N949CA

Part: FIRE DETECTOR — MALFUNCTIONED (LT ENGINE) · airframe 350 hrs · 489 cycles

THE PILOT REPORTED A LEFT ENGINE FIRE WARNING ILLUMINATED IN FLIGHT AND SHUT DOWN THE ENGINE ACCORDING TO THE QRH. MAINTENANCE INSPECTED AND REPLACED THE FIRE DETECTOR ASSEMBLY.

Part: MANIFOLD — CRACKED (FUEL DISTRIB) · airframe 31 hrs · 15 cycles

THE PILOT REPORTED DURING TAXI IN FUEL SMELL IN COCKPIT AND ON NACELLE. MAINTENANCE INSPECTED AND FOUND A CRACK IN THE FUEL DISTRIBUTION MANIFOLD PLUG RECEPTACLE. REMOVED AND REPLACED THE RIGHT FUEL MANIFOLD ASSEMBLY, WITH NO FURTHER DEFECTS NOTED.

Part: FIRE WARNING — INTERMITTENT (MAIN DECK CARGO) · airframe 76,533 hrs · 10,714 cycles

DURING CRUISE, THERE WAS AN ERRONEOUS INTERMITTENT MAIN DECK CARGO FIRE WARNING.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 75,514 hrs · 10,454 cycles

LEFT UPPER DECK EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK.

Part: ACCESS PANEL — CRACKED (THRUST REVERSER) · airframe 75,514 hrs · 10,454 cycles

NR 4 ENGINE RT THRUST REVERSER COWL CENTER DRIVE UNIT ACTUATOR ROD END ACCESS PANEL FOUND CRACKED.

Part: ACCESS PANEL — CRACKED (THRUST REVERSER) · airframe 75,514 hrs · 10,454 cycles

NR 1 ENGINE LT TRUST REVERSER BALLSCREW ACCESS PANELS HAS THREE CRACKS.

Part: ACCESS PANEL — CRACKED (THRUST REVERSER) · airframe 75,514 hrs · 10,454 cycles

NR 4 ENG LT THRUST REVERSER UPPER AND LOWER BALLSCREW ACTUATOR ROD END ACCESS PANELS FOUND CRACKED.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 75,514 hrs · 10,454 cycles

BODY FAIRING PANEL NR 294AR INTERIOR SURFACE FOUND CRACKED.

Part: DOOR — CRACKED (ZONE 200) · airframe 75,514 hrs · 10,454 cycles

COCKPIT EMERGENCY ESCAPE DEVICE DOOR CRACKED. CRACK LENGTH .7".

Part: FAIRING — CRACKED (CARGO DOOR) · airframe 75,514 hrs · 10,454 cycles

FORWARD CARGO DOOR AFT HINGE FAIRING CRACKED. CRACK LENGTH .2"

Part: DRIP TRAY — CRACKED (BS 440-460) · airframe 75,514 hrs · 10,454 cycles

MAIN ELECTRICAL CENTER DRIP SHEILD CRACKED AT OTBD FORWARD AND AFT CORNERS STA 440 & 460. REF AD 2011-16-06, S/B 747-25A3588.

Part: DOUBLER — CRACKED (BS 1140) · airframe 75,514 hrs · 10,454 cycles

UPPER DECK TENSION TIE, RT SIDE BS 1140, DOUBLER AND CHORD FOUND CRACKED 2 PLACES. CRACK LENGTH .007" REF AD 2007-23-18, SB 747-53A2507.

Part: SEAT TRACK — CRACKED (BS 1420) · airframe 75,514 hrs · 10,454 cycles

MAIN DECK CARGO COMPARTMENT STA 1420, LBL 11, SEAT TRACK CROWN BOTTOM AREA FOUND GOUGED AND CRACKED. CRACK LENGTH 4".

Part: TENSION TIE — CRACKED (ZONE 200) · airframe 75,514 hrs · 10,454 cycles

UPPER DECK TENSION TIE LT STA 1140 CHORD FOUND CRACKED IN 4 PLACES. CRACK LENGTH .07" REF AD 2007-23-18, S/B 747-53A2507.

Part: SEAT TRACK — GOUGED (BS 1410-1420) · airframe 75,514 hrs · 10,454 cycles

MAIN DECK CARGO COMPARTMENT STA 1410 TO 1420, RBL 11 SEAT TRACK CROWN BOTTOM AREA FOUND GOUGED.

Part: FRAME — CRACKED (BS 1200) · airframe 75,514 hrs · 10,454 cycles

UPPER DECK BS 1200, STRINGER 5 TO 6R FRAME DOUBLER CRACKED. REF AD 2007-23-18, SB 747-53A2507, CRACK LENGTH .13".

