N8908D

Part: BATTERY PACK — INOPERATIVE · airframe 28,839 hrs · 26,861 cycles

EMERGENCY LIGHTS AT EXTERIOR MIDS AND CABIN LIGHT #3 INOP "REPLACED BATTERY PACK #3 IAW CRJ-200 AMM 33-51-04. PN ON/OFF 2013-1ASMI. SN OFF 7362. SN ON 13504. OPS CHECKS GOOD IAW CRJ-200 AMM 33-51-04. "

Part: POST — CRACKED · airframe 28,839 hrs · 26,861 cycles

ON AC N8908, DURING 6K INSPECTION FOUND CRACK ON VERTICAL POST LOWER FLANGE STARTING AT LOWEST RIVET EXTENDING UPWARD TO THE FLANGE BEND RADIUS. A/C LOCATION IS @ F.S. 409+128 LBL 27.0.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,529 hrs · 26,464 cycles

EMERGENCE LIGHTS WILL NOT STAY ON. REMOVED AND REPLACED NR 3 BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD.

Part: FRAME — CRACKED (BS 333) · airframe 26,370 hrs · 23,943 cycles

FS 333 FRAME CRACKED BETWEEN STR 0 AND STR 1L. INCLUDES 8790841/276 REMOVED AND REPLACED FS 333 UPPER FRAME SECTOR IAW CRJ 200 SRM 51-42-06 AND 51-42-21. OPS CHECK GOOD. WVAC EMP 769 STAMP

Part: SKIN — DENTED (BS 687) · airframe 26,370 hrs · 23,943 cycles

AFT FUSELAGE SKIN HAS 1 EA PROTRUDING DENT AT FS 687.75 BETWEEN STR 23L AND STR 24L. INCLDUES 8790841/290 C/W ENDEAVOR EA CRJ 253-09791 IN ITS ENTIRETY FOR REPAIR OF FUSELAGE SKIN. WVAC EMP STAMP

Part: THRESHOLD — CORRODED (SERVICE DOORWAY) · airframe 26,370 hrs · 23,943 cycles

SERVICE DOOR THRESHOLD IS CORRODED LOCATED & DRILLED NEW SERVICE DOOR THRESHOLD IAW CRJ 200 SRM 51-40-11 TR51-42. WVAC EMP 771 STAMP

Part: SKIN — CORRODED (RT WING) · airframe 26,370 hrs · 23,943 cycles

RIGHT WING LWR PLANK 640BB LANDING HAS CORROSION IN THE NON-CRITICAL AREA. REPAIRED RIGHT WING LOWER PLANK 640BB LANDINGS IAW GREO 601R-57-21-030 REV. L DATED 2014-04-05. WVAC EMP STAMP 771

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 26,370 hrs · 23,943 cycles

PRESSURE FLOOR SUPPORT CHANNEL @ FS 484.0, LBL 36 OUTBD LEG CRACKED. REMOVED AND REPLACED SUPPORT CHANNEL IAW CRJ200 SRM 51-40-11 AND REO 601R-53-41-059 REV B DATED 2009-09-16. WVAC EMP STAMP 717

Part: SKIN — CORRODED (LT WING) · airframe 26,370 hrs · 23,943 cycles

LEFT WING LWR PLANK 540BB LANDING HAS CORROSION IN THE NON-CRITICAL AREAS. REPAIRED LEFT WING LOWER PLANK 540BB LANDING IAW GREO 601R-57-21-030 REV.L DATED 2014-04-05. WVAC EMP STAMP 771

Part: HOUSING — CRACKED (DOOR HANDLE) · airframe 26,370 hrs · 23,943 cycles

AVIONICS DOOR HANDLE HOUSING HAS MULTIPLE INDICATIONS 80% FSH AROUND ENTIRE CIRCUMFERENCE OF THE BASE OF THE HANDLE SHAFT. FAILED NDT INSPECTION. REMOVED AND REPLACED AVI DOOR HANDLE HOUSING IAW CRJ200 SRM 51-40-11 TR 51-42 AND 51-42-06. OPS CHECK GOOD. WVAC EMP STAMP

Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 26,370 hrs · 23,943 cycles

SCREW CHAFE ON FS 621 RPB WEB FWD FACE AT RBL 36 WL 103. REPAIRED FS 621 BULKHEAD IAW REO 601R-53-61-1285 REV E. EMP #6449

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 26,370 hrs · 23,943 cycles

ONE ARE OF CRACK INDICATIONS NOTED ON FS 621 RPB WEB IN HEEL LINE AREA OF VERT POST AT BL0 WL108-WL112 60% FSH. FAILED NDT INSP. REPAIRED FS 621 BULKHEAD IAW REO 601R-53-61-1285 REV E. EMP #6449

Part: CROSSBEAM — CRACKED (BS 280) · airframe 26,370 hrs · 23,943 cycles

FS 280 CROSSBEAM RBL 9 OB ATTACH ANGEL CRACKED UPON FURTHER INVESTIGATION, FOUND BULKHEAD WEB TO BE PREVIOUSLY REPAIRED PER REO 601R-53-11-926. FABRICATED ANGLE IAW BOMBARDIER REO 601R-53-11-926 REV B FLAGNOTE 20, FROM PREFORMED ANGLE PN S6144-13 PO W56689 & INSTALLED IAW CRJ 200 SRM 51-42-21. WVAC EMP 769 STAMP

