N797MX

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR SLIDE) · airframe 66,294 hrs · 39,195 cycles

L2 DOOR EVACUATION SLIDE GIRT MATERIAL WAS HANGING TO LOW. / R&R GIRT MATERIAL IAW MT.

Part: FITTING — CRACKED (LT WING) · airframe 66,043 hrs · 39,049 cycles

LT WING FITTING ON TE OF WEB AT LT WBL 201.90 HAS CRACK ON UPPER AREA / REMOVED AND REPLACED LT WING FITTING ON TE OF WEB AT LT WBL 201.90 PER SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 66,043 hrs · 39,049 cycles

R/H WING TRAILING EDGE SUPPORT ANGLE WEB CRACKED AT FIXED TRAILING EDGE UPPER PANEL LOWER SURFACE BETWEEN #7 AND #8 SPOILERS. / R&R WEB PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 66,031 hrs · 39,041 cycles

EXIT LIGHT BY FORWARD L/H JUMP SEAT WAS LOOSE. / R&R LENS PER AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 65,980 hrs · 39,006 cycles

L1 DOOR ESCAPE SLIDE BUSTLE WAS DANGLING. / ADJUSTED SLIDE PER MT.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 65,800 hrs · 38,898 cycles

A/C ENTRY FOUND FORWARD ENTRY FLOOR LEVEL EMERGENCY EXIT LENS HANGING LOOSE. / SECURED LENS PER SIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,659 hrs · 38,155 cycles

L/H EMERGENCY EXIT LIGHT OVERWING INOP. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,828 hrs · 37,623 cycles

RT BULLNOSE EMERGENCY LIGHT INOP AT SEAT 22. RELAMPED EMERGENCY LIGHT PER AMM.

Part: HOOK AND LOOP — DISCONNECTED (L1 DOOR) · airframe 63,700 hrs · 37,533 cycles

L1 DOOR SLIDE WAS HANGING OUT "EXCESSIVELY." CONNECTED HOOK AND LOOP ON GIRT TO GIRT FLAP-ON SLIDE CONTAINER PER MT.

Part: HOOK AND LOOP — DISLODGED (L1 DOOR) · airframe 63,691 hrs · 37,525 cycles

L1 DOOR SLIDE FLAP WAS HANGING OUT. FLAP HOOK AND LOOP DISLODGED FROM MATING HOOK AND LOOP REATTACHED HOOK AND LOOP IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,474 hrs · 36,756 cycles

RT EMERGENCY LIGHT INOP AT BS 540, SEAT ROW 8. RELAMPED LIGHT PER AM.

Part: FUSE — BLOWN (CABIN) · airframe 62,474 hrs · 36,756 cycles

UPPER AND FORWARD OF DOOR LT EMERGENCY EXIT HATCH LIGHTS INOP. R&R FUSE PER AMM.

Part: LENS — MISSING (CABIN) · airframe 62,474 hrs · 36,756 cycles

RT EMERGENCY AISLE LIGHT LENS CLIP MISSING AT ROW 8. R&R LENS IAW AMM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY NUT PLATE STRAP CORRODED BETWEEN BS 787 TO BS 794, RBL 20. R&R STRAP PER SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AROUND FASTENER HOLES INTERCOSTAL CORRODED BETWEEN BS 787 TO BS 794, STR 25R. R&R INTERCOSTAL PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500B TO BS 500C, LBL 20. R&R INTERCOSTAL PER SRM AND DWG.

Part: SIGN — BROKEN (CABIN) · airframe 62,474 hrs · 36,756 cycles

AFT ENTRY OVERHEAD PANEL EXIT SIGN MOUNT BROKEN. R&R SIGN PER AMM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS 947, RBL 24. R&R ANGLE PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, STR 25R. R&R INTERCOSTAL PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

INTERCOSTAL CORRODED BETWEEN BS 500C TO BS 500D, STR 24R. R&R INTERCOSTAL PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

INTERCOSTAL CORRODED BETWEEN BS 500B TO BS 500C, STR 24R. R&R INTERCOSTAL PER SRM AND DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

BULKHEAD ATTACH ANGLE CORRODED AROUND FASTENER HOLES AT BS 867, LBL 11. R&R ANGLE PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 927 TO BS 947, RBL 20. R&R INTERCOSTAL PER DWG AND SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

INTERCOSTAL CORRODED BETWEEN BS 500A TO BS 500B, STR 24R. R&R INTERCOSTAL PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 887 TO BS 947, RBL 20. R&R SUPPORT PER SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY RT SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 20. R&R SHIELD IAW DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY RT SHIELD CORRODED BETWEEN BS 767 TO BS 794, RBL 20. R&R SHIELD PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 494 TO BS 500A, RBL 24. R&R SUPPORT IAW DWG.

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 62,474 hrs · 36,756 cycles

PANEL 195CR AFT EDGE CRACKED AT CORNER / PANEL 195CR CRACK AT THE AFT CORNER WAS REPAIRED IAW SRM 51-70-04-2R-6

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

FORWARD CARGO BAY SUB WEB THRESHOLD CORRODED. R&R WEB PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 24. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 24. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 430 TO BS 440, RBL 24. R&R SUPPORT PER SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED BETWEEN LBL 25 TO RBL 25. R&R ANGLE PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 767+5, LBL 8. REPAIRED FLOORBEAM PER EA & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY FLOOR TRACK CORRODED BETWEEN BS 887 TO BS 947, RBL 14. R&R FLOOR TRACK PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY LOWER FLOOR INTERCOSTAL CORRODED BETWEEN BS 727A TO BS 727B, LBL 3. R&R INTERCOSTAL PER SRM AND DWG.

