N820AY

Part: RELAY — INOPERATIVE · airframe 31,964 hrs · 30,057 cycles

AT GATE WITH AC POWER ON AIRCRAFT EMER LIGHTS ON STATUS COMES ON WHEN EMER LIGHTS ARE ARMED REMOVED AND REPLACED AC ESS BUS SENSE (K1XD) IAW CRJ-200 AMM 24-51-27. OPS TEST GOOD EMERGENCY LIGHTS ARE BACK IN WORKING ORDER.

Part: BATTERY — INOPERATIVE (EMEGENCY LIGHT) · airframe 80,199 hrs · 27,867 cycles

FWD EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED FWD EMERGENCY LIGHT BATTERY, IAW CRJ 200 AMM 33-51-04. P/N OFF AD-2013-1A S/N OFF 85293, P/N ON 2013-1ASMI S/N ON 12738. OPERATIONS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,595 hrs · 27,166 cycles

EMERGENCY LIGHTS WILL NOT ILLUMINATE REMOVED AND REPLACED BATTERY PACK ASSEMBLY IAW CRJ 200 AMM 33-51-04 P/N ON/OFF AD-2013-1A S/N ON 85293 S/N OFF 177931

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,133 hrs · 25,642 cycles

FOUND EMERGENCY LIGHTING INOP. REMOVED AND REPLACED BATTERY PACK #4 IAW CRJ 200 AMM 33-51-04. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY #4 IAW CRJ 200 AMM 33-51-05. OPS CHECK GOOD.

Part: TORQUE BOX — CRACKED (THRUST REVERSER) · airframe 28,127 hrs · 25,636 cycles

LH THRUST REVERSER HAS A CRACK NEAR BLOCKER DOOR #9. REPAIRED LH THRUST REVERSER NEAR BLOCKER DOOR #9 IAW IAW REO 601R-78-30-26-16 AAR SM 33

Part: PLATE — CRACKED (CARGO STEP) · airframe 28,127 hrs · 25,636 cycles

CRACK IN FWD RADIUS OF CARGO STEP PLATE FOUND. REMOVED CRACK AND FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 52-00-00 AAR AP 377

Part: FRAME — CORRODED (BS 349) · airframe 28,127 hrs · 25,636 cycles

FRAME 349 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STGR 26L AND 26R, IN THE FWD E & E BAY. REMOVED/REPLACED LWR FRAME SECTOR 349 IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-21 PERFORMED OPS TEST GOOD IAW CRJ 200 AMM 22-12-00-710-802 AAR SM 33

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 28,127 hrs · 25,636 cycles

LBL 27 O/B LANDING HAS CORROSIN BETWEEN FS 605 AND FS 621, IN THE CARGO BAY. INSTALLED REPAIR STRAP IAW EA CRJ253-08726 REV. IR.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 28,127 hrs · 25,636 cycles

CARGO DOOR I/B UPPER FWD BACK-UP FITTING IS CRACKED. REMOVED AND REPLACED CARGO DOOR 1B UPPER FWD BACK-UP FITTING IAW CRJ 200 SRM 51-42-10.

Part: SEAT TRACK — CORRODED (BS 405-409) · airframe 28,127 hrs · 25,636 cycles

RIGHT HAND SEAT TRACK, STICK #2 HAS SEVERAL AREAS OF CORROSION. REMOVED/REPLACED WITH NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11.

Part: SEAT TRACK — CORRODED (RT CABIN) · airframe 28,127 hrs · 25,636 cycles

RIGHT HAND SEAT TRACK, STICK #6 HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED · airframe 28,127 hrs · 25,636 cycles

RIGHT HAND SEAT TRACK, STICK #4 HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED · airframe 28,127 hrs · 25,636 cycles

LEFT HAND SEAT TRACK, STICK #2 HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED LT SEAT TRACK #2 PART #601R 31/032-21 IAW AMM 63-01-11.

Part: SPAR — NICKED (NR 1 PYLON) · airframe 28,127 hrs · 25,636 cycles

1 ENG PYLON FWD MOUNT AFT UPPER HOLE HAS TWO NICKS COMPLIED WITH BOMBARDIER REO 601R-54-51-193 DATED:3/15/2019 TO REMOVE NICK DAMAGE BY BLENDOUT, ROTOPEEN AND RESTORE FINISH (MATERIAL LOSS A:.325LX.325LX.175"W X.004" D). AAR SM 39

Part: SEAT TRACK — CORRODED (BS 559) · airframe 28,127 hrs · 25,636 cycles

SEAT TRACK ON TOP OF RBL 27 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED/REPLACED SEAT TRACK IAW CRJ 200 AMM 53-00-49 AAR SM 58

Part: INTERCOSTAL — CRACKED (EXHAUST NOZZLE) · airframe 28,127 hrs · 25,636 cycles

R/H ENGINE EXHAUST NOZZLE HAS BENT INTERCOSTAL BY O/B ACCESS PANEL INNER SECTION. REMOVED AND REPLACED WITH NEW INTERCOASTAL ON R/H ENGINE EXHAUST NOZZLE O/B INNER SECTION I.A.W. CRJ-200 BOMB CMM 20-42-06 AND CMM 20-42-20.

