Detailed information about the 100 most recent patent applications.
| Application Number | Title | Filing Date | Disposal Date | Disposition | Time (months) | Office Actions | Restrictions | Interview | Appeal |
|---|---|---|---|---|---|---|---|---|---|
| 18971137 | JET ENGINE | December 2024 | March 2025 | Allow | 3 | 0 | 0 | Yes | No |
| 18712427 | GAS TURBINE PLANT, METHOD FOR OPERATING SAME, AND METHOD FOR MODIFYING SAME | May 2024 | March 2025 | Allow | 10 | 0 | 1 | Yes | No |
| 18252833 | METHOD AND ARCHITECTURE FOR SUPPLYING AIR TO AN AUXILIARY POWER UNIT OF AN AIRCRAFT | May 2023 | December 2024 | Allow | 19 | 2 | 0 | Yes | No |
| 18309262 | COMBUSTOR ASSEMBLY FOR A TURBINE ENGINE | April 2023 | March 2025 | Allow | 23 | 2 | 0 | Yes | No |
| 18034119 | COMBUSTION DEVICE HAVING A FLAMELESS COMBUSTION CHAMBER, USE OF SUCH A DEVICE AND ELECTRICITY PRODUCTION OR ENERGY COGENERATION APPARATUS COMPRISING SUCH A DEVICE | April 2023 | January 2024 | Allow | 9 | 0 | 0 | Yes | No |
| 18129238 | FUEL SUPPLY PIPE ASSEMBLY, GAS TURBINE COMBUSTOR, AND GAS TURBINE | March 2023 | March 2024 | Allow | 11 | 1 | 0 | Yes | No |
| 18120183 | RADIALLY ORIENTED INTERNALLY MOUNTED CONTINUOUS IGNITION DEVICE | March 2023 | May 2024 | Allow | 14 | 2 | 0 | Yes | No |
| 18113446 | TURBINE ENGINE FUEL INJECTOR ASSEMBLY WITH ANNULAR FUEL OUTLET | February 2023 | May 2025 | Allow | 27 | 4 | 0 | Yes | Yes |
| 18158979 | FUEL NOZZLES | January 2023 | July 2024 | Abandon | 17 | 2 | 0 | No | No |
| 18152903 | AIRCRAFT PROPULSION SYSTEM | January 2023 | April 2025 | Allow | 27 | 3 | 1 | Yes | No |
| 18093044 | COMPONENT FOR A GAS TURBINE ENGINE | January 2023 | August 2024 | Abandon | 19 | 2 | 0 | No | No |
| 18149895 | REHEAT ASSEMBLY FOR GAS TURBINE ENGINE | January 2023 | February 2025 | Abandon | 26 | 4 | 0 | Yes | No |
| 18067367 | Igniter Port Retention System | December 2022 | June 2024 | Abandon | 18 | 2 | 0 | Yes | No |
| 17928771 | FUEL INJECTOR, COMBUSTOR INCLUDING THE FUEL INJECTOR, AND GAS TURBINE INCLUDING THE COMBUSTOR | November 2022 | January 2025 | Allow | 25 | 3 | 0 | Yes | No |
| 17980273 | MULTITUBE PILOT INJECTOR HAVING A SPLIT AIRFLOW FOR A GAS TURBINE ENGINE | November 2022 | January 2024 | Allow | 14 | 2 | 0 | Yes | No |
| 17980263 | MULTITUBE PILOT INJECTOR HAVING A FLAME ANCHOR FOR A GAS TUBINE ENGINE | November 2022 | April 2025 | Allow | 29 | 2 | 0 | Yes | No |
| 17976413 | GAS TURBINE ENGINE COMPONENT WITH INTEGRAL HEAT EXCHANGER | October 2022 | July 2025 | Allow | 32 | 5 | 0 | Yes | No |
| 17803601 | Pulsed Supersonic Air-Turbine Engine with Speed Control | September 2022 | August 2023 | Allow | 12 | 1 | 0 | Yes | No |
| 17891756 | FUEL ASSEMBLY FOR A GAS TURBINE ENGINE | August 2022 | November 2023 | Allow | 15 | 1 | 1 | Yes | No |
| 17798860 | TURBOFAN ENGINE | August 2022 | January 2024 | Abandon | 17 | 1 | 0 | No | No |
