, PW306A,
PW306B, PW306C,
PW307A, PW308A,
PW308C, PW530A,
PW535A, PW535B,
PW545A, PW545B,
PW545C, PW610F-A,
PW617F-E, PW6 15F-A,
PW2037,PW2037M,
PW2040, PW2043,
PW2240, PW2 143,
PW2643, PW2040D,
PW2337, PW2037D,
Fl17-PW-100,
JFTD12A-4A,
JFTDI2A-5A, JT8D-208,
JT8D-2 17, JT8D-21 7A,
JT8D-217C, JT8D-219,
JT9D-3A, JT9D-7,
JT9D-7H, JT9D-7 A,
JT9D-7AH, JT9D-7F,
JT9D-20, JT9D-7J,
FEDERAL AVIATION ADMINISTRATION-PARTS MANUFACTURER APPROVAL
PMA No.:
Supplement No.:
Date:
Aerospace Sealants LLC
4 Plum Ct.
Sleepy Hollow, 11 60118
Article Name
Approved
Replacement For
Pa rt Number Part Number
Approval Basis and
Approved Design Data
Make Eligibility
Pratt & Whitney
ASI06
GE 106,
RTV 106
Test and Computations per
14 CFR 21.303
Report No:
Aerospace Sealants
Product Analysis Report:
PAR106
Rev: A
Date: 12/ 18/06 or a later
FAA-approved revision
and
Report No:
Flammability and Analytical
Test Report:
FfAR106
Rev: A
Date: 12/24/07 or a later
FAA-approved revision
Same as above
Same as above
Same as above
Same as above
McDonnell Douglas
Same as above
Same as above
Same as above
Same as above
Cessna
Sealant
6/ 14
_
P~
Q3
;....8...;.
8.;...
6C
;_E;___ _ __
13 Rev. 3
December 10,2012
~--~~~~-----
Model E ligibility
JT9D-20J, JT9D-59A,
JT9D-7Q3, JT9D-7R4E,
JT9D-7R4H I, JT9D-70A.,
JT9D-7R4D, JT9D-7R4El ,
JT9D-7R4E4, JT9D-7Q,
JT9D-7R4DI ,
JT9D-7R4G2,
PW4050, PW4052,
PW4056, PW4060,
PW4060A, PW4060C,
PW4062, PW4062A,
PW4152, PW4156,
PW4156A, PW4158,
PW4 160, PW4460,
PW4462, PW4650,
PW4074, PW4077,
PW4077D, PW4084,
PW4084D, PW4090,
PW4090-3, PW4074D,
PW4090D, PW4098,
PW4164, PW4168,
PW4 168A, PW4164C,
PW4164C/B, PW4170,
PW4168A-ID,
PW4168- ID, PW4164-ID,
PW4164C-ID,
PW4 164C/B-ID,
PW6122A, PW6124A
DC-8-11, DC-8-12,
DC-S-21, DC-8-31 ,
DC-S-32, DC-S-33,
DC-S-41 , DC-S-42,
DC-S-43, DC-S-51 ,
DC-S-52, DC-S-53,
DC-SF-54, DC-SF-55,
DC-S-55, DC-S-61 ,
DC-S-61F, DC-S-62,
DC-8-62F, DC-8-63,
DC-8-63F, DC-S-71,
DC-S-71F, DC-S-72,
DC-S-72F, DC-S-73,
DC-S-73F,
MD- 11 , MD-11F
120, 140, 140A, 150, 150A.,
1508, 150C, 1500, 150E,
150F, 150G, 150H, 150J,
1501<., Al50K, ISOL,
Al50L, 150M, Al50M,
152, AI 52, 170, 170A, 1708,
172, 172A, 1728,
172C, 1720, 172E, 172F,
1720, 172H, 170B, 1721,
FEDERAL AVIATION ADMINISTRATION-PARTS MANUFACTURER APPROVAL
PMA No.:
Supplement No.:
Date:
Aerospace Sealants LLC
4 Plum Ct.
Sleepy Hollow, Il 60118
Article Name
Sealant
Approved
Replacement For
Part Number Part Number
AS I 06
OE I 06,
RTV 106
Approval Basis and
Approved Design Data
Test and Computations per
14 CFR 21.303
Report No:
Aerospace Sealants
Product Analysis Report:
PAR106
Rev: A
Date: 12/18/06 or a later
FAA-approved revision
and
Report No:
Flammability and Analytical
Test Report:
FTARI06
Rev: A
Date: I 2/24/07 or a later
FAA-approved revision
7/ 14
Make Eligibility
Cessna
..;..P~Q.;..;38;..;;.8..;..6C
;;.;;E;;.....__ _ __
_I_
3 _R_
e_v ._3_ _ _ _ __
December 10, 2012
Model Eligibility
172K, 172L, 172M, 172N,
172P, 172Q, 172R, 1728,
177, 177A, 1778, 180,
180A, 1808, 180C, 1800,
180E, 180F, 1800, 180H,
1801, 180K, 182, 182A,
1828, 182C, 1820, 182E,
182F, 1820, 182H, 182J,
1828, 182T, 182K, 182L,
182M, J82N, 182P, 182Q,
182R, R182, T182, TR182.
