N423AW

Part: PROXIMITY SENSOR — WARNING MESSAGE · airframe 42,229 hrs · 40,292 cycles

AFTER TAKEOFF RECEIVED GEAR DISAGREE WARNING WHEN SELECTING GEAR UP. APPROX 6 SECONDS AFTER GEAR SELECTION. ALSO RECEIVED NOSE DOOR WARNING MESSAGE. AFTER OPERATING MANUAL RELEASE, RECEIVED A/SKID IB AND PARKING BRAKE SOV. NO ICING, TURBULENCE OR EXCESSIVE MOVEMENT.ALL HYD PARAMETERS WERE NORMAL. WHEN MALFUNCTION OCCURED 1,2, AND 3B WERE IN AUTO. NO EMERGENCY DECLARED ***AIRCRAFT REMOVED FROM SERVICE **** ADJUSTED NLG PROX SENSOR PCF14GA IAW AMM 32-61 OPS CHECK GOOD.

Part: NONE — NONE · airframe 41,692 hrs · 39,778 cycles

GEAR DISAGREE IN FLIGHT DURING CRUISE WHILE LANDING LEVER WAS UP, PER QRH PULLED MANUAL LEVER AND MESSAGES DISAPPEARED. MESSAGE LASTED FOR ABOUT 15SEC, THE NOSE GEAR SHOWED A RED BOX, HYD PRESSURES AND QUANTITY WAS ALL IN GREEN, THERE WERE NO OTHER ASSOCIATED MESSAGES AT THE TIME. AIRCRAFT RETURNED TO THE AIRPORT KIAD ****AIRCRAFT REMOVED FROM SERVICE*** PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSTION AND RETRACTION SYSTEM IAW 32-30-00 OPS TEST GOOD AT THIS TIME.

Part: NONE — NONE · airframe 41,330 hrs · 39,418 cycles

CREW REPORTS SMOKE/HAZE IN CABIN ON TAXI-OUT, ALSO RECEIVED APU OIL PRESS AND APU OIL TEMP CAUTION MESSAGES, ACCOMPANIED BY APU SHUT DOWN. OIL FOUND ON BELLY AND IN ENCLOSURE UPON GATE RETURN. ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESS *****SUPPLEMENTAL INFORMATION****** CREW REPORTS SMOKE/HAZE IN CABIN ON TAXI-OUT, ALSO RECEIVED APU OIL PRESS AND APU OIL TEMP CAUTION MESSAGES, ACCOMPANIED BY APU SHUT DOWN. OIL FOUND ON BELLY AND IN ENCLOSURE UPON GATE RETURN. ***AIRCRAFT REMOVED FROM SERVICE*** FOUND APU OIL COOLER LEAKING. REMOVED OIL COOLER IAW AMM 49-91-07. REF 334869-4 FOR INSTALLATION. INSTALLED OIL COOLER IAW AMM 49-91-07-400-801 OPS AND LEAK CHECK GOOD

Part: CONTROL UNIT — FAILED (FLAP SYSTEM) · airframe 40,786 hrs · 38,851 cycles

DURING APPROACH WHEN SELECTING FLAPS TO 30 DEGREES, RECEIVED A FLAPS FAIL CAUTION MESSAGE. LH FLAP SHOWS 22 DEGREES, RH SHOWS 23 DEGREES. C/W SUPP 98-018I, FLAPS DID NOT RESET ***AIRCRAFT REMOVED FROM SERVICE*** REF WO 305693 MX WC #6-11 FOR ALL WORK PERFORMED "R&R FECU" OPS CHECK GOOD

Part: SEAT TRACK — CORRODED (BS 559 RBL9) · corrosion level 2 · airframe 40,699 hrs · 38,724 cycles

SEAT TRACK AT LAV FS559+80 RBL9 CORRODED. REQUIRES REPLACEMENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK AT FS559+80, RBL 9 IAW REO 601R-53-00-764

Part: BRACKET — DAMAGED (NLG) · airframe 39,624 hrs · 37,621 cycles

DURING T/O SELECTED GEAR UP, GEAR DISAGREE W/ NLG DOOR EICAS MSG, OCCURED DURING BANK, MANUAL RELEASE USED. HYP PUMP AUTO-ON-AUTO- AUTO, APPROX 160 KTS, NORMAL LANDING 45,500 LBS. AIRCRAFT REMOVED FROM SERVICE R/R PROX SENSOR BRACKET BEHIND STRUT AND UNDER UPPER TORQUE LINK AND PERFORM FUNTCTIONAL CK OF LANDING GEAR EXT AND RET IAW AMM 32-20-00 CMM 32-20-32 OPS CK GOOD

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 38,625 hrs · 36,658 cycles

AFTER DEPARTING RIC THE CREW EXPERIENCED A FLAP FAIL CAUTION MESSAGE. THEY ADVISED DISPATCH, DECLARED AN EMERGENCY WITH ATC AND DECIDED TO CONTINUE TO ORD. THEY ADVISED THE FLIGHT ATTENDANT OF THE SITUATION. APPROACH AND LANDING ON 10L WAS NORMAL, ARFF FOLLOWED AIRCRAFT TO THE GATE AS A PRECAUTION. NORMAL TAXI TO THE GATE PIREP: FLAP FAIL CAUTION MESSAGE IN FLIGHT FLAPS FAILED AT ZERO DEGREES C/W QRH LANDED WITHOUT INCIDENT FLAPS FAILED ABOVE 20,000 FEET IN CLIMB.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 38,618 hrs · 36,651 cycles

"RECIEVED FLAP FAIL CAUTION MESSAGE DURING INTIAL CLIMB. FLAPS WERE SET AND INDICATED ZERO" CREW DID NOT DECLARE AN EMERGENCY. AIRCRAFT LANDING WENT WELL THE BTMS WAS READING A LITTLE HIGH. THE BTMS WAS READING "NORMAL" AT 6-8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,497 hrs · 36,544 cycles

LBL27 FLOORBEAM CAP IS CORRODED BETWEEN FS 589 TO FS 605.

Part: BEAM — GOUGED (CARGO DOOR) · airframe 38,497 hrs · 36,544 cycles

DAMAGE FOUND ON FWD LOWER PORTION OF CARGO DOOR BEAM THAT REQUIRES FURTHER INSPECTION. CABLE GOUGED INTO BEAM IN TWO PLACES.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,497 hrs · 36,544 cycles

RT FLOOR SILL IS CORRODED BETWEEN F.S.559+80 TO F.S.559+96.

