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INDY ASSET—EXCHANGE—

2010 AGUSTA AW139 msn 31285

TOTAL TIME: 1505

8 VIP swiveling seats

Floor provision for 15 seat configuration

5 Displays including 2 MFD’s and 1 moving map

Super Silent soundproofing system

Enhanced Vision System (EVS)

Goodrich Hoist (winch) equipment

*Honeywell ADF, AHRS, ILS DME, VOR, Dual FDS

*FMS phase 5 upgrade

*EGPWS

*Primus 660 weather radar

*Aux fuel tank

*Mast vibration absorber

Extra Wide club seats with flat bed capability and a full berthing divan

Cabin management system with wireless interface for complete control on aircraft’s environmentand entertainment from your personal device

Spacious wardrobe and inflatable mattresses

For Specifications and Pricing CallTim Palma

317-414-1044Email:

[email protected]

10291 North Meridian St, Suite 200, Indianapolis, IN 46290

317.414.1044

A/C REGN. : VT-JSA ENGINE TYPE : PT6C-67C DATE : 25-Feb-2016 CAT A OPS Hrs: 337:31

SERIAL No. : 31285 LH ENGINE HRS: 1506:45 RH ENGINE HRS : 1506:45 CURRENT AFH: 1506:45 07:00

LH ENG: PCE-KB0664 LH ENGINE CT: 1499 RH ENGINE CT : 1458 LANDINGS: 2631 0

RH ENG: PCE-KB0665 LH ENGINE PT: 1533 RH ENGINE PT : 1529 HOIST HRS: 04:21 445:46

LH ENGINE IMP: 1686 RH ENGINE IMP : 1600 HOIST LIFTS: 38 444

S/N DESCRIPTION PART No. SL No.

INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F

HRS/CYC/ DATEREMARKS

1 INSURANCE 1 Y 10-Aug-2015 165 D 8-Aug-20162 AIRCRAFT WEIGHING 5 Y 20-Feb-2015 1456 D 20-Feb-20203 ARC 1 Y 16-Oct-2015 232 D 14-Oct-2016

4 AERO MOBILE LICENCE 2 Y 31-Dec-2014 309 D 30-Dec-2016ATA CH- 5 ROUTINE INSPECTION

1 25 HRS. INSPECTION 25:00 H 1495:57 14:12 H 1520:57 Lubrication


3 100 HRS. INSPECTION 100:00 H 1444:05 37:20 H 1544:05 Lubrication4 150 HRS. SPECIAL INSPECTION 150:00 H 1430:08 73:23 H 1580:08 Inspection5 200 HRS. INSPECTION 200:00 H 1465:21 158:36 H 1665:21 Inspection


7 600 HRS. INSPECTION 600:00 H 1147:17 240:32 H 1747:17 Inspection8 1200 HRS. INSPECTION 1200:00 H 1147:17 840:32 H 2347:17 Lubrication9 150 HRS./ 1 YEAR INSPECTION 150:00 H 1506:45 150:00 H 1656:45 Lubrication

150 HRS./ 1 YEAR INSPECTION 1 Y 9-Sep-2015 195 D 7-Sep-2016 Inspection10 300 HRS./1 YEAR INSPECTION 300:00 H 1465:21 258:36 H 1765:21 Inspection

300 HRS./1 YEAR INSPECTION 1 Y 2-Jan-2016 310 D 31-Dec-2016 Lubrication11 1200 HRS/ 2 YEAR INSPECTION 1200:00 H 1474:05 1167:20 H 2674:05 Lubrication

1200 HRS/ 2 YEAR INSPECTION 2 Y 31-Jan-2016 705 D 30-Jan-2018 Inspection12 1500Hrs / 2 YEAR INSPECTION 1500:00 H 1474:05 1467:20 H 2974:05 Inspection

1500Hrs / 2 YEAR INSPECTION 2 Y 1-Feb-2016 706 D 31-Jan-2018 Inspection13 6 MONTHS INSPECTION 6 M 31-Dec-2015 125 D 29-Jun-2016 Lubrication14 1 YEAR INSPECTION 1 Y 31-Jan-2016 339 D 29-Jan-2017 Inspection15 2 YEAR INSPECTION 2 Y 31-Jan-2016 705 D 30-Jan-2018 Inspection16 4 YEAR INSPECTION 4 Y 4-Sep-2014 921 D 3-Sep-2018 Inspection17 300 HRS. ENGINE INSPECTION 300:00 H 1444:05 237:20 H 1744:05 Inspection18 600 HRS. ENGINE INSPECTION 600:00 H 1147:17 240:32 H 1747:17 Inspection19 900 HRS. ENGINE INSPECTION 900:00 H 876:07 269:22 H 1776:07 Inspection

900 HRS./12 MONTHS ENGINE

INSPECTION900:00 H 1474:05 867:20 H 2374:05 Inspection

900 HRS./12 MONTHS ENGINE

INSPECTION12 M 1-Feb-2016 340 D 30-Jan-2017 Inspection

150 FH/03 Months Corrosion

Inspection150:00 H 1495:57 139:12 H 1645:57 Inspection


Inspection3 M 21-Feb-2016 86 D 21-May-2016 Inspection


Inspection300:00 H 1506:45 300:00 H 1806:45 Inspection


Inspection6 M 21-Feb-2016 176 D 19-Aug-2016 Inspection

23

BT 139-311 Subfloor Frame STA 2105

retromodification P/N

3G5306P47211, installation of (EASA

AD 2014-0048) Part I

300:00 H 1495:57 289:12 H 1795:57

22

Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

20

21

Landings (>27Kts):

Page 1 of 14 COSL VT-JSA







INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F


Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

Landings (>27Kts):

24




AD 2014-0048) Part I

6 M 19-Feb-2016 175 D 18-Aug-2016 Inspection

25




AD 2014-0048) Part II

1200:00 H 993:42 686:57 H 2193:42At the issue of BT 139-311

Dt 21-Feb-14, 993:42 Hrs.

