N865GA

Part: UNKNOWN — ODOR (CABIN & COCKPIT)

THE ACFT HAD JUST CLIMBED FROM FL310 TO FL330. THERE WAS A SMOKE SMELL REPORTED IN THE CABIN BY THE FA`S. THE PILOTS ALSO COULD SMELL THIS IN THE COCKPIT. THERE WAS NO VISIBLE SMOKE. THE FA`S REPORTED THAT THE AFT LT LAV WAS VERY HOT INSIDE. THE WALL OF THE AFT LT LAV WAS ALSO HOT. THE FA`S IN THE REAR OF THE ACFT REPORTED AN ABNORMAL PULSING SOUND FROM THE REAR OF THE ACFT. FA`S LATER REPORTED THAT THE FLOOR OF THE ACFT WAS GETTING HOT. BASED ON THE SMELL & THE REPORTS FROM THE FA`S THE CAPTAIN DECIDED TO DECLARE AN EMER WITH ATC & PVD WAS RECOMMENDED. THEY WERE GIVEN PRIORITY HANDLING & DID AN EXPEDITED DESCENT. COMPLETED QRH PROCEDURES FOR CABIN FIRE & SMOKE ON PAGE 26.2, NORMAL LANDING. THE CREW DID NOT HAVE THE PAXS BRACE FOR THE LANDING. THE AIRPORT DID HAVE THE EMER EQUIP ROLL OUT TO MEET THE ACFT. THE CREW TAXIED TO THE NORTH TRANSIENT RAMP & PARKED. THE AIRPORT BROUGHT OUT PORTABLE AIR STAIRS & BUSES FOR THE PAXS. THE EMER SLIDES WERE NOT USED. BEFORE & AFTER THE ACFT WAS PARKED THE FIRE DEPARTMENT'S THERMAL SENSING EQUIP DETECTED A HEAT SIGNATURE IN THE BACK OF THE ACFT. THIS WAS VERBALLY REPORTED TO THE CAPTAIN. CAPTAIN WILL COMPLETE AN AIRSMS REPORT FOR THE EVENT.

Part: SEAL — DAMAGED (ANTI-ICE SYS) · airframe 51,135 hrs · 34,355 cycles

THE ACFT HAD JUST CLIMBED FROM FL310 TO FL330. THERE WAS A SMOKE SMELL REPORTED IN THE CABIN BY THE FA'S. THE PILOTS ALSO COULD SMELL THIS IN THE COCKPIT. THERE WAS NO VISIBLE SMOKE. THE FA'S REPORTED THAT THE AFT LT LAV WAS VERY HOT INSIDE. THE WALL OF THE AFT LT LAV WAS ALSO HOT. THE FA'S IN THE REAR OF THE ACFT REPORTED AN ABNORMAL PULSING SOUND FROM THE REAR OF THE ACFT. THE FA'S LATER REPORTED THAT THE FLOOR OF THE ACFT WAS GETTING HOT. BASED ON THE SMELL & THE REPORTS FROM THE FA'S. DECLARED AN EMER WITH ATC. THEY WERE GIVEN PRIORITY HANDLING & DID AN EXPEDITED DESCENT. THE CREW COMPLETED THE QRH PROCEDURES FOR CABIN FIRE & SMOKE ON PAGE 26.2. THERE WAS A NORMAL LANDING. DID NOT HAVE THE PAXS BRACE FOR THE LANDING. THE AIRPORT DID HAVE THE EMER EQUIPMENT ROLL OUT TO MEET THE ACFT. TAXIED TO THE NORTH TRANSIENT RAMP & PARKED. THE AIRPORT BROUGHT OUT PORTABLE AIRSTAIRS & BUSES FOR THE PAXS. THE EMER SLIDES WERE NOT USED. BEFORE & AFTER THE ACFT WAS PARKED THE FIRE DEPARTMENT'S THERMAL SENSING EQUIPMENT DETECTED A HEAT SIGNATURE IN THE BACK OF THE ACFT. THIS WAS VERBALLY REPORTED TO THE CAPTAIN. CAPTAIN WILL COMPLETE AN AIRSMS REPORT FOR THE EVENT. FOUND WING ANTI-ICE LI9NE LEAKING AT COUPLING IN AFT BAG BIN JUST FWD OF P DOME. REPLACED SEALS IN COUPLING & REPLACED COUPLING IAW AMM 30-10-07. LEAKS CHECKED GOOD WITH APU AIR.