Part: ANGLE — CRACKED (BS 625) · airframe 38,497 hrs · 36,544 cycles

F.S.625 R/H OBLIQUE ANGLE IS CRACKED

Part: BRACKET — CRACKED (RT MLG WW) · airframe 38,497 hrs · 36,544 cycles

HYDRAULIC LINE BRACKET IN RH WHEEL WELL PRESSURE FLOOR AT F.S.524 RBL 22 IS CRACKED.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 38,497 hrs · 36,544 cycles

PRESSURE TRANSDUCER BRACKETG IN LH WHEEL WELL PRESSURE FLOOR AT F.S.529 LBL 22 IS CRACKED.

Part: POST — CRACKED (FUSELAGE) · airframe 38,497 hrs · 36,544 cycles

FOUND INDICATIONS ON FS 409+128 INBD & OTBD POSTS AT RBL18 AFT FLANGE APPROX. 0.50" LONG, 50% FSH, FAILS NDT.

Part: POST — CRACKED (FUSELAGE) · airframe 38,497 hrs · 36,544 cycles

FOUND INDICATIONS ON FS 409+128 VERTICAL POSTS, BL 0.0, LT & RT AFT FLANGE RADIUS APPROX. 0.50" LONG, 70% & 80% FSH, FAILS NDT.

Part: PULLEY BRACKET — CRACKED (PAX DOOR) · airframe 38,497 hrs · 36,544 cycles

PAX DOOR SUPPORT WHEEL PULLEY BRACKET IS CRACKED.

Part: POST — CRACKED (FUSELAGE) · airframe 38,497 hrs · 36,544 cycles

FOUND INDICATION ON FS 409+128 LBL 18 VERTICAL POSTS INBD & OTBD SIDES AFT FLANGE RADIUS APPROX. 0.50" LONG 50% FSH FAILS NDT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 38,479 hrs · 36,521 cycles

ON INITIAL CLIMB RCVD MULTIPLE INTERMITTENT L ENG OIL PRESS WARNING MSGS. OIL PRESS AND OIL TEMP INDICATONS APPEARED NORMAL. PERFORMED AIR RETURN TO DAY.

Part: GENERATOR — FAILED (APU) · airframe 35,660 hrs · 33,730 cycles

APU GENERATOR FAILED IN FLIGHT DURING CLIMBOUT, COMPLIED WITH QRH, THE APU GEN WOULD NOT RESET, RETURNED TO DEPARTURE. R & R THE APU GENERATOR IAW AMM 24-22-01, OPS AND LEAK CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 35,383 hrs · 33,438 cycles

RECEIVED HYD 1 LO PRESS CAUTION MSG IN FLIGHT. AC PUMP ON, PRESSURE CONTINUED TO FALL. TURNED OFF ACMP AFTER 1 MINUTE OF OPERATION. DIVERTED TO CLT. EDP OPERATED 1 HOUR. QTY SHOWED DASHES. REPLACED EDP1, HYD LINE AND FITTING, SERVICED AND BLED NR 1 HYD SYS OPS & LEAK CHECK GOOD.

Part: FRAME — CORRODED (BS 349) · corrosion level 2 · airframe 35,214 hrs · 33,288 cycles

FRAME BS 349 HAS CORROSION SPOTS ON FWD AND AFT SIDES BETWEEN STRINGERS 26L AND 23R.

Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 35,214 hrs · 33,288 cycles

LEFT INBD FLAP LOWER INBD SKIN SURFACE CORRODED.

Part: FLOOR SUPPORT — CORRODED (BS 303-310) · airframe 35,214 hrs · 33,288 cycles

RT FLOOR SUPPORT CORRODED BS 310 - 303, RBL 41. REPAIRED IAW SRM 51-21-06, 53-21-43, 51-42-10, 51-42-21.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 35,214 hrs · 33,288 cycles

LEFT INBD FLAP VANE LEADING EDGE CHAFED AT CENTER. REPLACED THE FLAP VANE IAW SRM 51-42-13.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 35,214 hrs · 33,288 cycles

LBL9 FLOORBEAM ANGLE CRACKED AT BS 280. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 35,214 hrs · 33,288 cycles

LEFT WING INBD FLAP VANE L/E CHAFED ON INBD SIDE. REPLACED THE FLAP VANE IAW SRM 51-42-13.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 35,214 hrs · 33,288 cycles

RBL 9 FLOORBEAM OTBD ANGLE CRACKED AT BS 280. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 35,214 hrs · 33,288 cycles

LBL 9 FLOORBEAM OTBD ATTACH ANGLE CRACKED AT BS 280. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · corrosion level 2 · airframe 35,214 hrs · 33,288 cycles

FLOOR SUPPORT CORRODED FROM BS 589 TO 621, LBL 27. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-21 AND REO 601R-53-61-3778 REV-A.

Part: INTERCOSTAL — CORRODED (BS 349-364) · corrosion level 2 · airframe 35,214 hrs · 33,288 cycles

INTERCOSTAL CORRODED BETWEEN BS 349 TO 364, STRINGER 25R. REPLACED THE INTERCOSTAL IAW EA CRJ253-00687 REV-IR.

Part: STRUT — DISCHARGED (NLG) · airframe 35,046 hrs · 33,124 cycles

NOSE WHEEL STEERING INOPERATUVE CAUTION MESSAGE INFLIGHT. COMPLIED WITH QRH, MESSAGE REMAINED. DURING CLIMB AT APROX FL 21, NWS WAS ARMED MESSAGE CAME ON AFTER SELECTING OFF MESSAGE WENT OUT. R & R THE TILLER IAW AMM 32-51-01, NO FIX, SERVICED NLG SHOCK STRUT IAW AMM 12-12-32 AND MTCM 000-12-710-002. OPS AND TAXI CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG WW OVERHEAT)

ENROUTE, RECIEVED MLG BAY OVERHEAT WARNING MESSAGE, COMPLIED WITH THE QRH. BTMS INDICATIONS WERE ALL AT 1. LANDED WITHOUT INCIDENT

Part: SERVICE DOOR — STICKS (CABIN) · airframe 33,868 hrs · 32,083 cycles

SERVICE DOOR IS HARD TO OPEN FROM INSIDE AND OUTSIDE. HANDLE OPERATES NORMALLY, DOOR HARD TO PULL FROM AIRFRAME.

Part: APU — SEIZED (APU BAY) · airframe 33,418 hrs · 31,644 cycles

APU LOW OIL PRESSURE CAUTION INFLIGHT FOLLOWED BY APU FAULT CAUTION MESSAGE, FOLLOWED BY APU AUTO SHUTDOWN. CHECKED APU ECU FAULT CODE HOT SHUTDOWN, 92. VERIFIED APU IS SEIZED AND WOULD NOT TURN REF 288966/3 FOR MEL.

