N8968E

Part: COFFEEMAKER — FUMES (GALLEY) · airframe 30,420 hrs · 28,639 cycles

COFFEE MAKER EMITTED FUMES IN FLIGHT, TURNED IT OFF AND THE FUMES WERE MITIGATED BUT SMELL STILL EXISTS FLIGHT 3643 - FILED CLOSEDDEFERRED COFFEE MAKER. COMPLIED WITH MX ACTION. PLACARDS INSTALLED. AUTH. BY MCC.

Part: FRAME — CORRODED (BS 605) · airframe 30,263 hrs · 28,454 cycles

FS 605.0 FRAMAE CORRODED BETWEEN STR 21L AND STR 22L (C-CHECK) RO 12/31/2019 BLENDED CORROSION ON FRAME. FOUND CORROSION OUT OF LIMITATIONS IAW CRJ200 SRM. REMOVED FRAME BETWEEN LEFT AND RIGHT FACTORY SPLICES. MATCH DRILLED REPLACEMENTAND INSTALLED WET IAW CRJ200 SRM. COMPLETED FORM M-337. COMPLETED SKY FORM.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 30,263 hrs · 28,454 cycles

FS 589.0 BETWEEN LBL9 AND LBL 27 FLOOR SUPPORT HAS POSSIBLE CORROSION (C-CHECK) RO 12/31/2019 DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED AND MANUFACTURED PART PER BOMBARDIER DRAWING. -R PART MARKED "AVMAX P/N 60135031-165" INSTALLED MANUFACTURED PART AT F.S. 589.0 BETWEEN LBL 9 AND LBL 27 PER CRJ200 SRM.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 30,263 hrs · 28,454 cycles

LH SIDE SEAT RAILS FROM FS 409.00+128 TO FS 559.00+79 HAVE AREAS OF CORROSION (C-CHECK) RO 12/31/2019 REMOVED L/H SIDEWALL SEAT TRACKS FROM STA. 409 +128 TO STA. 559 +80 AND INSTALLED REPLACEMENT SEAT TRACKS IAW CRJ 200 AMM. FABRICATED REPLACEMENT LH SIDE SEAT RAILS 3EA IAW REO. 10-50 IN/LB TQ WRENCH, AV 7327 CAL: 11/20

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 30,263 hrs · 28,454 cycles

RH SIDE SEAT RAILS FROM FS 409.00+128 TO FS 559.00+79 HAVE AREAS OF CORROSION. (C-CHECK) RO 12/31/2019 REMOVED CORROSION PER CRJ 200 SRM. FOUND TO BE OUT OF LIMITS PER CRJ 200 SRM. LOCATED, DRILLED, ALODINED, FR PRIMED, TOP COATED AND INSTALLED NEW SEAT TRACKS PER CRJ 200 SRM. OK TO INSTALL SEAT TRACKS. TORQUED SCREWS PER CRJ 200 AMM. REFERENCE: REFERENCE AMM FOR REMOVAL/INSTALLATION. CALIBRATED TOOLS USED: TORQUE WRENCH (50" IN. LBS.), ID NO.: AV7327. CAL DUE: 11/20. DIGITAL CALIPERS, ID NO. AV7110, CAL DUE: 6/20. DAIL DEPTH GAGE, ID NO.: AG1186, CAL DUE: 12/20. PARTS USED: (2 EA.) SEAT TRACKS P/N 6656-0160, BATCH NO. 151708. (9 EA.) SCREW, P/N NAS 517-3-3, BATCH NO.: 143033. (20 EA.) SCREW, P/N NAS 517-3-4, BATCH NO.: 151782, (8 EA.) SCREW, P/N NAS 517-3-5, BATCH NO. 150425. (20 EA.) SCREW, P/N NAS 517-6-6, BATCH NO.: 135917. (8 EA.) SCREW, P/N B/AS1580A3T18, BATCH NO.: 149043. (44 EA.) WASHER, P/N NAS1149DO363K, BATCH NO.: 150388. (8 EA.) SCREW, P/N NAS1580A3T17, BATCH NO.: 65S-1532. (8 EA.) SCREW, P/N NAS1580A3T16, BATCH NO.: 135716. (A/R) ALODINE 1132 PEN, P/N 1445846, BATCH NO. 150857.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 30,263 hrs · 28,454 cycles