Part: FITTING — CRACKED (BS 460) · airframe 26,370 hrs · 23,943 cycles

FS 460 FLOOR FITTING CRACKED ON OB SIDE OF RBL 9 REMOVED & REPLACED CRACKED 460 FITTING OB SIDE OF RBL 9 PN 600-31068-19 IAW CRJ 200 SRM 51-40-11 TR 51-42 & BOMBARDIER REO 601R-53-41-2609 REV-- DATED 10/20/19. WVAC EMP STAMP

Part: SEAT TRACK — CORRODED (BS 400-409) · airframe 26,370 hrs · 23,943 cycles

SEAT TRACK AT RBL 9 FS 400 TO 409+120 IS CORRODED REMOVED & REPLACED CORRODED SAT TRACK AT RBL 9 FS 409 TO FS 409+120 IAW REO 601R-53-00-485. SEAT TRACK PART #20276-288-0-0 REV W. WVAC EMP 769 STAMP

Part: SEAT TRACK — CORRODED (BS 400-409) · airframe 26,370 hrs · 23,943 cycles

THE CABIN FLOOR SEAT TRACK AT LBL 9 FS 40 TO 409+120 IS CORRODED REMOVED & REPLACED CORRODED SEAT TRACK AT LBL 9 FS 400+0 FS 40+120 IAW REO 601R-53-00-485. SEAT TRACK PT #20276-288-0-0 REV W. WVAC EMP STAMP

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 26,370 hrs · 23,943 cycles

FLOOR SEAT TRACK AT FS 364-409+16 LBL 9 CORRODED REMOVED & REPLACED SEAT TRACK SECTION IAW CRJ 200 AMM 53-01-11-400-802. WVAC EMP STAMP

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 26,370 hrs · 23,943 cycles

FLOOR SEAT TRACK AT FS 364-409+16 RBL 9 CORRODED REMOVED & REPLACED SEAT TRACK PN 601R31032-15 BETWEEN FS 364 - FS 399.. REF JOB 8790841/286 FOR REPLACEMENT OF TRACK BETWEEN FS 399 - 409+16 IAW CRJ 200 AMM 53-01-11-400-802. WVAC EMP STAMP

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 26,370 hrs · 23,943 cycles

STRINGER 3L FWD UPPER ATTACHED ANGLE CRACKED JUST AFT OF FS 280 BULKHEAD REMOVED & REPLACED CLIP AT STGR 3L JUST AFT OF FS 280 IAW CRJ 200 SRM 51-40-11, 51-42-06 AND 51-42-21. WVAC EMP STAMP

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 26,370 hrs · 23,943 cycles

PRESSURE FLOOR SUPPORT CHANNEL @ FS 484.0 RBL 36 IB LEG CRACKED LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE IB CLIP PN 601R31171-9 ON PRESSURE FLOOR SUPPORT CHANNEL AT FS 484 RBL 36 IAW CRJ 200 SRM 51-40-11 TR 51-42- AND 51-42-21.

Part: SUPPORT CHANNEL — CRACKED (BS 574) · airframe 26,370 hrs · 23,943 cycles

CARGO DOOR FWD TRACK SUPPORT CHANNEL PN 601R35050-129 FLANGES BENT END GOUGED REMOVED TAPE, REMOVED AND REPLACED CARGO DOOR SUPPORT CHANNEL IAW CRJ 200 SRM 51-42-06. WVAC EMP STAMP

Part: HOUSING — DEFECTIVE (EXTERIOR LIGHT) · airframe 25,589 hrs · 23,137 cycles

FWD LT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED FWD LT EMER LIGHT HOUSING IAW AMM 33-51-21 OPS CHK GOOD OK FOR SVC.

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 25,260 hrs · 22,792 cycles

DURING COMPLIANCE OF SDI RPB FWD FACE NOTED FOLLOWING DAMAGE 7 WEBSTRICKS FROM LINER HARDWARE LOCATION AS FOLLWS LBL 27.5, 18, 9.5 RBL 18, 27.5, 36.2AND ONE AT1.5" IB OF THE STRIKE AT LBL 9.5 ALL IN LINE HORIZONTALLY APPROX 29.75" UP FROM CARGO FLOOR SUPERFICAL 5 RIVET HEAD COMPLETED REPAIR OF 7 WEBSTRIKES IAW BOMBARIDER REO 601R-53-61-2155 COMPLETED REPLACEMENT OF DAMAGED RIVET HEADS IAW CRJ200 SRM 51-42-06 WEBSTRIKES NDI INSPECTION COMPLETED NO CRACKS FOUND

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,576 hrs · 22,026 cycles

MOST FWD SEGMENT OF FLOOR TRACK EMERGENCY LIGHTING INOP. REMOVED AND REPLACED MOST FWD SEGMENT OF FLOOR TRACK EMERGENCY LIGHTING P/N 36491-1 IAW AMM 33-51-01.

Part: POST — CRACKED (BS 409) · airframe 24,153 hrs · 21,550 cycles

VERTICAL POST AT RBL 18, BS 409+128 WAS CRACKED AT THE BOTTOM FLANGE, OTBD AFT SIDE. REPAIRED THE VERTICAL POST IAW REO 601R-53-41-0056. MAJOR REPAIR

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 24,145 hrs · 21,541 cycles

CABIN FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW AMM 25-61-04.

Part: PBE — DAMAGED (COCKPIT) · airframe 23,632 hrs · 20,973 cycles

PBE ENCLOSURE TORN AFT TOP BEHIND CAPTAIN'S SEAT. REMOVED AND REPLACED THE PBE IAW AMM 200 35-30-00

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 23,195 hrs · 20,514 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECKED GOOD.

