N441ZW

Part: FLAP SYSTEM — FAULTED · airframe 42,622 hrs · 41,369 cycles

WHILE ON APPROACH TO KORD, AT 3500 FEET, THE CREW SELECTED FLAPS 8 AND RECEIVED A FLAP FAIL MESSAGE AT 0 DEGREES. THEY INITIATED A GO AROUND, DECLARED AN EMERGENCY WITH ATC, COMPLIED WITH THE QRH AND BRIEFED THE PASSENGERS. THEY LANDED WITHOUT FURTHER ISSUE ON RUNWAY 28R AND WITH NO REPORTED ADVERSE PASSENGER REACTION TO THE EVENT. AIRCRAFT REMOVED FROM SERVICE. COMPLETED RIGGING OF BPSU IAW AMM 27-51-10 FLAPS OPS CK GOOD AT THIS TIME

Part: SKIN — DENTED (FS755) · airframe 42,201 hrs · 40,866 cycles

DENT ON LEFT AFT FUSELAGE SKIN AT FS755.00 TO 67.5% SPAR DATUM S24L. AIRCRAFT REMOVED FROM SERVICE EVALUATED DENT ON AFT FUSELAGE SKIN AT FS755.00 Ï¿½ 67.5% SPAR DATUM AND S21L TO S23L. ACCOMPLISHED DOUBLER REPAIR IAW EA AWAC-CRJ253-02025 REV IR DATED 01/04/2024. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW. WORK PERFORMED UNDER WORK ORDER 004174, CARD NO. 20014 TT: 41,171:36 TC: 40,836.

Part: STRUCTURE — CORRODED (FS574 TO FS605) · corrosion level 2 · airframe 42,171 hrs · 40,836 cycles

20090 335262 453-280-600 MFG00716 HRS 64.15. AIRCRAFT HAS BEEN REMOVED FROM SERVICE. CORROSION AT 7 PLACES ON REAR PRESSURE BULKHEAD FRAME CAP FROM FS574 TO FS605. ALL AT RBL41.75. ORIGINAL MATERIAL THICKNESS 0.050Ï¿½.Ï¿½ P1 - L= 1.300Ï¿½ X W= 0.900Ï¿½ X D= 0.005Ï¿½, FS574 REMAINING THICKNESS 0.046Ï¿½. P2 - L= 0.900Ï¿½ X W= 0.800Ï¿½ X D= 0.005Ï¿½, FS574+3 REMAINING THICKNESS 0.045Ï¿½. P3 - L= 1.300Ï¿½ X W= 1.00Ï¿½ X D= 0.035Ï¿½, FS574+9 REMAINING THICKNESS 0.015Ï¿½. P4 - L= 1.200Ï¿½ X W= 0.900Ï¿½ X D= 0.007Ï¿½, FS589+12 REMAINING THICKNESS 0.045Ï¿½. P5 - L= 0.700Ï¿½ X W= 0.400Ï¿½ X D= 0.004Ï¿½, FS605 REMAINING THICKNESS 0.046Ï¿½. P6 - L= 1.300Ï¿½ X W= 0.900Ï¿½ X D= 0.040Ï¿½, FS605+11 REMAINING THICKNESS 0.010Ï¿½. P7 - L= 1.100Ï¿½ X W= 1.00Ï¿½ X D= 0.045Ï¿½, FS605+14 REMAINING THICKNESS 0.005Ï¿½. BLENDED CORROSION AT 7 PLACES ON REAR PRESSURE BULKHEAD FRAME CAP AT FS574 TO FS605 AT RBL41.75. P1, P2, P4, AND P5 WITHIN LIMITS REF REO 601R-53-00-526 REVÏ¿½DATED 22-MAY-2013 PERFORMED HFEC WITH NO INDICATIONS IAW CRJ200 NDTM 51-20-06 PART 1 REV 44. ACCOMPLISHED REPAIR ON P3, P6, AND P7 IAW MHIRJ REO 601R-53-61-8139 REV-- DATE 2024-01-13. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 004174, CARD NO. 20090, TT: 42,171:36 TC: 40,836.

Part: STRAP — CORRODED (FLOOR STRUCTURE) · corrosion level 2 · airframe 41,171 hrs · 40,836 cycles

CORROSION ON FLOOR STRUCTURE RH STRAP PN 601R31025-29 AT FS 559.00 AND LBL27 - 45. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND INSTALLED FLOOR STRUCTURE RH STRAP PN 601R31025-29 AT FS 559.00 AND LBL27 - 42 WITH FABRICATED NEW STRAP WITH MATERIAL 7075-T6, THICKNESS 0.050Ï¿½. DIMENSIONS L= 15.100Ï¿½ X W= 2.600Ï¿½. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW SRM 53-00-00 REV 39, SRM 51-24-36 REV 39, SRM 51-40-11 REV 39, SRM 51-42-06 REV 39, SRM 51-21-11, REV 39 AND SRM 51-25-16 REV 39. 51-25-06, REV 39. WORK PERFORMED UNDER AERSALE WORK ORDER 003813, CARD NO. 20095, TT: 42,171:36 TC: 40,836.

Part: STRAP — CORRODED (FLOOR STRUCTURE) · corrosion level 2 · airframe 42,171 hrs · 40,836 cycles

CORROSION ON FLOOR STRUCTURE RH STRAP PN 601R31025-29 AT FS 559.00 AND RBL27 - 42. ***** AIRCRAFT REMOVED FROM SERVICE *****

Part: ACTUATOR — FAULTED (LT MLG) · airframe 40,608 hrs · 39,181 cycles

RECEIVED GEAR DISAGREE AND LH MLG INDICATED RED ON SELECTION OF GEAR DOWN. APROX 1500 FT. CW QRH LH MLG REMAINED UNSAFE. CW TOWER FLYBY. GEAR APPEARED TO BE DOWN AND LOCKED. EMERG GEAR HANDLE WAS PULLED. LANDED WITHOUT INCEIDENT. AFTER LANDING NOTED THE PROX SYS FAULT STATUS MSG APPEARED. TAXIED TO THE GATE UNEVENTFUL GEAR APPEARS TO BE DOWN AND LOCKED.PUT GEAR PINS IN CHOCKED AC MAX BTMS ON LOB 6.ALL 3 INDICATIONS REMAIN ***AIRCRAFT REMOVED FROM SERVICE *** R/R LH MLG SIDE STAY PER AMM 32-32 OPS AND LEAK CHECK GOOD.

Part: NONE — NONE · airframe 40,429 hrs · 39,004 cycles

AFTER T/O UPON SELECTING THE LANDING GEAR HANDLE UP RECEIVED WARNING MSG, NOSE DOOR OPEN AND GEAR DISAGREE. PERFORMED GEAR EMER EXTENSION PER QRH BOTH WARNING MSG'S CLEARED AND GEAR SHOWED NORMAL DOWN. (CONT) LP 337510/1 MSG 'S APPEARED ALMOST IMMEDIATELY AFTER SELECTING GEAR UP. GEAR INDICATION WERE MAINS WHITE AND NOSE GREEN. EMER HANDLE WAS PULLED AND STOWED. ALL HYD PRESS NORMAL NO HIGH TEMP. MC: MC: (LANDING WT 46,800LBS) ****AIRCRAFT REMOVED FROM SERVICE ***** C/W M ACTION FOR MEL 32-30-01 REF 337510/2 FOR MEL REMOVED AND REPLACED NLG WOFFW NO#2 AND CENTRAL HARNESS ASSEMBLY IAW AMM SUPP 12-029E. PERFORMED MULTIPLE GEAR SWINGS IN REF TO AMM 32-30. SWINGS AND OPS TEST GOOD. REMOVED PLACARD AND FROM MEL

Part: NONE — NONE · airframe 39,718 hrs · 38,323 cycles

DURING CLIMB THROUGH 18,000 NOTICED CABIN ALT INCREASING AT APROX 2000 FT PER MIN, ECS PAGE SHOWED BOTH L & R 10TH STAGE VALVES CLOSED. INITIATED DECENT TO 0,000 FT (BLK 3) AT APROX 12,000 FT RECEIVED CABIN ALT CAUTION MSG C/W QRH LEFT L&R 10 TH STAGE VALVES WOULD NOT OPEN. STARTED APU AND OPENED LCV AND ISO VALVES (BLK 4) A/C PRESSURIZED NORMALLY. CONTINUED TO NORMAL LANDING. ON GROUND LH OPENS RT DOES NOT. ***AIRCRAFT REMOVED FROM SERVICE*** REF 343014/4 FOR R&R OF LH PRSOV, REACTIVATED BOTH AIR CONDITIONING PACKS IAW AMM 21-51-00, REACTIVATED OVERBOARD EXHAUST SOV AND RAM AIR SOV TO IT'S ORIGINAL POSITION IAW AMM 21-24-00 AND 21-52-00. REMOVED PLACARD REMOVED FROM MEL

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 37,911 hrs · 36,407 cycles

SHORTLY AFTER TAKEOFF, THE FLIGHT CREW RECEIVED A FLAP FAIL CAUTION MESSAGE. THE CREW REVIEWED THE QRH, CONTACTED DISPATCH AND ATC, DECLARED AN EMERGENCY AND CONTINUED TO DESTINATION WITH AN OTHERWISE NORMAL LANDING. RECEIVED FLAPS FAIL AT 8 DEG WHEN COMPLETING AFTER TAKE-OFF CHECKLIST. "AIRCRAFT REMOVED FROM SERVICE" REPLACED RIGHT BPSU PER AMM 27-51-10 SN OFF 2382 SN ON 1702A DMB

Part: ANGLE — CORRODED (FS 319 - 349) · corrosion level 2 · airframe 37,590 hrs · 36,103 cycles

SERVICE DOOR LWR SILL FS 319 TO FS 349 HAS MULTIPLE AREAS OF CORROSION REMOVED, FABRICATED AND INSTALLED ANGLE 601R38303-105 FROM 7075-T6 REF CRJ 200 SRM 53-21-23 REV. 37. AIRCRAFT REMOVED FROM SERVICE. REMOVED, FABRICATED AND INSTALLED ANGLE 601R38303-105 FROM 7075-T6 REF CRJ 200 SRM 53-21-23 REV. 37.

