N903NV
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.
18 reports on file, 2013-02-05 – 2016-08-07.
Part: MONITOR — FAILED (LT ENGINE) · airframe 74,433 hrs · 26,096 cycles
EMERGENCY DECLARED, LT ENGINE VIB 2.6 WITH CLB, Z-POWER, ALTITUDE 17,000, EST, PERFORMED QRH ENGINE VIBRATION, 72.18, RETARDING THRUST. RETURNED VIBRATION TO NORMAL LEVEL, HOWEVER VIBRATION APPEARED TO SLOWLY INCREASE AS FLT PROGRESSED WITH CRUISE POWER. AT LOW POWER SETTING ENGINE WAS WELL WITHIN LIMITS. REPLACED LT ENGINE VIBRATION MONITOR UNIT. BITE CHECKED GOOD REF MM 77-31-00, LOG PAGE 642889 FOR OPS CHECK.
Part: PANEL — CRACKED (FAIRING) · airframe 73,973 hrs · 25,972 cycles
FAIRING PANEL 197NL, THE PANEL IS CRACKED & HAS THE OUTER SKIN PENETRATED, BETWEEN FS 1240 - 1300 AT STRINGER 28R. THE DAMAGED AREA MEASURES 12 INCHES LONG BY 3 INCHES WIDE. REPAIRED BODY FAIRING 197N IAW SRM 53-00-70 REPAIR 1 & ERO 536-006 REV ORIG.
Part: SKIN — GOUGED (FUSELAGE) · airframe 73,973 hrs · 25,972 cycles
2ND FUSELAGE SKIN GOUGE DAMAGE. THE GOUGE STARTS AT STRINGER 28R TO 5 INCHES FROM STRINGER 26R. THE GOUGE DAMAGE MEASURES 8 INCHES LONG BY 0.50 INCHES WIDE WITH DAMAGE DEPTHS RANGING FROM 0.002 INCHES TO A MAX DEPTH OF 0.007 INCHES. REWORKED & BLENDED FS SKIN AT 1200 - 1300, BETWEEN STRINGERS 28L & 26R IAW EA 25-2016-139.
Part: SKIN — GOUGED (FUSELAGE) · airframe 73,973 hrs · 25,972 cycles
1ST FUSELAGE SKIN GOUGE DAMAGE. THE GOUGE STARTS 3 INCHES OTBD OF STRINGER 27L TO 1 INCH OTBD OF STRINGER 27R, ALONG THE LOWER SECTION OF THE FUSELAGE. THE GOUGE DAMAGE MEASURES 20 INCHES LONG BY 0.125 INCHES WIDE WITH DAMAGE DEPTHS RANGING FROM 0.001 INCH TO A MAX DEPTH OF 0.024 INCHES. THERE ARE TWO DENTS ALONG THIS GOUGE WITH THE FIRST DENT MEASURING 2 INCHES BY 1.75 INCH WITH A MAX DEPTH 0.043 INCHES. THE SECOND DENT MEASURES 1.38 INCH BY 2.25 INCH WITH A MAX DEPTH OF 0.043 INCHES. REWORKED & BLENDED FS SKIN AT 1200 - 1300, BETWEEN STRINGERS 28L & 26R IAW EA 25-2016-139.
Earlier reports · 2013–2015 · 14 reports
2015
Part: SLIDE — MISINSTALLED (CABIN) · airframe 73,044 hrs · 25,685 cycles
L1, R1, L2, R2, L4, R4 DOOR SLIDES PACK, INCORRECTLY INSTALLED. REMOVED & CHANGED LOCATION OF SURVIVAL KIT ATTACH STRAPS TO CORRECT POSITION IAW AMM 25-66-01. OPERATIONS CHECKED GOOD. REMOVED BUSTLE & CORRECTLY PLACED SURVIVAL KIT STRAPS IAW AMM 25-66-01. OPERATIONS CHECKED GOOD. PLACED D RING ON SLIDE BUSTLE AS REQUIRED IAW AMM 25-66-01, OK FOR SERVICE.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 73,030 hrs · 25,677 cycles
HIGH SPEED ABORT AT 110-120, DUE TO RT ENG EGT CAUTION 79, LT N3 CAUTION 9. DUE TO HIGH SPEED ABORT FUSE PLUGS BLEW ON ALL LT TIRES 1, 2, 3 & 4 RT TIRES INBD. NOTED BY MX IAW FIM FAULT TREE 71-05 819. NO FURTHER INSPECTION REQUIRED. REF LOG PAGE 602001, 602002. NR 1 - 8 MLG TIRES R & R IAW AMM 32-45-01. NR 5 - 8 TIRES R & R IAW AMM 32-45-01. NR 1 - 4 MAIN TIRES R & R IAW AMM 32-45-01.
