2. 7-9 September 2010
Hilton Orlando – Orlando, Florida
CTOL, STOVL and CV
Test Flights
2
3. 7-9 September 2010
Hilton Orlando – Orlando, Florida
F-35A CTOL
F-35A – Conventional Take Off and Landing (CTOL) variant will
replace U.S. Air Force F-16s and A-10s, as well as aircraft employed
by seven allied nations.
3
4. 7-9 September 2010
Hilton Orlando – Orlando, Florida
F-35B STOVL
F-35B Short Takeoff/Vertical Landing (STOVL) variant will replace U.S.
Marine Corps AV-8B Harriers and F/A-18s, U.K. Royal Air Force and
Royal Navy Harrier GR.7s, GR.9s and Sea Harriers and Italian Harriers.
4
5. 7-9 September 2010
Hilton Orlando – Orlando, Florida
F-35C CV
F-35C Carrier Variant (CV) will replace U.S. Navy F/A-18s.
5
6. 7-9 September 2010
Hilton Orlando – Orlando, Florida
Partners
Lockheed Martin is developing the F-35 with its principal
industrial partners, Northrop Grumman and BAE Systems.
Partner countries are the United Kingdom, Italy, the
Netherlands, Turkey, Canada, Australia, Denmark and Norway.
The F-35 program has about 900 suppliers worldwide.
6
7. 7-9 September 2010
Hilton Orlando – Orlando, Florida
CTOL Manufacturing Sequence Flow
J291 J294
SIDE PANEL AFT EQUIPMENT
LH ASSEMBLY BAY ASSEMBLY
J712 ENGINE J475
J714
FLAPERONS UPPER WING Wing to NACELL
J353 FIXED TIP INNER WING
SKINS Body E J292
CENTER FUSELAGE MODULE 2 FS496- J293
Fairings SKINS SIDE PANEL
L/H DUCT ASSEMBLY LOWER WING J480 556 J280 FORWARD EQUIPMENT
J354 RH ASSEMBLY
SKINS SUBSTRUCTURE MILL BAY ASSEMBLY
CENTER FUSELAGE INNER WING
BUILD-UP; Auto-drill; UNDERSTRUCT
R/H DUCT ASSEMBLY MODULE 1 FS425-472 J290
NACELLE SKIN URE
SUBSTRUCTURE COMPONENT MATE
J461 (LH) / J462 (RH) INSTL & MOLDABLE SHIM APPLICATION
J440 BUILD-UP; Auto-drill;
J270
INLET LIPS J711 OUTER WING SUBSTRUCTURE NACELLE SKIN INSTL TEMPORARY SKIN
DEBURR
LEADING BUILD-UP; AUTODRILL UPPER AND
STRUCTURE, INSTALL INSTALLATION &
J355 EDGE FLAPS LOWER SKINS; INSTL WTBF
SPLICE AREA NUT AUTODRILL
CENTER TANK DETAILS; FINAL INSTL LOWER
PLATES; FUEL SEAL; COCKPIT
STRUCTURE WING SKINS;INSTL NUTPLATES; Upper/Lower
ASSEMBL FUEL SEAL; FINAL INSTL & TEST J470 FLOORS
Straps J260
(No SWBS Number for J351 CONDUITS, BAY PAINT
INNER WING MODULE 1 FLOOR &
AF-14 and on per CR- FS 270-365 CENTER TANK & 2 ASSY; NACELLE CONSOLE
013699) STRUCTURE, SPLICE INSTL; DRILL & INSTALLATION
BRACKETS & SYSTE J430
INSTL UPPER & LOWER
J350 J460 ACCESS STRAPS AND
SUBSYSTEMS & EQUIPMENT J250
FS 270-425 UPPER MATE INSTL COMPLETION & OUTER WING TO INNER FIXED SKIN; DRILL I&R BAY PAINT
ASSEMBLY • ARRESTING GEAR ACTUATOR FUNCTIONAL TEST WING MATE; SUB- HOLE PATTERNS;
AFT DUCT & TANK J240
• AVIONICS RACKS FRAME INSTL; INSTL NUTPLATES;
TUBE & WIRE
• HEAT EXCHANGERS REMAINING WTBF FUEL SEAL; BAY PAINT
J356 J345 HARNESS INSTL EODAS
• IN FLIGHT REFUEL RECEPTICLE) DETAILS INSTL;
FS 365-425 AUTODRILL,
• IN FLIGHT REFUEL RECEPTICLE DOOR PARTIAL SYS INSTL
AFT DUCT NUTPLATE
ACTUATORS