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 62,474 hrs · 36,756 cycles

***CORROSION*** AFT CARGO BAY FLOOR BOARD SPLICE HAS CORROSION AT STA727D+6. (MARKED) / RECEIVED NEW SERVICEABLE ACB FLOOR SPLICE FOR BS 727D+6 ON SWA P.O. 712941 WILL BE INSTALLED ON SWA CARD #JPANEL-141-CLOSE

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY FLOOR TRACK CORRODED BETWEEN BS 887 TO BS 947, LBL 3. R&R FLOOR TRACK PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 887, RBL 20. R&R SUPPORT ASSEMBLY PER DWG AND SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 847 TO BS 867, LBL 17. R&R INTERCOSTAL PER SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY LOWER FLOOR INTERCOSTAL CORRODED BETWEEN BS 867 TO BS 887, LBL 10. R&R INTERCOSTAL PER DWG & SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY FLOOR TRACK CORRODED BETWEEN BS 807 TO BS 827, RBL 14. R&R FLOOR TRACK PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 767+5, LBL 12. REPAIRED FLOORBEAM PER EA AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 20. R&R SUPPORT PER SRM & DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 62,474 hrs · 36,756 cycles

***CORROSION***AFT CARGO BAY FLOOR SPLICE STRAP HAS CORROSION AT BS887 FROM RBL22-LBL8 / REMOVED OLD AFT CARGO BAY FLOOR SPLICE STRAP @ B.S. 887 FROM RBL 22-LBL 8 PER SRM 51-40-02-0G-0; REPLACE WITH NEW FLR. STRAP PER SRM 51-40-02-0G-0 AND DRW. 149A8104.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 20. R&R SUPPORT PER SRM & DWG.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY LOWER FLOOR ANTENNA SUPPORT GUSSET CORRODED AT BS 727D+5, LBL 7. R&R GUSSET PER SRM AND DWG.

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 62,474 hrs · 36,756 cycles

***CORROSION*** AFT CARGO BAY FLOOR BOARD SPLICE HAS CORROSION AT BS767+5 FROM RBL20 TO LBL20. MARKED. / CORROSION ON ACB FLOOR BOARD SPLICE FOUND OUT OF LIMITS DUE TO NO GIVEN LIMITS IN SRM. REPLACED FLOOR BOARD SPLICE AT BS 767+5 FROM RBL 20 TO LBL 20 PER SRM 51-10-02 STEP 9.C AND AIPC 53-42-11-30. 57546U 04DEC18 RECIEVED PORT; FOR TRACKING PURPOSES ONLY. 57546U 24DEC18

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY LOWER FLOOR INTERCOSTAL CORRODED BETWEEN BS 727A TO BS 727B, RBL 3. R&R INTERCOSTAL PER SRM & DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 62,474 hrs · 36,756 cycles

FWD CARGO BAY FORWARD CORNER SCUFF PLATE CRACKED (MARKED) / REPAIRED FWD CARGO BAY FWD CORNER SCUFF PLATE PER: EA 1-A53-2076 REV 11

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

FUSELAGE UNDER DORSAL FIN CORRODED BETWEEN BS 887 TO BS 1007. REPAIRED DORSAL FIN PER ER AND EA.

Part: SHEAR TIE — CORRODED (AFT FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

***CORROSION*** DURING DVI (IAW EA#1-A53-33503 IR); STEP 8; FOUND CORROSION ON SHEAR-TIE AT BS 667; RBL 69; WL 200 (MARKED) / REMOVED CORROSION ON SHEAR TIE AT BS 667 RBL 69 WL 200 AND APPLIED PROTECTIVE FINISH PER ER 18-05575 REV IR AND EA 1-753-33764 REV IR.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL IAW DWG AND SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

R2 DOOR MOPSILL INNER CHORD CORRODED AT BS 971, RBL 50. R&R CHORD IAW DWG AND SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 294 TO BS 312, RBL 18. R&R FLOOR SUPPORT PER DWG AND SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO DOORWAY LOWER THRESHOLD STRAP BELOW INBOARD CHORD LOWER SURFACE CORRODED BETWEEN BS 842 TO BS 847, RBL 16. R&R STRAP PER SRM AND DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

L1 DOOR LOWER SILL MOPSILL ATTACH ANGLE CORRODED AT BS 317, LBL 57. R&R ATTACH ANGLE PER SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO DOORWAY LOWER THRESHOLD STRAP, BELOW INBOARD CHORD LOWER SURFACE CORRODED BETWEEN BS 795 TO BS 806, RBL 16. R&R STRAP PER SRM AND DWG.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

L1 DOOR MOPSILL CRACKED AT BS 303, LBL 55. R&R MOPSILL PER SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO BS 294, BL 0. R&R FLOOR SUPPORT IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO DOORWAY LOWER THRESHOLD SUB WEB CORRODED BETWEEN BS 795 TO BS 847, RBL 20. R&R WEB PER SRM & DWG.

