STAVATTI AEROSPACE BRIEFING FEB 2022.pdf

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COPYRIGHT © 2022 STAVATTI AEROSPACE LTD
FEB 2022 CAGE CODE: 8GT89 DUNNS: 117383324 PSC: 1510
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SM-47 Super Machete
Air Defense Fighter
SM-100
STOL Intermodal Transport
SM-36 Stalma
Multi-Role Fighter
SM-39 Razor
Air Dominance Fighter

Brian D. Colvin
Vice President &
Director of UAS

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• Stavatti Aerospace Ltd (“Stavatti”) was founded in April 2014 in Eagan, Minnesota
• Stavatti was Reorganized as a Wyoming C Corporation in December 2019
• Stavatti acquired the Former USARC Facility (SNAPPER) at the Niagara Falls Internation-
al Airport (KIAG) on 30 October 2020. Totalling 173,358 sq ft on 19.8 Acres this facility now
serves as Stavatti Headquarters and Prototype Development Center.

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SM-27 Machete
Turboprop
Attack/Close Air Support
400 KTAS
8,000 lb Warload
870 nm Radius
$15 Million Unit Flyaway Cost
Cost Per Flight Hour (CPFH): $2,563
The SM-27 Machete is a Next Generation Turboprop Attack and Close Air Support (CAS) aircraft.
Heavily armored and with a 30mm cannon, the Machete series will provide a dedicated Close Air
Support (CAS) aircraft, replacing A-1s, OV-10s, AT-6Bs, Super Tucanos and A-10s. Satisfying the
need for a Future Close Air Support Aircraft, the SM-27 will have a maximum level speed of 400
KTAS, a tactical radius of over 870 nm and an external warload of over 8,000 lbs.

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1,148
PC-21
2,448
A-1H
2,820
A-29
950
PA-48
3,380
AT-6B
1,978
IA-58
1,220
OV-10A
Landing Distance (ft)
Over 50 ft Obstacle or as Published
1,148
SM-27
2,448
A-1H
2,820
A-29
950
PA-48
3,380
AT-6B
1,978
IA-58
1,220
OV-10A
480
795
PC-21
1,995
SM-27
2,500
A-1H
1,805
A-29
1,200
PA-48
2,145
AT-6B
2,313
IA-58
2,800
OV-10A
Takeoff Distance (ft)
1,600
PC-21
4,000
SM-27
1,600
A-29
1,100
AT-6B
2,700
A-1H
2,455
PA-48
1,956
IA-58
2,080
OV-10A
Maximum Power (SHP)
Maximum Sea Level Power
4,960
PC-21
4,275
SM-27
4,724
A-29
4,500
AT-6B
2,300
A-1H
5,000
PA-48
3,543
IA-58
2,650
OV-10A
Maximum Climb Rate (ft/min)
At Sea Level, Standard Day
Maximum Warload (lbs)
With Maximum Internal Fuel
2,292
PC-21
8,000
SM-27
3,307
A-29
3,120
AT-6B
8,000
A-1H
4,000
PA-48
3,307
IA-58
3,600
OV-10A
800
PC-21
3,800
SM-27
1,495
A-29
1,500
AT-6B
3,240
A-1H
1,997
PA-48
2,002
IA-58
1,240
OV-10A
Maximum or Ferry Range (nm)
With Maximum Internal + Maximum External Fuel
400
PC-21
870
SM-27
423
A-29
425
AT-6B
275
A-1H
407
PA-48
190
IA-58
198
OV-10A
Tactical Radius (nm)
0.50
PC-21
0.25
SM-27
0.44
A-29
0.41
AT-6B
0.22
A-1H
0.747
PA-48
0.92
IA-58
0.84
OV-10A
Relative Fuel Burn Ratio
Fuel (lbs) to move 1,000 lbs of Warload 1 nm
370
PC-21
405
SM-27
301
A-29
316
AT-6B
297
A-1H
350
PA-48
270
IA-58
244
OV-10A
Maximum Level Speed (KTAS)
Aircraft in Clean Configuration

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0.48
A-4M
SCORPION
0.31
A-10A
2.02
A-37B
0.65
Su-25 M-346
1.63
ARES
0.40
0.25
SM-27
0.61
8,440
A-4M
4,275
SM-27
SCORPION
6,000
A-10A
6,990
A-37B
5,000
Su-25
21,000
M-346
?
ARES
?
8,200
A-4M
8,000
SM-27
SCORPION
16,000
A-10A
4,100
A-37B
9,700
Su-25
6,614
M-346
900
ARES
Maximum External Warload (lbs)
6,200
0.46
A-4M
SCORPION
0.36
A-10A
0.41
A-37B
0.51
Su-25 M-346
0.44
ARES
Thrust-to-Weight (t/w)
Maximum Sea Level Thrust/MTOW
0.38
0.33
SM-27
0.60
1,740
A-4M
3,800
SM-27
SCORPION
2,454
A-10A
878
A-37B
1,450
Su-25
1,500
M-346
1,500
ARES
2,400
3,670
A-4M
480
SM-27
SCORPION
2,000
A-10A
1,710
A-37B
1,312
Su-25
1,900
M-346
2,000
ARES
?
3,520
A-4M
1,995
SM-27
SCORPION
4,000
A-10A
2,596
A-37B
1,970
Su-25
920
M-346
1,500
ARES
?
595
A-4M
405
SM-27
SCORPION
381
A-10A
440
A-37B
526
Su-25
585
M-346
375
ARES
450
440
A-4M
870
SM-27
SCORPION
540
A-10A
230
A-37B
380
Su-25
270
M-346
?
ARES
?

