N726SW

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,941 hrs · 42,590 cycles

LEFT AFT ENTRY DOOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,410 hrs · 41,575 cycles

AFT PRESSURE BULKHEAD CRACKED AT BS. 1016, RBL 1. REPAIRED WEB PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,108 hrs · 40,707 cycles

L1 DOOR EMERGENCY EXIT LIGHT ABOVE DOOR BULB INOP. R&R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,108 hrs · 40,707 cycles

RT OVERWING EMERGENCY EXIT AFT LIGHT BULB INOP. R&R BULB IAW AMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

BAFFLE CRACKED AT BS 500C, RBL 25. R&R CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

FRAME CORRODED AT BS 663, BETWEEN STR 4L TO STR 5L. REPAIRED FRAME IAW SRM AND EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

INTERCOSTAL CORRODED BETWEEN BS 867 TO BS 847, STR 26L. R&R INTERCOSTAL IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

SHEAR TIE CORRODED AT BS 867, BETWEEN STR 23L TO STR 25L. R&R SHEAR TIE IAW SRM & EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

R1 DOOR STUB FRAME CUTOUT CRACKED AT BS 295, STR 8R. R&R STUB FRAME IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

AFT CARGO INTERCOSTAL CORRODED BETWEEN BS 847 TO BS 867, STR 25L. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STRAP — CORRODED (RT HORIZ STAB) · airframe 69,108 hrs · 40,707 cycles

HORIZONTAL STABILIZER COMPARTMENT STRAP CORRODED AT BS 1088, BETWEEN RBL 23 TO RBL 29. R&R STRAP IAW SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

AFT PIT CUTOUT CORRODED BETWEEN BS 847 TO BS 867, BETWEEN STR 26L TO STR 23L. REPAIRED CUTOUT IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

RT CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A. R&R CREASE BEAM WEB IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

E&E BAY STRINGER CORRODED AT BS 365, STR 26L. R&R STRINGER SPLICE IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 69,108 hrs · 40,707 cycles

CENTER WING BOX HORSESHOE BRACKET INBOARD UPPER ATTACH ANGLE CRACKED AT BS 663, RBL 17. R&R DOUBLER ASSEMBLY IAW DWG AND SRM.

Part: STRUCTURE — CRACKED (RT MLG WW) · airframe 69,108 hrs · 40,707 cycles

CENTER WING BOX UPPER CHORD CRACKED AT BS 663, RBL 10. REPAIRED CHORD PER EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

FORWARD CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS 500C, STR 19L. R&R CLIP IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,108 hrs · 40,707 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED. R&R RIB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

AFT CARGO AT FLOOR BOARD SPLICE STRAP SUPPORT STRUCTURE CORRODED AT BS 767+5, RBL 3. REPAIRED SUPPORT IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

AFT CARGO AT FLOOR BOARD SPLICE STRAP SUPPORT STRUCTURE CORRODED AT BS 767+5, LBL 3. REPAIRED STRUCTURE IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,108 hrs · 40,707 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED 35" FROM ROOT. R&R RIB IAW DWG & SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

FORWARD CARGO COMPARTMENT BAFFLE CLIP CRACKED AT BS 500A, LBL 24. R&R BAFFLE CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

AFT CARGO AT FLOOR BOARD SPLICE STRAP SUPPORT STRUCTURE CORRODED AT BS 767+5, RBL 8. REPAIRED SUPPORT IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

AFT CARGO Z ANGLE CORRODED BETWEEN BS 827 TO BS 727E+10, LBL 20. R&R Z ANGLE IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

FORWARD CARGO COMPARTMENT BAFFLE FLIP CRACKED AT BS 500B, LBL 24. R&R BAFFLE CLIP IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

AFT CARGO INTERCOSTAL CORRODED BETWEEN BS 727A TO BS 727B, LBL 17. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 69,108 hrs · 40,707 cycles

LT HORIZONTAL STABILIZER RIB STIFFENER CRACKED AT STAB STA 101.90, 2ND VERTICAL NEAR LOWER END. REPAIRED STIFFENER IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

