N762AS

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 71,158 hrs · 47,322 cycles

AFT ACFT RT OVERWING EXIT LIGHT SIGN FELL OFF. ACFT GROUNDED. REPLACED AFT ACFT RT OVERWING EXIT LIGHT ASSY IAW AMM 33-51-11, OPS CHECK GOOD.

Part: INTERCOSTAL — CRACKED (BS 277-294) · airframe 70,700 hrs · 46,955 cycles

INTERCOSTAL AT BS 277 AND STR 14R CRACKED IN RADIUS. ACFT GROUNDED. R & R DAMAGED INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: SKIN — CRACKED (BS 485-500A) · airframe 70,700 hrs · 46,955 cycles

ACFT SKIN APPEARS TO BE CRACKED FWD AND AFT OF NR 2 VHF COMM ANTENNA. ACFT GROUNDED. REPAIRED SKIN FWD, AND AFT OF NR 2 VHF ANTENNA BS 5000 TO 500A IAW EA 400-53EA-16730. THIS REPAIR IS CATEGORY B. FUSELAGE SKIN REPAIR AT VHF-2 ANTENNA LOCATION FROM BS 485 TO BS 500A+10 BETWEEN S-27L AND S-27R. INSPECTION THRESHOLD 75,000 TOTAL FLT. CYCLES. FUSELAGE FRAME REPAIR AT BS 500 BETWEEN S-28L AND S-28R.

Part: SUPPORT FITTING — CRACKED (LT WING MLG) · airframe 70,700 hrs · 46,955 cycles

LT WING REAR SPAR MLG SUPPORT BEAM AFT SUPPORT FITTING CRACKED IN RADIUS 4 FAST OTBD. ACFT GROUNDED. ACCOMPLISHED INSPECTIONS TO LT MLG BEAM AFT SUPPORT FITTING IAW EA 400-57EA-16720. THIS IS A CATEGORY C REPAIR LT MLG BEAM AFT SUPPORT FITTING MUST BE R & R BEFORE ACFT REACHES 58.955 TOTAL FLT CYCLES. REFER TO EC TYPE EA 400-57EA-16721 AND ASSOCIATED T/C 400-57EA-16721-1 FOR FITTING REMOVAL AND REPLACEMENT.

Part: SUPPORT FITTING — CRACKED (RT WING MLG) · airframe 70,700 hrs · 46,955 cycles

R/W REAR SPAR MLG BEAM AFT SUPPORT FITTING CRACK IN RADIUS 2ND FASN OTBD. ACFT GROUNDED. ACCOMPLISHED INSPECTIONS TO RT MLG BEAM AFT SUPPORT FITTING IAW EA 400-57 EA-16718. THIS IS A CATEGORY C REPAIR RT WING MLG BEAM AFT SUPPORT FITTING MUST BE R & R BEFORE ACFT REACHES 58,955 TOTAL FLT CYCLES. REFER TO EC TYPE EA 400-57EA-16719 AND ASSOCIATED T/C 400-57EA-16719-1 FOR FITTING REMOVAL AND REPLACEMENT.

Part: FRAME — GOUGED (BS 1061) · airframe 70,700 hrs · 46,955 cycles

TAILCOMP TOP SIDE OF FRAME 1061 GOUGED ON AFT RADIUS AT LBL 18, ABOVE LIGHT SWITCH. ACFT GROUNDED. REPAIRED TOP SIDE OF FRAME 1064 IAW EA 400 53EA 16732 REPAIR HAS 1ST STAGE APPROVAL SR4-3198637333, AND 8100-9 REQUIRE 2ND STAGE APPROVAL WITHIN 24 MOS.

Part: SKIN — DENTED (BS 1064-1088) · airframe 70,700 hrs · 46,955 cycles

LT AFT FUSELAGE PANEL OTBD OF TAILSKID FAIRING HAS SEVERAL PROTRUSIONS AND DENTS. ACFT GROUNDED. REPAIRED LT AFT FUSELAGE SKIN IAW EA 400-53EA-16728. THIS REPAIR IS CATEGORY A REPAIR AND DOES NOT REQUIRE DTI ASSESSMENT.

Part: SKIN — CRACKED (BS 727D) · airframe 69,884 hrs · 46,280 cycles

CRACK IN FUSELAGE, RT SIDE .8750 LONG, 1.5 FWD 727E, TOP SIDE OF S-24R TRANSFERRED FROM N/R 00001 DEFECT NR 11426711. ACFT GROUNDED. REPAIRED SKIN CRACK DAMAGE IAW SRM 53-00 01-2R-31 DET IDX. THIS IS A CAT B REPAIR INITIAL THRESHOLD IS SET FOR 66,000 CYCLES REFER TO OPERATORS REPAIR ASSESSMENT PROGRAM FOR INSPECTION METHODS AND INTERVALS.

Part: LOCK — BROKEN (CARGO TRACK) · airframe 69,124 hrs · 45,613 cycles

FLOOR PALLET LOCK BROKEN , NR 1 POSITION FAR RT INBD SIDE, FWD. ACFT GROUNDED. REMOVED DAMAGED TRACK MATERIAL IN POSITION NR 1, REF SRM 53-00-52, REPAIR OPTION NR 1. DRILLED FASTENER HOLES ON NEW SEAT TRACK EXTRUSION PIECE REF SRM 53-00-52. REPAIR OPTION NR 1. ALODINED, PRIMED AND PAINTED SEAT TRACK EXTRUSION PIECE AND ASSOCIATED RADIOUS FILLER PIECE AS WELL AS EXISTING SEAT TRACK REF SRM 53-00-52, REPAIR OPTION NR 1 AND EA 400-53EA-15189. COMPLETED INSTALLATION OF SEAT TRACK EXTRUSION IN CARGO POSITION NR 1, REF SRM 53-0-52, REPAIR OPTION NR 1.

Part: SKIN — DAMAGED · airframe 68,317 hrs · 44,937 cycles

LIGHTING STRIKE DAMAGE AT FRONT LT SIDE OF ACFT FS 291, STRINGER 21L, REF LP 11338892. ACFT GROUNDED. REPAIRED LIGHTNING STRIKE DAMAGE AT LT SIDE FS 291, STR 21L IAW EA 400 53 EA, 14603.

Part: SKIN — DAMAGED · airframe 68,317 hrs · 44,937 cycles

LIGHTING STRIKE DAMAGE AT FRONT LT SIDE OF ACFT FS 291, STRINGER 21L REF LP 11338892. ACFT GROUNDED. REPAIRED LIGHTNING STRIKE DAMAGE AT LT SIDE FS 291, STR 21L IAW EA 400, 53EA 14603.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,588 hrs · 44,347 cycles

L2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMP, OPS NORMAL.

Part: DOOR — OUT OF RIG (L2) · airframe 65,607 hrs · 42,620 cycles

F/A REPORTS L2 DOOR DIFFICULT TO CLOSE. ACFT GROUNDED. FOUND L-2 DOOR OUT OF RIG. ACCOMPLISHED RIG ON L-2 DOOR HORIZONTAL ROD, GUIDE ARM & STOP PINS IAW AMM 52-13-00-705-001 & OTHER RIG CHECKS CHECKED GOOD IAW AMM 52-13-00-705-001. ACCOMPLISHED LUBRICATION OF L-2 DOOR REF. AMM 12-25-11-608-001. ACCOMPLISHED L-2 DOOR OPS CHECK & CHECKED GOOD REF AMM 52-13-00-705-034.

Part: SKIN — CRACKED (BS 941-944) · airframe 65,416 hrs · 42,463 cycles

CRACK FOUND ON FUSELAGE SKIN STA 941 TO 944.2, BETWEEN STR 24R AND 25R. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01-2R-31, CAT B REPAIR INSPECTION THRESHOLD 66,000, FOR METHOD AND INTERVAL REFER TO OPERATORS REPAIR ASSESSMENT PROGRAM.

Part: SKIN — CRACKED (BS 941-944) · airframe 65,416 hrs · 42,463 cycles

FOUND A CRACK AT BS 941 TO 944, 2.75 INCHES LONG BETWEEN STRINGERS 24 & 25R. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01-2R-31, CAT B REPAIR.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 65,387 hrs · 42,444 cycles

AFT EXIT LIGHT COVER LOOSE. ACFT GROUNDED. REPLACED AFT L2 DOOR EXIT LIGHT ASSY. OPTS CHECKED GOOD IAW AMM 33-51-11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,987 hrs · 42,043 cycles

AFTER REMOVAL OF FWD PIT VHF DOUBLER FOUND DOUBLER SUPPORT ANGLE CRACKED. FABRICATED NEW ANGLE, TREAT, PRIMED AND TOPCOATED IAW SWRM 51-20-01-0G-0. AND INSTALLED.

Part: DOUBLER — CRACKED (VHF ANTENNA) · airframe 64,987 hrs · 42,043 cycles

FWD CARGO VHF ANTENNA DOUBLER FOUND CRACKED AFTER CLEANING FOR PEELING PAINT NR MIG5 SN 5413337. R & R CRACKED ANTENNA DOUBLER IAW SRM 51-40-02-0G-0.

