N387SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2009-07-13 – 2009-07-13 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2009-07-13 – 2009-07-13 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AFT CARGO DOOR CUTOUT AFT EDGE, FINGER EDGE COVER, LOWER END CRACKED. REPAIRED CUTOUT PER EA.
R2 DOOR EMERGENCY EVAC SLIDE MOUNT BRACKET CRACKED. R&R BRACKET PER AMM.
R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
RIGHT OVERWING EMERGENCY EXIT LIGHT BROKEN. R & R THE LIGHT ASSEMBLY IAW AMM.
R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BEZEL CRACKED. REPAIRED LENS PER MM.
LT ELEVATOR TAB INBOARD ATTACH CUTOUT DAMAGED AT UPPER INBOARD EDGE. R&R LT ELEVATOR TAB IAW AD & EA.
RT ELEVATOR TAB MECHANISM INBOARD AND OUTBOARD AFT HINGE BUSHING CORRODED. R&R MECHANISM IAW AMM & EA.
RT ELEVATOR INBOARD AFT TAB MECHANISM BEARING CRACKED. R&R MECHANISM IAW AMM & EA.
RT INBOARD ELEVATOR CONTROL ROD CORRODED. R&R CONTROL ROD IAW AMM & EA.
RT OUTBOARD ELEVATOR TAB CONTROL ROD CORRODED. R&R CONTROL ROD IAW AMM & EA.
LT OUTBOARD ELEVATOR CONTROL ROD CORRODED. R&R CONTROL ROD IAW AMM & EA.
LT INBOARD ELEVATOR CONTROL ROD CORRODED. R&R CONTROL ROD IAW AMM & EA.
RIGHT FORWARD EMERGENCY FLASHLIGHT SAFETY STRAP BROKEN. R&R THE STRAP IAW AMM.
LEFT FORWARD EMERGENCY FLASHLIGHT SAFETY STRAP BROKEN. R & R THE STRAP IAW AMM.
R2 DOOR EMERGENCY SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
LT AFT ENTRY DOOR CEILING EMERGENCY LIGHT INOP. R&R BATTERY PACK IAW AMM.
L1 DOOR EMERGENCY EXIT SIGN MISSING. R & R SIGN IAW MM.
RT WING NR 5 GROUND SPOILER INBOARD LUG BROKEN. R&R NR 5 GROUND SPOILER PER AMM.
RIGHT WING RT 4 LE SLAT DELAMINATED INBD EDGE. R & R SLAT IAW AMM.
CENTER TANK STIFFENER CRACKED AT BS 546, LBL 58. R & R STIFFENER IAW SRM.
L1 DOOR BEAR STRAP SKIN CUT OUT CRACKED AT BS 303.9, STRINGER 13L. REPAIRED CUT OUT IAW SRM.
STRINGER SPLICE CRACKED AT BS 360, STRINGER 4L. REMOVED SPLICE IAW ER & EA.
STRINGER SPLICE CRACKED AT STATION 360, STRINGER 15L. R & R STRINGER SPLICE IAW SRM.
R1 DOOR MOP SILL CORRODED. R & R MOP SILL IAW SRM.
RIGHT WING OTBD VERTICAL ATTACH ANGLE, CRACKED AT 2ND OTBD AILERON SWEEPER WEB. R & R ANGLE IAW SRM.
FUSELAGE FRAME CRACKED AT STATION 328, STRINGER 20R - 21R. REPAIRED FRAME IAW ACO.
LONGITUDINAL FLOORBEAM SUPPORT BRACKET ANGLE CRACKED AT BS 727B, BBL 0. REPAIRED ANGLE IAW SRM.
STRINGER CLIP CRACKED AT STATION 490, STRINGER 24R. R & R CLIP IAW SRM.
L1 DOOR EMER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.
FORWARD ENTRY DOOR EMER EXIT LIGHT COVER LOOSE. R & R LIGHT COVER IAW SIP.
L1 DOOR INNER SKIN CRACKED BELOW THE TORQUE BOX. REPAIRED SKIN IAW EA.
LEFT WING NR 2 SLAT DELAMINATED INBD & OTBD TE. R & R NR 2 SLAT IAW MM.
R2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.
L2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
R1 DOOR CRACKED LOWER EDGE FRAME AT AFT LOWER CORNER STOP FITTING. R & R DOOR IAW AMM.
FORWARD FLASHLIGHT BROKEN. R & R FLASHLIGHT IAW CMM.
R1 DOOR EMER EVAC SLIDE FLOOR BRACKETS ADAPTER PLATE DAMAGED. R & R PLATE IAW AMM.
