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Class 2 microlight aircraft in this Subpart includes a Class 1 microlight helicopter.
(a) The requirements of rule 91.101(a)(1)(i) do not apply to a person operating a microlight aircraft.
(b) A person must not fly a Class 2 microlight aircraft unless there is in force for the aircraft, a flight permit or a temporary flight permit issued in accordance with this Part.
Each applicant for a flight permit for a Class 2 microlight aircraft must submit the information required by rule 103.207 to the Director with a payment of the appropriate fee prescribed by regulations made under the Act.
(a) The Director may issue a microlight flight permit in accordance with section 75 of the Act for a Class 2 microlight aircraft if—
(1) the applicant for the flight permit provides documented evidence that—
(i) a microlight flight permit, or equivalent document acceptable to the Director, has been issued for the type by the competent authority of an ICAO Contracting State; or
(ii) the aircraft conforms to a type design that complies with 1 of the following standards:
(A) British Civil Airworthiness Requirements Section S (CAP 482 dated March 1983 and amended October 1988) issued by the Civil Aviation Authority of the United Kingdom:
(B) Civil Aviation Orders 95.32 (Issue 1 dated 28 February 1990 and Amendment 57 dated 1 August 1990) and 101.55 (Issue 1 dated 7 January 1988 and amendment 90 dated 28 August 1991) issued by the Civil Aviation Safety Authority of Australia:
(C) Document TP10141E issued by Transport Canada:
(D) any other equivalent standard acceptable to the Director; or
(iii) 6 or more aircraft of the type have been operated and the aircraft type has achieved a documented satisfactory airworthiness history of at least 150 hours of flight including at least 50 hours of flight on one aircraft; or
(iv) a temporary flight permit has been issued for the aircraft under paragraph (b) and the aircraft has completed an endurance test in accordance with rule 103.211; and
(2) the applicant provides—
(i) satisfactory evidence that the aircraft complies with every applicable requirement prescribed under Parts 47, 91, and 103; and
(ii) a statement of hours flown by the aircraft both in total and since any previous flight permit or equivalent document was issued; and
(iii) a statement that any inspection, replacement, overhaul, or other maintenance of the microlight aircraft or its engine or engine components that is considered mandatory by the manufacturer has been complied with; and
(3) the aircraft has been inspected by a person authorised by the Director and that person has certified in the applicable aircraft maintenance record required by rule 91.617 that the aircraft has no hazardous design features.
(b) The Director may issue a temporary microlight flight permit for a New Zealand designed and manufactured prototype Class 2 microlight aircraft that does not comply with the requirements in paragraphs (a)(1)(i), (ii), or (iii) if the prototype aircraft has passed a wing static limit load test and a landing gear drop test in accordance with British Civil Airworthiness Requirements Section ‘S’.
(c) A temporary microlight flight permit issued under paragraph (b) must—
(1) contain operating limitations that the Director considers necessary in the interests of aviation safety; and
(2) not be issued for a period of more than 6 months.
(d) The pilot of a Class 2 microlight aircraft that is operated under the authority of a temporary microlight flight permit must comply with the operating limitations contained in the temporary flight permit.
(e) A microlight flight permit remains in force until it expires or it is suspended or revoked.
Where a Class 2 microlight is modified in any manner that may affect the airworthiness of the aircraft, the operator must ensure that the aircraft is reinspected and reassessed for compliance with rule 103.207 before further flight.
(a) An endurance test for a microlight aircraft must consist of—
(1) for aircraft constructed from drawings and raw materials, 40 hours of flight; or
(2) for series aircraft constructed from a kitset of raw materials, 25 hours of flight; or
(3) for series aircraft constructed from a kitset of prefabricated components, 10 hours of flight; or
(4) for series aircraft constructed entirely from pre-manufactured factory components and assemblies, 2 hours of flight.
(b) The endurance test must be restarted after any modification is made or defect occurs.
A pilot-in-command of a microlight aircraft who completes the endurance testing in accordance with rule 103.211, must enter in the applicable maintenance record required by rule 91.617—
(1) details of every manoeuvre completed during the testing together with details of the demonstrated flight speeds; and
(2) the following statement (which must include the flight time hours completed) followed by the pilot’s name, licence or certificate number, signature and the date of the final test:
I certify that this aircraft has satisfactorily completed …… hours flight time in compliance with Part 103 and the aircraft has adequate performance, is controllable through its normal range of speeds and throughout all manoeuvres completed, and is airworthy.
