N386AE
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.
22 reports on file, 1997-09-07 – 2004-12-17.
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 14,217 hrs · 16,598 cycles
DURING PRE-FLIGHT CREW FOUND THE EMERGENCY LIGHT AT 4A TO BE INOPERATIVE. MAINTENANCE REPLACED THE DOME LIGHT AT 4A AND AN EMERGENCY POWER SUPPLY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501824) (K)
Part: FRAME — DENTED (FUSELAGE)
ABI - DUIRNG AN MBV INSPECTION, THE CARGO FRAME AT STATION 677 WAS FOUND DENTED. PERFORMED A CUTOUT OF THE DAMAGE AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007323 PARA 1, DATED JUNE 29, 2004. (M)
Part: FRAME — DENTED (FUSELAGE)
DURING AN MBV INSPECTION, THE CARGO FRAME AT STATION 640 WAS FOUND DENTED. PERFORMED A CUT OUT OF THE DAMAGED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB 340 STATEMENT 340SDS007323, PARA 1 DATED JNE 29, 2004. (M0
Part: FRAME — DENTED (FUSELAGE)
ABI - DURING AN MBV INSPECTION, THE CARGO FRAME AT FS 649 WAS FOUND DENTED. PERFORMED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB 340 REPAIR STATEMENT 340SDS007323, PARA 1 DATED JUNE 29, 2004. (M)
Part: SKIN — DENTED (HORIZONTAL STAB)
ABI - DURING MBV INSPECTION AND REPAIR OF HAIL DAMAGE. THE LEFT HORIZONTAL STABILIZER TOP SKIN PANEL HAIL DAMAGE WAS BEYOND SRM LIMITS. REMOVED EXISTING TOP SKIN. PREPARED NEW SKIN AND INSTALLED SKIN. WORK DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 43, CHAPTERS 51-40-21, 22-23, 24, 51-20-50 AND 51-20-56. (M)
Part: SKIN — DENTED (HORIZONTAL STAB)
DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. THE RIGHT HORIZONTAL STABILIZER TOP SKIN PANEL, HAIL DAMAGE WAS BEYOND SRM LIMITS. REMOVED EXISTING TOP SKIN PANEL. PREPARED NEW RIGHT HORIZONTAL TOP SKIN AND INSTALLED. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 43, CHAPTERS 51-40-21, 22, 23, 24, 51-20-50 AND 51-20-56. (M)
Part: FRAME — DENTED (FUSELAGE)
ABI - DURING AN MBV INSPECTION, THE UNDER FLOOR CARGO FRAME AT FS 658.5 FOUND DENTED. PERFORMED A CUT OUT OF THE DAMAGED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB 340 REPAIR STATEMENT 340SDS007323 PARA 1 DATED JUNE 29, 2004. (M)
Earlier reports · 1997–2003 · 15 reports
2003
Part: RELAY — INOPERATIVE (RT ENGINE)
DFW - FLT 3572 - CREW REPORTED THE RIGHT ENGINE FAILED ON FINAL APPROACH TO DFW. DURING TROUBLESHOOTING AS PER A SAAB MX FOUND RELAY 68KF TO BE AT FAULT. RELAY WAS REPLACED AND OPERATIONAL CHECK WERE COMPLIED WITH. AIRCRAFT WAS RELEASED FOR FCF. CHECK FLIGHT WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
2002
Part: CONTROL PANEL — FAULTY (COCKPIT)
DFW - FLT 3533 - DURING CRUISE FLIGHT, CREW REPORTED THE GEAR IN TRANSIT LIGHT CAME ON AND REMAINED ON IN FLIGHT. HYDRAULIC PUMP DID NOT RUN AND GEAR APPEARED TO REMAIN LOCKED AND UP. AIRCRAFT WAS RETURNED TO DFW. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL PANEL IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: ENGINE — POWER LOSS (RIGHT)
LBB - FLT 3493 - DURING FINAL APPROACH, CREW REPORTED THE LOSS OF RIGHT ENGINE TORQUE FOLLOWED BY ALL OTHER ENGINE PARAMETERS FALLING OFF RAPIDLY. NO ABNORMAL NOISES OR VIBRATIONS WERE NOTED. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SGF - FLT 3567 - EMERGENCY EXIT SIGN ABOVE FORWARD EMERGENCY EXIT WILL NOT ILLUMINATE. RAI RIGHT FORWARD EMERGENCY EXIT SIGN IAW AMM 33-50-35. (M)
