N447AW

Part: STRUT — DISCHARGED (NLG) · airframe 38,290 hrs · 37,140 cycles

AFTER TO NWS CAU MSG. C/W QRH MSG CLEARED. AIR RETURN TO DAY. ***AIRCRAFT REMOVED FROM SERVICE*** FOUND NLG STRUT EXTENSION LOW, DE-SERVICED AND SERVICED NLG STRUT WITH NITROGEN IAW 12-12-32. PERFORMED RIG CHECK OF LH AND RH FEEDBACK RVDT PER AMM 32-51-20. RIG CHECK GOOD. OPS TEST OF NWS SYSTEM IS GOOD PER AMM 32-51-10. NO FURTHER DEFECTS NOTED.

Part: VALVE — MALFUNCTIONED (NLG STEERING) · airframe 38,262 hrs · 37,106 cycles

RECEIVED NWS INOP CAUTION AFTER GEAR RETRACTION DURING DEPARTURE. C/W QRH. MSG PERSISTED. NO OTHER ASSOCIATED MSGS. SELECTED NWS AFTER LANDING, SEEMED TO BE OPERATIVE AND MSG CLEARED. AIRCRAFT REMOVED FROM SERVICE, REMOVED AND REPLACED EHSV IAW AMM 32-51-15. OPS CHECK OF NWS SYSTEM CHECKED GOOD IAW AMM 32-51-10. OKAY FOR SERVICE. P/N: 16736-105, S/N OFF: 1605, S/N ON: DU1315 ARW

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 37,929 hrs · 36,742 cycles

ON ARRIVAL AT GATE, PAX DOOR UNABLE TO OPEN FROM INSIDE OR OUTSIDE. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPERATIONAL TEST, IAW AMM 52-11-00-05. OPERATIONS CHECK OK, INSIDE AND OUTSIDE OPERATIONAL NORMAL.

Part: BONDING JUMPER — OUT OF POSITION (PICALO TUBE) · airframe 37,891 hrs · 36,699 cycles

REVIVED ANTI ICE DUCT WARNING MESSAGE ON DEPARTURE RAN QRH MESSAGE CLEARED. ANTI-ICE WAS SELECTED OFF. MESSAGE CLEARED WHEN 14TH STAGE VALVES WERE CLOSED. AIRCRAFT REMOVED FROM SERVICE. FOUND PICALO TUBE BONDING JUMPER BEHIND ACCESS PANNEL 630MZ LOOSE AND MAKING CONTACT WITH THERMAL SWITCH TERMINAL STUD. REPOSITIONED AND SECURED PICALO TUBE BONDING JUMPER BEHIND ACCESS PANNEL 630MZ, REF AWAC SUP 18-136 DATED 4/26/2018 AND CRJ200 AMM 30-11-41-400-801.

Part: ATTACH ANGLE — CRACKED · airframe 37,890 hrs · 36,698 cycles

SUSPECTED CRACK ON EXISTING REPAIR OF PAX DOOR AFT DRAG ANGLE INBOARD OF MOTOR ASSIST PULLEY. AIRCRAFT REMOVED FROM SERVICE. EVALUATED AND FOUND TO BE CRACKED 1.25''L. REMOVED EXISTING REPAIR, REF CRJ 200 SRM 51-42-22. FABRICATED REPAIR SPLICE FROM 601R1907-3015 UID 3579592, REF CRJ 200 SRM 51-31-59. INSTALLED REPAIR SPLICE, REF CRJ 200 SRM 51-42-06, 51-42-13 AND 51-42-22.

Part: FLOOR SUPPORT — CORRODED (BS 428) · corrosion level 2 · airframe 37,890 hrs · 36,698 cycles

LT PRESSURE FLOOR SILL PANEL AT FS 428 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL PANEL AT FS 428 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 0.70''L X 0.65''W. ORIGINAL THICKNESS MEASURES 0.055'', PER REO 601R-53-41-666 DATED 2012-11-06 REV-C. PERFORMED UT THICKNESS MEASUREMENT ON BLENDED AREA OF PRESSURE FLOOR SILL PANEL AT FS 428 AND LBL 47. THICKNESS MEASURES 0.051'', REF CRJ 200 NDTM PART 4 REV 41 51-00-001 UT GAUGE S/N DBT-CT-1033 CAL DUE 02/19/21. PERFORMED HFEC INSPECTION ON BLENDED AREA OF PRESSURE FLOOR SILL PANEL AT FS 428 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 NDTM PART 1 REV 41 51-20-06, NO INDICATIONS NOTED. EDDY CURRENT TESTER S/N 200051301 CAL DUE 01/24/21. EVALUATED REWORKED AREA OF PRESSURE FLOOR SILL PANEL AT FS 428 AND LBL 47 ORIGINAL THICKNESS IS 0.055'', REMAINING THICKNESS IS 0.051'', FOUND TO BE WITHIN LIMITS PER REO 601R-53-41-666 DATED 2012-11-06 REV-C.

Part: FLOOR SUPPORT — CORRODED (BS 556) · corrosion level 2 · airframe 37,890 hrs · 36,698 cycles

LT PRESSURE FLOOR SILL PANEL AT FS 556 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL PANEL AT FS 556 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 0.62''L X 0.57''W. ORIGINAL THICKNESS MEASURES 0.080'', PER REO 601R-53-41-666 DATED 2012-11-06 REV-C. PERFORMED UT THICKNESS MEASUREMENT ON BLENDED AREA OF PRESSURE FLOOR SILL PANEL AT FS 556 AND LBL 47. THICKNESS MEASURES 0.078'', REF CRJ 200 NDTM PART 4 REV 41 51-00-001 UT GAUGE S/N DBT-CT-1033 CAL DUE 02/19/21. PERFORMED HFEC INSPECTION ON BLENDED AREA OF PRESSURE FLOOR SILL PANEL AT FS 556 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 NDTM PART 1 REV 41 51-20-06, NO INDICATIONS NOTED. EDDY CURRENT TESTER S/N 200051301 CAL DUE 01/24/21. EVALUATED REWORKED AREA OF PRESSURE FLOOR SILL PANEL AT FS 556 AND LBL 47 ORIGINAL THICKNESS IS 0.080'', REMAINING THICKNESS IS 0.078'', FOUND TO BE WITHIN LIMITS PER REO 601R-53-41-666 DATED 2012-11-06 REV-C.

Part: FLOOR SUPPORT — CORRODED (BS 502) · corrosion level 2 · airframe 37,890 hrs · 36,698 cycles

LT PRESSURE FLOOR SILL ANGLE AT FS 502 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL ANGLE AT FS 502 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 1.15''L X 0.85''W. ORIGINAL THICKNESS MEASURES 0.080'', PER REO 601R-53-41-666 DATED 2012-11-06 REV-C. PERFORMED UT THICKNESS MEASUREMENT ON BLENDED AREA OF PRESSURE FLOOR SILL ANGLE AT FS 502 AND LBL 47. THICKNESS MEASURES 0.079'', REF CRJ 200 NDTM PART 4 REV 41 51-00-001 UT GAUGE S/N DBT-CT-1033 CAL DUE 02/19/21. PERFORMED HFEC INSPECTION ON BLENDED AREA OF PRESSURE FLOOR SILL ANGLE AT FS 502 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 NDTM PART 1 REV 41 51-20-06, NO INDICATIONS NOTED. EDDY CURRENT TESTER S/N 200051301 CAL DUE 01/24/21. EVALUATED REWORKED AREA OF PRESSURE FLOOR SILL ANGLE AT FS 502 AND LBL 47 ORIGINAL THICKNESS IS 0.080'', REMAINING THICKNESS IS 0.079'', FOUND TO BE WITHIN LIMITS PER REO 601R-53-41-666 DATED 2012-11-06 REV-C.

