N8894A

Part: LIGHT — INOPERATIVE (CENTER CABIN) · airframe 31,134 hrs · 29,421 cycles

RT FWD CENTER EMERGENCY LIGHT OUT. REMOVED AND INSTALLED RT FWD CENTER EMERGENCY LIGHT, IAW CRJ 200 AMM 33-51-01. OPERATIONS CHECK EMERGENCY LIGHT. OPERATIONS CHECK GOOD. P/N ON/OFF: 1317

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,445 hrs · 28,079 cycles

CREW REPORTED ALL EMERGENCY LIGHTS INOPERATIVE. R & R 4 EMERGENCY LIGHT BATTERY PACKS IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,442 hrs · 25,932 cycles

EMERGENCY FLOOR LIGHT STRIP NOT LIGHTING. REMOVED AND REPLACED 8CD EMERGENCY FLOOR TRACK LIGHT STRIP IAW AMM 33-51-01. OPS CHECK GOOD.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 28,323 hrs · 25,808 cycles

AFT PRESSURE BULKHEAD CRACK AT CARGO DOOR TRACK LBL 27.5, AND DENT NEXT TO REPAIR AREA LBL 18.0 - W.L 121.9 - 137.5. REPAIRED AFT BULKHEAD IAW REO 601R-53-61-6927 OPS CK GOOD OF CARGO DOOR WARNING SYS IAW AMM 52-70-02-710-801. OPS CK GOOD OF CARGO DOOR IAW AMM 52-31-00-710-801, FUNCTIONAL CK GOOD IAW AMM 27-41-00.

Part: RETAINER — CRACKED (PYLON PANEL SEAL) · airframe 28,323 hrs · 25,808 cycles

DURING SEAL REPLACEMENT ON PANEL 412AB, FOUND RETAINER TO BE CRACKED AND BROKEN. REMOVED OLD SEAL RETAINER/REPLACED WITH NEW SEAL ON PNL 412AB IAW 51-42-06.

Part: ATTACH BRACKET — CRACKED (WINDOW POST) · airframe 28,323 hrs · 25,808 cycles

WINDSHIELD CTR POST LWR RH MACHINED ATTACH BRACKET CRACKED. REMOVED/REPLACED WINDSHIELD POST LWR RH ATTACH BRACKET IAW CRJ 200 SRM 51-42-21 AAR SM 33

Part: FITTING — WORN (PAX DOOR) · airframe 28,323 hrs · 25,808 cycles

PASSENGER DOOR CUTOUT, AFT PULL IN CAM IS WORN. FOUND PAX DOOR OPENING AFT PULL IN CAM WORN BEYOND SERVICEABLE LIMITS AND INSTALLED NEW CAM IAW SRM 51-42-21 OPS CKS PERFORMED IAW AMM 33-22-00-710-801 CK GOOD.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,323 hrs · 25,808 cycles

LH FLOOR SEAT RAIL LBL9 STICK 4 HAS CORROSION. REMOVED CORROSION ON LBL9 FLOOR SEAT TRACK STICK #4 FOUND TO BE OUT OF LIMITS. REMOVED CORRODED SEAT TRACK/INSTALLED NEW FLOOR SEAT TRACK IAW SRM 51-21-06, 53-41-49, EA DWG S6487 REV A, AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,323 hrs · 25,808 cycles

LH FLOOR SEAT RAIL LBL9 STICK 3 HAS CORROSION. REMOVED CORROSION ON LBL9 FLOOR SEAT TRACK #3 FOUND TO BE OUT OF LIMITS. INSTALLED NEW LBL9 STICK #3 FLOOR SEAT TRACK IAW SRM 51-21-06, 53-41-49, EA DWG S6487 REV A, AMM 53-01-11.

Part: HANDLE — CRACKED (E/E BAY DOOR) · airframe 28,323 hrs · 25,808 cycles

AVIONICS DOOR HANDLE HOUSING IS CRACKED AT BASE. REMOVED/REPLACED AVIONICS DOOR HANDLE HOUSING IAW CRJ 200 SRM 51-42-21 OPS CK GOOD IAW AMM 52-70-08-710-801.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,323 hrs · 25,808 cycles

RH FLOOR SEAT RAIL RBL9 STICK 3 HAS CORROSION. EVALUATED CORROSION ON RBL9 FLOOR SEAT TRACK STICK #3 AND FOUND TO BE OUT OF LIMITS REMOVED CORRODED SEAT TRACK AND INSTALLED NEW FLOOR SEAT TRACK IAW CRJ 200 SRM 53-41-49, EA DWG S6487 REV A, CRJ 200 AMM 53-01-11.