STRUCTUR INSTALLATION
• OBIGGS J450 FWD J230
DOOR RIGGING, SEAL J200
UPPER SKIN • PAO PUMP RESERVOIR FUSELAGE SKIN &
& TEST DRILL SPLICE AREA; FORWARD FUSELAGE
PANELS & • WEAPON BAY DOOR CONTROLLERS LOOSE SYSTEMS
ACCESS • WEAPON BAY DOOR POWER DRIVE UNIT BORE MLG & DRAG LINK; ASSEMBLY COMPLETE INSTALLATIO
J330 COMPONENT FORWARD
PANELS • EODAS FINAL PREP UPPER WING S N
STRUCTURE COMPLETE, SKINS FUSELAGE
SKINS & DOORS NLG DOORS
J341, J342, INSTALLATION
J343
J220
FS 365-425 J570 NOSE LANDING GEAR FINAL SYSTEMS AND
LOWER CTR FUS R/H BOOM
SUBASSEMBLIES ASSEMBLE, SHIM
J320 J420 FUNCTIONAL TEST
(No SWBS SYSTEMS INSTALLATION
IFRR DOORS & DRILL Final Install Fixed Upper Skins
Numbers for AF-8 J560 SUBSTRUCTURE,
& TEST
and on per CR- & Fuel Covers; Install Fixed
013699) R/H BOOM MC EEE JOINTS Wing Tip Edges & Fairings; MAIN LANDING GEAR
GUN VENT UPPER / LOWER J310 Wing Exterior; Combined Fuel CM DOORS ACCESS PANELS
DOOR SURFACES MILL / DOOR CLOSE-OUT Tank Leak Test; LE Actuators & DOORS
J571
J550 DRILL & FINAL INSPECT
L/H BOOM J210
R/H BOOM (FOG)
ASSEMBLE, FINAL FINISHES
DEBURR, WET J300 (CTOL/CV)
J540 SHIM & DRILL
R/H BOOM ASSEMBLE SUBSTRUCTUR CENTER FUSELAGE WEAPONS BAY
J561 E, ASSEMBLY COMPLETE J834
COMPLETE DOORS
L/H BOOM MC EEE JOINTS & SHIP CANOPY
UPPER SKIN MLG
J530 UPPER / LOWER • MLG CHINES BUILD-UP
INSTALL & CENTER CLOSE-OUT
RH BOOM SURFACES MILL • FUSELAGE FAIRINGS
PAINT FUSELAGE PANELS
INSTALL J551 / DRILL
INTERNAL BAYS LOOSE
SYSTEMS & L/H BOOM (FOG) MAIN LANDING
COMPONENT • ADVANCED ESA RADAR ARRESTING GEAR
TEST FLUID DEBURR, WET GEAR DOORS
J541 S J862 DOORS
SYSTEMS ASSEMBLE • EOTS GUN
L/H BOOM AFT FUSELAGE
• DMC COMPUTER
COMPLETE FINAL FINISHES
J500 • VMC COMPUTER
UPPER SKIN J860 • 28V CONVERTERS
AFT FUSELAGE FUSELAGE
INSTALL & • 28V & 270V BATTERIES ARRESTING GEAR
J531 PREP FOR SHIP STRUCTURE
PAINT • AILERON ACTUATORS
LH BOOM AND SHIP MATE
J511 INTERNAL • FLAPERON ACTUATORS
INSTALL BAYS J515
TAIL HOOK SYSTEMS & TEST • IPP TURBOMACHINE NOSE RADOME
AND TRESSLE J520 EXTERNAL • RUDDER ACTUATORS
FLUID SYSTEMS FINISHES J753
ASSEMBLY BOOM • H/T ACTUATORS
STRUCTURAL VERTICAL TAIL
(CTOL, CV) VERTICAL TAIL • FIRE EXTINGUISHERS
MATE, INSTALL & RUDDER TIPS EJECTION
J851 ASSEMBLY COMPLETE • FLAPERON E/Us
SEAT Lockheed Martin
CROSS SHIP
SYSTEMS & J751 RUDDER, LEADING EDGES, BUILD-UP
ELECTRICAL RUDDERS SEAL INSTALLATION & Northrop Grumman
TEST EXTERNAL FINISHES
J510 J850
AFT FUSELAGE SUBSYSTEMS
HORIZONTAL TAIL MATE / TAIL
BAE Systems
LOOSE SHIP
J752 ASSEMBLY COMPLETE INSTALLATION
COMPONENTS
LEADING CONTROL J852 Fokker
SUB-ASSEMBLIES EDGES SURFACES HORIZONTAL TAIL
& EDGES EDGES INSTALLATION &
J611 EXTERNAL FINISHES
VERTICAL TAIL
J830
LOOSE SHIP
• STARTER / GENERATOR FINAL
COMPONENTS J742
• MAIN HYDRAULIC PUMPS ASSEMBLY
J620 J612 TRAILING EDGES
• SKATE ASSEMBLY & SYSTEMS TEST
VERTICAL TAILS PREP FOR
SUB-ASSEMBLIES • SIDE LINK
ASSEMBLE, SHIM SHIPMENT &
• LUBE OIL PUMP (CTOL/CV)
