N458AW

Part: SENSOR — OUT OF TOLERANCE (OLOE) · airframe 41,201 hrs · 39,995 cycles

GEAR DISAGREE ON TAKEOFF *****AIRCRAFT REMOVED FROM SERVICE******** INSP AND FOUND NLG OLOE SENSOR OUT OF TOLERANCE ADJ OLEO SENSOR IAW AMM 32-61 OPS CK GOOD. PERF NLG DOOR OPERATING IAW AMM 32-21-00 OPS CK GOOD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,848 hrs · 39,572 cycles

6178 - RECEIVED GEAR DISAGREE WARNING MESSAGE WHEN SELECTING GEAR UP AFTER TAKEOFF BETWEEN 600 TO 1K FEET AGL. NOSE DOOR OPEN WARNING MESSAGE ASSOCIATED. ALL HYD SYSTEM INDICATIONS NORMAL. NOSE GEAR REMAINED DOWN AND LOCKED WITH GREEN INDICATION, AND MANUAL GEAR EXTENSION HANDLE WAS PULLED PER QRH. FOUND PROX SENSOR BRACKET BENT. R&R NLG PROX SENSOR BRACKET IAW AMM 32-61-05. AND CMM 32-20-04. OPS CHECK GOOD AT THIS TIME.

Part: HINGE — CHAFED (PAX DOOR) · airframe 39,976 hrs · 38,547 cycles

PAX DOOR PIANO HINGE HALF DOOR SIDE HAS CHAFED MARKS *****AIRCRAFT REMOVED FROM SERVICE******** REPAIRED IAW REO 601R-52-11-2938

Part: PLATE — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 39,583 hrs · 38,164 cycles

FRAME STATION 467 LH SILL PLATE CORROSION BLEND OUT OF LIMITS .018 REMAINING MATERIAL. *****AIRCRAFT REMOVED FROM SERVICE******** FABRICATED REPAIR FOR FS467 LH SILL PLATE & INSTALLED. RESTORED FINISH PER CRJ200 EA#AWAC-CRJ253-01888 REV IR.

Part: APU — NONE (ZONE 100) · airframe 39,947 hrs · 38,519 cycles

SMOKE TOILET CAUTION MSG AFTER T/O AT 1000 FT C/W QRH RETURNED TO PVD MSG CLEARED ON FINAL. NOTE APU FAILED ON THE PRIOR FLIGHT. AIRCRAFT REMOVED FROM SERVICE. INSPECTED FOUND SMOKE SMELL CAUSED BY APU FAILURE PERFORMED CLEARING OF UNUSUAL ODORS IAW AWA SUP 09-037D WITH THE HELP OF THE CREWCLEARING OPS CHECKED GOOD, SMOKE DET OPS CHECK GOOD.REMOVED AND REPLACED APU ASSY IAW MTCM SUPP 13-005 TASK CARD 000-49-310-001AW. OPS AND LEAK CHECSK GOOD. REMOVED PLACARD AND FROM MEL

Part: NONE — NONE · airframe 39,022 hrs · 37,612 cycles

WHILE EN ROUTE, THE AIRCRAFT EXPERIENCED AN ISSUE WITH THE #1 ENGINE COWL ANTI ICE SYSTEM. IN ORDER TO AVOID ICING CONDITIONS, THE CREW AND DISPATCHER HAVE AGREED TO DIVERT TO PIT. THE FLIGHT SHOULD BE ON THE GROUND IN PIT AT 1445EST. ***AIRCRAFT REMOVED FROM SERVCE*** R&R COWL A/ICE VALVE AND REPACKED TURKEY POPPER. FOUND TURKEY POPPER POPPED AFTER OPS CHECK. UNABLE TO MEL DUE TO CONFLICTING MEL WILLIAM CALVIN A&P 3500209 P/N: 5399-00-1, S/N OFF: 0382B, S/N ON: 1768B ARW

Part: SEAT TRACK — CORRODED (FS 559) · corrosion level 2 · airframe 37,303 hrs · 35,867 cycles

SEAT TRACK AT RBL 9, FS 559 TO FS 559+80 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT RBL 9, FS 559 TO FS 559+80, IAW REO 601R-53-00-764.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 37,303 hrs · 35,867 cycles

SEAT TRACK HAS CORROSION FROM FS 559+80 TO FS 559+88, RBL 9. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK FROM FS 559+80 TO FS 559+88, RBL 9, IAW REO 601R-53-00-764.

Part: TEE FITTING — CORRODED (CABIN) · corrosion level 2 · airframe 37,303 hrs · 35,867 cycles

T-CAP EXTRUSION ON LBL 27 AT FS 570 TO FS 605 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T CAP EXTRUSION AT LBL 27, FS 570 TO FS 605, IAW CRJ 200SRM 51--42-00 AND BOMBARDIER DWG 601R35031 REV P.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 37,303 hrs · 35,867 cycles

SEAT TRACK HAS CORROSION FROM FS 599+80 TO 599+88, LBL 9. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK FROM FS 599+80 TO 599+88 LBL 9, IAW REO601R-53-00-764.

Part: TEE FITTING — CORRODED (CABIN) · corrosion level 2 · airframe 37,303 hrs · 35,867 cycles

TCAP EXTRUSION ON LBL 27, FS 570 TO FS 605 CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T CAP AT LBL 27, FS 570 TO FS 605, IAW CRJ200 SRM 51-42-21-00 AND BOMBARDIER DRAWING 601R35031 REV P.

Part: FMS — FAILED · airframe 36,281 hrs · 34,876 cycles

FULL FMS FAILURE THRU 6000FT ON CLIMB OUT C/W FIM RESET FMS RESET TO NORMAL

Part: WARNING MESSAGE — ILLUMINATED (CARGO SMOKE) · airframe 35,951 hrs · 34,541 cycles

ON DESCENT AT 15,000 FEET THE CREW RECEIVED A CARGO SMOKE WARNING MESSAGE. REFERENCED THE QRH, DECLARED AN EMERGENCY AND CONTINUED DESCENT TO KDAY. LANDING WAS NORMAL AND MET BY ARFF ON RUNWAY. NO SMOKE OR FIRE DETECTED. AIRCRAFT PROCEEDED TO THE GATE WITH NO FURTHER ISSUES. NO INJURIES OR ADVERSE PASSENGER REACTIONS.

Part: A/C PACK — WARNING MESSAGE (LEFT)

CREW RECEIVED L PACK HI PRESS CAUTION MESSAGE AFTER TAKEOFF WITH RIGHT PACK ALREADY ON MEL. COMPLIED WITH QRH AND THE MESSAGE REMAINED. FLIGHT RETURNED TO IAD.

Part: ACM — MALFUNCTIONED (RIGHT) · airframe 35,062 hrs · 33,719 cycles

AT FLIGHT LEVEL 280 IN NORMAL DECENT, RIGHT PACK WENT OFF LINE AND CREW OBSERVED RIGHT 10TH STAGE BLEED ARMED OPEN MESSAGE ON ED2 ON ECS PAGE. CREW OBSERVED RIGHT 10TH STAGE BLEED WAS CLOSED AND RIGHT HAND PACK WAS RECIEVING NO PRESSURE. BEGAN COMPLYING WITH QRH PROCEDURES. NOTE CABIN PRESSURE RISING DURING CHECKLIST. CABIN ALTITUDE MASTER CAUTION OCCURED AS PRESSURE ROSE TO 8,500. AT CABIN ALT 10,000 RECIEVED MASTER CABIN ALTITUDE WARNING. QRH INSTRUCTED CABIN PASSENGER OXYGEN TO DEPLOY. DURING DESCENT, RIGHT HAND PACK CYCLED ON/OFF MULTIPLE TIMES. UPON LANDING, RIGHT HAND PACK WAS OPERATIONAL. CREW DECLARED EMERGENCY LANDING INTO ATW.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 34,696 hrs · 33,372 cycles

CARGO DOOR BEAM MEMBER HAS TWO SPOTS WHERE CABLE HAS CUT INTO OB FLANGE. REMOVE AND REPLACED CARGO DOOR BEAM MEMBER IAW SRM 51-42-21.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,696 hrs · 33,372 cycles

FLOOR STRAP AT FS 559 RBL28 TO RBL42 CORRODED. REPLACED.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,696 hrs · 33,372 cycles

PAX DOOR SURROUND STRUCTURE LOWER SILL ANGLE CORRODED. REPLACED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 34,696 hrs · 33,372 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 34,696 hrs · 33,372 cycles

PAX DOOR AFT INTERCOSTAL IN LINE WITH GUIDE PLATE IS CRACKED. REPLACED.