Part: SKIN — CHAFED (BS 2300-2598) · airframe 75,514 hrs · 10,454 cycles

FUSULAGE SKIN AT VERTICAL FIN INTERFACE AREA CHAFFED. REF AD 2009-14-02, S/B 747-53A2721.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 75,514 hrs · 10,454 cycles

UPPER DECK TENSION TIE BS 1180, FRAME FOUND CRACKED. CRACK LENGTH .07". REF AD 2007-23-18, SB 747-53A2507.

Part: STRAP — CRACKED (DOOR FRAME) · airframe 75,514 hrs · 10,454 cycles

MAIN DECK RT NR 1 DOOR FWD EDGE FRAME ATTACH STRAP AT LOWER GUIDE ARM CUT OUT AREA FOUND CRACKED.

Part: STRUCTURE — CRACKED (ZONE 200) · airframe 75,514 hrs · 10,454 cycles

BS 2598 RT UPPER AFT INNER CHORD ONE FASTNER HOLE FOUND CRACKED AT AFT INNER CHORD. CRACK LENGTH .030". REF AD 2010-14-07, SB 747-53A2427.

Part: SUPPORT ANGLE — CRACKED (DOOR HINGE) · airframe 75,514 hrs · 10,454 cycles

LOWER AFT CARGO DOOR FWD HINGE SUPPORT ANGLE FOUND CRACKED. CRACK LENGTH .9". GENERATED FROM INSPECTION CARD 52-808-01-01.

Part: ANGLE — CRACKED (BS 400) · airframe 75,514 hrs · 10,454 cycles

LOWER FORWARD CARGO COMPARTMENT AT MAIN ELECTRIC CENTER BS 400, RBL 25, UNDER FLOOR, ANGLE FOUND CRACKED. CRACK LENGTH .8".

Part: SUPPORT — CRACKED (BS 2180-2200) · airframe 75,514 hrs · 10,454 cycles

BULK CARGO COMPARTMENT BS 2180 TO 2200 LBL 20, SUPPORT STRAP FOUND CRACKED. CRACK LENGTH .4" GENERATED FROM INSPECTION CARD 53-862-01-01.

Part: ANGLE — CRACKED (RT MLG DOOR) · airframe 75,514 hrs · 10,454 cycles

RIGHT WING LANDING GEAR INBD STRUT DOOR MOST AFT ANGLE FOUND CRACKED. CRACK LENGTH .4"

Part: SEAT TRACK — CRACKED (BS 1920) · airframe 75,514 hrs · 10,454 cycles

AFT CARGO COMPARTMENT BS 1920, RBL 22 SEAT TRACK FOUND CRACKED. CRACK LENGTH 1.5"

Part: BULKHEAD WEB — CRACKED (BS 2598) · airframe 75,514 hrs · 10,454 cycles

BS 2598, LT LOWER AFT INNER CHORD ONE FASTNER HOLE FOUND CRACKED AT BULKHEAD LOWER WEB. CRACK LENGTH .030" REF AD 2010-014-07, SB 747-53A2427.

Part: ATTACH BRACKET — CRACKED (FIRE BOTTLE) · airframe 75,514 hrs · 10,454 cycles

LOWER BULK CARGO COMPARTMENT RT SIDE - SIDEWALL AREA, FIRE BOTTLE LOWER INBD ANGLE BRACKET AT STA 2063, RBL 44 CRACKED. CRACK LENGTH 1".

Part: DEPRESSOR — CRACKED (CARGO DOOR SEAL) · airframe 75,514 hrs · 10,454 cycles

AFT CARGO DOOR CUT OUT SEAL DEPRESSOR, AFT MID POSITION FOUND CRACKED. CRACK LENGTH 1.5"

Part: SUPPORT — CRACKED (LT MLG FAIRING) · airframe 75,514 hrs · 10,454 cycles

LEFT WING LANDING GEAR INBD STRUT DOOR FAIRING SUPPORT FOUND CRACKED 2 EA PLACES. CRACK LENGTH .5"

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 75,514 hrs · 10,454 cycles

RT HORIZONTAL STABILIZER UPPER SURFACE T/E FIXED PANEL FOUND CORROSION IN AREA OF LOGO LIGHT.

Part: FITTING — CORRODED (ACCESS PANEL) · corrosion level 2 · airframe 75,513 hrs · 10,454 cycles

AIR CONDITION ACCESS PANEL 191 HOLD OPEN ROD PANEL, SIDE FITTING CORRODED.

