N183AN
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| American Airlines | Operator | 2015-10-21 – 2015-10-21 | Operator named in NTSB report |
| AMERICAN AIRLINES, INC. (AALA) | Operator | 2015-10-21 – 2015-10-21 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AIRCRAFT IN BASE MAINTENANCE. CORROSION FOUND ON THE POTABLE WATER DOOR LANDING PLATE AT BS 361, BETWEEN STRINGERS 22R AND 23R. REPLACED THE PLATE IAW 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MID LAVATORY SERVICE DOOR AT BS 71 AND S22L. REPLACED MID LAVATORY SERVICE DOOR PER AMM 52-10-02.
AIRCRAFT WAS GROUNDED: L4 DOOR EXTERIOR SLIDE LIGHT WAS INOPERABLE. MAINTENANCE RELAMPED SLIDE LIGHT PER AMM 33-51-06.
R4 DOOR, SLIDE BUSTLE WAS LOOSE AND INTERFERING WITH DOOR OPENING. MAINTENANCE REROUTED BUSTLE STRAP AND REINSTALLED BUSTLE IAW AMM 25-66-01.
MAINTENANCE FOUND THE ESCAPE SLIDE MOORING LINE NOT SECURE. SECURED THE SLIDE STATIC MOORING LINE IAW AMM 25-66-10. OK FOR SERVICE.
SEAT MOUNTED EMERGENCY LIGHTS WERE DIM DURNG A TEST. MAINTENANCE REPLACED THE BATTERY PACK IAW AMM 33-51-01, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.
L1 DOOR FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY DISCHARGED. THE AIRCRAFT WAS GROUNDED. REPLACED THE BATTERY IAW AMM 25-64-00.
THE L4 DOOR FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY WAS DISCHARGED. REPLACED THE BATTERY IAW AMM 25-64-00.
FLASHLIGHT BATTERY AT THE FLIGHT ATTENDANT SEAT WAS INOPERATIVE. REPLACED THE BATTERY IAW AMM 25-60-00. OPS CHECKED GOOD.
THE RIGHT WING OUTBOARD TRAILING EDGE FLAP HAS MOISTURE INGRESS. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLAP IAW AMM 27-51-22.
THE LEFT WING OUTBOARD TRAILING EDGE FLAP HAS MOISTURE INGRESS. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLAP IAW AMM 27-51-22.
L4 DOOR EXTERAL HANDLE, IMPROPERLY STOWED LEAVING THE DOOR STUCK OPEN. RELEASED THE DOOR, CLOSED DOOR, OPS NORMAL.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT DECK PLATE BETWEEN STA 1709 TO STA 1720. REPAIRED DECK PLATE PER SRM 53-60-51-2R-18.
CORROSION ON TOP OF THE FLOOR SUPPORT, BS 1620 TO 1640, RBL 20. REPLACED THE FLOOR SUPPORT IAW 51-00-05.
DURING A TEST, RIGHT OVERWING EXIT SLIDE DEPLOYED BUT FAILED TO INFLATE ENTIRELY. THE SLIDE TOOK AN ADDITIONAL 30 SECONDS TO FULLY DEPLOY. SLIDE COMPLETELY DEFLATED 30 MINUTES AFTER DEPLOYMENT. REPLACED INFLATION BOTTLE AND SLIDE.
FIRST OFFICER'S SLIDING WINDOW DIFFICULT TO OPEN & CLOSE, THE HANDLEWAS BINDING. ADJUSTED FIRST OFFICER'S NR 2 WINDOW IAW MM 56-11-02, AND SECURED THE HANDLE MOUNT. OPS CHECKED NORMAL.
AIRCRAFT WAS GROUNDED: AFTER TAKEOFF, RIGHT HAND ENGINE GENERATOR FAILED AND ACCOUNT ELECTRICAL ISSUE. EMERGENCY DECLARED, AIRCRAFT LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLE SHOT RIGHT ENGINE INTEGRATED DRIVE GENERATOR PER FIM 24-20-00-810-802 AND REPLACED RIGHT ENGINE INTEGRATED DRIVE GENERATOR PER AMM 24-11-01, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
DURING POST FLIGHT WALKAROUND, FOUND THE NR 3 MAIN LANDING GEAR TIRE TREAD SEPERATED. REMOVED AND REPLACED WHEEL ASSY IAW AMM 32-45-01. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.
