image imagewidth (px) 736 6.74k | text stringlengths 0 32.8k |
|---|---|
Diamond AIRCRAFT
DA 40 Series
AMM
Next to the LH and RH fuel filler neck If OÄM 40-348 is carried out:
Usable Fuel Qty .: 14.0 US gal / 53,0 |
WARNING USE ONLY JET FUEL JET-A1 or see Airplane Flight Manual
Total Fuel Qty .: 15.0 US gal / 56,8 |
If OÄM 40-348 and OAM 40-130 is carried out:
If MAM 40-139
Usable Fuel Qty ... | |
| | 0 | 1 | 2 |
|---:|:----|:--------------------|:-----------|
| 0 | | STROBE LIGHT SYSTEM | |
| 1 | | | MODEL 182Q |
## SUPPLEMENT
## STROBE LIGHT SYSTEMUES
## SECTION 1 GENERAL
The high intensity strobe light system enhances anti-collision p... | |
## Geodetic datum
A minimum set of parameters required to define location and orientation of the local reference system with respect to the global reference system/frame.
## Geoid
The equipotential surface in the gravity field of the Earth which coincides with the undisturbed mean sea level (MSL) extended continuously ... | |
Flight Controls
Diamond AIRCRAFT
DA 40 Series AMM
Intentionally left blank
Page 102
27-38-00
18 Oct 2019
| |
OXYGEN DURATION CHART (48 CUBIC FEET CAPACITY)
1800
GAGE PRESSURE - (PSI)
PILOT & 3 PASSENGERS
PILOT & 2 PASSENGERS
PILOT & 1 PASSENGER
1600
1400
PILOT ONLY
1200
1000 :unselected:
800
600 :unselected:
400
200
O
2 3 4 5 6 7 8
9
OXYGEN DURATION - (HOURS)
NOTE: This chart is based on a pilot with an orange color-coded oxy... | |
Diamond AIRCRAFT
8
7
6
1
5
1
4
3
F
VOLTAGE REGULATOR
NEF DA4-4224-10-42
ALT FAL
DHCRIETE IN 1
STARTER MOTOR
ANALOG IN 6 HI
INTEGRATED AMONIO
RB-400 1 B
.
TTOMAMAEL
J3414
PM414
INTEGRATED ANCHICA
RB-40028
GEARS IN1A GEARS 46 18
77011004
E
PITOT SWITCH
PITOT HEAT AMPS SENSOR
PITO
ANALOG IEN
DO IN & LO
1018822WH
MD1842ZWE... | |
| | SAMPLE LOADING PROBLEM | SAMPLE AIRPLANE | | YOUR AIRPLANE | |
|---:|:------------------------------------------------------------------------------------------... | |
PAGE INTENTIONALLY LEFT BLANK
| |
DA 40 Series AMM
Diamond AIRCRAFT
Auto Flight
- ALERT (altitude alert) annunciation. This annunciation is only used when the altitude preselect option is installed.
- It illuminates continuously in the region of from 200 to 1000 feet from the selected altitude if the airplane was previously outside of this region.
- It... | |
Indicating Systems
Diamond AIRCRAFT
DA 42 Series AMM
## Trouble-Shooting
## 1. General
The table below lists the defects you could have with the control panel in the center console. If you have the trouble detailed in the Trouble column read across to the Possible Cause column. Then do the repair given in the Repair co... | |
Landing Gear
Diamond AIRCRAFT
DA 42 Series
AMM
B. Install the Parking Brake Valve
| | | Detail Steps/Work Items ... | |
PAGE INTENTIONALLY LEFT BLANK
| |
Oil System
Diamond AIRCRAFT
DA 40 Series
AMM
Intentionally left blank
Page 2
79-TITLE
18 Oct 2019
| |
Indicating Systems
Diamond AIRCRAFT
DA 40 Series AMM
Intentionally left blank
Page 204
31-12-00
18 Oct 2019
| |
Table 25-2. Common Weather Chart Symbols
| | Feature | Symbol | Definition |
|---:|:----------|:---------|:---------------------------... | |
## WT9 Dynamic LSA / Club Aircraft Maintenance Manual
AERO POOL SINCE 1991
- AS-AMM-01-000
(2) Nose wheel bearings replacement:
(a) Remove the wheel (Chapter 32-40).
