N13331
Registered owner: CJC AVIATION INC TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| CONTINENTAL AIRLINES INC | Operator | on 1988-03-10 | Operator named in NTSB report |
Accident & incident history
Operated by CONTINENTAL AIRLINES (per NTSB report)
Operated by CONTINENTAL AIRLINES (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.
8 reports on file, 1995-10-13 – 1999-12-05.
Part: KEELBEAM — CORRODED (BS 500D)
INSPECTION FOUND KEEL BEAM CORRODED AT STA 500D, S28R. REPAIRED IAW SRM 53-30-12.
Part: SKIN — CRACKED (BS 211)
INSPECTION FOUND A .5 INCH CRACK IN SKIN OF CAPTAIN'S SLIDING WINDOW FORWARD UPPER FRAME AT STA 211. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5330-02833.
Part: SPACER — JAMMED (LANDING GEAR)
THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE OVERRIDE TRIGGER WAS PULLED AND THE GEAR THEN RETRACTED NORMALLY. THE FLIGHT WAS CONTINUED AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR LOCK LEVER SYSTEM AND TROUBLESHOT PER MM 32-31-21. MAINTENANCE FOUND TELEFLEX CABLE BINDING DUE TO SISSOR LINK SPACER JAMMED. THE SPACER WAS REMOVED AND REPLACED, THE CABLE WAS LUBRICATED. THE LEVER LOCK SYSTEM OPERATED NORMALLY IAW MM 32-31-11.
Part: FLOORBEAM — CORRODED (BS 986.5)
INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5 FROM L-2 TO R-2 DOOR. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51 AND ECRA 5310-03450.
Part: FLOORBEAM — CORRODED (BS 312)
INSPECTION FOUND FLOORBEAM CORRODED AT BS 312, BL 0 TO RBL 15. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51 PAGE 221, FIGURE 205.
Part: COUPLER — INOPERATIVE (YAW DAMPER)
FLT NR 716 - IAH - THE AIRCRAFT WAS EXHIBITING DUTCH ROLL TENDENCY, ESPECIALLY AT ALTITUDE. THERE WAS NO MOVEMENT OF YAW DAMPER INDICATOR NOTED IN FLIGHT. THE FLIGHT WAS UNEVENTFUL. THE YAW DAMPER COUPLER WAS REMOVED AND REPLACED AND THE SYSTEM CHECKED GOOD PER MM 22-12-31. THE FAILURE HAS BEEN CONFIRMED. TEARDOWN FINDINGS REVEALED THE RATE GYRO WAS AT FAULT. (M)
Part: SKIN — DENTED (BS 294.5-344)
HOU - INSPECTION FOUND A .25 INCH DENT IN FUSELAGE SKIN BELOW R-2 DOOR BETWEEN STA 294.5 AND STA 344. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 210. (X)
Part: SKIN — CRACKED (NR 2 SLAT)
HOU - INSPECTION FOUND CRACKS EXTENDING FROM RIVET HOLES OF NR 2 SLAT LOWER SKIN. THE CRACKS RAN FROM RIVET TO RIVET. ONE CRACK TOTALED 6 INCHES IN LENGTH AND THE OTHER TOTALED 5 INCHES IN LENGTH. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5750-01159 AND BOEING DRAWING NR 65C30133. (X)