N409AW

Part: HINGE — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

FWD PAX DOOR AIRFRAME HINGE PN:601R31980-41 AT FS:310.00 TO FS:349.00 LHS HAS CORROSION AT NUMEROUS LOCATIONS. **** AIRCRAFT REMOVED FROM SERVICE. **** REPLACED WITH A FWD PAX DOOR AIRFRAME HINGE PN:601R31980-41 AT FS:310.00 TO FS:349.00 LHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM:52-11-04-000-801 (REV 66), AMM:51-11-04-400-801 (REV 66). WORK PERFORMED UNDER JD AERO MAINTENANCE W/O:240218 CARD NO:174 TT: 46,096.27 HRS TC: 43,568 CYC

Part: STEP — CORRODED (PAX DOOR) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

FWD PAX DOOR UPPER STEP PN:5667007 AT FS:315.00 TO FS:344.00 LHS HAS CORROSION AT NUMEROUS LOCATIONS. **** AIRCRAFT REMOVED FROM SERVICE. **** REPLACED WITH A NEW FWD PAX DOOR UPPER STEP PN:5667007 AT FS:315.00 TO FS:344.00 LHS ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM:51-11-04-000-801 (REV 66), AMM:51-11-04-400-801 (REV 66). WORK PERFORMED UNDER JD AERO MAINTENANCE W/O:240218 CARD NO: 174 TT: 46,096.27 HRS TC: 43,568 CYC

Part: CROSSTUBE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

FWD PAX DOOR HANDRAIL CROSS TUBE PN:600-3196-9 AT FS:315.00 TO FS:344.00 LHS HAS CORROSION AT NUMEROUS LOCATIONS. AIRCRAFT REMOVED FROM SERVICE. REPLACED WITH A FWD PAX DOOR HANDRAIL CROSS TUBE PN:600-3196-9 AT FS:315.00 TO FS:344.00 LHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM:52-11-05-000-801(REV66), 52-11-05-000-802(REV66),51-11-05-400-801(REV66),52-11-05-400-802(REV66), WORK PERFORMED UNDER JD AERO MAINTENANCE W/O:240218 CARD NO: 227 TT: 46,096.27 HRS TC: 43,568 CYC

Part: SUPPORT BRACKET — CORRODED (ZONE 800) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

FWD PAX DOOR BOTTOM PIVOT FITTING OB SUPPORT PN:601R38394-13 AT FS:319.00 TO FS:340.00 LHS HAS CORROSION AT NUMEROUS LOCATIONS. AIRCRAFT REMOVED FROM SERVICE. REPLACED WITH A NEW FWD PAX DOOR BOTTOM PIVOT FITTING OB SUPPORT PN:601R38394-13 AT FS:319.00 TO FS:340.00 LHS ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM:52-11-23-000-833 (REV 66), AMM:52-11-23-400-833 (REV 66). WORK PERFORMED UNDER JD AERO MAINTENANCE W/O:240218 CARD NO: 117 TT: 46,096.27 HRS TC: 43,568 CYC

Part: SUPPORT BRACKET — CORRODED (ZONE 800) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

FWD PAX DOOR BOTTOM PIVOT FITTING IB SUPPORT PN:601R31625-1 AT FS:319.00 TO FS:340.00 LHS HAS CORROSION AT NUMEROUS LOCATIONS. AIRCRAFT REMOVED FROM SERVICE. REPLACED WITH A NEW FWD PAX DOOR BOTTOM PIVOT FITTING IB SUPPORT PN:601R31625-1 AT FS:319.00 TO FS:340.00 LHS ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM:52-11-23-000-833 (REV 66), AMM:52-11-23-400-833 (REV 66). WORK PERFORMED UNDER MAINTENANCE W/O:240218.

Part: BRACKET — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

FWD GALLEY LOWER INBOARD FLOOR BRACKET PN:4602319-5 AT FS:310.00 TO FS:319.70 RHS HAS CORROSION. **** AIRCRAFT REMOVED FROM SERVICE. **** REPLACED WITH A NEW LOWER INBOARD FLOOR BRACKET PN:4602319-5 AT FS:310.00 TO FS:319.70 RHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM:51-41-02-00 (REV 39) WORK PERFORMED UNDER JD AERO MAINTENANCE W/O:240218 CARD NO: 252 TT: 46,096.27 HRS TC: 43,568 CYC

Part: RETAINER — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

FWD PAX DOOR FRAME AFT RETAINER PN:444-2439-001 AT FS:345.00 TO FS:350.00 LHS HAS CORROSION AT NUMEROUS LOCATIONS. **** AIRCRAFT REMOVED FROM SERVICE. **** REPLACED WITH A NEW FWD PAX DOOR FRAME AFT RETAINER PN:444-2439-001 AT FS:345.00 TO FS:350.00 LHS ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM:51-42-21-00 (REV 39) WORK PERFORMED UNDER JD AERO MAINTENANCE W/O:240218 CARD NO: 138 TT: 46,096.27 HRS TC: 43,568 CYC

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

SEAT RAIL AT FS:409.128 TO FS:599.00 LHS HAS CORROSION AT NUMEROUS LOCATIONS. **** AIRCRAFT REMOVED FROM SERVICE. **** REPLACED WITH A NEW SEAT RAIL PN:601R31032-7 AT FS:409.128 TO FS:599.00 LHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM:51-40-11-00 (REV 39), SRM:51-41-04-00 (REV 39). WORK PERFORMED UNDER JD AERO MAINTENANCE W/O:240216 CARD NO: 65 TT: 46,096.27 HRS TC: 43,568 CYC

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

SEAT RAIL PN:601R31032-7 AT FS:409.128 TO FS:599.00 RHS HAS CORROSION AT NUMEROUS LOCATIONS. AIRCRAFT REMOVED FROM SERVICE. REPLACED WITH A NEW SEAT RAIL PN:601R31032-7 AT FS:409.128 TO FS:599.00 RHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM:51-40-11-00 (REV 39), SRM:51-41-04-00 (REV 39). WORK PERFORMED UNDER JD AERO MAINTENANCE W/O:240216 CARD NO: 65 TT: 46,096.27 HRS TC: 43,568 CYC

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

INTERCOASTAL PN:600-31902-279 AT FS:310.00 TO FS:349.00 LHS AT DATUM 7 HAS CORROSION. **** AIRCRAFT REMOVED FROM SERVICE. **** REPLACED WITH A NEW INTERCOASTAL PN:600-31902-279 AT FS:310.00 TO FS:349.00 LHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM:51-23-00-00 (REV 39), SRM:51-40-11-00 (REV 39), 51-42-06-00(REV 39), 51-42-13-00(REV 39) AND51-45-00-00(REV 39) WORK PERFORMED UNDER JD AERO MAINTENANCE W/O:240218 CARD NO:226 TT: 46,096.27 HRS TC: 43,568 CYC

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

SEAT RAIL PN:601R38312-21 AT FS:409.00 TO FS:448.00 LHS HAS CORROSION AT NUMEROUS LOCATIONS. AIRCRAFT REMOVED FROM SERVICE. REPLACED WITH A NEW SEAT RAIL PN:601R38312-21 AT F:409.00 TO FS:448.00 LHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM:51-40-11-00 (REV 39), SRM:51-41-04-00 (REV 39). WORK PERFORMED UNDER JD AERO MAINTENANCE W/O:240216 CARD NO: 121 TT: 46,096.27 HRS TC: 43,568 CYC

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

LEADING EDGE PICOLO TUBE SPLICE BRACKET PN:601R120371-23 BETWEEN WS:139.54 TO WS:149.58 LHS HAS CORROSION AT NUMEROUS LOCATIONS. **** AIRCRAFT REMOVED FROM SERVICE. **** REPLACED WITH A NEW SPLICE BRACKET PN: PN:601R120371-23 BETWEEN WS:139.54 TO WS:149.58 LHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM:51-42-06-00 (REV 39). WORK PERFORMED UNDER JD AERO MAINTENANCE W/O:240216 CARD NO: 79 TT: 46,096.27 HRS TC: 43,568 CYC

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

LEADING EDGE PICOLO TUBE SPLICE BRACKET PN:601R120371-24S BETWEEN WS:139.54 TO WS:149.58 RHS HAS CORROSION AT NUMEROUS LOCATIONS. **** AIRCRAFT REMOVED FROM SERVICE. **** REPLACED WITH A NEW SPLICE BRACKET PN: PN:601R120371-24S BETWEEN WS:139.54 TO WS:149.58 RHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM:51-42-06-00 (REV 39). WORK PERFORMED UNDER JD AERO MAINTENANCE W/O:240216 CARD NO: 81 TT: 46,096.27 HRS TC: 43,568 CYC

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 46,096 hrs · 43,568 cycles

LEADING EDGE PICOLO TUBE SPLICE BRACKET PN:601R21071-24S BETWEEN WS:139.54 TO WS:149.58 RHS HAS CORROSION AT NUMEROUS LOCATIONS. **** AIRCRAFT REMOVED FROM SERVICE. **** REPLACED WITH A NEW SPLICE BRACKET PN: PN:601R21071-24S BETWEEN WS:139.54 TO WS:149.58 RHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM:51-42-06-00 (REV 39). WORK PERFORMED UNDER JD AERO MAINTENANCE W/O:240216 CARD NO: 81 TT: 46,096.27 HRS TC: 43,568 CYC

Part: HOSE — CHAFED (RT MLG WW) · airframe 45,982 hrs · 43,428 cycles

RECEIVED HYD 1 LO PSI AT 500 FT AGL. C/W QRH. MESSAGE PERSISTED, WITH 0 PIS AND "--" % READOUT. RETURNED TO MLI. SHUT DOWN #1 ENGINE AFTER LANDING. HYD 1 LOW PSI RAN FOR 25 MINS. AIRCRAFT REMOVED FROM SERVICE. VISUALLY INSPECTED #1 HYD RESERVOIR QUANTITY GAUGE. RESERVOIR GAUGE READS 0%. INSPECTED AIRCRAFT FOR EVIDENCE OF HYD LEAK. FOUND TWO HYDRAULIC FLEX LINES IN RH MLG WHEEL WELL CHAFFING AND CAUSING LEAK. REF 323370-2 - 4 FOR ADDITIONAL WRITE-UPS. INSTALLED OB GND SPOILER HOSE ASSY IAW AMM 20-22-01. LEAK CHECK GOOD . INSTALLED RETURN HOSE ASSY IAW AMM 20-22-01. LEAK CHECK GOOD. C/W AMM 05-51-33-210-801 3D. NO DEFECTS NOTED.