& DRILL SUB- SHIP J741 • THRUST PINS
STRUCTURE J621 LEADING EDGES J831
J619 • PTMS VALVES
HORIZONTAL TAIL
MILL & DRILL J630 • MAIN FUEL LINE ENGINE BUILD-UP
J613 LOOSE SHIP
INNER / HORIZONTAL • ENG BLEED DUCT
EXTERNAL COMPONENTS
OUTER TAILS • ESG OIL RESEVOIR
SURFACES FINISHES ASSEMBLE, • HYD HOSE ASSEMBLIES J825
J618
STRIP DOWN, (FOG) SHIM & DRILL Ground Ops
J616
DEBURR, NUT SKIN J629 SUB- (Fuel Op/Wt,
J622
PLATES & WET INSTALLATI MILL & DRILL UPPER STRUCTURE IPP Run, Eng
PREP FOR
ASSEMBLE ON / LOWER SURFACES Runs)
SHIPMENT &
(FOG) SHIP
J617
J623
SYSTEMS J628 EXTERNAL
INSTALLATION MILL & DRILL FINISHES J820
BUMP FINAL
STRUCTURE J624
EXTERNAL
(FOG) INSTALL
FINISHES
J627 UPPER SKIN,
STRIP DOWN, BUMP
DEBURR & STRUCTURE & J810
INSTALL NUT J625 J801 J805 FIELD
FAIRINGS
PLATES SYSTEMS FLIGHT LINE FINAL FINISHES OPERATIONS
J626
OPS AND RCS
7
INSTALLATIO CTOL
WET ASSEMBLE
N & TEST J800 (AIRWORTHINE TESTING
STRUCTURE &
AIRCRAFT COMPLETE SS)
07 JANUARY 2010 INSTALL LOWER
SKIN
8. 7-9 September 2010
Hilton Orlando – Orlando, Florida
Major Deliveries
NGC - Center FOKKER - Misc
Fuselage Doors
Lockheed Martin
BAE - Aft Fuselage, Palmdale -
Horizontal & Vertical Tails Control Surfaces
and Edges
8
10. 7-9 September 2010
Hilton Orlando – Orlando, Florida
F-35 IUID Selection Process Output
End Items Aircraft/SE/
AME/Trainers
Embedded DoD Air Vehicle Hardware
Serially Configuration Items
Managed Parts
Depot Level Repairable
Other End Item Embedded Items
10
11. 7-9 September 2010
Hilton Orlando – Orlando, Florida
Supplier Requirements
Three Major Supplier Actions:
• Develop Engineering (Unless Build-to-Package (BTP)
Supplier)
• Review and approval by Prime (LMA, BAE, NGC)
• Create UID Label
• Ensure HRI and MRI Compliance (MIL-STD-130)
• Supplier Responsible for Verification and Validation
• Submit Data for each Delivered Part
• First time submittals to F-35 Data Library
• Future submittals via LM UID Portal
11
12. 7-9 September 2010
Hilton Orlando – Orlando, Florida
F-35 UID Label Requirements
• F-35 Suppliers create labels in compliance with
MIL-STD-130
– Design Authority Suppliers can use any material and
marking method that meets the F-35 operational
environment. The supplier must certify to MIL-STD-130 for
verification requirements.
– BTP suppliers create labels in compliance with MIL-STD-
130, LMA-PN008 and released engineering.
• Approved materials are Photo-metal, Polyester and Tedlar
decals.
• LMA is currently testing DPM methods
• Text Element Identifier format (TEI)
12
14. 7-9 September 2010
Hilton Orlando – Orlando, Florida
Supplier Data Requirement
Suppliers are required to submit UID records using a Excel template for
each part shipped.
• The spreadsheet requires additional columns for Purchase Order and
Line Item numbers.
• When parts are received at LM Aero a query is made to I-GUIDES
that looks for records with the same PO/Line Item numbers as the
parts that were received.
