N833AY

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,996 hrs · 34,095 cycles

FORWARD FA OVERHEAD (EXIT SIGN) CALL LIGHT INOP "DEFERRING FWD MID CABIN FLT ATTENDANT CALL LIGHT (MIDDLE-BLUE) IAW MEL 23-40-1J (B) ENTERED INTO MM02 MXC NOTIFIED 96184//////INSTALLED NEW LAMP HOLDER AND BULB IAW CRJ 200 AMM 33-51-14 PAX CALL ANNUNCIATOR LIGHT OPS CHECKS GOOD.

Part: BULKHEAD WEB — CHAFED (AFT) · airframe 24,729 hrs · 25,130 cycles

FS 621 BULKHEAD WEB CHAFED 2 LOCATIONS: FWD FACE WL 137.00, RBL 8.0 AND LBL 8.0. PERFORMED LPI OF FS 621 RPB FWD FACE WL 137 RBL 8 & LBL 8. REWORKED AREAS, IAW MHIRJ REO 601R-53-61-7500 REV- DATED 2020-12-04 STEP 3 NR 3. NO INDICATIONS NOTED AT THIS TIME.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 24,729 hrs · 25,130 cycles

POTABLE WATER DRAIN HOSE DOUBLER AT FS 605.00 BETWEEN STR 26R AND 25R HAS ONE SMALL AREA OF CORROSION. REMOVED & REPLACED POTABLE WATER DRAIN MAST DOUBLER AT FS 605, IAW CRJ 200 SRM 51-42-06 AND 51-40-11.

Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 24,729 hrs · 25,130 cycles

(2) CHAFES ON FS 621 BULKHEAD FWD FACE WL 87.5, RBL 18.0 AND 27.0. COMPLIED WITH STEP 4 OF MHIRJ REO 601R-53-61-7500 REV- DATED 2020-12-04. RESTORED FINISH OF REWORKED AREAS A010, PER SRM 51-21-16.

Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 24,729 hrs · 25,130 cycles

FS 621.00 BULKHEAD WEB CHAFED, FWD SIDE, AT WL 104.00, RBL 8.0, 18.0, 27.0, 36.0 AND LBL 8.0, 18.0 AND 27.0. COMPLIED WITH STEP 4 OF MHIRJ REO 601R-53-61-7500 REV- DATED 2020-12-04. RESTORED FINISH OF REWORKED AREAS A010, PER SRM 51-21-16.

Part: HANDLE — CHAFED (PAX DOOR) · airframe 24,729 hrs · 25,130 cycles

PAX DOOR INNER HANDLE CHAFED (UPPER ANGLE). REMOVED AND REPLACED PAX DOOR INNER HANDLE UPPER ANGLE, IAW CRJ 200 SRM 51-40-11 AND 51-42-06.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 24,729 hrs · 25,130 cycles

RT SIDE SEAT RAIL CORRODED BETWEEN FS 495.98 AND FS 535.02. R & R SIDE SEAT RAIL AT FS 495.98 TO 535.02 (RT SIDE), IAW MHIRJ REO 601R -53-00-055, REV C DATED 3/21/17 AND AMM 53-01-11-000/400-802.

Part: HANDLE — CHAFED (PAX DOOR) · airframe 24,729 hrs · 25,130 cycles

PAX DOOR INNER HANDLE ANGLE CHAFED. REMOVED AND REPLACED PAX DOOR INNER HANDLE, IAW CRJ 200 SRM 51-40-11.

Part: HOUSING — CRACKED (E&E DOOR) · airframe 22,195 hrs · 22,391 cycles

AVIONICS BAY DOOR HANDLE HOUSING IS CRACKED AROUND THE BASE OF THE HANDLE SHAFT. (NDT HAS VERIFIED.) DOT 262A001 REMOVED/REINSTALLED AVIONICS DOOR IAW AMM 52-42-00 OPS TEST OF THE AVIONICS DOOR WARNING SYSTEM GOOD IAW AMM 52-70-08 INSTALLED NEW HANDLE HOUSING IAW SRM 51-42-21.

Part: DOUBLER — CRACKED (LT WING) · airframe 22,195 hrs · 22,391 cycles

LEFT WING O/B L/E HAS A CRACK BETWEEN PANELS 530LZ AND 530KZ. REPAIRED CRACK ON LT WING OUTBOARD LEADING EDGE IAW EA 257-08321 REV B.

