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Britten-Norman Islander Maintenance Manual (BBBN-M-C) — Essco Aircraft - Uploaded by |
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Britten norman islander maintenance manual download
Notes: 1. Rectify manial installations before further flight. Inspection - within brittrn next 50 hours TIS unless already accomplished and thereafter at intervals not exceeding hours TIS ссылка на продолжение modified.
After britten norman islander maintenance manual download inspect at intervals not exceeding hours TIS. All affected seats maintenahce be repaired by 31 January or retired norrman service. After rectification per para. Rectification in продолжение здесь britten norman islander maintenance manual download SB 76 Issue 4, must britten accomplished before further flight if cracks are found, otherwise within the next hours TIS or by 16 June for top hinge and by 31 May for centre and bottom hinges, whichever is the sooner in each case.
Modification - Before further flight if cracking or other defects found, but must be embodied in all aircraft not later than 30 Britten norman islander maintenance manual download Inspect within the next 5 hours TIS, unless already accomplished, and thereafter at intervals not to exceed 50 hours TIS. Rectify any defects found, before further flight. Modify per Automotive Products Ltd. Britten norman islander maintenance manual download the next hours TIS or landings, whichever is the sooner, and thereafter at intervals not to exceed hours TIS or landings, whichever is the sooner.
Repair installations found defective, before further flight. Inspection - Within the next 10 hours TIS or by maintenancs August whichever is the sooner, unless already accomplished and thereafter at intervals not exceeding 50 hours TIS until modified. Rectify defective installations, before further flight. Within the next hours TIS or by 27 December whichever is the sooner, unless already accomplished. Cracked seat units must be rectified as prescribed, before further flight.
Remove defective parts from service before further flight. Part A: Eddy Current Inspection. Part B: Repetitive Visual Inspection. Installations found defective during inspection must be reworked, before further flight. Rework britten norman islander maintenance manual download By 27 Octobernormxn already accomplished.
Not later than 27 Septemberborman already accomplished, and thereafter at intervals not to exceed 2 years. Within the next hours TIS or by 27 Octoberwhichever is the sooner, unless already продолжение здесь. Replace any brackets found cracked before further flight. Model BN-2 majntenance Constructor Numbers throughthroughexceptand Repair if necessary per SB before further flight.
Within next hours TIS or when the rudder system is next dismantled, whichever is the sooner. SASW embodied. Brtiten ensure continued safe operation of modified aircraft, accomplish the following:. If any buckling is found, inspect internal fuselage structure for damage britten norman islander maintenance manual download repair all damage found, before further flight.
Initial inspection by 13 Apriland if no cracks are found, thereafter inspect britten norman islander maintenance manual download intervals not to exceed hours TIS.
If only horizontal cracks are found and these are less than 6. Within next 50 landings. If no cracks are found, thereafter at intervals not to exceed hours TIS. If cracks are found which are less than 5mm in length, inspect at intervals not to exceed 50 britten norman islander maintenance manual download.
Before further flight if stiffness or restriction is found in the function of the rudder and nose wheel steering system or at the next hour inspection. By 31 July and thereafter at intervals britten norman islander maintenance manual download to exceed hours TIS.
Repair any damage found per the SB before further flight. If any damage is found per the SB, replace the hinge bracket per Part 2 of the SB before brigten flight. To prevent cracking of the engine mount from progressing to the point where it may require extensive spar repairs or degrade the integrity of the engine mount, inspect manjal upper engine mounts per BN SB In addition to the inspection area described in the SB, inspect the entire length of the flange that attaches the engine mount to the spar as shown on the diagram below.
Inspect both inboard islandet outboard жмите of each engine mount. Initial inspection within hours TIS. Repeat inspection at intervals not to exceed hours TIS or landings whichever occurs first. All BN-2 series where any control column universal joint has been replaced since December Replace any undersized control column universal joints before further flight. To prevent over-length bolts from restricting aileron movement, inspect bolts securing access panels at W.
STA UK AD refers. Within 50 hours Downooad and thereafter whenever the elevator trim tab control rod is disconnected. To prevent the loss of the electrically powered artificial horizon gyro in the event of the loss of both engine driven generators, comply with SB This SB details the procedure for recalculating the electrical loads analysis to ensure the aircraft remains capable of at maitnenance 30 minutes safe flight on battery power alone.
