N424NV
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
44 reports on file, 2012-03-21 – 2017-10-08.
Part: BEAM — CORRODED (BS 160-200) · corrosion level 2 · airframe 61,388 hrs · 51,873 cycles
FOUND THE DOOR FRAME BEAM TO BE CORRODED. REMOVED AND REPLACED THE BEAM IAW SRM 51-30-5.
Part: RIB — CRACKED (VERTICAL STAB) · airframe 61,388 hrs · 51,873 cycles
VERTICAL STAB LOWER L/E, THIRD RIB UP FROM BOTTOM, CRACKED AT LOWER ATTACH FASTENER LT SIDE. REMOVED AND REPLACED DAMAGED RIB IAW SRM 51-30-2, FIG 19-20, AND 51-30-5.
Part: RIB — CRACKED (VERTICAL STAB) · airframe 61,388 hrs · 51,873 cycles
VERTICAL STAB LOWER L/E FIFTH RIB UP FROM BOTTOM, CRACKED AT LOWER ATTACHED FASTENER, RT SIDE. REMOVED AND REPLACED DAMAGED THE RIB IAW 51-30-2, FIG 19-20, AND 51-30-5.
Part: RIB — CRACKED (VERTICAL STAB) · airframe 61,388 hrs · 51,873 cycles
VERTICAL STAB LOWER L/E, FOURTH RIB, UP FROM BOTTOM CRACKED AT LOWER ATTACHED FASTENER, RT SIDE. REPAIRED THE RIB IAW 55-02, FIG 27, SHEET 3 AND 4. INSTALLED IAW SRM 51-30-2, FIG 19-20, AND 51-30-5.
Part: SKIN — CORRODED (BS 237-256) · corrosion level 2 · airframe 61,388 hrs · 51,873 cycles
FUSELAGE SKIN CORRODED. REPAIRED THE SKIN IAW EA 42-2017-024.
Part: DOOR — CRACKED (LT WING) · airframe 61,388 hrs · 51,873 cycles
LEFT WING OTBD BUTTE DOOR, OTBD SIDE CRACKED. REMOVED AND REPLACED BUTTE DOOR IAW SRM 51-30-5, PARA 7.
Part: SKIN — CORRODED (LAV SERVICE DOOR) · corrosion level 2 · airframe 61,388 hrs · 51,873 cycles
FORWARD LAVATORY SERVICE DOOR EXTERNAL SKIN CORRODED BETWEEN SKIN AND INTERNAL DOUBLER. REPAIRED FWD LAV SERVICE DOOR FWD LOWER CORNER FUSELAGE CUTOUT IAW EA 25-2017-110.
Part: ANGLE — DAMAGED (BS 1154) · airframe 61,388 hrs · 51,873 cycles
AFT CARGO ANGLE CRACKED OR HAS DEEP GOUGE BS 1154, STRINGER 21R. REMOVED AND REPLACED THE ANGLE IAW SRM 51-30-5.
Part: STIFFENER — CRACKED (BS 1418) · airframe 61,388 hrs · 51,873 cycles
AFT FUSELAGE FRAME CRACKED ON AFT SIDE OF FRAME INNER LIP AROUND FASTENER. REMOVED AND REPLACED EXISTING CRACKED REPAIR STIFFENER IAW MD80 SRM 51-30-5.
Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 61,388 hrs · 51,873 cycles
LT WING TRAILING EDGE OUT BOARD BUTE DOOR ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED LT WING TRAILING EDGE OUT BOARD BUTE DOOR ATTACH BRACKET IAW SRM 51-30-5 PG 12 STEP 7 AND 51-30-2 PG 26B STEP 8.
Part: SKIN — CRACKED (BS 200-218) · airframe 61,388 hrs · 51,873 cycles
CRACK FOUND IN THE SKIN AND DOUBLER AT LOWER AFT CORNER OF AIRSTAIR DOOR.
Earlier reports · 2012–2016 · 33 reports
2016
Part: ACTUATOR — INOPERATIVE (OUTFLOW VALVE) · airframe 58,714 hrs · 50,518 cycles
IN CRUISE, TRANSFER LOCKOUT, LIGHT ILLUMINATED. QRH 21.10 COMPLIED & LIGHT REMAINED ILLUMINATED. TROUBLE SHOT & TESTED SYS IAW AMM 21-32-00. BIT CHECK OF NR 1 CONTROLLER SHOWS ACTUATOR FAULT. R & R CABIN OUTFLOW VLV ACTUATOR ASSEMBLY IAW AMM 21-32-05. OPERATIONS CHECKED GOOD.
Part: SPAR CAP — CRACKED (LT WING) · corrosion level 2 · airframe 58,714 hrs · 50,518 cycles
LEFT WING FWD SPAR LOWER CAP, UPPER SURFACE FWD FLANGE CORRODED AT STATION XFS 570. DURING THE REPAIR, A .200" CRACK WAS NOTED, BETWEEN TWO FASTENER HOLES. DAMAGE WAS REPAIRED IAW STS EA 30-2016-093 DATED 03 26 16.
Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 58,714 hrs · 50,518 cycles
FLOOR PANEL AT R1 DOOR GIRT BAR FLOOR LATCHES CORRODED OUT OF SRM 53-01 LIMITS. REPLACED FLOOR PANEL WITH SERVICEABLE PART IAW SRM 51-10-4.
Part: SPAR CAP — CRACKED (LT WING) · airframe 58,714 hrs · 50,518 cycles
LEFT WING FWD SPAR, LOWER CAP UPPER SURFACE, FWD FLANGE CORRODED AT STATION XFS 570. DURING REPAIR, A .200"" CRACK WAS NOTED, BETWEEN TWO FASTENER HOLES. DAMAGE WAS REPAIRED IAW EA 30-2016-093 DATED 03 26 16.
