I. Approving National Avi at ion Authority/Country 2 · AUTHORIZED RELEASE CERTIFICATE 3 · Form Tracking Number: FAA/United States FAA Form 8130-3, AlRWORTHINESS APPROVAL TAG ' . 4. Organization Name and Address: Hami lt on Sundstrand Worldwide Repair Windsor Locks Hamilton Sundstrand Division United Technologies Corporati on I Hamilton Road Windsor Locks, Cr 06096 S13R842L 6. lie 7. Descri lion MOTOR ANO PUMP. AUXILIARY 13. Rema rks Return to Service 8. Part Number 9. E li ibili NIA 782655-3 PART 4122-006009/782655-3 AND RECORDS WERE INSPECTED TO DETERMINE IT HAS NO TIME IN SERVICE SINCE MAINTENANCE AND / OR ALTERATION. PART WAS MODIFIED AS DOCUMENTED ON 8130-3 TRACKING NUMBER 121017 ATTACHED. ALL RECORDS ARE ON FILE AT THIS REPAIR STATION . THIS INSPECTION IS IN ACCORDANCE WITH FAA ORDER 8130-21 AS AMENDED. 15973 5642885 1.000 5. Work O rder / Contract/Invoice Number: w.o. 7665658 Cust. P.O. 9-77874 atch Number: 12. Status o rk INSPECTED TT TSO TSR TCSN UNK 41364.50 0.00 UNK Pertinent detail of the workscope identified in Block 12 are on file at this repair station under wor k order n o. ~ork performed by Repair Station SI3R842L 7665658 Certifies work specified in Bl ocks I 2/ 13 was ca rried out in accordance with EASA Part 145, and with respect to that work, the component is considered ready for release to service under EASA Part 145 Approval Number: EASA 145-4983. Other reg ul ation specified in Block 13 Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations, part 43 and in respect to that work, the items are approved for return to service. Name (Typed or Print ed : Hampson,Robert 21. Approval/Certificate No.: SI3R842L 23. Date (m/d/y): May212013 It is imponant to understand th at the existence of this document alone does not automatically constitute authority to insta ll the pan/ component/ assembly. Where the user / installer perfonns work in accordance with the national regulations of an airwo1thiness authority difTer cnt than th e airwonhiness authority of the country specified in Block I. it is essential that the user/insta ller ensures that his/her airwonhiness authori ty accept.~ pan s/components/assemblies from the airwo1thiness authority of the coun try spec ifi ed in block I. Statements in Block 14 and 19 do not constitute installa tion cenification. In a ll casl. 'S aircraft maintenance records must contain an insta llation cenification issued in accordance with the national regulations by the user/ insta ll er before the aircraft may be fl own. FAA Fonn 8 I 30-3 (06/0 I) *Installer must cross check eligibility with applicable technical data. NSN: 0052-00-01 2-9005
5
Embed
I . Approving Natio n a l 2 AUTHORIZED RELEASE ......I . Approving Natio n a l Aviation Authority /Country 2 · AUTHORIZED RELEASE CERTIFICATE 3 · Form Tracki ng Number: FAA/United
This document is posted to help you gain knowledge. Please leave a comment to let me know what you think about it! Share it to your friends and learn new things together.
Transcript
I. Approving National Aviation Authority/Country
2· AUTHORIZED RELEASE CERTIFICATE 3· Form Tracking Number:
FAA/United States FAA Form 8130-3, AlRWORTHINESS APPROVAL TAG ' .
4. Organization Name and Address: Hamilton Sundstrand Worldwide Repair Windsor Locks Hamilton Sundstrand Division United Technologies Corporation I Hamil ton Road Windsor Locks, Cr 06096 S13R842L
6. lie 7. Descri lion
MOTOR ANO PUMP. AUXILIARY
13. Remarks Return to Service
8. Part Number 9. Eli ibili
NIA 782655-3
PART 4122-006009/782655-3 AND RECORDS WERE INSPECTED TO DETERMINE IT HAS NO TIME IN SERVICE SINCE MAINTENANCE AND/ OR ALTERATION. PART WAS MODIFIED AS DOCUMENTED ON 8130-3 TRACKING NUMBER 121017 ATTACHED. ALL RECORDS ARE ON FILE AT THIS REPAIR STATION . THIS INSPECTION IS IN ACCORDANCE WITH FAA ORDER 8130-21 AS AMENDED.
15973
5642885 1.000
5. Work Order/Contract/Invoice Number:
w.o. 7665658 Cust. P.O. 9-77874
atch Number: 12. Status ork
INSPECTED
TT TSO TSR TCSN
UNK 41364.50
0.00 UNK
Pertinent detail of the workscope identified in Block 12 are on file at this repair station under wor k order no.
~ork performed by Repair Station SI3R842L
7665658
Certifies work specified in Blocks I 2/13 was carried out in accordance with EASA Part 145, and with respect to that work, the component is considered ready for release to service under EASA Part 145 Approval Number: EASA 145-4983.
~ Other regulation specified in Block 13
Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was accomplished in accordance with
Title 14, Code of Federal Regulations, part 43 and in respect to that work,
the items are approved for return to service.