Part: ATTACH BRACKET — CRACKED · airframe 64,897 hrs · 42,043 cycles

ATTACH BRACKET CRACKED BS 291 AND RBL 60, BELOW STR 18 FOUND AFT REMOVING SHEAR WEB. ACFT GROUNDED. FABRICATED NEW ATTACH BRACKET ALODINED PRIMED AND TOPCOATED IAW DWG 69-37402-4, SRM 51-40-05-0G-0, AMM 51-21-21-307-014 AND 51-21-99-307-022.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 64,897 hrs · 42,043 cycles

RT HORIZONTAL LOWER SKIN IS CRACKED AT APPROX STAB STA 113 JUST FWD OF REAR SPAR. ACFT GROUNDED. REPAIRED SKIN IAW SRM 55-10-01-2R-13

Part: SHEAR WEB — CRACKED (BS 328) · airframe 64,897 hrs · 42,043 cycles

AFTER REMOVAL OF UPPER TEE ANGLE OF FRAME AT BS 328, FOUND SHEAR WEB GOUGED AND CRACKED RBL 60 ON LOWER SURFACE. ACFT GROUNDED. REMOVED SHEAR WEB FABRICATED NEW SHEAR WEB, ALODINED, PRIMED, TOPCOATED AND INSTALLED IAW SRM 51-40-05 0G-0, 51-40-02-0G-0, AMM 51-21-21-307-014 AND 51-21-99-307-022.

Part: WEB — CORRODED (BS 967-986) · corrosion level 2 · airframe 64,897 hrs · 42,043 cycles

AFTER REMOVAL OF LT AFT MOP SEAL LOWER SURFACE OF WEB IS CORRODED, STA 967-986 AT STR 18 LT. ACFT GROUNDED. REMOVED CORRODED ON LT AFT MOP SEAL WEB AND FOUND TO BE OUT OF LIMITS OF SRM 53-60-15-1A-1. R & R WITH NEW WEB IAW SRM 51-40-02-0G-0, W 4", O .056", R .049", L 19", D .007.

Part: FRAME — CRACKED (BS 480) · airframe 64,897 hrs · 42,043 cycles

RT FUSELAGE FRAME, BS 480 CRACKED ABOVE SHEAR WEB. R & R FRAME ASSY IAW SRM 51-40-05 AND 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 64,897 hrs · 42,043 cycles

FLOOR SUPPORT CRACKED AT FS 344 AND LBL 47, ACFT GROUNDED. R & R FLOOR SUPPORT IAW SRM 51-40 02.

Part: STRINGER CLIP — CRACKED (BS 500) · airframe 64,897 hrs · 42,043 cycles

STRINGER CLIP 6R ON AFT SIDE OF FRAME AT BS 500 HAS EVIDENCE OF A CRACK AT FASTENER HOLE. R & R STRINGER CLIP IAW SRM 51-40-02.

Part: ANGLE — CRACKED (BS 194) · airframe 64,897 hrs · 42,043 cycles

FORWARD GALLEY SERVICE DOOR BS 194.5 S9R EVIDENCE OF A CRACK FIN RADIUS OF FRAME SUPPORT. ACFT GROUNDED. R & R FRAME SUPPORT IAW SRM 51-40-05-0G-0.

Part: DOOR FRAME — CRACKED (BS 440) · airframe 64,897 hrs · 42,043 cycles

DOOR FRAME IS CRACKED APPROX 1.25 AT LOWER DOORSTOP FITTING MOUNTING AREA EXTENDING FROM LOWER OTBD CORNER INWARD. REMOVED OLD FRAME, DRILLED AND INSTALLED NEW FRAME IAW SRM 51-40-02, SRM 51-40-05 AT STA 440.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 64,897 hrs · 42,043 cycles

LEFT INBD AFT FLAP OTBD UPPER AND LOWER SURFACES DELAMINATED. REPAIRED LT INBD AFT FLAP OTBD UPPER AND LWR SURFACES IAW SRM 51-70-10-2R-4, REPAIR 4. PERMANENT REPAIR.

Part: BEAR STRAP — CRACKED (BS 959-960) · airframe 64,612 hrs · 41,796 cycles

SUSPECT CRACK FWD OF L2 DOOR SILL APPROX BS 957. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AND BEAR STRAP IAW SRM 53-00-01-2R-32 REPAIR 32.

Part: FRAME — CRACKED (BS 500C) · airframe 62,390 hrs · 39,870 cycles

FRAME BS 500C HAS A CRACK .25 LONG EXTENDING I/B FROM EDGE OF THE 1.04 WIRE PENETRATION HOLE. FRAME REPAIRED IAW SRM 53-00-07.

Part: FRAME — CRACKED (BS 520) · airframe 62,390 hrs · 39,870 cycles

FRAME 520, RT SIDE HAS 2 CRACKS, 1 INBD BRACKET HOLE BETWEEN STR 8R AND 9R, AND 1 OTBD BRACKET HOLE ABOVE STR 8. ACFT GROUNDED. REPAIRED FRAME 520 RT IAW ASA EA AD20062609 400 53 131.

Part: SKIN — CHAFED (NR 3 SLAT) · airframe 62,390 hrs · 39,870 cycles

LT WING L/E NR 3 SLAT LOWER INBD T/E CHAFED THRU REPAIR DOUBLER. ACFT GROUNDED. REPAIRED NR 3 SLAT LWR INBD CORNER DAMAGE IAW SRM 51 70 10 PAR 20, PG 254, REP 4 PG 201.

Part: FLOOR SUPPORT — CRACKED · airframe 62,390 hrs · 39,870 cycles

LONGITUDINAL FLOOR SUPPORT RBL 24.5 UPPER CHORD CRACKED AT FS 664. REPAIRED LONGITUDINAL BEAM AT FS 664, RBL 24.5 IAW EA NR AD20080506-400-57-1-101.

Part: SKIN — CRACKED (BS 727D) · airframe 62,390 hrs · 39,870 cycles

LT FUSELAGE SKIN BS 727D HAS A CRACK .75 LONG BELOW STR 23L IN CHEM MILLED AREA. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01, FIG 201.

Part: FRAME — CRACKED (BS 500B) · airframe 62,390 hrs · 39,870 cycles

FRAME AT BS 500B RT SIDE HAS A CRACK .375 LONG EXTENDING INBD FROM EDGE OF THE 1.04 WIRE PENETRATION HOLE. ACFT GROUNDED. FRAME REPAIRED IAW SRM 53 00 07, REPAIR 13. THIS IS A CAT B REPAIR.

Part: SKIN — CHAFED (NR 3 SLAT) · airframe 62,390 hrs · 39,870 cycles

LT WING L/E NR 3 SLAT LOWER INBD T/E CHAFED. REPAIRED IAW SRM 51-70-10, PARA 20, PG 254, REP 4, PG 201.

Part: GUIDE ARM — WORN (L1 DOOR) · airframe 60,782 hrs · 38,435 cycles

L2 DOOR IS DIFFICULT TO OPEN. FOUND AFT ENTRY DOOR SNUBBER INOP. REPLACED SNUBBER REF AMM 52 13 71. FOUND GUIDE ARM AND DOWL PIN WORN. REPLACED GUIDE ARM REF AMM 52 13 31. ADJUSTED AFT ENTRY DOOR VERTICAL REF AMM 52 13 00 705 001 PERFORMED AFT ENTRY DOOR TEST, OPS CK NORMAL REF AMM 52 13 00 705 034.

Part: DOOR — LACK OF LUBE (L2) · airframe 60,479 hrs · 38,161 cycles

AFT ENTRY DOOR (L2) REPORTED "SQUEAKY" AND DIFFICULT TO OPERATE BY FLIGHT ATTENDANT CREW. INSPECTED AND LUBRICATED AFT ENTRY (L2) DOOR. OPS CHECK NORMAL. OK FOR SERVICE.

Part: SIGN — CRACKED (CABIN) · airframe 60,361 hrs · 38,051 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN CRACKED AND WILL NOT STAY IN PLACE. REPLACED L1 DOOR EMERGENCY EXIT SIGN.

Part: SKIN — DENTED (HORIZ STAB) · airframe 60,353 hrs · 38,043 cycles

DURING PREFLT W/A DAMAGED NOTED ON UNDERSIDE OF RT HORIZ STAB ABOUT 8" FROM ROOT. 2" AFT OF LEADING EDGE. DAMAGED AREA EST TO BE APPROX 6" LONG 3" WIDE & 1/2 TO 3/4" DEEP. DAMAGE DIMENSIONS = .044D X 6"L X 3" W STAB L/E STA 68 LOWER SIDE APPROX 4" DOWN FROM FWD EDGE (FIXED L/E). DENT IS OVER RIB OUT OF LIMITS REF SRM 55 10 01AO 1 PG 106 PAR (P). REPAIRED THE RT HORIZ STAB INBOARD FIXED L/E REF EA400 55EA 06749.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,174 hrs · 37,887 cycles

CRACK FOUND DURING MFEC RT STA 727D BELOW STR 23R. CUT OUT DAMAGED SECTION. REPAIRED CRACKED SKIN IAW B737 400 SRM 53 00 01 FIG 201 REPAIR 31.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,174 hrs · 37,887 cycles

R2 DOOR CUTOUT LOWER FWD CORNER EXTERNAL SKIN CRACKED. REPAIRED R2 DOOR CUTOUT LOWER EXTERNAL SKIN & BEAR STRAP IAW B737 400 SRM 53 00 01 FIG 201 REPAIR 32 DETAIL V.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,174 hrs · 37,887 cycles

BS 500G RT WIRE PENETRATION HOLE FOUND CRACKED AT INBD 9 O'CLOCK POSITION BETWEEN S 20R AND S 21 R GROUNDED YES. TRIMMED OUT DAMAGE FABRICATED REPAIR DOUBLERS AND INSTALLED IAW B737 400 SRM 53 00 07 REPAIR 13.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 60,025 hrs · 37,756 cycles

PHOTOLUMINESCENT TRACK LIGHT AT ROW 19C LOOSE. REPLACED APPROX 5 FT OF PHOTOLUMINESCENT FLOOR TRACK LIGHT FROM 17C, 19C.

