N8888D

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 26,505 hrs · 24,011 cycles

FIRST OFFICER`S FLASHLIGHT LED NOT BLINKING. R & R THE FLASHLIGHT IAW AMM 25-61-00. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,092 hrs · 23,582 cycles

SEVERAL FLOOR EMERGENCY LIGHTS FOUND INOPERATIVE. REMOVED AND REPLACED THE NR 3 INVERTER IAW AMM 33-51-07, OPS CHECKED GOOD.

Part: FIRE BOTTLE — LOW (LAVATORY) · airframe 25,910 hrs · 23,375 cycles

LAVATORY FIRE BOTTLE NOT SHOWING GREEN. REMOVED AND REPLACED THE LAVATORY FIRE EXTINGUISHER IAW AMM 26-26-01.

Part: STRUT — LOW PRESSURE (NLG) · airframe 25,871 hrs · 23,335 cycles

AFTER GEAR HANDLE SELECTED UP GEAR DISAGREE WARNING MESSAGE, WOW INPUT CAUTION MESSAGE, STEERING INOPERATIVE CAUTION MESSAGE, STAB TRIM CAUTION, MACH TRIM CAUTION MESSAGE. COMPLIED WITH GEAR DISAGREE QRH, EXTENDED GEAR AND GEAR DISAGREE MESSAGE WENT AWAY. STAB AND MACH TRIM MESSAGES WENT AWAY AFTER RESET PER QRH. STEERING RESET ON GROUND PER QRH. LANDED AT 37000 LBS AND RATE OF DESCENT 200 FPM. SERVICED NOSE STRUT IAW JOBCARD 12-710-002. PERFORMED EXT/RETRACTION CK OF LANDING GEAR IAW AMM 32-30-00. PERFORMED OPS CK OF STAB CONTROL SYSTEM IAW AMM 27-41-00. NO DEFECTS NOTED. SEE NRC# 631461 FOR DETAILS AND WORK PERFORMED.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 25,332 hrs · 22,756 cycles

FA FLASHLIGHT BY JUMPSEAT IS NOT FLASHING AND WHITE BAND IS NOT CONNECTED. REMOVED AND REPLACED THE F/A FLASHLIGHT BATTERY AND TAMPER STRAP IAW AMM 25-61-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,213 hrs · 22,628 cycles

ON F/A PRE FLT, FOUND HANDHELD EMERGENCY FLASHLIGHT INOP. R&R F/A HANDHELD FLASHLIGHT BATTERY IAW CMM 25-60-02. FLASH LIGHT OK FOR SVC.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,025 hrs · 22,422 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT BULB BURNED OUT AND STUCK IN SOCKET ASSY. REMOVED AND REPLACED LH AFT EXTERIOR EMERGENCY LIGHT ASSY AND REPLACED THE BULB IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: MOUNT — CRACKED (AC BAY) · airframe 23,828 hrs · 21,219 cycles

AFT ACCESSORY COMPARTMENT, RT ACM MOUNT FLANGE IS CRACKED. R & R RT ACM MOUNT FLANGE IAW SRM 51-42-06, S/M-123.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

LEFT FWD LOWER NOSE COMP-SYS NR 3 BRAKE ACCUMULATOR FWD OTBD MOUNT BRACKET CRACKED. R & R CRACKED SYS NR 3 BRAKE ACCUMULATOR FWD OTBD MOUNT BRACKET IAW SRM 51-42-06 AND SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

CABIN, LEFT SIDE SEAT RAIL, STICK NR 2 HAS MULTIPLE AREAS OF CORROSION. REPLACED LT SIDE NR 2 SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

LBL9 SEAT TRACK, FS 559.00 TO FS 559.00+80 HAS CORROSION. R & R SEAT TRACK AT LBL9 BETWEEN STA 559 AND 559+80 IAW AMM 53-01-11-420-001, PARA B.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

AFT ACCESSORY COMPARTMENT, AFT PRESSURE BULKHEAD, RBL 36, STR 13 ANGLE IS CRACKED. R & R CRACKED OBLIQUE ANGLE AT RBL 36, STR 13, FS 675 IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

IN MAIN CABIN RT FLOOR SEAT TRACK NR 2 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R RT NR 2 FLOOR SEAT TRACK IAW AMM 53-01-11-420-001, PARA B STEPS 1, 3-8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

IN MAIN CABIN LT FLOOR SEAT TRACK NR 3 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. R & R SEAT TRACK LT 3 IAW AMM 53-01-11-420-001, PARA B, STEPS 1-8.

