N767AS

Part: GATE — CRACKED (L2 DOOR LOWER) · airframe 75,750 hrs · 44,089 cycles

CRACK FOUND ON L2 DOOR LOWER GATE, AFT END. ACFT GROUNDED. REPLACED THE DOOR GATE.

Part: DOUBLER — CORRODED (NR 3 SLAT) · corrosion level 2 · airframe 74,648 hrs · 43,240 cycles

NR 3 SLAT TAI DUCT NOSE BEAM DOUBLER CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE SLAT TAI DUCT NOSE BEAM DOUBLER IAW SRM 51-40-02-0G-0.

Part: FITTING — CORRODED (NLG) · corrosion level 2 · airframe 74,648 hrs · 43,240 cycles

NLG DOWNLOCK ACTUATOR LT AND RT ATTACH FITTINGS HAVE CORR IN BUSHING LUGS. GROUNDED - YES. REMOVED AND REPLACED LT AND RT FITTINGS IAW SRM 51-40-02-0G-0.

Part: SUPPORT — CORRODED (BS 227) · corrosion level 2 · airframe 74,648 hrs · 43,240 cycles

AT FWD SIDE OF BS 227 BULKHEAD LOWER LT DOOR STOP BACKUP SUPPORT FITTING EXFOLIATED PANEL RACK. ACFT GROUNDED. FABRICATED A NEW SUPPORT IAW SRM 51-40-06-0G-0 AND BDWG 65-45801.

Part: ATTACH ANGLE — CRACKED (BS 277) · airframe 74,648 hrs · 43,240 cycles

STRINGER 10R ATTACH ANGLE CRACKED AT BS 277. ACFT GROUNDED. REMOVED AND REPLACED THE STRINGER ATTACH ANGLE IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (BS 277) · airframe 74,648 hrs · 43,240 cycles

INTERCOSTAL IS CRACKED AT BS 277, STRINGER 14R, APPROXIMATELY .050 INCHES AT FORWARD RADIUS TRIMOUT. ACFT GROUNDED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: FITTING — CRACKED (RT SPOILER HINGE) · airframe 74,648 hrs · 43,240 cycles

RIGHT INBD NR 5 GROUND SPOILER INBD ACTUATOR HINGE FITTING LUG IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE FITTING IAW SRM 51-10-02.

Part: FRAME — CORRODED (BS 227 BULKHEAD) · corrosion level 2 · airframe 74,648 hrs · 43,240 cycles

FWD SIDE OF BS 227 BULKHEAD LOWER FRAME IS CORRODED AT BL0 TO RBL5. ACFT GROUNDED. REPAIRED IAW SRM 53-10-08-2R-13.

Part: STIFFENER — CORRODED (BS 227) · corrosion level 2 · airframe 74,648 hrs · 43,240 cycles

FRAME AFT OF FWD ACCESSORY DOOR CUTOUT HAS CORROSION. ACFT GROUNDED. REMOVED, FABRICATED, AND INSTALLED A NEW VERTICAL STIFFENER IAW SRM 51-40-05-0G-0 AND DWG AND10137.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 73,058 hrs · 42,154 cycles

L1, L2, AND R2 DOOR EMERGENCY EXIT SIGN LAMPS INOPERATIVE AND RT AFT OVERWING EMERGENCY EXIT HANDLE LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS. OPS CHECKED NORMAL.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 74,647 hrs · 43,240 cycles

NR 3 SLAT OTBD AUX TRACK LOWER SKIN CRACKED. ACFT GROUNDED.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 72,361 hrs · 41,723 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN AT R-1 DOOR HAS BROKEN LENS. ACFT GROUNDED. R & R LENS AND TESTED LIGHT ASSY IAW AMM 33-51-81-962-011. OPS NORMAL.

Part: SKIN — CRACKED (BS 727C-727D) · airframe 72,330 hrs · 41,706 cycles

CRACK IN FUSELAGE SKIN AT EDGE OF BONDED DOUBLER, BS 727D+2 AND STR 23R. ACFT GROUNDED. REPAIRED SKIN CRACK IN FUSELAGE SKIN AT EDGE OF BONDED DOUBLER AT BS 727D+2 AND STR 23R IAW SRM 53 00 01, R31 DETAIL IX THIS IS A CATEGORY A REPAIR.

Part: SUPPORT ANGLE — CRACKED (BS 727D) · airframe 72,330 hrs · 41,706 cycles

AFT CARGO COMPT VHF 3 SUPPORT ANGLE IS CRACKED BETWEEN 727D AND 727E WHERE IT ATTACHES TO CHANNEL ON LT SIDE. ACFT GROUNDED. R & R NR 3 VHF SUPPORT ANGLE IAW EA 400-53EA-16633.

Part: FRAME — CRACKED (BS 500B) · airframe 72,330 hrs · 41,706 cycles

FRAME AT BS 500B, RT WIRE PENETRATION HOLE IS CRACKED BETWEEN STR 20 AND 21R. ACFT GROUNDED. REPAIRED FRAME 500B RT IAW SRM 53-00-07-2R-20, THIS IS A CATEGORY B REPAIR WITH A THRESHOLD OF 66000 CYCLES AND A INTERVAL OF 24,000 CYCLES.

Part: FRAME — CRACKED (BS 500B) · airframe 72,330 hrs · 41,706 cycles

FRAME AT BS 500B LT WIRE PENETRATION HOLE IS CRACKED BETWEEN STR 20 AND 21L. ACFT GROUNDED. REPAIRED FRAME 500B LT IAW SRM 53-00-07-2R-20. THIS IS A CATEGORY B REPAIR WITH A THRESHOLD OF 66000 CYCLES AND A INTERVAL OF 24,000 CYCLES. CYCLES AT TIME OF REPAIR 41706.

Part: CARGO TRACK — CRACKED (BS 727C) · airframe 69,221 hrs · 39,732 cycles

AFT CARGO BAY LT CARGO TRACK AT BS 727C IS CRACKED IN THE RADIUS. ACFT GROUNDED. REPAIRED THE DAMAGE IAW SRM 53-00-53-2R-2.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 69,221 hrs · 39,732 cycles

FLOORBEAM BS 540, RBL 24 TO BL 0 IS CRACKED ON UNDER SIDE AROUND FASTENER HOLE. ACFT GROUNDED. R & R FLOORBEAM IAW SRM 51-40-02-0G-0 AND AMM 20-50-11-912-002.

Part: SHEAR TIE — CRACKED (BS 847) · airframe 69,221 hrs · 39,732 cycles

AFT CARGO BAY SHEAR TIE, BS 847 S24 - 25L CRACKED. ACFT GROUNDED. REPAIRED THE SHEAR TIE IAW SRM 53-00-07-2R-7, REPAIR 7, CATEGORY B.

Part: CHANNEL — CORRODED (BS 986-989) · corrosion level 2 · airframe 69,221 hrs · 39,732 cycles

AFT DRAIN MAST SUPPORT CHANNEL HAS CORROSION ON INTERNAL SURFACE. ACFT GROUNDED. R & R AFT DRAIN MAST SUPPORT CHANNEL IAW EA 400, 53 EA 13935.