Part: STEP — CRACKED (PAX DOOR) · airframe 34,696 hrs · 33,372 cycles

PAX DOOR FWD STEP WEB AT LOWER STEP CRACKED. REPAIRED

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 34,696 hrs · 33,372 cycles

AFT EQUIPMENT BAY STR 13L INTERCOSTAL CRACKED. REPLACED

Part: ANGLE — CRACKED (BS 621-625) · airframe 34,696 hrs · 33,372 cycles

AFT EQUIPMENT BAY STR 14R CLIP AT FUSELAGE SKIN CRACKED. REPLACED

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 34,696 hrs · 33,372 cycles

AFT PRESSURE BULKHEAD FWD FACE HAS A CRACK DETECTED WITH UT @RBL 36.20 @ TOP CLIP OF LOWER PANEL ON RH SIDE OF CLIP JUST BELOW THE UPPER RIVET APPROX .25 LONG. REPAIRED

Part: POST — CRACKED (BS 409) · airframe 34,696 hrs · 33,372 cycles

STA 409+128 VERTICAL POST AT BL0 IS CRACKED IN THE RH AFT RADIUS AT APPROX WL 69.0. REPLACED

Part: ANGLE — CRACKED (BS 625) · airframe 34,696 hrs · 33,372 cycles

OBLIQUE ANGLE @ FS 625 AND STR 15L CRACKED. REPLACED REPLACED OBLIQUE ANGLE @ FS 625 AND STR 15L IAW CRJ 200 SRM 51-42-21

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,696 hrs · 33,372 cycles

AFT PRESSURE BULKHEAD FWD FACE HAS A CRACK DETECTED WITH HFEC AT BL 0 APPROX 35" FROM FLOOR ON LT SIDE OF RIVET LINE 1-3/4" LONG. REPAIRED APB IAW REO 601R-53-61-1285 REV E.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,696 hrs · 33,372 cycles

FS 484 CLIP AT IB RBL 36 CRACKED. REMOVED AND REPLACED CLIP AT FS 484 IAW REO 601R-53-41-59 REV B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,696 hrs · 33,372 cycles

UPPER IB CLIP ON CARGO BEAM AT APB CRACKED. REMOVED AND REPLACED UPPER IB CLIP IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,696 hrs · 33,372 cycles

FS 484 CLIP AT OB LBL 27 CRACKED. REMOVED AND REPLACED CLIP IAW REO 601R-53-47-59 REV B.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,696 hrs · 33,372 cycles

AFT LOWER CLIP ON CARGO BEAM AT APB IS CRACKED. REMOVED AND REPLACED AFT LOWER CLIP IAW SRM 51-42-21.

Part: SELECTOR VALVE — FAULTY (NLG) · airframe 33,429 hrs · 32,137 cycles

GEAR DISAGREE WARNING MESSAGE UPON GEAR EXTENSION. FLAPS WERE SELECTED 30. GRINDING NOISES HEARD BEFORE GEAR SHOWED DOWN AND LOCKED, AIRCRAFT WAS IN ICING CONDITIONS DURING EXTENSION, 3A PUMP SELECTED ON, ALL OTHERS WERE IN AUTO, EMERGENCY WAS DECLARED. ALL 3 GEAR SHOWED DOWN AND LOCKED AFTER APPROXIMATELY 10-15 SECONDS. REMOVED AND REPLACED NLG SELECTOR VALVE IAW AMM 32-33-10 OPS AND LEAK CHECK GOOD AT THIS TIME.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 33,293 hrs · 32,000 cycles

DURING APU START ED1 AND ED2 WENT BLANK WITH STRONG ELECTRICAL SMELL. ED1 AND ED2 RETURNED TO NORMAL AFTER APU START. UPON ARRIVAL NO BURNING ELECTRICAL SMELL. C/W DEPOWER/REPOWER. APU BATT CK GOOD. C/W NORMAL APU START. INSPECTED AVIONICS BAY, MDC, NO FAULTS FOUND. CYCLED DISPLAY FANS ADN ARINC FANS. NO DEFECTS NOTED.

Part: WIRE HARNESS — SHORTED (CABIN) · airframe 32,688 hrs · 31,379 cycles

PAX DOOR AND SEVICE DOOR EMERGENCY LIGHTS INOP. FOUND SHORT AT FIRST ROW ORANGE FLOOR TRACK LIGHT. R&R EMERGENCY FLOOR TRACK RIBBON IAW AMM. OPS CHECK GOOD.

Part: CABLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,645 hrs · 31,340 cycles

EMERGENCY FLOOR LIGHTS ROW 8 AND AFT WILL NOT ILLUMINATE. R & R THE CABLE ASSY IAW ESPM 24-20-00, OPS CHECKED GOOD.

Part: RESERVOIR — LEAKING (HYD SYSTEM) · airframe 32,379 hrs · 31,098 cycles

RECEIVED A HYD 3 LOW PRESSURE CAUTION MESSAGE DURING LANDING GEAR EXTENTION, HYD SYN PG SHOWED 5 PERCENT QTY ON SYS 3, QRH INSTRUCTED MANUAL GEAR EXTENTION, ALL LANDING GEAR SHOWED GREEN DOWN AND LOCKED, RECEIVED A NOSE GEAR DOOR WARNING MESSAGE AND GEAR DISAGREE WARNING MESSAGE. FOUND HYD SYSTEM NR 3 RESERVOIR LEAKING FLUID, REMOVED AND REPLACED NR 3 HYD SYSTEM RESERVOIR IAW AMM 29-12-30, NO FURTHER LEAKS, OPS CHECKED GOOD.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 32,334 hrs · 31,057 cycles

EMERGENCY FLOOR LIGHTS INTERMITTENT ROW 9 AFT. SEATED THE CONNECTORS AT ROW 8 AND ROW 12. EMERGENCY LIGHTS OPS CHECKED GOOD IAW AMM 33-51-00.

Part: CONNECTOR — LOOSE (CABIN) · airframe 32,292 hrs · 31,017 cycles

AFT EMERGENCY FLOOR TACK LIGHT IS INOP. REATTACHED LOOSE CONNECTION AT ROW 12, OPS TEST GOOD.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 32,021 hrs · 30,757 cycles

NO LIGHT OFF ON APU FIRST ATTEMPT, STARTED ON SECOND ATTEMPT. NOTICED STRONG FUEL ODOR IN COCKPIT AND CABIN, SHUT APU OFF. OPS CHECKED APU IAW AMM 49-10-00, OPS CHECKED GOOD. RAN APU FOR 20 MINUTES, NO ODOR PRESENT.

Part: CONNECTOR — DIRTY (CABIN) · airframe 32,002 hrs · 30,741 cycles

EMERGENCY LIGHTS ROW 8 AFT WOULD NOT ILLUMINATE. CLEANED CONNECTORS AND PERFORMED AN OPS CHECK IAW AMM 33-51-00 OPS CHECKED GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,866 hrs · 30,615 cycles

PRIOR TO FIRST FLIGHT OF THE DAY, CREW REPORTED THAT THE EMERGENCY LIGHTS DID NOT WORK AFT OF ROW 8. ROW 9 THROUGH 12 ARE NOT WORKING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,787 hrs · 30,548 cycles

EMERGENCY FLOOR TRACK LIGHTS FROM ROW 9 AFT WILL NOT ILLUMINATE

Part: AILERON — BINDING · airframe 31,792 hrs · 30,551 cycles

AILERON CONTROL BINDING AND CLICKING DURING FLIGHT CONTROL CHECK, ON FO'S SIDE, NO BINDING FELT ON CAPT SIDE

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 31,736 hrs · 30,504 cycles

EMERGENCY FLOOR LIGHTING BEYOND ROW 8 IS NOT WORKING. REMOVED & REPLACED EMERGENCY FLOOR TRACK LIGHTING AFT CONNECTOR HARNESS AS REQUIRED. OP CHECKS GOOD

Part: FITTING — LEAKING (APU FUEL) · airframe 31,422 hrs · 31,205 cycles

ON APU START ATTEMPT IN THE AIR, RECEIVED AN APU FAULT. APU AUTO SHUTDOWN. STARTED APU ON GROUND, NOTICED FUEL ODOR AND SHUTDOWN APU. INSPECTED APU AND PACKS IN AFT EQUIPMENT BAY. NO DEFECTS NOTED. PERFORMED OPS CHECK OF APU. OPS CHECKED GOOD. PERFORMED PACK BURNOUT IAW AWAC SUP 09-037A. FUEL ODOR IS GONE. ACFT OK FOR SERVICE. PERFORMED VISUAL INSPECTION OF APU FOUND FUEL AND OIL IN ENCLOSURE AND FUEL COMING FROM CUMBUSTOR, EXHAUST DRAIN, CLEANED AREA. RAN ENGINES AND PACKS NO FUEL ODOR NOTED. R & R FITTING. OPS AND LEAK CHECKED GOOD.

