F-35 Cancelled, then what ?
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Original quote by Lonewolf_50:
The decision was made at high levels in government, secretarial level, to put all eggs in one basket. Over a decade ago.
The decision was made at high levels in government, secretarial level, to put all eggs in one basket. Over a decade ago.
Original quote by ORAC:
Hmmm. Remind me, just about when was the F136 engine cancelled?
Hmmm. Remind me, just about when was the F136 engine cancelled?
December 2, 2011
Joint Statement From GE and Rolls-Royce
The GE Rolls-Royce Fighter Engine Team (FET) has reached the decision to discontinue self-funded development of the F136 engine for the Joint Strike Fighter (JSF) beyond 2011.
The decision, reached jointly by GE and Rolls-Royce leadership, recognizes the continued uncertainty in the development and production schedules for the JSF Program.
"GE and Rolls-Royce are proud of our technology advancements and accomplishments on the F136," said Dan McCormick, President of the FET. "However, difficult circumstances are converging that impact the potential benefit of a self-funded development effort."
With the F136 engine development almost 80 percent complete, the Department of Defense terminated the program in April of this year. Following termination, the GE Rolls-Royce FET had offered to self-fund F136 development through fiscal year 2012, but will now end its development work. The FET will continue to fulfill its termination responsibilities with the federal government.
For 15 years, the FET has developed a competitive fighter engine for JSF with the world's most advanced propulsion technologies, including numerous patented technologies from both companies.
Before the program was terminated, six F136 development engines had accumulated more than 1,200 hours of testing since early 2009. The FET consistently delivered on cost and on schedule, and was rewarded with high marks by the Department of Defense in a successful joint venture between GE and Rolls-Royce.
Throughout the F136 program, GE and Rolls-Royce have been leading advocates of defense acquisition reform - offering unique and aggressive fixed-price proposals for F136 production engines for the JSF program.
"GE and Rolls-Royce are deeply grateful to our many Congressional supporters on both sides of the aisle over these many years as well as the military experts who have supported competing engines for JSF," said McCormick. "We do not waver in our belief that competition is central to meaningful defense acquisition reform."
Source: Rolls-Royce, GE
Joint Statement From GE and Rolls-Royce
The GE Rolls-Royce Fighter Engine Team (FET) has reached the decision to discontinue self-funded development of the F136 engine for the Joint Strike Fighter (JSF) beyond 2011.
The decision, reached jointly by GE and Rolls-Royce leadership, recognizes the continued uncertainty in the development and production schedules for the JSF Program.
"GE and Rolls-Royce are proud of our technology advancements and accomplishments on the F136," said Dan McCormick, President of the FET. "However, difficult circumstances are converging that impact the potential benefit of a self-funded development effort."
With the F136 engine development almost 80 percent complete, the Department of Defense terminated the program in April of this year. Following termination, the GE Rolls-Royce FET had offered to self-fund F136 development through fiscal year 2012, but will now end its development work. The FET will continue to fulfill its termination responsibilities with the federal government.
For 15 years, the FET has developed a competitive fighter engine for JSF with the world's most advanced propulsion technologies, including numerous patented technologies from both companies.
Before the program was terminated, six F136 development engines had accumulated more than 1,200 hours of testing since early 2009. The FET consistently delivered on cost and on schedule, and was rewarded with high marks by the Department of Defense in a successful joint venture between GE and Rolls-Royce.
Throughout the F136 program, GE and Rolls-Royce have been leading advocates of defense acquisition reform - offering unique and aggressive fixed-price proposals for F136 production engines for the JSF program.
"GE and Rolls-Royce are deeply grateful to our many Congressional supporters on both sides of the aisle over these many years as well as the military experts who have supported competing engines for JSF," said McCormick. "We do not waver in our belief that competition is central to meaningful defense acquisition reform."
Source: Rolls-Royce, GE
Original quote by Lonewolf_50:
Other nations may have more flex in making a choice to opt out.
Other nations may have more flex in making a choice to opt out.
Original quote by Hempy:
Strangely enough, Spaz, Engines, JSFan et al have been noticeably quiet of late
Strangely enough, Spaz, Engines, JSFan et al have been noticeably quiet of late
Much of the GE owned technology developed for the F136 will be apparent in the new commercial engines, soon to become a reality…
The decision was made decade ago by the UTC/PWA lobby in Washington to eliminate the competition as the Pratt engine was far superior compared to the GE/Rolls Royce engine, and the Connecticut Congressional delegation agreed, they didn't want to lose another engine war. Actual funding continued through part of 2011 and then GE/RR self funded to the end of 2011. Somewhere there are six engines encased in bubble wrap, preserved as a reminder to dimwits in Washington that they are still dimwits.
