NSL Aerospace - NSL1422 Airline PMA Approval Packet

Transcription

NSL1422
NSL1422 Class A & B
Aircraft Integral Fuel Tank Sealant
PMA Approval Packet
Contents:
FAA PMA Supplement: Page 2
Class A TDS: Page 32
Class B TDS: Page 33
Class A MSDS: Page 34
Class B MSDS: Page 38
PMA Cross Reference Chart: Page 42
(800) 527.0011
www.nslaerospace.com
This document contains proprietary information and is not to be transmitted, reproduced or disclosed to anyone without written permission of NSL Aerospace.
US . Department of Transportat ion
Federal Aviation Administration
- PARTS MANUFACTURER APPROVAL
PMA No.: "-P""Q;:.;
38:.,::6CE
8:::."'=--_ _ __
8.:..R.:...:.;
Supplement No.: .:.,1.:.
"v ...,:I-,-_ _ _ __
Date: May 1,20 12
Aerospace Sealants LLC
4 Plum Ct.
Sleepy Holl ow, II 60 11 8
Ar ticle Nam e
Scalant
Approved
Replacement Fo r
Pa rt Number Part Numhcr
NSI.1422-A 1/2 PRC -OcSOIO Sealant
I'R-1422-A II2,
PR- 1440 A II2,
ProSea l 890
A ppr()\,'a l Bas is and
Approved Design Data
Make Eligibility
I est and "'"Imputations per
14 CFR 21.303
CFM International,
SA
Product Analvsis Report:
PARJ 204
R v' A
!hi!!;;. 05/04/07 or a later
FM -:.lpprovcd revis ion
1/5 1
Model Eligibi.lity
CFM56-2. CFM56-2A,
CFM56-2D. CFM56-3.
CFM56-JIl, CFM56-3l',
C FMS6-S. C FMS6-S-A Ifr.
C FMS6-5A3. CFM56-SA4,
CFM56-SA4/F,
CFM56-SA5.
CFMS6-5AStr.
CFM56-5BI,
CFM56-5B 1/3 .
Cf M5(,-5132!P,
CFMSG-SB4/3 ,
CFM56-5BJ/2P.
CFM56-5B41P I,
CFM56-5B51P,
CFM56-5B7,
CFM56-5B7/3,
CFMS6-5C2.
CFM56-5 ::lit;,
CFM56-5 C3/F4,
CFM56-5 C4.
CFM56-5BI /P.
CFM56-5B2/3,
FMS6-5B2/2P.
CFM56-5B4/3 B I,
CFM56-5LlJ/2PI,
CFM56-5B4/2P,
C FMS<>-SIJ6,
CFM56-5B71P,
CFM56-5BRIJ.
CFM56-5C2/4.
CFM56-5 C2/(i4,
C FM56-5CJ /(i.
C FM56-5 C4/P,
CFM56-SB 1/21',
CFM56-5B3 /J ,
CFMS6-5B31P.
CFMsr.-5I3SIJ ,
CFM56-5B4,
CFM56-5B4/2PI ,
CFM56-SB6IP
CFM56-SfWP.
CFM56-SI39/J.
CFM56-5 C2/F.
CFM56-5C21P.
Cl M,6-5C.l/(i4,
FEDERAL AVIATION
~DMINISTRATION
- PARTS MANUFACTURER APPROVAL
PMANo.:
Supplement No.:
Date:
Aerospace Sealants LLC 4 Plum Ct. Sleepy Hollow, II 60)18 Article Name
Approved
Repl.cement for
Part Number Part Nun,lwr
Approval Oasis and
Approved ncsign Dat.
i est and Computations per
14 cm 21 3 03
SL 1422-/\ 112
Product
PruS':i..Jt 890
Anal ~ s h
PQ3886CE
IS Rev. I
May 1.2012
Make Eligibility
Model Eligibili ty
FM Inh:nHltiunal,
F M56-5 4/ 1.
CFM56-5B2,
SA
C FM56-5U3/3B I,
C FM56-503/P I.
CFM 56-506/3.
CFM56-5B4/P,
CFM56-5U5,
C FM56-5B6/2P.
C FM56-5B91P,
CFM56 -5139/21'.
CI'M56-5C21F4.
CF M56-5 C3/F,
CFM;6-5 JIP,
CfM56-5C411 P,
CFM56-7B20,
CFM56-7822,
C FM56-7131213.
(:FM56-7I124,
CFM56-71l1 413.
C FM56-7lJ26,
CFM56-71.l26/3B I.
CFM56-7B27,
CFM56-7B27/3,
CF M56-7B27/BI,
CFM50-7B27/3 B [,
CI'M56-7B2m llll ',
CFM56-7020/1,
CFM56-7lJ20/2.
Cf M56-7B22l2.
C FM56-7B22/3B I,
CFM56-7B24/2,
CFM56-7 B2413 B I,
CFM56 -7Il26. _.
C FM56-71126!Jfl2F.
CfM5 6-7lt27/\.
CF M56- 7B27 P
C FM56·1D2 7ffi J.
Ct' M56-7B27/JfJ3.
CFM56-7132 2/B 1,
CFM56-7B24!B I,
CFM56-7lJ26;1.
CFM56-71126!111.
C FM56-71l26!31',
RCQQrt:
PAR32 04
~A
DrHb 05104/07 or (t Inter
FAA-appro\lt.:d revi sion
CI ~ M56-7n2(lm2,
CFM56-7lJ16i JIJ2.
C FM56-7lll7!2,
C FM56·7ll27A13,
CfM56·7B27E!F
('I'M56·5C2.
C FM56-5C2IO,
CI' M56-5C3/F4.
Sealant
Same as above
Same as ahove
Snme us ahove
Boeing 727 Serles. 727-100 Series,
727C Series,
2/5 )
FEDERAL AVIATION ADMINISTRATION - PARTS MANUFACTU RER APPROVAL PMA No.:
Supplement No.:
Date:
4 Plum ('I.
Sleepy Hollow, II 60118
.:..P""Q.:,
38"'8:.:;6.:;C,;;;E_ _ _ __
.,:.1.:,8.:..R=c.:..v.,,:I:-:-:_ _ _ __
May 1,2012
Approved
Replacement For
Article Name
SeahUH
Part Number Part Number
NSL I422·'\ 112
PRe-DeSoto Sealant
PR-1422-AI /2.
PR-1440 A 1/ 2,
P",S",1890
Approval Ras is a nd
Te~ 1
aml C Olnputnlil)l1S per
Make Eligibility
Boeing
Model Eligibility
727-IOOC~ cri est
727-200 Series,
727-2001' Series.
737-100 S(.'ries,
737-200 Ser ies,
n7-200C Series,
7.17-3UO Series,
737-4UO Series.
737-500 Series.
737-600 Se ri es.
737-700 Serles.
737-800 Series.
737-900 Series.
737-9001iR Series,
747-100 Series,
14 C FR 21.303
Product Anol\ sis Report:
PAJU204
~A
Pate: 05 /04107 or n later
FA.A. -approved revision
747-2008 Series,
747-200F Sl.::rie",s.
7 <I 7-200e Series,
747SR Series,
747SP Seri es,
747- 1(0 1) Series.
747-300 ries,
747-1008 S UD Series.
747-400 Series,
747-4000 Series.
7.:t7-400r Series,
757-2UO Serk's,
757-2UOPF Seric.s.
757-200C8 Series.
757-300 Series,
7!l7-200 Scril.!s,
767-300 Series,
767-3001' Seri...
767-400ER Series.
777-200 ::)eries,
777-300 Series,
777-300ER Series.
777-200LR Scri!;.':),
777F Series
Si..'alant
Sam ~
as above
Same ; IS above
Sam\.' a... aho ve
Bombardier Inc
nU-IOO-IAIO. BO-700-1 A IO. I\O-700- IA II , ('1 .-215-6/\ I0, CI.-2 I 5-0fl I I (CL-2 IST Variant). CL-2 I5-(,13 II (CL-l 15 Varian t). ('L-600- I-A I I «('1.-600), C L-60U-2A 12 (CL-60 1-3A V8 ri~III) ,
CL-60tI-2B I6 (CL-600-3R
Va riant),
CL-600-2B 16 (CL-604
3/5 1
FEDERAL A VIAnON ADM INISTRA no
PARTS MAN FACTURER APPROVAL
PMA No,: .:..P.:;;Q;;,;
J8~8.::;6C:::.;
' E~'_ _ _ __
Supplement No.: ..:,1::.8,::R:::ev,:,:,,.:I_ _ _ _ __
Date: May 1,2012
4 Plum Ct.
Article Name
Seal ant
Approved
Replacement For
Part Number Part umbe r
NSLl422-,\ 1/2
PRe -De oto Sealant
PR-I 'I22-A 112,
PR-1440 AI I2,
ProSew 890
Approval Basis and
Approved I)esign Data
Tcst and omputations per
14 erR 21.303
Producl Analysis Report'
PARJ204
R ' \" A
Qlal;; 05104/07 or a lalcr
Make Eligibility
Bomhilnlicr Tne
FAA-approv..::d revi sion
Model Eligibility
Variant),
CL-600-2B 19 (Regiooal
Series 100 & 440),
CL-600-2CI0 (Regional
Series 700. 70 I & 702),
CL-600-20 15 (Regional
Seri.;s 705).
CI.-600-21>24 (Regiooal
Sl:rj~ s
leI
leI
leI
leI
lJOO).
01 IC-R-I 00 Series,
OJ I( '-8<WO Series,
01 1(,-8-31l0 Senes,
01 IC-8-400 Series
:Sculanl
Same as above
Same a~ nhove
SatHe as aho\'c
Pmll & WhiIO<Y
1'1'I SO-1. lT150-1 A,
JT150-1 D, lTISO-4 ,
JTI5D-41l, lTI5D-4c'
lTI5D-40, JTI51J-5,
1 1'1 SO-SA, JTISD-SI1.
HI5D-SC, HI5D-5!"
):1'I5I)-5It HI5D-5D,
PT6/\-6, P niJ\-6J\.
P'1'6A-Gn, PTM-6/C20,
PT6A-II, I' 1'6A-I, lAG,
PT6A-I5AG, I'T6A-20.
P'1'M-20A. PTGA-20B,
PTM-25, P·IM-25A.
PT6A-25C PTM-27, PT6A
28, PT6A-29,
Pl(lA-3 ,1. I'T()A-J.JU. I'T6A ·
34M;, PTM -.15,
PT6J\-36, PT6J\-J8,
P10A-40, I'TOA-41,
PTM-41 AO. P 16A-42,
P'['()!\.· 12!\. PT'6 /\-4\
PTr..~ -4SA, P 1·(,,\-45R.
P I·M--I5K . 1'16A-50,
PT6A-I>II, 1"1 M-60A. PT6A
601\0, Hr.A-6I ,
PT6A-61 A, PTr.A-65B,
PT6A -65R, PT6A-65AR,
PT6A-65I\G, I'TM-II 0,
PTGA-112 , HGA-I 14,
PTr.!\-114A , PT6A -114A ,
PT6A-116, PT61\-121,
PT6A-135, I'T61\-135A,
PT6A-52, I'T6A-66,
PT6A-(,6!\. )'T6l\-67,
PT6A-671\ PTM-67I\F,
PT6A-671',I'T6 A-67B,
PT(IA-67D, PT6A-M.
P r61\-66 B, PT()/\-M~,
PTM-67I\G, PT6A-67T,
PTM-600, PT6A-67f,
4/5 1
FEDERAL A VIAnON ADMINISTRATION - PARTS MANUFACTURER APPROVAL
PMA No.: ..:.P",Q::,;
38:..;:8.;:.6C::,:E=' _ _ _ __
Supplement No.: .,.1.:.8..;,R;,;c,,;,v;"";,.1-:-:-_ _ _ __
Date: May 1,2012
4 Plum Cl.
Article Nam e
Sealant
Approved
Replacement For
Purt Number Part Number
NS LI 422·A II2
PRC-Oc Soto
~cala nl
PR-[422-A[/2,
I'R-[44U A[/2,
ProSc-u! R90
Appro"III, Basis and
Appro,'ed Design Data
l ese and omputal iu lls Pl:J'
14 CFR 2 [.303
Product AnalvsLo; Report"
I'AR3204
Rev: A
Date: 05 /04107 or a later
FAA-approved revision
Make Eligibilitv
Pratt & Whitney
Model Eligibility
PT611 -36. PT60-3M, PT6B
36B. PTGB-37,
PT6ll-37A,
PTGC-67D. PT6C-{i7C.
PT6"-3, PT6T-JA,
PT6T-3B. PT6T-3BG,
I'T6T-3lJ E, P 6T-6,
PT61'-3D. 1'1'61'-9,
PTtiT-3Dc .l'rr,T-JDF.
PT6T-3Br.
PWI ·18. PWI ·18A.
PWIIXll.I'WI19B.
PWI19C. PWI2 0,
I'WI20A,PWI21,
PWI21A PW123.
P\V 123M'. PW 1238,
PWI2JC, I'WI231l.
PWI23E, PWI24B.
I'W 125n. PW 126/\.
I'WI27,I'WI27L..
PW 1271', I'll' 127G,
PWI2701. PWI50!\.
PW206/\. PW2068,
PW2UuIl2.PW206('.
PW20ul ·:. I'W207C.
PW207D. rW2U7DI.
PW207D2,
I'W305. PW305/\.
PW30SB. PW 3U6A,
PW 30uR. I'W JU6t'.
PW307 .~, PWJORA,
PW.lORt;. PW5JOA.
PW5J5A. I'W5358.
PWS'IS/\, PW545R.
PW.l,!OC. PW(, [[11-'-/\,
PW617F- P-, rW615F-A.
['W2037.I'W2OJ7M.
PW10otO. PW:?,O-H.
PW22 . W, PW2143,
PW2(,4 3, rW2040D, PW2337, PW2037D, F117-PW-100. JFTD 12A-4A. JPTD 12A-5A, JTSD-208, JTRD-2 17. JTSD-2 ·17A. JTSD-217C, JT8U-219, JT9J>- 3A. JT9D- 7. J'I9D-711. JT9IJ-7A, JT9D-7!\1I, JT9D-7F. JT9U-20, JT9D-7.1, JT~J)-2I)J, JT9D-5~A,
J19D-7Q3, JT91)-7R4E.
