N617SW

Part: LENS — CRACKED (R1 DOOR SLIDE) · airframe 66,485 hrs · 52,792 cycles

R1 DOOR SLIDE COVER CRACKED. R & R THE LENS IAW AMM & MT.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 66,429 hrs · 52,757 cycles

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

Part: LAMP — BROKEN (EMERGENCY LIGHT) · airframe 65,868 hrs · 52,408 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. R & R THE LAMP IAW MM.

Part: LUG — BROKEN (LT SPOILER) · airframe 65,723 hrs · 52,307 cycles

LEFT WING NR 4 INBD GROUND SPOILER OTBD LUG BROKEN. R & R SPOILER IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 64,685 hrs · 51,635 cycles

LEFT OVERWING EMER EXIT LIGHT LENS MISSING. INSTALLED LIGHT ASSEMBLY IAW SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,581 hrs · 51,566 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT INOPERATIVE. CHARGED BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,581 hrs · 51,566 cycles

LEFT EMER EXIT PATHWAY LIGHTING INOPERATIVE, BETWEEN ROW 2 - 6. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,581 hrs · 51,566 cycles

RIGHT EMER EXIT PATHWAY LIGHTING INOPERATIVE, BETWEEN ROW 20 - 24. R & R BATTERY PACK IAW MM.

Part: LINK — CORRODED (LT WING) · airframe 64,581 hrs · 51,566 cycles

LEFT WING SUPPORT BEAM SWING LINK ASSEMBLY CORRODED. R & R SWING LINK ASSEMBLY EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING UPPER TE PANEL SUPPORT CLIP CRACKED. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING UPPER SKIN TE RIVET HOLE 66, CRACKED AT 12 O'CLOCK POSITION. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING, UPPER SKIN HOLE 136 AT REAR SPAR, CRACKED AT 5 O'CLOCK POSITION. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING, UPPER SKIN CRACKED AT HOLE 139 AT REAR SPAR, AT 5 O'CLOCK POSITION. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING UPPER SKIN TE RIVET HOLE 69, CRACKED AT 7 O'CLOCK POSITION. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING REAR SPAR WEB CRACKED INDICATION AT 12 O'CLOCK POSITION AT LOWER CHORD, UPPER FASTENER HOLE, RSS 170.2. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,581 hrs · 51,566 cycles

LEFT WING UPPER SKIN CRACKED AT HOLE NR 71. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 64,581 hrs · 51,566 cycles

LEFT WING UPPER SKIN CRACKED AT HOLE NR 78. REPAIRED SKIN IAW EA.

Part: FITTING — CRACKED (LT WING) · airframe 64,581 hrs · 51,566 cycles

LEFT WING REAR SPAR FITTING CRACKED AT NR 5 HOLE. R & R FITTING IAW EA.

Part: FITTING — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING REAR SPAR FITTING CRACKED AT NR 1 HOLE. R & R FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING REAR SPAR GROUP OF 12 HOLES, HOLE 5 CRACKED, IN WEB AT 6 O'CLOCK POSITION. R & R WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING REAR SPAR HOLE NR 8, CRACKED IN UPPER CHORD AT 12 O'CLOCK POSITION. R & R CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,581 hrs · 51,566 cycles

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

Part: FITTING — CRACKED (LT WING) · airframe 64,581 hrs · 51,566 cycles

LEFT WING REAR SPAR HOLE NR 5 CRACKED AFT SUPPORT FITTING AT 7 O'CLOCK POSITION. R & R FITTING IAW SRM & EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING REAR SPAR GROUP OF 12 HOLES, CRACKED IN AFT SUPPORT FITTING AT 6 O'CLOCK POSITION. R & R FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING REAR SPAR HOLE NR 5 CRACKED IN UPPER CHORD, AT 6 O'CLOCK POSITION. R & R CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,581 hrs · 51,566 cycles

LEFT WING REAR SPAR HOLE NR 4 CRACKED UPPER CHORD AT 6 O'CLOCK POSITION. R & R CHORD IAW SRM & EA.

Part: FITTING — CRACKED (LT WING) · airframe 64,581 hrs · 51,566 cycles

LEFT WING REAR SPAR HOLE NR 7 CRACKED FWD SUPPORT FITTING AT 2 O CLOCK. R & R FITTING IAW SRM & EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,581 hrs · 51,566 cycles

LEFT WING REAR SPAR WEB CRACKED, BETWEEN RSS 211 - 238. R & R WEB IAW EA.

Part: FITTING — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING REAR SPAR FITTING CRACKED AT NR 2 HOLE. R & R FITTING IAW EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING REAR SPAR GROUP OF 12 HOLES, HOLE 3 CRACKED IN AFT SUPPORT FITTING AT 7 O’CLOCK POSITION. R & R FITTING IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,581 hrs · 51,566 cycles

LEFT WING REAR SPAR HOLE NR 5 CRACKED UPPER CHORD AT 7 O'CLOCK POSITION. R & R CHORD IAW SRM & EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,581 hrs · 51,566 cycles

RIGHT WING REAR SPAR WEB CRACKED, BETWEEN RSS 211 - 235. R & R WEB IAW EA.

Part: SWITCH — FAULTY · airframe 64,515 hrs · 51,526 cycles

AIR TURN BACK. ON DEPARTURE NOSE GEAR WOULD NOT RETRACT, NOSE GEAR RED & NOSE GEAR GREEN INDICATIONS, CYCLED GEAR, NO HELP. R & R SWITCH 5846 IAW AMM.

Part: CABLE — MISROUTED (R2 DOOR) · airframe 64,179 hrs · 51,300 cycles

R2 DOOR EMER EVAC SLIDE LATCH CABLE MIS-ROUTED. RE-ROUTED CABLE IAW AMM.