AFT CARGO Z ANGLE CORRODED BETWEEN BS 727E TO BS 727B+6, LBL 20. R&R Z ANGLE IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,108 hrs · 40,707 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED 26" FROM ROOT. R&R RIB IAW DWG & SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,108 hrs · 40,707 cycles

FORWARD CARGO COMPARTMENT BAFFLE CLIP CRACKED AT BS 500C, LBL 24. R&R BAFFLE CLIPS IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,108 hrs · 40,707 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED 45" FROM ROOT. R&R RIB IAW DWG & SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,108 hrs · 40,707 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED 82" INBOARD FROM ROOT. R&R RIB IAW DWG & SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,108 hrs · 40,707 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED BETWEEN BS 663 TO BS 675, LBL 31. REPAIRED WEB IAW EA.

Part: SKIN — CORRODED (TE FLAP) · airframe 69,108 hrs · 40,707 cycles

RT WING OUTBOARD AFT TRAILING EDGE FLAP UPPER SKIN CORRODED AT AFT INBOARD CORNER. REPAIRED AFT FLAP IAW SRM & AMM.

Part: VAPOR BARRIER — DELAMINATED (RT MLG WW) · airframe 69,108 hrs · 40,707 cycles

RT MAIN WHEEL WELL VAPOR BARRIER DELAMINATED AT STA 663. REPAIRED WEB IAW SRM.

Part: RETAINING CLIP — OUT OF ADJUST (L1 DOOR) · airframe 68,127 hrs · 40,084 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK OUT OF ADJUST. ADJUSTED CLIPS IAW AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 67,826 hrs · 39,896 cycles

MID CABIN EMERGENCY EXIT SIGN COVER MISSING. SECURED COVER PER AMM.

Part: BRACKET — CRACKED (RT WING) · airframe 66,927 hrs · 39,343 cycles

RIGHT WING FIXED UPPER TRAILING EDGE PANEL CENTER SUPPORT ATTACH BRACKET CRACKED. R & R THE BRACKET IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 66,927 hrs · 39,343 cycles

RIGHT WING UPPER WING PANEL 651AT LOWER INBOARD SUPPORT ATTACH BEAM FORWARD L BRACKET CRACKED. R & R THE BRACKET IAW SRM.

Part: BRACKET — CRACKED (RT WING TE) · airframe 66,927 hrs · 39,343 cycles

RIGHT WING FIXED UPPER TRAILING EDGE PANEL PIVOT ARM INBOARD FORWARD ATTACH BRACKET TO SUPPORT CRACKED. THE R & R THE BRACKET IAW SRM.

Part: STRAP — CRACKED (LT WING) · airframe 66,927 hrs · 39,343 cycles

LEFT WING INBOARD EDGE STRAKE SPLICE STRAP CRACKED. R & R THE STRAP IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 66,281 hrs · 38,931 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 66,130 hrs · 38,838 cycles

LT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER EA.

Part: HOOK — LOOSE (R1 DOOR) · airframe 66,010 hrs · 38,760 cycles

R1 DOOR EMERGENCY EVAC SLIDE FORWARD GIRT BAR FITTING LOOSE. SECURED HOOK IAW SIP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,745 hrs · 38,588 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 64,958 hrs · 38,108 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 64,958 hrs · 38,108 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 62,828 hrs · 36,852 cycles

CABIN EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATIONS MO1674. R & R BATTERY IAW AMM AND DWG.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,828 hrs · 36,852 cycles

CABIN EMERGENCY LIGHT BATTERY, FAILED CAPACITY CHECK AT LOCATIONS MO1672. R & R THE BATTERY IAW AMM AND DWG.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,828 hrs · 36,852 cycles

CABIN EMERGENCY LIGHT CHARGER BASES INOPERATIVE AT LOCATION MO1675. R & R THE CHARGER IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 62,828 hrs · 36,852 cycles

CABIN EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATIONS MO1673. R & R THE BATTERY IAW AMM AND DWG.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 62,828 hrs · 36,852 cycles

CABIN EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATIONS MO1675. R & R BATTERY IAW AMM AND DWG.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,828 hrs · 36,852 cycles

CABIN EMERGENCY LIGHT CHARGER BASES INOPERATIVE AT LOCATION MO1673. R & R THE CHARGER IAW AMM.