Part: SKIN — DENTED (RT WING) · airframe 50,973 hrs · 34,274 cycles

FOUR DENTS L/E RT WING, ONE IS A HOLE, CAUSED BY TOO LONG HARDWARE AT THE 0-1 SLAT ANTI-ICE DUCT COVER. PERFORMED HFEC INSPECTION TO FOUR LOCATIONS OF THE REWORKED AREAS OF THE RT L/E WING IAW EA 20-2015-331, REV A, SECTION 1, AND NOT SPM 06-10-01.001, NO CRACKS FOUND. C/W EA 20-2015-331, REV A, INTERIM NREPAIR IAW EA 20-2015-331, REV A, INSTRUCTIONS. SECTIONS 1. BY REMOVING DAMAGE AND INSTALLING BLIND FASTENERS AT THE 3 OTBD HOLES, IAW SRM 51-30. FILLED INBD HOLE. REMOVED EXCESS AND BLENDED AERO DYNAMICALLY SMOOTH IAW SRM 51-70.

Part: UNKNOWN — ODOR (CABIN) · airframe 50,942 hrs · 34,259 cycles

SUDDEN ODOR OCCURRED, CLIMBING FROM 15 TO 20,000 FT DISAPPEARED WITHIN 2 MINUTES PNEUAMATIC IN NATURE NO RE-OCCURRENCE AFTERWARDS, C/W ALLEGIANT WC 21-59-002, CABIN ODOR/SMOKE TROUBLESHOOTING, TYPE 4, NO ODOR PRESENT NO FURTHER MAINTENANCE REQUIRED. ACFT OK FOR SERVICE.

Part: SPAR CAP — CRACKED (HORIZ STAB) · airframe 50,073 hrs · 33,798 cycles

HORIZONTAL STABILIZER CTR BOX UPPER SPAR CAP IS CRACKED. R & R SPAR CAP IAW SRM 51-30-1, 51-30-2 & 51-30-5. WORK ACCOMPLISHED ON WO 246844 M301 ITEM 647 & WO 1011703 3400-0108.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 50,073 hrs · 33,798 cycles

HORIZONTAL STABILIZER FAIL SAFE FITTING IS CORRODED. R & R HORIZONTAL STABILIZER FAIL SAFE FITTING IAW SRM 51-30-05. WORK ACCOMPLISHED ON WO 246844 M301 ITEM 673 & WO 1011703 3300-0107.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 50,073 hrs · 33,798 cycles

SEAT TRACK GOUGED AT FS 316, RBL 44. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-05 FIG 4F. WORK ACCOMPLISHED ON WO 1011703-2400-0106 M301 ITEM 526.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,876 hrs · 33,704 cycles

L2 DOOR EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW WDM 33-51-14. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 49,519 hrs · 33,527 cycles

L2 DOOR BLUE EMER EXIT SIGN IS INOPERATIVE. FOUND LOOSE PLUG, SECURED IAW AMM 33-53-01. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 49,519 hrs · 33,527 cycles

AFT LT OVERWING EXIT ABOVE DOOR, EXIT SIGN, 1 BULB INOPERATIVE. RELAMPED IAW AMM 33-53-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: PROBE — DEFECTIVE (FUEL SYSTEM) · airframe 49,351 hrs · 33,435 cycles

DURING CLIMB OUT INTERMITTENT LT FUEL INLET LOW PRESS ILLUMINATED IN CONJUNCTION WITH ABNORMAL FUEL DECREASE IN LT MAIN TANK. IN CLIMB & LEVEL FLIGHT FUEL QTY DECREASE CONSISTENTLY FROM 9100 LBS TO 8300 LBS INDICATED, IN DESCENT FUEL QTY REMAINED STEADY. LT NR 6 FUEL QTY PROBE & LT COMPENSATOR PROBE WAS REPLACED IAW LOG PG 535583. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (COCKPIT)

EMERGENCY LIGHTS IN FLIGHT DECK ARE DIM. R & R EMER LIGHT BATTERY AT FWD LAVATORY CEILING IAW AMM 33-35-00. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R POWER SUPPLY BATTERY PACK AND OPS CHECKED IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MX REMOVED AND REPLACED BATTERY PACK AND OPS CHECK ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

Part: PIN — MISSING (EVAC SLIDE)

L1 DOOR SLIDE SAFETY PIN NOT INSTALLED. REMOVED AND REPLACED L1 DOOR SLIDE REF TASK CARD R0902502.