TI82T, 185, 185A, 1858,
185C, 185D, 185E, Al85E,
Al85F, 188, 188A, 1888,
A188, AI88A, Al888,
TI88C, 190, 195, 195A,
1958,
206, P206, P206A, P2068,
P206C, P206D, P206E,
U206, U206A, 206H,
U2068, U206C, U206D,
U206E, U206F, U2060,
TP206A, TP2068, TP206C,
T206H, TP206D, TP206E,
TU206A,TU2068, TU206C,
TU206D, TU206E, TU206F,
TU2060, T207, T207 A,
208, 2088, 210,210A,
2 108, 210C, 2100, 210E,
2IOF, T2IOF, 2100,
T2100, 210H, T210H,
2101, T210J, 210K, T210K,
210L, T210L, 210M,
T210M, 210N, P210N,
T210N, 210R, P210R,
T2 10R, 210-5, 210-5A,
3 10, 310A, 310B, 310C,
3 10D,310E, 310F, 3100,
310H, E310H, 3101, 310J,
310J-1, E310J, 3IOK, 310L,
310N,310P, T310P, 310Q,
T310Q, T3 10Q, 310R,
T31 OR., 320, 320-1 , 320A,
3208, 320C, 3200, 320E,
320F, 335, 340, 340A, 32 1,
326, 337, 337A, 3378,
M337B, 337C, T337C,
3370, T337D, 337E,
T337E, 337F, T337F, 337G,
T3370, 337H, P337H,
T337H, T337H-SP, 401,
401A, 401B, 402, 402A,
4028, 402C, 411, 41IA,
414, 414A, 421, 42IA, 4218,
FEDERAL AVIATION ADMINISTRATION - PARTS MANUFACTURER APPROVAL
PMA No.: ..;...
P..;:,.
Q3;;...;8;..;;.8..;_
6C;;..;;E;;.....__ _ __
Supplement No.: _1_3_R_e_v._3_ _ _ _ __
Date: December 10,2012
Aerospace Sealants LLC
4 Plum Ct.
Sleepy Hollow, ll 6011 8
Article Name
Sealant
Same as above
Approved
Replacement For
Part Number Part Number
Approval Basis and
Approved Design Data
ASI06
GE 106,
RTV 106
Test and Computations per
14 CFR 21.303
Report No:
Aerospace Sealants
Product Analys is Report:
PAR I06
Rev: A
Date: 12/ 18/06 or a later
FAA-approved revision
and
Report No:
Flammability and Analytical
Test Report:
