N602SW

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 68,299 hrs · 54,482 cycles

LEFT WING NR 3 SPOILER UPPER SKIN DELAMINATED. R & R SPOILER IAW MM.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 68,299 hrs · 54,482 cycles

RIGHT WING NR 6 SPOILER UPPER SKIN DELAMINATED. R & R NR 6 FLIGHT SPOILER IAW AMM.

Part: CIRCUIT CARD — FAULTY (LANDING GEAR) · airframe 64,660 hrs · 51,308 cycles

AIR TURNBACK AFTER LANDING GEAR RETRACT WHEN POSITIONING GEAR TO OFF, RT RED AND GREEN LIGHTS REMAINED ILLUMINATED GEAR EXTENDED NORMALLY. R & R RT GEAR UP AND LOCK CARD M982 IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,789 hrs · 54,153 cycles

FORWARD EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 67,789 hrs · 54,153 cycles

LT EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2. SECURED LENS IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 67,789 hrs · 54,153 cycles

RIGHT EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 2. SECURED LENS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,788 hrs · 54,152 cycles

LEFT EMERGENCY AISLE LIGHT INOPERATIVE AT ROW 2. R & R LIGHT IAW AMM.

Part: CONNECTOR — MISSING (EMERGENCY LIGHT) · airframe 67,788 hrs · 54,152 cycles

AFT LAVATORY EXIT LIGHT CONNECTOR MISSING. REPLACED THE CONNECTOR IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 67,788 hrs · 54,152 cycles

R2 DOOR EMERGENCY EXIT SIGN DAMAGED. R & R LIGHT ASSY IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 67,788 hrs · 54,152 cycles

AFT LAV WALL EXIT LIGHT DAMAGED. R & R LIGHT IAW AMM.

Part: ANGLE — CRACKED (RT WING) · airframe 67,788 hrs · 54,152 cycles

RT WING TRAILING EDGE FORWARD OF AILERON SECOND BAY FROM INBOARD SIDE, OUTBOARD COVE ANGLE CRACKED. R & R THE ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 67,788 hrs · 54,152 cycles

FORWARD CARGO AFT FRAME LOWER DOOR FITTING CRACKED AT BS 492. R & R THE FITTING IAW SRM & DWG.

Part: BRACKET — CRACKED (LT WING) · airframe 67,788 hrs · 54,152 cycles

LEFT WING UPPER REAR SPAR BRACKET CRACKED AT RSS. 235. REPAIRED THE BRACKET IAW DWG AND SRM.

Part: TIE — CRACKED (FUSELAGE) · airframe 67,788 hrs · 54,152 cycles

STRINGER TIE CRACKED AT BS 986, STR 19R. R & R STRINGER TIE IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (LT WING) · airframe 67,788 hrs · 54,152 cycles

LEFT WING LOWER CHORD AFT FASTENER HOLE CRACKED AT RSS 226.64. REPAIRED CHORD IAW ER AND EA.

Part: SKIN — CRACKED (LT WING) · airframe 67,788 hrs · 54,152 cycles

LEFT WING TRAILING EDGE OF UPPER SKIN CRACKED BETWEEN RSS. 239.1 TO RSS. 255.1. REPAIRED SKIN IAW ER AND EA.

Part: STRUCTURE — CRACKED (RT WING) · airframe 67,788 hrs · 54,152 cycles

RIGHT WING LOWER CHORD CRACKED AT AFT FASTENER HOLE AT RSS 226.04. REPAIRED CHORD IAW ER & EA.

Part: FITTING — CRACKED (LT WING) · airframe 67,788 hrs · 54,152 cycles

LEFT WING FORWARD BEAM FITTING CRACKED AT RSS. 221.64, COMMON TO WEB. REPAIRED THE FITTING IAW ER AND EA.

Part: SKIN — CRACKED (RT WING) · airframe 67,788 hrs · 54,152 cycles

RIGHT WING UPPER SKIN TRAILING EDGE CRACKED BETWEEN RSS. 254.94 TO 268.84. REPAIRED SKIN IAW ER AND EA.

Part: FITTING — CRACKED (LT WING) · airframe 67,788 hrs · 54,152 cycles

LEFT WING AFT BEAM FITTING CRACKED AT RSS. 224.14, 7 O'CLOCK POSITION. REPAIRED THE FITTING IAW ER AND EA.

Part: SPAR — CRACKED (LT WING) · airframe 67,788 hrs · 54,152 cycles

LEFT WING REAR SPAR WEB CRACKED BETWEEN RSS 211 TO RSS 238. REPAIRED THE SPAR IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 67,788 hrs · 54,152 cycles

LEFT WING REAR SPAR CRACKED. REPAIRED THE SPAR IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 67,788 hrs · 54,152 cycles

RIGHT WING REAR SPAR CRACKED AT RSS 285. REPAIRED THE SPAR IAW EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 67,788 hrs · 54,152 cycles

FORWARD ENTRY DOOR LOWER AFT CORNER BEAR STRAP CRACKED AT BS 339.5 TO BS 347.5, STR 17L. REPAIRED BEAR STRAP IAW SRM.

Part: FITTING — CRACKED (RT WING MLG) · airframe 67,788 hrs · 54,152 cycles

RIGHT WING AFT MAIN LANDING GEAR FITTING CRACKED. REPAIRED THE FITTING IAW ER AND EA.

