. . 1. Approving Competent Authority / Country 2. AUTHORIZED RELEASE CERTIFICATE 3. Form Tracking Number ... 633264 CAA/The Netherlands EASA FORM 1 4. Organization 0 ~ponent Services, Amsterdam Kruisweg 705, 2132 ND Hoofddorp, The Netherlands 5. Work Order /Contract/Invoice Name and P.O. Box 2130 AB Hoofddorp, The Netherlands Address: Tel: 31 (0)206552222 Fax: 31 (0)206534777 5017008642 I 6. Item 7. Description 8. Part No . 9. Qty 10. Serial No. 11 . Status/Work 1 CAB PRESS CONT 2117804-1 1 96-741 INSPECTED / TESTED 12. Remarks Item maintained in accordance with Component Maint. Manual 21-31-70, Revision 2, dated 29-Jul-2011 . The work identified in block 11 and described herein has been CSN: 27455, TSN : 24903 hours. accomplished in accordance with 14 CFR part 43 and in respect to that work, the items are approved for return to service under FAA certificate No. QT1Y438K. - Mod. status: Series 2. 138. Certifies the Items Identified above were manufactured In confonnlty to: 14a. 00 Part-145.A.50 Release to Service. 00 Other regulation specified in Block 12 D approved design data and are In a condition for safe operation Certifies that unless otherwise specified in block 12, the work identified in block 11 and described in block D non-approved design data specified In block 12 12 was accomplished in accordance with Part 145 and in respect to that work the items are considered !Bady for release to service. - ·' .. 13b. Authorized Signature 13c. ApprovaVAuthorlzatlan Ntmber 14b. Authorized Signature ilwa,,n! 14c. Certificate/Approval Ref. No. NL. 145. 1133 .. 13d. Name 138. Date (dd mmm yyyy) 14d. Name ® 14e. Date (dd mmm yyyy) F. P. de Waard 24 APR 2017 ' USER/INSTALLER RESPONSIBILITIES This certificate does not automatically constitute authority to install the item(s). Where the user/installer performs work in accordance with regulations of an airworthiness authority different than the airworthiness authority specified in block 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts items from the airworthiness authority specified in block 1. Statements in blocks 13a and 14a 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. EASA Form 1 -MF/145 -issue 2
22
Embed
2. AUTHORIZED RELEASE CERTIFICATE 633264 CAA/The ... · This is to certify that within the provisions of STANAG 4107 , AQAP2070 and the agreed RGQA , the services identified above
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
. . 1. Approving Competent Authority / Country 2. AUTHORIZED RELEASE CERTIFICATE 3. Form Tracking Number
... 633264 CAA/The Netherlands EASA FORM 1
4. Organization
0 ~ponent Services, Amsterdam
Kruisweg 705, 2132 ND Hoofddorp, The Netherlands 5. Work Order/Contract/Invoice
Name and P.O. Box 2130 AB Hoofddorp, The Netherlands
Item maintained in accordance with Component Maint. Manual 21-31-70, Revision 2, dated 29-Jul-2011 . The work identified in block 11 and described herein has been
CSN: 27455, TSN: 24903 hours. accomplished in accordance with 14 CFR part 43 and in respect to that work, the items are approved for return to service under FAA certificate No. QT1Y438K.
-
Mod. status: Series 2.
138. Certifies the Items Identified above were manufactured In confonnlty to: 14a. 00 Part-145.A.50 Release to Service. 00 Other regulation specified in Block 12
D approved design data and are In a condition for safe operation Certifies that unless otherwise specified in block 12, the work identified in block 11 and described in block
D non-approved design data specified In block 12 12 was accomplished in accordance with Part 145 and in respect to that work the items are considered !Bady for release to service .
13d. Name 138. Date (dd mmm yyyy) 14d. Name ® 14e. Date (dd mmm yyyy)
F. P. de Waard 24 APR 2017 '
USER/INSTALLER RESPONSIBILITIES This certificate does not automatically constitute authority to install the item(s).
Where the user/installer performs work in accordance with regulations of an airworthiness authority different than the airworthiness authority specified in block 1,
it is essential that the user/installer ensures that his/her airworthiness authority accepts items from the airworthiness authority specified in block 1.
Statements in blocks 13a and 14a 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
Incoming inspection :Item visually inspected and found ok. Complaint not confirmed.
Work performed:
Actual work :
Mod. status :
Remarks:
Temperature tested, hot and cold found ok. All functions found in normal condition.
Inspected/ Tested
Unit tested and found serviceable.
