N782AS

Part: RETAINING RING — OUT OF POSITION (L1 DOOR) · airframe 45,322 hrs · 25,336 cycles

L1 DOOR HARD TO OPEN. FOUND RETAINING RING OFF PIN. RE-ATTACHED RING TO PIN. OP CHECKS GOOD. REF ILLUSTRATION FROM MM 52-11-21 PG 402.

Part: SKIN — DENTED (BS 360-365) · airframe 42,674 hrs · 23,853 cycles

PREVIOUS REPAIR ON FUSELAGE IS DENTED. REMOVED THE DAMAGED EXITING REPAIR DOUBLER AND TRIMMED OUT THE DAMAGED AREA OF SKIN FABRICATED AND INSTALLED A SKIN FILLER AND EXTERNAL REPAIR DOUBLER IAW ASA EA 5330 02171 AND AAR EA 11803.

Part: SKIN — DENTED (LT WING) · airframe 42,674 hrs · 23,853 cycles

THE LEFT WING TRAILING EDGE I/B FORE FLAP LWR SURFACE HAS AN EXISTING REPAIR WITH MULTIPLE DENTS AND DINGS AT WBL 90. REMOVED THE EXISTING REPAIR DOUBLER AND DAMAGED AREA OF LOWER SKIN FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 42,674 hrs · 23,853 cycles

THE LT HORIZ STAB LE WAS DROPPED DURING INSTALLATION RESULTING IN A SKIN DENT AT TWO EXITING REPAIRS. REMOVED THE TWO EXITING REPAIR DOUBLERS AND FILLERS CUTOUT THE DAMAGED AREA OF SKIN FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 55 10 01 FIG 201.

Part: SKIN — DENTED (TE FLAP) · airframe 42,674 hrs · 23,853 cycles

THE RIGHT WING TRAILING EDGE I/B FORE FLAP LWR SURFACE HAS MULTIPLE DENTS AND DINGS FROM WBL 101.5 - 121.5. REMOVED THE DAMAGED AREA OF LOWER SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20.

Part: SKIN — DENTED (TE FLAP) · airframe 42,674 hrs · 23,853 cycles

THE LEFT WING TRAILING EDGE I/B FORE FLAP LWR SURFACE IS DINGED AT WBL 126. REMOVED THE DAMAGED AREA OF LWR SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20.

Part: SKIN — DENTED (TE FLAP) · airframe 42,674 hrs · 23,853 cycles

THE LEFT WING TRAILING EDGE I/B FORE FLAP HAS A DING AT WBL 96.5. CUT OUT THE DAMAGED AREA ON THE LWR SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20.

Part: SKIN — DENTED (TE FLAP) · airframe 42,674 hrs · 23,853 cycles

THE LEFT WING TRAILING EDGE I/B FORE FLAP LWR SURFACE HAS AN EXISTING REPAIR WITH MULTIPLE DENTS AND DINGS AT WBL 119. REMOVED THE EXISTING REPAIR DOUBLER AND DAMAGED AREA OF LWR SKIN FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20.

Part: PANEL — DENTED (NR 4 SPOILER) · airframe 42,674 hrs · 23,853 cycles

LEFT WING NR 4 SPOILER LWR SURFACE HAS DENTS AND DINGS AT WBL 122. REMOVED THE DAMAGED AREA OF THE LWR SURFACE, FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 42,674 hrs · 23,853 cycles

PASSENGER CABIN FLOORBEAM CORRODED OUT OF LIMITS. REMOVED THE DAMAGED AREA OF THE BEAM UPPER HORIZONTAL FLANGE, FABRICATED AND INSTALLED A REPAIR T-CHORD SECTION 2 SPLICE ANGLES 2 SPLICE STRAPS AND FILLERS IAW ASA EA 5310 02690 AND AAR EA 11805.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 42,674 hrs · 23,853 cycles

THE RIGHT WING NR 5 SPOILER LWR SURFACE HAS A DING AT WBL 112.75. REMOVED THE DAMAGED AREA OF LOWER SKIN FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 51-70-10 PARA 7, 8, 11, 15, 18 AND 20.

