N780AS

Part: FITTING — WORN (CARGO BAY) · airframe 43,793 hrs · 24,601 cycles

AFT CARGO PIT NET TIE DOWN FITTING WORN AT BS 787 LBL 18. AFT CARGO NET TIE DOWN TRACK AT BS 727G+10 807+12 IAW SRM 53-00-53 REPAIR 2 (LBL 18).

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 43,793 hrs · 24,601 cycles

CORROSION FOUND BEYOND LIMITS ON THE RT CARGO TIE DOWN TRACK. REPLACED WITH NEW PART IAW SRM 53-00-53 REPAIR 2 FIG 201.

Part: FRAME — DAMAGED (FUSELAGE)

PAE: DAMAGED FRAME AT BSTA 500A, RBL 22, UNDER SIDE OF UPPER FLANGE. REPAIRED FRAME AT BSTA 500A, RBL 22, IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE)

PAE: FRAME CRACKED AT BIN RAIL. REPAIRED FRAME AT BSTA 907 RT BIN RAIL ATTACH POINT IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE)

PAE: FRAME CRACKED AT BIN RAIL ATTACH POINT. REPAIRED FRAME AT BSTA 500A LT BIN RAIL ATTACH POINT SRM. FABRICATED REPAIR PARTS. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE: CORROSION ON FLOORBEAM. BLENDED CORROSION, FABRICATED REPAIR STRAP AND INSTALLED IAW SRM. (K)

Part: FRAME — CORRODED (FUSELAGE)

PAE: CORROSION ON BSTA 794, FRAME BETWEEN STR 23R-26R. REMOVED AND REPLACED FRAME AT BSTA 794 BETWEEN STRINGERS 16 RT TO 26 RT IAW SRM. (K)

Part: FLOORBEAM — CORRODED (BS 986)

PAE - FOUND CORROSION ON FLOORBEAM AT BS 986.5, RBL 44 TO LBL 44, WL 208. REPAIRED PER ER 05-5163, AND EA 5310-02558. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

PAE: CORROSION ON FLOORBEAM. REPAIRED IAW ER, EA, AND SRM. (K)

Part: FLOORBEAM — CORRODED (FS 947)

PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED FLOORBEAM PER ER 05-5162 AND IAW B737-400 SRM 53-60-51, 51-40-02. (M)

Part: THRESHOLD — CORRODED (FS 807)

PAE - FOUND CORROSION ON AFT CARGO BAY DOOR CUT OUT SUB THRESHOLD WEB. REMOVED AND REPLACED AFT CARGO BAY SUB THRESHOLD WEB IAW B737-400 SRM 51-40-02. (M)

Part: FRAME — CORRODED (FS 270)

PAE - FOUND CORROSION ON FRAME AT BS 270, WL 208, RBL 8. REMOVED AND FABRICATED NEW FRAME IAW B737-400 SRM 51-40-05 AND 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON FLOORBEAM AT BS 312, WL 208, LBL 11. REMOVED AND REPLACED SECTION IAW B737-400 SRM 53-10-51 AND ASA EA 5310-02552. (M)

Part: FRAME — CORRODED (BS 847)

PAE - FOUND CORROSION ON BS 847 FRAME. REMOVED AND REPLACED FRAME IAW B737-400 SRM 51-40-05, 51-40-02, AND DWG 65-47960. (M)

Part: SILL — CORRODED (FS 914)

PAE - FOUND CORROSION ON LT MOPSILL AT BS 950, WL 208. REMOVED AND REPLACED MOPSILL IAW B737-400 SRM 5360-15, 51-40-02, 51-40-08, AND AMM 51-21-41. (M)

Part: STRAP — CORRODED (FS 775-810)

PAE - FOUND CORROSION ON AFT CARGO BAY DOORWAY FLOOR STRAP. REMOVED AND REPLACED STRAP IAW B737-400 SRM 53-60-15 AND 51-40-02. (M)

Part: FRAME — CORRODED (FS 794)

PAE - FOUND CORROSION ON BS 794, FRAME BETWEEN STRINGER 23R-26R. REMOVED AND REPLACED FRAME AT BS 794, BETWEEN STRINGERS 16 TO 26 RT, IAW B737-400 SRM 51-40-02. (M)

Part: SILL — CORRODED (BS 950)

PAE - FOUND CORROSION ON LT MOPSILL AT BS 950, WL 208. REMOVED AND REPLACED MOPSILL IAW B737-400 SRM 53-60-15, 51-40-02, 51-40-08 AND AMM 51-21-41. (M)

Part: STRINGER CLIP — CRACKED (FS 500A)

PAE - FOUND STRINGER CLIP CRACKED AT BS 500A, STRINGER 11 RT. REMOVED AND REPLACED STRINGER CLIP AT BS 500A, STRINGER 11 RT IAW B737-400 SRM 51-40-02. (M)

Part: SILL — CORRODED (FS 950-990)

PAE - FOUND RIGHT MOPSILL AT BS 950 TO 990 WL 208 CORRODED. REMOVED AND REPLACED RT MOPSILL AT BS 950-990 IAW B737-400 SRM 53-60-15.

