N471ZW

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 41,115 hrs · 43,287 cycles

REQUEST INSPECTION FOR F/O'S WINDSHIELD CRACKS. INSPECTED AND FOUND F/O WINDSHIELD TO BE OUT OF LIMITS IAW AWAC SUPP 14-201D REQUIRES REPLACEMENT. AIRCRAFT REMOVED FROM SERVICE.

Part: ADC — FAULTED (NR 2) · airframe 41,082 hrs · 43,258 cycles

AT 28000 FT DURING DECENT F/O AIRSPEED DECREASING AND EFIS COMP MON IAS CAUTION PRESENT AT 16000 FT F/O AIRSPEED RETURNED TO NORMAL. REMOVED AND REPLACED #2 ADC. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME

Part: IDG — FAULTED (LEFT) · airframe 41,007 hrs · 43,187 cycles

ON CLIMB OUT REC'V GEN 1 OFF CAUTION MESSAGE. C/W QRH MESSAGE DISAPPEARED. REMAINED EXTINGUISHED REST OF FLIGHT. ***** AIRCRAFT REMOVED FROM SERVICE ***** R/R #1 IDG ASSEMBLY IAW AMM 24-11-01 REF 370816-4 FOR REQ LEAK AND OPS CHECK. SERVICED IDG IAW AMM SUP 17-086

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 39,837 hrs · 41,843 cycles

SMOKE TOILET CAU MSG IN FLT NO FIRE OR SMOKE PRESET IN LAV CAU PERSISTED C/W QRH MSG PERSITED UNTIL LANDING. NO ONE IN LAV WHEN MSG APPEARED. NO OVERWEIGHT LDG. AIRCRAFT REMOVED FROM SERVICE. R/R LAV SMOKE DETECTOR PER AMM 26-16-01 OPS CHECK GOOD AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,681 hrs · 41,660 cycles

DURING TAKE-OFF ROLL, RECEIVED IDG 2 DISC CAUTION FOLLOWED BY YD 2 INOP STATUS MESSAGE AND CONFIG SPLRS WARNING MESSAGE FOLLOWED BY GEN 2 OFF CAUTION MESSAGE. ABORTED TAKE-OFF AT 56 KNOTS. ALL BRAKE TEMPS BELOW 5, BTMS REMAINED GREEN. *******AIRCRAFT REMOVED FROM SERVICE******** INSPECTED AND FOUND OVERFLOW DRAIN CAP LEFT OFF ON IDG #2 NO OIL IN IDG TS PER FIM 24-10-00. IDG 2 DISCONNECT. SERVICED IDG #2 IN REF AWAC SUP 16-364A. NO LEAKS NOTED.OPS CHECK OF THE RIGHT IDG GOOD AT THIS TIME EF AMM 24-11-01. PERFORMED OPS CHECK OF THE YAW DAMP PANEL IN REF AMM 22-22-01. OPS CHECK GOOD. OPS CHECK SPLRS FEF AMM 27-61-00 OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,333 hrs · 39,307 cycles

AFTER GEAR RETRACTION RECIEVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MSGS. C/W QRH MSGS CLEARED. ****AIRCRAFT REMOVED FROM SERVICE*********** INSP AND FOUND NLG PROX SW DMG'ED. PULLED CODE S23 NGOEXT. OPS CHECKED NLG DOOR IAW AMM 32-22-01. OPS CK GOOD. C/W M ACTION OF MEL 32-30-01. REF 363274-2 FOR MEL. REPLACED THE WOFFW NO. 2 AND CENTERED HARNESS ASSEMBLY PER AWA SUPP 12-029E, OPS CHECK GOOD. REMOVED PLACARD AND MEL.

Part: BRACKET — CORRODED (RH WING) · corrosion level 2 · airframe 39,576 hrs · 41,531 cycles

471 20123 457-900-342 10HOURS ***** AIRCRAFT REMOVED FROM SERVICE ***** RH WING LEADING EDGE AT ANTI ICE STUB DUCT INBOARD BRACKET FOUND WITH CORROSION. REMOVED AND REPLACED 1EA BRACKET P/N 601R120371-245 AT RH FORWARD SPAR AT WS139.54 TO WS149.58. IAW CRJ200 SRM 51-42-06 REV 39. TT:39,576, TC:41531

Part: ANGLE — CORRODED (FS319-FS349) · corrosion level 2 · airframe 39,576 hrs · 41,531 cycles

471 20081 330500 MFG 453-900-500 41.3 HRS RH FLOOR DOOR SILL STRUCTURE HAS 4 SPOTS OF EXFOLIATION FS295-FS349. AIRCRAFT REMOVED FROM SERVICE. BLENDED CORROSION ON ANGLE P/N 601R38303-239 TO SERVICE DOOR SILL BETWEEN FS319.7 TO FS349 AND EVALUATED ORIGINAL MATERIAL THICKNESS IS 0.063Ï¿½. MINIMUM REMAINING THICKNESS IS 0.037, L= 4.5Ï¿½ X W=1.5Ï¿½ FWD BLEND #1 AND MINIMUM REMAINING THICKNESS IS 0.043 L=9.5Ï¿½ X W=1.5Ï¿½ AFT BLEND #2. TEMPORARY DISPOSITION: THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 5,000 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF REO # 601R53-21-3661 REVÏ¿½DATED 2023-11-10. AND REMOVED AND REPLACED 1EA ANGLE SUPPORT P/N 601R38783-13 AND 1EA FITTING P/N 601R38672-3 AT FS349 RBL36 TO RBL41 ON RH FLOOR STRUCTURE IAW CRJ SRM 51-42-06, 51-42-13, AND 51-42-20.PERFORMED HFEC WITH NO INDICATIONS. VERIFIED NO LOOSED OR PULLED RIVETS AND DENT IS SMOOTH AND FREE OF CREASE.

Part: BRACKET — CORRODED (FS333+8) · corrosion level 2 · airframe 39,576 hrs · 41,531 cycles

471 20103 330500 MFG 427-680-100 3 HRS LH UPPER FLOOR SKIN AND SILL HAVE NUMEROUS AREAS OF CORROSION BETWEEN FS339-FS259. ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED 1EA CLEAT P/N 601R31527-176, 1EA BRACKET ASSY P/N 601R31527-217 ON PASSENGER DOOR SURROUND STRUCTURE AT FS333+8 LBL42 AND 1EA ANGLE SUPPORT P/N 601R38673-43 ON LH FLOOR STRUCTURE AT FS349 LBL36 TO LBL42 AND RESTORED ALL FINISHES IAW CRJ200 SRM 51-42-06, 51-42-13, AND 51-42-20 PERFORMED HFEC WITH NO INDICATIONS.

Part: CLEAT — CORRODED (FS333+8) · corrosion level 2 · airframe 39,576 hrs · 41,531 cycles

471 20103 330500 MFG 427-680-100 3 HRS LH UPPER FLOOR SKIN AND SILL HAVE NUMEROUS AREAS OF CORROSION BETWEEN FS339-FS259. ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED 1EA CLEAT P/N 601R31527-176, 1EA BRACKET ASSY P/N 601R31527-217 ON PASSENGER DOOR SURROUND STRUCTURE AT FS333+8 LBL42 AND 1EA ANGLE SUPPORT P/N 601R38673-43 ON LH FLOOR STRUCTURE AT FS349 LBL36 TO LBL42 AND RESTORED ALL FINISHES IAW CRJ200 SRM 51-42-06, 51-42-13, AND 51-42-20 PERFORMED HFEC WITH NO INDICATIONS.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 39,567 hrs · 41,531 cycles

DENT ON THE R/H INBD UPPER SURFACE INBD END. DENT ON R/H INBD FLAP UPPER SKIN WS 50.489+13. L=5.200Ï¿½ X W=0.400Ï¿½ X D=0.008Ï¿½ FOUND TO BE OUT OF LIMITS IAW SRM 57-52-00 REV 39. AIRCRAFT REMOVED FROM SERVICE. PERFORMED HFEC WITH NO INDICATIONS. VERIFIED NO LOOSED OR PULLED RIVETS AND DENT IS SMOOTH AND FREE OF CREASE.