| 17758997 | FUEL SUPPLY CIRCUIT FOR A COMBUSTION CHAMBER OF A TURBOMACHINE | July 2022 | October 2023 | Allow | 15 | 2 | 0 | Yes | No |
| 17861878 | EFFUSION COOLING FOR DILUTION/QUENCH HOLE EDGES IN COMBUSTOR LINER PANELS | July 2022 | July 2024 | Allow | 24 | 3 | 0 | Yes | No |
| 17835525 | CONTINUOUS IGNITION DEVICE EXHAUST MANIFOLD | June 2022 | September 2023 | Allow | 16 | 2 | 0 | Yes | No |
| 17740484 | DRY LOW NOx STAGED COMBUSTION SYSTEM | May 2022 | July 2024 | Allow | 26 | 0 | 0 | Yes | No |
| 17662535 | DIFFUSER WITH PASSLETS | May 2022 | June 2025 | Allow | 38 | 5 | 1 | Yes | No |
| 17755306 | SYSTEM AND METHOD FOR OPERATING A COMBUSTOR WITH MULTIPLE LIQUID FUELS | April 2022 | June 2025 | Allow | 37 | 4 | 1 | Yes | No |
| 17655679 | BURNER HEAD | March 2022 | October 2024 | Abandon | 31 | 4 | 1 | Yes | No |
| 17686759 | AIRCRAFT HAVING AN ENGINE AND A COOLING SYSTEM | March 2022 | October 2023 | Abandon | 20 | 2 | 0 | No | No |
| 17686911 | TORCH IGNITER COOLING SYSTEM | March 2022 | May 2023 | Allow | 14 | 1 | 0 | Yes | No |
| 17639762 | GAS TURBINE COMBUSTOR, GAS TURBINE, AND COMBUSTION METHOD FOR OIL FUEL | March 2022 | April 2025 | Abandon | 38 | 4 | 0 | Yes | No |
| 17676949 | TURBINE ENGINE EXHAUST DUCT SYSTEM AND METHODS FOR NOISE DAMPENING AND ATTENUATION | February 2022 | January 2025 | Allow | 34 | 4 | 0 | Yes | No |
| 17581358 | CONNECTING FUEL INJECTORS AND NOZZLES TO MANIFOLDS | January 2022 | January 2025 | Abandon | 36 | 4 | 1 | Yes | No |
| 17568359 | SYSTEMS AND METHODS FOR PROVIDING OUTPUT PRODUCTS TO A COMBUSTION CHAMBER OF A GAS TURBINE ENGINE | January 2022 | March 2024 | Allow | 26 | 3 | 0 | Yes | No |
| 17562100 | MICRO-MIXER BUNDLE ASSEMBLY, AND COMBUSTOR AND GAS TURBINE HAVING SAME | December 2021 | October 2023 | Allow | 22 | 2 | 0 | Yes | No |
| 17561962 | INJECTION NOZZLE, COMBUSTOR INCLUDING SAME NOZZLE, AND GAS TURBINE INCLUDING SAME COMBUSTOR | December 2021 | January 2024 | Allow | 25 | 3 | 1 | Yes | No |
| 17554853 | GAS TURBINE ENGINE SYSTEM WITH MIXED FLOW AUXILIARY POWER UNIT | December 2021 | February 2024 | Allow | 26 | 3 | 0 | Yes | No |
| 17533682 | FUEL INJECTOR SYSTEMS FOR TORCH IGNITERS | November 2021 | November 2023 | Allow | 24 | 2 | 0 | Yes | No |
| 17609895 | FUEL GAS SUPPLY DEVICE AND METHOD | November 2021 | January 2025 | Abandon | 39 | 4 | 0 | No | No |
| 17498705 | SYSTEM AND METHOD FOR SWEEPING LEAKED FUEL IN GAS TURBINE SYSTEM | October 2021 | September 2023 | Allow | 23 | 2 | 0 | Yes | No |
| 17492783 | SYSTEM FOR COOLING AN AIRCRAFT TURBOJET ENGINE | October 2021 | February 2025 | Abandon | 41 | 3 | 0 | Yes | No |
| 17485567 | LASER IGNITION DEVICE, SPACE ENGINE, AND AIRCRAFT ENGINE | September 2021 | February 2024 | Abandon | 29 | 2 | 0 | No | No |
| 17475440 | FUEL SYSTEM WITH ECOLOGY FUNCTION | September 2021 | February 2024 | Allow | 29 | 2 | 0 | Yes | No |
| 17406655 | START-UP SEQUENCE FOR GASEOUS FUEL ENGINE | August 2021 | September 2023 | Abandon | 24 | 2 | 0 | No | No |