Note: If any parts were replaced, a record of parts used as replacements is being held at AAA. This record is available upon request.
Series 2.
Item maintained in accordance with Component Maint. Manual 21-31-70, Revision 2, dated 29-Jul-2011 .
CSN: 27455, TSN: 24903 hours.
Shop Manager: H.A. Pauw
24-Apr-2017
--------,-
I
Certificate of Conformance (only signed if released under non-civil aviation regulations)
This is to certify that the services to the component as described above conform in all A~thorized : respects to the specification(s) , drawings and order relative thereto and that the component Signature has been inspected and tested i.a.w the conditions and requirements of the order and was found airworthy for return to service.
I This is to certify that within the provisions of STANAG 4107, AQAP2070 and the agreed RGQA, the services identified above have been subject to Government QA and are
I considered to comply with the provisions of the applicable contract.
,--
Apr. 24, 2017 Docld:JSR001· 1013739
GOAR Signature
AAA Form No.~~Rev. Ju-;;0101
FAA Air Agency Certificate QT1 Y 438 K - EASA Approval Certificate NL.145.1133
I. Approving Competent Authority/Count!)' ,
CAA-NL / THE NETHERLANDS 2. AUTHORISED RELEASE CERTIFICATE·,
EASAFORM 1
3. Form Tracking Number
1316004030
4. Approved Organisation
Name and Address :
Fokker Services B.V. Hoeksteen 40 2132 MS Hoofddorp THE NETHERLANDS
Location Oude Meer
6. Item 7. Description 8. Part No
1 HIGH PRESSURE SHUTOFF VALVE 778686-3
12. Remarks - USED DOCUMENTATION: CMM 21-32-06 REV 9 DATE DEC 18/ 13 -Accompanying shopfinding report is part of this EASA Form I -
USER/INSTALLER RESPONSIBILITIES This certificate does not automatically constitute authority to install the item(s).
5. Work Order/ Contract/ Invoice
9. Quantity
I EA
9-94025
I 0. Serial No
840235
11 . Status/Work
REPAIRED
The work identified in Block 11 and described herein has been accomplished in accordance with 14 CFR part 43 and in respect to that work, the items are approved for return to serviae under certificate no. NQ I Y357K. Perti,1ent details of the repair are on file at this repair station under the order number referenced in block 3.
[xi Part- t1S.A.S0 Release to Service [xi Other regulation specified in Block 12 Certifies that un1:ss otherwise specified in block 12, the work identified in block 11 and describ d in block 12, was~ ccomplished m accordance with Part-145 and in respect to that work the items are considered re:::dy for release to service.
14b. Authorised Signature
14d. Name Adnan Hanif
14c. Certificate/ Approval Ref. No NL.145.1174 14e. Date (dd MMM yyyy) 14 JUL 2016
Where the user/installer perfonns work in accordance with regulations of an airworthiness authority different that the airworthiness authority specified in block I, it is essential that the user/installer ensures that his/her airworthiness authority accepts items from the airworthiness authority specified in block I. Statements in blocks 13a and 14a do not constitute installation certification. 1n all cases aircraft maintenance records must con ain an installation certification issued in accordance with the national regulations by the user/installer before the aircraft may be flown.
-ASAFonn I-MF/ 1451ssue2
Fokker Services B.V. Location Oude Meer Hoeksteen 40 2132 MS Hoofddorp
..._ GKNAEROSPACE THE NETHERLANDS Internet: www.fokkerservices.com
Shop Finding Report Page: 1 of 2
Technician Deliverv: COMMUTAIR Attn: Mr. Craig Hatch, Records Manager 85 SICKER ROAD 12110 NY LATHAM USA Tel. : 518-690-9080 120 Fax : 518-690-9079
For Customer : COMMUTAIR 5.0. No. : 2516012043 Line No. :
Cust P.O. : 9-94025 P/N : 778686-3 Batch/Lot Our Ref# Desc : HIGH PRESSURE SHUTOFF VALVE Cust.Ref Contract# :AG-003477 S/N :840235 Work Perf. Vend Ref# : R0281316 MFG : HAMIL TON SUNDSTRAND Manual Project# : N837CA Qty : 1.00000 Cond As:sv Revision Completed P/N: 778686-3 S/N As : 840235 Into Bin Loe : l!:ompanv : 1 Division : 12 I Deoartment : 2400 Contract No. :AG-003477 Type : Exchanae / Repair/ Lease Stock Order Date : May-20-2016 Received Date: May-20-2016 Due Date : Jul-19-2016 I Print Date : Jul-14-2016
WORK ORDER No. 1316004030 Contract No. AG-0034 77 - Exchange I Repair/ Lease Stock Re~orted B:i Customer LH HP BLEED INOP
UNIT SUBMITTED FOR REPAIR AND RETURN TO SERVICE REPAIR TO LATEST MOD STATUS Receiving Condition UPON RECEIPT NO VISUAL DAMAGE lns~ection -INCOMING TEST FAILS:
-SOLENOID DEFECT NOT WORKING AT ALL. -SHUTOFF VALVE DIRTY. -SEALS DIRTY.
