ESN724108 PW4060-1C Lease Data Pack January 2010 Table of Contents 1. 2. 3. 4. 5. 6. 7. 8. Engine Specification Summary LLP Status Key SB & AD Status Shop Visit History & Modular Workscope Summary QEC/Accessory Status Performance/ECM Summary/MPA Run Latest EASA Form 1/FAA 8130-3 Borescope Inspection Summary a) Last BSI Report b)Last Full Front to Back BSI Report If not covered in (8a) 9. Preservation Details 10. Non Incident / Accident Statement Lease Engine Data pack ESN 724108 1. Engine Specification Summary TES Engine Specification Sheet PW4060-1C ESN 724108 Engine Details Status Date Engine Standard TSN CSN TSO CSO HPT 2 Blades CSN HPT 2 Blades PN Available For Certification 13-Aug-2009 Phase I 65,644 10,809 9257 1266 1,737 (post SB 72-716) 54L232 Sale Lease or Exchange FAA / EASA Form 1 Thrust LLP Limit (Fan) LLP Limiter (Fan) LLP Limit (Core) LLP Limiter (Core) RCC Status (Ad 2003-19-15) Latest EGTM Date of last BSI Date Available Engine Stand Available 58,000 lbs 4,191 Hub Front Compressor 4,191 Hub HPC Front Rotor RCC Compliant 52 degrees 20-Aug-2009 Immediately Yes Current Condition Serviceable with no repeat inspections QEC Configuration Items not included: IDG Starter Starter Ducts Exhaust Centre Body High Pressure Pilot Controller Starter Control Valve Inlet Cowl Hydraulic Pump Exhaust Sleeve Pressure Controller Anti Ice Duct TAI Valve AVM Last SV Details Date Shop TSN CSN 30 Nov 2006 SRT 56,387 9,543 CHM + RCC Workscope Summary TES Aviation Ltd - Lease Engine Specification Page 1 of 2 09/11/2009 Lease Engine Data pack ESN 724108 2. LLP Status . 6 Disk Stage 2 Disk Stage 3 Disk Stage 4 724108 CSN Part Number 50B321 50B422 0 Unknown Unknown Unknown 50A281 51H572 51H005 52H926-01 50H936 56H279 50H218 51L201 52L002 50L485 50L242 50L659 53L030 50N003 50N024 50N405 50N486-01 50N008 50N007 50N346 50N347 50A077 10.LLP Parts TSN Module Name LPC Module ESN 65.Lease Engine Specification Page 2 of 2 04-Nov-2009 .6-4 Disk Stage 1.644 Part Name Hub Front Compressor Disk Drum Rotor Stages 1.809 Serial Number R48533 R38203 0 Unknown Unknown Unknown P49488 N71530 N71364 R34932 R31946 P49292 RY7574 S80290 S59952 UD8771 TR4624 C331AA0534 CKLBD25578 R58379 R32180 R34499 R32107 RG6182 RY8003 TE1080 UF7427 S76017 Date 04-Nov-09 4060 / 4060A / 4060 / 4060A / 4060 / 4060A / 4060C Cycles Data 4060C Cycles Limit 4060C Cyc Remaining 10809 10809 10809 10809 10809 10809 10809 10809 10809 10338 10338 10338 10338 9642 5407 10809 10809 10809 10809 10809 10809 10809 10809 9085 15000 15000 30000 15000 15000 15000 15000 15000 15000 15000 15000 15000 15000 15000 15000 15000 15000 15000 15000 15000 15000 15000 15000 30000 4191 4191 19191 4191 4191 4191 4191 4191 4191 4662 4662 4662 4662 5358 9593 4191 4191 4191 4191 4191 4191 4191 4191 20915 LPC/LPT Coupling Turbine Shaft (LPC/LPT) Coupling HPC Module Hub HPC Front Rotor Disk Stage 5 Disk Drum Rotor Stages 6-12 Disk Drum Rotor Stg 13-15 and HPC Drive Shaft Disk Drum Rotor Stages 13-15 HPC Inlet Airseal Diffuser Airseal Hub Turbine Stage 1 Hub Turbine Stage 2 HPT Stage 1 Outer Rotating Air Seal Plate HPT Stage 2 Blade Retaining HPT Stage 1 Inner Rotating Air Seal HPT Stage 2 Rotating Air Seal HPT Stage 1 Ring LPT Disk Stage 3 LPT Disk Stage 4 Hub Rear Turbine Stage 5 