# US 2026/0084818 A1 · Method of providing access and egress to an open cockpit of an aircraft > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 2026/0084818 A1 - Document ID: US20260084818A1 - Status: Published application - Kind: A1 - Application number: 18/895,054 - Filed: 2024-09-24 - Published: 2026-03-26 - Earliest claimed: 2024-09-24 - Assignees: Government of the United States as Represented by the Secretary of the Air Force - Applicants: Government of the United States as represented by the Secretary of the Air Force - Inventors: Nicholas Atkins - Web page: https://patentgrep.com/patent/US20260084818A1 ## CPC - B64D 11/00: Passenger or crew accommodation; Flight-deck installations not otherwise provided for - B64D: EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT ## Abstract A hinged ladder for ascending to and descending from a cockpit of an aircraft and method of using the ladder for access to and egress from the cockpit. The ladder is suspended from an anchor which supports the combined weight of the ladder and a user. The ladder comprises a plurality of rung plates connected by hinges. The rung plates have respective holes to accept the foot of a user. In use, the ladder is suspended from an anchor in use, and extends longitudinally. The ladder has a standoff to provide single point contact against a fuselage of the aircraft, preventing damage during use. The standoff may articulate outwardly from a rung plate about an X axis. The standoff may be braced by paired struts which articulate about respective Y axes, preventing collapse of the standoff. Each strut may be locked in position by a respective latch which articulates about a respective Z axis. ## Claims ### Claim 1 A method of providing access and egress to an open cockpit of an aircraft and comprising the steps of: a. providing an extendable ladder having a plurality of hingedly connected rung plates, each rung plate having opposed hinge edges with hinges generally perpendicular to a longitudinal axis of the ladder and being configured to fanfold the plurality of rung plates into a footprint, each rung plate having a hole therethrough, a first rung plate hingedly joined to a second rung plate of the plurality of rung plates and an attachment means joined to the first rung plate and adapted to removably suspend the ladder proximate a fuselage of the aircraft, the extendable ladder being fanfolded to lie withing a footprint of the first rung plate; b. disposing the ladder proximate the aircraft while being folded to lie within the footprint of the first rung plate; c. extending the ladder to be longitudinally elongate; and d. removably suspending the ladder from an edge of the cockpit so that a pilot can climb into or out of the cockpit using the ladder without the first rung plate or any of the rung plates touching a fuselage of the aircraft, wherein steps c and d are performed in any order. ### Claim 2 (depends on 1) A method according to claim 1 wherein the step of disposing the ladder proximate the aircraft while being folded comprises disposing the ladder within a map compartment inside the cockpit. ### Claim 3 (depends on 1) A method according to claim 1 wherein the step of disposing the ladder proximate the aircraft while being folded comprises moving the ladder from a first aircraft on a tarmac to a second aircraft on the same tarmac. ### Claim 4 (depends on 1) A method according to claim 1 wherein the step of removably suspending the ladder from an edge of the cockpit comprises hanging the ladder from the edge of the cockpit using a strap joined to the first rung plate. ### Claim 5 (depends on 1) A method according to claim 1 further comprising the steps of articulating a standoff outwardly from one of the rung plates; and disposing the standoff against the fuselage to prevent contact of the rung plates therewith. ### Claim 6 (depends on 5) A method according to claim 5 further comprising the step of disposing at least one strut between the standoff and a rung plate to stabilize the standoff in position against the fuselage. ### Claim 7 (depends on 6) A method according to claim 6 comprising the step of articulably disposing two symmetrically opposed struts between the standoff and the rung plate to stabilize the standoff in position against the fuselage. ### Claim 8 (depends on 7) A method according to claim 7 further comprising the step of securing the two struts to the rung plate. ### Claim 9 (depends on 8) A method according to claim 8 wherein the step of securing the struts to the rung plates comprises articulating a corresponding latch to engage the respective strut, the latch being joined to and articulating parallel to the rung plate. ### Claim 10 (depends on 6) A method according to claim 6 further comprising the step of obliquely angular disposing two adjacent rung plates in fixed position. ### Claim 11 (depends on 10) A method according to claim 10 wherein the two adjacent rung plates are the second rung plate and third rung plate. ### Claim 12 (depends on 10) A method according to claim 10 wherein the step of angularly disposing the two adjacent rung plates in fixed position comprises disposing a lock plate in fixed relationship therebetween and bridging a hinge connecting the two adjacent lock plates. ### Claim 13 A method of providing access or egress to a cockpit of an aircraft using a ladder having a longitudinal axis and a transverse direction perpendicular thereto, the method comprising the steps of: providing an extendable ladder having a plurality of hingedly connected rung plates, each rung plate having opposed hinge edges with hinges generally parallel to the transverse direction and being configured to fanfold the plurality of rung plates into a footprint, each rung plate having a hole therethrough, a first rung plate hingedly joinable to a second rung plate of the plurality of rung plates and an attachment means for joining the first rung plate to an anchor and adapted to removably suspend the ladder outside the aircraft, the extendable ladder being foldable to lie withing a footprint of the first rung plate; disposing the ladder proximate the aircraft; extending the ladder to be longitudinally elongate; and removably suspending the ladder from the aircraft so that a person can climb into or out of the cockpit. ### Claim 14 (depends on 13) A method according to claim 13 further comprising the step of articulably disposing a standoff intermediate a predetermined rung plate and a fuselage of the aircraft so that the ladder only contacts the fuselage at the standoff. ### Claim 15 (depends on 14) A method according to claim 14 wherein the standoff is hingedly joined to the predetermined rung plate. ### Claim 16 (depends on 15) A method according to claim 15 wherein the standoff is hingedly joined to the predetermined rung plate by a standoff hinge parallel to the transverse direction. ### Claim 17 (depends on 14) A method according to claim 14 wherein the step of articulably joining the standoff intermediate the predetermined rung plate and fuselage is performed before extending the ladder to be longitudinally elongate. ### Claim 18 A method of providing access or egress to a cockpit of an aircraft using a ladder having a longitudinal axis and a transverse direction perpendicular thereto, the method comprising the steps of: providing an extendable ladder having a plurality of hingedly connected rung plates, each rung plate having opposed hinge edges with hinges generally parallel to the transverse direction and being configured to fanfold the plurality of rung plates into a footprint, each rung plate having a hole therethrough, a first rung plate hingedly joinable to a second rung plate of the plurality of rung plates and an attachment means for joining the first rung plate to an anchor and adapted to removably suspend the ladder outside the aircraft, the extendable ladder being foldable to lie withing a footprint of the first rung plate; disposing the ladder proximate the aircraft; extending the ladder to be longitudinally elongate; removably suspending the ladder from the aircraft so that a person can climb into or out of the cockpit; and removing the ladder from the aircraft. ### Claim 19 (depends on 18) A method according to claim 18 further comprising the step of locking two adjacent rung plates in oblique angular relationship with a lock plate joined to a first adjacent rung plate by a lock plate hinge and being releasably joinable to a second adjacent lock plate by a hook. ### Claim 20 (depends on 19) A method according to claim 19 wherein the step of locking two adjacent rung plates in oblique angular relationship is performed after removably suspending the ladder from the aircraft.