N454AW

Part: BUTTON — ENGAGED (APU FIRE) · airframe 40,993 hrs · 40,015 cycles

REVEIVED APU FIRE INDICATION AFTER APU START, C/W QRH MSG CLEARED IN 5 SECONDS. ALSO HAD APU FIRE FAIL AND APU ECU FAULT CAUTION MSG'S -ALL MSG'S CAME ON AT THE SAME TIME APU FIRE BOTTLE NOT BLOWN. AIRCRAFT REMOVED FROM SERVICE. FOUND APU FIRE PUSHBUTTON ENGAGED, DISENGAGED APU FIRE PUSHBUTTON. AND PERFORMED OPS CHECK OF APU FIRE EXT SYSTEM IAW AMM 26-22-00. OPS CHECK GOOD.

Part: CONTROL UNIT — FAULTED (MAIN AVIONICS CO) · airframe 40,783 hrs · 39,777 cycles

FLAP FAIL AT 20 ON APPROACH WHILE SELECTING FLAPS 30 PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. R&R FECU IAW AMM 27-51-05-04. OPS CHECK GOOD AT THIS TIME. REMOVED PLACARD AND REMOVED FROM MEL .

Part: APU — SMOKE (AFT) · airframe 40,543 hrs · 39,512 cycles

SMOKE TOILET CAUTION MSG SHORTLY AFTER TAKE OFF. MSG DISAPPEARED 3 MINUTES LATER. C/W QRH. ********AIRCRAFT REMOVED FROM SERVICE********* REF LP 338553-4 FOR CORRECTIVE ACTION. SMOKE DETECTOR OPS CHECK NORMAL IAW AMM 26-16-00. REF WO 335707, APU R&R FOR CORRECTIVE ACTION. REMOVED PLACARD AND FROM MEL.

Part: APU — SMOKE (AFT) · airframe 40,543 hrs · 39,512 cycles

APU SHUTDOWN ON GND AND CAUSED SMOKE IN CABIN *****AIRCRAFT REMOVED FROM SERVICE********** PREFORMED PAC BURN OUT PROCEDURE IAW AWAC SUP 09-037E, NO UNUSUAL SMELLS OR SMOKE IN CABIN AFTER PROCEDURE. REF 338553-4 FOR MEL OF APU. AIRCRAFT OK FOR RTS. REF WO 335707, APU R&R FOR CORRECTIVE ACTION. REMOVED PLACARD AND FROM MEL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,397 hrs · 389,338 cycles

364734-1 FO REPORTS SMOKE SMELL SIMILAR TO MARIJUANA COMING FROM THE GASPER, NO AIRCRAFT SYSTEM ABNORMALITY NOTED. C/W AWAC SUP 09-037D FOR USUAL ODORS, NO SMOKE SMELL NOTED AC OK FOR SERVICE

Part: FUEL CONTROL — UNKNOWN (ENGINE) · airframe 39,424 hrs · 38,226 cycles

DURRING OUR DECENT WE NOTICED N1 WILL NOT REDUCE BELOW 67% ON LH ENGINE. THROTTLE LEVER DID MOVE TO FLIGHT IDLE POSITION. NO CHANGE IN N1. WAS ABLE TO INCREASE N1 WHEN COMMANDED. ********AIRCRAFT REMOVED FROM SERVICE******** R&R LH FUEL CONTROL IAW AMM 73-21-01 OPS CHECK GOOD, LEAK CHECK GOOD. GOOD TO CONTINUE SERVICE

Part: INDICATOR — INOPERATIVE (STANDY ALTIMETER) · airframe 39,207 hrs · 38,013 cycles

ABORTED TAKE-OFF AT APPROX. 100 KNOTS DUE TO STANDBY ASI NOT COMING ALIVE. STANDBY ASI REMAINED AT ZERO. BRACKET TEMPS SHOWED 5,6,5,4. NO BRAKE OVERHEAT WARNING DISPLAYED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED STBY ALT /IND ASI (SA/IAS) IAW AMM 34-12-01 OPS CHECK GOOD. ORIG SUBMISSION DATE: 1/23/2023

Part: PLATE — CORRODED (THRESHOLD) · corrosion level 2 · airframe 39,124 hrs · 37,933 cycles

SERVICE DOOR THRESHOLD PROTECTOR (P/N; 601R38957-31) CORRODED INBD LOWER SURFACE. AIRCRAFT REMOVED FROM SERVICE. REPLACED SERVICE DOOR THRESHOLD PROTECTOR PER SRM 51-41-02 PAR 7

Part: ANGLE — CRACKED (BS 406) · airframe 39,124 hrs · 37,933 cycles

CRACKED MLG WHEEL BAY WEB, FWD OF OUTBOARD SIDE AT BS 409+128 ON THE AFT SPAR. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE ANGLE IAW EA AWAC-CRJ253-01913, REV IR.

Part: SEAT TRACK — CORRODED (BS 349-409) · corrosion level 2 · airframe 39,124 hrs · 37,933 cycles

LEFT CABIN SEAT TRACK, BS 349 - 409 HAD EVIDENCE OF SURFACE CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK BS 349 - 409 IAW AMM 53-01-11.