(b) Deflate the tire to zero pressure.
(c) Separate the tire (1, Fig. 32-16) from the discs (2; 3).
(d) Unscrew the bolts (4) and disassemble the discs (2... | |
DA 42 Series AMM
Diamond AIRCRAFT
Engine Indicating
00
Crankshaft Sensor
Crankshaft Sensor
Screw
Screw
A
:selected:
Figure 2: Crankshaft (RPM) Sensor Installation for the TAE 125-01 Engine
77-40-00
15 Nov 2021
| |
Flight Controls
Diamond AIRCRAFT
DA 42 Series
AMM
Intentionally left blank
Page 102 15 Nov 2021 27-39-00
| |
PERIODIC INSPECTIONS
WT9 Dynamic LSA / Club Aircraft Maintenance Manual - ·AS-AMM-01-000
AERO
POOL
SINCE 1991
This page is left blank intentionally
| | GENERAL | | Chapter 05-00 |
|---:|:----------|:-----------------|:----------------|
| 0 | Page 05-6 | Effectivity: ALL | 22. 05. 2017 | | |
Flight Controls
Diamond AIRCRAFT
DA 42 Series
Push Rods from Fuselage
To RH Wing
Actuator Control Rod
Flap Idler Lever
in the Fuselage
Push Rods from Fuselage
LH Wing Shown, RH Wing Similar
Rigging Pin Hole
Left Flap Rib
1
Left Inner Flap
8
Guide Rollers
To Left Outer Flap
Figure 2: Flap Pushrods and Bellcranks in the ... | |
Figure 5-59. Wing and horizontal stabilizer vortices on an MD-11.
and-level flight, it is also said to have positive dynamic stability. The airplane, however, may pass through level flight and remain pitched down, and then continue the recovery process by pitching back up. This pitching up and then down is known as an ... | |
Controlling the wind correction angle during a turn can be complex to understand. The concept may be understood by comprehending the difference between the number of degrees that the airplane has turned over the ground versus the number of degrees that the airplane has turned in the air. As an example, assume the airpl... | |
## UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION STANDARD AIRWORTHINESS CERTIFICATE
| | 1 NATIONALITY AND REGISTRATION MARKS | 2 MANUFACTURER AND MODEL | 3 AIRCRAFT SERIAL NUMBER | 4 CATEGORY |
|---:|:---------------------------------------|:---------------------------... | |
## Normal Take-off and Landing
10. It is normal practice to hover the helicopter immediately prior to landing and immediately after take-off. This enables the pilot to correct for any lateral motion before touching down and also allows him to check that the helicopter has been correctly loaded before committing the air... | |
There, amidst divans, deep rugs, tent hangings and mementos of the desert, she dismissed the Fremen amazons Stilgar had assigned as her personal guardians.
