ESN 858790
TECHNICAL DATA
CFM56‐3C1
ESN 858790 Summary Information
• Engine Serial Number (ESN): 858790
• Engine Model: CFM56‐3C1
• Engine Total Time (ETSN): 30,052
• Engine Total Cycles (ECSN): 12457
• Reason for Last Shop Removal: Damage Observed on HPT Blades
• Engine Total Time Since Last Shop Visit (TTSLSV): 0
• Engine Total Cycles Since Last Shop Visit (TCSLSV): 0
• Last Operator: Turpial Airlines
• Last Installation: B737‐4H6 MSN 27352 ( A/C Reg YV621T )
ESN 858790 Summary Information
• Date of Shop Visit: February 2021
• MRO: Advanced Turbine Systems (ATS)
• Reason for Last Shop Removal: Damage on HPT Blades
• Engine Total Time at shop visit (ETSN): 0
• Engine Total Cycles at shop visit (ECSN): 0
• Date of Shop Visit: July 8th,2019
• MRO: FJ Turbine Power
• Reason for Last Shop Removal: TOP CASE REPAIR
• Engine Total Time at shop visit (ETSN): 48,778
• Engine Total Cycles at shop visit (ECSN): 31,997
ENGINE S/N: 858790TSN: 49345CSN: 32456
Removal Reason: HPT BLADES DAMAGESWork Order: TBC
Customer: TAARevision No.: 1
Revision Date: 26-Jan-21
ATA REF. BSI? REPLACE? MX LEVEL PROPOSED WORKSCOPE
21X FAN AND BOOSTER 72-21-00 NO NO MIN
22X NO.1 AND NO.2 BEARING SUPPORT ASSEMBLY 72-22-00 NO NO MIN
23X FAN FRAME ASSEMBLY 72-23-00 NO NO MIN
61X INLET GEARBOX AND NO.3 BEARING ASSEMBLY 72-61-00 NO NO MIN
63X ACCESSORY GEARBOX ASSEMBLY 72-63-00 NO NO MIN
62X TRANSFER GEARBOX ASSEMBLY 72-62-00 NO NO MIN
31X COMPRESSOR ROTOR ASSEMBLY 72-31-00 NO NO REPAIR TOP CASE REPAIR
32X COMPRESSOR FRONT STATOR ASSEMBLY 72-32-00 NO NO MIN
33X COMPRESSOR REAR STATOR ASSEMBLY 72-33-00 NO NO MIN
41X COMBUSTION CASE ASSEMBLY 72-41-00 NO NO MIN
42X COMBUSTION CHAMBER ASSEMBLY 72-42-00 NO NO MIN
51X HPT NOZZLE ASSEMBLY 72-51-00 NO YES REPAIR REPAIR AS APPLICABLE
52X HPT ROTOR ASSEMBLY 72-52-00 NO YES REPAIR REPAIR AS APPLICABLE
53X HPT SHROUD/STAGE 1 LPT NOZZLE ASSEMBLY 72-53-00 NO YES REPAIR REPAIR AS APPLICABLE
54X LPT ROTOR/STATOR ASSEMBLY 72-54-00 NO YES REPAIR REPAIR AS APPLICABLE
55X LPT SHAFT ASSEMBLY 72-55-00 NO NO MIN
56X TURBINE FRAME ASSEMBLY 72-56-00 NO NO MIN
NO LLP REPLACEMENT AT THIS SHOP VISIT
FUEL NOZZLE TO FLOW CHECK
POST TEST VIDEO BSI & REPORT
AD 2013-26-01 - AGB Handcranking pad cover inspection
AD 2017-14-08 - Perform paragraph (f)(3) Repetitive Inspection of Pull Force Check of Stages 1, 3 & 3 of the Compressor VSV Actuation SystemPOST TEST PRESERVATION FOR 365 DAYS.
SINGLE RELEASE CERTIFICATE (FAA)
Technical Aviation Advisors
SPECIAL INSTRUCTIONS
FAN
SECTIO
N
72-2
0-0
0
ACCESSO
RY D
RIV
E
SECTIO
N
72-6
0-0
0
HPC S
ECTIO
N
72-3
0-0
0
CO
MBU
STIO
N
SECTIO
N
72-4
0-0
0
OUTGOING ENGINE MPA RUN IAW AMM 71-00-00 Test N0. 5
INCOMING ENGINE PHYSICAL INSPECTION
WORKSCOPE PROPOSAL FOR ENGINES CFM56-3
TU
RBIN
E S
ECTIO
N
72-5
0-0
0
MODULE DESCRIPTION
REV. 1 (JAN 2021) PAGE 1 OF 1 FORM TAA-E001
DRAFT
MEMO/DIR-CAC/N° 046-20
Recipient: To Whom It May Concern Lugar y Fecha: Valencia, 11/23/2020. Non Incident /Non Accident Statement
Engine Model: CFM56‐3C1 Engine Serial Number: 858‐790This letter is to confirm that with regard to the above mentioned CFM56‐3C1 bearing manufacture serial number 858‐790 Turpial Airlines C.A. confirms that to the best of our knowledge the above mentioned Engine during it´s operation with Turpial Airlines C.A. from 09/21/2016 to current day has not been:
1. Damage during, or identified as the root cause of, any reportable incident oraccident as defined by Chapter 1 of ICAO Annex 13; and
2. Subjected to several stress or heat (such as major engine failure, accident, or fire)or submersed in the salt water; and
3. Subjected to Government or Military use unless so operated under an Air OperatorCertificate issued for civil air transport.
