N429AW

Part: STRUT — UNDERSERVICED (NLG) · airframe 44,100 hrs · 42,850 cycles

AFTER SELECTING GEAR LEVER UP NOSE GEAR REMAINED DOWN RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WRINGING MSGS C/W QRH ALL GEAR DOWN AND NORMAL LANDING. SMOOTH LANDING, LAND WEIGHT WAS 46,700. GEAR MESSAGES APPEARED, APPROX 10 SECONDS AFTER SELECTION. MANUAL RELEASE HANDLE USED. HYDS PUMPS IN AUTO THEN SELECTED TO ON AFTER QRH. EMERGENCY DECLARED. AIRCRAFT REMOVED FROM SERVICE. INSPECTED AND FOUND NLG SHOCK STRUT IMPROPERLY SERVICED. SERVICED NLG STRUT REF AMM SUPP 16-250A. C/W NLG SWING REF AMM 32-33-00. OPS CHECK GOOD. REF WO 342233 WORK CARD 4 FOR 24HR EXTENSION CHECK.

Part: ENGINE — FAULTED (RIGHT) · airframe 44,014 hrs · 42,745 cycles

IN CLIMB RIGHT ENGINE HAD SPIKE IN ITT AND REDUCTION IN N1 AND N2 AND WAS UNRESPONSIVE FOR 10-20 SECONDS. THEN RETURNED TO NORMAL. ON APPROACH RIGHT ENGINE AGAIN HAD SAME INDICATION AND AIRCRAFT HAD VIBRATIONS. DURING BOTH EVENTS THRUST WAS BEING REDUCED BY PILOTS. AIRCRAFT REMOVED FROM SERVICE. R&R RH ENGINE REF W/O 342015 FOR WORK PERFORMED REFERENCES, CHECKS AND RII'S.

Part: BRACKET — BENT (NLG WIRE HARNESS) · airframe 42,899 hrs · 41,428 cycles

GEAR DISAGREE WARNING AFTER SELECTING GEAR UP DEPARTING ORD. NLG NEVER MOVED & ALSO RECEIVED NLG DOOR OPEN WARING AFTER MLG DISAGREE WARING ACFT REMOVED FROM SERVICE. INTERROGATED PSEU & FOUND CODES: NG0EXT FAR S23, S35 NEAR NGDLK2, S21 NGDLK01, S22 FAR NGUPLK S30 FAR, LNDRCL S31FAR, RNDLCL S32 FAR. NDRUPLK S32 & FOUND PROX SENSOR HARNESS BRACKET BENT. REF 352506-2-3 352507-4 AND 352508-1-2 FOR R & R OF NLG HARNESS & SENSORS OPS CHECK & T/S ACFT. OK FOR SERVICE. REPLACED LOCK NUTS ON ELECRICAL HARNESS IAW AWAC SUP 12-029E ADJUSTED PROX SENSOR & COMPLETED POST INSTALL TEST OF NLG ELECRICAL HARNESS IAW AWAC SUP 12-029E OPS CHECKED GOOD, C/W RETRACTION & EXTENSION OF MLG. OPS CHECKED GOOD IAW AMM 32-30-00.

Part: BUSHING — WRONG PART (RT AILERON) · airframe 41,404 hrs · 39,789 cycles

ELONGATED HOLE DUE TO WRONG BUSHING INSTALLED. WRONG BUSHING OUTSIDE DIAMETER .750, INSIDE DIAMETER .627 / AILERON HOLE .815" OUTSIDE DIAMETER, .611" INSIDE DIAMETER. ***AIRCRAFT REMOVED FROM SERVICE ***** RH AILERON PN: CC670-13000-2 SN: 7711 UPWARD PCU IB SIDE OF FORK HAD WRONG BUSHING INSTALLED. WRONG PN INSTALLED PN: S10009-225Y. RIGHT PN: S6500B10P47. REF IPC 57-60-00 FIG 1A PG 3. REPLACED BUSHING IAW AMM 20-26-00.

Part: OIL SYSTEM — WARNING MESSAGE · airframe 41,123 hrs · 39,524 cycles

****SUPPLEMENTAL INFORMATION ******AT CRUISE NOTICED LH ENG OIL PRES FLUCTURATE BETWEEN 25-53 PSI NO MSG PRESENT. NORMAL DESCENT. ON SHORT FINAL RCVD LH ENG OIL PRES WARNING MSG INTERMIATELY. RAN QRH SHUTDOWN LH ENG. LANDED SAFELY. ***AIRCRAFT REMOVED FROM SERVICE*** UPON GVI FOUND LH ENG OIL TANK QUANITY LOW. REQUIRED 3.5 QTS TO FILL TO MAX. REF AMM 12-13-79. C/W LH ENG OIL CONSUMPTION CHECK IAW AWAC AMM SUP 05-014A OIL CONSUMPTION RESULTS 0 PTS IN 10 MINS CONSIDERED TO BE WITHIN LIMITS.

Part: NONE — NONE · airframe 40,730 hrs · 39,148 cycles

RECEIVED STALL FAIL CAUTION AT 500'. C/W QRH. DIVERTED TO DAY. ON GROUND PERFORMED GPWS TEST, GPWS FAIL STATUS MSG POSTED. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED GPWS TEST TO CLEAR GPWS FAIL MESSAGE. IAW AWA SUP 20-137. ALSO PERFORMED TEST OF STALL PROTECTION SYSTEM. IAW AMM 27-35-01 OPS TEST GOOD.

Part: TRIM SWITCH — FAULTED (FO FIRST OFFICER) · airframe 40,584 hrs · 39,005 cycles

RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES AT CRUISE. QRH DIRECTED FLAPS 20 LANDING, WHICH WAS SUCCESSFUL WITH NO ISSUES. ATTEMPTED TO REENGAGE MULTIPLE TIMES WITHOUT SUCCESS. AIRCRAFT REMOVED FROM SERVICE. ACARS EMAILS REPORT FO STAB TRIM DISCONNECT SWITCH STUCK. R&R FO STAB TRIM DISCONNECT SWITCH IAW AWA SUP 10-048D. OPS CHECK GOOD

Part: WARNING MESSAGE — ILLUMINATED (STAB TRIM) · airframe 40,569 hrs · 38,990 cycles

STAB TRIM CAUTION MSG IN FLT COULD NOT ENGAGE CHANNEL 1 OR 2 AT FLT LEVEL 340. CW QRH L.5 HRS LATER AT 6000 FT BOTH CHANNELS REENGAGED AND STAYED ENGAGED THE REMAINDER OF THE FLT. NORMAL LANDING FLAPS 20. AIRCRAFT REMOVED FROM SERVICE. PERFORMED SUP 05-029A. NO DEFECTS NOTED.

Part: NONE — NONE · airframe 40,397 hrs · 38,814 cycles

WHILE ENROUTE TO PWM THE CREW REPORTED RECEIVING A STAB TRIM AND MACH TRIM CAUTION. THEY DECLARED AND EMERGENCY AND WILL CONTINUE TO PWM. AT FL310 RECEIVED STAB & MACH TRIM CAUTIONS. C/W QRH, TRIM WOULD NOT RE-ENGAGE. ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESS

Part: SKIN — DENTED (LT WING LE) · airframe 39,813 hrs · 38,228 cycles

LEFT HAND WING INBOARD LEADING EDGE HAS 3 DENTS AT WS96.134-WS101.00, WS101.00 Ï¿½ WS108.70 AND WS124.10 - 131.80. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DRESS BACK OF DENTS #1 AND #3 TO ORIGINAL CONTOUR PER GREO 601R-57-41-436 REV A DATED 2013-06-19. PERFORMED DRESS BACK OF DENT #2 TO PER REO 601R-51-00-309 REV A DATED 2017-08-23 AND REO 601R-57-41-1130 REV (-) DATED 2021-07-19 WHICH IS A DEVIATION TO GREO 601R-57-41-436 REV A DATED 2013-06-19. #1 WS96.134-WS101.00, MEASURES L = 2.00Ï¿½ X W = 1.00Ï¿½ X D = 0.036Ï¿½. #2 WS101.00 Ï¿½ WS108.70, MEASURES L = 7.750Ï¿½ X W = 0.500Ï¿½ X D = .038Ï¿½. #3 WS124.10- 131.80, MEASURES L = 2.40Ï¿½ W = 2.00Ï¿½ X D = 0.043Ï¿½.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 39,813 hrs · 38,228 cycles

RH WING RIB CHANNEL IS PITTING CORROSION AT WS53.60 AND WHEEL WELL HYDRAULIC GUARD ACCESS PANEL AREA. ***AIRCRAFT REMOVED FROM SERVICE*** FOUND RIB CHANNEL CORROSION TO BE OUT OF LIMITS CREATING A HOLE THROUGH RIB CHANNEL THICKNESS OF 0.050Ï¿½. REMOVED AND REPLACED RH WING RIB CHANNEL P/N 601R10203-28 AT WS53.60 AND WHEEL WELL HYDRAULIC GUARD ACCESS PANEL AREA. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 57-21-12, SRM 51-42-20, SRM 51-23-00 AND SRM 51-42-06 REV 38.

