N166AA
Registered owner: E D SANTOS & ASSOCIATES LLC TRUSTEE, DE (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.
15 reports on file, 1995-03-07 – 1997-08-01.
Part: HYD FUSE — CRACKED (NR 3 HYD SYSTEM)
SFO - FLT 682 - AFTER TAKEOFF SFO DURING CLIMB-OUT WITH LANDING GEAR RETRACTED, LOST HYDRAULIC SYSTEM 3. ACCOMPLISHED ABNORMAL PROCEDURES, DUMPED FUEL, AND AIRCRAFT RETURNED TO SFO LANDING WITHOUT INCIDENT. REPLACED TRIM CYLINDER INTERLOCK FUSE. SERVICED HYDRAULIC SYSTEM 3. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)
Part: ANGLE — CORRODED (BS 1641-1661)
TULE - Z-ANGLE CORRODED STATION 1641-1661. SPLICED IN NEW SECTION OF 2 CHANNEL AND INSTALLED PER AARD 51-01-00 PAGE 05. (M)
Part: LONGERON — CORRODED (BS 1109)
TUL - DEEP CORROSION ON LONGERON FROM SPLICE AT STATION 1109 TO STATION 1156. REMOVED AND INSTALLED NEW LONGERON 48L AS PER SRM 51-00-00 PAGE 5 SPLICED FRAME TO FACILITATE LONGERON INSTALLATION AS PER 53-30-00 PAGE 5. (M)
Part: CHANNEL — CORRODED (BS 1521-1701)
TUL - 2-CHANNEL HAS CORROSION FROM STATION 1521-1701 LEFT. SPLICED IN NEW SECTION OF 2 CHANNEL AND INSTALLED PER AARD 51-01-00 PAGE 05. (M)
Part: CASTING — CORRODED (BS 1870)
TUL - CORROSION IN TWO LOWER HOLES OF NR 2 LATCH BRACKET MOUNT CASTING FOR AFT CARGO DOOR. REMOVED CORROSION AND INSTALLED BUSINGS PER SRM 53-50-00 PAGE 81. (M)
Part: DOOR FRAME — CORRODED (BS 1705)
TULE - DOOR FRAME CORRODED AT STATION 1705 LOWER FORWARD CORNER. INSTALLED REPAIR ANGLE PER ESO 7349 DATED 5-14-97. (M)
Part: FLOOR BEAM — DAMAGED (BS 1907)
TUL - REPAIRS DUE TO CORROSION DAMAGE ON FLOOR BEAM, MORE CORROSION FOUND ON C-V. REMOVED AND REPLACED FLOOR BEAM IAW SRM 53-00-01. TST: 81,156 HOURS. CYCLES: 24,004. (X)
Part: ANGLE — CORRODED (BS 1360)
TUL - CORROSION WAS FOUND ON VERTICAL CAP ANGLE IN LT MLG WW. REMOVED ANGLE AEA0474-1. INSTALLED NEW ANGLE AEA0474-1 IAW SRM VOL 1 51-00-00 PAGE 2. (M)
Part: SKIN — DENTED (BS 1721-1701)
TUL - TWO DENTS BETWEEN STA 1721 AND STA 1701 OUT OF LIMITS REF: ADL 0032 AT 36 LT LONGERON FORWARD OF AFT CARGO DOOR. INSTALLED CLASS I PERMANENT REPAIR PER SRM 53-20-00 FIG 6. TST: 81,156.07 HOURS. CYCLES: 24,004. (X)
Part: SPLICE — CORRODED (BS 1718)
TUL - LONGERON SPLICE PLATE CORRODED AT 48R STA 1718. REMOVED OLD PLATE, CLEANED AREA, TREATED, AND PRIMED. INSTALLED NEW SPLICE FITTING. TST: 81,156.07 HOURS. CYCLES: 24,004. (x)
Part: STRUCTURE — CORRODED (BS 1145)
TUL - STRUCTURE CORRODED IN AREA FWD OF BATTERY, LIGHT CORROSION ON SKIN. INSTALLED NEW LONGERONS 52, 51L, 51R. NEW SUPPORT FOR BATTERY BOX. SPLICED FRAME BETWEEN 48L AND 48R. REMOVED LIGHT CORROSION ON SKIN. TST: 81,156 HRS. CYCLES, 24,004. (X)
Part: SHEAR TIE — CORRODED (BS 1784)
TUL - DURING C-CHECK, FOUND CORROSION ON SHEAR TIE BETWEEN LONGERON 47R AND LONGERON 48R INSIDE AFT CARGO COMPARTMENT AT STA 1784. REMOVED AND REPLACED SHEAR TIE PER SRM 51-21-01, VOL II, AND SRM 51-31-01, VOL II. TST: 81,156.07 HRS. CYCLES, 24,004. (X)
Part: ANGLE — CORRODED (BS 1561)
TUL - CORROSION FOUND ON Z-ANGLE FROM STA 1561 TO STA 1600. SPLICED IN NEW SECITON PER SRM 53-00-01. TST: 81,156 HRS, CYCLES, 24,004. (X)
Earlier reports · 1995–1996 · 2 reports
1996
Part: BULKHEAD TEE — CRACKED (BS 1156)
TUL - DURING C-CHECK, FOUND CRACK IN FS 1156 BULKHEAD RIGHT TEE CAP INBOARD OF FIFTH FASTENER IN THE LOWER ROW OF FASTENERS FROM THE OUTBOARD END. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ESO 7349 DATE 5-14-97 AND SRM 51-35-01 VOL II, SRM 51-21-01, VOL II, SRM 51-38-01, VOL II. TST: 81,156.07 HRS. CYCLES, 24,004. (X)
1995
Part: EEL WIRE — BROKEN (CABIN)
JFK - FLT 678 - DURING APPROACH, EMERGENCY FLOOR LIGHTS AT RT BETWEEN R1 AND R3 DOORS ILLUMINATED. ACFT LANDED JFK WITHOUT INCIDENT. REPAIRED BROKEN/SHORTED WIRING FROM AM1 TO 8. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)