N427NV
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.
32 reports on file, 2012-04-22 – 2016-09-02.
Part: DOOR FRAME — GOUGED (FUSELAGE) · airframe 58,613 hrs · 43,932 cycles
FORWARD CARGO DOOR JAMB PAN HAS A GOUGE FORWARD OF THE LOWER AFT CORNER. REPAIRED FORWARD CARGO DOOR JAMB PAN IAW SRM 53-05, FIG 44A.
Part: PAN — CRACKED (BS 905) · airframe 58,613 hrs · 43,932 cycles
RH CABIN WINDOW RING PAN BETWEEN OVER WING EXITS IS CRACKED AT LOWER AFT FASTNER. REPAIRED RH CABIN WINDOW RING PAN IAW MD80 SRM 53-05 FIG 122.
Part: PAN — CRACKED (WINDOW) · airframe 58,613 hrs · 43,932 cycles
LEFT CABIN WINDOW RING PAN IS CRACKED A UPPER FWD FASTNER. REPAIRED LEFT CABIN WINDOW RING PAN IAW SRM 53-05 FIG 122.
Part: PAN — CRACKED (BS 886) · airframe 58,613 hrs · 43,932 cycles
LH CABIN WINDOW RING PAN BETWEEN OVER WING EXITS IS CRACKED AT UPPER FWD FASTNER. REPAIRED LH CABIN WINDOW RING PAN IAW MD80 SRM 53-05 FIG 122.
Part: CHANNEL — CRACKED (FUSELAGE) · airframe 58,613 hrs · 43,932 cycles
MID CARGO CEILING PANEL ATTACH RAIL CRACKED. REPAIRED MID CARGO CEILING ATTACH CHANNEL IAW SRM 53-01, FIG 2.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 58,613 hrs · 43,932 cycles
FLOOR SUPPORT FITTING CRACKED. R & R FLOOR SUPPORT FITTING IAW SRM 51-30-5, PARA 7 AND 8.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,613 hrs · 43,932 cycles
FLOORBOARD SUPPORT INTERCOSTAL CRACKED. R & R INTERCOSTAL IAW SRM 51-30-2.
Part: FLOOR SUPPORT — CRACKED (BS 788) · airframe 58,613 hrs · 43,932 cycles
FLOOR SUPPORT CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-30-5 PAR 7 AND 8.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,613 hrs · 43,932 cycles
FLOOR SUPPORT INTERCOSTAL CRACKED. R & R INTERCOSTAL IAW SRM 51-30-2 PAR 1, 51-30-5, PAR 1.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 58,045 hrs · 43,622 cycles
RIGHT AFTER 80 KNOTS, STABILIZER TAKEOFF WARNING SOUNDED & TAKEOFF WAS REJECTED. PERFORMED ACFT DISCREPANCY HISTORY CHECK BACK TO 04 01 2016, NO ASSOCIATED DISCREPANCIES FOUND. SEE LOG PAGES 667872 & 667873 FOR ADDITIONAL MX PERFORMED. ACFT RETURNED TO SERVICE. PERFORMED HI ENERGY STOP CHECK IAW AMM 05-57-00, DFDR DOWNLOAD REF TC 31-057-001 & TAKEOFF WARNING SWITCH CHECK IAW AMM 27-40-00 SECT L. NO DEFECTS NOTED AT THIS TIME.
Earlier reports · 2012–2015 · 22 reports
2015
Part: DADC — FAULTY (NR 2) · airframe 57,346 hrs · 43,273 cycles
DURING CLIMB, BOTH CADC 1 & 2 FAILED. THERE WAS AT LEAST A 500' DISCREPANCY, BETWEEN CAPTAIN & FIRST OFFICERS ALTIMETERS WITH CAPTAINS SHOWING THE HIGHER ALTITUDE. THE BACKUP ALTIMETER WAS ABOUT THE SAME AS CAPTAINS ALTIMETER. LOST BOTH FLIGHT DIRECTORS, AUTO THROTTLES, AUTOPILOT & ALTITUDE PRESELECT. THE ALTIMETERS MATCHED UP AFTER LEVEL OFF AT 28000'. ALSO FIRST OFFICERS VSI WAS UNRELIABLE. TROUBLE SHOT FOUND STATIC LINE TO NR 2 DADC UNSECURED. R & R NR 2 DADC IAW AMM 34-16-01. OPERATIONS CHECKED GOOD. NR 1 & 2 DFGC RTS GO IAW AMM 22-01-05. NO FURTHER ACTION REQUIRED. NR 1 DADC OPERATIONS CHECKED GOOD IAW AMM 34-16-01. NR 1 DADC WAS NOTED TO BE SELECTED TO BOTH SIDES ON NR 1 WHEN ACFT ARRIVED.
Part: SPOILER — OUT OF ADJUST (WING) · airframe 57,346 hrs · 43,273 cycles
AIRCRAFT ROLLS TO THE RT DURING FLIGHT SPOILER DEPLOYMENT. REF LOG PAGE 602447, ANGLE DEFLECTION CHECK FOUND OTBD FLIGHT SPOILER MISMATCH, SPOILERS ADJUSTED IAW AMM 27-60-00 TO SERVICE SPEC OF SPOILER SPEED BRAKE CONTROL TEST. TEST E
Part: SMOKE DETECTOR — FALSE ACTIVATION · airframe 57,259 hrs · 43,228 cycles
LEFT AFT & LEFT FWD, LAVATORY SMOKE DETECTORS FALSE ALARM. DEFERRED IAW MEL 2607 S1 CAT C. M PROCEDURE COMPLIED WITH & PLACARD INSTALLED.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,003 hrs · 43,090 cycles
TAIL COMPARTMENT, EMERGENCY LIGHTS INOPERATIVE. R & R TAIL COMPARTMENT EMERGENCY LIGHTS BATTERY. PERFORMED OPERATIONS CHECK. OPERATIONS CHECKED GOOD IAW 33-53-00.
