CABIN. DESCRIPTION This section covers cabin compartment seats, seat harnesses, trim, cabin headliner, floor covering, sunvisors, grab handles, headset hooks, coat hooks, drink holders, storage pockets, and radio module assembly. A. Cabin Seats This airplane has two individual front crew seats. The seat s forward and aft travel path is adjusted through seat position control located below the center of the seat cushion. The lower seat cushion is supported by an energy absorption module that reduces impact stroke in the event of a crash. Recline position is controlled through levers located on either side of seat back. Rotating the lever to the recline position when there is no pressure on the seat back will return the seat back to the full up position. Serials -000 thru -8 before SB X-5-07 or SB X-5-: Each front crew seat has a fourpoint restraint, with a single inertia-reel retractor on the shoulder belt. Serials -000 thru -8 after SB X-5-07, -9 thru -99, -50 thru -59 before SB X-5-: Each front crew seat has a four-point restraint, with a dual inertia-reel retractor on the shoulder belt. Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs: Each crew seat has an inflatable, four-point restraint, with a dual inertia-reel retractor on the shoulder belt. An electronic module assembly, mounted below the cabin floor, contains a crash sensor, battery, and related circuitry to monitor the deceleration rate of the airplane. In the event of a crash, the electronic module assembly sends a signal to an inflator assembly mounted to the aft seat frame. The inflator assembly inflates an air bag integral to the shoulder belts that reduces impact trauma to the passenger. Serials w/o + Rear Seat: The rear split passenger seat bench has a fixed seat bottom and features backrests that fold forward independently for each side. Seat backs can be folded forward, with detent pins removed, to provide a semi-flat surface for bulky cargo extending forward from the baggage compartment. The detent pins are located at the base of the backrest. The lower seat cushion is supported by an energy absorption module that reduces impact stroke in the event of a crash. Serials -88 & subs, T-068 & subs w/ + Rear Seat: The rear seats employ a one-piece bench seat and two seat backs configured in 60/0 split. This "+" seating configuration provides for a center seat/restraint area for a third passenger on the pilot-side (LH) seat. Each seat back reclines independently of each other and can be folded forward to provide a semi-flat surface for cargo extending forward from the baggage compartment. Recline position is controlled through a lever located on either side of the seat. The lower seat cushion is supported by an energy absorption module that reduces impact stroke in the event of a crash. Shoulder belt options include two-harness (standard) and threeharness (optional). Additionally, a cargo net between the seat backs and bulkhead secures cargo in the baggage compartment. The aircraft is equipped with provisions for installing two LATCH compliant child seats in the outboard rear seat positions, OR one non-latch compliant seat in the center rear seat position. Lower anchors for the LATCH compliant seats are located in the outboard seat positions. The non-latch compliant seat must be installed using the center seat belt. Three top tether anchors for the child seats are located on the rear bulkhead. For installation of child seat attach fittings, refer to Chapter 5, Attach Fittings. (Refer to 5-0) B. Radio Module Assembly Serials w/o Perspective Avionics: The radio module assembly, mounted to the bolster panel and center console, contains the audio panel, GPS/COM/NAV receivers, transponder, and autopilot. A rearmounted cooling fan and series of cooling ducts prevent the avionics from overheating. Serials w/ Perspective Avionics: The radio module assembly, mounted to the bolster panel and center console, contains the FMS keyboard, autopilot, audio panel, and optional ADF receiver. A rearmounted cooling fan and series of cooling ducts prevent the avionics from overheating. All Page 0 Jan 0
C. Troubleshooting - Serials -88 & subs, T-068 & subs w/ + Rear Seat Trouble - Rear Seats Probable Cause Remedy Seat recline position does automatically spring forward when levers are rotated. Seat recline position does not lock into one or more locations. Grinding noise and/or resistance during seat reclination. Weight and/or object on seat preventing seat break-over position. Seat recline pins are not disengaging from lock hole. Low tension in clock spring. Parts damaged. Seat recline pins are not engaging into lock hole. Parts damaged. Washer not installled between clock spring and seat flange. Remove weight and/or object. Perform Adjustment/Test - Passenger Seat Back Recline Pin Engagement. (Refer to ) Ensure clock spring is installed correctly per passenger seat back installation. (Refer to ) Replace damaged parts. Perform Adjustment/Test - Passenger Seat Back Recline Pin Engagement. (Refer to ) Replace damaged parts. Install washer per passenger seat back installation. (Refer to ) Page 0 Jan 0 Serials -88 & subs, T-068 & subs w/ + Rear Seat
. MAINTENANCE PRACTICES A. Crew Seats (See Figure ) CAUTION: Avoid kneeling or stepping on seats so as to not crush energy absorption modules. () Removal - Crew Seats (a) Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, - 500, -50 & subs, T-000 & subs: Disconnect inflatable restraint interface cable from inflator cable. (b) Remove seat stop bolts and washers from seat rails. (c) Lift up on seat latch and slide seat forward off seat tracks. () Disassembly - Crew Seats (a) Recline handle At side of crew seat back, loosen set screws securing crew seat recline handle to shaft, and slide handle off shaft. Repeat on opposite side of crew seat. (b) Seat back top Disassemble crew seat recline handle. (Refer to ) CAUTION: Use care to avoid damaging upholstery on recline handle shafts. At lower, aft crew seat back, release reclosable fasteners and slide upholstery upward to expose seat back frame. Disassemble crew seat harness lap belt attach clip. (Refer to ) Remove seat belt straps from upholstery, then