Part: BEAM — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

BEAM UPPER CHORD CORRODED AT BS 986, BETWEEN RBL 50 TO LBL 50. REPAIRED CHORD PER ER AND EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 62,474 hrs · 36,756 cycles

LT MAIN WHEEL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN LBL 34 TO LBL 29. REPAIRED WEB PER ER AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO BS 360, RBL 11. R&R INTERCOSTAL IAW DWG AND SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO DOORWAY LOWER THRESHOLD INBOARD CHORD UPPER AND LOWER SURFACES CORRODED BETWEEN BS 787 TO BS 855, RBL 16. R&R STRAP PER SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

L1 DOOR LOWER SILL Z ANGLE CORRODED AT BS 317, LBL 60. R&R Z ANGLE PER SRM AND DWG.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 62,474 hrs · 36,756 cycles

HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS 663 TO BS 675, BETWEEN RBL 39 TO RBL 60. REPAIRED DECK IAW EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

R1 DOOR THRESHOLD SUPPORT ANGLE UPPER SURFACE CORRODED BETWEEN BS 298 TO BS 329, STR 17R. R&R ANGLE PER DWG AND SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

R1 DOORWAY BEHIND FORWARD DOOR FRAME ANGLE CRACKED AT BS 295, STR 17R. R&R ANGLE PER DWG AND SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 62,474 hrs · 36,756 cycles

AFT CARGO BAY AFT CORNER THRESHOLD CRACKED. / RECIEVED AFT CARGO BAY AFT CORNER THRESHOLD P.O. NUMBER 716841 59359U 03DEC18

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 62,474 hrs · 36,756 cycles

COMPOSITE BULKHEAD CRACKED AT BS 663, LBL 34. REPAIRED BULKHEAD IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 62,474 hrs · 36,756 cycles

COMPOSITE BULKHEAD UPPER ATTACH ANGLE CRACKED AT BS 663, RBL 10. REPAIRED ANGLE PER EA AND ER.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 62,474 hrs · 36,756 cycles

UPPER ATTACH ANGLE CRACKED AT BS 663, LBL 10. REPAIRED ANGLE PER EA & ER.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 62,474 hrs · 36,756 cycles

COMPOSITE BULKHEAD VERTICAL STIFFENER CRACKED AT BS 663, RBL 30. R&R STIFFENER PER SRM AND DWG.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 62,474 hrs · 36,756 cycles

COMPOSITE BULKHEAD VERTICAL STIFFENER CRACKED AT BS 663, LBL 30. R&R STIFFENER ASSEMBLY PER SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,474 hrs · 36,756 cycles

RT WING NR 7 SLAT CRACKED AT SLAT ACTUATOR ATTACH POINT, OUTBOARD ROW, 3RD FASTENER AFT. REPAIRED NR 7 SLAT SKIN PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 62,193 hrs · 36,582 cycles

SEAL RIB UNDER LEFT WING FIXED TRAILING EDGE CRACKED / REMOVED AND REPLACED RIB SEAL REF SRM 51-40-02 PER AMM.

Part: RETAINER — CRACKED (LT WING) · airframe 62,193 hrs · 36,582 cycles

SEAL RETAINER BRACKET UNDER LEFT WING FIXED TRAILING EDGE PANEL CRACKED / REMOVED AND REPLACED BRACKET REF SRM 51-40-02 PER AMM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 62,193 hrs · 36,582 cycles

R/H WING TRAILING EDGE PANEL ANGLE CRACKED JUST AFT OF ENGINE PYLON / REMOVED AND REPLACED PER SRM 51-40-02.

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 62,193 hrs · 36,582 cycles

(TRANSFERRED FROM PCS G595906). VAPOR BARRIER CRACKED;LH WHEEL WELL DIRECTLY FORWARD OF A SYSTEM RETURN FILTER APPROX 8 IN LONG MOD / APPLIED SPEED TAPE INTERIM REPAIR PER 57-10-10-1A-2 PAR 2C SRM MAKE SURE THE TAPE IS IN SATISFACTORY CONDITION AT EACH 600 FLIGHT CYCLES INTERVAL; OR MORE FREQUENTLY. CRACK IS APPROX 8IN LONG LOCATION LBL 25-34. REFERENCE TSR201808296 REPEAT INSPECTION REQUIRED:

Part: WEB — CRACKED (WHEEL WELL LH) · airframe 60,264 hrs · 35,353 cycles

(QC) EVIDENCE OF CRACK IN L/H MLG WW AT 663 LOWER WEB; LBL 10; APPROX. WL 148 (MARKED) / STOP DRILLED CRACK IN L/H MLG WW AT BS 663 LOWER WEB LBL 10 APROX. WL 148; L=1.2' IAW SRM 57-10-10-1A-2 PAR. 2.C. (4)(A) LEAD 122 21MAR18 APPLIED ALUMINUM FOIL TAPE IAW SRM 57-10-10-1A-2 STEP 2.C.(2) AND STEP 2.C.(4)(A) 1.)-5.)

