### BEFOR ETH EU.S . DEPARTMEN T O FTRANSPORTATIO N The Honorabl e Chie f

Administrativ e Law Judg e Ronni e A . Yode r rifT'. i



## I nthe matter

of BRENDA NAIRWAYS , LLC , d/b/aUSA300 0 Airline s

Responden

t DM S No. : FAA-2009-003 2 FA A Docket No. : CP09EA0007 FA A Cas e No. : 2008EA17003 8 RESPONS ET O COMPLAINANT' S FIRS T SE T O FINTERROGATORIES , REQUES T FO RADMISSIONS , AN D REQUES T FO RPRODUCTIO NO F

DOCUMENT S Come s no w th e Respondent , BrendanAirways , LL C d^/ aU S A300 0 Airline s [hereinafter "USA3000" ] an dRESPOND S t o th e Complainant' s Firs t Se t o f Interrogatories , Reques t

for Admissions , an dReques t for Productio no f

Documents . Response s t o Interrogatorie s 1 . Identif y th e names , titles , busines s o r hom e addresse s an dtelephon e number s o f eac h perso nwho mth e Responden t intend s t o cal l a s awitnes s a t th e hearin g o f

thi s matter . Response : Th e identity o f

an y witnesse s i s amatte r o f trial strategy that

ha s no t ye t bee ndecided . Th e Responden t

reserve s th e righ t

t o amen dthi s answe r

a s trial witnesse s ar e identified . 2 . Provid e th e substanc e o f th e testimon y t o b e offere db y eac ho f sai dwitnesses . Response : Th e identity o f

an y witnesse s i s amatte r o f trial strategy that

ha s no t ye t bee ndecided . Th e Responden t

reserve s th e righ t

t o amen dthi s answe r

a s tria l witnesse s ar e identified .



## L 

# o 11 1 C 3 

### 3 . Withrespec t t o eac hexper t

witnes s identifie di nrespons e t o reques t Nos . 1 an d2 above : (a ) identif y th e subjec t

matte r o nwhic hth e expert

i s expecte dt o testify ; (b ) lis t th e substanc e o f

th e fact s an dopinion s t o whic hth e expert i s expecte dt o testify ; (c ) provid e asummar y o f th e ground s for

eac hopinion ; (d ) i f th e Responden t

intend s t o introduc e int o evidenc e o r otherwis e rel y upo n a writte ncurriculu mvita e o r othe r writte ndocumen t

listin g th e expert' s professiona l qualifications , identif y an dattac hcopie s o f

al l suc hdocuments . 

# o o Q 

## C D ^ ^ 

# 5 : U J

### Response :

Th e identity o f

an y expert

witnesse s i s amatte r

o f trial strateg y that

ha s not ye t bee ndecided . Th e Responden t

reserve s th e righ t

t o amen dthi s answe r

a s expert witnesse s ar e identified . 4 . T o th e exten t

no t encompasse di nyou r

respons e t o Nos . 1,2 , an d3 above , identif y an d produc e statement s o f

al l individual s wh o spok e to , o r wer e interviewe dby , th e Responden t regardin g thi s matter . Response : W e objec t t o thi s interrogatory t o th e exten t that i t migh t b e interprete dt o includ e interview s conducte db y Counsel , o nth e ground s tha t suc hinterview s ar e protecte dfro mdiscovery a s Attorne y Wor

k Product . Al l Responden t

conversation s ar e detaile di naJun e 11 , 2008 , lette r fro mResponden t

t o Laurenc e Johnson , outlinin g th e interview s conducte dan ddescribin g th e informatio ngleane d fromthem . That

lette r i s attached . Tw o additional document s exis t that ar e als o responsiv e (bothar e als o attached) :

• Th e Responden t

intervie w o f

Jo e Mille r

resulte di naseparat e summary o f th e interview . A cop y o f th e Jun e 13 , 200 8 lette r

tha t wa s produce da s asummary o f th e intervie w i s attached . • Th e Responden t

aske dChie f

Pilo t Ti mLyon s wh y Captai nWalke r wa s i nth e lef

t seat durin g th e flight. A Jun e 3 , 200 8 emai l describin g th e answe r i s attached . 5 . Identif

y an dproduc e copie s o f

an y an dal l document s o nwhic hth e Responden t anticipate s relying , o r

wil l rely , i nsupport

o f th e cas e i t

wil l presen t

at th e hearin g i nthi s matter , includin g but

not limite dt o document s yo u inten dt o introduc e int o evidence . Response : Responden t

anticipate s relyin g o n • Th e ttanscript

o f th e enforcemen t

actio nBabbitt

v . Surratt

an dWalke r

(NTS B Docke t Nos . SE-18562andSE-18563) . • Th e Decisio no f

Judg e Fowle r

i nth e enforcemen t

actio nBabbitt

v . Surratt

an dWalker NTS B Docke t

Nos . SE-1856 2 an dSE-1856 3 (Issue dorall y Augus t 12 , 200 9 an dissue d i nwritin g o nSeptembe r

2 , 2009) . • Th e Decisio no f

th e NTS B denyin g th e appea l o f th e enforcemen t

actio nBabbitt

v . Surratt an dWalke r

EA-551 4 (NTS B Marc h23 , 2010) . • Th e Decisio no f

th e NTS B denyin g th e petitio nfor reconsideratio ni nth e appea l o f th e enforcemen t

acfio nBabbit t

v . Surratt

an dWalke r

EA-552 7 (NTS B Jun e 25 , 2010) . • Th e four

document s attache dt o th e Respondent' s Discovery Reques t date dJun e 21 , 2010 , whic hhav e previousl y bee nprovide dt o th e Complainan t (withtha t

Discovery Request) . • Th e document s attache dt o thi s Response .

### Responden t objects t o th e directio nt o produc e copie s o f th e case s an dtranscript s mentione d above , a s th e transcript s an dcas e decision s ar e alread y i nth e possessio no f th e FA A an dth e case s ar e als o availabl e throug hstandar donlin e researc hmechanisms . Th e specifi c identity o f

additional exhibit s i s amatte r o f tria l strateg y tha t

ha s not ye t bee n decided . Th e Responden t reserve s th e righ t

t o amen dthi s answe r

a s tria l exhibit s ar e identified . 6 . Identif

y wh o place dth e aircraft' s spoile r serv o actuator s for

lef t win g rol l spoiler s thre e an dfive i nth e maintenanc e mod e prio r t o th e flight

an dbetwee nApri l 29,200 8 an dMarc h17 , 2008 . Response : Durin g th e perio dApri l 18-Apri l 29 , AARplace dth e aircraft' s spoile r serv o actuato r

for lef t win g spoile r

thre e i nth e maintenanc e mode . AA Rstate di naMay 30 , 200 8 lette r t o th e FA A that th e aircraft' s spoile r

serv o actuato r

for lef t win g spoile r

thre e wa s returne dt o operationa l mod e o nApri l 29 . Thi s th e onl y tim e tha t th e aircraft' s spoile r

serv o actuato r

for lef t win g spoile r thre e wa s place di nth e maintenanc e mod e betwee nMarc h17 , 200 8 an dApri l 29 , 2008 . Accordin g t o th e record s w e have , th e aircraft' s spoile r serv o actuato r

for lef t win g spoile r

five wa s not place di nmaintenanc e mod e betwee nMarc h17 , 200 8 an dApri l 29 , 2008 . 7 . Explai nal l reason s wh y th e aircraft' s spoile r serv o actuator s for

lef t win g rol l spoiler s thre e an dfive wer e place di nth e maintenanc e mod e prio r t o th e flight

an dbetwee nApri l 29 , 200 8 an dMarc h17 , 2008 . Response : T o ou r knowledge , th e aircraft' s spoile r serv o actuato r

for lef t win g spoile r

thre e (bu t

not five) shoul dhav e bee nplace di nth e maintenanc e mod e onl y onc e betwee nMarc h17 , 200 8 an dApri l 29,2008 . Betwee nApri l 1 8 an dApri l 29 , 2008 , AARwa s workin g o nth e lef t wing' s numbe r thre e spoile r

control . Thi s wa s don e a s par t o f anon-routin e maintenanc e activity tha t was accomplishe dpursuan t

t o A 3 2 0 AM M 27-64-43 . A successfu l operationa l chec k o nApri l 2 9 confirme dtha t

thi s spoile r

wa s returne dt o th e operationa l mode . 8 . Identif y wh o and/o r

what entity i s responsibl e for

th e aircraft' s spoile r

serv o actuator s for lef t win g rol l spoiler s thre e an dfive bein g place di nmaintenanc e mod e prio r t o th e flight

an d explai nwh y yo u believ e tha t perso no r

entity i s responsible . Response : Asid e fromth e work

describe di nth e respons e t o interrogatory 7 , w e d o no t kno w wh o and/o r what entity i s specificall y responsibl e fo r th e aircraft' s spoile r

serv o actuator s for

lef t win g rol l spoiler s thre e an dfive bein g place di nmaintenanc e mod e prio r t o th e flight.

### 9 . Answe r whethe r afailur e o f

on e o f th e aircraft' s spoile r

servojack s coul dcaus e a nambe r LA FDEGRADE D messag e t o appear o nth e aircraft' s E C AM . Response : Yes , that i s on e o f th e man y scenario s unde r whic hanambe r

LA FDEGRADE D messag e migh t appea r o nth e aircraft' s E C AM . 10 . Explai nal l reason s for you r belie f that th e aircraf

t canb e dispatche dwhe nlef t an drigh t win g spoiler s thre e an dfive ar e inoperative . Response : W e objec t t o thi s interrogator y o nth e ground s that i t assume s a"belie f

tha t Responden t

ha s not professed . Responden t

als o objects t o thi s interrogatory o nth e ground s o f relevance , becaus e th e terminoperativ e i s define da s " asyste mo r componen t

malfunction " an dth e spoiler s i nthi s cas e wer e i nmaintenanc e mode , no t malfunctionin g 11 . I f yo u believ e tha t

th e aircraf

t i s i naconditio nfor

saf e operatio nwhe nth e aircraft' s lef t an drigh t win g rol l spoiler s thre e an dfive ar e inoperativ e pleas e stat e an dexplai nal l reason s for you r belie f Response : Responden t

objects t o thi s interrogator y o nth e ground s that thi s interrogator y call s for a n opinio nconcernin g safety , for whic hResponden t

doe s no t hav e appropriat e engineerin g dat at o respond . Responden t

als o objects t o thi s interrogatory o nth e ground s o f relevance , becaus e th e terminoperativ e i s define da s " asyste mo r componen t

malfunction " an dth e spoiler s i nthi s cas e were i nmaintenanc e mode , no t malfunctionin g Withou t waivin g thes e objections . Responden t state s that generally , i f

spoiler s ar e know nt o b e inoperative , the nth e aircraf t shoul donl y b e dispatche di naccordanc e withth e aircraft' s MEL . 12 . If yo u believ e tha t

th e aircraf

t conform s t o it s typ e certificat e and/o r typ e desig nwhe n th e spoile r serv o actuator s fo r

lef t win g rol l spoiler s thre e an dfive ar e place di nth e maintenanc e mod e pleas e stat e an dexplai nal l reason s for you r belie f Response : Maintenanc e mod e i s provide db y th e manufacture r a s origina l equipmen t

o nth e aircraf

t an di s therefore describe di nth e typ e desig nfor th e aircraft .

### 13 . Explai nal l reason s for you r belie f that th e placemen t

o f lef t win g rol l spoiler s thre e an d five i nth e maintenanc e mod e was not part o f an y maintenanc e performe do nth e aircraft . Response : W e objec t t o thi s interrogatory o nth e ground s that i t misstate s ou r

contention . W e hav e neve r claime dthat

that th e placemen t

o f lef t win g rol l spoiler s thre e an dfive i nth e maintenanc e mod e was not part o f an y maintenanc e performe do nth e aircraft . W e d o not kno w ho w o r

whe n th e lef t win g rol l spoiler s thre e an dfive wer e place di nth e maintenanc e mode . Ou r contentio n i s that th e placemen t

o f lef t win g rol l spoiler s thre e an dfive i nth e maintenanc e mod e wa s no t part o f any maintenanc e tha t

wa s ordere dby , o r

withi nth e contro l of

, US A 3000 . Inalette r t o th e FA A date dMa y 30 , 2008 , AAR(th e maintenanc e contractor ) admitte dthat durin g th e cours e o f

th e visit , o no r

before Apri l 29 , 2008 , th e serv o switche s fo r th e #2 , # 3 an d #4 LEF T spoiler s an dth e #4 an d# 5 RIGH T spoiler s wer e place di nth e 'Maintenance ' mode. " AA Rindicate s that

o no r before Apri l 29 , it s investigatio nshow s tha t th e serv o switc hfor

th e # 3 LEF T spoile r

wa s place di nth e 'Maintenance ' mode " but the nwas returne dt o th e operational mode . AA Rindicates tha t it s record s an dinvestigatio nsugges t tha t th e serv o switc hfor

th e # 5 LEF T spoile r

wa s neve r

place di nth e 'Maintenance ' mod e durin g maintenanc e performe dfor USA3000 . AAR' s lette r

indicate s tha t

th e servos wer e returne dt o th e operationa l mod e o no r befor e Apri l 2 9 an dtherefor e i f

the y wer e place di nth e maintenanc e mod e i t ha dt o hav e happene dafte r th e Apri l 2 9 inspectio ntha t

confirme dthe y wer e i nth e operationa l mode . That May 3 0 lette r

explain s that

whil e th e physica l evidenc e show s tha t o no r befor e May 17 , 2008 , lef t win g rol l spoiler s thre e an dfive wer e place dinth e maintenanc e mode , "ther e i s n o recor do f suc hactio nan dw e wer e unabl e t o determin e wh o may hav e bee ninvolved. " USA300 0 require s all maintenanc e t o b e performe daccordin g t o work card s o r non-routin e cards . Th e USA300 0 work card s wer e completed , an dther e appear s t o b e n o othe r spoiler relate dirregularitie s i nth e work card s o r th e non-routin e cards . Non e o f th e work card s an dnon routin e card s tha t

wer e accomplishe do no r after Apri l 29 , 200 8 require dth e lef t win g rol l spoiler s thre e an dfive t o b e place di nth e maintenanc e mode . O nMay 15,2008 , Mr . Mille r an dMr . Bea l o f

US A 300 0 performe dengin e test s o nth e aircraft . Durin g th e cours e o f

thos e tests , Mr . Mille r

ha doccasio nt o performaflight contro l test . H e receive dn o ECA M warning s abou t th e spoiler s an dreceive dn o indicatio ntha t th e spoiler s were i nmaintenanc e mode . A s o f thi s date , al l o f

th e maintenanc e performe do nth e aircraf t before th e flight, ha dbee naccomplished . 14 . Identif y wha t sectio no f

th e US A 300 0 Airline s Minimu mEquipmen t List , i f any , states , implies , o r

infer s tha t

th e aircraf

t canb e dispatche dwhe ntw o pai r o f symmetrica l spoile r surface s thre e an dfive ar e inoperative . Response : Non e

### 15 . Pleas e identif y an y malfunction s that

occurre di nth e aircraft' s ECA M syste mthat occurre ddurin g th e flight but prio r t o takeoff

. Response : Unknown . 16 . Pleas e describ e al l way s i nwhic hi t was determine dtha t

th e ECA M syste m malfunctione ddurin g th e flight but prio r t o takeof f Response : W e objec t t o thi s interrogator y i nthat i t eithe r i s duplicativ e o f

interrogatory 15 , o r

els e i f i t i s substantivel y differen t

fro minterrogatory 1 5 the ni t i s askin g for

somethin g tha t

w e canno t understan d(to o vague) . 17 . I f i t i s you r belie f tha t th e ECA M faile dt o report tha t lef t an drigh t win g rol l spoiler s thre e an dfive wer e inoperativ e and/o r wer e locke dou t

at an y tim e prio r

t o takeof f pleas e explai n al l reason s wh y yo u hol dthi s belief. Response : Durin g th e matte r

Babbit t v . Surratt

an dBabbitt

v . Walker , Captai nWalke r an dCaptai nSurratt eac htestifie dthat

at th e tim e o f

take-off , th e onl y messag e o nth e ECA M wa s "LA FDegraded. " LA FDegrade dindicate s tha t th e Loa dAlleviatio nFunctio n(LAF ) i s no t operatin g correctly , an d i s for cre w awarenes s only . 18 . I f i t i s you r belie f tha t th e pilot s aboar dth e aircraf t performe dasuccessfu l flight contro l chec k for th e flight, wit hrespec t

t o th e check s for

th e spoilers , pleas e explai nal l reason s why yo u hol dthi s belie f Response : W e objec t t o thi s interrogator y o nth e ground s o f relevance . Without

waivin g th e objection , w e stat e that durin g th e matte r

Babbit t v . Surratt

an dBabbitt

v . Walker , Captai nWalke r testifie dthat h e complete dasuccessfu l flight contro l chec k

for th e flight, an dCaptai nSurratt testifie dthat

hi s flight contro l chec k

wa s deeme dcomplet e after th e seemingly-spuriou s warning s wer e cleared . 19 . Identif y an ddescrib e all reason s wh y durin g th e flight th e aircraft' s lef

t win g ti p contacte dth e runwa y durin g th e aircraft' s first landin g attempt . Response : Objec t o nth e ground s tha t

i t call s fo r speculation . Withou t

waivin g thi s objection , th e forc e o f gravity overcam e th e counteractin g force s o f lif t withrespec t

t o th e wing .

### 20 . Identif y an ddescrib e what

mechanica l malfunction s i nth e aircraft , i f any , occurre d durin g th e flight. Response : A cop y o f th e aircraf

t lo g page s describin g th e mechanica l malfunction s i s attached . 21 . Identif

y an ddescrib e what

error s wer e committe db y th e pilot s durin g th e flight, i f any , that le dt o th e aircraft' s lef

t win g ti p contactin g th e runway durin g th e flight. Response : Non e identified . 22 . Describ e what

impact , i f

any , th e inoperativ e win g rol l spoiler s ha do nth e pilot s ability t o maneuve r th e aircraf

t durin g th e flight. Response : W e objec t o nth e ground s tha t

th e spoiler s wer e i nmaintenanc e mod e - the y wer e not inoperative . Inoperativ e mean s asyste mo r componen t

malfunction , an dmaintenanc e mod e i s different from amalfunction . Withou t waivin g thi s objectio nw e repl y tha t th e actua l impac t

th e win g rol l spoiler s ha do nth e pilot s ability t o maneuve r th e aircraf

t durin g th e flight

i s unknown . Durin g flight, th e aircraf

t neede dt o b e trimme dan dthi s may hav e bee ncause db y th e win g rol l spoiler s bein g i nmaintenanc e mod e but th e specifi c causal effec t i s unknown . 23 . Answe r

whethe r a nambe r LA FDEGRADE D messag e o nth e ECA M i s suppose dt o g o of f i f spoile r 5 i s inoperable . Response : W e objec t o nth e ground s tha t

thi s i s argumentativ e an d(a s drafted ) not relevant . Ther e ar e man y reason s wh y aLA Fdegrade dmessag e migh t appear . Withou t

waivin g thi s objection . Responden t

state s tha t

spoile r five wa s part

o f th e loa dalleviatio nfianctionsystem . If spoile r 5 wer e inoperable , the nyes , thi s i s on e o f th e events that

migh t caus e a nambe r

LA FDEGRADE D messag e t o appear

o nth e ECAM .

### 24 . Pleas e stat e whethe r th e documen t

attache da s Exhibi t

1 i s anaccurat e recordin g o f a conversatio ntha t

Jo e Miller , Directo r

o f Maintenanc e an dEngineerin g for Brenda nAirway s LLC , d/b/ aUS A 300 0 Airlines , ha dwitha nAviatio nSafet y Inspecto r

employe dwithth e FAA . Response : Althoug hi t

appear s t o b e generall y accurat e a s t o th e inspector' s perception , i t i s not averbati m recor do f th e conversation . 25 . I f yo u disagre e withth e followin g statemen t foun di nExhibi t

1 , o r i f yo u don' t

believ e thi s statemen t

wa s mad e b y Mr . Miller , explai nal l reason s for you r belief : "Canno t

hav e both# 3 an d# 5 spoiler s INOP. " Response : W e objec t t o thi s questio no nth e ground s tha t i t misleadingl y misstate s th e Jo e Mille r statemen t b y takin g th e statemen t

ou t o f context . I ncontext , th e statemen t wa s limite dt o arespons e t o a questio nabou t

dispatchin g anaircraf

t know nt o hav e inoperativ e spoilers , pursuan t t o th e USA300 0 MEL . Takin g th e interrogator y at fac e valu e (i nwhic hth e statemen t doe s no t hav e it s limitin g context) , w e d o disagree , becaus e i f aproble mi s discovere ddurin g flight, the nth e pilot s ar e expecte dt o refer t o th e Quic k

Referenc e Handboo k

(QRH ) for

instructions . I f

tw o set s o f

spoiler s are discovere dt o b e inoperativ e durin g flight, th e QR H state s that th e pilot s shoul dconfirmthat th e intende dlandin g site ha s arunwa y that i s at leas t 1.2 5 time s longe r

tha nth e minimu mrunway requirement . Th e QR H provide s n o othe r operatin g instructio nfor inoperativ e spoilers . Thus , on e coul dhav e tw o set s o f inoperativ e spoiler s durin g flight. 26 . Describ e th e relationshi p betwee nAA RAircraf t Service s an dBrenda nAirways , LLC , d/b/aUS A 300 0 Airlines , withregard s t o th e aircraf t i nth e tim e betwee nApri l 1 , 200 8 andMay 17,2008 . Response : AA RAircraf

t Service s wa s amaintenanc e vendo r for US A 300 0 Airlines . 27 . Answe r

whethe r o r no t yo u pai dAARAircraf

t Service s for

maintenanc e performe do n th e aircraf t betwee nApri l 1,200 8 an dMa y 17 , 2008 . Response : W e objec t t o thi s interrogator y o nth e ground s tha t i t i s ambiguou s whethe r

i t i s seekin g informatio nabou t

maintenanc e performe ddurin g thi s period , o r paymen t durin g thi s period . Withou t waivin g th e objection , th e answe r i s yes , w e pai dAARAircraf t Service s for maintenanc e tha t

wa s performe do nth e aircraf t betwee nApri l 1 , 200 8 an dMay 17,2008 .