Part: SPAR — CRACKED (RT WING) · airframe 67,788 hrs · 54,152 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 211 TO 238. REPAIRED THE SPAR IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,788 hrs · 54,152 cycles

L1 DOOR CUTOUT LOWER AFT CORNER FUSELAGE SKIN CRACKED AT BS 342.5, STR 17L. REPAIRED SKIN IAW SRM.

Part: STRAP — CRACKED (L1 DOOR) · airframe 67,788 hrs · 54,152 cycles

L1 DOOR FORWARD HINGE CUTOUT H-STRAP CRACKED AT BS 303, STR 10L, LOWER AFT RADIUS. REPAIRED H-STRAP IAW AMM.

Part: FRAME — CRACKED (BS 348) · airframe 67,788 hrs · 54,152 cycles

FRAME CRACKED AT BS 348.2, STRINGER 16L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,788 hrs · 54,152 cycles

FRAME CRACKED AT BS 492, BETWEEN STR 17R TO STR 26R. R & R FRAME IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 67,788 hrs · 54,152 cycles

FLOORBEAM CORRODED AT BS 986.5, RBL 24.75-45.5. REPAIRED THE FLOORBEAM IAW SRM AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,788 hrs · 54,152 cycles

INTERCOSTAL OUTER CHORD CRACKED AT BS 291.5, BETWEEN STR 10R TO STR 11R. R & R INTERCOSTAL IAW ER AND EA.

Part: LENS — LOOSE (CABIN) · airframe 67,399 hrs · 53,903 cycles

RIGHT OVERWING EXIT LOWER EMER EXIT LIGHT LENS COVER LOOSE. SECURED LENS IAW EA.

Part: LENS — MISSING (CABIN) · airframe 67,069 hrs · 53,686 cycles

FORWARD SERVICE DOOR EMER LIGHT LENS MISSING. R & R LIGHT ASSEMBLY IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 66,962 hrs · 53,625 cycles

FORWARD ENTRY EMER EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: SIGN — MISSING (CABIN) · airframe 66,920 hrs · 53,601 cycles

L1 DOOR EMER EXIT SIGN MISSING. INSTALLED SIGN IAW MM.

Part: SPOILER — BROKEN (RT WING) · airframe 66,886 hrs · 53,577 cycles

NUMBER 5 GND SPOILER HINGE ATTACH POINT BROKEN. R & R SPOILER IAW MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 66,655 hrs · 53,432 cycles

L2 DOOR EMER EVAC SLIDE COVER OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: FAN — FAILED (CABIN) · airframe 66,287 hrs · 53,185 cycles

DIVERSION & DECLARED EMER, STRONG BURNING SMELL IN CABIN ROW 7 - 9. R & R RECIRC FAN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,981 hrs · 52,970 cycles

LEFT OVERWING EMER EXIT LIGHT ON LOWER SIDEWALL BULB INOPERATIVE. R & R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 65,981 hrs · 52,970 cycles

FORWARD LAVATORY EMER EXIT SIGN BULB INOPERATIVE. R & R BULB IAW AMM.

Part: CASTING — SHEARED (RT SPOILER) · airframe 65,932 hrs · 52,936 cycles

RIGHT WING INBD GND SPOILER CASTING SHEARED AT FWD ATTACH FITTING. R & R CASTING IAW SRM.

Part: ROLLER — DAMAGED (LE SLAT) · airframe 65,634 hrs · 52,716 cycles

DIVERSION & DECLARED EMER, LE FLAPS TRANSIT LIGHT ILLUMINATED ON TAKEOFF. FOUND NR 4 SLAT, INBD AUXILIARY TRACK ROLLER DAMAGED, CAUSING RESTRICTED MOVEMENT OF NR 4 SLAT. R & R ROLLER IAW MM.

Part: ENGINE — FAILED (LEFT) · airframe 64,659 hrs · 52,026 cycles

INFLIGHT SHUTDOWN & DECLARED EMER. NR 1 ENG FAILED AT 3000 AGL. PROCEEDED BY COMPRESSOR STALL ROLLED BACK. AFTER SHUTDOWN RED LIGHT EGT 950 DEGREE, COOLED IMMEDIATELY. R & R NR 1 ENG IAW MT.

Part: SKIN — CRACKED (L1 DOOR) · airframe 64,234 hrs · 51,739 cycles

L1 DOOR CRACKED AT LOWER HINGE BOX INTERIOR SKIN & VERTICAL FRAME. REPAIRED SKIN IAW EA.

Part: COVER — CRACKED (CABIN) · airframe 64,169 hrs · 51,689 cycles

L1 EMER EXIT LIGHT COVER CRACKED. R & R COVER IAW SIP.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 64,142 hrs · 51,669 cycles

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

Part: ACCESS PANEL — LEAKING (RT WING) · airframe 63,307 hrs · 51,106 cycles

DIVERSION, FLUID LEAK AT RT WING ACCESS PANEL DURING FLIGHT. R & R FULL PANEL 8817R IAW MM.