Part: DOUBLER — CRACKED (FOREFLAP) · airframe 59,785 hrs · 37,539 cycles

LT WING I/B FOREFLAP HAS CRACKED REPAIR DOULBER ON UPPER SURFACE JUST O/B OF MIDSPAN. REPAIRED DAMAGE TO UPPER SURFACE AND CORE OF LT WING I/B FOREFLAP IAW B737 400 SRM 57 53 02 AND SRM 51 70 10.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,458 hrs · 37,257 cycles

RT INTERIOR OVERWING EXIT EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY IN CHARGER M1468 CHECKS GOOD REF MM 33 51 02.

Part: DOOR — DIRTY (L2) · airframe 58,206 hrs · 36,152 cycles

F/A REPORTS L2 DOOR HARD TO OPEN AND MAKES LOUD SQEAKING SOUND WHEN OPENING. CLEANED AND LUBRICATED DOOR, OPS CHECK GOOD.

Part: SLAT — DELAMINATED (NR 1) · airframe 57,368 hrs · 35,406 cycles

NR 1 SLAT L/E DELAMINATED I/B AFT CORNER. REMOVED DAMAGE, INSTALLED AND BONDED REPAIR DOUBLER.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 57,368 hrs · 35,406 cycles

NR 1 SLAT UPPER O/B AFT CORNER DELAMINATED. REMOVED DAMAGE AND INSTALLED REPAIR.

Part: SKIN — GOUGED (TE FLAP) · airframe 57,368 hrs · 35,406 cycles

RIGHT O/B MID FLAP INBOARD LEADING EDGE IS GOUGED. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER AND INSTALLED REPAIR.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 57,368 hrs · 35,406 cycles

SHEAR TIE DAMAGED WITH OVERSIZED HOLES. REMOVED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SKIN — CHAFED (FOREFLAP) · airframe 57,368 hrs · 35,406 cycles

LEFT O/B FORE FLAP OUTBOARD LOWER SKIN CHAFED. REMOVED REPAIR DOUBLER AND INSTALLED NEW DOUBLER.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 57,368 hrs · 35,406 cycles

STR 21R HAD DAMAGED OVERSIZED HOLES FROM STA 314 370. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 57,368 hrs · 35,406 cycles

SHEAR TIE DAMAGED WITH OVERSIZED HOLES. REMOVED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 57,368 hrs · 35,406 cycles

SHEAR TIE DAMAGED WITH OVERSIZED HOLES. REMOVED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 57,368 hrs · 35,406 cycles

SHEAR TIE DAMAGED WITH OVERSIZED HOLES. REMOVED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SKIN — CHAFED (LE SLAT) · airframe 57,368 hrs · 35,406 cycles

NR 4 SLAT LOWER TRAILING EDGE I/B END IS CHAFED. REMOVED DAMAGE, INSTALLED REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,368 hrs · 35,406 cycles

DENT AFT OF L2 DOOR BETWEEN STR 12L AND 13L IS WITHIN 3 INCHES OF SKIN BUTT SPLICE. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 57,368 hrs · 35,406 cycles

STR 22R HAD DAMAGED OVERSIZED HOLES FROM STA 320-360. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 57,368 hrs · 35,406 cycles

NR 2 SLAT INBOARD AFT CORNER IS DELAMINATED. REMOVED DAMAGED AREA, BONDED THE REPAIR.

Part: FRAME — GOUGED (FUSELAGE) · airframe 57,368 hrs · 35,406 cycles

AFT PIT FRAME GOUGED BETWEEN STR 24R 25R. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 57,368 hrs · 35,406 cycles

STR 20R HAD DAMAGED OVERSIZED HOLES FROM STA 320-360. REMOVED DAMAGED AREA, INSTALLED REPAIR.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 57,368 hrs · 35,406 cycles

NR 2 SLAT O/B AFT CORNER DELAMINATED. REMOVED PREVIOUS REPAIR AND INSTALLED NEW.

Part: SKIN — DENTED (SPOILER) · airframe 57,368 hrs · 35,406 cycles

LEFT NR 3 FLIGHT PANEL HAS A DENT ON LOWER SKIN. REPAIRED NR 3 SPOILER.

Part: LIMIT SWITCH — DEFECTIVE (RT MLG) · airframe 55,850 hrs · 34,093 cycles

RIGHT MAIN SECONDARY GEAR ILLUMINATED INDICATING TR MAIN GEAR DOWN WITH LANDING GEAR LEVER SELECTED UP AFTER TAKEOFF. REPLACED RT MLG SECONDARY WARNING SWITCH.

Part: SHEAR TIE — DAMAGED (BS 420) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO BAY DAMAGED SHEAR TIE IN. REMOVED DAMAGED SHEAR TIE FABRICATED REPAIR PARTS AND INSTALLED.

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 54,119 hrs · 32,562 cycles

SKIN AT AFT CARGO DOOR DENTED. REMOVED AND REPLACED AFT CARGO DOOR SKIN IAW SRM.

Part: SHEAR TIE — DAMAGED (BS 380) · airframe 54,119 hrs · 32,562 cycles

DAMAGED SHEAR TIE IN FWD CARGO BAY. REMOVED DAMAGED SHEAR TIE FABRICATED REPAIR PARTS AND INSTALLED.

Part: SKIN — DENTED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

AIRCRAFT DENTED AT FWD CARGO DOOR. REMOVED AND REPLACED DENTED SKIN PANEL AT FWD CARGO DOOR.

Part: BEAR STRAP — MISREPAIRED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

L1 UPPER HINGE CUTOUT REPAIR REQUIRES REPLACEMENT WITH APPROVED REPAIR. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR PARTS AND INSTALLED.

Part: SUPPORT BEAM — WORN (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

LT RAM AIR INLET DUCT UPPER AFT O/B SUPPORT BRACKET WORN BS 570. REPLACED BRACKET.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FRAME DAMAGED BS 727D STR 8L IAW EA 400-53EA-00717. FABRICATED REPAIR PARTS AND INSTALLED.

Part: STRUCTURE — CRACKED (ELEVATOR) · airframe 54,119 hrs · 32,562 cycles

LT ELEVATOR CRACKED UNDER PANEL 9142 ON I/B LEADING EDGE. REMOVED AND INSTALLED ROBBED ELEVATOR PER 27 31 11 404 025.

Part: DOOR FRAME — CHAFED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD ENTRY DOOR AFT EDGE FRAME TOP CORNER IS CHAFED. REPAIRED IAW.

Part: STRAP — CRACKED (BS 312) · airframe 54,119 hrs · 32,562 cycles

STABILIZER STRAP CRACKED. REPAIRED STABILIZER STRAP.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMPARTMENT INTERCOSTAL CRACKED. REMOVED & REPLACED INTERCOSTAL PER SRM 51 40 02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMPARTMENT INTERCOSTAL CRACKED. REMOVED & REPLACED INTERCOSTAL PER SRM 51 40 02.

Part: BEAM — CRACKED (PAX DOOR) · airframe 54,119 hrs · 32,562 cycles

FWD ENTRY DOOR LOWER GATE BEAM CRACKED BEYOND STOP DRILL. REPAIRED LOWER GATE BEAM PER SRM 51 70 11.

Part: SUPPORT — PUNCTURED (CARGO BAY) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMP LT FLOOR TO SIDEWALL SUPPORT IS PUNCTURED. REMOVED SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED PER SRM 51 40 02.

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO BAY INTERCOSTALS BENT LBL 24.20 (9 EACH). REPLACED WITH NEW PARTS PER SRM 51 30 01 AND DWG 69 41473.

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO BAY INTERCOSTAL BENT. REPLACED INTERCOSTAL PER SRM 51 30 01 AND DWG 69 18388.

Part: RIB — CHAFED (LT WING) · airframe 54,119 hrs · 32,562 cycles

LT WING T/E RIB IS CHAFED ON LOWER SURFACE OF UPPER FLANGE. BLENDED AND TREATED CHAFED AREA PER EA 400 57EA 00956. RE-INSPECTION WITHIN 24 MONTHS.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMPARTMENT INTERCOSTAL CRACKED. REMOVED INTERCOSTAL, FABRICATED NEW INTERCOSTAL AND INSTALLED PER SRM 51 40 02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMPT BS 500E TO 500F WL 150 RBL 20 INTERCOSTAL CRACKED AT BOTH ENDS. REMOVED AND REPLACED INTERCOSTAL IAW SRM 57 40 02.