FTARI06
Rev: A
Date: 12/24/07 or a later
FAA-approved revision
Same as above
Same as above
Same as above
Make Eligibility
Cessna
Rolls-Royce Corp
Model Eligibility
421C, 425, 441,
500, S550, 560,550, 552,
560XL, 501, 551 , 510, 525,
525A, 5258, 650, 680, 750,
F150F, F150G, F150H,
F150J, FI50K, F150L,
F150M, Fl52, FA150K,
FA150L, FAI50M, FAI52,
FRA 150L, FRA 150M,
F172D, F172E, FI72F,
FI72G, F172H, F I72L,
F172M, F172N, Fl72P,
FI77RG, FI82P, FI82Q,
FR182, F337E, FT337E,
F337F, FT337F, F337G,
FT337GP, F337H,
FT337HP, FR172E,
FRI72F, FR172G,
FR172H, FR172J,
FR172K,
LC40-550FG,
LC42-550FG,
LC41-550FG,
175, 1758, Pl72D, R172E,
R172F, Rl72G, RI72H,
Rl72J, 172RG, 175A,
175C, Rl72K, T-50,
T303
250-C l O, 250-ClOB,
250-ClOD, 250-C18,
250-C 18A, 250-C18B,
250-C18C, 250-CI9,
250-C20, 250-C20B,
250-C20C, 250-C20F,
250-C20J, 250-C20S,
225-ClO, 225-C10A,
250-C20R, 250-C20R/1 ,
250-C20R/2, 250-C20R/4,
250-C20W, 250-CJOO/AI ,
250-C300/B I,
250-B I5A, 250-BISE,
250-815G, 250-817,
250-8178, 250-B 17C,
250-817D, 250-B17E,
250-8 17F, 250-B 17F/ I,
250-8 17F/2,
250-C28, 250-C288,
250-C28C, 250-C30,
250-CJOG, 250-CJOG/2,
250-C30M, 250-C30P,
250-C30R, 250-C30R/I ,
250-C30S, 250-C30U,
250-C40B, 250-C47B,
8/ 14
FEDERAL AVIATION ADMINISTRATION-PARTS MANUFACTURER APPROVAL
PMA No.: _P~Q,_
38
_8_6_
C_
E _ _ _ __
Supplement No.: _I_
3 _R_e_v._3_ _ _ _ __
Date: December 10, 2012
Aerospace Sealants LLC
4 Plum Ct.
Sleepy Hollow, II 60118
Article Name
Sealant
Approved
Replacement For
Part Number Part Number
AS I 06
GE I 06,
RTV 106
Approval Basis and
Approved Design Data
Test and Computations per
14 CFR 21.303
Report No:
Aerospace Sealants
Product Analysis Report:
PARl06
Rev: A
Date: 12/ 18/06 or a later
FAA-approved revision
and
Report No:
Flammability and Analytical
Test Report:
FTARI06
Rev: A
Date: 12/24/07 or a later
FAA-approved revision
9/ 14
Make Eligibility
Rolls-Royce Corp
Model Eligibility
250-C47M, 250-C30R/3,
250-C30R/3M,
501-Dl3, 50l-Dl3A,
50l-Dl3D, 50l-DI3E,
501-Dl3H, 501-022,
501-D22A, 501-D22C,
50 1-D22G, AE I I 07C,
AE 2100A, AE2100C,
AE 21 OOD2, AE 21 OOD2A,
AE 210003, AE 21001,
AE2100P,
AE 3007C, AE 3007 A,
AE 3007AI/1 ,
AE 3007AI/2, AE 3007Al ,
AE 3007Al/3,
AE 3007AlP, AE 3007A3,
AE 3007CI , AE 3007AIE,
BR700-710Al-IO,
BR700-710A2-20,
BR700-7 10C4-ll,
BR700-725Al-12,
BR700-715A 1-30,
BR700-715Bl-30,
BR700-715Cl-30,
DART 511 , 514, 511-7E,
514-7,
DART 525, 528-7E,
528D-7E, 529-7£,
529D-7E, 529-7H,
529D-7H, 529-SE,
529D-8E, 529-SH,
529D-8H, 529-SX,
529D-8X, 529-SY,
528D-8Y, 529-SZ,
529D-8Z,
531 , 532-7, 532-2L, 532-7L,
532-7N, 532-7P, 532-7R,
535-2, 5357R, 551-7,
551-7R, 552-2, 552-7,
552-7R,
TAY 611-8, TAY 620-15,
TAY 651-54, TAY 650-15,
TAY 611-8C,
RB2 11-22B-02,
RB211-22B (MOD 72-8700),
RB211-22C-02,
RB211-524B-02,
RB211-524B-B-02,
RB211-524B2-19,
RB2ll-524B-B-19,
RB211-524B3-02,
RB211-524B4-02,
RB21 I ·52484-D-02,
RB211-524C2-19,
FEDERAL AVIATION ADMINISTRATION-PARTS MANUFACTURER APPROVAL
PMA No.:
Supplement No.:
Date:
