N940DN
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.
22 reports on file, 2013-02-03 – 2018-12-04.
Part: SWITCH — MALFUNCTIONED (FLAP POSITION) · airframe 45,998 hrs · 37,403 cycles
SHIP 9240 - ATO - AT 110 KNOTS DUE TO SLAT CONFIGURATION WARNING. CORRECTIVE ACTION: DURING TROUBLESHOOTING FOUND FLAP/SLAT HANDLE POSITION SWITCH HARNESS 671 SHORT TO GROUND. REPLACED FLAP/SLAT HANDLE POSITION SWITCH. OK FOR SERVICE. (LP# 5298224)
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,712 hrs · 36,600 cycles
EMERGENCY EXIT SIGN ABOVE THE L2 DOOR WAS INOPERATIVE. INSTALLED A NEW BATTERY AND POWER SUPPLY. OPS CHECKED GOOD.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 44,215 hrs · 36,286 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 21 WILL NOT ILLUMINATE. DURING INSPECTION FOUND WIRE BROKEN AT TERMINAL. REPAIRED THE WIRE. OPS CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,051 hrs · 36,193 cycles
DURING AN A CHECK, FOUND THE EXIT SIGN B5-231 BATTERY INOPERATIVE. REPLACED THE BATTERY AND CHECKED GOOD.
Earlier reports · 2013–2016 · 18 reports
2016
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 40,403 hrs · 34,125 cycles
RIGHT UPPER AFT SKIN CRACKED. COMPLIED WITH ERA 551649-14AD.
Part: CONTROL UNIT — MALFUNCTIONED (FLT CONTROL) · airframe 38,312 hrs · 32,871 cycles
AT CRUISE ALTITUDE, ACFT PORPOISES UP AND DOWN +/- 300 FPM. MAINTENANCE FOUND LT EPCU WITH EXCESSIVE PLAY CAUSING 2" OF MOVEMENT IN ELEVATOR. R & R EPCU IAW MM. OPERATION AND LEAK CHECKS OK.
2015
Part: D-RING — DETACHED (COCKPIT) · airframe 38,185 hrs · 32,802 cycles
FLIGHT DECK DOOR EMERGENCY EGRESS DETACH CABLE/RING BROKEN OFF. REMOVED DOOR, INSTALLED NEW CABLE FOR D-RING. OPERATION CHECKS OK.
Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 36,121 hrs · 31,515 cycles
VERTICAL STABILIZER LT SIDE INTERNAL ATTACH ANGLE IS CRACKED AT STA 1475. REPLACED ANGLE IAW SRM 51-30-00.
Part: ANGLE — CRACKED (BS 1494) · airframe 36,121 hrs · 31,515 cycles
CRACKED CLIP AT BS1494, TAIL INTERIOR. R & R CLIP IAW SRM 51-00-01 AND 51-30-00.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 35,745 hrs · 31,279 cycles
AFT AIRSTAIR EMERGENCY LIGHT L2-848 HAS BROKEN A WIRE AND THE LIGHT IS INOPERATIVE. REPAIRED THE WIRE IAW SWPM. OPS CHECKED GOOD.
2013
Part: TIRE — FAILED (MLG) · airframe 32,776 hrs · 29,406 cycles
LEFT CENTER BUTTE DOOR ON LT SIDE HAS IMPACT DAMAGE FROM BLOWN TIRE EVENT. REMOVED LEFT CENTER BUTE DOOR. FORWARD TO CDL PER 57-50-02.
Part: TIRE — FAILED (MLG) · airframe 32,776 hrs · 29,406 cycles
LEFT GEAR SPRAY DEFLECTOR ASSEMBLY HAS IMPACT DAMAGE FROM BLOWN TIRE EVENT. R & R SPRAY DEFLECTOR ON LT MLG IAW AMM.
Part: TIRE — FAILED · airframe 32,776 hrs · 29,406 cycles
AIRCRAFT BLEW NR 1 AND NR 2 TIRES ON LANDING. MAINTENANCE BITE AACU. SHOWED L1, WHEEL SPIN LOCKUP AND IRU FAULTS. R & R LEFT INBD AND OTBD WHEEL SPEED TRANSDUCERS, AACU, LT/RT DACOMS, AND NR 1/NR 2 IRU'S IAW AMM. ALL OPERATIONS CHECKED GOOD.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,400 hrs · 29,161 cycles
DURING SERVICE CHECK, CATWALK EMERGENCY LIGHTS FOUND INOPERATIVE. R & R TEN LAMPS. OPS CHECKED GOOD.
