1. Capture
the
maximum
value
of
your
team
Engineering
excep6onal
aerospace
outcomes
2. Mission
Statement
“As
the
engineering
and
design
partner
of
choice,
we
will
enable
our
clients
to
optimize
project
performance
by
applying
our
high
end
technical
talent
to
deliver
engineering
solutions.
Our
personnel’s
expertise
reflects
comprehensive
capabilities
and
broad
industry
experience
that
will
be
employed
in
a
timely,
agile
and
extremely
cost
competitive
manner.”
3. Classifica0on
Small
Minority
Owned/Disadvantaged
Business
Cage
Code:
3DHZ5
Primary
NAICS
Codes
541712
Research
and
Development
541330
Engineering
Services
423690
Other
Electronic
Parts
&
Equipment
Wholesale
Manufactures
541511
Custom
Computer
Programming
Services
561910
Packaging
&
Labeling
Services
(Customized
Tool
Kits)
4. Core
Competencies
Program/Project
Management
Subcontract
Management
Systems
Engineering
Aviation
Systems
Hardware
Design
Reverse
Engineering
5. FlexInterface
Project
Fulfillment™
Integrity’s
innova0ve
project
methodology
Interface
at
any
stage
or
step*
of
the
product
development
process
(*
Over
160
steps
iden0fied
within
the
LEAN
Process)
• Defini0on
of
Requirements
(26
step
process)
• Preliminary
Design
(36
step
process)
• Detailed
Design
(73
step
process)
• Build
and
Test
(20
step
process)
• Documenta0on
(7step
process)
6. FlexInterface
Project
Fulfillment™
Defini0on
of
Requirements
Preliminary
Design
Detailed
Design
Prototype
Build
Characterize
and
Test
Produc0on
Ready
Documenta0on
System
Requirement
Review
(SRR)
Preliminary
Design
Review
(PDR)
Detailed
Design
Review
(DDR)
Technical
Data
Package
(TDP)
Test
Data
Review
(TDR)
Produc0on
Readiness
Review
(PRR)
Customer
Deliverables
7. FlexInterface
Advantage
• Maintain
greater
visibility
throughout
your
design
cycle
• Address
each
level
of
involvement
required
• Expedite
transi0on
0mes
between
development
stages
• An0cipate
and
avoid
process
complica0ons
• Specialized
exper0se
and
competency
–
selected
for
the
culture
• Direct
interface
with
suppliers
• Senior
level
supervision
(Project
Management)
• Up
to
MRL
7
product
level
standards
• Proven
performance
A
truly
collabora,ve
workflow
from
ini,a,on
to
comple,on!
8. Process
Op0miza0on
A1tude
of
Ownership
Addi9onal
layer
of
Senior
program
oversight
• Iden0fy
poten0al
manufacturing
improvements
• Implement
innova0ons
to
reduce
fabrica0on
and
assembly
costs
• Coordinate
suppliers
to
capture
opportuni0es
for
0me
and
cost
gains
• Reduce
lifecycle
costs
and
obsolescence
risks
9. Program
Management
Program
Management
• Project
Leadership
• Technical
Lead
and
Direc0on
• Cost
and
Schedule
Management
(Earned
Value
System)
• Hardware
and
Soware
systems
• Risk
and
Opportunity
Management
• Contract
Management
• Engineering
Change
Management
• Subcontract
Management
• Supply
Chain
Management
• Supplier
and
vendor
management
• Counterfeit
Parts
Management
• Purchasing
• Parts
planning
• RFP
and
Proposal
Development
and
Management
• Product
market
value
analysis
10. Logis0cs
• Life
Cycle
Logis0cs
support
to
US
Air
Force
and
Navy
Customers
and
their
Prime
Contractors
• Align
and
refine
product
support
package
(product
support
elements)
and
sustainment
processes
to
achieve
sustainment
metrics
• Op0mize
or
reduce
the
logis0cs
demand
(including
the
logis0cs
footprint)
and
support
processes
(training,
technical
data,
supply
chain,
maintenance,
etc.)
based
on
actual
condi0ons
• Develop
inventory
management
strategy
and
tools
for
Government
Furnished
Material
and
Contractor
Furnished
Material.
• Coordina0ng
and
resolving
data
interface
and
security
classifica0on
issues
across
the
en0re
supply
chain.