Aerospace Sealants LLC
4 Plum Ct.
Sleepy Hollow, ll 60118
Article Name
Sealant
Approved
Replacement For
Part Number Part Number
AS I 06
GE I 06,
RTV 106
Approval Basis and
Approved Design Data
Test and Computations per
14 CFR 21.303
Report No:
Aerospace Sealants
Product Analysis Report:
PARI06
Rev: A
Date: 12/ 18/06 or a later
FAA-approved revision
and
Report No:
Flammability and Analytical
Test Report:
FTAR106
Rev: A
Date: 12/24/07 or a later
FAA-approved revision
10/ 14
Make Eligibility
Rolls-Royce Corp
.;.P..;:Q:;;.3.;;..88;;.;6;..;;C.;;;E_ _ _ __
13 Rev. 3
-------------------December 10, 2012
Model Eligibility
RB211-524C2-8-19,
RB211-524D4-19,
RB211-524D4-39,
RB211-524D4-8-19,
RB211-524D4X-19,
RB211-524D4-8-19,
RB211-535C-37,
RB211-535E4-37,
RB211-535E4-8-37,
RB211-535E4-8-75,
RB211-535E4-C-37,
RB211-524G2-19,
RB211-524G3-19,
RB211-524H-36,
RB211-524H2-19,
RB211-524G2-T-19,
RB211-524G3-T-19,
RB211-524H-T-36,
RB211-524H2-T-19,
RB21 I-TRENT 892-17,
RB211-TRENT 884-17,
RB211-TRENT 8928-1 7,
RB211-TRENT 895-1 7,
RB211-TRENT 875-17,
RB211-TRENT 8848-1 7,
RB211-TRENT 877-1 7,
RB211-TRENT 970-84,
RB211-TRENT 9708-84,
RB211-TRENT972-84,
RB211-TRENT 9728-84,
RB211-TRENT 977-84,
RB21 1-TRENT 9778-84,
RB211-TRENT 980-84,
RB211-TRENT 553-61 ,
RB211 -TRENT 556B-61 ,
RB211-TRENT 556-61 ,
RB211-TRENT 560-61 ,
RB211-TRENT 553A2-61
RB211-TRENT 556A2-61 ,
RB211-TRENT 55682-61 ,
RB211-TRENT 560A2-61 ,
RB211-TRENT 768-60,
RB21 I-TRENT 772-60,
RB211-TRENT 7728-60,
Trent I 000-A,
Trent I 000-C,
Trent 1000-D,
Trent 1000-E,
Trent I OOOG,
Trent I 000-H
FEDERAL AVIATION ADMINISTRATION- PARTS MANUFACTURER APPROVAL
PMA No.: _P...,.
Q_
38_8_
6C_E_ _ _ __
Supplement No.: 13 Rev. 3
Date: December 10,2012
Aerospace Sealants LLC
4 Plum Ct.
Sleepy Hollow, ll 6011 8
Article Name
Sealant
-------------------
Approved
Replacement For
Part Number Part Number
AS I 06
GE 106,
RTV 106
Approval Basis and
Approved Design Data
Test and Computations per
14 CFR 21.303
Report No:
Aerospace Sealants
Product Analysis Report:
PARI06
Rev: A
Date: 12/18/06 or a later
FAA-approved revision
and
Report No:
Flammability and Analytical
Test Report:
