N766SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2016-08-27 – 2016-08-27 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2016-08-27 – 2016-08-27 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
R1 DOOR EMERGENCY EXIT SIDE LIGHT INOP AT M1674. R&R BATTERY PACK IAW AMM.
LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD LUG BORE HAD EVIDENCE OF CORROSION. REPAIRED LUG PER EA.
MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING, LOWER OUTBOARD FACE (HAT BUSHING SIDE) HAD EVIDENCE OF CORROSION. REPAIRED FITTING PER EA & SRM.
MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING, UPPER OUTBOARD FACE (HAT BUSHING SIDE) HAD EVIDENCE OF CORROSION. REPAIRED FITTING PER EA & SRM.
LT MAIN LANDING GEAR FORWARD LOWER INBOARD TRUNNION SUPPORT FITTING LUG FACE HAD EVIDENCE OF CORROSION. REPAIRED LUG PER EA.
LT MAIN LANDING GEAR FORWARD LOWER OUTBOARD TRUNNION SUPPORT FITTING LUG FACE HAD EVIDENCE OF CORROSION. REPAIRED LUG PER EA.
LT MAIN LANDING GEAR FORWARD UPPER INBOARD TRUNNION SUPPORT FITTING LUG FACE HAD EVIDENCE OF CORROSION. REPAIRED LUG PER EA.
LT MAIN LANDING GEAR FORWARD UPPER OUTBOARD TRUNNION SUPPORT FITTING LUG FACE HAD EVIDENCE OF CORROSION. REPAIRED LUG PER EA.
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG BORE HAD EVIDENCE OF CORROSION. REPAIRED LUG PER EA.
LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG BORE HAD EVIDENCE OF CORROSION. REPAIRED LUG PER EA.
MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING, UPPER INBOARD FACE (HAT BUSHING SIDE) HAD EVIDENCE OF CORROSION. REPAIRED FITTING PER EA.
MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD FACE (HAT BUSHING SIDE0 HAD EVIDENCE OF CORROSION. REPAIRED FITTING PER EA AND SRM.
LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG BORE HAD EVIDENCE OF CORROSION. REPAIRED LUG PER EA.
MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING, LOWER INBOARD FACE (HAT BUSHING SIDE) HAD EVIDENCE OF CORROSION. REPAIRED FITTING PER EA AND SRM.
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD LUG BORE HAD EVIDENCE OF CORROSION. REPAIRED LUG PER EA.
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG BORE HAD EVIDENCE OF CORROSION. REPAIRED LUG PER EA.
MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING, LOWER INBOARD FACE (HAT BUSHING SIDE) HAD EVIDENCE OF CORROSION. REPAIRED FITTING PER EA & SRM.
MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING, UPPER INBOARD FACE (HAT BUSHING SIDE) HAD EVIDENCE OF CORROSION. REPAIRED FITTING PER EA & SRM.
RT MAIN LANDING GEAR FORWARD UPPER INBOARD TRUNNION SUPPORT FITTING BORE HAD EVIDENCE OF CORROSION. REPAIRED FITTING PER EA.
LT MAIN LANDING GEAR FORWARD UPPER OUTBOARD TRUNNION SUPPORT FITTING BORE HAD EVIDENCE OF CORROSION. REPAIRED FITTING PER EA.
RT MAIN LANDING GEAR FORWARD LOWER INBOARD TRUNNION SUPPORT FITTING LUG FACE HAD EVIDENCE OF CORROSION. REPAIRED LUG PER EA.
RT MAIN LANDING GEAR FORWARD UPPER INBOARD TRUNNION SUPPORT FITTING LUG FACE HAD EVIDENCE OF CORROSION. REPAIRED LUG PER EA.
RT MAIN LANDING GEAR FORWARD UPPER OUTBOARD TRUNNION SUPPORT FITTING LUG FACE HAD EVIDENCE OF CORROSION. REPAIRED LUG PER EA.
FORWARD LAVATORY EMERGENCY LIGHT ASSEMBLY ON THE AFT WALL FOUND DAMAGED. R & R THE LIGHT ASSEMBLY IAW AMM.
CABIN SEAT TRACK CORRODED BETWEEN BS 520 TO 520 -10, LBL 45. R & R THE SEAT TRACK IAW SRM.