slide upholstery upward and off seat back. 5 Slide head rest upward and off top of seat back. 6 Serials -0795, -080 thru -99, -50 thru -59 before SB X-5-, -000 thru -079, -0796 thru -089: Remove screws, washers, spacers, fairlead plates, and rub strips securing upholstery angle to seat back top. 7 Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs: Remove bolts, washers, spacers, fairlead plates, shoulder belt guides, and rub strips securing upholstery angle to seat back top. (c) Seat adjustment handle Remove crew seat. (Refer to ) Remove screw, washers, and nut securing handle and seat pins to lower seat frame. Repeat on opposite side of seat frame. Remove handle and spring-loaded seat pins from seat frame. (d) Seat recline locks Fold crew seats to break-over positions. At lower, aft crew seats, release reclosable fasteners to expose lower seat frame. Remove bolts, washers, and nuts securing aft lateral tube and recline locks to lower, aft sides of seat frame. () Assembly - Crew Seats (a) Recline handle At side of crew seat back, position recline handle onto shaft so that handle is pointing in a downward direction, slide reclining handle on shaft, then tighten set screws securing crew seat reclining handle to shaft. Repeat on opposite side of crew seat. (b) Seat back top All Page 0 Jan 0
CAUTION: When routing seat belt straps, ensure belts do not become twisted. Route seat belt straps from inertia reel up seat back until straps rest over top of seat back. Serials -0795, -080 thru -99, -50 thru -59 before SB X-5-, -000 thru -079, -0796 thru -089: Position rub strips between each seat belt strap and top of seat back. Secure upholstery angle to seat back with screws, washers, spacers, fairlead plates, and rub strips. Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs: Position rub strips and shoulder belt guides between each seat belt strap and top of seat back. Secure upholstery angle to seat back with bolts, washers, spacers, fairlead plates, shoulder belt guides, and rub strips. Install head rest on top of seat back. 5 Slide seat back upholstery over the seat back far enough to pass the seat belt straps through the pass-through hole in the upholstery. 6 Assemble crew seat lap belt attach clip. (Refer to ) 7 Place seat back upholstery into position and press firmly on reclosable fasteners to secure upholstery to seat back. 8 Assemble crew seat recline handle. (Refer to ) (c) Seat adjustment handle At bottom of seat, install spring-loaded seat pins into seat frame pin holes. Position handle to attachment points on seat frame. Install screw, washers, and nut securing seat pin and handle to lower seat frame. Repeat on opposite side of seat frame. Install crew seat. (Refer to ) (d) Seat recline locks Position aft lateral tube and recline locks to seat frame and install bolts, washers, and nuts securing recline locks to seat frame. Torque to 0-0 in-lb (. -.5 Nm). Place seat back upholstery into position and press firmly on reclosable fasteners to secure upholstery to seat back. () Installation - Crew Seats CAUTION: Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs: Interface and inflator cable connections requires that LH and RH crew seats are installed at their designated locations. (a) (b) Position seat channel onto forward edge of seat tracks. Lift up on seat latch and slide seat aft onto tracks. Slide seat back to the neutral position. CAUTION: Ensure seat stop screw is installed on LH track of pilot s and co-pilot s seat track. (c) Torque each seat stop screw assembly to 5.0 in-lb (.8 Nm). (d) Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, - 500, -50 & subs, T-000 & subs: Connect inflatable restraint interface cable to inflator cable. (e) Perform Inspection/Check - Crew Seats. (Refer to ) (f) Perform Adjustment/Test - Crew Seat Harness. (Refer to ) Page 0 Jan 0 All
Serials -0795, -080 thru -99, and -50 thru -59 after SB X-5-, Serials -500, -50 & subs, T-000 & subs. 5 8 6 7 5 6 0 9 Serials -0795, -080 thru -99, and -50 thru -59 before SB X-5-, Serials -000 thru -079, -0796 thru -089. NOTE Refer to sheet of for continuation. LEGEND. Bolt. Washer. Spacer. Upholstery Angle 5. Fairlead Plate 6. Rub Strip 7. Screw 8. Shoulder Belt Guide 9. Recline Handle 0. Set Screw. Head Rest Assembly SR_MM5_9B All Figure Crew Seat Installation (Sheet of ) Page 5 0 Jan 0
LEGEND. Bolt. Washer. Spacer 7. Screw. Seat Frame. Energy Absorption Module. Tape, Two Sided 5. Panel, Load Spreader 6. Tray Retainer 7. Aft Lateral Tube 8. Three Hole Recline Lock 9. Two Hole Recline Lock 0. Seat Pin. Spring. Handle. Placard. Nut 7 7 6 5 7 6 7 Serials -000 thru -59. 7 9 0 7 7 CABIN FLOOR NOTE Refer to sheet of for continuation. Serials -0795, -080 thru -99, -50 thru -59 after SB X-5- and Serials - 500, -50 & subs, T-000 & subs : Part of inflatable harness assembly. Ensure seat stop screw is installed on LH track of pilot's and co-pilot's seat track. Page 6 0 Jan 0 Figure Crew Seat Installation (Sheet of ) All SR_MM5_50B
(5) Inspection/Check - Crew Seats (a) Verify security of attach brackets and seat stop screw. CAUTION: If seat is misaligned and cannot be corrected by Adjustment/Test - Crew Seat Longitudinal Alignment, contact Cirrus Design for disposition. (b) (c) (d) Verify seat forward/aft position adjustment catches both seat pins in all locking positions. To determine if both seat pins are engaged, skew seat forward-and-aft, and note whether second seat pin engages after the first seat pin. If seat position adjusts smoothly and seat pins engage simultaneously, seat track is aligned with seat. If seat position is difficult to adjust and/or seat pins require that seat is skewed before seat pins are aligned with seat track holes, perform Adjustment/Test - Crew Seat Longitudinal Alignment. (Refer to ) Verify seat recline lock functions in all recline positions. Visually inspect harness webbing for cut or worn edges, damaged stitching, broken fabric threads, tears, excessive chafe marks, excessive wear, and excessive fraying. Note: A limited amount of frayed webbing will retain sufficient strength necessary to meet the strength requirements of the webbing. Frayed webbing is defined as broken filaments from either the longitudinal or transverse yarns. (e) (f) Verify that broken or fraying webbing filaments are not numerous enough to obscure the identity of any yarn when viewed from a distance of about 8.0 inches (0. cm). Verify amount of fray comprises less than 0% of webbing width and does not exceed 8 inches (0. cm) in length. Ensure edge of webbing is free from cuts or tears. At non-edge locations, verify number of broken yarns does not exceed 5. 