N613SW

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 67,203 hrs · 53,354 cycles

FORWARD EMERGENCY FLASHLIGHT HOLDER STRAP BROKEN. R&R STRAP PER MM.

Part: FITTING — OUT OF POSITION (L2 DOOR) · airframe 67,154 hrs · 53,325 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIPS OUT OF POSITION. REPAIRED CLIPS PER MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 67,147 hrs · 53,320 cycles

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

Part: STRAP — BROKEN (CRADLE) · airframe 66,336 hrs · 52,768 cycles

FORWARD OUTBOARD FLASHLIGHT STRAP BROKEN. R & R STRAP IAW SIP.

Part: CASTING — BROKEN (LT WING SPOILER) · airframe 66,197 hrs · 52,681 cycles

LT WING NR 4 GROUND SPOILER OUT BOUND HINGE CASTING TOP BROKEN. R & R NR 4 GROUND SPOILER IAW AMM.

Part: SKIN — CRACKED (RT WING LE) · airframe 66,016 hrs · 52,551 cycles

RIGHT WING LEADING EDGE BULL NOSE SKIN CRACKED. REPAIRED THE SKIN IAW SRM.

Part: CASTING — CRACKED (LT WING K FLAP) · airframe 66,016 hrs · 52,551 cycles

LEFT WING NR 1 KRUEGER FLAP CRACKED ON INTERNAL CASTING. R & R THE NR 1 KRUEGER FLAP IAW AMM.

Part: SKIN — CRACKED (LT WING LE) · airframe 66,016 hrs · 52,551 cycles

LEFT WING FIXED LEADING EDGE BULL NOSE CRACKED. REPAIRED THE SKIN IAW EA AND SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 66,016 hrs · 52,551 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER LENS LOOSE. SECURED THE LENS IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 65,143 hrs · 51,967 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LENS — LOOSE (EXIT SIGN) · airframe 64,286 hrs · 51,400 cycles

RIGHT OVERWING EXIT SIGN LENS LOOSE. SECURED LENS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 63,988 hrs · 51,182 cycles

L1 DOOR OVERHEAD EMER EXIT SIGN LENS LOOSE. SECURED LENS IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 63,322 hrs · 50,706 cycles

RIGHT OVERWING OVERHEAD EMER EXIT SIGN LOOSE. INSTALLED SIGN IAW MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 63,254 hrs · 50,655 cycles

RIGHT OVERWING EMER EXIT HATCH SIGN LENS MISSING. REINSTALLED LENS IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 62,733 hrs · 50,274 cycles

LEFT OVERWING EMER EXIT LENS LOOSE. SECURED LENS MM.

Part: LENS — CRACKED (CABIN) · airframe 62,533 hrs · 50,134 cycles

RIGHT OVERWING EMER EXIT LIGHT LENS CRACKED. R & R LENS IAW MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 62,533 hrs · 50,134 cycles

FORWARD OTBD EMER FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 62,533 hrs · 50,134 cycles

R2 DOOR SLIDE UPPER FWD BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

BULKHEAD ATTACH ANGLE CRACKED BS 947, STRINGER 22R. R & R ANGLE IAW DWG & SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

SHEAR TIE CORRODED AT BS 727E, BETWEEN STRINGER 27L - 27R. REPAIRED SHEAR TIE IAW ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

STRINGER CLIP CRACKED AT BS 1120, STRINGER 2L. R & R CLIP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, RBL 8. REPAIRED BEAM IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

SHEAR TIE CORRODED AT BS 986.5, BETWEEN STRINGER 27R TO 27L. R & R SHEAR TIE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

SHEAR TIE CORRODED AT BS 967, BETWEEN STRINGER 26L - 27L. R & R SHEAR TIE IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED BEAM IAW EA & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, LBL 8. REPAIRED BEAM IAW EA & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 772, LBL 12.5. REPAIRED BEAM IAW EA & SRM.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

NUMBER 3 VHF ANTENNA SUPPORT CHANNEL CORRODED AT BS 727D+10, LBL 1.5. REPAIRED CHANNEL IAW ER & EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

LOWER FWD HOLE CHORD CRACKED AT BS 727, STRINGER 18A. REPAIRED CHORD IAW ER & EA.

Part: WEB — CRACKED (NLG WW) · airframe 62,336 hrs · 50,004 cycles

RIGHT NOSE WW WEB CRACKED AT BS 247.2. REPAIRED WEB IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

CHORD CRACKED AT BS 727, STRINGER 18A LT. REPAIRED CHORD IAW EA & ER.

Part: WEB — CRACKED (NLG WW) · airframe 62,336 hrs · 50,004 cycles

RIGHT NOSE WW WEB CRACKED AT BS 258.5. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

R2 DOOR LOWER HINGE SKIN CUT OUT LOWER FWD CORNER CRACKED. REPAIRED SKIN IAW EA & ER.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

CHANNEL CRACKED AT BS 359, STRINGER 8L. R & R CHANNEL IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 5L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

STRINGER CLIP CRACKED AT BS 908, STRINGER 7L. R & R CLIP IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 767 - 787. R & R WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 500A - 500B. R & R WEB IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

FLOORBEAM CORRODED AT BS 986.5, LBL 0. REPAIRED BEAM IAW EA.

