N8580A
Registered owner: AM PM SERVICES LLC - ALPHA SERIES, IL (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
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.
27 reports on file, 2002-05-24 – 2013-05-22.
Part: OXYGEN MASK — MALFUNCTIONED (CABIN) · airframe 25,325 hrs · 22,393 cycles
PASSENGER OXYGEN MASK AT SEAT 12AB FAILED TO DROP DURING FUNCTIONAL CHECK RE-PACKED MASK AND RE-LATCHED DOOR IAW CRJ 200 AMM 35-21-05. COMPLIED WITH OPERATIONAL TEST OF THE PASSENGER OXYGEN SYSTEM 2 TIMES IAW CRJ 200 AMM 35-20-00-00-710-801. NO DEFECTS NOTED AT THIS TIME.
Part: SMOKE GOGGLES — BROKEN (COCKPIT) · airframe 25,319 hrs · 22,388 cycles
FIRST OFFICER'S SMOKE GOOGLES BROKEN. REMOVED AND REPLACED FIRST OFFICER'S SMOKE GOOGLES AS REQUIRED PER AMM 25-61-00. ALL CHECKS GOOD. OK FOR SERVICE.
Part: DEFIBRILLATOR — UNSERVICEABLE (CABIN) · airframe 25,261 hrs · 22,332 cycles
AED DEFIB MISSING GREEN SAFETY TAB AND ACCESSORY KIT. REPLACED WITH BREAK AWAY WIRE, CHECKS GOOD.
Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 25,259 hrs · 22,330 cycles
RIGHT WING LOWER ACCESS HOLE FOR PANELS 640BB AND 650EB HAVE CORROSION. REPAIRED IAW BOMBARDIER REO 601R-57-21-1919.
Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 25,259 hrs · 22,330 cycles
LEFT WING LOWER WING ACCESS HOLES FOR PANELS 510AB AND 540BB CORRODED. REPAIRED IAW BOMBARDIER REO 601R-57-21-1921.
Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 25,258 hrs · 22,330 cycles
MULTIPLE CHAFES DAMAGES TO THE FORWARD FACE OF THE FS 621 PRESSURE BULKHEAD FROM WL 73.5 TO WL 125.5, LBL 36 TO RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155 AND REO 601R-53-61-4895.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,062 hrs · 22,143 cycles
DURING ROUTINE OPERATIONS AT IND MAINTENANCE FOUND THE FUSELAGE SKIN, STRINGER, AND FRAMES DAMAGED FROM FS 379 TO FS 394 AND BETWEEN S-19L AND S-23L. REPAIRED IAW EA CRJ253-01384 AND ASSOCIATED 8110-3.
Part: CABLE — BROKEN (PAX DOOR) · airframe 24,974 hrs · 22,054 cycles
ON FLIGHT 3747 (DTW TO YUL) THERE WAS AN INCREDIBLY LOUD NOISE FROM MAIN CABIN DOOR ON DEPARTURE. COMMUNICATIONS WITH FLIGHT ATTENDANT ALMOST IMPOSSIBLE DUE TO NOISE. HAPPENS COMING FROM RIGHT SIDE, WORSE AT HIGHER ALTITUDE/AIRSPEED. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT PERFORMED AN AIR RETUN TO DTW WHERE IT LANDED SAFELY. FOUND PAX DOOR FLAPPER DOOR ICE BREAK CABLE BROKEN, INHIBITING FLAPPER DOOR TO CLOSE. REMOVED AND REPLACED FLAPPER DOOR ICE BREAK CABLE IAW AMM 52-11-15. OPS CHECKS GOOD. OK FOR SERVICE.
Earlier reports · 2002–2012 · 19 reports
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,202 hrs · 21,288 cycles
EMERGENCY FLOOR LIGHTING INOPERATIVE ROW 1 THRU 6. REMOVED AND REPLACED LIGHT, OP CHECKED GOOD IAW AMM 33-51-00.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 24,070 hrs · 21,133 cycles
AIRCRAFT REQUIRED EXTREME RIGHT WING DOWN AILERON TRIM AND NOSE LEFT RUDDER TRIM TO FLY STRAIGHT. ALSO AILERON FEEL IN CONTROLS IS VERY SLOPPY OVER 1 INCH OF LATERAL PLAY AT YOKE. CLEANED INBOARD FLAPS. REMOVED AND REPLACED INBOARD FLAP SEAL INSPECTED FLAPS FOR DAMAGE. CHECKED RIGGING IAW AMM 27-54-00-220-801 AND FOUND WITHIN LIMITS. OPS CHECK OF AILERON SYSTEM, NO DEFECTS NOTED IAW AMM 27-11-00-710-203, REFERENCE NON-ROUTINE CARD #N24787.
Part: UNKNOWN — UNKNOWN (AILERONS) · airframe 24,065 hrs · 22,128 cycles
CREW REPORTED AILERONS FELT SLOPPY, OVER 1 INCH OF LATERAL PLAY AT YOKE. PERFORMED OPS TEST OF AILERON CONTROL SYSTEM NO DEFECTS NOTED. CREW REPORTED SLOP WITH TRIM OUT OF CENTER DETENT, NO DEFECTS NOTED IAW AMM 27-11-00-710-803.
Part: A/C PACK — SEIZED (LEFT) · airframe 23,990 hrs · 21,049 cycles
ON FINAL, DETECTED GUN POWDER BURNING ODOR. LEFT PACK CONTROLLER IN AUTO AND MANUAL, TEMP CONTINUED TO RISE ABOVE 100. ON ENTERING THE COCKPIT DISCOVERED THAT THE FLIGHT CREW LEFT THE LEFT PACK SWITCH ON THE "ON" POSITION. FURTHER TROUBLESHOOTING REVEALED THE LEFT PACK TO BE SEIZED. REMOVED AND REPLACED THE LEFT PACK IAW AMM 25-51-05. OPS CHECKS GOOD, DM 67178 CLEARED, PLACARD OFF AND AIRCRAFT OK FOR SERVICE.
