N648SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2008-02-24 – 2008-02-24 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2008-02-24 – 2008-02-24 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
LT WING NR 3 LEADING EDGE SLAT DELAMINATED. R&R NR 3 SLAT IAW AMM.
RT WING OUTBOARD AFT FLAP DELAMINATED. R&R AFT FLAP PER AMM.
RT WING NR 8 GROUND SPOILED DELAMINATED. R&R #8 SPOILER IAW AMM.
LEFT AFT OVERWING EXIT LIGHT INOPERATIVE. REPLACED THE BULB IAW AMM.
FORWARD EMERGENCY FLASHLIGHT SAFETY STRAP BROKEN. R & R SAFETY STRAP IAW MAINTENANCE.
RT WING INBD AFT FLAP T/E DELAMINATED. R & R AFT FLAP IAW AMM.
RIGHT WING OVERWING EMER HATCH LIGHT DIM. R & R LAMP IAW AMM.
LEFT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 251, AFT OF REAR SPAR. REPAIRED SKIN IAW EA & ER.
RIGHT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 249, AFT OF REAR SPAR. REPAIRED SKIN IAW ER & EA.
LEFT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 269, AFT OF REAR SPAR. REPAIRED SKIN IAW EA & ER.
LEFT WING UPPER SKIN CRACKED, AT FASTENER HOLE AT RSS 268, AFT OF REAR SPAR. REPAIRED SKIN IAW EA & ER.
LEFT WING UPPER SKIN CRACKED, AT FASTENER HOLE AT RSS 239, AFT OF REAR SPAR. REPAIRED SKIN IAW EA & ER.
RIGHT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 237.5, AFT OF REAR SPAR. REPAIRED SKIN IAW EA.
LEFT WING UPPER SKIN CRACKED AT FASTENER HOLE AT RSS 255 AFT OF REAR SPAR. REQUIRED SKIN IAW EA.
RIGHT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 264, AFT OF REAR SPAR. REPAIRED SKIN IAW ER & EA.
RIGHT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 253, AFT OF REAR SPAR. REPAIRED SKIN IAW ER & EA.
LEFT WING RIB CRACKED AT WBL 135.50, AFT LOWER END. REPAIRED RIB IAW EA.
RIGHT WING REAR SHEAR TIE BROKEN AT RSS 201, WBL 135. R & R SHEAR TIE IAW DWG & SRM.
RIGHT WING MLG AFT FITTING CORRODED. R & R FITTING IAW SRM.
LEFT WING PRESS WEB LOWER ANGLE CRACKED AT RSS 277. R & R ANGLE IAW SRM.
RIGHT WING REAR SPAR WEB CRACKED AT RSS 223. REPAIRED WEB IAW ER & EA.
LEFT WING REAR SPAR WEB CRACKED AT RSS 223. REPAIRED WEB IAW EA.
LEFT WING UPPER REAR SPAR CHORD CRACKED AT RSS 223. REPAIRED CHORD IAW EA & ER.
RIGHT WING UPPER REAR SPAR CHORD CRACKED AT RSS 223. REPAIRED CHORD IAW ER & EA.
R1 DOOR AFT FRAME TORQUE BOX CUT OUT AREA AFT LOWER CORNER FRAME CRACKED. R & R R1 DOOR IAW AMM.
R2 DOOR EMER EVAC SLIDE CABLE MISROUTED. REROUTED CABLE IAW AMM.
RIGHT WING NR 7 SPOILER DELAMINATED. R & R SPOILER ASSEMBLY IAW MM.
R2 DOOR EMER EVAC SLIDE ASSEMBLY OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW MT.
RIGHT WING NR 4 SLAT CRACKED ON BRACKET LOCATED ON SEAL DOOR ACTUATOR. REPLACED NR 4 SLAT IAW SRM & DWG.
THE STRINGER CLIP WAS FOUND CRACKED AT BS 360, STRINGER 2L. R&R THE STRINGER CLIP IAW THE SRM.
TIE CLIP CRACKED AT STATION 360, STRINGER 2R. R & R CLIP IAW SRM.
