N606SW

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 67,331 hrs · 53,507 cycles

LEFT WING OUTBD AFT T/E FLAP DELAMINATED. REPAIRED THE FLAP ASSY IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 66,876 hrs · 53,199 cycles

LT OUTBOARD SUPPORT BRACKET CRACKED FOR FORWARD STABILIZER TRIM DRUM UPPER LINK SUPPORT STRUCTURE. R&R BRACKET PER EA.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,876 hrs · 53,199 cycles

LEFT LOWER OVERWING EMERGENCY EXIT LIGHT BULB INOPERTIVE. R & R BULB IAW AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 66,876 hrs · 53,199 cycles

L2 DOOR SLIDE OUT OF POSITION. POSITIONED THE SLIDE IAW CNN.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 66,876 hrs · 53,199 cycles

FRAME SHEAR TIE CORRODED AT BS 787, BETWEEN STRINGERS 26 - 27R. R & R THE SHEAR TIE IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 66,876 hrs · 53,199 cycles

LEFT WING NR 1 PYLON SPRING DOOR ATTACH ANGLE CRACKED AT UPPER SPRING ATTACH POINT. R & R THE ATTACH ANGLE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,876 hrs · 53,199 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: DOOR SILL — CORRODED (BS 915-1006) · airframe 66,876 hrs · 53,199 cycles

R2 DOOR MOP SILL CORRODED BETWEEN BS 915 TO 1006. R & R DOOR SILL IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,876 hrs · 53,199 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 66,876 hrs · 53,199 cycles

LEFT WING UPPER TRAILING EDGE PANEL JUST OUTBOARD OF NR 1 PYLON ATTACH ANGLE CRACKED AT AFT END. R & R ANGLE IAW SRM.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 66,876 hrs · 53,199 cycles

AFT CARGO BAY ON FRAME TO STRINGER ATTACH CLIP CORRODED AT BS 767, STR 27L. R&R CLIP IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 66,876 hrs · 53,199 cycles

LEFT WING NR 1 PYLON INBOARD UPPER AFT PANEL ATTACH ANGLE CRACKED. R & R THE ATTACH ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING AILERON) · airframe 66,876 hrs · 53,199 cycles

LEFT WING RSS. 547 WIPER WEB SUPPORT ANGLE CRACKED ON INBOARD SIDE OF NR 2 AILERON HINGE SUPPORT FITTING. R & R THE ANGLE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,876 hrs · 53,199 cycles

FRAME CORRODED AT BS 500C, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 277) · airframe 66,876 hrs · 53,199 cycles

STRINGER CLIP 10R CRACKED AT BS 277. R & R STRINGER CLIP IAW ER AND EA.

Part: FRAME — CORRODED (BS 847) · airframe 66,876 hrs · 53,199 cycles

AFT CARGO BAY FRAME CORRODED AT BS 847, BETWEEN STRINGERS 28L TO 28R. REPAIRED THE FRAME IAW ER AND EA.

Part: FRAME — CORRODED (BS 747) · airframe 66,876 hrs · 53,199 cycles

AFT CARGO BAY ON FRAME CORRODED AT BS 747, BETWEEN STRINGERS 26 - 27R. REPAIRED THE FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (BS 807) · airframe 66,876 hrs · 53,199 cycles

SHEAR TIE CORRODED AT BS 807, BETWEEN STRINGERS 27L TO 27R. REPAIRED THE SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (BS 500B) · airframe 66,876 hrs · 53,199 cycles

FORWARD CARGO BAY SHEAR TIE CORRODED AT BS 500B, BETWEEN STRINGERS 28L TO 28R. / REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500D) · airframe 66,876 hrs · 53,199 cycles

FORWARD CARGO BAY FRAME CORRODED AT BS 500D, BETWEEN STRINGER 28L TO 28R. R & R THE SHEAR TIE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 66,876 hrs · 53,199 cycles

SHEAR TIE CORRODED AT BS 787, BETWEEN STRINGERS 26L TO 27L. R & R THE SHEAR TIE IAW SRM.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 66,876 hrs · 53,199 cycles

AFT CARGO BAY ON FRAME TO STRINGER ATTACH CLIP CORRODED AT BS 767, STR 27R. R&R CLIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,876 hrs · 53,199 cycles

AFT CARGO BAY ON FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: SUPPORT FITTING — CRACKED (RT WING AILERON) · airframe 66,876 hrs · 53,199 cycles

RIGHT WING NR 2 AILERON HINGE SUPPORT FITTING INBOARD LOWER TRAILING EDGE PANEL SUPPORT ANGLE ASSEMBLY CRACKED. R & R THE ASSEMBLY IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 66,876 hrs · 53,199 cycles

RIGHT WING RSS. 547 WIPER WEB SUPPORT ANGLE CRACKED ON INBOARD SIDE OF NR 2 AILERON HINGE SUPPORT FITTING. R & R ANGLE IAW SRM.

Part: SHEAR TIE — CORRODED (BS 500D) · airframe 66,876 hrs · 53,199 cycles

FORWARD CARGO BAY FRAME SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGERS 27 TO 28L. R & R THE SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,876 hrs · 53,199 cycles

AFT CARGO BAY ON FRAME CORRODED AT BS 727D, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME IAW SRM.