Part: BALLAST — FAILED (CABIN)

FLIGHT ATTENDANT NOTICED SMOKE BY SEAT 19A. PASSENGER STATED SHE NOTICED SMOKE AFTER AN OVERHEAD SIDWALL LIGHT WENT OUT. AFTER TROUBLESHOOTING SYSTEM A BAD BALLAST AT ROW 19 LEFT FOR THE LOWER SIDEWALL LIGHTS. REMOVED AND REPLACED THE BALLAST SYSTEM. OPERATION CHECK WAS GOOD.

Part: SKIN — CORRODED (FUSELAGE)

EXFOLIATION CORROSION AT THE LOWER CORNERS OF THE AFT WASTE SERVICE PANEL. REPAIR FROM FS 1287-1338 BETWEEN L18L TO L23L PER MD80 SRM 51-10-38 PG 1. REMOVED CORROSION FROM OUTER SKIN AT THE FWD LOWER CORNER OF THE AFT LAV SERVICE DOOR CUTOUT. REMOVED CORROSION FROM INNER DOUBLER AT THE FWD LOWER CORNER OF THE AFT LAV SERVICE DOOR CUTOUT. FAB'D PARTS IAW MD-80 SRM 53-02. FABRICATED 2 EA FILLER IAW STS EA 12-2012-348. FABRICATED REPAIR DOUBLER AND TRIPLER IAW STS EA12-2012-348. INSTALLED REPAIR DOUBLER AND TRIPLER AND 2 EA FILLERS AT AFT LAV SERVICE PAN CUTOUT PER STS EA12-2012-348. INSTALLED REPAIR PARTS AT STA 1338-1389 LONGERON 24L PER MD-80 SRM 53-02 FIG 18.

Part: SKIN — CORRODED (FUSELAGE)

EXFOLIATION CORROSION AT THE LOWER CORNERS OF THE AFT WASTE SERVICE PANEL. REPAIR FROM FS 1287 TO FS 1338 BETWEEN LONGERON L-18L TO L-23L PER MD80 SRM 51-10-38 PG 1. CUT OUT AND REMOVED CORROSION FROM OUTER SKIN AND DOUBLER AT THE FWD LOWER CORNER OF THE AFT LAV SERVICE DOOR CUTOUT. FABRICATED FILLER, DOULBER AND TRIPLER IAW STS EA 12-2012-348. INSTALLED REPAIR DOUBLER AND TRIPLER AND 2 EA FILLERS AT AFT LAV SERVICE PAN CUTOUT PER STS EA12-2012-348. INSTALLED REPAIR PARTS AT STA 1338-1389 LONGERON 24L PER MD-80 SRM 53-02 FIG 18.

Part: LONGERON — CRACKED (FUSELAGE)

RIGHT WHEEL WELL STA 1030 AREA, LONGERON 20A CRACKED. CUT OUT DAMAGED AREA, HFEC INSPECTED FILLER AND DOUBLERS, LOCATED, DRILLED AND INSTALLED IAW MD80 SRM 53-03 FIG 2.

Part: SPAR CAP — CORRODED (RT WING)

RIGHT WING FWD SPAR STA 533, LOWER CAP FLANGE CORRODED, REMOVED CORROSION, REMAINING THICKNESS .124, 1.0" IN LENGTH, HFEC INSPECTED AREA. NO CRACKS NOTED PER NDT SPM PART 06-10-01-063, PROCEDURE 3. INSTALLED FILLER AND REPAIR STRAP IAW STS ENGINEERING 10-2012-061, PERMANENT REPAIR.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: VANE — GOUGED (TE FLAP)

RIGHT WING OUTBOARD FLAP INBOARD VANE LEADING EDGE IS GOUGED IN 2 PLACES. REPAIRED RIGHT WING O/B FLAP I/B VANE IAW MD80 SRM 57-03 PG 27.

Part: FLOOR PANEL — CORRODED (CABIN)

PASSENGER FLOOR PANEL HAS MULTIPLE CORRODED INSERTS FS 160 TO 198 LBL 10 TO LBL 50. FABRICATED CABIN FLOOR PANEL IAW MD80 SRM 53-05 PARA 59.

Part: FLOOR PANEL — PUNCTURED (CABIN)

PASSENGER CABIN FLOOR PANEL HAS PUNCTURES FS 927, LBL 42. FABRICATED CABIN FLOOR PANEL IAW MD80 SRM 53-05 PARA 59.