| 17392653 | EXCESS FUEL FLOW TO DRIVE TURBINE | August 2021 | March 2025 | Allow | 43 | 2 | 0 | Yes | Yes |
| 17388618 | GAS TURBINE ENGINE HAVING A HEAT EXCHANGER LOCATED IN AN ANNULAR DUCT | July 2021 | April 2024 | Abandon | 32 | 3 | 0 | Yes | No |
| 17367440 | COMBUSTOR NOZZLE, AND COMBUSTOR AND GAS TURBINE INCLUDING THE SAME | July 2021 | June 2023 | Allow | 24 | 3 | 0 | Yes | No |
| 17350652 | COMBUSTOR HAVING FUEL SWEEPING STRUCTURES | June 2021 | May 2022 | Allow | 11 | 0 | 0 | Yes | No |
| 17346768 | GAS TURBINE FACILITY | June 2021 | October 2023 | Abandon | 28 | 2 | 1 | No | No |
| 17333986 | SUPPLEMENTAL THRUST SYSTEM WITH ROTATING DETONATION COMBUSTOR | May 2021 | July 2024 | Allow | 38 | 4 | 1 | Yes | No |
| 17329566 | FUEL MANIFOLDS | May 2021 | February 2023 | Allow | 20 | 1 | 0 | Yes | No |
| 17323088 | PASSIVE FUEL COUPLED DYNAMIC MITIGATION DEVICE | May 2021 | July 2024 | Abandon | 37 | 4 | 0 | Yes | No |
| 17317102 | INTEGRAL FUEL-NOZZLE AND MIXER WITH ANGLED JET-IN-CROSSFLOW FUEL INJECTION | May 2021 | July 2024 | Abandon | 38 | 5 | 0 | No | No |
| 17244275 | Gas Turbine Combustor | April 2021 | January 2024 | Abandon | 32 | 3 | 0 | Yes | No |
| 17242462 | FUEL INJECTION DEVICE, NOZZLE, AND COMBUSTOR INCLUDING THE SAME | April 2021 | January 2024 | Allow | 33 | 4 | 0 | Yes | No |
| 17228433 | DILUTION HORN PAIR FOR A GAS TURBINE ENGINE COMBUSTOR | April 2021 | March 2024 | Abandon | 35 | 3 | 1 | No | No |
| 17216952 | AIRFOIL WITH RADIALLY-SPACED RIBS AND INTERLOCKING TAB | March 2021 | July 2022 | Allow | 16 | 1 | 0 | Yes | No |
| 17194917 | NOZZLE WITH JET GENERATOR CHANNEL FOR FUEL TO BE INJECTED INTO A COMBUSTION CHAMBER OF AN ENGINE | March 2021 | April 2023 | Abandon | 25 | 2 | 0 | No | No |
| 17193369 | VANE ARC SEGMENT WITH RADIALLY PROJECTING FLANGES | March 2021 | February 2023 | Allow | 24 | 2 | 0 | Yes | Yes |
| 17173429 | FLOWPATH ASSEMBLY WITH COMPOSITE TUBE ARRAY | February 2021 | April 2025 | Abandon | 50 | 4 | 1 | Yes | No |
| 17166551 | FUEL INJECTION DEVICE FOR GAS TURBINE | February 2021 | February 2023 | Abandon | 24 | 2 | 0 | Yes | Yes |
| 17136131 | MAGNETIC TURBOMACHINE SEALING ARRANGEMENT | December 2020 | February 2022 | Allow | 14 | 0 | 1 | Yes | No |
| 17132066 | SYSTEMS AND METHODS UTILIZING TURBINE COMPRESSOR DISCHARGE FOR HYDROSTATIC MANIFOLD PURGE | December 2020 | September 2023 | Allow | 33 | 4 | 0 | Yes | No |
| 17127250 | FUEL INJECTOR SYSTEMS FOR TORCH IGNITERS | December 2020 | September 2021 | Allow | 10 | 0 | 0 | Yes | No |
| 17125072 | RADIALLY ORIENTED INTERNALLY MOUNTED CONTINUOUS IGNITION DEVICE | December 2020 | July 2023 | Abandon | 31 | 3 | 0 | No | No |
| 17123741 | CONTINUOUS IGNITION DEVICE EXHAUST MANIFOLD | December 2020 | March 2022 | Allow | 15 | 1 | 0 | Yes | No |
| 17123778 | HIGH-PRESSURE CONTINUOUS IGNITION DEVICE | December 2020 | September 2021 | Allow | 9 | 1 | 0 | Yes | No |