Part: LIGHT — CORRODED (FUSELAGE) · airframe 23,059 hrs · 20,369 cycles

DURING WALK AROUND, NOTICED EMERGENCY LIGHT ABOVE WING CORRODED. REPLACED THE LAMP EMERGENCY LIGHT IAW CRJ 200 AMM 33-51-21-04. OPS CHECKS GOOD. P/N ON/OFF: 1317

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,775 hrs · 20,070 cycles

EMERGENCY LIGHT, EXTERIOR, RT AFT, NOT ILLUMINATING. REMOVED AND REPLACED LIGHT IAW AMM 33-51-2. OPS CHECKED GOOD.

Part: HANDLE — MISSING (AED) · airframe 22,625 hrs · 19,903 cycles

AED MISSING HANDLE LCD "OK" INDICATOR HANDLE CONTENTS HAVE NOT BEEN USED. REMOVED AND REPLACED AED IAW TS 004766.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 22,616 hrs · 19,894 cycles

ON ARRIVAL, MAIN CABIN DOOR WOULDNT OPEN FOR THE FLIGHT ATTENDANT. VERIFIED ALL GREEN MARKS WERE IN PLACE, BUT AFTER LIFTING THE HANDLE THE DOOR DIDN'T OPEN FREELY. LUBRICATED THE MAIN PASSENGER DOOR. PERFORMED AN OPS CHECK OF DOOR. CHECKED GOOD IAW 52-11-00.

Part: OXYGEN MASK — LEAKING (FIRST OFFICER'S) · airframe 22,135 hrs · 19,371 cycles

FIRST OFFICER`S OXYGEN MASK LEAKS. REPLACED THE DAMAGED OXYGEN MASK IAW AMM 35-11-12. OPS & LEAK CHECKED GOOD.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 21,948 hrs · 19,174 cycles

OBSERVER LIFE VEST PACKAGE IS RIPPED OPEN. R&R LIFE VEST IAW AMM 25-61-03.

Part: BRACKET — DAMAGED (NLG) · airframe 21,811 hrs · 19,040 cycles

GEAR DISAGREE MESSAGE + NOSE DOOR OPEN MESSAGE AFTER T/O WHEN GEAR HANDLE UP. REMOVED AND REPLACED NOSE LANDING GEAR SENSOR BRACKET. REINSTALLED TOW GUARD COLLAR, SERVICED NLG STRUT IAW AMM 12-12-32. PERFORMED EXTENSION AND RETRACTION TEST IAW AMM 32-30-00. ALL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,678 hrs · 18,908 cycles

EMERGENCY LIGHT AT BS 409.00+120.50 IS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY IAW AMM 33-51-21.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,561 hrs · 18,788 cycles

AFT EMERGENCY FLOOR TRACK LIGHTING ROWS 9-13, INOP. REMOVED AND REPLACED NR 4 INVERTER P/N ON/OFF 5925-7 IAW AMM 33-51-07.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 21,508 hrs · 18,730 cycles

DURING TREND 6097 O2 SERVICING NOTED CAPTS. O2 MASK LEAKING/NOT TESTING PROPERLY. REPLACED CAPTS OXYGEN MASK, ASL REF/ 35-11-12, OPS & LEAK CHECKS GOOD. P/N MF10-08-01 ON & OFF. S/N ON 1097171, S/N OFF SEO5163.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,428 hrs · 18,657 cycles

AFT EMERGENCY LIGHTS FOUND INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY LIGHT INVERTER IAW AMM 33-51-07 .

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,406 hrs · 18,636 cycles

RIGHT CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21-420-002 STEP B.(1) OPS TESTED GOOD IAW AMM 33-51-00-710-801

Part: RETAINER — CRACKED (LT WING) · airframe 21,406 hrs · 18,636 cycles

LEFT WING FLAP HINGE FAIRING 583AB HAS CRACKED SEAL RETAINER. REMOVED AND REPLACED SEAL RETAINER IAW CRJ 200 SRM 51-42-19 AAR SM-14

Part: FLOOR SUPPORT — CORRODED (BS 473-559) · airframe 21,406 hrs · 18,636 cycles

FLOOR SUPPORT RBL 9 I/B LANDING HAS CORROSION SPOTS BETWEEN BS 473.15 TO 559, REPAIRED FLOOR SUPPORT IAW REO 601R-53-41-2105 AND REO 601R-53-41-2104 AND REO 601R-53-00-005

Part: HAND RAIL — LOOSE (PAX DOOR) · airframe 21,406 hrs · 18,636 cycles

PAX DOOR HAND RAIL AFT STOW CLIP IS LOOSE. REMOVED AND REPLACED IAW SRM 51-42-06 AAR SM-58

Part: ATTACH FITTING — CHAFED (NR 2 INLET) · airframe 21,406 hrs · 18,636 cycles

NR 2 ENGINE UPPER NOSE INLET COWL (FAN) OUTBOARD ATTACHMENT STRIP IS CHAFED ALONG LOWER EDGE. REMOVED AND REPLACED THE NR 2 ENG UPPER NOSE TCOWL ATTACHMENT STRIP IAW CMM 71-14-01 AND RETURNED TO ORG FINISH. CMM IAW TASK 71-14-01-300-814-A01.