Part: ATTACH ANGLE — CORRODED (BS 747) · airframe 66,876 hrs · 53,199 cycles

AFT CARGO BAY, FRAME TO STRINGER ATTACH ANGLE CORRODED AT BS 747, STRINGER 27L. R & R THE ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (BS 500B) · airframe 66,876 hrs · 53,199 cycles

FORWARD CARGO BAY FRAME CORRODED AT BS 500B, BETWEEN STRINGERS 27 TO 28L. REPAIRED THE FRAME IAW SRM.

Part: WEB — CORRODED (BS 291-332) · airframe 66,876 hrs · 53,199 cycles

FORWARD GALLEY SERVICE DOOR THRESHOLD WEB CORRODED BETWEEN BS 291 TO 332. REPAIRED THE WEB IAW SRM & DWG.

Part: ROD — DETACHED (RT MLG DOOR) · airframe 66,876 hrs · 53,199 cycles

RIGHT MAIN LANDING GEAR CENTER DOOR, FORWARD LOWER SUPPORT ROD DETACHED. R & R DOOR IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,839 hrs · 53,174 cycles

RIGHT OVERHEAD BIN EMERGENCY LIGHTS INOPERATIVE BETWEEN ROW 1 TO ROW 16. R & R BATTERY PACK IAW AMM.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 66,410 hrs · 52,877 cycles

R/H EMERGENCY EXIT SIGN BROKEN. R & R THE SIGN IAW AMM.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 66,361 hrs · 52,839 cycles

LEFT GEAR SIDE STRUT SUPPORT FITTING CORRODED AT BS 685 AFT LUG. REPAIRED FITTING IAW EA.

Part: FITTING — CORRODED (LT MLG) · airframe 66,361 hrs · 52,839 cycles

LEFT MLG WALKING BEAM LINK FITTING ON AFT MLG SUPPORT BEAM OTBD LUG BORE CORRODED. R & R FITTING IAW AMM.

Part: ANGLE — CRACKED (RT WING) · airframe 64,097 hrs · 51,352 cycles

RIGHT WING TE SEAL BULKHEAD LOWER ANGLE CRACKED AT WBL 209. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 64,097 hrs · 51,352 cycles

LEFT WING TE SEAL BULKHEAD LOWER ANGLE CRACKED AT WBL 209. R & R ANGLE IAW SRM.

Part: FITTING — CRACKED (LT WING) · airframe 64,097 hrs · 51,352 cycles

LEFT WING FWD BEAM TO SPAR FITTING CRACKED AT UPPER ROW FASTENER HOLE 2ND FROM INBD EDGE. REPAIRED FITTING IAW ER & EA.

Part: FITTING — CRACKED (LT WING) · airframe 64,097 hrs · 51,352 cycles

LEFT WING AFT BEAM TO SPAR, FITTING CRACKED AT UPPER ROW INBD HOLE. REPAIRED FITTING IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,097 hrs · 51,352 cycles

RIGHT WING REAR SPAR WEB, CRACKED AT UPPER CHORD AT MLG FWD SUPPORT FITTING. REPAIRED SPAR WEB IAW ER & EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 64,097 hrs · 51,352 cycles

RIGHT WING REAR SPAR AFT MLG SUPPORT FITTING CRACKED. R & R FITTING IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,097 hrs · 51,352 cycles

LEFT WING REAR SPAR WEB, CRACKED ABOVE BEAM TO SPAR FITTING. REPAIRED SPAR WEB IAW ER & EA.

Part: LINK — CORRODED (LT MLG) · airframe 64,097 hrs · 51,352 cycles

LEFT MLG SWING LINK CORRODED. REPAIRED SWING LINK IAW ER & EA.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 64,097 hrs · 51,352 cycles

AFT CARGO BAY BULKHEAD LT CHANNEL STIFFENER CORRODED AT BS 1016, BL 0, AFT OF ANGLE STIFFENER. REPAIRED STIFFENER IAW ER & EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 64,097 hrs · 51,352 cycles

AFT CARGO BAY BULKHEAD, RT CHANNEL CORRODED AT BS 1016, AFT OF ANGLE STIFFENER. REPAIRED CHANNEL IAW ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,097 hrs · 51,352 cycles

LEFT WING TE UPPER SPAR CHORD CRACKED AT RSS 222.2. REPAIRED CHORD IAW ER & EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 64,097 hrs · 51,352 cycles

AFT CARGO BAY BULKHEAD PRESS WEB CORRODED AT BS 1016, BETWEEN LBL 3 TO RBL 3, AFT OF ANGLE STIFFENER. REPAIRED WEB IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,097 hrs · 51,352 cycles

RIGHT WING TE, UPPER SPAR CHORD CRACKED AT RSS 222.2. REPAIRED CHORD ER & EA.

Part: SIGN — UNSECURE (CABIN) · airframe 63,874 hrs · 51,186 cycles

L1 DOOR OVERHEAD EXIT SIGN LIGHT ASSEMBLY FELL OFF. R & R LIGHT ASSEMBLY IAW AMM.

Part: LUG — BROKEN (LT SPOILER) · airframe 63,306 hrs · 50,757 cycles

NUMBER 4 GND SPOILER HAS BROKEN HINGE LUG. R & R NR 4 SPOILER IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 62,090 hrs · 49,946 cycles

LEFT OVERWING EMER EXIT LIGHT LENS COVER BROKEN. R & R COVER IAW MM.