Part: SEAT TRACK — CORRODED · airframe 28,323 hrs · 25,808 cycles

RH FLOOR SEAT RAIL RBL9 STICK 2 HAS CORROSION. REMOVED/REPLACED SEAT RAIL IAW AMM 53-01-11.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 28,323 hrs · 25,808 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED UNSERVICEABLE DRAG ANGLE/REPLACED WITH NEW SERVICEABLE DRAG ANGLE IAW BOMBA REO 601R-52-11-513 REV B AAR SM 107

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 28,323 hrs · 25,808 cycles

FAIRLEAD SUPPORT OTBD ATTACH ANGLE FS 484.0 LBL36 CRACKED. REMOVED/REPLACED ATTACH ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV B AAR SM 33

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 28,323 hrs · 25,808 cycles

FAIRLEAD SUPPORT INTERCOSTAL INBD ATTACH CLIP CRACKED AT FS 484 RBL 27. REMOVED/REPLACED ATTACH CLIP IAW BOMBARDIER REO 601R-53-41-059 REV B AAR SM 33

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 28,323 hrs · 25,808 cycles

AFT CARGO FLOOR SUPPORT STRUCTURE HAS LBL9 CORRODED BETWEEN FS605.0 AND FS621. REPAIRED AFT CARGO FLOOR SUPPORT STRUCTURE ON LBL9 FS 605-FS 621 IAW EA 253-08758.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 28,323 hrs · 25,808 cycles

FLOOR SUPPORT BEAM LBL27 OTBD FLANGE HAS CORROSION AT FLOOR PNL ATTACH HDWR FS 575.0 TO FS605. REMOVED/REPLACED FLOOR BEAM CAP WITH NEW LOCATED/DRILLED CAP IAW ENDEAVOR AIR EA CRJ 253-08651.

Part: MOUNT — CORRODED (PICCOLO TUBE) · airframe 28,323 hrs · 25,808 cycles

RIGHT WING OUTBOARD LEADING EDGE PANEL INBOARD PICCOLO TUBE MOUNT HAS CORROSION REMOVED AND REPLACED R/H WING OB L/E PANEL I/B PICOLO TUBE MOUNT (RIB) IAW CK 200 SRM 51-42-06 AND SRM 51-42-10. AAR R SM 4

Part: RIB — CRACKED (LT WING) · airframe 28,323 hrs · 25,808 cycles

L/H WING LEADING EDGE PANEL 530KL HAS I/B END CAP CORRODED. REMOVED AND REPLACED WITH NEW END CAP RIB IAW SRM 51-42-06 AND CRJ 200 SRM 51-42-13. AAR SM 58

Part: BRACKET — CHAFED (LT WING) · airframe 28,323 hrs · 25,808 cycles

LEFT WING HINGE FAIRING 597BB HAS A CHAFED BRACKET. REMOVED/REPLACED WITH NEW BRACKET ON LH WING HINGE FAIRING 597BB IAW CRJ 200 SRM 51-42-06 AAR SM 58

Part: ANGLE — CRACKED (DOOR FRAME) · airframe 28,323 hrs · 25,808 cycles

AFT EQUIPMENT BAY DOOR LH SURROUND FRAME CLIP AT FS700 CRACKED. REMOVED/REPLACED FS700 FRAME CLIP IAW CRJ 200 SRM 51-42-06 AAR SM 58

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 28,323 hrs · 25,808 cycles

FAIR LEAD SUPPORT OTBD ATTACH ANGLE FS 484.0 LBL27 CRACKED. REMOVED/REPLACED ATTACH ANGLE IAW CRJ 200 SRM 53-41-43 AAR SM 33

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 28,323 hrs · 25,808 cycles

LH FLOOR SUPPORT SILL AT CARGO DOOR THRESHOLD HAS CORROSION FS 574.0 TO FS 621.0. REPAIRED LH FLOOR SUPPORT SILL @ FS574 TO FS621 IAW CRJ 200 SRM 51-42-06. FOR OPS / RIG CHECK REFER TO 1016818 2000-0217. AAR SM 107

Part: ANGLE — CRACKED (BS 589) · airframe 28,323 hrs · 25,808 cycles

ANGLE CLIP ON THE FWD SIDE OF FRAME 589 JUST UNDER THE LH FLOOR SILL IS CRACKED, IN THE CARGO BAY BELOW THE FLOOR. REMOVED/REPLACED ANGLE CLIP ON FWD SIDE OF FS589 UNDER LH FLOOR SILL IAW CRJ 200 SRM 51-42-21 AAR SM 107

Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,323 hrs · 25,808 cycles

RH FLOOR SEAT RAIL RBL9 STICK 4 HAS CORROSION. REMOVED DAND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11. AAR SM 58

Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,323 hrs · 25,808 cycles

LH FLOOR SEAT RAIL LBL9 STICK 2 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11. AAR SM 58

Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,323 hrs · 25,808 cycles

RH FLOOR SEAT RAIL RBL9 STICK 1 HAS CORROSION. REMOVED AND REPLACED WITH NEW SEAT TRACK I.A.W. CRJ-200 AMM 53-01-11-420-01. AAR SM 58

Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,323 hrs · 25,808 cycles

LH FLOOR SEAT RAIL LBL9 STICK 1 HAS CORROSION. REMOVE AND REPLACE NEW SEAT TRACK IAW AMM 53-01-11-420-01. AAR SM 58

Part: MOUNT — CHAFED (NR 2 ENGINE) · airframe 28,323 hrs · 25,808 cycles

NR 2 ENG FWD MOUNT FWD AFT AND UPPER LUG SMALL NICK AND MINOR CHAFF C/W BOMBARDIER REO 601R-54-51-194 TO REMOVE CHAFE DAMAGE ROTO PEEN SURFACE FAND RESTORE FINISH (.003: MAX MATERIAL LOSS) AAR SM 39

Part: PIN — NOT SEATED (EXIT SIGN) · airframe 24,234 hrs · 24,658 cycles

ENTRANCE DOOR 'EXIT' LIGHT INOP. FOUNBD PIN IN WIRING NOT INSTALLED ALL OF THE WAY CAUSING DISRUPTION IN ELECTRICITY. REINSTALLED PIN AND OPS CHECKED GOOD IAW AMM 33-51-10.

Part: OXYGEN BOTTLE — EMPTY (CABIN) · airframe 27,007 hrs · 24,405 cycles

DURING MORNING PREFLIGHT BY FLIGHT ATTENDANT FOUND PORTABLE 02 BOTTLE TO BE ON AND EMPTY. REMOVED AND REPLACED PORTABLE 02 BOTTLE WITH NEW UNIT. PN ON & OFF 5500-C1A-Y0EE SN ON 191291 SN OFF 174826 IAW AMM 35-31-01.

Part: BULKHEAD WEB — DENTED · airframe 26,989 hrs · 24,386 cycles

WHILE COMPLYING WITH JC 53-310-600, A DETAILED INSPECTION OF THE REAR PRESSURE BULKHEAD, VERTICAL STIFFENERS AND WEB. A SMOOTH DENT WAS FOUND IN THE WEB LOCATED BETWEEN LBL 27.5 - LBL 18 AND BELOW WL 137.5 - WL121.9. THERE ARE NO SHARP EDGES OR CREASES. AN EDDY CURRENT WAS CONDUCTED AND NO CRACKS WERE FOUND. COMPLETED A TEMP REPAIR IAW REO 601R-53-61-6578.

Part: POST — CRACKED (BS 409) · airframe 26,989 hrs · 24,386 cycles

VERTICAL POST, RBL 27, HAS A .75 INCH CRACK ORIGINATING AT THE BOTTOM INBD CHANNEL & EXTENDING UPWARDS UP TO & PAST THE FIRST RIVET, ENDING HALFWAY BETWEEN FIRST & SECOND RIVETS, BS 409+128. REPAIRED IAW REO 601R-53-41-0056. MAJOR REPAIR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,915 hrs · 24,287 cycles

LEFT OVERWING EMERGENCY LIGHT OUT. R&R LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD NO DEFECTS.

Part: SIGN — INOPERATIVE (CABIN) · airframe 26,915 hrs · 24,287 cycles

LIGHTED FLOOR LEVEL EXIT SIGN FOUND INOP. R&R FLOOR LEVEL EXIT SIGN IAW AMM 33-51-10 OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME PN ON/OFF 6020-6 NON SERIALIZED PART.

Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 25,200 hrs · 22,439 cycles

GEAR DISAGREE WARNING MESSAGE WHEN GEAR EXTENDED. PERFORMED GO AROUND, WHEN SPEED INCREASED, THE MESSAGE WENT AWAY. RAN QRH AND LANDED. INSPECTED NLG AREA AND FOUND NO DEFECTS. INTERROGATED PSEU FOR CODES, PLACED GEAR EXTENSION AND RETRACTION SYSTEM ON MEL 32-30-01. TROUBLESHOT IAW FIM 32-60-09. FOUND MLG SELECTOR VALVE INOPERATIVE. FOUND NLG PRIORITY VALVE INOPERATIVE, BLED HYDRAULIC SYSTEM NR 3 IAW AMM 29-10-00. PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION/RETRACTION SYS IAW AMM 32-30-00 FUNCTIONAL TESTED GOOD.