LPT Disk Stage 6 LPT Stage 3 Outer Air Seal LPT Stage 3 Inner Air Seal LPT Stage 4 Air Seal LPT Stage 5 Air Seal Front Compressor Drive Turbine (LPT) Shaft HPT Module LPT Module PW4000 Limit Set created from Engine Manual Revision 090 Dated 01 Sep 09 TES Aviation Ltd . Lease Engine Data pack ESN 724108 3. Key SB & AD Status . W. N FAA /CAA AD DGAC CN R Amdt D ESN: 724108 Engine TSN: 65634 Engine CSN: 10807 Compilation Issue: 2 TITLE METHOD OF COMPLIANCE / REMARKS LAST DATE HRS CYC Date: 09 Feb 2010 Latest FAA AD issue date: 01/02/10 Latest EASA AD issue date: 09/02/10 COMPLIANCE NEXT DATE HRS CYC REMARKS F-1990228-IMP (B) 90-22-02 39-6783 N LPT SHAFT INSPECTION. 4156.4056. A300 and A310 Series.A. (ATA 72) To prevent a LPT Shaft Break. B767.PW4000 Master Airworthiness Directive List MSN / Pos: n/a Engine Type: PW4000 Compilation Date: 09 Feb 2010 EASA No. perform an Eddy Current Inspection I. installed on B747. 4152.40 P&W.4052. before 01-Jan-1991 (For DGAC CN) or 31-Oct1990 (For FAA AD).4060. Template Issue 16 Page 1 of 13 Template Issue Date: 22/12/2008 . Concerns P&W Types Inspection performed at manufacture by 4050.4158 and 4460 Verified by P&W statement. 60A. SB PW4ENG A72-328. and thereafter at intervals not to exceed 10.Replace P/N FILTER BYPASS S332T004-23 with a new -23 Switch INDICATION OR LOSS OF OIL 2 – For Pratt & Whitney JT9D-7R4 Engines: QUANTITY FROM Replace P/N S332T004-25.000 total service hours.PW4000 Master Airworthiness Directive List MSN / Pos: n/a Engine Type: PW4000 Compilation Date: 09 Feb 2010 EASA No. SWITCHES modification in accordance with Boeing SB 76779-0008 is required in order to install a -29 switch configuration Pressure switches removed following the accumulation of 10.000 total service hours replace the engine oil filter differential pressure switches as follows: PREVENT FALSE OIL 1 – For Pratt & Whitney Engines: . N FAA /CAA AD DGAC CN R Amdt D ESN: 724108 Engine TSN: 65634 Engine CSN: 10807 Compilation Issue: 2 TITLE METHOD OF COMPLIANCE / REMARKS LAST DATE HRS CYC Date: 09 Feb 2010 Latest FAA AD issue date: 01/02/10 Latest EASA AD issue date: 09/02/10 COMPLIANCE NEXT DATE HRS CYC REMARKS Within 60 days after 28-May-1991 or prior to accumulating 10. -25 or -29 with a new FAILED PRESSURE 29 Switch. If a -2 or -25 Switch currently installed.000 total service hours shall not be re-installed on any airplane Concerns Model 767 series airplanes equipped with engine oil filter differential pressure switched on JT9D-7R4 and PW4000 engines - 91-09-15 N N/A by P/N Template Issue 16 Page 2 of 13 Template Issue Date: 22/12/2008 . whichever occurs later. 4060 and 4060A turbofan engines only.PW4000 Master Airworthiness Directive List MSN / Pos: n/a Engine Type: PW4000 Compilation Date: 09 Feb 2010 EASA No. N FAA /CAA AD DGAC CN R Amdt D ESN: 724108 Engine TSN: 65634 Engine CSN: 10807 Compilation Issue: 2 TITLE METHOD OF COMPLIANCE / REMARKS LAST DATE HRS CYC Date: 09 Feb 2010 Latest FAA AD issue date: 01/02/10 Latest EASA AD issue date: 09/02/10 COMPLIANCE NEXT DATE HRS CYC REMARKS F-1993130-IMP (B) 93-08-16 39-8564 N HPC FAILURE CAUSED BY AIRSEAL INTERFERENCE. (ATA 73) Apply "Boeing" ASB's 747-73A2055 and 76773A0033. 4052. 