Part: LENS — UNSECURE (CABIN) · airframe 61,804 hrs · 49,759 cycles

FORWARD EXIT LIGHT LENS FELL OFF. REINSTALLED LENS IAW MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,377 hrs · 49,463 cycles

FUSELAGE SKIN CORRODED BETWEEN BS 747 TO 767 BETWEEN STRINGER 27R TO 27L. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,377 hrs · 49,463 cycles

FUSELAGE FRAME SHEAR TIE CRACKED AT STATION 360 STRINGER 13R. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,377 hrs · 49,463 cycles

STRINGER CLIP CRACKED AT BS 360 STRINGER 8L. R & R CLIP IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,377 hrs · 49,463 cycles

SHEAR TIE CORRODED AT BS 500A BETWEEN LBL 2 TO RBL 2. REPAIRED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,377 hrs · 49,463 cycles

AFT CGO DOOR SKIN CUT OUT FWD LOWER CORNER CRACKED. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,377 hrs · 49,463 cycles

FUSELAGE FRAME SHEAR TIE CORRODED AT STATION 500 STRINGER 27R. REPAIRED SHEAR TIE IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,377 hrs · 49,463 cycles

AFT PIT FWD DOOR FRAME LOWER WEB CRACKED. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,377 hrs · 49,463 cycles

FUSELAGE FRAME CRACKED AT STATION 727 LT STRINGER 18A. REPAIRED FRAME IAW EA.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 61,377 hrs · 49,463 cycles

PRESSURE DECK OVER MAIN WW BEADED PANEL CRACKED AT BS 666 LBL 39. R & R PANEL IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,377 hrs · 49,463 cycles

FRAME CHORD OTBD CHORD CRACKED AT BS 727 STRINGER 18A FWD LOWER HOLE LT SIDE. REPAIRED CHORD IAW EA.

Part: LENS — LOOSE (EXIT SIGN) · airframe 61,227 hrs · 49,361 cycles

LEFT EMER EXIT SIGN LENS LOOSE. SECURED SIGN IAW EA.

Part: SENSOR — FAULTY (LE FLAP) · airframe 60,898 hrs · 49,120 cycles

AIR TURN BACK NR 1 LE FLAP TRANSIT LIGHT ILLUMINATED DURING CLIMB OUT ABOVE 10,000'. R & R NR 1 LE FLAP UP STOW STRINGER 168 SENSOR IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 60,559 hrs · 48,885 cycles

LEFT EMER EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 2. SECURED LENS IAW SIP.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,033 hrs · 48,522 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 59,932 hrs · 48,455 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: WARNING SYSTEM — ERRATIC (COCKPIT) · airframe 58,813 hrs · 47,698 cycles

LANDING GEAR & FIRE WARN BELL SOUNDED. R & R AURAL WARN UNIT IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 58,595 hrs · 47,552 cycles

LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: CASTING — BROKEN (LT SPOILER) · airframe 58,430 hrs · 47,425 cycles

LT WING NR 4 GROUND SPOILER OTBD ACTUATOR HINGE CASTING ON SPOILER BOARD BROKEN. R & R SPOILER IAW AMM.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 58,430 hrs · 47,425 cycles

NR 7 FLAP TRACK MATING SURFACE TO AFT SPAR CORRODED ON MATING SURFACE & AROUND BOLT HOLES. R & R NR 7 FLAP TRACK IAW MM.

Part: HINGE FITTING — CRACKED (RT SPOILER) · airframe 57,754 hrs · 46,917 cycles

RT WING INBD GROUND SPOILER INBD HINGE FITTING CRACKED. R&R SPOILER IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,690 hrs · 46,863 cycles

RT AFT EMERGENCY EXIT LIGHTS INOPERATIVE. R&R BATTERY PACK ASSEMBLY IAW AMM.

Part: CHARGER — MALFUNCTIONED (E&E BAY) · airframe 57,483 hrs · 46,709 cycles

BUSSES WOULD NOT STAY POWERED BY APU OR GROUND POWER. BURNING SMELL FILLED COCKPIT. COULD SMELL 4 ROWS INTO CABIN. ALL T/R CB'S POPPED AND BATTERY CHARGER & NORMAL EQUIP COOLING FAN POPPED. R & R APU GENERATOR AND BATTERY CHARGER, APU TRANSFORMER, APU FIRE LOOP IAW MM. U FIRE LOOP IAW MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 57,153 hrs · 46,456 cycles

RIGHT WING NR 4 SLAT O/B END DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER AMM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

MAIN CABIN - PRODUCTION SPLICE AT BS 908 STRINGER 4R IS CRACKED. REMOVED & REPLACED STRINGER SPLICE PER SRM AND DRAWING.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

CORROSION ON CREASE BEAM AT STA 727D TO 727E STR 17R UPPER SURFACE. REMOVED & REPLACED CREASE BEAM WEB FROM STA 727D TO STA 727E AT STR 17R IAW B737-300 SRM 51-40-02 & BOEING DWG 65C26402 REV A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 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 SB 737-53-1306 REV 2, SECT 3.B.3. AND TASK CARD 10075 FIG 9. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS787+10 LOWER WINDOW CORNER HAD HFEC CRACK AT HOLES 1, 3, 9, 10. REPAIRED SKIN IAW IAW TASK CARD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

