V2527E-A5 ENGINE MINI-PACK
|
|
- Laurence Edwards
- 6 years ago
- Views:
Transcription
1 V2527E-A5 ENGINE MINI-PACK Engine Serial Number: Total Time / Total Cycles: V ,579:58 / 23,093 Time/Cycles Since Last 5,994 / 11,562 Shop Visit LHT 2012 Time/Cycles Since Last 5,994 / 11,562 Performance shop visit LHT st LLP Limiter: 8,438 Fan Disk Current Location: Arizona Fortress Investment Group LLC 1345 Avenue of the Americas - 45th floor New York, NY 10105
2
3
4
5
6
7
8 Don Maddock s BORESCOPE ON VIDEO, INC. (PHX AZ) 83 South Mountain View Rd. Apache Junction AZ - USA Business Cell Inspected by: Dave Wiedman don@borescopeonvideo.com Since 1996 DVD Video Borescope Inspection Report 1658 S Litchfield Road, Goodyear AZ ESN V10136 POSITION Two ENG TYPE IAE V2527E-A5 DATE October 22, 2017 MODEL A MSN 561 REG# LY-VEP REASON Acceptance Inspection JOB SITE AerSale, Goodyear AZ (GYR) TSN N/A CSN N/A General Inspection Reference AMM Exterior Inspection LH fan case, wire harnesses, fuel lines and hydraulic lines are secure with no leaks, chafing or broken standoffs. No visible damage to the oil tank, fuel/oil heater or fuel flow transmitter. RH fan case, wire harnesses secure with no visible broken mounts. No visible damage to the Starter duct/valve and anti-ice duct. EEC appears secure with no visible damage. Accessory Drive Gearbox Starter, hydraulic pump, angle gear box, IDG, fuel pump Oil Pump and FCU are secure with no visible evidence of leaks. No visible damage to the plumbing or tubes. Compressor Cases No visible damage to the LP VBV actuators. No visible bent or broken HP variable stator vanes. No visible damage to the VSV actuators. Customer service ducts have no visible cracks or evidence of leaking. No visible damage to the over board bleed valves. Fuel nozzles and tubes have no evidence of leaking. Exhaust Cases HP turbine cooling tubes and LP turbine cooling tubes have no visible dents. No visible evidence of cracks or broken hangers. Exhaust Cone No discrepancies noted at this time. Suggested Action: None.
9 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 2 Low Pressure Compressor Reference AMM LPC 1 Fan LE of the fan blades are smooth to the touch with no missing material or heavy rubs around the running seal. Acoustical panels were secure with no visible loose or missing fasteners. Exit Guide Vanes No discrepancies noted at this time. LPC 1.5 Blades No discrepancies noted at this time. LPC 2.5 Blades No discrepancies noted at this time. Suggest Action: None. High Pressure Compressor Reference AMM Stage 3 Blades LE No discrepancies noted at this time. 38 Stage 4 Blades LE No discrepancies noted at this time. 64 Stage 5 Blades TE No discrepancies noted at this time. 79 Stage 6 Blades LE No significant discrepancies noted at this time.
10 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 3 93 Stage 7 Blades TE No significant discrepancies noted at this time. Stator path liner No discrepancies noted at this time. 84 Stage 8 Blades LE No significant discrepancies noted at this time. Stator path liner No discrepancies noted at this time. 89 Stage 9 Blades LE No significant discrepancies noted at this time. Stator path liner No discrepancies noted at this time. 85 Stage 10 Blades LE No significant discrepancies noted at this time. Stator path liner No discrepancies noted at this time. 78 Stage 11 Blades TE No significant discrepancies noted at this time. Stator path liner No discrepancies noted at this time. 71 Stage 12 Blades LE No significant discrepancies noted at this time. Suggest Action: None. Minor LE dents <.010 observed on a few blades in HPC 6-12 are permitted.
11 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 4 Combustor Reference AMM Bulkhead No discrepancies noted at this time. Fuel Nozzles No discrepancies noted at this time. Deflectors Radial cracks and burn back of deflector edges observed on several fuel nozzle positions is permitted. Subtask A pg. 68 attached. Inner & Outer Liners Minor burn back observed on both liners less than.700 is permitted. Coating loss is permitted. Subtask A pg. 58 & 64 attached. HPT NGV s Reference AMM HPT 1 NGV s LE Minor ceramic coating loss is permitted. HPT 1 NGV s TE A few vanes observed with TE axial cracks and minor missing material are permitted. Ceramic coating loss is permitted. Subtask A pg. 23 attached. Suggest Action: None.
12 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 5 High Pressure Turbine Reference AMM HPT 1 BOAS Ceramic coating loss spalling is permitted. Subtask A pg. 23 attached. 64 HPT Stage 1 LE Ceramic coating loss is permitted. Subtask A pg. 21 attached. 64 HPT Stage 1 TE Ceramic coating loss is permitted. Subtask A pg. 21 attached. 72 HPT Stage 2 LE No discrepancies noted at this time. HPT 2 BOAS Ceramic coating loss is permitted. 72 HPT Stage 2 TE No discrepancies noted at this time. Suggest Action: None.
