N629SW

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 68,975 hrs · 53,683 cycles

EMERGENCY EXIT LIGHT AT L-1 DOOR INOP. REMOVED AND REPLACED L-1 EMERGENCY EXIT BATTERY PACK AND OPS CHECKED GOOD AT M1674/STA 344 IAW B737-300 AMM 33-51-51. PN ON 2013-1ASMI, SN ON 13419

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 68,975 hrs · 53,683 cycles

EMERGENCY EXIT LIGHT AT R-1 DOOR INOP. REMOVED AND REPLACED R-1 EMERGENCY EXIT BATTERY PACK AND OPS CHECKED GOOD AT M1675/ STA 344 IAW B737-300 AMM 33-51-51 PN ON 2013-1ASMI, SN ON 13418

Part: COALESCER BAG — ODOR (AC BAY) · airframe 66,684 hrs · 52,451 cycles

DISCREPANCY: SMELL OF OIL IN COCKPIT AND CABIN BELOW 10,000 FEET. CORRECTIVE ACTION: REPLACE BOTH PACK COELECER SOCKS. LOGPAGE # 28543.

Part: LENS — BROKEN (CABIN) · airframe 66,386 hrs · 52,284 cycles

LT SIDEWALL EXIT LIGHT LENS BROKEN. R&R LENS PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 66,086 hrs · 52,077 cycles

L1 DOOR ESCAPE SLIDE INADVERTENTLY FELL OUT FROM CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: COVER — UNSECURE (EXIT SIGN) · airframe 65,702 hrs · 51,794 cycles

FORWARD LOWER ENTRY EXIT SIGN LENS COVER FELL OFF. R&R COVER IAW MM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 65,329 hrs · 51,524 cycles

AFT CARGO DOOR FWD FRAME CRACKED AT LOWER CORNER. R&R DOOR PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 65,144 hrs · 51,393 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 65,129 hrs · 51,383 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 65,088 hrs · 51,352 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITON. REPOSITIONED SLIDE ASSEMBLY IAW MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 64,886 hrs · 51,231 cycles

R1 DOOR EMERGENCY EVAC SLIDE GAGE OUT OF POSITION. REPOSITION SLIDE PER MT.

Part: DOOR — CRACKED (CABIN) · airframe 64,570 hrs · 51,005 cycles

R1 DOOR LOWER HINGE CUTOUT CRACKED. R&R DOOR PER MM.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 64,376 hrs · 50,884 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LATCHES AND GUIDE ARM ASSEMBLY STRIPPED. R&R SLIDE ARM IAW MM.

Part: SNUBBER — OUT OF POSITION (R1 DOOR) · airframe 64,118 hrs · 50,709 cycles

R1 DOOR GIRT BAR SNUBBER OUT OF POSITON. R&R SNUBBER PER MM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 63,808 hrs · 50,510 cycles

LEFT WING NR 1 SLAT LOWER SKIN CRACKED AT OUTBOARD AUXILIARY TRACK. REPAIRED THE SKIN IAW SRM.

Part: FITTING — LOOSE (R1 DOOR GIRT BAR) · airframe 63,808 hrs · 50,510 cycles

R1 DOOR EMERGENCY SLIDE GIRT BAR FITTING LOOSE. SECURED THE FITTING IAW SRM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 63,476 hrs · 50,307 cycles

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

Part: UPLOCK SENSOR — FAULTED (LT MLG) · airframe 63,432 hrs · 50,280 cycles

LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING DESCENT. R & R THE LT UPLOCK SENSOR IAW MM.

Part: UPLOCK SENSOR — FAULTY (LT MLG) · airframe 63,432 hrs · 50,280 cycles

LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING DESCENT. R & R THE MAIN LANDING GEAR UPLOCK SENSOR IAW MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,256 hrs · 49,479 cycles

SHEAR TIE CORRODED AT BS 400, BETWEEN STRINGER 24L - 25L. REPAIRED SHEAR TIE IAW EA.

Part: ROLLER — MISSING (TE FLAP) · airframe 62,256 hrs · 49,479 cycles

RIGHT WING MID FLAP, FWD OTBD GUIDE ROLLER MISSING. R & R ROLLER IAW CMM.

Part: SKIN — CRACKED (LT WING) · airframe 62,256 hrs · 49,479 cycles

LEFT WING UPPER SKIN TE, FASTENER HOLES CRACKED, BETWEEN LOCATIONS RSS 226 - 266. REPAIRED SKIN IAW ER & EA.

Part: FITTING — CRACKED (LT WING) · airframe 62,256 hrs · 49,479 cycles

LEFT WING FWD MLG FITTING CRACKED. REPAIRED FITTING IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 62,256 hrs · 49,479 cycles

RIGHT WING UPPER SKIN TE HOLES CRACKED, BETWEEN LOCATION RSS 228 - 267. REPAIR SKIN IAW EA & ER.

