N718SW

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,688 hrs · 45,737 cycles

INOPERABLE BULLNOSE EMERGENCY LIGHT 20ABC. RE-LAMPED EMERGENCY AREA LIGHT AT 20 ABC, PER AMM 33-51-03.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,688 hrs · 45,737 cycles

EMERGENCY LIGHT ABOVE 20 ABC IS INOPERABLE. RE-LAMPED EMERGENCY LIGHT ABOVE 20 ABC, PER AMM 33-51-03.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,744 hrs · 45,131 cycles

EMERGENCY LITES @ ROW 16 & 19 RIGHT & AFT GALLEY INOP / REMOVED &N REPLACED BATTERY PACK IN AFT OVERHEAD GALLEY IAW AMM 33-51-06

Part: RETAINER — DAMAGED (HORIZONTAL STAB) · airframe 75,347 hrs · 44,877 cycles

LH UPPER HORIZONTAL STAB AFT BLADE SEAL RETAINER IS DAMAGED / REMOVED DAMAGED LH UPPER HSTAB AFT BLADE SEAL RETAINER APPLIED TOPCOAT TO NEW PART AND INSTALLED SEAL RETAINER IAW SRM 51-40-02-0G-0 SECTION 9 AND AMM 51-21-73-370-801. ATAG: U10971

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 75,347 hrs · 44,877 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1670 FAILED BATTERY PACK CAPACITY CHECK. / R&R BATTERY PACK M1670 IAW AMM.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 75,347 hrs · 44,877 cycles

LEFT MLG WHEEL WELL STA 663 LBL28 WL 148; VERTICAL STIFFENER IS CRACKED. / REMOVED AND REPLACE LH MLG WHEEL WELL STA 663 LBL 28 WL 148 VERTICAL STIFFENER IAW SRM 51-40-02-0G-0 & 51-40-05-0G-0 & DWG 111A100 REV -

Part: INTERCOSTAL — CORRODED (AFT CARGO) · airframe 75,347 hrs · 44,877 cycles

AFT CARGO COMPARTMENT; STA 727A + 14 TO 727B LBL3 WL160; INTERCOSTAL HAS CORROSION ON RH SIDE. / BLENDED CORROSION ON INTERCOSTAL IN AFT CARGO COMPARTMENT STA 727A TO 727B LBL 3 WL 160. OUT OF LIMITS REPLACED INTERCOSTAL IAW BOEING DWG# 146A7500 AND 737 SRM 51-40-02-0G-0. FOUND ORIG T .040' LOSS .021' REMIANING .019' OUT OF LIMITS IAW SRM 53-00-53-1A-2

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 75,347 hrs · 44,877 cycles

LEFT WHEEL WELL UPPER ATTACH ANGLE CRACKED AT BS. 663, BETWEEN LBL 44 TO LBL 45. / REPAIRED ANGLE IAW SRM & AMM.

Part: FLOOR SUPPORT — CORRODED (BS 847) · airframe 75,347 hrs · 44,877 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE, R/H FACE OF INTERCOSTAL AFT CORRODED AT BS. 847, RBL 6. / R&R INTERCOSTAL IAW SRM, AMM, & DWG.

Part: SEAL — DAMAGED (HORIZONTAL STAB) · airframe 75,347 hrs · 44,877 cycles

DOT #2; RH HOZ STAB; PANEL 343AB; SLIDING SEAL KNIFED EDGED. / REMOVED AND REPLACED SLIDING SEAL KNIFED EDGED IAW SRM 51-40-02-0G-0 SECTION 4; AMM 51-21-41-370-802 AND 51-21-72-370-801. ATAG: WN2574

Part: SEAL — DAMAGED (HORIZONTAL STAB) · airframe 75,347 hrs · 44,877 cycles

DOT #004; LH HOZ STAB; PANEL 333AB; SLIDING SEAL KNIFED EDGED. / REMOVED AND REPLACED L/H HORZ STAB PANEL 333AB SLIDING SEAL IAW B737-700 SRM 51-40-02-0G-0 STEP 4 PAGE 2 WN6447

Part: SUPPORT ANGLE — CRACKED (VERTICAL STAB) · airframe 75,347 hrs · 44,877 cycles

INSIDE VERTICAL STABILIZER LATERAL SUPPORT ANGLE CRACKED IN RADIUS AT BS. 1016, LBL 12, 8" ABOVE FUSELAGE SKIN / R&R ANGLE IAW DWG AND SRM.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 75,347 hrs · 44,877 cycles

PASSENGER CABIN FLOORBOARD 231ZF HAS UPPER PLY DAMAGE / REPAIRED FRAYING/EXPOSED COMPOSITE AT UPPER SURFACE FACESHEET ON FLOORBOARD 231ZF IAW B737 SRM 53-00-50-2R-1; PAR 3 (A;C;E+F; K1;L1;M1) + SRM 53-00-50-2R-0; PAR 5 - REV 69.

Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 75,347 hrs · 44,877 cycles

PASSENGER CABIN FLOORBOARD 241DF HAS UPPER PLY DAMAGE. REPAIRED DAMAGE ON FLOOR PANEL 241DF. BONDED REPAIR PLIES AND CURED. TAP TEST GOOD. IAW B737-700 SRM 53-00-50-2R-1 REV 69; SRM 53-00-50-2R-0 REPAIR GENERAL REV 69.

Part: SUPPORT WEB — CORRODED (BS 747-767) · airframe 75,347 hrs · 44,877 cycles

AFT PIT Z-ANGLE RH SIDE SUPPORT WEB HAS EVIDENCE OF CORROSION FROM STA 747 TO STA 767 RBL 21 AND W/L 158 / REMOVED CORROSION ON Z-ANGLE SUPPORT WEB FROM STA 747 - 767. NO PUBLISHED LIMITS FOUND. OUT OF LIMITS. REMOVED SUPPORT WEB AND DRILLED UP NEW SUPPORT WEB P/N 146A1500-8. INSTALLED SUPPORT WEB IAW SRM 51-40-02-0G-0. REFERENCE USED 51-40-05-0G-0 AND 53-00-53-1A-2 AND DWG 146A7502 REV A (STAT 747 TO 767 RBL 21' AND W/L 158) P/N 146A7505-8 ATAG WN9928

Part: RETAINER — CHAFED (BS 1156) · airframe 75,347 hrs · 44,877 cycles

EXTERNAL FUSELAGE; RH SIDE. STA 1156; LOWER AFT SLIDING SEAL RETAINER HAS CHAFING DAMAGE. / INSPECTED PANEL ASSY AND FOUND NO STRUCTURAL WEAK LIMITS PUBLISHED REMOVED AND REPLACED R/H STA 1156 LOWER AFT SLIDING SEAL RETAINER IAW SRM 51-40-02 AND DWG 181A8050 REV-

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 75,347 hrs · 44,877 cycles

LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL IN FUSELAGE IS CRACKED ABOVE AFT CLEVIS / REMOVED AND REPLACED LEFT HORIZONTIAL STAB FWD UPPER SLIDING SEAL IAW B737 AMM 53-31-31.

Part: ANGLE — CORRODED (BS 747-767) · airframe 75,347 hrs · 44,877 cycles

AFT PIT Z-ANGLE R/H SIDE HAD SPOTS OF CORROSION BETWEEN BS. 747 TO BS. 767, RBL 21. / R&R Z-ANGLE IAW SRM.

Part: CARGO TRACK — CORRODED (BS 767-887) · airframe 75,347 hrs · 44,877 cycles

AFT CARGO COMPARTMENT R/H RAIL CORRODED BETWEEN BS. 767+10 TO BS. 887, RBL 15. / R&R TRACK SECTION IAW SRM.

Part: ANGLE — CORRODED (BS 727E-767) · airframe 75,347 hrs · 44,877 cycles

AFT PIT Z-ANGLE L/H SIDE HAD SPOTS OF CORROSION BETWEEN BS. 727E TO BS. 767+8, LBL 24. / R&R Z-ANGLE IAW SRM.

Part: ANGLE — CORRODED (AFT CARGO) · airframe 75,347 hrs · 44,877 cycles

AFT PIT LH ZANGLE HAS SPOTS OF CORROSION FROM STA 767+8' TO STA 827 WL 156 LBL 24 REMOVED CORROSION ON LH ZANGLE PN 146A75021 STA 767+8' TO STA 827. FOUND ORIG T .040' LOSS .020' REMAINING .020' OUT OF LIMITS IAW SRM 5300531A1 REPAIRED Z ANGLE ON NRC Y164910

Part: ANGLE — CORRODED (AFT CARGO) · airframe 75,347 hrs · 44,877 cycles

AFT PIT Z-ANGLE LH SIDE HAS SPOTS OF CORROSION FROM STA 727C TO 727E WL 156 LBL24 REMOVED CORROSION ON L.H ZANGLE PN 146A75021 STA 727C-727E FOUND ORIG T .040' WITH .015' LOSS .025' REMAINING. OUT OF LIMITS IAW SRM 5300531A1. REPAIRED Z ANGLE ON NRC Y164910

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 75,347 hrs · 44,877 cycles

AFT CARGO COMPARTMENT FLOOR TRANSITION STRIP AT STA 887 RBL 20-LBL 15 W/L 157 IS CORRODED / REMOVED AND INSTALLED NEW STRIP ON AFT CARGO COMPARTMENT FLOOR TRANSITION STA 887 RBL 20 LBL 15 W/L 157. SRM 51-40-02-0G-0 & DRAWING #146A9401 REV C.

Part: PLATE — CRACKED (LT WING) · airframe 75,347 hrs · 44,877 cycles

LT WING REAR SPAR LOWER CHORD 10" INBOARD OF #3 FLAP TRACK WIGGLE PLATE HAD EVIDENCE OF A CRACK AT FASTENER HOLE. R&R WIGGLE PLATE IAW SRM.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 75,347 hrs · 44,877 cycles

CABIN FLOOR STRUCTURE; PANEL BREAK CRACKED AT FASTENER STA 540 LBL 1 WL 208 / REPLACED CABIN FLOOR STRUCTURE PANEL BREAK IAW SRM 51-40-02 AND BOEING DWG 143A5240 REV- STA 540 LBL 1. 'A' TAG WN6323

Part: PLATE — DAMAGED (L1 DOOR HANDLE) · airframe 75,347 hrs · 44,877 cycles

L1 DOOR HANDLE; CAM PLATE IS DAMAGED. / REMOVED AND REPLACED WITH A NEW L1 DOOR HANDLE CAM PLATE I/A/W CMM 52-16-01.

