VIP AVIA is pleased to provide you with our proposal for the management of continuing airworthiness as per EASA Part-M Subpart G requirements under EASA approved Continuing Airworthiness Management Organization (Ref. LV CAA approval No. LV.MG.0003).As well to provide you with our full maintenance support as PART 145 approved organization including line and base maintenance (Ref LV.145.0012).
SCOPE OF WORK The following are inspected, maintained or repaired in accordance with the approved maintenance data:
Aircraft Defect rectification, minor repairs and modifications, line and base maintenance as per limitations below:
Class
Rating
Limitation
Line
Base
Aircraft
A1
Canadair Challenger CL-600-2B16 (Variant 604)
Up to and including 36m / 1600 hours inspection
Yes
Yes
A1
(Hawker Beechcraft) BAe 125 / Series 800 / 800XP / 850XP series
Up to and including E (12m) / B (800 hours) inspection
Yes
Engines
B1
N/A
APU
B3
N/A
Components other than complete engines or APUs
C5
Electrical Power
Nickel-Cadmium and Lead-Acid Batteries (see 1.9.4)
Specialised Services
D1
N/A
Engine maintenance Currently engine maintenance is limited only to “on-airframe” tasks within the above work scope. Electrical power The following maintenance is performed under C5 rating: Scheduled inspection and maintenance of Ni-Cad and Sealed Lead-Acid batteries in accordance with the relevant airframe maintenance schedule, the battery manufacturer's service instructions and as detailed in MOE 2.24.7. 'Operational procedure for aircraft Ni-Cad and sealed Lead-Acid battery shop'.
Парк самолётов