N395SW

Part: COVER — OUT OF POSITION (L1 DOOR) · airframe 69,762 hrs · 55,946 cycles

L1 DOOR EMERGENCY EVAC SLIDE HANDLE COVER OUT OF POSITION. REPOSITIONED COVER PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,606 hrs · 55,162 cycles

AFT CARGO DOORWAY FORWARD FRAME CLOSE OUT WEB CRACKED AT LOWER EDGE. R&R WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,606 hrs · 55,162 cycles

LONGITUDINAL BEAM WEB CRACKED AT BS 617, LBL 45, SECOND HOLE FROM THE TOP. REPAIRED WEB IAW ER AND EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 68,606 hrs · 55,162 cycles

CHORD CRACKED AT BS 540, LBL 5. REPAIRED CHORD IAW EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 68,606 hrs · 55,162 cycles

FRAME ATTACH CLIP CRACKED AT BS 348.2, STR 16L. R&R CLIP IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,606 hrs · 55,162 cycles

FUSELAGE SKIN CORRODED BETWEEN BS 525 TO BS 540, BETWEEN LBL 9 TO RBL 9. REPAIRED SKIN IAW ER AND EA.

Part: PLATE — CORRODED (FUSELAGE) · airframe 68,606 hrs · 55,162 cycles

PASSENGER CABIN FLOOR PANEL 2342 GIRT BAR MOUNT PLATE CORRODED. R & R PLATE IAW DWG.

Part: SUPPORT — CORRODED (L1 DOOR) · airframe 68,606 hrs · 55,162 cycles

L1 DOOR FORWARD GIRT BAR FITTING SUPPORT CORRODED ON UPPER SURFACE. R & R SUPPORT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,606 hrs · 55,162 cycles

STUB BEAM FRAME INNER CHORD CRACKED AT BS 616, STR 17L. R&R STUB BEAM IAW ER AND EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 68,606 hrs · 55,162 cycles

L1 DOOR BEAR STRAP UPPER HINGE CUTOUT CRACKED AT BS 303.90, STR 10L. REPAIRED CUTOUT IAW ER AND EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 68,606 hrs · 55,162 cycles

L1 DOOR BEAR STRAP LOWER HINGE CUTOUT CRACKED AT BS 305, STR 13L. REPAIRED CUTOUT IAW ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,606 hrs · 55,162 cycles

STRINGER CLIP CRACKED AT BS 277, STR 15L. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,606 hrs · 55,162 cycles

LT FRAME INNER CHORD CRACKED AT BS 616, WL 201. REPAIRED CHORD IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,606 hrs · 55,162 cycles

INTERCOSTAL OUTER CHORD CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STR 11R TO STR 12R. R&R CHORD IAW SRM & EA.

Part: CHANNEL — CRACKED (TE FLAP) · airframe 68,606 hrs · 55,162 cycles

LEFT WING OTBD MAIN FLAP CENTER FORE FLAP GUIDE CHANNEL CRACKED. R & R CHANNEL IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 68,606 hrs · 55,162 cycles

LEFT WING LOWER T/E PANEL ATTACH ANGLE CRACKED OTBD SIDE NR 1 PYLON. REPAIRED DOUBLER IAW EA.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 68,606 hrs · 55,162 cycles

LEFT WING ATTACH ANGLE CRACKED INSIDE NR 1 PYLON AT UPPER AFT CORNER OF INBD FLAP TORQUE TUBE CUTOUT. R & R ANGLE IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 68,606 hrs · 55,162 cycles

LEFT WING ATTACH ANGLE CRACKED INSIDE NR 1 PYLON AT FORWARD LOWER CORNER OF INBD FLAP TORQUE TUBE CUTOUT. R & R ANGLE IAW DWG AND SRM.

Part: LINK — MISSING (RT MLG) · airframe 66,991 hrs · 54,087 cycles

RIGHT MLG MISSING FITTING, UPPER DOWNLOCK LINK. R & R DOWNLOCK LINK IAW AMM.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 66,991 hrs · 54,087 cycles

LEFT WING UPPER INBD TE PANEL SUPPORT FITTING, CRACKED AT RSS 82.64, AT AFT END UPPER SURFACE. R & R FITTING IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 66,991 hrs · 54,087 cycles

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

Part: LINK ASSY — CORRODED (RT MLG) · airframe 66,991 hrs · 54,087 cycles

RIGHT MLG BEAM SWING LINK CORRODED. REPAIRED LINK ASSEMBLY IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 66,991 hrs · 54,087 cycles

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

Part: LINK ASSY — CORRODED (LT MLG) · airframe 66,991 hrs · 54,087 cycles

LEFT MAIN LANDING BEAM SWING LINK CORRODED. REPAIRED LINK ASSEMBLY IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 66,991 hrs · 54,087 cycles

RIGHT WING, REAR SPAR WEB, CRACKED AT MLG SUPPORT FITTING. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 66,991 hrs · 54,087 cycles

LEFT WING REAR SPAR WEB CRACKED AT MLG SUPPORT FITTING. REPAIRED WEB IAW EA.