Part: FLOOR SUPPORT — CRACKED (BS 473.15) · airframe 28,127 hrs · 25,636 cycles

RH OVERWING ACCESS PNL SUPPORT BRACKET AT FS473.15 IS CRACKED. REMOVED AND REPLACED R/H OVERWING SUPPORT BRACKET @ F.S. 473.15 I.A.W. CRJ-200 SRM 51-42-06 AND 51-42-21.

Part: BULKHEAD WEB — GOUGED (BS 621) · airframe 28,127 hrs · 25,636 cycles

REAR PRESSURE BULKHEAD HAS GOUGE ON PREVIOUS REPAIR ON RBL18.00. REMOVED AND REPLACED GOUGED TRIPLER IAW REO 601R-53-61-1285 REV. E REO 601R-53-61-6918. AAR SM 33

Part: FLOORBEAM — CRACKED (BS 460) · airframe 28,127 hrs · 25,636 cycles

UNDER 262CRF AT RBL9 FS460 THERE IS A CRACKED ANGLE BRACKET. MARKED BY RED PENCIL. REMOVED CRACKED FITTING FS 460 RBL-9 AND INSTALLED NEW FITTING IAW CRJ 200 SRM 51-42-21 AAR SM 39

Part: BULKHEAD WEB — GOUGED (BS 621) · airframe 28,127 hrs · 25,636 cycles

REAR PRESSURE BULKHEAD IS GOUGED ON PREVIOUS REPAIR AT RBL 36.20. REMOVED AND REPLACED GOUGED TRIPLER IAW BOMBARDIER REO 601R-53-61-1285 REV. E REO 601R-53-61-6918. AAR SM 33

Part: BULKHEAD WEB — GOUGED (BS 621) · airframe 28,127 hrs · 25,636 cycles

REAR PRESSURE BULKHEAD IS GOUGED AT PREVIOUS REPAIR AT RBL27.50. REMOVED AND REPLACED GOUGED TRIPLER IAW BOMBARDIER REO 601R-53-61-1285 REV. E. REO 601R-53-61-6918. AAR SM 33

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 28,127 hrs · 25,636 cycles

AFT PRESSURE BULKHEAD WEB HAS A CRACK AT BL 0 AND WL 111. REPAIRED CRACK IN AFT PRESSURE BULKHEAD IAW BOMBARDIER REO 601R-53-61-1285 REV. C.

Part: BULKHEAD — GOUGED (BS 621) · airframe 28,127 hrs · 25,636 cycles

REAR PRESSURE BULKHEAD FWD FACE IS GOUGED IN 2EA AREAS. BLENDED DAMAGE IAW CRJ 200 SRM TR51-41. MATERIAL LOSS OF .010 WITHIN LIMITS IAW BOMBARDIER REO 601R-53-61-2155 REV. A.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 28,127 hrs · 25,636 cycles

RH SIDEWALL SEAT TRACK STICK 3 HAS CORROSION SPOTS BETWEEN FS 409+16 THRU FS 409+112, IN THE CABIN. REMOVED/REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11 AAR SM 58

Part: ANGLE — CRACKED (BS 529) · airframe 28,127 hrs · 25,636 cycles

UNDER FLOORBOARD 262DRF AT RBL27 AT OR AROUND FS529.0 THERE IS A CRACKED ANGLE BRACKED. MARKED BY RED PENCIL. REPLACED CRACKED ANGLE UNDER FLOORBOARD AT RBL27 AND FS529 IAW CRJ 200 SRM 51-42-21. AAR SM 33

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 28,127 hrs · 25,636 cycles

AFT PRESURE BULKHEAD AFT FACE HAS ANGLE AT STR15 ON R/H HAS CRACK. REMOVED AND REPLACED WITH NEW R/H ANGLE ON AFT PRESSUR BULKHEAD AFT FACE AT STR 15 IAW CRJ 200 SRM 51-42-06. AAR SM 58

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 28,127 hrs · 25,636 cycles

AFT PRESURE BULKHEAD AFT FACE HAS ANGLE AT STR15 ON L/H HAS CRACK. REMOVED AND REPLACED WITH NEW L/H ANGLE ON AFT PRESSURE BULKHEAD AFT FACE AT STR15 IAW CRJ 200 SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 364-405) · airframe 28,127 hrs · 25,636 cycles

LEFT HAND SEAT TRACK, STICK #1 HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACE SEAT TRACK IAW CRJ 200 AMM 53-01-11.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 28,127 hrs · 25,636 cycles

UNDER FLOORBOARD 261DLF BETWEEN LBL36 AND LBL27 AT OR AROUND FS484 THERE IS A CRACKED ANGLE BRACKET IN BOTH CORNERS. REPLACED CRACKED ANGLE AT LBL36 AT FS484 IAW REO #601R-53-41-059 AND ANGLE AT LBL27 AND FS484 IAW CRJ 200 SRM 51-42-21. AAR SM 33