Part: BONDING PLATE — CORRODED (BS 736) · corrosion level 2 · airframe 37,590 hrs · 36,103 cycles

NR 2 PYLON UPPER TRAILING EDGE, TWO BONDING PLATES HAD CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACE BOTH BONDING PLATES IAW SRM TEMP REV 51-42, SRM 51-42-10, & 51-25-00 REV 37.

Part: STRUCTURE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 37,590 hrs · 36,103 cycles

ENTRY DOOR INNER STRUCTURE FROM FS 311.75 TO 347.25 HAS CORROSION. ITEMS AS IDENTIFIED REF CRJ 200 SRM 52-10-14 ITEM 1 FORMER INNER, FS 320.10 601R31902-455, ITEM 18 FORMER 601R31902-409, ITEM 19 FORMER 601R31902-13, ITEM 25 INTERCOSTAL 601R31902-318, ITEM 26 INTERCOSTAL 601R31902-317, ITEM 35 INTERCOSTAL 601R31902-459, ITEM 54 CLEAT 600R31902-335, ITEM 54A CLEAT 600-31902-269, AND ITEM 62 CLIP 601R31902-69. CORROSION REMOVED WITHIN ALLOWABLE LIMITS REF CRJ 200 SRM 51-21-06 REV 37. AIRCRAFT REMOVED FROM SERVICE CORROSION REMOVED WITHIN ALLOWABLE LIMITS REF CRJ 200 SRM 51-21-06 REV 37.

Part: CONTROL CABLE — FRAYED (RT AILERON) · airframe 37,590 hrs · 36,103 cycles

RIGHT OTBD AILERON FUSELAGE CONTROL CABLE IS FRAYED AT THE RT REAR QUADRANT. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE O/B AILERON FUSELAGE CONTROL CABLE AND ACCOMPLISHED RIGGING IAW AMM 27-00-00 & 27-11-00, REV 60. ACCOMPLISHED AILERON TRIM OPS CHECKED GOOD IAW AMM 27-11-00-710-804 REV 60.

Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 37,084 hrs · 35,639 cycles

AFTER ROTATION RECEIVED STEERING INOP CAUTION AFTER GEAR RETRACTION, GEAR INDICATED UP/LOCKED. AT 700FT AGL RECEIVED WOW INPUT CAUTION C/W QRH FOR NWS MESSAGE REMAINED. DECLARED AN EMERGENCY AND LANDING IN IAD WAS UNEVENTFUL.

Part: AILERON — CORRODED (LT WING) · corrosion level 2 · airframe 35,826 hrs · 34,442 cycles

LEFT AILERON OUT BOARD PCU ATTACHMENT POINT ON AILERON FOUND TO HAVE CORROSION.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG DOOR) · airframe 34,662 hrs · 33,348 cycles

RECEIVED NOSE GEAR DOOR OPEN WARNING MESSAGE IN A TURN AT 200 KTS. AT 230 KTS THE MESSAGE CLEARED. WHEN TRUE AIRSPEED IS ABOVE 250 MESSAGE CAME BACK. APPEARS DOOR IS NOT OPEN. NOSE LANDING GEAR FORWARD DOOR SENSOR RIGGING WITHIN LIMITS IAW AMM 32-00-00. PERFORMED A FULL GEAR SWING. NO DEFECTS NOTED.

Part: PROXIMITY SENSOR — FAILED (NLG DOOR) · airframe 34,661 hrs · 33,347 cycles

NOSE DOOR OPEN WARNING INFLIGHT AT 14,000FT. MESSAGE CLEARED AT 230KTS . REMOVED & REPLACED NLG DOOR LT FWD PROXIMITY SENSOR IAW AMM 32-61-05, OPS CHECKED GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 34,641 hrs · 33,326 cycles

ON ARRIVAL, HEARD A NOISE SIMILAR TO A BIRDSTRIKE AND NOTICED THE FIRST OFFICER`S WINDOW CRACKED. RECEIVED A WINDOW HEAT MESSAGE. COMPLIED WITH QRH. REDUCED SPEED TO 205 KIAS. DECLARED EMERGENCY. LANDED NORMALLY. CHANGED THE WINDOW.

Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 34,192 hrs · 32,892 cycles

3769 INFLIGHT RECIEVED NWS INOP CAUTION MSG COMPLIED WITH QRH MSG PERSISTED LANDED WITH NWS INOP. COMPLIED WITH FIM RESET MSG CLEARED

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 34,112 hrs · 32,807 cycles

RECEIVED LEFT HAND ANTI ICE CAUTION AFTER TAKEOFF. COMPLIED WITH QRH, MESSAGE DID NOT CLEAR. COWL SHOWED AMBER ON ANTI-ICE SYNOPTIC, COWL ANTI ICE SOV SHOWED CLOSED. LANDING WEIGHT 47,000LBS.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 34,036 hrs · 32,730 cycles

3762 GEAR DISAGREE WARNING MESSAGE ON RETRACTION. C/W QRH. RETURNED TO ATW. CHANGED HYD PUMP AND DRAG BRACE. TEST NOT COMPLETED.

Part: ACCESS PANEL — DAMAGED · airframe 34,012 hrs · 32,705 cycles

PANEL 332AB SCREW HOLE ELONGATED.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 34,012 hrs · 32,705 cycles

REAR PRESSURE BULKHEAD FORWARD FACE DAMAGED IN MULTIPLE LOCATIONS. SCREW DAMAGE. REPAIRED.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,012 hrs · 32,705 cycles

SERVICE DOOR THRESHOLD IS CORRODED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,012 hrs · 32,705 cycles

280 BEAM UPPER ANGLE STRIP IS SUSPECTED TO BE CRACKED JUST O/B OF RBL9, IN THE CABIN BELOW FLOOR.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 34,012 hrs · 32,705 cycles

LOWER REPAIR ANGLES AT FS280 AND LBL12 AND RBL12 ARE DAMAGED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,012 hrs · 32,705 cycles

BATHTUB FITTING IS CRACKED AT THE O/B SIDE OF LBL9 AT FS461, IN THE MAIN CABIN.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,012 hrs · 32,705 cycles

STR 3L IS CRACKED JUST FWD OF FRAME 379, IN THE CABIN.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 34,012 hrs · 32,705 cycles

INTERCOSTAL AT FS 319 - FS 333 AND STR 22L CORRODED.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,012 hrs · 32,705 cycles

PAX DOOR CUT OUT STRUCTURE CORRODED, FS 310.00 TO 349.00 STR 18L. REPLACED ANGLE SUPPORT IAW SRM 51-42-06, 51-42-21, 53-21-23.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,012 hrs · 32,705 cycles

ANGLE CLIP IS CRACKED AT THE I/B SIDE OF RBL 36 AT FS 484 IN THE CABIN BELOW THE FLOOR.

Part: RIB — CRACKED (LT PYLON) · airframe 34,012 hrs · 32,705 cycles

LT PYLON LOWER RIB CRACKED AT FS605.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,012 hrs · 32,705 cycles

FRAME 605 IS CRACKED IN 2 SPOTS ABOVE AND BELOW STR 9L IN THE CARGO BAY.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,012 hrs · 32,705 cycles

LT OBLIQUE ANGLE CRACKED ON AFT PRESSURE BULKHEAD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,012 hrs · 32,705 cycles

FS280 FWD UPPER ANGLE IS CRACKED.

Part: RETAINER — CRACKED (PYLON) · airframe 34,012 hrs · 32,705 cycles

PANEL 422BT SEAL RETAINER CRACKED.

Part: RETAINER — CRACKED (PYLON) · airframe 34,012 hrs · 32,705 cycles

CRACKED SEAL RETAINER ON PYLON PANEL 412BT.

