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Internet at http://dms.dot.gov; or at the National Archives and Records Administration (NARA). For
information on the availability of this material at the NARA, call (202) 741-6030, or go to
http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
Table 3 – Service Bulletins Incorporated by Reference
Bombardier Service Bulletin Revision Level Date
SB 23-28-6 Original Issue April 21, 1998
SB 24/25-28-3 2 February 21, 1998
SB 28/29-28-4 3 June 2, 1999
SB 31-28-7 3 January 26, 2001
SB 35/36-28-11 4 December 4, 2000
SB 55-28-13 3 December 15, 2000
2007-04-18 4
54 BW 2007-04
Table 4 – Temporary Changes Incorporated by Reference
Learjet Temporary
Flight Manual
(TFM) Change
Date To the Learjet Airplane Flight Manual
TFM 96-08 May 30,
1996
24 (FM-004), 24B (FM-006), 24D (FM-009), 24E (FM-011),
24F (FM-012), 24 ECR 736 (FM-008), 25 (FM-014), 25B/C
(FM-016), 25D/F (FM-018), 28/29 (FM-100), 31 (FM-112),
31A (FM-121), 35/36 (FM-019), 35A/36A FC-200 (FM-102),
35A/36A FC-530 (FM-108), 55 (FM-103), 55B (FM-110), 55C
(FM-114)
TFM 96-09 May 30,
1996
24 (FM-004), 24B (FM-006), 24D (FM-009), 24E (FM-011),
24F (FM-012), 24 ECR 736 (FM-008), 25 (FM-014), 25B/C
(FM-016), 25D/F (FM-018), 28/29 (FM-100), 31 (FM-112),
31A (FM-121), 35/36 (FM-019), 35A/36A FC-200 (FM-102),
35A/36A FC-530 (FM-108), 55 (FM-103), 55B (FM-110), 55C
(FM-114)
TFM 98-01 May 11,
1999
23 (FM-003)
TFM 98-02 May 11,
1999
23 (FM-003)
Issued in Renton, Washington, on February 6, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E7-2640 Filed 2-15-07; 8:45 am]
AIRCREW TRAINING SOLUTIONS
Airbus A320 & A319 Study Guide ã
A I R B U S A 3 2 0 / 3 1 9 S T U D Y G U I D E
1
A I R B U S A 3 2 0 / 3 1 9 S T U D Y G U I D E
1
Overhead Panel - Part 1
1) ON BAT LIGHT
The aircraft batteries are powering one or more ADIRU.
When power is lost, ADIRU’s 2 & 3 will remain ON BAT for 5 minutes, to
retain alignment data while generator power can be restored. ADIRU 1 or
whichever unit the captain has selected will remain ON BAT until generator
power is restored.
2) IR LIGHTS
FAULT - (Flashing FAULT) ATT & HDG may be recoverable.
(Steady FAULT) Fault in IR unit, and is not recoverable.
ALIGN - (Flashing) Alignment fault, No present position entered within 10 minutes or
1° LAT/LONG difference between its last known position.
Note: A dual IR failure will increase landing distance. IR’s supply antiskid
with deceleration info. Dual IR failure limits the deceleration rate to 5.6 fps².
IR supplies: HDG, ATT, and VS to PFD
ADR supplies: AS, ALT, and backup VS to PFD
The A320 & A319 have the capability to incorporate GPS inputs to the
GNADIRS.
3) NAV SELECTOR
NAV - Normal position for alignment and navigation. Full alignment requires 7-10
minutes. Fast alignments take 3 minutes. A fast alignment may be
accomplished only if the IR’s have been previously aligned. Fast alignment is
accomplished by selecting each IR to OFF then ON within 5 seconds and
entering a new present position.
ATT - Used to retain attitude & heading information when IR has faulted
4) ADR P/B
FAULT - Failure of the Air Data Reference system.
OFF - When pressed to OFF Air data output is disconnected
Chapter 1
A I R B U S A 3 2 0 / 3 1 9 S T U D Y G U I D E
2
5) GEN 1 LINE P/B
OFF - Generator 1 Line contactor opens. #1 fuel pump in each wing tank is powered
from the generator 1 feeder
SMOKE - Smoke is detected in the avionics ventilation duct
EMERG GEN TEST P/B
This test is normally performed by maintenance. Tests the emergency
generator without deploying the RAT.
5 KVA 115/200V 400Hz utilizing the blue hydraulic system.
7) RAT/EMERG GEN FAULT LIGHT
FAULT - Emergency generator is not supplying power when:
AC Buses 1&2 are not powered and the nose landing gear is up.
A319 - AC Bus 1&2 are not powered, Emergency generator is not supplying
power, nose landing gear extended or retracted.
8) EMERG GEN P/B
AUTO - RAT extends when AC Bus 1&2 are not powered, and airspeed is above 100
knots, with the nose landing gear up. The emergency generator, powered by
the blue hydraulic system, will couple within 3 seconds if all parameters are
normal. The emergency generator will provide electrical power until
approximately 140 knots.
A319- RAT extends when AC Bus 1&2 are not powered, regardless of nose
landing gear position. The A319 RAT is more efficient. Therefore, the RAT
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