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METADATA_SOURCE: .
METADATA_FILENAME: EFTA00011669.pdf
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el, --
MAJOR REPAIR AND ALTERATION
US Department
Of Tm114104/111011
(Airframe, Powerplant, Propeller, or Appliance)
FOsteral Aviation
Adednitrallen
OM No.21200020
Exp. 541/2011
Ettoternie TM:alp Wetter
Ems.
For FAA Use °My
INSTRUCTIONS: Pita or type all entries. See Title 14 CFR §43.9. Part 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for
instructIons and disposition of tNs form. This report Is required by law (49 U.S.C. §44701). Failure to report can result Ina mil penally for each
such violation. (49 U.S.C. §46301(a))
1. Aircraft
Nationality and Registration Mark
UNITED STATES / N188TS
Serial No. RK-244
'make
RAYTHEON AIRCRAFT COMPANY
Model
400A
Series
2. owner
Name (As shown on registration certificate)
THORAIR LLC
Address As shown on registration certificate)
Address
04.
SANDUSKY
SUM OHIO
re
44871-2218
cam/
UNITED STATES
3. For FAA Use Only
4. Type
5. Unit Identification
Repair
Alteration
Untt
Make
Model
Serial No.
ril
I
I
AIRFRAME
MYTHEOMARCROST COWAIN
(As described in Item I above)
RK.244
K
POWERPLANT
K
PROPELLER
APPLIANCE
Type
Manufacturer
I Conformity Statement
A. Agency's Name and Address
B. Kind of Agency
in
Coastal'. Aviation LLC
U. S. Genic/mad Mechanic
I Idanufaclurer
Meese
Foreign Cerbhcated Ilechanic
C. Certificate No.
cis
CLEVELAND
sys OH
Conticaled Repair Station
ai
44143
c.,,,,,,,, USA
Certificated Maintenance organization
CRS#WC7R346J
D. I certify That the repair and/or alteration made to the una(s
have been made In accordance with the requirements of
furnished herein is true and
Identified
Part
In Item 5 above and described on the
of the U.S. Federal Aviation Regulations
reverse or attachments hereto
and That the Information
Extended range fuel
per 14 CFR Part 43
App. B
10/04/2019
umTotemic.
Pursuant to the authority g
Administrator of the Federal
i,
rsons spec ' • ..
, t e un
Administreti• ' and is
n leg
I
In Item 5
Approved
vial nspected in the manner prescribed by the
Rejected
BY
—
Manufacturer
Maintenance Organization
—
Persons Approved by Canadian
Department of Transom'
____j
FM RI Standards
Inspector
FM Designee
MI
Repair Station
pectIon Authorization
Other (Specify)
Certificate or
Desi nation No. CRS#
WC7R346J
Signature/Da
f Author ed Individual
__
...._---------
10/04/2019
FAA Form 337 (10/06)
Page I
EFTA00011669
--- PAGE 2 ---
NOTICE
Weight and balance or operating limitation changes shall be entered In the appropriate aircraft record. M alteration must be
compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements.
S. Description of Work Accomplished
(Il more space is moulted. attach additional sheets. Identify mitt steal? nationally end registratIon m** end date work completed)
UNITED STATESIMOSTS
mov2019
Nationality and RegistraMn Mark
Date
Engine Inlet Rivet Repair
Installed blind rivets in place of the damaged solid rivets on the lip of the right hand engine inlet
forebody assembly part number 541000-004, serial number R0010, In accordance with nextant
aerospace engineering order NT-EO-1118-31 rev IR dated 11/29/2018 with FM form 8110-3
dated 11/30/2018.
Instructions for Continued Airworthiness: Follow the maintenance inspection practices in the
aircraft maintenance manual. Inspection intervals shall remain as indicated in the aircraft
maintenance manual or operators approved inspection program as appropriate.
Weight and Balance unaffected.
Reference Constant Aviation work order CCM-3160
END
=Additional Sheets Arc Attached
FAA Form 337 (10/06)
Pagc 2
EFTA00011670
--- PAGE 3 ---
U.S. DEPARTMENT OF TRANSPORTAllON
FEDERAL AVIATION ADMINISTRATION
STATEMENT OF COMPLIANCE WITH AIRWORTHINESS STANDARDS
1. DATE
November 30, 2018
AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION
2. MANE
Textron Aviation
3. MODEL NO.
N541000-004
4. TYPE Mkorst &*e. Propeller, ea)
Forebody Assy
S. NAME OF APPLICANT
Nextant Aerospace LLC
Cleveland, Ohio
LIST OF DATA
SLREIffla
NT-EO-1118-31
Rev. IR
November 29, 2018
Engine Inlet Rivet Repair.
---
Notes:
1) The structural aspects only of the above listed data are approved herein. This
approval Is only for the engineering data. It Indicates the data listed above
demonstrates compliance only vAth the regulations specified by paragraph and
subparagraph listed below as 'Applicable Requirements."
2) This form constitutes FAA approval of all the engineering data necessary for
substantiation of compliance to necessary requirements for the entire repair.
e. PURPOSE OF DATA: Engineering data to support repair procedure for Textron 400A Forebody May PIN N541000-004,
SRN R0010 under Nextant Aerospace Work Order No.10585.1.1.