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Issued: 8
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8 March 201
LANNING A. EFFEC . REASO . DESCR . COMP
. APPRO . TOOLI G. WEIGH . REFER HOURS . WARR 9
G INFORMA
CTIVITY ON
RIPTION LIANCE OVAL NG
HT AND BA RENCE
S REQUIRE
RANTY COV ENGINE ATION M 7 7 D P ( t T a P P P P B N
ALANCE N 7 ED P P VER N E FUEL MODEL 750XL 750XL During a Powerplant (forward of the Engin e Transducer adjacent El PART A:
PART B:
PART A:
PART B:
By delegate N/A Negligible.
750XL Main Part A – 1 H Part B – 4 H Normal Wa MAN FEED L
(Aircraft with Air C Alternator review o f t Fuel Line s the Engine e Fuel Fee rs could ectrical Wir Inspection Line and a Corrective Carry out v flight hours Corrective within 300 If chafing the (oran g Fuel Line damage i s corrective out before ed authority ntenance M Hour.
Hours.
rranty cond P A NDATO LINE S/N 101 thru 21 8001, 8 provisioned Conditioning
r) f the ins t s and Elect r e Firewall), d Line an d potentially ring and the of the E n adjacent Ele actions (if re visual inspe
s.
action mu s flight hours is found w ge) outer Firesleeve s found to E actions a r e further flig
y.
Manual.
ditions apply
ACSB / XL IS ORY S N 15, 220 8002 d for or in s g and/or Sta tallation o f rical Installa it was foun d Fuel Pr e chafe a g e Ignition Ex ngine Fuel ectrical Wirin required).
ection withi st be carri e
s.
which pen e covering o or if chaf i Electrical W re to be c ght.
y.
L / 113 SSUE 2 Page 1 o SERVI stalled andby f the ations d that essure gainst xciter.
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n 165 ed out etrates of the ing or Wiring, carried of 6 CE B U L L E T I N
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age 2 of 6 ACCOM N
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MPLISHME OTE: Th rev ins de Fo loc rec Ele – Inspectio ial inspectio ocedures de he Engine F Figure 1 bel FIGU pect the F u afing, payi n nnector and pect the Ele nnectors an chafing is esleeve or ailed in PAR o chafing is hin 300 hou
ENT INSTR e procedu r vised Fuel L stallation o f tailed in Fig or Aircraft fit cated in a d commended ectrical Wiri on of Engin on may be etailed in the Fuel Feed l ow, then ca RE 1 I N uel Feed L i ng particul a d the Batter ectrical Wiri nd along the found whi c if chafing RT B are to s found, co urs.
RUCTIONS res below a Line and Ign f Air Con d gure 1 below tted with the different loc d that a s ng are carr ne Fuel Fee carried out e Approved ine and Ign arry out insp
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e Fuel Feed cation from survey of t h ried out for s ed Line t in conjun c Maintenan nition Excite pection deta N AREA – L.
from the Fi r to the ar e able.
adjacent to t ount Tubing tes the (o r e is found out before tions are to d specifica er installatio nd/or Stan d d Hose and that detaile he Fuel Li signs of cha ction with t h nce Manual.
er are instal ailed below H.S OF POW rewall to t h eas adjace n the Fuel Pre g for signs o range) out e to Electri c further fligh be carried
PA I lly for airc r ons to provi dby Altern a d/or Ignition ed in Figur e nes and a afing.
he normal 1
led in the c .
WERPLANT he Oil/Fuel nt to the I g essure Swit of chafing.
er coverin g cal Wiring, ht.
out in acco
ACSB / XL IS Issued: 8 Ma raft with ision for ator as n Exciter e 1, it is adjacent 150 hour in configuratio
Heater for gnition Ex c tch and Tra
g of the F u corrective ordance wit L / 113 SSUE 2 arch 2019 spection n shown
signs of citer and ansducer uel Line actions h Part B
Issued: 8 PA
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2)
3)
4)
5)
6) 8 March 201 RT B – Cor With refe procedur Remove mounted the inlet the Fue l Wiring L If inspec affected Fuel Hos Reinstall Switch/T Hose to Flow Tra and Figu Attach t h using t h AN960-1 Ensure a electrica Battery L Figure 3
9 rrective Ac erence to 75 res for fuel the Fuel F d Fuel Heat and outle t l Flow Tra n ooms as re ction in PAR Fire Sleev se requires l the (lo n Transducer run from th ansducer an ure 3 below he Pressur e he existing 10L Washer all Fuel Li n l wiring prio Leads are P ).
