Platform Qualification Standard (PQS) — Draganfly Heavy Lift · PQS-HL-01, Revision A (Draft)
About this standard. This standard follows the FAA Airman Certification Standards model — task, objective, measurable standard, evaluation — combined with the proficiency coding the Air Force uses in its specialty training standards. One document defines what a qualified Heavy Lift pilot must know and do, to what standard, and how it is evaluated. Everything downstream derives from these tasks: syllabi, lesson plans, exams, practical evaluations, grade sheets, and training records.
Tasks are filed in eight areas, in the order a pilot’s operating handbook uses. Courses teach them in the six-block sequence described on The Training System page.
Document Control
| Document | PQS-HL-01, Rev A (Draft — sample for demonstration) |
| Platform | Draganfly Heavy Lift (octocopter, 30 kg payload class) |
| Source documents | Heavy Lift Operator’s Manual Rev 1.1 (cited as HL) · Herelink ground control station (GCS) Pilot’s Manual Rev 1.2 (cited as GCS) |
| Regulatory basis | 14 CFR Part 107 · FAA-S-ACS-10B (structural model) |
| Owner | Training Standards & Development Lead |
| Change trigger | Any revision to a source document, safety finding, or regulatory change generates a review of every task citing it (Section 7) |
1. Proficiency & Evaluation Codes
| Code | Meaning | Applies |
|---|---|---|
| Knowledge | ||
| K1 | Recall: state facts, limits, and procedures from memory. | Written exam |
| K2 | Apply: interpret system indications and select the correct procedure for a given condition. | Written and oral evaluation |
| Performance | ||
| P1 | Perform the task with instructor guidance. | Training only |
| P2 | Perform the task unassisted, to the stated standard. | Qualification level |
| P3 | Perform, teach, and evaluate the task. | Instructor level (IQS-01) |
| Special flags | ||
| M | Memory item: the initial steps must be performed immediately, correctly, and from memory, before reference to any checklist. | Graded to 100% |
| R | Recurrent item: re-evaluated at each recurrent evaluation. | Proposed 12-month interval |
| Transfer column | ||
| C | Common: carries across Draganfly multirotor platforms. | Credited with differences training |
| PS | Platform-specific. | Retrained and re-evaluated per type |
| Evaluation method | ||
| WE / OE / PE | Written exam · oral evaluation · practical evaluation (flight or hands-on). | Section 5 |
The Transfer column drives the transition-course derivation (Section 6).
| Grade | Meaning |
|---|---|
| U | Unable — task not performed or safety intervention required |
| F | Familiar — performs with instructor assistance; does not meet standard |
| Q | Qualified — performs unassisted to the stated standard; proficiency code P2 |
| QI | Qualified-Instructor — performs to standard while teaching and evaluating; proficiency code P3 |
Qualification requirements (initial): written exam ≥ 85% · all memory items verbatim-correct · all P2 tasks graded Q on a single qualification evaluation by a qualified instructor. (Proposed values — final thresholds set with Manager, Flight Operations.)
2. Critical Knowledge — Memorization Bank
The platform’s boldface: limits and immediate-action values a pilot must produce from memory. Any miss on a memory item fails the written exam regardless of overall score. All values from source manuals as cited.