Part: FILLER — CRACKED (PAX DOOR) · airframe 23,828 hrs · 21,219 cycles

MAIN PASSENGER ENTRY DOOR AFT STAIR WEB HAS CRACKED REPAIR FILLER. R & R ENTRY DOOR AFT STAIR WEB FILLER IAW REO 601R-52-11-702.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

AFT ACCESSORY COMPARTMENT, AFT PRESSURE BULKHEAD, LBL 36, STR 13 ANGLE IS CRACKED. R & R CRACKED OBLIQUE ANGLE AT LBL36, STR13, FS 625 IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

IN MAIN CABIN RT FLOOR SEAT TRACK NR 3 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. R & R TRACK NR 3 IAW AMM 53-01-11-420-001, PARA B, STEPS 1-8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

IN MAIN CABIN RT FLOOR SEAT TRACK, NR 1 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R NR 1 RT FLOOR SEAT TRACK IAW AMM 53-01-11, SUBTASK 53-01-11-420-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

CABIN, LT SIDE SEAT RAIL STICK NR 4 HAS MULTIPLE AREAS OF CORROSION. R & R NR 4 LT SIDE SEAT TRACK IAW AMM 53-01-11, SUBTASK 53-01-11-420-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

RBL9, SEAT TRACK FS 559.00 TO FS 559.00+80 HAS CORROSION. R & R SEAT TRACK AT RBL9 BETWEEN STA 559 TO 559+80 IAW AMM 53-01-11-420-001, PARA B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

IN MAIN CABIN LT FLOOR SEAT TRACK NR 1 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R NR 1 LT FLOOR SEAT TRACK IAW AMM 53-01-11, SUBTASK 53-01-11-420-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

CABIN, RT SIDE SEAT RAIL STICK NR 6 HAS MULTIPLE AREAS OF CORROSION. R & R SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

CABIN, LT SIDE SEAT RAIL STICK NR 5 HAS MULTIPLE AREAS OF CORROSION. R & R LT NR 5 SIDE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

CABIN, LEFT SIDE SEAT RAIL STICK NR 7 HAS MULTIPLE AREAS OF CORROSION. R & R LT SIDE SEAT RAIL STICK NR 7 IAW AMM 53-01-11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

FRAME 333 IS CRACKED AT TOOLING HOLE JUST INBD OF STR 1L, ABOVE PAX DOOR OPENING, IN CABIN. REPAIRED 333 FRAME IAW REO 601R-53-21-2724, REV A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

CABIN, RT SIDE SEAT RAIL STICK NR 7 HAS MULTIPLE AREAS OF CORROSION. R & R SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

CABIN, LT SIDE SEAT RAIL STICK NR 6 HAS MULTIPLE AREAS OF CORROSION. R & R LT SIDE SEAT TRACK NR 6 IAW AMM 53-01-11.

Part: BRACKET — CRACKED (COCKPIT) · airframe 23,828 hrs · 21,219 cycles

CENTER COCKPIT WINDSHIELD RT LOWER BRACKET AT STATION FS202.75 IS CRACKED. R & R CENTER COCKPIT WINDSHIELD RT LOWER BRACKET, FITTING AT FS 202.75 IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

CABIN, RT SIDE SEAT RAIL STICK NR 4 HAS MULTIPLE AREAS OF CORROSION. R & R RT NR 4 SEAT RAIL SEAT TRACK IAW AMM 53-01-11.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

PAX CABIN, STR ATTACH BRACKET CRACKED AT S-3L AND FS280. R & R 2EA STRINGER ATTACH BRACKETS AT S-3L, FS 280 IAW SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

PILOT'S WINDOW SIDE POST LOWER OTBD FITTING IS CRACKED. R & R PILOT'S WINDOW SIDE POST LOWER OTBD FITTING IAW SRM 51-42-21, AAR SM-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

CABIN, RT SIDE SEAT RAIL STICK NR 5 HAS MULTIPLE AREAS OF CORROSION. R & R RT NR 5 SEAT RAIL IAW AMM 53-01-11.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

CARGO DOOR FWD TRACK LOWER ATTACH CHANNEL IS CRACKED. R & R CARGO DOOR FWD TRACK LOWER ATTACH CHANNEL, PN 601R35050-25, T/N B70567 IAW SRM 51-40-11, SRM 51-42-06.