Part: UNKNOWN — ODOR · airframe 31,422 hrs · 30,215 cycles

ON APU START ATTEMPT IN THE AIR, RECEIVED AN APU FAULT. APU AUTO SHUTDOWN. STARTED APU ON GROUND. NOTICED FUEL ODOR AND SHUTDOWN APU.INSPECTED APU AND PACKS IN AFT EQUIPMENT BAY. NO DEFECTS NOTED. PERFORMED OPS CHECK OF APU. OPS CHECKED GOOD. PERFORMED PACK BURNOUT IAW AWAC SUP 09-037A. FUEL ODOR IS GONE. ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (ANTI ICE DUCT) · airframe 31,310 hrs · 30,108 cycles

RECEIVED ANTI ICE DUCT WARNING MESSAGE AT 16000 FEET WITH WINGS OFF AND COWLS ON, COMPLIED WITH QRH MESSAGE REMAINED. RT FUSELAGE DUCT RED WITH 14TH STAGE VALVE OPEN. WHEN CLOSED MESSAGE STILL REMAINS

Part: FLOOR SUPPORT — CORRODED (BS 615-621) · corrosion level 2 · airframe 31,256 hrs · 30,062 cycles

CARGO FLOOR SUPPORT FROM BS 559+80 - 621 AT LBL 10 CORRODED. REPAIRED THE FLOOR SUPPORT.

Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,256 hrs · 30,062 cycles

FLOORBEAM CAP AT LBL 9 FS 574 TO 615 CORRODED. REPLACED

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,256 hrs · 30,062 cycles

FRAME AT FS 333 BETWEEN STR 0 AND STR 1L CRACKED. REPLACED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,256 hrs · 30,062 cycles

FRAME FS605 CRACKED AT LOWER FLANGE AT STGR18L, FOUND DURING CARGO FLOOR SILL REPLACEMENT.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,256 hrs · 30,062 cycles

IN AFT CARGO FLOORSILL HAS CORROSION LBL42 TO LBL46 FS559+112 TO FS621.

Part: SKIN — CHAFED (RT AILERON) · airframe 31,256 hrs · 30,062 cycles

O/B LEADING EDGE OF RIGHT AILERON IS CHAFED.

Part: SKIN — CHAFED (RT AILERON) · airframe 31,256 hrs · 30,062 cycles

I/B LEADING EDGE OF RIGHT AILERON IS CHAFED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,256 hrs · 30,062 cycles

STR 3L CLIP CRACKED AT FS 280.00. REPLACED CLIP AT FS 280.00 AND STR 3L IAW SRM 51-42-06 , 51-42-21.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,256 hrs · 30,062 cycles

RIGHT SIDE OVERWING PNL ATTACHMENT ANGLE AT FS471 IS CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,256 hrs · 30,062 cycles

ANGLE CLIP IS CRACKED AT THE O/B SIDE OF LBL9 AT FS484, IN CABIN BELOW FLOOR.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,256 hrs · 30,062 cycles

ANGLE CLIP IS CRACKED AT THE O/B SIDE OF RBL27 AT FS484, IN CABIN BELOW FLOOR.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,256 hrs · 30,062 cycles

ANGLE CLIP IS CRACKED AT THE I/B SIDE OF LBL36 AT FS484, IN CABIN BELOW FLOOR.

Part: ATTACH ANGLE — CRACKED (BS 449) · airframe 31,256 hrs · 30,062 cycles

RIGHT OVERWING PANEL ATTACH ANGLE AT BS 449 IS CRACKED.

Part: ATTACH ANGLE — CRACKED (BS 439) · airframe 31,256 hrs · 30,062 cycles

RIGHT OVERWING PANEL ATTACH ANGLE AT BS 439 IS CRACKED

Part: FITTING — CRACKED (BS 461) · airframe 31,256 hrs · 30,062 cycles

BATHTUB FITTING IS CRACKED AT LBL 9, BS 461

Part: ATTACH ANGLE — CRACKED (BS 449) · airframe 31,256 hrs · 30,062 cycles

LEFT OVERWING ACCESS PANEL ATTACH BRACKET AT BS 449.85 IS CRACKED.

Part: FITTING — CRACKED (BS 461) · airframe 31,256 hrs · 30,062 cycles

BATHTUB FITTING IS CRACKED AT RBL 9, BS 461 IN CABIN BELOW FLOOR.

Part: ATTACH ANGLE — CRACKED (BS 461) · airframe 31,256 hrs · 30,062 cycles

LEFT OVERWING ACCESS PANEL ATTACH ANGLE AT BS 461 IS CRACKED.

Part: ATTACH ANGLE — CRACKED (BS 461) · airframe 31,256 hrs · 30,062 cycles

OVERWING PANEL ATTACHMENT ANGLE AT BS 461 IS CRACKED

Part: CARGO TRACK — DAMAGED (BS 559) · airframe 31,256 hrs · 30,062 cycles

CARGO TRACK BS 559+112, RBL 9 IS CORRODED AND GOUGED.

Part: ANGLE — CRACKED · airframe 31,256 hrs · 30,062 cycles

CO-PILOTS SIDE POST LOWER O/B ANGLE IS CRACKED

Part: ANGLE — CRACKED · airframe 31,256 hrs · 30,062 cycles

PILOTS SIDE POST LOWER OTBD ANGLE IS CRACKED

Part: BRACKET — CRACKED (RT WING) · airframe 31,256 hrs · 30,062 cycles

RIGHT WING PICCOLO TUBE SUPPORT BRACKET CRACKED AT WS 149.58

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,016 hrs · 29,841 cycles

EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE BETWEEN ROWS 8-13.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 29,836 hrs · 28,751 cycles

GEAR DISAGREE AFTER TAKEOFF NOSE GEAR DOWN, BOTH MAINS RETRACTED. WARNING APPEARED APPROX 28 SECONDS AFTER SELECTING GEAR. EMER GEAR RELEASE OPERATED. LANDING WEIGHT 36500 LBS.

Part: SECU — MALFUNCTIONED (SPOILER SYSTEM) · airframe 29,686 hrs · 28,599 cycles

FLIGHT 3976 ON FINAL AT FLAPS 20, RECEIVED OB GND SPOILER CAUTION. COMPLIED WITH QRH, ALL SPOILERS DEPLOYED ON TOUCHDOWN. COMPLIED WITH FIM RESET, MSG DID NOT CLEAR. R & R SECU 1 IAW AMM 27-65-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,372 hrs · 28,310 cycles

DURING RON, FOUND EMER FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 8 - 12.

Part: CAP — MISSING (CABIN) · airframe 29,027 hrs · 27,987 cycles

FORWARD END CAP FOR THE FLOOR LEVEL EMER LIGHTING IS MISSING 3766. EMER LIGHT FIXTURE BY PAX DOOR, FWD BULKHEAD BROKEN.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 28,967 hrs · 27,935 cycles

AFTER DEPARTURE COULD SMELL BURNING SMELL IN FRONT & BACK OF ACFT. COMPLIED WITH QRH FOR SMOKE & FUMES. DECLARED EMER & LANDED BELOW 47,000 LBS. BLEEDS WERE ON ENGS. COMPLIED WITH FIM 79-20-01 R & R LT & RT COALESCE BAGS IAW CUP 14-192. OPERATIONS CHECKED BOTH PACKS WITH BLEED AIR FROM ENGS AT HIGH POWER FOR 20 MINUTES, NO SMOKE & NO FUMES OR ODOR AT THIS TIME.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 28,843 hrs · 27,814 cycles

FLIGHT NR 3983, ON TAKEOFF, APPROX 700 FT, AUTOPILOT ENGAGED, FLAPS 8, RECEIVED STAB TRIM CAUTION MSG FOLLOWED BY MACH TRIM CAUTION. THEN RECEIVED AUTOPILOT TRIM CAUTION MSG. DISCONNECTED AUTOPILOT, FOLLOWED AN ABRUPT NOSE UP PITCH CHANGE. COMPLIED WITH QRH, REENGAGED STAB CH 2 & REGAINED NORMAL CONTROL OF ACFT. ACTION TAKEN IN PROGRESS.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,397 hrs · 27,369 cycles

FLIGHT 3762 EMERGENCY EXIT FLOOR LIGHTING INOPERATIVE 6 - 8 & LOWER RT EMERGENCY EXIT SIGN INOPERATIVE. R & R EMERGENCY LIGHT INVERTER FOR PAS CHECK NR 3. OPS CHECKED OK IAW AMM 33-51-00.

