N415NV

Part: SEAT TRACK — GOUGED (BS 816-916) · airframe 54,131 hrs · 37,371 cycles

SEAT TRACK GOUGED. REMOVED DAMAGED SECTION OF SEAT TRACK AND SPLICED IN REPLACEMENT SECTION IAW SRM 53-05 FIG 4.

Part: FLOOR SUPPORT — CRACKED (BS 786-807) · airframe 54,131 hrs · 37,371 cycles

CENTER FLOOR SUPPORT CRACKED IN MULTIPLE PLACES. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-30-2 AND 51-30-5.

Part: FLOOR SUPPORT — CRACKED (BS 1287-1309) · airframe 54,131 hrs · 37,371 cycles

FLOOR SUPPORT BETWEEN CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-30-02, 51-10-4.

Part: FLOOR SUPPORT — CRACKED (BS 712) · airframe 54,131 hrs · 37,371 cycles

CENTER FLOOR SUPPORT CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-30-5.

Part: ATTACH ANGLE — CRACKED (BS 598) · airframe 54,131 hrs · 37,371 cycles

FLOOR SUPPORT ATTACH ANGLE CRACKED. REMOVED AND REPLACED FLOOR SUPPORT ATTACH ANGLE IAW SRM 51-30-2 AND 51-30-5 FIG 2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,244 hrs · 36,343 cycles

TAIL CONE L2 DOOR EMERGENCY EXIT LIGHT INOP. / OP TESTED LIGHT CHECK GOOD ,INSTALLED NEW BATTERY PACK,FOUND EMERGENCY STILL TO BE INOPERATIVE.

Part: UNKNOWN — ODOR (CABIN) · airframe 52,070 hrs · 36,254 cycles

LEAD FLIGHT ATTENDANTS REPORTS ELEC SMELL IN CABIN. PERFORMED TYPE 3 BURNING ELEC MD80 CABIN ODOR & SMOKE TROUBLESHOOTING TC 21-059-002, NO DISCREPANCIES NOTED. ACFT OK FOR CONTINUED SERVICE.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 51,878 hrs · 36,145 cycles

SMOKE SMELL IN CABIN AROUND OVERWING EXIT, ALL CREW MEMBERS CONFIRMED. PERFORMED CABIN SMOKE TROUBLESHOOTING IAW CARD 21-059-002, NO DEFECTS FOUND. REPLACED COALESCE BAGS & PERFORMED PACK BURN IAW CARD 21-059-008. ACFT OK FOR SERVICE.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 51,569 hrs · 35,990 cycles

CABIN FLOOR RT CUSP WEB CRACKED STATION 1287 TO 1309. CUT OUT DAMAGED AREA ON CUSP WEB, FABRICATED RING DOUBLERS IAW SRM 53-05 FIG 131A-1. REPLACEMENT CUSP WEB INSTALLED IAW SRM 51-30-2 & 51-30--5. WORK ACCOMPLISHED ON WO 251791 M301 ITEM 312 & WO 1011838-0000-0019.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,319 hrs · 35,865 cycles

LEFT MAIN GEAR DOOR AFT JAM HAS CRACK OUT OF LIMITS. STOP DRILLED CRACK & INSTALLED REPAIR FITTING IAW SRM 53-05 FIG 141. THIS IS A PERMANENT REPAIR & ONLY REQUIRES NORMAL VISUAL MX.

Part: PROXIMITY SENSOR — FAULTY (NLG) · airframe 51,271 hrs · 35,841 cycles

NOSE GEAR UNSAFE ONLY ON APPROACH. NOSE GEAR LIGHT FLICKERED RED WITH AURAL WARNING INTERMITTENTLY. RAN QRH CHECKLIST, NOSE GEAR PIN EXTENDED. R & R NLG LOCK SENSOR. INSTALLATION & OPERATIONS CHECKED NORMAL IAW MM 32-60-05.

Part: LOCK SENSOR — FAULTY (NLG) · airframe 51,271 hrs · 35,841 cycles

NOSE GEAR UNSAFE ONLY ON APPROACH. NOSE GEAR LIGHT FLICKERED RED WITH AURAL WARNING INTERMITTENTLY. RAN QRH CHECKLIST NOSE GEAR PIN EXTENDED. R & R NLG LOCK SENSOR. INSTALLATION & OPERATIONS CHECKED NORMAL IAW MM 32-60-05.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,006 hrs · 35,705 cycles

TAIL COMPARTMENT SIDEWALL EMER LIGHTS INOPERATIVE. REPLACED BATTERIES IAW AMM 33-53-01. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

TAIL COMPARTMENT SIDEWALL EMER LIGHTS INOPERATIVE. REPLACED BATTERIES IAW AMM 33-53-01. OPERATIONS CHECKED GOOD.

Part: BATTERY — LOW (E&E BAY) · airframe 50,972 hrs · 35,685 cycles

EMERGENCY POWER INOPERATIVE, WILL NOT TEST. R & R MAIN SHIP BATTERIES IAW AMM 24-30-01. OPERATIONS CHECKED NORMAL. EMER POWER TEST GOOD IAW AMM 24-23-02.