Part: REGULATOR — FAULTY (BLEED AIR SYS) · airframe 62,966 hrs · 50,864 cycles

AIR TURN BACK DURING CLIMB NR 1 ENG BLEED 0 PSI. PRESS WOULD NOT RETURN. R & R BLEED AIR REGULATOR IAW MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,488 hrs · 50,515 cycles

STRAP CRACKED AT BS 344 RBL 40. REPAIRED STRAP IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,432 hrs · 50,471 cycles

L1 DOOR EMER EXIT LIGHT INOPERATIVE. REPAIRED BULB IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

FRAME AUXILIARY & OTBD CHORD CRACKED AT BS 727 STRINGER 18A RT AT LOWER FWD HOLE. R & R CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

FRAME AUXILIARY & OTBD CHORD CRACKED AT BS 727 STRINGER 18A LT FWD LOWER HOLE. R & R CHORD IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 62,432 hrs · 50,471 cycles

LEFT WING OTBD AFT FLAP DELAMINATED. REPAIR AFT FLAP IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

AFT CARGO FLOOR SUPPORT CHANNEL CORRODED AT BS 727C+6.5 RBL 3.0. REPAIRED ANGLE IAW SRM & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

AFT PIT FLOOR SUPPORT CHANNEL ANGLE CORRODED AT BS 772 RBL 13. REPAIRED ANGLE IAW SRM & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

AFT PIT FLOOR SUPPORT CHANNEL ANGLE CORRODED AT BS 772 LBL 8.0. REPAIRED ANGLE IAW SRM & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

AFT PIT FLOOR SUPPORT CHANNEL ANGLE CORRODED AT BS 772 LBL 3. REPAIRED ANGLE IAW EA & SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

AFT PIT FLOOR SUPPORT CHANNEL ANGLE CORRODED AT BS 772 RBL 8.0. REPAIRED ANGLE IAW SRM & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

AFT PIT FLOOR SUPPORT CHANNEL ANGLE CORRODED AT BS 772 RBL 3.0. REPAIRED ANGLE IAW SRM & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

AFT PIT FRAME SHEAR TIE CORRODED AT BS 727C BETWEEN STRINGER 26L TO 26R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

SHEAR TIE ANGLE CORRODED AT BS 727D STRINGER 27R. REPAIRED ANGLE IAW SRM & DWG.

Part: FAIRING — DELAMINATED (LT WING) · airframe 62,432 hrs · 50,471 cycles

LEFT WING OUTER TAB FAIRING DELAMINATED ON UPPER SURFACE. REPAIRED FAIRING IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

SHEAR TIE ANGLE CORRODED AT BS 727E STRINGER 27L. R & R ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

AFT CARGO FLOOR SUPPORT ANGLE CORRODED BETWEEN BS 727D TO 727E STRINGER 27R. REPAIRED ANGLE IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

FRAME SHEAR TIE CORRODED AT BS 727E STRINGER 26R. REPAIRED SHEAR TIE IAW SRM.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

AFT PRESS BULKHEAD CHANNEL STIFFENERS CORRODED AT BS 1016 WL 208. REPAIRED STIFFENER IAW EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

SPLICE CHANNEL CRACKED AT BS 360 STRINGER 15L. R & R CHANNEL IAW SRM & DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

STRINGER SPLICE CRACKED AT BS 907 STRINGER 18L. R & R SPLICE IAW SRM & DWG.

Part: WEB — CRACKED (NLG WW) · airframe 62,432 hrs · 50,471 cycles

NOSE LANDING GEAR WW WEB LT SIDE PANEL CRACKED AT BS 259. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 663 TO 668 RBL 24.5. REPAIRED CHORD IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

INTERCOSTAL STRAP CRACKED AT BETWEEN BS 348 TO 351 STRINGER 16L. R & R INTERCOSTAL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

L1 DOOR ENTRY AREA UNDER FLOOR SUPPORT CORRODED AT BS 328 LBL 28. REPAIRED SUPPORT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

FRAME AUXILIARY & OTBD CHORD CRACKED AT BS 727 STRINGER 18A RT LOWER FWD HOLE. R & R CHORD IAW EA.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 62,432 hrs · 50,471 cycles

R1 EMER EXIT DOOR FRAME CRACKED AT LOWER FWD EDGE WEB. REPAIRED FRAME IAW SRM.

Part: ATTACH BRACKET — CRACKED (LE SLAT) · airframe 62,432 hrs · 50,471 cycles

RIGHT WING NR 6 SLAT INBD MAIN TRACK COVER PLATE ATTACHING BRACKET CRACKED. R & R BRACKET IAW DWG.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 62,432 hrs · 50,471 cycles

C2 DOOR CROSSBEAM WEB CRACKED AT LOWER FASTENER. R & R C2 DOOR IAW MM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 62,432 hrs · 50,471 cycles

MAIN CABIN PRESS DECK BEADED WEB PANEL OVER MAIN WW CRACKED AT BS 673 LBL 42.50. REPAIRED WEB IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 62,432 hrs · 50,471 cycles

OUTBOARD CHORD CRACKED AT BS 727 STRINGER 18A LT FWD LOWER HOLE. R & R CHORD IAW EA.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 62,148 hrs · 50,273 cycles

R2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: SIGN — LOOSE (CABIN) · airframe 61,449 hrs · 49,779 cycles

FORWARD ENTRY DOOR LOWER EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,021 hrs · 49,501 cycles

RT WING OTBD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: FLAP — OUT OF POSITION (EVAC SLIDE) · airframe 60,672 hrs · 49,272 cycles

R2 DOOR SLIDE LOWER FLAP OUT OF POSITION. REPOSITIONED R2 DOOR SLIDE LOWER FLAP IAW MT.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 58,042 hrs · 47,324 cycles

MID CABIN EMERGENCY CABIN LIGHT INOP. REMOVED EMERGENCY CABIN LIGHT AND ACCESSED BATTERY PACK IAW SRM 51-40-02. REMOVED AND REPLACED BATTERY PACK HOUSING STA 603 LT. RE-INSTALLED EMERGENCY CABIN LIGHT IAW AMM TASK 33-51-51-962-016, OP CHECK GOOD.