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 60,264 hrs · 35,353 cycles

BULKHEAD WEB CRACKED AT BS 663, LBL 17. REPAIRED THE BULHEAD WEB IAW SRM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 60,264 hrs · 35,353 cycles

EMERGENCY LIGHT BATTERY PACK FAILED A CAPACITY TEST AT M01669. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 60,264 hrs · 35,353 cycles

EMERGENCY LIGHT BATTERY PACKS FAILED A CAPACITY TEST AT M01674. R & R THE BATTERY PACK IAW MM.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 59,921 hrs · 35,122 cycles

FORWARD DOOR EXIT SIGN BROKEN. R & R THE SIGN IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 59,260 hrs · 34,698 cycles

L2 LOWER EXIT SIGN MISSING DIRECTIONAL ARROW. R&R LENS PER AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 59,260 hrs · 34,698 cycles

R2 LOWER EXIT SIGN MISSING DIRECTIONAL ARROW. R&R LENS PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 59,243 hrs · 34,684 cycles

LT EXIT SIGN LOOSE JUST FORWARD OF OVERWING EXIT. ADJUSTED SIGN PER CMM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 58,638 hrs · 34,300 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: TIRE — FAILED (NLG) · airframe 58,459 hrs · 34,193 cycles

NOSE TIRE TREAD LOST ON TAKE OFF ROLL. TAXIED TO GATE. R & R THE LT NOSE TIRE IAW AMM.

Part: TIRE — FAILED (NLG) · airframe 58,459 hrs · 34,193 cycles

NOSE TIRE TREAD LOST ON TAKE OFF ROLL. RETURNED TO DEPARTURE. R & R THE RT NOSE TIRE IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 58,452 hrs · 34,189 cycles

AFT GALLEY OVERHEAD EXIT SIGN LOOSE. SECURED SIGN PER SIP.

Part: PLATE — CRACKED (RT WING) · airframe 58,303 hrs · 34,090 cycles

RT WING FORWARD ATTACH POINT FOR PANEL 651GB WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 58,293 hrs · 34,084 cycles

FORWARD LT EMERGENCY BATTERY FAILED TIME TEST. R&R BATTERY PER AMM.

Part: PLATE — CRACKED (LT WING) · airframe 58,293 hrs · 34,084 cycles

LT WING FORWARD ATTACH POINT FOR PANEL 551GB WIGGLE PLATE CRACKED. R&R WIGGLE PLATE PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 58,293 hrs · 34,084 cycles

CENTER RT EMERGENCY BATTERY FAILED TIME TEST. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 58,293 hrs · 34,084 cycles

AFT RT EMERGENCY BATTERY FAILED TIME TEST. R&R BATTERY PER AMM.

Part: SKIN — DELAMINATED (FUSELAGE) · airframe 58,020 hrs · 33,923 cycles

SKIN DELAMINATED AT BS 1100, AT APU COWL DOOR RIGHT HAND SIDE. REPAIRED SKIN PER SRM.

Part: LENS — UNSECURE (CABIN) · airframe 57,922 hrs · 33,868 cycles

RT OVERWING EXIT SIGN LENS FELL OFF. SECURED LENS PER SIP.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 57,880 hrs · 33,843 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE FUSE IAW MM.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 56,936 hrs · 33,293 cycles

R1 DOOR EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,814 hrs · 33,218 cycles

RIGHT OVERWING EMERGENCY LIGHT LENS MISSING. INSTALLED A LENS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,112 hrs · 32,813 cycles

R2 DOOR EMERGENCY EXIT LIGHT BULB INOP. R&R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,112 hrs · 32,813 cycles

L2 DOOR EMERGENCY EXIT LIGHT BULB INOP. R&R BULB IAW AMM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 56,112 hrs · 32,813 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM AND DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 56,112 hrs · 32,813 cycles

LT OVERHEAD STOWAGE BIN BULLNOSE AISLE LIGHT BROKEN BETWEEN ROW 3 TO ROW 5. R&R LIGHT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,112 hrs · 32,813 cycles

SKIN CRACKED BETWEEN BS 500D TO BS 540, BETWEEN STR 21L TO STR 23L. REPAIRED SKIN IAW EA.

Part: COVER — DETERIORATED (R2 DOOR) · airframe 56,112 hrs · 32,813 cycles

R2 DOOR EMERGENCY EVAC SLIDE GAUGE COVER DETERIORATED. R&R COVER IAW DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,112 hrs · 32,813 cycles

RT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 25 TO RBL 45. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,112 hrs · 32,813 cycles

EXTERNAL GROUND ELECTRICAL POWER ACCESS DOOR CUTOUT CRACKED. REPAIRED CUTOUT IAW SRM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 53,576 hrs · 31,313 cycles

OVERWING EMER EXIT SIGN INOPERATIVE. R & R SIGN IAW MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 52,512 hrs · 30,707 cycles

L1 EXIT SIGN COVER LENS LOOSE. SECURED LENS IAW EA.

Part: LENS — CRACKED (CABIN) · airframe 52,174 hrs · 30,510 cycles

RIGHT OVERWING EXIT LIGHT COVER LENS AT FLOOR LEVEL CRACKED. R & R LENS IAW AMM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 52,132 hrs · 30,487 cycles

L2 DOOR EMER EVAC SLIDE, GIRT BAR LOOSE. R & R SLIDE IAW MT.