Part: ANGLE — CRACKED (RT WING) · airframe 64,179 hrs · 51,300 cycles

RIGHT WING ANGLE CRACKED IN AILERON REAR SPAR BAY AT APPROX RSS 545. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 64,179 hrs · 51,300 cycles

LEFT WING TE INTERIOR, FWD OF AILERON NR 2 HINGE, LT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 63,439 hrs · 50,801 cycles

LEFT WING NR 2 LE SLAT DELAMINATED ON OTBD CORNER. R & R NR 2 SLAT IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 63,439 hrs · 50,801 cycles

LEFT WING, OTBD AFT FLAP TE DELAMINATED IN CTR OF FLAP. R & R AFT FLAP IAW AMM.

Part: SLAT — DELAMINATED (RT WING) · airframe 63,439 hrs · 50,801 cycles

RIGHT WING NR 5 LE SLAT DELAMINATED ON INBD & OTBD CORNERS. R & R NR 5 SLAT IAW MM.

Part: LENS — DEFECTIVE (CABIN) · airframe 63,043 hrs · 50,517 cycles

RIGHT EXIT LENS MISSING ARROW. R & R LENS IAW AMM.

Part: SKIN — CRACKED (BS 960) · airframe 62,663 hrs · 50,236 cycles

FOUND THE FUSELAGE SKIN CRACKED AT BS 960, STRINGER 17R. REPAIRED THE SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,663 hrs · 50,236 cycles

FOUND THE FUSELAGE SKIN CRACKED AT L2 DOOR FWD LOWER CORNER CUTOUT. REPAIRED THE SKIN IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 62,588 hrs · 50,181 cycles

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

Part: BATTERY — BROKEN (CABIN) · airframe 62,180 hrs · 49,904 cycles

M1675 EMER EXIT LIGHT POWER SUPPLY BATTERY LATCH BROKEN. R & R BATTERY IAW AMM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

FORWARD CARGO BAY FRAME SHEAR TIE CORRODED AT BS 500C, BETWEEN STRINGER 28L - 28R. REPAIRED SHEAR TIE IAW SRM.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

LEFT KEEL BEAM INBD TEE SUPPORT CRACKED AT BS 727, LBL 7. R & R TEE FITTING IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

RIGHT AUXILIARY STRAP CRACKED AT BS 727. R & R STRAP IAW DWG & SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

WEB CORRODED AT BS 993, STRINGER 21R. R & R INTERCOSTAL SAM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED AROUND SEVERAL NUTPLATE HOLES BETWEEN BS 490 - 500D. R & R SUPPORT IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 62,180 hrs · 49,904 cycles

LEFT WING OTBD AFT FLAP LOWER SURFACE SKIN DELAMINATED AT THE TE JUST INBD OF THE INBD FAIRING RUB STRIPS. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

SKIN CORRODED AT BS 727D+10, RBL 1. REPAIRED SKIN IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

FRAME CRACKED AT BS 520, BETWEEN STRINGER 20L - 21L. REPAIRED FRAME IAW ER & EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

STRINGER SPLICE CORRODED AT BS 907, STRINGER 19L. R & R SPLICE IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

STRINGER SPLICE CORRODED AT BS 907, STRINGER 20L. R & R SPLICE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

AFT GALLEY FLOORBEAM UPPER T CHORD CORRODED AT BS 986.5, BETWEEN LBL 4 TO RBL 55. R & R T CHORD IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

AFT GALLEY FLOORBEAM CORRODED AT BS 967, RBL 25. REPAIRED CHORD IAW ER & EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

STRINGER CORRODED BETWEEN BS 967 - 1016, STRINGER 25L. R & R STRINGER IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

FORWARD CARGO BILGE AFT SECTION BAFFLE BRACKET CRACKED AT BS 500C, BETWEEN STRINGER 26R - 25R. R & R BAFFLE BRACKET IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

AFT CARGO BAY, BILGE AREA SPLICE ANGLE CORRODED AT BS 847, STRINGER 27R. REMOVED & REPLACED SPLICE ANGLE IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

EXTERNAL FUSELAGE SKIN CRACKED AT GND AIR CONDITION DOOR CUT OUT AT FASTENER FWD RT CORNER. REPAIRED SKIN IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 62,180 hrs · 49,904 cycles

OUTBOARD CHORD CRACKED AT BS 727, STRINGER 18A RT. REPAIRED CHORD IAW EA.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 62,180 hrs · 49,904 cycles

RIGHT WING TE NO STEP PANEL INBD ATTACH BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 62,157 hrs · 49,885 cycles

LEFT OVERWING EMER EXIT SIGN COVER LOOSE. R & R COVER IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 62,101 hrs · 49,846 cycles

L1 DOOR EMER EXIT SIGN LENS BROKEN. R & R LENS IAW MM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 61,469 hrs · 49,447 cycles

FORWARD EXIT SIGN COVER LOOSE. SECURED SIGN COVER IAW MM.

Part: RIB — CRACKED (RT WING) · airframe 60,889 hrs · 49,048 cycles

RIGHT WING RIB LOWER CHORD AT WBL 135.5 CRACKED. REPAIRED RIB IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,889 hrs · 49,048 cycles

INTERCOSTAL CRACKED AT BS 348.2 STRINGER 16L. R & R INTERCOSTAL IAW DWG & SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 60,879 hrs · 49,041 cycles

RIGHT WING INBD AFT FLAP DELAMINATED AT INBD EDGE UPPER SURFACE TE. R & R AFT FLAP IAW AMM.

Part: SKIN — CRACKED (RT WING) · airframe 60,879 hrs · 49,041 cycles

RIGHT WING INBD FIXED LE CRACKED AT PREVIOUS TRIM OUT INBD OF PYLON AT FSS 197.5. REPAIRED SKIN IAW SRM & EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,879 hrs · 49,041 cycles

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

Part: BRACKET — CRACKED (RT WING) · airframe 60,879 hrs · 49,041 cycles

RIGHT WING AILERON COVE BRACKET CRACKED AT LOWER RADIUS. R & R BRACKET IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 60,533 hrs · 48,794 cycles

LEFT OVERWING EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM & SIP.

