N706SW

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

FLOOR SUPPORT CRACKED AT BS. 540, BETWEEN RBL 24 TO BL 0. / R&R PANEL BREAK IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT DOOR SURROUND FORWARD SHIELD CORRODED BETWEEN BS 767 TO BS 794, RBL 21, ON UPPER AND LOWER SURFACE. R&R SHIELD IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT DOOR SURROUND LOWER SILL VERTICAL WEB CORRODED AT BS 767+6, RBL 20, UPPER FLANGE LOWER SURFACE. R&R WEB IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT FLOOR RAIL CORRODED AT BS. 727D+5, RBL 8, ON UPPER SURFACE AT PREVIOUS REPAIR. / R&R AFT CARGO FLOOR RAIL REPAIR FILLER IAW EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT STRINGER CLIP CORRODED AT BS 847, STR 27L. R&R STRINGER CLIP IAW DWG & SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT STRINGER CLIP CORRODED AT BS 807, STR 27R. R&R STRINGER CLIP IAW DWG & SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

FORWARD CARGO BAY ZEE ANGLE CORRODED BETWEEN BS. 500A TO BS. 500D, RBL 23. / R&R ZEE ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT RIGHT SIDE PLATE CORRODED ON UPPER SURFACE BETWEEN BS 727A+5 TO BS 767 RBL 21. R&R ZEE ANGLE IAW SRM.

Part: FRAME — CORRODED (BS 727B) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT FRAME CORRODED EMITTING UNDER SIDE PLATE AT BS. 727B, BETWEEN LBL 14.5 TO LBL 21. / REPAIRED FRAME IAW EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT FLOOR RAIL CORRODED AT BS. 727D+5, LBL 8, ON UPPER SURFACE AT PREVIOUS REPAIR. / R&R AFT CARGO FLOOR RAIL REPAIR IAW EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT FLOOR TRACK CORRODED ON UPPER SURFACE AROUND FASTENER HOLES BETWEEN BS 927+7 TO BS 927+19, LBL 3. R&R TRACK IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT FLOOR RAIL UPPER SURFACE CORRODED AT BS 727D+5, LBL 12.5. REPAIRED RAIL IAW SRM AND AMM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT LT SIDE PLATE UPPER SURFACE CORRODED BETWEEN BS 727+11 TO BS 787+17, LBL 21. REPAIRED Z-ANGLE IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT STRINGER CLIP CORRODED AT BS 727C, STR 26L. R&R STRINGER CLIP IAW DWG AND SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT STRINGER CLIP CORRODED AT BS. 867, STR. 27L, ON OUTBOARD FLANGE. / R&R STRINGER CLIP IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT FLOOR INTERCOSTAL WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 6.5. R&R INTERCOSTAL IAW DWG AND SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT FLOOR INTERCOSTAL WEB CORRODED AT BS 847+1, RBL 6 ON OUTBOARD SURFACE. R&R WEB IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT OUTBOARD STRINGER CLIP CORRODED AT BS. 747, STR. 27R. / R&R STRINGER CLIP IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT FLOOR RAIL CORRODED AT BS. 727D+5, RBL 3, ON UPPER SURFACE AT PREVIOUS REPAIR. / REPAIRED FLOOR RAIL IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

PASSENGER COMPARTMENT SEAT TRACK CORRODED BETWEEN BS. 480 TO BS. 480+6.50, RBL 24. / R&R SEAT TRACK IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 75,855 hrs · 45,009 cycles

AFT CARGO PIT OUTBOARD STRINGER CLIP CORRODED AT BS. 727E, STR. 27R. / R&R STRINGER CLIP IAW SRM & DWG.

Part: PLATE — CRACKED (RT WING) · airframe 75,855 hrs · 45,009 cycles

RT WING AFT TRAILING EDGE CAVITY ORSS 261 WIGGLE PLATE CRACKED AND BROKEN. R&R WIGGLE PLATE IAW SRM.