Part: FRAME — CORRODED (BS 927) · corrosion level 2 · airframe 69,221 hrs · 39,732 cycles

AFT CARGO LOWER FRAME BS 927 HAS MULTIPLE AREAS OF CORROSION FROM SPLICE TO SPLICE. ACFT GROUNDED. REPAIRED IAW EA 400, 53 EA 13932.

Part: CARGO TRACK — CORRODED (BS 727F) · corrosion level 2 · airframe 69,221 hrs · 39,732 cycles

AFT CARGO TRACK LBL 17.2 CORRODED AT BS 727F+8. ACFT GROUNDED. REPAIRED THE CARGO TRACK IAW EA 400 53, EA 13978.

Part: STIFFENER — CORRODED (BS 1088) · corrosion level 2 · airframe 69,221 hrs · 39,732 cycles

AFT FUSELAGE COMPARTMENT BULKHEAD INBD FLANGE FOR APU INLET IS CORRODED AT STA 1088. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-40-02-0G-0, W 1, O .070, R .046, L 1.5, D .024.

Part: CARGO TRACK — CORRODED (BS 757-877) · corrosion level 2 · airframe 69,221 hrs · 39,732 cycles

CARGO TRACK, RBL 13.8 HAS MULTIPLE AREAS OF CORROSION BS 757 - 877. ACFT GROUNDED. CUT OUT AND REPLACED DAMAGED SECTION OF CARGO TRACK IAW SRM 53-00-53-2R-2 AND EA 400, 53 & EA, 13968.

Part: SKIN — CORRODED (BS 493) · corrosion level 2 · airframe 69,221 hrs · 39,732 cycles

FUSELAGE SKIN IS CORRODED INSIDE FWD CARGO DOOR CUTOUT, LOWER AFT CORNER. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A-1. REPAIRED SKIN IAW SRM 53-00-01-2R-3R. THIS IS A CAT B REPAIR. FURTHER INSPECTIONS ARE AS GIVEN IN SB 737 53A1228, W 2", O .112, R .050, L 2", D .062.

Part: ANGLE — CRACKED (BS 296) · airframe 69,221 hrs · 39,732 cycles

ANGLE AT FWD SIDE OF THE R1 DOOR BS 296 AT S11R IS CRACKED. ACFT GROUNDED. R & R THE ANGLE IAW SRM 51-40-04-0G-0.

Part: SHEAR TIE — CORRODED (BS 847) · corrosion level 2 · airframe 69,221 hrs · 39,732 cycles

AFT CARGO BAY SHEAR TIE BS 847 S27L - 27R IS CORRODED. ACFT GROUNDED. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM 51-10-0G-0. REPAIRED DAMAGE IAW SRM 53-00-07-2R-3 CATEGORY B REPAIR.

Part: BULKHEAD WEB — CORRODED (BS 1016) · corrosion level 2 · airframe 69,221 hrs · 39,732 cycles

AFT PRESSURE BULKHEAD FWD SIDE HAS LIGHT SURFACE CORRODED AROUND FASTENER AT LBL 2, BS 1016. ACFT GROUNDED. REPAIRED BULKHEAD WEB IAW EA 400 53, EA 13975 .

Part: INTERCOSTAL — CRACKED (BS 927-947) · airframe 69,221 hrs · 39,732 cycles

AFT WET AREA INTERCOSTAL AT BL 0 LOCATED BETWEEN S 927 AND 947.5 HAS CRACK ON TOP SUPPORT ANGLE. ACFT GROUNDED. R & R THE INTERCOSTAL SUPPORT ANGLE IAW SRM 51-40-02-0G-0.

Part: CHANNEL — CORRODED (MOP SILL) · airframe 69,221 hrs · 39,732 cycles

FWD ENTRYWAY L1 DOOR MOP SILL HAS SEVERAL AREAS OF CORROSION NEAR L1 ENTRYWAY. ACFT GROUNDED. REMOVED CORROSION ON L1 DOOR LOWER SILL INNER CHORD, MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-1, FIG 101. R & R CHORD IAW SRM 51-40-02-0G-0.

Part: CUSP WEB — CORRODED (BS 727D-727E) · corrosion level 2 · airframe 69,221 hrs · 39,732 cycles

RIGHT CUSP WEB HAS CORROSION BETWEEN FRAMES AT BS 727D AND 727E. ACFT GROUNDED. R & R THE CUSP WEB IAW SRM 51-40 02-0G-0 PARA 4.

Part: FRAME — CRACKED (BS 787) · airframe 69,221 hrs · 39,732 cycles

FRAME AT BS 787, RT IS CRACKED BETWEEN S8 - 9 RT. ACFT GROUNDED. FABRICATED, LOCATED, DRILLED AND INSTALLED A REPAIR IAW AD 20062609-400-53-1-767.

Part: CUSP WEB — CORRODED (BS 727E-727F) · corrosion level 2 · airframe 69,221 hrs · 39,732 cycles

RIGHT CUSP WEB HAS CORROSION BETWEEN FRAMES AT BS 727E AND 727F. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13-1A-1, DETAIL V. R & R CUSP WEB IAW SRM 51-40-02-0G-0 PARA 4.

Part: FRAME — CRACKED (BS 727) · airframe 69,221 hrs · 39,732 cycles

FRAME AT BS 727B, RT IS CRACKED BETWEEN S8 - 9 RT. ACFT GROUNDED. REPAIRED THE FRAME IAW AD20062609 400-53-1-767.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 69,221 hrs · 39,732 cycles

AFT WET AREA BS 986.5 AT RBL 30 AND 45 HAS SURFACE CORROSION ON TOP OF FLOORBEAM. ACFT GROUNDED. BLENDED DAMAGED AREA IAW SRM 51-10-02-0G-0 MATERIAL REMAINING IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-51-1A-1, REPAIRED DAMAGED AREA IAW EA 400-53EA-13928, REV NEW DATED 12DEC14 ORIGINAL MATERIAL THICKNESS .150 MATERIAL, REMAINING IS .108.

Part: CUSP WEB — CORRODED (BS 767-787) · corrosion level 2 · airframe 69,221 hrs · 39,732 cycles

RIGHT CUSP WEB HAS CORROSION BETWEEN FRAME AT FS 767 AND FS 787. ACFT GROUNDED. R & R CUSP WEB IAW SRM 51-40-02-0G-0.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 66,794 hrs · 38,235 cycles

L1 DOOR EXTERIOR SLIDE LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED LAMP AND R & R M1133 EMERGENCY BATTERY PACK. INSTALLATION OF M133 EMERGENCY BATTERY PACK AND L1 DOOR EXTERIOR SLIDE LIGHT GOOD IAW 33-51-22-962-001.

Part: FRAME — CRACKED (BS 500F) · airframe 66,794 hrs · 38,235 cycles

FWD CARGO BAY RT FRAME AT BS 500F CRACKED AROUND OLED. ACFT GROUNDED. REMOVED DAMAGE ON FRAME AND ACCOMPLISHED REPAIR ON FWD PIT RT FRAME AT STATION 500F IAW SRM 53-00-07. REPAIR 13, FIGURE 203, DETAIL 1. THIS IS A CATEGORY B REPAIR TO BE INSPECTED AT INTERVAL 24,000 FLIGHT CYCLES IAW STM 53-00-07. REPAIR 13, FIG 205, TABLE V.