Part: SIGN — BROKEN (CABIN) · airframe 51,955 hrs · 30,383 cycles

RIGHT OVERWING EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: CIRCUIT BREAKER — INOPERATIVE (CABIN) · airframe 51,217 hrs · 29,930 cycles

EMERGENCY CHARGER FWD CB INOPERATIVE. RESET CB IAW AMM.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 50,642 hrs · 29,603 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR OUT OF ADJUSTMENT. ADJUSTED GIRT BAR ASSEMBLY IAW SIP.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,069 hrs · 29,280 cycles

SEAT TRACK FLANGE OTBD CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: RIB — CRACKED (RT WING) · airframe 50,069 hrs · 29,280 cycles

RIGHT WING UPPER TE SHELF PANEL CTR SUPPORT RIB CRACKED, APPROX ORSS 272. R & R RIB IAW SRM.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 50,069 hrs · 29,280 cycles

FLOORBEAM DAMAGED AT BS 727B, LBL 45.5 AROUND FASTENER HOLE C. REPAIRED FLOORBEAM IAW EA.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 50,069 hrs · 29,280 cycles

FLOORBEAM DAMAGED AT BS 727B, LBL 45.5 AROUND FASTENER HOLE E. REPAIRED FLOORBEAM IAW EA.

Part: TRACK — CRACKED (FUSELAGE) · airframe 50,069 hrs · 29,280 cycles

FORWARD TRACK AFT OTBD HOLE CRACKED AT BS 727B, LBL 45. REPAIRED TRACK IAW EA.

Part: TRACK — CRACKED (FUSELAGE) · airframe 50,069 hrs · 29,280 cycles

FORWARD TRACK AFT OTBD HOLE CRACKED AT BS 727B, RBL 45. REPAIRED TRACK IAW EA.

Part: TRACK — CRACKED (FUSELAGE) · airframe 50,069 hrs · 29,280 cycles

FORWARD TRACK, FWD INBD HOLE CRACKED AT BS 727B, LBL 45. REPAIRED TRACK IAW EA.

Part: TRACK — CRACKED (FUSELAGE) · airframe 50,069 hrs · 29,280 cycles

FORWARD TRACK FWD OTBD HOLE CRACKED AT BS 727B, RBL 24. REPAIRED TRACK IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,069 hrs · 29,280 cycles

LEFT NR 1 FLIGHT DECK WINDOW FRAME DAMAGED AT THE UPPER OTBD CORNER. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,069 hrs · 29,280 cycles

RIGHT WING NR 7 SLAT LOWER SKIN CRACKED AT ACTUATOR FITTING RIBS. REPAIRED SKIN IAW SRM.

Part: COVER — MISSING (CABIN) · airframe 46,045 hrs · 26,939 cycles

RT EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER IAW SIP.

Part: SKIN — CRACKED (LE SLAT) · airframe 45,463 hrs · 26,590 cycles

RT WING NR 8 SLAT SKIN CRACKED AT ONE OF THE LOWER LE SKIN FASTENERS. REPAIRED SKIN IAW EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

FORWARD ENTRY DOOR LOWER FWD SCUFF PLATE IS CRACKED AT FASTENER HOLE. REPAIRED FWD ENTRY DOOR LOWER FWD SCUFF PLATE IAW EA 1-A53-2076.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

STRINGER CLIP CRACKED BS 380 STR 7L. REMOVED & REPLACED CRACKED STRINGER CLIP AT BS 380 STR 7L IAW SRM 51-40-02-0G-0.

Part: SILL — CORRODED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

CORROSION WHILE WORKING CUSTOMER CARD T174875 FOUND CORROSION ON ASD MOPSILL WEB, BS 955- BS 992, RBL46, WL208. REMOVED CORRODED MOP SILL WEB AT ASD BS 955-992 RBL 46 WL 208 AND REPLACED WITH NEW WEB IAW ER 13-01419 BOEING DWG 147A8510 SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0 & EA 1-793-21711.

Part: RETAINING CLIP — BENT (R2 DOOR) · airframe 43,213 hrs · 25,217 cycles

AFT SERVICE DOOR ESCAPE SLIDE SHROUD AFT GIRT BAR RETAINING CLIP IS BENT. FORMED AFT SERVICE DOOR ESCAPE SLIDE SHROUD AFT GIRT BAR RETAINING CLIP TO ORIGINAL CONDITION PER BAC 5300-2 AND DRAWING 65C16820.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 43,213 hrs · 25,217 cycles

AT STAB STA 92.70 RIB ASSY CRACKED AT LOWER I/B FLANGE COMMON TO VERTICAL STIFFENER NR 4 (RIGHT HORIZ STAB). REPAIRED RIB PER EA.

Part: RETAINING CLIP — LOOSE (R2 DOOR) · airframe 43,213 hrs · 25,217 cycles

AFT SERVICE DOOR ESCAPE SLIDE SHROUD FWD GIRT BAR RETAINING CLIP DOES NOT RETAIN THE GIRT BAR. FORMED AFT SERVICE DOOR ESCAPE SLIDE SHROUD FWD GIRT BAR RETAINING CLIP TO ORIGINAL CONDITION TO RETAIN THE GIRT BAR PER BAC5300-2 AND DRAWING 65C16820.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,212 hrs · 25,217 cycles

THE FRAME AT THE SUPPORT BRACKET AT BS 480 STR 8R IS CRACKED. PERFORMED FRAME REPAIR AT BS 480 STR 8R PER EA 1-A53-12114R2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

THE FRAME AT THE SUPPORT BRACKET AT BS 727D STR 8L IS CRACKED. REPAIR OF FRAME AT BS 727D STR 8L WILL BE ACCOMPLISHED ON EA 1-A53-12114 R2.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 43,213 hrs · 25,217 cycles

RIGHT HORIZONTAL STAB LEADING EDGE RIB IS CRACKED L/E STA 105.26. REMOVED AND REPLACED RIB AT RIGHT HORIZONTAL STABILIZER LEADING EDGE STA 105.26 IAW SRM 51-40-02-0G-0 STEP 4 AND SRM 51-40-05-0G-0. 88964U 06FEB13