Much of the GE owned technology developed for the F136 will be apparent in the new commercial engines, soon to become a reality
Ecce Homo! Loquitur...
I was alluding to the previous diagram and the dramatic decline in engine life.
If one was cynical one could suppose that the manufacturer had been spending waaaay over revealed costs to produce early engines above spec to match/best the opposition and that; once it was cancelled; they went back to contract spec and time.
Gee, you want it better? Meet my lawyers and engineers.........
If one was cynical one could suppose that the manufacturer had been spending waaaay over revealed costs to produce early engines above spec to match/best the opposition and that; once it was cancelled; they went back to contract spec and time.
Gee, you want it better? Meet my lawyers and engineers.........
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Was it the same time as the manufacturer promised "The Turkey" would out perform the current service aircraft 
Anyone have details on just what are the procedures and processes for F35B ECU replacement?
[I could do with a laugh]
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Original quote by Lonewolf_50:
Is that the same brand of "soon" as the "F-35 will IOC soon" or is it another brand?
Is that the same brand of "soon" as the "F-35 will IOC soon" or is it another brand?
The CFM LEAP family represents the engines of choice for the next-generation single-aisle aircraft. The LEAP-1A is an option on the Airbus A320neo; the LEAP-1B is the exclusive power plant for the Boeing 737 MAX; and the LEAP-1C is the sole Western powerplant for the COMAC C919. Two engine families have contributed significantly to the design of the LEAP engine, the CFM56 and the GE90/GEnx series of engines. The GE90/GEnx contributed the high-efficiency core architecture to minimize fuel consumption, while the CFM56 legacy drove reliability and maintenance cost design practices.
Airbus just rolled out the first A320neo LEAP powered aircraft and it will start ground testing and flight certification testing this year. I believe over 5,000 LEAP engines have been sold at this point in time. Revenue service will start in 2016.
FYI, the CFM56 core came from the F101 engine designed for the B-1A/B bomber. There have been over 25,000 CFM56 engines produced for Boeing and Airbus. The GE90/GEnx core evolved out of the GE engine offered for what is now the F-22 fighter.
I suspect the promised dates will be met as advertised along with up to a 15% improvement in fuel efficiency verses the best of the current CFM56 engines, further reduced maintenance costs, and a 1000 pound weight reduction contribution for each A320neo aircraft verses current A320 aircraft.
P&W fights US government criticisms of F-35 engine reliability - 4/30/2015 - Flight Global
Interesting to see the VTOL engine is almost twice as reliable as the CTOL engine. Counter intuitive. I wonder why that is.
The drop off after F136 cancellation is interesting. I assume there is more to this though, were there also cost/weight/production changes that explain the drop off? I suspect "Engines" would know.
Interesting to see the VTOL engine is almost twice as reliable as the CTOL engine. Counter intuitive. I wonder why that is.
The drop off after F136 cancellation is interesting. I assume there is more to this though, were there also cost/weight/production changes that explain the drop off? I suspect "Engines" would know.
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From Flightglobal
“The engine is reliable, and we’ll continue trying to make it more reliable,” Bennett Croswell, president of P&W’s military engines business, told reporters on 27 April. Croswell acknowledges the accuracy of the GAO’s numbers, but says that report does not reflect the overall picture of the F135’s reliability record.
“The engine is reliable, and we’ll continue trying to make it more reliable,” Bennett Croswell, president of P&W’s military engines business, told reporters on 27 April. Croswell acknowledges the accuracy of the GAO’s numbers, but says that report does not reflect the overall picture of the F135’s reliability record.
The other business history lesson is that you never publicly criticize your customer whether you are President or not, especially when you say your deficient management systems don't represent the end product.
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P&W fights US government criticisms of F-35 engine reliability - 4/30/2015 - Flight Global
Interesting to see the VTOL engine is almost twice as reliable as the CTOL engine. Counter intuitive. I wonder why that is.
Interesting to see the VTOL engine is almost twice as reliable as the CTOL engine. Counter intuitive. I wonder why that is.
