N946CA
Registered owner: EQUITY VENTURES II LLC, CO (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| CIVIL AIR PATROL | Operator | on 2017-09-12 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
VERTICAL BEAM AT F.S. 409+128 RBL 27 CRACKED. VERTIDCAL BEAM AT F.S. 49+128 RBL 18 CRACKED. VERTICAL BEAM AT 409+128 LBL 27 CRACKED. NOTE: ALL BEAMS WERE CRACKED AT THE BOTTOM RIVET REF MAINT LOG PAGES #390153,#390154,#390155.VERTICAL BEAMS WERE REPAIRED I/A/W WVAC EO 601R-53-2838 AND STANDARD CRJ SRM PRACTICES.
ENGINE SUPPORT BEAM AT F.S. 625 L/H WEB CRACKED, R/H SIDE WEB REPAIR INSTALLED PER CUSTOMER REQUEST. ALSO CENTER BEAM, UPPER AND LOWER WEBS CRACKED.PERFORMED A MAJOR REPAIR TO F.S. 625 ENGINE SUPPORT BEAM L/H AND R/H LOWER WEBS IAW REO 601R-53-61-366 REV C. REF MAINT LOG PAGES #390151 AND #390156. PERFORMED TEMPORARY REPAIR TO F.S. 625 ENGINE SUPPORT BEAM CENTER, UPPER AND LOWER WEBS IAW REO 601R-53-61-345 REV B. REF MAINT LOG PAGE #390142.
FLIGHT #6015. DURING TAXI OUT RECEIVED A LEFT WINDOW AND LEFT WINDSHIELD OVERHEAT CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE.COOLED SUN HEATED WINDOWS WITH COLD WATER.
FLOOR EMERGENCY LIGHTING FOR ROWS 9 THROUGH 12 FOUND INOPERATIVE.CLEANED CONNECTOR CONTACTS FOR AFFECTED LIGHTING, OPERATIONAL CHEECK WAS SATISFACTORY.
LEFT INBOARD FLAP, INTERIOR SKIN CHAFFED AT OUTBOARD ACTUATOR BONDING STRAP ATTACH POINT.REPLACED LEFT INBOARD FLAP WITH A SERVICEABLE PART S/N:SB/RJ/027.
RIGHT INBD FORE-FLAP CHAFFED AT IMPACT STRIPS.PERFORMED S/B 601R-57-022.
STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER.
GEAR DISAGREE WARNING, NLG DID NOT RETRACT. REPLACED THE NLG DRAG BRACE ASSY.
STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER.
N.L.G. DID NOT RETRACT. REPLACED THE PSEU.
STALL FAIL CAUTION DURING TAKE OFF. RESET THE STALL COMPUTER.
LEFT ENGINE FAILED DURING CLIMB. TURBINE SEIZED. REMOVED AND REPLACED LEFT ENGINE.
LOUD SQUEAL FROM CABIN DOOR. REPLACED DOOR SEAL.
OVERHEAD EMERGENCY LIGHT AT ROW 4 IS INOPERABLE. DEFERRED MAINT PER MEL.
VERTICAL J-ANGLE INSIDE CBP1 FS 280 LEFT HAND SIDE IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE AND INSTALLED IAW WVAC EO 601R-53-1363.
TOP OF FLOORBEAM CAPS LBL 27, LBL 9, RBL 27, RBL 9 AT FS 280 TO 409 CORRODED BEYOND LIMITS. INSTALLED NEW FLOORBEAM CAPS (P/N 601R31113-67) FROM FS 280 TO FS 409 IAW REO 601R-53-00-027 REV N/C DATED 4 NOV 97.
THE PASSENGER DOOR THRESHOLD ANGLE IS CORRODED AS WELL AS THE ANGLES FORWARD AND AFT OF THE MAIN ANGLE. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED ANGLES BETWEEN FS 310 - FS 349 LBL 42 IAW WVAC EO 601R-53-1361.
FWD J-CHANNEL (P/N 600-34017-351) AT FS 280 CORRODED. REMOVED AND REPLACED FWD J-CHANNEL AT FS 280 IAW WVAC EO 601R-53-1367.
BOTH CLIPS AT FS 280 - LBL 9 ARE CRACKED. REMOVED AND REPLACED CLIPS IAW WVAC EO 601R-53-1364.
FOUND CLIPS AT FS 280 RBL 9 (P/N 601R31113-58) TO BE CRACKED. INSTALLED NEW CLIPS IAW WVAC EO 601R-53-1364.
FOUND FLOOR MEMBER (P/N 600-34017-17) AT FS 280.0 TO BE CRACKED L/1 - .75 INCH TO THE RIGHT OF FLOOR SUPPORT RBL 9.0. REPAIRED FLOOR MEMBER AT FS 280.0 AND RBL 9.0 IAW WVAC EO 601R-53-1366.
SERVICE DOOR ANGLE IS CORRODED (P/N 601R38303-105). REMOVED AND REPLACED CORRODED THRESHOLD ANGLE IAW WVAC EO 601R-53-1360.