Part: FRAME — CRACKED (BS 500C) · airframe 66,794 hrs · 38,235 cycles

FWD CARGO BAY FRAME AT BS 500C HAS CRACKS AROUND HOLE. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07-2R-13, REPAIR 13.

Part: WEB — CORRODED (BS 794-847) · corrosion level 2 · airframe 66,794 hrs · 38,235 cycles

AFT CARGO DOOR SILL WEB THRESHOLD CORRODED. ACFT GROUNDED. REMOVED AFT CARGO DOOR WEB IAW SRM 51-40-02 INSTALLED WEB ON AFT CARGO DOOR IAW DWG A-5330018186, REV NEW AND SRM 51-40-02 AND DWG 65-47957, REV D.

Part: SKIN — CRACKED (BS 927-969) · airframe 65,723 hrs · 37,532 cycles

FUSELAGE SKIN CRACKED AT L2 DOOR LWR FORWARD CUTOUT. ACFT GROUNDED. REPAIRED CRACKED SKIN IAW SRM 53-00-01-2R-32.

Part: ESCAPE ROPE — FRAYED (FLIGHT DECK) · airframe 65,292 hrs · 37,290 cycles

FOUND CAPTIANS CONTROL CABIN ESCAPE ROPE FRAYED. R & R CAPTAINS SIDE ESCAPE ROPE ASSY. OPS NOW NORMAL REF 25-61-10 AMM.

Part: DOOR — OUT OF ADJUST (L1) · airframe 64,566 hrs · 36,845 cycles

L1 DOOR HARD TO CLOSE. ADJUSTED L1 DOOR IAW AMM 52-11-00, OPS CHECKED NORMAL.

Part: ROLLER — FROZEN (L2 WINDOW) · airframe 63,470 hrs · 36,178 cycles

L2 SLIDING WINDOW NOT SLIDING VERY WELL. ACFT GROUNDED. REPLACED FROZEN AFT LWR ROLLER ON L2 WINDOW AND LUBED TRACKS. REF MM 56-12-11-308-008. OPS CK GOOD.

Part: HOUSING — WORN (CARGO DOOR) · airframe 63,470 hrs · 36,178 cycles

FWD CARGO DOOR HANDLE WILL NOT STOW FLUSH. FOUND HOUSING WORN. ACFT GROUNDED. R & R HANDLE HSG IAW DWG 65-46921.

Part: DOOR — LACK OF LUBE (L1) · airframe 63,041 hrs · 35,921 cycles

F/A REPORTS ROCKER ARM ON FWD L-1 DOOR VERY STIFF AND DIFFICULT TO CLOSE CANT KEEP MOMENTUM OF DOOR SWINGING INWARD TO CLOSE W/O EXERTING EXCESS PRESSURE TO CLOSE AND LATCH. LUBED L-1 DOOR LATCH CRANKS AND HINGES OPS NORMAL NO HISTORY 90 DAYS

Part: LENS — BROKEN (CABIN) · airframe 62,387 hrs · 35,566 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN AT LEFT FORWARD OVERWING EXIT HAS BROKEN LENS. REPLACED LENS AND TESTED PER MM 33 51 81 962 011, OPS NORMAL.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 61,079 hrs · 34,775 cycles

F/A REPORTS THAT THE L1 DOOR IS TO CLOSE. ADJUSTED DOOR GUIDE ARM IAW AMM 52 11 00, OPS CHECK GOOD.

Part: STRAP — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 60,350 hrs · 34,370 cycles

AFT CARGO DOOR FWD FRAME DOUBLER AND STRAP ARE CORRODED. REMOVED AND REPLACED DOUBLER AND STRAP IAW BAC DWG 65 47959 67.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,350 hrs · 34,370 cycles

AFT CARGO DOOR CUTOUT FWD FRAME DOUBLER AND STRAP ARE CORRODED. REMOVED AND REPLACED DOUBLER AND STRAP IAW BAC DWG 65 47959 REV B.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 60,350 hrs · 34,370 cycles

CABIN OVER WING BOX RBL 65.5 STA.601 MAIN FRAME LOWER INBOARD CHORD ATTACH FITTING IS CRACKED. INSTALLED REPAIR ANGLE IAW REO G13803 REV A.

Part: FAIRLEAD — BROKEN (STAB TRIM) · airframe 60,350 hrs · 34,370 cycles

STAB TRIM CABLE GUIDE FAIRLEAD WAS FOUND BROKEN BS 1040 LBL 6. REPLACED FAIRLEAD IAW ASA EA 400 27EA 05729.

Part: FAIRLEAD — BROKEN (STAB TRIM) · airframe 60,350 hrs · 34,370 cycles

STAB TRIM CABLE GUIDE FAIRLEAD WAS FOUND BROKEN BS 1040 RBL 6. REPLACED FAIRLEAD IAW ASA EA 400 27EA 05729.

Part: STOP FITTING — GOUGED (CARGO DOOR) · airframe 60,350 hrs · 34,370 cycles

AFT CARGO DOOR LOWER AFT STOP FITTING IS GOUGED. REMOVED AND REPLACED IAW B737 400 SRM 51 40 02.

Part: JAM-NUT — LOOSE (L1 DOOR) · airframe 57,303 hrs · 22,535 cycles

L1 DOOR IS VERY HARD TO SHUT AND PUSH HANDLE ALL THE WAY DOWN. ACCOMPLISHED FWD ENTRY DOOR TEST PER AMM 52 11 00 755 051, OUT OF LIMITS. FOUND GUIDE ARM JAM NUT LOOSE. RE-ADJUSTED GUIDE ARM COARSE ADJUSTMENT REF MM 52 11 00 705 007. ACCOMPLISHED FWD ENTRY DOOR TEST REF 52 11 00 755 051. OPS CHECK GOOD.

Part: GROUND WIRE — DISCONNECTED (CABIN) · airframe 53,266 hrs · 33,204 cycles

EMERGENCY EXIT LIGHTS AT 9D AND RT FWD OVERWING EXIT INOP. RECONNECTED A DISCONNECTED GROUND WIRE AND REPLACED BULB.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 32,346 hrs · 9,359 cycles

FWD GALLEY DOOR CUTOUT FWD UPPER CORNER REVEAL IS CRACKED.

Part: INTERCOSTAL — CRACKED (BS 295 S12L) · airframe 56,991 hrs · 32,346 cycles

CRACKED INTERCOSTAL AT BS 295 STR 12L. REMOVED AND REPLACED INTERCOSTAL.

Part: STRINGER — CRACKED (BS 1012 S27L) · airframe 56,991 hrs · 32,346 cycles

FOUND STRINGER AT STA 1012 LT 27 CRACKED ON UPPER FLANGE. REMOVED STRINGER SECTION FABRICATED AND INSTALLED REPLACEMENT SECTION.