Part: NOT REPORTED — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 33,031 hrs · 31,289 cycles

EMERGENCY LIGHTS IN COCKPIT & CABIN ILLUMINATE FOR APPROX 1 SECOND THEN GO OUT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,697 hrs · 30,992 cycles

DURING PRE-FLIGHT INSPECTION, FIRST FLIGHT OF THE DAY, CREW REPORTS ORANGE STRIP EMER LIGHTS BY ROW 1 WOULD NOT ILLUMINATE.

Part: DOOR SEAL — DEFECTIVE (SERVICE DOOR) · airframe 32,027 hrs · 30,353 cycles

PILOT REQUESTED OPERATIONAL INSPECTION OF THE SERVICE DOOR DUE TO FLIGHT ATTENDANT REPORT THAT THE SERVICE DOOR WAS DIFFICULT TO OPEN & CLOSE. INSPECTED SERVICE DOOR, FOUND DOOR OUT OF RIG, RIGGED SERVICE DOOR IAW AMM 52-41-00. RIG WITHIN LIMITS, DOOR OPENS & CLOSES, STILL HARD TO OPEN & CLOSE. R & R SERVICE DOOR SEAL IAW AMM 52-41-07 & SUPP 11-027. PERFORMED OPERATIONS CHECK & LEAK CHECK IAW AMM 52-41-07. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 31,429 hrs · 29,761 cycles

FLIGHT 3981 AT 28000 FT, PAS OX 1 ON CAUTION MSG & ALL PAX O2 MASKS AUTO DEPLOYED. CABIN ALTITUDE 3800, PRESS DIF 8.1. MASKS DID NOT DEPLOY SEAT ROW 1AC & 10AC. REPACKED PAX O2 MASKS IAW AMM 35-21-09. PERFORMED DROP TEST IAW AMM 35-20-00. OPERATIONS CHECKED GOOD. INTERROGATED MDC NO FAULTS FOUND. PERFORMED FUNCTION CHECK OF CPC IAW AMM 21-31-16. NO DEFECTS NOTED. ACFT OK FOR SERVICE AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,864 hrs · 29,212 cycles

REAR CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP. OPS CHECKED GOOD.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 30,675 hrs · 29,041 cycles

PAX DOOR OUTER HANDLE HAS A CRACK NEAR THE LOCK HOLE & THE FLAPPER ALSO IS CRACKED.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 27,405 hrs · 26,467 cycles

PAX DOOR AFT VENT PANEL SUPPORT HAS A CRACK AT BOTTOM RIVET.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 30,675 hrs · 29,041 cycles

FS 409+128, LBL 27 STIFFENER HAS A CRACK IN AFT LOWER INBD CORNER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 30,675 hrs · 29,041 cycles

FS 280.00, STRINGER 3L INBD CLIP IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,675 hrs · 29,041 cycles

LEFT 484 INBD & OTBD CLIPS ARE CRACKED.

Part: STIFFENER — CRACKED (FUSELAGE)

FS 409+128, RBL STIFFENER HAS CRACK IN AFT LOWER OTBD CORNER.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,675 hrs · 29,041 cycles

LEFT UPPER OBLIQUE ANGLE CRACKED ON AFT 621 BULKHEAD.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 30,675 hrs · 29,041 cycles

CHANNEL AT BASE OF FWD CARGO DOOR TRACK IS CRACKED.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 30,675 hrs · 29,041 cycles

CARGO DOOR AFT LOWER CORNER FRAME CRACKED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,675 hrs · 29,041 cycles

PASSENGER DOOR LOWER SILL HAS CORROSION INBD & OTBD SIDES.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 30,675 hrs · 29,041 cycles

FS 409+128, LBL 18 STIFFENER HAS CRACK IN AFT LOWER OTBD CORNER.

Part: SKIN — DENTED (TE FLAP) · airframe 30,675 hrs · 29,041 cycles

DENT IN LOWER SKIN OF THE LT INBD FLAP.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 30,675 hrs · 29,041 cycles

STIFFENER CRACKED IN RT WW AT WS 48.

Part: FITTING — CHAFED (FUSELAGE) · airframe 30,675 hrs · 29,041 cycles

FORWARD & AFT PULL IN LEVER CAM FITTINGS ARE CHAFED AT PAX DOOR CUT OUT.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 30,675 hrs · 29,041 cycles

STIFFENER IN LT WW AT WS48 IS CRACKED.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 30,675 hrs · 29,041 cycles

CTR VERTICAL STIFFENER CHAFED AFT OF FS 621 BULKHEAD AT BL 0.00.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 30,675 hrs · 29,041 cycles

MOUNTING BRACKET FOR 1 HYD SYS FILTER MANIFOLD IS CRACKED.

Part: POST — CRACKED (FUSELAGE) · airframe 30,675 hrs · 29,041 cycles

RBL 27 VERTICAL POST CRACKED AT FS 409+128 BULKHEAD.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,675 hrs · 29,041 cycles

FLOOR SUPPORT CROSSBEAM FS 349 AT RBL 29 - RBL 41 CORRODED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,675 hrs · 29,041 cycles

SERVICE DOOR LOWER SILL SUPPORT ANGLE CORRODED.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 30,349 hrs · 28,734 cycles

EMERGENCY LIGHT, LT SIDE OF SERVICE DOOR INOPERATIVE. FOUND WIRE PULLED FROM CONNECTOR. REPAIRED WIRE IAW ESPM 20-16. OPERATIONS CHECKED GOOD.

Part: CONTROLLER — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 29,806 hrs · 28,216 cycles

IN STANDBY, WING OVERHEAT MASTER WARNING AFTER TAKEOFF, BOTH WINGS. COMPLIED WITH QRH, MSG CLEARED, NORMAL CONTROL ON MEL. DECLARED EMER & DIVERTED. R & R WING ANTI-ICE CONTROLLER IAW AMM 30-12-00. OPERATIONS CHECKED & RAN ACFT WITH CREW, STBY MODE WORKS NORMAL. NORMAL MODE STILL INOPERATIVE & ON MEL.