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The SM-28 is a single engine non-afterburning turbofan powered Close Air Support and Lead-In
Trainer. Armed with a 30mm cannon and able to carry 12,000 lbs of stores, the SM-28 has a maxi-
mum speed of over 0.90 Mach and a tactical radius of over 700 nm on internal fuel. Heavily
armored, the SM-28 can replace A-10 and all other subsonic CAS aircraft with greater effective-
ness, efficiency and survivability.
SM-28 Machete
Turbofan
Attack/Close Air Support
0.85+ Mach
12,000 lb Warload
700 nm Radius

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677
SM-28
440
A-4M
SCORPION
540
A-10A
230
A-37B
380
Su-25
270
M-346
?
ARES
?
0.48
A-4M
SCORPION
0.31
A-10A
2.02
A-37B
0.65
Su-25 M-346
1.63
ARES
0.40
0.61
0.30
SM-28
8,440
A-4M
SCORPION
6,000
A-10A
6,990
A-37B
5,000
Su-25
21,000
M-346
?
ARES
?
17,000
SM-28
8,200
A-4M
SCORPION
16,000
A-10A
4,100
A-37B
9,700
Su-25
6,614
M-346
900
ARES
Maximum External Warload (lbs)
6,200
12,000
SM-28
0.46
A-4M
SCORPION
0.36
A-10A
0.41
A-37B
0.51
Su-25 M-346
0.44
ARES
Thrust-to-Weight (t/w)
Maximum Sea Level Thrust/MTOW
0.38
0.60
0.41
SM-28
1,740
A-4M
SCORPION
2,454
A-10A
878
A-37B
1,450
Su-25
1,500
M-346
1,500
ARES
2,400
3,830
SM-28
3,670
A-4M
SCORPION
2,000
A-10A
1,710
A-37B
1,312
Su-25
1,900
M-346
2,000
ARES
?
2,063
SM-28
3,520
A-4M
SCORPION
4,000
A-10A
2,596
A-37B
1,970
Su-25
920
M-346
1,500
ARES
?
1,765
SM-28
595
A-4M
SCORPION
381
A-10A
440
A-37B
526
Su-25
585
M-346
375
ARES
450
595
SM-28
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$85,000 Unit Flyaway Cost
Cost Per Flight Hour (CPFH): $46.50
The SM-150 is a Next Generation two seat Sport Aircraft. Stylish and affordable, this advanced
sportplane will introduce a new generation to aviation. A three-surface aircraft, the SM-150 has
forward swept wings, canard foreplanes, twin V-tails and inverted vertical stabilizers. Constructed
from advanced aluminum foam metal sandwich materials, the SM-150 will be produced in
turbodiesel and hybrid powered variants as well as eVTOL personal air vehicle configurations.
SM-150
Turbo-Piston
2 Seat Sportplane
135 KTAS
575 lb Useful Load
850 nm Range

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Maximum Useful load (lbs)
Aircraft at MTOW
590
C-140
489
C-150
585
415-G
600
SM-150
610
A5
590
XL2
584
DA20
582
PA-38
Landing Distance (ft) Comparison
1,530
C-140
1,075
C-150
1,750
415-G
267
SM-150
1,590
A5
750
XL2
1,360
DA20
1,545
PA-38
Cabin Width (in)
Maximum Interior Cabin Width
36
C-140
34
C-150
36
415-G
60
SM-150
46
A5
48
XL2
41
DA20
42
PA-38
1,850
C-140
1,385
C-150
2,100
415-G
605
SM-150
1,130
A5
1,250
XL2
1,640
DA20
1,440
PA-38
Aircraft at Optimum Altitude for Maximum Speed
104
C-140
109
C-150
99
415-G
137
SM-150
95
A5
132
XL2
140
DA20
109
PA-38
Maximum Range (nm)
391
C-140
420
C-150
360
415-G
800
SM-150
427
A5
500
XL2
543
DA20
468
PA-38
640
C-140
670
C-150
550
415-G
1,243
SM-150
500
A5
669
XL2
1,000
DA20
720
PA-38
Nautical Miles Per Gallon (nmpg)
Maximum Range as Attained with Maximum Internal Fuel
16.9
C-140
13.0
C-150
16.3
415-G
33.3
SM-150
23.1
A5
18.4
XL2
24.5
DA20
15.8
PA-38
Maximum Wing Loading (lbs/sq ft)
Aircraft at MTOW
9.1
C-140
10.2
C-150
9.8
415-G
11.7
SM-150
11.6
A5
15.6
XL2
14.1
DA20
13.4
PA-38
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SM-26 Sleek
Turbo Piston/Turboprop
High Performance Sportplane
330 KTAS
1,150 lb Useful Load
1,100 nm Range
$850,000 Unit Flyaway Cost
Cost Per Flight Hour (CPFH): $331
The SM-26 is a High Performance Sportpane that delivers fighter handling, agility and style
to general aviation. Produced in both turbocharged as well as turboprop variants, the
SM-26 will be the world’s fastest FAR 23 certified piston powered aircraft. Available as a
civil sportplane as well as a military trainer and light attack aircraft, the SM-26 is a 66%
scale replica of its CAS cousin, the SM-27 Machete.

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SM-26 SLEEK SPECIFICATIONS
Dimensions
Powerplant
Weights
Loadings
Performance
Internal Dimensions
Aircraft: SM-26 Sleek Sportplane
Unit Flyaway Cost: $850,000
Manufacturer: Stavatti Aerospace Ltd
First Flight: Contact Stavatti
Accommodation
Avionics & Displays
HUD
HDD
COMM/GPS
IFF
Autopilot
FCS
Audio Panel
ELT/ULB
Crew
Seating
Two Seat Tandem
Crashworthy Sport Seats
Number
Type
Model
Manufacturer
Max HP
Prop RPM
Prop Type
Prop Diameter
Number of Blades
Max Wingspan
Max Length
Max Height
Wing Area
Wing Aspect Ratio
Wing LE Sweep
36 ft 0 in
25 ft 8 in
8 ft 6 in
156.6 sq ft
8.4
4.25°
1
Turbodiesel or Turboprop
NT750
NeoThrust
750
2,057
CS Scimitar
96 in
5
Wing Loading (MTOW)
Power Loading (MTOW)
Design Load Factor (MTOW)
Ultimate Load Factor (MTOW)
23.6 lbs/sq ft
4.9 lbs/hp
+6.50
+9.75
Canopy Embedded Display (CED)
SD224 LED Primary Display
Dual WASS GPS/COMM/NAV
ADS-B Out & In Transponder
All-Axis Digital Autopilot
Digital Power-By-Wire
Digital Bluetooth® Audio Panel
406 MHZ ELT & ULB
Empty
Max Internal Fuel
Max Baggage
Useful Load
Typical Landing (TLW)
Max Take-Off (MTOW)
2,550 lbs
660 lbs
130 lbs
1,150 lbs
3,140 lbs
3,700 lbs
Cabin Length
Cabin Width-Max
Cabin Height-Max
114.0 in
27.0 in
44.0 in
Max Level Speed @ SL
Max Level Speed @ FL50
Max Cruise Speed @ SL
Max Cruise Speed @ FL100
Max Cruise Speed @ FL200
Typical Cruise Speed @ FL100
Takeoff Speed; MTOW
Stall Speed; MTOW
Max Climb Rate @ SL
Service Ceiling
Max Speed Range @ SL
Max Speed Range @ FL300
Eco Cruise Range @ SL
Eco Cruise Range @ FL100
Eco Cruise Range @ FL300
Takeoff Ground Roll, TTW
Takeoff over 50 ft, TTW
Landing Ground Roll, TLW
Landing over 50 ft, TLW
268 Ktas
282 Ktas
296 Ktas
330 Ktas
311 Ktas
233 Ktas
257 Ktas
285 Ktas
219 Ktas
242 Ktas
65 KTAS
52 KTAS
5,081 ft/min
40,000 ft
440 nm
887 nm
575 nm
681 nm
1,019 nm
226 ft
659 ft
597 ft
1,023 ft