Part: SKIN — CRACKED (LT WING) · airframe 56,991 hrs · 32,346 cycles

LEFT WING FIXED LEADING EDGE CRACKED ABOVE NR 3 SLAT O/B CRACK CUTOUT. REPAIRED BY TAPER SANDING AREA AND PERFORMING PLY REPLACEMENT VACUUM BAGGING AND CURED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

MAIN CABIN FLOOR SUPPORT CRACKED. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT SHEAR TIE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

FWD CARGO BAY BS 500+12 SKIN AT ANTENNA CUTOUT IS CORRODED. REMOVED CORROSION ON CHANNEL SUPPORT FOUND CRACKED FABRICATED AND INSTALLED NEW CHANNEL SUPPORT.

Part: INTERCOSTAL — CRACKED (S10L) · airframe 56,992 hrs · 32,346 cycles

FWD ENTRY DOOR UPPER HINGE THE LOWER INTERCOSTAL WEB IS CRACKED AT O/B RADIUS JUST ABOVE STRINGER 10L. REMOVED AND REPLACED INTERCOSTAL WEB, ACCOMPLISHED REPAIRS.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

MAIN CABIN FLOOR SUPPORT CRACKED FROM BS 933 - 939 BL 0 WL 208. REMOVED DAMAGED FLOOR SUPPORT ANGLE, FABRICATED NEW AND INSTALLED.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

FWD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT IS CRACKED. REMOVED AND FABRICATED FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT.

Part: PLATE — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FWD CARGO COMPARTMENT SEAL PLATE ATTACHED TO LOWER BULKHEAD SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED SEAL PLATE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

INTERCOSTAL HAS AREA OF WEAR AT NUT PLATE HOLES 2EA. REMOVED AND REPLACED INTERCOSTAL.

Part: SUPPORT — CRACKED (BS 500F-500G) · airframe 56,992 hrs · 32,346 cycles

SIDEWALL SUPPORT BAFFLE IN FWD CARGO BAY IS CRACKED. REMOVED CRACK, FABRICATED AND INSTALLED.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FWD CARGO COMP SIDEWALL SUPPORT BAFFLE IS CRACKED. REMOVED FABRICATED AND INSTALLED BAFFLE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT WEB BS 500G 500D IS CRACKED AT FWD END UPPER FLANGE. REMOVED CRACKED SIDEWALL SUPPORT WEB FABRICATED NEW WEB AND INSTALLED SIDEWALL SUPPORT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AT BS 296.5. FOUND REPAIR DOUBLER ON FRAME AT BS 296 TO BE CRACKED. FABRICATED REPAIR PARTS AND REPLACED DOUBLER.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FWD CARGO COMP FLOOR TO SIDEWALL SUPPORT WEB IS CRACKED AT FWD END UPPER FLANGE. REMOVED FABRICATED AND INSTALLED BAFFLE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT WEB IS CRACKED AT AFT END UPPER FLOOR. REMOVED FABRICATED AND INSTALLED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FUSELAGE EXTERIOR SKIN AFT ENTRY DOOR UPPER HINGE CUTOUT CRACK IN SKIN AT UPPER FWD CORNER. REMOVED DAMAGE AND REPAIRED DOOR HINGE CUTOUT.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FWD CARGO COMPARTMENT SIDEWALL SUPPORT BAFFLE IS CRACKED. REMOVED FABRICATED AND INSTALLED SUPPORT BAFFLE.

Part: FRAME — CRACKED (BS 360 S8L) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE JUST ABOVE STR 8L AT BS 360. CUTOUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (BS 380) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE AT BS 380. REPLACED FRAME.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME CRACKED AT FASTENER STA 727B BETWEEN STR 8 & 9 LEFT. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME CRACKED AT FASTENER STA 907 BETWEEN STR 8 & 9L. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME CRACKED AT FASTENER STA 827 BETWEEN STR 8 & 9R. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: SKIN — DEBONDED (LE SLAT) · airframe 56,991 hrs · 32,346 cycles

NR 2 SLAT T/E WEDGE LWR SURFACE DISBONDED OUT OF LIMITS. REMOVED DAMAGE AND PREVIOUS REPAIR AND INSTALLED DOUBLER REPAIR.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

AFT CARGO BAY FLOOR TRACK STA 747 RBL 14 IS CRACKED. CUT OUT SECTION OF FLOOR TRACK AND SPLICED IN NEW SECTION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE AT BS 400 JUST BELOW STRINGER 8L.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

FRAME CRACKED AT FASTENER BS 727F BETWEEN STR 8R AND STR 9R. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (BS 727D) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE AT BS 727D. REPAIRED FRAMES, INSTALLED REINFORCEMENT ANGLES.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE AT 787. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE BS 747. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE BS 400. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE BS 827. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE AT 867. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE AT 747. REPAIRED FRAMES, INSTALLED REINFORCEMENT ANGLES.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE BS 500A. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: SUPPORT — CRACKED (NR 2 PYLON) · airframe 32,346 hrs · 9,359 cycles

NR 2 PYLON AFT SUPPORT HAS WEAR IN LOWER AFT CORNER FOUND TO BE CRACKED UPON REMOVAL. REMOVED AND REPLACED AFT SUPPORT.

Part: FRAME — CRACKED (FUSELAGE)

FRAME CRACKED AT FASTENER BS 727F STR 8L. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE AT BS 480 BELOW STR 8R. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE)

FRAME CRACKED AT FASTENER. REPAIRED FRAME, CUT OUT CRACKED AREA AND INSTALLED REINFORCEMENT ANGLES.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE AT BS 440 JUST BELOW STRINGER 8L. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,991 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE AT BS 400 JUST BELOW STRINGER 8R. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

CRACKED STRINGER CLIP STA 601 STR 5R. REPLACED STRINGER CLIP WITH A 69 56037UI. REF ASA DWG 53100265832 AND SRM 51 40 02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

STRINGER CLIP CRACKED AT BS 500A STR 10L. REMOVED AND REPLACED STRINGER CLIP IAW ASA DWG A53100265816 & SRM 51 40 02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

BS 867 STR 9L STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW ASA DWG A53100265816 & SRM 51 40 02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

CRACKED STRINGER CLIP STATION 616 & 5L. REMOVED CRACKED STRINGER CLIP AT BS 616 S5L, INSTALLED NEW CLIP. REMOVED AND RE-INSTALLED INTERCOSTAL AT BS 616 TO BS 594 FOR ACCESS IAW DRAWING A53160265832 1 4 & SRM 51 40 02 PG 1&2.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

SHEAR TIE IS CRACKED AT BS 360 BETWEEN STRINGER 14R TO 15R. REMOVED CRACKED SHEAR TIE AND FABRICATED AND INSTALLED SHEAR TIE.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

STRINGER CLIP IS CRACKED AT FRAME BS 787 STR 10L STRINGER CLIP. REMOVED AND REPLACED IAW ASA DWG A53100265816.