This electrical HG is powered from the inverter circuit. Aircraft with avionics modified per other approved modification schemes should be assessed for applicability.
To prevent landing gear components remaining in service beyond their finite fatigue lives, determine the number of landings accumulated on all FHL main and nose landing gears per B-N Group SBIssue 1. Any landing gear assemblies or components that have exceeded the fatigue lives stated in Paragraph 6 of SB Issue 1 must be removed from service before further flight. To prevent failure of passenger seat rear frames, inspect each passenger seat frame per B-N Group SB If damage is found replace the seat frame with a serviceable item prior to further flight.
To prevent corrosion of the interior surface of the elevator 9.0 free download for windows 10 rod which could result in failure or collapse of the rod, resulting in loss of control dowjload britten norman islander maintenance manual download of the elevator silander, inspect per B-N Group SB issue 1.
To prevent loose horizontal stabiliser attachment bolts, inspect idlander horizontal stabiliser attachement bolts and anchor nuts, per B-N Group Ltd Service Bulletinrevision 2 or later EASA approved revision. Within the next britten norman islander maintenance manual download hours TIS or two months, whichever occurs sooner, unless already islnder, and thereafter at intervals not to exceed hours TIS.
Visually inspect the elevator tip assemblies top and bottom surfaces for deformation and signs of concavity per the instructions in paragraphs 6 and 9 of Britten-Norman Aircraft SB No. If any signs of concavity is foundinspect the elevator tip for delamination per the instructions in paragraph 9 of SB No.
If delamination is foundreplace the elevator tip with a serviceable part per drawing NB or NB as applicable, before further isander. Replace concave elevator tips with a serviceable part per drawing NB or NB as briften. Do not install an elevator tip to any aircraft unless the elevator tip is free from concavity and delamination per the instructions in SB No.
At the next daily inspection unless previously accomplished, and if any signs of concavity is found inspect thereafter for delamination at intervals not to exceed 50 hours TIS until requirement 2 of this AD is accomplished. You are here Home Aircraft Airworthiness directives Print. Search rules. Published : 26 July Notes: 1. The date above indicates the amendment date of this schedule. Cancelled R1 - Cancelled - Effective 4 October Cancelled - Cancelled maintneance Effective 2 November Cancelled - Cancelled - Effective 5 September Modification - at next engine removal for whatever reason.
Inspection to be carried out within the next 25 hours TIS. Within next 50 hours TIS unless alredy accomplished. Requirement: 1. At intervals not to exceed 50 hours TIS. Requirement: Modify per Automotive Products Ltd. By 27 Augustunless already britren. Modification - By 27 December Part C: Replacement Within landings or 12 months whichever occurs first.
Inspection - Within the next hours TIS. By 27 Octoberunless already accomplished. Within the next 50 hours TIS, britteb already accomplished. Requirement: To ensure continued safe operation of modified aircraft, accomplish the по этой ссылке 1.
Within the next 5 hours TIS, unless already accomplished. Requirement: To prevent cracking of the engine mount from progressing to the point where it may require extensive spar repairs or degrade the integrity of the engine mount, inspect the upper engine mounts per BN SB When repairing or installing pneumatic de-icer boots. Requirement: To prevent the loss of the electrically powered artificial horizon gyro in mankal event of the loss islandrr both engine mnaual generators, comply with SB Requirement: To prevent landing gear components remaining in service britten norman islander maintenance manual download their finite maintenanxe lives, determine the number of landings accumulated on all FHL main and nose landing gears per B-N Group SBIssue 1.
Requirement: To prevent normman of passenger seat rear frames, inspect each passenger seat frame per B-N Group SB Requirement: To prevent corrosion of the interior surface of the elevator control rod /26603.txt could result in failure or collapse of the rod, resulting in loss of control or jamming of the elevator system, inspect per B-N Group SB issue 1.
By 25 June 3. From читать полностью March As detailed.
- Britten Norman Islander Maintenance Manual Chapter 1/3 - [PDF Document]
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