DGCA CAR-66 · MODULE 10 · Syllabus 10.9 · 10.5 · 10.7

Chapter 11: National Airworthiness Requirements (CAR Section 2)

A guided tour of the CAR Section 2 series that DGCA papers love — weight and balance, log books, flight testing, taxy permits, medical kits, flammability, fuelling, flight recorders, GPWS, ACAS, transponders, age of imported aircraft and the light-aircraft CARs (gliders, microlights, balloons, gyroplanes, powered hang gliders).

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🎬 Explainer video

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🎯 What you'll learn
  • Series X — weight and balance (Part II), medical supplies (III), flammability (IV), log books (VI), taxy permit (VIII)
  • Series T Part II — when a test flight is required
  • Series H — fuelling procedures and aviation fuel at airports
  • Series I — flight data recorders, cockpit voice recorders, GPWS and ACAS
  • Series R — communication/navigation installations and transponders
  • Series F Part XX — age limits for imported aircraft
  • Light aircraft CARs — gliders, microlights, balloons, gyroplanes and powered hang gliders
📖 The lesson

Why this chapter exists

Besides the big “named” CARs, CAR Section 2 contains dozens of short Series/Part CARs. DGCA Module 10 papers regularly draw questions from them — especially Series X. The syllabus table allots 3 questions (B categories) to this national-requirements area. Here are the numbers that matter.

Weight and balance — Series X Part II

  • Implements Rule 58: every aircraft is weighed and its CG determined.
  • Aircraft of more than 2 000 kg MTOW are re-weighed every five years; those of 2 000 kg or less need no routine re-weighing.
  • Re-weighing is also required after a major repair, major alteration or major change to the interior arrangement that cannot be computed accurately — DGCA's decision is final — and whenever DGCA requires.
  • The Regional Airworthiness Office may grant an ad-hoc extension of the weighing period of up to 3 months.
  • The weight schedule is prepared by a person approved by DGCA (or by the compliance monitoring manager of an approved organisation); a copy is displayed in a prominent place or carried on board, easily accessible.
  • Empty weight excludes removable equipment and disposable load but includes fixed equipment and items like fixed ballast, hydraulic fluid and unusable fuel and oil.

Log books — Series X Part VI

Implements Rule 67 (journey, aircraft, engine, variable-pitch propeller and radio log books). Entries are made in ink or indelible pencil, signed and dated by the appropriately licensed AME or approved/authorised person, with the licence/approval number beneath the signature.

RecordPreservation
Aircraft log bookUntil the aircraft is permanently withdrawn and its C of R cancelled
Engine and propeller log booksUntil the engine/propeller is permanently withdrawn from use
After an accident with damage beyond economic repairAircraft, engine and propeller log books kept 2 years after the accident
Journey log book / technical log / Flight Report Book36 months after the last entry
Other log books3 years from the last entry

If log books are not kept as prescribed, the aircraft is deemed not to be maintained in an airworthy condition.

Taxy permit — Series X Part VIII

Engine starting and ground manoeuvring by untrained people can damage aircraft, so only qualified, approved engineering personnel may taxi:

  • Issued by the operator's Quality Manager.
  • The holder must have a valid, type-rated CAR-66 B1 licence for the specific aircraft/engine combination, be trained in taxying, and have his taxying ability assessed by a pilot of the operator qualified on type.
  • Qualified to use the radiotelephone — otherwise the permit is endorsed to be accompanied by an RT licence holder.
  • Conversant with the aerodrome layout, signs, markings, lighting, ATC phraseology and signals.

Flight testing — Series T Part II

A test flight checks that flight characteristics have not deteriorated, performance is as scheduled and equipment works. It is required:

  1. after a major inspection as specified by the manufacturer (scheduled airlines with an approved performance-monitoring system need not test each aircraft for the ARC — the Continuing Airworthiness Manager certifies continuous monitoring instead);
  2. at issue/extension of the ARC for aircraft other than scheduled airline aircraft if the ARC has expired or the aircraft has not flown in the 15 days before ARC expiry;
  3. after maintenance, repair or modification that affects flight characteristics;
  4. to evaluate fuel consumption, engine power, radio/radar/navigation or instruments that cannot be checked on the ground;
  5. after an engine change — on a twin, it may be waived where an approved engine ground-test procedure exists, but not if both engines are changed.

Before the flight, authorised certifying staff issue a certificate that the aircraft is fit for the test flight (in duplicate); the flight test report and adjustments are recorded.

Medical supplies and flammability — Series X Parts III and IV

  • Part III: first-aid kits (for injuries in flight or minor accidents), a medical kit of life-saving drugs to be used only by a qualified medical practitioner, and a universal precaution kit. Scheduled airlines on international flights longer than 2 hours carry an AED.
  • Part IV: flammability requirements for furnishing materials in every crew, passenger, cargo and baggage compartment (self-extinguishing, burn-test standards).