Part: SKIN — CORRODED (FS 295-310 S0) · corrosion level 2 · airframe 39,813 hrs · 38,228 cycles

CORROSION ON SKIN AT UPPER TCAS ANTENNA AT TWO LOCATIONS BETWEEN FS295 TO FS310. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION AT TWO LOCATIONS ON SKIN AT UPPER TCAS ANTENNA LOCATION FS295 + 4Ï¿½, RH STR 0 + 2Ï¿½, DIMENSION L = 3.00Ï¿½ X W = 2.00Ï¿½ AND FS295 + 10Ï¿½, LH STR 0 + 2Ï¿½, DIMENSION L = 3.00Ï¿½ X W = 2.00Ï¿½. ORIGINAL THICKNESS OF 0.058Ï¿½ AND MATERIAL LOSS OF 0.002Ï¿½ REMAINING THICKNESS OF 0.056Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AIR WISCONSIN SUPPLEMENT NO.: 20-135A REV A, DATE OF ISSUE 5/12/2021.

Part: SKIN — SCRATCHED (LT WING TE FLAP) · airframe 39,813 hrs · 38,228 cycles

SCRATCH ON LH INBOARD FLAP UPPER SKIN AT INBOARD TRAILING EDGE. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED SRM 57-52-00 INBOARD FLAP REPAIR NO. 2 ON LH INBOARD FLAP UPPER SKIN AT INBOARD TRAILING EDGE. CUTOUT DAMAGED SECTION OF UPPER SKIN INBOARD TRAILING EDGE, DIMENSIONS ARE L = 3.100Ï¿½ X W = 3.100Ï¿½. FABRICATED DOUBLER, STRAP AND FILLER. DOUBLER DIMENSION L = 3.700Ï¿½ X W = 3.700Ï¿½. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW CRJ200 SRM 57-52-00 REV 38 AND SRM 51-21-11 REV 38.

Part: BULKHEAD WEB — DAMAGED (FS 621) · airframe 39,813 hrs · 38,228 cycles

THREE SCRATCH DAMAGES ON FORWARD FACE OF FS621 BULKHEAD WEB P/N 601R36008. #1 RBL23.875 TO RBL24.25 AT WL135.50 TO WL136.00, MEASURES L = 0.700Ï¿½ X W = 0.200Ï¿½ X D = 0.003Ï¿½ #2 RBL22.125 TO RBL22.325 AT WL134.25, MEASURES L = 0.400Ï¿½ X W = 0.200Ï¿½ X D = 0.003Ï¿½ #3 RBL20.50 AT WL132.125 TO 133.25, MEASURES L = 1.400Ï¿½ X W = 0.200Ï¿½ X D = 0.004Ï¿½ ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SCRATCH DAMAGES #1 AND #3 AT FS621 BULKHEAD WEB FORWARD FACE IAW REO601R53-61-7686 REV Ï¿½ DATED 2021-07-03. BLENDED SCRATCH #2 AT FS621 BULKHEAD WEB FORWARD FACE IAW REO601R53-61-2155 REV A DATED 2013-08-13.PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO601R53-61-7686 REV Ï¿½ DATED 2021-07-03 AND REO601R53-61-2155 REV A DATED 2013-08-13.

Part: FRAME — GOUGED (BS 718 S25R-26L) · airframe 39,813 hrs · 38,228 cycles

FUSELAGE FRAME AT FS718 HAS TWO GOUGES; 1 AT STR26L AND ANOTHER AT STR25R. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE AT FS718 AND STR26L MEASURING .280"L X .200"W X .011"D AND GOUGE AT FS718 AND STR25R MEASURING .600"L X .200"W X .013"D IAW CRJ200 SRM 51-12-00 REV 38. HFEC INSPECTION WAS PERFORMED AT BLEND AREAS WITH NO INDICATIONS FOUND IAW CRJ200 NDTM PART 1 51-20-06 REV 42. FABRICATED AND INSTALLED REPAIR ANGLES FROM NEW FRAME P/N: 600-36030-23 AT BLEND AREAS LOCATED AT FS718 AND STR26L AND STR25R IAW ASAP EA# AWAC-CRJ253-01648 REV IR DATED 06/22/2021. RESTORED SURFACE PROTECTION AT BOTH REPAIR AREAS IAW ASAP EA# AWAC-CRJ253-01648 REV IR DATED 06/22/2021.

Part: PLATE — CORRODED (FS 319-349) · airframe 39,813 hrs · 38,228 cycles

CORROSION ON DOOR SILL PANEL ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED SERVICE DOOR SILL PANEL P/N 601R38957-31 AND SHIM P/N 601R38695-19 AT FS319 TO FS349. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-40-11 REV 38.

Part: SKIN — DAMAGED (FS 559 S17-18L) · airframe 39,813 hrs · 38,228 cycles

ELONGATED FASTENER HOLE AND TOOLING DAMAGE LH AFT FUSELAGE SKIN AT FS559.00 + 64 Ï¿½ FS559.00 + 80 AND S17L Ï¿½ S18L. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED A REPAIR AT LH AFT FUSELAGE SKIN AT FS559.00 + 64Ï¿½ FS559.00 + 80 AND S17L Ï¿½ S18L. ELONGATED FASTENER HOLE MEASURES L = 0.392 X W = 0.2095Ï¿½ AND TOOL MARK MEASURES L = 1.090Ï¿½ X W = 0.300Ï¿½ X D = 0.008Ï¿½. CUTOUT DAMAGED SECTION OF SKIN, MEASURING 1.200Ï¿½ IN DIAMETER. CUT OUT SECTION OF STRINGER 18L MEASURES 13.50Ï¿½ IN LENGTH. FABRICATED DOUBLER AND FILLER. DOUBLER DIMENSION L = 8.700Ï¿½ X W = 6.650Ï¿½ AND FILLER DIMENSION IS 1.150Ï¿½ DIAMETER. CUTAWAY DAMAGED SECTION OF SKIN AND STRINGER. SMOOTHED AND BLEND ALL REWORKED AREAS, ADDED FILLER AND INSTALLED A REPAIR DOUBLER. PERFORMED HFEC WITH NO INDICATIONS. RESTORED ALL SURFACE FINISHES. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA # AWAC-CRJ253-01651 REV IR DATED 7/14/2021.

Part: ANGLE — DENTED (CARGO DOOR) · airframe 39,813 hrs · 38,228 cycles

CARGO DOOR FWD: TRACK FRAME HAS 4 EACH DENTS ON FLANGE AND THE UPPER/LOWER SUPPORT CHANNELS HAVE DENTS AND ARE BENT. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED/REPLACED FWD CARGO DOOR CAM TRACK ANGLE P/N: 601R35050-15 (NSN) AT FS 574 FROM STR 8LH TO STR 17LH IAW CRJ200 SRM 51-42-00 REV 38. DRESSED OUT UPPER AND LOWER SUPPORT CHANNELS AT FS 574.00 AND STR 8LH AND STR 17LH IAW CRJ200 SRM 51-24-16 REV38. HFEC INSPECTION WAS PERFORMED ON UPPER/LOWER SUPPORT CHANNELS AT FS 574.00 AND STR 8LH AND STR 17LH IAW CRJ200 NDT PART 1 51-20-06 REV42 WITH NO INDICATIONS FOUND AT THIS TIME.

Part: DOOR — CHAFED (RT WING BUTTE) · airframe 39,813 hrs · 38,228 cycles

RH BUTTE DOOR (694PB) HAS CHAFFING CONDITION ON LOWER SURFACE AT WS242. ****AIRCRAFT REMOVED FROM SERVICE****** BLENDED CHAFFING CONDITION ON RH BUTTE DOOR (694PB) LOWER SURFACE AT WS242. ORIGINAL MATERIAL THICKNESS 0.040Ï¿½, MATERIAL LOSS 0.006Ï¿½ WITH REMAINING THICKNESS 0.034Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA # AWAC-CRJ257-01650 REV IR DATED 6/24/2021.

Part: CHANNEL — DENTED (FS 689-694) · airframe 39,813 hrs · 38,228 cycles

AFT EQUIPMENT COMPARTMENT FUSELAGE FRAME CHANNEL FROM FS 689.5 TO FS 694.00 STR 24 LH HAS MULTIPLE DENTS. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGED FRAME CHANNEL AND REPLACED WITH FABRICATED FRAME CHANNEL AT FS 689.5 TO FS 694.00 STR 24 LH. NEW CHANNEL PART NUMBER 601-35013 FORMED IAW CRJ200 SRM 51-24-21 REV. 38. RESTORED SURFACE FINISH IAW CRJ200 SRM 51-25-00 REV 38. CHANNEL INSTALLED IAW CRJ200 SRM 51-42-21 AND SRM 51-42-06 REV 38. APPLIED TOPCOAT IAW CRJ200 SRM 51-25-00 REV 38.