Part: PRESSURE DECK — CORRODED (BS 537) · corrosion level 2 · airframe 37,890 hrs · 36,698 cycles

LT PRESSURE FLOOR SILL PANEL AT FS 537 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL PANEL AT FS 537 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 0.57''L X 0.52''W. ORIGINAL THICKNESS MEASURES 0.055'', PER REO 601R-53-41-666 DATED 2012-11-06 REV-C. PERFORMED UT THICKNESS MEASUREMENT ON BLENDED AREA OF PRESSURE FLOOR SILL PANEL AT FS 537 AND LBL 47. THICKNESS MEASURES 0.054'' REF CRJ 200 NDTM PART 4 REV 41 51-00-001 UT GAUGE S/N DBT-CT-1033 CAL DUE 02/19/21. PERFORMED HFEC INSPECTION ON BLENDED AREA OF PRESSURE FLOOR SILL PANEL AT FS 537 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 NDTM PART 1 REV 41 51-20-06, NO INDICATIONS NOTED. EDDY CURRENT TESTER S/N 200051301 CAL DUE 01/24/21. EVALUATED REWORKED AREA OF PRESSURE FLOOR SILL PANEL AT FS 537 AND LBL 47 ORIGINAL THICKNESS IS 0.055'', REMAINING THICKNESS IS 0.054'', FOUND TO BE WITHIN LIMITS PER REO 601R-53-41-666 DATED 2012-11-06 REV-C REV C DTD 2012-11-06.

Part: FLOOR SUPPORT — CORRODED (BS 507) · corrosion level 2 · airframe 37,890 hrs · 36,698 cycles

RT PRESSURE FLOOR SILL ANGLE AT FS 507 AND RBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL ANGLE AT FS 507 AND RBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 0.64''L X 0.38''W. ORIGINAL THICKNESS MEASURES 0.080'', PER REO 601R-53-41-666 DATED 2012-11-06 REV-C. PERFORMED UT THICKNESS MEASUREMENT ON BLENDED AREA OF PRESSURE FLOOR SILL ANGLE AT FS 507 AND RBL 47. THICKNESS MEASURES 0.077'', REF CRJ 200 NDTM PART 4 REV 41 51-00-001 UT GAUGE S/N DBT-CT-1033 CAL DUE 02/19/21. PERFORMED HFEC INSPECTION ON BLENDED AREA OF PRESSURE FLOOR SILL ANGLE AT FS 507 AND RBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 NDTM PART 1 REV 41 51-20-06, NO INDICATIONS NOTED. EDDY CURRENT TESTER S/N 200051301 CAL DUE 01/24/21. EVALUATED REWORKED AREA OF PRESSURE FLOOR SILL ANGLE AT FS 507 AND RBL 47, ORIGINAL THICKNESS IS 0.080'', REMAINING THICKNESS IS 0.077'', FOUND TO BE WITHIN LIMITS PER REO 601R-53-41-666 DATED 2012-11-06 REV-C.

Part: FLOOR SUPPORT — CORRODED (BS 507) · corrosion level 2 · airframe 37,890 hrs · 36,698 cycles

LT PRESSURE FLOOR SILL ANGEL AT FS 507 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL ANGLE AT FS 507 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 0.64''L X 0.38''W. ORIGINAL THICKNESS MEASURES 0.080'', PER REO 601R-53-41-666 DATED 2012-11-06 REV-C. PERFORMED UT THICKNESS MEASUREMENT ON BLENDED AREA OF PRESSURE FLOOR SILL ANGEL AT FS 507 AND LBL 47. THICKNESS MEASURES 0.077'', REF CRJ 200 NDTM PART 4 REV 41 51-00-001 UT GAUGE S/N DBT-CT-1033 CAL DUE 02/19/21. PERFORMED HFEC INSPECTION ON BLENDED AREA OF PRESSURE FLOOR SILL ANGEL AT FS 507 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 NDTM PART 1 REV 41 51-20-06, NO INDICATIONS NOTED. EDDY CURRENT TESTER S/N 200051301 CAL DUE 01/24/21. EVALUATED REWORKED AREA OF PRESSURE FLOOR SILL ANGEL AT FS 507 AND LBL 47, ORIGINAL THICKNESS IS 0.080'', REMAINING THICKNESS IS 0.077'', FOUND TO BE WITHIN LIMITS PER REO 601R-53-41-666 DATED 2012-11-06 REV-C.

Part: FLOOR SUPPORT — CORRODED (BS 494) · corrosion level 2 · airframe 37,890 hrs · 36,698 cycles

LT PRESSURE FLOOR SILL PANEL AT FS 494 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL PANEL AT FS 494 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 0.80''L X 0.77''W. ORIGINAL THICKNESS MEASURES 0.055'', PER REO 601R-53-41-666 DATED 2012-11-06 REV-C. PERFORMED UT THICKNESS MEASUREMENT ON BLENDED AREA OF PRESSURE FLOOR SILL PANEL AT FS 494 AND LBL 47. THICKNESS MEASURES 0.054, REF CRJ 200 NDTM PART 4 REV 41 51-00-001 UT GAUGE S/N DBT-CT-1033 CAL DUE 02/19/21. PERFORMED HFEC INSPECTION ON BLENDED AREA OF PRESSURE FLOOR SILL PANEL AT FS 494 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 NDTM PART 1 REV 41 51-20-06, NO INDICATIONS NOTED. EDDY CURRENT TESTER S/N 200051301 CAL DUE 01/24/21. EVALUATED REWORKED AREA OF PRESSURE FLOOR SILL PANEL AT FS 494 AND LBL 47 ORIGINAL THICKNESS IS 0.055'', REMAINING THICKNESS IS 0.054'', FOUND TO BE WITHIN LIMITS PER REO 601R-53-41-666 DATED 2012-11-06 REV-C.

Part: FLOOR SUPPORT — CORRODED (BS 555) · corrosion level 2 · airframe 37,890 hrs · 36,698 cycles

LT PRESSURE FLOOR SILL PANEL AT FS 555.5 AND RBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL PANEL AT FS 555.5 AND RBL 47, PER REO 601R-53-41-666 AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 0.77''L X 0.50''W. ORIGINAL THICKNESS MEASURES 0.080'', PER REO 601R-53-41-666. PERFORMED UT THICKNESS MEASUREMENT ON BLENDED AREA OF PRESSURE FLOOR SILL PANEL AT FS 555.5 AND RBL 47. THICKNESS MEASURES 0.077'', REF CRJ 200 NDTM PART 4 REV 41 51-00-001 UT GAUGE S/N DBT-CT-1033 CAL DUE 02/19/21. PERFORMED HFEC INSPECTION ON BLENDED AREA OF PRESSURE FLOOR SILL PANEL AT FS 555.5 AND RBL 47, PER REO 601R-53-41-666 AND CRJ 200 NDTM PART 1 REV 41 51-20-06, NO INDICATIONS NOTED. EDDY CURRENT TESTER S/N 200051301 CAL DUE 01/24/21. EVALUATED REWORKED AREA OF PRESSURE FLOOR SILL PANEL AT FS 555.5 AND RBL 47 ORIGINAL THICKNESS IS 0.080'', REMAINING THICKNESS IS 0.077'', FOUND TO BE WITHIN LIMITS PER REO 601R-53-41-666 REV C DTD 2012-11-06.

Part: SKIN — GOUGED (BS 682) · airframe 37,890 hrs · 36,698 cycles

PROTRUDING DENT ON AFT FUSELAGE AT FS 682.00 BETWEEN STR 23R AND 24R. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CIRCULAR CUTOUT 1.5''D ON REPAIR AREA FS 682.00 BETWEEN STR 23R AND STR 24R, REF EA: AWAC-CRJ253-01514 REV IR DATED 10/13/20. PERFORMED HFEC INSPECTION ON CUTOUT AT FS 682.00 BETWEEN STR 23R AND STR 24R, PER EA: AWAC-CRJ253-01514 REV IR DATED 10/13/20 AND CRJ 200 NDTM PART 1 REV 41 51-20-06, NO INDICATIONS NOTED. EDDY CURRENT TESTER S/N 200051301 CAL DUE 01/24/21. FORMED REPAIR DOUBLER 2024-T3 0.063'', PER EA: AWAC-CRJ253-01514 REV IR DATED 10/13/20. INSTALLED REPAIR DOUBLER, IAW EA: AWAC-CRJ253-01514 REV IR DATED 10/13/20.