Part: STRINGER CLIP — CRACKED (FS 500B)

PAE - FOUND STRINGER CLIP CRACKED AT BS 500B, STRINGER 11 RT. REMOVED AND REPLACED STRINGER CLIP AT BS 500B, STRINGER 11 RT IAW B737-400 SRM 51-40-02. (M)

Part: STRINGER CLIP — CRACKED (BS 500D)

PAE - FOUND STRINGER CLIP CRACKED AT BS 500D, STRINGER 11 RT. REMOVED AND REPLACED STRINGER CLIP AT BS 500D, STRINGER 11 RT IAW B737-400 SRM 51-40-02. (M)

Part: FAILSAFE — CORRODED (FS 794)

PAE - FOUND FAILSAFE AT BS 794, RBL 19, CORRODED. REMOVED AND REPLACED FAILSAFE AT BS 794, RBL 19, IAW B737-400 SRM 51-40-02. (M)

Part: CREASE BEAM — CORRODED (FS 540-663)

PAE - FOUND CORROSION ON CREASE BEAM AT BS 601, LBL 64, WL 208. REMOVED AND REPLACED CREASE BEAM AT BS 540 TO 663, LBL 64, WL 208, PER B737-400 SRM 53-60-13 PAGE 106, DETAIL 5, SRM 53-60-13, PAGE 2, DETAIL 1. (M)

Part: CREASE BEAM — CORRODED (BS 639)

PAE - FOUND CORROSION ON CREASE BEAM AT BS 639, RBL 64, WL 208. REMOVED AND REPLACED CREASE BEAM AT BS 540 TO 663, RBL 64, WL 208, PER B737-400 SRM 51-40-02 PAGE 1-2, STEP 4, SRM 51-10-02 SRM 53-60-13. (M)

Part: STRUCTURE — CORRODED (BS 270)

CORROSION ON STRUCTURE AT BS 270, WL 208, RBL 8. REMOVED, REPLACED, AND FABRICATED NEW STRUCTURE IAW SRM. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION ON FWD CARGO BAY AT BSTA 500B BETWEEN STR 28L AND 28R SHEAR TIE CORROSION AT LWR FWD SURFACE. REPAIRED FRAME AT BSTA 500B BETWEEN STRINGERS 28L AND 28R IAW SRM. (K)

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2

SUB THRESHOLD ANGLE CORRODED AT BSTA 795, RBL 19-23. REMOVED AND REPLACED SUB THRESHOLD ANGLE AT BSTA 795, RBL 19-23 IAW SRM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON FLOORBEAM UPPER CHORD. REPAIRED FLOORBEAM IAW SRM. (K)

Part: FRAME — CORRODED (FUSELAGE)

FWD CARGO BAY STA 500D BETWEEN STRINGERS 28L AND 28R SHEAR TIE CORRODED. REPAIRED FWD CARGO BAY STA 500D FRAME BETWEEN STR 28L AND 28R SHEAR TIE. (K)

Part: FRAME — CORRODED (FUSELAGE)

CORROSION ON FWD CARGO BAY AT BSTA 500C BETWEEN STR 28L AND 28R AND STR 28R SHEAR TIE HAS CORROSION AT LWR FASTENER TO SKIN. REPAIRED FRAME AT BSTA 500C BETWEEN STRINGERS 28L AND 28R IAW SRM. (K)

Part: FITTING — CORRODED (FUSELAGE)

FWD LAV AFT WALL IB TIE DOWN FITTING CORRODED. REMOVED AND REPLACED FWD LAV AFT WALL IB TIE DOWN FITTING IAW SRM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON FLOORBEAM UPPER STRUCTUREAT BS 312, WL 208, LBL 11. REMOVED AND REPLACED STRUCTURE IAW SRM AND EA. (K)

Part: SKIN — DENTED (CARGO DOOR)

AFT CARGO DOOR EXTERNAL SKIN DENTED AND GOUGED. REPLACED SKIN IAW SRM. (K)

Part: SKIN — DENTED (CARGO DOOR)