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Aircraft at MTOW
1,231
1,150
SM-26
489
C-150
1,115
SR-22T
615
Long-EZ
1,000
Ultra
1,020
G36
1,070
TTX SR-22GTS
1,178
1,023
SM-26
1,075
C-150
2,535
SR-22T
1,000
Long-EZ
2,650
Ultra
1,450
G36
2,640
TTX SR-22GTS
1,868
659
SM-26
1,385
C-150
2,080
SR-22T
1,000
Long-EZ
2,100
Ultra
1,913
G36
1,900
TTX SR-22GTS
Maximum Power Loading (lbs/hp)
Aircraft at MTOW
11.6
4.9
SM-26
16.0
C-150
11.4
SR-22T
11.5
Long-EZ
12.0
Ultra
12.2
G36
11.6
TTX SR-22GTS
183
330
SM-26
106
C-150
213
SR-22T
161
Long-EZ
242
Ultra
176
G36
235
TTX SR-22GTS
Maximum Range (nm)
900
1,113
SM-26
420
C-150
853
SR-22T
1,746
Long-EZ
1,100
Ultra
920
G36
1,270
TTX SR-22GTS
1,270
5,081
SM-26
670
C-150
1,203
SR-22T
1,750
Long-EZ
1,375
Ultra
1,230
G36
1,400
TTX SR-22GTS
9.8
SR-22GTS
10.1
SM-26
12.0
C-150
9.3
SR-22T
33.6
Long-EZ
12.4
Ultra
12.4
G36
12.5
TTX
Aircraft at MTOW
24.8
23.6
SM-26
10.2
C-150
24.8
SR-22T
16.2
Long-EZ
19.2
Ultra
20.2
G36
25.5
TTX SR-22GTS

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SM-31 Stiletto
Afterburning Turbofan
Trainer and Light Fighter
1.5+ Mach
7,000 lb Warload
2,000+ nm Range
The SM-31 Stiletto is an Advanced, 5th Generation Supersonic Trainer and Light
Fighter. Produced in Single Seat (SM-31S) and Two Seat (SM-31T) configurations, the
SM-31 is a stealthy, single engine aircraft with an internal weapons bay. The SM-31
will replace F-5, T-38, T-50, Boeing T-7A and MiG-21 Aircraft worldwide.

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8,600
F-CK-1A
8,818
TEJAS
7,100
SM-31S
4,400
F-5E
14,330
MiG-21
8,378
JF-17
7,000
JAS-39E
7,716
L-15B
With Partial Internal Fuel
Over 50 ft Obstacle or As Published
?
F-CK-1A
?
TEJAS
1,805
F-5E
1,608
MiG-21
2,690
JF-17
2,500
JAS-39E
?
L-15B
1,503
SM-31S
Over 50 ft Obstacle or As Published
?
F-CK-1A
?
TEJAS
2,625
F-5E
1,295
MiG-21
2,001
JF-17
2,900
JAS-39E
?
L-15B
940
SM-31S
Thrust-to-Weight Ratio
MTOW @ Maximum Power
0.70
F-CK-1A
0.68
TEJAS
0.72
F-5E
0.62
MiG-21
0.68
JF-17
0.41
JAS-39E
0.72
L-15B
0.80
SM-31S
Typical Combat Weight @ Sea Level, Standard Day
50,000
F-CK-1A
39,370
TEJAS
44,280
F-5E
50,000
MiG-21
?
JF-17
34,500
JAS-39E
39,370
L-15B
59,686
SM-31S
?
F-CK-1A
1,619
TEJAS
971
F-5E
2,200
MiG-21
1,879
JF-17
2,010
JAS-39E
1,926
L-15B
2,441
SM-31S
With Maximum Internal Fuel or As Published
?
F-CK-1A
270
TEJAS
323
F-5E
432
MiG-21
377
JF-17
165
JAS-39E
340
L-15B
364
SM-31S
Maximum Level Speed (MACH)
Aircraft in Clean Configuration @ Altitude
1.70
F-CK-1A
1.60
TEJAS
2.05
F-5E
2.00
MiG-21
1.60
JF-17
1.64
JAS-39E
1.40
L-15B
2.19
SM-31S
F-CK-1A
TEJAS
1.63
F-5E
0.37
MiG-21
0.63
JF-17
0.58
JAS-39E
L-15B
0.84
0.67
0.64
0.38
SM-31S

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6,614
M-346
6,614
Hawk
4,530
T-38
6,062
T-50
7,716
L-15B
7,100
T-4
5,952
L-159B
0
With Maximum Internal Fuel or As Published
SM-31T
1,540
M-346
1,980
Hawk
2,200
T-38
2,319
T-50
T-33 T-4
2,675
L-159B
4,904
?
1,490
SM-31T
1,050
M-346
2,100
Hawk
1,800
T-38
1,131
T-50
?
L-15B T-4
4,185
L-159B
4,002
SM-31T
1,370
0.60
M-346
0.29
Hawk
0.45
T-38
0.60
T-50
0.72
L-15B T-4
0.36
L-159B
0.53
0.59
SM-31T
21,000
M-346
11,800
Hawk
10,000
T-38
39,567
T-50
39,370
L-15B T-4
12,220
L-159B
33,600
39,554
SM-31T
1,500
M-346
1,700
Hawk
900
T-38
1,403
T-50
1,926
L-15B T-4
1,242
L-159B
1,093
1,982
SM-31T
270
M-346
538
Hawk
280
T-38
377
T-50
340
L-15B T-4
299
L-159B
479
393
SM-31T
0.89
M-346
0.88
Hawk
0.90
T-38
1.50
T-50
1.40
L-15B T-4
0.76
L-159B
1.3
1.72
SM-31T
0.46
M-346
0.33
Hawk
0.67
T-38
0.53
T-50
L-15B T-4
0.80
L-159B
0.52
0.64
0.35
SM-31T

