GENERAL DATA. Number of aircraft in fleet 2 un.
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1 FLEET COMPOSITION REGISTRY CS-HGH CS-HGU SERIAL NUMBER YEAR AIRCRAFT MANUFACTURER AGUSTAWESTLAND AGUSTAWESTLAND AIRCRAFT MODEL AW139 AW139 ENGINES MANUFACTURER PRATT&WHITNEY PRATT&WHITNEY ENGINES MODEL PT6C-67C PT6C-67C
2 GENERAL DATA Number of aircraft in fleet 2 un. At 31/12/211 From 1/7/211 to 31/12/211 Number of aircraft in service 2 un. CS-HGH Total Hours 389:5 FH CS-HGH Total Cycles 1143 LDG CS-HGU Total Hours 1181:25 FH CS-HGU Total Cycles 2469 LDG Total calendar days 368 DY Total flying days 9 DY Rate of calendar operational activity,24 - Total Hours flown 177:45 FH Total Cycles 467 LDG Average daily utilization 1:58 FH Daily Cycles 5,19 LDG Average flight time :22 FH Failure Rate,15 AN/H MTBF 6:35 FH Reliability,9458-2,
3 FLIGHT LOG JUL'11 AUG'11 SEP'11 OCT'11 NOV'11 DEC'11 FLIGHT HOURS 36:2 48:5 : 14:55 45:5 33:2 LANDINGS AGUSTAWESTLAND AW139 - FLIGHT LOG FLIGHT HOURS 6: 48: 36: 24: 12: : 48:5 36:2 : 29,25 #VALOR! 45:5 33:2 14:55 JUL'11 AUG'11 SEP'11 OCT'11 NOV'11 DEC' LANDINGS FLIGHT HOURS LANDINGS
4 ANOMALIES CRITICAL NON-CRITICAL TOTAL JUL' AUG' SEP'11 OCT' NOV' DEC' NUMBER OF ANOMALIES AGUSTAWESTLAND AW139 - ANOMALIES JUL'11 AUG'11 SEP'11 OCT'11 NOV'11 DEC'11 CRITICAL NON-CRITICAL AGUSTAWESTLAND AW139 - ANOMALIES PER ATA ANOMALIES ATA
5 CRITICAL PARTS REGISTRY OCCURENCE INFORMATION COMPONENT SYSTEM AND/OR COMPONENTS (OUT) SYSTEM AND/OR COMPONENTS (IN) ANOMALIES REPORTED DATE FH LDGS ATA CRITICAL DESCRIPTION PART NUMBER SERIAL NUMBER DESCRIPTION PART NUMBER SERIAL NUMBER CS-HGH 12-ago-11 34:2 946 NLG ASSY SHOCK ABSORBER COLLAPSED 32 YES NOSE LANDING GEAR ASSY 3G322V NOSE LANDING GEAR ASSY 3G322V CS-HGH 27-ago : MAIN ROTOR DAMPER LEAKING FROM PISTON 62 YES MAIN ROTOR DAMPER 3G622V MAIN ROTOR DAMPER 3G622V B CS-HGH 11-out : BEARING LOOSEN BELLCRANK 67 YES LEVER ASSY 3E6722A LEVER ASSY 3E6722A CS-HGH 23-nov :1 114 MAIN ROTOR DAMPER WITH EXCESSIVE LEAK 62 YES MAIN ROTOR DAMPER 3G622V B MAIN ROTOR DAMPER 3G622V REGISTRY OCCURENCE INFORMATION COMPONENT SYSTEM AND/OR COMPONENTS (OUT) SYSTEM AND/OR COMPONENTS (IN) ANOMALIES REPORTED DATE FH LDGS ATA CRITICAL DESCRIPTION PART NUMBER SERIAL NUMBER DESCRIPTION PART NUMBER SERIAL NUMBER CS-HGU 7-jul : TAIL ROTOR BLADE WITH CRACK 64 YES TAIL ROTOR BLADE 3G641A131 Q946 TAIL ROTOR BLADE 3G641A131 P777 CS-HGU 14-nov : SWASHPLATE SPHERICAL BEARING FRICTION TOO LOW 62 YES CS-HGU 14-nov : TAIL ROTOR CONTROL SLIDER BUSHING WORN OUT OF LIMITS 64 YES SLIDER BUSHING 3G643V253 UNK SLIDER BUSHING 3G643V253 11X CS-HGU 14-nov : HYDRAULIC LEAK FROM FWD MAIN ROTOR SERVO 67 YES MAIN SERVO ACTUATOR 3G673V531 HSC MAIN SERVO ACTUATOR 3G673V531 HSC23125 CS-HGU 14-nov : TAIL ROTOR HUB & SPIDER ASSY - FLANGED BUSHINGS WORN 64 YES SCISSOR COUPLING 3G643A SCISSOR COUPLING 3G643A CS-HGU 14-nov : LOWER MRH CONICAL RING DAMAGED 62 YES LWR CONICAL RING 3G622A1951 N185 LWR CONICAL RING 3G622A1951 Q423
