N8524A
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.
13 reports on file, 2005-05-26 – 2011-10-27.
Part: HYDRAULIC SYSTEM — WARNING LIGHT · airframe 23,647 hrs · 20,331 cycles
ABORTED TAKE OFF DUE TO NR 3 HYD LOW PRESSURE MESSAGE. RESET NR 3 HYD SYSTEM, CREW PERFORMED ENGINE RUN FOR OPS CHECK, OPS NORMAL AT THIS IAW AMM 12-00-06. HYD LOW PRESSURE SYSTEM 3 AT V1, ROTATED AT GEAR UP GEAR DISAGREE WARNING, NOSE GEAR WARNING. SYSTEM 3 DROPPED TO 1400 PSI. RETURNED FOR LANDING. BLED NR 3 HYD SYSTEM IAW AMM 29-10-00. COMPLIED WITH PA 05-018B. OP CHECKED GOOD. GEAR RETRACTION AND EXTENSION CHECKS GOOD IAW AMM 32-30-00. A/C OK FOR SERVICE.
Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 23,526 hrs · 20,216 cycles
UNCOMMANDED STAB CH 2 & MACH TRIM DISCONNECT AT GATE. REMOVED AND REPLACED HSTCU. OP CHECKS & BITE CHECKS GOOD AT THIS TIME. REF AMM 27-40-00. SYSTEM CERTIFIED CAT II & RVSM. A/C OK FOR SERVICE. PART EFFECTIVITY VERIFIED.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 23,526 hrs · 20,216 cycles
CAPT'S EMERGENCY FLASHLIGHT FAILS "RED" LED TEST. REMOVED AND REPLACED CAPT'S EMERGENCY FLASHLIGHT BATTERY OP'S CHECK GOOD IAW MM 25-60-00, VERIFIED PARTS EFFECTIVITY.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 23,268 hrs · 19,972 cycles
THE UNPRESSURIZED SKIN BETWEEN AT FS 682 BETWEEN STRINGERS S-23R AND S-24R WERE DAMAGED AS A RESULT FROM CONTACT WITH MAINTENANCE EQUIPMENT. THE DAMAGE WAS REPAIRED IAW BOMBARDIER REO 601R-53-61-4167.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 23,156 hrs · 19,915 cycles
CREW DECLARED AN EMERGENCY & DIVERTED TO MKE FROM DSM FOR F/O'S WINDSHIELD CRACKED FLIGHT. LANDED SAFELY WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED F/O`S WINDSHIELD IAW AMM 56-11-01.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,110 hrs · 18,921 cycles
FS 559.00 BULKHEAD WEB WAS FOUND CRACKED AND REQUIRES REPAIR. COMPLIED WITH BOMBARDIER REO 601R-53-41-260 AND BOMBARDIER REO 601R-53-41-609 REV B.
Earlier reports · 2005–2009 · 7 reports
2009
Part: O-RING — LEAKING (HYD LINE)
ON APPROACH TO RUNWAY 35, GEAR SELECTED DOWN FOLLOWED BY "GEAR DISAGREE" MESSAGE THEN FOLLOWED BY HYD LOW PRESSURE ON NR 3 SYS. QRH FOLLOWED, EMERGENCY DECLARED WITH UNEVENTFUL LANDING. MX INSPECTED SYS FOUND THE NR 3 HYD BALL ATTENUATOR UNION LEAKING. REMOVED AND REPLACED O-RING ON UNION OF THE BALL ATTENUATOR. SYS SERVICED AND PRESSURE TESTED IAW AMM. (K)
2005
Part: FCU — FAILED (TE FLAPS)
( REF NR: 05-104) FLAP FAILURE. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT (FECU) IAW AMM. (K)
Part: FCU — FAILED (TE FLAPS)
(REF NR: 05-098) FLAP FAILURE AT 0, QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU) IAW AMM. (K)
Part: CONTROL SYSTEM — FAILED (TE FLAPS)
(REF NR: 05-079) FLAPS FAIL ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAP SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)
Part: FCU — FAILED (TE FLAPS)
(REF NR: 05-080) FLAP FAIL ON TAXI, RETURNED TO GATE. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU) IAW AMM, SYSTEM TESTS GOOD. (K)
Part: CONTROL SYSTEM — FAILED (TE FLAPS)
(REF NR: 05-074) FLAPS FAIL MESSAGE AT ZERO WHEN RETRACTED. EMERGENCY DECLARED QRH FOLLOWED UNEVENTFUL LANDING WITH FLAPS 0. RESET FLAPS AND PLAED ON 72 HOUR WATCH IAW AD 98-20-01. (K)
Part: CONTROL SYSTEM — FAILED (TE FLAPS)
(REF NR: 05-068) FLAP FAIL. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD98-20-01. (K)