13 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 6 Low Pressure Turbine Reference AMM LPT Stage 3 LE Minor dents observed in the LE area 3.1 on a few blades <.024 in depth are permitted. Shop blends are acceptable. Subtask A pgs. 20 & 21 attached. LPT Stage 7 TE No discrepancies noted at this time. Suggest Action: None. The contents of this report are based on attentive inspection and review. It is exclusive of any damage not detectable without removal and disassemble of the unit. This report is submitted in confidence to the above named client. The external video walk around is for cursory purposes only which covers general cleanliness, obvious damage and leaks, a more detailed inspection should be provided by the maintenance facility. Some service bulletins and AD s may be incorporated as routine but specific SB s should be requested with the work order. Although this report is believed to be a true and fair representation of the condition of the engine, the client acknowledges that BOV s liability is limited to the amount of the invoice. The engines inspected may have been prepared for borescope by the facility named above under job site and returned to original condition by the same facility. Maintenance Manual pages attached to this report if any are uncontrolled and are for general reference only. Verify limits with current MM effective for this engine and or aircraft. SIGNATURE A&P DATE October 22, 2017
14 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 7
15 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 8
16 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 9
17 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 10
18 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 11
19 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 12
20 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 13
21 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 14
22 DVD Video Borescope Inspection Report ESN V /OCT/ 17 Page 15
23
24
25
26
27
28
29
30
31
32
33
34 ENGINE CONDITION MONITORING A LY-VEP MSN 561 Sep 2017 Engine No. 1 IAE V2527-A5 S/N V10134 LSV date 1-Jun-2012 LSV TSN FH LSV CSN FC Engine TSN 47,865 FH Engine CSN 23,590 FC EGT Margin 67 Engine No. 2 IAE V2527-A5 S/N V10136 LSV date 2-Oct-2012 LSV TSN FH LSV CSN FC Engine TSN 47,550 FH Engine CSN 23,081 FC EGT Margin 71 Prepared by / Checked by Anna Trofimovica / Robert Bauer Report Date: 15/10/17 Page 1 of 10
35 Fleet Performance Report Sep 2017 (last data point ) Report Date: 15/10/17 Page 4 of 10
36 Fleet Performance Report Sep 2017 (last data point ) Reference (last 365 days) to show long term trend: Report Date: 15/10/17 Page 5 of 10
37 Fleet Performance Report Sep 2017 (last data point ) Report Date: 15/10/17 Page 6 of 10
38 Fleet Performance Report Sep 2017 (last data point ) Reference (last 365 days) to show long term trend: Report Date: 15/10/17 Page 7 of 10
39 Fleet Performance Report Sep 2017 (last data point ) Report Date: 15/10/17 Page 8 of 10
40 Fleet Performance Report Sep 2017 (last data point ) Reference (last 365 days) to show long term trend: Report Date: 15/10/17 Page 9 of 10
41 Fleet Performance Report Sep 2017 (last data point ) Condition Summary No. 1 Engine S/N V10134 Main parameters EGT Margin 67 Oil Pressure 226 (DMU) Vibrations 1,3 (DMU) Watch Items Certain parameter missing Data transfer check required Conclusions/Recommendations Check data and DMU reporting Performed actions by previous Data Transfer issues under investigation recommendations No. 2 Engine S/N V10136 Main parameters EGT Margin 71 Oil Pressure 244 (DMU) Vibrations 1,6 (DMU) Watch Items Certain parameter missing Data transfer check required Conclusions/Recommendations Check data and DMU reporting Performed actions by previous Data Transfer issues under investigation recommendations Report Date: 15/10/17 Page 10 of 10
42 KATS EGT Margin Summary A320 / V2500-A5 PA Check A320 / V2500-A5 Test 4 Aricraft No. LY-VEP Engine S/N - Pos 1 V10134 MSN ---- Engine S/N - Pos 2 V10136 Eng. Model V2527E-A5 Run Date 10/7/2017 Location GYR Ref: SIL 057 Rev. 7 ECAM Inputs Pos 1 Pos 2 EPRi Mn TAT - Deg C EGT Observed - Deg C ECS : OFF(0) ; ON(1) WAI : OFF(0) ; ON(1) CAI : OFF(0) ; ON(1) Altitude - Ft. EGT Correction for Alt. from SIL057 - C Outputs Pos 1 Pos 2 EGT actual EGT_co EGT_bo EGT_bto EGT_cto EGT EGT Margin - Deg C EGT Margin - Corrected for ECAM Altitude - Deg C Accomplished by: Test 4 Download provided by Fortress Reviewed by: Francisco Garcia / Sr. Mgr. - Technical Date: 10/23/2017
43 Input only in the yellow fields! Input : EPRi : MN : The EGT-Margin is calculated for "EGT-Margin calculation Point" : TAT : C full rated T/O at OAT = 30 C, Sea level. EGT : C <= Cockpit SIL Rev.6 ECS : OFF(0) ; ON(1) 0 any additional requirement as higher OAT, higher altitude or bleeds WAI : OFF(0) ; ON(1) 0 is reducing this value! CAI : OFF(0) ; ON(1) 1 EGTM f.r., SL, 30 C Engine Version:===> V2522-A5 V2524-A5 V2527M-A5 V2500-A1 V2527-A5 V2527E-A5 V2530-A5 V2533-A5 V2525-D5 V2528-D5 A319 A319 A319 A320 A320 A320 A321 A321 MD-90.. MD-90.. specific Parameters : EPRI (Packs off) MN T/O TAT T/O C Redline : [ C] = RLL in Cockpit! EGT const. until [ C] EGT -factor EGT-adder EGT-step after EGT-adder EGT exponent X coefficients : C C C C C C C exchng.in Rev.7! C Results not good with 7! C C C calculated values EGT actual C EGT cor.obs. K EGT Basel.obs. K EGT B.T/O K EGT T/O K EGT C EGT margin C POSITION 2
44
45
46
47
48
49
50
51
52
53
54
APS 2000 Shop Findings Report
APU S/N : SP-E912042 AIRCRAFT REGISTRATION: EI-CZG APU P/N : 170101-106 CUSTOMER : Air One R/O N : 78202418 EVENT N : 1379 REVISION N : 685265 TSN : 16143 TSI : 2655 DATE OF REMOVAL: 18.04.07 CSN : 15386
More informationMINI PACK. ENGINE Model: PW127M BUILD SPEC ESN: TSN: 32, CSN: 33,815 TSO: 9, CSO: 8,813 TSHSI: 0.