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That is exactly what P&W said about the PW F100-PW-200 engine that powered the F-16A/B. What happened subsequently is history. The one thing about history is we learn we don't learn. Mr. Croswell apparently never studied the history of the F-16 Fighter and its initial single sourced engine.
The other business history lesson is that you never publicly criticize your customer whether you are President or not, especially when you say your deficient management systems don't represent the end product.
The other business history lesson is that you never publicly criticize your customer whether you are President or not, especially when you say your deficient management systems don't represent the end product.
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Original quote by glad rag:
Anyone have details on just what are the procedures and processes for F35B ECU replacement?
Anyone have details on just what are the procedures and processes for F35B ECU replacement?
TI Number Mod CR Title
TI-0000-1089 CR-021694 LRIP 3 Aux Air Inlet (AAI) Door Install
TI-0000-1324 CR-022656 Structural Cracking of Aft MLG Door Drive Link U-Joint
TI-0000-0116 CR-011738B Full Qualified Clutch Cooling Fan
TI-0000-0367 CR-014114C Engine Trailer Adapter Kit - FS556 Interface, J27006/J27007
TI-0000-0121 CR-014289B Lift Fan Exhaust/Inboard Weapon Bay Door Interference
TI-0000-0396 CR-014289C WBDD Limit Life, ECU
TI-0000-0655 CR-014819D EO DAS Center Fuselage Vibration Testing
TI-0000-0373 CR-015026B Aux Air Inlet Lock Actuation Mechanism
TI-0000-0423 CR-016270C Bleed Air System Ducting Design
TI-0000-0099 CR-017502 J75503 Wrap Around Adapter Set
TI-0000-0683 CR-017534&B Rev-HT Bearing Issues
TI-0000-0463 CR-017913B Support-Fairing, Mid, LH/RH
TI-0000-0058 CR-018274 Back-Up Radio Tray Clearance
TI-0000-0968 CR-018524 Material Removal Allowance for IPP Blocker and Screen
TI-0000-0027 CR-018524A IPP Exhaust (STOVL)
TI-0000-0138 CR-018564B Wingtip Light Improvement For FAA Compliance
TI-0000-0825 CR-022768D LEF Improvements
TI-0000-0031 CR-018835 Nose Wheel Steering (NWS) Motor
TI-0000-0015 CR-018836 Stress Failure of Hydraulic Tube Support Bracket
TI-0000-0063 CR-018838A Bootstrap Accumulator Redesign
TI-0000-0045 CR-019003 CTOL/STOVL MLG SDD & LRIP Part Number Rolls
TI-0000-0056 CR-019004B IPP Controller Part Number Roll
TI-0000-0057 CR-019005 STOVL GO3 Control Valve Part Number Roll
TI-0000-0117 CR-019107 CTOL Trestle Inst Cotter Pin
TI-0000-0165 CR-019135B R3 Float Valve with Mechanical Thread Locking
TI-0000-0231 CR-019340B PTMS EHA Cooling Orifices - CTOL & STOVL
TI-0000-0101 CR-023102A Lift Fan Inlet Door Full Qualification Part Number Roll
TI-0000-0245 CR-019469C Antenna Switch Unit
TI-0000-0264 CR-019516A PTMS Controller
TI-0000-0124 CR-019533 Controller, Motor Pump Qual Failure (GMMP)
TI-0000-0561 CR-019683E STOVL FS 496 Bulkhead Trunnion
TI-0000-0280 CR-019841 Cockpit Panels Pushbutton Switch Simultaneity
TI-0000-0398 CR-019930C Arresting Hook Aft Door Spring Damper Part Number Roll
TI-0000-0375 CR-019979 STOVL IRCM Doors Bushing to Lug Interference
TI-0000-0208 CR-020003A CTOL Arresting Gear Push Rods
TI-0000-0424 CR-020066A Firewall Shutoff Valve Part Number Roll