| 17115877 | COMBUSTOR MIXING ASSEMBLY | December 2020 | May 2023 | Allow | 29 | 2 | 1 | Yes | No |
| 16972777 | POWER PLANT WITH NATURAL GAS REGASIFICATION | December 2020 | January 2024 | Abandon | 37 | 5 | 0 | No | No |
| 16972765 | EXPANDED GAS TURBINE PROCESS WITH NATURAL GAS REGASIFICATION | December 2020 | November 2021 | Allow | 11 | 1 | 0 | Yes | No |
| 17112615 | METHODS AND APPARATUS TO OPERATE A GAS TURBINE ENGINE WITH HYDROGEN GAS | December 2020 | December 2021 | Allow | 12 | 1 | 0 | Yes | No |
| 17112447 | Gas Turbine Combustor | December 2020 | March 2024 | Abandon | 40 | 4 | 0 | No | No |
| 17110619 | SUPPLEMENTAL THRUST SYSTEM FOR A GAS TURBINE ENGINE | December 2020 | June 2025 | Allow | 55 | 7 | 1 | Yes | No |
| 17102638 | FUEL SWIRLER FOR PRESSURE FUEL NOZZLES | November 2020 | February 2025 | Allow | 51 | 7 | 1 | Yes | No |
| 17089250 | TORCH IGNITER COOLING SYSTEM | November 2020 | November 2021 | Allow | 12 | 0 | 0 | Yes | No |
| 17080410 | FLASHBACK RESISTANT PREMIXED FUEL INJECTOR FOR A GAS TURBINE ENGINE | October 2020 | February 2023 | Allow | 27 | 3 | 0 | Yes | No |
| 17050080 | FUEL NOZZLE AND COMBUSTOR FOR GAS TURBINE, AND GAS TURBINE | October 2020 | April 2024 | Abandon | 41 | 4 | 0 | Yes | No |
| 17049442 | INJECTION SYSTEM FOR A TURBINE ENGINE ANNULAR COMBUSTION CHAMBER | October 2020 | November 2021 | Allow | 13 | 1 | 0 | Yes | No |
| 17036745 | FUEL INJECTION ASSEMBLY FOR A TURBOMACHINE | September 2020 | April 2023 | Allow | 30 | 2 | 0 | Yes | No |
| 16980998 | COMBUSTOR AND GAS TURBINE INCLUDING THE SAME | September 2020 | March 2022 | Allow | 17 | 2 | 0 | Yes | No |
| 17020034 | INTEGRATED ENVIRONMENTAL CONTROL AND BUFFER AIR SYSTEM | September 2020 | July 2022 | Allow | 22 | 2 | 0 | Yes | No |
| 16976354 | COMBUSTION CHAMBER HAVING A DOUBLE CHAMBER BOTTOM | August 2020 | November 2021 | Allow | 15 | 1 | 0 | Yes | No |
| 16940953 | COMBUSTOR CAP ASSEMBLY HAVING IMPINGEMENT PLATE WITH COOLING TUBES | July 2020 | August 2022 | Allow | 25 | 3 | 0 | Yes | No |
| 16929142 | FUEL INJECTOR | July 2020 | February 2022 | Allow | 19 | 1 | 0 | Yes | No |
| 16928056 | TRANSLATING INLET FOR ADJUSTING AIRFLOW DISTORTION IN GAS TURBINE ENGINE | July 2020 | May 2022 | Allow | 22 | 2 | 0 | Yes | No |
| 16917213 | AIRCRAFT WITH ENVIRONMENTAL CONTROL SYSTEM | June 2020 | December 2021 | Allow | 17 | 1 | 0 | Yes | No |
| 16888147 | VARIABLE SUPERSONIC ENGINE INLET | May 2020 | November 2022 | Allow | 29 | 1 | 0 | Yes | No |
| 15929768 | METHODS AND SYSTEMS FOR SUPPLYING FUEL TO GAS TURBINE ENGINES | May 2020 | March 2021 | Allow | 10 | 1 | 1 | Yes | No |
| 15929770 | SYSTEMS AND METHODS UTILIZING TURBINE COMPRESSOR DISCHARGE FOR HYDROSTATIC MANIFOLD PURGE | May 2020 | February 2021 | Allow | 9 | 0 | 1 | Yes | No |
| 16871124 | SYSTEM AND METHOD FOR PURGING A FUEL MANIFOLD OF A GAS TURBINE ENGINE USING AN ACCUMULATOR | May 2020 | January 2022 | Abandon | 20 | 1 | 0 | No | No |