Part: INVERTER — FAULTY (CABIN) · airframe 28,397 hrs · 27,369 cycles

FLIGHT 3765, 3920, FLOOR LEVEL EMERGENCY EXIT SIGN AT ROW 8DF WILL NOT ILLUMINATE. SWAPPED NR 3 & 4 INVERTERS IAW AMM 33-51-07. PERFORMED OPS CHECK IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 28,220 hrs · 27,204 cycles

FLIGHT 3777, FLOOR TRACK LIGHTS AT BACK OF ROW 5 TO FRONT OF ROW 9 INOPERATIVE. ALSO ROW 8 RT SIDE EXIT LOWER. CHARGED EMERGENCY LIGHTS & COMPLIED WITH OPS CHECK, NO DEFECTS NOTED AT THIS TIME. OPS CHECKED GOOD IAW AMM 33-51.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 27,582 hrs · 26,589 cycles

EMERGENCY FLOOR LIGHTING COVER ROW 11 - 12 LOOSE, LIGHT STRIP NOT IN TRACK. INSPECTED & FOUND BROKEN INSULATION ON FLOOR TRACK WIRING. SPLICED & INSTALLED ENVIRONMENTAL SPLICES IAW AMM 20-11-00. OPS CHECKED GOOD.

Part: WARNING MESSAGE — ACTIVATED (NLG STEERING) · airframe 27,361 hrs · 26,387 cycles

STEERING INOPERATIVE CAUTION MESSAGE INFLIGHT. RAN QRH, WOULD NOT CLEAR. AFTER GEAR EXTENSION MESSAGE WOULD NOT RESET & ON GROUND MESSAGE WOULD NOT RESET.

Part: WARNING MESSAGE — ILLUMINATED (NLG) · airframe 27,038 hrs · 26,084 cycles

GEAR DISAGREE DURING RETRACTION. NLG DID NOT RETRACT, WOW INPUT CAUTION & WOW OUTPUT FAIL STATUS MSG. WARNING POSTED APPROX 6 SECONDS AFTER HANDLE MOVEMENT. NOSE DOOR OPEN & STEERING INOPERATIVE MSGS POSTED. NLG REMAINED AS GREEN DOWN & LOCKED. NLG SEEMED EXCESSIVELY BOUNCY ON TAXI TO RUNWAY.

Part: WARNING MESSAGE — ACTIVATED (LANDING GEAR) · airframe 26,987 hrs · 26,034 cycles

AFTER TAKEOFF, RECEIVED GEAR DISAGREE WARNING MESSAGE. NOSE INDICATED DOWN & LOCKED, MLG UP, INDICATED XX, GEAR LEVER IN UP POSITION. COMPLIED WITH QRH FOR GEAR DISAGREE, PULLED MANUAL EXTENSION & MAINS INDICATED DOWN & LOCKED.

Part: FITTING — CRACKED (WING) · airframe 26,798 hrs · 25,890 cycles

PRESSURE REFUEL PORT OTBD MOUNT FITTING CRACKED & GOUGED.

Part: MOUNT BRACKET — CRACKED (RT MLG WW) · airframe 26,798 hrs · 25,890 cycles

RIGHT MLG WW BRAKE TRANSDUCER MOUNT BRACKET IS CRACKED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,798 hrs · 25,890 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED.

Part: FITTING — CRACKED (WING) · airframe 26,798 hrs · 25,890 cycles

PRESSURE REFUEL PORT INBD FITTING GOUGED AT OTBD LOWER CORNER.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 26,798 hrs · 25,890 cycles

55025-5000-0023 OTBD LE ATTACH ANGLE CRACKED AT LT WING TRANSITION DUCT.

Part: DECK PLATE — CRACKED (FUSELAGE) · airframe 26,798 hrs · 25,890 cycles

LEFT FWD EQUIPMENT DECK IS CRACKED AT AFT OTBD DOOR FRAME AT FS 319.00.

Part: ACCESS PANEL — DAMAGED (FUSELAGE) · airframe 26,798 hrs · 25,890 cycles

55025-2000-0005 COMPLIED WITH CARD 4DMI17925 REPAIR ACCESS PANEL 131AL. FREEZE PLUGS REQUIRE REPLACEMENT ON PANEL 131AL SURROUND DOUBLER.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 26,798 hrs · 25,890 cycles

AFT FACE OF PRESS BULKHEAD U CHANNEL CRACKED AT MOLD LINE SKIN & STRINGER 14L.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 26,798 hrs · 25,890 cycles

PASSENGER DOOR POWER ASSIST MOTOR MOUNT BRACKET CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,798 hrs · 25,890 cycles

CARGO DOOR SUPPORT BEAM HAS CRACKED CLIP ON FWD FACE OF FS 621 BULKHEAD.

Part: RIB — CRACKED (LT WING) · airframe 26,798 hrs · 25,890 cycles

LEFT MLG WW BATTERY RIB CRACKED.

Part: RIB — CRACKED (RT WING) · airframe 26,798 hrs · 25,890 cycles

RIGHT MLG WW BATTERY RIB CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,798 hrs · 25,890 cycles

RIGHT NR 1 FLOOR SEAT TRACK CORRODED AT FWD END FS 364.00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,798 hrs · 25,890 cycles

FLOOR SUPPORT AT FS 559.0 FROM LBL 27 TO LT SILL CORRODED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,798 hrs · 25,890 cycles

FLOOR SUPPORT AT FS 559.00 AT RBL 27 TO RT FLOOR SILL IS CORRODED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,798 hrs · 25,890 cycles

CLIPS CRACKED AT FS 484 RBL 27 & RBL 36.

Part: VANE — CHAFED (TE FLAP) · airframe 26,798 hrs · 25,890 cycles

LEFT INBD FLAP VANE LE INBD SECTION CHAFED BEYOND LIMITS.

Part: BRACKET — CRACKED (RT MLG) · airframe 26,798 hrs · 25,890 cycles

RIGHT MLG WW BRAKE PRESS TRANSDUCER LINE BRACKET CRACKED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,798 hrs · 25,890 cycles

FORWARD FLOOR SUPPORT ANGLE AT FS 280 CORRODED.

Part: PLATE — CRACKED (FUSELAGE) · airframe 26,798 hrs · 25,890 cycles

AIRCRAFT GND POWER RECEPTACLE MOUNTING PLATE CRACKED.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 26,798 hrs · 25,890 cycles

HYD SYS 1 RETURN MANIFOLD MOUNT BRACKET IS CRACKED.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 26,798 hrs · 25,890 cycles

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

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,798 hrs · 25,890 cycles

PASSENGER DOOR SILL FLOOR SUPPORT LOWER ANGLE IS CORRODED.

Part: WIRE HARNESS — DEFECTIVE (NLG STEERING) · airframe 25,686 hrs · 24,788 cycles

3848 NWS INOPERATIVE CAUTION MSG AFTER TAKEOFF AT APPROX 500 FT. COMPLIED WITH QRH MSG REMAINS UPON LANDING RE ENGAGED NWS, NO MSG. R & R NWS ELEC HARNESS IAW SUPP 12-029C. OPERATIONS CHECKED GOOD.

Part: RVDT — FAULTY (NLG STEERING) · airframe 24,743 hrs · 23,866 cycles

INFLIGHT WITH GEAR UP, RECEIVED NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE. COMPLIED WITH QRH & MESSAGE PERSISTS WITH GEAR DOWN. R & R LT & RT NWS RVDT'S IAW 32-51-20 TAXI TESTED GOOD IAW 09-20-00 SN OFF NSN 458 1-NSN 458 2 & SN ON D0720 D0709.

Part: SWITCH — FAULTY (THRUST REVERSER) · airframe 22,086 hrs · 21,249 cycles

WHILE CLIMBING THROUGH APPROXIMATELY 14,500FT CREW EXPERIENCED A RUMBLE SIMILAR TO CONTINUOUS LIGHT CHOP, FOLLOWED BY LEFT THRUST REVERSER UNLOCK CAUTION MESSAGE. CREW REQUESTED & RECEIVED CLEARANCE BACK TO 14,000. DESCENT WAS INITIATED AND QRH PROCEDURES PERFORMED. CREW WAS ABLE TO REGAIN USE OF THE LEFT ENGINE AND COORDINATED RETURN TO PHL PER THE QRH. DECLARED AN EMERGENCY AND LANDED ON RUNWAY 27L AND TAXIED TO THE GATE WITH NO ASSISTANCE. REMOVED AND REPLACED LEFT THRUST REVERSER STOW SWITCH IAW AMM 78-37-01 AND AWAC SUPPLEMENT 11-014. OPS CHECK GOOD.