26SB 41060 (FAA AD 2013-03-14,

DGCA/P&W PT6C-67C/01)- LH600:00 H 1349:12 442:27 H 1949:12

SB 41060 (FAA AD 2013-03-14,

DGCA/P&W PT6C-67C/01)- LH900 PT 1680 1047 C 2580

27SB 41060 (FAA AD 2013-03-14,

DGCA/P&W PT6C-67C/01)- RH600:00 H 1349:12 442:27 H 1949:12

SB 41060 (FAA AD 2013-03-14,

DGCA/P&W PT6C-67C/01)- RH900 PT 1676 1047 C 2576

28BT 139-288 Tail rotor control duplex

bearing.3000:00 H 558:40 1493:15 H 3000:00

At the issue of BT 139-288

Dt 3-Aug-12, 558:40 Hrs.

29

BT 139-296 TR shaft reinforcement


3G5306P42512, installation of

1500:00 H 1117:37 1110:52 H 2617:37

BT 139-296 TR shaft reinforcement


3G5306P42512, installation of

730 D 9-May-2014 74 D 9-May-2016

34New Misc 158 (FAA AD 2013-06-51)

5 year & 30 Hrs Hoist Hrs1825 D 17-Jul-13 872 D 16-Jul-18

New Misc 158 (FAA AD 2013-06-51)

5 year & 30 Hrs Hoist Hrs30:00 H 03:06 28:45 H 33:06 Monitoring on Hoist Hrs

35 BT 139-366 365 H 28-Sep-15 215 D 27-Sep-16

36 BT 139-402 600:00 H 1346:07 439:22 H 1946:07

37 BT 139-402 12 M 9-Jun-15 104 D 8-Jun-16

39BT 139-430 - GOODRICH RESCUE

HOIST OVERLOAD CLUTCH Part IV,

EASA AD 2015-0160

400 Lift 38 400 Lift 438

40 BT 139-410 30:00 H 1482:15 05:30 H 1512:15

11- PLACARDS AND MARKINGS








INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F


Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

Landings (>27Kts):

1 Decal (Phosphorescent)

A180A, A181A,

A182A, A241A,

A307A, A308A,

A907A, AW001DE,

3G1130A01393,

3G1130A01394,

3G1130A01395,

3G1130A01398,

3G1130A01399,

3G1130A01451,

3G1130A01453,

3G1130A01454,

3G1130A01651,

3G1130A01652,

3G1130A01653,

3G1130A01654,

3G1130A01655,

-- 5 Y 4-Sep-15 -- -- 1651 D 2-Sep-20Discard - Extension taken

from DGCA








INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F


Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

Landings (>27Kts):

18 - VIBRATION AND NOISE ANALYSIS AND ATTENUATION1 MVA Rod Assy. 3G1860A03535 R166/1 4500:00 H 08:50 00:00 -- 3002:05 H 4508:50 Discard

21 - ENVIRONMENT SYSTEM

1 Compressor pack drive belt (ECS) 1768-60 -- 600:00 H 1325:41 00:00 -- 418:56 H 1925:41

2 Compressor pack drive belt (ECS) 1768-60 -- 2 Y 10-May-2015 00:00 -- 439 D 9-May-2017 Discard

24 - ELECTRICAL POWER

1 Starter Generator 1152546-21152546-02403

(No. 1)1000:00 H 993:39 00:00 -- 486:54 H 1993:39 Overhaul

2 Starter Generator 1152546-21152546-02402

(No. 2)1000:00 H 993:39 00:00 -- 486:54 H 1993:39 Overhaul

3 45/25 kVA AC Generator4G2420V00451/15

1---

4 Main Aircraft Battery (44AH) 33204-002

(Marathon) 10803034 6 M 21-Feb-2016 -- -- 178 D 21-Aug-2016 CT & Re-conditioning

5 Aux. Aircraft Battery SAFT (27AH) 2778-1 U03527 6 M 31-Dec-2015 -- -- 125 D 29-Jun-2016 CT & Re-conditioning25 - EQUIPMENT / FURNISHINGS

1 Cargo Net Assembly 3G2550A00231 ---- 12 Y 29-Mar-2010 -- -- 2223 D 28-Mar-2022 Discard

2 Artex ELT C406-2HM 453-5001-419 170-10808 1 Y 31-Jan-2016 -- -- 340 D 30-Jan-2017Inspection (Part of 1Yr

Inspection)