Part: LENS — LOOSE (CABIN) · airframe 59,841 hrs · 48,300 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS IAW SIP.

Part: SIGN — BROKEN (CABIN) · airframe 59,491 hrs · 48,067 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 59,290 hrs · 47,938 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 59,129 hrs · 47,825 cycles

LT EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 59,064 hrs · 47,780 cycles

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

Part: LENS — MISSING (CABIN) · airframe 58,838 hrs · 47,629 cycles

LT OVERWING EMERGENCY EXIT LENS MISSING. INSTALLED LENS IAW SIP.

Part: COVER — BROKEN (CABIN) · airframe 57,644 hrs · 46,817 cycles

EMERGENCY EXIT LIGHT COVER BROKEN FWD ENTRY DOOR. R&R LIGHT ASSEMBLY IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 57,561 hrs · 46,746 cycles

LT EMERGENCY EXIT LIGHT LENS COVER CRACKED. R&R COVER IAW AMM.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 56,673 hrs · 46,102 cycles

COCKPIT FLOOR PANEL IN FRONT OF DOOR CRACKED. REMOVED AND REPLACED PANEL IAW BAC DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

SHEAR TIE CRACKED AT STA 500D STR 12L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

SKIN CRACKED AT STA 380, STR 14L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

SKIN CRACKED BETWEEN STA 379.5 AND STA 380.5, STR 14R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

SKIN CRACKED BETWEEN STA 379.5 AND STA 380.5, STR 14R. REPAIRED SKIN IAW EA.

Part: TIE ROD — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

STOW BIN TIE ROD CRACKED AT STA 440, STR 8L. REMOVED AND REPLACED TIE ROD IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

STRINGER CRACKED AT STA 380, STR 5L. REPAIRED STRINGER IAW EA.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

STRINGER DAMAGED AT STA 440, STR 9L. REPAIRED STRINGER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

FUSELAGE SKIN CRACKED AT BS 847 UPPER AFT RIGHT WINDOW CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

RIGHT BS 787 AFT UPPER WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 9. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

LEFT BS 807 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 6, 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

FUSELAGE SKIN CRACKED AT BS 807 UPPER AFT RIGHT WINDOW CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

LEFT BS 847 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3, 7, 8. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

RIGHT BS 827 AFT UPPER WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

RIGHT BS 847 FORWARD LOWER WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

LEFT BS 867 FORWARD LOWER WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 5, 6. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

LEFT BS 847 FORWARD LOWER WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

LEFT BS 787 FORWARD LOWER WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 6, 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

FUSELAGE SKIN CRACKED AT BS 807 LOWER FWD LEFT WINDOW CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

FUSELAGE SKIN CRACKED AT BS 887 UPPER AFT RIGHT WINDOW CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

LEFT BS 827 FORWARD LOWER WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3. REPAIRED SKIN IAW SB.

Part: WINDOW — CRACKED (CABIN) · airframe 56,673 hrs · 46,102 cycles

LEFT UPPER AFT WINDOW CORNER CRACKED AT BS 767 HOLES 2, 3. REPAIRED WINDOW IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

RIGHT BS 767 AFT UPPER WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 9. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

LEFT BS 767 FORWARD LOWER WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

RIGHT BS 827 FORWARD LOWER WINDOW SKIN CUTOUT CRACKED AT HOLE NR 2. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

LEFT BS 827 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 6, 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

RIGHT BS 767 FORWARD LOWER WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

RIGHT BS 867 AFT UPPER WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

FUSELAGE SKIN CRACKED AT BS 787 UPPER AFT RIGHT WINDOW CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

LEFT BS 887 FORWARD LOWER WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3, 5. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

LEFT BS 867 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

RIGHT BS 867 FORWARD LOWER WINDOW SKIN CUTOUT CRACKED AT HOLES 1, 2, 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,673 hrs · 46,102 cycles

RIGHT BS 787 FORWARD LOWER WINDOW SKIN CUTOUT CRACKED AT HOLES 2, 3. REPAIRED SKIN IAW BOEING SB.

Part: LENS — LOOSE (CABIN) · airframe 56,664 hrs · 46,096 cycles

FWD GALLEY RIGHT LOWER EMERGENCY EXIT LIGHT COVER LOOSE. SECURED LENS COVER PER M/M.

Part: LIGHT — CRACKED (CABIN) · airframe 56,387 hrs · 45,890 cycles

G-1 GALLEY EMERGENCY "EXIT" LIGHT CRACKED. REMOVED AND REPLACED LIGHT IAW AMM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 56,387 hrs · 45,890 cycles

PASSENGER CABIN STATION 294.5 S13L FRAME ATTACH CLIP IS CRACKED ON FWD SIDE OF 294 FRAME. NEW CLIP WAS ORDERED, DRILLED AND INSTALLED IAW SRM 51-40-02 AND BOEING DWG.

Part: STRAP — CRACKED (TE FLAP) · airframe 56,387 hrs · 45,890 cycles

RIGHT NR 6 FLAP DRIVE, INBOARD FLAP WEAR STRAP INSIDE FAIRING CRACKED. REPLACED INBOARD FLAP WEAR STRAP AT NR 6 FLAP DRIVE INSIDE FAIRING IAW SRM 51-40-02 AND DWG 65C26300.

Part: STRIP — DEBONDED (LT WING) · airframe 56,387 hrs · 45,890 cycles

LEFT WING L/E ACCESS PANEL 6226, FWD EDGE DELAMINATED. DISBONDED STRIP IAW SRM.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 56,387 hrs · 45,890 cycles

PRESSURE DECK IS CRACKED AT STATION 663+9", LBL 39.75". REPAIRED WEB IAW EA.