Part: ENGINE — FAILED (LEFT) · airframe 29,648 hrs · 28,074 cycles

CLIMBING THRU 19,000 FEET, HEARD A LOUD THUD & LT ENGINE N2 WENT TO ZERO. COMPLIED WITH QRH, ENGINE SHUTDOWN, DIVERTED. OIL PRESSURE AT ZERO.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 28,476 hrs · 26,968 cycles

CAPTAIN'S SIDE WINDOW OUTER PANE SHATTERED AT FL 280. EMERGENCY DECLARED & FLIGHT DIVERTED TO BOS. R & R CAPTAIN`S SIDE WINDOW IAW AMM 56-12-01. WINDOW ELEC CHECK GOOD. RAN PRESSURIZATION CHECK TO .4 DP IAW 21-31-00. PRESSURIZATION & LEAK CHECKED GOOD. SN OFF 01344H4909 & SN ON 13312H5433.

Part: UPLOCK — FAULTY (LT MLG) · airframe 27,241 hrs · 25,764 cycles

3856 ON TAKEOFF, GEAR DISAGREE RED WARNING. LT MLG HAD RED DASHES, COMPLIED WITH QRH PROCEDURE. AFTER QRH COMPLETION ALL GEAR INDICATED DOWN & 3 GREEN, RETURNED TO ORF, DID NOT LAND OVERWEIGHT. R & R LT UP LOCK ASSEMBLY MLG OPERATIONS CHECKED GOOD & NO LEAKS NOTED IAW AMM 32-32-05.

Part: RECEPTACLE — CRACKED (GROUND POWER) · airframe 26,193 hrs · 24,739 cycles

ACFT GROUND POWER RECEPTACLE PLUG STRUCTURE IS CRACKED. R & R RECEPTACLE PLUG STRUCTURE.

Part: ATTACH FITTING — CORRODED (NLG DOOR) · airframe 26,193 hrs · 24,739 cycles

CORROSION FOUND UNDER NLG FOLLOW UP DOOR LEFT ATTACH FITTING. REMOVED CORROSION ACCOMPLISHED CUT OUT INSTALLED DOUBLER SHIM AND FILLER 2 EA ANGLES.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 26,193 hrs · 24,739 cycles

CARGO DOOR HANDLE HOUSING CRACKED. R & R CARGO DOOR HANDLE ASSY IAW 200 51-42-02.

Part: ANCHOR — CRACKED (CARGO DOOR) · airframe 26,193 hrs · 24,739 cycles

CARGO BAY DOOR MIDDLE ANCHOR PLUG PLANK HAS CRACK ON FWD INBD CORNER. R & R CARGO BAY MIDDLE ANCHOR RING PLATE IAW SRM 51-42-06.

Part: VANE — CHAFED (TE FLAP) · airframe 26,193 hrs · 24,739 cycles

CHAFED L/E ON RT INBD FLAP VANE. R & R INBD & CTR L/E IAW SRM 51-40-11 & SRM 51-42-13.

Part: PLATE — DAMAGED (FUSELAGE) · airframe 26,193 hrs · 24,739 cycles

PAX DOOR FWD ANCHORS FWD PLATE IS MISDRILLED. R & R PLATE WITH NEW SERVICEABLE.

Part: ACCESS PANEL — CHAFED (NACELLE) · airframe 26,193 hrs · 24,739 cycles

LEFT UPPER NOSE ACCESS COWL 432AT CHAFE IN SEVERAL SPOTS ALONG T/E. R & R WITH NEW SERVICEABLE IAW CMM 71-14-01.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 26,193 hrs · 24,739 cycles

LEFT INBD FLAP HAS A DENT ON THE INBD T/E LOWER SIDE. REPAIR NR 3 OF SRM 57-22-00 NON FLUSH SKIN REPAIR.

Part: SUPPORT ANGLE — CRACKED (DOOR FRAME) · airframe 26,193 hrs · 24,739 cycles

CARGO BAY DOOR LOWER SEAL HAS 2 FWD SUPPORT ANGLES CRACKED UNDER SEAL PLATE. REMOVED ANGLES AND REPLACED WITH NEW SERVICEABLE ANGLES.

Part: SEAT TRACK — CHAFED (BS 552) · airframe 26,193 hrs · 24,739 cycles

LEFT SIDE SEAT TRACK HAS CRACK NEAR FS 552. BLENDED CHAFE TO SMOOTH CONTOUR IAW REO 6014R-53-41-1708.

Part: BULKHEAD — CRACKED (BS 280) · airframe 26,193 hrs · 24,739 cycles

BULKHEAD FS 280 AT RBL 9 CRACKED ON UPPER FLOOR ANGLE. REPAIRED IAW REO 601R-53-11-137, REV A.

Part: ANGLE — CRACKED (BS 280) · airframe 26,193 hrs · 24,739 cycles

INBD AND OTBD ANGLES AT RBL 9 AND LBL 9 ARE CRACKED AT FS 280. ALL ANGLES INBD AND OTBD AT RBL 9 AND LBL 9 AT FS 280. R & R IAW SRM 51-42-21.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 26,193 hrs · 24,739 cycles

CARGO DOOR SUPPORT BEAM HAS A CRACKED SUPPORT ANGLE AT THE 621 BULKHEAD AT THE BOTTOM OF THE BEAM. R & R WITH SERVICEABLE PART IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 574) · airframe 26,193 hrs · 24,739 cycles

ANGLE CRACKED AT FS 574 RBL 9. R & R ANGLE AT FS 574, RBL 9.

Part: SEAT TRACK — CHAFED · airframe 26,193 hrs · 24,739 cycles

RT SIDE SEAT TRACK HAS CHAFE AT FS 424. REMOVED UNSERVICEABLE SECTION OF RT SIDE SEAT TRACK BETWEEN FS 409+110 AND FS 489. FABRICATED AND INSTALLED NEW SERVICEABLE SEAT TRACK OF RT SIDE SEAT TRACK IAW SRM 51-50-11 & AMM 53-01-11.

Part: BULKHEAD — CHAFED (BS 280) · airframe 26,193 hrs · 24,739 cycles

RT AFT FS 280 BULKHEAD SKIN AND RIVET HANDS HAVE CHAFE DAMAGE. REPAIRED DAMAGE WITH SKIN CUT OUT AND DOUBLER INSTALLATION IAW REO 601R-53-11-1727, REV E.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 26,193 hrs · 24,739 cycles

CORROSION FOUND AT FS 364 ON END OF SEAT TRACK FOUND TO BE OUT OF LIMITS. R & R WITH SERVICEABLE SEAT TRACK.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 26,193 hrs · 24,739 cycles

RIGHT OTBD FLOORBEAM ANGLE AT FS 484 IS CRACKED. REPAIRED RT OTBD FLOORBEAM IAW REO 601R-53-41-059, REV B.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,193 hrs · 24,739 cycles

AFT DRAG ANGLE ON PASSENGER DOOR IS CRACKED BY DOOR ASSIST MOTOR CABLE PULLER BRACKET. REPAIRED IAW REO 601R-53-11-513, REV A.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 24,064 hrs · 22,701 cycles

APPLICATION OF TAKE OFF POWER, FELT VIBRATION IN AIRFRAME FOLLOWED BY LT ENGINE LOW OIL PRESSURE CAS MESSAGE. ABORTED TAKE OFF AT LESS THAN 20 KTS. PULLED ACFT OFF RUNWAY, NOTICED ITT WAS FULL SCALE AND N1 AND N2 VIB MESSAGES APPEARED. LEFT ENGINE REPLACEMENT COMPLIED WITH CLEANING OF OIL CONTAMINATED DUCTING FOR RIGHT PACK IAW AWAC SPP 07-037A, OPS CHECKS GOOD.

