출처: 국토교통부
항공기 형식별 비행시험 검사표 관리요령 개정 요약한 글입니다. 항공기 형식별 비행시험 검사표 관리요령 개정 파일 전체가 필요하신 분은 페이지 하단으로 이동하여 항공기 형식별 비행시험 검사표 관리요령 개정 pdf를 다운로드 해주시기 바랍니다.
행정규칙(훈령·예규·고시)
www.molit.go.kr
항공기 형식별 비행시험 검사표 관리요령 개정
비행시험 검사표 목차
1.
AT-502
30.
PA-25-235
2.
BEECH1900D
31.
TRAVEL AIR 95
3.
C90GT
32.
BARON 95-55
4.
Cessna152
33.
Extra EA 300/LT
5.
Cessna172 Series
C-172M, C-172P, C-172R, C-172S(1), 172S(2)
34.
CIRRUS SR20(G1,5,6)
6.
Cessna206 Series - T-206H,
TU-206G , U206G
35.
Hawker 750
7.
Cessna207 Series - T-207A
36.
PITTS S-2B
8.
Cessna208 Series - 208/B
37.
E-90
9.
560(Citation V)
38.
DA-40NG
10.
Cessna 404
39.
AT-802
11.
C-525, C-525(FJ44-1A Engine)
40.
C-500
12.
CL-601-3R
41.
C-182S/182M
13.
G-IV
42.
C-23
14.
GV-SP
43.
KC-100
15.
L410UVP
44.
T188C
16.
M-20J
45.
G-Ⅵ
17.
MXT-7-180
46.
King Air 350HW (B300)
18.
PA31-350
47.
PIPER PA-31T
19.
PA34-200
48.
LAKE-250
20.
PA34-220T
49.
C-550
21.
PA44-180
50.
PA31-310
22.
P68C
51.
CIRRUS VISION SF50
23.
Z-142
52.
P2006T
24.
A188B
25.
R172K
26.
TB-9
27.
DA-42 / DA-42-NG
28.
CIRRUS SR22
29.
SA227-DC
비행시험 검사표
HL
국 토 교 통 부
서울지방항공청
◇ AT-502
1. 일반사항
등 록 부 호
HL
장 소
항공기 기체시간
발동기시간
비 행 일 자
비 행
시 간
BLOCK TIME
RAMP OUT
RAMP IN
FLIGHT TIME
TAKE OFF
LANDING
비 행 목 적
승 무 원
검사원 / 확인정비사
정 부 검 사 관
2. 비행 전 점검
가. 외부점검
1) FUEL DRAINS-----------------------------
SAT□, UNSAT□
2) MAIN GEAR-------------------------------
SAT□, UNSAT□
3) PROPELLER----------------------------
SAT□, UNSAT□
4) SKIN-----------------------------------
SAT□, UNSAT□
5) TRIM TAP-----------------------------
SAT□, UNSAT□
6) T.W LOCK--------------------------------
SAT□, UNSAT□
나. 내부점검
1) CONTROL MOVEMENT------------------
SAT□, UNSAT□
2) TRIM------------------------------
SAT□, UNSAT□
3) PLACARDS----------------------------
SAT□, UNSAT□
4) HARNESS-----------------------------
SAT□, UNSAT□
5) FUEL VALVE---------------------------
SAT□, UNSAT□
6) CONTROL LOCK---------------------------
SAT□, UNSAT□
7) PARKING BRAKE-----------------------
SAT□, UNSAT□
8) ENG CONTROL------------------------
SAT□, UNSAT□
3. 엔진시동 및 엔진관련 점검
가. 시동전 점검
1) ELECTRIC S/W-------------------------
SAT□, UNSAT□
2) CIRCUIT BRAKERS----------------------
SAT□, UNSAT□
3) CAUTION LIGHTS----------------------
SAT□, UNSAT□
4) INSTRUMENT & GAGES-----------------
SAT□, UNSAT□
나. 시동 후 점검
1) I.T.T (400-675℃): ℃----------
SAT□, UNSAT□
2) LO IDLE (51-53%): ℅----------
SAT□, UNSAT□
3) HIGH ILDE (68-70%): ℅--------
SAT□, UNSAT□
4. TAKE OFF POWER
가. TAXING
1) STEERING----------------------------
SAT□, UNSAT□
2) BRAKE-------------------------------
SAT□, UNSAT□
나. TAKE-OFF POWER
1) NG (50-101.5%): %M---------
SAT□, UNSAT□
2) NP (300-2200RPM): RPM-------
SAT□, UNSAT□
3) OIL PRESS (80-100PSI): PSI-----
SAT□, UNSAT□
4) OIL TEMP (10-99℃): ℃--------
SAT□, UNSAT□
5. CRUISE CHECK
가. CRUISE (ALT 1,500FT)
1) I.T.T. (400-675℃): ℃----------
SAT□, UNSAT□
2) VOLT (28V): V--------------
SAT□, UNSAT□
3) NG (50-101.5%): %M-----------
SAT□, UNSAT□
4) NP (1800-2200RPM): RPM-------
SAT□, UNSAT□
5) OIL PRESS (80-100PSI): PSI-----
SAT□, UNSAT□
6) OIL TEMP (10-99℃): ℃--------
SAT□, UNSAT□
나. STALL WARNING
1) POWER ON, FLAP UP-------------------
SAT□, UNSAT□
6. LANDING & ENG SHUT OFF
가. LANDING
1) BRAKE-------------------------------
SAT□, UNSAT□
2) REVERSE-----------------------------
SAT□, UNSAT□
3) TAIL WHEEL LOCK---------------------
SAT□, UNSAT□
나. ENG SHUT DOWN
1) PARKING BRAKE-----------------------
SAT□, UNSAT□
2) ALL S/W OFF--------------------------
SAT□, UNSAT□
3) TIME FOR NG ZERO (35±1SEC)-----------
SAT□, UNSAT□
7. 시험비행결과
기 장 :
서명 :
검사원 또는 확인정비사 :
서명 :
정 부 검 사 관 :
서명 :
시 험 비 행 일 자 :
◇ Beech1900D
1. 일반사항
등 록 부 호
HL
장 소
항공기 기체시간
발동기시간
L/H
R/H
비 행 일 자
20 년 월 일
비 행
시 간
BLOCK TIME
RAMP OUT
RAMP IN
FLIGHT TIME
TAKE OFF
LANDING
비 행 목 적
승 무 원
검사원 / 확인정비사
정 부 검 사 관
2. SERVICE
FUEL
OIL
MAIN
AUX
L/H
LBS
LBS
Q/T
R/H
LBS
LBS
Q/T
3. PRE-FLIGHT INSPECTION------------------------COMPLETE☐
4. PASSENGER/CREW BRIEFING --------------------COMPLETE☐
5. BEFORE ENGINE STARTING CHECK
Refer to P.O.H ----------------------------------COMPLETE☐
6. ENGINE STARTING
1) RIGHT IGNITION and START SWITCH ----------------ON☐
(R FUEL PRESS LO ANNUNCIATOR-EXTINGUISHER)
2) RIGHT CONDITION LEVER (AFTER N1 accelerates thru 12%)
------------LOW IDLE☐