Part: ATTACH BRACKET — CRACKED (RT AILERON) · airframe 56,387 hrs · 45,890 cycles

RIGHT AILERON WING TRAILING EDGE FIXED I/B CLOSE OUT PANEL (O/B) ATTACH BRACKET IS CRACKED (FLAGGED). REMOVED ATTACH BRACKET AT RIGHT AILERON WING T/E FIXED I/B CLOSE OUT PANEL IAW 8737-300 SRM 51-40-02. LOCATED AND DRILLED NEW ATTACH BRACKET P/N GS-46460-47 TDG 29686 IAW B737-300 SRM 51-40-05 AND BOEING DWG G5-46460 REV P. INSTALLLED NEW ATTACH BRACKET WET WITH SEALANT IAW 8737-300 SRM 51-40-02 AND BOEING DWG 65-46460 REV P AND APPLIED CIC TO NEW ATTACH BRACKET IAW B737-300 AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,387 hrs · 45,890 cycles

RIGHT Z-ANGLE, STATION 500, CRACKED AT FASTENER HOLE COMMON TO FRAME. REMOVED AND REPLACED Z-ANGLE IAW SRM AND BOEING DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,387 hrs · 45,890 cycles

FORWARD CARGO COMPARTMENT, STATION 500C, FRAME, SHEAR TIE BETWEEN STRINGER 26 LEFT AND STRINGER 27 LEFT, CORRODED. REMOVED FASTENERS COMMON TO SHEAR TIE AND TBS 500C BTWEEN STR 26L AND NO27L IAW B737-300 SRM 51-40-02. REMOVED CORROSION COMMON TO SHEAR TIE AT BS 5000 BETWEEN STR 26C AND 27L IAW B737-300 SRM 53-00-07-1A-1 DETAIL II. CHECKED LIMITS ORIG "T" .045" MAT LOSS .004" MAT REMAINING .041". FOUND TO BE WITHIN LIMITS IAW B737-300 SRM 53-00-07-1A-1 DETAIL II. ALODINED, PRIMED AND APPLIED TOP COAT TO

Part: STRIP — DEBONDED (LT WING) · airframe 56,387 hrs · 45,890 cycles

LEFT WING L/E ACCESS PANEL 6231 DELAMINATED AT 2 EA LOCATIONS ON FWD EDGE. REBONDED STRIP IAW SRM.

Part: CURTAIN — CRACKED (LE SLAT) · airframe 56,387 hrs · 45,890 cycles

LEFT WING L/E, NR 1 SLAT CURTAIN IS CRACKED. REMOVED AND REPLACED LEFT WING L/E NR 1 SLAT CURTAIN IAW AMM 27-81-51-004-001 AND AMM 27-81-51-404-008.

Part: RIVET — CRACKED (WINDOW FRAME) · airframe 56,387 hrs · 45,890 cycles

PILOT WINDOW FRAME BETWEEN NR 1 AND NR 2 WINDOWS HAS CRACKED RIVIT AT TOP OF FRAME. REMOVED CRACKED RIVET & INSTALLED NEW RIVET AT UPPER MOST FASTENER HOLE COMMON TO SKIN & NR 1 WINDOW FRAME IAW SRM 51-40-02 AND DWG 05-86040.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 56,387 hrs · 45,890 cycles

FLOORBEAM STA 328 RBL 30, FLOORBEAM WEB VERTICAL STIFFENER CRACKED AT LOWER END. REMOVED AND REPLACED STIFFENER IAW SRM AND BOEING DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 56,387 hrs · 45,890 cycles

E&E COMPARTMENT, LOWER FLOORBEAM STA 312 RBL 46, FLOOR STIFFENER STRAP CRACKED, MARKED. REMOVED AND REPLACED FLOOR STIFFENER E+E COMPARTMENT AT LOWER FLOORBEAM STA 312 RBL 46 IAW SRM 51-40-02 AND DWG 65-45834. APPLIED CIC TO REPAIR AREA IAW AMM 51-21-91.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 56,387 hrs · 45,890 cycles

FRAME TO INTERCOSTAL ATTACH CLIP CRACKED AT STATION 500C, BETWEEN STRINGERS 25 LEFT AND 26 LEFT. REMOVED AND REPLACED CLIP IAW SRM & DWG.

Part: COVER — BROKEN (CABIN) · airframe 56,385 hrs · 45,889 cycles

FORWARD LOWER EMERGENCY EXIT LIGHTT COVER BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ASSY PER MM OPS CHECK NORMAL.

Part: FASTENER — LOOSE (RT WING) · airframe 55,889 hrs · 45,524 cycles

RIGHT WING UPPER LEADING EDGE INBOARD OF PYLON HAS LOOSE FASTENERS. REMOVED DISCREPANT FASTENERS AND REPLACED WITH REPAIR FASTENERS PER EA 1-357-7779.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,680 hrs · 45,372 cycles

FOUND INDICATION OF 1" SUBSURFACE FUSELAGE SKIN CRACK AT BS 747 + 11" ABOVE STRINGER 4R. REPAIRED PER EA 1-A53-5808 REV 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,680 hrs · 45,372 cycles

FOUND INDICATION OF 4" SUBSURFACE FUSELAGE SKIN CRACK AT BS 807 + 8" ABOVE STRINGER 4R. REPAIRED PER EA #1-A53-5808.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,707 hrs · 44,621 cycles

AFT GALLEY THRESHOLD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,512 hrs · 44,465 cycles

EMERGENCY LIGHT ABOVE SEAT 4D INOP. RELAMPED PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 54,039 hrs · 44,103 cycles

L1 DOOR EMERGENCY "EXIT SIGN" BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 53,371 hrs · 43,594 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 52,872 hrs · 43,230 cycles

