N934EV

Part: WIRE HARNESS — UNSERVICEABLE (NLG STEERING) · airframe 14,823 hrs · 13,685 cycles

ON CLIMB OUT PUT GEAR UP, CAME UP NORMALLY BUT THEN RECEIVED A NOSE WHEEL STEERING INOPERATIVE MESSAGE. RAN QRH WOULD NOT RESET. EMERGENCY DECLARED. FOUND DEFECTIVE WIRE IN NLG STEERING HARNESS. R & R NLG STEERING HARNESS IAW AMM 32-61-25. OPS TESTED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,293 hrs · 13,065 cycles

RT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT OVER WING EMERGENCY LIGHT IAW AMM 33-51-21.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 14,260 hrs · 13,028 cycles

F/A LIGHT SWITCH WAS NOT OPERATING IN POWER UP BUT AFTER 10 MINUTES OF CHARGING WORK PROPERLY. OPS CHECKED EMERGENCY LIGHTS IAW AMM 33-51-01. CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,428 hrs · 12,083 cycles

EMERGENCY LIGHTS AMBER OFF LIGHT OTC. REPLACED EMERGENCY LIGHTS OFF SWITCH LIGHT. OPS CHECK GOOD.

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT NACELLE)

LT COWL ANTI-ICE CAUTION MESSAGE AT FL280 STAYED ON REMAINDER OF FLIGHT UNTIL FINAL APPROACH. COMPLIED WITH QRH. (EMERGENCY DECLARED) REPLACED LT COWL ANTI-ICE VALVE IAW AMM 30-22-01, OPS TEST GOOD. NO FURTHER DEFECTS NOTED. REPLACED LT COWL ANTI-ICE VALVE IAW AMM 30-22-01. OPS TESTED GOOD.

Part: TRANSDUCER — FAILED (RIGHT) · airframe 13,243 hrs · 11,863 cycles

STALL FAIL CAUTION MESSAGE IN FLIGHT AT FL280, STAYED ON REMAINDER OF FLIGHT. COMPLIED WITH QRH. (EMERGENCY DECLARED) R & R RT TRANSDUCER IAW AMM 27-35-05. PERFORMED OPS TEST OF TRANSDUCER IAW AMM 27-35-05-710-801 AND AIR DATA SENSOR HEATER CONTROLLERS IAW AMM 30-31-15-710-801. NO DEFECTS NOTED.

Part: HOUSING — CRACKED (EMERGENCY LIGHT) · airframe 13,081 hrs · 11,665 cycles

LEFT FWD PASSENGER ENTRANCE FLOOR LEVEL EMERGENCY FLOOD LIGHT HOUSING CRACKED. R & R LT FWD PASSENGER ENTRANCE FLOOR LEVEL EMERGENCY LIGHT HOUSING IAW AMM 33-51-19. R & R LT FWD PASSENGER ENTRANCE FLOOR LEVEL EMERGENCY LIGHT HSG IAW AMM 33-51-19.

Part: ECU — INOPERATIVE (NLG STEERING) · airframe 12,944 hrs · 11,511 cycles

ASCENDING THROUGH 10-11K RECEIVED NWS INOP CAUTION COULD NOT EXTINGUISH. RETURN TO DEPARTURE. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) PERFORMED OPS CHECK OF NWS ECU IAW AMM 32-51-10-05. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (CLOSED)

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 12,775 hrs · 11,283 cycles

FAIRLEAD INTERCOSTAL CLIP AT RBL 27 FS 484.00 IS CRACKED. REPAIRED PANEL 282AZ IAW MM 25-52-21, STEPS B1-8. NEEDS 1559A/B APPLIED. APPLIED 1559A/B IAW CMM 25-52-21 STEPS 9 AND 10. (CLOSED)

Part: BULKHEAD — CRACKED (BS 280) · airframe 12,775 hrs · 11,283 cycles

2 EA CRACKS 1.5" LONG ON FS 280 BULKHEAD 3' FROM FLOOR STRUCTURE. (OPEN)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,775 hrs · 11,283 cycles

FS 280, CLIPS AT RBL 9 AT INBD AND OTBD SIDE OF THE FLOORBEAM ARE CRACKED. REMOVED 2 EA CLIPS AT RBL 9 INBD AND OTBD SIDE OF FLOORBEAM AND REPLACED WITH NEW SERVICEABLE ONES IAW SRM 51-42-06 AND 51-42-21. (CLOSED)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,775 hrs · 11,283 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. (OPEN)

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 12,775 hrs · 11,283 cycles

EMERGENCY PHOTOLUMINISCENT FLOOR TRACK LIGHT IS CRACKED AND DISCOLORED. (OPEN)

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 12,775 hrs · 11,283 cycles

EMERGENCY EXIT LIGHT LENS CRACKED ON THE LT WINDSCREEN. R & R CRACKED LT WINDSCREEN EMERG EXIT LIGHT LENS IAW MM 32-51-13-400-801. (CLOSED)