4056. N/A by P/N Concerns P&W Types 4050. Template Issue 16 Page 3 of 13 Template Issue Date: 22/12/2008 . Template Issue 16 Page 4 of 13 Template Issue Date: 22/12/2008 . N FAA /CAA AD DGAC CN R Amdt D ESN: 724108 Engine TSN: 65634 Engine CSN: 10807 Compilation Issue: 2 TITLE METHOD OF COMPLIANCE / REMARKS LAST DATE HRS CYC Date: 09 Feb 2010 Latest FAA AD issue date: 26/10/09 Latest EASA AD issue date: 03/11/09 COMPLIANCE NEXT DATE HRS CYC REMARKS F-1998423-IMP (B) 98-19-03 39-10746 N SECOND STAGE HPT ROTATING AIRSEALS P/N's 50L156 or 50L195. apply ASB PW4ENG 72628 R1. SB PW4ENG 72636 and 72-637 constitutes T/A.4460. To prevent Rotating airseal cracking. Within 6 Years after 09-Nov-1998.Nov 1997 . A330. 4158.4156A. at the next HSI (Any time HPT Module is disassembled) and subsequently each HSI.4062.W.4 152. modify Second (ATA 72) Stage Ring Segments and Vane Clusters and install modified Rotating Airseals I.4056. with 2nd stage high pressure turbine (HPT) rotating airseals.Eng CSN 5402 Concerns P&W Model 4052. fitted to A300. P/N's 50L156 or 50L195 installed. B767 & MD11. SB72636 . B747.Eng CSN 5402 SB72-637 .4060. Terminating action embodied. A310.4164 & 4168 turbofan engine.4462.PW4000 Master Airworthiness Directive List MSN / Pos: n/a Engine Type: Compilation Date: 09Feb 2010 EASA No.A.Nov 1997 . 4256.A. 4158. TITLE METHOD OF COMPLIANCE / REMARKS LAST DATE HRS CYC Date: 09 Feb 2010 Latest FAA AD issue date: 01/02/10 Latest EASA AD issue date: 09/02/10 COMPLIANCE NEXT DATE HRS CYC Concerns only P&W Model 4050.4650 turbofan engine.4160. REMARKS FAA /CAA AD Amdt N/A by SB status SB72-484 – Apr 1995 – Eng CSN 3371 SB72-486 – Apr 1995 – Eng CSN 3371 SB72-514 – Nov 1994 – Eng CSN 3218 SB72-575 – Nov 1997 – Eng CSN 5402 F-1999030-IMP (B) 98-23-08 39-10873 N HIGH PRESSURE COMPRESSOR (HPC) SURGE.4156A. Incorporate Stage 9 through 12 aluminium oxide blade tips and grind HPC blade tips at the rotor assembly I.W.15th stage zirconium oxide blade tips I.A. Modify HPC 8 . 72-486 R1. SB PW4ENG-72-514 R1. Modify 1st stage HPT cooling duct (TOBI Duct). 4062.W. P&W SB PW4ENG-72484 R3. 3.4056. Model Number. DGAC CN ESN: 724108 Engine TSN: 65634 Engine CSN: 10807 Compilation Issue: 2 N R D Within 1.4 462. (ATA 72) 2. 4. install metering plug in N°2 bearing thrust balance vent tube and incorporate 1st stage HPT vanes with increased airflow area I. not incorporating at least one of the modifications described in SB's listed in items 1) through 6). Incorporate HPC 13th . whichever occurs first. or prior to 30Jun-1999. 1) PW4ENG 72-484 R3.W.14 stage stators I.A. 2) PW4ENG 72-484 R3.4060/A /C.400 CIS after 12-Jan-1999.4052. excluding those engines having a (-3) identifier next to the Eng. perform the following modifications: 1.A.4156. SB PW4ENG-72-486 R1.PW4000 Master Airworthiness Directive List MSN / Pos: n/a Engine Type: PW4000 Compilation Date: 09 Feb 10 EASA No. th th Template Issue 16 Page 5 of 13 Template Issue Date: 22/12/2008 . 