The Civil Aviation (Operation of Aircraft-General Aviation Aeroplanes) Regulations, 2018

Section 1. Citation. Section These Regulations may be cited as the Civil Aviation (Operation of Aircraft—General Aviation—Aeroplanes) Regulations.

Section 2. Interpretation. Section unlawful seizure of aircraft in flight;

Section 3. Applicability. Section These Regulations shall be applicable to general aviation operations with aeroplanes as described in Part II and Part III.

Section 4. Compliance with laws, regulations and procedures. Section comply with the Kenyan laws, regulations, and procedures;

Section 5. Dangerous goods. Section 5(1)(a) the Authority has granted to the operator a dangerous goods permit, subject to such conditions as the Authority finds it fit, to carry dangerous goods on board its aeroplane; and Section 5(1)(b) the provisions approved by the Authority and any conditions to which such approval may be subject; and Section 5(1)(b)(i) the provisions approved by the Authority and any conditions to which such approval may be subject; and Section 5(1)(b)(ii) in accordance with the Technical Instructions for the Safe Transport of Dangerous Goods by Air approved and published by the Authority in compliance with the decisions of the Council of the International Civil Aviation Organisation for the time being in force. Section 5(2)(a) be submitted to the Authority for consideration before the proposed date of shipment; and Section 5(2)(b) contain the information required by the Authority and the duly completed dangerous goods transport document at the time the application is made. Section 5(3) The Authority may issue a dangerous goods permit for the carriage of dangerous goods on a single return flight (ad hoc permit) or on more than 10 return flights over a period...

Section 6. Use of psychoactive substances. Section 6(1) A member of a flight crew shall not perform any function specified in the privileges applicable to his licence if he is under the influence of any psychoactive substance which may render him unable to perform such functions in a safe and proper manner. Section 6(2) Safety-sensitive personnel shall not undertake any function while under the influence of any psychoactive substance, by reason of which human performance is impaired.

Section 7. Specific approvals.

Section 8. Operating facilities. Section The pilot-in-command shall ensure that a flight will not be commenced unless it has been ascertained by every reasonable means available that the ground or water facilities including communication facilities and navigation aids available and directly required for such flight, for the safe operation of the aeroplane, are adequate for the type of operation under which the flight is to be conducted.

Section 9. Operational management. Section 9(1)(a) has been duly authorized by the owner or in the case where it is leased the lessee, or a designated agent; Section 9(1)(b) is fully competent to taxi the aeroplane; Section 9(1)(c) is qualified to use the radio if radio communications are required; and Section 9(1)(d) has received instructions from a competent person with respect of aerodrome layout, and where appropriate, information on routes, signs, marking, lights, ATC signals and instructions, phraseology and procedures, and is able to conform to the operational standards required for safe aeroplane movement at the aerodrome. Section 9(2) The pilot-in-command shall establish aerodrome operating minima in accordance with criteria specified by the Authority, for each aerodrome to be used in operations. Such minima shall not be lower than any that may be established for such aerodromes by the State of the Aerodrome, except when specifically approved by that State. Section 9(3) The Authority may approve operational credit(s) for operations with aeroplanes equipped with automatic landing systems, a HUD or equivalent displays, EVS, SVS or CVS. Such approvals shall not affect the cla...

Section 10. Flight preparation. Section 10(1)(a) the aeroplane is airworthy, duly registered and that appropriate certificates with respect thereto are aboard the aeroplane; Section 10(1)(b) the instruments and equipment installed in the aeroplane are appropriate, taking into account the expected flight conditions; Section 10(1)(c) any necessary maintenance has been performed in accordance with Regulations 39, 40, and 41; Section 10(1)(d) the mass of the aeroplane and centre of gravity location are such that the flight can be conducted safely, taking into account the flight conditions expected; Section 10(1)(e) any load carried is properly distributed and safely secured; and Section 10(1)(f) the aeroplane operating limitations, contained in the flight manual, or its equivalent, will not be exceeded. Section 10(2) The pilot-in-command should have sufficient information on climb performance with all engines operating to enable determination of the climb gradient that can be achieved during the departure phase for the existing take-off conditions and intended take-off technique. Section 10(3)(a) a study of available current weather reports and forecasts; and Section 10(3)(b) the plann...