MINI PACK ENGINE Model: PW127M BUILD SPEC. 1237 ESN: 127051 TSN: 32,200.90 CSN: 33,815 TSO: 9,194.80 CSO: 8,813 TSHSI: 0.00 CSHSI: 0 RGB SN. 127051 TSN: 32,200.90 CSN: 33,815 TSO: 6,063.40 CSO: 4,971 CONTENTS:
More informationMINI PACK ENGINE MODEL: PW123E BUILD SPEC: BS869 TM SN: TSN: 38, CSN: 36,637 TSO: 9, CSO: 9,231 TSHSI: - CSHSI: -
MINI PACK ENGINE MODEL: PW123E BUILD SPEC: BS869 TM SN: 123234 TSN: 38,554.97 CSN: 36,637 TSO: 9,280.00 CSO: 9,231 TSHSI: - CSHSI: - RGB SN: 123233 TSN: 39,018.20 CSN: 37,200 TSO: 9,280.00 CSO: 9,231 FUEL
More informationMINI PACK N/A N/A N/A N/A FA0995 N/A
MINI PACK ENGINE MODEL: PW150 BUILD SPEC: 885 TM SN: FA0995 TSN: 4,327.60 CSN: 4,194 TSO: CSO: TSHSI: CSHSI: N/A N/A N/A N/A RGB SN: FA0995 TSN: 4,327.60 CSN: 5,194 TSO: N/A CSO: N/A CONTENTS: - TMM Transport
More informationMINI PACK BUILD SPEC. 885 ESN: FA0278 TSN: 15, CSN: 15,815 TSO: N/A CSO: N/A TSHSI: 2, CSHSI: 2,373 RGB SN. FA0278
MINI PACK ENGINE Model: BUILD SPEC. 885 ESN: PW150A FA0278 TSN: 15,012.30 CSN: 15,815 TSO: N/A CSO: N/A TSHSI: 2,056.00 CSHSI: 2,373 RGB SN. FA0278 TSN: 15,012.30 CSN: 15,815 TSO: 3,596.40 CSO: 3,863 CONTENTS:
More informationTHOMSON AIRWAYS LIMITED DISCREPANCY SHEET
IPC REF FIG ITEM DESCRIPTION FROM 72.35.01 01 085/220 ROTATING FAIRINGS 72.31.11 01 280 LP BLADES (22 OFF) 73.11.07 01 645/725 MAIN FUEL INLET TUBE 29.11.03 02 100 HYD. SUPPLY,RIGID TUBE 29.11.03 02 200
More informationLM2500 BORESCOPE INSPECTION REPORT
LM2500 BORESCOPE INSPECTION REPORT UC DAVIS CUSTOMER UNIT NAME/NUMBER: N/A ENGINE SERIAL NUMBER: 481-743 TCT SALES ORDER NUMBER: US9010290 DATE INSPECTED:11-29-2018 SERVICEABILITY AT DATE OF INSPECTION:
More informationCOMPONENT IDENTIFICATION
This CFMI publication is for Training Purpose Only. The information is accurate at the time of compilation; however, no update service will be furnished to maintain accuracy. For authorized maintenance
More informationCFM REGULATION THE POWER OF FLIGHT
CFM56-3 3 REGULATION 1 CFM56-3 2 Speed Governing System Fuel Limiting System VBV VSV N1 Vs P Idling System HPTCCV N1 Vs Z N1 Vs T Main Tasks Additional Tasks Corrections MEC PMC CFM 56-3 ENGINE OPERATIONAL
More informationAIRCRAFT HOLDINGS AND LEASING LLC. 50 CENTRAL AVENUE SARASOTA FL LAST ACTUALS
OWNER: ADDRESS: PHONE: FAX: DEEP BLUE AVIATION LLC 1732 SOUTH KINGS AVENUE BRANDON FL 33511-622 813-676-515 OPERATOR: ADDRESS: PHONE: FAX: AIRCRAFT HOLDINGS AND LEASING LLC. 5 CENTRAL AVENUE SARASOTA FL
More informationPreliminary Report. 19 October, For. Burak Marine. Aliağa İzmir TURKEY ESN Under. Mehmet AKIN (Granite)
Preliminary Report 19 October, 2012 For Burak Marine Aliağa İzmir TURKEY ESN 456-675 Under Customer Representative: GE Field Service Representative: Burak ALDEMİR Adnan LEBLEBİCİ Mehmet AKIN (Granite)
More informationEngine Model: PW ESN: Time Since New: 84,463. Cycles Since New: 13,974
Engine Mini Pack Engine Model: PW 4056-3 ESN: 724307 Time Since New: 84,463 Cycles Since New: 13,974 Time Since Last Shop Visit: 9,015 Cycles Since Last Shop Visit: 1,793 Last Shop Visit: Eagle Services
More informationEngine/Module Repair Requirements /
AIR CHINA TECHNICS Engine/Module Repair Requirements / ERR No. PW4K7277110901R0 Engine Type Engine S/N Executive Base Prepared By Checked By Approved By PW4056-3 P727711 Ameco 2009-6-1 EWR PW4K7277110901R0
More informationChromalloy. Borescope and Test Report. Prepared for. Triumph Air Repair A Triumph Group Company
A Triumph Group Company Borescope and Test Report Prepared for Chromalloy Customer P.O.#: S2669 A.P.U. Model #: GTCP331-200ER A.P.U. Serial #: P-2796 A.P.U. Part #: 3800298-1 Triumph SRO #: S000013678
More informationTSE (PPOH) AIRWORTHINESS MANAGEMENT DIVISION MINIPACK GE CF6-50E2 ESN P a g e ESN
MINIPACK GE CF6-50E2 455-358 1 P a g e CUURENT DATA TYPE CF6-50E2 S/N 455-358 64659 25342 TSO 4061 CSO 1363 REASON OF REMOVAL CONVINIENT DATE OF REMOVAL LAST SHOP STATUS LAST TEST CELL EGT MARGIN 08-May-2013
More informationCFM56-7B POWER PLANT REMOVAL & INSTALLATION
Task No: 737-71-00-00 NG Maint Prog Ref: BAL/BOE/11 Station: A/C Reg: Issue: 5 Date: NOV 2017 A.M.M. Ref: 71-00-02 Check: Aircraft Type CAA App Ref. UK.145.00112 Scheduled / Unscheduled Delete as applicable
More informationDVD Video Borescope Inspection Report Country Club Blvd, Suite 110, North Olmsted, Ohio REG# N837CA ENG TYPE PW123 REG# N837CA