Part: WIRE — BROKEN (RT MLG) · airframe 58,042 hrs · 47,324 cycles

AIR TURNBACK ON TAKEOFF, INITIAL CLIMB, LANDING GEAR LEVER WAS RAISED TO THE UP POSITION. ALL GREEN LIGHTS EXTINGUISHED, BUT THE RT MAIN GEAR RED LIGHT REMAINED ILLUMINATED. R & R WIRE IAW AMM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 727 PRODUCTION SPLICE STA 13 HAS CRACKED AT HOLE NR 4. REMOVED AND REPLACED SPLICE IAW BAC DWG.

Part: DOUBLER — PUNCTURED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

STA 278 I/B OF STR 2R INTERNAL DOUBLER HAS 1EA O/S HOLE. REPAIRED O/S HOLE AT STA 278 I/B OF STR 2R IN INTERNAL DOUBLER IAW REO G15826 REV IR AND EA 1-353-21488 REV - .

Part: DOUBLER — PUNCTURED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

STA 266 TO STA 271 I/B OF STR 2R, INTERNAL DOUBLER HAS 2EA O/S HOLES. REPAIRED O/S HOLES AT STA 266 TO 271 I/B OF STR 2R IAW REO G15826 REV IR AND EA 1-353-21488 REV - .

Part: DOUBLER — PUNCTURED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

STA 266 O/B OF STR 2L INTERNAL DOUBLER HAS 1EA O/S HOLE. REPAIRED O/S HOLE AT STA 266 O/B OF STR 2L IN INTERNAL DOUBLER IAW REO G15826 REV IR AND EA 1-353-21488 REV - . FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: DOUBLER — PUNCTURED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

STA 286 TO STA 281 I/B OF STR 2L, INTERNAL DOUBLER HAS 3EA O/S HOLES. REPAIRED IAW REO G15826 REV IR AND EA 1-353-21488 REV - AT STA 286 TO STA 281 I/B OF STR 2L. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

LEFT BS 400+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 3. REPAIRED LEFT BS 400 +10 UPPER 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 58,037 hrs · 47,322 cycles

LEFT BS 500B+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 4, 5. REPAIRED LEFT BS 500B +10 LOWER AFT WINDOW CORNER IAW EA 1-353-21438 REV - , REO G15806 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

LEFT BS 380+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4, 6. REPAIRED LEFT BS 380 +10 UPPER 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 58,037 hrs · 47,322 cycles

LEFT BS 460+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 8. REPAIRED LEFT BS 460 +10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21454 REV -, REO G15822 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

LEFT BS 460+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED LEFT BS 460 +10 LOWER AFT WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2 SECT 3.B.3 PER TASK CARD 10072, R3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

LEFT BS 440+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 4, 5. REPAIRED LEFT BS 440 +10 UPPER 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 58,037 hrs · 47,322 cycles

LEFT BS 500B+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 5, 6, 8. REPAIRED LEFT BS 500B +10 UPPER FORWARD WINDOW CORNER IAW SB 737-53-1306 R2 SEC 3.B.3 AS PER TASK CARD 10072, STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

LEFT BS 520+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 4, 5, 6. REPAIRED LEFT BS 520 +10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21422 REV - , REO G15811 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

LEFT BS 807+10 LOWER WINDOW SKIN CUTOUT CRACKED. REPAIRED SKIN IAW BOEING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

LEFT BS 787+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED LEFT BS 787+10 LOWER FORWARD WINDOW CORNER IAW BOEING SB737-53-1306 REV 2 AND TASK CARD 10075 STEP 8 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 500A+10 LOWER WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 7. REPAIRED SKIN IAW BOEING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RT BS 360+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 4, 5, 7, 8. REPAIRED RT BS360+10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21493 REV1, REO G15810 REV A FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 440+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 4, 5, 6. REPAIRED RIGHT BS 440+10 UPPER FORWARD WINDOW CORNER IAW BOEING S/B737-53-1306 REV 2 SECT 3.B.3, PER TASK CARD 10073 REV 3 STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 520+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 6, 7, 8. REPAIRED RIGHT BS 520 +10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21470 REV - , REO G15809 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

LEFT BS 727+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 4 ,5, 6, 7. REPAIRED LEFT BS 727 +10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21434 REV - , REO G15815 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 887+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 7. REPAIRED RIGHT BS 887 +10 UPPER AFT WINDOW CORNER IAW EA 1-353-21426 REV - , REO G15812 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

LEFT BS 747+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE 7. REPAIRED LEFT BS 747+10 UPPER AFT WINDOW CORNER IAW EA 1-353-21433 REV-, REO G15817 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 4. REPAIRED WINDOW CORNER RIGHT BS 867 +10 UPPER AFT IAW SB 737-53-1306 REV 2 AND TASK CARD 10074. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

