N775AS

Part: SKIN — DENTED (TE FLAP) · airframe 51,605 hrs · 29,055 cycles

LEFT I/B FLAP HAS DENT LOCATED 29 INCHES FROM I/B END 7 INCHES FROM TOP ON TOP OF SKIN. PREPPED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED REPAIR DOUBLER 29 INCHES FROM I/B EDGE 7 INCHES FROM TOP ON UPPER SKIN IAW ASA EA 400 57EA 00702.

Part: COTTER PIN — MISSING (R1 DOOR) · airframe 49,979 hrs · 28,139 cycles

R1 DOOR WILL NOT CLOSE FOUND LOWER AFT DOOR LATCH BEARING MISSING COTTER PIN AND NUT BACKING OFF. SECURED LOOSE NUT AND INSTALLED COTTER PIN OPS CHECK GOOD REF MM 52 41 00.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 45,331 hrs · 25,469 cycles

VERTICAL STABLIZER AT REAR SPAR AREA PANEL ATTACH ANGLE CRACKED AT APPROX FIN STA 140. VERTICAL STABLIZER REAR SPAR TO SKIN PANEL ATTACH ANGLE AT FIN STATION 140 REPLACED IAW SRM 51-40-02.

Part: SKIN — CHAFED (NR 2 SLAT) · airframe 45,331 hrs · 25,469 cycles

SLAT NR 2 OUTBOARD UPPER TRAILING EDGE PREVIOUS REPAIR IS DAMAGED. NR 2 SLAT REPAIRED CORE AND DOUBLER IAW SRM 51-70-10.

Part: SKIN — CHAFED (RT TE FLAP) · airframe 45,331 hrs · 25,469 cycles

RIGHT OUTBOARD MID FLAP INBOARD SIDE LWR SURFACE OF LEADING EDGE HAS CHAFING DAMAGE. REPAIRED OUTBOARD MID FLAP LEADING EDGE IAW SRM 57-53-01 FIG 201.

Part: FRAME — CORRODED (BS 794 S19-27R) · corrosion level 2 · airframe 45,331 hrs · 25,469 cycles

AFT CARGO DOORWAY FWD FRAME WEB CORRODED 3 INCHES ABOVE STR 25R BS 794.3. REPAIRED WITH FABRICATED REPAIR PART IAW SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (BS 787-794 S25R) · airframe 45,331 hrs · 25,469 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED. INTERCOSTAL REPAIRED IAW SRM 51-40-05 AND 51-40-02.

Part: SPAR — DELAMINATED (LT AILERON) · 25,469 cycles

THE LEFT WING AILERON REAR SPAR IS DELAMINATED AT THE INBOARD END. LEFT WING AILERON REAR SPAR DELAMINATION REPAIRED IAW SRM 51-70-04 AND ERO 6448 AND EA 2710 01106.

Part: SKIN — DENTED (LT SPOILER) · airframe 45,331 hrs · 25,469 cycles

THE LEFT SPOILER NR 3 HAS UPPER SURFACE IRREGULARITY (DENT) NR 3 LT WING SPOILER REPAIRED IAW SRM 57-70-01.

Part: DOUBLER — DAMAGED (L/E SLAT) · airframe 45,331 hrs · 25,469 cycles

SLAT NR 2 O/B UPPER TRAILING EDGE PREVIOUS REPAIR IS DAMAGED. REPAIRED NR 2 SLAT CORE AND DOUBLER IAW SRM 51-70-10.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 45,331 hrs · 25,469 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED. REPAIRED INTERCOSTAL IAW SRM 51-40-02.

Part: SKIN — CHAFED (T/E FLAP) · airframe 45,331 hrs · 25,469 cycles

RIGHT OUTBOARD MID FLAP INBOARD SIDE LWR SURFACE OF L/E HAS CHAFING DAMAGE. REPAIRED OUTBOARD MID FLAP L/E IAW SRM 57-53-01 FIG 201.

Part: SKIN — DENTED (BS 380-400) · airframe 44,454 hrs · 24,972 cycles

DENTS IN RIGHT FUSELAGE APPROX 62.5 INCHES AFT OF R1 DOOR AND 6 INCHES BELOW LAP SEAM. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01.