Watchdogs, more likely! When they had gone, muttering and objecting, but more fearful of her than they were of Stilgar, she stripped off her robe, leaving only the ... | |
| | AIRBUS DEFENCE AND SPACE | CABIN SYSTEMS PRERECORDED ANNOUNCEMENTS |
|---:|:----------------------------|:----------------------------------------------------|
| 0 | A330-GOS | |
| 1 | CABIN CREW OPERATING MANUAL | OPERATION ... | |
Diamond AIRCRAFT
DA 42 Series AMM
## Section 32-20 Nose Landing Gear
## 1. General
The nose landing gear is housed in the nose gear bay and is attached to the surrounding structure by the nose landing gear mounting-bracket. The nose gear leg has an oleo-pneumatic strut and a single wheel. The nose gear bay has 2 compos... | |
AIRBUS DEFENCE AND SPACE
CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) PRELIMINARY PAGES SUMMARY OF HIGHLIGHTS
A330-GOS CABIN CREW OPERATING MANUAL
| | Localization Title | Toc Index | ID | Reason |
|---:|:------------------------------------|:------------... | |
Diamond AIRCRAFT
DA 42 Series AMM
## TABLE OF CONTENTS
## CHAPTER 32 LANDING GEAR
| | 0 | 1 | 2 |
|---:|----:|:------------------------|----:|
| 0 | 1 | General | 1 |
| 1 | 2 | Description | 1 |
| 2 | 3 | Operation on the Ground | 4 |
| 3 | 4 ... | |
DA 40 Series
AMM
Diamond AIRCRAFT
Engine Controls
## C. Power Lever
Figure 3 shows the engine power lever installation. The power lever is a large 'T'-shaped lever. It is located in the center console. The power lever has a friction lock. The lock holds the power lever in the set position. A bar below the 'T' lets you ... | |
RSAFOSP 14 RIFRM
## OFFICIAL CLOSED
The process of correlating a particular radar return or radar position symbol with a specific aircraft.
## Radar Information Service (RIS)
An on-request service provided to assist pilots of VFR flights, within radar coverage in Class E and Class G airspace, to avoid other aircraft or... | |
DA 40 Series AMM
Diamond AIRCRAFT
Power Plant
## 7. Engine Starting
See the Lycoming Operator's Manual for operating limits.
| | | Detail Steps/Work Items | Key Items/References |
|---:|:-----|:--------------------... | |
Face-Dancer disguises. Other histories point out the spies in Muad'dib's household. They make much of the Dune Tarot which clouded Muad'dib's powers of prophecy. Some show how Muad'dib was made to accept the services of a ghola, the flesh brought back from the dead and trained to destroy him. But certainly they must kn... | |
Standard Practices/Structures
Diamond AIRCRAFT
DA 42 Series AMM
## 5. Holding a Component During a Repair
You must hold a component in the correct position when you do a repair. If you do not hold a component correctly it may move during the repair and cause further damage. It can also change the airplane alignment.
Ho... | |
AERO
POOL SINCE 1991
## WT9 Dynamic LSA / Club Aircraft Maintenance Manual AS-AMM-01-000
PERIODIC INSPECTIONS
5. SCHEDULED INSPECTION PROGRAM
| | 0 | 1 | 2 | 3 |
|---:|:--------------------------------------------|:-----------------------|:-... | |
4/20/23
AIM
TBL 4-3 Item 10b Surveillance Capabilities
| | 0 | 1 ... | |
LA MS CSTL WTRS CIG OVC001 - OVC006. TOPS TO FL240. VIS 1/4 - 3/4 SM FG. SWLY WND. 16Z CIG OVC010 VIS 2 SM BR. OCNL VIS 3-5SM -RN BR OVC009. OTLK ... MVFR CIG VIS. FL CIG BKN020 TOPS TO FL180. VIS 1-3 SM BR. SWLY WND. 18Z BRK030. OTLK ... MVFR CIG.
At this time, there are no SIGMETs or PIREPs reported. However, there a... | |
(2) Subsequent Actions - Receiver. When spokes damage occurs, the drogue may shed debris; and there is a significant probability of the receiver's engine(s) ingesting the debris. When clear of the tanker, receiver pilots are to check engine instruments to assess possible damage, and if practical, have an airborne inspe... | |
2.7 Light aircraft flying on airways shall, in addition to radio communication apparatus, be equipped with a radio compass.
2.8 All fixed wing aircraft are to use the runway for take-off and landing. After landing, pilots are to vacate the runway via the first available exit taxiway to the left or right or as instructe... | |
DA 40 Series AMM
Diamond AIRCRAFT
Wiring Diagrams
10 9
1
8
7
6
1
5
4
3
2
F
-
E
-
D
MAIN BUSS
FAN/OAT
J3120 P3120
31200A22 31201A22N 2
1
O.A.T.