Part: TRUNNION — DAMAGED (MLG) · airframe 21,702 hrs · 20,887 cycles

DURING COLD WORK OF FASTENER HOLES IN MLG TRUNNION FLANGES FOUND 2 EA OVERSIZED HOLES. REWORKED OVERSIZED FASTENER HOLES IN LEFT & RIGHT MLG TRUNNION FLANGES IAW REO 601R-57-21-1779.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 21,702 hrs · 20,887 cycles

COMPLIED WITH AWAC CARD 4DMI16047 REPAIR DENT BELOW GALLEY SERVICE DOOR. COMPLIED WITH AWAC J/C 4DMI16047 IAW BOMBARDIER REO 601R-53-21-2364 BY CUTTING OUT DAMAGE AND INSTALLING DOUBLER.

Part: GUIDE — CHAFED (TE FLAP) · airframe 21,702 hrs · 20,887 cycles

RIGHT O/B FLAP ROLLER GUIDE FITTING IS CHAFED. REPAIRED RIGHT O/B FLAP ROLLER GUIDE FITTING IAW REO 601R-57-53-956. REV -.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,702 hrs · 20,887 cycles

LBL 27 FLOORBEAM CAP FROM FS 574 TO FS 621 IS CORRODED AROUND SCREW HOLES. REPAIRED DAMAGED AREAS ON LBL 27 FLOORBEAM CAP FROM FS 574 TO 621 IAW REO 601R-53-00-005 REV B AND REO 601R-53-61-4691.

Part: FITTING — CHAFED (TE FLAP) · airframe 21,702 hrs · 20,887 cycles

LEFT O/B FLAP ROLLER GUIDE FITTING IS CHAFED. REPAIRED LEFT O/B FLAP ROLLER GUIDE FITTING IAW REO 601R-57-53-956 REV -.

Part: SKIN — DENTED (TE FLAP) · airframe 21,702 hrs · 20,887 cycles

LEFT I/B FLAP LOWER SKIN SURFACE HAS A DENT. REPAIRED DENT ON LEFT I/B FLAP LOWER SKIN IAW CRJ 200 SRM 57-52-00 SECTION B FIGURE 202 (SHEET 3).

Part: DOOR — CHAFED (LT MLG) · airframe 21,702 hrs · 20,887 cycles

LEFT MLG DOOR LEADING EDGE IS CHAFED IN SEVERAL PLACES. INSTALLED REPLACEMENT FILLER FROM PREVIOUS REPAIR IAW REO 601R-52-82-034.

Part: DOOR — CHAFED (MLG) · airframe 21,705 hrs · 20,887 cycles

REPAIRED MLG DOOR LEADING EDGE IS CHAFED IN SEVERAL PLACES. REMOVED AND REPLACED CHAFED FILLER AND BLENDED ADDITIONAL CHAFING UP FROM FILLER IAW CRJ 200 SRM 51-12-00. RESTORED FINISH TO A023.

Part: GUIDE — WORN (TE FLAP) · airframe 21,702 hrs · 20,887 cycles

RIGHT WING CONTACT POINT OF THE RIGHT O/B FLAP ROLLER GUIDE IS WORN. MEASURED & BLENDED AREA FOUND TO BE WITHIN LIMITS IAW B/A REO 601R-57-51-143.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,702 hrs · 20,887 cycles

CLIP CRACKED AT FS 484 LBL 36. REPAIRED CRACKED CLIP AT FS 484 LBL 36 IAW REO 601R-53-41-059 REV B.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,702 hrs · 20,887 cycles

LEFT INTERCOSTAL AT FS 621 & 625 ARE CRACKED. REMOVED & REPLACED LEFT INTERCOSTAL AT FS 621-625 IAW REO 601R-53-61-422.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,702 hrs · 20,887 cycles

RIGHT INTERCOSTAL LOCATED AT FS 621 & 625 ARE CRACKED. REMOVED & REPLACED RIGHT INTERCOSTAL AT FS 621 & 625 PER REO 601R-53-61-422.

Part: WARNING MESSAGE — ILLUMINATED (WINDOW HEAT) · airframe 21,189 hrs · 20,382 cycles

LEFT WINDOW HEAT CAUTION MESSAGE, COMPLIED WITH FIM RESET MESSAGE CLEARED. ABORTED TAKE OFF.

Part: LANDING GEAR — MALFUNCTIONED · airframe 21,110 hrs · 20,303 cycles

AFTER TAKEOFF, RECEIVED GEAR DISAGREE MESSAGE APPROX 6 SECONDS AFTER HANDLE SELECTION. IN TRANSIT MESSAGE CONFIRMED FOR ABOUT 20 MINUTES. MAINS SHOWED YELLOW DURING THE 20 MINUTES.

Part: SELECTOR VALVE — INOPERATIVE (MLG)

AFTER TAKEOFF, RECEIVED GEAR DISAGREE MESSAGE APPROXIMATELY 6 SECONDS AFTER HANDLE SELECTION. IN TRANSIT MESSAGE CONFIRMED FOR ABOUT 20 MINUTES. MAINS SHOWED YELLOW DURING THE 20 MINUTES. R & R MLG SELECTOR VALVE IAW 32-32-10. OPS CHECK/LEAK CHECK GOOD. GEAR RETRACTION/EXTENSION GOOD. REMOVED PLACARD AND FROM MEL.

Part: LANDING GEAR — MALFUNCTIONED · airframe 20,492 hrs · 19,666 cycles

AFTER TAKE OFF, RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES. NOSE GEAR INDICATED DOWN WHILE MAINS WERE UP. NOSE INDICATED DOWN AND GREEN THE ENTIRE TIME. RETURNED TO DEPARTURE. ALL GEAR LOCKED DOWN NORMALLY. FOUND OLEO EXTEND, F23 OUT OF RIG. RIGGED PS23 NOSE GEAR. OPS CHECKED NORMAL IAW AMM 32-61-05 AND AWAC SUP 10-087.

Part: SOLENOID — LEAKING (APU) · airframe 17,995 hrs · 17,055 cycles

FLT 3687, FUEL ODOR COMING FROM VENTS ON BOTH APU AIR AND ENGINE AIR INFLIGHT AND ON GROUND. INSPECTED APU ENCLOSURES FOUND FUEL SOLENOID VALVE. LEAKING WITH APU SHUTDOWN, NO LEAK NOTED. PLACED ON MEL. R & R APU FUEL SOLENOID VALVE IAW AMM 49-31-05. OPS AND LEAK CHECKED GOOD.

Part: BRACKET — CRACKED (BS 179) · airframe 17,679 hrs · 16,838 cycles

FWD LT BRACKET FOR NR 3 ACCUMULATOR IS CRACKED. R & R FWD LT BRACKET FOR NR 3 BRAKE ACCUMULATOR PN 601RA.

Part: TRACK — MISLOCATED (LT WING) · airframe 17,795 hrs · 16,843 cycles

FOUND TRACK RIVET AT LT OTBD L/E LOCATION TOO CLOSE TO SCREW HOLE. REPAIRED IAW REO 601R-57-41-747.

Part: PANEL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 17,795 hrs · 16,843 cycles

PAX DOOR PANEL 832ET CORROSION ON HINGE ABOVE TOP STEP. REMOVED UNSERVICEABLE HINGE AND REPLACED WITH SERVICEABLE HINGE IAW SRM 51-41-00.

Part: PANEL — DAMAGED (RT WING TE FLAP) · airframe 17,795 hrs · 16,843 cycles

(2) SCREW HOLES ON RT INBD FLAP L/E UNDER PANEL 684 JB ARE ELONGATED. REPAIR HOLES (2EA) ON RT INBD FLAP L/E UNDER PANEL NR 684 JB IAW REO 601R-57-52-1685.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 17,795 hrs · 16,843 cycles

LT MLG DOOR L/E IS CHAFED IN 2 PLACES. REPAIRED LOWER CHAFE DAMAGE ON LT MLG DOOR L/E IAW SRM 51-42-06 AND REO 601R-52-82-034. REPAIRED UPPER CHAFE DAMAGE ON LT MLG DOOR L/E IAW SRM 51-21-11, 51-25-06 AND 51-25-16.