Part: NONE — NONE · airframe 44,182 hrs · 41,656 cycles

AT FL230 CABIN ALT SPIKED TO 5,900FT. AT 3,700 FPM. AT 10000FT, CABIN ALT DECREASED TO 900FT AT 300 FPM. FROM 10000 FEET TO LANDING, PSI'N ACTED NORMALLY. PRESSURIZATION WAS IN AUTO MODE FOR THE ENTIRE EVENT. BOTH PACKS OPERATED NORMALLY THE ENTIRE FLIGHT. NO CABIN ALT WARNING OR AURAL MESSAGES. ***AIRCRAFT REMOVED FROM SERVICE*** R&R #1 CABIN PRES CONTROLLER PER CRJ 200 AMM 21-31-16 PRES AC PER CRJ 200 AMM 21-32-00 OPS CK GOOD P/N: 2119768-8, S/N OFF: 112-C1551, S/N ON: 123-C1876 ARW

Part: NONE — NONE · corrosion level 2 · airframe 44,035 hrs · 41,507 cycles

WHEN REMOVING FIXED BALLAST FOUND CORROSION IN SEAT TRACK FROM F.S 559+112 TO 574 R/H O/B SEAT TRACK ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM SEAT TRACK

Part: DOUBLER — DAMAGED (BS 220-235) · airframe 41,648 hrs · 39,067 cycles

FWD LHS FUSELAGE ACCESS PANEL 131AL SURROUND DOUBLER HAS TWO SCREW HOLES WITH DEEP COUNTERSINKS AT 1 O"CLOCK & 3 O"CLOCK. AIRCRAFT REMOVED FROM SERVICE REPAIRED IAW BOMBARDIER REO 601R-11-162 REV.C, DATED 2015/11/16.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 41,648 hrs · 39,067 cycles

INDICATION NOTED AT F.S. 621 REAR PRESSURE BULKHEAD FWD FACE AT LBL 36.20, WL79.0, 100% FULL SCREEN HEIGHT AND .70" LONG FAILING NDT. AIRCRAFT REMOVED FROM SERVICE REPAIRED DAMAGE AT F.S. 621 REAR PRESSURE BULKHEAD AT LBL 36.20, WL79.0 IAW BOMBARDIER REO 601R-53-61-1240, REV-D, DATED 2016-10-31.

Part: SKIN — DENTED (BS 654 - 672) · airframe 41,648 hrs · 39,067 cycles

FOUND 1EA. PROTRUDING DENT LOCATED BETWEEN F.S.654.50 AND F.S.672.20 BETWEEN STGR27 AND STGR26R. AIRCRAFT REMOVED FROM SERVICE REPAIRED DENT DAMAGE TO FUSELAGE LOWER SKIN FROM F.S.654.50 TO F.S.672.20, STGR 27 TO STGR26R IAW ASAP EA# AWAC-CRJ253-01371.

Part: BEAM — GOUGED (CARGO DOOR) · airframe 41,648 hrs · 39,067 cycles

FOUND CARGO DOOR HORIZONTAL BEAM TO BE CHAFED ON FWD SIDE BELOW THE GROVED PULLEY. REF WVAC JOB 6744745 OP 109. AIRCRAFT REMOVED FROM SERVICE REPLACED DAMAGED BEAM IAW CRJ SRM 200 51-42-01, 51-42-21, 51-40-11 AND AWAC EO# E18/001/452.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

R/H BATT RIB AT W.S.53.60 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED CORRODED R/H BATT RIB AT W.S.53.60 AND INSTALLED NEW SERVICABLE BATT RIB IAW CRJ 200 SRM 51-42-21, 51-42-06 AND 51-42-10.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

RBL18 SEAT TRACK IS CORRODED BETWEEN F.S.559+48 TO F.S.559+64. AIRCRAFT GROUNDED REMOVED AND REPLACED SEAT TRACK AT RBL18 BETWEEN FS559+49 AND FS559+64 IAW CRJ200 AMM TASK 53-01-11-000-802 AND 53-01-11-400-802.

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

F.S.605 FRAME IS CORRODED ON BOTH FWD AND AFT SIDES BETWEEN STGR27 AND STGR26L.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

LH SIDE WALL SEAT TRACK IS CORRODED BETWEEN FS409+16 AND F409+112

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

RBL9 SEAT TRACK IS CORRODED BETWEEN FS559 TO FS559+80.

Part: SEAT TRACK — CORRODED (BS 544-559) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

RH SIDE SEAT TRACK IS CORRODED BETWEEN FS544 AND FS559+80.

Part: SEAT TRACK — CORRODED (BS 499-544) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN FS499 AND FS544

Part: SEAT TRACK — CORRODED (BS 364-409) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

RH SIDE SEAT TRACK IS CORRODED BETWEEN FS364 AND 409+16.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

RBL9 FLOOR SEAT RAIL IS CORRODED BETWEEN FS409 AND FS409+128.

Part: SEAT TRACK — CORRODED (BS 544-559) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

RH SIDE SEAT TRACK IS CORRODED BETWEEN FS544 AND FS559+80.

Part: SEAT TRACK — CORRODED (BS 449-499) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

LH SIDE WALL SEAT TRACK IS CORRODED BETWEEN FS449.85 AND FS499.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

LBL9 FLOOR SEAT RAIL IS CORRODED BETWEEN FS409 AND FS 409+128

Part: CUP — CORRODED (DOOR HAND RAIL) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

PAX DOOR FWD AND AFT HAND RAIL CUPS ARE CORRODED.

Part: SEAT TRACK — CORRODED (BS 364-399) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

FLOOR SEAT RAIL CORRODED F.S.364 TO F.S.399.50 AT RBL9.

Part: SEAT TRACK — CORRODED (BS 409-449) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

R/H SIDE WALL SEAT TRACK IS CORRODED BETWEEN F.S.409+112 TO F.S.449.85.

Part: SEAT TRACK — CORRODED (BS 634-399) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

FLOOR SEAT RAIL CORRODED F.S.364 TO F.S.399.50 AT LBL9.

Part: DOUBLER — CORRODED (LEFT WING) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

L/H BATT RIBS AT W.S.53.60 AND 58.88 ARE CORRODED. AIRCRAFT REMOVED FROM SERVICE REPLACED OTBD BATT RIB AT W.S 58.88 IAW CRJ200 SRM 51-42-06 AND 51-42-21. BLENDED BATT RIB AT W.S.53.60 IAW CRJ200 SRM 51-21-06.

Part: SEAT TRACK — DAMAGED (BS 250-280) · airframe 41,648 hrs · 39,067 cycles

O/B COPILOT SEAT TRACK DAMAGED BEYOND LIMITS, REQUIRES REPLACEMENT. AIRCRAFT REMOVED FROM SERVICE REPAIRED CO-PILOT'S O/B SEAT TRACK IAW AIR WISCONSIN EO# E15/004/453 REV. A.

Part: BEAM — CHAFED (BS 574-621) · airframe 41,648 hrs · 39,067 cycles

FOUND CARGO DOOR HORIZONTAL BEAM TO BE CHAFED ON FED SIDE BELOW THE GROOVE PULLEY.

Part: SEAT TRACK — DAMAGED (BS 280-280) · airframe 41,648 hrs · 39,067 cycles

I/B COPILOT SEAT TRACK DAMAGED BEYOND LIMITS. REQUIRES REPLACEMENT. AIRCRAFT REMOVED FROM SERVICE REPAIRED CO-PILOT'S I/B SEAT TRACK IAW AIR WISCONSIN EO# E15-004-453 REV. A.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 41,648 hrs · 39,067 cycles

O/B PILOT SEAT TRACK DAMAGED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE REPAIRED PILOT'S O/B SEAT TRACK IAW AIR WISCONSIN E.O# E15/003/453 REV. A

Part: SEAT TRACK — WORN (BS 235-280) · airframe 41,648 hrs · 39,067 cycles

PILOT FWD INBOARD SEAT TRACK IS WORN BEYOND ALLOWABLE LIMITS.

Part: POST — CRACKED (BS 409) · airframe 41,648 hrs · 39,067 cycles

FOUND FS409+128 VERTICAL POST RBL18.0 HAS INDICATION INBD SIDE .300 LONG 50% FSH AT AFT FLANGE RADIUS, FAILS NDT. AIRCRAFT REMOVED FROM SERVICE REPLACED FS409+128 VERTICAL POST AT RBL18.0 INBD SIDE IAW CRJ200 SRM 51-42-06, BOMBARDIER REO 601R-53 41-889 REV. D, DATED 2018-10-04 AND BOMBARDIER REO 601R-53-41-1418 REV. --, DATED 2011-05-21.

Part: SEAT TRACK — CORRODED (BS 364-409) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

L/H SIDE WALL SEAT TRACK IS CORRODED BETWEEN F.S.364 TO F.S.409.

Part: STIFFENER — CRACKED (BS 409) · airframe 41,648 hrs · 39,067 cycles

FOUND FS409+128 VERTICAL POST AT BL0.00 LEFT SIDE HAS INDICATION .400 LONG 80% FSH AT AFT FLANGE RADIUS, FAILS NDT. AIRCRAFT REMOVED FROM SERVICE REPLACED FS409+128 BL0.00 VERTICAL POST LEFT SIDE IAW CRJ200 SRM 51-42-06 AND BOMBARDIER REO 601R-53 41-889 REV. D, DATED 2018-10-04.

Part: STIFFENER — CRACKED (BS 409) · airframe 41,648 hrs · 39,067 cycles

FOUND FS409+128 VERTICAL POST BL0.00 RIGHT SIDE HAS INDICATION NOTED .300 LONG 70% FSH AT AFT FLANGE RADIUS, FAILS NDT. AIRCRAFT REMOVED FROM SERVICE REPLACED FS409+128 VERTICAL POST AT BL0.00 RIGHT SIDE IAW CRJ200 SRM 51-42-06 AND BOMBARDIER REO 601R53-41-889 REV. D, DATED 2018-10-04.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S.409+16 TO F.S.409+112.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

LBL9 SEAT TRACK IS CORRODED FROM F.S.559+0 TO F.S.559+80.

Part: ANGLE — CORRODED (BS 310-349) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

PAX DOOR UPPER SILL ANGLE IS CORRODED AROUND THE PROX SENSOR,& NUTPLATE FWD OF PROX SENSOR. AIRCRAFT REMOVED FROM SERVICE REPLACED PAX DOOR SILL ANGLE IAW CRJ200 SRM 51-42-06.

Part: CROSSBEAM — CORRODED (BS 349) · corrosion level 2 · airframe 41,648 hrs · 39,067 cycles

F.S.349 CROSSBEAM IS CORRODED AT RBL 36.