31201A22N
GS-IP-2
C
B
A
-
| | REV. | SCHEMATIC | DRAWING NO. | SHEET |
|---:|:-------|:------------|:---------------|:--------|
| 0 | C | O.A.T. | DA4-9... | |
UNITI
CH
C
SO
N
EBeč Effect
Comul
-------
Carlos
UNITEL
CH
SO
Certogel
UNITED!
CHA
NOR
Efectivi
ConsulSut Map://www. Warning: RX
Published li Carlographi Department
## Federal Aviation Administration
## UNITED STATES GOVERNMENT FLIGHT INFORMATION PUBLICATION
CHART SUPPLEMENT SOUTHEAST U.S.
Effective 0901Z
15 SEP 2016 1... | |
## OFFICIAL (OPEN) ANNEX A TO NATIONAL SRD - SINGAPORE
## APPENDIX A2 - ANNEX A TO NATIONAL SRD - SINGAPORE A330
## MRTT BOOM
Figure A2-1: Singapore A330 MRTT Pilot Director Lights Diagram
Down
D
F
Forward
Elevation Position
Telescopic Position
Up
A
Att
Flight Direction
Figure A2-2: Singapore A330 MRTT Boom Pilot Direc... | |
## OFFICIAL CLOSED
## Go-Around Mode
25.115 In most systems the go-around mode is armed as a standard procedure whilst on final approach; in the system described, GA is armed automatically when flap is selected or on capturing the ILS glideslope. When required, the go-around button on the throttle lever is pressed, com... | |
STANDARD
PRACTICES - AIRFRAME
## WT9 Dynamic LSA / Club
Aircraft Maintenance Manual AS-AMM-01-000
AERO
POOL
SINCE 1991
This page is left blank intentionally
| | Chapter 20-20 | | SAFETYING |
|---:|:----------------|:-----------------|:-------------|
| 0 | Page 20-18 | Effectivity: ALL |... | |
AIM
1. Minimum altitude will be depicted with the altitude value underscored. Aircraft are required to maintain altitude at or above the depicted value, e.g., 3000.
2. Maximum altitude will be depicted with the altitude value overscored. Aircraft are required to maintain altitude at or below the depicted value, e.g., 4... | |
AD 2.WSSS-43 25 JAN 2024
| | Name | Latitude | Longitude | Radius/Distance from VTK | Radius/Distance from SJ |
|---:|:-------------|:-----------|:------------|:---------------------------|:--------------------------|
| 0 | KADAR | 000647S | 1074342E | VTK R-112.4 / D240.5 | SJ ... | |
Immediately after the engine starts, check the oil pressure indicator. If oil pressure does not show within 30 seconds, stop the engine and determine the trouble. If oil pressure is indicated, adjust the throttle to the aircraft manufacturer's specified rpm for engine warm up. Warm up rpm is usually between 1,000 to 1,... | |
Table 2-2: Taking over controls
| | Taking Over of Controls (NFP from FP) | | |
|---:|:----------------------------------------|:---------... | |
Engine Controls
Diamond AIRCRAFT
DA 42 Series AMM
| | | Detail Steps/Work Items | Key Items/References |
|---:|:-----|:----------------------------------------------------------... | |
Diamond AIRCRAFT
TABLE OF CONTENTS
-
Section 20-00
## Standard Practices
1. General.
1
## Section 20-10
## Standard Practices - Airframe
| | 0 | 1 | 2 |
|---:|----:|:-----------------------------------------|----:|
| 0 | 1 | General | ... | |
DA 40 Series AMM
## Trouble-Shooting
## 1. General
The table below lists the defects you could have with the starting system. If you have the trouble detailed in the Trouble column read across to the Possible Cause column. Then do the repair given in the Repair column.
