数字机型检查表
Bristell
Bristell B23-912iS Garmin ACE 检查表
通过结构清晰、可编辑的模板,把 Bristell B23-912iS - Rotax 912iS 导入 ACE,让准备工作更快、更从容。
可通过 iPhone、iPad 和 Mac 上的 ACE Checklist Editor 使用。
BRM Aero
Bristell B23-912iS - Rotax 912iS检查表内部预览
查看 Bristell B23-912iS - Rotax 912iS 检查表
浏览完整目录,并预览每个部分最多 3 个条目。
- 检查表数量
- 56
- 条目总数
- 555
- 文件格式
- ACE
仅供预览。此示例并非运行用检查表,请务必使用适用的、经批准的机型资料。
01 PreflightPreflight Inspection 55 个条目
另有 52 个条目可在应用中查看。
02 PreflightBefore Engine Starting 9 个条目
- 01 Allow the Rotax 912iS time to adjust to any new situation. Many actions are followed by a check of a warning light which may take a few seconds.
- 02 Luggage and Loose Objects SECURED
- 03 Rudder Pedal Position SET
另有 6 个条目可在应用中查看。
03 PreflightEngine Starting 46 个条目
- 01 Engine starting is limited to ambient temperature below 50°C and oil temperature above -20°C.
- 02 Backup Battery Check
- 03 Backup Battery Switch ON, WAIT FOR PFD NORMAL MODE
另有 43 个条目可在应用中查看。
04 PreflightAfter Engine Start 7 个条目
另有 4 个条目可在应用中查看。
05 PreflightEngine Warmup 5 个条目
- 01 Power Lever APPROX 2000 RPM FOR APPROX 2 MIN
- 02 Power Lever 2500 RPM UNTIL OIL TEMP 50°C
- 03 Engine Instruments CHECK TEMPERATURES AND PRESSURE
另有 2 个条目可在应用中查看。
06 PreflightBefore Taxiing 4 个条目
- 01 Nav Light (At Night) AS REQUIRED
- 02 Landing and Taxi Light AS REQUIRED
- 03 PFD, EFIS, MFD CHECK ADAHRS STABILIZED
另有 1 个条目可在应用中查看。
07 PreflightTaxiing 4 个条目
- 01 Keep engine speed below 2500 RPM until oil temperature reaches 50°C. Taxi carefully when wind exceeds 20 knots; hold the stick to properly deflect a crosswind.
- 02 Ground Control CHECK NOSE GEAR STEERING
- 03 Brakes CHECK FUNCTION
另有 1 个条目可在应用中查看。
08 PreflightEngine Run-Up 42 个条目
- 01 Perform the run-up heading upwind and not on loose terrain, or the propeller may suck grit and damage the blade leading edges.
- 02 After a full-load ground test allow a short cooling run at idle speed to prevent vapor formation in the cylinder head.
- 03 Park Brake SET, FEET READY ON BRAKE PEDALS
另有 39 个条目可在应用中查看。
09 PreflightBefore Takeoff 15 个条目
另有 12 个条目可在应用中查看。
10 In FlightTakeoff 9 个条目
- 01 Park Brake PUSH KNOB FORWARD TO RELEASE
- 02 Wheel Brakes RELEASE
- 03 Power Lever MAX (FULL FORWARD)
另有 6 个条目可在应用中查看。
11 In FlightShort and Soft Field Takeoff 12 个条目
另有 9 个条目可在应用中查看。
12 In FlightClimb 8 个条目
- 01 Climb Speed BEST RATE 74 KIAS, BEST ANGLE 62 KIAS
- 02 Power Lever MAX (FULL FORWARD)
- 03 Maximum 5800 RPM for 5 minutes, then reduce to maximum continuous 5500 RPM. Consider early reduction to reduce noise and engine stress.
另有 5 个条目可在应用中查看。
13 In FlightCruise 4 个条目
- 01 Fuel Selector LEFT OR RIGHT
- 02 Switch tanks in regular intervals of about 25 min. A low fuel caution indicates about 5 liter usable remaining in that tank, roughly 20 min at moderate power.