Part: FLOORBEAM — CORRODED · airframe 21,406 hrs · 18,636 cycles

RT FLOOR SUPPORT AT RBL 9 BETWEEN FS 559+16-559+112 IS CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT SRM 51-42-06 AND REO 601R-53-00-005

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 21,406 hrs · 18,636 cycles

LEFT AISLE SEAT TRACK HAS CORROSION BETWEEN BS 394 TO 409+112. REMOVED AND REPLACE THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 21,406 hrs · 18,636 cycles

MAIN CABIN RIGHT SEAT TRACK HAS MULTIPLE AREAS OF CORROSION AND GOUGES BS 559 - 559+80, RBL9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 21,406 hrs · 18,636 cycles

LT AISLE SEAT TRACK HAS CORROSION ON THE TOP AND SIDES BETWEEN BS 409+128 AND 559. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 21,406 hrs · 18,636 cycles

RIGHT SEAT TRACK HAS CORROSION ON THE TOP AND SIDES BETWEEN BS 409+128 AND 559. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 21,406 hrs · 18,636 cycles

FLOORBEAM CORRODED. REPAIRED IAW REO 601R-53-00-005 AND SRM 53-00-43.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 21,406 hrs · 18,636 cycles

CARGO DOOR THRESHOLD HAS CRACKED HINGE. REMOVED AND REPLACED CARGO DOOR THRESHOLD HINGE IAW SRM 51-42-11 TOPCOATED IAW SRM 51-25-16.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 21,406 hrs · 18,636 cycles

REAR PRESSURE BULKHEAD FORWARD FACE HAS A CRACK EXTENDING FROM END OF DOOR TRACK AT LBL 18 APPROX 1/2 LONG. REPAIRED IAW REO 601R-53-61-1541.

Part: ATTACH ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 21,406 hrs · 18,636 cycles

AFT PRESSURE BULKHEAD INTERCOSTAL AT STRINGER 16L HAS CRACKED ANGLE. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-5265.

Part: ATTACH ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 21,406 hrs · 18,636 cycles

AFT PRESSURE BULKHEAD INTERCOSTAL AT STRINGER 14L HAS CRACKED ANGLE. REMOVED AND REPLACED THE IAW SRM 51-42-21, AND REO 601R-53-61-5265.

Part: ATTACH ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 21,406 hrs · 18,636 cycles

AFT PRESSURE BULKHEAD INTERCOSTAL AT LONGERON 13L HAS CRACKED ANGLE. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-21, AND REO 601R-53-61-5265.

Part: FLANGE — CRACKED (APU BAY) · airframe 21,406 hrs · 18,636 cycles

APU ENCLOSURE AFT UPPER FLANGE HAS TWO BROKEN WELDS AT SUPPORT RIBS. REMOVED DAMAGE AND REPAIRED IAW REO 601R-49-11-071.

Part: OXYGEN BOTTLE — INOPERATIVE · airframe 21,406 hrs · 18,636 cycles

PORTABLE OXYGEN BOTTLE S/N: 184341 FAILED OPS CK. REMOVED & REPLACED PORTABLE OXYGEN BOTTLE S/N 184341 IAW TS000340-2012. C/W OPERATIONAL CHECK IAW AMM 35-31-01-710-801. CHECKS GOOD.

Part: RUB STRIP — CHAFED (NR 2 NACELLE) · airframe 21,406 hrs · 18,636 cycles

NR 2 ENGINE UPPER NOSE INLET COWL RUBSTRIP IS CHAFED IN NUMEROUS AREAS. REMOVED & REPLACED IAW CMM 71-14-01.

Part: SEAT TRACK — CORRODED (BS 520-537) · airframe 21,406 hrs · 18,636 cycles

LEFT SEAT TRACK HAS CORROSION FROM BS 520 TO 537. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409-443) · airframe 21,406 hrs · 18,636 cycles

LEFT SEAT TRACK HAS CORROSION AT BS 409+113 TO 409+131 AND 426 TO 443. REMOVED & REPLACED THE SEAT TRACK IAW REO 601R-53-00-055. REV B.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 21,406 hrs · 18,636 cycles

CARGO FLOORBEAM ANGLE AT BS 621 BETWEEN RBL 45 AND LBL 45 HAS CORROSION. REMOVED CORROSION AND FOUND AREA IN LIMITS IAW REO 601R-53-61-4690. ONE AREA AT LBL 15 OUT OF LIMITS, REPAIRED IAW EA CRJ253-04812.

Part: SEAT TRACK — CORRODED (BS 550-559) · airframe 21,406 hrs · 18,636 cycles

LEFT SEAT TRACK HAS CORROSION AT BS 550 TO 566, 559+23 TO 559+40 AND 559+55 TO 559+72. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 457-499) · airframe 21,406 hrs · 18,636 cycles

LEFT SEAT TRACK HAS CORROSION AT BS 457 TO 477 AND 486 TO 499. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 21,406 hrs · 18,636 cycles

LEFT SEAT TRACK HAS CORROSION AT BS 409+21 TO 409+37, 409+50 TO 409+68 AND 409+83 TO 409+100. REMOVED & REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 449-500) · airframe 21,406 hrs · 18,636 cycles

RIGHT SIDE SEAT TRACK HAS CORROSION FROM BS 449 TO 500. REMOVED & REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 550-559) · airframe 21,406 hrs · 18,636 cycles

RIGHT SEAT TRACK HAS CORROSION AT BS 550 TO 553 AND 559+23 TO 559+28. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: FLOOR SUPPORT — CORRODED · airframe 21,406 hrs · 18,636 cycles

