Back to Course

PVT Regulations

0% Complete
0/0 Steps
  1. Part 61 Regulations

    §61.3 Requeriments for certificates
  2. §61.19 Duration of pilot certificates
  3. §61.23 Medical Certificates: Requirement and Duration
  4. §61.31 Type Rating and additional training requirements
  5. §61.51 Pilot Logbooks
  6. §61.56 Flight Review
  7. §61.57 Recent flight experience: Pilot in command
  8. §61.60 Change of address
  9. §61.103 - Eligibility requirements
  10. §61.113 Private pilot privileges and limitations
  11. Part 91 Regulations
    §91.3 Responsibility and authority of the pilot in command
  12. §91.7 Civil aircraft airworthiness
  13. §91.9 Civil aircraft flight manual, marking, and placard requirements
  14. §91.13 Careless or reckless operation
  15. §91.15 Dropping objects
  16. §91.17 Alcohol or drugs
  17. §91.21 Portable electronic devices
  18. §91.103 Preflight action
  19. §91.105 Flight crewmembers at stations
  20. §91.107 Use of safety belts and shoulder harnesses
  21. §91.109 Flight instruction; Simulated instrument flight
  22. §91.111 Operating near other aircraft
  23. §91.113 Right-of-way rules: Except water operations
  24. §91.117 Aircraft speed
  25. §91.119 Minimum safe altitudes: General
  26. §91.121 Altimeter settings
  27. §91.123 Compliance with ATC clearances and instructions
  28. §91.125 ATC light signals
  29. §91.144 Temporary restriction on flight operations during abnormally high barometric pressure conditions
  30. §91.151 Fuel requirements for flight in VFR conditions
  31. §91.155 Basic VFR weather minimums
  32. § 91.157 Special VFR weather minimums
  33. §91.159 VFR cruising altitude or flight level
  34. §91.203 Civil aircraft: Certifications required
  35. §91.205 Instrument and equipment requirements
  36. §91.207 Emergency locator transmitters
  37. §91.209 Aircraft lights
  38. §91.211 Supplemental oxygen
  39. §91.213 Inoperative instruments and equipment
  40. § 91.215 ATC transponder and altitude reporting equipment and use
  41. §91.409 Inspections
  42. §91.413 ATC transponder tests and inspections
  43. NTSB 830
    §830.1 Applicability
  44. §830.2 Definitions
  45. §830.5 - Immediate notification
  46. §830.6 - Information to be given in notification
  47. Miscellaneous
    Part 43 Appendix A Part C
  48. References
Lesson 45 of 48
In Progress

§830.5 – Immediate notification

Mateo Espin January 21, 2021

§830.5 – Immediate notification

The operator of any civil aircraft, or any public aircraft not operated by the Armed Forces or an intelligence agency of the United States, or any foreign aircraft shall immediately, and by the most expeditious means available, notify the nearest National Transportation Safety Board (NTSB) office, 1 when:

1 NTSB headquarters is located at 490 L’Enfant Plaza SW., Washington, DC 20594. Contact information for the NTSB’s regional offices is available at http://www.ntsb.gov. To report an accident or incident, you may call the NTSB Response Operations Center, at 844-373-9922 or 202-314-6290.

(a) An aircraft accident or any of the following listed serious incidents occur:

(1) Flight control system malfunction or failure;

(2) Inability of any required flight crewmember to perform normal flight duties as a result of injury or illness;

(3) Failure of any internal turbine engine component that results in the escape of debris other than out the exhaust path;

(4) In-flight fire;

(5) Aircraft collision in flight;

(6) Damage to property, other than the aircraft, estimated to exceed $25,000 for repair (including materials and labor) or fair market value in the event of total loss, whichever is less.

(7) For large multiengine aircraft (more than 12,500 pounds maximum certificated takeoff weight):

(i) In-flight failure of electrical systems which requires the sustained use of an emergency bus powered by a back-up source such as a battery, auxiliary power unit, or air-driven generator to retain flight control or essential instruments;

(ii) In-flight failure of hydraulic systems that results in sustained reliance on the sole remaining hydraulic or mechanical system for movement of flight control surfaces;

(iii) Sustained loss of the power or thrust produced by two or more engines; and

(iv) An evacuation of an aircraft in which an emergency egress system is utilized.

(8) Release of all or a portion of a propeller blade from an aircraft, excluding release caused solely by ground contact;

(9) A complete loss of information, excluding flickering, from more than 50 percent of an aircraft’s cockpit displays known as:

(i) Electronic Flight Instrument System (EFIS) displays;

(ii) Engine Indication and Crew Alerting System (EICAS) displays;

(iii) Electronic Centralized Aircraft Monitor (ECAM) displays; or

(iv) Other displays of this type, which generally include a primary flight display (PFD), primary navigation display (PND), and other integrated displays;

(10) Airborne Collision and Avoidance System (ACAS) resolution advisories issued when an aircraft is being operated on an instrument flight rules flight plan and compliance with the advisory is necessary to avert a substantial risk of collision between two or more aircraft.

(11) Damage to helicopter tail or main rotor blades, including ground damage, that requires major repair or replacement of the blade(s);

(12) Any event in which an operator, when operating an airplane as an air carrier at a public-use airport on land:

(i) Lands or departs on a taxiway, incorrect runway, or other area not designed as a runway; or

(ii) Experiences a runway incursion that requires the operator or the crew of another aircraft or vehicle to take immediate corrective action to avoid a collision.

(b) An aircraft is overdue and is believed to have been involved in an accident.