Part: PLATE — CRACKED (LT WING) · airframe 75,347 hrs · 44,877 cycles

LT WING TRAILING EDGE PANEL 551GB WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM & DWG.

Part: COVER — OUT OF POSITION (R1 DOOR) · airframe 74,846 hrs · 44,534 cycles

R1 DOOR SLIDE PULL HANDLE YELLOW COVER WAS NOT SHOWING/ PULLED COVER DOWN AND SECURED TO VELCRO IAW SIP.

Part: LIGHT — DELAMINATED (CABIN) · airframe 73,250 hrs · 43,465 cycles

AFT GALLEY AREA L/H AND R/H EGRESS STRIPS DELAMINATED. R&R EGRESS STRIPS PER DRAWING.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 72,893 hrs · 43,231 cycles

AFT OF R/H WING EMERGENCY LIGHT INOP. R&R LIGHT PER AMM.

Part: SENSOR — FAULTY (TE FLAP) · airframe 72,392 hrs · 42,917 cycles

DECLARED EMERGENCY, ON TAKEOFF OUT OF SMF LEADING EDGE FLAP TRANSMIT LIGHT ILLUMINATED. RAN QRH. LIGHT EXTINGUISHED. ON APPROACH TO LAX. PUT FLAP LEVER TO POSITION I, NO MOVEMENT ON FLAP GAUGE OR LE DEVICES PANEL. FLAP GAUGE NEEDLES HAD A SMALL SPLIT. RAN QRH FOR TRAILING EDGE FLAPS UP LANDING WITH FLAP ASYMMETRY LANDING UNEVENTFUL. R&R NR 1 FLAP SKEW DETECTION SENSOR PER MM.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 71,541 hrs · 42,364 cycles

FORWARD LAV SMOKE ALARM WENT OFF IN FLIGHT. R&R SMOKE DETECTOR PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,670 hrs · 41,784 cycles

LT EMERGENCY LIGHT INOP AT ROW 1. RELAMPED LIGHT IAW AMM.

Part: CONTROLLER — ARCED (COCKPIT) · airframe 70,145 hrs · 41,451 cycles

R2 WINDOW ARCED. R&R R2 WINDOW HEAT CONTROLLER PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 70,145 hrs · 41,451 cycles

R2 WINDOW ARCED. R&R WINDOW PER MT.

Part: HOOK — LOOSE (R2 DOOR GIRT BAR) · airframe 69,216 hrs · 40,875 cycles

R2 DOOR SLIDE GIRT BAR RETAINING HOOK LOOSE. R & R THE GIRT BAR IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 69,204 hrs · 40,865 cycles

RT OVERWING EMERGENCY EXIT HATCH LIGHT COVER BROKEN. R&R LIGHT PER AMM.

Part: HOOK AND LOOP — LOOSE (EMERGENCY EXIT) · airframe 69,050 hrs · 40,770 cycles

RIGHT EMERGENCY EXIT DOOR, CLOSING STRAP HANDLE COVER LOOSE. SECURED THE HOOK AND LOOP IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,007 hrs · 40,740 cycles

R2 DOOR EMERGENCY EVAC SLIDE EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: DRAIN — CRACKED (FUSELAGE) · airframe 69,007 hrs · 40,740 cycles

AFT FUSELAGE DRAIN CRACKED AT BS 1016. R&R DRAIN IAW SRM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 69,007 hrs · 40,740 cycles

EMERGENCY BATTERY PACK DID NOT PASS CAPACITY CHECK AT BS 603, RBL 67. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 69,007 hrs · 40,740 cycles

EMERGENCY EXIT BATTERY DID NOT PASS CAPACITY CHECK AT BS 603, LBL 67. R&R BATTERY PACK IAW AMM.

Part: ATTACH ANGLE — CRACKED (BS 653-663) · airframe 69,007 hrs · 40,740 cycles

LOWER FUSELAGE ATTACH ANGLE CRACKED BETWEEN BS 653 TO 663, LBL 27.5. R & R THE ATTACH ANGLE IAW SRM AND DWG.

Part: CONNECTOR — MISSING (CABIN) · airframe 69,007 hrs · 40,740 cycles

G4 GALLEY EMERGENCY EXIT LIGHT CONNECTORS MISSING. R&R CONNECTORS IAW SWPM AND AMM.