3) ITT and N1-------------------MONITOR (1000℃ maximum)☐
4) Right OIL PRESS---------------------------------CHECK☐
5) Right Ignition and Engine Start Switch(at 50% N1 or above) --------------- OFF☐
6) Right Condition Lever-------------------------HIGH IDLE☐ 7) Right Generator-------------------------RESET, THEN ON☐ a. L and R GEN TIE OPEN Annunciators-----EXTINGUISHED☐
If R GEN TIE OPEN Annunciator Does Not Extinguish:
b. Bus Sense Switch
------HOLD TO RESET FOR APPRXIMATELY 5 SECONDS☐
c. Repeat as required until R GEN TIE OPEN annunciator remains extinguished.
d. Battery----------------------------------------CHARGE☐ (until loadmeter reads approximately 50% or less)
8) L and R AC Bus---------------------------------CHECK☐
a. Left and Right AC Bus -----------------------------ON☐
b. L and R AC BUS Annunciators-------------EXTINGUISHED☐
c. L and R Inverter Frequency --------------------380-420 Hz☐
d. Left AC Bus ---------------------------OFF, Then XFER☐
L AC BUS Annunciator--ILLUMINATED, then EXTINGUISHED☐
(the left AC bus is now powered by the right inverter)
e. Left AC Bus ---------------------------------------ON☐
f. Right AC Bus ---------------------------OFF, then XFER☐
*R AC BUS Annunciator----ILLUMINATED, then EXTINGUISHED
(the right AC bus is now powered by the left inverter)
g. Right AC Bus --------------------------------------ON☐
9) Left Ignition and Engine Start Switch--------------------ON☐ [L fuel press LO ANN-EXTINGUISHED)
10) Left Condition Lever (AFTER N1 accelerates thru 12%)
---LOW IDL☐
11) ITT and N1-----------------MONITOR (1000℃ maximum)☐ 12) Left Oil Pressure------------------------------CHECK☐ 13) Left Ignition and Engine Start (50% N1 or above)-------OFF☐ 14) Right Condition Lever--------------------------LOW IDLE☐ 15) RIGHT Generator ---OFF(L and R GEN TIE OPEN Annunciators
------ILLUMINATED☐
16) Left Generator--------------------GEN RESET, THEN ON☐ (L and R gen TIE OPEN Annumciator-EXTINGUISHED)
17) VOLT METER-------------------------------CHECK☐ a. BATT, R and L GEN, CTR BUS----------27.5 - 29 VOLTS
b. TPL BUS--------------------------------26.5 - 28 VOLTS
c. EXT PWR -------------------------------------0 VOLTS
18) RIGHT Generator----------------GEN RESET, THEN ON☐ 19) GEN TIES Switch---------------------------------OPEN☐
a. L and R GEN TIE OPEN Annumciator -----------ILLUMINATED☐
b. TPL BUS Voltage----------------------- 26.5 - 28 VOLTS☐
20) GEN TIES Switch -----------------------------NORMAL☐
* L and R GEN TIE OPEN Annumciator ---------- EXTINGUISHED☐
21) BUS Sence Switch---------------------------------TEST☐ a. L and R GEN TIE OPEN and BATT TIE OPEN Annunciator
-------------------------- ILLUMINATED☐
b. CTR BUS Voltage---------------------------------ZERO☐
22) BUS Sense Switch--------------------------------RESET☐
* L and R GEN TIE OPEN and BATT TIE OPEN Annumciator
---------------------------- EXTINGUISHED☐
23) Loadmeters-------------------- PARALLELED WITHIN 10%☐
7. BEFORE TAXI CHECK
1) Panel Lights-------------------------------AS REQUIRED☐ 2) Exterior Lights-----------------------------AS REQUIRED☐ 3) Cabin Lights-----------------------------AS REQUIRED☐ 4) Cabin Sign(if installed)-------------------------------FSB☐ 5) Avionics--------------------------------------------ON☐ 6) EFIS Aux Power-------------------------------------ON☐ (AUX ARM Annunciator - ILLUMINATED)
7) Copilot's Electronic Altimeter(if installed)------ILLUMINATED☐ 8) STBY HORIZ PWR or STBY INST PWR----------------ON☐ (AUX ARM Annunciator - ILLUMINATED)
9) EFIS Power Switches---------------------------------ON☐ 10) Flight Data Recorder------------------------------CHECK☐ * Serials With F1000 Flight Data Recorder Installed:
a. FLT RCDR OFF Annunciator------------- EXTINGUISHED
b. REPEAT Button(if installed)------PRESS UNTIL CODING LAMP ILLUMINATES(if desired) Serials UE-362 and after With FA2100 Flight Data Recorder,
If Installed:
* FDR FAULT and FDAU STATUS Annunciators
-----EXTINGUISHED
11) Envir Mode Control--------------------------------AUTO☐ 12) Instruments--CHECK, EFIS BRIGHTNESS SET TO MINIMUM☐ Standby Attitude Indicator-----------------------UNCAGE☐
(at least 1 minute after power applied. OFF Flag out of sight, AUX ARM Annunciator - ILLUMINATED.)