LEFT EEPLS BROKEN BETWEEN BS 342 TO BS 380. R & R EEPLS IAW DWG.
R2 DOOR EMERGENCY EVAC SLIDE FLOOR BRACKETS ADAPTER PLATE DAMAGED. R & R PLATE IAW AMM.
SPLICE FITTING CORRODED AT BS 663, LT WING WL 71.24. R & R FITTING IAW EA & DWG.
LEFT WW BULKHEAD FITTING CORRODED AT BS 663, WL 71.24. REPAIRED FITTING IAW EO & EA.
LEFT WING NR 3 FLAP TRACK FAIRING ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.
RIGHT WING NR 6 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.
LEFT WING NR 3 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.
RIGHT WW BULKHEAD FITTING CORRODED AT BS 663, BETWEEN WBL 71.24 TO WL 194. REPAIRED FITTING IAW EO & EA.
RIGHT WING SPLICE FITTING CORRODED AT BS 663, BETWEEN WBL 71.24 TO WL 194. R & R FITTING IAW EO & EA.
AFT CARGO COMPARTMENT WEB CORRODED BETWEEN BS 947.5 TO BS 967, BETWEEN STRINGER 25R TO STRINGER 26R. R & R WEB IAW SRM & DWG.
LEFT WING NR 3 FLAP TRACK FAIRING STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.
CHANNEL STIFFENER CRACKED AT BS 1016+1, RBL 1. REPAIRED STIFFENER IAW EA.
FRAME LOWER FLANGE CORRODED AT BS 747, BETWEEN STRINGER 25R TO STRINGER 26R. REPAIRED FRAME IAW SRM.
LEFT WING REAR SPAR UPPER CHORD CRACKED BETWEEN RSS 224.14 TO 215.97. REPAIRED CHORD IAW EO & EA.
RIGHT WING TO BODY FAIRING SUPPORT LOWER STRUCTURE SKIN SPLICE CRACKED AT BS 680 WW AREA. R & R SPLICE IAW SRM & DWG.
RIGHT WING REAR SPAR UPPER CHORD CRACKED BETWEEN RSS 224.14 TO 215.97. REPAIRED CHORD IAW EO & EA NO.
RIGHT WING TO BODY FAIRING LOWER SUPPORT STRUCTURE ANGLE CRACKED AT BS 680, WW AREA. R & R ANGLE IAW SRM & DWG.
LEFT WING INBD FIXED LE SKIN CRACKED AT 208. REPAIRED SKIN IAW EA.
LEFT WING NR 2 SPINDLE CARRIAGE WORN OF THE INNER RACE. R & R BEARING ASSEMBLY IAW CMM.
RIGHT WING NR 6 FLAP TRACK FAIRING STIFFENER CRACKED. R & R STIFFENER IAW SRM.
LEFT WING NR 3 FLAP TRACK FAIRING DOUBLER CRACKED. R & R DOUBLER IAW SRM & DWG.
RIGHT WING NR 7 SPINDLE CARRIAGE INBD WORN OF THE INNER RACE. R & R BEARING ASSEMBLY IAW CMM.
RIGHT WING NR 8 SPINDLE CARRIAGE INBD WORN OF THE INNER RACE. R & R BEARING ASSEMBLY IAW CMM.
SHEAR TIE CRACKED AT BS 344, BETWEEN STRINGER 27R TO STRINGER 26R. R & R SHEAR TIE IAW SRM & DWG.
AFT CARGO COMPARTMENT DOME WEB CRACKED AT BS 1016, RBL 5. REPAIRED WEB IAW EA.
SUPPORT ANGLE CRACKED AT BS 312+9, STRINGER 20L. R & R ANGLE IAW SRM & DWG.
SUPPORT ANGLE CRACKED AT BS 336, STRINGER 20L. R & R ANGLE IAW SRM & DWG.
RIGHT WING SUPPORT ANGLE INTERNAL AREA OF RSS 507 CRACKED. R & R ANGLE IAW SRM & DWG.
AFT PRESS BULKHEAD DOME CAP WEB CRACKED AT BS 1016, STRINGER 18R. REPAIRED WEB IAW SRM.
SKIN CRACKED AT BS 727D, BETWEEN STRINGER 27L TO 27R. REPAIRED SKIN IAW EA.
RIGHT WING SUPPORT ANGLE INTERNAL AREA CRACKED AT RSS 533. R & R ANGLE IAW SRM & DWG.
