N482DA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AEROSIM ACADEMY INC | Operator | on 2018-07-25 | Operator named in NTSB report |
Accident & incident history
Operated by Aerosim Academy Inc. (per NTSB report)
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.
25 reports on file, 1995-03-28 – 1999-10-03.
Part: BATTERY — DISCHARGED (ROW 27)
LEFT AFT EMERGENCY OVERWING EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS NOW OK .
Part: ANGLE — CRACKED (NR 3 SPOILER ACT)
FOUND ON E-1 LETTER CK, NR 3 SPOILER O/B ACTUATOR ATTACH CASTING CRACKED. REPAIRED PER MM 57-42-0.
Part: FRAME — CRACKED (PAX DOORWAY)
FOUND AT E-1 LETTER CK, RT AFT ENTRY DOOR FRAME HAS VISABLE CRACK AT UPPER CUT OUT. REPAIRED PER SRM 53-10-9.
Part: FRAME — CRACKED (CARGO DOORWAY)
FUSELAGE FRAME C1 DOOR CUTOUT AFT FRAME WEB, CRACK REPAIR. THE AFT FRAME OF THE C1 DOOR CUTOUT WAS FOUND WITH A 1.5 CRACK IN THE FRAME WEB JUST INBD OF THE DOOR STOP FITTING. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH A TITANIUM REPAIR DOUBLER PER ER/A 367224-14.
Part: SKIN — CRACKED (BS 380-460)
PERFORMING INSPECTIONS PER SI 4-74176-12AD, 12 CRACK INDICATIONS WERE FOUND BETWEEN BS 380 TO 460 IN THE SKIN LAP JOINT AT S4L. REPAIRED PER ERA 332914-14AD.
Part: FRAME — CRACKED (BS 761)
DURING ACCOMPLISHMENT OF INSPECTIONS PER SI 4-61904-12AD, A CRACK WAS NOTED IN THE 2ND FAST HOLE ABOVE THE FLOORLINE. ALSO, THE 4TH FASTENER HOLE ABOVE THE FLOORLINE FELL OUT IN THE RADIUS OF THE REPAIR ANGLE. REPAIRED PER 332907-14AD.
Part: SKIN — CRACKED (BS 620-640)
PERFORMING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATIONS WAS NOTED IN THE S4R LAP JOINT BETWEEN BS 620 AND 640. THE INDICATION WAS LOCATED IN FASTENER ROW NR 11 AS IDENTIFIED IN FIGURE 6 OF THE SI. REPAIRED PER ERA 332909-14AD.
Part: SKIN — CRACKED (BS 570-580)
PERFORMING INSPECTIONS PER SI 4-74176-12AD, A CRACK INDICATION WAS FOUND IN THE S4R LAP JOINT BETWEEN BS 560 TO 580. THE CRACK INDICATION WAS LOCATED AT FASTENER ROW 8 AS IDENTIFIED IN FIGURE 6 OF THE SI. REPAIRED PER ERA 332910-14AD.
Part: KEEL BEAM — CRACKED (BS 870)
KEEL BEAM LT LWR CHORD WAS FOUND CRACKED IN THE UPPER FLANGE TYPICAL OF THAT DESCRIBED BY SB 727-53-0208, REV 1. REPAIRED PER ERA 332906-14.
Earlier reports · 1995–1998 · 16 reports
1998
Part: BATTERY — DISCHARGED (GALLEY DOOR)
AFT GALLEY DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY.
Part: BATTERY PACK — DISCHARGED (SERVICE DOOR)
AFT SERVIVCE DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY RACK.
Part: FRAME — CRACKED (BS 910)
REF SHIP NR 482, TPA, LETTER CHK D2, CRACK AT STA 910 FRAME FWD OUTBOARD RADIUS. REPAIRED PER MM 53-11-0.
Part: RIB — CRACKED (LT HORIZ STAB)
LT ELEV HINGE SUPPORT RIB CRACKED, ELEV STA 99.79 AFT I/B END. REPAIRED PER MM 55-10-31 FIG 802.