TI-0000-0477 CR-020097A CTOL EHAS Panels
TI-0000-0875 CR-020189 CV Main Landing Gear Retract Actuator
TI-0000-0130 CR-020289 Emergency Control Valve Qual Failure
TI-0000-0575 CR-020289A ULF & 3BSD Emergency Control Valve
TI-0000-0608 CR-020396D Fwd Upper Engine Mount (CTOL)
TI-0000-0456 CR-020396D Bulkhead - FS 450
TI-0000-0457 CR-020396D Bulkhead - FS 472
TI-0000-0458 CR-020396D Bulkhead - FS 518 (Upper)
TI-0000-0460 CR-020396D Bulkhead - FS 556
TI-0000-0432 CR-020397A Short Life - CTOL Wing Forward Root Rib
TI-0000-0602 CR-020398A Brake Control Unit (BCU)
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TI-0000-0412 CR-020680B Wing Lighting Controller Salt Fog Failure
TI-0000-0331 CR-020725 WBDDS RGAs Limited Life - Change Request Approval
TI-0000-0654 CR-020726A IDMS Connector Ref Des Swap
TI-0000-0673 CR-020743B Ordnance Quick Latch System (OQLS) Clip Lock
TI-0000-0137 CR-020793 Pump, Motor GND Maint Qual Failure
TI-0000-0132 CR-020907B Valve, Mechanical Sequence - T Qual Failure
TI-0000-0811 CR-021167A 2WSH54239: CV Rear Spar
TI-0000-0810 CR-021168 2WSH64241: CV Frame
TI-0000-0817 CR-021170 2WSH44162: CV RH Tail Hook Longeron
TI-0000-0631 CR-021180 Countermeasures Doors & NNMSB/WSESRB Concerns
TI-0000-0263 CR-021181 Power Panel 1, 2, 3
TI-0000-0544 CR-021194 Limited Life STOVL Mid Fairing Longeron
TI-0000-0558 CR-021194 Short Life Parts: Keel Beam RH
TI-0000-0559 CR-021194 Short Life Parts: NLG Drag Brace Ftg
TI-0000-0566 CR-021194 Short Life Parts: Support, Otbd, FS 502.65 LH/RH
TI-0000-0617 CR-021194 Limited Life STOVL STA 3/9 Aft Rib
TI-0000-0545 CR-021217 Limited Life STOVL Nacelle Vent Inlet
TI-0000-0564 CR-021217 STOVL Forward Root Rib (L6/U6)
TI-0000-0808 CR-021259 Weapons Bay Door Uplock Sealing
TI-0000-0098 CR-022768D CTOL Nose Landing Gear
TI-0000-0910 CR-021395A PCD EU Cooling Rework
TI-0000-0607 CR-021434 Limited Life CTOL STA 3/9 Aft Rib
TI-0000-0135 CR-021459B Engine Driven Pump Life Limit
TI-0000-0895 CR-021557A Arm Disable Current Leakage Path Correction
TI-0000-0848 CR-021621 2CSH20930 Splice, Fuel Floor/Root Rib, FS 402, RHS/LHS
TI-0000-0377 CR-021694 Aux Air Inlet Door Redesign
TI-0000-0845 CR-021891 CV VT Aft Moment Fitting Life Limited Structures Part
TI-0000-0626 CR-021905A SMSFRIU SDD/LRIP Arm Disable Input
TI-0000-0998 CR-021915B CTOL and CV Refuel System Mod
TI-0000-0897 CR-022058 Roll Control Nozzle Door Redesign
TI-0000-0495 CR-022105F OBIGGS & Pressure/Vent Changes for Lightning Protection
TI-0000-0133 CR-022196A Filter Module, Pressure Qual Failure
TI-0000-1011 CR-022226A L-Band Pre-Selector (LBPS) Calibration for Mode 5
TI-0000-0802 CR-022695 CTOL Main Landing Gear
TI-0000-0703 CR-022515A Roll Post Door Actuator Life Limitation
TI-0000-1101 CR-022647A GMMP Controller EEE outage
TI-0000-1092 CR-022666 Landing Taxi Light Redesign
TI-0000-0119 CR-022736 MWARS Replacement
TI-0000-0866 TBD Production Ejection Seat (-0023)
TI-0000-1099 CR-022841B ATQA Mounting Bolt Interface
TI-0000-0064 CR-022872 Counter Measures Door Control Valve on AF:6
TI-0000-0158 CR-022877 WBDD Flexible Cable Re-design
TI-0000-0191 CR-024623 270V BCCU
TI-0000-0574 CR-023121B/D Electronics Units Modifications
TI-0000-1485 CR-023282CA F1 Feed Tank Gasket
TI-0000-1540 CR-023332A CV Rudder Hinge 2