2015
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,236 hrs · 50,290 cycles
EMERGENCY EXIT LAMP INOPERATIVE AT ROW 26. REPLACED THE LAMP IAW AMM 33-53-00, OPS CHECKED GOOD.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 58,209 hrs · 50,278 cycles
AFTER LANDING, SMOKE ALARM FOR AFT RT LAV WENT OFF, F/A REPORTS NO EVIDENCE OF SMOKE OR FIRE. PLACED AFT RT LAV SMOKE DETECTOR ON MEL 26-07 S1, AUTHORIZATION NR 21374, EXPIRES 12/6/15, CAT C. MAINTENANCE ACTION COMPLETED, PLACARD INSTALLED."
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 57,572 hrs · 49,939 cycles
TAIL COMPARTMENT HIGH LIGHT ON OAP AT ROTATION QRH 21.4. LIGHT EXTINGUISHED AFTER 60 SEC. REF WO 00260196-1 & 0020196-2. COMPLIED WITH TC 21-059-010 & TC 21-059-005.
Part: BATTERY — DISCHARGED (CABIN) · airframe 57,566 hrs · 49,937 cycles
FOUND ON WAKE UP, FWD CABIN EMER LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.
Part: A/C PACK — ODOR (AC BAY) · airframe 57,499 hrs · 49,895 cycles
FLIGHT ATTENDANT'S REPORTED A STRONG PLASTIC BURNING SMELL SHORTLY AFTER TAKEOFF. VERIFIED ODOR COMING FROM LT PACK DURING POWER RUNS. DEFERRED LT PACK IAW MEL 21-01, CAT C, EXPIRES 6 15 15, PLACARD INSTALLED.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
FORWARD WING EMER EXIT LIGHTS INOPERATIVE. R & R EMER EXIT LT POWER SUPPLY IAW 33-53-01. FWD WING EMER EXIT LTS CHECKED GOOD.
Part: LIGHT — BROKEN (AC BAY)
TAIL COMPARTMENT RT AFT EMER EXIT LIGHT INOPERATIVE & ASSEMBLY BROKEN. R & R RT AFT TAIL COMPARTMENT E & E LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL IAW AMM 33-53-00.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,041 hrs · 49,649 cycles
RIGHT EXTERIOR EMER EXIT LIGHT INOPERATIVE. REPLACED RT OVERWING EMER EXIT LIGHT ASSEMBLY IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.
Part: FLAP — CRACKED (LT WING) · airframe 56,990 hrs · 49,621 cycles
LEFT OTBD FLAP TE CRACKED. REPAIRED DAMAGED SECTION OF LT OTBD FLAP TE IAW SRM 57-03.
2014
Part: PROXIMITY SENSOR — FAULTY (RT MLG) · airframe 56,473 hrs · 49,356 cycles
GEAR RETRACTION ON TAKEOFF RT GEAR INDICATION REMAINED RED WITH GEAR HANDLE UP. RAN QRH 32.9, HYD PRESS & QTY NORMAL. R & R RT MLG UPLOCK & DOWNLOCK PROXIMITY SENSORS IAW AMM 32-60-05. PERFORMED PSEU CHECKS ON REPLACED SENSORS WITH GO & NO GO GAUGE & BITE. PERFORMED GEAR SWING IAW AMM 32-32-00. ALL INDICATORS OPERATE NORMALLY AT THIS TIME.
Part: APU — LEAKING (APU BAY) · airframe 56,424 hrs · 49,331 cycles
IMMEDIATELY AFTER TAKEOFF ALL FLIGHT ATTENDANT`S & FIRST OFFICER`S SMELLED A STRONG CHEMICAL ODOR, SMELL DISSIPATED OVER 10 MINUTES. QRH 26.5 REFERENCED. PACKS ON TAKEOFF IAW WORK ORDER 00233607 NR 1, TASK CARD F0592102 & TASK CARD S0592101, APU LEAK IDENTIFIED ON LP 541445 & DEFERRED. PACK BURNOUT INCLUDED ON WORK ORDER & TASK CARD S0592101, NO ORDERS DETECTED AT THIS TIME.
Part: BATTERY — DISCHARGED (CABIN)
FWD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY BATTERIES AT FWD GALLEY POSITION IAW 33-53-00, OPERATIONS CHECKED GOOD.
2013
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R BATTERY PACK AND OPS CHECKED IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.
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 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 SYS WOULD NOT TEST. MX R & R POWER SUPPLY BATTERY PACK AND OPS CHECKED IAW AMM 33-50-00, SYSTEM OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R BATTERY PACKS 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 THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MX R & R 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: 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 — INOPERATIVE (EMERGENCY LIGHTS)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE REPORTED A PORTION OF THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED BATTERY PACK IN POWER SUPPLY. OPS CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.
Part: DRAG ANGLE — CRACKED (FUSELAGE)
LEFT CANTED BULKHEAD 1463 DRAG ANGLE CRACKED IN EXISTING DOUBLER. REMOVED AND REPLACED DRAG ANGLE AT 181.
Part: DRAG ANGLE — CRACKED (FUSELAGE)
RIGHT CANTED BULKHEAD 1463 DRAG ANGLE CRACKED. REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE AND INSTALLED.
Part: BULKHEAD — CRACKED (FUSELAGE)
RIGHT CANTED BULKHEAD 1463 AS 2 EACH CRACKS AT LONGERON 17R AND 18R. STOP DRILLED CRACKS, FABRICATED REPAIR DOUBLERS AND SHIMS.
2012
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: 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: 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 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.