CROSS BEAM FLOOR SUPPORT AT 559.0 BETWEEN LBL 27 TO LBL 32.0 CORRODED (C-CHECK) RO 12/31/2019 BLENDED PER SRM. FOUND TO BE OUT OF LIMITS. REMOVED LH STRAP PN 601R31025-29, FS 559.00 LBL27-LBL42. FABRICATED REPLACEMENT STRAP PER DRAWING FROM 0.050 7075 T6. MARKED PART (AVMAX PN 601R3102-29) INSTALLED NUTPLATES ON STRAPS AND INSTALLED STRAP PN 601R31025-29 IAW SRM / CAL. TOOL AV7110 DATE JUN/2020.

Part: SEAT TRACK — CORRODED (BS 547-559) · airframe 30,263 hrs · 28,454 cycles

SEAT TRACK LBL 9 AT FS 547.0 TO FS 559.0+72 CORRODED (C-CHECK) RO 12/31/2019 REMOVED CORROSION PER CRJ 200 SRM 51-21-11. FOUND TO BE OUT OF LIMITS PER SRM. REQUESTED REO'S TO REWORK SEAT TRACK(S). COMPLIED WITH ALL (4 EA.) REO'S. OK TO INSTALL SEAT TRACK(S). CUT, LOCATED, DRILLED, ALODINED, FR PRIMED, TOP COATED AND INSTALLED NEW SEAT TRACK(S) PER CRJ 200 SRM. TORQUED SCREWS (35" IN. LBS.) PER CRJ 200 AMM, NDI WAS PERFORMED PER CRJ 200 NTM NO DEFECTS FOUND. CALIBRATED TOOLS USED: TORQUE WRENCH, ID NO.: AV7330. CAL DUE: 11/20. DIGITAL CALIPERS, ID NO. AV7110, CAL DUE: 6/20. DAIL DEPTH GAGE, ID NO.: AG1186, CAL DUE: 12/20. PARTS USED: (2 EA.) SEAT TRACK(S), P/N 6656-160, BATCH NO. 151708. (20 EA.) SCREW, P/N NAS 517-3-3, BATCH NO.: 149261. (20 EA.) SCREW, P/N NAS 517-3-4, BATCH NO.: 151821. (3 EA.) BLIND NUT P/N BN360-428-3, BATCH NO.: 152046. (3 EA.) BLIND NUT, P/N BN360-428-5, BATCH NO.: 152090. (3 EA.) BLIND NUT, P/N BN360PB1032DU3, BATCH NO.: 151642. (A/R) ALODINE 1132 PEN, P/N 1445846, BATCH NO. 150857. FR PRIMER, P/N CA7233, BATCH NO. 145102. TOP COAT - INTERI

Part: FLOORBEAM — CORRODED (BS 280) · airframe 30,263 hrs · 28,454 cycles

CORROSION FOUND ON 280 BEAM FLOOR SUPPORT AT STATION FS 280 AND BL0.00 (C-CHECK) RO 12/31/2019 CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED NEW 280 BEAM FLOOR SUPPORT ANGLE. ALODINED, PRIMED AND PAINTED. WET INSTALLED ALL FASTENERS. IAW CRJ200 SRM.