5 Ensure number of torn stitches in a stitch pattern does not exceed 5. 6 Verify frayed or distorted webbing does not interfere with proper operation of the restraint system. Ensure harness is clean and does not contain dirt, oil, grease, or other unwanted particles or substances. If necessary, clean harness. (Refer to -0) Inspect break-over pin alignment. Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Vernier Caliper - Any Source Measure All Fold crew seats to break-over positions. At lower, aft crew seats, release reclosable fasteners to expose lower seat frame. Using caliper, verify clearance between center of break-over pin and seat back frame at bottom of upper break-over guide is equal to 0.580 ±0.0 inch (.7 ±0.058 cm). (See Figure ) 5 Verify clearance between center of break-over pin and seat back frame at tangent of lower break-over pin is equal to 0.580 ±0.0 inch (.7 ±0.058 cm). 6 If measurement is not equal to that specified, perform Adjustment/Test - Break-Over Pin Alignment. (Refer to ) 7 Repeat break-over pin alignment inspection for opposite seat. (6) Adjustment/Test - Crew Seat Longitudinal Alignment (See Figure ) Page 7 0 Jan 0
(a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Seat Track Longitudinal Alignment Tool 596-00 Cirrus Design Measure Caliper - Any Source Measure Lithium Marine Grease 50665-00 Cirrus Design Lubricate Permanent Marker - Any Source Mark (b) Remove crew seat. (Refer to ) (c) Verify seat track longitudinal alignment tool slots are free of debris, pins are secure, sliding pin moves freely forward and aft, and calibration label is identified. (d) Align seat track longitudinal alignment tool to seat tracks with sliding mechanism positioned at the upper RH corner. (e) Install slots of tool onto seat tracks. Press sliding and stationary pins on tool into corresponding seat track holes. Note: There is about 0.5 inch (.7 cm) of movement forward to aft when the tool is properly seated on the seat tracks. (f) Move RH side of tool forward and aft to ensure proper movement of the tool. CAUTION: Using 7.0 to 0.0 lbs (. to.5 kg) of force, push tool until binding occurs between the tool and seat tracks. Excessive force will produce inaccurate measurements. (g) (h) Push RH side of tool aft to furthermost orientation. Measure distance between top edge of the tool and top edge of the sliding pin with a caliper. Record measurement as the aft value. CAUTION: Using 7.0 to 0.0 lbs (. to.5 kg) of force, push tool until binding occurs between the tool and seat tracks. Excessive force will produce inaccurate measurements. (i) (j) (k) (l) (m) Push RH side of tool forward to furthermost orientation. Measure distance between top edge of the tool and top edge of the sliding pin with a caliper and record measurement as the forward value. Remove tool from seat tracks. Determine if forward value is within acceptable tolerance. For example: If aft value is 0. inch (0.508 cm) and forward value is -0.5 inch (0.6 cm), use the following formula: Acceptable Forward Value Range = - (Aft Value) ±0.05 Acceptable Forward Value Range = - (0.) ±0.05 = -0. ±0.05 If forward value is within acceptable tolerance, offset pins are not required: Install crew seat. (Refer to ) If forward value is not within acceptable tolerance, offset pins are required. Page 8 0 Jan 0 All
Determine offset required to correct mismatch. Mismatch Range (in inches) Greater Than Maximum Less Than Minimum LH Side RH Side RH Side LH Side 0.0 to 0.00 - Red (+0.00) Black (-0.00) - 0.0 to 0.050 - Orange (+0.00) White (-0.00) - 0.05 to 0.070 - Yellow (+0.060) Purple (-0.060) - 0.07 to 0.090 - Green (+0.080) Blue (-0.080) - 0.09 to 0.0 Black (-0.00) Green (+0.080) Blue (-0.080) Red (0.00) 0. to 0.0 White (-0.00) Green (+0.080) Blue (-0.080) Orange (0.00) 0. to 0.50 Purple (-0.060) Green (+0.080) Blue (-0.080) Yellow (0.060) 0.5 to 0.60 Blue (-0.080) Green (+0.080) Blue (-0.080) Green (0.080). Maximum of 0.60 inch (.06 mm) mismatch may be accommodated, If mismatch is greater than 0.60 inch (.06 mm), contact Cirrus Design for disposition. For example, if aft value is 0. inch (0.508 cm) and forward value is -0.5 inch (0.6 cm), the forward value is out of tolerance below the minimum acceptable value of -0.5 inch (-0.57 cm). To correct this mismatch, use the following formula: Mismatch = (Measured Aft Value + Measured Forward Value) / Mismatch = (0. + (-0.5)) / = -0.0 Note: Mismatch is corrected by replacing aft pin with offset pin where sum of offset and mismatch is closest to the nominal value of zero. Order placard and the appropriate offset pin to correct mismatch. Description P/N or Spec. Supplier Purpose Placard Refer to IPC, Interior Placards and Overlays for approved placards Cirrus Design Label Seat Pin, Red (0.00 inch) Refer to IPC, Forward Seat Installation for Seat Pin, Black (-0.00 inch) approved seat pins Seat Pin, Orange (0.00 inch) Seat Pin, White (-0.00 inch) Seat Pin, Yellow (0.060 inch) Seat Pin, Purple (-0.060 inch) Seat Pin, Green (0.080 inch) Cirrus Design Offset Pin All Seat Pin, Blue (-0.080 inch) Page 9 0 Jan 0