Part: UNKNOWN — MALFUNCTIONED (FLIGHT CONTROL) · airframe 50,796 hrs · 35,608 cycles

ON APPROACH WITH FLAPS 40 CONFIGURED FOR LANDING AT 134 KTS WING DOWN TRIM REQUIRED 4 UNIT OF RT TRIM & ACFT STILL ROLLED TO LT WING DOWN. PERFORMED GVI OF AILERON & SPOILER SYSTEMS, NO DEFECTS NOTED. PERFORMED AILERON CHECK IAW AMM 27-10-00. SYS OPERATIONS CHECKED NORMAL ON GND. LUBRICATED SPOILERS & AILERONS IAW AMM 12-21-02.

Part: OIL SYSTEM — LEAKING (RT ENGINE) · airframe 50,405 hrs · 35,410 cycles

ON CLIMB OUT FIRST OFFICER NOTICED OIL QTY WAS A 7, AT GATE WE HAD 12 QUARTS BEFORE START UP. QRH 12.16 WAS RUN. AFTER OIL QTY WAS AT ZERO & ENG NR 2, RT ENG, WAS AT IDLE, OIL PRESS DROPPED BELOW 35 & ENG 2 WAS SHUTDOWN. EMER DECLARED & RETURNED. NR 2 ENG WAS WIND MILLING FOR APPROX 20 MINUTES WITHOUT OIL, IE OIL QTY WAS AT ZERO. FIRST OFFICER NOTICED OIL PRESS WAS AT ZERO FOR AT LEAST 10 MINUTES ON DESCENT BACK & PROBABLY MORE LIKE 15 MINUTES. CORRECTIVE ACTION TO BE ADDED WHEN AVAILABLE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 50,284 hrs · 35,343 cycles

RIGHT OIL PRESS DROPPING TO ZERO, FOLLOWED BY ZERO OIL QTY. ENG WAS SHUTDOWN WITHIN 30 SECONDS. NORMAL LANDING. R & R NR 2 ENG IAW TASK CARD R0807101. OPERATIONS & LEAK CHECKED GOOD.

Part: TRANSFORMER — FAULTY (COCKPIT)

LEFT OIL PRESS, HYD PRESS, HYD QTY & FLAP IND DISPLAYED DASHES CB K9 LT INSTRUMENT TRANSFER POPPED. CALLED MX CONTROL & INSTRUCTED DO NOT RESET. DID AIR RETURN IAW DISPATCH. REPLACED LT INSTRUMENT TRANSFORMER. OPERATIONS CHECKED GOOD IAW AMM 24-00-00 & 77-42-00. 8/5/14 COULD NOT DUPLICATE BUT REPLACED LT INSTRUMENT TRANSFORMER T1-19 THAT CONTROLS ALL OF THOSE SYSTEMS. NO REPEATS.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT INOPERATIVE AT 24DEF. RELAMPED IAW AMM 33-50-00. OPERATIONS CHECKED GOOD.

Part: BALLAST — DEFECTIVE (CABIN)

ON TAXI OUT FAS CALLED THE FLIGHT DECK REPORTING SMOKE IN THE CABIN COMING FROM THE OVERHEAD BINS. THE SMOKE COULD NOT BE CONTROLLED & THE ACFT WAS EVACUATED. STRONG SMELL, CHEMICAL SMELL, COMING FROM ROWS 15 - 20. BALLAST AT 19L & 20L INOPERATIVE & SMELLS. R & R BURNED BALLAST AT 19A-C & INOPERATIVE BALLAST AT 20AC. OPERATIONS CHECKED GOOD IAW AMM 33-21-03.

Part: SKIN — DENTED (FUSELAGE)

FUSELAGE SKIN DENTED AT STATION 236 BETWEEN LONGERON 17L & 18L. REMOVED DAMAGE, FABRICATED & INSTALLED SKIN & DOUBLER IAW SRM 53-04 FIG 12C. WORK ACCOMPLISHED ON WO 1010863-2000-0001.

Part: APU — FAULTED

BOTH AFT LAV SMOKE DETECTORS WENT OFF DURING TAXI OUT. VISIBLE SMOKE IN AFT CABIN. EMERGENCY EVACUATION OCCURRED. R & R APU IAW TC R0594902. LEAK AND OPS CHECKED GOOD.

Part: SLIDE — SPLIT (L1 DOOR)

L1 DOOR SLIDE DEPLOYED, FAILED TO INFLATE, SEAM FOUND SPLIT. REPLACED L1 DOOR SLIDE IAW CARD R0902502.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R BATTERY PACK AND OPS CHECKED GOOD IAW AMM 33-50-00. ACFT 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: 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 REMOVED AND REPLACED THE APPROPRIATE EMERGENCY FLOOR PATH ILLUMINISCENT LIGHT ASSY 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: SKIN — DAMAGED (RUDDER)

RUDDER LOWER RT AREA OF HINGE CUT OUT SMALL AREA OF EDGE DAMAGE. REPAIRED COMPOSITE DEFECTS IAW SRM 51-70-1A.

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)

IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE 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: 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 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.