SUPPORT BRACKET CRACKED AT BS 294.5, STRINGER 23L. R & R BRACKET IAW SRM & DWG.
L1 DOOR LOWER SEAL SWEEPER RETAINER PLATE CRACKED. R & R PLATE IAW SRM & DWG.
TIE CLIP BROKEN AT BS 787, STRINGER 23R. R & R TIE CLIP IAW SRM.
AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 947.5, BETWEEN STRINGER 24R TO STRINGER 25R. R & R ANGLE IAW SRM & DWG.
TIE CLIP CRACKED AT BS 727B, STRINGER 25L. R & R TIE CLIP IAW SRM & DWG.
TIE CLIP CRACKED AT BS 727B, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.
TIE CLIP CRACKED AT BS 727A, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.
TIE CLIP CRACKED AT BS 727C, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.
TIE CLIP CRACKED AT BS 727D, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.
TIE CLIP CRACKED AT BS 727E, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.
TIE CLIP CRACKED AT BS 747, STRINGER 21L. R & R TIE CLIP IAW SRM & DWG.
TIE CLIP CRACKED AT BS 747, STRINGER 20L. R & R TIE CLIP IAW SRM.
RIGHT WING FUEL TANK RIB LOWER CHORD CRACKED AT WBL 135.5 IN THE RADIUS AREA BETWEEN STRINGER 2 & 3. REPAIR CHORD IAW EA.
TIE CLIP CRACKED AT BS 747, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.
CLIP CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW SRM & DWG.
TIE CLIP CRACKED AT BS 727A, STRINGER 19L. R & R TIE CLIP IAW SRM & DWG.
RIGHT WING FUEL TANK WBL 114.00 RIB UPPER CHORD CRACKED NEXT TO STRINGER 2. REPAIRED CHORD IAW EO & EA.
FRAME ANGLE CORRODED AT BS 747, BETWEEN STRINGER 26R TO STRINGER 27R. REPAIRED FRAME IAW SRM.
FRAME INNER CHORD CRACKED AT BS 348.2, STRINGER 17L. R & R CHORD IAW SRM & EA.
SHEAR TIE CORRODED AT BS 520, BETWEEN STRINGER 27L TO STRINGER 28L. R & R SHEAR TIE IAW SRM & DWG.
FRAME CORRODED AT BS 867, BETWEEN STRINGER 27L TO 27R. REPAIRED FRAME IAW SRM.
TIE CLIP CRACKED AT BS 947.5, STRINGER 25R. R & R TIE CLIP IAW SRM & DWG.
INTERNAL ANGLE CLIP CRACKED BETWEEN BS 348.2 TO BS 351.2, STRINGER 16L. R & R CLIP IAW SRM & DWG.
CLIP CORRODED AT BS 847, AT STRINGER 26R. R & R CLIP IAW SRM & DWG.
FRAME CORRODED AT BS 847, BETWEEN STRINGER 27R TO 27L. REPAIRED FRAME IAW EA.
WEB CORRODED AT BS 1016, LBL 2. REPAIRED WEB IAW EA.
SUPPORT CHANNEL CORRODED BETWEEN BS 727C TO 727D BETWEEN STRINGER 27R TO 27L. REPAIRED CHANNEL IAW SI.
AFT FRAME OF FWD CARGO DOOR CUT OUT CRACKED AT BS 492, STRINGER 24R. R & R FRAME IAW SRM & DWG.
RIGHT WING EXTERNAL SKIN CRACKED AT STATION 208, INBD SIDE. REPAIRED SKIN IAW EA.
SUPPORT ANGLE CRACKED BETWEEN BS 927 TO BS 947.5, BL 0. R & R ANGLE IAW SRM & DWG.
FRAME CRACKED AT BS 947.5, STRINGER 19L. R & R FRAME IAW SRM & DWG.
TIE CLIP CRACKED AT BS 500A, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.
TIE CLIP CRACKED AT BS 460, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.
STRAP CRACKED BETWEEN BS 312 TO BS 344, RBL 31.6. R & R STRAP IAW SRM.
STRAP CRACKED BETWEEN BS 312 TO BS 344, LBL 45.6. R & R STRAP IAW SRM.
VERTICAL STABILIZER ACCESS PANEL 9536 CRACKED. REPAIRED PANEL IAW SRM.
CENTER WING BOX SEAT TRACK CRACKED AT BS 727B, BETWEEN LBL 23.8 TO LBL 25.8. REPAIRED SEAT TRACK IAW EA.