Part: UPLOCK TARGET — LOOSE (LT MLG) · airframe 24,625 hrs · 21,851 cycles

GEAR DISAGREE WARNING AFTER T/O LEFT MAIN GEAR INDICATED RED, NOSE & MAIN INDICATED UP RAN QRH PERFORMED MEL MAINTENANCE PROCEDURES, DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL 32-30-01. T/S IAW FIM 32-00-00. CODES FROM PSEU AS FOLLOWS: S30 FAR, S31 FAR, S32 FAR, DI 14 ON, DI 15 ON, S20 FAR. FOUND LT MLG PROX SWITCH TARGET LOOSE AND OUT OF LIMITS. RESECURED AND ADJUSTED IAW AMM 32-61-05 AND TS #000896, TS #000284-2012. GEAR SWING OP CHECKS GOOD IAW AMM 32-30-00. THIS CLEARS CNTRL #3303481-1. MM02 UPDATED, MOC NOTIFIED #96054. PLACARDS REMOVED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,432 hrs · 21,660 cycles

NR 3 EXTERNAL E LIGHT RIGHT SIDE INOP. R&R NR 3 EXTERNAL E-LIGHT ON RIGHT SIDE IAW AMM 33-51-21, OPS CHECK IAW AMM 33-51-00 OPS CHECK GOOD.

Part: SKIN — DAMAGED (BS 409) · airframe 24,189 hrs · 21,428 cycles

DURING LIGHTNING STRIKE INSPECTION, FOUND DAMAGE TO FUSELAGE SKIN AT BS 409+65 ALONG STRINGER 14R. BLENDED THE DAMAGED AREA IAW SRM 51-12-00 AND INSTALLED FABRICATED REPAIR DOUBLER IAW EA CRJ253-04870.

Part: FRAME — CORRODED (BS 574) · airframe 23,799 hrs · 21,030 cycles

FRAME CORRODED AT BS 574 BETWEEN STRINGERS 25L-26R. REPAIRED FRAME IAW EA CRJ253-04482.

Part: RISER — CRACKED (PAX DOOR STEP) · airframe 23,799 hrs · 21,030 cycles

PAX DOOR LOWER STEP AFT RISER IS CRACKED. REPAIRED THE RISER IAW REO 601R-52-11-702. OPS CHECKED GOOD.

Part: SKIN — DENTED (LT FLT SPOILER) · airframe 23,799 hrs · 21,030 cycles

LT FLIGHT SPOILER IS DENTED. REPAIRED IAW CRJ257-04486

Part: ATTACH BRACKET — DAMAGED (LT WING) · airframe 23,799 hrs · 21,030 cycles

LEFT WING L/E ATTACH BRACKET ANGLE IS CRACKED/CHAFED, LOCATED BETWEEN MIDDLE AND OTBD L/E WS 260. R & R LT WING L/E BRACKET WS 260 IAW SRM 51-42-06 LEAK CHECK TRANSFERRED TO SN 4715690, W/O 1013044-5000-0058.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,799 hrs · 21,030 cycles

MAIN CABIN FLOORBEAM HAS A CRACKED ANGLE AT BS 280 LBL 9. REMOVED & REPLACED THE ANGLE IAW SRM 51-42-21.

Part: ATTACH ANGLE — CRACKED (BS 449) · airframe 23,799 hrs · 21,030 cycles

LT OVERWING TO FUSELAGE PANEL ATTACH ANGLE BS 449.85 IS CRACKED. REMOVED & REPLACED THE ATTACH ANGLE IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 621) · airframe 23,799 hrs · 21,030 cycles

INTERCOSTAL ANGLE AT BS 621 AND STRINGER 13L IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL ANGLE IAW SRM 51-42-06, & 51-42-21.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 23,799 hrs · 21,030 cycles

FLOORBEAM CORRODED AT BS 559+80, RBL 27. REPAIRED FLOORBEAM IAW SRM 53-00-43 FIG 203.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,799 hrs · 21,030 cycles

MAIN CABIN FLOOR STRUCTURE HAS A CRACKED ANGLE AT BS 280 RBL 9. REMOVED & REPLACED ANGLE IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

RIGHT SIDE SEAT RAIL STICK NR 4 HAS CORROSION. R & R SEAT TRACK STICK NR 4 IAW AMM 53-01-11.

Part: ANGLE — CRACKED (BS 621) · airframe 23,799 hrs · 21,030 cycles

INTERCOSTAL ANGLE AT BS 621 AND STRINGER 14L IS CRACKED IN THE AFT EQUIPMENT BAY. REMOVED AND REPLACED THE INTERCOSTAL ANGLE IAW SRM 51-42-21 & 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

MAIN CABIN LT SEAT TRACK AT 559+80 HAS CORROSION OUT OF LIMITS. R & R SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

SEAT TRACK ON RBL 27 AND FS 559+80 HAS CORROSION. R & R SEAT TRACK, RBL 27 AT FS-559+80 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

RIGHT SIDE SEAT RAIL, STICK NR 5 HAS CORROSION. REPLACED RT SEAT RAIL IAW AMM 53-01-11.

