N403NV

Part: ROD END — DISCONNECTED (RT MLG) · airframe 60,119 hrs · 43,386 cycles

GEAR DOOR OPEN LANDING, FOUND RT MLG DOOR OPEN AND DAMAGED. ALSO FOUND UPLOCK ROD END NOT CONNECTED. REMOVED GEAR DOOR. INSPECTED HINGE AND ACTUATOR MOUNT CASTING. NO DAMAGE NOTED CONTINUED ON LOG PAGE 708777.

Part: WEB — CORRODED (BS 1338) · corrosion level 2 · airframe 67,988 hrs · 43,363 cycles

CABIN FLOOR CORRODED ON VERTICAL WEB. REPAIRED WEB IAW EA 40-2016-317.

Part: CADC — FAILED (LEFT) · airframe 58,496 hrs · 43,249 cycles

FIRST OFFICER`S AIRSPEED INDICATOR READ"ZERO KIAS DURING TAKEOFF ROLL. ABORTED TAKE OFF, HIGH SPEED ABORTED TAKEOFF. CAPTAIN`S AIRSPEED INDICATOR READ 80 KIAS. THERE WERE NO FLAGS, TROUBLESHOOTING FOUND ALL FAULT LIGHTS ILLUMINATED AT NR 1 CADC, R & R THE NR 1 CADC IAW AMM 34-16-01, NR 1 & 2 DFGC RETURNED TO SERVICE IAW AMM 22-01-05. R & R THE NR 2 AIRSPEED INDICATOR IAW AMM 34-13-01. OPS CHECKED GOOD.

Part: ENGINE — FAILED (RIGHT) · airframe 67,207 hrs · 42,945 cycles

DURING THE TAKEOFF THE CREW NOTED A LOUD BANG FOLLOWED BY ALL PARAMETERS FLASHING ON THE RT ENG. FIRST OFFICER CALLED THE ABORT AT 100 KTS AFTER SEEING ALL OIL QTY GONE & DASHES ON THE N1. THERE WAS SMOKE IN THE CABIN AT THE TIME OF THE EVENT. THE CREW DECLARED AN EMER & PULLED OFF THE RUNWAY. THE CAPTAIN CALLED TO THE CABIN & ASKED IF THE SMOKE WAS DISSIPATING AS FIRE RESCUE INSPECTED THE EXTERIOR OF THE ACFT. THE FLIGHT TAXIED BACK TO THE GATE UNDER ITS OWN POWER & DEPLANED NORMALLY. CREW THEN CALLED INTO DISPATCH & DUTY PILOT. CAPTAIN SECURED THE CB FOR THE DFDR & THE CVR. ONE FLIGHT ATTENDANT WAS TREATED BY EMT'S FOR SMOKE INHALATION. CREW & PAXS WERE SECURED SEPARATELY. R&R NR 2 ENGINE.

Part: REGULATOR VALVE — FAULTY (AC BAY) · airframe 66,977 hrs · 42,832 cycles

WITH TAKEOFF POWER ON LATIER RALE OF TAKEOFF & CLIMB OUT STROAS BURNING RUBBER SMELL FILLED THE CABIN. FA RETRACED SMELL TO COMPORT 3 TO 4 MINUTES, AFTER CLIMB POWER SELECTED BURNING RUBBER SMELL DISSIPATED. R & R LT PRESS REGULATOR VLV IAW AMM 21-31-01-2. OPERATIONS CHECKED GOOD.

Part: ENGINE — STALLED (NR 2) · airframe 66,973 hrs · 42,829 cycles

DURING CLIMB NR 2 ENGINE HAD COMPRESSOR STALLS. PERFORMED QRH 72.8, STALLS STOPPED, CONTINUED FLIGHT. NR 2 ENGINE HAD LOW EPR & N1W & HIGH EGT & EQUAL N2. R & R RT ENGINE.

Part: OIL SYSTEM — LEAKING (LT ENGINE) · airframe 66,815 hrs · 42,751 cycles

AFTER TAKEOFF. LAVATORY SMOKE ANNUNCIATOR ILLUMINATED FOR FWD LAVATORY DURING QRH CHECKLIST, ANNUNCIATOR EXTINGUISHED. IN COCKPIT ODOR OF EVAPORATING OIL NOTED. TROUBLESHOOTING ACCOMPLISHED ON LP 610870 & 610871, LT ENG REPLACED IAW WO 279553. ENG RUNS ACCOMPLISHED.

