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// TRAINING DOCKET — FULL SYLLABUS
Canadian Military Airworthiness Course Curriculum
Five modules and thirty days of independent professional development, from the Canadian military airworthiness framework and the TAM to type design approval, design standards, continuing airworthiness and foreign military type designs.
BUNDLED COURSE SYLLABUS
| DOC NO. | AW30-PLAN-001 |
| REV | C |
| PAGE | 1 OF 30 |
| PREPARED | AIRWORTHY//30 COURSE CURRICULUM |
// MODULE 01 — DAYS 01–05
The Canadian Military Airworthiness Framework
The legal and institutional bedrock: the Aeronautics Act, the CAR 102.01(a) military carve-out, the Technical Airworthiness Manual, and the authorities who run the CAF's parallel airworthiness system.
- D01
Legal Foundation - The Aeronautics Act and the Military Carve-Out
Why DND runs a parallel airworthiness system: the MND as 'Minister' for defence and the CARs' military carve-out.
Aeronautics Act s. 3(1)(b)CAR 102.01(a)3+10+5 MIN - D02
The Technical Airworthiness Program and the TAM
The five-part TAM structure and the hierarchy of rules, standards, and advisories.
TAM C-05-005-001/AG-001ADSM AG-002DAOD 2015-13+10+5 MIN - D03
The Authorities - TAA, DTAES, OAA, and the Boards
The delegation chain under the Aeronautics Act, the ARB and AAB, and the Flight Test Authority.
TAA (DGAEPM)OAA (1 Cdn Air Div)AETE3+10+5 MIN - D04
Recognized Codes - Civil Standards and Military Codes
How Canada adopts AWM, 14 CFR, and EASA CS alongside military codes in a TAA-approved, fleet-specific certification basis.
MIL-HDBK-516EMACCDEF STAN 00-970AWM3+10+5 MIN - D05
Module Assessment - The CH-148 Cyclone Case
ASSESSMENTCase study: the cost of underestimating a developmental certification.
OAG 2010CH-148 CycloneGATE · 18 MIN
// MODULE 02 — DAYS 06–12
Type Design Approval & Certification in the CAF
The heart of the course. The DND Type Certificate, Type Design Examination, certification-basis construction, and the procedural machinery every CAF certification program runs on.
- D06
The DND Type Certificate and the Military Aircraft Register
The CAF lifecycle: TC, TDE, airworthiness clearances, and Release to Service.
DND Type CertificateAirworthiness ClearanceRelease to Service3+10+5 MIN - D07
Type Design Examination - TAM Part 2, Chapter 5
Assessment of Acceptability and Assessment of Applicability - credit toward a DND Type Certificate, not itself an approval.
TAM Part 2 Ch. 5TDE Levels 1/2/33+10+5 MIN - D08
The Certification Basis and the Certification Plan
Recognized code and/or OCA basic-vehicle basis, military additions, and special conditions.
TAM 2.1.2.R3/S3Special Conditions3+10+5 MIN - D09
Means of Compliance in Military Programs
Analysis, test, inspection, demonstration, similarity - compliance showing under AETE engineering flight test.
MoC CodesAETE Flight TestEFP3+10+5 MIN - D10
Pathways Case Lab - MOTS, Modified, and Developmental
CC-177 off the shelf, CH-147F modified via TDE, CH-148 developmental - and the F-35A with no civil TC.
CC-177 MOTSCH-147FCH-1483+10+5 MIN - D11
Design Changes in Service
Military modifications, contractor certification, and configuration control.
TAM Part 3 Ch. 2Design Change Certification3+10+5 MIN - D12
Module Assessment - Mock TDE Compliance Matrix
ASSESSMENTFull case study: rebuild the certification basis and defend the compliance matrix for a fleet modification gone sideways.
TAM Part 2 Ch. 5TAM 2.1.2.R3MIL-HDBK-516CGATE · 18 MIN
// MODULE 03 — DAYS 13–21
Design Standards & Safety Assessment
The design standards themselves: structures, systems safety, software, and hardware - civil codes adopted as TAA-recognized standards, with the military codes that borrow heavily from them.
- D13
Civil Design Standards as Recognized Codes - Part 23 vs. Part 25
Performance-based small-airplane rules vs. transport-category prescriptivism - civil codes the TAA recognizes.
Part 23 Amdt 64Part 253+10+5 MIN - D14
Flight Requirements - Performance and Flying Qualities
Takeoff/landing performance schedules and stability requirements in the recognized codes.
Section 25.21Section 25.107Section 25.1713+10+5 MIN - D15
Structures - Loads, Fatigue, and Damage Tolerance
Limit/ultimate loads and the damage-tolerance philosophy of Section 25.571.
Section 25.305Section 25.571AC 25.571-1D3+10+5 MIN - D16
Systems Safety Assessment - Section 25.1309 End to End
FHA, PSSA, SSA: probability budgets and severity classifications the military codes inherit.
Section 25.1309AC 25.1309-1AARP4754A3+10+5 MIN - D17
Software and Airborne Electronic Hardware
Design assurance levels, lifecycle data, and certification liaison for SW/AEH.