Part: FORMER — CRACKED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

RIGHT WING TO BODY FAIRING FORMER CRACKED AT BS 540, UPPER OTBD END. R & R FORMER IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

FLOORBEAM CORRODED AT BS 986.5, LBL 5. REPAIRED BEAM IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 420 - 440. REPAIRED WEB IAW SRM & DWG.

Part: SPAR — CRACKED (LT WING) · airframe 62,336 hrs · 50,004 cycles

LEFT WING UPPER REAR SPAR CHORD CRACKED AT RSS 226. REPAIRED CHORD IAW ER & EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,336 hrs · 50,004 cycles

STRINGER CLIP CRACKED AT BS 597, STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: SPAR — CRACKED (RT WING) · airframe 62,336 hrs · 50,004 cycles

RIGHT WING UPPER REAR SPAR CHORD CRACKED AT RSS 228. REPAIRED CHORD IAW ER & EA.

Part: STRAP — DETERIORATED (CABIN) · airframe 62,336 hrs · 50,004 cycles

RIGHT OVERWING EMER EXIT HATCH ESCAPE STRAP HOOK TOW COVER HAD DETERIORATED VELCRO. R & R STRAP ASSEMBLY IAW AMM.

Part: STRAP — DETERIORATED (CABIN) · airframe 62,336 hrs · 50,004 cycles

LEFT OVERWING EMER EXIT HATCH ESCAPE STRAP HOOK TOW COVER HAD DETERIORATED VELCRO. R & R STRAP ASSEMBLY IAW AMM.

Part: COVER — BROKEN (CABIN) · airframe 62,162 hrs · 49,890 cycles

L1 DOOR EMER EXIT LIGHT COVER BROKEN. R & R COVER IAW SIP.

Part: SPOILER — BROKEN (LT WING) · airframe 62,098 hrs · 49,846 cycles

LEFT WING INBD GND SPOILER ATTACH POINT TO OUTBOARD ACTUATOR BROKEN. R & R GND SPOILER IAW MM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 61,708 hrs · 49,582 cycles

L1 DOOR SLIDE FALLING OUT OF CONTAINER. SECURED SLIDE IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 61,708 hrs · 49,582 cycles

L1 DOOR SLIDE FALLING OUT OF CONTAINER. REPOSITIONED SLIDE IAW MM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 61,273 hrs · 49,283 cycles

U STIFFENER CORRODED BETWEEN BS 1016 TO 1016 + 5, RBL 1. REPAIRED U STIFFENER IAW SRM & EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,273 hrs · 49,283 cycles

STRINGER CORRODED BETWEEN BS 1006 TO 1016, STRINGER 26R. R & R STRINGER IAW DWG & SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 61,273 hrs · 49,283 cycles

U STIFFENER CORRODED BETWEEN BS 1016 TO 1016 + 6, LBL 1. REPAIRED U STIFFENER IAW SRM & EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 61,273 hrs · 49,283 cycles

AFT PRESS BULKHEAD CTR DOME PAN Z STIFFENER CRACKED AT BS 1016 STRINGER 3L. REPAIRED Z STIFFENER IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,273 hrs · 49,283 cycles

FORWARD ENTRY DOOR FRAME INNER CHORD CRACKED AT BS 348.2. R & R CHORD IAW EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 61,273 hrs · 49,283 cycles

AFT PRESS BULKHEAD WEB SKIN CORRODED AT BS 1016, BETWEEN LBL 0 TO LBL 3. REPAIRED WEB IAW SRM & EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 61,273 hrs · 49,283 cycles

AFT PRESS BULKHEAD CORRODED AT BS 1016, BETWEEN LBL 0 TO LBL 5. REPAIRED BULKHEAD IAW SRM & EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,235 hrs · 49,260 cycles

LEFT FLUORESCENT LIGHTS BETWEEN ROWS 4 TO ROWS 7 WENT OUT & PRODUCED A STRONG ACRID SMELL & LIGHT SMOKE. R & R LIGHT IAW MM.

Part: FAN — FAULTY (AC BAY) · airframe 60,643 hrs · 48,835 cycles

ELECTRICAL SMELL COMING FROM FWD & AFT GALLEY & SPREAD THRU CABIN. R & R RECIRC FAN IAW MM.

Part: LIGHT — MISSING (CABIN) · airframe 59,549 hrs · 48,073 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT COVER MISSING. R & R LIGHT ASSEMBLY IAW AMM.