Part: SHAFT — CRACKED (IDOOR HANDLE) · airframe 24,020 hrs · 22,668 cycles

SERVICE DOOR OUTER HANDLE WILL NOT STOW FROM OUTSIDE OR INSIDE. INSPECTED SERVICE DOOR FOUND OUTER HANDLE SHAFT CRACKED. DOOR OPERATES PROPERLY FORM INSIDE REF LP 228429/4 FOR MEL.

Part: ACTUATOR — MALFUNCTIONED (MLG) · airframe 22,581 hrs · 21,256 cycles

ON DEPARTURE, WHILE GEAR WAS IN TRANSIT, RECEIVED INBD ANTI-SKID MESSAGE, FOLLOWED BY GEAR DISAGREE WARNING. MESSAGE CLEARED WITHIN 20 SECONDS OF GEAR UP SELECTION. HAD NO RED GEAR INDICATION. BOTH MESSAGES CLEARED WITHOUT CREW ACTIONS. NO FURTHER INDICATIONS. TROUBLESHOT AND FOUND THAT DURING GEAR SWING, LT SIDE STAY SHOWS DOWNLOCK. STILL ENGAGED EVEN THOUGH THE GEAR IS SWINGING. SUSPECT BAD LT SIDE STAY. R & R LT SIDE STAY ACTUATOR, OPS CHECKED GOOD, REF AMM 32-32-01, AWAC SUPPLEMENT 11-015.

Part: PRIORITY VALVE — MALFUNCTIONED (MLG) · airframe 22,580 hrs · 21,254 cycles

AT 400 FT GEAR INTRANSIT, INBD AS MESSAGE APPEARED THEN GEAR DISAGREE WITHIN 10 SECONDS OF INITIAL GEAR UP SELECTION. NO RED INDICATIONS. BOTH MSGS CLEARED WITHOUT CREW ACTION. NORMAL EXTENSION AND NORMAL LANDING. NO INDICATIONS NOW. TROUBLESHOT AND R & R NLG PRIORITY VALVE AND PERFORMED LEAK CHECK AND MULTIPLE EXTENSION AND RETRACTION CHECKS IAW AMM 32-32-00 & 32-33-00. ALL CHECKS GOOD.

Part: HANDLE — DEFECTIVE (SERVICE DOOR) · airframe 22,535 hrs · 21,218 cycles

SERVICE DOOR HARD TO OPEN AND CLOSE FROM OUTSIDE. REMOVED AND REPLACED OUTER SERVICE DOOR HANDLE, CLEANED DOOR SEAL AND FRAME IAW AMM 52-41-03, OPS CHECK GOOD.

Part: SCISSOR LINK — DISCONNECTED (NLG) · airframe 22,365 hrs · 21,040 cycles

ON TAKE OFF RECEIVED A GEAR DISAGREE, NOSE GEAR WANRING WOW CAUTION AND NWS CAUTION, COMPLIED WITH QRH ALL MESSAGES CLEARED EXCEPT FOR WOW. GROUND CREW REPORTED SCISSORS DISCONNECTED. PERFORMED GVI OF NOSE GEAR, NOSE WHEEL WELL, AND NOSE TIRES. INSPECTED NOSE GEAR SCISSOR LINKS IAW AMM 32-21-10-02, CREW PERFORMED HIGH SPEED TAXI CHECK. NO DEFECTS NOTED.

Part: SEAL — LEAKING (CARGO DOOR) · airframe 21,523 hrs · 20,151 cycles

CLIMBING THROUGH FL 250, RECEIVED CABIN ALTITUDE CAUTION MESSAGE FOLLOWED IMMEDIATELY BY CABIN ALTITUDE WARNING. INITIATED TO FL 100 PERFORMED ALL APPROPRIATE CHECKLIST. DECLARED EMERGENCY AND LANDED. TROUBLESHOT SYS TO PRIMARY OUTFLOW VALVE BLEEDING AIR WHEEL CLOSED. PRIMARY OUTFLOW VALVE FOUND TO BE SERVICEABLE. ROOT CAUSE: CARGO DOOR SEAL.

Part: BRACKET — CRACKED · airframe 21,801 hrs · 20,438 cycles

HYDRAULIC BRAKE SYSTEM NR 3 BRAKE ACCUMULATOR FWD BRACKET CRACKED. R & R BRACKET IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 559-612) · corrosion level 2 · airframe 21,801 hrs · 20,438 cycles

SEAT TRACK LBL 27, FS 559+112 TO 621 HAS CORROSION AT THE NUTPLATE HOLES. REMOVED AND FABRICATED SEAT TRACK . INSTALLED NEW SEAT TRACK AT IAW REO 601R-53-61-3778, REV.

Part: RIB — CRACKED (RT WING)

RT MLG BATT RIB CRACKED. REPAIR IAW REO 601R-57-51-046.

Part: BRACKET — CRACKED (BS 510) · airframe 21,801 hrs · 20,438 cycles

RT WHEEL WELL INBD OTBD HYD LINE BRACKETS 2 EA CRACKED. R & R WITH 2 EA SERVICEABLE BRACKETS IAW SRM 51-42-06.

Part: CARGO TRACK — CORRODED (BS 559-620) · corrosion level 1 · airframe 21,801 hrs · 20,438 cycles

CARGO TRACK CORRODED. REMOVED UNSERVICEABLE AND INSTALL SERVICEABLE.

Part: WEB — CRACKED (PAX DOOR) · airframe 21,801 hrs · 20,438 cycles

PAX DOOR AFT STAIRCASE WEB CRACKED AT SECOND STEP CUTOUT DAMAGED AREA ON AFT STAIRCASE THEN FABRICATED AND INSTALLED NEW PARTS IAW REO 601R-52-11-702, REV C.