### 28 . Answe r whethe r o r no t Internationa l Leasin g Financ e Corporatio n(ILFC ) pai dAA R Aircraf t Service s for

an y maintenanc e performe do nth e aircraf t betwee nApri l 1,200 8 an dMay 17,200 8 an di f

paymen t wa s mad e identif

y wha t typ e o f maintenanc e th e paymen t wa s for . Response : Responden t

object s t o thi s interrogatory o nth e ground s tha t i t seek s informatio noutsid e o f Respondent' s knowledg e tha t woul dpos e a nundu e burde no nresponden t t o obtain . Withou t waivin g thi s objection , an dfollowin g reasonabl e inquiry . Responden t doe s not kno w th e answe r t o thi s question . 29 . Answe r

whethe r o r no t Stat e Transport

Compan y Russi a(STCR ) pai dAA RAircraf t Service s fo

r an y maintenanc e performe do nth e aircraf t betwee nApri l 29 , 200 8 an dMay 17 , 200 8 an di f

paymen t wa s mad e identif

y wha t typ e o f maintenanc e th e paymen t wa s for . Response : Responden t

objects t o thi s interrogatory o nth e ground s tha t i t seek s informatio noutside o f Respondent' s knowledg e tha t woul dpos e a nundu e burde no nresponden t t o obtain . Withou t waivin g thi s objection , an dfollowin g reasonabl e inquiry . Responden t doe s not kno w th e answe r t o thi s question . Response s t o Reques t fo r Admission s 1 . Durin g th e flight

th e aircraft' s spoile r

serv o actuator s for

lef t win g rol l spoiler s thre e an d five wer e i nth e maintenanc e mode . Response : Admitte d 2 . Whe nth e aircraft' s spoile r serv o actuator s for

lef t win g rol l spoiler s thre e an dfive are i n th e maintenanc e mod e th e aircraf t i s no t i nasaf e conditio nfor

flight. Response : W e objec t

t o thi s reques t

for admission s i nthat

i t seek s anopinio nabou t

safet y that woul drequir e detaile dengineerin g analysi s usin g engineerin g dat athat i s no t i nth e possessio n o f US A 3000 , an dtha t

suc ha nanalysi s woul dconstitut e anundu e burden . Followin g reasonabl e inquiry , thi s i s reques t

i s Denie dfor

lac k o f knowledge . 3 . Whe nth e aircraft' s spoile r serv o actuator s for

lef t win g rol l spoiler s thre e an dfive are i n th e maintenanc e mod e th e aircraf t doe s not conformt o it s typ e certificat e and/o r typ e design . Response : Denie d

### 4 . Whe nth e aircraft' s spoile r serv o actuator s for

lef t win g rol l spoiler s thre e an dfive are i n th e maintenanc e mod e th e aircraft' s lef t an drigh t win g rol l spoiler s thre e an dfive ar e inoperative . Response : Denie d 5 . Whe nth e aircraft' s spoile r serv o actuator s for

lef t win g rol l spoiler s thre e an dfive are i n th e maintenanc e mod e th e symmetrica l spoile r surface s thre e an dfive ar e inoperative . Response : Admitte d 6 . Pursuan t

t o th e US A 300 0 Airline s Minimu mEquipmen t Lis t th e aircraf

t canno t b e dispatche dwhe ntw o pai r o f symmetrica l spoile r

surface s thre e an dfive ar e inoperative . Response : Admitted . 7 . Page s 2-27-1 0 an d2-27-1 1 o f th e US A 300 0 Airline s Minimu mEquipmen t Lis t provid e informatio na s t o th e condition s unde r whic hth e aircraf

t canb e dispatche dwhe non e o r mor e o f th e spoiler s i s inoperative . Response : Admitte d 8 . Page s 2-27-1 0 an d2-27-1 1 o f th e US A 300 0 Airline s Minimu mEquipmen t Lis t do no t identif y an y condition s unde r

whic hth e aircraf

t ca nb e dispatche dwhe nlef t win g spoiler s thre e an dfive ar e inoperative . Response : Admitte d 9 . Page s 2-27-1 0 an d2-27-1 1 o f th e US A 300 0 Airiine s Minimu mEquipmen t Lis t d o no t identif y an y condition s unde r

whic hth e aircraf

t ca nb e dispatche dwhe ntw o pai r o f symmetrica l surface s 3 an d5 ar e inoperative . Response : Admitte d

### 10 . Th e aircraf t i s not i naconditio nfor

saf e operatio nwhe nlef

t win g an drigh t

win g rol l spoiler s No . 3 an dNo . 5 , ar e inoperative . Response : W e objec t

t o thi s reques t

fo r admission s i ntha t

i t seek s a nopinio nabou t

safet y that woul drequir e detaile dengineerin g analysi s usin g engineerin g dat atha t i s not i nth e possessio n o f US A 3000 . Th e requiremen t t o performsuc hdetaile dengineerin g analysi s usin g engineerin g dat atha t i s not i nth e possessio no f

US A 300 0 woul db e overl y burdensome . Withou t waivin g thi s objection , an dfollowin g reasonabl e inquiry , thi s i s reques t i s Denie dfor

lac k o f knowledge . 11 . Durin g th e flight, but

prio r t o takeoff

, th e ECA M indicate do nmor e tha non e occasio n that th e followin g win g rol l spoiler s wer e not operationa l and/o r

wer e locke dout : lef

t win g rol l spoile r No . 3 ; lef

t win g rol l spoile r

No . 5 ; righ t

win g rol l spoile r

No . 3 ; an dright

win g rol l spoile r No . 5 . Response : W e objec t

t o thi s reques t

fo r admissio no nth e ground s that thi s i s acompoun d statement . Withou t

waivin g thi s objection , paragrap h1 1 i s admitte di npart , t o th e exten t that suc hawarnin g was visibl e o nth e ECA M durin g eac hres t o f th e spoile r

elevato r computers , bu t denie di npart , i ntha t

th e warnin g wa s cleare dan dreasonabl y deeme db y th e flight cre w t o b e spurious , s o i t

di dno t indicat e aproblem . 12 . A t al l time s durin g th e flight th e aircraf

t was o nth e operation s specification s o f Brendan Airways , LL C d/b/ aUS A 300 0 Airiines . Response : Admitte d 13 . Brenda nAirways , LL C d/b/ aUS A 300 0 Airline s exercise doperationa l contro l over th e flight. Response : Admitte d 14 . A t th e tim e o f

th e flight Brenda nAirways , LL C d/b/ aUS A 300 0 Airline s wa s leasin g th e aircraf t fromInternationa l Leasin g Financ e Corporatio n(ILFC) . Response : Admitte d

### 15 . A t th e tim e o f

th e flight Brenda nAirways , LL C d/b/ aUS A 300 0 Airlines ' leas e o f th e aircraf t was nearin g it s en dan dth e flight wa s undertake na s part

o f th e proces s o f

th e aircraf

t bein g transferre dint o th e possessio no f ane w lessee . Response : W e objec t

t o thi s reques t

for admissio no nth e ground s tha t thi s i s acompoun d statement . Withou t

waivin g th e objection , th e reques t i s admitted . 16 . Th e ne w lesse e i s th e ai r carrie r State Transport

Compan y Russi a(STCR) . Response : W e objec t

t o thi s reques t

for admissio no nth e ground s tha t i t i s vague . Withou t waivin g th e objection , i f

th e reques t

i s referrin g t o th e ne w lesse e o f th e aircraft , the nth e reques t i s Admitted . 17 . Th e flight

wa s considere da"maintenanc e acceptanc e flight". Response : Admitte d 18 . Prio r t o th e flight, th e livery o f th e ne w lesse e (STCR ) wa s painte do nth e aircraft . Response : Admitte d 19 . Pursuan t

t o th e term s o f

th e Brenda nAirways , LL C d/b/ aUS A 300 0 Airline s leas e with ILF C th e aircraf

t wa s require dt o b e repainte dbefore th e aircraf t lef t th e possessio no f

Brendan Airways , LL C d^/ aUS A 300 0 Airiines . Response : Admitte d 20 . Th e spoile r

serv o actuator s for

lef t win g rol l spoiler s thre e an dfive wer e put i nth e maintenanc e mod e durin g th e proces s o f paintin g th e aircraf

t withlivery o f

th e ne w lesse e (STCR) . Response : Followin g reasonabl e inquiry . Responden t i s unabl e t o Admi t

o r Den y thi s statemen t becaus e Responden t

ha s n o specifi c knowledg e o f whe nth e spoile r

serv o actuator s for

lef t win g rol l spoiler s thre e an dfive wer e pu t i nth e maintenanc e mode . Discover y fromthir dpartie s int o th e factua l basi s o f thi s statemen t

i s ongoing .

### 21 . Th e aircraf t wa s painte dwithth e livery o f th e ne w lessee , (STCR) , b y AA RAircraf t Services . Response : Followin g reasonabl e inquiry . Responden t i s unabl e t o Admi t

o r Den y thi s statemen t becaus e Responden t

ha s n o specifi c knowledg e o f wh o painte dth e livery o f th e ne w lessee , (STCR ) o nth e aircraft . Discovery fro mthir dpartie s int o th e factual basi s o f thi s statemen t

i s ongoing . 22 . AARAircraf

t Service s i s arepai r

statio nthat

i s th e holde r

o f anFA A Ai r

Agenc y Certificate qualifyin g i t

t o conduc t

operation s unde r

Part 14 5 o f th e Federa l Aviatio n Regulations . Response : Admitte d 23 . Prio r t o th e flight, Brenda nAirways , LL C d/b/ aUS A 300 0 Airline s hire dAARAircraf t Service s t o performmaintenanc e o nth e aircraf t s o a s t o allo w i t

t o b e returne dt o aconditio n that woul dpermi t

i t t o b e returne dt o ILFC . Response : Admitte d 24 . Pursuan t

t o th e manual s o f

Brenda nAirways , LL C d/b/ aUS A 300 0 Airline s paintin g th e aircraf t coul di nsom e case s requir e that th e spoile r

serv o actuator s for

spoiler s thre e an dfive b e put i nth e maintenanc e mode . Response : Denie d 25 . If th e aircraft' s ECA M syste mi s workin g properl y i t wil l repor t

tha t lef t an drigh t win g rol l spoiler s thre e an dfive ar e inoperativ e whe nth e spoile r serv o actuator s fo r

lef t win g rol l spoiler s thre e an dfive ar e place di nth e maintenanc e mode . Response : Denie d 26 . A t n o tim e subsequen t

t o th e flight

di da ninspectio no f

th e ECA M syste mrevea l that ther e was aproble mwit hth e syste mtha t coul dhav e cause di t

t o malfunctio njus t

prio r t o takeof f durin g th e flight. Response : Admitte d

### 27 . Withi ntw o day s after th e flight th e spoile r

serv o actuator s o nlef

t win g rol l spoiler s thre e an dfive wer e agai nput

i nmaintenanc e mod e t o se e wha t message s woul dappear

o nth e ECA M an dth e ECA M reporte dtha t lef t an drigh t win g rol l spoiler s thre e an dfive wer e inoperable . Response : Admitte d 28 . Durin g th e flight

an dprio r t o takeof f th e pilot s aboar dth e aircraf t faile dt o complet e a successfu l flight

contro l check . Response : Denie d 29 . Durin g th e flight

an dprio r t o takeof f th e pilot s aboar dth e aircraf t faile dt o complet e a successfu l flight

contro l chec k

becaus e i t

wa s impossibl e for

th e spoiler s t o hav e reacte di n respons e t o input s fromth e cockpit . Response : Denie d

RESPECTFULL Y SUBMITTE D thi s 22n dday o f July , 2010 . WASHINGTO NAVIATIO NGROUP , P C AN D TH E LA WOFFICE S O FJASO NA . DICKSTEI N

Jaso n Dickstei n Wa^ingto nAviatio nGroup , P C an dth e La w Office s o f

Jaso nA . Dickstei n 223 3 Wisconsi nAvenue , NW , Suite 50 3

Washington , D C 2000 7 Tel : (202 ) 628-677 6 Attorne y for

Responden t

Brenda nAirways , LL C d/b/ aUSA300 0 Airline s

### BEFOR ETH EU.S . DEPARTMEN T O FTRANSPORTATIO N The Honorabl e Chie f

Administrativ e Law Judg e Ronnie A . Yode r I n th e matte

r o f BRENDA

N AIRWAYS , LLC , d^/aUSA300 0 Airline sResponden t DMS No. : FAA-2009-003 2 FA A Docket No. : CP09EA0007 FA A Cas e No. : 2008EA17003 8 RESPONS E T O COMPLAINANT' S FIRS T SE T O FINTERROGATORIES , REQUES T FO RADMISSIONS , AN D REQUES T FO RPRODUCTIO N O F

DOCUMENT S Th e undersigne dhereb y certifie s tha t sh e cause dth e attache d

• RESPONS ET O COMPLAINANT' S FIRS T SE T O F INTERROGATORIES , REQUES T FO RADMISSIONS , AN D REQUES T FO RPRODUCTIO NO FDOCUMENT S T o b e filedat

th e addresse s liste dbelo w b y overnigh t FedE x service , o n th e dat e indicate d below . Federal Aviatio nAdministratio n(fOeiGrlMA b ^M ^ °^ ^ COP^ ) ^ ^ 60 0 Independenc e Avenue , S W Wilbu r Wrigh t Buildin g - Suit e 2W100 0 Washington , D C 2059 1 Attn : Hearin g Docke t

Clerk , AGC-43 0 An dt o b e serve do n th e person s at th e addresse s liste dbelo w b y th e sam e metho da s th e filing method , o n th e dat e indicate dbelow . Davi dM . Cohen , Attorne y Federa l Aviatio nAdministratio n Offic e o f th e Regiona l Counsel , EAL- 7 1 Aviatio nPlaz a Jamaica , N Y 1143 4 Tel : (718 ) 553-327 0 Fax (718 ) 995-569 9 Th e Honorabl e Ronni e A . Yode r Chie f Administrativ e La w Judg e Offic e o f Hearings , M-2 0 Roo mEl2-32 0 U S Departmen t

o f Transportatio n 120 0 Ne w Jerse y Avenue , S E Washington , D C 2059 0 Tel : (202 ) 366-214 2 Fax : (202 ) 366-753 6

Katt Stanle y Date ' 

## 0

# C j f • ^f<-J ^ f . k 

# ^VSA300 0 AIRLINE S



## June 11 , 200 8 Laurenc e Johnso n Principa l Operation s Inspector

- USA3000 Philadelphi aFSDO-1 7 2 Int' l Plaza , Suit

e 11 0 Philidelphia , P

A 1911 3 Dea r Mr . Johnson , RE : LO I Fil e Numbe r

2008EA17003 8 an dVDRPReferenc e ID : 264 9 O nMa y 30,2008 , yo u sent

USA300 0 Airline s aLetter o f Investigatio n(LOI ) concerning th e maintenanc e acceptanc e tes t flight o f Brenda nAirway s L.L.C , db aUSA3000 Airline s aircraf

t N265AV , a

t MIA , o nMa

y 17,2008 . O

nJun e 4,2008 , you sen

t alette r t o Willia mHoffinan , USA3000 Airiine s Director o f Qualit y Control , acceptin g aVDR P wit hth e conditio nth e acceptanc e onl y relate dto th e maintenanc e aspect s o f th e tes t flight. Thi s reply t o th e LO I refer s onl y t o th e operation' s aspect s o f th e tes t flight. Thi s commentar y i s base do nth e Pilo t Safet y Reports , th e repor t

th e Directo r

o f Maintenanc e & Engineerin g gav e t o th e FAA o nMa y 19,2008 , conversation s wit h Jo e MiUer , Directo r

o f Maintenanc e & Engineerin g an dCaptai nSurrat t o nJun e 1 0 2008 , AIRBU S Industrie s an dUSA300 0 Airline s manuals , an dvariou s dat a downloads . USA300 0 Airiine s i s providin g t o yo u al l o f th e information , data , an d documentatio nwit hthi s lette r tha t i t ha s t o date . An y additiona l informatio ntha t come s t o ligh t

o r i s discovere dwil l b e forwarde dt o you r offic e a s soo na s possible . OnMa y 17,2008 , USA300 0 Airline s conducte daMIA-MIA , Par t 9 1 maintenanc e acceptanc e tes t

fligh t inpreparatio nfo

r returnin g MS N42 7 t o th e lessor . Internationa l Leas e Financ e Corp . Ehuio g th e flight contro l check

durin g th e taxi checklist , th e crew notedther e wa s a nECA M cautio no f

LAFDEGRADED . I t

wa s cleare db y resettin g the Spoile r Elevator Compute r (SEC ) pushbuttons . Accordin g to bot hCaptainSurrat

t and Jo e Miller , thi s cautio ni s no t un-common , andquickly cleared . The aircraf t ha daclea n uppe r ECA M pag e prio r

t o th e uneventful takeoff

. Whil e airborne , during routine pag e call-ups , th e ECA

M pane l displaye dsymmetrical , spoiler 3/ 5 L/ Rambe r indications . During th e fligh

t apilot , fromth e next

leasin g airline , lef

t th e cockpit

andreturne dnoting 33 5 Bisho p Hollo w Road , Suit e 10 0 Newtow n Square , P A 1907 3 Phone : 610.325.128 0 Fa x 610.325.128 5

### tw o spoiler s o nth e lef t win g wer e floating . A nUSA300 0 Airline s inspection' s employe e too k som e picture s o f

thos e spoiler s (photos , attachmen t 1) . Durin g th e flight , th e pilot s note dth e rudde r

tri mgoin g ou t

o f limits . Captai nWalke r

diseng^e dth e autopilo t an d manuall y trimme dth e aircraft . O n^proach . Captai nWalke r state dth e aircraf

t fel t "sloppy. " I nth e flare , th e aircraf t droppe dabruptly , bounce dan drolle dleft . Th e cre w initiate dago-aroun dan dfle w asecon dapproac hat Flap s 3 an dVREF+2S . O n th e secon dlandin g approach , o ntouchdown , th e aircraf t trie dt o rol l lef

t ^ai nbu t

wa s controllabl e t o alanding . After landing , i t

wa s discovere dtha t

aportio no f

lef t wingti p fenc e wa s groun doff . Repai r cos t i s abou t $33,00 0 (photos , attachmen t 2) . Th e initia l revie w o f

th e aircraf

t after landin g (wit hAA RService s personne l involved ) foun dspoiler s 3/ 5 o nth e lef t win g t o b e i n'Maintenanc e Mode' . Jo e Miller , USA300 0 Airline s Directo r

o f Maintenanc e & Engineering , w4io wa s aboar dth e flight, formall y requeste da nmvestigatio nb y AA RService s a t tha t tim e (Jo e Mille r

email , attachmen t

3) . O nMa y 19,2008 , Mr . Mille r provide dth e MI A FA A awritte nstatemen t (Jo e Mille r Memo , attachmen t

4) . Mr . Mille r

directe dth e digita l fligh t dat arecorde r

b e remove dan d quarantined . Th e DFD Rwa s sen t t o Honeywel l fo r

downloa dan danalysis . O nMa y 18,2008 , Ti mLyons , USA300 0 Airline s Chie f Pilot , spok e t o bot hpilots . O n Ma y 19,2008 , Jo e Guhin , USA300 0 Airline s Directo r o f Safety an dRegulator y Compliance , calle dbot hpilot s an ddirecte dsafety report s b e submitte d(Surratt Report , attachmen t

5 , Walke r

Report , attachmen t

6) . O nMa y 19,2008 , Jo e Guhi ncalle dth e Nationa l Transportatio nSafety Boaixl (NTSB ) Operation s cente r

an dspok e t o th e investigato r o nduty , Joh nLovell . Mr . Guhi n provide dth e essentia l informatio no f who , what , when , v^er e an dth e estimate dcos t Mr . Lovel l requeste dphoto s o f tbti damage , vMc hwer e emaile do nMa y 19,200 8 (attachmen t

2) . O nMa y 20,2008 , Mr . Lovell , vi aemail , wa s aske dan dconcurre dtha t th e NTS B ba dn o furthe r interes t i nth e even t

an dauthorize dreleas e o f th e flight dat a recorde r (email , attachmen t

7) . O nMa y 19,2008 , Th e FA A requeste dUSA300 0 Airline s se t aircraf t N265A V i nth e sam e configuratio na s i t

wa s prio r

t o th e tes t

flight o nMa y 17,2008 , (spoiler s 3/5 o n th e lef t win g i nmaintenanc e mode ) an dtak e apictur e o f th e ECA M faul t

panel . Th e phot o wa s emaile dt o th e FA A o nMa y 20,2(X) 8 ^hot o an demail , attachmen t 8) . O nMa y 22,2008 , Jo e Guhi naske dth e pilot s agai nt o submi t detaile dsummaries . O n May 23 , Jac k