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 27,794 hrs · 25,286 cycles

VERT BEAM RBL 18 AT FS 409+128 IS CRACKED LWR O/B FLANGE STARTING AT EDGE EXTENDING UP TO 1ST RIVET. COMPLETED REPAIR TO FS 128+ 128 RBL 18 O/B FLANGE IAW REO 601R-53-41-2410. REFERENCE CONTINUATION CARDS 114960 AND 114965 FOR DETAILS. THIS IS A MAJOR REPAIR.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 27,794 hrs · 25,286 cycles

VERT BEAM RBL27.00 AT FS 409.0 +128 IS CRACKED LWRIB STAARTING AT EDGE EXTENDING UP TO POAST 1ST RIVET BUT DOESNT EXTEND ALL THE WAY UP TO 2ND RIVET COMPLETED PERMANENT REPAIR TO FS409+128 RBL 27 LWR IB FLANGE IAW REO 601R-53-41-0056 REV F SEE CONT CARD 114961 FOR DETAILS

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 27,794 hrs · 25,286 cycles

VERT BEAM LBL 27.00 AT FS 409.0 +128 IS CRACKED LWROB FLANGE STARTING AT EDGE EXTENDING UP TO 1ST RIVET. COMPLETED REPAIR TO 409+128 VERT BEAM LBL 27 LWROB FLANGE IAW REO601R-53-41-0056 REV F.

Part: VERTICAL BEAM — CRACKED (FUSELAGE) · airframe 27,794 hrs · 25,286 cycles

VERT BEAM LBL 18.00 AT FS 409.0 +128 IS CRACKED LWROB FLANGE STARTING AT EDGE EXTENDING UP TO 1ST RIVET. COMPLETED PERMANENT REPAIR TO FS 409 +128 LBL 18 LWROB FLANGE IAW REO 601R-53-41-0056 REV F.

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY) · airframe 27,390 hrs · 24,848 cycles

LAV 02 MASK DEPLOYED. REPACKED 02 MAKS IAW AMM 35-21-03. NO DEFECTS NOTED AT THIS TIME.

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY) · airframe 27,280 hrs · 24,715 cycles

OXYGEN MASKS IN THE LAVATORY DROPPED. INSPECTED AND RESTOWED THE LAVATPRU OXYGEN MASKS IAW AMM 35-21-09.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 26,831 hrs · 24,222 cycles

F/A FLASHLIGHT NOT CHARGING IN CRADLE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY PACK REF AMM 25-61-02 OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,657 hrs · 22,944 cycles

RIGHT AND LEFT OVERWING EMERGENCY LIGHTS ARE OUT, ALL EMERGENCY LIGHTS RUNNING OFF BATTERY PACK INOPERATIVE. REMOVED AND REPLACED THE BATTERY CHARGER ASSY IAW AMM 33-51-05. CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,650 hrs · 21,863 cycles

DURING WALKAROUND, FOUND LEFT HAND AFT WING EMERGENCY LIGHT NOT ILLUMINATED. REPLACED THE LAMPS IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CRACKED (BS 621-625) · airframe 24,352 hrs · 21,563 cycles

BS 621 - 625 FLOOR SUPPORT IS CRACKED. REMOVED AND REPLACED IAW SRM 51-42-06, 51-42-21 AND 51-42-22.

Part: TORQUE BOX — CRACKED (THRUST REVERSER) · airframe 24,352 hrs · 21,563 cycles

NR 2 ENGINE THRUST REVERSER TORQUE BOX HAS CRACK FROM FASTENER HOLE AT 5 O’CLOCK POSITION. FOUND DURING FREEDOM OF MOVEMENT CHECK OF THRUST REVERSER. REPAIRED CRACK ON NR 2 THRUST REVERSER TORQUE BOX AT 5 O'CLOCK POSITION IAW REO 601R-78-30-2616.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

CABIN, LT SIDEWALL SEAT TRACK, STICK NR 4 HAS CORROSION AS MARKED. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW AMM 53-01-11. REMOVED CORROSION, NO ALLOWABLE DAMAGE IAW SRM 51-21-06 AND 53-21-49.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 24,352 hrs · 21,563 cycles

IN AFT CARGO AREA CARGO TRACK IS GOUGED AND CORRODED STA559+112 LBL9. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49 AND REO 601R-53-00-485.

Part: FLOOR SUPPORT — CRACKED (BS 621-625) · airframe 24,352 hrs · 21,563 cycles

BS 621 - 625 FLOOR SUPPORT IS CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-21 & 51-42-22

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

CABIN, RT SIDEWALL SEAT TRACK, STICK NR 6 HAS CORROSION AS MARKED. REMOVED AND REPLACED SEAT RAIL IAW AMM-53-01-11. NO ALLOWABLE DAMAGE IAW SRM 53-21-49.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

AFT PRESSURE BULKHEAD IS CRACKED AT LINTEL FITTING. REPAIRED AFT PRESSURE BULKHEAD AT LINTEL FITTING IAW REO 601R-53-61-1230 REV C.