JT9D-7R41 J [, JT9D-70A.
JT9D-7R4D, n~U-7R4EI.
5/5 1
FEDERAL AVIATION ADM IN ISTRATl
- PARTS MAN1JFACTURER APPROVAL
PMA No.: ..:.,P~
Q~38;:,;;8;;;,6C:;"E:;,,
' ~~~~_
Supplement No.: 18 Rev. 1
~.;..;,.;-,~---
Date: May 1,2012
4 Plwn Ct.
Sleepy Hollow, 1I 601 18
Approved
Replacement For
Part Number
PRC·D o to cilIum
PR·1422 -A I:2,
PR- I4-l UA I!2,
ProSl.!u1890
Approval Oasis and
Approved Desig n Dahl
Test and .ompuilltions per
Milke Eligibilitv
Prall & Whitney
14 CFR 21.3U3
Product Anol y~ is Renor!:
PAR3204
JT9D-7R4Ci2.
PW4050, PW4 052,
~I\
PW4056, PW406(),
l2ill£; 05104/07 or • I•• cr
PW40611A. PW-IU60C,
PW4062, PW4U62A.
P1I'4152,I'W4156.
P1I'41561\. PW41 53,
PW4 160, PW4460,
PW..J462, PW4650,
1'\\'4074. PW4077. PW4077/l. PW40K4, PW408'IO, PW4090, PW-I U9U-3 , PW40ND, PW409UD. PW4 mS, PW4164. I'W4168. PW4H,S,\. PIV41(>4C. PW4IMClB, PW4170. PW416M-ID. PW416K-I D.I'W4164-ID, P II' 4'ir>K-I D. PW4 164 C'il3- 1D. PW61 22A. PW6124A
Sealant
Same us ahove
Sa111l' as IlbO\ c
Model Eligibility
JI'9D-7R4E4, l1'9D-7
JT9D-7IUDI.
Sallle as uho\'c
Airhus
A.100, Model 132- 1A,
A300. Modt"l 132-1 C.
A3UO. Model B4-2C.
A300. Model B2K-3 C'.
1\300. Model B4-IOJ,
A:lOO. 1 ~l dclI32-2OJ .
AJ 10. Moud 204. A3 1II. Model 221, A3 1U, Muuci 222, A310, Mouel 2U3, A3 10. Model 322. A310, Model 324, A310, Maud 3U4, AJ IU, M"dd 325. A300. Model 64-60 I, A3UO, Model 64-603. A3UU, Mudel B4-62U. 1\ 300, Model H4-605R.
A300. ModI.!! B-l-622K.
A3UO. Mou<1 F4-6115R,
AJon. Mouel 1'" 4-622R,
AJOll , Moud C4-60SR
V..trianl
r.
A)OO, ~10del 62-622,
!l318 Mudel -I II .
AJI8 i'v1odl,.·I-112.
1\ 3 18 M(ldd -1 2 1.
A3 ) 8 ~Iodcl - 122,
A3 19 Modd - III ,
615 1
FEDERAl , AVIATION ADMINISTRAnON - PARTS MANUFACTURER A PPROVAL
4 Plum Ct.
Article N.me
S~aJaIlt
PMA No.:
Supplement No.:
Date:
Approved
Replacement For
Pari Number Part Number
NS L1422·A 1/2
PRe · DeSoto Sealant
PR-1422 -A I/2.
PR-IHUAI / 2.
ProSe;]! R90
Sealant
NSL I422-AI /2
PRC-OeSot" Scalant
I'R-1422-A I _.
I'R-1440-A 112,
Pn-,Sca1890
Tesl an d Cumputati ons per
14 erR 21.303
Product AnalYSis Report:
PAR3204
Rev: A
,l;!mg; 05/04 /07 or a latcr
FAA-approved revi.sion
Tc:-l and Computations per
14 cm 21.303
Product Analvs is Repor(:
PAR3204
Make Eligibility
r11C -DeSoto Sealant
PR-1422-AI /2_
PR- .44U-A 112,
ProS..:al 890
T cs l and Computations per
14 (TR 21.303
Producll\nill y-r-is Report :
PAJU204
Rn 1\
JEte:. 05104j()7 or n Inter
i :
FAA-arpro vcd n.:.. . i.':iion
7/51
Model Eligibility
Airbus
A319 Model-I 12,
A319Modcl-113,
A319 Model-I 14.
A319 Model-II),
A319Modd -131 ,
A3 19 Model -132 ,
1\3 19 MoJel- 133.
A32U MoJol-lll ,
/\320 M(ldl::! -21 1,
A320 ModeJ, -232,
A320 Model -233,
A321 Modd -III.
A321 Model-I 12.
A321 M"del-131 ,
A32 1 Model-211 ,
A321 Model-212,
A321 Model -213,
A321 Model -232 ,
1\330-20 I. A330-2U2.
A33U-2U3, A33U-223.
A3.1o.243. A.1.10-3U3.
A330-302, A3.1 0-321 ,
A330-322. A330-323 ,
A330-341, A330-342.
A3311-343 ,
A3411-211 , -212, -213,
A340-311 , -312,-313,
1\340-541. ,\3411-642,
A38U-S41 , A38U-842.
'\3S0-S61
ATR
A1'R42-200, ,\'I'R42-300,
A1'R4 2-32U, ATR42-500,
A1'R72 -IOI. '\' IR72-201,
A 11<72-102, AT R 72-202,
ATR72-21I, ATR72-2 12,
'\1'R72-212A
Date:. 051O-l/U7 or [I iall.:r
F/\A-approq.:J n.:\'i.':iioll
NS1I422·A 112
18 Rev. I
May 1,2012
Approval Oasis otnd
Re v; A
SeJ lant
PQ3886CE
McDunndlOougJas
DC-R-II ,OC-8-1 2,
DC-X-21. OC-8-31 >
OC-8-32. D -8-33.
OC-S-41. OC-8-42,
OC-R-43 , DC -R-51,
OC-8-52,OC-S-53.
DC-81'-54, DC-SF-55,
DC-8-55, D(: -8-61 ,
OC- R-61 F, DC-8-62,
DC-8-62F, DC-8-6J,
DC-8-6JF, OC-8-7 1.
DC-S-71 F. DC-8-n,
DC-R-72F, OC-S -73,
OC-8-73F.
MD-II , MO-IIF
FEDERAL AVlATJON ADMINISTRATION - PARTS MA UFACTLJRER APPROVAL
PMA No.: -'-P-"Q..:;.3.;;..88;.;;6...:C.=E_ _ _ __
Supplement No.: 18 Rev. I
Date: 7M7a-)";':-1,"::2-::0710::-_- - - -
Aerospace SeaJants LLC
4 Plum Ct.
Approved
Replaccl1ICllt For
Article Name
Se;}lnnt
Port Number Part Number
N ~L I422-!\112
PRC·DeSolo Stnlunt
PR-1412-AI12,
PR-1440-AI/2,
ProS tal Xl)U
Approval Basis and
Approved I)esign Data
Test and l\\mpulations rer
14 ('I'R 21..l03
Produc;,l Anal vs is Report:
PAR.1204
Make Eligibility
Lockheed
Model Eligibility
L-1UII-385-1, L-IOII-385-1-14, L-IIIII-J~5-1-IS,
L-IOII-385-J
&:LA
'tle: 05/0-U07 or a later
FAA.uppro\·t!d n.:\·isioll
Sealant
NSL 1422-A2
PRC-DeSoto Sealant
TeSl anJ Computations per
PR-1421-A2.
14 eFR 2UIl]
PR-1440-A2,
Product Analysis Repllrt:
ProSe-nl RC)O.
P R 3204
ProSeal 8YUM
Rev: A
OatiJ : 05/04/U7 or a hlh:r
I:'AA-appro\'I..:d n:visi{l!1
CFM Intemationa),
SA
CFM56-2, C FMS6-2A_
C FMS6-2B, C FM56-3.
C'FMS6-J B, FM56-3C,
C FM 56-S. CFM56-5-A IiI',
C FMS6-SAJ, Cr M56-5A4,
C FM56-5A4IF.
(' 1.'M56-5A5 .
CFM56-5i\5/1',
CFM56-5fll.
CFM56-5llI/3,
CFMS6-Sll2/1',
C FM5(,-5fl4/.l.
C FM56-5fl312P.
C FM56-5B41P I,
C FM56-5135/1',
C FM56-51l7,
C FM56-5[l7/J .
C FM56-5C2.
c r 156-5 2/G.
C FM56-SC31F4.
C FM56-5 '4,
C FM56-5BIIP,
C FM56-SB2/3,
CrMS6-5B2/2P,
CF M56-5U4/3fll,
CFM 5(,-5llJ /2P I,
CrM56-5B4 /2P.
CFM56-5 J36.
(' FM56-507/P,
CFMS6-5B8/J ,
CFM56-5 2/4,
CFM56-5 C2/G4 ,
CFM56-SC3/G.
C FM56-5C4/ P,
C FM56-5131 /2P,
CFM56-5J33/3.
C FMS6-5IlJ /P,
C FM56-SBSIJ.
('!'M 56-SR·l ,
CFM56-5B4/2PI,
C FM56-SB6/P
C FMS6-5lJ~/ P ,
CF/V156-S11WJ.
C FM56-5 C21F,
8/S I
FEDERAL A VIATlON ADMINISTRATION
PARTS MANUFACTURER APPROVAL
PM 1\ No .: .;,.P.,::.Q.:,.:;,:8c;.CE
38 6.:.."--_ _ __
Supplement 0.: -,1.;..S_R...:e_v_. _1_ _ _ _ __
Date: May J, 2012
Aerospace SC<Tlants LLC
4 Pl um Ct.
Sleepy Hollow, II 60 118
Article Name
Sealant
Part
Appro\'ed
Replacement For
umber Part Number
NSLI422-A2
PRC- DeSoto Sealant
PR-' 422-A2.
I'R-14·lO-A2.
ProSl..'aJRI)(),
ProSe,,1R9UM
Approval Ba,is a nd
Approved Uesign I)ata
Test and Computations per
14 ("I'll 21.303
Product Anal> sis Report
P IU204
Jill';..J\
~
05104 /07 or " la,er
F A-approved revi sion
Milke Eligibilitv
CFM In,ema,ional,
SA
Model Eligibility
CfMS6-5C2/P.
CFM56-5C3IG4,
CFMS6-5C4/1.
C FM56-5B2.
C fM56-5lJ3/3BI.
CI'MS6-5J33/1' t ,
CFM56-5J36/3.
CFM56-5B41l'.
CFM56-Sfl5,
CFM,6-5R6/ 2P,
CFMS6-5lJ9!I',
CFM,6-SUW2P,
CF M56-5C21F4,
C FM,(,-5C3 / F,
C FM,6-5 .lIP,
CfMS6-, C4I1P,
CFM56- 7B20,
C FM56-71122,
C I'M56-7fl22/3,
Cl'M,6·7B24 ,
C FM,6-71324/J.
C FM56-7Il26,
CFM56-71326/3B I,
C FMS6-7B27,
CFM56-7B27f3.
CFM56-71127fU l,
CFM56-7B27f.J n I,
CFM56-7B27/3B IF,
CFMS6-7B20f.J,
CFMS6-7B20I2,
FM56-7B22/2,
CFM56-71122/311 1.
CFM56-7ll2412,
CF M56-71124/JB I,
CFM5/,-7Il2612.
C I' M56-7132 6!3 B2F.
CTM56-7B27A.
CFM,6-7R27/3F,
CFM56-71127/1l3,
CfM56-7T127/3BJ.
CFMS6-7U221U I,
CTM,6-7U24/lJ I,
CFM,6-71126i3,
CF\156-7R261n I,
CF\156-7U26/3 F,
CFM56-7B26/ B2.
CFM56-7B26/3B2.
CFM56-7Il2712,
CFMS6- 71117
CFM,6-7B27
CFM 56-5C2.
('FM56-SC2/G,
CFM56-5CJlf4.
9/5 1
FEDERAL AVIATION ADMIN ISTRATIO
- PARTS MAN UFACTURER APPROVAL
PMA No.: ..:.P,""Q~38:::8:::6;;;.CE:.:.·_ _ _ __
S uppJement No.: ..c1...:8_R_e_v_.__I_ _ _ _ __
Date: May 1,2012
4 Plum Ct.
Approved
Article Name
Sealant
Replacement For
Pari Number Part Number
Approval Basis and
NS L 1422-Al
Test and Compuul1ions per
14 U'R 21.303
PR e -DeSoto Sea lant
PR-14'1 2-J\2,
PR-144U-A2.
ProScal S90,
Prod.uct Anal vsis R~nOJ1~
ProScul X90\:1
1kLA
Make Eligibility
72 7 Series, 727-100 Series,
727C Series,
727-IOOC Series,
727-200 Series,
727-200F Series.
737- 100 Se ries,
737-200 Series,
737-200C Series,
737-300 Scrie-:-;,
737-400 Series,
737-50U Series,
737-600 Series,
737-700 Series.
737-S00 Scrlc~,
737-900 Series,
7J7-900ER Series.
747-100 Series.
747-2008 Series,
747-200F Series,
747-200C S.rie"
747SR Series.
747SP Series,
747-1001) Series,
747-300 Se,ks,
747-IOOB SUD Series.
747-400 Series.
747-400D Seri"",
747-400 F Series.
757-20U Series,
757-2001'F Series.
757-200C B Series,
757-300 Series,
767-200 Sene.,
767-100 unc"
7n7-100 F Scri e ~ ,
767-400 ER Series.
777-200 Series.
777-300 Series,
777-300 ER Series.
777-200LR Series,
7771-' Series
Bombardier Ine
BD-lOO-IAIO.
BD-700-IAIO,
BD-700-IAII,
("1.-215-M I O.
CL-215-6BII (eL-215T
Variant).
CI.-215-61111 (CL-415
Variant).
CL-600-I-AII «("L-600).
CI.-600-2AI2 (CI.-601-3A
V[)rinnt).