Section 11. In-flight procedures. Section 11(1) A flight shall not be continued towards the aerodrome of intended landing, unless the latest available information indicates that at the expected time of arrival, a landing can be effected at that aerodrome or at least one destination alternate aerodrome, in compliance with the operating minima established in regulation (9) (2). Section 11(2) An instrument approach shall not be continued below 300 m (1 000 ft) above the aerodrome elevation or into the final approach segment unless the reported visibility or controlling RVR is at or above the aerodrome operating minimum. Section 11(3) If, after entering the final approach segment or after descending below 300 m (1 000 ft) above the aerodrome elevation, the reported visibility or controlling RVR falls below the specified minimum, the approach may be continued to DA/H or MDA/H. In any case, an aeroplane shall not continue its approach-to-land beyond a point at which the limits of the aerodrome operating minima would be infringed. Section 11(4) When weather conditions likely to affect the safety of other aircraft are encountered, they shall be reported as soon as possible. Section 11(5) H...

Section 12. Duties of pilot-in-command. Section 12(1) The pilot-in-command shall be responsible for the operation, safety and security of the aeroplane and the safety of all crew members, passengers and cargo on board. Section 12(2)(a) shall not be commenced if any flight crew member is incapacitated from performing duties by any cause such as injury, sickness, fatigue, the effects of any psychoactive substance; and Section 12(2)(b) shall not be continued beyond the nearest suitable aerodrome when flight crew members' capacity to perform functions is significantly reduced by impairment of faculties from causes such as fatigue, sickness or lack of oxygen. Section 12(3) The pilot-in-command shall be responsible for notifying the nearest appropriate authority by the quickest available means of any accident involving the aeroplane, resulting in serious injury or death of any person or substantial damage to the aeroplane or property.

Section 13. Cabin baggage (take-off and landing) Section The pilot-in-command shall ensure that all baggage carried onto an aeroplane and taken into the passenger cabin is securely stowed.

Section 14. Aeroplane perfomance operating limitations. Section 14(1)(a) in compliance with the terms of its airworthiness certificate or equivalent approved document; Section 14(1)(b) within the operating limitations prescribed by the Authority; and Section 14(1)(c) if applicable, within the mass limitations imposed by compliance with the applicable noise certificate issued by the Authority, unless otherwise authorised in exceptional circumstances for a certain aerodrome or a runway where there is no noise disturbance problem, by the competent authority of the State in which the aerodrome is situated. Section 14(2) A flight shall not be commenced unless placards, listings, instrument markings, or combinations thereof, containing those operating limitations prescribed by the Authority for visual presentation, are displayed in the aeroplane. Section 14(3) The pilot-in-command shall determine that aeroplane performance will permit the take-off and departure to be carried out safely.

Section 15. Aeroplane instruments, equipment and flight documents. Section In addition to the minimum equipment necessary for the issuance of a certificate of airworthiness, an aeroplane shall not fly unless the instruments, equipment and flight documents prescribed in the regulations hereunder are installed or carried, as appropriate, in aeroplanes according to the aeroplane use and to the circumstances under which the flight is to be conducted. The prescribed instruments and equipment, including their installation, shall be acceptable to the Authority.

Section 16. Aeroplanes on all flights. Section 16(1) An aeroplane shall be equipped with instruments which will enable the flight crew to control the flight path of the aeroplane, carry out any required procedural manoeuvres and observe the operating limitations of the aeroplane in the expected operating conditions. Section 16(2)(a) an accessible first-aid kit; Section 16(2)(b) the pilot's compartment; and Section 16(2)(b)(i) the pilot's compartment; and Section 16(2)(b)(ii) each passenger compartment that is separate from the pilot's compartment and that is not readily accessible to the flight crew; Section 16(2)(c) person over the age of 24 months; and Section 16(2)(c)(i) person over the age of 24 months; and Section 16(2)(c)(ii) seat and restraining belts for each berth; Section 16(2)(d) the flight manual or other documents or information concerning any operating limitations prescribed for the aeroplane by the Authority, required for the application of regulation 15; Section 16(2)(d)(i) the flight manual or other documents or information concerning any operating limitations prescribed for the aeroplane by the Authority, required for the application of regulation 15; Section 16(2...

Section 17. Marking of break-in points. Section Marking for break-in by rescue crews in emergency situations shall conform to the requirements outlined in the Civil Aviation (Aircraft Nationality and Registration Marks) Regulations.