Don Maddock's BORESCOPE ON VIDEO, INC. (PHX AZ) 83 South Mountain View Rd. Apache J unction AZ - USA 85119 9861 Business 480-671 6734 Cell 602-619-6633 Insp ected by: Dave Wiedman don@borescopeonvideo.com
More informationFuse: On-wing engine inspection
Figure 1 Assembled Commercial Turbofan Aircraft Engine -Trimetric View Figure 2 Assembled Commercial Turbofan Aircraft Engine Trimetric View - Partial Cutaway 1 1. Fan 2. Low Pressure Compressor (Booster)
More informationPreliminary Report. 17 October, For. Burak Marine. Aliağa İzmir TURKEY ESN Mehmet AKIN (Granite)
Preliminary Report 17 October, 2012 For Burak Marine Aliağa İzmir TURKEY ESN 560-040 Customer Representative: GE Field Service Representative: Burak ALDEMİR Adnan LEBLEBİCİ Mehmet AKIN (Granite) All technical
More informationGenx-1B P-N S-N Check List
Engine P/N Genx-1B P-N S-N Check List CM Project (if relevant) 2305M70G07 ACCESSORY GEARBOX ASSY (MODULE 64X) core lwr l/h 1962M22P01 ACCLRM-TURBINE CENTER FRAME core upr l/h 3291883-1 HPT ACTIVE CLEARANCE
More informationTSE (PPOH) AIRWORTHINESS MANAGEMENT DIVISION MINIPACK GE CF6-50E2 ESN P a g e ESN
MINIPACK GE CF6-50E2 517-131 1 P a g e CUURENT DATA TYPE CF6-50E2 S/N 517-131 57367 23857 TSO 2541 CSO 1147 TSR 2206 CSR 971 REASON OF REMOVAL DATE OF REMOVAL LAST SHOP STATUS LAST TEST CELL EGT MARGIN
More informationRolls -Royce M250--C47M OPERATION AND MAINTENANCE
TABLE 603 Inspection Checksheet Owner Date A/C Make/Model S/N Reg No. TSN Engine S/N TSN TSO This inspection checksheet is to be used when performing scheduled inspections. This form may be locally reproduced
More informationEuropean Aviation Safety Agency
European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET Number : IM.E.026 Issue : 03 Date : 04 January 2013 Type : Engine Alliance LLC GP7200 series engines Variants: GP7270 GP7277 List of Effective
More informationCF34 TURBOFAN ENGINE MAINTENANCE MANUAL LIFE LIMITS OF ROTATING ENGINE PARTS
LIFE LIMITS OF ROTATING ENGINE PARTS 1. General. A. The FAA has approved service life-limit cycles (Airworthiness Limitations) for rotating parts installed in the CF34-1A/-3A/-3A2 turbofan engines. B.
More informationEngine Maintenance Management
Engine Maintenance Management Managing Technical Aspects of Leased Assets Madrid, Spain / May 12 th, 2015 Presented By: Shannon Ackert SVP, Commercial Operations Jackson Square Aviation Agenda Technical
More informationTSE (PPOH) AIRWORTHINESS MANAGEMENT DIVISION MINIPACK GE CF6-50C2 ESN P a g e
MINIPACK GE CF6-50C2 528-154 1 P a g e CUURENT DATA TYPE CF6-50C2 S/N 528-154 46563 19073 REASON OF REMOVAL T/X DATE OF REMOVAL 22-May-2007 2 P a g e LLP SHEET NOMENCLATURE P/N S/N LIMIT REMAINING FAN
More informationMTU Maintenance Dallas, Inc. Integrated Management System. MM 03D-03 Capability List Manual
Chapter 0 Page 2 of 15 Revision: Initial Date: 01NOV2012 0.1 Table of Contents 0 Title Page... 1 0.1 Table of Contents... 2 0.2 List of Effective Pages... 3 0.3 Record of Revision... 4 0.4 Record of Temporary
More informationOffers for Sale or Lease
Offers for Sale or Lease CRJ200LR Serial Number 7391 TTSN 25,589 Flight Hours TCSN 21,550 Flight Cycles Page 1 of 10 Date of Manufacture: April, 2000 Model Designation: CL-600-2B19 Avionics Collins Proline
More informationRolls -Royce M250--C40B OPERATION AND MAINTENANCE. Table 603. Inspection Checksheet
Table 603 Inspection Checksheet Owner Date A/C Make/Model S/N Reg. No. TSN Engine S/N TSN TSO This inspection checksheet is to be used when performing scheduled inspections. This form can be locally reproduced
More informationENGINEERING ORDER EO. No: A320MO73-016/00 R11
EO. No: A320MO73-06/00 R Date: 2/9/2000 Rev. Date: 09/20/20 Pag of 20 SUBJECT: V2500 ENGINES-CONVERSION INSTRUCTIONS TO CHANGE THE V2500-A5 ENGINES RATING BY MODIFYING THE DATA ENTRY PLUG REFERENCES: COMPLIANCE
More informationRolls -Royce M250--C47M OPERATION AND MAINTENANCE
TABLE 603 Inspection Checksheet Owner Date A/C Make/Model S/N Reg. No. TSN Engine S/N TSN TSO This inspection checksheet is to be used when performing scheduled inspections. This form can be locally reproduced
More informationRolls -Royce M250--C47B OPERATION AND MAINTENANCE TABLE 603. Inspection Checksheet. A/C Make/Model S/N Reg. No. TSN