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TI-0000-1652 CR-023599 Rudder Slider Hinge Wear
TI-0000-1654 CR-023712 CV Right Hand (RH) Center Fuselage Avionics Bay Floor
TI-0000-2548 CR-023712 CV Center Fuselage FS 402 Outboard Joint Limited Life
TI-0000-2551 CR-024031 L-Band Power Amplifier (LBPA) Update for LINK-16
TI-0000-1709 CR-024114 Carrier Variant Marker Beacon Antenna
TI-0000-2513 CR-024153 CV IPP Shear Web Limited Life
TI-0000-1207 CR-024162 Vehicle Management Computer (VMC) Electrical Connection Issue
TI-0000-0441 CR-20773A CTOL FS 594 Centre Arch Low Life
TI-0000-1549 CR-023540A Firmware Update for AMS Cartridge Reset SPAR
TI-0000-0405 CR-23769 EDU Random Vibration Failures
TI-0000-0702 CR-24090 CV Fwd Arresting Gear Door Actuator Life Limitation
TI-0000-2554 CR-24872 J84001 Fiber Optic Inspection Set Extension Handle DR?s
TI-0000-0122 TBD 28V Battery and Charger Changes
TI-0000-0129 TBD MLG Control Valve Part Number Roll
TI-0000-0709 CR-022768D HT EHA Block Change for LRIP 4
TI-0000-0282 TBD Update to Audio Control Electronics (ACE) Unit
TI-0000-0469 TBD Composite BOS 2ZCH42000-0002 Assemblies
TI-0000-0583 TBD CTOL/STOVL Rudder EHA Design Change
TI-0000-0906 TBD NLG Lug Inspection and Support Stiffener
TI-0000-1097 CR-022972 Ball Joint Salt Fog Failure
TI-0000-0913 TBD LEFAS PDU Resolver and Rotor Shaft Seal Life
TI-0000-1113 CR-024000 AESG Power Connector Rating (Generator)
TI-0000-1256 TBD CV Nose Landing Gear Drag Brace Door Cracking
TI-0000-1396 TBD HTCA with End Gland Material Issue
TI-0000-0336 CR-024982 Panoramic Cockpit Display (PCD) Major Variances - DU
TI-0000-0343 CR-024982 Panoramic Cockpit Display (PCD) Major Variances - EU
TI-0000-0480 CR-025000 ICC Qual Issues
TI-0000-2784 TBD CNI 3A & 3B Integrated Backplane Assembly (IBA) Upgrades
TI-0000-0221 TBD DAS Refuel Lights Lenses
TI-0000-0406 CR-025271 Ordnance Hoist System (OHS) Hoist
TI-0000-1102 CR-022481B BH-1 Weapons Bay Doors
TI-0000-1472 TBD Gun Port Door Threads in Bearing Issue
TI-0000-0329 CR-021982 Refueling Bay and Nozzle Clash LRIP 1-3 Modification
TI-0000-0781 CR-023432 3BSM NBD - Assembly Changes
TI-0000-1446 TBD CV Fuel Dump
TI-0000-0908 CR-023802 STOVL Fuel Dump (CCDD LRIP2-051)
TI-0000-1000 CR-022481 Inboard Weapon Bay Door Flipper Door Design Change
TI-0000-1060 CR-022121 Final Finishes
TI-0000-1078 CR-025006 AF1 Nacelle Insulation
TI-0000-0180 TBD CTOL Fuel Floor Tooling Holes - Bay 207 to Gun Bay
TI-0000-0787 CR-024068 HMDS Path Forward
TI-0000-1048 CR-023982 Panoramic Cockpit Display-Electronic Unit (PCD-EU)
TI-0000-1062 TBD CV Main Landing Gear
TI-0000-1063 TBD CV Nose Landing Gear
TI-0000-0284 TBD STOVL Canopy frame
TI-0000-0316 TBD CTOL FS 496 Bulkhead Trunnion
TI-0000-0321 TBD Lift Fan Exhaust Door Aft Uplock Hook Failure
TI-0000-0467 TBD Fuel Floor - FS496-556, LH
TI-0000-0468 TBD Fuel Floor - FS496-556, RH
TI-0000-0486 TBD Short Life - STOVL Inner Wing FS518 Lower Bulkhead
TI-0000-0543 TBD Path Forward for Outboard Rib at Station 2 and 10
TI-0000-0556 TBD STOVL Short Life Parts: Aft Mid Keel
TI-0000-0638 TBD STOVL BL 0.0 Web Fwd Upper Engine Mount Support
TI-0000-0813 TBD CV Life Limited Structures Part - LH/RH Pylon Sta 3 Aft Rib
TI-0000-0815 TBD 2WSH24212 CV FWD Upper Engine Mount
TI-0000-0816 TBD 2WSH34496 - CV FS 496 Blkhd Station 6
