N755AS

Part: SKIN — GOUGED (BS 786-797) · airframe 66,684 hrs · 38,589 cycles

GOUGE IN FUSELAGE ON EDGE OF AFT CARGO DOOR CUTOUT, FWD EDGE, STRINGER 22R AREA. ACFT GROUNDED. REPAIRED SKIN AT AFT CARGO DOOR FWD CUTOUT IAW SRM 53-00-01-2R-32. THIS IS A CAT B REPAIR.

Part: SUPPORT BRACKET — CRACKED (BS 500) · airframe 66,684 hrs · 38,589 cycles

FWD CARGO BAY BS 500, SIDEWALL SUPPORT BRACKET CRACKED AT FASTENER HOLE BETWEEN STR 21L AND 22L, FOUND DURING CLEANING. REPAIRED SIDEWALL SUPPORT ANGLE IAW SRM 51-70-11-0G-0.

Part: SUPPORT — CRACKED (SERVICE DOOR) · airframe 66,684 hrs · 38,589 cycles

FORWARD SERVICE DOOR BS 294.5 S11R, EVIDENCE OF A CRACK IN RADIUS OF FRAME SUPPORT, ACFT GROUNDED. R & R FRAME SUPPORT IAW SRM 51-40-05-0G-0.

Part: INTERCOSTAL — CRACKED (BS 277) · airframe 66,684 hrs · 38,589 cycles

INTERCOSTAL FWD OF R1 DOOR BS 277 TO 292 WL 253 OTBD ANGLE APPEARS TO BE CRACKED IN RADIUS. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (BS 277-292) · airframe 66,684 hrs · 38,589 cycles

INTERCOSTAL FWD OF R1 DOOR BS 277 TO 292 WL 235 OTBD ANGLE APPEARS TO BE CRACKED IN RADIUS. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: ATTACH BRACKET — CORRODED (EMERGENCY EXIT) · airframe 66,684 hrs · 38,589 cycles

RT FWD EMERGENCY EXIT DOOR HAS CORROSION AROUND FASTENER HOLES ON ARMREST ATTACH BRACKET. ACFT GROUNDED. R & R ARMREST ATTACH BRACKET IAW SRM 51-40-02.

Part: CARGO TRACK — CORRODED (BS 867-947) · corrosion level 2 · airframe 66,684 hrs · 38,589 cycles

AFT CARGO TRACK, RBL 13.8, STA 919-947 HAS AREAS OF CORRODED. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1 DETAIL XIV, FABBED REPAIR PARTS IAW SRM 53-00-53-2R-2, INSTALLED REPAIR PARTS IAW SRM 53-00-53-2R 2, W .75", O .70", R .57", L 1.00", D .13".

Part: INTERCOSTAL — CRACKED (BS 277-291.5) · airframe 66,684 hrs · 38,589 cycles

INTERCOSTAL FWD OF R1 DOOR BS 277 TO 292, WL 240 OTBD ANGLE APPEARS TO BE CRACKED IN RADIUS. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (BS 277-292) · airframe 66,684 hrs · 38,589 cycles

INTERCOSTAL FWD OF R1 DOOR BS 277 TO 292 WL 258 OTBD ANGLE APPEARS TO BE CRACKED IN RADIUS. R & R ANGLE IAW SRM 51-40-02-0G-0.

Part: FRAME — CRACKED (BS 500G) · airframe 66,684 hrs · 38,589 cycles

FRAME BS 500G RT SIDE HAS A CRACK APPROXIMATELY .1250 INCH LONG EXTENDING INBD FROM THE EDGE OF THE 1.04 WIRE PENETRATION HOLE. REPAIRED FRAME AIW SRM 53-00-07-2R-13.

Part: FRAME — CRACKED (BS 500G) · airframe 66,684 hrs · 38,589 cycles

FRAME BS 500G HAS A CRACK APPROXIMATELY .1250 INCHES LONG EXTENDING INBD FROM THE EDGE OF THE 1.04, WORN PENETRATION HOLE. REPAIRED FRAME IAW SRM 53-00-07-2R-13.

Part: FRAME — CRACKED (BS 480) · airframe 66,684 hrs · 38,589 cycles

BS 480, STR 8-9R FRAME IS CRACKED AT AC DUCT ATTACH POINT. ACFT GROUNDED. REPAIRED FRAME CRACKED IAW T/C AD20062609 400-53-1-755, FIG 3.

Part: FRAME — CRACKED (BS 400) · airframe 66,684 hrs · 38,589 cycles

FRAME CRACKED AT BS 400 S8-9R. REPAIRED FRAME IAW T/C AD20062609 400 53 1755.

Part: PAN — CRACKED (BS 500-500A) · airframe 66,684 hrs · 38,589 cycles

FWD CARGO VHF ANTENNA PAN BS 500 TO 500A BL 0 IS CRACKED. ACFT GROUNDED. R & R VHF ANTENNA PAN IAW SRM 51-40-02-0G-0.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 64,979 hrs · 37,538 cycles

EMERGENCY LIGHT, AISLE LIGHT AT ROW 7 LT, MISSING LENS. REPLACED LENS AND TESTED IAW MM 33-51-21-962-001. OPS NORMAL.

Part: SIGN — MISSING (CABIN) · airframe 64,868 hrs · 37,479 cycles

RIGHT SIDE AFT OVERWING EXIT SIGN MISSING. REPLACED RT AFT OVERWING EXIT SIGN REF IPC 33-51-11-55A. OPS NORMAL REF MM 33-51-02.

Part: CONTROL CABLE — BROKEN (RIGHT WING) · airframe 64,433 hrs · 37,228 cycles

AT ROTATION, NOTICED SLIGHT LT YAW. DURING CLIMBOUT NOTICED SIGNIFICANT LT AILERON TO MAINTAIN WINGS LEVEL, APPROX 2.5 UNITS. AT CRUISE FL280 BETWEEN 3 TO 3.5 UNITS LT AILERON TRIM REQUIRED. FUEL BALANCED AND THRUST SYMMETRICAL. MAX MACH WAS .765. ATEMPTED TO ZERO OUT TRIM RESULTED IN RAPID ROLL TO RIGHT. SLIGHT HARMONIC VIBRATION, LOUD AIR NOISE AFT CABIN. DIVERTED TO LAS. REPLACED BROKEN WSB2-4 CONTROL CABLE FOR FLIGHT SPOILER NR 6 AND FRAYED WSB1-4 CONTROL CABLE FOR THE NR 7 FLIGHT SPOILER IAW MM20-10-91-404-002 AND STIFF/FROZEN SPOILER CABLE PULLEYS AT STATIONS 390 (WRAP AROUND PULLEYS) AND STATIONS 290 IAW MM20-10-09-404-007. ADJUSTED THE CONTROL CABLES IAW MM27-61-00-825-002. SPOILER CONTROL SYSTEM TEST GOOD IAW MM27-61-00-735-003. ALSO ADJUSTED THE NR 7 SPOILER INPUT ARM IAW MM27-61-00-715-001. GENERAL VISUAL INSP OF THE LT WING FLIGHT SPOILER SYS REVEALED NO FURTHER DEFECTS. YAW, EXCESSIVE AILERON INPUT, SLIGHT VIBRATION, AND NOISE DUE TO NR 6 FLIGHT SPOILER REMAINING NEARLY FULLY DEPLOYED DURING FLIGHT.

Part: INTERCOSTAL — CRACKED (BS 294.5) · airframe 62,973 hrs · 36,354 cycles

INTERCOSTAL WEB, STR 11L, STA 294.5, 303.9 CRACKED AT INBD FWD CORNER FROM FASTENER TO EDGE. REPAIRED INTERCOSTAL WEB AT STA 294.5, STR 11L IAW ASA EA AD20091614-400-53-107.

Part: SKIN — CHAFED (NR 4 SLAT) · airframe 62,973 hrs · 36,354 cycles

RT WING NR 4 SLAT T/E WEDGE INBD END LOWER SURFACE CHAFED. ACFT GROUNDED. REPARIED CHAFED AREA IAW SRM 51-70-10.

Part: A/C PACK — LACK OF LUBE (L1 DOOR) · airframe 62,834 hrs · 36,265 cycles

L1 DOOR VERY DIFFICULT TO CLOSE. FOUND HANDLE GUIDE PLATE DRY AND BINDING. LUBED GUIDE PLATE PER MM 12 25 21 643 007. OPS TEST GOOD FOR MM 52 11 00 705 065.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,188 hrs · 35,900 cycles

LEFT SIDE FRAME 500B CRACK IN 1 INCH WIDE PENETRATION HOLE. REPAIRED 500B LT FRAME IAW B737 400 SRM 53 00 07 REPAIR 13. THIS IS A CATEGORY B REPAIR WITH INSP THRESHOLD O 66 000 FLIGHT CYCLES AND 24 000 REPEAT INSP INTERVAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,188 hrs · 35,900 cycles

RT SIDE FRAME 520 CRACKED AT A 1" PENETRATION HOLE. REPAIRED RT FRAME AT STA 520 IAW B737 400 SRM 53 00 07 REPAIR 13. THIS IS A CATEGORY B REPAIR WITH INSP THRESHOLD O 66 000 FLIGHT CYCLES AND 24 000 REPEAT INSP INTERVAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,188 hrs · 35,900 cycles

LT SIDE FRAME AT 500D HAS CRACK IN 1" WIRE PENETRATION HOLE AND CRACK IN .5" HOLE. REPAIRED STA 500D LT FRAME IAW EA AD 20112305 400 53 100. THIS IS A CAT B REPAIR WITH INSP THRESHOLD OF 66 000 CYCLES AND REPEAT INSP AT 24 000 FLT CYCLES INTERVAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,188 hrs · 35,900 cycles

LEFT SIDE FRAME 500F HAS CRACK IN 1" WIDE PENETRATION HOLE. REPAIRED 500F LT FRAME IAW B737 400 SRM 53 00 07 REPAIR 13. THIS IS A CATEGORY B REPAIR INSPECTION THRESHOLD OF 66 000 CYCLES AND A REPEAT INSP AT 24 000 FLIGHT CYCLES.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,188 hrs · 35,900 cycles