TABLE 603 Inspection Checksheet Owner Date A/C Make/Model S/N Reg. No. TSN Engine S/N TSN TSO This inspection checksheet is to be used when performing scheduled inspections. This form can be locally reproduced
More informationP.O. Box 3149 Albany, GA Phone (229) Fax (229) March 7, 2006 FLAP CONTROL TORQUE SHAFT REPLACEMENT
THRUSH AIRCRAFT, INC. P.O. Box 3149 Albany, GA 31706-3149 Phone (229) 883-1440 Fax (229) 436-4856 SERVICE BULLETIN March 7, 2006 No. SB-AG-48 FLAP CONTROL TORQUE SHAFT REPLACEMENT MODELS AFFECTED: Aircraft
More informationCFM56-3 (FINAL_) 856A1027G01 Fixture, Lift - Compressor Rotor Stage 3 Disk And Blades 1 856A1028 Fixture 1
8100 Sweeney S/N STM014 1 107029435 BRKTs -3 Tooling 2 527241105 Fixture(combustion Chamber Fixture) 1 537241146 Fixture (combustion Chamber Fixture) 1 278114-1 CFM56-3 Fuel Pump Backlash Tool 1 301-360-005-0
More informationTYPE-CERTIFICATE DATA SHEET
Issue: 02 & LEAP-1C series engines Date: 11 March 2016 TYPE-CERTIFICATE DATA SHEET No. E.110 for Engine & LEAP-1C series engines Type Certificate Holder SA SA 2, boulevard du Général Martial Valin 75015
More informationInvestigation Report AS350B3e s/n: 7382
Investigation Report AS350B3e s/n: 7382 Date: 09.11.2016 Customer: Fonnafly AS Place: Voss Country: Norway Aircraft Version: AS350B3e Serial Number: 7382 Flight Hours: 1325,0 Manufacture Date: 2012 1 ATA
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET EASA.E.042 for RB211 Trent 700 series engines Type Certificate Holder 62 Buckingham Gate Westminster London SW1E 6AT United Kingdom For Models: RB211 Trent 768-60 RB211 Trent
More informationAVIATION INVESTIGATION REPORT A02P0168 ENGINE POWER LOSS
AVIATION INVESTIGATION REPORT A02P0168 ENGINE POWER LOSS TRANSWEST HELICOPTERS LTD. BELL 214B-1 (HELICOPTER) C-GTWH SMITHERS, BRITISH COLUMBIA, 10 NM S 07 AUGUST 2002 The Transportation Safety Board of
More informationRolls -Royce M250--C20R SERIES OPERATION AND MAINTENANCE
C. Alternate Inspection Schedule Based on current engine configuration and the use of modern oils, operators can use this alternate inspection schedule. Prerequisites for this include: (1) The use of High
More informationDASSAULT AVIATION Proprietary Data
FALCON 7X 02-70-05 CODDE 1 PAGE 1 / 6 GENERAL ACRONYMS LIST ACOC AGB APU A/T ATSV BOV CAS CB CL CMC CR DC DCU ECS EEC FADEC FBW FCU FF FOHE FSOV HP HPC HPT IGV ITT LP LPC LPT LRU MV N1 N2 PDU PLA PMA PMU
More informationFor Experimental Aircraft Only: Glastar, Sportsman 2+2, and Similar with Lycoming O320 or O360 Parallel Valve Engines
REPORT NAME: KIT PFS-16104 INSTALLATION INSTRUCTIONS AND INSTRUCTIONS FOR CONTINUED AIRWORTHINESS APPROVAL PFS ENG DATE: REPORT NUMBER: PFS-16250-EXP REVISION: A REPORT DATE: 02/14/06 PREPARED BY: Tom
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. IM.E.096 for PW800 Series Engines Type Certificate Holder 1000 Marie Victorin Longueuil, Quebec J4G1A1 Canada For : TE.CERT.00052 001 European Aviation Safety Agency, 2016.
More informationEngine Finance Rountable Managing an engine. Stephane Garson, General Manager Marketing. 1 st May 2008, New York
Engine Finance Rountable Managing an engine Stephane Garson, General Manager Marketing 1 st May 2008, New York Two Strong Aerospace Leaders Behind CFM CFM International is a Joint Company of Snecma & General
More informationRolls-Royce Corporation 501-D22 COMMERCIAL ENGINE BULLETIN (CEB) Technical Publications Index
Corporation 501-D22 COMMERCIAL ENGINE BULLETIN (CEB) Technical Publications Index May 1. 2018 72-- ENGINE 72--1001 Engine -- Reduction Gear Prop Recommended No Later Than 11--01--66 No. 2, 11--15--68 Brake
More informationBOMBARDIER AEROSPACE, As Exclusiv e Agent For Air Nostrum Offers for Sale or Lease Dash 8 Model 315 Aircraft, Serial Number 562
5B Auditor Report Date Owner code Operator Hours at Delivery Cycles at Air Nostrum 5-Jun-09 N/A Air Nostrum 0.0 0 Daily Utilization Aircraft Type A/C Serial No A/C Reg Build Date Total Hrs Total Cyc Hours
More informationGENERAL The Honeywell model TFE731-40AR turbofan engine is a lightweight, two-spool, geared-stage, front-fan, jet engine.
ENGINE GENERAL The Honeywell model TFE731-40AR turbofan engine is a lightweight, two-spool, geared-stage, front-fan, jet engine. The cross section of the engine is shown in Figure 7-71-1, page VII-71-3.
More informationRolls -Royce M250--B17 SERIES OPERATION AND MAINTENANCE. Table 602 Inspection Checksheet Owner Date. A/C Make/Model S/N Reg No.