Part: WEB — CRACKED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

FWD E&E FLOOR IS CRACKED AT FS 193 ON LT. REPAIRED E&E FLOOR FS 193 LT SIDE IAW REO 601R-53-11-081.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

CABIN, RT SIDEWALL SEAT TRACK, STICK NR 7 HAS CORROSION AS MARKED. BLENDED NR 7 RT SEAT TRACK OUT OF LIMITS NO ALLOWABLE DAMAGE IAW AMM 53-01-11. REPLACED WITH NEW SEAT TRACK IAW AMM 53-01-11.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

IN AFT CARGO APB FWD FACE HAS FOUR REPAIRS THAT ARE GOUGED. REMOVED AND REPLACED OUTER DOUBLER (4 EA) AFT CARGO FWD APB PER REO 601R-53-61-1285.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

CABIN, RT SIDEWALL SEAT TRACK, STICK NR 5 HAS CORROSION AS MARKED. REMOVED AND REPLACED CABIN RT SIDEWALL SEAT TRACK IAW AMM 53-01-11 NO ALLOWABLE DAMAGE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

CABIN, LT SIDEWALL SEAT TRACK, STICK NR 5 HAS CORROSION AS MARKED. REMOVED & REPLACED NR 5 LT SIDE SEAT RAIL IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

CABIN, LT SIDEWALL SEAT TRACK, STICK NR 7 HAS CORROSION AS MARKED. REMOVED & REPLACED NR 7 LT SIDE SEAT RAIL IAW AMM 53-01-11.

Part: STRIP — CHAFED (FAN COWL) · airframe 24,352 hrs · 21,563 cycles

NR 2 ENG LOWER FAN COWL T/E IS CHAFED IS SEVERAL AREAS. REMOVED AND REPLACED T/E IAW CMM-71-14-01.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

AFT PRESSURE BULKHEAD IS CRACKED AT TOP OF CARGO DOOR AFT TRACK. REPAIRED DAMAGE IAW REO 601R-53-61-1541 AND RESTORED FINISH IAW SRM 51-25-16. REPAIR HAS A THRESHOLD OR FINISH CYCLES 40, NO AND A REPEAT FLIGHT CYCLES OF 23860.

Part: MOUNT — DAMAGED (APU BAY) · airframe 24,352 hrs · 21,563 cycles

APU ENCLOSURE MOUNT ANGLE DAMAGED. REMOVED AND REPLACED MOUNT ANGLE IAW SRM 51-42-06.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,352 hrs · 21,563 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED BY ASSIST MOTOR CABLE PULLEY. REMOVED AND REPLACED DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

AFT CARGO DOOR SUPPORT BEAM LOWER AFT ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

CABIN, RT SIDEWALL SEAT TRACK, STICK NR 2 HAS CORROSION AS MARKED. REMOVED AND REPLACED RT NR 2 STICK SEAT TRACK IAW AMM 53-01-11. NO ALLOWABLE DAMAGE IAW SRM 53-21-49.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

FS 484.0 INTERCOSTAL OTBD OF LBL27 OTBD CLIP IS CRACKED. REMOVED & REPLACED ANGLE IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

CABIN, LT SIDEWALL SEAT TRACK, STICK NUMBER 2 HAS CORROSION AS MARKED. REMOVED AND PLACED CABIN LT SIDEWALL SEAT TRACK, STICK 2. NO ALLOWABLE DAMAGE LIMITS IAW SRM 53-21-49, AMM 53-01-11-400-802.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

CABIN, LT FLOOR SEAT TRACK, STICK NR 3 HAS SCRATCHES AND GOUGES. REMOVED AND REPLACED LT NR 3 SEAT TRACK IAW AMM 53-01-11, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

CABIN, LT FLOOR SEAT TRACK, STICK NR 1 HAS SCRATCHES AND GOUGES. REMOVED AND REPLACED LT FLOOR SEAT TRACK NR 1 STICK IAW AMM 53-01-11 TASK 51-23-00-390-810 STEPS 1-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 24,352 hrs · 21,563 cycles

CABIN, LT FLOOR SEAT TRACK, STICK NR 4 HAS SCRATCHES AND GOUGES. NR 4 LT SEAT TRACK DIMENSION U WAS BLENDED OUT OF LIMIT, ORG WAS .370 IAW DWG 56487 REV A BLEND OUT .030 REMAINING IS .340 OUT OF LIMITS IAW SRM 53-21-49. REPLACE SEAT TRACK IAW AMM 53-01-11.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,333 hrs · 21,544 cycles

EMERGENCY EXIT OVERHEAD FLOOD LIGHT AFT INOPERATIVE. R & R THE BULB OPS CHECK GOOD IAW AMM 33-51-00 .