| 16871271 | THRUST REVERSER FOR AN AIRCRAFT TURBOJET ENGINE NACELLE AND ASSOCIATED NACELLE | May 2020 | January 2022 | Abandon | 20 | 1 | 0 | No | No |
| 16861003 | WIND FUNNEL AND GAS COMBUSTION TURBINE SYSTEMS INCLUDING COMPRESSION SECTIONS | April 2020 | March 2021 | Allow | 11 | 1 | 0 | Yes | No |
| 16861122 | WIND FUNNEL, GAS COMBUSTION TURBINE AND POWER OUTPUT GENERATOR SYSTEMS | April 2020 | May 2025 | Abandon | 60 | 3 | 1 | Yes | Yes |
| 16854953 | COMBUSTOR WITH AXIAL FUEL STAGING SYSTEM AND GAS TURBINE HAVING THE SAME | April 2020 | January 2022 | Allow | 21 | 1 | 0 | Yes | No |
| 16838802 | TURBINE FRACTURING SEMI-TRAILER | April 2020 | February 2024 | Abandon | 46 | 7 | 0 | Yes | No |
| 16833938 | METHOD OF OPERATING A COMBUSTOR HEAD END ASSEMBLY | March 2020 | February 2023 | Abandon | 34 | 4 | 0 | Yes | No |
| 16827021 | TURBOFAN ENGINE COMPRISING A SERIES OF ROTARY BLADES FOR BLOCKING THE STREAM OF THE BYPASS AIR | March 2020 | May 2022 | Allow | 26 | 0 | 0 | Yes | No |
| 16814494 | AIRCRAFT PROPULSION SYSTEM INCLUDING A HEAT EXCHANGER SYSTEM | March 2020 | May 2021 | Allow | 15 | 0 | 0 | Yes | No |
| 16803990 | COMBUSTOR AND GAS TURBINE HAVING THE SAME | February 2020 | July 2021 | Allow | 17 | 1 | 0 | Yes | No |
| 16798969 | DIFFUSER CASE MIXING CHAMBER FOR A TURBINE ENGINE | February 2020 | June 2021 | Allow | 16 | 2 | 0 | Yes | No |
| 16797487 | HIGH SPEED PROPULSION SYSTEM WITH INLET COOLING | February 2020 | April 2021 | Abandon | 14 | 0 | 1 | No | No |
This analysis examines appeal outcomes and the strategic value of filing appeals for examiner KANG, EDWIN G.
With a 11.1% reversal rate, the PTAB affirms the examiner's rejections in the vast majority of cases. This reversal rate is in the bottom 25% across the USPTO, indicating that appeals face significant challenges here.
Filing a Notice of Appeal can sometimes lead to allowance even before the appeal is fully briefed or decided by the PTAB. This occurs when the examiner or their supervisor reconsiders the rejection during the mandatory appeal conference (MPEP § 1207.01) after the appeal is filed.
In this dataset, 14.3% of applications that filed an appeal were subsequently allowed. This appeal filing benefit rate is in the bottom 25% across the USPTO, indicating that filing appeals is less effective here than in most other areas.
⚠ Appeals to PTAB face challenges. Ensure your case has strong merit before committing to full Board review.
⚠ Filing a Notice of Appeal shows limited benefit. Consider other strategies like interviews or amendments before appealing.
Examiner KANG, EDWIN G works in Art Unit 3741 and has examined 322 patent applications in our dataset. With an allowance rate of 66.8%, this examiner allows applications at a lower rate than most examiners at the USPTO. Applications typically reach final disposition in approximately 35 months.