FUSELAGE WEB CRACKED AT STATION 727 BETWEEN RBL 38 & RBL 45. R & R WEB IAW SRM.
VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW EA.
SPLICE STRAP CRACKED AT BS 360, STRINGER 3R. REPAIRED STRAP IAW EA.
STRINGER SPLICE CRACKED AT BS 908, STRINGER 4L. REPAIRED SPLICE IAW EA.
FORWARD CABIN PHOTO LUMINESCENT STRIP DAMAGED. R & R STRIP IAW AMM.
FOUND AN INTERCOSTAL CRACKED AT BS 277 - 292, STRINGER 11R. REPAIRED THE INTERCOSTAL IAW EA.
LEFT WING INBD FIXED LE SKIN CRACKED AT STATION 208. REPAIRED SKIN IAW EA.
FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A, LT SIDE. REPAIRED CHORD IAW EA.
FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A RT. REPAIRED CHORD IAW EA.
L2 DOOR EMER EVAC SLIDE RELEASE CABLE DISCONNECTED. RECONNECTED SLIDE IAW MT.
BULLNOSE EXIT LIGHT BROKEN AT ROW 6 ABC. R & R LIGHT IAW MM.
BULLNOSE EXIT LIGHT BROKEN AT ROW 2 ABC. R & R LIGHT IAW MM.
INFLIGHT SHUTDOWN, AIR TURN BACK & DECLARED EMER. NR 1 ENG OIL PRESS LOW ON TAKEOFF & CLIMB OUT, INDICATED IN YELLOW BAND. NO OIL PRESS LIGHT ILLUMINATED. R & R NR 1 ENG OIL PRESS GAUGE IAW MM.
FRAME INNER CHORD CRACKED AT BS 348.2 STRINGER 17L. R & R CHORD IAW EA.
STRAP CRACKED AT BS 348.2 STRINGER 16L. R & R STRAP IAW SRM & DWG.
LEFT EMER OVERWING EXIT SIGN LOOSE. SECURED SIGN IAW AMM.
LEFT WING NR 1 FLIGHT SPOILER DELAMINATED. R & R NR 1 SPOILER IAW MM.
DIVERSION DECLARED EMERGENCY. A HYD SYS FAILED BOTH LOW PRESS LIGHT ILLUMINATED & A QTY DEPLETED. R & R A ELEC HYD PUMP IAW MM.
L1 DOOR OVERHEAD EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.
R2 DOOR EMER EVAC SLIDE RELEASE CABLE FRAYED. R & R CABLE IAW AMM.
L2 DOOR EMER EVAC SLIDE RELEASE CABLE FRAYED. R & R CABLE IAW MM.
BUTT STRAP DAMAGED AT BS 908, BETWEEN STRINGER 3L TO STRINGER 3R. R & R BUTT STRAP IAW DWG.
LOWER FWD WINDOW CORNER STRINGER SPLICE CRACKED AT BS 727+10, STRINGER 13R. R & R SPLICE IAW EA.
RIGHT BS 360+10 UPPER FWD WINDOW CORNER STRINGER 11 SPLICE ANGLE CRACKED IN HOLE 5. R & R ANGLE IAW DWG.
RIGHT BS 887+10 WINDOW FRAME FORGING CRACKED AT HOLE NR 5. R & R FORGING IAW BAC.
RIGHT BS 887+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.
LEFT BS 887+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
LEFT BS 867+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED AT HOLE 3. REPAIRED SKIN IAW EA.
LEFT BS 727+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.
RIGHT BS 887+10 LWR FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
RIGHT BS 807+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
LEFT BS 847+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.
LEFT BS 807+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.
LEFT BS 787+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.
RIGHT BS 867+10 LOWER FWD WINDOW CORNER CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.
RIGHT BS 847+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.
RIGHT BS 787+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.
RIGHT BS 727B+10 WINDOW FRAME FORGING CRACKED AT HOLE 7. R & R FORGING IAW DWG.