13) Brake Deice(if installed)---------------------------CHECK☐
a. Brake Deice---------------------------------------ON☐
L and R BK DEICE Annunciators----------ILLUMINATED☐
b. Brake Deice--------------------------------------OFF☐
L and R BK DEICE Annunciators-------- EXTINGUISHED☐
14) Stall Warn Heat--------------------------------------ON☐
(STALL HEAT Annunciator - EXTINGUISHED)
15) Power Steering(if installed)------------------AS REQUIRED☐
16) Brakes-------------------------RELEASED and CHECKED☐
17) Cabin Briefer---------------------------------TAKEOFF☐
8. BEFORE TAKEOFF (RUNUP) CHECK
1) EFIS------------------------------------------CHECK☐ a. Pilot and Copilot EADI/EHSI Dim Control
--------------SET BRIGHTNESS LEVEL☐ b. EFIS TEST, Pilot's Side(PLT TEST)---PUSH AND HOLD☐
c. EFIS Test, Copilot's Side(COPLT TEST)
---PUSH AND HOLD☐
d. Pilot and Copilot Display Select Panels
--SET AS REQUIRED☐
2) Air Data Computer(for airplanes equipped with autopilots)
--------------------CHECK☐
a. ADC TEST Button(on EFIS Reversionary panel)
---------PUSH AND RELEASE☐ b. Pilot's Altimeter----------------Digital Window Flagged
With Pointer Indicating 250 Feet☐
c. Altimeter Test Button-------------PUSH AND RELEASE☐ Digital window Flagged and Point Indicates 750 Feet
3) Standby Attitude Indicator
------PITCH ATTITUDE SET, GYRO STABILIZED☐
4) Pilot and Copilot Compass System-----------SLAVED MODE☐ (DG Not Displayed on EHSI's)
5) Mark-Ⅵ GPWS(if installed) (with flaps UP)------------TEST☐ a. GPWS Test Switch-------------------PRESS AND HOLD☐
(GPWS FLAP OVRD, GPWS INOP,& G/S CANCLD Annunciators - ILLUMINATED)
b. BELOW G/S Annunciator
---ILLUMINATED WITHIN 1 SECONDS☐
FOLLOWED BY "GLIDESLOPE" VOICE MESSAGE
c. GPWS Annunciator
-----ILLUMINATED WITHIN 4-5 SECONDS☐
FOLLOWED BY "PULL UP" VOICE MESSAGE SOUNDING 2-6 TIMES
d. GPWS Annunciator----------------------EXTINGUISHED☐ e. GPWS Test Switch--------------------------RELEASED☐ 6) Flight Director-----------------------------------CHECK☐ 7) Altitude Alerter----------------------------------CHECK☐ 8) TCAS791 (if installed)-----------------------------CHECK☐ a. Dim/off Knob-------ROTATE TO ON AND SET BRIGHTNESS☐ b. ENCD ALTM Switch(Avionics Panel)------SET TO ALTM 1☐ c. Pilot's Altimeter---------------------SET TO 29.92 In.Hg☐
d. Test Button (after the Start-Up screen reverts to the 5NM range, or standby screen)----------MOMENTARILY PRESS☐
e. Test Screen----------------------------------MONITOR☐ (Altitude at bottom of screen must be within ±100 feet of pilot's altimeter reading)
f. Voice Message--------------------"TCAS TEST PASSED"☐ (Display reverts to 5nm screen of standby screen)
g. Pilot's Altimeter-RESET TO CURRENT BAROMETRIC SETTING☐ h. ENCD ALTM Switch(Avionics Panel)----------AS DESIRED☐ 9) Autopilot(if installed)------------CHECK(refer to Supplement)☐ 10) Yaw Damp--------------------------------------CHECK☐ a. Rudder Boost/Yaw Damp Select Switch(if installed)-----LEFT☐ b. Yaw Damp-----------------------------------------ON☐ * YD Annunciator On Pilot's and Copilot's EADI
--ILLUMINATED
* YAW Annunciator On Pilot's or Copilot's Flight Contorl Panel ------------ILLUMINATED
c. Rudder Pedals----------CHECK FOR ADDED RESISTANCE☐ d. Control Wheel Disconnect Switch---PRESS TO FIRST LEVEL☐ e. Yaw Damp-----------------------------------------ON☐ f. Rudder Boost/Yaw Control Test Switch-YAW CONTROL TEST☐ (yaw damp will disengage, RUD BOOST OFF Annunciator- ILLUMINATED)
g. Rudder Boost/Yaw Select Switch-------RUDDER BOOSTER☐ (RUD BOOST OFF Annunciator - Extingushed)
h. Rudder Boost/Yaw Damp Select Switch (if install)----RIGHT☐
I. Repeat steps b. thru g.
J. Rudder Boost/Yaw Damp Select Switch-------AS REQUIRED☐
11) Weather Radar-----------------------------------CHECK☐ 12) Cockpit Voice Recorder----------------------------CHECK☐
a. Headset--------------------------PLUG INTO CVR JACK☐ b. CVR TEST Button---PRESS AND HOLD(5 seconds minimum)☐
c. Speak into area mic on glareshield. Voice should be heard in headset.