Part: FRAME — DENTED (FS 682) · airframe 39,813 hrs · 38,228 cycles

DENTS AND GOUGES ON FUSELAGE AFT FRAME FS682.00Ï¿½ STR S26L TO S27. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE DAMAGE AND HAND DRESSED DENTS TO FUSELAGE FRAME AT FS682.00 STR S26L TO S27. DENT DAMAGE MEASURES L = 7.250Ï¿½ X W = 0.500Ï¿½ X D = 0.070Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01649 REV IR DATED 6/23/2021.

Part: FRAME — DENTED (FS 672 S26-27R) · airframe 39,813 hrs · 38,228 cycles

AFT FUSELAGE FRAME DENT FS672.20Ï¿½ STR26R-S27. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED FRAME AT AFT FUSELAGE FS672.20Ï¿½ STR26R-S27. DAMAGE MEASURES L = 1.300Ï¿½ X W = 0.700Ï¿½ X D = 0.048Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01647 REV IR DATED 6/20/2021.

Part: SKIN — DENTED (FS 625 S24-25R) · airframe 39,813 hrs · 38,228 cycles

AFT FUSELAGE SKIN DENT FS625.30 + 13.5Ï¿½ S24R AND S25. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT ON SKIN AT FS625.30 + 13.5Ï¿½ AND S24R AND S25R. MEASURES L = 0.650Ï¿½ X W = 0.500Ï¿½ X D = 0.005Ï¿½. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA #AWAC-CRJ253-1646 REV IR DATED 6/19/2021.

Part: BUSHING — EXCESS PLAY (HORIZONTAL STAB) · airframe 39,813 hrs · 38,228 cycles

REFERENCE 347219/1 HORIZONTAL STABILIZER EXCESSIVE PLAY. HORIZONTAL STABILIZER PIVOT BUSHING DIAMETER HOLES IN THE AIRCRAFT STRUCTURE ARE BELOW THE REQUIREMENTS AWA MAINTENANCE TASK CARD SUPPLEMENT NUMBER 19-154 REV B, DATED 07/16/2019. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED Ï¿½INSPECTION AND LUBRICATION OF THE PIVOT ASSEMBLY Ï¿½SERVICE BULLETIN 601R-55-007, 2B, PART B. FOUND INNER DIAMETER OF BUSHING P/N 600-23068-1 AND OUTER DIAMETER OF PIN OUT OF TOLERANCE ON LH AND RH SIDE. HFEC PERFORMED WITH NO INDICATIONS IAW CRJ200 NDT MANUAL 51-20-06 PART 1 REV 42 DATED OCT 10/20. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW AWA MAINTENANCE TASK CARD SUPPLEMENT NUMBER 19-154 REV B, DATED 07/16/2019.

Part: SKIN — DENTED (E/E BAY DOOR) · airframe 39,813 hrs · 38,228 cycles

AFT EQUIPMENT BAY DOOR PERMANENT REPAIR FS712.00Ï¿½ STR 24R. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED A PERMANENT REPAIR TO AFT EQUIPMENT BAY DOOR OUTER SKIN FS712.00 AND STR 24R. DAMAGE MEASURES L = 1.200Ï¿½ X W = 0.500Ï¿½ X D = 0.024Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ252-01524 REV C DATED 6/29/2021.

Part: OIL SYSTEM — OVERHEATED (RT ENGINE) · airframe 39,482 hrs · 37,876 cycles

DURING CLIMB THROUGH FL220, NOTICED RT ENGINE OIL TEMP CLIMBING AND INDICATING IN THE RED AT 166. CW QRH FOR HIGH OIL TEMP. POWER LEVER ADJUSTMENTS DID NOT PREVENT OIL TEMP FROM CLIMBING. PERFORMED INFLIGHT ENGINE SHUTDOWN, AFTER SHUTDOWN, NEVER RECEIVED LOW OIL PRESSURE WARNING. AFTER LANDING, WITH MOC ASSISTANCE, CHECK ENGINE EXCEEDANCES. HIGH OIL TEMP LOGGED. MAX TEMP WAS 167. NO OIL PRESSURE EXCEEDANCES RECORDED. LANDING WEIGHT WAS 46,800 LBS. NO ABNORMAL BREAK TEMPS. AIRCRAFT REMOVED FROM SERVICE. DRAINED OIL TANK AND AGB ON RT ENGINE. SERVICED RT ENGINE OIL, PER AMM 12-13-79. RAN ENGINE, OIL TEMP AND OIL PRESSURE GOOD.

Part: CABLE — DAMAGED (AUTOPILOT SERVO) · airframe 38,665 hrs · 37,036 cycles

L/H VERTICAL STABILIZER AUTO PILOT SERVO HAS RUST ON CABLE AT DRUM. FOUND AUTO PILOT SERVO SERVO CABLE P/N S 601R900200-79 AND 601R90020-131 WITH MULTIPLE BROKEN CABLE STRANDS. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED DAMAGED CABLES P/N S 601R900200-79 AND 601R90020-79 REF CRJ 200 AMM 27-00-00 AND OPS CHECKS OK REF CRJ 200 AMM 22-11-24 REV.60.

Part: FAIRING — DAMAGED · airframe 38,656 hrs · 37,030 cycles

L/H T/R DIFFICULT TO OPEN & HAD L/H REV UNLOCK CAUTION AFTER CLEARING RUNWAY AMBER ICON REV ICON ON N1 GAUGE LEVER WAS DIFFICULT TO MOVE. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED UPPER STANG FAIRING THAT WAS FOUND TO BE DAMAGED. NO FURTHER DAMAGE NOTED AT THIS TOME. TROUBLESHOT REV UNLOCK MSG PER FIM. LUBRICATED PDU LOCK PISTON , PERFORMED OPS CHECK OF T/R I/A/W CRJ200 AMM 71-00-00 REV 60 OPS CHK GOOD.

Part: WIRE HARNESS — FAULTY (MLG) · airframe 38,331 hrs · 36,723 cycles

SUPPLEMENTAL INFORMATION, WOW INPUT CAUTION MSG RECEIVED INTERMITTENTLY SEVERAL TIMES AFTER T/O AND EARLY CLIMB. GEAR WAS STOWED IN UP POSITION WHEN MSG RECEIVED, MSG CLEARED WITHIN 10 MIN OF FLIGHT. AIRCRAFT REMOVED FROM SERVICE HISTORY OF A S02 CODE STORED. REMOVED AND REPLACED UPPER SECTION OF THE NR 1 MLG WOW HARNESS REF SUP, SWUNG GEAR MULTIPLE TIMES ALL OPS SN OFF 500103539 SN ON 500103048.

Part: A/C PACK — FAILED (LEFT) · airframe 37,414 hrs · 35,858 cycles

AT APPROXIMATELY FL190, THE FLIGHT CREW NOTED THE FAILURE OF THE LEFT PACK, REDUCED AIRFLOW IN THE COCKPIT AND A CLIMBING CABIN PRESSURE. THE CREW INITIATED A DESCENT TO 10,000', DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. LOSS LT PACK DURING C/O. TRIED TO RESET WOULDNT RESET, LOW PRESSURE MSG. FLT LEVEL 200 TRIED REST OF PACK AT 55% N1.PACK RESET ON GROUND.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,013 hrs · 33,527 cycles

FWD SIDE OF APB IS CRACKED ABOVE AFT CARGO DOOR TRACK AT ITS END. FOUND ON HFEC INSP.

Part: FRAME — CRACKED (BS 333) · airframe 35,013 hrs · 33,527 cycles

BS 333 FRAME ABOVE UPPER PAX DOOR SILL WAS FOUND CRACKED. REPLACED.

Part: FRAME — CRACKED (BS 605) · airframe 35,013 hrs · 33,527 cycles

FRAME BS 605 IS CRACKED JUST ABOVE AND BELOW STRINGER 9L. REPAIRED THE FRAME.

Part: BRACKET — CRACKED (BS 461) · airframe 35,013 hrs · 33,527 cycles

LEFT FUSELAGE BRACKET AT BS 461 WAS FOUND CRACKED. REPLACED

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 35,013 hrs · 33,527 cycles

PAX DOOR AFT RISER DRAG ANGLE BY THE ASSIST MOTOR YOKE WAS CRACKED. REPLACED THE DRAG ANGLE.

Part: BRACKET — CRACKED (BS 461) · airframe 35,013 hrs · 33,527 cycles

RT FUSELAGE BRACKET AT BS 461 FOUND CRACKED. REPLACED THE BRACKET.

Part: ANGLE — CRACKED (BS 280 BEAM) · airframe 35,013 hrs · 33,527 cycles

BEAM AT BS 280 UPPER ANGLE IS CRACKED JUST OTBD OF THE MLG ALTERNATE CABLE EXTENSION PULLEY BRACKET, OTBD OF LBL 9.

Part: BRACKET — CRACKED (BS 473) · airframe 35,013 hrs · 33,527 cycles

RIGHT FUSELAGE BRACKET AT BS 473 FOUND CRACKED. REPLACED THE BRAKCET.

Part: BRACKET — CRACKED (BS 473) · airframe 35,013 hrs · 33,527 cycles

LEFT FUSELAGE BRACKET AT BS 473 WAS FOUND CRACKED. REPLACED THE BRACKET.