RIGHT BS 807+10 WINDOW FRAME FORGING CRACKED AT HOLE NR 11. R & R FORGING IAW DWG.
LEFT WING OTBD FOREFLAP, INBD TE DELAMINATED. R & R FORE FLAP ASSEMBLY IAW MM.
SKIN CRACKED AT BS 500D+11 STRINGER 10R. REPAIRED SKIN IAW EA.
AIR TURN BACK, DECLARED EMERGENCY AFTER TAKEOFF. AT APPROXIMATELY 4000 FEET FWD LAVATORY SMOKE ALARM WAS ON WITH AN ACRID SMELL. RETURNED TO MIDWAY. R & R COALESCENT BAGS IAW MM.
LOUD NOISE & VIBRATION ON CLIMB OUT & SLIGHT SMELL IN MID CABIN. WENT TO HIGH IN PACKS, CLEARED SMELL. SWITCHED TO ALT COOLING FAN, VIBRATION STOPPED. GASPAR FAN OFF ENTIRE TIME. R & R EQUIPMENT COOLING BLOWER MOTOR IAW MMM.
DECLARED EMERGENCY NR 1 FUEL QUANTITY INDICATOR CLIMBED TO 10.8 THEN DESCENDED TO "0". FMC FUEL QUANTITY ERRATIC. NR 2 FUEL QUANTITY APPEARED TO BE DECREASING AT AN ABNORMAL RATE. R & R NR 1 FUEL TANK TSO & HARNESS IAW MM.
SLIGHT ELECTRICAL ODOR NOTED IN COCKPIT & CABIN WHEN RECIRCULATING FAN WAS ON. R & R FAN IAW MM.
FWD AISLE EMERGENCY EXIT SIGN LENS CRACKED. R & R LENS IAW MM.
LT AFT WING EMERGENCY LIGHT INOP. R & R LIGHT IAW MM.
RT EMERGENCY EXIT LIGHT INOP BETWEEN ROW 1 TO ROW 5. R & R BATTERY PACK IAW AMM.
FWD GALLEY EMERGENCY EXIT LIGHT INOP. REPAIRED BATTERY PACK IAW AMM.
LEFT ELEVATOR CLIP CRACKED AT ELEVATOR STA 63.93. R & R CLIP IAW SRM AND DWG.
SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.
AFT CARGO COMPARTMENT DOOR INTERIOR HANDLE OF INTERNAL PANEL COLLAR CRACKED. REMOVED AND REPLACED PANEL IAW SRM AND DRAWING.
WEB CRACKED BETWEEN BS 500B TO BS 500C, STR 26R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.
EMERGENCY EXIT LIGHT LENS LOCATED ON CURVED CEILING PANEL AT FWD CABIN BROKEN. REMOVED AND REPLACED LENS IAW AMM.
WEB CRACKED BETWEEN BS 500B TO 500C, STR 26L. REMOVED AND REPLACED WEB IAW SRM AND DWG.
REVEAL STRIP CRACKED AT BS 794, BETWEEN STR 19R TO STR 25R. REMOVED AND REPLACED REVEAL STRIP IAW SRM AND DWG.
LEFT OVERWING SUPPORT ASSY CRACKED. REMOVED AND REPLACED SUPPORT ASSY IAW DWG.
RIGHT WING OVERWING SUPPORT ASSY PANEL CRACKED. REMOVED AND REPLACED PANEL IAW DWG.
WEB CRACKED BETWEEN BS 178 TO BS 188, WL 207.8. REMOVED AND REPLACED WEB IAW SRM.
WEB CRACKED BETWEEN BS 616 AND BS 639, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.
SUPPORT BRACKET CRACKED BETWEEN BS 663.75 TO BS 675, BETWEEN RBL 30 TO RBL 40. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.
CLIP CRACKED AT BS 178, RBL 25. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.
LEFT SIDE ANGLE CRACKED AT BS 178, LBL 13.83. REMOVED AND REPLACED ANGLE IAW AND DRAWING.
WEB CRACKED BETWEEN BS 188 TO BS 196.5, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.