- 03 Power Lever SET AS DESIRED, MAX 5500 RPM
另有 1 个条目可在应用中查看。
14 In FlightDescent 5 个条目
另有 2 个条目可在应用中查看。
15 In FlightBefore Landing 14 个条目
另有 11 个条目可在应用中查看。
16 In FlightBalked Landing (Go-Around) 7 个条目
另有 4 个条目可在应用中查看。
17 In FlightLanding 4 个条目
另有 1 个条目可在应用中查看。
18 In FlightShort Field Landing 6 个条目
另有 3 个条目可在应用中查看。
19 In FlightSoft Field Landing 7 个条目
- 01 Touchdown ON MAIN WHEELS
- 02 Flare ADD POWER BEFORE TOUCHDOWN
- 03 Expect excessive ground friction. Power keeps the elevator effective to avoid a violent nose gear drop and keep weight off the nose wheel.
另有 4 个条目可在应用中查看。
20 PostflightAfter Landing 2 个条目
21 PostflightShutdown 17 个条目
另有 14 个条目可在应用中查看。
22 PostflightParking and Tie-Down 7 个条目
另有 4 个条目可在应用中查看。
23 Engine FailureEngine Failure During Takeoff Run 3 个条目
24 Engine FailureEngine Failure Enroute or During Takeoff 17 个条目
- 01 Speed GLIDE AT 67 KIAS
- 02 Below 150 FT AGL LAND IN TAKEOFF DIRECTION
- 03 Over 150 FT AGL AREA WITH LITTLE DEVIATION
另有 14 个条目可在应用中查看。
25 Engine FailureIn-Flight Engine Restart 9 个条目
另有 6 个条目可在应用中查看。
26 Smoke and FireEngine Fire on Ground at Engine Starting 8 个条目
另有 5 个条目可在应用中查看。
27 Smoke and FireFire on Ground With Engine Running 10 个条目
另有 7 个条目可在应用中查看。
28 Smoke and FireEngine Fire During Takeoff 11 个条目
另有 8 个条目可在应用中查看。
29 Smoke and FireEngine Fire in Flight 9 个条目
另有 6 个条目可在应用中查看。
30 Smoke and FireFire in the Cockpit 11 个条目
另有 8 个条目可在应用中查看。
31 Emergency LandingGlide 3 个条目
32 Emergency LandingLanding Without Engine Power 15 个条目
另有 12 个条目可在应用中查看。
33 Emergency LandingPrecautionary Landing 13 个条目
另有 10 个条目可在应用中查看。
34 Emergency LandingLanding With a Flat Tire 3 个条目
35 Emergency LandingLanding With Defective Landing Gear 4 个条目
- 01 Main Gear Damaged TOUCH DOWN AT LOWEST SPEED
- 02 If possible maintain direction during the landing run.
- 03 Nose Wheel Damaged HOLD NOSE OFF AS LONG AS POSSIBLE
另有 1 个条目可在应用中查看。
36 Emergency LandingAircraft Turn Over 5 个条目
- 01 Airplane LEAVE AS SOON AS POSSIBLE
- 02 Mitigates the risk of post-crash fire from leaking fuel.
- 03 Emergency Hammer USE IF CANOPY INTACT
另有 2 个条目可在应用中查看。
37 Unusual AttitudesLoss of Spatial Orientation 3 个条目
38 Unusual AttitudesRecovery From Unintentional Spin 9 个条目
另有 6 个条目可在应用中查看。
39 Rotax 912iS EmergenciesLANE Warning Lamps 6 个条目
- 01 LANE A and B warning lamps OFF is the nominal condition.
- 02 Both Lamps ON Steady LOSS OF ENGINE POWER POSSIBLE
- 03 The system relies on default values and tries to maintain operation. On ground: maintenance required, flight not permissible. In flight: landing as soon as practical is advised.