Part: BRACKET — CRACKED (BS 625) · airframe 21,801 hrs · 20,438 cycles

LEFT WHEEL WELL INBD HYDRAULIC LINE BRACKET CRACKED. REPLACED WITH SERVICEABLE BRACKET IAW SRM 51-42-06.

Part: BULKHEAD — CRACKED (BS 559) · airframe 19,865 hrs · 18,456 cycles

CRACK INDICATION AT WL 58.70 AND RBL9 REO601R5341260 REV E TO BE ACCOMPLISHED IAW AWAC JC 4MFG50672 AND 601R5341609 REV B AS NEEDED. REPAIRED CRACK ON FS 559 BULKHEAD AT WL 58.70 AND RBL 9 BY INCOPR OF REO 601R-53-41-260 REV E AND REO 601R-53-41-609, REV B7 DEVIATION E TO RT SIDE ONLY RBL9-27.

Part: BRACKET — WORN (RT WING) · airframe 19,865 hrs · 18,456 cycles

STUB FAIRING (RT) ATTACH BRACKET ON WING IS WORN. R & R RT STUB FAIRING ATTACH BRACKET ON WING IAW SRM 51-42-21.

Part: SKIN — DENTED (RT WING) · airframe 19,865 hrs · 18,456 cycles

RT WING L/E MIDDLE SECTION, IS DENTED AT THE CTR. REFORMED DENT TO CONTOUR BY PUSHING DENT IAW SRM 57-41-31. DENT MEASURES 1.5 IN L X 1.0 IN W X .004 IN.

Part: ACTUATOR — MALFUNCTIONED (YAW DAMPER) · airframe 17,778 hrs · 16,269 cycles

UNCOMMANDED RUDDER DEFLECTION IN FLIGHT, YAW DAMPNER 1 DISENGAGED. NO FURTHER UNCOMMANDED MOVEMENTS. R & R LT YAW DAMPNER LINEAR ACTUATOR. RIGGING AND OPS TEST GOOD REF AMM 22-22-01.

Part: FCU — MALFUNCTIONED (NR 1 ENGINE) · airframe 17,374 hrs · 15,878 cycles

ENG NR 1 W/N GO ABOVE 71.3 PERCENT N1 ON TAKEOFF POWER. ABORTED TAKEOFF BELOW 80 KTS, BRAKE TEMPS 2-2-2-2. SELECTED ENG SPEED CONTROL SYS OFF. C/W ENG RUNS WITH CREW ASSISTANCE BOTH ENGINES ENG RUNS WITH CREW ASSISTANCE BOTH ENGINES MADE AND SUSTAINED POWER OF THE DAY. REF 186989/2 FOR MEL. REMOVED AND REPLACED ENGINE NR 2 FUEL CONTROL UNIT IAW 73-21-03. (K)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 17,115 hrs · 15,637 cycles

CLIP AT FS 484.00, LBL 27.00 CRACKED. CLIP AT FS 484.00, LBL 27.00, REPLACED IAW SRM 200 51-42-21 AND 51-42-06. (K)

Part: ATTACH FITTING — CRACKED (FS 484) · airframe 17,115 hrs · 15,637 cycles

UNDERFLOOR FS 484.00 AND LBL 36.00 CLIP CRACKED. UNDER FLOOR FS 484 AND LBL 36 REPAIRED IAW REO 601R-53-41-059 REV A. (K)

Part: BRACKET — CRACKED (LT TAIL PIPE) · airframe 17,115 hrs · 15,637 cycles

LT TAIL PIPE FAIRING FWD BRACKET OF COVER ASSY CRACKED. LT TAIL PIPE FAIRING FWD BRACKET OF COVER ASSY. REPLACED IAW SRM 51-42-06. (K)

Part: SEAT — CRACKED (COCKPIT) · airframe 17,115 hrs · 15,637 cycles

BACKREST ASSY 210 LT AND 230 RT OF CO-PILOT SEAT CRACKED. BACKREST ASSY 210 LT AND 230 RT OF COPILOT SEAT REPLACED IAW SRM 51-42-10. (K)

Part: SEAL — CRACKED (SPOILERS) · airframe 17,115 hrs · 15,637 cycles

RT FLIGHT SPOILER SURFACE OTBD METAL SEAL CRACKED. RT FLIGHT SPOILER SURFACE OTBD METAL SEAL REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)

Part: ANGLE — CRACKED (PAX DOOR) · airframe 17,115 hrs · 15,637 cycles

PAX DOOR ASSIST MOTOR LOWER ANGLE (WHEN DOOR OPEN) CRACKED .500 INCH. PAX DOOR ASSIST MOTOR LWR ANGLE (WHEN DOOR OPEN) REPLACED IAW SRM 51-42-06. (K)

Part: BULKHEAD — CRACKED (BS 202) · airframe 17,115 hrs · 15,637 cycles

FWD PRESSURE BULKHEAD IS CRACKED AT FS 202.75, LBL27.5, WL 69.00 AND QTY 1 ELONGATED HOLE EXISTS IN WEB AND STIFFNER FS 202.75, LBL 9.00, WL 69.00. FWD PRESSURE BULKHEAD REPAIRED AT FS 202.75, WL 69.00 AND QTY 1 ELONGATED HOLE REPAIRE IN WEB AND STIFFNER FS 202.75, LBL 9.00, WL 69.00 IAW REO 601R-53-11-1174. (K)

Part: BRACKET — CRACKED (BS 621) · airframe 17,115 hrs · 15,637 cycles

BRACKET CRACKED AT FS 621, AFT OF PRESSURE BULKHEAD, NEAR STR 14 LT BRACKET AT FS 621, AFT OF PRESSURE BULKHEAD, NEAR STR 14 LT REPAIRED IAW REO 601R-53-61-100 AND REO 601R-53-61-422. (K)

Part: BRACKET — CRACKED (BS 621) · airframe 17,115 hrs · 15,637 cycles

BRACKET CRACKED AT FS 621, AFT OF PRESSURE BULKHEAD, NEAR STR 14 RT BRACKET AT FS 621 AFT OF PRESSURE BULKHEAD, NEAR STR 14 RT REPAIRED IAW REO 601R-53-61-100 AND REO 601R-53-61-422. (K)

Part: ANGLE — CRACKED (PRESSURE BLKHEAD) · airframe 17,115 hrs · 15,637 cycles

PRESSURE BULKHEAD LOWER FRAME CAP ANGLE IS CRACKED IN THE RADIUS. PRESSURE BULKHEAD LOWER FRAME CAP ANGLE REPAIRED IAW REO 601R-53-41-1022 AND REO 601R-53-41-260, REV C. (K)

