Cessna 680 User manual

CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
CONTENT Original Issue
Subject Forward Maintenance Parts
Aft Vanity ......................................................................................................... 25-40-01 ............... 25-40-02
Aft Bulkhead Closet ........................................................................................ 25-40-03 ............... 25-40-04
Toilet Installation ............................................................................................. 25-40-07 ............... 25-40-08
Table of Contents
Lavatories

CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
Page 1
25-40-01 Original Issue
AFT VANITY - MAINTENANCE
1 General
A. The aft vanity is located in the aft portion of the cabin on the left-hand side. The vanity has toekick and
accent lighting, a water system, storage drawers, trash container and can contain electrical outlets.
The vanity water system consists of a water tank, pump, water faucet and supply lines. Remove vanity
water tank prior to vanity removal to prevent damage to cabinet or aircraft surroundings.
CAUTION: Vanity cabinets incorporate electrical components and must have electrical wire bundle(s)
properly routed and secured.
(1) Verify appropriate circuit breaker is disengaged before performing maintenance on any
electrical components or wiring.
(2) Secure and protect electrical wires to prevent fraying and contact with moving parts such as
drawers and hardware.
(3) Ensure clearance between electrical wiring and heat generating components.
(4) Ensure electrical wiring is not crushed or pinched during removal/installation of the cabinets.
(5) Ensure electrical wiring insulation is not frayed and bare wires are repaired or replaced. Wire
bundles should be properly routed using grommets, necessary clamps and tie-straps.
2 AftVanity Removal/Installation
A. Remove Aft Vanity.
CAUTION: Disconnect battery and remove power.
Verify appropriate circuit breaker is disengaged before performing maintenance on any
electrical components or wiring.
Secure and protect electrical wires to prevent fraying.
Ensure electrical wiring is not crushed/pinched during removal/installation.
(1) Disconnect battery and remove external power from aircraft.
(2) Turn off L BATT, R BATT and INTERIOR electrical switches, located in Electrical panel on pilot side of
instrument panel. Electrical panel is located just right of pilot’s yoke and left of center console on the
lower portion of instrument panel.
(3) Disengage CB108V AFT VANITY and CB107V LH PATH LIGHTS circuit breakers, located in Interior
J-box. The Interior J-box is located in bottom of aft bulkhead closet on right-hand side. Lift latch and
remove access panel, which is held in place with latch and magnets, to access J-box cover. With
access panel removed, press J-box cover latch to release latch and open J-box cover. Pull breakers
to disengage.
(4) Remove passenger seats to make room for vanity removal and to prevent damage to seat or vanity
during removal, refer to section 25-21-01, Passenger Seat - Maintenance Practices, in the Maintenance
Manual.
(5) Remove vanity reveal panel by first removing vanity PSU fascia panel, refer to section 25-40-02,
Passenger Service Unit - Maintenance Practices, in the Maintenance Manual. Disengage hook and
pile fasteners by pulling top of vanity reveal panel inboard, then lift panel up and out of channels on
back of vanity to remove.
(6) Remove two (2) screws securing vanity to aft divider panel. Remove right-hand vanity drawers to access
screws from inside vanity.
(7) Remove left-hand aft divider to allow room to remove vanity. Refer to section 25-24-06, Cabin
Dividers - Maintenance Practices, in the Maintenance Manual.
(8) Empty water tank and replace (Refer to Aft Vanity Water System Operation below).
(9) Remove two (2) screws securing vanity to bulkhead closet. Remove left-hand drawers to access
screws from inside vanity.

CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
Page 2
25-40-01 Original Issue
AFT VANITY WATER SYSTEM OPERATION - MAINTENANCE
(10) Remove two (2) plugs, bolts and washers securing vanity to floorboard attach brackets and tag for
reinstallation.
(11) Move vanity inboard by first tilting top inboard, then move bottom inboard enough to disconnect
electrical wiring and remove drain hose.
(12) Tag and disconnect electrical wiring.
(13) Disconnect drain hose.
(14) Protect vanity and interior by covering before removal.
CAUTION: Two people are required to maneuver vanity from aircraft without causing damage
to vanity or other furnishings.
(15) Remove vanity from aircraft, being careful not to damage vanity or surroundings.
B. Install Aft Vanity.
(1) Position vanity in aircraft near installed position.
(2) Remove Rino-Hyde protective covering and clean as needed.
(3) Identify and connect electrical wiring.
(4) Connect water hoses.
(5) With top of vanity tilted inboard, place bottom in against sidewall, then tilt top back into position.
(6) Install (two) bolts, washers and plugs securing the closet to floorboard attach brackets.
(7) Replace left-hand aft divider. Refer to section 25-24-06, Cabin Dividers - Maintenance Practices, in the
Maintenance Manual.
(8) Replace two (2) screws securing vanity to aft divider panel and replace drawers.
(9) Replace two (2) screws securing vanity to bulkhead closet and replace drawers.
(10) Fill water tank in vanity and replace for water system testing (Refer to Aft Vanity Water System
Operation below).
(11) Replace vanity reveal panel. Tilt top of vanity reveal panel inboard while placing bottom edge of reveal
panel down and behind vanity. Press top of reveal panel outboard to engage hook and pile fasteners.
(12) Connect battery and replace external power from aircraft.
(13) Replace vanity PSU fascia. Refer to section 25-40-02, Passenger Service Unit - Maintenance Practices,
in the Maintenance Manual.
(14) Replace passenger seats. Refer to section 25-21-01, Passenger Seat - Maintenance Practices, in the
Maintenance Manual.
(15) Connect battery and replace external power to aircraft.
(16) Turn on L BATT, R BATT and INTERIOR electrical switches, located in Electrical panel on pilot side of
instrument panel. Electrical panel is located just right of pilot’s yoke and left of center console on the
lower portion of instrument panel.
(17) Engage CB108V AFT VANITY and CB107V LH PATH LIGHTS circuit breakers, located in Interior
J-box. The Interior J-box is located in bottom of aft bulkhead closet on right-hand side. Lift latch and
remove access panel, which is held in place with latch and magnets, to access J-box cover. With
access panel removed, press J-box cover latch to release latch and open J-box cover. Press breakers
in to engage.
(18) Check vanity lights and water heater for proper operation and evidence of shorting or overheating.
(19) Prime pump and check faucet for proper operation (Refer to Aft Vanity Water System Operation on next page).
3 Operations and Inspections
A. Inspect Aft Vanity.
(1) Inspect vanity for nicks, cracks, dents and security of installation.
(2) Check doors and drawers for proper operation.
(3) Check switches and controls for evidence of arcing, shorts or overheating.
(4) Check controls for proper operation.
(5) Check heated drains for security, damage and proper operation.
(6) Check plumbing for leaks or corrosion.

CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
Page 3
25-40-01 Original Issue
4 Aft Vanity Water System Operation
The vanity water system consists of a water tank, pump, water faucet and supply lines. The water tank is
located in the bottom-center compartment of the vanity and is easily removed for filling. The vanity switch
panel controls the temperature of the heater for the water tank.
CAUTION: If the aircraft is stored overnight or longer in temperatures below freezing, the vanity water system
must be drained to prevent pump failure or damage.
A. Drain Aft Vanity Water System.
Note: Make certain switch for hot water container is “Off” before attempting to remove water tank
from vanity. Vanity switch panel is located aft of vanity on bulkhead closet.
(1) Disconnect water tank by pressing release button to disconnect water line and empty water from
tank. Lift up slightly on front of hot water tank and slide inboard to remove. Unscrew lid and dump
water from tank.
(2) Reconnect empty water tank to system.
(3) Press water button to cycle the pump. Repeat until no water comes out of faucet for three
cycles of the water button.
(4) Disconnect water tank and empty any remaining water in tank and reconnect tank, or remove tank
from aircraft.
B. Prime Aft Vanity Water System.
Note: Make certain switch for hot water container is “Off” before attempting to replace water tank
into vanity. The vanity switch panel is located aft of vanity on bulkhead closet.
(1) Fill water tank with water and connect tank to system.
(2) Press water button to cycle pump. Repeat until water comes out of the faucet (the pump will
self prime).
(3) Check system for water leaks and security of installation.
5 Overboard Drain Operation
Note: For Overboard Maintenance Practices, refer to 38-30-02 WATER OVERBOARD DRAINS -
DESCRIPTION AND OPERATION in Maintenance Manual.
A. Potable and wash water waste is drained from aft vanity basin through a flexible hose to an overboard
drain weld assembly. The overboard drain weld assembly is installed through the bottom of aircraft
fairing and is electrically heated to prevent ice formation that could block or impair normal drainage.
For overboard drain locations, refer to Chapter 6 in the IPC, Aircraft Drains Locations - Description
and Operation. Waste water from aft vanity wash basin and/or potable water source is released through
a heated overboard drain by simply opening the basin drain. 28 VDC electrical power from aft interior
junction box electrical circuit is used to heat overboard drains.
(1) Check to make sure water flows freely down drain (water will exit bottom of aircraft).
AFT VANITY WATER SYSTEM OPERATION - MAINTENANCE