FLOOR SUPPORT LBL 9 HAS NUMEROUS CORROSION SPOTS BETWEEN BS 409+16 TO FS 409+128, IN CABIN. REMOVED & REPLACED THE FLOOR SUPPORT IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 21,406 hrs · 18,636 cycles

RIGHT SEAT TRACK HAS CORROSION AT BS 409+121 TO 409+137, 409+52 TO 409+55, 409+65 TO 409+69, 409+80 TO 409+89, 409+93 TO 409+101, AND 409+105 TO 409+110. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 21,406 hrs · 18,636 cycles

RIGHT SEAT TRACK HAS CORROSION FROM FWD END AT BS 409+114 TO 449. REMOVED & REPLACED THE SEAT TRACK IAW REO 601R-53-00-055 REV. B.

Part: SEAT TRACK — CORRODED (BS 367-409) · airframe 21,406 hrs · 18,636 cycles

RIGHT SEAT TRACK HAS CORROSION AT BS 367 TO 372, 382 TO 387, 399 TO 409+6. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 501-537) · airframe 21,406 hrs · 18,636 cycles

RIGHT SEAT TRACK HAS CORROSION AT BS 501 TO 506 AND 521 TO 537. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: BRACKET — CRACKED · airframe 21,406 hrs · 18,636 cycles

SINGLE POINT REFUEL/DEFUEL RECEPTACLE MOUNT STRUCTURE IS CRACKED LWR O/B CORNER. REMOVED AND REPLACED SINGLE POINT REFUEL/DEFUEL MOUNT STRUCTURE BRACKET IAW CRJ200 SRM'S 51-42-06.

Part: ATTACH BRACKET — CRACKED (BS 461) · airframe 21,406 hrs · 18,636 cycles

R/H WING TO FUSELAGE PANEL ATTACHMENT BRACKET FS. 461 IS CRACKED. REMOVED & REPLACED BRACKET BS 461.00 IAW SRM 51-42-06.

Part: ATTACH BRACKET — CRACKED (BS 449) · airframe 21,406 hrs · 18,636 cycles

RIGHT WING TO FUSELAGE PANNL ATTACHMENT BRACKET BS 449.85 IS CRACKED. REMOVED & REPLACED BROKEN BRACKET IAW SRM 51-42-06.

Part: OXYGEN MASK — DAMAGED (SEAT 4AC) · airframe 21,406 hrs · 18,636 cycles

OXYGEN MASK AT 4AC HAS CUT SUPPLY LINE. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-21-09-020-801, 35-21-09-860-802, 35-21-09-020-801, 35-21-09-420-801 AND 35-21-09-860-802.

Part: OXYGEN MASK — DAMAGED (SEAT 6AC) · airframe 21,406 hrs · 18,636 cycles

OXYGEN MASK AT SEAT 6AC HAS CUT SUPPLY LINE. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-21-09-020-801, 35-21-09-860-802, 35-21-09-020-801, 35-21-09-420-801 AND 35-21-09-860-802.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 21,406 hrs · 18,636 cycles

FLIGHT DECK LT WINDSHIELD SIDE POST AFT FITTING IS CRACKED. REMOVED AND REPLACE WINDSHIELD SIDE POST FITTING IAW SRM 51-42-21.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 21,406 hrs · 18,636 cycles

STRINGER CLIP 3L BS 280 IS CRACKED. REMOVED AND REPLACE THE STRINGER CLIP IAW SRM 51-40-11, SRM 51-24-21, AND SRM 51-42-06.

Part: MOUNT — CORRODED (GALLEY) · airframe 21,406 hrs · 18,636 cycles

FWD INBD GALLEY MOUNT IS CORRODED. REMOVED AND REPLACED THE GALLEY MOUNT IAW SRM 51-42-06.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 21,348 hrs · 18,583 cycles

LAST ROWS OF EMERGENCY FLOOR LIGHTS ARE OUT. FOUND LOOSE CONNECTOR ON EMERGENCY LIGHT STRIP, SECURED CONNECTOR. OPS CHECKED GOOD IAW AMM 33-51-01.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 20,339 hrs · 17,603 cycles

ON FLIGHT 4109 (DAY TO MSP) FUEL SMELL IN ACS WHEN BLEEDS ARE TURNED ON FROM APU. RESIDUAL SMELL REMAINED THROUGHOUT FLIGHT. CREW NOTED SMELL PRESENT WHEN BLEED SOURCE FROM APU. SMELL DISSIPATED WITH APU OFF AND ENGINE BLEEDS ON. COMPLETED LEAK CHECK OF APU AND NOTED NO EXTERNAL LEAKS PRESENT. VERIFIED SMELL PRESENT WITH APU BLEED ON. COMPLETED WORKSCOPE ISSUED BY MOTR GROUP. REPLACED LEFT AND RIGHT COALESCER SOCKS IAW AMM 21-51-13. PERFORMED LEFT AND RIGHT PACK BURN VIA ENGINE BLEEDS. NO SMELL NOTED. PLACED APU WITH INLET DOOR CLOSED ON MEL 49-10-11(C). MAINTENANCE PROCEDURES COMPLIED WITH. PLACARDED APU START PANEL. AIRCRAFT OK FOR SERVICE.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 19,712 hrs · 16,994 cycles

FLIGHT ATTENDANT LIFE VEST BAG TORN. REMOVED AND REPLACED FLIGHT ATTENDANT LIFE VEST IAW AMM 25-61-03.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 19,315 hrs · 16,593 cycles

PASSENGER DOOR VERY DIFFICULT TO OPEN. INSPECTED, CLEANED AND LUBED DOOR AFTER OPENING AS REQUIRED. DOOR OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,247 hrs · 16,534 cycles

GAS ODOR IN AIRCRAFT WHEN BLEEDS SWITCHED TO APU. REMOVED AND REPLACED APU COOLING FAN IAW AMM 49-52-05. LEAK AND OPS CHECKED GOOD.