3 First Aid Kit ---- ---- 1 Y 28-Sep-2015 -- -- 215 D 27-Sep-2016 Re-Certification26 – FIRE EXTINGUISHING

1 Cabin fire extinguisher (Portable) A072A02 06-2014 /00029 10 Y Sep-2009 -- -- 1284 D Sep-2019 Discard

2 Cabin fire extinguisher (Portable) A072A02 08-2009 / 06313 10 Y Aug-2009 -- -- 1253 D Aug-2019 Discard

3Pyrotechnic squib installed on Eng

Fire Exting 65411B1 Qty-02

30903914-1 &

30903915-1

Qty 01 of each

P/N10 Y May-2011 -- -- 1892 D May-2021

Discard (from date of

installation)

4Pyrotechnic squib installed on Eng

Fire Exting S/N 62355B1 Qty-02

30903914-1 /

30903915-1

Qty 01 of each

P/N10 Y Aug-2009 -- -- 1253 D Aug-2019

Discard (from date of

installation)

5 Fire extinguishing bottle (Engine) 3G2620V00131 61600B1 (LH) 5 Y May-2014 -- -- 1100 D Mar-2019 HST

6 Fire extinguishing bottle (Engine) 3G2620V00131 65411B1 (RH) 5 Y 24-Oct-2011 -- 240 D 22-Oct-2016 HST

28 – FUEL

1 Fuel Microbiological Test -- -- 1 Y 9-Sep-2015 -- -- 196 D 8-Sep-2016 MBT2 LH & RH Tanks Foam Installation 3G2810A00413 Qty 02 10 Y 1-Oct-2009 -- -- 1313 D 30-Sep-2019 Discard

29- HYDRAULIC POWER1 Power Control Module 3G2900V00651 1762 40000:00 H 1156:43 -- -- 39649:58 H 41156:43 Discard

31 - INDICATING/RECORDING

1 MAGNETIC COMPASS

3G3120A00231

(Mfr P/N - C2300L4-

24B)

AG3340

2Digital Clock battery ("AAA" Size

Alkaline) AT660100 7270 (Pilot) 2 Y 27-Oct-2014 -- -- 244 D 26-Oct-2016 Discard

3Digital Clock battery ("AAA" Size

Alkaline) AT660100 07938 (Co-Pilot) 2 Y 1-Feb-2016 -- -- 706 D 31-Jan-2018 Discard

On Condition (Last Done on 02-Oct-2010)

Not Installed on VT-JSA








INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F


Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

Landings (>27Kts):

4 ELT battery pack (C406-2HM) 452-0133 362965-060 5 Y 3-Sep-2014 -- -- 1253 D Aug/2019 Discard

5 MPFR CVR Flight Safety D51615-102 299011-005 3 M 31-Dec-2015 -- -- 34 D 30-Mar-2016 Downloading & analysis

6 MPFR CVR Airworthiness D51615-103 299011-005 6 M 1-Oct-2015 -- -- 35 D 31-Mar-2016 Downloading & readout

7 MPFR FDR Flight Safety D51615-102 299011-005 3 M 31-Dec-2015 -- -- 34 D 30-Mar-2016 Downloading & analysis

8 MPFR FDR Airworthiness D51615-103 299011-005 12 M 1-Oct-2015 -- -- 218 D 30-Sep-2016 Downloading & readout

9 CVR Annual Check D51615-102 299011-005 12 M 1-Oct-2015 -- -- 218 D 30-Sep-2016 As per CAR Annual Check

10 FDR Annual Check D51615-103 299011-005 12 M 1-Oct-2015 -- -- 218 D 30-Sep-2016 As per CAR Annual Check

11MPFR underwater beacon (Part of

MPFR)DK120 -- 6 Y 28-Aug-2015 -- -- 2011 D 28-Aug-2021 Overhaul

12MPFR underwater beacon (ULB)

battery kit810-2008/K ST27441

As per

Label28-Aug-2015 -- -- 1617 D 30-Jul-2020 Discard

13 MPFR D51615-102 386619-006 6 Y 1-Nov-2015 2076 1-Nov-2021 Overhaul

32 - LANDING GEAR

1 Left Main Landing Gear Assembly 3G3210V00137 00443 50000 L 0 0--

47369 L 50000 Retire

2 Right Main Landing Gear Assembly 3G3210V00237 00450 50000 L 0 0--

47369 L 50000 Retire

3 Nose Landing Gear Assembly 3G3220V00135 00462 50000 L 0 0 -- 47369 L 50000 Retire

4 Main Retracting Actuator Assembly 3G3230V00332 00737, 00738 50000 L 0 0 -- 47369 L 50000 Retire

5 Nose Retracting Actuator Assembly 3G3230V00132 00457 50000 L 0 0 -- 47369 L 50000 Retire

6Main Landing Gear Retracting

Actuator Bolt on Sponson Bracket 3G3210L00151 307PP, 328PP 160000 L 0 0 -- 157369 L 160000 Retire

33 - LIGHTS

1Emergency Exit Lighting Battery

Pack3G3350A01811 -- 2 Y

34-NAVIGATION1 ATC TRANSPONDER (Mode S) 7517400-887 0907F750 2 Y 9-Nov-2015 622 D 8-Nov-2017 Functional Check2 TCAS blindmate antenna system -- -- 4 Y N/A as TCAS blindmate kit installed (Long Nose Helicopter)