Part: SKIN — CORRODED (BS 2283) · corrosion level 2 · airframe 75,514 hrs · 10,454 cycles

MAIN ENTRY DOOR L5 DOOR CUT OUT AFT EDGE FOUND CORROSION AT STA 2283.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 75,514 hrs · 10,454 cycles

NR 3 ENGINE THRUST REVERSER FWD TORQUE BOX BULKHEAD AFT SURFACE AT 2 O`CLOCK POSITION ONE BRACKET CRACKED, CRACK LENGTH .7".

Part: ANGLE — CRACKED (DOOR FRAME) · airframe 75,514 hrs · 10,454 cycles

L1 MAIN ENTRY DOOR CUT OUT FWD UPPER CORNER BS 440, STR 16L, ONE ANGLE CRACKED, CRACK LENGTH .8".

Part: PANEL — CRACKED (CONTROL COLUMN) · airframe 75,514 hrs · 10,454 cycles

COCKPIT LT CONTROL COLUMN FORWARD LOWER COMPOSITE CLOSEOUT PANEL FOUND CRACKED.

Part: ANTI-ICE SYSTEM — WARNING LIGHT · airframe 28,230 hrs · 25,001 cycles

FLIGHT 5644 - ANTI-ICE DUCT MESSAGE AFTER TAKEOFF FROM CVG. AIRCRAFT RETURNED TO CVG AND LANDED WITHOUT INCIDENT. INSPECTED FORWARD FUSELAGE LOOPS AND PERFORMED OPS CHECK, CHECKS GOOD (CND).

Part: CIRCUIT BREAKER — MALFUNCTIONED (HYD PUMP) · airframe 27,763 hrs · 24,624 cycles

FLIGHT 5470 - DURING FLAP SELECTION FROM 8 DEGREES, RECEIVED 3B HYD PUMP CAUTION MESSAGE. CREW DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT. FOUND 3B CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER, PERFORMED OPS CHECK PER AMM, NO FURTHER DEFECTS NOTED.

Part: FLAP — MALFUNCTIONED (WING) · airframe 27,239 hrs · 24,229 cycles

FLIGHT 5480 - FLAP FAIL MESSAGE AFTER LANDING IN HSV, FAILED AT 20 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: FLAP — MALFUNCTIONED (WING) · airframe 27,186 hrs · 24,183 cycles

FLIGHT 4997 - FLAP FAIL CAUTION MESSAGE WHILE IN CRUISE FLIGHT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: FLAP — MALFUNCTIONED (WING) · airframe 27,178 hrs · 24,176 cycles

FLIGHT 5296 - DURING APPROACH RECEIVED FLAP FAIL MESSAGE AT 20 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: CAUTION MESSAGE — ILLUMINATED (TE FLAPS) · airframe 27,059 hrs · 24,080 cycles

FLIGHT 5581 - FLAP FAIL CAUTION MESSAGE WHILE SITTING AT GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 26,982 hrs · 24,019 cycles

FLIGHT 5199 - FLAP FAIL CAUTION MESSAGE CAME ON DURING TAXI. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 26,221 hrs · 23,380 cycles

FLIGHT 5130- DURING LANDING AT MSG RECEIVED A FLAP FAIL MESSAGE AT 45 DEGREES. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A ,B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 25,783 hrs · 23,006 cycles

FLIGHT 5903 - EMERGENCY FLOOR LIGHTNING INOPERABLE ROWS 9 TO 13. REPLACED THE EMERGENCY BATTERY.

Part: BULKHEAD — CRACKED (RT WHEEL WELL) · airframe 25,733 hrs · 22,964 cycles

WHILE PERFORMING TASK CRJ-2-162014, DETAILED INSPECTION OF THE PRESSURE BULKHEAD WEBS AND VERTICAL BEAMS AT FS 559.0, TWO CRACKS WERE DISCOVERED IN THE BULKHEAD WEB RADIATING FROM THE HOLES FOR THE ATTACH BOLTS OF THE RIGHT AILERON CONTROL CABLE REAR QUADRANT MOUNT BRACKET AT RBL 23. REPAIRED BULKHEAD WEB PER REO 601R-53-41-260 REV A.

Part: CONTROLLER — MALFUNCTIONED (AVIONICS) · airframe 23,995 hrs · 21,432 cycles

FLIGHT 5147 WING OVERHEAT MESSAGE. REPLACED THE CONTROLLER.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 23,941 hrs · 21,381 cycles

FLIGHT 5198, EMERGENCY FLOOR PATH LIGHTING INOP AT ROW 2 THRU 5. REPLACED WIRE CONNECTOR.