Part: BRACKET — CRACKED (LT WING) · airframe 62,256 hrs · 49,479 cycles

LEFT WING BRACKET CRACKED, AT RSS 235, COMMON TO UPPER SPAR CHORD. R & R BRACKET IAW SRM.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 62,256 hrs · 49,479 cycles

RIGHT WING AFT SPAR, AFT SUPPORT FITTING, HOLE CRACKED ABOUT 11 O CLOCK POSITION, LOCATED INBD OF RSS 224.14 HOLE NR 5. REPAIRED FITTING IAW ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,256 hrs · 49,479 cycles

LEFT WING AFT SPAR, REAR SPAR WEB HOLE, CRACKED ABOUT 7 O'CLOCK POSITION, LOCATED INBD OF RSS 224.14, HOLE 5. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,256 hrs · 49,479 cycles

RIGHT WING REAR SPAR, WEB HOLE CRACKED ABOUT 11 O CLOCK POSITION, LOCATED INBD OF RSS 224.14, HOLE NR 5. REPAIRED WEB IAW EA & ER.

Part: SPAR — CRACKED (RT WING) · airframe 62,256 hrs · 49,479 cycles

RIGHT WING REAR SPAR, UPPER CHORD CRACKED, ABOUT 11 O CLOCK POSITION, LOCATED INBD OF RSS 224.14, HOLE NR 5. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 62,256 hrs · 49,479 cycles

LEFT WING AFT SPAR, REAR SPAR UPPER CHORD HOLE, CRACKED ABOUT 7 O'CLOCK POSITION, LOCATED INBD OF RSS 224.14, HOLE 5. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 62,256 hrs · 49,479 cycles

RIGHT WING AFT SPAR, REAR SPAR WEB HOLE CRACKED ABOUT 11 O'CLOCK POSITION, LOCATED AT SECOND HOLE INBD OF RSS 224.14. REPAIRED WEB IAW EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 62,256 hrs · 49,479 cycles

LEFT WING AFT SPAR, AFT SUPPORT FITTING HOLE, CRACKED ABOUT 7 O'CLOCK POSITION, LOCATED INBD RSS 224.14, HOLE 5. REPAIRED FITTING IAW ER & EA.

Part: SKIN — CRACKED (L1 DOOR) · airframe 62,065 hrs · 49,354 cycles

L1 DOOR INNER SKIN CRACKED AT LOWER HINGE BOX. REPAIRED SKIN IAW EA.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 62,055 hrs · 49,348 cycles

R1 DOOR SLIDE GIRT BAR TOUCHING DOOR ASSEMBLY. ADJUSTED R1 DOOR GUIDE ARM IAW MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 61,742 hrs · 49,127 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR RETAINER OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW SIP.

Part: WIRE — BROKEN (EXIT SIGN) · airframe 61,709 hrs · 49,104 cycles

AFT EXIT IDENTIFIER SIGN WIRE BROKEN. REPAIRED SIGN ASSEMBLY IAW SWPM & AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

FRAME CRACKED AT BS 482, STRINGER 23R. R & R FRAME IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

CEILING SUPPORT STRUCTURE CHANNEL CRACKED, BETWEEN BS 767 - 787. R & R CHANNEL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

FRAME CRACKED AT BS 328, BETWEEN STRINGER 20R - 21R. REPAIRED FRAME IAW ACO.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

FORWARD ENTRY DOOR JAMB LOWER AFT CORNER CRACKED AT FASTENER HOLE. REPAIRED DOOR JAMB IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

E & E BAY ANGLE CRACKED AT BS 203, STRINGER 20L. R & R ANGLE IAW SRM.

Part: ATTACH BRACKET — CRACKED (R1 DOOR) · airframe 61,709 hrs · 49,104 cycles

R1 DOOR SLIDE ASSEMBLY GIRT BAR ATTACH BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

FORWARD SEAT TRACK HORIZONTAL INBD & OTBD FLANGES CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW ER & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45. REPAIRED CHORD IAW ER & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

R1 DOOR SKIN CUT OUT FWD UPPER CORNER COMMON TO REVEAL CRACKED. REPAIRED SKIN IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 500B - 500C, WL 208, LT SIDE. R & R WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

FORWARD GALLEY SERVICE DOOR CUT OUT FITTING CRACKED AT BS 296, STRINGER 8R. R & R FITTING IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

FRAME CORRODED AT BS 1006, BETWEEN STRINGER 17R - 19R. R & R FRAME IAW DWG & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

NOSE WW BELOW FWD LT PRESS PANEL, CUT OUT CRACKED AT FASTENERS, BETWEEN BS 245. 7 - 246.7. REPAIRED CUT OUT IAW EA & ER.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

STRINGER SPLICE FITTING CRACKED AT BS 360, STRINGER 7L. R & R FITTING IAW ER & EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

AFT CARGO DOOR, UPPER SILL CORRODED, BETWEEN BS 792 - 827 UPPER SURFACE. R & R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

LEFT CREASE BEAM WEB CORRODED, BETWEEN BS 500A - 500B, WL 208. R & R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 500 TO BS 500, WL 208 RT SIDE. R & R WEB IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

R1 DOOR FRAME CUT OUT CRACKED AT BS 296, STRINGER 7R, UPPER INBD FWD CORNER. REPAIRED STUB FRAME IAW ER & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