DURING SCHDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. R&R LIGHT ASSY PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767, BETWEEN STR 27L TO STR 26L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,862 hrs · 42,457 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT EMERGENCY EXIT LIGHT BULB INOP AT ROW 13. RELAMPED BULB PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, SKIN CORRODED AT BS 468, BETWEEN STR 28R TO STR 28L. REPAIRED SKIN PER EO.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, WEB CRACKED AT BS 639, LBL 45.5. REPAIRED WEB PER EO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, FLOORBEAM UPPER FLANGE CORRODED AT BS 986.5, BETWEEN RBL 5 TO RBL 32. REPAIRED BEAM PER EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, SKIN CRACKED BETWEEN BS 727D+10 TO BS 727D+13, BETWEEN S-27L TO S-27R 2. REPAIRED SKIN PER EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CORRODED BETWEEN BS 1117 TO BS 1127, STR 17R. REMOVED AND REPLACED STRINGER PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, WEB CRACKED AT BS 639, RBL 45.5. REPAIRED WEB PER EO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, FLOORBEAM UPPER FLANGE CORRODED AT BS 986.5, BETWEEN LBL 5 TO LBL 27. REPAIRED BEAM PER EO.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, WEB CORRODED BETWEEN BS 291.5 TO BS 294.5 AND STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: SKIN — CORRODED (LT WING) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, LT WING CORRODED ON UPPER SKIN AT STR 9, WSTA 557. REPAIRED SKIN IAW EO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R AFT CARGO COMPARTMENT. REPAIRED FRAME IAW SRM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, R1 DOOR SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, ANGLE CORRODED AT STA 767, BETWEEN STR 25L TO STR 25R AFT CARGO COMPARTMENT. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER SPLICE CORRODED AT BS 360, STR 19R. REMOVED AND REPLACED SPLICE PER SRM.

Part: PLATE — CORRODED (CABIN) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, L2 DOOR GIRT BAR FLOOR ADAPTER PLATE CORRODED. REMOVED AND REPLACED ADAPTER ASSY PER MM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, R2 DOOR CHORD CORRODED AT BS 947.5 TO BS 992.8, STR 17R. REMOVED AND REPLACED CHORD IAW BAC DWG AND SRM.

Part: SKIN — DELAMINATED (AILERON) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, RT WING AILERON DELAMINATED AT TRAILING EDGE LOWER SKIN. REMOVED AND REPLACED AILERON PER MM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER SPLICE CORRODED AT BS 332, STR 18R. REMOVED AND REPLACED SPLICE PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CHANNEL CORRODED BETWEEN STA 767 TO STA 787 AND RBL 8.10 AFT CARGO COMPARTMENT. REPAIRED CHANNEL EPR EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CORRODED AT STA 767 BETWEEN STR 25R TO STR 26R. REPAIRED FRAME IAW SRM.

Part: SKIN — CORRODED (LT WING) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, LT WING CORRODED ON UPPER SKIN AT STR 11, WSTA 557. REPAIRED SKIN PER EO.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CHANNEL CORRODED AT BETWEEN STA 767 TO STA 787 AND RBL 3.00 AFT CARGO COMPARTMENT. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CHANNEL CORRODED AT BS 807+18, LBL 8.10. REPAIRED CHANNEL IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CORRODED AT BS 727E AND BETWEEN STR 27R TO STR 27L AFT CARGO COMPARTMENT. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, FRAME CORRODED AT BS 500C, BETWEEN S-26R TO S-27R FWD CARGO COMPARTMENT. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT CARGO COMPARTMENT CHANNEL CORRODED BETWEEN BS 727C TO BS 727E, RBL 8.10. REPAIRED CHANNEL PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED OTS CHECK FOUND, CORROSION ON FRAME LOC BS 767 BETWEEN STR 26R TO STR 27R LOWER FLANGE AFT CARGO COMPARTMENT. REPAIRED FRAME SECTION IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED OTS CHECK FOUND, CORRODED ON FRAME LOC STA 727E AND BETWEEN STR 25R TO STR 26LA FT CARGO COMPARTMENT. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED OTS CHECK FOUND, CORROSION ON FRAME LOCATED AT BS 727B STR 26R TO STR 27R AFT CARGO COMPARTMENT. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED OTS CHECK FOUND, CORROSION ON EXISTING REPAIR LOC STA 747 AND BETWEEN STR 26R TO STR 27R AFT CARGO COMPARTMENT. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED OTS CHECK FOUND, CRACK ON LONGITUDINAL FLOORBEAM, AROUND FASTENER, LOCATED UPPER CHORD AFT END AT BS 727B AND LBL 24.8. REPAIRED BEAM PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED OTS CHECK FOUND, CORRODED ON EXISTING REPAIR OF FRAME LOCATED BS 727D BETWEEN STR 26R TO STR 27R AFT CARGO COMPARTMENT. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED OTS CHECK FOUND, CORROSION LOCATED ON STRINGER AT, APU COMPARTMENT STA 1121 RT SIDE. REMOVED AND REPLACED STRINGER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED OTS CHECK FOUND, CORROSION ON FWD FACE OF FRAME LOCATED BS 727D BETWEEN STR 26L TO STR 27L AFT CARGO COMPARTMENT. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND CRACK AFT CARGO COMPARTMENT, TIE CLIP, BS 727A AND STR 19L. REPAIRED PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK, FOUND CORROSION AFT CARGO COMPARTMENT CHANNEL, BS 727C TO BS 727E AND RBL 3. REPAIRED PER DOC.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK, FOUND CORROSION ON CHANNEL LOCATED BETWEEN BS 727C TO BS 727E AND LBL 3 AFT CARGO COMPARTMENT. REPAIRED CHANNEL PER EA.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK, FOUND CORROSION AFT CARGO COMPARTMENT TIE CLIP BS 787, STR 27L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, RBL 18. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, EXTERNAL SKIN CRACK ON LT WING ON SLAT NR 2 AT SLAT STA 165.53. REPAIRED PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CORROSION AFT CARGO COMPARTMENT, BULKHEAD AREA ON SHEAR TIE, BS 1006, STR 27L TO STR 27R. REPAIRED PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED BETWEEN BS 500A TO BS 500B, STR 17R. REPAIRED WEB PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CORROSION AFT PAX CABIN ON WEB LOCATED BETWEEN BS 927 TO BS 947.5, STR 17R. REPAIRED PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CORROSION AFT CARGO COMPARTMENT ON FRAME STA 787 AND BETWEEN STR 25L TO STR 26L. REPAIRED PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CORROSION AFT CARGO COMPARTMENT CHANNEL, BS 859.5 AND LBL 3.00. REPAIRED PER DOC.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CORROSION INTERNAL AREA OF E/E COMPARTMENT ON TIE CLIP ON BS 344, STR 21R. REPAIRED PER SRM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CORROSION FWD ENTRY DOOR SILL AREA, ALONG ZEE BEAM BETWEEN BS 312 TO BS 344, STR 17L. REPAIRED PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CRACK AFT SERVICE DOOR SURROUND STRUCTURE ON SHEAR TIE BS 942, STR 12R. REPAIRED PER SRM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK, FOUND CORROSION E/E COMPARTMENT TIE CLIP BS 344 STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED BETWEEN BS 1064 TO BS 1088, STR 12R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CRACK AFT ENTRY DOOR SURROUND STRUCTURE ON SHEAR TIE, BS 942, STR 12L. REPAIRED PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CORROSION AFT CARGO COMP CHANNEL, BS 859.5 AND RBL 3.00. REPAIRED PER DOC.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 50,839 hrs · 41,671 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,839 hrs · 41,671 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 29. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,839 hrs · 41,671 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 50,839 hrs · 41,671 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM ANGLE CORRODED AT BS 344, STR 17L AT L1 DOOR LOWER LEVEL. REMOVED AND REPLACED ANGLE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,839 hrs · 41,671 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