FTARI06
Rev: A
Date: 12/24/07 or a later
FAA-approved revision
11/ 14
Make Eligibility
General Electric
Company
Model Eligibility
CF34-IA, CF34-3A,
CF34-AI, CF34-3A2,
CF34-3B, CF34-3B I,
CF34-8C I, CF34-8C5,
CF34-8C5AI , CF34-8C5BI ,
CF34-8C5A2, CF34-8C5A3,
CF34-8E2, CF34-8E2AI,
CF34-8E5, CF34-8E5A I,
CF34-8E5A2, CF34-8E6,
CF34-8E6Al,
CF34-I OAI6, CF34-IOA18,
CF34- 10E2Al, CF34-10E5,
CF34- IOE5A I, CF34- I OE6,
CF34- 1OE6A t ,CF34- I OE7,
CF34-1 OE7-B,
CF6-6D, CF6-50C, CF6-50E,
CF6-6DI, CF6-50CA,
CF6-50El, CF6-6DIA,
CF6-50CI, CF6-50E2,
CF6-50C2, CF6-50E2B,
CF6-6K, CF6-50C2B,
CF6-6K2, CF6-50C2D,
CF6-45A, CF6-45A2,
CF6-50A,
CF6-80A, CF6-80C2B I,
CF6-80C2B IF I, CF6-80A I,
CF6-80C2B2,
CF6-80C2DI F, CF6-80A2,
CF6-80C2B4,
CF6-80C2A5F, CF6-80A3,
CF8-80C2B6,
CF6-80C2B7F,
CF6-80C2A I,
CF6-80C2BIF,
CF6-80C2BIF2,
CF6-80C2A2,
CF6-80C2B2F,
CF6-80C2B6FA,
CF6-80C2A3,
CF6-80C2B3F,
CF6-80C2B5F,
CF6-80C2A5,
CF6-80C2B4F,
CF6-80C2B8F,
CF6-80C2A8,
CF6-80C2B6F,
CF6-80C21 Ll F,
CF6-80C2K1F,
CF6-80E1Al , CF6-80EIA4,
CF6-80E I A4/B,
CF6-80E I A2, CF6-80E I A3,
CT58, I 00-2, CT58- I 10- 1,
CT58-110-2, CT58-140- I,
CT58-140-2,
FEDERAL AVIATION ADMINISTRATION-PARTS MANUFACTURER APPROVAL
PMA No.: _P_,.Q3_8_86_C_E_ _ _ __
Supplement No.: 13 Rev. 3
Date: December 10,2012
Aerospace Sealants LLC
4 Plum Ct.
Sleepy Hollow, 11 60118
Article Name
Sealant
Same as above
--------------------
Approved
Replacement For
Part Number Part Number
Approval Basis and
Approved Design Data
Make Eligibility
Model Eligibility
AS 106
GE 106,
RTV 106
Test and Computations per
14 CFR 21.303
Report No:
Aerospace Sealants
Product Analysis Report:
PAR106
Rev: A
Date: 12/18/06 or a later
FAA-approved revision
and
Report No:
Flammability and Analytical
Test Report:
FTARI06
Rev: A
Date: 12/24/07 or a later
FAA-approved revision
General Electric
Company
CT64-820-4,
GE90-76B, GE90-90B,
GE90-113B, GE90-77B,
GE90-94B, GE90-115B,
GE90-85B, GE90-II OBI
Same as above
Same as above
Same as above
Honeywell
International Inc.
TPE331-25A,
TPE33 I-25AA,
TPF331-25AB,
TPE331-25B,
TPE33 l-25C,
TPF331-25D,
TPE331-25DA,
TPE331-25DB,
TPF331-25E,
TPE33l-25F,
TPE331-25FA,
TPF331-29A,
TPE331-43,
TPE33 1-43-A,
TPE331-43-B,
TPF331-45, TPE331-47,
TPE331-47-A,
TPF331-47-B,
TPE331-51 , TPE331-55,
TPF33 1-55-A,
TPE331-55-B,
TPE331-57,
TPF331-57-B,
TPE331-61 ,
TPE331-61-A,
TPE331-I, TPE331-IU,
TPF331-IUA,
TPE331-2, TPE331-2U,
TPF331-2UA,
TPE331-3, TPE331-3U,
TPF331-3UW,
TPE331-3W,
TPE331-5, TPE331-5A,
TPF331-5AB, TPE331-5B,
TPE331-5U,
TPE331-6, TPE331-6A,
12/ 14
FEDERAL AVIATION ADMINISTRATION-PARTS MANUFACTURER APPROVAL
PMANo.: PQ3886CE
Supplement No.: 13 Rev. 3
Date: December 10,2012
Aerospace Sealants LLC
4 Plum Ct.
Sleepy Hollow, II 60118
Article Name
Sealant
Same as above
Approved
Replacement For
Part Number Part Number
Approval Basis and
Approved Design Data
Make Eligibility
AS106
GE 106,
RTV 106
Test and Computations per
14 CFR21.303
Report No:
Aerospace Sealants
Product Analysis Report:
PAR106
Rev: A
Date: 12/ 18/06 or a later
FAA-approved revision
and
Report No:
Flammability and Analytical
Test Report:
FTAR106
Rev: A
Date: 12/24/07 or a later
FAA-approved revision
Honeywell
International Inc.
Same as above
Same as above
Same as above
Embraer
-----------------------------------End of Listing------------------------------
13/ 14
Model Eligibility
TPF331-6U,
TPE331-8, TPE331-8A,
TPE331-9, TPE331-9U,
TPF331-1 0, TPE331-l OA,
TPE331-10AV,
TPE331-10B, TPE331-10G,
TPF331-10GP,
TPE331-10GR,
TPE331-10GT,
TPF331-IOJ, TPE331-10N,
TPE331-10P, TPF331-10R,
TPE331-10T, TPE331-IOU,
TPF331-10UA,
TPE331-l OUF,
TPE331-1 OUG,
TPF331-1 OUGR,
TPE331-IOUJ,
TPE331-1 OUK,
TPF331-10UR,
TPE331-l1U,
TPE331-11UA,
TPF331-12, TPE331-12B,
TPE331-12JR,
TPF331-12UA,
TPE331-12UAR,
TPE331-12UER,
TPF331-12UHR,
TPE331-3U,
TPF331-14A, TPE331-14B,
TPE331-14F,
TPF331-14GR,
TPE331-14HR,
TPE331-15AW
EMB-135BJ,
EMB-145,
EMB-145ER,
EMB-145MR,
EMB-145LR,
EMB-145XR,
EMB-145MP,
EMB-145EP
760 Springfield Dr.
Roselle, Illinois 60172
AS106 Rev. IR 12-21-06
▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬
AS106
Product Description:
AS106 is a high strength, fast curing, acetoxy
silicone RTV adhesive rubber developed for
applications requiring fast development of physical
properties and excellent adhesion.
AS106 is a 1 part high temperature silicone that
when applied to the substrate allows handling of
the bonded assembly within minutes. AS106
works well in manual and automatic dispensing
equipment.