Part: TRACK — CHAFED (RT PYLON) · airframe 17,795 hrs · 16,843 cycles

RT UPPER AND LOWER PYLON TRACK CHAFED. BLENDED OUT CHAFED DAMAGE ON RT UPPER AND LOWER PYLON TRACK FOUND REMAINING MATERIAL TO BE WITHIN LIMITS, IAW B/A REO 601R-78-34-3479 UPPER TRACK REMAINING THICKNESS .117 LOWER TRACK REMAINING THICKNESS .120. REQUIRED REMAINING THICKNESS, .115.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 17,795 hrs · 16,843 cycles

LT INBD 484 CLIP CRACKED, MATERIAL TAPE 7075-76 .050. REMOVED LT INBD 484 CLIP AND INSTALLED SERVICEABLE LT INBD CLIP, IAW SRM 51-42-06, 51-42-21. FABRICATED CLIP IAW SRM 53-41-23, REF FROM SHEET METAL TRACKER 412.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 17,795 hrs · 16,843 cycles

LT AILERON LWR SKIN OTBD L/E HAS CHAFE DAMAGE BLENDED OUT DAMAGED AREA ON LT AILERON LWR SKIN OTBD END OF L/E, MATERIAL ORIGINAL THICKNESS .090 ZONE 2 AND .055 ZONE 1 MATERIAL LOSS .005 IN ZONE 2, MATERIAL REMAINING .085 ZONE 2 AND .050 ZONE 1 FOUND TO BE WITHIN LIMITS IAW REO 601R-57-60-020.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 17,795 hrs · 16,843 cycles

RT MLG DOOR ASSY L/E IS CHAFED. REPAIRED RT MLG DOOR L/E IAW REO 601R-52-82-033, REV A AND 601R-52-82-034, REV NC STEP 6-12.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 17,795 hrs · 16,843 cycles

PAX DOOR STAIR STRUCTURE CRACKED NEXT TO AFT HANDRAIL BRACKET, 3RD STEP FROM TOP OF DOOR CUT OUT DAMAGED SECTION AND FABRICATED NEW SECTION AND INSTALLED IAW B/A 601R-52-11-702, REV C, ZONE 2.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 17,795 hrs · 16,843 cycles

PAX DOOR OUTER HANDLE IS CRACKED. REMOVED CRACKED OUTER HANDLE ON PAX DOOR THEN INSTALLED NEW SERVICEABLE OUTER HANDLE ONTO DOOR IAW AMM 52-11-03.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 17,795 hrs · 16,843 cycles

PAX DOOR STAIR STRUCTURE IS CRACKED NEXT TO FWD HANDRAIL BRACKET 3RD STEP FROM TOP STEP. CUT OUT DAMAGE SECTION THRU FABRICATED NEW PARTS NEW PARTS AND INSTALLED IAW B/A REO 601R-52-11-702, REV C, ZONE 2.

Part: PANEL — CORRODED (LT WING) · corrosion level 1 · airframe 17,795 hrs · 16,843 cycles

FUEL PANEL CUT OUT FOR 510AB HAS FRETTING CORROSION. REPAIRED CUT OUT CORROSION AT PANEL 510AB IAW REO 601R-57-21-030, REV H.

Part: PANEL — CRACKED (PAX DOOR) · airframe 17,795 hrs · 16,843 cycles

AFT DRAG ANGLE ON PAX DOOR STAIRS SIDE PANEL CRACKED AT PULLEY MOUNT. REMOVED CRACKED SECTION OF DRAG ANGLE AND SPLICED IN NEW SECTION IAW B/A REO 601R-52-11-513, REV A.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 17,795 hrs · 16,843 cycles

RT INBD FLAP VANE L/E CHAFED 3 SPOTS. REPAIRED 3 SPOTS ON RT INBD FLAP VANE L/E IAW REO 601R-57-52-004, REV C.

Part: BULKHEAD — CHAFED (BS280) · airframe 17,795 hrs · 16,843 cycles

AFT RT SIDE OF 280 BULKHEAD CHAFED FROM GALLEY LATCH. REPAIRED FS 280 BULKHEAD WEB AT RBL 11.0, BETWEEN STR 13A AND STR 14A IAW REO 601R-53-11-1727, REV 5, REPAIR NR 1.

Part: FLOORBEAM — CORRODED (BS 569) · corrosion level 2 · airframe 17,795 hrs · 16,843 cycles

LBL 27 FLOORBEAM CAP IN FRONT OF CARGO DOOR CORRODED AROUND NUTPLATE HOLES. REMOVED CORRODED FLOORBEAM CAP AT LBL 27.0 BETWEEN FS 569 IAW SRM 51-42-06 AND 51-42-21. DUPLICATED SERVICEABLE FLOORBEAM CAP IAW SRM 53-61-43 AND INSTALLED SERVICEABLE FLOORBEAM CAP AT LBL 27.0 BETWEEN FS 569 IAW REO 601R-53-6.

Part: SEAT TRACK — CORRODED (BS 394) · corrosion level 2 · airframe 17,795 hrs · 16,843 cycles

RBL9 SECOND SECTION OF FLOOR SEAT TRACK CORRODED. REMOVED UNSERVICEABLE SEAT TRACK FROM RBL 9 SECOND SECTION AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11F.

Part: SKIN — CHAFED (RT WING AILERON) · airframe 17,795 hrs · 16,843 cycles

RT AILERON UPPER AND LOWER L/E ARE CHAFED. BLENDED OUT CHAFE DAMAGE ON RT AILERON UPPER AND LOWER L/E. UPPER RT AILERON (MAX MATERIAL LOSS IN ZONE 1) .013 MAX ALLOWABLE .016, MAX MATERIAL LOSS IN ZONE 2, .021, MAX ALLOWABLE .027 LOWER RT MAX MATERIAL LOSS IN ZONE 1, .010 MAX ALLOWABLE .016 IAW REO.

Part: SEAT TRACK — GOUGED (BS 364-399) · airframe 17,795 hrs · 16,843 cycles

LBL 9 FIRST SECTION OF FLOOR SEAT TRACK GOUGED. REMOVED UNSERVICEABLE LBL 9 FIRST SECTION OF FLOOR SEAT TRACK AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 17,795 hrs · 16,843 cycles

LT AILERON UPPER SKIN L/E CHAFED IN 4 EA PLACES. REPAIRED LT AILERON UPPER SKIN L/E IAW REO 601R-57-60-013, REV NCN.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 17,795 hrs · 16,843 cycles

LT FLAP VANE L/E IS CHAFED IN 3 EA LOCATIONS. REPAIRED CHAFED ON LT FLAP VANE L/E ON 3 EA LOCATION IAW 601R-57-52-004, REV C.

Part: CASE — SPLIT (AGB) · airframe 17,498 hrs · 16,546 cycles

RECEIVED LT ENG OIL PRESSURE WARNING MESSAGE, OIL PRESSURE INDICATED BETWEEN 25-33 PSI, REDUCED THRUST AND OIL PRESSURE INDICATED 40 PSI, MESSAGE REAPPEARED IN 30 SECONDS, OIL PRESSURE INDICATED 25-35 PSI, SHUTDOWN ENG FOR REMAINING 15 MINUTES OF FLIGHT. DID NOT LAND OVERWEIGHT, BRAKE TEMPS NORMAL. REMOVED AGB ON LT ENG, SPLIT CASE AND VERIFIED METAL WAS CAUSED BY 2 BEARINGS. INSTALLED NEW AGB REF EMM 72-00-00. REINSTALLED FUEL PUMP AND MFG IAW EMM 72-00-00. OPS CK AND LK CK GOOD REF 223408/3 AND 223409/1 AND 2 FOR LRU. OPS CK AND INSTALL.

Part: OIL SYSTEM — FLUCTUATES (LT ENGINE) · airframe 17,486 hrs · 16,535 cycles

LT ENGINE OIL PRESSURE FLUX 28-44 PSI. CW QRH DIVERTED, OIL PRESSURE WARNING OCCURRED WHENEVER OIL PRESSURE INDICATED 28 PSI. TT FLUX 25 MINUTES. SERVICED ENGINE 5 PINTS OIL CHECKED MASTER SHIP DETECTOR IAW EMM 72-00-00, FAULT ISOLATION 15, FUZZ ON CHIP DETECTOR IS ALLOWABLE.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 16,203 hrs · 15,213 cycles

STEERING INOP CAUTION MSG 110 KTS ON TAKEOFF ROLL. ABORTED TAKEOFF, BRAKE TEMPS 10, 9, 9, 9. INTEROGATED NWS ECU. NO FAULTS. PERFORMED OPS TEST IAW AMM 32-51-00. OPS TEST GOOD PERFORMED TAXI TEST WITH CREW. NO DEFECTS NOTED.

Part: FEEL SENSOR — OUT OF ADJUST (AILERON) · airframe 15,728 hrs · 14,724 cycles

HIGHER THAN NORMAL CONTROL FORCE REQUIRED WHEN APPLYING AND NEUTRALIZING RT ROLL INPUTS FROM CTR OS ON BOTH YOKES IN FLIGHT. INSPECTED RIGGING OF AILERON FEEL AND SENSORY MECHANISM ON BOTH SIDES. ADJUSTED IAW AMM 27-11-00. OPS CHECK GOOD.