Part: A/C PACK — MALFUNCTIONED (AC BAY) · airframe 66,800 hrs · 42,741 cycles

SHORTLY AFTER TAKEOFF LAVATORY SMOKE ANNUNCIATOR WENT OFF & MASTER CAUTION LAVATORY SMOKE DETECTOR WAS AUDIBLE THROUGHOUT THE CABIN & FLIGHT DECK. FLIGHT ATTENDANTS REPORT AFT RT SMOKE DETECTOR GOING OFF & A GRAY HAZE BEGAN TO FILL CABIN & FLIGHT DECK WHICH DISSIPATED ON LANDING. WARM AREA FOUND INFLIGHT AROUND LAVATORY SMOKE DETECTOR. RT AFT LAVATORY COOLED AFTER LANDING. RAN ENGS 1 & 2 WHILE ISOLATING PACK OPERATION FROM RT TO LT PACK. WHILE DOING SO, CONFIRMED ODOR FROM LT PACK OPERATION. NR 1 PACK PLACED ON DEFERRAL & MEL 21-01 S1. COMPLIED WITH M ACTION, DMI 21596. CLASS C, PLACARDS INSTALLED.

Part: FILTER — DIRTY (AC BAY) · airframe 66,735 hrs · 42,702 cycles

JUST AFTER DEPARTURE, THE CREW RECEIVED, LAV SMOKE DET, ANNUNCIATOR WITH THE ASSOCIATED CAUTION LIGHT. THE CREW HEARD THE AUDIBLE LAVATORY SMOKE ALARM & THE FLIGHT ATTENDANTS CALLED FWD SHORTLY AFTER REPORTING WHAT WAS GOING ON & THAT THERE WAS A HAZE IN THE CABIN WITH A SMOKE SMELL. DECLARED AN EMER & EXECUTED QRH 26.9 LAVATORY SMOKE DETECTOR ACTIVATION CHECKLIST. ON THE BASE TO FINAL LEG THE ANNUNCIATOR WENT OUT & THE LANDING WAS UNEVENTFUL. THE PAXS WERE NOT BRACED. THE FIRE DEPARTMENT INSPECTED THE ACFT & THE FLIGHT RETURNED TO THE GATE UNDER ITS OWN POWER WHERE THE FD WAS ABLE TO GET TO THE LAVATORIES TO INSPECT THEM. MX WILL COME OUT TO TROUBLESHOOT, REPEAT ITEM. PERFORMED ENGINE RUNS FOUND WITH RT ENGINE RT PACK ON LT BLEED LT PACK OFF LAV SMOKE WAS INDICATED AT 7.0 PSI CABIN PSI. RAN LT ENGINE LT PACK ON RT BLEED OFF LT PACK OFF FOR 45 MINUTES NO LAV SMOKE INDICATED AT 7.0 PSI CABIN PSI. R&R WATER SEPARATOR FILTERS IAW AMM 21-20-02-4-0. RT ACM SHOWS SIGNS OF OIL LEAKING DEFERRED RT PACK IAW MEL 21-01 SIT 1 DMI 21176 CAT C PLACARD

Part: HYDRAULIC LINE — DAMAGED (HYDRAULIC SYS) · airframe 66,668 hrs · 42,667 cycles

FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN AFTER TAKEOFF. CBS J8, J9 & J10 ALL POPPED. 18 DURING TROUBLESHOOTING OF ODOR & SMOKE FOUND APU OIL FILTER LEAKING. R & R APU OIL FILTER O RING. LEAK CHECKED GOOD IAW MM 49-90-06. DURING TROUBLESHOOTING FOUND HYD FLUID LEAK RUNNING DOWN FUSELAGE & INTO APU INLET & FOUND RT HYD RESERVOIR RELIEF & BLEED VLV DRAIN HOSE DAMAGED, CAUSING HYD FLUID TO FILL KEEL BEAM & LEAKING DOWN FUSELAGE INTO APU INLET, REPAIRED. LEAK CHECKED GOOD IAW MM 29-10-03. R & R RECIRC FAN. REPLACED APU OIL FILTER O RINGS & FILTER. RT HYD RESERVOIR RELIEF BLEED HOSE DETERIORATED, REPLACED HOSE. PERFORMED TASK CARD 21-059-008 ACFT WATER SEPARATOR & PACK BURNOUT PROCEDURES COMPLIED WITH. SEE WO 00274708 PERFORMED TASK CARD 21-059-002. ALL ISSUES REPAIRED & OPERATIONS CHECKED GOOD.