NUMBER 2 PYLON RT NACELLE STRUT ACCESS PANEL 5864R CRACKED. REPAIRED PANEL IAW EA.
LEFT WING ACCESS PANEL 5764L CRACKED. REPAIRED PANEL IAW EA.
FUSELAGE FRAME CRACKED AT BS 500B, STRINGER 21L. REPAIRED FRAME IAW SRM.
ANTENNA BASE CRACKED AT PRESS BULKHEAD FWD FACE BS 178. R & R BASE IAW SRM & DWG.
R1 DOOR SKIN CRACKED AT BS 328, STRINGER 8R. REPAIRED SKIN IAW EO & EA.
CRACK ON CROSSBEAM E WEB FWD END & AFT EDGE OF THE AFT CARGO DOOR. REPAIRED T CHORD IAW EO & EA.
L2 DOOR LOWER CORNER FUSELAGE SKIN CRACKED AT BS 947.5+12, STRINGER 17L. REPAIRED SKIN IAW SRM.
LEFT FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A, AT FWD LOWER FASTENER HOLE. REPAIRED CHORD IAW EA.
EXTERNAL EMERGENCY EXIT LIGHTS LOOSE BETWEEN BS 727D TO BS 727E, BETWEEN STRINGER 22R TO STRINGER 23R. SECURE LIGHT IAW MM.
EXTERNAL EMERGENCY EXIT LIGHTS LOOSE BETWEEN BS 727D TO BS 727E, BETWEEN STRINGER 22L TO STRINGER 23L. SECURE LIGHT IAW MM.
RIGHT FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A, AT FWD LOWER FASTENER HOLE. REPAIRED CHORD IAW EA.
UPPER CHORD CRACKED AT BS 663+2, LBL 24.5. REPAIRED CHORD IAW EA.
R1 DOOR AFT EDGE FRAME CRACKED. REPAIRED FRAME IAW SRM.
RIGHT SIDE NLG WW CRACKED AROUND FASTENER HOLE AT BS 243.7+ 3.5, WL 169.1. REPAIRED WW IAW SRM.
RIGHT SIDE NLG WW AROUND FASTENER HOLE CRACKED AT BS 243.7+ 3.5, WL 169.1. REPAIRED WW IAW SRM.
RIGHT SIDE NLG WW AROUND FASTENER HOLE CRACKED AT BS 243.7+3.5, WL 169.1. REPAIRED WW IAW SRM.
LEFT NLG WW WEB CRACKED AT BS 259.5, BETWEEN WL 180 TO WL 182. REPAIRED WEB IAW SRM.
MAIN WW PRESS DECK CRACKED AT BS 665, LBL 24.5+7. REPAIRED DECK IAW SRM.
LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 24.8. REPAIRED CHORD IAW EA.
L2 DOOR SKIN CUT OUT FWD LOWER CORNER CRACKED AT BS 947.5+12, STRINGER 17L. REPAIRED SKIN IAW SRM & EA.
LEFT WING NR 4 GND SPOILER CTR OTBD HINGE FITTING BROKEN. R & R SPOILER IAW AMM.
LEFT WING NR 4 GND SPOILER INBD ACTUATOR CASTING BROKEN. R & R SPOILER IAW SRM.
RT WING INBD AFT FLAP TE UPPER SURFACE DELAMINATED. R & R AFT FLAP IAW MM.
FORWARD ENTRY UPPER HINGE CUT-OUT ON DOOR FRAME BRACKET CRACKED IN FORWARD OTBD AREA OF HINGE SHELF AREA, OTBD OF HINGE TRACK PLATE. R&R FITTING IAW SRM.
FORWARD ENTRY DOOR FRAME UPPER HINGE CUT OUT CRACKED AT HINGE CUT OUT RADIUS OF EXISTING REPAIR & EXTENDING FORWARD BETWEEN THE RIVET ROWS. REPAIR SKIN IAW SRM.
LEFT WING NR 2 FLAP TRACK FAIRING "A" FRAME CRACKED. REMOVED & REPLACED "A" FRAME PER CMM.
LEFT WING I/B FORE FLAP UPPER SURFACE CRACKED. REPAIRED FORE FLAP IAW SRM.
FWD ENTRY DOOR EMERGENCY LIGHT LENS MISSING. INSTALLED LENS PER MM.
AFT CABIN CEILING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS ASSY IAW AMM.
FWD ENTRY EMERGENCY EXIT LWR LIGHT ASSY DAMAGED. REMOVED AND REPLACED LIGHT ASSY PER MM.