RT FRAME 500B CRACKED AT .5" HOLE. REPAIRED STA 500B RT FRAME IAW EA AD 20112305 400 53 101 REV NEW ISSUED 12/16/2011. THIS IS A CAT B REPAIR WITH INSP THRESHOLD OF 66 000 FLIGHT CYCLES AND A REPEAT INSPECTION AT 24 000 FLT CYCLES.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,188 hrs · 35,900 cycles

RT FRAME 500F HAS CRACK AT 1" WIDE PENETRATION HOLE. REPAIRED 500F RT FRAME IAW B737 400 SRM 53 00 07 REPAIR 13. THIS IS A CATEGORY B REPAIR WITH INSP THRESHOLD O 66 000 FLIGHT CYCLES AND 24 000 REPEAT INSP INTERVAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,871 hrs · 35,719 cycles

FORWARD EMERGENCY LIGHT BATTERY PACKS M1132 AND M1133 DO NOT HAVE SUFFICENT CHARGE FOR FUNCTIONAL. REPLACED BATTERY PACKS M1132 AND M1133 AND PERFORMED GOOD INSTALLATION TEST PER M/M 33 51 51 962 015 33 51 51 963 016.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,871 hrs · 35,719 cycles

CRACK IN FUSELAGE LT SIDE AFT OF WING TO BODY FAIRING APPROX 4FT BELOW EMERGENCY LIGHT. REPAIRED LT SIDE SKIN AFT OF WING TO BODY FAIRING APPROX 4FT BELOW EMERGENCY LIGHT IAW SRM 53 00 01 REPAIR 31 PRODUCER V.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,729 hrs · 35,611 cycles

EMERGENCY LIGHT AISLE LIGHT AT ROW 12 RIGHT INOP. RELAMPED AND TESTED PER MM 33 51 81 962 044, OPS NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 61,729 hrs · 35,611 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN AT L 1 DOOR HAS MULTIPLE LAMPS INOP. RELAMPED AND TESTED PER MM 33 51 81 962 011, OPS NORMAL.

Part: BEARING — FAILED (R1 DOOR) · airframe 61,424 hrs · 35,423 cycles

R1 DOOR STUCK CLOSED. FOUND TORQUE TUBE LOWER HINGE PIN BEARING FAILED. REMOVED & REPLACED LOWER BEARING PER 52 41 41.

Part: LENS — CRACKED (EXIT SIGN) · airframe 60,830 hrs · 35,037 cycles

EXIT SIGN OVER RIGHT OVERWING EXIT FELL OFF. REPLACED EMERGENCY EXIT LIGHT LENS COVER AT RIGHT FORWARD OVERWING EXIT.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,937 hrs · 34,512 cycles

CORROSION ON BS 1016 BULKHEAD BL 0 RIGHT CHANNEL STIFFENER ON VERTICAL LEG OUTBOARD FACE AT WL 191. REPAIRED STIFFENER IAW ASA EA 400 53EA 04756 REV A.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

CORROSION ON BS 1016 BULKHEAD LOWER FORWARD CHORD FORWARD RADIUS AT RBL 2 AND WL 189. FABRICATED AND INSTALLED NEW SPLICE ANGLE IAW B737 400 SRM 53 80 08 FIG 101 51 40 05 51 20 01 AND 51 40 02.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,937 hrs · 34,512 cycles

CORROSION ON BS 1016 BULKHEAD WEB BL 0 ON BOTH SIDES OF CHANNEL STIFFENER FORWARD FACE WL 191. REMOVED CORRODED GORE WEB AND INSTALLED REPLACEMENT SECTION IAW ASA EA 400 53EA 04756 REV A.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

FRAME STRINGER TIE CLIP CRACKED BS 500C STR 11R. REMOVED AND REPLACED STRINGER TIE CLIP IAW B737 400 SRM 51 40 02 51 40 05 51 10 02 AND BOEING DRAWING 65 46536.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

STRINGER CLIP CRACKED AT BS 616 AT STR 5R. REMOVED AND REPLACED STRINGER CLIP IAW ASA DRAWING A53100265832.

Part: FAIRING — CRACKED (NR 2 PYLON) · airframe 59,937 hrs · 34,512 cycles

NR 2 PYLON INBOARD FAIRING ASSEMBLY IS CRACKED NAC STA 266. REMOVED AND REPLACED INBOARD FAIRING ASSEMBLY IAW BOEING DRAWING 313A1200 AND B737 400 SRM 51 40 05 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

FRAME CRACKED AT BS 787 STR 8R TO 9R. REPAIRED FRAME IAW ATS ER 11 01120.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

BS 827 FRAME CRACKED AT INBOARD FASTENER FOR A/C RAIL ATTACH BRACKET. REPAIRED FRAME IAW ATS ER 11 01120

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 41,570 hrs · 23,034 cycles

STRINGER SPLICE IS CRACKED AT BS 908 STR 4L REPLACED STRINGER SPLICE IAW B737 400 SRM 51 10 02 AND 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

BS 747 FRAME CRACKED AT INBOARD FASTENER FOR A/C RAIL ATTACH BRACKET. REPAIRED FRAME IAW ATS ER 11 01120.

Part: FRAME — CRACKED (BS 907) · airframe 59,937 hrs · 34,512 cycles

FRAME CRACKED AT BS 907 STR 8L TO 9L AT BIN RAIL. REPAIRED FRAME IAW AD20062609-400-53-111.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

CRACKED FRAME AT BS 867 STR 8-9R AT BIN RAIL. REPAIRED CRACKED FRAME IAW EA 400-53, EA 04727 AND ER 11-01258.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

BS 360 STR 16L STRINGER SPLICE CHANNEL IS CRACKED. REPAIRED CHANNELS IAW AD20091614-400-53-102 AND ER 11-01119.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

BS 727F FRAME CRACKED AT INBOARD FASTENER HOLE FOR A/C ATTACH BRACKET. REPAIRED FRAME IAW AD20062609-400-53-111.

Part: FRAME — CRACKED (BS 706) · airframe 59,937 hrs · 34,512 cycles

FUSELAGE UPPER LOBE FRAME CRACKED AT OUTBOARD ATTACH FASTENER FOR A/C RAIL ATTACH BRACKET BS 706 BETWEEN STR 8R AND 9R. REPAIRED FRAME IAW AD20062609-400-53-111.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

FRAME CRACKED AT BS 747 STR 8-9L AT BIN RAIL. REPAIRED FRAME IAW AD20062609-400-53-111.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

BS 440 FRAME CRACKED AT A/C RAIL SUPPORT BRACKET. REPAIRED FRAME IAW AD20062609-400-53-111.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

BS 727B FRAME CRACKED AT ATTACH FASTENER FOR A/C RAIL BRACKET. REPAIRED FRAME IAW AD20062609-400-53-111.

Part: FRAME — CRACKED (BS 787) · airframe 59,937 hrs · 34,512 cycles

BS 787 FRAME CRACKED AT A/C DISTRIBUTION ATTACH BRACKET. REPAIRED CRACKED FRAME IAW AD20062609-400- 53- 113 AND ER 11-01429.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

FRAME CRACKED AT BS 867 STR 8-9L AT BIN RAIL. REPAIRED FRAME IAW AD20062609-400-53-111.

Part: FRAME — CRACKED (BS 907) · airframe 59,937 hrs · 34,512 cycles

BS 907 FRAME CRACKED AT INBOARD ATTACH FASTENER FOR A/C RAIL ATTACH BRACKET. REPAIRED CRACKED FRAME IAW AD20062609-400-53-114 AND ER 11-01430.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 59,937 hrs · 34,512 cycles

LEFT WING INBOARD UPPER NO STEP PANEL INBOARD SUPPORT BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

BS 300 FRAME CRACKED AT A/C RAIL ATTACH BRACKET. REPAIRED FRAME IAW AD20062609-400-53-115 AND ER 11-01257.

Part: FRAME — CRACKED (BS 727D) · airframe 59,937 hrs · 34,512 cycles

FRAME CRACKED AT BS 727D STR 8R AND 9R AT BIN RAIL. REPAIRED FRAME IAW ER 11-011200 AND AD20062609 400-53-111.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

FRAME CRACKED AT BS 480 S8-9L AT A/C DISTRIBUTION RAIL SUPPORT BRACKET. REPAIRED FRAME IAW AD20062609-400-53-111.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

FRAME CRACKED AT BS 440 STR 8-9L. REPAIRED FRAME IAW AD20062609-400-53-111.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

FRAME CRACKED AT BS 380 STR 8R 9R AT BIN RAIL. REPAIRED FRAME IAW AD20062609-400-53-111.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

BS 500D FRAME STRINGER TIE CLIP CRACKED. REMOVED AND REPLACED STRINGER TIE CLIP IAW ASA DRAWING 53100265816.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 59,937 hrs · 34,512 cycles

RT HORIZONTAL STABILIZER STIFFENER FOUND CRACKED AT THE BOTTOM FASTENER HOLE STAB STA 92.7. REMOVED CRACKED STIFFENER FABRICATED REPLACEMENT AND INSTALLED IAW SRM 51-40-02

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

INTERCOSTAL SUPPORT ANGLE CRACKED. REMOVED ANGLE FABRICATED NEW ANGLE AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

BS 500A FRAME STRINGER TIE CLIP CRACKED. REMOVED AND REPLACED STRINGER TIE CLIP IAW ASA DRAWING 53100265816.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

WHILE WORKING FOUND FORWARD SERVICE DOOR THRESHOLD WEB CRACKED BS 301 WL 208 RBL 54. REMOVED AND REPLACED WEB IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

STRINGER TIE CLIP IS CRACKED BS 867 STR 1. REMOVED AND REPLACED STRINGER TIE CLIP IAW ASA DRAWING 53100265816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

STRINGER TIE CLIP IS CRACKED AT BS 867 STR 4R. REMOVED AND REPLACED STRINGER TIE CLIP IAW ASA DRAWING 53100265816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

INTERIOR FRAME STRINGER TIE CLIP CRACKED BS 380 STR 8R. REMOVED AND REPLACED STRINGER TIE CLIP IAW ASA DRAWING 53100265816.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

WHILE WORKING FOUND FRAME CRACKED BS 297 WL 209 RBL 55. REPAIRED CRACKED FRAME IAW EA 400-53, EA 04725 AND ER 11-01146.