R2 DOOR EMERGENCY EVACUATION SLIDE ARMED LIGHT IS ON WITH THE DOOR DISARMED. CLEANED BOTH THE GIRT BAR MICRO SWITCHES AND TARGET. OPERATIONAL CHECKED GOOD IAW AMM 25-66-01.
R2 DOOR EMERGENCY EVACUATION SLIDE ARMED LIGHT IS ON WITH THE DOOR DISARMED. CLEANED BOTH GIRT BAR MICRO SWITCHES AND TARGET. OPERATIONAL CHECKED GOOD IAW AMM 25-66-01.
AIRCRAFT WAS NOT GROUNDED. R2 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR SHOWS ARMED WHEN PHYSICALLY DISARMED. CLEANED GIRT BAR SLIDERS. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN AT R4 DOOR HAS A DETACHED LENS COVER. REINSTALLED LENS COVER IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN AT L2 DOOR HAS A LOOSE LENS COVER. SECURED LENS COVER IAW AMM 33-24-00. OPERATIONAL CHECK GOOD.
L2 DOOR EMERGENCY POWER RESERVOIR PRESSURE IS LOW. REMOVED AND REPLACED RESERVOIR IAW AMM 52-11-30. OPERATIONAL CHECKED GOOD.
SEAT MOUNTED EMERGENCY LIGHT AT SEAT 35D IS INOPERATIVE. SEATED THE LIGHT ASSEMBLY IAW AMM 33-51-11. OPERATIONAL CHECKED GOOD.
AIRCRAFT WAS GROUNDED. ON APPROACH, MAIN LANDING GEAR DOOR INDICATIONS ON EICAS. FOUND RIGHT MAIN GEAR DOOR DOWN AND RED GEAR DOOR UNSAFE LIGHT ON IN THE WHEEL WELL. REMOVED AND REPLACED MAIN LANDING GEAR EXTENSION HYDRAULIC FLOW FUSE IAW AMM 32-32-19-002-026. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS GROUNDED. ON FINAL APPROACH AFTER GEAR EXTENSION, GEAR DOORS EICAS MESSAGE AND GEAR DOOR LIGHT ILLUMINATED. REMOVED AND REPLACED RIGHT DOWNLOCK OPERATED DOOR SEQUENCE VALVE FOR THE RIGHT MAIN LANDING GEAR IAW AMM 32-32-07. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED. 1ST CLASS SEAT MOUNTED EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY AT M10798 IAW AMM 33-51-11. OPERATIONAL CHECK NORMAL.
AIRCRAFT WAS GROUNDED. SJU, AIR INTERRUPT, MIA-UVF. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT OVERWEIGHT. DURING CRUISE NR 1 ENGINE INDICATED LOW FUEL FLOW AND HIGH EPR. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE EPR TRANSMITTER AND EEC UNIT AND ACCOMPLISHED GROUND OPERATIONAL TEST IAW AMM 77-11-01 AND AMM 73-21-07. SYSTEM CHECKS NORMAL. SEE ALSO AALA20161025003.
AIRCRAFT WAS GROUNDED. SJU, AIR INTERRUPT, MIA-UVF. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT OVERWEIGHT. DURING CRUISE NR 1 ENGINE INDICATED LOW FUEL FLOW AND HIGH EPR. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE EPR TRANSMITTER AND EEC UNIT AND ACCOMPLISHED GROUND OPERATIONAL TEST IAW AMM 77-11-01 AND AMM 73-21-07. SYSTEM CHECKS NORMAL. SEE ALSO AALA20161025004.
ON CLIMB OUT CAPTAIN AND FIRST OFFICER FMCS BEGAN DEGRADING UP. NUMEROUS FLAGS APPEARRED. CAPTAINS AIR SPEED WENT TO 0 MOMENTARILY. EICAS SHOWED LEFT FMC FAIL. EMERGENCY DECLARED. LANDING UNEVENTFUL. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED BITE OF LEFT AND RIGHT FMCS AND ADC WITH NO FAULTS FOUND. REMOVED AND REPLACED BOTH LEFT AND RIGHT FMCS AMM 34-61-01 AND AMM 34-61-00 AND ADC IAW AMM 34-21-01.