Part: STRAP — CORRODED (PAX DOOR) · airframe 22,195 hrs · 22,391 cycles

PAX DOOR UPPER FRAME STRAP AT FS349 BY STR 3L IS CORRODED. REMOVED AND REPLACED UPPER INNER STRAP FS349 STR3L PER SRM 51-42-21.

Part: FRAME — CORRODED (FUSELAGE) · airframe 22,195 hrs · 22,391 cycles

FRAME 589 HAS CORROSION SPOTS ON THE FWD AND AFT SIDE BETWEEN STGR 23L AND STGR 24R, IN THE CARGO BAY. REPAIRED CORROSION DAMAGE TO FS589 FRAME STR 23L-24R PER EA 253-08396 LEAK CK OF THE MAIN FEED MANIFOLD CKS GOOD IAW AMM 21-20-00-790-801.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 22,195 hrs · 22,391 cycles

FS621 FLOOR SUPPORT AT LBL36 CRACKED. REMOVED CRACKED SECTION OF FLOOR SUPPORT AT FS. 621 AND LBL36 AND INSTALLED REPAIR SECTION. IAW REO 601R-53-61-117 REV E. DATED 01/15/2018.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,195 hrs · 22,391 cycles

INTERCOSTAL SUPPORTING HYDRAULIC FILTERS CRACKED ON LOWER AFT SIDE AFT EQUIPMENT BAY. REMOVED AND REPLACED INTERCOSTAL DUE TO CRACK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,195 hrs · 22,391 cycles

LBL 9 HAS CORROSION SPOTS ON THE O/B FLOOR PANEL LANDING BETWEEN FS 574 AND FS 605, IN THE CARGO BAY. REMOVED CORODED LBL 9 FLOORBEAM AND REPLACED WITH NEW BEAM IAW SRM 51-40-11 TR 51-42.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 22,195 hrs · 22,391 cycles

CARGO DOOR OPENING FOLDING STEP FWD ANGLE BRACKET ON THE LT FLOOR SILL IS CRACKED AND BENT AT FS 574. REPLACED FOLDING STEP FWD ANGLE BRACKET @ FS574 IAW SRM 51-42-21.

Part: PANEL — CHAFED (RT WING) · airframe 22,195 hrs · 22,391 cycles

PR PNL#684AB HAS CHAFFING. D-109-011. REMOVED CHAFED PANEL AND REPLACED WITH NEW PANEL, DRILLED AND LOCATED PANEL IAW SRM 51-41-11.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,195 hrs · 22,391 cycles

PASSENGER DOOR DRAG ANGLE, MIDDLE OF DOOR NEAR CABLE REEL, CRACKED. REPAIRED PASSENGER DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513.

Part: BRACKET — CRACKED (RT WING) · airframe 22,195 hrs · 22,391 cycles

RT WING FRONT SPAR FWD FACE HAS BRACKET AROUND WS149.58 O/B SECTION CRACKED. REMOVED AND REPLACED WITH NEW BRACKET ON RT WING FRONT SPAR FWD FACE AOUND WS149-58-01B IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,195 hrs · 22,391 cycles

RT SEAT TRACK STICK NR 3 IS CORRODED. REMOVED/REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 22,195 hrs · 22,391 cycles

CENTER WING BOX FWD SPAR RT FUEL FILL O/B PANEL IS CRACKED AT THE AFT LOWER RADIUS. REMOVED AND REPLACED CENTER WING BOX FWD SPAR RT FUEL FILL O/B PANEL IAW SRM 51-41-04 AND SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,195 hrs · 22,391 cycles

SEAT TRACK ON TOP OF RBL 9 HAS CORROSION BETWEEN FS 559+80 THRU FS 559+96, IN THE CARGO BAY. REMOVED/REPLACED SEAT TRACK IAW SRM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,195 hrs · 22,391 cycles

SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FS 559+112 THRU FS 574, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 22,195 hrs · 22,391 cycles

AFT PRESSURE BULKHEAD WEB AFT SIDE TOP LT INTERCOSTAL BETWEEN FS621-FS625 ANGLE BRACKET IS CRACKED. REMOVED BRACKET IAW SRM 51-42-06. FABRICATED NEW BRACKET IAW SRM 51-24-36 AND SRM 51-40-11 AND INSTALLED NEW BRACKET IAW SRM 51-42-06 AND SRM 51-42-20.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 22,195 hrs · 22,391 cycles

RT OVER WING, SUPPORT BRACKET BETWEEN PANELS 162DL AND 162EL IS CRACKED. REMOVED/REPLACED ANGLE SUPPORT BRACKET IAW SRM 51-42-06.