72-575 R1.4460. SB PW4ENG-72-575 R1.4152.W. Within 500 flight hours of 300 flight cycles after 24-Jan-2000. and attaching hardware are firmly attached). whichever occurs later. DGAC CN ESN: 724108 Engine TSN: 65634 Engine CSN: 10807 Compilation Issue: 2 N R D Initial and repetitive inspections: For group 1 & 2 airplanes: 1. evener bar. THE ENGINE FROM N whichever occurs later. accomplish work package 1 (a detailed visual inspection of the forward engine mount to ensure that the thrust link. LINKAGE FAILURE Thereafter repeat work package 2 on that engine at the intervals specified in the ASB. accomplish work package 3 (end cap bolt replacement of the forward engine mount). as listed in Boeing Alert SB 76771A0087 Template Issue 16 Page 6 of 13 Template Issue Date: 22/12/2008 . Prior to the accumulation of 16000 total flight cycles on any engine or within 500 flight hours SEPARATION OF of 300 flight cycles after 24-Jan-2000. accomplish work package 4 (bolt replacement) in accordance with ASB 767-71A0087. Replacement and terminating action: Within 3 years after 24-Jan-2000.Eng CSN 4670 F-2000047-IMP (B) 99-26-09 Concerns Model 767 series airplanes powered by P&W PW4000 and JT9D series engines. TITLE METHOD OF COMPLIANCE / REMARKS LAST DATE HRS CYC Date: 09 Feb 2010 Latest FAA AD issue date: 01/02/10 Latest EASA AD issue date: 09/02/10 COMPLIANCE NEXT DATE HRS CYC REMARKS FAA /CAA AD Amdt Terminating action embodied Boeing SB71A-0087 Nov 1996 . accomplish work THE AIRPLANE IN THE EVENT OF A package 2 non-destructive test inspection if the PRIMARY THRUST forward engine mount to ensure the proper condition if the engine thrust link components). associated lugs. For group 2 airplanes: Within 3 years after 24-Jan-2000.PW4000 Master Airworthiness Directive List MSN / Pos: n/a Engine Type: PW4000 Compilation Date: 09 Feb 10 EASA No. POSSIBLE 2. Thereafter repeat work package 1at the intervals specified in the Alert Service Bulletin until the requirements of the PREVENT AD are accomplished. 4156A.000 N CSN.500 CSN. with LPT 4th Stage air seal P/N's 50N478 or 50N478-001 installed.PW4000 Master Airworthiness Directive List MSN / Pos: n/a Engine Type: PW4000 Compilation Date: 09 Feb 2010 EASA No.500 & 6.000 CSN. replace prior further flight): 8.CN SUPERSEDES CN 2001-013-IMP R1AD SUPERSEDES AD 2000-25-06.000 CSN. 4158.4156A. B767 & MD-11. for those between 3.4060A.4060. and 4460 post SB PW4ENG72-657R1 fewer than 8. replace prior further flight): 4. N FAA /CAA AD DGAC CN R Amdt D ESN: 724108 Engine TSN: 65634 Engine CSN: 10807 Compilation Issue: 2 TITLE METHOD OF COMPLIANCE / REMARKS LAST DATE HRS CYC Date: 09 Feb 2010 Latest FAA AD issue date: 01/02/10 Latest EASA AD issue date: 09/02/10 COMPLIANCE NEXT DATE HRS CYC REMARKS F-2001113-IMP (B) 2001-05-07 39-12144 Replace the 4th stage air seal P/N 50N478 with a serviceable part P/N's 51N038 or 50N478-001 before the following limits (If limit exceeded.8.(ATA 72) 7.4164.4156. Concerns P&W Model 4052.4.000 CSN for PW4062 & 4462 fewer than FAILURE.000 CSN.4152. N/A by P/N N For PW4164. A330.500 CIS after 29-Dec-2000.000 CSN for those between 4. 7.4056.4156A.8. 1.000 & 4.500 CSN for PW4056. 4156 & 4158 fewer than 8.4060A.000 CSN for PW4056. 4062. and 4460 not LPT 4th STAGE AIR identified in Table 3 of AD and fewer than 8. 4060.500 CSN for those fewer or equal to 3. Template Issue 16 Page 7 of 13 Template Issue Date: 22/12/2008 .000 CSN for PW4052. 4152.4156A.4168A. 4460 & 4462 turbofan engine fitted to A300. 4152. 