Part: FLOORBEAM — CORRODED (BS 360) · corrosion level 2 · airframe 42,674 hrs · 23,853 cycles

PASSENGER CABIN FLOORBEAM IS CORRODED OUT OF LIMITS. REMOVED EXISTING REPAIR IN THE DAMAGE AREA REMOVED THE DAMAGED AREA OF UPPER CHORD HORIZONTAL FLANGE, FABRICATED AND INSTALLED A REPLACEMENT UPPER T-CHORD SEGMENT 2 SPLICE ANGLES AND TWO SPLICE STRAPS PER ASA EA 53 10 02691 AND AAR EA 11808.

Part: WEDGE — CHAFED (NR 5 SLAT) · airframe 42,675 hrs · 23,853 cycles

THE RIGHT WING NR 5 SLAT IS CHAFED ON THE T/E LOWER SURFACE AT SS 144 152 AND 189 199. PREPAIRED THE DAMAGED SURFACES FOR BONDING, FABRICATED AND INSTALLED TWO REPAIR DOUBLERS IAW SRM 51-70-10 REPAIR 2.

Part: ATTACH ANGLE — CRACKED (BS 360) · airframe 42,675 hrs · 23,853 cycles

STRINGER 11L ATTACH CLIP CRACKED AT FS 360. REMOVED THE DAMAGED CLIP AND INSTALLED A REPLACEMENT CLIP IAW EA 5310 02689 AND AAR EA 11818.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 42,675 hrs · 23,853 cycles

THE LEFT HORIZONTAL STAB L/E SKIN IS DENTED OUT OF LIMITS AT L/E STA 92. CUT OUT THE DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND INTERNAL REPAIR DOUBLER IAW SRM 55-10-01 FIG 201.

Part: SKIN — DENTED (SPOILER) · airframe 42,674 hrs · 23,853 cycles

THE LEFT WING NR 4 SPOILER LOWER SURFACE HAS NUMEROUS DENTS AND DINGS AT WBL 87.75. PREPAIRED THE DAMAGED SURFACE FOR BONDING, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 PG 211, 213, 221, 238, 244 AND 249.

Part: SILL — CORRODED (BS 920-1004) · corrosion level 2 · airframe 42,674 hrs · 23,853 cycles

THE L2 DOOR CUTOUT LOWER MAIN SILL INNER CHORD IS CORRODED OUT OF LIMITS AT FS 920 986.5 WL 208. REMOVED THE DAMAGED CHORD, LOCATED, DRILLED AND INSTALLED A REPLACEMENT CHORD IAW SRM 51-40-2 AND 51-40-5.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 42,674 hrs · 23,853 cycles

THE LEFT HORIZONTAL STABLIZER L/E SKIN IS DENTED OUT OF LIMITS AT L/E STA 98. CUT OUT THE DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED A SKIN FILLER AND INTERNAL REPAIR DOUBLER IAW SRM 55-10-01 FIG 201.

Part: SKIN — DENTED (NR 3 SPOILER) · airframe 42,674 hrs · 23,853 cycles

THE LEFT WING NR 3 SPOILER UPPER SURFACE IS DENTED AT WS 334. PREPAIRED THE DAMAGED SURFACE FOR BONDING, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 REPAIR 2.

Part: INTERCOSTAL — CORRODED (BS 947-967) · corrosion level 2 · airframe 42,674 hrs · 23,853 cycles

PASSENGER CABIN FLOOR INTERCOSTAL CORRODED OUT OF LIMITS AT FS 947.5 967 LBL 44. REMOVED THE DAMAGED INTERCOSTAL LOCATED DRILLED AND INSTALLED A REPLACEMENT INTERCOSTAL IAW SRM 51-40-05 AND 51-40-02.

