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TRANSMITTAL LETTER
Publication: AOM-145/1114-01 Airplane Operations Manual.
Dear Madam or Sir,
You are receiving the temporary revision 40.2 of AOM, which:
• Includes reference to the accomplishment of the Service Bulletin 145-21-0050;
• Includes the new block 1-12-60 code 01*, containing information about Ground Resets procedures;
• Includes airplane configuration with Rain Repellent Coating installation that can perform the Windshield Wiper functions;
• Includes information about EGPWS prior version -213-213, which does not account man-made obstacles;
• Includes information indicating that advancing thrust lever until 86% N2 represents normal system condition.
*This new block-code is not reflected in the List of Effective pages and must be included in your manual following the numbered sequence.
Temporary Revisions pages are printed in yellow paper. Revised pages should be included in your manual facing the current pages.
They will be incorporated in the next AOM scheduled revision.
The temporary revision will not be in cluded in the List of Effective Pages.
In case of any question, please contact:
Embraer Flight Operations Support by E-mail: opereng@embraer.com.br or phone: (+55 12) 3927 1706
THIS PAGE IS NOT PART OF THE MANUAL AND MUST NOT BE INCORPORATED IN YOUR AOM. PLEASE DISCARD IT AFTER READING.
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In connection with the use of this document, Embraer does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose.
Copyright © 2014 by Embraer S.A. All rights reserved.
AIRPLANE OPERATIONS MANUAL VOLUME 1
EMBRAER S.A.
This manual is applicable to the EMB-145 airplanes all models equipped with AE3007A, AE3007A1/1, AE3007A1, AE3007A1P and AE3007A1E engines, ERJ-140 airplanes all models equipped with AE3007A1/3 engines and to the EMB-135 airplanes all models equipped with AE3007A3 and AE3007A1/3 engines and operating under ANAC, FAA and JAA/EASA certifications.
THIS PUBLICATION IS INCOMPLETE WITHOUT AIRPLANE OPERATIONS MANUAL AOM–145/1114 VOLUME 2
AOM–145/1114-01 OCTOBER 31, 1996 TEMPORARY REVISION 40.2 – APRIL 04, 2014
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AIRPLANE
OPERATIONS MANUAL
RECORD OF
TEMPORARY
REVISIONS
TEMPORARY REVISION 40.2 RTR-1
RECORD OF TEMPORARY REVISIONS AOM–145/1114-01
TR 40.1 ............................................................................ DEC 19, 2013 TR 40.2 ............................................................................ APR 04, 2014
RECORD OF
TEMPORARY
REVISIONS
AIRPLANE
OPERATIONS MANUAL
RTR-2 TEMPORARY REVISION 40.2
INTENTIONALLY BLANK
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LIMITATIONS FAA
AIRPLANE
OPERATIONS MANUAL
1-01-12 Page 1 Code 05 TEMPORARY REVISION 40.2
AOM-145/1114
SUPPLEMENTARY OPERATIONAL
LIMITATIONS
OPERATIONAL ENVELOPE APPLICABLE ONLY TO EMB-145XR AND LR MODELS POST-MOD.
SB 145-21-0050 OR EQUIPPED WITH AN EQUIVALENT
MODIFICATION FACTORY INCORPORATED -5000 0 5000 10000 15000 20000 25000 30000 35000 40000 -70 -60 -50 -40 -30 -20 -10 0 10 20 30 40 50 60 ALTITUDE - ft c STATIC AIR TEMPERATURE - °C ISA + 35°C 145XRFAA100 - 30JUN2003 TAKEOFF, LANDING c 37000 ft -21.5°C -1000 ft 52°-54°C 10000 ft -65°C -40°C
NOTE: - In the event of a landing below -40°C, the airplane may not takeoff without further hard landing maintenance inspection (Refer to AMM Task 5-50-02).
- Minimum Total Air Temperature in cruise flight above 25000 ft is -45°C.
- Only APU T-62T-40C14 is allowed for operations on ground above 8000 ft.
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LIMITATIONS AIRPLANE
OPERATIONS MANUAL
1-01-30 Page 1 Code 01 TEMPORARY REVISION 40.2
AOM-145/1114
ENHANCED GROUND PROXIMITY WARNING
SYSTEM (EGPWS) The following limitations are applicable to the Enhanced Ground Proximity Warning System (EGPWS):
− The Allied-Signal Enhanced Ground Proximity Warning System Pilot’s Guide, Document Number 060-4241-000, March 1997 edition (or later revision of the manual) or ANAC accepted Operating Manual, must be available to the flight crew.
− Allied-Signal Application Software version 202 and Configuration Software version 202 or later must be installed.
− Navigation is not to be predicated on the use of the Terrain Awareness Display.
− The Terrain Display is intended to be used as a situational tool only and may not provide the accuracy and/or fidelity on which to solely base terrain avoidance maneuvering.
− The EGPWS displays and alerting algorithms prior version -213-213 currently do not account for man-made obstacles.
− The EGPWS must be inhibited in the following conditions:
NOTE: To inhibit the Terrain Awareness Alerting and Display function, press the TERRAIN SYS OVRD button.
− Within 15 NM of takeoff, approach or landing at airports that have no approved instrument approach procedure or not included in the EGPWS Allied Signal database (encompasses airports which runways are shorter than 1070 m);
− When GPS is failed;
− When FMS is operating in Dead Reckoning Mode.
NOTE: This will not affect the basi c GPWS functi ons (modes 1 to 7). If the FMS is restored after a period of inadequacy, the EGPWS may be enabled by pressing again the TERRAIN SYS OVRD button.
− During QFE operations for airplanes featuring EGPWS software versions prior to the -216 version;
NOTE: QFE operation is allowed with FMS Honeywell or FMS Universal Post-Mod. SB145- 34-0112 when featuring EGPWS software versions -216 and on.
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LIMITATIONS AIRPLANE
OPERATIONS MANUAL
1-01-30 Page 1 Code 03 TEMPORARY REVISION 40.2
AOM-145/1114
ENHANCED GROUND PROXIMITY WARNING
SYSTEM (EGPWS) The following limitations are applicable to the Enhanced Ground Proximity Warning System (EGPWS):
− The Allied-Signal Enhanced Ground Proximity Warning System Pilot’s Guide, Document Number 060-4241-000, March 1997 edition (or later revision of the m anual) or certification authority accepted Operating Manual, must be immediately available to the flight crew.
− Allied-Signal Application Software version 202 and Configuration Software version 202 or later must be installed.
− Navigation is not to be predicated on the use of the Terrain Awareness Display.
− The EGPWS displays and alerting algorithms prior version -213-213 currently do not account for man-made obstacles.
− Pilots should inhibit the Terrain Awareness Alerting and Display function by pressing the TERRAIN SYS OVRD button when within 15 NM of takeoff, approach, or l anding at an airport when any of the following conditions apply:
− The airport has no approved instrument approach procedure.
− The airport is not included in the Allied Signal data base.
− The longest runway is less than 1070 m (3500 ft) in length.
− Terrain Awareness Alerting and Display functionality must be manually inhibited when the flight crew knows in advance that:
− An approach to an airport not included in the EGPWS database will be performed;
− GPS is failed;
− QFE operation is the altimeter operational mode below the transition altitude on approach into an airport which is more than 200 ft above or below Sea Level (not applicable to EGPWS software version 216 and on with FMS Honeywell or FMS Universal Post Mod.SB145-34-0112).