Part: SKIN — CORRODED (BS 333-349) · corrosion level 2 · airframe 39,124 hrs · 37,933 cycles

EXTERIOR SKIN UNDER FORWARD DRAIN MAST CORRODED. AIRCRAFT REMOVED FROM SERVICE. BLENDED & CUT OUT CORROSION AND INSTALLED EXTERNAL DOUBLER IAW EA AWAC-CRJ253-01922.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 39,124 hrs · 37,933 cycles

LEFT STRUCTURE CRACKED AT MLG WHEEL WELL BAY WEB FWD OF OUTBOARD SIDE AT FS 409+128 ON AFT SPAR. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LT MLG WHEEL BAY ANGLE IAW AWAC-CRJ253-1914 REV IR.

Part: SEAT TRACK — CORRODED (BS 349-409) · corrosion level 2 · airframe 39,933 hrs · 37,933 cycles

L/H CABIN SIDE SEAT TRACK BS 349 - 409 WAS CORRODED. R & R THE SEAT TRACK.

Part: NONE — NONE · airframe 37,952 hrs · 36,777 cycles

AFTER TAKEOFF RECEIVED STEERING INOP. C/W QRH, MESSAGE PERSIST. WORKED AFTER LANDING. R&R STEERING ELECTRO HYD SERVO VALVE AND PERF OP CK IAW AMM 32-51-15. NO DEFECTS AT THIS TIME. P/N: 16736-105, S/N OFF; DUO534, S/N ON: 1457 ARW

Part: ANGLE — CRACKED (PAX DOOR) · airframe 36,877 hrs · 35,641 cycles

PASSENGER DOOR STAIR TO DOOR SKIN ANGLE CRACKED AFT OF DOOR ASSIST CABLE PULLEY BRACKET. AIRCRAFT REMOVED FROM SERVICE. REMOVED CRACKED DOOR SKIN ANGLE AFT SIDE PASSENGER DOOR AND INSTALLED NEW SKIN ANGLE, IAW PL 601R-52-11-513.

Part: SKIN — DENTED (RT WING LE FLAP) · airframe 36,877 hrs · 35,641 cycles

RIGHT INBOARD FLAP HAS A DENT 9" X 6.4" X .087". DENT OUT OF LIMITS DUE TO DENT ON FASTENER ROW, IAW CRJ200-SRM57-52-00. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT INBOARD FLAP, IAW CRJ 200 AMM 27-54-01.

Part: PRESSURE BLKHD — CRACKED (ZONE 200) · airframe 36,877 hrs · 35,641 cycles

CRACK DETECTED ON FWD FACE OF AFT PRESSURE BULKHEAD AT RBL 18.00 36 INCHES ABOVE FLOOR AND ON LBL 36.20 6 INCHES ABOVE FLOOR LEVEL ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DAMAGE AREAS ON AFT PRESSURE BULKHEAD AT RBL 18.00, 36 INCHES ABOVE FLOOR LEVEL AND AT LBL 36.20; 6 INCHES ABOVE FLOOR LEVEL IAW BOMBARDIER REO 601R-53-61-1285 REV E

Part: BULKHEAD WEB — CRACKED (FS 621) · airframe 36,877 hrs · 35,641 cycles

CRACK DETECTED ON FWD FACE OF AFT PRESSURE BULKHEAD AT FS 621 LBL 36.2, 6" ABOVE THE FLOOR LINE. AIRCRAFT REMOVED FROM SERVICE. CRACK REPAIRED AT FS 621 LBL 36.2, 6" ABOVE THE FLOOR LINE, IAW REO 601R-53-61-1285.

Part: SKIN — CRACKED (FS 193) · airframe 36,877 hrs · 35,641 cycles

TRANSFORMER RECTIFIER SUPPORT SKIN CRACKED BETWEEN FS 193.00 AND HYDRAULIC SYSTEM 2 & 3 ACCUMULATOR SUPPORT BRACKET. AIRCRAFT REMOVED FROM SERVICE. REPAIRED RECTIFIER SUPPORT SKIN AT FS 193, IAW REO 601R-53-11-111.

Part: SEAT TRACK — CORRODED (FS 559+88) · corrosion level 2 · airframe 36,877 hrs · 35,641 cycles

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

Part: BULKHEAD WEB — CRACKED (FS 621) · airframe 36,877 hrs · 35,641 cycles

CRACK DETECTED ON FWD FACE OF AFT PRESSURE BULKHEAD AT RBL 18 36" ABOVE FLOOR LEVEL FS 621. AIRCRAFT REMOVED FROM SERVICE. REPAIRED DAMAGE ON AFT PRESSURE BULKHEAD AT RBL 18 FS 621 36" ABOVE FLOOR LEVEL, IAW BOMBARDIER REO 601R-53-61-1285 REV D.

Part: STRUCTURE — CORRODED (FS 574-605) · corrosion level 2 · airframe 36,877 hrs · 35,641 cycles

T-CAP EXTRUSION AT FS 574 T0 FS 605+10 CORRODED. AIRCRAFT REMOVED FROM SERVICE. REPLACE CORRODED T-CAP EXTRUSION AT FS 574 T0 FS 605+10 LBL 27, IAW BOMBARDIER DRWG 601R35031 REV P.