(1.-6UU-2B 16 (CL-600-3R
PAR3204
~
05/04/U7 or a later
F'AA-a rprovcd revision
Scahillt
Sarl,lC il5. aho\'c
S'Ull!..:
<J..::i
above
Same <J~ Uhovl:
10/51
Model Eligibility
BoeIng
FEDERAL. AVIATION ADMIN ISTRATION - PA RTS MAN FACTURER APPROVAL PMA No.: .:.P;;::Q::;.38::,:8::;6:::;C,:::E_ _ _ __
Supplement No,: .:.1.;;.S.:.R.;.:e.:.v'-'-I_ _ _ _ __
Date: May 1.2012
4 Plum Ct.
Sleepy Hollow, \I 60118
Appro,'ed
Replacement IF or
Article Name
Sealant
L1422-A2
cal.onl
Approval' Basis and
Appl'o-v cd Design Data
T t,."Sf. ilnd C<.l mpultltions
14
cm 2 UOJ
~Ana!v;>i&
ProScal X90,
I-'n!Seal XI)()'i\1
pCI'
Make Eligibilitv
Bo mbardier Inc
.!kD.2.!b
Model Eligibility
VarimH).
CL-600-2lJ I 6 (CL-604
Variant) , CL-oOO-2B 19 (Regional Jet Seri es 100 & 440),
CL-600-2C I 0 (Regi onal Jel
Seri es 700. 70 I & 7(2),
CL-60U-2D 15 (Regional Jet
PAR 3204
Rev : A
DaLe: 05/04/07 or 8 later
FA A-approved re,\ ision
Series 705),
CL-600-2D24 (Regional Jet
Scri.:., 900),
DJ IC-8-1 00 Series,
DJ rC-S-200 Series.
DJ IC' -X-~OO Scric"S,
DJ IC-8-400 Series
Same
;I .')
Jbove
l?raU& Whitney
Sam!..: as abo\ 1J
],]'151)·I.J1'150·1A,
H I51l- Ill , ,II I SI)-4.
HISD-4B, JTISD-4 C
JHSD-4D, JTIS D-S.
JTI 51l-5A. HI SD-SB,
,IT I'SI)-5 C, HI 51)-5 F,
JT ISO-SR. ,1TI5D-5D.
Pl6A·h. PT6A·6A,
PThA·6 B. PT6A·6/C20,
I'TOA- I L P1'6A- I l AG,
PT6;\- I SA G, PTOA -20,
PT6A~20A~ PT6A~20B,
PT6A~25 , PT6 A~25A.
PTGA-2S C, 1'161\-27, P1'6A
28. p'r6A~29.
P1M"34. P1'OA-34B, P1'6A
34AG, I'T 6A-3S. PTUA-36, PT6A-J8, pnA·'ll, PT6 A-4 I, PTOA-4 lA G, PT6A-42, PT6A-42A, PT6A-45, Pl(,i\-'15A, P r6A-'15B,
PT(,A-4SR. I'TM-5 0. P1UA-(,0. PT6 A-60A, PT6A
60AG. PT6;\-6 I, P I'6A-6 I A, PT6A-65lJ, PT6A~65R , PT()A-65AR,
PT6A-65 ,\ O. PT6 A~ [ 10.
PIM-I 12. P1'6A-l 14.
P1('I\-1 14A PTGA-I 14A
PT6i\~116, PT6A-121.
PTOA-J3S, PT6A- I35A,
PT()A-52 , r 6A-66,
P I'M-6M, PT6A-6 7,
P' f 6i\-67A P"J'()i\-67AF.
P-lflA-671,l, P-T6A-6711,
PT6i\-n7D, P1'M-64,
PT6A-66B. I'T6A-68,
11/5 j
I :ll..!~...!:.All!
.LFE""DC!!E""RA!>£)JI,",-"A-,-V.!!
D!"1INrSTRA TIO, - PARTS M
PMA No.:
Acrospace Sealants LLC
4 Plum Ct.
Sleepy Hollow, Il 60 I 18
Article Name
cahm l
.:..P.:!
Q~
38:::8~6C.:::E
~ _ _ _ __
Supplement No.: ..:.1.::.8.:.R:.:v
e.:.;....:I_ _ _ _ __
Date: May 1,2012
Approved
Replacement For
N SLl422-A2
ACTURER APPROVAL
t aloot
Approval Basis a nd
Approved Design Oala
T est Md ComplllBllon.s per
14 cm 2 1.30.1
Product Analvsi Report:
PARJ204
jill;.A
Dllh:: 05/04/07 or a Imer
FA.A -app roved revision
Make Eligibility
y..mn & Whitney
Model Eligibility
PT6A·67AG. PT6A-6n .
I'T6A-66D, PT6A-67F.
I'T6B-36. 1'"I'68-36A. PT68
3GB. PT 6B-37,
PT6B-3 7A,
PJ'6C-67D, I'T6C-67C ,
I'T6T-3, PT6T-3A.
I'T6T-38. PT6T-3BG.
PT6T-3 B '.. I'rOT-6,
PT6T-3D. PT6T-9,
P1'6T-3DE, PT6T-3DF,
P1'6T-3B F.
PW118 , P,",' 11 8A,
Pil'I 188. 1'11'11 98,
1'11'119(',1'11'120,
PWI20A, PW121,
1'11'121 A. I'W 123 .
PII'123AF,I'WI2313.
PII'123C.I'WI13D.
1'1V123F.I'WI2413,
PII'125B.PII'126A,
PIV127.I'WI271:,
1'11'1271'. I'll' 127G.
PlY 127M. I'IY '150A.
I'IY206;\. 1'11'2068.
PW20(,II2, PW206C,
PW2061:, PW207 C.
PW207IJ. I'W207D I,
PW207D2,
PW)05. PW3 05A,
P1I'3051l, PII'306A.
PW3()(lB. PV\iJ06C.
P1V3ll7A, I'W30 8A.
I'II'J llSC, 1'1I'530A,
P\V535A, P W53513.
PW 545A, PW545B.
I'W 545c'I'W6 10F-A,
PIV 6 17 F-I·:. PW615 F-A,
PW20J7, PW203n1,
PW2040. PW2043,
PW2240, PW2143 ,
PW16-U. PW20400,
PW2337, PW 2037D,
F 11 7-PW- 100,
W[UI2A-4A ,
JITIJ12A-SA. JTSIJ-208,
Jl8!)-2 17, JT8IJ-2 17'\, JT81)-217c' J 1'8D-2 19, .IT9IJ- JA. JT9D-7, J1'91)-71L ll9D-7A. JT9D-7A H. J1'9D-7F. H9D-20, 119D-7J, JI (1I)-20J . JlI)D- 59A. JT91J-7Q3, J r9D- 7 R4E.
12/ 5 1
FE D RAL AVIATION ADMI ISTRATION - PARTS M
PMA No.: .:.1'-"Q"'3,:.:..;6:..;:
88 ·C:..;:E'- _ _ _ __
' ;,,1.,-:-_ _ _ __
Supple ment No.: .,:.1.:.8.,:.R;,,:e,,:,v;"
4 Plulll Ct.
Article Name
ScalaJll
Date:
Appro,'ed
Replacement For
NSLl422-A2
UFACTURER APPROVAL PRe -De OtO Sea lan t
PR 1422-A 2,
PR-144 0· A2,
ProSeal 890,
ProSea I 890M
Approval Basis and
A pproved Design Data
re I ;lnd Computation.s per
Make Eligibility
Prnu & WhiLney
14 FR 21.303
Product Anll\vsis Report :
PAR3204
\,. A
Dnle: 0 5104107 or n later
FAA-approved revi sion
Sealant
Same as ubovl!
Sam e a5 above
Same as above
Airbus
May 1,20 12
Model Eligibility
JT9D· 7R4111. JT9D·70A,
JT'lD-7R4D_ JT'lD· 7R41 ' I,
JT~D-7R4 E4. JT9D· 7Q,
JT9D-7 R41J1 ,
n'90-7R4G2.
PW4050. PW4052,
PW·Hl56. PW4060.
I'W41l60A. P\\,4060r.
PW4062. PW4062A,
PW4152. PW4156,
I'W4156A PW4158,
PW4160.I'W4460,
PW4462, PW4650,
PIV4074.PW4077.
PW4077D,PW-\084,
PW4IlS4 D, 1'1V4090,
1'11'4090-3,1'\\,40740,
PW40900, PW409R.
PW4164.PW4168.
PW4168A.I'W-\I64C,
PW4164C/B,PW4170,
PW4168/\-ID.
P\\,4168-ID.1'1V4164-1D.
PW4 J64C-lll.
P\\'4164C1B-1I1,
PW(d22A, PW6124A
1\300, Model B2-1 A,
A300. Model R2-1 C.
/\300. NhH.h;1 B4-1C ,
A300. Mudel B2K-3 C.
/\300. Model B4-103, AJUO, Model 1l2-203. /\J 10. Modd 204, AJ 10, " Iodd 221, A310. \>lode! 222, Aj 10. Mode1203. A31O, Model 322, 1\3 10. Model 324. /\3 10, M"dcl304. A310, Mode1325. A300. Modd B4-60 I. A300, Model 84-603. A300. Modd 84-620. A300, Mode I1l4-605R. A30() , j\'lodel U4-622R. AJOO, Modd F4-605R, /\3011. Model F..J-622R, A300, Model C4-605R Variant F. /\300, Model B2-62" A3J8 1\..lmld -III ,
A31S :v!odcl·112,
A318 ~lodcl-121,
1315 1
PMANo.:
Supplement No.:
Date:
4 Plum Ct.
PQ3886CE
18 Rev. I
May 1,2012
Approved
Article Name
Se,tlmH
Replacement For
Part Nu mber Part Number
SL I422-A2
PR e -DeSoto Sealruu
I'R-1422 -A2,
PR-144U-A2,
ProS(.'ai R90,
ProS,,:al 890M
Approv.1 B.sis and
Approved Design Dala
I'est an d Computations per
14
Make Eligibility
Ai rbus
FR 21.303
I)W~ll!,;:1 /jDll l :t:!~i:i I~k~ort :
PAR3 204
Rev; A
~ 05/04/07 or a laler
FM-appro\lcJ n!\'ision
Model Eligibili ty
A31 8 Model-In
A319 Mode l-III,
A31l) Model-112,
A319 Moud -113,
A319 \1mkl-114,
A319 Model -liS,
A3 19 Model -131 ,
,\319 :\'Iodd -\ .12.
A3 19 M(l{k'] -133,
A320 tviodel-III,
1\320 Modd -211,
A32il Modd -212.
A.nO Model -2.13,
A321 Model -I II ,
A321 Model-112 ,
A321 Model-13l,
A321 Modlo!J -211,
A321 Mod~I-212,
/\321 Model -213.
A321 tvlodd -2.12,
A330-20 1, A3 30-2U2,
/\.1311-203. A33t1-223,
,\3 30-243, A330-303.
A330-302. A33U-32I.
A330-3 22, A330-323 ,
1\3.10-H I, A3:;o-342,
A330-343,
A340-211. -21 2. -213 ,
A.140-3 II , -312. -31.1.
A.140-54 I, A.140-642,
1\.180-84 1, A3S0-842,
A.1S0-S61
Sealant
NS1.l422-A2
PRe-OeSu(() Sealalll
PR- I422-A2.
I'R-1440-A2,
l'roSI.'all:NO.
Pro Seal ~I)OM
Test and COlllpul;:uions pt"T
ATR
14 f R 21.303
PrQd\lt' 6DD)nl~ R~nQrt :
PAR3204
&l;;.A
Da'<: 05104/07 or a later
ATI!42-200, ATR42-300.
/I rH42-.12o. A1"R42-500,
/lTR 72-10 I. TR72-20 I,
ATR72-102, An02-202,
ATR72-21I , ATR72-2 12.
AT R72-212A
SealUIH
NSLI422-A2
PRC'-O\.:SOIO S\.:alant
PH-1422-I\2,
PR-1440-A2 ,
Pro Seal 890,
ProScal 890M
14 FR 21.303
Product 6nalvs i..: BCll(lrt :
I'I\J0 204
Rev: A
Date: 05/04/07 or a l<ltt-'r
I':AA-aprrovt"d revi sion
14 /5 1
MI."Donnell Ouuglas
OC-S-II. DC -8-12,
DC-R-2I , D '-8-31.
DC-R-32, DC-8-33,
DC-S-4I, DC-8-42,
OC-8-43 , DC-8-5I ,
OC-8-52. 0 -8-5.1.
DC-RI·'-54 , O '-S F-55,
DC-S-55. DC-8-6I,
DC-8-6IF, D -8-62,
\)C-~-62F . DC-8-63.
DC-8-63F, DC-R-71.
DC-8-7I F, D -8-71,
DC-S-72 F, OC-S-73.
FED ERAL A LATJON ADMINISTRATION PARTS MANUFACTURER APPROVAL PMA No.: .:..P:::i:Q.::;
38::::8::;,6C::;;~
'£ _ _ __
Supplement No.: ,,;,1,;;,8,,;,R,.;,c,,;,v.,,;,I_ _ _ _ __
Date: May 1, 2012
4 Plum Ct.
Sc8lam
Approved
Replacement For
ame as above
Same as above
:'\,:alal1l
NS Ll422-A2
Article Name
Approval Basis and
Same as abo...-e
PRe ·D~S()t() S~alall~
PR·1422 · A2.
PR-1440 A2,
ProSea) 890.
Test and Com putations pl-'r
ProSea I S"JOM
Re\l: A
Oale" 05/04/07 or a laler
Make Eligibilily
Model Eligibility
McDonne U Douglas DC-8-73F,
MD-II, MD- IIF
L-IOII-38S-I ,
L-IOII-38,-1-14,
L-lOll-38,- I- I"
L-lOll-38'-3
14 CFR 21.303
Product "n"I,';.;4<:; Repon:
PAR3204
FAA·"pprovcd rcvisi()n
Sam\,.' as above
Same as Above
S<.IIllt.:
as above
Da~ sJuh
A\ ialion Falcon 10, F,lkon :WOO. Falcon 2000EX, Mys terc·FaJcon 50,
MY.'ltcre·Fakoll 900.