Eastman , th e USA3000Airline s Directo r o f Operations , wa s calle db y an attorne y fo r

th e Internationa l Brotfaeiiioo do f Teamsters , Loca l 747 , tha t represent s th e pilot s i nth e emplo y o f

USA300 0 Airlines . Mr . Eastma nwa s advise dtha t th e effor t t o obtai nadditiona l informatio nwa s bein g considere dharasanen t b y th e Union . O n Jun e 10,2008 , Jo e Guhin , USA300 0 Airline s Directo r o f Safety an dRegulator y Compliance , spok e t o Jo e Miller , USA300 0 Airiine s Directo r o f Maintenanc e an dEngineering , v/h o

## provide dadetaile dsynopsi s of th e flight , an dhi s rationa

l o nwh y th e aircraf

t wa s saf e t o launch , fromhi s viewpoin

t inth e jtmi p seat . On1 0 June 2008 , Jo e Guhinspok e t o Captai nSuiratt , who provide daseparate andsunila r descriptio nandrationa

l o nprefligh

t indication s andfo

r feeling th e aircraf

t wa s saf e t o launch . Attachment

9 i s th e Aircraf

t Lo g sheet , (For

mM-3 ) fo r th e flight . Attachment

1 0 i s th e AIM S printout s fo r Pilot s Surrat

t an dWalke r showing the y wer

e schedule dfo

r th e flight . Attachment

1 1 i s aphoto o f

ECA M flight contro l displa

y wit hnorma l indications . Attachment

1 2 i s atrainin g documen

t pag e of th e ECA M F/CT Ldisplay , wit

ha n explanatio no f

th e displa y Attachment

1 3 i s a nFCOM pag e wit

halegen do f

th e color code s o nth e display s Attachment

1 4 i s aprint

out o f aportio no f

th e Pos t FUgh t Repor t (PFR) o f th e tes t flight showin g th e time o f

th e ECA M fault displays . Jo e Miller , commentedtha t th e F/CT L SPL Rfault s will b e momentar

y whenth e SEC pushbutton s ar e reset . Attachment

14 aare Airbu s TS M Manua l page s relate dt o th e LA

FDEGRADE

D fault . Attachment

1 5 i s th e FCOM pag e fo

r F/CTLSEC 1 (2 ) (3 ) Fault . Attachment

1 6 i s th e FCOM pag e fo

r F/CTLSPL

RFault . Attachment

1 7 i s th e FCOM pag e fo

r LA FACC U Fault . Attachment

1 S are trainin g document

page s fo r spoiler s an

dth e ECA M F/CT Ldisplay . Pag e on e ha s th e statement tha t whenon e spoiler

smfac e fails , th e symmetri c one onth e other win g i s inhibited . Attachment

1 9 are FCO M page s o f

warnin g an dcaution s fo

r Aircraf t N265AV . Attachment

20 i s a nFCOM pag e o n"SPEE D BRK " mem o displa y logic . Attachment

2 1 are page s fromth e USA300 0 Airline s Minimu mEquipmen

t Lis t (MEL) , Chg 22 , concernin g spoiler surfac e malfunctions . (Chang e 2 2 i s provided . Chang e 2 3 i s th e current

editio nanddoe s no t

include guidanc e onN265AV) . Attachment

2 2 i s th e A32 0 Expande dTAX I CheckUst

fromthe FCOM . Pag e 2 describe s th e flight contro l check .

## Attachmen t 2 3 i s subject

flight DFD Rtabula

r dat afo r commandstick

andflight

contro l position s during th e flight

contro l tes t

(1718:1 8 to 1719:3 8 UTC) . Th e DFDRdatadid no t hav e readout s o f

th e ECA M pane l displa

y indications . Attachmen

t 2 4 i s aflightaware.com, minute-by-minute , reca p o f position , speedand altitude of th e maintenanc e tes t

flight. O nMa y 30,2008 , Larr

y Johnso ninformedJo e Guhi nthat Pilo t Walke r wa s inth e lef

t sea t andwh y wa s PIC Surrat

t no t inth e lef t sea t andflying? Afle

r conferring wit

hChief Pilo t TimLyons , Jo e replie dvi aemail tha t Pilo t Walke r wa s Captainqualifie d(email , attachmen t 25) . Attachmen

t 2 6 i s acop y o f

th e FAA approve dUSA300 0 Airline s NORMA L CHECKLIS T If you hav e an

y question s o nthi s package , pleas e contac t me a t (610 ) 325-128 9 o

r at jguhin@usa3000.co m JosephM . Ouhin Director of Safet y & Regulator

y Complianc e USA3000 Airline s (610 ) 325-128 9 iguhin(a).USA3000.co

m Attachments : 1 . Photo s o f

lef t wii\g spoiler s floating 2 . Photo s o f

damagedwin g fenc e 3 . Email fix)mJo e Miller t o AARService s 4 . Jo e Miller

incident Memo t o MI

A FA A 5 . Safet y Report , Pilo t

Surrat t 6 . Safet y Report , Pilo t

Walke r 7 . Email fromNTS B releasin g DFD R 8 . Email & Photo o f

N265AV ECA

M panel wit

hspoiler fault s 9 . Lo g page , N265AV , Ma y 17,200 8 10 . AIM S schedul e pag e fo r Pilot s Surrat

t andWalke

r 11 . Phot o o f ECA M flight contro l pag e wit

hnorma l indication s 12 . ECA M F/CT Ldispla y legend 13 . ECA M color cod e legen d 14 . N265AVPFR,Mayl7,200 8 14 aAirbu s TS M Manua

l page s relate dt o th e LA

FDEGRADE

D faul t

## 15 . FCOM pag e fo r F/CT LSEC 1 (2 ) (3 ) Fault 16 . FCOM pag e fo

r F/CT LSPL RFault 17 . FCOM pag e fo

r LAFACC U Fault 18 . Trainin g doctmien

t page s fo r spoiler s andth e ECA

M F/CT Ldispla y 19 . FCOM page s o f

warnin g an dcaution s fo

r Aircraf t N265A V 20 . FCOM pag e o n"SPEED BRK " memo displa y logi c 21 . USA3000Airline s MEL , Chg 22 , spoiler surfac e malfunction s 22 . A32 0 TAX

I Checklist , fiwmth e FCOM 23 . DFD Rtabula

r dat afo r th e fligh t contro l check 24 . flightaware.com, flight reca p 25 . Emai l o nPilo t

Walke r bein g inlef

t sea t 26 . U S A 3 00 0 Airline s Normal Checklis t - pag e 7.0 1Josep h T o laurence.johnson@faa.gov GuhinAJSA3000/KCDAT A. ^ ^ ^ . „.^».,„^„^^».r»>=x..^rv., . , ccJosep h Guhin/USA3000/KCDATA@KCDATA , Ti m 06/03/200 8 12:3 1 P M Lyon8/USA3000/KCDATA@KCDATA . Jac k EastmanAJSA3000/KCOATA@KCDAT A bcc Subjec t MI A1 7 May , Pilot s i n Seats Goo d Afternoo n Larry . Yo u tol d m e las t wee k

abou t Pilo t Walke rbein g i n th e lef t sea t an d Pilo t Surrat t i n th e right sea t Yo u aske d i f tha t wa s norma l fo ra tes t flight. I discusse d th e issu e wit h Ti m Lyons . H e informe d m e tha t Pilo t Walke ri s Captai n qualifie d an d onl yo n F O statu s du e t o th e manpowe rrequirements o f th e company . USA300 0 i s intentionall ymaintainin g hi s lef t sea t currenc yt o allo wa instan t transitio n t o Captai n statu s whe n manpowe rneed s require . Jo e Guhi n Directo ro f Safet y& Regulator yComplianc e US A300 0 Airline s 33 5 Bisho p Hollo wRoa d Newtow n Square , P A1907 3 Phone : 610.325.128 9 Cell : 610.850.434 7 Fax : 610.356.793 6 Jguhin@usa3000airlines.co m

/ / /

# US A 300 0 I N

Jun e 13,200 8 Josep hGuhi n Directo r o f Regulator y Complianc e US A 300 0 Airline s Joe , SUBJECT : LO I FIL ENUMBE R2008EA17003 8 AN D VDR PID : 264 9 Furthe r t o ou r conversatio n o f

thi s dat e an di n a nattemp t t o provid e additiona l insigh t int o th e event s surroundin g th e Maintenanc e Acceptanc e Fligh t o f N265A V o f

1 7 Ma y 2008 , pleas e findbelo w areiteratio n o f m y memor y o f

th e event . Prefligh t check s wer e complete dwithou t incident . Aut o engin e start s wer e complete dwithou t incident . Pos t star t check s wer e complete dwithou t incident . Tax i check s wer e complete dwithou t incident . Durin g performanc e o f

th e fligh t

contro l check , th e Lowe r ECA M Fligh t

Contro l syste mpag e appeare dan dLA F DEGRADE D advisor y wa s displayed . I recal l n o Uppe r ECA M warnings . Afte r abrie f discussio n o nth e lengt ho f tim e th e aircraf

t ha dbee nou t

o f servic e an dth e norma l 'gremlins ' o f no t bein g powere dfo r

mos t o f th e pas t 4 5 day s w e proceede dt o rese t th e SE C computer s (durin g whic htim e ther e wer e momentar y transitor y faults , whic har e indicate db y th e Pos t Fligh t Repor t (PFR)) . Afte r

rese t th e LA FDEGRj-\DE D advisor y messag e disappeare dan dthe nafte r afe w second s reappeared . Th e SEC' s wer e rese t agai n (whic hagai ntriggere dmomentar y transitor y fault s o nth e PFR ) an dth e advisor y disappeare dan d di dno t return . Thes e reset s sho w a s tim e stamp s 1718-172 0 Fligh t Phas e (PH ) 02 . Durin g th e clim b t o FL31 0 aserie s o f test s wer e t o b e performe di naccordanc e wit hth e Airbu s Singl e Aisl e In-Servic e Aircraf

t Fligh t Tes t profile . Durin g thes e test s ther e i s asectio no nflight contro l authorit y checks . Durin g thi s proces s w e note dth e L.A. FDEGRADE D advisor y messag e an dspoiler' s 3 an d5 lef t an dright showin g ambe r

o nth e FL T CTR Lsyste mpag e an dth e SE C rese t wa s performe dagai n(tim e stam p 173 2 P H 06) . Th e LA FDEGRADE D advisor y an dspoile r 3/5 , L/ Rambe r

remained . Th e flight

continue dwit hvariou s relate d(F/CT LSPL RFAUL T a t 1951/195 2 whe ntestin g hydrauli c pump s affectivit y an dPowe r

Transfe r Uni t operation ) an dunrelate dfault s bein g triggere ddu e t o testin g and/o r actua l faults . Durin g th e lo w spee d'un-clean ' (flap s no t fuU y retracted ) test s th e cre w note dth e sli p indicato r o n th e Primar y Fligh t

Displa y an da nunusua l rudde r trim . Th e auto-pilo t

(AP ) wa s selecte dOFF , rudde r tri mreset , an dth e A Pwa s selecte dbac k ON . Afte r

som e tim e ha dpasse dth e cre w agai nnote dth e rudde r trim , selecte d A POF Fan dhan dflew th e remainde r o f th e fligh t

u p t o th e approach . Th e Quic k

Referenc e Handboo k

wa s reference dfo r

th e limitation s o f

spoiler s 3 an d5 (L/R ) inoperativ e (whic hwer e actuall y foun di nadua l hydrauli c failur e section ) an dw e compute dth e landin g distanc e penalt y fo r thi s condition . TTi e final step s inth e fligh t tes t require daCA T 11 1 Dua l approach , whic hw e wer e settin g u p fo r o nth e MI A 8 Rwhe nth e towe r

requeste dw e chang e t o ML \8L , whic hdi dno t hav e a nILS . W e accepte dth e runwa y change , alread y knowin g th e landin g distanc e penalty , an dproceede dt o lan do n \0 A 8L . 

## /4^ck^e^- f

i . f>'if e //» . 33 5 Bisho p Hollo w Road , Suit e 10 0 Newtow n Square , P A 1907 3 Phone : 610.325.128 0 Fa x 610.325.128 52 - Jun e 16 , 200 8

After th e attemp t

t o lando n MIA 8 Lwa s unsuccessfiil , th e cre w calle dfor GEA RUPan dFLAP S 3 . Ther e wa s abrie f

discussio na

t Mdiic hpoin t w e determine dth e aircraf t wa s flyin g well wit hFLAP S 3 , w e would procee do nth e secon dapproac hi ntha t configurario nan dou t

secon dattempt , whic hwa s t o 'MI A 8R , wa s successfiil . Upo n deplanin g w e note dth e damag e t o th e lef t win g tip . Regards , 

# ino A J^MiUe r Directo r o f Maintenanc e & Engineerin g US A 300 0 Airline s A . Kinnea

r J . Eastma n WHoffma

n T . Lyon s



# ^EUS A

# 300 0 I NUN i TE D STATl- S 01 - A.VI1;KIC A NATION.A LTR.\NSPORTATIO N SAII H Y HOARI. ) Ul-Tl i I O FADMINiSTK.MIVI" . 1 A W.1 1 'DGF S RAND Y BABBITT , Adminisirator , FA A ) DoAc LNu . SB-1856 2 an dSE-1856 3 ) .fiidi'. e h'owlv r V . ) FRAN K \VILI,IA.\ 1 WAI,KE R an d TON Y SCOTSURRAT r ) ) ) ) Respondents )

) DAVI D BEAL' S

FIRS T DECLAIMTIO N

( i 1 , DAVI D BLAL , unde r penalt y of"perjury , tleel.ir e a s loilows : 8 1 . 1 a maLin e Ivnginec r wit hBrenda nAirways , whic hdoe s busines s unde r ^ > th e trad e nam e US A ."^OOO . 1 0 2 . O nMa y 17 , 2008 , I V\M S presen t o nth e maintenanc e acceptanc e fligh t o f 1 1 th e aircraf

t bearin g U S registr y N265A V (tii c Aircrait) , ou t o f .VIIA . I 2 .3 . Severa l day s afte r tha t fligiit , i wa s aske dt o lak e picture s o f th e EC.^ M o f I ' ^ tliat aircraf t ba.se dupo n certai ninsl i uciions . 1 ^ 4 . 1 too k apictur e o f

tli c ECA M wil l al l spoiler s operational . I^ 5. 1 the nse t spoiler s 3 an d5 i nmaintenanc e mode , an dtoo k apictur e o f

th e 1 6 ECA M unde r

thos e conditions . 1 7 6 . I followe dappropriat e maintenanc e instruciion s an dprotocol s whe nI .se t I S th e .spoiler s i nmaintenanc e mode . 1' ' 7 . I wa s no t in.structc dt o recreat e al l o f th e condition s o f

th e Ma y 1 7 (light . 2 0 8 . Whe n1 too k th e pictures , 1 di dno t recreat e al l o f

th e condition s o f

th e 2 1 Ma y 1 7 night . DAVI D BE.^L' S FIRS' I DLCLAR A IIO N WasliinglonAviatio nGroup , P C an dtlic La w Oftlee s of

Jaso n.A . Dickstein 2?..'5 3 WisconsinAvenue . NW

, Suit e 50 3 

## \Vajii)i;.i.ji, . o r

7,nno 7 - TI : -xnc^z-^^ u

### 2 2 9 . i"l) e picture s that

1 too k were no t intende dto , an dd o not , relie dth e 2. 5 condition s o f

th e aircraf

t o n Ma y 1 7 . ? A 10 . I declar e unde r penalty o f

perjury unde r

th e (aw s o f

th e Unite dState s tha

t 2. S th e foregoin g i s tru e an dcorrect . 2 6 27 EXEC U TE D o n th e day o f

.Uily . 2009 . 2: { 

### ?.' )

DAVI D BEA L

DAVI D IJLAL' S FIRS T DLCLARATIO N Washingto n Aviatio n Group , P C an dth e La\ v Office s o f

Jaso n;\ . Dickstei n 223 3 Wisconsi nAvenue , XW , Suit e .503 Wai.liiiiiilon , D C ^000 7 • TJ : .'02-i',2^^ W

### US A300 0 AIRLINE S CHAPTE R 2 : MINIMU M EQUIPMEN TLIS T SECTIO N 2 7 FLIGH TCONTROL S 

### MINIMU M EQUIPMEN TLIS T Revision : 1 2 Ma y1,200 5 SYSTE M & SEQUENC E NUMBER S 2 7 FLIGH TCONTROL S 64-0 1 SPOILE R SURFACE S 1 (N265A

V Only) LITE M

C

C

C 2 . NUMBE R INSTALLE D

1 0

1 0

1 0 3 . NUMBE R REQUIRE D FO R DISPATC H

8

8

8 4 . REMARKS O R EXCEPTION S

(M ) (0 ) On e pai rof symmetrica l surface s 1o r3 ma yb e inoperativ e i n th e retracte d positio n provide d a ) SEC s associate d wit h operative spoilers operat e normally , an d b ) AF M perfomianc e penaltie s are applied . (M ) (0 ) On e pai ro f symmetrica l surface s 5 ma yb e inoperativ e i n th e retracte d positio n provide d SEC s associate d wit h operative spoilers normall y (M ) (0 ) On e pai ro f symmetrica l surface s 2 o r4 ma yb e inoperativ e i n th e retracte d positio n provided : a) SEC s associate d positio n wit h operativ e spoiler s operat e normally , an d b ) SFC S 2 fla p channe l operate s normally , an d c ) AF M performanc e penaltie s ar e applied . (Continued )



### 2-27-1 0

### USA300 0 AIRLINE S CHAPTE R 2 : MINIMU M EQUIPMEN TLIS T SECTIO N 2 7 FLIGH TCONTROL S 

### MINIMU M EQUIPMEN TLIST Revision : 1 2 Ma y1,200 5 SYSTE M & SEQUENC E NUMBER S 2 7 FUGH TCONTROL S 64-0 1 SPOILE R SURFACE S (CONTD ) (N265A V Only ) LITE M 2 . NUMBE R INSTALLE D

1 0

1 0 3 . NUMBE R REQUIRE D FO R DISPATC H

4 . REMARK S O R EXCEPTION S

(M ) (O ) Tw o pai ro f symmetrica l surface s 1 an d 2 ma yb e inoperativ e I n th e retracte d positio n provided : a ) SEC s associate d wit h operativ e spoiler s operat e nonmally , an d b ) SFC S 2 fla p channe l operate s normally , an d c ) AF M performanc e penaltie s ar e applied . (M ) (O ) Tw o pai ro f symmetrica l surface s 3 an d 4 ma yb e inoperativ e i n th e retracte d positio n provided : a ) SEC s asscjciate d wit h operativ e spoiler s operat e normally , an d b ) T R 1 an d T R 2 operat e nonnally , c ) D C Ti e Contracto r1 i s verifie d ck}se d befor e eac h departure , d ) SFC S 2 fla p channe l operate s normally , an d e ) AF M performanc e penaltie s ar e applied . NOTE : I f spoile r4 o r5 i s inoperative , LA F

i s i n degrade d mode . Refe rt o 27 - 64-02 , (Continued )



### 2-27-1 1

### USA300 0 AIRLINE S CHAPTE R 2 : MINIMU M EQUIPMEN TLIS T 

### SECTIO N 2 7 FLIGH TCONTROL S 

### MINIMU M EQUIPMEN TLIS T Revision : 1 9 Apri l 18 . 200 7 SYSTE M & SEQUENC E NUMBER S 2 7 FLIGH TCONTROL S 64-0 1 SPOILE R SURFACE S (CONTD ) (N260AV-N264AV , N266AV-N271A V Only ) 1 . ITE M

C

C

C 2 . NUMBE R INSTALLE D 1

1 0

1 0

1 0 3 . NUMBE R REQUIRE D FO R DISPATC H

8

8

8 4 . REMARK S O R EXCEPTION S

(M ) (O ) On e pai ro f symmetrica l surface s 1 o r3 ma yb e inoperativ e i n th e retracte d positio n provided : a ) SEC s associate d wit h operativ e spoiler s operat e normally , an d b ) AF M performanc e penaltie s ar e applied . (M ) (0 ) On e pai ro f symmetrica l surface s 5 ma yb e inoperativ e i n th e retracte d positio n provide d SEC s associate d wit h operativ e spoiler s operat e normally . (M ) (O ) On e pai ro f symmetrica l surface s 2 o r4 ma yb e inoperativ e i n th e retracte d positio n provided : a ) SEC s associate d wit h operativ e spoiler s operat e nomially , an d b ) SFC S 2 fla p channe l operate s nomnally , an d c ) AF M performanc e penaltie s ar e applied . (Continued )



### 2-27-1 2

### USA300 0 AIRLINE S CHAPTE R 2 : MINIMU M EQUIPMEN TLIS T SECTIO N 2 7 FLIGH TCONTROL S 

### MINIMU M EQUIPMEN TLIS T Revision : 1 9 Apri l 18,200 7

SYSTE M & SEQUENC E NUMBER S 2 7 FLIGH TCONTROL S 64-0 1 SPOILE R SURFACE S (CONTD ) (N260AV-N264A V N266AV-N271A V Only )

64-0 2 LOA D ALLEVIATIO N FUNCTIO N (LAF ) (N265AV ) LITE M

C

C

D 2 . NUMBE R INSTALLE D 1

1 0

1 0

1 3 . NUMBE R REQUIRE D FO R DISPATC H

6

6

0 4 . REMARK S O R EXCEPTION S 1

(M ) (0 ) Tw o pai ro f symmetrica l surface s 1 an d 2 ma yb e inoperativ e i n th e retracte d positio n provided : a ) SEC s associate d wit h operativ e spoiler s operat e nonnally , an d b ) SFC S 2 fla p channe l operate s nomnally , an d c ) AF M perfonnanc e penaltie s ar e applied . (M ) (0 ) Tw o pai ro f symmetrica l surface s 3 an d 4 ma yb e inoperativ e i n th e retracte d positio n provided : a ) SEC s associate d wit h operativ e spoiler s operat e nomnally , an d b ) T R 1 an d T R 2 operat e nonnally , c ) D C Ti e Contracto r1 i s verifie d close d befor e eac h departure . d ) SFC S 2 fla p channe l operate s normally , an d e ) AF M performanc e penaltie s ar e applied .