3 Air Data Module No. 1 & 2 HG1153CA0309063908,

090337732 Y 9-Nov-2015 0 -- 622 D 8-Nov-2017

Test i.a.w FAR 91.411

(EA43, Para. b, rev 01-01-

91)

4 Pitot-Static System Check -- -- 2 Y 9-Nov-2015 0 -- 622 D 8-Nov-2017

Test i.a.w FAR 91.411

(EA43, Para. a, rev 01-01-

91)

53- FUSELAGE1 TGB Fitting 3G5351A01152 DEM00006 7200:00 H 0:00 0:00 -- 5693:15 H 7200:00 Retirement Life2 Tail Assy. 3G5350A00135 A7/0701 19600:00 H 0:00 0:00 -- 18093:15 H 19600:00 Retirement Life

Tail Assy. 3G5350A00135 A7/0701 32000 L 0 0 -- 29369 L 32000

3 Main L/G LH Segment 3P5339A00333 0220 80000 L 0 0 -- 77369 L 80000 Retirement Life

4 Main L/G RH Segment 3P5339A00433 0222 80000 L 0 0 -- 77369 L 80000 Retirement Life

5 Rear Fuselage Assy. 3P5340A00133 PZL218 32000 L 0 0 -- 29369 L 32000 Retirement Life

6Tail Plane LH attachment Fitting on

Fin Upper3G5351A01433 DEM00015 7600:00 H 0:00 0:00 -- 6093:15 H 7600:00 Retirement Life

7Tail Plane RH attachment Fitting on

Fin Upper3G5351A01533 DEM00005 7600:00 H 0:00 0:00 -- 6093:15 H 7600:00 Retirement Life

N/A as Emergency Exit Lighting Not Installed








INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F


Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

Landings (>27Kts):

8Tail Plane Attachment Fitting on Fin

Lower3G5351A07532 DEM00011 10600:00 H 0:00 0:00 -- 9093:15 H 10600:00 Retirement Life

9 Tail Plane Upper LH Fitting 3G5309P03031 -- 7600:00 H 0:00 0:00 -- 6093:15 H 7600:00 Retirement Life

Tail Plane Upper LH Fitting 3G5351A08931 -- 7600:00 H 0:00 0:00 -- 6093:15 7600:00 Retirement Life

Tail Plane Upper RH Fitting 3G5309P03131 -- 7600:00 H 0:00 0:00 -- 6093:15 7600:00 Retirement Life

Tail Plane Upper RH Fitting 3G5351A09131 -- 7600:00 H 0:00 0:00 -- 6093:15 7600:00 Retirement Life

10 Tail Plane Lower Fitting 3G5351A09131 -- 10600:00 H 0:00 0:00 -- 9093:15 H 10600:00 Retirement Life

55- STABILIZER

1 Rod End (Fin end) 3G5510A03931 1301, 1292 4600:00 H 0:00 0:00 3066:56 1533:04 H 4600:00

Retire (Life Penality

Factor: Operation above

6400 kg= 4.5 FH)

2 Rod Sleeve (Pitch Link Sleeve) 3G5510A04152 931, 710 10000:00 H 0:00 0:00 -- 8493:15 H 10000:00 Retire

3 Rod End (Tail Plane End) 3G5510A04053 637, 638 10000:00 H 0:00 0:00 2844:03 7155:57 H 10000:00Retire (Life Penality


6400 kg, 4 FH)

4 Tail Plane Assy 3G5510A00133 -- 65000:00 H Not Installed. Installed Tail Plane P/N 3G5510A05431, S/N A7/126 is OC.

5 Rod Assyembly (Tail Plane) 3G5510A08931 -- 4600:00 H 0:00 0:00 3066:56 1533:04 H 4600:00Retire (Life Penality


6400 kg= 4.5 FH)

62 - MAIN ROTOR

1 Main Rotor Blade Assembly 3G6210A00131R1785, R1856,

Q1463, Q1280,

R1844

16800:00 H 0:00 0:00 -- 15293:15 H 16800:00 Retirement Life

2 Main Rotor Blade Assembly 3G6210A00131

R1785, R1856,

Q1463, Q1280,

R1845

50200 L 0 0 2631 47569 L 50200

Retirement Life (Life

Penalty Factor: Rotor

starts & stops with wind

speed above 27Kts=5

Landings)

3 Main Rotor Hub Assembly 3G6220A00332 Q294 46000:00 H 0:00 0:00 -- 44493:15 H 46000:00 Retirement Life

4 Main Rotor Rotating Swashplate 3G6230A00332 Q375 4800:00 H 0:00 0:00 1508:55 1784:19 H 4800:00Retirement Life (Life

Penalty Factor: External

Hoist Lift= 0.5H

5Main Rotor Rotating Swashplate

Reworked3G6206P01331 Not Installed

6Main Rotor Scissors Attachment

Flange Assembly 3G6220A00632 P297 47450:00 H 0:00 -- 45943:15 H 47450:00 Retirement Life