Part: WIRE HARNESS — DAMAGED (MLG) · airframe 24,307 hrs · 21,520 cycles

AFTER GEAR RETRACTION RECEIVED GEAR DISAGREE WARNING MSG NOSE GEAR IN RED QRH COMPLIED AND GEAR SELECTED DOWN ( 3 GREEN INDICATION) AIRCRAFT LANDED UNDER LANDING LIMITATIONS. R & R SENSOR BRACKET IAW CMM M32-20-04 REPLACED NLG ELECTRICAL HARNESS PER AMM 32-61-25 SVC NLG STRUT PER AMM 12-12-32 ADJ BOTH NLG PROXIMITY SENSOR IAW AMM 32-61-05 SWUNG GEAR PER AMM 32-33-00 ALL OP CHECKED GOOD. OK FOR SERVICE.

Part: PACKING — LEAKING (FUEL CONTROL) · airframe 24,249 hrs · 21,459 cycles

STRONG ODOR OF FUEL IN THE COCKPIT AND CABIN. SEEMS WORSE IN THE COCKPIT AND FLUCTUATES IN INTENSITY SEEMINGLY AT RANDOM. SEEMS TO GET WORSE WHEN THE TEMPERATURE IS TURNED UP ON THE PACKS OR THE BLEEDS ARE ON THE APU. THE ODOR SEEMS TO BE MOSTLY THE OF FUEL. R & R FUEL CONTROL UNIT UNION PACKINGS IAW AMM 49-31-01. LEAK CHECKED GOOD, OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,224 hrs · 21,430 cycles

A VERY BAD ODOR OF EXHAUST IN FLIGHT DECK WHEN TEMP IS TURN UP. REMOVED AND INSPECTED WATER SEPERATOR FOR SIGNS OF OIL IAW AMM 21-51-13. NO SIGNS OF OIL OR ANY FLUID. PERFORMED INSPECTION OF ACM IAW AMM 21-51-13. LEFT ACM OIL WAS A FEW SHADES DARKER THAN THE RIGHT ACM. SYSTEM OPERATES AS DESIGNED

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 23,845 hrs · 21,046 cycles

F/O O2 MASK INOPERATIVE. R & R F/O O2 MASK IAW AMM 35-11-12. OPS CHECKS GOOD.

Part: CONNECTOR — UNSECURE (COCKPIT) · airframe 22,805 hrs · 19,970 cycles

CAPTAINS SIDE O2 MASK MIC DOES NOT WORK. SECURED CONNECTOR FOR CAPTAINS O2 MASK. COMPLETED OPERATIONS CHECKS OF O2 MASK IAW AMM 35-11-12. ALL CHECKED GOOD.

Part: TARGET — DAMAGED (MLG) · airframe 22,236 hrs · 19,397 cycles

GEAR DISAGREE WARNING MESSAGE ON CLIMB OUT. R & R RT UPLOCK TARGET IAW AMM 32-32-05. OPS CHECKED GOOD. PERFORMED GEAR SWING IAW AMM 32-30-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,175 hrs · 19,329 cycles

EMERGENCY LIGHT BULB, 3RD OVER BACK, CTR AISLE 15 INOPERATIVE. R & R BULB. OPERATIONS CHECKED GOOD IAW AMM 33-51-14.

Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 21,696 hrs · 18,801 cycles

GEAR DISAGREE WARNING ON FINAL APPROACH. NOSE GEAR WOULD NOT SHOW GREEN, RAN QRH, CYCLED GEAR 3 TIMES ON 3RD ATTEMPT LG ALL DOWN 3 GREEN. SUSPECTED NLG EXTENSION & RETRACTION ACTUATOR HYD IN INTERNAL LEAK. R & R NLG EXTENSION & RETRACTION ACTUATOR IAW AMM 32-33-0. OPERATIONS CHECKED GOOD.

Part: CONTROL VALVE — MALFUNCTIONED (BRAKE SYSTEM) · airframe 21,693 hrs · 18,798 cycles

AFTER LANDING THE BRAKES APPEARED TO LOCKUP. BTMS SHOWED A TEMPERATURE OF 9 ON THE RT INBD BRAKE. LOCKING WENT AWAY 5 MINUTES AFTER LANDING & THE BRAKES FELT NORMAL. REFER TO AML 3013148. R & R NR 3 BRAKE CONTROL VLV IAW AMM 32-43-06. LEAK & OPERATIONS CHECKED GOOD. REFER TO NON-ROUTINE CONTINUATION CARD N-68411.

Part: BYPASS VALVE — FAULTY (NLG) · airframe 21,685 hrs · 18,788 cycles

NOSE GEAR WOULD NOT COME DOWN UNTIL ALL HYD PUMPS WERE TURNED ON. REPLACED NLG BYPASS VLV IAW 32-34-35. OPERATIONS & LEAK CHECKED GOOD.

Part: MOTOR — FAILED (PAX DOOR ASSIST) · airframe 21,625 hrs · 18,729 cycles

MAIN CABIN DOOR ASSIST DOESN`T BRING DOOR UP ALL THE WAY. R & R PASSENGER DOOR POWER ASSIST MOTOR IAW AMM 52-11-08. OPS CHECKED GOOD.