Part: STRINGER CLIP — CRACKED (BS 727D S7R) · airframe 59,937 hrs · 34,512 cycles

FUSELAGE UPPER LOBE STRINGER CLIP AT BS 727D STR 7R IS CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW DRAWING 53100265816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

FUSELAGE UPPER LOBE STRINGER CLIP AT BS 727D STR 5L IS CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW ASA DRAWING 53100265816.

Part: FRAME — CRACKED (BS 500A) · airframe 59,937 hrs · 34,512 cycles

INTERIOR FRAME CRACKED STA 500A BETWEEN STINGER 8R AND 9R AT THE AIR DISTRIBUTION SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW AD20062609-400-53-112 AND ER 11-01153.

Part: WEB — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

CRACKED WEB ASSY ATTACHED TO THE MAIN CABIN FLOORBEAM VIEWABLE FROM THE E/E COMPARTMENT LOCATED BS 360 WL 207 BL 0. REMOVED AND REPLACED WEB IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 59,937 hrs · 34,512 cycles

INTERCOSTAL SUPPORT ANGLE CRACKED BS 500G LBL 7 WL 155. REMOVED AND REPLACED INTERCOSTAL SUPPORT ANGLE IAW B737 400 SRM 51 40 02.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

SEAT TRACK LIP MISSING/CRACKED OFF. REMOVED DAMAGED SECTION INSTALLED NEW SECTION AND REPAIR PARTS IAW SRM 53 00 52 REPAIR 1.

Part: SKIN — DELAMINATED (ELEVATOR) · airframe 57,025 hrs · 32,801 cycles

RIGHT ELEVATOR UPPER SURFACE I/B AREA HAS BUBBLES IN PAINT. REPAIRED RIGHT ELEVATOR UPPER SURFACE.

Part: SKIN — DENTED (FUSELAGE) · airframe 26,262 hrs · 11,280 cycles

FUSELAGE SKIN LEFT OF BOTTOM CENTER LINE DENTED AND GOUGED AT BUTT SPLICE. REMOVED DAMAGED AREA OF SKIN AND REPLACED SKIN.

Part: SKIN — DENTED (FUSELAGE) · airframe 26,262 hrs · 11,280 cycles

FUSELAGE SKIN LEFT OF BOTTOM CENTER LINE DENTED AND GOUGED AT BUTT SPLICE. REMOVED DAMAGED AREA AND REPAIRED SKIN.

Part: SKIN — DENTED (FUSELAGE) · airframe 26,262 hrs · 11,280 cycles

LOWER BUTT SPLICE DENTED. REMOVED DAMAGED AREA OF SPLICE STRAP.

Part: RUB STRIP — DAMAGED (TE FLAP) · airframe 56,894 hrs · 32,719 cycles

RIGHT I/B MIDFLAP T/E WEDGE RUBSTRIP & REPAIR ON CORNER ARE DAMAGED. REMOVED DAMAGED REPAIR & RUBSTRIP, FABBED FILLER & DOUBLER & BONDED REPAIR & RUBSTRIP IAW B737 400 SRM 51 70 10 REP 4.

Part: SKIN — GOUGED (MIDFLAP) · airframe 56,894 hrs · 32,719 cycles

RT INBOARD MID FLAP LEADING EDGE UPPER SURFACE IS GOUGED. REMOVED DAMAGED AREA, FABBED FILLER & DOUBLER AND INSTALLED REPAIR PARTS IAW EA 13673.

Part: SKIN — DAMAGED (FOREFLAP) · airframe 56,894 hrs · 32,719 cycles

RT INBOARD FORE FLAP LOWER SURFACE HAS A DENT WITH A CREASE & GOUGE ON PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR, FABBED DOUBLER AND BONDED NEW REPAIR IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (TE FLAP) · airframe 56,894 hrs · 32,719 cycles

RIGHT I/B MIDFLAP T/E WEDGE CENTER AREA LOWER SURFACE HAS 3 EA SHARP DENTS 43 53 IN. FROM I/B END. REMOVED DAMAGED SKIN & DOUBLER, FABBED DOUBLER & FILLER, BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REP 4.

Part: SKIN — CHAFED (TE FLAP) · airframe 56,894 hrs · 32,719 cycles

RIGHT I/B FLAP T/E WEDGE IS CHAFED ON BOTTOM I/B END. REMOVED DAMAGED SKIN & DOUBLER, FABBED FILLER AND DOUBLER AND BONDED REPAIR IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 56,894 hrs · 32,719 cycles

NR 6 SLAT AFT I/B CORNER DAMAGED. REMOVED DAMAGE FABBED FILLER & DOUBLER, BONDED REPAIR IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: BEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,894 hrs · 32,719 cycles

AFT PIT BEAR STRAP AT STA 790 RBL 29 IS CORRODED. REMOVED CORROSION, FABBED REPAIR ANGLES AND INSTALLED REPAIR IAW EA 400 53EA 02496.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,894 hrs · 32,719 cycles

INTERCOSTAL AT STA 727+8 27L 27R HAS CORROSION ON THE WEB. REMOVED CORRODED WEB, FABBED REPLACEMENT WEB AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: BUSHING — LOOSE (NR 2 PYLON) · airframe 56,894 hrs · 32,719 cycles

NR 2 ENG OUTBOARD FUSE PIN PYLON BUSHING IS LOOSE. REMOVED AND REPLACED NR 2 ENG PYLON O/B BUSHING FOR FUSE PIN IAW EA 400 54EA 02499.

Part: BUSHING — LOOSE (NR 2 PYLON) · airframe 56,894 hrs · 32,719 cycles

NR 2 ENG I/B FUSE PIN BUSHING FELL OUT UPON CLEANING. REMOVED AND REPLACED NR 2 ENG PYLON I/B FUSE PIN BUSHING PER EA 400 54EA 02499.

Part: SKIN — GOUGED (HORIZ STAB) · airframe 56,984 hrs · 32,719 cycles

LT HORIZONTAL STAB L/E IS GOUGED AT L/E STA 148. REMOVED DAMAGED AREA, FABBED FILLER & DOUBLER, INSTALLED REPAIR PARTS IAW B737 400 SRM 55 10 01 FIG 201.

Part: SKIN — GOUGED (HORIZ STAB) · airframe 56,894 hrs · 32,719 cycles

LT HORIZONTAL STAB L/E IS GOUGED AT L/E STA 138. REMOVED DAMAGED AREA, FABBED FILLER & DOUBLER, INSTALLED REPAIR PARTS IAW B737 400 SRM 55 10 01 FIG 201.

Part: SKIN — CHAFED (TE FLAP) · airframe 56,894 hrs · 32,719 cycles

RIGHT I/B AFT FLAP CHAFED ON UPPER SURFACE I/B END. REMOVED DAMAGED AREA, FABBED FILLER & DOUBLER, BONDED REPAIR IAW B737 400 SRM 51 70 10 REP 4 ON UPPER SURFACE.

Part: SKIN — CHAFED (MID FLAP) · airframe 65,893 hrs · 32,719 cycles

LEFT WING O/B MID FLAP INBOARD LOWER SKIN CHAFED. REMOVED DOUBLER FABRICATED AND BONDED NEW DOUBLER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,893 hrs · 32,719 cycles

TWO DENTS AT FS 380 STR 14 DENTS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE AND INSTALLED DOUBLER AND FILLER.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 65,893 hrs · 32,719 cycles

L1 DOOR BEAR STRAP LOWER HINGE CUTOUT HFEC INSPECTION REVEALED CRACK AT 4TH INSPECTION FASTENER FROM HOLE FROM TOP. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS.

Part: SKIN — CHAFED (TE FLAP) · airframe 65,893 hrs · 32,719 cycles

LEFT WING O/B MID FLAP INBOARD LOWER SKIN CHAFED. REMOVED DOUBLER, FABRICATED AND BONDED NEW DOUBLER.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 65,893 hrs · 32,719 cycles

L1 DOOR BEAR STRAP LOWER HINGE CUTOUT HFEC INSPECTION REVEALED CRACK AT 2ND INSPECTION FASTENER FROM HOLE FROM TOP. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 56,688 hrs · 32,595 cycles

ON TAKEOFF SMELLED SMOKE ON THE FLT DECK, WITHIN 2 SECONDS F/A REPORTED SMOKE SMELL THROUGHOUT THE CABIN. DIVERTED BACK TO SIT AND ACCOMPLISHED QRH E3.1 SMOKE/FUMES OR FIRE IN FLT DECK OR PASSENGER CABIN. TURNING RECIRC FANS OFF SEEMED TO ELIMINATE THE FUMES. UPON INSPECTION OF A/C FOUND NO EVIDENCE OF FLUID INGESTION, FOREIGN MATTER OF FOD IN EITHER ENGINE INLET, APU INLET OR RAM AIR DOOR INLETS. INSPECTED GEAR AND WING AREAS FOR EVIDENCE OF HYD LEAKS WITH NONE NOTED. RAN NR 1 & NR 2 ENGINES SEPARATELY WITH BOTH PAX RUN INDIVIDUALLY WITH NO FUMES OR SMELL RAN APU AND PAC SEPARATELY WITH NO ODOR NOTED. COMPLIED WITH CABIN ODOR TROUBLESHOOTING AMM 055 60 00PG BLK 101, UNABLE TO DUPLICATE ANY ODOR. A/C OK FOR SERVICE, ALL LIGHTING C/BS GALLEYS CARGO COMPS LAVS CHECK NORMAL. SEAMC NOTIFIED, NO HISTORY IN PAST 15 DAYS.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 56,232 hrs · 32,330 cycles

CABIN ALTITUDE WARNING HORN SOUNDS AT CRUISE (FL330) CABIN ALT WAS 11 500FT. STANDBY MODE ARRESTED CLIMB AND REDUCED CABIN ALT TO JUST BELOW 10 000FT. PERFORMED DECAY CK REF AMM TASK 21 00 05 782 001, OPS CHECK GOOD. REMOVED A/C POWER REF AMM 24 22 00 862 011, REMOVED & REPLACED PRESSURE CONTROLLER REF AMM 21 31 21, OPS CHECK GOOD. REMOVED & REPLACED FOR PRECAUTION. SUPPLIED A/C POWER REF AMM 24 22 00 862 001, A/C OK FOR SERVICE.

Part: REFLECTOR — DEFECTIVE (EXTERIOR) · airframe 55,334 hrs · 31,805 cycles

EXTERIOR EMERGENCY EXIT LIGHT AT R1 DOOR INOP. REMOVED AND REPLACED R1 EXTERIOR EMERG LIGHT REFLECTOR ASSY REF CMM 33 50 27, OP CHECK NORMAL.

