N881YV
Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)
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.
17 reports on file, 2015-05-06 – 2024-12-22.
Part: ENGINE — SURGES (RIGHT) · airframe 101,504 hrs · 39,103 cycles
RIGHT ENGINE SURGING. IT STOPPED WHEN THROTTLES REDUCED. THERE WERE NO EXCEEDENCES. ENGINE OPERATON BECAME NORMAL AGAIN. PERFORMED BORESCOPE INSPECTION. NO DEFECTS NOTED.
Part: MODULE — FAULTED (MLG WW) · airframe 101,306 hrs · 38,884 cycles
ON APPROACH TO CVG SELECTED FLAPS AND GOT TRAINING EDGE FLAP DISAGREEE MESSAGE. LANDED WITH FLAPS AT 20 DEGREES.
Part: SKIN — CORRODED (RT WING) · corrosion level 3 · airframe 100,755 hrs · 38,683 cycles
CORROSION BEYOND LIMITS FOUND ON RH WING LOWER SKIN BETWEEN WS 1045.0 & WS 1070.59 AND THE REAR SPAR.
Part: SKIN — CORRODED (LT WING) · corrosion level 3 · airframe 100,755 hrs · 38,683 cycles
CORROSION FOUND ON LH WING UPPER SKIN BETWEEN STR U-2 AND U-4 AND SPLICE AND BODY STATION 97.42.
Earlier reports · 2015–2022 · 13 reports
2022
Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 99,375 hrs · 37,819 cycles
CORROSION FOUND ON RH INBOARD STABILIZER UPPER SKIN AT FRONT SPAR.
Part: SKIN — CRACKED (ZONE 100) · airframe 99,375 hrs · 37,819 cycles
CRACK FOUND ON RH SIDE OF LOWER FUSELAGE AT STA. 660.
2021
Part: COOLING DUCT — RUPTURED (LT ENGINE) · airframe 98,614 hrs · 37,246 cycles
LEFT ENGINE FIRE MASTER WARNING MESSAGE AT FLIGHT LEVEL 260. SHUTDOWN LEFT ENGINE AND RETURNED TO AIRPORT. FOUND LEFT ENGINE LOW PRESSURE TURBINE CASE COOLING DUCT RUPTURED. REPLACED DUCT.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 98,027 hrs · 36,867 cycles
CENTER WING-UPPER PLATING BETWEEN LBL 54 - LBL 43 AROUND REPAIR SPAR, CORROSION DAMAGE REPAIR.
Part: SKIN — CORRODED (LT WING) · corrosion level 3 · airframe 98,027 hrs · 36,867 cycles
LEFT WING, TRAILING EDGE STRUCTURE AT UPPER FORWARD SECTION BETWEEN WBL 296 TO 283, CORROSION DAMAGE REPAIR.
Part: SKIN — CORRODED (LT WING) · corrosion level 3 · airframe 98,027 hrs · 36,867 cycles
LEFT WING - UPPER PLATING BETWEEN WBL 190 TO 198 AROUND REAR SPAR, CORROSION DAMAGE REPAIR.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 98,027 hrs · 36,867 cycles
CENTER WING - UPPER PLATTING BETWEEN LBL 7-LBL 9.5 AROUND REAR SPAR, CORROSION DAMAGE REPAIR.
2015
Part: SENSOR — DIRTY (LE SLAT) · airframe 93,610 hrs · 34,875 cycles
AFTER TAKEOFF, CREW NOTICED DURING FLAP RETRACTION LE RETRACTION, LE SLAT ASYMMETRY AIR & GND DISAGREE, AFTER GEAR RETRACTION. AFTER FOLLOWING QRM PROCEDURES, CREW MADE DETERMINATION TO DIVERT. LANDED SAFELY WITH NO FURTHER INCIDENT. FOUND SENSORS VERY DIRTY. CLEANED SENSORS & PERFORMED BITE OF PSEU IAW FIM 32-09 FT805. SYS OPERATIONS CHECKED GOOD IAW 27-50-00. ALSO CLEANED SENSORS & PERFORMED BITE OF PROX BOX IAW FIM 32-09 FT805. SYS OPERATIONS CHECKED GOOD IAW AMM 32-09-03.