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The SM-47 is a single engine afterburning turbofan powered Air Defense Fighter, Strike Fighter
and Trainer. A super-maneuverable aircraft with Forward Swept Wings, the SM-47 has a Mach 2.2
maximum level speed and a tactical radius on internal fuel of 800 nm. Armed with a 20mm can-
non and 9 external hardpoints to carry 12,000 lbs, the SM-47 replaces F-16 ADFs, F/A-18A/Bs,
Mirage 2000s and JAS 39 Gripens.
SM-47 Super Machete
Air Defense Fighter
2.0+ Mach
12,000 lb Warload
625 nm Radius

584
F/A-35A
480
F-16C
432
Rafale
325
Typhoon JAS-39E
2.30
MiG-35
1.80
F/A-18E
2.27
SM-47
1.80
1.60
F/A-35A
2.01
F-16C
2.00
Rafale
2.00
Typhoon JAS-39E
0.84
MiG-35
0.58
F/A-18E
0.37
SM-47S
0.42
0.84
F/A-35A
0.25
F-16C
0.38
Rafale
0.37
Typhoon JAS-39E

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The SM-100 is a twin engine transport designed to carry 25,000 lbs to 35,000 lbs of cargo in a 35
ft long cargo bay that is 10 ft high and 11.82 ft wide. With a 310 knot cruise speed and a range of
nearly 3,000 nm while transporting a 12.5 ton load, the SM-100 can operate from short unpre-
pared runways. A rugged airlifter, the SM-100 will be suitable for all transport missions. The SM-
100 will be produced in turboprop, hybrid electric, electric and hydrogen powered variants.
$36 Million Flyaway Cost
SM-100
Twin Turboprop
Transport
390 KTAS
25,000 lb Payload
3,000 nm Range

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SM-100 SPECIFICATIONS
Dimensions
Powerplant
Weights
Loadings
Performance
Payload Configurations
Aircraft: SM-100 Transport
Unit Flyaway Cost: $32,000,000
Accommodation
Internal Dimensions
Cargo Hold Length
Cargo Hold Max Width
Cargo Hold Max Height
Cargo Hold Floor Area
Crew
Seating
2
72
Number
Type
Model
Manufacturer
Max SHP
Prop Type
Prop Diameter
Number of Blades
Continuous Speed @ FL150
Takeoff Speed @ MTOW, SL
Approach Speed @ TLW, SL
Stall Speed @ TLW, SL
Max Climb Rate @ SL
Service Ceiling
Max Range @ FL150
Max Range @ FL200
Max Range @ FL250
Max Payload Range @ FL150
Ferry Range with Roll-On Tank
Takeoff Over 50 ft, TTW
Landing Over 50 ft, TLW
Max Wingspan
Max Length
Max Height
Wing Area
Wing Aspect Ratio
Wing LE Sweep
100 ft 0 in
86 ft 0 in
21 ft 4 in
900 sq ft
11.1
0.0°
Empty
Max Internal Fuel (JP-8)
Max Fuel Payload
Max Payload
Useful Load
Max Take-Off (MTOW)
42,000 lbs
22,000 lbs
26,000 lbs
35,000 lbs
48,000 lbs
70,200 lbs
90,000 lbs
2
Turboprop
PW150 Derivative
P&W Canada
6,000
Scimitar Prop Fan
162 in
8
Wing Loading (TLW)
Wing Loading (MTOW)
Power Loading (TLW)
78.0 lbs/sq ft
100.0 lbs/sq ft
5.6 lbs/shp
7.5 lbs/shp
2.5 g
342 Ktas
390 Ktas
328 Ktas
374 Ktas
343 Ktas
350 Ktas
310 Ktas
116 Ktas
118 Ktas
91 Ktas
2,664 ft/min
>35,000 ft
2,703 nm
2,949 nm
2,986 nm
1,243 nm
1,355 nm
5,300 nm
1,787 ft
2,595 ft
1,190 ft
2,316 ft
35 ft 0 in
11 ft 10 in
10 ft 0 in
395 sq ft
20 ft Sea-Land Containers
LD-3 Containers
88” x 108” 463L Pallets
HMMWVs (Humvees)
Economy Seats @ 31 in Pitch
Business Seats @ 31 in Pitch
Max Combat Troops
Max Para Troops
Max Liter Patients
1
6
4
2
72
50
84
60
63

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Aircraft at MTOW
16,980
CN-235
32,662
C-27J
48,000
SM-100
78,531
C-130H
49,035
C-160
26,956
C-295
36,384
C-123K
84,709
C-130J
3,823
CN-235
2,826
C-27J
1,580
SM-100
2,750
C-130H
2,850
C-160
2,392
C-295
1,800
C-123K
2,550
C-130J
4,593
CN-235
2,100
C-27J
2,595
SM-100
5,160
C-130H
2,950
C-160
2,769
C-295
1,809
C-123K
4,700
C-130J
Aircraft at MTOW
10.4
CN-235
7.6
C-27J
7.5
SM-100
8.6
C-130H
9.2
C-160
9.7
C-295
14.5
C-123K
8.9
C-130J
248
CN-235
325
C-27J
390
SM-100
320
C-130H
320
C-160
260
C-295
198
C-123K
378
C-130J
Maximum Range (nm)
With Maximum Internal Fuel and Payload
3,732
CN-235
1,160
C-27J
2,986
SM-100
2,046
C-130H
2,590
C-160
2,900
C-295
1,470
C-123K
2,835
C-130J
1,527
CN-235
1,250
C-27J
2,664
SM-100
1,830
C-130H
1,300
C-160
2,083
C-295
1,150
C-123K
2,100
C-130J
0.28
CN-235
0.38
C-27J
0.91
SM-100
0.30
C-130H
0.22
C-160
2,900
C-295
0.64
C-123K
0.41
C-130J
Aircraft at MTOW
57
CN-235
79
C-27J
100
SM-100
89
C-130H
65
C-160
79
C-295
59
C-123K
94
C-130J