Part: CAM — GOUGED (L-1 DOOR) · airframe 42,722 hrs · 24,039 cycles

L1 DOOR HARD TO CLOSE AND GOUGE ON FWD LWR TORQUE TUBE ROLLER FITTING. REMOVED AND REPLACED 1 DOOR PER AMM 52-11-00 AND ACCOMPLISHED TEST PER AMM 52-11-00 PG 517 AND 518.

Part: DOOR FRAME — TORN

FWD CARGO DOOR OPENING DAMAGED ON FWD SIDE BY GROUND EQUIPMENT. INSTALLED REPAIR IAW SRM. (K)

Part: RIB — CRACKED (RT WING)

YXX - RIGHT WING FUEL TANK RIB AT WBL 135.5 CRACKED AT STRINGER 52. REPAIRED IAW ERO 5013, AND EA 5720-01283. (M)

Part: FLOORBEAM — CORRODED (FS 986.5)

YXX - FOUND CORROSION ON FLOORBEAM AT BS 986.5 AT CLIP NUTS. REPAIRED FLOORBEAM IAW ASA EA 5310-02525. (M)

Part: FLOORBEAM — CORRODED (FS 947)

YXX - FOUND FLOORBEAM AT BS 947.5 CORRODED FROM LBL 14 TO RBL 14. REPAIRED FLOORBEAM IAW ASA EA 5310-0257. (M)

Part: FLOORBEAM — CORRODED (BS 986)

YXX - FOUND FLOORBEAM AT BS 986.5 CORRODED AT CLIP NUT HOLES ALONG TOP SURFACE. REPAIRED FLOORBEAM IAW ASA EA 5310-02525 AND ERO 4999. (M0

Part: SILL — CORRODED (FS 360)

YXX - FOUND L1 DOOR SILL CHORD CORRODED. REPLACED SILL CHORD IAW B737-400 SRM 51-40-02. (M)

Part: ACCESS DOOR — CRACKED (FS 328-344)

YXX - E/E COMPARTMENT ACCESS DOOR OUTER SURFACE IS DENTED/CRACKED. OUTER SURFACED REPAIRED IAW B737-400 SRM 52-00-01 FIG 201. (M)

Part: ATTACH ANGLE — CRACKED (FS 291.5)

PAE - FOUND FORWARD OF R1 DOOR FRAME AT BS 291.5 ABOVE STRINGER 13 RT SKIN ATTACH ANGLE TO INTERCOSTAL CRACKED. FABRICATED REPAIR PART INSTALLED AT FORWARD OF R-1 DOOR FRAME AT BS 291.5 ABOVE STRINGER 13 RT SKIN ATTACH ANGLE TO INTERCOSTAL. (M)

Part: FRAME — CRACKED (FS 360 S8L)

YXX - FOUND CRACKED FRAME AT BS 360, STRINGER 8 LEFT. REPAIRED FRAME IAW B737-400 SRM 53-00-07 FIG 201. (M)

Part: DOOR FRAME — CRACKED (FS 291.5)

YXX - FOUND FORWARD OF R1 DOOR FRAME AT BS 29.1 ABOVE STRINGER 10 RT SKIN ATTACH ANGLE TO INTERCOSTAL IS CRACKED. REPLACED ATTACH ANGLE IAW B737-400 SRM 51-40-02. (M)

Part: HINGE — CHAFED (FS 450-480)

YXX - FOUND FORWARD CARGO DOOR WEB ABOVE HINGE ARMS CHAFED. REPAIRED WEB IAW B737-400 SRM 51-70-13. (M)

Part: WEB — CRACKED (FS 303.9)

YXX - FOUND CRACKED WEB AT BS 303.9, STRINGER 16 LEFT. REPAIRED IAW ERO NR 5039 AND ASA EA 5310-02523. (M)

Part: STRINGER — CORRODED (BS 1123)