Table 602 Inspection Checksheet Owner Date A/C Make/Model S/N Reg No. TSN Engine S/N TSN TSO This inspection checksheet is to be used when performing scheduled inspections. This form can be locally reproduced
More informationPARAVION TECHNOLOGY, INC AIRWAY AVENUE FT. COLLINS, COLORADO 80524
[Rev. 5, 11/07/07] PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FT. COLLINS, COLORADO 80524 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 407H-120M BLEED-AIR CABIN HEATER INSTALLATION BELL MODEL 407 HELICOPTERS
More informationREPAIR STATION MANUAL
Propulsion Technologies International, LLC. 15301 S.W. 29th Street Miramar, Florida 33027 REPAIR STATION MANUAL APPENDIX A CAPABILITIES LIST Manual Control #: Electronic Assigned To: PTI LLC TABLE OF CONTENTS
More informationAIR TRANSPORT INTERNATIONAL
16.04 B757 SERVICE CHECK (FORM 757-16.04-1) B757 SERVICE CHECK SIGNATURE RECORD (FORM 757-16.04-1) NOTE: The Sign-Off Section of the Service Check (Form 757-16.04-1) is a signature record and contains
More informationChris Ruot. October 21, APU System Update
Chris Ruot October 21, 2014 APU System Update HONEYWELL CONFIDENTIAL: This copyrighted work and all information are the property of Honeywell International, Inc., contain trade secrets and may not, in
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET No. IM.E.016 issue 10 for FJ44/FJ33 Series Engines Certificate Holder Williams International Co. Walled Lake Michigan 48390-0200 USA For Models: FJ44-1A FJ44-1AP FJ44-2A FJ44-2C
More informationEuropean Aviation Safety Agency
European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Number : IM.E.016 Issue : 07 Date : 21 May 2014 Type : Williams International Co. FJ44 Series Engines s FJ44-1A FJ44-1AP FJ44-2A FJ44-2C
More informationEuropean Aviation Safety Agency
European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Number : IM.E.043 Issue : 02 Date : 07 January 2013 Type : Pratt & Whitney PW4000-100 Series Engines Variants PW4164 PW4164C PW4164C/B PW4164-1D
More informationTable of Contents. 4. Before a New Turbocharger is Installed
Table of Contents 1. Turbocharger Overview ------------------------------------------------------------------ 1.1. Definition -----------------------------------------------------------------------------
More informationSERVICE BULLETIN. No. SB-AG-49 August 1, 2008 SEAT SUPPORT BRACKET INSPECTION AND REPAIR
THRUSH AIRCRAFT, INC. P.O. Box 3149 300 Old Pretoria Rd. Albany, GA 31706-3149 Product Support 229-883-1440 ext. 341 FAX 229-436-4856 jbays@thrushaircraft.com SERVICE BULLETIN No. SB-AG-49 August 1, 2008
More informationRAAF AE2100D3 Engine Health Management
RAAF AE2100D3 Engine Health Management SGT Andrew Wade CSC MScTech (Aviation) AE2100D3 EHMS ALSPO Propulsion Systems Engineering Royal Australian Air Force Acknowledgements FSGT Brendan Church CSC, Co-Author
More informationEngine Performance Analysis
Engine Performance Analysis Introduction The basics of engine performance analysis The parameters and tools used in engine performance analysis Introduction Parametric cycle analysis: Independently selected
More informationA1-F402B-MMI February 2003 Page A
1 February 2003 Page A NUMERICAL INDEX OF EFFECTIVE WORK PACKAGES/PAGES List of Current Changes Original...0...1 February 2003 (IRACs 4 thru 8 Inc.) Only those pages assigned to the manual are listed in
More informationAn agency of the European Union
TYPE-CERTIFICATE DATA SHEET No. E.115 for Engine LEAP-1B series engines Type Certificate Holder SA SA 2, boulevard du Général Martial Valin 75015 Paris France For Models: LEAP-1B21 LEAP-1B23 LEAP-1B25
More informationCHAPTER ICE AND RAIN PROTECTION SYSTEM
15--00--1 ICE AND RAIN PROTECTION SYSTEM Table of Contents REV 3, May 03/05 CHAPTER 15 --- ICE AND RAIN PROTECTION SYSTEM Page TABLE OF CONTENTS 15-00 Table of Contents 15--00--1 INTRODUCTION 15-10 Introduction
More informationEuropean Aviation Safety Agency
European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Number : E.036 Issue : 04 Date : 10 September 2013 Type : Rolls-Royce plc Trent 1000 series engines Models Trent 1000-A Trent 1000-A2 Trent
More informationLEAP-X Program Update
LEAP-X Program Update 29 Oct 09 NYC CFM International Proprietary Information The information in this document is CFM Proprietary Information and is disclosed in confidence. It is the property of CFM International
More informationRolls -Royce M250--C20R SERIES OPERATION AND MAINTENANCE. Table 602 Scheduled Inspections. Inspection Checksheet. A/C Make/Model S/N Reg. No.
Table 602 Scheduled Inspections Inspection Checksheet Owner Date A/C Make/Model S/N Reg. No. TSN Engine S/N TSN TSO This inspection checksheet is to be used when performing scheduled inspections. This
More informationGUADALUPE POWER PARTNERS, LP Section MAINTENANCE GT1 CI WORK SCOPE
Outage; Combustion Inspection on Gas Turbine #1 serial number 297365 Start Date; March 15, 2009 Completion Date; March 21, 2009 Test Fire and Tune Date; March 20, 2009 Work Scope Summary o Combustion Inspection
More informationPOPA June 12-14, 2014 Savannah, GA
POPA June 12-14, 2014 Savannah, GA EXPORT CLASSIFICATION Check this box if presentation contains no technical data OR summarize the export classifications of all slides in this presentation as instructed
More informationGENERAL TECHNICAL SPECIFICAITON
GENERAL TECHNICAL SPECIFICAITON AIRCRAFT TYPE Bombardier CL-600-2B19 RJ Series 200-LR SERIAL NUMBER 7457 COUNTRY OF REGISTRATION REGISTRATION NUMBER United States N655BR DATE OF MANUFACTURE December 9,
More informationN100YC PC12/45/47 STATUS REPORT
100 HOUR INSPECTION 150 N/A N/A N/A ANNUAL INSPECTION 12 971.7 1219 3-Jun-11 3-Jun-12-1 CHAPTER 4-00-00 AIRWORTHINESS LIMITATIONS STRUCTURAL LIMITATIONS - Note SB04-009 applies to MSN 193 and 244 - Beyond
More informationService Bulletin No: Ref No: 170 Modification No: EC ATA Chapter: 53
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 53-014 Ref No: 170 Modification No: EC-15-0854 ATA Chapter: 53 FUSELAGE - MAIN FRAMES REPLACE THE LEFT AND / OR RIGHT FRAME 11 FITTINGS 1.
