| Test ID | Requirement ID | Method | Sample size | Conditions | Acceptance criteria | Equipment | Who | When | Result | Revision tested |
|---|---|---|---|---|---|---|---|---|---|---|
| T01 | R01 / CTQ01 / DF01 | Internal proposed method: Cycle rig then 5 N outward retention pull | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Door remains latched in 100 dry capture cycles on each of 10 concept units; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T02 | R02 / CTQ02 / DF02 | Internal proposed method: Occlude either vent bank with paper surrogate; inspect remaining airflow path | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | At least two independent raised vent paths remain unobstructed in bedding surrogate trial; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T03 | R03 / CTQ03 / DF03 | Internal proposed method: Video-record unloaded representative-user task | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Release grip keeps fingers 30 mm from door path; 10 adult users complete unloaded task without path contact; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T04 | R04 / CTQ04 / DF04 | Internal proposed method: Fluorescent soil inspection after hand wash; biological efficacy not claimed | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Shell opens without tools; no visible fluorescent soil remains after defined wash on 10 units; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T05 | R05 / CTQ05 / DF05 | Internal proposed method: Force gauge pull and foreseeable misuse inspection | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Bait insert remains captive after 20 N pull on 10 units; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T06 | R06 / CTQ06 / DF06 | Internal proposed method: 10-user visibility/teach-back study; no live animals before ethical review | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Instructions require frequent manual checks; user can see occupancy without opening; welfare reviewer sets actual interval before use; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T07 | R07 / CTQ07 / DF07 | Internal proposed method: Probe each chamber loaded with surrogates in 50 cycles | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Proposed 3-compartment target; rigid mouse surrogates cannot back-drive baffle at 2 N; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T08 | R08 / CTQ08 / DF08 | Internal proposed method: Injected beam blockage, drift and stuck-value cases | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Detect surrogate in each chamber in 100 placements including dust challenge; zero false-empty permitted in concept screen; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T09 | R09 / CTQ09 / DF09 | Internal proposed method: Router loss/reconnect and phone permission fault injection | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Local occupancy indicator works without network; app marks offline within proposed 5 minutes; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T10 | R10 / CTQ10 / DF10 | Internal proposed method: Threat-model-led unauthorized pairing attempts on test build | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Provisioning requires physical button; unique device identity; unauthorized client denied in 50 attempts; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T11 | R11 / CTQ11 / DF11 | Internal proposed method: Interrupt update at 20 points; confirm last known good boot | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Local indication and mechanical capture remain safe after power interruption at each update phase; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T12 | R12 / CTQ12 / DF12 | Internal proposed method: Specialist battery fault evaluation; no destructive tests by unqualified users | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | No charging in wet state; proposed independent overtemperature cutoff at 45 C cell surface pending battery engineer review; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T13 | R13 / CTQ13 / DF13 | Internal proposed method: Assembly interlock test and controlled splash screen; no IP rating claimed | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Electronics detach before washing; power inhibited when cassette unseated; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T14 | R14 / CTQ14 / DF14 | Internal proposed method: Review data flows and test account deletion across backups | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Collect no precise location; proposed event retention 30 days with deletion request path; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T15 | R15 / CTQ15 / DF15 | Internal proposed method: Host pre-scan and authorization-path review; results not performed | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Choose candidate module only after grant, antenna and host obligations reviewed; no FCC ID invented; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T16 | R16 / CTQ16 / DF16 | Internal proposed method: Surrogate occupancy/thermal analysis first; ethical live study only if approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Capacity is not rated; proposed three isolated chambers require welfare specialist approval; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T17 | R17 / CTQ17 / DF17 | Internal proposed method: Test 20 surrogate obstruction positions with power isolated emergency stop | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Deployment requires clear-zone sensing and local supervised enable; obstruction forces stop before contact in unloaded trials; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T18 | R18 / CTQ18 / DF18 | Internal proposed method: Static 5x proposed payload proof test plus single-fault latch injection | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Two independent mechanical retention paths; release impossible until ground-contact confirmation; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T19 | R19 / CTQ19 / DF19 | Internal proposed method: Articulated probe and arm-inhibit single-fault tests | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | No rotor spin until guarded clearance zone verified; guarded ground fixture used first; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T20 | R20 / CTQ20 / DF20 | Internal proposed method: Hardware-in-loop injected 20 m position jumps and stale fixes | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Containment geofence independent of mission planner; abort on estimator disagreement; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T21 | R21 / CTQ21 / DF21 | Internal proposed method: Simulate doubled return energy and degraded pack capacity | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Return energy reserve proposed at least 40% under worst-case modeled payload and wind; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T22 | R22 / CTQ22 / DF22 | Internal proposed method: Disconnect phone, radio and cloud separately in simulation | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Phone is not safety-critical; autonomous supervisor reaches predefined safe state on link loss; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T23 | R23 / CTQ23 / DF23 | Internal proposed method: Inject release command in every mission phase; verify inhibited | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Release permitted only when stationary on validated landing surface with motors stopped; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T24 | R24 / CTQ24 / DF24 | Internal proposed method: Review jurisdiction and destination documents; no destination approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | No field release until actual local species rules, landowner permission and welfare assessment recorded; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T25 | R25 / CTQ25 / DF25 | Internal proposed method: FAA operational applicability review including line-of-sight and authorization questions | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | No unattended outdoor launch; flight operations require qualified review of route, operator, airspace and permissions; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T26 | R26 / CTQ26 / DF26 | Internal proposed method: Bench configuration and record review; no registration asserted | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Remote ID and registration applicability resolved for exact aircraft before any outdoor flight; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T27 | R27 / CTQ27 / DF27 | Internal proposed method: Specialist fault injection of short, misalignment and sensor open | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Dual isolation and independent thermal protection; no charge after failed dock alignment; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T28 | R28 / CTQ28 / DF28 | Internal proposed method: Hardware-in-loop gust and missing-sensor scenarios | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Research envelope proposed dry conditions and wind below 3 m/s; actual limits require flight validation; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T29 | R29 / CTQ29 / DF29 | Internal proposed method: Replay, tamper and privilege escalation tests in isolated rig | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Only authenticated signed mission plan; user cannot bypass safety envelope remotely; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
| T30 | R30 / CTQ30 / DF30 | Internal proposed method: Simulate moved dock, marker occlusion and blocked return path | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Indoor controlled bench; flight simulation only; representative misuse injected | Maximum one failed docking attempt then designated safe land; no repeated wall approach; scenario C1 not approved | Force gauge/temperature logger/video or HIL harness; calibration before use | Jordan Vale | Not ready — design/safety review first | Not performed — concept planning only; no approval or test evidence exists | C1 concept; no unit tested |
Sample — fictitious company. All numbers and people are invented scenario assumptions. This is draft concept paperwork; no physical testing, customer evidence, certification, filing or sign-off has occurred.