Falco n 900EX
Fan Jet falcon, Fan Jet Falcon Series C. Fan Jet Falcon Series D, Fan Jet falcon Series L Fan .Jet J.'alcoll ~ cri c:- F, Fan Jet Falcon Series G. Mystc:re· Faleon 200. Mystcrc·I'alco n 20·C5, MYSlC:n:.Fakoll 20·D5, Mystr.;rC'·falcon 20· £5 . Mysten;·Falcon 20·F5
l\SL I422-ll1 / 2
PRC-DcSolu Sealant
PR-1422-IJlI2_
I'R-1440-11l i2,
ProScaJ 890
Test and Computal.ion s per
14 CFR 21.303
Product t\nah'sis Report
PAR3204
Rev: 1\
Date: 05104107 or a later
I:AA-approvt.'1I revi... it )n
('[;[\1'1' Intcm illional,
SA
crM,6-2. CFM,G-2A,
CrM,(,-2n. CrMS6-3 .
CFMS6-3B, C FM,6-3C.
CFMS6-S , CFMS6-5-A III'.
CFMS6-SA3 . C FM 56-SA4.
,FMS6-5A4IF,
C'FM56-SA5 .
C'FM,6-;,\ , IF,
CFM56-SBI.
CFM56-SB I!3,
CFMS6-5JJ21P,
CrM56-5 U413,
CFM56-5 B311P.
CFMSG-SIJ4 /P I ,
CFMS(,-5 JJ6JP
CFM,6-S(WP.
CFM ;()-SU7.
CFM51i-5117/3.
CFM56·5C2,
CFM,6-5 C2/li.
CFMS6-S C3/F4,
CFM56·50 1.
C FMS G-SU lIP.
Cl-'M,6-Sll2/3,
CFM56-5U2/2 P,
ISiS I
FEDERAL A V!AT!ON AD MIN! T RAHON - PARTS MAN UFACTURER APPROV AL I'MA No.:
Supplement No.:
Date:
4 Plum Ct.
Article Name
~ e al alH
Approved,
Replacement For
. SU4 22-BI I2
PRe -DeSoto Seal ant
PR-1422-BI/2.
PR-144U-B 112.
ProSeal 890
PQ3886CE
18 Rev. j
May 1,2012
Approval Basis and
Tt;;Sl and C()mp utat ions pe r
14 c m 2 1.3(1.1
Product A nal vsis Report:
PARJ204
Make Eligibility
Model Eligibility
CFM intcmtltional , CFMS6-SB4/3BI ,
CTM56-5B3!2[)I,
SA
CFM56-5114/2P,
CF\·ISO-5fJ6.
CI~\tI56-5n7fP,
DaLe: 05104107 or a laler
FAA-upproveJ revision
CFM56-5fl8/3.
CFM56-5 C2/4,
CFM56-5 C2/G4.
C F:vt5(,-5C3/G,
Cf\1SO-' C4 n>.
CFM56-5flI/2P.
CI,':vt56-5 [33/3.
CTM56-5B3/P,
lTMSO-5B5 /3,
CFM56-5 8 4,
CTM56-5B4/2P I,
CFM56-5!38 /P,
('1 :1\1156<' 13913 ,
CFM56-5C2n' .
CFM56-5 C21P.
H..;15()-5C3 /G 4,
CF M56-5 C411,
CFM56-582,
CF M56-5113/3111.
C FM56-5113 /P I,
CF M56-5B6/3,
C FM 56-5134 / P,
CFM56-585,
CFM56-586/2P,
CFM56-51J91P.
CFIVI56-SI39!2P,
C rM I6-5C21 4,
CFM56-5 ('...J/i>.
C FM50-)(:;J /P.
CI,'MI6· I C4/1 p,
CI' M%-7Il20.
C FM 56-71322.
CFM56-7Il2li3,
CFM56-7Iln
CFM56-7Il24/3,
CFM56-71126,
CFM56-7B26/JB I,
CFM56-7827.
CFM 56-7Il27/3,
CFM56-7Il271ll1.
CI,'M5(,-71127/3B I,
CF M56-71327/31J I F,
CFM56-7112(1),
C FM56-7Il20/2,
CF M56-71122/2.
CFM56-7B22/3B I,
CFM50-71124i2.
CI,'M56-7Il24/.lfll,
CFM56-1IJ26/2,
16151
J-EDERAI. A VIAIIO
IRATlON - PARTS MANUFACI RER APPROVAL
Aerospace Sealanls LLC
4 Plwll Cl.
Sleepy Ho llow, II WI 18
Ar liel. Name
Stahmt
PMA No.:
Supplement No.:
Date:
Approved
Replacement For
Pa rt Number Part Number
N ' L I411-B ln PRe-Dc, tHO ealall l
PR-I ~22-1l 1 /2.
I' R-1.1411-11 112.
ProS,"uJ 8')0
Appro\'a l Oasis nod
App roved Design 08ta
Test rmd Computations pt:r
14 C'F R 21.303
PmdUCl A nnlysj.- R.~
PAR3204
Ma ke Eligibility
PM InlemOl ionnl,
~A
Rev: A
Date: OSI(J4 /07 or a later
FAA-approved revbion
Sealant
Same as above Same as above
Same as above Boeing
PQJ886CE
18 Rev. I
Mayl,2012
Model Eligibility
FM5 6-71.l26/3B2F.
CI'M56-7U27A.
C'l'M56-7112 7 F,
CTM56-7Il27/ B3.
('1'''156-7112713133,
CI'M56-7B221B I.
C FM56-7B241B 1,
C FM56-7fl26/3.
CFM56-7B26/1l1 ,
CFM56-7B26/JF.
CFM56-7B26i132.
CFM56-7B26/JB2,
CFM 56-7B27n,
CF 156-7Il27A13.
CFM56-7B27E1F
CFM56-5 2.
CFM56-5 C2/G.
CFM56-5C3/ F4.
727 Series, 727-1 00 Seri es,
727C Seri es,
727-IOOC St:rics.
727-200 Series.
727-2001' Series,
73 7-1 00 Series,
737-200 Series.
737-200
cries,
737-300 Series,
7.17-400 Series.
737-500 S~ ri es.
737-600 Series.
717-700 ."erie<,
737-KOO Series,
737-900 Series,
737-900ER Series,
747-100 Scric$,
747-200ll Seri ,
747-200F Series.
747-200C Series,
747SR Serie!'.,
747Sf> Series,
7 ~ 7- 1 oor; Series.
7-t 7-J OO Series.
747-1008 SUD Se ri es.
747-400 Series.
747-400D Series,
747-100F Series.
757-200 Series.
757-2001'1' Serie,,
757-200CB Series.
757-3 00 Series..
7ll7-200 ~cries.
767-300 Se ries,
767-300F Series.
17/ 5 1
FEDERAL AVIATIO N ADMINIST RATION - PARTS MANUFACTURER APPROVAl ,
PMA No.: .:..P:;.Q;:::38~8:::6(::.:'E::..._ _ _ __
S upp Iemen t No.: .;.1.:.8.;.R;:c.;.v,:,'.:.1_ _ _ _ __
Date: May 1.2012
4 Plum Ct.
Sleepy Hollow, Il 60118
Article Name
Sealant
Approved
Replacement For
Part Number Pari Number
Ns r, 1422-111 12
PRC-r1eSulO SealfiOl
Approval Basis and
Make Eligibilit"
'est a nd Computations per
14 C I'R 21.30J
PR-1 422-BI 12.
PR-1 440-BI I2 ,
fwili!~ (la !YSjs
ProSl.:"uJ 890
PAR 3 2Q4
Model Eligibilitv
767--WO ER Series,
777 -200 Seri es.
777-300 Series,
RCP9n '
777-300EI( Series,
777-200LR Series,
777 F Serit:s
.8.=A
D.le: OSI04107 or a later
J-'JV\-app roved revision
Sealant
Same ns above
Same as abo ve
Same
[IS
above
Airbus A.100. Model 132· lA,
,~30U, Model U2-1 C,
AJOO. Modd B4-2C
/\300. Model B2K-JC,
AJOO.
A.1UO.
AJ I O.
AJ I II.
A310,
A310.
AJ I U,
\1odclIl4-IDl.
Model B2-20J.
Model 204.
Mudel 2211,
Mo(\cl122,
Modd 2U3.
Model J22.
AJ 10, i\'1odcl 32.:1,
/\ 3 I 0,
~,rodcl
-,Ool,
A110, Model 325,
A3UO . Model U4-60 I,
AJ OO. Modd 114-603,
A300. M odel B4-620.
AJOO, !'vloJd B4-60SR,
A.100. ModelIl4-622R, AJIIII, Model 1'4-6USR. A300. MoJcl F4-612R, A~O() , tvloJel C4-(l(l5R Variant f. AJUO. Model U2-612, A31~ \'Iodel-II, I, A318 \I" dd -112, A318 Model-121. A318 Model-I22, AJI9 Model-III, AJl9 Model-112, ),\J
19 I'dodd -113, A319 Model -114, A3 t 9 JvtoJel -115, AJ 19 Model -131, A311) Modt ! -132, A.l19 Model -133, AnU Modd -I II. A120 \\'Iodcl -2 [ I, /\:120 Model -232, A.120 Model -233,
A311 'M odel -I 1 I,
18151
FEDERAL A VIA TID
ADMINISTRA TID - PARTS MANUFACTURER API:ROVAL Aerospace Sealants LLC
4 Plum ('I.
Sleepy Hollow, II 60 I 18
PMA No.:
Supplement No.:
Date:
PQ3886CE
18 Rev. I
May
1, 2012
Approved
Arlic le am.
& olanl
Replacement for
Purl Number Part Numbc.r
NS I.1421-ilIl2
P R '- DeSoto Sealant
PR-1422-1l1/2.
1']( -1440-111 12,
ProS..:a! M90
Appro,'al Basi, and
Approyed Design Data
14 cm 2 J.)OJ
Make Eligibility
A irbus
.~]2 1 Mndel -13 I,
A321 Modd -211,
A321 Model-:!l2,
AJ21 !\iodcl -213,
A321 \fodd -2]2.
1\3 30-20 I, A330-202,
1\330-203 , 1\3.10-223,
A3JO-24J , A3JO·30J ,
1\3]0-.102. 1\.1.10-321 ,
A330-322, A330-323,
A330-34I. A330-342.
A3]O-34] ,
A340-211, -212, -213,
1\]40-311. -312. -313,
1\340-541, A340-642.
A3RIl-84I. t\J80-842,
i\3S0·R61
Pr()dU~I/~nub'§jji 1~~nnD~
PAl~3204
R,,"v: A
Oate: 05/04/07 or a later
FAA-appro ...·.;d revision
"'-:~danL
SiJ.[m!
u.s abov!..:
Saml..: as above
Same as above
Model Eligibility
A321 Model-112 t
Bombardier Inc
BD-IOO-IAIO, AD-70IJ-I A I 0, 1l0-700-11\ I I, CI.-215-6A I 0, C L-215-6U II (CL-2IST Variant), ('1.-2 I S-GIlI I (CL-4IS Variant). ('1.-600-I-A II (CI.-600). CL-600-2A 12 (CI.-601-3A Variant.).
l'l.-600-2A 16 (CL-600-JR
Varinnt),
CI .-600-21116 (CL-604
Variant).
C'1,-600-2TI 19 (Regional
Series 1011 & 440 J.
CL-600-2CIO (Regional
Se rie, 7011. 701 & 7(2).
C I.-600-2DI5 (Regional
Series 705),
CL-600-21J24 (lh:gional
cries 900).
DH C-K-IOO Series.
])1ll'-X-2110 Series,
DIIC-R-300 Series,
DII C-K-400 Series
Sealant
Same as ahove
Sflllll"
ijS
ahovt
Sam...• as ahu,......·
Pran & Whitney
lTISfJ-I, lTIS!)-IA_
JTIS])-In. JTISfJ-4,
JT IS ])-413, JT 15 0-4C
JTI 5lJ-4lJ. Jll5lJ-S.
JTI5fJ-5 ,\, lTISll-Sll,
JTl51J-5 C,1TI50-5/-.
lTISD-SR. HISD-Sll,
19/5 1'
Jet
Jet
Jet
Jet
FEDERAL AVIATION ADMIN ISTRATION
PARTS MANUFACT RERAPPROVAL Aerospace Sealants LLC
4 Plum Ct.
Article Name
Se.'llam
PMA No.:
Supplcment No.:
Datc:
Approved
Replaeement For
Part Number Part Numher
NSL 1422·BII2
PRe· Dc. at<) . calunt
I'R-1422-B 1/2.
I'R-1440-01 12.
ProSe. I 890 Approval Basis and
Approved Design I)ata
Td l uno COlllpu lat i()IlS pcr
14 'FR 21.303
Product Anal>;:sjs R
PAR3204
n :
Rev : A
Oatl.': 05104 /07 or a later
FAA-<)pprovcd revision
Make Eligihilitv
Prall & Wh itney
PQ3886CE
18 Rev. I
May 1.2012
Model Eligibility
PT6t\.-6. PT6A-6A
PI"6A-6Ll. PT6A-6/C20.
PT6A-II . PT6A-IIAG.
pl6A-15ACi. PT6A-20.
PT6A-20A, 1'I"6'\-20B.
Pl'6A-25, PT6A-25A ,
PT6A-25C". I'TM-27 , PT6A
28. PT6A-29.
l' IM-34, PT6A-341J, PT6A
34AO, PT6A-35,
PT6A-36,I'T6A-38.
PT6A-40. PT6A-41,
PTM-41 AG, f'T6A-42.
PT6A-42A. PTM-45,
PT6A-45A. l'r6A-45S,
PT6A-45R. PT6A-50.
PT6i\-60, PT6A·oOi\. PTf;!\
60ACi. PT6A-(il,
P16A-6! A. P'161\-6513,
PT6A-65R. PT6A-65AIC
PT6A-65AG. PT6A·llU,
1'1'6,'\-112. PT(}A·114.
I'l6A-114A. PT6A-114·A.
I'l6A-l 16. I'l6A-121,
1'16A-135, PT6A-l 35A.
PT61\-52. PT6A-66,
PTM"66A. PTM-67.