Part: LATCH — OUT OF ADJUST (PAX DOOR) · airframe 19,104 hrs · 16,399 cycles

MAIN CABIN DOOR HANDLE HARD TO RELEASE ON OPENING ALSO DURING CLOSE OUTER LATCH NOT FLUSH. ADJUSTED PAX DOOR LATCH MECHANISM IAW AMM 52-11-21. OPS CHECKED GOOD, AIRCRAFT OK FOR SERVICE.

Part: HANDLE — BINDING (PAX DOOR) · airframe 18,811 hrs · 16,099 cycles

MAIN PASSENGER DOOR HANDLE IS JAMMING AND DIFFICULT TO OPEN AND CLOSED. COMPLIED WITH OPS CHECK OF PASSENGER DOOR IAW AMM 52-10-00. NO DEFECTS NOTED.

Part: WARNING SYSTEM — INTERMITTENT (COCKPIT) · airframe 18,086 hrs · 15,374 cycles

AIR RETURN FOR IDG NR 2 CAUTION MSG INTERMITTENT ON CLIMBOUT.

Part: WIRE — BROKEN (ELT) · airframe 18,032 hrs · 15,367 cycles

REPLACED ELT ASSY DUE TO BROKEN WIRE INSIDE OF UNIT. REMOVED AND REPLACED ELT IAW AMM 25-62-01. OPS CHECKED GOOD.

Part: WIRE — BROKEN (ELT) · airframe 18,032 hrs · 15,367 cycles

REPLACE ELT ASSY DUE TO BROKEN WIRE INSIDE OF UNIT & BATTERY EXPIRES MAR/2012. REMOVED AND REPLACED ELT IAW AMM 25-62-01. OPS CHECK GOOD.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,001 hrs · 15,333 cycles

AFT BULKHEAD (FS 621) CRACKED AT LINTEL FITTINGS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,001 hrs · 15,333 cycles

FWD PRESS BULKHEAD CRACKED AT PARKING BRAKE CABLE PASS-THRU.

Part: SHAFT — SATURATED (TE FLAP) · airframe 16,381 hrs · 13,655 cycles

FLAPS FAIL CAUTION MESSAGE (8 DEGREES) AT 4000 FT MSL ON APPROACH INTO DTW. NOTIFIED ATC - DECLARED AN EMERGENCY - DISCONTUNUED THE APPROACH. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD2009-06-12 PARAGRAPH (H) 96 (I), AMOC DATED MARCH 27,2009,TR#27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD27-052G. REMOVED WATER CONTAMINATION FROM LT NR 4 FLEXSHAFT IAW AMM 27-53-10. OPS CHECKS GOOD. FECU CODES-JAM, PDU DIFFERENTIAL, UNSPECIFIED 5 1A, 5 2B, 17 1B, 17 2A, 9 2A.

Part: COAX — LOOSE (RADIO ALTIMETER)

GEAR WARNING HORN AT 235 KIAS WITH THRUST LEVERS AT IDLE. GEAR WARNING ASSOCIATION WITH RAD ALT CODES IN PSEU. FOUND LOOSE COAX CABLES ON NR 1 & NR 2 RAD ALT. TIGHTENED CABLES IAW CRJ 200 AMM 34-44-01. OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: PROXIMITY SENSOR — DIRTY (LANDING GEAR) · airframe 17,915 hrs · 15,251 cycles

GEAR WARNING HORN INTERMITTENT ON APPROACH. FLAPS AT 20 AND THRUST AT 50 PERCENT. AIRSPEED 180-200 KTS. SEEMS TO BE AN ISSUE WITH THE THRUST QUADRANT. PERFORM BIT + F/C OF PSEU IAW CRJ 200 AMM 32-61-01. NO FAULTS FOUND. PERFORMED VISUAL INSPECTION AND CHECKED CLEARANCES OF ALL NLG AND MLG PROX SENSORS IAW CRJ200 AMM 32-61-05. ALL CLEARANCES WITHIN SPECS BUT DIRTY. CLEANED DIRTY PROX SENSORS IAW CRJ200 AMM 32-61-01. RE-PERFORMED BIT AND F/C IAW CRJ200 AMM 32-61-01. NO CODES FOUND. OKAY FOR SERVICE.

Part: GENERATOR — FAILED (NR 2) · airframe 19,902 hrs · 15,190 cycles

FLT 3850-20 DID AN AIR RETURN DUE TO GEN 2 FAILURE. HYD EDP WAS PREVIOUSLY DEFERRED AND CAN`T HAVE BOTH INOP. NO EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY IN MEM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,876 hrs · 15,165 cycles

CLIPS CRACKED AT 280.00 FLOORBEAM RBL 9 AND LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORPORATION STANDARD REPAIR 601R-53-0110.