Part: SELECTOR VALVE — UNRELIABLE (NLG) · airframe 23,220 hrs · 20,725 cycles

FLIGHT 5994 GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE.

Part: RESERVOIR — INOPERATIVE (NR 3 HYD SYS) · airframe 23,016 hrs · 20,565 cycles

FLIGHT 5492 GEAR DISAGREE WARNING. REPLACED THE SYSTEM 3 HYDRAULIC RESERVOIR.

Part: COMPUTER — MALFUNCTIONED (MACH TRIM) · airframe 22,406 hrs · 20,078 cycles

FLIGHT 5546 STAB TRIM AND MACH TRIM CAUTION. RESET HSTCU, COULD NOT DUPLICATE, OPERATIONAL CHECK NORMAL.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 20,890 hrs · 18,852 cycles

FLIGHT 5682 RIGHT THRUST REVERSER UNLOCK INFLIGHT. SECURED AND DEFERRED MAINT PER MEL.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 20,760 hrs · 18,754 cycles

FLIGHT 5815 CO-PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 20,652 hrs · 18,670 cycles

THE AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP. SECURED LOOSE WIRING CONNECTION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 20,501 hrs · 18,547 cycles

RT 718 FRAME FLANGE CRACKED BELOW STRINGER 10. REPAIRED FRAME IN ACCORDANCE WITH REO 601R-53-61-193.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 20,501 hrs · 18,547 cycles

PRESSURE FLOOR SKIN HAS CRACK AT FS 461.00. REPAIRED IN ACCORDANCE WITH REO 601R-53-41-102.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 20,501 hrs · 18,547 cycles

PRESSURE FLOOR SKIN HAS CRACK AT FS 461.00. REPAIRED IN ACCORDANCE WITH REO 601R-53-41-102.

Part: IDG — MALFUNCTIONED (LEFT) · airframe 19,397 hrs · 17,653 cycles

FLIGHT 5304 LEFT IDG CAUTION MESSAGE DURING T/O. DEFERRED MAINT PER MEL.

Part: POWER CABLE — INOPERATIVE (CABIN FLOOR) · airframe 17,799 hrs · 16,369 cycles

FLIGHT 5893 EMERGENCY FLOOR PATH LIGHTING IS INOP.REPLACED TRACK LIGHTING POWER STRIPS.

Part: LAMP · airframe 17,318 hrs · 15,987 cycles

FLIGHT 5480 EMERGENCY FLOOR LIGHT AT ROW 3 IS INOP.DEFERRED MAINT PER MEL

Part: LAMP · airframe 17,098 hrs · 15,797 cycles

FLIGHT 5284 1 SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP.DEFERRED MAINT PER MEL.

Part: CART · airframe 16,951 hrs · 15,675 cycles

A/C FUSELAGE STRUCK BY BAGGAGE CART AND SUSTAINED MAJOR DAMAGE BETWEEN F.S. 654 AND 672, AND STRINGERS 21L TO 23L.C/W REPAIR TO SKIN AND STRINGERS I/A/W SRM 53-00-31 AND 53-00-03 AND REO 601R 53-61-577 AND 579.

Part: SEAL — LEAKING (ACC GEAR BOX) · airframe 16,487 hrs · 15,268 cycles

FLIGHT 5298 LEFT ENGINE OIL PRESSURE WARNING AFTER T/O, AIRCRAFT RETURNED TO MSP. (IFSD)REPLACED ACCESSORY GEAR BOX OIL SEALS AT AXIS D&F.

Part: DOOR · airframe 15,772 hrs · 14,657 cycles

FLIGHT 5472 CABIN DOOR WARNING.COULD NOT DUPLICATE OPERATIONAL CHECK OF DOOR NORMAL. NO FAULT CODES IN COMPUTER.

Part: WINDOW — FRACTURED (L/H) · airframe 14,536 hrs · 13,557 cycles

FLIGHT 5903. PILOT'S SIDE WINDOW SHATTERED AT 29,000 FT.REPLACED THE PILOT'S SIDE WINDOW.

Part: ANGLE — CRACKED (FS 484.0 LBL9) · airframe 14,350 hrs · 13,383 cycles

LEFT SIDE INBOARD ANGLE AT F.S. 484.0 LBL 9 UNDER FLOOR PANEL 261CLF IS CRACKED.REPAIRED THE ANGLE AT FS 484.0 LBL9 I/A/W WVAC EO 601R-53-2711A.

