JARUS SORA v2.5 · Issued dossier · SAIL III
| Dossier Reference | SORA-DSR-0f2a1c-20260417-v3 |
| Mission / Programme ID | 3c4b8a1e-7d41-48e2-9e0b-1f7a2d3c4b8a |
| SORA Version | JARUS SORA v2.5 (January 2024) |
| Dossier Version | 3 (supersedes v2 following mitigation refinement) |
| Issued | 2026-04-17T09:14:02Z |
| Authorisation Validity | 2026-05-01 → 2026-07-31 (3-month programme) |
| Overall Status | ISSUED |
| SAIL | III |
| Critical OSO Gaps | 0 |
| Operator Acceptance | ACCEPTED BY APPROVER |
| Item | Value |
|---|---|
| Operator | Demo TC-B Operator (specimen) |
| UASOC Reference | SACAA-ROC-2022-047 |
| Operation Type | Infrastructure corridor inspection, BVLOS |
| Operational Area | Linear corridor, 8.2 km length, 500 m buffer each side |
| Location | N-class provincial highway corridor, Northern Cape (specimen location) |
| Mission Type | mission.type.infrastructure / infra.corridor.linear |
| Operating Mode | ops.mode.bvlos (daytime, VMC) |
| Aircraft | DJI Matrice 350 RTK (MTOW 9.2 kg, max speed 23 m/s) |
| UAS Class | Specific (non-C-class); Part 108 authorisation pathway |
| Max Altitude | 120 m AGL |
| Max Range from PIC | 4.1 km (BVLOS, with observer relay) |
| Kinetic Energy at Impact | ~3.9 kJ (95th-percentile descent profile) |
| Planned Duration | Programme: 3 months; per-sortie: 45–90 minutes |
| Pilot in Command Pool | 4 approved PICs (RPC + BVLOS + night endorsed) |
| Crew | PIC + Observer (mandatory, BVLOS) + Safety Officer |
UAS kinetic energy 3.9 kJ places UAS in SORA Annex A column "< 34 kJ". Operational volume intersects sparsely-populated (90% of corridor length) and populated (10% of corridor length, two villages). Per SORA §2.1 decision table, combined exposure gives GRC = 5.
M1 tactical-mitigation reduction of 1 step applied (per §M1.a). M2 emergency-response plan satisfies SORA §M2 minimum. M3 parachute recovery system (certified ballistic parachute) reduces energy on uncontrolled descent. Residual GRC = 4.
| Tier | Mitigation | Robustness | Evidence |
|---|---|---|---|
| M1 | Population avoidance: 500 m lateral buffer over populated sections; altitude limitation 60 m AGL when within 200 m of any dwelling; programme rescheduling if headcount forecast > 12 in any corridor segment | Medium | Site survey report; real-time headcount monitor; corridor geofence |
| M2 | Emergency Response Plan (ERP) covering out-of-control descent, battery anomaly, loss of C2 link, and crew injury. Local emergency services pre-notified. | Medium | ERP document linked to evidence archive; local SAPS + EMS acknowledgement on file |
| M3 | Ballistic parachute recovery system (C-class certified, manufacturer-approved for MTOW 10 kg) deployed on airframe. Auto-deploy on attitude exceedance and manual trigger from PIC station. | Medium | Parachute certification document; last deployment test 2026-03-22 (PASS) |
Operational volume is Class G (uncontrolled) throughout. Nearest controlled airspace is Class C at 18 km lateral distance. Nearest aerodrome is an unlicensed grass strip at 6.4 km. Historical encounter rate with manned aircraft in the corridor sector is below SORA §3.2 threshold. Per SORA §3.2 table, ARC initial = ARC-b.
No strategic air risk mitigation was required to achieve a lower ARC. Strategic operational restrictions (altitude cap 120 m AGL, daytime VMC only) keep exposure to other airspace users minimal. ARC final remains ARC-b.