| # | Item | Value | Ref |
|---|---|---|---|
| M-1 | Maximum takeoff weight | 80 kg | HL 2.2.1 |
| M-2 | Maximum payload weight | 30 kg | HL 2.2.1 |
| M-3 | Primary power minimum voltage | 79.2 V | HL 2.2.2 |
| M-4 | Low battery failsafe | <30% or <43.4 V — persistent warning, no automatic action; pilot returns at discretion | GCS 6.1 |
| M-5 | Critical battery failsafe | <10% or <42.3 V — aircraft enters land mode and lands in place | GCS 6.2 |
| M-6 | Radio-control (RC) failsafe action | Loss of hand-held controller (HHC) control input → return to launch (RTL) with GPS available or land mode (no GPS) | GCS 6.3 |
| M-7 | Loss of command-and-control (C2) link failsafe | Link not re-established within 5 seconds → autonomous RTL, land, disarm | GCS 5.16 |
| M-8 | RTL failsafe limitation | Functions only with GPS lock before takeoff; otherwise forced emergency landing at current location | GCS 5.16 |
| M-9 | Max descent rate (emergency landing) | 2.5 m/s | GCS 5.7 |
| M-10 | Max horizontal velocity at touchdown | 0.2 m/s | GCS 4.6 |
| M-11 | Landing gear auto-extension | Below 5 m above ground level (AGL) | GCS 4.6 |
| M-12 | Max GPS horizontal dilution of precision (HDOP) for launch | 1.7 | GCS App. B |
| M-13 | Compass recalibration triggers | Draganfly ground control software (DGCS) alarm · >500 km from last calibration · incorrect heading · abnormal flight behavior · tip-over/crash/impact | HL 6.2.3 |
| M-14 | Potential Thrust Loss prohibition | No Loiter or automated modes (incl. auto-RTL) while alarm present | GCS 5.4 |
| M-15 | Flight termination irreversibility | Once initiated, cannot be aborted | GCS 5.8 |
| M-16 | Battery max charge current | 30 A | HL 3.2 |
| M-17 | Battery storage / damage temps | Store 20–25 °C; permanent damage above 65 °C | HL 3.3 |
| M-18 | Swollen/damaged battery action | Discontinue, disconnect, isolate outdoors away from combustibles, observe ≥ 15 min | HL 3.1 |
3. Immediate Action Procedures (Memory Items)
Initial steps performed from memory; subsequent steps by reference. Condensed from GCS Manual Section 5.
| # | Condition | Immediate actions (memory) | Ref |
|---|---|---|---|
| IA-1 | Propulsion system failure | Announce “Crash, Crash, Crash” — flight termination inputs to disarm remaining motors — maintain visual line of sight (VLOS) for recovery | GCS 5.1 |
| IA-2 | Potential Thrust Loss alarm | Attitude mode — reduce speed <2 m/s — stop climb — announce “Thrust loss, manual flight” | GCS 5.4 |
| IA-3 | Fire (airborne) | Assess overflight area — announce “Emergency Landing ×3” — execute Emergency Landing (or termination if uncontrollable) | GCS 5.2 |
| IA-4 | Fly away | Announce “Fly Away ×3” — attempt recovery via mode toggles / GCS repositioning — VO records bearing, altitude, velocity, time remaining | GCS 5.5 |
| IA-5 | Compass/magnetometer failure | Attitude mode immediately — announce “Manual flight” — no automated modes | GCS 5.13 |
| IA-6 | Satellite navigation (GNSS) degradation / state-estimator (EKF) failsafe | Verify Attitude mode — stabilize — confirm cause before continuing | GCS 5.14 |
| IA-7 | Loss of C2 link | Attempt link recovery — announce “Comm Loss ×3” — monitor autonomous RTL | GCS 5.16 |
| IA-8 | Erratic/degraded flight | Attitude mode immediately — land if controllable; Emergency Landing if not | GCS 5.18 |
| IA-9 | Forced landing over unsafe area | Override via mode toggle + throttle — reposition in Attitude — land safe | GCS 5.10 |
| IA-10 | Flight termination decision | Attitude — overflight area clear — announce “Terminate ×3” — left stick lower-left 1 s + motor stop (alt: DGCS Disarm + slider) | GCS 5.8 |
4. Qualification Task Table