More informationENGINE LLP DOCUMENTATION CHECKLIST
OVERHAULED - 45 DAYS ENGINE LLP DOCUMENTATION CHECKLIST DATE OF DOCUMENT REVIEW 8/6/2012 PART NUMBER 2A5001 PART S/N PKLBEU5259 PART DESCRIPTION ENGINE MODEL V2527-A5 TURBINE HUB STAGE 1 PART TSN 20,504
More informationNATIONAL TRANSPORTATION SAFETY BOARD Office of Aviation Safety Washington, D.C POWERPLANT GROUP CHAIRMAN S FACTUAL REPORT
NATIONAL TRANSPORTATION SAFETY BOARD Office of Aviation Safety Washington, D.C. 20594 June 9, 2008 May 11, 2009 POWERPLANT GROUP CHAIRMAN S FACTUAL REPORT NTSB No: DCA-09-MA-021 A. ACCIDENT Location: Denver
More informationFrom: Icelandair Technical Services, Approval:...
Revision Highlights Ref. ICE/767/LM To Holders of Boeing 767 Line Manual, Ref. No. ICE/767/LM From Icelandair Technical Services, Approval... This is Revision to ICELANDAIR Boeing 767 Line Manual, Ref.
More informationCountry Customer Name Site Name USA Specific Reports Task Risk Assessment CSA/Invoice/Work Order Numbers Borescope Inspection YES N/A.
Country Customer Name Site Name US Specific Reports Task Risk ssessment CS/Invoice/Work Order Numbers orescope Inspection YES N/ orescope Completed y Package S/N Hours Starts S/N orescope Date PD Number
More informationSERVICE BULLETIN ENGINE - INSPECTION OF THE LOW -PRESSURE -TURBINE FORWARD -SHAFT AIR -COOLING HOLE
SERVICE BULLETIN ENGINE - INSPECTION OF THE LOW -PRESSURE -TURBINE FORWARD -SHAFT AIR -COOLING HOLE 1. PLANNING INFORMATION A. Effectivity (1) Engines All AE 3007A, A1/1, A1/3, A1, A1P, A1E and A2 engines.
More informationService Bulletin No: Ref No: 165 Modification No: EC ATA Chapter: 21
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 21-012 Ref No: 165 Modification No: EC-14-0359 ATA Chapter: 21 AIR CONDITIONING - COOLING INSTALL A COVER ASSEMBLY TO THE COMPRESSOR TO PROTECT
More information1500 Hour PM Inspection
1500 Hour PM Inspection Electrical Start Time Stop Time 1. Perform initial walk around RTG prior to start and verify no excessive damage to crane. Report to Maintenance team immediately if damage is found
More informationSERVICE LETTER. COMPLIANCE DISCRETIONARY. This service letter should be accomplished at a scheduled Check 1, Check 2, or HSI. LABOR HOURS KEY WORD
Citation SERVICE LETTER SL525C-71-01 TITLE POWER PLANT - TRANSMITTAL OF WILLIAMS INTERNATIONAL SERVICE BULLETIN ENGINE OIL BREATHER TUBE ASSEMBLY & FRONT BYPASS DUCT RH BOSS ASSEMBLY INSTALL EFFECTIVITY
More informationPreservation. A.1. Preservation for a Period of up to 30 Days. Pág. 2. Memoria ** ON A/C , , TASK
Annex Pág. 2 Memoria A Preservation A.1. Preservation for a Period of up to 30 Days ** ON A/C 001-010, 012-099, 201-299 TASK 72-00-00-600-001 Preservation for a Period of up to 30 Days 1. Reason for the
More informationAccident Prevention Program
Accident Prevention Program Maintenance Aspects of Owning Your Own Airplane Introduction As an owner-pilot, FAR Part 43 allows you to perform certain types of inspections and maintenance on your airplane.