Part: SUPPORT FITTING — CRACKED (LT MLG) · airframe 66,991 hrs · 54,087 cycles

LEFT MLG AFT SUPPORT FITTING, INBD UPPER HOLE CRACKED. R & R FITTING IAW SRM & EA.

Part: SPAR — CRACKED (LT WING) · airframe 66,991 hrs · 54,087 cycles

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

Part: SPAR — CRACKED (RT WING) · airframe 66,991 hrs · 54,087 cycles

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

Part: TAIL CONE — DELAMINATED (FUSELAGE) · airframe 66,860 hrs · 53,996 cycles

TAIL CONE DELAMINATED AT FWD LOWER SIDE AT DRAIN HOLE. R & R TAIL CONE IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,023 hrs · 52,661 cycles

LEFT BULLNOSE EMER LIGHT INOPERATIVE BETWEEN ROW 14 TO 18. R & R BATTERY PACK IAW MM.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 63,473 hrs · 51,579 cycles

AIR TURN BACK FLIGHT ATTENDANTS REPORTED STRONG SMELL OF BURNING RUBBER IN AFT GALLEY. R & R BALLAST IAW MM.

Part: LUG — CRACKED (RT SPOILER) · airframe 63,298 hrs · 51,444 cycles

RIGHT WING TE GND SPOILER FITTING LUG CRACKED. REPAIRED LUG IAW EA.

Part: SKIN PANEL — DAMAGED (TE FLAP) · airframe 63,298 hrs · 51,444 cycles

RIGHT WING OTBD FORE FLAP EXTERNAL UPPER SKIN PANEL DAMAGED AT WBL 213. REPAIRED SKIN IAW EO & EA.

Part: BEAM — BROKEN (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

HINGE BEAM BROKEN BETWEEN BS 1088 TO 1094 LOWER STRINGER 20R. R & R BEAM IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

SKIN CRACKED BETWEEN BS 1088 TO 1094 STRINGER 20R. REPAIRED SKIN IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

WEB CRACKED BETWEEN BS 1088 TO 1090 STRINGER 12R. REPAIRED WEB IAW EA.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 63,298 hrs · 51,444 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING INTERNAL AREA STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: BEARING — LOOSE (LT MLG) · airframe 63,298 hrs · 51,444 cycles

LEFT MLG BEAM FITTING BEARING LOOSE. R & R BEARING IAW DWG.

Part: BEARING — LOOSE (RT MLG) · airframe 63,298 hrs · 51,444 cycles

RIGHT MLG BEAM FITTING BEARING LOOSE. R & R BEARING IAW DWG.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 63,298 hrs · 51,444 cycles

R1 DOOR FWD LOWER CORNER FRAME CRACKED. REPAIRED FRAME IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,298 hrs · 51,444 cycles

RIGHT WING OTBD AFT FLAP OTBD END LOWER SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,298 hrs · 51,444 cycles

RIGHT WING OTBD AFT FLAP LOWER SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,298 hrs · 51,444 cycles

LEFT WING INBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: ANGLE — CRACKED (GALLEY DOOR) · airframe 63,298 hrs · 51,444 cycles

FORWARD GALLEY DOOR SPLICE ANGLE CRACKED ON AFT LOWER CORNER. R & R ANGLE IAW SRM & DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

KEEL BEAM SKIN ASSEMBLY CORRODED AT BS 616 BETWEEN LBL 6.30 TO RBL 6.30. R & R KEEL BEAM SKIN ASSEMBLY IAW EA.

Part: PLATE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

PLATE CRACKED BETWEEN BS 492 TO 500 BETWEEN STRINGER 24R TO 26R. REPAIRED PLATE IAW SRM.

Part: SPLICE PLATE — CRACKED (TE FLAP) · airframe 63,298 hrs · 51,444 cycles

RIGHT WING FORE FLAP OTBD SLICE PLATE CRACKED. REPAIRED FORE FLAP IAW EO & EA.

Part: LIGHT — DELAMINATED (CABIN) · airframe 63,298 hrs · 51,444 cycles

AFT CABIN EEPLS DELAMINATED. R & R EEPLS IAW MM.

Part: BRACKET — CRACKED (TE FLAP) · airframe 63,298 hrs · 51,444 cycles

LEFT WING NR 1 FLAP TRACK HINGE SUPPORT ASSEMBLY OTBD BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (TE FLAP) · airframe 63,298 hrs · 51,444 cycles

RIGHT WING NR 8 FLAP TRACK ASSEMBLY OTBD CRACKED ON INTERNAL SUPPORT BRACKET. R & R BRACKET IAW SRM & DWG.

