항공구조구급대 운영 규정[별지 제12호서식]

항공기 일일점검표(제35조제3항 관련)

AS365N2 비행 전 점검표
항공기 형식	등 록 번 호	제작사 번호	관련교범
AS365N2			AS365N2 FM

점검일자 20 . . .	정비사			기장			항공대장
	정비사			기장

※ 점검결과 상태에 따라 표시 (V = 양호 , X = 불량)
점검사항	내 용	방 법	상 태
외부점검	- 브레이크 압력 점검	작동검사
	- 항공기 전방 동체부분 외부 상태	육안검사
	- 전방유리 상태	육안검사
	- 전방착륙장치 상태	육안검사
	- 좌측 조종실 문 상태	육안검사
	- 좌측 오일 수준 상태	육안검사
	- 좌측 화물실 문 상태	육안검사
	- 좌측 주 회전익 상태	육안검사
	- 좌측 착륙장치 상태	육안검사
	- 좌측 엔진부분 상태	육안검사
	- 미부 회전익 계통 상태	육안검사
	- 우측 엔진부분 상태	육안검사
	- 우측 착륙장치 상태	육안검사
	- 우측 주회전익 계통상태	육안검사
	- 우측 오일수준 상태	육안검사
	- 우측 화물실문 외부 상태	육안검사
	- 우측 조종실 문 상태	육안검사
내부점검	- 조종실 내부 상태	육안검사
	- 승객실 내부 상태	육안검사
	- 소화기 상태 점검	육안검사
	- 각종 전기전기장치 스위치 확인	육안검사
	- 페달정렬 상태	육안검사
	- 조종석 조절 상태	작동검사
	- 안전벨트 조절 상태	작동검사
POWER-ON 점검	- 각종 스위치 상태	작동검사
	- 전기계기 작동 상태	작동검사
	- 연료량 상태	작동검사
	- 전원 스위치 OFF 확인	작동검사

210㎜×297㎜[백상지 80g/㎡]

AS365N2 비행 후 점검표
항공기 형식	등 록 번 호	제작사 번호	관련교범
AS365N2			AS365N2 FM

점검일자 20 . . .	정비사			기장			항공대장
	정비사			기장

※ 점검결과 상태에 따라 표시 (V = 양호 , X = 불량)
점검사항	내 용	방 법	상 태
내부점검	- 조종간(Collective)잠금 상태	육안검사
	- 페달정렬 상태	육안검사
	- 제동장치 잠금 상태	육안검사
	- 연료량 잔량 확인	육안검사
	- 전원 스위치 OFF 확인	육안검사
외부점검	- 항공기 전방 동체부분 외부 상태	육안검사
	- 전방유리 상태	육안검사
	- 전방착륙장치 상태	육안검사
	- 좌측 오일 수준 상태	육안검사
	- 좌측 화물실 문 상태	육안검사
	- 좌측 주 회전익 상태	육안검사
	- 좌측 착륙장치 상태	육안검사
	- 좌측 엔진부분 상태	육안검사
	- 미부 회전익 계통 상태	육안검사
	- 우측 엔진부분 상태	육안검사
	- 우측 착륙장치 상태	육안검사
	- 우측 주회전익 계통상태	육안검사
	- 우측 오일수준 상태	육안검사
	- 엔진 시스템 오일, 연료 누설흔적	육안검사
비행결과 기록	- 탑재용항공일지 기록	기록유지
	- 비행시간기록부 기록	기록유지

AS365N3 비행전 점검표

점검일자 20 . . .	정비사			기장			항공대장
	정비사			기장

1	INTRODUCTION a) In addition to examinations described below, carefully check the parts or systems that required work after the last flight check(A.L.F) for : -sealing. -foreign matters.-proper closing of doors or access panels. b) During the examination, check optional installations. c) Check that emergency locator beacon (if installed) is set to "AUTO"
2	CABIN EXTERIOR a) RADOME : Open. - RADOME COMPARTMENT : Electrical master box circuit breakers engaged. b) RADOME : Closed. - PITOT HEATS : Covers removed. c) OIL COOLER AIR INTAKE : Blanking cover removed d) NOSE LANDING GEAR : Visually check that the shock strut is not fully compressed and that the inflation pressure of tires. e) BATTERY : Connected. - COPILOT DOOR : Jettison mechanism snap wired.
3	TRANSMISSION DECK, L/H SIDE a) ENGINE AIR INTAKE BLANKING COVER : Removed. b) M.G.B COWLING : Open. - FUEL FILTER : Bleed. - ENGINE OIL RESERVOIR : Check level. c) ENGINE AIR INTAKE : No foreign matters. - M.G.B COWLING : Close, lock. d) TRANSMISSION DECK ACCESS FOOTSTEPS : Close. e) L/H HYDRAULIC RESERVOIR : Check level.
4	ENGINE DECK, L/H SIDE a) EXHAUST PIPE, AIR INTAKE BLANKING COVER : Removed. No foreign matters in exhaust pipe, air intake.
5	FUSELAGE STRUCTURE, L/H SIDE a) FUEL FILTER CAPS & DOOR : Close, lock. b) REAR SIDE FAIRING (BOTTOM STRUCTURE) : Open. c) FUEL TANK BLEED VALVES : Actuate. After bleeding, check that the bleed valves are correctly closed. d) REAR SIDE FAIRING : Close. e) PASSENGER DOORS : Check that jettison mechanism is snap wired. f) L/H MAIN LANDING GEAR UNIT: Visually check that the shock strut is not fully compressed & that the inflation pressure of tires is correct. g) STATIC PRESSURE PORTS : Blanking covers removed.
6	TAIL BOOM, L/H SIDE a) TAIL BOOM : General visual check. - STABILIZER-FIN : General visual check. b) TAIL ROTOR BLADES : General visual check.
7	TAIL BOOM, R/H SIDE a) TAIL BOOM : General visual check. b) STABILIZER-FIN : General visual check. c) T.G.B : Oil level. d) DRIVE SYSTEM FAIRING : Paint marks on cowling & DZUS correspond.
8	FUSELAGE STRUCTURE, R/H SIDE a) CARGO COMPARTMENT DOOR : Visual examination door closed. b) STATIC PRESSURE PORTS : Blanking cover removed. c) R/H MAIN LANDING GEAR UNIT : Visually check that the shock strut is not fully compressed & the inflation pressure of tires is correct. d) SIDE FAIRING : Close. e) PASSENGER DOORS: Check that the jettison mechanism is snap-wired.