13) pressurization----------------------------CHECK and SET☐
a. Cabin Altitude--------ADJUST SO THAT "CABIN ALT" DIAL INDICATES AN ALTITUDE 1000 FEET BELOW FIELD PRESSURE ALTITUDE
b. Rate Control Selector-SET INDEX AT 12-O'CLOCK POSITION☐
c. Cabin Pressure Switch-------------------HOLD IN "TEST"☐ d. Cabin Altitude Indicator-CHECK FOR DESCENT INDICATION☐
(May take up to 45 seconds)
e. Cabin pressure Switch(when pressurizing is confirmed)
---------RELEASE TO "PRESS"☐
f. Cabin Controller
----ADJUST SO THAT INNER SCALE(ACFT ALT) IS SET☐ AT PLANNED CRUISE ALTITUDE PLUS 1000 FEET(If this setting does not result in an outer scale)
(CABIN ALT) indication of at least 500 feet above take-off field pressure altitude, adjust as required)
14) Environmental System-----------------------------CHECK☐
a. Envir Mode Control-----------------------------"T" Test☐
L and R ENVIR FAIL, L and R ENVIR OFF Annunciators
---------ILLUMINATED☐
b. Envir Mode Control-------------------------------AUTO☐
c. Bleed Air Valves----------------------------ENVIR OFF☐
L and R ENVIR FAIL Annunciators--------EXTINGUISHED☐
d. Bleed Air Valves---------------------------------OPEN☐
L and R ENVIR OFF Annunciators---------EXTINGUISHED☐
e. Blowers-----------------------------------AS DESIRED☐
f. Temp Control------------------------------AS DESIRED☐
15) Electric Pitch Trim-------------------------------CHECK☐
a. ELEV TRIM Switch---------------------------------ON☐
b. Pilot's and Copilot's Trim Switches----------------CHECK☐
c. Trim Disconnect Switch--PRESS TO 2ND LEVEL AND RELEASE☐
1) PITCH TRIM OFF Annunciator-------------ILLUMINATED
2) Electric Pitch Trim-----------------------DEACTIVATED
d. ELEV TRIM Switch------------------------OFF, then ON☐
PITCH TRIM OFF Annunciator--------------EXTINGUISHED
16) Elevator Trim------------------------SET FOR TAKEOFF☐
Set trim in FWD range for C.G.'s in forward half of envelope.
Set trim in AFT range for C.G.'s in aft half of envelope.
17) Engine Control Friction Locks-------------------------SET☐ 18) Flaps----------------------------------CHECK AND SET☐
19) Flight Controls--------CHECK FOR FREEDOM OF MOVEMENT
AND PROPER DIRECTION OF TRAVEL☐
20) Engine Anti-Ice----------------------------------CHECK☐
21) Other Systems For Icing Flight, if required-----------CHECK☐
22) Autofeather System---------------------CHECK AND ARM☐
a. Autofeather Switch---------------------------------OFF☐
AUTOFTHER OFF Annunciator-------------ILLUMINATED☐
b. Autofeather Switch-------------------------------TEST☐
AFX DISABLE Annunciator-----------------ILLUMINATED☐
c. Power Levers-------------ADVANCE ABOVE 1000 FT-LBS☐ Approx 1000 Ft-Lbs - L and R AUTOFEATHER
and L and R AFX Annunciator---ILLUMINATEDS
AFX DISABLE Annunciator-------EXTINGUISHED
d. Power Levers-------------------RETARD INDIVIDUALLY☐
1) Approx 750 Ft-Lbs:
Opposite AUTOFEATHER and AFX Annunciators-EXTINGUISHED☐
AFX DISABLE Annunciator-------------ILLUMINATED☐
2) Below 500 Ft-Lbs - On-side AUTOFEATHER
and AFX Annunciators------------------EXTINGUISHED☐
3) Advance power lever above 1000 Ft-Lbs and repeat 1) and 2)
by retarding opposite power lever---☐
e. Power Levers-------------------------------------IDLE☐
L and R AUTOFEATHER and left and right AFX
Annunciators---------------------------EXTINGUISHED☐
AFX DISABLE Annunciator----------------ILLUMINATED☐
f. Auto feather Switch-----------------------OFF, then ARM☐
AFX DISABLE Annunciator-----------------EXTINGUISHED
(with switch on OFF or ARM position)
AUTO FEATHER OFF Annunciator----------EXTINGUISHED
(with switch in ARM position)
23) Manual Propeller Feathering------------------------CHECK☐
24) Propeller Controls------------------------FULL FORWARD☐
25) Overspeed Governors and Rudder Boost--------------CHECK☐
a. Prop Test Switch-------------------HOLD TO OVERSPEED
b. Power Levers(individually)---Increase until prop is stabilized at 1535 to 1595 rpm. Continue to increase until rudder pedal resistance is felt onside of advancing power(approximately 1200 Ft-Lbs differential torque). Observe ITT and torque limits.
c. Control Wheel Disconnect Switch----------------1ST LEVEL
1) Rudder Boost---------------------------INTERRUPTED
d. Power Levers-------------------------------- -----IDLE
e. Repeat steps b, c, d on the opposite engine
f. Prop Test Switch----------------------------- --RELEASE
26) Ground Idle Low Pitch Stops-----------------------CHECK☐
a. Power Levers-------------------------------------IDLE☐
b. Condition Levers------------HIGH IDLE, NOTE PROP RPM☐
c. Prop Test Switch------------------HOLD TO LOW PITCH☐
1) L & R RPM
--STABILIZED APPROX 200 RPM BELOW VALUE IN STEP b.
2) PROP GND SOL Annunciator
------ILLUMINATED IN APPROX 8 SECONDS
3) Each Power Lever-------INDIVIDUALLY LIFT & RELEASE
a. L & R RPM
--STABILIZED APPROX 200 RPM BELOW VALUE IN STEP b. AS EACH POWER LEVER IS LIFTED
b. PROP GND SOL Annunciator------------EXTINGUISHED
d. Prop Test Switch-----------------------------RELEASE☐
1) L & R RPM-------VERIFY RETURNS TO VALUE IN STEP b.