Product Features:
•
•
•
Fast Room Temperature Cure
Thixotropic paste
Excellent unprimed adhesion to metal and
glass
Curing:
Cure speed can be accelerated with increased
humidity to very rapid cures exhibiting fast
adhesion. Typical utilization involves dispensing in
open air and ambient humidity to result in a
durable adhesive rubber.
Replacement For:
GE 106 and Dow DC736. Tested and conforms to
requirements of MIL-A-46106 Type I Group III
material.
Packaging:
Available in standard 3 oz. tubes and 10.3 oz.
cartridges. Other size packaging available upon
request.
Shelf-life:
Sealed containers 1 year from date of shipment
when stored in a cool dry area below 70°F
High Strength
Fast Cure
Adhesive Sealant
Typical Properties:
UNCURED
Color:
Red
Viscosity, cps
500,000
Specific Gravity
1.08
Consistency
Thixotropic paste
Working time, mins. @ R.T.
4
Tack Free Time, mins. @ R.T. 12
Application Rate, 90 PSI, g/min. 250
Solids
98%
CURED – ROOM TEMPATURE
Cured – 72 hrs. @ R.T.
Tensile Strength, PSI
450
Elongation, %
600
Durometer, Shore A
32
Peel Strength, PPI
25
Tear Strength, PLI
40
Electrical
Dielectric Strength, v/mil
>500
Dielectric Constant
2.7
Dissipation Factor
0.001
Volume Resistivity, ohm/cm
1.1 x 1015
Thermal
Brittle Point, °F (°C)
-76 (-60)
Maximum Continuous
Operating Temperature, °F (°C) 500(260)
Thermal Conductivity
Btu/hr/ft2, °F/ft
0.11
Coefficient of Expansion
in/in/°F
15 x 10-5
This document contains propriety information and is not to be transmitted, reproduced or disclosed to anyone without written
permission of Aerospace Sealants
▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬▬
Voice: (630) 980-2174
FAX: (630) 980-2080
A erospace
S ealants
Application Instruction Sheet
for
AS106
Clean surface and dry thoroughly. If using the optional “Tube Nozzle”, cut to desired bead
size. Push sealant ahead by squeezing tube for uniform bead. The paste-like consistency
makes it easy to be tooled using a spatula or wooden paddle. Tooling time, approximately 5
minutes at Room Temperature. TACK FREE approximately 20 minutes at Room
Temperature. Normal Room Temperature cure time is 24 hours. Length of time for a full
cure depends on thickness of application and other factors including temperature and
humidity. Accelerated cure may be achieved using hot air. Thin bond line sections can be
heat accelerated cured using a1 minute hot air stream exposure. Test the exposure time on
a sample prior to final application.
Primerless adhesion too many metals including aluminum, stainless steel, steel, glass,
ceramics and many rigid plastics. Not for use on stovepipes, fireplaces or underwater. Not
for use in delicate electric or electronic applications. For industrial use only. KEEP OF
REACH OF CHILDREN.
FAA PMA Approved Products
Approved Eligibility for ALL Pratt & Whitney, Rolls Royce, Canadair, Boeing, GE Engines,
CFM Engines, Bombardier, McDonnell, Douglas/Boeing, Honeywell, and Cessna
when used per the Airworthiness Approvals for these Models
A erospace
S ealants
MATERIAL SAFETY DATA SHEET (MSDS)
PRODUCT:
AS106 High Strength, Fast Cure Silicone Adhesive Sealant
1. Chemical Product and Company Identification
Manufactured By:
Emergency Phone:
Silicone Solutions (SS-109Red REF.)
1670-C Enterprise Parkway
Twinsburg, Ohio 44087
330-405-4595
Revised:
Preparer:
Chemical Family:
Formula:
10-12-97
David M. Brassard
Silicone Rubber
Mixture
2. Composition / Information on Ingredients
Product Composition
CAS Reg. No.
Approx. %
Wt.
A. HAZARDOUS
NONE FOUND
B. NON HAZARDOUS
Polydimethylsiloxane
70131-67-8
Dimethylpolysiloxane
63148-62-9
Silica
68611-44-9
Methyltriacetoxysilane
4253-34-3
Trade Secret Component
Trade Secret Component
Dibutyltindilaurate
Red Iron Oxide
1332-37-2
ACGIH
TWA
TLV
STEL
OSHA
TWA
PEL
STEL
Units
45-60
--
NE
--
NE
NA
15-50
NE
NE
NE
NE
NA
10-19
10
10
10
15
mg/m3
3.0-12.0
10
NE
10
NE
ppm
2-8
1-5
0.1-3.0
2.0-5.0
NE
NE
NE
NE
NE
NE
NE
NE
NE
NE
NE
NE
NE
NE
NE
NE
NA
NA
NA
NA
3. HAZARDS IDENTIFICATION
Potential Health Effects:
Ingestion: ------------------------------------------------------------------ MAY BE HARMFUL IF SWALLOWED
Skin Contact: -------------------------------------------------------------- UNCURED PRODUCT WILL IRRITATE LIPS, GUMS AND
TONGUE.
