N412NV

Part: STIFFENER — CRACKED (LT NOSE COWL) · airframe 53,058 hrs · 26,288 cycles

LEFT NOSE COWL INNER BARRELL STIFFENER CRACKED AT THE 6 O-CLOCK POSITION. REPLACED STIFFENER IAW EA 40-2016-344.

Part: RADIO — FAILED (VHF COMM) · airframe 52,414 hrs · 26,164 cycles

DURING FREQUENCY SWITCHING NR 1 VHF RADIO STARTED POURING OUT SMOKE. R & R NR 1 VHF IAW AMM 23-20-02. OPS CHECK WAS GOOD.

Part: FUEL CAP — MISSING (FUEL SYSTEM) · airframe 51,180 hrs · 25,271 cycles

RAMPERS INFORMED FUELING PANEL WAS OPEN PULLING INTO GATE. FUEL CAP MISSING. EVIDENCE OF FUEL CAP BANGING AGAINST UNDERSIDE OF WING BEHIND FUEL PANEL BEFORE DEPARTING ACFT. DEFERRED RT WING FUEL CAP IAW MEL 28-17 SIT 1 CAT D AS AUTHORIZATION 19256 DATE DUE IS 12-18-2015. MX PROCEDURES COMPLIED WITH & PLACARDS INSTALLED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 51,044 hrs · 25,201 cycles

LOWER AFT EMER EXIT LIGHTS WILL NOT ILLUMINATE. R & R CTR BATTERY POWER SUPPLY AT ROW 25 DEF. SEE LP 542457.

Part: PROXIMITY SENSOR — FAULTY (LT MLG) · airframe 50,989 hrs · 25,171 cycles

INTERMITTENT GEAR DOOR OPEN LIGHT ON FINAL APPROACH. AFTER GO AROUND ALL INDICATIONS NORMAL. LIGHT CAME ON APPROX 1000 FT AGL, HYD PUMPS WERE ON & HIGH WITH 3000 PSI. ALL GEAR INDICATORS WERE GREEN. FOUND LT MLG DOOR OPEN PROX SENSOR AT FAULT. R & R LT MLG DOOR OPEN PROX SENSOR. OPERATIONS CHECKED GOOD IAW MM 32-60-05-2-0.

Part: GROUND STUD — LOOSE (CABIN)

EMERGENCY EXIT SIGN AT L1 DOOR INOPERATIVE. TROUBLE SHOT & FOUND GND STUD S281 LOOSE IN FRAME AT STATION 332R. SECURED GND STUD IAW SRM 51-30-01. EMER EXIT SIGN OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,705 hrs · 25,028 cycles

UPON REMOVAL OF WING TO BODY FAIRING N/P, DISCOVERED CORROSION ON EXTERNAL SKIN AROUND NUMEROUS N/P LOCATIONS. REPAIRED SKIN AT WING TO BODY FAIRING AREA IAW SRM 53-04 FIG 57. WORK ACCOMPLISHED ON WO 250305 M301 ITEM 719 WO 1011780 6000-0042.

Part: PAN — CORRODED (FUSELAGE) · airframe 50,705 hrs · 25,028 cycles

FORWARD CARGO DOOR LOWER DOOR JAMB PAN IS CORRODED. REMOVED LOWER JAMB PAN. FABRICATED & INSTALLED REPAIR PARTS & PAN IAW SRM 53-05 FIG 44A. WORK ACCOMPLISHED ON WO 1011780-1000-0025 M301 ITEM 052.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 50,705 hrs · 25,028 cycles

AFT CARGO COMPARTMENT RT AFT CARGO TRACK CORRODED. R & R CARGO TRACK IAW SRM 51-10-1-3-4. WORK ACCOMPLISHED ON WO 1011780-1000-0076 M301 ITEM 203.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 50,705 hrs · 25,028 cycles

RIGHT FWD ANGLE OF THE MLG JAMB CRACKED. REMOVED CRACKED CHANNEL, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-05 FIG 81. WORK ACCOMPLISHED ON WO 1011780-1700-0108 M301 ITEM 687.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,585 hrs · 24,975 cycles

AFT OVERHEAD EMER EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 49,850 hrs · 24,615 cycles

EMER LIGHT IN FLIGHT DECK DOES NOT TURN ON WHEN EMER LIGHTS SWITCH IS IN ON POSITION. R & R BATTERIES IAW AMM 33-53-01. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,845 hrs · 24,614 cycles

DURING COCKPIT PREFLIGHT CHECK, DISCOVERED COCKPIT EMER LIGHTS WOULD NOT ILLUMINATE DURING TEST. REPLACED FWD CABIN BATTERY PACK IAW AMM 33-50-00. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 49,828 hrs · 24,605 cycles