Part: BRACKET — CRACKED (LT PYLON) · airframe 58,608 hrs · 47,426 cycles

LT PYLON PANEL 5757L CUTOUT AFT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 58,369 hrs · 47,260 cycles

BURNING SMELL IN THE CABIN WHILE DESCENDING. FOUND GASPER FAN EMITTING ELECTRIC SMELL & NOISE. R & R GASPER FAN IAW MM.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 58,238 hrs · 47,150 cycles

NR 7 TE FLAP TRACK CORRODED AT WING SPAR ATTACH FITTINGS. R & R NR 7 TE FLAP TRACK IAW MM.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 58,238 hrs · 47,150 cycles

NR 2 TE FLAP TRACK CORRODED AT WING SPAR ATTACH FITTINGS. R & R NR 2 TE FLAP TRACK IAW MM.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 57,942 hrs · 46,911 cycles

FWD OTBD CABIN FLASHLIGHT INOPERATIVE. R&R BATTERY PACK IAW MM.

Part: FLAP — OUT OF ADJUST (RT WING) · airframe 57,351 hrs · 46,471 cycles

RT WING INBOARD AFT FLAP OUT OF ADJUSTMENT. ADJUSTED AFT FLAP IAW MM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

STRINGER CLIP CORRODED AT BS 351, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

STRINGER CLIP CORRODED AT BS 360, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

KEEL BEAM CLIP CORRODED AT BS 767, STR 27R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

KEEL BEAM CLIP CORRODED AT BS 767, STR 27L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRUCTURE — WORN (LE SLAT) · airframe 56,572 hrs · 45,908 cycles

RIGHT WING NR 6 SLAT I/B SLAT CAN WORN. REMOVED AND REPLACED SLAT I/B CAN IAW EA.

Part: SUPPORT ANGLE — CRACKED (L1 DOOR) · airframe 56,572 hrs · 45,908 cycles

L1 DOOR UPPER WEB SUPPORT ANGLE CRACKED BETWEEN BS 348.2 TO BS 351, STR 16L. REMOVED AND REPLACED ANGLE IAW DWG AND SRM.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 56,572 hrs · 45,908 cycles

L1 DOOR LOWER WEB SUPPORT ANGLE CRACKED BETWEEN BS 348.2 TO BS 351, STR 16L. REMOVED AND REPLACED ANGLE IAW DWG AND SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

SUPPORT ANGLE CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED ANGLE PER SRM.

Part: WEB — CRACKED (L1 DOOR) · airframe 56,572 hrs · 45,908 cycles

L1 DOOR WEB CRACKED AT BS 348.2, STR 16L. REMOVED AND REPLACED WEB IAW DWG AND SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

KEEL BEAM CLIP CORRODED AT BS 767, STR 27R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

SHEAR TIE CORRODED BS 767, BETWEEN STR 26L AND STR 27L LBL 10. REMOVED AND REPLACED FRAME IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

SHEAR TIE CORRODED AT BS 787, BETWEEN STR 23R TO STR 23L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: STRAP — CRACKED (CARGO BAY) · airframe 56,572 hrs · 45,908 cycles

AFT PIT DOOR CLOSURE SIDEWALL PANEL AFT STRAP CRACKED. REMOVED AND REPLACED STRAP IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

STRINGER SPLICE CORRODED BETWEEN BS 360 TO BS 380, STR 28L. REMOVED AND REPLACED SPLICE IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

SHEAR TIE CORRODED AT BS 767 BETWEEN, STR 27R. REMOVED AND REPLACED FRAME IAW EA.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 56,572 hrs · 45,908 cycles

RIGHT MAIN W/W VERTICAL STIFFENER CRACKED AT BS 663.75, RBL 6.15. REPAIRED STIFFENER IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27L AND STR 26R. REMOVED AND REPLACED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

SHEAR TIE CORRODED AT BS 500A, LBL 24. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 28R AND STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 56,572 hrs · 45,908 cycles

RIGHT VERTICAL STIFFENER CORRODED AT BS 500D, STR 28R. REMOVED AND REPLACED STIFFENER IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 56,506 hrs · 45,862 cycles

EMERGENCY FLASHLIGHT RED LIGHT NOT FLASHING. REMOVED AND REPLACED BATTERY PER MM.

Part: STRUCTURE — DAMAGED (LE SLAT) · airframe 56,269 hrs · 45,699 cycles

TRANSFERRED FROM NRC C797469 " NR 1 SLAT INBOARD SLAT CAN DAMAGED FROM CONTACT WITH SLAT TRACK/STOP". REMOVED & REPLACED NR 1 SLAT I/B CAN AND PERFORMED SATISFACTORY FUEL LEAK CHECK IAW SRM 51-40-02-01-0G-0 AND BAC DWG 65-45320 AND MM 28-11-00-658-148.

Part: STRUCTURE — DAMAGED (LE SLAT) · airframe 56,269 hrs · 45,699 cycles

NR 6 SLAT INBD SLAT CAN DAMAGED DUE TO CONTACT WITH SLAT TRACK/STOP. R & R NR 6 SLAT CAN IAW SRM AND DWG.