AFT CARGO DOOR EXTERNAL SKIN DENTED AND GOUGED. REPLACED SKIN IAW SRM. (K)

Part: SKIN — DENTED (CARGO DOOR)

PAE - AFT CARGO DOOR EXTERNAL SKIN DENTED AND GOUGED. REPLACED SKIN PER B737-400 SRM 52-30-01. (M)

Part: FRAME — CRACKED (FUSELAGE)

FRAME CRACKED AT BIN RAIL. REPAIRED FRAME IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE)

FRAME CRACKED AT BIN RAIL ATTACH POINT. REMOVED DAMAGE, FABRICATED AND REPAIRED FRAME IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE)

FRAME CRACKED AT BIN RAIL SUPPORT. REPAIRED FRAME AT BIN RAIL LOCATION IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE)

FRAME CRACKED AT BIN RAIL. REPAIRED FRAME AT BIN RAIL LOCATION IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE)

FRAME CRACKED AT BIN RAIL ATTACH POINT. INSTALLED FRAME REPAIR DOUBLER ON BSTA 480 FRAME RT AT BIN RAIL LOCATION IAW SRM. (K)

Part: DOUBLER — CORRODED (FUSELAGE)

CORROSION ON DOUBLER, BLENDED OUT OF LIMITS, FABRICATED NEW DOUBLER AND INSTALLED IAW ENGINEERING DWG. (K)

Part: FRAME — CRACKED (FUSELAGE)

PAE- FRAME CRACKED AT BIN RAIL ATTACH POINT. REPAIRED CRACKED FRAME IAW SRM. (K)

Part: ATTACH FITTING — CRACKED (FS 400)

PAE - FOUND FRAME CRACKED AT BIN RAIL ATTACH POINT. REPAIRED CRACKED FRAME IAW B737-400 SRM 53-00-07. (M)

Part: FLOOR SUPPORT — CORRODED (CARGO BAY FLOOR)

PAE-FWD CARGO BAY FLOOR SUPPORT CORRODED. CUT OUT DAMAGED FLOOR SUPPORT, FABRICATED AND INSTALLED REPAIR IAW SRM. (K)

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2

PAE: CORROSION ON TORQUE BOX STIFFENER. REMOVED AND REPLACED STIFFENER IAW SRM. (K)

Part: STIFFENER — CORRODED (FUSELAGE)

PAE: CORROSION ON TORQUE BOX STIFFENER. REMOVED AND REPLACED STIFFENER IAW SRM. (K)

Part: STRINGER — CORRODED (FUSELAGE)

PAE: CORROSION ON STRINGER END FITTING. REMOVED AND REPLACED FITTING IAW SRM. (K)

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2

PAE: CORROSION ON TORQUE BOX STIFFENER. REMOVED AND REPLACED STIFFENER IAW SRM. (K)

Part: WEB — TOOL DAMAGE (FUSELAGE)

PAE: GOUGE IN WEB AT BSTA 1016, BL0, WL 208. BLENDED OUT GOUGE IN WEB AT BSTA 1016, WL 208, BL0. AREA REMOVED 1.5 INCH X 3.0. 100 INCH MATERIAL REMOVED, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WEB AT BSTA 1016, BL 0 WL 208 IAW SRM. (K)

Part: WEB — TOOL DAMAGE (FUSELAGE)

PAE: RT SHEAR WEB AT BSTA 1016 BL 0, DAMAGED BELOW OVERLAP OF LT SHEAR WEB. FOUND PUNCTURE DAMAGE TO BE OUT OF LIMITS AT BSTA 1016, WL 208, RT SHEAR WEB. REMOVED AND REPLACED RT SHEAR WEB THROUGHOUT BS1016-1026, RBL 0-29 IAW SRM. (K)

Part: FRAME — CRACKED (FUSELAGE)

PAE-FRAME CRACKED AT BIN RAIL. REPAIRED FRAME AT BSTA 907RH BIN RAIL ATTACH POINT. (K)

Part: FRAME — GOUGED (FUSELAGE)

PAE- FRAME CRACKED AT BIN RAIL ATTACH POINT. INSTALLED FRAME REPAIR DOUBLER ON BSTA 480 FRAME RT AT BIN RAIL LOCATION. (K)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE-CORROSION ON SHEAR TIE BSTA 1006, STR 27LT TO 27 RT. REMOVED AND REPLACED SHEAR TIE IAW SRM. (K)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

PAE: CORROSION ON INTERCOSTAL AT BSTA 771, RBL 19, WI 156. REMOVED AND REPLACED INTERCOSTAL IAW SRM. (K)