Examiner KANG, EDWIN G's allowance rate of 66.8% places them in the 20% percentile among all USPTO examiners. This examiner is less likely to allow applications than most examiners at the USPTO.
On average, applications examined by KANG, EDWIN G receive 2.45 office actions before reaching final disposition. This places the examiner in the 84% percentile for office actions issued. This examiner issues more office actions than most examiners, which may indicate thorough examination or difficulty in reaching agreement with applicants.
The median time to disposition (half-life) for applications examined by KANG, EDWIN G is 35 months. This places the examiner in the 21% percentile for prosecution speed. Applications take longer to reach final disposition with this examiner compared to most others.
Conducting an examiner interview provides a +74.1% benefit to allowance rate for applications examined by KANG, EDWIN G. This interview benefit is in the 99% percentile among all examiners. Recommendation: Interviews are highly effective with this examiner and should be strongly considered as a prosecution strategy. Per MPEP § 713.10, interviews are available at any time before the Notice of Allowance is mailed or jurisdiction transfers to the PTAB.
When applicants file an RCE with this examiner, 23.8% of applications are subsequently allowed. This success rate is in the 24% percentile among all examiners. Strategic Insight: RCEs show lower effectiveness with this examiner compared to others. Consider whether a continuation application might be more strategic, especially if you need to add new matter or significantly broaden claims.
This examiner enters after-final amendments leading to allowance in 16.9% of cases where such amendments are filed. This entry rate is in the 12% percentile among all examiners. Strategic Recommendation: This examiner rarely enters after-final amendments compared to other examiners. You should generally plan to file an RCE or appeal rather than relying on after-final amendment entry. Per MPEP § 714.12, primary examiners have discretion in entering after-final amendments, and this examiner exercises that discretion conservatively.
When applicants request a pre-appeal conference (PAC) with this examiner, 36.4% result in withdrawal of the rejection or reopening of prosecution. This success rate is in the 33% percentile among all examiners. Note: Pre-appeal conferences show below-average success with this examiner. Consider whether your arguments are strong enough to warrant a PAC request.
This examiner withdraws rejections or reopens prosecution in 45.5% of appeals filed. This is in the 8% percentile among all examiners. Of these withdrawals, 20.0% occur early in the appeal process (after Notice of Appeal but before Appeal Brief). Strategic Insight: This examiner rarely withdraws rejections during the appeal process compared to other examiners. If you file an appeal, be prepared to fully prosecute it to a PTAB decision. Per MPEP § 1207, the examiner will prepare an Examiner's Answer maintaining the rejections.
When applicants file petitions regarding this examiner's actions, 66.7% are granted (fully or in part). This grant rate is in the 85% percentile among all examiners. Strategic Note: Petitions are frequently granted regarding this examiner's actions compared to other examiners. Per MPEP § 1002.02(c), various examiner actions are petitionable to the Technology Center Director, including prematureness of final rejection, refusal to enter amendments, and requirement for information. If you believe an examiner action is improper, consider filing a petition.
Examiner's Amendments: This examiner makes examiner's amendments in 0.0% of allowed cases (in the 39% percentile). This examiner makes examiner's amendments less often than average. You may need to make most claim amendments yourself.
Quayle Actions: This examiner issues Ex Parte Quayle actions in 0.0% of allowed cases (in the 40% percentile). This examiner issues Quayle actions less often than average. Allowances may come directly without a separate action for formal matters.
Based on the statistical analysis of this examiner's prosecution patterns, here are tailored strategic recommendations:
Not Legal Advice: The information provided in this report is for informational purposes only and does not constitute legal advice. You should consult with a qualified patent attorney or agent for advice specific to your situation.
No Guarantees: We do not provide any guarantees as to the accuracy, completeness, or timeliness of the statistics presented above. Patent prosecution statistics are derived from publicly available USPTO data and are subject to data quality limitations, processing errors, and changes in USPTO practices over time.
Limitation of Liability: Under no circumstances will IronCrow AI be liable for any outcome, decision, or action resulting from your reliance on the statistics, analysis, or recommendations presented in this report. Past prosecution patterns do not guarantee future results.
Use at Your Own Risk: While we strive to provide accurate and useful prosecution statistics, you should independently verify any information that is material to your prosecution strategy and use your professional judgment in all patent prosecution matters.