TI-0000-1440 TBD STOVL Thrust Mount Shear Webs
TI-0000-0723 TBD EOTS PBS Startup Timeline
TI-0000-0055 CR-019070 IPP Bay Vent Fan Electrical Bond
TI-0000-0281 CR-020226 Hoist Point Cover FIP Proposal
TI-0000-1023 CR-022936 Roll Nozzle and Duct Bay - BALD Sensors redesign
TI-0000-0193 CR-021921B EW Gain State Control Logic Error
TI-0000-1365 CR-022721A Cat Launch Shock Exceeds INS PBS
TI-0000-0448 TBD Add -0007 ASSCA/-0006 ATQA To Aircraft TVE
TI-0000-0842 TBD 2ESH10095 CV HT Rib 5 Life Limited Structures Part
TI-0000-0976 TBD BF6 and BF8 RCS ATP
TI-0000-0819 TBD Liquid Cooling System Cart - Facility AC Power Interface
TI-0000-1134 TBD Cabin Pressure Tester
TI-0000-1198 TBD HT Heating
TI-0000-0361 CR-023382 Vertical Tail 575 Fitting
TI-0000-0386 CR-025191 Fuel System Major Variance for LRIP 1-Signal Amplifier
TI-0000-0516 CR-022972 AAR Probe Weak Link Adaptor Re-design
TI-0000-0576 CR-020289A Refuel Probe/Tailhook Emergency Control Valve
TI-0000-0578 CR-020289A Aux Inlet Door Emergency Control Valve
TI-0000-1082 TBD Power Panel 1 & 2 Random Vibration Failures
TI-0000-1203 CR-021217 Life Limited 402 Frame
TI-0000-1289 CR022737 US16E Ejection Seat/MWARS Retrofit Configuration Proposal
TI-0000-1421 TBD STOVL Main Landing Gear
TI-0000-1422 CR-021388A STOVL Nose Landing Gear
TI-0000-1483 TBD Power Panel 3 Random Vibration Failures - Second Failure
TI-0000-1486 CR-023838 STOVL FS 503 Frame/IPP Shear Web Durability Test Failure
TI-0000-1515 CR-024000 ESG Service Life (Generator) -0003
TI-0000-1551 TBD 28V Battery Full Qualification
TI-0000-1589 CR-023300 Hydraulic System Single Point Failure
TI-0000-1786 CR-023729 FS-402 Frame (TIN-075)
TI-0000-1857 TBD 2GHH42033 Time Delay Valve - Fully Qualified Part
TI-0000-2467 CR-025204 CTOL FS 503 Frame Limited Life
TI-0000-2468 CR-025204 CTOL IPP Shear Web Limited Life Discovery
TI-0000-2641 CR-024341 STOVL - Short Shank Condition, Engine Access Panel
TI-0000-2674 CR-24794 Cracking of Bifurcation Seam Treatment
TI-0000-2892 CR-025079 BF5 IRCM Hinge to Drive Link Clash
TI-0000-1552 TBD 28V BCCU Lightning Compliance
TI-0000-2682 TBD AR Probe Light
TI-0000-0884 CR-024000 AESG - Material & Workmanship
TI-0000-1142 TBD Missionized Gun System Jumper Panel Hoses and Drain Seal
TI-0000-1796 CR-025271 Ordnance Hoist System (OHS) Motor
TI-0000-2506 TBD Gun Port Blast Mislocation
TI-0000-2546 TBD Weapon bay light departing aircraft during flight
TI-0000-2833 TBD Gun System Muzzle and Purge Door Time Out
TI-0000-0387 CR-016910 Fuel System Major Variance for LRIP 1 - Dive Rate Performance
TI-0000-1161 CR-22656 STOVL Aft MLG Door Cracking
TI-0000-1518 CR-024193 PAO Cooling Orifices In Center Fuselage Cold Liquid Loop
TI-0000-1783 TBD Canopy Boot Cracking
TI-0000-2633 CR-024265 Flaperon Blade Seal Buckling
TI-0000-2672 TBD Radome Shroud Gapping/Trimming
TI-0000-2909 CR-025167 IPP Bay High Flow Air Duct Separation
TI-0000-2931 TBD CV NLG Drag Brace Cylinder and Steering Motor
TI-0000-0236 CR-019412 FPS Fire and Bleed Leak Controller (FBLC) Redesign
TI-0000-0260 CR-016633C Canopy Actuation System
TI-0000-0738 CR-025142 Modified Fuel Dump Valve (T28a)
TI-0000-0772 TBD PTMS Turbomachine/ACCM Cable Interface Changes
TI-0000-0327 TBD STOVL High Sea State Fuel Stowage - Rev B to CR-016712A