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# InF O Informatio nfo

r Operator s U.S . Departmen t InF O 0803 2 o f Transportatio n DATE : 5/16/0 8 Federa l Aviatio n Administratio n Fligh t Standard s Servic e Washington , D C 

### http://www.faa.gov/othe

r visit/aviatio nindustry/airlin e operators/airlin e safety/inf o A nInF O contain s valuable informatio nfo r operator s that

shoul dhel p the

mmeet certai nadministrative , regulatory , o r operationa l requirement s wit hrelativel y lo w urgenc y o r impac t o nsafety . 

### Subject : Non-Routin e Fligh t Operation s (NRFO ) Purpose : Thi s InF O provide s informatio nandguidanc e fo r conductin g Non-Routin e Flight Operation s (NRFO ) fo

r purpose s other

tha nth e transport

o f peopl e or materials , and/or

afte r performin g maintenance , preventiv e maintenance , rebuilding , o r alteratio no na

nairplane . NOTE : Thi s InF O doe s no t addres s authorizatio nfo r ferr y flight s wit hon e engin e inoperative , a s se t

fort hinTitl e 1 4 o f

th e Cod e o f

Federa l Regulation s (1 4 CFR ) par t 91 , § 91.611 , no r

doe s i t addres s tes t

o r experimenta l flights. Background : Thi s InF O ha s bee n develope di nrespons e t o National Transportatio nSafet y Boar d(NTSB ) safet

y recommendation s A-97-49 , A-97-50 , A-97-5 1 andA-97-52 . Inaddition , it supersede s Fligh t

Standard s Informatio nBulleti nfo r Air Transportatio n(FSAT ) 04-02A . OnDecember

22 , 1996 , aDougla s DC-8-6 3 airplan e impacte dterrain , killin g thre e fligh t crewmember s andthre e maintenance/avionic s technician s onboard . Afte r conductin g it s investigatio ninto thi s accident , th e NTS B identifie dth e fligh t a s aPostmodificatio nFunctiona l Evaluatio nFlight

(PFEF) . Discussion : Fo r

further discussio no f

thi s accident

andfurthe

r guidance , see : http://www.faa.gov/other

visit/aviatio nindustry/airlineoperators/airlinesafety/info/allinfos / media/2008/InFO08032Sup.pd f Recommende daction : Director s o f safet y anddirector s o f

operation s (par

t 121) ; director s o f operation s (par

t 135) ; trainin g managers ; andpilot s o f transpor t aircraf t shoul db e familia

r wit h th e content

o f thi s InFO . The y shoul dwor k together t o ensure that

th e highes t

level o f safet y i s maintaine dwhil e conductin g Non-Routin e Flight Operation s (NRFOs) .

Approve dby : AFS-20 0 OPR : AFS-22 0

### Supplemen t t o InF O 0803 2 Discussio nof

Non-Routin e Fligh t

Operation s (NRFO ) a . Reason s fo r

NRFOs . 1 . Th e affecte dfligh

t wa s conducte dfo

r th e purpos e o f

achievin g complianc e wit h1 4 CF Rpar t 43 , § 43.5 , Approval fo

r retur nt o servic e afte

r maintenance , preventiv e maintenance , rebuilding , o r

alteration . 2 . For th e purpose s o f

thi s InFO , NRFO s ar

e thos e fligh

t operation s conducte dfo

r purpose s other

thanth e ordinar

y transpor t of peopl e o r material . Fo r

ai r carriers , thi s mean s all flight s no t involvin g commo ncarriage . (a ) Example s o f

NRFOs . (1 ) In-flight

functiona l evaluatio no f

th e aircraf

t and/o r it s systems , (2 ) Engin e inoperativ e ferr y flights . (NOTE : th e guidanc e inthi s InF O i s no t applicabl e t o Engin e inoperativ e ferr y flights.)

(3 ) In-flight

operational check s o f

maintenanc e performe do r alteration(s ) made , (4 ) Flight s conducte dfo

r th e purpos e o f

crewmember

trainin g o r

qualification , (5 ) Al l operation s conducte dunder aSpecia l Flight Permit , (6 ) Maintenanc e troubleshootin g flights , and/o r (7 ) Sale s o r

custome r demonstratio nflights . (b ) Fo r ai r carriers , th e lis t

include s all fligh

t operation s no t

conducte da s par

t o f th e air carrier' s schedule do r

nonschedule dpassenger

and/o r carg o carryin g operations . b . Clarificatio no f

Existin g Regulations . There ar e numerou s section s applicabl e t o NRFOs . Thes e include : 1 . Sectio n91.3(a ) state s that "th e pilo t i ncomman do f

a n aircraf t i s directl y responsibl e for , andi s th e final authority a s to , th e operatio nof that aircraft. " Thi s make s it

critical tha

t th e pilo t i s th e final authority o nwhethe r aflight starts , continues , o

r ends , andi s responsibl e to end any suc hflight

at th e tim e th e pilo t

finds safet

y i s compromised . Therefore , th e terminatio n o f a nNRF O woul db e appropriate , eve nbefore departure , i f th e pilo t finds that th e aircraf

t i s no t airworthy . 2 . Sectio n91.7 .

### (a ) Thi s sectio nset s fort hrequirement s concernin g th e airworthines s conditio no f all civi l aircraft . Sectio n91.7(a ) state s that "n o perso nma

y operate acivi l aircraf

t unles s it i s i n a n airworthy condition. " Sectio n91.7(b ) state s that "th e pilo t incomman do f

acivi l aircraf

t i s responsibl e fo

r determinin g whether

that aircraf t i s inconditio nfo

r saf e flight. Th e pilo t

i n comman dshal l discontinu e th e flight whe nunairworthy mechanical , electrical , or structural condition s occur. "

(b ) A clarificatio no f

th e ter mairworthy i s necessar

y becaus e there i s n o definitio n o f airworthy in1 4 CFR . Th e accepte ddefinitio nfo r "airworthy " come s fro

mFAA Order

8900.1 , Flight Standard s Informatio nManagement System(FSIMS) , Volume 7 , Chapter 7 , Sectio n 1 , Paragrap h7-22 3 an dfro

mlega l interpretatio nNo . 1988-16 , date dJun e 17 , 1988 , issue db y th e Assistant Chie f Counsel , Regulation s andEnforcement Division , Offic e o f

th e Chie f Counsel . 3 . Sectio n91.10 3 states , i npart , that

"eac hpilo t

incomman dshall , befor

e beginnin g a flight, become familia

r wit hal l availabl e informatio nconcernin g tha t flight." Therefore , th e PI C mus t b e aware o f

al l that wa s don e t o th e aircraf

t tha t might affect it s operation . 4 . Sectio n91.21 3 set s fort hth e requirement s fo

r operatin g a

naircraf t wit hcertai n instrument s an dequipmen t i na ninoperabl e condition . Guidance : Thi s guidanc e material fo r conductin g a

nNRF O i s advisor

y rather thanregulatory . The PI C mus t

make th e final decisio na s t o th e safet y o f th e flight afte r considerin g all relevant regulations , procedures , andguidance . a . Air Carrie r NRFOs . Th e air

carrier manua l shoul dcontain : 1 . Detaile dpolic y andprocedure s fo r th e authorization , control , andconduc t o f all non routin e flight

operations , 2 . Addresse s o f

thos e location s an darea s whic hca nb e use dt o conduc t

th e NRFO , and 3 . Detaile dinformatio ndescribin g th e level , amount , andtyp e o f require dtrainin g fo

r thos e flight

crewmember s authorize dt o conduc t thes e type s o f

flights. b . Airworthiness . Th e PI C mus t b e certai nthat

th e airplan e i s airworthy before operatin g it . Regulation s prohibi t

apilo t fro moperatin g a

nairplan e that

i s no t airworthy . Th e PI C mus t b e certai nthat : 1 . A nauthorize dperso napprove dth e aircraf t fo r retur nt o service , i

naccordanc e wit

h th e FAA-approve dcompany maintenanc e manual . 2 . Al l inspection , maintenance , an dalteratio ntask s were complete dbefor e bein g approve dfo

r retur nt o service . c . Determin e th e Require dCre w Qualifications .

### 1 . Thi s documen t divide s NRFO s into tw o groups . (a ) Grou p 1 include s thos e NRFO s inwhic hth e flightcrew shoul dconsis t o f afull y qualifie dandcurren t

PIC , first officer , and , i f

appropriate , flight

engineer . (b ) Grou p 2 include s thos e NRFO s inwhic hth e PIC , and , i f applicable , flight engineer , are qualifie dinstructors , chec k airmen , or

flight crewmember s that

hav e bee ntraine d andauthorize dby th e ai r

carrie r specifically fo

r conductin g NRFOs . 2 . Operations . (a ) Operation s appropriate to Group 1 NRFO s involv e th e operatio no f the aircraf

t i n accordanc e wit

hth e normal procedure s o f th e flight manual . Thes e include , bu t are no t limite d to :

• Normal operatio no f airplan e system s sucha s th e normal retractio nand extensio no f

th e aircraft' s landin g gea

r

• A flight

t o confir mth e proper

functionin g o f

th e aircraft' s communicatio n an d o r navigatio nradio s

• A flight

t o confir mth e prope r

functionin g o f

th e aircraft' s autopilo t (b ) Operation s appropriat e t o Group 2 NRFO s involv e procedure s describe dor listed , i nemergency , abnormal , or alternate procedures . Thes e flights includ e an y flight i n which an y systemo nth e aircraf

t i s de-powere di

norde r to confir maback-u p systemi s functional , such as :

• Any flight that involve s de-powerin g o f

an y o f th e aircraft' s electric , hydraulic , o r

pneumati c system s

• Alternat e extensio no f th e aircraft' s landin g gea

r

• Alternat e extensio no f th e aircraft' s flaps

• A flight

that involve s approac hor

actual entr

y int o astal l

• Actual shu t

dow no f a nengin e

• De-powerin g o f

any flight

contro l power

input

• Operatio no f

th e plane' s win g flaps followin g certai nprocedure s 3 . Training .

### (a ) Th e FAA require s that ever y PI C conductin g operation s unde r part 12 1 i s traine d andqualifie dt o operat e th e airplan e inall norma l procedures , andt o recove r andlandth e aircraf

t fro mproblem s that

might occur . (b ) Eventhoug hinstructor s chec k airmen , andspecifically traine dflight crewmember s ar e qualifie dt o simulate emergencie s andexpec t th e unexpected , ther e i s aneed fo r some additional trainin g fo r thes e pilots . Eac hcertificate holder shoul ddevelop , andhav e accepte dby th e Administrator , trainin g suchtha t eachNRF O wil l b e conducte di naccordanc e wit hprocedure s consisten t

wit hsaf e flight operations . d . Preparation/Pre-Flight . Proper andcomplete preparatio nbefore startin g a nNRF O might well b e more extensiv e tha nth e actual flight. 1 . Th e PI C shoul dcoordinate wit hmaintenanc e a s t o wh

y th e flight

i s needed . (a) Wha t wa s inoperative ? (b ) Wha t wa s repaired ? (c ) Wha t wa s replaced ? 2 . Th e PI C shoul ddetermin e wha t precaution s t o take andplanahea dwha t cours e o f actio nt o take i f

th e airplan e doe s no t

functioni

nth e intende dmanner . 3 . Th e cre w shoul dthoroughl y revie w all appropriate schematics , systems , and limitation s consisten t

wit hth e intende dNRFO . 4 . Th e PI C shoul dpre-plant o immediatel y landth e plan e i f it s conditio ndeteriorate s t o a conditio nthat

i s n o longer

airworthy . Th e NRF O i s no t ates t flight andth e cre w are no t qualifie dtes t

pilots . 5 . Th e PI C shoul ddetermin e where t o conduc t th e flight. 6 . Th e PI C shoul dmake prio r coordinatio nwit

hAir Traffi c Control . 7 . Th e PI C shoul ddetermin e that weather condition s are adequate t o safely conduc t th e NRFO . e . Durin g th e Flight . Followin g thi s methodolog y allow s th e cre w t o planaheadfo r unexpecte doccurrence s durin g th e NRFO . Shoul dth e flight encounter

suc hdifficulties , th e previousl y agreed-upo nprocedure s shoul db e sufficient t o permi t asaf e landing .

### May . 19 . 200 3 9:44A M Ho . 050 3 ? . j|<^iii)jtW>iliiiWM>>a(BHhrir.iir~ i 1 ii r'IHHIJ ; 

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# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : Februar y1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 )

CAUIIQN : 51-75-1 2 REPAI R O F PAIN TCOATING S

D O NO TUS E META L TOOL S T O REMOV E TH E UNWANTE D MATERIAL . META L TOOL S CA N CAUS E DAMAG E TO TH E SURFAC E O F TH E COMPONENT . CAUTION : AVOI D T O CU TPROTECTIV E FILMS , TAPES , MASK S O R MARKING S O N TH E AIRCRAF TSKI N T O

PREVEN TSCRIB E MARKS . I F THI S OPERATIO N I S REQUIRE D US E SCISSOR S O R APLAT E BETWEE N TH E FIL M (0. 6 M M (0.02 4 IN. ) THICKNES S MINIMU M WIT H META L AN D 2 M M (0.07 9 IN. ) THICKNES S WIT H HAR D PLASTIC ) AN D TH E AIRCRAF TSKI N O R US E ASPECIA L CUTTE R (REFERENC E MARTOR POLYPIC KNO . 46 9 FRO M 3M) , THE N INSPECT . 1 . Genera l NOTE : I t i s recommende d t o us e al l material s fro m on e supplie rfo rcompatibilit yreasons . A . Th e followin g pain t repair s ar e describe d i n Paragrap h 3 ^ thr u 1 ^ :

- Repai ro f damage d to p coa t fo rmetal , composit e an d glar e part s

- Renewa l o f pain t build-u p afte rdamag e t o meta l an d glar e part s

- Renewa l o f pain t build-u p o f composit e component s tha t requir e n o anti-erosio n pain t

- Renewa l o f pain t build-u p o f composit e component s tha t requir e anti-erosio n pain t

- Repai ro f peeled-of f pain t coating s o n fastene rhead s

- Applicatio n o f anti-erosio n tap e o n vertica l an d horizonta l stabilize rleadin g edg e

- Renewa l o f damage d fue l tan k to p coatin g o n cente rtan k an d horizonta l stabilize rtan k

- Renewa l o f externa l pain t build-u p wit h AM S 309 5 externa l pain t schem e Except fo rradome , antenna s an d area s covere d wit h ant i erosio n coating . Th e maximu m recommende d pain t thicknes s i s 35 0 micron s an d 40 0 micron s fo rnacelles , fo rantenna s refe rt o SI L 34-058 . I f recommende d pain t thicknes s i s exceeded , thi s ma ycaus e electrica l discharg e whic h mayinterfer e wit h communicatio n an d navigatio n systems . Aroun d stati cport s an d pito t probe s (RVSM) , th e ste p betwee n unpainte d an d painte d are a shoul d no t excee d 40 0 microns . 2 . Safet yPrecaution s NOTE : Whe n yo u d o repaintin g nea rAO Asensors , w e recommen d tha t yo u pu t a protectiv e cove r(Par t No . 98D5310300000 ) o n th e sensors . WARNING : OBE YTH E MATERIA L MANUFACTURER' S INSTRUCTION S WHE N YO U US E PAINTS , CHROMAT E

AGENTS , CLEANIN G AGENT S AN D SPECIA L COATINGS . MOS TO F THES E MATERIAL S AR E DANGEROU S AN D FLAMMABLE . CAUTION : I F TH E STANDAR D CERTIFIE D COLO R BA G 70 7 I S NO TT O B E USE D TO RESTOR E PAIN TO R

REPAINTIN G O F TH E UPPE R SURFACE S OF : TH E HORIZONTA L TAILPLANE , ELEVATOR , AILERONS , SPOILER S AN D FLAP S PLEAS E CONTAC TAIRBU S FO R APPROVA L O F TH E NONSTANDAR D PAIN T COLOR . CAUTION : MAK E SUR E THA TTH E MATERIALS , AREA S AN D PART S GIVE N BELO W AR E PROPERL YPROTECTE D

AGAINS TPAIN TMATERIAL S BY : MASKING : RUBBER , AL L COMPOSIT E PARTS , ACRYLI C MATERIALS , AERODYNAMI C SMOOTHER , META L BONDE D EDGES , PITO TPROBES , SENSORS , STATI C PORTS , ENGIN E AI R INTAKE , PRECOOLE R AI R OUTLE TSCREEN , ENGIN E EXHAUS TDUCT , AP U EXHAUST , AP U INTAKE S AN D OUTLETS , AI R CONDITIONIN G FRES H AI R INTAKE , CABI N PRESSURIZATIO N CONTRO L SYSTE M OUTFLO W VALV E (ZON E 172) , LANDIN G GEARS , DOO R SEALS , ACCES S DOORS , CABI N WINDO W AN D WINDSHIEL D PANEL S AN D SEALS , ELECTRICA L EQUIPMEN TAN D CABLES , PLASTI C MATERIALS , EXTERNA L SKI N PANE L JOINTS , HIG H STRENGT H STEE L PARTS , AVIONIC S SKI N TEMPERATUR E SENSO R (28HQ ) SUPPOR TEXTERNA L FAC E AN D BAL L LOC KFITTINGS . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 ) PLUGGING : DRAI N HOLES , VENTS . CAUTION : MAS KANTENNAS . FO R MOR E INF O O N ANTENN APAINTIN G REFE R TO SI L 34-058 . CAUTION : MAK E SUR E THA TTH E PAIN TMATERIAL S D O NO TCOM E I N CONTAC TWITH :

- TEFLON-LINE D SELF-LUBRICATE D BEARINGS ,

- ELECTRICA L TERMINA L PLUGS ,

- NYLON-COATE D WIRES ,

- NYLO N BRUSHES . TH E CHEMICAL S I N TH E PAIN TMATERIAL S CA N AFFEC TTHES E ITEMS . CAUTION : ENSUR E THA TAL L MASKIN G MATERIAL S AR E REMOVE D FRO M TH E REPAI R ARE AO N COMPLETIO N

O F WORK , PA YSPECIA L ATTENTIO N TO PITO THEAD S AN D STATI C PORTS . 3 . Repai ro f damage d to p coa t fo rmetal , composit e an d glar e part s A . Befor e yo u star t wit h th e repai rprocedur e examin e th e dept h o f th e damage d area . I f prime ri s damage d refe rt o Paragrap h 4, . I f antistati cpain t o n composit e surface s i s damage d refe rt o Paragrap h 5 , o r6, . B . Material s ITE M

-

-

-

-

-

-

-

- NOMENCLATUR E

Cleanin g agen t Polyurethan e prime r Epox yprime r Epoxyprime r Polyurethan e to p coa t Maskin g tap e an d pape r Emeryclot h Plasti cscrape r QT Y A R A R A R A R A R A R A R A R MATERIAL/REMARK S Materia l No . 11-00 3 (Refe rt o th e CML ) Materia l No . 16-00 1 (Refe rt o th e CML ) Materia l No . 16-00 6 (Refe rt o th e CML ) Materia l No . 16-06 0 (Refe rt o th e CML ) Accordin g t o SR M 5 1 -23-1 1 32 0 grad e C . Repai r (1 ) Remov e an yloos e pain t wit h a plasti cscraper . (2 ) Us e a n adhesiv e tap e t o chec k th e adhesio n o f th e remainin g paint . (3 ) Mas k of f th e adjacen t area , whic h wil l no t b e treated , wit h maskin g tap e an d paper . (4 ) Abrad e th e surfac e wit h emer yclot h (32 0 grade ) an d chamfe rth e edge s o f th e remainin g pain t aroun d th e damage d area . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . (5 ) Remov e th e abrasiv e grit , clea n an d degreas e th e surfac e wit h cleanin g agen t (Materia l No . 11-00 3 ) . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . (6 ) Appl yepox yprime r(Materia l No . 16-00 6 o r16-06 0 ) o rpolyurethan e prime r(Materia l No . 16-00 1 ) t o th e abrade d area . (7 ) Appl yth e appropriat e polyurethan e to p coa t (Refe rt o Chapte r51-23-1 1 ) . 4 . Renewa l o f pain t build-u p afte rdamag e t o meta l an d glar e part s o rafte rpain t strippin g o f metalli can d glar e part s A . Genera l 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 2 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 ) (1 ) Yo u mus t restor e th e surfac e protectio n afte rth e remova l o f corrosion , o ra structura l repai ro rpain t stripping . (2 ) Befor e yo u star t wit h th e procedur e refe rt o SR M 51-23-1 1 an d determin e th e require d pain t build-up . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-00 2 ) I S DANGEROUS . (3 ) Mak e sur e tha t th e interna l repai rpart s ar e completel ypainte d befor e the yar e assembled . Whe n th e part s ar e assembled , th e fastene rhead s hav e t o b e reprotecte d wit h epox yprime r(Materia l No . 16-00 6 ) an d additionall y wit h polyurethan e to p coa t (Materia l No . 16-00 2 ) i n CategoryC (Refe rt o Chapte r51-21-0 0 ) . B . Material s ITE M