LEFT BS 767+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2. REPAIRED LEFT BS 767+10 UPPER AFT WINDOW CORNER IAW BOEING SB737-53-1306 REV 2 AND TASK CARD 10075 STEP 8 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 460+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 4, 5, 7. REPAIRED RIGHT BS 460 +10 LOWER AFT WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2 SECT 3.B.3 PER TASK CARD 10073, STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 827+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 5, 6, 7. REPAIRED WINDOW CORNER RIGHT BS 827+10 UPPER AFT IAW SB 737-53-1306 REV 2 AND TASK CARD 10074 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

LEFT BS 807+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 8. REPAIRED LEFT BS 807 +10 UPPER AFT WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2 SECT 3B3, PER TASK CARD 10075 REV 3 STEP 8. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

LEFT BS 767+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 5, 10. REPAIRED LEFT BS 767+10 LOWER FORWARD WINDOW CORNER IAW BOEING SB737-53-1306 REV 2 AND TASK CARD 10075 STEP 8 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 767+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4. REPAIRED RIGHT BS 767 +10 UPPER AFT WINDOW CORNER IAW BOEING SB 737-53-1306, REV 2, SECTION 3.B.3 AS PER TASK CARD 10074, FIGURE 9.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 500A+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4. REPAIRED RIGHT BS 500A +10 UPPER FORWARD WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2 SECT 3.B.3 PER TASK CARD 10073, STEP 8. FACT AS A RESULT OF POST REPAIR I

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 360+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4, 5, 6. REPAIRED RIGHT BS 360 +10 LOWER AFT WINDOW CORNER IAW EA 1-353-21476 REV - , REO G15808 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 480+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED RIGHT BS 480 +10 LOWER AFT WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2 SECT 3.B.3 PER TASK CARD 10073, STEP 8. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

LEFT BS 727B+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 11. REPAIRED LEFT BS 727B +10 UPPER AFT WINDOW CORNER IAW EA 1-353-21437 REV - , REO G15816 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 500B+10 LOWER WINDOW SKIN CUTOUT CRACKED AT HOLES 3, 5, 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,037 hrs · 47,322 cycles

RIGHT BS 500B+10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 6. REPAIRED RIGHT BS 500B +10 UPPER FORWARD WINDOW CORNER IAW SB 737-53-1306 R2 SECT 3.B.3 AND EA 1-353-21447 REV - , REO G15823 REV IR. FACT AS A RESULT OF POST

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,992 hrs · 47,292 cycles

AT BS 727 +3" STRINGER 4R IS CRACKED DUE TO INCOMING REPAIR DOUBLER. COMPLIED WITH EA 1-353-21368 REV - & REO G15805 REV IR AT S4R STA 727D - 747.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,029 hrs · 46,580 cycles

LONGITUDINAL FLOORBEAM O/B WEB CRACKED AT BS 707, RBL 24.5. REPAIRED WEB IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,029 hrs · 46,580 cycles

LONGITUDINAL FLOORBEAM O/B WEB CRACKED AT BS 713, BBL 0.07. REPAIRED WEB IAW SRM AND SI.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,029 hrs · 46,580 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 665, RBL 24.5. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,029 hrs · 46,580 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, RBL 24.5. REPAIRED WEB PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,029 hrs · 46,580 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 709, RBL 24.5. REPAIRED WEB PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,029 hrs · 46,580 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 669, RBL 24.5. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,029 hrs · 46,580 cycles

FUSELAGE SKIN CRACKED AT L2 DOOR FWD LOWER CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,856 hrs · 46,447 cycles

FUSELAGE SKIN CRACKED AT BS 727D+9, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,856 hrs · 46,447 cycles

FUSELAGE SKIN CRACKED AT BS 500B+12, STR 7R. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,856 hrs · 46,447 cycles

FUSELAGE SKIN CRACKED AT BS 500A+7, STR 2R. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,856 hrs · 46,447 cycles

SKIN CRACKED AT BS 500B+12, STR 1L. REPAIRED SKIN IAW AAR EA AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,856 hrs · 46,447 cycles

FUSELAGE SKIN CRACKED AT BS 867+ 13, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,856 hrs · 46,447 cycles

SKIN CRACKED AT BS 500A +7, STR 2R. REPAIRED SKIN IAW AAR EA AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,803 hrs · 46,406 cycles

RIGHT SIDE EMERGENCY EXIT LIGHT INOP AT ROW 3. RELAMPED LIGHT PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 56,363 hrs · 46,058 cycles

LEFT FWD CEILING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 56,363 hrs · 46,058 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 54,837 hrs · 44,920 cycles

DURING SCHEDULED OTS CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FOREFLAP IAW MM.

Part: SLIDE — OUT OF LIMITS (L1 DOOR) · airframe 54,577 hrs · 44,716 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,866 hrs · 44,190 cycles

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

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 53,660 hrs · 44,031 cycles

DURING SCHEDULED OTS CHECK, FOUND LT MLG WHEEL WELL PRESSURE DECK WEB CRACKED AT BS 670, LBL 35. REPAIRED WEB PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,059 hrs · 43,595 cycles

DURING SCHEDULED MV2 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,059 hrs · 43,595 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,059 hrs · 43,595 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 420+6, STR 4L. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,020 hrs · 42,800 cycles

DURING SCHEDULED MV3 CHECK, FOUND FWD ENTRY EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,020 hrs · 42,800 cycles

DURING SCHEDULED MV3 CHECK, FOUND FWD ENTRY EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: ANGLE — CORRODED (NLG WW) · airframe 51,677 hrs · 42,537 cycles

SUPPLEMENTAL INFORMATION - DURING SCHEDULED 16Y CHECK, FOUND NOSE WHEEL WELL ANGLE CORRODED AT BS 244, RBL 17. REPAIRED ANGLE PER EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 907, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 211.8, STR 8R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 616, STR 17L. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 981, STR 7L. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727B, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 947.5, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 670, LBL 24.5. REPAIRED BEAM PER EA.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT AFT LOWER CORNER. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 847, STR 21R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 328, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 673, LBL 24.5. REPAIRED BEAM PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 520 TO BS 540, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN PER EA.