Part: SKIN — CRACKED (TE FLAP) · airframe 63,298 hrs · 51,444 cycles

RIGHT WING FORE FLAP OTBD SKIN CRACKED. REPAIRED FORE FLAP IAW EO.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

SUPPORT ANGLE CRACKED AT BS 312+9, STRINGER 20L. R & R ANGLE IAW SRM & DWG.

Part: TIE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

STRINGER TIE CRACKED AT BS 294.5, STRINGER 23L. R & R TIE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

ANGLE CRACKED BETWEEN BS 348.2 TO 351.2 STRINGER 16L LOWER SURFACE. R & R ANGLE IAW SRM & DWG.

Part: RIB — CRACKED (TE FLAP) · airframe 63,298 hrs · 51,444 cycles

RIGHT WING FORE FLAP OTBD RIB CRACKED AT WBL 213.0. REPAIRED FORE FLAP IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

TEE ANGLE CRACKED AT BS 540 BETWEEN STRINGER 22L TO 28L. R & R TEE ANGLE IAW DWG & SRM.

Part: RIB — CRACKED (RT WING) · airframe 63,298 hrs · 51,444 cycles

RIGHT WING FUEL TANK RIB UPPER WEB CRACKED AT WBL 198.6 STRINGER 5R. REPAIRED WEB IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

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

Part: PLATE — CRACKED (RT HORIZ STAB) · airframe 63,298 hrs · 51,444 cycles

RIGHT HORIZONTAL STABILIZER ACCESS PANEL 9226R PLATE CRACKED. R & R PLATE IAW DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

ANGLE CRACKED BETWEEN BS 348.2 TO 351.2 STRINGER 16L. R & R ANGLE IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

BULKHEAD ZEE DOME STIFFENER CRACKED AT BS 1016 LBL 5. REPAIRED STIFFENER CRACKED IAW EO & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

WEB CORRODED BETWEEN BS 420 TO 440 STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (GALLEY DOOR) · airframe 63,298 hrs · 51,444 cycles

FORWARD GALLEY DOOR FRAME CRACKED ON FWD LOWER CORNER. REPAIRED FRAME IAW EO.

Part: DOOR FRAME — CRACKED (GALLEY DOOR) · airframe 63,298 hrs · 51,444 cycles

FORWARD GALLEY DOOR FRAME CRACKED ON AFT LOWER CORNER. R & R FRAME IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 887 TO 907. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

SUPPORT ANGLE CRACKED AT BS 947.5 STRINGER 25R. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

SUPPORT ANGLE CRACKED AT BS 947.5, STRINGER 25R. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

FRAME INNER CHORD CRACKED AT BS 348.2 STRINGER 16L. REPAIRED CHORD IAW EA.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 63,298 hrs · 51,444 cycles

CARGO TRACK CRACKED AT BS 747 RBL 13.80. REPAIRED TRACK IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

SUPPORT ANGLE CRACKED AT BS 947.5, STRINGER 25L. R & R ANGLE IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

FORWARD ENTRY DOOR FRAME OUTER CHORD CRACKED AT BS 348.2. REPAIRED CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

FRAME CORRODED AT BS 767 BETWEEN STRINGER 26R TO 27R. REPAIRED FRAME IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

FRAME INNER CHORD CRACKED AT BS 348.2 STRINGER 17L. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 63,298 hrs · 51,444 cycles

AFT CARGO DOOR FWD END T CHORD CRACKED. REPAIRED T CHORD IAW EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

FRAME WEB CRACKED AT BS 492 STRINGER 24R. R & R WEB IAW SRM & EA.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

KEEL BEAM LOWER SKIN PANEL CRACKED BETWEEN BS 661 TO STATION 727 BETWEEN LBL 6.30 TO RBL 6.30. R & R SKIN IAW EO & EA.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 63,298 hrs · 51,444 cycles

LEFT HORIZONTAL STABILIZER LOWER STIFFENER CRACKED AT STAB STATION 120.30. R & R STIFFENER IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

FLOORBEAM CRACKED AT BS 663.75+8, LBL 24.5. REPAIRED BEAM IAW EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 63,298 hrs · 51,444 cycles

RIGHT WING SUPPORT ANGLE CRACKED AT LEVEL OF RSS 530. R & R ANGLE IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 63,298 hrs · 51,444 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 666 RBL 38. REPAIRED WEB IAW EO & EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,298 hrs · 51,444 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 664 LBL 17. REPAIRED WEB IAW EO & EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,298 hrs · 51,444 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 673.5 RBL 38. REPAIRED WEB IAW EO & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75+2, RBL 24.8. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