Part: STRUCTURE — CORRODED (R1 DOOR) · airframe 54,270 hrs · 31,195 cycles

R1 DOOR INSIDE HANDLE IS LOOSE MIG 2C 240086 INITIATED FOUND R1 DOOR TORQUE BOX BEARING BORES CORRODED FOR LATCHING CRANK ASSY. REMOVED AND REPLACED R1 DOOR REF MM 52-41-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 53,393 hrs · 30,749 cycles

FLOORBEAM AT STA 312, RBL 6 CORRODED. REMOVES STA 312 FLOOR BEAM " T" CAMP FABBED FLOORBEAM T CAP 2 + 3 REPAIR PARTS + INSTALLED REPLACEMENT T CAP 2 + 3 PARTS IAW SRM 53-10-51, REPAIR 5.

Part: CUSP WEB — CORRODED (BS 810-825) · airframe 53,393 hrs · 30,749 cycles

CUSP WEB IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR IAW SRM 51 70 13.

Part: FLOORBEAM — CRACKED (BS 312) · airframe 53,393 hrs · 30,749 cycles

FLOORBEAM LOWER STABILIZER AT STA 312, BL42 IS CRACKED STOP DRILLED, CRACKED FABBED DOUBLER AND INSTALLED REPAIR IAW SRM 53 10 51.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

FLOORBEAM STABILIZER AT STA 312 + BL 45 R IS CRACKED BROKEN FABRICATED DOUBLER + INSTALLED REPAIR IAW SRM 51-70-13, PG 3.

Part: INTERCOSTAL — CRACKED (BS 380-400) · airframe 53,393 hrs · 30,749 cycles

INTERCOSTAL BETWEEN STA 380-400 AT BL "0" HAS UPPER ANGLE CRACKED AT THE FWD END. REMOVED DAMAGED ANGLE & REPLACE IAW SRM 51-40-02.

Part: FITTING — GOUGED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

AT THE AFT SIDE OF THE APB STRINGER 4RT END FITTING IS GOUGED. REMOVED AND REPLACED STRINGER 4RT END FITTING ON THE AFT SIDE OF THE APB IAW SRM 51-40-02, P6.

Part: FITTING — GOUGED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

AT THE AFT SIDE OF THE APB STRINGER 5R END FITTING IS GOUGED. REMOVED AND REPLACED STRINGER 5R END FITTING ON THE AFT SIDE OF THE APB IAW SRM 51-40-02, FIG 8.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 53,393 hrs · 30,749 cycles

RT IB FOREFLAP LOWER SURFACE HAS A DENT ON IB END REMOVED DAMAGE FABBED FILLER & DOUBLER, BONDED IAW SRM 51-70-10 REPAIRS.

Part: SKIN — CHAFED (BS 855-881) · airframe 53,393 hrs · 30,749 cycles

FUSELAGE SKIN CHAFED FROM DORSAL FIN FWD SEAL BLENDED AREA FABRICATED AND INSTALLED REPAIR DOUBLER SPLICE STRAPS AND TAPERED FILLERS IAW SRM 53-60-01 REPAIR 10 PROCEDURE II.

Part: SKIN — DENTED (NR 6 SLAT) · airframe 53,393 hrs · 30,749 cycles

OB L/E OF NR 6 SLAT IS DENTED REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57 43 01 FIG 201.

Part: FITTING — GOUGED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

STRINGER 14 L, END FITTING ON THE AFT SIDE OF THE APB HAS A GOUGE MARKS. REMOVED AND REPLACED STRINGER 14L END FITTING IAW SRM 51-40-02, PG 4.

Part: FITTING — GOUGED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

STRINGER 16L END FITTING ON THE AFT SIDE OF THE APB HAS A GOUGE MARKS. REMOVED AND REPLACED STRINGER 16L END FITTING IAW SRM 51-40-02, PG 4.

Part: FITTING — GOUGED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

AT THE AFT SIDE OF THE APB STRING 17L END FITTING IS GOUGED REMOVE AND REPLACE APB STRINGER 17L END FITTING ON THE AFT SIDE OF THE APB IAW SRM 51-40-02, FIG 8, PG 6.

Part: FITTING — GOUGED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

AT THE AFT SIDE OF THE APB STRINGER 21L END FITTING IS GOUGED. REMOVED AND REPLACED STRINGER 21L END FITTING ON THE AFT SIDE OF THE APB IAW SRM 51-40-02, FIG 8.

Part: FITTING — GOUGED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

AT AFT SIDE OF THE APB STRINGER 18L END FITTING IS GOUGED. REMOVED AND REPLACED STRINGER 18L END FITTING ON THE AFT SIDE OF THE APB IAW SRM 51-40-02, P 4.

Part: FITTING — GOUGED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

AT THE APB STRINGER 15L END FITTING HAS GOUGES. REMOVED & REPLACED STRINGER 15L END FITTING ON THE AFT SIDE OF THE APB IAW SRM 51-40-05, P1.

Part: STRINGER FITTING — GOUGED (BS 1016 S17AL) · airframe 53,393 hrs · 30,749 cycles

AT THE AFT SIDE OF THE APB STRINGER 17A LT END FITTING IS GOUGED. REMOVED AND REPLACED STRINGER 17A LT END FITTING ON THE AFT SIDE OF THE APB IAW SRM 51-40-02, P4.

Part: FITTING — GOUGED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

AT THE AFT SIDE OF THE APB STRINGER 20L END FITTING IS GOUGED. REMOVED AND REPLACED STRINGER 20L END FITTING ON THE AFT SIDE OF THE APB IAW SRM 51-40-02, FIG 8.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 53,393 hrs · 30,749 cycles

NR 5 SPOILER DENTED ON THE TOP SIDE IB END CENTER OF PANEL PREPPED DAMAGED AREA FABBED DOUBLER & BONDED REPAIR IAW SRM 51 70 10 PG 257.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

FLOORBEAM LOWER STABILIZER AT STA 312 + BL "O" AS IS CRACKED STOPPED DRILLED THE CRACK, FABBED A DOUBLER + INSTALLED THE REPAIR IAW SRM 53-10-51, REPAIR 4.

Part: SKIN — DENTED (NR 3 SPOILER) · airframe 53,393 hrs · 30,749 cycles

NR 3 SPOILER LOWER SURFACE IB T/E IS DENTED. INSTALLED DOUBLERS AND BONDED REPAIRS IAW SRM 51-70-10.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

CENTER ISLE FLOOR SUPPORT AT STA 540 IS CRACKED REMOVED + REPLACE FLOOR SUPPORT IAW SRM 51-40-05.

Part: CHANNEL — CORRODED (L1 DOORWAY) · corrosion level 2 · airframe 53,393 hrs · 30,749 cycles

L 1 DOOR LOWER CUTOUT U CHANNEL IS CORRODED. REPLACED CHANNEL IAW SRM 51 40 02.

Part: ANGLE — CORRODED (BS 312-336) · corrosion level 2 · airframe 53,393 hrs · 30,749 cycles

FWD PASSENGER (L 1) DOOR LOWER CUTOUT Z ANGLE IS CORRODED. REPLACED ANGLE IAW SRM 51 40 02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

STRINGER 8R IS CRACKED AT NUMEROUS LOCATIONS FROM STA 500, 500A, AND 500B. REMOVED DAMAGED SECTION OF STRINGER, FABBED FILLER, REPAIR ANGLES AND INSTALLED PARTS IAW SRM 53-00-03, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (BS 767) · corrosion level 2 · airframe 53,393 hrs · 30,749 cycles

AFT PIT FLOOR SUPPORT AT STA 767, LBL 12.50 IS CORRODED REMOVED DAMAGED AREA FABBED REPAIR PARTS AND INSTALLED IAW EA 5320-01844.

Part: FLOOR SUPPORT — CORRODED (BS 767-779) · corrosion level 2 · airframe 53,393 hrs · 30,749 cycles

AFT PIT FLOOR SUPPORT AT STA 767 LBL 3.0 IS CORRODED REMOVED DAMAGED AREA FABBED REPAIR PARTS & INSTALLED IAW ASA EA 5320 01844.

Part: FLOOR SUPPORT — CORRODED (BS 767) · corrosion level 2 · airframe 53,393 hrs · 30,749 cycles

AFT PIT FLOOR SUPPORT AT STA 767, LBL 8.10 UPPER SURFACE IS CORRODED. REMOVED DAMAGED AREA FABBED REPAIR PARTS AND INSTALLED IAW EA 5320-01844.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 53,393 hrs · 30,749 cycles

RT IB FORE FLAP UPPER SURFACE CHAFED ALONG OB EDGE. REMOVED DAMAGED AREA FABBED FILLER, DOUBLER, BONDED REPAIR IAW SRM 51-70-10 REPAIR 4.

Part: FLOOR SUPPORT — CORRODED (BS 767-779) · corrosion level 2 · airframe 53,393 hrs · 30,749 cycles

CORROSION ON UPPER SURFACE OF FLOOR SUPPORT AT STA 767 RBL1380 REMOVED DAMAGE AND FABRICATED REPAIR PARTS & INSTALL PER ASA EA 5320 01844

Part: FLOOR SUPPORT — CORRODED (BS 767-779) · corrosion level 2 · airframe 53,393 hrs · 30,749 cycles

AFT CARGO FLOOR SUPPORT IS CORRODED REMOVED DAMAGED AREA FABRICATED REPAIR PARTS & INSTALLED IAW EA 53 20 01844.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 53,393 hrs · 30,749 cycles

AFT LT GALLEY FLOORBEAM FASTENER HOLE IS CORRODED. REPLACE EXISTING REPAIR STRAP IAW SRM 53-00-51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,393 hrs · 30,749 cycles

FLOORBEAM AT STA 328 FROM RBL 12 TO THE R1 DOOR HAS CORROSION ON THE UPPER T CAP. REMOVED FLOORBEAM, T CAP FABBED T CAP AND SPLICE REPAIR PARTS, INSTALLED ALL REPAIR PARTS IAW EA NR 12768.