• Projects
• F4,
F16
Mul0na0onal
Fighters,
U2,
and
SR71
• Consolidated
Afloat
Network
Enterprise
Services
,
Liboral
Combat
Ship
11. Systems
Engineering
• Comprehensive
Test
Engineering,
TEMP,
Test
Plans,
procedure,
scripts
development
• Lead
for
Honeywell’s
PDU
Subsystem
Orion
Special
Test
Equipment
• Design,
build,
test
;
Na0onal
Instruments
Test
Suite
Experience;
Labview
• Systems
Life
Cycle
Process,
Requirements
Development,
Management,
SEMP
– DOORS,
Ra0onal
Tool
Set
(ReqPro)
• CONOPS
development,
Customer
CONOPS,
ORD,
TRD
analysis
• Design
Reviews,
Audits
• Systems
Architecture,
DODAF
and
UML
modeling
• Metric
development
and
management,
• Systems
FMEA,
Systems
Analysis,
Simula0on
Modeling,
Verifica0on
• Technical
Wri0ng
• Sta0s0cal
Analysis
12. Aircra
Systems
FAA/EASA
requirements
for
component
cer0fica0on,
FAA
Cer0fica0on
Process,
FAR
Part
25,
DO-‐160,
D0-‐178x
and
D0-‐254/CMMI
processes
Commercial
– Airbus
A350,
A380,
A400
– Boeing
747/757/767/777/787
– Gulfstream,
Bombardier
DOD
– B1,
B2,
F4,
F15,
F16,
F22,
C130,
C17
– Helicopters:
Apache
(AH64),
Comanche,
CH47,
V-‐22
GE,
Rolls
Royce
Engines;
Gas
and
Air
Turbines
– T45,
T53,
T55,
ALF502
/507,
L159,
LTS101,
AGT1500,
T800,
TF40
– LF502/507,
TFE731,
CFE738,
F124,
F125,
TFE1042
and
TPE331
Special0es:
– Airborne
Radar
Systems,
Diff.
GPS
landing
systems,
HUD,
Control
Systems,
Thrust
Reversers,
System
and
Component
Tes0ng/Test
Equipment,
Pneuma0cs,
engine
bleed
air
over-‐heat
detec0on
system
(OHDS),
Satellite
Telephone
System
Integra0on
Mul0ple
Patents
(9)
13. Space
Systems
• Extensive
background
on
MILCOM
Systems,
Iridium,
MUOS,
and
others
• Communica0ons,
Bus
Systems,
Mission
Analyses,
Ground
Control,
ORS,
Constella0ons
• ISR
Systems
• Reac0on
Control
Subsystem
• AOCS
• GPS,
IMU,
EO
sensors,
Simula0ons
• Electrical
Power
Subsystem
• Telemetry
and
Command
Subsystem
• RS232,
RS422,
RSS485,
DOD
1553
14. Hardware
Design
Electrical
– Circuit
Design:
analog,
digital,
RF
and
mixed
signal
circuit
design
– Signal
Integrity
– Power
regula0on
on-‐card
design
– Configurable
logic
systems
– Parts
and
Components
determina0on
– Standards:
IPC–2222;
IPC–2223;
SM–782;
Mil-‐P-‐55110
– PCB
design/layout/fab,
Assembly
Drawings
(All
toolsets)
– FMEA
Mechanical
– Design,
fab,
assembly
of
commercial,
military
and
space
hardware
– Proper0es
of
Materials
– 3D
solid
modeling
;
2D
and
3D
mechanical
analysis
(Ansys-‐11.0)
;
3D
fluid
flow
analysis
(Ansys/CFX-‐11.0)
– Electro/Mechanical
packaging,
rack
and
panel
configura0ons,
cabling
and
rou0ng,
configura0on
control/ECO’s
– CAD/manual
design/draing,
2D/3D
modeling,
detailed
mechanical
assemblies
15. RECON
Engineering
RECON
Engineering
Services
Obsolescence/Legacy
Engineering
• Update
older
systems
that
rely
on
obsolete
parts,
discon0nued
soware,
and/or
outdated
processors
wriben
in
older
programming
languages
• Conduct
current
System
Analysis
and
replacement
development
• Concurrent
Process
Flow
• Deliverables
include
updated/validated
PCB
Database,
Gerber
files,
drawings,
test
documenta0on,
func0onally
tested
PCB’s,
and
Embedded
Soware
programs
Electrical
Hardware
Reverse
Engineering
16. Toolsets
Systems
Engineering
– DOORS,
Ra0onal
Tool
Set
(ReqPro)
– Clearcase
and
Clearquest
– Matlab/Simulink/Mathema0ca
Embedded
Systems
– Xilinx,
Virtex,
Cadence
ModelSim
Electrical
Design
– Mentor
Expedi0on,
Board
Sta0on,
Auto
RE,
DX
Designer,
Design
Capture,
Design
Architect,
Pantheon
Intercept,
Mosaic,
Cadence
Allegro,
OrCAD,
Valor,
Gerb
Tool,
Hyperlinks,
PSPICE
Mechanical
Design
– Pro
/
Engineer,
Siemens
NX
7.x,
SDRC
Ideas,
Solid
Works,
AutoCAD
17. FlexInterface
Project
Fulfillment™
Integrity
alleviates
program
value
risk
• Greater
design
cycle
visibility
• Expanded
customer
interface
throughout
• Highly
customized
exper0se
• Senior
level
oversight
• Company-‐wide
amtude
of
ownership
19. Case
Study
Program:
Orion
Crew
Vehicle
Program
Client:
Honeywell
Scope:
• Program
management
• Subcontract
services
• Mechanical
design
and
documenta0on
• Electrical
circuit
and
PCB
design
• Parts
procurement
• Manufacturing
and
assembly
Outcomes:
• Reduced
turn
0me
by
over
40%
• Comple0on
of
five
(5)
test
fixtures
within
5
½
months
20. Case
Study
Program:
Nepires
Missile
Program
Client:
Raytheon
Missile
Systems
Scope:
• PCB
design
• Interfaced
with
mul0ple
manufacturing
vendors
to
meet
customer
requirements
• Applied
latest
design
and
manufacturing
capabili0es
beyond
the
customer’s
internal
requirements
• Manufacturing
and
assembly
Outcomes:
• Reduced
turn
0me
by
over
70%
• Completed
within
budgetary
targets
• Successful
first
launch
21. Case
Study
Orion
Space
System
• Working
with
Honeywell
Space,
designed,
built,
and
tested
5
different
System
Test
Equipment
(STE’s)
units
• Different
card
types
for
the
Orion
Space
Crew
Explora0on
Vehicle’s
(CEV)
Power
and
Data
Unit
(PDU)
included:
• Pyro
Events
Controller
(PEC)
• Network
Switch
Card
(NSC)
• PDU
Controller
• Solenoid
Driver
Output
(SDO)
• Analog
Digital
Input/Output
(ADIO)
units
• All
STE’s
delivered
to
Honeywell,
Clearwater
site
22. Case
Study
Orion
Space
Program
(cont.)