Part: SHUTOFF VALVE — MALFUNCTIONED (RT A/C PACK) · airframe 36,681 hrs · 35,438 cycles

RECEIVED R PACK HIGH PRESS CAUTION AFTER TAKEOFF IN CLIMB,PER QRH PER MEL MESSAGE DID NOT CLEAR RAN APENDIX B PER MEL. "AIRCRAFT REMOVED FROM SERVICE" R/R RH PRSOV IAW CRJ 200 AMM 21-51-43 OPS CHECK GOOD NO MSG ON EICAS SN OFF 1845 SN ON 1277 LEF

Part: WARNING MESSAGE — ILLUMINATED (SERVICE DOOR) · airframe 35,604 hrs · 34,388 cycles

SHORTLY AFTER TAKEOFF CREW RECEIVED A SERVICE DOOR CAUTION MESSAGE. THEY CIRCLED BACK AROUND TO LAND AT IAD. CREW SPOKE WITH MAINTENANCE UPON LANDING AND THE SERVICE DOOR INDICATION SYSTEM WAS PLACED ON MEL. AIRCRAFT DEPARTED WITH NO FURTHER ISSUES. SERVICE DOOR CAUTION MESSAGE AFTER T/O. SERVICE OUTER HANDLE UNLOCKED MESSAGE ON GROUND. PLACARDED AND PLACED ON MEL

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,251 hrs · 33,045 cycles

LT TRU DOOR LANDING SKIN IS CRACKED AT AFT LATCH CUTOUT. REPLACED LT TRU DOOR LANDING IAW SRM 51-42-13, 51-42-06 AND SUPP 17-280.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,251 hrs · 33,045 cycles

STR 27 HAS PITTING BETWEEN THE APB AND FS 605 FRAME. REPAIRED STR 27 IAW REO 601R-53-61-6766 AND SRM 53-00-03.

Part: PLUG — PULLED (FUSELAGE) · airframe 34,251 hrs · 33,045 cycles

FWD LT PRESSURE PANEL 131AL CUT OUT PREVIOUS FREEZE PLUG PULLED OUT OF SURROUND DOUBLER. REPAIRED.

Part: SUPPORT CHANNEL — CRACKED (BS 574) · airframe 34,251 hrs · 33,045 cycles

CARGO DOOR FOWARD TRACK SUPPORT CHANNEL WAS CRACKED. REMOVED AND REPLACED THE SUPPORT CHANNEL IAW SRM 51-42-02, AND 51-42-06.

Part: SUPPORT BRACKET — CRACKED (EXTRNL POWER) · airframe 34,251 hrs · 33,045 cycles

OTBD FWD AND INDB AFT SCREW HOLES FOR EXTERNAL RECEPTACLE CRACKED. REMOVED AND REPLACED THE EXTERNAL POWER RECEPTACLE SUPPORT BRACKET IAW SRM 51-42-21, AND SRM 51-42-06

Part: BRACKET — CRACKED (LT MLG WW) · airframe 34,251 hrs · 33,045 cycles

LEFT FWD ZEE BRACKET WAS CRACKED ON THE OTBD SIDE FOR HYDRAULIC VOLUMETRIC FUSE. REMOVED AND REPLACED THE BRACKET IN THE LT WHEEL WELL IAW SRM 51-42-06.

Part: BRACKET — CORRODED (PAX DOOR) · corrosion level 2 · airframe 34,251 hrs · 33,045 cycles

PAX DOOR AFT BRACKET CORRODED. REPLACED THE PAX DOOR BRACKET IAW SRM 51-42-13, AND 51-42-06.

Part: BRACKET — CRACKED (BS 529) · airframe 34,251 hrs · 33,045 cycles

LEFT TRANSDUCER BRACKET WAS CRACKED. REPLACED THE BRACKET.

Part: SEAL DEPRESSOR — BENT (PAX DOOR) · airframe 34,251 hrs · 33,045 cycles

PAX DOOR AFT UPPER SEAL DEPRESSOR BENT. REPAIRED.

Part: SEAT TRACK — CORRODED (BS 364-399) · corrosion level 2 · airframe 34,251 hrs · 33,045 cycles

LEFT SEAT TRACK NR 1 WAS CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,251 hrs · 33,045 cycles

Z ANGLE FWD OF RT TRANSDUCER BRACKET IS CRACKED. REPLACED Z ANGLE IAW SRM 51-41-02, 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 34,251 hrs · 33,045 cycles

RT TRANSDUCER BRACKET CRACKED. REPLACED RT TRANSDUCER BRACKET IAW SRM 51-41-02, 51-42-06.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 33,574 hrs · 32,394 cycles

FLAP FAIL CAUTION WHEN MOVING FLAPS 8-20. FLAPS STUCK IN 8 DEG POSITION. R&R LT BPSU IAW AMM 27-51-10 RIG AND FUNCTION CHECK GOOD IAW AMM 27-54-00 OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,807 hrs · 31,626 cycles

4214 EMERGENCY FLOOR LIGHTS ROW 9-12 INOP. WHEN TURNED ON REMOVED AND REPLACED BROKEN HARNESS AND ROW 12 IAW AWAC SUPP 16-371A, ALSO INSTALLED NEW QUICK DISCONNECTOR TO AIRCRAFT WIRING IAW ESPM, OPS CHECK GOOD,

Part: FRAME — CRACKED (BS 333) · airframe 31,183 hrs · 30,051 cycles

FRAME BS 333 IS CRACKED BETWEEN STRINGERS 1 AND 2L.