Part: FLOOR SUPPORT — CORRODED (BS 452) · corrosion level 2 · airframe 37,890 hrs · 36,698 cycles

LT PRESSURE FLOOR SILL ANGLE AT FS 452 AND LBL 47 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL ANGLE AT FS 452 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 0.80''L X 0.77''W. ORIGINAL THICKNESS MEASURES 0.080'', PER REO 601R-53-41-666 DATED 2012-11-06 REV-C. PERFORMED UT THICKNESS MEASUREMENT ON BLENDED AREA OF PRESSURE FLOOR SILL ANGLE AT FS 452 AND LBL 47. THICKNESS MEASURES 0.079, REF CRJ 200 NDTM PART 4 REV 41 51-00-001 UT GAUGE S/N DBT-CT-1033 CAL DUE 02/19/21. PERFORMED HFEC INSPECTION ON BLENDED AREA OF PRESSURE FLOOR SILL ANGLE AT FS 452 AND LBL 47, PER REO 601R-53-41-666 DATED 2012-11-06 REV-C AND CRJ 200 NDTM PART 1 REV 41 51-20-06, NO INDICATIONS NOTED. EDDY CURRENT TESTER S/N 200051301 CAL DUE 01/24/21. EVALUATED REWORKED AREA OF PRESSURE FLOOR SILL ANGLE AT FS 452 AND LBL 47, ORIGINAL THICKNESS IS 0.080'', REMAINING THICKNESS IS 0.079'', FOUND TO BE WITHIN LIMITS PER REO 601R-53-41-666 DATED 2012-11-06 REV-C.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 37,890 hrs · 36,698 cycles

CLIP (INTERCOSTAL) CRACKED ON AFT SIDE OF PRESSURE BULKHEAD BETWEEN RBL 36.20 & S15R. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CLIP (INTERCOSTAL) ON AFT SIDE OF PRESSURE BULKHEAD AT FS 625.30 BETWEEN RBL 36.20 AND S15R, IAW CRJ 200 SRM 51-42-21 REV 38.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 37,890 hrs · 36,698 cycles

ACCOMPLISHED SDI OF AFT PRESSURE BULKHEAD FWD FACE 2 EA INDICATIONS FOUND. AIRCRAFT REMOVED FROM SERVICE. PERFORMED HFEC INSPECTION ON THE FWD SURFACE OF THE AFT PRESSURE BULKHEAD WEB AT FS 621.00 BETWEEN LBL 36.20 AND RBL 36.20 FROM WL 73.00 TO WL 150.00, IAW NDTM AWAL SUPPLEMENT 09-008 AND NDTM PART 1 REV 41 51-20-06 EDDY CURRENT TESTER OLYMPUS NORTEC 600 S/N 200051301. 2 EA INDICATIONS FOUND ON WEB. INDICATION NR 1 AT FS 621 & RBL 27.50 BETWEEN WL 109.75 AND WL 110.5 THAT MEASURES .75"L. INDICATION NR 2 AT FS 621 & RBL 18.00 AND BETWEEN WL 109.5 AND WL 110.5 THAT MEASURES 1.0"L PERFORMED CUTOUT ON CRACK LOCATION NR 1 L=2.950" X W=1.143". CUTOUT ON CRACK LOCATION NR 2 IS L=3.086" X W=1.256" WITH HFEC ACCOMPLISHED AND NO DEFECTS NOTED. FABRICATED LOCATION NR 1 DOUBLER FROM 2024 T-3 .040" L=11" X W=5.5", TRIPPLER FABRICATED FROM 2024 T-3 .063" L=9" X W=3.5", AND LOCATION NR 2 DOUBLER FABRICATED FROM 2024 T-3 .040" L=11 X 5.576" TRIPPLER FROM 2024 T-3 .063" L=9" X 3.5". LOCATION NR 1 INSTALLED AT FS 621 & RBL 27.50 BETWEEN WL 109.75 AND WL 110.5. LOCATION NR 2 INSTALLED AT FS 621 & RBL 18.00 BETWEEN WL 109.5 AND WL 110.5, REF BOMBARDIER REO 601R-53-61-1285 REV E DTD 2016-10-31.

Part: GEARBOX — CRACKED (APU) · airframe 37,591 hrs · 36,393 cycles

AFTER SELECTING PACKS ON FOLLOWING UNPRESSURIZED TAKEOFF SMOKE IN COCKPIT AND REPORTS OF CHEMICAL BURNING SMELL IN THE CABIN. SMOKE DISSIPATED QUICKLY FROM COCKPIT. SUPP 09-037 REQUIRED. AIRCRAFT REMOVED FROM SERVICE APU ON MEL FOUND OIL IN APU ENCLOSURE REMOVED AND REPLACED L/R COALACERS SOCKS . IAW AWA SUP 14-192A OPS CHECK GOOD AT THIS TIME. INSP FOUND APU GEAR BOX CRACKED AND ENCLOSURE FILLED WITH OIL REMOVED APU ASSY REF TC SUPP 13-005 CLEANED SPILLED OIL REF W/C #5 FOR APU INSTALL REPLACED APU

Part: A/C PACK — INOPERATIVE (CABIN) · airframe 36,519 hrs · 35,370 cycles

UNABLE TO COOL CABIN WITH RIGHT PACK ON MEL, CABIN TEMP ONLY WENT FROM 31C TO 28C ON 1HR 20 MINUTE FLIGHT. FLIGHT IS DIVERTING TO DAY WHERE WE HAVE A SPARE AIRCRAFT TO CONTINUE TO ORD WITH.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,942 hrs · 33,874 cycles

FUSELAGE SKIN AND DOUBLER IN THE FWD LOWER CORNER OF PAX DOOR CUTOUT DAMAGED. REPAIRED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,942 hrs · 33,874 cycles

FRAME 589 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGER 20L AND 26L IN THE CARGO BAY. REPAIRED FRAME 589 FROM STRINGER 20L TO 26L.

Part: SKIN — GOUGED (TE FLAP) · airframe 34,942 hrs · 33,874 cycles

RIGHT I/B FLAP, LOWER SKIN HAS GOUGE AND DENT. REPAIRED RIGHT I/B FLAP LOWER SKIN IAW REO 601R-57-52-1544 REV-.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,942 hrs · 33,874 cycles

FRAME 605.00 CRACKED AT LBL9. REPAIRED FRAME 605.00 AT LBL9 IAW REO 601R-53-61-5214 REV-A.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,942 hrs · 33,874 cycles

FRAME 605.00 CORRODED BETWEEN STR20L AND 20R. REPLACED FRAME IAW CRJ200 SRM 51-42-06, 51-42-21, 53-61-15.

Part: BRACKET — CORRODED (PAX DOOR) · corrosion level 2 · airframe 34,942 hrs · 33,874 cycles

PAX DOOR AFT HANDRAIL CUP CORRODED FROM FS 340.00 AND LBL38. REPLACED CUP BRACKET IAW SRM 51-42-06, 51-42-13, TR51-42, 51-21-06, 53-21-23.

Part: RETAINER — CRACKED (LT PYLON) · airframe 34,942 hrs · 33,874 cycles

LEFT PYLON PANEL 412DB HAS CRACKED SEAL RETAINER. REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: CLEAT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 34,942 hrs · 33,874 cycles

PAX DOOR LOWER AFT HANDRAIL CLEAT CORRODED. REPLACED CLEAT IAW SRM 51-42-06, TR51-42, 51-42-13, 51-21-06, 53-21-23.

Part: SKIN — CRACKED (TE FLAP) · airframe 34,942 hrs · 33,874 cycles

RIGHT I/B FLAP LOWER SKIN HAS POSSIBLE CRACK ON CENTER TRAILING EDGE. REPAIRED SKIN IAW SRM 57-52-00.

Part: BEAM — DAMAGED (CARGO DOOR) · airframe 34,942 hrs · 33,874 cycles

CARGO DOOR BEAM MEMBER PN: 601R35050-64 CUT BY CARGO DOOR CABLES. REPLACED BEAM IAW SRM 51-42-21, 51-42-06.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 34,942 hrs · 33,874 cycles

CARGO DOOR FWD SIDE SURROUND STRUCTURE HAS BENT/ TORN CLIP. REPLACED CLIP IAW SRM 51-42-21.

Part: RETAINER — CRACKED (RT PYLON) · airframe 34,942 hrs · 33,874 cycles

RIGHT PYLON PNL 422BT HAS CRACKED SEAL RETAINER. REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: RETAINER — CRACKED (RT PYLON) · airframe 34,942 hrs · 33,874 cycles

RIGHT PYLON PNL 422DB HAS CRACKED SEAL RETAINER. REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 34,703 hrs · 33,645 cycles

ON APPROACH FLAPS FAILED AT O DEGREES. PERFORMED FLAPS RESET PROCEDURE IAW SUP 98-18G BOX 12. PLACARDED AND PLACED ON MEL. CHANGED BPSU.