Part: SKIN — DENTED (LEFT WING) · airframe 41,648 hrs · 39,067 cycles

LH INBD FLAP TOP SKIN DENTED APPROX. 21" FROM I/B EDGE AND 19" FROM TRAILING EDGE.

Part: MOUNT — BROKEN (ELEVATOR SERVO) · airframe 40,378 hrs · 37,840 cycles

DURING CRUISE THE AUTOPILOT COULD NOT HOLD AN ALTITUDE. A/C WOULD CLIMB AND/OR DESCENT AT 20-500 FT/MIN. DURING T/S WE FOUND THAT THE AFT CABLE TO THE ELEVATOR SERVO MOUNT WAS SNAPPED IN TWO PIECES. WE HAD TO REPLACE ALL 3 CABLES AND THE SERVO MOUNT AS A PRECAUTION.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 39,187 hrs · 36,587 cycles

SERVICE DOOR FLOOR PROXIMITY EMERGENCY EXIT SIGN DS11LY INOP FWD CABIN. FOUND WIRES FOR GREEN EXIT LIGHT AT SERVICE DOOR AND WHITE EXIT SIGN LIGHT AT SERVICE DOOR SUPP AND PERFORMED OPS CHECK 33-51-00, OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,184 hrs · 36,586 cycles

EXTERNAL EMERGENCY LIGHTS INOPERATIVE, RT AFT OF OVERWING EXIT, LT FWD NR 2 EMERGENCY LIGHT, LT NR 4 EMERGENCY LIGHT, NR 2 & 4 EMERGENCY CEILING LIGHTS. REMOVED AND REPLACED THE BATTERY NR 4 IAW AMM 33-51-04. OPS CHECKED GOOD IAW AMM 33-51-04.

Part: HINGE — GOUGED (PAX DOOR) · airframe 39,184 hrs · 36,585 cycles

PAX DOOR HINGE HAS A DEEP GOUGE AT THE AFT LANDING.

Part: BEAM — CORRODED (BS 605) · corrosion level 2 · airframe 39,184 hrs · 36,585 cycles

AFT CARGO BEAM LBL 27 CORRODED AT BS 605

Part: FLOORBEAM — CORRODED (BS 605) · corrosion level 2 · airframe 39,184 hrs · 36,585 cycles

AFT CARGO HAS CORROSION ON FLOOR BEAM LBL27 I/B AND O/B AT FS 605

Part: SHROUD — CRACKED (RT WING) · airframe 39,184 hrs · 36,585 cycles

LEADING EDGE 630KL INNER LOWER SHROUD CRACKED AT EXTENSION JOINT

Part: WEB — CRACKED (RT WING) · airframe 39,184 hrs · 36,585 cycles

RIGHT WING L/E SHROUD LOWER ANGLE, CENTER WEB CRACKED. REPLACED THE WEB IAW SRM 52-41-29, 51-40-11, 51-42-06, AND 51-42-13.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 39,184 hrs · 36,585 cycles

LT WING IB FLAP VANE CTR LEADING EDGE IS CHAFED.

Part: WEB — DAMAGED (BS 589-605) · airframe 39,184 hrs · 36,585 cycles

FLOORBEAM WEB HAS OVERSIZED FASTENER HOLES. REPLACED THE WEB IAW SRM 51-42-06, 51-42-21, 51-40-11, AND 51-24-36.

Part: WEB — DAMAGED (BS 574-589) · airframe 39,184 hrs · 36,585 cycles

WEB HAS OVERSIZED FASTENER HOLES AT BS 574 TO 589, LBL 27. REPLACED THE WEB IAW SRM 51-42-06, 51-42-21, 51-40-11, AND 51-24-36.

Part: WEB — DAMAGED (BS 605-621) · airframe 39,184 hrs · 36,585 cycles

FLOORBEAM INBD WEB HAS OVERSIZED FASTENER HOLES, BS 605 TO 621, LBL 27. REPLACED THE WEB IAW 17-170.

Part: WEB — DAMAGED (BS 574-589) · airframe 39,184 hrs · 36,585 cycles

1014598-1000-0051 - BEAM CAP HAS OVERSIZED FASTENER HOLES. REPAIRED IAW CRJ 200 SRM 51-42-06, 51-42-21, 51-40-11, 51-24-36.

Part: WEB — DAMAGED (BS 589-605) · airframe 39,184 hrs · 36,585 cycles

FLOORBEAM INNER WEB HAS OVERSIZED FASTENER HOLES. REPLACED THE WEB IAW SRM 51-42-06, 51-42-21, 51-40-11, AND 51-24-36.

Part: FLOOR SUPPORT — DAMAGED (BS 605-621) · airframe 39,184 hrs · 36,585 cycles

FLOOR SUPPORT CAP HAS OVERSIZED FASTENER HOLES AT BS 605 TO 621, LBL 27. REPLACED THE FLOORBEAM CAP IAW 17-170.

Part: WEB — CRACKED (LT WING) · airframe 39,184 hrs · 36,585 cycles

LEFT WING OTBD LEADING EDGE WEB IS CRACKED AROUND FASTENER HOLES. REPLACED THE LT WING L/E WEB IAW SRM 51-42-06, AND 51-42-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,184 hrs · 36,585 cycles

AFT CARGO CORROSION ON FLOORBEAM LBL9 I/B, FS605.

Part: BULKHEAD — CRACKED (BS 621) · airframe 39,184 hrs · 36,585 cycles

AFT PRESSURE BULKHEAD CRACKED AT BS 621, RBL 18, WL 109.5. REPAIRED THE BULKHEAD IAW REO 601R-53-61-1285, REV-E.

Part: BULKHEAD — CRACKED (BS 621) · airframe 39,184 hrs · 36,585 cycles

AFT PRESSURE BULKHEAD CRACKED AT BS 621, LBL 9.5, WL 92. REPAIRED THE BULKHEAD IAW REO 601R-53-61-1285, REV-E.

Part: BULKHEAD — CRACKED (BS 621) · airframe 39,184 hrs · 36,585 cycles

AFT PRESSURE BULKHEAD CRACKED AT BS 621, RBL 9.5, WL 85. REPAIRED THE BULKHEAD IAW REO 601R-53-61-1285, REV-E.

Part: BULKHEAD — CRACKED (BS 621) · airframe 39,184 hrs · 36,585 cycles

AFT PRESSURE BULKHEAD CRACKED AT BS 621, RBL 27, WL 109. REPAIRED THE BULKHEAD IAW REO 601R-53-61-1285, REV-E.

Part: BULKHEAD — CRACKED (BS 621) · airframe 39,184 hrs · 36,585 cycles

AFT PRESSURE BULKHEAD CRACKED AT BL 0, WL 131. REPAIRED THE BULKHEAD IAW REO 601R-53-61-1285, REV-E.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 39,184 hrs · 36,585 cycles

FLOOR STRAP AT BS 559 IS CORRODED BETWEEN RBL 27 AND RT FLOOR SUPPORT.

Part: FRAME — CRACKED (BS 718) · airframe 39,184 hrs · 36,585 cycles

RT FRAME AT BS 718, STRINGER 16 TO 17R. REPAIRED IAW EA 253-00718, REV IR.

Part: STIFFENER — CRACKED (RT TAILPIPE) · airframe 39,184 hrs · 36,585 cycles

RIGHT TAILPIPE HAS A CRACKED STIFFENER AT 9 O'CLOCK POSITION 2ND FROM LE

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,184 hrs · 36,585 cycles

ANGLE CLIP CRACKED ON O/B SIDE OF RBL27 AT FS 484.00. REPLACED ANGLE CLIP IAW REO 601R-53-41-059 REV-B.

Part: FLOORBEAM — CORRODED (BS 605) · corrosion level 2 · airframe 39,184 hrs · 36,585 cycles

CARGO FLOORBEAM HAS CORROSION AT BS 605, RBL 27. REPLACED THE FLOORBEAM IAW 15-279.

Part: HANDLE — UNSECURE (E/E BAY DOOR) · airframe 38,712 hrs · 36,155 cycles

AVIONICS BAY DOOR AMBER MESSAGE DISPLAYED DURING LIFT OFF. RETURNED TO DEPARTURE. FOUND HANDLE OUT.

Part: DOOR — STUCK (CABIN) · airframe 38,076 hrs · 35,553 cycles

PASSENGER DOOR WILL NOT OPEN FROM BOTH INSIDE AND OUTSIDE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 37,807 hrs · 35,299 cycles

FLIGHT 3908, ROW 10 AND AFT EMERGENCY FLOOR LIGHTING INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY LIGHT STAIR CONNECTOR AND PIN IAW AMM 20-10-00. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 37,655 hrs · 35,156 cycles

CREW REPORTED ON ACCEPTANCE INSPECTION, THAT THE EMERGENCY FLOOR LEVEL LIGHTS DID NOT ILLUMINATE FROM ROW 8 AFT. R & R NR 4 INVERTER. OPS CHECK GOOD IAW AMM 33-51-07.

Part: UNKNOWN — ODOR · airframe 36,560 hrs · 34,142 cycles

FLIGHT 3827, FUEL SMELL DURING APU START IN FLIGHT, SHUT APU OFF SMELL CLEARED. RAN APU, NO FUEL SMELL NOTED AT THIS TIME IAW AMM 49-10-00.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 36,532 hrs · 34,120 cycles

FIRST OFFICER REPORTS CREW OXYGEN MASK DIFFICULT TO EXHALE IN.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 26,516 hrs · 34,106 cycles

PASSENGER DOOR HANDLE WILL NOT TURN TO OPEN DOOR. CLEANED & LUBED PAX DOOR OUTER HANDLE IAW SUP 12-093. PERFORMED OPERATIONS CHECK IAW AMM 52-11-00. OPERATIONS CHECKED GOOD.

Part: ANTI-ICE VALVE — FAULTY (RT ENGINE) · airframe 36,161 hrs · 33,779 cycles

RIGHT COWL ANTI-ICE CAUTION MSG WHEN COWL ANTI-ICE SELECTED OFF. COMPLIED WITH QRH & SELECTED RT 14TH STAGE SOV OFF & MSG CLEARED. R & R RT ENG COWL ANTI-ICE VLV IAW AMM SUP 10-094, OPERATIONS CHECKED GOOD.

