What are the various logbooks?
Thread Starter
Join Date: Oct 2006
Location: London UK & Uzes France
Posts: 91
Likes: 0
Received 0 Likes
on
0 Posts
What are the various logbooks?
Hi guys,
I have been searching around the internet, but only found a confusing amount of contradictory information...
Can someone pelase explain what the various logbooks are (and tell me if I have the general idea wrong) on a commercial aircraft.
- Aircraft Logbook : General log of every flight.
- Engine Logbook : Log of engine (hours / faults etc)?
- Aircraft Technical Logbook : How does this differ from the A/C Logbook? Are faults not recorded in the A/C Logbook?
- Maintenance Logbook : Record of maintenance on the A/C? Is this not recorded with the faults in the other logbooks?
Are there any others?
Is the idea of a "logbook" somewhat misleading? Rather than a ledger of each flight, are there several pages of info for each flight/sector?
Many thanks!
Martin
I have been searching around the internet, but only found a confusing amount of contradictory information...
Can someone pelase explain what the various logbooks are (and tell me if I have the general idea wrong) on a commercial aircraft.
- Aircraft Logbook : General log of every flight.
- Engine Logbook : Log of engine (hours / faults etc)?
- Aircraft Technical Logbook : How does this differ from the A/C Logbook? Are faults not recorded in the A/C Logbook?
- Maintenance Logbook : Record of maintenance on the A/C? Is this not recorded with the faults in the other logbooks?
Are there any others?
Is the idea of a "logbook" somewhat misleading? Rather than a ledger of each flight, are there several pages of info for each flight/sector?
Many thanks!
Martin
Log Books
Hope this helps.
(EASA) Regulation (EC) No. 2042/2003
M.A.305 Aircraft continuing airworthiness record system
(a) At the completion of any maintenance, the associated M.A.801 certificate of release to service shall be entered in the aircraft continuing airworthiness records. Each entry shall be made as soon as practicable but in no event more than 30 days after the day of maintenance action.
(b) The aircraft continuing airworthiness records shall consist of, as appropriate, an aircraft logbook, engine logbook(s) or engine module log cards, propeller logbook(s) and log cards, for any service life limited component and the operator's technical log.
(c) The aircraft type and registration mark, the date, together with total flight time and/or flight cycles and/or landings, as appropriate, shall be entered in the aircraft logbooks.
(d) The aircraft continuing airworthiness records shall contain the current:
1. status of airworthiness directives and measures mandated by the competent authority in immediate reaction to a safety problem;
2. status of modifications and repairs;
3. status of compliance with maintenance programme;
4. status of service life limited components;
5. mass and balance report;
6. list of deferred maintenance.
(e) In addition to the authorised release document, EASA Form 1 or equivalent, the following information relevant to any component installed shall be entered in the appropriate engine or propeller logbook, engine module or service life limited component log card:
1. identification of the component, and;
2. the type, serial number and registration of the aircraft to which the particular component has been fitted, along with the reference to the installation and removal of the component, and;
3. the particular component accumulated total flight time and/or flight cycles and/or landings and/or calendar time, as appropriate, and;
4. the current paragraph (d) information applicable to the component.
(f) The person responsible for the management of continuing airworthiness tasks pursuant to M.A. Subpart B, shall control the records as detailed in this paragraph and present the records to the competent authority upon request.
(g) All entries made in the aircraft continuing airworthiness records shall be clear and accurate. When it is necessary to correct an entry, the correction shall be made in a manner that clearly shows the original entry.
(h) An owner or operator shall ensure that a system has been established to keep the following records for the periods specified:
1. all detailed maintenance records in respect of the aircraft and any life-limited component fitted thereto, at least 24 months after the aircraft or component was permanently withdrawn from service, and;
2. the total time and flight cycles as appropriate, of the aircraft and all life-limited components, at least 12 months after the aircraft or component has been permanently withdrawn from service, and;
3. the time and flight cycles as appropriate, since last scheduled maintenance of the component subjected to a
service life limit, at least until the component scheduled maintenance has been superseded by another scheduled maintenance of equivalent work scope and detail, and;
4. the current status of compliance with maintenance programme such that compliance with the approved aircraft maintenance programme can be established, at least until the aircraft or component scheduled maintenance has been superseded by other scheduled maintenance of equivalent work scope and detail, and;
5. the current status of airworthiness directives applicable to the aircraft and components, at least 12 months after the aircraft or component has been permanently withdrawn from service, and;
6. details of current modifications and repairs to the aircraft, engine(s), propeller(s) and any other component vital to flight safety, at least 12 months after they have been permanently withdrawn from service.