For example, if mismatch is -0.0 inch (-0.058 cm), use pin required to offset as close to zero as possible. Offset = - (Mismatch) Offset = - (-0.0) = 0.0 A pin with offset of 0.00 inch (Red) will bring longitudinal mismatch within tolerance. Note: It may be necessary to use opposite displacement seat pins on each side of seat to compensate for misalignment. For example, if mismatch is -0.09 inch (-0. cm), use combination of pins required to offset as close to zero as possible. Offset = - (Mismatch) Offset = - (-0.09) = 0.09 A pin with offset of 0.080 inch (Green) installed at RH side and a pin with offset of 0.00 inch (Black) installed at LH side will bring longitudinal mismatch within tolerance. Disassemble crew seat adjustment handle. (Refer to ) Note: Mismatch measured using the Seat Track Longitudinal Alignment Tool is only nominal track alignment. Other factors such as seat shape may also influence pin engagement function. Any selection of offset pins may be used such that best engagement function is achieved. Replace the existing pin(s) with the offset pin(s). Discard the existing pin(s). 5 Assemble crew seat adjustment handle. (Refer to ) 6 Lubricate seat pins with lithium marine grease. 7 Verify screws are loose enough to permit smooth, unrestricted forward and aft travel of seat. CAUTION: Once seat is modified using offset seat pins, it may only be installed in seat location affected by longitudinal mismatch. 8 Install crew seat. (Refer to ) 9 Verify seat forward and aft position adjusts to all locking positions with relative ease. 0 Using marker on placard, indicate pins utilized, location of each pin, and seat location (pilot or co-pilot). Attach placard to visible location on lower seat frame. Page 0 0 Jan 0 All
SEAT TRACK SEAT TRACK CALIBRATION LABEL FRONT VIEW SLIDING PINS STATIONARY PINS BACK VIEW SLOTS SLIDE PLATE Example: - 0.5 inch (0.6 cm) SLIDE PLATE Example: + 0. inch (0.508 cm) FORWARD (NEGATIVE) VALUE POSITION NOTE Verify seat track longitudinal alignment tool slots are free of debris, pins are secure, sliding pin moves freely forward and aft, and calibration label is identified. Install slots of tool onto the seat tracks. Press sliding and stationary pins into corresponding seat track holes. Using 7.0 to 0.0 lbs (. to.5 kg) of force, push tool until binding occurs between the tool and seat tracks. Excessive force will produce inaccurate measurements. All Figure Seat Track Longitudinal Adjustment AFT (POSITIVE) VALUE POSITION LEGEND. Seat Track Longitudinal Alignment Tool SR_MM5_8 Page 0 Jan 0
(7) Adjustment/Test - Break-Over Pin Alignment (See Figure ) (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Caliper - Any Source Measure (b) Free break-over pin by slightly loosening four sets of attaching hardware securing breakover guides to seat frame. (c) Press break-over pin and guides inboard or outboard as required until break-over pin is positioned within tolerance. (d) Using a caliper, verify clearance between center of break-over pin and seat back frame at bottom of upper break-over guide is equal to 0.580 ±0.0 inch (.7 ±0.058 cm). (e) Verify clearance between center of break-over pin and seat back frame at tangent of lower break-over pin is equal to 0.580 ±0.0 inch (.7 ±0.058 cm). (f) Tighten four sets of attaching hardware securing break-over guides to seat frame. (8) Cleaning - Crew Seats Periodically vacuum and clean crew seats with approved cleaning solutions to ensure surface dirt and dust removal. (Refer to -0) Page 0 Jan 0 All
0.580 ±0.0 inch (.7 ±0.058 cm) BREAK-OVER GUIDES 0.580 ±0.0 inch (.7 ±0.058 cm) 5 BREAK-OVER PIN SEAT FRAME NOTE Measure distance between center of break-over pin and seat frame at bottom of upper break-over guide. Measure distance between center of break-over pin and seat frame at tangent of lower break-over pin. All Figure Break-Over Pin Alignment LEGEND. Bolt. Washer. Nut SR_MM5_5 Page 0 Jan 0
B. Crew Seat Harness (See Figure ) () Removal - Crew Seat Harness (a) Remove crew seat. (Refer to ) (b) Disassemble crew seat back top. (Refer to ) (c) Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, - 500, -50 & subs, T-000 & subs: Disconnect harness inflator hose from inflator assembly. (d) Serials -000 thru -8 before SB X-5-07: Remove inertia reel cover from inertia reel. (e) Serials -000 thru -8 before SB X-5-07: Remove bolts and washers securing single inertia reel to crossover bar on back of crew seat. (f) Serials -000 thru -8 after SB X-5-07: Remove bolts, washers, and nuts securing dual inertia reel to crossover bar on back of crew seat. (g) Serials -9 & subs, T-000 & subs: Remove bolts and washers securing dual inertia reel to crossover bar on back of crew seat. () Disassembly - Crew Seat Harness Lap Belt Attach Clip (a) Disassemble crew seat recline handle. (Refer to ) CAUTION: Use care to avoid damaging upholstery on recline handle shafts. (b) At lower, aft crew seat back, release reclosable fasteners and slide upholstery upward to expose seat back frame. (c) Serials -000 thru -0 before SB X-5-09: Remove bolt, washers, and spacer securing lap belt attach clip to side of lower crew seat frame. Repeat on opposite side of crew seat. (d) Serials -000 thru -0 after SB X-5-09, -05 & subs, T-000 & subs: Remove bolt, washer, spacer, and anti-rotation tab securing lap belt attach clip to side of lower crew seat frame. Repeat on opposite side of crew seat. () Assembly - Crew Seat Harness Lap Belt Attach Clip (a) Serials -000 thru -0 before SB X-5-09: At forward lap belt installation hole, secure lap belt attach clip to lower seat assembly with spacer, washers, and bolt. Torque bolt to 55 in-lb (6. Nm). Verify lap belt attach clip rotates freely. Repeat on opposite side of seat. (b) Serials -000 thru -0 after SB X-5-09, -05 & subs, T-000 & subs: At forward lap belt installation hole, secure lap belt attach clip to lower seat assembly with anti-rotation tab, spacer, washer, and bolt. Torque bolt to 55 in-lb (6. Nm). Verify lap belt attach clip rotates freely from stop to stop. Repeat on opposite side of crew seat. (c) Place seat back upholstery into position and press firmly on reclosable fasteners to secure upholstery to seat back. (d) Assemble crew seat recline handle. (Refer to ) () Installation - Crew Seat Harness (a) Serials -000 thru -8 before SB X-5-07: Position single inertia reel to crossover bar with reel positioned upward and secure to seat back with bolts and washers. (b) Serials -000 thru -8 after SB X-5-07: Position dual inertia reel to crossover bar with reels positioned upward and secure to seat back with bolts, washers, and nuts. (c) Serials -9 & subs, T-000 & subs: Position dual inertia reel to crossover bar with reels positioned upward and secure to seat back with bolts and washers. (d) Serials -000 thru -8 before SB X-5-07: Press inertia reel cover to inertia reel. Page 0 Jan 0 All