Part: FUSE — BLOWN (CABIN) · airframe 56,184 hrs · 45,640 cycles

OVERHEAD LEFT EXIT SIGN AT L1 DOOR IS INOP. REMOVED & REPLACED M1674 BATTERY POWER FUSE SUPPLY AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,184 hrs · 45,640 cycles

LEFT ESCAPE SLIDE LIGHT IN INOP. RELAMPED LEFT DOOR ESCAPE SLIDE LIGHT (FWD), PER B737-3 AMM

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

STA 380 STR 5L HAS EXISTING CRACK IN STRINGER RADIUS. REPAIRED STRINGER PER EA.

Part: STRINGER CLIP — BROKEN (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

STR CLIP AT BS 727C STR 1 BROKEN. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STAND OFF — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

STA 272 BETWEEN STR 2L AND 3L HAS A CRACKED WIRING STANDOFF ON INTERCOSTAL. REMOVED DAMAGED STANDOFF; INSTALLED REPLACEMENT IAW B737-300 SRM 51-40-02 AT STA 272 S-2L AND S-3L.

Part: STAND OFF — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

STA 277 AT STR 2R LOCATION HAS A CRACKED WIRING STANDOFF ON AFT SIDE OF FRAME. REMOVED DAMAGED STANDOFF; INSTALLED REPLACEMENT IAW B737-300 SRM 51-40-02 AT STA 277 S-2R.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

STRINGER CLIP IS CRACKED AT STA 344 STR 3L. REMOVED AND REPLACED STRINGER CLIP AT STA 344 STR 3L IAW DWG 65-45815 AND 69-35352, B737-300 SRM 51-40-02. ALODINED & PRIMER IAW B737 SRM 51-20-01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

STRINGER CRACKED AT BS 500D, STRINGER 2L. REPAIRED STRINGER IAW SRM 53-00-03-2R-3 AND REO G15726 REV IR AND EA 1-353-21198.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT FUSE STA 927 DOOR SURROUND SEAL FITTING HAS INCOMING CRACK AT TOP EDGE. LOCATED, DRILLED, DEBURRED AND INSTALLED NEW DOOR SURROUND SEAL FITTING IAW B737 SRM 51-40-02 AND BOEING DWG 65-52874 REV L FAY SEALED FITTING IAW BAC 5000.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 908 S4R STRINGER SPLICE FITTING HAS INCOMING CRACKS AROUND FASTENER HOLES. REMOVED & INSTALLED NEW STRINGER SPLICE P/N 65-51698U47 PO 761729.1 IAW BAC DWG 65-51698 & B737 SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 3. REPAIRED LEFT BS 867+10 UPPER AFT WINDOW CORNER IAW SB737-53-1306 REV 2 SECT 3.B.3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 767+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED RIGHT BS 767 +10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306, REV 2, SECTION 3.B.3. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT BS 847+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 9, 10, 11. REPAIRED LEFT BS 847+10 UPPER AFT WINDOW CORNER IAW SB 737-53-1306 REV 2 SECT 3.B.3 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 727A+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 6. REPAIRED RIGHT BS 727A+10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21244 REV -, REO-G15695 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT BS 767+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 3. REPAIRED LEFT BS 767+10 UPPER AFT WINDOW CORNER IAW SB737-53-1306 REV 2 SECT 3.B.3 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT BS 767+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3. REPAIRED LEFT BS 767 +10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306, REV 2, SECT 3.B.3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4. REPAIRED RIGHT BS 867+10 UPPER AFT WINDOW CORNER IAW EA 1-353-21225 REV- AND REO-15691 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT BS 727+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 7. REPAIRED LEFT BS 727 +10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21209 REV - , REO G15700, REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 807+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 9. REPAIRED RIGHT BS 807 +10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306, REV 2, SECT 3.B.3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 887+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 8. REPAIRED RIGHT BS 887 +10 LOWER FORWARD WINDOW CORNER IAW BOEING SB 737-53-1306, REV 2, SEC 3.B.3 AS PER TASK CARD 10074, STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT BS 807+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 5. REPAIRED LEFT BS 807 +10 LOWER FORWARD WINDOW CORNER IAW BOEING SB 737-53-1306, REV 2, SECT 3.B.3. PER TASK CARD 10075.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT BS 807+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 5. REPAIRED LEFT BS 807 +10 UPPER AFT WINDOW CORNER IAW BOEING SB 737-53-1306, REV 2 SECT 3.B.3 PER TASK CARD 10075. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT BS 827+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4. REPAIRED LEFT BS 827 +10 UPPER AFT WINDOW CORNER IAW BOEING SB 737-53-1306, REV 2 SECT 3.B.3. PER TASK CARD 10075. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 767+10 UPPER WINDOW CORNER HAS HFEC NOISE AT HOLE 7 AND CRACKED AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT BS 787+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 3, 9. REPAIRED LEFT BS 787 +10 UPPER AFT WINDOW CORNER IAW SB 727-53-1306, REV 2, SECT 3.B.3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 887+10 UPPER WINDOW CORNER HAS HFEC NOISE AT HOLES 4, 5 AND HFEC CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 847+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 10. REPAIRED RIGHT BS 847+10 LOWER FORWARD WINDOW CORNER IAW SB737-53-1306 R2 SECT 3.B.3 AS PER TASK CARD 10074 STEP 8 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT BS 787+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3. REPAIRED LEFT BS 787+10 LOWER FORWARD WINDOW CORNER IAW SB737-53-1306 REV 2 SECT 3.B.3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 827+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 8, 9, 10. REPAIRED RIGHT BS 827 +10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306, REV 2, SECT 3.B.3. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 807+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED RIGHT BS 807 +10 UPPER AFT WINDOW CORNER IAW SB 737-53-1306, REV 2, SECT 3.B.3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT BS 827+10 LOWER WINDOW CORNER HAS HFEC CRACKED AT HOLES 1, 2, 3, 5. REPAIRED SKIN IAW BOEING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 727+10 LOWER FORWARD WINDOW CORNER HAS HFEC NOISE INDICATION AT HOLE NR 7. REPAIRED RIGHT BS 727 +10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21203 REV - , REO G15692, REV IR.