FLOORBEAM UPPER CHORD, CRACKED AT BS 727B, LBL 45.5, AFT OTBD FASTENER. REPAIRED CHORD IAW ER & EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

AFT CARGO FRAME TO DOOR SILL CLIP CRACKED AT BS 807, STRINGER 25R. R & R CLIP IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

RIGHT KEEL BEAM CORRODED, BETWEEN BS 707 - 727, LOWER SURFACE. R & R KEEL BEAM IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

AFT CARGO FRAME CORRODED AT BS 807, STRINGER 26L. R & R FRAME IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

AFT CARGO FLOOR SUPPORT CORRODED, AT BS 942, LBL 3. REPAIRED SUPPORT IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

FLOORBEAM UPPER CHORD ATTACH STRAP CRACKED AT BS 727B, RBL 24.8, FWD OTBD FASTENER HOLE. R & R CHORD IAW ER & EA.

Part: PANEL — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

PANEL BREAK ASSEMBLY CRACKED AT BS 540, BETWEEN BL 0 TO RBL 25. R & R PANEL ASSEMBLY IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS 944, STRINGER 25R. REPAIRED SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS 942, RBL 3. REPAIRED SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 40 TO RBL 50. REPAIRED FLOORBEAM IAW ER & EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

AFT ENTRY DOOR INNER CHORD MOPSILL, CORRODED BETWEEN BS - BS 1006. R & R CHORD IAW SRM & DWG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

LONGITUDINAL BEAM UPPER CHORD CRACKED AT BS 664+6, LBL 24.8. R & R CHORD IAW EA & SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

LONGITUDINAL FLOORBEAM, WEB CRACKED BETWEEN BS 707 - 709, LBL 24.8. REPAIRED WEB IAW EA & AMM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

PANEL BREAK ASSEMBLY CRACKED AT BS 540, BETWEEN BL 0 TO LBL 25. R & R PANEL ASSEMBLY IAW DWG & SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

STRINGER CLIP CORRODED, AT BS 787, STRINGER 26L. R & R CLIP IAW SRM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

PANEL BREAK ASSEMBLY CRACKED AT BS 540, BETWEEN LBL 25 - 45. R & R PANEL ASSEMBLY IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

AFT CARGO FLOOR SUPPORT, CORRODED AT BS 944, STRINGER 25L. REPAIRED SUPPORT IAW SRM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

PANEL BREAK ASSEMBLY CRACKED AT BS 540, BETWEEN LBL 45 - 65. R & R PANEL ASSEMBLY IAW DWG & SRM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

AFT CARGO COMPARTMENT FWD CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW SRM & EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

AFT CARGO FWD BULKHEAD, HORIZONTAL STIFFENER, CRACKED AT BS 727, STRINGER 27R. R & R STIFFENER IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

FLOORBEAM STABILIZER STRAP CRACKED AT BS 320, LBL 48. REPAIRED STRAP IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 61,709 hrs · 49,104 cycles

HORIZONTAL STIFFENER CRACKED AT BS 178, RBL 16. R & R STIFFENER IAW SRM.

Part: SPOILER — LOOSE (LT WING) · airframe 61,988 hrs · 49,302 cycles

LEFT WING, INBD GND SPOILER LOOSE. R & R SPOILER IAW AMM.

Part: FITTING — MISSING (EVAC SLIDE) · airframe 61,483 hrs · 48,940 cycles

L1 DOOR EMER EVAC SLIDE, METAL CLIP MISSING. R & R SLIDE IAW MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 60,547 hrs · 48,262 cycles

R1 DOOR EMER SLIDE PACK OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 60,409 hrs · 48,166 cycles

R1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: FLAP — DELAMINATED (LT WING) · airframe 60,400 hrs · 48,159 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 60,200 hrs · 48,017 cycles

R1 WINDOW ARCED DURING FLIGHT. R & R R1 WINDOW IAW AMM.

Part: WINDOW — ARCED (COCKPIT) · airframe 60,200 hrs · 48,017 cycles

R1 WINDOW ARCED. R & R R1 WINDOW IAW AMM.

Part: FUSE — INOPERATIVE (LE SLAT) · airframe 59,839 hrs · 47,779 cycles

AIR TURN BACK, LE DEVICES WILL NOT RETRACT NR 3 & 5, INDICATE IN TRANSIT. R & R LE EXTEND FUSE IAW AMM.

Part: FUSE — FAILED (COCKPIT) · airframe 59,741 hrs · 47,714 cycles

AIR TURN BACK, BOTH WING LE DEVICES, FLAPS & SLATS FAILED TO RETRACT AFTER TAKEOFF. TE FOLLOWED FLAP LEVER SETTING. RESET B SYS EXTEND FUSE IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 59,574 hrs · 47,600 cycles

LEFT EMER LIGHT BULLNOSE LENS LOOSE AT ROW 6. R & R LIGHT ASSEMBLY IAW AMM.