RIGHT BS 807+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 4. REPAIRED RIGHT BS 807+10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21670 REV- , REO G15902 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 847+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 9, 11. REPAIRED LEFT BS 847+10 LOWER FWD WINDOW CORNER IAW EA 1-353-21746 REV- & REO-G15906 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 500 +10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 5. REPAIRED LEFT BS 500+10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21743 REV- & REO-G15894 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 460+10 UPPER FORWARD WINDOW CORNER HAS HFEC NOISE INDICATION AT HOLE NR 2 AND HFEC CRACK INDICATION AT HOLES 3, 4, 5, 6, 7. REPAIRED LEFT BS 460 +10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21726 REV - , REO G15899 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 380 +10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 4, 5, 9. REPAIRED LEFT BS 380+10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21672 REV-, REO G15909 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 380 +10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 5, 9, 10. REPAIRED LEFT BS 380+10 LOWER AFT WINDOW CORNER IAW EA 1-353-21729 REV- , REO G15911 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

RIGHT BS 807+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 5, 6, 7, 9, 10. REPAIRED RIGHT BS 807+10 UPPER AFT WINDOW CORNER IAW EA 1-353-21702 REV-, REO G15918 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

RIGHT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 5. REPAIRED RIGHT BS 867+10 UPPER AFT WINDOW CORNER IAW SB 737-53-1306 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 56,562 hrs · 46,058 cycles

LEFT BS 827+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 4, 9, 10. REPAIRED LEFT BS 827 +10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21698 REV - AND REO G15904 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 500B +10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 6, 5. REPAIRED LEFT BS 500B+10 UPPER FWD WINDOW CORNER IAW EA 1-353-21752 REV- & REO-G15895 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 460+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 7. REPAIRED LEFT BS 460+10 LOWER AFT WINDOW CORNER IAW SB 737-53-1306 REV 2 AND TASK CARD 10072, STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 400 +10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4, 5, 6, 7. REPAIRED LEFT BS 400 +10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21736 REV - , REO G15910 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 807+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 9, 10. REPAIRED LEFT BS 807+10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306 REV 2, SECT 3.B.3 AND TASK CARD 10075 FIG 9. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 827+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 4, 6, 9. REPAIRED LEFT BS 827 +10 UPPER AFT WINDOW CORNER IAW EA 1-353-21697 REV - , REO G15905 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 500B+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4, 5. REPAIRED WINDOW CORNER AT 500B+10 (LWR AFT) IAW EA 1-353-21741 REV- & REO-G15914 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

RIGHT BS 867+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3. REPAIRED RIGHT BS 867+10 LOWER FORWARD WINDOW CORNER IAW SB737-53-1306 REV 2 SECTION 3.B.3 AS PER TASK CARD 10074 STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

INFORMATION LT BS 500A +10 UPPER WINDOW CORNER HAD HFEC CRACK AT HOLES 1, 2, 3, 6, 9. REPAIRED SKIN IAW MFG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

RIGHT BS 887+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 11. REPAIRED RIGHT BS 887+10 LOWER FORWARD WINDOW CORNER IAW SB737-53-1306 REV 2 SECTION 3.B.3 AS PER TASK CARD 10074 STEP 8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 480 +10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 6. REPAIRED LEFT BS 480+10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21760 REV - AND REO-G15898 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 847+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4, 5, 6. REPAIRED LEFT BS 847 +10 UPPER AFT WINDOW CORNER IAW EA 1-353-21735 REV - AND REO G15922 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 480+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED LEFT BS 480+10 LOWER AFT WINDOW CORNER IAW SB737-53-1306 REV 2 AND TASK CARD 10072, STEP 8. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

RIGHT BS 827+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 9, 10. REPAIRED RIGHT BS 827 +10 UPPER AFT WINDOW CORNER IAW EA 1-353-21671 REV -, REO G15890 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 400 +10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 3. REPAIRED WINDOW CORNER BS 400+10 LOWER AFT IAW SB737-53-1306 REV 2 AND TASK CARD 10072

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

RIGHT BS 887+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED RIGHT BS 887+10 IAW EA 1-353-21652 REV -, REO G15889 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 520 +10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 5, 6, 7, 8. REPAIRED LEFT BS 520+10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21739 REV- REO G15907 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 500C +10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 5, 6, 7. REPAIRED LEFT BS 500C+10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21755 REV- & REO-G15901 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 767+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 3, 4, 5, 6, 7, 9, 10. REPAIRED LEFT BS 767 +10 UPPER AFT WINDOW CORNER IAW EA 1-353-21742, REV - , REO G15921 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 847+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4, 5, 6. REPAIRED LEFT BS 847 +10 UPPER AFT WINDOW CORNER IAW EA 1-353-21735 REV - AND REO G15922 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 867+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 4, 5. REPAIRED LEFT BS 867+10 UPPER AFT WINDOW CORNER IAW BOEING SB 737-53-1306 REV 2 SECT 3.B.3 PER TASK CARD 10075 STEP 8 FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 787+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4, 5, 11. REPAIRED LEFT BS 787+10 UPPER AFT WINDOW CORNER IAW EA 1-353-21750 REV- AND REO-G15920 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 440 +10 UPPER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 3, 4, 5, 6, 7, 9. REPAIRED LEFT BS 440+10 UPPER FORWARD WINDOW CORNER IAW EA 1-353-21658 REV-, REO-G15900 REV IR.