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9	ENGINE DECK, R/H SIDE EXHAUST PIPE, AIR INTAKE BLANKING COVER : Removed. No foreign matters in exhaust pipe, air intake.
10	TRANSMISSION DECK, R/H SIDE a) ENGINE AIR INTAKE : Blanking cover removed. b) M.G.B COWLING : Open. . c) ENGINE OIL RESERVOIR : Check level. d) ENGINE AIR INTAKE : No foreign matters. e) M.G.B COWLING : Close, lock. f) TRANSMISSION DECK ACCESS FOOTSTEPS : Close. g) R/H HYDRAULIC RESERVOIR : Check level. h) FUEL FILTER : Bleed
11	FINAL STEPS a) BLADE SOCKS & ALL GUARDS: Removed. b) MAIN BLADES : General visual check.
13	SLIDING DOORS a) Check that doors operate correctly & are held in closed & open positions. b) Check that 'door closed' indicating system operate correctly.
14	MAIN LANDING GEAR a) Severe climatic conditions and salt-laden atmosphere. b) Ring carbon and piston tube with fresh water at a pressure lower than 2 bar.
15	NOSE LANDING GEAR a) Severe climatic conditions and salt-laden atmosphere. b) Ring with fresh water at a pressure lower than 2 bar.
16	STRUCTURE a) Washing the structure after flight over the sea.
17	HOIST a) Check hoist system & its attachment for condition.(Work card 25.63.01.601 or 25.63.02.601) b) Check in particular : - the hoist operator's safety belt & retaining cable, - the hoist cable. - the condition of the pyro technical cartridge& its expire date, - that the cable cutter is in place. c) Check hoist power supply insulation. Set mission selector to 'off'. Operate the switch on the control grip & check that the hoist does not move. d) Using the tool (z), check the metallic stop 20mm MIN. height (Figure 1). Note : The cable & checking & replacement criteria are give in the hoist manufacture's documents.
18	SAND FILTERS a) Check condition of filtering units and ejection nozzles. b) Check that cowling are correctly locked.
19	RADIO-NAVIGATION a) Check the radio-navigation system (Work card 24.00.00.600).
20	COMMUNICATIONS SYSTEMS a) Check the communications systems b) Check in particular the HF/SSB antenna (Work card 23.11.12.601).
21	OPTIONAL EQUIPMENT INSTALLATION a) Check general condition & security.(Life Rafts. Cargo Hook. Fuel Flowmeter. Belly Tank. Search L/T. Loud speaker)
22	PREFLIGHT CHECK IN COLD WEATHER MET 05. 21. 00. 605
23	AD 2009-188 (ASB05.00.54) TGB OIL LEVEL.
24	AD 2006-057 (ASB05.00.49) T/R BLADE CHECK
25	기내 비치서류 확인