Part: SKIN — CORRODED (BS 340-360) · airframe 54,119 hrs · 32,562 cycles

SEVERAL SMALL AREAS OF CORROSION AROUND BELLY DRAINS AT LOWER FUSELAGE BS 360 BETWEEN STA 24L AND 24R. CORROSION FOUND TO BE IN LIMITS ALODINED AND PRIMED.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

WX RADAR R/T UNIT LT SUPPORT CHANNEL CRACKED. REMOVED AND REPLACED CHANNEL PER SRM 51-40-02.

Part: SKIN — CORRODED (AC BAY DOOR) · airframe 54,119 hrs · 32,562 cycles

GROUND AIR CONDITIONING ACCESS DOOR EXTERNAL SKIN PILLOWING AND INTERNAL SKIN CORRODED. REPLACED GROUND AIR CONDITIONING ACCESS DOOR PER SRM 51 40 02.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 54,119 hrs · 32,562 cycles

LT WING I/B TRAILING NO STEP PANEL O/B SUPPORT ANGLE IS CRACKED. REPLACED SUPPORT ANGLE (FITTING) PER SRM 51 40 02.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FLOORBEAM WHERE SEAT TRACK ATTACHES AFT FASTENER HOLE IS A DOUBLE HOLE. REPAIRED FLOORBEAM AT BS 727D.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

SUPPORT ANGLE ABOVE ANTI COLLISION LIGHT CORRODED. REPLACED SUPPORT ANGLE PER SRM 51-40-02 AND DWG 65-45866.

Part: SUPPORT ANGLE — DAMAGED (LT WING) · airframe 54,119 hrs · 32,562 cycles

LT WING T/E CAVITY NO STEP PANEL I/B ANGLE AFT FASTENER HOLE IS OUT OF ROUND. REPLACED SUPPORT ANGLE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

SEAT TRACK BS 727B 800 LBL 24 HAS NUMEROUS AREAS OF MECHANICAL DAMAGE AND OR CORROSION OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK BS 727B 927 LBL 24.

Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

CORROSION ON NR 4 FLAP TRACK. REMOVED AND REPLACED FLAP TRACK.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

INTERCOSTAL CRACKED. REMOVED FABRICATED NEW AND INSTALLED INTERCOSTAL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

SEAT TRACK CORROSION OUT OF LIMITS BS 727B 840. REMOVED AND REPLACED SEAT TRACK.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

ANGLE REVEAL DOUBLER TORN BS 312 STR 10L 11L. REMOVED AND INSTALLED NEW ANGLE REVEAL DOUBLER BS 312 STR 10L 11L PER SRM 51 40 02.

Part: DOUBLER — TORN (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

ANGLE REVEAL DOUBLER TORN BS 312 STR 10L 11L. REMOVED AND INSTALLED NEW ANGLE REVEAL DOUBLER BS 312 STR 10L 11L PER SRM 51 40 02.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

WHILE REPLACING BOLTS ON 1016 BULKHEAD FOUND STR 27 LT TO HAVE DAMAGE.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO DOOR CUTOUT AFT FRAME HAS AN OUT OF ROUND HOLE RBL 26 WL 156. REMOVED AND REPLACED FRAME PER DWG 69-18202 AND SRM 51-40-02.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

BS 294 FLOORBEAM REINFORCEMENT ANGLE HAS A FACTORY HOLE NEXT TO A PILOT HOLE CREATING A DOUBLE HOLE. REMOVED AND REPLACED ANGLE PER SRM 51-40-02, 51-40-05 AND DWG 65C33940.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

INTERCOSTAL CORRODED AT BS 959. REMOVED AND REPLACED INTERCOSTAL.

Part: STRAP — CRACKED (GALLEY DOOR) · airframe 54,119 hrs · 32,562 cycles

FWD GALLEY DOOR AFT STRAP CRACKED AT LOWER STOP FITTING ATTACH BOLT. REPAIRED FWD GALLEY DOOR AFT STRAP.

Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

CORROSION ON RIGHT I/B FLAP LEADING EDGE. REPAIRED LEADING EDGE.

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 54,119 hrs · 32,562 cycles

LEFT O/B AFT FLAP LOWER AFT SKIN IS DISBONDED AT I/B AFT CORNER. LEFT O/B AFT FLAP LWR AFT SKIN DISBOND WAS REPAIRED PER SRM.

Part: BEAM — CRACKED (GALLEY DOOR) · airframe 54,119 hrs · 32,562 cycles

FWD GALLEY DOOR LOWER GATE BEAM CRACKED 3 INCHES FWD OF AFT FRAME 1 INCH O/B OF INNER SKIN. REMOVED AND REPLACED LOWER GATE BEAM.

Part: FRAME — ACTIVATED (BS 500G) · airframe 54,119 hrs · 32,562 cycles

OUT OF ROUND HOLE ON FRAME UPPER FLANGE. REMOVED DAMAGE FROM FRAME, FABRICATED REPAIR PARTS AND INSTALLED.

Part: SILL — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

L2 MOP SILL IS CORRODED. REPLACED MOP SILL PER SRM 51-40-02 AND DWG 65-52878.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

OUT OF ROUND HOLES THROUGH STRINGER. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-00-53.

Part: SKIN — CHAFED (LE SLAT) · airframe 54,119 hrs · 32,562 cycles

NR 5 SLAT I/B TRAILING EDGE LOWER SURFACE IS CHAFED AT PREVIOUS REPAIR. REMOVED AND REPLACED REPAIR.

Part: SKIN — DEBONDED (MIDFLAP) · airframe 54,119 hrs · 32,562 cycles

RIGHT I/B MID FLAP TRAILING EDGE WEDGE LWR SKIN IS DISBONDED 30 INCHES FROM O/B END AND 6 INCHES FWD OF AFT EDGE. REPAIRED RIGHT I/B MID FLAP TRAILING EDGE WEDGE LWR SKIN IS DISBONDED 30 INCHES FROM O/B END AND 6 INCHES FWD OF AFT EDGE.

Part: SKIN — DEBONDED (MIDFLAP) · airframe 54,119 hrs · 32,562 cycles

LEFT I/B MID FLAP TRAILING EDGE WEDGE LWR SKIN IS DISBONDED 44 INCHES FROM I/B END AND 5 INCHES FWD OF AFT EDGE. REPAIRED LT IB MID FLAP TRAILING EDGE WEDGE LWR SKIN IS DISBONDED 44 INCHES FROM IB END AND 5 INCHES FWD OF AFT EDGE. PER SRM 51 70 10.

Part: SKIN — GOUGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FUSELAGE SKIN DAMAGED. REPAIRED PER ER 09-2021 & EA 800-53EA-00963.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,966 hrs · 32,029 cycles

NUMEROUS AREAS OF CORROSION/MECH DAMAGE TO SEAT TRACK. REMOVED AND REPLACED SEAT TRACK.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMPARTMENT OPEN HOLE IN FWD EDGE OF FRAME UPPER CHORD. REPAIRED PER ER 09-1754-EA-400-53EA-00971.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

MAIN CARGO DOOR LOWER FRAME SUPPORT HAS MULTIPLE DRILL STARTS AND A HOLE DRILLED THROUGH RADIUS. REMOVED DAMAGED SECTION OF FRAME, FABRICATED REPAIR PARTS AND INSTALLED PER EA 400-53EA-00971.

Part: SKIN — DEBONDED (MIDFLAP) · airframe 54,119 hrs · 32,562 cycles

RIGHT I/B MID FLAP TRAILING EDGE WEDGE LWR SKIN HAS DENT WITH DISBOND 50 INCHES FROM O/B END AND 4 INCHES FWD OF AFT EDGE. REPAIRED RIGHT I/B MID FLAP TRAILING EDGE WEDGE LWR SKIN 50 INCHES FROM O/B END AND 4 INCHES FWD OF AFT EDGE.

Part: INTERCOSTAL — GOUGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

INTERCOSTAL STA 480 520 STR 25L HAS A CUT MARK THROUGH UPPER RADIUS. FABRICATED AND REPLACED.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

NUMEROUS AREAS OF CORROSION AND OR MECHANICAL DAMAGE TO SEAT TRACK SEGMENT BS 727B-907 RBL 24. REMOVED AND REPLACED SEAT TRACK.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

CORROSION ON STRINGER CLIP BS 867 S26L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

CORROSION ON STRAP. REMOVED AND REPLACED STRAP PER SRM 53-60-51.

Part: BRACKET — CRACKED (LE SLAT) · airframe 54,119 hrs · 32,562 cycles

NR 6 SLAT ACTUATOR LOWER ATTACH PANEL FWD BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET.

Part: SKIN — CHAFED (MIDFLAP) · airframe 54,119 hrs · 32,562 cycles

RIGHT O/B MID FLAP LWR AFT SKIN LWR SURFACE IS CHAFED 13 INCHES O/B OF NR 1 AFT TRACK ON DOUBLER. REPAIRED CHAFED AREA.