Part: LANYARD — OUT OF POSITION (TAILCONE SLIDE) · airframe 30,959 hrs · 28,318 cycles
TAILCONE EVACUATION SLIDE RT LANYARD HAS BEEN DISPLACED FROM ITS ENGAGED CONFIGURATION. RE-ENGAGED TAIL CONE EVAUCATION SLIDE LANYARD (RT) IAW A/C 9240 CARD 2500-4332.
Part: RELEASE CABLE — WORN (TAILCONE) · airframe 30,959 hrs · 28,318 cycles
DURING CHECK, AFT TAILCONE RELEASE CABLE HAS WEAR SPOT AT UPPER LT SIDE. R & R AFT TAILCONE RELEASE CABLE ASSY IAW MM. PERFORMED FUNCTIONAL TEST RELEASE SYS. OPS CHECKS GOOD.
Part: DRAIN — CRACKED (WINDOW) · airframe 30,959 hrs · 28,318 cycles
F/O LIGHTNING WINDOW DRAIN HOLE IS CRACKED, BS 120-050) CLEARVIEW SLIDING WINDOW. HFEC, VERIFIED CRACK, MARKED END. ROUTED OUT CRACK. NO DEFECTS NOTED. ALODINED AND PRIMED IAW ERA 504837-14 REV O AND SRM 51-10-03, VOL 2, PARA 14 AND 21. REPAIR TAG IAW PS 900-5-1, NR 4.
Part: DRAIN — CRACKED (WINDOW) · airframe 30,959 hrs · 28,318 cycles
DURING CHECK, CAPTAINS LIGHTNING WINDOW DRAIN HOLE IS CRACKED, STA 120-050 (CLEARVIEW SLIDING WINDOW) HFEC, VERIFIED CRACK, MARKED END. ROUTED OUT EXISTING CRACK, NO DEFECTS NOTED. ALODINED AND PRIMERED IAW ERA 504837-14, REV O AND SRM 51-10-03, VOL 2, PARA 14 AND 21, PS 900-5-1 NR 4.
Part: SKIN — DAMAGED (BS 351) · airframe 30,959 hrs · 28,318 cycles
EXTERIOR FUSELAGE AT BS 351 + 7" AND LONGERON 16R SKIN IS SUNKEN AROUND FASTENERS. CUT OUT DAMAGED AREA. FABRICATED DOUBLER, FILLER AND FINGER DOUBLER. TREATED, INSTALLED REPAIR PARTS IAW SRM 53-31-03, 51-10-05, 51-10-03, PARA 14& 21.
Part: BUSHING — CORRODED (RT MLG STRUT) · airframe 30,959 hrs · 28,318 cycles
RT MLG SUPPORT FITTING BUSHING BORE HAS EVIDENCE OF CORROSION. REAMED INBD BORE TO REMOVE CORROSION, FINAL BORE SIZE 2.315 DIAMETER IAW AMDS 5742-01025-02 AND DWG SR09570087. COMPLIED FD NDI OF BORE AREA IAW PS 900-6-3 NO 02. NO DEFECTS NOTED.
Part: SUPPORT FRAME — CORRODED (BS 71) · airframe 30,959 hrs · 28,318 cycles
RT FORWARD NLG DOOR AFT HINGE SUPPORT FRAME CORRODED, FORWARD AND TOP SIDE OF FRAME, STA 71 BETWEEN 26R AND 27R MRB 53-100-02. REMOVED FRAME AND CORROSION. FOUND TO BE OUT OF LIMITS WITH MATERIAL LOSS GREATER THAN 20 PERCENT. FABRICATED NEW FRAME, ALODINED, PRIMED AND TOP COATED. INSTALLED FRAME IAW SRM 51-10-01, FIG 1, 51-10-03, PARA 14, 21 AND 26. 51-30-02, FIG 1, 51-30-05, PARA 7, 53-00-01, FIG 3 AMM AND DWG 9957852.
Part: SPRING — CORRODED (RELEASE MECH) · airframe 30,959 hrs · 28,318 cycles
TAIL-CONE JETTISON RELEASE MECHANISM PIN SPRINGS ARE CORRODED. R & R TAIL CONE JETTISON RELEASE MECHANISM PIN SPRINGS IAW AMM.