DURING CLIMB OUT CAPTAIN AND FIRST OFFICER FMCS BEGAN DEGRADING UP. NUMEROUS FLAGS APPEARRED. CAPTAINS AIR SPEED WENT TO 0 MOMENTARILY. EICAS SHOWED LEFT FMC FAIL. EMERGENCY DECLARED. LANDING UNEVENTFUL. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED BITE OF LEFT AND RIGHT FMCS AND ADC WITH NO FAULTS FOUND. REMOVED AND REPLACED BOTH LEFT AND RIGHT FMCS AMM 34-61-01 AND AMM 34-61-00 AND ADC IAW AMM 34-21-01.
DURING CLIMB OUT, CAPTAIN AND FIRST OFFICER FMCS BEGAN DEGRADING UP. NUMEROUS FLAGS APPEARRED. CAPTAINS AIR SPEED WENT TO 0 MOMENTARILY. EICAS SHOWED LEFT FMC FAIL. EMERGENCY DECLARED. LANDING UNEVENTFUL, AND THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED BITE OF LEFT AND RIGHT FMCS AND ADC WITH NO FAULTS FOUND. REMOVED AND REPLACED BOTH LEFT AND RIGHT FMCS AMM 34-61-01 AND AMM 34-61-00 AND ADC IAW AMM 34-21-01.
AIRCRAFT WAS GNDED, AIR INTERRUPT, EMER WAS DECLARED, LANDING UNEVENTFUL, ACAFT NOT OVERWEIGHT. DURING CRUISE, FIRST OFFICERS WINDOW CRACKED & WHOWED ELEC ARCING. T & R FIRST OFFICER, STRINGER R1 WINDOW AS IAW AMM 56-11-0. SYS CHECKED NORMAL.
AIRCRAFT WAS NOT GNDED. DURING EMER LIGHT TEST, FOUND EMER AISLE LIGHT DIM AT ROWS 26 - 36. R & R EMER LIGHT BATTERY, BETWEEN AFT LAVATORY CEILING IAW MM 33-51-11.
ON CLIMB OUT, RT ENGINE INDICATION FLUCTUATION AT ALL POWER SETTINGS. THE FLIGHT DECLARED AN EMERGENCY & RETURNED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. R & R FUEL FLOW GOVERNOR IAW MCM 73-94-01. OPERATIONS & LEAK CHECKED NORMAL.
EMERGENCY LIGHT AT 28 DEF INOPERATIVE. FOUND LOOSE CONNECTOR UNDER SEAT 28 DEF. RESET CONNECTOR & PERFORMED OPERATIONAL CHECK IAW AMM 33-51-00. SYS CHECKED NORMAL.
DURING CLIMB RT ENG BLEED OFF ILLUMINATED. DIVERTED, EMERGENCY DECLARED, AND LANDING UNEVENTFUL. R & R RT ENGINE PRESSURE REGULATING & SOV IAW MM 36-11-09. PERFORMED OPERATIONAL CHECKS. SYS CHECKED NORMAL.
DURING CLIMB, THE RT ENG BLEED OFF EICAS MSG ILLUMINATED. DIVERTED AND MX CHECK PRESOV & RFCC LINE FOR SECURITY IAW FIM 36-10-00 WITH NO LEAKS FOUND. R & R RT ENGINE SPEED CARD IAW FIM 36-10-00 & MM 77-12-04. ACCOMPLISHED CHECK OF LT & RT AIR DISTRIBUTION SYS IAW 36-11-00-710-801. SYS CHECKED NORMAL.
AIR INTERRUPT, RETURNED, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. THE LT ENG BLEED OFF LIGHT ILLUMINATED, BLEED AIR WOULD NOT RESET & ACFT WOULD NOT HOLD PRESSURIZATION ON SINGLE PACK OPERATION. REPLACED THE LT ENG PRESS REGULATING & PRSOV IAW AMM 36-11-09. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
OVERWING FILL PORT FAILED BONDING CHECK, FOUND CORROSION BETWEEN PORT FLANGE & WING FAYING SURFACE AS FAULT. REPAIRED IAW EA 252057.