Part: FRAME — CRACKED (BS 380) · airframe 56,992 hrs · 32,346 cycles

FRAME IS CRACKED AROUND FASTENER HOLE AT BS 380 JUST 2 INCHES ABOVE STRINGER HOLE. REPAIRED FRAME AT BS 380.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

FWD FUSELAGE BS 312 RBL 31 WL 198 TENSION STRAP IS CRACKED AT LOWER SURFACE OF FLOORBEAM. REMOVED AND REPLACED TENSION STRAP AT BS 312 RBL 31 BOTTOM OF FLOORBEAM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

STRINGER CLIP CRACKED IN RADIUS OUT OF LIMITS. REMOVED AND REPLACED STRINGER CLIP AT BS 727A STR 10L IAW ASA DWG A53100265816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

STRINGER CLIP CRACKED AT STR 8L STA 867. REMOVED AND REPLACED STRINGER CLIP AT STR 8L BS 867 IAW ASA DWG A53100265816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

STRINGER CLIP CRACKED AT FRAME BS 727B STR 4R. REMOVED CRACKED STRINGER CLIP AND REPLACED WITH NEW IAW ASA DRG 53100265816.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 56,992 hrs · 32,346 cycles

BS 500C TO BS 500D RBL 24 SUPPORT BAFFLE IS CRACKED. REMOVED FABRICATED AND INSTALLED BAFFLE.

Part: FRAME — CRACKED (FUSELAGE)

FRAME CRACKED AT FASTENER BS 727D BETWEEN STR 8L AND 9L. CUT OUT CRACK AND REPAIRED WITH DOUBLERS.

Part: DOUBLER — MISREPAIRED (L1 DOOR) · airframe 53,802 hrs · 30,421 cycles

GATE AGENT REPORTS UPPER L1 DOOR RUBBING INIT MIG 2C 212173 98040. L1 DOOR UPPER HINGE LWR CAM PLATE BOLTS REPLACED AND TORQUED TO REMOVE LOOSENESS. L1 DOOR GUIDE ARM LOCKPLATE ATTACH BOLT/NUT TORQUED TO REMOVE LOOSENESS. REF CLOSED MIG 2C 212173 FOR WORK ACCOMPLISHED. TRIMMED L1 DOOR UPPER AND LOWER HINGE CUTOUTS DOUBLER AND TRIPLER RADIUS TO RELIEVE INTERFERENCE. REF AAR EA 12977. REPLACED UPPER HINGE COVER PER MM 20 50 11. DOOR RIG ADJ CK OK PER MM 52 11 0.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 53,795 hrs · 30,419 cycles

L1 DOOR HINGE CUTOUT FOUND DOOR DOUBLER CRACKED AT LOWER HINGE. REPAIRED DOUBLER IAW ASA EA 5330 02402 BY INSTALLING DOUBLER AND TRIPLER.

Part: SKIN — DELAMINATED (NR 5 SPOILER) · airframe 53,795 hrs · 30,419 cycles

NR 5 SPOILER FOUND DELAMINATED ON UPPER AND LOWER SURFACE. THREE REPAIRS. REMOVED DELAMINATED SKIN, FABBED FILLERS AND DOUBLERS, AND BONDED REPAIRS IAW B737 400 SRM 51 70 10 REP 4 ON 3 EA REPAIRS.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,795 hrs · 30,419 cycles

FUSELAGE SKIN IS DENTED AT STA 1002 AND STR 14L 2.5 INCHE ABOVE LAP 6 INCHES FROM CUTOUT 2 INCHES FROM REPAIR. REMOVED SKIN PANEL, FABBED NEW SKIN PANEL AND BONDED DOUBLER TO IT AND INSTALLED REPLACEMENT SKIN PANEL ASSEMBLY IAW B737 400 SRM 51 40 02.

Part: SKIN — DENTED (TE FLAP) · airframe 53,795 hrs · 30,419 cycles

LEFT INBD AFT FLAP LOWER SURFACE HAS MULTIPLE DENTS. PREPPED DAMAGED AREA AND BONDED THE REPAIR IAW B737 400 SRM 51 70 16 REP 11 IN THE SRM.

Part: SKIN — DENTED (MIDFLAP) · airframe 53,795 hrs · 30,419 cycles

LT WING INBOARD MID FLAP WEDGE UPPER SURFACE HAS A DENT. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, AND BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REP 2.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,795 hrs · 30,419 cycles

SKIN DENTED AT STA 1000 AND STR 14L JUST BELOW THE LAP. REMOVED DAMAGED AREA, FABBED FILLER DOUBLER AND TRIPLER AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 01 REP 31.

Part: SKIN — CHAFED (FOREFLAP) · airframe 53,795 hrs · 30,419 cycles

RT OUTBOARD FORE FLAP IS CHAFED ON THE OUTBOARD LEADING EDGE. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, AND INSTALLED IAW B737 400 SRM 57 53 01.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,795 hrs · 30,419 cycles

DENT FOUND ON BELLY SKIN AT BS 1020 RBL 13.5, DENT IS WITHIN 3 INCHES OF SKIN SPLICE. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 80 01 REP 2.

Part: SKIN — DENTED (TE FLAP) · airframe 53,795 hrs · 30,419 cycles

RT INBOARD AFT T/E FLAP UPPER SURFACE HAS 2 EA DENTS 3 INCHES OUTBOARD OF INBOARD EDGE. PREPPED DAMAGED AREAS, FABBED DOUBLER AND BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REP 2.

Part: SKIN — DENTED (TE FLAP) · airframe 53,795 hrs · 30,419 cycles

LT INBOARD AFT FLAP HAS MULTIPLE DENTS ON THE UPPER SURFACE. REMOVED DAMAGED AREAS, FABBED FILLERS AND DOUBLER, AND BONDED REPAIRS 2 EA IAW B737 400 SRM 51 70 10 REP 4.

Part: SKIN — DENTED (LE SLAT) · airframe 53,795 hrs · 30,419 cycles

NR 2 SLAT HAS A DENT ON THE UPPER SUFACE 3.5 INCHES FROM T/E AND 34 INCHES FROM OUTBOARD END. PREPPED DAMAGED AREA, FABBED DOUBLER AND BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REP 2.

Part: SKIN — DENTED (TE FLAP) · airframe 53,795 hrs · 30,419 cycles

LT TRAILING EDGE FLAP LOWER SURFACE DENT AT 42 INCHES FROM INBOARD AND 3.5 INCHES FWD OF TRAILING EDGE. PREPPED DAMAGED AREA AND BONDED THE REPAIR IAW B737 400 SRM 51 70 16 REP 11.

Part: SKIN — DENTED (T/E FLAP) · airframe 50,159 hrs · 28,495 cycles

LEFT OUTBOARD AFT FLAP DENTED IN 2 PLACES ON UPPER SURFACE. LEFT OUTBOARD AFT FLAP UPPER SURFACE AT APPROX RSS 300 312 REPAIRED IAW SRM 51-70-10.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 50,158 hrs · 28,495 cycles

FRAME TO INTERCOSTAL ATTACH CLIP CRACKED. REPLACED CRACKED CLIP WITH NEW PAR IAW EA 5310 02732.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,158 hrs · 28,495 cycles

AFT CABIN ZEE ANGLE CORRODED. REPLACED WITH FABRICATED REPAIR PART IAW SRM 51-40-02 AND 51-40-05.

Part: SKIN — WORN (L/E SLAT) · airframe 50,158 hrs · 28,495 cycles

NR 3 SLAT INBOARD T/E LWR SURFACE SKIN WORN. REPAIRED SLAT DAMAGE IAW SRM 51-70-10.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,158 hrs · 28,495 cycles

INTERCOSTAL CRACKED. REPLACED WITH NEW PART IAW EA 5310 02732.