Part: TRIM SYSTEM — FAULTED (STAB & MACH) · airframe 38,486 hrs · 40,321 cycles

STAB AND MACH TRIM DROPPED OFFLINE. AIRCRAFT REMOVED FROM SERVICE. OPS CHECKED GOOD, COULD NOT DUPLICATE. R & R HSTCU IAW AMM 27-41-01, PREVENTIVE. OPS CHECKED GOOD.

Part: FLAP SYSTEM — FAULTED · airframe 36,666 hrs · 38,530 cycles

FLAP FAILURE CAUTION. FLAPS FAILED AT 8 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL ***AIRCRAFT REMOVED FROM SERVICE*** FLAP FAILURE CAUTION. FLAPS FAILED AT 8 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL ***ATW RON 8/23*** 1MH

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 35,934 hrs · 37,754 cycles

AFTER THE CREW SELECTED FLAPS OUT OF ZERO THEY RECEIVED FLAP FAIL CAUTION MESSAGE. THE CREW COMPLIED WITH THEIR QRH AND PERFORMED A FLAP ZERO LANDING. THE CREW STATED THEY HAD A SMOOTH LANDING. MESSAGE WAS RESET AND A/C WAS FERRIED TO MKE FOR REPAIR. AIRCRAFT REMOVED FROM SERVICE. REF AWAC WO 301427 FOR TROUBLESHOOTING AND DETAIL MX OF REPLACEMENT OF 8 FLAP ACTUATOR FOR OFF WING FREEZE TEST. FLAP SYS RETURNED TO FULLY SERVICEABLE CONDITION REF ASSOCIATED MX WC FOR ALL REQUIRED RII.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 35,934 hrs · 37,754 cycles

AFTER THE CREW SELECTED FLAPS OUT OF ZERO THEY RECEIVED FLAP FAIL CAUTION MESSAGE. THE CREW COMPLIED WITH THEIR QRH AND PERFORMED A FLAP ZERO LANDING. THE CREW STATED THEY HAD A SMOOTH LANDING. MESSAGE WAS RESET AND A/C WAS FERRIED TO MKE FOR REPAIR. AIRCRAFT REMOVED FROM SERVICE. MX IN PROGRESS.

Part: BPSU — MALFUNCTIONED (LT WING TE FLAPS) · airframe 35,390 hrs · 37,751 cycles

FLAPS FAIL CAUTION ON APPROACH, FLAPS FAILED AT 20 DEGREES. CREW PREFORMED GO-AROUND AND COMPLIED WITH THE QRH. ONCE ON THE GROUND AND AT THE GATE FLAP RESET PROCEDURE WAS FOLLOWED, IAW AWAC SUPPLEMENT 98- 18I BOX 12. FLAPS RESET. AIRCRAFT REMOVED FROM SERVICE. REF WORKORDER 301426 AND MX WORK CARD 15, FOUND LT BPSU DOES NOT HOLD TOLERANCE. R & R BPSU, IAW AMM 27-51-10. REMOVED PLACARD AND REMOVED FROM MEL.

Part: POWER SUPPLY — NO TEST (TE FLAPS) · airframe 35,896 hrs · 37,716 cycles

FLAPS FAIL AT 20 ON APROACH CW QRH LANDED UNEVENTFULLY. FLAP FAIL OCCURED WHEN SELECING FROM 20 TO 30 DEG. PERFOREMED FLAP RESET PROCEEDURE, IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. T/S RT BPSU FOUND TO BE BAD. R & R RT BPSU, IAW AMM 27-51-10. OPERATIONS CHECK GOOD. REM PLACARD REMOVED FROM MEL

Part: APU — MAKING METAL (APU BAY) · airframe 35,435 hrs · 37,244 cycles

***SUPPLEMENTAL**** ODOR OF FUEL IN COCKPIT AFTER APU START IN FLT. ODOR DISSIPATED AS SOON AS BLEED WHERE TURN OFF. AIRCRAFT REMOVED FROM SERVICE THE APU WAS PLACED ON MEL,48-10-01-01 AND MX C/W SUP 09-037C FOR UNUSUAL ODORS OF CONTAMINATION FROM THE APU OR ACM. TROUBLESHOOT AND FOUND APU AUTOSHUTDOWN TWICE @60% DURING START. METAL FOUND ON DIL DRAIN PLUG. SUSPECT FUEL ISSUE CAUSING FUEL SMELL IN CABIN IS OVERFUELING APU POSSIBLE FUEL CONTROL INTERMITTENT FAIL. NO NEW CODES ON ECU AFTER BOTH SHUTDOWN IN HANGAR APU AND GEN REQUIRE REPLACEMENT. REPLACED APU.

Part: IGNITER — FAILED (APU) · airframe 35,430 hrs · 37,238 cycles

STRONG FUEL SMELL IN COCKPIT& CABIN AFTER STARTING APU. R&R EXCITER PER AMM 49-41-01-000-801, OPS CHECK GOOD. R&R BOTH APU IGNITORS PER AMM 49-41-05-000-801, OPS CHECK GOOD. SN OFF:1366J SN ON:J11060014 C/W AWA SUP 09-037C, NO UNUSUAL SMELL NOTED, NO FUEL LEAKS FOUND.

Part: FUEL LINE — LOOSE (APU) · airframe 35,428 hrs · 37,235 cycles

FUEL SMELL IN COCKPIT AND CABIN IN FLIGHT IMMEDIATELY AFTER APU START FOUND BOTH FUEL FEED AND FUEL RETURN LINES @ APU FUEL CONTROL LOOSE TIGHTENED AS REQUIRED.OPS CHECK GOOD IAW, AMM 49-10 AND AMM 21-00. NO UNUSAUL ODORS AT THIS TIME C/W SUP 09-037C. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: WIRE HARNESS — DAMAGED (NLG WOW) · airframe 35,401 hrs · 37,207 cycles

AFTER TAKEOFF, RECEIVED GEAR DISAGREE WARNING, NLG BOX WAS RED & NOSE DOOR WARNING MESSAGE. OCCURED IN ICING. MESSAGE CLEARED ON ITS OWN. THEN DURING APPROACH, RECEIVED GEAR DISAGREE AGAIN WITH RED NLG BOX & NOSE DOOR WARNING. CYCLED GEAR AND PUT HYD 2B & 3B PUMPS ON, MESSAGE THEN CLEARED. ALL HYD INDICATIONS WERE NORMAL. NO OTHER MESSAGES. AIRCRAFT REMOVED FROM SERVICE INSTALLED GEAR PINS IAW AWAC SUPP 11-054A. REF 312214/4 FOR MEL CHRISTOPHER PYLE A&P 3019835 R/R'D WOFF W2 SENSOR HARNESS (PS46A) REF AMM 32-61-05 UP TO 4.A. BOTH PROX SENSORS REQ'D ADJUSTMENT AND OPS CK REF 32-61-00-710-801 REF NEW WORK CARD FOR ADJUSTMENT AND CLOSEOUT

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYSTEM) · airframe 35,095 hrs · 36,905 cycles

LEFT WING A/ICE (C) MSG CAME ON IN FLT. C/W QRH. MSG PERSISTS. WERE IN ICING CONDITIONS. CLIMBED TO HIGHER ALTITUDE TO LEAE ICING CONDITIONS. LEFT FUSELAGE AND WING SHOWED IN AMBER. AFTER CLIMBING ABOVE ICING CONDITIONS RCVD L WINGA/ICE, R WING A/ICE + ICE (C) MSG WITH BOTH WING+COWL WAS ON POSITION. AS WE INSPECTED WING FROM THECOCKPIT IT APPEARED CLEAN OF ICE. AIRCRAFT REMOVED FROM SERVICE PERFORMED OPS TEST OF ICE DET. SYSTEM IAW AMM 30-81-00, AND TEST OF WING ANTI-ICE IAW AMM 30-12-00 AND ENGINE COWLS TEST IAW AMM 30-22-00, ALL CHECKS GOOD. REMOVED PLACARD AND FROM MEL.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSER) · airframe 35,085 hrs · 36,896 cycles