L1 DOOR EMERGENCY LIGHT SIGN CRACKED. REMOVED AND REPLACED SIGN ASSY PER MM.
RIGHT WING UPPER SURFACE, AFT PYLON AREA, PANEL 58710R PLASTIC NUT PLATE STRIP CRACKED. REMOVED AND REPLACED RIGHT WING UPPER SURFACE PANEL 58710R NUT STRIP AS PER SRM. SEE SAM 326 FOR INDIVIDUALS STEP AND FUEL TANK ENTRY SAM 1045 AND PERFORMANCE WO# 13027 FOR REPAIR.
RIGHT WING UPPER SURFACE, AFT PYLON AREA, PANEL 58710R PLASTIC NUT PLATE STRIP CRACKED. REPAIRED NUT PLATE STRIP PER EA 1-354-1480.
LEFT WING O/B TRAILING EDGE FORE FLAP DELAMINATED. REMOVED & REPLACED FORE FLAP PER MM.
RIGHT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 8. SECURED LENS PER MM.
LEFT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 6. INSTALLED LENS PER MM.
BS 663 BULKHEAD STIFFERNER CRACKED AT LBL 7, WL 163. REPAIRED STIFFENER PER EA.
BS 663, RBL 7, WL 164 CENTER TANK REAR SPAR VERTICAL STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER PER EA & EO.
SKIN CRACKED AT BS 665, STR 4R. REPAIRED SKIN PER SI & AMM.
SKIN CRACKED AT BS 662, STR 4R. REPAIRED SKIN PER SI & AMM.
SKIN CRACKED AT BS 665, STR 4L. REPAIRED SKIN PER SI & AMM.
BS 663.75, RBL 6.15, WL 169 CENTER TANK REAR SPAR VERTICAL STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER PER ACO.
SHEAR TIE CORRODED AT BS 500, LBL 12, WL 157. REPAIRED SHEAR TIE IAW SRM.
RT WING O/B AFT FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.
RT WING I/B MIDFLAP UPPER SURFACE T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER SRM.
RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP IAW SRM.
LEFT WING I/B AFT FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.
LT WING I/B MID FLAP UPPER SURFACE T/E WEDGE IS DELAMINATED. REPAIRED MID FLAP IAW SRM.
LEFT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.
STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STRINGER CLIP IAW SRM AND BAC DWG.
STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
RIGHT BS 400+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.
STRINGER CRACKED AT BS 500A+17, STR S9R. REMOVED & REPLACED STRINGER SEGMENT IAW SRM.
RIGHT BS 807+10 UPPER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB.
RT BS 867+10 UPPER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB.
RT BS 400+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.
LEFT BS 827+10 UPPER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.
RT BS 380+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.
RIGHT BS 480+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.
RIGHT BS 500B+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB.
RIGHT BS 500C+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.
RIGHT BS 380+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.
RIGHT BS 420+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.
RIGHT BS 480+10 LOWER AFT WINDOW SKIN CRACKED. REPAIRED SKIN IAW SB AND EA.
RIGHT BS 500+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.
RIGHT BS 500B+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.
LEFT BS 420+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.
LEFT BS 460+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.
LEFT BS 380+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB & EA.
LEFT BS 500+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.
RIGHT BS 460+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA.
RIGHT BS 500+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.
RIGHT BS 500A+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW SB AND EA.
RIGHT BS 360+10 LOWER AFT WINDOW SKIN CRACKED. REPAIRED SKIN IAW EA.
RIGHT BS 460+10 LOWER AFT WINDOW SKIN CRACKED. RIGHT SKIN PER EA.
RIGHT BS 500C+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA.
LEFT BS 500B+10 UPPER FORWARD WINDOW SKIN CORNER AT CRACKED. REPAIRED SKIN IAW SB AND EA.
LEFT BS 500C+10 UPPER FORWARD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB AND EA.
RIGHT BS 360+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW REO & EA.
LT BS 887+10 UPPER AFT WINDOW SKIN CORNER CRACKED. REPAIR SKIN PER EA.
RT BS 847+10 UPPER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN PER EA.
LEFT BS 360+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW REO & EA.
LEFT BS 520+10 UPPER FORWARD WINDOW SKIN CORNER CRACKED. REPAIRED SKIN IAW EA & REO.
RIGHT BS 520+10 LOWER AFT WINDOW SKIN CORNER CRACKED. REPAIRED SKIN PER EA & REO.
MAIN CABIN STA 360 AT STRINGER S5L STRINGER CLIP FOUND TO BE CRACKED. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
DURING SCHEDULED HC2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENSE CRACKED. REMOVED AND REPLACED PER MM.
DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 877, STR 4R. REPAIRED SKIN IAW SRM.
DURING SCHEDULED CV CHECK FOUND, EEPLS LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED SPV CHECK, FOUND LT EEPLS LOOSE AT ROW 6. SECURED EEPLS PER MM.
DURING SCHEDULED SPV CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS DIRTY. CLEANED EEPLS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.
DURING SCHEDULED RON CHECK, FOUND CHEM MILL SKIN CRACKED AT BS 727C+5, STR 4R. REPAIRED SKIN IAW EA.
DURING SCHEDULED RON CHECK, FOUND CHEM MILL SKIN CRACKED AT BS 727C+10, STR 4R. REPAIRED SKIN IAW EA.
DURING SCHEDULED SPV CHECK, FOUND RT WINDOW SKIN CRACKED AT BS 500C+10, LOWER AFT CORNER. REPAIRED SKIN IAW TC.
DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN IAW SRM.
DURING SCHEDULED OTS CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 125. REPAIRED SKIN IAW EA.
DURING SCHEDULED OTS CHECK, FOUND R2 DOOR UPPER FWD CORNER STUB FRAME CRACKED. REMOVED AND REPLACED FRAME PER SRM.
DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT STA 125. REPAIRED SKIN PER EA.
DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.
DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE UPPER AFT ATTACH BRACKET LOOSE. SECURED BRACKET PER MM.
DURING SCHEDULE HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 125. REPAIRED SKIN PER SRM.
DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 807+10, STR 4R. REPAIRED SKIN PER EA.
DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT BS 827+10, STR 4R. REPAIRED SKIN PER EA.
L2 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED LENS PER MM.
DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.
DURING SCHEDULED MV2 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED MV1 CHECK, FOUND AFT EEPLS INOP. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED 16Y CHECK, FOUND LT WING LOWER T/E SUPPORT ROD AT NR 4 SPOILER I/B ACTUATOR SUPPORT FITTING BROKEN. REMOVED AND REPLACED FITTING PER MM.
DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 SLAT LOWER SKIN CRACKED AT O/B END. REPAIRED NR 1 SLAT PER MM.
DURING SCHEDULED 16Y CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP BETWEEN ROW 15 TO ROW 16. REPAIRED WIRE PER WDM.
DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 420 TO BS 440, RBL 67. REMOVED AND REPLACED WEB PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 727E, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED FRAME PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 FLAP TRACK CORRODED AT MOUNT PAD. REMOVED AND REPLACED FLAP TRACK PER MM.
DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, RBL 2. REMOVED AND REPLACED SHEAR TIE PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BETWEEN RBL 0 TO RBL 46. REMOVED AND REPLACED BEAM PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 400 TO BS 420, RBL 67. REMOVED AND REPLACED WEB PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND FRAME ANGLE CRACKED AT R1 DOOR LOWER FWD CORNER CUTOUT. REMOVED AND REPLACED ANGLE PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 9L. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 460 TO BS 480, LBL 67. REMOVED AND REPLACED WEB PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 460 TO BS 480, RBL 67. REMOVED AND REPLACED WEB PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND STRINGER FITTING CRACKED AT BS 332, STR 8R. REMOVED AND REPLACED FITTING PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND STUB FRAME ANGLE CRACKED AT BS 639, RBL 45. REMOVED AND REPLACED STUB FRAME PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND STUB FRAME ANGLE CRACKED AT BS 639, LBL 45. REMOVED AND REPLACED STUB FRAME PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 25R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER BAC DWG AND SRM.
DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO BAY FRAME CORRODED AT BS 727E, BETWEEN STR 23L TO STR 27R. REPAIRED FRAME PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR MOUNT PAD CORRODED. REMOVED AND REPLACED PAD PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO BAY FRAME CORRODED AT BS 727E, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED FRAME PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT LOWER LATCH PLATE CORRODED. REMOVED AND REPLACED PLATE PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR MOUNT PAD CORRODED. REMOVED AND REPLACED PAD PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 616, LBL 65. REPAIRED FRAME PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND LT CREASE BEAM CORRODED BETWEEN BS 400 TO BS 420, LBL 67. REPAIRED BEAM PER SRM.
DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 738E, STR 4R. REPAIRED SKIN PER EA.
DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 738B, STR 4R. REPAIRED SKIN PER EA.
DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.
DURING SCHEDULED HC2 CHECK, FOUND RT WING AILERON BALANCE TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.
DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER MM.
DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 500D, STR 8R. REPAIRED SKIN PER EA.
LEFT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. REMOVED AND REPLACED LENS PER MM.
RIGHT EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 19. SECURED LENS PER MM.
FWD LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
DECLARED EMERGENCY/DIVERSIONS. PRESSURIZATION EVENT AT 33K FT. MASKED DROPPED, EMERGENCY DESCENT. DIVERTED TO CRW. FOUND FUSELAGE SKIN CRACKED BETWEEN BS 827 TO BS 847, STR 2L. REPAIRED SKIN PER SWA EA.
DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP FADED AT ROW 23. REMOVED AND REPLACED EEPLS PER MM.
LT OVERWING EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER MM.
DURING SCHEDULED 14Y CHECK, FOUND SKIN CHORD ANGLE CRACKED AT BS 303, LBL 60, WL 218. REPAIRED SKIN PER EA.
DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR AFT GIRT BAR HOLDER CORRODED. REMOVED AND REPLACED BRACKET PER MM.
DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR AFT GIRT BAR HOLDER CORRODED. REMOVED AND REPLACED BRACKET PER MM.
DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS. 727B, RBL 44. REPAIRED BEAM PER EA.
DURING SCHEDULED 14Y CHECK, FOUND STRINGER WEB CRACKED AT BS 291, STR 14R. REPAIRED STRINGER PER SRM.
DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 25. REPAIRED BEAM PER EA.
DURING SCHEDULED 14Y CHECK, FOUND NOSE WHEEL WELL CEILING PANEL SKIN CRACKED AT SNUBBER ATTACH PLATE, LBL 7.75. REPAIRED SKIN PER ACO.
DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.
L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM.
DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1001, STR 5R. REPAIRED SKIN PER SRM.
DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1006, STR 5R. REPAIRED SKIN PER SRM.
DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.
DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CRACKED AT BS 492. REMOVED AND REPLACED STRINGER SECTION PER SRM.
DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT ASSY BROKEN AT L1 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED C3 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.
DURING SCHEDULED C1 CHECK, FOUND RT WING NR 4 SPOILER OUTBD ACTUATOR HINGE CASTING CRACKED. REMOVED AND REPLACED SPOILER ASSY PER MM.
DURING SCHEDULED C1 CHECK, FOUND RT WING NR 5 SPOILER OUTBD ACTUATOR HINGE CASTING CRACKED. REMOVED AND REPLACED SPOILER ASSY PER MM.
DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY LOWER EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.
DIVERSION, ELECTRICAL SMELL IN CABIN. FOUND NORMAL EQUIPMENT COOLING BLOWER INOP. REMOVED AND REPLACED BLOWER PER MM.
LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.
L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.
DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EVACUATION SLIDE LATCH CABLE MISROUTED. REROUTED CABLE PER MM.
AIR TURNBACK. LOST B-SYSTEM HYDRAULIC FLUID. REMOVED AND REPLACED HYDRAULIC LINE FROM B-SYSTEM MODULE TO B-SYSTEM HYDRAULIC ACCOUSTIC FILTER PER MM.
AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.
DURING SCHEDULED RON, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.
CABIN OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED LENS PER MM.
DURING SCHEDULED C3 CHECK, FOUND BEAR STRAP AT BS 294.5, STRINGER 10L, CRACKED. REPAIRED BEAR STRAP PER EA.
DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING, CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SRM.
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 500B, STRINGER 11R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.
DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION CLEVIS, CORRODED. REPAIRED HORIZONTAL STAB PER SRM.
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9R. REPAIRED FRAME PER SRM.
DURING SCHEDULED D-CHECK, FOUND CREASE BEAM ZEE CHORD AT BS 270, RBL 10, CORRODED. REMOVED AND REPLACED CREASE BEAM Z CHORD PER SRM.
DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727D, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.
DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT BS 727D + 5, LBL 12, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.
DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727B, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.
DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.
DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 328, RBL 20, CORRODED. REPAIRED WEB PER SRM.
DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT LEFT BS 296, WL 209, CRACKED. REPAIRED SKIN PER SRM.
DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 787, BS 827, BS 867,BS 907, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM.
DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS AT BS 663, STRINGER 10L, BS 707, STRINGER 11L, BS 663, STRINGER 10R CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.
DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 9L, CRACKED. REPAIRED FRAME PER SRM.
ON DESCENT, ACRID ODOR REPORTED IN CABIN BY F/A'S. NO ODOR NOTED IN COCKPIT. ODOR DISSIPATED AFTER TURNING OFF GASPER FAN. REMOVED AND REPLACED GASPER FAN PER MM.