Part: ANGLE — CORRODED (NLG WW) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND NOSE WHEEL WELL ANGLE CORRODED AT BS 244, RBL 7. REPAIRED ANGLE PER EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT SKIN DELAMINATED. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL ANGLE CRACKED AT BS 692, LBL 24.75. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED BETWEEN BS 277 TO BS 294.5, STR 14R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 767, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 7 TO LBL 45.5. REPAIRED BEAM PER SRM.

Part: WEB — CRACKED (CARGO BAY) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPARTMENT WEB CRACKED BETWEEN BS 500A TO BS 500B, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CHANNEL CORRODED AT BS 430, STR 18R. REMOVED AND REPLACED STRINGER CHANNEL PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (LE SLAT) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 SLAT SUPPORT ANGLE CRACKED ON L/E AREA LOWER SURFACE. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WEB CORRODED BETWEEN BS 947.5 TO BS 967. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (BS 772) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, RBL 8.10. REPAIRED CHANNEL PER EA AND SRM.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED BETWEEN BS 294.5 TO BS 303.9, STR 16L. REMOVED AND REPLACED ANGLE PER SRM.

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 3. REPAIRED CHANNEL PER EA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ZEE CRACKED AT BS 734C, STR 25R. REMOVED AND REPLACED ZEE PER SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 SLAT SKIN DELAMINATED. REPAIRED SKIN PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL ANGLE CRACKED AT BS 692, RBL 24.75. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT SKIN DELAMINATED. REPAIRED SKIN PER SRM.

Part: BOLT — CORRODED (GIRT BAR) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLATE ATTACH BOLTS CORRODED. REMOVED AND REPLACED ATTACH ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 807, BETWEEN STR 27R TO STR 21L. REPAIRED FRAME PER SRM AND BAC DWG.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING FORE FLAP LOWER SKIN I/B DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME FLANGE CRACKED AT BS 520, STR 22L. REPAIRED FLANGE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 1114 TO BS 1125. REMOVED AND REPLACED STRINGER PER SRM AND BAC DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME ANGLE CRACKED AT BS 947.5, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED ANGLE PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR WEB CRACKED AT BS 246, RBL 24. REPAIRED WEB PER ACO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 947.5, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 336, STR 20L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 640, STR 15L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 1100, STR 20R. REPAIRED SKIN PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,677 hrs · 42,537 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,138 hrs · 46,665 cycles

FUSELAGE WINDSHIELD SKIN UPPER CORNER OF CUTOUT CRACKED AT BS 211.8, STR 8R. REPAIRED SKIN IAW EO AND SRM.

Part: HINGE FITTING — BROKEN (SPOILER) · airframe 51,016 hrs · 42,019 cycles

DURING SCHEDULED CV CHECK, FOUND LT WING NR 4 GROUND SPOILER O/B HINGE LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 50,131 hrs · 41,375 cycles

FWD ENTRY EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,644 hrs · 41,005 cycles

RT OVERWING EMERGENCY EXIT BULLNOSE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,579 hrs · 40,216 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT AFT BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,579 hrs · 40,216 cycles

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

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 48,578 hrs · 40,215 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: STRIP — DAMAGED (CABIN) · airframe 46,901 hrs · 38,979 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP DAMAGED BETWEEN ROW 3 TO ROW 5. INSTALLED STRIP PER MM.

Part: STRIP — MISSING (CABIN) · airframe 46,901 hrs · 38,979 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP MISSING AT ROW 8. INSTALLED STRIP PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 46,901 hrs · 38,979 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: STRIP — DAMAGED (CABIN) · airframe 46,901 hrs · 38,979 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP DAMAGED BETWEEN ROW 8 TO ROW 10. INSTALLED STRIP PER MM.

Part: STRIP — DAMAGED (CABIN) · airframe 46,901 hrs · 38,979 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP DAMAGED BETWEEN ROW 5 TO ROW 7. INSTALLED STRIP PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 3 L/E SLAT I/B UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT CREASE BEAM WEB BETWEEN BS 727D TO 727E CORRODED. REMOVED AND REPLACED WEB PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 2 L/E SLAT I/B UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING NR 5 L/E SLAT O/B ARM CRACKED. REMOVED AND REPLACED SLAT PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING I/B AFT FLAP O/B LOWER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME WEB CRACKED AT BS 303, STR 16L. REPAIRED WEB PER ACO.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 500C TO BS 500B. REMOVED AND REPLACED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 847 TO BS 867. REMOVED AND REPLACED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420. REMOVED AND REPLACED BEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CRACKED AT BS 787, LBL 9. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 2 L/E SLAT O/B UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM CRACKED AT BS 312, RBL 25. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO BAY, SHEAR TIE HORIZONTAL FLANGE CRACKED AT BS 787, BETWEEN LBL 7 TO LBL 11. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 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 46,626 hrs · 38,791 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,626 hrs · 38,791 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 46,269 hrs · 38,552 cycles