Part: FLOORBEAM — CRACKED (BS 559) · airframe 30,263 hrs · 28,454 cycles

FS 559.0 AT RBL 27 TO SILL PLATE CROSS BEAM FLOOR SUPPORT CORRODED (C-CHECK) RO 12/31/2019 BLENDED PER SRM. FOUND OUT OF LIMITS. REMOVED STRAP PN 601R31025-29 FS 559.00, RBL 27-RBL 42 PER SRM. FABRICATED REPLACEMENT STRAP FROM 0.050" 7075 T6 PER DRAWING 601R31025 REV N 7-11-90. INSTALLED REPLACEMENT STRAP PN 601R31025-29 IAW SRM 51-42-06, SRM 51-23-00, SRM 51-40-11. INSTALLED NUTPLATES ON STRAP / PIN MIC AV1070 12/19 DIGITAL CALIPERS AV7110 6/20

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,263 hrs · 28,454 cycles

CRACK FOUND ON CLIP AT STA FS280 LBL 8.0. CRACK FOUND ON CLIP AT STA FS 280 LBL 10.0 CRACK ON 280 BEAM AT STATION FS 280+LBL 11.0. CRACK FOUND ON OB CLIP AT STATION FS 280 RBL 10.0 (C-CHECK) RO 12/31/2019 PERMANENTLY REPAIRED. CUT-OUT DAMAGED AREA AND INSTALLED REPAIR PARTS IAW REO. COMPLETED STRUCTURAL REPAIR FORM AND M-337 FORM.

Part: BULKHEAD WEB — GOUGED (BS 621) · airframe 30,263 hrs · 28,454 cycles

AFT PRESSURE BULKHEAD- GOUGED RBL 27.50 30" ABOVE FLOOR (C-CHECK) RO 12/31/2019 DAMAGE FOUND TO BE OUT OF LIMITS PERFORMED CUTOUT AND MANUFACTURED AND INSTALLED REPAIR DOUBLERS ON AFT PRESSURE BULKHEAD AT RBL 27.50 30" ABOVE FLOOR IAW BOMBARDIER REO. ACCOMPLSHED HFEC PER CRJ 200 NTM. NO DEFECTS NOTED. ACCOMPLISED U/T THICKNESS CRJ200 NTM. OLYMPUS 600 NORTEC, AV8958 CAL DUE: JULY, 2020. OLYMPUS 605 EPOC AV8959 CAL DUE: JULY,2020. PRESSURIZATION LEAK CHECK: GOOD / ** REF M337- WEIGHT NEGLGIBLE** / ** REF REO FOR IN SERVICE REINSPECTION REQUIREMENTS.**

Part: BULKHEAD WEB — GOUGED (BS 621) · airframe 30,263 hrs · 28,454 cycles

AFT PRESSURE BULKHEAD- GOUGED RBL 36.20 30" ABOVE FLOOR (C-CHECK) RO 12/31/2019 DAMAGE FOUND TO BE OUT OF LIMITS PERFORMED CUTOUT AND MANUFACTURED AND INSTALLED REPAIR DOUBLERS ON AFT PRESSURE BULKHEAD AT RBL36.20 30" ABOVE FLOOR IAW BOMBARDIER REO. ACCOMPLSHED HFEC PER CRJ 200 NTM. NO DEFECTS NOTED. ACCOMPLISED U/T THICKNESS CRJ200 NTM 51-00-04 PART1. OLYMPUS 600 NORTEC, AV8958 CAL DUE: JULY, 2020. OLYMPUS 605 EPOC AV8959, CAL DUE: JULY,2020. PRESSURIZATION CHECK: GOOD / ****WEIGHT CHANGE- NEGLIGIBLE**** / **** REF: (REO) FOR IN-SERVICE DEVIATION INSPECTION REQUIREMENTS.****

Part: SUPPORT — CRACKED (CARGO DOOR TRACK) · airframe 30,263 hrs · 28,454 cycles

BOTTOM FITTING FOR CARGO DOOR FWD TRACK SUPPORT ASSY I/B OF FRAME FS 574.00 IS CORRODED (C-CHECK) RO 12/31/2019 REMOVED FASTENERS AND CRACKED PART. INSTALLED NEW PART AND FASTENERS, SEALENT AND PAINTED. TORQUED BOLTS TO 25 POUND INCHES. ALL WORK PERFORMED IAW BOMBARDIER CRJ 200 SRM. EQUIPMENT USED: TORQUE WRENCH AV6522 CAL DUE JAN 2020.