FIGURE 2 ction 50XL Maint system ma Feed Line (r er inlet) inc t Fuel Hos e nsducer an quired to al RT A has ide e and insp replacemen ger) P/N Manifold to he Firewall nd the Fuel .
e Switch/T r hardware r and P/N M nes are rou t or to tighten P-clipped to RELOCA tenance Ma intenance.
running from cluding all a es (P/Ns 1 5 d the Fuel llow reposit entified cha ect the Fu e nt in additio 156F003-8 the engine Tee to the l Pressure S ransducer M (P/N MS2 1 MS21042L3 ted to pre v ning the fittin o the Fuel
ATED HOSE anual Chapt m the Engin ttaching P C 56F003-8D Pressure ioning of Fu fing of the F el Hose fo r on to the co 8D-0154 H
e. Reinstall Fuel Flow Switch/Tran Manifold to 1919WDG1 Nut).
vent chafin g ngs and ins Feed Hose ES – L.H.S. O er 28, carry ne Firewall Clips and T -0154 and Switch/Tran uel Transdu Fuel Hose F r chafing. A rrective acti Hose to r the (shorte Transducer nsducer Ma the Uppe r 6 P Clip, g against a d stalling the P e to ensure
OF POWERP PACSB y out norma Tee Fitting Tyraps (if us 156F003-8 nsducer M a ucers and S Fire Sleevin A chaffed F ion detailed run from er) P/N 156F r inlet. Rei anifold. Re f r Engine M P/N AN3- 1 djacent co m P Clips. En positive se PLANT B / XL / 1 ISSUE Page 3 o al preparatio to the eng sed). Remo 8D-0140) f r anifold. U n witch.
ng, remove Fire Sleeve d below.
the Press F003-8D-01 nstall the F fer to Figure ount Tube 17A Bolt, P mponents a nsure the M eparation (S
13 E 2 of 6 on ine ove rom ntie the e or ure 140 Fuel e 2 re- P/N and ain See
Pa age 4 of 6
7) P C the the (Se FIGUR Clip the lo w Engine D r Fuel hose ee Figure 4) RE 3 R E wer Fuel H o riven Fuel P which runs ).
2.FIGU
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P CLIPPING .H.S. OF PO -0140) to t h Tee Fitting.
ven Fuel P u
OF HOSES PA I
OWERPLANT he Fuel ho s P Clip the ump to the
ACSB / XL IS Issued: 8 Ma
T se which r u Oil Cooler Firewall Te L / 113 SSUE 2 arch 2019 uns from Hose to ee Fitting
Issued: 8
8)
3. C E Rec The insp
4. M A De P P P P P BR SC SC W N 8 March 201 Remove Clips (Se Main Loo
ERTIFICAT cord compli e accomplis pection sho
ATERIAL R escription CLIP CLIP CLIP CLIP CLIP RACKET CREW CREW WASHER UT 9 Tyraps att ee Figure 5 oms and tie
3.FIGU TION iance with t shment of th ould be perfo
REQUIRED aching Elec
5). Rerout e e/secure as URE 5 P his Service his Service ormed IAW D ctrical Loom e Fuel Tra n required I.A
CLIPPING O Bulletin in Bulletin is a W 750XL Ma Part N MS219 MS219 MS219 MS219 MS219 AN743 AN525 AN525 AN960 MS210 m to Engin e nsducer and A.W. AC43.
OF ELECTR
the Aircraft a terminatin intenance M umber 919WH6 919WH10 919WH15 919WH16 919WH19 3-12 5-10R7 5-10R8 0-10L 042L3 e Mount Tru d Pressure 13-1B Para
RICAL LOOM Log Book.
g action. Th Manual Sec PACSB uss (if fitted Switch Wir a 11-96.
M hereafter, th ction 05-10- Q B / XL / 1 ISSUE Page 5 o ) and insta ring to exis t he repetitive -00.
ty Require 2 3 1 3 3 1 4 2 6 6 13 E 2 of 6 ll P ting
e d
Pa
age 6 of 6
INT
TENTIONAALLY LEFTT BLANK PA I
ACSB / XL IS Issued: 8 Ma L / 113 SSUE 2 arch 2019