Part: SKIN — CRACKED (FUSELGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 867+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 9,10. REPAIRED RIGHT BS 867 +10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21215 REV - , REO G15697 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

RIGHT BS 847+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 9, 10. REPAIRED RIGHT BS 847+10 UPPER AFT WINDOW CORNER IAW SB737-53-1306 REV 2, SECTION 3.B.3 AS PER TASK CARD 10074 STEP 8 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT BS 867+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3. REPAIRED LEFT BS 867+10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306 REV 2 SECT 3.B.3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,184 hrs · 45,640 cycles

LEFT BS 887+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 3. REPAIRED LEFT BS 887 +10 UPPER AFT WINDOW CORNER IAW EA 1-353-21208 REV - , REO G15699 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 55,392 hrs · 45,032 cycles

FORWARD BULKHEAD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER M/M.

Part: FLAP — PUNCTURED (RT WING) · airframe 55,165 hrs · 44,858 cycles

RIGHT INBOARD FORE FLAP PUNCTURED. REMOVED AND REPLACED FORE FLAP PER M/M.

Part: LENS — MISSING (CABIN) · airframe 54,857 hrs · 44,632 cycles

CENTER CEILING EMERGENCY EXIT LIGHT LOWER LEFT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,601 hrs · 44,434 cycles

SKIN CRACKED AT BS 727D, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,601 hrs · 44,434 cycles

SKIN CRACKED AT BS 757, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,601 hrs · 44,434 cycles

SKIN CRACKED AT BS 799, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,601 hrs · 44,434 cycles

SKIN CRACKED BETWEEN BS 776 TO BS 777, STR 4R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,601 hrs · 44,434 cycles

SKIN CRACKED BETWEEN BS 727C+10 TO BS 727+15, STR 4R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,826 hrs · 46,095 cycles

LEFT WING NR 1 SLAT CRACKED ON LOWER SKIN I/B END AT AFT ROW OF FASTENERS. REPAIRED NR 1 SLAT PER EA AND SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,579 hrs · 45,912 cycles

RIGHT WING NR 5 SLAT CRACKED ON LOWER SKIN AT AFT ROW OF FASTENERS. REMOVED AND REPLACED NR 5 SLAT IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,579 hrs · 45,912 cycles

LEFT WING NR 2 SLAT CRACKED ON LOWER SKIN AT AFT ROW OF FASTENERS. REMOVED AND REPLACED NR 2 SLAT IAW AMM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 53,805 hrs · 43,837 cycles

IMMEDIATELY AFTER SECURING GASPER FAN ON CLIMBOUT FLIGHT ATTENDANTS REPORTED STRONG ELECTRICAL WIRING BURNT SMELL. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 52,818 hrs · 43,105 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. REINSTALLED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,562 hrs · 42,899 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: FASTENER — MISSING (EVAC SLIDE) · airframe 52,313 hrs · 42,713 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE BRACKET FASTENER MISSING. INSTALLED FASTENER PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,148 hrs · 42,588 cycles

AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CORRODED AT BS 807, BETWEEN LBL 5 TO RBL 5. REPAIRED FRAME PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO FLOOR SUPPORT BEAM CORRODED AT BS 943, LBL 17. REPAIRED BEAM PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK FOUND, KEEL BEAM CORRODED AT BS 807, RBL 7. REPAIRED BEAM PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK FOUND, LT WING NR 2 SLAT O/B T/E WEDGE DELAMINATED. REPAIRED SLAT EPR SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK FOUND, CENTER CABIN BEADED WEB CRACKED AT BS 671, RBL 39. REPAIRED WEB PER EA.