Part: TIRE — BLOWN (NLG) · airframe 28,981 hrs · 27,981 cycles

NOTICED NOSE WHEEL SHIMMY ON TAKEOFF. ABORTED TAKEOFF AT 70 KNOTS & UNABLE TO STEER ACFT ONCE OFF THE RUNWAY, BTMS 4-6-4-5. NOSE WHEELS LT & RT BLOWN.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 35,819 hrs · 33,449 cycles

LEFT AOA HEAT CAUTION MSG ON APPROACH. COMPLIED WITH FIM RESET, MSG REMAINS.

Part: HANDLE — DEFECTIVE (PAX DOOR) · airframe 35,800 hrs · 33,428 cycles

PASSENGER DOOR VERY DIFFICULT TO OPEN FROM CABIN. DOOR INTERMITTENTLY WILL NOT OPEN FROM INSIDE. FOUND OUTER HANDLE LATCH RELEASE BUTTON WORN. R & R OUTER HANDLE IAW AMM 52-11-03. OPERATIONS CHECKED GOOD. OK FOR SERVICE.

Part: HANDLE — DEFECTIVE (PAX DOOR) · airframe 35,619 hrs · 33,260 cycles

PASSENGER DOOR WILL NOT OPEN WITHOUT TOOL ASSISTANCE, OR STOW FROM INSIDE OR OUTSIDE. R & R PAX DOOR OUTER HANDLE ASSEMBLY IAW AMM 52-11-03. PERFORMED OPERATIONS CHECK IAW AMM 52-11-03. CHECKED GOOD.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 35,491 hrs · 33,132 cycles

FLIGHT 3862, EMER LIGHTING ON THE FLOOR IS INOPERATIVE FROM ROW 8 TO THE REAR OF ACFT. SECURED CONNECTOR ON ROW 8 LIGHT STRIP. OPERATIONS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 34,855 hrs · 32,506 cycles

EMERGENCY FLOOR LEVEL LIGHTS ROWS 2 - 4 INOPERATIVE RIGHT SIDE. EMERGENCY LIGHTS CYCLED SEVERAL TIMES, WALKED OVER LIGHT TO ENSURE GOOD CONNECTION. OPS CHECKED GOOD AT THIS TIME IAW 33-51-01.

Part: SKIN — DENTED (LT SPOILER) · airframe 34,838 hrs · 32,494 cycles

LEFT INBD GND SPOILER HAS DENTS IN LOWER SKIN.

Part: CHANNEL — CHAFED (TE FLAP) · airframe 34,838 hrs · 32,494 cycles

LEFT OTBD FLAP ROLLER CHANNEL CHAFED.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 34,838 hrs · 32,494 cycles

PAX DOOR AFT FRAME MEMBER IS CRACKED IN RADIUS FS 338.00.

Part: STRIKER — CRACKED (FUSELAGE) · airframe 34,838 hrs · 32,494 cycles

PAX DOOR SURROUND LOWER SEAL STRIKER CRACKED.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 34,838 hrs · 32,494 cycles

PAX DOOR FWD FRAME MEMBER IS CRACKED IN RADIUS AT FS 320.10.

Part: SKIN — DAMAGED (RT WING) · airframe 34,838 hrs · 32,494 cycles

RIGHT AFT LOWER WING PLANK WATER DRAIN HOLE AT RBL 5.0, BETWEEN STRINGER 5 & 7, DAMAGED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,838 hrs · 32,494 cycles

55370-2000-0074 OUTBOARD CLIP AT LBL 9 & OTBD CLIP AT RBL 9 ARE CRACKED AT FS 280 FLOOR SUPPORT BEAM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 34,838 hrs · 32,494 cycles

FLIGHT CONTROL LEAD FAIRLEAD INTERCOSTAL AT FS 484 LT INBD ATTACH ANGLE IS CRACKED.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,838 hrs · 32,494 cycles

SERVICE DOOR LOWER SILL UPPER & LOWER ANGLES BOTH ARE CORRODED AT MULTIPLE LOCATIONS FROM FS 319 - 349.

Part: ANGLE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 34,838 hrs · 32,494 cycles

FS 280 FLOOR SUPPORT CROSSBEAM TOP AFT ANGLE HAS CORROSION BETWEEN LBL 9 & RBL 9, CRACKED AT LBL 12.

Part: SEAL — CRACKED (RT SPOILER) · airframe 34,834 hrs · 32,494 cycles

RIGHT FLIGHT SPOILER OTBD SPRING SEAL IS CRACKED.

Part: STIFFENER — CRACKED (RT EXHAUST) · airframe 34,601 hrs · 33,494 cycles

THE 2ND STIFFENER FROM LE IS CRACKED ON RT ENG EXHAUST NOZZLE FAIRING AT APPROX. 9 O'CLOCK POSITION.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,834 hrs · 32,494 cycles

FS 280 STRINGER 3 CLIP CRACKED.

Part: SKIN — CHAFED (LT WING) · airframe 34,838 hrs · 32,494 cycles

LEFT UPPER WING PLANK DRY BAY PANEL 540AT & 540BT, CUT OUTS CHAFFED.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 34,838 hrs · 32,494 cycles

LEFT INBD FLAP VANE LE CHAFED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,838 hrs · 32,494 cycles

FLOOR SEAT RAIL AT RBL 9 HAS CORROSION FROM FS 370 TO AFT END OF RAIL AT FS 398.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,838 hrs · 32,494 cycles

FLOOR SEAT RAIL AT LBL 9 HAS CORROSION NEAR FWD END AT FS 370 & 390.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,838 hrs · 32,494 cycles

AFT SIDE OF FS 621 BULKHEAD OBLIQUE ANGLE CRACKED AT STRINGER 14L.

Part: POST — CRACKED (FUSELAGE) · airframe 34,838 hrs · 32,494 cycles

FORWARD SIDE FS 409+128 BULKHEAD LBL 9 INBD VERTICAL POST IS CRACKED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 34,838 hrs · 32,494 cycles

NLG WW CUT OUT AFT RADIUS CRACKED, FS 235 AT LBL 6 & RBL 6.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 34,757 hrs · 32,417 cycles

EMERGENCY EXIT SIGN FWD OF THE SERVICE DOOR BROKEN.

Part: OXYGEN MASK — MALFUNCTIONED (CABIN) · airframe 34,679 hrs · 32,346 cycles

WORK ORDER 225183 & 282073 101 PAX O2 MASK DOES NOT DEPLOY AT ROW 12AC & 12DF.

Part: LANDING GEAR — ICED (NOSE) · airframe 33,990 hrs · 31,697 cycles

DURING GO AROUND IN MODERATE TO HEAVY ICING, RECEIVED GEAR DISAGREE APPROXIMATELY SIX SECONDS AFTER SELECTING GEAR UP. NOSE GEAR SHOWED RED. MESSAGE CLEARED AFTER APPROXIMATELY THIRTY SECONDS, HYD PRESSURE GOOD. POST FLIGHT INSPECTION SHOWED MODERATE ICE ON GEAR.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 33,979 hrs · 31,689 cycles

RECEIVED DISPLAY COOL CAUTION MSG IN FLIGHT. COMPLIED WITH QRH, MSG PERSISTS IN STBY. DECLARED EMER & DIVERTED. MSG EXTINGUISHED ON APPROACH. MADE NORMAL LANDING AT 39,000 LBS WITH NO FURTHER ISSUES. ALL THREE DISPLAY FANS, OPERATIONS CHECKED IAW AMM 21-24-19.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,727 hrs · 31,444 cycles

EMERGENCY LIGHTS ARE INOPERATIVE, ROW 8 & AFT.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 33,013 hrs · 30,769 cycles

CLIMB THREW 14,000 FT, FLIGHT ATTENDANT REPORTED SMOKE IN GALLEY THAT APPEARED TO BE COMING FROM THE COFFEE MAKER. LANDING WEIGHT 48,200 LBS. PERFORMED INSPECTION WIRE HARNESS BEHIND COFFEE MAKER, NO DEFECTS NOTED. PERFORMED INSPECTION OF GALLEY LIGHTS, HEATERS, FAN & NO DEFECTS NOTED. R & R GALLEY COFFEE MAKER IAW AMM 25-30. OPERATIONS CHECKED GOOD, ACFT OK FOR SERVICE. REF 272205 2 FOR CORRECTIVE ACTION FOR OVERWEIGHT LANDING.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 30,477 hrs · 28,291 cycles

FLAP FAIL AT 20 DEGREES DURING APPROACH.. FLAPS WERE AT 20 FOR A COUPLE OF MINUTES, APPROACH WAS IN HEAVY RAIN. PERFORMED FLAP RESET PROCEDURE IAW SUPP 98-18F, BOX 12, FLAPS RESET. INTEREGATED FECU REF 27-51 AT SUPP 98-018F. R & R FECU IAW AMM 2751. OPS CHEKCED GOOD.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 29,958 hrs · 27,772 cycles

LEFT SIDE OF 280 BULKHEAD INBD FACE STRUCTURE AT ENTRANCE TO FLIGHT COMPARTMENT HAS TORN AND DAMAGED METAL. REMOVED & REPLACED LEFT SIDE OF 280 BULKHEAD FACE STRUCTURE ANGLE IAW CRJ 200 SRM 51-42-06.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 29,958 hrs · 27,772 cycles

CALL BACK CAPT & F/O SEAT TRACK. REMOVED WORN PILOT & COPILOT SEAT TRACKS AND REPLACED WITH NEW SERVICEABLE TRACKS.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 29,958 hrs · 27,772 cycles

NOSE HYD COMPARTMENT FWD O/B MOUNT BRACKET ON UPPER ACCUMULATOR IS CRACKED. BOMBARDIER REO 601R-53-12-183 REV A.

Part: HEAT SHIELD — PUNCTURED (RT COWLING) · airframe 29,958 hrs · 27,772 cycles

RIGHT LWR CORE COWL FWD HEAT SHIELD PUNCTURED. REPAIRED RIGHT LWR CORE COWL FWD HEAT SHIELD IAW REO 601R-71-12-4163.

Part: SKIN — CRACKED (RT AILERON) · airframe 29,958 hrs · 27,772 cycles

RIGHT AILERON EDGE IS CRACKED DOWN TO THE METAL. REMOVED UNSERVICEABLE RIGHT SKIN SECTION REPLACED WITH NEW SERVICEABLE P/N 601R3031-148 IAW CRJ SRM 51-42-06.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 29,958 hrs · 27,772 cycles

PAX DOOR LOWER AFT CORNER INTERCOSTAL UNDER PANEL 832AR CRACKED. REMOVED CRACKED INTERCOSTAL THEN INSTALLED NEW SERVICEABLE INTERCOSTAL.