DO-178CDO-254AC 20-152A3+10+5 MIN - D18
Rotorcraft Standards - Parts 27/29 and ADS-51
How the standards shift for rotorcraft - and the US Army ADS-51 basis behind the CH-147F.
Part 27Part 29ADS-513+10+5 MIN - D19
Engines and Propellers - Parts 33/35
The recognized standards for engines and propellers in a certification basis.
Part 33Part 353+10+5 MIN - D20
Unmanned Aircraft - UAS and the Military RPAS Angle
Airworthiness for unmanned systems under recognized codes and military RPAS operations.
UASMilitary RPAS3+10+5 MIN - D21
Module 3 Capstone - Systems Safety Scenario Review
ASSESSMENTIntegrated scenario: assign DALs and MoCs across a flight-control system.
Section 25.1309Section 25.571DO-178CGATE · 18 MIN
// REGULATION EXCERPT — THE FLAVOR OF THE COURSE
“The airplane systems and associated components, considered separately and in relation to other systems, must be designed so that the occurrence of any failure condition which would prevent the continued safe flight and landing of the airplane is extremely improbable… catastrophic failure conditions must not result from a single failure.”
§ 25.1309(b) — Equipment, Systems, and Installations14 CFR, retained as a TAA-recognized code · As amended by Amendment 25-152 (2024)
→ Day 16: You will map this clause to FHA/SSA DAL allocations
Plain-English — Probability Classes
Per failure-condition class guidance (AC 25.1309-1B), severity is priced in probability per flight hour:
- ≥ 10⁻⁵Probable — anticipated to occur during the life of the fleet
- 10⁻⁵ – 10⁻⁹Improbable — not expected fleet-wide, may occur per airframe
- < 10⁻⁹Extremely improbable — so unlikely they need not be foreseen
// MODULE 04 — DAYS 22–26
Continuing Airworthiness in CAF Service
Airworthiness doesn't end at Release to Service. Maintenance programs, flight authorities, TAA airworthiness directives, and the reviews that keep the CAF fleet airworthy.
- D22
The Continuing Airworthiness Framework - TAM Part 3
Maintenance programs built from ICAs, Airworthiness Limitations, and lifed items - from the Weapon System Manager to the Wing.
TAM Part 3ICAsAWLsECIR3+10+5 MIN - D23
Maintenance Release and People - MRA, ARA, and the MPM
Organizationally assigned authority under a TAA-approved Maintenance Process Manual - no personal mechanic's licence in the CAF.
MRA (ACA/SCA)ARAMPM3+10+5 MIN - D24
Flight Authority and Airworthiness Review - CofA, EFP/SPFP, and the ARB
TAA flight authority, the ARB's annual per-fleet review, and Release to Service.
CofAEFP/SPFPARB Annual Review3+10+5 MIN - D25
TAA Airworthiness Directives and In-Service Monitoring
TAA ADs, foreign AD equivalence, and fleet implementation via special and urgent inspections.
TAA ADs - Part 5 Ch. 6In-Service Monitoring3+10+5 MIN - D26
Aging Aircraft Programs + Module Assessment - ASIMP, MSIP, ESIP
ASSESSMENTStructural life extension and integrity programs: CP-140 ASLEP and the CF-188 IFOSTP.
ASIMPCP-140 ASLEPCF-188 IFOSTPGATE · 18 MIN
// MODULE 05 — DAYS 27–30
Foreign Type Designs & Harmonization
Airworthiness crosses borders. Recognizing foreign military airworthiness authorities, certifying foreign type designs in Canada, and the final synthesis of everything in the docket.
- D27
Recognizing Foreign Military Airworthiness Authorities
USAF TAA, NAVAIR, UK MAA, and the other recognized authorities - and how Canada itself is recognized abroad.
Joint Advisory 2016-04MARQ3+10+5 MIN - D28
Certifying Foreign Military Type Designs in Canada - The Playbook
No civil-style bilateral with the US military: the TDE does the work - credit determination and building the certification basis for a foreign design.
TAM 2.5.1.2Assessment of Acceptability3+10+5 MIN - D29
Case Certification Lab - CH-147F, CC-130J, and CC-177
End-to-end: ADS-51 to TDE to SPFP and Release to Service - sustainment as continued certification.
CH-147FCC-130JCC-177 GSP3+10+5 MIN - D30
Capstone - The Canadian Military Airworthiness Lifecycle
FINAL EXAMOne lifecycle, start to finish - harmonization outlook and the final-exam briefing.
TAM C-05-005-001/AG-001NATO Airworthiness PolicyEMAD-RFINAL · 30 Q
// ASSESSMENT CADENCE
Daily rhythm. Module gates.
Every day runs the same three-phase protocol. Every module closes with an assessment gate. Day 30 closes the docket with the comprehensive final.
spaced-repetition recall of prior days
the regulation, read like an engineer
3 questions — 80% keeps the streak
// ENROLLMENT
Open your docket.
Day 1 unlocks at 06:00 your local time the morning after enrollment.