YXX - APU COMPARTMENT RIGHT TORQUE BOX STRINGER AT BS 1126 IS CORRODED. REPLACED STRINGER IAW B737-400 SRM 51-40-02. (M)

Part: WEB — CRACKED (FUSELAGE)

YXX-SB, WEB MOD AT BSTA 360, STR 16 LT, TO BE COMPLIED WITH. SB ACCOMPLISHED IAW EO. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

YXX - FLOORBEAM AT BSTA 344, BL 0, TO LBL 65 CORRODED AT ANCHOR NUT HOLES. REPAIRED IAW SRM. (K)

Part: BRACKET — CRACKED (DOOR)

YXX - R-1 DOOR INTERIOR, AT AFT BOTTOM CORNER, PLATE CRACKED THROUGH AT FASTENER HOLES. REPAIRED BY INSTALLING REPAIR PARTS IAW SRM. (K)

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

YXX - CORROSION ON TOP SURFACE OF FLOORBEAM AT BSTA 294.5, LBL 12 TO RBL 12. FLOOR BEAM UPPER CHORD REPAIRED BY SPLICE IAW SRM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

YXX - FOUND CORROSION ON FLOORBEAM AT BS 312, LBL 12-50. DAMAGED SECTION OF FLOORBEAM REPLACED PER B737-400 SRM 53-10-51 FIG 201. (M)

Part: GUIDE ARM — OUT OF RIG (R1 DOOR)

SEA - RIGHT FORWARD SERVICE DOOR R-1 WILL NOT CLOSE. DOOR GUIDE ARM AND HORIZONTAL ROD WERE FOUND OUT OF RIG. RIGGED DOOR PER AMM 53-41-00. ACCOMPLISHED DOOR LUBE. DOOR NOW OPENS AND CLOSES NORMALLY. (M)

Part: SKIN — DEBONDED (TE FLAP)

OKC - FOUND RIGHT WING INBOARD AFT FLAP LOWER SKIN AT PREVIOUS REPAIR IS DISBONDED ON FORWARD END AT SECOND TRACK. REMOVED DISBONDED AREA, REPAIRED AREA WITH FIBERGLASS OVERLAY VIA HOTBOND IAW 737-400 SRM 51-70-06 PARAGRAPH 3A. (M)

Part: WEDGE — DEBONDED (NR 2 SLAT)

OKC - FOUND NR 2 SLAT T/E WEDGE PREVIOUSLY INSTALLED REPAIR IS DISBONDED AT AFT OUTBOARD CORNER. PREPARED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR DOUBLER AND BONDED, IAW 737-400 SRM 51-70-10 REPAIR 8. (M)

Part: SKIN — DELAMINATED (FORE FLAP)

OKC - FOUND RIGHT INBOARD FORE FLAP UPPER SKIN IS DELAMINATED 60 INCHES FROM INBOARD END AND 8 INCHES FROM T/E. REMOVED DAMAGED AREA, FABRICATED SKIN FILLER AND DOUBLERS AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10 REPAIR 21. (M)

Part: SKIN — DENTED (TE FLAPS)

OKC - FOUND LEFT INBOARD FORE FLAP HAS 2 EACH GROUPS OF DENTS ON LOWER SURFACE. FILLED DENTS, FABRICATED AND INSTALLED SKIN DOUBLERS IAW 737-400 SRM 51-70-10 REPAIR 2. (M)

Part: SKIN — DAMAGED (HORIZONTAL STAB)

OKC - FOUND LEFT HORIZONTAL STAB LEADING EDGE STAB STATION 131.54 HAS NUMEROUS CREASES. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW 737-400 SRM 55-10-01 FIGURE 203. (M)

Part: SKIN — DELAMINATED (TE FLAP)

OKC - FOUND RIGHT INBOARD FORE FLAP UPPER IS DELAMINATED 34 INCHES FROM OUTBOARD END AND 8 INCHES FROM T/E. REMOVED DAMAGED AREA, FABRICATED SKIN FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10 REPAIR 21. (M)

Part: SKIN — DENTED (HORIZONTAL STAB)