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AS365N3 비행간 점검표

점검일자 20 . . .	정비사			기장			항공대장
	정비사			기장

1	EXTERIOR CHECK LIST a) Check for leaks without opening cowlings. b) Head the aircraft in to the wind (if possible). c) Check the fuel tank filler caps. d) LANDING GEAR UNITS & DOORS : Visual examination. e) ENGINE AIR INTAKE : Clear. On snow-covered ground, check (opening M.G.B. cowling if necessary), the there is no snow or ice built up inside air intake ducts. Carefully remove any trace of snow from the grid, around the air intakes, from the cowlings & top of fuselage. f) HYDRAULIC RESERVOIRS : Fluid level. g) ENGINE OIL TANKS : Oil level. Wait at least 15 minutes after shutdown for level to stabilize (oil consumption 0.3ℓ/hour maxi). ENG COMPARTMENT OIL LEAK. h) FUEL FILTERS : Clogging indicator not visible. I) MAIN ROTOR BLADES : Overall visual check from ground level. J) TAIL ROTOR : Blade condition ; no chafing on tunnel. k) TAIL GEAR BOX : Oil level. l) ALL COWLINGS : Closed, locks in place. m) DRIVE SYSTEM FAIRING : Paint mark on cowling & DZUS correspond.
2	INTERIOR CHECK LIST a) CABIN : General check (condition, freight tied down, passenger arrangement, etc...) b) DOORS : Closed & locked, flog not visible, "DOORS"indicator light off. jettison mechanism snap-wired. c) FIRE EXTINGUISHER : In place ; safety pin snap-wire. d) CIRCUIT-BREAKERS : ALL engaged. e) YAW PEDALS : Adjusted. f) SEATS : Adjusted. g) SEAT BELTS & HARNESSES : Fastened. NOTE : If the copilot seat is unoccupied. check that the seat belt It is fastened.
3	SLIDING DOORS a) Check that doors are locked or open positions.
4	DISTRESS BEACON (E.L.T) a) According to beacons, check the following : - that the function selector switch on the beacon is set to "AUTO" (ARM) - that the function selector switch on the beacon is set to "ON" & the locking system is set to "LOCK" b) Check that door is in place.
5	HOIST a) Unwind two or three meters of cable in order to free the up limit lever. b) Push the lever upward then release & check that the return spring operates correctly. c) Visually check that the two free arms of the spring are still in place & that they are pressed against the up limit lever. d) If one or both free arms are broken, remove the hoist & send it to the repair shop. e) Check that the cable cutter is in place. f) check condition of the frequency adapter elastomer. According to version : g) Check that sliding door guard is in place(Work Card 25. 63. 01. 406 or 25. 63. 02.406) h) Check that protective trays are in place (Work Card 25. 63. 01. 405)
6	SAND FILTERS a) Operate "SAND FILT" switch and check that blue light come on and goes out accordingly.
7	기타 OPTIONAL EQUIPMENT INSTALLATION a) Check General condition & security ( Life Raft. Fuel flowmeter. ) b) check in cold weather.

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AS365N3 비행후 점검표

점검일자 20 . . .	정비사			기장			항공대장
	정비사			기장

1	PRELIMINARY STEP a) Before each inspection, refer to the aircraft log book and into account the pilot's comments (anomalies and incidents). b) Unless otherwise specified in the text, the inspection described are performed "visually" or by "feel"
2	DEFINITION OF THE TERMS EMPLOYED IN THE MAINTENANCE OPERATION a) Condition The visual inspection covers the general external appearance of the item, distortion, breakage, cracks, scratches, corrosion, signs of overheating, wear, etc. b) Attachment points The visual inspection cover the attachment points of the item and the condition of safetying. c) Locking Lock the item and/or ensure the locking is correct. To check the locking, close and check the correct position of the cowling, fairing, hatches, panels, caps etc. d) Sealing The visual inspection is intended to detect any seepage or leakage of fluids. e) Absence of abnormal play Unless specified otherwise there is no requirement to measure play: but any "abnormal" play may, in certain circumstances be detected by applying a manual force to the item to be checked f) Cleanliness Cleanliness is intended to signify : absence of foreign bodies, seepage or splashing of liquids, "soiled" zones which may mask a visual defect. g) Pipes The inspection of pipes consists in checking their condition(wear due to friction, tears etc.)
3	GENERAL INSTRUCTION FOR THE INSPECTION AFTER THE FLIGHT OF THE DAY. a) Structure During the inspection circuit, check in general the condition of the skins the structure, the canopy(cleanliness of the transparent panels),hatches and opening panels and their attachment points, as well as those of the pilot, copilot and passenger seats, and of the equipment. b) Doors For each door : general condition, operation, correct closure, absence of abnormal play, in particular at the hinges. Condition of the attachment or locking brackets, closing pins and locking system, rails and rollers, stops. c) Cowling For each cowling : as it opened and during inspection of the compartment, perform a detailed visual inspection of the condition of the skin, the structure, the attachment points, the fastening of the rails, free operation. Operate the locking hooks to check : - the appearance and play at the locking hooks - freedom from play in the handles d) Transmission and eng decks for each inspection station: - general condition and attachment of the items and equipment in the station. - presence and condition of safetying devices or safety pins, - absence of interference, compliance with clearances and gaps between items - absence of leaks or seepage from couplings and pipes, e) Electrical circuit Inspect the condition and attachment points of the visible parts of the electric looms, components,leads,connectors,bonding braids, wiring, principally at the bulkhead or deck feed-throughs, antennas, navigation light, landing light, electrostatic discharge wicks and other equipment(start-generator, alternator) f) Fire-extinguishing circuit. g) Condition and attachment of fire-extinguisher bottles, correct pressure.