- LATEST MOD IS L3 ALREADY INCORPORATED.
Name: Date: Sign:
1 4 JUL 2016 (s1~2s) · /1.V"'"°
A, HANIF ,ov iS's i:iv1c~'<i ·
Continued on next page ...
Copyright (c) PENTAGON2000Software, Inc. Ser #:(2003.70129] Ver 9.00.03 Build 20
.
Fokker Services B.V. Location Oude Meer Hoeksteen 40 2132 MS Hoofddorp
.._ GKNAEROSPACE THE NETHERLANDS Internet: www.fokkerservices.com
Shop Finding Report WORK ORDER No. 1316004030
- USED INTERNAL INSTRUCTIONS: AWi H-01141 REV:B DATE 11 MAY 2016 Action Taken - SOLENOID AND SEALS REPLACED. - CLEANED UNIT. - NO FAILURES WERE FOUND DURING FINAL TEST.
Item Part Number/ Description
PARTS & MATERIALS- 1 17 747767-1
SOLENOID 3 69494J13
SEAL 18 69494J12
SEAL
,
.
.
Name:
Copyright (c) PENTAGON2000Software, Inc. Ser #:[2003. 70129] Ver 9.00.03 Build 20
CAA-NL I THE NETHERLANDS 2. AUTHORISED RELEASE CERTIFICATE
EASAFORM l
3. Fonn Tracking Number
1316001807
4. Approved Organisation
Name and Address :
Fokker Services B.V. Hoeksteen 40 2132 MS Hoofddorp THE NETHERLANDS
Location Oude Meer
6. Item 7. Description 8. Part No
1 HIGH PRESSURE SHUTOFF VALVE 778686-3
12. Remarks -Accompanying shopfinding report is part of this EASA Fonn I -- USED DOCUMENTATION: CMM 21-32-06 REV 9 DATE DEC 18/ 13
USER/INSTALLER RESPONSIBILITIES This certificate does not automatically constitute authority to install the item(s).
5. Work Order/ Contract/ Invoice
9. Quantity
I EA
9-92698
10. Serial No 11. Status/Work
960513 INSPECTED/TESTED
The work identified in Block 11 and described herein has been accomplished in accordance with 14 CFR part 43 and in respect to that work, the items are approved for return to service under certificate no. NQ I Y357K. P•minent details of the repair are on file at this repair station under the order number referenced in block 3.
14a. [xi Part-145.A.50 Release to Service [xi Other regulation specified in Block 12
Certifies that unless otherwise specified in block 12, the work identified in block 11 and describ d in block 12, was accomplished in accordance with Part-145 and in respect to that work the items are considered ready for release to service.
14b. Authorised Signature
14d. Name
Adnan Hanif
14c. Certificate/ Approval Ref. No NL.145.1174 14e. Date (dd MMM yyyy)
03 MAR2016
Where the user/ installer performs work in accordance with regulations of an airworthiness authority different that the airworthiness authority specified in block I, it is essential that the user/ installer ensures that his/her airworthiness authority accepts items from the airworthiness authority specified in block I .
Statements in blocks 13a and 14a 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.
EASAFonn 1-MF/ 145 lssue2
Fokker Services B.V. Location Gude Meer Hoeksteen 40 2132 MS Hoofddorp
~ GKNAEROSPACE THE NETHERLANDS Internet: www.fokkerservices.com
\
Shop Finding Report Delivery: COMMUTAIR Attn: Mr. Craig Hatch, Records Manager 85 SICKER ROAD 12110 NY LATHAM USA Tel. : 518-690-9080 120 Fax: 518-690-9079
For Customer : COMMUTAIR 5.0. No. : 2516005286 Line No. :
Cust P.O. : 9-92698 P/N : 778686-3 Batch/Lot Our Ref# Desc: HIGH PRESSURE SHUTOFF VALVE Cust.Ref Contract# :AG-003477 S/N :960513 Work Pert. Vend Ref# MFG : HAMIL TON SUNDSTRAND Manual Project# : N361PH Qty : 1.00000 Cond As:sv Revision Completed P/N: 778686-3 S/N As : 960513 Into Bin Loe : Comoanv : 1 Division : 12 I Deoartment : 2400 Contr~ct No. :AG-003477 Tvoe : Exchanqe i Reoair / Lease Stock
· Order Date : Feb-29-2016 Received Date: Feb-29-2016 Due Date : Mar-13-2016 I Print Date It
. WORK ORDER No.1316001807 ..