Part: HOOK — LOOSE (L2 DOOR GIRT BAR) · airframe 75,618 hrs · 44,862 cycles

L2 DOOR SLIDE GIRT BAR BRACKET VERY LOOSE. IF FACING DOOR FLIGHT ATTENDANT SAID ITS THE BRACKET ON THE R/H. / ADJUSTED HOOK PER AMM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 75,272 hrs · 44,640 cycles

L/H OVERWING EXIT LIGHT COVER NEEDED TO BE RE-SECURED. / SECURED COVER PER SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 73,873 hrs · 43,755 cycles

RT FORWARD EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 73,873 hrs · 43,755 cycles

LT AFT EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK PER MM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 71,787 hrs · 42,471 cycles

FUSELAGE LT WHEEL WELL UPPER PRESSURE DECK WEB CRACKED AT BS 663, LBL 32. REPAIRED DECK PER EA.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 69,280 hrs · 40,892 cycles

LT OVERWING INTERIOR EMERGENCY EXIT DOOR FORWARD LOWER EMERGENCY SIGN INOP AT BS 603, LBL 67. R&R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 69,280 hrs · 40,892 cycles

RT OVERWING INTERIOR EMERGENCY EXIT DOOR FORWARD LOWER EMERGENCY SIGN INOP AT BS 603, RBL 67. R&R POWER SUPPLY IAW AMM.

Part: PANEL — CRACKED (LE SLAT) · airframe 69,280 hrs · 40,892 cycles

RT WING NR 5 SLAT PANEL 622AB CRACKED AFT INBOARD CORNER AT FASTENER. REPAIRED NR 5 SLAT PANEL PER ER & EA.

Part: STRINGER CLIP — CORRODED (BS 947) · airframe 69,280 hrs · 40,892 cycles

STRINGER CLIP CORRODED AT STA 947.5, STR 20. / R&R CLIP PER SRM.

Part: FLOOR PANEL — CRACKED (BS 211-219) · airframe 69,280 hrs · 40,892 cycles

RT COCKPIT FLOOR STRUCTURE CRACKED BETWEEN BS 211.8 TO 219.8, RBL 64. R & R THE FLOOR PANEL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 747-767) · airframe 69,280 hrs · 40,892 cycles

UPPER FLANGE OF FLOOR SUPPORT CORRODED BETWEEN BS 747 TO 767, RBL 22. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,280 hrs · 40,892 cycles

POTABLE WATER DOOR SKIN CUTOUT CORRODED. REPAIRED SKIN PER ER AND EA.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,280 hrs · 40,892 cycles

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

Part: SKIN — CRACKED (RT WING SLAT) · airframe 69,280 hrs · 40,892 cycles

RIGHT WING NR 5 SLAT PANEL 622DB CRACKED ON OUTBOARD EDGE THROUGH FASTENER HOLE. R & R THE NR 5 SLAT PANEL IAW DWG AND EA.

Part: FITTING — CRACKED (LE SLAT) · airframe 69,280 hrs · 40,892 cycles

RT WING NR 7 SLAT ACTUATOR FITTING CRACKED. R&R NR 7 SLAT ASSEMBLY IAW AMM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,280 hrs · 40,892 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,280 hrs · 40,892 cycles

SKIN CORRODED AT BS 953, BETWEEN STR 26L TO STR 27L. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,280 hrs · 40,892 cycles

SKIN CORRODED AT BS 972, BETWEEN STR 26L TO STR 27L. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 69,280 hrs · 40,892 cycles

LEFT WING NR 1 SLAT LOWER SKIN CRACKED AT SLAT STATION 451. R & R THE NR 1 SLAT IAW AMM.

Part: BULKHEAD — CRACKED (BS 663) · airframe 69,280 hrs · 40,892 cycles

LT LOWER FORWARD BULKHEAD GEAR WELL CRACKED AT BS. 663, LBL 26. REPAIRED THE BULKHEAD IAW SRM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,539 hrs · 39,217 cycles

LEFT OVERWING AFT EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. R & R FUSE IAW MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 65,231 hrs · 38,411 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED THE COVER IAW MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

AFT CARGO FLOOR STRUCTURE, CARGO BEAM CORRODED AT BS 767+5, BETWEEN LBL 50 TO RBL 50. REPAIRED BEAM IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

FORWARD LAVATORY AFT INBD MOUNTING STRUCTURE AROUND & IN FASTENER HOLE ON MACHINED INTERCOSTAL, CORRODED AT BS 294.5+9, LBL 12.5. REPAIRED INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 63,110 hrs · 37,141 cycles

FORWARD CARGO INTERCOSTAL CRACKED BETWEEN BS 500 TO BS 500A, LBL 24. REPAIRED INTERCOSTAL PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

SUPPORT ANGLE AROUND NUTPLATE HOLE CORRODED, AT BS 949, RBL 53. REPAIRED ANGLE IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,110 hrs · 37,141 cycles

LEFT WING OTBD AFT FLAP DELAMINATED ON INBD END TOP SURFACE. R & R AFT FLAP IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

R1 DOOR FLOOR INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, RBL 32. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