TI-0000-0737 TBD IPP Purge Issue Due to Low Fuel Shutdown
TI-0000-1650 CR-022737 MWARS for Production Seat
TI-0000-1653 CR-23490 Ground Maintainance Valve Deletion to Prevent PAO in Cockpit
TI-0000-2416 TBD CV Drag Strut - Alt Gear Extension
TI-0000-2450 CR-023901 Bleed Air Sensor Fitting Galling
TI-0000-2635 TBD CV NLG Interference Problems - OBOGs routing
TI-0000-2725 CR-024162 Vehicle Management Computer (VMC)
TI-0000-2834 CR-024904 Boarding Ladder Cracks
TI-0000-2889 TBD WBDDS Supplier Disclosure on Lower Breakaway Torque
TI-0000-0771 CR-16464B Install Battery into CNI Rack 3A and 3B
TI-0000-0945 TBD CTOL Audio Control Electronics (ACE) In-Flight Refueling
TI-0000-1056 CR-016660C RADAR 1A & 1B Racks -0002 Cut-in
TI-0000-2818 CR-025046 EOTS LoS Pointing Angle
TI-0000-1093 CR-023616 CV Arresting Gear
TI-0000-0358 TBD Production Ejection Seat (-0021)
TI-0000-0514 TBD Lift Fan Inlet Maintenance Fix
TI-0000-0579 TBD Auto Pilot
TI-0000-1520 TBD CV Nose Landing Gear Aircraft Integration
TI-0000-1761 TBD HT EHA Solenoid Valve (SOV) Qual Test Failure
TI-9999-0655 TBD EO DAS Center Fuselage Vibration Testing
TI-0000-0730 TBD CV Rudder EHA
TI-0000-0833 CR-021053 Short Shank Condition on Engine Inspection Panels
TI-0000-1122 TBD LEFAS Foldbox Lug Cracking
TI-0000-1192 TBD CTOL Thrust Mount Shear Web
TI-0000-1494 TBD PTMS Turbomachine Configuration to Correct Qualification Failures
TI-0000-1499 TBD FS 472 Bulkhead Crack BH-1
TI-0000-1541 TBD CV HT LOWER SKIN BOLTS SD-2013-010
TI-0000-1649 TBD CV LEFAS Asymmetry Brake Lug Cracking
TI-0000-1655 CR-024025 STOVL RH and LH Rear Spar Lower Flange Fatigue Cracks
TI-0000-2423 TBD CV Lower FS 518 Design Change
TI-0000-2448 CR-023966A CV Thrust Mount Shear Web - Service Life
TI-0000-2670 TBD Durability Findings 2013 - Bulkhead FS 496
TI-0000-2813 TBD Durability Findings - FS 450, 472, 556, 518 Lower and IRCM Fitting
TI-0000-2814 TBD Durability Findings 2013 - FS 575 Center Arch Frame
TI-0000-1104 TBD CTOL Ventilation Leakage from Bay 207L
TI-0000-0992 CR-013553 Outboard Vertical Tail Seal Redesign
TI-0000-0904 CR-021759 Backup Radio Guide Pin Misalignment
TI-0000-1053 CR-022138 Fire Suppression Bottle Low Clearance
TI-0000-2675 TBD Roll Nozzle Bay - BALD Sensors - Supplier Disclosure
TI-0000-2921 CR-025116 Gun Vent Door Unpainted Brackets
TI-0000-0485 TBD J12003 Ejection Seat Stand Design Issues
TI-0000-0660 TBD J26007 LF Driveshaft
TI-0000-0799 TBD Canopy Sling
TI-0000-1337 TBD DR 1-2076141 Tool Boxes not within weight standards
TI-0000-1338 TBD DR 1-2565051 Tool Set Shipboard FOD Hazard
TI-0000-1629 TBD Deployable Mission Rehearsal Trainer #1
TI-0000-1658 TBD Changes to Support Turning on AMC’s Algorithms in ALIS
TI-0000-2440 TBD J26035 Adapter, Drive Shaft Compression Galling issue
TI-0000-2699 CR-023093C Fibre Channel Switch Design Issues -0005
TI-0000-2797 TBD SE Weight Label and Forklift Provisions
TI-0000-2954 TBD STOVL NLG EEE Failure
TI-0000-1408 TBD AEL, Aft Sector
TI-0000-2865 TBD TR2 - SP-SPIO Issue
TI-7777-0004 CR-013644D MLG Strut Redesign
TI-7777-0007 CR-015718A OBOGS Plenum HEPA Filter Provisioning
TI-7777-0010 CR-016660B Radar Harness Redesign
TI-7777-0024 CR-018697 Gun Gas Purge & Gun Port Door Actuators
TI-7777-0031 CR-018544 Brake Control Electronic Unit Update