Area I — System Knowledge & Operating Limitations
| Code | Task | Standard | Prof | Train | Eval | Transfer | R | Ref |
|---|---|---|---|---|---|---|---|---|
| HL.I.1 | Operating limitations & failsafe values | Recite all Memorization Bank items (M-1–M-18) verbatim | K1 M | Ground | WE/OE | PS | R | Section 2 |
| HL.I.2 | Airframe & propulsion system | Describe octocopter configuration, folding-arm/latch architecture, 8×LiPo power system, motor/prop layout | K1 | Ground | WE | PS | HL 2.1–2.2 | |
| HL.I.3 | Avionics, sensors & redundancy | Describe redundant baro/accel/gyro suite, GPS, rangefinder, camera placement; state which failures have no cockpit indication | K2 | Ground | WE/OE | PS | HL 2.1, GCS 5.17 | |
| HL.I.4 | Flight modes & control logic | Explain Attitude vs. Loiter vs. Auto/Guided/RTL behavior, incl. wind-drift in Attitude and GPS dependence of automated modes | K2 | Ground | WE/OE | C | R | GCS 3.3, 5.13–5.14 |
| HL.I.5 | Failsafe hierarchy | Given a scenario, predict automatic behavior (low/critical battery, RC, EKF, C2 loss, geofence) | K2 | Ground | WE/OE | C | R | GCS 6.1–6.5 |
| HL.I.6 | Procedural terminology | Apply must/shall/should/may and Warning/Caution/Note conventions | K1 | Ground | WE | C | HL 1.1 |
Area II — Abnormal & Emergency Procedures
| Code | Task | Standard | Prof | Train | Eval | Transfer | R | Ref |
|---|---|---|---|---|---|---|---|---|
| HL.II.1 | Immediate action procedures | Recite and correctly initiate IA-1–IA-10 from memory; follow-on steps by reference | K1/P2 M | Ground/Flight | WE/OE/PE | C | R | Section 3 |
| HL.II.2 | Emergency landing | Area selection with VO, callout ×3, Attitude, descent ≤2.5 m/s, post-landing actions, ops suspension | P2 | Flight | PE | C | R | GCS 5.7 |
| HL.II.3 | Mission abort | Recognize abort conditions; execute abort/pause/recover sequence | K2/P2 | Flight | PE | C | R | GCS 5.9 |
| HL.II.4 | Sensor degradation management | Disposition baro drift/EKF lane switch (>3 in 30 s → abort), rangefinder failure, visual-aid loss | K2 | Ground/Sim | OE | C | R | GCS 5.6, 5.12, 5.15 |
| HL.II.5 | Post-crash procedure | E-stop/disarm, injury triage priority, documentation, battery quarantine, no-power-on rule, log recovery, reporting | K2/P2 | Ground | OE/PE | C | R | GCS 5.19 |
| HL.II.6 | Object strike / structural failure | State that structural failures present no alarm; select correct response path | K2 | Ground | WE/OE | C | R | GCS 5.17, 5.20 |
| HL.II.7 | Pilot incapacitation (visual observer task) | As visual observer (VO): command RTL via DGCS, manage medical response, complete reporting | P2 | Field | PE | C | R | GCS 5.21 |
Area III — Batteries & Ground Safety
| Code | Task | Standard | Prof | Train | Eval | Transfer | R | Ref |
|---|---|---|---|---|---|---|---|---|
| HL.III.1 | Lithium-polymer (LiPo) hazard knowledge | State ignition conditions, gas hazards, re-ignition behavior, and the ≥15-minute quarantine rule | K1 M | Ground | WE | C | R | HL 3.1, GCS 5.3 |
| HL.III.2 | Charging operations | Charge a battery group: correct grouping by state of charge, ≤30 A, attended, flame-retardant area | P2 | Ground | PE | PS | HL 3.2 | |
| HL.III.3 | Storage & transport | Prepare batteries for storage/shipment: storage charge, 20–25 °C, UN3480 Class 9 / UN 38.3 documentation | K2/P2 | Ground | OE/PE | PS | HL 3.3, 2.2.3 | |
| HL.III.4 | Battery fire response | Execute battery-fire response: upwind, CO₂ + sand, EMS contact, SDS reference | K2 M | Ground | OE | C | R | GCS 5.3 |
| HL.III.5 | Rotor/ground hazard discipline | Personnel positioning, “Clear” discipline, never approach before disarm confirmed | P2 | Field | PE | C | R | HL 1.2, GCS 4.5–4.6 |