RIGHT INTERCOSTAL CRACKED, BETWEEN BS 400 - 420. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

FORWARD FLOOR STRUCTURE INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, LBL 45 AT FASTENER HOLE. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

FORWARD FLOOR STRUCTURE INTERCOSTAL CRACKED, BETWEEN BS 328 - 344, LBL 45 AT FASTENER HOLE. R & R INTERCOSTAL IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

FORWARD FLOOR STRUCTURE, FLOORBEAM CORRODED ON UPPER SURFACE AT BS 328, BETWEEN RBL 23 - 50. REPAIRED BEAM IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

L1 DOOR FRAME CORRODED AT BS 303.9, WL 208.1, LOWER FORWARD DOOR STOP FITTING ASSEMBLY. REPAIRED FRAME PER SRM.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

L1 DOOR FWD GIRT BRACKET ATTACH FITTING CORRODED AROUND GIRT BRACKET FASTENER HOLE. R & R BRACKET IAW SRM.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

R1 DOOR THRESHOLD SUPPORT BRACKET CORRODED. R & R BRACKET IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

R1 DOOR THRESHOLD Z ANGLE CORRODED. R & R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

AFT GALLEY DOOR Z ANGLE CORRODED, BETWEEN BS 937 - 990. R & R Z ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

FLOORBEAM NUTPLATE HOLE IN & AROUND, CORRODED AT BS 987, BETWEEN BL 0 TO RBL 50. R & R FLOORBEAM IAW SRM.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

L1 DOOR AFT GIRT BRACKET ATTACH FITTING CORRODED AROUND GIRT BRACKET FASTENER HOLES. R & R FITTING IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

AFT CARGO COMPARTMENT, FLOOR STRAP BEAM CORRODED AT BS 770, BETWEEN RBL 21 TO LBL 21. REPAIRED BEAM IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

FORWARD GALLEY DOOR CUT OUT, FWD STUB FRAME CRACKED OTBD OF UPPER CAM PLATE. R & R STUB FRAME IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

AFT CARGO COMPARTMENT FLOOR STRAP CORRODED, BETWEEN BS 787 - 847, RBL 13.84. R & R STRAP IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

AFT CARGO THRESHOLD WEB CORRODED. R & R WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,110 hrs · 37,141 cycles

AFT CARGO "J" BRACKET CRACKED AT BS 807, FLOOR SUPPORT COMMON TO THE THRESHOLD. REPAIRED SUPPORT PER SRM.

Part: MODULE — INOPERATIVE (CABIN) · airframe 62,110 hrs · 36,546 cycles

EMERGENCY EXIT LIGHTS SWITCH GUARD ON P5 OVERHEAD PANEL IN COCKPIT INOPERATIVE. R & R MODULE IAW SIP.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 62,082 hrs · 36,530 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: BATTERY — FAILED (CABIN) · airframe 61,712 hrs · 36,297 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 61,712 hrs · 36,297 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 61,712 hrs · 36,297 cycles

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

Part: BRACKET — CRACKED (RT WING) · airframe 61,712 hrs · 36,297 cycles

RIGHT WING L BRACKET CRACKED THAT ATTACHES AT INBD SIDE OF DEFLECTION CONTROL RIB. R & R L BRACKET IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 61,712 hrs · 36,297 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R & R BATTERY IAW AMM.

Part: PLATE — CRACKED (LT WING) · airframe 61,712 hrs · 36,297 cycles

LEFT WING LOWER TE PANEL 651GB FWD SUPPORT BRACKET, WIGGLE PLATE CRACKED. R & R WIGGLE PLATE IAW SRM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 61,153 hrs · 35,998 cycles

LEFT OVERWING EMER EXIT SIGN COVER LOOSE. SECURED COVER IAW SRM.

Part: COVER — MISSING (CABIN) · airframe 61,024 hrs · 35,928 cycles

AFT GALLEY EMER EXIT LIGHT COVER MISSING. INSTALLED COVER IAW AMM.

Part: SIGN — CRACKED (CABIN) · airframe 60,489 hrs · 35,625 cycles

R2 DOOR OVERHEAD EMER EXIT SIGN CRACKED. R & R SIGN IAW MM.