Part: ACM — SMOKE · airframe 29,960 hrs · 28,117 cycles

ON FINAL APPROACH AROUND 500 FEET BOTH THE FO AND CA SMELLED SMOKE. INITIAL THOUGHT WAS THAT IT WAS FROM A FIRE OUTSIDE ON THE GROUND. THERE WAS NO SIGN OF SMOKE IN THE AIRPLANE AT THE TIME. LANDING WAS NORMAL AND AROUND 80 OR 70 KNOTS THE FO CALLED OUT SMOKE. IT APPEARED TO BE COMING FROM THE CA SIDE. THE SMOKE BEGAN TO GET THICKER. WE PULLED THE AIRPLANE ONTO THE NEXT TAXIWAY AND CALLED THE FA, HE SAID THERE WAS SOME SMOKE IN THE CABIN. AS THE FO AND CA WERE RUNNING OUR CHECKLIST WE GOT A SMOKE TOILET CAUTION MESSAGE. THERE WERE NO PRIOR EICAS MESSAGES, IRREGULAR ENGINE GAUGES, OR HOT BRAKES. THE BLEEDS WERE ON THE APU, WHICH WE STARTED ON DESCENT PASSING THROUGH 9,500 FEET. WE DIDN€™T NOTICE IF ANY CIRCUIT BREAKERS WERE POPPED PRIOR TO LEAVING THE AIRCRAFT. REMOVED AND REPLACED LEFT ACM IAW AMM. ALSO REMOVED AND REPLACED LEFT AND RIGHT ACM COALESCER BAGS IAW AMM. PERFORMED ENGINE RUNS AT MULTIPLE POWER SETTINGS WITH PACKS RUNNING OFF ENGINE BLEEDS.

Part: IDG — UNDERSERVICED (NR 2) · airframe 28,522 hrs · 26,459 cycles

IDG 2 CAUTION IN FLIGHT. IDG 2 DISCONNECTED PER QRH. [FLT #4562] CLOSED SERVICED IDG IAW AMM. DEFERRED #2 IDG IAW MEL.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 28,433 hrs · 26,358 cycles

NOSE GEAR DOOR AND GEAR DISAGREE WARNING MESSAGES ON DEPARTURE, RAN QRH PROCEDURES, MESSAGES CLEARED, DOWN AND THREE GREEN INDICATIONS. NORMAL LANDING. (FLT 4118) CLOSED ADJUSTED PROX SENSOR PS14GA TO CORRECT TARGET CLEARANCE IAW AMM. PERFORMED MULTIPLE GEAR SWINGS IAW AMM. OPS CHK NORMAL.

Part: DOOR SILL — CORRODED (BS 574-621) · airframe 26,965 hrs · 24,735 cycles

AFT CARGO CUT-OUT AT BS 574 TO 621 LOWER SILL IS CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED THE DOOR SILL IAW SRM AND REO.

Part: DOOR SILL — CORRODED (BS 319-349) · airframe 26,965 hrs · 24,735 cycles

SERVICE DOOR LOWER SILL HAS CORROSION AT FWD EDGE BS 319 AND AFT EDGE BS 349. REPLACED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 26,965 hrs · 24,735 cycles

LEFT AFT CARGO FLOOR SUPPORT, BS 559 + 112 TO 621, LBL 27 IS CORRODED IN SEVERAL AREAS. REPLACED THE FLOOR SUPPORT IAW SRM.

Part: STRUCTURE — DENTED (BS 672-682) · airframe 26,965 hrs · 24,735 cycles

DENT LOCATED BETWEEN BS 672.2 AND 682. REPAIRED IAW REO.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 26,965 hrs · 24,735 cycles

THERE IS A DENT LOCATED ON THE RIGHT WING INBOARD FLAP LOWER SKIN. REPAIRED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 23,320 hrs · 20,744 cycles

LEFT FLOOR SEAT TRACK HAS MULTIPLE AREAS OF CORROSION, BS 409+125 -- 559+4 LBL 9. R & R THE SEAT TRACK IAW SRM AND AMM.