R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: COVER — LOOSE (CABIN) · airframe 45,781 hrs · 38,195 cycles

DURING SCHEDULED MV1 CHECK, FWD EMERGENCY EXIT LIGHT LENS COVER FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 44,972 hrs · 37,613 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,601 hrs · 36,592 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 43,601 hrs · 36,592 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CASTING — CRACKED (NR 4 SPOILER) · airframe 43,601 hrs · 36,592 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING NR 4 SPOILER OUTBOARD CASTING CRACKED. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: LENS — CRACKED (CABIN) · airframe 43,601 hrs · 36,592 cycles

DURING SCHEDULED HC1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 7 DEF. REMOVED AND REPLACED LENS PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 43,521 hrs · 36,531 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 4 DOOR STOP. REPAIRED FRAME PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 42,012 hrs · 35,350 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING OUTBOARD T/E FLAP DELAMINATED INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 40,198 hrs · 33,946 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND BROKEN WIRE AT LIGHT ASSY. REPAIRED BROKEN WIRE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 39,219 hrs · 33,178 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 39,203 hrs · 33,159 cycles

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

Part: FRAME — CORRODED (BS 807 S26L) · airframe 39,196 hrs · 33,152 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 26L. REPAIRED FRAME SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 39,196 hrs · 33,152 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 4 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER ACO.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 39,194 hrs · 33,151 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN INOP. REPAIRED BROKEN WIRE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,100 hrs · 33,083 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 38,380 hrs · 32,523 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,380 hrs · 32,523 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT FWD ENTRY DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 38,145 hrs · 32,348 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. SECURED LIGHT ASSY CONNECTOR PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 37,498 hrs · 31,852 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 35,469 hrs · 30,248 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 35,469 hrs · 30,248 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FAN — FAULTY (COCKPIT) · airframe 34,006 hrs · 29,055 cycles

ELECTRICAL ODOR IN CABIN WHEN RECIRCULATING FAN ON. ODOR DISPENSES WHEN TURNED OFF. REMOVED AND REPLACED FAN PER MM.

Part: BOTTLE — DISCHARGED (R2 DOOR SLIDE) · airframe 33,821 hrs · 28,916 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED R2 DOOR SLIDE PER MM.

Part: SLIDE — DISLODGED (L2 DOOR) · airframe 33,821 hrs · 28,916 cycles

L2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED L2 DOOR SLIDE PER MM.

Part: B-NUT — LOOSE (NR 1 HYD SYSTEM) · airframe 33,604 hrs · 28,742 cycles

A-SYSTEM HYDRAULICS FAILED. RECONNECTED NR 1 ENGINE HYDRAULIC SUPPLY LINE B-NUT PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND 4 EACH SHEAR TIES BETWEEN BS 727D AND BS 787, FROM LBL 11 TO RBL 14, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500B, BETWEEN STRINGERS 27L AND 28R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 33,542 hrs · 28,961 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL STABILIZER PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT RIGHT BS 616, CRACKED. REPAIRED FLOORBEAM CHORD PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500, STRINGER 28R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH LONGITUDINAL FLOORBEAMS CRACKED AT BS 727A +18, BETWEEN RBL 23 AND RBL 48. REPAIRED FLOORBEAMS PER ER.

Part: WEB — CRACKED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORWEB AT BS 178, LBL 24, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 767, BETWEEN RBL 8 AND RBL 12, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 1006, LBL 1, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500A, STRINGER 16R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 907, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 360, STRINGER 5L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EACH SHEAR TIES CORRODED BETWEEN BS 727E AND BS 787, LBL 18 AND RBL 9. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME SECTION AT BS 400, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EACH FRAMES CRACKED BETWEEN BS 827 AND BS 907, STRINGER 8L. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH FLOORBEAMS CRACKED AND CORRODED BETWEEN BS 947 AND BS 986, LBL 53 AND RBL 48. REMOVED AND REPLACED FLOORBEAM SECTIONS PER ER.

Part: SHEAR TIE — CORRODED (BS 727C) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED IN AFT CARGO COMPARTMENT, BS 727C, RBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 727B TO BS 727D, RBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 941, RBL 56, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT FRAME AT BS 500A, BETWEEN STRINGERS 28L AND 28R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,452 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT FRAME AT BS 520, BETWEEN STRINGERS 27L AND 28L, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM ZEE CHORD AT BS 270, BETWEEN LBL 11 AND RBL 11, CORRODED. REMOVED AND REPLACED ZEE CHORD PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT FRAME AT BS 500C, BETWEEN STRINGERS 27R AND 28L, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: ATTACH FITTING — CRACKED (LT WING SLAT) · airframe 33,542 hrs · 28,691 cycles

DURING SCHEDULED D-CHECK, FOUND LT WING L/E NR 3 SLAT ACTUATOR ATTACH FITTING CRACKED. REPAIRED SLAT FITTING PER SRM.