(e) Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, - 500, -50 & subs, T-000 & subs: Connect inflator hose to inflator assembly. Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Loctite Any Source Inflator hose installation. Route inflator hose from seat belt assembly between seat belt webbing and seat back web, ensuring twists and bends are minimized. Apply Loctite to threads of harness inflator hose fitting. Connect harness inflator hose to inflator assembly. Torque hose fitting to 0-0 in-lb (. -.7 Nm). (f) Assemble crew seat back top. (Refer to ) (g) Install crew seat. (Refer to ) (h) Perform Adjustment/Test - Crew Seat Harness. (Refer to ) (5) Inspection/Check - Crew Seat Harness - Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs (a) Serials -0795, -080 thru -60, -60 thru -80, -8 thru -89, - 8 thru -86: Remove RH crew seat. (Refer to ) (b) Serials -60, -8, -80, -86 & subs, T-000 & subs: Remove LH crew seat. (Refer to ) (c) Serials -0795, -080 thru -60, -60 thru -80, -8 thru -89, - 8 thru -86: Remove cabin floor access panel CFR. (Refer to 06-00) (d) Serials -60, -8, -80, -86 & subs, T-000 & subs: Remove cabin floor access panel CFL. (Refer to 06-00) (e) Verify security of electronic module assembly mounting hardware. (f) Verify security of connection between electronic module assembly and cable interface assembly. (g) Disassemble crew seat recline handle. (Refer to ) CAUTION: Use care to avoid damaging upholstery on recline handle shafts. All (h) At lower, aft crew seat back, release reclosable fasteners and slide upholstery upward to expose seat back frame. (i) Verify security of inflator assembly mounting hardware. (j) Verify security of connection between harness inflator hose and inflator assembly. If loose, torque hose fitting to 0-0 in-lb (. -.7 Nm). (k) Serials w/ inflator part number 090-005: Verify security of connection between inflator assembly fitting and inflator assembly. If loose, torque fitting to 50-70 in-lb (5.6-7.9 Nm). (l) Verify security of connection between inflator cable assembly and inflator assembly. (m) Visually inspect exposed hoses and cables for tears, fraying, and excessive wear. (n) Serials -0795, -080 thru -60, -60 thru -80, -8 thru -89, - 8 thru -86: Install cabin floor access panel CFR. (Refer to 06-00) (o) Serials -60, -8, -80, -86 & subs, T-000 & subs: Install cabin floor access panel CFL. (Refer to 06-00) (p) Place seat back upholstery into position and press firmly on reclosable fasteners to secure upholstery to seat back. (q) Assemble crew seat recline handle. (Refer to ) (r) Serials -0795, -080 thru -60, -60 thru -80, -8 thru -89, - 8 thru -86: Install RH crew seat. (Refer to ) AMM_TR_-0 Page 5 0 May 06
(s) Serials -60, -8, -80, -86 & subs, T-000 & subs: Install LH crew seat. (Refer to ) (t) Perform Adjustment/Test - Crew Seat Harness. (Refer to ) (6) Adjustment/Test - Crew Seat Harness - Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs The system diagnostic tool (SDT) is a electronic, hand-held testing device used to verify inflatable restraint system functionality and facilitate component troubleshooting. The SDT connects directly to the diagnostic connector on the inflatable restraint cable interface assembly. LEDs for battery, sensor, and inflator indicate green for pass and red for fail. A three-position switch enables testing of multiple seats. WARNING: Electronic module assembly must be securely installed in airplane prior to testing or inadvertent system deployment may occur. (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose System Diagnostic Tool 508987-0 AmSafe Aviation Phoenix, Arizona 850 800-8-567 Test inflatable restraint system. (b) Set SDT power switch to ON position. (c) Verify SDT battery indicator illuminates green. If SDT battery indicator illuminates red, replace SDT battery. (d) Set SDT toggle switch to number of seats connected to electronic module assembly. (e) Remove right mid console trim. (Refer to ) (f) Disconnect diagnostic connector from center console by sliding plug off rail from connector plug. CAUTION: Disconnect SDT from diagnostic connector once test is completed. If SDT remains connected to diagnostic connector for an extended period of time, power is drained from electronic module assembly. (g) Connect SDT connector to diagnostic connector on interface cable. (h) Verify LEDs on SDT indicate green. (i) If one or more of the LEDs indicate red, perform the following steps: Check all cable assembly connectors and retest. If battery and/or sensor LED indicates red, replace the electronic module assembly and retest. (Refer to ) If inflator LED indicates red, replace the inflator cable assembly and retest. (Refer to ) If inflator LED still indicates red, replace the inflator assembly and retest. (Refer to ) 5 If any fail condition exists after replacing electronic module assembly, inflator cable, and inflator assembly, replace the interface cable and retest. (Refer to ) (j) Set SDT power switch to OFF position. (k) Disconnect SDT connector from diagnostic connector on interface cable. (l) Install diagnostic connector to RH center console flange by sliding plug forward onto rail until connector locks into place with connector plug. (m) Install right mid console trim. (Refer to ) AMM_TR_-0 Page 6 0 Jan 0 All