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

THE FRAME AT THE SUPPORT BRACKET AT BS 400 STR 8R IS CRACKED. ACCOMPLISHED FRAME REPAIR AT BS400 STR 8R PER EA 1-A53-12114 R2.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 43,213 hrs · 25,217 cycles

RIGHT HORIZONTAL STAB RIB AT STAB STA 92.7 IS CRACKED AT NR 2 AND NR 3 VERTICAL STIFFENERS. REPAIRED RIGHT HORIZONTAL STAB RIB AT STAB STA 92.7 PER SRM 55-10-09-2R-4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

THE FRAME AT THE SUPPORT BRACKET AT BS 787 STR 8R IS CRACKED. INSTALLED FRAME REPAIR AT BS 787 STR 8R IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

FRAME CRACKED AT I/B FASTENER HOLE FOR PSU RAIL SUPPORT BS 500A STR 8 - 9R. INSTALLED FRAME REPAIR AT BS 500A STR 8-9R IAW EA 1-A53-12114 REV 2.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 43,213 hrs · 25,217 cycles

RIGHT HORIZONTAL STAB LEADING EDGE RIB IS CRACKED LE STA 142.45. REMOVED AND REPLACED RIGHT HORIZONTAL STAB L/E RIB AT L/E STA 142.5 IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 43,212 hrs · 25,217 cycles

LEFT WING UPPER TRAILING EDGE PANEL SUPPORT ANGLE IS CRACKED AT RSS 270. REMOVED AND REPLACED CRACKED SUPPORT ANGLE AT LEFT WING UPPER TRAILING EDGE PANEL PER SRM 51-10-02-0G-0, & SOPM 20-50-01. 12872U 04FEB13

Part: ATTACH ANGLE — CRACKED (TE FLAP) · airframe 43,213 hrs · 25,217 cycles

(RIGHT WING) TRANSVERSE WEB ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT. REMOVED AND REPLACED CRACKED ATTACH ANGLE AT TRANSVERSE WEB AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM PER SRM 51-10-02-0G-0 & SRM 51-40-02-0G-

Part: GUSSET — CRACKED (RT WING) · airframe 43,213 hrs · 25,217 cycles

(RIGHT WING) UPPER T/E PANEL JUST O/B OF NR 7 SPOILER LOWER SURFACE GUSSET IS CRACKED AT LWR FWD ATTACH POINT. REMOVED AND REPLACED SUPPORT ANGLE AT RT WING UPPPER T/E PANEL O/B OF NR 7 SPOILER IAW SRM 51-40-02, STEP 9 AND SRM 51-40-05-0G-0. 88964

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

THE FRAME AT THE SUPPORT BRACKET AT BS 747 STR 8L IS CRACKED. REPAIR OF FRAME AT BS 747 STR 8L WILL BE ACCOMPLISHED ON EA 1-A53-12114 R2.

Part: FRAME — CRACKED (FUSELAGAE) · airframe 43,213 hrs · 25,217 cycles

THE FRAME AT THE SUPPORT BRACKET AT BS 827 STR 8R IS CRACKED. REPAIRED CRACKED FRAME AT THE SUPPORT BRACKET BS 827 STR 8R PER EA 1-A53-12114R2

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

FRAME CRACKED AT I/B FASTENER HOLE FOR PSU RAIL SUPPORT BS 500C STR 8 - 9L. FRAME REPAIR AT BS 500C STR 8-9L WILL BE ACCOMPLISHED ON EA 1-53-12114 R2.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 46,330 hrs · 27,111 cycles

LT NR 1 WINDOW CUTOUT FRAME CRACKED AT UPPER OTBD CORNER. REPAIRED FRAME IAW ER & SWA EA.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 43,213 hrs · 25,217 cycles

AFT CARGO BAY FLOOR PANEL 140CF IS CORRODED ALONG THE EDGES. UPON FURTHER INVESTIGATION FOUND FLOOR PANEL TO BE OUT OF LIMITS DUE TO CORROSION EXCEEDED MORE THAN 3" LONG OUT OF LIMITS IAW SRM 53-00-53-1A-1. FABRICATED NEW PANEL OUT OF 2024T3 .080" LOT 1056674. LOCATED DRILLED & COUNTERSUNK, ALODINED AND PRIMED IAW SRM 51-40-05-0G 51-40-08-0G, & 51-20-01-0G.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

ANGLE CRACKED O/B OF RT FWD MOPSILL FWD OF 294 FRAME. REMOVED, LOCATED, DRILLED AND INSTALLED NEW ANGLE O/B OF RT FWD MOPSILL FWD OF 294 FRAME PER SRM 51-40-0G-0 AND 51-40-05-0G-0.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

CORROSION FLOOR TO SIDEWALL SUPPORT RIGHT STA 767- 787 AREAS OF CORROSION. INVESTIGATED CORROSION, FOUND TO BE OUT OF LIMITS, DUE TO NO ALLOWABLE LIMITS IN SRM. REMOVED OLD FLOOR TO SIDEWALL SUPPORT, RECEIVED NEW FLOOR TO SIDEWALL SUPPORT,

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

CORROSION BS 496-500A WL 154 RT FLOOR TO SIDEWALL SUPPORT HAS AREAS OF CORROSION ON UPPER AND LOWER SURFACES. REMOVED & REPLACED BS 496-500A WL 154 RT FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-01