Part: MOUNT BRACKET — CRACKED (CARGO DOOR) · airframe 29,958 hrs · 27,772 cycles

CARGO DOOR FWD LOWER TRACK MOUNT IS CRACKED. REMOVED AND REPLACED WITH NEW SERVICEABLE BRACKET IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-25-16.

Part: DOOR — CHAFED (RT MLG) · airframe 29,958 hrs · 27,772 cycles

RIGHT MLG DOOR L/E CHAFED AT PREVIOUS REPAIR. PERFORMED REPAIR ON RIGHT MLG DOOR IAW REO 601R-52-82-016 REV-.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 29,958 hrs · 27,772 cycles

ANGLE IS CRACKED ON APB IN AEB. REMOVED AND REPLACED ANGLE PER SRM.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 29,958 hrs · 27,772 cycles

ADG DOOR CUTOUT AND LANDING LOWER SIDE DAMAGED. REPAIRED PER REO 601R-53-11-2494.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,958 hrs · 27,772 cycles

CLIP ANGLE CRACKED AT FS 589 UNDER CARGO DOOR FLOOR SILL. REMOVE & REPLACE SLIP IAW CRJ 200 SRM 51-40-11, 51-42-13, 51-42-21, 51-40-02, 51-42-06, 51-21-11, 51-25-06, 51-25-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,958 hrs · 27,772 cycles

CLIP ON CRACKED AT FS 605 UNDER CARGO DOOR SILL. REMOVED AND REPLACED CLIP IAW CRJ 200 SRM 51-40-11, 51-42-13, 51-42-21, 51-42-02, 51-42-06, 51-21-11, 51-25-06, 51-25-16.

Part: FITTING — CRACKED (COCKPIT) · airframe 29,958 hrs · 27,772 cycles

LEFT WINDSHIELD SIDE POST SUPPORT IS CRACKED ON O/B CLIP. REMOVED UNSERVICEABLE O/B CLIP AND REPLACED WITH SERVICEABLE O/B CLIP.

Part: RIB — CRACKED (WING) · airframe 29,958 hrs · 27,772 cycles

BATT RIB'S ARE CRACKED IN RIGHT AND LEFT MLG WHEEL WELL'S. REPAIRED PER BOMBARDIER REO 601R-57-51-046 REV B.

Part: FITTING — CRACKED (COCKPIT) · airframe 29,958 hrs · 27,772 cycles

RIGHT WINDHSIELD SIDE POST SUPPORT IS CRACKED ON O/B CLIP. REMOVED UNSERVICEABLE O/B CLIP AND REPLACED WITH SERVICEABLE O/B CLIP IAW CRJ SRM 51-42-21.

Part: SILL — CORRODED (FUSELAGE) · airframe 29,958 hrs · 27,772 cycles

PAX DOOR LOWER SILL IS CORRODED. REMOVED CORRODED SILL AND INSTALLED DUPLICATED SILL IAW CRJ 200 SRM 51-40-11, 51-21-11, 51-24-16, 51-25-06, 51-25-16, 51-42-06, 51-42-13, 51-42-21, 51-45-00, 51-23-00.

Part: WARNING MESSAGE — ILLUMINATED (WINDOW HEAT) · airframe 25,606 hrs · 23,418 cycles

RT WINDOW HEAT CAUTION MESSAGE INFLIGHT, CW QRH MESSAGE PERSISTS. C/W FIM RESET PROCEDURE, MESSAGE CLEARED. C/W OPS CHECK IAW AMM 30-01-01. OPS CHECKS GOOD.

Part: LINE — LEAKING (HYD MANIFOLD) · airframe 25,503 hrs · 23,307 cycles

HYDRAULIC 2 QTY READS ZERO, HYD FLUID LEAKING FROM AFT EQUIPMENT BAY. FOUND LEAK FROM NR 2 HYD MANIFOLD PRESSURE LINE INPUT REDUCER. REPLACED O-RING, REF 29-11-05 OF AMM. REF LP 221209/2 FOR LK AND OPS CKS.

Part: BALLAST — BURNED (LAVATORY LIGHT) · airframe 25,492 hrs · 23,295 cycles

REQUEST LAVATORY LIGHT BALLAST CHECKED FOR BURNING ODOR. REMOVE AND REPAIRED BALLAST. OPS CHECKED GOOD.

Part: IDG — MALFUNCTIONED (NR 2) · airframe 25,662 hrs · 23,478 cycles

GEN 2 CAUTION MESSAGE RECEIVED DURING T/O ROLL, AROUND 80 KTS, ABORTED TAKEOFF. R & R NR 2 IDG ASSY, OPS AND LEAK CHECKED.

Part: BULKHEAD — CHAFED (BS 621) · airframe 25,326 hrs · 23,121 cycles

FS621 BULKHEAD FWD SIDE HAS 4 EA CHAFED SPOTS FROM FASTENERS. REPAIRED CHAFED AREAS IAW REO 601R-53-61-215.

Part: ROLLER TRACK — DAMAGED (RT WING TE FLAP) · airframe 25,326 hrs · 23,121 cycles

RT OTBD FLAP, INBD ROLLER BEARING TRACK DAMAGED. REPAIRED RT OTBD FLAP ROLLER TRACK IAW REO 601R-57-51-140.

Part: FITTING — CHAFED (LT WING TE FLAP) · airframe 25,326 hrs · 23,121 cycles

LEFT OTBD FLAP GUIDE CHAFED. BLENDED CHAFED AREA WITHIN LIMITS.

Part: GUIDE — CHAFED (LT WING TE FLAP) · airframe 25,326 hrs · 23,121 cycles

LT OTBD FLAP GUIDE CHAFED, BLENDED CHAFED AREA WITHIN LIMITS.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 25,326 hrs · 23,121 cycles

CHAFE (OUT OF LIMITS) ON RT INBD FLAP VANE L/E ON INBD END OF FLAP VANE L/E. REMOVED DAMAGED L/E SEGMENT (PN 601R14303-53) AND REPLACED WITH SERVICEABLE L/E SEGMENT.

Part: SKIN — DAMAGED (LT WING) · airframe 25,326 hrs · 23,121 cycles

LT OTBD L/E HAS DAMAGED SCREW HOLE FROM SCREW REMOVED ON INBD LOWER SIDE. REPAIRED DAMAGED SCREW HOLE FROM SCREW REMOVED ON LT OTBD L/E IAW REO 601R-57-41-760 AND REO 601R-41-761.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 25,326 hrs · 23,121 cycles

LT INBD FLAP DENTED NEAR PANEL 584AB. REPAIR IAW REO 601R57-52-1720.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 25,326 hrs · 23,121 cycles

TIE DOWN TRACKS IN CARGO COMPARTMENT. HAVE CORROSION LBL 27 FWD, LBL 9 FWD, RBL9 AFT, RBL9 FWD AND RBL 27. R & R TIE DOWN TRACKS IAW SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 25,326 hrs · 23,121 cycles

FLOOR SUPPORT CAP NUT PLATE HOLES HAVE CORROSION OTBD LBL 27, FS 559.0+112 TO FS 621.0. R & R FLOOR SUPPORT CAP IAW REO 601R-53-00-0005, SRM 51-24-36 & 51-40-11.

Part: SKIN — DENTED (BS 200) · airframe 25,326 hrs · 23,121 cycles

DENT IN FUSELAGE BELOW RT 1 STRAP AFT OF RVSM AREA AT FS 200.00. REPAIRED DENT DAMAGE ON FS 200 BELOW RT 1 STRAP AFT OF RVSM AREA.

Part: SKIN — DAMAGED (LT WING) · airframe 25,326 hrs · 23,121 cycles

(REPAIRED LT WINGLET STRIKE DAMAGE) COMPLIED PERMANENT REPAIR WITH REO 601R-57-31-1108 AT LT WINGLET.

Part: SKIN — DAMAGED (BS 200) · airframe 25,326 hrs · 23,121 cycles

DENT IN FUSELAGE BELOW RT 1 STRAP AFT OF RVSM AREA AT FS 200.00. REPAIRED DENT DAMAGE ON FS 200 BELOW RT 1 STRAP AFT OF RVSM AREAS.

Part: FLOORBEAM — CRACKED (BS 280) · corrosion level 1 · airframe 25,326 hrs · 23,121 cycles

FS 280, FLOORBEAM CRACKED AT LBL9 CUT OUT DAMAGED AREA AND PERFORMED REPAIR IAW REO 601R-53-11-171, REV 1.

Part: SKIN — DAMAGED (LT WING TE FLAP)

LT OTBD FLAP T/E 601R-57-53-722A. REPAIRED LT OTBD FLAP T/E BY REMOVING AND REPLACING THE OTBD T/E WEDGE AND BY CUTTING OUT DAMAGED LOWER CORNER SKIN INSTALLED FILLER AND DOUBLER TO CUTOUT AREA. IAW SRM 57-53-00, REPAIR NR 3 SRM 51-42-06.

Part: ACTUATOR — WORN (RT WING TE FLAP) · airframe 25,326 hrs · 23,121 cycles

RT INBD FLAP OTBD FLAP VANE ACTUATOR TUBE ASSY WORN. REPAIRED RT INBD FLAP OTBD FLAP VANE ACTUATOR IAW REO 601R-57-52-1714.

Part: VANE — WORN (LT WING TE FLAP) · airframe 25,326 hrs · 23,121 cycles

LT INBD FLAP VANE INBD CTR, OTBD ACTUATORS CARRIAGE ASSY ARE WORN AND SPRINGS ARE CORRODED. REPAIRED LT INBD FLAP VANE INBD CTR, OTBD ACTUATORS IAW REO 601R-57-52-1713.

Part: TUBE — DAMAGED (LT FLAP ACTUATOR) · airframe 25,326 hrs · 23,121 cycles

LT INBD FLAP VANE INBD CENTER, OTBD ACTUATORS, CARRIAGE ASSY ARE WORN AND SPRINGS ARE CORRODED. REPAIRED LT INBD FLAP VANE INBD CENTER, OTBD ACTUATORS IAW REO 601R-57-52-1713.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 25,326 hrs · 23,121 cycles

RBL 9 INBD CLIP CRACKED. REMOVED UNSERVICEABLE CLIP, FABRICATED AND INSTALLED SERVICEABLE CLIP IAW REO 601R-53-11-171, REV D.

Part: ACTUATOR — WORN (RT WING TE FLAP) · airframe 25,326 hrs · 23,121 cycles

RT INBD FLAP INBD FLAP VANE ACTUATOR TUBE ASSY WORN. REPAIRED RT INBD FLAP INBD FLAP VANE ACTUATOR IAW REO 601R-57-52-1714.