另有 3 个条目可在应用中查看。
40 Rotax 912iS EmergenciesInternal Generator Failure 13 个条目
- 01 If Generator A fails, the ECU automatically switches the EMS supply to Generator B with no performance drop. Both lamps flash: the airframe is then not supplied by an internal generator.
- 02 Suspected GEN B Failure
- 03 A GEN B failure in flight is not detected by the ECU and not annunciated.
另有 10 个条目可在应用中查看。
41 Rotax 912iS EmergenciesEmergency Engine Shut-Off 4 个条目
- 01 LANE A OFF
- 02 LANE B OFF
- 03 The ECU must be deactivated before the fuel pumps. Shutting down by fuel pumps alone is only allowed in emergency situations.
另有 1 个条目可在应用中查看。
42 Rotax 912iS EmergenciesSprag Clutch Fails to Decouple 3 个条目
43 Rotax 912iS EmergenciesFuel Pressure Outside Range 8 个条目
- 01 Reduce engine power to the minimum necessary and prepare for in-flight shutdown and precautionary landing.
- 02 High Fuel Pressure
- 03 If AUX Pump ON AUX PUMP OFF
另有 5 个条目可在应用中查看。
44 Rotax 912iS EmergenciesLoss of Oil Pressure 5 个条目
- 01 Engine Power REDUCE TO MINIMUM NECESSARY
- 02 Oil Temperature CHECK
- 03 If Temperature High CONTINUE ON LOW POWER
另有 2 个条目可在应用中查看。
45 Rotax 912iS EmergenciesHigh Oil Pressure 4 个条目
- 01 Engine Power REDUCE TO MINIMUM NECESSARY
- 02 Engine RPM (Propeller) REDUCE BELOW 5000
- 03 Speed 67 KIAS
另有 1 个条目可在应用中查看。
46 System EmergenciesVibration 4 个条目
- 01 Engine Speed SET WHERE VIBRATIONS ARE LOWEST
- 02 In case of severe vibration of powerplant origin endangering structural integrity, shut the engine down.
- 03 Land AS SOON AS PRACTICAL
另有 1 个条目可在应用中查看。
47 System EmergenciesAutopilot Malfunction 5 个条目
- 01 AP OFF Button (Stick) PRESS
- 02 Autopilot CB (Blue Marked) PULL
- 03 Takeoff, initial climb, final approach and landing with autopilot engaged, and any operation with a malfunctioning autopilot, are PROHIBITED.
另有 2 个条目可在应用中查看。
48 System EmergenciesControl Upset (Trim or Flap Runaway) 12 个条目
- 01 For an electric flap, aileron or elevator trim system failure leading to runaway or uncontrollable positioning. The CBs of all systems susceptible to runaway are marked blue.
- 02 Flap Runaway
- 03 Speed REDUCE BELOW 84 KIAS (FLAP SPEED)
另有 9 个条目可在应用中查看。
49 System EmergenciesBus System Failure 14 个条目
- 01 The bus system has two main sections, Pilot/GEN A/B with the avionics sub-bus and BATT/ALT C, connected via the BUS TIE circuit breaker.
- 02 Upon Complete Loss of Electric Power
- 03 Backup Power ON
另有 11 个条目可在应用中查看。
50 System EmergenciesOvervoltage 6 个条目
- 01 Overvoltage is more than 15 volts.
- 02 Engine RPM REDUCE (PROPELLER AND POWER)
- 03 GEN A/B and ALT C CHECK TO IDENTIFY FAULTY SIDE
另有 3 个条目可在应用中查看。
51 System EmergenciesInadvertent Icing Encounter 6 个条目
- 01 Operation in known icing conditions is PROHIBITED.
- 02 Pitot Heat ON
- 03 Icing Conditions EXIT, CHANGE ALTITUDE OR TURN BACK
另有 3 个条目可在应用中查看。
52 System EmergenciesLoss of Primary Instruments 5 个条目
- 01 The independent standby EFIS is the primary flight display. In case of Garmin display malfunction or discrepancy refer to the standby EFIS.