Contract No. AG-003477 - Exchange/ Repair/ Lease Stock ReQorte.d B:t Customer 8 PSI ON DEICE PRESSURE GAUGE WHEN PERFORMING PROCEDURE PER MEL ~EPAIR TO LATEST MOD STATUS Receiving Condition ) ,:,ON RECEIPT NO VISUAL DAMAGE
3Qection -INCOMING TEST: NO FAILURE FOUND DURING THE TEST.
-USED INTERNAL INSTRUCTIONS: AWi H-01141 REV:A
Action Taken · NO FAILURE FOUND DURING THE FINAL TEST.
Name: Date:
A, HANIF 0 3 MAR 2016
Copyright (c) PENTAGON2000Software, Inc. Ser #: [2003.70129] Ver 9.00.03 Build 15
DATE 03-12-2012
Sign:
(s1~2s) ttW"I .~~~ -se,qv,c~c;i
Page: 1 of 1
: Mar-03-2016
I. Approving Competent Authority/Country
CAA-NL I THE NETHERLANDS 2. AUTHORISED REL~ASE C , RTIFICATE
EASAFORM 1
3. Form Tracking Number
1315004674
4. Approved Organisation
Name and Address :
6. Item 7. Description
Fokker Services B. V. Hoeksteen 40 2132 MS Hoofddorp THE NETHERLANDS
VALVE PACK TEMP CONT
Location Oude Meer
8. Part No
778727-7
12 . Remarks • Accompanying shopfmding report is part of this EASA Form I · USED DOC.
CMM : 21-61-47 REV.: 7 DATE: FEB 10/ 11
USER/INSTALLER RESPONSIBILITIES This certificate does not automatically constitute authoiity to install the item(s).
5. Work Order/ Contract/ Invoice
9. Quantity
I EA
9-88628
10. Serial No II. Status/Work
9610077 REPAlRED
Certifies that the work specified in block 11 / 12 was carried out in accordance with FAR part 43 and in respect to that work the part(s) is (are) approved for return to service for FAA Repair Station: Fokker Services B.V. under FAA Approval Number: NQ I Y357K Pertinent details of the repair are on file at this repair station under the order number referenced in block 3
Date: 15JUN2015 ,-:Ji}--Name: Albert van Dasler Signature: ~
14a. [xi Part-145.A.50 Release to Service [xi Other regulation specified in Block 12
Certifies that unless otherwise specified in block 12, the work identified in block 11 and described in block 12, was accomplished in accordance with Part-145 and in respect to that work the items are considered ready for release to service.
14h. Authorised Signature
14d. Name
Albert van Dasler
14c. Certificate/ Approval Ref. No
NL.145.1174
14e. Date (dd MMM yyyy)
15 JUN 2015
Where the user/installer perfonns work in accordance with regulations of an airworthiness authority different that the ailworthiness authority specified in block I, it is essential that the user/installer ensures that his/her airworthiness authority accepts items from the airworthiness authority specified in block I.
Statements in blocks 13a and 14a 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.