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4	PERMANENT INSTRUCTIONS a) In the event of a fault observed or in the event of doubt during the aircraft inspection refer to the various work cards associated with the ATA chapters concerned. b) Eng oil level - Check the oil level within 15 minutes of shutting down the eng. (eng oil consumption:0.2L/H) c) Free rotation of the eng rotor shaft. d) Oil level in gearboxes e) Operation of engine/MGB cowlings f) Precautions on the ground in strong winds g) Purging-It is recommended to purge the fuel tank every day h) In the event of detecting a fault or experiencing any doubt whistling inspecting the engine
5	PRELIMINARY STEP a) If necessary, wash the aircraft
6	CABIN EXTERIOR a) Oil cooler air inlet grille : Cleanliness b) Air intake : Condition, free of now or foreign bodies c) Radome : Condition, closed d) Windshield wipers : Condition e) TO temperature probe : Condition f) Outside air temperature probe : Condition, attachment point g) Total pressure tapping : Condition, bled, caps fitted h) Landing light retracted : Condition I) Copilot's door : Condition, hinges, locking, emergency jettison mechanism wire-locked J) Battery : Connected, compartment locked k) Nose landing gear : Inflation of oleo and tire, sealing, hoses, condition l) Engine bleed valve and overspeed governor : Check that a flow has occurred from the drain pipe
7	TRANSMISSION DECK, LH SIDE a) LH hydraulic reservoir : Fluid level b) MGB LH fairing : Opening. condition of the fairing, hinge and locks. c) Oil cooling system : Cleanliness - air inlet : Free of foreign bodies - radiator : Condition, attachment points, cleanliness - air plenum and duct : Condition, attachment points - engine oil reservoir : Level, condition cleanliness, cap locked d) Fuel system :Clogged filter indicator retracted e) Hydraulic system : Clogged filter indicator on manifold retracted f) Flight control : Condition, attachment points. g) Engine-MGB drive, flexible coupling on MGB side : Inspection of discs, absence of racks or splaying greater than 1mm h) MGB outlet flexible coupling : Inspection of discs, absence of cracks or playing greater than 1mm i) MGB assembly and accessories : Condition, attachment points, cleanliness j) Servo controls : Condition, attachment points, cleanliness, hoses k) MGB suspension bars : Condition, attachment points l) Engine air intake : Condition, absence of foreign bodies, free rotation of the engine rotor shaft without noise m) MGB LH cowling : Closure, locking
8	ENGINE DECK, LH SIDE a) LH engine cowling : Opening, condition of cowling, hinges and locks b) Engine and accessory : Condition, sealing, cleanliness, pipes, magnetic plug c) Firewall and seal : Condition, attachment point d) Magnetic plug on engine reduction gearbox : No metallic particles, sealing, locking e) Fuel filter : Clogged filter indicator retracted - Drain holes : Not obstructed, clean, no leaks f) Jetpipe : Condition, attachment point - Engine free turbine : Free rotation without noise g) Fire-extinguisher bottle : Correct pressure - LH engine cowling : Closure, Locking

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9	FUSELAGE STRUCTURE LH SIDE a) Passenger door : Condition, hinges, jettison device wire locked, locking b) Fuel mounting plates : Sealing, general condition c) Main landing gear : Inflation of oleo and tire, sealing, general condition, ground electrostatic discharge point d) Static pressure point : Cleanliness, cap fitted
10	TAIL BOOM LH SIDE a) Horizontal stabilizer, side fin, tail skid, navigation light and antennas : Condition, attachment points b) Tail rotor hub : Blade 365A12.0060.01 Visual inspection without removal of the TRH - Condition of the skin for impact damage, debonding, blistering, scores, cracks or distortion - Leading edge erosion shield for perforation or impact damage c) Rotor hub body and fairing :TRH365A33.3501 - Absence of damage (dent,cracks,scratches,corrsion) on the visible faces of the hub body, external journal and fairing - Tip clearance between the blade and the duct - Absence of abnormal play between the journals and the blade roots. - Alignment between the paint witness marks on the fairing/hub body.
11	TAIL BOOM RH SIDE a) TGB : Oil level, condition, cap locked. Fairing in position b) Horizontal stabilizer, side fin, tail skid, navigation lights and antennas : Condition attachment point c) Tail drive shaft fairings : Attachment points, locking d) RH luggage compartment door : Condition, hinges, jettison device wire-locked, locking e) Fuel tank mounting plates : Sealing, condition
12	FUSELAGE STRUCTURE RH SIDE a) Passenger access door : Condition, hinges, jettison device wire-locked, locking b) Fuel tank mounting plates : Sealing, condition c) Main landing gear : Inflation of oleo and tire, sealing, general condition d) Static pressure points : Cleanliness cap fitted
13	ENGINE DECK, RH SIDE a) RH engine cowling : Opening, condition of cowling, hinges and locks b) Engine and accessory : Condition, sealing, cleanliness, pipes, magnetic plug c) Firewall and seal : Condition, attachment point - Engine oil filter : Clogged filter indicator retracted d) Fuel filter : Clogged filter indicator retracted - Drain holes : Not obstructed, clean, no leaks e) Jet pipe : Condition, attachment point - Engine free turbine : Free rotation without noise f) Fire-extinguisher bottle : Correct pressure - RH engine cowling : Closure, Locking
14	TRANSMISSION DECK, RH SIDE a) RH hydraulic reservoir : Fluid level b) MGB RH fairing : Opening. condition of the fairing, hinge and locks. c) MGB, housing, rotor brake and disk : Inspection, ensure that the rotor brake disk does not touch the pads and sleeve d) Engine oil reservoir : Level, condition cleanliness, cap locked e) Fuel system : Clogged filter indicator retracted f) Hydraulic system : Clogged filter indicator on manifold retracted g) Flight control : Condition, attachment points. h) Engine-MGB drive, flexible coupling on MGB side : Inspection of discs, absence of cracks or splaying greater than 1mm.