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

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 50,839 hrs · 41,671 cycles

DURING SCHEDULED 16Y CHECK, FOUND INNER CHORD CORRODED BETWEEN BS 303 TO BS 360, STR 17L. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,839 hrs · 41,671 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, DELAMINATION OUTBD EDGE UPPER SKIN OF INBD AFT FLAP LT WING. REMOVED AND REPLACED FLAP PER MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CORROSION FWD PAX CABIN ON WEB LOCATED BETWEEN BS 360 TO BS 380, STR 17L. REPAIRED PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CORROSION CENTER SECTION PAX CABIN ON WEB LOCATED BETWEEN BS 616 TO BS 639, STR 17R. REPAIRED PER SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND CORROSION FWD GALLEY DOOR LOWER SILL, BS 296 AND BS 330, STR 17R. REPAIRED PER SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CORROSION FWD GALLEY DOOR LOWER SILL AREA ALONG INNER CHORD LOCATED BETWEEN BS 291.5 AND BS 344, STR 17R. REPAIRED PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CORROSION AFT PAX CABIN ON WEB LOCATED BETWEEN BS 827 TO BS 847, STR 17L. REPAIRED PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,015 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK FOUND, CORROSION AFT PAX CABIN ON UPPER FLANGE OF FLOORBEAM, BS 967 BETWEEN RBL 5 TO RBL 18. REPAIRED PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,016 hrs · 41,807 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 529, LBL 5. REPAIRED SKIN PER EA.

Part: LENS — BROKEN (EXIT SIGN) · airframe 50,938 hrs · 41,747 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,616 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 517, STR 9L. REPAIRED SKIN PER EA.

Part: LENS — MISSING (CABIN) · airframe 50,568 hrs · 41,473 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 50,478 hrs · 41,404 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. INSTALLED LENS PER MM.

Part: SPINDLE — CRACKED (TE FLAP) · airframe 48,966 hrs · 40,224 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING O/B FLAP NR 7 CARRIAGE SPINDLE CRACKED. REMOVED AND REPLACED SPINDLE PER MT.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,742 hrs · 38,065 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: SIGN — LOOSE (CABIN) · airframe 47,702 hrs · 39,275 cycles

EMERGENCY EXIT SIGN NEAR L1 DOOR LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — CRACKED (LT WING) · airframe 47,488 hrs · 39,124 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING L/E SKIN CRACKED AT STA 213. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,488 hrs · 39,124 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 47,488 hrs · 39,124 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 47,488 hrs · 39,124 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: DOOR LATCH — BROKEN (COCKPIT) · airframe 47,326 hrs · 39,010 cycles

LEFT COCKPIT EMERGENCY ESCAPE ROPE DOOR LATCH BROKEN. REMOVED AND REPLACED LATCH ASSY PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 46,994 hrs · 38,774 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 986 RBL 18. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,994 hrs · 38,774 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 303.9, WL 216.5. REPAIRED FRAME PER ER.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 46,994 hrs · 38,774 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR AFT LOWER FRAME CRACKED. REMOVED AND REPLACED FRAME PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,994 hrs · 38,774 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,994 hrs · 38,774 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,994 hrs · 38,774 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,994 hrs · 38,774 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,994 hrs · 38,774 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,994 hrs · 38,774 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 46,994 hrs · 38,774 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,994 hrs · 38,774 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,994 hrs · 38,774 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 46,994 hrs · 38,774 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 46,022 hrs · 38,066 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 46,022 hrs · 38,066 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,022 hrs · 38,066 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,896 hrs · 37,976 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FWD EMERGENCY BULLNOSE LIGHT INOP. RELAMPED PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 45,593 hrs · 37,738 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED FROM O/B END. REPAIRED FORE FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,593 hrs · 37,738 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT AT BS 304, BETWEEN WL 235 TO WL 261. REPAIRED SKIN PER ER.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 45,593 hrs · 37,738 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 45,342 hrs · 37,566 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 44,785 hrs · 37,159 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 44,598 hrs · 37,031 cycles

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

Part: SLAT — CRACKED (RT WING) · airframe 42,955 hrs · 35,845 cycles

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

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 42,955 hrs · 35,845 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 42,805 hrs · 35,745 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT MLG WHEEL WELL CEILING CRACKED AT BS 664, LBL 31. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 42,747 hrs · 35,697 cycles

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

Part: SKIN — DELAMINATED (NR 6 SPOILER) · airframe 40,958 hrs · 34,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 6 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 40,958 hrs · 34,409 cycles

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

Part: BEARING — FAILED (LT ELEVATOR) · airframe 40,958 hrs · 34,409 cycles

DURING SCHEDULED BRDG CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER MM.