Part: LIGHT — INOPERATIVE (AC BAY)
TWO EMER LIGHTS IN TAIL COMPARTMENT INOPERATIVE. RELAMPED EMER LIGHTS IN TAIL COMPARTMENT & REPLACED BATTERIES IAW AMM 33-53-00. OPERATIONS CHECKED GOOD AT THIS TIME.
Part: BATTERY — DISCHARGED (CABIN)
CENTRAL STAIR WAY EMER LIGHTING INOPERATIVE. R & R EMER BATTERY IAW 33-53-00. OPERATIONS CHECKED GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,712 hrs · 42,916 cycles
FORWARD EMER EXIT LIGHTS INOPERATIVE. R & R FWD EMER EXIT LIGHT BATTERY PACK IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.
Part: BATTERY — DISCHARGED (CABIN) · airframe 56,588 hrs · 42,848 cycles
TAIL COMPARTMENT EMER LIGHTS INOPERATIVE. REPLACED EMER LIGHTS BATTERIES IAW AMM 33-53-00.
Part: BATTERY — DISCHARGED (CABIN) · airframe 56,543 hrs · 42,823 cycles
FORWARD EMER EXIT LIGHTS INOPERATIVE. R & R FWD EMER EXIT LIGHT BATTERIES IAW AMM 33-53-01-4.
Part: ATTACH FITTING — CRACKED (LT WING) · airframe 56,257 hrs · 42,682 cycles
LEFT WING FIXED LE RIB ATTACH CLIP STATION XRS 111.5 CRACKED. REMOVED, FABRICATED & REPLACEMENT CLIP IAW SRM 57-01FIG 3.
2014
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 55,901 hrs · 42,508 cycles
FOUND AFT TAIL COMPARTMENT EMER LIGHTS INOPERATIVE. R & R EMER LIGHTS POWER SUPPLY IAW AMM 33-53-00. LIGHTS OPERATIONS NORMAL.
Part: ANTI-ICE VALVE — INOPERATIVE (RT ENGINE) · airframe 55,398 hrs · 42,270 cycles
DURING CLIMB OUT TURNED ENG ANTI-ICE ON & THE RT ENG VLV INDICATION ILLUMINATED ON THE OAP. RAN QRH, NO HELP, DIVERTED. R & R NOSE COWL ANTI-ICE VLV & OTBD ANTI-ICE VLV IAW AMM 75-10-01. NO LEAKS NOTED AT THIS TIME. OPERATIONS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (CABIN)
OVERHEAD EMER LIGHT AT ROW 26 INOPERATIVE. RE-LAMPED OVERHEAD CEILING EMER LIGHT IAW MM 33-53-00. OPERATIONS CHECKED GOOD.
Part: BATTERY — DISCHARGED (CABIN)
FOUND ON WAKE UP. EMER LIGHTS AT AFT FLIGHT ATTENDANT STATION & TUNNEL SIDEWALLS INOPERATIVE. REPLACED BATTERIES. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.
2013
Part: CONTROLLER — INOPERATIVE (CABIN TEMP)
AFTER TAKEOFF ON CLIMBOUT RT PACK WENT FULL HOT WITH SMELL OF SMOKE. ALL 3 SMOKE DETECTORS ACTIVATED. QRH 26.9 AND FOLLOWED PROCEDURE. ALSO PERFORMED QRH 21.9 TEMPERATURE AUTO CONTROL FAILURE. SMELL AND SMOKE STOPPED AFTER RT PACK SHUTOFF. DIVERTED IAW MX CONTROL AND DISPATCH BT 1737Z. INSPECTED IAW WC F0592102, FOUND DUCT CLAMP AT LT PACK HEAT EXCHANGER FAN DISCONNECTED, RESECURED CLAMP. IAW 21-51-01. INSPECTED DUCTING AT COLESER BAGS NO OIL FOUND. RUN BOTH PACKS, FOUND AUTO TEMP CONTROL ON RIGHT PACK INOPERATIVE. VERIFIED RT PACK OPERATES OK IN MAN MODE. PLACED CONTROLLER ON MEL 21-30 SITA 1 CAT "C", EXPIRES 11-25-13, DMI 5308, "M" PROCEDURE C/W, PLACARD INSTALLED.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MX R & R BATTERY PACK IN POWER SUPPLY AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK 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 INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R THE APPROPRIATE BATTERY PACKS IN POWER SUPPLY AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. THE ACFT 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: SLIDE — UNSERVICEABLE (TAIL CONE)
SLIDE PACK ON TAIL CONE INDICATES IN RED. REMOVED AND REPLACED TAIL CONE EVAC SLIDE IAW TASK CARD R0902503 REF 25-62-01.
Part: EYEBOLT — DETACHED (ELEVATOR)
AFTER TAKEOFF ELEVATOR HAD VIBRATION AND ABNORMALLY DIFFICULT TO MOVE. TAKEOFF TRIM 8.0 AFTER TAKEOFF TRIMMED TO 0. LANDED WITH 3.0. FOUND RT ELEVATOR EYEBOLT ON ACTUATOR DETACHED FROM ELEVATOR. INSTALLED EYEBOLT PER AMM 27-30-08. ACP SYSTEM TEST. ALL NORMAL. ALSO COMPLIED WITH EO 2730-01 MD80 ELEVATOR POWER CONTROL ACTUATING CYLINDER ROD END INSPECTION/RESTORATION.
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.
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.