Part: ANGLE — CRACKED (FS 484.0 RBL 36) · airframe 14,350 hrs · 13,383 cycles

RIGHT SIDE ELEVATER AND RUDDER PULLEY SUPPORT BRACKET AT F.S. 484.0 UNDER FLOOR PANEL 262DRF IS CRACKED.REPAIRED THE RIGHT SIDE ELEVATER AND RUDDER SUPPORT BRACKET AT F.S. 484.0 I/A/W WVAC EO 601R-53-2711A.

Part: ANGLE — CRACKED (FS 484.0 LBL27) · airframe 14,350 hrs · 13,383 cycles

LEFT SIDE INBOARD ANGLE AT F.S. 484.0 LBL 27 UNDER FLOOR PANEL 261DLF IS CRACKED.REPAIRED THE ANGLE AT F.S. 484.0 LBL27 I/A/W WVAC EO 601R-53-2711A.

Part: CAP — CHAFED (FLAP LEADING EDG) · airframe 14,351 hrs · 13,383 cycles

THE R/H INBOARD FLAP LEADING EDGE VANE CAP MIDDLE SKIN IS CHAFED WHERE THE FLAP CONTACTS THE TEFLON BUMPER PAD.REMOVED THE CHAFED MIDDLE VANE CAP. INSTALLED A NEW CAP (P/N 601R14303-10) IAW AERODESIGN ENGINEERING REPORT NO. 1286-1.

Part: CAP — CHAFED (FLAP LEADING EDG) · airframe 14,351 hrs · 13,383 cycles

THE L/H AND R/H INBOARD FLAP LEADING EDGE INBOARD VANE CAPS ARE CHAFED WHERE THEY CONTACT THE TEFLON BUMPER PADS.REMOVED THE CHAFED INBOARD VANE CAPS. INSTALLED NEW VANE CAPS L/H (601R14303-53S) AND R/H (601R14303-54) IAW WVAC EO 601R-57-2706.

Part: BUSHING — WORN (VERTICAL STAB) · airframe 14,350 hrs · 13,383 cycles

HORIZONTAL STABILIZER RHS VERTICLE BUSHING WORN.REMOVED R/H VERTICAL STAB BUSHING P/N 600-21061 INSTALLED NEW BUSHING ALT P/N 600-21061-7/SB I/A/W CRJ MM 20-26-00-910-803 FINAL REAMED BUSHING 1.50 I/A/W CANADAIR REO 601R-55-11-022 MACHINED BUSHING HAT I/A/W WVAC EO 601R-55-2707.

Part: WEB — CRACKED · airframe 14,137 hrs · 13,189 cycles

ENGINE SUPPORT BEAM LOWER WEB CRACKED ON RIGHT SIDE.PERFORMED A MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER WEB I/A/W CANADAIR REO 601R-53-61-366 REV C.

Part: WEB — CRACKED · airframe 14,137 hrs · 13,189 cycles

ENGINE SUPPORT BEAM LOWER WEB CRACKED ON LEFT SIDE.PERFORMED A MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER NIB I/A/W CANADAIR REO 601R-53-61-366 REV C.

Part: WEB — CRACKED · airframe 14,137 hrs · 13,189 cycles

ENGINE SUPPORT BEAM IS CRACKED ON CENTER OF TOP WEB.PERFORMED A TEMPORARY MAJOR REPAIR TO CRACKED ENGINE SUPPORT BEAM I/A/W CANADAIR REO 601R-53-61-315 REV B.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS SYSTEM) · airframe 13,735 hrs · 12,794 cycles

FLAP FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE IAW AD 98-20-01.

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 13,595 hrs · 12,670 cycles

LEFT ENGINE OIL PRESSURE FLUCTUATING BETWEEN 30 AND 48 PSI. REPLACED THE ACCESSORY DRIVES CARBON SEALS.

Part: BULB — BURNED OUT (CABIN) · airframe 13,523 hrs · 12,603 cycles

EMERGENCY LIGHT AT ROW 5 IS INOP. REPLACED LIGHT BULB.

Part: WARNING SYSTEM — MALFUNCTIONED (PITOT HEAT) · airframe 13,317 hrs · 12,423 cycles

STANDBY PITOT HEAT CAUTION MESSAGE. REPLACED THE NR 3 ADSHC.

Part: SEAL — DAMAGED (PAX DOOR) · airframe 13,100 hrs · 12,231 cycles

LOUD SQUEAL FROM CABIN DOOR AREA. REPAIRED DOOR SEAL NIB DAMAGE I/A/W REO 601R-5211-108.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 13,039 hrs · 12,138 cycles

FRAME WEB DAMAGED AT FS 654.5 BETWEEN STRINGER 21B AND 22B LEFT HAND. CAUSED BY ELECTRICAL ARCING AT APU GROUND CABLE (N1232) . REMOVED DAMAGED FRAME SECTION AND SPLICED IN A NEW SECTION IAW REO 601R-53-61-301.