Part: LENS — MISSING (CABIN) · airframe 60,489 hrs · 35,625 cycles

RIGHT OVERHEAD BIN EMER LIGHT LENS COVER MISSING BETWEEN ROW 2 - 11. INSTALLED LENS IAW MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 59,585 hrs · 35,084 cycles

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

Part: HOOK — OUT OF ADJUST (R1 DOOR) · airframe 57,944 hrs · 34,140 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR HOOK OUT OF ADJUSTMENT. ADJUSTED HOOK IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,089 hrs · 33,665 cycles

LEFT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 20. RE LAMPED LIGHT IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 57,062 hrs · 33,647 cycles

RIGHT OVERWING EMERGENCY EXIT BATTERY CHARGER INOPERABLE. R & R CHARGER IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME INNER ATTACH FASTENER FOR A/C DUCT ATTACH BRACKET CRACKED AT BS 747, BETWEEN STRINGER 8R TO STRINGER 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME ANGLE CRACKED AT BS 907, STRINGER 8L. REPAIRED ANGLE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME WEB CRACKED AT BS 400, BETWEEN STRINGER 8R TO STRINGER 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME ANGLE CRACKED AT BS 907, BETWEEN STRINGER 8R TO STRINGER 9R. REPAIRED ANGLE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME CRACKED AT BS 360, BETWEEN STRINGER 8R & STRINGER 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME CRACKED AT BS 867, BETWEEN STRINGER 8R TO STRINGER 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME AT INNER ATTACH FASTENER FOR A/C DUCT ATTACH BRACKET CRACKED AT BS 500A, BETWEEN STRINGER 8R TO STRINGER 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8R & STRINGER 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME CRACKED AT BS 480, BETWEEN STRINGER 8R TO STRINGER 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME WEB CRACKED AT BS 440, BETWEEN STRINGER 8R TO STRINGER 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

FRAME CRACKED AT BS 747 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

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

Part: POST — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

LEFT NR 3 FLIGHT DECK WINDOW FRAME CRACKED INDICATION AT E - F POST SECOND LOWER FASTENER HOLE. REPAIRED POST IAW MM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 57,062 hrs · 33,647 cycles

LEFT HORIZONTAL STABILIZER INBD AT STAB STATION 92.7 FWD VERTICAL STIFFENER CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,062 hrs · 33,647 cycles

SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,062 hrs · 33,647 cycles

RIGHT WING NR 5 SLAT LOWER NOSE SKIN CRACKED AT STATION 85.19. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,062 hrs · 33,647 cycles

LEFT WING NR 3 SLAT SKIN CRACKED AT STATION 202.4. REPAIRED SKIN IAW SRM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 56,877 hrs · 33,541 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW SWA MT.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,546 hrs · 33,352 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, LBL 43. REPAIRED WEB IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,183 hrs · 33,146 cycles

EMERGENCY LIGHT SYS INOPERATIVE. RELAMPED EMERGENCY LIGHT SYS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,584 hrs · 32,799 cycles

LT OVER WING EMERGENCY LIGHT EXTENSION INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 55,191 hrs · 32,552 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,232 hrs · 31,989 cycles

SEAT TRACK CRACKED AT STA 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,232 hrs · 31,989 cycles

SEAT TRACK CRACKED AT STA 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,232 hrs · 31,989 cycles

SEAT TRACK CRACKED AT STA 727B, RBL 24.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,232 hrs · 31,989 cycles

SEAT TRACK OTBD FLANGE AFT HOLE CRACKED AT STA 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,232 hrs · 31,989 cycles

SEAT TRACK CRACKED AT STA 727B, LBL 24.75. REPAIRED SEAT TRACK IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,232 hrs · 31,989 cycles

SEAT TRACK CRACKED AT STA 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,232 hrs · 31,989 cycles

SEAT TRACK CRACKED AT STA 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: BATTERY — DEFECTIVE (FLASHLIGHT) · airframe 53,599 hrs · 31,612 cycles

FORWARD EMERGENCY FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: ENGINE — FAILED (LEFT) · airframe 52,443 hrs · 30,873 cycles

INFLIGHT SHUT DOWN/AIR TURNBACK/DECLARED EMERGENCY. LOUD BANG HEARD IN COCKPIT FOLLOWED BY FAILURE OF THE NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: HOOK — LOOSE (R1 DOOR) · airframe 52,020 hrs · 30,619 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER GIRT BAR FWD HOOK LOOSE. SECURED HOOK PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,106 hrs · 30,047 cycles

ONE FLASHLIGHT IN FWD EMERGENCY EQUIPMENT COMPARTMENT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: LIGHT — WORN (CABIN) · airframe 50,850 hrs · 29,899 cycles