Part: SKIN — GOUGED (BS 265) · airframe 34,565 hrs · 33,522 cycles

DURING AN INSPECTION, A GOUGE WAS FOUND IN THE FUSELAGE SKIN MEASURING 0.006 INCHES DEEP LOCATED AT BS 265, 0.1875 INCHES BELOW STRINGER 22L. THE GOUGE WAS REPAIRED IAW EA CRJ253-00968, REV IR.

Part: OIL COOLER — MALFUNCTIONED (APU) · airframe 34,341 hrs · 33,302 cycles

APU OIL TEMP CAUTION ILLUMINATED INFLIGHT WITH THE NR 2 IDG ON MEL REPLACED OIL COOLER FOR BEING CLOGGED AND REPLACED APU.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 33,995 hrs · 32,916 cycles

WHILE PERFORMING SPECIAL DETAILED INSPECTION OF THE AFT PRESSURE BULKHEAD FORWARD FACE A CRACK WAS FOUND AT FS621.0, LBL 27.5, WL 132.0 THAT WAS 1.5 INCHES LONG.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 33,152 hrs · 32,069 cycles

EMERGENCY LIGHTS BLINKING IN BACK OF CABIN SECURED LIGHT CONNECTOR IAW AMM 33-51-00. OP CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 31,580 hrs · 30,581 cycles

FLOOR LEVEL EMERGENCY LIGHTING AFT OF ROW 8 INITIALLY DID NOT TURN ON, WHEN DID TURN ON LIGHTS WERE VERY DIM. CONNECTED AND SECURED ROW 8 FLOOR TRACK LIGHTING CONNECTORS IAW SUP 13-022. OPS TEST GOOD.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 31,421 hrs · 30,432 cycles

ON CLIMBOUT, EXPERIENCED SEVERAL OCCURRENCES OF UNCOMMANDED YAW. ACFT WOULD YAW TO ALMOST FULL BRICK OF DEFECTION, THEN JOLT BACK TO CENTER, FOLLOWED BY SMALL JOLT LT AND RT WITH INDICATION FCC-AMP-Y, RT: 6547, REPAIR RT: 008000, INTERROGATED FCC AND FOUND REPAIR CODE 008000 AND AMP Y ERROR CODE 6547 ON RT SIDE, REF 285707, BLOCK 2 FOR NEW WRITE UP.

Part: PANEL — CRACKED (PAX DOOR) · airframe 31,432 hrs · 30,289 cycles

PASSENGER DOOR FOWARD RISER PANEL CRACKED AT LOWER CORNER, FOUND DURING REPAIR OF AFT RISER PANEL.

Part: POST — CRACKED (FUSELAGE) · airframe 31,324 hrs · 30,342 cycles

VERTICAL POST RBL 18 AT FS 409+128 IS CRACKED AT BOTTOM OTBD FLANGE.

Part: RIB — CRACKED (LT ELEVATOR) · airframe 31,324 hrs · 30,342 cycles

LEFT ELEVATOR RIBLET AT ES 62.02 CRACKED.

Part: SKIN — DAMAGED (TE FLAP) · airframe 31,324 hrs · 30,342 cycles

RIGHT INBD FLAP LOWER SKIN HAS 2 EA LARGE AREAS HEAVILY PITTED, DEBRIS DAMAGE ON INBD SIDE.

Part: SKIN — CHAFED (FUSELAGE) · airframe 31,342 hrs · 30,342 cycles

RIGHT MLG APRON STRUCTURE SKIN OUTER SURFACE GOUGED JUST FWD OF FS 554.

Part: POST — CRACKED (FUSELAGE) · airframe 31,324 hrs · 30,342 cycles

VERTICAL POST LBL18, OTBD OF FS 409+128 IS CRACKED AT BOTTOM END. REPAIRED VERTICAL POST AT FS 409+128 AND LBL18 IAW REO 601R-53-41-056, REV-F DATED 2011/09/02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,342 hrs · 30,342 cycles

FS 484, CLIP AT RBL 36 IS CRACKED. R & R CLIP, REPAIRED INTERCOSTAL AT FS 484.00 AND RBL36 IAW EA AWAC-CRJ253-00482, REV-A DATED 8/17/2016.

Part: SKIN — DAMAGED (TE FLAP) · airframe 31,324 hrs · 30,342 cycles

LEFT INBD FLAP LOWER SKIN HAS 2 LARGE AREAS WITH CHIPPED PAINT AND PITTING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 31,324 hrs · 30,342 cycles

BS 280 FLOORBEAM AFT UPPER ANGLE CRACKED AT OTBD RBL 9. REPAIRED THE FLOORBEAM ANGLE IAW REO601R-53-11-137 REV-A.

Part: ATTACH BRACKET — CRACKED (CARGO DOOR) · airframe 31,324 hrs · 30,342 cycles

ATTACH BRACKET AT LOWER END OF FWD CARGO DOOR TRACK IS CRACKED

Part: ATTACH BRACKET — CRACKED (CARGO DOOR) · airframe 31,324 hrs · 30,342 cycles

ATTACH BRACKET AT LOWER END OF FWD CARGO DOOR TRACK IS CRACKED.

Part: FRAME — CRACKED (BS 333) · airframe 31,324 hrs · 30,342 cycles

FRAME BS 333 CRACKED JUST INBD OF STRINGER 2L IN CABIN.

Part: ATTACH BRACKET — CRACKED (BS 449) · airframe 31,324 hrs · 30,342 cycles

LEFT OVERWING PANEL 161DL ATTACH BRACKET AT BS 449.85 IS CRACKED

Part: ATTACH BRACKET — CRACKED (BS 473) · airframe 31,324 hrs · 30,342 cycles

RIGHT OVERWING PANEL 162EL ATTACH BRACKET AT BS 473.15 IS CRACKED.

Part: ATTACH BRACKET — CRACKED (BS 461) · airframe 31,324 hrs · 30,342 cycles

RIGHT OVERWING PANEL 162DL ATTACH BRACKET AT BS 461 IS CRACKED.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 31,324 hrs · 30,342 cycles

STRINGER 15L INTERCOSTAL BS 625 CRACKED.

Part: ATTACH BRACKET — CRACKED (BS 461) · airframe 31,324 hrs · 30,342 cycles

LEFT OVERWING PANEL 161DL ATTACH BRACKET CRACKED AT BS 461.

Part: INTERCOSTAL — DAMAGED (BS 621) · airframe 31,324 hrs · 30,342 cycles

STRINGER 16L INTERCOSTAL DAMAGED

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 31,324 hrs · 30,342 cycles

STRINGER 16L INTERCOSTAL ANGLE BS 625 IS CRACKED

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 31,324 hrs · 30,342 cycles

RIGHT WING FLAP VANE L/E IS CHAFED AT APROX WS 105.

Part: SUPPORT — CRACKED (LT WING) · airframe 31,324 hrs · 30,342 cycles

ANTI-ICE DUCT SUPPORT IS CRACKED AT UPPER AND LOWER OUTBOARD SEIDES, LEADING EDGE LEFT WING SPAR STATION 149.58

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 31,324 hrs · 30,342 cycles

STRINGER 13L INTERCOSTAL FS 625 IS CRACKED

Part: FLOORBEAM — CORRODED (BS 621) · airframe 31,324 hrs · 30,342 cycles

MAIN CABIN FLOORBEAM ANGLE AT FS 621 LBL 42 TO RBL 42 FASTENER HOLES CORRODED. REPLACED THE FLOORBEAM ANGLE.

Part: ANGLE — CRACKED (BS 202) · airframe 31,324 hrs · 30,342 cycles

CENTER WIELDSHIELD POST AT BS 202 RIGHT LOWER ANGLE IS CRACKED

Part: FRAME — CRACKED (THRUST REVERSER) · airframe 31,324 hrs · 30,342 cycles

LEFT THURST REVERSER TORQUE BOX CRACKED AT 5 0-CLOCK AFT SIDE.

Part: ANGLE — CRACKED (BS 202) · airframe 31,324 hrs · 30,342 cycles

CENTER WINDSHIELD POST AT BS 202 LOWER LEFT ANGLE IS CRACKED

Part: ANGLE — CRACKED (BS 280) · airframe 31,324 hrs · 30,342 cycles

BOTH ANGLE BS 280 STRINGER 3L ARE CRACKED. REPLACED.