C. Inflatable Restraint System, Inflator Assembly - Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs (See Figure ) WARNING: The inflator assembly is a stored, gas/energetic material device. Severe personal injury or bodily harm may be caused by misuse and/or tampering. Do not tamper with or mishandle the product in any way. Never attempt to open the inflator to service the inflator system. Never apply electrical current to the electronics connection. () Removal - Inflator Assembly (a) Remove crew seat. (Refer to ) (b) Disassemble crew seat recline handle. (Refer to ) CAUTION: Use care to avoid damaging upholstery on recline handle shafts. (c) At lower, aft crew seat back, release reclosable fasteners and slide upholstery upward to expose seat back frame. (d) Disconnect inflator cable assembly from inflator assembly. (e) Disconnect harness inflator hose from inflator assembly. (f) Loosen bolts, washers, spacers, and nuts securing inflator assembly clamps. (g) Remove inflator assembly from seat back. (h) Serials w/ inflator part number 090-005: To remove inflator assembly fitting, disconnect fitting from inflator assembly. () Installation - Inflator Assembly (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Loctite Any Source Inflator hose and inflator assembly fitting installation. (b) (c) (d) (e) Serials w/ inflator part number 090-005: To install inflator assembly fitting: Apply Loctite to threads of inflator assembly fitting. Connect fitting to inflator assembly. Torque fitting to 50-70 in-lb (5.6-7.9 Nm). Position inflator assembly into clamps and secure to seat with bolts, washers, spacers, and nuts. Apply Loctite to threads of harness inflator hose fitting. Connect harness inflator hose to inflator assembly. Torque hose fitting to 0-0 in-lb (. -.7 Nm). Note: Serials w/ inflator part number 090-00: Inflator cable connection is adjacent to hose fitting. (f) (g) Serials w/ inflator part number 090-005: Inflator cable connection is on upper end of inflator assembly. Connect inflator cable assembly to inflator assembly. Place seat back upholstery into position and press firmly on reclosable fasteners to secure upholstery to seat back. (h) Assemble crew seat recline handle. (Refer to ) (i) Install crew seat. (Refer to ) (j) Perform Adjustment/Test - Crew Seat Harness. (Refer to ) Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs AMM_TR_-0 Page 7 0 May 06
D. Inflatable Restraint System, Electronic Module Assembly - Serials -0795, -080 thru - 99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs (See Figure ) WARNING: Avoid magnetic fields near the electronic module assembly as inadvertent system deployment may occur. Secure electronic module assembly to fuselage floor before connecting wire harness. An unsecured, electrically connected electronic module assembly may result in inadvertent system deployment. Do not drop the electronic module assembly as damage to the electronics, battery, or sensor may occur. () Removal - Electronic Module Assembly (a) Serials -0795, -080 thru -60, -60 thru -80, -8 thru -89, - 8 thru -86: Remove RH crew seat. (Refer to ) (b) Serials -60, -8, -80, -86 & subs, T-000 & subs: Remove LH crew seat. (Refer to ) (c) Serials -0795, -080 thru -60, -60 thru -80, -8 thru -89, - 8 thru -86: Remove cabin floor access panel CFR. (Refer to 06-00) (d) Serials -60, -8, -80, -86 & subs, T-000 & subs: Remove cabin floor access panel CFL. (Refer to 06-00) (e) Disconnect cable interface assembly from electronic module assembly. (f) Remove screws and nut plates securing electronic module assembly to fuselage floor. (g) Remove electronic module assembly from airplane. () Installation - Electronic Module Assembly (a) Position electronic module assembly to fuselage floor with directional arrow facing forward and secure with screws and nut plates. (b) Torque screws to 6.0 ±.0 in-lb (0.68 ±0. Nm). Torque stripe not required. (c) Connect interface cable to electronic module assembly. (d) Serials -0795, -080 thru -60, -60 thru -80, -8 thru -89, - 8 thru -86: Install cabin floor access panel CFR. (Refer to 06-00) (e) Serials -60, -8, -80, -86 & subs, T-000 & subs: Install cabin floor access panel CFL. (Refer to 06-00) (f) Serials -0795, -080 thru -60, -60 thru -80, -8 thru -89, - 8 thru -86: Install RH crew seat. (Refer to ) (g) Serials -60, -8, -80, -86 & subs, T-000 & subs: Install LH crew seat. (Refer to ) (h) Perform Adjustment/Test - Crew Seat Harness. (Refer to ) AMM_TR_-0 Page 8 0 Jan 0 Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs
E. Inflatable Restraint System, Interface Cable - Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs (See Figure ) () Removal - Interface Cable (a) Remove crew seats. (Refer to ) (b) Serials -0795, -080 thru -60, -60 thru -80, -8 thru -89, - 8 thru -86: Remove cabin floor access panels CFR, CFR, and CFL. (Refer to 06-00) (c) Serials -60, -8, -80, -86 & subs, T-000 & subs: Remove cabin floor access panels CFR, CFL, and CFL. (Refer to 06-00) (d) Remove right mid console trim. (Refer to ) (e) At RH center console flange, disconnect diagnostic connector assembly from center console by sliding connector assembly forward and off mounting rail. (f) Remove screw, washer, and clamp securing interface cable to bracket mounted on seat attach bracket. Repeat for opposite side of airplane. (g) Remove cable ties securing interface cable to cable tiedowns on spar tunnel. (h) Disconnect interface cable from electronic module assembly. (i) Serials -0795, -080 thru -60, -60 thru -80, -8 thru -89, - 8 thru -86: Route interface cables. At RH aft corner of fuselage floor, route RH branch of interface cable from electronic module assembly aft along floor, and down through fuselage floor. Route interface cable along forward surface of spar tunnel, RH forward longeron, and up through RH pass-through hole. At LH aft corner of fuselage floor, route LH branch of interface cable down through fuselage floor, along forward surface of spar tunnel, LH forward longeron, and up through LH pass-through hole. (j) Serials -60, -8, -80, -86 & subs, T-000 & subs: Route interface cables. At LH aft corner of fuselage floor, route LH branch of interface cable from electronic module assembly aft along floor, and down through fuselage floor. Route interface cable along forward surface of spar tunnel, LH forward longeron, and up through LH pass-through hole. At RH aft corner of fuselage floor, route RH branch of interface cable down through fuselage floor, along forward surface of spar tunnel, RH forward longeron, and up through RH pass-through hole. (k) At center console, locate diagnostic connector assembly of interface cable extending from two pass-through holes in fuselage floor just aft of the forward pulley gang. Retrieve remaining interface cable from pass-through holes and remove interface cable from airplane. () Disassembly - Interface Cable To disassemble diagnostic connector mounting rail, perform the following steps: (a) Remove right mid console trim. (Refer to ) (b) At RH center console flange, disconnect diagnostic connector assembly from center console by sliding connector assembly forward and off mounting rail. (c) Remove screws securing mounting rail to RH center console flange. () Assembly - Interface Cable To assemble diagnostic connector mounting rail, perform the following steps: (a) Install screws securing mounting rail to RH center console flange. (b) Install connector assembly to RH center console flange by sliding plug aft on mounting rail until connector assembly locks into place. (c) Install right mid console trim. (Refer to ) Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs Page 9 0 Jan 0