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Aircraft at MTOW
18,008
C-2A
22,487
An-32
16,093
ATR-42
48,000
SM-100
24,150
DHC-5D
26,873
Q400
20,943
ATR-72
72,750
An-12
1,735
C-2A
4,123
An-32
3,415
ATR-42
1,580
SM-100
2,010
DHC-5D
4,221
Q400
2,832
ATR-72
1,640
An-12
2,560
C-2A
3,940
An-32
3,825
ATR-42
2,595
SM-100
2,875
DHC-5D
4,605
Q400
4,485
ATR-72
2,520
An-12
Aircraft at MTOW
5.5
C-2A
5.8
An-32
8.5
ATR-42
7.5
SM-100
7.9
DHC-5D
6.4
Q400
9.2
ATR-72
8.4
An-12
343
C-2A
286
An-32
300
ATR-42
390
SM-100
250
DHC-5D
360
Q400
275
ATR-72
419
An-12
Maximum Range (nm)
1,106
C-2A
647
An-32
801
ATR-42
2,986
SM-100
600
DHC-5D
1,360
Q400
825
ATR-72
1,945
An-12
2,610
C-2A
1,500
An-32
1,851
ATR-42
2,664
SM-100
1,820
DHC-5D
1,500
Q400
1,355
ATR-72
1,970
An-12
0.63
C-2A
0.36
An-32
0.54
ATR-42
0.91
SM-100
0.29
DHC-5D
0.78
Q400
0.50
ATR-72
0.42
An-12
Aircraft at MTOW
78
C-2A
74
An-32
70
ATR-42
100
SM-100
52
DHC-5D
95
Q400
77
ATR-72
103
An-12

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SM-100AT SPECIFICATIONS
Dimensions
Powerplant
Weights
Loadings
Performance
Retardant Delivery (RADS)
Aircraft: SM-100AT Airtanker & Water Bomber
Accommodation
Internal Dimensions
Cargo Hold Length
Cargo Hold Max Width
Cargo Hold Max Height
Cargo Hold Floor Area
Crew
Seating
2
72
Number
Type
Model
Manufacturer
Max SHP
Prop Type
Prop Diameter
Number of Blades
Takeoff Speed @ MTOW, SL
Approach Speed @ TLW, SL
Stall Speed @ TLW, SL
Max Climb Rate @ SL
Service Ceiling
Max Range @ FL150
Max Range @ FL200
Max Range @ FL250
Ferry Range with Roll-On Tank
Takeoff Over 50 ft, TTW
Landing Over 50 ft, TLW
Max Wingspan
Max Length
Max Height
Wing Area
Wing Aspect Ratio
Wing LE Sweep
100 ft 0 in
86 ft 0 in
21 ft 4 in
900 sq ft
11.1
0.0°
2
Turboprop
PW150 Derivative
P&W Canada
6,000
Scimitar Prop Fan
162 in
8
Wing Loading (TLW)
Wing Loading (MTOW)
Power Loading (TLW)
51.2 lbs/sq ft
100.0 lbs/sq ft
3.8 lbs/shp
7.5 lbs/shp
2.5 g
342 Ktas
390 Ktas
328 Ktas
374 Ktas
343 Ktas
350 Ktas
310 Ktas
116 Ktas
118 Ktas
91 Ktas
2,664 ft/min
>35,000 ft
2,703 nm
2,949 nm
2,986 nm
1,243 nm
1,355 nm
5,300 nm
1,787 ft
2,595 ft
1,190 ft
2,316 ft
35 ft 0 in
11 ft 10 in
10 ft 0 in
395 sq ft
Empty
Max Internal Fuel (JP-8)
Max Retardant Payload
Max Fuel with Retardant
Useful Load
Max Take-Off (MTOW)
43,550 lbs
22,000 lbs
35,000 lbs
10,500 lbs
46,450 lbs
46,075 lbs
90,000 lbs
RADS Manufacturer
RADS Model
RADS Capacity (USG)
RADS Capacity (lbs)
RADS Flow Rate (gpm)
RADS Net Weight (lbs)
RADS & Retardant (lbs)
Max Fuel with Retardant (lbs)
Coulson
RADS-XXL
4,200
35,000
1,600
2,760
37,760
10,500

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Retardant Capacity (USG)
As Published
3,000
146-200
913
Firecat
1,621
CL-415
3,000
P-3C
4,200
SM-100AT
2,362
P2V-5
3,500
LM-100J
4,000
C-130Q
3,620
146-200
2,500
Firecat
2,000
CL-415
2,770
P-3C
1,580
SM-100AT
3,192
P2V-5
3,100
LM-100J
2,750
C-130Q
4,950
146-200
4,000
Firecat
2,770
CL-415
5,490
P-3C
2,595
SM-100AT
4,365
P2V-5
3,050
LM-100J
3,580
C-130Q
414
146-200
220
Firecat
197
CL-415
411
P-3C
390
SM-100AT
284
P2V-5
355
LM-100J
325
C-130Q
Maximum Range (nm)
With Maximum Internal Fuel Only
1,570
146-200
1,100
Firecat
1,310
CL-415
4,830
P-3C
2,986
SM-100AT
3,457
P2V-5
2,390
LM-100J
2,046
C-130Q
2,000
146-200
1,200
Firecat
1,229
CL-415
1,950
P-3C
2,664
SM-100AT
1,940
P2V-5
2,100
LM-100J
1,900
C-130Q
Maximum Range as Achieved with Maximum Internal Fuel
0.51
146-200
1.43
Firecat
0.86
CL-415
0.52
P-3C
0.91
SM-100AT
1.00
P2V-5
0.35
LM-100J
0.30
C-130Q
Aircraft at MTOW
Aircraft at MTOW
40,316
146-200
12,323
Firecat
15,450
CL-415
80,509
P-3C
46,450
SM-100AT
35,970
P2V-5
83,650
LM-100J
78,531
C-130Q
112
146-200
54
Firecat
41
CL-415
109
P-3C
100
SM-100AT
80
P2V-5
94
LM-100J
89
C-130Q

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SM-36 Stalma
Multi-Role Fighter
Mach 2.6+
20,000 lb Warload
900 nm Radius
The SM-36 Stalma is a single engine, afterburning turbofan powered, Lo-Observable Air
Superiority and Multi-Role Fighter. Equipped with variable geometry swing wings, canard
foreplanes, internal weapons carriage and thrust vectoring exhaust nozzles, the SM-36 is a
Mach 2.6, super-maneuverable, 6th generation, STOL supercruise fighter intended to
replace F/A-18E/Fs and F/A-35s.