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15	i) MGB outlet flexible coupling : Inspection of discs, absence of cracks or splaying greater than 1 mm. j) MGB assembly and accessories : Condition, attachment points, cleanliness k) Non electric magnetic plug : Inspection for particles. Condition, locking l) servo controls : Condition, attachment points, cleanliness, hoses m) MGB suspension bars : Condition, attachment points n) Engine air intake : Condition, absence of foreign bodies, free rotation of the engine rotor shaft without noise o) MGB RH cowling : Closure, locking
16	MAIN ROTOR HUB a) Turn the rotor by hand to inspect the MRH as a whole and the main blades b) Pitch change rods : Condition, attachment points, lack of play c) Frequency adapter : Check the absence of local debonding, cracks or blisters over the entire lateral surface of the elastomer pads d) Spherical thrust bearings : P/N LB4-1209-2-1 : Check the absence of debonding, deep cracking or rubber strips emerging from the lateral surface of the external laminated zone. e) Star arms : Static observation : no cracks, splintering or continuous cracking of the paint. f) Cyclic swashplate and bearing assembly : Check that there are no grease runs from the swashplates. Check that there are no color change or flaking of the paint on the swashplates. Feel whether the temperature of the swashplate is normal. g) Main rotor hub : Attachment points, condition of the parts as a whole h) Pitch change rods : Condition, attachment points I) Coning stops : Condition, attachment points, effectiveness of the return springs. j) Labyrinth seals : Condition, attachment points k) Rotating scissors : Condition, attachment points l) Main rotor blades : Condition, attachment points, PU protection, absence of debonding, splaying, dents, scratches, distortion, perforation by erosion. m) Bonding braids : Condition n) Rotor fairing : Condition, attachment points
17	CABIN INTERIOR a) Cabin : Condition, cleanliness, layout of seats and equipment b) Seats, belts and harnesses : Condition, attachment points c) Fire extinguisher and first aid kit : Correctly stowed d) Landing gear control lever : Locked and pinned e) Pilot's door : Condition, hinges, locking, emergency jettison device wire-locked
18	FINAL STEPS a) If necessary, re-install the covers, blanks and caps, as applicable. b) Check correct operation of the locking device. c) Clear away any access equipment employed d) Check in cold weather e) OPT-sand filter insp f) eng health insp.
19	AD2006-057 (ASB 05.00.49) T/R blade check (stainless ring check)
20	AD 2009-188 (ASB05.00.54) TGB OIL LEVEL.
21	AD 2008-135 (ASB05.00.51) CHECK OF THE BUSHES ANC CHECK FOR ABSENCE OF DELAMINATION ON STARFLEX STAR ARM ENDS

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AW139 일일점검표	기장	대장

2011년 월 일		기지 :	검사자 (전)	검사자 (후)	전	후
1	Main and tail rotor tie downs.(if present) - Remove
2	Nose exterior - Condition
3	Pitot-Static Probe(Left side) - Cover removed, condition and un-obstructed.
4	Left side brake lines in brake pedal area(looking through bottom transparent panel) - Condition
5	Nose landing gear - Condition, shock strut extension, leaks, tire pressure
6	Ventilation air intakes(in landing gear bay) - Un-obstructed
7	Nose compartment access door - latched and Secure
8	Pitot-Static Probe(Right side) - Cover removed, condition and obstructions
9	Right side brake lines in brake pedal area(looking through bottom transparent panel) - Condition
10	Windshield and roof transparent panel - Condition, cleanliness
11	Windscreen wiper - Condition
12	Fuselage exterior - Condition
13	Pilot cabin door - Condition, cleanliness, window secure
14	Passenger cabin door - Condition, cleanliness
15	Right side emergency exits - Verify secure
16	Main landing gear - Condition, shock strut extension, leaks, tire pressure
17	Drains and vent lines - Free of obstructions
18	Fuel tank sump area(Right side) - Confirm no leaks
19	Baggage compartment, tie down/net - Condition, cargo(if on board) correctly secure
20	Baggage door - Secure
21	Engine area - check for fuel and/or oil leaks
22	Engine oil level and oil filter impending bypass indicator check
23	Cowling and fairings - Condition and latched
24	Air intakes - Clear and unobstructed
25	Main rotor components and blades - General condition
26	Main rotor damper indicators - Position
27	Engine air intake screen - Cover removed, free of damage and obstruction
28	Engine cowling - Secure
29	Gravity fuel filler cap - Secure
30	Engine exhaust - Cover removed, condition
31	Fire Bottle over-pressure indicator - Green
32	Tail boom exterior - Condition
33	Antenna(1) - Condition
34	Stabilizer - Condition and secure
35	Navigation light - Condition
36	Tail fin - Condition
37	Intermediate and tail rotor gearbox - check for leaks
38	Tail navigation and anti-collision lights - Condition
39	Tail rotor pitch change mechanism - Condition
40	Tail boom exterior - Condition
41	Stabilizer - Condition and secure
42	Navigation light - Condition