4168 & 4168A.000 CSN.500 CSN. replace the 4th stage air seal P/N's 50N478 or 50N478-001 with a serviceable part P/N's 51N038 before the following limits (If limit exceeded. 6. A310.000 SEAL CSN. B747.000 CSN for PW4056.4168. 4152. 4460 pre SB PW4ENG72-657R1 fewer than 4. N FAA /CAA AD DGAC CN R Amdt D ESN: 724108 Engine TSN: 65634 Engine CSN: 10807 Compilation Issue: 2 TITLE METHOD OF COMPLIANCE / REMARKS LAST DATE HRS CYC Date: 09 Feb 2010 Latest FAA AD issue date: 01/02/10 Latest EASA AD issue date: 09/02/10 COMPLIANCE NEXT DATE HRS CYC REMARKS N 1-Perform an initial inspection of HPC front rotors IAW on-wing §1 through 13 of PW ASB PW4ENG A72-722 or Rev. 18th May 2007 Eng CSN 9. 4062. PREMATURE CRACKING OF THE and the suspect crack indication extends from the knife-edges to the disk radius directly adjacent to HPC FRONT DRUM spacer wall of the sixth or seventh stage.000 CSN. remove and replace the HPC front drum rotor before further flight. 4060.184 th Template Issue 16 Page 8 of 13 Template Issue Date: 22/12/2008 . 4156A. 10 April 2008 Eng CSN 10. perform an E/C inspection within 5 cycles after item 1. for HPC front drum rotor with 1. 1): within 500 CIS after accumulating 1. and if necessary items 2.000 CSN or more. inspection of items 1.200 CSLI. 4-If the presence of a crack is confirmed. or within 500 CIS after 31-Jul-2002.543 N F-2002394-IMP (B) 2002-12-15 39-12787 N/A N N/A Concerns P&W Model 4052.384 N N/A N 5-Repeat every 2. DETECTION OF 3-If the presence of a crack needs to be confirmed. 3 or 4. perform an ROTOR(ATA 72) E/C inspection before further flight. 4152.000 CSN on 31-Jul-2002. SUPERSEDES CN 2001-514-IMP SUPERSEDES AD 2001-20-13. Sooner of: Next piece part exposure Or Eng CSN 12. 4056.PW4000 Master Airworthiness Directive List MSN / Pos: n/a Engine Type: PW4000 Compilation Date: 09 Feb 2010 EASA No. 4460 & 4462 Turbofan engines. for HPC front drum rotor less than 1. 4158. 2-If the presence of a crack needs to be confirmed. PREVENTION OF ENGINE POWER LOSSES DUE TO HPC SURGE. 4156. 4156A. 4158. 4460.PW4000 Master Airworthiness Directive List MSN / Pos: n/a Engine Type: PW4000 Compilation Date: 09 Feb 2010 EASA No.(ATA Thereafter. 4052. determine the applicable limits depending 72) on the engine configuration. 4060. 4060C.THIS CN SUPERSEDESCN 2002564-IMP (B) R1THIS AD SUPERSEDES AD 200221-10THIS AD SUPERSEDES AD 200311-18 Template Issue 16 Page 9 of 13 Template Issue Date: 22/12/2008 . N FAA /CAA AD DGAC CN R Amdt D ESN: 724108 Engine TSN: 65634 Engine CSN: 10807 Compilation Issue: 2 TITLE METHOD OF COMPLIANCE / REMARKS LAST DATE HRS CYC Date: 09 Feb 2010 Latest FAA AD issue date: 01/02/10 Latest EASA AD issue date: 09/02/10 COMPLIANCE NEXT DATE HRS CYC REMARKS N F2003382IMP Determine the engine configuration as per table 1 of present AD. 4160. SB 72-755 – May 07 – Eng CSN 9543 2003-19-15 N Concerns P&W Model 4050. Terminating action embodied. 4152. 4056. 4060A. 4462 & 4650 Turbofan engines. 4062. See AD for details. and 51A751. Part Numbers 50A443.PW4000 Master Airworthiness Directive List MSN / Pos: n/a Engine Type: PW4000 Compilation Date: 09 Feb 2010 EASA No. revise the Time Limits Section (TLS) of the Engine Manuals (EMs). 51A342. PW4000 SERIES 51A345. as TURBOFAN applicable ENGINES TIME Air carriers to revise the LIMITS SECTION approved continuous REVISION airworthiness maintenance program. 