Part: SKIN — DENTED (MID FLAP) · airframe 50,158 hrs · 28,495 cycles

RIGHT INBOARD MID FLAP DENT ON UNDERSIDE LOCATED 9 INCHES OUTBOARD OF INBOARD END AND 3 INCHES FWD OF T/E. FLAP DENT REPAIRED IAW SRM 51-70-10.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,158 hrs · 28,495 cycles

AFT CABIN ZEE ANGLE CORRODED. REPLACED WITH FABRICATED REPAIR IAW SRM 51-40-03 AND 51-40-02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 50,158 hrs · 28,495 cycles

INTERCOSTAL STRAP CRACKED. REPLACED WITH NEW PART IAW EA 5310 02732.

Part: SKIN — DENTED (T/E FLAP) · airframe 50,158 hrs · 28,495 cycles

LEFT O/B AFT FLAP HAS NUMEROUS DENTS AT LWR SURFACE. LEFT O/B AFT FLAP LWR SURFACE AT RSS 300 312 REPAIRED IAW SRM 51-70-10.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,158 hrs · 28,495 cycles

INTERCOSTAL CRACKED. REPLACED WITH NEW PART IAW EA 5310 02732.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,158 hrs · 28,495 cycles

AFT CABIN DOORWAY SILL CHORD CORRODED. REPLACED WITH NEW PART PER SRM 51-40-02.

Part: SKIN — CRACKED (L/E SLAT) · airframe 50,158 hrs · 28,495 cycles

RIGHT WING NR 6 SLAT I/B CORNER 2 INCH CRACK FOUND. RIGHT WING NR 6 SLAT I/B CORNER CRACK REPAIRED IAW SRM 57-43-01 FIG 201.

Part: SKIN — DENTED (FORE FLAP) · airframe 50,159 hrs · 28,495 cycles

LEFT INBOARD FORE FLAP UPPER CAMBER HAS APPROX 12 X 15 INCHES DENT AT RSS 264 276. REPAIRED FLAP IAW SRM 51-70-10.

Part: SKIN — GOUGED (RUDDER) · airframe 46,516 hrs · 26,462 cycles

RUDDER LEADING EDGE IS GOUGED AT NUMBER 1 HINGE CUTOUT. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW ASA EA 5540 01124.

Part: STRUCTURE — DELAMINATED (L/E SLAT) · airframe 46,516 hrs · 26,462 cycles

NUMBER 2 SLAT IS BULGED AND DELAMINATED AT TRAILING EDGE INBOARD CORNER. PREPPED DELAMINATED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-10.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 46,516 hrs · 26,462 cycles

NR 5 SPOILER (GROUND) HAS NUMEROUS SMALL DENTS. REMOVED DAMAGED AREAS, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW SRM 51-70-10.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 46,516 hrs · 26,462 cycles

STRINGER 26R IS CORRODED. REMOVED CORRODED SECTION OF STRINGER. FABRICATED AND INSTALLED REPLACEMENT SECTION OF STRINGER AND REPAIR PIECES IAW SRM 53-00-03 FIG 201.

Part: SKIN PANEL — DELAMINATED (NR 8 SPOILER) · airframe 46,516 hrs · 26,462 cycles

NR 8 SPOILER PANEL DELAMINATED ON UPPER SURFACE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW SRM 51-70-10.

Part: STRUCTURE — DELAMINATED (L/E SLAT) · airframe 46,516 hrs · 26,462 cycles

NR 2 SLAT DELAMINATED AT OUTBOARD TRAILING EDGE CORNER. PREPPED DELAMINATED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-10.

Part: FITTING — GOUGED (NR 9 SPOILER) · airframe 46,516 hrs · 26,462 cycles

NR 9 SPOILER HAS A DEEP GOUGE AT ACTUATOR LUG. REMOVED AND REPLACED NR 9 SPOILER IAW AMM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 46,516 hrs · 26,462 cycles

SHEAR WEB CORRODED. REMOVED CORRODED SECTION OF WEB, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-13 FIG 1 AND SRM 51-40-02.

Part: STRAP — CRACKED (FLOORBEAM) · airframe 46,516 hrs · 26,462 cycles

FLOORBEAM STABILIZER STRAP IS CRACKED. REPAIRED FLOORBEAM STABILIZER STRAP IAW SRM 53-10-51 FIG 201.

Part: SKIN — PUNCTURED (NR 5 SPOILER) · airframe 46,516 hrs · 26,462 cycles

NR 5 SPOILER HAS PUNCTURE IN CENTER OF LOWER SURFACE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW SRM 51-70-10.

Part: SKIN — DENTED (T/E FLAP) · airframe 46,516 hrs · 26,462 cycles

RIGHT O/B AFT LEADING EDGE DAMAGED. REMOVED DAMAGED SECTION OF LEADING EDGE SKIN. REPLACED SECTION OF LEADING EDGE SKIN IAW SRM 51-40-05 AND 51-40-02.

Part: WEB — CORRODED (FUSELAGE) · airframe 46,516 hrs · 26,462 cycles

FWD PIT LOWER JAMB WEB IS CORRODED. REMOVED CORRODED WEB FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 51-30-01 AND 51-40-02.

Part: STRUCTURE — CRACKED (L/E SLAT) · airframe 46,516 hrs · 26,462 cycles

NUMBER 2 SLAT LOWER TEE CHORD CRACKED AT ACTUATOR. REMOVED DAMAGED TEE CHORD, FABRICATED NEW TEE CHORD. DRILLED, TREATED, PRIMED AND INSTALLED IAW SRM 51-40-02, 51-30-01 FIG 7, 51-40-05 AND 51-21-21 PG 705.

Part: SKIN — DELAMINATED (SPOILER) · airframe 46,516 hrs · 26,462 cycles

SPOILER 0 SEAL SCREWS ARE TOO LONG CAUSING BULDGES ON THE UPPER SURFACE AND POSSIBLE DELAMINATION. REPAIRED PER SRM 51-70-10 PG 221, 238, 249 REPAIR 4.

Part: SKIN PANEL — DENTED (RT SPOILER) · airframe 46,516 hrs · 26,462 cycles

RIGHT WING NUMBER 6 SPOILER PANEL HAS 4EA SMALL DENTS ON I/B UPPER SURFACE. REPAIRED RIGHT WING NUMBER 6 SPOILER UPPER SURFACE DAMAGE IAW SRM 51-70-10 PG 201.

Part: SKIN — DELAMINATED (SPOILER) · airframe 46,516 hrs · 26,462 cycles

SPOILER 1 SEAL SCREWS ARE TOO LONG CAUSING BULDGES ON THE UPPER SURFACE AND POSSIBLE DELAMINATION. REPAIRED SPOILER 1 PER SRM 51-70-10 REPAIR 4 PG 238 AND 249.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 46,516 hrs · 26,462 cycles

RT WING NR 6 SPOILER PANEL DELAMINATED ON UPPER SURFACE. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED (BONDED) REPLACEMENT SKIN ONTO SPOILER IAW SRM 51-70-10.