Part: DOOR — BROKEN (CABIN)
EMERGENCY EQUIPMENT DOOR AT LT OVERWING EXIT BROKEN & SHEARED CASE. REPAIRED EMER EQUIPMENT DOOR CRACK IAW CMM 25-00-66.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,493 hrs · 25,509 cycles
EMERGENCY LIGHTS UNARMED LIGHT, 1/2 LIGHT INOPERATIVE. R & R EMER LIGHTS, PAX OXYGEN CONTROL PANEL IAW AMM 33-51-08. OPERATIONS CHECKED GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,211 hrs · 25,440 cycles
L4 DOOR, EMER EXIT, SIGN INOPERATIVE. R & R L4 DOOR SIGN BATTERY PACK IAW AMM 33-21-01 & 33-51-07. OPERATIONS CHECKED GOOD.
2014
Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 71,880 hrs · 25,349 cycles
DOOR 1R GIRT BAR EMER LIGHT OFF WITH EVACUATION SLIDE ARMING LEVER IN ARMED. ENGAGE POSITION RELAMPED R1 DOOR SLIDE ARMED ANNUNCIATOR IAW AMM 33-16-01. OPERATIONS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (L4 DOOR) · airframe 71,584 hrs · 25,263 cycles
L4 DOOR EMER SLIDE OUT. RELAMPED L4 DOOR SLIDE EMER LIGHT IAW MM 33-51-06. OPERATIONS CHECKED GOOD.
Part: BATTERY — DISCHARGED (MEGAPHONE)
FORWARD CABIN MEGA PHONE NOT WORKING. R & R MEGA PHONE BATTERIES IAW MM 23-64-00. OPERATIONS CHECKED GOOD.
Part: SMOKE GOGGLES — MISSING (COCKPIT)
ONE EACH PAIR SMOKE GOGGLES MISSING FROM FLIGHT DECK. REPLACED SMOKE GOGGLES IAW MM 25-60-00.
Part: SLIDE — LOOSE (L2 DOOR)
SLIDE PACK AT THE L2 DOOR CAME LOOSE WHEN GATE AGENT WAS CLOSING DOOR. REPLACED SLIDE IAW MM 25-66-01. OPERATIONS CHECKED GOOD.
Part: EXHAUST VALVE — FAULTY (AC BAY)
LEVEL AT FL350 CABIN ALERTED EICAS & HORN. CABIN ALTITUDE QRC COMPLIED WITH. MODE SELECTOR IN MANUAL & OUTFLOW VLV FULLY CLOSED, CABIN CONTINUED TO CLIMB AT 500 FPM. CREW INITIATED RAPID DESCENT. FRM 21-30-21-00 REPLACED EQUIPMENT COOLING OVERBOARD EXHAUST VLV IAW AMM 21-58-05 PG 401 - 405. OPERATIONS CHECKED NORMAL. PERFORMED EXCESSIVE CABIN LEAKAGE TEST IAW AMM 05-51-24 PG 201 - 211 PRESSURIZATION NORMAL.
2013
Part: BATTERY PACK — DISCHARGED (FLASHLIGHT)
LEFT INBD AFT EMERGENCY FLASHLIGHT INOPERATIVE. R & R LT INBD AFT CABIN EMERGENCY FLASHLIGHT & BATTERY PACK IAW AMM 25-60-00, OPERATIONS CHECKED GOOD.
Part: FUSE — BLOWN (POWER SUPPLY)
AFT LEFT POWER SUPPLY FOR EMERGENCY LIGHTS FUSE BLOWN. R & R AFT EMERGENCY POWER SUPPLY ASSY IAW MM 33-51-07. OPS CHECKED GOOD.
Part: SWITCH — FAULTY (LE SLAT)
ON FINAL WHEN EXTENDING FLAPS 20 TO 30 FLAPS STOPPED MOVING AT 25 AND LEADING EDGE SLAT ASYM EICAS AND LEADING EDGE ANNUNCIATOR ILLUMINATED. PERFORMED FSEU BITE PROCEEDURE BLOCKS 1, 2, 3 AND 33 OF FIM. NO DEFECTS NOTED. FURTHER TROUBLESHOT TO ISLOLATION OF LEFT WING I/B - O/B SLAT SENCING SWITCH.