Section 18. All aeroplanes operated as VFR flights. Section magnetic heading;

Section 19. Aeroplanes on flights over water. Section 19(1)(a) one life jacket, or equivalent individual floatation device, for each person on board, stowed in a position readily accessible from the seat or berth; Section 19(1)(b) equipment for making the sound signals prescribed in the International Regulations for Preventing Collisions at Sea, where applicable; Section 19(1)(c) one anchor; and Section 19(1)(d) one sea anchor (drogue), when necessary to assist in maneuvering. Section 19(2)(a) flying en route over water beyond gliding distance from the shore; or Section 19(2)(b) taking off or landing at an aerodrome where, in the opinion of the pilot-in-command, the take-off or approach path is so disposed over water that in the event of a mishap there would be a likelihood of a ditching. Section 19(3) All aeroplanes operated on extended flights over water shall be equipped with, at a minimum, one life jacket or equivalent individual floatation device for each person on board, stowed in a position easily accessible from the seat or berth of the person for whose use it is provided. Section 19(4) The pilot-in-command of an aeroplane operated on an extended flight over water shall det...

Section 20. Aeroplanes on flights over designated land areas. Section Aeroplane, when operated across land areas which have been designated by the Authority concerned as areas in which search and rescue would be especially difficult, shall be equipped with such signaling devices and life-saving equipment (including means of sustaining life) as may be appropriate to the area overflown.

Section 21. Aeroplanes on high altitude flights. Section 21(1) Aeroplanes intended to be operated at high altitudes shall be equipped with oxygen storage and dispensing apparatus capable of storing and dispensing the oxygen supplies required in regulation 9. Section 21(2) Pressurised aeroplanes for which the individual certificate of airworthiness was first issued on or after the 1st January, 1990 shall not be operated at flight altitudes at which the atmospheric pressure is less than 376 hPa unless it is equipped with a device to provide positive warning to the flight crew of any dangerous loss of pressurisation.

Section 22. All aeroplanes operated in accordance with the instrument flight rules. Section magnetic heading (standby compass);

Section 23. Aeroplanes when operated at night. Section the equipment specified in regulation 22;

Section 24. Aeroplanes complying with the noise certification. Section A person shall not operate an aeroplane unless there is carried on board a document attesting noise certification in accordance with the Civil Aviation (Airworthiness) Regulations.

Section 25. Mach number indicator. Section A person shall not operate an aeroplane with speed limitations expressed in terms of Mach number unless the aeroplane is equipped with a means of displaying Mach number.

Section 26. Aeroplanes required to be equipped with Ground Proximity Warning Systems (GPWS). Section 26(1) A person shall not operate a turbine-engined aeroplane of maximum certificated take-off mass in excess of 5 700 kg or authorized to carry more than nine passengers unless the aeroplane is equipped with a ground proximity warning system which has a forward-looking terrain avoidance function. Section 26(2) The ground proximity warning system required in subregulation (1) shall provide automatically a timely and distinctive warning to the flight crew when the aeroplane is in potentially hazardous proximity to the earth’s surface. Section 26(3)(a) excessive descent rate; Section 26(3)(b) excessive altitude loss after take-off or go-around; and Section 26(3)(c) unsafe terrain clearance. Section 26(4)(a) excessive descent rate; Section 26(4)(b) excessive terrain closure rate; Section 26(4)(c) excessive altitude loss after take-off or go-around; Section 26(4)(d) unsafe terrain clearance while not in landing configuration; Section 26(4)(e) gear not locked down; Section 26(4)(f) flaps not in a landing position; and

Section 27. Emergency Locator Transmitter (ELT). Section at least one ELT of any type;

Section 28. Microphones. Section When operating under the instrument flight rules all flight crew members required to be on flight deck duty shall communicate through boom or throat microphones below the transition level or altitude.

Section 29. Aeroplanes required to be equipped with a pressure-altitude reporting transponder. Section 29(1) A person shall not operate an aeroplane unless the aeroplane is equipped with a pressure-altitude reporting transponder which operates in accordance with the Civil Aviation (Instrument and Equipment) Regulations and Civil Aviation (Surveillance and Collision Avoidance Systems) Regulations. Section 29(2) Unless exempted by the Authority, no person shall undertake VFR flights with an aeroplane unless the aeroplane is equipped with a pressure-altitude reporting transponder which operates in accordance with the Civil Aviation (Instrument and Equipment) Regulations and Civil Aviation (Surveillance and Collision Avoidance Systems) Regulations.