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

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

LEFT MAIN WW SUPPORT ANGLE CRACKED AT BS 680. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

FUSELAGE SKIN CRACKED AT BS 328 STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

UPPER CHORD OVAL HOLE CRACKED AT BS 663.75+4, LBL 24.5. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,298 hrs · 51,444 cycles

UPPER CHORD CRACKED AT BS 663.75+2, LBL 24.5. REPAIRED CHORD IAW EA.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 62,817 hrs · 51,105 cycles

MID AFT EMERGENCY EXIT LIGHT INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 61,584 hrs · 50,260 cycles

LT WING NR 3 FLIGHT SPOILER DELAMINATED. R & R NR 3 SPOILER IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,741 hrs · 49,647 cycles

AFT CARGO DOOR CUTOUT SKIN CRACKED AT FASTENER HOLE STATION 799. REPAIRED DOUBLER IAW EA.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 59,313 hrs · 48,574 cycles

RIGHT AFT OVERWING EGRESS LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY PER MM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 58,164 hrs · 47,744 cycles

LEFT WHEEL WELL CEILING BEADED WEB CRACKED AT BS 664, LBL 32. REPAIRED WEB PER EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 58,164 hrs · 47,744 cycles

LEFT MAIN WHEEL WELL CEILING BEADED WEB CRACKED AT BS 664, LBL 39. REPAIRED WEB PER EA.

Part: SPOILER — DELAMINATED (LT WING) · airframe 58,164 hrs · 47,744 cycles

LEFT WING NR 1 SPOILER. REMOVED AND REPLACED NR 1 SPOILER PER AMM.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 57,293 hrs · 47,089 cycles

RIGHT WING NR 7 I/B SPOILER ACTUATOR LEAKED. REMOVED AND REPLACED ACTUATOR IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,293 hrs · 47,089 cycles

FUSELAGE FRAME CRACKED AT BS 500B, STR 19R TO STR 22R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,293 hrs · 47,089 cycles

FUSELAGE FRAME CRACKED AT BS 500B, STR 20L TO STR 21L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,293 hrs · 47,089 cycles

FUSELAGE FRAME CRACKED AT BS 500B, STR 20R TO STR 21R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,293 hrs · 47,089 cycles

FRAME INNER CHORD CRACKED AT BS 616, RBL 60.5. REPAIRED CHORD IAW EA.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 57,293 hrs · 47,089 cycles

L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,293 hrs · 47,089 cycles

FUSELAGE FRAME CRACKED AT BS 639, STR 17L. REPAIRED FRAME PER EA.

Part: CIRCUIT BREAKER — TRIPPED (MLG) · airframe 56,664 hrs · 46,610 cycles

AFTER TAKEOFF, LANDING GEAR DOOR WOULD NOT RETRACT. FOUND GEAR LATCH BREAKER OUT, RECYCLED BREAKER, LOWERED AND RAISED GEAR NORMALLY. RESET CICUIT BREAKER PER AMM.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 56,664 hrs · 46,610 cycles

AIR TURNBACK - AFTER TAKEOFF, LANDING GEAR DOOR WOULD NOT RETRACT. FOUND GEAR LATCH BREAKER OUT RECYCLED BREAKER, LOWERED AND RAISED GEAR NORMALLY. RESET CIRCUIT BREAKER PER AMM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 56,584 hrs · 46,543 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

FUSELAGE STRINGER CRACKED AT BS 797 TO BS 908, STR 10R. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN BS 787+10 UPPER AFT WINDOW CORNER CRACKED. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED BS 847+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 787+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT BS 807+10 UPPER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 827+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 807+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 767+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 827+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT BS 767+10 LOWER FORWARD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 380+10 UPPER FORWARD CORNER WINDOW CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 520+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 420+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 500+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA & REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 500C+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 480+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 440+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 500A+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 400+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 460+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 500A+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA & REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT BS 440+10 FORWARD UPPER WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 500B+10 LOWER AFT WINDOW CORNER. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 460+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 420+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 360+10 FORWARD UPPER WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA & REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 360+10 UPPER FORWARD WINDOW CORNER. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 450+10 UPPER FWD WINDOW CORNER. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 400+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 480+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 440+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 440+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT BS 500+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 360+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 480+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LOWER AFT WINDOW CORNER CUTOUT CRACKED AT RT BS 500C+10. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 500B+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 500B+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 520+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA & REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 500B+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 380+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 500+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 500A+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA & REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 380+10 LOWER AFT WINDOW CORNER. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 360+10 LOWER AFT WINDOW CORNER. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 460+10 UPPER FWD WINDOW CORNER. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 420+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW BOEING SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 380+10 FORWARD UPPER WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA & REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 460+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA & REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT FUSELAGE SKIN CRACKED AT BS 480+10 LOWER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT BS 500C+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

RT BS 400+10 FORWARD UPPER WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 400+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

LT FUSELAGE SKIN CRACKED AT BS 500+10 UPPER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

STRINGER CLIP CRACKED AT BS 440, STR 9R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

STRINGER CLIP CORRODED AT BS 520, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND BAC DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,584 hrs · 46,543 cycles

STRINGER CRACKED AT BS 831, STR 9R. REPAIRED STRINGER IAW SRM.