Part: FITTING — CORRODED (FUSELAGE) · airframe 22,195 hrs · 22,391 cycles

LBL 27 I/B FLOOR PANEL LANDING HAS CORROSION SPOTS BETWEEN FS 605 AND FS 621, IN THE CARGO BAY, REPAIRED FLOOR PANEL LANDING IAW EA NR CRJ253-08313 REV IR.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,555 hrs · 21,718 cycles

FLIGHT ATTENDANT'S FLASHLIGHT NOT BLINKING. R&R FLIGHT ATTENDANT'S FLASHLIGHT IAW AMM 25-61-00, OPS CHECK GOOD, A/C OK FOR SVC.

Part: HARNESS — FAULTY (NLG) · airframe 20,789 hrs · 20,841 cycles

AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. RAN QRH AND RETURNED TO DEPARTURE. REMOVED AND REPLACED THE NLG WOW NR 2 AND CENTERING HARNESS IAW AMM 32-61-25, OPS CHECK GOOD. REMOVED AND REPLACED CENTERING SENSOR BRACKET IAW IAW MM 32-20-04

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,558 hrs · 20,597 cycles

RIGHT NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,558 hrs · 20,597 cycles

LEFT NR 1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — NO TEST (LAVATORY) · airframe 20,542 hrs · 20,581 cycles

SMOKE TOILET CAUTION MESSAGE DURING TAXI. LAVATORY SMOKE DETECTOR DOES NOT TEST PROPERLY. REMOVED AND REPLACED THE SMOKE DETECTOR IAW 26-16-01. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,708 hrs · 19,663 cycles

BURNING PLASTIC ODOR FROM THE VENTS DURING FLIGHT AND REPORTED BY PREVIOUS CREW. PERFORMED OPS CHECK OF PACKS IAW AMM 21-50-00-02. OPS CHECKED GOOD.

Part: BRACKET — DAMAGED (NLG) · airframe 19,598 hrs · 19,551 cycles

NOSE GEAR DISAGREE WARNING, NOSE GEAR DOOR OPEN WARNING, QRH COMPLETED, RETURN TO DEPARTURE. REPLACED THE PROXIMITY SENSOR BRACKET IAW AMM 32-21-01. R & R THE TOW COLLAR IAW 32-21-00-H235-1, SERVICED THE NOSE STRUT IAW 12-710-002. GEAR SWINGS CHECKED GOOD IAW AMM 32-30-00.

Part: UNKNOWN — ODOR · airframe 18,712 hrs · 18,602 cycles

FUME SMELL COMING FROM PACKS WHILE APU RUNNING. PERFORMED OPS TEST ON LT/RT PACKS IAW AMM 21-51-00, AND INSPECTED THE CABIN/FLIGHT DECK FOR FUEL SMELL, NO FUEL SMELL NOTED. A/C OK FOR SVC.

Part: OXYGEN BOX — INOPERATIVE (COCKPIT) · airframe 18,694 hrs · 18,585 cycles

OBSERVER MASK DOES NOT SHOW FLOW INDICATION WHEN TESTED. REMOVED AND REPLACED THE OXYGEN MASK BOX. OPERATIONAL TEST PASSED. NO LEAK.

Part: FCU — INOPERATIVE (RT ENGINE) · airframe 18,662 hrs · 18,556 cycles

WHEN STARTING RIGHT ENGINE ANOTHER FLIGHT CREW REPORTED A RIGHT ENGINE FIRE WITH FIRE SHOOTING 12 FEET FROM ENGINE, N1 WAS 3% N2 WAS 25% ITT NEVER WENT OVER 40(DEGREE)C. FUEL FLOW WAS 2200LBS. WE NEVER RECEIVED A FIRE INDICATION IN THE COCKPIT. ENGINE WAS SHUTDOWN & DRY MOTORED. FIRE DEPARTMENT SPRAYED WATER IN TAIL CONE TO EXTINGUISH RESIDUAL FIRE. PREVIOUS WRITE UPS OF FUEL SMELL IN BOTH PACKS. R&R RT FUEL CONTROL, SEE CONT CARDS 103240 & 103245 FOR WORK COMPLETED. OK FOR SERVICE. CHANGED IAW AMM 73-21-01. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,662 hrs · 18,556 cycles

BURNED JET FUEL ODOR ON BOTH LEFT AND RIGHT PACK WHILE BLEEDING OFF OF BOTH THE ENGINES AND WHEN BLEEDING OFF THE APU. PERFORMED LEFT AND RIGHT PACK RUN FROM APU AND VERIFIED NO FUEL LEAK OR FUEL ODOR AT THIS TIME. COMPLIED WITH SMOKE AND FUME WORK SCOPE.