-

-

-

-

-

-

-

-

-

, -

- NOMENCLATUR E

Cleanin g agen t Chemica l conversio n coatin g Polyurethan e prime r Epox yprime r Polyurethan e to p coa t Was h prime r Ant i erosio n pain t Lo wVO C prime r Lo wVO C to p coa t Clea rcoa t varnis h UV R Elastomeri ccoatin g SCOTCH-BRIT E Maskin g tap e Maskin g pape r QT Y A R A R A R A R A R A R A R A R A R A R A R A R A R MATERIAL/REMARK S Materia l No . 11-00 3 (Refe rt o th e CML ) Materia l No . 13-00 2 (Refe rt o th e CML ) Materia l No . 16-00 1 (Refe rt o th e CML ) Materia l No . 16-00 6 o r16-04 9 ( Refe rt o th e CML ) Materia l No . 16-01 8 o r16-04 8 (Refe rt o th e CML ) Materia l No . 16-02 0 (Refe rt o th e CML ) Materia l No . 16-03 1 (Refe rt o th e CML ) Materia l No . 16-06 0 (Refe rt o th e CML ) Materia l No . 16-05 9 (Refe rt o th e CML ) Materia l No . 07-01 8 (Refe rt o th e CML ) Materia l No . 07-00 4 (Refe rt o th e CML ) Loca l purchas e Loca l purchas e Loca l purchas e C . Repai r (1 ) Mas k of f th e adjacen t area , whic h wil l no t b e treated , wit h maskin g tap e an d paper . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . (2 ) Clea n an d degreas e th e surfac e wit h cleanin g agen t (Materia l No . 11-00 3 ) . NOTE : Alternativ e solven t ca n b e used , refe rt o SI L 20-01 0 an d AIM S 09-00-002 . NOTE : I f excessiv e sandin g o raci d typ e pain t strippe rstrippe r(Materia l No . 12-01 4 ) ha s bee n use d fo rpain t stripping , the n inspec t th e meta l pretreatment . I f th e meta l pretreatment , th e CAAlayer , i s no t damage d the n procee d t o Paragrap h 4.C.(4) . (3 ) Pretrea t th e surfac e o f th e repai rare a i n accordanc e wit h Chapte r51-21-1 1 . WARNING i STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-02 0 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . WARNING : PRETREATMEN TFO R PAINTIN G (MATERIA L NO . 13-00 2 ) I S POISONOUS . (4 ) Appl yth e appropriat e prime ra s follows : 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 3 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 )

- Polyurethan e prime r(Materia l No . 16-00 1 ) o n to p o f was h prime r(Materia l No . 16-02 0 ) .

- Polyurethan e prime r(Materia l No . 16-00 1 ) o repox yprime r(Materia l No . 16-00 6 o r16-04 9 ) o rLo wVO C prime r(Materia l No . 16-06 0 ) o n to p o f chemica l conversio n coatin g (Materia l No . 13-00 2 ) . WARNING : PRETREATMEN TFO R PAINTIN G (MATERIA L NO . 13-00 2 ) I S POISONOUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-03 1 ) I S DANGEROUS . (5 ) Whe n erosio n damag e occur s o n th e win g leadin g edge s abov e th e pylons , th e win g tip s an d th e win g ti p fences , apply :

- I f th e bar e meta l i s expose d appl ychemica l conversio n coatin g (Materia l No . 13-00 2 ) .

- Polyurethan e prime r(Materia l No . 16-00 1 )

- Anti-erosio n pain t (Materia l No . 16-03 1 )

- Polyurethan e to p coa t (Refe rt o Chapte r51-23-1 1 ) . (6 ) Appl yfurtherlayer s o f pain t i n accordanc e wit h th e require d pain t build-up , whic h i s give n i n Chapte r51-23-11 . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-02 0 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-01 8 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-02 0 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . WARNING : LAQUE R (MATERIA L NO . 07-00 4 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : PRETREATMEN TFO R PAINTIN G (MATERIA L NO . 13-00 2 ) I S POISONOUS . (7 ) Appl yfurthe rlayer s o f pain t i n accordanc e wit h th e require d pain t build-up , whic h i s give n i n Chapte r51-23-1 1 . Th e typica l externa l pain t schem e applie d (excep t o n win g bo xuppe rsurfaces ) i s a s follows :

- Standard : Was h prime r(Materia l No . 16-02 0 ) + polyurethan e prime r(Materia l No . 16-00 1 ) + polyurethan e to p coa t (Materia l No . 16-01 8 ) .

- Alternat e 1 : Chemica l conversio n coatio n (Materia l No . 13-002 ) + epox yprime r(Materia l No . 16-04 9 ) + to p coa t (Materia l No . 16-04 8 ) .

- Alternat e 2 : Chemica l conversio n coatio n (Materia l No . 13-002 ) + lo wVO C prime r(Materia l No . 16-060 ) + lo wVO C to p coa t (Materia l No . 16-059) . Th e typica l externa l pain t schem e applie d o n win g bo xuppe rsurface s i s a s follows :

- Standard : was h prime r(Materia l No . 16-02 0 ) , polyurethan e prime r(Materia l No . 16-00 1 ) , elastomeri c coatin g (Materia l No . 07-00 4 )

- Alternat e 1 : Was h prime r(Materia l No . 16-020 ) + Lo wVO C win g coatinm g (Materia l No . 16-061 ) o r

- Alternat e 2 : Lo wVO C prime r(Materia l No . 16-060 A) + Lo wVO C win g coatin g (Materia l No . 16-061 A) . NOTE : I f step s L an d 4.C.(4) . hav e bee n omitted , lightl yabrad e th e surface s wit h SCOTCH-BRIT E an d clea n wit h lin t fre e clot h soake d wit h cleanin g agen t (Materia l No . 11-00 3 o ralternativ e solvent s accordin g t o SI L 20-010) . Befor e th e applicatio n o f epox yprime r(Materia l No . 16-04 9 ) o r(Materia l No . 16-06 0 ) appl ychemica l conversio n coatin g (Materia l No . 13-00 2 ) o n bar e expose d aluminu m parts , refe rt o Chapte r51-21-1 1 , Paragrap h 2 . B. . NOTE : Fo rexterna l pain t schem e us e a pain t syste m fro m th e sam e manufacturer . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 4 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 ) 5 . Renewa l o f pain t build-u p o f composit e component s tha t requir e n o anti-erosio n pain t A . Genera l (1 ) Afte ra structura l repai ro f composit e component s i t i s necessaryt o restor e th e remove d o rdamage d pain t layers . I n cas e o f pain t damag e t o composites , reprotec t immediatel yt o avoi d fibe rerosio n an d wate r entrapment . (2 ) Th e followin g pain t procedur e mus t b e adhere d to . B . Material s ITE M

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Antistati cpain t Cleanin g agen t Polyurethan e prime r Epox yprime r Polyurethan e prime r Por e fille r Antistati cpain t (lo wresistivity ) Antistati cpain t (hig h resistivity ) Polyurethan e to p coa t Plasti cscrape r Abrasiv e alumin e powde r Emeryclot h Adhesiv e tap e Maskin g tap e an d pape r QT Y A R A R A R A R A R A R A R A R A R A R A R A R A R A R MATERIAUREMARK S Materia l No . 07-00 5 , 07-00 6 o r16-03 0 ) (Refe rt o th e CML ) Materia l No . 1 1 -00 3 (Refe rt o th e CML ) Materia l No . 16-00 1 (Refe rt o th e CML ) Materia l No . 16-00 6 , 16-006 B o r16-006 C (Refe rt o th e CML ) Materia l No . 16-02 4 (Refe rt o th e CML ) Materia l No . 16-02 4 withou t thinne r(Refe rt o th e CML ) Materia l No . 07-00 5 (Refe rt o th e CML ) Materia l No . 07-00 6 (Refe rt o th e CML ) Accordin g t o Chapte r5 1 -23-1 1 32 5 mes h 32 0 grad e C . Preparatio n (1 ) Remov e an yloos e pain t wit h a plasti cscraper . (2 ) Us e a n adhesiv e tap e t o chec k th e adhesio n o f th e remainin g paint . (3 ) I n cas e o f repainting , mas k th e surfac e aroun d th e touc h u p area , leavin g a n overla p o f approximatel y1 0 m m (0.39 4 in. ) wit h th e existin g paint . CAUTION : D O NO TDAMAG E TH E FIBERS , TEDLA R FOI L (WHER E EXISTENT ) O R ALUMINU M FOI L

(WHER E EXISTENT ) DURIN G THI S PROCESS . (4 ) I f i t i s require d t o repaint th e part completely , th e remainin g pain t ha s t o b e abrade d dow n t o th e tedla rfoi l (wher e existent ) o raluminu m foi l (wher e existent ) o rfirs t laye ro f prime ro n composit e materials . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . (5 ) Clea n an d degreas e th e surfac e wit h cleanin g agen t (Materia l No . 11-00 3 ) . (6 ) Abrad e th e surfac e wher e th e pain t ha s peele d of f fro m th e composit e wit h emeryclot h (32 0 grade ) o rabrasiv e alumin e powde r32 5 mes h o requivalent . (7 ) Smoot h dow n th e edge s o f th e remainin g pain t i f necessar ywit h emeryclot h (32 0 grade) . 

### Prin t Date : Jul y16 , 201 0 Local Tim e Pag e 5 o f 1 9

# AIRBU S Customer : EN V Type : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 ) WARNING : LAQUE R (MATERIA L NO . 07-00 5 ) I S DANGEROUS . WARNING : LAQUE R (MATERIA L NO . 07-00 6 ) I S DANGEROUS . (8 ) I n cas e o f loca l reprotection , a strip e o f antistati cpain t (Materia l No . 07-00 5 o r07-00 6 ) 1 5 m m (0.59 1 in. ) wid e shoul d b e visibl e al l aroun d th e area . NOTE : Th e us e o f antistati cpain t i s no t necessaryo n t o Carbonfibe rReinforce d Plasti c(CFRP ) components . (9 ) Rins e wit h wate ran d carryou t a wate rbrea k test . (a ) Onc e th e abradin g proces s i s complete , was h th e are a wit h water . I f th e wate rcover s th e are a a s a n unbroke n film , th e are a i s clean . (b ) I f th e wate rform s smal l droplet s o n th e surfac e thi s i s a n indicatio n tha t th e are a i s contaminate d an d tha t cleanin g i s no t complete . I n thi s cas e repea t step s 5.C.(6) . thr u 5.C.(9). . (c ) Dr yth e are a wit h a clea n cloth . D . Reprotectio n (1 ) Surface s covere d wit h aluminu m foil : (a ) Pretrea t th e surfac e o f th e repai rare a i n accordanc e wit h ChapteL51-23-1_l . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-02 0 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . WARNING : PRETREATMEN TFO R PAINTIN G (MATERIA L NO . 13-00 2 ) I S POISONOUS . (b ) Appl yth e appropriat e prime ra s follows :

- Polyurethan e prime r(Materia l No . 16-00 1 ) o n to p o f was h prime r(Materia l No . 16-02 0 )

- Polyurethan e prime r(Materia l No . 16-00 1 ) o repox yprime r(Materia l No . 16-00 6 ) , o n to p o f chemica l conversio n coatin g (Materia l No . 13-00 2 )

- Polyurethan e to p coa t i n accordanc e wit h Chapte r51-23-1 1 . CAUTION : D O NO TCOVE R TH E 1 5 M M (0.59 1 IN. ) WID E STRI P O F ANTISTATI C PAIN TWIT H PRIME R

(REFE R T O PARAGRAP H 5.C.(8) . . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-006 B ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-006 C ) I S DANGEROUS . WARNING. : STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . WARNING : LAQUE R (MATERIA L NO . 07-00 5 ) I S DANGEROUS . WARNING : LAQUE R (MATERIA L NO . 07-00 6 ) I S DANGEROUS . (2 ) Surface s covere d wit h tedla rfoil :

- Appl yepox yprime r(Materia l No . 16-006 B o r16-006 C ) o rPolyurethan e prime r(Materia l No . 16-00 1 ) ,

- antistati cpain t (Materia l No . 07-00 5 , 07-00 6 o r16-03 0 ) ,

- polyurethan e to p coa t i n accordanc e wit h Chapte r51-23-1 1 . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-02 4 ) I S DANGEROUS . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 6 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 ) WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-018 C ) I S DANGEROUS . (3 ) CFR P (Carbonfibe rReinforce d Plastic ) parts :

- Appl ypolyurethan e prime ra s a por e fille r(Materia l No . 16-02 4 ) wher e necessary ,

- polyurethan e prime r(Materia l No . 16-04 0 ) ,

- polyurethan e finis h pain t (Materia l No . 16-018 C ) . CAUTION : D O NO TCOVE R TH E 1 5 M M (0.59 1 IN. ) WID E STRI P O F ANTISTATI C PAIN TWIT H PRIME R

(REFE R T O PARAGRAP H 5.C.(8) . . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-024 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-02 4 ) I S DANGEROUS . WARNING : LAQUE R (MATERIA L NO . 07-00 5 ) I S DANGEROUS . WARNING : LAQUE R (MATERIA L NO . 07-00 6 ) I S DANGEROUS . (4 ) AFR P (Aramidfibe rReinforce d Plastic ) o rGFR P (Glassfibe rReinforce d Plastic ) parts :

- Appl yPolyurethan e prime r(Materia l No . 16-02 4 ) o repox yprime r(Materia l No . 16-00 6 ) ,

- por e fille r(Materia l No . 16-02 4 withou t thinner ) wher e necessary ,

- antistati cpain t (Materia l No . 07-00 5 , 07-00 6 o r16-03 0 ) a s required ,

- polyurethan e to p coa t i n accordanc e wit h Chapte r51-23-1 1 . NOTE : T o achiev e a sufficien t pain t coverag e i t ca n b e necessaryt o appl yprime rprio rt o to p coa t t o avoi d a n overthicknes s o f th e to p coat . 6 . Renewa l o f pain t build-u p o f composit e component s tha t requir e anti-erosio n pain t A . Genera l (1 ) Afte ra structura l repai ro f composit e components , i t i s necessaryt o restor e th e remove d o rdamage d pain t layers . I n cas e o f pain t damag e t o composites , reprotec t immediatel yt o avoi d fibe rerosio n an d wate r entrapment . B . Material s ITE M

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Antistati cpain t (lo wresistivity ) Antistati cpain t (hig h resistivity ) Cleanin g agen t Polyurethan e prime r Por e fille r Polyurethan e to p coa t Anti-erosio n pain t Plasti cscrape r Abrasiv e alumin e powde r Emeryclot h Adhesiv e tap e Maskin g tap e an d pape r QTY A R A R A R A R A R A R A R A R A R A R A R A R MATERIAL/REMARK S Materia l No . 07-00 5 (Refe rt o th e CML ) Materia l No . 07-00 6 (Refe rt o th e CML ) Materia l No . 11-00 3 (Refe rt o th e CML ) Materia l No . 16-02 4 (Refe rt o th e CML ) Materia l No . 16-02 4 withou t thinne r(Refe rt o th e CML ) Accordin g t o Chapte r51-23-1 1 Materia l No . 16-03 1 (Refe rt o th e CML ) 32 5 mesh 32 0 grad e C . Preparatio n 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 7 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 ) (1 ) Remov e an yloos e pain t wit h a plasti cscraper . (2 ) Us e a n adhesiv e tap e t o chec k th e adhesio n o f th e remainin g paint . (3 ) Mas k off th e adjacen t area , whic h wil l no t b e treated , wit h maskin g tap e an d paper . CAUTION : D O NO TDAMAG E TH E FIBER S DURIN G THI S PROCESS . (4 ) I f i t i s require d t o repain t th e part completely , th e remainin g pain t ha s t o b e abrade d dow n t o th e basi cprimer . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . (5 ) Clea n an d degreas e th e surfac e wit h cleanin g agen t (Materia l No . 11-00 3 ) . (6 ) I n cas e o f partia l repainting , mas k th e surfac e aroun d th e repai rarea , leavin g a n overla p o f approximatel y1 0 m m (0.39 4 in. ) wit h th e existin g paint . (7 ) Abrad e th e surfac e wher e th e pain t ha s peele d of f fro m th e composit e wit h abrasiv e alumin e powde r32 5 mesh o requivalent . (8 ) Smoot h dow n th e edge s o f th e remainin g pain t i f necessar ywit h emeryclot h grad e 320 . WARNING : LAQUE R (MATERIA L NO . 07-00 5 ) I S DANGEROUS . WARNING : LAQUE R (MATERIA L NO . 07-00 6 ) I S DANGEROUS . (9 ) I n cas e o f loca l reprotection , abrad e th e adjacen t area s unti l a stri p o f antistati cpain t (Materia l No . 07-00 5 o r07 - 00 6 ) 1 5 m m (0.59 1 in. ) wid e show s aroun d th e area . NOTE : Th e us e o f antistati cpain t i s no t necessar yo n CFR P (Carbonfibe rReinforce d Plastic ) components . (10 ) Rins e wit h wate ran d carr you t a wate rbrea k test . (a ) Onc e th e abradin g proces s i s complete , was h th e are a wit h water . I f th e wate rcover s th e are a a s a n unbroke n film , th e are a i s clean . (b ) I f th e wate rform s smal l droplet s o n th e surfac e thi s i s a n indicatio n tha t th e are a i s contaminate d an d tha t cleanin g i s no t complete . I n thi s cas e repea t step s 6.C.(6) . thr u 6.C.(10). . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . (c ) Degreas e th e surfac e wit h cleanin g agen t (Materia l No . 11-00 3 ) . D . Reprotectio n CAUTION : D O NO TCOVE R TH E 1 5 M M (0.59 1 IN. ) WID E STRI P O F ANTISTATI C PAIN TWIT H PRIME R

(REFE R T O PARAGRAP H 6.C.(9) . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-02 4 ) I S DANGEROUS . (1 ) Appl yPolyurethan e prime r(Materia l No . 16-02 4 ) . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-02 4 ) I S DANGEROUS . (2 ) Appl ypor e fille r(Materia l No . 16-02 4 withou t thinner ) wher e necessaryan d abrade . WARNING i LAQUE R (MATERIA L NO . 07-00 5 ) I S DANGEROUS . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 8 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : Februar y1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 ) WARNING : LAQUE R (MATERIA L NO . 07-00 6 ) I S DANGEROUS . (3 ) Appl yantistati cpain t (Materia l No . 07-00 5 o r07-00 6 ) i f necessary . (4 ) Mas k countersun k

hole s wit h maskin g tap e fo rconductivit yreasons . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-03 1 ) I S DANGEROUS . (5 ) Appl yanti-erosio n pain t (Materia l No . 16-03 1 ) i n ra m are a a s required . NOTE : Ra m are a i s tha t are a designate d a s bein g mos t directl yoppose d t o th e airflow . (6 ) Appl ypolyurethan e to p coa t i n accordanc e wit h Chapte r51-23-1 1 . NOTE : T o achiev e a sufficien t pain t coverag e i t ca n b e necessaryt o appl yprime rprio rt o to p coa t t o avoi d a n overthicknes s t o th e to p coat . 7 . Repai ro f peeled-of f pain t coating s o n fastene rhead s A . Genera l (1 ) I f yo u fin d peeled-of f pain t coating s o n fastene rheads , i t i s ofte n th e resul t o f corrosio n o rpoo rpain t adhesion , whic h break s th e surfac e protection . (2 ) Therefor e i t i s necessaryt o examin e th e fastene ran d th e adjacen t are a fo rcorrosio n damage . I f yo u fin d corrosion , refe rt o Chapte r51-74-0 0 an d Chapte r51-43-0 0 fo rremova l o f corrosio n an d oversiz e replacement . (3 ) Befor e yo u start wit h th e procedur e refe rt o Chapte r51-23-1 1 an d determin e th e require d pain t build-up . B . Material s ITE M