M.A.306 Operator's technical log system
(a) In the case of commercial air transport, in addition to the requirements of M.A.305, an operator shall use an aircraft technical log system containing the following information for each aircraft:
1. information about each flight, necessary to ensure continued flight safety, and;
2. the current aircraft certificate of release to service, and;
3. the current maintenance statement giving the aircraft maintenance status of what scheduled and out of phase maintenance is next due except that the competent authority may agree to the maintenance statement being kept elsewhere, and;
4. all outstanding deferred defects rectifications that affect the operation of the aircraft, and;
5. any necessary guidance instructions on maintenance support arrangements.
(b) The aircraft technical log system and any subsequent amendment shall be approved by the competent authority.
(c) An operator shall ensure that the aircraft technical log is retained for 36 months after the date of the last entry.
(EASA) Regulation (EC) No. 2042/2003
M.A.305 Aircraft continuing airworthiness record system
(a) At the completion of any maintenance, the associated M.A.801 certificate of release to service shall be entered in the aircraft continuing airworthiness records. Each entry shall be made as soon as practicable but in no event more than 30 days after the day of maintenance action.
(b) The aircraft continuing airworthiness records shall consist of, as appropriate, an aircraft logbook, engine logbook(s) or engine module log cards, propeller logbook(s) and log cards, for any service life limited component and the operator's technical log.
(c) The aircraft type and registration mark, the date, together with total flight time and/or flight cycles and/or landings, as appropriate, shall be entered in the aircraft logbooks.
(d) The aircraft continuing airworthiness records shall contain the current:
1. status of airworthiness directives and measures mandated by the competent authority in immediate reaction to a safety problem;
2. status of modifications and repairs;
3. status of compliance with maintenance programme;
4. status of service life limited components;
5. mass and balance report;
6. list of deferred maintenance.
(e) In addition to the authorised release document, EASA Form 1 or equivalent, the following information relevant to any component installed shall be entered in the appropriate engine or propeller logbook, engine module or service life limited component log card:
1. identification of the component, and;
2. the type, serial number and registration of the aircraft to which the particular component has been fitted, along with the reference to the installation and removal of the component, and;
3. the particular component accumulated total flight time and/or flight cycles and/or landings and/or calendar time, as appropriate, and;
4. the current paragraph (d) information applicable to the component.
(f) The person responsible for the management of continuing airworthiness tasks pursuant to M.A. Subpart B, shall control the records as detailed in this paragraph and present the records to the competent authority upon request.
(g) All entries made in the aircraft continuing airworthiness records shall be clear and accurate. When it is necessary to correct an entry, the correction shall be made in a manner that clearly shows the original entry.
(h) An owner or operator shall ensure that a system has been established to keep the following records for the periods specified:
1. all detailed maintenance records in respect of the aircraft and any life-limited component fitted thereto, at least 24 months after the aircraft or component was permanently withdrawn from service, and;
2. the total time and flight cycles as appropriate, of the aircraft and all life-limited components, at least 12 months after the aircraft or component has been permanently withdrawn from service, and;
3. the time and flight cycles as appropriate, since last scheduled maintenance of the component subjected to a
service life limit, at least until the component scheduled maintenance has been superseded by another scheduled maintenance of equivalent work scope and detail, and;
4. the current status of compliance with maintenance programme such that compliance with the approved aircraft maintenance programme can be established, at least until the aircraft or component scheduled maintenance has been superseded by other scheduled maintenance of equivalent work scope and detail, and;
5. the current status of airworthiness directives applicable to the aircraft and components, at least 12 months after the aircraft or component has been permanently withdrawn from service, and;
6. details of current modifications and repairs to the aircraft, engine(s), propeller(s) and any other component vital to flight safety, at least 12 months after they have been permanently withdrawn from service.
M.A.306 Operator's technical log system
(a) In the case of commercial air transport, in addition to the requirements of M.A.305, an operator shall use an aircraft technical log system containing the following information for each aircraft:
1. information about each flight, necessary to ensure continued flight safety, and;
2. the current aircraft certificate of release to service, and;
3. the current maintenance statement giving the aircraft maintenance status of what scheduled and out of phase maintenance is next due except that the competent authority may agree to the maintenance statement being kept elsewhere, and;
4. all outstanding deferred defects rectifications that affect the operation of the aircraft, and;
5. any necessary guidance instructions on maintenance support arrangements.
(b) The aircraft technical log system and any subsequent amendment shall be approved by the competent authority.
(c) An operator shall ensure that the aircraft technical log is retained for 36 months after the date of the last entry.