Section 30. Aeroplanes equipped with automatic landing systems, a Head-Up Display (HUD) or equivalent displays, Enhanced Vision Systems (EVS), Synthetic Vision Systems (SVS) or Combined Vision Systems (CVS). Section 30(1) The Authority shall establish acriteria for the safe operations of aeroplanes equipped with automatic landing systems, a HUD or equivalent displays, EVS, SVS or CVS, or any combination of those systems into a hybrid system. Section 30(2)(a) the equipment meets the appropriate airworthiness certification requirements; Section 30(2)(b) the operator or owner has carried out a safety risk assessment associated with the operations supported by the automatic landing systems, a HUD or equivalent displays, EVS, SVS or CVS; Section 30(2)(c) the operator or owner has established and documented the procedures for the use of, and training requirements for, automatic landing systems, a HUD or equivalent displays, EVS, SVS or CVS.

Section 31. Flight data recorders and aircraft data recording system Section 31(1)(a) types I and IA FDRs shall record the parameters required to determine accurately the aeroplane flight path, speed, attitude, engine power, configuration and operation; and Section 31(1)(b) type II FDRs shall record the parameters required to determine accurately the aeroplane flight path, speed, attitude, engine power and configuration of lift and drag devices. Section 31(2) A person shall not operate an aeroplane for which the application for type certification is submitted to a Contracting State on or after the 1 st January 2016, and which are required to be fitted with an FDR shall record the pilot input or control surface position and primary controls (pitch, roll, yaw) parameters at a maximum recording interval of 0.125 seconds. Section 31(3)(a) engraving metal foil FDRs; Section 31(3)(b) analogue FDRs using frequency modulation (FM); Section 31(3)(c) photographic film FDRs; and Section 31(3)(d) magnetic tape FDRs. Section 31(4) All FDRs shall be capable of retaining the information recorded during at least the last 25 hours of their operation.

Section 32. Cockpit voice recorders and cockpit audio recording systems. Section 32(1) Magnetic tape and wire CVRs are prohibited. Section 32(2) All CVRs shall be capable of retaining the information recorded during at least the last 30 minutes of their operation. Section 32(3) All CVRs shall be capable of retaining the information recorded during at least the last two hours of their operation.

Section 33. Applicability of data link recorders. Section 33(1) All aeroplanes for which the individual certificate of airworthiness is first issued on or after the 1st January, 2016, which utilize any of the data link communications applications listed in 5.1.2 of the Third Schedule and are required to carry a Cockpit Voice Recorder (CVR), shall record on a flight recorder all data link communications messages. Section 33(2) All aeroplanes which are modified on or after 1 st January 2016 to install and utilize any of the data link communications applications listed in 5.1.2 of the Third Schedule and are required to carry a CVR shall record on a flight recorder the data link communications messages. Section 33(3) Data link recording shall be able to be correlated to the recorded cockpit audio. Section 33(4) The minimum recording duration shall be equal to the duration of the CVR.

Section 34. Flight recorders: General. Section 34(1) Flight recorders shall be constructed, located and installed so as to provide maximum practical protection for the recordings in order that the recorded information may be preserved, recovered and transcribed and flight recorders shall meet the prescribed crashworthiness and fire protection specifications. Section 34(2) Flight recorders shall not be switched off during flight time. Section 34(3) To preserve flight recorder records, flight recorders shall be deactivated upon completion of flight time following an accident or incident and the flight recorders shall not be reactivated before their disposition. Section 34(4) The pilot-in-command or the owner or operator, shall ensure, to the extent possible, in the event the aeroplane becomes involved in an accident or incident, the preservation of all related flight recorder records, and if necessary the associated flight recorders, and their retention in safe custody pending their disposition as determined in accordance with Civil Aviation (Aircraft Accident and Incident) Regulations. Section 34(5) Operational checks and evaluations of recordings from the flight recorder systems sh...