Part: FLASHLIGHT — INOPERATIVE (FWD GALLEY) · airframe 62,765 hrs · 36,809 cycles

FORWARD GALLEY LOWER FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

INTERCOSTAL WEB CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R WEB PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

INTERCOSTAL CRACKED AT BS 947, RBL 23. R&R INTERCOSTAL IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

RT CREASE BEAM WEB CORRODED BETWEEN BS 727C TO BS 727D. R&R WEB PER DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

STUB FRAME CRACKED AT BS 294.5, RBL 54, WL 208.5. REPAIRED STUB FRAME PER ER AND EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

RT CREASE BEAM WEB CORRODED BETWEEN BS 727A TO BS 727B. REPAIRED WEB PER DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

RT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420. REPAIRED WEB PER ER AND EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

L2 DOOR LOWER SILL WEB CORRODED BETWEEN BS 951 TO BS 993, WL 208. R&R WEB IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

R2 DOOR LOWER SILL WEB CORRODED BETWEEN BS 951 TO BS 993, WL 208. R&R WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 23. R&R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

AFT CARGO BAY, FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 807, LBL 23. R&R SUPPORT IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

AFT CARGO BAY SHIELD CORRODED BETWEEN BS 767 TO BS 787, RBL 23. R&R SHIELD IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

INTERCOSTAL CORRODED ON UPPER FLANGE BETWEEN BS 294 TO BS 312, LBL 12. R&R INTERCOSTAL IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

L1 DOOR THRESHOLD INBOARD SUPPORT ANGLE CORRODED. R&R ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

AFT CARGO BAY LOWER BULKHEAD ANGLE CORRODED AT BS 947, BETWEEN STR 25R TO STR 25L. R&R ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

FLOORBEAM CORRODED AT BS 312, RBL 21. REPAIRED FLOORBEAM PER ER AND EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

AFT CARGO BAY LAV BULKHEAD STANCHION LOWER CLIP CRACKED AT BS 867, LBL 12. R&R CLIP PER SOPM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

FLOORBEAM CORRODED AT BS 987, RBL 20. REPAIRED FLOORBEAM PER ER AND EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

INTERCOSTAL WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 6. R&R INTERCOSTAL PER SRM & DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

AFT CARGO BAY FLOOR SPLICE CORRODED AT BS 887, RBL 10. R&R SPLICE PER SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

R2 DOOR MOPSILL WEB CORRODED BETWEEN BS 986 TO BS 1016. R&R WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 62,757 hrs · 36,804 cycles

LT MAIN WHEEL WELL VERTICAL SPAR PRESSURE WEB CRACKED AT BS 663, LBL 28. REPAIRED WEB IAW EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 62,757 hrs · 36,804 cycles

AFT CARGO BAY, CARGO TIE DOWN TRACK CORRODED BETWEEN BS 727B TO BS 867, RBL 13. R&R TRACK IAW SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

L2 DOOR MOPSILL WEB CORRODED AT BS 1016. R&R WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

FLOORBEAM CORRODED AT BS 328, RBL 41. REPAIRED FLOORBEAM PER SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

AFT CARGO BAY, SHIELD AFT OF CARGO DOOR CORRODED BETWEEN BS 847 TO BS 867, RBL 23. R&R SHIELD IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

FORWARD CARGO BAY SHIELD CORRODED BETWEEN BS 492 TO BS 500A, RBL 23. R&R SHIELD IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

AFT CARGO BAY, SUB THRESHOLD CORRODED BETWEEN BS 827 TO BS 847, RBL 23. R&R SUB THRESHOLD PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 62,757 hrs · 36,804 cycles

RT HORIZONTAL BEAD PRESSURE WEB CRACKED AT BS 664, RBL 43. REPAIRED WEB PER ER AND EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 62,757 hrs · 36,804 cycles

LT WING UPPER TRAILING EDGE PANEL BETWEEN NR 5 AND 6 SPOILER LOWER SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT. R&R ANGLE IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,757 hrs · 36,804 cycles

RT WING NR 5 SLAT BULLNOSE SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 62,757 hrs · 36,804 cycles

LT WING NR 2 SLAT BULLNOSE SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED SKIN IAW ER AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,757 hrs · 36,804 cycles

LT WING OVERWING EXIT EMERGENCY LIGHT INOP. R&R LIGHT PER AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 62,424 hrs · 36,600 cycles

L1 DOOR SLIDE PACK LOOSE IN CASE. R & R SLIDE ASSEMBLY IAW MAINTENANCE.