Part: COALESCER BAG — ODOR · airframe 18,662 hrs · 18,556 cycles

BURNED FUEL ODOR EVIDENT FROM PACKS DURING ALL PHASES OF FLIGHT. INSPECTED APU & ENGINES FOR OIL OR FUEL LEAKS. CHECKED IAW AMM 71-00-00 AND 49-30-00. NO LEAKS NOTED. R & R THE COALESCER BAGS IAW AMM 21-51-13. RAN THE PACKS AT FULL HOT FOR HALF HOUR WITH THE ENGINES AND APU. NO ODOR NOTED AT THIS TIME. ACFT OK FOR SERVICE.

Part: LIGHT — WORN (CABIN) · airframe 18,389 hrs · 18,273 cycles

ALL CABIN EMERGENCY LIGHTS DISCOLORED AND WORN. REMOVED & REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-01. OPS TESTED GOOD IAW AMM 33-51-00-710-802.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,389 hrs · 18,273 cycles

NR 1 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-16. OPS TESTED GOOD IAW AMM 33-51-00.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 18,389 hrs · 18,273 cycles

RIGHT SIDEWALL SEAT TRACK HAD CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11 AND REO 601R-53-00-055.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,389 hrs · 18,273 cycles

PAX CABIN FLOOR SEAT TRACKS AT RBL9 BETWEEN FS 409 - 409+112 HAVE CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11 AND REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 554-559) · airframe 18,389 hrs · 18,273 cycles

LEFT SIDEWALL SEAT TRACK HAD CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11 AND REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 499-541) · airframe 18,389 hrs · 18,273 cycles

LEFT SIDEWALL SEAT TRACK HAD CORROSION BS 499 - 541. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 18,389 hrs · 18,273 cycles

LEFT SIDEWALL SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 18,389 hrs · 18,273 cycles

LEFT SIDEWALL SEAT TRACK CORRODED. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11-020-002 A, & 53-01-11-420-001.

Part: ANGLE — CRACKED (BS 621) · airframe 18,389 hrs · 18,273 cycles

ANGLE AT AFT SIDE OF BS 621 BULKHEAD AND STRINGER L14 CRACKED. REMOVED AND REPLACED THE INTERCOSTAL ANGLE IAW SRM 51-42-21 & 51-42-22

Part: PANEL — CRACKED (PAX DOOR) · airframe 18,389 hrs · 18,273 cycles

PAX DOOR AFT RISER PANEL IS CRACKED AT FIRST FIXED STEP. REPAIRED PANEL IAW REO 601R-52-11-702.

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 18,389 hrs · 18,273 cycles

ANGLE AT AFT SIDE OF BS 621 BULKHEAD AND STRINGER L15 IS CRACKED. REMOVED & REPLACED THE ANGLE IAW SRM 51-42-21 & 51-42-22.

Part: ANGLE — CRACKED (BS 621) · airframe 18,389 hrs · 18,273 cycles

OBLIQUE ANGLE AT AFT SIDE OF FS621 BULKHEAD AND STRINGER R14 IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW REO 601R-53-61-422 REV NC, SRM 51-42-06, AND SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 18,389 hrs · 18,273 cycles

LEFT SIDEWALL SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11 AND REO 601R-53-00-485.

Part: ANGLE — CRACKED (WINDOW FRAME) · airframe 18,389 hrs · 18,273 cycles

PILOTS SIDE WINDOW FRAME HAS A CRACKED LOWER AFT ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 449-541) · airframe 18,389 hrs · 18,273 cycles

RIGHT SEAT TRACK HAD CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: ANGLE — CRACKED (WINDOW FRAME) · airframe 18,389 hrs · 18,273 cycles

CO-PILOTS SIDE WINDOW FRAME HAS CRACKED LOWER AFT ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21.