EASA Fonn I-MF/ 145 Issue 2
Fokker Services B.V. Location Oude Meer Hoeksteen 40 2132 MS Hoofddorp THE NETHERLANDS Internet: www.fokkerservices.com
Shop Finding Report Page: 1 of 2
Delivery : COMMUTAIR Attn: Mr. Craig Hatch, Records Manager 85 SICKER ROAD 12110 NY LATHAM USA Tel. : 518-690-9080 120 Fax : 518-690-9079
For Customer : COMMUTAIR S.O. No. : 2515014918 Line No. :
Cust P.O. : 9-88628 P/N : 778727-7 Batch/Lot Our Ref# Desc : VALVE PACK TEMP CONT Cust.Ref Contract# :AG-003477 S/N : 9610077 Work Perf. Vend Ref# MFG : HAMIL TON SUNDSTRAND Manual Project# : N379PH Qty : 1.00000 Cond As:sv Revision Completed P/N : 778727-7 S/N As : 9610077 Into Bin Loe :
C(~1';Janv : 1 Division :12 I Department : 2400 Contract No. :AG-003477 Type : Exchange / Repair i Lease Stock Orger Date : Jun-08-2015 Received Date: Jun-04-2015 Due Date : Jun-23-2015 I Print Date : Jun-15-2015 ,,.,,, <nn ' '.: ,,
+t W40RI( ORDER No~ 1315Q04~74 I
iii ' ' "''"; w,;;,' 0 Ji f,
-' Contr.act No. AG-003477 - Exchange/ Repair/ Lease Stock -ReQorted Bl Customer REMOVAL REASON REPORTED BY CUSTOMER: CABIN DOES NOT COOL DOWN DUCT TEMP OF 20 C IN FLIGHT
MAINTENANCE TAG REMOVAL REASON: TROUBLESHOOTING
BOX#46173
Receiving Condition SHIPPING CONTAINER CONDITION: OKAY lnsQection USED INTERNAL INSTRUCTIONS : AWi : H-01149 REV. : C DATE : 30 AUG 2010
INCOMING TEST FAULT : - POSITION OF THE LINK OF THE THROTTLE VALVE IS NOT CORRECT INSTALLED Action Taken
Name: Date: "'1(; G'i'Ok1r(', A ~
A.van Dasler .s>g1118 )
15 JUN 2015 '9111c1;.S
Continued on next page ...
Copyright (c) PENTAGON 2000 Software, Inc. Ser #:(2003.70129) Ver 9.00.02 Build 19
Fokker Services B.V. Location Oude Meer Hoeksteen 40 2132 MS Hoofddorp THE NETHERLANDS Internet: www.fokkerservices.com
Shop Finding Report Page: 2 of 2
WORK ORDER No. 1315004674 .
INSTALLED LINK OF THE THROTTLE VALVE CORRECT POSITION COMPLETE UNIT TESTED PERFORMED FINAL TEST; NO FAILURES WERE FOUND .
..
Name:
A. van Dasfer
Copynght (c) PENTAGON 2000 Software, Inc. Ser #:[2003.70129) Ver 9.00.02 Build 19
Date:
15 JUN 2015
.. _,
I. Cot1ntry 2 3. Certificate Re f" :'\o.
THE ~ETHERLAI\'DS CERTIFICATE OF C01'FORMITY 1215027017 / 14967430
4. Organization Fokker Services B.V. Location Oudc Meer 5. Work Order/ Contract/ Invoice Hoeksteen 40 Hoofddorp, 2132 MS 9-88628 THE NETHERLA DS
6. Item 7. Description 8. Part No 9. Eligibility* IO. Qty 11 . Serial No. 12. Purchase Condition
VALVE PACK TEMP CONT 778727-7 N/A I 9610077 SERVICEABLE EA
14. As an authorised representative of Fokker Services B. Y. for subject matter, I hereby certify that 18. As an au sed representative of Fokker Services B. V. for subject matter, we are a di stributor in compliance with ISO 9001 :2000 and AS 91 OOC, and are enclosing a copy I hereby certify tha are a distributor in compliance with ISO 900 I :2000 S 9100C. of the appli cab le airworthiness certifi cate from the PAHi OEM or Maintenance Station. The parts described above been maintained in a controlled envi ent throughout the duration The original is being maintained on file at Fokker Services B.V. 0f storage at the relevant Fokker Se s B. V. facility, and t C's received with the parts To the best of our knowledge. are on file at Fokker Services BY. based on the information provided by the supplier, the parts described above were not obtained from any government or military source nor were they incident or accident rel ated.
IS .Name 16. Signa1'?} {l 19. Name 20.S~
::,;0¥-Kf=A ,£, J~_"") Troy Tew (Fsf602J 17. Date (i MMMfYl>'YY 21 Date (dd/MMM/yyyy~ iS,E'RV10'i;: 17/J UN/ 15 --
COC Form - Issue I
1. Approving Civil Aviatior\ 2. Authority/Country
FAA/ UNITED STATES
4 . Organization Name and Address:
6 . Item: 7. Descri tion:
1 RECIRCULATION FAN
12. Remarks:
AUTHORIZED RELEASE CERTIFICATE FAA FORM 8130-3, AIRWORTHINESS APPROVAL TAG
NORTH BAY AVIATION 424 EXECUTIVE CT N S:E E FAIRFIELD, CA 94534-4019 (UYVR051J) Tel : 707-863-4970 / Fax: 707-863-4968
8. Part Number: 9 . Quantity :
778728-6 1
10. Serial Number:
850548
3. Form Tracking Number:
59108-15
5. Work Order/Contract/Invoice Number:
59108
11 . Status/Work:
INSPECTED
Serviced in accordance with CMM/DWG GEK 118268 revision 2_ issued FEB 03 2014 . No SB's or AD's were complied with .