OKC - FOUND SPEED TAPE INSTALLED AT THE L/E IN THE RIGHT HORIZONTAL STABILIZER. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR DOUBLER AND FILLER IAW 737-400 SRM 55-10-01 FIG 203. (M)

Part: FRAME — CORRODED (FS 807)

OKC - FRAME 807 FORWARD FACE CORRODED BETWEEN STRINGERS 27L AND 27R. REMOVED DAMAGED SHEAR TIES. FABRICATED AND INSTALLED REPAIR PIECES IAW 737-400 SRM 53-00-07 FIGURE 210. (M)

Part: SKIN — DAMAGED (HORIZONTAL STAB)

OKC - FOUND LEFT HORIZONTAL STAB L/E STAB STATION 192.54 HAS 2 EACH CREASES. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW 737-400 SRM 55-10-01 FIGURE 203. (M)

Part: SKIN — DENTED (TE FLAP)

OKC - FOUND RIGHT INBOARD FORE HAS A DENT ON THE LOWER SIDE ABOVE INBOARD TRACK. PREPARED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR DOUBLER AND BONDED, IAW 737-400 SRM 51-70-30 REPAIR 2. (M)

Part: SKIN — DENTED (TE FLAP)

OKC - FOUND RIGHT INBOARD FLAP LOWER SKIN IS DENTED AND DELAMINATED JUST OUTBOARD OF CENTER TRACK. REMOVED DAMAGED AREA, FABRICATED SKIN FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10 REPAIR 21. (M)

Part: SKIN — DENTED (FS 370)

OKC - FOUND DENT IN FUSELAGE EXTERIOR SKIN AT BS 370 BELOW STRINGER 17L. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED DOUBLER IAW 737-400 SRM 53-00-01 FIG 23L. (M)

Part: ANGLE — CORRODED (FUSELAGE)

OAK - AFT CARGO COMP RIGHT 'Z' ANGLE CORRODED STATION 727D TO 727G. REMOVED AND REPLACED Z-ANGLE RT STATION 727D TO 727G. (M)

Part: SKIN — GOUGED (FUSELAGE)

OAK - DURING MAINTENANCE IN SEA, A GOUGE WAS NOTED ON FUSELAGE SKIN BS 1029 S-16L. GOUGE WAS BLENDED SMOOTH. MEASUREMENT 1 INCH BY 1 INCH BY .021 INCH DEEP. INSTALLED NEW REPAIR DOUBLER AND FILLER RED SRM 53-80-01 PAGE 206-211. (M)

Part: ANGLE — CORRODED (FS)

OAK - FOUND AFT CARGO COMPARTMENT RIGHT Z-ANGLE CORRODED STATION 727D TO 747. REMOVED AND REPLACED Z-ANGLE RT STATION 727D TO 747. (M)

Part: LIGHT — DISCONNECTED (CABIN)

ANC - FOUND FORWARD GALLEY ENTRANCE RED FLOOR TRACK LIGHT UNPLUGGED. REINSTALLED FORWARD GALLEY RED FLOOR TRACK LIGHT, OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - FOUND FIRST TWO ROWS OF EMERGENCY LIGHTS INOPERATIVE. RELAMPED AND SECURED LOOSE WIRES AND INSTALLED MISSING COVER AT SEAT ROW 1AC. (M)

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 13 INOPERATIVE. REPAIRED WIRE AND OPERATIONAL CHECKED GOOD. (M)

Part: STRUCTURE — CHAFED (RT WING)

DURING C-CHECK, FOUND RIGHT WING INBOARD EXHAUST FATE UPPER SURFACE CHAFED AT OUTBOARD FORWARD EDGE. REPAIRED IAW SRM. (M)

Part: SKIN — GOUGED (FUSELAGE)

DURING C-CHECK, FOUND FUSELAGE EXTERIOR SKIN IS GOUGED AT BS 919-928. REPAIRED IAW SRM. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND LEFT KEELBEAM IS CORRODED AT FUSELAGE DRAIN. REPAIRED IAW SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORRODED FRAME AT BS 500. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND FLOOR SUPPORT STRAP IS CORRODED AT BS 792. REPAIRED IAW SRM. (M)