Crew
Seating
Single (S) or Two Seat (T)
MK18 or ACES 5 Ejection Seats

584
F/A-35A
480
F-16C
432
Rafale
325
Typhoon JAS-39E
976
SM-36
2000C
340
1.80
F/A-18E
1.80
1.60
F/A-35A
2.01
F-16C
2.00
Rafale
2.00
Typhoon JAS-39E
2.60
SM-36
2000C
2.20
0.51
F/A-18E
0.55
0.85
F/A-35A
0.64
F-16C
0.44
Rafale
0.45
Typhoon JAS-39E
0.44
SM-36
2000C
0.63

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18,000
J-20
21,000
17,630
17,673
15,432
18,085
9,766
8,378
SM-36
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
?
J-20
1,312
2,460
1,969
2,427
1,100
2,035
2,690
SM-36
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
?
J-20
1,399
1,805
1,313
1,398
1,100
1,475
2,001
SM-36
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
0.80
J-20
0.80
0.84
0.62
0.74
0.97
0.75
0.68
SM-36
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
59,842
J-20
65,000
55,000
?
58,260
69,120
59,000
?
SM-36
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
2,968
J-20
3,400
2,430
2,160
1,889
2,953
2,807
1,879
SM-36
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
727
J-20
976
768
648
459
748
810
377
SM-36
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
2.20
J-20
2.60
2.25
1.80
2.30
2.44
2.35
1.60
SM-36
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
0.76
J-20
0.44
0.74
0.56
0.56
0.66
0.64
0.63
SM-36
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27

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The SM-39 Razor is a 6th generation twin engine Air Superiority and Air Dominance Fighter
designed for both land and carrier based operations. Powered by two next generation variable
cycle afterburning turbofans, the SM-39 will have a maximum level speed in excess of Mach 4.0,
a tactical radius greater than 1,300 nm, internal weapons carriage and super-maneuverability.
The SM-39 will replace F/A-22, F-15, F-14, Su-27 and Su-57 aircraft.
SM-39 Razor
Afterburning Turbofans
Air Dominance Fighter
Mach 4+
25,000 lb Warload
1,300 nm Radius

SM-39 RAZOR SPECIFICATIONS
Dimensions
Max Wingspan
Max Length
Max Height
Wing Area
Wing Aspect Ratio
Wing LE Sweep
Powerplant
Number
Type
Model
Manufacturer
Afterburning Thrust (lbs)
Military Thrust (lbs)
Air Inlets
Nozzle
Weights
Loadings
Performance
Fixed Internal
Ammunition
Stores Stations (Internal & External)
Max Warload
Armament
Aircraft: SM-39 Razor
Accommodation
Avionics & Electronic Warfare
2
ACE; E1400-NT-520
GEAE; NeoThrust
52,000
40,000
Internal Compression
LO VG Thrust Vectoring
54 ft 6 in
78 ft 6 in
13 ft 8 in
1,132 sq ft
2.62
50.0°
46,000 lbs
30,000 lbs
25,000 lbs
65,000 lbs
100,000 lbs
Empty
Max Internal Fuel (IF)
Max External Warload
Typical Combat (TCW)
Max Take-Off (MTOW)
57.4 lbs/sq ft
88.3 lbs/sq ft
1.60 to 1
1.04 to 1
11.2 g
7.5 g
Wing Loading-TCW
Wing Loading-MTOW
Thrust-to-Weight-TCW
Thrust-to-Weight-MTOW
Design Load Factor-TCW
Design Load Factor-MTOW
1 x 20mm M61A2 or DEW
1,000 rds
6
25,000 lbs
Supercruise Speed @ FL350
Takeoff Speed: MTOW
Stall Speed: MTOW
Approach Speed: TLW
Stall Speed; TLW
Max Climb Rate @ SL
Service Ceiling
Max Speed Range, IF
Max Speed Radius, IF
Supercruise Range, IF
Supercruise Radius, IF
0.85 Mach Range, IF
0.85 Mach Radius, IF
0.85 Mach Ferry Range
1.30 Mach
4.00 Mach
2.50 Mach
136 Ktas
123 Ktas
115 Ktas
96 Ktas
>75,000 ft/min
>100,000 ft
950 nm
463 nm
1,200 nm
585 nm
2,800 nm
1,300 nm
5,000 nm
752 ft
1,460 ft
Radar
IRST
HUD
Comm
IFF
Data Link
GPS/INS
RF ECM
MAWS
DAS
SPJ
Chaff/Flare
ARACR AESA
EOTS or AEOTS
CED or HMD
AN/ASQ-242 or ACNI
AN/ASQ-242 or ACN
AN/ASQ-242 or ACN
FALCN
AN/ASQ-239 or AFIDEWS
AN/ASQ-239 or ADAS
AN/ALE-52
Crew
Seating
Single (S) or Two Seat (T)
MK18 or ACES 5 Ejection Seats
S
SM
M-
-3
39
9 R
RA
AZ
ZO
OR
R

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SM
M-
-3
39
9 C
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BFL Over 50 ft Obstacle
1,985
SM-39
1,476
F-15E
700
F/A-35A
3,000
F-16C
2,540
A-6E
657
F-22A
1,740
F/A-18E
2,400
F-14D
1,457
SM-39
984
F-15E
550
F/A-35A
1,500
F-16C
4,560
A-6E
1,574
F-22A
2,500
F/A-18E
2,500
F-14D
Thrust to Weight Ratio
1.05
SM-39
0.72
F-15E
0.66
F/A-35A
0.62
F-16C
0.31
A-6E
0.84
F-22A
0.67
F/A-18E
0.75
F-14D
75,000
SM-39
50,000
F-15E
60,000
F/A-35A
50,000
F-16C A-6E
60,000
F-22A
44,882
F/A-18E
45,000
F-14D
7,620
25,000
SM-39
24,500
F-15E
18,000
F/A-35A
19,272
F-16C
18,000
A-6E
20,000
F-22A
17,700
F/A-18E
14,500
F-14D
3,700
SM-39
3,100
F-15E
2,000
F/A-35A
2,400
F-16C
2,818
A-6E
2,000
F-22A
1,660
F/A-18E
1,735
F-14D
1,100
SM-39
790
F-15E
584
F/A-35A
740
F-16C
439
A-6E
410
F-22A
760
F/A-18E
665
F-14D
4.0+
SM-39
2.5
F-15E
1.6
F/A-35A
2.0
F-16C
0.98
A-6E
2.25
F-22A
1.8
F/A-18E
2.34
F-14D
0.46
SM-39
0.83
F-15E
0.85
F/A-35A
0.63
F-16C
1.08
A-6E
1.26
F-22A
1.22
F/A-18E
0.89
F-14D