() Installation - Interface Cable (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Cable Ties - Any Source Secure cable. (b) At center console, locate pass-through holes in fuselage floor aft of forward pulley gang. (c) Serials -0795, -080 thru -60, -60 thru -80, -8 thru -89, - 8 thru -86: Route interface cables. Route LH branch of interface cable through LH pass-through hole, LH forward longeron, along forward surface of spar tunnel, and up through LH aft corner of fuselage floor. Route RH branch of interface cable through RH pass-through hole, RH forward longeron, and along forward surface of spar tunnel. At RH aft corner of fuselage floor, route RH branch of wire harness up through fuselage floor, and electronic module assembly branch of wire harness forward along floor. (d) Serials -60, -8, -80, -86 & subs, T-000 & subs: Route interface cables. Route RH branch of interface cable through RH pass-through hole, RH forward longeron, along forward surface of spar tunnel, and up through RH aft corner of fuselage floor. Route LH branch of interface cable through LH pass-through hole, LH forward longeron, and along forward surface of spar tunnel. At LH aft corner of fuselage floor, route LH branch of wire harness up through fuselage floor, and electronic module assembly branch of wire harness forward along floor. (e) Connect interface cable to electronic module assembly. (f) Position interface cable to cable tiedowns on spar tunnel and secure with cable ties. (g) Position interface cable to bracket mounted on seat attach bracket and secure with screw, washer, and clamp. Repeat for opposite side of airplane. (h) Install connector assembly to RH center console flange by sliding plug aft on mounting rail until connector assembly locks into place. (i) Install right mid console trim. (Refer to ) (j) Serials -0795, -080 thru -60, -60 thru -80, -8 thru -89, - 8 thru -86: Install cabin floor access panels CFR, CFR, and CFL. (Refer to 06-00) (k) Serials -60, -8, -80, -86 & subs, T-000 & subs: Install cabin floor access panels CFR, CFL, and CFL. (Refer to 06-00) (l) Install crew seats. (Refer to ) (m) Perform Adjustment/Test - Crew Seat Harness. (Refer to ) Page 0 0 Jan 0 Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs
F. Inflatable Restraint System, Inflator Cable - Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs (See Figure ) () Removal - Inflator Cable (a) Disassemble crew seat recline handle. (Refer to ) CAUTION: Use care to avoid damaging upholstery on recline handle shafts. (b) At lower, aft crew seat back, release reclosable fasteners and slide upholstery upward to expose seat back frame. (c) Remove cable ties securing inflator cable to cable tiedowns on seat back. (d) Disconnect inflator cable from inflator assembly. (e) Disconnect inflator cable from interface cable. Remove inflator cable from airplane. () Installation - Inflator Cable (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Cable Ties - Any Source Secure cable. (b) Connect inflator cable to interface cable. Note: Serials w/ inflator part number 090-00: Inflator cable connection is adjacent to hose fitting. Route inflator cable to lower end of inflator assembly. (See Figure ) Serials w/ inflator part number 090-005: Inflator cable connection is on upper end of inflator assembly. Route cable through crew seat tube to upper end of inflator assembly. (See Figure ) (c) Connect inflator cable to inflator assembly. Note: If replacing inflator part number 090-00 with 090-005, an additional cable tiedown must be installed on seat back. (See Figure ) (d) (e) Position inflator cable to cable tiedowns on seat back and secure with cable ties. Place seat back upholstery into position and press firmly on reclosable fasteners to secure upholstery to seat back. (f) Assemble crew seat recline handle. (Refer to ) (g) Perform Adjustment/Test - Crew Seat Harness. (Refer to ) Serials -0795, -080 thru -99, -50 thru -59 after SB X-5-, -500, -50 & subs, T-000 & subs AMM_TR_-0 Page 0 May 06
INFLATOR ASSEMBLY NOTE Refer to sheet of for Inflator Assembly. Serials -9 & subs, T-000 & subs. 9 6 0 5 9 6 0 Serials -000 thru -8 after SB X-5-07. Serials -000 thru -8 after SB X-5-09 and SB X-5-07 optional lap belt relocation. AMM_TR_-0 Page 0 May 06 Serials -000 thru -8 before SB X-5-07. Serials -000 thru -0 before SB X-5-09. 6 0 6 0 Serials -000 thru -8 after SB X-5-09 and before SB X-5-07 optional lap belt relocation. Figure Crew Seat Harness and Inflatable Restraint System Installation (Sheet of ) 9 All LEGEND. Dual Inertia Reel. Bolt. Washer 5. Nut 6. Spacer 9. Anti Rotation Tab 0. Lap Belt Attach Clip. Inertia Reel Cover. Single Inertia Reel SR_MM5_D
7 5 6 8 Serials w/ Inflator p/n 090-00. 6 5 8 7 7 0 9 6 0 8 5 8 9 7 RH CENTER CONSOLE FLANGE 7 NOTE WIRE HARNESS Serials -0795, -080 thru -60, -60 thru -80, -8 thru -89, -8 thru -86: Installed on RH side of cabin floor. 5 6 CABIN FLOOR LEGEND. Dual Inertia Reel. Clamp. Bolt. Washer 5. Nut 6. Spacer 7. Inflator Hose 8. Inflator Cable 9. Anti Rotation Tab 0. Lap Belt Attach Clip. Inflator Assembly. Bracket 5. Electronic Module Assembly 6. Plate Assembly 7. Interface Cable 8. Screw 9. Mounting Rail 0. Connector Plug. Fitting If replacing inflator part number 090-00 with 090-005, an additional cable tiedown must be installed on seat back. Serials -0795, -080 thru -99 and, -50 thru -59 after SB X-5-, Serials -500, -50 & subs, T-000 & subs. SR_MM5_5C All Figure Crew Seat Harness and Inflatable Restraint System Installation (Sheet of ) AMM_TR_-0 Page 0 May 06