Part: FITTING — CRACKED · airframe 34,012 hrs · 32,705 cycles

PANEL 422BT DIVIDER PANEL CLIP CRACKED. REPLACED CLIP IAW SRM 51-40-11, 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,012 hrs · 32,705 cycles

ANGLE CLIP CRACKED AT THE O/B SIDE OF RBL 27 AT FS 484 IN THE CABIN BELOW THE FLOOR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,012 hrs · 32,705 cycles

SEAT TRACK ON LBL 9 HAS CORROSION BETWEEN FS 605 AND FS 621, IN THE CARGO BAY.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,012 hrs · 32,705 cycles

CARGO NET TIE DOWN FITTINGS CORRODED FROM FS 574.00 TO 605.00, LBL9. REPLACED FITTINGS IAW SRM 53-61-49, 51-41-02.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,012 hrs · 32,705 cycles

CARGO NET TIE DOWN FITTINGS CORRODED AT FS 559+96 AND 574.00, LBL27. REPLACED TIE DOWNS IAW SRM 53-61-49, 51-41-02.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 34,012 hrs · 32,705 cycles

CARGO DOOR OPENING LOWER SILL IS CRACKED AT FS 605.00. REPAIRED SILL IAW REO 601R-53-61-433 REV-C.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 33,815 hrs · 32,497 cycles

RECEIVED A GEAR UP DISAGREE AND NOSE DOOR WARNING AFTER TAKE OFF. COMPLIED WITH QRH, NOSE WHEEL DID NOT RETRACT, MLG UP AND LOCKED, NOSE SHOWING DOWN AND LOCKED. REMOVED AND REPLACED NOSE LANDING GEAR BRACKET SUB ASSY, RIGHT PROXIMITY SENSORS, WOW NR 2 AND OLEO CENTERED & EXTENDED HARNESS IAW AMM 32-61-05, AND 32-24-01. OPS CHECKED GOOD AND RIG CHECKED GOOD.

Part: BEAM — DAMAGED (AFT BULKHEAD) · airframe 33,636 hrs · 32,313 cycles

DURING SCHEDULED INSPECTION OF THE AFT PRESSURE BULKHEAD, INSPECTION FOR THE CARGO DOOR CROSS BEAM DAMAGED. DAMAGE WAS CAUSED BY THE CARGO DOOR CABLE.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 33,636 hrs · 32,313 cycles

DURING SCHEDULED INSPECTION OF THE AFT PRESSURE BULKHEAD, DAMAGE WAS FOUND AT BS 621, RBL 36.2, WL 103. DAMAGE WAS CAUSED BY A SCREW PROTRUDING THROUGH THE CARGO BAY LINERS AND CONTACTING THE BULKHEAD SURFACE.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 33,636 hrs · 32,313 cycles

DURING SCHEDULED INSPECTION OF THE AFT PRESSURE BULKHEAD, A CRACK WAS FOUND AT LBL 28 JUST ABOVE THE TOP OF THE CARGO DOOR TRACK.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 33,405 hrs · 32,086 cycles

FLAPS FAILED CAUTION MESSAGE DURING CRUISE AT 31,000 FT. FLAPS INDICATED ZERO. NO FLAP HANDLE INPUTS. REPLACING THE RT BPSU.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 33,401 hrs · 32,083 cycles

DURING CRUISE FLT AT 28000 FT RECEIVED FLAP FAIL CAUTION MESSAGE. COMPLIED WITH QRH & FLAPS SHOW ZERO. PERFORMED FLAP RESET PROCEDURE IAW 98-018G BOX 11 & FLAPS RESET.

Part: SENSOR — MALFUNCTIONED (BRAKE) · airframe 33,385 hrs · 32,067 cycles

FLAPS FAIL CAUTION WITH FLAPS AT ZERO DEGREES, 20,000 FT, 285 KTS WITH NO CREW INPUT. ACFT IS OPERATING UNDER MEL 27-50-01. MAX BTMS AFTER ZERO FLAP LANDING 9,9,10,10. NO BRAKE OVERHEAT INDICATION CHECKED RESISTANCE FROM FECU TO BPSU 17-J =1, 4952, 22-K=1.5052, 13-C=1.4552, 5-B = 1.4452, 12-A = 1.4852, 18-F = 1.4852, 23-G=1.4652, 20-H =1, 5052 END TO END MEGGAR CHECK AT 500V ALL WIRES SHOWED 0.00 MEGGER CHECK FROM PIN TO GROUND AT 500 V SHOWED OPEN AND NO BLEED OVER. REMOVED AND REPLACED RIGHT FLAP BPSU IAW AMM 27-50. INSTALLED PN 855D100-15. OPS CHECKED GOOD, R & R LEFT BRAKE AND POSITION SENSOR UNIT IAW AMM 27-51-10. OPS TEST GOOD AT TIME. A MCF IS REQ TO CONFIRM CORRECTIVE ACTION FOR PREVIOUS FLAP FAIL. ACHIEVE CRUISE ALT OF 28K FT, PERFORM SEVERAL TURNS AND ALTITUDE CHANGES. DECINED BELOW 15K FTCYCLE THE FLAPS THRU EACH INCREMENT TO FULL EXTENSION SEVERAL TIMES.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 33,381 hrs · 32,064 cycles

RECEIVED FLAPS FAIL CAUTION MESSAGE ENROUTE. FLAPS FAILED AT ZERO DEGREE DETENT. NO HANDLE MOVEMENT. PERFORMED FLAP RESET IAW 98-018G, BOX 12. FLAPS RESET.

Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 32,946 hrs · 31,652 cycles

DURING CLIMB WITH AUTOPILOT ENGAGED AT FL 250, RECEIVED A PRESISTANT UNCOMMANDED YAW. COMPLIED WITH QRH, CONDITION PRESISTED, DIVERTED. YAW BECAME MORE PRONOUCED AT SLOWER AIRSPEEDS.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 32,258 hrs · 31,001 cycles

AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. RECEIVED A GEAR DISAGREE WARNING MESSAGE. COMPLIED WITH QRH, RECEIVED GEAR DOWN AND LOCKED INDICATION. MESSAGE APPEARED 28 SECONDS AFTER HANDLE MOVEMENT. NOSE EGAR SHOWED RED ON EICAS, MANUAL RELEASE SYSTEM WAS UTILIZED. EMERGENCY WAS DECLARED. RECEIVED STEERING INOPERATIVE CAUTION MESSAGE AS WELL.

Part: HYDRAULIC SYSTEM — MALFUNCTIONED (MLG) · airframe 32,240 hrs · 30,985 cycles

FLT 4136. AFTER T/O NOSE GEAR SLOW TO RETRACT RECEIVED GEAR DISAGREE WITH GEAR FULLY RETRACTED MSG CLEARED. RECEIEVED MESSAGE ABOUT 5 SECONDS AFTER GEAR HANDLE MOVEMENT, NLG RED ONLY HYDS NORMAL PSI AND TEMP PUMPS IN AUTO. M/C RECEIVED AT 180 KNOTS ALSO NOTED A LEAK AT NOSE UNKOWN IF OLD OR FRESH LEAK. EXTENTION HAD NO ISSUES. PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION/RETRACTION SYSTEM IAW AMM 32-30-00. NLG AND MLG EXTENSION AND RETRACTION WITHIN ALLOWABLE LIMITS. BLED NR 3 HYDRAULIC SYSTEM AND SERVICED IAW AMM 12-12-29 LEAK CHECK AND OPS CHECKED GOOD.

Part: STRUT — DISCHARGED (NLG) · airframe 32,229 hrs · 30,915 cycles

FLT. 4020. AFTER TAKEOFF, NOSE LANDING GEAR DID NOT RETRACT, RECEIVED GEAR DISAGREE MASTER WARNING AND NOSE STEERING INOPERATIVE CAUTION. COMPLIED WITH QRH. STEERING NORMAL BACK TO GATE. BTMS NORMAL. SERVICED THE NOSE LANDING GEAR STRUT, LEAK AND OPS CHECKED GOOD IAW MTCM 000-12-710-002 AND SUPP 09-055.

Part: PROXIMITY SENSOR — OUT OF RIG (NLG DOOR) · airframe 32,089 hrs · 30,846 cycles

AFTER TAKEOFF WHILE ACCELERATING TO 250 KNOTS RECEIVED NOSE DOOR OPEN WARNING MESSAGE AND VOICE. AT 235 KNOTS SLOWED AIRCRAFT TO TOO KNOTS MESSAGE CLEARED AFTER 15 SECONDS. ALL OTHER GEAR INDICATIONS NORMAL, AIRCRAFT WAS OPERATING UNDER MEL 32-30-01. AIRCRAFT WEIGHT ON LANDING 46,800 LBS. GEAR HANDLE WAS NOT TOUCHED BY CREW. FOUND PROX SENSOR ON NLG DOOR OUT OF LIMITS RE RIGGED BOTH PROX SENSOR IAW AMM 32-61-05, OPS CHECKED GOOD.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 32,089 hrs · 30,846 cycles

FLIGHT 4099, AFTER TAKE OFF, RECEIVED GEAR DISAGREE WARNING, NOSE GEAR UNSAFE, 25 SECONDS AFTER SELECTING GEAR UP. COMPLIED WITH QRH, MANUALLY SELECTED GEAR DOWN. GEAR INDICATED 3-GREEN-DOWN. LANDED AT 46000 GROSS.PSEU SHOWS S22 DN FAR, S30DN FAR,S31 DN FAR,S3S32 DN FAR. D114 DN ON. R & R NLG EXT/RETRACT PRIORITY VALVE IAW 32-33-15. REPACKED THE SHOCK STRUT FLOATING PISTON IAW 32-21-25. GEAR SWING CHECKED GOOD.