Part: INTERCOSTAL — CORRODED (BS 947-967) · corrosion level 2 · airframe 42,674 hrs · 23,853 cycles

PASSENGER CABIN FLOOR INTERCOSTAL CORRODED OUT OF LIMITS AT FS 947.5 967 RBL 44. REMOVED THE DAMAGED INTERCOSTAL, LOCATED, DRILLED AND INSTALLED A REPLACEMENT INTERCOSTAL IAW SRM 51-40-05 AND 51-40-02.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,675 hrs · 23,853 cycles

PASSENGER CABIN FLOOR WEB IS CORRODED OUT OF LIMITS. CUT OUT THE DAMAGED AREA OF THE WEB FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM 51-70-13 FIG 1.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,675 hrs · 23,853 cycles

PASSENGER CABIN FLOOR IS CORRODED OUT OF LIMITS AT THE G4 OUTBOARD AFT FLOOR FITTING FS 1016 LT SIDE. CUT OUT DAMAGED AREA OF THE WEB, FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-13 FIG 1.

Part: FLOORBEAM — CORRODED (BS 767) · airframe 40,569 hrs · 22,708 cycles

AFT CARGO PIT HAS CORROSION ON ALL FLOORBEAMS FROM LT TRANSITION PANEL TO RT TRANSITION PANEL. FLOORBEAMS REPAIRED IAW ASA EA 5310 02617.

Part: SILL — CORRODED (BS 492-440) · airframe 40,569 hrs · 22,708 cycles

FOUND CORROSION ON FWD CARGO COMPARTMENT DOOR OPENING SILL WEB. REMOVED AND INSTALLED NEW SILL WEB IAW SRM 51 40 02 PG 3 PARA 5B.

Part: SKIN — CHAFED (TE FLAP) · airframe 40,569 hrs · 22,708 cycles

LT WING OB MID FLAP LE SKIN IS CHAFED AT IB CORNER. BLENDED CHAFED AREA CHECKED OUT OF LIMITS. REPAIRED IAW SRM 57 53 01 FIG 201 REPAIR 8.

Part: SKIN — DENTED (BS 1000-1010) · airframe 40,569 hrs · 22,708 cycles

FOUND FUSELAGE EXTERNAL SKIN DENTED. DENT WITHIN 3" OF LAP. DENT APPEARS TO CROSS THE LAP AT STR 14R. REPAIRED EXTERNAL SKIN IAW ASA EA 5330 02081.

Part: SKIN — CHAFED (TE FLAP) · airframe 40,569 hrs · 22,708 cycles

RT OB FORE FLAP CHAFED ON IB LE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57 53 01 FIG 201 REPAIR 1.

Part: SKIN — CHAFED (LT NR 3 SLAT) · airframe 40,569 hrs · 22,708 cycles

LT WING NR 3 SLAT IB LWR T/E IS CHAFED. REPAIRED SLAT IAW SRM 51 70 10 PARA 1 REPAIR 4 PG 201.

Part: HOUSING — CORRODED (R1 DOOR HANDLE) · airframe 40,569 hrs · 22,708 cycles

FOUND CORROSION AROUND HANDLE SHAFT BEARING HOUSING OF R1 DOOR. REMOVED AND REPLACED R1 DOOR HANDLE SHAFT HOUSING (TORQUE BOX) IAW BOHM 52 46 06.

Part: STRINGER CLIP — CORRODED (BS 787 S26R) · airframe 40,569 hrs · 22,708 cycles

AFT PIT CORROSION ON STRINGER CLIP. REMOVED AND DISCARDED CORRODED STRINGER CLIP FABRICATED DRILLED UP AND INSTALLED NEW STRINGER CLIP PER SRM 51 40 02 PG 2 3 6 AND 7.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 40,569 hrs · 22,708 cycles

ACCESS PANEL 7420 RT WING 45 INCHES FM IB END PNL HAS A DENT. REPAIRED THE DAMAGED AREA OF RT WING FLAP PNL 7420 IAW SRM 51 70 10 PG 211 PARA 7 PG 213 PARA 8 PG 238 APRA 15 AND PG 249 PARA 20.

Part: SKIN — DENTED (LT WING) · airframe 40,569 hrs · 22,708 cycles

UPPER LT WING PNL NR 7220L IS DENTED ON THE LWR SURFACE AS MARKED. REPAIRED THE DAMAGED AREA OF THE LT WING PANEL NR 7220L IAW SRM 51 70 10 PG 211 PARA 7 PG 213 PARA 8 PG 238 PARA 15 AND PG 249 PARA 20.