Part: FRAME — CRACKED (BS 312) · airframe 69,007 hrs · 40,740 cycles

FUSELAGE FRAME CRACKED AT BS 312, BETWEEN STRINGERS 5L TO 6L. REPAIRED THE FRAME IAW EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,007 hrs · 40,740 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE RIB FLANGE CRACKED AT HSS 78.29. R & R THE RIB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 270) · airframe 69,007 hrs · 40,740 cycles

COCKPIT ENTRY FLOORBEAM ANGLE CORRODED AT BS 270, LBL 9 TO RBL 9. R & R THE FLOORBEAM ANGLE IAW SRM AND EA.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 69,007 hrs · 40,740 cycles

BULKHEAD TO TOP SKIN PANEL CRACKED AT BS 663, LBL 35. REPAIRED ANGLE IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 69,007 hrs · 40,740 cycles

RT WING INBOARD OF INBOARD DEFLECTOR RIB, UPPER FIXED PANEL CENTER CURVED STIFFENER ANGLE RIB CRACKED. R&R ANGLE IAW SRM AND DWG.

Part: CHANNEL — CRACKED (VERTICAL STAB) · airframe 69,007 hrs · 40,740 cycles

VERTICAL STABILIZER PANEL 324AR METAL CHANNEL CRACKED. R&R CHANNEL IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,007 hrs · 40,740 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB FLANGE CRACKED AT HSS 105.26. R & R THE RIB IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,007 hrs · 40,740 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB FLANGE CRACKED AT STA 142.45. R&R RIB ASSEMBLY IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,007 hrs · 40,740 cycles

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

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,007 hrs · 40,740 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB FLANGE CRACKED AT HSS 151.75. R & R THE RIB IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,007 hrs · 40,740 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB FLANGE CRACKED AT HSS 95.96. R & R THE RIB ASSEMBLY IAW SRM AND DWG.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 69,007 hrs · 40,740 cycles

RT WHEEL WELL U SHAPED STIFFENER CRACKED AT BS 663, RBL 15. R&R STIFFENER IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,007 hrs · 40,740 cycles

RT L ANGLE STIFFENER CRACKED AT BS 663. R&R STIFFENER IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,007 hrs · 40,740 cycles

RT AIR CONDITION BAY BULKHEAD ''L'' ANGLE CRACKED AT BS 663. REPAIRED "L" ANGLE IAW EA..

Part: PLATE — CRACKED (RT WING) · airframe 69,007 hrs · 40,740 cycles

RT WING LOWER TRAILING EDGE WAFFLE PLATE CRACKED AT STA ORSS 261. R&R PLATE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,007 hrs · 40,740 cycles

EXTERNAL FUSELAGE FAIRING ATTACH STRUCTURE FRAME CRACKED AT BS 500D, BETWEEN STR 18L TO STR 19L. R&R FRAME IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,007 hrs · 40,740 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS 663+2, BETWEEN LBL 32 TO LBL 34. R&R WEB IAW EA.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 69,007 hrs · 40,740 cycles

FORWARD CARGO BAY AFT CORNER SCUFF PLATE CRACKED. REPAIRED THE SCUFF PLATE IAW EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 69,007 hrs · 40,740 cycles

FORWARD CARGO PIT FORWARD CORNER SCUFF PLATE CRACKED. R&R SCUFF PLATE IAW SRM AND EA.

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 69,007 hrs · 40,740 cycles

BS 663 BULKHEAD LEADING EDGE STIFFENER CRACKED, RBL 50. REPAIRED THE BULKHEAD IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,007 hrs · 40,740 cycles

RT WING NR 5 SLAT NOSE SKIN CRACKED AT STA 85.19 AT OUTBOARD LOWER FASTENER HOLE. REPAIRED SKIN IAW SRM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 67,688 hrs · 39,888 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS COVER LOOSE. R&R SIGN ASSEMBLY IAW AMM.

Part: TIE — MISSING (R1 DOOR) · airframe 66,219 hrs · 38,978 cycles

R1 DOOR EMERGENCY EVAC SLIDE AFT LANYARD CLIP LADDER TIE MISSING. INSTALLED LADDER TIE PER SIP.

Part: SUPPORT FITTING — CORRODED (RT WING) · airframe 66,091 hrs · 38,897 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.

Part: SUPPORT FITTING — CORRODED (LT WING) · airframe 66,091 hrs · 38,897 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 65,299 hrs · 38,420 cycles

CABIN PRESSURE FAILED AT TOD, THROTTLES RETARDED AND CABIN PRESSURE WAS LOST. MANUAL SELECTED & CABIN PRESSURE RISE STOPPED AT 11,000 MSL, THEN PRESSURE RECOVERED TO 5000' EMERGENCY DESCENT CONTINUE TO 24,000 THEN FURTHER TO 16000'. DECLARED EMERGENCY. R & R NR 1 CABIN PRESSURE CONTROLLER IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 65,191 hrs · 38,357 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 65,191 hrs · 38,357 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 65,191 hrs · 38,357 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R&R BATTERY PER AMM.

Part: FITTING — LOOSE (L2 DOOR) · airframe 64,762 hrs · 38,110 cycles

L2 DOOR SLIDE LINER HOLDING CLIP LOOSE. SECURED CLIP IAW SIP.

Part: MOUNT — MISSING (L2 DOOR SLIDE) · airframe 64,718 hrs · 38,082 cycles

L2 DOOR SLIDE FORWARD MOUNTING BOLT FOR AFT DOOR THREADS MISSING. R & R THE MOUNTING ASSEMBLY IAW MT & AMM.