Part: SKIN — CRACKED (FUSELAGAE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 887+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3. REPAIRED LEFT BS 887+10 UPPER AFT WINDOW CORNER IAW EA 1-353-21695 REV-, REO G15915 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 500C+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 5, 6, 7, 8. REPAIRED LEFT BS 500C+10 LOWER AFT WINDOW CORNER IAW EA 1-353-21747 REV- AND REO-G15916 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 360 +10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 6, 9. REPAIRED LEFT BS 360+10 LOWER AFT WINDOW CORNER IAW EA 1-353-21759 REV- AND REO G15908 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

RIGHT BS 847+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 5. REPAIRED RIGHT BS 847+10 LOWER FORWARD WINDOW CORNER IAW SB 737-53-1306 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 56,562 hrs · 46,058 cycles

LEFT BS 500+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 5, 4. REPAIRED LEFT BS 500+10 LWR AFT WINDOW CORNER IAW EA 1-353-21751 REV- & REO-G15912 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 500A+10 LOWER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 4, 6, 7, 9. REPAIRED LEFT BS 500A+10 LOWER AFT WINDOW CORNER IAW EA 1-353-21754 REV- AND REO-G15913 REV IRF.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 827+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 4, 9, 10. REPAIRED LEFT BS 827 +10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21698 REV - AND REO G15904 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,562 hrs · 46,058 cycles

LEFT BS 767+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 3, 9, 10. REPAIRED LEFT BS 767 +10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-21753 REV - , REO G15903 REV IR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: ACTUATOR — BROKEN (NR 5 SPOILER) · airframe 55,820 hrs · 45,512 cycles

RIGHT WING NR 5 O/B GROUND SPOILER ACTUATOR BROKEN. REMOVED AND REPLACED ACTUATOR IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,820 hrs · 45,512 cycles

STUB FRAME CRACKED AT BS 947+10.5, STR 17R. REPAIRED STUB FRAME IAW EO AND EA.

Part: WEB — CRACKED (NLG WW) · airframe 55,820 hrs · 45,512 cycles

RIGHT WEB CRACKED AT BS 243.7, WL 169.1. REPAIRED WEB IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,820 hrs · 45,512 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,820 hrs · 45,512 cycles

ANGLE CRACKED AT BS 303.9+5, STR 8L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,820 hrs · 45,512 cycles

WEB CRACKED AT BS 178+2, LBL 5.7. REPAIRED WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 55,820 hrs · 45,512 cycles

SUPPORT ANGLE CRACKED AT BS 303.9+6, STR 15L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,820 hrs · 45,512 cycles

ANGLE CRACKED AT BS 348.2, STR 16L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,820 hrs · 45,512 cycles

CLIP CRACKED AT BS 348.9, STR 16L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,820 hrs · 45,512 cycles

FUSELAGE SKIN CRACKED AT AFT GALLEY DOOR CUTOUT FORWARD LOWER CORNER. REPAIRED SKIN IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,820 hrs · 45,512 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 665 TO BS 670, LBL 24.5. REPAIRED CHORD IAW EA AND EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,820 hrs · 45,512 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 645 TO BS 685, RBL 24.5. REPAIRED CHORD IAW EA AND EO.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,820 hrs · 45,512 cycles

STRAP CRACKED AT BS 727B, RBL 24.5. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,820 hrs · 45,512 cycles

WEB CRACKED BETWEEN BS 705 TO BS 710, RBL 24.5. REPAIRED WEB IAW EA AND EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,820 hrs · 45,512 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, LBL 24.8. REPAIRED WEB IAW EO AND EA.

Part: LENS — LOOSE (CABIN) · airframe 55,581 hrs · 45,338 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,497 hrs · 45,275 cycles

SKIN CRACKED AT BS 727A, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,497 hrs · 45,275 cycles

SKIN CRACKED AT BS 807+6, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,497 hrs · 45,275 cycles

SKIN CRACKED AT BS 727E+5, STR 10L. REPAIRED SKIN PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 55,402 hrs · 45,205 cycles

LEFT KEEL BEAM CORRODED BETWEEN BS 723 TO BS 727. REPAIRED BEAM PER ER AND EA.

Part: SIGN — BROKEN (CABIN) · airframe 55,382 hrs · 45,189 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 55,324 hrs · 45,143 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 55,324 hrs · 45,143 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: VSI — MALFUNCTIONED (COCKPIT) · airframe 55,061 hrs · 44,940 cycles

SMELL OF ELECTRICAL SMOKE DETECTED BEHIND CAPTAIN'S INSTRUMENT PANEL. REMOVED AND REPLACED LEFT VERTICAL SPEED INDICATOR PER MM.

Part: LENS — CRACKED (CABIN) · airframe 54,469 hrs · 44,470 cycles

OVERHEAD EXIT LIGHT AT ROW 1 LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 54,123 hrs · 44,202 cycles

LT SIDE INNER CHORD IS CRACKED AT BS 616, LBL 60. INSTALLED REPAIR IAW EA.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 53,955 hrs · 44,077 cycles

AFT GALLEY SMOKE ODOR DETECTED. ODOR GONE WITH GALLEY LIGHTS EXTINGUISHED. REMOVED AND REPLACED AFT GALLEY WORK LIGHT ASSY PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,887 hrs · 44,031 cycles

SUB-SURFACE CRACK APPROX AT BS 520+ 6", STR 4L. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,580 hrs · 43,826 cycles

DURING SCHEDULED 2HC2 CHECK FOUND, LT WING O/B AFT FLAP DELAMINATED O/B LOWER SURFACE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 53,580 hrs · 43,826 cycles