Part: SKIN — DENTED (FORE FLAP) · airframe 40,570 hrs · 22,708 cycles

FOUND RT IB FORE FLAP HAS SHARP DENT ON LWR SURFACE 28" FM IB END. REPAIRED PER SRM 51 70 10 REPAIR 4.

Part: SKIN — DELAMINATED (NR 9 SPOILER) · airframe 40,570 hrs · 22,708 cycles

RT WING NR 9 SPOILER UPPER SURFACE IS DELAMINATED WITH A DENT. REPAIRED PER SRM 51 70 10 REPAIR 4.

Part: ANGLE — CRACKED (BS 285) · airframe 40,569 hrs · 22,708 cycles

FOUND L ANGLE CRACKED 9" FWD OF FWD GALLEY DOOR NR 4 (FROM TOP) STOP PAD FITTING. REMOVED FABRICATED AND REPLACED ANGLE.

Part: SLIDE — DISCHARGED (L-1 DOOR) · airframe 40,427 hrs · 22,631 cycles

FOUND L1 DOOR SLIDE PRESSURE NOT IN THE "GREEN". REMOVED AND REPLACED THE L1 SLIDE PER AMM 25 61 35 PG 201 218.

Part: SKIN — DELAMINATED (NR 5 SLAT)

RT NR 5 SLAT OB T/E IS DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)

Part: SKIN — PUNCTURED (SPOILER)

NR 4 SPOILER HAS A HOLE PIERCED THROUGH. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)

Part: FLOORBEAM — CORRODED (BS 344)

FLOORBEAM FORWARD UPPER TEE IS CORRODED AT BSTA 344 LBL 15. REMOVED DAMAGED (T) CHORD, FABRICATED AND INSTALLED A REPLACEMENT (T) CHORD IAW SRM. (K)

Part: SKIN — DELAMINATED (WING)

RT NR 5 SLAT IB T/E IS DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)

Part: WEB — CRACKED (FUSELAGE)

MAIN CABIN STA 344 APPROX. LBL 45 AT T-CHORD IS CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPLACEMENT DOUBLER, A REPAIR PLATE, AND REPAIR WEB SEGMENT. (K)

Part: WEDGE — CHAFED (RT WING)

RT WING IB T/E MIF FLAP T/E WEDGE IS CHAFFED. REMOVED DAMAGED WEDGE, ORDERED AND REPLACED WITH A NEW WEDGE IAW SRM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TOP OF FLOORBEAM CORRODED AT STA 312, LBL 12. REMOVED DAMAGED UPPER CHORD, FABRICATED AND INSTALLED A REPLACEMENT UPPER CHORD IAW SRM. (K)

Part: CONNECTOR — DAMAGED (ROW 20-25)

DURING LINE CHECK, FOUND FLOOR TRACK LIGHTING INOPERATIVE AT ROWS 20-25. REPLACED CONNECTOR, OPS CHECKED GOOD. (M)

Part: BRACKET — CRACKED (RT WING AILERON)

PAE - DURING C-CHECK, FOUND CRACKED BRACKET RIGHT AILERON INBOARD BALANCE BAY OUTBOARD RIB FITTING AND WEB. REPAIRED IAW SRM. (M)

Part: ANGLE — CRACKED (FUSELAGE)

PAE DURING C-CHECK, FOUND LEFT AFT RAM AIR INLET PLENUM OUTBOARD ATTACH SKATE ANGLE IS CRACKED. REPAIRED IAW SRM. (M)

Part: WIRE — BROKEN (ROW 19)

SEA - DURING LINE CHECK, FOUND THE EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 19. REPAIRED BROKEN WIRE. TRACK LIGHTS THEN OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 17, 18, 19, DISCONNECTED WIRES. RECONNECTED WIRES, OPS CHECKED NORMAL. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - TRACK LIGHTS INOPERATIVE AT ROWS 18-20. RECONNECTED WIRES, OPS CHECKED NORMAL. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - AFT CABIN TWO RED TRACK LIGHTS INOPERATIVE. RECONNECTED WIRES, OPS CHECKED NORMAL. (M)

