7-9 September 2010Hilton Orlando – Orlando, Florida
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F-35 IUID Program Implementation
Bill StillLockheed Martin Aeronautics
© 2010 Lockheed Martin Corporation
7-9 September 2010Hilton Orlando – Orlando, Florida
CTOL, STOVL and CVTest Flights
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F-35A CTOLF-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.
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F-35B STOVLF-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.
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F-35C CVF-35C Carrier Variant (CV) will replace U.S. Navy F/A-18s.
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PartnersLockheed 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.
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CTOL Manufacturing Sequence Flow
J834CANOPYBUILD-UP
J714FIXED TIP
J712FLAPERONS
J711LEADING
EDGE FLAPS
(CTOL/CV)
HORIZONTAL TAIL ASSEMBLY COMPLETE
VERTICAL TAIL ASSEMBLY COMPLETE
J852HORIZONTAL TAIL
EDGES INSTALLATION &EXTERNAL FINISHES
CM DOORS
MLG CLOSE-OUT
PANELS
• MLG CHINES • FUSELAGE FAIRINGS
GUN
NOSE RADOME
EJECTION SEAT
BUILD-UP
(CTOL/CV)
J831ENGINE BUILD-UP
• ADVANCED ESA RADAR• EOTS
• STARTER / GENERATOR• MAIN HYDRAULIC PUMPS• SKATE ASSEMBLY• SIDE LINK• LUBE OIL PUMP• THRUST PINS• PTMS VALVES• MAIN FUEL LINE• ENG BLEED DUCT• ESG OIL RESEVOIR• HYD HOSE ASSEMBLIES
J850SUBSYSTEMS MATE / TAIL
INSTALLATION
WEAPONS BAY DOORS
MAIN LANDING GEAR DOORS ARRESTING GEAR
DOORS
J860FUSELAGE
STRUCTUREMATE
J862AFT FUSELAGEFINAL FINISHES
MAIN LANDING GEAR
CTOLJ800
AIRCRAFT COMPLETE
NOSE LANDING GEAR
ARRESTING GEAR
J825Ground Ops (Fuel Op/Wt, IPP Run, Eng
Runs)
J820FINAL
EXTERNALFINISHES
J830FINAL
ASSEMBLY& SYSTEMS TEST
ENGINE NACELL
ESKINSLOWER WING
SKINS
J851RUDDER, LEADING EDGES,
SEAL INSTALLATION &EXTERNAL FINISHES
J611VERTICAL TAILLOOSE SHIP
COMPONENTS
Lockheed Martin
Northrop Grumman
BAE Systems
Fokker
J510AFT FUSELAGE
LOOSE SHIP COMPONENTS
SUB-ASSEMBLIES
J620VERTICAL TAILS ASSEMBLE, SHIM
& DRILL SUB-STRUCTURE
J616SKIN
INSTALLATION
J630HORIZONTAL
TAILS ASSEMBLE,
SHIM & DRILL SUB-
STRUCTURE
J628MILL & DRILL
BUMP STRUCTURE
(FOG)
J621HORIZONTAL TAIL
LOOSE SHIPCOMPONENTS
J751RUDDERS
J752LEADING
EDGES
J753VERTICAL TAIL& RUDDER TIPS
J742TRAILING EDGES
J741LEADING EDGES
J629MILL & DRILL UPPER / LOWER SURFACES
(FOG)
J531LH BOOM INSTALL
SYSTEMS & TEST FLUID SYSTEMS
J561L/H BOOM
UPPER / LOWER SURFACES MILL
/ DRILL(FOG)
J571L/H BOOM ASSEMBLE,
SHIM & DRILL SUBSTRUCTUR
E,MC EEE JOINTS
J560R/H BOOM
UPPER / LOWER SURFACES MILL /
DRILL(FOG)
J570R/H BOOM
ASSEMBLE, SHIM & DRILL
SUBSTRUCTURE,MC EEE JOINTS
J550R/H BOOM
DEBURR, WET ASSEMBLE
J500AFT FUSELAGEPREP FOR SHIP
AND SHIP
J540R/H BOOMCOMPLETE UPPER SKIN INSTALL &
PAINT INTERNAL BAYS J551
L/H BOOMDEBURR, WET
ASSEMBLE
J530RH BOOMINSTALL
SYSTEMS & TEST FLUID SYSTEMS J541
L/H BOOM COMPLETE UPPER SKIN INSTALL &
PAINT INTERNAL
BAYS J515EXTERNAL FINISHES
J617SYSTEMS
INSTALLATION
J618STRIP DOWN, DEBURR, NUT
PLATES & WET ASSEMBLE
J619MILL & DRILL
INNER / OUTER
SURFACES(FOG)
J613EXTERNAL FINISHES
J612PREP FOR
SHIPMENT & SHIP
SUB-ASSEMBLIES
J627STRIP DOWN,
DEBURR & INSTALL NUT
PLATES
J624INSTALL
UPPER SKIN, BUMP
STRUCTURE & FAIRINGS
J623EXTERNAL FINISHES
J626WET ASSEMBLE STRUCTURE &
INSTALL LOWER SKIN
J622PREP FOR
SHIPMENT & SHIP
J625SYSTEMS
INSTALLATION & TEST
J511TAIL HOOK