• If three parts are received, but only two records reside in
I-GUIDES, the parts are held in receiving until the additional
records are added or corrected in I-GUIDES.
14
15. 7-9 September 2010
Hilton Orlando – Orlando, Florida
Supplier Portal
• The spreadsheets can be directly imported by suppliers using
Lockheed Martin’s Supplier UID Portal.
• Once a submittal is made an email response will include an Excel
file showing error or acceptance messages.
15
16. 7-9 September 2010
Hilton Orlando – Orlando, Florida
LM I-GUIDES
Integrated Global UID Enterprise Solution (I-GUIDES) is Lockheed
Martin’s UID database. Below a query can be made on Purchase
Order and Line Item numbers and all UID records received for a
particular PO can be reviewed.
16
17. 7-9 September 2010
Hilton Orlando – Orlando, Florida
I-GUIDES Query Result
Return query shows 11 records received for this PO/Line Item.
UID PO Number PO Line Item
D941172ZXX63042-00010041 623003 0003
D941172ZXX63042-00010042 623003 0003
D941172ZXX63042-00010043 623003 0003
D941172ZXX63042-00010044 623003 0003
D941172ZXX63042-00010045 623003 0003
D941172ZXX63042-00010046 623003 0003
D941172ZXX63042-00010047 623003 0003
D941172ZXX63042-00010048 623003 0003
D941172ZXX63042-00010049 623003 0003
D941172ZXX63042-00010050 623003 0003
D941172ZXX63042-00010051 623003 0003
11 records found displayed on 1 page
17
18. 7-9 September 2010
Hilton Orlando – Orlando, Florida
Data Flow
DB Queries
Parts are UID Marked Parts Received at LM Receiving/ I-GUIDES for UID
at Source Aero Fort Worth Purchasing Record for Part I-GUIDES
DB Received
Record Not Record
Grief Status until Data Found Found
Added or Corrected in
I-GUIDES
Parts Issued to
Aircraft for
Installation
UID Data Available for:
Automated
• Field R&R
Logistics
• Maintenance Actions
Integrated
Engineering •Supply Chain Transactions
System
Data Base
Part
Scanned into Parent & Children
Shop Floor UIIs Submitted to
Manager DoD Registry after Registry
A/C Delivery
18
19. 7-9 September 2010
Hilton Orlando – Orlando, Florida
Scanning of UID on Production Line
UID Parts are scanned prior to installation. Once a part is scanned,
the Shop Floor Manager (SFM) program queries I-GUIDES for a
matching data record.
Mechanic opens the
Actuator installation
operation in SFM
19
20. 7-9 September 2010
Hilton Orlando – Orlando, Florida
Mechanic selects the Scan UID icon in the operation step of
SFM to begin IUID collection
20
21. 7-9 September 2010
Hilton Orlando – Orlando, Florida
1. The IUID
mark on the
part’s label. 2. The mechanic
searches for the IUID
mark following SFM
instructions to
observe and record
3. Mechanic IUID.
scans the IUID
with hand held
reader.
21
22. 7-9 September 2010
Hilton Orlando – Orlando, Florida
After the scan, the
mechanic connects the
reader to the computer
to transfer the scan
information to SFM.
SFM is linked to I-GUIDES
and the pop-up in this
picture shows the data
has been retrieved
successfully. The
mechanic checks the
serial number, cage code
and part number.
22
23. 7-9 September 2010
Hilton Orlando – Orlando, Florida
The Actuator CAGE, Original Part Number and Serial
Number = UII D821062ARV01110-00080013 are collected and
linked to the parent aircraft UII.
23
24. 7-9 September 2010
Hilton Orlando – Orlando, Florida
The Actuator
installed on the
aircraft with the UID
mark visible.
24
25. 7-9 September 2010
Hilton Orlando – Orlando, Florida
UID Shop Floor Callboard Action
• If the record is not found in I-GUIDES, the technician must manually
enter the required data fields and a Callboard action is logged.
• A F-35 UID integrator must resolve the issue to close out the call
board request.
25
26. 7-9 September 2010
Hilton Orlando – Orlando, Florida
Summary
• Clear requirements and upfront coordination with
suppliers are essential in receiving correct UID
marks and associated data submittals.
• Check points within the process help ensure
correct marks and data are available when parts
are scanned prior to installation.
• UID data is linked across multiple LMA databases
(I-GUIDES, Automated Logistics Integrated
System, SAP) and provides asset management
throughout production and sustainment
processes.
26