2) PROP GND SOL Annunciator----REMAINS EXTINGUISHED
e. Condition Levers-----------------------------LOW IDLE☐
27) Primary Governors-----------------EXERCISE AT 1500 RPM☐
28) Vacuum/Pneumatic Pressure----------------CHECK AT IDLE☐
a. Left Bleed Air Valve-------------------INST & ENIR OFF☐
(Suction in wide green arc, press at 17.5 - 19.0 psi)
b. Right Bleed Air Valve------------------INST & ENIR OFF☐
1) Suction and Pressure----------------------------ZERO☐
2) L and R BL AIR FAIL Annunciator-------ILLUMINATED☐
c. Left Bleed Air Valve------------------------------OPEN☐
(Suction in wide green arc, press at 17.5 - 19.0 psi)
L and R BL AIR FAIL Annunciators--------EXTINGUISHED☐
d. Right Bleed Air Valve-----------------------------OPEN☐
29) Fuel Quantity, Flight and Engine Instruments----------CHECK☐
9. BEFORE TAKEOFF (FINAL ITEM) CHECK
1) Propeller Levers----------------CONFIRM FULL FORWARD☐ 2) Flaps-------------------------------------CONFIRM SET☐
3) Trim-------------------------------------CONFIRM SET☐ 4) Brake Deice(if installed)------------------------------OFF☐ 5) Stall Warn Heat----------------------------CONFIRM ON☐
(STALL HEAT Annunciator - EXTINGUISHED)
6) Left and Right Pitot Heat------------------------------ON☐ (L and R PITOT HEAT Annunciator - EXTINGUISHED)
7) Autofeather----------------------------CONFIRM ARMED☐ 8) Transponder-----------------------------------------ON☐ 9) Ice Protection------------------------------AS REQUIRED☐
a. Eng Auto Ignition, if required-----------------------ARM☐
b. Eng Anti-Ice------------CONFIRM ON(if required), of OFF☐
c. WSHLD Anti-Ice---------------------------NORMAL/HI☐ d. Prop Deice, if required----------------------------AUTO☐
e. L and R Fuel Vent Heat, if required--------------------ON☐
f. Alt Static Heat, if required----------------------------ON☐
10) Bleed Air Valves---------------------------AS REQUIRED☐ 11) Blowers-------------------------------------HI or AUTO☐ 12) Envir Mode Control------------------------AS REQUIRED☐ 13) Generator Load-----------------------------------CHECK☐ 14) Annunciators-------------EXTINGUISHED OR CONSIDERED☐
Takeoff with the BATTERY CHARGE annunciator illuminated is permitted if a decreasing battery charge current is confirmed. See NICKEL_CADMIUM BATTERY CHECK in OTHER NORMAL PROCEDURES of this section.
15) Interior/Exterior Light-----------------------AS REQUIRED☐ 16) V1, VR, V2, Static Take-off Power-----------------CONFIRM☐ 17) TCAS791(if installed)--------------------------------SET☐
a. Display Mode-------------------------------------SET☐
If in Standby Mode:
RNG Button-----------PRESS TO SELECT ABV DISPLAY MODE
(or other desired mode) If not in Standby Mode:TEST Button-PRESS AS REQUIRED TO SELECT ABV DISPLAY MODE(or other desired mode)
b. RNG Button---------PRESS TO SELECT 5 or 10nm RANGE☐
10. TAKEOFF CHECK
1). Power Steering(if installed)----------------------------OFF☐
2). Brakes-------------------------------------------HOLD☐ 3). Power Levers/Prop Levers------Set STATIC TAKE-OFF POWER☐ 4). Autofeather Annunciators--------------------ILLUMINATED☐ 5). Brakes----------------------------------------RELEASE☐
6). VR-----------------------ROTATE TO APPROXIMATELY 8° ]7). Landing Gear (When positive climb established)-----------UP☐
11. CLIMB
1). Flaps(if extended)-------------------------------------UP☐ 2). Envir Mode Control--------------------------------AUTO☐ 3). Bleed Air Valves-----------------------------------OPEN☐ 4). Blowers-----------------------------------AS REQUIRED☐ 5). Yaw Damp------------------------------------------ON☐ 6). Climb Power----------------------------------------SET☐ 7). Propellers--------------------------------------1550 RPM☐
8). Prop Sync-------------------------------------------ON☐ 9). Windshield Anti-Ice------------------------------NORMAL☐ 10). Engine Instruments-----------------------------MONITOR☐
11). Cabin Pressurization-------------------------------CHECK☐
12). Light-------------------------------------AS REQUIRED☐
13). Cabin Sign(if installed)--------OFF, IF CONDITIONS PERMIT☐
12. CRUISE CHECK
1). Cruise Power---------------------------------------SET☐ 2). Autofeather-----------------------------------------OFF☐ 3). Engine Instruments-----------------------------MONITOR☐ 4). Auxiliary Fuel Quantity--------------------------MONITOR☐ (ensure fuel is being transferred FROM THE AUXILIARY TANKS)
5). TCAS791(if installed)---------------------------------SET☐
6). Cabin Sign(if installed)--------OFF, IF CONDITIONS PERMIT☐
13. DESCENT CHECK
1). TCAS791-------------------------------------------SET☐ a. TEST Button----PRESS TO SELECT BLW DISPLAY MODEL☐
(or other desired mode)
b. RNG Button----------PRESS TO SELECT DESIRED RANGE☐ 2). Pressurization---------------------------------------SET☐
a. Cabin Altitude-SET per PRESSURIZATION CONTROLLER SETTING FOR LANDING graph, or so that "CABIN ALT"DIAL INDICATES LANDING FIELD PRESSURE ALTITUDE PLUS 500 FEET
b. Rate Control Selector------------------------AS REQUIRED
3). Altimeter-------------------------------------------SET☐ 4). Windshield Anti-Ice ------------------------AS REQUIRED☐ (well before descent into warm, moist air, to aid in defogging) 5). Prop Deice(at ambient temperatures above 10℃)-----------OFF☐
6). Fuel Balance------------------------------------CHECK☐ 7). Power----------AS REQUIRED to give desired rate of descent☐ 8). Cabin Briefer-----------------------------------LANDING☐