(a) An operator of a microlight aircraft must ensure that—
(1) the aircraft is maintained in an airworthy condition; and
(2) every applicable airworthiness directive is complied with as required by Part 39; and
(3) between required inspections, every defect is rectified.
(b) An operator of a microlight aircraft that meets a type design standard specified in rule 103.207(a)(1), must ensure that the aircraft is maintained in accordance with the designer or kitset manufacturer maintenance requirements.
(c) Subject to paragraphs (d) and (g), a person must not operate a microlight aircraft unless—
(1) an annual inspection of the condition of the aircraft has been carried out within the preceding 12 months; and
(2) paragraph (a)(2) is complied with; and
(3) any applicable tests and inspections required under the following rules have been complied with:
(i) rule 91.605(e)(2) regarding test and inspection of automatic pressure altitude reporting system if the microlight aircraft is equipped with a surveillance transponder:
(ii) rule 91.605(e)(3) if the microlight aircraft is equipped with a surveillance transponder:
(iii) rule 91.605(e)(8) if the microlight aircraft is equipped with flotation equipment.
(d) The annual condition inspection required by paragraph (c)(1) must be—
(1) performed by—
(i) a person authorised by a microlight organisation to perform annual condition inspections; or
(ii) the Director; or
(iii) a person who holds a current aircraft maintenance engineer licence with appropriate aircraft and engine group ratings issued under Part 66; and
(2) acceptable to the Director with regard to the items and components inspected.
(e) The person who performs the annual condition inspection required by paragraph (c)(1) must, if the person finds the aircraft to be in an airworthy condition,—
(1) certify in an inspection form that the aircraft is airworthy; and
(2) permanently affix the inspection form required under paragraph (e)(1) to the aircraft in a prominent place adjacent to the point of entry; and
(3) retain a copy of the inspection form required under paragraph (e)(1) as a record of the certification; and
(4) for a class 2 microlight aircraft, enter the details of the certification in the applicable maintenance record required under rule 91.617.
(f) The aircraft inspection form required under paragraph (e)(1) must include the—
(1) aircraft registration markings; and
(2) aircraft type; and
(3) due date for the next annual condition inspection; and
(4) date, signature, and licence or certificate number of the engineer or inspector who carried out the annual condition inspection.
(g) If the annual condition inspection that is required under paragraph(c)(1) shows that the aircraft is not airworthy, the operator of the aircraft must not permit the aircraft to be flown until it has been reinspected and certified as airworthy under paragraphs (d), (e), and (f).
A person is not required to comply with Part 148 if they are constructing a microlight aircraft—
(1) from drawings and raw materials; or
(2) from a kitset of raw materials; or
(3) from a kitset of prefabricated components; or
(4) from pre-manufactured factory components and assemblies.
(a) Subject to paragraph (b), each operator of a microlight aircraft must equip the aircraft with—
(1) instruments and equipment required—
(i) to conform with the aircraft type design; and
(ii) by the aircraft designer or kit manufacturer; and
(2) the means of indicating—
(i) airspeed; and
(ii) altitude in feet; and
(iii) magnetic heading.
(b) The operator of a powered parachute is not required to equip the aircraft with a means of indicating airspeed.
(c) The following requirements in Part 91, Subpart F do not apply to a person operating a microlight aircraft—
(1) rule 91.501(1), in respect of the minimum instruments and equipment required by rule 91.509; and
(2) rule 91.501(2)(i), in respect of the seating standards specified in Appendix A, A.3.
Each person operating a microlight aircraft towing a hang glider in flight must, in addition to rule 103.221, ensure that—
(1) the aircraft is equipped with—
(i) a towing installation enabling the tow pilot to release the tow rope at any time, comprising a tow hook and attachment assembly which meets the aircraft’s design standard; and
(ii) a rear vision mirror; and
(iii) a tow line, which has a weak link incorporated at the tow plane end, with a breaking strength of not more than 100 kg; and
(2) the hang glider is equipped with a quick release mechanism for hang glider pilot activation with a simple and positive releasing action with tow rope loads of up to 100 kg rearward from the tow hook within a cone of 45 degrees upwards, 30 degrees downwards, and 30 degrees sideways.