Area IV — Assembly, Inspection & Servicing Awareness
| Code | Task | Standard | Prof | Train | Eval | Transfer | R | Ref |
|---|---|---|---|---|---|---|---|---|
| HL.IV.1 | Case removal & assembly | With one assistant: gear receivers latched, arms extended with security latches engaged, zero dropped-aircraft events | P2 | Field | PE | PS | HL 2.3 | |
| HL.IV.2 | Pack-away & transport prep | Fold, case, and secure aircraft and components per procedure | P2 | Field | PE | PS | HL 2.4 | |
| HL.IV.3 | Propeller check | 3-point check (rock, edge feel, twist); correct pass/fail disposition per stated criteria | P2 | Field | PE | PS | R | HL 6.2.1 |
| HL.IV.4 | Visual inspection | Structural inspection: fasteners, dome seating, latch engagement, carbon-fiber condition | P2 | Field | PE | PS | R | HL 6.2.2 |
| HL.IV.5 | Compass calibration | State the five triggers (M-13); perform calibration via DGCS Vehicle Setup | K1/P2 | Field | OE/PE | C | HL 6.2.3, GCS 4.8 | |
| HL.IV.6 | Scheduled maintenance awareness | State inspection tiers and which items require factory-trained personnel | K1 | Ground | WE | PS | HL 6.1 | |
| HL.IV.7 | Data log backup | Download and archive flight logs; state the 10-log support submission after abnormal occurrence | P2 | Field | PE | C | HL 6.2.4, 6.1.6 |
Area V — Mission Planning & Regulatory Compliance
| Code | Task | Standard | Prof | Train | Eval | Transfer | R | Ref |
|---|---|---|---|---|---|---|---|---|
| HL.V.1 | Site survey | Complete Site Survey Template with zero blank fields: airspace, aerodrome data, obstacles, radio/electromagnetic interference (RFI/EMI) sources, hazards, notices to air missions (NOTAMs), emergency medical services (EMS) info | P2 | Ground/Field | PE | C | R | GCS App. D |
| HL.V.2 | Part 107 application | Apply Part 107 to the planned operation (airspace authorization, VLOS, weather minimums, waiver provisions) | K2 | Ground | WE/OE | C | R | 14 CFR 107; ACS-10B |
| HL.V.3 | Weather & environmental limits | Evaluate conditions vs. platform limits (precipitation, icing, RFI/EMI) and make a correct go/no-go call | K2 | Ground | OE | C | R | HL 1.2.2 |
| HL.V.4 | Automated flight plan construction | Build, save, brief a DGCS mission: waypoints, altitudes, speeds, camera, mission end, RTL altitude, geofence, ceiling | P2 | Ground | PE | C | GCS 1.4 | |
| HL.V.5 | Crew brief | Deliver brief covering mission, roles, callouts, emergency plan, abort criteria | P2 | Field | PE | C | R | GCS 4.1 |
| HL.V.6 | Pre-flight documentation | Complete Appendix A incl. RTL altitude, geofence, ceiling entries; authority documentation on hand | P2 | Field | PE | C | R | GCS App. A |
Area VI — Normal Procedures
| Code | Task | Standard | Prof | Train | Eval | Transfer | R | Ref |
|---|---|---|---|---|---|---|---|---|
| HL.VI.1 | Initialization & connection | Power sequence, DGCS launch, heading verification vs. true, AHRS response check | P2 | Field | PE | C | R | GCS 4.2 |
| HL.VI.2 | Pre-takeoff checks | Complete Appendix B: avionics, payload, motor response, antennas, props, latches, HDOP <1.7 | P2 | Field | PE | PS | R | GCS App. B |
| HL.VI.3 | Manual takeoff & hover | Arm with callouts, 3-s spool, stable hover; control response all axes; alt ±1 m, position ±2 m (proposed) | P2 | Flight | PE | C | R | GCS 4.3 |
| HL.VI.4 | Manual flight maneuvering | Commanded headings/altitudes/patterns in Attitude and Loiter; wind-drift anticipation | P2 | Flight | PE | C | R | GCS 3.3 |
| HL.VI.5 | Automated mission launch & monitoring | Launch with callouts; monitor; ready to assume manual control at all times | P2 | Flight | PE | C | R | GCS 4.4 |