Part: LENS — CRACKED (CABIN) · airframe 56,584 hrs · 46,543 cycles

EMERGENCY EXIT LIGHT LENS CRACKED, AFT WALL OF FWD LAV. REMOVED AND REPLACED LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,244 hrs · 46,298 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 827+9, STR 10R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,244 hrs · 46,298 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 887+9, STR 10R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,244 hrs · 46,298 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 727A+11, STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,244 hrs · 46,298 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 827+8, STR 2R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,244 hrs · 46,298 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 867+10, STR 4R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,244 hrs · 46,298 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 887+6, STR 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,240 hrs · 46,297 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 867+10, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,240 hrs · 46,297 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727A+11, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,240 hrs · 46,297 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 887+6, BETWEEN STR 10 TO STR 10L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,240 hrs · 46,297 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 827+8, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 767 S4R) · airframe 55,822 hrs · 45,974 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 767+11, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 747 S4R) · airframe 55,822 hrs · 45,974 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 747+11, S4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 328 S4R) · airframe 55,822 hrs · 45,974 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 328+6, S4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,819 hrs · 45,968 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 328+6, STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,819 hrs · 45,968 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 767+11 STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,819 hrs · 45,968 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 747+11 STR 4R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 54,395 hrs · 44,891 cycles

DURING SCHEDULED CV CHECK FOUND, R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED PER AMM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 54,058 hrs · 44,647 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (CABIN) · airframe 53,912 hrs · 44,545 cycles

DURING SCHEDULED OTS CHECK, FOUND L2 DOOR EMERGENCY SLIDE GAUGE NOT VISIBLE. ADJUSTED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,912 hrs · 44,545 cycles

DURING SCHEDULED OTS CHECK, FOUND CRACK IN RADIUS OF CHEM-MILL POCKET STA 496-498 , BELOW STR 2L. REPAIRED PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,912 hrs · 44,545 cycles

DURING SCHEDULED OTS CHECK, FOUND CRACK STA 838 TO 839.5, ABOVE STR 4R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,912 hrs · 44,545 cycles

DURING SCHEDULED OTS CHECK, FOUND CRACK AT STA 819-819.5, ABOVE STR 4R. REPAIRED PER ER/EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,908 hrs · 44,544 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE CRACK STA 838 TO 839.5 ABOVE STR 4R. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,908 hrs · 44,544 cycles

DURING SCHEDULED MV2 CHECK, FOUND CRACK AT STA 819 TO 819.5 ABOVE STR 4R. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,908 hrs · 44,544 cycles

DURING SCHEDULED MV2 CHECK, FOUND 3.5 INCH FUSELAGE CRACK AT STA 490 TO 498 BELOW STR 2L. REPAIRED PER SRM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 53,893 hrs · 44,530 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,871 hrs · 44,365 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR SKIN CUTOUT CRACKED AT AFT UPPER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,871 hrs · 44,365 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR SKIN CUTOUT CRACKED AT AFT UPPER CORNER. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 53,588 hrs · 44,303 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 17. INSTALLED LENS PER MM.

Part: GUIDE ARM — DEFECTIVE (L1 DOOR) · airframe 53,568 hrs · 44,290 cycles

L1 DOOR WILL NOT OPEN. REMOVED AND REPLACED GUIDE ARM ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 665, LBL 24.5. REPAIRED BEAM PER EO.

Part: RIB — CRACKED (RT WING) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING LOWER RIB CRACKED AT WBL 135.5, BETWEEN S 2 TO S 3. REPAIRED RIB PER ACO.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 672, LBL 24.5. REPAIRED BEAM PER EO.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 SLAT T/E UPPER SURFACE I/B DELAMINATED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER ACO.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT SKIN T/E UPPER SURFACE O/B DELAMINATED. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 927, STR 7L. REPAIRED STRINGER PER EO.

