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A1-F18EA-LWS-000 AIRBORNE WEAPONS/STORES LOADING MANUAL NAVY MODEL F/A-18E/F AND EA-18G AIRCRAFT; SECTION II QUESTIONS WITH COMPLETE SOLUTIONS€12,25
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A1-F18EA-LWS-000 AIRBORNE WEAPONS/STORES LOADING MANUAL NAVY MODEL F/A
18E/F AND EA-18G AIRCRAFT; SECTION II
1. Describe the content of Section II in the manual.: ans- Section II provides de-
scriptive information on the F/A-18E/F and EA-18G aircraft conventional weapons
systems, suspension and accessory equipment, weapons and stores data, and ground
support equipment.
2. What does the airframe of the manual cover?: ans- The airframe section covers dif-
ferences in configuration identified by effectivity notes, applicable data to F/A-18E/F and
EA-18G aircraft, and notations for peculiar data to F/A-18E and F/A-18F.
3. How are differences in configuration identified in the manual?: ans- Differences in
configuration are identified by effectivity notes on illustrations and in the related text.
Effectivity data on sheet one of a multiple sheet illustration is applicable to all aircraft.
4. Define effectivity notations as used in the manual.: ans- Effectivity notations in the
manual specify data common to F/A-18E and F/A-18F, data common to F/A-18E/F and
EA-18G, and data peculiar to F/A-18E or F/A-18F with specific model and serial number
ranges.
5. What is an example of effectivity notation for data common to F/A-18E and F/A-
18F?: ans- An example is '165533 AND UP' which indicates data common to F/A-18E
and F/A-18F.
6. Describe how effectivity data is presented for configurations without effec- tivity
notes.: ans- Configurations or illustrations without effectivity notes are applicable to
F/A-18E/F and EA-18G aircraft.
,7. What does the manual specify for data peculiar to F/A-18E or F/A-18F?: The manual
specifies using model and serial number as applicable for data peculiar to F/A-18E or F/A-
18F.
8. How is effectivity data shown for data peculiar to F/A-18E?: Effectivity data peculiar
to F/A-18E is shown using the model and specific serial number range, for example, 'F/A-
18E 165660 THRU 165667'.
9. Do all illustrations in the manual have effectivity notes?: No, only illustrations with
differences in configuration have effectivity notes to specify the applicability to different
aircraft variants.
10.Describe the effectivity notations used to combine production and retrofit
effectivities.: Effectivity notations combine production and before or after retrofit
effectivities using the word ALSO as the separator.
11.What is an example of effectivity notations combining production and retrofit
effectivities?: 165668 AND UP; ALSO 165541 THRU 165544 AFTER F/A-18 AFC 74
12.What should ordnance loading crews do regarding the hazards presented by the
aircraft?: Ordnance loading crews should familiarize themselves with the hazards and use
caution in operations around the aircraft.
, 13.What are ground safety devices and when are they installed?: Ground safety
devices are installed immediately after aircraft flight.
14.Do loading crew personnel need to install ground safety devices?: While it may not
be their responsibility, loading crew personnel must be aware of the requirement for
ground safety devices.
15.What should personnel do before working in or around the aircraft regard- ing
ground safety devices: Personnel should verify that ground safety devices are installed
prior to working in or around the aircraft.
16.What provisions are incorporated for external power application in the air- craft?:
Provisions are incorporated for external power application, with deck/ground power
supplied via the external power receptacle.
17.Where is the external power receptacle located on the aircraft?: The exter- nal
power receptacle is located on the left side of the forward fuselage at door 9, accessible
from deck level.
18.Describe the function of the external power connector.: The external power
connector connects 115 volt, three phase, 400 hertz AC external power to the AC bus.
19.What provides protection for the aircraft electrical system powered from the
aircraft buses?: Protection of the aircraft electrical system is provided by circuit breakers.
20.What is the purpose of the ground power control panel assembly?: The ground
power control panel assembly provides toggle to control the application of external
power to avionic and instrument systems.
21.Where is the three position toggle switch for external power control locat- ed?: The
three position toggle switch for external power control is located on the ground power
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