| HL.VI.6 | Commanded RTL | Path/landing-zone assessment with VO, announce, confirm slider, monitor descent, confirm disarm, “Clear” | P2 | Flight | PE | C | R | GCS 4.5 |
| HL.VI.7 | Manual landing | Stable position, gear check <5 m, no visible drift at touchdown, within the target landing location, straight-back throttle, 3-s disarm hold, “Clear” after prop stop | P2 | Flight | PE | C | R | GCS 4.6, 3.4 |
| HL.VI.8 | Shutdown & post-flight | Shutdown sequence and Appendix C: inspection, logbook, log backup, regulatory reporting | P2 | Field | PE | C | R | GCS 4.7, App. C |
Area VII — Automated & Payload Operations
| Code | Task | Standard | Prof | Train | Eval | Transfer | R | Ref |
|---|---|---|---|---|---|---|---|---|
| HL.VII.1 | Survey pattern missions | Configure and fly survey/transect with correct pattern, overlap, camera settings | P2 | Flight | PE | C | GCS 1.4.23–24 | |
| HL.VII.2 | Guided-mode operations | Guided repositioning and ROI pointing | P2 | Flight | PE | C | GCS 1.4.25–27 | |
| HL.VII.3 | Payload installation & verification | Install per class procedure; verify security, power, function, weight and balance within M-1/M-2 | P2 | Field | PE | PS | R | HL 4.1–4.3 |
| HL.VII.4 | Alarm & message interpretation | Given DGCS alarms, state meaning and required response | K2 | Ground | WE/OE | C | R | GCS 2 |
Area VIII — Crew Coordination & Communication
| Code | Task | Standard | Prof | Train | Eval | Transfer | R | Ref |
|---|---|---|---|---|---|---|---|---|
| HL.VIII.1 | Standard callouts | Use all prescribed callouts without omission during evaluation | P2 | Flight | PE | C | R | GCS 4–5 |
| HL.VIII.2 | Pilot-in-command (PIC) / VO duty split | Correct task allocation during normal and emergency sequences | P2 | Flight | PE | C | R | GCS 4–5 |
5. Evaluation Construction Rules
- Written exam — drawn only from K-coded tasks; every M item on every version; ≥85% with zero M-item misses (proposed).
- Oral evaluation — scenario-based from K2 tasks; same session as practical.
- Practical evaluation — every P2 task graded; U or F on any M-flagged or emergency-procedure task (Area II) fails qualification; up to two F on non-critical tasks may be retrained and re-evaluated within 7 days without full re-evaluation (proposed).
- Evaluator — any pilot holding QI on this platform under IQS-01 and current per the instructor standardization program.
6. Program Derivations — How One Standard Becomes Six Programs
| Program | Rule applied to this standard |
|---|---|
| Initial | Every task in this standard, to the stated proficiency. |
| Recurrent | Tasks flagged R, plus the full memorization bank and the IA bank, at the recurrent interval. |
| Transition | Tasks marked C in the Transfer column are credited with differences training; tasks marked PS are retrained and re-evaluated against the gaining platform’s standard. |
| Mission-specific | This standard plus an added task block for the tasking. |
| Customer | This standard scoped to the customer’s requirements and mission-specific tasks. |
| Instructor | P3 proficiency on designated tasks, plus the teaching and evaluating tasks in IQS-01. |
7. Change Control
Each row carries a source reference. A manual revision, safety finding, or regulatory change triggers: (1) identify affected tasks by reference; (2) revise those tasks, republish at next revision letter; (3) regenerate affected lesson plans, exam items, and checklists; (4) disposition currently-qualified pilots (bulletin / differences training / re-evaluation) with an effectivity date. Records retain the PQS revision in effect at each evaluation, preserving the audit chain: grade sheet → PQS revision → manual revision.