Part: SLAT — DELAMINATED (LT WING) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SLAT TRAILING EDGE O/B END DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 380, STR 26R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: SLAT — DELAMINATED (LT WING) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING TRAILING EDGE I/B END SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 12.5. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 500C, STR 26R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 777, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 380, STR 26R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: SUPPORT — CRACKED (TE FLAP) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT TRAILING EDGE FLAP ANGLE SUPPORT CRACKED. REMOVED AND REPLACED SUPPORT PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 400, STR 26R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 19L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 400, STR 26R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 328, RBL 21. REMOVED AND REPLACED CHORD PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 52,634 hrs · 43,581 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 328, RBL 42. REMOVED AND REPLACED CHORD PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 12L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 28. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 328, RBL 15. REMOVED AND REPLACED CHORD PER SRM AND BAC DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 328, RBL 54. REMOVED AND REPLACED CHORD PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT LOWER SKIN I/B CRACKED. REPAIRED SKIN PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.5. REPAIRED BEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

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

Part: SLAT — DELAMINATED (RT WING) · airframe 52,634 hrs · 43,581 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

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

Part: FITTING — CRACKED (CARGO BAY) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED FITTING PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 986.5, BETWEEN BL 0 TO RBL 51. REMOVED AND REPLACED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED AT BS 277, STR 14R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

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

Part: CHANNEL — CORRODED (CARGO BAY) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO COMPARTMENT CHANNEL CRACKED BETWEEN BS 492.4 TO BS 500, STR 26R. REMOVED AND REPLACED CHANNEL PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 1006, STR 17R. REPAIRED FRAME PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING FORE FLAP UPPER SKIN O/B EDGE DELAMINATED. REPAIRED FORE FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 380, BETWEEN STR 20L TO STR 21L. REMOVED AND REPLACED ANGLE PER AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 13R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 SLAT LOWER SKIN CRACKED ON I/B END. REPAIRED SKIN PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM SUPPORT ANGLE CRACKED AT BS 639, LBL 45.50. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 52,634 hrs · 43,581 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM SUPPORT ANGLE CRACKED AT BS 639, RBL 45.50. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,633 hrs · 43,581 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,633 hrs · 43,581 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,558 hrs · 43,517 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 525, STR 8R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,558 hrs · 43,517 cycles

DURING SCHEDULED CV CHECK, FOUND R1 DOOR EXTERIOR SKIN AT UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,028 hrs · 43,102 cycles

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

Part: LENS — CRACKED (EXTERIOR) · airframe 51,708 hrs · 42,863 cycles

L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 51,372 hrs · 42,616 cycles

FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,061 hrs · 42,392 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 795, STR 4R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,270 hrs · 41,813 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 50,270 hrs · 41,813 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT FWD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 50,249 hrs · 41,792 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: STRIP — WORN (CABIN) · airframe 49,596 hrs · 41,299 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS STRIP WORN AT EMERGENCY EXIT. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,548 hrs · 41,260 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 816.5, STR 10R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — CRACKED (CABIN) · airframe 46,800 hrs · 39,285 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT EEPLS CRACKED AT ROW 20 ABC. REMOVED AND REPLACED EEPLS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,749 hrs · 39,249 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,749 hrs · 39,249 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,749 hrs · 39,249 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,749 hrs · 39,249 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,749 hrs · 39,249 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 303, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,749 hrs · 39,249 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — BROKEN (CABIN) · airframe 46,749 hrs · 39,249 cycles

DURING SCHEDULED 14Y CHECK, FOUND OVERHEAD CENTER AISLE EMERGENCY EXIT LIGHT COVER BROKEN. REPLACED COVER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,749 hrs · 39,249 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,749 hrs · 39,249 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,749 hrs · 39,249 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 46,749 hrs · 39,249 cycles

DURING SCHEDULED 14Y CHECK, FOUND LEFT WING O/B AFT FLAP INBOARD SIDE DELAMINATED AT TRAILING EDGE. REMOVED AND REPLACED FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,749 hrs · 39,249 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,749 hrs · 39,249 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 46,749 hrs · 39,249 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,749 hrs · 39,249 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,749 hrs · 39,249 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 45,477 hrs · 38,353 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD UPPER SURFACE. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 45,477 hrs · 38,353 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 45,477 hrs · 38,353 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING NR 5 L/E SLAT OUTBOARD T/E DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 45,477 hrs · 38,353 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 44,474 hrs · 37,595 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 42,769 hrs · 36,298 cycles

DURING SCHEDULED MV4 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED AFT FLAP PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 42,205 hrs · 35,859 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 41,943 hrs · 35,632 cycles

FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: PRESSURE PANEL — CORRODED (NLG WW) · airframe 41,902 hrs · 35,601 cycles

DURING SCHEDULED BRDG CHECK, FOUND NLG W/W LEFT UPPER CEILING CORRODED AT BS 251.652, LBL 2. REPAIRED W/W CEILING PER EA.