Part: FRAME — GOUGED (FUSELAGE)

PAE - DURING SI C-CHECK, FOUND AFT BAY FORWARD DOOR FRAME IS GOUGED AT BS 794, RBL 27 WL 156 AND RBL 31 AND WL 158. REPAIRED PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FLOORBEAM AT BS 1016, LBL 29 AND WL 208 IS CORRODED. REPAIRED PER EA. (M)

Part: SKIN — CRACKED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CRACK ON FORWARD APU DOOR HINGE CUTOUT. REPAIRED PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI C-CHECK, FOUND CORROSION ON TOP OF FLOORBEAM AT BS 344, LBL 17 TO 43. REPAIRED PER EA. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON FLOORBEAM AT STATION 344, LBL 60 AND WL 206. REPAIRED IAW EA. (M)

Part: FITTING — CORRODED (FWD ENTRY)

PAE - DURING SI CHECK, FOUND CORROSION ON GRIT BAR ATTACHMENT AT BS 344, LBL 53 AND WL 209. REPLACED PER SRM. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

PAE - DURING SI CHECK, FOUND SEAT TRACK GOUGED AT BS 538, LBL 45.5 AND WL 208. REPLACED PER SRM. (M)

Part: ATTACH FITTING — CORRODED (GIRT BAR)

PAE - DURING SI CHECK, FOUND CORROSION ON GIRT BAR ATTACHMENT AT BS 312, LBL 53, WL 209. REPLACED PER SRM. (M)

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FLOOR SUPPORT AT BS 951, LBL 16-25 AND WL 208 HAS MECHANICAL DAMAGE. REPLACED FLOOR SUPPORT PER SRM. (M)

Part: FLOORBEAM — DAMAGED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FLOORBEAM AT BS 967 RBL 16 AND WL 208 HAS MECHANICAL DAMAGE. REPAIRED PER SRM. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON MOP SILL AT BS 307-344, LBL 55 AND WL 208. REPLACED MOP SILL PER SRM. (M)

Part: ANGLE — CORRODED (GALLEY)

PAE - DURING SI CHECK, FOUND GALLEY SUPPORT ANGLE CORRODED AT BS 993, LBL 32-44, WL 208. REPLACED PER SRM. (M)

Part: STRINGER — GOUGED (FUSELAGE)

PAE - DURING SI CHECK, FOUND GOUGE ON STRINGER 16 RT ON UPPER SIDE JUST FORWARD OF 500F FRAME. REPAIRED PER SRM. (M)

Part: STIFFENER — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON STIFFENER AT BS 335, LBL 10 AND WL 208. REPLACED IAW SRM. (M)

Part: ANGLE — CORRODED (GALLEY)

PAE - DURING SI CHECK, FOUND GALLEY SUPPORT ANGLE CORRODED AT BS 986-1016, RBL 32, WL 208. REPLACED IAW SRM. (M)

Part: STRINGER — GOUGED (FUSELAGE)

PAE - DURING SI CHECK, FOUND STRINGER 16 RIGHT HAS GOUGE ON UPPER SIDE JUST FORWARD OF BS 500 FRAME. REPAIRED PER SRM. (M)

Part: ATTACH FITTING — CORRODED (GALLEY)

PAE - DURING SI CHECK, FOUND CORROSION ON GALLEY ATTACH FITTINGS AT BS 333, RBL 9 AND WL 209. REPLACED PER SRM. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND L2 MOPSILL AT BS 951-992, LBL 55 AND WL 208 CORRODED. REPLACED PER SRM. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND R-2 MOPSILL AT BS 951-992, RBL 55 AND WL 208 CORRODED. REPLACED PER SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CRACK IN FRAME AT BS 1006 WL 208 AND LBL 41. REPAIRED IAW SRM. (M)

Part: ANGLE — DAMAGED (GALLEY)