RIGHT TR UNLOCK CAUTION MESSAGE DISPLAYED DURING FLIGHT C/W QRH EMER STOW MESSAGE REMAINED. CREW LANDED NEAREST SUITABLE AIRPORT (IND) PER QRH. AIRCRAFT REMOVED FROM SERVICE LUBRICATED RT TR IAW AMM 12-20 OPS CHECK GOOD AT THIS TIME REMOVED PLACARD REMOVED FROM MEL

Part: CONTROL CABLE — FAILED (TE FLAPS) · airframe 35,061 hrs · 36,875 cycles

RECEIVED FLAP FAIL CAUTION MESSAGE ON APPROACH. EICAS INDICATES FLAPS @ 30 DEGREES. COMPLIED WITH QRH, EMERGENCY DECLARED. FLAPS SUCCESSFULLY RESET IAW AWAC SUPP. 98-018G AIRCRAFT REMOVED FROM SERVICE COULD NOT DUPLICATE FLAP FAIL CAUTION MSG. INTEREGATED F.E.C.U. FAULT CODES IAW FIM 27-50-00 & AWA SUPP 98-018G. REPLACED FLAP POSITION HANDLE ASSY IAW CRJ AMM 27-51-01. PERFORMED OPS CHECK OF FLAPS (27-54-00--710-801). REMOVED PLACARD, REMOVED FROM MEL.

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · corrosion level 2 · airframe 34,959 hrs · 36,783 cycles

RH FLOOR SILL FS 559+80 TO FS574 HAS CORROSION. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED RH FLOOR SILL FS 559+80 TO FS574 IAW CRJ 200 SRM 51-42-06

Part: FLOOR SUPPORT — CORRODED (BS 409) · corrosion level 2 · airframe 34,959 hrs · 36,783 cycles

RH FLOOR SILL FS 409+96 TO 409+112 HAS CORROSION. REPAIRED AIRCRAFT REMOVED FROM SERVICE REPAIRED RH FLOOR SILL FS 409+96 TO 409+112 IAW ASAP EA# AWAC-CRJ253-01375

Part: RETAINER — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 34,959 hrs · 36,783 cycles

SERVICE DOOR SEAL RETAINER AT BOTTOM CENTER OF DOOR HAS CORROSION AROUND FASTENERS AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED SEAL RETAINER ON SERVICE DOOR IAW AWAC SUPPLEMENT 19-310

Part: SKIN — CRACKED (BS 235) · airframe 34,959 hrs · 36,783 cycles

NOSE LANDING GEAR SPADE DOOR CUT OUT RH AND LH AFT CORNERS CRACKED AIRCRAFT REMOVED FROM SERVICE REPAIRED NOSE LANDING GEAR SPADE DOOR CUTOUT SKIN RH AND LH CORNERS IAW BOMBARDIER REO 601R-53-11-010

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 34,959 hrs · 36,783 cycles

LT INBOARD FLAP VANE HAS 3 CHAFES ON LEADING EDGE AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FLAP VANE LEADING EDGE SKIN IAW CRJ200 SRM 51-42-13

Part: STRIKER — GOUGED (PAX DOOR) · airframe 34,959 hrs · 36,783 cycles

PAX DOOR SEAL STRIKER IS GOUGED AT PREVIOUS REPAIR NEAR TOP, AFT, LATCH PIN FITTING AIRCRAFT REMOVED FROM SERVICE REPLACED DAMAGED STRIKER REPAIR IAW B/A REO 601R-53-22-033

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 34,959 hrs · 36,783 cycles

LH FLOOR SEAT RAIL FROM FS 409+128 TO FS 559 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE REPLACED LH FLOOR SEAT RAIL FROM FS 409+128 TO FS 559 IAW AWAC SUPP 19-254A

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 34,959 hrs · 36,783 cycles

RH FLOOR SEAT RAIL FROM FS 409+128 TO 559 HAS CORROSION. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED RH FLOOR SEAT RAIL FROM FS 409+128 TO 559 IAW CRJ 200 AMM 53-01-11

Part: DOUBLER — CORRODED (BS 559-574) · corrosion level 2 · airframe 34,959 hrs · 36,783 cycles

UPON REMOVAL OF FLOOR SILL FS559+80 TO FS 574 FOUND LOWER DOUBLER CORRODED. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED LOWER DOUBLER IAW CRJ 200 SRM 53-51-43

Part: ANGLE — CRACKED (BS 409 VERT POST) · airframe 34,959 hrs · 36,783 cycles

FS 409+128 VERTICAL POST AT BL0 ANGLE CRACKED. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED FS 409+128 VERTICAL POST AT BL0 ANGLE IAW REO 601R-53-41-889 REV D

Part: SKIN — CHAFED (RT AILERON) · airframe 34,959 hrs · 36,783 cycles

RIGHT AILERON LEADING EDGE HAS CHAFFING MARKS ALONG UPPER SIDE AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED R/H L/E OF AILERON IAW CRJ200 SRM 51-42-06 AND AWAC SUP. 14-270

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · corrosion level 2 · airframe 34,959 hrs · 36,783 cycles

RIGHT PRESSURE FLOOR SILL CORRODED. AIRCRAFT REMOVED FROM SERVICE REPAIRED IAW CRJ 200 SRM 51-42-06, REO 601R-53-41-666 REV-C.

Part: BEAM — DAMAGED (CARGO DOOR) · airframe 34,959 hrs · 36,783 cycles

CARGO DOOR BEAM 601R35050-64 CUT BY CABLE ASSIST. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED CARGO DOOR BEAM 601R35050-64 IAW CRJ 200 SRM 51-42-06

Part: TAB — CRACKED (LT HINGE BOX) · airframe 34,959 hrs · 36,783 cycles

LEFT WING HINGE BOX @ WS80-50 HAS BROKEN BONDING WIRE TAB. AIRCRAFT REMOVED FROM SERVICE REPLACED TAB IAW CRJ 200 SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,959 hrs · 36,783 cycles

SUPPLEMENTAL INFORMATION, NR 1 FLOOR SEAT TRACK ON RBL 9 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REPLACED NR 1 FLOOR SEAT TRACK ON RBL 9 IAW AMM 53-01-11.

Part: BRACKET — CRACKED (BS 621 BULKHEAD) · airframe 34,959 hrs · 36,783 cycles

AFT PRESSURE BULKHEAD COUNTER BALANCE SPRING BOX MOUNT BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED MOUNT BRACKET IAW CRJ-200 SRM 51-52-06

Part: ATTACH ANGLE — CRACKED (CARGO DOOR BEAM) · airframe 34,959 hrs · 36,783 cycles

CARGO DOOR BEAM ATTACH ANGLE IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED ANGLE IAW CRJ 200 SRM 51-42-21, 53-61-23, TR51-42.

Part: ANGLE — CRACKED (BS 280) · airframe 34,959 hrs · 36,783 cycles

FS 280 RBL 9 INBOARD CLIP IS CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CLIP IAW CRJ200 SRM 51-42-06 AND 51-42-42

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 34,959 hrs · 36,783 cycles

FWD CARGO DOOR TRACK LOWER ATTACH POINT IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FWD CARGO TRACK LWR ATTACH POINT BRACKET IAW CRJ 200 SRM 51-42-21 AND 51-41-00

Part: FLAP — FAILED (WING) · airframe 33,819 hrs · 35,688 cycles

DURING CRUISE FLIGHT, THE FLIGHT CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE WITH FLAPS AT ZERO DEGREES. THE CREW COORDINATED WITH DISPATCH, DECLARED AN EMERGENCY AND LANDED IN IAD WITHOUT FURTHER INCIDENT. FLAP RESET ATTEMPT WAS NOT SUCCESSFUL.