Full details of work documented on Work Order No. 59108.
This repair station certifies that the work specified in Block 11/12 was carried out in accordance with EASA Part-145 and in respect to that work the
com anent is considered read for release to service under EASA Part-- 145 A roval Number: EASA.145.5308.
14a.~ 14 CFR 43.9 Return to Service ~ Other regulation specified in Block 12
Certifies that unless otherwise specified in Block 12, the work identified in Block 11 and described in Block 12 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):
JULIAN CEBALLOS
User/ Installer Responsibilities
14c. Approval/Certificate No.:
UYVR051J 14e. Date ( dd/mmm/yyyy):
02 I Sep/ 2015
It is important to understand that the existence of this documer.t alone does not automaticaliy constitute authority to install the aircraft engine/propeller/article.
Where the user/installer performs work in accordance with the national regulations of an airNorthiness 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 acc,~pts aircraft engine9s)/propeller(s)/article(s) from the airworthiness authority of the country
specified in Block 1 .
Statements in Blocks 13a and 14a 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 (02-14) NSN 0052-00-012-9005
NORTH BAY AVIATION 424 Executive Ct. N. Ste. E Fairfield, CA 94534-4019
' 14. As an authorised representative of Fokker Services B. V for subject matter, I hereby certi fy that 18. As an au ·sed representative of Fokker Services B.Y. for subject matter, we a re a di stributor in compliance with ISO 900 I :2000 and AS 91 00C, and are enclosing a copy I hereby certify tha a re a di stributor in comp liance with ISO 900 l :2000 S 9l00C. of the app licable a irworthiness certificate from the PAHi OEM or Maintenance Station. T\1e parts described above been maintained in a controlled envi 11ent throughout the duration The orig inal is being mainta ined on file at Fokker Services B.V or torage a t the rel evant Fokker Ser s B.Y. facility, and t C's received with the parts To the best of our knowledge, a eon fil e at Fokker Services BY. based on the information provided by the suppli er, the parts described above were no t obtain ed ' from any government or military source nor were they incident or acc ident re lated. I
15.Name !IL.a: ':?.Pl- ~
20.S~ ~0KKE,9
Jimmy Bacon (Fsioo5J .S£RVlG~ 17 /)ate (cllflM MM/yyyy) 21 Date(dd/MMM/yyyy~
Serviced in accordance with CMM/DWG GEK 118268 revision i issued FEB 03 2014. No SB's or AD's were complied with. Full details of work documented on Work Order No. 58640.
This repair station certifies that the work specified !n Block 11 /12 was carried out in accordance with EASA Part-145 and in respect to that work the com onent is considered read for relea~e to service under EASA Part-145 A roval Number: EASA.145.5308. 14a.[8] 14 CFR 43.9 Return to Service [8J Other regulation specified in Block 12
Certifies that unless otherwise specified in Block 12, the work identified in Block 11 and described i~ Block 12 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.
EUGENE GOODMAN
14c. Approval/Certificate No.:
UYVR051J 14e. Date (dd/mmm/yyyy) :
13/Jul/2015
It is important to understand that the existence of this document alone does not automatically constitute authority to install the aircraft engine/propeller/article. Where the user/installer performs w_ork in accordance with _the nat!onal r~gulations of_an airworthi~ess auth~rity different than the _airworthiness authority of the country specified in Block
1, it is essential that the user/installer ensures that his/her a1rworth1ness authority accepts aircraft engine9s)/propeller(s)/art1cle(s) from the airworth iness authority of the country specified in Block 1.
Statements in Blocks 13a and 14a 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.
FM Form 81 30-3 (02-14) NSN: 0052-00-012-9005
'. 1. Approving Civil Aviation Authority / Country 2. 3. Form Tracking No.
- AUTHORIZED RELEASE CERTIFICATE Transport Canada W23274
Form One 4. Organization Name and Address 5. Work Order I Contract/ Invoice
GA C Global Aerospace Corporation, 7075 Fir Tree Drive PH: 905-678-6311
6. Item 7. Description 8. Part No. 9.Qty. 10. Serial / Batch No. 11 . Status I Work
1 Air Cycle Machine 782790-18 1 940394 Overhauled
12. Remarks:
* EASA Approval No. EASA.145.7031
* Overhauled in accordance with CMM # 21-51-53 Rev #16, dated 23 July 2014, and RDA# O-RA06-088/D, O-RA08-151 , O-RA05-037,
and O-RA05-260.