NUMBER 1 ENG PYLON CRITICAL FASTENER HOLE NR 9 SHOWS CRACK INDICATION IAW NDT INSPECTION. REPAIRED HOLE IAW EA 251628.
LEFT WING SKIN CORRODED AT OVERWING FUEL FILL PORT FAYING SURFACE. REPAIRED SKIN IAW SRM 57-20-01-2R & AMM 28-11-04.
DECK SUPPORT CLIP AT RBL 16.12 & FS 1520 CRACKED. R & R CLIP IAW AARD 51-00-05-1.
CORROSION ON RT TRANSITION PANEL BETWEEN STATION 1440 - 1640. REPLACED TRANSITION PANEL.
AFT CARGO CEILING AREA, STATION 1320 - 1340, UPPER ANGLE OF CTR WEB IS CRACKED AROUND AFT NUTPLATE LOCATION. REPLACED ANGLE IAW AARD 51-00-05-1.
CORROSION ON RT TRANSITION PANEL, FWD OF AFT CARGO DOOR STATION 1320 - 1380. REPLACED RT TRANSITION PANEL FROM STATION 1310 - 1380 IAW AARD 51-00-05.
AFT CARGO COMPARTMENT RT TRANSITION PANEL IS CORRODED BETWEEN FS 1380 & 1440. R & R TRANSITION PANEL SECTION IAW AARD 51-00-05.
RIVETS SHEARED FOR FLOORBEAM STABILIZER STRAP AT FS 377.7 & LBL 45. ACCOMPLISHED STRAP PLATE & FILLER REPAIR IAW SRM 53-10-51-2R-1.
SCATTERED HEAVY CORROSION ON AFT DECK PLATE AT 1715 BETWEEN LBL 51 & RBL 50. R & R AFT DECK PLATE IAW SRM 51-20-01, AARD 51-00-05-1 & DWG 146N5300.
LT INBD MAIN FLAP UPPER SURFACE CORROSION. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B757-57-033281.
MULTIPLE EMERGENCY EXIT SEAT LIGHTS IN COACH INOPERATIVE. REPLACED BATTERY PACK ABOVE 19DEF. OPERATIONS CHECKED NORMAL.
MULTIPLE EMERGENCY EXIT SEAT LIGHTS IN COACH INOPERATIVE. REPLACED BATTERY PACK ABOVE 9DEF. OPERATIONS CHECKED NORMAL.
MULTIPLE EMERGENCY AISLE LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY AISLE LIGHT BATTERY PACK ABOVE FIRST CLASS LAVATORY. OPERATIONS CHECKED NORMAL.
ANGLE CRACKED AT STATION 680 LEFT BUTTLINE 46. REPLACED ANGLE PER AARD 51-00-05-1 REPAIR 1.
AFT ATTACH ANGLE ON INTERCOSTAL AT STATION 680 LEFT BUTTLINE 46 DAMAGED. INSTALLED WEB ATTACH ANGLE PER AARD 51-00-05-1 REPAIR 1.
AFT CARGO, BELOW THE CABIN FLOOR BETWEEN STATIONS 1580 TO 1600, THE INTERCOSTAL AT BUTTLINE 0 TOP L-ANGLE IS CRACKED AT THE AFT NUT PLATE. INSTALLED NEW L-ANGLE PER SRM 51-10-02-0G AND AARD 51-00-05-1, REPAIR 1.
AFT FLOOR STRUCTURE FROM STATIONS 1640 TO 1672 AT RIGHT BUTTLINE 55 HAS CORROSION AT FASTENER HOLES. INSTALLED NEW AFT GUTTER SUPPORTS AT RIGHT NUMBER 4 DOOR PER AARD 51-00-05-1.
CORROSION ON LEFT GUTTERBOX FLOOR SUPPORT AT STATION 1677 AND LEFT BUTTLINE 53. INSTALLED NEW LEFT AFT GUTTERBOX PER AARD 51-00-05-1, REPAIR 1, AND SRM 51-10-02-0G.