Part: UNKNOWN — SMOKE (CABIN)

THE CREW SMELLED SMOKE AT ROTATION. FLIGHT ATTENDANTS CALLED SECONDS LATER. SMOKE WAS COMING FROM GASPERS IN THE FWD GALLEY. SMOKE WAS SO THICK THAT THE FLIGHT ATTENDANTS IN THE BACK OF THE AIRPLANE COULD NOT SEE THE FRONT. AN EMER WAS DECLARED WITH THE TOWER. TURNED OFF PACKS, DID THE AIR RETURN CHECKLIST & RETURNED TO LAND. FIRE RESCUE MET THE ACFT ON THE RNWY & SAID EVERYTHING ON THE OUTSIDE OF THE ACFT, APPEARED TO BE OKAY. THE CREW THEN RETURNED TO THE GATE & THE PAXS DEPLANED. THIS ACFT WAS NOT OVERWEIGHT FOR LANDING.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 66,550 hrs · 42,601 cycles

AFT EMER FLASHLIGHT INOPERATIVE. REPLACED BATTERY IAW LOPA & MM 25-60-01".

Part: ENGINE — OVERTEMP (LEFT) · airframe 66,486 hrs · 42,557 cycles

CLIMBING OUT OF 16,000 FEET THE CREW NOTICED THAT THEY HAD AN INDICATION OF OIL TEMP HIGH ON THE NR 1 ENG. THE OIL TEMP WAS 145 & THE FUEL TEMP WAS 99. THE AUTO FUEL HEAT SYS WAS ON, BUT HEAT WAS NOT BEING APPLIED AT THE TIME. THE CREW DID THE QRH PROCEDURE FOR OIL TEMP HIGH ON PAGE 72.17. AFTER THE ENG OIL TEMP WAS OVER 135 FOR GREATER THAN 15 MINUTES, THE CREW SHUT THE NR 1 ENG DOWN. THEY DECLARED AN EMER & RETURNED FOR LANDING. R&R ENGINE IAW TASK CARD 71-080-003 OIL TEMPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 66,003 hrs · 42,320 cycles

AFT FLIGHT ATTENDANT STATION OVERHEAD EMER LIGHTS & TAIL CONE LOWER LIGHT INOPERATIVE. BATTERIES CHECKED GOOD WITH EMER LIGHTS ON CHECK, POWER TO THE POWER SUPPLY TERMINALS, NO VOLTAGE NOTED. REPLACED POWER SUPPLY. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,705 hrs · 25,028 cycles

AFT FLIGHT ATTENDANT STATION EMER LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: BATTERY — DISCHARGED (CABIN)

AFT FLIGHT ATTENDANT STATION EMER LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: WIRE — DAMAGED (CABIN) · airframe 65,695 hrs · 42,153 cycles

EMERGENCY LIGHTS ALONG TAIL COMPARTMENT RAMP INOPERATIVE. WIRES BROKEN. REPAIRED DAMAGED WIRING BY R & R TERMINALS AT LIGHT L2-847 IAW SWPM 20-20-01. EMER LIGHTS TESTED GOOD IAW MM 33-53-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,654 hrs · 42,133 cycles

UPON REMOVAL OF RT MLG JAMB CHANNEL FOUND INTERCOSTAL TO BE CRACKED. REMOVED, LOCATED & DRILLED NEW INTERCOSTAL & INSTALLED IAW SRM 51-30-2, 51-30-5 & 51-10-4.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 65,654 hrs · 42,133 cycles

RIGHT SUPPORT CHANNEL CRACKED STATION 946.0 NEXT TO KEEL BEAM. STOP DRILLED CRACK, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-01 FIG 2.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 65,654 hrs · 42,133 cycles