Part: FLOOR PANEL — CORRODED (CABIN)

CABIN FLOOR PANEL STA 160-200 RT HAS MULTIPLE CORRODED INSERTS. FABRICATED NEW FLOOR PANEL IAW MD80 SRM 53-05, PARP 59.

Part: FLOOR PANEL — PUNCTURED (CABIN)

PASSENGER CABIN RT O/B FLOORBOARD PANEL FS 886 TO 927 HAS MULTIPLE PUNCTURES. REPAIR CABIN FLOORBOARD PANEL IAW DC9/MD80 SRM 53-05, FIG 1 AND SRM 51-30-02 FIG 3.

Part: FLOOR PANEL — CORRODED (CABIN)

CABIN FLOOR PANEL STA 200-256 CENTER HAS MULTIPLE AREA OF DAMAGE AND CORRODED INSERTS. FABRICATED NEW FLOOR PANEL IAW MD80 SRM 53-05, PARA 59.

Part: FLOOR PANEL — PUNCTURED (CABIN)

PASSENGER CABIN RIGHT O/B FLOORBOARD PANEL FS 886 TO 927 HAS MULTIPLE PUNCTURES. REPAIR CABIN FLOORBOARD PANEL IAW DC9/MD80 SRM 53-05 FIG 1, AND SRM 51-30-02 FIG 3.

Part: TAB — DAMAGED (AILERON)

DURING PREPARATION FOR PAINT, FOUND RT AILERON TAB DAMAGED COMPOSITE AT CENTER HINGE AREA. REPAIRED DAMAGED COMPOSITE ON RT AILERON CONTROL TAB AT CENTER HINGE AREA IAW BOEING MD80 SRM 51-70-1A, PAGE 41.

Part: DOUBLER — CRACKED (FUSELAGE)

RT WINDOW NR 9 (NOT INCLUDING PLUG) INTERNAL CUT OUT DOUBLER AFT LOWER CORNER IS CRACKED (FS 408). CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-05, FIG 122.

Part: DOUBLER — CRACKED (FUSELAGE)

RT WINDOW 38 (NOT INCLUDING PLUG OR EXIT HATCH) INTERNAL CUTOUT DOUBLER FWD UPPER CORNER IS CRACKED (FS 984). CUT OUT DAMAGED AREA, INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-05, FIG 122.

Part: DOUBLER — CRACKED (FUSELAGE)

LEFT FS 946 PAX CABIN WINDOW CUTOUT INTERNAL DOUBLER (RING PAN) IS CRACKED AT FWD UPPER CORNER. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-05, FIG 122.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REPLACED OVERWING EMERGENCY LIGHT ASSEMBLY AS REQUIRED. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (FUSELAGE)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: CUSP WEB — CRACKED (ZONE 100)

ONE INCH CRACK IN CUSP AT STA 806 RT SIDE.

Part: BALLAST — BURNED (CABIN LIGHTS)

FOUND SMOKE IN FORWARD LAV WHILE DEPLANING PASSENGERS. ODOR LIKE ELECTRICAL SMOKE. DISCOVERED BY CAPTAIN. IMMEDIATELY REMOVED ELECTRICAL POWER FROM AIRCRAFT. MAINTENANCE DEPARTMENT PERSONNEL REPLACED LIGHT BALLAST AND ELECTRICAL CONNECTER. SYSTEM OPERATIONAL CHECK NORMAL. ACFT OK TO RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: A/C PACK — SMOKE (LEFT)

FLIGHT 603 FROM BLI, THE FLIGHT CREW DETECTED SMOKE IN THE CABIN, DECLARED AN EMERGENCY AND RETURN TO BLI. ON CALL MX PERSONNEL WERE DISPATCHED TO THE ACFT BY MX CONTROLLER. AIR CONDITIONING SYSTEM WAS INSPECTED AND IT WAS DETERMINED THAT THE LT AIR CONDITIONING SYSTEM WAS AT FAULT AND THE SYSTEM WAS DEFERRED. ADDITIONALLY IAW GMM PROCEDURES AN AIRBORNE SYSTEM TEST WAS ACCOMPLISHED WITH THE LT AIR CONDITIONING SYSTEM "OFF", NO SMOKE WAS DETECTED IN THE CABIN. THE LT AC SYSTEM DEFERRAL WAS CORRECT BY INSPECTING AND CLEANING THE LT PACK CABIN DUCT SENSOR. ACCOMPLISHMENT OF THE OPERATIONAL CHECK IAW AMM 21-61-00. CHECKED NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL BOX — MALFUNCTIONED (ANTI SKID SYSTEM)