RT EEPLS WORN BETWEEN ROW 7 TO ROW 8. REMOVED AND REPLACED EEPLS IAW DWG AND SOPM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,850 hrs · 29,899 cycles

L1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 50,850 hrs · 29,899 cycles

RT WING O/B AFT FLAP INBD T/E CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,850 hrs · 29,899 cycles

LT WING O/B AFT FLAP INBD T/E CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 48,449 hrs · 28,490 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 46,412 hrs · 27,298 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 46,412 hrs · 27,298 cycles

DURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT LIGHT BATTERY CHARGER INOP. REMOVED AND REPLACED CHARGER PER MM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,412 hrs · 27,298 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHT BATTERY CHARGER INOPERATIVE. REMOVED AND REPLACED CHARGER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 46,412 hrs · 27,298 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 45,744 hrs · 26,918 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND EMERGENCY EXIT BATTERY CHARGER FUSES INOP. REMOVED AND REPLACED FUSE PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE PER WDM.

Part: STRUCTURE — CRACKED (HORIZ STAB) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT HORIZONTAL L/E T-CHORD UPPER AFT FASTENER HOLE CRACKED. REPAIRED STABILIZER PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 43. REPAIRED BEAM PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 947, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CRACKED AT BS 303, STR 4L. R&R STRINGER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 15. REMOVED AND REPLACED BEAM PER SRM.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM SUPPORT CHANNEL CORRODED BETWEEN BS 259.5 TO BS 268.25, BETWEEN LBL 3 TO RBL 3. REMOVED AND REPLACED SUPPORT CHANNEL PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO BAY SUPPORT STRUCTURE CORRODED BETWEEN BS 505 TO BS 511, BL 0. REMOVED AND REPLACED SUPPORT PER BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 15. REMOVED AND REPLACED BEAM PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING SUPPORT STRUCTURE CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 827, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 43,893 hrs · 25,832 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO BAY FRAME WEB DAMAGED AT BS 440, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED WEB PER BAC DWG.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 43,137 hrs · 25,376 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — LOOSE (CABIN) · airframe 42,677 hrs · 25,091 cycles

RIGHT EMERGENCY LIGHT LOOSE AT ROW 8. REMOVED AND REPLACED EMERGENCY LGIHT PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 42,512 hrs · 24,998 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 42,136 hrs · 24,761 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,802 hrs · 23,324 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,616 hrs · 22,634 cycles

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

Part: TRUNNION — CORRODED (NLG) · airframe 37,557 hrs · 21,969 cycles

DURING SCHEDULED 10Y CHECK, FOUND NLG TRUNNION CORRODED. REPAIRED TRUNNION PER EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 37,548 hrs · 21,964 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 35,911 hrs · 20,996 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 35,402 hrs · 20,692 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 35,152 hrs · 20,541 cycles

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

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 35,152 hrs · 20,541 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 34,571 hrs · 20,196 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: ENGINE — MAKING METAL (NR 2) · airframe 34,202 hrs · 19,988 cycles

INFLIGHT SHTDOWN / DIVERSION / DECLARED EMERGENCY. VIBRATION NR 2 ENGINE FOLLOWED BY LOSS OF OIL QUANTITY AND PRESSURE. INSPECTED CHIP DETECTORS, FOUND FOD IN MIDDLE DETECTOR. REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,712 hrs · 19,157 cycles

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

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 32,641 hrs · 19,111 cycles

DURING SCHEDULED HC1 CHECK, RIGHT CENTER EMERGENCY EXIT LIGHT BATTERY PACK FAILED TIME TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WIRE HARNESS — FAULTY (WINDOW HEAT) · airframe 31,700 hrs · 18,582 cycles

ELECTRICAL SPARKS, SMOKE EMINATING FROM R2 COCKPIT WINDOW. REMOVED AND REPLACED R2 COCKPIT WINDOW HEAT HARNESS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 30,392 hrs · 17,838 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 30,053 hrs · 17,657 cycles

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

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 30,053 hrs · 17,657 cycles

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

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 30,053 hrs · 17,657 cycles

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

Part: GUIDE ARM — BENT (FWD ENTRY DOOR) · airframe 30,041 hrs · 17,650 cycles

DURING SCHEDULED MV1 CHECK, FWD ENTRY DOOR WOULD NOT OPEN. REMOVED AND REPLACED GUIDE ARM PIN PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,949 hrs · 17,584 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328 RBL 33. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 29,949 hrs · 17,584 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 14. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 29,949 hrs · 17,584 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: HOOK — LOOSE (L1 DOOR) · airframe 29,901 hrs · 17,548 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 29,892 hrs · 17,541 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED EVAC SLIDE GIRT BAR PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 26,905 hrs · 15,881 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 25,361 hrs · 15,001 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY EXIT) · airframe 23,464 hrs · 13,884 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHTS AT ROWS 9 ADC AND 11 ABC, INOP. RELAMPED LIGHTS PER MM.