Part: ENGINE — FLUCTUATES (RIGHT) · airframe 14,866 hrs · 13,859 cycles

ON CLIMB ABOVE 10000 FT RT ENG FLUCTUATIONS, APPROX 2 PERCENT N1 AND N2, 200 LBS F/F AND 20/30 DEG ITT FOR SEVERAL MIN, THEN ENG STABILIZED, ON DESCENT AND APPROACH MULTIPLE REPEAT EPISODE OF FLUX EXPERIENCED FDR EVENTS NOTED. EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. RAN RT ENG WITH SPEED CONTROL OFF OPS CHECKS OK IAW 71-00. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,402 hrs · 12,455 cycles

MWC 132430-61 - FLOORBEAM AND CLIPS (2EA) CRACKED AT F/S 280.00 RBL 9.0, AT F/S 280.00 RBL 9.0, REPAIR PERFORMED IAW REO 601R-53-11-171. (K)

Part: STIFFENER — BENT (BS 621-640) · airframe 13,402 hrs · 12,455 cycles

MWC 132430-37 - ENGINE BEAM UPPER WEB STIFFENER BENT AT RBL 9.5. ENGINE BEAM UPPER WEB STIFFENER AT RBL 9.5 FABRICATED IAW CRJ 200 51-24-36, AND INSTALLED IAW SRM 51-42-06/51-42-21 AND TREATED IAW SRM 51-21-16. (K)

Part: SILL — CRACKED (FUSELAGE) · airframe 13,402 hrs · 12,455 cycles

MWC 132430-218 - CARGO BAY DOOR FLOOR SILL CRACKED AT FS 574.00 (1X.10 INCH + 0.120 INCH LENGTH) CARGO BAY FLOOR SILL CUTOUT AND PARTS FABRICATED IAW CRJ 200 REO 601R-53-61-1741. E/C PERFORMED, AMO 9-86. NO CRACK FOUND. PARTS ARE INSTALLED IAW CRJ200 REO 601-53-61-1741. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 13,402 hrs · 12,455 cycles

MWC 132430-95 - ANGLE AT FUSELAGE STA. 484.00, RBL 27.0 CRACKED. ANGLE AT F/S 484.00, RBL 27.0 FABRICATED IAW CRJ 200, SRM 51-24-36. ANGLE AT F/S 484.00 RBL 27.00, INSTALLED IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (K)

Part: STIFFENER — CRACKED (SUPPORT BEAM) · airframe 13,402 hrs · 12,455 cycles

MWC 132430-36 - ENGINE SUPPORT BEAM UPPER STIFFENER AT RBL 6 CRACKED (.200 FT LENGTH). ENGINE SUPPORT BEAM UPPER STIFFENER AT RBL 6 REPLACED IAW CRJ200 51-42-06 AND 51-24-36. (K)

Part: SUPPORT BRACKET — CRACKED (BS 193) · airframe 13,402 hrs · 12,455 cycles

MWC 132430-199 - CRACK EXISTS ON SKIN BEHIND AC GROUND POWER RECEPTACLE (ACCESS 122BR) AC GROUND POWER RECEPTACLE SUPPORT BRACKET REPLACED IAW SRM 51-42-06 AND 51-42-13. (K)

Part: SHIM — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 13,402 hrs · 12,455 cycles

SERVICE DOOR CUTOUT LOWER PROTECTIVE PLATE SHIM CORRODED. REPLACED SHIM ON IAW SRM 51-40-11. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 13,402 hrs · 12,455 cycles

MWC 132430-164- UPPER AFT FLOOR ANGLE CRACKED AT F/S 280.0, LBL 9.0 UPPER AFT FLOOR ANGLE AT F/S 280.0, LBL 9.0, REPAIR PERFORMED IAW CRJ 200 REO 601R-53-11-138. (K)

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 13,402 hrs · 12,455 cycles

MWC 132430-173 - PASSENGER DOOR ASSIST MOTOR STIFFENER FOUND CRACKED. PASSENGER DOOR ASSIST MOTOR STIFFENER REPLACED IAW SRM 51-42-13. (K)

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,402 hrs · 12,455 cycles

MWC 132430-162-BEAM AND CLIPS (2X) CRACKED AT F/S 280.00 LBL 9.0. REPAIR PERFORMED AT F/S 280.00, LBL 9.0 IAW CRJ 200 REO 601R-53-11-171, REV "SCHEME B". (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 13,402 hrs · 12,455 cycles

MWC 132430-180- ANGLE AT F/S 484.00, RBL 36 CRACKED. ANGLE AT F/S 484.00 CUTOUT IAW CRJ 200, REO 601R-53-41-059, EDDY CURRENT PERFORMED ON CUTOUT AND FABRICATED PARTS - PARTS FABRICATED AND INSTALL IAW REO 601R-53-41-059, REV A. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 13,402 hrs · 12,455 cycles

MWC 132430-170- PASSENGER DOOR STAIRS AFT DRAG ANGLE FOUND CRACKED. PASSENGER DOOR STAIRS AFT DRAG ANGLE REPLACED IAW REO 601R-52-11-513. (K)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 13,402 hrs · 12,455 cycles

MWC 132430-18- FWD PRESSURE BULKHEAD CRACKED ON LT SIDE AT F/S 202.75, W/L 66.275 AT PARKING BRAKE LOCATION. FWD PRESSURE BULKHEAD ON LT SIDE AT F/S 202.75, W/L 66.275, REPAIR IAW REO 601R-53-11-563. (K)

Part: STRUCTURE — CRACKED (APU BAY) · airframe 13,402 hrs · 12,455 cycles

MWC 132430-24 - APU ENCLOSURE CRACKED AT 2 LOCATIONS. REPAIRED PERFORMED IAW REO 601R-49-11-017. (K)

Part: PRESSURE BLKHD — CRACKED (BS 621) · airframe 13,402 hrs · 12,455 cycles

MWC 132431-25 - F/S 621.00 LHS, REAR PRESSSSUE BULKHEAD FOUND CRACKED AT LINTEL LOCATION (CRACK LENGTH .250) REPAIR PERFORMED ON FS 621.0 LT PRESSURE BULKHEAD AT LINTEL LOCATION IAW REO 601R-53-61-1230. (K)

Part: FLAP SYSTEM — FAILED (TE FLAP)

FLAPS FAIL AT ZERO DEGREES ON APPROACH DURING SELECTION TO 8 DEGREES. INFLIGHT AIR TEMP -28 DEGREES. C/W RESET PROCEDURE IAW SUP 98-018B, STEPS 1.3 AND 1.4 FLAP RESET, OK. (K)

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 12,456 hrs · 11,552 cycles

FIRST OFFICERS WINDSHIELD CRACKED DURING DESCENT. REF 186497/2 R&R RT WINDSHIELD. APPLIED AERODYNAMIC FILLER TO RT WINDOW STRAP. APPLIED SPEED TAPE. TAPE MUST BE REMOVED AFTER 48 HRS. IAW AMM 56-11-01 PLACED ON DIL.

Part: SKIN — DELAMINATED (RT WINGLET) · airframe 10,718 hrs · 9,845 cycles

REQUEST INSPECTION RIGHT WINGLET TRAILING EDGE DELAMINATED/PILOT FOUND ON WALK AROUND. (M)

Part: BPSU — FAILED (T/E FLAP)

REF 183967/2 DUE TO RECENT FLAP HISTORY AND CRJ AMM TEMP REVISION 05-035, AIRCRAFT REQUIRES FURTHER FLAP TROUBLESHOOTING AND RECTIFICATION CW CRJ AMM TR 05-035. REMOVED AND REPLACED LT BPSU, OPS TEST GOOD IAW AMM 27-51-10. (K)

Part: PITCH CONTROL — INOPERATIVE (PITCH FEEL) · airframe 10,152 hrs · 9,304 cycles

CONTROL COLUMN BINDS IN PITCH WHEN MOVED FORWARD AND AFT OF NEUTRAL AND FEELS HEAVIER THAN NORMAL THRU WHOLE RANGE OF MOVEMENT IN-FLIGHT AND ON GROUND AT ALL FLAP ANGLES. REMOVED AND REPLACED PITCH FEEL SIMULATOR. (K)

Part: DRIVE UNIT — MALFUNCTIONED (TE FLAPS)

FLAP FAIL CAUTION MESSAGE INFLIGHT. LANDED WITH FLAPS AT 8 DEGREES. LANDING WEIGHT 40,300 LBS. SPEED 150 KNOTS VERTICAL SPEED LESS THAN 400 FT MINUTE MAX BTMS READING =3. REMOVED AND REPLACED FLAPS POWER DRIVE UNIT IAW AMM 27-52-01. PERFORMED OPS CHECK IAW AMM 27-54-00, OPS CHECK GOOD. (K)

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS)

DURING MISSED APPROACH WHEN FLAP HANDLE MOVED TO 8 DEGREES, FLAP FAIL CAS MESSAGE ILLUMINATED AND FLAP STAYED AT 45 DEGREES. ALL 8 FLAPS ACTUATORS REPLACED ALSO RIGHT BPSU UNIT. REPLACED UE TO FLUCTUATION CAUSING JAMMING. FLAP SYSTEM. OPS CHECK GOOD.