Part: FLAP — FAILED (WING) · airframe 33,768 hrs · 35,638 cycles

FLAPS FAILED AT 0 DEGREES AT CRUISE FLIGHT.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS SYS) · airframe 33,703 hrs · 35,576 cycles

DURING CRUISE FLIGHT, THE FLIGHT CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AND CONTINUED TO DESTINATION. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 33,596 hrs · 35,470 cycles

FLAPS FAIL AT 20 DEGREES ON APROACH PERFORMED FLAPS RESET PROSEDURE IAW AWAC SUP 98-018G FLAPS RESET PLACARDED AND PLACED ON MEL

Part: BULKHEAD WEB — CRACKED (BS 202) · airframe 33,460 hrs · 35,344 cycles

FORWARD PRESSURE BULKHEAD FS 202.75 & BL 23.71 IS CRACKED IN FIVE PLACES WHERE THE THE PARKING BRAKE CABLE PASSES THROUGH. CAN BE REPAIRED WITH GREO 601R-53-11-0563

Part: LINK — OUT OF ADJUST (AILERON PCU) · airframe 13,663 hrs · 13,166 cycles

AIRCRAFT HAS EXCESSIVE RIGHT HAND ROLL TENDENCY DURING ROTATION AND CLIMB. BOTH AUTOPILOTS ON AND OFF. REQUIRES APPROX 1/2 LEFT HAND WING DOWN TRIM FOR STRAIGHT AND LEVEL FLIGHT. THRUST WAS MATCHED FOR N1. FLIGHT CONTROL PAGE INDICATES LEFT AILERON SLIGHTLY UP. AIRCRAFT SPEED AND FLAP POSITION MAKE NO DIFFERENCE. AIRCRAFT REMAINS TOTALLY CONTROLLABLE IN ALL PHASES OF FLIGHT. AIRCRAFT WAS RIGGED CORRECTLY LAST NIGHT IN MKE. POSSIBLY PREVIOUS REPAIRS TO FLAPS. OTHER THAN AN REO MAY NEED TO CHANGE 2 FLAPS WHERE DAMAGE WAS REPAIRED. REPAIRS ARE 2 BY 2 AND THERE ARE 2 PATCHES ON 2 FLAP PANELS. INSPECTED BOTH AILERONS FOUND THE RT AILERON SLIGHTLY UP FROM CENTER (0) ADJUSTED RT AILERON PCU INPUT LINK 1/2 TURN IAW AMM 27-11-00. TRAVEL CHECKS OK.

Part: LINK — OUT OF ADJUST (RT AILERON) · airframe 32,033 hrs · 33,948 cycles

AIRCRAFT HAS EXCESSIVE RIGHT HAND ROLL TENDENCY DURING ROTATION AND CLIMB. BOTH AUTOPILOTS ON AND OFF. REQUIRES APPROX 1/2 LEFT HAND WING DOWN TRIM FOR STRAIGHT AND LEVEL FLIGHT. THRUST WAS MATCHED FOR N1. FLIGHT CONTROL PAGE INDICATES LEFT AILERON SLIGHTLY UP. AIRCRAFT SPEED AND FLAP POSITION MAKE NO DIFFERENCE. AIRCRAFT REMAINS TOTALLY CONTROLLABLE IN ALL PHASES OF FLIGHT. AIRCRAFT WAS RIGGED CORRECTLY LAST NIGHT IN MKE. POSSIBLY PREVIOUS REPAIRS TO FLAPS. OTHER THAN AN REO MAY NEED TO CHANGE 2 FLAPS WHERE DAMAGE WAS REPAIRED. REPAIRS ARE 2 BY 2 AND THERE ARE 2 PATCHES ON 2 FLAP PANELS INSPECTED BOTH AILERONS FOUND THE RT AILERON SLIGHTLY UP FROM CENTER (0) ADJUSTED RT AILERON PCU INPUT LINK 1/2 TURN IAW AMM 27-11-00. TRAVEL CHECKS OK.

Part: OVERHEAT SENSOR — FALSE ACTIVATION (JET PIPE) · airframe 13,466 hrs · 12,952 cycles

CLIMBING THOUGH 9000 FT, RECEIVED A LT JET OVERHEAT FAIL CAUTION MESSAGE. 15 SECONDS LATER RECEIVED A LT JETPIPE OVERHEAT WARNING WITH AUDIO. COMPLIED WITH QRH AND MESSAGE CLEARED AT 70% N1. LANDED, NORRMAL BRAKING. PERFORMED GVI OF LEFT JETPIPE SENSING ELEMENT AND CONNECTORS AND WIRES IAW AMM 26-11-04, PERFORMED CONTINUITY TEST ON THE LEFT JETPIPE SENSING ELEMENT IAW CMM 26-11-67, PERFORMED AN OPS TEST OF JETPIPE IAW AMM 26-11-00, OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: SKIN — CRACKED (RT WING) · airframe 31,782 hrs · 33,673 cycles

RIGHT WING LOWER SKIN CRACKED AT WS 148.019.

Part: SKIN — CRACKED (LT WING) · airframe 31,782 hrs · 33,673 cycles

LEFT WING LOWER SKIN CRACKED AT WS 148.019.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,782 hrs · 33,673 cycles

PAX DOOR AFT RISER PANEL DRAG ANGLE IS CRACKED BY ASSIST MOTOR PULLEY YOKE.

Part: PANEL — CRACKED (PAX DOOR) · airframe 31,782 hrs · 33,673 cycles

PAX DOOR AFT RISER PANEL CRACKED BEHIND AFT DRAG ANGLE.

Part: FLOOR SUPPORT — CRACKED (BS 589) · airframe 31,782 hrs · 33,673 cycles

LEFT FLOOR SUPPORT CRACKED AT BS 589, IN THE CARGO BAY

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 31,782 hrs · 33,673 cycles

PREVIOUS REPAIR ON THE RT FLOOR SUPPORT HAS CORROSION AT BS 559+96, IN THE CARGO BAY.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 31,782 hrs · 33,673 cycles

FLOOR SUPPORT AT BS 484, RBL 36 CRACKED.

Part: ATTACH ANGLE — CRACKED (RT A/C BAY) · airframe 31,782 hrs · 33,673 cycles

RIGHT AIR CONDITIONING PRESSURE MANIFOLD LOWER ATTACH ANGLE CRACKED.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 32,037 hrs · 31,014 cycles

RIGHT AFT PRESSURE BULKHEAD ZEE ANGLE TO BS 625 FRAME INTERCOSTAL CRACKED OTBD OF RBL 36

Part: RISER — CRACKED (PAX DOOR) · airframe 32,037 hrs · 31,014 cycles

PAX DOOR FWD RISER ANGLE FILLER FROM PREVIOUS REPAIR IS CRACKED

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 31,782 hrs · 33,673 cycles

CARGO DOOR LOWER AFT VERTICAL STRUCTURE CRACKED. REPLACED THE VERTICAL STRUCTURE IAW SRM 51-42-07, 51-42-13, AND 51-42-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,782 hrs · 33,673 cycles

COMPLY WITH PERMANENT REPAIR PER ORDER CARD 263160 / 4DMI19173. COMPLIED WITH PERMANENT REPAIR IAW SRM 51-42-06, SUPP 17-280 DATED 11/06/2017 AND REO 601R-53-11-3151 REV -- DATED 2017-11-13.

Part: SHIELD — CRACKED (RT TAIL PIPE) · airframe 31,782 hrs · 33,673 cycles

RT TAIL PIPE FIRE SHIELD CRACKED AT 9 O'CLOCK POSITION. REPAIRED FIRE SHIELD IAW CMM 78-11-00-350-012-A01.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 31,782 hrs · 33,673 cycles

RIGHT INBD FLAP LWR SKIN IS DENTED AT THE OTBD AFT CORNER.

Part: FITTING — DAMAGED (BS 621 BULKHEAD) · airframe 31,782 hrs · 33,673 cycles

PRESSURE BULKHEAD WEB FITTING BS 621 DAMAGED. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-1230 REV-F.