Part: WARNING MESSAGE — ILLUMINATED (NLG) · airframe 32,069 hrs · 30,829 cycles

AFTER TAKE OFF, RECIEVED A NOSE GEAR DISAGREE MESSAGE. COMPLIED WITH QRH MESSAGE CLEARED. MESSAGE APEARED WHEN SELECTING UP APPROX 28 SECONDS AFTER SELECTION. NO ASSOICATED MESSAGES. LANDING GEAR LEVERS WERE NOT MOVED UNTILL QRH. MANUAL RELEASE USED. NO ICEING, HIGH TURBULANCE OR EXSESIVE MOVEMENTS OF FLT CONTROL IN TRANSIT. HYD TEMPS, PRESSURE, AND QTY NORMAL. HYD SYSTEMS IN AUTO NO EMEREGENCY DECLARED AIR SPEED 180 KNOTTS

Part: WARNING LIGHT — ILLUMINATED

GEAR RETRACTION AFTER TAKE OFF GEAR DISAGREE MESSAGE RECEIVED. MESSAGE DID NOT CLEAR UNTIL CYCLING GEAR DOWN PER QRH. MESSAGE REMAINED FOR 3 MIN NO OTHER ASSOCIATED EICAS MESSAGE. NOSE GEAR SHOWED RED ON EICAS DISPLAY. HYDRAULIC INDICATIONS NORMAL.

Part: UPLOCK — MALFUNCTIONED (NLG) · airframe 32,022 hrs · 30,791 cycles

NOSE GEAR DISAGREE WHEN SELECTED UP ON DEPARTURE ABOUT 25 SECONDS AFTER HANDLE MOVEMENT. C/W QRH, GEAR DOWN, 3 GREEN. LANDED AT 45500 GROSS. NORMAL LANDING NORMAL BRAKING.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,490 hrs · 29,365 cycles

SERVICE DOOR SILL FWD T FITTING IS CORRODED. R & R FWD T FITTING IAW SRM 51-23-00 & 51-42-21.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,490 hrs · 29,365 cycles

RIGHT FLOOR SILL FS 559.00+80 - 605.00 HAS 5 CORRODED FASTENER HOLES. REPAIRED RT FLOOR SILL FROM FS 559.00+80 - 605.00 IAW REO 601R-53-00-526 & EA CRJ253-00302.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,490 hrs · 29,365 cycles

FRAME 333.00 IS CRACKED, BETWEEN STRINGER 1L & 2L IN CABIN. REPAIRED FRAME 333.00 CRACK IAW REO 601R-53-21-2073 DATED 3 10 2016.

Part: PANEL — CRACKED (PAX DOOR) · airframe 30,490 hrs · 29,365 cycles

PASSENGER DOOR, THIRD STEP FROM BOTTOM, HAS CRACK ON AFT RISER PANEL. REPAIRED PAX DOOR RISER PANEL ON AFT SIDE OF DOOR AT THIRD STEP FROM BOTTOM IAW REO 601R-52-11-702.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,490 hrs · 29,365 cycles

RIGHT FLOOR SILL, BETWEEN FS 605 & 621 IS CORRODED OUT OF LIMITS, REMAINING MATERIAL IS 0.017. REPAIRED RT FLOOR SILL FROM FS 605 - 621 IAW REO 601R-53-00-526 & EA CRJ 253-00300.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 30,490 hrs · 29,365 cycles

FRAME BS 333 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STR 25L AND 25R, IN THE FWD ELECTRONIC EQUIPMENT BAY. REPAIRED CORRODED FRAME 333 BETWEEN STR 25L AND 25R IN THE FWD ELECTRONIC EQUIPMENT BAY IAW EA CRJ253-00290.

Part: NOT REPORTED — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,490 hrs · 29,365 cycles

AFTER REMOVING NLG AFT DOOR RT HINGE FITTING, FOUND AREA TO BE CORRODED BEHIND HINGE FITTING. REPAIRED CORROSION AT FS 231 & STRINGER 26R, UNDER THE NLG AFT DOOR HINGE FITTING IAW EA CRJ253-00310.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,490 hrs · 29,365 cycles

THE UNDER SURFACE OF RT FLOOR SILL, FS 559+112 HAS CORROSION. R & R SPLICE ANGLE FROM RT FLOOR SILL AT FS 559+112 IAW SRM 51-42-06, 51-42-11 & 51-21-11.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,490 hrs · 29,365 cycles

FRAME 349 HAS CORROSION ON THE AFT & FWD SIDE, BETWEEN STRINGER 25L & 26R, IN THE FWD E & E BAY. REPAIRED FS 349 FRAME, BETWEEN STRINGER 25L & 26R IAW EA CRJ253-00296 REV-A.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,490 hrs · 29,365 cycles

NUTPLATES UNDER RT FLOOR SILL, FS 574.00 - 621.00 ARE CORRODED. FLOOR SILL FOUND TO BE CORRODED. NON-ROUTINE GENERATED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,490 hrs · 29,365 cycles

RIGHT OBLIQUE ANGLE FS 625.00, STRINGER 14R IS CRACKED. R & R RT OBLIQUE ANGLE IAW SRM 51-42-21.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 30,490 hrs · 29,365 cycles

PASSENGER DOOR UPPER WEB, UPPER TOP FOLDING STEP AFT CORNER IS CRACKED. REPAIRED CRACKED ANGLE IAW REO601R-52-11-279 DATED 2001 10 18.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,490 hrs · 29,365 cycles

ANGLE CLIP ON FRAME 280.00 IS CRACKED, AT STRINGER 3L, IN CABIN. R & R ANGLE ON FRAME 280, AT STRINGER 3L IAW SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,490 hrs · 29,365 cycles

OUTBOARD ANGLE FS 621.00, STRINGER 13L IS CRACKED. R & R OTBD ANGLE AT FS 621.00, STRINGER 13L IAW SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,490 hrs · 29,365 cycles

OUTBOARD ANGLE FS 621.00, STRINGER 14L, IS CRACKED, R & R OTBD ANGLE, AT FS 621.00 & STRINGER 14L IAW SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,490 hrs · 29,365 cycles

OUTBOARD ANGLE FS 621.00, STRINGER 15L CRACKED. R & R OTBD ANGLE, AT FS 621.00 & STRINGER 15L, IAW SRM 51-42-06.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,490 hrs · 29,365 cycles

CARGO TIE DOWN TRACK RBL 9, FS 559+88 HAS CORROSION. R & R CARGO TIE DOWN TRACK & RESTORED FINISH IAW REO 601R-53-00-485.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,490 hrs · 29,365 cycles

FS 484 FLOOR SUPPORT STRUCTURE OTBD CLIP AT RBL 27 IS CRACKED, REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,490 hrs · 29,365 cycles

FS 484 FLOOR SUPPORT STRUCTURE CLIP AT LBL 36, IS CRACKED. REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,490 hrs · 29,365 cycles

BOTH ANGLE CLIPS ON STRINGER 3L CRACKED, JUST AFT OF FS 280.00 IN THE CABIN. R & R BOTH CLIPS AT STRINGER 3L IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,490 hrs · 29,365 cycles

RIGHT NR 1 FLOOR SEAT TRACK HAS CORROSION FS 364.00-FS 394.00. R & R NR 1 FLOOR SEAT TRACK, AT FS 364.00-394.00 IAW AMM 53-01-11.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 30,415 hrs · 29,299 cycles

RIGHT WING ANTI-ICE CAUTION ON TAKEOFF, ABORTED AT 60 - 70 KNOTS, BTMS 2,1,2,4, WING ANTI-ICE SELECTED ON. COMPLIED WITH OPERATIONS CHECK OF RT WING ANTI-ICE SYS IAW AMM 30-12-00. OPERATIONS CHECKED GOOD IN NORMAL & STANDBY MODE, 14TH STAGE VLV, OPERATIONS CHECKED AS WELL IAW FIM 30-10-00.

Part: SERVICE DOOR — LACK OF LUBE (CABIN) · airframe 30,372 hrs · 29,258 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. INSPECTED SERVICE DOOR OUTER HANDLE & LUBRICATED IAW SUPP 11-029B. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 30,330 hrs · 29,213 cycles

RIGHT WING ANTI-ICE CAUTION ILLUMINATED ON TAKEOFF, ABORTED AT 60 KTS, NORMAL BRAKING. WING ANTI-ICE WAS ON & IN NORMAL MODE. COMPLIED WITH OPERATIONAL TEST OF WING ANTI-ICE & INDICATION SYS IAW AMM 30-12-00. OPERATIONS CHECKED NORMAL. COULD NOT DUPLICATE MALFUNCTION. ACFT IS OK FOR SERVICE.