* Full details of work performed in work order W23274.
* For the replacement parts refer to Teardown Report.
- I~ the items identified above were manufactured in conformity to: 14a.
Approved design data and are in condition for safe aper · . [g] CAR 571 .10 Maintenance Release.
D Non a ved design data specified in blo ~ Other regulations specified in block 12.
Certifies that unless otherwise specified in block 12, the work identified in
block 11 and described in block 12, has been performed in compliance with the Canadian Aviation Regulations.
13b. Signature
~ 13~nization Number 14b. Signature
K·r:5~ }. 14c. Approved Organization Number
160-93
~ 13e. Date (dd/mmm/y~ 14d. Name
I~
14e. Date (dd/mmm/yyyy)
03/May/2017 Reza Bahra
(Previously form 24-0078) Important: See notes
Installer Responsibilities
This certificate does not constitute authority to install.
Installer working in accordance with the national regulations of a country other that that specified in block 1, must ensure that their regulations recognize certifications from the country specified .
Statements in blocks 13a and 14a do not constitute installation certification . In all cases, the technical record must contain an installation certification issued in accordance with the applicable
national regulations before the aircraft may be flown.
1. Approving Civil Aviation Authority I Country 2.
Transport Canada
4. Organization Name and Address
AUTHORIZED RELEASE CERTIFICATE
Form One
G Ac Global Aerospace Corporation, 7075 Fir Tree Drive Mississauga, Ontario, Canada.
* Overhauled in accordance with CMM # 21-51-53 Rev #16, dated 23 July 2014, and RDA# O-RA06-088/D, O-RA08-151, O-RA05-037, and O-RA05-260. 1
* Full details of work performed in work order W2327 4.
* For the replacement parts refer to Teardown Report.
l~if~t the items identified above were manufactured in conformity to:
I 7'----J_ Approved design data and are in condition for safe oper · . -------D Nona ved design data specified in blo
14a.
~ CAR 571 .10 Maintenance Release.
~ Other regulations specified in block 12.
Certifies that unless otherwise specified in block 12, the work identified in 1
block 11 and described in block 12, has been performed in compliance with the Canadian Aviation Regulations. '
13b. Signature ~ 13~proved Organization Number 14b. Signature ;'(: 1
£ _ / " 14c. Approved Organization Number
A..J~ 160-93 , I
(Previously form 24-0078)
This certificate does not constitute authority to install .
13e. Date (dd/mmm/y~ 14d. Name ~ 14e. Date (dd/mmm/yyyy) 1
~ Reza Bahra~i ~-·, ) 03/May/2017
Installer Responsibilities
Important: See notes
I
I Installer working in accordance with the national regulations of a country other that that specified in block 1, must ensure that their regulations recognize certifications from the country specified.
I
Statements in blocks 13a and 14a do not constitute installation certification. In all cases, the technical record must contain an installation certification issued in accordance with the applicable national regulations before the aircraft may be flown .
Global Aerospace Corp. 7075 Fir Tree Drive Mississauga, ON L5S 1J7 Canada Ph: 905-678-6311 , Fax : 905-678-6312
Ship To: Fokker Services Inc 456 Aerotron Parkway LaGrange,GA 30240 United States o
" Early failure - failed before reaching 1500 hours/cycles after installation . Investigate failure and advise root failure. Please perform repair under warranty. END."
Faults:
Snag Confirmed
1. Please refer report prepared by Quality Department & e-ailed by Debby. 2. Sump cover pin 782166-1 found damaged. 3. Drive shaft p/n 753385-2 damaged. 4. Turbine housing p/n 758073-111 cracked , dish repair required . 5. Turbine rotor p/n 785733-5 damaged. 6. Bearings damaged. 7. Other parts reauired as listed below.