Part: FITTING — CORRODED (NLG DOOR) · corrosion level 2 · airframe 31,183 hrs · 30,051 cycles

UPON REMOVAL OF THE NLG SPADE DOOR FOUND EVIDENCE OF CORROSION UNDER THE LH HINGE FITTING

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · corrosion level 2 · airframe 31,183 hrs · 30,051 cycles

MAIN CABIN FLOOR SUPPORT IS CORRODED AT FASTENER HOLES LBL 28 BS 559+80 - 621.

Part: CARGO TRACK — CORRODED (BS 559-621) · corrosion level 2 · airframe 31,183 hrs · 30,051 cycles

THE CARGOTRACK WAS CORRODED AT BS 621-559+112 LBL 9 IN AFT CARGO

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,183 hrs · 30,051 cycles

FRAME 333 HAS CORROSION ON THE FWD SIDE BETWEEN STR 23R AND 22R.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,183 hrs · 30,051 cycles

FRAME FS333 HAS CORROSION ON AFT SIDE BETWEEN STR 26L AND 24R.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,183 hrs · 30,051 cycles

INTERCOSTAL THAT SITS ON TOP OF STR 25R HAS CORROSION ON BOTH SIDES BETWEEN FRAMES 349 AND 333.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,183 hrs · 30,051 cycles

SERVICE DOOR SILL ANGLE ATTACH FITTING AT FS 319.70 HAS CORROSION.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,183 hrs · 30,051 cycles

LT WING TO FUSELAGE PNL ATTACH STRUCTURE FS 476.00 IS CRACKED.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,183 hrs · 30,051 cycles

RT WING TO FUSELAGE PNL ATTACH STRUCTURE FS 469.65 IS CRACKED.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 31,183 hrs · 30,051 cycles

RT WING IB FLAP VANE CTR LE IS CHAFED AT STOP.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 31,183 hrs · 30,051 cycles

LT IB FLAP VANE IB LE CHAFED BY STOP.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,183 hrs · 30,051 cycles

RT FLOOR SILL DOUBLER FS 317 HAS CORROSION.

Part: PANEL — CRACKED (RT WING) · airframe 31,183 hrs · 30,051 cycles

RT WING LEADING EDGE, FUELING POINT ASSY, O/B SIDE PANEL IS CRACKED AT THE LOWER AFT CORNER.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 31,183 hrs · 30,051 cycles

RIGHT WINDOW SIDE POST LOWER OTBD CLIP IS CRACKED.

Part: BRACKET — CRACKED (COCKPIT) · airframe 31,183 hrs · 30,051 cycles

LEFT SIDE OF WINDSHIELD, LOWER CENTER POST BRACKET CRACKED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,183 hrs · 30,051 cycles

FS 621 TO FS 625 INTERCOSTAL MEMBER AT STR 14L IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,183 hrs · 30,051 cycles

FS 621 TO FS 625 CLIP, OBLIQUE ANGLE, ADJACENT TO FRAME FS 625 AT STR 14L IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,183 hrs · 30,051 cycles

484 CLIP CRACKED AT LBL27.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,183 hrs · 30,051 cycles

484 CLIP CRACKED AT LBL 36.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,183 hrs · 30,051 cycles

LEFT WING TO FUSELAGE PANEL ATTACH STRUCTURE FS 449.85 IS CRACKED.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,183 hrs · 30,051 cycles

LEFT WING TO FUSELAGE PANEL ATTACH STRUCTURE FS 461 IS CRACKED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,183 hrs · 30,051 cycles

FS 621 TO FS 625 INTERCOSTAL MEMBER AT STR 13L IS CRACKED.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,183 hrs · 30,051 cycles

RIGHT WING TO FUSELAGE PANEL ATTACH STRUCTURE, FS471.00 IS CRACKED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 31,183 hrs · 30,051 cycles

STR 3L AT FS 280.00 CRACKED.

Part: UNKNOWN — UNKNOWN · airframe 30,789 hrs · 29,702 cycles

ABORTED TAKE OFF DUE TO STRONG PULL TO THE RIGHT, BTMS READS 4,5,3,2 ABORTED AT 50 KNOTS.

Part: TIRE — BLOWN (LT MLG) · airframe 29,220 hrs · 28,210 cycles

BLEW TIRE ON LANDING, LT OUTER TIRE. NR 1 BRAKE HAD ICE ACCUMULATION. MX STATED THE TIRE LOOKS LIKE IT FLAT SPOTTED & BLEW. HYD QD'S WERE ATTACHED & NO OTHER VISIBLE ISSUES WITH BRAKE. CHANGING TIRE & BRAKE ASSEMBLY IAW 262050 2.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 28,262 hrs · 27,267 cycles

ABORTED TAKEOFF AT 60 KNOTS CONFIGURE SPOILER WARNING. FLIGHT SPOILER STATUS MSG INDICATED. BTMS 4,3 & 5,4. 1B PUMP TURNED BACK ON FLIGHT SPOILER STATUS MSG CLEARED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 28,260 hrs · 27,265 cycles

RECEIVED CONFIG SPLRS MSG ON TAKEOFF ROLL, ABORTED AT 70 KNTS. SPLRS WERE RETRACTED. TAKEOFF CONFIG OK MSG WAS PRESENT BTMS 5554.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 27,334 hrs · 26,359 cycles

EMERGENCY LIGHTING ROW 1 DOES NOT ILLUMINATE. RIBBON CABLE CONNECTOR IS WORN & REPLACED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,704 hrs · 25,754 cycles

EMERGENCY LIGHTS FLOOR LEVEL ROW 8 & BEYOND DO NOT ILLUMINATE.