7 Main Rotor Damper Bolt 3G6220A01251Q2693, Q2689,

Q2692, Q2691,

Q2690


8 Main Rotor Elastomeric Bearing 3G6220V001540800, 0799, 0802,

0803, 0801100000 L 0 0 -- 97369 L 100000 Retirement Life

9 Upper Scissor Lever Assembly 3G6230A00832 Q920, Q921 14300:00 H 0:00 0:00 -- 12793:15 H 14300:00 Retirement Life

10 Lower Scissor Lever Assembly 3G6230A00932 Q1101, Q1104 20100:00 H 0:00 0:00 -- 18593:15 H 20100:00 Retirement Life

11 Main Rotor Damper 3G6220V01352 1176 2400:00 H 936:59 1791:12 -- 39:02 H 1545:47 Overhaul

12 Main Rotor Damper 3G6220V01352 MCR6006 2400:00 H 1367:13 558:00 -- 1702:28 H 3209:13 Overhaul

13 Main Rotor Damper 3G6220V01352 MCR5529 2400:00 H 936:59 484:15 -- 1345:59 H 2852:44 OverhaulPage 6 of 14 COSL VT-JSA







INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F


Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

Landings (>27Kts):

14 Main Rotor Damper 3G6220V01352 MCR5049 2400:00 H 936:59 1136:45 -- 693:29 H 2200:14 Overhaul15 Main Rotor Damper 3G6220V01352 1591 2400:00 H 936:59 648:12 -- 1182:02 H 2688:47 Overhaul

16 Main Rotor Rotating Swashplate 400:00 1258:35 00:00 -- 151:50 1658:35

MI62-06 - Inspection for

integrity of the bolts and

ring retaining the duplex

bearing - 39-A62-31-06-

00A-286A-A








INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F


Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

Landings (>27Kts):

63 - MAIN ROTOR DRIVE1 MGB Case, Top Assembly 3G6320A01035 Q217 17000:00 H 0:00 0:00 -- 15493:15 H 17000:00 Retirement Life

2 MGB Shaft, Main Rotor 3G6320A01853 Q318 15300:00 H 0:00 0:00 2080:31 11712:43 H 15300:00Retirement Life (Life

Penalty Factor CAT A

Training Ops= 1.7 3 MGB Shaft, Main Rotor 3G6320A01853 Q318 54000 L 0 0 -- 51369 L 54000 Retirement Life4 MGB Case, Main Assembly 3G6320A02738 Q237 10000:00 H 0:00 0:00 -- 8493:15 H 10000:00 Retirement Life

5 MGB Case, Main Assembly 3G6320A02738 Q237 77500 L 0 0 -- 74869 L 77500 Retirement Life

6 MGB Upper Fitting 3G6330A00232R1619, R1620,

R1621, R162295800 L 0 0 3519 89650 L 95800


Penality Factor: Operation

above 6400 kg= 2L)

7 MGB Antitorque Beam 3G6330A00532 Q489 20000:00 H 00:00 0:00 -- 18493:15 H 20000:00 Retirement Life

8 MGB Antitorque Beam 3G6330A00533 Q190 63000 L 0 0 -- 60369 L 63000 Retirement Life

9 Anti-torque Beam Bolts 3G6330L00351PPA0388,

PPA0451, 56000:00 H 00:00 0:00 -- 54493:15 H 56000:00 Retirement Life

10 Rotor Brake Disk 3G6351V00551 FR0409Ref.

Remarks Discard every 2 pads replacement or after emergency braking activation

11 MGB gimbal support assembly 3K6320A01132KHI-MMC-879,

KHI-MMC-81746000:00 H 00:00 0:00 -- 44493:15 H 46000:00 Discard

12 MGB input shaft and coupling 3G6310V00152 0771 , 0770 23500 L 0 0 -- 20869 L 23500 Discard

13 MGB input shaft and coupling 3G6310V00152 772 , 0770 5000:00 H 0:00 0:00 -- 3493:15 H 5000:00 Overhaul

14 Main gearbox assembly 3G6320A00135 R89 5000:00 H 0:00 0:00 -- 3493:15 H 5000:00 Overhaul

15 Torque tube (Gimbal Input) Assy. LH 3G6310A00532 MO.556 5000:00 H 0:00 0:00 -- 3493:15 H 5000:00 Overhaul

16 Torque tube (Gimbal Input) Assy. RH 3G6310A00532 MO.557 5000:00 H 0:00 0:00 -- 3493:15 H 5000:00 Overhaul

17 Number 1 Gimbal Crosshead 3G6310A00351 MO.130 5000:00 H 0:00 0:00 -- 3493:15 H 5000:00 Overhaul

18 Number 2 Gimbal Crosshead 3G6310A00451 MO.178 5000:00 H 0:00 0:00 -- 3493:15 H 5000:00 Overhaul

19 Lubricating Pump, MGB 3G6320V04252 0695, 0701 2500:00 H 0:00 0:00 -- 993:15 H 2500:00 Overhaul

20 Main Gearbox oil cooling fan 3G6320V03853 141600190 2400:00 H 0:00 0:00 -- 893:15 H 2400:00 Overhaul

21 Rotor Brake Actuator 3G6352V02452 334 33000 L 1518 0 -- 31887 L 34518 Overhaul

64 - TAIL ROTOR

2 Tail Rotor Blade Assembly 3G6410A00133 V3162 (Yellow) 40000 L -- -- -- 37369 L 40000 Retirement Life 4 Tail Rotor Blade Assembly 3G6410A00133 V3199 (Red) 40000 L -- -- -- 37369 L 40000 Retirement Life