AFT CARGO BAY ANGLE CORRODED BETWEEN BS 807 TO 747+6, LBL 22. R & R THE ANGLE IAW SRM AND DWG.
STRINGER CRACKED AT BS 927, STR 8L. R&R STRINGER IAW DWG.
AFT WET AREA CREASE BEAM FLANGES CORRODED BETWEEN BS 951 TO 986+10, RBL 54. R & R THE CREASE BEAM IAW SRM & DWG.
AFT WET AREA FLOOR SUPPORT CORRODED AT BS 947+6, RBL 8. R&R FLOOR SUPPORT IAW SRM AND DWG.
FORWARD WET AREA INTERCOSTAL CORRODED AT BS 312-5, LBL 12. R&R INTERCOSTAL IAW SRM AND DWG.
AFT WET AREA WEB STRAP CORRODED BETWEEN BS 1016, LBL 3. R & R THE WEB STRAP IAW DWG & SRM.
FORWARD CARGO BAY FLOOR Z ANGLE CORRODED BETWEEN BS 500 TO BS 500D, RBL 23. R&R Z ANGLE IAW SRM & DWG.
FORWARD WET AREA GIRT BAR ATTACH Z CORRODED AT BS 344, LBL 61. REPAIRED GIRT BAR IAW SRM AND DWG.
AFT WET AREA WEB CORRODED AT BS 1016, LBL 34. R&R WEB IAW DWG.
FORWARD CARGO CUTOUT INNER FRAME STRAP CORRODED AT BS 440, RBL 25. R&R STRAP IAW SRM AND DWG.
FORWARD CARGO DOOR CUTOUT FORWAR LOWER THRESHOLD SCUFF PLATE CRACKED. REPAIRED THE SCUFF PLATE IAW EA.
HORIZONTAL PRESSURE WEB CRACKED AT BS 670, LBL 35. REPAIRED THE WEB IAW EA.
RT WING TRAILING EDGE PANEL CENTER SUPPORT BRACKET CRACKED BETWEEN WSTA 253 AND WSTA 278.50. R&R ANGLE IAW SRM.
HORIZONTAL PRESSURE DECK WEB CRACKED AT BS. 675, RBL 40. REPAIRED WEB IAW EA.
CEILING PANEL OVERWING EMERGENCY EXIT LIGHT MOUNT BROKEN. R & R THE LIGHT ASSEMBLY IAW AMM.
R2 DOOR SLIDE AFT GIRT BAR FLOOR MOUNT FITTING DAMAGED. R & R THE FITTING IAW AMM.
R2 DOOR SAFETY STRAP VELCRO LOOSE. R&R STRAP IAW SIP.
R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR LOOSE. R&R PLATE ASSEMBLY PER SIP.
R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED THE SLIDE IAW AMM.
R2 DOOR SLIDE OUT OF ADJUSTMENT. ADJUSTED THE SLIDE IAW AMM.
L2 DOOR SLIDE OUT OF ADJUSTMENT. ADJUSTED THE SLIDE IAW AMM.
L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED THE SLIDE IAW AMM.
FLOORBEAM INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL PER SRM.
R1 DOOR EMERGENCY EVAC SLIDE COVER AFT BUMPER END CAP MISSING. INSTALLED AFT BUMPER AMM.
R1 DOOR EMERGENCY EVAC SLIDE COVER FORWARD GIRT BAR HANGER LOOSE. SECURED HANGER PER AMM.
STRINGER 14L DAMAGED AT BS 500D+5. REPAIRED THE STRINGER IAW SRM.
STRINGER 15L DAMAGED AT BS 500D+14. REPAIRED THE STRINGER IAW SRM.
LEFT WING RIB CRACKED INBOARD LEADING EDGE FRAME. R & R THE RIB IAW EA.
SKIN DAMAGED BETWEEN BS 500D TO 520, BETWEEN STRINGERS 13 TO 18L. REPAIRED SKIN IAW EA.
L/H HORIZONTAL STABILIZER LEADING EDGE DAMAGED FROM IMPACT. / R&R STABILIZER IAW AMM.
NR 1 ENGINE FAILED AT CRUISE FL 390. DIVERTED. R & R NR 1 ENGINE IAW MT.
RIGHT OVERWING EXIT SIGN LENS LOOSE. R & R THE LENS IAW MM.