PN Description Qty Needed Disposition .,·
094-0500MCP PIN, SPRING-SPIRAL 2 Consumable
094-0625MCP PIN.SPRING-SPIRAL 2 Consumable
540628 WIRE, SPRING 1 Consumable
570057-8 PIN, STRAIGHT HEADED 2 Consumable
6925384 IDENTIFICATION PLATE 1 Consumable
69494J111 PACKING 1 Consumable
69494J139 PACKING 1 Consumable
69494J154 PACKING, PREFORMED 1 Consumable
69494J262 PACKING, PREFORMED 1 Consumable I
69494J262 PACKING, PREFORMED 1 Consumable
69494K113 PACKING, PREFORMED 1 Consumable
69494K151 PACKING 1 Consumable
727455-11 BUSHING, WICK 2 Consumable t
738612-3 WASHER, TAB 1 Consumable
Form created with Quantum Con/rol(/m) technology. Product Licensed to: Global Aerospace Corp.
- =--Global Aerospace Corp. Tear Downllasoection 7075 Fir Tree Drive Work Order#: W23274 Mississauga, ON L5S 1J7 Date Printed: 4/26/17 Canada Ph: 905-678-6311, Fax: 905-678-6312 Time: 11 :45:34 AM
AUTHORIZED RELEASE CERTIFICATE Transport Canada W22912
For.m One 4. Organization Name and Address 5. Work Order / Contract/ Invoice
GA C Global Aerospace Corporation, 7075 Fir Tree Drive PH: 905-678-6311 Mississauga, Ontario, Canada. FX: 905-678-6312 5016015237 L5S 1J7 www.globalaeros~ace.com
6. Item 7. Description 8. Part No. I 9.Qty. 10. Serial / Batch No. 11 . Status / Work '
1 Air Cycle Machine 782790-18 1 HSM0111A Repaired
12. Remarks:
* EASA Approval No. EASA.145.7031
* Repaired in accordance with CMM # 21-51-53 Rev #16, dated 23 July 2014. * Full details of work performed in work order W22912.
* For the replacement parts refer to Teardown Report. * TSO- 2,162.60; CSO- 2,498.
•.
Certifies that the items identified above were manufactured in conformity to: 14a . • ~ Approved design data and are in condition for safe aper CAR 571.10 Maintenance Release.
·o Non a ved design data specified in blo ~ Other regulations specified in block 12.
Certifies that unless otherwise specified in block 12, the work identified in block 11 and described in block 12, has been performed in compl iance with the Canadian Aviation Regulations .
13b. Signature
~ 13~nization Number 14b. Signature
/ .IS~ 14c. Approved Organization Number
l 160-93
~ 13e. Date (dd/mmm/y~ 14d{ Name
CID 14e. Date (dd/mmm/yyyy)
Reza Bahrami 15/Sep/2016 C
(Previously form 24-0078) - Important: See notes
Installer Responsibilities This certificate does not constitute authority to install.
Installer working in accordance with the national regulations of a country other that that specified in block 1, must ensure that their regulations recognize certifications from the country specified.
Statements in blocks 13a and 14a do not constitute installation certification . In all cases , the technical record must contain an installation certification issued in accordance with the appl icable national regulations before the aircraft may be flown .
.. ,
Global Aerospace Corp. 7075 Fir Tree Drive Mississauga, ON L5S 1J7 Canada Ph: 905-678-6311 , Fax: 905-678-6312
Ship To: Fokker Services Inc 5169 Southridge Parkway Suite 100 Atlanta,GA 30349 United States o
" Cabin temp duct (Bleed air) over 60 degrees celcius when #2 engine started . Could not cool our plane down. Warranty check requested . END."
Faults:
Note
•• Unit previously overhauled in March 2015 •• 1. Screen/ mesh of containment housing damaged due to stones of air intake. 2. Stone marks on fan blades .
••• No fault found during testing ••• 1. Option 1 : Repair screen & unit tested & re-certified : Quote $ 1320.00 USD. 2. Ootion 2: Reoair screen , reolace fan o/n 762049-1 , retest & certifv: : Quote $ 2540.00 USD.
PN · Description " Qty Needed 69494J111 PACKING 1
69494J139 PACKING 1
69494J154 PACKING, PREFORMED 1
69494J262 PACKING, PREFORMED 1
69494K11 PACKING, PREFORMED 3
69494K151 PACKING 1
753443-2 GASKET OUTLET 1
753443-2 GASKET OUTLR 1
753453-40 SCREEN INLET 1
762049-1 FAN, COOLING 1
808519-3 WICK, NONMETALIC 2
89803 10-32 KEYSERTS, THINWALL UNF 1
Dispo~ition
Consumable
Consumable
Consumable
Consumable
Consumable
Consumable
Consumable
Consumable
Consumable
Consumable
Consumable
Repair
Form created with Quantum Control(tm) technology. Product Licensed to: Global Aerospace Corp.