Part: BATTERY — UNKNOWN (CABIN) · airframe 23,617 hrs · 20,668 cycles
NR 2 EMERGENCY LIGHT BATTERY RS. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW AMM 33-51-04-04.
Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 23,340 hrs · 20,414 cycles
FLAPS FAIL AT 20 ON FINAL. NO EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY. REPLACED FECU, OP CK GOOD
Part: UPLOCK — MALFUNCTIONED (NLG) · airframe 23,294 hrs · 20,371 cycles
LANDING GEAR DISAGREE ON APPROACH. NOSE GEAR DIDNâT INDICATE DOWN. QRH COMPLETED. REMOVED AND REPLACED NLG UPLOCK ASSY IAW AMM 32-33-05. OP CHECK, LEAK CK GOOD.
Part: TAB — OUT OF ADJUST (CABIN DOOR) · airframe 23,238 hrs · 20,316 cycles
MAIN CABIN DOOR HAS LOUD POPPING NOISE WHEN OPENING AND CLOSING DOOR GETS HUNG UP MOMENTARILY BEFORE OPENING AND CLOSING. MADE DOOR ADJUSTMENTS TO HINGE TABS. OPS CHK NORMAL W/REF TO CRJ AMM 52-11-00. OK FOR SVC.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 23,201 hrs · 20,282 cycles
F/A'S FLASHLIGHT INOP. REMOVED AND REPLACED F/A FLASHLIGHT BATTERY IAW AMM 25-61-02.
2011
Part: PANEL — MALFUNCTIONED (AUTOPILOT SYS) · airframe 22,848 hrs · 19,941 cycles
YAW DAMPER 1 IS JAMMED, WILL NOT DISCONNECT. REMOVED AND REPLACED YAW DAMPER PANEL PER AMM 22-22-04. OPS CK GOOD. OK FOR SERVICE.
Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 20,810 hrs · 18,101 cycles
LARGE DIFFERENCE BETWEEN KNOB AND A HALF WHEN RIGHT T/L BROUGHT TO IDLE WENT TO 150 PPH BEFORE GOING BACK TO 250. PERFORMED HIGH POWER ENGINE RUNS IAW AMM 71-00-00. ALL ENGINE PARAMETERS NORMAL. NO THROTTLE SPLIT NOTED. OK FOR SVC.
Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 22,667 hrs · 19,812 cycles
MEL 28-23-01 RT FUEL PUMP INOP. REMOVED AND REPLACED RT BOOST PUMP IAW AMM 28-23-01. OPC GOOD. THIS CLEARS DM 55293. PLACARD REMOVED. "VERIFIED PART EFFECTIVITY."
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 22,247 hrs · 19,369 cycles
ABORTED TAKEOFF IN LSE DUE TO CONFIG SPOILER WARNING MESSAGE AT APPROX 100 KNOTS AND ALL BRAKES NEVER EXCEEDED 7 ON THE BRAKE TEMPS.
Part: ANGLE — DAMAGED (FUSELAGE) · airframe 21,510 hrs · 18,711 cycles
DAMAGED HOLE IN SPLICE ANGLE AT 3.2 INCH OUTBOARD OF STRINGER 25R AT FS 559. REPAIRED IAW BOMBARDIER REO 601R-53-41-1396.
Part: WIRE HARNESS — DEFECTIVE (PAX DOOR) · airframe 21,373 hrs · 18,587 cycles
PASSENGER DOOR MASTER WARNING AT 33,000. CREW RAN QRH, MESSAGE CLEARED ON DESCENT, DIVERTED TO OMA. MAINTENANCE FOUND BURNT PIN AT P7MB. REPLACED DOOR HARNESS PER 52-70-04, OPS CHECK GOOD.
2010
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,159 hrs · 17,489 cycles
LOWER PASSENGER DOOR SILL AND CLEATS CORROSION. REMOVED AND REPLACED LOWER PASSENGER DOOR SILL AND CLEATS.
Part: TRIM SWITCH — DEFECTIVE (STABILIZER) · airframe 18,991 hrs · 16,287 cycles
STAB TRIM MACH TRIM CAUTION MESSAGES INFLIGHT. REMOVED AND REPLACED STAB TRIM DISENGAGE SWITCH IAW AMM 27-41-30. OPS CHECK GOOD. OK FOR SERVICE.
2006
Part: A/C PACK — LEAKING (RIGHT) · airframe 11,404 hrs · 9,832 cycles
ON TAXI SMOKE APPEARED IN COCKPIT AND CABIN. LEFT ACM WAS ALREADY DEFERRED UNDER MEL RIGHT PACK DEFERRED BY OUTSTATION. LATER INVESTIGATION SUGGEST APU INTERNAL OIL LEAK. RIGHT PACK DEFER CLEARED AND APU DEFERRED PER MEL.
2002
Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT)
AIRCRAFT HAD A LAVATORY SMOKE CAUTION MESSAGE IN FLIGHT. FLIGHT CREW DECLARED AN EMERGENCY AND AN OTHERWISE UNEVENTFUL LANDING WAS MADE. MAINTENANCE PERFORMED A SUCCESSFUL OPERATIONAL CHECK OF THE SMOKE DETECTION SYSTEM IAW APPROVED AMM PROCEDURES.