Part: SEAL — DAMAGED (LAVATORY) · airframe 18,486 hrs · 21,381 cycles

AFT LAVATORY WALL SMOKE SEAL DAMAGED. R & R SMOKE SEAL ON UPPER OTBD EDGE OF LAVATORY AFT WALL IAW SRM 51-22-00.

Part: DOOR SEAL — TORN (EMERGENCY EXIT) · airframe 18,486 hrs · 21,381 cycles

LEFT OVERWING EMER EXIT SEAL IS TORN. R & R LT EMER EXIT SEAL IAW AMM 52-21-07. REFER TO NR RS-5, WO 55019-1000-0001 FOR OPERATIONS CHECK PERFORMED.

Part: FITTING — CHAFED (HORIZ STAB) · airframe 21,366 hrs · 18,472 cycles

HORIZONTAL STAB TRIM ACTUATOR LT UPPER FITTING NICKED & CHAFED. REPAIRED IAW REO 601R-55-11-501.

Part: ATTACH FITTING — DAMAGED (HORIZ STAB) · airframe 21,366 hrs · 18,472 cycles

HORIZONTAL STAB TRIM UPPER ATTACH FITTING ON INBD SIDE HAS TOOLING MARK 0.1 INCH LONG. REPAIRED IAW REO 601R-55-11-501.

Part: ACM — SEIZED (AC BAY) · airframe 20,910 hrs · 18,006 cycles

ON FINAL, ODOR LIKE SOMETHING BURNING & AS WE TAXIED IN, RT PACK OVERHEATED. CABIN TEMP ROSE TO 120C. RT ACM SEIZED. REPLACED PN OFF & ON 782790-15, SN OFF 2004090645 & SN ON 200490044 IAW AMM 21-51-10. OPERATIONS TESTED GOOD SEE NON-ROUTINE N54513 FOR DETAILS.

Part: BRAKE — MALFUNCTIONED (MLG) · airframe 20,531 hrs · 17,618 cycles

UPON EXITING RUNWAY BRAKES LOCKED, PUMPED SEVERAL TIMES BRAKES EVENTUALLY UNLOCKED PEAK BTMS 03. VERIFIED HYD RETURN MANIFOLD DELTA PINS NOT SET PERFORMED ASCU BIT CHECK ALL PASSED LT OTBD BRAKE TEMP 2 POINTS HIGHER THAN OTHERS. R & R LT OTBD BRAKE USING 200 AMM 32-43-26 AS REF, PN ON OFF 5010520-1 SN OFF NOV 01-3122 SN ON OCT 03-4363. BLEED LT OTBD & LT INBD BRAKES, REMOVED SIGNIFICANT AMOUNT OF AIR FROM BOTH SYSTEMS OPERATIONS CHECK OF BRAKE SYS GOOD.

Part: BRAKE SYS — CONTAMINATED (LEFT) · airframe 20,293 hrs · 17,376 cycles

ON LANDING AS WE TRANSFERRED CONTROLS THEN EXITED RWY 36R, THE LT BRAKE DID NOT RELEASE. A COUPLE SECONDS AFTER EXITING THE RNWY IT RELEASED. BRAKING FROM THAT POINT STILL FELT AS IF PARTIAL BRAKES WERE BEING APPLIED EVEN WHEN I WAS NOT APPLYING BRAKES. BLED LT INBD & LT OTBD MLG BRAKES IAW AMM 32-43-00. LT OTBD HAD LARGE QTY OF AIR. PERFORMED BRAKE CHECK IAW AMM 32-43-00 & TAXI CHECK, COULD NOT DUPLICATE STICKING BRAKE. BRAKE TEMPS NORMAL READING 3, 3, 4 & 3. OPERATIONS CHECKED GOOD, OK FOR SERVICE.

Part: BRAKE SYS — CONTAMINATED (MLG) · airframe 20,261 hrs · 17,353 cycles

UPON LANDING, APPLIED BRAKES & TR, WE BEGAN SLOWING AT A RATE NOT COINCIDING WITH AMOUNT OF PRESS. LET OFF BRAKES & IT WAS OBVIOUS A BRAKE OR BRAKES WERE STUCK. DID NOT NOTICE ONLY PULL TO THE LT OR RT SO BOTH MAIN BRAKES COULD HAVE BEEN LOCKED UP. EVIDENCE OF POSSIBLE SKID ON LHOB TIRE. BLEED LHOB BRAKES IAW AMM 32-43-00. OPERATIONS CHECK BRAKES & PERFORMED TAXI CHECK, NO DEFECTS NOTED.

Part: PBE — UNSERVICEABLE (CABIN) · airframe 20,154 hrs · 17,250 cycles

PBE IN AFT CABIN UNSERVICEABLE. R & R WITH SERVICEABLE PBE IN AFT CABIN IAW CRJ200 AMM 25-60-00.