Section 35. Electronic Flight Bags (EFBs). Section 35(1) Where portable Electronic Flight Bags (‘EFBs’) are used on board an aeroplane, the pilot-in-command or the operator or owner shall ensure that they do not affect the performance of the aeroplane systems, equipment or the ability to operate the aeroplane. Section 35(2)(a) assess the safety risk(s) associated with each EFB function; Section 35(2)(b) establish the procedures for the use of, and training requirements for, the device and each EFB function; and Section 35(2)(c) ensure that, in the event of an EFB failure, sufficient information is readily available to the flight crew for the flight to be conducted safely. Section 35(3) The Authority shall establish criteria for the operational use of EFB functions to be used for the safe operation of aeroplanes. Section 35(4)(a) the EFB equipment and its associated installation hardware, including interaction with aeroplane systems if applicable, meet the appropriate airworthiness certification requirements; Section 35(4)(b) the operator or owner has assessed the risks associated with the operations supported by the EFB function(s); Section 35(4)(c) the operator or owner has establ...

Section 36. Communication equipment. Section 36(1) An aeroplane to be operated in accordance with the instrument flight rules or at night shall be provided with radio communication equipment in accordance with the Kenya Civil Aviation (Instrument and Equipment) Regulations and such equipment shall be capable of conducting two-way communication with those aeronautical stations and on those frequencies prescribed by the Authority. Section 36(2) When compliance with regulation 37 requires that more than one communication equipment unit be provided, each shall be independent of the other or others to the extent that a failure in any one will not result in failure of any other. Section 36(3) An aeroplane to be operated in accordance with VFR, but as a controlled flight, shall, unless exempted by the appropriate authority, be provided with radio communication equipment capable of conducting two-way communication at any time during flight with such aeronautical stations and on such frequencies as may be prescribed by the appropriate Authority. Section 36(4) An aeroplane to be operated on a flight to which the provisions of Regulation 20 or 21 apply shall, unless exempted by the Authority,...

Section 37. Navigation equipment. Section 37(1)(a) in accordance with its flight plan; and Section 37(1)(b) in accordance with the requirements of air traffic services; Section 37(2)(a) be provided with navigation equipment which will enable it to operate in accordance with the prescribed navigation specification(s); and Section 37(2)(b) have information relevant to the aeroplane navigation specification capabilities listed in the flight manual or other aeroplane documentation approved by the State of Design or the Authority; and Section 37(2)(c) where the aeroplane is operated in accordance with a MEL, have information relevant to the aeroplane navigation specification capabilities included in the MEL. Section 37(3) The Authority shall establish criteria for operations where a navigation specification for PBN has been prescribed. Section 37(4)(a) normal and abnormal procedures including contingency procedures; Section 37(4)(b) flight crew qualification and proficiency requirements, in accordance with the appropriate navigation specifications; Section 37(4)(c) training for relevant personnel consistent with the intended operations; and Section 37(4)(d) appropriate maintenance proce...

Section 38. Surveillance equipment. Section 38(1) A person shall not operate an aeroplane unless the aeroplane is provided with surveillance equipment that will enable it to operate in accordance with the requirements of air traffic services. Section 38(2)(a) the aeroplane in addition to the requirements specified in subregulation (1) is provided with surveillance equipment which will enable it to operate in accordance with the prescribed RSP specification(s); Section 38(2)(b) has information relevant to the aeroplane RSP specification capabilities listed in the flight manual or other aeroplane documentation approved by the State of Design or the Authority; and Section 38(2)(c) where the aeroplane is operated in accordance with a MEL, has information relevant to the aeroplane RSP specification capabilities included in the MEL. Section 38(3) The Authority shall establish criteria for operations where an RSP specification for PBS has been prescribed. Section 38(4)(a) normal and abnormal procedures, including contingency procedures; Section 38(4)(b) flight crew qualification and proficiency requirements, in accordance with appropriate RSP specifications; Section 38(4)(c) a training pr...

Section 39. Owner’s maintenance responsibilities. Section 39(1)(a) the aeroplane is maintained in an airworthy condition; Section 39(1)(b) the operational and emergency equipment necessary for an intended flight is serviceable; and Section 39(1)(c) the certificate of airworthiness of the aeroplane remains valid. Section 39(2) The owner or operator shall not operate the aeroplane unless it is maintained and released to service under a system acceptable to the Authority. Section 39(3) When the certificate of release to service is not issued by an approved maintenance organization in accordance with the Civil Aviation (Airworthiness Regulations), the person signing the certificate of release to service should be licensed in accordance with Civil Aviation (Personnel Licensing Regulations). Section 39(4) The owner or operator shall ensure that the maintenance of the aeroplane is performed in accordance with a maintenance programme acceptable to the Authority.

