EPSTEIN
page 4 / 530 . OCR, unverified
MS20426AD540C
• Prepare ham by aging and reaming to the required rivet Sae, as required, per ClwayMaa clocunent CA.1015
• Determine be correct gdp Sangth for to fasteners to be used. cabana Cherybax document CA-1015.
• Using the manufacturers reornmended installation ton install Ne reel fasteners per ChemyMax dowdiest CA.1015.
• Inspect the conedeted rivet set lo verify te lodeng coiled has been inserted and the stem has hazed flush with the rivet head.
Refer to Chemyttix anseent CA-1015 Ix Inspection ad verification.
-END
•
LAKTATIONS
None
INSTRUCTIONS FOR CONTINUING AIRWORTHINESS (ICA's)
Follow the maintenance inspection practices in Ne aircraft rnslaenevce manual. Inspection intervals shall roman as indicated vita eircrin't marilenanco manual or waralas
approved inspection program as appropnan
COMPLIANCE
AH.:RNI M0DEI
~AT
~TPA,»
t/uS8 13
San crIstAtall A
RSA WC7R346J
AlxaAfleB1W NIMILA
lc 2•Vel
DATE
10/27
Form No. NT.E0-01 I Rev A
Page 2 ol 3
This Document is Unconuolled Once Printed
EFTA00011679
--- PAGE 12 ---
•
•
•
EFTA00011680
--- PAGE 13 ---
ry
•
•
nextant aerospace
//REINiAGiNED //RESULT //MORN
EO /: NT-E0:11111-31
I Title: Engine Inlet Rivet Repair
ENGINEERING ORDER
Figure 1: Damaged Rivet Location on RH Engine Inlet Up (Typical Shown)
Page 3 ol 3
Form No. NT•EOA1 I Rev A
This Document Is Uncontrolled Once Printed
EFTA00011681
--- PAGE 14 ---
S
•
•
EFTA00011682
--- PAGE 15 ---
MAJOR REPAIR AND ALTERATION
US DepeVret
of Tranwortefon
(Airframe, Powerplant, Propeller, or Appliance)
Wend Avliclon
Adearileintlein
DNB ,40- 2120'0020
Exp. Pamela
Elearerie Track0g Witco
For FAA Use Only
INSTRUCTIONS: Print 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 oft* form. This report is required by law (49 U.S.C. §44701). Failure to report can result in a civil penalty lor each
such violation. (49 U.S.C. §48301(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 certiecate)
Address
coy
SANDUSKY
SYS OH
2p
44871
Cathy
UNITED STATES
3. For FAA Uso Only
4. Type
6. Unit identification
Repair
Alteration
Unk
Make
Model
Serial No.
I-1
m,
AIRFRAME
MYPEOP.A0CRAFT COMM"
(As described in Men; 1 above)
MOEN
POWERPLANT
PROPELLER
APPLIANCE
Type
Menet/were..
6. Conformity Statement
A. Agency's Name and Address
B. Kind of Agency
Now
CONSTANT AVIATION
U. & Caollkated Mechanic
I
Manufacturer
Adana
Foreign CatilloNed Mechank
C. Certificate No.
Ott
CLEVELAND
sew OR
i
♦
CalLated
Certificated Repair Stallion
CRS# WC7R346J
44143
Candy UNITED STATES
Maintenance Organ/wk.,
D. I certify that the repair andior alteration made to the unks Identified in Item 5 above and deathbed on the reverse or attachments hereto
have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the Information
furnished herein Is true and correct to the best of m knovA i • i i
Extended range fuel
per 14 CFR Part 43
Am. B
Sign
10/7/2019
7. A • proval for Return to Service
Pursuant to the authority paten persons specified below. the Lilt Wenn, In item 6 va tinspected
Administrator of the Federal Aviation Administration and la
I
Approved
In the mama prescribed by the
Rigel:led
BY
--"' FAA Fit. Standards
Inspector
—
Manufacturer
—
—
Maintenance OrgaNzatlon
Persons Approved by Canadian
Depaitrnen1 of Transport
=
FM Designee
I
^
Repair Station
Inspection Authorization
Other (Specify)
Certificate or
Designation No.
C RS#
WC7R346J
Signature) . e
uthori ed Individual
,,i
10/7/2019
FAA Form 337 (10/06)
Page 1
EFTA00011683
--- PAGE 16 ---
NOTICE
Weight end balance or operating Nmitallon changes shell be entered in the appropriate aircraft record. An alteration must be
compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements.
S. Description of Work Accomplished
al more space is requirec( attach additional sheets. Mandy *eh thrash nationally and registration mark and date oak completed)
mire, STATES /N1887/3
107/2019
Nationality and Registration Mark
Date
INSTALLATION OF ADS-B OUT ON PART 25 AIRCRAFT
Complied with installation of BHE & Associates, LTD. STC# ST11216DS Installation of Automatic
Dependent Surveillance-Broadcast Out on Part 25 Aircraft IAW BHE & Associates,LTD. Master
Data List (MDL) number 584-00-0001 Rev.G. Dated 8/29/2019.
Reference BHE & Associates, LTD. Aircraft Flight Manual Supplement (AFMS) Installation of
ADS-B Out on Part 25 Aircraft. Report number 584-00-0046 Rev.C. Dated 5/4/2019.
Reference BHE & Associates, LTD. Electrical Load Analysis (ELA) Installation of ADS-B Out on