CHANNEL CRACKED BETWEEN BS 616 TO BS 639, STR 2R. REMOVED AND REPLACED CHANNEL IAW SRM AND DRAWING.
VERTICAL DUCT ASSY WEB CRACKED BETWEEN BS 294.5 TO BS 312, STR 27R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.
WEB CRACKED BETWEEN BS 188 TO BS 195.5, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.
INNER CHORD WEB AND STUB BEAM CRACKED AT BS 616, WL 208. R & R STUB BEAM IAW EA.
WEB CORRODED BETWEEN BS 807 TO BS 827, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.
BULKHEAD RT SIDE CHORD CRACKED AT BS 178, WL 217 LT SIDE. R & R CHORD IAW EA.
FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME IAW SRM AND DWG.
BULKHEAD RT SIDE CHORD CRACKED AT BS 178, WL 217 RT SIDE. R & R CHORD IAW EA.
INTERCOSTAL CRACKED BETWEEN BS 639 TO BS 663.75, STR 15R. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DRAWING.
CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
CLIP CRACKED AT BS 580, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.
ATTACH CLIP CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED ANGLE IAW AND DWG.
THRESHOLD WEB CORRODED BETWEEN BS 947.5 TO BS 987, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME IAW SRM AND DWG.
INNER CHORD AND WEB CRACKED AT BS 616, STR 18L. REPAIRED INNER CHORD, OUTER CHORD AND WEB IAW EA.
INNER CHORD AND WEB CRACKED AT BS 616, STR 18L. REPAIRED INNER CHORD, OUTER CHORD AND WEB IAW EA.
CHANNEL STRINGER CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER IAW SRM.
SHEAR TIE CORRODED AT BS 325.38, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DRAWING.
ANGLE CRACKED AT BS 328, RBL 55. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.
STOP PAD CRACKED AT BS 616, STR 11R. REMOVED AND REPLACED STOP PAD IAW SRM.
VERTICAL DUCT ASSY CHANNEL CRACKED BETWEEN BS 294.5 TO BS 312, STR 27R. REMOVED AND REPLACED CHANNEL IAW SRM & DRAWING.
TIE CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
CLIP CRACKED AT BS 580, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.
WEB CORRODED BETWEEN BS 400 TO BS 420, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.
DUCT ASSY CRACKED BETWEEN BS 294.5 TO BS 312, BETWEEN STR 26R TO STR 26L. REPAIRED DUCT ASSY IAW EO AND EA.
SUPPORT ANGLE CRACKED AT BS 328, RBL 34. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
SUPPORT ANGLE CRACKED AT BS 325.38, BETWEEN STR 20L TO STR 21L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
SUPPORT ANGLE CRACKED BETWEEN 380 TO BS 400, BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.
ANGLE CRACKED BETWEEN BS 294.5 TO BS 312, STR 25L. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.
TIE CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG 46525.
CLIP CRACKED AT BS 560, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
SUPPORT CLIP CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.
STRAP CRACKED BETWEEN BS 277 TO BS 294.5, STR 17R. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.
SIDEWALL PANEL CRACKED AT BS 380, BETWEEN STR 25L TO STR 28L. REMOVED AND REPLACED PANEL IAW SRM AND DRAWING.
WEB CRACKED BETWEEN BS 351 TO BS 360, BL 0. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.
THRESHOLD WEB CRACKED BETWEEN BS 294.5 TO BS 328, STR 17R. REMOVED AND REPLACED WEB IAW SRM & DWG.
WEB CRACKED AT BS 328, BETWEEN STR 23R TO STR 24R. REMOVED AND REPLACED WEB IAW SRM.
WEB CRACKED BETWEEN BS 500A TO BS 500B, STR 26R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.
STRINGER SPLICE CORRODED AT BS 787+3, STR 22R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.
FLOORBEAM UPPER CHORD CORRODED AT BS 967, LBL 27. REPAIRED BEAM IAW EA.
STRINGER SPLICE CORRODED AT BS 787+3, STR 21R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.
VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB IAW SRM.
TIE CLIP CRACKED AT BS 947.5, STR 23R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
LONGITUDINAL FLOORBEAM WEB CRACKED ON ACCESS PANEL 2212 AT CONTROL CABIN. REPAIRED WEB IAW EA.
SKIN CRACKED AT BS 328, STR 17R. REPAIRED SKIN IAW SRM.
FRAME WEB CRACKED AT BS 420, BETWEEN STR 11L TO STR 13L. REPAIRED WEB IAW SRM.
VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB IAW SRM.
CHANNEL CRACKED AT BS 540, LBL 1.0. REMOVED AND REPLACED CHANNEL IAW SRM AND DRAWING.
RUB STRIPS MISSING ON CUT OUT OF NACELLE STRUT ACCESS NR 5831R ENGINE NR 2. INSTALLED RUB STRIP IAW DWG.
CHANNEL CRACKED AT BS 540, RBL 1.0. REMOVED AND REPLACED CHANNEL IAW SRM AND DRAWING.
STRINGER CORRODED BETWEEN BS 967 TO BS 986.5, STR 21R. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.
RUB STRIP MISSING ON CUT OUT OF NACELLE STRUT ACCESS NR 5828R ENGINE NR 2. INSTALLED RUB STRIP IAW DWG.
STOP PAD FITTING CRACKED BETWEEN BS 616 TO BS 639, STR 11L. REMOVED AND REPLACED FITTING IAW DWG.
SUPPORT ANGLE CRACKED AT STA 540, RBL 1.0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
RUB STRIPS MISSING ON CUT OUT OF NACELLE STRUT ACCESS NR 5827R ENGINE NR 2. INSTALLED RUB STRIP IAW DWG.
NR 1 ENGINE STRUT TORQUE BOX ACCESS NR 5757L ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED TIE CLIP IAW EA.
WEB CRACKED BETWEEN BS 277 TO BS 291.5, STR 14R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.
ANGLE CRACKED AT BS 540, LBL 1.0. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.
SUPPORT ANGLE CRACKED AT BS 344, BETWEEN STR 4L TO STR 7L. REMOVED AND REPLACED ANGLE AND IAW SRM AND DRAWING.
ANGLE CRACKED AT BS 947.5, BETWEEN STR 24L TO STR 25L. REMOVED AND REPLACED ANGLE IAW SRM.
FLOOR STRUCTURE BEAM UPPER CHORD CRACKED AT BS 947.5, LBL 54. REPAIRED CHORD IAW EA.
FRAME CRACKED AT BS 947.5, STR 19R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.
ANGLE CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
SUPPORT ANGLE CRACKED BETWEEN BS 277 TO BS 291.5, STR 13R. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.
STIFFENER CRACKED BETWEEN BS 294.5 TO BS 303.9, STR 16L. REMOVED AND REPLACED STIFFENER IAW SRM AND DRAWING.
STIFFENER CRACKED BETWEEN BS 294.5 TO BS 303.9, STR 15L. REMOVED AND REPLACED STIFFENER IAW SRM AND DRAWING.
ANGLE CRACKED AT BS 540, STR 22L. REPAIRED ANGLE IAW SRM.
STIFFENER CRACKED BETWEEN BS 312 TO BS 328, RBL 30. REMOVED AND REPLACED STIFFENER IAW SRM AND DRAWING.
L1 DOOR EMERGENCY EVAC SLIDE SUPPORT NUT PLATE BROKEN. REMOVED AND REPLACED NUT PLATE IAW SRM.
FORWARD ENTRY DOOR FWD CORNER OF LOWER TRIM SWEEPER PLATE CRACKED. REMOVED AND REPLACED PLATE IAW SRM AND DRAWING.
ANGLE CRACKED AT BS 540, STR 22R. REPAIR ANGLE IAW SRM.
FLOORBEAM CORRODED AT BS 986.5, RBL 45.5. REPAIRED CHORD IAW EA.
STRAP CRACKED BETWEEN BS 306 TO BS 348.5, RBL 46. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.