Part: WEB — CRACKED (BS 671) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK FOUND, CENTER CABIN BEADED WEB CRACKED AT BS 671, LBL 41. REPAIRED WEB PER EA.

Part: FLOORBEAM — CRACKED (BS 663.75) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK FOUND, LONGITUDINAL FLOORBEAM LOWER CHORD L ANGLE CRACKED AT BS 663.75, RBL 45.50. REPAIRED ANGLE PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,714 hrs · 42,626 cycles

DURING SCHEDULED 16Y CHECK FOUND, LT CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A, STR 17L. REPAIRED BEAM PER BAC DWG AND EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,714 hrs · 42,626 cycles

DURING SCHEDULED 16Y CHECK FOUND, LT CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A, STR 17L. REPAIRED BEAM PER BAC DWG AND EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,714 hrs · 42,626 cycles

DURING SCHEDULED 16Y CHECK FOUND, LT CREASE BEAM WEB CORRODED BETWEEN BS 500A TO BS 500B, STR 17L. REPAIRED BEAM PER BAC DWG AND EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,714 hrs · 42,626 cycles

DURING SCHEDULED 16Y CHECK FOUND, LT CREASE BEAM WEB CORRODED BETWEEN BS 414 TO BS 418, STR 17L. REPAIRED BEAM PER BAC DWG AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT GALLEY FLOOR BEAM FLANGE CORRODED AT BS 986, BETWEEN RBL 36 TO RBL 42. REMOVED AND REPLACED BEAM PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK FOUND, FLOORBEAM CORRODED AT BS 312, BL 0. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK FOUND, SHEAR TIE CORRODED AT BS 1006, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,714 hrs · 42,262 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD OPC CRADLE SKIN CUTOUT CRACKED AT BS 255, RBL 23. REPAIRED SKIN PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,602 hrs · 41,408 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 50,602 hrs · 41,408 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD EMERGENCY FLASHLIGHT BREAK-AWAY RETAINER STRAPS BROKEN. REMOVED AND REPLACED STRAPS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 50,458 hrs · 41,309 cycles

LT FWD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,057 hrs · 41,011 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: WEB — CRACKED (NLG) · airframe 49,117 hrs · 40,295 cycles

RT SIDE WEB NOSE WHEEL WELL BETWEEN ACCESS PANELS CRACKED AT BS 259, WL 174. REPAIRED WEB PER EA.

Part: LIGHT — LOOSE (CABIN) · airframe 46,598 hrs · 38,441 cycles

LEFT EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 2. SECURED LIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 46,548 hrs · 38,401 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 46,499 hrs · 38,362 cycles

AFT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304.65, WL 258.38. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING I/B FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 304.65, WL 238.18. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304.65, WL 262.38. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14YD CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,189 hrs · 38,135 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,173 hrs · 38,126 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR AT UPPER FWD CORNER. REPAIRED SKIN PER SRM.

Part: ISOLATION VALVE — LEAKING (HYDRAULIC SYS) · airframe 46,042 hrs · 38,025 cycles

AIR TURNBACK / DECLARED EMERGENCY. LOST "A" SYSTEM HYDRAULICS ON TAKEOFF. REMOVED AND REPLACED MANUAL ISOLATION VALVE FOR NR 2 RUDDER PCU/YAW DAMPER PER MM.

Part: STRAP — OUT OF POSITION (EMERGENCY EXIT) · airframe 45,020 hrs · 37,299 cycles

LT OVERWING EMERGENCY EXIT DOOR STRAP OUT OF POSITION. REPOSITIONED STRAP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 44,760 hrs · 37,107 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 44,760 hrs · 37,107 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 44,760 hrs · 37,107 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 44,760 hrs · 37,107 cycles

DURING SCHEDULED SPV CHECK, FOUND BS 178 BULKHEAD VERTICAL WEB CRACKED, LBL 17, WL 228. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (BULKHEAD) · airframe 44,760 hrs · 37,107 cycles

DURING SCHEDULED SPV CHECK, FOUND BS 178 BULKHEAD CHORD CRACKED, LBL 17, WL 218. REPAIRED WEB PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 44,551 hrs · 36,952 cycles

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

Part: FITTING — LOOSE (GIRT BAR) · airframe 44,551 hrs · 36,952 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR SLIDE GIRT BAR FWD CLIP LOOSE. SECURED CLIP PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHTS) · airframe 43,021 hrs · 35,828 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 6 ABC. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 42,242 hrs · 35,282 cycles

EEPLS LENS CRACKED AT ROW 6 ABC. REMOVED AND REPLACED LENS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,005 hrs · 34,353 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,974 hrs · 34,334 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 40,974 hrs · 34,333 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 40,414 hrs · 33,893 cycles

DURING SCHEDULED MV1 CHECK, R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: BEARING — WORN (RT ELEVATOR TAB) · airframe 39,370 hrs · 33,033 cycles

DURING SCHEDULED C4 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED INPUT ROD BEARING PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 38,124 hrs · 32,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 358, STR 16L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 38,124 hrs · 32,047 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME WEB CRACKED AT BS 846, STR 18R. REPAIRED WEB SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 38,124 hrs · 32,047 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 37,753 hrs · 31,763 cycles

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

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 37,446 hrs · 31,502 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED INBOARD FORE FLAP PER MM.