More informationPARAVION TECHNOLOGY, INC AIRWAY AVENUE FORT COLLINS, COLORADO REPORT NO. PR-206H-900M CABIN HEATER SYSTEM INSTALLATION INSTRUCTIONS
PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FORT COLLINS, COLORADO 80524 REPORT NO. CABIN HEATER SYSTEM INSTALLATION INSTRUCTIONS BELL 206A/B HELICOPTERS Page i PR- Rev. P, 04/06/09 REVISIONS REV. DATE
More informationOffers for Sale CRJ700 ER. Serial Number TTSN 42,073 Flight Hours TCSN 27,760 Flight Cycles
Offers for Sale CRJ700 ER Serial Number 10023 TTSN 42,073 Flight Hours TCSN 27,760 Flight Cycles Page 1 of 8 Date of Manufacture: 2001 Model Designation: CL-600-2C10 Series 700 Avionics Extended Range
More informationInspection and Repair of Compressor Wheels
Subject: Applicable EXTEX Engineered Products Part Numbers: Installations: Revision History: Reason: Description: Inspection and Repair of Compressor Wheels E23057111 (Stage 1), E23057112 (Stage 2-3),
More information1) Scheduled maintenance checks
1) Scheduled maintenance checks Definition This section lists the periodic inspections which must be carried out after a specified periods of operation. Intervals Periodic inspections are those which must
More informationF135 Propulsion Integration Topics for Symposium on Jet Engines Haifa, Israel
F135 Propulsion Integration Topics for Symposium on Jet Engines Haifa, Israel Tom Johnson Program Chief Engineer Operational Military Engines 25 October 2012 J6924_F135_Propulsion_2012-1 Agenda F135 Development
More informationFOR REVIEW SERVICE BULLETIN SB-AG-65. Installation of Click Bond Electrical Grounding Spacer Stud on the Header Tank. Revision IR 11/20/2017
SERVICE BULLETIN SB-AG-65 Revision IR 11/20/2017 Installation of Click Bond Electrical Grounding Spacer Stud on the Header Tank James Alman Vice President of Engineering i AIRCRAFT AFFECTED: MODEL SERIAL
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET For Models: No. IM.E.102 for Engine GEnx Series Engines Type Certificate Holder GE Aviation One Neumann Way Cincinnati Ohio 45215 United States of America GEnx 1B GEnx 2B GEnx
More information2018 Capabilities International Blvd Cincinnati, OH Phone: (513) Fax: (513)
Aviation Repair & Overhaul FAA Certificate CL1R064K EASA Certificate 145.4358 CAAC Certificate F00100499 2018 Capabilities 9970 International Blvd Cincinnati, OH 45246-4898 Phone: (513) 870-6780 Fax: (513)
More informationEngine Compartment Inspection
Engine Compartment Inspection Unit Contents Student Page Student Components Learning Activities Sheet... 7 3 Abbreviated Checklist.... 7 5 Objective Sheet... 7 7 Expanded Checklist... 7 9 * Job Sheets
More informationRolls-Royce Corporation T56-A-14LFE COMMERCIAL ENGINE BULLETIN (CEB) Technical Publications Index
Corporation T56-A-14LFE COMMERCIAL ENGINE BULLETIN (CEB) Technical Publications Index November 1, 2017 72-- ENGINE 72--4001 Cancelled Prior to Publication A--72--4002 Engine -- Reduction Gear, Propeller
More informationSERVICE INFORMATION LETTER
SERVICE INFORMATION LETTER Document Number: 0001 Release Date: January 24, 2003 Revision: A PRODUCTS AFFECTED Corporation Aircraft Data Acquisition System (ADAS) and Corporation Aircraft Data Acquisition
More information2003 CATERPILLAR 140H Dealer Owned Rental Return Inspection
2003 CATERPILLAR 140H Dealer Owned Rental Return Inspection MOTOR GRADERS Serial #: APM00999 Inspection Number: Date Created: 08/07/2015 12:11:25 PM CDT Engine Serial #: N/A Last Updated: 08/12/2015 11:07:54
More informationAl -F402A-MMI-200 Change 2-10 April 1997 Page A
Al -F4A-MMI- - 1 April 1997 Page A NUMERICAL INDEX OF EFFECTIVE WORK PACKAGES Original.... 15 November 199 (INCL previously inc IRAC 1 and RACs through 8) RAC..... 9. 15 December 1991 RAC.. 11...... 15
More informationDGCANO SUBJECT REFERENCE COMPLIANCE APPLICABILITY TURBINE (IPT) AND INTERMEDIATE PRESSURE COMPRESSOR (IPC) SHAFT SPLINE FLANK WEAR
DGCA/RR RB 211-TRENT 700/800 SERIES/01 DGCA/RR RB 211-TRENT 700/800 SERIES/02 DGCA/RR RB 211-TRENT 700/800 SERIES/03 TO PREVENT THRUST REVERSER HINGE FAILURE TO PREVENT INTERMEDIATE PRESSURE TURBINE (IPT)
More informationSymbols used: Please, pay attention to the following symbols throughout this document emphasizing particular information.
This SB revises SB-912-064/SB-914-045 Initial issue dated 10 October 2013 Periodic checking of the crankshaft journal (power take off side) for ROTAX Engine Type 912 and 914 (Series) ATA System: 72-20-00
More informationSUPER KING AIR B300 (350) S/N FL-492 N726TT
SUPER KING AIR B300 (350) S/N FL-492 N726TT OWNER: ADDRESS: PHONE: FAX: QUINT, LLC 820 GESSNER ROAD HOUSTON TX 77024 713-206-7422 OPERATOR: ADDRESS: PHONE: FAX: ELITE AIR, INC. 100 2ND AVENUE SOUTH ST.
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET No. IM.E.093 for PW1100G-JM Series Engines Type Certificate Holder 400 Main Street East Hartford, CT 06118 United States of America For Models: PW1133G-JM PW1133GA-JM PW1130G-JM
More informationAirworthiness Directive
Airworthiness Directive AD No.: 2014-0152R1 Issued: 02 March 2018 EASA AD No.: 2014-0152R1 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) 216/2008
More informationGeneral. APU Control System. APU Door System
.10 -Description and Operation General The Auxiliary Power Unit () provides electrical and pneumatic power for engine start and air conditioning, and supplies ground and in-flight electrical power. Pneumatic
More informationPremier Aircraft LLC. Differences Manual
Premier Aircraft LLC Differences Manual UPGRADE DIFFERENCES Page 2 NOTICE This document is intended to provide an overview of the modifications to Falcon 50 airplanes when Premier Aircraft LLC STC ST01951LA
More informationJet Propulsion. Lecture-13. Ujjwal K Saha, Ph. D. Department of Mechanical Engineering Indian Institute of Technology Guwahati
Lecture-13 Prepared under QIP-CD Cell Project Jet Propulsion Ujjwal K Saha, Ph. D. Department of Mechanical Engineering Indian Institute of Technology Guwahati 1 GE J79 Turbojet 2 Features Highly used
More information