SHARP EDGES ON BLENDED GOUGE AT STATION 648 BETWEEN STRINGERS 1 AND 2 RIGHT. INSTALLED SKIN DOUBLER PER EA B757-53-025376.
RIGHT NUMBER 4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 4 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.
DENT IN FUSELAGE SKIN BETWEEN STATIONS 720 TO 740. REPAIRED DENT PER SRM 53-00-01-2R AND EA B757-53-020175.
SFO - CREW REPORTED BOTH FLIGHT MANAGEMENT COMPUTERS DISPLAYED "STANDBY ONE" AND ALL NAV FUNCTIONS (INPUTS) WERE LOCKED OUT. BOTH ROUTE 1 AND 2 UNUSABLE. FLIGHT RETURNED SFO LANDED WITHOUT INCIDENT. REPLACED THE NUMBER 1 FLIGHT MANAGEMENT COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.
AFT LEFT OVERWING HATCH EXIT MARKER STICKER PEELING. REMOVED AND REPLACED LEFT AFT OVERWING HATCH EXIT MARKER STICKER. OPS CHECKED GOOD.
EMERGENCY LIGHT AT SEAT 23D MISSING SHROUD. REPLACED SHROUD AT SEAT 23D.
EMERGENCY LIGHT AT SEAT ROW 1EF INOPERATIVE. SECURED EMERGENCY LIGHT WIRING AT SEAT 1EF.
DFW - LEFT FORWARD EMERGENCY OVERWING EXIT SIGN DECAL PEELED BACK. INSTALLED NEW PLACARD AT LEFT FORWARD EMERGENCY OVERWING EXIT.
DFW - RIGHT AFT EMERGENCY OVERWING EXIT SIGN DECAL PEELED BACK. INSTALLED NEW PLACARD AT RIGHT AFT EMERGENCY OVERWING EXIT.
SFO - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
ORD - EXTERIOR EMERGENCY LIGHT AT RIGHT MID PASSENGER ENTRANCE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIGHT MID PASSENGER ENTRANCE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
LAS - EMERGENCY LIGHT AT AFT GALLEY LEFT NUMBER FOUR DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
SFO - OVERHEAD EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED NORMAL OPERATION.
MIA EMERGENCY LIGHT AT FORWARD RIGHT NUMBER ONE DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FORWARD RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)
LAX - EMERGENCY LIGHTS AT SEAT 36D INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 36D FOR EMERGENCY LIGHTS AT SEAT 36D. SYSTEM GROUND CHECKED NORMAL OPERATION.
PHL - INFLIGHT LEFT ENGINE FAILURE ON TAKEOFF. ENGINE HAD LARGE VIBRATION FOLLOWED BY WHAT FELT LIKE SEIZURE. ENGINE GENERATOR TEMPERATURE 975C. REPORTS OF FIRE AND SMOKE BY AIR TRAFFIC CONTROL, OTHER AIRCRAFT AND PASSENGERS. NO FIRE WARNING. ENGINE SHUTDOWN PER QRH PROCEDURE. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.