Part: PANEL — DAMAGED (PYLON) · airframe 18,389 hrs · 18,273 cycles

SEPARATOR PANELS ON PANEL 422DB ARE KNIFE EDGED. REMOVED & REPLACED 2 EA SEPARATOR PANELS ON PANEL 422DB IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,389 hrs · 18,273 cycles

PAX CABIN FLOOR SEAT TRACKS AT LBL9 BETWEEN FS 409-409+112 HAVE CORROSION . REMOVED & REPLACED FLOOR RAIL IAW AMM 53-01-11-020-002 B & 53-01-11-420-001 B.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 18,389 hrs · 18,273 cycles

LBL 27 CARGO TRACK AT BS 559+78 - 559+95 HAS CORROSION. REMOVED & REPLACED THE CARGO TRACK IAW AMM 53-00-49-020-001 A, & 53-00-49-420-001A.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 18,389 hrs · 18,273 cycles

RBL 9 SEAT TRACK FROM BS 559+4 TO 559+86 HAS CORROSION. REMOVED & REPLACED SEAT TRACK IAW AMM 53-01-11-020-002 B, & AMM 53-01-11-420-001 B.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 18,389 hrs · 18,273 cycles

LBL 9 CARGO TRACK FROM BS 559+86 TO 559+95 HAD CORROSION. REMOVED & REPLACED THE CARGO TRACK IAW AMM 53-00-49-020-001 A & 53-00-49-420-001A.

Part: DRAG ANGLE — CRACKED (PASSENGER DOOR) · airframe 18,389 hrs · 18,273 cycles

PAX DOOR AFT RISER DRAG ANGLE IS CRACKED BY ASSIST CABLE GUIDE. REPAIRED THE DRAG ANGLE AND RESTORED FINISH IAW REO 601R-52-11-513.

Part: BRACKET — CRACKED (BS 200) · airframe 18,389 hrs · 18,273 cycles

BRACKET FOR AC RECEPTACLE IS CRACKED. REMOVED AND REPLACED THE BRACKET IAW REO 601R-53-11-009.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 18,389 hrs · 18,273 cycles

RIGHT SIDEWALL SEAT TRACK HAD CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 18,389 hrs · 18,273 cycles

RIGHT SIDEWALL SEAT TRACK HAD CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: ACCESS PANEL — DAMAGED (PYLON) · airframe 18,389 hrs · 18,273 cycles

BOTH SEPARATOR PANELS ON PANEL 412DB ARE KNIFE EDGED. REMOVED & REPLACED THE SEPERATOR PANELS IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 18,389 hrs · 18,273 cycles

RIGHT SIDEWALL SEAT TRACK HAD CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 18,389 hrs · 18,273 cycles

RIGHT SIDEWALL SEAT TRACK HAD CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,389 hrs · 18,273 cycles

PAX CABIN RT FLOOR SEAT TRACK BETWEEN FS 379-409 HAS CORROSION. REMOVED & REPLACED SEAT TRACK IAW AMM 53-01-11-020-002 B & 53-01-11-420-001 B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,389 hrs · 18,273 cycles

PAX CABIN LT FLOOR SEAT TRACK BETWEEN FS 379-409 HAS CORROSION. REMOVED & REPLACED SEAT TRACK IAW AMM 53-01-11-020-002 B & 53-01-11-420-001 B.

Part: LIGHT — BROKEN (CABIN) · airframe 17,701 hrs · 17,552 cycles

EMERGENCY EXIT LIGHT CTR AISLE IS BROKEN. SECURED EMER EXIT SIGN IAW AMM 33-51-14.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 17,676 hrs · 17,527 cycles

CAPTAINS O2 MASK SPEAKER INOPERATIVE. OK TO DEFER OBSERVER AUDIO PANEL IAW MEL 23-51-06 CAT A MM02 UPDATED & PLACARD INSTALLED. SWAPPED THE OBSERVERS ACP TO THE CAPTAINS POSITION IAW AMM 23-51-04. OPERATIONS CHECKED GOOD. R & R ACP IAW AMM 23-51-04. MMO2 UPDATED & PLACARD REMOVED.

Part: LIGHT — BROKEN (CABIN) · airframe 17,450 hrs · 17,291 cycles

EXIT LIGHT ASSEMBLY ON LT WARDROBE, AFT WALL, BROKEN. R&R LIGHT ASSEMBLY PN BR9279-013 IAW AMM 33-51-13. OPERATIONS CHECKED GOOD.