9). Cabin Sign(if installed)-------------------------------FSB☐
14. BEFOR LANDING CHECK.
1) Cabin Sigb(if installed)--------------------------------FSB☐
2). Approach Speeds--------------------------------CONFIRM☐ 3). Cockpit Door(curtain)------------------------------CHECK☐ 4). Autofeather ----------------------------------------ARM☐ 5). Pressurization------------------------------------CHECK☐
6). Flaps-----------------------------------------------17°☐
7). Landing Gear----------------------------------------DN☐
8). Lights------------------------------------ AS REQUIRED☐ 9). Surface Deice------------------------CYCLE, IF REQUIRED☐
15. NORMAL LANDING CHECK
1). Flaps-----------------------------------------------35°☐ 2). Airspeed -------------------------------------------VREF☐
3). Yaw Damp -----------------------------------------OFF☐ 4). Power Levers --------------------------------------IDLE☐ 5). Prop Levers -----------------------------FULL FORWARD☐ After Touchdown :
6). Power Levers ------------LIFT AND SELECT GROUND FINE☐ 7). Brakes ---------------------------------- AS REQUIRED☐
16. AFTER LANDING CHECK
1). Power Steering(if installed)------------------ AS REQUIRED☐ 2). Propeller Levers------------------------------------TAXI☐ 3). Lights------------------------------------AS REQUIRED☐ 4). Eng Anti-Ice---------------------------ON, AS REQUIRED☐ 5). Stall Warn Heat-------------------------------------OFF☐ 6). Left and Right Pitot Heat-----------------------------OFF☐ 7). Ice Protection---------------------------------------OFF☐ a. Eng Auto Ignition-----------------------------------OFF☐
b. WSHLD Anti-Ice-----------------------------------OFF☐ c. Prop Deice-----------------------------------------OFF☐
d. Left and Right Fuel Vent Heat------------------------OFF☐ e. Alt Static Heat-------------------------------------OFF☐
8). TCAS791(if installed)---------------------------------OFF☐ 9). Transponder-----------------------------------STANDBY☐ 10). Trim----------------------------------------------SET☐
11). Flaps-----------------------------------------------UP☐
12). Radar----------------------------------------------OFF☐
17. SHUTDOWN AND SECURING
1). Parking Brakes -------------------------------------SET☐ 2). Power Steering(if installed)----------------------------OFF☐ 3). EFIS Power Switches---------------------------------OFF☐ 4). Standby Attitude Indicator--------------CAGED, POWER OFF☐ 5). EFIS Aux Power Switches----------------------------OFF☐ 6). Avionics Switch-------------------------------------OFF☐ 7). Left and Right AC Bus-------------------------------OFF☐ 8). Oxygen Control(After last flight of the day)--------PUSH OFF☐ 9). Autofeather Switch-----------------------------------OFF☐ 10). Light----------------------------------------------OFF☐ 11). Instrument Emergency Lights(for night shutdown)----------ON☐ 12). Blowers------------------------------------------AUTO☐ 13). Envir Mode Control----------------------------------OFF☐ 14). Fuel System Aux Pump Switches-----------------------OFF☐ 15). Battery----------------------------------------CHARGE☐
16). ITT----------------STABILIZED AT MINIMUM OBTAINABLE TEMPERATURE FOR ONE MINUTE
17). Condition Levers --------------------------FUEL CUT OFF☐ 18). Propellers-----------------------------------FEATHERED☐ 19). Overhead Panel Switched-----------------------------OFF☐ 20). Battery and Generator Switches(below 15% N1)-----------OFF☐ 21). Control Locks-----------------------------------INSTALL☐ 22). Instrument Emergency Lights--------------------------OFF☐ 23). Cabin Door----------------------------------------OPEN☐ 24). Lavatory Trash Container----CHECK FOR EVIDENCE OF FIRE☐ 25). Tie Downs and Chocks---------------------------INSTALL☐ 26). Parking Brake---------------------------------------OFF☐ 27). External Covers---------------------------------INSTALL☐
18. 시험비행결과
기 장 :
서명 :
검사원 또는 확인정비사 :
서명 :
정 부 검 사 관 :
서명 :
시 험 비 행 일 자 :
◇ C90GT ,<King Air>
1. 일반사항
등 록 부 호
HL
장 소
항공기 기체시간
발동기시간
L/H
R/H
비 행 일 자
20 년 월 일
비 행
시 간
BLOCK TIME
RAMP OUT
RAMP IN
FLIGHT TIME
TAKE OFF
LANDING
비 행 목 적
승 무 원
검사원 / 확인정비사
정 부 검 사 관
2. SERVICE
FUEL
OIL
NACELL
WING
L/H
G/L
G/L
Q/T
R/H
G/L
G/L
Q/T
3. PRE-FLIGHT INSPECTION----------------------------COMPLETE☐
4. PASSENGER/CREW BRIEFING ------------------------COMPLETE☐
5. BEFORE ENGINE STARTING CHECK
Refer to P.O.H --------------------------------------COMPLETE☐
6. ENGINE STARTING
1) BOOSTER PUMP----------------------------------------ON☐
2) GEN TIES ---------------------------------MANUAL CLOSE☐
[MAN TIES CLOSE] - ILLUMINATED
[R GEN TIE OPEN] & [R GEN TIE OPEN] - EXTINGUISHED
3) Right Ignition and Engine Start-----------------------------ON☐
[R IGNITION ON] - ILLUMINATED
4) Right Condition Lever (12% N1 minimum)--------------LOW IDLE☐
5) Rright ITT and N1 ---------------MONITOR (1900°C maximum)
6) Right Oil Pressure-------------------------------------CHECK☐
7) Right Ignition and Engine Start (51% N1 or above)------------OFF☐
8) Right Generator------------------------------RESET, THEN ON☐
[R DC GEN], [MAN TIES CLOSE], [L GEN TIE OPEN]
& [R GEN TIE OPEN] - EXTINGUISHED
9) Battery---------------------------------------------CHARGE☐
(until loadmeter reads approximately 50% or less)
10) Left Ignition and Engine Start-------------------------------ON☐
[L IGNITION ON] - ILLUMINATED