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Cleanin g agen t Chemica l conversio n coatin g Epox yprime r Fina l pain t syste m Maskin g tap e an d pape r Emer yclot h SCOTCH-BRIT E pad s QT Y A R A R A R A R A R A R A R MATERIAL/REMARK S Materia l No . 11-00 3 (Refe rt o th e CML ) Materia l No . 13-00 2 (Refe rt o th e CML ) Materia l No . 16-00 6 (Refe rt o th e CML ) Accordin g t o Chapte r51-23-1 1 32 0 Grad e C . Repai r (1 ) Mas k of f th e adjacen t area , whic h wil l no t b e treated , wit h maskin g tap e an d paper . (2 ) Remov e an d abrad e th e loose , broke n pain t layer s wit h emer yclot h unti l th e surfac e i s smooth . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . (3 ) Remov e th e abrasiv e gri t an d degreas e th e surfac e o f th e repai rare a wit h cleanin g agen t (Materia l No . 1 1 -00 3 ) . WARNING : PRETREATMEN TFO R PAINTIN G (MATERIA L NO . 13-00 2 ) I S POISONOUS . (4 ) I f th e component s an d fastener s ar e mad e o f aluminu m alloy , appl ychemica l conversio n coatin g (Materia l No . 13-00 2 ) . Othe rmaterial s hav e onl yt o b e slightl yabrade d wit h Scotchbrit e pads . (5 ) Appl yepox yprime r(Materia l No . 16-00 6 ) . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 9 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 ) (6 ) Appl yth e fina l pain t syste m accordin g t o Chapte r51-23-1 1 . 8 . Applicatio n o f ant i erosio n tap e o n vertica l stabilize rleadin g edg e A . Genera l (1 ) Anti-erosio n tap e ma yb e use d a s a preventiv e measur e agains t pain t erosio n o ra s a temporar yrepai rsolution . (2 ) I n cas e o f pain t damag e t o composites , reprotec t immediatel yt o avoi d fibe rerosio n an d wate rentrapment . (3 ) Th e tap e ca n b e temporaril ydirectl yo n to p o f th e fibers , provide d th e surfac e i s abrade d t o smoot h dow n th e pain t edges . (4 ) I n cas e o f erosion , whic h cause d damag e t o th e fiber , th e structur e mus t b e repaire d t o restor e th e outsid e contou ran d structura l integrit ybefor e tap e application . B . Material s ITE M

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Cleanin g agen t Polyurethan e anti-erosio n tap e Polyurethan e anti-erosio n tap e (erosio n protectio n fo rHT P leadin g edge ) Abrasiv e san d Adhesiv e tap e Maskin g tap e an d pape r Plasti cspatul a QT Y A R A R A R A R A R A R A R MATERIAL/REMARK S Materia l No . 1 1 -00 3 (Refe rt o th e CML ) Materia l No . 05-13 2 o rMateria l No . 05-06 5 (Refe rt o th e CML ) Materia l No . 05-09 6 (Refe rt o th e CML )

C . Preparatio n o f Leadin g Edge s fo rTap e Applicatio n (1 ) Cu t th e polyurethan e tap e t o th e require d length , refe rt o Figur e 5 (2 ) D o no t remov e th e releas e pape rfro m th e polyurethan e tape . Pu t thi s tap e i n positio n o n th e leadin g edge . (3 ) Fi xth e polyurethan e tap e i n positio n wit h adhesiv e tap e an d mar k th e area . (4 ) Enlarg e th e marke d are a o n eac h sid e b yapproximatel y5 m m (0. 2 in. ) longitudina l directio n an d mas k off th e are a wit h a n adhesiv e tape , refe rt o Figur e 001 . L5JFigur e 00 1 (shee t 1 ) Applicatio n o f Ant i - erosio n Tap e (5 ) Remov e th e polyurethan e tap e subsequen t t o maskin g an d marking . (6 ) Lightl yabrad e th e applicatio n are a wit h dr yabrasiv e sand . WARNING.: CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . (7 ) Remov e th e sandin g residue s an d clea n wit h cleanin g agen t (Materia l No . 11-00 3 ) . D . Tap e Applicatio n Appl yself-adhesiv e transparen t polyurethan e tap e t o leadin g edge s a s follows : (1 ) Immediatel yafte rcleaning , howeve ronl yafte rth e complet e evaporatio n o f th e cleanin g agen t (allo w2 0 t o 3 0 minute s fo revaporatio n the n wip e th e are a wit h a clea n absorben t clot h t o avoi d an ycondensation) , plac e th e adhesiv e tap e wit h releas e pape ri n fina l positio n o n th e leadin g edges . Tac k alon g th e ful l lengt h o n bot h sides . (2 ) Graduall yremov e th e adhesiv e tackin g o n on e sid e an d pee l of f a n approximatel y5 0 m m (2. 0 in. ) wid e stri p o f releas e pape rfro m th e polyurethan e tape , refe rt o Figur e Q0 2 . 

### Prin t Date : Jul y16 , 201 0 Local Tim e Pag e 1 0 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 ) (3 ) Slightl ypres s th e polyurethan e tap e agains t th e leadin g edge . L^JFlgur e 00 2 (shee t 1 ) Applicatio n o f Anti-erosio n Tap e lj*jFigur e 00 3 (shee t 1 ) Applicatio n o f Anti-erosio n Tap e [jLlFigur e 00 4 (shee t 1 ) Applicatio n o f Anti-erosio n Tap e (4 ) Remov e th e adhesiv e tackin g o n th e opposit e sid e an d tur n u p th e polyurethan e tape . Pee l of f th e remainin g releas e paper , refe rt o Figur e 00 3 . CAUTION : D O NO TSTRETC H TH E POLYURETHAN E ANTI-EROSIO N TAP E DURIN G APPLICATION . (5 ) Graduall ypres s th e polyurethan e anti-erosio n tap e agains t th e leadin g edge , refe rt o Figur e 00 4 . (6 ) Chec k

i f th e polyurethan e tap e ha s bee n applie d withou t th e formatio n o f bubbles . CAUTION : D O NO TAPPL YEXCESSIV E PRESSURE . (7 ) I f necessary , carefull ysqueez e ou t an ytrappe d ai rusin g a plasti cspatul a o rroller . (8 ) Allo wbondin g o f th e tap e t o cur e fo ra t leas t 1 hou ra t a minimu m temperatur e o f 1 5 C ° (59 . F °) . LjLlFigur e 00 5 (shee t 1 ) Applicatio n o f Anti-erosio n Tap e 9 . Renewa l o f damage d fue l tan k to p coatin g o n cente rtan k an d horizonta l stabilize rcente rtan k A . I n th e even t o f a fue l lea k fro m th e cente rtan k

(Sectio n 21 ) o rth e horizonta l stabilizer-cente rtan k i t i s necessaryt o rene wth e externa l coatin g (Materia l No . 16-01 5 ) , a s wel l a s th e interna l sealin g i n th e are a o f th e leak . Refe rt o Chapte r51-76-1 2 fo rinformatio n concernin g th e interna l sealing . B . Material s ITE M

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Cleanin g agen t Prime rcoatin g epox y Fue l tan k

to p coatin g Polyurethan e coatin g (protectiv e coating ) Was h prime r Maskin g tap e an d pape r Abrasiv e cloth/pape r Plasti cscraper s QT Y A R A R A R A R A R A R A R A R MATERIAL/REMARK S Materia l No . 1 1 -00 3 (Refe rt o th e CML ) Materia l No . 16-00 6 (Refe rt o th e CML ) Materia l No . 16-01 5 o r09-03 2 (Refe rt o th e CML ) Materia l No . 16-042 Ao r16-02 1 (Refe rt o th e CML ) Materia l No . 16-02 0 (Refe rt o th e CML ) Loca l suppl y Grad e 10 0 an d 28 0 Loca l suppl y C . Repai r (1 ) Remov e th e fue l tan k to p coatin g (Materia l No . 16-01 5 ) fro m aroun d th e are a o f th e fue l lea k b yabrading . Us e abrasiv e cloth/pape r10 0 grad e an d finis h wit h 28 0 grade . Chamfe rth e edge s o f th e abrade d pain t t o giv e a smoot h finish . NOTE : I t i s necessar yt o remov e th e pain t dow n t o th e meta l surfac e t o ensur e goo d adhesio n o f th e ne wpain t coat . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . (2 ) Clea n th e abrade d an d surroundin g are a wit h cleanin g agen t (Materia l No . 11-00 3 ) . (3 ) Mas k off th e are a tha t i s t o b e repainted . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 1 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 ) WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-02 0 ) I S DANGEROUS . WARNING : PRETREATMEN TFO R PAINTIN G (MATERIA L NO . 13-00 2 ) I S POISONOUS . (4 ) Appl ywas h prime r(Materia l No . 16-02 0 ) t o th e expose d meta l surface , allo wwas h prime rt o dr yfo ra minimu m o f 1 hou rbu t no t exceedin g 2 4 hour s o rappl yChemica l Conversio n Coatin g (Materia l No . 13-00 2 ) (Refe rt o Chapte r51-21-1 1 ) . WARNING : PRETREATMEN TFO R PAINTIN G (MATERIA L NO . 13-00 2 ) I S POISONOUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . WAR.N1NG : STRUCTUR E PAIN T(MATERIA L NO . 16-02 0 ) I S DANGEROUS . (5 ) O n to p o f Chemica l Conversio n Coatin g (Materia l No . 13-00 2 ) appl yPrime rCoatin g Epoxy(Materia l No . 16 - 00 6 ) t o th e are a includin g an yfastene rheads , o rappl yPolyurethan e Prime r(Materia l No . 16-00 1 ) o n to p o f Was h Prime r(Materia l No . 16-02 0 ) . Allo wt o dr yunde rambien t condition s fo ra minimu m o f 2 hour s bu t no t exceedin g 2 4 hours . CAUTION : TH E ARE ATHA TI S T O B E REMASKE D SHOUL D ENSUR E THA TTH E FUE L TAN KCOATIN G

THA TI S T O B E APPLIE D DOE S NO TCONTAC TAN YOTHE R EXISTIN G PAIN TFINIS H EXCEP T TH E EPOX YPRIME R O R EXISTIN G FUE L TAN KCOATING . (6 ) Remov e maskin g tap e an d paper , remas k th e are a t o includ e a n overla p o n t o th e existin g fue l tan k coatin g (Materia l No . 16-01 5 o r09-03 2 ) , bu t observ e th e CAUTIO N give n above . (7 ) Appl yfue l tan k

coatin g (Materia l No . 16-01 5 o r09-03 2 ) wit h a soft hai rbrus h a s follows :

- 2 coats o n horizonta l surface s

- 3 coats o n vertica l surfaces . Afte reac h coa t ha s drie d fo rapproximatel y1 5 minutes , smoot h ou t b ybrus h an ybubble s o rruns . Allo w3 t o 4 hour s dryin g tim e unde rambien t condition s betwee n coats . Thi s tim e ca n b e reduce d t o 2 hour s i f force d dryin g i s used . NOTE : Fina l pain t thicknes s shoul d b e 30 0 t o 40 0 micron s (1181 1 t o 15748 microinches) . (8 ) Allo wa fina l dryin g tim e o f 2 4 hour s unde rambien t conditions . 10 . Renewa l o f externa l pain t build-u p wit h AM S 3095 externa l pain t schem e A . Genera l NOTE : D o no t rene wwit h AM S 309 5 fo rth e followin g parts :

- Radome ,

- Antenna s (Refe rt o SI L 34-058) ,

- Al l area s covere d wit h anti-erosio n coating . NOTE : Th e maximu m recommende d pain t thicknes s i s 35 0 t o 40 0 micron s o n nacelles . NOTE : Aroun d stati cport s an d pito t probe s (RVSM) , th e ste p betwee n unpainte d an d painte d area s mus t no t excee d 40 0 microns . NOTE : I f th e recommende d pain t thicknes s i s exceeded , thi s ca n caus e electrica l discharge , whic h ca n interfer e wit h communicatio n an d navigatio n systems . CAUTION : THI S PROCEDUR E I S NO TAPPLICABL E T O RADOME , ANTENNA S AN D I S NO TRECOMMENDE D

FO R UPPE R WIN G BOX . 

### Prin t Date : Jul y16 , 201 0 Local Tim e Pag e 1 2 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 ) (1 ) Thi s procedur e i s applicabl e afte rcomplet e pain t strippin g accordin g t o Chapte r51-75-1 1 . (2 ) Th e wor k

consist s i n applyin g a n externa l pain t schem e qualifie d accordin g t o AM S 3095 instea d o f AIRBU S approve d externa l pain t schem e o n externa l surface s only . (3 ) Befor e yo u start wit h th e procedur e refe rt o Chapte r51-23-1 1 an d determin e th e require d pain t build-up . (4 ) Fo rhorizonta l composit e surface s ensur e tha t th e to p coa t colo rrequirement s ar e met , contac t AIRBUS . B . Material s ITE M

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Cleanin g agen t Fina l pain t syste m Chemica l conversio n coatin g Polyurethan e prime r Epoxyprime r Was h prime r Ant i stati ccoatin g Ant i erosio n coatin g Maskin g tap e Maskin g pape r Abrasiv e pape r QT Y MATERIAL/REMARK S Materia l No . 11-00 3 (Refe rt o th e CM L o rt o SI L 20 - 010 ) accordin g t o AM S 309 5 Materia l No . 13-00 2 (Refe rt o th e CML ) Materia l No . 16-00 1 (Refe rt o th e CML ) Materia l No . 16-00 6 (Refe rt o th e CML ) Materia l No . 16-02 0 (Refe rt o th e CML ) Materia l No . 07-00 5 o rMateria l No . 07-00 6 o r Materia l No . 16-03 0 (Refe rt o th e CML ) Materia l No . 16-03 1 (Refe rt o th e CML ) Loca l purchas e Loca l purchas e Loca l purchas e Grad e 10 0 an d 28 0 C . Repai r

- Fo rRenewa l o f externa l pain t build-u p o n metalli cparts , refe rt o Paragrap h lO.C.(l) . .

- Fo rRenewa l o f externa l pain t build-u p o n composit e part s requirin g n o ant i erosio n coating , refe rt o Paragrap h 10.C.(2 V .

- Fo rRenewa l o f externa l pain t build-u p o n composit e part s requirin g ant i erosio n coating , refe rt o Paragrap h 10 ^ (3). . (1 ) Renewa l o f externa l pain t build-u p o n metalli cpart s (a ) Mas k off area s whic h wil l no t b e repainted , refe rt o Paragrap h 4, . WARNING : PRETREATMEN TFO R PAINTIN G (MATERIA L NO . 13-00 2 ) I S POISONOUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-02 0 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . WARNING : PRETREATMEN TFO R PAINTIN G (MATERIA L NO . 13-00 2 ) I S POISONOUS . (b ) I f C/V\

anodi ccoatin g o n aluminu m part s ha s bee n damage d during pain t stripping , reprotec t expose d bar e meta l a s follows :

- wit h chemica l conversio n coatin g (Materia l No . 13-00 2 ) an d prime r(Materia l No . 16-00 1 o r16-00 6 ) , refe rt o Chapte r51-21-1 1 , Paragrap h 2.B. . o r

- wit h was h prime r(Materia l No . 16-02 0 ) an d prime r(Materia l No . 16-00 1 ) . NOTE : O n titaniu m part s follo wth e sam e instruction s excep t d o no t appl ychemica l conversio n coatin g (Materia l No . 13-002) . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 3 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 ) (c ) Prepar e th e surfac e accordin g t o AM S 3095 an d pain t manufacturer' s instructions . (d ) Appl yAM S 3095 externa l pain t schem e accordin g t o pain t manufacturer' s instructions. NOTE : Fo rarea s requirin g ant i erosio n paint , refe rt o Chapte r51-23-1 1 . (2 ) Renewa l o f externa l pain t build-u p o n composit e part s requirin g n o ant i erosio n coatin g (a ) Repea t Paragrap h 4 ^ thr u 5, . (b ) Appl yexterna l pain t schem e accordin g t o AM S 309 5 an d pain t manufacturer' s instructions . (3 ) Renewa l o f externa l pain t build-u p o n composit e part s requirin g ant i erosio n coatin g (a ) Repea t Paragrap h 6.A . thr u 6.C . . (b ) Repea t Paragrap h 6.D.(1) . thr u 6.0.(5) . . (c ) Appl yexterna l pain t schem e (prime ran d to p coat ) accordin g t o AM S 309 5 an d pain t manufacturer' s instructions .



### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 4 o f 1 9I ' 

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 )

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### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 5 o f 1 9i X 

### Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 )

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### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 6 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 )

Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 7 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 )

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### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 8 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 2 - REPAI R O F PAIN TCOATING S (Revdat e = Ju n 01/09 ) '.; !

Figur e 00 5 (shee t 1 ) Applicatio n o f Anti-erosio n Tap e



### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 9 o f 1 9

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = May01/06 ) 51-75-1 1 STRIPPING/PAIN TREMOVA L CAUTION : AVOI D T O CU TPROTECTIV E FILMS , TAPES , MASK S O R MARKING S O N TH E AIRCRAF TSKI N TO

PREVEN TSCRIB E MARKS . I F THI S OPERATIO N I S REQUIRED , US E SCISSOR S O R APLAT E BETWEE N TH E FIL M 0. 6 M M (0.02 4 IN. ) MINIMU M THICKNES S WIT H META L AN D 2 M M (0.07 9 IN. ) THICKNES S WIT H HAR D PLASTIC ) AN D TH E AIRCRAF TSKIN , O R US E ASPECIA L CUTTE R (REFE R TO MANUFACTURE R COD E 3 M MARTOR-POLYPIC KN0.469) , THE N INSPECT . REFE R T O FIGUR E 00 1 . 1 . Genera l A . Th e remova l o f pain t fro m meta l surface s i s don e b yeithe rchemica l strippin g o rb yabrasio n (to p coa t only) . B . Composit e surface s mus t no t b e chemicall ystrippe d a s th e stripper s mayattac k th e resins . Therefore , onl yabrasio n shoul d b e used . C . Alternativ e strippin g processe s no t referre d t o i n Chapte r5 1 -75-1 1 t o remov e externa l pain t system s ca n b e evaluate d an d qualifie d b yth e use ran d approve d b ynationa l airworthines s authoritie s a s documente d i n SA E MA487 2 plu s additiona l test s specifi ct o AIRBU S requirements . Whe n usin g th e SA E MA487 2 procedur e i t i s mandatoryt o firs t contac t AIRBU S t o ascertai n whic h additiona l test s wil l b e require d fo rth e proces s t o b e qualified . Th e documen t SA E MA487 2 i s availabl e from : SAE40 0 Commonwealt h DriveWarrendaleP AA5096-0001US A L^Jpigur e 00 1 (shee t 1 ) Protecte d cuttin g procedur e 2 . Chemica l Pain t Strippin g Procedur e - Metalli cStructur e Onl y- Methylen e Chlorid e Base d Pain t Strippe r A . Genera l (1 ) Th e wor k

consist s of , throug h applicatio n o f chemica l strippers , removin g th e externa l pain t syste m dow n t o th e basi cprime r(fo rth e pain t buildup , refe rt o Chapte r51-23-1 1 ) . Afte rpreparatio n o f th e strippe d surface , th e ne w pain t syste m wil l b e applied . (2 ) Mak e sur e tha t th e strippe ri s remove d withi n 3 0 minute s afte rapplication . T o ensur e thi s limit , i t i s recommende d tha t on e perso n shoul d onl yappl yth e strippe rt o a n are a no t greate rtha n 4 m ^ (4 3 sq . ft. ) a t on e time . B . Safet yPrecaution s C . Repai rMaterial s WARNING : OBE YTH E MANUFACTURER' S INSTRUCTION S WHE N YO U US E STRIPPERS . TH E STRIPPER S

AR E DANGEROUS . WARNING : OBE YTH E MANUFACTURER' S INSTRUCTION S WHE N YO U US E TH E CLEANIN G AGENT S (MAT .