Part: CUSP WEB — CORRODED (BS 802-804) · airframe 53,393 hrs · 30,749 cycles

CUSP WEB CORRODED. REMOVED DAMAGED SECTION AND INSTALLED FILLER AND DOUBLER IAW SRM 51 70 13.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

CHORD CORRODED. REPLACED CHORD IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

STRINGER CLIP IS CRACKED. REPLACED CLIP PER SRM 51 40 02.

Part: CUSP WEB — CORRODED (BS 827-847) · airframe 53,393 hrs · 30,749 cycles

CUSP WEB CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR PARTS IAW SRM 51 70 13.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

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

Part: FLOORBEAM — CORRODED (BS 294) · corrosion level 2 · airframe 53,393 hrs · 30,749 cycles

FLOORBEAM UPPER CHORD AT STA 294.5 FROM RBL 26-RBL 50 IS CORRODED UNDER FWD GALLEY REMOVED DAMAGED AREA FABBED REPAIR PARTS & REPAIR ANGLES & INSTALLED IAW SRM 53-10-51 FIG 201.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,393 hrs · 30,749 cycles

AFT PIT INTERCOSTAL AT STA 847, 867 AT STR 35 R IS CORRODED REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-05, FIG 2.

Part: FLOOR SUPPORT — CORRODED (BS 727) · corrosion level 2 · airframe 53,393 hrs · 30,749 cycles

AFT PIT FLOOR SUPPORT RAIL IS CORRODED AFT OF STA 727 RT IB OF STRINGER 28 LT. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND INSTALLED IAW EA 5320 01845.

Part: CARGO TRACK — CORRODED (BS 911-947) · airframe 53,393 hrs · 30,749 cycles

AFT CARGO TIE DOWN TRACK IS CORRODED. REPLACED TIE DOWN TRACK.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

CORROSION ON FAILSAFE AT STA 847 BETWEEN STR 28L, 28R IN AFT CARGO PIT REMOVED DAMAGED AREA FABBED FILLER, REPAIR ANGLE, INSTALLED IAW SRM 53-70-11, FIG 1.

Part: FRAME — DENTED (FUSELAGE) · airframe 53,393 hrs · 30,749 cycles

AFT PIT FRAME AT STA 727C IS DENTED ABOVE THE STR 24L REMOVED DAMAGED AREA FABBED FILLER + REPAIR ANGLES + INSTALLED IAW SRM 51-70-11, FIG 1.

Part: FLOOR SUPPORT — CORRODED (BS 727F) · corrosion level 2 · airframe 53,393 hrs · 30,749 cycles

AFT PIT FLOOR SUPPORT RAIL AFT OF STA 727F IB OF STRINGER 28R IS CORRODED REMOVED DAMAGED AREA FABRICATED REPAIR PARTS & INSTALLED IAW EA 5320 1844.

Part: FLOOR SUPPORT — CORRODED (BS 767) · corrosion level 2 · airframe 53,393 hrs · 30,749 cycles

AFT PIT FLOOR SUPPORT AT STA 767, RBL 3.0 IS CORRODED. REMOVED DAMAGED AREA FABBED REPAIR PARTS AND INSTALLED IAW EA 5320 01845.

Part: CARGO TRACK — CORRODED (BS 911-947) · airframe 53,393 hrs · 30,748 cycles

AFT CARGO TIE DOWN TRACK IS CORRODED. REPLACED TIE DOWN TRACK IAW SRM 51-40-02.

Part: SKIN — DENTED (NR 3 SPOILER) · airframe 53,393 hrs · 30,749 cycles

NR 3 SPOILER DENTED ON LOWER SURFACE 4" IB OF OUBD END & 5" AFT OF FWD EDGE PREPAIRED DAMAGED AREAS FABRICATED REPAIR DOUBLERS & BONDED REPAIR IAW SRM 51-70-10 REPAIR 2.

Part: SKIN — CHAFED (SLAT) · airframe 53,393 hrs · 30,749 cycles

SLAT LOWER SURFACE IB END IS CHAFED. REMOVED DAMAGED AREA FABRICATED A DOUBLER AND BONDED THE REPAIR SRM 51-70-10 REPAIR 4.

Part: SKIN — DENTED (FOREFLAP) · airframe 53,393 hrs · 30,749 cycles

LT OB FOREFLAP SURFACE IS DENTED. BOND REPAIRED WITH DOUBLER IAW SRM 51-70-10.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 53,393 hrs · 30,749 cycles

RT IB FORE FLAP LOWER SURFACE DENTED APPROX 2" IB OF THE 2ND TRACK. REMOVED FACTORY DOUBLER PREPPED AREA FABBED REPAIR DOUBLER & BONDED REPAIR IAW SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 53,393 hrs · 30,749 cycles

LT IB FORE FLAP T/E DENTED ON LOWER SURFACE ABOVE THE CENTER TRACK REMOVED DAMAGE FABBED FILLER & REPAIR PARTS, BONDED IAW SRM 51-70-10 REPAIR 4.

Part: SKIN — CHAFED (NR 7 FLAP) · airframe 53,393 hrs · 30,749 cycles

RT OB MID FLAP CHAFED ABOVE NR 7 FLAP TRACK FAIRING. REMOVED DAMAGED AREA FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 51 70 10 REPAIR 4.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 53,393 hrs · 30,749 cycles

LT OB MID FLAP LOWER SURFACE IS CHAFED ABOVE NR 2 FLAP TRACK FAIRING. IB & OB SIDES REMOVED DAMAGE FABBED FILLER & DOUBLER & BONDED IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 53,393 hrs · 30,749 cycles

RT IB FORE FLAP CHAFED ON THE TOP IB SIDE REMOVED PREVIOUS DOUBLER PREPPED AREA, FABBED REPAIR & BONDED REPAIR IAW SRM 51-70-10 REPAIR 2.

Part: SKIN — DENTED (NR 5) · airframe 53,393 hrs · 30,749 cycles

NR 5 GROUND SPOILER HAS SEVERAL DENTS ON LOWER SURFACE. PREPPED DAMAGED AREA FABRICATED REPAIR DOUBLERS & BOND IAW SRM 51-70-10 PG 251.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 53,393 hrs · 30,749 cycles

RT IB FORE FLAP HAS SEVERAL DENTS ON THE LOWER SURFACE ABOVE THE IB TRACK REMOVED PREVIOUS REPAIR & FACTORY DOUBLER FABBED REPAIR DOUBLER & BLENDED REPAIR IAW SRM 51-70-10 REPAIR 2.

Part: WEDGE — DENTED (T/E FLAP) · airframe 53,393 hrs · 30,749 cycles

LT IB MID FLAP T/E WEDGE IS DENTED ON LOWER SURFACE. REMOVED DAMAGED SECTION AND INSTALLED FILLER DOUBLER AND BONDED REPAIR IAW SRM 51-70-10.

Part: WEDGE — DENTED (LT WING TE FLAP) · airframe 53,393 hrs · 30,749 cycles

LT IB MID FLAP T/E WEDGE IS DENTED. INSTALLED DOUBLER AND BONDED REPAIR IAW SRM 51-70-10.

Part: SKIN — DENTED (T/E FLAP) · airframe 53,393 hrs · 30,749 cycles

LT OB MID FLAP LOWER SURFACE IS DENTED. BOND REPAIRED WITH DOUBLER IAW SRM 51-70-10.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 53,393 hrs · 30,749 cycles

RT OB AFT FLAP LOWER SURFACE IS DENTED. INSTALLED BONDED DOUBLERS IAW SRM 51-70-10.

Part: SKIN — DENTED (NR 8 SPOILER) · airframe 53,393 hrs · 30,749 cycles

NR 8 SPOILER LOWER SURFACE IS DENTED. INSTALLED REPAIR DOUBLER IAW SRM 51-70-10.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 53,393 hrs · 30,749 cycles

RT IB AFT FLAP LOWER SURFACE DENTED. BOND REPAIRED IAW SRM 51-70-16.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 53,393 hrs · 30,749 cycles

LT IB FORE FLAP T/E IS DENTED ON LOWER SURFACE ABOVE IB TRACK REMOVED DAMAGE. FABBED FILLER & DOUBLER & BOUNDED REPAIR IAW SRM 51-70-10 REPAIR 2.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 53,393 hrs · 30,749 cycles

LT OB AFT FLAP LOWER SURFACE CHAFED. REMOVED DAMAGED EXISTING DOUBLER AND INSTALLED NEW DOUBLER IAW SRM 51-70-10.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 53,393 hrs · 30,749 cycles

LT OB FOREFLAP L/E IS GOUGED ON PREVIOUS REPAIR DOUBLER AT THE INBOUND END REMOVED DAMAGE ED DOUBLER FABBED & INSTALLED REPAIR IAW SRM 57 53 01 PG 202 203.

Part: SKIN — DENTED (NR 6 SPOILER) · airframe 53,393 hrs · 30,749 cycles

NR6 SPOILER LOWER SURFACE IS DENTED. INSTALLED REPAIR DOUBLER AND BONDED REPAIR IAW SRM 51-70-10.

Part: SKIN — DENTED (BS 1088 S24L) · airframe 53,393 hrs · 30,749 cycles

FUSELAGE SKIN DENTED STA 1088 STR 24L REMOVED DAMAGE FABRICATED AND INSTALLED DOUBLER AND STRUCTURAL FILLER IAW ASA EA 5330-02372.

Part: SKIN — DENTED (BS 860-876) · airframe 53,393 hrs · 30,749 cycles

FUSELAGE SKIN IS DENTED. REMOVED DAMAGED SECTION AND INSTALLED FILLER DOUBLER AND TRIPLER IAW SRM 53 27.

Part: SKIN — DENTED (BS 196) · airframe 53,393 hrs · 30,749 cycles

REF SAD 5785173: DENT & CREASE ON BOTTOM OF FUSELAGE AT APPROX STA 196 FWD OF ACCY DOOR REMOVED DAMAGED AREA FABBED REPAIR PARTS AND INSTALLED IAW EA 5330 02373.

Part: SKIN — DENTED (BS 1026-1040) · airframe 53,393 hrs · 30,749 cycles

DENT IN FUSELAGE LT SIDE AFT OF PRESSURE BULKHEAD CUTOUT DAMAGED AREA FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW ASA EA 533002375.