11) Left Condition Lever (12% N1 minimum)----------------LOW IDLE☐
12) Left ITT and N1 ------------------MONITOR (1900°C maximum)
13) Left Oil Pressure--------------------------------------CHECK☐
14) Left Ignition and Engine Start (51% N1 or above)-------------OFF☐
15) Left and Right Prop RPM------------------------1100 MINIMUM☐
16) Voltmeter (L GEN)----------------------------27.5 to 29.0 Volts☐
17) Left Generator-------------------------------RESET, THEN ON☐
[L DC GEN] - EXTINGUISHED
18) Right Generator------------------------------RESET, THEN ON☐
[L GEN TIE OPEN] & [R GEN TIE OPEN] (remain extingusher with switch in the reset position)
19) Condition Lever---------------------------------AS REQUIRED☐
20) ENGINE STARTING-------------------------------COMPLETE☐
7. BEFORE TAXI CHECK
1) Transfer Pumps-----------------------------------------AUTO☐
2) Crossfeed----------------------------------------------AUTO☐
3) Both Inverters-----------------------------------------CHECK☐
(freq'=360~420Hz, volts=105~120,
[INVERTER] illuminates with inverter off)
4) Inverter To Be Used---------------------------------------ON☐
5) Electrical System (N-20)--------------------------------CHECK☐
6) Avionic Master--------------------------------------------ON☐
7) EFIS Aux Power------------------------------------------ON☐
8) EFIS Power----------------------------------------------ON☐
9) External Light----------------------------------AS REQUIRED☐
10) Environmental System Control (N-21)-----------------------SET☐
(observe N1, ITT, and generator limits if
air conditioning or electric heat is used)
11) Cabin Sign-------------------------FSB OR NO SMOKE & FSB☐
12) Instruments------------------------------------------CHECK☐
8. TAXI CHECK
1) Brakes ---------------------------------------------CHECK☐
2) Gyros-----------------------------------------------CHECK☐
9. BEFORE TAKEOFF (RUNUP) CHECK
1) Boost Pumps and Auto Crossfeed (N-21)-------------------TEST☐
2) Avionics and Radar------------------------------------CHECK☐
3) EFIS (if installed)-------------------------------------CHECK☐
4) Pressurization (N-22)--------------------------CHECK and SET☐
5) Autopilot and Yaw Damp (if installed) (N-22)--------------CHECK☐
6) Electric Elevator Trim (N-23)---------------------------CHECK☐
7) Trim Tabs----------------------------------------------SET☐
8) Engine Control Friction Locks-----------------------------SET☐
9) Flaps--------------------------CHECK AND SET AS DESIRED☐
10) Flight Controls--------------------------------------CHECK☐
FREEDOM OF MOVEMENT AND PROPER DIRECTION OF TRAVEL
11) Governors, Rudder Boost, & Pneu/Vac Systems (N-24)-----CHECK☐
12) Autofeather (N-24)-----------------------------------CHECK☐
13) Autofeather-------------------------------------------ARM☐
14) Prop Feathering (manual)----------------------CHECK (Lo Idle)☐
15) Ice Protection Equipment (if required) (N-25)-------------CHECK☐
16) Fuel Quantity, Flight and Engine Instruments-------------CHECK☐
17) Takeoff Speeds------------------------------------CONFIRM☐
10. BEFORE TAKEOFF (FINAL ITEM) CHECK
1). Engine Auto Ignition ------------------------ARM (if required)☐
[L IGNITION ON] & [R IGNITION ON]---- ILLUMINATED
2) Engine Anti-Ice--------------------------------AS REQUIRED☐
[L ENG ANTI-ICE] & [R ENG ANTI-ICE]--- ILLUMINATED, if on
3) Autofeather--------------------------------CONFIRM ARMED☐
4) Exterior Lights--------------------------------AS REQUIRED☐
5) Ice Protection---------------------------------AS REQUIRED☐
a. Windshield Anti-Ice---------------------NORMAL (if required)
b. Prop Deice--------------------------------ON (if required)
c. Left and Right Fuel Vent Heat---------------------------ON☐
d. Stall Warning Heat-------------------------------------ON☐
e. Left and Right Pitot Heat-------------------------------ON☐
6). Transponder-------------------------------------------ALT☐
7). Prop Levers-----------------------CONFIRM FULL FORWARD☐
8). Trim----------------------------------------CONFIRM SET☐
9). Flaps----------------------------------------CONFIRM SET☐
10). Bleed Air Valves----------------------------CONFIRM OPEN☐
11). Interior Lights--------------------------------AS REQUIRED☐
12). Generator Load--------------------------------------CHECK☐
13). Battery Ammeter------------------------------------CHECK☐
(charge current 10 amps or less if required)
14). Annunciators-----------------EXTINGUSHER OR CONCIDERED☐
15). BEFORE TAKEOFF CHECK-----------------------COMPLETE☐
11. TAKEOFF CHECK
1). Brakes------------------------------------------------HOLD☐
2). Power--------------------------------------------------SET☐
3). [L AUTOFEATHER] nad [R AUTOFEATHER]------ ILLUMINATED☐
4). Brakes---------------------------------------------RELEASE☐
5). Power Levers-------------------------ADJUST TO MAINTAIN
MINIMUM TAKEOFF POWER
6). VR-------------------------ROTATE TO APPROXIMATELY 10°
7). Landing Gear (When positive climb established)----------------UP☐
8). Flaps ( At 108 knots minimum )-----------------------------UP☐
12. CLIMB
1). Landing Gear--------------------------------------------UP☐
2). Climb Power--SET(Observe maximum ITT, TORQUE and N1 Limits)
3). Prop RPM---------------------------------------------1,900☐
4). Windshield Anti-Ice---------------------------------NORMAL☐
5). Engine Instruments---------------------------------MONITOR☐
6). Cabin Sign------------------------------------AS REQUIRED☐
