EPSTEIN
page 3 / 530 . OCR, unverified
N541000-004
4. TYPE (Aber* Engine, People, art)
Forebody Assy
& NAME OF APPLICANT
Nextant Aerospace LLC
Cleveland, Ohio
LIST OF DATA
& PENTIF(GM.PN
7. TITLE
NT-EO-1118-31
Rev. IR
November 29, 2018
—
Engine Inlet Rivet Repair.
Notes:
1) The structural
approval is
demonstrates
subparagraph
2) This form constitutes
substantiation
data are approved herein. This
the data listed above
specified by paragraph and
engineering data necessary for
for the entire repair.
—END
aspects only of the above Ilsted
only for the engineering data. It Indicates
compliance only with the regulations
listed below as 'Applicable Requirements."
FAA approval of all the
of compliance to necessary requirements
a. PURPOSE OF DATA: Engineering data to support repair procedure for Textron 400A Forebody May PIN N541000-004,
S/N R0010 under Nextant Aerospace Work Order No.10565.1.1.
9. APPLICABLE REOUREMENTS (LMIIPodfic MadanN
CFR nee 14 Pad 25.301[25-23], 25.303(25.23], 25.305(a)(b)(cX25-23), 25.307(aX25-23), 25.801[25-00),
25.603(aXb)(c)[25-38], 25.605(a)(25-00), 25.807[25-23), 25.609(a)(bX25-001, 25.811[25-23), 25.613(eXbXcX25-00),
25.619[25-23), and 25.625(aXbXcX25-23).
10. CERTIFICATION - WON surely veiled byAvalon of the Adeninistrstor end I n azeardance WM conekns end IrkatIons of appolnonent under I 4 CFR
Pert 163. data bled above and cn attached thetas numbered N/A have been exalted In accordance wilh colablahed procedurea and found to complyv/4h
aPIANON requarrmega of the AINronnIness Standards Listed
p Recommend approval of these data
I (We) Therefore
El Approve Omni dale
I I. SIGNATURES) OF DESIGNATED ENGINEERNO REPRESENTAT1VE(SI
12. DESIGNATION NU)eERS(S)
13. CLASSFICATION(S)
ptridia
..----C.o.
DENT-410115-CE
Structures
FM Form 8110-3 (03.10) SUPERSEDES PREVIOUS EDITION
Flle Number H18777-01
Page 1 of 1
EFTA00011675
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EFTA00011676
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nextant aerospace
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I EO Ik NT-EO•1118-31
I Tine: Engine Intet Rivet Repelt
ENGINEERING ORDER
ARTICLE DESCRIPTION
Locklithaageke
Teatret Aviden 400A
Alrenol Soorial Naait)
See Rerrans
onnette nier Mam
Die purpose of Ibis EO is to am for te ins:asem "kid Sits gmt CR32124-XX)of »vroor-iet° lengt in pace of te damaged sol» rivet (PIN: MS20426AD5-XX)on tie
enge Int» forebody neemt*: The repair wil be accennistied on It» RH engen ijkt forelndy assembly (PIN: N541000-004. Sin. Ft0010)
REGULATORY
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remenitenyeas
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Resafidaterom
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PM: N541000-004
SIN: R0010
Wtr. 10565.1.1 (Original WO. IR wit approval) 13003 (IR.1 WO)
OberrytAex Proclise Specificeer:n: CA;1015
REVISION
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CfACRPTION
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Form No. NT.E0-01 I Ree A
Page 1013
This Document h Unzontroted Onc• Ptt:lied
EFTA00011677
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EFTA00011678
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nextant aerospace
ITEM
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EO a: NT.EO1118-31
DISTRUCTIONS
Title: Engine Inlet Rivet Repair
ENGINEERING ORDER
PROCEDURES
Visually rasped the engine inlet hp and barrel for any other damaged, missing a loose bsteners.
• If no addennal discrepancies are detected, calla° with repair as °dined below.
- If additional descepamies me rant canted Nettie Aerospace la depositors
CiEs•C«
Visualy inspect No engine roan es defined in Sib Task 724140420-801of hi Mann Inlombonel LivE WtINTENANCE
MANUAL- FJ443AP 111030402 (blest re'
).
• If no additional cracrepanOes are detected. conatie with repair u coined below.
• If Mai:anal durepancies me noted. corded Nettant Aerospace for deposition.
NVE
C.A.C.
OSS
e
41/ 2
Cs4.c,
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Locale damaged rivets as shown in Figure 1 end carefully and completely dal al the remaining hateier material. making sure not to
damage, ably, a oversize the fastener hole.
Prepare the holed the missing bsteners for instillation of Caiegyailax Riven RN CR3212-5.XX in feu of nominal solid rivets