Part: LENS — MISSING (CABIN) · airframe 63,514 hrs · 37,395 cycles

RIGHT BULLNOSE EMER LIGHT LENS MISSING AT ROW 6. INSTALLED LENS IAW MM.

Part: TORQUE TUBE — CORRODED (TE FLAP) · airframe 62,939 hrs · 37,067 cycles

LEFT WING INBD FLAP, INBD CARRIAGE PRIMARY TORQUE TUBE CORRODED. R & R TORQUE TUBE IAW AMM.

Part: TORQUE TUBE — CORRODED (TE FLAP) · airframe 62,939 hrs · 37,067 cycles

LEFT WING INBD FLAP, INBD CARRIAGE SECONDARY TORQUE TUBE CORRODED. R & R TORQUE TUBE IAW AMM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

INTERCOSTAL CORRODED, BETWEEN BS 1006 - 1016, RBL 39. R & R INTERCOSTAL IAW SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 62,939 hrs · 37,067 cycles

LEFT WING NR 2 SLAT DELAMINATED ON LOWER SIDE OF TE OF WEDGE. R & R NR 2 SLAT IAW SRM.

Part: WEB — DAMAGED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

WEB DAMAGED, BETWEEN BS 987 - 1006, BETWEEN LBL 31 - 41. R & R WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

TOP T CAP OF FLOORBEAM SKIN, CORRODED AT BS 987, BETWEEN RBL 51 TO LBL 51. REPAIRED SKIN IAW SRM.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 62,939 hrs · 37,067 cycles

AFT CARGO FLOOR CARGO TIE DOWN CRACKED, AT BS 767, RBL 14. R & R TRACK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

R1 DOOR FWD FRAME CRACKED, AT STATION 294.5, LOWER CORNER. REPAIRED FRAME IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

FASTENER HOLES & GALLEY MOUNT BRACKET WEBBING CORRODED, BETWEEN BS 987 - 1016, RBL 40. REPAIRED WEB IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

LEFT L ANGLE CORRODED, BETWEEN BS 955 - 940, LBL 50. R & R L ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

RIGHT L ANGLE CORRODED, BETWEEN BS 947 - 997, RBL 55. R & R L ANGLE IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

AFT GALLEY DOOR FRAME CORRODED AT BS 992, BEHIND SPACER BLOCK AT FLOOR Z ANGLE. REPAIRED FRAME IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

INTERCOSTAL CORRODED, BETWEEN BS 767 - 787, RBL 6. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, RBL 31. R & R INTERCOSTAL IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

RIGHT LOWER Z ANGLE CORRODED, BETWEEN BS 291 - 360. R & R Z ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, LBL 44. R & R INTERCOSTAL IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

SHEAR TIE AT FRAME CRACKED AT BS 380, STRINGER 17L. R & R SHEAR TIE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

INTERCOSTAL CRACKED, BETWEEN BS 328 - 344, LBL 44. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

INTERCOSTAL CORRODED AT BS 807, RBL 6. R & R INTERCOSTAL IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

AFT CARGO FLOOR WEB CORRODED, BETWEEN BS 847 - 867, RBL 20. R & R WEB IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 62,939 hrs · 37,067 cycles

LEFT WING LOWER TE SHELF PANEL INBD OF DEFLECTION RIB WS 261, WAFFLE PLATE CRACKED. R & R WAFFLE PLATE IAW SRM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 62,939 hrs · 37,067 cycles

LEFT WING UPPER TE SHELF PANEL, INBD OF DEFLECTION RIB WS 253, AFT SUPPORT BRACKET CRACKED. REPAIRED BRACKET IAW SRM.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 62,939 hrs · 37,067 cycles

FORWARD CARGO DOOR SKIN CREASED IN FWD LOWER CORNER, 3" ABOVE SKIN LOWER EDGE. REPAIRED SKIN IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,939 hrs · 37,067 cycles

FUSELAGE SKIN CREASED, BETWEEN BS 378 - 381.5, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: COVER — DETERIORATED (CABIN) · airframe 62,939 hrs · 37,067 cycles

LEFT EMER EXIT, LOWER LIGHT LENS COVER DETERIORATED. R & R COVER IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 59,543 hrs · 35,098 cycles

LEFT WING OTBD AFT FLAP TE DELAMINATED ON INBD TE. R & R AFT FLAP IAW MM.

Part: LENS — MISSING (CABIN) · airframe 59,335 hrs · 34,978 cycles

L1 DOOR EMER EXIT LENS MISSING. R & R LENS IAW MM.