DECLARED EMERGENCY LOSS OF PRESSURIZATION AT FL300 DESCENDING TO FL270 MADE EMERGENCY DESCENT TO 10,000 FT. CABIN ALTERNATE NEVER EXCEEDED 10,000 FT, ONLY LIGHT WARNING WAS CABIN ALTERNATE. WARNING HORN ALONG WITH CABIN ALTERNATE LIGHT. R & R NR 2 ENGINE PRESSURE REGULATOR SHUTOFF VALVE IAW AMM.
LEFT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 17. REPLACED THE LAMP IAW AMM.
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT M1672. R & R THE BATTERY PACK IAW DWG.
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT M1669. R & R THE BATTERY PACK IAW DWG.
RIGHT EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 13. REPLACED THE LAMP IAW AMM.
LEFT WING NR 4 SLAT FITTING CRACKED AT STATION 85.74. R & R NR 4 SLAT IAW AMM.
FORWARD FACE SUPPORT ANGLE CRACKED AT BS 663.75, BETWEEN LBL 8 - 31. R & R ANGLE IAW SRM & DWG.
SUPPORT ANGLE CRACKED AT BS 663.7, LBL 19. R & R ANGLE IAW SRM & DWG.
LEFT WING NR 3 FLAP TRACK FAIRING CRACKED. REPAIRED FAIRING IAW EA & SRM.
LEFT WING NR 4 LE SLAT SKIN CRACKED AT STATION 85.74. R & R SLAT IAW MM.
MAIN WW COMPARTMENT, STIFFENER CRACKED AT BS 663.75, LBL 16. R & R STIFFENER IAW SRM & DWG.
SUPPORT BRACKET CRACKED AT BS 559, RBL 5. R & R BRACKET IAW SRM.
FRAME WEB CRACKED AT BS 440, STRINGER 8. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 727D, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME WEB CRACKED AT BS 907, BETWEEN STRINGER 7R - 8R. REPAIRED FRAME IAW EA.
LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 24.75 INBD FLANGE AT 5 & 7 O'CLOCK AT CTR WING BOX. REPAIRED FLOORBEAM IAW EA.
LONGITUDINAL FLOORBEAM AFT SEAT TRACK, INBD FLANGE CRACKED AT BS 727B, LBL 24.50 AT CTR WING BOX. REPAIRED SEAT TRACK IAW EA.
LONGITUDINAL FLOORBEAM FITTING CRACKED AT BS 727B, RBL 45.50, AT CTR WING BOX. R & R FITTING IAW SRM & DWG.
LONGITUDINAL FLOORBEAM FITTING, CRACKED AT BS 727B, RBL 24.50, AT CTR WING BOX. R & R FITTING IAW SRM & DWG.
LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 45.50, INBD FLANGE AT CTR WING BOX. REPAIRED FLOORBEAM IAW EA.
LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 45.50, AT CTR WING BOX. REPAIRED FLOORBEAM IAW EA.
LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.50, OTBD FLANGE 12 O'CLOCK AT CTR WING BOX. REPAIRED FLOORBEAM IAW EA.
LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.50, INBD FLANGE 12 O'CLOCK AT CTR WING BOX. REPAIRED FLOORBEAM IAW EA.
LONGITUDINAL FLOORBEAM OTBD FLANGE, CRACKED AT BS 727B, RBL 45.50, 6 O'CLOCK AT CTR WING BOX. REPAIRED FLOORBEAM IAW EA.
LONGITUDINAL FLOORBEAM FITTING CRACKED AT BS 727B, LBL 24.50, AT CTR WING BOX. R & R FITTING IAW SRM & DWG.
LEFT WING LE NR 3 SLAT NOSE SKIN, CRACKED AT STATION 322.71. REPAIRED SKIN IAW SRM.
FORWARD ENTRY DOOR EGRESS LIGHT COVER FELL OFF. SECURED COVER IAW SIP.
L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
L2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.
RIGHT AFT EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.
DIVERSION & DECLARED EMER. FWD CARGO FIRE LIGHT CAME ON IN FLIGHT, FLASHED SEVERAL TIMES THEN STEADY. PERFORMED QRH PROCEDURE, INCLUDING BOTTLE DISCHARGE. NO FIRE INDICATION IN CARGO BIN UPON INSPECTION. R & R CARGO FIRE CONTROL PANEL IAW AMM.