7). Cabin Pressurization-----------------------------------CHECK☐
13. CRUISE CHECK
1). Cruise Power------SET per CRUISE POWER TABLES or GRAPHS☐
2). Autofeather--------------------------------------------OFF☐
3). Engine Instruments---------------------------------MONITOR☐
4). Pressurization-------------------------------------MONITOR☐
(Refer if cruise altitude changes by 1000 feet or more)
14. DESCENT CHECK
1). Pressurization ------------------------------------------SET☐
a. Cabin Altitude Selector Knob ----------------------------SET☐
per PRESSURZIATION CONTROLLER
SETTING FOR LANDING table, or so that
CABIN ALT dial indicates landing field
pressure altitude plus 500 feet
b. Rate Control Selector Knob----------------------AS REQUIRED☐
2). Altimeter ----------------------------------------------SET☐
3). Cabin Sign ------------------------------------AS REQUIRED☐
4). Windshield Anti-Ice -----------------------------AS REQUIRED☐
(well before descent into warm, moist air, to aid in defogging)
5). Power ----------------------------------------AS REQUIRED☐
6). Recognition Lights------------------------------AS REQUIRED☐
7). Seats and Tables --------------------------------POSITIONED☐
a. ALL Seats - Seatbacks Uplight, Headsets fully extended.
b. Lateral-tracking Seats - Outboard Position
c. Tables - Stowed
15. BEFOR LANDING CHECK.
1) Approach Speed ------------------------------------CONFIRM☐
2). Pressurization ---------------------------------------CHECK☐
3). Cabin Sign------------------------FSB OR NO SMOKE & FSB☐
4). Autofeather -------------------------------------------ARM☐
5). Flaps -------------------------------------------APPROACH☐
6). Landing Gear ----------------------------------------DOWN☐
7). Lights -------------------------------------- AS REQUIRED☐
8). Radar --------------------------------------- AS REQUIRED☐
9). Surface Deice---------------------------CYCLE AS REQUIRED☐
If Residual ice Remains On Wing Boots :
10). Approach Speed and Landing Distance ----------------INCREASE☐
16. NORMAL LANDING CHECK
1). Flaps------------------------------------------------DOWN☐
2). Airspeed ----------------NORMAL LANDING APPROACH SPEED☐
3). Yaw Damp ---------------------------------------------OFF☐
4). Power Levers ------------------------------------------IDLE☐
5). Prop Levers ---------------------------------FULL FORWARD☐
After Touchdown :
6). Power Levers ----------------LIFT AND SELECT GROUND FINE☐
7). Brakes -------------------------------------- AS REQUIRED☐
17. MAXIMUM REVERSE THRUST LANDING
1). Flaps ------------------------------------------------DOWN☐
2). Airspeed ------------------NORMAL LANDING APPROACH SPEED
(increase with residual ice)
3). Yaw Damp ---------------------------------------------OFF☐
4). Power Levers ------------------------------------------IDLE☐
5). Prop Levers ---------------------------------FULL FORWARD☐
After Touchdown :
6). Power Levers ----------------LIFT AND SELECT GROUND FINE☐
7). Brakes ---------------------------------------AS REQUIRED☐
18. AFTER LANDING CHECK
1). Landing and Taxi Lights ----------------------- AS REQUIRED☐
2). Engine Anti-Ice -----------------------------------------ON☐
3). Ice Protection ------ ------------------------- AS REQUIRED☐
4). Transponder -------------------------------------STANDBY☐
5). Radar ------------------------------------STANDBY or OFF☐
6). Electrical Load -----------------------------OBSERVE LIMITS☐
7). Trim -------------------------------------------------SET☐
8). Flaps --------------------------------------------------UP☐
9). Pressurization ------------------------------------VERIFY 0 ☐
19. SHUTDOWN AND SECURING
1). Parking Brakes -----------------------------------------SET☐
2). Transfer Pumps ----------------------------------------OFF☐
3). Crossfeed ------------------------------------------CLOSED☐
4). EFIS Aux Power ---------------------------------------OFF☐
5). EFIS Power -------------------------------------------OFF☐
6). Avionic Master -----------------------------------------OFF☐
7). Inverter -----------------------------------------------OFF☐
8). Autofeather --------------------------------------------OFF☐
9). Vent Blower ------------------------------------------AUTO☐
10). Cabin Mode Control -------------------------------------OFF☐
11). Subpanel Switch -----------------------OFF OR AS REQUIRED☐
12). Oxygen System Control ----------------------------PUSH OFF☐
13). Battery -------------------------------------------CHARGE☐
14). ITT ------------------STABILIZED AT MINIMUM OBTAINABLE
TEMPERATURE FOR ONE MINUTE 15). Instrument Emergency Lights (if desired for a night shutdown)--ON☐
16). Power Levers -----------------------------------------IDLE☐
17). Condition Levers -----------------------------FUEL CUT OFF☐
18). Props --------------------------------------------FEATHER☐
19). Booster Pumps (below 10% N1) ---------------------------OFF☐
20). Control Locks -------------------------------- AS REQUIRED☐
21). Parking Brakes (if required)-------------------------------OFF☐
22). Battery and Generator -----------------------------------OFF☐
23). Overhead Panel Light Switchs -------------------AS REQUIRED☐
24). Instrument Emergency Lights -----------------------------OFF☐
25). External Covers, Tie Downs and Chocks --INSTALL AS REQUIRED☐
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