Part: CONNECTOR — LOOSE (CABIN) · airframe 41,902 hrs · 35,601 cycles

DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. SECURED LOOSE CONNECTOR PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,902 hrs · 35,601 cycles

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

Part: BEARING — WORN (LT ELEVATOR TAB) · airframe 41,518 hrs · 35,299 cycles

DURING SCHEDULED OTS CHECK, FOUND LEFT ELEVATOR TAB BEARING WORN AT CONTROL ROD ATTACH POINT. REMOVED AND REPLACED BEARING PER MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 41,509 hrs · 35,291 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR FRAME CRACKED AT LOWER AFT CORNER. REMOVED AND REPLACED R1 DOOR PER MM.

Part: FAN — FAULTY (E&E BAY) · airframe 40,846 hrs · 34,770 cycles

FIVE MINUTES BEFORE LANDING STRONG ACRID ODOR IN CABIN. SMELL RETURNED ANYTIME EITHER PACK IS TURNED ON. REMOVED AND REPLACED GASPER FAN PER MM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 39,661 hrs · 33,839 cycles

DURING SCHEDULED C4 CHECK, FOUND KEELBEAM PANEL CRACKED AT RT BS 714. REPAIRED PANEL IAW SRM.

Part: SKIN — CRACKED (R2 DOOR) · airframe 38,839 hrs · 33,201 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,839 hrs · 33,201 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT FWD LOWER CORNER BEAR STRAP. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 373) · airframe 36,743 hrs · 31,576 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 373, BETWEEN STR 28L & STR 28R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 36,149 hrs · 31,084 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 35,816 hrs · 30,823 cycles

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

Part: FRAME — CRACKED (FWD CARGO) · airframe 35,109 hrs · 30,252 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,535 hrs · 29,054 cycles

DURING SCHEDULED D CHECK, FOUND 6 EACH FRAMES AT BS 787, BS 867, BS 907, STRINGER 8R, BS 827, BS 867, BS 907, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,535 hrs · 29,054 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 747, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 33,534 hrs · 29,053 cycles

DURING SCHEDULED D-CHECK, FOUND L1 COCKPIT WINDOW POST UPPER RT CORNER CRACKED. REPAIRED WINDOW POST PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 335,335 hrs · 29,054 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM SHEAR WEB AT BS 500, LBL 69, CORRODED. REMOVED AND REPLACED FLOORBEAM SHEAR WEB PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,535 hrs · 29,054 cycles

DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT WEB AT BS 807 TO BS 887, LBL 70, CORRODED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM.

Part: FITTING — CORRODED (SLIDE GIRT BAR) · airframe 33,535 hrs · 29,054 cycles

DURING SCHEDULED D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FWD AND AFT FITTIGS PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,534 hrs · 29,053 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,534 hrs · 29,053 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 727A, RBL 44, CRACKED. REPAIRED FLOORBEAM PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,534 hrs · 29,053 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 794, RBL 25, WL 155, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,534 hrs · 29,034 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 492, STRINGER 24R, CRACKED. REPAIRED FRAME SECTION PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,534 hrs · 29,053 cycles

DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 986.5, LBL 18 TO RBL 44, CORRODED. REPAIRED FLOORBEAM PER ER.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,534 hrs · 29,053 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,534 hrs · 29,053 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT LT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 33,534 hrs · 29,053 cycles

DURING SCHEDULED D-CHECK, FOUND LT FLOOR PANEL AT BS 188 TO BS 196, CRACKED. REMOVED AND REPLACED FLOOR PANEL SECTION PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 29,854 hrs · 26,141 cycles

EEPLS LENS MISSING AT ROW NR 13. REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,606 hrs · 25,939 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP (6 EA) IN CABIN. REPAIRED WIRING AND RELAMPED EEPLS PER MM.

Part: GUIDE ARM — WORN (PAX DOOR) · airframe 29,520 hrs · 25,858 cycles

FWD ENTRY DOOR DIFFICULT TO OPEN AND CLOSE. REMOVED AND REPLACED DOOR GUIDE ARM PER MM.

Part: HOOK — BROKEN (GIRT BAR) · airframe 29,193 hrs · 25,600 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD RETAINER HOOK BROKEN. REMOVED AND REPLACED RETAINER HOOK PER MM.