Part: DOOR FRAME — DAMAGED (OXYGEN ACCESS) · airframe 22,594 hrs · 20,034 cycles

BIRD STRIKE, RT SIDE NOSE ON THE O2 ACCESS PANEL DOOR FRAME. R & R IAW SRM.

Part: ACTUATOR — INOPERATIVE (NR 1) · airframe 21,471 hrs · 18,923 cycles

DECLARED EMER FOLLOWED NEW POLICY IN FOM. PROGRESSIVELY GOT WORSE INTO DUTCH ROLL. OSCILLATING BOTH DIRECTIONS, FOLLOWED QRH DISCONNECT YD. HARD PUSH ON RT RUDDER, NEEDED TO COUNTER WITH LT INPUT PRIMARILY, ONCE IT LEVELED DRIFTED TO LT FROM HAVING INPUT TO CORRECT THE PUSH ON RT. LANDED SAFELY & CONTACTED MOC. VERIFIED NR 1 YAW DAMPER ACTUATOR FAILS DURING OPERATIONAL CHECK INITIALLY, HARD FAIL WOULD NOT RESET. R & R NR 1 & 2 IAW MX CONTROL, YAW NR 1 DAMPER ACTUATOR WITH SERVICEABLE ACTUATOR IAW AMM 22-22-01 & SYS OPERATIONAL TEST GOOD IAW AMM 22-22-01.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 21,413 hrs · 18,856 cycles

CAPTAIN'S LIFE VEST PACKAGE TORN. R & R LIFE VEST.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,172 hrs · 18,619 cycles

ROOF EMER LIGHT OVER ROW 5 OTS. RELAMPED IAW MM 33-51-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — DELAMINATED (CABIN) · airframe 20,773 hrs · 18,229 cycles

EMERGENCY LIGHT ON RT SIDE AT ROWS 11 - 12, SECOND TO LAST PIECE WITH ARROWS, DELAMINATED MIDWAY.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 20,798 hrs · 18,194 cycles

EMERGENCY FLOOR PATH LIGHTING, PHOTO LUMINESCENT, STRIP AT ROWS 11 - 12 C & D HAS DELAMINATION MEASURING ABOUT 4 INCHES IN LENGTH AT MID-POINT OF STRIP.

Part: PBE — UNSERVICEABLE (COCKPIT) · airframe 20,732 hrs · 18,189 cycles

COCKPIT & WARDROBE PBES BOTH SQUISHY. R & R COCKPIT & WARDROBE PBE'S IAW PBE USER REFERENCE & PROCEDURES MANUAL, OK FOR SERVICE.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 20,457 hrs · 17,922 cycles

FORWARD FACE OF FS 621 BULKHEAD HAS MULTIPLE SCREW MARKS, WL 76.5 TO WL 103.5, RBL 36.2 - LBL 9, 0.010 INCHES MAX DEPTH. REPAIRED IAW REO 601R-53-61-2155.

Part: PBE — DAMAGED (COCKPIT) · airframe 19,320 hrs · 16,801 cycles

PBE IS DAMAGED. R & R COCKPIT PBE IAW AMM 35-30-00. NO FURTHER DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,292 hrs · 16,776 cycles

EMERGENCY LIGHT OVER ROW 5 IS INOPERATIVE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,101 hrs · 16,586 cycles

FS 559 SEMI-PREUSSRE BULKHEAD CAP ANGLE FOUND CRACKED AT RBL 18 AND LBL 18. REPAIRED IAW PA 53-025C AND BOMBARDIER REO 601R-53-41-260 AND 601R-53-41-609.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,914 hrs · 16,404 cycles