Part: CLEAT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 31,782 hrs · 33,673 cycles

PAX DOOR LOWER AFT CLEAT CORRODED. REPLACED THE CLEAT IAW SRM 53-00-00, 51-40-06, 53-21-23, 51-21-06, AND 51-42-06.

Part: DRAG ANGLE — CRACKED (BS 529-559) · airframe 31,782 hrs · 33,673 cycles

LEFT MLG WHEEL WELL BAT RIB DRAG ANGLE IS CRACKED. REPLACED THE DRAG ANGLE IAW SRM 51-42-21.

Part: CONTROL PANEL — ARCED (COCKPIT) · airframe 13,350 hrs · 12,831 cycles

SPARKS COMING FROM THE APU START & STOP PANEL ON OVERHEAD. REMOVED ALL POWER FROM AIRCRAFT, NO ARCING AT THIS TIME. NO FUMES OR ODORS NOTED. APU WAS RUNNING AND APU GENERATOR WAS ON. R & R THE APU POWER & FUEL AND START/STOP SWITCHES IAW ESPM 24-00. OPS CHECKED GOOD. INSPECTED PANEL, NO EVIDENCE OF DAMAGE NOTED.

Part: WARNING MESSAGE — ILLUMINATED (ANTI ICE SYS) · airframe 31,670 hrs · 33,569 cycles

4199 ON CLIMBOUT RECEIVED ANTIICE DUCT WARNING MSG. CW QRH MSG PERSISTS. MSG CLEARED ON DECENT WITH THRUST LEVERS AT IDLE. MSG RETURNED WITH THRUST LEVERS ADVANCED. ANTIICE WAS SELETED OFF DURING THE EVENT (MC-AS PART OF THE QRH PROCEEDURE) RH FUSELAGE WAS RED ON THE ANTIICE SYNOPTIC PAGE. THE 14TH STAGE SHUTOFF VLV WAS CLOSED AS PART OF THE QRH PROCEEDURE. RETURNED TO PHL. LANDING WEIGHT 45000LBS MAX BTMS READINGS WERE 5,6,3,5. SHORTLY AFTER ANTIICE DUCT WARNING MSG WAS RECEIVED, RECEIVED RIGH COWL ANTIICE CAUTION MSG. MSG CLEARED WHEN 14TH STAGE SOV WAS CLOSED. 14TH STAGE ISOLATION VLV WAS CLOSED AT ALL TIMES. MC-DIDNT SELELECT STBY, CAPTAIN THOUGHT THE DUCT FAIL AND OVERHEATLIGHTS WERE ON ON THE OVERHEAD PANEL

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 13,148 hrs · 12,648 cycles

FLOOR EMERGENCY LIGHTS INOPERATIVE ROW 9 THROUGH 13. FOUND A LOOSE CONNECTOR, CONNECTED IAW AMM 33-51-01, OPS CHECKED GOOD.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 30,832 hrs · 32,769 cycles

A STRONG ODOR OF BURNING PLASTIC IN GALLEY AREA. INSPECTED GALLEY LIGHT , BALLAST, AND VENTILLATION IAW AMM 33-26-AND 25-21 NO ODORS DETECTED . INSPECTED SIDEWALL BALLAST IN OVERHEAD BIN 3DF, AND FOUND THE BALLAST WARM TO THE TOUCH AND ASSOCIATED LIGHTS BURNED OUT. REMOVED POWER FROM BALLAST AND THE ODOR CLEARED.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 30,363 hrs · 32,333 cycles

DURING CRUISE FLIGHT AT FL320, FLAPS DEGRADED STATUS MESSAGE. FLAPS REPEATEDLY MOVED FROM 0-3 AND BACK TO ZERO. AP ENGAGED, AIRCRAFT PORPOISED REPEATEDLY. 270KTS. ALL 3 B PUMPS INTERMITTENT. AIRSPEED RASTER RED. PULLED CBP1-B5 AND CBP2-B5 FLAPS REMAINED AT ZERO. DIVERTED WITH A SMOOTH LANDING.

Part: UNKNOWN — NOISE (NLG) · airframe 29,852 hrs · 31,871 cycles

AFTER SELECTING GEAR UP- 3 GREEN UP, A LOUD BANGING FROM NOSE GEAR DOOR AREA. SELECTED GEAR DOWN AND BANGING WENT AWAY. NO MESSAGES. RETURNED TO DEPARTURE AND LANDED NORMAL.

Part: WIRE — BROKEN (ANTI-SKID SYS) · airframe 10,961 hrs · 10,583 cycles

RECEIVED A, SKID OTBD AND INBD CAUTION MSGS WHEN EXTENDING GEAR ON APPROACH. C/W QRH, LANDED WITH NO ISSUES, BTMS 2-3-3-2. REPAIRED BROKEN WIRE AT LT INBD TRANSDUCER IAW AWAC SUP 12-075B. SYSTEM OPS CHECKS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,191 hrs · 31,224 cycles

REQUEST INSPECTION OF BURNED RUBBER ODOR AT ROW 6 & ROW 7.

Part: SIGN — INOPERATIVE (CABIN) · airframe 10,222 hrs · 9,857 cycles

EMERGENCY EXIT LIGHT PLACARDS WILL NOT ILLUMINATE BY PAX & SERVICE DOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,108 hrs · 9,750 cycles

FLIGHT 3782, FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROW 1.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 10,004 hrs · 9,685 cycles

FLIGHT 4007 EMERGENCY EXIT LIGHTS, FLOOD, AT PAX & SERVICE DOOR ARE NOT OPERATING. CONNECTED EMERGENCY LIGHTS AT 1DF, OPS CHECKED IAW AMM 33-11-00. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,214 hrs · 30,278 cycles

ROWS 5 - 8 EMER FLOOR TRACK LIGHTING INOPERATIVE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,835 hrs · 29,914 cycles

LEFT INTERCOSTAL MEMBER OTBD AT STRINGER 13L & FS 624.00 IS CRACKED, REPLACED.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,835 hrs · 29,914 cycles

GALLEY MOUNT SUPPORT PLATE ON THE SILL AT FS 310 CORRODED, REPLACED.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,835 hrs · 29,914 cycles

LOWER FRAME BRACKET AT FS 319.70 IS EXFOLIATED, REPLACED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,835 hrs · 29,914 cycles

RIGHT FLOOR SILL, JUST FWD OF THE SERVICE DOOR OPENING ASST FS 319.70 CORRODED, REPLACED.

Part: FLOORBOARD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,835 hrs · 29,914 cycles

FLOORBOARD LANDING ON THE OTBD SIDE OF LBL 27, BETWEEN FS 571 - 621 HAS SEVERAL CORROSION SPOTS, REPLACED.

Part: INTERCOSTAL — GOUGED (FUSELAGE) · airframe 27,835 hrs · 29,914 cycles

INTERCOSTAL AT FS 473.15, STRINGER 10L GOUGED, REPLACED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,835 hrs · 29,914 cycles

RIGHT WINDSHIELD OTBD SIDE POST, LOWER AFT ANGLE FITTING IS CRACKED, REPLACED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,835 hrs · 29,914 cycles

RIGHT FLOOR SILL, BETWEEN FS 559+80 - 559+112 HAS CORROSION SPOTS, REPAIRED.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 27,835 hrs · 29,914 cycles

ATTACH ANGLE IN LT MLG BAY AT APPROX FS 529.0 & LBL 50 CRACKED, REPLACED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,835 hrs · 29,914 cycles

SKIN BELOW AFT LATCH FOR PANEL 211AL CRACKED, REPAIRED.

Part: LANDING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,835 hrs · 29,914 cycles

INBD FLOOR LANDING ON LBL 27, BETWEEN FS 559+80 - FS 574 HAS CORROSION, REPLACED.

Part: RUB STRIP — CHAFED (TE FLAP VANE) · airframe 27,835 hrs · 29,914 cycles

RIGHT WING INBD FLAP VANE LE RUBSTRIP IS CHAFED, WS 120.382.