I'T6A-6 7 A. 1'1"6'\-67 AI-,
PTGA-67P. PT6A-67R
PT6A-67D, P'1'61\-04.
PT6A-66B. PT6A-(J8.
PT61\-67I\G. PT61\-67T.
I'T6A-660, I'T6A-671 ',
PT6B-36. 1>T6B-36A , PT6S
3GB. PT6B-37.
PTGB -37A.
PTGC-670, PT6C-67C,
P1"6"1"-J. PT6T-3A.
PT6T-3B, PT6T-3 IlG,
PT6T-mE. PT6T-6,
PT6T-3D.PT6T-9,
1''r6' '-3DE. PT6T-3UF.
PTliT·mr.
PWIIS, PWIIKA,
PWII81l. PW1191l.
PWlltJC, PW120,
PW120,\. PWJ21.
PW121A, PW123.
PWJ23AF, PWI23S ,
PWI23C P\VI2 3 D.
PW 123E. PW 124B,
PWI25B.PWI26A,
PWI27. PWI27
PWI27 F, PWI27G,
20/5 I
TlON ADMINISTRA nON - PARTS MA lJ FACTU RER APPROV AL
PMA No. : .:..P~Q.::;
JS::..:S~6C:;:.E
:::.
· _ _ _ __
Supplement No.: IS Kev. 1
Date: May 1, 2012
4 Plum Cl.
~~~~----
Appro"ed
ReplacernclIl 'For
Approval Basis and
.:.A"r-,t",
ic",I':,N=a"m"c,---,",a;-,rt
P~ 7N"",u",m,:,b",e;-r-7.P",.c;,r;.,t;e
N",u",n""b:.;e:o,r=-:::-_..;;A;>p"p"r."vc
o.,.:;:·d:'c"0"'c"'si"'ge;n:-'O"'."'t"'a,-----'.:-';"",
M k·"e,,E'O',,:
lig~i'2'b",il",it,",Y_~
M"07'd;;c,;..;1E Iigi bi Ii ty~_ __
. enlam
NS L 1422-B 111
I'RC-L>eSolo Sealant
PR·1422·1J1 12.
Test ood Compuuui()n$ per
14 eFR 21.3113
PR-J44()-I3I f2 .
Product AgOlysjs R cn() rt~
PW2()(,U2. I'W206<.".
PruSe,,1890
PAR3204
lkY;. A
PW206E. PW207C.
PW207l). PW207DI.
PW207D2.
~
05 /04107 or a latt:r
FAA-appro ved ~vision
Pratt & Whimey
PW 127M. PW 150A.
I'W2I1M.PW206B.
PWJ05. PW305A ,
I'W30511.I'W306A.
PW3(16Jl. PW.l 06C,
I'W3117A. PW30M.
I'W,lOSC,PW530A.
PW535A , l'W535B.
rW545A. P W545B.
PW545 C, PW(,IOF·.\.
PW(,1 7F·I; . I'W615F·A.
PW2037. PW20J7M,
PW1040. PW20:l .l
rW2240. PW2143,
I'W2643 . PW20411D.
1'11'2337. PW20J7U.
f I1 7·I'W·1 00.
WmI2A·4A.
1FT)) 12A·5A. Jl KJ)·20X.
JTXl)·217. JT8l) · 2 17A.
nm·217c, .IT8l)·219 •
.IT,!J)·JA. n·'JD· 7.
JT9D· 711. .IT9D· 7A.
n9D·7AII. JT9D·7F.
JT<)J)·211. n9J)· 7J.
H<)))·20.l.iT9J).,,!A.
JT<)f)·7{).1. JT'!D· 7J{-lE,
.vI''!)). 7J{4111. JT'JD·70,\.
JT<)J). 71(4 D. JT9l)· 7R4E I •
.1 '1'91)·71(41;)4. JT9l)· 7Q.
H'!!)· 71(4!) I.
JT<)D·7R4G2 ,
PW4050.I'W4052.
PW4056. PW4060.
PW4 0()(I!I. PW4060C.
rW4062. PW40li2A
I'W41 52. PW4156.
I'W4156A. ·1'11'4158.
1'11'4160. 1'11'4460.
PW4462 . PW:.l6S0,
I'W4074. I'W4077.
I'W4077D. I'W4084.
PW40X41l. 1'1V4090.
PW40<)0·.1 . PW4074D.
PW4090D. I'W409R.
I' W4164. PW4168.
PW4168A. 1'1V4 164C.
PW4164 C/Il.PW4170,
PW4108A·ILJ.
I'W4168·1 D. I'W4164·1 D.
21 /51
FEDERAL AVIATION ADM INISTRATION - PARTS MAN UFACTU RER APPROVAL Sealants LLC
PM A No .:
-,P",!,Q",
] 8:..:8.;:.
6C",E;:.._
'
_ _ __
4 P lum Ct.
S leepy Hol low, /I 60118
Supp lement No .:
Date :
18 Rev. I .,..::..c..:..::,c..:.,'::-:-::----
Aero~pace
Approved
Replacement For
Pa rt Number Pa rt Num be r
Approval Basis a nd
Approved Desig n Oata
. en lilnt
Same as u.bo ve
Same a:-; above
Same as above
Scalant
NSLl422 -BII2
PRe-DeSoto Sc;,\lnnt
PR- I. .t 22-B II2,
PR- I -I-IO-RI .'2.
PmS..;a l W)O
rest nnd ('o mpufations per
14 CFR 2 1 OJ
Article
am e
Pr~uC1
,oDBlyotis
Make Eligibility
Pratt & Whitney
ATR
Re~ort:
PIIR32
Rev : A
Dau:: 05/04/07 or a laler
FI\i\-,'I pproved revision
Sea lant
Sam..: as above
Same as above
Same as above
McDonnell Douglas
Sell!nn!
Same as above
Same as n\1(wc.;
Snme as nho\'c
l.m::kh~ed
P R C - OcSl) l (~
I ~~ t anu I..:olll pulall oll s pl.:f
14 C I K 2 !.JUJ
NSL 1-l22-U2
PR -I -l22 -U2.
1'1(· 14411-1.12.
ProSt:ili 890
Sealan t
Product
!\nal \'~ is
Ih:port:
Ci 'i\'1' il ltt:rnali lmnl.
SA
Mayl,20 12
Model Eligibility PW4 Ih4C-IIl, PW4 164l"1D- 1D, PW6 122A, PW6 124A ATR42-200. II"FR42-300 .
ATR42-320.IIT[(42-S00,
II1'R72- IOf . IITR72-20 1.
ATR72- lm.IITR72-202,
ATR72-2 11 , ATR72-2 12.
ATR72-2 12A
DC-8-1 1. DC-8-12.
DC-8-2 1,DC-8-3i.
DC-8-32. OC-8-3.l.
llC-H-4 1.D '-8-42.
OC-8-43. DC-8-S I.
DC-8-52. DC-8-53.
DC-XF-54.
-8 1'"- 55.
DC-H-55. D -8-61.
DC-8-6Ir. J) -8-62.
DC-8-62f'. DC-8-63.
DC-8-63 F, DC-8-71 .
DC-8-7 IF, D -R-72.
DC-R-nf', DC-S-73.
DC-8-73 F,
MD-II. MD-IIF
1.-1011 -385- 1.
1.-1011-1R5-1-14.
L-IOII-385 - 1- 15.
L-IOII -385-3
CJ-"M'I>-2. CFM56-2A.
CJ-"M5(>-2 B, (·FM51i-3 .
Rc.v: r\
C I'M56-JB . CF MS6-J C,
CFM56-S. CFM56-5-A III',
CFM5h-5A3. CFM56-5A4.
~
C F~1S6-5A4/F.
1'/I IU204
05/0·1/07 or a la[er
FAJ\-approvcd rc\'is ion
C r ~·1 56-5'\5.
C'FM5('·SII5/ F.
\"FM56-S11I,
CFM56-SIII /J.
CFM56-5B2IP.
CFM56-SIl4JJ ,
C"FM56· SB3np.
l"FM5b-51l4/ P I .
<:,;i\'156-5B5fP.
CFM56-5117.
CFM56-5 117/3,
C FM56-5C2 .
22/5 1
FEDERA l" AVIATION ADMINISTRATlO, - PA RTS MANUFACT RERAPPROVAL
PMA No_:
Supplement No_:
Date:
Aerospace Sealants LtC 4 Plum Ct. Sleepy Hollow, II 60118 PQ3886CE
18 Rev. 1
..,..;-;--':'-'::~---
May 1,2012
~~~~-------
Approved
Article Name
Seill£uH
Replacement For
NS1.1422-B2
PRe-DeSoto Sealant
PR~
1412-B2,
PR-14..J:()-B1,
ProSe-at X90
Approval Basis and
A pp roved Design ."D-="-=,
ta --,Ma"
;.;;: k::;.e-;oE".1i,.g",",ic;.:
i b li",t',--' ;-~M~od"e:;:Ic:E",::,
I ig",i",
b.:.:
il.:.:
ityL_ _ __
14 cm 21.303
Prod uct An[l l y~is Rworl:
PAR.3 2Q4
ll.,":; A
Dut(": 05i04/07 or n lall'r
l"AA-approv~J
r("vision CFM tnb:rnaliollo t, CFM56-SC2! J. SA
CFM56-SC3/F4, CHvI56-5 C4, GI'M56-511I IP, C FM56-SB2/3,
C FM56-5B2J2P,
CfM56-5U4/3B I,
C FMS6-513.J/2P I.
CFM56-5134/2P.
C FM56-5B6.
GF MS6-SB71P,
GFMS6-5B8/3.
CFMS6-S C2/4.
C FM5<1-S C2/(i4,
CFM S6-5C3/G,
CFMS6- 5C4/P.
GfM S6-S Bl I2P.
crMS6-S83/3,
CFMS6-5B3/P,
CFMS6-5BS/3,
CF MS6-SU4,
FMS6- 5B4 /2P I,
C FM56-SB8/P,
CFM56-Sll9/3,
C FM56-5 C2IF,
GFM56-5 C2fl',
(F\156-5 - /CA,
CFMS6-5 C4/I ,
CfM56-SB2,
GfM 56-5B3 /3B I,
GFM56-S B3IPI,
C FMS6-SIJ6/3,
C:1'i\1 50-5134/P,
C FM56-5A5 ,
Cf l\156-5B6/2P,
Ct-M 5(J-5INiP.
C rM5n -5 IWI2P,
CI' M56-5 C2/F4,
CFM56-5 CVI',
C"~ M5(}-5 CJ !P .
CI'M5n-S C4IlP,
CFM56-7B21\.
C FM56-7B22,
CT1vIS6-7f322I3 ,
CFM56-7B24,
CFMS6-71124!3,
CF M56-71l26,
C FM56-7B2613B I,
CFMS6-71327.
CI'M56-71127I3 .
CI'M56-TB27lB I.
CFM 56-7 1l27/.l 13 I,
CfM S6-7U27I.lB 1F.
C FM56-7B2013,
23/51
FEDERAL AVTATIO
A~rospac~
ADMIN ISTRATION - PARTS MANUFACT
ER APPROVAL PMA No.: .:.P~Q-=38:..:8;.:.6C
.::.E='
_ _ __ Supplement 0.: 18 Rev. 1 -:'7-'--":--::-::-:-=---
Dale: May 1, 2012
Sealants LLC
4 Plum Ct.
Sleepy Hollow. II 60 11 8
Approved
Replacement POr
Article Name
Sea lan t
Part umber Part Number
N ' L1422 -1l2
PRe-DeSoto Sealant
1'1(-1422-U2,
J'R-I ·UIJ·R1.
RIJO
iproS~al
Model Eli ibilil
CTM56-71l2012,
CFM56-7Il2212.
CFM56-7IlP U I,
CFM56-7R2412.
CTMj(,-71124 131,
CFM5G-7Il2612.
CFM56-7Il26/3U1F.
CFM56- 711271\.
CFM56-711271JF,
CFM56-71l27/133,
CFM56-71J27/JI33,
CFM56-7112 21B I,
CFM56-711241B I.
CFM56-7n26/3,
CFM56-7D26113 I.
CFM56-7 1126/3F.
CFM56-71l261132.
CFM56-7Il26!J 132.
CFM56-7Il27/2.
CFMSI>-7U27AJJ,
CF\156-7U27 EJF
("I'M 56-5('2,
CTMS6-5C2IG,
CFM56-5C31f'4,
P CO!JUCl An alysis HI..'port:
PARJ 204
lill';..A
Dale: 05/04107 or a latn
I'AA-appro\,ct! rc.."ision
Same
a~
above
Same as ahm;c
Smne as (lhn"~
Boeing
727 Series. 727-100 Series,
727C Series.
72 7-100C S<:ries.
727-200 Series.
727-200F Scri~s.
737-100 Series.
737-200 Series.
737-200(' Series.
737-300 Series.
7J 7-400 Series.
737-500 Series.
737-600 Seri es.
737· 70() Series.
73 7-KO() Series.
737·c)()0 St:rics.
737-900ER S<:rics,
747- 100 Series.
747-2009 Scric~
747-200 P Se ries,
747-200C rics.
747SR S<:rics,
747SP Series,
747-10013 Series,
747-300 S<:ries.
747 -IIXJB S 0 Series,
747-400 S<-rl es.
747-400D Series.
747·4001' Series,
757-2UU Series,
24 /51
FEDERA l. A VIATION A DM INISTRATION - PARTS MANUFACTURER APPROV AL
PMA No.: _1'.Q
.;",3.;..8""86:..C,-P",,._ _ _ __ Supplement No.: 18 Rev. I
-:-:--:-:=---
Date: May 1, 2012
4 Plum Ct.
Sleepy Hollow, II 60118 Article N.",e
Sealunt
Approved
Replaceme-nt For
NSL 1-l22·H:!
['ltC-DeSolo SCillaI1l
PR-1412-B2.
PR-I .... 40-B2.
ProSeal890
Approval Basis and
14 em 21.303
Make Eligibility
Boeing
Product An.l1ysjs Reooo'
PAR3204
Model Eligibility
7S7-200PF Serks,
757-200CB Series,
757-300 Series,
767-200 Series.
767-3{)() Series,
Rev: A
~ ()5 /(J4 /07 or a later
767·3001' Series.