Part: COVER — MISSING (CABIN) · airframe 58,758 hrs · 34,648 cycles

L1 DOOR EXIT LIGHT COVER MISSING. REPLACED COVER IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,758 hrs · 34,648 cycles

EMERGENCY LIGHT BATTERY PACK M1673 FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: SKIN PANEL — ERODED (VERTICAL STAB) · airframe 58,758 hrs · 34,648 cycles

VERTICAL FIN LE HF ANTENNA PANEL HAS A HOLE ERODED THROUGH. REPAIRED PANEL IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,437 hrs · 33,903 cycles

RIGHT EEPLS INOPERATIVE AT ROW 6. RELAMPED EEPLS IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

RIGHT NR 1 WINDOW FRAME UPPER HOLE CRACKED IN OTBD WINDOW POST. R & R FRAME IAW ACO.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,437 hrs · 33,903 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 92.7 CRACKED AT 2ND & 3RD VERTICAL STIFFENERS AFT AT BOTTOM. REPAIRED RIB IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 57,437 hrs · 33,903 cycles

LEFT HORIZONTAL STAB VERTICAL STIFFENER RIB CRACKED AT STATION 147.9. REPAIRED STIFFENER RIB PER EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

RIGHT NR 1 FLIGHT DECK WINDOW FRAME, 1ST INBD HOLE CRACKED AT BS 217, WL 258. R & R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 57,437 hrs · 33,903 cycles

COCKPIT LT WINDOW NR 3 POST FRAME CRACKED. R & R FRAME IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FLIGHT DECK RT NR 1 WINDOW FRAME UPPER OTBD CORNER CRACKED. R & R FRAME IAW ACO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

LONGITUDINAL FLOORBEAM FLANGE HOLES CRACKED BETWEEN BS 727A+17 TO 727A+18, RBL 45.5. REPAIRED FLANGE IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

LONGITUDINAL FLOORBEAM INBD & OTBD FLANGE HOLES CRACKED AT BS 727A+18.25, LBL 24.75. REPAIRED FLANGE IAW ER & EA.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 57,437 hrs · 33,903 cycles

COCKPIT RT WINDOW NR 3 POST FRAME CRACKED. R & R FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FUSELAGE FRAME CRACKED AT STATION 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FUSELAGE FRAME CRACKED AT STATION 500A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FUSELAGE FRAME CRACKED AT STATION 520, STRINGER 8L. REPAIRED FRAME IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FUSELAGE FRAME CRACKED AT STATION 440, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FUSELAGE FRAME CRACKED AT STATION 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FUSELAGE FRAME CRACKED AT STATION 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FUSELAGE FRAME CRACKED AT STATION 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FUSELAGE FRAME CRACKED AT STATION 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FUSELAGE FRAME CRACKED AT STATION 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 57,437 hrs · 33,903 cycles

CENTER WING LOWER BULKHEAD CHORD CRACKED AT BS 540, BETWEEN STRINGER 22R TO 23R. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,437 hrs · 33,903 cycles

LEFT WING NR 3 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: ACTUATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 56,280 hrs · 33,243 cycles

DIVERSION, FUEL IMBALANCE IN FLIGHT CROSS FEED CB POPPED IN FLIGHT. R & R ENGINE FUEL CROSS FEED VLV ACTUATOR IAW AMM.

Part: CONNECTOR — DIRTY (FUEL SYSTEM) · airframe 56,085 hrs · 33,133 cycles

DIVERSION ON CLIMB OUT, "FUEL EMPTY " ALERT. P6-3:B7 CB POPPED. RESET FUEL CROSS FEED VLV CB & CLEANED CONNECTOR IAW MM.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 54,661 hrs · 32,280 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINER CLIP LOOSE. SECURED CLIP IAW SRM.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 54,661 hrs · 32,280 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD & AFT RETAINER CLIPS LOOSE. SECURED CLIPS IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 54,661 hrs · 32,280 cycles

RT AFT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. R&R BATTERY IAW AMM.

Part: BALLAST — OVERHEATED (CABIN) · airframe 52,854 hrs · 31,221 cycles

PUT RIGHT PACK ON FOR AIR AND IMMEDIATELY SMELLED AN ODOR SIMILAR TO A BLOWN OUT MATCH. GASPER FAN AND RECIRC FAN SWITCHES WERE BOTH IN THE OFF POSITION. REMOVED AND REPLACED CEILING LIGHT ASSY BALLAST AT ROW 14 TO 16 RIGHT SIDE DUE TO EXCESS / BALLAST HEAT AS PER M/M.

Part: ACTUATOR — CRACKED (RT SPOILER) · airframe 52,372 hrs · 30,901 cycles

NR 12 SPOILER ACTUATOR HOUSING IS CRACKED. REMOVED AND REPLACED NR 12 SPOILER ACTUATOR PER M/M.

Part: LIGHT — BROKEN (CABIN) · airframe 50,976 hrs · 30,010 cycles

R1 DOOR EGRESS LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 50,466 hrs · 29,702 cycles

RIGHT WING INBOARD MAIN FLAP LOWER SURFACE TRAILING EDGE DELAMINATED. REPAIRED MAIN FLAP IAW SRM & AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,252 hrs · 29,568 cycles

AFT LT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,252 hrs · 29,568 cycles

FWD LT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,252 hrs · 29,568 cycles

AFT RIGHT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 49,318 hrs · 29,028 cycles

RT HORIZ STAB LOWER SKIN CRACKED AT STAB STA 129.5. REPAIRED SKIN IAW AMM AND SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 47,952 hrs · 28,246 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. SLIDE WILL BE RE-INSTALLED PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,632 hrs · 26,936 cycles