Part: SKIN — DENTED (FUSELAGE) · airframe 17,498 hrs · 14,946 cycles

THE FUSELAGE SKIN TO BE DENTED APPROXIMATELY 2.5 FORWARD OF FS 654 BETWEEN S-2OL AND S-21L. REPAIRED IAW EA CRJ253-00188 REV A AS APPROVED BY ASSOCIATED 8110-3 DATED 11/7/2011.

Part: RIB — CRACKED (LT WING) · airframe 17,876 hrs · 15,165 cycles

LEFT WING BATT RIB ASSEMBLY AT WS 53.60 CRACKED AT TOP AFT FASTENER APPROXIMATELY 1 INCH LONG. REPAIRED IAW BOMBARDIER REO 601R-57-51-046.

Part: SPAR — DAMAGED (LT WING) · airframe 17,876 hrs · 15,165 cycles

NR 30 HOLE DRILLED IN LT FWD SPAR FLANGE AT WS 349. REPAIRED IAW BOMBARDIER REO 601R-57-21-1539.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 17,710 hrs · 15,013 cycles

GROUND SPOILER DEPLOY ADVISORY MSG DURING TAXI OUT. STATUS PAGE SHOWS SPOILERONS AND I/B GROUND SPOILERS DEPLOYED. CYCLED CB'S PER CRJ FIM. MESSAGE CLEARED OK FOR SERVICE.

Part: SECU — MALFUNCTIONED (SPOILER) · airframe 17,053 hrs · 14,383 cycles

LEFT FLT SPOILER DEFLECTED UNCOMMANDED IN CRUISE BRIEFLY. REMOVED AND REPLACED RT NR 2 SECU IAW AMM 27-61-05. OPS CHECK NORMAL, HAVE VERIFIED PART AFFECTIVITY.

Part: A/C PACK — FAULTY (AC BAY) · airframe 16,921 hrs · 14,257 cycles

CABIN AIR CONTAMINATION WITH APU AND PACKS ON. CREW REPORTED SMOKE IN CABIN. FIRE DEPARTMENT CALLED. DEFERRED RT PACK PER MEL 21-51-01.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 16,699 hrs · 14,090 cycles

8908 FLT 4210 MEM-CMH IS RETURNING TO MEM FOR SMOKE IN LAV (FALSE) INDICATION. NO EMERGENCY DECLARED. MX REMOVED AND REPLACED LAV SMOKE DETECTOR IAW AMM 26-16-01, OP CHECK GOOD.

Part: SKIN — DENTED (SPOILER) · airframe 16,218 hrs · 13,606 cycles

TWO DENTS WERE FOUND ON THE RIGHT WING INBOARD BOARD GROUND SPOILER UPPER SURFACE: .584 DIA X .003 DEEP, .629 DIA X .004 DEEP. REPAIRED IAW STS ENGINEERING EA 9-2011-22.

Part: SKIN — DENTED (SPOILER) · airframe 16,218 hrs · 13,606 cycles

DENT WAS FOUND ON THE LEFT WING OUTBOARD BOARD GROUND SPOILER UPPER SURFACE: .667 DIA X .005 DEEP. REPAIRED IAW STS ENGINEERING EA 9-2011-23.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 15,915 hrs · 13,331 cycles

TWO FASTENERS IN THE FUSELAGE LEFT SIDE ACCESS PANEL 131AL WERE DAMAGED. THE TWO DAMAGED FASTENERS WERE AT THE 12 O’CLOCK POSITION AND THE 6 O’CLOCK POSITION. AT THE 12 O’CLOCK LOCATION, THE CRUCIFIX RECESS WAS STRIPPED AND THE FASTENER COULD NOT BE REMOVED. AT THE 6 O’CLOCK POSITION, THE COUNTERSUNK HEAD SHEARED OFF. THE FASTENERS ARE P/N NAS1581A3T3 REDUCED HEAD COUNTERSUNK HEAD SCREWS. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-287. AT THE NEXT A CHECK MAINTENANCE INTERVAL, NOT TO EXCEED 500 FH, REMOVE AND REPLACE THE DAMAGED FASTENERS IAW STS ENGINEERING EA 5-2010-287, SRM 51-40-11, AMM 53-10-34-000-801 AND AMM 53-10-34-400-801.

Part: PRESSURE SWITCH — FAILED (ANTI-ICE SYSTEM) · airframe 15,839 hrs · 13,253 cycles

RT COWL ANTI ICE CAUTION. REMOVED AND REPLACED COWL ANTI ICE PRESS SWITCH IAW AMM 30-22-07. OPS CHECK GOOD.

Part: PUMP — WORN (ZONE 400) · airframe 14,780 hrs · 12,307 cycles

AT CRUISE ALTITUDE OF FL330 ON A REVENUE FLIGHT FROM KAUS TO KMEM, THE R ENG OIL PRESS WARNING MESSAGE ILLUMINATED. THE FLIGHT CREW COMPLETED THE QRH AND CONTACTED COMPANY DISPATCH AND MAINTENANCE. BECAUSE OF PREVIOUS OIL PRESSURE FLUCTUATION WRITE UPS ON THIS AIRCRAFT AND ENGINE, THE FLIGHT CREW ELECTED TO DIVERT TO KLIT. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KLIT. MAINTENANCE REPLACED THE LUBE AND SCAVENGE PUMP ON THE RIGHT ENGINE. GROUND RUNS WERE NORMAL AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — DEFECTIVE (LT ENGINE) · airframe 13,963 hrs · 11,543 cycles