Part: SPRING — MALFUNCTIONED (PAX DOOR) · airframe 16,539 hrs · 16,357 cycles

PASSENGER DOOR SLAMS SHUT & DOES NOT EXTEND OPEN WHEN INNER OR OUTER HANDLE IS UNLATCHED. R & R FWD & AFT COUNTERBALANCE GAS SPRINGS OF PAX DOOR IAW AMM 52-11-17. ALL CHECKED GOOD. SEE NRCC N70771 FOR WORK PERFORMED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 16,424 hrs · 16,233 cycles

ELECTRICAL BURNT & SHORT SMELL COMING FROM CAPTAINS SIDE WINDSHIELD HEATING MODULE ELEMENT ONLY OCCURRED ON LAST FLIGHT. PERFORMED VISUAL INSPECTION OF WIRES AROUND TERMINAL BLOCK ON THE CAPTAINS SIDE WINDSHIELD, NO SIGN OF BURNING OR ARCING WIRES. PERFORMED OPERATIONS CHECK OF WINDSHIELD HEAT WITH TASKS IN AMM 56-11-01. PERFORMED OPERATIONS CHECK OF MAP LIGHT IAW AMM 33-13-07 & TASK 33-13-00-710-801. OPERATIONS CHECK OF FLOOD LIGHTS IAW AMM 33-13-01 & TASK 33-13-00-710-801. ALL OPERATIONS CHECKED GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 16,064 hrs · 15,824 cycles

FLAPS FAIL CAUTION MSG ON APPROACH WHEN SELECTING FLAPS FROM 20 TO 30 DEGREES, EXTENSION. AIRSPEED OF 180 KNOTS & OAT OF -9 DEGREES C. QRH COMPLETE, LANDED WITH FLAPS AT 20 DEGREES. PERFORMED TROUBLESHOOTING IAW FIM REV 48 IAW AD 2009-06-12 PARAGRAPH H 6 I, AMOC LOG 14-105 DATED 12/30/2014 & TS 001100R1 FIM TECHNICAL SUPPLEMENT. FAULT CODES 19C1 & 19C2. FLAPS RESET & OPERATIONS TESTED GOOD IAW AMM 27-54-00.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 15,919 hrs · 15,669 cycles

GEAR DISAGREE WARNING MLG DOWN & LOCKED NORMALLY NLG HANDLE UP. NLG DOORS WERE OPEN. USED LG EMER RELEASE HANDLE IAW QRH. NOSE GEAR CAME DOWN IMMEDIATELY. NOSE WHEEL STEERING INOPERATIVE AFTER LANDING. R & R NLG SELECTOR VLV IAW AMM 32-33-10. OPERATIONS & LEAK CHECKED GOOD. OPERATIONS CHECK NWS IAW AMM 32-51-00, NO FAULT FOUND ON NWS.

Part: GROMMET — MISSING (RT ENGINE) · airframe 15,449 hrs · 15,192 cycles

RIGHT ENG VGV MISSING GROMMET & SEVERAL LOOSE. SEAL AT AFT BOTTOM CORNER OF RT ENG ATR BOX IS TORN 432-24. R & R RT ENG IAW CF 34 3 ENG CHANGE CHECKLIST & IAW AMM 71-00-00. COMPLIED WITH ALL REQUIRED OPERATIONS & LEAKS CHECK IAW CF 34 3 ENG CHANGE CHECKLIST & AMM 71-00-00-400-801, NO DEFECTS NOTED. TW 2797 DUE 11/06/14, MILLIOHM METER 13 DUE 8/20/15, TW 2796 CAL DUE 8/6/15 & TW 1209 DUE 12/12/14. R & R ENG IAW WO 54944 4000 0048.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 15,449 hrs · 15,191 cycles

FS 202 BULKHEAD CRACKED AT BRAKE CABLE PASS THROUGH. REPAIRED IAW REO 601R-53-11-563.

Part: RELAY — FAULTY (ELECTRICAL SYS) · airframe 14,714 hrs · 14,434 cycles

ACFT ESS BUS CAUTION JUST AFTER ROTATION COMPLETED, QRH, NO FIX MSG CONTINUED TO CYCLE ON & OFF 4 - 6 TIMES PER MINUTE. ALL SYSTEMS REF IN QRH THAT ARE LOST CONTINUED TO FUNCTION NORMALLY. EMERGENCY LIGHTS CYCLED ON & OFF WITH CAUTION MSG. R & R ESS BUS SENSE RELAY K1XD IAW MM CH 24-51-27, ALL CHECKED GOOD.