Part: ANGLE — CRACKED (BS 484) · airframe 31,324 hrs · 30,342 cycles

BS 484 ANGLE AT LBL 27 IS CRACKED. REPLACED ANGLE IAW REO 601R-53-41-059 REV-B.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 31,324 hrs · 30,342 cycles

RIGHT OBLIQUE INTERCOSTAL IS CRACKED. REPLACED THE INTERCOSTAL IAW REO601R-53-61-422.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 31,324 hrs · 30,342 cycles

RIGHT WING INBD FLAP VANE L/E IS CHAFED AT APROX WS 56. REPLACED THE FLAP VANE IAW SRM 51-42-13, 51-25-16.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,324 hrs · 30,342 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 31,324 hrs · 30,342 cycles

LEFT WING ANTI-ICE DUCT AT WS 149.58 OUTBD SUPPORT BRACKET CRACKED. REPLACED

Part: FRAME — CRACKED (BS 235) · airframe 31,324 hrs · 30,342 cycles

FLIGHT DECK LEFT FRAME WEB AT BS 235 BELOW WINDSHIELD SIDE POST IS CRACKED. REPLACED THE WEB IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,324 hrs · 30,342 cycles

BS 280 FLOORBEAM FWD ANGLE IS CRACKED AT LBL 9

Part: CARGO TRACK — CORRODED · corrosion level 2 · airframe 31,324 hrs · 30,342 cycles

THREE CARGO TRACKS AT LBL 27 CORRODED. REPLACED THE CARGO TRACK IAW AMM 53-00-49.

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 31,324 hrs · 30,342 cycles

FLIGHT DECK LEFT WINDSHIELD SIDE POST LOWER FITTING CRACKED. REPLACED THE FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (WINDSHIELD FRAME) · airframe 31,324 hrs · 30,342 cycles

FLIGHT DECK RT WINDSHIELD SIDE POST LOWER FITTING IS CRACKED. REPLACED POST LOWER FITTING IAW SRM 51-42-21, AND 51-40-11.

Part: CARGO TRACK — CORRODED (BS 585-605) · corrosion level 2 · airframe 31,324 hrs · 30,342 cycles

CARGO TRACK AT LBL9 AND BS 605 - 585 CORRODED. REPLACED THE CARGO TRACK IAW AMM 53-00-49.

Part: A/C PACK — OVERTEMP · airframe 31,099 hrs · 30,130 cycles

PACK TEMP 117 DEGREES AND CLIMBING, SMOKE IN COCKPIT AT GATE AFTER SWITCHING FROM GROUND AIR TO APU AIR.

Part: UNKNOWN — SMOKE (CABIN) · airframe 30,853 hrs · 29,904 cycles

ON TAXI OUT RECEIVED A RT PACK HI TEMP MSG. MOMENTS LATER FLIGHT ATTENDANT ADVISED SMOKE IN CABIN. ON APU AIR PACK TEMP CONTROLS IN AUTO. RETURNED TO GATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,612 hrs · 29,679 cycles

ROW 9 & AFT EMER FLOOR TRACK LIGHTS INOPERATIVE.

Part: APU — SHUTDOWN (APU BAY) · airframe 29,436 hrs · 28,573 cycles

APU AUTO SHUTDOWN ON GROUND (AT GATE) SMOKE COMING FROM EXHAUST

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT COWLING) · airframe 27,203 hrs · 26,429 cycles

3727 LEFT COWL ANTI-ICE CAUTION INFLIGHT WITH SWITCH OFF. LEFT COWL SHOWED YELLOW. 14TH STAGE SOV WAS OPEN WHILE CAUTION MSG WAS PRESENT. COMPLIED WITH QRH & RETURNED, EMER DECLARED. R & R LT ENG COWL ANTI-ICE VLV IAW SUPP 10-094. OPERATIONS CHECKED GOOD AT THIS TIME. SN OFF 0123B & SN ON 1968B.

Part: SKIN — DENTED (FUSELAGE) · airframe 26,505 hrs · 25,764 cycles

CARD 4DMI16840 REPAIR FS 589 - 605.

Part: HOUSING — CRACKED (E&E DOOR) · airframe 26,505 hrs · 25,764 cycles

AVIONICS DOOR HANDLE HOUSING CRACKED.

Part: SEAL — CRACKED (RT SPOILER) · airframe 26,505 hrs · 25,764 cycles

RIGHT FLIGHT SPOILER INBD SPRING SEAL IS CRACKED .

Part: CHANNEL — CRACKED (LT WING) · airframe 26,505 hrs · 25,764 cycles

INBD CHANNEL UNDER LT OTBD GND SPOILER IS CRACKED.

Part: HOUSING — CRACKED (FUSELAGE) · airframe 26,505 hrs · 25,764 cycles

EXTERNAL POWER RECEPTACLE HOUSING CRACKED.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 26,505 hrs · 25,764 cycles

LEFT INBD FLAP VANE SKIN LE IS CHAFED IN 3 LOCATIONS FROM STOPS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,505 hrs · 25,764 cycles

INBD & OTBD FLOORBEAM CLIPS ARE CRACKED AT RBL 9 & FS 280.

Part: DRAG BRACE — CRACKED (RT MLG) · airframe 26,505 hrs · 25,764 cycles

RIGHT MLG DRAG BRACE COMMON TO BATTERY RIB CRACKED.

Part: DRAG BRACE — CRACKED (LT MLG) · airframe 26,505 hrs · 25,764 cycles

LEFT MLG DRAG BRACE COMMON TO BATTERY RIB CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,505 hrs · 25,764 cycles

INBD & OTBD FLOORBEAM CLIPS ARE CRACKED AT LBL 9FS 280.

Part: MOUNT BRACKET — CRACKED (RT WING) · airframe 26,505 hrs · 25,764 cycles

REFUEL DEFUEL DOOR NOZZLE MOUNTING BRACKET ON RT FRONT WING SPAR IS CRACKED AT LOWER OTBD CORNER AT RBL 50.0.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,505 hrs · 25,764 cycles

LBL 27 FLOOR CAP CORRODED AROUND NUT PLATES AT FS 574 - 621.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 26,505 hrs · 25,764 cycles

CARGO DOOR SUPPORT BEAM AFT LOWER CLIP CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,505 hrs · 25,764 cycles

LBL 9 FLOOR SEAT TRACK CORRODED IN CARGO BAY FS 559.00+80.

Part: MOUNT BRACKET — CRACKED (RT WING) · airframe 26,505 hrs · 25,764 cycles

RIGHT LE INBD TRANSITION DUCT OTBD MOUNT BRACKET CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,505 hrs · 25,764 cycles

NUMBER 1 FLOOR SEAT RAIL AT RBL 9 IS CORRODED AT FS 364 TO 374.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,505 hrs · 25,764 cycles

RIGHT NR 4 FLOOR SEAT TRACK CORRODED AT FS 559.0 TO 559.00+80.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,505 hrs · 25,764 cycles

FLOOR SEAT RAIL AT LBL 9 IS CORRODED AT FWD END FROM FS 364 TO FS 379.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,505 hrs · 25,764 cycles

PAX DOOR LOWER SILL IS CORRODED AT INBD & OTBD SIDES BETWEEN FS 310 & 349.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,505 hrs · 25,764 cycles

PAX DOOR FWD & AFT CLEATS AT LOWER SILL ARE CORRODED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,831 hrs · 25,145 cycles

ROW 13AC CEILING LIGHT INOPERATIVE. CAN SMELL ELEC BURNING ON GND AT GATE.

Part: FLAP — FAILED (WING) · airframe 22,636 hrs · 22,066 cycles

ON DEPARTURE, DURING FLAP RETRACTION, FLAPS FAILED AT 11 DEGREES. COMPLIED WITH QRH. LANDED AT DCA. BTMS 7, 4, 3, 3. C/B RESET DID NOT WORK. ATTEMPTED FLAP RESET PER AWAC SUP 98-018E. FLAP FAIL MESSAGE DID NOT EXTINGUISH. REF 235830/4 AND 235831/1 AND /2 FOR FURTHER ACTION.