Part: SPAR WEB — CRACKED (CENTER SECTION)
WING CENTER SECTION REAR SPAR WEB, RBL 3 AND LBL 10 : REPAIR FOR WEB CRACK. THE WING CENTER SECTION REAR SPAR WEB WAS FOUND WITH TYPICAL CRACKS NEAR THE UPPER CAP AT RBL 3 AND LBL 10. THE DAMAGED AREAS OF WEB WERE CUTOUT AND REPAIRED WITH ALUMINUM REPAIR DOUBLERS. THE REPAIRS WERE ACCOMPLISHED PER ER/A 365002-14AD, REV B. THE REPAIRS ARE CONSIDERED TEMPORARY UNTIL HMV WHEN THE FULL SPAR WEB MODIFICATION WILL BE ACCOMPLISHED PER AD 97-25-15.
1997
Part: DOWNLOCK SENSOR — MALFUNCTIONED (RT MLG)
AFTER GEAR RETRACTION RIGHT MAIN GEAR INDICIATION WAS BOTH THE RED AND GREEN RIGHT GEAR INDICATORS ILLUMINATED WITH GEAR HANLDE UP. WITH HANDLE DOWN ALL GEAR INDICATED DOWN AND LOCKED. REPLACED RT LANDING GEAR DOWN LOCK SENSOR.
1996
Part: STIFFENER — CRACKED (RT WING SPAR)
FOUND ON C1 LETTER CK, 2 INCH CRACK IN WING FWD SPAR STIFFNER AT THE NR 7 SLAT INBD TRACK. REPAIRED PER MM 57-20-21.
Part: DOOR — CRACKED (R-2 SERVICE)
A .25 INCH VISIBLE CRACK UPPER FWD END OF RT AFT SERVICE DOOR. REPAIRED PER SRM 52-40-2 FIG 4, INSTALLED DOOR ON AIRCRAFT AND LEAK OPS CHECK OK.
1995
Part: TRANSVERSE BEAM — CRACKED (BS 1273)
THERE IS A CRACK IN THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1273. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AD 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129.
Part: SKIN — CRACKED (RT ELEVATOR)
FOUND ON B1 LETTER CK, RT ELEVATOR LWR SKIN CRACKED TWO PLACES, ONE INCH EACH, 12 INCHES FWD OF TAB OUTBD END. REPAIRED PER SRM 55-20-3 FIG 4.
Part: WINDOW — SHATTERED (CABIN)
DURING CRUISE, RIGHT FORWARD OVERING EXIT DOOR WINDOW OUTER PANE SHATTERED AND DEPARTED AIRCRAFT, LANDED DEN. WINDOW WAS REPLACED. REMAINS OF SHATTERED WINDOW ROUTED TO ENGINEERING FOR EVALUATION.
Part: SEPARATOR ASSY — BURST (LOWER ACM COMP)
ON CLIMBOUT AT FL 2,500, HEARD LOUD BANG FOLLOWED BY VIBRATION AND RISING CABIN ALTITUDE, RETURNED ATL. FOUND LEFT PACK WATER SEPARATOR ASSEMBLY BURST. REPLACED SAME, OPERATION NORMAL.
Part: FUEL CONTROL — MALFUNCTIONED (NR 3 ENGINE)
DURING CRUISE, NR 3 ENGINE HAD FLUCTUATING FUEL FLOW AND N1, AND EPR. RETARDED THROTTLE, THEN ENGINE FLAMED-OUT. LANDED PHL WITHOUT INCIDENT. ENGINE WAS CHECKED PER MM, ALL PARAMETERS NORMAL. AS A PRECAUTION, THE FUEL CONTROL AND FUEL PUMP WERE REPLACED.
Part: RIB — CRACKED (NR 4 SLAT)
THE NR 4 L/E SLAT RIB CRACKED .5 INCHES O/B SIDE. FOUND DURING A-2 LTR CHECK. REPAIRED PER MM 57-54-0 PG 803.
Part: SKIN — CRACKED (LT ELEV)
A FIVE INCH CRACK AT LOWER SKIN OF LT ELEV SKIN O/B SIDE. FOUND DURING A-2 LTR CK, TPAMM 3/28/95. REPAIRED PER SRM 55-20-3 FIG 5.
Part: SKIN — CRACKED (NR 6 SLAT)
FOUND DURING E-2 LETTER CHECK, BOLT SHEARED AND UPPER SKIN WEDGE CRACKD 1 INCH NR 6 SLAT I/B GUIDE HOOK. REPAIRED PER SRM 57-50-3 FIG 10.