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43	Antenna - Condition
44	Tail rotor drive shaft cover - Secure
45	Fuselage exterior - Condition
46	Engine exhaust - Cover removed, condition
47	Fire Bottle over-pressure indicator - Green
48	Baggage compartment, tie down/net - Condition, cargo(if on board) correctly secure
49	Baggage door - Secure
50	Engine area - Check for fuel and/or oil leaks
51	Engine air intake screen - Cover removed, clear of damage and obstructions
52	Engine cowling - Secure
53	Air intakes - Clear and unobstructed
54	Main rotor components and blades - General condition
55	Left side emergency exits - Confirm secure
56	Drains and vent lines - Free of obstructions
57	Fuel tank sump area(Left side) - Confirm no leaks
58	Main landing gear - Condition, shock strut extension, leaks, tire pressure
59	Passenger door - Secure
60	Cowling and fairing - Condition
61	Co-pilot cabin door - Condition, cleanliness, window secure
62	Windshield and roof transparent panel - Condition and cleanliness
63	Windscreen wiper - Condition
64	Passenger Emergency exits - Verify secure
65	Cabin interior - Equipment and cargo secure
66	First Aid Kit - On board
67	Cabin fire extinguisher - Secure, charge
68	Passenger doors - Secure
69	Pilot and Copilot safety belt and inertia reel - Secure
70	Pilot and Copilot seat - Secure
71	Pilot and Copilot flight control - Condition and secure
72	Lower and lateral transparent panels - Integrity, cleanliness and no signs of brake fluid
73	Pilot and Copilot door - Secure
74	Instrument, panels and circuit breakers - Condition and legibility
75	D-Lock External Hoist Hook - General visual inspection for damage
76	Rescue Hoist - O.C of the full-out and full-in limit switches of the hoist assembly for correct operation
77	Rescue Hoist - O.C of the intermediate speed limit switches of the hoist assembly for correct operation
78	Rescue Hoist - O.C of the hand wheel assembly bearing of the hook assembly for freedom of rotation
79	Rescue Hoist - GVI of the BUMPER assembly of the hook assembly for damage and condition
80	Rescue Hoist - GVI of cable cutter of the hoist assembly to make sure that the cotter pin is correctly installed
81	Rescue Hoist - OC of the cable foul assembly of the hoist assembly for correct operation
82	Rescue Hoist - GVI of entire usable length of the cable for damage and condition
83	Rescue Hoist - After use in a salt water environment clean the cable and the hook assembly with fresh water, then dry with a lint free cloth
84	Rescue Hoist oil level sight and adjacent areas - DO a GVI to check for correct oil level and leaks
85	Rescue Hoist boom - Do a GVI for condition, security and damage. Task includes a GVI of adjacent fuselage area
86	Cargo hook electrical cables - Do a GVI for condition and damage, including cleaning of cables water, then dry with a lint free cloth
87	헬기 기내 비치서류 확인