Part: MODULE — FAULTY (LT MLG) · airframe 58,958 hrs · 47,185 cycles

DURING LANDING LT MAIN GEAR WOULD NOT EXTEND, UNSAFE INDICATION, CYCLED GEAR. R & R LT GEAR MODULAR PACKAGE IAW AMM.

Part: DOWNLOCK SENSOR — OUT OF ADJUST (LT MLG) · airframe 58,873 hrs · 47,114 cycles

AFTER EXTENDING LG LT MAIN INDICATED RED. RECYCLED GEAR & CAME BACK WITH ALL 3 GREEN. ADJUSTED DOWNLOCK SENSOR GAP IAW MM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 58,845 hrs · 47,092 cycles

LEFT ELEVATOR TAB DELAMINATED. R & R TAB IAW MM.

Part: FITTING — CORRODED (RT MLG WW) · airframe 58,399 hrs · 46,771 cycles

FRAME LOWER FITTING CORRODED AT BS 685 ON FWD & AFT LUG OF RT GEAR. REPAIRED FITTING IAW EA.

Part: ACTUATOR — LEAKING (LT MLG) · airframe 58,239 hrs · 46,655 cycles

DIVERSION LT MLG EXTENDED WHEN FIRST OFFICER PUT LG HANDLE TO OFF. R & R LT MLG INBD ACTUATOR ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,627 hrs · 45,523 cycles

LT INTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. RELAMPED LIGHTS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,627 hrs · 45,523 cycles

RT INTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. RELAMPED LIGHTS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,621 hrs · 45,522 cycles

RT EEPLS INOPERATIVE AT ROW 29. R & R EEPLS IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 56,621 hrs · 45,522 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW SWA MT.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

SPLICE CHANNEL CRACKED AT BS 908, STRINGER 4R. R & R CHANNEL IAW SRM & BAC DRAWING.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

SPLICE CRACKED AT BS 908, STRINGER 4L. R & R SPLICE IAW SRM & BAC DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

STRINGER CLIP CRACKED AT BS 440 STRINGER 9L. R & R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

STRINGER CLIP CRACKED AT BS 440, STRINGER 8L. R & R CLIP IAW SRM.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 887+10 LOWER FWD CORNER OF WINDOW FORGING CRACKED AT HOLE NR 7. R & R FORGING IAW BAC DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

STRINGER CRACKED BETWEEN BS 380 TO BS 400 STRINGER 8L. REPAIRED STRINGER IAW EA.

Part: SKIN — BUCKLED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 520+10 UPPER FWD & UPPER AFT WINDOW CORNERS SKIN BUCKLED. REPAIRED SKIN IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

STRINGER CRACKED AT BS 380 STRINGER 5L. REPAIRED STRINGER IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

SUB STRUCTURE ANGLE CRACKED AT BS 259 STRINGER 4L. R & R ANGLE IAW SRM & DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

STRINGER SPLICE CRACKED AT BS 359 STRINGER 4R. R & R SPLICE IAW SWA EA.

Part: FORGING — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 380+10 WINDOW FORGING UPPER FWD CORNER CRACKED AT HOLE NR 7. R & R FORGING IAW BAC DRAWING.

Part: LENS — BROKEN (CABIN) · airframe 56,621 hrs · 45,522 cycles

AFT LAVATORY EMERGENCY EXIT SIGN LENS BROKEN. R & R LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 520+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLE 3 TO 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 500A+10 UPPER FWD SKIN CUTOUT CRACKED AT HOLES 2, 4, 5, 6 & 8. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 807 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 500+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 2 TO 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 807+10 UPPER AFT SKIN CUTOUT CRACKED INDICATION AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 847+10 UPPER AFT SKIN CUTOUT CRACKED INDICATION AT HOLE 2. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 400+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 2 TO HOLES 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 380+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 3 TO 7. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 500A+10 LOWER AFT SKIN CUTOUT CRACKED AT HOLES 2 & 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 400+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED BETWEEN HOLE 3 TO 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 380+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 4 TO 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 380+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 1 TO 9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 500C+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLES 4 TO 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 480+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLE 4 TO 11. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 520+10 LOWER AFT WINDOW SKIN CUT OUT CRACKED AT HOLE 4. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 767+10 LOWER FWD SKIN CUTOUT CRACKED INDICATION AT HOLE 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 420+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLE 2 & 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 500C+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 380+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 500B+10 UPPER FWD SKIN CUTOUT CRACKED AT HOLES 2, 4, 5 & 8. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 500A+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED BETWEEN HOLE 2 TO HOLE 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 440+10 UPPER FWD SKIN CUTOUT CRACKED AT HOLE 3 & 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 400+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

LT BS 480+10 UPPER FWD SKIN CUTOUT CRACKED AT HOLES 3, 5 & 8. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

RT BS 360+10 LOWER AFT WINDOW SKIN CUT OUT CRACKED AT HOLES 2 - 7. REPAIRED SKIN IAW EA.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 56,621 hrs · 45,522 cycles

RT DORSAL FIN CLOSURE PANEL RETAINER ANGLE CRACKED. R & R ANGLE IAW BAC DRAWING & SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 56,621 hrs · 45,522 cycles

AFT SIDE OF FWD LAVATORY EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,083 hrs · 45,146 cycles

STRINGER CLIP CRACKED AT STATION 887, STRINGER 2R. R &R CLIP IAW SRM & DRAWING.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,083 hrs · 45,146 cycles

SKIN CORRODED BETWEEN BS 314 TO BS 316. REPAIRED SKIN IAW SRM & DRAWING.