Part: BULKHEAD WEB — GOUGED (BS 621) · airframe 23,799 hrs · 21,030 cycles

FWD FACE OF AFT BULKHEAD BS 621, RBL 36.20 IS GOUGED. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1285 REV D.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

IN MAIN CABIN, LEFT FLOOR SEAT TRACK NR 4 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R LT FLOOR SEAT TRACK NR 4 IAW AMM-53-01-11 AND REO 601R-53-00-485.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

IN MAIN CABIN LEFT FLOOR SEAT TRACK NR 2 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. REPLACED LEFT FLOOR SEAT TRACK NR 2 IN MAIN CABIN IAW AMM 53-01-11.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

FRAME ATTACH ANGLE IS CRACKED AT FS 280, STRINGER 3L. REMOVED CRACKED ATTACH ANGLE AT FS 280, STRINGER 3L, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-42-06.

Part: PANEL — CHAFED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

SINGLE POINT REFUEL STRUCTURE INBD SIDE HAS 2 CHAFES. R & R PANEL, PN 600-62440-17, TAG B48703 IAW SRM 51-40-11.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

IN MAIN CABIN, LT FLOOR SEAT TRACK NR 3 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R SEAT TRACK IAW REO 601R-53-00-485.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

RT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE FS 470.00 IS CRACKED. R & R SUPPORT ANGLE AND RESTORED FINISH IAW SRM 51-42-06 AND SRM 51-25-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

RIGHT SIDE SEAT RAIL STICK NR 3 HAS CORROSION. R & R RT SIDE NR 3 SEAT RAIL IAW AMM 53-01-11-020-002 AND AMM 53-01-11-420-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

SEAT TRACKS ON RBL 9 AND FS 559+80 AND AFT HAVE CORROSION. R & R SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

IN MAIN CABIN RT FLOOR SEAT TRACK NR 3 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R RT SIDE SEAT TRACK RAIL STICK NR 3 IAW AMM 53-01-11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

FLT DECK PILOT'S SIDE FRAME WEB CRACKED BELOW WINDSHIELD/SIDE WINDOW POST, MARKED DOT68A-029. R & R FRAME WEB BELOW WINDSHIELD ON PILOT'S SIDE IN FLIGHT DECK IAW SRM 51-42-06.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

IN MAIN CABIN LEFT FLOOR SEAT TRACK NR 1 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R IN MAIN CABIN LT SEAT TRACK NR 1 FLOOR IAW AMM 53-01-11-400-802, STEP 2B 1-8 RE-36.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 23,799 hrs · 21,030 cycles

IN MAIN CABIN, RT FLOOR SEAT TRACK NR 1 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R IN MAIN CABIN RIGHT FLOOR SEAT TRACK NR 1 IAW MM 53-01-11-400-802, STEP 2B 1-8, SM-123.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,753 hrs · 20,982 cycles

ROW 5 EMER FLOOR LIGHTING INOPERATIVE. OK TO DEFER EMER FLOOR LIGHT BULB ROW 5DC INOPERATIVE IAW MEL 33-51-17 MM 02. UPDATED PLACARD INSTALLED. R & R EMER FLOOR LIGHT STRIP IAW AMM 33-51-01. OPERATIONS CHECKED GOOD. THIS CLEARS DM 000343. PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,238 hrs · 20,477 cycles

EMERGENCY LIGHT STRIP AT ROW 5 INOPERATIVE. R & R LIGHT STRIP IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,190 hrs · 20,431 cycles

EMERGENCY FLOOR LIGHTS NOT WORKING ROW 2 - 5. REPLACED ROW 5 FLOOR TRACK LIGHT STRIP IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.

Part: COMPUTER — INOPERATIVE (FUEL SYSTEM) · airframe 23,021 hrs · 20,262 cycles

DIVERTED DUE TO FUEL IMBALANCE, EMER DECLARED. MAINTENANCE IS CURRENTLY WORKING ISSUE. EN ROUTE FUEL IMBALANCE LT TANK SHOWING 1100 LBS MORE FUEL THAN RT TANK. RAN QRH & COULD NOT GET FUEL BALANCED. LANDED UNEVENTFULLY. R & R FUEL COMPUTER IAW AMM 28-41-16. PERFORMED OPERATIONS CHECK OF GRAVITY CROSS FLOW SOV & OPERATIONS CHECK OF FUEL CROSS FLOW SOV IAW AMM 28-13-16 & 28-13-45. EICAS DISPLAY, REFUEL & DEFUEL PANEL & MLI QTY MATCH. NO DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,915 hrs · 20,146 cycles