Part: DOOR SEAL — DAMAGED (SERVICE DOOR) · airframe 26,593 hrs · 25,647 cycles

NOTED LOUD NOISE FROM SERVICE DOOR. ACFT DEPRESSURIZED AT FL210. CREW DONNED OXYGEN MASK & DECLARED AN EMER. CREW DESCENDED TO 11000 INITIALLY & DIVERTED. INSPECTED SERVICE DOOR & SEAL, FOUND HOLE IN SEAL ON UPPER AFT CORNER. R & R SERVICE DOOR SEAL IAW AMM 52-41-07. PERFORMED LEAK CHECK OPERATIONS, CHECKED GOOD.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 26,588 hrs · 25,643 cycles

54953-8000-0016 PAX DOOR OUTER HANDLE IS CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,587 hrs · 25,643 cycles

NUMBER 1 FLOOR SEAT TRACK RAIL AT LBL 9 IS CORRODE AT FWD FS 364.00 TO 370.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,587 hrs · 25,643 cycles

RIGHT CABIN FLOOR SUPPORT STRUCTURE INBD & OTBD FS 484 CLIPS CRACKED.

Part: SUPPORT — CRACKED (COCKPIT) · airframe 26,587 hrs · 25,643 cycles

RIGHT WINDSHIELD SIDE WINDOW POST SUPPORT IS CRACKED .

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,587 hrs · 25,643 cycles

NUMBER 1 FLOOR SEAT RAIL AT RBL 9 IS CORRODED AT FS 364 TO 370.

Part: SEAT TRACK — GOUGED (FUSELAGE) · corrosion level 2 · airframe 26,587 hrs · 25,643 cycles

LEFT SIDE SEAT AFT TRACK HAS GOUGE AT FS 551.00 & 559+25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,587 hrs · 25,643 cycles

RIGHT FLOOR SEAT TRACK HAS CORROSION NEAR FS 559+64.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 26,588 hrs · 25,643 cycles

CLOSING PANEL SUPPORT AT PAX DOOR CAM LATCH LEVER IS CRACKED.

Part: DRAG ANGLE — CRACKED (RT WING`) · airframe 26,588 hrs · 25,643 cycles

LEFT BATTERY RIB DRAG ANGLE IN RT MLG WW IS CRACKED.

Part: MOUNT BRACKET — CRACKED (HYD ACCUMULATOR) · airframe 26,588 hrs · 25,643 cycles

HYDRAULIC ACCUMULATOR NR 3, FWD MOUNT BRACKET CRACKED.

Part: MOUNT BRACKET — CRACKED (RT MLG WW) · airframe 26,588 hrs · 25,643 cycles

BRAKE PRESS TRANSDUCER MOUNT BRACKET IN RT MLG WW IS CRACKED.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 26,588 hrs · 25,643 cycles

CARGO DOOR SILL PLATE CRACKED FROM RIVET AT FS 589 & 605.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,588 hrs · 25,643 cycles

INBOARD & OUTBOARD FLOORBEAM ATTACH CLIPS AT FS 280 & RBL 9 ARE CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,588 hrs · 25,643 cycles

INBOARD & OTBD FLOORBEAM ATTACH CLIPS CRACKED AT FS 280 & LBL 9.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,588 hrs · 25,643 cycles

PASSENGER DOOR LOWER SILL LOWER FLOOR SUPPORT ANGLE CORRODED AT NUTPLATES, GND TERMINAL & PROX SENSOR.

Part: HINGE FITTING — GOUGED (RUDDER) · airframe 26,588 hrs · 25,643 cycles

54953-3000-0039 RUDDER UPPER CTR HINGE FITTING LOWER HALF GOUGED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,588 hrs · 25,643 cycles

FS 280 BULKHEAD WEB LOWER FLANGE CRACKED AT RBL 12 - 14.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,588 hrs · 25,643 cycles

RIGHT UPPER OBLIQUE ANGLE CRACKED AT FS 621 - 625.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,588 hrs · 25,643 cycles

AFT FLOOR SUPPORT ANGLE ON FS 280 BULKHEAD IS CRACKED AT LBL 14.

Part: POST — CRACKED (FUSELAGE) · airframe 26,588 hrs · 25,643 cycles

RBL 18 VERTICAL POST ON FS 409+128 BULKHEAD CRACKED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,588 hrs · 25,643 cycles

54953-8000-0006 PAX DOOR STAIR AFT DRAG ANGLE CRACKED.