Part: SKIN — CRACKED (LT WING) · airframe 56,083 hrs · 45,146 cycles

LT WING LE SKIN INBD OF THE NR 1 PYLON AT CORNER OF CUTOUT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 56,083 hrs · 45,146 cycles

LT NR 4 FLAP TRACK FWD ATTACH REAR BOLT HOLE OTBD SIDE CORRODED. REPAIRED FLAP TRACK IAW MM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 56,083 hrs · 45,146 cycles

MAIN WW TOP PRESSURE DECK CRACKED BETWEEN BS 665.187 TO BS 664.875 RBL 39.75. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,083 hrs · 45,146 cycles

LT WING LE NR 2 SLAT CRACKED. REPAIRED SKIN IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 56,083 hrs · 45,146 cycles

MAIN WW TOP PRESSURE DECK CRACKED BETWEEN BS 672.750 TO BS 673.0 RBL 42.0. REPAIRED WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,083 hrs · 45,146 cycles

L1 DOOR AFT DOOR FRAME CLIP CRACKED AT BS 348.2 STRINGER 15L AT LOWER END. R & R CLIP IAW SRM & DRAWING.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 56,083 hrs · 45,146 cycles

RT WING OTBD FIREBOX LOWER OTBD EDGE OF WING PANEL ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,083 hrs · 45,146 cycles

RT CREASE BEAM WEB CORRODED BETWEEN BS 500B & BS 500C. REPAIRED WEB IAW SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 56,083 hrs · 45,146 cycles

LT WING NR 2 LE SLAT OTBD AFT CORNER DELAMINATED. REPAIRED NR 2 SLAT IAW SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,083 hrs · 45,146 cycles

FUSELAGE SKIN DENTED AT LOWER LOBE BETWEEN STATION 796 TO STATION 807, BETWEEN STRINGER 25R TO 27R. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,083 hrs · 45,146 cycles

UPPER FLOOR BEAM ''T'' CAP CRACKED AT BS 312 RBL 20. REPAIRED ANGLES IAW SRM.

Part: DOOR FRAME — CRACKED (GALLEY DOOR) · airframe 56,083 hrs · 45,146 cycles

PASSENGER CABIN FWD GALLEY DOOR AFT DOOR STOP FITTING THIRD FROM BOTTOM CUTOUT CRACKED ON INTERIOR RADIUS. R & R FRAME ASSEMBLY IAW SRM & DRAWING.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,083 hrs · 45,146 cycles

SKIN DAMAGED AT STATION 852, BETWEEN STRINGER 1 TO STRINGER 2R. REPAIRED SKIN IAW EA.

Part: CONNECTOR — LOOSE (FIRE DETECTOR) · airframe 55,956 hrs · 45,054 cycles

NR 2 ENGINE FIRE LIGHT ILLUMINATED. DECLARED EMERGENCY. NR 2 ENGINE SHUT DOWN. FOUND CONNECTOR D406 & BACKSHELL OF D1208 LOOSE. SECURED CONNECTORS AND REPOSITIONED WIRE PER SWP.

Part: LENS — MISSING (CABIN) · airframe 55,866 hrs · 44,985 cycles

RT SIDE OVERWING EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS IAW MM.

Part: DOOR — DELAMINATED (RT MLG) · airframe 55,522 hrs · 44,736 cycles

RT MLG INBD DOOR DELAMINATED ON LE. R&R RT MLG INBD STRUT DOOR IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,207 hrs · 43,083 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 52,999 hrs · 42,918 cycles