Part: ANGLE — TORN (LT WING) · airframe 54,119 hrs · 32,562 cycles

ANGLE AT RSS 272 WBL 201 IS TORN LT WING. REPLACED ANGLE.

Part: SKIN — CHAFED (MIDFLAP) · airframe 54,119 hrs · 32,562 cycles

RIGHT O/B MID FLAP LWR AFT SKIN LWR SURFACE IS CHAFED AT NR 4 AFT FLAP TRACK. OUT OF LIMITS. DAMAGE WAS REMOVED 1" X 1.5" X .032 REPAIRED PER SRM.

Part: SKIN — CHAFED (MIDFLAP) · airframe 54,119 hrs · 32,562 cycles

RIGHT O/B MID FLAP LWR AFT SKIN UPPER SURFACE IS CHAFED AT NR 3 AFT FLAP TRACK. OUT OF LIMITS. DAMAGE WAS REMOVED 1" X 2" X .032 REPAIRED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FUSELAGE SKIN PREVIOUSLY BLENDED AREAS OUT OF LIMITS. REMOVED DAMAGED SKIN AND INSTALLED REPAIR.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

BS 480 RBL 62 LATERAL TRACK HAS EXTREME WEAR. REPLACED LATERAL TRACK PER SRM 51-40-02.

Part: SPAR — CRACKED (MIDFLAP) · airframe 54,119 hrs · 32,562 cycles

LEFT I/B MID FLAP REAR SPAR UPPER CHORD IS CRACKED AT FOUR LOCATIONS NEAR I/B AND O/B NUT PLATE. REMOVED AND REPLACED LEFT I/B MID FLAP REAR SPAR UPPER CHORD PER DWG 65 47841 AND SRM 51 40 02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

CORROSION AFT CARGO BAY WEB IS CORRODED BETWEEN BS 767 787 RBL 22.5. REMOVED AND REPLACED AFT CARGO BAY WEB.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

STRINGER CLIP CRACKED BS 500G STR 26R. REMOVED AND REPLACED STRINGER CLIP.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

CRACKED STRINGER SPLICE STA 907 STR 4R. REMOVED AND REPLACED STRINGER SPLICE.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

STRINGER CLIP CRACKED BS 500G STR 26R. REMOVED AND REPLACED STR CLIP.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

CORROSION ON AFT CARGO BAY LOWER AFT FLANGE OF FRAME ANGLE. REMOVED AND REPLACED FRAME ANGLE.

Part: STOP FITTING — SCRATCHED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO DOOR STOP PIN FITTING AT AFT BOTTOM CORNER IS SCRATCHED. REPAIRED PER ATS ER 09 1826 AND ASA 800 52EA 00790 BY BLENDING AREA AND RE-APPLYING PROTECTIVE FINISH.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMPARTMENT CORROSION ON SHEAR TIE. REMOVED DAMAGED SHEAR TIE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-00-07 REPAIR 3.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMPARTMENT DRILL START ON FRAME. REPAIRED PER ER 09-1870 & EA 400-53EA-00989.

Part: WEB — WORN (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

OUTBOARD WALL OF RT RAM AIR INLET HAS 2 AREAS OF WEAR CAUSED BY BULB SEALS. REPAIRED O/B WALL OF RT RAM AIR INLET.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMP INTERCOSTAL ATTACH BRACKET CRACKED. REMOVED BRACKET, FABRICATED NEW BRACKET AND INSTALLED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

GOUGE IN FUSELAGE EXTERNAL SKIN. REPAIRED SKIN PER SRM 53-00-01 REPAIR 31.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

SHEAR WEB BS 1016+4 RBL 25 WL 208. REMOVED AND REPLACED SHEAR WEB PER SRM 51-40-02.

Part: SEAT TRACK — DAMAGED (BS 727-727B) · airframe 54,119 hrs · 32,562 cycles

MECHANICAL DAMAGE ON SEAT TRACK. REPLACED SEAT TRACK.

Part: SEAT TRACK — DAMAGED (BS 727-727B) · airframe 54,119 hrs · 32,562 cycles

MECHANICAL DAMAGE ON SEAT TRACK. REPLACED TRACK.

Part: FRAME — CRACKED (BS 827) · airframe 54,119 hrs · 32,562 cycles

FRAME CRACKED AT I/B FASTENER HOLE FOR A/C BRACKET. REPAIRED CRACKED FRAME.

Part: BEAM — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

LONGITUDINAL BEAM CORNER CRACKED. REPAIRED CRACKED LONGITUDINAL BEAM PER EA 400-53EA-00978.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

MECHANICAL DAMAGE ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK.

Part: SEAT TRACK — DAMAGED (BS 727-727B) · airframe 54,119 hrs · 32,562 cycles

MECHANICAL DAMAGE ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK.

Part: BRACKET — GOUGED (BS 767) · airframe 54,119 hrs · 32,562 cycles

AFT CARGO BAY BRACKET AT I/B OF CARGO GOUGED. REMOVED AND REPLACED BRACKET WITH FABRICATED BRACKET.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

FWD CARGO SHEAR TIE CORROSION OUT OF LIMITS BS 500 WL 148 STR 27R. REMOVED DAMAGED SHEAR TIE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-00-07 REPAIR 3.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

NOSE GEAR VIEWER SUPPORT BRACKET IS CRACKED AT BS 260 RBL 4. REMOVED AND REPLACED NOSE GEAR VIEWER SUPPORT BRACKET.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

FWD CARGO SHEAR TIE CORROSION OUT OF LIMITS BS 500 WL 148 STR RBL 5 LBL 5. REMOVED DAMAGED SHEAR TIE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-00-07 REPAIR 3.

Part: SEAT TRACK — CRACKED (BS 540-730) · airframe 54,119 hrs · 32,562 cycles

SEAT TRACK BS 520-730 RBL 43 CORROSION AND MEC DAMAGE OUT OF LIMITS. REPLACED TRACK.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

AFT CARGO FLOOR RT SUPPORT ZEE ELONGATED HOLES OUT OF LIMITS BS 847-947 RBL 22 WL 156. FLOOR TO SIDEWALL SUPPORT PLATE REMOVED AND REPLACED BS 867-947.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

L1 DOOR LOWER HINGE CRACK INDICATION AT OPEN HOLE IN BEAR STRAP. REPAIRED L1 DOOR LOWER HINGE.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

BS 1116 RBL 24 LOWER CHORD IS CORRODED. REMOVED AND REPLACED LOWER CHORD.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO BULKHEAD SUPPORT BS 500G WL 160 STR LBL 34 CORROSION OUT OF LIMITS. REMOVED AND REPLACED SUPPORT PER SRM 53-30-53 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

AFT CARGO RT SUPPORT ZEE CORROSION OUT OF LIMITS BS 867-947 RBL 22 WL 156. REMOVED AND REPLACED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 54,119 hrs · 32,562 cycles

AFT CARGO FLOOR SUPPORT CORROSION OUT OF LIMITS BS 812 LBL 3 WL 156. REPAIRED BY REPLACING SUPPORT ANGLES PER SRM 53-00-53.

Part: WEB — CORRODED (BS 847) · airframe 54,119 hrs · 32,562 cycles

AFT CARGO WEB CORROSION OUT OF LIMITS BS 867 RBL 22 WL 156. REPLACED WEB.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

FWD CARGO SHEAR TIE CORROSION OUT OF LIMITS BS 500D WL 148 RBL 4. REMOVED DAMAGED SHEAR TIE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-00-07.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

CORROSION ON FLOORBEAM AT BS 270 RBL 10 LBL 10 WL 207. REMOVED UPPER ZEE CHORD, FABRICATED & INSTALLED NEW ZEE CHORD PER SRM 51-40-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

BS 1126 RBL 24 WL 230 APU COMPARTMENT TEE CHORD IS CORRODED. REMOVED AND REPLACED TEE CHORD.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMPARTMENT DRILL START IN FRAME. REPAIRED PER SRM 51-70-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

AFT CARGO FLOOR SUPPORT CORROSION OUT OF LIMITS BS 823 RBL 3 WL 156. REPAIRED BY REPLACING SUPPORT ANGLES PER SRM 53-00-53.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

UPPER CHORD CORRODED BS 1116 RBL 24 WL 238 APU COMPARTMENT. REMOVED AND REPLACED UPPER CHORD.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

FWD CARGO SHEAR TIE CORROSION OUT OF LIMITS BS 500 WL 148 STR BL 0. REMOVED DAMAGED SHEAR TIE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-00-07 REPAIR 3.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

AFT CARGO SUPPORT CORROSION OUT OF LIMITS BS 832 LBL 22 WL 156. REMOVED AND REPLACED ZEE FROM BS 817-947.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

NUMEROUS AREAS OF CORROSION/DAMAGE ON SEAT TRACK SEGMENT BS 540 727 LBL 23. REMOVED AND REPLACED SEAT TRACK.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

SEAT TRACK BS 540 727 LBL 44 CORROSION AND MEC DAMAGE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-52.