PAE - DURING SI CHECK, FOUND GALLEY SUPPORT Z-ANGLE AT BS 993, RBL 32-44, AND WL 208 HAS MECHANICAL DAMAGE. REPLACED PER SRM. (M)

Part: ANGLE — CORRODED (GALLEY)

PAE - DURING SI CHECK, FOUND GALLEY SUPPORT ANGLE QT BS 986 TO 1016 AND WL 208 IS CORRODED. REMOVED AND REPLACED ANGLE IAW SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON FLOORBEAM AT STATION 360 WL 208 AND RBL 19 AND 26. REPAIRED IAW SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CRACK AT BS 747 BETWEEN STRINGER 8 AND 9 LEFT. REPAIRED CRACKED FRAME PER SRM. (M)

Part: STRAP — DAMAGED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FLOOR WEB STRAP AT BS 1020 RBL 18 AND WL 208 HAS MECHANICAL DAMAGE. REPLACES STRAP PER SRM. (M)

Part: STRAP — DAMAGED (FUSELAGE)

PAE - DURING SI CHECK, FOUND FLOOR WEB STRAP AT BS 1020 RBL 4 AND LBL 4 AND WL 208 HAS MECHANICAL DAMAGE. REPLACED STRAP PER SRM. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION TOP OF FLOORBEAM AT BS 312 LBL 1, 6, 15 AND WL 208. REPAIRED IAW SRM. (M)

Part: ANGLE — CORRODED (BULKHEAD)

PAE - DURING SI CHECK, FOUND CORROSION ON BULKHEAD SUPPORT ANGLE AT STATION 500G LBL 24 TO RBL 24 AND WL 156. FABRICATED AND INSTALLED ANGLE IAW SRM. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - DURING SI CHECK, FOUND CORROSION ON MOPSILL RBL 55 AT BS 274, 283, 294 AND 346 AND WL 208. REMOVED AND REPLACED MOPSILL IAW SRM. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - DURING SI CHECK, FOUND STUB FRAME AT BS 294.5, WL 208, RBL 60 IS CRACKED. REPAIRED IAW SRM. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT MID CABIN INOPERATIVE, WIRE BROKEN. REPAIRED BROKEN WIRE. OPS CHECK NORMAL. (M)

Part: THRESHOLD — CRACKED (CARGO BAY)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY CENTER THRESHOLD CRACKED. REMOVED AND REPAIRED IAW ASA EA 5320-01442. (M)

Part: GUARD — DAMAGED (CARGO BAY)

PAE - DURING INSPECTION, FOUND FORWARD CARGO COMPARTMENT LEFT BLOW OUT PANEL GRATE DAMAGED. REMOVED FORWARD CARGO COMPARTMENT LEFT BLOWOUT PANEL GRATE, ACCOMPLISHED PERMANENT REPAIR PER SRM 51-40-02 AND EA 2550-C1151 AND REINSTALLED. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 18-20 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: SIGN — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT TRACK LIGHTS AND THE R1 DOOR EMERGENCY EXIT IDENTIFIER WERE FOUND INOPERATIVE. REPLACED THE AFT TRACK LIGHT ASSEMBLY AND THE R1 DOOR EMERGENCY EXIT IDENTIFIER AND LIGHTS OPERATED NORMALLY. REF: OPER CNTRL NR ASAA9940165.

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT TRACK LIGHTS AND THE R1 DOOR EMERGENCY EXIT IDENTIFIER WERE FOUND INOPERATIVE. REPLACED THE AFT TRACK LIGHT ASSEMBLY AND THE R1 DOOR EMERGENCY EXIT IDENTIFIER AND LIGHTS OPERATED NORMALLY. REF: OPER CNTRL NR 2000ZZZX252. (X)

Part: BATTERY CHARGER — DISCHARGED (ROW 8)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 8 TO THE FIRST OVERWING EXIT. REPLACED BATTERY PACK, CHARGER, AND REPAIRED WIRING, LIGHTS OPERATED NORMALLY. (M)

Part: CHARGER — INOPERATIVE (ROW 8)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 8 TO THE FIRST OVERWING EXIT. REPLACED BATTERY PACK, CHARGER, AND REPAIRED WIRING, LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY CHARGER — INOPERATIVE (ROWS 13 & 14)

JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 13 AND 14. REPLACED BATTERY CHARGER AND LIGHTS OPERATED NORMALLY. (X)

Part: LENS — MISSING (R2 EXIT SIGN)

PDX - DURING MAINTENANCE CHECK, THE EXIT SIGN LENS AT THE R-2 DOOR WAS FOUND MISSING. REPLACED 'EXIT' SIGN LENS ASSEMBLY. (M)

Part: LATCH — OUT OF ADJUST (L1 DOOR)

PDX - PRIOR TO FLT 348, THE ATTENDANT REPORTED THAT THE L1 DOOR WAS HARD TO CLOSE. LUBRICATED HINGE POINTS AND ADJUSTED THE FORWARD UPPER LATCH CAM FITTING. DOOR OPERATED NORMALLY. (M)

Part: CAM ROLLER — CONTAMINATED (PAX DOOR)

SEA - PRIOR TO FLT 75 - THE CREW REPORTED THAT THE L1 DOOR WAS DIFFICULT TO CLOSE. REMOVED LINER AND INSPECTED LINKAGE AND ROD ENDS, NO DEFECTS NOTED. FOUND CAM ROLLERS GUMMED UP, CLEANED SAME. LUBRICATED DOOR MECHANISM AND DOOR OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - FLT 27 - PRIOR TO FLT, ONE WHITE EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 27. REPLACED LAMP BASE ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (R1 DOOR)

SEA - PRIOR TO FLT 549, THE R1 DOOR WAS FOUND DIFFICULT TO OPEN. REPLACED THE R1 DOOR HANDLE CENTERING CAM BEARING AND LUBRICATED DOOR. DOOR OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (AFT CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 27 AFT. REPLACED LIGHT SOCKET ASSEMBLY AND LIGHTS OPERATED NORMALLY. (X)

Part: MECHANISM — LACK OF LUBE (L1 DOOR)

SEA - PRIOR TO F340, THE L1 DOOR WAS FOUND TO BE VERY STIFF DURING OPENING AND CLOSING. LUBRICATED DOOR HINGE AND CYCLED DOOR SEVERAL TIMES, DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

YVR - FLT 656 - CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE FROM ROW 21 THROUGH 26. CONTRACT MAINTENANCE REPAIRED WIRE AT ROW 26 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 5 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (L2 DOOR)

PDX - FLT 544 - CATERING REPORTED, THAT THE L2 DOOR WAS DIFFICULT TO OPEN. LUBED AND ADJUSTED DOOR AND DOOR OPERATED NORMALLY. (M)

Part: BOLTS — LOOSE (L1 DOOR)

SEA - FLT 579 - PRIOR TO DEPARTURE, THE CREW REPORTED THAT THE L1 DOOR STICKS DURING OPENING. MAINTENANCE FOUND THE BOTTOM GATE SEAL BOLTS LOOSE. TIGHTENED BOLTS AND DOOR OPERATED NORMALLY. (M)

Part: MECHANISM — LACK OF LUBE (PAX DOOR)

SEA - FLT 193 - CREW REPORTED L2 DOOR SOMEWHAT TIGHT DURING OPENING SEQUENCE. LUBED DOOR AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

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

Part: WIRE — DISCONNECTED (CABIN)

LAX - FLT NR 157 - CREW REPORTED, THE AFT 5 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RESECURED LOOSE WIRING AT ROW 25 AND THE LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

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

Part: WIRE — DISCONNECTED (CABIN)

SNA - FLT 489 - CREW REPORTED THE AFT 6 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RESECURED LOOSE CONNECTION AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL WIRING — DISCONNECTED (CABIN)

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

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LOOSE CONNECTOR AT THIRD LIGHT AND ALL LIGHTS OPERATED NORMALLY. (X)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROWS 1 THROUGH 3. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (Z)

Part: EEL WIRING — LOOSE (CABIN)

SEA - CHECK -- AFT 3 EMERGENCY LIGHTS INOP. MAINTENANCE RECONNECTED WIRING HARNESS. (X)