DURING SCHEDULED 2HC2 CHECK FOUND, LT WING I/B FORE FLAP UPPER CENTER AREA DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 53,457 hrs · 43,741 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,307 hrs · 43,629 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 500D+12, STR 10R. REPAIRED SKIN IAW AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,307 hrs · 43,629 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 500B+12, STR 4R. REPAIRED SKIN IAW AAR EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLAT — CRACKED (RT WING) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND NR 6 L/E SLAT CRACKED AT OUTBD END. REPAIRED SLAT PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE KEEL BEAM CORRODED AT BS 807, STR 27R. REPAIRED KEEL BEAM PER ER AND SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 727, RBL 8, WL 151. REPAIRED WEB PER ER AND SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 867, STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM AND SWA EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727B, STR 27R TO STR 27L. REPAIRED FRAME PER ER AND SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BULKHEAD LOWER CHORD CRACKED AT BS 727, RBL 8, WL 150. REPAIRED CHORD PER ER AND SWA EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 947, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 351, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 500, RBL 24.5. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 27R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER ER.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 731, RBL 8. REMOVED AND REPLACED SUPPORT PER SRM AND EA.

Part: SILL — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO COMPARTMENT LOWER SILL WEB CORRODED BETWEEN BS 767 TO BS 787, RBL 11. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND PRESSURE DECK WEB CRACKED AT BS 674.75, RBL 41. REPAIRED WEB PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 27R TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO COMPARTMENT LOWER SILL WEB CORRODED BETWEEN BS 787 TO BS 795, RBL 21. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 731, LBL 3. REMOVED AND REPLACED SUPPORT PER SRM AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 751, LBL 8. REMOVED AND REPLACED SUPPORT PER SRM AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 731, LBL 12. REMOVED AND REPLACED SUPPORT PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND PRESSURE DECK WEB CRACKED AT BS 664.75, LBL 32. REPAIRED WEB PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO COMPARTMENT FAIL SAFE SPLICE CHORD CORRODED AT BS 947, STR 26R. REMOVED AND REPLACED CHORD PER SRM AND BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM ANGLE CRACKED AT BS 727B, RBL 46. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 13R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26R TO BS 27R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 312, RBL 20. REPAIRED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 380 TO BS 400, STR 17R. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 361, RBL 1. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 380, STR 5L. REMOVED AND REPLACED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 947, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 375. REPAIRED BEAM PER SRM AND BAC DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,392 hrs · 41,398 cycles

DURING SCHEDULED SPV CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BS 510. REMOVED AND REPLACED WEB PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 50,238 hrs · 41,280 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING 32 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 50,238 hrs · 41,280 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LENS — LOOSE (CABIN) · airframe 49,735 hrs · 40,894 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 49,642 hrs · 40,825 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CASE, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MT.

Part: COVER — CRACKED (CABIN) · airframe 49,357 hrs · 40,595 cycles

DURING SCHEDULED CV CHECK, FOUND RT EEPLS COVER CRACKED AT ROW 23. REMOVED AND REPLACED COVER PER MM.

Part: SPINDLE — BROKEN (TE FLAP) · airframe 49,150 hrs · 40,427 cycles

DIVERSION / DECLARED EMERGENCY. MOVING FLAPS FROM POSITION 30 TO POSITION 40 HEARD LOUD BANG WITH LEFT WING ROLL. FOUND NR 1 & NR 2 T/E FLAP SPINDLES BROKEN. REMOVED AND REPLACED BOTH SPINDLES PER MM.

Part: LENS — LOOSE (EVAC SLIDE) · airframe 48,548 hrs · 39,988 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LENS LOOSE. REMOVED AND REPLACED LENS PER EA.

Part: LENS — MISSING (CABIN) · airframe 48,497 hrs · 39,953 cycles

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

Part: ACTUATOR — FAULTY (RT MLG DOWNLOCK) · airframe 47,683 hrs · 39,358 cycles

ON APPROACH LOWERED LANDING GEAR. INITIALLY RED, MAIN RED, TAPPED HANDLE INDICATED GREEN, 15-20 SECONDS LATER RED LIGHT RETURNED AND HORN ON. RECYCLED GEAR UNTIL ALL GEARS IN GREEN LIGHT. REMOVED AND REPLACED RT MLG DOWNLOCK ACTUATOR PER MM.

Part: LENS — LOOSE (CABIN) · airframe 47,058 hrs · 38,889 cycles

EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: PRIORITY VALVE — FAULTY (RT MLG) · airframe 46,713 hrs · 38,653 cycles

ON APPROACH INTO HOU HAD AN UNSAFE (RED) RT MLG LIGHT. BROUGHT GEAR HANDLE TO THE OFF POSITION, WAITED A FEW SECONDS, LOWERED THE GEAR AGAIN AND GOT AN ALL GREEN INDICATION. REMOVED AND REPLACED RT MLG PRIORITY MODULAR VALVE PER MM.

Part: DOWNLOCK SENSOR — FAULTY (RT MLG) · airframe 46,619 hrs · 38,584 cycles

DECLARED EMERGENCY. ON FINAL, RIGHT MAIN LIGHT TURNED RED. CYCLED LANDING GEAR HANDLE TO OFF, RED TURNED TO GREEN. PUT LANDING GEAR HANDLE DOWN. ALL 3 LANDING GEAR INDICATIONS REMAINED GREEN. REMOVED AND REPLACED RT GEAR DOWNLOCK SENSOR PER MM.