L2 DOOR EMER EXIT SIGN LENS COVER MISSING. INSTALLED COVER IAW MM.
AFT ENTRY DOOR EMER EXIT SIGN LOOSE. R & R SIGN IAW MM.
SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.
LT NR 1 WINDOW FRAME ASSEMBLY CRACKED. R & R FRAME ASSEMBLY IAW ACO.
RT HAND HORIZONTAL STABILIZER INBD VERTICAL STIFFENER CRACKED AT 92.70. REPAIRED STIFFENER IAW SRM.
VERTICAL PRESS WEB CRACKED AT BS 663, LBL 28. REPAIRED WEB IAW EA.
VERTICAL PRESS WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB IAW SRM & EA.
SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.
RT HORIZONTAL STABILIZER STAB STATION 92.70 SECOND VERTICAL STIFFENER FROM FWD CRACKED. REPAIRED STABILIZER IAW EA.
VERTICAL PRESS WEB CRACKED AT BS 663, RBL 40. REPAIRED WEB IAW SRM.
RT HORIZONTAL STABILIZER STATION 92.7 VERTICAL STIFFENER CRACKED THIRD FROM FWD SPAR. REPAIRED STIFFENER IAW SRM.
RT HORIZONTAL STABILIZER RIB INBD 92.70 FWD VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.
RT NR 3 FLIGHT DECK FIXED WINDOW FRAME FWD SIDE CRACKED. REPAIRED FRAME IAW ACO.
RT NR 3 FLIGHT DECK FIXED WINDOW FRAME, FWD SIDE WINDOW PANE CRACKED. REPAIRED FRAME IAW ACO.
LT NR 3 FLIGHT DECK FIXED WINDOW FRAME, FWD SIDE WINDOW PANE CRACKED. REPAIRED FRAME IAW ACO.
LT WING INBD FIXED TE INTERCOSTAL ANGLE CRACKED ABOVE NR 1 ENG AFT PYLON FAIRING. R & R ANGLE IAW SRM & DRAWING.
LT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.
RT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.
DECLARED EMERGENCY DUAL BLEED TRIP FAILURE @ FL 410 RT BLEED TRIP LIGHT ILLUMINATED FOLLOWED BY LT BLEED TRIP LIGHT INITIATED EMERGENCY DESCENT. FOUND BAD PRECOOLER CONTROL VALVE. R & R NR 1 ENGINE PRECOOLER CONTROL VALVE IAW MM.
AFT RIGHT EMERGENCY LIGHT COVER (PLASTIC LENS) MISSING. R & R LIGHT ASSY IAW MM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STABILIZER STA 101.9. REPAIRED SKIN PER SRM.
CAPTAIN'S L1 WINDOW FRAME OTBD POST CRACKED NEAR TOP OF POST. REPAIRED FRAME IAW EA.
MID-CABIN EMERGENCY EXIT SIGN BROKEN. REPLACED MID CABIN EMERGENCY EXIT SIGN PER MM, OPS CHECK NORMAL.
LEFT FWD EXTERIOR EMERGENCY EVAC SLIDE LIGHT INOP. RELAMPED IAW AMM.
BELT FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA.
BELT FRAME CRACKED AT BS STR 8R, BS 360. REPAIRED FRAME IAW EA.
FRAME CRACKED AT STR 8L BS 520. REPAIRED FRAME PER SRM.
BELT FRAME CRACKED AT BS STR 8R, BS 827. REPAIRED FRAME IAW EA.
BELT FRAME CRACKED AT BS STR 8R, BS 440. REPAIRED FRAME IAW EA.
RT COCKPIT WINDOW ARCED AND CRACKED. REMOVED AND REPLACED WINDOW IAW MM.
MAIN FUEL TANKS DO NOT FEED PROPERLY; NR 2 (RIGHT) FEEDS SLOWER THAN NR 1 AT A RATE OF ABOUT 300LBS PER 15 MINUTES AT CRUISE, FL 380. REMOVED AND REPLACED CENTER TANK CROSSFEED VALVE PER MM.
DURING SCHEDULED HC2 CHECK LT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC2 CHECK RT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
OVERHEAD EMERGENCY EXIT LIGHT LOOSE AT MID CABIN. SECURED LIGHT PER MM.
DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 729B, LBL 2. REMOVED AND REPLACED BEAM SECTION PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND LT WING O/B LEADING EDGE NR 2 SLAT EXTERNAL SKIN CRACKED. REPAIRED NR 2 SLAT PER AAR EA.
DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR ANGLE CORRODED AT BS 270, LBL 10 TO RBL 10. REPAIRED ANGLE PER EA.
DURING SCHEDULED 10Y CHECK, FOUND EMERGENCY LIGHTS INOP AT ROW1 TO ROW 6. REPAIRED LIGHT SOCKET PER MM & WD.
DURING SCHEDULED HC2 CHECK, FOUND LT WING O/B TRAILING EDGE AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.
DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR SKIN CRACKED AT AFT UPPER CORNER. REPAIRED SKIN PER SRM.
AFT GALLEY EMERGENCY FLASHLIGHT LOW VOLTAGE. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION SUPPORT FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.
DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION SUPPORT FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.
AFT I/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.
DURING SCHEDULED MV2 CHECK, FOUND RT WING INBOARD T/E FLAP PUNCTURED. REMOVED AND REPLACED FLAP PER MM.
FOUND R1 DOOR SLIDE LOW PRESSURE. REMOVED AND REPLACED SLIDE PER MT.
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 951, RBL 5. REPAIRED FLOORBEAM PER EA.
DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 807 AND BS 847, RBL 70. REMOVED AND REPLACED CREASE BEAM PER SRM.
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 32 TO RBL 50. REPAIRED FLOORBEAM PER SRM.
DURING SCHEDULED 8Y CHECK, FOUND RT WING NR 7 L/E SLAT CRACKED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM.
DURING SCHEDULED CABIN VISIT, FOUND L2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
ON CLIMBOUT OF MCO NR 1 ENGINE EXPERIENCED COMPRESSOR STALL. ENGINE PARAMETERS NORMAL. REMOVED AND REPLACED NR 1 ENGINE PER MT.
DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 7 DEF. REMOVED AND REPLACED STRIP PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 9 ABC. REMOVED AND REPLACED STRIP PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR VIEWER WINDOW MISSING. INSTALLED WINDOW PER MM.
DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
R1 DOOR EMERGENCY EVAC SLIDE CONTAINER LOOSE. SECURED SLIDE CONTAINER PER MM.
EEPLS TRACK LOOSE AT ROW 9 ABC. REMOVED AND REPLACED EEPLS TRACK SECTION PER MM.
DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EEPLS STRIP PEELING. REMOVED AND REPLACED EEPLS STRIP PER MM.
DURING SCHEDULED HC2 CHECK, FWD AND MID CABIN EMERGENCY LIGHTING BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
FWD SERVICE DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.
FWD SERVICE DOOR LOWER EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.
DURING SPV, FOUND EMERGENCY EXIT LIGHTS AT R1, R2 AND L1 DOORS, INOP. REMOVED AND REPLACED EMERGENCY EXIT BATTERIES PER MM.
DURING SCHEDULED SERVICE CHECK, (SI 11038-55), RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 3 AND NR 4 HINGE BUSHINGS PER MM.
DURING SCHEDULED SERVICE CHECK, (SI 11038-55), LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 3 AND NR 4 HINGE BUSHINGS PER MM.
DECLARED EMERGENCY, INFLIGHT SHUTDOWN, AIR TURNBACK. DURING CLIMB POSSIBLE COMPRESSOR STALL OF NR 1 ENGINE, FOLLOWED BY SEVERE VIBRATION. REMOVED AND REPLACED NR 1 ENGINE PER MM.
AFT SVC DOOR EMERGENCY EVAC SLIDE DEPLOYED INADVERTENTLY. R&R SLIDE PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY EMERGENCY EVAC SLIDE PRESS INDICATOR LOW. REMOVED AND REPLACED FWD ENTRY SLIDE PER MM.
ABORTED TAKEOFF, AFT CARGO DOOR LIGHT ILLUMINATED. VERIFIED DOOR CLOSED AND DEFERRED PER MEL, LATER DURING RON AT MDW, ADJUSTED AFT CARGO DOOR TARGET PER MM.
ABORTED TAKEOFF, AFT CARGO DOOR LIGHT ILLUMINATED. REMOVED DEBRIS FROM AFT CARGO DOOR LIGHT POSITION SWITCH. OPS CHECK GOOD.