2005-25-09 N Template Issue 16 Page 10 of 13 Template Issue Date: 22/12/2008 . CYC Date: 09 Feb 2010 Latest FAA AD issue date: 01/02/10 Latest EASA AD issue date: 09/02/10 COMPLIANCE NEXT DATE HRS CYC REMARKS LPC Front Hub HPC5 Disk HPC Front Drum HPC Rear Drum Hub Turb Front Hub Turb Rear Airseal HPT2 LPT3 Disk LPT4 Disk LPT5 Disk LPT6 Disk 18 May 2007 18 May 2007 18 May 2007 18 May 2007 Next piece part Next piece part Next piece part Next piece part Next piece part Next piece part Next piece part Next piece part Next piece part Next piece part Next piece part This AD supersedes AD 2002-03-08. by adding the applicable parts of paragraph (f)(1) of this AD under the heading: “MANDATORY INSPECTIONS". 50A605. N FAA /CAA AD DGAC CN R Amdt D ESN: 724108 Engine TSN: 65634 Engine CSN: 10807 Compilation Issue: 2 TITLE METHOD OF COMPLIANCE / REMARKS LAST DATE HRS Within the next 60 days after the effective date of this AD. AD applies to all PW4000-94"/-100"/-112" engine Models. 50A822. 2009 (the effective date of this AD): (1) Perform a one-time visual inspection of the EEC131 model EECs to identify. and PW4462 turbofan engines preceding data) Template Issue 16 Page 11 of 13 Template Issue Date: 22/12/2008 . Group 2. PW4156A. report all inspection findings to Kevin Dickert. and mark them as a Group 1. PW4152. categorize. (3) Within 30 calendar days of completing paragraph (f)(1) of this AD.A73N CONTROL 214 R2 to inspect. Engine & Propeller Directorate. 12 New England Executive Park. (2) Use paragraphs 1 through 7 in the ENGINE FUEL AND Accomplishment Instructions of SB PW4000. Or PW4056. Burlington. EEC belongs to Group 2 Remove EEC by the sooner of: Applicable to PW4052. CSN 10647 at 21 Dec 2008 – closest PW4460. MA 01803.647 (eng PW4062. and mark the EECs. Eng CSN 15. 9 July 2011.PW4000 Master Airworthiness Directive List MSN / Pos: n/a Engine Type: PW4000 Compilation Date: 09 Feb 2010 EASA No. Group 3. PW4060. Engine Certification Office. categorize. (4) The Office of Management and Budget (OMB) has approved the reporting requirements and assigned OMB control number 2120-0056. or Group 4 EEC. N FAA /CAA AD DGAC CN R Amdt D ESN: 724108 Engine TSN: 65634 Engine CSN: 10807 Compilation Issue: 2 TITLE METHOD OF COMPLIANCE / REMARKS LAST DATE HRS CYC Date: 09 Feb 2010 Latest FAA AD issue date: 01/02/10 Latest EASA AD issue date: 09/02/10 COMPLIANCE NEXT DATE HRS CYC REMARKS N-200824-13 (B) 2008-24-13 Onetime Visual Inspection and Reporting Requirements (f) Within 600 operating hours after January 8. PW4158. 000 CIS after January 8. N FAA /CAA AD DGAC CN R Amdt D ESN: 724108 Engine TSN: 65634 Engine CSN: 10807 Compilation Issue: 2 TITLE METHOD OF COMPLIANCE / REMARKS LAST DATE HRS CYC Date: 09 Feb 2010 Latest FAA AD issue date: 01/02/10 Latest EASA AD issue date: 09/02/10 COMPLIANCE NEXT DATE HRS CYC REMARKS Replacement of Group 1 EECs (g) Replace Group 1 EECs with a serviceable EEC before reaching 2. as follows: (1) Group 2 EECs. PW4156A. Applicable to PW4052. and PW4462 turbofan engines N-200824-13 (B) {Cont’d} 2008-24-13 {CONT’D} Template Issue 16 Page 12 of 13 Template Issue Date: 22/12/2008 . (3) There are no scheduled replacement requirements for Group 4 EECs. 2009. 