TI-7777-0042 CR-018487A Return Fuel Cooler HX Coating
TI-7777-0057 CR-018378 Nacelle Fan - Full Qualified Configuration
TI-7777-0077 CR-009382B Small Diameter Bomb (SDB) Rack Strut
TI-7777-0081 CR-014768E 270V BCCU Change
TI-7777-0083 TBD EHAS/LEFAS -0011 EU & Rack Config Update
TI-7777-0084 CR-016708A ACCM Filter Pin
TI-7777-0085 CR-016758A Replacement of Door Actuator Lock Assemblies
TI-7777-0087 CR-016909A Flaperon EHA Pump Design Change
TI-7777-0089 CR-017095 Avionics Bay Environmental Seal Change
TI-7777-0093 CR-017505 Flow Sensor EMI/Vibration
TI-7777-0095 CR-017773 Manual Drive Unit
TI-7777-0097 CR-017937A IEU Lightning Compliance
TI-7777-0098 TBD CTOL Structure Redesign for Updated Gun Loads
TI-7777-0101 CR-15956A NLG Down Lock Actuator
TI-7777-0102 CR-016633C Canopy Actuation System
TI-7777-0106 CR-016912 WBD Fwd Uplock Roller Bracket
Remember Apollo 13?
Gene Kranz: Let's look at this thing from a... um, from a standpoint of status. What do we got on the craft that's good?
[pause]
Sy Liebergot: I'll get back to you, Gene.
[pause]
Sy Liebergot: I'll get back to you, Gene.
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Here's the most expensive weapons system ever and all of its ammunition in one photo
Says it all really, and this being a supposedly cheaper alternative to the F22.
Says it all really, and this being a supposedly cheaper alternative to the F22.
Designed and manufactured at Lockheed Martin's massive production facility in Fort Worth, Texas, the F-35 Lightning II can carry
an impressive 18,000 pounds of lethal ammunition.
an impressive 18,000 pounds of lethal ammunition.
The business insider puff piece caters to ... whom?
Commence nitpicking.
How cost was presented. The article called it the most expensive, at $103 million per copy. The single most expensive weapons carrying vehicle that I am familiar with is a Seawolf submarine: something over 3 billion. The next most pricy aircraft is the B-2, at something close to a billion a copy. On the other hand, the volume of these probably tips the program cost into the highest ever category ... the mini article noted the notional size of the buy, but didn't do the arithmetic to show why it's the most expensive program
End nitpicking
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Lethal Wing Tanks and Baggage Pods
Just to split hairs, is this saying that with a 426 gallon wing tank or two and a baggage pod, that a further 18,000 lbs can be carried, or are these classed as ammo?
Or is this just sadly poor PR?
Or is this just sadly poor PR?
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Original quote by Lonewolf_50:
The article called it the most expensive, at $103 million per copy.
The article called it the most expensive, at $103 million per copy.
Lockheed says that each F-35A jet, also referred to as the Conventional Takeoff and Landing ( CTOL ), costs $103 million (not including engine) and is the most requested of the three aircrafts.
BTW, Bennett Croswell, President of Pratt's Military operation, told the Flightglobal folks "The company stands by a commercially-derived programme that it has adapted for the F135."
Don't know what is meant by "commercially-derived" but hopefully that isn't what they do on their commercial product offerings.