Part: ANCHOR FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,835 hrs · 29,914 cycles

ANCHOR FITTING AT FS 349.00 CORRODED, REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,835 hrs · 29,914 cycles

SEAT TRACK ON RBL 9 HAS CORROSION, BETWEEN 559+112 & FS 574, REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,835 hrs · 29,914 cycles

LEFT OTBD CLIP AT STRINGER 12L & FS 624.00 IS CRACKED, REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,835 hrs · 29,914 cycles

COMPLIED WITH JC 4DMI17389, REPAIR INTERCOSTAL AT FS 621 BH CAP 601R-53-61-5079, REPAIRED.

Part: RUB STRIP — CHAFED (TE FLAP VANE) · airframe 27,835 hrs · 29,913 cycles

RIGHT WING INBD FLAP, LE VANE RUB STRIP IS CHAFED, WS 75.27.

Part: SKIN — CRACKED (LT COWLING) · airframe 27,835 hrs · 29,914 cycles

LEFT LOWER CORE COWL OUTER SKIN AT NR 4, LATCH IS CRACKED, REPAIRED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,835 hrs · 29,914 cycles

RIGHT OTBD CLIP AT STRINGER 12R & FS 624 IS CRACKED, REPLACED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,835 hrs · 29,914 cycles

RIGHT FLOOR ANGLE ON FWD SIDE OF FS 621 BULKHEAD IS CRACKED, REPLACED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,835 hrs · 29,914 cycles

PASSENGER DOOR SILL FLOOR SUPPORT ANGLE, HAS CORROSION INBD & OTBD SURFACES FROM FS 310.00 - 349.00, REPLACED.

Part: RUB STRIP — CHAFED (TE FLAP VANE) · airframe 27,835 hrs · 29,914 cycles

RIGHT WING, INBD FLAP VANE LE RUB STRIP IS CHAFED, WS 104.099.

Part: PLATE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 27,835 hrs · 29,914 cycles

CARGO NET FLOOR TIE DOWN MOUNTING PLATE HAS SEVERAL CORROSION SPOTS, BETWEEN FLOORBEAMS 589 & 606, JUST INBD OF CARGO DOOR LOWER SILL, REPAIRED.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,835 hrs · 29,914 cycles

PASSENGER DOOR OPENING LOWER SILL, AFT CLEAT IS CORRODED IN CABIN. REMOVED CORRODED AFT CLEAT & BRACKET & INSTALLED REPLACEMENT AFT CLEAT & BRACKET ON PAX DOOR LOWER SILL IAW SRM 51-21-06, 53-00-00, 51-42-06, 51-42-13, 51-40-11 & 51-25-16.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,835 hrs · 29,914 cycles

PASSENGER DOOR LOWER SILL, FWD CLEAT IS CORRODED IN CABIN. REMOVED CORRODED FWD CLEAT & BRACKET. INSTALLED REPLACEMENT FWD CLEAT & BRACKET ON PAX DOOR LOWER SILL IAW SRM 51-21-06, 53-00-00, 51-42-06, 51-42-13, 51-40-11 & 51-25-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,835 hrs · 29,914 cycles

ANGLE CLIP IS CRACKED AT THE OTBD SIDE OF RBL 9, AT BEAM 280, REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,835 hrs · 29,914 cycles

ANGLE CLIP IS CRACKED AT THE OTBD SIDE OF LBL 9 AT BEAM 280, REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,835 hrs · 29,914 cycles

ANGLE CLIP IS CRACKED ON THE OTBD SIDE OF RBL 27 AT FS 484, REPLACED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,650 hrs · 29,736 cycles

FLIGHT 3758 FLOOR LEVEL LIGHT ROW 9 - 12 NOT COMING ON.

Part: YAW DAMPER — FAULTY (NR 1) · airframe 27,454 hrs · 29,542 cycles

FLIGHT 3846 ON CLIMB OUT, RT RUDDER TRAVELING TO THE LT & NOSE KICKING TO THE RT, FELT & SAW INDICATION ON ED2. HAPPENED ON CLIMB OUT, CRUISE & DESCENT, NO MSGS OBSERVED. R & R NR 1 & NR 2 YAW DAMP ACTUATORS.

Part: PSEU — FAULTY (LANDING GEAR) · airframe 27,201 hrs · 29,289 cycles

FLIGHT 3868 IN CRUISE FLIGHT, RECEIVED PROXIMITY SYSTEM FAULT STATUS MESSAGE. 30 MINUTES LATER, WITH FLAPS 20, ON GEAR DOWN RECEIVED PARKING BRAKE SOV & INBOARD ANTI-SKID AMBER CAUTION MESSAGES. GO AROUND GEAR UP, CAUTION MESSAGES CLEARED, PROXIMITY REMAINED. ON GEAR DOWN, CAUTION MESSAGES RETURNED AT GATE. PSEU FLAGGED ELECTRONIC UNIT FAILURE. R & R PSEU ELECTRONIC UNIT IAW AMM 32-61-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — FAILED (GALLEY) · airframe 27,170 hrs · 29,261 cycles

FLIGHT 3739, SMOKE COMING FROM LIGHTS OVER SERVICE DOOR IN GALLEY. SHUT LIGHTS OFF, SMOKE STOPPED. R & R A BURNED RECEPTACLE ON THE SECOND TO BOTTOM GALLEY LIGHT ASSEMBLY IAW ESPM 20-16. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,165 hrs · 29,256 cycles

LOWER EMERGENCY LIGHT DOES NOT LIGHT UP AT ROW 1.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 7,559 hrs · 7,301 cycles

ON DIVERSION RECEIVED GLD UNSAFE CAUTION. QRH PROCEDURE COMPLIED WITH. MSG CLEARED BUT FLIGHT SPOILERS GO INTERMITTENT DEPLOYMENT ON FLIGHT CONTROL PAGE WITH HYD SYS PRESSURIZED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 25,514 hrs · 27,706 cycles

AFTER TAKEOFF THRUST APPLIED RECEIVED IDG NR 2 CAUTION & GEN NR 2 CAUTION MSG. ABORTED TAKEOFF AT LESS THAN 20 KTS.

Part: SOLENOID — FAULTY (MLG) · airframe 5,688 hrs · 5,523 cycles

ON SELECTING GEAR DOWN, GOT GEAR DISAGREE WARNING. RAN QRH, NOSE WAS GREEN, BOTH MAINS WERE WHITE BOXES. USED MANUAL RELEASE TO GET THE MAINS DOWN. COMPLIED WITH ACTION OF MEL 32-30-01. PSEU REPORTS CURRENT FAILURE D043 DOWN ERROR MAIN GEAR EXTEND. SOLENOID REPLACED MAIN GEAR SELECTOR VLV IAW AMM 32-30. OPERATIONS & LEAKS CHECKED GOOD. REMOVED PLACARD REMOVED MEL.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 5,296 hrs · 5,168 cycles

STRONG FUEL SMELL OBSERVED DURING APU OPERATION INFLT & ON THE GND. SMELL DISSIPATES WHEN APU IS SHUTDOWN. INSPECTED APU & FOUND FUEL TO BE COMING FROM POWER SECTION. PERFORMED ENG RUNS & NO FUEL SMELL IN COCKPIT OR CABIN WITH APU OFF. R & R APU POWERPLANT IAW 49-10-00 & MTC 000-49-310-001AW. OPERATIONS CHECKED LEAK, CHECKED GOOD.

Part: RETAINER — CRACKED (RT PYLON) · airframe 23,095 hrs · 25,405 cycles

RIGHT PYLON PANEL 422AT HAS CRACKED SEAL RETAINER. REMOVED, FABRICATED & INSTALLED NEW SEAL RETAINER.

Part: HINGE — CRACKED (LT WING) · airframe 23,095 hrs · 25,405 cycles

LEFT BUTE DOOR HINGE CRACKED. R & R BUTE DOOR HINGE.

Part: SILL — CORRODED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

CARGO DOOR FLOOR SILL HAS CORROSION ALONG THE LENGTH FROM FS 621 TO FS 570. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED UNSERVICEABLE FLOOR SILL & INSTALLED A SERVICEABLE FLOOR SILL IAW REO 601R-53-61-1574 REV A.