CRACK FOUND ON FORWARD FACE OF FS621 BULKHEAD ALONG THE UPPER EDGE OF THE CARGO DOOR LINTEL 0.125" AFT OF INBOARD CORNER MEASURING 3/32" LONG. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: ECU — FAULTY (TE FLAP) · airframe 18,499 hrs · 15,996 cycles

WORK IN PROGRESS ON DM 76256 FLAP FAIL CAUTION MESSAGE. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 43 IAW AD2009-06-12 PARA (H) (6)(I), AMOC DATED 19,2012, AND PA AD27-052H. REMOVED AND REPLACED FECU IAW CRJ AMM 27-51-05-400-801. OPS CHECK GOOD. DEFERRAL DM76256 CLEARED.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 18,266 hrs · 15,762 cycles

CORROSION AROUND PAX DOOR PROX SWITCH ANGLE. REMOVED AND REPLACED IAW SRM 51-24-16.

Part: SEAT TRACK — GOUGED (FUSELAGE) · corrosion level 2 · airframe 18,266 hrs · 15,762 cycles

LEFT SIDE NR 3 SEAT TRACK GOUGED. REPAIRED IAW AMM 53-01-11.

Part: SKIN — CHAFED (LT SPOILER) · airframe 18,266 hrs · 15,762 cycles

LEFT FLIGHT SPOILER LOWER SURFACE CHAFED. DETERMINED TO BE WITHIN THE ALLOWABLE LIMITS OF BOMBARDIER REO 601R-57-73-204.

Part: SEAT TRACK — GOUGED (FUSELAGE) · corrosion level 2 · airframe 18,266 hrs · 15,762 cycles

LEFT SIDE NR 5 SEAT TRACK GOUGED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — GOUGED (FUSELAGE) · corrosion level 2 · airframe 18,266 hrs · 15,762 cycles

RIGHT SIDE NR 3 SEAT TRACK GOUGED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — GOUGED (FUSELAGE) · corrosion level 2 · airframe 18,266 hrs · 15,762 cycles

LEFT SIDE NR 6 SEAT TRACK GOUGED. REPAIRED IAW AMM 53-01-11.

Part: SPOILER — CHAFED (LT WING) · airframe 18,266 hrs · 15,762 cycles

LEFT FLIGHT SPOILER LOWER LEADING EDGE CHAFED. WITHIN THE LIMITS OF BOMBARDIER REO 601R-57-73-204.

Part: SEAT TRACK — GOUGED (FUSELAGE) · corrosion level 2 · airframe 18,266 hrs · 15,762 cycles

RIGHT SIDE NR 5 SEAT TRACK GOUGED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — GOUGED (FUSELAGE) · corrosion level 2 · airframe 18,266 hrs · 15,672 cycles

RIGHT SIDE NR 6 SEAT TRACK GOUGED. REPAIRED IAW AMM 53-01-11.

Part: SKIN — CHAFED (LT SPOILER) · airframe 18,266 hrs · 15,762 cycles

LEFT FLIGHT SPOILER LOWER SURFACE CHAFED INBOARD OF OUTBOARD HINGE. DETERMINED TO BE WITHIN THE ALLOWABLE LIMITS OF BOMBARDIER REO 601R-57-73-204.

Part: SEAT TRACK — GOUGED (FUSELAGE) · corrosion level 2 · airframe 18,266 hrs · 15,762 cycles

LEFT SIDE NR 4 SEAT TRACK GOUGED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — GOUGED (FUSELAGE) · corrosion level 2 · airframe 18,266 hrs · 15,762 cycles

LEFT SIDE NR 7 SEAT TRACK GOUGED. REPAIRED IAW AMM 53-01-11.

Part: SKIN — DENTED (LT SPOILER) · airframe 18,266 hrs · 15,762 cycles

LEFT FLIGHT SPOILER LOWER SURFACE DENTED INBOARD OF ACTUATOR HINGE. WITHIN THE LIMITS OF BOMBARDIER REO 601R-57-73-204.