- 02 Loss of One GDU460 CONTINUE FLIGHT
- 03 Loss of Both GDU460 LAND AS SOON AS PRACTICAL
另有 2 个条目可在应用中查看。
53 System EmergenciesRPM Overspeed or Propeller Vibration 4 个条目
- 01 Propeller control by the hydraulic governor depends on the oil circuit, a chain of mechanical connections, and the SLPC unit.
- 02 Power Lever ADJUST FOR SMOOTH RUNNING
- 03 If Engine Within Limits LAND AS SOON AS PRACTICAL
另有 1 个条目可在应用中查看。
54 System EmergenciesMain Battery Fault (MAIN BATT Warning) 9 个条目
- 01 A fault detected by the lithium battery management system shows the yellow MAIN BATT warning on the PFD together with the master caution light.
- 02 Slow Flashing Battery LED, Normal Voltage NO ACTION IN FLIGHT
- 03 Possible cell to cell charge imbalance. Report to maintenance; do not dispatch the aircraft.
另有 6 个条目可在应用中查看。
55 System EmergenciesSLPC System Malfunction 6 个条目
- 01 Power Lever ADJUST TO MAINTAIN SAFE FLIGHT
- 02 Most SLPC failures (EMU loss, display bus data loss, governor servo failure, servo blockage or end stop signal loss) leave the propeller RPM constant, at an end stop, or slowly decaying to the minimum RPM stop. Anticipate reduced climb rate...
- 03 Oscillating Propeller RPM
另有 3 个条目可在应用中查看。
56 Rescue SystemAEPS Activation (If Installed) 19 个条目
- 01 Use the airplane emergency parachute system as a last resort for loss of control, loss of structural integrity, loss of spatial orientation or inability to land safely.
- 02 The rescue system must be unlocked during flight to allow immediate use in emergency.
- 03 Minimum effective altitude is 1000 ft above ground. Avoid activation in strong updrafts; leave the updraft first if possible.
另有 16 个条目可在应用中查看。
Garmin 兼容性
在这些 Garmin 设备上加载 Bristell B23-912iS 检查表
ACE 会将此模板导出为标准的 Garmin .ace 检查表文件。确认设备软件版本后,复制到 SD 卡,即可加载到下列任一设备。
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认证/实验/LSA
G3X™ 和 G3X Touch™ 玻璃驾驶舱套件
用于实验飞机和 LSA 飞机的模块化玻璃驾驶舱
适用于 G3X Touch 的机型检查表 -
综合驾驶舱
G3000® 航空电子套件
使用早于 GDU™ 显示软件版本 20.x 的显示软件版本
适用于 G3000 的机型检查表 -
手持导航仪
GPSMAP® 695 和 GPSMAP® 696
便携式航空GPS导航仪
适用于 GPSMAP 695/696 的机型检查表 -
便携式GPS
aera® 796 和 aera® 795
了解如何通过 ACE-Editor 创建要在 aera 795 或 aera 796 上使用的清单
适用于 aera 795/796 的机型检查表 -
GPS导航仪
GTN™系列
移动地图 GPS 导航器,软件版本为 5.13 或更高版本
适用于 GTN 的机型检查表 -
综合驾驶舱
Garmin 综合飞行甲板 (GIFD)
包括 G900X® / G950® / G1000® / G2000® / G3000® / G5000® 飞行甲板,其显示软件版本早于 GDU™ 显示软件版本 20.x
适用于 G1000 的机型检查表
从商店到驾驶舱
让检查表贴合你的飞机
模板省去从零开始的麻烦,同时让你掌控每一个运行细节。
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到手即有清晰结构
打开的是条理清楚的机型专属检查表基础,而不是从空白文档里逐条誊写。
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在 ACE 中完全可编辑
可核对、重新排序、添加批注,并按你的已装设备和经批准的运行资料调整条目。
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随时随地可用
已安装的模板可离线使用,并通过 ACE 在受支持的 Apple 设备间同步可用。
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