Part: PITOT LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 30,100 hrs · 28,996 cycles

DURING QUARTERING HEADWIND OF GUSTING 20 KTS ON TO THE FIRST OFFICERS ASI READS 20 KTS ABOVE THE CAPTAINS. ABORTED TO AT 60 KTS IND ON CAPTAINS ASI. BTMS READS 5433. DID NOT NOTE STBY ASI INDICATION. ACFT WAS JUST DE-ICED PRIOR TO TAKEOFF. PURGED PITOT STATIC SYS IAW AMM 24-11-00, FOUND SMALL AMOUNT OF WATER IN RT PITOT LINE. PERFORMED BITE TEST FOR ADC IAW AMM 34-13-00, OPERATIONS CHECKED GOOD. PERFORMED PITOT STATIC TEST IAW SUPP 12-055, OPERATIONS CHECKED GOOD.

Part: HANDLE — DEFECTIVE (SERVICE DOOR) · airframe 30,070 hrs · 28,965 cycles

SERVICE DOOR WILL NOT OPEN. REPLACED SERVICE DOOR OUTER HANDLE IAW AMM 52-41-0. OPERATIONS CHECKED GOOD.

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 29,878 hrs · 28,786 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. CLEANED & LUBED SERVICE DOOR HANDLE IAW SUPP 11-029B. OPERATIONS CHECKED GOOD.

Part: SHAFT — CRACKED (SERVICE DOOR) · airframe 29,821 hrs · 28,728 cycles

SERVICE DOOR HARD TO OPEN FROM OUTSIDE. INSPECTED & FOUND SERVICE DOOR OUTER HANDLE SHAFT CRACKED. R & R SERVICE DOOR HANDLE LATCH ASSEMBLY IAW AMM 52-41-03 & SRM CHAPTER 51.

Part: IDG — MALFUNCTIONED (NR 2) · airframe 29,722 hrs · 28,639 cycles

INTEGRATED DRIVE GENERATOR 2 CAUTION MSG DURING CLIMB. COMPLIED WITH QRH, DISCONNECTED IDG & STARTED APU. RETURNED & LANDING WEIGHT 46,500 BTMS 5, 4, 3, & 3.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 29,090 hrs · 28,020 cycles

FLIGHT 3850, 3840, 3840, 3850 ELEC ODOR ROW 5 & AFT. LIGHTING SUFFICIENT FOR CREW. PLACARDED & PLACED ON MEL. R & R BALLASTS AT 11FD, 8AC & BOTH BALLASTS AT 9FD. ALSO REPLACED 1 FLUORESCENT BULB AT 9FD. OPERATIONS CHECKED GOOD. REMOVED PLACARD & MEL.

Part: CONTROLLER — MALFUNCTIONED (ADG) · airframe 28,644 hrs · 27,586 cycles

ADG DEPLOYMENT UNCOMMANDED AT WOW. R & R ADG AUTO DEPLOY CONTROLLER. OPS TESTED GOOD.

Part: LANDING GEAR — INOPERATIVE (NOSE) · airframe 25,465 hrs · 24,549 cycles

ON CLIMB OUT RECEIVED GEAR DISAGREE WARNING MSG. COMPLIED WITH QRH. NOSE GEAR DID NOT RETRACT.

Part: RETAINER — CRACKED (LT PYLON) · airframe 25,629 hrs · 24,699 cycles

LEFT ENG PYLON PANEL 412DB SEAL RETAINER CRACKED. R & R UNSERVICEABLE SEAL RETAINER ON PANEL 412DB WITH NEW SERVICEABLE SEAL RETAINER PN 601-37003-303 IAW CMM'S 20-40-11 & 20-42-06.

Part: SKIN — DENTED (RT WING) · airframe 25,629 hrs · 24,699 cycles

RIGHT WING CTR LE HAD MULTIPLE LARGE DENT AREAS, PREVIOUSLY TEMP REPAIRED IAW SRM SUPP 10-096. R & R SKIN ON RT WING CTR LE PN 601R12057-4 IAW CRJ 200 SRM 51-40-11, 51-42-06 & 51-42-13.

Part: SEAL — DEFECTIVE (FUSELAGE) · airframe 25,629 hrs · 24,699 cycles

COMPLIED WITH AWAC CARD 4DMI16241 REPAIR SVC DOOR SEAL STRIKER JOINT 601R-53-22-162. R & R CORNER SEAL AT SERVICE DOOR LOWER RT SIDE IAW CRJ SRM 51-77-00 PARA 3 PG 1 & IAW CRJ SRM 51-42-06 PARA PG 11.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 25,629 hrs · 24,699 cycles

PASSENGER DOOR INNER HANDLE CRACKED. R & R PAX DOOR INNER HANDLE WITH SERVICEABLE PN 600-31887-15 IAW CRJ 200 SRM 51-40-11.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 25,630 hrs · 24,699 cycles

CRACK IN PAX CABIN FLOOR BEAM INTERCOSTAL NEAR FS 461, RBL 11. R & R NEW SUPPORT FITTING PN 600-31068-09 IAW CRJ 200 SRM 51-42-20, 51-40-11.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 25,629 hrs · 24,699 cycles

PASSENGER DOOR PRESS VENT SUPPORT CLIP IS CRACKED. R & R INNER ANGLE AT LT PAX DOOR FRAME STRUCTURE IAW SRM 51-42-06 PARA 9B 1 PG 11 REV 32.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 25,630 hrs · 24,699 cycles

CARGO FLOOR TRACK ON LBL 9 CORRODED AT FS 559.112. REMOVED UNSERVICEABLE CARGO FLOOR TRACK AT LBL 9 FS 559+112, THEN INSTALLED NEW SERVICEABLE TRACK IAW CRJ 200 AMM 53-01-11, SRM 53-21-49, 53-24-02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 25,630 hrs · 24,699 cycles

CARGO FLOOR TRACK ON RBL 9 CORRODED AT FS 559+112. REMOVED UNSERVICEABLE CARGO FLOOR TRACK, THEN INSTALLED NEW SERVICEABLE TRACK IAW AMM 53-01-11, SRM 53-21-49, 51-41-02.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 25,629 hrs · 24,699 cycles

CARGO DOOR FWD TRACK LOWER MOUNT BRACKET CRACKED. R & R BRACKET WITH SERVICEABLE PN 601R35050-25 IAW SRM 51-40-11 & 51-42-06.

Part: DRAG ANGLE — CRACKED (RT MLG) · airframe 25,629 hrs · 24,699 cycles

RIGHT DRAG ANGLE COMMON TO BATT RIB CRACKED. RT DRAG ANGLE COMMON TO BATT RIB CRACKED.

Part: HOUSING — CRACKED (EXTERNAL POWER) · airframe 25,630 hrs · 24,699 cycles

EXTERNAL POWER RECEPTACLE HOUSING CRACKED. REMOVED CRACKED HOUSING & INSTALLED NEW SERVICEABLE HOUSING IAW SRM 51-42-06, 51-42-13, 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 25,629 hrs · 24,699 cycles

EXTERNAL POWER CONTROL PANEL LOWER MOUNT ANGLE CRACKED. R & R ANGLE WITH SERVICEABLE PART IAW SRM 51-40-11 & 51-42-06.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 25,629 hrs · 24,699 cycles

CARGO DOOR HANDLE HOUSING IS CRACKED. R & R WITH SERVICEABLE HOUSING PN H3415-31 IAW SRM 51-40-11 & 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,629 hrs · 24,699 cycles

RIGHT BUTT LINE 9 OTBD CLIP CRACKED AT FS 280. R & R WITH SERVICEABLE CLIP IAW REO 601R-53-11-171 REV D DATED 13-FEB-07.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 25,630 hrs · 24,699 cycles

PASSENGER DOOR POWER ASSIST PULLEY BRACKET DRAG ANGLE IS CRACKED. REPAIRED PAX DOOR AFT POWER ASSIST PULLEY BRACKET DRAG ANGLE IAW REO 601R-52-11-513 REV A DATED 03-09-05 & SRM 51-42-06.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 25,629 hrs · 24,699 cycles

PASSENGER DOOR POWER ASSIST MOTOR SUPPORT AFT ANGLE CRACKED. R & R WITH SERVICEABLE PART IAW SRM 51-40-11, 51-42-06 & 51-42-21.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 25,629 hrs · 24,699 cycles

FLOOR BEAM ATTACH CLIPS AT FS 280 LBL 9 INBD & OTBD SIDES ARE CRACKED. R & R CLIPS WITH SERVICEABLE PARTS IAW 601R-53-11-171 REV D DATED 13-FEB-07.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 25,629 hrs · 24,699 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT RBL 27 & FS 484. R & R CLIP WITH SERVICEABLE PART IAW SRM 51-40-11 & 51-42-21.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 25,629 hrs · 24,699 cycles

RIGHT MLG WW BRAKE TRANSDUCER BRACKET IS CRACKED. R & R WITH SERVICEABLE PN 601R75262-157 IAW SRM 51-40-11 & 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 25,629 hrs · 24,699 cycles

ANGLE CRACKED ON FS 621 - 625 BULKHEAD AREA NEAR STRINGER 14L. R & R ANGLE WITH SERVICEABLE PART IAW SRM 51-40-11 & 51-42-21.