INTEGRITY’s
responsibili0es
• Overall
project
management
of
STE
development
• Interfaced
directly
with
both
Honeywell
Management
and
Engineering,
Tandel
Systems
Integra0on
personnel,
plus
all
subcontractors,
contract
shops
and
key
suppliers
and
vendors
• Requirements
and
Specifica0on
Development
• Architecture
comple0on
• STE
design,
review
and
verifica0on
• HW
design
and
review
• CDR
prep,
presenta0on
and
customer
buyoff
• Parts
iden0fica0on,
selec0on,
buy
and
review
• Mechanical
drawing
genera0on
from
architecture
to
component
level
• PCB
design,
layout,
fabrica0on
&
assembly
23. Case
Study
Commercial
AircraA
• Standards
• EUROCAE
ED-‐14D/RTCA
DO-‐160D
(Environmental
and
EMI/HIRF
Hardware
Test
Standards),
EUROCAE
ED-‐12B/RTCA
DO-‐178B
(Soware
Test
Standards)
and
RTCA
DO-‐254
(Design
Assurance
Standards
for
Airborne
Electronic
Hardware)
• A350
Extended
Mechanical
System
Perimeter
(EMSP)
• Validated
over
30
ABD
documents
through
mul0ple
revisions
• Populated
the
DOORS
database
with
flow
down
requirements
that
are
linked
from
the
ABD0100
and
ABD0200
requirements
• Established
and
con0nue
to
maintain
trace
links
from
the
DOORS
requirements
to
lower
level
Honeywell
systems
• Management
of
the
EMSP
System
Development
Plan
and
the
EMSP
Valida0on
and
Verifica0on
Plan
• Detailed
tracking
of
Work
Package
documenta0on
and
hardware
• Evalua0ng
and
verifying
the
interconnec0vity
between
all
Work
Packages
• Audit
support
across
all
levels
of
program
work
assignments
• Test
stand
integra0on,
checkout
and
commissioning
• Developing
detailed
component
and
systems
integra0on
procedures
to
authorize
ini0al
‘Power-‐On’
tes0ng
24. Case
Study
Commercial
AircraA
(cont.)
• A380
Electrical
Thrust
Reverser
Actua0on
System
(ETRAS)
• Supported
Preliminary
and
Cri0cal
Design
Reviews
including
Qualifica0on
and
Cer0fica0on
Review
mee0ngs.
• Provided
development,
audit
and
release
support
for
Valida0on
and
Verifica0on
documenta0on
deliverables.
• Performed
field
tes0ng
at
General
Electric
in
Ohio
and
at
Prab
&
Whitney
in
Florida
• Performed
lab
systems
tes0ng
for
design
assurance
(all
soware
versions)
and
for
mul0ple
qualifica0on
tests
(soware
versions
for
Airworthiness
Authority
approval)
• Developed
requirements
based
test
procedures,
performed
the
qualifica0on
test
and
wrote
the
test
reports
that
cover
soware
versions
FCS2,
FCS2+,
FCS2++,
• Updated
Test
Procedures
for
future
soware
revisions
(FCS3)
25. Case
Study
• Interna9onal
Space
Sta9on
Docking
System
– Prime
Contractor
Boeing
• INTEGRITY
supported
Honeywell
tes0ng
and
analysis
associated
with
linear/rotary
actuators
for
the
Low
Impact
Docking
System
(LIDS)
• INTEGRITY
supported
Honeywell
technical
inves0ga0ons,
design
evalua0ons,
and
key
supplier
development
issues
using
6
Sigma/
Lean
process
tools
– Presented
analysis
and
recommenda0ons
to
Boeing
customer
during
program
reviews