Part: GLOWSTRIP — OUT OF POSITION (CABIN) · airframe 22,543 hrs · 13,378 cycles

DURING SPV, FOUND PHOTOLUMINSCENT STRIP OUT OF POSITION. PLACED PHOTOLUMINESCENT STRIP IN PROPER POSITION PER ACO.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,543 hrs · 13,378 cycles

DURING SPV, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,333 hrs · 12,739 cycles

DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD CABIN. REMOVED AND REPLACED BATTERY PACK AT M1673 BALLAST PER MM.

Part: BOOT — LEAKING (BLEED AIR DUCT) · airframe 19,482 hrs · 11,731 cycles

AIR TURNBACK, AIRCRAFT WOULD NOT PRESSURIZE. REMOVED AND REPLACED PNEU BLEED AIR DUCT BOOT AT KEELBEAM AND THREE BODY DRAINS, TIGHTENED CLAMPS AND REMOVED AND REPLACED WATER SEPARATOR SEALS PER MM.

Part: WINDOW — MISSING (FWD ENTRY DOOR) · airframe 16,443 hrs · 10,039 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND VIEWING WINDOW MISSING. INSTALLED WINDOW PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,825 hrs · 9,706 cycles

DURING SCHEDULED PM SERVICE CHECK, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,846 hrs · 8,582 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT ROW NR 7. RELAMPED EEPLS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 13,344 hrs · 8,293 cycles

EEPLS COVER LOOSE AT ROW NR 1. REINSTALLED COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 12,703 hrs · 7,927 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS BROKEN ( 4 EA ) IN CABIN. R&R COVERS PER MM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 12,535 hrs · 7,835 cycles

DURING SCHEDULED A2 CHECK ( SI 11157-53 ), FOUND AFT PRESSURE BULKHEAD AFT SIDE OIL CANNED AT STR'S 3L, 5L, 7L & 9L. REPAIRED PRESS BULKHEAD PER SRM & SWA RA 1-753-2690.

Part: BEARING — LOOSE (TAIL) · airframe 11,356 hrs · 7,161 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11055-55, FOUND LH & RH ELEVATORS # 4 ELEVATOR HINGE BEARINGS LOOSE. R&R BOTH ELEVATOR HINGE ASSY'S PER SWA RA.

Part: BEARING — WORN (ELEVATOR TAB) · airframe 10,772 hrs · 6,831 cycles

DURING SCHEDULED PM CHECK ( SI-11079-27 ), FOUND RT ELEVATOR TAB, OTBD AFT ROD END BEARING WORN. R&R ROD END BEARING PER MM.

Part: COVER — MISSING (CABIN) · airframe 10,600 hrs · 6,735 cycles

EEPLS TRACK COVER MISSING AT ROW 9. INSTALLED TRACK COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 10,044 hrs · 6,378 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 8. INSTALLED TRACK COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 9,891 hrs · 6,284 cycles

EEPLS TRACK COVER MISSING AT ROW 9. REMOVED AND REPLACED TRACK COVER PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 9,341 hrs · 5,954 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS INTERMITTENT BETWEEN ROWS 12 - 16. RESECURED EEPLS WIRING PER MM.

Part: FITTING — CRACKED (LT ELEVATOR) · airframe 8,313 hrs · 5,371 cycles

DURING SCHEDULED C1 CHECK, FOUND LT ELEVATOR TAB MAST ATTACH FITTING CRACKED. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: COVER — CRACKED (CABIN) · airframe 7,306 hrs · 4,787 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 19. REMOVED AND REPLACED TRACK COVER PER MM.

Part: LIGHT — LOOSE (ROW 18)

EEPLS LIGHT LOOSE AT ROW 18. SECURED LIGHT ASSY TO TRACK PER MM.

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

DURING SCHEDULED A2 CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (SERVICE DOOR)

DURING SCHEDULED C3 CHECK, FOUND FORWARD SERVICE DOOR HAS 1.25 INCH CRACK AT LOWER AFT CORNER. CRACK IS .75 INCH FROM O/B SIDE AND .5 INCH FROM BOTTOM. REPAIRED PER SWA RA 1-753-2024.