Fuel — Series H

  • Part II — fuelling procedures: fuelling under supervision of a person nominated by the operator, by authorised oil-company staff; approved vehicles/installations only; no leaking equipment; fuelling zone extends 6 m radially from fuelling points, vents and equipment; efficient bonding between aircraft and fuel source, and earthing through apron earthing points. (Rule 25A distances: 15 m from buildings, 30 m no ignition sources.)
  • Part III — aviation fuel at airports: storage, handling and quality control of fuel.
  • Organisations supplying fuel are approved under Series E Part VI (Chapter 5).

Instruments and recorders — Series I

CARKey requirement
I Part IIInstruments and equipment for flying training organisations and aerial work
I Part V — FDRFDRs retain at least the last 25 hours of operation (with specified exceptions); carriage depends on MTOM (e.g. above 5 700 kg, above 27 000 kg) and C of A date; periodic read-out and checks of recorder serviceability
I Part VI — CVRAeroplanes over 27 000 kg with first C of A on or after 1 Jan 2022: CVR retains the last 25 hours; cockpit audio recording systems (CARS) required from 1 Jan 2025 retain at least the last 2 hours; turbine aeroplanes of 2 250–5 700 kg operated by more than one pilot need a CVR or CARS
I Part VII — GPWSAll turbine aeroplanes above 5 700 kg or authorised for more than 9 passengers: GPWS with a forward-looking terrain avoidance function; terrain/obstacle database kept current
I Part VIII — ACASCAT turbine aeroplanes above 15 000 kg, or more than 30 passengers, or payload above 3 tonnes: ACAS II (TCAS II v7.1 is equivalent). ACAS I gives traffic advisories only; ACAS II adds vertical resolution advisories

Radio — Series R

  • Part II — installation of communication, navigation and radar equipment (approved type, approved installation, kept serviceable — Rule 57).
  • Part IV — Mode A/C and Mode S transponders. Mode S allows discrete (selective) interrogation of each aircraft via its unique address and a data link, and supports ACAS II resolution advisories.

Age of imported aircraft — Series F Part XX

AircraftImport limit
Pressurised, passenger (scheduled/non-scheduled) or GANot completed 20 years or 65% of design economic life in pressurisation cycles, whichever is earlier. If older than 18 years, it must have flown at least 100 hours in the last 6 months (unless major maintenance with a satisfactory test flight in that period)
UnpressurisedCase by case; flown 50 hours in the last 6 months; normally not more than 25 years old
CargoNot completed 25 years or 75% of design economic life in pressurisation cycles

Rationale: manufacturers typically set a design economic life around 20 years or 60 000 landings/pressurisation cycles; beyond it corrosion and fatigue in inaccessible areas become a concern. Local acquisition of Indian-registered aircraft maintained to DGCA procedures is exempt.

Light aircraft CARs

CARAircraftKey facts
F Part XIIIGlidersAirworthiness requirements for gliders
F Part XIVMicrolightSingle-seat: AUW ≤ 330 kg; two-seat: AUW ≤ 450 kg; wing area ≥ 10 m²
F Part XVHot air balloonsManufacture, registration and airworthiness control
F Part XXIVGyroplanesLight gyroplanes: ≤ 2 occupants, AUW ≤ 600 kg, day VFR only; a gyroplane has a non-power-driven rotor in forward flight
O Part VIPowered hang glidersManufacture, registration and operation

These aircraft are certified by category L, A, B1 or B3 licence holders or authorised persons (66.A.100) and generally hold a special C of A (Series F Part XXIII).

Chapter summary

  • W&B: > 2 000 kg re-weigh every 5 years (+3 months extension); after major repair/alteration; weight schedule displayed.
  • Log books: ink/indelible pencil + licence number; journey/tech log 36 months; others 3 years; accident write-off 2 years.
  • Taxy permit: Quality Manager issues to type-rated B1, trained and pilot-assessed, RT-qualified.
  • Test flight: after major inspection, ARC expired / not flown 15 days (non-airline), flight-affecting maintenance, engine change.
  • FDR 25 h; CVR 25 h (> 27 t, C of A ≥ 2022); CARS 2 h; GPWS > 5 700 kg or > 9 pax; ACAS II > 15 t or > 30 pax.
  • Import age: pressurised pax 20 yrs / 65%; cargo 25 yrs / 75%; unpressurised normally ≤ 25 yrs.
  • Microlight 330/450 kg; light gyroplane 600 kg, 2 occupants, day VFR.
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