Part: ACTUATOR — WORN (RT WING TE FLAP) · airframe 25,326 hrs · 23,121 cycles

RT INBD FLAP CTR FLAP VANE ACTUATOR TUBE ASSY WORN. REPAIRED INBD FLAP CTR FLAP VANE ACTUATOR IAW REO 601R-57-52-1714.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 25,326 hrs · 23,121 cycles

FS 280, LBL9 INBD AND OTBD CLIPS CRACKED. REMOVED UNSERVICEABLE CLIPS AT LBL AND RBL 9 OF FS280 AND REPLACED WITH SERVICEABLE INBD AND OTBD CLIPS IAW REO 601R-53-11-171, REV 1.

Part: TUBE — WORN (RT FLAP ACTUATOR) · airframe 23,121 hrs

RT INBD FLAP CENTER FAP VANE ACTUATOR TUBE ASSY WORN. REPAIRED INBD FLAP CENTER FLAP VANE ACTUATOR IAW REO 601R-57-52-1714.

Part: TUBE — WORN (RT FLAP ACTUATOR) · airframe 25,326 hrs · 23,121 cycles

RT INBD FLAP OTBD FLAP VANE ACTUATOR TUBE ASSY WORN. REPAIRED RT INBD FLAP OTBD FLAP VANE ACTUATOR IAW REO 601R-57-52-1714.

Part: ATTACH FITTING — CRACKED (PAX DOOR) · airframe 25,326 hrs · 23,121 cycles

UPPER CABLE ATTACHMENT POINT OF PAX DOOR SUPPORT WHEEL SYSTEM IS CRACKED. REMOVED CRACKED PAX DOOR WHEEL CABLE SUPPORT FITTING AND INSTALLED NEW SUPPORT FITTING IAW SRM 51-42-06, 51-40-11.

Part: POST — CRACKED (BS 409) · airframe 25,326 hrs · 23,121 cycles

VERTICAL POST AT 409+128, RBL 18 OTBD IS CRACKED AT BOTTOM END. REPAIRED RBL 18, OTBD POST AT FS 469+128 IAW REO`S 601R-53-41-056, REV E, & REO 601R-53-41-1417.

Part: BULKHEAD — CHAFED (BS 621) · airframe 25,326 hrs · 23,121 cycles

CHAFING ON CENTER VERTICAL STIFFENER OF REAR BULKHEAD BEHIND 10TH STAGE VALVE. REPAIRED DAMAGED AREA ON CENTER VERTICAL STIFFENER OF BULKHEAD IAW REO 601R-53-61-1523.

Part: STIFFENER — CHAFED (BS 621 BULKHEAD) · airframe 25,326 hrs · 23,121 cycles

CHAFING ON CTR VERTICAL STIFFENER OF REAR BULKHEAD BEHIND 10 STAGE VALVE. REPAIRED DAMAGE AREA ON CTR VERTICAL STIFFENER OF BULKHEAD IAW REO 601R-53-61-1523.

Part: SUPPORT BRACKET — CRACKED (BS 718) · airframe 25,326 hrs · 23,121 cycles

H2 HYD MANIFOLD SUPPORT BRACKET CRACKED IN LOWER RADIUS. REPAIRED IAW REO 601R-53-62-031.

Part: POST — CRACKED (BS409) · airframe 25,326 hrs · 23,121 cycles

VERTICAL POST AT FS 409.00+128, LBL 27.00 INBD IS CRACKED AT BOTTOM END. REPAIRED FS 409.00+128, LBL 27.00, INBD VERTICAL POST IAW REO 601R-53-41-056, REV E & REO 601R-53-41-1417.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 25,326 hrs · 23,121 cycles

LT INBD FLAP VANE L/E CHAFED. BLENDED INBD FLAP VANE L/E AT INBD LOCATION, WITHIN ALLOWABLE LIMITS IAW REO 601R-57-52-004, REV C.

Part: SKIN — CHAFED (RT AILERON) · airframe 25,326 hrs · 23,121 cycles

RT AILERON UPPER FIXED L/E CHAFED. SMOOTHED AREA IAW REO 601R-57-60-013, REV NC FOUND WITHIN LIMITS IAW REO NDI WITH NO DEFECTS NOTED, TREATED, PRIMED TOP COATED IAW SRM 51-21-11/SRM 51-25-06/ SRM 51-25-16.

Part: FLOORBEAM — CORRODED (BS 349) · corrosion level 2 · airframe 25,326 hrs · 23,121 cycles

FS 349 FRAME CAP CORRODED OTBD OF RBL 27 AT LIGHTING PROTECTION PANEL CLIP. FLOOR SUPPORT ANGLE DETERMINED TO BE OUT OF LIMITS, FABRICATED AND INSTALLED NEW SUPPORT ANGLE IAW SRM 51-11-20, 51-24-16, 51-42-06.

Part: POST — CRACKED (BS 409 LBL18) · airframe 25,326 hrs · 23,121 cycles

VERTICAL POST AT FS 409.0+128, LBL 18.0 OTBD IS CRACKD AT BOTTOM END. REPAIRED VERTICAL POST AT FS 409.0+128, LBL 18.0 OTBD CRACK AT BOTTOM END BY FULLY INCORPORATING REPAIR SHOWN IN VIEW CC OF REO 601R-53-41-056, REV E 6/28/06 AND REO 601R-53-41-1417 REV - 5/14/11.

Part: FLOORBEAM — CRACKED (BS409) · airframe 25,326 hrs · 23,121 cycles

FLOORBEAM ANGLE IS CRACKED AT FS 409.00+112 AND LBL 27.0. R & R BRACKET AT FS 409.112, LBL 27.0 INBD SIDE IAW SRM 51-42-06.

Part: SKIN — CRACKED (LT WING) · airframe 25,326 hrs · 23,121 cycles

AFT SKIN OF LEFT L/E 520JL IS CRACKED AT A FASTENER HOLE FOR ACCESS PANEL 520AS. R & R LT INBD L/E 520JL SHROUD BETWEEN W/S 86.45 & 96.34 IAW SRM 51-42-13.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 25,326 hrs · 23,121 cycles

FS 484, RBL 36 CLIP IS CRACKED. REMOVED UNSERVICEABLE CLIP AND REPLACED WITH SERVICEABLE CLIP IAW REO 601R-53-41-059.

Part: SKIN — CRACKED (LT WING) · airframe 25,326 hrs · 23,121 cycles

AFT SKIN OF LT L/E 520JL IS CRACKED AT FASTENER HOLE FOR ACCESS PANEL 520AS. R & R LT INBD L/E 520JL SHROUD BETWEEN W/S 86.45 AND 96.34 IAW SRM 51-42-13.

Part: PANEL — CHAFED (PAX DOOR) · airframe 25,326 hrs · 23,121 cycles

PANEL 832, HAS PITTING AND CHAFING AND IS DENTED. REPAIR DAMAGE ON PANEL 832 IAW SRM 51-12-00.

Part: FILLER — WORN (RT MLG DOOR) · airframe 25,326 hrs · 23,121 cycles

INSIDE FILLERS WORN BEYOND LIMITS ON RT MLG DOOR ON FWD EDGE. REMOVED UNSERVICEABLE FILLERS FABRICATED SERVICEABLE FILLERS IAW REO 601R-52-82-034 AND REINSTALLED.

Part: PANEL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 25,326 hrs · 23,121 cycles

PANEL 832AT HAS PITTING AND CHAFING AND IS CRACKED. REPAIRED DAMAGE ON PANEL 832AT, IAW SRM 51-12-00H.

Part: SKIN — CHAFED (LT AILERON) · airframe 25,326 hrs · 23,121 cycles

LT AILERON UPPER FIXED L/E HAS CHAFE DAMAGE. REPAIRED LT AILERON UPPER L/E IAW SRM 51-12-00, 57-60-00.

Part: SKIN — CHAFED (LT AILERON) · airframe 25,326 hrs · 23,121 cycles

LT AILERON UPPER FIXED L/E HAS CHAFE DAMAGE. REPAIRED LT AILERON UPPER L/E IAW SRM51-12-00, 57-60-00.

Part: TRACK — GOUGED (CARGO DOOR) · airframe 25,326 hrs · 23,121 cycles

CARGO DOOR AFT TRACK IS GOUGED AND BENT. REPAIRED CARGO DOOR AFT TRACK IAW REO 601R-53-62-024.

Part: SKIN — UNKNOWN (PAX DOOR) · airframe 25,326 hrs · 23,121 cycles

PAX DOOR CUT OUT 601R-53-21-1207. REPAIRED FUSELAGE SKIN AT FS 310.00, STR 16L IAW REO 601R-53-21-180, REV A.

Part: BULKHEAD — CHAFED (BS 280) · airframe 25,326 hrs · 23,121 cycles

RT AFT 280 BULKHEAD SKIN GOUGED. CUT OUT DAMAGED AREA AND FABRICATED 1 DOUBLER AND 2 FILLERS IAW REO 601R-53-11-1727.

Part: BULKHEAD — GOUGED (BS 280) · airframe 25,326 hrs · 23,121 cycles

RT AFT 280 BULKHEAD SKIN GOUGED. CUT OUT DAMAGED AREA AND FABRICATED 1 DOUBLER AND 2 FILLERS IAW REO 601R-53-11-1727.

Part: SKIN — CORRODED (LT WING) · airframe 25,326 hrs · 23,121 cycles

FUEL PANEL WING PLANK ACCESS HOLE AT 540BB HAS FRETTING CORROSION. REPAIRED IAW AWACS E06/021 REV A & REO 601R-57-21-030, REV H OUTSIDE OF CRITICAL AREA.

Part: DOOR — BINDING (SERVICE) · airframe 24,918 hrs · 22,707 cycles

SERVICE DOOR WOULD NOT OPEN OR CLOSE, STUCK HALF OPEN. R & R SERVICE DOOR HSG ASSY AND DOOR SEAL, ALL WORK DONE ON W/O 16056. ALL OPS CK GOOD.

Part: ANGLE — CRACKED (BS 621) · airframe 23,945 hrs · 21,691 cycles

FS 621 CARGO DOOR FWD TRACK REINFORCEMENT BEAM, AFT LOWER ATTACHMENT ANGLE THAT CONNECTS BEAM TO FS621 BULKHEAD HAS 2 EA CRACKS. REMOVED CRACKED ANGLE AT CARTGO DOOR FWD TRACK REINFORCEMENT BEAM, AFT LWR ATTACHMENT AND INSTALLED NEW ANGLE IAW SRM 51-24-21 & 51-42-21.

