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Transcript of Commercially Sensitive and TEI Confidential Information This document and any attachments are for...
Commercially Sensitive and TEI Confidential Information
This document and any attachments are for the sole use of the intended recipients and may contain TEI proprietary and/or confidential information which may be privileged or otherwise protected from disclosure. Any unauthorized review, use, disclosure or distribution is prohibited. If you are not the intended recipients, please contact the sender by reply with any means and destroy the original document and any copies of the document as well as any attachments to the original document. Furthermore, the information contained in this document and/or attachment may contain information which is subject to governmental export control regulations (ITAR, EAR etc.). This information may not be exported, released or disclosed to third parties without first complying with the necessary governmental authorizations.
Tusaş Engine Industries, Inc.
February 11, February 11, 20102010
Rotating Parts / Modules Shafts - Fan, HPT, LPT Shafts and Disk+Shaft Combinations Seals - HPT, LPT, HPC, LPC Seals, Spacer Seals Disks - HPC, LPC and HPT, LPT Disks
Fabricated Parts - Exhaust Module and Combustor Components; Actuators, Manifolds, Honeycomb
Seals
Structural Parts - Casings, Frames, Housings, Support Rings
Commercially Sensitive and TEI Confidential InformationSubject to Restrictions on the Cover/First Page
588 Different Part Numbers for 33 Engine Programs
Engine Parts Mfg
Commercial
MilitaryGEnx
53,000-70,000 lbs.
✈ B787✈ B747
✈ B777GE9074,000-115,000 lbs.
✈ A319/A320/A321/A340✈ DC8✈ B737✈ KC135✈ E-3/E-6/KE-3A
CFM5622,000-27,000 lbs.
✈ A380GP720083,000 lbs.
✈ HondaJet✈ Spectrum FreedomHF120
2,630 lbs.
SaM14614,000-17,300 lbs.
✈ SUKHOI Superjet
CF640,000-73,000 lbs.
✈ A300
✈ A310
✈ A330
✈ B747
✈ B767
F110 100/129/132/400/SLE
P27,000-32,000 lbs.
✈ F-14✈ F-15✈ F-16
✈ T-50✈ F/A-18✈ F-117A✈ Gripen
F40410,300-18,100 lbs.
✈ B-2✈ U-2F118
17,000-19,000 lbs.
✈ C-5TF3922,000-26,320 lbs.
✈ AW A129
CTS8001,360 shp.
✈ F35 Joint Strike Fighter
F13640,000 lbs.
✈ A400MTP40010,000 shp.
J7917,820-18,730 Ibs.
✈ B-58✈ F-4✈ F-104✈ Kfir✈ A3J Vigilante✈ F-16/79
CF349,220-20,000 lbs.
✈ CRJ700✈ CRJ900✈ 604✈ 170/175✈ 190/195
T7003,000 shp.
✈ H-60✈ 214ST✈ AH-1W
LM series Marine Engines
J852,850-5,000 Ibs.
✈ T-38✈ F-5E/F Tiger II
CT71,700-2,145 Ibs.
✈ CN235✈ 214ST✈ EH101✈ S70/S80/S92
Engine Programs
Commercially Sensitive and TEI Confidential InformationSubject to Restrictions on the Cover/First Page
Commercially Sensitive and TEI Confidential InformationSubject to Restrictions on the Cover/First Page
1987
1997
1999
Cougar HelicopterEngine AIT (Makila1A1)
NATO Awacs A/CEngine DLM (TF33)
F16 A/CEngine AIT (F110)
F110 SLEP Upgrade & ENSIP Maintenance for TuAF2008
CT7-9C Repair & Overhaul for TuAF2008
Cougar HelikopterEngine DLM (Makila1A1)
2009
POIV, F16 A/C Engine AIT(F110-GE-129B)
2009
Engine Assy & Overhaul
AIT & MRO Center for TAF & Region
F110... Full DLM Capabilities incl. Testing
CT7/T700... MRO Capabilities
Makila 1A1... Assy. & O/H Capabilities incl. Testing
Commercially Sensitive and TEI Confidential InformationSubject to Restrictions on the Cover/First Page
Design Engineering
Development of J85 Ejector System (1997)
A400M / TP400 Project (RRSP) (2003)
F136 Component Design (2005)
Türkiye Technology Center (TTC) (2007)
RRSP / RSP RRSP / RSP PartnershipsPartnerships
Indigenous Indigenous DesignDesign
UAV Turboprop / Turbojet Engine Projects (2004)
Commercially Sensitive and TEI Confidential InformationSubject to Restrictions on the Cover/First Page
Potential Collaboration Areas
AIT & MRO business opportunities in the region
Engineering work & module responsibility for commercial & military engines in multi-disciplinary design activities
Engineering work on research projects (e.g. FP7)
Engine Module/Parts production opportunities with OEM’s
RRSP/RSP opportunities in commercial engine programs
Possible partnership on UAV Turboprop / Turbojet engine projects
Commercially Sensitive and TEI Confidential InformationSubject to Restrictions on the Cover/First Page
Thank You!