Part: RETAINER — CORRODED (E/E DOOR) · corrosion level 2 · airframe 17,115 hrs · 15,637 cycles

MAIN AVIONICS DOOR SEAL RETAINERS CORRODED. MAIN AVIONICS DOOR SEAL RETAINERS REPLACED IAW SRM 51-42-06. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,115 hrs · 15,637 cycles

UPPER AFT ANGLE AT FS 280.00, LBL 11.00, WL 72 IS CRACKED. UPPER AFT ANGLE AT FS 280.00, LBL 11.00, WL 72 REPAIRED IAW REO 601R-53-11-138. (K)

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 17,115 hrs · 15,637 cycles

AFT PRESSURE BULKHEAD WEB IS CRACKED ABOVE CARGO DOOR TRACK AT F/S 621.0, LBL 27, WL 130, REO 601R-53-61-1541 REV B CARRIED OUT. (K)

Part: FLOOR SUPPORT — CRACKED (BS 605) · airframe 17,115 hrs · 15,637 cycles

FLOOR EDGE MEMBER CRACKED AT FS 605, LBL 45, WHERE RIVET ATTACHED TO FLOORBEAM. (CRACK LENGTH .250 INCH) FLOOR EDGE MEMBER REPAIR AT FS 605, LBL 45 IAW REO 601R-53-61-433. (K)

Part: SILL — CORRODED (BS 574) · airframe 17,115 hrs · 15,637 cycles

CARGO BAY FLOOR SILL IS CRACKED AT FS 574.00, LBL 44.00, WL 72.00, CRACK LENGTH IS .350". CARGO BAY FLOOR SILL FS 574.00, LBL 44.00, WL 72.00, REPAIRED IAW REO 601R-53-61-1741. (K)

Part: SKIN — CORRODED (BS 364) · corrosion level 1 · airframe 17,115 hrs · 15,637 cycles

MAIN COMPARTMENT DOOR CUT-OUT INTERNAL SKIN FWD AND AFT SIDE CORRODED. MAIN AVIONIC COMPARTMENT DOOR CUT-OUT INTERNAL SKIN FWD AND AFT SIDE REPAIRED IAW REO 601R-53-21-676, REV A. (K)

Part: SILL — CORRODED (BS 574-621) · corrosion level 1 · airframe 17,115 hrs · 15,637 cycles

CARGO DOOR SILL AT LBL 45 CORRODED FROM FS 574 TO 621 AROUND STOW PLATE ATTACHING HOLES. CORROSION ON CARGO DOOR SILL AT LBL 45 FROM FS 574 TO FS 621 AROUND STOW PLATE ATTACHING HOLES, REMOVED IAW SRM 51-21-06. (K)

Part: SEAT TRACK — CORRODED (BS 349-409) · corrosion level 2 · airframe 17,115 hrs · 15,637 cycles

LT FLOOR SEAT RAIL CORRODED BTW FS 349.00 AND FS 409.00, LBL 9.0 LT FLOOR RAIL REPLACED BTW FS 349.00 AND FS 409.00, LBL 9.00 IAW AMM TASK 53-01-400-802. (K)

Part: CROSSBEAM — CRACKED (BS 280) · airframe 17,115 hrs · 15,637 cycles

LOWER RADIUS OF CROSSBEAM AT FS 280.00, LBL 9.00, WL 72.00 IS CRACKED. REPAIR CARRIED OUT IAW REO 601R-53-11-171. (K)

Part: PRESSURE BLKHD — CRACKED (BS 621) · airframe 16,714 hrs · 15,257 cycles

MWC 136501-2 - AFT PRESSURE BLKHD WEB AT FS 621 LINTEL LOCATION IS CRACKED. AFT PRESSURE BULKHD FS 621 REPAIRED IAW REO 601R-53-61-1230, REV D. (K)

Part: DISPLAY — MALFUNCTIONED (COCKPIT)

CAPT PFD WENT BLANK ON INITIAL TAKEOFF ROLL. ABORTED TAKEOFF PRIOR TO 80 KNOTS. BRAKE TEMP NORMAL. PERFORMED OPS TEST CHECK OUT IAW AMM 24-25-00-710-801. NO DEFECTS NOTED AT THIS TIME ACFT OK FOR SERVICE. (K)

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 13,580 hrs · 12,225 cycles

DAMAGE ON LT FUSALAGE AT STA 220. REPAIRED CUTOUT ON LT FUSELAGE IAW REO 601R-53-11-1332. (K)

Part: SKIN — TORN (PAX DOOR) · airframe 13,580 hrs · 12,225 cycles

PAX DOOR STAIR HAVE APPROX 1.5 IN X 1.5 IN TEAR IN FWD FACE SKIN AT FWD HANDRAIL DOWN STOP BRACKET POINT. REPAIRED IAW REO 601R-52-11-702, REV A. (K)

Part: BULKHEAD — CRACKED (BS 202) · airframe 12,427 hrs · 11,092 cycles

FORWARD PRESSURE BULKHEAD AT FS 202.75 CRACKED AT HYDRAULIC SYS NR 3 RT IB BRAKE FITTING LT LOWER SIDE. (K) MAINTENANCE REPAIRED BULKHEAD IAW BOMBARDIER SERVICES CORP EO 601R-53-12466. (M)

Part: CHANNEL — CRACKED (BS 574) · airframe 12,427 hrs · 11,092 cycles

U-CHANNEL AT BOTTOM OF CARGO DOOR FWD ROLLER TRACK IS CRACKED .2500 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED U-CHANNEL IAW CRJ 200 SRM 51-42-06. (M)

Part: ANGLE — CRACKED (BS 625) · airframe 12,427 hrs · 11,092 cycles

FS 625.0 INTERCOSTAL OBLIQUE ANGLE (UPPER) CRACKED. (K) MAINTENANCE REMOVED AND REPLACED INTERCOSTAL P/N 601-35012-51 IAW BOMBARDIER REO 601R-53-61-422. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 12,427 hrs · 11,092 cycles

RT FS 484 INTERCOSTAL ANGLE CRACKED AT RBL 27 APPROX .1 INCH LONG UNDER CABIN FLOOR PANEL 262DRF. (K) MAINTENANCE REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE AND INSTALLED IAW BSC STANDARD REPAIR 601R-53-0029B AND 601R-53-41-059. (M)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,427 hrs · 11,092 cycles