Part: PBE — UNSERVICEABLE (CABIN) · airframe 20,154 hrs · 17,250 cycles

PBE IN GALLEY CLOSET UNSERVICEABLE. R & R WITH SERVICEABLE PBE IN GALLEY CLOSET IAW CRJ200 AMM 25-60-01.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 19,349 hrs · 16,442 cycles

WHEN SELECTED FLAPS 45, LT SIDE WAS AT 43, RT SIDE AT 45. PERFORMED OPS CHECK OF FLAP POSITION TRANSMITTERS IAW AMM 27-55-01. COULD NOT DUPLICATE DISCREPENCY. SYS CHECKS GOOD. OK FOR SERVICE.

Part: ACCESS PANEL — UNKNOWN (LT WING) · corrosion level 2 · airframe 19,340 hrs · 16,434 cycles

LEFT WING INBD TANK ACCESS PANEL 510AB AT WS54.897. REPAIRED IAW REO 601R-57-21-030.

Part: POST — CRACKED (BS 559 BULKHEAD) · airframe 19,340 hrs · 16,434 cycles

FS 559 SEMI-PRESSURE BULKHEAD, RBL 9 INBD POST CRACKED FROM LOWER EDGE PAST FIRST RIVET FROM BOTTOM EDGE. REPAIRED IAW REO 601R-53-41-057.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 19,187 hrs · 16,277 cycles

EMERGENCY LIGHTS NOT WORKING PROPERLY. POWERED ACFT AND CHARGED EMERGENCY LIGHT BATTERY. OPERATES NORMALLY AT THIS TIME.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,446 hrs · 15,553 cycles

FS 280 BULKHEAD LOW WEB CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-926.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 18,446 hrs · 15,553 cycles

RIGHT ELEVATOR UPPER SKIN AT TRAILING EDGE HAS LIGHTNING STRIKE DAMAGE AT ES69.1. REPAIRED IAW BOMBARDIER REO 601R-55-21-030.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 18,446 hrs · 15,553 cycles

RIGHT ELEVATOR LOWER SKIN AT TRAILING EDGE HAS LIGHTNING STRIKE DAMAGE AT ES94.52. REPAIRED IAW BOMBARDIER REO 601R-55-21-030.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,446 hrs · 15,553 cycles

PARKING BRAKE CABLE PASS THRU HOLE IS CRACKED ON PRESSURE BULKHEAD AT FS 202.75 AND LBL 23.75. REPAIRED IAW BOMBARDIER REO 601R-53-11-563.

Part: WEB — CRACKED (FUSELAGE) · airframe 18,446 hrs · 15,555 cycles

FS 280 WEB CRACKED JUST OUTBOARD OF LBL 9 ON LOWER ANGLE. REPAIRED IAW BOMBARDIER REO 601R-53-11-926.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,054 hrs · 15,163 cycles

CAPTAINS EMERGENCY FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED CAPTAIN'S EMERGENCY BATTERY IAW AMM 25-60-00. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,185 hrs · 14,302 cycles

OVERHEAD CABIN EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED OVERHEAD CABIN EMERGENCY LIGHT IAW AMM 33-50-00.

Part: PBE — DAMAGED (COCKPIT) · airframe 16,848 hrs · 13,979 cycles

PBE IN COCKPIT APPEARS VIOLATED. DISK IS NOT LIGHT BLUE BUT DARK IN COLOR. BAG IS NO LONGER VACUUM SEALED AND RED DUCK TAPE IS NO LONGER HOLDING SECURELY AROUND BAG. REMOVED AND REPLACED CREW PBE IAW ESSEX CREW PBE CMM. OK FOR SERVICE.

Part: MCU — DEFECTIVE (HORIZ STAB) · airframe 16,192 hrs · 13,393 cycles

STAB TRIM NR 1 + 2 AND MACH TRIM DISENGAGED MULTIPLE TIMES DURING FLT WITH AUTO-PILOT NOT NOT ENGAGED WOULD RESET MOMENTARILY ONCE AUTO PILOT WAS ENGAGED ONLY STAB TRIM CHANNEL 1 STATUS MESSAGE APPEARED 3 TIMES. R/R STAB TRIM ACTUATOR IAW AMM 27-42-01. OP/C GOOD. REMOVED AND REPLACED MCU IAW AMM 27-42-05.

Part: UNKNOWN — MALFUNCTIONED (STAB TRIM) · airframe 16,192 hrs · 13,393 cycles

STAB TRIM CH1 + CH2 AND MAX TRIM ALL DISENGAGE IN FLIGHT SOMETIMES WHILE OPERATING TRIM. OPS CHECK HSTCU SYSTEM IAW AMM 27-41-00. NO FAULTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: CONTROL UNIT — DEFECTIVE (HORIZ STAB) · airframe 16,184 hrs · 13,385 cycles

STAB TRIM & MACH TRIM DISENGAGE RANDOMLY DURING FLIGHT. RESET HSTCU & OPS CK AMM 27-41-00. NO CURRENT FAULTS MDC OR LRU. OK FOR SERVICE.