Part: WEB — GOUGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO BAY CLOSE OUT WEB GOUGED OUT OF LIMITS PER SRM 53-30-15. REMOVED CLOSE OUT WEB, FABRICATED NEW WEB AND INSTALLED PER SRM 53-30-15 AND 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

SEAT TRACK BS 480-520 LBL 23 CORROSION/ MECHANICAL DAMAGE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK.

Part: SEAT TRACK — DAMAGED (BS 727B-907) · airframe 54,119 hrs · 32,562 cycles

SEAT TRACK BS 727B 907 RBL 45 CORROSION/ MECHANICAL DAMAGE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

CORROSION OUT OF LIMITS AFT CARGO BAY WEB BS 847 867 RBL 22 PER SRM 50-60-53. REMOVED AND REPLACED WEB.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

CORROSION AFT CARGO BAY LOWER AFT FLANGE OF FRAME AT BODY STA 767 RBL 11.5. REPLACED FRAME FLANGE (ANGLE) PER SRM 53-60-08, 51-40-02 AND 51-40-05.

Part: SUPPORT ANGLE — CRACKED (FAIRING) · airframe 54,119 hrs · 32,562 cycles

UPPER AFT SUPPORT ANGLE CRACKED (WING TO BODY FAIRING SUPPORTS) RT SIDE OF RAM AIR INLET. REMOVED DAMAGED SECTION, FABRICATED SPLICE PARTS.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

AREAS CORROSION ON INNER CREASE BEAM LT SIDE BS 500C-520. REMOVED AND REPLACED CREASE BEAM.

Part: SUPPORT ANGLE — CRACKED (FAIRING) · airframe 54,119 hrs · 32,562 cycles

UPPER AFT SUPPORT ANGLE CRACKED (WING TO BODY FAIRING SUPPORTS) BS 540 LT SIDE OF RAM AIR INLET. REMOVED DAMAGED SECTION, FABRICATED SPLICE PARTS.

Part: SEAT TRACK — CORRODED (BS 480-520) · airframe 54,119 hrs · 32,562 cycles

NUMEROUS AREAS OF CORROSION AND MECHANICAL DAMAGE ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

BS 986 STR 76 FRAME IS CRACKED AT STRINGER CUTOUT. REPAIRED PER EA 400-53EA-00968.

Part: WEB — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

LT WEB STA 986-1016 LBL 44 CORRODED. REMOVED AND REPLACED WEB PER SRM 53-60-53.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

STR 6R CLIP CRACKED BS 601. REMOVED CRACKED CLIP, INSTALLED NEW CLIP PER ASA DWG A53100265816 AND SRM 51 40 02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

CORROSION AFT CARGO BAY AFT BULKHEAD PANEL LOWER CENTER SUPPORT. REMOVED SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED PER SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

STR 5R CLIP CRACKED BS 578. REMOVED CRACKED STR 5R CLIP, INSTALLED NEW PER ASA DWG A53100265823 AND SRM 51 40 02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

STR 5L CLIP CRACKED BS 578. REMOVED CLIP, INSTALLED NEW CLIP PER ASA DWG A53100265823 AND SRM 51 40 02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

CORROSION AFT CARGO BAY FLOOR SUPPORT STA 807+16 RBL 3. REPAIRED FLOOR.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

R2 DOOR MOP SILL CREASE BEAM CORRODED. REMOVED AND REPLACED R2 MOP SILL.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMPARTMENT ANTENNA SUPPORT CHANNEL CRACKED AND CORRODED. REMOVED, FABRICATED NEW CHANNEL AND INSTALLED.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

AFT CARGO BAY CORROSION ON FLOOR TO SIDEWALL SUPPORT. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: SUPPORT — CORRODED (BS 500D-500G) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT HAS CORROSION. REMOVED SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

CORROSION AFT CARGO BAY RT SUPPORT ZEE CHANNEL. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: SUPPORT — CORRODED (CARGO BAY) · airframe 54,119 hrs · 32,562 cycles

CORROSION ON AFT CARGO BAY FLOOR SUPPORT. REPAIRED AFT CARGO FLOOR SUPPORT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMPARTMENT BS 500F STR 25L STRINGER CLIP IS CRACKED. REPLACED STR CLIP.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

AFT CARGO BAY LT SUPPORT ZEE HAS NUMEROUS ELONGATED FASTENER HOLES BETWEEN STA 847 AND 947. REMOVED, FABRICATED NEW AND INSTALLED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMPARTMENT BS 500G STR 26R STRINGER CLIP IS CRACKED. REMOVED AND REPLACED STRINGER CLIP.

Part: SUPPORT — CORRODED (BS 727C-727G) · airframe 54,119 hrs · 32,562 cycles

AFT CARGO BAY CORROSION ON FLOOR TO SIDEWALL SUPPORT. REPLACED SUPPORT.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

CORROSION AFT CARGO BAY LT SUPPORT ZEE. REMOVED, FABRICATED NEW AND INSTALLED.

Part: SUPPORT — CORRODED (BS 500A-500G) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT HAS CORROSION. REMOVED SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

BS 986 FLOORBEAM UPPER CAP CORRODED. REPAIRED FLOORBEAM PER ER 09-1817-EA-400-53EA-00969.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

CORROSION ON FLOORBEAM. REMOVED TOP CHORD OF FLOORBEAM, FABRICATED REPAIR PARTS AND NEW TOP CHORD AND INSTALLED PER SRM 53-10-51.

Part: SKIN — DENTED (BS 1001) · airframe 54,119 hrs · 32,562 cycles

FUSELAGE SKIN HAS DENT 15 INCHES AFT OF AFT SERVICE DOOR CUTOUT. REMOVED AND REPLACED FUSELAGE SKIN.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FLOOR SUPPORT CORRODED AT SPLICE REPAIR. REPAIRED FLOOR SUPPORT PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

L1 DOOR MOP SILL CREASE BEAM CORRODED. REMOVED AND REPLACED MOP SILL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

CORROSION ON FLOORBEAM. REMOVED UPPER CHORD AND INSTALLED REPAIR CHORD SECTION AND SPLICES.

Part: SUPPORT — CORRODED (CARGO BAY) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO BAY SIDEWALL SUPPORT HAS CORROSION. REMOVED SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED PER SRM 51-40-02.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,119 hrs · 32,562 cycles

R1 DOOR CREASE BEAM CORRODED. REMOVED AND REPLACED CREASE BEAM PER SRM 51-40-02.

Part: SUPPORT — CORRODED (CARGO BAY) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO BAY SIDEWALL SUPPORT HAS CORROSION. FABRICATED NEW SUPPORT AND INSTALLED PER SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

AFT CARGO BAY CORROSION ON FLOOR TO SIDEWALL SUPPORT. REMOVED, FABRICATED NEW AND INSTALLED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

SKIN GOUGED AT AND BELOW LAP. REMOVED AND REPLACED SKIN.

Part: SUPPORT — PUNCTURED (BS 500B) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT PUNCTURED. FLOOR TO SIDEWALL SUPPORT PLATE REMOVED AND REPLACED STA 500A-500G.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

FWD CARGO BAY SIDEWALL SUPPORT ANGLE HAS CORROSION. REMOVED SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED.

Part: WEB — CORRODED (BS 986-1016) · airframe 54,119 hrs · 32,562 cycles

WEB CORRODED BS 986-1016. REPLACED WEB.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 54,119 hrs · 32,562 cycles

NUMEROUS AREAS OF CORROSION AND OR MECHANICAL DAMAGE TO SEAT TRACK SEGMENT BS 727B 907 RBL 24. REMOVED AND REPLACED SEAT TRACK.

Part: SHEAR TIE — CORRODED (BS 520) · airframe 52,642 hrs · 33,555 cycles

FWD CARGO BAY SHEAR TIE CORRODED AT STA 520 BETWEEN STA 28R AND 28L. REMOVED DAMAGED SHEAR TIE, FABRICATED, LOCATED, DRILLED AND INSTALLED REPLACEMENT SHEAR TIE IAW B737 400 SRM 51 40 02 PG 2 4 AND DRW 65 46534.

Part: SKIN — DENTED (FUSELAGE) · airframe 51,782 hrs · 30,433 cycles

LOWER FUSELAGE DENTED STA 7270+13. DENT REPAIRED AT STA 7270+13 IAW B737 400 SRM 53 00 01 REPAIR 31.

Part: LINK — BROKEN (L1 DOOR) · airframe 51,517 hrs · 30,189 cycles

L1 DOOR IS DIFFICULT TO CLOSE. NOT A SMOOTH ACTION, FEELS LIKE IT CATCHES ON SOMETHING. FOUND RADIUS LINK BROKEN. REPLACED LINK ASSY & SNUBBER. NO HELP, DOOR STILL HARD TO CLOSE. ADJUSTED L1 GUIDE ARM. DOOR OPERATES NORMALLY.