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KA - 32T 일일점검표	기장	대장

년월일	20 . . .	기지						종 류	PR(비행전)	RE(비행간)				RE(비행간)		RE(비행간)	PO(비행후)
								검사자
검 사 항 목			pr	re	re	po	검 사 항 목				pr	re	re	po	검 사 항 목			pr	re	re	po
BEFORE CHECK							Pendulum부착, Bearing Assy 상태								CREW CPMPARTMENT			pr	re	re	po
															Cockpit Door, 비상 도어 작동 상태
점검 준비, 헬기카바, 타이다운 제거							Blade 전연부표면의 부풀림 상태 Rotor Blade손상시⇒운용실험(I.O)								SERVICEABILITY CHECK			pr	re	re	po
판널, 점검 도어 개방							drop stop, flapping restrain 검사								밧데리 장착 상태
헬기 접지, 바퀴멈치 고정							POWER PLANT				pr	re	re	po	Movement과 Swashplate Inchin- ation의 작동상태
비행중 특이사항 청취							apu Eng 오일량								Rotor Sys Brake 작동상태
NOSE SECTION			pr	re	re	po	APU Eng 연료, 오일 누설 흔적								Oil Filter 장착 상태
Skin 상태							공기흡입구, 엔진낫셀내부 이물질								Fuel Filter 장착 상태
도어카바 장착 및 잠금장치 상태							Drain Pipe 청결상태
윈실드 와이퍼 계통 장착 상태							Eng Nacelle, Door Cover Locking								F.C.U Filter 장착 상태
Window 상태							Eng Protection Device 상태(장착시)								СЛГ-300 Winch, Hoisting- swinging Mechanism, Boom상태
STARBOARD SIDE			pr	re	re	po
Sock Absorber 오일 누출							Main Eng 외부 점검								FUELING AND CHARGING			pr	re	re	po
조종석문, 비상 Hatch Cover 상태							Fuel, Oil Sys 점검
우측 및 하부 동체 상태							Flexible Roller Casing Support, Clamp 상태 점검								ЭКСР-46 Signal Flare Bottom 과 Switch Off 상태
연료, 오일, 작동유 누출 여부							Free Turbine, Support Ⅳ,Ⅴ상태								Signal Flare장착, Make Up Colours
5번 연료탱크 주입구, Drain Cock 상태							Eng Exhaust Extenders 상태								연료 탱크내 불순물 제거
전방L/G휠, 스키드, 타이어 상태							엔진낫셀 Heating Sys Pipeline 상태
타이어 압력 상태							방열카바의 과열 흔적								Refuel
유압 댐퍼, Absorber 오일 누출							Alcohol량 점검								Eng Drainage Collective Tank 에서 Fuel Drain
Absorber Sorber 충전상태							Oil량 점검								Main engine Oil Tank의 refill
메인L/G 휠, 스키드, 타이어 상태							엔진낫셀내 Hyd Sys 파이프, 호스 상태								Gear Box의 refill
타이어 압력 상태							Hyd Oil량, 연결부 점검								APU Oil Tank의 refill
휠 브레이크 Pipeline 연결상태							G/B 외부점검, Oil Sys 조임 상태								Hyd Tank의 refill
쇽 압소바 충전 상태 및 오일 누출 검사							G/B Oil량								Alcohol Tank
							CARGO COMPARTMENT				pr	re	re	po
TAILBOOM TAILUNIT			pr	re	re	po	비상구 문의 잠금 작동등 상태								PREVENTIVE MAINTENANCE			pr	re	re	po
우측 및 하부 Tail Boom 상태							Mooring 장비 상태 점검								5km 해상, 습기 지역비행시 엔진 콤프레셔 세척
							Hoist Seat, Belt 상태								엔진 running time 기록
Tail Unit 상태															Cockpit Window 세척검사
							Shut-off, Crossfeed, Fueling Valve 상태
															FINAL OPERATION			pr	re	re	po
							Float, Swivel 작동 상태
좌측 Tail Boom 상태															검사 및 점검후 고장내역 수정
							Safety Belt 작동 상태
															점검창 Close
FUSELAGE PORTSIDE			pr	re	re	po	SIMPLEX FIRE ATTACK SYS				pr	re	re	po	비상구 Clamp로 고정
Cargo Compartment 상태							Main Center Support의 충격, 장착의 안전성, 균열, 과도한마모, 부식 굽음, Hardware의 조임등 검사								co-121M Ice Detector 장착.
조종석문 부착 상태							System Shroud상태 및 안전성 검사								헬기 카바, 브레이드 Lash, Mooring
좌측 및 하부 동체							Fire Attack Tank의 장착 핏팅 및 구조물의 안전성 및 상태검사								공구, 장비 점검 aircraft equipment part2 점검 electronics part3 점검
연료, 오일, 작동유 누출 여부							Hydraulic Lines의 상태 및 장착의 안전성 검사
5번 연료탱크 주입구, Drain Cock							Hydraulic Reservoir의 하이드로릭량 검사 및 헬기장착부 검사								서류 정리
메인L/G휠, 스키드, 타이어 상태							Hydraulic Power Unit의 헬기 장착부, 전기연결부, 하이드로릭 호스아세이 안전성과 상태검사								헬기 Cover, Ice Detector, Wheel Chock, Landing Strut 제거
휠 브레이크 Pipeline 연결상태
타이어 압력상태							Electrical Power Cable 상태 및 연결부의 안전성 검사
Sock Absorber 충전 상태							Foam Tanks탱크의 Liquid Level 검사								비상구 Hatch Door Drop Handle Release, 헨들카바 Close
메인 L/G Sock Absorber 오일 누출
전방 L/G 유압댐퍼, Absorber 오일 누출							Hover Refill Pumpfill 호스 연결부의 상태 및 안전성 검사 Snorkel 펌프 하이드로릭 연결부의 상태 검사								Blade Lash Off, Unfold. Nose Wheel Towing, Steering Arm Rudder 스쿠류 크램프. 수송 피 라미드, Nose Wheel Inline-Of -Flight Latch, Helipad F.O.D 제거
전방 L/G 휠, 스티드, 타이어 상태
ROTOR SYS			pr	re	re	po
Blade lead, Trail Rubber Coating