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 23,095 hrs · 25,405 cycles

CARGO DOOR OUTER HANDLE IS CRACKED. R & R IAW CRJ 200 SRM 51-42-21 PN 601R35060-5.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

FUSELAGE STATION 379, 3L STRINGER CRACKED. REPAIRED IAW SRM 53-00-03.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 23,095 hrs · 25,405 cycles

PASSENGER DOOR MOTOR ASSIST LOWER MOUNT BRACKET IS CRACKED AT BOTTOM. R & R PN 601R317745-7 IAW CRJ 200 SRM 51-42-06.

Part: SEAL — CRACKED (RT SPOILER) · airframe 23,095 hrs · 25,405 cycles

RIGHT FLIGHT SPOILER INBD SPRING SEAL IS CRACKED. R & R UNSERVICEABLE SPRING SEAL.

Part: ATTACH BRACKET — CRACKED (CARGO DOOR) · airframe 23,095 hrs · 25,405 cycles

CARGO DOOR LOWER FWD ATTACH BRACKET CRACKED. R & R PN 601R35050-25 IAW CRJ 200 SRM 51-42-06.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 23,095 hrs · 25,405 cycles

RIGHT INBD FLAP FIXED VANE LE CHAFED. R & R FLAP VANE LE SKIN AT WING STATION 143.

Part: STIFFENER — GOUGED (RT EXHAUST) · airframe 23,095 hrs · 25,405 cycles

RIGHT EXHAUST FAIRING FWD UPPER STIFFENER IS GOUGED. R & R DAMAGED STIFFENER.

Part: FITTING — GOUGED (PAX DOOR) · airframe 23,095 hrs · 25,405 cycles

PASSENGER DOOR UPPER AFT CAM FITTING GOUGED ON LOWER EDGE. R & R PAX DOOR UPPER AFT CAM FITTING.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

BRACKET CRACKED LT SIDE AFT FACE OF 621 PRESS BULKHEAD STRINGER 14L AREA. CONDITION ACCEPTABLE AS IS 6000 FH IAW REO 601R-53-61-5079.

Part: STRIKER — GOUGED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

PASSENGER DOOR AFT SEAL STRIKER HAS DEEP GOUGE. REPAIRED PAX DOOR AFT SEAL STRIKER IAW REO 601R-53-22-033,

Part: MOUNT BRACKET — CRACKED (WHEEL WELL) · airframe 23,095 hrs · 25,405 cycles

WHEEL WELL BRAKE HYD LINE MOUNT BRACKET CRACKED. R & R HYD LINE BRACKET.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

LEFT LOWER NOSE HYD BAY UPPER HYD ACCUMULATOR FWD ATTACH BRACKET CRACKED. R & R LT NOSE HYD COMP UPPER HYD ACCUMULATOR FWD ATTACH BRACKET IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,095 hrs · 25,405 cycles

FLOOR SEAT RAILS AT FS 349-409+112 ARE CORRODED. R & R UNSERVICEABLE SEAT RAIL SECTIONS AT FS 344-409+112 LBL & RBL WITH NEW SERVICEABLE SEAT RAILS IAW CRJ 200 AMM 53-01-11.

Part: MOUNT — CRACKED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

RETURN FILTER MOUNT HAS CRACK. REPAIR IAW REO 601R-53-62-031 REV A.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

CARGO DOOR SILL SUPPORT STRUCTURE CLIP IS CRACKED AT FS 605.0 FWD INBD ANGLE. R & R CRACKED CLIP.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

FLOOR SUPPORT INTERCOSTAL ATTACH CLIP AT FS 484 BL 57 CRACKED. REPLACED FLOOR SUPPORT INTERCOSTAL ATTACH CLIP AT FS 484 BL 57 IAW REO 601R-53-41-059.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

FLOOR SUPPORT INTERCOSTAL ATTACH CLIP AT FS 484 BL 27 CRACKED. REPLACED FLOOR SUPPORT INTERCOSTAL ATTACH CLIP AT FS 484 BL 27 IAW REO 601R-53-41-059.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

BRACKET CRACKED LT SIDE AFT FACE OF 621 PRESS BULKHEAD APPROXIMATELY 8 INCHES INBD OF STRINGER 14L. R & R.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

BRACKET CRACKED RT SIDE AFT FACE OF FS 621 PRESS BULKHEAD APPROXIMATELY 8 INCHES INBD OF STRINGER 14R. R & R.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

LBL & RBL 9 280 INBD CLIPS CRACKED. R & R LBL & RBL 9 280 INBD CLIPS.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

STRINGER 32 INBD & OTBD CLIPS CRACKED, AFT SIDE PILOTS 280 BULKHEAD TIE IN ANGLE WAS ALSO CRACKED. REMOVED UNSERVICEABLE INBD & OTBD CLIPS. REPLACED, FABRICATED SERVICEABLE CLIPS FOR INBD & OTBD & TIE IN ANGLE WAS R & R WITH SERVICEABLE FABRICATED ANGLE.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 23,095 hrs · 25,405 cycles

FLOOR SUPPORT INTERCOSTAL ATTACH CLIP AT FS 484 RBL 36 IS CRACKED. FABRICATED & INSTALLED NEW SERVICEABLE CLIP IAW REO 601R-53-41-059 REV B.

Part: TRUNNION — DAMAGED (MLG) · airframe 23,095 hrs · 25,405 cycles

DURING INCORPORATION OF THE MLG TRUNNION LOWER FLANGE, COLD WORKING FOUND TWO EACH OVERSIZED HOLES IN THE STRAP, PLANK & LOWER FLANGE. ONE ON THE LT SIDE & ONE ON THE RT SIDE. COMPLIED WITH REO 601R-57-21-2020 REV FOR COLD WORKING TWO EACH OVERSIZED FASTENER HOLES.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 20,883 hrs · 23,245 cycles

AFT LOWER SUPPORT CLIPS ON CARGO BAY DOOR RAIL SUPPORT BRACKET AT 621 BULKHEAD CRACKED. REMOVED CRACKED CLIP, THEN FABRICATED NEW SERVICEABLE CLIP AND INSTALLED IAW CRJ SRM 51-24-16.

Part: CABLE — BROKEN (PAX DOOR) · airframe 19,704 hrs · 22,131 cycles

DURING CLIMBOUT, VERY LOUD SQUEAL HEARD FROM PAX DOOR. R & R BROKEN ICE DOOR CABLE IAW AMM 52-11-15 PRESSURIZED ACFT, OPS CHECKED GOOD.

Part: FITTING — CRACKED (PAX DOOR LATCH) · airframe 18,370 hrs · 20,782 cycles

PAX DOOR AFT LATCH MECHANISM TORQUE TUBE PASS THROUGH FITTING UNDER PANEL 832AR IS CRACKED. REMOVED DOUBLER, LOCATED AND INSTALLED SERVICEABLE DOUBLER PN 601R318894-2 IAW SRM 51-40-11.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 18,370 hrs · 20,782 cycles

BRACKET IS CRACKED IN FUEL TANK. R & R BRACKET.

Part: POST — CRACKED (FS 409) · airframe 18,370 hrs · 20,782 cycles

POST AT FS 409+128 LBL 27 APPEARS CRACKED AT LOWER INBD SIDE REPAIRED LBL POST AT FS 409+128 BY REMOVING DAMAGE AND INSTALLING FILLER AND REPAIR ANGLE IAW REO 601R-53-41-056, REV E.