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

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 51,025 hrs · 41,462 cycles

FWD ENTRY SLIDE OUT OF GREEN BAND. REMOVED AND REPLACED SLIDE 1 PER MM AND MT G25-61-06.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 500C, STR 17R. REMOVED AND REPLACED WEB IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN RBL 8 TO RBL 12. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 360, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT MAIN WHEEL WELL UPPER PRESSURE DECK SKIN CRACKED AT BS 664, BETWEEN LBL 33 TO LBL 35. REPAIRED SKIN IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 440 TO BS 460, STR 17R. REMOVED AND REPLACED WEB IAW DWG.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPARTMENT KEEL BEAM VERTICAL STIFFENER CORRODED AT BS 500D, RBL 7. REMOVED AND REPLACED STIFFENER PER SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL WEB CRACKED AT BS 639, LBL 45.5. REPAIRED WEB IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPARTMENT Z-ANGLE CORRODED AT BS 500D, STR 25L. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 706, LBL 46. REPAIRED WEB IAW EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WHEEL WELL RT KEEL BEAM CORRODED AT BS 727. REPAIRED BEAM IAW SRM AND EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP PER EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT Z-ANGLE CORRODED BETWEEN BS 767 TO BS 794, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPARTMENT FRAME ENFORCEMENT STRAP CORRODED AT BS 492. REMOVED AND REPLACED STRAP PER SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPARTMENT SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN STR 26L TO STR 26R. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 360, STR 17R. REPAIRED WEB IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CORRODED AT BS 986.5+5, STR 20R. REPAIRED WEB IAW MM AND DWG.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR WEB CRACKED BETWEEN BS 986 TO BS 1016, RBL 38. REMOVED AND REPLACED SHEAR WEB IAW SRM AND DWG.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT I/B UPPER SURFACE T/E WEDGE DELAMINATED. REPAIRED NR 2 SLAT PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17R. REPAIRED BEAM IAW SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED AT BS 986.5, LBL 5. REPAIRED SKIN IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 848 TO BS 907, STR 22R. REPAIRED STRINGER PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED AT BS 986.5, RBL 44. REPAIRED SKIN IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 300 TO BS 400, LBL 68. REPAIRED WEB IAW SRM AND WG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 847, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRRACKED AT BS 640, RBL 45.5. REPAIRED WEB IAW SRM AND EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN LBL 16 TO LBL 20. REPAIRED SHEAR TIE IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 500, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT INNER FRAME CHORD CRACKED AT BS 616. REPAIRED CHORD PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

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

Part: PLATE — CORRODED (GIRT BAR) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLATE CORRODED AT BS 312. REMOVED AND REPLACED PLATE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CORRODED (GIRT ABR) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED AT BS 312, LBL 55. REMOVED AND REPLACED FITTING IAW MM AND DWG.

Part: FITTING — CORRODED (GIRT BAR) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED AT BS 312, LBL 55. REMOVED AND REPLACED FITTING IAW MM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 50,996 hrs · 41,439 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727D, LBL 15. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,260 hrs · 39,329 cycles

RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 47,359 hrs · 38,636 cycles

RT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 46,786 hrs · 38,181 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED AT O/B END. REMOVED AND REPLACED SLAT PER MM.

Part: STRUCTURE — PUNCTURED (ELEVATOR) · airframe 45,976 hrs · 37,538 cycles

DURING SCHEDULED CV CHECK, FOUND RT ELEVATOR PUNCTURED. REMOVED AND REPLACED ELEVATOR PER MM.

Part: HOUSING — BROKEN (CABIN) · airframe 45,454 hrs · 37,147 cycles

DURING SCHEDULED 14Y CHECK, FOUND EMERGENCY EXIT BATTERY CHARGER HOUSING BROKEN. REMOVED AND REPLACED HOUSING PER MM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 45,454 hrs · 37,147 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 2L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,454 hrs · 37,147 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 45,454 hrs · 37,147 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 3L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,454 hrs · 37,147 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,454 hrs · 37,147 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 2L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,454 hrs · 37,147 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,454 hrs · 37,147 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,454 hrs · 37,147 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,454 hrs · 37,147 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,454 hrs · 37,147 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,454 hrs · 37,147 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: TAB — DELAMINATED (AILERON) · airframe 45,454 hrs · 37,147 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,454 hrs · 37,147 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SI.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,454 hrs · 37,147 cycles

DURING SCHEDULED 14Y CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CRACKED BETWEEN BS 178 TO BS 184, RBL 17.0. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,454 hrs · 37,147 cycles

DURING SCHEDULED 14Y CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CRACKED BETWEEN BS 178 TO BS 184, LBL 17.0. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 44,223 hrs · 36,254 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 44,223 hrs · 36,254 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,880 hrs · 36,003 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 982, BETWEEN STR 22R TO STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,880 hrs · 36,003 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 811, STR 3R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,880 hrs · 36,003 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CUTOUT CRACKED AT R2 DOOR LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 43,880 hrs · 36,003 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING O/B TRAILING EDGE FLAP I/B END DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,621 hrs · 45,522 cycles

FUSELAGE SKIN CRACKED AT BS 811 STRINGER 3R. REPAIRED SKIN IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 43,104 hrs · 35,425 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 43,104 hrs · 35,425 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LAMP ASSY PER MM.

Part: MOTOR — FAULTY (NR 2 ENGINE) · airframe 42,430 hrs · 34,936 cycles

RT WING NR 2 ENGINE WOULD NOT MAKE CLIMB POWER AT FL 33.5 WITH THRUST LEVER FULL FWD. REMOVED AND REPLACED VBV MOTOR AND STOP PER MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 42,247 hrs · 34,808 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN INOP. RELAMPED SIGN PER MM.