Part: ANGLE — CRACKED (BS 559) · airframe 23,945 hrs · 21,691 cycles

LBL 18 CAP ANGLE CRACKED FROM BOTTOM RIVET TO EDGE AND RBL 9, WL 58.7 HAS CRACK INDICATION. REPAIRED LBL18 CAP ANGLE & RBL 9, WL 58.7. CRACKED BY FULL INCORPORATION OF REO 601R-53-41-260, REV E & 601R-53-41-609, REV B DEVIATION E ON FS 559 BULKHEAD LT & RT SIDES, LBL 27 TO RBL 27A.

Part: TUBE — CORRODED (CARGO DOOR LATCH) · corrosion level 2 · airframe 21,074 hrs · 18,812 cycles

INTERNAL CARGO DOOR LATCHING MECHANISM, FWD TUBE ASSY CORRODED. INTERNAL CARGO DOOR LATCHING MECHANISM. FWD TUBE ASSY REPLACED IAW AMM 52-31-02-420-004. (K)

Part: CARGO TRACK — CORRODED (BS 574) · airframe 21,074 hrs · 18,812 cycles

RAILS IN CARGO COMPARTMENT AT FS 574, LBL 9 AND RBL 9 ARE CORRODED BEYOND SRM LIMITS. RAILS IN CARGO COMPARTMENT AT FS 574, LBL 9 AND RBL 9 REPLACED IAW SRM 51-41-04. (K)

Part: COVER — CRACKED (PAX DOOR) · airframe 21,074 hrs · 18,812 cycles

PAX DOOR AFT UPPER CORNER COVER CRACKED. PAX DOOR AFT UPPER CORNER COVER REPLACED IAW SRM 51-42-13. (K)

Part: PRESSURE BLKHD — CRACKED (BS 621) · airframe 21,074 hrs · 18,812 cycles

REAR PRESSURE BULKHEAD AFT SIDE LT AND RT MIDDLE ANGLES CRACKED FS 621.00 REAR PRESSURE BULKHEAD AFT SIDE LT AND RT MIDDLE ANGLES REPAIRED IAW REO 601R-53-61-100, REV A AND REO 601R-53-61-422. (K)

Part: ACCESS DOOR — DAMAGED (FUSELAGE) · airframe 21,074 hrs · 18,812 cycles

QTY 5 HOLES IN THE FWD ACCESS PANEL DOOR 131AL SURROUND DOUBLER ARE ELONGATED. QTY 5 HOLES IN THE FWD ACCESS PANEL DOOR 131AL SURROUND DOUBLER REPAIRED IAW REO 601R-53-11-162, REV B. (K)

Part: FLOORBEAM — CORRODED (BS 461) · airframe 21,074 hrs · 18,812 cycles

PRESSUE FLOOR SUPPORT STRUCTURE, SUPPORT FITTING CRACKED AT FS 461, RBL 9. PRESSURE FLOOR SUPPORT STRUCTURE, SUPPORT FITTING REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 21,074 hrs · 18,812 cycles

PAX DOOR AFT EDGE MEMBER CRACKED. PAX DOOR AFT EDGE MEMBER IAW REO 601R-52-11-279. (K)

Part: DOOR FRAME — CRACKED (BS 589-605) · airframe 21,074 hrs · 18,812 cycles

CARGO DOOR SURROUND LANDING PLATE IS CRACKED AT FS 589 AND FS 605. CARGO DOOR SURROUND LANDING PLATE AT FS 589 AND FS 605 REPAIRED IAW REO 601R-53-61-433. (K)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 21,074 hrs · 18,812 cycles

CLIP CRACKED AT FS 484.00 AND LBL 27.00 UNDER FLOOR. CLIP AT FS 484.00 AND LBL 27.00 UNDER FLOOR REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)

Part: ANGLE — CRACKED (BS 484) · airframe 21,074 hrs · 18,812 cycles

EXISTING REPAIR ANGLE CRACKED AT FS 484.00 AND LBL 36.00. EXISTING REPAIR ANGLE AT FS 484.00, LBL 36.00. REPLACED IAW REO 601R-53-41-059, REV A. (K)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 21,074 hrs · 18,812 cycles

CLIP CRACKED AT FS 484.00 AND RBL 27.00 UNDER FLOOR CLIP REPLACED AT FS 484.00 AND RBL 27.00 UNDER FLOOR IAW SRM 51-42-06 AND 51-42-21. (K)

Part: PROCESSOR — MALFUNCTIONED (POS 2) · airframe 20,929 hrs · 18,668 cycles

TOTAL ERRONEOUS FLIGHT DIRECTOR READING AND NAV INDICATION ON ILS 9R. BOTH FD`S PROVIDED COMMANDS TO DIVE ACFT TO GROUND. DISCONNECTED FD AND AP AND LANDED NORMALLY. GLIDESLOPE W/N CAPTURE ON FO`S SIDE. REMOVED AND REPLACED FO`S DCP IAW AMM 34-25-04 PERFORMED FUNCTIONAL TEST AND LOCALIZER AND GLIDESLOPE IAW AMM 34-51-00. REMOVED AND REPLACED FMC CARDS NR 1 AND NR 2 IN ORDER TO ACCOMPLISH MOD IAW AMM 22-11-00. A/P AND ILS OPS CHECK GOOD AT THIS TIME. (K)

Part: PRESSURE BLKHD — CRACKED (BS 621) · airframe 20,633 hrs · 18,427 cycles

MFG 135153-10-AFT PRESSURE BULKHD CRACKED AT FS 621.00 LT LINTEL ASSY AREA. AFT PRESSURE BULKHEAD AT FS 621.00 LT REPAIRED IAW REO 601R-61-1230 REV. D. (K)

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 19,723 hrs · 17,522 cycles

AFTER TAKEOFF FROM WET RUNWAY, CLIMBED TO FL320 IN RAIN/SNOW. TEMP -48`C IN CRUISE. WHILE MAKING LT TURN, WITH AP, RECEIVED LT WING DOWN AUTOPILOT TRIM CAUTION MSG MOMENTARILY. PERFORMED VISUAL INSP AILERON SYS FROM BULKHEAD TO AILERONS WHILE OPERATING THE SYS. FOUND NO OBSTRUCTION. ALL PULLEYS AND QUADRANTS, OPS NORMAL. INSP FLUTTER.

Part: COALESCER BAG — ODOR (CABIN AIR) · airframe 19,021 hrs · 16,852 cycles

LT PACK AIR HAS AN ODOR OF OIL/ RUBBER. CLEANED LT COALESCER IAW AMM 21-51-13 PERFORMED OPS CK OF LT ACM IAW AMM 21-51-00. NO DEFECT NOTED, NO ODOR DETECTED. (K)

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 17,918 hrs · 15,813 cycles

OUTBOARD GROUND SPOILER FAULT MESSAGE AND SPOILERON FAULT MESSAGE IN FLIGHT. AFTER LANDING ONLY OUTBOARD GROUND SPOILER MESSAGE EVIDENT. PERFORMED RESET PER FIM PROCEDURE. MESSAGE CLEARED. FLIGHT CREW PERFORMED INITIAL RESET. PROBLEM CLEARED LOCAL MAINTENANCE NOTED NO MESSAGE. AIRCRAFT RELEASED. (M)

Part: SWITCH — ARCED (LAVATORY SIGN)

ORDINANCE SIGN CIRCUIT BREAKER POPPED. LAV OCCUPIED MICROSWITCH HAD SIGNS OF ELECTRICAL ARCING. REMOVED AND REPLACED LAV OCCUPIED SWITCH PER AMM 33-25-11. OPS CHECK GOOD. REMOVED PLACARD, REMOVED FROM MEL. (M)

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 16,195 hrs · 14,176 cycles

RT WING PLANK ACCESS HOLE R 2 (610AB) WS 12.245 HAS PITTING ALONG FWD HALF OF HOLE, APPROX .007 DEEP LOCATED IN CRITICAL AREA. (K) MAINTENANCE REMOVED MINOR PITTING, NDT, ROTO-PEENED AND TREATED AREA. (M)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 16,195 hrs · 14,176 cycles

LT WING PLANK ACCESS HOLE NR 2, (510AB) WS 12.245 HAS PITTING AT IB AND OB ENDS APPROX .005 INCH DEEP LOCATED IN NON-CRITICAL AREA. (K) MAINTENANCE REMOVED PITTING, NDT, ROTO-PEENED AND PROTECTIVE TREATED. (M)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 16,195 hrs · 14,176 cycles

LT WING PLANK ACCESS HOLE NR 11, (550CB) WS 209.040 HAS PITTING ON IB AND OB ENDS APPROX .005 INCH DEEP LOCATED IN NON CRITICAL AREA. (K) MAINTENANCE REMOVED PITTING, NDT, ROTO PEENED AND PROTECTED TREATED AREA. (M)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 16,195 hrs · 14,176 cycles

LT WING PLANK ACCESS HOLE NR 1, (540BB) WS 54.897 HAS PITTING ON IB END ON NON CRITICAL AREA APPROX .002 INCH DEEP, AND ALONG AFT EDGE IN CRITICAL AREA APPROX .005 INCH DEEP. (K) MAINTENANCE REMOVED MINOR PITTING, NDT, ROTO PEENED AND PROTECTIVE TREAT NR 1 ACCESS HOLE. (M)

Part: INTERCOSTAL — DAMAGED (BS 461)

TOP RIVET IS MISSING FROM INTERCOSTAL FLANGE AT FS 461, LBL 9. MAINTENANCE INSTALLED RIVET IAW CRJ SRM 51-45-06. (M)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 16,195 hrs · 14,176 cycles

INTERCOSTAL FLANGE AT FS 484.00, LBL 9.0, IS CRACKED NEAR RADIUS APPROX .20 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED INTERCOSTAL FLANGE AT FS 484 LBL 9 IAW BSC STANDARD REPAIR 601R-53-0029B AND SRM 51-42-21. (M)

Part: CHANNEL — CRACKED (BS 527) · airframe 16,195 hrs · 14,176 cycles

CHANNEL (PN 601R75262-157) IN RT MLG WHEEL WELL IS CRACKED APPROX .5 LONG. (K) MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED A NEW BRACKET P/N 601R75262-157 IAW CRJ SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 16,195 hrs · 14,176 cycles

INTERCOSTAL FLANGE AT FS 484.00, RBL 9.0, IS CRACKED NEAR RADIUS APPROX .15 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED INTERCOSTAL FLANGE AT FS 484 RBL 9 IAW BSC STANDARD REPAIR 601R-53-0029B AND CRJ200 SRM 51-42-21. (M)