Part: BRACKET — BENT (NLG PROX SENSOR) · airframe 12,334 hrs · 10,770 cycles

NOSE GEAR WOULD NOT RETRACT ON TAKEOFF, RECEIVED RED "NOSE GEAR OPEN" MESSAGE, AND RED "GEAR DISAGREE" MESSAGE. EMERGENCY DECLARED AS A PRECAUTION -- ACFT RETURNED TO DEPARTURE AFTER T/O. FOUND NOSE GEAR CENTERED EXTENDED PROX SENSOR BRACKET BENT, REPLACED BRACKET IAW CMM 32-20-04, ADJUSTED PROX SENSOR IAW AMM 32-61-05. OPS CHECK OF LANDING GEAR SYS GOOD IAW AMM 32-30-00-720-801. ACFT OK FOR SERVICE.

Part: COMPUTER — FAILED (FUEL QTY) · airframe 11,731 hrs · 10,057 cycles

DURING FLT FUEL IMBALANCE CAUTION MESSAGE POSTED ON EICAS TOT FUEL DECREASED FROM 4900 TO 4000 IN 30 SEC THEN TO 3000 IN 45 SEC TOT FUEL THEN INCREASED TO 3900 AND REMAINED THERE FOR THE REMAINDER OF FLT. ACFT DIVERTED DUE TO MX -- EMERGENCY DECLARED --REF DEFECT 525788 R & R FUEL QTY COMPUTER IAW AMM 28-41-16. OPS CK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 10,258 hrs · 8,528 cycles

EMERGENCY FLOOR EXIT SIGN ON WARDROBE LIGHT BASE BROKEN.

Part: TRIM SWITCH — INTERMITTENT (STABILIZER) · airframe 9,506 hrs · 7,799 cycles

STAB TRIM STUCK AT T/O TRIM SETTING DISCONNECTED AND RECONNECTED STAB TRIM AND THEN GOT NOSE UP RUNAWAY AT POINT 1 FOR EACH 5 SECONDS, RAN QRH. ENDED UP AT 10 DEGREES NOSE UP. EN ROUTE TO ATL, A/C DIVERTED TO SAV DUE TO MTC. FLT 5469 DEL 189 MINS. FOUND INTERMITTENT CONTACTS ON PILOTS PITCH TRIM SWITCH. REMOVED AND REPLACED PILOTS PITCH TRIM SWITCH IAW AMM 27-41-05-000-801 AND OPS CHECK GOOD IAW 27-40-00-710-802. RTS FOR CAT II OPERATIONS COMPLIED WITH IAW AMM SUPP 22-11-00-710-801.

Part: MOTOR — MALFUNCTIONED (PAX DOOR) · airframe 9,224 hrs · 7,528 cycles

MAIN PASSENGER DOOR WILL NOT CLOSE. FLT 5405 DEL 47 MINS. REMOVED AND REPLACED PAX DOOR POWER ASSIST MOTOR ASSY IAW CRJ 200 AMM 52-11-01. OP'S CHECK GOOD. DMIL CLEARED PLACARD REMOVED.

Part: PLACARD — WORN (PAX DOOR) · airframe 8,854 hrs · 7,182 cycles

PAX DOOR PLACARDS 1 EXIT, 2 OPEN, AND 3 RED ARROW ARE WORN.

Part: ANGLE — CRACKED (CARGO BAY) · airframe 8,854 hrs · 7,182 cycles

CARGO CENTER BULKHEAD ANGLE IS CRACKED. REPAIRED PANEL CTR BULKHEAD AND ANGLE IAW CMM 25-52-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,854 hrs · 7,182 cycles

LBL 27 OUTBOARD SIDE AT FS 484 INTERCOSTAL ANGLE CRACKED IN UPPER RADIUS. REMOVED AND REPLACED LBL 27 OUTBOARD SIDE AT FS 484 INTERCOSTAL ANGLE IAW REO 601R-53-41-059. SA EC/TC REQUIRED. C/W ASA EC/TC REO 601R-53-41-059. RII C/W 56300045.

Part: STRUCTURE — CORRODED (CARGO DOOR) · airframe 8,854 hrs · 7,182 cycles

UPON FURTHER INVESTIGATION FOUND CORROSION ON CARGO DOOR FLOOR EDGE MEMBER TO BE WITHIN ALLOWABLE REPAIRABLE LIMITS IAW SRM 53-00-00. BLENDED CORROSION ON CARGO DOOR EDGE MEMBER IAW SRM 51-21-06. APPLIED CONVERSION COATING, PRIMER, AND PAINT IAW SRM 51-25-06 AND 51-25-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,854 hrs · 7,182 cycles