Part: TORQUE SHAFT — BINDING (LT WING TE FLAPS) · airframe 51,312 hrs · 30,015 cycles

FLAPS WOULD NOT EXTEND BEYOND 9 + 1. FLAPS WERE SYMMETRICAL BUT DID NOT AGREE WITH FLAP HANDLE COMMAND TO 15DEGS. FLAP WOULD NOT MOVE USING "ALT FLAPS". OPS FROM QRC EMERGENCY DECLARED. DIVERTED TO KTN. FOUND LT WING INBD FLAP MID FLAP TORQUE SHAFT DOOR BINDING AND RESTRICTING FLAP MOVEMENT. RELEASED PER CDL 57 53 1. LT INBD MID FLAP TORQUE SHAFT CLEARANCE DOOR REMOVED.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 51,278 hrs · 29,983 cycles

L1 DOOR IS DIFFICULT TO CLOSE. LENGTHENED FWD ENTRY DOOR GUIDE ARM (REF AMM52 11 00). LATCH OP CHECKS OK THIS DATE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,100 hrs · 28,042 cycles

INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,100 hrs · 28,042 cycles

STRINGER 7L INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW SRM 51-40-02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 49,100 hrs · 28,042 cycles

STRINGER 16L STRAP ON INTERCOSTAL BROKEN. REPLACED STRAP IAW SRM 53-10-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,100 hrs · 28,042 cycles

FRAME CRACKED. REPAIRED CRACKED FRAME IAW SRM 53-00-07 FIG 201.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,100 hrs · 28,042 cycles

FRAME CRACKED. REPAIRED FRAME IAW SRM 53-00-07 FIG 201.

Part: INTERCOSTAL — CRACKED (BS 294-303) · airframe 49,100 hrs · 28,042 cycles

INTERCOSTAL CRACKED. REPLACED INTERCOSTAL PER SRM 51-40-01 AND 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,100 hrs · 28,042 cycles

INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,100 hrs · 28,042 cycles

STRINGER CLIP CRACKED. REPLACED CLIP IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,100 hrs · 28,042 cycles

SHEAR TIE CRACKED REPLACED SHEAR TIE IAW SRM 51-40-02.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 49,100 hrs · 28,042 cycles

AFT CARGO AFT FRAME EXISTING REPAIRS INSTALLED. REPLACED EXISTING REPAIR FRAME IAW SRM 51-40-02.

Part: SLIDE — TWISTED (R1 DOOR) · airframe 48,350 hrs · 27,615 cycles

R 1 DOOR EMERGENCY SLIDE ON ACFT 762 TWISTED ON DEPLOYMENT. SLIDE FULLY INFLATED BUT WAS UNUSEABLE DUE TO THE MANOR IN WHICH IT DEPLOYED. REPLACED SLIDE AND OPENED DOOR FASTER.

Part: WIRE — SHORTED (FIRE WARNING) · airframe 46,261 hrs · 26,490 cycles

MOMENTARY APU FIRE INDICATION WITH APU NOT RUNNING DURING CRUSE FLIGHT. FOUND WIRE TO APU TAIL PIPE OVERHEAT DETECTOR RUBBING AND SHORTING TO APU COWLING. TEMPORARY REPAIR DONE TO WIRE AND REPOSITIONED PER SWPM 20 10 13 PG 122.

Part: SKIN — BIRD STRIKE (FUSELAGE)

OKC - FOUND FUSELAGE SKIN L/E NEAR RADOME SEAM RIGHT SIDE DAMAGED FROM BIRD STRIKE. TEMPORARY REPAIR INSTALLED, REF EM 5330-02004. REMOVED EXISTING TEMPORARY REPAIR. FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW ASA EA 5310-02519. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - FUSELAGE SKIN DENTED IN FIVE LOCATIONS BETWEEN BS 360-368, AT STRINGER 16-18 LEFT. CUT OUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED A REPAIR DOUBLER, TRIPLER AND FILLER IAW ASA EA 5330-02022. (M)

Part: SKIN — DENTED (FUSELAGE)

FOUND FUSELAGE SKIN DENT OUT OF LIMITS AT BS 246, 5 INCHES BELOW AND 5 INCHES AFT OF THE EXTERNAL POWER RECEPTACLE. CUT OUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED A REPAIR DOUBLER, TRIPLER AND FILLER IAW B737-400 SRM 53-00-01 FIGURE 201 REPAIR 31 AND ASA EA 5330-02018. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DENT IN FUSELAGE SKIN BETWEEN STRINGER 20R-21R, BS 294-296. TEMPORARY REPAIR INSTALLED. REMOVED EXISTING REPAIR, CUTOUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED A REPAIR DOUBLER, TRIPLER, FILLERS AND TWO TEAR STRAP INTERNAL DOUBLERS IAW B737-400 SRM 53-00-01, FIG 201, AND REPAIR 31. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - FOUND FUSELAGE SKIN DENTED OUT OF LIMITS ON EITHER SIDE OF STRINGER 27 LEFT AT BS 853-855. DAMAGE IS ADJACENT TO AN EXISTING REPAIR AT BS 837-850 STRINGER 226 RT-27 RT. REMOVED DAMAGED AREA OF SKIN, REMOVED EXISTING REPAIR DOUBLER. FABRICATED AND INSTALLED A REPAIR DOUBLER, TRIPLER AND FILLER IAW B737-400 SRM 53-00-01, FIG 201, AND REPAIR 31. (M)

Part: SKIN — DAMAGED (FUSELAGE)

OKC - FUSELAGE SKIN EXTERIOR DAMAGE REMOVAL OUT OF LIMITS AT BS 868, 1 INCH BELOW STRINGER 21 RT. CUT OUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED A REPAIR DOUBLER, TRIPLER, AND FILLERS PER B737-400 SRM 53-00-01, FIG 201, AND REPAIR 31. (M)

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: DOOR FRAME — DENTED (FUSELAGE)

AFT CARGO DOOR CUT OUT, AFT FRAME WEB BENT. ACCOMPLISHED REPAIR IAW EA ON AFT FRAME.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT LT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: FLOORBEAM — DAMAGED (FUSELAGE)

OVERSIZED HOLES IN LOWER FLANGE OF FLOORBEAM. REPAIRED FLOORBEAM.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

CORRODED SHEAR TIE. REPAIRED WITH DOUBLER.

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

CORRODED INNER SKIN AFT OF AFT CARGO DOOR. REMOVED CORROSION AND INSTALLED DOUBLER.

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

CORROSION ON INNER SKIN FORWARD OF AFT CARGO DOOR. REMOVED DAMAGE, INSTALLED DOUBLER.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT RT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,473 hrs · 23,874 cycles

STRINGER 4L CRACKED AT FASTENER. REPLACED STRINGER SPLICE AND CLIP.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT RT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT LT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: SKIN — GOUGED (FUSELAGE)

GOUGES IN SKIN. BLENDED GOUGED SKIN, AND INSTALLED DOUBLER.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT RT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT RT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,473 hrs · 23,874 cycles

FRAME IS CRACKED AT LT OVERHEAD BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: SPLICE — DAMAGED (STRINGER)

DAMAGED STRINGER SPLICE. REPLACED STRINGER SPLICE.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT RT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: SKIN — GOUGED (FUSELAGE)

NUMEROUS GOUGES ON SKIN BELOW AFT CARGO THRESHOLD. BLENDED GOUGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT RT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT LT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,473 hrs · 23,874 cycles

FRAME IS CRACKED AT RT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE)

FRAME IS CRACKED AT RT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE)

STRINGER CLIP CRACKED. REPLACED STRINGER CLIP.

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

CORROSION ON FLOORBEAM. REMOVED CORRODED UPPER CHORD, FABRICATED REPAIR PARTS AND INSTALLED.

Part: SPLICE — MISDRILLED (STRINGER)

MISDRILLED STRINGER SPLICE. REPLACED STRINGER SPLICE.

Part: SKIN — DAMAGED (FUSELAGE)

DOUBLE HOLE DRILLED IN SKIN AND BEARSTRAP. REAMED UP HOLE AND INSTALLED DOUBLER.

Part: SKIN — CANNING (FUSELAGE)

EXTERNAL SKIN OIL CANNING/DENTED. REMOVED OIL CANNING/DENTED SKIN, FABRICATED REPAIR PARTS AND INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE)

CORROSION ON FLOORBEAM UPPER FLANGE. REMOVED UPPER FLANGE OF FLOORBEAM, FABRICATED REPAIR PARTS AND INSTALLED.

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

PAE - CORROSION ON MOP SILL. REPLACED MOP SILL.

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

PAE - CORROSION ON MOP SILL. REPLACED MOP SILL.

Part: SHEAR TIE — CRACKED (FUSELAGE)

PAE - CRACK IN FRAME SHEAR TIE. REMOVED AND REPLACED SHEAR TIE.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2

PAE - CORROSION ON CREASE BEAM WEB AT NUT-PLATE HOLES. REMOVED FABRICATED AND INSTALLED NEW WEB.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2

PAE - CORROSION AFT CARGO BAY ON FRAME SHEAR TIE. REPAIRED SHEAR TIE.

Part: STRINGER CLIP — CRACKED (FUSELAGE)

OKC - CRACKED STRINGER CLIP. REMOVED AND REPLACED STRINGER CLIP.

Part: SEAT TRACK — DAMAGED (FUSELAGE)

PAE - MECHANICAL DAMAGE TO TOP OF SEAT TRACK. REMOVED AND REPLACED SEAT TRACK.