Part: BATTERY — DISCHARGED (APU) · airframe 13,034 hrs · 12,185 cycles

APU BATTERY AT ZERO VOLTS, APU BATTERY CHARGER IS INTERMITTENT. APU GROUND CABLE ARCHING AT GROUND STUD N1232, WHICH CAUSED SUBSTANTIAL DAMAGE AT FRAME 654.5. REPAIRED DAMAGED FRAME AND RELOCATED GROUND STUD IAW S/B 601R-49-014.

Part: CONNECTOR — LOOSE (CABIN) · airframe 12,822 hrs · 12,006 cycles

SEVERAL EMERGENCY LIGHTS AND SIGNS ARE INOP, FWD CABIN AREA. SECURED LOOSE CONNECTION AT FLOOR TRACK LIGHTING.

Part: TRANSDUCER — FAILED (STALL WARNING) · airframe 12,714 hrs · 11,900 cycles

STALL FAIL CAUTION MESSAGE DURING TAKEOFF, AIRCRAFT RETURNED TO THE GATE. REPLACED THE NR 1 AOA TRANSDUCER.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 12,713 hrs · 11,899 cycles

THE FWD J ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED FWD J ANGLE AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 IAW WVAC EO 601R-53-1681.

Part: FLOORBEAM — DAMAGED (CABIN) · airframe 12,713 hrs · 11,899 cycles

THE OUTBOARD FLANGE OF THE BEAM AT RBL 9.0 AND FS 409 + 8 WAS PREVIOUSLY REPAIRED. THIS EO PROVIDES FOR MODIFYING THE SPLICE ANGLE TO ACCOMODATE THE REPAIR. PERFORMED A MAJOR REPAIR TO THE OUTBOARD FLANGE OF THE BEAM AT RBL 9.0 AND FS 409 + 8 IAW WVAC EO 601R-53-1677.

Part: FLOORBEAM — DAMAGED (CABIN) · airframe 12,713 hrs · 11,899 cycles

DURING ACCOMPLISHMENT OF SB 601R-53-037 REV A, THE I/B FLANGE OF THE FLOORBEAM AT RBL 27.0 FS 409 + 8 WAS FOUND TO HAVE A PREVIOUS REPAIR. PERFORMED A MAJOR REPAIR BY REMOVING EXISTING REPAIR AND INSTALLING A SPLICE ANGLE ON FLOORBEAM RBL 27.0 FS 409 + 8 IAW WVAC EO 601R-53-1683.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 12,713 hrs · 11,899 cycles

THE OUTBOARD FLANGE OF THE FLOORBEAM AT RBL 9.0 AND FS 409+8 WAS PREVIOUSLY REPAIRED. REPAIRED PER WVAC EO 601R-53-1677.

Part: FLOORBEAM — CRACKED (CABIN) · airframe 12,713 hrs · 11,899 cycles

FLOOR MEMBER (P/N 600-34017-17) AT FS 280.0 HAS A CRACK APPROXIMATELY .5 INCH LONG, LOCATED TO THE RIGHT OF FLOOR SUPPORT AT RBL 9.0. REPAIRED PER WVAC EO 601R-53-1672.

Part: SPLICE — MISMANUFACTURED (FUSELAGE) · airframe 12,713 hrs · 11,899 cycles

TWO SPLICE PLATES 601R31030-77 WERE FABRICATED INCORRECTLY BY THE MANUFACTURER. REPAIRED PER WVAC EO 601R-53-1676.

Part: ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 12,226 hrs · 11,471 cycles

STANDBY AIR SPEED INDICATED ZERO DURING TAKEOFF. REPLACED AIR SPEED INDICATOR.

Part: PISTON — LEAKING (NLG) · airframe 12,136 hrs · 11,387 cycles

GEAR DISAGREE, NLG DID NOT RETRACT. REPLACED DEFECTIVE NLG PISTON ASSY.

Part: VALVE — MALFUNCTIONED (RT ENGINE) · airframe 11,934 hrs · 11,217 cycles

RIGHT HAND 14 STAGE BLEED AIR LEAK WARNING. REPLACED THE 14TH STAGE BLEED AIR SHUT OFF VALVE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 11,846 hrs · 11,141 cycles

IAPS DEGRADED MESSAGE. CYCLED AIRCRAFT POWER, MESSAGE CLEARED.

Part: WIRE — BROKEN (CABIN)

RIGHT EMERGENCY EXIT SIGN IS INOPERABLE. REPAIRED BROKEN WIRE AT EXIT SIGN.