6 Tail Rotor Blade Assembly 3G6410A00133 V3166 (Blue) 40000 L -- -- -- 37369 L 40000 Retirement Life 8 Tail Rotor Blade Assembly 3G6410A00133 V3192 (White) 40000 L -- -- -- 37369 L 40000 Retirement Life








INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F


Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

Landings (>27Kts):

9 Tail Rotor Blade Bolt 3G6420A00252 33500:00 H 0:00 0:00 -- 31993:15 H 33500:00 Retirement Life

10 Tail Rotor Hub Assembly 3G6420A00332 Q363 11250:00 H 0:00 0:00 1618:11 9743:15 H 11250:00



above 6400kg: 1.25FH)

11 Tail Rotor Hub Assembly 3G6420A00332 Q363 67500 L 0 0 3519 64869 L 67500

12Tail Rotor Elastomeric Spherical

Bearing 3G6420V00154

Yellow-0709,

Red-0715,

Blue-0716,

White-0717


13 Tail Rotor Elastomeric Damper 3G6420V00455 LK11036 (Yellow) 20000:00 H 1367:13 0:00 -- 19860:28 H 21367:13 Retirement Life

14 Tail Rotor Elastomeric Damper 3G6420V00455 LK4181 (White) 20000:00 H 787:27 518:24 -- 18762:18 H 20269:03 Retirement Life

15 Tail Rotor Elastomeric Damper 3G6420V00455 LK2565 (Red) 20000:00 H 723:00 687:36 -- 18528:39 H 20035:24 Retirement Life

16 Tail Rotor Elastomeric Damper 3G6420V00455 LK2014 (Blue) 20000:00 H 723:00 919:24 -- 18296:51 H 19803:36 Retirement Life

65 - TAIL ROTOR DRIVE1 Tail Rotor Shaft Drive Assy, No. 1 3T6510A00144 WRA0332 100000 L 2598 0 -- 99967 L 102598 Retirement Life

2 Tail Rotor Shaft Drive Assy, No. 2 3T6510A00241 TBL9552 16000:00 H 0:00 0:00 -- 14493:15 H 16000:00Retirement Life

3 Tail Rotor Shaft Drive Assy, No. 2 3T6510A00241 TBL9552 44800 L 0 0 3519 38650 L 44800



above 6400kg: 2L)

4 Tail Rotor Shaft Drive Assy, No. 3 3T6510A00339 TBR8405 16000:00 H 0:00 0:00 -- 14493:15 H 16000:00Retirement Life

5 Tail Rotor Shaft Drive Assy, No. 3 3T6510A00339 TBR8405 44800 L 0 0 3519 38650 L 44800



above 6400kg: 2L)

6 Tail Rotor Drive Flexible Coupling 3T6510V00152 2462, 2544, 2472,

2501, 255260000 L 0

0

-- 57369 L 60000

Retirement Life

7 TGB Input Flange Coupling 3T6521A07353 TBM0037 100000 L 0 0 -- 97369 L 100000 Retirement Life

8 IGB Output Flange Coupling 3T6521A07353 TBM0005 100000 L 0 0 -- 97369 L 100000 Retirement Life

9 TGB Output Housing 3T6522A05339 TBK4940 48000 L 0 0 -- 45369 L 48000 Retirement Life

10 TGB Center Housing 3T6522A05144 TBK4811 10000:00 H 0:00 0:00 -- 8493:15 H 10000:00 Retirement Life

11 TGB Center Housing 3T6522A05144 TBK4811 72200 L 0 -- 69569 L 72200 Retirement Life

12 IGB Input Flange Coupling 3T6521A05657 TBR7992 100000 L 0 0 -- 97369 L 100000 Retirement Life

13 IGB Housing Assembly, Centre 3T6521A05135 TBK4757 100000 L 0 0 -- 97369 L 100000 Retirement Life

14 Bearing support assembly 3T6510A00443 TBK0050 5000:00 H 0:00 0:00 -- 3493:15 H 5000:00 Overhaul

15 Intermediate gearbox 3T6521A00149 TBU4396 7500:00 H 0:00 0:00 -- 5993:15 H 7500:00 Overhaul

16 Tail gearbox Assy 3T6522A00243 TBU2470 7500:00 H 0:00 0:00 -- 5993:15 H 7500:00 Overhaul








INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F


Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

Landings (>27Kts):

67 - ROTOR FLIGHT CONTROLS1 Main Rotor Actuator Assy. 3G6730V00531 HSC238259 3000:00 H 1235:48 10:15 -- 2729:03 H 4235:48 Overhaul2 Main Rotor Actuator Assy. 3G6730V00531 HSC214810 3000:00 H 658:05 1447:38 -- 703:42 H 2210:27 Overhaul

3 Main Rotor Actuator Assy. 3G6730V00531 HSC220893 3000:00 H 658:05 182:30 -- 1968:50 H 3475:35 Overhaul

4 Tail Rotor Actuator Assy. 3G6730V00731 HSC246257 3000:00 H 1120:47 0:00 -- 2614:02 H 4120:47 Overhaul

71 – POWER PLANT

1Left main panel (Engine Inlet

Particle Separator System)3G7160V03751 RT5-4748 OC H On Condition Overhaul

2Right main panel (Engine Inlet

Particle Separator System) 3G7160V03851 RT3-3863 OC H On Condition Overhaul

3Shut Off Valve (Engine Inlet Particle

Separator System) (2 off) 3G7160V01451 0291, 0292 10000:00 H 00:00 0:00 -- 8493:15 H 10000:00 Overhaul

