Southeast Aerospace will be closed December 23rd - January 3rd for the Holidays.
Regular business hours will resume on Monday, January 6th. AOG Services are available.

Picture of product GDU-1240A

Part #: 011-01440-10

Model: GDU-1240A

OEM:

Garmin

Desc:

Multi-Function/Primary Flight Display
Part Number :

 

 

GDC-1240A

 

FEATURES

  • Central Display and user interface for Garmin Integrated Flight Deck
  • Commonly used with Garmin Perspective Systems found in Cirrus SR-20/SR-22
  • GDU 1240A provides a central display and user interface for the Garmin Integrated Flight Deck
  • Display is mounted flush to the aircraft instrument panel using six ¼ turn fasteners
  • Can beconfigured as either a Multi Function Display (MFD) or Primary Flight Display (PFD)
  • Display of attitude (pitch and roll), rate of turn, slip/skid, heading, airspeed, altitude, and vertical speed information (PFD or reversionary modes only)
  • Control and display of the HSI, Selected Heading and Selected Course (PFD or reversionary
  • Display of engine and airframe instrumentation (MFD or reversionary modes only)
  • Approach navigation functions and associated databases
  • Display of the AFCS flight director command bars and modes (PFD or reversionary modes only)
  • Baro-altitude Vertical Navigation (see Section 1.2.4 for exceptions)
  • Display of position and ground speed for use by the pilot/flight crew
  • Area navigation functions using the determined position/velocity and stored navigation data
  • Display of stored navigation and map databases for use by the pilot/flight crew

PLEASE NOTE:
This part has special configuration, alignment or software requirements. Please consult with the installer to verify that all of the resources needed for the installation are available. Failure to adhere to the manufacturer’s guidelines will result in adverse operation of the part and/or system.

 

SPECIFICATIONS

WIDTH: 13.40 inches (340.36 mm) height: 9.50 inches (241.30 mm)
Depth with Connector Kit 4.39 inches (111.4 mm) connectors kit weight: 0.2 lbs. (0.09 kg)
Operating Temperature Range: -40°C to +55°C Humidity: 95% non-condensing
Altitude Range: -1,500 ft to 55,000 ft Software Compliance: RTCA/DO-178B levels A, B, C, D, and E*
Hardware Compliance: RTCA/DO-254 Level A Environmental Compliance: RTCA/DO-160E
Power Requirements: 14/28 Vdc. See the Environmental Qualification Formfor details on surge ratings and minimum/maximum operating voltages GDU 1240A Ambient Temperature Above -15°C: 28V (Maximum) 1.8A, 28V (Typical) 1.4A
GDU 1240A Ambient Temperature At Or Below -15°C: 28V (Maximum) 3.0A, 28V (Typical) 2.7A GDU 1240A Display Viewing Angles: Edge of Display( left) Viewing Angle 45°, Right - 45°, Upper- 45°, Lower - 10°
Part Number: Description:
011-01440-00 Multi-Function/Primary Flight Display, Control of Dual VOR/ILS
Receivers, Control of Dual COM Transceivers, Control and Display of Flight Management System, Control of Barometric
Settings (weight 9.3 lbs.  4.22 kg)
011-01440-10 Multi-Function/Primary Flight Display, Control of Dual VOR/ILS
Receivers, Control of Dual COM Transceivers, Control and Display of Flight Management System, Control of Barometric
Settings (weight 9.3 lbs. 4.22 kg)
011-01440-20 Multi-Function/Primary Flight Display, Control of Dual VOR/ILS
Receivers (weight 9.1 lbs. 4.12 kg)
011-01440-30 Multi-Function/Primary Flight Display, Control of Dual COM
Transceivers, Control and Display of Flight Management System, Control of Barometric Settings (weight 9.2 lbs. 4.19 kg)
011-01440-40 Multi-Function/Primary Flight Display, Control of Dual VOR/ILS
Receivers, Control of Heading and Altitude Select Control of Dual COM Transceivers, Control and Display of Flight Management System, Control of Course Settings, Control of Barometric
Settings (weight 9.4 lbs. 4.26 kg)
011-01440-50 Multi-Function/Primary Flight Display, Control of Dual VOR/ILS Receivers, Control of Heading and Altitude Select, Control of Dual COM Transceivers, Control and Display of Flight Management System, Control of Course Settings, Control of Barometric
Settings, Control and Display of the AFCS Modes of Operation, 
VNAV AFCS Interface and Control, YD AFCS Interface and
Control (wight 9.4 lbs. 4.26 kg)

 

 

 

 

 

 

Serial # 18T005423
Condition SV
Mods None
Tag Date 07/25/23
Shop Garmin
Warranty 6 Months
011-01440-10
- Multi-Function/Primary Flight Display
Price Condition Status
$4,450.00 SV OUTRIGHT 1 IN STOCK
$2,750.00 SV EXCHANGE 1 IN STOCK
011-01440-00
- Multi-Function/Primary Flight Display
Price Condition Status
REQUEST SV EXCHANGE REQUEST LEAD TIME
011-01440-20
- Multi-Function/Primary Flight Display
Price Condition Status
REQUEST SV OUTRIGHT REQUEST LEAD TIME
011-01440-30
- Multi-Function/Primary Flight Display
Price Condition Status
REQUEST SV EXCHANGE REQUEST LEAD TIME
011-01440-40
- Multi-Function/Primary Flight Display
Price Condition Status
REQUEST AR EXCHANGE REQUEST LEAD TIME
011-01440-50
- Multi-Function/Primary Flight Display
Price Condition Status
REQUEST SV EXCHANGE REQUEST LEAD TIME

Click on a question below to see the answer. If you have a question about this model that is not answered below, please contact questions@seaerospace.com


In relation to NE (New) parts, many OEMs change their prices and availability without any notice to dealers or the industry. Therefore, through the REQUEST or RFQ indication, we ask that customers contact us for the most accurate price and availability.

In relation to SV & OH parts, the used parts aftermarket in the aviation industry is not an infinite supply. It is a dynamic, constantly changing market that is significantly affected by and susceptible to highs and lows in supply and demand. Therefore, although we attempt to, at times, we are unable to predict the exact moment when an item may be available. Once again, through the REQUEST or RFQ indication on our website, we ask that customers contact us for the most current and accurate price and availability.

"As Removed" or condition "AR" parts are in the same condition as they were removed from an aircraft. The reasons for removal include aircraft upgrades, teardowns, or certain types of incidents. In most cases, AR parts have not been inspected or tested. They do not include airworthiness certification such as FAA Form 8130 or EASA Form 1. Southeast Aerospace encourages avionics in this condition to be tested and recertified before using in an aircraft.