Part: POST — CRACKED (FS 409) · airframe 18,370 hrs · 20,782 cycles

POST AT FS 409+128, RBL 18 APPEARS CRACKED AT LOWER OTBD SIDE. REPAIRED RBL 18 POST AT FS 409+128 BY REMOVING DAMAGE AND INSTALLING FILLER AND REPAIR ANGLE IAW REO 601R-53-41-056, REV E.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,370 hrs · 20,782 cycles

LT SIDE SEAT TRACK NR 6 POS SHOWS SIGNS OF CORROSION. R & R NR6 LT SIDE SEAT TRACK IAW AMM 53-01-11-000-802 & SRM 51-24-34 & 51-40-11 & 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,370 hrs · 20,782 cycles

RT SIDE SEAT TRACK NR6 POSITION SHOWS SIGNS OF CORROSION. R & R NR6 SIDE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-24-34, 51-21-11, & 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,370 hrs · 20,782 cycles

LT SIDE SEAT TRACK NR 5 SHOWS SIGNS OF CORROSION. R & R NEW SERVICEABLE NR 5 LT SIDE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-24-36, 51-40-11, 51-21-11, AMM 53-01-11, PG 406.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 18,370 hrs · 20,782 cycles

PAX DOOR STAIR ATTACHMENT ANGLE (AFT) IS CRACKED (MOTOR SUPPORT AREA) DRAG ANGLE REMOVED PREVIOUSLY INSTALLED REPAIR ANGLE FABRICATED NEW ANGLE AND INSTALLED IAW REO 601R-52-11-513.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,370 hrs · 20,782 cycles

LT SIDE SEAT TRACK NR 7 POSITION SHOWS SIGNS OF CORROSION. R & R NR 7 SIDE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-24-34, 51-40-11, 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,370 hrs · 20,782 cycles

LT SIDE SEAT TRACK NR 4 POSITION SHOWS SIGNS OF CORROSION. R & R NR4 LT SIDE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-24-34 & 51-40-11, 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,370 hrs · 20,782 cycles

LT SIDE SEAT TRACK NR3 POS SHOWS SIGNS OF CORROSION. R & R LT NR3 SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-24-34, 51-40-11, 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,370 hrs · 20,782 cycles

RT SIDE SEAT TRACK NR4 SHOWS SIGNS OF CORROSION. R & R NEW SERVICEABLE RT SIDE SEAT TRACK NR 4 IAW AMM 53-01-11-000-802, SRM 51-23-36, 51-21-11, AMM 53-01-11, PG 406.

Part: SEAT TRACK — CORRODED (RT SIDE) · airframe 18,370 hrs · 20,782 cycles

RT SIDE SEAT TRACK NR 5 POSITION SHOWS SIGNS OF CORROSION. R & R RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-24-34, 51-40-11, 51-21-11.

Part: SKIN — DAMAGED (LT NACELLE) · airframe 18,370 hrs · 20,782 cycles

LT UPPER CORE COWL INBD L/E DAMAGE. REPAIRED DAMAGE TO LT UPPER CORE COWL IAW CMM 71-12-01.

Part: FLOOR SUPPORT — CRACKED (BS 574-621) · airframe 18,370 hrs · 20,782 cycles

FLOOR SUPPORT UNDER FLOORBOARD 281LLF ARE CORRODED IN SEVERAL PLACES. FLOORBEAM FOUND TO BE CRACKED. REMOVED FLOORBEAM CAP FROM FS 621 TO 574 AT SPLICE, TRIMMED, DRILLED, AND INSTALLED NEW BEAM CAP.

Part: SILL — DAMAGED (BS 559) · airframe 18,370 hrs · 20,782 cycles

RT FLOOR SILL BETWEEN 559+80 TO 559+112 BLEND AS REQUIRED AND NDT FOR FURTHER DAMAGE.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 18,370 hrs · 20,782 cycles

PAX DOOR SUPPORT WHEEL PULLEY BRACKET ATTACHED TO LOWER STAIR IS CRACKED. R & R PAX DOOR SUPPORT WHEEL PULLEY BRACKET IAW SRM 51-42-06.

Part: HEAT SHIELD — CRACKED (APU BAY) · airframe 18,370 hrs · 20,782 cycles

APU HEAT SHIELD CRACKED AT 7 O`CLOCK POSITION. REPAIRED IAW REO 601R-49-81-003.

Part: SUPPORT — CRACKED (AEB DOOR) · airframe 18,370 hrs · 20,782 cycles

DOOR CRACKED AT FWD SUPPORT. FABRICATED AND INSTALLED NEW SERVICEABLE FWD SUPPORT STRUCTURE.

Part: DOOR — CHAFED (LT MLG) · airframe 18,370 hrs · 20,782 cycles

LT MLG DOOR CHAFED ON LOWER L/E. REPAIRED IAW REO 601R-52-82-034.

Part: ACCESS PANEL — CHAFED (RT WING) · airframe 18,370 hrs · 20,782 cycles

RT ACCESS PANEL 699BB CHAFED. REPAIRED IAW REO 601R-57-60-020.

Part: SILL — CORRODED (BS 473.15) · corrosion level 1 · airframe 18,370 hrs · 20,782 cycles

CORROSION ON RT FLOOR SILL IN AREA JUST AFT OF OVERWING EXIT REPAIRED IAW 601R-53-41-666.

Part: SKIN — CHAFED (RT NACELLE) · airframe 18,370 hrs · 20,782 cycles

CHAFE CAUSED BY BLOCKER DOOR ON RT LOWER CORE COWL BY FWD LATCHES. R & R CHAFED DOUBLER IAW CMM 71-12-01.

Part: SKIN — CHAFED (RT AILERON) · airframe 18,370 hrs · 20,782 cycles

RT AILERON LWR L/E CHAFED IN 2 PLACES. BLENDED CHAFED AREAS IAW SRM 51-12-00 AND REO 601R-57-60-020.

Part: STRUCTURE — CHAFED (LT WING TE FLAP) · airframe 18,370 hrs · 20,782 cycles

LT INBD FLAP CHAFED 3 PLACES. BLENDED CHAFED AREAS IAW SRM 51-12-00 AND REO 601R-57-52-004.

Part: STRUCTURE — CHAFED (FS 621) · airframe 18,370 hrs · 20,782 cycles

RT SIDE OF FS 621 BLK FWD FACE HAS 3 CHAFE MARKS 2-.5 FT ABOVE FLOOR. BLEND OUT DAMAGE IAW REO 601R-53-61-2155.

Part: BULKHEAD — CHAFED (FS 621) · airframe 18,370 hrs · 20,782 cycles

THE LT LOWER FWD SIDE OF FS 621 BULKHEAD HAS 3 CHAFED SPOTS FROM FASTENERS APPROX 2" OFF FLOOR BLEND OUT DAMAGE IAW REO 601R-53-61-2155.

Part: FLOORBEAM — CRACKED (FS 280) · airframe 18,370 hrs · 20,782 cycles

FS 280, RBL 10 FLOORBEAM CRACKED. REMOVED UNSERVICEABLE TEE AND REPLACED WITH SERVICEABLE TEE.

Part: STIFFENER — CHAFED (BULKHEAD) · airframe 18,370 hrs · 20,782 cycles

REAR PRESSURE BULKHEAD CENTER VERTICAL STIFFENER CHAFED FROM ISOLATOR VALVE (E-VAL) BLEND OUT CHAFING IAW REO 601R-53-61-1523 AND SRM 51-12-00.

Part: STRIKER — MISREPAIRED (PAX DOOR) · airframe 18,370 hrs · 20,782 cycles

BOTH REPAIRS TO PAX DOOR CUT OUT SEAL STRIKER ARE DAMAGED/BENT. REPAIRS WERE NOT FINISHED CORRECTLY. REMOVED/REPLACED 2 EA POPCYCLE REPAIRS ON PAX DOOR CUT OUT SEAL STRIKER IAW REO 601R-53-22-033.

Part: FLOOR SUPPORT — CORRODED (FS 349) · airframe 18,370 hrs · 20,782 cycles

FLOOR SUPPORT SYS AFT OF PAX DOOR CUT OUT HAS CORROSION ON RT SIDE. UPON FURTHER INVESTIGATION FOUND ONLY RIVET HEADS, 10 EA CORRODED. REMOVED AND INSTALLED 10 EA CORRODED RIVETS PN CR 3212-5-4. NO OTHER DEFECTS NOTED IAW SRM 51-42-10.