NO . 11-00 3 AN D 11-00 4 ) . THES E CLEANIN G AGENT S AR E DANGEROUS . CAUTION : MAK E SUR E THA TTH E RUBBER , AL L COMPOSIT E PARTS , ACRYLI C MATERIALS ,

AERODYNAMI C SMOOTHER , META L BONDE D EDGES , PITO TPROBES , SENSORS , STATI C PORTS , ENGIN E AI R INTAKE , PRECOOLE R AI R OUTLE TSCREEN , ENGIN E EXHAUS TDUCT , AP U EXHAUST , AP U INTAKE S AN D OUTLETS , AI R CONDITIONIN G FRES H AI R INTAKE , LANDIN G GEARS , DOO R SEALS , ACCES S DOORS , CABI N WINDO W AN D WINDSHIEL D PANEL S AN D SEALS , ELECTRICA L EQUIPMEN TAN D CABLES , PLASTI C MATERIALS , EXTERNA L SKI N JOINTS , AVIONIC S SKI N TEMPERATUR E SENSO R (28HQ ) SUPPOR TEXTERNA L FAC E CAUTION : MAS KANTENNAS . FOR E MOR E INF O O N ANTENN APAINTIN G REFE R TO SI L 34-058 . CAUTION : MAK E SUR E THA TDRAI N HOLE S AN D VENT S AR E PROPERL YPROTECTE D AGAINS T

STRIPPER S B YPLUGGING . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Page l o f 1 4

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = May01/06 ) CAUTION : MAK E SUR E THA TTH E PAIN TSTRIPPER S D O NO TCOM E I N CONTAC TWIT H TEFLON-LINE D

SELF-LUBRICATE D BEARINGS , ELECTRICA L TERMINA L PLUGS , NYLON-COATE D WIRE S AN D NYLO N BRUSHES . TH E CHEMICAL S I N TH E PAIN TSTRIPPERS WIL L ATTAC KTHES E ITEMS. CAUTION : ENSUR E THA TAL L MASKIN G MATERIAL S AR E REMOVE D FRO M TH E REPAI R ARE AO N

COMPLETIO N O F WORK , PA YSPECIA L ATTENTIO N TO PITO THEAD S AN D STATI C PORTS . ITE M 1 2 3 4 5 6 7 8 9 1 0 1 1 NOMENCLATUR E

Strippe r Cleanin g agen t Clea n dot h Syntheti cspong e Emeryclot h Polyethylen e fil m Adhesiv e aluminu m tap e Maskin g pape r Plasti cscrape r SCOTCH-BRIT E Brus h QT Y A R A R A R A R A R A R A R A R A R A R A R A R MATERIAL/REMARK S Materia l No . 12-00 5 o r12-01 0 (Refe rt o Chapte r51 - .35j:0 g ) <^1 , > Materia l No . 11-00 3 o r11-00 4 (Refe rChapte r51-35 - 00 ) Grad e 22 0 o r32 0 CHEMTE X A T166 , TESAfil m 132 , TESAfil m 65 9 Materia l No . 05-015 C (Refe rt o Chapte r51-35-0 0 ) , 3M-42 5 Sof t Ver yfin e c1 > Us e onl ystripper s tha t ar e permitte d b yyou rnationa l regulations . NOTE : Th e quantit yo f strippe rrequire d shoul d b e enoug h fo rthre e applications . Th e strippe rshoul d b e store d i n accordanc e wit h th e Manufacturer' s dat a sheet s befor e bein g used . D . Pain t Strippin g (1 ) Mas k area s no t t o b e stripped , an d area s tha t mus t b e protecte d agains t stripper s wit h polyethylen e fil m (CHEMTE X A T16 6 o rTES Afil m 13 2 o rTES Afil m 659 ) an d adhesive aluminu m tap e (Materia l No . 05-015 C o r 3M-425) . NOTE : Externa l ski n panel joint s (excep t fue l tan k areas ) d o no t hav e t o b e maske d if :

- ther e ar e n o bonde d doubler s i n th e joints ,

- th e tota l tim e o f strippe rapplicatio n i s les s tha n 4 hours . I f maskin g i s no t used , th e ski n join t sealan t bead s hav e t o b e renewe d (Refe rt o Chapte r51-76-0 0 ) . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . (2 ) Clea n th e are a t o b e strippe d wit h cleanin g agen t (Materia l No . 11-00 3 o r11-00 4 ) an d a clea n cloth . NOTE : Mak e sur e tha t th e cleane d surface s t o b e strippe d ar e perfectl ydrybefor e yo u start th e nex t step . WARNING : STRIPPER S AR E DANGEROUS . (3 ) Appl ya thic k

coa t o f strippe ri n accordanc e wit h th e manufacturer' s instructions . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 2 o f 1 4

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = Ma y01/06 ) NOTE : I t i s preferabl e t o stri p a t temperature s abov e 2 0 ° C (6 8 ° F ) bu t no t i n ho t sunligh t o rrain . Belo w1 8 ° C (6 4 ° F) , th e strippe rtake s muc h longe rt o reac t (u p t o twic e a s long) . WARNING : STRIPPERS AR E DANGEROUS . (4 ) Withi n 3 0 minute s remov e pain t an d strippe rresidue s carefull ywit h a sof t plasti cscraper . Thi s wil l reduc e th e ris k o f damag e t o maskin g an d th e basi cprimer . WARNING : STRIPPERS AR E DANGEROUS . (5 ) I f th e to p coa t i s onl ypartiall yremove d repea t steps 2.D.(3) . an d 2.0.(4) . , bu t onl yi n th e area s wher e th e pain t wa s no t removed . (a ) Betwee n th e strippe rapplications , inspec t an d repai rmasking , i f necessary , a s describe d i n ste p 2.0.(1) . above . (b ) Rins e carefull ywit h a wate rhose , brus h th e surfac e an d rins e agai n an d le t th e surfac e dry . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . (6 ) Afte rth e las t strippe rapplication , clea n wit h a clea n clot h soake d i n cleanin g agen t (Materia l No . 1 1 -00 3 o r1 1 - 004) . (7 ) Remov e al l maskin g tape , film s an d plugs . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . (8 ) Inspec t th e area s tha t wer e maske d fo rdamage d pain t an d presenc e o f stripper . An ystrippe rremainin g mus t b e remove d wit h cleanin g agen t (Materia l No . 11-00 3 o r11-00 4 ) an d a clea n cloth . I f th e pain t ha s bee n damaged , refe rt o ste p 2.D.(10) . below . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . (9 ) Clea n th e expose d prime rwit h cleanin g agen t (Materia l No . 1 1 -00 3 o r1 1 -00 4 ) an d dr yi t wit h a clea n cloth . (10 ) Mechanicall ylightl yabrad e area s tha t wer e maske d durin g th e strippin g an d whic h als o requir e pain t removal . Abrad e als o an yremainin g loca l spot s o f th e ol d pain t systems . D o thi s wit h emeryclot h (grad e 22 0 o r320) . (11 ) Lightl yabrad e th e strippe d area s wit h SCOTCH-BRIT E prio rt o repainting . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . (12 ) Clea n th e abrade d are a wit h cleanin g agen t (Materia l No . 1 1 -00 3 o r1 1 -00 4 ) an d dr yi t wit h a clea n cloth . (13 ) Repai rth e sealan t bead s a s describe d i n Chapter s 51-76-1 1 an d 51-76-1 2 . (14 ) Fo rrepaintin g th e strippe d are a an d 'touc h up ' o f an ydamage d pain t i n adjacen t areas , refe rt o Chapte r5 1 -23 - 0 0 an d Chapte r51-75-1 2 . 3 . Pain t Remova l byAbrasio n 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 3 o f 1 4

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = Ma y01/06 ) A . Genera l (1 ) Thi s procedur e i s use d primaril yo n composit e surface s bu t coul d als o b e use d o n meta l surface s a s a n alternativ e t o chemica l stripping . (2 ) Th e purpos e o f thi s procedur e i s t o remov e th e to p coa t partiall yo rcompletely , bu t no t t o remov e th e basi c prime r(fo rth e pain t buildup , refe rt o Chapte r51-23-1 1 ) . B . Safet yPrecaution s WARNING : OBE YTH E MANUFACTURER' S INSTRUCTION S WHE N YO U US E TH E CLEANIN G AGENT S

(MATERIA L NO . 11-00 3 AN D 11-00 4 ) . THES E CLEANIN G AGENT S AR E DANGEROUS . CAUTION : MAK E SUR E THA TTH E MATERIA L SURFACES , ESPECIALL YCOMPOSITES , AR E NO TDAMAGE D

WHE N ABRADING . CAUTION : ENSUR E THA TAL L MASKIN G MATERIAL S AR E REMOVE D FRO M TH E REPAI R ARE AO N

COMPLETIO N O F WORK , PA YSPECIA L ATTENTIO N TO PITO THEAD S AN D PORTS . C . Repai rMaterial s ITE M 1 2 3 4 5 NOMENCLATUR E

Cleanin g agen t Clea n clot h Emeryclot h SCOTCH-BRIT E Maskin g tap e an d pape r QTY A R A R A R A R A R MATERIAL/REMARK S Materia l No . 11-00 3 o r11-00 4 (Refe rt o Chapte r51 - 35_-5 0 ) Grad e 32 0 Veryfin e D . Pain t Remova l (1 ) Mas k of f th e adjacen t area , whic h wil l no t b e abraded , wit h maskin g tap e an d paper . (2 ) Lightl yabrad e th e surfac e wit h emer yclot h (grad e 320 ) unti l th e laye ro f prime ri s exposed . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . (3 ) Remov e th e abrasiv e grit , clea n an d degreas e th e surfac e wit h a clea n cloth , soake d wit h cleanin g agen t (Materia l No . 11-00 3 o r11-00 4 ) . (4 ) Lightl yabrad e th e are a wit h SCOTCH-BRIT E prio rt o repainting . (5 ) Remov e al l maskin g paper . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . (6 ) Clea n th e abrade d are a wit h a clea n clot h soake d wit h cleanin g agen t (Materia l No . 11-00 3 o r11-00 4 ) . (7 ) Repai rsealan t bead s a s describe d i n Chapte r51-76-1 1 an d Chapte r51-76-1 2 . (8 ) Fo rrepaintin g th e abrade d area , refe rt o Chapte r51-23-0 0 an d Chapte r51-75-1 2 . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 4 o f 1 4

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = May01/06 ) (9 ) Inspec t th e areas , tha t wer e masked , fo rdamage d paint . I f th e pain t ha s bee n damage d repea t steps 3.0.(1) . thr u 3.0.(9) . . 4 . One-Tim e Ful l Chemica l Pain t Strippin g Procedur e - Fuselag e Metalli cStructur e Onl y- Aci d Activate d Pain t Strippe r A . Genera l (1 ) Th e wor k

consist s of , throug h applicatio n o f chemica l strippers , removin g th e externa l pain t syste m dow n t o th e basi cprime r(fo rth e pain t buildup , refe rt o Chapte r51-23-1 1 ) . Afte rpreparatio n o f th e strippe d surface , th e ne w pain t syste m wil l b e applied . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-02 0 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-01 8 ) I S DANGEROUS . (2 ) Aci d activate d pain t strippe r(Materia l No . 12-014 ) wa s formulate d t o stri p 3 coat s pain t syste m (Materia l No . 16 - 02 0 , 16-00 1 , 16-01 8 ) an d 2 coat s pain t syste m (Materia l No . 16-05 9 an d 16-060) . (3 ) Thi s procedur e i s limite d t o one-tim e strippin g o f fuselag e onl yfo reac h aircraft . Mak e sur e tha t th e maximu m contac t tim e allowe d i s no t exceeded . Du e t o th e aggressivenes s o f aci d activate d pain t strippe ri t i s possibl e tha t ther e ma yb e a reductio n o f th e corrosio n protectio n therefor e ensur e tha t thoroug h rinsin g i s performed . B . Safet yPrecaution s WARNING : OBE YTH E MANUFACTURER' S INSTRUCTION S WHE N YO U US E STRIPPERS . TH E STRIPPER S AR E

DANGEROUS . WARNING : OBE YTH E MANUFACTURER' S INSTRUCTION S WHE N YO U US E TH E CLEANIN G AGENT S (MAT .

NO . 11-00 3 AN D 11-00 4 ) . THES E CLEANIN G AGENT S AR E DANGEROUS . CAUTION : MAK E SUR E THA TTH E RUBBER , AL L COMPOSIT E PARTS , ACRYLI C MATERIALS , AERODYNAMI C

SMOOTHER , META L BONDE D EDGES , PITO TPROBES , SENSORS , STATI C PORTS , ENGIN E AI R INTAKE , PRECOOLE R AI R OUTLE TSCREEN , ENGIN E EXHAUS TDUCT , AP U EXHAUST , AP U INTAKE S AN D OUTLETS , AI R CONDITIONIN G FRES H AI R INTAKE , LANDIN G GEARS , DOO R SEALS , ACCES S DOORS , CABI N WINDO W AN D WINDSHIEL D PANEL S AN D SEALS , ELECTRICA L EQUIPMEN TAN D CABLES , PLASTI C MATERIALS , EXTERNA L SKI N JOINTS , HIG H STRENGT H STEE L PART S HEA TTREATE D ABOV E 1400MPA , AVIONIC S SKI N TEMPERATUR E SENSO R (28HQ ) SUPPOR TEXTERNA L FAC E AN D BAL L LOC KFITTING S AR E PROPERL YPROTECTE D AGAINS T STRIPPERS B YMASKING . CAUTION : MAK E SUR E THA TDRAI N HOLE S AN D VENT S AR E PROPERL YPROTECTE D AGAINS TSTRIPPER S

B YPLUGGING . CAUTION : MAK E SUR E THA TTH E PAIN TSTRIPPER S D O NO TCOM E I N CONTAC TWIT H TEFLON-LINE D SELF LUBRICATE D BEARINGS , ELECTRICA L TERMINA L PLUGS , NYLON-COATE D WIRE S AN D NYLO N BRUSHES . TH E CHEMICAL S I N TH E PAIN TSTRIPPER S WIL L ATTAC KTHES E ITEMS . CAUTION : ENSUR E THA TAL L MASKIN G MATERIAL S AR E REMOVE D FRO M TH E REPAI R ARE AO N

COMPLETIO N O F WORK , PA YSPECIA L ATTENTIO N T O PITO THEAD S AN D STATI C PORTS . CAUTION l ENSUR E THA TROOM S FO R PAIN TREMOVA L HAV E ADEQUAT E VENTILATIO N C . Repai rMaterial s 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 5 o f 1 4

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = May01/06 ) ITE M 1 2 3 4 5 6 7 8 9 1 0 1 1 1 2 NOMENCLATUR E

Strippe r Cleanin g agen t Clea n whit e clot h Syntheti cspong e Emeryclot h Polyethylen e fil m Adhesiv e aluminu m tap e Maskin g pape r Plasti cscrape r SCOTCH-BRIT E Brus h Cleanin g agen t QTY A R A R A R A R A R A R A R A R A R A R A R A R A R MATERIAL/REMARK S Materia l No . 12-01 4 (Refe rt o Chapte r51-35-0 0 ) <1 > Materia l No . 11-00 3 o r11-00 4 (Refe rChapte r51-35 - 00 ) Grad e 22 0 o r32 0 CHEMTE X A T166 , TES Afil m 132 , TES Afil m 65 9 Materia l No . 05-015 C o r08-05 2 (Refe rt o Chapte r 51-35-0 0 ) , 3M-42 5 KRAF TPape rTap e Sof t Veryfin e Suitabl e fo rapplicatio n typ e stripper s Materia l No . 11-00 1 (Refe rt o Chapte r51-35-00 ) <1 > Us e onl ystripper s tha t ar e permitte d b yyou rnationa l regulations . NOTE : Th e quantit yo f strippe rrequire d shoul d b e enoug h fo rtw o applications . Th e strippe rshoul d b e store d i n accordanc e wit h th e manufacturer' s dat a sheet s befor e bein g used . D . Pain t Strippin g WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 1 ) I S DANGEROUS . (1 ) Dependin g o n th e degre e o f contaminatio n clea n th e are a t o b e strippe rwit h cleanin g agen t (Materia l No . 11 - 00 1 ) , refe rt o AM M Chapte r12-21-11-301 . We t surface s mus t b e dried . NOTE : Mak e sur e tha t th e cleane d surface s t o b e strippe d ar e perfectl ydrybefor e yo u start th e next step . WARNING : BONDIN G AN D ADHESIV E COMPOUN D (MATERIA L NO . 08-05 2 ) I S DANGEROUS . (2 ) Mas k area s no t t o b e stripped , an d area s tha t mus t b e protecte d agains t stripper s wit h polyethylen e fil m (CHEMTE X A T16 6 o rTES Afil m 13 2 o rTES Afil m 659 ) an d adhesiv e aluminu m tap e (Materia l No . 05-015 C o r 08-052) . NOTE : Externa l ski n panel joint s (excep t fue l tan k areas ) d o no t hav e t o b e maske d i f ther e ar e n o bonde d doubler s i n th e joints . I f maskin g i s no t used , th e ski n join t sealan t bead s ca n b e damage d an d hav e t o b e renewe d (Refe rt o Chapte r51-76-00) . NOTE : Chec k

tha t al l repair s mad e wit h hig h strengt h stee l fastener s (hea t treate d abov e 1400Mpa ) ar e protected . WARNING : STRIPPER S AR E DANGEROUS . (3 ) Appl ya thic k

unifor m coa t o f strippe r(Materia l No . 12-01 4 wit h a non-atomizin g spra yo rwit h a brus h i n accordanc e wit h manufacturer' s instructions . NOTE : Th e ski n surfac e temperatur e mus t no t excee d 3 0 C ° (8 6 F °) . D o no t hea t th e ski n wit h th e strippe rusin g a n ai rblowe ri n th e directio n o f th e surfac e t o b e stripped . I t i s preferabl e t o stri p a t temperature s abov e 2 0 C ° (6 8 F ° ) bu t no t i n ho t sunligh t o rrain . Belo w1 8 C ° (6 4 F ° ) take s muc h longe rt o react an d become s inefficient . WARNING : STRIPPER S AR E DANGEROUS . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 6 o f 1 4

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = Ma y01/06 ) (4 ) Withi n 8 t o 1 2 hour s o rsoone ri f th e pain t hav e loosened , remov e strippe ran d pain t residue s wit h a soft plasti c scraper . Thi s wil l reduc e th e ris k o f damag e t o basi cprime ran d th e strippe rwil l no t dryo n th e surface . WARNING : STRIPPER S AR E DANGEROUS . (5 ) I f th e externa l pain t syste m i s onl ypartiall yremove d repea t on e tim e onl ystep s 4.0.(3) . an d 4.D.(4). , bu t onl yi n th e area s wher e th e pain t wa s no t removed . (a ) Betwee n th e strippe rapplications , inspec t an d repai rmasking , i f necessary , a s describe d i n ste p 4JD^2) ^ above . (b ) Optional : betwee n th e strippe rapplication s rins e carefull ya s describe d i n 4.0.(6). , le t th e surfac e dr yan d reappl yth e stripper . NOTE : Mak e sur e tha t th e tota l applicatio n tim e doe s no t excee d 2 4 hours . (6 ) Afte rth e las t strippe rapplication , rins e carefull yth e surface , t o completel yremov e pain t an d strippe rresidue s an d t o neutraliz e th e strippe d areas . Us e on e o f th e followin g procedures : WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 1 ) I S DANGEROUS . (a ) Preferre d procedure :

- clea n difficul t area s wit h wate ran d SCOTCH-BRITE , rins e carefull yth e strippe d area s wit h col d o rwar m wate ru p t o 6 5 C ° (14 9 F ° ) wit h a wate rhos e (pressur e limite d t o 6 ba r(8 7 psi) ) o ra wate rhig h pressur e cleane r(pressur e max . 5 0 ba r(725. 7 psi) , distance/angl e nozzle/part 25 0 m m (9.8 4 in.)min . an d no t a t 9 0 ° ) the n rins e wit h cleanin g agen t (Materia l No . 11-00 1 ) accordin g t o AM M Chapte r12-21 - 1 1 -301 . Le t th e surfac e dry . (b ) Alternativ e procedure :

- clea n difficul t area s wit h wate ran d SCOTCH-BRITE , rins e carefull yth e strippe d area s wit h wate ru p t o 6 5 C ° (14 9 F ° ) wit h a wate rhos e (pressur e limite d t o 6 ba r(8 7 psi ) o ra wate rhig h pressur e cleane r (pressur e max . 5 0 ba r(725. 7 psi) , distance/angl e nozzle/part 25 0 m m (9.8 4 in.)min . an d no t at 9 0 ° ) , rinsin g i s finishe d whe n th e spen t wate rreache s a neutra l p h o f 7 . Le t th e surfac e dry . (7 ) Remov e al l maskin g tape , film s an d plugs . (8 ) Inspec t th e area s tha t wer e strippe d fo ran ydamag e o rcorrosion . (9 ) Inspec t th e area s tha t wer e maske d fo rdamage d pain t an d presenc e o f stripper . An ystrippe rremainin g mus t b e remove d wit h a clea n clot h o rspong e dampene d wit h water . I f th e pain t ha s bee n damaged , refe rt o ste p 4.D . (11) . below . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . (10 ) Clea n th e expose d prime rwit h cleanin g agen t (Materia l No . 1 1 -00 3 o rMateria l No . 1 1 -00 4 ) an d dryi t wit h a clea n cloth . (11 ) Mechanicall ylightl yabrad e area s tha t wer e maske d durin g th e strippin g an d whic h als o requir e pain t removal . Abrad e als o an yremainin g loca l spots o f th e ol d pain t systems . D o thi s wit h emeryclot h (grad e 22 0 o r320) . (12 ) Lightl yabrad e th e strippe d area s wit h SCOTCH-BRIT E prio rt o repainting . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 7 o f 1 4

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = Ma y01/06 ) (13 ) Clea n th e abrade d are a wit h cleanin g agen t (Materia l No . 1 1 -00 3 o rMateria l No . 1 1 -00 4 ) an d dryi t wit h a clea n cloth . (14 ) Repai rth e sealan t bead s a s describe d i n Chapter s 51-76-1 1 an d 51-76-1 2 . (15 ) Fo rrepaintin g th e strippe d are a an d 'touch up ' o f an ydamage d pain t i n adjacen t areas , refe rt o Chapte r51-23 - 0 0 an d Chapte r51-75-1 2 . (16 ) Recor d th e strippin g operation . 5 . Chemica l Pain t Strippin g Procedur e - Fuselag e Metalli cStructur e Onl y- Hydroge n Peroxid e base d Pain t Strippe r A . Genera l (1 ) Th e wor k

consist s of , throug h applicatio n o f chemica l strippers , removin g th e externa l pain t syste m dow n t o th e basi cprime r(fo rth e pain t buildup , refe rt o Chapte r51-23-1 1 ) . Afte rpreparatio n o f th e strippe d surface , th e ne w pain t syste m wil l b e applied . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-02 0 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-00 1 ) I S DANGEROUS . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-01 8 ) I S DANGEROUS . (2 ) Hydroge n peroxid e base d pain t strippe r(Materia l No . 12-01 5 ) formulate d t o stri p 2 coat s pain t syste m (Materia l No . 16-04 9 an d 16-04 8 ) o r(Materia l No . 16-06 0 an d 16-05 9 ) , ca n b e use d als o fo r3 coat s pain t syste m (Materia l No . 16-02 0 , 16-00 1 , 16-01 8 ) . (3 ) Du e t o th e agressivenes s o f hydroge n peroxid e base d pain t strippe ri t i s possibl e tha t ther e mayb e a reductio n o f th e corrosio n protectio n therefor e ensur e tha t thoroug h rinsin g i s performed . B . Safet yPrecaution s WARNING : OBE YTH E MANUFACTURER' S INSTRUCTION S WHE N YO U US E STRIPPERS . TH E STRIPPER S AR E

DANGEROUS . WARNING : OBE YTH E MANUFACTURER' S INSTRUCTION S WHE N YO U US E TH E CLEANIN G AGENT S (MAT .