4 Bellows (Engine Breather Air Tube) 3G7130V00152 40000:00 H 00:00 0:00 -- 38493:15 H 40000:00 Discard

72 - ENGINE (P&W PT6C-67C) (LH- PCE-KB0664)

1 Engine 3045379-01 PCE-KB0664 5000:00 H 00:00 0:00 -- 3493:15 H 5000:00 Overhaul

2

Engine Accessories (Except FMM &

FCOC) -- --- 5000:00 H 00:00 0:00 -- 3493:15 H 5000:00 Overhaul

3 Fuel Management Module 3048676-07 16638388 5500:00 H 00:00 0:00 -- 3993:15 H 5500:00 Overhaul4 Fuel Cooled Oil Cooler 3118263-01 WA37506 5500:00 H 00:00 0:00 -- 3993:15 H 5500:00 Overhaul5 Compressor Rotor Stub Shaft 3054380-01 PKAAA274613 20000 C 0 0 -- 18314 C 20000 Life Limit

6 Compressor Rotor ( 1st stage) 3039001 TXA1C0672 20000 C 0 0 -- 18314 C 20000 Life Limit

7 Compressor Rotor ( 2nd stage) 3040952 EAAB000X076 20000 C 0 0 -- 18314 C 20000 Life Limit

8 Compressor Rotor ( 3rd stage) 3040933 EAAB000X083 20000 C 0 0 -- 18314 C 20000 Life Limit

9 Compressor Rotor ( 4th stage) 3040944 EAAB000X228 20000 C 0 0 -- 18314 C 20000 Life Limit

10 Impeller, Centrifugal 3055309-01 EAAB000X236 20000 C 0 0 -- 18314 C 20000 Life Limit

11 Compressor Turbine Disk 3053496-01 A002M62X 12000 C 0 0 -- 10501 C 12000 Life Limit

12 Power Turbine Disk (1st stage) 3045407-01 A002M758 12000 C 0 0 -- 10467 C 12000 Life Limit

13 Power Turbine Disk (2nd stage) 3058015-01 A002M758 12000 C 0 0 -- 10467 C 12000 Life Limit

14 Compressor Turbine Blades 3058991-01

HWCN3932,

HWCP1861

HWCX6869,

HWCX6873,

HWCX6879,

HWCX6880,

HWCX6888,

HWCX6892,

HWCX6898,

HWCX6903,

HWCX6908,

HWCX6910,

HWCX6913,

HWCX6922,

HWCX6924,

HWCX6925,

HWCX6930,

HWCX6934,

10000:00 H 0:00 0:00 -- 8493:15 H 10000:00Replace (at 10000Hrs or

60% creep whichever

comes first)








INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F


Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

Landings (>27Kts):

15 Power Turbine Blades, 1st Stage 3045412-01

HWCE1321,

HWCE1347,

HWCE1383,

HWCL5093,

HWCL5094,

HWCL5104,

HWCL5110,

HWCL5111,

HWCW5436,

HWCW5439,

HWCW5441,

HWCW5444,

HWCW5449,

HWCW5454,

HWCW5462,

HWCW5473,

HWCW5474,

HWCW5477,

15000:00 H 0:00 0:00 -- 13493:15 H 15000:00Replace (at 15000H or

50% creep whichever

comes first)








INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F


Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

Landings (>27Kts):

16 Power Turbine Blades, 2nd Stage 3045433-01

HWBW6741,

HWBW6742,

HWBW6832,

HWCN9724,

HWCN9734,

HWCN9751,

HWCN9759,

HWCN9762,

HWCN9768,

HWCN9770,

HWCN9783,

HWCN9806,

HWCN9812,

HWCN9814,

HWCN9833,

HWCN9835,

HWCN9838,

HWCN9841,

15000:00 H 00:00 00:00 13493:15 H 15000:00Replace (at 15000H or

50% creep whichever

comes first)

72 - ENGINE (P&W PT6C-67C) (RH- PCE-KB0665)1 Engine 3045379-01 PCE-KB0665 5000:00 H 00:00 3493:15 H 5000:00 Overhaul

2Engine Accessories (Except FMM &

FCOC) -- ----- 5000:00 H 00:00 3493:15 H 5000:00 Overhaul

3 Fuel Management Module 3048676-07 16637156 5500:00 H 00:00 3993:15 H 5500:00 Overhaul4 Fuel Cooled Oil Cooler 3118263-01 WA37512 5500:00 H 00:00 3993:15 H 5500:00 Overhaul