Part: SEAT TRACK — DAMAGED (FUSELAGE)

PAE - MECHANICAL DAMAGE TO TOP OF SEAT TRACK. REMOVED AND REPLACED SEAT TRACK.

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP.

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

PAE - CORROSION ON FLOORBEAM AT PREVIOUS REPAIR. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLE.

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - CRACKED STRINGER CLIP AT FASTENER. REMOVED AND REPLACED STRINGER SPLICE AND CLIP.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

PAE - LIGHTNING STRIKE ON FUSELAGE SKIN. REPAIRED LIGHTNING STRIKE.

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - CRACKED STRINGER CLIP. REMOVED AND REPLACED STRINGER CLIP.

Part: STRINGER CLIP — BENT (FUSELAGE)

PAE - AFT CARGO BAY STRINGER CLIP BENT. REMOVED AND REPLACED STRINGER CLIP.

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - CRACKED STRINGER CLIP. REMOVED AND REPLACED STRINGER CLIP.

Part: STRINGER CLIP — CRACKED (FUSELAGE)

CRACKED STRINGER CLIP. REMOVED AND REPLACED CRACKED STRINGER CLIP. (REV 1)

Part: STRINGER CLIP — WORN (FUSELAGE)

LOOSE STRINGER CLIP. REMOVED AND REPLACED LOOSE STRINGER CLIP.

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 14-17 INOPERATIVE. RECONNECTED WIRES. OPERATIONAL CHECKED GOOD. (M)

Part: TERMINAL — DISCONNECTED (CABIN)

FAI - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROWS 14, 15, 16 AND 17 INOPERATIVE. RECONNECTED WIRE TERMINAL ENDS. LIGHTS THEN FUNCTIONED PROPERLY. (M)

Part: TERMINAL — DISCONNECTED (CABIN)

JNU - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROW 16 INOPERATIVE. RECONNECTED WIRE TERMINAL ENDS, OPS CHECKED GOOD. (M)

Part: SKIN — DENTED (CARGO DOOR)

PAE - DURING C-CHECK, FOUND FORWARD CARGO DOOR HAS NUMEROUS DENTS, AND PREVIOUS REPAIRS TO EXTERNAL SKIN. REMOVED AND REPLACED SKIN IAW SRM. (M)

Part: FRAME — DAMAGED (FUSELAGE)

PAE - DURING C-CHECK, FOUND MECHANICAL DAMAGE ON FRAME IN AFT CARGO BAY UNDER RIGHT FLOOR TO SIDE WALL SUPPORT AT BS 947, RBL 18, WL 175. REPAIRED IAW SRM. (M)

Part: THRESHOLD — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND THRESHOLD AT AFT CARGO DOOR HAS CORROSION ON WEB AT STATION 794-847 AND RBL 21-28. REMOVED AND REPLACED WEB IAW SRM. (M)

Part: SKIN — DAMAGED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CREASE IN FUSELAGE SKIN 17 INCHES LONG AT BS 399-416 AND STRINGER 20 RT. REPAIRED IAW SRM. (M)

Part: LIGHT — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 9-10. RECONNECTED FLOOR TRACK LIGHTS, OPS NORMAL. (M)

Part: INVERTER — BURNED (E/E BAY)

FAI - FLT 111 - DURING CRUISE, AT APPROXIMATELY 3 MILES FROM FAI, A STRONG SMELL OF BURNING ELECTRICAL WIRING WAS NOTED. REPLACED STATIC INVERTER AND NO DEFECTS NOTED. THE REMOVED STATIC INVERTER UNIT WAS SENT FOR TROUBLESHOOTING AND/OR REPAIR. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 18-21 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: LEVER — BENT (R1 DOOR)

PDX - DURING MAINTENANCE CHECK, THE R1 DOOR WOULD NOT STAY OPEN WITH THE LEVER ASSEMBLY. REPLACED HOLD OPEN LEVER ASSEMBLY AND DOOR REMAINS OPEN NORMALLY. (M)

Part: SLIDE — FAILED (PAX DOOR)

SAN - PRIOR TO FLIGHT 557, THE R2 DOOR SLIDE WAS NOT DISARMED WHEN DOOR WAS OPENED AND SLIDE DID NOT DEPLOY. FERRIED AIRCRAFT TO SEA FOR REPAIR DUE TO SLIDE NOT BEING ABLE TO BE RESTOWED. SEA MAINTENANCE REPLACED THE R1 DOOR SLIDE. THE SLIDE WAS ROUTED TO THE SHOP WHERE IT WAS ADJUSTED AND REPACKED. (M)

Part: WIRE — DISCONNECTED (CABIN)

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

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK THE FORWARD TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

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

Part: WIRE — DISCONNECTED (CABIN)

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

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD TWO AND AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED BOTH THE FORWARD AND AFT LIGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

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

Part: WIRE — LOOSE (CABIN)

JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE ILLUMINATING WITHOUT ANY MOVEMENT OF SWITCH. RESEATED WIRE IN EMERGENCY LIGHT SWITCH CANNON PLUG AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT EMERGENCY EXIT FLOOR TRACK LIGHTS, AFT EMERGENCY EXIT SIGN, AND L2 DOOR EMERGENCY EXIT IDENTIFIER WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT EMERGENCY EXIT FLOOR TRACK LIGHTS AND THE AFT GALLEY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 26C AND 27C, L2 DOOR OVERHEAD EXIT, AND AISLE OVERHEAD EXIT BETWEEN L2 AND R2 DOORS WOULD NOT ILLUMINATE. REPLACED BATTERY PACK IN AFT CABIN OVERHEAD AND ALL LIGHTS OPERATED NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, ROW 25 AND THE AFT CABIN EMERGENCY EXIT TRACK LIGHTS AND THE LT DOOR EXIT IDENTIFIER WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND THE LIGHTS WERE FOUND TO BE INOPERATIVE. (M)

Part: DOUBLER — WORN (RT TE MIDFLAP)

SEAT - DURING C-CHECK, THE RT WING OUTBOARD MID FLAP WAS FOUND TO BE WORN ON THE INBOARD LEADING EDGE. REPAIRED PER EA 5750-01166 AND BOEING TELEX ASA-SEA-94-0483TR. (M)

Part: RAM AIR DOOR — MIGRATED (PIN)

SEA - DURING C-CHECK, THE LEFT RAM AIR DOOR HINGE PIN WAS FOUND TO HAVE MIGRATED CAUSING DAMAGE TO THE WING TO BODY FAIRING. REPAIRED PER EA 2150-01007 AND BOEING SERVICE LETTER 737-SL-21-037. (M)

Part: SKIN — DELAMINATED (RT AILERON)

SEA - DURING C-CHECK, THE RT AILERON LOWER SKIN WAS FOUND TO BE DELAMINATED. REPAIRED PER EA 5760-01010 AND BOEING TELEX ASA-SEA-98-0063RR. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FWD AND AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

YVR - FLT 582 - PRIOR TO FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 10. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

OAK - DURING MAINTENANCE CHECK, ONE SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN THE FORWARD CABIN. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: FLOOR BEAM — CORRODED (BS 967)

SEA - DURING C-CHECK, THE UPPER AFT FLANGE OF THE FLOOR BEAM AT STATION 967 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01502 AND BOEING TELEX ASA-SEA-96-0584RR. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 110 - DURING CREW PRE-FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE NEAR THE AFT GALLEY AREA. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: CLIP — MISSING (L1 DOOR)

SEA - AFTER PASSENGERS HAD BOARDED, CREW TRIED TO CLOSE LEFT FORWARD ENTRY DOOR. DOOR WOULD NOT CLOSE. FOUND LEFT FWD DOOR HINGE LOCK PIN CLIP MISSING, CAUSING PIN TO SLIP. REPLACED CLIP ON UPPER HINGE LOCK PIN. DOOR OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING TO LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

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

Part: EEL CONNECTION — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LOOSE CONNECTION AT FOURTH LIGHT AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — LOOSE (CABIN)

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

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - LAST FOUR EMERGENCY TRACK LIGHTS INOP. MAINTENANCE RECONNECTED WIRES. OPS CHECKED NORMAL. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

ANC - CHECK, 4 AFT TRACK LIGHTS INOP. MAINTENANCE SECURED WIRING AND OPS CHECKED OK. (Z)

Part: SOCKET — MELTED (AFT LAVATORY)

PDX - DURING PRE-DEPARTURE ON THE GROUND AT PDX, ELECTRICAL SMELL NOTED IN AFT LEFT LAVATORY. MAINTENANCE REMOVED FLUORESCENT LIGHT COVER AND FOUND ARCING, FLAME AND SMOKE WITH LIGHT SOCKET MELTED. LAVATORY BLOCKED AND AIRCRAFT RELEASED PER MEL 25-10. MAINTENANCE SUBSEQUENTLY, REMOVED AND REPLACED SOCKET. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - AT CHECK, THE AFT 2 RED PEEPLS LIGHTS ARE INOP. MAINTENANCE RECONNECTED WIRING AT THE FWD MOST OF THE AFT PEEPLS LIGHTS. (W)