3. 2009. Replacement of Groups 2. 2011. or any EEC that does not violate N the EEC installation procedure as provided by CONTROL paragraphs (k). PW4152. (2) Group 3 EECs. 2010. before reaching 13. (l). PW4062.PW4000 Master Airworthiness Directive List MSN / Pos: n/a Engine Type: PW4000 Compilation Date: 09 Feb 2010 EASA No.000 CIS after January 8. but not later than July 8. 2015. and 4 EECs (h) Replace the following groups of EECs with a ENGINE FUEL AND serviceable EEC. but not later than July 8. PW4158. PW4060. but not later than January 8. PW4056. 2009. PW4460. before reaching 5.000 cycles-in-service (CIS) after January 8. and (m) of this AD. PW4460. (j) Information on obtaining a serviceable EEC can be found in SB PW4000. 2009. and marking of EECs before January 8.73-216. 2010 or any Group 1 EEC that has accumulated an additional 2. or a Group 4 EEC.000 CIS from January 8. 2011 N CONTROL or any Group 2 EEC that has accumulated an additional 5. categorizing. PW4062.000 CIS from January 8. (m) Do not install any Group 3 EEC after July 8. (l). ENGINE FUEL AND (l) Do not install any Group 2 EEC after July 8. PW4158. and PW4462 turbofan engines Template Issue 16 Page 13 of 13 Template Issue Date: 22/12/2008 .000 CIS from January 8. PW4060.PW4000 Master Airworthiness Directive List MSN / Pos: n/a Engine Type: PW4000 Compilation Date: 09 Feb 2010 EASA No. and (m) of this AD. 2015 or any Group 3 EEC that has accumulated an additional 13. N FAA /CAA AD DGAC CN R Amdt D ESN: 724108 Engine TSN: 65634 Engine CSN: 10807 Compilation Issue: 2 TITLE METHOD OF COMPLIANCE / REMARKS LAST DATE HRS Definition of Serviceable EECs (i) A serviceable EEC is an EEC that does not violate the EEC installation procedure as provided by paragraphs (k). PW4056. 2009. PW4156A. Previous Credit (n) Inspecting. CYC Date: 03 Nov Latest FAA AD issue date: 01/02/10 Latest EASA AD issue date: 09/02/10 COMPLIANCE NEXT DATE HRS CYC REMARKS N-200824-13 (B) {Cont’d} 2008-24-13 {CONT’D} EEC Installation Prohibition (k) Do not install any Group 1 EEC after January 8. 2009. END OF STATUS Applicable to PW4052. satisfy the requirements of paragraph (f)(1) of this AD. PW4152.A73214 original issue or Revision 1. 2009 performed using the Accomplishment Instructions of SB PW4000. Lease Engine Data pack ESN 724108 4. Shop Visit History & Modular Workscope Summary . 5th Lock found Broken Overhaul .334 15.402 7.599 19.372 3.721 UNK UNK UNK UNK M10 . Found HPC Rear Case worn & 11-14 Stator Damage Issue 2 Template issue Date:11/02/05 1 of 2 .266 CSLSV: Position/MSN: In storage At date: 04/10/2009 hours cycles hours cycles TSN Installed Removed 12-Jul-1989 3-Aug-1989 CSN Pos A/C Rag 28 26 1 OY KDH 306 53 Operator SAS 53 801 Operator 801 2.092 5. Eng Mods.engine update (Campaign) Installed Removed 24-Nov-1994 28-Jan-1995 19.218 Operator 3.1 & 1.071 29.371 4.Timex HPT Module Installed Removed 11-Jan-1994 20-Oct-1994 15.644 222168:00:00 TSLSV: 1.599 UNK UNK UNK UNK 6th HPC Blade L/E Torn (BMOD) Due. GB Deoiler & HSG DMG Installed Removed 30-Jun-1995 5-Oct-1996 18.046 19.046 UNK UNK UNK UNK Mod .301 4.5 Brg CD's.Engine History Summary Sheet ESN: 724108 Engine model: PW 4060-1c Date of Manufacture: TSN: 10.063 Operator 2 EC FCU SPP UNK UNK UNK UNK