Part: MOUNT BRACKET — CRACKED (ASSIST MOTOR) · airframe 35,013 hrs · 33,527 cycles

PAX DOOR POWER ASSIST MOTOR MOUNTING BRACKET FOUND CRACKED. REPLACED THE MOUNT.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 33,013 hrs · 33,527 cycles

RIGHT INBD FLAP LOWER SKIN DENTED, 6 LOCATIONS AND PITTING IN TWO AREAS. REPLACED THE FLAP SKIN

Part: SKIN — CRACKED (BS 169-202) · airframe 35,013 hrs · 33,527 cycles

LEFT FWD FUSELAGE SKIN IS CRACKED AT BS 202 BY FWD EQUIPMENT BAY AFT LATCH. REPLACED THE SKIN.

Part: RISER — CRACKED (DOOR STEP) · airframe 35,013 hrs · 33,527 cycles

PAX DOOR LOWER STEP RISER IS CRACKED. REPAIRED IAW AWAC 13-134.

Part: BEAM — GOUGED (BS 618-621) · airframe 35,013 hrs · 33,527 cycles

BEAM INBD OF CARGO DOOR, BS 618 - 621 HAS SEVERAL GOUGES. REPLACED THE BEAM.

Part: ANGLE — CRACKED (CARGO DOOR BEAM) · airframe 35,013 hrs · 33,527 cycles

CARGO DOOR BEAM AFT LOWER ANGLE AT BS 621 BULKHEAD IS CRACKED. REPLACED THE BEAM.

Part: STRINGER — CRACKED (BS 364) · airframe 35,013 hrs · 33,527 cycles

STRINGER 3L AFT OF BS 364, PAX DOOR UPPER SILL IS CRACKED. REPAIRED THE STRINGER IAW SRM 53-00-03.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,013 hrs · 33,527 cycles

BATHTUB FITTING CRACKED AT FS 461, LBL9. REPLACED FITTING IAW SRM 51-42-06., 51-42-21.

Part: BRACKET — CRACKED (BS 202.75) · airframe 35,013 hrs · 33,527 cycles

LEFT LOWER NOSE HYDRAULIC COMPARTMENT BRACKET ABOVE ACCUMULATOR IS CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

FLOORBEAM CAP CORRODED AT FS574.00, RBL9 TO RBL27. REPLACED BEAM CAP IAW SRM5142-06, 53-00-00, 51-21-00, 51-41-11, 51-24-36.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

RIGHT FLOOR SEAT TRACK NR 2 CORRODED. REPLACED SEAT TRACK IAW SRM 53-01-11, REO601R-53-00-485 REV-C.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

RIGHT FLOOR SEAT TRACK NR 3 CORRODED. REPLACED SEAT TRACK IAW SRM 53-01-11, REO601R-53-00-485 REV-C.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

RIGHT SIDE PACKER PLATE CORRODED AT FS 310.00 TO 349.70, RBL47. REPLACED PACKER PLATE IAW SRM 53-41-43.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

RIGHT SIDEWALL SEAT TRACK NR 5 CORRODED FROM FS 449.85 TO 499.00. REPLACED SEAT TRACK NR 5 IAW SUPP 13-074.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

LEFT FLOOR SEAT TRACK NR 3 CORRODED. REPLACED SEAT TRACK IAW SRM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

LEFT FLOOR SEAT TRACK NR 4 CORRODED. REPLACED SEAT TRACK IAW SRM 53-21-49 AND REO 601R-53-00-485 REV-D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

LEFT SIDEWALL SEAT TRACK NR 3 CORRODED FROM FS409+16 TO 409+112. REPLACED SEAT TRACK NR 3 IAW SUPP 13-074.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

RIGHT FLOOR SEAT TRACK NR 1 CORRODED. REPLACED SEAT TRACK IAW REO 601R-53-00-485 REV-C, SRM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

LEFT SIDEWALL SEAT TRACK NR 6 CORRODED FROM FS 474.00 AND 544.00. REPLACED SEAT TRACK IAW SUPP 13-074.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

LEFT FLOOR SEAT TRACK NR 5 CORRODED. REPLACED SEAT TRACK IAW SRM 53-21-49 AND REO601R-53-00-485 REV-C.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

LEFT FLOOR SEAT TRACK NR 1 CORRODED. REPLACED SEAT TRACK NR 1 IAW SRM 51-40-11, 51-24-36, 51-21-06, AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

RIGHT FLOOR SEAT TRACK NR 5 CORRODED FROM FS559.00 TO 559+80. REPLACED SEAT TRACK IAW SRM 53-21-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

RIGHT SIDEWALL SEAT TRACK NR 6 CORRODED. REPLACED SEAT TRACK IAW SUPP 13-074.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

RIGHT SIDEWALL SEAT TRACK NR 3 CORRODED FROM FS 409+16 TO 409+112, RBL47. REPLACED SEAT TRACK NR 3 IAW SUPP 13-074.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

RIGHT SIDEWALL SEAT TRACK NR 2 CORRODED FROM FS364.00 TO 409+16, RBL 47. REPLACED SEAT TRACK IAW SUPP 13-074.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

RIGHT SIDEWALL SEAT TRACK NR 4 CORRODED. REPLACED SEAT TRACK IAW SUPP 13-074.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,013 hrs · 33,527 cycles

RIGHT FLOOR SEAT TRACK NR 4 CORRODED FROM FS 409+128 TO 559.00. REPLACED SEAT TRACK NR 4 IAW SRM 51-40-11.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,772 hrs · 33,273 cycles

NWS INOP CAUTION ON APPROACH. C/W QRH, MESSAGE PERSISTS. C/W FIM RESET MESSAGE CLEARED. NOTED BY MX

Part: TIRE — FAILED (NR 3) · airframe 34,243 hrs · 32,725 cycles

NR 3 MLG TIRE BURST

Part: TIRE — FAILED (NR 3 MLG) · airframe 34,242 hrs · 32,724 cycles

NR 3 MLG TIRE FAILED ON TAKEOFF R & R THE NR 3 MLG TIRE IAW SUP 12-015F.

Part: STATUS MESSAGE — ACTIVATED (COCKPIT) · airframe 32,296 hrs · 30,925 cycles

RECEIVED SMALL UN-COMMANDED YAW AND YAW DAMP 2 INOPERATIVE STATUS MESSAGE CLIMBING THRU FL 230.

Part: YAW DAMPER — DISENGAGED · airframe 32,296 hrs · 30,925 cycles

DURING FINAL DESCENT RECEIVED YAW DAMP 2 STATUS MESSAGE APPEARED, AND YAW DAMP 2 DIS-ENGAGED, UPON RE-ENGAGEMENT, ACFT UN-COMMANDED YAWED RT APPROXIMATELY 10 DEGREES. COMPLIED WITH QRH, DISCONNECTED YAW DAMPER FOR REMAINDER OF LIGHT.

Part: WARNING SYSTEM — MULTIPLE FAIL (COCKPIT) · airframe 32,181 hrs · 30,818 cycles

IMMEDIATELY AFTER TAKEOFF RECEIVED NOSE DOOR OPEN, PROXY SYS CHANNEL, PARKING BRAKE SOV, STEERING INOPERATIVE, ANTI-SKID INBD, ANTI-SKID OTBD, DID NOT RECEIVE GEAR DISAGREE MSG, LG LEVER STAYED IN DOWN LOCKED POSITION. FOLLOWED QRH & LANDED AT APPROX 46600 LBS.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZ STAB) · airframe 32,008 hrs · 30,657 cycles

REQUEST INSPECTION OF TRIM SYS FOR RUNAWAY PITCH TRIM ON APPROACH. FIRST OFFICERS CONTROLS.

Part: BRACKET — CRACKED (WINDSHIELD) · airframe 31,618 hrs · 30,301 cycles

LEFT CTR WINDSHIELD LOWER BRACKET CRACKED. R & R LT CTR WINDSHIELD LOWER BRACKET IAW SRM 51-42-21.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,619 hrs · 30,301 cycles

FRAME 333 HAS CORROSION ON THE FWD, TOP & AFT SIDES, BETWEEN STRINGER 23R - 21R, IN THE FWD E & E BAY.

Part: SKIN — DENTED (TE FLAP) · airframe 31,618 hrs · 30,301 cycles

LEFT INBD FLAP, LOWER SKIN SURFACE AFT OF THE INBD HINGE ARM HAS 2 DENTS. REPAIRED LT FLAP, LOWER SKIN SURFACE AT INBD HINGE ARM IAW EA CRJ257-00305 REV A.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,619 hrs · 30,301 cycles

FRAME 394 HAS CORROSION ON THE FWD & AFT SIDE, BETWEEN STRINGER 23L & 22L, IN THE FWD E & E BAY.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,618 hrs · 30,301 cycles

INTERCOSTAL ON TOP OF STRINGER 25R AT FS 364, CORRODED, REPAIRED.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 31,618 hrs · 30,301 cycles

NLG WW CUT OUT RT SKIN DOUBLER GOUGED, REPAIRED.