STUB FRAME CRACKED AT BS 296.4, STR 7R. REPAIRED STUB FRAME IAW EA.
WEB CRACKED AT BS 520+5, BETWEEN STR 22L TO STR 24L. REMOVED AND REPLACED WEB IAW SRM AND DWG.
ANGLE CRACKED AT BS 440, STR 26L. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.
SUPPORT ANGLE CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
Z-ANGLE CORRODED BETWEEN BS 294.5 TO BS 360, LBL 62. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 500D, STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.
STRAP CRACKED BETWEEN BS 306 TO BS 348.5, LBL 33. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.
FLOORBEAM CORRODED AT BS 328, RBL 45. REPAIRED BEAM IAW SRM AND EA.
STRAP CRACKED BETWEEN BS 306 TO BS 348.5, LBL 10. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.
STRAP CRACKED BETWEEN BS 306 TO BS 348.5, BL 0. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.
STRAP CRACKED BETWEEN BS 306 TO BS 348.5, LBL 45.5. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.
FLOORBEAM CORRODED AT BS 967, BETWEEN BL 0 TO RBL 40. REPAIRED BEAM IAW EA.
FLOORBEAM CORRODED AT BS 328, LBL 52. REPAIRED CHORD IAW SRM.
SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.
FRAME CORRODED AT BS 727E, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME IAW SRM.
ACCESS PANEL AFT EDGE STRIP CRACKED ON NR 3403R. REMOVED AND REPLACED STRIP IAW SRM AND DRAWING.
CHANNEL CRACKED BETWEEN BS 420 TO BS 440, STR 26R. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.
CHANNEL CRACKED BETWEEN BS 500 TO BS 500A, STR 26R. REMOVED AND REPLACED ZEE ANGLE IAW SRM AND DWG.
WEB CRACKED AT BS 712, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED WEB IAW SRM AND DWG.
SUPPORT CHANNEL CRACKED AT BS 727A, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED CHANNEL IAW SRM & DRAWING.
RUB STRIP MISSING AT INTERNAL AREA OF CUT OUT OF PYLON ACCESS PANEL 5724L NR 1 ENGINE. INSTALLED RUB STRIP IAW DWG.
TIE CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM.
SKIN CUTOUT CRACKED AT BS 328, STR 17R. REPAIRED SKIN IAW SRM.
LEFT WING NR 2 SLAT TRACK CORRODED ON ROLLER. REMOVED AND REPLACED ROLLER IAW AMM.
STIFFENER CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.
FRAME CORRODED AT BS 500A, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME IAW SRM.
FRAME CORRODED AT BS 500B, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME IAW SRM.
FRAME CORRODED AT BS 500, BETWEEN STR 28L AND STR 28R. REPAIRED FRAME IAW SRM.
STRINGER CORRODED BETWEEN BS 460 AND BS 480, STR 27R. REMOVED AND REPLACED STRINGER IAW SRM AND DRAWING.
STIFFENER CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED STIFFENER IAW SRM AND DRAWING.
SUPPORT ANGLE CRACKED AT BS 727, RBL 3. REMOVED AND REPLACED ANGLE IAW SRM.
FRAME LOWER FLANGE CORRODED AT BS 727E, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.
LEFT WING AILERON ANGLE CRACKED AT LEVEL OF RSS 533 INTERIOR CAVITY. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
SKIN CRACKED AT BS 715 AND STR 27L. REPAIRED SKIN IAW SRM.
STUB BEAM CRACKED AT BS 706, BETWEEN LBL 45.57 AND LBL 60.5. REPAIRED STUB BEAM IAW EO AND EA.
RIGHT WING NR 6 SLAT LOWER SURFACE CRACKED. REPAIRED NR 6 SLAT IAW SRM.
SKIN CRACKED AT BS 520 +7, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN IAW EA.
R1 DOOR EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED LENS IAW AMM.