Part: GUSSET — CHAFED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

PAX CABIN, GUSSET CHAFED FWD OF SERVICE DOOR CUTOUT AT S-10R. BLENDED AREA IAW SRM 51-12-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, FABRICATED NEW GUSSET IAW SRM 51-24-16, LOCATED AND DRILLED IAW SRM 51-40-11, FINISH COAT IAW SRM 53-21-23, INSTALLED NEW PART IAW SRM 51-42-20.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

LBL27, FS 621 FLOORBEAM ATTACH FITTING HAS A CORRODED FASTENER HOLE OTBD FLANGE. REPAIRED LBL27, FS 621, FLOORBEAM ATTACH FITTING IAW EA CRJ253-04444.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 23,828 hrs · 21,219 cycles

PAX DOOR OPENING, AFT CLEAT HAS CORROSION. REMOVED CORROSION FROM BRACKET WITHIN LIMITS IAW SRM 53-00-00. REPLACED CLEAT IAW SRM 51-42-06.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,162 hrs · 20,583 cycles

R & R NR 1 EMER LIGHT BATTERY IAW AMM 33-51-04. OPERATIONS CHECKED GOOD.

Part: LIGHT — DETACHED (CABIN) · airframe 22,685 hrs · 20,117 cycles

THE EMER FLOOR TRACK LIGHT ON 1C DETACHED FROM ITS POSITION. SECURED EMER FLOOR TRACK LIGHT & OPERATIONS CHECKED GOOD IAW AMM 33-51-01.

Part: CONTAINER — TORN (LIFE VEST) · airframe 21,742 hrs · 19,222 cycles

CAPT LIFE VEST BAG IS TORN. REMOVED AND REPLACED CAPTAIN'S LIFE VEST IAW AMM 25-61-03.

Part: LIGHT — BROKEN (CABIN) · airframe 20,545 hrs · 18,034 cycles

EMERGENCY FLOOD LIGHT IS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-10.

Part: STRIP — MISSING (CABIN) · airframe 20,483 hrs · 17,975 cycles

EMERGENCY EXIT FLOOR TRACK LIGHTING AT SEAT 1C MISSING ORANGE STRIP. INSTALLED EMERGENCY EXIT FLOOR TRACK ORANGE STRIP IAW AMM 33-50-00.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 13,912 hrs · 13,305 cycles

MAINTENANCE FOUND CHAFE DAMAGE TO THE CARGO DOOR OUTER SKIN, AT THE TOP OF THE DOOR. THE DAMAGE MEASURES 1.10" LONG AND .438" WIDE AND .046" DEEP AT THE TOP EDGE AND 0.03" DEEP WITHIN 2D OF THE NEAREST ADJACENT FASTENER. REPAIRED IAW EA CRJ252-01341 AND ASSOCIATED 8110-3.

Part: SEAL — UNKNOWN (NLG) · airframe 20,304 hrs · 17,796 cycles

ON FLIGHT 3839 (SWF TO DTW) CREW REPORTED SHORTLY AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED UP. THEY RECEIVED A NOSE WHEEL STEERING INOPERABLE MESSAGE FOLLOWED BY A GEAR DISAGREE WARNING MESSAGE AND NOSE DOOR WARNING MESSAGE. COMPLETED QRH FOR GEAR UP DISAGREE AND NOSE WHEEL STEERING INOPERABLE. GOT THE 3 GREEN AND DOWN INDICATION. CREW DECLARED AN EMERGECNY AND PERFORMED AN AIR RETURN TO SWF. REMOVED AND REPLACED NOSE LANDING GEAR SHOCK STRUT LOWER BEARING SEALS UPPER BEARING SEAL, AND REMOVED AND REPLACED LOWER BEARING (PN 16176-9). PERFORMED OPS CHECK OF LANDING EXTENSION AND RETRACTION AND NOSE WHEEL STEERING. OK FOR SERVICE. WORK DONE IAW AMM 32-21-20, 32-21-30, 32-33-00, AND 32-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,008 hrs · 17,509 cycles

CREW REPORTS FRONT FLOOR EMERGENCY LIGHT IS INOPERABLE. REMOVED AND REPLACED FORWARD EMERGENCY FLOOR TRACK LIGHT IAW AMM 33-51-01. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,774 hrs · 17,281 cycles

FLOOR TRACK EMERGENCY LIGHT AT 1CD INOP. REMOVED AND REPLACED FLOOR TRACK EMERGENCY LIGHT AT 1 CD IAW CRJ200 AMM 33-51-01. OPS CHECKS GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 19,548 hrs · 17,048 cycles

COCKPIT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY IAW CMM 25-60-11 AND REINSTALLED IAW AMM 25-61-04. OPS CHECKED GOOD.