Name (Typed or Printed :
Hampson,Robert
21. Approval/Certificate No.:
SI3R842L
23. Date (m/d/y): May212013
It is imponant to understand that the ex istence of this document alone does not automatically constitute authority to install the pan/component/assembly. Where the
user/installer perfonns work in accordance with the national regulations of an airwo1thiness authority difTercnt than the airwonhiness authority o f the country specified in
Block I . it is essential that the user/insta ller ensures that his/her airwonhiness authority accept.~ pans/components/assemblies from the airwo1thiness authority of the
country specified in block I. Statements in Block 14 and 19 do not constitute installation cenification. In all casl.'S aircraft maintenance records must contain an insta llation
cenification issued in accordance with the national regulations by the user/ installer before the aircraft may be flown.
FAA Fonn 8 I 30-3 (06/0 I) *Installer must cross check elig ibility with applicable technical data. NSN: 0052-00-012-9005
1. Approving National Aviation: 2. 3. Form Tracking Numbers:
Authority/Country: AUTHORIZED RELEASE CERTIFICATE 121017 FAA/UNITED STATES FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG
4. Organization Name and Address: AeroControlex Group, Inc. 4223 Monticello Blvd., South Euclid, OH 44121 (FAA PMA PQ2093CE) A34O423J
5. Work Order/Contract/Invoice Number: 1052773/MR20260
6. ltemsj7. Description: !8. Part Number: !9. Eligibility:* !10. Quantity: Serial/Batch Number: f 12. Status/Work:
13. Remarks
AUXILIARY PROPELLER FEATHERING PUMP
4122-006009 / 782655-3 15973
N/A MODIFIED
PUMP ASSEMBLY WAS MODIFIED FROM P/N 4122-006009 S/N UNK TO P/N 4122-006009 S/N 15973 MAND RETROFIT PER SERVICE BULLETIN 14SF-61-A165 ORIGINAL ISSUE DATE: SEP 25112, MANUFACTURES APPROVED DATA AND C.M.M. 61-21 -28 REV. 3 DATED APRIL 20, 2007. REF. P/N 782655-3 P.O.# 6626194 TSN:UNK CSN:UNK
AeroControlex certifies that the work specified in blocks 12/13 was carried out in accordance with EASA 145 and with respect to that work the aircraft component is considered ready for release to service under EASA Certificate Number EASA.145.6259.
Work Performed By: DAMON M.
P" 14 CFR 43.9 Return to Service P" Other regulation Specified in Block 13
Certifies that unless otherwise specified In Block 13, the work identified in Block 12
and described in Block 13 was accomplished in accordance with Title 14, Code of
Federal Regulations, part 43 and in respect to that work, the items are approved for
return to service.
21 .Approval/Certificate NO.:
A34D423J
23.Date(m/d/y):
APR/3/2013
User/Installer Responsibilities
It is important to understand that the existence of this document alone does not automatically constitute authority to install the part/component/assembly
When the user/installer performs work in accordance with the national regulations of an aiworthiness authority different than the airworthiness authority of the country specified
in Block 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country
specified in Block 1.
Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance
with the national regulations by the user/installer before the aircraft may be flown.
FAA FORM 8130-3(6-01) *Installer must cross-check eligibilty with applicable technical data. NSN :0052-00-012-9005
PROGRESSIVE INSPECTION: D REQUIRED [Z]NOT REQUIRED (2]1D TAG ISSUED
INSP.STAMP: 6 ~ REPAIR TAG ISSUED O uNSERVICEABLE TAG..1ssuED
WORK PERFORMANCE/CORRECTIVE ACTION : PUMP ASSEMBLY WAS MODIFIED FROM P/N 4122-006009 S/N UNK TO P/N 4122-006009 S/N 15973 MAND RETROFIT PER SERVICE BULLETIN 14SF-61-A165 ORIGINAL ISSUE DATE: SEP 25/12, MANUFACTURES APPROVED DATA AND C.M.M. 61-21-28 REV. 3 DATED APRIL 20, 2007. REF. P/N 782655-3 P.O.# 6626194 TSN :UNK CSN:UNK
REPAIR TECHNICIAN SIGNATURE: ',,..~,,~~
0 27 5_.,. DATE WORK:
+ro r.'-'-<, APR O 3 2013
WORK ORDER REVIEWED AND COMPLETE: INSP.STAMP:
'09 ~ MAINTENANCE RELEASE ISSUED D FAA FORM #337 D RETURNED AS 1s (NOT REPAIRED) .... ~"-o
CZJFINAL ACCEPTANCE
4 i 5,., -:,,_ "
INSP.STAMP V'r·· · . C •
..J
:,
COMPONENT RETURN-TO-SERVICE RECORD -,
THIS SECTION TO BE COMPLETED BY PARTS ROOM ,,
"· THIS SECTION TO BE COMPLETED BY MECHp:NIC/TE~HNICIAN ~)'_ SHOP LOG WORK ORDER / '/ '2 0 I -. !NITIAL I REP AIR I r I OVERHAUL I I ASSEMBLY
NUMBER ~,,;, EVALUATION I MODIFICATION I I INSPECT I Ril y I I N
DISCREPANCY
'.
SPACE IS PROVIDED ON BACK Of FORM FOR CONTINUATION OF CORRECTIVE ACTION(S) AND PART(S) USED RECORD