WARNING:
DO NOT ALLOW PERSONS TO ENTER THE DANGER ... | |
103°45'
103°50'
103° 55'
104°00'
2024 Civil Aviation Authority Singapore
TEBRAU CITY MALL
1
1
01°
CTR-
01°
30'
POINT 'X'
01 28 30N 103 49 54E
C SELETAR 'B'
30'
3 000ft ALT
CTR
ABM
(PU R-297/7 DME)
SELETAR TWR
D PAYA LEBAR
WM P228
PWR STN
3 000ft ALT
5 000ft ALT
PAYA LEBAR TWR
GND
CHANGES : Removal of Runway 2 closure c... | |
These gaps may occur due to:
· Undiscovered and long-standing shortcomings in the defenses,
. The temporary unavailability of some elements of the system due to maintenance action,
· Equipment failure,
Human interaction, and
Policy/Decision-making.
## 2.5.2 Hazard Defenses
Designers of NAS hardware and software must st... | |
Indicating Systems
Diamond AIRCRAFT
DA 40 Series AMM
Intentionally left blank
Page 102
31-12-00
18 Oct 2019
| |
Very expensive processing equipment
· Lack of standardized system of methodology
Great variety of materials, processes, and techniques
· General lack of repair knowledge and expertise
· Products often toxic and hazardous
Lack of standardized methodology for construction and repairs
The increased strength and the abilit... | |
DA 40 Series
AMM
Diamond
AIRCRAFT
12
13
14
15
16
17
18
19 20
21
11
10
22
10
9000 :selected: :selected:
00000000 00 00
00000000000
10
:unselected:
:unselected: :unselected: :unselected:
000
:selected:
:selected:
000
000000
000000
:unselected:
:selected:
00
:unselected: :unselected:
:unselected:
:selected:
:unselected:
:... | |
AIM
case turn of 30 degrees toward the adjacent final approach course, closing speeds of 135 feet per second could occur that constitute the need for quick reaction. A blunder has to be recognized by the monitor controller, and breakout instructions issued to the endangered aircraft. The pilot will not have any warning... | |
RSAFOSP 14 RIFRM
## OFFICIAL CLOSED
parameter in amber or red. During engine start and shutdown, inappropriate messages are inhibited.
## Non-EFIS Flight Instruments
26.116 The Mach/airspeed indicator (MASI) is essentially the same as found on the conventional instrument panel, and shown in Figure 26-48. The difference... | |
What brings you now from your lurking-place in the Shire?"
"The Nine have come forth again," I answered. "They have crossed the River. So Radagast said to me."
'"Radagast the Brown!" laughed Saruman, and he no longer concealed his scorn. "Radagast the Bird-tamer! Rada- gast the Simple! Radagast the Fool! Yet he had jus... | |
AIRBUS DEFENCE AND SPACE
STANDARD OPERATING PROCEDURES CABIN CREW SAFETY-RELATED DUTIES
A330-GOS CABIN CREW OPERATING MANUAL
CABIN CREW SAFETY-RELATED DUTIES PRE-PASSENGER BOARDING
Applicable to: ALL
| | PURSER | CABIN CREWMEMBER ... | |
Standard Practices
Diamond
AIRCRAFT
DA 40 Series
AMM
90
85
80
75
70
65
Pound-Force Inch (Ibf.in.)
60
55
50
45
40
- -
--
35
30
25
-
20
15
-
10
5
41
0.5 1.0 1.5 2.0 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0 6.5 7.0 7.5 8.0 8.5 9.0 9.5 10.0
Newton.Metre (Nm)
Find the Nm value on the horizontal axis. Move vertically to the solid bla... | |
Engine Indicating
Diamond AIRCRAFT
DA 40 Series
AMM
## Maintenance Practices
## 1. General
These Maintenance Practices tell you how to replace an integrated-engine-instrument and a manifold temperature sensor. Refer to the related Chapter for maintenance data on the sensors.
Where the engine control system provides dat... | |
4 INVESTIGATION
4.1 All Incident Reports filed will be thoroughly investigated and the complainant will be notified of the results of the investigation as soon as possible.
