N466DA
Registered owner: AEROSEEDER LLC, IA (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, 1995-03-31 – 1999-08-08.
Part: HYD SYS — REQD SERVICE (A HYD SYS)
HYD 'A' FLUID LEVEL DROPPED TO 2.0 GAL DURING FLIGHT AND PASSENGERS REPORTED SMELLING FUMES NEAR/IN SEATS OVERWING AREA. ALT FLAPS AND MANUAL GEAR USED. A/C ARRIVED AT GATE WITH HYD QTY 3.75 GAL. SERVICED HYD TO FULL, 1 GAL ADDED. INSPECTED NOSE AND MAIN GEAR AND WING SLATS AND FLAPS AND RUDDER. RAN ENGS NR 1 AND NR 2 CKD HYD LINES FOUND OK. WITH NEGS RUNNING, NO SMELL IN CABIN.
Part: SWITCH — FAILED (RT MLG DOOR)
AFTER T/O, AFTER GEAR RETRACTION, RED DOORS WARNING LIGHT AND R GEAR DOOR WARNING LIGHTS ILLUMINATE WHEN GEAR. HANDLE PLACED TO OFF. INSPECTION AND REPLACED RT GEAR DOOR SWITCH AND SYS CKS OK.
Earlier reports · 1995–1998 · 15 reports
1998
Part: BATTERY PACK — DISCHARGED (CABIN)
AFT LEFT EMERGENCY LIGHT INOP. REPLACED BATT PACK. LIGHT NOW WILL NOT TURN OFF. REPLACED BATTERY RACK. CKS GOOD PER MM.
Part: SPAR WEB — CRACKED (CENTER WING)
THE CENTER WING REAR SPAR WEB WAS FOUND WITH 3.5 INCH LONG CRACK AT RBL 3. THE CRACK IS NEAR THE UPPER CAP AT A CHEM-MILL RADIUS IN THE WEB AND IS TYPICAL OF AD 97-25-15. THE CRACK WAS ROUTED OUT AND A LOCAL DOUBLER REPAIR WAS INSTALLED PER ER/A 364880-14, REV B. MANDATED INSPECTIONS ARE CONTINUED UNTIL COMPLETE SPAR MODIFICATION AT NEXT HMV.
1997
Part: BULKHEAD WEB — CRACKED (BS 178)
SEVERAL CRACKS FOUND IN THE FS 178 BLKHD RBL 6, LBL 5 AND BL 0. REPAIRED PER ERA 330815-14.
Part: SKIN — DENTED (BS 1090)
THREE SKIN DENTS WERE FOUND AT APPROX FS 1090 TO 1100 AT STRINGER 18L. THE DIMENSIONS OF THE DENTS WERE BEYOND SRM ALLOWABLE DAMAGE. THE THREE DAMAGE LOCATIONS HAVE BEEN CUT OUT WITH DIMENSIONS OF APPROX 2.0 X 1.5, 2.0 X 1.0, AND 1.0 X 1.0. THIS ER/A WILL AUTHORIZE USING ONE EXTERNAL SRM REPAIR DUE TO CLOSE PROXIMITY OF THE 3 DENTS, DAL B727 SRM 53-30-3, FIGURE 3.
1995
Part: SKIN — CORRODED (BS 540)
AT CV2 IN TPA, THE FUSELAGE SKIN AT STA 540 BETWEEN S-26R AND S-27R, JUST BELOW THE LAP SPLICE HAS BEEN TRIMMED TO REMOVE CORROSION. THE CUT OUT MEASURES 5 INCH BY 11 INCH. THIS ER/A REPAIRS THE AREA BY ADDING A .090 2024-T3 CLAD FILLER, .050 2024-T3 CLAD DOUBLER AND A .063 2024-T3 CLAD TRIPLER. ACCOMPLISHED REPAIRS PER DL ERA 302359-14.
Part: FRAME — CUT (BS 990)
FOUND ON CV2 CHECK, CUT STA 990 FRAME AND FAIL-SAFE CHORD FOR ACCESS TO REPAIR STR 29L, REF NRC 256. REPAIRED FRAME AND CHORD PER MM 53-12-0 PG 806 AND 807, REPAIRED CHORD PER SRM 51-40-3.
Part: SKIN — CRACKED (LT SERVICE DOOR)
FOUND ON CV2 CK, FED LOWER CORNER OF LT AFT SERVICE DOOR OUTER SKIN CRACKED. REPAIRED PER M/M 52-11-01.
Part: FLOORBEAM — CORRODED (BS 344)
FOUND ON CV2 CHECK, CORROSION AROUND FASTENER HOLES FLOORBEAM UPPER SURFACE STA 344 LBL 45 RBL 13. REPAIRED PER SRM 53-10-8 FIG 10.
Part: ANGLE — CRACKED (WING)
A .75 INCH CRACK BELOW NR 8 SLAT TAI ON SUPPORT ANGLE. REPAIRED PER M/M 57-54-0 PG 807A, FOUND AT LETTER CHECK.
Part: ELEVATOR — DENTED (RT ELEVATOR)
FOUND ON CV CK, DENT TOP SIDE OF RT ELEVATOR OB SIDE .5 BY .3125, .1875 DEEP. REPAIRED PER SRM 55-20-3 FIG 4.
Part: SKIN — CRACKED (VERT STAB)
A .5 INCH CRACK RT SIDE OF VERT STAB BELOW AND AFT OF SADDLE PANEL 9501. FOUND AT B-1 LETTER CK. REPAIRED PER SRM 55-30-3.
Part: SKIN — CRACKED (VERT STAB)
A ONE INCH CRACK LT SIDE OF VERT STAB AT STR-6 APPROX FIN STA 160. FOUND AT B-1 LETTER CK. REPAIRED PER SRM 55-30-3.
Part: SLAT — CRACKED (NR 2)
CRACK BELOW ANTI-ICE TUBE NR 2 SLAT OPN 5535 AD. FOUND AT B-1 LETTER CHECK. REPAIRED PER MM 57-54-0 FIG 805A.
Part: SKIN — CRACKED (VERT STAB)
A .5 INCH CRACK RT SIDE OF VERT STAB BELOW PANEL 9501. FOUND DURING B-1 LTR CK. REPAIRED PER SRM 55-30-3.
Part: WEB — CRACKED (TORQ BX)
A ONE INCH CRACK ON LIGHTENING HOLE RT SIDE OF TORQUE BOX IN 48 SEC. FOUND AT B-1 LETTER CK. REPAIRED PER MM 53-11-0.