Per SORA §3.3, TMPR for ARC-b specifies a Medium robustness tactical mitigation against airborne conflict. Implemented through:
| GRC (final) | ARC (final) | SAIL (SORA v2.5 §4 matrix) |
|---|---|---|
| 4 | ARC-b | SAIL III |
| # | Objective | SAIL III Robustness | Status / Evidence |
|---|---|---|---|
| 01 | Ensure the operator is competent and/or proven | M | MET — UASOC + 3yr history |
| 02 | UAS manufactured by competent and/or proven entity | L | MET — DJI Type 3 manufacturer |
| 03 | UAS maintained by competent and/or proven entity | L | MET — in-house Part 101 programme |
| 04 | UAS developed to authority-recognised standards | L | MET — CE / FCC / EMC certified |
| 05 | UAS designed considering system safety and reliability | M | MET — redundant IMU, GPS, motors |
| 06 | C3 (command, control, communication) link performance is appropriate | L | MET — encrypted link, Medium robustness |
| 07 | Inspection of UAS (product inspection) for flight-readiness | M | MET — pre-flight checklist enforced by platform |
| 08 | Operational procedures defined, validated, and adhered to | M | MET — Operations Manual + SMS |
| 09 | Remote crew trained and current | M | MET — RPC + BVLOS + night endorsed |
| 10 | Safe recovery from technical issue | M | MET — ballistic parachute + return-to-home + flight termination |
| 11 | Procedures defined for deviations from normal | M | MET — ERP v2.3 |
| 12 | The UAS is designed to manage deterioration of external systems supporting UAS operation | L | MET — GPS-denied RTH; lost-link procedure |
| 13 | External services supporting UAS operations are adequate | L | MET — weather, airspace, credential surveillance |
| 14 | Operational procedures defined, validated, and adhered to (for environmental conditions) | M | MET — wind/visibility/ceiling thresholds enforced |
| 15 | C3 link performance is appropriate for the operation | L | MET — observer VLOS relay |
| 16 | Multi-crew coordination | M | MET — PIC/VO/SO roles with briefing artefact |
| 17 | Remote crew is fit to operate | M | MET — IMSAFE + medical + ELP active |
| 18 | Automatic protection of the flight envelope | H | PARTIAL — geofence + altitude limit; envelope protection at M robustness, planned upgrade to H |
| 19 | Safe recovery from Human Error | M | MET — checklist execution, RTH bound |
| 20 | A Safety Risk Assessment is completed | M | MET — this SORA dossier |
| 21 | SMS Human Factors evaluation has been performed | M | MET — SMS hazard register |
| 22 | The UAS is designed and qualified for adverse environmental conditions | L | MET — manufacturer IP certifications |
| 23 | Environmental conditions for safe operations are defined, measurable, and adhered to | L | MET — weather gate at M3 Phase 1B |
| 24 | Operator is connected with other airspace users, public authorities | M | MET — ATC briefing, NOTAM published, local EMS notified |
| Issuing authority (once granted) | SACAA — specific-category authorisation under Part 108. This dossier is the submission artefact; SACAA's decision is the authorisation. Operator accepts the dossier internally; the operator does not self-authorise a Part 108 operation. |
| Platform role | Advisory only — FlightDocket generates the dossier from the ten-step SORA assessment, not the authorisation. |
| Dossier status (specimen) | ACCEPTED INTERNALLY · ready for SACAA submission (SACAA response outside scope of this specimen) |
| SAIL | III |
| Validity window | 2026-05-01 → 2026-07-31 (inclusive) |
| Approved aircraft | DJI Matrice 350 RTK, registration ZA-SWUASROC-001 |
| Approved PIC pool | 4 approved PICs (actor references redacted in specimen) |
| Operating mode limitation | BVLOS, daytime, VMC only. Night operations excluded from this authorisation. |
| Altitude limitation | 120 m AGL maximum; 60 m AGL within 200 m of dwellings |
| Operational volume limitation | Linear corridor as defined in §1 ConOps; deviation > 500 m terminates sortie |
| Crew requirement | PIC + Observer + Safety Officer, minimum |
| OSO-18 conditional acceptance | Accepted at Medium robustness for this programme; Automatic flight envelope protection upgrade to High robustness tracked as corrective action CA-2026-041, due 2026-06-15. |
| Emergency response | ERP v2.3 activated for the duration of the programme; SAPS and EMS notified |
| Dossier SHA-256 | 7a3f4c8b9e2d1f56a8b4c7e3d0f2a1b6c4e8d3f7a2b9c5e1d8f0a6b3c7e4d2f9 |
| Evidence artefact ID | ev-0f2a1c3b-4e5d-6f7a-8b9c-0d1e2f3a4b5c |
| Storage | Append-only immutable archive, 7-year retention |
| Assessment source | FlightDocket SORA assessment engine v1.0 against JARUS SORA v2.5 (January 2024) |
| Regulatory framework | SACAA CAR/CATS Part 101 (25th/26th Amendment 2023); Part 108 (specific-category pathway); ICAO Annex 19 Safety Management |
The Tenant Approver accepts this SORA dossier internally as complete and correct, before it is submitted to SACAA for Part 108 specific-category authorisation. FlightDocket is advisory. Operator acceptance is not an operational authorisation — the SACAA authorisation, once granted, is the authority to fly.
Tenant Approver name: K. Raath (specimen)
Designation: Accountable Manager / Chief Remote Pilot
Signed at: 2026-04-17T09:14:02Z
Digital signature: sig-0f2a1c3b-4e5d-...
Safety Officer acknowledgement: M. Raath (specimen)
Signed at: 2026-04-17T09:16:41Z