Prosecution Insights
Last updated: October 25, 2026
Application No. 19/291,136

HYDROGEN-POWERED AIRCRAFT WITH ANTENNA FOR SATELLITE INTERNET ACCESS

Final Rejection §112
Filed
Aug 05, 2025
Priority
Aug 07, 2024 — DE 102024122482.7
Examiner
SANDERSON, JOSEPH W
Art Unit
3619
Tech Center
3600 — Transportation & Electronic Commerce
Assignee
Airbus Operations GmbH
OA Round
2 (Final)
77%
Grant Probability
Favorable
3-4
OA Rounds
1y 7m
Est. Remaining
91%
With Interview

Examiner Intelligence

Grants 77% — above average
77%
Career Allowance Rate
724 granted / 935 resolved
+25.4% vs TC avg
Moderate +14% lift
Without
With
+13.8%
Interview Lift
resolved cases with interview
Typical timeline
2y 10m
Avg Prosecution
14 currently pending
Career history
954
Total Applications
across all art units

Statute-Specific Performance

§101
2.9%
-37.1% vs TC avg
§103
34.4%
-5.6% vs TC avg
§102
22.5%
-17.5% vs TC avg
§112
31.3%
-8.7% vs TC avg
Black line = Tech Center average estimate • Based on career data from 935 resolved cases

Office Action

§112
DETAILED ACTION The present application, filed on or after March 16, 2013, is being examined under the first inventor to file provisions of the AIA . Claim Rejections - 35 USC § 112 The following is a quotation of 35 U.S.C. 112(b): (b) CONCLUSION.—The specification shall conclude with one or more claims particularly pointing out and distinctly claiming the subject matter which the inventor or a joint inventor regards as the invention. The following is a quotation of 35 U.S.C. 112 (pre-AIA ), second paragraph: The specification shall conclude with one or more claims particularly pointing out and distinctly claiming the subject matter which the applicant regards as his invention. Claims 10-12, 14, and 15 are rejected under 35 U.S.C. 112(b) or 35 U.S.C. 112 (pre-AIA ), second paragraph, as being indefinite for failing to particularly point out and distinctly claim the subject matter which the inventor or a joint inventor (or for applications subject to pre-AIA 35 U.S.C. 112, the applicant), regards as the invention. Claim 10 recites a fairing partially covering the antenna. This fairing is a component of the embodiment of Figs 5 and 6. However, claim 1 requires the antenna to be at least partially countersunk, according to the embodiments of Figs 1-4. The claim accordingly is unclear for combining two mutually exclusive species. See MPEP 2173.03. Similarly for claim 14, which requires the covering skin flush with the fuselage from claim 13. Claim 12 recites a transport pipe of “the system”, however it is unclear as to which system this refers. Similarly for claim 15. Allowable Subject Matter Claims 1, 4-9, 13, and 16-21 are allowed. Claims 10-12, 14, and 15 would be allowable if rewritten to overcome the rejection(s) under 35 U.S.C. 112(b) or 35 U.S.C. 112 (pre-AIA ), 2nd paragraph, set forth in this Office action and to include all of the limitations of the base claim and any intervening claims. Response to Arguments Applicant’s arguments with respect to the claim(s) have been considered but are moot because the new ground of rejection does not rely on any reference applied in the prior rejection of record for any teaching or matter specifically challenged in the argument. Conclusion Applicant's amendment necessitated the new ground(s) of rejection presented in this Office action. Accordingly, THIS ACTION IS MADE FINAL. See MPEP § 706.07(a). Applicant is reminded of the extension of time policy as set forth in 37 CFR 1.136(a). A shortened statutory period for reply to this final action is set to expire THREE MONTHS from the mailing date of this action. In the event a first reply is filed within TWO MONTHS of the mailing date of this final action and the advisory action is not mailed until after the end of the THREE-MONTH shortened statutory period, then the shortened statutory period will expire on the date the advisory action is mailed, and any nonprovisional extension fee (37 CFR 1.17(a)) pursuant to 37 CFR 1.136(a) will be calculated from the mailing date of the advisory action. In no event, however, will the statutory period for reply expire later than SIX MONTHS from the mailing date of this final action. Any inquiry concerning this communication or earlier communications from the examiner should be directed to Joseph W Sanderson whose telephone number is (571)272-6337. The examiner can normally be reached Mon-Thu 6-3 ET. Examiner interviews are available via telephone, in-person, and video conferencing using a USPTO supplied web-based collaboration tool. To schedule an interview, applicant is encouraged to use the USPTO Automated Interview Request (AIR) at http://www.uspto.gov/interviewpractice. If attempts to reach the examiner by telephone are unsuccessful, the examiner’s supervisor, Anna Momper can be reached at 571-270-5788. The fax phone number for the organization where this application or proceeding is assigned is 571-273-8300. Information regarding the status of published or unpublished applications may be obtained from Patent Center. Unpublished application information in Patent Center is available to registered users. To file and manage patent submissions in Patent Center, visit: https://patentcenter.uspto.gov. Visit https://www.uspto.gov/patents/apply/patent-center for more information about Patent Center and https://www.uspto.gov/patents/docx for information about filing in DOCX format. For additional questions, contact the Electronic Business Center (EBC) at 866-217-9197 (toll-free). If you would like assistance from a USPTO Customer Service Representative, call 800-786-9199 (IN USA OR CANADA) or 571-272-1000. /JOSEPH W SANDERSON/ Primary Examiner, Art Unit 3619
Read full office action

Prosecution Timeline

Aug 05, 2025
Application Filed
May 13, 2026
Non-Final Rejection mailed — §112
Aug 11, 2026
Response Filed
Sep 14, 2026
Final Rejection mailed — §112 (current)

Precedent Cases

Applications granted by this same examiner with similar technology

Patent 12765674
CHAIR AND FURNITURE COMPOSITION
2y 5m to grant Granted Oct 20, 2026
Patent 12767340
AIRCRAFT PROPULSION ASSEMBLY HAVING AN ENGINE, A PYLON AND MEANS FOR ATTACHING THE ENGINE TO THE PYLON
1y 10m to grant Granted Oct 20, 2026
Patent 12752903
AIRCRAFT FUSELAGE SECTION
1y 9m to grant Granted Oct 06, 2026
Patent 12746887
SYSTEMS AND METHODS FOR RESTRAINING A PASSENGER VIA A VARIABLE-STIFFNESS BLANKET
2y 6m to grant Granted Sep 29, 2026
Patent 12735170
VEHICLE HAVING A BODY WITH A NOSE SECTION
2y 11m to grant Granted Sep 15, 2026
Study what changed to get past this examiner. Based on 5 most recent grants.

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Prosecution Projections

3-4
Expected OA Rounds
77%
Grant Probability
91%
With Interview (+13.8%)
2y 10m (~1y 7m remaining)
Median Time to Grant
Moderate
PTA Risk
Based on 935 resolved cases by this examiner. Grant probability derived from career allowance rate.

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