Part: SKIN — DENTED (NR 6 SLAT) · airframe 53,393 hrs · 30,749 cycles

NR 6 SLAT HAS 3 DENTS IN T/E WEDGE UPPER SURFACE 19-32" FROM IB END PREPAIRED DAMAGED AREA FABRICATED REPAIR PARTS & BONDED IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — DENTED (BS 907-915) · airframe 53,393 hrs · 30,749 cycles

FUSELAGE SKIN IS DENTED. REMOVED DAMAGED AREA. INSTALLED FILLER DOUBLER AND TRIPLER PER SRM 53 00 01

Part: SKIN — DENTED (NR 6 SPOILER) · airframe 53,393 hrs · 30,749 cycles

NR 6 SPOILER UPPER SURFACE IS DENTED. INSTALLED REPAIR DOUBLER AND BONDED REPAIR IAW SRM 51-70-10.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 53,393 hrs · 30,749 cycles

REF SAD 5060511: NR 5 SPOILER UPPER SURFACE DENTED 6" FROM T/E 12" FROM OB EDGE PREPPED DAMAGED AREA FABBED DOUBLER + BONDED REPAIR IAW SRM 51 70 10 PG 257.

Part: SKIN — DENTED (BS 348-366) · airframe 53,393 hrs · 30,749 cycles

REF SAD 6058905: FUSELAGE LOWER SKIN DENT AT STA 354 STR 23 24R. DENT IS CREASED WITHIN 3" OF A SPLICE REMOVED DAMAGE AREA FABBED FILLER DOUBLER, TRIPLER & INSTALLED REPAIR PARTS IAW SRM T.R 53-27 FIG 201 DETAIL XXIX.

Part: SKIN — DENTED (BS 355-379) · airframe 53,393 hrs · 30,749 cycles

DENT IN FUSELAGE SKIN ALONG STR 17L OVER 2 RIVETS AT STA 375 REMOVED PREVIOUS REPAIR REMOVED DAMAGED AREA FABBED FILLERS + DOUBLERS + INSTALLED REPAIR IAW EA NR12755.

Part: SKIN — DENTED (BS 986-1016) · airframe 53,393 hrs · 30,749 cycles

FUSELAGE SKIN IS DENTED. REPLACED DAMAGED SECTION IAW SRM 51-40- 02.

Part: SKIN — DENTED (BS 323-355) · airframe 53,393 hrs · 30,749 cycles

FUSELAGE DENTED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53 27.

Part: SKIN — DENTED (BS 727E S26L) · airframe 53,393 hrs · 30,749 cycles

REF SAD 4745257: EXTERIOR FUSELAGE STA 727E+13 IS DENTED ABOVE STR 26L DENT IS CREASED, REMOVED THE DAMAGE FABBED FILLER, DOUBLER, TRIPLER & INSTALLED REPAIR PARTS IAW SRM 53-00-01 REPAIR PG 231-233.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,627 hrs · 28,594 cycles

INTERCOSTAL CRACKED. CRACKED INTERCOSTAL REPLACED WITH NEW PART IAW SRM 51-40-05 AND 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,627 hrs · 28,594 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,627 hrs · 28,594 cycles

FLOOR SUPPORT CORRODED. FLOOR SUPPORT REPLACED WITH NEW PART IAW SRM 51-40-02 AND 51-40-05.

Part: SLAT — DEBONDED (NR 2) · airframe 49,627 hrs · 28,594 cycles

HL NR 2 LEADING EDGE SLAT UPPER I/B TRAILING EDGE CORNER DISBONDED. REPAIRED IAW SRM 51-70-10 REPAIR NR 4.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,627 hrs · 28,594 cycles

CORROSION FOUND ON R2 SILL CHORD. CORRODED SILL CHORD REPLACED WITH NEW PART IAW SRM 51-40-05 AND 51-40-02.

Part: TIE CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,627 hrs · 28,594 cycles

TIE CLIP CORRODED. REPLACED TIE CLIP WITH FABRICATED REPAIR PART IAW SRM 51-40-02 AND 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,627 hrs · 28,594 cycles

AFT CABIN CORROSION FOUND ON FLOOR SUPPORT ANGLE. CORRODED FLOOR ANGLE REPLACED WITH FABRICATED REPAIR PART IAW SRM 53-60-51 FIG 20, 51-40-05 AND 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,627 hrs · 28,594 cycles

CORROSION ON FLOORBEAM. REPAIRED CORRODED FLOORBEAM IAW EA 5310 02713.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,627 hrs · 28,594 cycles

AFT CARGO PIT RIGHT BULKHEAD PANEL LWR SUPPORT ANGLE LWR SURFACE CORRODED. CORRODED SUPPORT ANGLE REPLACED WITH FABRICATED REPAIR PART IAW SRM 51-30-01, 51-40-02, 51-40-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,627 hrs · 28,594 cycles

INTERCOSTAL CRACKED. CRACKED INTERCOSTAL REPLACED WITH NEW ONE IAW SRM 51-40-05 AND 51-40-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,627 hrs · 28,594 cycles

STR 11L FOUND CRACKED AT FASTENER HOLES. CRACK REPAIRED IAW EA 5310 02714.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,627 hrs · 28,594 cycles

INTERCOSTAL SHEAR CLIP CRACKED. SHEAR CLIP REPLACED WITH FABRICATED REPAIR PART AT INTERCOSTAL IAW EA 5310 02714.

Part: SKIN — CRACKED (RT WING) · airframe 49,627 hrs · 28,594 cycles

RIGHT WING O/B LEADING EDGE AT WS 290 FIXED LEADING EDGE SKIN CRACKED. FIXED LEADING EDGE SKIN REPAIRED IAW SRM 51-70-17.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,627 hrs · 28,594 cycles

L2 DOORWAY LOWER SILL CHORD CORROSION FOUND. REPLACED LWR SILL CHORD WITH NEW PART IAW SRM 51-40-05 AND 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,627 hrs · 28,594 cycles

INTERCOSTAL BETWEEN FRAMES CRACKED AT FWD END. REMOVED AND REPLACED CRACKED INTERCOSTAL PER SRM 51-30-01 AND 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,627 hrs · 28,594 cycles

FRAME CRACKED AT 37L INTERCOSTAL ATTACHMENT HOLE. FRAME REPAIRED IAW EA 5310 02714.

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

THE LEFT KEEL BEAM LWR CHORD IS CORRODED CLOSE TO THE BS 540 BUTT JOINT. KEEL BEAM REPAIRED WITH REPAIR PART IAW EA 5310 02688.

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

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

Part: SKIN — DENTED (BS 800 S26R) · airframe 45,915 hrs · 26,554 cycles

FOUND FUSELAGE SKIN DENTED OUT OF LIMITS AT STA 800 UNDER AFT CARGO DOOR CUTOUT. REMOVED DAMAGED SECTION OF SKIN FABRICATED AND INSTALLED REPAIR STRAP FILLERS DOUBLERS AND TRIPLERS IAW ASA EA 5330 02050.

Part: SKIN — DENTED (BS 810 S26L) · airframe 45,915 hrs · 26,554 cycles

FOUND FUSELAGE SKIN DENTED OUT OF LIMITS AT BSTA 810 UNDER AFT CARGO DOOR CUTOUT. REMOVED DAMAGED SECTION OF SKIN FABRICATED AND INSTALLED REPAIR STRAP FILLERS DOUBLERS AND TRIPLERS PER ASA EA 5330 02050.

Part: BEAR STRAP — CORRODED (BS 767-787) · airframe 45,915 hrs · 26,554 cycles

AFT CARGO BAY BEAR STRAP DOUBLER IS CORRODED OUT OF LIMITS IN 3 LOCATIONS AT RBL 22 BETWEEN BS 767 & 787. REMOVED DAMAGED SECTION OF BEARSTRAP FABRICATED REPAIR STRAP FILLERS DOUBLERS TRIPLERS AND INSTALLED REPAIR PIECES IAW ASA EA 5330 02050.

Part: SKIN — PUNCTURED (T/E FLAP) · airframe 45,911 hrs · 26,553 cycles

THE RT INBD MIDFLAP T/E IS PUNCTURED ON THE LWR SURFACE. REMOVED DAMAGED AREAS OF LWR SKIN FABRICATED AND INSTALLED TWO FILLERS AND TWO DOUBLERS IAW SRM 51 70 10 PARA 7 8 12 15 AND 20.

Part: FRAME — CORRODED (FUSELAGE) · airframe 45,911 hrs · 26,553 cycles

FRAME CORRODED OUT OF LIMITS.

Part: TAB — DELAMINATED (ELEVATOR) · airframe 45,911 hrs · 26,553 cycles

RT ELEV TAB IS DELAMINATED ALONG THE TRAILING EDGE. REMOVED DAMAGED AREA OF TAB SURFACE PLY FABRICATED AND APPLIED ONE REPAIR PLY AND TWO SANDING PLIES IAW SRM 51 70 04 REPAIR 9. SANDED SMOOTH AND RESTORED FINISH.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 45,911 hrs · 26,553 cycles

LT CREASE BEAM SHEAR WEB IS CORRODED OUT OF LIMITS.