DURING SCHEDULED HC1D CHECK, L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,632 hrs · 26,936 cycles

DURING SCHEDULED HC1D CHECK, R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 44,271 hrs · 26,119 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 7. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — PUNCTURED (SPOILER) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING I/B NR 7 GROUND SPOILER LOWER SKIN PUNCTURED. REMOVED AND REPLACED SPOILER PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 6.14. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO COMPT FLOOR LEFT Z-ANGLE CORRODED BETWEEN BS 493 TO BS 511B. REMOVED AND REPLACED Z-ANGLE SECTION PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM CORRODED AT BS 330.65. REPAIRED BEAM PER SRM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT WING I/B AFT FLAP LOWER SURFACED PUNCTURED. REMOVED AND REPLACED AFT FLAP PER SRM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING I/B AFT FLAP LOWER SURFACE PUNCTURED. REMOVED AND REPLACED AFT FLAP ASSY PER MM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM FORWARD OF L1 DOOR CRACKED AT BS 302.5. REMOVED AND REPLACED CHORD PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,893 hrs · 25,879 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM AT R2 DOOR CORRODED, BETWEEN BS 967 TO BS 986.5. REPAIRED BEAM PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 43,536 hrs · 25,672 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 40,355 hrs · 23,761 cycles

R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 37,569 hrs · 22,081 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,602 hrs · 22,100 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT EXTERNAL POWER RECEPTACLE DOOR CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,133 hrs · 21,202 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,146 hrs · 21,208 cycles

R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,143 hrs · 20,593 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,143 hrs · 20,593 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,028 hrs · 20,528 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,625 hrs · 19,667 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 33,462 hrs · 19,565 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,990 hrs · 19,282 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 32,869 hrs · 16,218 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROW 6 DEF AND ROW 11 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 32,600 hrs · 19,052 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (CABIN) · airframe 31,850 hrs · 18,584 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 30,325 hrs · 17,738 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,872 hrs · 17,452 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 36 TO LBL 40. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CORRODED (BS 508) · airframe 29,872 hrs · 17,425 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 508, BL 0. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,872 hrs · 17,475 cycles

DURING SCHEDULED 8Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: BEAM — CORRODED (FUSELAGE) · airframe 29,872 hrs · 17,475 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 5 TO RBL 44. REPAIRED FLOORBEAM PER SWA EA.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 29,872 hrs · 17,475 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT AND RT HORIZONTAL STAB LUG FACES CORRODED. REPAIRED HORIZONTAL STAB PER SWA EA.

Part: BEAM — CORRODED (FUSELAGE) · airframe 29,872 hrs · 17,475 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 8 TO RBL 12. REPAIRED FLOORBEAM PER SWA EA.

Part: COVER — LOOSE (CABIN) · airframe 29,806 hrs · 17,425 cycles

EEPLS LIGHT COVER LOOSE AT ROW 6 ABC TO ROW 8 ABC. REMOVED AND REPLACED LIGHT COVER PER MM.

Part: HEAT EXCHANGER — LEAKING (NR 1 ENGINE) · airframe 29,781 hrs · 17,414 cycles

DECLARED EMERGENCY, NR 1 ENGINE FUEL LEAK AT CRUISE, 1500 LBS PER HOUR MORE THAN NR 2 ENGINE. REMOVED AND REPLACED NR 1 ENGINE FUEL/OIL HEAT EXCHANGER PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 29,500 hrs · 17,262 cycles

DURING SCHEDULED HC2 CHECK, ROW 16 ABC EMERGENCY EXIT LIGHT FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 29,500 hrs · 17,262 cycles

DURING SCHEDULED HC2 CHECK, RT OVERWING EMERGENCY EXIT LIGHT FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 29,500 hrs · 17,262 cycles

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

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 29,500 hrs · 17,262 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 28,910 hrs · 16,925 cycles

R2 DOOR EMERGENCY EXIT EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,428 hrs · 16,112 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS STRIP DAMAGED. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 26,973 hrs · 15,880 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — PUNCTURED (T/E FLAP) · airframe 23,736 hrs · 14,069 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING T/E INBD AFT FLAP SKIN PUNCTURED NEAR INBOARD END. REPAIRED AFT FLAP PER SWA EA.

Part: LIGHT — DELAMINATED (CABIN) · airframe 23,504 hrs · 13,938 cycles

DURING SCHEDULED MV2 CHECK, FOUND 2 EACH SECTIONS OF EEPLS STRIPS BETWEEN ROWS 6 DEF AND 10 DEF, DELAMINATED. REMOVED AND REPLACED EEPLS STRIPS PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 22,246 hrs · 13,244 cycles

DURING SPV, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 19 ABC, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 22,191 hrs · 13,216 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,566 hrs · 10,685 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACKS FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: ENGINE — FLAMED OUT (NR 1) · airframe 17,059 hrs · 10,380 cycles

IN-FLT SHUTDOWN, DIVERSION, DECLARED EMERGENCY. EN ROUTE TO MCI, NR 1 ENGINE FLAMED OUT. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: FILTER — DIRTY (LT ENGINE) · airframe 11,052 hrs · 10,376 cycles

IN-FLIGHT SHUTDOWN, DECLARED EMERGENCY. DURING CRUISE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE SUPPLY OIL FILTER & SCAVENGE OIL FILTER PER MM. C/W ENGINE RUN, NO DEFECTS FOUND.