767-400ER Series,
777-200 Se ri es,
FAA-ap proved revis ion
777-300
~er i es ,
777-300ER, cri.s,
777-200I.R Series.
777F Serj~s
Sl: <llant
Same as above
Sam e a:- above
Same
;IS
nhovc
BornharJh:r Inc DIl-IOO-IAIO,
UO-700-IAI0.
BIl-700-1 A I I.
C'L-21 5-6'\ I 0,
C'1.-2I S-61l11 (CL-2151'
Variaot).
C L-21 5-6UI I (CI.-41 5
Vilriant).
C'1.-600-I-A II (CI.-OOO).
C'1,·oOO-2A I2 (l'I,-601-3A
Varialll).
C l.-600-2BI6lCL-600-3R Varimll). C I.-600-211 16 (Ci .-604 Variant). C I.-600-2B 19 ( Rq;iu"al l e. Series 100/1; 440). CL-600-2C I 0 (Regiu" al Jc. Seri es 70il. 70 I & 702), CL-(lOO-2 1> 1-" (Rcg,iullaJ Je( S~ri es
7(5). CI r 60/l-21l2·1 (Reg ional .I" I\eri c..~ 900). Dlle -8-1 00 Series. DIIC-H-100 Series, OHC-R-300 Series, 01IC-S-400 Series S~" I < Hl[
Same' a~ above
Sam~
as ubovc
Sam!..:
<I.,)
,.tb {)v~
2515 I
Prall & Whitney lTISIl-1. J\'IS])· IA,
Yl' 15D-IB, JTISD-4.
JT ISIl-41l. JT ISO-4l'.
JT IStl·41J, J n SO-5.
l T I5D-SA, J1'151:>-51l,
.ITISD-5l'. J"i' ISIl-5F,
JT l SD -SR ..1,(, ISIl-5D.
PTM-~. I'TM-6A.
PTM -6B, PTM-6/C20.
I'I'M-II , P1'6f\-11 AG,
P IM-15AG, PT6A-20,
I'T6A-20A 1'1'6f\-201l.
FEDERAL AVIATIO
ADM INISTRATIO - PA RTS MAN lJFACTURE R APPROY AL
Aerospace Sealants LLC PMA No,: -'-P"'Q"'38"'8:;:6,::.C;::
E_ _ _ __
Supplement No,: 18 Rev , 1
Date: 7rv7Ia-y-:'-,720~,:O:l-----
4 Plum C1. Sleepy l-Iollow, II 60118 Article Name
Sealant
Appro\'ed
Reptacement For
Part Number Part Numher
NS L1422-U2
PR · DeSmo Sea lant
PR-1422-IG .
I'R-I44U-112,
PruScal 890
1
App""'." Oasis and
Te$( and Complllutions per
14 n R 2U()3
Product Ana1v:sis Report ;
PARJ:!04
Rev: /\
~
05/0·1/07 or a 1;1tcr
FA;\-JPpr(\\· ~J revi~ion
Make Eligibility
Pra tt & Whitm:y
Model EliGibility
1''1'61\-2', PT6A-2,/\,
PT6A-2,c:. I'T6A- 27, I'TM
28, I'T6A-29,
Pli6A<i4 . PT6A-J-1n. PT6.'\
34/\G. PTM-J 5,
PTM-30. I'rI>A-38.
PT6/\-40. I'T6A-41.
PTM-41 fIG. 1''1'61\-42,
PT6/\-42/\, I'II>A·45,
PT6/\-4511 . PTM-4,fl.
PT6A-4,R, PT6A-50,
PT6A-6(). PT6A-60A. PT()A
60/\G, PT611-61,
PTM-6IA, PT6A-65 fl.
I'T6A-65R. I'T6/\-~5/\R ,
PTM-6SAG, 1''1'61\-11 u.
I'TM-112, P'f'6A-114.
I'TM-114/\, PTr,A-114A,
PT6A-116.I'TM- 121,
PT(lA-IJ5. Pl6A-135A
PT6A-,2. I'T6A-66,
PT6A-66 ,\ P'j'hA-67.
PT6/\-67/\ . I'T6/\-67/\F.
P'I'M-671'. I'T6A-67B,
PThA-67 I>, PT6A-64,
I)T6A-66H. 1"j "6A-6H.
pr6A-67A G. PT6A-67"
j'"!·6A-66JJ . P"j"6,\-67F,
I'l6B-J!>. I'T6I3-36A, P'l6[l
J(,B. P"I"6 1.1-37.
PT613-37A. I'T6('-670. PT6C-67C, I'T61-3,I'T61-3A, I'TbT-JO.I'T6T-.l BG. I'T6T·3 AE, I'T61'-6, I'T6T-3D. 1'1'6'1'-9, 1'1 (,-r-.1D I;. PTGT-.lDF, pI'6T·3 1.1F, pII'II~ . I'WII~/\ ,
PWI18B. PWI191l.
I'WII~C. I'W1 20.
PWI20A " I'WJ21 .
PWI 2 IA , PWI2J.
pWI2JAF, I'WI2JIl,
PWI2J C. PW123D,
I'll' 123 E. PW 12~B,
I'WI2513.I'WI26A,
1'\\,127, PWI27E,
PW 1271'. rw 127G.
I'WI27M, PWI'UA.
PW20(,A. PW206 B,
P\V206H2. PW206C..
[>W2061·:. P\\'207C
PW2U7D. 1'\\,2U7D I,
26/51 FEDERAL AV I ATION ADMI ISTRATION - PARTS MANUFACTURER APPROVAL
PM A No.:
Supplement No.:
Date:
Aerospace Sealants LLC 4 Plum Ct.
Sleepy Hollow, II 60118 ~P.:iQ~38:::8:::6.;;:C.:;;:E_ _ _ __
18 Rev. I
7M:-a-y--:I-. -::'20~1:-::2:-----
Approved
Article Name
Sea lanl
Replacement Fur
NS1..1411-1l1 PRC~I)eSOlu
)lR·I'421·Bl,
I'R·144U·1I2.
PruScal SI)O
Sr.:a lallt
ApIU""m'al Oasis and
Approved Design Da ta
Te:;t and
O IllP\l\illl()ll ~
per
14 CFR 2UIlJ
Product Anul ysls R..:port:
PAR3204
Rev: A
Dat..:: 05 /04/01 or a later
FAA-appro\ cd n!' ision
Make Eligibilitv
l'trou &. Wh itnc),
Model Etig ibility
PW207))2,
PWJ05. PW305A.
PWJ05Il. PW306A.
PWJ0613. PW306C.
PIV307,'.PW30SA.
PW]OKt'. PWjJOA.
PIYjJ5A , P1V535B.
PWj45A. 1'1I'545B,
PW545C. PW6IOf-.\ .
PW(>l7f- E, I'W6 ISF-A ,
PII'20J 7. PW2UJ 7M.
1'11'2040. I'W2114J,
PW2240.PII'2 14J.
1'11'2643. PW20401l.
I'W23] 7, I'W2UJ 7[),
F117-PW-100.
JFT )) 12A-4A.
JITIl12A-5A. JTSD-20B,
)TW-2 17, JT8Il-217A.
J I'SIl-2I 7l'. )TW-2 1Y.
JT9D-JA. JT9D-7.
JT9D-7H. J 1'91J-7 A.
J 1'9I,l-7A II . JT91J-7F.
JT9D-20, J f9D -7J,
JT91l-20J , JT91l- 59A.
JT90-7Q3. JT90 -7R4E.
J 1'91J-7R'1HI , JT9D-70/1.
H91l-7R 'IIJ, JT91l-7R4 P. 1.
H91l-7R4 E4. JT9D-7Q.
JT9D-7R4 D I.
Jl'91l-7R4n 2,
P1V4050. PW4051.
PW'105r., PW4060.
I' W40MlA , PW4060C.
PW4062. P1V4062A.
P\\',11 5 2. PW,115(1.
PW4IlM. 1'11'41 58,
PW41 60. I'WH60,
PW4462. PW4650.
PW4074 . PW4077,
PII'40771.l. 1'1I'4U84.
PW40841l. 1'11'4090.
PW409(1-J . PW4ll74D..
PW4090D. PW4098.
PW4 164. I>W4168.
PW4168i\. PW4164C, PIV416K111. I'W41 70, 1'1'141 ('~A- ))). P\V416R-Ill. I'W4164-10. PW41 64 ·-ID. PW4 164 C!J)-IU. PW6122A . PW6124A 27/5 1
FE DERA L A VIATION ADMIN ISTRA T[O PMA No. :
Supplement No.:
Date:
4 Plum CI.
Sleepy Hollow, 11 60118
Article Name
Approved
Replacement For
.part Number Part Number
App rov a l Basis and
Make Eligibility
..;.P...
Q,;;,88
3;;,;;,.;;6.,;;
C.,;;
E_ _ _ __
..;.1,;.
8..;.R..;.V.
o..;.,,:I.,.,.,,_ _ _ __
M"y 1. 20 12
Model Eligibility
~~s~c~al~~~~~
ru1l
N~S~I~.1~4~2~2-~B~
2 ~~
PIZ~-~~~
DeS~o~
' o~Se~
~ ul~M-.--~
'
T~c~~:t~tI~
,"~I C~O,~Il~Pl~l'~at~il~"'~'~pe~r~~~~A~ir~h~u~
.' ~~-A~.~l(~I O~~
. Mfo~e
d~1~1~12~-~IA~.-----PR-1422 -82.
PR-1 44 0- B2.
ProSea l 890
14 e FR 21.303
Produc t Ana lys is Report:
PAR3204
Rev : A
Date: 05104/07 or a later
FAA-uprrovcd rev isio n
AJOII . Model fl2-I C .
/\300 . Modcl lH·2 C.
A300. Mudd 8 2K-3 C.
A3 00, Mlldclll4-I 03 ,
A300. ~1odeJ m -203 ,
AJ I 0, MoLlcl 204,
A] 10. Model 221.
1\3 10, Mudd 212 ,
AJi O. Model 203.
A3 10. '\.Iodol 322.
A3 1O. Model 324.
11.1 10, .,- todel .104.
A310, Modd 315,
A300. Model B4-60 I.
A31111. MOlIeI B4-603.
113011. Mudd B4-o20.
1\300. Mod,,:] B4-60SH.. ,
A301l . MUlkl 8 4-612R.
A300. Mudel 1'4-60SR.
AJ OO, Modcl l'4-622 R.
AJOO. ModeJ C4-60 5R
Varian t 1-~
A300. M"del 82-622.
A3 18 Model -I I I.
AJJ8 Model - 112.
J\J I H Mvdel - I' 2 1,
AJ I X M ll liel - 1,22.
J\3 1 ~
Moo", - I II .
A3 19 M" Jd -I, 12,
J\3 19 IVlodd- IJ 3,
MI ') Model- I 14.
"1 1C) ivh,de l - 115.
AJ I l) Moo d · l3l .
1\3 1'J Model - 1:'1,
A] 1'> \!lodel - L11.
A.'UO Mnde l -I i' 1,
i.\32fl Vlnde! -2 1, 1,
A.nn Mndel -231 .
A320 \ 10dc.1 -21\
11.121 Model- III .
A3 2 1 ModcJ -112 ,
A32 1 Moud -J.ll.
1\32 1 Model -2 11,
A32 1 ~'loueJ -2 12.
A32 1 Model -211.
A12 1 M oucl-2J2,
A330-20 I. A330-202.
1\330-20.1. 1\330-223.
1\330-243. ADO-JO}.
A3311-302. A3.10· 32I ,
113.111-.1 22. A.130-323,
A330-34 I. 1\ .130- 342.
A330-343.
28/5 1
fEDERAL A VIAnON A DMlN ISTRA TION - PART
PMA No. : .:.P. ::sQ.3"'
::. 88"'6C=E_
"'
_ _ __
SupplemcDt No.: .,:.1.:.8. :.R:.e..:.
;: v· 1:.,....,_ _ _ __
7
Oate: Ma y 1, 2012
Acrospacc Sealanls LLC
4 Phun Ct.
Artic le Name
Sealant
Approved
Replacement For
, arne a..<i above
Appro,.I IInsis and
Snw liS abo \'e
Make Eligihilit\'
Airbus
Model Eligibility
340·211.
1'13 ·10-311.
A34U-54 I'.
1'1.180-841'.
-212. -213.
-312. -313.
A340-642.
A3~1l-842.
AJSO·X() [
SC<lbnr
NS1. 142 2-B2
Same as ahove
PRC· l kSo((l S~ahllll
PR-1411-B2.
PR-1440-112.
ProSl:ill X90
T c t and Computations per
14 'P R 2l..l03
AT\(
Prod ct Anahl ~ i , Rc ull:
PA R3204
Rev: A
)atc: 05f 04lO7 or OJ lalcr
A m42-2UO. AT R42-3UO.
AIR42-320. ,\ 1'R42-500.
A f"R 72 -1 0 I. Am 71-20 I.
AT\(72- \(12. A1'\(72-202.
AT\(72-211. ATR72-212.
ATR72-2 12A
FAA -approved re vision
S\.:alant
Save a:, above
Same as above
Same az.; above
McDonnell Duuglas DC-8-1 I. lJC-8-12,
DC-X-21. DC-S-)I,
llC-H-J? [lC-R-)),
DC-H-41. DC-8-42,
f)C-8-43. DC-8-51.
DC-H-52. DC-H-53,
DC-SF-5 4. IX'-RI'-55,
DC-8-55. \lC-8-61.
D '-8-6 1F. DC-8-62.
DC-X-62F. DC-S-C..l.
DC-H-b3f'. DC-R-7 1,
DC-R- 7 1F. J)C-R-72,
o '-B-72F, OC-8-73,
OC-8-7JF.
DC-9-11. J)C-')-12,
OC-9-J.l, n C-9-14.
0'-9-15 , 1lC'-9-15 f .
D '-9-21. OC-9-31.
-9-32. DC-9-31 (VC-9C),
DC-9-32!'.
DC-9-.l2 (C-,!'\' C -9Bi.
DC-9-34. IlC-9-)4F.
f)
'-9-4' I. Ix '-9-51.