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 23,184 hrs · 22,356 cycles

CLIMBING THROUGH FL210, FELT BUMP IN ACFT SIMILAR TO WAKE TURBULANCE. IMMEDIATELY FOLLOWED BY O/B GROUND SPOILERS AND SPOILERONS STATUS MESSAGES. MESSAGES CLEARED. SEQUENCE REPEATED TWO MORE TIMES. LOSS OF INTERCONNECT FOR SECU 1 LOGGED IN MDC. REMOVED AND REPLACED SECU 1 AS PER AMM 27-61-05. OPS CHECKED GOOD S/N OFF 1046 S/N ON 01513

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 23,132 hrs · 22,302 cycles

AFTER TAKEOFF, GEAR DISAGREE WARNING ILLUMINATED ALONG WITH RED CROSS-HATCH SYMBOL FOR RIGHT MAIN GEAR. USING THE QRH, THE GEAR WAS SUCCESSFULLY LOWERED. ATC ISSUED DELAYING VECTORS FOR US TO REACH LANDING WEIGHT. WE DECLARED AN EMERGENCY TO HAVE CFR STANDING BY AS A PRECAUTION. A NORMAL LANDING IN HSV OCCURRED AND MAINTENANCE CONTROL WAS CONTACTED AFTER THE FLIGHT. REF 244351/1 GEAR DISAGREE AFTER T/O C/W M ACTION. T/S PER FIM , SUP 08-067 NO DEFECTS NOTED. C/W SYS TEST ON LANDING GEAR PRIORITY VALVE, OP CHECK GOOD. FUNCTIONAL TEST OF EXT/RETRACTION ALL IAW 32 30 00, OP CHECK GOOD. REMOVE PLACARD/MEL.

Part: CONTROL UNIT — INOPERATIVE (NLG STEERING) · airframe 20,597 hrs · 19,873 cycles

STEERING INOPERATIVE CAUTION ON CLIMBOUT. WOULD NOT RESET IAW QRH. MESSAGE CLEARED WITH STEERING OFF. EMERGENCY DECLARED, LANDED UNEVENTFULLY. DUPLICATED FAULT, FOUND ECU DOES NOT GO INTO AIR MODE INTERMITTENTLY, REPLACED ECU IAW AMM 32-41-01. STEERING OPS CK GOOD.

Part: TERMINAL BLOCK — BURNED (WINDWSHIELD) · airframe 18,390 hrs · 17,534 cycles

STRONG BURNING ODOR COMING FROM CAPTS WINDSHIELD IN FLT. TURNED OFF WINDSHIELD HEAT ODOR DISAPATED. FOUND LT HEATER RING TERMINAL RING BURNED RETERMINATED RING TERMINALS P1 AND P2 LT W/D HEATER PERFORMED OPS TEST TEMP CONTROLLER IAW 30-41-01, OPS CK GOOD.

Part: WIRE HARNESS — MALFUNCTIONED (ANTI SKID SYS) · airframe 17,823 hrs · 16,932 cycles

ANTISKID OTBD FAIL OCCURRED AFTER T/O AND RT THRUST REVERSER UNSAFE, PERFORMED QRH, DIVERTED, ANTISKID OTBD MESSAGE REOCCURRED ON LANDING. CHANGED ANTISKID SUB ASSY HARNESS, OPS CK GOOD.

Part: FAIRING — CHAFED (FUSELAGE) · airframe 17,484 hrs · 16,586 cycles

RT STUB FAIRING HAS CHAFING DAMAGE, REMOVED SEAL RETAINERS, LOCATED AND INSTALLED NEW SERVICEABLE SEALS ON NEW SERVICEABLE STUB FAIRING PN 601R3199-92.

Part: FITTING — CHAFED (TE FLAP) · airframe 17,484 hrs · 16,586 cycles

LT OTBD FLAP, FLAP ROLLER GUIDE FITTING CHAFED. REPAIRED LT OTBD FLAP, FLAP ROLLER GUIDE FITTING IAW REO 601R-57-53-839, REV.

Part: FITTING — CHAFED (E/E BAY DOOR) · airframe 17,484 hrs · 16,586 cycles

MAIN AVIONICS COMPARTMENT DOOR FWD LT DOOR SUPPORT FITTING CHAFED. REPAIRED IAW REO 601R-53-21-1218.

Part: STRUCTURE — GOUGED (CARGO DOOR) · airframe 17,484 hrs · 16,586 cycles

BAGGAGE DOOR LWR COAMING HALF IS GOUGED AT FWD LWR AND AFT SIDES. R & R CARGO DOOR UPPER AND LWR COAMING IAW SRM 51-42-02 & 51-42-13.

Part: HINGE FITTING — DAMAGED (TE FLAP) · airframe 17,484 hrs · 16,586 cycles

LT INBD FLAP HINGE BOX CHANGE BLENDED OUT DAMAGE IAW REO 601R-57-21-1371.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,484 hrs · 46,586 cycles

FS559 PRESSURE BULKHEAD REQ`S REO 601R-53-41-260, 601R-53-41-609 CURRENT REVISIONS TO BE COMPLIED WITH IAW CUSTOMER REQUEST. COMPLIED WITH REPAIR OF FS 559. PRESSURE BULKHEAD IAW CUSTOMER REQUEST BY FULL INCORPORATION OF REO 601R-53-41-260 REV E. INCLUDING DEVIATIONS REO`S 601R-53-41-609, REV B DEVIATION E & 601R-53-41-1326 LT & RT LBL27-RBL27.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,484 hrs · 16,586 cycles

FS559 PRESSURE BULKHEAD REQ`S REO 601R-53-41-1116 CURRENT REVISION TO BE COMPLIED WITH IAW CUSTOMER REQUEST. COMPIED WITH THE REPAIR & REINFORCEMENT OF THE FS559 LOWER CAP ANGLES AT BL9 & 1/8 LT & RT SIDE IAW REO 601R-53-41-1116, REV B.