Part: BULKHEAD — GOUGED (FUSELAGE)

PAE - BS 178 AFT PRESSURE BULKHEAD SKIN GOUGED AT LBL 25 WL 206. REPAIRED IAW EA AND ER. (K)

Part: FRAME — DAMAGED (RT FAIRING)

PAE - RT AFT WING -TO-BODY FAIRING FORMER HOLES ELONGATED. REMOVED AND INSTALLED NEW T-ANGLE IAW SRM. (K)

Part: SKIN — DENTED (FUSELAGE)

PAE - EXTERNAL SKIN DENTED AT BS791, RBL61, WL193, JUST FORWARD OF AFT CARGO DOOR. REPAIRED DENT ON EXTERNAL SKIN B-STA791, RBL 61, WL 193, IAW EA. (K)

Part: STOP FITTING — GOUGED (CARGO DOOR)

PAE - AFT CARGO BAY FWD CTR DOOR STOP FITTING HAS MECHANICAL DAMAGE. REPLACED IAW SOPM. (K)

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2

PAE - CORROSION AFT CARGO BAY, ON FLOOR TO SIDEWALL SUPPORT RT FROM BS 867-887. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. (K)

Part: LIGHT — DISCONNECTED (ROW 15-16)

FOUND EMERGENCY EXIT FLOOR LIGHTING AT ROW 15-16 HAVE COME APART AND UNPLUGGED. INSTALLED LAMP ASSEMBLY AT ROW 16 PER AMM 33-51-02. OPS CHECK GOOD. (M)

Part: CONNECTOR — UNSECURE (CABIN)

BUR - DURING MAINTENANCE, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 20-23. RE-SECURED AND CONNECTED FLOOR TRACK WIRING. OPERATIONAL CHECKED GOOD. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

ANC - DURING LINE CHECK, FOUND NEAR ROW 13 FLOOR TRACK LIGHTING INOPERATIVE. REATTACHED LOOSE CONNECTION, SYSTEM OPERATIONAL CHECKED GOOD. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

ANC - DURING LINE CHECK, FOUND NEAR ROW 14-19 FLOOR TRACK LIGHTING INOPERATIVE. REATTACHED LOOSE CONNECTION, REPLACED LAMP, SYSTEM OPERATIONAL CHECKED GOOD. (M)

Part: SUPPORT — GOUGED (NR 2 NACELLE)

GYR - DURING SI CHECK FOUND SUPPORT CHORD GOUGED ON NR 2 PYLON AT NAC 166.5 TO 196. REPAIRED IAW EA. (M)

Part: FITTING — GOUGED (LT ELEVATOR)

GYR - DURING SI CHECK, FOUND LEFT ELEVATOR HINGE FITTING WORN AT STAB STA 213.43. REPAIRED IAW EA. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

GYR - DURING SI CHECK, FOUND DOUBLER AT STATION 907 IS CORRODED. REPAIRED IAW SRM. (M)

Part: SKIN — GOUGED (FUSELAGE)

GYR - DURING SI CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 793. REPAIRED IAW EA. (M)

Part: ATTACH ANGLE — CRACKED (RT WING)

GYR - DURING SI CHECK, RT WING FUEL TANK RIB ATTACH ANGLE CRACKED AT STATION 135.5. REPAIRED IAW EA. (M)

Part: SKIN — DELAMINATED (L/E SLAT)

PAE - DURING C-CHECK, FOUND LEFT NR 2 SLAT UPPER AND LOWER TRAILING EDGE WEDGE SKIN IS DELAMINATED AT OUTBOARD END. REPAIRED IAW SRM. (M)

Part: ANGLE — CRACKED (WING)

PAE - DURING C-CHECK, FOUND NR 3 IFOT FAIRING HAS A CRACKED ANGLE OUTBOARD OF SIDE UPPER EDGED JUST INBOARD OF NR 3 SPOILER. REMOVED AND REPLACED ANGLE IAW SRM. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

PAE - DURING C-CHECK, FOUND INTERCOSTAL BETWEEN BS 747 TO 767 CRACKED. REMOVED, FABRICATED AND INSTALLED NEW PART IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY RIGHT FLOOR TO SIDEWALL SUPPORT PLATE IS CORRODED AT BS 727 TO 767 AND RBL 17. REMOVED CORRODED PLATE, FABRICATED NEW FLOOR TO SIDEWALL SUPPORT AND INSTALLED IAW SRM. (M)

Part: FAILSAFE — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON FAIL/SAFE AT BL 0 BS 767 AND WL 149. REMOVED AND FABRICATED NEW SECTION IAW SRM. (M)

Part: HINGE — DAMAGED (SPOILER)

PAE - DURING C-CHECK, FOUND DAMAGE ON UPPER SURFACE OF SPOILER HINGE WEB AT INBOARD CORNER OF NR 2 SPOILER. REMOVED AND REPLACED IAW SRM. (M)

Part: SKIN — CRACKED (L/E SLAT)

PAE - DURING C-CHECK, FOUND NR 6 SLAT EXTERNAL SKIN IS CRACKED ON LOWER L/E AT FASTENERS AT OUTBOARD END. REPAIRED IAW SRM. (M)

Part: ANGLE — CRACKED (FUSELAGE)

PAE - DURING C-CHECK, FOUND WIPER WEB LEFT ANGLE IS CRACKED. REMOVED, FABRICATED NEW AND INSTALLED PART IAW SRM. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY LEFT FLOOR TO SIDEWALL SUPPORT PLATE AT BS 727 TO 727E IS CORRODED. REMOVED AND FABRICATED NEW AND INSTALLED IAW SRM. (M)

Part: SUPPORT — CORRODED (SIDE WALL)

DURING C CHECK FOUND AFT CARGO BAY LEFT HAND FLOOR TO SIDE WALL SUPPORT PLATE AT BS 727 TO 947 IS CORRODED. REMOVED AND FABRICATED NEW IAW SRM.

Part: WEB — CRACKED (CARGO BAY)

DURING C CHECK FOUND AFT CARGO BAY WEB CRACKED AT BS 794.5 AND STR 25R.

Part: SKIN — GOUGED (BS 934.1)

DURING C CHECK FOUND FUSELAGE SKIN GOUGED AT BS 934.1INCH BELOW STRINGER 16R. REMOVED AND FABRICATED NEW SKIN IAW SRM.

Part: INVERTER — FAULTY (E/E BAY)

SEA - DURING LINE MAINTENANCE IT WAS NOTICED THAT SMOKE WAS COMING FROM THE E/E BAY AREA. IT WAS FOUND THAT THE STATIC INVERTER HAD A COMBUSTION EVENT. CLEANED THE E3-1 RACK, REPLACED THE STATIC INVERTER, BATTERY CHARGER, BOTH TR'S, AND THE MOISTURE SHROUD. REMOVED AND REINSTALLED SEVERAL OTHER COMPONENTS TO ALLOW THE CLEANING OF THE RACKS. OPS CHECKED AFFECTED SYSTEMS, ALL OPERATIONS WERE NORMAL. (M)

Part: SKIN — CRACKED (CARGO DOOR)

PAE - DURING CHECK FORWARD CARGO DOOR INNER SKIN FOUND CRACK AT CONTROL ROD ACCESS PANEL. REPAIRED IAW SRM. (M)

Part: SKIN — DENTED (CARGO DOOR)

PAE - DURING CHECK FOUND, NUMEROUS DENTS IN FORWARD CARGO DOOR OUTER SKIN. REMOVED AND REPLACED SKIN IAW SRM. (M)

Part: WIRE — DISCONNECTED (MID CABIN)

PDX - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 13-15. RECONNECTED WIRES. TRACK LIGHTS THEN OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS NEAR ROW 1 INOPERATIVE. REATTACHED WIRES ON INOPERATIVE SECTIONS. OPERATIONAL CHECKED GOOD. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SEA - DURING C-CHECK, FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STATION 857 LBL 12.50. REPAIRED IAW ENGINEERING AUTHORIZATION. (M)

Part: THRUST REVERSER — WORN (RT ENGINE)

SEA - DURING C-CHECK, FOUND RIGHT ENGINE THRUST REVERSER BULLNOSE WORN IN SEVERAL AREAS FROM CONTACT WITH BLOCKER DOORS AT THE NR 1, 3 AND 5 O'CLOCK POSITIONS. REPAIRED IAW ENGINEERING AUTHORIZATION. (M)

Part: ATTACH FITTING — GOUGED (HORIZ STAB)

SEA - DURING C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER AFT SPAR ATTACH FITTING UPPER LUG ON FUSELAGE GOUGED. REPAIRED IAW ENGINEERING AUTHORIZATION. (M)

Part: COWLING — DAMAGED (RT ENGINE)

PAE - DURING C-CHECK, FOUND RIGHT ENGINE INLET COWL OUTSIDE RIGHT SURFACE DAMAGED AT 4 O'CLOCK AND 6 INCHES FORWARD OF AFT FLANGE. REPAIRED IAW ENGINEERING AUTHORIZATION. (M)

Part: STRUCTURE — DAMAGED (NR 2 PYLON)

SEA - DURING C-CHECK, FOUND RIGHT ENGINE STRUT PYLON NR 2 CROWN BEAM AFT BEARING BORE HAS PITTING ON INNER SURFACE. REPAIRED IAW ENGINEERING AUTHORIZATION. (M)

Part: SKIN — CORRODED (FUSELAGE)

SEA - DURING SCHEDULED C-CHECK, THE AFT CARGO DOOR CUTOUT EDGE WAS FOUND TO BE CORRODED. REPAIRED PER EA 5330-01431. (M)

Part: WEB — CRACKED (RUDDER)

SEA - DURING SCHEDULED C-CHECK, THE RUDDER LOWER WEB WAS FOUND TO BE CRACKED. REPAIRED PER EA 5540-01047. (M)

Part: PLATE — BROKEN (STABILIZER)

SEA - DURING SCHEDULED C-CHECK, THE STABILIZER TRIM CABLE GUIDE PLATE WAS FOUND TO BE BROKEN AT STATION 1024 RIGHT SIDE. REPAIRED PER EA 2740-01047. (M)

Part: FLAP TRACK — CORRODED (NR 2)

SEA - DURING SCHEDULED C-CHECK, THE NR 2 FLAP TRACK WAS FOUND TO BE PITTED AND CORRODED. REPAIRED PER EA 5750-01408. (M)

Part: FLAP TRACK — WORN (NR 6)

SEA - DURING SCHEDULED C-CHECK, THE NR 6 FLAP TRACK WAS FOUND TO BE WORN. REPAIRED PER EA 5750-01404. (M)

Part: FLAP TRACK — CORRODED (NR 4)

SEA - DURING SCHEDULED C-CHECK, THE NR 4 FLAP TRACK WAS FOUND TO BE WORN AND CORRODED. REPAIRED PER EA 5750-01406. (M)

Part: RIB — BENT (THRUST REVERSER)

SEA - DURING SCHEDULED C-CHECK, THE NR 2 ENGINE INBOARD THRUST REVERSER FIFTH RIB WAS FOUND TO BE BENT AND SCRATCHED. REPAIRED PER EA 7830-01112. (M)

Part: SLIDE — FAILED (SERVICE DOOR)

SEA - DURING C-CHECK, THE L-2 SLIDE FAILED TO INFLATE DURING TEST. REPLACED SLIDE ASSEMBLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, MULTIPLE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN THE FORWARD CABIN. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)

Part: SUPPORT — CORRODED (BS 867-947)

PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT FROM STATION 867-947 STRINGER 25R WAS FOUND TO BE CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-02 AND 53-60-53. (M)

Part: SUPPORT — CORRODED (BS 947-967)

PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOOR SUPPORT BETWEEN STATION 947-967 LBL 16 WAS FOUND TO BE CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-01. (M)