Part: WEB — GOUGED (FUSELAGE)

DURING C-CHECK, FOUND AFT CARGO DOOR CUTOUT FORWARD LOWER CLOSE OUT WEB GOUGED. REPAIRED IAW SRM. (M)

Part: SUPPORT BRACKET — WORN (RT WING)

DURING C-CHECK, FOUND RT WING TRAILING EDGE LOWER SURFACE PANEL SUPPORT BRACKET WORN AT NR 5 SPOILER OUTBOARD ACTUATOR. REPAIRED IAW SRM. (M)

Part: SKIN — DENTED (HORIZONTAL STAB)

DURING C-CHECK, FOUND LEFT HORIZONTAL STAB LE HAS DENT AT 91 IN OUTBOARD FROM REMOVEABLE LE SKIN INBOARD END. REPAIRED IAW SRM. (M)

Part: THRESHOLD — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND AFT CARGO DOOR CUTOUT THRESHOLD WEB IS CORRODED. REPAIRED IAW SRM. (M)

Part: SKIN — CHAFED (FUSELAGE)

DURING C-CHECK, FOUND SKIN HAS AREAS OF CHAFING DAMAGE AT THE LEFT AFT LOWER SLIDE SEAL AT BS 1154. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT FROM BS 727E PLUS 14, 835 IS CORRODED. REPAIRED IAW SRM. (M)

Part: SKIN — CHAFED (FUSELAGE)

DURING C-CHECK, FOUND EMPENNAGE SKIN HAS CHAFING DAMAGE AT RIGHT LOWER AFT HORIZONTAL STAB SEAL. REPAIRED IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

DURING C-CHECK FOUND FLOOR SUPPORT WEB IS CORRODED FROM BS 814-847. REPAIRED IAW SRM. (M)

Part: FRAME — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORRODED FRAME AT BS 500B. REPAIRED IAW SRM. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND STRINGER CLIP CORRODED AT BS 787. REPAIRED IAW SRM. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING LINE CHECK, FOUND RED FLOOR TRACK LIGHTS NEAR ROW 1 INOPERATIVE. REMOVED AND REPLACE TRACK LIGHT ASSEMBLY. OPS CHECKED NORMAL. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEA - DURING LINE CHECK, FOUND OVERHEAD BIN EMERGENCY LIGHT AT ROW 16 RIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY, OPERATIONAL CHECKS NORMAL. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - BEFORE FLIGHT, FOUND FLOOR TRACK LIGHTING IN MID CABIN INOPERATIVE. RECONNECTED WIRING, OPERATIONAL CHECK NORMAL. (M)

Part: PANEL — CRACKED (SLAT)

PAE - DURING C-CHECK INSPECTION, FOUND SLAT ACCESS PANEL NR 6516 CORNER CRACKED. REPAIRED IAW ASA EA 5740-01231. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING C-CHECK INSPECTION WHILE PERFORMING AN EDDY CURRENT EXAMINATION, FOUND CRACK AT LEFT SIDE CHORD AT BS 178 BELOW THE FLOOR FROM WATERLINE 202 TO 207 AND BUTTLINE 4.7. REPAIRED IAW ASA EA 5310-01883. (M)

Part: CLIP — GOUGED (THRUST REVERSER)

PAE - DURING SI CHECK, FOUND THRUST REVERSER BLOCKER DOOR ANTI-ROTATION CLIPS HAVE GOUGED THE C-DUCT BULL NOSE BEYOND MFG LIMITS. REPAIRED IAW EA5430-01084. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 986, WL 208, LBL 65 - RBL 65 IS CORRODED AROUND NUTPLATE. REPAIRED IAW EA 5310-01885. (M)

Part: FITTING — GOUGED (AILERON)

PAE - DURING SI CHECK, FOUND LEFT AILERON INBOARD HINGE FITTING A/C SIDE WAS GOUGED ON INBOARD LUG OUTBOARD SIDE. REPAIRED IAW ASA EA5750-01491. (M)

Part: NUT — LOOSE (MLG STRUT)