Part: LIFE VEST — TORN (CABIN) · airframe 13,588 hrs · 13,316 cycles

ONE INFANT LIFE VEST TORN, REMOVED INFANT LIFE VEST IAW PA 25-096A.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 13,496 hrs · 13,225 cycles

LEFT PACK HIGH PRESSURE ILLUMINATED ON TAKEOFF ROLL. RAN QRH ON CLIMBOUT. PACK WOULD ONLY RESET WITH APU RUNNING. AIR RETURN, NO EMERGENCY DECLARED. C TAXIED ACFT TO RUN PAD AND PRESSURIZED BOTH PACKS FROM ENGINES IAW AMM 21-50-00-863-805. NO DEFECTS NOTED AT ALL POWER SETTINGS. AIRCRAFT OK FOR SERVICE.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 12,477 hrs · 12,229 cycles

LEFT ELEVATOR HAS 4 AREAS OF THE LEADING EDGE OF THE UPPER SKIN THAT ARE DAMAGED AT THE HINGE POINTS. REPAIRED IAW BOMBARDIER REO 601R-55-21-379.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,476 hrs · 12,229 cycles

FLOOR CLIP AT FS 280 AND RBL 9 IS CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-136.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,476 hrs · 12,229 cycles

LEFT FS 480 CLIPS CRACKED AT LBL 27 AND LBL 30. REPAIRED IAW BOMBARDIER REO 601R-53-41-059.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 12,476 hrs · 12,229 cycles

FLOOR STRUCTURE IS CRACKED AND FS 280 BULKHEAD AT LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,476 hrs · 12,229 cycles

LEFT FS 480 CLIPS CRACKED AT LBL 27 AND LBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-41-059.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,476 hrs · 12,229 cycles

RIGHT FS 480 CLIPS CRACKED AT RBL 27 AND RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-41-059.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,476 hrs · 12,229 cycles

FLOOR CLIP AT FS 280 AND LBL 9 IS CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-136.

Part: LIGHT — CRACKED (CABIN) · airframe 12,100 hrs · 11,853 cycles

EMERGENCY LIGHTING ASSEMBLY, IN ZONE 231 FORWARD WALL OF PASSENGER ENTRANCE, IS CRACKED. REPLACED EMERGENCY LIGHTING ASSEMBLY AT FLOOR LEVEL EXIT SIGN NEAR PASSENGER DOOR IAW CRJ200 AMM 33-51-10. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 10,917 hrs · 10,540 cycles

DURING THE CEILING LIGHTS CHANGE, NOTED BATTERY PACK FOR EMERGENCY LIGHTS AT FS 439 INOP. REMOVED AND REPLACED EMERGENCY BATTERY CHARGER AT FS 439 P/N 11-0049 S/N OFF C02905 S/N ON C02760, AND REPLACED NEW BATTERY ASSY P/N 2013-1A, S/N OFF 69331 S/N ON 105842. OPS TEST GOOD IAW AMM 33-51-04.

Part: WIRE — FAILED (POWER RECEPTICAL) · airframe 9,547 hrs · 8,962 cycles

CREW AND OPS REPORTED EXT POWER CORD WAS PULLED TIGHT AGAINST AC RECEPTACLE UPON JET BRIDGE MOVEMENT WITH POWER CORD ATTACHED. FOUND AIRCRAFT SUSTAINED STRUCTURAL DAMAGE BEHIND RECEPTACLE. REMOVED EXTERNAL AC POWER RECEPTACLE PER 200 AMM 24-41-03. COVERED AND SECURED EXT. AC WIRE TERMINALS PER REO 601R-53-11-2082. DEFERRED EXT AC PER 200 MEL 24-41-3C. ENTERED INTO MM02, MXC NOTIFIED 990267 REO 601R-53-11-2082. SECURED EXT A/C DOOR CLOSED WITH SPEED TAPE. REPLACED EXTERNAL AC RECEPTACLE BACKING PLATE AND RECEPTACLE IAW SRM AND REO 601R-53-11-569. REMOVED FROM MM02 MXC NOTIFIED 22609.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,218 hrs · 8,596 cycles

FWD OVERWING EMERGENCY LIGHT INOP. FWD OVERWING EMERGENCY LIGHT RE-LAMPED PN ON/OFF 1317.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,285 hrs · 6,532 cycles

ON RT SIDE OF FUSELAGE, THE MIDDLE OF THE 3 OVERWING EMERGENCY LIGHTS INOP. RELAMPED IAW AMM 33-51-21. OPS CHECK GOOD. P/N ON/OFF:1317.