Part: HANDLE — DIRTY (COCKPIT) · airframe 40,063 hrs · 33,171 cycles

ON FINAL APPROACH TO DAL AT 600 FEET 3 GREEN AND 3 RED GEAR LIGHTS ILLUMINATED, AT 500 FEET "TOO LOW GEAR" WARNING SOUNDED. INITIATED A GO-AROUND LOWERED GEAR, NORMAL INDICATIONS. INSPECTED FOUND LANDING GEAR SELECTOR HANDLE INNER SHAFT STICKING, CLEANED AND LUBED PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,572 hrs · 32,815 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727D, STR 27L AND STR 26R. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 39,572 hrs · 32,815 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL STABILIZER SPAR RT AND LT AFT OUTBOARD LUG FITTINGS CORRODED. REPAIRED FITTINGS PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,572 hrs · 32,815 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 26L AND STR 26R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,572 hrs · 32,815 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807 BETWEEN STR 26L AND STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,572 hrs · 32,815 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727E, STR 26L AND STR 26R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,572 hrs · 32,815 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, STR 26L AND STR 26R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,570 hrs · 32,814 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, STR 28L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,570 hrs · 32,814 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,570 hrs · 32,814 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,570 hrs · 32,814 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,570 hrs · 32,814 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,570 hrs · 32,814 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,570 hrs · 32,814 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,570 hrs · 32,814 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,570 hrs · 32,814 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,570 hrs · 32,814 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,570 hrs · 32,814 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: HOOK — LOOSE (GIRT BAR) · airframe 39,238 hrs · 32,560 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,238 hrs · 32,560 cycles

DURING SCHEDULED HC1 CHECK, FOUND KEEL BEAM SKIN CRACKED AT BS 698, RBL 5 TO LBL 5. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,238 hrs · 32,560 cycles

DURING SCHEDULED HC1 CHECK, FOUND KEEL BEAM SKIN CRACKED AT BS 715, RBL 5. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 39,119 hrs · 32,480 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,406 hrs · 31,094 cycles

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

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 36,792 hrs · 30,613 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD LOWER END. REMOVED AND REPLACE FLAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,669 hrs · 30,515 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 10 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: MECHANISM — WORN (ELEVATOR TAB) · airframe 34,684 hrs · 29,008 cycles

DURING SCHEDULED PM CHECK, FOUND EXCESSIVE PLAY AT RIGHT ELEVATOR TAB CONTROL MECHANISM FWD ATTACH POINT. REMOVED AND REPLACED ELEVATOR TAB CONTROL MECHANISM PER MM.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 33,801 hrs · 28,301 cycles

AIR TURNBACK. NR 2 KRUEGER FLAP FULLY EXTENDED WITH FLAPS SELECTED UP. REMOVED AND REPLACED NR 2 FLAP ACTUATOR.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT AND LT HORIZONTAL STAB CENTER SECTION CLEVIS LUG FACES CORRODED. REPAIRED HORIZONTAL STAB LUGS PER SRM.

Part: FAILSAFE — CORRODED (T/E FLAP) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING T/E FLAP INBOARD FAIL SAFE STRAP CORRODED. R&R FAIL SAFE STRAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOOR BEAM ZEE CHORD CORRODED AT BS 270, RBL 12 TO LBL 12. R&R ZEE CHORD PER SRM.

Part: RIB — CORRODED (RT WING) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING T/E FLAP OUTBOARD RIB CORRODED. REMOVED AND REPLACED RT WING T/E FLAP RIB PER SRM AND CMM.

Part: TORQUE TUBE — CORRODED (LT WING TE FLAP) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING T/E INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED LT WING MID FLAP INBOARD TORQUE TUBE PER SRM AND CMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 460 TO BS 480, RBL 65. R&R WEB PER SRM.

Part: TORQUE TUBE — CORRODED (T/E MID FLAP) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING T/E INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. R&R LT WING MID FLAP OUTBOARD TORQUE TUBE PER SRM AND CMM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND FRAME CRACKED BS 867, STR 8R AND STR 8L. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME SECTION PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND STR SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND FRAME CORRODED AT BS 986.5, WL 208. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R AND STR 8L. REPAIRED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME SECTION PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 348, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 43. REPAIRED FLOORBEAM PER SRM AND ER.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR LOWER HINGE FITTING CRACKED AT LOWER HALF. REMOVED AND REPLACED R1 DOOR LOWER HINGE FITTING PER EA.

Part: TORQUE TUBE — CORRODED (MID FLAP) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED INBOARD TORQUE TUBE PER SRM AND CMM.

Part: TORQUE TUBE — CORRODED (MID FLAP) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED OUTBOARD TORQUE TUBE PER SRM AND CMM.

Part: DRAG BRACE — CORRODED (TAIL SECTION) · airframe 33,295 hrs · 27,928 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT VERTICAL STAB RT AFT DRAG BRACE CORRODED. REMOVED AND REPLACED RT DRAG BRACE PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,768 hrs · 27,505 cycles

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

Part: LIGHT — WORN (CABIN) · airframe 32,768 hrs · 27,505 cycles

DURING SCHEDULED C1 CHECK, FOUND CABIN EEPLS WORN BETWEEN ROW 9 TO ROW 13. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 32,768 hrs · 27,505 cycles

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

Part: GLOWSTRIP — WORN (ROW 7) · airframe 31,783 hrs · 26,754 cycles

DURING SCHEDULED C4 CHECK, FOUND PHOTOLUMINESCENT STRIP WORN AT ROW 7. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 30,855 hrs · 25,973 cycles