LPC Low Stab.402 Operator 2 EC FHA SPP UNK UNK UNK UNK High EGT.301 39.372 Operator 2.218 3.809 CSN: 65.071 3.670 5.371 Operator 1 LN RCB SAS 2 SE DOA SAS 2 EC FHA SPP 1 EC FCU SPP MSN TAT UNK UNK TAC UNK UNK Reason for removal/ additional comments Stg 5 Blade found over limit During BSI Installed Removed 11-Oct-1989 12-Sep-1990 306 4334 UNK UNK UNK UNK Installed Removed 4-Feb-1991 25-Sep-1993 4.670 Operator 2 EC FHA SPP UNK UNK UNK UNK BSI 6th Stg HPC blade Crack Installed Removed 13-Nov-1996 7-Aug-1997 26. Refurbished & overhauled Installed Removed 14-Nov-1997 29-Oct-1999 29.721 26. 635 9.644 10.615 7.390 19.063 8.Engine History Summary Sheet ESN: 724108 Installed Removed 26-Jan-2001 13-Apr-2002 39.001 Operator 1 LN RCH SAS UNK UNK UNK UNK Convenience Installed Removed 26-Mar-2005 8-Oct-2005 53.915 101.911 56.448 Operator 2 EC FHA SPP UNK UNK UNK UNK Convenience owner Repos Engine Installed Removed 26-May-2002 30-Jun-2003 49.001 9.615 53.543 Operator 1 PH AHX HXL UNK UNK UNK UNK Removed for Fuel Pump.092 49.807 10.543 10.924 19.807 Operator 1 PH MCI MPH UNK UNK UNK UNK Convenience A/C Parked Installed Removed TBC 19-Aug-2009 65.911 8.392 Ferry flight Issue 2 Template issue Date:11/02/05 2 of 2 .387 65. No Further info Available.809 Operator 1 PH MCG MPH 101.387 9. SV for O/H & RCC Incorporation Installed Removed 14-Jun-2007 16-Apr-2009 56.448 9.635 65. 266 11.809 CHM + RCC CHM + RCC CHM + RCC CHM + RCC CHM + RCC CHM + RCC 30-Nov-2006 30-Nov-2006 30-Nov-2006 30-Nov-2006 30-Nov-2006 30-Nov-2006 9.809 11.338 10.266 1.257 9.257 1.644 Total TSN 724108 CSN Total CSN 10.644 65.266 65.257 1.Modules Status TSN Module Name ESN 65.257 9.644 65.266 1.809 10.257 9.266 1.644 10.266 1.644 62.257 9.266 1.257 9.809 10.808 65.644 65.644 65.644 65.257 9.Lease Engine Specification 04-Nov-2009 .266 1.644 10.266 TES Aviation Ltd .809 Last Shop Visit Workscope CHM + RCC SV Date Date Hrs since SV 04-Aug-09 Cyc since SV Heavy Maintenance Date 19-Apr-2004 Hrs since SV Cyc since SV LPC Module LPC/LPT Coupling HPC Module HPT Module LPT Module Fan Case Fan Blade Module Intermediate Case Diffuser / Combustion Turbine Nozzles Turbine Exhaust Case Angle Gear Box Assy Main Gear Box Module 65.257 9.266 1.809 10.257 9.809 CHM + RCC CHM + RCC CHM + RCC CHM + RCC 30-Nov-2006 30-Nov-2006 30-Nov-2006 30-Nov-2006 9.257 1.480 10.809 30-Nov-2006 9.809 10.266 1.809 10.088 65.644 10.733 1.084 65. Lease Engine Data pack ESN 724108 5. QEC/Accessory Status . Template Issue 1 Page 1 of 5 Template Issue Date: 23/3/05 . Template Issue 1 Page 2 of 5 Template Issue Date: 23/3/05 . Template Issue 1 Page 3 of 5 Template Issue Date: 23/3/05 . Template Issue 1 Page 4 of 5 Template Issue Date: 23/3/05 . Lease Engine Data pack ESN 724108 6. Performance/ECM Summary/MPA Run . . . . . . Lease Engine Data pack ESN 724108 7. Latest EASA Form 1/FAA 8130-3 . . Lease Engine Data pack ESN 724108 8. Borescope Inspection Summary a) b) Last BSI Report Last Full Front to Back BSI Report If not covered in (a) . Lease Engine Data pack ESN 724108 8a) Last BSI Report . . . . . . Lease Engine Data pack ESN 724108 8b) Not Applicable . Lease Engine Data pack ESN 724108 9. Preservation Details . . Lease Engine Data pack ESN 724108 10. Non Incident / Accident Statement .