Section 40. Maintenance records. Section 40(1)(a) the total time in service (hours, calendar time and cycles, as appropriate) of the aeroplane and all life-limited components; Section 40(1)(b) the current status of compliance with all applicable mandatory continuing airworthiness information; Section 40(1)(c) appropriate details of modifications and repairs; Section 40(1)(d) the time in service (hours, calendar time and cycles, as appropriate) since the last overhaul of the aeroplane or its components subject to a mandatory overhaul life; Section 40(1)(e) the current status of the aeroplane's compliance with the maintenance programme; and Section 40(1)(f) the detailed maintenance records to show that all requirements for the signing of a certificate of release to service have been met. Section 40(2) The records in subregulation (1)(a) to (e) shall be kept for a minimum period of 90 days after the unit to which they refer has been permanently withdrawn from service and the records in subregulation (1)(f) for a minimum period of one year after the signing of the certificate of release to service. Section 40(3) In the event of a temporary change of owner or operator, the records shall...

Section 41. Modifications and repairs. Section 41(1) A person shall not perform modifications and repairs to an aircraft unless those modification and repairs comply with airworthiness requirements acceptable to the Authority. Section 41(2)(a) establish the procedures to ensure that records supporting compliance with the airworthiness requirements are retained; Section 41(2)(b) ensure that major repairs or major modifications are carried out in accordance with technical data acceptable to the Authority; Section 41(2)(c) promptly, upon completion of a major modification or major repair, prepare a report of each major modification or major repair of an airframe, aircraft engine, propeller or appliance of an aircraft operated by the operator; and Section 41(2)(d) submit a copy of each report of a major modification and repair to the Authority and keep a copy of each report of a major repair and modification available for inspection.

Section 42. Certificate of release to service.

Section 43. Composition of the flight crew. Section A person shall not operate an aeroplane unless the number and composition of the flight crew are not be less than that specified in the flight manual or other documents associated with the certificate of airworthiness.

Section 44. Qualifications. Section 44(1)(a) ensure that each flight crew member holds a valid licence issued by the Authority, or if issued by another Contracting State, rendered valid by the Authority; Section 44(1)(b) ensure that flight crew members are properly rated; and Section 44(1)(c) be satisfied that flight crew members have maintained competency. Section 44(2) The pilot-in-command of an aeroplane equipped with an airborne collision avoidance system (ACAS II) shall ensure that each flight crew member has been appropriately trained to competency in the use of ACAS II equipment and the avoidance of collision.

Section 45. Flight manual. Section 45(1)(a) a current Aeroplane Flight Manual accepted by the Authority; or Section 45(1)(b) a current accepted Pilot Operating Handbook or Owner’s manual, markings and placards, or any combination thereof which provide the pilot-in-command with the necessary limitations for safe operation. Section 45(2) A person shall not operate an aircraft within or over Kenya without complying with the operating limitations specified in subregulation (1). Section 45(3) The Aeroplane Flight Manual shall be updated by implementing changes made mandatory by the Authority.

Section 46. Journey log book. Section 46(1) The operator shall ensure a journey log book is maintained for every aeroplane engaged in air navigation in which particulars of the aeroplane, its crew and each journey is entered. Section 46(2)(a) aeroplane nationality and registration; Section 46(2)(b) date; Section 46(2)(c) crew member names and duty assignments; Section 46(2)(d) departure and arrival points and times; Section 46(2)(e) purpose of flight; Section 46(2)(f) observations regarding the flight; and Section 46(2)(g) signature of the pilot-in-command.

Section 47. Records of emergency and survival equipment carried. Section The owner of an aeroplane, or operator, shall at all times have available for immediate communication to rescue coordination centres, lists containing information on the emergency and survival equipment carried on board the aeroplane. The information shall include, as applicable, the number, colour and type of life rafts and pyrotechnics, details of emergency medical supplies, water supplies and the type and frequencies of the emergency portable radio equipment.

Section 48. Security of aereoplane. Section The pilot-in-command shall be responsible for the security of the aeroplane during its operation.

Section 49. Reporting acts of unalawful interference. Section Following an act of unlawful interference, the pilot-incommand shall submit a report in writing of such an act to the designated local Authority.

Section 50. Applicability.