Part: CONTROL UNIT — DEFECTIVE (HORIZ STAB) · airframe 16,184 hrs · 13,385 cycles

T/S STAB TRIM DISCONNECT IN FLIGHT RANDOMLY, STAB DOES RE-ENGAGE. REMOVED AND REPLACED HSTCU IN ACCORDANCE WITH AMM 27-41-01. VERIFIED PART EFFECTIVITY. OK FOR SERVICE.

Part: TRIM SYSTEM — MALFUNCTIONED (TAIL) · airframe 16,114 hrs · 13,321 cycles

LOST TRIM & MACH TRIM 3 TIMES IN FLIGHT. ABLE TO RE-ENGAGE ALL 3 TIMES. BOTH STAB TRIM AND MACH TRIM. OPS CHECKED STAB TRIM AND MACH TRIM SYSTEM IAW 27-41-01. OPS CHECK GOOD.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 150,011 hrs · 12,236 cycles

CREW REPORTS BURNING SMELL IN CABIN. REMOVED AND REPLACED SIDEWALL LIGHT POWER SUPPLY IAW AMM 33-21-10 OPC GOOD. NO SMELL NOTED.

Part: BALLAST — SMOKE (CABIN LIGHTS) · airframe 14,964 hrs · 12,227 cycles

CREW REPORTS ELECTRICAL FUMES WHILE PARKED AT GATE. MAINTENANCE REMOVED AND REPLACED SIDEWALL LIGHT POWER SUPPLY AT SEATS 4C&D IAW AMM 33-21-10. OPS CHECK GOOD.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 14,433 hrs · 11,719 cycles

THE 621 PRESSURE BULKHEAD AT LBL 9 AND WL 86 MEASURING 0.15 INCH DIA BY 0.001 INCH DEEP AND AT LBL 9, LBL 27, AND LBL 36, 0.001 INCH DEEP. REPAIR IAW BOMBARDIER REO 601R-53-61-2155.

Part: BULKHEAD — UNKNOWN (FUSELAGE) · airframe 14,433 hrs · 11,719 cycles

PREVIOUS REPAIR TO PRESSURE BULKHEAD WEB FWD FACE AT RBL 36, WL 103 - .15 INCH DIA BY 0.017 INCH DEEP. REPAIR IAW BOMBARDIER REO 601R-53-61-1285.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 14,433 hrs · 11,719 cycles

PREVIOUS REPAIR TO 621 PRESSURE BULKHEAD FOUND CHAFED AT RBL 27, 0.009 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-1285.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 14,433 hrs · 11,719 cycles

PREVIOUS REPAIR TO 621 PRESSURE BULKHEAD FOUND CHAFED AT RBL 18, .008 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-1285.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 14,433 hrs · 11,719 cycles

PREVIOUS REPAIR TO 621 PRESSURE BULKHEAD WEB CHAFED AT LBL 18, 0.006 INCH DEEP. REPAIR IAW BOMBARDIER REO 601R-53-61-1285.

Part: HOUSING — CRACKED (E&E DOOR) · airframe 13,517 hrs · 10,859 cycles

AVIONICS BAY DOOR HANDLE HOUSING, P/N H3445-5 WAS FOUND WITH A 0.80 INCH LONG CRACK. THE CRACK IS LOCATED IN THE HANDLE HOUSING BOSS WITH NO DAMAGE IS PRESENT IN THE DOOR SKIN OR ADJACENT STRUCTURE. TEMPORARY REPAIR AND FLY ON NOT TO EXCEED 100 FH PER STS ENGINEERING EA 5-2010-178 WITHIN WHICH TIME AVIONICS BAY DOOR HANDLE ASSEMBLY WILL BE REMOVED AND REPLACED.

Part: FLAP SYSTEM — UNKNOWN

FLAPS FAIL, SECOND OCCURRENCE WITHIN 72 HOURS.

Part: UNKNOWN — UNKNOWN · airframe 4,937 hrs · 3,634 cycles

AFTER ESTABLISHING CRUISE ALTITUDE OUT OF DTW, THE FLIGHT CREW WAS ALERTED TO HIGHER THAN NORMAL N1 VIBRATION ON THE LEFT ENGINE. WHEN VIBRATION LEVELS CONTINUED TO INCREASE, THE QRH CHECKLIST WAS COMPLETED AND THE ENGINE WAS SHUT DOWN. THE FLIGHT CREW DECLARED AN EMERGENCY AND TURNED BACK TO DTW. AN OTHERWISE UNEVENTFUL SINGLE ENGINE APPROACH AND LANDING WAS MADE. MAINTENANCE PERSONNEL OBSERVED A LARGE QUANTITY OF ICE BUILT UP ON THE FAN SPINNER AND BLADES. THE ICE WAS REMOVED AND ENGINE VIBRATION RUNS WERE PERFORMED. VIBRATION LEVELS WERE NORMAL. THERE WERE NO REPORTED MALFUNCTIONS OF THE ENGINE'S ANTI-ICE SYSTEM.