Part: SENSOR — OUT OF ADJUST (LE SLATS) · airframe 93,610 hrs · 34,876 cycles
AFTER TAKEOFF, CREW NOTICED DURING FLAP RETRACTION, LE SLAT DISAGREE & LE SLAT ASYMMETRICAL STATUS MESSAGE, LE SLAT SHUTDOWN AIR & GROUND DISAGREE, AFTER GEAR RETRACTION. AUTO BRAKES INOPERATIVE. CREW MADE DETERMINATION TO RETURN, DUE TO PREVIOUS DIVERT FOR SAME ISSUE. LANDED SAFELY WITH NO FURTHER INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED PSEU DRIVE CARD 007. PERFORMED BITE ON PSEU, NO FAULTS. VERIFICATION FLIGHT FAILED. ACFT MX FERRY FOR CORRECTION. ADJUSTED LE SLAT SENSOR S286 IAW AMM 27-11-00. LE RVDT M548 ADJUSTED IAW AMM 27-81-02. REPLACED FSEU IAW AMM 27-51-01. ADJUSTED SENSOR S268 FOR AIR & GND DISAGREE. AUTO BRAKES TESTED GOOD IAW AMM & FIM.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 93,606 hrs · 34,874 cycles
DURING C CHECK INSPECTION, INSPECTORS FOUND FLIGHT DECK EMER EXIT LIGHT INOPERATIVE. R & R EXIT LIGHT ASSEMBLY IAW MM 33-51-001. OPERATIONAL CHECKED NORMAL IAW MM 33-51-00 202.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 56,028 hrs · 34,781 cycles
DURING A3 CHECK, INSPECTION FOUND COCKPIT DOOR EMER LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM 33-51-01. OPERATIONAL TESTED NORMAL.
Part: TERMINAL — BROKEN (FIRE LOOP) · airframe 93,157 hrs · 34,693 cycles
AIRCRAFT ARRIVED WITH NO INBD WRITE-UPS. WHILE MX WAS DOING THE ENG START CHECKLIST TO START TROUBLESHOOTING THE LT ENG PRSOV MEL, IT WAS FOUND THAT THE LT ENG FIRE DETECT SYS WOULD NOT TEST & ONLY NR 2 OVHT LOOP WOULD TEST. AFTER OPENING THE LT ENG COWLINGS FOUND TERMINALS BROKEN ON THE AFT UPPER A LOOP & AFT LOWER B LOOP & TERMINAL BROKEN ON THE SYS 1 OVHT LOOP. R & R LT ENG UPPER AFT FIRE ELEMENT IAW AMM 26-11-02 201. TROUBLE SHOT IAW FIM 26-11 FT-804. R& R LT ENG FIRE OVERHEAT DETECTOR ELEMENT IAW AMM 26-11-02 201. OPERATIONAL TEST NORMAL & ACFT RETURNED TO SERVICE.
Part: TURBINE BLADES — DAMAGED (LT ENGINE) · airframe 93,151 hrs · 34,690 cycles
CLIMBING THROUGH 4000' CREW HAD HIGH ENG VIBRATION WITH EGT GOING INTO YELLOW ARC ON LT ENG. ENG PULLED BACK TO IDLE THRUST & STILL HAD VIBRATION. ENG SHUTDOWN & RETURNED. VISUAL DAMAGE TO TURBINE BLADES. UPON INSPECTION, BORESCOPE, IT WAS DETERMINED THAT TURBINE BLADE FAILURE WAS THE REASON FOR THE VIBRATION. R &R NR 1 ENG, PERFORMED VISUAL INSPECTION OF THE PYLON, COMPLETED ENG RUN CHECKS & LEAK CHECKS, SEE LOG PAGES 005040 THRU LOGPAGES 005150. ENG CHANGE COMPLIED WITH & ALL ITEMS CLEARED. ACFT READY FOR SERVICE.