Part: SKIN — BENT (BS 349)

FUSELAGE SKIN DAMAGED BY PASSENGER DOOR LOCK PIN AT FS 349.0 STR 16 LHS. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 349.0 STR 16 LHS IAW CRJ REO 601R-53-21-024 REV B.

Part: SKIN — BENT (BS 310)

FUSELAGE SKIN DAMAGED BY PASSENGER DOOR LOCK PIN AT FS 310.0 STR 16 LHS. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 310.0 STR 16 LHS IAW CRJ REO 601R-53-21-160 REVA.

Part: SEAL BRACKET — BENT (BS 310)

PASSENGER DOOR SEAL STRIKER AT FS 310.0 STR 16 LHS DAMAGED BY PAX DOOR LOCK PIN. PERFORMED A MAJOR REPAIR TO PASSENGER DOOR SEAL STRIKER AT FS 310.0 STR 16 LHS IAW CRJ REO 601R-52-11-008 REV B.

Part: SKIN — BENT (PAX DOOR)

PASSENGER DOOR INNER SKIN LOWER O/B CORNER AT FS 310.0 DAMAGED BY HANDRAIL LOCK PIN. PERFORMED A MAJOR REPAIR TO PASSENGER DOOR INNER SKIN AT FS 310.0 IAW CRJ REO 601R-52-11-040.

Part: DETECTOR — MALFUNCTIONED (FUSELAGE)

ANTI-ICE DUCT WARNING. REPLACED BLEED AIR LEAK DETECTION LOOP, RIGHT HAND FUSELAGE AREA.

Part: PANEL — CRACKED (WS 116 - 586.68)

CRACKS WERE DISCOVERED AS A RESULT OF EDDY CURRENT INSPECTION TO FUEL ACCESS OPENINGS 540AB-WS 568.68, 550 AB-WS 163,000, 550CB -WS 209.040, 640EB - WS 116.366, 650AB - WS 163,000, 650CB - WS 209.040, AND 650 GB - WS 294.048. REPAIRED DAMAGE TO AFFECTED AREAS IAW CANADAIR REO 601R-57-21-030.

Part: WIRE — DEFECTIVE (AVIONICS)

PILOTS RA DISPLAY IS INTERMITTENT. REPLACED THE NR 1 RADIO ALTIMETER COAX.

Part: FRAME — CRACKED (BS 718)

FS 718 RIGHT SIDE FRAME AND DOUBLER CRACKED IN RADIUS BETWEEN STR 10-12. REPAIRED FS 718 RIGHT SIDE FRAME AND DOUBLER IAW REO 601R-53-61-193 REV A.

Part: DOUBLER — CRACKED (BS 718)

FS 718 LEFT SIDE DOUBLER CRACKED IN RADIUS. REPAIRED FS 718 LEFT SIDE DOUBLER IAW REO 601R-53-61-193 REV A.

Part: RVDT — FAILED (NLG)

DURING CRUISE, FLIGHT THE STEERING FAIL CAUTION MESSAGE ACTIVATED. REPLACED THE RVDT (RIGHT).

Part: ENGINE — FAILED (RIGHT)

RIGHT HAND ENGINE FAILED AFTER TAKEOFF (IFSD). REPLACED THE RIGHT HAND ENGINE.

Part: CLEAT — CRACKED (BS 484)

CLEAT (P/N 601R31171-009) AT FS 484 RBL 27 HAS AN APPROXIMATELY 0.75 INCH CRACK IN THE RADIUS. PERFORMED A MAJOR REPAIR BY REPLACING CRACKED CLEAT (P/N 601R31171-009) AT FS 484 RBL 27 IAW WVAC EO 601R-53-0312A.

Part: CLEAT — CRACKED (BS 484)

CLEAT (P/N 601R31171-009) AT FS 484 RBL 27 HAS AN APPROXIMATELY 0.75 INCH CRACK IN THE RADIUS. PERFORMED A MAJOR REPAIR BY REPLACING CRACKED CLEAT (P/N 601R31171-009) AT FS 484 RBL 27 IAW WVAC EO 601R-53-0312B.

Part: CLEAT — CRACKED (BS 484)

CLEAT (P/N 601R31171-009) AT FS 484 RBL 27 HAS AN APPROXIMATELY 0.75 INCH CRACK IN THE RADIUS. PERFORMED A MAJOR REPAIR BY REPLACING CRACKED CLEAT (P/N 601R3117-009) AT FS 484 RBL 27 IAW WVAC EO 601R-53-0312B.