Part: SENSOR — MALFUNCTIONED (TE FLAP) · airframe 22,564 hrs · 22,001 cycles

JUST AFTER TAKEOFF WHILE MOVING FLAP LEVER 20 DEG TO 8 DEG RECEIVED FLAP FAIL CAUTION MSG. COMPLIED WITH QRH. COMPLIED WITH RESET PER AWAC SUP 98-018E. RESET FAILED. REMOVED AND REPLACED SENSORS L3 AND L4 REF AMM 27-51-15. OPS CHECK GOOD. RE-ACTIVATED SDU REF SUPP 06-076A. REMOVED PLACARD, REMOVED FROM MEL.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 22,383 hrs · 21,822 cycles

FLAPS FAIL AT 41 DEGREES, MISSED APPROACH. COMPLIED WITH QRH, LANDED UNEVENTFUL AT LGA, EMERGENCY DECLARED. PERFORMED FLAP RESET PROCEDURES IAW AWAC SUPP 98-18E BOX 12 FLAPS RESET. REMOVED AND REPLACED FECU. PERFORMED FUNCTIONAL AND OPS CHECK, ALL CHECKED GOOD. REMOVED PLACARD AND REMOVED FROM MEL.

Part: TUBE — DENTED (FLAP ACTUATOR) · airframe 21,527 hrs · 20,971 cycles

RT FLAP CENTER & INBD VANE ACTUATOR TUBES HAVE INDENTATIONS FROM THE ROLLERS. REPAIRED IAW REO 601R-57-52-1544, REV A.

Part: SKIN — GOUGED (LT NACELLE) · airframe 21,527 hrs · 20,971 cycles

LT LOWER CORE COWL INNER SKIN GOUGED 3 SPOTS, 10 GOUGED LOCATIONS ON LT LOWER CORE COWL INNER SKIN 4 FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS AND TO 6 AREAS. REPAIRED IAW REO 601R-71-12-4122.

Part: SKIN — DENTED (LT NACELLE)

LT LOWER CORE COWL INNER SKIN DENTED IN MULTIPLE SPOTS. 10 DENTS LOCATIONS ON LT LOWER CORE COWL. INNER SKIN WITH FOUR REQUIRED AND 6 FOUND TO BE WITHIN ALLOWABLE DAMAGE REO.

Part: SKIN — GOUGED (FS 559) · airframe 21,527 hrs · 20,971 cycles

GOUGED ON FUSELAGE AT FS 559 FROM CONTACT WITH RT STUB FAIRING COMPLIED WITH REO 601R-53-41-610.

Part: FITTING — CRACKED (FS 461) · airframe 21,527 hrs · 20,971 cycles

FITTING CRACKED OUT APPROX FS 461, RBL 9. REMOVED CRACKED FITTING AT FS 461, RBL 9. INSTALLED NEW SERVICEABLE FITTING PN 600-31068-19.

Part: SKIN — GOUGED (NACELLE) · airframe 21,527 hrs · 20,971 cycles

PANEL 445AB HAS NUMEROUS SMALL DENTS AND GOUGES ON INNER SKIN. REPAIR IAW REO 601R-71-12-4124.

Part: BEAM — DAMAGED (WS 60-137) · airframe 21,527 hrs · 20,971 cycles

LT INBD FLAP VANE ACTUATORS SLIDING BEAMS HAVE DAMAGE ON UPPER AND LOWER SURFACES FROM ROLLERS. REPAIRED BY BLENDING IAW REO 601R-57-52-1942.

Part: FLOOR SUPPORT — CORRODED (FS 621) · airframe 21,527 hrs · 20,971 cycles

CORROSION ON FLOOR SUPPORT STRUCTURE FS 621 & LBL 31 AT NUTPLATE HOLE BLENDED CORROSION ON FLOOR STRUCTURE. FOUND TO BE WITHIN LIMITS IAW REO 601R-53-61-4600.

Part: FLOOR SUPPORT — CORRODED (FS 621.0) · corrosion level 1 · airframe 21,527 hrs · 20,971 cycles

CORROSION AT FLOOR SUPPORT STRUCTURE FS 621 & LBL14 NUTPLATE HOLE. REMOVED CORROSION, MEASURED & FOUND IT TO BE WITHIN ALLOWABLE LIMITS, DEPTH .012" WITH .05" LENGTH 0.7" IAW REO 601R-53-61-4600.

Part: MOUNT BRACKET — CRACKED (FS 169-193) · airframe 21,527 hrs · 20,971 cycles

SYS 3 BROKEN ACCUMULATOR FWD MOUNTING BRACKET CRACKED. REMOVED UNSERVICEABLE BRACKET AND REPLACED WITH SERVICEABLE BRACKET, PN 601R75250-25, IAW AWC SRM 51-42-06, 51-40-11 AND 51-42-21.

Part: BULKHEAD — DAMAGED (FS 559) · airframe 21,527 hrs · 20,971 cycles

DOUBLE DRILLED HOLE ON FS 559 BULKHEAD AT RBL 18. DURING INCORPORATION OF GREO 601R-53-41-1116, REV B. CW REO 601R-53-41-1594 BY CUTTING OUT DAMAGED REINFORCING ANGLE STEPPING UP HOLES, AND INSTALLING FREEZE PLUGS AND A FILLER.

Part: ANGLE — CRACKED (BS 484) · airframe 21,527 hrs · 20,971 cycles

ANGLE CRACKED AT APPROX FS 484, RBL 27. REMOVED CRACKED ANGLE AT FS 484, RBL 27, DUPLICATED ANGLE AND INSTALLED ANGLE IAW REO 601R-53-41-059, REV B.

Part: DOOR — CHAFED (LT MLG) · airframe 21,527 hrs · 20,971 cycles

LT MLG DOOR L/E CHAFED. LT MLG DOOR L/E PREVIOUS. R & R IAW REO 601R-52-82-016.

Part: SKIN — CHAFED (FS 449-529) · airframe 21,527 hrs · 20,971 cycles

INNER SKIN CHAFED ON BUTTE DOOR 694PB. R & R SKIN IAW SRM 51-42-06, 51-40-11, 51-25-16.

Part: FLOOR SUPPORT — CORRODED (FS 574-605) · airframe 21,527 hrs · 20,971 cycles

CARGO FLOOR SUPPORT LBL 27 HAS CORRODED NUTPLATE HOLES BETWEEN FS 574 AND FS 605. REMOVED UNSERVICEABLE, LBL 27 FLOOR SUPPORT AND INSTALLED SERVICEABLE FLOOR SUPPORT IAW 51-40-11, 51-42-06, 51-24-36. REMOVED UNSERVICEABLE WEB AND INSTALLED SERVICEABLE WEB IAW SRM 51-42-06.

Part: MOUNT BRACKET — CRACKED (FS 338) · airframe 21,527 hrs · 20,971 cycles

PAX DOOR POWER ASSIST MOTOR MOUNT BRACKET CRACKED. R & R PAX DOOR POWER ASSIST MOTOR MOUNT BRACKET IAW SRM 51-42-06 & 51-42-13.

Part: DOOR — CHAFED (LT MLG) · airframe 21,527 hrs · 20,971 cycles

LT MLG DOOR IS CHAFED ON THE INSIDE T/E. REPAIRED LT MLG DOOR CHAFE ON THE INSIDE T/E IAW REO 601R-52-82-351, REV A.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,918 hrs · 19,317 cycles

DETECTED A STRONG ELECTRICAL ODOR AFTER LANDING AND DURING TAXI, ODOR CONTINUED TO GATE WITH ENGINE SHUTDOWN, PERFORMED INSPECTION OF ACFT LOWER AVIONICS BAY, PAX COMPARTMENT BALLASTS, GALLEY HEATERS, & COFFEEMAKER. NO FAULTS INDICATED. NO ODOR NOTED AT THIS TIME.

Part: LANDING GEAR — UNKNOWN · airframe 19,074 hrs · 18,392 cycles

GEAR DISAGREE WARNING MESSAGE AFTER T/O. WHEN GEAR SELECTING UP. C/W QRH NOSE GEAR DASHED AMBER MSG CLEARED 20 SECONDS AFTER GEAR UP SELECTED DOWN AGAIN GOT GEAR DISAGREE WITH NLG SHOWING DASHED. INSPECTED ALL 3 GEAR BAY/LEGS NO DISCREPANCIES NOTED.

Part: SILL — GOUGED (FUSELAGE) · airframe 17,079 hrs · 16,225 cycles

SERVICE DOOR SILL HAS GOUGE BEYOND REPAIRABLE LIMITS NEEDS TO BE REPLACED. SERVICE DOOR SILL R & R IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 17,079 hrs · 16,225 cycles

AFT RT SIDE OF SEAT TRACK IN CARGO BAY CORRODED AROUND SCREW HOLES. R & R SEAT TRACK AT RBL 9.