Part: STRINGER CLIP — CRACKED (BS 440 S9R) · airframe 40,958 hrs · 34,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 500A S8R) · airframe 40,958 hrs · 34,409 cycles

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

Part: FRAME — CRACKED (BS 500A S8R) · airframe 40,958 hrs · 34,409 cycles

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

Part: STRINGER CLIP — CRACKED (BS 328 S20L) · airframe 40,958 hrs · 34,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 318 S20L) · airframe 40,958 hrs · 34,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 318, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 338 S20L) · airframe 40,958 hrs · 34,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 338, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,458 hrs · 34,409 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,958 hrs · 34,409 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,958 hrs · 34,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,958 hrs · 34,409 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,958 hrs · 34,409 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,958 hrs · 34,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,958 hrs · 34,409 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: LENS — LOOSE (EMERGENCY LIGHTS) · airframe 40,560 hrs · 34,086 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 39,950 hrs · 33,585 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,565 hrs · 33,297 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 38,222 hrs · 32,238 cycles

DURING SCHEDULED SPV CHECK, FOUND RIGHT AFT CABIN EMERGENCY EXIT LIGHTS INOP. FOUND LOOSE CONNECTOR, RECONNECTED CONNECTOR D10744 PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 38,189 hrs · 32,214 cycles

DURING SCHEDULED C3 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED LOWER INBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.

Part: ESCAPE ROPE — LOOSE (CABIN) · airframe 36,331 hrs · 30,767 cycles

DURING SCHEDULED C1 CHECK, FOUND ESCAPE ROPE LOOSE AT LT EMERGENCY EXIT CUTOUT. SECURED ESCAPE ROPE PER MM.

Part: FITTING — STRIPPED (R2 DOOR) · airframe 36,331 hrs · 30,767 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD MOUNT FITTING STRIPPED. REMOVED AND REPLACED EVAC SLIDE FWD FITTING PER MM.

Part: TAB — CRACKED (LT ELEVATOR) · airframe 36,331 hrs · 30,767 cycles

DURING SCHEDULED C1 CHECK, FOUND LT ELEVATOR TAB CRACKED AT NR 3 UPPER HINGE. REMOVED AND REPLACED TAB PER MM.

Part: FRAME — CRACKED (BS 867) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L TO STR 9L AND STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,291 hrs · 28,341 cycles

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

Part: FRAME — CRACKED (BS 440) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R TO STR 9R AND STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 827) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 500A) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, LBL 46. REPAIRED FLOORBEAM PER BFG ER.

Part: FRAME — CRACKED (BS 727D) · airframe 33,291 hrs · 28,341 cycles

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

Part: FRAME — CRACKED (BS 616) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 17R AND STR 17L. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (BS 360) · airframe 33,291 hrs · 28,341 cycles

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

Part: FRAME — CRACKED (R1 DOOR) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND R1 DOOR CUTOUT STUB FRAME CRACKED AT FWD UPPER CORNER. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380) · airframe 33,291 hrs · 28,341 cycles

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

Part: FRAME — CRACKED (BS 380) · airframe 33,291 hrs · 28,341 cycles

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

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 9. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (BS 294.5-360) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 294.5 TO BS 360. REPAIRED CREASE BEAM PER SRM.

Part: CREASE BEAM — CORRODED (BS 380-500B) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 380 TO BS 500B. REPAIRED CREASE BEAM PER SRM.

Part: CREASE BEAM — CORRODED (BS 500-500A) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A. REPAIRED CREASE BEAM WEB SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,291 hrs · 28,341 cycles

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

Part: FITTING — CORRODED (CABIN FLOOR) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND CORROSION ON L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR FITTINGS. REMOVED AND REPLACED GIRT BAR FLOOR FITTINGS PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM TEE CORRODED AT BS 270, LBL 11 TO RBL 11. REMOVED AND REPLACED FLOORBEAM T-CHORD PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 312, LBL 1.0. REPAIRED FLOORBEAM PER SRM.

Part: CREASE BEAM — CORRODED (CABIN FLOOR) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 294.5 TO BS 360, LBL 70.53. REPAIRED CREASE BEAM PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND LT & RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED LUG FACES PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 807, LBL 19. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIES CORRODED AT BS 727E, LBL 9 & LBL 19. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIES CORRODED AT BS 807, RBL 3, LBL 3 & LBL 9. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 19. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 947, RBL 18. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CLIP — CORRODED (AFT CARGO) · airframe 33,291 hrs · 28,341 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: ENGINE — VIBRATION (RIGHT) · airframe 32,895 hrs · 28,058 cycles

NR 2 ENGINE HAD NOTICABLE SHUDDER. VIBRATION GAUGE INDICATED 4.5. IDLE DESCENT OK. INCREASE POWER AT 12,000FT & ENGINE VIBRATION INDICATED OFF THE SCALE. REMOVED AND REPLACED NR 2 ENGINE ASSY PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 32,347 hrs · 27,606 cycles

L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER (DID NOT DEPLOYED). REINSTALLED SLIDE ASSY PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 32,171 hrs · 27,480 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 31,929 hrs · 27,282 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF HOUSING. SLIDE DID NOT DEPLOY. REINSTALLED R1 DOOR SLIDE PER MM.