Part: COVER — LOOSE (CABIN) · airframe 45,989 hrs · 38,115 cycles

L1 DOOR EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 45,280 hrs · 37,614 cycles

OVERHEAD EMERGENCY EXIT SIGN COVER LOOSE AT ROW 2. SECURED COVER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,160 hrs · 37,530 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 45,203 hrs · 37,560 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

DURING SCHEDULED 14Y CHECK, FOUND RADIO ALTIMETER CUTOUT SKIN CRACKED AT APPROX BS 390, RBL 3. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REPAIRED CLIP PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,203 hrs · 37,560 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 45,203 hrs · 37,560 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,160 hrs · 37,530 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB PER SRM.

Part: HOLDER — LOOSE (GIRT BAR) · airframe 45,031 hrs · 37,442 cycles

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

Part: SIGN — OUT OF POSITION (CABIN) · airframe 44,137 hrs · 36,807 cycles

R1 EMERGENCY EXIT SIGN LENS FELL OFF. INSTALLED LENS PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 43,613 hrs · 36,421 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 43,613 hrs · 36,421 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM.

Part: CHARGER — FAULTY (BATTERY) · airframe 43,499 hrs · 36,328 cycles

AIR TURNBACK, ACRID ODOR REPORTED IN CABIN AND FLIGHT DECK. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,004 hrs · 53,792 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 26L. R&R STRINGER CLIP PER SRM.

Part: ACTUATOR — MALFUNCTIONED (L/E SLAT) · airframe 43,138 hrs · 36,056 cycles

ON APPROACH FLAPS EXTENDED TO 5 DEGREES HAD AMBER L/E FLAP TRANSIT LIGHT ILLUMINATED, AND HAD IMMEDIATE ROLL. REMOVED AND REPLACED NR 3 L/E ACTUATOR PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,855 hrs · 35,850 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 42,510 hrs · 35,595 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING NR 5 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 42,062 hrs · 35,271 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,473 hrs · 34,022 cycles

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

Part: SKIN — DAMAGED (BS 361-372 S19R) · airframe 40,331 hrs · 3,899 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CREASED BETWEEN BS 361 AND BS 372, STR 19R. REPAIRED SKIN PER EA.

Part: SKIN — DAMAGED (BS 383-391 S19R) · airframe 40,331 hrs · 3,899 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CREASED BETWEEN BS 383 AND BS 391, STR 19R. REPAIRED SKIN PER EA.

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 39,203 hrs · 32,986 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT WING INBOARD MID FLAP WEDGE DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 39,203 hrs · 32,986 cycles

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

Part: GEARBOX — WORN (T/E FLAP) · airframe 39,088 hrs · 32,890 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT 90 DEGREE FLAP DRIVE ANGLE GEARBOX TO FLAP DRIVE MOTOR TORQUE TUBE WORN. REMOVED AND REPLACED RIGHT 90 DEGREE FLAP DRIVE ANGLE GEARBOX PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 37,131 hrs · 31,374 cycles

FWD ENTRY EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 35,489 hrs · 30,070 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 35,489 hrs · 30,070 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E FOREFLAP UPPER SKIN DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 35,155 hrs · 29,810 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 34,489 hrs · 29,298 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 34,489 hrs · 29,298 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,629 hrs · 27,780 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65, WL 201. REPAIRED FRAME PER PAE ER.

Part: MECHANISM — INOPERATIVE (L1 DOOR) · airframe 32,335 hrs · 27,541 cycles

L1 DOOR WOULD NOT OPEN. INSTALLED RELEASE MECHANISM RETAINING SCREW PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 992, RBL 55, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB BETWEEN BS 360 AND BS 380, LBL 64, CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500D, STRINGER 27L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT FWD CARGO COMPT BS 440, STRINGER 24R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 246, RBL 9, CORRODED. REMOVED AND REPLACED FLOORBEAM WEB PER ER.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR FWD LWR STUB FRAME CORRODED. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 440, RBL 6, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGERS CRACKED AT BS 992, STRINGER 13R AND STRINGER 15R. REMOVED AND REPLACED STRINGER SECTIONS PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 353, LBL 62, CORRODED. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT BS 616, RBL 65, CRACKED. REPAIRED FRAME CHORD SECTION PER ER.

Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND LT AND RT HORIZONTAL STAB FWD SPAR FWD AND AFT CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER CLIPS CRACKED AT BS 706, BETWEEN STRINGERS 11R AND 11L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER CLIPS CRACKED BETWEEN BS 560 AND BS 580, STRINGER 11R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND RT AND LT CREASE BEAM WEBS BETWEEN BS 727B AND BS 747, CORRODED. REMOVED AND REPLACED CREASE BEAM WEBS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 380, STRINGER 9L, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 9R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE IN AFT CARGO COMPARTMENT BS 767, RBL 8, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,088 hrs · 27,340 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EACH FRAMES CRACKED BETWEEN BS 787 AND BS 907, STRINGER 9L. REPAIRED FRAME SECTIONS PER SRM.