CRACKED LOCATED ON MAIN WHEEL WELL PRESSURE DECK LOCATED AT BS 665.75, RBL 39.5. REPAIRED PRESSURE DECK IAW SRM.
CRACKED LOCATED ON MAIN WHEEL WELL PRESSURE DECK LOCATED AT BS 672.75, RBL 42. REPAIRED DECK IAW SRM.
CRACKED FOUND ON MAIN WHEEL WELL PRESSURE DECK LOCATED AT BS 674.25, RBL 37. REMOVED AND REPLACED DOUBLER IAW SRM AND DWG.
LEFT WING NR 2 SLAT LOWER SURFACE CRACKED. REPAIRED SKIN IAW SRM.
LEFT WING NR 1 SLAT LOWER SURFACE CRACKED. REPAIRED SKIN IAW SRM.
RIGHT WING NR 5 SLAT LOWER SURFACE CRACKED. REPAIRED NR 5 SLAT IAW SRM.
LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75, RBL 24.5. REPAIRED CHORD IAW EA.
STUB FRAME CRACKED AT BS 706, BETWEEN RBL45.5 TO RBL 60.5. REPAIRED BEAM IAW EA.
LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75+8, LBL 24.5. REPAIRED BEAM IAW EA.
MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 665.25, LBL 39. REPAIRED WEB IAW EO AND EA.
MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 665.75, LBL 42.5. REPAIRED WEB IAW EO.
STUB BEAM CRACKED AT BS 685, BETWEEN LBL 45.57 AND LBL 60.5. REPAIRED BEAM IAW EA.
MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 672.75, LBL 42. REPAIRED WEB IAW EO AND EA.
RIGHT SIDE CRACKED LOWER CHORD LOCATED AT MAIN LANDING GEAR BAY AT BS 680. REMOVED AND REPLACED CHORD IAW SRM AND DRAWING.
FUSELAGE CRACKED AT BS 500D+9 ABOVE STR 10L. REPAIRED SKIN PER EA.
FUSELAGE CRACKED AT BS 500D+9 ABOVE STR 9L. REPAIRED SKIN PER EA.
SPLICE CHANNEL CRACKED AT BS 360, STR 28L. REMOVED AND REPLACED CHANNEL IAW SRM AND EA.
SKIN CRACKED AT BS 360 + 19, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN IAW AAR EA.
DURING SCHEDULED MV2 CHECK, FOUND RT WING T/E EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
DURING SCHEDULED CV CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING. INSTALLED LENS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500B+7, STR 4L. REPAIRED SKIN PER EA.
DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER EA AND EA.
DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, RBL 45.5. REPAIRED WEB PER ER.
DURING SCHEDULED 14Y CHECK, FOUND FRAME CAP CORRODED AT BS 847, STR 25R. REMOVED AND REPLACED FRAME PER SRM.
DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER ER.
DURING SCHEDULED 14Y CHECK FOUND, VERTICAL SUPPORT BEAM WEB CRACKED AT BS 180, LBL 5.7. REPAIRED WEB PER SRM.
DURING SCHEDULED 14Y CHECK FOUND, FAIL-SAFE FRAME CORRODED AT BS 807, STR 27L. REMOVED AND REPLACED FRAME PER SRM.
DURING SCHEDULED MV2 CHECK, FOUND NR 4 FLIGHT SPOILER HINGE BROKEN. REMOVED AND REPLACED SPOILER ASSY PER MM.
INFLIGHT SHUTDOWN/ DECLARED EMERGENCY. NR 2 ENGINE SHUTDOWN INFLIGHT DUE TO "0" OIL QUANTITY AND "0" OIL PRESSURE. FOUND AGB PAD LEAKED. REMOVED AND REPLACED AGB COVER.
DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE COVER GIRT BAR AFT STORAGE CLIP BROKEN. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED MV2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 1 TO ROW 4. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED 2HC2 CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVE AND REPLACED TAB PER MM.
DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 807, BETWEEN STR 27R TO STR 26L. REPAIRED FRAME PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 767, BETWEEN STR 25L TO STR 25R. REPAIRED FRAME PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 947, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND 178 PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED BETWEEN BS 172 TO BS 176, RBL 17.0. REMOVED AND REPLACED WEB PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 2R. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4R. REMOVED AND REPLACED STR CLIP PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED STR CLIP PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED STR CLIP PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2L. REMOVED AND REPLACED STR CLIP PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STR CLIP PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED STR CLIP PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND LT HORIZONTAL STAB L/E NR 6 RIB CRACKED. REPAIRED RIB PER SRM.
R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.
DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 528, STR 19R. REPAIRED SKIN PER SWA EA.
DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
KEEL BEAM LOWER SKIN PANEL CRACKED AT FS 726.75, RBL 6.30. REPAIRED PANEL PER SRM.
DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DSBONDED AT OUTBOARD END. R&R FLAP PER MM.
DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED HC1 CHECK, FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR TORQUE TUBE BEARINGS HAVE RADIAL PLAY. REMOVED AND REPLACED TORQUE TUBE BEARINGS PER MM.
DURING SCHEDULED 10Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE, HORN BEARING AND BOLTS PER MM.
DURING SCHEDULED 10Y CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE AND HORN BEARING PER MM.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD UPPER SURFACE DELAMINATED. R&R AFT FLAP PER MM.
DURING SCHEDULED 10Y CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT PER MM.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R AND 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R AND 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R AND 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R AND 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.
DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 ABC. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.
DURING SCHEDULED SPV CHECK, FOUND FWD LAV EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.
DURING SCHEDULED SPV CHECK, FOUND FWD RT EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.
DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.
DURING SCHEDULED C2 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT FLAP PER MM.
DURING SCHEDULED C1 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT SIGN LENS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM.
DURING SCHEDULED C4 CHECK, FOUND LT WING T/E INBD FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.
DIVERSION, EVIDENCE OF ELECTRICAL ODOR IN COCKPIT. FOUND WIRES DAMAGED IN OVERHEAD P-5 PANEL, NR 1 ENGINE FUEL SHUT-OFF VALVE & MLG POSITION SENSOR CIRCUIT BREAKERS POPPED. REPAIRED WIRES PER SWPM. REMOVED AND REPLACED P52 FUEL MODULE & T492 LEFT MLG POSITION SENSOR PER MM.
DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.
DURING SCHEDULED C2 CHECK, FOUND L1 & R1 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.
R1 DOOR LOWER EMERGENCY EXIT SIGN LENS LOOSE. SECURED EXIT SIGN LENS PER MM.
R1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM.
DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 664, LBL 31.5, CRACKED. REPAIRED PRESSURE WEB PER SRM.
DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.
DURING SCHEDULED 1/4D CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED RT WING AILERON TAB PER MM.
DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E MID FLAP, CRACKED. REPAIRED RT WING MID FLAP PER SRM.
DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING AFT FLAP PER MM.
L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.
R1 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.
L2 DOOR SLIDE PRESSURE GAUGE IN THE RED. REMOVED AND REPLACED L2 DOOR SLIDE PER MM.
DIVERSION, LANDING GEAR WOULD NOT RETRACT. FOUND, LANDING GEAR LEVER LATCH CIRCUIT BREAKER TRIPPED, RESET CIRCUIT BREAKER AND CYCLED GEAR PER MM. OPS CHECKED GOOD PER MM.
DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
L1 DOOR ESCAPE SLIDE PARTIALLY FELL OUT OF CONTAINER. REINSTALLED THE L1 ESCAPE SLIDE PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND LT MLG STRUT AND TRUNNION PIN CORRODED. REMOVED AND REPLACED LT MLG STRUT AND TRUNNION PIN PER MM.
FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.
DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED AT STOP CUTOUT, 4TH FROM TOP. REPAIRED FRAME PER SRM.
DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 986.5, STR 24L. REMOVED AND REPLACED STR CLIP PER SRM.
DURING SCHEDULED 1/2D CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.
AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR LENS LOOSE. SECURED LENS ASSY PER MM.