Part: SILL — CORRODED (BS 270-360) · corrosion level 2

PAE-CORROSION AT R-1 DOORWAY MOPSILL FROM BSTA 270-360. REMOVED AND REPLACED R-1 DOOR MOPSILL IAW SRM. (K)

Part: FRAME — GOUGED (FUSELAGE)

PAE: RT FRAME WEB GOUGED. INSTALLED REPAIR IAW SRM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE: CORROSION ON FLOORBEAM. BLENDED CORROSION, FABRICATED REPAIR STRAP AND INSTALLED IAW SRM. (K)

Part: SKIN — CRACKED (DOOR)

PAE: L-1 DOOR INNER SKIN CRACKED ON FWD EDGE. REPAIRED IAW SRM. (K)

Part: GUIDE ARM — OUT OF ADJUST (PAX DOOR)

SEA - MAIN PASSENGER DOOR (L-1) IS VERY DIFFICULT TO CLOSE. REPLACED MAIN ENTRY DOOR GUIDE ARM ROD END AND ADJUSTED IAW AMM. (K)

Part: SKIN — CRACKED (HORIZ STAB) · airframe 36,403 hrs · 20,507 cycles

RT HORIZONTAL STABILIZER, LOWER SKIN CRACKED 2 INCHES FWD OF BREAK SPAR. REPAIRED CRACK IAW EA.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,402 hrs · 20,505 cycles

LT WING LOWER EXTERIOR SKIN IS DENTED. REPLACED LOWER EXTERNAL SKIN IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE)

JNU - DURING WINDSHIELD CHANGE DISCOVERED .75 INCH CRACK IN WINDSHIELD CUT OUT UPPER LEFT CORNER. REPAIRED IAW SRM. (M)

Part: PANEL — CORRODED (FUSELAGE)

GYR - DURING C-CHECK FOUND CORROSION AT ELECTRICAL DISCONNECT PANEL. REPAIRED IAW EA. (M)

Part: WIRE — BROKEN (CABIN)

DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE FROM FORWARD GALLEY TO ROW 2. REPAIRED BROKEN WIRES, REPLACED LIGHT SECTION, OPS CHECKED NORMAL RELEASED FOR SERVICE (M)

Part: SPAR — CRACKED (RT WING LE)

DURING C CHECK FOUND RT LEADING EDGE INBOARD OF NR 2 ENGINE HAS 2 INCH CRACK ON PRIMARY STRUCTURE. REPAIRED CRACK PER EA.

Part: RUB STRIP — CRACKED (FUSELAGE)

DURING C CHECK, FOUND PANEL 6301 RUB STRIP CRACKED. REMOVED AND REPLACED RUB STRIP.

Part: STRUCTURE — CRACKED (CARGO DOOR)

DURING C CHECK FOUND FORWARD CARGO DOOR CRACKED AT FASTENER HOLE ON LOWER AFT FRAME. REPAIRED IAW SRM.

Part: FRAME — CRACKED (CARGO DOOR)

DURING C CHECK FOUND FORWARD CARGO DOOR CRACKED AT FASTENER HOLE ON LOWER CENTER FRAME. REMOVED AND REPLACED LOWER CENTER FRAME.

Part: DOOR FRAME — CRACKED (CARGO BAY)

DURING C CHECK FOUND FORWARD CARGO DOOR FRAME CRACKED. REPAIRED IAW EA.

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 6-12. WIRE DISCONNECTED. RECONNECTED WIRE, OPS CHECK GOOD. (M)

Part: WIRE — DAMAGED (CABIN)

SEA - DURING RON CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 1-3. REPAIRED WIRE, OPS NORMAL. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FLOORBEAM SUPPORT ANGLE AT BS 328 TO 338, RBL 63, AND WL 208 CORRODED. REPAIRED IAW SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON THE L ANGLE LOWER SILL SUPPORT OF THE GALLEY DOOR AT BS 328 TO 338, WL 208, AND BUTT LINE 65 RT. REPAIRED IAW SRM. (M)

Part: SKIN — DENTED (FUSELAGE)

PAE - DURING SI CHECK, FOUND SKIN DENTED AT BS 843, WL 175, AND STRINGER 21 RT. REPAIRED IAW EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 486.5, WL 208 AND BUTT LINE 13.5 TO 19.5. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON UPPER CHOD OF 947 FLOORBEAM AT BS 947, WL 208, AND LBL 15 TO RBL 15. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CHORD CRACKED .25 INCH LONG AT BS 178, WL 207, AND BUTT LINE 25 LEFT AND RIGHT SIDES. REPAIRED IAW EA. (M)