ANGLE STIFFENER LOCATED AT THE FORWARD SIDE OF FS 280 AT LBL 9.0 WAS FOUND CRACKED. FABRICATED AND INSTALLED NEW ANGLE IAW WVAC EO 601R-53-1363.
THE FUSELAGE SKIN HAS MULTIPLE DENTS BETWEEN FS 574.0 - FS 621.0 BETWEEN STR 29-23 LHS. PERFORMED A MAJOR REPAIR TO DENTED SKIN BETWEEN FS 574.0 - FS 621.0 STRI 20-23 LHS IAW WVAC EO 601R-53-1357.
FOUND TOP PLATES AT FS 349.00 TO BE CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED TOP PLATES IAW WVAC EO 601R-53-1362 A.
SEAL STRIKER ON PASSENGER DOOR AT FS 310.00 AND 349.00 DAMAGED CONTACT WITH DOOR PINS. REPAIRED IAW REO 601R-52-11-008 REPAIR A.
GEAR DISAGREE WARNING DURING TAKEOFF. REPLACED THE NLG DRAG BRACE ASSY.
LEFT HAND PITOT, STATIC AND AOA HEAT CAUTION MESSAGE. REPLACED THE LEFT ADSHC.
RIGHT WINDSHIELD CRACKED DURING FLIGHT AT 31,000 FEET, DESTINATION IAW. AIRCRAFT DIVERTED TO LIT. REPLACED RIGHT WINDSHIELD.
CABIN DOOR LATCH MESSAGE ON EICAS. DEFERRED DOOR WARNING SYSTEM PER MEL.
RIGHT HAND LOW OIL PRESSURE. REPLACED CRACKED EXHAUST FRAME.
CARGO SMOKE WARNING. REPLACED DAMAGED SMOKE DETECTOR IN CARGO COMPARTMENT.
A 14TH STAGE BLEED AIR DUCT LEAK MESSAGE IFSD. REPLACED THE RT PYLON LEAK SENSOR LOOP.
FLAPS FAILED. RESET FLAP SYSTEM, AIRCRAFT RETURNED TO SERVICE.
FLOOR EMERGENCY LIGHT STRIP TOP COVER BROKEN. REPLACED COVER.
UPPER APU EXHAUST HEAT BLANKET HAS HOLES. REPLACED HEAT BLANKET.
APU EXHAUST DUCT HAS SEVERAL BROKEN TABS. REPLACED DUCT.
FS 718 AND STR 11 (LHS) HAS A CRACK IN THE RADIUS EXTENDING BETWEEN THE FIRST AND SECOND FASTENER HOLE ABOVE STRINGER 11 IN THE FLANGE ATTACHING TO THE SKIN AND A CRACK IN THE DOUBLER ON THE AFT SIDE OF FRAME. FRAME FLANGE REPAIRED IAW WVAC EO 601R-53-0066. DOUBLER ON AFT SIDE OF FRAME REPAIRED IAW EO 601R-53-0068.
FS 718 AND STR 11 (RHS), DISCOVERED DURING 24 MONTH INSPECTION TO HAVE A CRACK IN THE RADIUS EXTENDING BETWEEN THE SECOND AND THIRD FASTENER HOLE ABOVE STR 11 IN THE FLANGE, A CRACK IN THE FLANGE EXTNEDING THROUGH THE FIRST FASTENER HOLE, AND A CRACK IN THE DOUBLER ON THE AFT SIDE OF THE FRAME. FRAME FLANGE FS 718 REPAIRED IAW WVAC EO 601R-53-0067. DOUBLER ON AFT SIDE OF FRAME FS 718 REPAIRED IAW WVAC EO 601R-53-0069.
LOWER APU EXHAUST HEAT BRACKET HAS HOLES. REPLACED HEAT BLANKET.
CARGO DOOR SLIDE BRACKET SUPPORT CRACKED. REPLACED SUPPORT.
LEFT INBOARD ELEVATOR FLUTTER DAMPENER LEAKING. REPLACED FLUTTER DAMPENER.
APU EXHAUST FINGER CLAMP HAS BROKEN AND CHAFED FINGERS. REPLACED CLAMP.
APU EXHAUST SUPPORT DUCT ASSY IS WORN ON INBOARD SIDE. REPLACED DUCT.
ANGLE BRACKET ON REAR PRESSURE BULKHEAD RIGHT AFT SIDE IS CRACKED. REPLACED ANGLE BRACKET.
ANGLE BRACKET ON REAR PRESSURE BULKHEAD, LEFT AFT SIDE IS CRACKED. REPLACED ANGLE BRACKET.
AFTER LANDING RETRACTED FLAPS TO 30 DEGREES, FLAPS INDICATED 30 DEGREES BUT FLAP CAUTION MESSAGE APPEARED. COMPLIED WITH EO 27-045 AD EO 27-046 AD. REMOVED AND REPLACED FLAP HANDLE.
DURING TAXI, AFTER NR 1 ENGINE START, COCKPIT FILLED WITH SMOKE. AIR DUCT BETWEEN LEFT HAND ACM AND HEAT EXCHANGER CAME OFF. REINSTALLED DUCT.
FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP SELECTOR HANDLE.
FLAPS FAILED AFTER TAKEOFF. REPLACED THE LEFT HAND BPSU.
FLAPS FAIL MESSAGE. INSPECTED FLAPS PER AD 98-20-01. NO DEFECTS FOUND.
AFT SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. SECURED WIRING CONNECTOR BETWEEN LIGHT STRIPS.
FLAPS FAIL MESSAGE DURING LANDING. PERFORMED VISUAL INSPECTION OF FLAPS. PERFORMED SELF TEST, CYCLED FLAPS. COULD NOT DUPLICATE.
FLAPS FAIL MESSAGE PRESENT DURING LANDING. REPLACED RIGHT HAND BPSU AND FECU.
FLAP FAIL MESSAGE DURING CRUISE FLIGHT. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.
CONFIG TRIM WARNING. REPLACED THE HORIZONTAL TRIM ACTUATOR.
NOISE FROM CABIN DOOR AREA. REPLACED THE GALLEY DRAIN ASSY.
CABIN DOOR, SERVICE DOOR AND CARGO DOOR WARNINGS. RESET CIRCUIT BREAKERS, CLEARED FAULTS FROM PSEU. SYSTEM TEST SATISFACTORY.
CABIN DOOR WARNING DURING CRUISE AT 26,000 FEET, PERFORMED EMERGENCY DEPRESSURIZATION AS PER QRH LANDED SAFELY AT BMI. REPLACED DEFECTIVE SECTIONS OF DOOR WARNING WIRING HARNESS, WIRE NR MB20C22 AND WIRE NR MB67B22 AT CONNECTOR P1MB.
AFT CABIN OVERHEAD EMERGENCY LIGHT INOPERABLE. REPLACED BULB.
FLAPS FAILED AT 8 DEGREES. REPLACED THE FECU.
APU OIL TEMP CAUTION INDICATION. REPLACED THE OIL COOLER.
PILOTS SIDE WINDSHIELD SHATTERED. REPLACED WINDOW.
WING OVERHEAT WARNING DURING TAKEOFF. DEFERRED NORMAL WING DE-ICE SYSTEM. AIRCRAFT CONTINUED SERVICE ON STANDBY SYSTEM.
LT MLG DISAGREE MESSAGE ON EICAS AFTER LANDING GEAR RETRACTED. TIGHTENED LOOSE SENSOR TARGET ON LT MLG.
AFTER REPLACEMENT OF ENGINE DRIVEN HYDRAULIC PUMP VALVE PLATE BOLTS AS IN VICKERS SERVICE BULLETIN 887055-29-01, HYDRAULIC PUMP LEAKAGE OCCURRED. DISCOVERED HOLE IN PUMP FLANGE O-RING RECESS. REPLACED HYDRAULIC PUMP.
LEFT REVERSER UNLOCK MESSAGE ILLUMINATED. DEFER PER 78-30-1.
UNABLE TO RETRACT GEAR ON TAKEOFF, UPON SELECTION OF GEAR UP, NOSE GEAR ONLY. REPLACED NOSE LANDING GEAR DRAG BRACE, OPERATIONAL CHECK GOOD.
WHITE FLIGHT SPOILER MESSAGE CAME ON AFTER LANDING. REPAIRED LT INBD FLIGHT SPOILER POWER CONTROL UNIT.
FLAPS FAIL MESSAGE ON EICAS. FLAPS WILL NOT OPERATE. REPLACED DEFECTIVE FLEX DRIVE CABLE ON LEFT INBOARD FLAP.
NR 3 HYDRAULIC SYSTEM LOST ALL FLUID IN CRUISE FLIGHT. REPLACED O-RING.
PILOT'S SIDE WINDSHIELD CRACKED. REPLACED WINDOW. PART TOTAL CYCLES, 1,663.
THE NOSE LANDING GEAR DID NOT RETRACT. REPLACED THE NLG DRAG BRACE ASSY.
THE LEFT ENGINE POWER LEVER IS BINDING AND CANNOT BE MOVED TO REVERSE THRUST POSITION. REPLACED THE THROTTLE CONTROL GEARBOX.
LEFT ENGINE N2 VIBRATION WARNING ON EICAS. REMOVED AND REPLACED THE LT ENGINE DUE TO FOD CAUSED BY A DEFECTIVE BORESCOPE PLUG, WHICH SEPERATED AND ENTERED THE ENGINE.
RIGHT ENGINE START MESSAGE ON EICAS. REPLACED THE RIGHT ENGINE START VALVE.
FLAP FAULT MESSAGE ON EICAS, ZERO FLAPS LANDING. COULD NOT DUPLICATE PROBLEM. SYSTEM TEST NORMAL AND ACFT RETURNED TO SERVICE.
ANTI-ICE DUCT MESSAGE AFTER 20 MINUTES OF USE, EICAS INDICATED LT WING. STANDBY SYSTEM OPERATES NORMAL. REPLACED DUCT LEAK SENSORS 527WK, 519WK, 525WK, 515WK.