ON PREFLIGHT FLIGHT ATTENDANT FOUND EMER LIGHT AT ROW 6 CEILING EXIT. DEFER EMER LIGHT IAW MEL 33-51-13 & PLACARD INSTALLED. RE-LAMPED CEILING EMER LIGHT IAW AMM 33-51-16. PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,909 hrs · 20,141 cycles

EMERGENCY FLOOD LIGHT AT ROW 8 EXIT IS INOPERATIVE. RE-LAMPED CEILING EMER LIGHT IAW AMM 33-51-16.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 22,710 hrs · 19,951 cycles

CAPTAIN`S LIFE VEST HAS HOLE IN BAG. R & R CAPTAIN`S LIFE VEST IAW AMM 25-61-03.

Part: LENS — CRACKED (CABIN) · airframe 22,618 hrs · 19,848 cycles

GALLEY OVERHEAD EMER LIGHT LENS CRACKED. R & R GALLEY OVERHEAD EMERGENCY LIGHT LENS IAW AMM 33-51-13.

Part: LIGHT — LOOSE (CABIN) · airframe 22,549 hrs · 19,780 cycles

EMER LIGHT FLOOR STRIP COMING LOOSE FROM ROW 4 TO 7. SECURED EMER LIGHT FLOOR STRIP FROM ROW 4 TO 7 IAW AMM 33-51-01.

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 22,143 hrs · 19,371 cycles

AFTER TAKEOFF, WHEN RETRACTING GEAR, GEAR DISAGREE MASTER WARNING SOUNDED, LEFT MAIN GEAR SHOWED RED. COMPLIED WITH GEAR SWINGS IAW AMM 32-30-00, CYCLED FIVE TIMES WITH NO DEFECTS NOTED. COMPLIED WITH LANDING GEAR EXTENSION & RETRACTION GEAR DISAGREE TEST IAW AMM TASK 32-30-00-750-801, NO DEFECT NOTED. COMPLIED WITH PA 05-018K SCENARIO 1, SUSPECT ICE & SLUSH BUILD UP, NO CONTAMINATES WERE FOUND.

Part: COVER — DAMAGED (CABIN) · airframe 22,116 hrs · 19,341 cycles

EMERGENCY FLOOR LIGHTING COVER DAMAGED. R & R EMERGENCY FLOOR LIGHT COVER IAW AMM 33-51-01.

Part: OXYGEN MASK — MISSING (PORTABLE O2) · airframe 21,768 hrs · 18,996 cycles

PASSENGER O2 BOTTLE USED IN FLIGHT & NOW PRESS IS LOW & BLUE MASK IS MISSING. R & R PORTABLE OXYGEN CYLINDER IAW CRJ 200 AMM 35-31-01, AIRCRAFT OK FOR SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 21,569 hrs · 18,805 cycles

ROW 3 EMERENGCY LIGHT INOPERATIVE. SECURED EMERGENCY LIGHT IAW AMM 33-51-01-04. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 596) · corrosion level 2 · airframe 21,372 hrs · 18,614 cycles

FLOOR SUPPORT NUTPLATE HAS CORROSION AROUND HOLE, BLENDED OUT OF LIMITS AT LBL 27 AND FS 596. REPAIRED IAW SRM 53-00-43.

Part: SKIN — DENTED (BS 626) · airframe 21,373 hrs · 18,614 cycles

MX FOUND A DENT IN THE RT FUSELAGE SKIN AT FS 626 ABOVE S17R. REPAIRED IAW EA CRJ253-01859A.

Part: BULKHEAD — GOUGED (BS 202.75) · airframe 21,372 hrs · 18,614 cycles

SMALL GOUGE ON FWD SIDE OF FS 202.75 BULKHEAD WHERE BRAKE CABLE PASSES THRU. REPAIRED IAW REO 601R-53-11-563.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 21,372 hrs · 18,614 cycles

FLOOR SUPPORT NUTPLATE HAS CORROSION AROUND HOLE AT LBL 27 FS 559+7. REPAIRED IAW SRM 53-00-45.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,177 hrs · 18,415 cycles

EMERGENCY LIGHT DIM AT ROW 7 & 8. R & R NR 3 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD IAW AMM 33-51-07.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,177 hrs · 18,415 cycles

ROWS 2 THROUGH 5 FLOOR EMERGENCY LIGHTS INOPERATIVE. R & R NR 2 EMERGENCY LIGHT INVERTER IAW AMM 33-51-04. CHECKED GOOD. OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 21,171 hrs · 18,408 cycles

FORWARD F/A FLASHLIGHT IAW AMM 25-61-04. FORWARD FLASHLIGHT IAW AMM 25-61-04.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 21,129 hrs · 18,364 cycles

FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED & REPLACED EMERGENCY LIGHT CABLE BETWEEN ROWS 2-8 IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 21,135 hrs · 18,370 cycles

EMERGENCY LIGHTS ARE INOPERATIVE. R & R EMERGENCY LIGHT CABLE BETWEEN ROWS 2-8 IAW AMM 33-51-01 OPS CHECKED GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,112 hrs · 18,349 cycles

EMERGENCY LIGHT INOPERATIVE FROM EMERGENCY ROW FWD. REPLACED EMERGENCY LIGHT AT ROW 7CD TESTED GOOD IAW AMM 33-51-00.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 20,827 hrs · 18,063 cycles

TWO INFANT LIFE VEST HAVE HOLES IN BAGS. REMOVED AND REPAIRED TWO INFANT LIFE VESTS IAW PA 25-096A.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 20,688 hrs · 17,927 cycles

CAPTAIN LIFE VEST HAS HOLE IN PACKAGE. REMOVED AND REPLACED CAPTAIN LIFE VEST IAW AMM 25-61-03.

Part: TIRE — BLOWN (LT MLG) · airframe 20,492 hrs · 17,753 cycles

ON FLIGHT 4272 (MSP TO YYZ) THE CREW REPORTED THAT IT FELT LIKE A TIRE BLEW ON LANDING. MAINTENANCE WAS CALLED TO MEET THE PLANE AND FOUND BOTH LEFT MAIN LANDING GEAR TIRES BLOWN. REMOVED AND REPLACED LEFT INBOUND AND OUTBOUND TIRES AND BRAKES. AN INSPECTION WAS ALSO PERFORMED. AIRCRAFT OK FOR SERVICE.

Part: WIRE HARNESS — FAULTY (NLG STEERING) · airframe 19,856 hrs · 17,120 cycles

ON FLIGHT 4080 FROM JFKL TO CLE UPON GEAR RETRACTION GOT STEERING INOP CAUTION. RAN QRH, WOULD NOT GO AWAY. UPON GEAR RETRACTION (AT REQUEST OF MOC) RECYCLED THE STEERING AND MESSAGE WENT AWAY. FLIGHT LANDED AT ORIGINALLY SCHEDULED AIRPORT (CLE). REPEAT FROM PREVIOUS FLIGHT. REMOVED AND REPLACED NOSE LANDING GEAR STEERING HARNESS ASSEMBLY IAW AMM 32-20-04. OPS CHECKS GOOD, AIRCRAFT OK FOR SERVICE.

Part: SERVO VALVE — FAULTY (NLG STEERING) · airframe 19,851 hrs · 17,115 cycles

DURING FLIGHT 3841 FROM YYZ TO JFK RECEIVED NOSE WHEEL STEERING CAUTION MESSAGE. IT WOULD NOT RESET PER QRH. EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TOWED OFF THE RUNWAY AND THE SYSTEM WAS RESET. REMOVED AND REPLACED ELECTRO HYDRAULIC SERVO VALVE IAW AMM 32-51-15. OPS CHECK PERFORMANCE IAW AMM 32-51-10. OPS CHECKS GOOD FOR SERVICE.

Part: FLUTTER DAMPER — DEFECTIVE (RT ELEVATOR) · airframe 19,078 hrs · 16,358 cycles

DURING APPROACH AND LANDING ELEVATOR HAD SIGNIFICANT RESISTANCE FORWARD AND AFT. PER FIM TROUBLESHOOTING RIGHT ELEVATOR O/B FLUTTER DAMPNER NOT TESTING. REMOVED AND REPLACED RIGHT ELEVATOR O/B FLUTTER DAMPNER IAW AMM 27-34-05. OPS CHECK GOOD.

Part: UNKNOWN — BINDING (FLT CONTROLS) · airframe 19,039 hrs · 16,318 cycles

FELT BINDING & RESISTANCE IN FLIGHT OFFICERS FLIGHT CONTROL. PERFORMED INSPECTION OF ELEVATOR CONTROL CABLES. NO DEFECTS NOTED. RANGE OF MOTION OF THE ELEVATOR FORWARD AND AFT WITHIN LIMITS, NO BINDING OR RESISTANCE NOTED IAW AMM 27-31-0. OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 18,832 hrs · 16,111 cycles

ROW 1, 1.5 FT CLEAR EMERGENCY LIGHT COVER, MISSING. REMOVED AND REPLACED FWD SECTION EMERGENCY FLOOR TRACK LIGHT, AND TRACK TOP. OP CHECKED GOOD IAW AMM 33-51-01.