Part: LENS — MISSING (SLIDE INDICATOR) · airframe 29,193 hrs · 25,600 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND VIEWING WINDOW LENS MISSING. INSTALLED VIEWING WINDOW LENS PER MM.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 29,082 hrs · 25,510 cycles

EEPLS WIRES EXPOSED AT ROW 11. REMOVED AND REPLACED EEPLS TRACK COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 29,011 hrs · 25,458 cycles

EEPLS COVER CRACKED IN CABIN. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,999 hrs · 25,453 cycles

DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 28,314 hrs · 24,918 cycles

EEPLS BROKEN AT OVERWING EXIT. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: SLIDE — OUT OF POSITION (FWD SVC DOOR) · airframe 27,767 hrs · 24,496 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,401 hrs · 22,561 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL WEB CRACKED AT BS 178, WL 180 AT RBL 5.7. REPAIRED WEB PER CASCADE AEROSPACE ERO.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,399 hrs · 22,559 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS INOP AT ROW NR 22 AND AFT. REMOVED AND REPLACED BATTERY PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 25,399 hrs · 22,559 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 230 AT RBL 17.1. REMOVED AND REPLACED WEB PER SRM.

Part: SERVICE DOOR — OUT OF RIG (AFT) · airframe 25,299 hrs · 22,474 cycles

AIR TURNBACK, DURING CLIMB AIRCRAFT WOULD NOT PRESSURIZE. FOUND AFT SVC DOOR OUT OF RIG. RIGGED DOOR, OPS CHECK GOOD PER MM.

Part: COVER — MISSING (CABIN) · airframe 25,176 hrs · 22,382 cycles

EEPLS COVERS MISSING AT MID CABIN. INSTALLED COVERS PER MM.

Part: COVER — MISSING (CABIN) · airframe 25,154 hrs · 22,360 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS COVER MISSING AT ROW 22. INSTALLED COVER PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 24,646 hrs · 21,968 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP AT ROW 18. REPAIRED EEPLS WIRES PER MM.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 24,506 hrs · 21,856 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP IN AFT SECTION. REMOVED AND REPLACED POWER SUPPLY PER MM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 22,153 hrs · 19,839 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 21,858 hrs · 19,601 cycles

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

Part: COVER — MISSING (CABIN FLOOR) · airframe 21,284 hrs · 19,139 cycles

EEPLS TRACK COVER MISSING. REPLACED TRACK COVER PER MM.

Part: FRAME — CRACKED (BULKHEAD) · airframe 20,334 hrs · 18,347 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKS AT LT AND RT SIDE CHORDS, WL 207. REMOVED AND REPLACED SIDE CHORDS PER ACO 7338-53 AND 7342-53.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 19,982 hrs · 18,025 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING O/B AFT T/E FLAP DELAMINATED NEAR I/B END. REPAIRED FLAP PER MM.

Part: GIRT BAR — OUT OF POSITION (ESCAPE SLIDE) · airframe 19,019 hrs · 17,184 cycles

AFT SERVICE DOOR EVACUATION SLIDE GIRT BAR DIFFICULT TO REMOVE AND INSTALL INTO CONTAINER HOOKS. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR)

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

Part: CLAMP — LOOSE (NR 1 ENGINE)

AIR TURNBACK, NR 1 ENG OVERHEAT LIGHT ILLUMINATED DURING CLIMB AFTER NOSE COWL ANTI-ICE VALVE WAS TURNED ON. REPLACED FWD ATTACH ANTI-ICE VALVE CLAMP.

Part: BRACKETS — INCORRECT INSTAL (AFT ENTRY)

AFT ENTRY DOOR EVACUATION SLIDE GIRT BAR RETAINING BRACKETS INCORRECTLY INSTALLED. REINSTALLED BRACKETS PER MM.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE)

AIR TURNBACK, ACFT WOULD NOT MAINTAIN CABIN PRESS AT 27,000 FEET. C/W PRESS DECAY CHECK AND FOUND NR 2 ENG PNEU BLEED PRESS LOW AT IDLE, UNLOCKED NR 2 ENG HIGH STAGE PRESS BLEED VALVE AND OPS CK GOOD PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 12 AND RBL 7. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED A2 CHECK, FOUND FLOOR TRACK LIGHTS AT 16 ROW INOP. RELAMPED FLOOR TRACK AT ROW 16 PER BOEING MM. REMOVED AND REPLACED PER BOEING SRM.

Part: STRAP — NOT SECURED (FWD SERV DOOR)

RETURNED TO BWI, DUE TO FWD SERVICE DOOR STRAP LEFT OUTSIDE AND BANGING AGAINST FUSELAGE. INSPECTED A/C EXTERIOR, NO DEFECTS NOTED.

Part: SLIDE — LOW PRESS (R2 DOOR)

DURING WALKAROUD CHECK, FOUND R2 DOOR SLIDE PRESSURE LOW. REPLACED PER BOEING M/M.

Part: YAW DAMPER — MALFUNCTIONED (AUTO-PILOT)

EN ROUTE, EXPERIENCED UNCOMMANDED YAW INPUT AFTER TAKEOFF. CREW CONTINUED AND LANDED WITHOUT INCIDENT AT OAK. REPLACED YAW DAMPER AND RUDDER PCU PER BOEING M/M.