N8673D
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
32 reports on file, 2003-06-30 – 2013-06-22.
Part: LIFE VEST — TORN (CABIN) · airframe 24,012 hrs · 21,528 cycles
FOUND INFANT LIFE VEST TORN. R & R INFANT LIFE VEST AS REQUIRED IAW AMM 25-60-00.
Part: SIGN — INOPERATIVE (CABIN) · airframe 23,217 hrs · 20,735 cycles
EMERGENCY LIGHTS INOPERABLE - SERVICE DOOR/CLOSET/1SR ROW ORANGE STRIP. REMOVED AND REPLACED LEFT FORWARD CLOSET LIGHTED FLOOR LEVEL EXIT SIGN IAW AMM 33-51-10. OPS CHECK GOOD.
Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 23,187 hrs · 20,707 cycles
CAPTAIN LIFE VEST BAG TORN. REMOVED AND REPLACED VEST IAW AMM 25-61-03.
Earlier reports · 2003–2012 · 29 reports
2012
Part: SKIN — CRACKED (FUSELAGE) · airframe 22,774 hrs · 20,288 cycles
SKIN AT FS 621 CRACKED AROUND LINTEL FITTING. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,238 hrs · 19,755 cycles
CABIN EMERGENCY FLOOD LIGHT 1 BULB INOP. REMOVED AND REPLACED NR 3 EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-18. OP CK NORMAL DM65184, CLEARED PLACARD REMOVED.
Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 22,238 hrs · 19,755 cycles
AFT SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. CLEANED AND CONNECTED LIGHT. OPS CHECKED NORMAL IAW AMM 33-51-01. OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,186 hrs · 19,707 cycles
CABIN EMERGENCY FLOOR LIGHT AT ROW 9 INOP. REMOVED AND REPLACED CABIN EMERGENCY FLOOR LIGHT AT ROW 9 IAW AMM 33-51-01. OPS CHECK GOOD.
Part: LIFE VEST — DAMAGED (COCKPIT) · airframe 22,169 hrs · 19,689 cycles
FIRST OFFICER`S LIFE VEST BAG DAMAGED. REMOVED AND REPLACED FIRST OFFICER`S LIFE VEST IAW AMM 25-61-03.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,135 hrs · 19,662 cycles
EMERGENCY FLOOR LIGHT AT ROW 10 INOP. RE-SECURED EMERGENCY LIGHT STRIP AT ROW 10 IAW CRJ AMM 33-50-00, OPS CHECK GOOD. OK FOR SERVICE.
Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 22,003 hrs · 19,524 cycles
F/O'S LIFE VEST BAG TORN. REMOVED AND REPLACED F/O'S LIFE VEST IAW AMM 25-61-03.
Part: LIGHT — INOPERATIVE (SEAT 10C) · airframe 21,911 hrs · 19,436 cycles
FLOOR LIGHT EMERGENCY STRIP LIGHT AT 10C INOPERATIVE FLT 4020. REPLACED LIGHT IAW AMM 33-51-00
Part: PUMP — FAILED (HYD SYSTEM) · airframe 21,876 hrs · 19,406 cycles
HYDRAULIC 3 LOW PRESSURE CAUTION MESSAGE DURING GEAR EXTENSION. CAME ON FOR 5 SECONDS AND WENT AWAY. 2900 PSI SHOWING 65 PERCENT 35C. GEAR SEEMED TO TAKE LONGER THAN NORMAL TO EXTEND AND RT MAIN WAS LAST TO LOCK DOWN. REMOVED AND REPLACED HYD PUMP 3B IAW AMM 29-12-03. OPS CHECKED GOOD. OK FOR SERVICE. OPS CHECKED GEAR SWING IAW AMM 32-30-00.
Part: LOCK — DIRTY (COCKPIT DOOR) · airframe 21,643 hrs · 19,194 cycles
COCKPIT DOOR STICKY, VERY DIFFICULT TO LOCK/UNLOCK. CLEANED COCKPIT DOOR LOCKS IAW AMM 25-18-00, OK FOR SVC.
Part: AILERON SYS — UNKNOWN · airframe 21,602 hrs · 19,157 cycles
AILERON CONTROLS ARE HEAVY AND DIFFICULT TO MOVE ON GROUND AND IN AIR, ACFT ALSO HAS SLUGGISH FEEL DURING FLIGHT. PERFORMED OPERATIONAL CHECK OF AILERON CONTROL SYSTEM IAW 27-11-00, OPS CHECKED GOOD. PERFORMED VISUAL CHECK OF AILERON CONTROL CABLES IAW 27-11-06, ACFT OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,592 hrs · 19,147 cycles
EMERGENCY LIGHTS OUT IN CABIN BY ROWS 8 & 9, THE LIGHT TRACK LOOSE. SECURED EMERGENCY LIGHT IAW AMM 33-50-00, OPS CHECKED GOOD. OK FOR SERVICE.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,560 hrs · 19,115 cycles
FS 484 LEFT INTERCOSTAL CLIP CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-41-059.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,560 hrs · 19,115 cycles
CARGO DOOR SILL HAS CORROSION AROUND NUT PLATE HOLE AT FS 607. REPAIRED IAW SRM 53-00-00.
Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 21,436 hrs · 18,997 cycles
RUDDER TRIM CONTROL ON CENTER PEDESTAL RUNS UNCONTROLLABLY. REMOVED AND REPLACED RUDDER AND AILERON TRIM CONTROL PANEL IAW CRJ 200 AMM 27-12-10. OPS CHECK GOOD.
2011
Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER) · airframe 21,264 hrs · 18,862 cycles
OB GND SPLRS CAUTION MESSAGE. PER MOC CYCLED CB'S PER CRJ FIM. MSG CLEARED. OK FOR SERVICE.
Part: CONTROL MODULE — MALFUNCTIONED (NLG STEERING) · airframe 20,938 hrs · 18,510 cycles
STEERING INOP CAUTION MSG IN FLIGHT QRH RUN MSG STILL PERSIST EMERGENCY DECLARED. REMOVED AND REPLACED STEERING ECU IAW AMM 32-51-10.NO FIX. VERIFIED PART EFFECTIVITY. REMOVED AND REPLACED NOSE AND CONTROL MODULE IAW AMM 32-51-01. NO FIX. VERIFIED PART EFFECTIVITY. REMOVED AND REPLACED NOSE GEAR ELECTR HYD SERV VALVE IAW AMM 32-51-15. OPC GOOD. VERIFIED PART EFFECTIVITY. REMOVED AND REPLACED NOSE GEAR HYD MANIFOLD IAW AMM 32-51-15. OPC GOOD. VERIFIED PART EFFECTIVITY.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 20,143 hrs · 17,749 cycles
GEAR DISAGREE A/C IS STILL IN WORK.
Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 20,036 hrs · 17,654 cycles
OVERBOARD COOL FAIL DEFERRED PER MEL 21-24-61.
Part: UNKNOWN — FAILED (CABIN) · airframe 20,036 hrs · 17,654 cycles
OVERBOARD COOL FAIL DEFERRED PER MEL 21-24-61.
2010
Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 17,784 hrs · 15,540 cycles
FS 280 FLOORBEAM BETWEEN FWD AND AFT J-ANGLES AT DOORWAY THRESHOLD BETWEEN LBL 9 AND RBL 9 CORRODED. REPAIRED FLOOR SUPPORT WEB IAW BOMBARDIER REO 601R-53-11-926 REV B.
2009
Part: FCU — FAILED (TE FLAPS) · airframe 17,060 hrs · 14,824 cycles
FLAPS FAILED AT 2 ON RETRACTION 120 KNOTS 3HR 10MIN 1C. REMOVED AND REPLACED FECU IAW AMM 27-51-05 OPC NORMAL. PERFORMED TS PER BOMBARDIER FIM REV 3 9 IAW AD 2009-06-12 PARAGRAPH H 6 I PER AMOC DATED MAR 27 2009 & PA AD 27-05 2F 860D100-18ABCD.
2008
Part: STOP FITTING — OUT OF ADJUST (EMERGENCY EXIT)
RIGHT OVERWING EMERGENCY EXIT WOULD NOT OPEN. ADJUSTED RT EMERGENCY DOOR FRAME STOPS IAW AMM 52-22-01. OPERATIONALLY CHECKS GOOD. (A)
2006
Part: FLAP — MALFUNCTIONED (WING) · airframe 8,953 hrs · 7,972 cycles
FLAPS FAILED (WITHIN 72 HOURS OF MONITORING).
Part: FLAP — MALFUNCTIONED (WING) · airframe 8,950 hrs · 7,970 cycles
FLAPS FAIL AT ZERO. MONITORING FOR 72 HRS PER AD 98-20-01.
Part: SWITCH — LOOSE (STAB TRIM) · airframe 8,002 hrs · 7,227 cycles
UPON REACHING CRUISE STAB TRIM CAUTION MESSAGE. QRH FOLLOWED WITH CAUTION NOT CLEARING. QRH STATED A FLAPS 20 LANDING FOR THIS. FLAP TWENTY LANDING PERFORMED UNEVENTFUL. MAINTENANCE FOUND THE STAB TRIM CHANNEL NR 2 SWITCH LOOSE AND RESECURED SWITCH WITH SYSTEM OPERATIONAL CHECKED IAW AMM.
2004
Part: FLAP — MALFUNCTIONED (WING)
RECEIVED (FLAPS HALF-SPEED) MESSAGE ON BLOCK OUT. FLAP SYSTEM INSPECTED FECU CHECKED FOR CODES, NO CODES FOUND. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01.
Part: FCU — FAILED (TE FLAPS)
FLAP FAILURE AT PUSH BACK. REMOVED AND REPLACED FECU. (FLAP ELECTRONIC CONTROL UNIT)
2003
Part: SMOKE DETECTOR — FAULTY (CARGO BAY)
CARGO SMOKE WARNING ON APPROACH, FIRE EXTINGUISHERS ACTIVATED. FOUND NR 1 CARGO SMOKE DETECTOR FAILED. REMOVED AND REPLACED DETECTOR, BOTTLES, AND SQUIBS. (M)