Part: HINGE — WORN (FUSELAGE) · airframe 31,618 hrs · 30,301 cycles

PASSENGER DOOR HINGE ON FUSELAGE SIDE WORN TO LIMITS, REPLACED.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,618 hrs · 30,301 cycles

SERVICE DOOR THRESHOLD IS CORRODED, REPLACED.

Part: SUPPORT BEAM — CHAFED (FUSELAGE) · airframe 31,618 hrs · 30,301 cycles

CARGO DOOR FWD TRACK SUPPORT BEAM HAS A HOLE CHAFED THROUGH, REPAIRED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,618 hrs · 30,301 cycles

SERVICE DOOR LOWER SILL HAS CORROSION AT MULTIPLE LOCATIONS, FROM FS 319 - 349.

Part: FRAME — CORRODED (BS 379) · corrosion level 2 · airframe 31,618 hrs · 30,301 cycles

FRAME BS 379 HAS CORROSION ON THE FWD SIDE, BETWEEN STRINGER 22 & 23R IN THE FWD E & E BAY.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,618 hrs · 30,301 cycles

APB AFT FACE INTERCOSTAL ATTACH ANGLE AT STRINGER 14 CRACKED.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 31,618 hrs · 30,301 cycles

RIGHT WING LE AT WS 143.189, UPPER SHROUD ATTACH ANGLE CRACKED, REPLACED.

Part: TORQUE BOX — CRACKED (THRUST REVERSER) · airframe 31,618 hrs · 30,301 cycles

NUMBER 1 ENG TR TORQUE BOX AFT FLANGE AT 7O CLOCK CRACKED, REPAIRED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,618 hrs · 30,301 cycles

CARGO SEAT RAIL BEAM, LBL 27 FROM FS 559.00+112 - 621.00, OTBD FLANGE FASTENER HOLES CORRODED, REPLACED.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,618 hrs · 30,301 cycles

FRAME 409 AFT SIDE LOWER ANGLE, BETWEEN STRINGER 26L & 26R CORRODED, REPLACED.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,618 hrs · 30,301 cycles

FLOOR SEAM ATTACH FITTING, RBL 27 INBD FLANGE, HAS A CORRODED FASTENER HOLE, REPAIRED.

Part: FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 31,618 hrs · 30,301 cycles

PASSENGER DOOR FWD ANCHOR FITTING CAP CORRODED, REPLACED.

Part: BEARING — WORN (RUDDER) · airframe 31,618 hrs · 30,301 cycles

LOWER RUDDER BEARING FAILED PROOF LOAD, REPLACED.

Part: PLATE — CORRODED (LT PYLON) · corrosion level 2 · airframe 31,618 hrs · 30,301 cycles

LEFT PYLON UPPER INBD BONDING PLATE CORRODED, REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,618 hrs · 30,301 cycles

COMPLIED WITH PERM REPAIR OF THE INTERCOSTAL AT STRINGER 13L, BETWEEN FS 621 & 625, REPLACED.

Part: ANGLE — CRACKED (WING) · airframe 31,618 hrs · 30,301 cycles

SHROUD ASSEMBLY ANGLE, BETWEEN 630KL & 630JL, OTBD END IS CRACKED, REPLACED.

Part: PANEL — CHAFED (AILERON) · airframe 31,318 hrs · 31,301 cycles

PANEL 599 AB IS CHAFED. REPAIRED PANEL 599 AB IAW ASAP EA CRJ257-00294 DATED 02 25 2016 & SUPPLEMENT 16-068.

Part: FLOOR SUPPORT — GOUGED (FUSELAGE) · airframe 31,618 hrs · 30,301 cycles

FS 559.00+80 FLOOR SUPPORT, BETWEEN LBL 9 & LT SILL HAS A GOUGE ON THE LOWER SURFACE OF THE AFT FLANGE ON THE OTBD FASTENER HOLE INTO THE RADIUS. REPAIRED FLOOR SUPPORT, BETWEEN LBL9 & LT FLOOR SILL IAW SUPPLEMENT 16-061 DATED FEB 23 2016.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,618 hrs · 30,301 cycles

STRINGER CLIP AT 3L JUST AFT OF THE 280.00 BULKHEAD IS CRACKED. REMOVED & REPLACED CLIP AT STRINGER 3L, JUST AFT OF THE FS 280.00 BULKHEAD IAW CRJ 200 SRM 51-42-06.

Part: WEB — CRACKED (FUSELAGE) · airframe 31,618 hrs · 30,301 cycles

RIGHT FWD E & E COMPARTMENT, FLOOR UNDER ADG PUMP IS CRACKED AT FS 193.00. REPAIRED CRACK AT RT FWD E & E OMPARTMENT, FLOOR UNDER ADG PUMP IAW REO601R-53-11-245 REV-B.

Part: BRACKET — CRACKED (LT BRAKE) · airframe 31,618 hrs · 31,301 cycles

LEFT BRAKE TRANSDUCER BRACKET IS CRACKED. R & R LT BRAKE TRANSDUCER BRACKET IAW SRM 51-42-06.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,618 hrs · 30,301 cycles

RIGHT WINDSHIELD SIDE POST OUTER LOWER ATTACH ANGLE CRACKED.. R & R CRACKED RT WINDSHIELD SIDE POST LOWER AFT ATTACH FITTING WITH SERVICABLE FITTING IAW SRM 51-42-21 & 51-40-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,618 hrs · 30,301 cycles

LEFT SIDE FS 484 FLOOR SUPPORT STRUCTURE CLIP AT LBL 27 IS CRACKED. R & R FS 484, LBL 27 CLIP, IAW CRJ 200 SRM 53-41-43, 51-40-11, 51-24-36 & REO 601R-53-41-059 REV-B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,618 hrs · 30,301 cycles

LEFT SIDEWALL SEAT TRACK, STICK BETWEEN FS 554 & 559+80 CORRODED, REPLACED.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 31,618 hrs · 30,301 cycles

PASSENGER DOOR UPPER WEB AFT REPAIR ANGLE IS CRACKED, REPAIRED.

Part: FLAP — FAILED (WING) · airframe 30,861 hrs · 29,590 cycles

FLAPS FAILED IN CRUISE AT FL 290 AT ZERO DEGREES. COMPLIED WITH QRH. HIGHEST BTMS READING WAS 9 UNITS. PERFORMED FLAP RESET PROCEDURE IAW SUPP 98-018G BOX 12. FLAPS RESET, PLACARDED & PLACED ON MEL.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,688 hrs · 29,415 cycles

FLIGHT ATTENDANT & PAX REPORT STRONG ODOR IN REAR OF ACFT ON LANDING, REQUEST INSPECTION. PACKS WERE OPERATING OFF APU AIR. RAN PACKS ON APU AIR, PRESSURIZED ALL 3 HYD SYSTEMS, NO ODOR NOTED AT THIS TIME. INSPECTED AFT EQUIPMENT BAY, NO LEAKS NOTED.

Part: LIGHT — MISSING (CABIN) · airframe 30,525 hrs · 29,240 cycles

TWO STRIPS FLOOR LEVEL EMERGENCY LIGHTING, ROW 1DF ORANGE OVERLAY STRIP MISSING. REPLACED IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 28,402 hrs · 27,222 cycles

DURING TAKEOFF ROLL AT APPROX 20 KNOTS, RECEIVED GEN 1 OFF CAUTION MSG. ABORTED TAKEOFF.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,242 hrs · 27,076 cycles

SECTION OF EMER LIGHTING ADJACENT TO ROW 6 LIGHTS OUT.

Part: ANGLE — BROKEN (RT ENG BEAM) · airframe 26,625 hrs · 25,577 cycles

ANGLE ON UPPER RT ENGINE BEAM IS BROKEN. R & R ANGLE IAW SRM 51-42-21.

Part: PANEL — CRACKED (PAX DOOR) · airframe 26,625 hrs · 25,577 cycles

PASSENGER DOOR FWD PANEL WHERE RADIUS OF TOP 7 MID STEPS JOIN CRACKED. REPAIRED PAX DOOR FWD PANEL IAW REO 601R-52-11-702 REV C.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,625 hrs · 25,577 cycles

FRAME FS 349 IN AVIONICS BAY IS CORRODED. R & R LOWER FRAME SECTION FS 349 WITH SERVICEABLE PN 601R32005-69 IAW CRJ 200 SRM 51-40-11 & 51-42-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,625 hrs · 25,577 cycles

REAR BULKHEAD AT LT STRINGER 13A INTERCOSTAL CRACKED ON RADIUS. COMPLIED WITH TEMPORARY REPAIR IAW REO 601R-53-61-5189.

Part: PANEL — CRACKED (PAX DOOR) · airframe 26,625 hrs · 25,577 cycles

PASSENGER DOOR AFT PANEL, WEB, RADIUS OF TOP & MID STEP JOINS IS CRACKED. REPAIRED PAX DOOR AFT SIDE PANEL IAW REO 601R-52-11-702 REV C DATED 03/09/2010.