UNCURED PRODUCT MAY IRRITATE THE SKIN.
Inhalation: ------------------------------------------------------------------ CAUSES IRRITATION TO THE MOUTH, NOSE AND
THROAT.
THIS APPLIES IN THE UNCURED STATE ONLY.
Eye Contact: --------------------------------------------------------------- UNCURED PRODUCT CONTACT IRRITATES EYES.
Medical Conditions Aggravated: --------------------------------------- NONE KNOWN
Subchronic (TARGET ORGAN) Effects: ----------------------------- NONE KNOWN
Chronic Effects/Carcinogenity: ---------------------------------------- THIS PRODUCT OR ONE OF IT’S INGREDIENTS
PRESENT 0.1% or MORE IS NOT LISTED OR
SUSPECTED AS A CARCINOGEN BY NTP, IARC OR
OSHA
Principle Routes of Exposure: ------------------------------------------- NONE KNOWN
Other:
ACETIC ACID RELEASED DURING CURE.
This product contains methylpolysiloxanes which can
generate formaldehyde upon exposure above 300 degrees
Centigrade in atmospheres which contain oxygen.
Formaldehyde is a skin, eye, and throat irritant.
A erospace
S ealants
4. FIRST AID MEASURES
Ingestion: ------------------------------------------------------------------ RINSE MOUTH WITH WATER SEVERAL TIMES
Skin: ----------------------------------------------------------------------- REMOVE COMPLETELY WITH A DRY CLOTH OR
PAPERTOWEL.
WASH WITH SOAP AND WATER.
Inhalation: ---------------------------------------------------------------- MOVE PERSON TO FRESH AIR.
In case of eye contact: -------------------------------------------------- FLUSH WITH WATER FOR 15 MINUTES AND GET
MEDICAL ATTENTION IF IRRITATION PERSISTS.
Note to physician: ------------------------------------------------------- NONE KNOWN
5. FIREFIGHTING MEASURES
Flash point: --------------------------------------------------------------Method: -----------------------------------------------------------------Ignition temp. -----------------------------------------------------------Flammable limits in air - lower % -----------------------------------Flammable limits in air - upper % -----------------------------------Sensitivity to mechanical impact: ------------------------------------Sensitivity to static discharge: ----------------------------------------Extinguishing media: --------------------------------------------------Special firefighting procedures: ---------------------------------------
>300ºC or 600ºF
NA
Unknown
NA
NA
NO
NO
ALL STANDARD FIREFIGHTING MEDIA
NONE KNOWN
6. ACCIDENTAL RELEASE MEASURES
Action to be taken if material is released or spilled: ---------------- SCRAPE-UP and PLACE IN AN INERT
MATERIAL FOR DISPOSAL
7. HANDLING and STORAGE
Precautions to be taken during handling and storage: --------------
CURE ONLY WHERE APPROPRIATE
VENTILATION SYSTEMS EXIST.
8. EXPOSURE CONTROLS / PERSONAL PROTECTION
Engineering controls: ---------------------------------------------------Respiratory protection: -------------------------------------------------Protective gloves: -------------------------------------------------------Eye and face protection: ------------------------------------------------Other protective equipment: -------------------------------------------Ventilation: ----------------------------------------------------------------
NONE KNOWN
NONE REQUIRED
CLOTH GLOVES
SAFETY GLASSES
NONE REQUIRED
CURE IN WELL VENTILATED AREAS
9. PHYSICAL and CHEMICAL PROPERTIES
Boiling point: ------------------------------------------------------------Vapor pressure: ----------------------------------------------------------Vapor density: -----------------------------------------------------------Freezing point: -----------------------------------------------------------Melting point: ------------------------------------------------------------Physical state: ------------------------------------------------------------Odor: ----------------------------------------------------------------------% Volatile by volume: --------------------------------------------------Evaporation rate: --------------------------------------------------------Specific gravity: ---------------------------------------------------------Density: (Kg/M3) ------------------------------------------------------Acid/alkalinity -----------------------------------------------------------PH: -------------------------------------------------------------------------VOC: ----------------------------------------------------------------------Solubility in water: ------------------------------------------------------Solubility in organic solvents: -------------------------------------------