Part: ANGLE — CRACKED (BS 626) · airframe 17,079 hrs · 16,225 cycles

RT OBLIQUE ANGLE IN THE AFT SIDE OF AFT PRESSURE BULKHEAD IS CRACKED. R & R UNSERVICEABLE RT OBLIQUE ANGLE AND REPLACED WITH NEW ANGLE IAW SRM.

Part: HANDLE — GOUGED (CARGO DOOR) · airframe 17,079 hrs · 16,225 cycles

CARGO DOOR OUTER HANDLE CUT OUT IS GOUGED IN 3 PLACES. REPAIRED CARGO DOOR OUTER HANDLE CUT OUT IAW REO 601R-52-31-133 REV, ORIGINAL DATED 8/29/10.

Part: SEAT TRACK — CORRODED (BS 559-621) · corrosion level 2 · airframe 17,079 hrs · 16,225 cycles

CARGO SEAT TRACK SIDE IS CORRODED. R & R SEAT TRACK.

Part: SILL — CORRODED (BS 562.72) · airframe 17,079 hrs · 16,225 cycles

CARGO BAY DOOR CUT OUT FLOOR SILL HAS CORROSION. R & R CARGO BAY DOOR CUT OUT FLOOR SILL IAW REO 601R-53-61-1574.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,079 hrs · 16,225 cycles

LT OBLIQUE ANGLE CRACKED. R & R.

Part: SPAR — CHAFED (BS 625.3) · airframe 17,079 hrs · 16,225 cycles

RT PYLON FWD ENGINE MOUNT SUPPORT SPAR HAS CHAFE DAMAGE FROM 14TH STAGE DUCT BLEND IAW REO 601R-54-51-091.

Part: ATTACH ANGLE — CRACKED (BS 574) · airframe 17,079 hrs · 16,225 cycles

FWD CARGO DOOR LOWER TRACK CHANNEL CRACKED. R & R CARGO DOOR FWD TRACK LOWER ATTACH ANGLE IAW SRM 51-40-11, 51-42-21, 51-42-06, AND 51-25-21.

Part: RIB — CRACKED (LT WING) · airframe 17,079 hrs · 16,225 cycles

BATT RIB CRACKED IN LT MLG WHEEL WELL. REPAIRED LT BATT RIB IAW REO 601R-57-51-046 REV B REPAIR NR 2.

Part: DOOR — CHAFED (MLG) · airframe 17,079 hrs · 16,225 cycles

RT MLG DOOR L/E IS CHAFED IN 2 PLACES. REPAIRED DOOR (RT MLG) IAW REO 601R-52-82-102 AND REO 601R-52-82-033, REV A.

Part: RIB — CRACKED (RT WING) · airframe 17,079 hrs · 16,225 cycles

BATT RIB IN RT W/W IS CRACKED. REAPIRED RT BATT RIB IAW REO 601R-57-51-046 REV B, REPAIR NR 2.

Part: BULKHEAD — CHAFED (BS 280) · airframe 17,079 hrs · 16,225 cycles

AFT SIDE OF THE 280 BULKHEAD IS CHAFED NEXT TO MISC JACK. REPAIRED FS 280 BULKHEAD WEB BETWEEN RBL 11.00 & RBL 18.00, BETWEEN STR 134 & STR 14A IAW REO 601R-53-11-1727, REV C.

Part: STRUCTURE — CHAFED (MLG DOOR) · airframe 17,079 hrs · 16,225 cycles

LIGHT CHAFING ON MLG L/E DOOR. REPAIRED IAW REO 601R-52-82-016 & REO 601R-52-82-102.

Part: WIRE — LOOSE (APU) · airframe 13,360 hrs · 124,478 cycles

APU AUTO SHUTDOWN AND TOWER REPORTS SMOKE FROM AIRCRAFT. REMOVED AND REPLACED APU FUEL SOLENOID CONNECTOR PLUG AND BACKSHELL (P5) IAW ESPM 20-17-10. APU OPS CHECK GOOD, REMOVED FROM MEL. (K)

Part: DOOR SEAL — DAMAGED (EMERGENCY EXIT) · airframe 13,453 hrs · 12,561 cycles

RT OVER-WING EMERGENCY EXIT SEAL DAMAGED AT BOTTOM CORNER. SEAL REPAIRED IAW REO 601R-52-21-019. (K)

Part: ATTACH BRACKET — CRACKED (RT MLG WW) · airframe 13,347 hrs · 12,646 cycles

HYD LINES BRACKET CRACKED IN RT W/W, RBL 18 TO RBL 27, FS 523.6. CRACKED HYD LINE BRACKET FABRICATED AND REPLACED IAW REO 601R-53-42-007, REV A. (K)

Part: ATTACH BRACKET — CRACKED (RT MLG WW) · airframe 13,347 hrs · 12,646 cycles

HYD LINES BRACKET IN RT W/W RBL 18 TO RBL 27, FS 527.73, 2 CRACKS. HYD LINES BRACKET MFG AND REPLACED IAW REO 601R-53-42-007, REV A. (K)

Part: PRESSURE BLKHD — CRACKED (BS 202) · airframe 13,347 hrs · 12,464 cycles

CRACK FOUND ON PRESSURE BULKHEAD FS 202.75 AT BL 36.71 AROUND PARKING BRAKE CABLE. CRACK ON PRESSURE BULKHEAD FS 202.75 AT LBL 36.71 REPAIRED IAW REO 601R-53-11-563. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 13,347 hrs · 12,646 cycles

CRACK FOUND ON PILOT BULKHEAD FS 280, RBL 9. REPAIR TO PILOT BULKHEAD CARRIED OUT IAW REO 601R-53-11-171, REV D. (K)

Part: ANGLE — CRACKED (BS 280) · airframe 13,347 hrs · 12,646 cycles

CRACK FOUND ON PILOT BULKHEAD AFT ANGLE FS 280, LBL 9 REPAIR TO BULKHEAD AFT ANGLE FS 280, LBL 9 CARRIED OUT IAW REO 601R-53-11-138. (K)

Part: BRACKET — CRACKED (BS 280)

CRACK FOUND ON BRACKET FS 280, RBL 9 INBD NEW BRACKET INSTALL AT FS 280, RBL 9 INBD IAW SRM 51-42-21. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,347 hrs · 12,646 cycles

CRACK FOUND ON BRACKET FS 280, LBL 9 INBD AND OTBD NEW BRACKET INSTALL AT FS 280, RBL 9 INBD AND OTBD IAW SRM 51-42-21. (K)

Part: SILL — CRACKED (BS 575) · airframe 13,347 hrs · 12,646 cycles

CARGO DOOR FLOOR SILL UPPER SURFACE CRACKED UNDER ANGLE AT FS 575.00. CARGO DOOR FLOOR SILL UPPER SURFACE REPAIRED DOOR. UNDER ANGLE AT FS 575 IAW REO 601R-53-61-1741. (K)

Part: PANEL — CRACKED (PAX DOOR) · airframe 13,347 hrs · 12,646 cycles

PAX DOOR FWD SIDE PANEL FOUND CRACK (ZONE 2) (CRACK LENGTH .250) PAX DOOR FWD SIDE PANEL REPAIRED IAW REO 601R-52-11-702. (K)

Part: FITTING — CRACKED (CARGO DOOR) · airframe 13,347 hrs · 12,464 cycles

FWD UPPER FITTING ON CARGO FOUND CRACK FWD UPPER FITTING ON CARGO DOOR REPLACED IAW SRM 51-42-13. (K)

Part: PANEL — CRACKED (PAX DOOR) · airframe 13,347 hrs · 12,464 cycles

PAX DOOR AFT SIDE PANEL FOUND CRACK (ZONE 2 AND ZONE 3) (CRACK LENGTH .300) PAX DOOR AFT SIDE PANEL REPAIR CARRIED OUT IAW REO 601R-52-11-700, REV A. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 13,347 hrs · 12,464 cycles

PAX DOOR AFT DRAG ANGLE FOUND CRACKED PAX DOOR AFT DRAG ANGLE REPAIRED IAW REO 601R-52-11-513, REV A. (K)

Part: CABLE — OUT OF POSITION (COCKPIT) · airframe 13,453 hrs · 12,561 cycles

PILOTS RT PEDAL LEVER FOULING WITH PARKING BRAKE CABLE. LEVER CAN’T RETURN TO FULL FWD POSITION THIS CAN CAUSE BRAKE PRESSURE ON RT SIDE. PARKING BRAKE CABLE RE-ROUTED IAW AMM TASK 32-45-01-400-801 AND AWAC SUPPLEMENT 06-027A. (K)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 12,768 hrs · 11,917 cycles

AFT PRESSURE BULKHEAD WEB AT FS 621.00 AT THE LINTEL INSTALLATION IS CRACKED. AFT PRESSURE BULKHEAD WEB AT FS 621.00 LINTEL INSTALLATION REPAIRED IAW CRJ 200 REO 601R-53-61-1230 REV D.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 12,172 hrs · 11,350 cycles

FLAPS FAIL CAUTION CAS MESSAGE IN FLIGHT WHEN SELECTING 8 DEGREES. LT AND RT INDICATE NORMAL LANDING, BRAKES ALL GREEN. PERFORMED FLANGE RELAY PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4. FLAPS RESET. ACFT RELEASED FOR SERVICE.