Part: DOOR — CHAFED (RT MLG) · airframe 17,484 hrs · 16,586 cycles

RT MLG DOOR L/E HAS CHAFING DAMAGE IN 2 PLACES. REPAIRED CHAFE DAMAGE ON RT MLG DOOR L/E IAW REO 601R-52-82-297.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,484 hrs · 16,586 cycles

RT RBL9 BATHTUB FITTING CRACKED. REMOVED UNSERVICEABLE BATHTUB FITTING, INSTALLED SERVICEABLE BATH TUBE FITTING PN 600-31168-19 IAW SRM 51-42-21.

Part: SKIN — DENTED (SPOILER) · airframe 17,484 hrs · 16,586 cycles

RT INBD GROUND SPOILER LWR SKIN HAS MULTIPLE DENTS. REMOVED PAINT ONLY, FOUND 1 DENT TAP TEST NDI AND RESTORED FINISH IAW SRM 51-21-11, 51-25-16, 51-25-06, 51-72-00 AND REO 601R-57-71-252.

Part: ANGLE — CHAFED (LT PYLON) · airframe 17,484 hrs · 16,586 cycles

LT PYLON PANDL 412BT ANGLE CHAFED THRU. REMOVED UNSERVICEABLE ANGLE FROM LT PYLON PANEL 412BT. INSTALLED SERVICEABLE ANGLE PN 601-37003-183 ON LT PYLON PANEL 412BT.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 17,484 hrs · 16,586 cycles

RT RBL 27 AND 36, 484 CLIPS CRACKED. R & R CLIP AT FS 484, RBL 36 IAW REO 601R-53-41-059, REV B. REF TO WO 51981/1000/0042 FOR REPLACEMENT OF FS484, RBL 27 CLIP.

Part: RETAINER — CRACKED (LT PYLON) · airframe 17,484 hrs · 16,586 cycles

LT PYLON PANEL 412DB HAS A CRACKED SEAL RETAINER. R & R SEAL RETAINER IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,484 hrs · 16,586 cycles

FLOORBEAM IS CORRODED AROUND 7 SCREW HOLES UNDER CARGO PIT FLOORBOARD 281 LLF. R & R FLOORBEAM CAP AT LBL 27.0, BETWEEN FS 569 AND FS 610, WL 73.10 IAW REO 601R-53-61-3778.

Part: SEPARATOR — WORN (LT PYLON) · airframe 17,484 hrs · 16,586 cycles

LT PYLON PANEL 412DB SEPARATORS ARE KNIFE EDGE. R & R SEPARATORS IAW SRM 51-42-06.

Part: SEAL — CHAFED (RT COWLING) · airframe 17,484 hrs · 16,586 cycles

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

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 17,484 hrs · 16,586 cycles

RT HYDRAULIC SYSTEM NR2 FILTER BRACKET CRACKED. REPAIRED NR2 HYD SYSTEM MANIFOLD SUPPORT BRACKET IAW REO 601R-53-62-031, REV A.

Part: SEAL — CHAFED (RT COWLING) · airframe 17,484 hrs · 16,586 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,484 hrs · 16,586 cycles

LT OBLIQUE ANGLE CRACKED. R & R LT OBLIQUE ANGLE IAW REO 601R-53-61-422, REV NC.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,484 hrs · 16,586 cycles

RT OBLIQUE ANGLE CRACKED. R & R RT OBLIQUE ANGLE IAW REO 601R-53-61-422, REV NC.

Part: WEB — TORN (FUSELAGE) · airframe 17,484 hrs · 16,586 cycles

WEB UNDER LBL 9 POST IS TORN AT UPPER HI LITE FASTENER HOLE . REPAIRED FS 559 WEB UNDER LBL 9 POST AT UPPER HI LITE FASTENER IAW REO 601R-53-41-1321-1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,484 hrs · 16,586 cycles

LT LBL27 & 36 484 CLIPS CRACKED. R & R CRACKED CLIP AT FS 484, LB 27 OTBD SIDE IAW REO 601R-53-41-059, REV B (REF TO W/O 51981/1000/0041 FOR REPLACEMENT OF CLIP AT FS 484, LBL 36).

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,484 hrs · 16,586 cycles

INTERCOSTAL CLIP CRACKED AT FS484, LT OTBD LBL36. R & R CLIP AT FS484, LT OTBD LBL36 IAW REO 601R-53-41-059, REV B.

Part: SKIN — CORRODED (RT INTAKE) · airframe 17,484 hrs · 16,586 cycles

RT ENG INLET LIP SKIN PITTED. REMOVED LIGHT PITTING ON RT ENG INLET LIP SKIN BY SANDING. REMOVING .004 MATERIAL WITH .059 MATERIAL REMAINING, THE LIPSKIN IS WITHIN LIMITS IAW CMM 71-61-01, FIG 5003 LIGHT.

Part: SKIN — ERODED (LT INTAKE) · airframe 17,484 hrs · 16,586 cycles

LT ENGINE INLET LIP SKIN HAS EROSION DAMAGE. LT ENGINE INLET LIPSKIN HAS CORROSION AT 315 AREA, SANDED LIPSKIN REMAINING .003 MATERIAL WITH .060 MATERIAL. REMAINING AREA IS WITHIN LIMITS IAW CMM 71-61-01, FIG 5003N.