Part: SKIN — CRACKED (BS 378) · airframe 37,446 hrs · 31,502 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT E&E COOLING EXHAUST DUCT CUTOUT, BS 378.5, LBL 2.8. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 36,623 hrs · 30,851 cycles

FWD RIGHT EMERGENCY EXIT LIGHT LEFT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,583 hrs · 30,821 cycles

DURING SCHEDULED C1 CHECK, FOUND KEEL BEAM PANEL SKIN CRACKED AT BS 690, WL 148.5. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 36,583 hrs · 30,821 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,199 hrs · 30,523 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD RT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: PUMP — FOD (NR 1 ENGINE) · airframe 35,982 hrs · 30,352 cycles

AIR TURNBACK. ENGINE DRIVEN PUMP -A- SYSTEM HYDRAULIC QUANTITY DROPPED TO 1/4 FULL. FOUND NR 1 ENGINE DRIVEN HYDRAULIC PUMP CONTAMINATED WITH METAL. REMOVED AND REPLACED PUMP PER MM.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 35,982 hrs · 30,351 cycles

AIR TURNBACK, ENGINE DRIVEN "A" SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. "A" SYSTEM QUANTITY DROPPED TO 1/4 FULL. R&R "A" SYSTEM HYDRAULIC ELECTRIC DRIVEN PUMP PRESSURE LINE PER MM.

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 34,665 hrs · 29,370 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR LOWER FUSELAGE HINGE BOX FITTING CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SRM.

Part: SLIDE — OUT OF ADJUST (AFT CABIN) · airframe 33,675 hrs · 28,589 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 & L2 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: FRAME — CRACKED (FWD CARGO) · airframe 33,659 hrs · 28,574 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R TO STR 26R. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (FWD CARGO) · airframe 33,659 hrs · 28,574 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER BFG ER.

Part: STRAP — CRACKED (FUSELAGE SKIN) · airframe 33,506 hrs · 28,442 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN STRAP CRACKED AT BS 440, STR 24R. REMOVED AND REPLACED SKIN STRAP SECTION PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, LBL 17. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65 & RBL 65, WL 200. REPAIRED FRAME PER BFG ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 24R. REPAIRED FRAME PER BFG ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 6 TO RBL 6. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (COCKPIT FLOOR) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOORBEAM UPPER CHORD CORRODED AT BS 259.5, LBL 6 TO RBL 11. REPAIRED FLOORBEAM PER BFG ER.

Part: BRACKET — CORRODED (L1 DOOR SLIDE) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD & AFT FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED ATTACH BRACKETS PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT VERTICAL STAB ATTACH FITTING FWD & AFT PRIMARY CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, LBL 45 TO RBL 45. REPAIRED FLOORBEAM PER BFG ER.

Part: FLOOR SUPPORT — CORRODED (CABIN FLOOR) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND CABIN LONGITUDINAL UPPER CHORD CORRODED AT BS 270, BL 0, WL 208. REPAIRED UPPER CHORD PER SRM.

Part: FRAME — CRACKED (BS 380) · airframe 33,469 hrs · 28,410 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380 TO BS 400, STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,463 hrs · 28,404 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 1064, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 31,889 hrs · 27,196 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FORE FLAP PER MM.

Part: STRIP — WORN (CABIN) · airframe 31,889 hrs · 27,196 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP WORN AT ROWS 1 ABC & 3 ABC. REMOVED AND REPLACED EEPLS STRIPS PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 30,010 hrs · 25,672 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 29,683 hrs · 25,400 cycles

IN FLIGHT THE R2 WINDOW ARCED, COMPLIED WITH QRH. REMOVED AND REPLACED R2 WINDOW PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 29,683 hrs · 25,400 cycles

DURING SCHEDULED RON, L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, SLIDE DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 29,601 hrs · 25,339 cycles

L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 28,812 hrs · 24,716 cycles

R1 DOOR EVAC SLIDE LOOSE. RE-INSTALLED R1 DOOR EVAC SLIDE PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,563 hrs · 22,938 cycles

AFT CABIN EMERGENCY FLASHLIGHT BATTERY WEAK. REMOVED AND REPLACED BATTERY PER MM.

Part: RIB — CRACKED (RH WING) · airframe 25,460 hrs · 22,078 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN S2R & S3R. REPAIRED RIB PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 25,238 hrs · 21,910 cycles

DURING SCHEDULED BC1 CHECK, FOUND R2 DOOR ESCAPE SLIDE OUT OF ADJUSTMENT. ADJUSTED ESCAPE SLIDE PER MM.