Part: DRIVE ASSY — UNKNOWN (TE FLAPS) · airframe 9,982 hrs · 9,143 cycles

WHEN FLAP HANDLE SELECTED FROM 20 DEGREES TO 8 DEGREES IN FLIGHT, FLAP FAIL CAS MESSAGE STAYED AT 20 DEGREES. REMOVED AND REPLACED FLEX DRIVE NR 5 PER CRJ AMM 27-50-00, OPS CHECK GOOD. (M)

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 9,949 hrs · 9,108 cycles

AFTER TAKEOFF FLAPS FAILED AT 13 DEGREES OAT +6 DEGREES CELCIUS, WHEN FLAPS BEING RETRACTED FROM 20 DEGREES TO 8 DEGREES. RESET FLAPS IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4 FLAPS RESET, AIRCRAFT RELEASED FOR SERVICE. (K)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 9,903 hrs · 9,067 cycles

RECEIVED SMOKE CARGO WARNING MESSAGE FOR 5-10 SECONDS. INSPECTED CARGO COMPARTMENT AND FOUND NO EVIDENCE OF SMOKE OR FIRE. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS IAW 26-15-01, OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM)

HIGH SPEED ABORT DUE TO RED WARNING STAB CONFIGURATION. AIRCRAFT WEIGHT 47200 SPEED 120 KNOTS BRAKE TEMPS AFT 5 MINUTES 10, 8, 8, 8 (STAB CHANNEL 1 INOP). REMOVED AND REPLACED MOTOR CONTROL UNIT, HORIZONTAL STAB TRIM ACTUATOR, AND HORIZONTAL STAB TRIM CONTROL UNIT IAW AMM 27-40, OPS CHECK GOOD. (M)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 8,648 hrs · 7,859 cycles

LT WING LOWER PLANK ACCESS HOLE NR 1 FOR PANEL 540BR HAS FRETTING/ CORROSION DAMAGE AREA ABOUT 2 INCHES LONG AT FWD/ OB QUADRANT, NO IN CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 1 PANEL 540BB IAW BOMBARDIER REO 601R-57-21-030 REV A. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 8,648 hrs · 7,859 cycles

LT WING LOWER PLANK ACCESS HOLE NR 3 FOR PANEL 510BR HAS FRETTING/ CORROSION DAMAGE AT IB END 1 INCH LONG NOT IN CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 3 PANEL 510BB IAW BOMBARDIER REO 601R-57-21-030 REV A. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 8,648 hrs · 7,859 cycles

LT WING LOWER PLANK ACCESS HOLE NR 9 FOR PANEL 550AB HAS FRETTING/ CORROSION DAMAGE 1 INCH AREAS AT IB END NOT IN CRITICAL AREA. (K) [07-17-07] MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 9 PANEL 550AB IAW BOMBARDIER REO 601R-57-21-030 REV A. (M)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 8,648 hrs · 7,859 cycles

LT WING LOWER PLANK ACCESS HOLE NR 2 FOR PANEL 510AB HAS FRETTING/ CORROSION DAMAGE AT IB END, ALL ALONG FWD SIDE AND OB END, IN AND OUT OF CRITICAL AREA. S/D MAINTENANCE REPAIRED LT WING LOWER PLANK ACCESS HOLE NR 2 PANEL 510AB IAW BOMBARDER REO 601R-57-21-0303 REV A. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,648 hrs · 7,859 cycles

FS280, FLOORBEAM CLIP AT IB SIDE OF LBL 9.0 IS CRACKED IN RADIUS APPROX. .20 INCH LONG. S/D - MAINTENANCE REPLACED CLIP IAW BSC EO 601R-53-0057A. (K)

Part: INTERCOSTAL — CRACKED (FS 484) · airframe 8,648 hrs · 7,859 cycles

INTERCOSTAL AT FS 484.00 HAS CRACKED FLANGE AT LBL 27.0 CRACK MEASURES APPROX .50 INCH LONG. S/D MAINTENANCE REPLACED CLIP IAW BSC SR 601R-53-0029B. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,648 hrs · 7,859 cycles

INTERCOSTAL AT FS 484.00 HAS CRACKED FLANGE AT LBL 36.0 CRACK MEASURES APPROX .20 INCH LONG. S/D MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-53-41-059. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,648 hrs · 7,859 cycles

FS 280 FLOORBEAM CLIP AT OB SIDE OF RBL 9.0 IS CRACKED IN RADIUS APPROX .60 INCH LONG. (K) [07-17-07] MAINTENANCE REPLACED CLIP IAW BSC EO 601R-53-0057A. (M)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,648 hrs · 7,859 cycles

FS 280 FLOORBEAM CLIP AT OB SIDE OF LBL 9.0 IS CRACKED IN RADIUS APPROX .20 INCH LONG. (K) [07-17-07] MAINTENANCE REPLACED CLIP IAW BSC EO 601R-53-0057A. (M)

Part: INTERCOSTAL — CRACKED (FS 484) · airframe 8,648 hrs · 7,859 cycles

INTERCOSTAL AT FS 484.00 HAS CRACKED FLANGE AT RBL 27.0 CRACK MEASURES APPROX .20 INCH LONG. S/D MAINTENANCE REPLACED CLIP IAW BSC SR 601R-53-0029B. (K)

Part: FLOORBEAM — CRACKED (FS 280) · airframe 8,648 hrs · 7,859 cycles

FS 280, FLOORBEAM CLIP AT IB SIDE OF RBL 9.0 IS CRACKED IN RADIUS APPROX .30 INCH LONG. S/D MAINTENANCE REPLACED CLIP IAW BSC EO 601R-57-0057A. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,648 hrs · 7,859 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. (K) [07-17-07] MAINTENANCE REMOVED DAMAGED SECTION OF DRAG ANGLE AND INSTALLED REPAIR PARTS IAW REO 601R-52-11-513 REV A. (M)

Part: STRUCTURE — CRACKED (RT MLG)

RT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER PLUMBING (Z) MEMBER ASSY PN 601R75262-153, IS CRACKED THRU ON OB LEG. (K) [07-17-07] MAINTENANCE REPLACED ZEE MEMBER IAW CRJ SRM 51-42-06. (M)

Part: CHANNEL — CRACKED (LT MGL WW) · airframe 8,648 hrs · 7,859 cycles

LT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER HAT CHANNEL, PN 601R75262159, IS CRACKED AT OB LEGS LONGEST CRACK IS APPROX. .25 INCH LONG. (K) [07-17-07] MAINTENANCE REPLACED CHANNEL IAW CRJ SRM 51-42-06. (M)

Part: CHANNEL — CRACKED (RT MGL WW) · airframe 8,648 hrs · 7,859 cycles

RT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER HAT CHANNEL PN 601R75262157, IS CRACKED THRU ON IB LEGS. (K) [07-17-07] MAINTENANCE REPLACED CHANNEL IAW SRM 51-42-06. (M)

Part: TARGET — OUT OF ADJUST (MLG)

GEAR DISAGREE WARNING MESSAGE AFTER DEPARTING PHL. COMPLIED WITH QRH. GEAR DOWN 3 GREEN. (M) ADJUSTED RT MLG UPLOCK TARGET REF CMM 32-30-15, OPS CHECK GOOD. (K)

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 5,061 hrs · 4,402 cycles

FLAPS FAIL AT 8 DEGREES UPON FLAP RETRACTION. COMPLIED WITH SUPPLEMENT 98-18, FLAPS RESET, NO HISTORY IN PAST 72 HOURS. (K)

Part: WARNING LIGHT — FALSE INDICATION (MLG)

DURING GEAR RETRACTION, RECEIVED RED WARNING NOSE DOOR OPEN, GEAR DISAGREE LIGHT AND CAUTION STEERING INOPERATIVE WOW INPUT STATES MESSAGE WOW OUTPUT FAIL. RECONNETED TORQUE LINKS PERFORMED GEAR RETRACTIONS SWINGS IAW AMM CH23-30-00. NO DEFECTS OR WARNING NOTED SWINGS PERFORMED AFTER BOTH NLG TIRES CHANGED. INSPECTED NOSE FOR DAMAGE, NONE FOUND. (M)