Part: SEAT TRACK — GOUGED (FUSELAGE) · corrosion level 2 · airframe 18,266 hrs · 15,762 cycles

RIGHT SIDE NR 7 SEAT TRACK GOUGED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — GOUGED (FUSELAGE) · corrosion level 2 · airframe 18,266 hrs · 15,762 cycles

RIGHT SIDE NR 4 SEAT TRACK GOUGED. REPAIRED IAW AMM 53-01-11.

Part: STRUCTURE — NICKED (LT WING) · airframe 18,266 hrs · 15,762 cycles

LEFT WING PANEL CUTOUT AT WS 303.861, HOLES NR 16, HAS KNICK ON INNER LIP IN NON-CRITICAL AREA. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 18,266 hrs · 15,762 cycles

LEFT FUSELAGE HAS DENT AT FS 718. REPAIRED IAW SRM 53-00-31.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 17,931 hrs · 15,406 cycles

RECEIVED A GEAR DISAGREE AFTER RETRACTING THE GEAR AFTER TAKE OFF FROM IMT (FLIGHT NUMBER 3849) GEAR WAS EXTRACTED AND THREE LOCK INDICATIONS WERE GIVEN, CREW DID NOT DECLARE EMERGENCY AND LANDED. NOSE GEAR DRESSED ASSY REPLACED AND COMPLIANCE TO PA 05-018G ACCOMPLISHED. LANDING GEAR SYSTEM OPS CHECKS GOOD.

Part: DOOR — UNSECURE · airframe 178,121 hrs · 15,300 cycles

AFTER TAKEOFF, A LOUD NOISE FROM NOSE GEAR, VIBRATION IN BOTH RUDDER PEDDLES. NOISE AND VIBRATION CONTINUED UP TO 230 KNOTS. BELOW 160 KNOTS NOISE QUIT. QRH COMPLETED FOR STALL FAIL. EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO DEPARTURE. FOUND O2 SERVICE DOOR AND CAP OPEN. NO DAMAGE WAS FOUND TO DOOR OR SURROUNDING STRUCTURE CAP ON PANEL. CLOSED DOOR, OPS CHECK OF STALL PROTECTION SYS GOOD IAW AMM 27-35-00. OK FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 17,694 hrs · 15,175 cycles

RT SIDE WINDOW CRACKED DURING CLIMB-OUT. REMOVED AND REPLACED RT WINDOW IAW AMM 56-12-01. OK FOR SERVICE.

Part: PROXIMITY SWITCH — OUT OF POSITION (RT MLG) · airframe 17,480 hrs · 14,974 cycles

RT MAIN GEAR WILL NOT COME UP, GEAR DISAGREE MSG ON TAKEOFF QRH COMPLETED RETURNED TO DTW. ALL INDICATIONS NORMAL AFTER QRH PROCEDURE. COMPLIED WITH PA 05-018 REVF SCENARIO 1. REFER TO NON-ROUTINE WORK CARD N 24312 FOR WORK PERFORMED. RE-TIGHTENED UPLOCK (RT MLG) TARGET AND REPOSITIONED UPLOCK PROX SWITCH. TARGET DONE IAW CMM 32-30-15. PROX SWITCH DONE IAW AMM 32-32-05.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,142 hrs · 14,649 cycles

RBL 9 AND LBL 9 FS 280 CLIPS AND WEB CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,142 hrs · 14,649 cycles

FS 202.75 BULKHEAD IS CRACKED. REPAIRED IAW BOMBARDIER REO 601R53-11-563.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,142 hrs · 14,649 cycles

LEFT WING FUEL ACCESS PANEL CUTOUT AT 510AB HAS CORROSION. THE CUTOUT AT 550AB AND 550FH HAVE SMALL SCRATCHES. ALL ARE IN THE NON-CRITICAL ZONES. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 17,142 hrs · 14,649 cycles

SEAT TRACK AT LBL 9 AND RBL 9 AT FS 559 CORRODED. REPAIRED IAW SRM 51-21-06 AND 51-41-02.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 17,142 hrs · 14,649 cycles

AFT PRESSURE BULKHEAD FORWARD FACE HAS 12 AREAS SCRATCHED/DAMAGED ABOVE FLOOR FROM LONGER SCREWS. REPAIRED IAW REO 601R-53-61-2155.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 17,142 hrs · 14,649 cycles

LEFT INBOARD FLAP VANE EDGE HAS 3 CHAFES AT WS137, WS98.5, AND WS60. REPAIRED IAW BOMBARDIER REO 601R-57-52-004.