LEFT SUPPORT CHANNEL CRACKED AT THE INBD CORNER. STOP DRILLED CRACK, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-01 FIG 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,654 hrs · 42,133 cycles

FLOORBEAM AT FS 256 HAS CORROSION BETWEEN RBL 22 & RBL 44. FABRICATED & INSTALLED FLOOR SUPPORT IAW SRM 51-10-4 & 51-30-5, WITH 4½ LENGTH 1½ ORIGINAL .070 REMAINING 0. LEVEL 2 WORK ACCOMPLISHED ON WO 243433 M301 ITEM 530 & WO 1011609 2000-0183.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,654 hrs · 42,133 cycles

FLOORBEAM AT FS 256 HAS CORROSION BETWEEN LBL 22 & RBL 22. FABRICATED & INSTALLED FLOOR SUPPORT IAW SRM 51-10-4 & 51-30-5 WITH 2 1/2 LENGTH 1 1/2 ORIGINAL .070 REMAINING 0 LEVEL 2. WORK ACCOMPLISHED ON WO 243433 M301 ITEM 529 & WO 1011609 2000-0182.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 65,654 hrs · 42,133 cycles

VERTICAL FLOORBEAM SUPPORT CRACKED FS 905 LBL 44. REMOVED, FABRICATED & INSTALLED NEW SUPPORT IAW SRM 51-30-5, 51-10-4 & 51-10-3.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 65,297 hrs · 41,944 cycles

L1 DOOR EMER FLASHLIGHT INOPERATIVE. R & R L1 DOOR EMER FLASHLIGHT IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT)

FOUND ON WAKE UP. FLIGHT DECK EMER LIGHTS INOPERATIVE. RELAMPED FLIGHT DECK EMER LIGHTS. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: LIGHT — INOPERATIVE (TAILCONE)

FOUND ON WAKE UP. TAIL CONE EMER LIGHTS INOPERATIVE & TWO AFT DROP PANEL LIGHTS BETWEEN THE LAVATORIES. RELAMPED CTR TAIL CONE LIGHT. REPLACED BATTERIES FOR THE LOWER TAIL CONE LIGHT & THE TWO DROP PANEL LIGHTS. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: CIRCUIT BREAKER — FAULTY (CSD)

R CSD GAUGE RISE FUNCTION INOPERATIVE. REF LOG PG 507302 REPLACED CSD OIL TEMP B1-179. OPERATIONS CHECKED GOOD IAW MM 24-10-01. 7/29/14 R & R RELAY R2-80, NO HELP. R & R CB B1-179 & FIXED PROBLEM. NO REPEATS OR HISTORY. 8/5/14 NO REPEATS AFTER CB REPLACED. 31 FLIGHTS WITH NO REPEATS.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EXTERIOR EMER LIGHTS INOPERATIVE ON BOTH RT & LT SIDE. R & R BATTERY POWER SUPPLY IAW AMM 33-50-00. OPERATIONS CHECKED GOOD.

Part: ENGINE — MALFUNCTIONED (LEFT)

AT 11,000 FT DURING CLIMB OUT, LT OIL PRESS LOW AOP WITH FALLING LT OIL PRESS ON GAUGE <30 PSI & FALLING FAST. IAW QRH 72/14 WITH OIL PRESS BELOW 35 PSI, SHUT DOWN ENG. COMPLIED WITH QRH PROCEDURE 72.3, ENG SHUTDOWN, LANDED SINGLE ENG. IAW WORK ORDER 228642 REPLACED LT ENG. LEAK OPERATIONS CHECKED GOOD.

Part: CHIP DETECTOR — UNSECURE (LT ENGINE)

AIR RETURN FOR LOSS OF LT ENG OIL PRESS. DURING INSPECTION, FOUND GEARBOX MAGNETIC CHIP DETECTOR MISSING FROM HOUSING & HANGING FROM FUEL BRIDLE. REPLACED CHIP DETECTOR ASSEMBLY IAW AMM 79-20-05. NO LEAKS NOTED, SERVICED LT ENG OIL TO FULL.

Part: LENS — DAMAGED (CABIN)

EMERGENCY LIGHT LENS COVER AISLE DAMAGED. INSTALLED EMER LIGHT LENS COVER AT AISLE 21 IAW MM 33-53-01. NO FURTHER DEFECTS NOTED.