AND TRESSLE ASSEMBLY(CTOL, CV)
J520BOOM
STRUCTURAL MATE, INSTALL
CROSS SHIP SYSTEMS & ELECTRICAL
TEST
CONTROL SURFACES
& EDGES
J320SYSTEMS INSTALLATION
& TEST
J350FS 270-425 UPPER MATE
ASSEMBLYAFT DUCT & TANK
J356FS 365-425 AFT DUCT
STRUCTUR
UPPER SKIN PANELS & ACCESS PANELS
J355CENTER TANK STRUCTURE
ASSEMBL(No SWBS Number for AF-14 and on per CR-
013699)
J353CENTER FUSELAGEL/H DUCT ASSEMBLY
INLET LIPS
J300CENTER FUSELAGE
ASSEMBLY COMPLETE& SHIP
J310DOOR CLOSE-OUT
& FINAL INSPECT
J330STRUCTURE COMPLETE,
SKINS & DOORSINSTALLATION
J345AUTODRILL, NUTPLATE
INSTALLATION DOOR RIGGING, SEAL
& TEST
J351FS 270-365 CENTER TANK
STRUCTURE, BRACKETS & SYSTE
J354CENTER FUSELAGE
R/H DUCT ASSEMBLY
J341, J342, J343
FS 365-425 LOWER CTR FUS SUBASSEMBLIES
(No SWBS Numbers for AF-8 and on per CR-
013699)GUN VENT
DOOR
CENTER FUSELAGE
LOOSE COMPONENT
S
IFRR DOORS
• ARRESTING GEAR ACTUATOR• AVIONICS RACKS• HEAT EXCHANGERS• IN FLIGHT REFUEL RECEPTICLE)• IN FLIGHT REFUEL RECEPTICLE DOOR
ACTUATORS• OBIGGS• PAO PUMP RESERVOIR• WEAPON BAY DOOR CONTROLLERS• WEAPON BAY DOOR POWER DRIVE UNIT• EODAS
• DMC COMPUTER• VMC COMPUTER• 28V CONVERTERS• 28V & 270V BATTERIES• AILERON ACTUATORS• FLAPERON ACTUATORS• IPP TURBOMACHINE• RUDDER ACTUATORS• H/T ACTUATORS• FIRE EXTINGUISHERS• FLAPERON E/Us
ACCESS PANELS& DOORS
COCKPIT FLOORS
J293FORWARD EQUIPMENT
BAY ASSEMBLY
J250BAY PAINT
J270TEMPORARY SKIN INSTALLATION &
AUTODRILL
J291SIDE PANEL
LH ASSEMBLY
J292SIDE PANEL
RH ASSEMBLYJ280 MILL
UNDERSTRUCTURE
J210FINAL FINISHES
J200FORWARD FUSELAGEASSEMBLY COMPLETE
J294AFT EQUIPMENTBAY ASSEMBLY
J230SKIN & SYSTEMSINSTALLATION
FWD FUSELAGE
LOOSE COMPONENT
S
J220FINAL SYSTEMS AND FUNCTIONAL TEST
J290COMPONENT MATE
& MOLDABLE SHIM APPLICATION
J260FLOOR & CONSOLE
INSTALLATION
J240TUBE & WIRE
HARNESS INSTL
FORWARD FUSELAGE
NLG DOORS
UPPER WING SKINS
J450
DRILL SPLICE AREA; BORE MLG & DRAG LINK; FINAL PREP UPPER WING
SKINS
J440
DEBURR STRUCTURE, INSTALL
SPLICE AREA NUT PLATES; FUEL SEAL;
J420
Final Install Fixed Upper Skins & Fuel Covers; Install Fixed Wing Tip Edges & Fairings;
Wing Exterior; Combined Fuel Tank Leak Test; LE Actuators
07 JANUARY 2010
J461 (LH) / J462 (RH)
OUTER WING SUBSTRUCTURE BUILD-UP; AUTODRILL UPPER AND
LOWER SKINS; INSTL WTBF DETAILS; FINAL INSTL LOWER
WING SKINS;INSTL NUTPLATES; FUEL SEAL; FINAL INSTL & TEST
CONDUITS, BAY PAINTJ470
INNER WING MODULE 1 & 2 ASSY; NACELLE
SPLICE INSTL; DRILL & INSTL UPPER & LOWER ACCESS STRAPS AND FIXED SKIN; DRILL I&R
HOLE PATTERNS; INSTL NUTPLATES;
FUEL SEAL; BAY PAINT
J460
OUTER WING TO INNER WING MATE; SUB-
FRAME INSTL; REMAINING WTBF
DETAILS INSTL; PARTIAL SYS INSTL
J430
SUBSYSTEMS & EQUIPMENT INSTL COMPLETION &
FUNCTIONAL TEST
J480
INNER WING MODULE 1 FS425-472
SUBSTRUCTURE BUILD-UP; Auto-drill;
NACELLE SKIN INSTL
J475
INNER WING MODULE 2 FS496-
556 SUBSTRUCTURE
BUILD-UP; Auto-drill; NACELLE SKIN
INSTL
Upper/Lower Straps
Wing to Body
Fairings
J810FIELD
OPERATIONSJ805
FINAL FINISHES AND RCS TESTING
J801FLIGHT LINE
OPS (AIRWORTHINE
SS)
EODAS
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Major DeliveriesNGC - Center
Fuselage
BAE - Aft Fuselage, Horizontal & Vertical Tails
FOKKER - Misc Doors
Lockheed Martin Palmdale -
Control Surfaces and Edges
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OSD IUID Selection Guide
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F-35 IUID Selection Process Output