NO . 11-00 3 AN D 11-00 4 ) . THES E CLEANIN G AGENT S AR E DANGEROUS . CAUTION : MAK E SUR E THA TTH E RUBBER , AL L COMPOSIT E PARTS , ACRYLI C MATERIALS , AERODYNAMI C

SMOOTHER , META L BONDE D EDGES , PITO TPROBES , SENSORS , STATI C PORTS , ENGIN E AI R INTAKE , PRECOOLE R AI R OUTLE TSCREEN , ENGIN E EXHAUS TDUCT , AP U EXHAUST , AP U INTAKE S AN D OUTLETS , AI R CONDITIONIN G FRES H AI R INTAKE , LANDIN G GEARS , DOO R SEALS , ACCES S DOORS , CABI N WINDO W AN D WINDSHIEL D PANEL S AN D SEALS , ELECTRICA L EQUIPMEN TAN D CABLES , PLASTI C MATERIALS , EXTERNA L SKI N JOINTS , HIG H STRENGT H STEE L PART S HEA TTREATE D ABOV E 1400MPA , AVIONIC S SKI N TEMPERATUR E SENSO R (28HQ ) SUPPOR TEXTERNA L FAC E CAUTION : MAK E SUR E THA TDRAI N HOLE S AN D VENT S AR E PROPERL YPROTECTE D AGAINS TSTRIPPER S

B YPLUGGING . CAUTION : MAK E SUR E THA TTH E PAIN TSTRIPPER S D O NO TCOM E I N CONTAC TWIT H TEFLON-LINE D SELF LUBRICATE D BEARINGS , ELECTRICA L TERMINA L PLUGS , NYLON-COATE D WIRE S AN D NYLO N BRUSHES . TH E CHEMICAL S I N TH E PAIN TSTRIPPER S WIL L ATTAC KTHES E ITEMS. CAUTION : ENSUR E THA TAL L MASKIN G MATERIAL S AR E REMOVE D FRO M TH E REPAI R ARE AO N

COMPLETIO N O F WORK , PA YSPECIA L ATTENTIO N T O PITO THEAD S AN D STATI C PORTS . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 8 o f 1 4

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = Ma y01/06 ) CAUTION : ENSUR E THA T ROOM S FO R PAIN T REMOVA L HAV E ADEQUAT E VENTILATIO N CAUTION : ENSUR E THA T PERSONNE L WEA R SUITABL E PROTECTIV E CLOTHING , GLOVE S AN D EYE/FAC E PROTECTIONAN D RESPIRATOR Y PROTECTIO

N C . Repai rMaterial s ITE M 1 2 3 4 5 6 7 8 9 1 0 1 1 1 2 NOMENCLATUR E

Strippe r Cleanin g agen t Clea n whit e clot h Syntheti cspong e Emeryclot h Polyethylen e fil m Adhesiv e aluminu m tap e Maskin g pape r Plasti cscrape r SCOTCH-BRIT E Brus h Cleanin g agen t QTY A R A R A R A R A R A R A R A R A R A R A R A R A R MATERIAL/REMARK S Materia l No . 12-01 5 (Refe rt o Chapte r51-35-0 0 ) <1 > Materia l No . 11-00 3 o r11-00 4 (Refe rChapte r51-35 - 00 ) Grad e 22 0 o r32 0 CHEMTE X A T166 , TESAfil m 132 , TESAfil m 65 9 Materia l No . 05-015 C o r08-05 2 (Refe rt o Chapte r 51-35-00) . 3M-42 5 KRAF TPape rTap e Sof t Ver yfin e Suitabl e fo rapplicatio n typ e stripper s Materia l No . 11-00 1 (Refe rt o Chapte r51-35-00 ) <1 > Us e onl ystripper s tha t ar e permitte d b yyou rnationa l regulations . NOTE : Th e strippe rshoul d b e store d i n accordanc e wit h th e manufacturer' s dat a sheet s befor e bein g used . D . Pain t Strippin g WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 1 ) I S DANGEROUS . (1 ) Dependin g o n th e degre e o f contaminatio n clea n th e are a t o b e strippe rwit h cleanin g agen t (Materia l No . 11 - 00 1 ) , refe rt o AM M Chapte r12-21-11-301 . We t surface s mus t b e dried . NOTE : Mak e sur e tha t th e cleane d surface s t o b e strippe d ar e perfectl ydr ybefor e yo u star t th e next step . WARNING.: BONDIN G AN D ADHESIV E COMPOUN D (MATERIA L NO . 08-05 2 ) I S DANGEROUS . (2 ) Mas k area s no t t o b e stripped , an d area s tha t mus t b e protecte d agains t stripper s wit h polyethylen e fil m (CHEMTE X A T16 6 o rTES Afil m 13 2 o rTES Afil m 659 ) an d adhesiv e aluminu m tap e (Materia l No . 05-015 C o r 08-05 2 ) . Mas k

al l cadmiu m plate d stee l fastener s usin g aluminu m tap e (Materia l No . 05-015 C 08-052) . Contact AIRBU S fo rdetectio n procedur e an d localisation . NOTE : Externa l ski n panel joint s (excep t fue l tan k areas ) d o no t hav e t o b e maske d i f ther e ar e n o bonde d doublers i n th e joints . I f maskin g i s no t used , th e ski n join t sealan t bead s ca n b e damage d an d hav e t o b e renewe d (Refe rt o Chapte r51-76-00) . NOTE : Chec k

tha t al l repair s mad e wit h hig h strengt h stee l fastener s (hea t treate d abov e 1400Mpa ) ar e protected . WARNING : STRIPPER S AR E DANGEROUS . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 9 of 1 4

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = Ma y01/06 ) (3 ) Appl ya thic k

unifor m coa t o f strippe r(Materia l No . 12-01 5 wit h a non-atomizin g spra yo rwit h a brus h i n accordanc e wit h manufacturer' s instructions . NOTE : Th e ski n surfac e temperatur e mus t no t excee d 3 0 C ° (8 6 F °) . D o no t hea t th e ski n wit h th e strippe rusin g a n ai rblowe ri n th e directio n o f th e surfac e t o b e stripped . I t i s preferabl e t o stri p a t temperature s abov e 2 0 C ° (6 8 F ° ) bu t no t i n ho t sunligh t o rrain . Belo w1 8 C ° (6 4 F ° ) take s much longe rt o react an d become s inefficient . WARNING : STRIPPER S AR E DANGEROUS . (4 ) Withi n 8 t o 1 2 hour s o rsoone ri f th e pain t hav e loosened , remov e strippe ran d pain t residue s wit h a soft plasti c scraper . Thi s wil l reduc e th e ris k o f damag e t o basi cprime ran d th e strippe rwil l no t dryo n th e surface . WARNING : STRIPPER S AR E DANGEROUS . (5 ) I f th e externa l pain t syste m i s onl ypartiall yremove d repea t steps 5.0.(3) . an d 5.D.(4). , bu t onl yi n th e area s wher e th e pain t wa s no t remove d betwee n th e strippe rapplications , inspec t an d repai rmasking , i f necessary , a s describe d i n ste p 5.0.(2) . above . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 1 ) I S DANGEROUS . (6 ) Afte rth e las t strippe rapplication , rins e carefull yth e surface , t o completel yremov e pain t an d strippe rresidues . Clea n difficul t area s wit h wate ran d SCOTCH-BRITE , rins e carefull yth e strippe d area s wit h col d o rwar m wate r u p t o 6 5 C ° (14 9 F "^

) wit h a wate rhos e (pressur e limite d t o 6 ba r(8 7 psi ) o ra wate rhig h pressur e cleane r (pressur e max . 5 0 ba r(725. 7 psi) , distance/angl e nozzle/par t 25 0 m m (9.8 4 in.)min . an d no t at 9 0 ° ) , the n a s a n optio n rins e wit h wit h cleanin g agen t (Materia l No . 11-00 1 ) accordin g t o AM M Chapte r12-21-11-301 . Le t th e surfac e dry . (7 ) Remov e al l maskin g tape , film s an d plugs . (8 ) Inspec t th e area s tha t wer e strippe d fo ran ydamag e o rcorrosion . (9 ) Inspec t th e area s tha t wer e maske d fo rdamage d pain t an d presenc e o f stripper . An ystrippe rremainin g mus t b e remove d wit h a clea n clot h o rspong e dampene d wit h water . I f th e pain t ha s bee n damaged , refe rt o ste p 5.D . (11) , below . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . (10 ) Clea n th e expose d prime rwit h cleanin g agen t (Materia l No . 11-00 3 o rMateria l No . 11-00 4 ) an d dryi t wit h a clea n cloth . (11 ) Mechanicall ylightl yabrad e area s tha t wer e maske d durin g th e strippin g an d whic h als o requir e pain t removal . Abrad e als o an yremainin g loca l spots o f th e ol d pain t systems . D o thi s wit h emeryclot h (grad e 22 0 o r320) . (12 ) Lightl yabrad e th e strippe d area s wit h SCOTCH-BRIT E prio rt o repainting . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . (13 ) Clea n th e abrade d are a wit h cleanin g agen t (Materia l No . 1 1 -00 3 o rMateria l No . 1 1 -00 4 ) an d dr yi t wit h a clea n cloth . (14 ) Repai rth e sealan t bead s a s describe d i n Chapter s 51-76-1 1 an d 51-76-1 2 . (15 ) Fo rrepaintin g th e strippe d are a an d 'touc h up ' o f an ydamage d pain t i n adjacen t areas , refe rt o Chapte r51-23 - 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 0 o f 1 4

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = May01/06 ) 0 0 an d Chapte r51-75-1 2 . 6 . Chemica l Pain t Strippin g Procedur e - Metalli cStructur e Onl y- Alkalin e Benzy l Alcoho l base d Pain t Strippe r- Intermediat e Coa t Pain t Syste m A . Genera l (1 ) Th e wor k

consist s of , throug h applicatio n o f chemica l strippers , removin g th e externa l pain t syste m dow n t o th e prime r(fo rth e pain t buildup , refe rt o Chapte r51-23-1 1 ) . Afte rpreparatio n o f th e strippe d surface , th e ne wpain t syste m wil l b e applied . WARNING : STRUCTUR E PAIN T(MATERIA L NO . 16-006 B ) I S DANGEROUS . (2 ) Pain t Strippe r(Materia l No . 12-013 ) wa s formulate d t o stri p intermediat e coa t pain t syste m (Materia l No . 16 - 006 B , 16-06 2 an d 16-05 9 ) . Thi s strippe rallow s strippin g o f to p coa t an d intermediat e coa t withou t strippin g th e primer . (3 ) Th e entir e fuselag e ca n b e treate d a t th e sam e tim e o rdivide d i n sections . I f pain t strippe r(Materia l No . 12-013 ) intend s t o dry , kee p th e surfac e we t b yapplyin g a ligh t coa t o f strippe rove rth e existin g laye ro f stripper . B . Safet yPrecaution s WARNING : OBE YTH E MANUFACTURER' S INSTRUCTION S WHE N YO U US E STRIPPERS . TH E STRIPPER S AR E

DANGEROUS . WARNING : OBE YTH E MANUFACTURER' S INSTRUCTION S WHE N YO U US E TH E CLEANIN G AGENT S (MAT .

NO . 11-00 3 AN D 11-00 4 ) . THES E CLEANIN G AGENT S AR E DANGEROUS . CAUTION : MAK E SUR E THA TTH E RUBBER , AL L COMPOSIT E PARTS , ACRYLI C MATERIALS , AERODYNAMI C

SMOOTHER , META L BONDE D EDGES , PITO TPROBES , SENSORS , STATI C PORTS , ENGIN E AI R INTAKE , PRECOOLE R AI R OUTLE TSCREEN , ENGIN E EXHAUS TDUCT , AP U EXHAUST , AP U INTAKE S AN D OUTLETS , AI R CONDITIONIN G FRES H AI R INTAKE , LANDIN G GEARS , DOO R SEALS , ACCES S DOORS , CABI N WINDO W AN D WINDSHIEL D PANEL S AN D SEALS , ELECTRICA L EQUIPMEN TAN D CABLES , PLASTI C MATERIALS , EXTERNA L SKI N JOINTS , HIG H STRENGT H STEE L PART S HEA TTREATE D ABOV E 1400MPA , AVIONIC S SKI N TEMPERATUR E SENSO R (28HQ ) SUPPOR TEXTERNA L FAC E CAUTION : MAK E SUR E THA TDRAI N HOLE S AN D VENT S AR E PROPERL YPROTECTE D AGAINS TSTRIPPER S

B YPLUGGING . CAUTION : MAK E SUR E THA TTH E PAIN TSTRIPPER S D O NO TCOM E I N CONTAC TWIT H TEFLON-LINE D SELF LUBRICATE D BEARINGS , ELECTRICA L TERMINA L PLUGS , NYLON-COATE D WIRE S AN D NYLO N BRUSHES . TH E CHEMICAL S I N TH E PAIN TSTRIPPER S WIL L ATTAC KTHES E ITEMS . CAUTION : ENSUR E THA TAL L MASKIN G MATERIAL S AR E REMOVE D FRO M TH E REPAI R ARE AO N

COMPLETIO N O F WORK , PA YSPECIA L ATTENTIO N T O PITO THEAD S AN D STATI C PORTS . CAUTION : ENSUR E THA TROOM S FO R PAIN TREMOVA L HAV E ADEQUAT E VENTILATIO N C . Repai rMaterial s

ITE M 1 2 NOMENCLATUR E

Strippe r Cleanin g agen t QT Y A R A R A R MATERIAL/REMARK S Materia l No . 12-01 3 (Refe rt o Chapte r51-35-0 0 ) <1 > Materia l No . 11-00 3 o r11-00 4 (Refe rChapte r51-35 - 00 ) 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 1 o f 1 4

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = Ma y01/06 ) 3 4 5 6 7 8 9 1 0 1 1 1 2 Clea n whit e clot h

Syntheti cspong e Emer yclot h Polyethylen e fil m Adhesiv e aluminu m tap e Maskin g pape r Plasti cscrape r SCOTCH-BRIT E Brus h Cleanin g agen t A R A R A R A R A R A R A R A R A R A R Grad e 22 0 o r32 0 CHEMTE X AT166 , TES Afil m 132 , TES Afil m 65 9 Materia l No . 05-015 C o r08-05 2 (Refe rt o Chapte r 51-35-00) . 3M-42 5 KRAF TPape rTap e Sof t Veryfin e Suitabl e fo rapplicatio n typ e stripper s Materia l No . 11-00 1 (Refe rt o Chapte r51-35-00 ) <1 > Us e onl ystripper s tha t ar e permitte d b yyou rnationa l regulations . NOTE : Th e strippe rshoul d b e store d i n accordanc e wit h th e manufacturer' s dat a sheet s befor e bein g used . D . Pain t Strippin g WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 1 ) I S DANGEROUS . (1 ) Dependin g o n th e degre e o f contaminatio n clea n th e are a t o b e strippe rwit h cleanin g agen t (Materia l No . (Materia l No . 11-00 1 ) , refe rt o AM M Chapte r12-21-11-301 . We t surface s mus t b e dried . NOTE : Mak e sur e tha t th e cleane d surface s t o b e strippe d ar e perfectl ydr ybefor e yo u start th e nex t step . WARNING : BONDIN G AN D ADHESIV E COMPOUN D (MATERIA L NO . 08-05 2 ) I S DANGEROUS . (2 ) Mas k area s no t t o b e stripped , an d area s tha t mus t b e protecte d agains t stripper s wit h polyethylen e fil m (CHEMTE X A T16 6 o rTES Afil m 13 2 o rTES Afil m 659 ) an d adhesive aluminu m tap e (Materia l No . 05-015 C o r 08-05 2 ) . NOTE : Externa l ski n panel joint s (excep t fue l tan k areas ) d o no t hav e t o b e maske d i f ther e ar e n o bonde d doubler s i n th e joints . WARNING : STRIPPER S AR E DANGEROUS . (3 ) Appl ya thic k

close d unifor m coa t o f strippe r(Materia l No . 12-01 3 ) wit h a non-atomizin g spra yo rwit h a brus h i n accordanc e wit h manufacturer' s instructions . NOTE : I t i s recommende d t o appl ypain t strippe r(Materia l No . 12-013 ) b ysprayin g usin g airles s pum p wit h 10: 1 rati o an d spra ynozzl e creatin g a wid e fa n typ e sprayin g pattern . NOTE : Th e ski n surfac e temperatur e mu t no t excee d 3 5 C " (9 5 F °) . I t i s preferabl e t o stri p a t temperature s abov e 2 0 C ° (6 8 F ° ) bu t no t i n ho t sunligh t o rrain . Belo w1 8 C ° (6 4 F ° ) i t take s muc h longe rt o react . (4 ) Allo wt o dwel l fo rsufficien t tim e t o lif t th e paint . Typicall ystart s t o reac t afte r1 t o 2 hour s wit h standar d thi n to p coa t bu t les s tha n 1 0 hour s whe n pain t ha s loosened . Remov e strippe ran d pain t residue s wit h a soft plasti c scrape r(ensur e no t t o rebon d th e residue s o n th e surfac e wit h th e scraper) . NOTE : D o no t us e metalli cscraper . NOTE : Kee p th e surfac e we t i f strippe rintend s t o dr yb yreapplyin g a mis t coa t o f stripper . Strippe rtend s t o dr ya s th e solven t react s wit h th e interdediat e coat . NOTE : A n excessiv e applicatio n tim e (superio rt o 2 0 hours ) ma ydegrad e th e primer . 

### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 2 o f 1 4

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = May01/06 ) (5 ) I f th e externa l pain t syste m i s onl ypartiall yremove d an d t o ensur e tha t ai l intermediat e coa t ha s bee n removed , repea t step s 6.D.(3) . an d 6.D.(4) . . I n th e area s wher e th e pain t wa s no t remove d betwee n th e strippe r applications , inspec t an d repai rmasking , i f necessary , a s describe d i n ste p 6.D.(2) . above . WA_RNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 1 ) I S DANGEROUS . (6 ) Afte rth e las t strippe rapplication , rins e carefull yth e surface , t o completel yremov e pain t an d strippe rresidues . Clea n difficul t area s wit h wate ran d SCOTCH-BRITE , rins e carefull yth e strippe d area s wit h col d o rwar m wate r u p t o 6 5 C ° (14 9 F ° ) wit h a wate rhos e (pressur e limite d t o 6 ba r(8 7 psi ) o ra wate rhig h pressur e cleane r (pressur e max . 5 0 ba r(725. 7 psi) , distance/angl e nozzle/par t 25 0 m m (9.8 4 in. ) min . an d no t a t 9 0 °) , the n a s a n optio n rins e wit h wit h cleanin g agen t (Materia l No . 11-00 1 ) accordin g t o AM M Chapte r12-21-11-301 . Le t th e surfac e dry . (7 ) Remov e al l maskin g tape , film s an d plugs . (8 ) Inspec t th e area s tha t wer e stripped . (9 ) Inspec t th e area s tha t wer e maske d fo rdamage d pain t an d presenc e o f stripper . An ystrippe rremainin g mus t b e remove d wit h a clea n clot h o rspong e dampene d wit h water . I f th e pain t ha s bee n damaged , refe rt o ste p 6.D . (XI X below . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . (10 ) Clea n th e expose d prime rwit h cleanin g agen t (Materia l No . 1 1 -00 3 o rMateria l No . 1 1 -00 4 ) an d dr yi t wit h a clea n cloth . (11 ) Mechanicall ylightl yabrad e area s tha t wer e maske d durin g th e strippin g an d whic h als o requir e pain t removal . Abrad e als o an yremainin g loca l spots o f th e ol d pain t systems . D o thi s wit h emeryclot h (grad e 22 0 o r320) . (12 ) Lightl yabrad e th e strippe d area s wit h SCOTCH-BRIT E prio rt o repainting . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 3 ) I S DANGEROUS . WARNING : CLEANIN G AGEN T(MATERIA L NO . 11-00 4 ) I S DANGEROUS . (13 ) Clea n th e abrade d are a wit h cleanin g agen t (Materia l No . 1 1 -00 3 o rMateria l No . 1 1 -00 4 ) an d dr yi t wit h a clea n cloth . (14 ) Afte rpain t strippin g an yexpose d sealan t i.e . no t covere d wit h primer , i s considere d a s damaged . Repai ran y damage d sealan t bead s a s describe d i n Chapte r51-76-1 1 an d 51-76-1 2 . (15 ) Fo rrepaintin g th e strippe d are a an d 'touc h up ' o f an ydamage d pain t i n adjacen t areas , refe rt o Chapte r51-23 - O Q an d Chapte r51-75-1 2 .



### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 3 o f 1 4

# AIRBU S Customer : EN V Typ e : A318/A319/A320/A32 1 Rev . Dat e : February1 , 201 0 Manual : SRM_A32 0 Selecte d effectivity : AL L 51-75-1 1 - STRIPPING/PAIN TREMOVA L (Revdat e = May01/06 )



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Figur e 00 1 (shee t 1 ) Protecte d cuttin g procedur e



### Prin t Date : Jul y16 , 201 0 Loca l Tim e Pag e 1 4 o f 1