Part: FINGER DOUBLER — CORRODED (AFT CARGO BAY)

AFT CARGO PIT FINGER DOUBLER EXFOLIATED ABOVE LONG 26L AT BS 1302. CUT OUT DAMAGED AREA, FABRICATED, FILLER, DOUBLER, LOCATED, DRILLED, AND INSTALLED IAW STS EA 12-2013-462

Part: WEB — PUNCTURED (BS 148.5)

FLT DECK FLOOR PAN WEB PUNCTURED STA 148.5, RBL 28. CUTOUT DAMAGED AREA, FABRICATED DOUBLER, FILLER, LOCATED, DRILLED, AND INSTALLED IAW SRM 51-70-4.

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 — 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 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 — 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: CUSP WEB — CRACKED (BS 1174-1193)

PASSENGER CABIN RT CUSP WEB CRACKED BETWEEN FS 1174 & 1193. REPAIRED RT CUSP WEB IAW SRM 53-01 FIG 4.

Part: FRAME — GOUGED (BS 1136 L17R)

PASSENGER CABIN FS 1136 L17R FRAME GOUGED AT LONGERON 17R. REPAIRED FRAME IAW SRM 53-04 FIG 4.

Part: CUSP WEB — CRACKED (BS 1231-1250)

RIGHT CUSP WEB CRACKED BETWEEN FS 1231 & 1250. REPAIRED WEB IAW DWG SG09530019.

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 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 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: LINE — DEFECTIVE (NR 1 ENGINE)

DURING DESCENT THROUGH FL 190 OIL PRESSURE LOW ANNUNCIATOR ON AMD OIL PRESSURE DROPPING BELOW 35 PSI, FOLLOWED EQRH EFFECTED ENGINE (NR 1). REPLACED NR 4 BEARING OIL SUPPLY LINE IAW AMM 79-20-00 LEAKED CHECKED LINE, NO LEAKS NOTED, AIRCRAFT GOOD FOR 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: WEB — GOUGED (NLG WW)

NOSE GEAR LOCK LINK ACTUATOR BAY RIGHT INBOARD WEB FACE GOUGED. REPAIRED WEB IAW MD80 SRM 51-70-4 FIG 2.

Part: FRAME — CORRODED

FRAME CORRODED AFT SIDE STA 1193 BETWEEN LONG 30 AND 29L. REPAIRED FRAME STA 1193 IAW MD80 SRM 51-10-4 AND SRM 51-30-2.

Part: FRAME — CORRODED (FUSELAGE)

FS 1231 FRAME CORRODED ON TOP AND BACKSIDE OF L27-L30 LEFT, ADDRESSED AS REQUIRED.

Part: THRESHOLD — CORRODED (FUSELAGE)

AFT CARGO PIT THRESHOLD LOWER WEB AT DOOR CUTOUT CORRODED. REMOVED DAMAGED WEB. LOCATED, DRILLED AND INSTALLED A REPLACEMENT WEB IAW MD80 SRM 51-10-4, 51-30-2 AND 51-30-5.

Part: LONGERON SPLICE — CRACKED (FUSELAGE)

AFT CARGO PIT LONGERON SPLICE AT STA 1211 AND LONGERON 28L CRACKED. REMOVED AND REPLACED LONGERON SPLICE FWD OF STA 1211 AT LONGERON 28L IAW MD80 SRM 51-30-5.

Part: SHEAR TIE — CORRODED (FUSELAGE)

UPON ACCESSING AFT CARGO PIT BEAM REPAIR, FOUND SHEAR TIE FS 1136, L28R AND L29R CORRODED. FABRICATED NEW SHEAR TIE IAW MD80 SRM 51-10-4 PG 1 AND DAC DRAWING 9936578.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

AFT CARGO PIT INTERCOSTAL CORRODED STA 1322 BETWEEN LONGERON 28R AND 27R. REMOVED DAMAGED INTERCOSTAL, LOCATED DRILLED AND INSTALLED A REPLACEMENT INTERCOSTAL IAW MD80 SRM 51-30-2 AND 51-30-5.