Part: RELAY — FAULTY (ELECTRICAL SYS) · airframe 25,170 hrs · 24,270 cycles

3733, DURING CLIMB AT APPROXIMATELY 12,000 FEET RECEIVED AC ESS BUSS CAUTION & EMERGENCY LIGHT CAME ON. THE MESSAGE CLEARED & LIGHTS WENT OUT APPROXIMATELY 20 SECONDS LATER WITHOUT CREW ACTION. THE MESSAGE & EMERGENCY LIGHTS BEGAN TO CYCLE APPROXIMATELY EVERY 10 - 20 SECONDS, COMPLIED WITH QRH. R & R RELAY K1XD IAW AMM 24-51-27, OPERATIONS CHECKED GOOD IAW CR J AMM 24-51-27. OPERATION CHECK EMERGENCY LIGHTS IAW AMM 33-51-00, OPERATIONS CHECKED GOOD.

Part: HYDRAULIC LINE — CRACKED (HYDRAULIC SYS) · airframe 22,505 hrs · 21,698 cycles

DURING CLIMB THROUGH FL250, HYDRAULIC 1 LOW PRESSURE CAUTION MESSAGE, COMPLIED WITH QRH, DIVERTED TO GSP. REPLACED HYD SYSTEM 1 GROUND PRESSURE PORT TO PRESSURE MANIFOLD LINE PER AMM 29-11-05, LEAK CHECK GOOD AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,313 hrs · 21,518 cycles

EXCESSIVE FUEL VAPORS IN CABIN WHILE REFUELING. CREW REPORTED FUEL VAPOR ODOR EITHER APU BLEED OR GROUND AIR ONLY-WITH APU AND ENGINES NOT RUNNING. INSPECTED FOR LEAKS-NO LEAKS NOTED AT THIS TIME.

Part: FIRE BOTTLE — LOW PRESSURE (CARGO BAY) · airframe 21,874 hrs · 21,093 cycles

CARGO BOTTLE LOW, CAUTION MESSAGE. R & R LT CARGO FIRE BOTTLE IAW AMM 26, OPS CHECKED GOOD.

Part: SILL — CORRODED (FS 574-621) · corrosion level 2 · airframe 20,938 hrs · 20,139 cycles

CARGO BAY DOOR SILL HAS CORROSION AROUND NUT PLATES. R & R CARGO DOOR SILL IAW SRM 51-42-06.

Part: THRESHOLD — CORRODED (FS 310-349) · airframe 20,939 hrs · 20,139 cycles

PAX DOOR THRESHOLD AND ATTACHING HARDWARE CORRODED. REMOVED SURFACE CORROSION ON THRESHOLD IAW SRM 51-21-06. REPLACED THRESHOLD STEP HINGE IAW SRM 51-40-00.

Part: FLOOR SUPPORT — CORRODED (FS 574-621) · airframe 20,938 hrs · 20,139 cycles

CARGO BAY FLOOR SUPPORT BETWEEN FS 574 AND FS 621 HAS CORROSION NUT PLATE HOLES ON OTBD SIDE OF SEAT TRACK. REMOVED DAMAGED FLOOR SUPPORT CAP AND REPLACED WITH NEW FABRICATED SERVICEABLE PART IAW REO 601R-53-61-3178 IAW SRM 51-42-34. CUT OUT DAMAGED SECTION OF FLOOR SUPPORT ABOVE PULLEY BRACKET AND REPAIRED IAW REO 601R-53-61-4396.

Part: FLOOR SUPPORT — CORRODED (FS 574-621) · airframe 20,938 hrs · 20,139 cycles

CARGO BAY RT OTBD EDGE MEMBER HAS CORRODED AROUND NUT PLATES FROM FS 574 TO FS 621. R & R FLOOR EDGE MEMBER.

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 20,938 hrs · 20,139 cycles

ELONGATED HOLE UNDER MOLDED SEAL. REPAIRED IAW REO 601R-78-30-4091.

Part: SKIN — CHAFED (WING) · airframe 20,938 hrs · 20,139 cycles

UNDER EACH OTBD END OF PANEL 193AR WING SKIN HAS CHAFING. REPLACED SKIN DAMAGE 2 PLACES UNDER EACH OTBD END OF PANEL 193AB IAW SRM 51-12-00 AND REO 601R-57-21-880, REV C.

Part: SKIN — CHAFED (FS 409) · airframe 20,938 hrs · 20,139 cycles

UNDER EACH OTBD END OF PANEL 193AB WING SKIN HAS CHAFING. REPAIRED CHAFED SKIN DAMAGE 2 PLACES UNDER EACH OTBD END OF PANEL 193AB IAW SRM 51-12-00 AND REO 601R-57-21-880, REV C.

Part: DOUBLER — DAMAGED (RT TRUNNION) · airframe 20,938 hrs · 20,139 cycles

OVERSIZED HOLE DISCOVERED DURING COLD WORKING OF MLG TRUNNION LOWER FLANGE RT MOST AFT HOLE DOUBLER. REPAIRED DESCREPANT OVERSIZED HOLE IN RT MLG LOWER TRUNNION FLANGE DOUBLER IAW REO 601R-57-21-1596, REV.

Part: HINGE — GOUGED (RT WING LE FLAP) · airframe 20,938 hrs · 20,139 cycles

FWD SCREW JAMMED INTO RT OTBD FLAP OUTLET HINGE FLPA ARM AND HINGES BOX CLEVIS ARE GOUGED. BLENDED AREA RT OTBD FLAP, OTBD HINGE FLAP ARM AND HINGE BOX CLEVIS IAW REO 601R-57-54-210 AND REO 601R-57-21-1600.

Part: PLATE — CHAFED (PAX DOOR STRIKER) · airframe 20,938 hrs · 20,139 cycles

PAX DOOR FWD AND AFT STRIKER PLATES ARE CHAFING. BLENDED CHAFED AREA ON PAX DOOR FWD AND AFT STRIKER PLATES IAW CRJ 51-12-00. REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW REO 601R-52-11-296.

Part: SEAL — CHAFED (RT NACELLE) · airframe 20,938 hrs · 20,139 cycles

RT LOWER NOSE COWL HAS CHAFED T/E SEAL. R & R RT NOSE COWL T/E SEAL IAW CMM 71-14-01, SRS 091.

Part: RIB — CRACKED (RT NACELLE) · airframe 20,938 hrs · 20,139 cycles

NR 2 FRAME & RIB IN RT JET PIPE FAIRING IS CRACKED AT 9:00 POSITION AND DENTED AT A 3:00 POSITION. REMOVED AND REPLACED RIB.

Part: SKIN — CORRODED (SERVICE DOOR) · airframe 20,938 hrs · 20,139 cycles

SIX AREAS OF CORROSION AROUND SCREW HOLES ON INNER SKIN OF SERVICE DOOR. CORROSION FOUND TO BE SURFACE NO MATERIAL LOSS DETECTED IAW SRM 52-00-31.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 20,938 hrs · 20,139 cycles

CARGO HANDLE CUT OUT CHAFED IN 4 AREAS. BLENDED CARGO DOOR HANDLE CUT OUT CHAFED AREAS, MEASURED. FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO 601R-52-31-08.

Part: BULKHEAD — CHAFED (FS 280) · airframe 20,938 hrs · 20,139 cycles

FWD BULKHEAD FWD OF GALLEY CHAFED AND DENTED BY FWD LOWER COMPARTMENT DOOR. REPAIRED FWD BULKHEAD BS 280 BULKHEAD IAW REO 601R-53-11-1727.

Part: PANEL — CHAFED (FUSELAGE) · airframe 20,938 hrs · 20,139 cycles

PNL 412DB FWD BLADE CHAFED. REMOVED UNSERVICEABLE PANEL 412DB FWD BLADES AND REPLACED WITH SERVICEABLE BLADE PN 601R37138-25, 601R-37138-27 IAW SRM 57-42-06, 51-40-11.

Part: PANEL — CHAFED (AILERON) · airframe 20,938 hrs · 20,139 cycles

PANEL 594PB HAS CHAFING. BLENDED CHAFE AREA IAW SRM 51-12-00. REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW SRM 57-51-31.

Part: DOOR — CHAFED (MLG) · airframe 20,938 hrs · 20,139 cycles

MLG DOOR CHAFED. REMOVED EXISTING FILLER ON LT MLG DOOR L/E SRM 51-42-06 AND REPLACED WITH SERVICEABLE FILLER. BLENDED AREA ON LT MLG DOOR L/E MLG DOOR L/E IAW SRM 51-12-00, FOUND AREA IN LIMITS IAW REO 601R-52-82-033.

Part: FAIRING — MISSING (TE FLAP) · airframe 20,738 hrs · 19,935 cycles

AFTER TAKE OFF, AFTER FLAPS WERE RETRACTED, FELT ACFT SHUDDER, ON POST FLIGHT INSPECTION FOUND RT INBD FLAP, INBD AFT FLAP FAIRING MISSING, REQUEST INSPECTION. INSP RT INBD FLAP INBD HINGE POINT AND FOUND AFT FLAP FAIRING MISSING. R & R RT INBD FLAP ASSY.