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ST
TA
A
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A
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TT
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AE
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RO
OS
SP
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AC
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E
?
J-20
1,457
1,805
?
1,398
1,100
1,475
2,001
SM-39
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
0.80
J-20
1.05
0.84
0.62
0.74
0.97
0.75
0.68
SM-39
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
18,000
J-20
25,000
17,630
17,673
12,125
18,085
9,766
8,378
SM-39
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
727
J-20
1,100
768
648
459
748
810
377
SM-39
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
0.76
J-20
0.46
0.74
?
0.56
0.66
0.64
0.63
SM-39
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
?
J-20
1,985
2,460
?
2,427
1,100
2,035
2,690
SM-39
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
59,842
J-20
75,000
55,000
?
58,260
69,120
59,000
?
SM-39
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
2,968
J-20
3,700
2,430
2,160
1,889
2,953
2,807
1,879
SM-39
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
2.20
J-20
4.0+
2.25
1.80
2.30
2.44
2.35
1.60
SM-39
Su-35
J-31 Su-57
MiG-35 JF-17 Su-27
S
SM
M-
-3
39
9 C
CO
OM
MP
PA
AR
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IS
SO
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N

A Family of Modular Launch Vehicles
100 to 2,500 ton launch mass
5 to 100 ton Payload to LEO
Produced in Niagara Falls, NY Beginning in 2025
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• Stavatti’s Vision includes the design and production of Interplanetary and Interstellar Spacecraft
• Stavatti is pioneering Advanced Fusion Propulsion and Starship Enabling Technologies
• Interplanetary Vehicles will include Orbital Shuttles, Moon/Mars Transports & Space Fighters
• Stavatti’s Long Range Vision Concentrates on Interstellar Starships for Human Spaceflight
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UM
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FL
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AIRCRAFT
Patented & Novel Vehicle Configurations
Internal Compression Air Intakes
Wave Drag Reducing Configurations
Channel Wing STOL Configurations
Circulation & Boundary Layer Control
Non-Conventional Lift/Inertial Propulsion
AIRCRAFT SYSTEMS
Forth Power-By-Wire Flight Controls
Compact Electromechanical Actuators
Piezo-Electric Deicing
AIRFRAME
Novel Structural Configurations
Foam Metal Sandwich Structures
Nano-Corrosion Control
ARMOR
Foam Metal Sandwich Armor
Beskar™ Iridium Alloy Armor
HMWPIB Reactive Armor
Molecular Chromium Plate
AUTONOMY
Active Synthetic Intelligence (ASI)
BATTERIES & CAPACITANCE
Lithium-Graphene-Silicon Anode Battery
CREW PROTECTION
Standard Armor G-Suite (STAGS)
Modular Armored Cockpit (MAC)
Proprietary Zero-Zero Ejection Seats
POWERPLANTS & PROPULSION
Liquid Hydrogen & Hydrogen Fuel Cell Power
Electric and Hybrid Diesel Electric Power
Variable Cycle Turbojet Powerplants
MagnetoHydrodynamic Energy Bypass (MHEB)
Bladeless Boundary Layer Turbines
Radioisotope Gas Turbines
Hi ISP Plasma Rockets and Ion Engines
Integrated MicroGrid Solutions (IMGS)
Inertial Propulsion System (IPS)
Warp Drive By 2035
ROBOTICS
Autonomous Flight Droid (Aeromech Droid™)
SENSOR & AVIONICS
Micro AESA Sensor Technology
Charge Telescope
Stavatti Avionics System Architecture (SASA)
SOFTWARE
Stavatti Proprietary CAD/CAM/PLM Solution
STEALTH & LOW OBSERVABILITY
Active Wave Attenuation (AWA)
Active Plasma Cavity Stealth (APCS)
Ceramic-Metal Radar Absorbent Material
Nano-Stealth
WEAPON SYSTEMS
Gas Dynamic Directed Energy Weapons
Positron Warhead
Compact Air-To-Air Missile (CAAM)
Next Generation 20mm and 30mm Cannon Systems
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IN
NG
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COCKPIT & HUMAN FACTORS
Proprietary Crewstation Climate Systems
Proprietary Flight and Throttle Grips
COMPUTING
HyperKnowledge™
Photonic Processors
EtherForth and GreenArrays
DISPLAYS
Canopy Embedded Display (CED)
Holographic Multi-Functional Display (HMFD)
Full Panel Active Displays
ENERGY & POWER
K-Capture Electron Reactor
Fusor Reactor
Modulated Interference Fusion (MIF)
Thermo-Alpha Radio-Isotope Fuel Cell
Economical Synthesis of Radioisotope Fuels
MANUFACTURING TECHNOLOGIES
Directed Light Fabrication
Explosive Forming and Joining
Laserwelding and Friction Stir Welding
Laserforming of Titanium
Femtosecond Laser Machining
MATERIALS
Non-Carbothermic Titanium Diboride
Scandium Aluminum & Titanium
Boron & Graphene Nano-Fiber Composites
US5670574 High Temperature Resin
Beskar™ Iridium Alloy & Beskar Steel™
Key Enabling Breakthrough and Disruptive Technologies that Stavatti is
Developing or Has Licensed For Direct Applications Include:

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2M
M P
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• Stavatti’s Proposed 2M Plant will have a footprint of 2 Million sq ft and provide over
2 Million sq ft of combined office and aircraft manufacturing and assembly space.
• The 2M Plant is designed to manufacture 3 or more Stavatti aircraft models simul-
taneously under one roof and could serve as Headquarters to Stavatti Aerospace.
• The 2M Plant will employ 10,000 or more workers for a minimum of 20 years.
• Stavatti’s has begun the site selection process for the 2M Plant and is evaluating
more than 20 potential candidate sites at which to establish this facility.
• Ground-Breaking on the iconic 2M Plant is planned for 2023-2028.

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STA
V
ATTI AEROSPACE L
TD.
(Est 2014/2019)
STA
V
ATTI UKRAINE
(Est 2017)
STA
V
ATTI CORPORATION
(Est 1994)
STA
V
ATTI INDUSTRIES L
TD.
(Est 2016)
STA
V
ATTI EUROPE
(Est 2017)
STA
V
ATTI™

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OR
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STA
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ATTI AEROSPACE L
TD
STA
V
ATTI GENERAL AVIATION
STA
V
ATTI MISSILES & ORDNANCE
STA
V
ATTI INTERSTELLAR
STA
V
ATTI AEROSPACE SYSTEMS
STAVATTI INTERPLANETARY
STAVATTI COMMERCIAL AEROSPACE
STAVATTI MILITARY AEROSPACE

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STAVATTI ARMAMENT
STAVATTI MINING
STAVATTI INDUSTRIES LTD
STAVATTI SENSORS & AVIONICS
STAVATTI ADVANCED MATERIALS
STAVATTI AUTOMOTIVE
STAVATTI NAVAL SYSTEMS
STAVATTI ENERGY
STAVATTI NEOTHRUST
STAVATTI CYBERNETICS
STAVATTI MEDICAL
STAVATTI Pictures