Part: SKIN — DAMAGED (ELEVATOR TAB)

LEFT ELEVATOR LIGHTNING STRIKE AT TRAILING EDGE CENTER AREA OF GEAR TAB. REMOVED DAMAGED SKIN AT LIGHTNING STRIKE AREA. PREPPED, FABRICATED AND BONDED REPAIR DOUBLER IAW MD 80 SRM 51-70-2 PARAGRAPH E PG 174.

Part: BEAM — CORRODED (CARGO BAY)

AFT CARGO PIT LONGERON 29R BEAM CORRODED AT PREVIOUS REPAIR STA 1195. REMOVED DAMAGED BEAM STA 1117 TO STA 1250 LOCATED, DRILLED, INSTALLED A REPLACEMENT BEAM IAW MD80 SRM 51-20-2 AND 51-30-5.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

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: POWER SUPPLY — 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 REMOVED AND REPLACED THE APPROPRIATE EMERGENCY BATTERY POWER SUPPLY 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: APU — LEAKING (APU BAY) · airframe 56,615 hrs · 37,784 cycles

SMOKE SMELL IN CABIN UTILIZING RIGHT PACK AND APU AIR SOURCE.

Part: CUSP WEB — DAMAGED (ZONE 100)

DURING THE MAINTENANCE CHECK FOR ACFT N403NV AT AAR TULSA MAINTENANCE BASE. THE LEFT CUSP SHOOT AT STA 807 LT WAS FOUND TO BE DAMAGED. THE DAMAGE CONSISTED OF A HOLE APPROX 1/2 INCH IN DIAMETER. A REPAIR DOUBLER WAS INSTALLED PER ESO 80559 AND AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (ZONE 100)

CORROSION ON CUSP AT STATION 876 RT SIDE BLENDED CORROSION OUT OF LIMITS. INSTALLED DOUBLER PER AARD 53-20-00-16 AND EO 80559 DATWED 9/8/09.

Part: SENSE LINE — BROKEN (OIL SYSTEM)

LEFT OIL QUANTITY SHOW EITHER --(DASHES) OR EN ROUTE. ALL OTHER INDICATIONS NORMAL. DURING DESCENT OIL PRESSURE DROPPED TO 32 PSI, IDLE - 25 PSI AT 1.4 EPR. RAN QRH AND SECURED LEFT ENGINE. MAINTENANCE DEPARTMENT PERSONNEL INSPECTION FOUND DIFFERENTIAL PRESSURE SWITCH LOW OIL PRESSURE SENSE LINE BROKEN AT PORT LP5. REMOVED AND REPLACED OIL PRESSURE DIFFERENTIAL SWITCH SENSE LINE IAW AMM 79-36-01, LEAK CHECK GOOD, NO DEFECTS NOTED, AIRCRAFT RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (MASTER BATTERY)

AIRCRAFT ARRIVED AT THE BLI GATE AND WAS BEING OBSERVED BY MAINTENANCE DEPARTMENT PERSONNEL. THEY NOTICED WHITE SMOKE AND YELLOW FLUID LEAKING FROM TWO PORTS BEHIND THE NOSE GEAR WELL AREA. ALL PASSENGER'S DISEMBARKED THE AIRCRAFT WITHOUT INCIDENT. INSPECTION OF THE EQUIPMENT BAY WAS PERFORMED AND BOTH MAIN BATTERIES AND THE BATTERY CHARGER AND IT WAS DETERMINED THAT THE CHARGER HAD FAILED AND OVERHEATED THE BATTERIES WHICH IN TURN BOILED OFF THE BATTERY WATER. ALL COMPONENTS WHERE REPLACED AND A SYSTEM OPERATIONAL CHECK PERFORMED WITH NORMAL OPERATION. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — SMOKE

FLT 552, FLIGHT DECK PERSONNEL OBSERVED VISIBLE SMOKE FROM THE OVERHEAD PANEL DURING TAXI. THE CREW RETURNED TO THE GATE AND MAINTENANCE DEPARTMENT PERSONNEL WERE NOTIFIED. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE OVERHEAD PANEL AND DETERMINED THE IGNITION ROTARY SWITCH WAS DEFECTIVE. REPLACING THE SWITCH AND PERFORMING A SYSTEM OPERATIONAL CHECK. SYSTEM CHECK WAS NORMAL AND THE ACFT WAS RETURNED TO SERVICE.