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End Items Aircraft/SE/AME/Trainers
Air Vehicle HardwareConfiguration Items
Depot Level Repairable
Embedded DoD Serially
Managed Parts
Other End Item Embedded Items
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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
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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
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F-35 Aircraft Nameplate
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7-9 September 2010Hilton Orlando – Orlando, Florida
Supplier Data RequirementSuppliers 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.
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Supplier Portal
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• 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.
7-9 September 2010Hilton Orlando – Orlando, Florida
LM I-GUIDESIntegrated 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.
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I-GUIDES Query Result
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Return query shows 11 records received for this PO/Line Item.
UID PO Number PO Line ItemD941172ZXX63042-00010041 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 000311 records found displayed on 1 page
7-9 September 2010Hilton Orlando – Orlando, Florida
Data Flow
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Parts Received at LM Aero Fort Worth
Record Not Found
Record Found
Automated Logistics Integrated
System
UID Data Available for:• Field R&R • Maintenance Actions•Supply Chain Transactions
Receiving/ Purchasing
DBI-GUIDES
DB Queries I-GUIDES for UID Record for Part
Received
Parts Issued to Aircraft for Installation
Parent & Children UIIs Submitted to
DoD Registry after A/C Delivery
Registry
Grief Status until Data Added or Corrected in
I-GUIDES
Parts are UID Marked at Source
Engineering Data Base
Part Scanned into Shop Floor
Manager
7-9 September 2010Hilton Orlando – Orlando, Florida
Scanning of UID on Production LineUID 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.
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Mechanic opens the Actuator installation
operation in SFM
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Mechanic selects the Scan UID icon in the operation step of SFM to begin IUID collection
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1. The IUID mark on the part’s label.
3. Mechanic scans the IUID with hand held reader.
2. The mechanic searches for the IUID mark following SFM instructions to observe and record IUID.
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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.
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The Actuator CAGE, Original Part Number and Serial Number = UII D821062ARV01110-00080013 are collected and
linked to the parent aircraft UII.
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The Actuator installed on the aircraft with the UID mark visible.
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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.
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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.
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QUESTIONS?
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