Part: SKIN — DENTED (FUSELAGE) · airframe 46,516 hrs · 26,462 cycles

DENT IN FUSELAGE SKIN ACROSS SHEAR TIE. REMOVED DAMAGED AREA OF SKIN FABRICATED AND INSTALLED REPAIR FILLER DOUBLER AND TRIPLER IAW SRM 53-00-01 FIG 201.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 45,097 hrs · 25,736 cycles

IN FIRST CLASS AC LT, EMERGENCY FLOOR TRACK LIGHT STRIP LOOSE AND PULLING UP. REMOVED AND REPLACED PHOTOLUMINSCENT STRIP AND CHARGE STRIP IAW AMM. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND AFT GALLEY AREA STATION 947.5 FLOORBEAM HAS CORROSION AT FASTENER HOLES LBL 16 TO RBL 16. REPAIRED FLOORBEAM. (M)

Part: CREASE BEAM — GOUGED (FUSELAGE)

GYR - FOUND CREASE BEAM WEB AT STATION 304, R1 DOOR HAS DEEP GOUGE JUST INBOARD OF CREASE BEAM INNER CHORD. REMOVED AND REPLACED WEB. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND CABIN FLOORBEAM STATION 986.5 CORRODED RBL 48 TO LBL 48. REPLACED FLOORBEAM. (M)

Part: FRAME — CORRODED (FUSELAGE)

GYR - FOUND AFT CARGO PIT FRAME AT STATION 727G FORWARD SIDE HAS CORROSION BETWEEN STRINGER 26R-27R LOWER ANGLE. REPAIR FRAME, STATION 26R TO 27R. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

GYR - FLOOR CREASE BEAM AT L2 JAMB CORRODED STATION 947 TO 1006. REMOVED AND REPLACED CREASE BEAM CHORD STATION 947-1006 LBL 50. (M)

Part: WEB — GOUGED (FUSELAGE)

GYR - FOUND AFT GALLEY AREA HAS GOUGE IN FLOOR WEB STATION 1016, LBL 40. REMOVED AND REPLACED WEB. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

GYR - FOUND MAIN DECK SEAT TRACK AT STATION 344 LBL 26.5 UPPER SURFACES OF INBOARD AND OUTBOARD FLANGES CORRODED. REPAIRED SEAT TRACK AT STATION 344 LBL 26.5. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

GYR - MAIN DECK SEAT TRACK AT STATION 344 LBL 45.6 UPPER SURFACE OF INBOARD AND OUTBOARD FLANGES FOUND CORRODED. REPAIRED SEAT TRACK AT STATION 344 LBL 45.6 IAW SRM 737 53-00-52. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

GYR - RIGHT CREASE BEAM WEB AT STATION 986 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED WEB. (M)

Part: BEARING — DEFECTIVE (NR 1 PYLON)

GYR - FOUND NR 1 ENGINE PYLON, UPPER LINK ATTACH POINT ROTATING IN UPPER SPAR FITTING. REMOVED AND REPLACED CROWN BEAM BEARING. (M)

Part: ANGLE — CORRODED (FUSELAGE)

GYR - AFT BAG PIT BS 767 FRAME FAIL/SAFE CHORD ANGLE IS CORRODED FROM 26R TO BL 0. REPAIRED BS 767 FRAME FAIL/SAFE CHORD ANGLE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND AFT GALLEY AREA, CORROSION ON STATION 967 FLOORBEAM LBL 28 AND RBL 18. REPAIRED FLOORBEAM AT STATION 967, LBL 28, RBL 18 TO LBL 27 WITHIN LIMITS. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

GYR - RIGHT KEEL BEAM CHORD AT STATION 502 HAS CORROSION. REPAIRED KEEL BEAM AT STATION 502. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

GYR - AFT GALLEY AREA FORE TO AFT FLOOR SUPPORT BEAM HAS CORROSION STATION 947 TO 967 RBL 50. REMOVED AND REPLACED FLOOR SUPPORT BEAM STATION 947 TO 967 RBL 50. (M)

Part: FITTING — CORRODED (L1 DOOR)

GYR - FOUND L1 DOOR GIRT BAR FITTINGS AT STATION 312 AND 344 ARE CORRODED. REMOVED AND REPLACED ATTACH FITTINGS. (M)

Part: BUSHING — WORN (NR 2 PYLON)

GYR - NR 2 PYLON LOWER SPAR FITTING INBOARD BUSHING MIGRATED. REMOVED AND REPLACED LOWER SPAR FITTING BUSHINGS. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

GYR - AFT PIT INTERCOSTAL AT STATION 787-790 STRINGER 25R CORRODED UPPER SURFACES. REMOVED AND REPLACED INTERCOSTAL STATION 767 TO 790 STRINGER 25R. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

GYR - R-1 DOOR LOWER THRESHOLD CREASEBEAM UPPER SURFACE HAS SEVERAL AREAS OF CORROSION BETWEEN STATION 294.5 AND 344 RBL 50. REMOVED AND REPLACED CREASEBEAM (CHORD) AT R1 DOOR 294.5 TO 344 RBL 50. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

GYR - FLOOR CREASE BEAM AT R2 JAMB CORRODED STATION 947 TO STATION 990. REMOVED AND REPLACED CREASE BEAM STATION 947 TO 1006 RBL 50. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

GYR - AFT GALLEY AREA FORE TO AFT FLOOR SUPPORT CHORD HAS CORROSION STATION 947 TO 967 LBL 50. REMOVED AND REPLACED SUPPORT STATION 947-967 LBL 50. (M)

Part: BEARING — LOOSE (NR 2 PYLON)

GYR - NR 2 PYLON, UPPER SPAR ATTACH FITTING BEARING IS LOOSE IN LUG. REMOVED AND REPLACED CROWN BEAM BEARING. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

GYR - AFT CARGO PIT CENTER BELLY BETWEEN STATION 727D AND 727E, VHF ANTENNA SUPPORT STRUCTURE CORRODED. REMOVED AND REPLACED VHF ANTENNA SUPPORT STRUCTURE. (M)

Part: BUSHING — WORN (NR 1 PYLON)

GYR - NR 1 ENGINE PYLON, DIAGONAL BRACE, LOWER SPAR ATTACH FITTING, INBOARD BUSHING MIGRATING. REMOVED AND REPLACED BUSHING. (M)

Part: WEB — CORRODED (FUSELAGE)

GYR - FOUND AFT PIT DOOR JAMB INBOARD BEAM AT FS 846 ABOVE STATION 25L CORRODED. REMOVED AND REPLACED WEB AT STATION 740-847 AT STRINGER 25R. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

GYR - AFT BAG PIT RIGHT TRANSITION Z-CHANNEL IS CORRODED IN NUMEROUS PLACES FROM BS 867 TO 947. REMOVED AND REPLACED Z-CHANNEL STATION 867 TO 947, 25R. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

CYR - AFT BAG PIT LEFT TRANSITION Z-CHANNEL IS CORRODED IN NUMEROUS PLACES FROM STATION 797 TO 947. AFT CARGO PIT LEFT SIDE Z-CHANNEL REMOVED AND REPLACED 797 TO 947, 25L TO 25L. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

GYR - FOUND AFT BAG PIT RIGHT TRANSITION Z-CHANNEL IS CORRODED FROM STATION 847 TO 867. REMOVED AND REPLACED TRANSITION AT STATION 847 TO 867, 25 RT TO 25 RT. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