Part: SUPPORT — CORRODED (BS 967-987)

PHX - DURING SCHEDULED SI, THE FLOOR SUPPORT AT STATION 967-987 RBL 16 WAS CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-00. (M)

Part: SUPPORT — CORRODED (BS 727-769)

PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 727C-769 STRINGER 25R WAS CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-02 AND 53-60-53. (M)

Part: SUPPORT — CORRODED (BS 303-348)

PHX - DURING SCHEDULED SI, THE FLOOR SUPPORT AT BS 303-348 LBL 70.53 WAS FOUND TO BE CORRODED. REPLACED CHORD PER SRM 51-40-2. (M)

Part: SUPPORT — CORRODED (BS 727)

PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 727B-727E STRINGER 25L WAS CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-02 AND 53-60-53. (M)

Part: SUPPORT — CORRODED (BS 867-947)

PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 867-947 STRINGER 25R WAS CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-02 AND 53-60-53. (M)

Part: SEAT TRACK — CORRODED (BS 480-500)

PHX - DURING SCHEDULED SI, FOUND CORROSION ON THE RIGHT OUTBOARD SEAT TRACK AT STATION 480-500A. REPLACED SEAT TRACK PER SRM 53-30-52. (M)

Part: FLOORBEAM — CORRODED (BS 987)

PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOORBEAM AT STATION 987 LBL 36 - RBL 43 WAS FOUND TO BE CORRODED. REPAIRED FLOORBEAM PER EA 5310-01641. (M)

Part: FLOORBEAM — CORRODED (BS 344)

PHX - DURING SCHEDULED SI, THE FORWARD CABIN UPPER SURFACE FLOORBEAM AT STATION 344 LBL 14-55 WAS FOUND TO BE CORRODED. REPLACED UPPER CHORD FLOORBEAM PER SRM 53-10-51. (M)

Part: FLOORBEAM — CORRODED (BS 947)

PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOORBEAM AT STATION 947 LBL 4 AND RBL 5 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01642. (M)

Part: SKIN — DENTED (LT TE FLAP)

PHX - DURING SCHEDULED SI, THE LEFT WING T/E INBOARD FOREFLAP LOWER SURFACE WAS FOUND TO HAVE THREE DENTS. REPAIRED PER SRM 57-53-02 AND SRM 51-70-10 REPAIR NR 20. (M)

Part: SEAT TRACK — CORRODED (BS 360-500)

PHX - DURING SCHEDULED SI, THE RIGHT INBOARD SEAT TRACK FROM STATION 360-500E WAS FOUND TO BE CORRODED. REPLACED SEAT TRACK PER SRM 53-00-52. (M)

Part: INTERCOSTAL — CRACKED (BS 294.5-312)

PHX - DURING SCHEDULED SI, THE INTERCOSTAL AT BS 294.5-312 STRINGER 4L WAS FOUND TO BE CRACKED. REPLACED INTERCOSTAL PER SRM 51-40-2. (M)

Part: FLOORBEAM — CORRODED (BS 312)

PHX - DURING SCHEDULED SI, THE FORWARD CABIN UPPER SURFACE FLOORBEAM AT STATION 312 LBL 13 - RBL 10 WAS FOUND TO BE CORRODED. REPLACED T-CHORD PER SRM 53-10-51. (M)

Part: FLOORBEAM — CORRODED (BS 360)

PHX - DURING SCHEDULED SI, THE FLOORBEAM AT STATION 360 RBL 20-30 WAS FOUND TO BE CORRODED. REPLACED FLOORBEAM SECTION PER SRM 53-00-51. (M)

Part: SUPPORT — CORRODED (BS 312-328)

PHX - DURING SCHEDULED SI, THE FORWARD CABIN UPPER SURFACE FLOOR SUPPORT AT STATION 312-328 LBL 13 WAS FOUND TO BE CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-30-02 AND 51-40-02. (M)

Part: SUPPORT — CORRODED (BS 947-967)

PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOOR SUPPORT BETWEEN STATION 947-967 LBL 24 WAS FOUND TO BE CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-01. (M)

Part: SUPPORT — CORRODED (BS 947-967)

PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOOR SUPPORT AT STATION 947-967 RBL 16 WAS FOUND TO BE CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-00. (M)

Part: FLOORBEAM — CORRODED (BS 967)

PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOORBEAM AT STATION 967 RBL 18 WAS FOUND TO BE CORRODED. INSTALLED REPAIR SECTION, SPLICE AND STRAP PER SRM 53-00-51. (M)

Part: SUPPORT — CORRODED (BS 727-807)

PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 727B-807 STRINGER 25L WAS CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-02 AND 53-60-53. (M)

Part: FLOORBEAM — CORRODED (BS 1016)

PHX - DURING SCHEDULED SI, THE UPPER SURFACE OF THE FLOORBEAM AT STATION 1016 LBL 29 WAS FOUND TO BE CORRODED. REPAIRED PER SRM 53-00-51. (M)

Part: INTERCOSTAL — CORRODED (BS 1016)

PHX - DURING SCHEDULED SI, THE UPPER SURFACE OF THE INTERCOSTAL AT STATION 1016 RBL 27 WAS CORRODED. REPLACED STRAP PER SRM 51-40-02. (M)

Part: SUPPORT — CORRODED (BS 947)

PHX - DURING SCHEDULED SI, THE AFT CABIN UPPER SURFACE FLOOR SUPPORT AT STATION 947 BETWEEN RBL 24 AND RBL 50 WAS FOUND TO BE CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-02. (M)

Part: SUPPORT — CORRODED (BS 54)

PHX - DURING SCHEDULED SI, THE FLOOR SUPPORT AT BS 334 RBL 54 WAS FOUND TO BE CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-30-02. (M)

Part: SKIN — WORN (LT TE MIDFLAP)

PHX - DURING SCHEDULED SI, THE LEFT WING OUTBOARD T/E MIDFLAP WAS FOUND TO BE WORN AT THE LEADING EDGE. REPAIRED PER EA 5750-01311. (M)

Part: SUPPORT — CORRODED (BS 328-344)

PHX - DURING SCHEDULED SI, THE UPPER SURFACE SUPPORT AT STATION 328-344 LBL 13 WAS CORRODED. REPLACED SUPPORT PER SRM 51-40-2. (M)

Part: SUPPORT — CORRODED (BS 947)

PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 947 STRINGER 26R WAS FOUND TO BE CORRODED. REPAIRED SECTION PER 53-00-53. (M)

Part: SUPPORT — CORRODED (BS 967-987)

PHX - DURING SCHEDULED SI, THE UPPER SURFACE OF THE FLOOR SUPPORT AT STATION 967-987 LBL 16 WAS CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-00. (M)

Part: SUPPORT — CORRODED (BS 947)

PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 947 BETWEEN STRINGER 25L AND 26L WAS FOUND TO BE CORRODED. REPAIRED SECTION PER 53-00-53. (M)

Part: SUPPORT — CORRODED (BS 807-947)

PHX - DURING SCHEDULED SI, THE AFT CARGO COMPARTMENT FLOOR SUPPORT AT STATION 947-807 STRINGER 25L WAS CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-40-02 AND 53-60-53. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS FAILED TO TEST. REPLACED ALL BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M)

Part: FITTING — WORN (RT WING)

SEA - DURING C-CHECK, WEAR WAS FOUND ON THE LOWER SURFACE OF THE UPPER FLANGE ON THE RT WING T/E RIB FITTING. REPAIRED PER EA 5750-01269 AND BOEING TELEX M-7200-98-00052. (M)

Part: BELLCRANK — MISMANUFACTURED (TE FLAP)

SEA - DURING C-CHECK, THE BELLCRANK ASSEMBLY ON THE OUTBOARD AFT FLAP IS MISSING DRAIN HOLE. REPAIRED PER EA 2750-01036. (M)

Part: SKIN — WORN (LT PYLON)

SEA - DURING C-CHECK, WEAR WAS FOUND ON THE LEFT ENGINE PYLON SKIN. REPAIRED PER EA 5450-01012 AND BOEING TELEX ASA-SEA-97-0507RR. (M)

Part: SLIDE — MISINSTALLED (LT AFT DOOR)

OAK - DURING C-CHECK, DURING THE REINSTALLATION OF THE LEFT AFT DOOR EMERGENCY EXIT SLIDE, THE SLIDE WAS FOUND TO HAVE HAD A RED SECURING STRAP WRAPPED AROUND THE SLIDE. REMOVED STRAP AND COMPLETED SLIDE INSTALLATION. (M)

Part: CHARGER — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE L-2 DOOR EMERGENCY EXIT IDENTIFIER WAS FOUND INOPERATIVE. REPLACED PACK CHARGER AND LIGHT OPERATED NORMALLY. (X)

Part: CONNECTOR — LOOSE (CABIN)

ANC - MAINTENANCE CHECK, FOUND EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 27 AFT. RESEATED CONNECTOR/WIRING AT ROW 27 AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

JNU - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED 4TH FROM LAST LAMP BASE AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED TRACK LIGHT WIRING, REPLACED LENS AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL WIRING — DISCONNECTED (CABIN)

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

Part: EEL ASSY — INOPERATIVE (CABIN)

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

Part: EEL WIRING — DISCONNECTED (MAIN CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 19-22 WERE FOUND INOPERATIVE. RELAMPED DEFECTIVE LIGHT AND RECONNECTED WIRING. LIGHTS OPERATED NORMALLY. REFERENCE NR ASAA9540054.

Part: EEL LAMP — FAILED (MAIN CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 19-22 WERE FOUND INOPERATIVE. RELAMPED DEFECTIVE LIGHT AND RECONNECTED WIRING. LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - CHECK, AFT TWO RED TRACK LIGHTS INOP. MAINTENANCE RECONNECTED LIGHTS. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - PILOT REPORTED, AFT TWO EMERGENCY TRACK LIGHTS INOP. MAINTENANCE RECONNECTED WIRES. (Z)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - AT CHECK, AFT 2 EMERGENCY TRACK LIGHTS INOP. MAINTENANCE SECURED LIGHT HARNESS TO LIGHT ASSY. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING CHECK, THE LAST 2 EMERGENCY TRACK LIGHTS INOP. MAINTENANCE RECONNECTED WIRING AND OPS CHECKED NORMAL. (W)