Part: VALVE — STUCK (RT A/C PACK) · airframe 62,150 hrs · 36,426 cycles

AIRCRAFT CANNOT MAINTAIN PRESSURIZATION. AIR TURNBACK. FOUND FLIGHT PACK VALVE TO BE INTERMENITTENT. R & R RIGHT PACK VALVE PER MM.

Part: SPOILER — OUT OF ADJUST (LT WING) · airframe 59,887 hrs · 35,075 cycles

LEFT WING NR 5 FLIGHT SPOILER OUT OF ADJUSTMENT. ADJUSTED SPOILER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,759 hrs · 35,009 cycles

RIGHT OVERWING EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,244 hrs · 34,704 cycles

FORWARD ENTRY EGRESS LIGHT INOPERATIVE. RELAMPED LIGHT IAW SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,121 hrs · 34,626 cycles

EMERGENCY BATTERY PACKS FAILED CAPACITY TEST AT M1675. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,121 hrs · 34,626 cycles

EMERGENCY BATTERY PACKS FAILED CAPACITY TEST AT M1673. R & R BATTERY PACK IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

FUSELAGE FRAME CRACKED AT STATION 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL 24.75. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, LBL45.5. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, RBL 45.5. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 727B, RBL 24.75. REPAIRED BEAM IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

RIGHT NR 1 WINDOW FRAME CRACKED. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

LEFT NR 3 FLIGHT DECK WINDOW FRAME SECOND LOWER FASTENER HOLE CRACKED. REPAIRED FRAME IAW ACO.

Part: SKIN — CRACKED (LE SLAT) · airframe 57,001 hrs · 33,452 cycles

LEFT WING NR 1 SLAT ACTUATOR ATTACH POINT LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,001 hrs · 33,452 cycles

RIGHT LOWER BULKHEAD CHORD SKIN CRACKED AT BS 540. REPAIRED SKIN IAW EA.

Part: BATTERY — FAILED (CABIN) · airframe 56,766 hrs · 33,313 cycles

AFT GALLEY EMER LIGHT FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 56,766 hrs · 33,313 cycles

FORWARD GALLEY EMER LIGHT FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 56,766 hrs · 33,313 cycles

LEFT AFT EMER LIGHT FAILED CAPACITY CHECK AT ROW 1. R & R BATTERY IAW AMM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 56,020 hrs · 32,897 cycles

LEFT WW FWD BULKHEAD WEB CRACKED AT BS 663, BETWEEN LBL 41 TO 43. REPAIRED WEB IAW EA.

Part: TIRE — FAILED (LT MLG) · airframe 56,037 hrs · 32,909 cycles

AIR TURN BACK, DECLARED EMER NR 1 TIRES FAILED ON TAKEOFF. R & R NR 1 MAIN WHEEL ASSEMBLY IAW MM.

Part: TIRE — FAILED (LT MLG) · airframe 56,037 hrs · 32,909 cycles

AIR TURN BACK, DECLARED EMER NR 2 TIRES FAILED ON TAKEOFF. R & R NR 2 MAIN WHEEL ASSEMBLY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 54,440 hrs · 31,983 cycles

FWD ENTRY EMERGENCY LIGHT FAILED CAPACITY CHECK. R & R LIGHT BATTERY IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,440 hrs · 31,983 cycles

ROW 5 EMERGENCY LIGHT FAILED CAPACITY CHECK. R & R LIGHT BATTERY PACKS IAW MM.