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검 사 항 목	pr	re	re	po	검 사 항 목	pr	re	re	po	검 사 항 목	pr	re	re	po
BEFORE CHECK	pr	re	re	po	BEFORE NIGHT FLIGHT	pr	re	re	po	FUNCTIONAL CHECK	pr	re	re	po
외부전원 확인					라이트 상태 점검					pitot-static tubes의 작동 여부.
공구 및 장비 준비					돔 라이트 상태 점검					CO-121M ice detector의 작동상태
비행 로그 기록					라이트 상태 점검					CO-121M ice detector의 작동시 cover제거. 점검 후 cover 장착.
비행중 특이사항 청취
NOSE SECTION	pr	re	re	po	СБК램프 레드 라이트 상태 점검
밧데리 및 밧데리실 점검
upy-3, upy-4 상태 점검					호이스트 라이트 점검					FDR БУР-1 작동검사.
충돌 방지등, 서치, 랜딩 라이트 상태					FINAL OPERATION	pr	re	re	po	소화기의 폭약 electric circuit상태.
radio compass 상태 점검					점검중 발견한 결함 점검					FDR 기본자료 기입
TAILBOOM TAILUNIT	pr	re	re	po	DC, AC 외부전원 분리					FINAL OPERATION	pr	re	re	po
py-11 퓨즈의 상태 점검					밧데리 분리					점검중 고장부분 repair
항법 및 위치 라이트 상태 검사					공구 및 교범 등 정리					power supply 분리.
ADF 안테나 상태					HELICOPTER INSTRUMENT PREPARATORY OPERATION	pr	re	re	po	공구 및 작업일지 정리.
ANCC-32 및 RADIO ALT" 상태					공구 및 장비 준비					공구, КПА check
X-PONDER 안테나 상태					비행기록부 기록					excute service papers.
POWER PLANT ROTOR SYS	pr	re	re	po	INSPECTION	pr	re	re	po	SIMPLEX FIRE ATTACK SYS	pr	re	re	po
충돌 방지등 및 로타 팁 라이트 상태					피토트 튜브 계통 점검					하이드로릭 오일 레벨 검사
CARGO COMPARTMENT	pr	re	re	po	POWER PLANT	pr	re	re	po	Hydraulic Power Unit 안전성 검사
UPY-1, UPY-2, PY-7, PY-12 상태					ICE DETECTOR 상태 점검					Hover Refill Pump의 핏팅 및 구조물의 안전성 검사
MH-10 실내통화 계통 점검					소화기 압력 상태					Foam Tank 상태 및 안전성 검사
FLIGHT COMPARTMENT	pr	re	re	po	CARGO COMPARTMENT	pr	re	re	po	Foam Tank 필터의 세척 및 검사
AC, DC 전원 계통 점검					계기 판넬의 상태 점검					소방망 무전기	pr	re	re	po
밧데리 전압 상태 점검					COMPASS SYS의 상태 점검					장착 상태 및 안전성 검사
RECTIFIRE DC 전압 상태 점검					NULL 계기 및 중앙 콘솔의 상태 점검					안테나 장착 상태 및 안전성 검사
ПTC, ПOC 인버터 상태					КИ-13К의 장착 및 상태
비상경고 계통 상태					АК-59П의 장착 및 상태 검사					탐색. 구조 장비	pr	re	re	po
연료펌프 상태 점검					FUNCTIONAL CHECK	pr	re	re	po	안테나 장착상태 및 안전성 검사
SHUT-OFF, CROSS-FEED 밸브 상태					ВД-10ВК의 상태 점검					display Unit 장착 상태 및 안전성 검사
FIRE WARNING SYS 상태					속도 계기 계통 점검					방송장비 시스템	pr	re	re	po
연료지시 계통 점검					GYRO ГПК-52의 상태					스피커 장착 상태 및 안전성 검사
호이스트 절단 계통 점검					GYRO HORIZONS의 상태					전원 케이블 안전성 검사
수동,자동,비상 작동 상태 (카고훅 장착시)					GREBEN의 상태					AMPLIFIER 장착 상태 및 안전성 검사
통신계통 점검					VERTICAL GYRO의 상태					REMOTE CONTROL 장착 상태 및 안전성 검사
APK-19 계통 점검					HSI의 상태
ДИCC-32의 YC-ПC와 БПК 판넬 상태					FLIGHT DIRECTOR의 상태					응급의료장비(E.M.S)	pr	re	re	po
RADIO ALT' 계기 상태					ROLL CONTROL UNIT의 상태					E.M.S장비 상태 및 안전성 검사
X-PONDER 상태					연료량 게이지 계통 점검					전원 케이블 연결부 안전성 검사
통신 및 항법 장비 점검					VIBRATION MONITORING 계기 상태					비상 위치 수신기(E.L.T)	pr	re	re	po
TAPE RECORDER 상태 및 세척					전원공급on, off시 instrument pointers의 정확한 지시					장착 안테나 및 본체 안전성 검사
ДИCC-32의 БПК 계기 점검										기 타 사 항	pr	re	re	po
A-036 RADIO ALT' 점검					CHK -78-1의 상태					밧데리 기한 점검
ДНВ와 МП-617 의 상태 점검					clock의 작동 검사. 태엽을 준다					수직안정판 드레인홀 검사

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