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

Part: CABLE — FRAYED (L2 DOOR) · airframe 29,049 hrs · 24,568 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,049 hrs · 24,568 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR UPPER HINGE BOX PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 28,102 hrs · 23,853 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 28,014 hrs · 23,785 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 28,002 hrs · 23,777 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,985 hrs · 23,760 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,910 hrs · 23,694 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,910 hrs · 23,694 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,903 hrs · 23,685 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,840 hrs · 23,634 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,831 hrs · 23,628 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,763 hrs · 23,576 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 27,127 hrs · 23,044 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 25,522 hrs · 21,816 cycles

R1 DOOR EVACUATION SLIDE PRESS INDICATOR NOT VISIBLE. READJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,459 hrs · 21,766 cycles

R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,276 hrs · 21,622 cycles

R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 25,223 hrs · 21,577 cycles

R2 DOOR EVACUATION SLIDE LOOSE. REINSTALLED SLIDE ASSY PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,163 hrs · 21,528 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 771, RBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 25,163 hrs · 21,528 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 4 EA LONGITUDINAL FLOOR SUPPORT CORRODED AT BS 771, LBL 3, LBL 8, LBL 12 AND LBL 17. REPAIRED FLOOR SUPPORT PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,163 hrs · 21,528 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 771, RBL 8. REPAIRED FLOORBEAM PER EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 24,905 hrs · 21,338 cycles

FWD SERVICE DOOR EVACUATION SLIDE OUT OF POSITION. REINSTALLED SLIDE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 24,778 hrs · 21,233 cycles

DURING PREFLIGHT INSP, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 24,739 hrs · 21,199 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: CLIP — OUT OF ADJUST (ENTRY DOOR) · airframe 24,345 hrs · 20,878 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE RETAINING CLIP OUT OF ADJUST. ADJUSTED RETAINING CLIP PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 24,314 hrs · 20,849 cycles

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

Part: INDICATOR — OUT OF POSITION (SLIDE) · airframe 24,162 hrs · 20,728 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 23,860 hrs · 20,475 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 23,817 hrs · 20,438 cycles

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

Part: PIN — SHEARED (LT MLG) · airframe 20,665 hrs · 17,904 cycles

AIR TURN BACK, LEFT MAIN GEAR WOULD NOT RETRACT AFTER T/O, GEAR INDICATED DOWN AND LOCKED ON ALL 3 AFTER PUTTING HANDLE BACK DOWN, UNEVENTFUL LANDING AT ONT. FOUND LEFT MLG TRUNNION PIN SHEARED AT MAIN GEAR ACTUATOR. FOUND LT MLG FWD TRUNNION YOKE OTBD LOCK BOLT SHEARED. REMOVED AND REPLACED BOTH LT TRUNNION PIN AND TRUNNION LOCK BOLT PER MM. MX FERRY TO PHX FOR GEAR SWING. FOUND BROKEN HAT BUSHING CORRODED. REMOVED AND REPLACED LT MLG PER MM.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 20,530 hrs · 17,791 cycles

AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 19,847 hrs · 17,235 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 18,735 hrs · 16,311 cycles

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

Part: COVER — MISSING (CABIN) · airframe 17,052 hrs · 14,897 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY LIGHT COVER MISSING AT FWD LAV OUTER WALL. INSTALLED LIGHT COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 16,849 hrs · 14,731 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS TRACK TO HAVE MISSING AND CRACKED COVERS AT ROWS 7, 9, 12 AND 13. R&R TRACK COVERS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,768 hrs · 13,850 cycles

DURING SCHEDULED PM CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY PER MM.

Part: SLIDE — DEPLOYED (FWD SERVICE DOOR) · airframe 15,680 hrs · 13,781 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 15,389 hrs · 13,537 cycles

EEPLS TRACK COVER CRACKED AT ROW 18. R&R TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 14,245 hrs · 12,585 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND EXTERNAL RT OVERWING EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 14,001 hrs · 12,384 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT OUTBD AFT T/E FLAPS DELAMINATED. R&R FLAP ASSY PER MM.

Part: FAN — FAILED (CABIN)

F/A'S REPORTED STRONG SMOKE SMELL IN CABIN. ALSO, NOTICEABLE HAZE FROM ROW 7 FORWARD. REMOVED AND REPLACED GASPER FAN, COALESCER BAGS, AND HEPA FILTER PER MM. OPS CHECKED RECIRCULATION FAN AND RAN PACKS, PRESSURIZED TO 3 PSI WITH ENGINES AT 80 PERCENT N1, NO SMOKE SMELL OR HAZE NOTICEABLE. SYSTEM OPS, CHECKED GOOD PER MM AT THIS TIME.

Part: SKIN — DAMAGED (BS 1080)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 1080, AT S27R. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SERVICE CHECK, FOUND RT OVERWING EXIT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK FOR OVERWING RT EXIT PER BOEING MM, OPS NORMAL.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

DURING SCHEDULED C4-CHECK, FOUND NUMEROUS AREA OF LIGHTNING STRIKE DAMAGE AT BS 253, 256, 259, 313, 320, 213, 317, AND 213. REPAIRED PER BOEING SRM.