WHEN REDUCING THRUST FOR DESCENT INTO KDTW, IT WAS OBSERVED THAT THE LEFT ENGINE HAD LIMITED RESPONSE TO THRUST INPUT. WITH THE THRUST LEVER AT IDLE, THE ENGINE WOULD NOT RETARD BELOW 66-68 PERCENT N1. THE FLIGHT CREW PERFORMED THE QRH, CONTACTED ATC AND COMPANY MAINTENANCE. THE FLIGHT CREW ESTABLISHED THE AIRCRAFT INTO THE TERMINAL AREA, DECLARED AN EMERGENCY AND SHUT DOWN THE LEFT ENGINE. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KDTW. MAINTENANCE DETERMINED THE LEFT MAIN FUEL CONTROL WAS DEFECTIVE. THE FUEL CONTROL WAS REPLACED AND GROUND RUNS WERE PERFORMED. ENGINE CONTROL AFTER THE FUEL CONTROL CHANGE WERE NORMAL AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUT — UNDERSERVICED (NLG) · airframe 13,184 hrs · 10,801 cycles

ON APPROACH INTO KDTW, THE FLIGHT CREW CONFIGURED THE AIRCRAFT FOR LANDING. DURING THE LOWERING OF THE LANDING GEAR, BOTH CREW MEMBERS HEARD AN ABNORMAL SOUND FROM THE NOSE LANDING GEAR AREA. THIS WAS FOLLOWED BY THE ILLUMINATION OF THE MASTER WARNING GEAR DISAGREE MESSAGE. THE FLIGHT CREW REQUESTED KDTW TOWER FOR A LOW PASS TO DETERMINE IF THE NOSE GEAR WAS DOWN. KDTW APPROVED THE LOW PASS AND DETERMINED THAT THE NOSE GEAR DOORS WERE OPEN, BUT THE NOSE GEAR WAS NOT DOWN. THE FLIGHT WAS CLEARED TO 4000 FEET AND THE CREW PERFORMED THE QRH. THE LANDING GEAR WAS CYCLED AND INDICATED THREE DOWN AND GREEN. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KDTW. MAINTENANCE DETERMINED THAT THE NOSE GEAR STRUT WAS UNDER SERVICED. THE STRUT WAS SERVICED AND A GEAR EXTENSION AND RETRACTION CHECK WAS PERFORMED IAW AMM 32-30-00. NO DEFECTS WERE NOTED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — FAILED (TE FLAPS) · airframe 12,914 hrs · 10,539 cycles

FLIGHT 2816 ALB/DTW WHEN FLAPS SELECTED DOWN ON APPROACH RECEIVED "FLAPS FAIL" MESSAGE, QRH FOLLOWED WITH UNEVENTFUL LANDING. SYSTEM TROUBLESHOT PER BOMBARDIER FIM FOUND FLAP ELECTRONIC CONTROL UNIT (FECU) FAILED. REMOVED AND REPLACED THE FECU PER BOMBARDIER AMM, OPERATIONAL TEST PERFORMED WITH NO DEFECTS.

Part: EXHAUST DUCT — FIRE (APU)

DURING POSTFLIGHT WALKAROUND AT KIDA, THE FIRST OFFICER SPOTTED AN APU EXHAUST PIPE FIRE. THE CAPTAIN PUSHED THE APU FIRE SWITCH AND WHEN THE FIRE CONTINUED, DISCHARGED THE APU FIRE BOTTLE. THE FIRE ABATED TEMPORARILY, BUT THEN REIGNITED. THE FIRST OFFICER EXTINGUISHED THE FIRE WITH A PORTABLE FIRE EXTINGUISHER SUPPLIED BY GROUND PERSONNEL. MAINTENANCE INSPECTED THE APU AND DETERMINED THERE WAS NO FIRE OUTSIDE OF THE APU ITSELF. THE APU WAS DEFERRED PER ESTABLISHED COMPANY PROCEDURES AND THE ACFT RELEASED FOR SERVICE. (S)

Part: FLAP — MALFUNCTIONED (WING) · airframe 5,724 hrs · 4,619 cycles

RECEIVED -FLAP FAIL- MESSAGE ON TAXI OUT. RETURNED TO BLOCKS. SYSTEM RESET PER AD 98-20-01 AND PLACED ON 72 HOUR WATCH.

Part: COALESCER BAG — CONTAMINATED (A/C BAY) · airframe 5,309 hrs · 4,250 cycles

ABORTED TAKEOFF DUE TO SMOKE IN COCKPIT AND CABIN. MAINT INVESTIGATED FOUND ACM WATER SEPARATOR SOCKS CONTAMINATED WITH ENGINE OIL. ACM SYSTEM DEFERRED PER MEL.

Part: LANDING GEAR — NONE · airframe 5,140 hrs · 4,103 cycles

ON APPROACH WHEN SELECTING GEAR DOWN MAINS SHOWED DOWN AND LOCKED NOSE SHOWED IN RED. EMERGENCY DECLARED, RAH FOLLOWED WITH UNEVENTFUL LANDING. MAIN PULLED PSEUDO CODES AND PERFORMED OPERATIONAL AND FUNCTIONAL CHECKS PER AM WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: FLAP — MALFUNCTIONED (WING)

FLAPS FAILED ON CLIMB OUT FROM DSM QRH FOLLOWED CONTINUED WITH UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD98-20-01.

Part: FCU — FAILED (TE FLAPS)

FLAP FAILURE ON TAXI. REMOVED AND REPLACED FECU, FLAP ELECTRONIC CONTROL UNIT. (M)