R1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY AT R1 DOOR.
DURING SCHEDULED CHECK, FOUND LT HORIZ STAB SKIN CRACKED AT STA 157.10 JUST FWD OF REAR SPAR. REPAIRED SKIN PER SRM.
DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.
DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 747, STR 26R. REPAIRED FRAME PER SRM.
DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL WEBSCRACKED (2 EA) AT BS 180, WL 231, LBL 17.1 AND RBL 17.1. REMOVED AND REPLACED WEBS PER SRM.
ABORTED TAKEOFF, AT APPROX 100 KNOTS A LARGE BIRD WAS INGESTED INTO NR 1 ENGINE. COMPLIED WITH BIRD STRIKE INSP AND FOUND DAMAGED FAN BLADES. REMOVED AND REPLACED FAN BLADES PER MM.
DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 8. R&R EEPLS COVER PER MM.
DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE MOUNT BRACKET CRACKED. R&R MOUNT BRACKET PER MM.
DURING SCHEDULED RON CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.
DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD VERTICAL WEB CRACKED AT LBL 17, WL 190. REPAIRED BULKHEAD VERTICAL WEB PER SRM.
DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 5, WL 198 & RBL 5, WL 201. REPAIRED BULKHEAD WEB PER SRM.
EEPLS TRACK COVER DAMAGED AND WIRES EXPOSED AT ROW 20. REMOVED AND REPLACED TRACK COVER PER MM.
EEPLS INOP IN THREE PLACES. SECURED EEPLS WIRING PER MM.
DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT PROXIMITY LIGHT LENS LOOSE AT ROW 23. SECURED LIGHT ASSY PER MM.
FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS PER MM.
EEPLS TRACK COVER MISSIND AT ROW 2. REPLACED COVER PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND EEPLS AFT COVER MISSING. REPLACED COVER PER MM.
FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM.
DURINNG FLIGHT A STRONG BURNING SMELL ENTERED THE CABIN AND COCKPIT. (LAX TO MCI). FOUND EQUIPMENT COOLING FAN BURNED OUT. REMOVED AND REPLACED COOLING FAN PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND LAST FOUR EEPLS INOP. REMOVED AND REPLACED TRACK LIGHT ASSY PER MM.
EEPLS LIGHTS PULLED UP AT FWD END. RESECURED LIGHTS PER MM.
AIR TURBACK, LANDING GEAR WOULD NOT RETRACT DURING TAKEOFF. HANDLE WOULD NOT MOVE ABOVE OFF POSITION. ADJUSTED MAIN GEAR SAFETY SENSOR TELEFLEX CABLE AND PERFORMED GEAR SWING CKECK PER MM.
DURING SCHEDULED 1/2D CHECK, FOUND FWD GALLEY DOOR, LOWER FWD FRAME CRACKED. REPAIRED FRAME PER SRM.
AIR TURNBACK - DURING AIRCRAFT ROTATION AND UP TO 75 KNOTS AFTER LANDING, STALL WARNING INDICATION, (CONTROL COLUMN VIBRATOR WENT ON). DISCOVERED CAPTAIN'S AOA SENSOR DAMAGED. REMOVED AND REPLACED AOA SENSOR PER MM.
NR 2 FUEL FLOW ERRATIC INDICATOR WILL ROLL BACK AT HIGH POWER SETTINGS. INDICATOR DOES NOT BLANK OR LOOSE POWER, BUT WENT TO NEARLY ZERO INDICATION. REPLACED FUEL FLOW TRANSMITTER PER MM.
FUEL SMELL NOTED IN FORWARD GALLEY AREA. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. INSPECTED CABIN AND CARGO AREAS, CHECKED A/C PACKS AND PERFORMED ENGINE RUN, NO DEFECTS NOTED.
FOUND EXIT FLOOR LIGHTING INOPERATIVE IN ONE AREA. REPAIRED TRACK WIRING PER BOEING M/M.
DURING DESCENT INTO ELP, EXPERIENCED NUMBER 1 ENGINE FAILURE. AIRCRAFT MADE AN UNEVENTFUL LANDING AT ELP. INSPECTED AND FOUND NUMBER 1 ENGINE TOWER SHAFT FAILURE. REMOVED AND REPLACED ENGINE ASSEMBLY PER BOEING M/M.
NUMBER 1 AIR TEMP PROBE LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED TOTAL AIR TEMP PROBE PER BOEING M/M.