G. Passenger Seats - Serials -000 & subs, T-000 & subs w/o + Rear Seat (See Figure 5-05) CAUTION: Detent pins must be installed when occupants are seated in the passenger seats. Avoid kneeling or stepping on seats so as to not crush energy absorption modules. () Removal - Passenger Seats (a) Remove seat cushion. (b) Remove cotter pins used to secure the seat assembly to floor. Note: Access to detent pins is best achieved through the baggage door. (c) Remove the detent pins from the seat back. (d) Lift forward edge of seat assembly up, pull seat assembly forward, and remove seats. () Installation - Passenger Seats (a) Install seats on aft floor and insert the rear studs into the attach fittings. (b) Secure forward seat brackets with cotter pins. (c) Place the detent pins into position. (d) Secure seat cushion. () Cleaning - Passenger Seats (Refer to -0) Periodically vacuum and clean crew seats with approved cleaning solutions to ensure surface dirt and dust removal. (Refer to -0) AMM_TR_-0 Page 5 Dec 0 Serials -000 & subs, T-000 & subs w/o + Rear Seat
H. Passenger Seats - Serials -88 & subs, T-068 & subs w/ + Rear Seat (See Figure 5-05), (See Figure 6) CAUTION: Avoid kneeling or stepping on seats so as to not crush energy absorption modules. Remove seat base assembly secured with reclosable fasteners carefully so as to not damage fasteners. () Removal - Passenger Seat Base (a) Remove cotter pins used to secure the seat base assembly to floor. (b) Lift forward edge of seat base assembly up, pull seat base assembly forward to release reclosable fasteners, and remove seat base assembly. () Installation - Passenger Seat Base (a) Install seat base assembly on aft floor and press rear seat base assembly firmly onto reclosable fasteners. Note: If seat base wobbles, one to three washers may be installed at each pin below the seat or cotter pin to eliminate excess pin engagement. (b) Secure forward seat brackets with cotter pins. () Removal - Passenger Seat Back (a) At outboard seat, slip harness strap free of seat belt guide and stow harness aft of seat. (b) Serials w/ three-harness installation: If removing LH seat, disengage LH center harness latch securing seat harness to LH center harness mount. Unbuckle seat harness, and route harness aft through seat pass-through hole. (c) With no pressure on seat back, rotate lever to recline position and fold seat back forward. (d) Remove bolts, washers, clock spring, housing, and nuts securing seat back to floor brackets, and remove seat back assembly. () Disassembly - Passenger Seat Back (a) Recline handle At outboard seat, loosen set screws securing crew seat recline handle to shaft, and slide handle off shaft. (b) Seat belt guide At aft seat, remove screws securing seat belt guide to seat. (c) Baggage strap anchor plates At aft seat, remove screws securing anchor plates to seat. (d) Actuator assembly At outboard seat, loosen jam nut at base of recline pin housing. Depress pin shoulder flush with recline pin housing while loosening barrel nut until pin slot can be detached from cable ball. Remove spring from recline pin housing. Remove recline handle. (Refer to ) 5 Remove retaining ring securing actuator shaft to seat. 6 Slide actuator shaft inboard at flanged bushing and disengage from cable S-hook. 7 Remove flanged bushing from seat. 8 Remove screws and washers securing recline pin housing to seat. 9 Release cable clip and remove cable from pass-through hole. 0 Remove grommet from pass-through hole. (e) Seat hinge plates At inboard/outboard seat, remove screws, washers, and nuts securing seat hinge plates to seat. Serials -88 & subs, T-068 & subs w/ + Rear Seat Page 5 0 Jan 0
(5) Assembly - Passenger Seat Back (a) Recline handle Position recline handle onto shaft so that handle is pointing in a downward direction, slide reclining handle on shaft, then tighten set screws securing crew seat reclining handle to shaft. (b) Seat belt guide At aft seat, position seat belt guide to aft seat and install screws securing seat belt guide to seat. (c) Baggage strap anchor plates At aft seat, install screws securing anchor plates to seat. (d) Actuator assembly At outboard seat, install grommet at pass-through hole. Route cable in pass-through hole and secure to cable clip. Install screws and washers securing recline pin housing to seat. Install flanged bushing into seat. 5 Engage actuator shaft onto cable S-hook and slide actuator shaft outboard through seat at flanged bushing. 6 Install retaining ring securing actuator shaft to seat. 7 Install recline handle. (Refer to ) 8 Install spring into recline pin housing. 9 Route cable through recline pin housing and position cable ball in pin slot. 0 Depress pin shoulder flush with recline pin housing while tightening barrel nut until spring compression is maintained by pin tension. Tighten jam nut at base of recline pin housing. (e) Seat hinge plates At inboard/outboard seat, install screws, washers, and nuts securing seat hinge plates to seat. (6) Installation - Passenger Seat Back (a) Position clock spring to outboard floor bracket so that outer clock spring tab is facing aft, and inner clock spring tab is captured by slot in outboard floor bracket. (b) Position seat back to floor brackets so that lower edge of aft outboard seat flange contacts outer clock spring tab. Secure seat to floor brackets with bolts, washers, clock spring, housing, and nuts. (c) Fold passenger seat to upright position. CAUTION: When routing seat belt straps, ensure belts do not become twisted. (d) At outboard seat, slip outboard harness into seat belt guide and route harness forward. (e) Serials w/ three-harness installation: If installing LH seat, route center harness forward through seat pass-through hole and engage LH center harness latch to LH center harness mount. Buckle seat harness. (f) If actuator assembly was removed, perform Adjustment/Test - Passenger Seat Back Recline Pin Engagement. (Refer to ) (7) Adjustment/Test - Passenger Seat Back Recline Pin Engagement (See Figure 5) (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Vernier Caliper - Any Source Measure Page 6 0 Jan 0 Serials -88 & subs, T-068 & subs w/ + Rear Seat