Part: SIGN — LOOSE (ENTRY DOOR) · airframe 23,208 hrs · 20,239 cycles

FWD ENTRY DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 22,057 hrs · 19,297 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB HAS A HOLE AT BS 178, WL 183 AND RBL 17.1. REMOVED AND REPLACED WEB PER SWA ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,057 hrs · 19,297 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT CHORD CRACKED AT BS 178, WL 207 AND RBL 34.5. REPAIRED CHORD PER SWA ACO.

Part: SLIDE — OUT OF ADJ (R1 DOOR) · airframe 21,557 hrs · 18,903 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: ENGINE — OVERTEMP (NR 1) · airframe 21,174 hrs · 18,584 cycles

(AIR TURNBACK) DURING CLIMB NR 1 ENG HAD 2 HIGH EGT INDICATIONS, (1100 DEGS & 950 DEGS), FOLLOWED BY ANOTHER HIGH EGT DURING APPROACH (950 DEG). REMOVED AND REPLACED NR 1 ENG PER MM.

Part: TRANSMISSION — INOPERATIVE (T/E FLAP) · airframe 20,125 hrs · 17,667 cycles

DURING APPROACH FLAPS WOULD NOT PASS 2.1 POSITION. FOUND NR 3 T/E FLAP TRANSMISSION INOP ALONG WITH DAMAGE TO AFT LT WING BODY FAIRING, NR 4 FLAP TRACK ATTACH CASTING, INBOARD MID FLAP FAIRING. REMOVED AND REPLACED NR 3 FLAP TRANSMISSION, NR 4 FLAP TRACK ATTACH CASTING. REPAIRED LT WING BODY FAIRING PER SWA RA AND REMOVED INBOARD MID FLAP FAIRING PER CDL, MX FERRY TO DAL FOR REPAIRS.

Part: TRANSMISSION — FAILED (T/E FLAP) · airframe 20,125 hrs · 17,667 cycles

DURING SCHEDULED SPECIAL VISIT CHECK DUE TO NR 3 T/E FLAP TRANSMISSION FAILURE, (MX FERRY TO DAL). REMOVED AND REPLACED LT INBD AFT FLAP, LT INBD FORE FLAP. REMOVED AND REPLACED LT WING BODY FAIRING, REMOVED AND REPLACED CRACKED LT INBD MID FLAP FAIRING ATTACH PLATE, REPAIRED LT WING TO BODY FAIRING AFT SUPPORT FRAME PER SWA RA & MM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 17,228 hrs · 15,225 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AISLE EMERGENCY EXIT LIGHT INOP BETWEEN BS 430 - 500. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 17,199 hrs · 15,196 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT NR 3 STOP. REPAIRED FRAME PER TI-152-003.

Part: CREASE BEAM — CRACKED (CABIN) · airframe 17,199 hrs · 15,196 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED, BS 827 TO BS 847. REPAIRED CREASE BEAM SECTION PER SRM.

Part: ANGLE — CRACKED (GALLEY) · airframe 17,199 hrs · 15,196 cycles

DURING SCHEDULED 1/2D CHECK, FOUND ANGLES CRACKED, BS 292, STRINGER 12R AND BS 294, STRINGER 9R. REMOVED AND REPLACED ANGLES PER SRM.

Part: FLOORBEAM — CORRODED (GALLEY) · airframe 17,199 hrs · 15,196 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 328 FLOORBEAM CORRODED AROUND NUT PLATE, RBL 42. REPAIRED BEAM PER TI-553-048.

Part: SWITCH — OUT OF ADJ (CARGO DOOR) · airframe 15,926 hrs · 14,102 cycles

AIR TURNBACK, AFT CARGO DOOR LIGHT ILUMMINATED ON TAKEOFF. VERIFIED DOOR CLOSED AND DEFERRED PER MEL. LATER ON AT BWI ADJUSTED DOOR POSITION SWITCH PER MM.

Part: SLIDE — DISCHARGED (SERVICE DOOR) · airframe 15,864 hrs · 14,050 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR LOW. R&R SLIDE ASSY PER MM.

Part: SENSOR CABLE — OUT OF ADJUST (RT MLG)

AIR TURNBACK, GEAR HANDLE WOULD NOT COME UP AFTER TAKEOFF. RIGGED MLG GROUND SHIFT SENSOR CABLE ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FLOOR TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED CTR FLOOR TRACK LIGHTING BATTERY PACK AND POWER SUPPLY, OPS CHECK GOOD PER BOEING MM.

Part: ENGINE — FOD (NR 2)

ON TAKEOFF ROLL, PLASTIC BAG REPORTED INGESTED INTO NR 2 ENG. BEGAN ABORTED T/O AT 30 KTS INTO 20 KT HW. PERFORMED BIRD STRIKE INSPECTION PER BOEING MM. NO DAMAGED NOTED. INSPECTED NR 2 ENGINE FOR FOD, NONE FOUND AND NO DAMAGE.