Part: HINGE — DAMAGED (RUDDER) · airframe 26,625 hrs · 25,577 cycles

VERTICAL STABILIZER, RUDDER CTR HINGE, LOWER, BOTH UPPER & LOWER HALVES ARE DAMAGED. REPLACED THREE EACH HINGE HALVES IAW AWAC SUPPLEMENT 12-030 & 3-12-2012.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,625 hrs · 25,577 cycles

FLOOR BEAM CAP AT LBL 27 IN CARGO AREA CORRODED. R & R SECTION OF FLOOR BEAM CAP ON LBL 27 FROM FS 559+106 TO FACTORY SPLICE FWD OF FS 574 IAW SPLICE REPAIR CRJ 200 SRM 53-00-43.

Part: TRUNNION — DAMAGED (MLG) · airframe 26,625 hrs · 25,577 cycles

DURING COLD WORKING OF MLG TRUNNION LOWER FLANGES, FOUND EXISTING OVERSIZED HOLES. ONE ON LT & EIGHT ON RT SIDE. REPAIRED OVERSIZED HOLES ON LT & RT MLG TRUNNIONS IAW REO 601R-57-21-2112.

Part: ANGLE — CRACKED (LT WING) · airframe 26,625 hrs · 25,577 cycles

UPPER ANGLE BEHIND TRANSITION DUCT ON LT WING IS CRACKED. REMOVED CRACKED ANGLE & REPLACED WITH NEW SERVICEABLE ANGLE IAW CRJ 200 SRM 51-42-02,51-42-06.

Part: DRAG ANGLE — CRACKED (LT MLG WW) · airframe 26,625 hrs · 25,577 cycles

LEFT MLG WW DRAG ANGLE CRACKED ON AFT SIDE. R & R DRAG ANGLE IAW SRM 51-42-21.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 26,625 hrs · 25,577 cycles

CARGO DOOR HANDLE HOUSING CRACKED. REMOVED UNSERVICEABLE CARGO DOOR HANDLE & INSTALLED A NEW SERVICEABLE HANDLE PN H3415-23 IAW CRJ 200 SRM 51-40-11, 51-42-21, 51-25-06, 51-25-16 & 51-23-00.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 26,625 hrs · 25,577 cycles

CRACKED STIFFENER IN RT MLG WW JUST BELOW & OTBD OF MLG P LOCK. R & R SERVICEABLE STIFFENER ON RT WW PN 600-10389-2

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 26,625 hrs · 25,577 cycles

BULKHEAD GOUGED FROM GALLEY FWD LOWER DOOR. PERFORMED REO 601R-53-11-1727 TO REPAIR GOUGES TO PILOT BULKHEAD FS 280.

Part: RIB — CRACKED (RT WING) · airframe 26,625 hrs · 25,577 cycles

RIGHT BATT RIB CRACKED WS 53.60. REPAIRED BATT RIB IAW REO 601R-57-51-046 REV B DATED 2002-02-28.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 26,625 hrs · 25,577 cycles

BRAKE PRESS TRANSDUCER BRACKETS CRACKED IN RT WW. R & R WITH SERVICEABLE PARTS PN 601R75262-157 & 601R75262-155 IAW CRJ 200 SRM 51-40-11 & 51-42-06.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,625 hrs · 25,577 cycles

TIE DOWNS IN CARGO BAY CORRODED BEYOND LIMITS ON LBL 9. R & R TWO EACH PN 601R38663-21 PLATES IAW CRJ 200 AMM 53-01-11.

Part: SILL — CRACKED (FUSELAGE) · airframe 26,625 hrs · 25,577 cycles

CARGO DOOR SILL CRACKED AT FWD & AFT STOP FITTINGS. REPAIRED CARGO DOOR SILL AT FWD TO AFT STOP FITTINGS IAW REO 601R-53-61-433.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,625 hrs · 25,577 cycles

UNDERFLOOR CLIP CRACKED AT LBL 36 & FS 484. R & R WITH SERVICEABLE PART IAW REO 601R-53-41-059 REV B DATED 2009-09-16.

Part: BALLAST — MALFUNCTIONED (LAVATORY) · airframe 23,371 hrs · 22,451 cycles

STRONG ELECTRICAL SMELL IN LAV. REMOVED AND REPLACED LAVATORY LIGHT ASSY BALLAST IAW AMM 33-23-00. NO BURN ELECTRICAL SMELL NOTICED.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 22,853 hrs · 21,952 cycles

FLAPS DEGRADED - WHILE DESCENDING THRU 17,000 FT A/P ENGAGED. VERT SPEED SET AT 1500 FPM & SPEED AT 280 KIAS, AIRPLANE PITCHED NOSE-DOWN MOMENTARILY. OVERSPEED TAPE APPEARED ON SPEED TAPE. RECEIVED FLAPS DEGRADED STATUS MESSAGE. RECEIVED HYD PUMP 2B & 3B CAUTION MESSAGES MOMENTARILY. EACH TIME THE OVERSPEED TAPE APPEARED, FLT CONTROLS WOULD FEEL HEAVY WHILE HAND-FLYING. FLAPS WERE AT ZERO WITH NO FLAP HANDLE SELECTIONS WERE MADE. R & R LT FLAP POSITION TRANSMITTER IAW AMM 27-55-01. OPS CHECK GOOD.

Part: CARGO TRACK — CORRODED (BS 610) · airframe 21,914 hrs · 21,015 cycles

CARGO TIE DOWN TRACK CORRODED. INSTALLED SERVICEABLE CARGO TIE DOWN AMM 53-01-11.

Part: ELEMENT — SHORTED (OVERHEAT LOOP) · airframe 21,917 hrs · 21,018 cycles

LEFT JETPIPE FAIL CAUTION MESSAGE FOLLOWED BY LEFT JETPIPE OVERHEAT WARNING MESSAGE, COMPLIED WITH QRH, MESSAGE CLEARED AT 50 PERCENT N1. FOUND ELEMENT TERMINALS SHORTING TO GROUND. REPOSITIONED ITEMS IAW AMM 26-11-04. CHECKED LOOPS A & B FOR SHORT TO GROUND, NONE FOUND. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FS 589-605) · corrosion level 2 · airframe 21,914 hrs · 21,015 cycles

LBL 27 HAS MULTIPLE AREAS OF CORROSION ON INBD AND OTBD SIDE OF FLOOR SUPPORT FS 589-621. REMOVED UNSERVICEABLE LBL27 FLOOR BEAM CAP AND REPLACED WITH SERVICEABLE FLOOR BEAM CAP IAW REO 601R-53-61-3778, REV A AND SRM 51-42-06, 51-42-21, 51-40-11 AND SRM 51-42-22.

Part: RIB — DAMAGED (LT WING TE FLAP) · airframe 22,116 hrs · 21,224 cycles

LEFT INBD FLAP HAS MISDRILLED HOLES UNDER INBD SEAL PN 601R14016-31 RIB ASSY. R & R LT INBD RIB ASSY PN 601R14016-31.

Part: RIB — DAMAGED (LT WING TE FLAP) · airframe 21,914 hrs · 21,015 cycles

LEFT INBD FLAP HAS MISDRILLED HOLES UNDER INBD SEAL PN 601R14016-31 RIB ASSY. R & R LT INBD RIB ASSY PN 601R14016-31.

Part: STEP — CRACKED (PAX DOOR) · airframe 21,914 hrs · 21,015 cycles

FWD AND AFT SIDE OF PAX DOOR AT 3RD STEP CRACKED. REPAIRED AFT SIDE OF PAX DOOR IAW REO 601R-52-11-702, REV C FWD SIDE WAS NDT AND FOUND TO NOT BE CRACKED.

Part: PANEL — DAMAGED (PAX DOOR) · corrosion level 2 · airframe 21,914 hrs · 21,015 cycles

PAX DOOR ASSIST CABLE PANEL DAMAGED. REPAIRED PAX DOOR AFT SIDE PANEL IAW REO 601R-52-11-2048.

Part: SILL — CORRODED (PAX DOOR) · airframe 21,914 hrs · 21,015 cycles

PAX DOOR LOWER SILL CORRODED AND CRACKED THE ENTIRE LENGTH OF THE DOOR. REMOVED CORRODED, CRACKED DOOR SILL IAW SRM 51-42-06 FAB NEW SILL IAW SRM 53-21-23. INSTALLED NEW PAX DOOR SILL IAW SRM 51-42-06.

Part: ATTACH ANGLE — CRACKED (FS 484) · airframe 21,914 hrs · 21,015 cycles

LEFT FS 484, BL 27 INBD ATTACH ANGLE IS CRACKED. R & R ANGLE IAW REO 601R-53-41-059, REV B.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 21,914 hrs · 21,015 cycles

CARGO TRACKS CORRODED. R & R FLOOR TRACKS IAW AMM 53-01-11.

Part: CARGO TRACK — CORRODED (FS 574-559) · airframe 21,914 hrs · 21,015 cycles

CARGO TIE DOWN FLOOR TRACKS FS 574 AND 559+112. R & R TRACK DUE TO EXFOILIATION IAW AMM 53-01-11.