5 Compressor Rotor Stub Shaft 3054380-01 PKAAA274617 20000 C 0 0 18400 C 20000 Life Limit

6 Compressor Rotor ( 1st stage) 3039001 TXA1B9096 20000 C 0 0 18400 C 20000 Life Limit

7 Compressor Rotor ( 2nd stage) 3040952 TXA1C0376 20000 C 0 0 18400 C 20000 Life Limit

8 Compressor Rotor ( 3rd stage) 3040933 EAAB000W942 20000 C 0 0 18400 C 20000 Life Limit

9 Compressor Rotor ( 4th stage) 3040944 EAAB000X070 20000 C 0 0 18400 C 20000 Life Limit

10 Impeller, Centrifugal 3055309-01 TXA1C0480 20000 C 0 0 18400 C 20000 Life Limit

11 Compressor Turbine Disk 3053496-01 A002M62W 12000 C 0 0 10542 C 12000 Life Limit

12 Power Turbine Disk (1st stage) 3045407-01 A002M757 12000 C 0 0 10471 C 12000 Life Limit

13 Power Turbine Disk (2nd stage) 3058015-01 A002M75D 12000 C 0 0 10471 C 12000 Life Limit








INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F


Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

Landings (>27Kts):

14 Compressor Turbine Blades 3058991-01

HWCX6854,

HWCX6857,

HWCX6872,

HWCX6885,

HWCX6886,

HWCX6895,

HWCX6900,

HWCX6907,

HWCX6914,

HWCX6915,

HWCX6916,

HWCX6920,

HWCX6927,

HWCX6928,

HWCX6931,

HWCX6936,

HWCX6938,

HWCX6941,

10000:00 H 00:00 00:00 8493:15 H 10000:00

Replace (at 10000Hrs or

60% creep whichever

comes first)

15 Power Turbine Blades, 1st Stage 3045412-01

HWCW5338,

HWCW5403,

HWCW5406,

HWCW5408,

HWCW5419,

HWCW8616,

HWCW8626,

HWCW8640,

HWCW8681,

HWCW8695,

HWCW8696,

HWCW8707,

HWCW8727,

HWCW8993,

HWCW9007,

HWCW9017,

HWCW9020,

HWCW9034,

15000:00 H 00:00 00:00 13493:15 H 15000:00Replace (at 15000H or

50% creep whichever

comes first)

16 Power Turbine Blades, 2nd Stage 3045433-01

HWCN4879,

HWCN4881,

HWCN4937,

HWCN4942,

HWCN5052,

HWCN5146,

HWCN5155,

HWCP0512,

HWCP0553,

HWCP0603,

HWCP1208,

HWCP1281,

HWCP1394,

HWCP1418,

HWCP3468,

HWCP3530,

HWCP3736,

HWCP3742,

15000:00 H 00:00 00:00 -- 13493:15 H 15000:00Replace (at 15000H or

50% creep whichever

comes first)








INTERVAL

HRS/CYC

(LIFE LIMIT)

TYP

E1

INSTALLED

ON/DONE ON

AT A/F

HRS/DATE

COMPONENT

HRS. AT THE

TIME OF INST.

LIFE

PENALTY

HOURS /

LANDINGS

REMAINING

TIME (HRS/

MONTHS/ CYC)

T

Y

P

E

DUE AT A/F


Rotor Start/Stop at

wind>27Kts:

Ops >6400Kg Hrs:

Ops >6400Kg Lndg:

Landings (>27Kts):

73 – ENGINE FUEL AND CONTROL

1Fuel Pump Filter, Element (Both

Engines)

3059779-01

(Alt -3033355)--- 900:00 H 657:45 00:00 -- 51:00 H 1557:45 Replace

2Fuel Pump Filter, Element (Both

Engines)

3059779-01

(Alt -3033355)--- 3 Y 31-Dec-2015 -- -- 1038 D 29-Dec-2018

73 – ENGINE FUEL AND CONTROL

1 Oil Filter, Element (Both Engines) 3059678-01

(Alt:3107548-01)--- 900:00 H 723:00 00:00 -- 116:15 H 1623:00 Replace

2 Oil Filter, Element (Both Engines) 3059678-01

(Alt:3107548-01)--- 3 Y 21-Apr-2013 -- -- 55 D 20-Apr-2016

OPTIONAL EQUIPMENT LIFE MONITORING

1 External Hoist Cable Assy. 42325-298 --- 1500 HL 0 22 -- 1478 HL 1500 Retirement Life

2 External Hoist Cable Assy. 42325-298 --- 4 Y Aug-2013 -- -- 583 D Sep-2017

3 Ball Spline Assy 42277-118 --- 17791:00 H 00:00 00:00 -- 16284:15 H 17791:00 Retirement Life

4 Cable Drum 42325-213 --- 42360:00 H 00:00 00:00 -- 40853:15 H 42360:00 Retirement Life

5 Main Housing 44308-130 --- 4600:00 H 00:00 00:00 -- 3093:15 H 4600:00 Retirement Life

6Hoist Core K2 (Goodrich Rescue

Hoist Assy.)

3G2591V01531

(44316-12-101)0090 111:00 H 00:00 00:00 -- 106:39 H 111:00 Overhaul

7Hoist Core K2 (Goodrich Rescue

Hoist Assy.)

3G2591V01531

(44316-12-101)0090 10 Y --- Jul-09 -- 1222 C 1-Jul-2019

8 Cartridge, Cable Cutter 42315-281 6042 5 Y --- May-14 -- 1203 D Jun-19

Prepared by: Date: Checked by: Date:

Below 30 days, 30Hrs, 30L, 30C Below 100D, 100Hrs, 100L, 100C


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