MIA - INFLIGHT LEFT HAND ENGINE BEGAN HIGH FREQUENCY VIBRATION AND OVER TEMPERATURE AT 230 IN HEAVY PRECIPITATION. POWER WAS REDUCED TO IDLE AND DESCENT ACCOMPLISHED BUT OVER TEMPERATURE CONTINUED TO MAX ENGINE GENERATOR TEMPERATURE OF 900C. ENGINE WAS SHUTDOWN PER QRH PROCEDURE AND UNEVENTFUL FOR SINGLE ENGINE APPROACH. VISUALLY INSPECTED INLET AND EXHAUST NO DAMAGE NOTED. ACCOMPLISHED BOROSCOPE OF HPC HPT IPT AND LPT ACCOMPLISHED BITE CHECK OF EEC BVCU TPU AND AVM MONITOR. REPLACED AVM MONITOR AND ACCELORMETER. REPLACED BVCU AND TPU. REPLACED TPU SENSOR AND DEDICATED GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
MCO - AFTER INTERMEDIATE LEVEL OFF AT FL220 SMOKE IN COCKPIT VERY SUDDEN & EVIDENT. FIRST CLASS F/A SMELLED SMOKE, ROW 26 PASSENGER INFORMED AFT F/A SMOKE SMELLED. ACCOMPLISHED CABIN SMOKE FIRE PROCEDURE TURNING OFF BOTH UTILITY BUS SWITCHES, BOTH RECIRCULATION FAN SWITCHES & RT PACK CONTINUE SELECT. SMOKE PERSISTED 20 PLUS MINUTES THROUGH LANDING. SMOKE DETECTED COCKPIT THEN FIRST CLASS F/A THEN MID CABIN. F/A REPORTED SEEING HAZE IN CABIN. WHILE PREPARING FOR DIVERSION TO MCO NOTICED LEFT HAND ENGINE VIBRATION 3.0 (AMBER) IN NR 1 POSITION. ALL SYSTEMS OPERATED NORMAL IN DESCENT TO MCO. REPLACED APU, & REPLACED VIBRATION ACCELEROMETER TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION.
SFO - OVERHEAD EMERGENCY AISLE LIGHTS AT ROWS 23 AND 27 INOPERATIVE. ADJUSTED LAMP CONTACTS AT OVERHEAD STORAGE BIN 27ABC FOR OVERHEAD EMERGENCY AISLE LIGHTS AT ROWS 23 AND 27. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - MAINTENANCE OBSERVED EMERGENCY LIGHTING INOPERATIVE AT SEAT 29D. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
SNA - FLT 1599 - FLIGHT ATTENDANT OPENED THE L2 DOOR WITHOUT DISARMING THE SLIDE. SLIDE SEPARATED FROM PACK. NO DEPLOYMENT OF INFLATION OF THE SLIDE. DOOR ASSIST BOTTLE WAS FOUND TO BE FLAT. REPLACED THE L2 DOOR SLIDE AND DOOR ASSIST BOTTLE. GROUND CHECKED NORMAL. (M)
LAX - DURING OVERNIGHT CHECK, RIGHT AFT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT AFT EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM ROW 16 AFT INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
LAX - RIGHT ENGINE N3 INDICATION. RIGHT N3 INOPERATIVE. REPLACED RIGHT ENGINE N3 TACH GENERATORS, GROUND CHECKS NORMAL. (M)
LAX - EMERGENCY FLOOR PATH LIGHTS INOPERATIVE FROM SEAT 3E TO 63. REPLACED BROKEN AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
MIA - FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE BETWEEN SEAT 3F AND 6F. REMOVED AND REPLACED BROKEN CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
DFW - AFT LAVATORY EMERGENCY PATH FLOOR TRACK EXIT MARKER LIGHT OUT. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
DFW - LEFT AND RIGHT EMERGENCY LIGHTS AND EMERGENCY EXITS ARE INOPERATIVE. REPLACED BATTERY PACK AND MODULE AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
DFW - FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE FROM SEAT ROW 17 THROUGH 34. REPLACED BATTERY PACK AND MODULE AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
DFW - FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT LEFT AND RIGHT SERVICE DOORS. REPLACED BATTERY PACK AND MODULE AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT DIM. REPAIRED EMERGENCY EXIT LIGHT SPLICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
CCS - FLT 2155 - EN ROUTE DFW-CCS, SHORTLY AFTER LANDING CAPTAIN REPORTED PROBLEMS WITH NOSE LANDING GEAR STEERING SYSTEM. ARRIVED CCS GATE WITHOUT FURTHER INCIDENT. REPLACED NOSE LANDING WHEEL STEERING VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4 THROUGH 12 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTORS AT SEAT 4 AND 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. RE-CONNECTED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT ROW 9 AND ROW 6 INOPERATIVE. REPLACED BAD CONNECTORS AT ROW 9. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT NEAR OVERHEAD BIN AT SEAT 10D INOPERATIVE. TIGHTENED LOOSE WIRES AT SEAT 10D. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN ROWS 3 AND 12 INOPERATIVE. REPLACED END CONNECTOR ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)