Part: CLAMP — LOOSE (BLEED DUCT)

DEPARTING, AT 400 FT AGL, CARGO BOTTLE LOW MESSAGE C/W QRH. RETURN TO LAND, DURING TROUBLESHOOTING, FOUND LOOSE 10TH STAGE CLAMP ON BLEED AIR DUCT. RESECURED CLAMP. LEAK CHECKED IAW AWAC SUPP 99-15. R & R CARGO FIRE BOTTLE IAW AWAC SUPP 10-099. OPS CHECK GOOD.

Part: FIRE BOTTLE — LOW (CARGO BAY) · airframe 19,791 hrs · 18,957 cycles

"CARGO BLT LOW" MESSAGE - RETURN TO DEPARTURE. R & R LT CARGO FIRE BOTTLE IAW 26-25-20. CHECKED GOOD. REMOVED PLACARD AND MEL.

Part: BALLAST — FAILED (LAVATORY LIGHTS) · airframe 19,195 hrs · 18,323 cycles

STRONG PLASTIC ODOR THROUGHOUT CABIN. FOUND LAV LIGHT BALLAST BAD, R & R BALLAST.

Part: GASKET — DAMAGED (AC SUPPLY DUCT) · airframe 18,454 hrs · 17,569 cycles

VERY STRONG ODOR OF FUEL ONCE APU WAS RUNNING, SHUTDOWN APU AND APU SLOW TO SHUTDOWN. R & R GASKET ON BOTH AC SUPPLY DUCT IAW 21-51-13. OPS CK APU IAW 49-10-33. OPS CK GOOD RETURN TO SERVICE.

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 17,996 hrs · 17,116 cycles

SERVICE DOOR EXT BUTTON WILL NOT RELEASE. UNABLE TO OPEN SERVICE DOOR FROM EXTERIOR. LUBED SERVICE DOOR OUTER HANDLE ASSY IAW AMM 52-41-03. OPS CKS GOOD.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 16,734 hrs · 15,781 cycles

FS 559 BULKHEAD MISDRILLED AT STR 23L, REPAIRED IAW REO 601R-53-41-1203.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 16,734 hrs · 15,781 cycles

DURING VISUAL INSP OF FS 559, LBL 9, OTBD ANGLE CRACKED FROM LOWEST RIVET TO EDGE OF ANGLE. REPAIRED IAW REO 601R-53-41-260, REV D AND 601R-53-41-609, REV B.

Part: RIB — CRACKED (LT WING) · airframe 16,734 hrs · 15,781 cycles

BATT RIB IN LT WHEEL WELL IS CRACKED. REPAIRED IAW REO 601R-57-51-046, REV B.

Part: BRACKET — DETERIORATED (LT ENGINE) · airframe 16,734 hrs · 15,781 cycles

REPAIR SENSE LINE BRACKETS (C-CHECK) 601R-71-61-3941 - (BRACKETS ON LT ENGINE NOSE INLET COWL ATTACH FLANGE). REPLACED 4 STAND OFF BRACKETS IAW REO 601R-71-61-3941, PN 228-50020-145, -161, -162, -165.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 16,734 hrs · 15,781 cycles

HYD SYS NR 1 PRESSURE/RETURN FILTER MANIFOLD MOUNT BRACKET CRACKED ON AFT END. REPAIRED NR 1 HYD MANIFOLD SUPPORT BRACKET IAW REO 601R-53-62-031, REV A.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 16,734 hrs · 15,781 cycles

HYD SYS NR 2 PRESSURE/RETURN MANIFOLD MOUNT BRACKET CRACKED ON AFT END. REPAIRED NR 2 HYD MANIFOLD SUPPORT BRACKET IAW REO 601R-53-62-031, REV A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,734 hrs · 15,781 cycles

FS 280 FLOOR SUPPORT LBL INBD CLIP IS CRACKED. R & R CLIP PN 601R3111357 IAW REO 601R-53-11-138, REV NC.

Part: BRACKET — CRACKED (BS 529) · airframe 16,734 hrs · 15,781 cycles

BRAKE TRANSDUCER MOUNTING BRACKET IN RT MLG WHEEL WELL IS CRACKED. R & R WITH SERVICEABLE BRACKET PN 601R75262-157 AT RT MLG WHEEL WELL ALL WORK DONE IAW SRM 51-40-11, 51-42-06, 51-22-00, 51-21-11, 51-25-06, 51-25-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,734 hrs · 15,781 cycles

FS 280, FLOOR SUPPORT RBL 9 OTBD CLIP IS CRACKED. R & R CLIP IAW REO 601R-53-11-171, REV D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,734 hrs · 15,781 cycles

FS 280 FLOOR SUPPORT RBL 9 INBD CLIP IS CRACKED. R & R CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 16,734 hrs · 15,781 cycles

FS 280 FLOOR SUPPORT UPPER ANGLE IS CRACKED AT LBL 12. REPAIRED IAW REO 601R-53-11-138, REV NC.

Part: PLATE — CRACKED (BS 589) · airframe 16,734 hrs · 15,781 cycles

CARGO DOOR LANDING PLATE CRACKED AT FS 589. REPAIRED LANDING PLATE IAW 601R-53-61-433, REV B.

Part: LUG — GOUGED (TE FLAP) · airframe 16,734 hrs · 15,781 cycles

RT INBD FLAP HINGE BOX AFT LUGS ON WING ARE GOUGED (DWG 601R10315 REF). REPAIRED DAMAGED LUGS ON TR INBD FLAP, INBD HINGE BOX AFT LUGS IAW REO 601R-57-21-1276.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 16,734 hrs · 15,781 cycles

RT FS 484 INTERCOSTAL, INBD CLIP APPEARS CRACKED. RBL 27 R & R UNIT SERVICEABLE CLIP PN 601R31171-9, PO 961346 AT RT FS 484, RBL 27. INBD SIDE ALL WORK DONE IAW REO 601R-53-41-059, REV B AND SRM 51-25-16.

Part: COALESCER BAG — ODOR (NR 1) · airframe 16,733 hrs · 15,781 cycles

AFTER APU START UP JET-A SMELL IN COCKPIT. R & R PACK NR 1 COALESCER IAW 21-51-13 IAW AMM 21-51-13. OPS CHECK GOOD, SUSPECT APU OVER OIL SERVICED, CLEANED UP OIL, NO LEAKS.

Part: APU — ODOR · airframe 16,604 hrs · 15,653 cycles

AFTER APU START-UP, JET A SMELL IN COCKPIT. R & R NR 1 PACK COALESCER IAW AMM 21-51-13. OPS CK GOOD, SUSPECT APU OIL OVERSERVICED, CLEANED UP OIL, NO LEAKS NOTED.

Part: PCU — OUT OF RIG (AILERONS) · airframe 13,792 hrs · 12,879 cycles

DURING FLT AN ABNORMAL AMOUNT OF LT AILERON TRIM WAS REQUIRED F/O WINGS LEVEL FLIGHT, FLT CTL POS IND, LT AILERON UP AND RT AILERON CTR. FOUND LT AILERON PCU OUT OF RIG. RIGGED LT AILERON PCU IAW AMM 27-11-00. OPS CHECK GOOD AT THIS TIME. (K)

Part: BRACKET — CRACKED (LT NACELLE) · airframe 12,094 hrs · 11,249 cycles

LT ENGINE INLET, QTY (2) BRACKETS CRACKED AT 4 & 5 O`CLOCK POSITION NEAR LOWER OUTBOARD T/R ACTUATOR (LOOKING AFT). QTY (2) BRACKETS AT 4 & 5 O`CLOCK POSITION NEAR THE LOWER OUTBOARD T/R ACTUATOR OF THE LT ENGINE INLET REPLACED IAW CRJ 200 SRM 51-42-06. (S)

Part: WEB — CRACKED (BS 280) · airframe 12,094 hrs · 11,249 cycles

CRACK FOUND ON WEB STRUCTURE FS 280 RBL 9. REPAIRED IAW REO 601R-53-11-171 REV D. (S)

Part: BULKHEAD — CRACKED (BS 621) · airframe 12,094 hrs · 11,249 cycles

REAR PRESSURE BULKHEAD CRACKED AROUND LINTER FITTING ATTACHMENT POINT. REPAIRED IAW CRJ 200 REO 601R-53-61-1230 REV D. (S)

Part: BRACKET — CRACKED (BS 280) · airframe 12,094 hrs · 11,249 cycles

BRACKET CRACK ON FS 280 LBL 9 ON FLOOR STRUCTURE. ON FS 280 LBL 9 ON FLOOR STRUCTURE (2) BRACKET REPLACED IAW SRM 51-42-21 AND SRM 51-42-06. (S)

Part: FLAP SYSTEM — INOPERATIVE (TE FLAPS) · airframe 11,962 hrs · 11,121 cycles

FLAPS FAILED AT 20 DEGREES, COMPLIED WITH QRH, LANDED DCA. LANDED NORMAL, MAX BTMS READING 4 FOR ALL BRAKES. RESET PER AWAC SUPPLEMENT 98-018B. (M)