Part: SKIN — CRACKED (LT SPOILER) · airframe 54,440 hrs · 31,983 cycles

LT WING NR 2 FLIGHT SPOILER UPPER SURFACE CRACKED AT HINGE CUTOUT. REPAIRED SPOILER IAW SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,951 hrs · 31,718 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,257 hrs · 30,697 cycles

RT EMERGENCY EXIT LIGHTING BATTERIES FAILED CAPACITY CHECK. R&R EMERGENCY BATTERY PACKS IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,257 hrs · 30,697 cycles

LT EMERGENCY EXIT LIGHTING BATTERIES FAILED CAPACITY CHECK. R&R EMERGENCY BATTERY PACKS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 51,674 hrs · 30,384 cycles

AFT SERVICE DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED LENS IAW SIP.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 51,048 hrs · 30,006 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. REMOVED AND REPLACED SLIDE IAW MT.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 49,919 hrs · 29,313 cycles

LEFT HORZ STAB FWD ATTACH LUG LOWER SLIDING SEAL IS CRACKED. REMOVED AND REPLACED LEFT HORZ STAB FWD ATTACH LUG LOWER SLIDING SEAL PER AMM

Part: RIB — BROKEN (TE FLAP) · airframe 49,919 hrs · 29,313 cycles

RIGHT WING OUTBOARD T/E FLAP INBOARD DEFLECTION CONTROL ROLLER RIB UPPER ATTACH LUG FOR T/E PANEL BROKEN. REMOVED AND REPLACED RIGHT WING OUTBOARD T/E DEFLECTION CONTROL ROLLER RIB PER MM SEE SUBTASK SIGNOFFS AND PER TECHICAL SERVICE REQUEST #201205241.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 49,919 hrs · 29,313 cycles

RIGHT HORZ STAB FWD ATTACH LUG LOWER SLIDING SEAL IS CRACKED. REMOVED AND REPLACED RIGHT HORZ STAB FWD ATTACH LUG LOWER SLIDING SEAL PER AMM.

Part: RETAINER — CRACKED (RT WING) · airframe 49,919 hrs · 29,313 cycles

RIGHT WING T/E UPPER SHELF PANEL FWD BULB SEAL RETAINER CRACKED OUTBOARD OF NR 6 FLAP TRACK. REMOVED AND REPLACED RIGHT WING T/E UPPER SHELF PANEL FWD BULB SEAL RETAINER PER MM AND SRM 51-40-02.

Part: RETAINER — CRACKED (RT WING) · airframe 49,919 hrs · 29,313 cycles

RIGHT WING T/E SHELF PANEL AFT BULB SEAL RETAINER CRACKED OUTBOARD OF NR 6 FLAP TRACK. REMOVED AND REPLACED RIGHT WING T/E SHELF PANEL AFT BULB SEAL RETAINER PER MM AND SRM 51-40-02.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,917 hrs · 29,312 cycles

BS 663, RBL 40, WL 197, CRACK IN PRESSURE BULKHEAD. REPAIRED BS 663 RBL 40 WL 197 PRESSURE BULKHEAD PER ER 12-03539 AND EA 1-757-7691.

Part: FRAME — BUCKLED (FUSELAGE) · airframe 49,917 hrs · 29,312 cycles

BS 188 LOWER FRAME WEB BUCKLED AT RBL 11, AT INBD CHORD. REMOVED AND REPLACED BS 188 LOWER FRAME WEB PER SRM 51-10-02 AND SRM 51-40-02.

Part: COVER — OUT OF POSITION (EXIT SIGN) · airframe 49,398 hrs · 28,997 cycles

FORWARD ENTRY LOWER EMERGENCY EXIT SIGN COVER FELL OFF. REMOVED AND REPLACED SIGN PER AMM.

Part: BRACKET — OUT OF ADJUST (L1 DOOR) · airframe 48,071 hrs · 28,200 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 47,135 hrs · 27,641 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: FUSE — BLOWN (CABIN) · airframe 47,021 hrs · 27,555 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FUSE PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 45,499 hrs · 26,683 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,839 hrs · 25,723 cycles