Part: DOOR — MISINSTALLED (EMERGENCY EXIT)
ON PREFLIGHT, FOUND OVERWING EMERGENCY EXIT DOORS INSTALLED ON WRONG SIDES OF A/C. INSTALLED EMERGENCY EXIT DOORS IN THE CORRECT POSITIONS. (M)
Part: CONNECTOR — LOOSE (COCKPIT)
LAX - FLT 3236 - FOUND RIGHT MLG GREEN INDICATION DID NOT COME ON WHEN GEAR WAS SELECTED DOWN. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LOOSE CANNON PLUG 6GA AND RESECURED. (M)
2001
Part: LIGHT — INOPERATIVE (CABIN)
DFW - MAINTENANCE REPORTED THE EMERGENCY LIGHT STRIP AT SEATS 3A AND 4A TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP AT 3A AND 4A IAW SAAB MM 33-50-20. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
2000
Part: VALVE — FAILED (MLG)
LRD - FLT 3296 - LANDING GEAR WILL NOT RETRACT AFTER TAKEOFF. ALL 3 GREEN LIGHTS ON. DISAGREEMENT LIGHT ON. GEAR HANDLE IN UP POSITION. REMOVED AND REPLACED LANDING GEAR CONTROL VALVE IAW AMM 32-31-15. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
1999
Part: CONTROL VALVE — FAILED (LANDING GEAR)
ABI - FLT 5251 - MAIN LANDING GEAR WOULD NOT EXTEND. HAD TO USE MANUAL OVERRIDE. REMOVED AND REPLACED LANDING GEAR CONTROL VALVE. LEAK AND FUNCTIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — DAMAGED (BS 710-718)
ABI - FOUND DAMAGE TO AFT FUSELAGE SKIN BETWEEN FRAMES AT STA 710 AND STA 718 JUST ABOVE SL 1520 WITH MINOR DAMAGE TO INTERNAL SPLICE PLATE. PERFORMED A CUT-OUT OF DAMAGED SKIN, EDDY CURRENT INSP, NO DEFECTS. FABBED EXT DOUBLER AND TRIPLER .032 INCH THICK, DOUBLER 9.75 INCHES BY 7.01 INCHES, AND TRIPLER 9.75 INCHES BY 10.0 INCHES. FABBED FILLER .050 INCH THICK TO DIMENSIONS OF CUT-OUT. POSITIONED REPAIR DOUBLER, TRIPLER, FILLER, AND DRILLED, DEBURRED, BROKE ALL SHARP EDGES. APPLIED COATING OF ALODINE AND EPOXY PRIMERS. FAY SEALED ALL REPAIR PARTS AND WET INSTALLED ALL FASTENERS. EDGE SEALED REPAIR. RESTORED FINISH. WORK DONE IAW SAAB 72SDS1597 AND SAAB 340 SRM. AIRCRAFT OK FOR SERVICE. (X)
1998
Part: SEAT TRACK — CORRODED (BS 297)
SEAT TRACK AT FS 297, BL 18.3L, FOUND TRACK CORRODED BEYOND LIMITS. A SPLICE REPAIR WAS DONE ON LT SEAT TRACK AT FS 297, BS 18.3L IAW SAAB SRM 53-70-60. AIRCRAFT RETURNED TO SERVICE. (X)
Part: AIRSTAIR TRACK — CORRODED (BS 225-272)
AIRSTAIR TRACK HAD CORROSION BEYOND LIMITS AT FS 225 - FS 272, BL 28L. REMOVED AND REPLACED AIRSTAIR TRACK IAW SAAB SRM 51-40-2. AIRCRAFT RETURNED TO SERVICE. (X)
Part: CAP END — CORRODED (BS 296)
ABI - LEFT SEAT TRACK END CAP HAD CORROSION BEYOND LIMITS AT FS 296, BL 18.3L. REMOVED AND REPLACED LT SEAT TRACK END CAP IAW SAAB SRM 53-00-00. AIRCRAFT RETURNED TO SERVICE. (X)
Part: GALLEY TRACK — CORRODED (BS 225-261)
ABI - RT LAVATORY AND GALLEY TRACK AT FS 225 - FS 261, BL 324, HAS CORROSION BEYOND LIMITS. REMOVED AND REPLACED RT LAVATORY AND GALLEY TRACK IAW SAAB SRM 51-40-25. AIRCRAFT RETURNED TO SERVICE. (X)
1997
Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMP)
DFW - FLT 3707 - ON TAKEOFF ROLL, RECEIVED A CARGO SMOKE INDICATION. TAKEOFF ABORTED. FIRED NR 1 EXTINGUISHER BOTTLE. INDICATION WENT OUT. FOUND NO EVIDENCE OF FIRE/SMOKE IN CARGO COMPARTMENT. REMOVED AND REPLACED CARGO COMPARTMENT SMOKE DETECTORS AND FIRE BOTTLE AND RETURNED AIRCRAFT TO SERVICE. (X)