Part: SCAVENGE PUMP — FAILED (LT ENGINE OIL) · airframe 12,071 hrs · 11,252 cycles

AT CRUISE, AT FL310, LT OIL PRESSURE WARNING MESSAGE, OIL PRESSURE WENT TO 15-20 PSI. RAN QRH, AT IDLE PSI RETURNED TO APPROX 30 PSI FOR LESS THAN 1 MINUTES. THEN RECEIVED LT OIL PRESSURE WARNING AGAIN AND PERFORMED LT ENGINE SHUTDOWN. ENGINE WINDMILLED FOR 39 MINUTES, OIL PRESSURE NEVER GOT LOWER THAN 15 PSI. NORMAL LANDING AND ROLLOUT. BRAKE TEMPS NORMAL. REMOVED AND REPLACED ENGINE NR 1 LUBE AND SCAVENGE PUMP PER AMM 79-21-01. RAN ENGINE AND NO LEAKS APPARENT. C/W OIL CONSUMPTION CHECK AND OIL PRESSURE INSPECTION. NO DEFECTS NOTED. (A)

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 10,561 hrs · 9,798 cycles

SMOKE AND ELECTRICAL FIRE ODOR COMING FROM F/O`S SIDE PANEL NEAR WINDSHIELD. FOUND FLOOD LIGHT ON F/O`S SIDE INOPERATIVE AND CIRCUIT BREAKER FOR FLOOD LIGHT POPPED. INSPECTED WIRE HARNESS, NO DEFECTS NOTED. (M)

Part: ACTUATOR — MALFUNCTIONED (PITCH FEEL)

DURING TAKEOFF/LANDING, ELEVATOR REQUIRES GREATER THAN NORMAL FORCE TO MOVE AFT, NO BINDING FELT. REMOVED AND REPLACED FIRST OFFICERS PITCH FEEL LINEAR ACTUATOR IAW AMM 27-31-23. OPERATIONAL CHECK GOOD. (M)

Part: FLOORBEAM — CRACKED (BS 621)

FOUND RIGHT SIDE CARGO FLOOR ANGLE AT FS 621 BULKHEAD CRACKED APPROX .5 INCH LONG. (M) MAINTENANCE REPAIR CRACK IAW REO 601R-53-61-117 REV C BY INSTALLING REPAOR ANGLE AND STRAPS. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1

FOUND LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT HOLE NR 16 PN. 550HB, HAS MINOR PITTING AT IB END IN AN AREA APPROX 3.25 INCH LONG BY .003 INCH DEEP IN NON-CRITICAL AREA. (M) MAINTENANCE REPAIRED WING PLANK HOLE NR 16 (550 HB) IAW REO 601R-57-21-030 REV F AND EO E06/021/457, REV A. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1

FOUND LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT HOLE NR 2 (PNL 510AB, HAS MINOR PITTING AT INBOARD END IN AN AREA APPROX 3 INCHES LONG BY .005 INCH DEEP IN NON-CRITICAL AREA. (M) MAINTENANCE REPAIRED WING PLANK HOLE NR 2 (510AB) IAW REO 601R-57-21-030 REV F AND AWAC EO E06/021/457 REV A. (K)

Part: SKIN — CORRODED (RT WING) · corrosion level 1

RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OUT HOLE NR 8 (PNL 640FB) HAS MINOR CORROSION AT IB AND OB ENDS APPROX 3 INCH LONG BY .003 INCH DEEP AT IB END AND 1.25 INCH LONG BY .002 INCH DEEP AT OB END. BOTH IN NON-CRITICAL AREA. (M)MAINTENANCE REPAIRED WING PLANK HOLE NR 8 (640FB) IAW REO 601R-57-21-030 REV F AND E06/021/457 REV A. (K)

Part: SKIN — CORRODED (RT WING) · corrosion level 1

RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OUT HOLE NR 2 (610AB) HAS MINOR PITTING AT IB END IN AN AREA APPROX 1.5 INCH LONG BY .005 INCH DEEP IN NON-CRITICAL AREA. (M) MAINTENANCE REPAIRED WING PLANK HOLE NR 2 (610 AB) IAW REO 601R-57-21-030 REV F AND EO E06/021/457, REV A. (K)

Part: INTERCOSTAL — CRACKED (BS 621-625)

FOUND LEFT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. (M)

Part: ANGLE — CRACKED (FS621,STR 14R)

FOUND RT SIDE FS 621 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX .50 INCH LONG NEAR RADIUS. MAINTENANCE REPLACED CRACKED INTERCOSTAL WITH NEW INTERCOSTAL PN 601-35012-52 IAW SRM 51-42-06. (K)

Part: ISOLATION VALVE — LEAKING (FIRE BOTTLE) · airframe 8,166 hrs · 7,504 cycles

CARGO BOTTLE LOW MASTER CAUTION MESSAGE ILLUMINATED. REMOVED AND REPLACED LT CARGO FIRE BOTTLE, FOUND BOTTLE WAS THERMALLY DISCHARGED, CAUSED BY A LEAK ON THE 10TH STAGE ISOLATION VALVE CLAMP, TIGHTENED CLAMPS, NO LEAKS, REF AMM. (K)

Part: ANGLE — CRACKED (OBLIQUE ANGLE)

FOUND LEFT SIDE FS 621 TO 625.30 INTERCOSTAL AT STRINGER 14L CRACKED APPROX 1.1 INCH LONG NEAR RADIUS. (M) MAINTENANCE REMOVED AND REPLACED OBLIQUE ANGLE IAW SRM 51-40-11 AND 51-42-06. (K)

Part: MECHANISM — LACK OF LUBE (SERVICE DOOR)

UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE. LUBED SERVICE DOOR IAW 12-20-52, OPS CHECK GOOD. (M)

Part: WARNING LIGHT — ILLUMINATED (ANTI ICE SYS) · airframe 6,437 hrs · 5,834 cycles

ICE CAUTION LIGHT ILLUMINATED AT 80 KNOTS. ABORTED TAKEOFF, BRAKE APPLICATION AT 100 KNOTS. ICE CAUTION EXTINGUISHED 30 SECONDS AFTER LEAVING RUNWAY. MAX BTMS READINGS: 1=6, 2=5, 3=5, 4=6. PERFORMED FUNCTIONAL TEST OF THE ICE DETECTOR AMM, FOUND OK, REMOVED FROM MEL. (K)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

ON TAKEOFF, ABORTED TAKEOFF DUE TO SPOILERON CONFIG WARNING. NOTE SPEED 60 KNOTS, BTMS HIGHEST READING 4 AND 2. SENT MECHANIC FROM IAS TO BTV. PERFORMED FUNCTION CHECK OF SECU SYSTEM, AND BITE CHECK. ALL CHECKED GOOD PER 27-61-05. (M)

Part: BUSHING — MIGRATED (LT MLG)

FOUND LT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .041 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 1ST OVERSIZED BUSHING IAW BOMBARDIER REO 601R-57-21-003 REV B. (M)

Part: BUSHING — MIGRATED (TRUNNION)

RT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .045 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 1ST OVERSIZED BUSHING IAW BOMBARDIER REO 601R-57-21-003 REV B. (M)

Part: ODOR — DETECTED (CARGO BAY) · airframe 3,404 hrs · 3,019 cycles

RAMPER SMELLED BURNED PLASTIC WHEN OPENING CARGO DOOR. VISUALLY INSPECTED CARGO BAY, COULD NOT SMELL ANY PLASTIC SMELL. CARGO FAN OPS TESTED GOOD AND PERFORMED OPS TEST OF SMOKE DETECTOR IAW AMM. OPS CHECK GOOD. (M)