Part: UNKNOWN — VAPOR (CABIN) · airframe 6,839 hrs · 6,056 cycles

ON DESCENT INTO DSM, F/A REPORTED A BLUE HAZE SMOKE WITH NO ODOR FILLED THE CABIN. CHECKED APU OIL LEVEL AND COMPARTMENT, FOUND FULL AND DRY, OPERATED APU PER AMM 49, FOUND NO FAULTS, OIL LEAKS.

Part: ENGINE — ODOR (APU) · airframe 6,404 hrs · 5,593 cycles

HOT ELECTRICAL ODOR IN THE COCKPIT AND GALLEY. LANDED UNDER WT 47000 LBS. INSPECTED COCKPIT, CABIN AND GALLEY FOUND APU TO BE GIVING OFF ODOR INTO ACM. MEL'D APU PER 49-10-1(C) ENTERED INTO MMO2 MX NOTIFIED 18175 RAN ENGINE NR 1 AND NR 2 PACKS TO VERIFY NORMAL ODOR OPS CHECK GOOD. MX PROCEDURE ON PAGE 49.7 COMPLIED WITH. PERFORMED A VISUAL INSPECTION OF APU AND SYS COMPONENTS, RAN APU FOR 20 MIN. NO ODORS DETECTED IN CABIN, FLIGHT DECK OR APU AREA, OIL LEVEL WAS AT SERVICEABLE LEVEL. COULD NOT DUPLICATE DISCREPANCY FROM MM02 MXC 18106.

Part: PROXIMITY SENSOR — MALFUNCTIONED (RT MLG) · airframe 5,837 hrs · 5,005 cycles

AFTER TAKEOFF WHEN GEAR HANDLE WAS SELECTED UP WE RECEIVED A RED MASTER WARNING FOR GEAR DISAGREE AND THE ACCOMPANYING AURAL ALERT ALSO RIGHT MAIN GEAR SHOWED RED HAS MARKS PULLED LANDING GEAR MANUAL RELEASE HANDLE AND EICAS SHOWED THREE GREEN. THE CREW FOLLOWED THE POM AND RETURNED TO AND LANDED IN CVG. AN EMERGENCY WAS DECLARED. AFTER FOLLOWING THE POM THE CREW WAS ABLE TO ESTABLISH 3 GREEN GEAR INDICATION FOR LANDING. THE AIRCRAFT WAS TOWED TO THE GATE. RETRIEVAL CODES FROM PSEU AND FOUND RT MLG NOT UP AND LOCKED FOUND RT MLG UPLOCK TARGET LOOSE TORQUED RT MLG UPLOCK TARGET AND ADJUSTED PROXIMITY SENSOR PERFORMED GEAR SWING AND FOUND SYSTEM TO BE OPERATING NORMALLY AT THIS TIME IAW CRJ AMM 32-32-05.

Part: INDICATION SYS — MALFUNCTIONED (MLG) · airframe 5,829 hrs · 4,997 cycles

ON DEPARTURE FROM MLI, THE RIGHT GEAR LIGHT STAYED RED AND THEY GOT THE GEAR DISAGREE LIGHT. THE CREW FOLLOWED THEIR PROCEDURES AND WAS ABLE TO GET THE GEAR DOWN AND LOCKED WITH NORMAL INDICATIONS. THE FLIGHT RETURNED TO MLI WITHOUT INCIDENT. CYCLED GEAR NORM/EMERGENCY RETRACTION OPS CHECK GOOD. CK OP OF FLT CONTROL PRIORITY VALVE.

Part: SKIN — GOUGED (BS 349 S16L) · airframe 5,793 hrs · 4,961 cycles

FUSELAGE SKIN GOUGE FS 349 S16L REQUIRES PERMANENT REPAIR. REPAIRED LT FUSELAGE AT FS 349 AND S16L IAW MESABA EO NR C53047.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 4,330 hrs · 3,520 cycles

2 EXTERNAL EMERGENCY LIGHTS FOUND INOPERATIVE DURING LINE CHECK. EMERGENCY BATTERY PACK DEAD. REMOVED AND REPLACED BATTERY, PS4LF, PS4LF P/N ON: 2013-1A, P/N OFF: 2013-BR, S/N ON: 101367, S/N OFF: B0298 IAW CRJ200 TASKCARD 33-900-701.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 4,330 hrs · 3,520 cycles

2 EXTERNAL EMERGENCY LIGHTS FOUND INOPERATIVE DURING LINE CHECK. REMOVED AND REPLACED BATTERY, IAW TASKCARD 33-900-701.