Page 1
25-40-02-01 Original Issue
CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
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DETAIL A
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16,24,25,27
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29

CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
Page 2
25-40-02-01 Original Issue
No. Part Number Description Vendor
-4479324-1 VANITY CABINET ASSEMBLY
1CLE106-01 LIGHT ASSY (5 ea) 0GZF3
2CO35-32 SMALL OVAL BAR SINK GBKP
3C3-205P DOOR LATCH GRABBER (2 ea) 94222
4DALCLP-100 MOUNTING CLIP (14 ea) 0GZF3
5DELTA10OZBR SOAP BOTTLE 4W953
6DELTA1000 SOAP DISPENSOR 4W953
7D26141 DELTA SPOUT 0KAT4
8G-06349-42 ELBOW 4W953
9LCD100-06 COUPLING 62661
10 LCD260-04 COUPLING 62661
11 L21995 PUMP ASSY 32042
12 MS21919WDF11 CLAMP (2 ea)
13 MS21919WDG12 CLAMP (2 ea)
14 MS3106A18-10S CONNECTOR
15 S-1014 TUBING
16 SAM280-5 LATCH ASSY (8 ea) 31845
17 SL2337-3 MOUNT (4 ea) 97393
18 S08 SOCKET 63681
19 S2357-1 CLAMP (4 ea)
20 S2800-633 TOILET PAPER ROLLER
21 TKL100-014 TOE KICK LIGHT ASSY 0GZF3
22 V7-1B17D8-263 MICROSWITCH (5 ea) 91929
23 102570 DRAIN PULL 089X8
24 12325-17 WIRE STRIKER (8 ea) 4W953
25 12325-19 STRIKER CLAMP (8 ea) 4W953
26 12325-25-31 SPACER / STOP (5 ea) 4W953
27 12325-31-31 SPACER / STOP 4W953
28 12515-25 SOCKET BRACKET 4W953
29 12520-25 DOUBLE RELAY BRACKET 4W953
30 12538-59 CONNECTOR ANGLE 4W953
31 12589-37 LH SIDE TANK BRACKET 4W953
NOTE: Parts not available as complete installations.
When ordering plated parts, the plating number found in section 25-00-06 must follow the
part number without a space.

Page 3
25-40-02-01 Original Issue
CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
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36

CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
Page 4
25-40-02-01 Original Issue
No. Part Number Description Vendor
-4479324-1 VANITY CABINET ASSEMBLY - Continued
32 12589-39 RH SIDE TANK BRACKET 4W953
33 12614-1 2 GAL.WATER TANK 4W953
34 1281012-10 SLIDE ASSY - 10 INCH (4 ea)
35 1281012-13 SLIDE ASSY - 13 INCH (6 ea)
36 1281012-14 SLIDE ASSY - 14 INCH (4 ea)
37 12962-11 WATER TANK RETAINER 4W953
38 12962-15 BREAKER ANGLE 4W953
39 12962-35 DRAIN ASSY 4W953
40 12962-37 MOUNTING CLIP (4 ea) 4W953
41 12962-39 DRIP TRAY 4W953
42 12962-47 TOILET PAPER BRACKET 4W953
43 12962-49 HINGE ASSY (2 ea) 4W953
44 12962-61 PLUG MOUNTING BRACKET ASSY 4W953
45 12962-69 DRAIN ROD COUPLING 4W953
46 12962-9 HANDLE ASSY WITH MICROSWITCH 4W953
47 13084-1 VANITY INLAY 4W953
48 4479123-2 TRASH CONTAINER, TYPE III
49 4479323-1 VANITY SHELL
50 5002830 BARBED ELBOW (2 ea) 06034
51 6-HBU-SS 90 DEGREE FITTING 4W953
52 6-2FBU-SS MALE CONNECTOR (2 ea) 24984
53 71393-1 HYDRAULIC BLOCK 80477
54 79001-06-0100 HOSE WITH FLARELESS FITTINGS 24984
55 79006G-0120-0180 HOSE ASSY 24984
56 79339-010 HOSE ASSY 24984
57 80853-3 RETAINER (2 ea) 4W953
58 88867103 RELAY 63681
NOTE: Parts not available as complete installations.
When ordering plated parts, the plating number found in section 25-00-06 must follow the
part number without a space.

CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
Page 1
25-40-03 Original Issue
AFT BULKHEAD CLOSET - MAINTENANCE
1. General
A. The aft bulkhead closet is located in extreme aft portion of cabin. The aft bulkhead closet is built in three
sections that are separated during removal/installation. It is necessary to first remove the mirror/veneer
cover panels before closet can be split. To remove closet, it will be necessary to first remove passenger
seats, side-facing seat, psu fascias, aft dividers, toilet fascia and upholstery, and vanity.
2. Aft Closet Removal/Installation
A. Remove Closet.
CAUTION: Disconnect battery and remove power.
Verify appropriate circuit breaker is disengaged before performing maintenance on any
electrical components or wiring.
Secure and protect electrical wires to prevent fraying.
Ensure electrical wiring is not crushed/pinched during removal/installation.
(1) Disconnect battery and remove external power from aircraft.
(2) Turn off L BATT, R BATT and INTERIOR electrical switches, located in Electrical panel on pilot side of
instrument panel. Electrical panel is located just right of pilot’s yoke and left of center console on the
lower portion of instrument panel.
(3) Disengage CB101V A/V SHIPSIDE, CB100V A/V COMPARTMENT, CB113V AFT CLOSET,
CB108V AFT VANITY, CB111V DRAIN HEATERS, CB114V VANITY INDIRECT LIGHTS,
CB110V TOILET, CB118V TOILET SERVICE PANEL, CB107V, LH PATH LIGHTS, RH PATH LIGHTS,
CB102V UPWASH INDIRECT LIGHTS and CB103V DOWNWASH INDIRECT LIGHTS circuit breakers,
located in Interior J-box. The Interior J-box is located in bottom of aft bulkhead closet on right-hand
side. Lift latch and remove access panel, which is held in place with latch and magnets, to access
J-box cover. With access panel removed, press J-box cover latch to release latch and open J-box
cover. Pull breakers to disengage.
(4) Remove passenger seats.
(5) Remove cabin and lavatory PSU fascias.
(6) Remove aft dividers.
(7) Remove aft vanity.
(8) Remove toilet fascia and upholstery.
(9) Remove vanity switch bezel.
(10) The electrical outlet is removed to allow cover panels to be removed. Remove four (4) screws that
secure electrical outlet wire closeout and remove closeout. Remove four (4) screws that secure
access panel in bottom of center section of closet and remove panel to access electrical outlet
disconnect. Disconnect electrical outlet from relay box and tag wires for reinstallation. Remove
four (4) nuts securing outlet to bracket and remove outlet. Tag nuts and screws for reinstallation.
(11) Remove door stay from closet door. Tag screws for reinstallation.
(12) Press hinge release button on each of the four (4) door hinges and remove door from hinges. Remove
door from aircraft.
(13) Mirror/veneer cover panels must be removed to gain access to screws that secure left and right closet
sections to center section. Remove screws from inside bulkhead closet. The cover panel below door
is held in place with two (2) screws that are accessed from outside closet. The top cover panel is
held in place with three (3) screws. Left-hand cover panel is held in place with seven (7) screws. The
right-hand cover panel is held in place with eight (8) screws. The door cover panel does not need to
be removed (will be removed with door). Remove cover panels and remove from aircraft. Take care
not to damage panels or surroundings. Tag screws for reinstallation.

CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
Page 2
25-40-03 Original Issue
(14) Remove screws joining left-hand section to center section. A vertical row of six (6) screws is found
along outside edge where left-hand section and center section meet. Remove screws and tag for
reinstallation. From inside closet, remove four (4) screws along top of closet where left-hand section
meets center section. Remove pin cover (cover is held in place with one screw). Remove two (2)
down-facing screws on bottom shelf of left-hand section. Remove vertical row of four (4) screws in
back of closet where left-hand section and center section meet. Tag screws for reinstallation.
(15) Disconnect wiring for closet lights found at top of left-hand section. Tag wires for reinstallation.
(16) Disconnect wiring for switch panel and tag wires for reinstallation.
(17) Retract two (2) installation pins and slide left-hand section forward. Remove from aircraft, being
careful not to damage closet section or surroundings.
(18) Remove screws joining right-hand section to center section. A vertical row of five (5) screws is found
along outside edge where right-hand section and center section meet. Remove screws and tag for
reinstallation. From inside closet, remove four (4) screws along top of closet where right-hand section
meets center section. Remove pin cover (cover is held in place with one screw). Remove two (2)
screws on bottom shelf of right-hand section. Remove vertical row of four (4) screws in back of closet
where right-hand section and center section meet. Tag screws for reinstallation.
(19) Remove access panel and disconnect wiring for audio/video equipment. Tag wires for reinstallation.
(20) Retract two (2) installation pins and slide right-hand section forward. Remove from aircraft, being
careful not to damage closet section or surroundings.
(21) Remove plugs, bolts and washers securing the center section of the closet to floorboard attach
brackets and tag for reinstallation.
(22) Carefully remove center section from aircraft, being careful to not damage closet or surroundings.
B. Install Closet.
(1) Position center section of closet in airplane near installed position
(2) Identify and connect any electrical wiring previously disconnected.
(3) Secure to floorplates with two (2) bolts, washers and plugs previously removed.
(4) Position right-hand section of closet in airplane near installed position.
(5) Engage two (2) installation pins.
(6) Identify and connect any electrical wiring previously disconnected.
(7) Replace all screws joining right-hand section to center section. A vertical row of five (5) screws is
found along outside edge where right-hand section and center section meet. From inside closet,
replace pin cover and four (4) screws along top of closet where right-hand section meets center
section. Replace two (2) screws on bottom shelf of right-hand section. Replace vertical row of four (4)
screws in back of closet where right-hand section and center section meet.
(8) Position left-hand section of closet in airplane near installed position.
(9) Engage two (2) installation pins.
(10) Connect wiring for closet lights found at top of left-hand section.
(11) Connect wiring for switch panel and tag wires for reinstallation.
(12) Replace all screws joining left-hand section to center section. A vertical row of six (6) screws is found
along outside edge where left-hand section and center section meet. From inside closet, replace pin
cover and four (4) screws along top of closet where left-hand section meets center section. Replace
two (2) down-facing screws on bottom shelf of left-hand section. Replace vertical row of four (4) screws
in back of closet where left-hand section and center section meet.
(13) Position and secure mirror/veneer cover panels. The cover panel below door is held in place with
two (2) screws that are accessed from outside closet. The top cover panel is held in place with
three (3) screws. Left-hand cover panel is held in place with seven (7) screws. The right-hand cover
panel is held in place with eight (8) screws.
(14) Replace closet door on hinges.
(15) Replace door stay to closet door.
(16) Position electrical outlet and secure outlet to bracket with four (4) nuts. Connect electrical outlet wiring
to relay box. Replace access panel in bottom of center section of closet with four (4) screws. Replace
electrical outlet closeout with four (4) screws.
AFT CLOSET - MAINTENANCE

CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
Page 3
25-40-03 Original Issue
AFT CLOSET - MAINTENANCE
(17) Replace vanity switch bezel.
(18) Replace toilet fascia and upholstery.
(19) Replace aft vanity.
(20) Replace aft dividers.
(21) Replace cabin and lavatory PSU fascias.
(22) Replace passenger seats.
(23) Connect battery and external power to aircraft.
(24) Turn on L BATT, R BATT and INTERIOR electrical switches, located in Electrical panel on pilot side of
instrument panel. Electrical panel is located just right of pilot’s yoke and left of center console on the
lower portion of instrument panel.
(25) Engage CB101V A/V SHIPSIDE, CB100V A/V COMPARTMENT, CB113V AFT CLOSET,
CB108V AFT VANITY, CB111V DRAIN HEATERS, CB114V VANITY INDIRECT LIGHTS,
CB110V TOILET, CB118V TOILET SERVICE PANEL, CB107V, LH PATH LIGHTS, RH PATH LIGHTS,
CB102V UPWASH INDIRECT LIGHTS and CB103V DOWNWASH INDIRECT LIGHTS circuit breakers,
located in Interior J-box. Push breakers to Engage.
(26 ) Test switches, lights and controls for proper operation and evidence of arcing, shorting or overheating.
3. Operations and Inspections
A. Inspect Closet.
(1) Inspect closet for nicks, cracks, dents and security of installation.
(2) Check doors for proper operation.
(3) Check switches and controls for evidence of arcing, shorts or overheating.
(4) Check controls for proper operation.