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

FLOOR TO SIDEWALL SUPPORT LEFT STA 727D +10 TO 787 AREAS OF CORROSION. REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 727D + 10 TO 787, FOUND TO BE OUT OF LIMITS, 100% MATERIAL LOSS, IAW SRM 53-00-53-1A-2

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,213 hrs · 25,217 cycles

LT HORIZONTAL STAB SKIN CRACKED AT STAB STA 101.90 RIB, 28.5" FWD OF REAR SPAR, APPROX .75" LONG. REPAIR ON THIS NRC, LT HORIZONTAL STAB SKIN CRACKED AT STAB STA 101.9 RIB, 28.5" FWD OF REAR SPAR. 75" LONG (LOWER SKIN) WILL BE ACCOMPLISH ON NRC T1747.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,213 hrs · 25,217 cycles

RT HORIZONTAL STAB SKIN CRACKED AT REAR SPAR, STAB STA 92.70-101.90 APPROX 1.5" LONG. REPAIRED RT HORIZ STAB LOWER SKIN COMMON TO REPAIR SPAR CHORD, AT STAB STA 92.70 TO 101.90 PER SRM 55-10-01-2R-11.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,213 hrs · 25,217 cycles

LEFT HORIZONTAL STAB SKIN CRACKED AT REAR SPAR, STAB STA 92.70-101.90, APPROX 1.5" LONG. REPAIRED LEFT HORIZONTAL STAB LOWER SKIN AT STAB STA 92.70 TO 101.9 PER SRM 55-10-01-2R-11.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 43,213 hrs · 25,217 cycles

FSD ESCAPE SLIDE FWD STOWAGE BRACKET IS LOOSE. REMOVED AND REPLACED FSD ESCAPE SLIDE FWD STOWAGE BRACKET PER SRM 51-40-02-0G-0 LEAD NR 46 06FEB13

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 43,213 hrs · 25,217 cycles

CORROSION CORROSION ON FWD CARGO DOORWAY SUB THRESHOLD UPPER SURFACE. REMOVED CORROSION AT FWD CARGO DOOR SUB THRESHOLD IAW SRM 53-30-15-1A-1 FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1. REMOVED, LOCATED, DRILLED & INSTALLED

Part: LENS — BROKEN (CABIN) · airframe 43,213 hrs · 25,217 cycles

OVERHEAD BIN AT SEAT ROW 2-3 FED BULLNOSE EMERGENCY LIGHT LENSE BROKEN. REPLACED BROKEN LIGHT LENSE ON OVERHEAD BIN AT SEAT ROW 2-3 FED BULLNOSE EMERGENCY LIGHT IAW AMM 35-51-03-960-801, STEP 20.

Part: MOTOR — FAULTY (TE FLAP) · airframe 43,213 hrs · 25,217 cycles

ALTERNATE FLAP DRIVE MOTOR INOP, SWITCH WILL NOT DRIVE FLAPS TO THE DOWN POSITION. REMOVED AND REPLACED THE ALTERNATE FLAP ELECTRIC DRIVE MOTOR IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 42,615 hrs · 24,819 cycles

EMERGENCY LIGHT TRACK COVER AT 1 ABC CRACKED. REMOVED AND REPLACED TRACK COVER PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,920 hrs · 24,390 cycles

RIGHT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 3. REMOVED & REPLACED BULB PER AMM.

Part: LIGHT — MISSING (CABIN) · airframe 41,815 hrs · 24,316 cycles

LEFT EEPLS MISSING AT ROW 15. INSTALLED EEPLS PER M/M.

Part: FLAP — DELAMINATED (LT WING) · airframe 41,561 hrs · 24,138 cycles

LEFT WING O/B AFT FLAP I/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER AMM.

Part: COVER — LOOSE (EVAC SLIDE) · airframe 40,399 hrs · 23,479 cycles

R2 DOOR EMERGENCY EXIT SLIDE COVER LOOSE. SECURED COVER IAW MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 40,389 hrs · 23,472 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: GIRT BAR — MISSING (L2 DOOR) · airframe 40,389 hrs · 23,472 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT OUT OF ADJUST. RE-INSTALLED GIRT PER MT.

Part: COVER — BROKEN (CABIN) · airframe 39,355 hrs · 22,879 cycles

EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 39,300 hrs · 22,839 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 39,300 hrs · 22,839 cycles

DURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 36,847 hrs · 21,405 cycles

DURING SCHEDULED 10Y CHECK, EMERGENCY EXIT LIGHT BATTERY PACK FAILED OPS CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 36,847 hrs · 21,405 cycles

DURING SCHEDULED 10Y CHECK, EEPLS EMERGENCY BATTERY PACK FAILED 15 MINUTE POWER CHECK BETWEEN ROW 11 TO ROW 17. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 36,847 hrs · 21,405 cycles

DURING SCHEDULED 10Y CHECK, EMERGENCY EXIT LIGHT BATTERY PACK TEST SWITCH INOP. REMOVED AND REPLACED BASE PER MM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,847 hrs · 21,405 cycles

DURING SCHEDULED SPV CHECK, FOUND CENTER WING BOX SHEAR STIFFENER CRACKED AT BS 540, RBL 7. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,847 hrs · 21,405 cycles