DURING SCHEDULED 12Y CHECK, FOUND ANGLE CORRODED AT BS 500B, STR 26R. REMOVED AND REPLACED ANGLE PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 43,839 hrs · 25,723 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR GIRT BAR FITTING UPPER SURFACE CORRODED AT BS 344, LBL 60. REMOVED AND REPLACED FITTING PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,839 hrs · 25,723 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 951 TO BS 992. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: FITTING — CORRODED (GIRT BAR) · airframe 43,839 hrs · 25,723 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR GIRT BAR FITTING UPPER SURFACE CORRODED BETWEEN BS 360 TO BS 350, LBL 60. REMOVED AND REPLACED FITTING PER SRM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,839 hrs · 25,723 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR CREASE BEAM CHORD CORRODED BETWEEN BS 328 TO BS 344, LBL 60. REMOVED AND REPLACED BEAM PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,839 hrs · 25,723 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING NR 4 SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED NR 4 SLAT PER EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,839 hrs · 25,723 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT RT Z-ANGLE CORRODED AT BS 767. REMOVED AND REPLACED Z-ANGLE PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,839 hrs · 25,723 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, RBL 19. REPAIRED BEAM PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 43,839 hrs · 25,723 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLIGHT DECK CEILING UPPER CENTER I-BEAM CRACKED AT BS 204, LBL 0.05. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 43,839 hrs · 25,723 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,134 hrs · 25,297 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 13. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,078 hrs · 24,069 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,078 hrs · 24,069 cycles

DURING SCHEDULED SPV, FOUND LT OVERWING EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,078 hrs · 24,069 cycles

DURING SCHEDULED SPV, FOUND RT OVERWING EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,078 hrs · 24,069 cycles

DURING SCHEDULED SPV, FOUND R2 DOOR EXIT LIGHT INOP. RELAMPED PER MM.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 40,044 hrs · 23,448 cycles

DIVERSION - COMPRESSOR STALL NR 1 ENGINE. NR 1 ROLLED BACK ON ITS ON AT FL 360. FUEL FLOW DROPPED OFF AND N1 DECREASED TO ABOUT 40 PERCENT WITH A 40 PERCENT SPLIT BETWEEN ENG NR 2. WENT BOTH & FLT ON IGNITES AND TURNED OFF ENG NR 1. AFTER CHECKLISTS, ENG NR 1 OPERATED NORMALLY. ENGINE NR 1 VIB READ 2 REST OF FLIGHT. PERFORMED BORESCOPE INSPECTION AND REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,398 hrs · 23,017 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT SIGN INOP. RELAMPED LIGHT ASSY PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 37,157 hrs · 21,667 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING NR 8 L/E SLAT CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,157 hrs · 21,667 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 270, BL 0. REPAIRED BEAM PER SRM.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 36,128 hrs · 21,060 cycles

AIR TURNBACK / DECLARED EMERGENCY. COMPRESSOR STALL IN THE NR 2 ENGINE AT 1,100 FT. WHILE REDUCING POWER TO CLIMB THRUST. REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,407 hrs · 20,612 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION SUPPORT UPPER & LOWER LUGS CORRODED. REPAIRED PER SWA EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,407 hrs · 20,612 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 34,615 hrs · 20,140 cycles

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

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 34,452 hrs · 20,047 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,384 hrs · 20,003 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — DEBONDED (T/E FLAP) · airframe 34,244 hrs · 19,913 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING INBOARD T/E AFT FLAP LOWER SURFACE DISBONDED. REMOVED AND REPLACED FLAP PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,673 hrs · 18,368 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,415 hrs · 18,212 cycles

DURING SCHEDULED MV3 CHECK, FOUND AFT LEFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FITTING — DAMAGED (R1 DOOR) · airframe 30,955 hrs · 17,961 cycles

R1 DOOR STUCK CLOSED. FOUND LOWER AFT CAM FITTING DAMAGED. REMOVED AND REPLACED CAM ROLLER FITTING PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,709 hrs · 17,812 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 30,008 hrs · 17,391 cycles

DURING SCHEDULED 8Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, STR 24L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 30,008 hrs · 17,391 cycles

DURING SCHEDULED 8Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, STR 24L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,008 hrs · 17,391 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 5 TO RBL 49. REPAIRED FLOORBEAM PER SWA EA.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 26,960 hrs · 15,625 cycles