DURING TAKEOFF ROLL WHEEL NOT TURNING LIGHT ILLUMINATED AT 70 KNOTS. NO DRAG FROM WHEELS WAS NOTED. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE AT LAS VEGAS. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED AND REPLACED ANTI-SKID CONTROL BOX IAW M/M 32-43-00. OPERATIONAL CHECK NORMAL IAW MM 32-43-02, AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL RELAMPED THE EMERGENCY LIGHT ASSEMBLY AS REQUIRED. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A SERVICE CHECK MAINTENANCE DEPARTMENT PERSONNEL IN LAS VEGAS REPORTED THAT EMERGENCY FLOOR PATH LIGHTING WAS INOP AND MISSING SEGMENTS. LAS VEGAS MAINTENANCE REPLACED AND SECURED EMERGENCY FLOOR PATH LIGHTING. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: SWITCH — MALFUNCTIONED (SLAT/FLAPS)

FLIGHT 485 BIL/LAS, THE FLIGHT CREW REPORTED THAT THE AUTOSLAT FAIL ANNUNCIATOR ILLUMINATED ON APPROACH WHEN FLAPS 15 WAS SELECTED. LAS VEGAS MAINTENANCE REPORT THAT TROUBLESHOOTING REVEALED FLAP/SLAT POSITION SWITCH S1-467 HAD FAILED. LAS VEGAS FURTHER REPORT THE REMOVAL AND INSTALLATION OF THE FLAP/SLAT POSITION SWITCH AT THE FLAP SELECT LEVER PER AMM 27-80-07. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 27-80-07. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING)

FLIGHT 453 ICT/LAS - THE FLIGHT CREW REPORTED THAT "AUTOSLAT FAIL" ANNUNCIATOR ILLUMINATED DURING APPROACH TO LAS. WHILE THE LOGBOOK ENTRY SPECIFIES THAT A QRH PROCEDURE WAS ACCOMPLISHED IT DOES NOT SPECIFY WHETHER A SINGLE STALL SYSTEM WAS IDENTIFIED OR BOTH. LAS VEGAS MAINTENANCE REPORT THE REMOVAL AND REPLACEMENT OF THE NR 1 STALL WARNING COMPUTER. A SATISFACTORY OPERATIONAL CHECK OF THE STALL WARNING SYSTEM PER AMM 34-19-02 AND OF THE AUTOSLAT SYSTEM PER AMM27-81-00 WAS ACCOMPLISHED. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: CSD — OVERSERVICED (RIGHT)

FLIGHT 478 LAS/FAR, THE FLIGHT CREW REPORTED THAT THE RIGHT CSD OIL TEMPERATURE INDICATION WAS READING HIGH AND DISCONNECTED THE RIGHT CSD. THE FLIGHT CREW DID NOT SPECIFY. FAR CONTRACT MAINTENANCE DEFERRED THE CSD/GENERATOR UNDER THE DIRECTION OF MAINTENANCE CONTROL PER MEL 24-01. THE AIRPLANE RETURNED TO LAS WHERE MAINTENANCE REPORT THAT THE RIGHT CSD WAS FOUND OVER SERVICED. LAS VEGAS MAINTENANCE FURTHER REPORT THAT THE CSD WAS CORRECTLY SERVICED PER AMM 12-12-01. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE MEL REMOVED. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN

FLIGHT 479 FAR/LAS - THE FLIGHT CREW REPORTED THAT AT 250KIAS, AERODYNAMICALLY "CLEAN", THE 'ELEVATOR POWER ON' ANNUNCIATOR ILLUMINATED MOMENTARILY. SIMULTANEOUSLY, THERE WAS A "JOLT" TO THE AIRPLANE. THE FLIGHT CONTINUED TO LAS, THE FLIGHT CREW MADE NO MENTION OF ANY PROCEDURE PERFORMED, WHERE IT LANDED WITHOUT FURTHER REPORTED INCIDENT. LAS VEGAS MAINTENANCE REPORT AN ACCEPTABLE OPERATIONAL CHECK OF THE ELEVATOR POWER SYSTEM PER AMM27-30-07, AN ACCEPTABLE AUTO PILOT SYSTEM OPERATIONAL CHECK PER AMM22-01-05 AND AN ACCEPTABLE OPERATIONAL CHECK OF THE HORIZONTAL STABILIZER TRIM SYSTEM PER AMM 27-40-00. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: SKIN — GROUND DAMAGE (PAX DOOR)