DURING SCHEDULED SPV CHECK, FOUND CENTER WING BOX SHEAR STIFFENER CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,847 hrs · 21,405 cycles

DURING SCHEDULED SPV CHECK, FOUND CENTER WING BOX SHEAR STIFFENER CRACKED AT BS 540, LBL 7. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,847 hrs · 21,405 cycles

DURING SCHEDULED SPV CHECK, FOUND CENTER WING BOX SHEAR STIFFENER CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 36,847 hrs · 21,405 cycles

DURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 103.83. REPAIRED SKIN PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,847 hrs · 21,405 cycles

DURING SCHEDULED SPV CHECK, FOUND CENTER WING BOX SHEAR STIFFENER CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,847 hrs · 21,405 cycles

DURING SCHEDULED SPV CHECK, FOUND CENTER WING BOX SHEAR STIFFENER CRACKED AT BS 540, LBL 42. REMOVED AND REPLACED STIFFENER PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,838 hrs · 21,397 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 5. RELAMPED PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,018 hrs · 20,343 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,018 hrs · 20,343 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: PIN — LOOSE (EVAC SLIDE) · airframe 34,273 hrs · 19,891 cycles

R1 DOOR EMERGENCY EVAC SLIDE RETAINING PIN LOOSE. SECURED PIN ASSY PER MM.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 33,739 hrs · 19,589 cycles

AIR TURNBACK, ON CLIMBOUT AS FLAPS UP B-SYSTEM ELEC PUMP LIGHT CAME ON, B PRESS OK. REMOVED AND REPLACED B-SYSTEM ELECTRIC HYDRAULICS PUMP PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,205 hrs · 19,266 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 32,434 hrs · 18,802 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 30,228 hrs · 17,471 cycles

DURING SCHEDULED HC1 CHECK, CENTER RT EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 30,228 hrs · 17,471 cycles

DURING SCHEDULED HC1 CHECK, FWD LT EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 30,228 hrs · 17,471 cycles

DURING SCHEDULED HC1 CHECK, CENTER LT EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 29,894 hrs · 17,259 cycles

DURING SCHEDULED 8Y CHECK, L1 DOOR EMERGENCY EVAC SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: CAP — BROKEN (CABIN) · airframe 29,895 hrs · 17,259 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS FLOOR END CAP BROKEN AT FRONT GALLEY. REMOVED AND REPLACED END CAP PER MM.

Part: LENS — DAMAGED (CABIN) · airframe 29,894 hrs · 17,259 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS LIGHT LENS DAMAGED AT ROW 21. REPAIRED LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,894 hrs · 17,259 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT FLOORBEAM CORRODED AT BS 328, RBL 20. REPAIRED BEAM PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 29,894 hrs · 17,259 cycles

DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR FRAME CRACKED AT BS 294. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,894 hrs · 17,259 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 986, BETWEEN RBL 50 TO LBL 50. REMOVED AND REPLACED FLOORBEAM T-CAP PER SRM.

Part: LENS — MISSING (CABIN) · airframe 29,732 hrs · 17,169 cycles

FWD CABIN EGRESS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,795 hrs · 16,599 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 3 SEAT C. REPAIRED EEPLS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 28,725 hrs · 16,556 cycles

FOUND EEPLS COVER LOOSE AT ROW 1 TO ROW 2. SECURED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 28,725 hrs · 16,556 cycles

FOUND FWD EEPLS COVER LOOSE AT ROW 1 TO ROW 2. SECURED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,960 hrs · 16,077 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 27,960 hrs · 16,077 cycles

DURING SCHEDULED HC2 CHECK, LT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,960 hrs · 16,077 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,486 hrs · 14,608 cycles

DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,486 hrs · 14,608 cycles

DURING SCHEDULED HC1 CHECK, RT OVERWING EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,486 hrs · 14,608 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 25,244 hrs · 14,456 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,282 hrs · 12,695 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 11 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,282 hrs · 12,695 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 9 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,282 hrs · 12,695 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 13 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 21,334 hrs · 12,172 cycles

FLIGHT COMPT R2 WINDOW ARCHED AND THEN CRACKED. REMOVED AND REPLACED R2 WINDOW PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 18,293 hrs · 10,390 cycles

DURING SCHEDULED HC2 CHECK, CABIN EMERGENCY EXIT LIGHT BATTERIES FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: LENS — MISSING (AFT GALLEY) · airframe 16,920 hrs · 9,638 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF LIMITS (L2 DOOR) · airframe 16,609 hrs · 9,443 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATES OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SIGN — MISSING (EMERGENCY EXIT) · airframe 12,560 hrs · 7,102 cycles

AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN, MISSING. REPLACED EMERGENCY EXIT SIGN PER MM.

Part: LENS — LOOSE (CABIN) · airframe 4,262 hrs · 2,466 cycles

EEPLS LENS LOOSE AT ROW NR 1. SECURED LENS PER MM.

Part: SLIDING WINDOW — ARCED (COCKPIT) · airframe 3,061 hrs · 1,751 cycles

ELECTRICAL SMELL AND SMOKE DUE TO F/O'S SLIDING WINDOW ARCING. REMOVED AND REPLACED WINDOW PER MM.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 951 hrs · 544 cycles

DURING SCHEDULED SERVICE CHECK, SI 11052, FOUND PLAY AT RH ELEVATOR TAB # 3 HINGE. R&R # 3 HINGE BUSHING PER MM.