N826CR
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.
14 reports on file, 1998-01-30 – 2000-08-12.
Part: ADC — FAILED (E/E BAY)
AIR TURNBACK DUE TO NR 2 AIR DATA COMPUTER FAILURE. NORMAL APPROACH AND LANDING WITH NO FUEL DUMPED. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. OPS CHECK GOOD IAW L1011 MM 34-14-01. (M)
Part: FILTER — FAILED (NR 1 ENGINE)
NR 1 ENGINE OIL FILTER PRESSURE LIGHT ON IN-FLIGHT. ENGINE WAS SHUTDOWN. AIRCRAFT DIVERTED TO JFK WITH A NORMAL APPROACH AND LANDING. TROUBLESHOT IAW 79-00-00 FIG 106. REPLACED FINE SCAVENGE AND PRESSURE FILTERS IAW MM 72-01-00. RAN ENGINE PER 71-00-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: FILTER — FAILED (NR 1 ENGINE)
NR 1 ENGINE OIL FILTER PRESSURE LIGHT ON IN-FLIGHT. ENGINE WAS SHUTDOWN. AIRCRAFT DIVERTED TO JFK WITH A NORMAL APPROACH AND LANDING. TROUBLESHOT IAW 79-00-00 FIG 106. REPLACED FINE SCAVENGE AND PRESSURE FILTERS IAW MM 72-01-00. RAN ENGINE PER 71-00-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: FILTER — FAILED (NR 3 ENGINE)
NR 3 ENGINE OIL FILTER PRESSURE LIGHT ON IN-FLIGHT. ENGINE SHUTDOWN. AIRCRAFT RETURNED TO BASE WITH A NORMAL APPROACH AND LANDING. TROUBLESHOT IAW 79-00-00 FIG 106. REPLACED FINE SCAVENGE AND PRESSURE FILTERS IAW 72-01-00. RUN ENGINE PER 71-00-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
Part: FILTER — FAILED (NR 3 ENGINE)
NR 3 ENGINE OIL FILTER PRESSURE LIGHT ON IN-FLIGHT. ENGINE SHUTDOWN. AIRCRAFT RETURNED TO BASE WITH A NORMAL APPROACH AND LANDING. TROUBLESHOT IAW 79-00-00 FIG 106. REPLACED FINE SCAVENGE AND PRESSURE FILTERS IAW 72-01-00. RUN ENGINE PER 71-00-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
Earlier reports · 1998–1999 · 9 reports
1999
Part: CONNECTOR — CORRODED (NR 3 ENGINE)
DURING DESCENT FIRE WARNING OCCURRED ON NR 3 ENGINE. ENGINE FIRE DRILL COMPLETED. A/C LANDED WITHOUT INCIDENT. CORRECT ACTION IAW FIM 26-11-00 REG 112. FOUND CORRODED CONNECTOR. FALSE FIRE WARNING, REMOVED AND REPLACED CONNECTOR IAW SRM 20-24-06. OPS CHECK NORMAL. A/C RETURNED TO SERVICE. (M)
Part: PIN — NOT REMOVED (NLG)
DEPARTED MBJ, NOSE GEAR WOULD NOT RETRACT. DUMPED APPROX 40,000 LBS OF FUEL AND LANDED WITHOUT FURTHER INCIDENT. AT RETURN TO MBJ, NOSE GEAR DOWNLOCK PIN WAS FOUND INSTALLED. REMOVED PIN AND RETURN AIRCRAFT TO SERVICE. (M)
Part: CLAMP — LOOSE (ECS BAY)
AT FLT LEVEL 28,000 FT, THE FLIGHT CREW HEARD A LOUD NOISE FOLLOWED BY THE CABIN VSI INDICATING A 1000 FT CLIMB. THE AIRCRAFT THEN DESCENDED TO 12,000 T. AT THAT POINT THE DECISION WAS MADE TO DIVERT TO SAN JUAN, PUERTO RICO TO INVESTIGATE THE PROBLEM. FOUND THE NR 3 WATER SEPARATOR RUBBER BOOT CLAMP LOOSE. RECLAMPED BOOT AND ACCOMPLISHED PRESSURIZATION TEST AND LEAK CHECK IAW 21-31-00. (M)
Part: CLAMP — LOOSE (NR 3 ACM)
CABIN PRESS FAULT LEGEND, CABIN ALT CLIMBING WITH BOTH OUTFLOW VALVES CLOSED. WHEN LEVELING FLT 350, CABIN PRESS WARNING HORN CAME ON FOLLOWED BY CABIN PRESS FAULT LIGHT ON AND DIFF PRESS AT 5000 AND CABIN ALT AT 11.5 COULD NOT CONTROL IN STANDBY OR MNL MODE. NO AIRFLOW IN AIRCRAFT. FOUND CLAMP ON RUBBER BOOT LOOSE AT NR 3 PACK WATER SEPARATOR. REPOSITIONED BOOT AND RESECURED CLAMP IAW 21-31-00. (M)
1998
Part: SLIDE — LOOSE (PASSENGER DOOR)
UPON OPENING THE L3 DOOR, DISCOVERED A PORTION OF THE SLIDE/RAFT ASSY WAS HANGING DOWN AND VISIBLE TO THE FLIGHT ATTENDANT. THE DOOR WAS THEN RE-CLOSED AND SECURED AND THE SLIDE/RAFT WAS DEFERRED FOR ONE FLIGHT. AFTER FURTHER INVESTIGATION, DETERMINED THE IDENTIFICATION FLAP HAD BECOME DETACHED. THE FLAP WAS RE-SECURED AND THE DEFERRAL CLEARED.
Part: BATTERY — DISCHARGED (CABIN)
ON PERFORMING 2A CHECK EMERGENCY FLASHLIGHT, FOUND WITH LOW BATTERY. FLASHLIGHT REPLACED. (M)
Part: WIRE — BROKEN (CABIN)
ON PERFORMING LAYOVER SERVICE, FOUND BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHTING SYSTEM AT SEAT ROWS 45 HJ. BROKEN WIRE REPAIRED.
Part: POWER PACK — INOPERATIVE (CABIN)
EMERGENCY EXIT LIGHTS INOPERABLE AT L-3 DOOR. REMOVED AND REPLACED EMERGENCY POWER PACK IAW 33-21-19. OPS CHECK SATISFACTORY. (X)
Part: SLIDE/RAFT — MISMANUFACTURED (L1 DOOR)
WHEN ATTEMPTING TO EXECUTE MINI-EVAC DRILL, L-1 DOOR OPENED PARTIALLY AND L-1 SLIDE/RAFT FAILED TO DEPLOY. DRILL CALLED OFF AND L-2 DOOR SLIDE/RAFT REMOVED FOR RE-INSPECTION. L-1 DOOR SLIDE/RAFT REMOVED FOR INSPECTION. FOUND GIRT BAR STRAP TOO SHORT TO ALLOW RELEASE CABLE TO PULL PINS ON COVER. RETURNED TO VENDOR FOR FURTHER EVALUATION AND TEAR DOWN REPORT.