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

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 26,960 hrs · 15,625 cycles

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

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 26,274 hrs · 15,229 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY EXIT) · airframe 24,389 hrs · 14,178 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 22,056 hrs · 12,863 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,322 hrs · 12,411 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 9 ABC AND 11 ABC, INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: BRACKET — CRACKED (VERTICAL STAB) · airframe 19,572 hrs · 11,465 cycles

DURING SCHEDULED HC1 CHECK, FOUND VERTICAL STAB SPRING BRACKET AT BS 1016, RBL 11, CRACKED. REPAIRED VERTICAL STAB SPRING BRACKET PER EA.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 18,433 hrs · 10,825 cycles

DURING SCHEDULED C1 CHECK, FOUND 2 EACH AFT GALLEY EMERGENCY FLASHLIGHT BATTERIES FAILED. REMOVED AND REPLACED BOTH BATTERIES PER MM.

Part: BALLAST — INOPERATIVE (EMERGNECY LIGHT) · airframe 18,433 hrs · 10,825 cycles

DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT WINDOW LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: CONTROLLER — FAILED (WINDSHIELD) · airframe 17,753 hrs · 10,448 cycles

L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED L2 COCKPIT WINDOW AND HEAT CONTROLLER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,936 hrs · 9,954 cycles

DURING SCHEDULED A CHECK, FOUND EEPLS INOP AT ROW NR 20 THROUGH ROW NR 25. REPAIRED EEPLS PER MM.

Part: ENGINE — LEAKING (RIGHT) · airframe 13,829 hrs · 8,198 cycles

IN-FLT SHUTDOWN, DECLARED EMERGENCY, NR 2 ENGINE OIL PRESS WENT TO 0, OIL QUANTITY DROPPED TO 0, SHUTDOWN ENGINE. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 13,352 hrs · 7,938 cycles

DURING SCHEDULED A2 CHECK, SWA SI 11038, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS ON NR 2, NR 3 AND NR 4 TAB HINGE ATTACH POINTS PER MM.

Part: COVER — MISSING (CABIN) · airframe 13,037 hrs · 7,751 cycles

EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: HINGE — WORN (BOTH ELEVATORS) · airframe 12,068 hrs · 7,148 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND LT AND RT TAB HINGE BOLTS WILL NOT ROTATE AT HINGES NR 1 THROUGH NR 4. REMOVED AND REPLACED LT AND RT TAB HINGES NR 1 THROUGH NR 4 PER MM.

Part: BUSHING — WORN (ELEVATORS) · airframe 11,066 hrs · 6,610 cycles

DURING SCHEDULED SERVICE CHECK, (SI NR 11038-55), BOTH LT AND RT ELEVATORS FAILED FREE PLAY CHECKS. REMOVED AND REPLACED LT ELEVATOR TAB ATTACH BUSHINGS AT NR 3 AND NR 4 POSITION, AND REMOVED AND REPLACED RT ELEVATOR TAB ATTACH BUSHINGS AT NR 2 AND NR 4 POSITION PER MM..

Part: BUSHING — WORN (RH ELEVATOR) · airframe 8,976 hrs · 5,437 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11075-55, FOUND RH ELEVATOR TAB HINGE BUSHINGS WORN AT HINGE'S #2, #3 & #4. R&R HINGE BUSHINGS PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 1,947 hrs · 5,437 cycles

DURING SCHEDULED SERVICE CHECK SWA SI 11075-55, FOUND LT ELEVATOR TAB HINGE BUSHINGS WORN AT HINGE'S NR 2, 3 & 4. REMOVED AND REPLACED HINGE BUSHINGS PER MM.

Part: SLIDE — DEPLOYED (SERVICE DOOR) · airframe 8,433 hrs · 5,131 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 5,841 hrs · 3,606 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER CRACKED AT FWD SECTION. REMOVED AND REPLACED TRACK COVER PER MM.

Part: BREAKER — TRIPPED (COCKPIT)

AIR TURNBACK, AFTER TAKEOFF, LANDING GEAR LEVER WOULD NOT GO INTO THE UP POSITION. FOUND GEAR LATCH AND PRESSURE WARNING C/B TRIPPED. RESET C/B AND OPS CK GOOD PER MM.