FLIGHT DECK EMER LIGHTS INOPERATIVE. INSTALLED NEW EMER LIGHT BATTERIES. OPERATIONS CHECKED OK MM33-53-00.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 49,823 hrs · 24,603 cycles

FLIGHT DECK EMER LIGHTS INOPERATIVE. INSTALLED NEW EMER LIGHT BATTERIES. OPERATIONS CHECKED OK MM33-53-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,762 hrs · 24,569 cycles

R1 & L1 EMER LIGHTS INOPERATIVE. REPLACED BATTERIES IN THE EXIT IDENT PACK IAW AMM 33-53-01. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 49,662 hrs · 24,523 cycles

EMERGENCY LIGHT IN OVERHEAD COCKPIT PANEL INOPERATIVE. REPLACED EMER LIGHT BATTERIES FOR OVERHEAD COCKPIT LIGHTS IAW MM 33-53-00. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 49,647 hrs · 24,516 cycles

FORWARD LOWER FLASHLIGHT INOPERATIVE. REPLACED FWD LOWER FLASHLIGHT. OPERATIONS CHECKED GOOD IAW AMM 25-60-00.

Part: FCU — LEAKING (APU) · airframe 49,515 hrs · 24,446 cycles

APU AIR SMELLS OF JET FUEL. FOUND FUEL LEAKING FROM APU FUEL CONTROL PUMP FILTER CAP. DEFERRED APU IAW MEL 49-01 SIT 1, DMI 11127. PLACARDS INSTALLED M ACTIONS COMPLIED WITH WITH PACS ON. RAN BOTH ENGS AT 70% N1 FOR 15 MINUTES IAW AMM 71-00-00. OUTGOING FLIGHT CREW REPORTED NO ODOR IN CABIN DURING RUN. THIS MEL 49-01-00 SIT 1 REMAINS OPEN. R & R FUEL CONTROL UNIT FOR APU IAW AMM 49-30-01. OPERATIONS CHECKED GOOD. LEAK CHECKED GOOD. DUE TO SUSPECTED FUEL INGESTION INTO PACKS DUCT IAW LP 541849 FOR AIR CONDITIONING SYS. THIS CLEARS MEL 49-01 SIT1 DMI 11129. PLACARDS REMOVED M PROCEDURES COMPLIED WITH.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,477 hrs · 24,424 cycles

OVERHEAD EMER LIGHTS AT ROW 29 & 34 INOPERATIVE. RELAMPED, OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: BATTERY — DISCHARGED (CABIN)

THE EMER LIGHT AT TOP OF OVERHEAD PANEL DOES NOT COME ON WITH EMER LIGHT SWITCH ON. REPLACED FWD BATTERY OPERATIONS CHECKED GOOD IAW 33-53-00.

Part: BATTERY PACK — DISCHARGED (CABIN)

AFT EMER EXIT ROW LIGHTS INOPERATIVE. REPLACED POWER SUPPLY BATTERY PACK & OPERATIONS CHECKED NORMAL IAW AMM 33-50-01.

Part: BATTERY — DISCHARGED (CABIN)

L1 & R1 DOOR EXIT IDENTIFIER SIGNS INOPERATIVE. LOCATED BATTERY PACK, REPLACED BATTERIES & CHARGED THE SAME. OPERATIONS CHECKED OK IAW MM 33-51-14. STATION 338 BATTERY PACK CHANGED, OPERATIONS CHECKED OK IAW MM 33-51-33.

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

EMERGENCY SLIDE LANYARD DISCONNECTED ON THE FWD R1 DOOR. CONNECTED SERVICE DOOR LANYARD IAW MM 25-62-00.

Part: FRAME — CORRODED (BS 1271)

AFT CARGO BAY FRAME BS 1271 CORRODED BETWEEN LONGERONS 29L AND 29R. CUT OUT DAMAGE AREA OF FRAME, FABRICATED FRAME SPLICES, REPAIR PARTS, LOCATED, DRILLED AND INSTALLED IAW SRM 53-03, FIG 2A.

Part: LONGERON — CRACKED (BS 490-518)

LONGERON 4L IS CRACKED BETWEEN BS 490 TO 518. CUTOUT DAMAGED AREA, NEW LONGERON SEGMENT, FABRICATED, LOCATED, DRILLED, REPAIR SPLICES, REPAIR PARTS, AND INSTALLED REPAIR IAW SRM 53-02, FIG 18.