DURING ROUTINE C-CHECK INSPECTION, FOUND LEFT MAIN LANDING GEAR LOWER SIDE STRUT LOWER ATTACH POINT HAD A .250 INCH GAP BETWEEN NUT AND STRUT AND NUT HAD NO LOCKING FEATURE. IPC 32-30-00-03A FIG NR A ITEM 40. (X)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING SI CHECK, FOUND RIGHT AND LEFT SIDE CHORDS AT BODY STATION 178, WATERLINE 2.6.5 TO 208 ARE CRACKED. BULKHEAD WEB IS ALSO CRACKED AT WATER LINE 201.5 TO 202, RBL 4.7 FUSELAGE 154, CRACK IN WEB, FUSELAGE 155 RIGHT CHORD, FUSELAGE 156 LEFT CHORD. SIDE CHORD CRACKS ARE 1.5 INCHES LONG AND WEB CRACK IS .5 INCHES LONG. REPAIRED IAW ASA EA 53-10-01883. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 12-16. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, SIX EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: DOOR — OUT OF ADJUST (FUSELAGE)

OAK - PRIOR TO FLIGHT 340, THE R2 DOOR INNER HANDLE WAS REPORTED TO SEEM LOOSE, NOT ALLOWING THE DOOR TO CLOSE TIGHTLY. MAINTENANCE ADJUSTED DOOR AND THE DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD 2 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING/LIGHTS AND THE LIGHTS OPERATED NORMALLY. (X)

Part: CLIP — MISSING (PAX DOOR)

SNA - UPON ARRIVAL OF FLT 486, THE L1 DOOR COULD NOT BE OPENED. CONTRACT MAINTENANCE REPLACED MISSING C-CLIP ON THE UPPER ARM ASSEMBLY AND THE DOOR OPERATED NORMALLY. (M)

Part: CLIP — MISSING (L1 DOOR)

OAK - PRIOR TO FLIGHT 493 - THE L-1 DOOR WAS FOUND TO BE DIFFICULT TO OPEN. FOUND RETAINER CLIP MISSING FROM PIN ON THE UPPER HINGE CAUSING INTERFERENCE. REPLACED MISSING RETAINER CLIP AND DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SNA - FLT 445 - PRIOR TO FLIGHT, THE AFT SIX EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPAIRED WIRE CONNECTION AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14 TO 17 WERE FOUND INOPERATIVE. RECONNECTED WIRING HARNESS AND LIGHTS OPERATED NORMALLY. (W)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 6 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LIGHTS AND REPLACED AFT BATTERY PACK. LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ANC - DURING MAINTENANCE CHECK, THE FIRST EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND INOPERATIVE. REPLACED FORWARD LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL FUSE — BLOWN (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT SIX EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED FUSE IN BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL PICO FUSE — BLOWN (CABIN)

JNU - DURING MAINTENANCE CHECK, SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN MAIN CABIN. REPLACED PICO FUSE IN BATTERY POWER SUPPLY AND ALL LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS FROM ROW 22 AND AFT WERE FOUND INOPERATIVE. RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — LOOSE (CABIN)

SEA - AT CHECK, EMERGENCY FLOOR LIGHTS INOP AT ROW 26 AFT. MAINTENANCE SECURED LOOSE CONNECTION IN WIRING. (W)

Part: TIRE — FAILED (LT MLG)

SEA - FLT 67 - ON DEPARTURE, THE NR 1 MLG TIRE TREAD SEPARATED FROM ITS CASING CAUSING DAMAGED TO THE LT GEAR DOORS, LT I/B MID-FLAP, LT I/B TRAILING EDGE FLAP, LT LOWER WING SKIN, LT I/B THRUST REVERSER COWLING AND THE LT HORIZONTAL STABILIZER. MAINTENANCE REPLACED NR 1 MLG WHEEL ASSEMBLY AND REPLACED OR REPAIRED CONSEQUENTIAL DAMAGE AS REQUIRED. THE NR 2 MLG WHEEL ASSEMBLY WAS REPLACED AS A PRECAUTION. (W)