Part: PSEU — MALFUNCTIONED (LANDING GEAR)

PROX SYSTEM FAULT MESSAGE. LANDING GEAR WOULD NOT EXTEND. REPLACED THE PSEU.

Part: ACTUATOR — FAILED (LT TE FLAP FLAP)

FLAPS FAILED AT 17 DEGREES WHEN SELECTED FOR LANDING APPROACH. REPLACED DEFECTIVE FLAP ACTUATOR, LEFT HAND OUTBOARD FLAP.

Part: LINKAGE — OUT OF ADJUST (CABIN DOOR)

CABIN DOOR OUTER HANDLE WARNING MESSAGE. ADJUSTED DOOR HANDLE LINKAGE.

Part: WARNING — ACTIVATED (PAX DOOR)

CABIN DOOR OUTER HANDLE CAUTION MESSAGE ON EICAS. INSPECTED DOOR MECHANISM AND FOUND NO DEFECTS. DEFERRED DOOR WARNING SYSTEM PER MEL.

Part: ACTUATOR — FAILED (LT TE FLAP)

FLAPS FAIL MESSAGE AFTER TAKEOFF WHEN FLAPS SELECTED UP. REPLACED DEFECTIVE LEFT HAND OUTBOARD FLAP ACTUATOR.

Part: WARNING — ACTIVATED (PAX DOOR)

CABIN DOOR OUTER HANDLE CAUTION MESSAGE ON EICAS. DEFERRED OUTER HANDLE WARNING SYSTEM AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

FLIGHT ATTENDANT FLASHLIGHT IS INOP. REPLACED BATTERY.

Part: WIRE HARNESS — DEFECTIVE (CABIN)

A PORTION OF THE FLOOR PATH EMERGENCY LIGHTING IS INOP. REPLACED LIGHT ASSY HARNESS.

Part: CONTROL UNIT — MALFUNCTIONED (RIGHT)

ANTI-ICE DUCT WARNING MESSAGE ON EICAS. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE RT BLEED LEAK UNIT FOR TROUBLESHOOTING.

Part: CONTROLLER — INOPERATIVE (AVIONICS BAY)

LEFT SIDE AIR DATA SYSTEM HEAT CAUTION MESSAGE. REPLACED AIR DATA SYSTEM HEAT CONTROLLER, OPERATIONAL CHECK GOOD.

Part: PACKING — DETERIORATED (NR 2 HYD SYST)

NR 2 HYDRAULIC SYSTEM LOW PRESSURE MESSAGE ON EICAS. SYSTEM QUANTITY INDICATES ZERO. REPLACED A DETERIORATED O-RING SEAL ON FILTER DRAIN PLUG. SYSTEM SERVICED AND AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTION — LOOSE (CABIN)

THE FORWARD FLOOR PATH EMERGENCY LIGHTING IS INOP. REPAIRED LOOSE WIRING CONNECTION, FLOOR PATH LIGHTING OPERATES NORMAL.

Part: SERVICE DOOR — OPENED IN FLIGHT (OXY COMPT)

OXYGEN SERVICE DOOR OPENED IN FLIGHT. INSPECTED AND FOUND NO DAMAGE OR DEFECTS WITH SERVICE DOOR. SECURED DOOR AND ACFT RETURNED TO SERVICE.

Part: PITOT — WATER CONTAM (LEFT)

PILOTS AIRSPEED IS FLUCTUATING 20 KNOTS. DRAINED WATER FROM NR 1 PITOT SYSTEM.

Part: DUCT — FAILED (AFT EQUIP BAY)

AT 31,000 FEET CABIN STARTED DEPRESSURIZING RAPIDLY. FOUND AIR CONDITIONING DUCT SEPARATED FROM THE WATER SEPARATOR. REPLACED DUCT.

Part: STALL WARN UNIT — DEFECTIVE (AVIONICS)

AT 37,000 FEET THERE IS A 12 KNOT DIFFERENCE BETWEEN PILOTS AND COPILOTS STALL WARNING SYSTEM. REPLACED THE STALL PROTECTION UNIT.

Part: ACCESS PANEL — NOT SECURED (COCKPIT)

ACCESS PANEL ON LT SIDE OF CENTER INSTRUMENT PEDESTAL CAME LOOSE AND JAMMED RUDDER PEDALS. SECURED THE THREE FASTENERS ON ACCESS PANEL AND ACFT RETURNED TO SERVICE.

Part: WINDSHIELD — SHATTERED (RT COCKPIT)

DURING FLIGHT, RT SIDE WINDSHIELD SHATTERED. REPLACED THE COPILOT'S SIDE WINDSHIELD ASSY.