DC-9-~1
(MD-RII.
DC-9-H2 (MIl-X21.
DC-V-H3 (MIl-H.1 I.
DC-9-X 7 ('VID-87).
~m-HX. MD-90-30.
7 17-200
\1.1)-1 I. Ml).J' I F
Sealant
S<.u111.' as aho \'{:
S<Ulh.• as abu\-\,:
Smnl.' as alJl)\ c
2lJ!5!
J .uckJh..' cd
L-IilII-385-1.
l.-1011-385-1-14 ,
L-1011-3X5-1-15.
L-IOII-385-3
FEDERAL AVIATIQN ADMINISTRATION - PA RTS MANUFACTURER APPROVAL Aerospace Sealants tLC
PMA No.:
Supplement No.:
Date:
4 Plum Ct.
Sleep), Hollow. II' 60118
Article Name
S~aJanl
Approved
Replacement For
NS L1.:t22-B2
PI{ '-DeSoto s.::ulunt
PR-1422-U2,
PR-144U-B2 ,
PmScall'NO
Approval Bnsis and
T e:; Lillld Compuilltioll s per
Make Eligibility
Dussnuh A viation
PQ38S6CE
18 Rev. I
MilY I. 2012
Model Eligibilitv
I'aktlll 10,
]:alcon 2000.
14 Gf' R 21.303
Fa.lcon 20UOEX, MY~I~ r ..:-I:akon 50, Product A nal vs is RepJ.U1:
I'AR3204
Rey; A
Mystcn:-falcon 9110. 12,11 : 05104/07 or a later
Falcon 9001::X Fan Jel Fulcon, F.I\A-approvlo:d revi s ion
r an Je t Falcon ScriC:i C. Fan Jet Falcon Seric $ D, pan Jet Fulcon Series C. r. Fan Jet Falcon Series
Fan J et Fa lcon Series G. Myslcre-Fa1con 200. Mysterc-f."n!con 10-C5, Mystcrc-Falcon 20-D5, M y::'1~re -Falco n 20- E5. Mystcre-Fakon 20-FS Sca!an(
NS L 18:!6-B I /~
I'R<. '·)kSoto Sea lant
PR-IX26-ll Il4
r C.' 1 anJ Computations pCI'
em
14
21.30.1
I'rodUl:t Anal vsi:-o Reporl:
PAR3204
Uomhan.lic:r Inc
nD-lOO-IA10,
llD-700-1 /\ I 0,
1)1l-700-1 ,\l1 .
CL-215-(,AIO.
GL-215-flIHI (C I.-21 5T
Rev ; A
Date: 05104/07 or :t laLer
Variant),
FAA-approwd rev ision
C L-215-6811 (GL-415 Variunt). C L-600-I-AII (CI.-600), CL-6uO-2A 12 \CL-601-JA Variant),
CI..-600-21316 (CL-600-3R
Y"riant),
Ct..-600-211 16 «("1.-604
VarialH).
CL-600-2flI 9 ( Reg ional J et Series 100 & 440), CL-600-2(, I 0 (Region,1 Jet Series 700. 701 & 702). C L-6()()-2D 15 (R~giona l Jet Series 7(5). CL-600-:!D24 (Regional kl' Series ~OO).
DH ( '-S·\ 00 Serie::;,
DJ 1('-S-20(j Series,
DI-IC-g-300 Scri,"s.
DJ.'C-8--400 Series
30/51
NSL1422
Rev. C 07-15-12
NSL1422 Class A
Product Description:
NSL1422 Class A is a fuel resistant sealant for
use on integral fuel tanks and pressurized cabins
as well as other areas subject to contact with
aircraft fuels, lubricants, oils, water and/or weathering.
NSL1422 Class A is a two-part polysulfide base
compound which cures at room temperature
to a flexible, resilient rubber.
When mixed, NSL1422 Class A is a self leveling
liquid. For mixed application life details see cure
profile below.
Product Features:
• Excellent adhesion to aluminum, magnesium, titanium, steel and numerous other aircraft substrates.
• Designed to withstand the attack of sulfur compounds that are present in jet fuels and aviation gas.
• Service temperature range -65ºF (-54ºC)
to 250ºF (121ºC) with excursions to 275ºF (135 ºC).
• Suitable for application by brush to thickness of up to 25 mils.
Heat-Accelerated Curing:
Increased temperature and relative humidity
will reduce work life and speed up the cure.
Reduced temperature and relative humidity will
extend work life and slow the cure.
Packaging:
Available in 2½- and 6-oz. cartridges, pint, quart
and gallon kits. Also available in premixed and
frozen cartridges. Other-size packaging available
upon request.
Shelf Life:
Sealed containers: 9 months when stored below
80°F. Slight changes in work life, viscosity and curing
rate may occur but will not affect end performance of
the product.
Typical Properties:
UNCURED
Color: Base Curing Agent Mixed Mixing Ratio: (by weight) (by volume) Non-volatile Content Viscosity, poise
Base
Curing Compound Specific Gravity Consistency CURED – ROOM TEMPERATURE
Cured – 7 days @ R.T.2
Tensile Strength, PSI Elongation, % Durometer, Shore A Min. Peel Strength, PPI
Flash Point
Fungus Resistance Replacement For:
PR-1422 Class A, PR-1440 Class A, P/S 890 &
P/S 890M Class A
Conforms3 To:
AMS-S-8802 & BMS5-26U by FAA-PMA Approval
Off-white
Gray
Gray
100:10
100:8.3
86%
2501
1,000¹
1.25
Self Leveling
250
250
50
30
90ºF
Non-nutrient
¹ Brookfield RVF Spindle #6
2
Conditions 77ºF and 50% R.H.
3
Material and data depicted on this TDS is provided to Aerospace Sealants
by the approved manufacture supplier(s) for this material. Qualification and
inclusion on the QPL(s) is by the supplier(s) per their material identification
and conforms as required by the governing specification.
Cure Profile:
A-1/2
A-2
Application Life (hrs) 1/22
2
Tack Free Time (hrs) 2
<8<24
Cure Time to 35 Shore A (hrs)
30
72
Aerospace Sealants FAA PMA
4 Plum Ct. - Sleepy Hollow, Illinois 60118
(800) 527.0011
This document contains proprietary information and is not to be transmitted, reproduced or disclosed to anyone without written permission of Aerospace Sealants.
NSL1422
Rev. C 07-15-12
NSL1422 Class B
Product Description:
NSL1422 Class B is a fuel resistant sealant for
use on integral fuel tanks and pressurized cabins
as well as other areas subject to contact with
aircraft fuels, lubricants, oils, water and/or weathering.
NSL1422 Class B is a two-part polysulfide base
compound which cures at room temperature to a
flexible, resilient rubber.
When mixed, NSL1422 Class B is a thixotropic
paste that will not flow. For mixed application life
details see cure profile below.
Product Features:
• Excellent adhesion to aluminum, magnesium, titanium, steel and numerous other aircraft substrates.
• Designed to withstand the attack of sulfur compounds that are present in jet fuels and aviation gas.
• Service temperature range -65ºF (-54ºC)
to 250ºF (121ºC) with excursions to 275ºF (135 ºC).
• Suitable for application by extrusion gun
or spatula.
Heat-Accelerated Curing:
Increased temperature and relative humidity
will reduce work life and speed up the cure.
Reduced temperature and relative humidity will
extend work life and slow the cure.
Available in 2½- and 6-oz. cartridges, pint, quart
and gallon kits. Also available in premixed and
frozen cartridges. Other-size packaging available
upon request.
Shelf Life:
Sealed containers: 9 months when stored below
80°F. Slight changes in work life, viscosity and curing
rate may occur but will not affect end performance of
the product.
Typical Properties:
UNCURED
Color: Base Curing Agent Mixed Mixing Ratio: (by weight) (by volume) Non-volatile Content Viscosity, poise
Base
Curing Compound Specific Gravity Consistency CURED – ROOM TEMPERATURE
Cured – 7 days @ R.T.³
Tensile Strength, PSI Elongation, % Durometer, Shore A Min. Peel Strength, PPI
Flash Point
Fungus Resistance Replacement For:
PR-1422 Class B, PR-1440 Class B, P/S 890 &
P/S 890M Class B
Conforms4 To:
AMS-S-8802 & BMS5-26U by FAA-PMA Approval
Cure Profile:
Packaging:
B-1/2
B-2
Application Life (hrs) ³ 1/22
Tack Free Time (hrs) ³
<824
Cure Time to 35 Shore A (hrs)
30
72
Off-white
Gray
Gray
100:10
100:8.3
96%
11,000²
1,000¹
1.25
Paste
250
250
50
35
>200ºF
Non-nutrient
¹ Brookfield RVF Spindle #6
² Brookfield RVT Spindle #7
³ Conditions 77ºF and 50% R.H.
4
Material and data depicted on this TDS is provided to Aerospace Sealants
by the approved manufacture supplier(s) for this material. Qualification and
inclusion on the QPL(s) is by the supplier(s) per their material identification
and conforms as required by the governing specification.
Aerospace Sealants FAA PMA
4 Plum Ct. - Sleepy Hollow, Illinois 60118
(800) 527.0011
This document contains proprietary information and is not to be transmitted, reproduced or disclosed to anyone without written permission of Aerospace Sealants.
Material Safety Data Sheet
HMIS HAZARD RATING
Polysulfide Class A, Part A only
2
3
0
H
FED-STD-313
Latest Revision
May be used to comply with
OSHA's Hazard Communication Standard
29 CFR 1910. 1200 Standard must be
consulted for specific requirements
OMB registration Number
None
Health
Flammability
Reactivity
PPE
Type of Data Sheet
New
SECTION I General Information
X
Revised
Commercial ID (as on label and list)
Number of revised section:
Government contract or order number
NSL1422 Class A (Part A)
Manufactures Name Flamemaster Corporation
National Stock Number /CAN LSN /SIN
N/A
Manufactured For:
National Sealants & Lubricants
33110 Old Hempstead Road
Magnolia, TX 77355
Emergency Telephone Number
N/A
Part number, product and or trade name
Hazardous items
Yes
Information telephone number
(800) 424-9300 CHEM TREC
X
Date prepared
(800) 527-0011
Mfgr. CAGE code
05/14/2007
Name of Preparer
14439
Signature of preparer
On File
Billy Matthews
NRC License number
EPA Registration Number
N/A
Specification Number
N/A
Spec. Type
No
AMS S-8802
Spec. Grade.
Spec. Class
II
B
A 1/2 - A 2 - A 4
SECTION II - Hazardous Ingredients SARA III Information*
Hazardous Components (Specific chemical identity:
Common Name (s)
Other limits
By % weight
OSHA PEL
ACGHI TLV
NIOSH #
CAS #
55%
N/E
N/E
**
68611-50-7
10%
50 ppm
50 ppm
XS5250000
00108-88-3
** Liquid polysulfide polymer
(none CFR 1910.1200)
Toluene (Methyl Benzene)
** Toxic Data Not Established
All remaining Constituents are non-hazardous per FED-STD-313 All Constituents are listed in TSCA inventory; complete mixture is excluded Per TSCA Par. 710.4 (d)
95 (6) (7) Constituents are not listed in TSCA 12b CORR. LIST
* Indicates toxic chemical (s) subject to the reporting requirements of section 313 of Title III and of 40 CFR 372
SECTION III Physical /Chemical Characteristics
Boiling Point
Specific Gravity (H2 O = 1)
2310 F
Auto ignition Temperature
1.5
PH
Vapor Pressure (mm hg)
2
% Volatile by Volume
8.5
Evaporation rate (Butyl Acetate = 1)
2.0
Melting Point
Liquid at room temperature
Vapor Density Air = 1
3.1
Solubility in Water
Negligible
Decomposition Temperature
N/A
N/A
Magnetism (milligauss)
15
N/A
Viscosity
Corrosion Rate:
300 Poises
N/A
Temp
Material Reference
Blank
Appearance and Odor:
Volatile Organic Compound VOC
White Paste / Polysulfide odor
140 grams / liter
SECTION - IV Fire and Explosion Hazard Data
Flash Point (method used)
320 C ----- 900 F TCC
Extinguishing Methods:
Dry chemical, CO2 , Foam, Water
Flammable Limits
LEL
N/A
UEL
1.3
Special Fire Fighting Procedures
In confined areas wear self contained breathing apparatus, cool exposed containers with fog nozzles
Unusual Fire and Explosion Hazards
Vapors are heavier than air and will collect at low points see (Section V)
SECTION V - Reactivity Data
Stable
Unstable
Conditions to avoid
X
Neutralizing Agents
Open Flame High Heat
Incompatibility (materials to avoid)
Strong oxidizing agents
Hazardous Polymerization
May Occur
Will not Occur
N/A
Hazardous Decomposition products
H2S, CO, CO2, SO2, Smoke
X
Conditions to avoid
N/A
7.1
FED-STD-313 Latest Rev
Material:
Page 2
Date
05/14/2007
Polysulfide Class A part A only
SECTION VI - Health Hazard Data
Route (s) of entry
Inhalation?
Skin?
Ingestion?
yes
yes
yes
Health Hazards (Acute and Chronic) Non established (possible skin irritation) not considered a primary skin irritant may lead to muscular
weakness and dizziness, long-term exposure may lead to dermatitis, liver and kidney damage.
INHALATION: vapor will irritate nose throat and respiratory tract, high concentration may cause dizziness
INJESTION: can cause irritation of the gastrointestinal tract
Carcinogsnicity:
NTP?
IARC Monographs?
NO
NO
OSHA Regulated?
NO
Medical conditions generally aggravated by exposure:
Pre existing skin disorders, respiratory tract, liver and kidney damage
Signs and symptoms of exposure:
Skin or eye irritation head ache and nausea with impaired coordination
Emergency and first aid Procedures: Eyes: Flush with large amounts of water consult physician. Skin: wash with soap and water.
Ingestion: If swallowed get immediate medical attention.