FLIGHT 461 PIA/LAS - AFTER PASSENGER LOADING, BEFORE PUSHBACK, AN EFFORT WAS MADE TO CLOSE THE MAIN ENTRY DOOR BUT IT WAS RESTING ON THE JETWAY DECK. THE JETWAY OPERATOR RETRACTED THE JETWAY WITHOUT LOWERING IT. AS A RESULT, THE L1 DOOR SKIN SUSTAINED A .5 BY .6 INCH AREA OF DAMAGE. THE AIRPLANE WAS PREPARED FOR FERRY AND WAS DELIVERED TO TULSA WHERE AMERICAN AIRLINES ACCOMPLISHED A PERMANENT REPAIR OF THE L1 DOOR IN ACCORDANCE WITH ESO NR 80559 DATED 22 FEB, 2007. HFEC INSPECTION REVEALED NO CRACKS. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: CONTROL BOX — MALFUNCTIONED (O2 MASK)

LAS - DLH - CREW REPORTED THE FIRST OFFICERS TRANSMITTER INOPERATIVE ON ANY MIC. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FIRST OFFICERS OXYGEN MASK SYSTEM CAUSING DISTORTION IN THE FIRST OFFICERS COMM. REMOVED AND REPLACED FIRST OFFICERS OXYGEN MASK BOX ASSEMBLY IAW MM 35-10-04. COMM OPERATIONALLY CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

LAS - MAINTENANCE REPORTED EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE.

Part: COALESCER BAG — CONTAMINATED (ACM)

IFP - ABORTED TAKEOFF (HIGH SPEED 110-115 KNOTS) DUE TO STRONG AND PRONOUNCED ACRID/RUBBERY SMELL. MAINTENANCE INSPECTED ACM’S, WATER SEPARATORS, DRAINS AND ANTI-ICE SCREENS WITH NO DEFECTS NOTED. MAINTENANCE CLEANED COALESCER BAGS. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 21-20-02. AIRCRAFT RETURNED TO SERVICE.

Part: COALESCER BAG — CONTAMINATED (CABIN AIR)

RNO TO YKM - CREW REPORTED STRONG SULPHURIC SMELL COMING OUT OF THE VENTS ON CLIMB-OUT. AIRCRAFT RETURNED TO RNO WHERE CREW REPORTED RUBBER/ACRID SMELL ON FINAL DESCEND. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND DIRTY COALESCER BAGS, MAINTENANCE REMOVED AND REPLACED COALESCER BAGS IAW MM 21-20-02. PERFORMED HIGH POWER RUNS AND COULD NOT DUPLICATE SMELL. AIRCRAFT RETURNED TO SERVICE.

Part: ANNUNCIATOR — ILLUMINATED (AIRSTAIR DOOR)

IFP TO SJC-AFT STAIRWAY DOOR ANNUNCIATOR ILLUMINATED DURING TAKEOFF. TAKEOFF WAS ABORTED. CREW CONTACTED MAINTENANCE CONTROL, AFT STAIRWAY ANNUNCIATOR WAS DEFERRED IAW MEL 52-7. AIRCRAFT RETURNED TO SERVICE.

Part: STEERING SYS — MALFUNCTIONED (NLG)

FNL TO LAS - CREW CONTACTED MAINTENANCE CONTROL TO REPORT AIRCRAFT NOSE WHEELS DROVE OFF TAXIWAY INTO DIRT AT FNL. MAINTENANCE POSITIONED AIRCRAFT BACK ONTO TAXIWAY AND INSPECTED NOSE LANDING GEAR IAW 05-51-03 A-CHECK. NO DAMAGE NOTED, OKAY FOR CONTINUED SERVICE. AIRCRAFT RETURNED TO SERVICE .

Part: LIGHT — INOPERATIVE (CABIN)

LAS-MAINTENANCE REPORTED EMERGENCY OVERHEAD LAMPS BURNED OUT (3 EACH). MAINTENANCE RELAMPED OVERHEAD LAMPS (3 EACH), OPERATIONALLY CHECKED GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE.

Part: STRUCTURE — BIRD STRIKE (LT WING)

LAS - CREW REPORTED BIRD STRIKE LEFT WING TRAILING EDGE. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-51-08. NO DAMAGE FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

LAS-MAINTENANCE REPORTED EMERGENCY LIGHT INOPERATIVE AT ROW 15 CEILING. MAINTENANCE RE-LAMPED BURNT OUT BULB IAW 33-52-00. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.