RBL 36 AT FS 484 INTERCOSTAL IS CRACKED IN UPPER RADIUS. REPAIRED RBL 36 AT FS 484 INTERCOSTAL IAW REO 601R-53-41-059 REV A. AND IAW STD MANUAL 56144. REMOVED RUDDER PULLEY BRACKET AT FS 484 RBL 36 BY REMOVING 2 BOLT & NUT COMBINATION. INSTALLED RUDDER PULLEY BRACKET WITH 2 BOLTS AND NUTS, TORQUED IAW SRM 51-41-04. C/W EC/TC REO 601R-53-41-059. RII C/W 5400005.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,854 hrs · 7,182 cycles

LBL 36 AT FS 484 INTERCOSTAL IS CRACKED IN UPPER RADIUS. UNBOLTED PULLEY BRACKET AT LBL 36 FS 484 INTERCOSTAL IAW SRM 51-41-00. REPAIRED CRACKED INTERCOSTAL AT FS 484 LBL 36 IAW REO 601R-53-41-059. ALL STEPS C/W. PULLEY BRACKET REQUIRES INSTALL. INSTALLED PULLEY BRACKET AT FS 484 LBL 36 IAW SRM 51-41-00. C/W EC/TC REO 601R-53-41-059.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,854 hrs · 7,182 cycles

RT 621 OBLIQUE ANGLE CRACKED. REMOVED AND REPLACED RH 621 OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,854 hrs · 7,182 cycles

LT 621 OBLIQUE ANGLE CRACKED. REMOVED AND REPLACED LT OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,854 hrs · 7,182 cycles

RBL 27 OUTBOARD SIDE AT FS 484 INTERCOSTAL ANGLE IS CRACKED IN UPPER RADIUS. REMOVED CRACKED ANGLE, REPLACED WITH SERVICEABLE ANGLE IAW CRJ 200 SRM 51-42-06.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 8,854 hrs · 7,182 cycles

PASSENGER DOOR OUTER HANDLE IS CRACKED.

Part: PLACARD — MISSING (CABIN) · airframe 8,854 hrs · 7,182 cycles

CREW ESCAPE HATCH-EMERGENCY EXIT PLACARD FWD OF THE HANDLE IS MISSING. APPLIED NEW SILKSCREEN FWD OF HANDLE ON CREW ESCAPE HATCH IAW CRJ MM 11-10-03-400-801. SUPPLEMENTAL-SDR CLOSED 11/14/2008.

Part: SKIN — CRACKED (PAX DOOR) · airframe 8,854 hrs · 7,182 cycles

PASSENGER DOOR AFT SIDE SKIN IS CRACKED IN 3 AREAS: TOP STEP, MID STEP AND CUTOUT FOR BOLT HOLE. REPAIRED PASSENGER DOOR AFT SIDE SKIN IAW REO 601R-52-11-702. ECTC REQUIRED. COMPLIED WITH PAX DOOR SIDE SKIN REPAIRS IAW ASA EC/TC REO 601R-52-11-702.

Part: SKIN — CRACKED (PAX DOOR) · airframe 8,854 hrs · 7,182 cycles

PASSENGER DOOR FWD SIDE SKIN IS CRACKED AT TOP STEP. REPAIRED PASSENGER DOOR FWD SIDE SKIN IAW BOMBARDIER REO 610R-52-11-702 AND ASA EC/TC CARD REO 601R-52-11-702. SUPPLEMENTAL-SDR CLOSED 11/14/2008.

Part: CONTROL UNIT — MALFUNCTIONED (T/E FLAP) · airframe 8,463 hrs · 6,829 cycles

FLAPS FAIL CAUTION MSG WHEN SELECTING FROM 20 TO 30 DEGREES (EMERGENCY DECLARED). REMOVED AND REPLACED FECU, PERFORMED TEST GOOD. OPERATED FLAPS NUMEROUS TIMES. OPS CHECK GOOD. NO MESSAGES NOTED REF CRJ200 AMM 27-51-05, 27-51-10 AND 27-51-00. (S)

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 8,437 hrs · 6,805 cycles

CREW REPORTED FLAP FAIL. (ACFT RETURNED TO ATL AFTER TAKEOFF, EMERGENCY VEHICLES ON STANDBY AS A PRECAUTION). FLT 4615 DEL 150 MINS. REMOVED AND REPLACED FLAP CONTROL LEVER IAW CRJ 200 AMM 27-51-01. OPS CHECK GOOD. (S)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,719 hrs · 5,327 cycles

SEVERAL EMERGENCY LIGHTS INOP.

Part: DOOR — INOPERATIVE (MAIN PAX) · airframe 5,122 hrs · 4,088 cycles

PAX DOOR WOULD NOT OPEN.

Part: FLAP — MALFUNCTIONED (WING) · airframe 3,157 hrs · 2,588 cycles

FLAPS FAIL 30 DEGREES APPROACH AT 175KTS. AN EMERGENCY WAS DECLARED.

Part: PLACARD — UNKNOWN (CABIN) · airframe 2,641 hrs · 2,183 cycles

ASD EXIT PLACARD NEEDS REPLACED.