Part: TRIM SWITCH — DIRTY (COCKPIT) · airframe 18,636 hrs · 15,923 cycles

F/O'S STAB TRIM SWITCH STICKY ON TRIMMING DOWN. CLEANED SWITCH MOVES FREELY NOW, CORRESPONDS W/TRIM INDICATIONS. REFERENCED AMM 27-40-00. A/C OK FOR SVC.

Part: STRIP — PEELING (CABIN) · airframe 18,388 hrs · 15,679 cycles

THE EMERGENCY LIGHT STRIP HAS LOST ITS PROTECTIVE COVER AND IS NOW PEELING FROM THE FLOOR. INSTALLED FLOOR EMERGENCY LIGHT COVER AT SEAT 1C IAW AMM 33-51-01. VERIFIED PART EFFECTIVITY. OK FOR SVC.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,198 hrs · 15,492 cycles

AFT PRESSURE BULKHEAD CRACKED AT FS 621 AT LT LINTEL FITTING. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,151 hrs · 15,446 cycles

CAPTAINS FLASHLIGHT BATTERY DEAD. REMOVED AND REPLACED CAPTAINS FLASHLIGHT BATTERY IAW AMM 25-60-01. VERIFIED PARTS EFFECTIVITY. OPS CHECK GOOD.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 17,574 hrs · 14,893 cycles

WING PLANK ACCESS HOLE AT PANEL 540BB HOLE NR 1 IS PITTED/ CORRODED. THIS IS IN A NON-CRITICAL AREA. REMOVED 0.002" FROM FAYING SURFACE IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: BEAM — CRACKED (FUSELAGE) · corrosion level 2 · airframe 17,574 hrs · 14,893 cycles

FS 280 TRANSVERSE BEAM IS CRACKED 2 AREAS 2.0 INCH LONG IN LOWER RADIUS OUTBD OF LBL 9 AND RBL 9, BOTH ATTACH CLIPS AT RBL 9 ARE CRACKED IN UPPER RADIUS AND THE UPPER J-ANGLE IS CRACKED 1.5" BETWEEN RIVETS OUTBD OF LBL 9 AND THERE IS CORROSION ON UPPER EDGE OF THE FWD J-ANGLE. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B.

Part: SENSOR — FAULTY (AINTI-ICE SYSTEM) · airframe 16,678 hrs · 14,054 cycles

ANTI ICE DUCT MESSAGE AIR RETURN TO MSP. REPLACED WING ANTI ICE SENSORS IAW AMM 30-10-00.

Part: SKIN — GOUGED (FUSELAGE) · airframe 15,949 hrs · 13,362 cycles

ONE (1) DENT WITH CENTRAL GOUGE IN FUSELAGE SKIN AT FS 626.0 & STR I7R. DENT DIMENSIONS ARE: 2.0" LONG X 1.5" WIDE X .078" DEEP. GOUGE DIMENSIONS ARE: 0.315" LONG X 0.157" WIDE X 0.030" DEEP. TEMPORARY REPAIR IAW BOMBARDIER REO 601R-53-61-3848 FLY ON FOR 1200 FH WITHIN WHICH TIME A PERMANENT REPAIR MUST BE MADE.

Part: YAW DAMPER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 14,170 hrs · 11,694 cycles

CONSTANT OSCILLATION WITH AUTO PILOT ON. REMOVED AND REPLACED LT AND RT YAW DAMPER IAW AMM 22-22-01 FOUND RUDDER POSITION TRANSMITTER TO BE MISS RIGGED. RE-RIGGED IAW AMM 27-21-0 5, OPS CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (SMOKE WARNING) · airframe 5,399 hrs · 4,395 cycles

ON TAXI, RECEIVED LAVATORY SMOKE EICAS MESSAGE. RETURNED TO GATE. MAINT INSPECTED AIRCRAFT, FOUND NO DEFECTS AND TESTED SYSTEM WITH NO DEFECTS PER AMM.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 5,305 hrs · 4,315 cycles

AFTER TAKEOFF ON CLIMBOUT WHEN RETRACTING FLAPS. FLAPS STOPPED AND STAYED AT 8 DEGREES. PERFORMED QRH DECLARED EMERGENCY AND RETURNED TO AIRPORT WITH UNEVENTFUL LANDING. FLAPS RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,680 hrs · 3,797 cycles

FLAPS FAILED AT 8 DEGREES WHEN SELECTED TO 20 DEGREES. LANDING UNEVENTFUL. REMOVED AND REPLACED FLAP ELECTRICAL CONTROL UNIT (FECU) IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL(AMM). OPERATIONALLY TEST AND CHECK RIGGING OF BRAKE POSITON SENSOR UNIT (BPSU) IAW AMM. AIRCRAFT OKAY FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,675 hrs · 3,793 cycles

FLAPS FAIL CAUTION AT FLAPS 2 DEGREES. LANDING UNEVENTFUL. SYSTEM REST AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.