Part: MODULE — LEAKING (RT MLG W/W) · airframe 16,173 hrs · 9,913 cycles

AIR TURNBACK, DECLARED EMERGENCY, SLIGHT HYDRAULIC SMELL DURING TAXI, STRONG HYDRAULIC SMELL AT HIGH POWER DURING TAKEOFF. REMOVED AND REPLACED HYDRAULIC RESEVOIR AIR PRESSURE MODULE, BOTH COALESCER BAGS AND HEPA FILTER PER MM.

Part: HINGE — WORN (LT ELEVATOR) · airframe 15,593 hrs · 9,563 cycles

DURING SCHEDULED PM CHECK, SWA SI 11075-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE PER SRM.

Part: LENS — MISSING (CABIN) · airframe 14,981 hrs · 9,204 cycles

EEPLS LENS MISSING AT ROW NR 11. INSTALLED LENS PER MM.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 14,369 hrs · 8,885 cycles

INFLIGHT SHUT DOWN, DIVERSION, DURING CRUISE NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED, LIGHT REMAINED ON EVEN AT IDLE. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: SLIDE — OUT OF ADJUST (AFT CABIN DOORS) · airframe 14,059 hrs · 8,698 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: BUSHING — WORN (BOTH ELEVATORS) · airframe 13,892 hrs · 8,593 cycles

DURING SCHEDULED SERVICE CHECK, SI 11038-55, FOUND BOTH LT AND RT ELEVATOR TAB HINGE BUSHINGS WORN. REMOVED AND REPLACED ALL 4 HINGE BUSHINGS ON BOTH TABS PER MM.

Part: COVER — MISSING (CABIN) · airframe 12,128 hrs · 7,570 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER MISSING AT ROW 2. INSTALLED COVER PER MM.

Part: BRACKET — LOOSE (FWD ENTRY DOOR) · airframe 11,747 hrs · 7,336 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE CONTAINER RH ATTACH BRACKET LOOSE. SECURED BRACKET PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,941 hrs · 6,877 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED OVERWING EXIT LIGHT PER MM.

Part: COVER — CRACKED (CABIN FLOOR) · airframe 10,498 hrs · 6,639 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROW'S 1, 2, 4, 6, 13, 15, 16, 17 & 23. R&R EEPLS TRACK COVERS PER MM.

Part: LIGHT — INOPERATIVE (ROW 19) · airframe 7,944 hrs · 5,094 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY LIGHT INOP AT ROW 19 RT. REMOVED AND LAMP PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 7,789 hrs · 4,999 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY. REINSTALLED SLIDE ASSY PER MM.

Part: CONTROLLER — ERRATIC (COCKPIT) · airframe 7,612 hrs · 4,904 cycles

CABIN PRESS ALT WARNING HORN SOUNDED, DESCENDED TO 10,000 FT AND O2 MASKS DEPLOYED. C/W SINGLE PACK CONFIDENCE CK. OPS CK GOOD PER MM. RESTOWED O2 MASKS PER MM.

Part: COVER — LOOSE (CABIN)

EEPLS COVER LOOSE AT FWD END. SECURED TRACK COVER PER MM.

Part: INDICATOR — DISLODGED (ESCAPE SLIDE)

FWD SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — DAMAGED (ROW 1ABC)

EMERGENCY ESCAPE FLOOR TRACK LIGHTING KICKED OUT OF PLACE AND DAMAGED AT ROW 1 ABC. REMOVED AND REPLACED TRACK ASSY PER MM.

Part: SKIN — DAMAGED (BS 348)

BELT LOADER CONTACTED FUSELAGE APPROXIMATELY BS 348L WL 265 SHEETMETAL REPAIR ACCOMPLISHED PER SWA RA 1-753-1964 AND SRM UNDER ATTACHED SAM FORM 326.

Part: COFFEEMAKER — DIRTY (GALLEY)

F/A REPORTED SMELLING SMOKE FROM AN ELECTRICAL SOURCE FROM AFT GALLEY. AFTER PULLING BOTH COFFEEMAKERS AND CIRCUIT BREAKERS, SMOKE SMELL DISSIPATED. CLEAN DEBRIS OFF AFT GALLEY COFFEEMAKER RACKS. OPS CK GOOD PER MM.

Part: DISTR PANEL — SHORTED (E/E BAY)

JUST PRIOR TO ENGINE START AN ACRID ELECTRICAL SMELL ENTERED CABIN AT THE TIME THE DUS WENT BLANK AND SEVERAL SYSTEMS FELL OFF LINE. FOUND P-91 WIRES TO BE BURNT. REMOVED AND REPLACED POWER DISTRIBUTION PANEL 91 PER M/M 24-21-21-4 OPERATIONAL CHECK OF SYSTEM OK.