Part: LIGHT — MISSING (CABIN) · airframe 31,726 hrs · 27,059 cycles

DURING SPV, FOUND RT FWD GALLEY LOWER FACE EMERGENCY EXIT LIGHT MISSING. INSTALLED EMERGENCY EXIT LIGHT PER BAC DRAWING.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 31,650 hrs · 26,997 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: GASPER FAN — FAULTY (E/E BAY) · airframe 29,212 hrs · 25,022 cycles

AT CRUISE FL 35, FLIGHT ATTENDANTS REPORTED A METALLIC SMELL AT MID CABIN. TURNED GASPER FAN OFF SMELL IMPROVED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: FIRE LOOP — FAULTY (APU) · airframe 28,615 hrs · 24,559 cycles

DECLARED EMERGENCY, APU FIRE WARNING INDICATION WITH APU NOT RUNNING. FOUND APU TAIL PIPE DETECTOR LOOP SHORTED TO GROUND. REMOVED AND REPLACED APU TAIL PIPE FIRE LOOP AND APU FIRE LOOP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,128 hrs · 24,179 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 378.5, LBL 2.9 AND LBL 2.8 AT EQUIPTMENT COOLING EXHAUST PORT. REPAIRED SKIN PER SRM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 28,055 hrs · 24,121 cycles

R2 COCKPIT WINDOW CRACKED AND ARCING. REMOVED AND REPLACED R2 COCKPIT WINDOW ASSY PER MM.

Part: SENSOR — FAULTY (NLG) · airframe 27,474 hrs · 23,648 cycles

AIR TURNBACK, DECLARED EMERGENCY, NOSE LANDING GEAR INDICATED UNSAFE. REMOVED AND REPLACED NOSE GEAR S846 LOCK SENSOR PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 27,199 hrs · 23,419 cycles

DURING SCHEDULED C3 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE HARDWARE AND BUSHING PER MM.

Part: GAUGE — OUT OF POSITION (ESCAPE SLIDE) · airframe 26,530 hrs · 22,904 cycles

FWD SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — DEPLOYED (FWD SVC DOOR) · airframe 25,961 hrs · 22,450 cycles

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

Part: PIN — CORRODED (LT/RT MLG) · airframe 25,364 hrs · 21,970 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH LT AND RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG TRUNNION PINS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 25,266 hrs · 21,899 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING DOOR. REINSTALLED SLIDE PER MM.

Part: FRAME — CRACKED (FWD SVC DOOR) · airframe 25,146 hrs · 21,800 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT AFT LOWER CORNER. REPAIRED DOOR FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,146 hrs · 21,800 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 773, LBL 13. REPAIRED FLOORBEAM PER SWA RA.

Part: BRACKET — CRACKED (AFT SVC DOOR) · airframe 25,146 hrs · 21,800 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE, FWD AND AFT ATTACHMENT BRACKETS CRACKED. REMOVED AND REPLACED FWD AND AFT ATTACHMENT BRACKETS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 24,311 hrs · 21,151 cycles

DURING SCHEDULED BC4 CHECK, FOUND RT AFT INBD T/E FLAP DELAMINATED AT INBD AFT END. REMOVED AND REPLACED RT AFT INBD T/E FLAP PER MM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 24,311 hrs · 21,151 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR OUTER SKIN CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 23,414 hrs · 20,437 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED 14 INCHES FROM FWD EDGE AND 3 INCHES FROM LOWER EDGE. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 23,171 hrs · 20,257 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: GASPER FAN — FAULTY (CARGO BAY) · airframe 21,463 hrs · 18,929 cycles

FOUND GASPER FAN NOISY AND PRODUCING ELECTRICAL ODOR. REMOVED AND REPLACED GASPER FAN PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,214 hrs · 18,717 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LT & RT SIDE CHORDS CRACKED AT BS 178, WL 207. REMOVED AND REPLACED CHORDS PER SRM & SWA ACO 7395-53.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,833 hrs · 18,372 cycles

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

Part: BEARING — WORN (TAIL) · airframe 20,815 hrs · 18,358 cycles

DURING SCHEDULED C4 CHECK, BOTH LH & RH ELEVATORS FAILED FREE PLAY CHECK. INSTALLED ELEVATOR PUSH ROD BEARINGS PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 20,634 hrs · 18,200 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LENS — CRACKED (CABIN) · airframe 19,660 hrs · 17,405 cycles

EMERGENCY EXIT LIGHT LENS CRACKED AT FWD F/A STATION. REMOVED AND REPLACED LENS PER MM.

Part: CABLE — BROKEN (GIRT BAR) · airframe 18,822 hrs · 16,713 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE BROKEN. REPLACED CABLE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 17,852 hrs · 15,874 cycles

FWD ENTRY DOOR EMERGENCY LIGHT LENS ATTACH FITTINGS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM.

Part: SKIN — DELAMINATED (LT TE FLAP) · airframe 17,011 hrs · 15,141 cycles

DURING SCHEDULED C4 CHECK, FOUND LT I/B TRAILING EDGE AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 16,928 hrs · 14,895 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT ELEVATOR TAB DELAMINATED AT T/E. REMOVED AND REPLACED TAB ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 16,478 hrs · 14,667 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LENS COVER MISSING AT OVERWING EXIT. REPLACED LENS COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND ROW 14 FLOOR TRACK LIGHTING INOP. RELAMPED PER MM.

Part: LIGHTS — LOOSE (CABIN)

DURING C1 CHECK, FOUND NUMEROUS FLOOR TRACK LIGHTS TAPED DOWN IN CABIN. RE-ATTACHED AND TESTED AS REQUIRED PER BOEING M/M.

Part: SKIN — CREASED (BS 787)

DURING SCHEDULED RON, FOUND WINDOW FRAME SKIN CREASED AT BS 787, BETWEEN NR 30 AND 31 WINDOWS, RIGHT SIDE. REPAIRED PER BOEING SRM.