N76073
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| RIVER CITY AIR/CHARTER | Operator | on 1983-11-08 | Operator named in NTSB report |
Accident & incident history
Operated by RIVER CITY AIR/CHARTER (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.
16 reports on file, 1995-01-30 – 1999-09-05.
Part: STIFFENER — CORRODED (BS 2007)
INSPECTION FOUND STIFFENER CORRODED IN AFT CARGO COMPARTMENT AT STA 2007. REPAIRED IAW ECRA 531-01069.
Part: WEB — CRACKED (NR 2 PYLON)
INSPECTION FOUND A 5 INCH CRACK AT FORWARD WEB OF NR 2 PYLON AFTER REMOVING VERTICAL FIN. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-31-01.
Part: SPAR — SHEARED (TAILCONE)
INSPECTION FOUND THE TAIL CONE WORK PLATFORM SPAR SHEARED IN SEVERAL PLACES. THE SHEARED AREAS WERE TRIMMED OUT AND REINFORCED WITH DOUBLERS IAW SRM 53-00-01, FIGURE 4 AND 51-31-01.
Part: SUPPORT — CORRODED (BS 1871)
INSPECTION FOUND LT LAV FLOOR SUPPORT CORRODED AT ZONE 290, STA 1871. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01.
Part: RIB — CRACKED (TAILCONE)
INSPECTION FOUND A 1 INCH CRACK IN RIB AT LT INNER CAVITY OF TAIL CONE. THE RIB WAS TRIMMED OUT AND THE AREA WAS REINFORCED WITH AN ANGLE REPAIR IAW SRM 53-00-00, FIGURE 1 AND 51-31-01.
Earlier reports · 1995–1998 · 11 reports
1998
Part: SKIN — CRACKED (WS 906)
INSPECTION FOUND AN 8 INCH CRACK ON LEFT WING LEADING EDGE SKIN AT WING STA XOS 906.00. REPAIRED IAW ECRA 5731-01009.
Part: FUSE — BLOWN (CABIN)
INSPECTION FOUND EMERGENCY LIGHT IN ZONE-D ON RT SIDE, SEATS 37KL-45KL INOPERATIVE. A BLOWN FUSE FOR BATTERY PACK WAS FOUND. THE FUSE WAS REPLACED AND OPERATION OF THE EMERGENCY LIGHTS WAS RESTORED.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION FOUND EMERGENCY LIGHTS IN LEFT AFT ZONE INOPERATIVE. THE BATTERY AND BATTERY CHARGER WERE REMOVED AND REPLACED.
Part: BALLAST — FAILED (CABIN)
SMOKE STARTED COMING FROM OVERHEAD ABOVE ROW 44L JUST PRIOR TO LANDING. HALON WAS APPLIED AND THE SMOKE CEASED. MAINTENANCE FOUND SIDEWALL BALLAST AT ROW 44L BURNT. THE BALLAST WAS REMOVED AND THE SIDEWALL LIGHT WAS PLACARD INOPERATIVE.
1997
Part: BULKHEAD WEB — CRACKED (BS 1521)
INSPECTION FOUND A 17 INCH CRACK ON PRESSURE BULKHEAD WEB AT STA 1521 BETWEEN Z= 74 AND 80. FILLER, DOUBLER, AND A FINGER DOUBLER WERE FABRICATED AND INSTALLED IAW ECRA 5330-02559 AND SRM 53-20-00, FIGURE 6.
Part: SUPPORT — CORRODED (BS 460)
INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 460, LBL 28. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-35-01.
Part: SUPPORT — CORRODED (BS 440)
INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 440, BETWEEN BL 0 AND LBL 28. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-35-01.
1995
Part: FRAME — CORRODED (FS 1701/1721)
KUL - INSPECTION FOUND CORROSION ON FRAME CAPS AT STATION 1701 AND 1721 BETWEEN LONGERONS 50L AND 50R. THE FRAME CAPS WERE REPAIRED IAW ECRA 5310-03101. (W)
Part: CORNER — CORRODED (CARGO DR CUTOUT)
KUL - INSPECTION FOUND CORROSION ON THE FORWARD CARGO DOOR CUTOUT FORWARD LOWER CORNER. THE FORWARD CARGO DOOR CUTOUT FORWARD LOWER CORNER WAS REPAIRED IAW ECRA 5330-02272. (W)
Part: ACTUATOR BOLT — SHEARED (RT MLG)
KUL - THE RT MLG RETRACT ACTUATOR ATTACH FITTING UPPER FORWARD BOLT WAS FOUND SHEARED. THE BOLT WAS REPLACED PER STANDARD PRACTICE CHAPTER 20 OF THE MAINTENANCE MANUAL AND SERVICE BULLETIN 57-67. (W)
Part: FIRE LOOP — INOPERATIVE (NR 1 ENGINE)
HNL - FLT 0906 - THE NR 1 ENGINE FIRE WARNING 'B' LOOP LIGHT BEGAN TO FLICKER ON AND OFF AND EVENTUALLY ILLUMINATED STEADILY WHILE ON DESCENT INTO HNL. THE NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND THE PYLON FORWARD 'B' LOOP AT FAULT. THE PYLON FORWARD 'B' LOOP WAS REMOVED AND REPLACED. IN ADDITION, THE PYLON AFT LOOP A AND B ASSEMBLY WAS REPLACED. OPERATION OF THE 'B' FIRE DETECTION LOOP CHECKED GOOD. (X)