Part: CUSP WEB — CORRODED (BS 598-617)

PASSENGER CABIN RT CUSP WEB CORRODED BETWEEN BS 598 TO 617. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-05.

Part: DOOR — DENTED (L1 PAX DOOR)

L1 PAX DOOR OTBD SKIN IS DENTED IN THE UPPER AFT CORNER. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 520-05, PAR 33.

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 THE BATTERY PACK AND OPS CHECKED GOOD IAW AMM 33-50-00. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R EMERGENCY EXIT LIGHT ASSY AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED 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, MX REPORTED A PORTION OF EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MX R & R APPROPRIATE BATTERIES IN THE POWER SUPPLY AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

Part: SKIN — DENTED (BS 1510)

FUSELAGE SKIN DAMAGED AT BS 1510 OTBD OR RT LOWER TAILCONE LATCH ASSY. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED.

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: UNKNOWN — ODOR (CABIN)

APPROACHING 19000FT ON CLIMB, F/A REPORTS STRONG SMOKE ODOR IN CABIN BUT NO SMOKE VISABLE. VERIFIED BY BOTH PILOTS. TURNING AUTO TEMP CONTROLLER COLDER STOPPED SMELL. SHIP RETURNED TO ORG BASE AND HIGH POWER END RUNS WITH PACKS ON - COULD NOT DUPLICATE.

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 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: DOOR FRAME — CORRODED (FUSELAGE)

AFT CARGO DOOR CUTOUT LOWER JAMB STA 1154 TO 1211 CORRODED. REPAIRED AFT CARGO DOOR CUTOUT LOWER BEAM STA 1154 TO 1211 IAW MD80 SRM 53-05 FIG 123 OPT 1.

Part: BULKHEAD — CRACKED (FUSELAGE)

FLIGHT COMPARTMENT LOWER VERTICAL BULKHEAD WED IS CRACKED AT RBL 8-63 AND LBL 3-3 AS FS 120. CUT OUT DAMAGED AREAS, FABRICATED REPAIR DOUBLERS, FILLERS AND INSTALLED IAW BOEING DWG #9911590 AND MD80 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 — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN POWER SUPPLY BATTERY PACK. AN OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, OPS CHECKED NORMAL. AIRCRAFT 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: 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 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: 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: FCU — FAULTY (APU)

AT THE GATE STARTED APU AND AFTER RIGHT PACK TURNED ON, FUEL FUMES CAME INTO CABIN AND FUEL DRIPPING UNDERNEATH APU. REMOVED AND REPLACED APU FCU AND SEQUENCE OIL PRESSURE SWITCH, WORK PERFORMED IAW AMM 49-30-01 AND 49-30-03. OPS AND LEAK CHECK GOOD.

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: SKIN — DENTED (LT WING)

LEFT WING HAS A DENT I/B END AREA WING STATION XCW75.0 AND 30 INCHES FWD OF TRAILING EDGE FIXED PANEL DENT IS .035 IN DEPTH AND 1.5 INCHES IN LENGTH AND 2.0 INCHES WIDE. REPAIRED LT WING LOWER SKIN IAW MD80 SRM 57-03 FIG 30.

Part: FLOORBEAM — CORRODED (FUSELAGE)

LEFT AFT LAV FLOORBEAM CORRODED STA 1322, LBL 27 TO RBL 27. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW MD80 SRM 53-05 FIG 79A AND SRM 51-10-4 PAGE 1 AND PARA 6, FIG 3A.

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFT CARGO PIT AREA CABIN FLOORBEAM IS CORRODED FS 1309, LBL 15 TO LBL 22. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW MD80 SRM 51-70-5 FIG 2.

Part: TAB — DAMAGED (AILERON)

RIGHT AILERON CONTROL TAB TRAILING EDGE COMPOSITE DAMAGED. REPAIRED DAMAGED AREA IAW MD80 SRM 51-70-1A PARA 11. BALANCED TAB TO -3.45 IN LBS NOSE HEAVY CONDITION IAW MD80 SRM 57-50-1.

Part: VANE — CHAFED (TE FLAP)

LT WING O/B FLAP VANE L/E EXISTING REPAIR CHAFED ABOVE NR 3 FLAP ACTUATOR. REPAIRED LT WING O/B FLAP VANE L/E ABOVE NR 3 FLAP ACTUATOR IAW MD 80 SRM 51-70-2 REPAIR 18.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

PASSENGER CABIN FLOOR SUPPORT AT LBL 15, STA 200 TO STA 256, CORRODED. REMOVED AND REPLACED FLOOR SUPPORT AT LBL 15, STA 200 TO STA 256 IAW SRM 51-30-2, FIG 20.

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.

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 BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.