Part: FITTING — WORN (LT WING) · airframe 21,914 hrs · 21,015 cycles

STUB FAIRING FITTING ON LT WING WORN. REMOVED WORN STUB FITTING IAW SRM 51-42-06 LOCATED, DRILLED, AND DEBURRED. NEW STUB FAIRING FITTING PN 601R10371-1 IAW SRM 51-40-11. INSTALLED NEW STUB FITTING IAW SRM.

Part: ANGLE — CRACKED (FS 625) · airframe 21,914 hrs · 21,015 cycles

LT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-40-11. LOCATED, DRILLED, AND INSTALLED NEW ANGLE IAW SRM 51-40-11. TREATED, PRIMED, AND TOP COATED IAW SRM 51-25-16, 51-25-06.

Part: FAIRING — CHAFED (RT WING) · airframe 21,914 hrs · 21,015 cycles

RT STUB FAIRING CHAFED. REPLACED RT STUB FAIRING WITH SERVICEABLE STUB FAIRING.

Part: PRIORITY VALVE — INOPERATIVE (NLG) · airframe 21,097 hrs · 20,147 cycles

GEAR DISAGREE WARNING INFLIGHT WITH UNSAFE NOSEWHEEL INDICATION. COMPLIED WITH QRH. NOSE WHEEL SHOWED SAFE PRIOR TO EMERGENCY GEAR EXTENSION HANDLE BEING PULLED. EXECUTED NORMAL LANDING. DOWNLOADED DATA VERIFIED GEAR DISAGREE WAS "28 SECOND" FAULT ALSO VERIFIED MLG`S WENT DOWN AND LOCKED NLG UPLOCK RELEASED NLG FAILED INTRANSIT, PERFORMED FUNCTION TEST OF NLG PRIORITY VALVE. FAILED TEST R & R NLG PRIORITY VALVE, OPS CHECK GOOD.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 20,391 hrs · 19,398 cycles

ON CLIMBOUT, SMELLED ELECTRICAL BURNING ODOR IN COCKPIT AND CABIN. BOTH PACKS REMAINED ON WITH ENG AIR. APU WAS OFF. CABIN LIGHTING REMAINED ON. ODOR WAS STRONGEST FROM ROW 8, AFT. REMOVED AND INSPECTED LIGHT BALLAST AT 11/12 DF OVERHEAD CENTER UPON REINSTALLATION FOUND BALLAST FAILED. NO EVIDENCE OF EXTERNAL SHORT. INSPECTED AND RELAMPED OVERHEAD LIGHTS AT 11DF. NO DAMAGE FOUND AND LAMPS OPERATE NORMALLY. NO EVIDENCE OF ELECTRICAL SHORT REF 33-21-01.

Part: ATTACH FITTING — WORN (LT MLG DOOR) · airframe 20,134 hrs · 19,125 cycles

LT MLG DOOR ATTACH FITTING WORN BEYOND LIMITS. R & R ATTACH FITTING.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 17,065 hrs · 15,894 cycles

LT SIDEWALL SEAT RAIL HAS SMALL AREA OF CORROSION UNDER OVER WING DOOR CUTOUT TOWARD CTR. R & R SEAT RAIL.

Part: ATTACH FITTING — CRACKED (LT WING) · airframe 17,065 hrs · 15,894 cycles

OTBD ACTUATOR ATTACH FITTING IS CRACKED ON LT WING T/E UNDER SPOILERON. R & R OTBD ACTUATOR FITTING WITH NEW IAW SRM 51-42-06, 51-42-21 AND 51-42-22.

Part: FITTING — CHAFED (LT WING TE FLAP) · corrosion level 1 · airframe 17,065 hrs · 15,894 cycles

LT OB FLAP HINGE BOX AFT FITTING CHAFED. REPAIRED LT WING OTBD FLAP OB HINGE BOX AFT HINGE FITTING IAW REO 601R-57-21-1232.

Part: VANE — CRACKED (THRUST REVERSER) · airframe 17,065 hrs · 15,894 cycles

RT ENGINE THRUST REVERSER TOP CASCADE HAS 1 (EA) VANE GOUGED AND 1 (EA) VANE CRACKED. REPAIRED 1 INCH CRACK & 1 GOUGE ON RT ENGINE T/R TOP CASCADE IAW DWG AW 78-30-0711-04.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 17,065 hrs · 15,894 cycles

PAX DOOR ASSIST MOTOR LOWER MOUNT FITTING CRACKED. REMOVED CRACKED STIFFENER AND REPLACED WITH NEW SERVICEABLE STIFFENER PN 601R317745-7.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,065 hrs · 15,894 cycles

CORROSION FOUND AT FS 333.00, STRINGER 26L-26R FLANGE. ALSO CORROSION FOUND AT FS 349.00, STRINGER 26L-27L. REPAIRED DAMAGE TO FS 333.00, STRINGER 26L-26R IAW REO 601R-53-21-1092. REPAIRED DAMAGE TO FS 349.00, STRINGER 26L-27L IAW REO 601R-53-21-1091.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 17,065 hrs · 15,894 cycles

PAX DOOR INNER HANDLE SUPPORT ANGLE CRACKED. REMOVED CRACKED ANGLE AND DUPLICATED IAW SRM.

Part: ANGLE — CRACKED (BS 625) · airframe 17,065 hrs · 15,894 cycles

RT OBLIQUE ANGLE UNDERBEAM CRACKED. REMOVED RT OBLIQUE ANGLE AND REPLACED RT OBLIQUE ANGLE IAW SRM 51-24-16.

Part: ANGLE — CRACKED (BS 621) · airframe 17,065 hrs · 15,894 cycles

LT OBLIQUE ANGLE UNDER ENGINE BEAM CRACKED. R & R LT OBLIQUE ANGLE PN 601-35012-51 IAW SRM 51-40-11, 51-42-21, 51-25-16.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 13,637 hrs · 12,571 cycles

FLAP FAIL CAUTION MESSAGE. FLAPS AT ZERO. DIVERTED TO BWI. FOUND LT BPSU CODES CONTINUITY CHECK AND MEGGED LT WING WIRING PER WM AND FIM CHAP 27. NO FAULTS FOUND. CURRENT BPSU INSTALLED HAS REPEAT HISTORY OF FAULTS IN OTHER ACFT. SUSPECT BAD PART. REPLACED BPSU PER AMM CHAP 27. FLAP OPS CHECK GOOD. S/N OFF 2243, S/N ON 1995

Part: BPSU — MALFUNCTIONED (T/E FLAP) · airframe 13,595 hrs · 12,525 cycles

FLAPS FAIL CAUTION MESSAGE. FLAPS FAILED AT 8 DEGREES IN FLIGHT. R&R RT BPSU AND RE-RIGGED FLAPS IAW AMM 27-50.

Part: DOOR — STIFF (MAIN PAX) · airframe 13,171 hrs · 12,118 cycles

PASSENGER DOOR WILL NOT OPEN WITHOUT EXCESSIVE FORCE. CLEANED AND LUBED PAX DOOR IAW AMM 12-26-52 AS REQUIRED OPS CHECKS SEVERAL TIMES NO DEFECTS NOTED AT THIS TIME. (A)

Part: GENERATOR — FAILED (NR 1) · airframe 12,665 hrs · 11,636 cycles

DEPARTING BUFFALO, GENERATOR NR 1 DROPPED OFF LINE AT 700 FT PER QRH RESET. GENERATOR 2 DROPPED OFF LINE AT 1200 FT AND RESET PER QRH. BOTH GENERATORS OFF LINE FOR APPROXIMATELY 1 MINUTE. SERVICED GEN/IDG 1 WITH 4-5 PUMPS OF OIL. OPS CHECK GOOD. NO LEAKS NOTED REF MM 12-13-24-610-801. OPS CHECK PER 24-20-00-710-801. ACFT OK FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 12,619 hrs · 11,598 cycles

FIRST OFFICERS SIDE WINDOW CRACKED. REMOVED AND REPLACED WINDOW IAW AMM 56-12-01.