5 CO-ORDINATION/INVESTIGATION AUTHORITY
5.1 Co-ordination/Investigation Authority responsible for the Co-ordination/Investigation of Near Collision... | |
List of Effective Pages
Diamond AIRCRAFT
DA 40 Series AMM
| | CH-SE-SU | Page | Revision Date |
|---:|:-----------|-------:|:----------------|
| 0 | 27-38-00 | 101 | 18 Oct 2019 |
| 1 | 27-38-00 | 102 | 18 Oct 2019 |
| 2 | 27-38-00 | 201 | 18 Oct 2019 |
| 3 | 27-38-00 | 20... | |
## CONVECTIVE SIGNIFICANT METEOROLOGICAL INFORMATION- (See CONVECTIVE SIGMET.)
COOPERATIVE SURVEILLANCE- Any surveillance system, such as secondary surveillance radar (SSR), wide-area multilateration (WAM), or ADS-B, that is dependent upon the presence of certain equipment onboard the aircraft or vehicle to be detected... | |
Engine instruments in a split-shaft/free turbine engine typically consist of the following basic indicators. [Figure 15-7]
1. ITT indicator 2. Torquemeter 3. Propeller tachometer
4. N1 (gas generator) tachometer 5. Fuel flow indicator 6. Oil temperature/pressure indicator
ITT+ 50
+
0 PROP
O ITT+ 50 N1
+
0 3
0.0
FF PRES... | |
DA 40 Series AMM
Diamond
AIRCRAFT
Turbines
Intercooler
Intercooler Top Attachment
Engine Mounting Frame
Intercooler Bottom Attachments
Manifold Temperature Sensor
Manifold Pressure Connection
Engine Air Intake Manifold
10
Airplanes with
TAE 125-02 Engine
Turbocharger
Figure 2: Intercooler Installation - TAE 125-02-99 E... | |
DA 42 Series AMM
Diamond AIRCRAFT
## TABLE OF CONTENTS
CHAPTER 78 EXHAUST
1
1. General
2. Description 1
Trouble-Shooting
1. General
101
## Maintenance Practices
1.
2.
3.
| | 0 | 1 |
|---:|:------------------------------------------------------------... | |
Equipment/Furnishings
Diamond AIRCRAFT
DA 42 Series AMM
| | | Detail Steps/Work Items | Key Items/References |
|---:|:----|:----------------------------------... | |
Auto Flight
Diamond AIRCRAFT
DA 42 Series AMM
PFD
GDU 1040
Reversionary Switch
MFD
GDU 1045
GMU 44
GRS 77
GDC 74
GIA 63
GMA 1347
GIA 63
GSA 81
Roll Servo
GSA 81
Pitch Servo
GSA 81
Pitch Trim Servo
GSA 80 Yaw Servo
G1000 LRU
Digital Communication
Discrete I/O
Figure 1: GFC 700 Autopilot Schematic Diagram
Page 2 15 Nov 2... | |
DA 40 Series AMM
Diamond AIRCRAFT
Doors
| | | Detail Steps/Work Items | Key Items/References |
|---:|:----|:------------------------------------------------------------------------------------------------------... | |
Flight Controls
Diamond AIRCRAFT
DA 42 Series AMM
5. Flap Pushrod Access
| | Flap Pushrod | Remove/Install Access | References |
|---:|:---------------------------------------------... | |
Electrical Power
Diamond AIRCRAFT
DA 40 Series AMM
## (6) Power Relay
The power relay connects the relay junction box bus and ECU bus to the main bus. The essential bus switch controls the power relay.
## (7) Essential Tie Relay
In the usual (de-energized) condition, the essential tie relay connects the main bus to the... | |
| | AIRBUS DEFENCE AND SPACE | AAR ABNORMAL AND EMERGENCY PROCEDURES | 01.02A |
|---:|:----------------------------------|:----------------------------------------|:----------|
| 0 | A330-GOS QUICK REFERENCE HANDBOOK | | 24 OCT 23 |
CONSOLE RESET TABLE
| | WC... |
End of preview. Expand in Data Studio
Dataset Card for "nougat-15k"
Source: https://www.kaggle.com/datasets/therealoranges/nougat-15k by therealoranges
- Downloads last month
- 58