N841JS
Registered owner: FE XL 5253 LLC, NC (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
EMER PRESS ACM OVERHEAT, LT BLEED AIR OVERHEAT, ALSO SMELLED SOMETHING BURNING.
HISSING NOISE FROM MAIN CABIN DOOR FROM 6K TO 39K, SUSPECT ACOUSTIC SEAL IS BROKE. REMOVED FOREIGN OBJECT FROM CABIN DOOR HINGE AREA THAT WAS BLOCKING DOOR SEAL.
TAKEOFF WAS ABORTED AT 85 KIAS DUE TO UNUSUALLY HIGH AIRFLOW FROM THE ECS VENTS AND AN âACM OâHEATâ ANNUNCIATOR. TROUBLE SHOT SYSTEM AND COULD NOT DUPLICATE DISCREPANCY
PRIOR TO 80 KNOTS RECEIVED A âACM OâHEATâ ANNUNCIATION. PERFORMED VOLTAGE AND CONTINUITY CHECK OF ACM OVERHEAT TEMPERATURE SENSOR (ST012) IAW CE560XL AMM 21-51-00. NO DEFECTS NOTED. PERFORMED VISUAL INSPECTION OF ECU EXHAUST DUST, ACM AND ECU STRUCTURE, AND BLEED AIR TUBING FOR CRACKS AND DEFORMATIONS IAW CE560XL AMM 21-51-00. NO DEFECTS NOTED GAINED ACCESS TO L BLEED AIR OVER HEAT TEMPERATURE SENSOR (ST017), TAIL TEMPERATURE SENSOR (TT0OL), AND TEMPERATURE SENSOR (ST021) LOCATED ON L BLEED AIR TUBING COMING FROM THE L PRECOOLER IAW AMM 36-11-01. PERFORMED OPS CHECK OF PRECOOLER DOOR ACTUATION IAW AMM 36-11-00. NO DEFECTS NOTED. PERFORMED RESISTANCE CHECK OF SENSOR (TT00L) AND VISUAL EXAMINATIONS OF ALL SENSORS IAW AMM 36-11-01. NO DEFECTS NOTED. REINSTALLED ALL PANELS REMOVED TO GAIN ACCESS !AW AMM 36-11-01. NO DEFECTS NOTED. SWAPPED POSITIONS OF LEFT BL-LEVEL FLOW CONTROL VALVE AND RIGHT BL-LEVEL FLOW CONTROL VALVE FOR TROUBLESHOOTING PURPOSES. IAW AMM 21-11-00. NO DEFECTS NOTED. EVALUATION FLIGHT REQUIRED TO DETERMINE IF ISSUE REMAINS ON LEFT HAND SIDE OR TRANSITIONS TO RIGHT HAND SIDE.
ACM OVERHEAT, BLEED AIR OVERHEAT, WING OVERHEAT, FUMES IN COCKPIT. INSPECTED ACM , NO DEFECTS NOTED. RUN APU AND OPS CHECK ENVIRONMENTAL SYS , ALL PARAMETERS NORMAL, ALL COCKPIT INDICATION NORMAL, TROUBLESHOT LT & RT ENGS PYLON RAM AIR ACTUATOR. PERFORMED TAXIING & HIGH POWER RUNS & FOUND NORMAL HEATING ON BOT LT & RT AI SYS. FOUND ANNUNCIATIONS FOR L & R O'HEAT TO BE NORMAL BUT WAS NOTED DURING (TO) DETENT THAT ACM O'HEAT LIGHT WAS ILLUMINATING . DID NOT HAVE ANY RESISTANCE INCREASE WHEN APPLYING HEAT. FUNCTIONAL TEST OF ANNUNCIATION LIGHT ON COCKPIT ON HARNESS SIDE WERE NORMAL WHEN JUNPING PIN ( A ) & ( B ) "ON" PT007 & PT008 FOR L & R O'HEAT LIGHTS. FOR ACM O'HEAT WAS NOTED THAT THE O'HEAT SWITCH ( ST012 ) RESISTANCE WAS AT 8.3 OHMS WHEN IT SHOULD BE 5 OHMS ON PINS 1 & 2.. ALSO WHEN APPLING HEAT THERE WAS NO CHANGE IN RESISTANCE. FUNCTIONAL CHECK OF ANNUNCIATION WAS NORMAL PIN (1 AND 2) WHEN JUMPED ON THE HARNESS SIDE ( PT038 ) ACM O'HEAT LIGHT WAS TURNING (ON). R & R LT & RT BLEED O'HEAT SWITCHES & ACM TEMP SENSOR IAW 36-11-00, 25-52-00 . WM REF: 21-52-00. R & R ACM OVER HEAT TEMP SWITCH ST012 FOLLOWED BY FUNCTIONAL TEST WITH NORMAL RESULTS DURING HIGH POWER RUN " NO" ACM O'HEAT NOTED DURING STEPS. WORK PERFORMED IAW MM REF: 36-11-00, 25-52-00 ,76-11-00. WM REF: 21-52-00. R & R LT & RT BLEED AIR O'HEATS SWITCHES ( ST017 & ST014 ) PERFORMED OPS CHECKS WITH NORMAL RESULTS IAW MM 36-11-00, 25-52-00 ,76-11-00. WM REF: 21-52-00.ALL ACCESS CLOSED.
ACZM OVERHEAT, BLEED AIR OVERHEAT, WING OVERHEAT, FUMES IN COCKPIT
HIGH SPEED TAKE OFF ABORT DUE TO A LOUD BANG AND AIRCRAFT YAW. BELIEVED TO BE A COMPRESSOR STALL. CLEARED THE RUNWAY, FOD FROM THE ENGINE FOUND IN THE AFTERMATH. NO INJURIES OR ADDITIONAL DAMAGE TO THE AIRCRAFT.
FLT NR 4066 - WHILE APPLYING TAKEOFF POWER, RIGHT ENGINE FLAMED OUT AT APPROXIMATELY 70 PERCENT TORQUE. AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. OUT STATION MAINTENANCE INSPECTED THE RIGHT ENGINE AND DISCOVERED THE PLENUM ON THE ENGINE WAS CRACKED. DAY MX LATER REMOVED AND REPLACED THE RIGHT ENGINE IAW MM 71-00-00. GROUND RUN CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
FLT NR 4134 - FLAP POSITION WARNING SOUNDED WHEN CREW WAS PREPARING FOR LANDING, ATTEMPTS TO POSITION FLAPS FOR LANDING WERE UNSUCCESSFUL. CREW PREPARED FOR NO FLAPS LANDING AND DECLARED AN EMERGENCY CRASH TRUCKS DISPATCHED. AIRCRAFT LANDED WITHOUT INCIDENT. DAY MAINTENANCE RIGGED FLAP POSITION MICRO-SWITCH IAW MM 27-50-00. GROUND CHECK GOOD, AIRCRAFT RELEASED FOR SERVICE.
FLT NR 4032 - CREW ELECTED TO RETURN TO FIELD, NOT ABLE TO GET LEFT GENERATOR ON LINE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE REPLACED LEFT S/G, GROUND CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.