CYR - AFT CARGO PIT FLOORBEAM HAS CORROSION TOPSIDE WHERE FLOORPANEL SPLICE STRAP CROSSES, AFT OF 727F, LBL 16 TO RBL 16. REPAIRED AFT PIT FLOORBEAM AT STATION 727F, RBL 16. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

GYR - FOUND L1 DOOR LOWER THRESHOLD CREASE BEAM UPPER HAS CORROSION FROM STATION 294.5 TO 344, LBL 50. REMOVED AND REPLACED CREASE BEAM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

GYR - FOUND AFT BAG PIT BS 947 FLOOR SUPPORT ANGLE IS CORRODED AT SEVERAL PLACES LBL 25 TO RBL 25. REMOVED AND REPLACED FLOOR SUPPORT ANGLES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND MAIN DECK FLOORBEAM AT FS 294.5 UPPER T-CAP UPPER SURFACE HAS SEVERAL AREAS OF CORROSION FROM LBL 24 TO RBL 50. REPAIRED UPPER CHORD AT STATION 294.5 FROM LBL 24 TO RBL 50. (M)

Part: SKIN — SCRATCHED (FUSELAGE)

GYR - FOUND FUSELAGE EXTERNAL SKIN HAS SCRATCHES STATION 247, 10 INCHES ABOVE 24R. CUTOUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW 737-400 SRM 53-10-01. (M)

Part: WEDGE — DENTED (TE FLAP)

WHILE PERFORMING C-CHECK, FOUND LT IB MIDFLAP T/E WEDGE HAS A DENT APPROX 3 IN FROM END. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROW 15-21 INOPERATIVE, WIRE DISCONNECTED. RECONNECTED WIRE. OPS CHECK NORMAL. (M)

Part: WIRE — DISCONNECTED (CABIN)

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

Part: LIGHT — DISCONNECTED (ROW 3 TO 6)

SEA-DURING LINE CHECK, FOUND WHITE EMERGENCY FLOOR TRACK LIGHTS DISCONNECTED AT ROW 3-6. RECONNECTED FLOOR TRACK WIRES AND REPLACED 1 LENS COVER, OPERATIONAL CHECKED NORMAL.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR EVACUATION SLIDE BOTTLE WAS FOUND TO HAVE LOW PRESSURE. REPLACED THE L1 DOOR EVACUATION SLIDE ASSEMBLY. ROUTED THE SLIDE ASSEMBLY FOR INSPECTION AND REPAIR. (M)

Part: GUIDE — LACK OF LUBE (PAX DOOR)

SEA - PRIOR TO FLIGHT 62, THE L1 DOOR WAS FOUND TO BE DIFFICULT TO CLOSE. INSPECTED L1 DOOR AND LUBRICATED DOOR GUIDE, THE DOOR OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN) · airframe 25,302 hrs · 15,054 cycles

SEA - FLT 360 - PRIOR TO FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INTERMITTENT IN THE FIRST CLASS AREA. RECONNECTED WIRING AND REPLACED DAMAGED COVER, LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN) · corrosion level 3 · airframe 25,172 hrs · 14,986 cycles

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 2-7. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: BEAM — CORRODED (BS 947.5-967.5)

SEA - DURING SI CHECK, FOUND THE R-2 DOOR CREASE BEAM CORRODED FROM STATION 947.5 TO 967.5, RBL 62. REPLACED BEAM PER SRM 51-10-02 AND 53-60-15. (M)

Part: BUSHING — FRETTED (NR 2 PYLON)

SEA - DURING SI CHECK, FOUND THE NR 2 ENGINE PYLON UPPER LINK FORWARD OF FRONT SPAR, FORWARD END BUSHING FRETTING AND HAD GAP. REPAIRED PER EA 5440-01011. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT 517 - PRIOR TO FLT, THE FORWARD TWO RED 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 AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: CHARGER — INOPERATIVE (CABIN)

SJC - FLT 455 - PRIOR TO FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 22-25, AND THE LAST 4 ROWS. REPLACED BATTERY PACK AND CHARGER AND LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTROL NR ASAA9740103.

Part: BATTERY PACK — DISCHARGED (CABIN)

SJC - FLT 455 - PRIOR TO FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 22-25, AND THE LAST 4 ROWS. REPLACED BATTERY PACK AND CHARGER AND LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTROL NR 98ZZZX374. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 27 AFT. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

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

Part: GIRT — PULLED OUT (CABIN SLIDE)

FOUND BOTH THE LEFT AND RIGHT FORWARD EMERGENCY ESCAPE SLIDE GIRTS PULLED OUT OF THE CONTAINERS. WHEN GIRT IS PULLED FROM CONTAINER, IT DRAGS ON THE FLOOR. TO IDENTIFY IF IT IS PULLED OUT, THE VELCRO FUZZY LOOP MATERIAL ON THE BACK SIDE OF THE GIRT CAN BE FELT BY RUNNING HAND BEHIND. MECHANICS SHOULD BE CAUTIONED WHEN RESTOWING, TO FOLLOW MAINTENANCE PROCEDURES. GIRT MUST NOT EXCEED PROPERLY STOWED LENGTH.

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD 2 AND AFT 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR)

SEA - FLT 571 - AFTER ARRIVAL, CREW REPORTED THAT THE L1 DOOR HANDLE WAS DIFFICULT TO CLOSE TO THE LOCKED POSITION. ADJUSTED GUIDE ARM ASSEMBLY AND DOOR OPERATED NORMALLY. (M)

Part: CONNECTOR — DIRTY (CABIN)

ANC - DURING MAINTENANCE, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 1 AND 2. FOUND DEBRIS PREVENTING PROPER CONNECTION OF ELECTRICAL CONNECTOR. REMOVED DEBRIS, RECONNECTED AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (L2 DOOR SLIDE)

SEA - DURING DEPLOYMENT OF L2 DOOR SLIDE FOR TRAINING, THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REMOVED AND REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT NR 98 - CREW REPORTED THAT THE FORWARD 4 EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING THAT HAD BECOME DISCONNECTED AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 21 THROUGH 24. RECONNECTED TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: SNUBBER — DEFECTIVE (L1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND DIFFICULT TO OPEN AND CLOSE. REPLACED DOOR SNUBBER ASSEMBLY AND OPERATED NORMALLY. (M)

Part: LAMP BASE — DEFECTIVE (CABIN)

JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS FROM ROW 22 AFT WERE FOUND INOPERATIVE. REPLACED LAMP BASE ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING ON FORWARD TRACK AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL WIRING — DISCONNECTED (CABIN)

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

Part: EEL WIRING — DISCONNECTED (CABIN)

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

Part: EEL WIRING — DISCONNECTED (CABIN)

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

Part: EEL CONNECTOR — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN THE AFT CABIN. RECONNECTED LOOSE CONNECTOR AT SECOND FROM LAST RED LIGHT AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SEA - DURING MAINTENANCE CHECK, TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN THE AFT CABIN. RECONNECTED LOOSE CONNECTOR AT SECOND FROM LAST RED LIGHT AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AFT OF ROW 27. RECONNECTED WIRE HARNESS IN TWO PLACES AFT OF ROW 27 AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

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