Part: SKIN — DENTED (FUSELAGE)

PAE - DURING SI CHECK, FOUND SKIN DENTED AT BS 843, WL 175, AND STRINGER 21 RIGHT. (M)

Part: THRESHOLD — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION OF SUB THRESHOLD WEB AT STATION 795-847 AND RBL 20-28 AND WL 160. REMOVED AND REPLACED SUB THRESHOLD IAW SRM. (M)

Part: THRESHOLD — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION OF SUB THRESHOLD WEB AT STATION 787-794 AND RBL 20 AND WL 157. REMOVED AND REPLACED SUB THRESHOLD IAW SRM. (M)

Part: SKIN — WORN (RAM AIR DOOR)

SEA-DURING C CHECK FOUND RT RAM AIR INLET DUCT LOWER WEB SKINS AT STATION 530 TO 540 HAVE WEAR AREA'S FROM DOOR MOVEMENT. REPAIRED IN ACCORDANACE WITH EA 5320-01440.

Part: SKIN — WORN (WING)

SEA - DURING C-CHECK INSPECTION, FOUND WEAR DAMAGE ON THE INNER SURFACE OF WING LOWER SKIN AT THE FUEL BOOST PUMP ACCESS PANEL CUTOUT LOCATED AT APPROX WBL 151.0 AND S-7. REPAIRED IAW EA 5720-01187. (M)

Part: SKIN — WORN (WING)

SEA - DURING C-CHECK INSPECTION, FOUND WEAR DAMAGE ON INNER SURFACE IF WING SKIN AT THE INBOARD FUEL BOOST PUMP ACCESS PANEL CUTOUT LOCATED AT APPROXIMATELY WL 120 AND S-7. REPAIRED IAW ASA EA 5720-01189. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY/HARNESS AND LIGHTS OPERATED NORMALLY. (M)

Part: DOOR — LACK OF LUBE (FUSELAGE)

PDX - PRIOR TO FLIGHT 419, THE L1 DOOR WAS FOUND TO BE HARD TO CLOSE. LUBRICATED DOOR AND DOOR OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

JNU - DURING MAINTENANCE CHECK, ONE SECTION OF THE EMERGENCY EXIT FLOOR TRACK LIGHTS AISLE LOCATION L2 AND R2 DOOR EXIT WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE L2 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED POWER SUPPLY AND LIGHT OPERATED NORMALLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

SEA - FLT 75 - PRIOR TO FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 15 THROUGH 18. TIGHTENED LOOSE CONNECTION AND LIGHTS OPERATED NORMALLY. (X)

Part: SNAP RING — MISSING (L1 DOOR)

SEA - FLT 95 - CREW REPORTED, L1 FORWARD ENTRY DOOR HARD TO OPEN. FOUND MISSING SNAP RING ON L1 FORWARD ENTRY DOOR UPPER HINGE. REINSTALLED SNAP RING AND DOOR OPERATED NORMALLY. (M)

Part: PIN — MISINSTALLED (L1 DOOR)

PHX - FLT 794 - AT GATE THE L1 FORWARD ENTRY DOOR JAMMED IN THE PARTIALLY OPEN POSITION. FOUND UPPER HINGE LOWER PIVOT PIN RECESSED. PROPERLY INSTALLED PIN AND DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14 THROUGH 17. RECONNECTED WIRES AND LIGHTS OPERATED NORMALLY. (M)

Part: ROLLER — OUT OF ADJUST (R1 DOOR)

PDX - FLT NR 437 - CREW REPORTS, THAT THE R-1 DOOR HANDLE POPS UP FROM THE CLOSE POSITION. FOUND FORWARD LOWER ROLLER OUT OF RIG TOLERANCE. RE-RIGGED PER MM AND HANDLE OPERATED NORMALLY. (M)

Part: LIGHT SW — INOPERATIVE (AFT F/A STA)

SEA - FLT 103 - EMERGENCY EXIT LIGHTS WILL NOT TURN ON FROM AFT EMERGENCY LIGHT SWITCH. LIGHTS FAILED FROM AFT F/A STA WITH FLIGHT DECK SWITCH IN 'ARM' . CYCLED BOTH SWITCHES TO OFF AND BACK ON, EMERGENCY EXIT LIGHTS OPERATED NORMALLY IN ALL SWITCH POSITIONS. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 20-25 WERE FOUND INOPERATIVE. RECONNECTED WIRING ON AFT TRACK AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROWS 22 TO 26. MAINTENANCE SECURED LOOSE CONNECTION AT ROW 26. (W)