6 ALERT LEVEL Number of ALERT LEVEL PIREPs MAREPs TOTAL PIREPs MAREPs TOTAL ATA DESCRIPTION PIREPs MAREPs 1 PARKING, MOORING, STORAGE NO NO 21 AIR CONDITIONING AND PRESSURIZATION 4 4,35,35 NO NO 22 AUTO FLIGHT ,9,9,2,17,2 NO NO 23 COMMUNICATIONS ,17,2,43,61,2 NO NO 24 ELECTRICAL POWER 1 1,9,9 NO NO 25 EQUIPMENT/FURNISHINGS 4 3 7,35,26,61 NO NO 26 FIRE PROTECTION ,9,2,9,2 NO NO 27 FLIGHT CONTROLS NO NO 28 FUEL ,87,17,2 1,4,2 NO NO 29 HYDRAULIC POWER ,17,4,56,35,2,56,52,6 1,13 NO NO 3 ICE AND RAIN PROTECTION NO NO 31 INDICATING / RECORDING SYSTEM 4 3 7,35,26,61 NO NO 32 LANDING GEAR ,78,2,43,6 1,13 1,21,81 1,13 NO YES 33 LIGHTS ,9,2,56,61,6,56,69,81 1,13 NO NO 34 NAVIGATION ,43,2,56,17,2,56,61,4 1,13 NO NO 35 OXYGEN NO NO 36 PNEUMATIC NO NO 37 VACUUM NO NO 38 WATER/WASTE NO NO 39 ELECTRICAL - ELECTRONIC PANELS AND MULTIPURPOSE CO NO NO 4 MULTISYSTEM NO NO 41 WATER BALLAST NO NO 42 INTEGRATED MODULAR AVIONICS NO NO 44 CABIN SYSTEMS NO NO 45 DIAGNOSTIC AND MAINTENANCE SYSTEM NO NO 46 INFORMATION SYSTEMS NO NO 47 NITROGEN GENERATION SYSTEM NO NO 48 IN FLIGHT FUEL DISPENSING NO NO 49 AIRBORNE AUXILIARY POWER NO NO 5 CARGO AND ACCESSORY COMPARTMENTS NO NO 52 DOORS NO NO 53 FUSELAGE ,9,43,6 1,69,52,6 1,69 NO YES 54 NACELLES/PYLONS NO NO 55 STABILIZERS ,87,81,87,81 NO NO 56 WINDOWS ,9,9,2,17,2 NO NO 57 WINGS NO NO 62 ROTOR ,61 2,69 3,43 2,81 3,29 3,43 2,81 NO YES 63 ROTOR DRIVE ,17,2,56,26,6 1,13,43,81 1,69 NO NO 64 TAIL ROTOR ,95 1,1 1,69,95 1,1 1,69 NO YES 65 TAIL ROTOR DRIVE ,35,2,56,35,2,56 NO NO 67 ROTORS FLIGHT CONTROL ,26,61,6 1,69,87,6 1,69 NO YES
7 ALERT LEVEL ATA DESCRIPTION Number of ALERT LEVEL PIREPs MAREPs TOTAL PIREPs MAREPs TOTAL PIREPs MAREPs 71 POWER PLANT ,17,2,56,17,2,56 NO NO 72 ENGINE - RECIPROCATING 1 1,9,9 NO NO 73 ENGINE - FUEL AND CONTROL NO NO 74 IGNITION NO NO 75 BLEED AIR NO NO 76 ENGINE CONTROLS NO NO 77 ENGINE INDICATING NO NO 78 EXHAUST 1 1,9,9 NO NO 79 OIL NO NO 8 STARTING NO NO 95 OPTIONAL EQUIPMENT 2 2,17,17 NO NO
8 32 - LANDING GEAR 53 - FUSELAGE 1,21 1,13 1,13 1,69 1,69,78,2,43,6,81,9,43,6,6, ROTOR 64 - TAIL ROTOR 2,69 3,43 3,29 3,43 2,81 2,81 1,69 1,69,95 1,1,95 1,1, ROTORS FLIGHT CONTROL 1,69 1,69,87,26,61,6,6
ANOMALIES AND RELIABILITY CONTROL BOOK
01 CS-HGH 11-ago-08 73:30 260-20080500 MAREP DISPLAY UNIT MALFUNCTION DISPLAY UNIT REPLACED 31 NO DISPLAY UNIT 7023460-804 06022721 DISPLAY UNIT 7023460-804 05092319 02 CS-HGH 11-ago-08 73:30 260-20080500
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