Part: FIRE DETECTOR — FAULTY (AFT CARGO BAY) · airframe 33,395 hrs · 28,575 cycles

DIVERSION/DECLARED EMERGENCY, AFT CARGO COMPARTMENT FIRE INDICATION IN FLIGHT, QRH PROCEDURES FOLLWED. REMOVED AND REPLACED CARGO FIRE DETECTORS, METERING VALVE, DIVERTER VALVE, CARGO FIRE CONTROL PANEL PER MM.

Part: SLIDE — OUT OF LIMITS (FWD SVC DOOR) · airframe 27,942 hrs · 24,087 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (AFT CABIN DOORS) · airframe 28,981 hrs · 25,063 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 28,845 hrs · 24,959 cycles

FWD ENTRY DOOR EMERGENCY EXIT EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 27,643 hrs · 23,931 cycles

EEPLS STRIP LOOSE IN CABIN. SECURED EEPLS PER MM.

Part: LENS — BROKEN (CABIN FLOOR) · airframe 26,822 hrs · 23,292 cycles

EELPS LENS BROKEN AT FWD ENTRY AREA. REMOVED AND REPLACED LENS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 26,244 hrs · 22,814 cycles

DURING SCHEDULED C2 CHECK, FOUND LT INBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT INBD AFT T/E FLAP PER MM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 25,199 hrs · 22,000 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT ELEVATOR TAB DELAMINATED ON UPPER SKIN AT NR 1 HINGE CUT OUT. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 24,296 hrs · 21,263 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. RE INSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,524 hrs · 20,623 cycles

DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM SKIN CRACKED ON BOTH LT AND RT SIDES AT BS 705. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 23,457 hrs · 20,566 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, WL 177 AND LBL 5.7. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,457 hrs · 20,566 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT SIDE CHORD CRACKED AT BS 178, WL 207 AND RBL 24.0. REMOVED AND REPLACED SIDE CHORD PER SWA ACO.

Part: TAB — DELAMINATED (ELEVATOR) · airframe 23,457 hrs · 20,566 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND LT ELEVATOR TAB DELAMINATED ON TOP T/E. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,453 hrs · 20,560 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, LBL 5.0, WL 201 AND WL 199. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,453 hrs · 20,560 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED .50 INCH LONG AT BS 178, RBL 17.1 AND WL 227. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM.

Part: LIGHT — INOPERATIVE (ENTRY DOOR) · airframe 23,446 hrs · 20,552 cycles

DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LENS — MISSING (CABIN) · airframe 21,546 hrs · 18,993 cycles

EMERGENCY EXIT LIGHT NEAR FWD ENTRY DOOR MISSING LENS. INSTALLED LENS PER MM.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 20,813 hrs · 18,359 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 20,646 hrs · 18,214 cycles

EMERGENCY EXIT LIGHT LENS LOOSE AT AFT CABIN. SECURED LENS PER MM.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 18,661 hrs · 16,649 cycles

ELECTRICAL ODOR FROM REAR COFFEEMAKERS. REMOVED AND REPLACED AFT GALLEY NR 2 COFFEEMAKER PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 5. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS LOOSE AND INOP AT ROWS 14, 18 AND 19. SECURED TRACK AND RECONNECTED LIGHTS PER MM.

Part: LENS — LOOSE (PASSENGER DOOR)

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY LIGHT LENS COMING LOOSE. RESECURED LENS PER MM.

Part: SLIDE — DETACHED (PASSENGER DOOR)

EMERGENCY EXIT SLIDE AT MAIN ENTRY DOOR CAME LOOSE FROM MOUNTING BRACKET. SECURED MOUNTING BRACKET AND REPOSITIONED SLIDE ASSY PER MM.

Part: COVER — LOOSE (CABIN)

EMERGENCY FLOOR TRACK EGRESS LIGHT COVERS CAME LOOSE AT FWD SECTON. SECURED COVERS PER MM.

Part: LIGHT — INOPERATIVE (ROW 8, 18 & 20)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT FLOOR TRACK LIGHTS INOP AT ROWS 8, 18 AND 20. RELAMPED LIGHTS PER MM.

Part: WIRE — LOOSE (CABIN)

DURING PREFLIGHT, FOUND ROW 23 LEFT AFT 3 EMERGENCY FLOOR LIGHTS INOP. RESECURED LOOSE WIRING PER BOEING M/M.

Part: WIRE — LOOSE (CABIN)

DURING PREFLIGHT CHECK, FOUND CAPT SIDE EMERGENCY EXIT LIGHT RED LENS LOOSE AND EXPOSING WIRES. REPLACED LENS, RESECURED WIRING AND OP CHECKED PER BOEING MM.

Part: O-RING — FAILED (LT PITOT SYS)

AIR TURNBACK DUE TO ALTIM AND AIRSPEED CAPTAIN SIDE ERRONEOUS AFTER TAKEOFF. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED O-RING ON NR 1 AIR DATA PITOT LINE. OPS AND LEAK CK GOOD AS PER BOEING SRM.

Part: LAMP — FAILED (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND SEVERAL FWD CABIN EMERGENCY EXIT LIGHTS INOP. RELAMPED AND REPAIRED AS REQUIRED PER BOEING M/M.

Part: EEL WIRES — DISCONNECTED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND FLOOR TRACK LIGHTING FROM ROWS 19 THROUGH 21 INOP. RECONNECTED WIRE TERMINALS TO LIGHT ASSEMBLY PER BOEING MM.