Prosecution Insights
Last updated: October 02, 2026

Examiner: BONNETTE, RODNEY ANDREW

Tech Center 3600 • Art Units: 2837 2852 3642 3644 3647

This examiner grants 90% of resolved cases

Analysis

Rodney Andrew Bonnette has handled 1001 resolved cases, primarily in Tech Center 3600 and Art Unit 2837. The allowance rate is high at 90.5 percent, suggesting a very high probability of securing a patent. The median days to allowance is 778, which indicates a relatively efficient path through the USPTO. The 1001 resolved cases make this a data-rich profile.

The interview lift is 6.4 percent. While this is a positive contribution, the high baseline allowance rate of 90.5 percent means that most applications are successful even without an interview. However, for difficult cases, the 6.4 percent lift still offers a useful advantage. Practitioners can expect a consistent experience in Art Unit 2837 given the volume of 1001 resolved cases.

The 778 day median pendency is competitive, and the 6.4 percent interview lift provides a small but helpful tool for navigating the final stages of prosecution. With a 90.5 percent allowance rate, the examiner demonstrates a clear path to grant. This efficiency is reflected in the 778 day timeline, which is favorable for applicants in Tech Center 3600. The data is highly reliable.

Written from this page's own data; every figure is computed from USPTO records and verified before publication.

Performance Statistics

90.5%
Allow Rate
+38.5% vs TC avg
1,019
Total Applications
+6.4%
Interview Lift
778
Avg Prosecution Days
Based on 1001 resolved cases, 2023–2026

Rejection Statute Breakdown

2.3%
§101 Eligibility
29.6%
§102 Novelty
34.9%
§103 Obviousness
23.0%
§112 Clarity

Currently Pending Office Actions

App #TitleStatusAssignee
18993374 MANAGEMENT OF THE DRAWING OF MECHANICAL POWER FROM A TWO-SPOOL OR THREE-SPOOL TURBINE ENGINE Non-Final OA SAFRAN AIRCRAFT ENGINES
19226678 AIRCRAFT STRUCTURE Non-Final OA Airbus Operations Limited
19539684 A MEASUREMENT APPARATUS FOR DETERMINING A VELOCITY OF A FLUID Non-Final OA AIRBUS HELICOPTERS DEUTSCHLAND GMBH
19154327 METHOD FOR CONTROLLING ANTI-ICING MEANS IN AN AIRCRAFT AS A FUNCTION OF THE ICE ACCRETION RATE, AND CORRESPONDING SYSTEM Final Rejection SAFRAN AEROSYSTEMS
19370593 ADDITIVE MANUFACTURED INTEGRAL FASTENING SYSTEM FOR MISSION ADAPTABLE UNMANNED AERIAL VEHICLES Non-Final OA Firestorm Labs, Inc.

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