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AE
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RO
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AC
CE
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CEO
PRESIDENT
SHAREHOLDERS
BOARD OF DIRECTORS
VICE PRESIDENTS AGENTS
ADVISERS
CTO
FSO
Chief Engineer
EXECUTIVE VICE PRESIDENT
CFO
SECRETARY
CIO
Non-executive personnel
COO
L
Le
ea
ad
de
er
rs
sh
hi
ip
p

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Stavatti business practices adhere to distinct Core
Values including...
• Best-in-Class Products
• Customer Success
• Mission Focus
• Responsibility and Patriotism
• Commercial Best Practices
• Employee Achievement and Success
• Revenue Creation
• Absolute Quality
• Leadership with Strategic Vision
• Individual Ability
• Continuous Learning, Improvement and Innovation
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lu
ue
es
s

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• New Aircraft Development Programs are funded by the internal resources
of Stavatti Aerospace and strategic investment partners through equity and
debt financing as well as a combination of sources.
• Investors include accredited investors, institutional investors, corpora-
tions, industry team members or government entities.
• Investors fund a portion or all of the development costs of a program in
exchange for an equity or royalty position in the joint venture company, a
direct royalty from the revenues of a specific aircraft product line or a value
added interest payment.
• All funding is provided in phases including a risk reducing Demonstration
and Validation (Dem/Val) phase, followed by Full Scale Development (FSD)
and finally Low Rate Initial Production (LRIP).
• Alternatively, certain programs, in particular special access development
programs, are funded entirely by end-user customers under contract, such
as the SM-39 Razor which may be funded under a USAF/DoD contract.
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UN
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STA
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ATTI MACHETE L
TD
STA
V
ATTI AEROSPACE L
TD
MILITARY AEROSPACE DIVISION INVESTOR(S)/Strategic Partner(S)
SM-27 MACHETE SM-28 MACHETE SM-47 SUPER MACHETE
Each Aircraft Program is typically structured as a stand-alone joint venture company
owned by Stavatti Aerospace Ltd and Investors and/or Strategic Partners. Joint ven-
ture companies are named after their associated program. Programs are managed
by an appropriate division of Stavatti Aerospace Ltd. Example aircraft program orga-
nizational structures include:
P
PR
RO
OG
GR
RA
AM
M S
ST
TR
RU
UC
CT
TU
UR
RE
E

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og
gr
ra
am
m P
Pr
ro
oc
ce
es
ss
s
Stavatti aerospace programs follow a streamlined, design, development,
production and customer support process unique to the industry...
Implementing this process, Stavatti develops and delivers entirely new,
advanced aircraft without sacrificing quality, performance or value.
Requirements &
Specifications Generation
Conceptual
Design
Advanced
Design
Detailed Design
& Integration
Demonstration &
Validation (Dem/Val)
Full Scale
Development (FSD)
Low Rate Initial
Production (LRIP)
Full Rate
Production (FRP)
Line Termination
& Reclamation

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Stavatti conducts all engineering and design in-house using PLM CAD tools
including SolidWorks Premium and CATIA
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EN
NG
GI
IN
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EE
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IN
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G

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• Military aircraft will be flight
tested at the Air Force Flight Test
Center (AFFTC), Edwards AFB to
ensure military qualification.
• Additional US DoD facilities,
including China Lake, will be
employed throughout the Stavatti
weapon system testing effort.
• General Aviation aircraft undergo a complete FAA Type and Production
Certification program, such as FAR Part 23, including flight testing at cen-
ters in California. Team Members including AESI will provide support.
• Stavatti will utilize Vehicle Systems Simulators (VSS or ‘Iron Birds’) for
lifetime fatigue testing as well as Full Mission Simulators for crew training.
DoD Stock Photo
• Stavatti aircraft will undergo extensive flight and operational testing to
achieve Military Qualification and/or FAA Type and Production Certification

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• Stavatti will provide total procurement
packages, including ground support
systems, ordnance, spares and delivery.
• Stavatti will provide complete aircrew
flight/combat training services as well
as maintenance instruction.
• All aircraft will have a 2,000 Hour Nose-
to-Nozzle Manufacturers Limited War-
ranty on all new aircraft and 24/7 world-
wide customer assistance.
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t
• Stavatti customers will benefit from full Contractor Logistical Support
(CLS) of a comprehensive aerospace defense enterprise.
• Stavatti can provide CLS directly
or can work with customers to
establish organic logistical support.

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• Stavatti now has the infrastructure to service essential customer aircraft
and defense needs now and for decades to come.
• Stavatti has been registered with the State Department-Office of Defense
Trade Controls as a manufacturer & exporter of US munitions list items.
• Stavatti sites have been licensed by the ATF and State DOTs. Stavatti is
registered with SAM and has CAGE codes 8GT89, 7C5S4, 1DRG1 and 4D9A0.
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S

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• North American Industry Classification System Codes (NAICS Codes)
Applicable to Stavatti Aerospace Ltd and Stavatti Industries Ltd Include:
N
NA
AI
IC
CS
S C
CO
OD
DE
ES
S
336411 Aircraft Manufacturing
336412 Aircraft Engine and Engine Parts Manufacturing
336413 Other Aircraft Parts and Auxiliary Equipment Manufacturing
488190 Other Support Activities For Air Transportation
336414 Guided Missile and Space Vehicle Manufacturing
336415 Missile and Space Vehicle Propulsion Unit Manufacturing
336419 Missile and Space Vehicle Auxiliary Equipment Manufacturing
336111 Gas Turbines Except Aircraft Manufacturing
332995 Aircraft Artillery Manufacturing
332993 Ammunition Except Small Arms Manufacturing
332994 Small Arms, Ordnance, and Ordnance Accessories Manufacturing
333132 Oil and Gas Field Machinery and Equipment Manufacturing
333131 Mining Machinery and Equipment Manufacturing
332710 Machine Shop
333249 Other Industrial Machinery Manufacturing
332117 Powder Metallurgy Part Manufacturing
541618 Other Management Consulting Services

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Contact Stavatti today at:
STAVATTI MAIL STOP
P.O. Box 3010
Niagara Falls, NY 14304
MN Tel: 651-238-5369
NY Tel: 716-205-8396
email: aerospace@stavatti.com
http://www.stavatti.com
STAVATTI NIAGARA
9400 Porter Road
Niagara Falls, NY 14304
STAVATTI MINNESOTA
P.O. Box 211258
Eagan, MN 55121
STAVATTI BUFFALO
4455 Genesee Street
Buffalo, NY 14225
STAVATTI WYOMING
30 N Gould Street, Ste 2247
Sheridan, WY 82801

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