Part: SKIN — DEBONDED (LT WING SLAT) · airframe 31,601 hrs · 27,025 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT DISBONDED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 30,642 hrs · 26,273 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 30,642 hrs · 26,273 cycles

DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED RT LIGHT LENS PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 29,711 hrs · 25,512 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E AFT FLAP PER MM.

Part: PANEL — CRACKED (COCKPIT) · airframe 27,620 hrs · 23,848 cycles

CAPT'S EMERGENCY ESCAPE ROPE DOOR WOULD NOT OPEN. TEMP REPAIRED TRIM PANEL PER MX NOTE.

Part: SLIDE — DISLODGED (FWD PAX DOOR) · airframe 26,380 hrs · 22,824 cycles

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

Part: FITTING — CORRODED (RT MLG) · airframe 25,027 hrs · 22,354 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG WALKING BEAM FITTING CORRODED. REMOVED AND REPLACED RT MLG WALKING BEAM FITTING PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,613 hrs · 22,184 cycles

DURING SCHEDULED 1/4 D CHECK, FOUND FUSELAGE FRAME SHEAR TIES CORRODED, WL 148, BETWEEN RBL 20 AND LBL 20, BS 787 AND BS 767. REPAIRED SHEAR TIES PER SRM.

Part: FRAME — CRACKED (BULKHEAD) · airframe 25,613 hrs · 22,184 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT BULKHEAD CHORD CRACKED AT BS 178, WL 207. REMOVED AND REPLACED LT BULKHEAD CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,613 hrs · 22,184 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 180 & LBL 16. REMOVED AND REPLACED BULKHEAD WEB PER SWA ACO & SRM.

Part: TAB — CRACKED (LT ELEVATOR) · airframe 24,263 hrs · 21,110 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT ELEVATOR TAB CRACKED AT NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 24,198 hrs · 21,053 cycles

FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 23,003 hrs · 20,056 cycles

EEPLS LOOSE AT ROW NR 8. REMOVED AND REPLACED EEPLS STRIP AT ROW NR 8 PER MM.

Part: STRAP — BROKEN (CABIN) · airframe 20,674 hrs · 18,145 cycles

FWD EMERGENCY FLASH LIGHT STRAP BROKEN. R&R STRAP PER MM.

Part: CREASE BEAM — CORRODED (CABIN) · airframe 17,331 hrs · 15,381 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 952 - 986, RBL 50, WL 208. REPAIRED CREASE BEAM WEB PER SRM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 17,331 hrs · 15,381 cycles

DURING SCHEDULED 1/2D CHECK, FOUND GIRT BAR FITTING ATTACH BRACKET CORRODED AT FWD ENTRY DOOR. REMOVED AND REPLACED GIRT BAR ATTACH BRACKET PER SRM.

Part: FRAME — CORRODED (CARGO BAY) · airframe 17,331 hrs · 15,381 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME CORRODED AT BS 727D, RBL 7.5, WL 149. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 17,331 hrs · 15,381 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOOR BEAM CORRODED AT CLIP NUT HOLES BS 986, WL 208, LBL 45 - RBL 45. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,331 hrs · 15,381 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR CUTOUT CRACKED AT LOWER STUB FRAME, BS 295, RBL 53.5, WL 208. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 17,331 hrs · 15,381 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 16,705 hrs · 14,846 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT ASSY DRAGGING ON FLOOR. REPOSITIONED SLIDE ASSY PER MM.

Part: BULKHEAD — BIRD STRIKE (FUSELAGE) · airframe 15,411 hrs · 13,741 cycles

BIRD STRIKE DAMAGE TO BS 178 BULKHEAD, LBL 2.5 - 5.7. REPAIRED BULKHEAD PER SWA RA 1-353-2252.

Part: LIGHT — LOOSE (CABIN)

EEPLS LOOSE AT MID CABIN. SECURED AND RELAMPED EEPLS AT MID CABIN PER MM.

Part: ENGINE — LEAKING (NR 1)

AIR TURNBACK, DURING ROTATION SMOKE AND OIL ODOR DEVELOPED IN COCKPIT AND CABIN. FOUND COALESCER BAG CONTAMINATED WITH OIL FROM NR 1 ENG. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: SLIDE — OUT OF POSITI0N (FWD SRVCE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVCUATION SLIDE GIRT ASSY EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASSY PER MM.

Part: KEEL BEAM — CRACKED (BS 697)

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE KEEL BEAM CRACKED, BS 697. REPAIRED PER TRM AND SB 737-53-1104.

Part: COVER — BROKEN (ROW 3,5,9,20,22)

DURING SCHEDULED BC4 CHECK, FOUND EEPLS LIGHT STRIPS COVERS BROKEN AT ROWS 3, 5, 9, 20 AND 22. REMOVED AND REPLACED EEPLS STRIP COVERS PER MM.

Part: FAN — FAILED (CABIN)

PRIOR TO ARRIVAL, CREW NOTICED ELECTRICAL TYPE FUMES IN GALLEY AREA. TURNED OFF GALLEY POWER, FUMES DISSIPATED. MADE AN UNEVENTFUL LANDING AT DTW. REMOVED AND REPLACED RECIRCULATION FAN, PER BOEING MM.

Part: AIR DISTR — ODOR (CABIN)

IN-FLIGHT, NOTED ELECTRICAL/RUBBER ODOR IN AFT CABIN AREA. NO VISIBLE SMOKE. NO EMERGENCY DECLARED. AIRCRAFT RETURNED TO BUR AND MADE AN UNEVENTFUL LANDING. INSPECTED ALL FLUORESCENT LIGHTING, SIDEWALL LIGHTS, COFFEMAKERS, LAVATORIES, HEATERS, FLIGHT RECORDER COMPT, CARGO COMPTS, PAX LIGHTS AND PSU'S, E & E COMPT, RAN A/C GASPER FANS, NO EVIDENCE OF SMOKE OR SMELL.