Part: CHANNEL — CRACKED (BS 527) · airframe 16,195 hrs · 14,176 cycles

CHANNEL (PN 601R75262-159) IN LT MLG WHEEL WELL CRACKED. (K) MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED A NEW BRACKET, P/N 601R75262-159 IAW CRJ SRM 51-42-06. (M)

Part: ANGLE — CRACKED (BS 520) · airframe 16,195 hrs · 14,176 cycles

Z-ANGLE (PN 601R75262-153) IN RT MLG WHEEL WELL IS CRACKED. (K) MAINTENANCE INSTALLED SERVICEABLE ANGLE P/N 601R75262-153 IAW CRJ 200 SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (FS 621)

RIGHT FS 621 TO 625 OBLIQUE ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601-35012-52 IAW CRJ SRM 51-42-06. (M)

Part: ANGLE — CRACKED (BS 621-625 S14) · airframe 16,195 hrs · 14,176 cycles

LT FS 621.00 TO 625.00 OBLIQUE ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. (K) MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED A NEW ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-06. (M)

Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 15,521 hrs · 13,520 cycles

AFTER ROTATION, NOTICED ODOR LIKE (BURNED TOAST) IN COCKPIT. FLIGHT ATTENDANT REPORTED SIMILAR ODOR IN CABIN, STRONGER TOWARDS THE REAR OF THE CABIN. BOTH PACKS OPERATING ON APU. TRANSFERRED TO ENGINE BLEEDS, SMELL DISSIPATED. NO VISIBLE SMOKE SEEN. OPS CHECK PACKS WITH APU AND ENGINES IAW AMM 21-40 AND 21-50. OPERATED HOT AND COLD, NO ABNORMAL ODOR NOTED IN CABIN OR FLIGHT DECK. (K)

Part: ANGLE — CRACKED (LT FS 280) · airframe 11,225 hrs · 9,473 cycles

LT FS 280.00 AT LBL 9 IB CLIP ANGLE IS CRACKED .5 INCH LONG. REPLACED CLIP IAW SRM. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 11,225 hrs · 9,473 cycles

LT SIDE FS 484 INTERCOSTAL IS CRACKED AT LBL 36. CRACK IS APPROX 1.1 INCH LONG. REPAIRED LT SIDE FS 484 INTERCOSTAL AT LBL 36 IAW MFGREO. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 9,473 hrs · 9,469 cycles

RT FS 280 AT RBL 9 IB CLIP ANGLE IS CRACKED .5 INCH LONG. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 11,225 hrs · 9,473 cycles

RT FS 280 AT RBL 9 IB CLIP ANGLE IS CRACKED .5 INCH LONG. REPLACED CLIP IAW SRM. (K)

Part: INTERCOSTAL — CRACKED (RT FS 484) · airframe 11,225 hrs · 9,473 cycles

RT SIDE FS 484 INTERCOSTAL IS CRACKED AT RBL 36. CRACK IS APPROX 0.4 INCH LONG. REPAIRED RT SIDE FS 484 INTERCOSTAL IAW MFG REO. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 11,225 hrs · 9,473 cycles

LT FS 280 AT LBL 9 IB CLIP ANGLE IS CRACKED .5 INCH LONG. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 11,225 hrs · 9,473 cycles

LT FS 280 AT LBL 9 OB CLIP ANGLE IS CRACKED .5 INCH LONG. REPLACED CLIP IAW SRM. (K)

Part: STRINGER CLIP — CRACKED (RT FS280)

RT FS 280 AT RBL 9, OB CLIP ANGLE IS CRACKED .5 INCH LONG. REPLACED CLIP IAW SRM. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 11,225 hrs · 9,473 cycles

RT FS 280 AT RBL 9 OB CLIP ANGLE IS CRACKED .5 INCH LONG. (K)

Part: STRUT — UNDERSERVICED (NLG)

NLG WOULD NOT RETRACT ON DEPARTURE. CYCLED GEAR AND COMPLIED WITH QRH. GEAR DISAGREE RED CAS. AMBER NWS CAS AND AMBER WOW INPUT CAS. SERVICED NLG STRUT IAW AMM 32-21-30. OPS GOOD IAW 32-33-00. (M)

Part: CONTROLLER — MALFUNCTIONED (AIR DATA HEAT)

INTERMITTENT RIGHT STATIC HEAT, TAT PROBE HEAT, RT AOA HEAT, RT PITOT HEAT MESSAGE INFLIGHT ONLY. REMOVED AND REPLACED AIR DATA HEAT CONTROLLER IAW AMM 30-31-15. OPS CHECK GOOD. (M)

Part: WARNING LIGHT — ILLUMINATED (APU OIL TEMP)

APU OIL TEMP CAUTION MESSAGE, DIVERTED TO ATL REF IDG NR 1 ON MEL. INTERROGATED ECU, TROUBLESHOT SYSTEM, REMOVED AND REPLACED HOT OIL TEMPERATURE SENSOR IAW AMM 49-91-25. RAN APU 15 MINUTES WITH LOADS APPLIED. NO DEFECTS NOTED, LEAK CHECK GOOD. (M)

Part: ANGLE — CRACKED (FUSELAGE)

REINFORCEMENT ANGLES, P/N 601-36001-29/30 FOUND CRACKED. REINFORCEMENT ANGLES, P/N 601-36001-29/30. REPLACED DURING INCORPORATION OF SERVICE BULLETING 601R-53-061. (M)

Part: SKIN — CRACKED (FUSELAGE)

FOUND FS 640 LT SIDE BETWEEN STRINGER 9 AND STRINGER 17 CRACK ON DOUBLER. INSPECTED AND REPAIRED DOUBLER AS BOMBARDIER SB 601R-53-061. (M)

Part: SKIN — CRACKED (FUSELAGE)

FOUND RIGHT FS 64 BETWEEN STRINGER 9 AND STRINGER 12 ON AFT SIDE OF FRAME CRACK FOUND ON SKIN DOUBLER. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND RIGHT FS 640 BETWEEN STRINGER 9 AND STRINGER 12 ON AFT SIDE OF FRAME CRACKED AT SKIN DOUBLER. RIGHT REINFORCEMENT ANGLE REPLACED WHILE INCORPORATING SB 601R-53-061 REV E. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND LT FS 625 OBLIQUE ANGLE P/N 601-35012-51 IS CRACKED. (M)

Part: VANE — CHAFED (TE FLAP)

RIGHT INBOARD FLAP VANE LEADING EDGE IS CHAFED 3 PLACES, WS 56.177= .004 INCH DEEP, WS 104.429= .003 INCH DEEP AND WS 140.364 = .003 INCH DEEP. BLENDED DAMAGE AREAS, RESTORE FINISH AND APPLIED TEFLON FILLED ABRASION RESISTANT COATING IAW BOMBARDIER, INC REO 601R-57-52-004 REV B. (M)

Part: SUPPORT — CRACKED (SUBFLOOR)

THE LEFT AND RIGHT SIDE UNDERFLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621, WL 73, LBL 40. REPAIRED LEFT AND RIGHT UNDERFLOOR SUPPORT STRUCTURE IAW BOMBARDIER, INC REO 601R-53-61-117 REV B. (M)

Part: WARNING LIGHT — FALSE INDICATION (LT ENG OVRHT)

BLEED AIR DUCT MASTER WARNING ILLUMINATED ON TAKEOFF REMAINS ON EVEN AFTER LEFT ENGINE SHUTDOWN PER QRH COMPLIED WITH 14TH STAGE DUCT LEAK CHECK. NO LEAKS. OHMED OVERHEAT ELEMENTS. ALL CHECK GOOD. COMPLIED WITH CHECK FLIGHT, NO DEFECTS NOTED. (M)

Part: LINE — LEAKING (HYD SYSTEM) · airframe 5,881 hrs · 4,833 cycles

HYD NR 2 LOW PSI CAS MESSAGE. NR 2 HYD FLUID INDICATES ZERO. REMOVED AND REPLACED NR 2 HYD RETURN LINE. REMOVED AND REPLACED NR 2 HYD PSI LINE. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYD PUMP.

Part: SHUTOFF VALVE — FAILED (RT ENGINE)

RIGHT COWL ANTI-ICE CASS RECEIVED INFLIGHT, COMPLIED WITH QRH PROCEDURES, MESSAGE REMAINS. REMOVED AND REPLACED RIGHT ENGINE PRESSURE RELIEF SHUTOFF VALVE. (M)

Part: IDG — LACK OF LUBE (NR 2)

IDG NR 2 CAS MESSAGE DURING TAKEOFF POWER APPLICATION SERVICED NR 2 IDG WITH OIL. NO LEAKS NOTED. (M)

Part: COFFEEMAKER — DEFECTIVE (GALLEY)

EXPLOSION NEAR RIGHT COFFEE MAKER AND FILLED AREA WITH WHITE POWDER. MAINTENANCE INSPECTED COFFEE MAKER AND FOUND WATER RESERVOIR HEATING ELEMENT SHORTED AND DETACHED. MAINTENANCE REMOVED AND REPLACED COFFEE MAKER. (M)

Part: THRUST REVERSER — CRACKED (NR 2 ENGINE) · airframe 3,700 hrs · 3,081 cycles

NR 1 ENGINE THRUST REVERSER UPPER CASCADE IS CRACKED. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER UPPER CASCADE.

Part: THRUST REVERSER — CRACKED (NR 2 ENGINE) · airframe 3,700 hrs · 3,081 cycles

NR 2 ENGINE THRUST REVERSER UPPER CASCADE IS CRACKED. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE THRUST REVERSER UPPER CASCADE.

Part: FAIRING — CRACKED (THRUST REVERSER) · airframe 3,700 hrs · 3,081 cycles

NR 2 ENGINE UPPER STANG FAIRING CRACKED MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE UPPER STANG FAIRING.

Part: FAIRING — CRACKED (THRUST REVERSER) · airframe 3,700 hrs · 3,081 cycles

NR 1 ENGINE UPPER STANG FAIRING CRACKED MAINTENANCE REMOVED AND REPLACED UPPER STANG FAIRING.

Part: PSEU — FAULTY (MLG)

ANTI-SKID IB AMBER CAS MESSAGE AND PARK BRAKE SOV AMBER CAS UPON GEAR RETRACTION. GEAR DID NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE PSEU, OPERATED GEAR SEVERAL TIMES. OPS CHECKED GOOD. (M)

Part: COWL DOOR — SEPARATED (RT ENGINE) · airframe 489 hrs · 452 cycles

LOWER ENGINE COWL DOOR (RT) FELL OFF ON LANDING. MAINTENANCE REPLACED THE RT ENGINE LOWER COWL DOOR.