Page 1
25-40-04-01 Original Issue
CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
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CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
Page 2
25-40-04-01 Original Issue
No. Part Number Description Vendor
4479557-1 AFT BULKHEAD CLOSET ASSY
NAS451-52 BUTTON PLUG (2 ea)
4479061-18 CLOSEOUT PANEL (2 ea)
4479061-20 J-BOX ACCESS PANEL ASSY
(Refer to Chapter 25 in the IPC)
4479096-2 AFT BULKHEAD CLOSET ASSY-RH
(Refer to Chapter 25 in the IPC)
4479096-3 ELECTRICAL COMPONENT ACCESS PANEL ASSY
(Refer to Chapter 25 in the IPC)
4479115-10 AIR SHOW 410 EQUIPMENT INSTL
4479115-11 CABIN MANAGEMENT EQUIPMENT INSTL
4479115-2 STEREO SPEAKER AMP INSTL
(Refer to Chapter 25 in the IPC)
4479543-3 AFT BULKHEAD CLOSET ASSY-LH
4479562-2 AFT BULKHEAD CLOSET-CENTER CABINET
NOTE: Parts not available as complete installations.
When ordering plated parts, the plating number found in section 25-00-06 must follow the
part number without a space.
-
1
2
3
4
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6
7
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Page 1
25-40-04-02 Original Issue
CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
7
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4
3
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CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
Page 2
25-40-04-02 Original Issue
No. Part Number Description Vendor
4479543-3 AFT BULKHEAD CLOSET ASSY-LH
1435-M09-F16-632 HEX STANDOFF MALE/FEMALE (3 ea) 04729
4479010-15 SPRING PIN CLOSEOUT ASSY
(Refer to Chapter 25 in the IPC)
4479010-16 SHELF LIP (3 ea)
4479010-24 ACCESS PANEL
4479061-5 SWITCH COVER ASSY
(Refer to Chapter 25 in the IPC)
4479062-7 AFT BULKHEAD CLOSET SHELL-L
(Refer to Chapter 25 in the IPC)
4479291-5 SHELF LIP - LH LOWER
4479472-6 LIGHT LENS
4479472-7 LIGHT ASSY
4479533-4 AIRSHOW 410-4000 MODULE
4479533-7 MOUNTING PLATE ASSY-FAN
4479533-8 MOUNTING PLATE-FAN
99K31.03 MAGNET LVTL
NOTE: Parts not available as complete installations.
When ordering plated parts, the plating number found in section 25-00-06 must follow the
part number without a space.
-
1
2
3
4
5
6
7
8
9
10
11
-
12

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CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
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DETAIL A
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CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
Page 2
25-40-04-03 Original Issue
No. Part Number Description Vendor
4479472-7 LIGHT ASSY
LTBLK-1X2-02 LIGHT BLOCK 0GZF3
LTBLK-1X3-01 LIGHT BLOCK (2 ea) 0GZF3
4479472-8 LIGHT MOUNTING PLATE
NOTE: Parts not available as complete installations.
When ordering plated parts, the plating number found in section 25-00-06 must follow the
part number without a space.
-
1
2
3

Page 1
25-40-04-04 Original Issue
CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
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DETAIL A
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CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
Page 2
25-40-04-04 Original Issue
No. Part Number Description Vendor
4479533-4 AIRSHOW 410-4000 MODULE
4479533-5 COVER PANEL ASSY
4479533-9 BRACKET ASSY
4479256-8 BRACKET ASSY
4479533-5 COVER PANEL ASSY
4479533-9 BRACKET ASSY
99K31.03 MAGNET (4 ea) LVTL
161.16.500 BRASS HANDLE HAAM
4479061-21 BACKING PLATE-FINGER PUL
99K31.03 MAGNET (4 ea) LVTL
4479533-10 BRACKET
NOTE: Parts not available as complete installations.
When ordering plated parts, the plating number found in section 25-00-06 must follow the
part number without a space.
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25-40-04-05 Original Issue
CESSNA AIRCRAFT COMPANY
MODEL 680
INTERIOR MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG
A
1
DETAIL A
3,10
4,8,11
5
7
69
12
14
2
13