4. No part has been installed on the aircraft/component which was obtained fromany Government, Military or unapproved source or was previously fitted to a non‐ civil aircraft.
Furthermore, during the time the above mentioned engine was operated by Turpial Airlines C.A. and maintained in accordance with applicable INAC regulations. Also we can confirm that this engine was not altered from its original approved Type Certificate and has not been altered in type design. Usage Details:
Aircraft Model / Registration / MSN Pos Date FH FC
B737‐4H6 / YV621T / 27352 2 start op. 09/21/2016 47.380,00 30660
Removal 03/8/2020 49.345,00 32456
Sincerely,
Ing. Amalec Adan Dir. QAC
Turpial Airlines C.A.
1. Approving Civil Aviation 2. AUTHORIZED RELEASE CERTIFICATE
3. Form Tracking Number Authority/Country:
FANUnited States FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG 800886
4. Organization Name and Address: 5. Work Order/Contract/Invoice Number:
F. J. Turbine Power, Inc., 8195 West 20th Avenue, Hialeah, FL 33014 (FAA Approved Repair Station F7JR192Y) 800886 / 858-790
6. Item: 7. Description: 8. Part Number: 9. Quantity 10. Serial Number: 11. Status/Work:
1 TURBOFAN ENGINE CFM56-3C-1 1 858-790 REPAIRED
12. Remarks: INSPECTED AND REPAIRED AS PER CFM56-3, CFMI-SM.5, REV. 76, DATED DECEMBER 2018, MANUFACTURER'S SPECIFICATIONS
AND CUSTOMER INSTRUCTIONS.
THE FOLLOWING A.D.'s, ASB's & SB's WERE COMPLIED WITH/ VERIFIED THIS SHOP VISIT:
A.D. 2006-26-01 INSTALLED NEW FUEL FILTER P/N ACC462F2038. A.D. 2013-26-01 PERFORMED AN INDEPENDENT INSPECTION OF THE INSTALLATION OF THE AGB HANDCRANKING PAD COVER AFTER MAINTENANCE. A.D. 2017-14-08 COMPLIED WITH INSPECTION PER SB 72-1169 R2. SB 72-1169 R2 COMPLIED WITH PULL CHECK OF VARIABLE STATOR VANE ACTUATION RINGS.
DETAILS OF THIS REPAIR ARE ON FILE UNDER FJTP WO# 800886. FOR MORE DETAILS SEE FAA FORM 337, DISK SHEET (FORM FJT 7020A) AND A.D. SUMMARY (FORM FJT 7019A).
TOTAL TIMES AND CYCLES SUPPLIED BY OPERATOR: TSN: 48,778 CSN: 31,997
ENGINE WAS TESTED PER AMM 71-00-00, TEST NO. 10 AND PRESERVED FROM 1 TO 365 DAYS BY XTREME AVIATION, LLC. CRS #4XAR847C UNDER WO 003466, DATED 08-JUL-2019.
FOR FOREIGN REGISTERED PRODUCTS THIS FORM IS SUBJECT TO ACCEPTANCE BY THE GOVERNING CIVIL AVIATION AUTHORITY.
13a. Certifies the Items identified above were manufactured in conformance to: 14a.~ 14 CFR 43.9 Return to service. LJ Other regulation specified in Block 12.
□ Approved design data and are in condition for safe operation. 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
□ Non-approved design data specified in Block 12. Federal Regulations, part 43 and in respect to that work, the items are approved for return to service. -
13b. Authorized Signature: 13c. Approval/Authorization No.: 14b. Authcfr)zed Sighatur~/ 14c. Approval/Certificate No.:
,,~{, {)/ / CG~ F7JR192Y 13d. Name (Typed or Printed): 13e. Date ( dd/mm/yyyy): 14d. NpJrl'e (Typed or Printed): ~ 14e. Date (dd/mmm/yyyy):
Jorge C. Ramirez 1 0-Jul-2019 User/Installer Responsibilities
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 work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in
6i: Block 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts aircraft engine(s)/propeller(s)/article(s) from the airworthiness authority of the country specified in Block 1.
Statements in block 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