Mooney M20TN, Руководство по обслуживанию и ремонту

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MOONEY AVIATION COMPANY, INC.
M20TN SERVICE & MAINTENANCE MANUAL
Page
Date
16
2006
Rev Date
AIRCRAFT
FORWARD
EMA PIGTAIL
TOWARD REAR OF AIRCRAFT
TYPICAL EMA AIRCRAFT FORWARD
INSTALLATION
FIGURE 25--5
8. Connect End--Release Buckle Assembly to aircraft
structure or seat mounting point (for Aftermarket instal-
lations, refer to AmSafe Installation drawings 509760 --
pilot--co--pilot seats or 509780 -- passenger seats).
9. Connect Cable Interface Assy(s)’ connector(s) to
SAA connector(s). Connect mated halves together in
proper orientation and slide Red Locking Tab forward to
locking position.
10. Secure Three--Point Airbag Belt(s) inertia reel or
manual adjustor connection point to aircraft structure.
Secure lap--belt to aircraft structure or seat mounting
point (for Aftermarket installations, refer to AmSafe
Installation drawings 509760 -- pilot--co--pilot seats or
509780 -- passenger seats).
11. Remove Safety Cable Tie from airbag buckle
tongue before performing functional testing.
12. Perform functional test on system (refer to V23 Sys-
tem Diagnostic Tool -- Operation and Maintenance
Manual for testing procedures).
NOTE:
It is required, after completion of functional test-
ing, to document this task as an entry in the
aircraft’s logbook.
25--10--04 -- CABIN LIGHTING
Two pair of 24 volt overhead interior lights are located in
the cabin headliner for crew and passenger use. Power
to these lamps is available with Master Switch in either
the ON AND OFF position.
-- CAUTION --
The cabin light rocker switches are connected
directly to the battery.
All passenger overhead lights are controlled by the
Master Light switch located on the pilot’s arm rest. With
Master Light switch ON, individual overhead cabin
lights are controlled by rocker switches located on each
passenger’s arm rest (excluding front seat passenger).
The rockers switches control light ON, OFF and DIM.
Front seat passenger’s light switch is located forward of
the cabin door hinge on the interior side panel.
A 24 volt baggage compartment light is located in the
baggage compartment left hand headliner and is con-
trolled by a rocker switch mounted in the baggage
compartment right hand headliner assembly. Depress-
ing the rocker switch energizes a capacitor which in
turn energizes the fixture lamp. The duration that the
switch is depressed and held in the ON position will de-
termine the length of time the lamp remains illuminated.
This light will automatically turn OFF after approximate-
ly 10 minutes.
Refer to Chapter 33--20--00 for Interior Light mainte-
nance procedures.
25--50--00 -- BAGGAGE COMPARTMENT
The M20TN baggage compartment, located aft of the
rear passenger seats, has a capacity of 20.9 cu. ft.
(0.59 cu. M) and a maximum allowable load of 120 lbs.
(54 Kg). Floor tiedown straps are provided (Refer to
“Seat Belts/Restraints” cleaning instructions outlined
above for Tiedown web and metal hardware cleaning
guidelines).
Additional cargo space (38.6 cu. ft./1.09 cu. M.) is avail-
able by removing rear seat, bottom cushion and seat
back cushion/cover and folding seat back down into
seat bottom frame. This can be accomplished by pull-
ing UP on the appropriate aft seat back reclining locking
handles located on the front of the spar.
A small storage area located aft of the top of the aft bag-
gage compartment bulkhead (hat rack) is restricted to
10 lbs. (4.5 Kg) capacity. This area will not be available
for storage if the optional air conditioning system is
installed in the aircraft.
The engine Hour Meter is located in the baggage
compartment rear panel.
25--10--04
AUGUST 2010