Part: LIGHT — SHORTED (COCKPIT) · airframe 11,865 hrs · 11,030 cycles

BOTH CAPTAIN AND FIRST OFFICER MAP LIGHTS ARE OUT, CBP2 U6 POPPED. RECYCLED BREAKER ONCE, FIRST OFFICER MAP LIGHT SPARKED AND SHORTED WHEN MOVED, CBP2 U6 POPPED AGAIN. (M)

Part: BRAKE ASSY — MALFUNCTIONED (MOTOR BRAKE) · airframe 11,660 hrs · 10,844 cycles

FLAPS HALF SPEED MESSAGE ON ED2. REMOVED AND REPLACED MOTOR BRAKE UNIT IAW 27-52-05. OPS CHECK GOOD AT THIS TIME. (M)

Part: DETECTOR — MALFUNCTIONED (T/E FLAP) · airframe 11,660 hrs · 10,844 cycles

ON SHORT FINAL FLAPS FAILED AT 45 DEGREES. RAN QRH. NO FURTHER PROBLEMS. REMOVED AND REPLACED SKEW DETECTION UNIT IAW AMM 27-51-15. OPS CHECK GOOD IAW AMM 27-54-00. (K)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

NOSE GEAR DISAGREE WHEN GEAR RETRACTED. NOSE GEAR SHOWED RED, ALSO HEARD CLICKING NOISE BELOW FEET. AIR RETURN TO BTV, UPON GEAR EXTENSION GEAR SHOWED 3 GREEN DOWN AND LOCKED. (K)

Part: FLAP — STUCK (WING) · airframe 11,573 hrs · 2,128 cycles

INFLIGHT, FLAPS STUCK AT 42 DEGREES WHEN SELECTED 45 DEGREES. AFTER 10 MINUTES, FLAPS WENT TO 45 DEGREES, NO FAULT MESSAGES ILLUMINATED. (K)

Part: FLAP — FAILED (WING) · airframe 11,573 hrs · 10,758 cycles

FLAPS FAIL CAUTION IN FLIGHT. FLAPS FAILED AT 40 DEGREES. EMERGENCY LANDING DECLARED. LANDING UNEVENTFUL. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-108B STEPS 1.3 AND 1.4, FLAPS SYSTEM RESET OK. (K)

Part: BPSU — FAULTY (T/E FLAP) · airframe 11,573 hrs · 10,756 cycles

FLAPS FAIL CAS MESSAGE, BOTH FLAPS INDICATE 42 DEGREES. PERFORMED FLAPS RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4 FLAPS RESET OK. (FERRIED TO ORF DUE TO HISTORY) LT BPSU WON`T STAY IN RIG. REMOVED AND REPLACED LT PBSU IAW AMM 27-51-10-. OPS CHECK GOOD. (K)

Part: TRIM SYSTEM — MALFUNCTIONED (STABILIZER)

ON CLIMBOUT WITH FLAPS 8 DEGREES, STAB AND MACH TRIM WOULDN`T REMAIN ENGAGED. COMPLIED WITH QRH, RE-ENGAGED STAB AND MACH TRIM, BOTH DISENGAGED AND WOULDN`T REENGAGE. SET FLAPS TO 2- DEGREES, RETURNED TO DEPARTURE. REMOVED AND REPLACED FO`S HORIZONTAL STAB TRIM SWITCH IAW AMM 27-14-05, NO FIX. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. OPS CHECK GOOD, IAW AMM 27-40-00. (K)

Part: PCU — UNKNOWN (AILERONS)

EXCESSIVE LEFT DOWN AILERON TRIM REQUIRED FOR LEVEL FLIGHT, REQUEST INSPECTION. REMOVED AND REPLACED NR 1 AILERON PCU PER AMM 27-14-01, OPS AND LEAK CHECK GOOD. RIG CHECK PER AMM 27-11-00, RIG CHECK GOOD. (M)

Part: DOOR SEAL — UNKNOWN (SERVICE DOOR) · airframe 8,560 hrs · 7,824 cycles

SERVICE DOOR DIFFICULT TO LATCH AND UNLATCH. REMOVED AND REPLACED SERVICE DOOR SEAL IAW 52-41-07. (K)

Part: FLOOR SUPPORT — CRACKED (BS 621)

FOUND CARGO FLOOR SUPPORT ANGLE AT FS 621 CRACKED APPROX .5 INCH LEFT SIDE. MAINTENANCE REPAIRED LT FS 621 FLOOR SUPPORT ANGLE BY REMOVING DAMAGED ANGLE AND INSTALLING NEW ANGLES AND STRAP IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)

Part: ANGLE — CRACKED (BS 484)

FOUND ANGLE CRACKED AT FS 484 RBL 27 IN UPPER CORNER APPROX .5 INCH IN RADIUS. MAINTENANCE FABRICATED REPAIR ANGLE FROM MATERIAL P/N 56144-14 IAW BSC STANDARD REPAIR 601R-53-0029 AND INSTALLED ANGLE AT FS 484 RBL 27 IAW BOMBARDIER AEROSPACE REO 601R-53-41-059. (M)

Part: FLOOR SUPPORT — CRACKED (BS 621)

FOUND CARGO FLOOR SUPPORT ANGLE AT FS 621 CRACKED APPROX .5 INCH RIGHT SIDE. MAINTENANCE REPAIRED RT FS 621 FLOOR SUPPORT ANGLE BY REMOVING DAMAGED ANGLE AND INSTALLING NEW ANGLES AND STRAP IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FOUND INTERCOSTAL CRACKED AT FS 484 RBL 36 IN UPPER RADIUS. MAINTENANCE REPAIRED FS 484.0 INTERCOSTAL AT RBL 36 BY REMOVING DAMAGED FLANGE AREA, FABRICATING NEW ANGLE ABD INSTALLING IAW BOMBARDIER REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 601R-53-0030A. (M)

Part: ANGLE — CRACKED (BS 625)

FOUND FS 625 OBLIQUE ANGLE IS CRACKED .500 INCH LONG. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601-35012-51, IAW CRJ SRM 51-42-06. (M)

Part: ACTUATOR — INOPERATIVE (NLG WW) · airframe 6,597 hrs · 5,949 cycles

BETWEEN GEAR RETRACTION AND EXTENSION, HEARD FLAPPING SOUND FROM NOSE AREA. REMOVED AND REPLACED NLG DOOR ACTUATOR. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,532 hrs · 6,229 cycles

RT FS 484.00 AT RBL 36 ANGLE CRACKED.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

PERMANENT REPAIR TO LIGHTNING STRIKE DAMAGE AT FS 755, STRINGER 25L. REPAIRED DAMAGE BY ENLARGING FASTENER HOLE TO .1875 INCH AND INSTALLED RIVET MS2042AD6 IAW BRAS WO 601R-53-5674.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 3,805 hrs · 3,314 cycles

PERFORMED PERMANENT REPAIR TO LIGHTNING STRIKE DAMAGE AT FS 280 TO FS 349 ALONG STRINGER L26 (5) LOCATIONS. PERFORMED PERMANENT REPAIR TO FUSELAGE AT FS 280 TO FS 349 ALONG STRINGER 26L IAW EO 601R-53-5672.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 3,769 hrs · 3,284 cycles

INTERCOSTAL CRACKED IN RADIUS APPROX 1.1 INCH LONG, FS 621- FS 625.1, STR 14R. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE PN 601-35012-52 USING MS20470AS5 RIVETS IAW CRJ SRM 57-040-06.

Part: CONTROL UNIT — FAILED (TE FLAPS)

FLAP FAIL MESSAGE ILLUMINATED AT 13000 FT, COMPLIED WITH QRH PERFORMED ZERO FLAP LANDING, BRAKES APPLIED AT LESS THAN 80 KNOTS, MAX BRAKES TEMP INDICATION WAS '2'. TOUCHDOWN AT 172 KNOTS. REMOVED AND REPLACED FECU IAW AMM 27-51-05. COMPLIED WITH OPS CHECK OF FLAP SYSTEM IAW AMM, OPS CHECK GOOD. (M)

Part: CONTROL HANDLE — FAILED (TE FLAPS)

UNCOMMANDED FLAP ACTUATION IN FLIGHT AT CRUISE 0-6 DEGREES WITH FLAP SETTING ZERO ALL OTHER SETTINGS NORMAL OPERATION. REMOVED AND REPALCED FECU AND FLAP HANDLE. (M)

Part: TAIL CONE — DAMAGED (FUSELAGE)

DAMAGE TO TAIL CONE, RESULTING IN DELAMINATION OF INNER AND OUTER SKINS AND CORE DAMAGE. REPAIR, FABRICATED SKIN PLIES TWO EACH AND EXTRA PLY ONE EACH FOR EACH DAMAGED SKIN FROM KEVLAR 49 STYLE 281 FABRICATED PREPEG CMS532-01. EXTRA PLY TO EXTEND .5 INCHES PAST THE OUTER SCARF LINE. FABRICATE CORE PLUG FROM CMS599-01, .050 INCHES THICK. (M)