RT FS 484 INTERCOSTAL CRACKED AT RBL 36 APPROX .1 INCH LONG UNDER CABIN FLOOR PANEL 262DRH. (K) MAINTENANCE REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND REO 601R-53-41-059. (M)

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 12,427 hrs · 11,092 cycles

RT FS 280 FLOOR SUPPORT CLIPS CRACKED APPROX .2 INCHES LONG AT RBL 9, IB AND OB LOCATIONS. (K) MAINTENANCE REMOVED AND REPLACED SUPPORT CLIPS IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ 200 SRM 51-42-21. (M)

Part: FRAME — CRACKED (BS 280) · airframe 12,427 hrs · 11,092 cycles

FS 280 FRAME CRACKED APPROX 2 INCH LONG OB AT RBL 9, BELOW W/L 73. (K) MAINTENANCE REMOVED DAMAGED SECTION AND INSTALLED REPAIR IAW BOMBARDIER REO 601R-53-11-171. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 12,427 hrs · 11,092 cycles

LT FS 484 INTERCOSTAL PREVIOUS REPAIR ANGLE AT LBL 36 CRACKED APPROX .1INCH LONG UNDER CABIN FLOOR PANEL 261DLF. (K) MAINTENANCE REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW BSC STANDARD REPAIR 601R-53-0030A AND REO 601R-53-41-059. (M)

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 12,427 hrs · 11,092 cycles

LT FS 280 FLOOR SUPPORT CLIPS CRACKED APPROX .2 INCH LONG AT LBL 9 IB AND OB LOCATIONS. (K) MAINTENANCE REMOVED AND INSTALLED SERVICEABLE CLIPS TWO P/N 601R3113-57 IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ 200 SRM 51-42-21 AND 51-42-13. (M)

Part: SELECTOR VALVE — UNKNOWN (NLG)

NOSE GEAR DISAGREE ILLUMINATED ON GEAR RETRACTION. FOLLOWED QRH, PUT GEAR DOWN, MESSAGE CLEARED. REMOVED AND REPLACED NOSE LANDING GEAR SELECTOR VALVE PER AMM 32-22-02, OPS CHECK GOOD. (M)

Part: PCU — UNKNOWN (INBD RT WING)

FLIGHT SPOILER CONFIG WARNING AND AURAL WHEN APPLICATION OF POWER UNTIL THRUST LEVERS MOVED BACK TO IDLE, THE RT FLIGHT SPOILER TURNED WHITE ON SYSTEM PAGE. REMOVED AND REPLACED RT INBOARD FLIGHT SPOILER PCU PER AMM. OPS CHECK GOOD. (M)

Part: THRESHOLD — CRACKED (CARGO BAY) · airframe 7,438 hrs · 6,316 cycles

CARGO DOOR THRESHOLD PLATE HAS A .2500 INCH CRACK AT FS 589.00, LBL 41.5. REPAIRED BY REMOVING DAMAGED SECTION OF FLOOR LANDING PERFORMING EDDY CURRENT INSP, PAINTING REPAIR AREA AND FILLED REDUNDANT HOLE IAW MFG REO. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,438 hrs · 6,316 cycles

RT FS 621.00 ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING ANGLES AND STRAP, INSTALLING REPAIR PART IAW MFG REO. (K)

Part: ANGLE — CRACKED (FUSLEAGE) · airframe 7,438 hrs · 6,316 cycles

LT FS 621.00 ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING REPAIR ANGLES AND STRAP, INSTALLING REPAIR PARTS IAW MFG REO. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,438 hrs · 6,316 cycles

RT FS 460.00 ANGLE AT RBL 9 HAS A .5 INCH CRACK. REMOVED CRACK ANGLE AND INSTALL NEW ANGLE AT RBL 9. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

RT FS 484.00 INTRCOSTAL AT LBL 36.0 HAS A .5 INCH LONG CRACK. FABRICATED ANGLE IAW EO. REMOVED FLANGE AND INSTALLED ANGLE IAW MFG REO. (K)

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 6,186 hrs · 5,232 cycles

NOSE GEAR WOULD NOT EXTEND. MANUAL EXTENSION OK. COMPLIED WITH GEAR SWING 8 TIMES. (5 TIMES REGULAR/ 3 TIMES ON EMERGENCY) OPS CHECK GOOD. (K)

Part: INDICATOR — CONTAMINATED (AIRSPEED) · airframe 5,721 hrs · 8,443 cycles

ON TAKEOFF ROLL THROUGH 80 KNOTS, STANDBY AIRSPEED INDICATION REMAINED AT 0 KNOTS. INSPECTED STANDBY SYSTEM AND FOUND WATER TO BE IN SYSTEM. PURGED WATER FROM SYSTEM AND PERFORMED LEAK CHECK IAW MM 34-11-00. OPS CHECK GOOD.

Part: UNKNOWN — FUMES (COCKPIT)

FUMES ENTERING COCKPIT AND CABIN WHEN ADJUSTING THE TEMP. PERFORMED OPS CHECK OF NR 1 AND NR 2 PACK NO FUMES NOTED. OK FOR SERVICE. (M)

Part: IDG — LOW (NR 2)

GEN NR 2 CAS MESSAGE AFTER TAKEOFF. RETURNED TO CID. SERVICED NR 2 IDG IAW MM. OPS CHECK NORMAL.

Part: BUSHING — LOOSE (WING)

FOUND LT MLG AFT WING SPAR BUSHING MIGRATED .052 INCH. REMOVED MIGRATED BUSHING ON LEFT MLG, AND INSTALLED FIRST OVERSIZE BUSHING, P/N 601R-57-21-003-21 IAW REO 601R-57-21-003 REV B. (M)

Part: SKIN — CHAFED (TE FLAP)

FOUND LEFT OUTBOARD FLAP HAS DEEP CHAFF IN FIXED VANE AT FAR OUTBOARD END LEADING EDGE .050 TO .075 DEPTH. PERFORMED A MAJOR REPAIR TO THE LEFT OUTBOARD FLAP LEADING EDGE FIXED VANE BY REMOVING AND REPLACING LEADING EDGE CAP, P/N 601R-14574-7 IAW CRJ SRM 57-30-00, 51-40-11 AND 51-42-13. (M)

Part: SMOKE DETECTOR — INOPERATIVE · airframe 622 hrs · 456 cycles

SMOKE CARGO FIRE WARNING DURING CLIMB C/W QRH FOR SMOKE CARGO, DISCHARGED BOTH CARGO FIRE BOTTLES. MAINTENANCE REMOVED AND REPLACED CARGO SMOKE DETECTOR, OPS CHECKED GOOD.