Part: ANGLE — CRACKED (BULKHEAD) · airframe 19,263 hrs · 16,764 cycles

CRACK FOUND IN FS 559 SEMI-PRESSURE BULKHEAD CAP ANGLES AT LBL 18 AND RBL 18. REPAIRED IAW REO 601R-53-41-260 AND 601R-53-41-609.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,037 hrs · 16,543 cycles

FLIGHT ATTENDANT CALL LIGHT INDICATION ON EMERGENCY EXIT (MID CABIN) LIGHT INOP. REMOVED AND REPLACED FLIGHT ATTENDANT CALL LIGHT INDICATION, OP CHECK GOOD IAW AMM 33-51-14. OK FOR SERVICE.

Part: HANDLE — DEFECTIVE (COCKPIT) · airframe 19,001 hrs · 16,507 cycles

FLAPS FAIL AT 20 ON FINAL. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39, IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED MARCH27 ,2009AND PA AD 27-052G. FOUND CODES 9 2B, 21 C1, 19 C2, 25 BC. REMOVED AND REPLACED FLAP HANDLE IAW AMM 27-51-01, OP CHECKS GOOD. THIS CLEARS DM #63611, OK FOR SERVICE.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 18,876 hrs · 16,381 cycles

CAPTAIN'S LIFE VEST HAS TEAR IN BAG. REMOVED AND REPLACED CAPTS LIFE VEST IAW AMM 25-61-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,848 hrs · 16,336 cycles

EMERGENCY FLOOR STRIP LIGHT INOPERATIVE ROW 10. REMOVED AND REPLACED LIGHT, OPS CHECKED GOOD.

Part: WHEEL — FAULTY (PAX DOOR) · airframe 18,325 hrs · 15,860 cycles

PASSENGER DOOR WHEEL DOES NOT ROTATE DOWN WHEN OPENED. INSPECTED AND LUBED AND CLEANED MCD SUPPORT WHEEL ASSY IAW AMM 52-10-00. OPS CK GOOD. OK FOR SVC.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 17,885 hrs · 15,399 cycles

F/O`S FLASHLIGHT INOP. REMOVED AND REPLACED F/O`S FLASHLIGHT IAW AMM 25-61-02. VERIFIED PART EFFECTIVITY OP/C GOOD.

Part: PROXIMITY SENSOR — OUT OF ALIGNMENT (NLG) · airframe 17,336 hrs · 14,888 cycles

AIR RETURN FOR NOSE GEAR DISAGREE UNCLEAR IF EMERGENCY DECLARED FOUND NLG OLEO CENTERED/EXTENDED PROX SENSOR OUT OF ALIGNMENT. ADJUSTED NLG OLEO CENTERED/EXTENDED PROX SENSOR (PS14GA) IAW CRJ 200 AMM 32-61-05 GEAR SWINGS C/W IAW AMM 32-30-00. OPS CHECK GOOD. OK FOR SERVICE.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 17,176 hrs · 14,743 cycles

FS 621 BULKHEAD CHAFED AT WL 103, LBL 16 (0.155"L X 0.140"W X 0.007" DEEP), RBL 18 (0.160"L X 0.118"W X 0.005" DEEP), RBL 27 (0.175"L X 0.150"W X 0.007" DEEP), AND RBL 36 (0.190"L X 0.185"W X 0.007" DEEP). REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: OIL SYSTEM — LOW PRESSURE (RT ENGINE) · airframe 16,641 hrs · 14,255 cycles

RT ENG LOW OIL PRESS IN FLIGHT. AN EMERGENCY WAS DECLARED. A/C LANDED SAFELY.

Part: BPSU — FAILED (TE FLAP) · airframe 15,637 hrs · 13,261 cycles

PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-60-12 PARAGRAPH(H)(B)(I) USING FIM REV 39 PER AMOC DATING MARCH 27, 2009, TR#27-012 PER AMOC DATED DEC 18, 2009 AND PA AD27-0520. REMOVED AND REPLACED RT BPSU IAW AMM 27-51-10. OPC GOOD. FEW CODES-FECU, R BPSU, WIRING, 1121A, 1122B. OK FOR SERVICE.

Part: UPLOCK — BYPASSING (NLG) · airframe 14,203 hrs · 11,912 cycles

LANDING GEAR DISAGREE ON TAKEOFF, NLG IND WAS RED AFTER GEAR RETRACTION. MTX RAR THE NLG UP LOCK ASSY.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 6,497 hrs · 5,295 cycles

FLAP FAIL AT 20 ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.

Part: CONTROL SYSTEM — FAILED (TE FLAPS)

(REF NR: 05-063) FLAP FAILED AT 20 ON APPROACH. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAP)

FLAPS FAILED AT 0 WHEN SELECTED TO 20. SYSTEM RESET IAW FIM, FLAPS PLACED UNDER WATCH FOR 72 HOURS IAW AD 98-20-01.