NA
NA
NA
NA
NA
PASTE
VINEGAR
<3
<1
1.14
1140
SLIGHTLY ACIDIC
NA
NT
INSOLUBLE
PARTIALLY SOLUBLE IN TOLUENE
A erospace
S ealants
10. STABILITY and REACTIVITY
Stability: ------------------------------------------------------------------- STABLE
Hazardous polymerization: --------------------------------------------- WILL NOT OCCUR
Hazardous thermal decomposition/combustion products: ---------- CARBON DIOXIDE, CARBON MONOXIDE
SILICON DIOXIDE, FORMALDEHYDE, ACETIC ACID
Conditions to avoid: ----------------------------------------------------- NONE KNOWN
11. TOXICOLOGICAL INFORMATION
Product Information:
Acute Oral LD50: --------------------------------------------------------- UNKNOWN
Acute Dermal LD50: ----------------------------------------------------- UNKNOWN
Acute Inhalation LC50: -------------------------------------------------- UNKNOWN
Ames Test: ----------------------------------------------------------------- UNKNOWN
12. ECOLOGICAL INFORMATION
Ecotoxicological Information: ------------------------------------------ UNKNOWN
Chemical Fate Information: --------------------------------------------- UNKNOWN
13. DISPOSAL CONSIDERATIONS
Disposal Method: -------------------------------------------------------- DISPOSAL SHOULD BE MADE IN ACCORDANCE WITH
FEDERAL, STATE, AND LOCAL CONSIDERATIONS
14. TRANSPORT INFORMATION
DOT Shipping Name: --------------------------------------------------DOT Hazard Class: ----------------------------------------------------DOT Label: -------------------------------------------------------------UN/NA Label: ----------------------------------------------------------Placards: -----------------------------------------------------------------IATA: --------------------------------------------------------------------IMO IMDG-code: ------------------------------------------------------European Class:
RID ( OCTI ): ---------------------------------------------ADR ( ECE ): ---------------------------------------------RAR ( IATA ): ---------------------------------------------
NA
NOT DOT REGULATED
NA
NA
None
NA
NA
NA
NA
NA
15. REGULATORY INFORMATION
SARA Section 302: ---------------------------------------------------SARA ( 311, 312 ) Hazard Class: ------------------------------------SARA ( 313 ) Chemicals: ---------------------------------------------CPSC Classification: ---------------------------------------------------WHMIS Hazard Class: -------------------------------------------------Export Schdle B/HTSUS -----------------------------------------------ECCN:
Hazard Rating Systems
HMIS: -------------------------------------------------------NFPA: -------------------------------------------------------California Proposition 65: ------------------------------------------------
NONE FOUND
NONE
NONE
NA
NONE
3910.00 Silicones in primary form.
EAR99
HEALTH 1, FLAMMABILITY 0, REACTIVITY 0
HEALTH 1, FLAMMABILITY 0, REACTIVITY 0
NONE
16. OTHER
This product or its components are on the European inventory (EINECS) of existing commercial chemicals. This data is offered in
good faith as typical values and not as a product specification. No warranty, either expressed or implied, is made. The recommended
handling procedures are believed to be generally applicable. However, each user should review these recommendations in the
specific content of the intended use.
PMA CROSS REFERENCE CHART
FAA PMA Sealant Cross Reference Chart
PMA Part Number
Class
PRC/PPG Product
PMA No. / Supplement No.
NSL870
B1/2, B2, B4
P/S 870
PQ3886CE/ 28
NSL890RC
A1/2, A2, B1/2, B2, B4
P/S 890
PQ3886CE/ 28
NSL1422
A1/2, A2, B1/2, B2
PR-1422
PQ3886CE/ 18
NSL1422RC
A1/2, A2, B1/2, B2
PR-1422
PQ3886CE/ 28
NSL1428
B1/2, B2
PR-1428
PQ3886CE/ 18
NSL1440RC
A1/2, A2, B1/2, B2
PR-1440
PQ3886CE/ 28
NSL1750
B1/2, B2
PR-1750
PQ3886CE/ 18
NSL1776M
B1/2, B2
PR-1776M
PQ3886CE/ 28
FAA PMA Silicone Cross Reference Chart
PMA Part Number
GE-Momentive / Dow Corning Product
PMA No. / Supplement No.
AS106
GE106, Dow Corning 736
PQ3886CE/ 13
AS112
GE112
PQ3886CE/ 3
AS116
GE116
PQ3886CE/ 3
AS118
GE118
PQ3886CE/ 3
AS157
GE157, Dow Corning 732
PQ3886CE/ 3
AS159
GE159, GE106, Dow Corning 736
PQ3886CE/ 3
AS3145 & AS3145P
GE162, Dow Corning 3145
PQ3886CE/ 3
(800) 527.0011
www.nslaerospace.com