Part: STRUCTURE — CRACKED (CABIN) · airframe 12,335 hrs · 11,323 cycles

REPAIR CRACK ON PAX DOOR AFT SIDEWALL LOWER SIDE FWD OF DOOR ASSIST MOTOR PULLEY ASSY. (K) CRACK ON PAX DOOR REPAIRED IAW REO 601-52-11-513 REV A. (M)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 12,335 hrs · 11,323 cycles

CRACK FOUND ON REAR PRESSURE BULKHEAD WEB FS 621.00, WL 106.17, LBL 36.00 (LINTEL ATTACHMENT FITTING). (K) REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1230 REV D. (M)

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 12,335 hrs · 11,323 cycles

CRACK SUSPECTED IN AC GROUND POWER BOX. (K) A/C CONNECTOR SUPPORT MEMBER REPLACED IAW SRM 51-42-06. (M)

Part: BRACKET — CRACKED (FUSELAGE) · airframe 12,335 hrs · 11,323 cycles

CRACK EXIST ON BRACKET FS 280, LBL 9, ABD RBL 9 CRACK LENGTH .200. (K) REPAIR PERFORMED IAW REO 601R-53-11-171, FABRICATED NEW ANGLE. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,335 hrs · 11,323 cycles

CRACK EXIST ON INTERCOSTAL FS 484, RBL 36 CRACK LENGTH .200. (K) REPAIRED INTERCOSTAL IAW REO 601R-53-41-059. (M)

Part: STRUCTURE — CRACKED (FUSELAGE)

CRACK EXIST ON FLOOR STRUCTURE FS 280, RBL 9 CRACK LENGTH .150. (K) CUT OUT DAMAGE IAW REO 601R-53-11-171. REPAIR PERFORMED IAW REO 601R-53-11-171. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,335 hrs · 11,323 cycles

CRACK EXIST ON INTERCOSTAL FS 481, LBL 36 AND LBL 27 CRACK LENGTH .200. (K) REPAIRED IAW REO 601R-53-41-059. (M)

Part: SCUFF PLATE — CORRODED (SERVICE DOOR) · corrosion level 1 · airframe 12,335 hrs · 11,323 cycles

SCUFF PLATE OF SERVICE DOOR FOUND CORRODED. (K) SCUFF PLATE REPLACED IAW SRM 51-42-06 AND 51-41-02. (M)

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 12,335 hrs · 11,323 cycles

ANGLE CRACK AT FS 621.0 AND MEMBER BEAM OF CARGO DOOR. (K) ANGLE REPLACED IAW SRM 51-2-16 AND 51-42-20. (M)

Part: RADOME — CRACKED (FUSELAGE) · airframe 12,335 hrs · 11,323 cycles

LIGHT GLAZING ON RADOME FOUND CRACK. (K) REPLACED IAW SRM 51-42-20. (M)

Part: SILL — CRACKED (FUSELAGE) · airframe 12,335 hrs · 11,323 cycles

CRACK FOUND ON LOWER SILL FS 572, LBL 40, UNDER BRACKET SCUFF PLATE RETAINER. LOWER SILL PLATE REPLACED IAW REO 601R53-61-690 REV D. (M)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 12,335 hrs · 11,323 cycles

LT LWR NOSE COMPARTMENT CRACK FOUND ON PRESSURE BULKHEAD AROUND BRAKE FS 202. (K) JOB PERFORMED IAW REO 601R-53-11-563. (M)

Part: WHEEL — VIBRATION (NLG) · airframe 10,297 hrs · 9,333 cycles

HIGH SPEED ABORTED TAKE-OFF DUE TO NOSEWHEEL VIBRATION. SPEED WAS 135 KNOTS, BRAKE TEMPS WERE 7-7-7-7. COMPLIED WITH REJECTED TAKEOFF INSPECTION IAW AMM 05-51-27-210-801. NO DAMAGE NOTED. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,377 hrs · 6,510 cycles

RT SIDE FS 621.0 TO FS 625.3 INTERCOSTALS AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX .75 INCH LONG. MAINTENANCE REMOVED RT INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,377 hrs · 6,510 cycles

LT SIDE FS 621.0 TO FS 625.3 INTERCOSTAL AT STRINGER 14L ISS CRACKED NEAR RADIUS APPROX .80 INCH LONG. MAINTENANCE LT INTERCOSTAL REMOVED AND INSTALLED NEW ANGLE INTERCOSTAL IAW SRM. (K)

Part: APU — ODOR (APU BAY) · airframe 6,956 hrs · 6,104 cycles

STRONG SMELL OF JET FUEL AFTER APU START IN FLIGHT APU SHUTDOWN. PERFORMED OPS TEST AND LEAK CHECK OF APU. OPS TEST GOOD AT THIS TIME, IAW AMM. NO LEAKS NOTED. NO FAULT CODES NOTED AFTER INTEROGATION OF ECU, OPS CHECK ACM SYSTEM. NO FUEL SMELL NOTED AT THIS TIME. (K)

Part: APU — SMOKE (APU BAY) · airframe 6,956 hrs · 6,104 cycles

REQUEST INSPECTION OF APU COMPARTMENT DUE TO EXTREME AMOUNT OF SMOKE AFTER AUTO SHUTDOWN. INSPECTED APU AW CRJ AMM. NO DEFECTS NOTED. (K)

Part: CONNECTOR — UNSECURE (RT A/C PACK) · airframe 6,161 hrs · 5,321 cycles

SHORTLY AFTER TAKEOFF, STRONG SMELL OF SMOKE IN COCKPIT AND CABIN. NO VISUAL SMOKE, PACK TEMP NORMAL. (AIR RETURN) DURING TAXI PACK NR 2 HI TEMP INDICATION. INSPECTED AFT EQUIPMENT BAY AREA AND FOUND RT PACK ACM TEMP SWITCH HANGING FROM CONNECTOR PLUG. NO NOTICE OF OIL OR OTHER CONTAMINANTS. SECURED PLUG, RAN ENGINES WITH RT PACK (OFF) AND LT PACK OPERATING, NO ODOR OR VISUAL SMOKE NOTED. (K)

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 5,996 hrs · 5,175 cycles

(CONFIG SPOILER) CAS MESSAGE ILLUMINATED ON TAKEOFF, ABORTED TAKEOFF. PERFORMED BELOW 20 KNOTS. REMOVED AND REPLACED SECU NR 1 IAW AMM. OPS CHECK GOOD. (K)

Part: SMOKE — DETECTED (NR 2 ENGINE)

EXCESSIVE SMOKE OUT OF RT ENGINE ON SHUTDOWN ALL INDICATIONS WERE NORMAL. PERFORMED ENGINE RUN OF ENGINE NR 2 IAW CRJ AMM TASK 71-00-00-848-806. NO DEFECTS NOTED. AIRCRAFT SAFE FOR SERVICE. (M)

Part: BRACKET — BENT (CENTER SENSOR)

SELECTING GEAR UP RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE MSG. PERFORMED QRH AND RETURNED TO FIELD. PERFORMED QRH AND RETURNED TO FIELD. FOUND BRACKET FOR NOSE LANDING GEAR CENTERED SENSOR BENT. REMOVED AND REPLACED BRACKET AND ADJUSTED SENSOR PS14GA IAW AMM 32-61-05, C/W GEAR SWING. NO DEFECTS NOTED. (M)

Part: BUSHING — MIGRATED (MLG TRUNNION)

AFT RIGHT MLG MOUNTING TRUNNION BUSHING IS MIGRATED .015, WS 66. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED RIGHT MLG AFT TRUNNION BUSHING AND INSTALLING FIRST OVERSIZE BUSHING. (M)

Part: BUSHING — MIGRATED (LT MLG TRUNNION)

AT LEFT MLG MOUNTING TRUNNION BUSHING IS MIGRATED .004 WS 66. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED LEFT MLG AFT TRUNNION BUSHING AND INSTALLED FIRST OVERSIZE BUSHING P/N 601R5720113-21, IAW BOMBARDIER REO 601R-57-21-003 REV B. (M)

Part: VANE — CHAFED (TE FLAP)

RIGHT INBOARD FLAP VANE AT FLAP STATION 60.005 IS CHAFED .012 INCH DEEP. PERFORMED A MAJOR REPAIR TO RIGHT INBOARD FLAP VANE BY REMOVING INBOARD END LEADING EDGE SKIN AND INSTALLING NEW LEADING EDGE SKIN, P/N 601R14303-54 IAW CRJ SRM 51-42-13. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FOUND FLOOR SILL SUPPORT ANGLE AT FS 621 RBL 45 IS CRACKED. PERFORMED A MAJOR REPAIR BY TRIMMING OUT CRACKED AREA OF SUPPORT AGNLE AND INSTALLING REPAIR ANGLE P/N 601R53-61-117-4 IAW BOMBARDIER REO 601R-53-61-117 REV B. (M)

Part: STRIKER — DAMAGED (PAX DOOR)

PASSENGER DOOR SEAL STRIKER HAS DAMAGE AT FS 349 APPROXIMATELY MID POINT OF DOOR OPENING. REPAIRED PASSENGER DOOR SEAL STRIKER AT FS 349 IAW BOMBARDIER REO 601R-53-22-033 REPAIR 4. (M)

Part: STRIKER — DAMAGED (PAX DOOR)

PASSENGER DOOR SEAL STRIKER HAS DAMAGE AT FS 310 APPROXIMATELY MID POINT OF DOOR OPENING. REPAIRED PASSENGER DOOR SEAL STRIKER AT FS 310 IAW BOMBARDIER REO 601R-53-22-033. (M)

Part: FLAP — STUCK (WINGS)

ON TAKEOFF, FLAPS STUCK AT 20 DEGREES. FECU INTERROGEAED NIL FAULTS FOUND. AIRCRAFT HANGARED 4.5 HOURS. FECU SYSTEM TESTED AS PER 27-51-05-946-009 JOB TASK. FLAPS CYCLED ALL POSITIONS, CHECKED SERVICEABLE. (M)

Part: IDG — LACK OF LUBE (NR 2 GENERATOR) · airframe 1,550 hrs · 1,368 cycles

GENERATOR 2 FAILED UPON APPLICATION OF TAKEOFF POWER. SERVICED IDG OIL AS REQUIRED, OPS CHECK GOOD.