SECTION VII - - Precautions for Safe Handling and Use
Steps to be taken in the event the material is released or spilled:
Remove sources of ignition. Scoop up and transfer to container for reaction with curing agent. Clean up remainder with sand or
sweeping compound. Wash area with soap and water. Wear appropriate clothing and protective equipment. (section VIII)
Waste disposal method:
React with curing agent and dispose of as solid hazardous waste per Federal, State and local regulations
Precautions to be taken handling or storing:
Empty drums may contain explosive vapors Store below 120 degrees dry area away from acids, oxidizers, open flame or other possible
ignition sources Ground containers when transfering.
Other precautions:
Wash hands thoroughly after handling this product prior to eating , drinking or smoking
SECTION VIII - Control Measures
Respiratory protection (specify type)
When applying in any circumstances likely to produce airborne levels of solvent vapors in excess of the TLV or when mechanically
abrading the cured material use an organic vapor cartridge or air supplied respirator.
Ventilation:
Local exhaust
Special:
Air
Protective gloves Type:
Solvent resistant gloves
Mechanical (general)
N/A
Other
Fan
Eye protection Type:
N/A
Safety Glasses / face shield
Other protective clothing or Equipment
Appropriate clothing to avoid prolonged skin contact
Work /Hygienic practices:
Safety shower, eye wash station and washing facilities should be available
SECTION IX - Transportation
Applicable regulations:
49CFR X
IMO X
IATA
Shipping name:
Not regulated
Unit container
Hazard class:
X
Military Air (AFR 71-4)
ID Number
N/A
DOT Spec. container
N/A
IMDG
Marine Pollutant No
Reportable Quantity
UN number
UN 1133
N/A
Net explosive weight:
N/A
Labels:
3
DOT Exempt /DOD CCN
Flammable Liquid
Limited Quantity:
N/A
Aerosol propellant (s)
Varies with quantity
U.S. Postal regulations:
N/A
124.122 Harmful mater
Disposal Information:
Incineration or land fill as is, or react with Part B dispose as hazardous solid waste
EPA hazardous waste number /Code:
Hazardous waste characteristics:
D-001 ignitable
Sludge
Disposal methods:
Incineration or land fill, The material must be handled, packaged and transported according to Federal, State or local regulations
The information in this MSDS has been obtained from sources that we believe to be reliable. However since much of this information has been received
from sources outside of the company, it is provided without any warranty expressed or implied regarding its correctness or suitability for specific
situations. The conditions of handling, storage, use and disposal is beyond our control and may be beyond our knowledge.
OMB registration
None
HMIS HAZARD RATING
1
Health
1
Flammability
1
Reactivity
G
PPE
NSL1422 part B only page 1
FED-STD-313
Latest Revision
Type of Data Sheet
New X Revised
NSL1422 Class A (part B)
Flamemaster Corporation
N/A
Manufactured For:
Magnolia, TX
NRC License number
Date prepared
Name of Preparer
(800) 527-0011
14439
05/14/2007
Billy Matthews
On File
N/A
AMS-S-8802
N/A
Spec. Type
NSL1422 Class A (part B)
Yes X
No
Hazardous items
(800) 424-9300 CHEM TREC
Mfgr. CAGE code
N/A
Manufactures Name
Spec. Grade.
Spec. Class
N/A
N/A
N/A
Common Name (s)
Manganese Dioxide
Other limits
By % weight
OSHA PEL
ACGHI TLV
N/E
< 65%
5 ppm
5mg /m
3
NIOSH #
CAS #
0P0350000
1313-13-9
Manganese Dioxide is in a wetted out dispersion exposure limits based on dust that is not present in this composition.
All remaining Constituents are non-hazardous per FED-STD-313 All Constituents are listed in TSCA inventory; complete mixture is excluded Per TSCA Para. 710.4
(d) 95 (6) (7) Constituents are not listed in TSCA 12b CORR. LIST
Boiling Point
N / Av.
2.0
PH
9
Non Volatile
Melting Point
N/A
N/A
Solubility in Water
Negligible
Not flammable
Unknown
2.0
N/A
Viscosity
Corrosion Rate:
1000 Poises
N/A
Temp
Material Reference
Blank
Black paste negligible oily odor
Non Volatile
> 930 C ----- > 2000 F TCC
Flammable Limits
LEL
N/A
UEL
N/A
Explosion hazard if heated with oxidizable materials
Stable
Unstable
Conditions to avoid
X
Neutralizing Agents
Easily oxidizable materials
May Occur
Will not Occur
N/A
Oxides of nitrogen, Carbon, manganese compounds
X
Conditions to avoid
None
N/A
Material:
Page 2
Date
05/14/2007
NSL1422 Part B Manganese
NSL1422 Page 2 part B only
Route (s) of entry
Inhalation?
Skin?
Ingestion?
Yes
No
Yes
Health Hazards (Acute and Chronic)
Impairment of central nervous system
Carcinogsnicity:
NTP?
IARC Monographs?
No
OSHA Regulated?
No
No
None known
Sluggishness, Sleeplessness, and / or Weakness in legs
Emergency and first aid Procedures:
Eyes: Flush with large amounts of water consult physician. Skin: wash with soap and water.
Ingestion: get immediate medical attention.
Dike and cover with non-oxidizable absorbent. Scoop up and transfer to container for reaction with base. Clean up remainder with
sand or non-oxidizable sweeping compound. Wash area with soap and water. Wear appropriate clothing and protective equipment.
(section VIII)
React with curing agent and dispose of as solid waste per Federal, State and local regulations
Keep container tightly closed, store in a dry location away from flammables (see Section VIII) wash hands thoroughly after handling
Other precautions:
When mechanically abrading the cured material use an organic vapor cartridge or air supplied respirator.
Ventilation:
Local exhaust
Special:
Air
N/A
Chemical resistant gloves
Other
Fan
N/A
Chemical goggles / face shield
49CFR X
IMO X
IATA X
IMDG
Marine Pollutant No
UN number
N /A
Shipping name:
ID Number
Reportable Quantity
N/A
N/A
Not regulated
Unit container
DOT Spec. container
< 20 gms. in plastic container
N/A
N/A
Hazard class:
Labels:
N/A
Not required
DOT Exempt /DOD CCN
Limited Quantity:
N/A
N/A
N/A
Incineration or land fill as is, or react with Part A dispose as solid waste
N/A
Sludge
Disposal methods:
When disposing of this material, the material must be handled, packaged and transported according to Federal, State or local
regulations
HMIS HAZARD RATING
Polysulfide Class B, Part A only
1
1
0
H
FED-STD-313
Latest Revision
OMB registration Number
None
Health
Flammability
Reactivity
PPE
Type of Data Sheet
New
X
Revised
NSL1422 Class B (Part A)
Manufactures Name Flamemaster Corporation
N/A
Manufactures Address (No Street, City, State and zip)
Magnolia, TX 77355
NRC License number
Hazardous items
Yes
Date prepared
Name of Preparer
(800) 527-0011
14439
No
(800) 424-9300 CHEM TREC
Mfgr. CAGE code
N/A
Billy Matthews
05/14/2007
On File
N/A
N/A
Spec. Type
X
AMS S-8802
Spec. Grade.
Spec. Class
II
B
B 1/2 - B 2 - B 4
Common Name (s)
Other limits
Liquid polysulfide polymer (none CFR 1910.1200)
Toluene
By % weight
OSHA PEL
ACGHI TLV
NIOSH #
CAS #
< 70%
< 5%
N/E
100 ppm
N/E
50 ppm
None
None
68611-50-7
00108-88-3
All remaining Constituents are non-hazardous per FED-STD-313 All Constituents are listed in TSCA inventory; complete mixture is excluded Per TSCA Par. 710.4 (d)
95 (6) (7) Constituents are not listed in TSCA 12b CORR. LIST
Boiling Point
N/A
1.52
PH
NIL
8.5
NIL
Melting Point
NIL
Solubility in Water
Negligible
N/A
N/A
3.0
N/A
Viscosity
Corrosion Rate:
12000 Poises
N/A
Temp
Material Reference
Blank
White Paste / Polysulfide odor
13 grams / liter
> 930 C ----- > 2000 F TCC
Flammable Limits
LEL
N/A
N/A
Vapors are heavier than air and will collect at low points see (Section V)
Stable
Unstable
Conditions to avoid
Neutralizing Agents
X
Open Flame
Strong oxidizing agents
May Occur
Will not Occur
N/A
H2S, CO, CO2, SO2, Smoke
X
Conditions to avoid
N/A
UEL
N/A
Material:
Route (s) of entry
Inhalation?
Page 2
Date
05/14/2007
Skin?
Polysulfide Class B part A only
Ingestion?
yes
yes
Health Hazards (Acute and Chronic) Non established (possible skin irritation) not considered a primary skin irritant
INHALATION: vapor will irritate nose throat and respiratory tract, high concentration may cause dizziness
INJESTION: can cause irritation of the gastrointestinal tract
Carcinogsnicity:
NTP?
IARC Monographs?
NO
NO
yes
OSHA Regulated?
NO
None known
Skin or eye irritation
Emergency and first aid Procedures: Eyes: Flush with large amounts of water consult physician. Skin: wash with soap and water.
Ingestion: If swallowed induce vomiting get immediate medical attention.
Scoop up and transfer to container for reaction with curing agent. Clean up remainder with sand or sweeping compound.
Wash area with soap and water. Wear appropriate clothing and protective equipment. (section VIII)
Empty drums may contain explosive vapors
Store below 120 degrees dry area away from acids, oxidizers, open flame or other possible ignition sources
Other precautions:
When applying in any circumstances likely to produce airborne levels of solvent vapors in excess of the TLV or when mechanically
abrading the cured material use an organic vapor cartridge or air supplied respirator.
Ventilation:
Local exhaust
Special:
Air
Solvent resistant gloves
N/A
Other
Fan
N/A
Safety Glasses
49CFR X
IMO X
IATA
Shipping name:
Not regulated
Unit container
Hazard class:
X
ID Number
N/A
DOT Spec. container
N/A
IMDG
Marine Pollutant No
Reportable Quantity
UN number
N/A
N/A
Labels:
N/A
DOT Exempt /DOD CCN
Not required
Limited Quantity:
N/A
N/A
N/A
Incineration or land fill as is, or react with Part B dispose as hazardous solid waste
D-001 ignitable
Sludge
Disposal methods:
Incineration or land fill, The material must be handled, packaged and transported according to Federal, State or local regulations
OMB registration
None
NSL1422 part B only page 1
FED-STD-313
Latest Revision
HMIS HAZARD RATING
1
Health
1
Flammability
1
Reactivity
G
PPE
Type of Data Sheet
New X
Revised
Manufactures Name
NSL1422 (part B)
Flamemaster Corporation
Manufactured For:
N/A
Magnolia, TX
NRC License number
Date prepared
Name of Preparer
(800) 527-0011
14429
Billy Matthews
X
05/14/2007
On File
N/A
AMS-S-8802
N/A
Spec. Type
NSL1422 (part B)
Yes
No
Hazardous items
(800) 424-9300 CHEM TREC
Mfgr. CAGE code
N/A
Spec. Grade.
Spec. Class
N/A
N/A
N/A
Common Name (s)
Manganese Dioxide
Other limits
By % weight
OSHA PEL
ACGHI TLV
N/E
< 65%
5 ppm
5mg /m
3
NIOSH #
CAS #
0P0350000
1313-13-9
Manganese Dioxide is in a wetted out dispersion exposure limits based on dust that is not present in this composition.
All remaining Constituents are non-hazardous per FED-STD-313 All Constituents are listed in TSCA inventory; complete mixture is excluded Per TSCA Para. 710.4
(d) 95 (6) (7) Constituents are not listed in TSCA 12b CORR. LIST
Boiling Point
N / Av.
2.0
PH
9
Non Volatile
Melting Point
N/A
N/A
Solubility in Water
Negligible
Not flammable
Unknown
2.0
N/A
Viscosity
Corrosion Rate:
1000 Poises
N/A
Temp
Material Reference
Blank
Black paste negligible oily odor
Non Volatile
> 930 C ----- > 2000 F TCC
Flammable Limits
LEL
N/A
UEL
N/A
Explosion hazard if heated with oxidizable materials
Stable
Unstable
Conditions to avoid
X
Neutralizing Agents
May Occur
Will not Occur
N/A
Oxides of nitrogen, Carbon, manganese compounds
X
Conditions to avoid
None
N/A
Material:
Page 2
Date
06/07/04
NSL1422 Part B Manganese
NSL1422 Page 2 part B only
Route (s) of entry
Inhalation?
Skin?
Ingestion?
no
No
Yes
Health Hazards (Acute and Chronic)
Impairment of central nervous system
Carcinogsnicity:
NTP?
IARC Monographs?
No
OSHA Regulated?
No
No
None known
Sluggishness, Sleeplessness, and / or Weakness in legs
Emergency and first aid Procedures:
Eyes: Flush with large amounts of water consult physician. Skin: wash with soap and water.
Ingestion: get immediate medical attention.
Dike and cover with non-oxidizable absorbent. Scoop up and transfer to container for reaction with base. Clean up remainder with
sand or non-oxidizable sweeping compound. Wash area with soap and water. Wear appropriate clothing and protective equipment.
(section VIII)
Keep container tightly closed, store in a dry location away from flammables (see Section VIII) wash hands thoroughly after handling
Other precautions:
When mechanically abrading the cured material use an organic vapor cartridge or air supplied respirator.
Ventilation:
Local exhaust
Special:
Air
N/A
Chemical resistant gloves
Other
Fan
N/A
Chemical goggles / face shield
49CFR X
IMO X
IATA X
IMDG
Marine Pollutant No
UN number
N /A
Shipping name:
ID Number
Reportable Quantity
N/A
N/A
Not regulated
Unit container
DOT Spec. container
< 20 gms. in plastic container
N/A
N/A
Hazard class:
Labels:
N/A
Not required
DOT Exempt /DOD CCN
Limited Quantity:
N/A
N/A
N/A
Incineration or land fill as is, or react with Part A dispose as solid waste
N/A
Sludge
Disposal methods:
When disposing of this material, the material must be handled, packaged and transported according to Federal, State or local
regulations
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
PQ3886CE/ 3
AS159
GE159, GE106, Dow Corning 736
PQ3886CE/ 3
AS3145 & AS3145P
PQ3886CE/ 3
(800) 527.0011

NSL Aerospace - NSL1422 Airline PMA Approval Packet

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