Part: SEAT BELT — OUT OF POSITION (CABIN) · airframe 18,257 hrs · 14,449 cycles

SEAT 13B SEATBELT FELL OFF. RE-ATTACHED SEATBELT AT SEAT 13B PER CMM 25-21-39.

Part: O-RING — DEFECTIVE (APU) · airframe 16,872 hrs · 14,416 cycles

APU AUTO SHUTDOWN, OIL PRESS WARNING, FUEL LEAK. REMOVED AND REPLACED APU FCU O-RING IAW AMM49-31-01 CLEAR DM, OP CHECK GOOD.

Part: ACTUATOR — OUT OF ADJUST (NLG DOOR) · airframe 16,595 hrs · 14,105 cycles

NOSE DOOR OPENS WITH HYD'S OFF & SERVICE PANEL SWITCH IN FLT NORM. ADJUSTED NOSE DOOR ACTUATOR IAW AMM 32-22-00. OPC GOOD SEVERAL TIMES A/C OK FOR SERVICE SEE AML 836191 FOR GEAR SWING.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 15,352 hrs · 12,957 cycles

ON APPROACH CREW RECEIVED RT MAIN LANDING GEAR DOWN DISAGREE "NO" EMERGENCY DECLARED FLIGHT LANDED WITHOUT INCIDENT.

Part: FLAP — FAILED (WING) · airframe 15,228 hrs · 12,846 cycles

FLAP FAIL. DEFERRED PER MEL 27-50-00 DM 40050.

Part: STRUT — LOW (NLG) · airframe 14,865 hrs · 12,532 cycles

GEAR DISAGREE. DEFERRED IAW MEL. INTEGRATED PSEU AND FOUND CODES (S22DOWNFAR, S30DOWNFAR, S31DOWNFAR, S32DOWNFAR, DI14DOWNON, DI15DOWNON) PERFORMED SERVICING OF NLG STRUT IAW AMM 12-12-32. OPS CHECK GOOD. C/W PA 05-018A THIS CLOSES WO 299210. THIS CLEARS DM 36280. OK FOR SERVICE. GEAR SWING OPS CHECK GOOD IAW AMM 32-30-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 14,808 hrs · 12,484 cycles

NOSE GEAR DISAGREE. C/W PA 05-018A. PSEU CODES (28FAR,S22 FAR, S30 FAR, S31 FAR S32FAR DI14ON,AI15ON DI11 PFF DI09 ON). OPS CHECKS GOOD IAW AMM 32-30-00. OK FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (NLG) · airframe 14,838 hrs · 12,493 cycles

CREW REPORTS A NLG DISAGREE AFTER TAKEOFF. MAINTENANCE WILL DEFER THE LANDING GEAR AND FLY WITH THE GEAR PINNED.

Part: WIRE HARNESS — DEFECTIVE (ITT) · airframe 14,223 hrs · 11,886 cycles

ON TAKEOFF ROLL AT KCVG, THE LEFT ENGINE ITT INDICATED AN OVER TEMPERATURE WHEN TAKEOFF POWER WAS SELECTED. A GATE RETURN WAS ACCOMPLISHED AND THE AIRCRAFT SWAPPED OUT. MAINTENANCE FOUND THE INBOARD ITT THERMOCOUPLE HARNESS BAD. THE THERMOCOUPLE HARNESS WAS REPLACED AND THE ENGINE RUNS WERE NORMAL. THE AIRCRAFT WAS RELEASED FOR SERVICE.