Part: CONTROLLER — MALFUNCTIONED (WINDSHIELD HEAT) · airframe 17,339 hrs · 16,428 cycles

RT WINDSHIELD HEAT CONTROLLER CAUTION MESSAGE INFLIGHT. DUE TO WEATHER, PERFORMED AIR RETURN TO DEPARTURE. R & R RT WINDSHIELD HEAT CONTROLLER IAW AMM 30-41-01. OPS CK GOOD.

Part: DETECTOR — MALFUNCTIONED (FLAP SKEW) · airframe 14,144 hrs · 13,134 cycles

UPON CLIMBOUT FLAP FAIL AT 20 DEGREES WHEN HANDLE SELECTED TO 8 DEGREES. RESET IAW SUPP 98-018C. REF 190586/2 - TROUBLESHOT TO SKEW DETECTION UNIT, REMOVED AND REPLACED SKEW DETECTION UNIT IAW AMM 27-51-15, CYCLED FLAPS 8 CYCLES. OPS CHECK GOOD. REMOVED FROM MEL. (K)

Part: WIRE — SHORTED (WINDOW HEAT) · airframe 13,352 hrs · 12,363 cycles

ENROUTE, CAPTS MAIN WINDOW HEATING ELEMENT SPARKED OR GLOWED. SMALL BLUE ARC APPEARED. TURNED OFF LT WINDOW HEAT. GLOW WENT AWAY. BURNING ODOR WENT AWAY . FOLLOWED QRH PROCEDURES CONTINUED TO DESTINATION. HAPPENED WITHIN 10 MINUTES OF DESTINATION. INSPECTED WIRES HC72C14WHT AND HC73C19BLU CONNECTIONS TO HEATING ELEMENTS. FOUND HC73C14BLU CONNECTION AT HEATING ELEMENT TO BE SHORTED TO GROUND. REPLACED TERMINAL AND REINSTALLED IAW ESPM. FOLLOWED FIM 30-41-00, PAGE 2, SHEET 1 OF 7 AND AMM 30-41-00. OPS CHECK GOOD AT THIS TIME. (K)

Part: UNKNOWN — FUMES (COCKPIT) · airframe 13,352 hrs · 12,363 cycles

ELECTRICAL FUMES IN COCKPIT, UNABLE TO IDENTIFY SOURCE. COMPLIED WITH QRH (30 MILES ON APPROACH). INSP ACFT FWD CABIN AND COCKPIT LIGHTS, COOLING FANS AND DISPLAY SCREENS OPER BATT AC PAD FROM BATT ENG AND APU AIR. ALSO INSP GALLEY AREA AND COFFEEMAKER, NO ELECTRICAL ODOR OBSERVED. ACFT IS OK FOR SERVICE. (K)

Part: HYDRAULIC SYSTEM — OVERSERVICED · airframe 13,352 hrs · 12,363 cycles

UPON GEAR RETRACTION RT MLG DISAGREE MSG. MSG CLEARED AFTER 30 SECONDS. HYD QTY 3 WAS 95 DEGREE SHOWN WHITE ON ED2, TEMP WAS 21 DEGREE C. OTHER QTY`S ALL IN GREEN (INDICATION CAME ON AFTER 28 SECONDS). DESERVICED NR 3 AND NR 2 HYD SYS TO CORRECT QTY OF 55 PERCENT AND 60 PERCENT FUNCTIONAL TEST OF LANDING GEAR EXTENSION/RETRACTION TEST GOOD IAW AMM 32-33-00. (K)

Part: SKIN — DAMAGED (BS 228-230) · airframe 12,988 hrs · 12,025 cycles

LT FWD FUSELAGE SKIN, QTY (4) HOLES FOR ACCESS PANEL 131AL ARE ELONGATED. REPAIR IAW REO 601R-53-11-162, REV B. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 12,988 hrs · 12,025 cycles

AFT PRESSURE BULKHEAD AT FS 621.00 AT THE LINTEL LOCATION CRACKED. REPAIRED IAW REO 601R-53-61-1230, REV D. (K)

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 11,744 hrs · 10,861 cycles

AFTER TAKEOFF "FLAPS FAIL" MESSAGE. FLAPS FAILED AT 20 DEGREES. COMPLIED WITH QRH. LANDING WEIGHT WITHIN LIMITS (46,400 LBS), BRAKE TEMPERATURES NORMAL. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4. FLAP SYSTEM RESET OK. (S)

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 11,027 hrs · 10,180 cycles

CANNOT OPEN SERVICE DOOR FROM OUTSIDE. CLEANED AND LUBED SERVICE DOOR HANDLE AS REQUIRED IAW AMM 52-40-00. OPS CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,406 hrs · 7,666 cycles

LT FS 621.00 FLOOR SUPPORT ANGLE CRACKED. MAINTENANCE REPAIRED CRACK IAW REO 601R-53-61-117, REV C. (K)

Part: ANGLE — CRACKED (BS 625)

RIGHT OBLIQUE ANGLE AT FS 625 IS CRACKED 1 INCH LONG. (M) MAINTENANCE REMOVED AND INSTALLED NEW SERVICEABLE OBLIQUE ANGLE IAW SRM 51-42-06. (K)

Part: SKIN — CRACKED (PAX DOOR)

PAX DOOR AFT SIDE SKIN CRACKED APPROX .2 INCH LONG. (M) MAINTENANCE CUT OUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER IAW REO 601R-52-11-702, REV A. (K)

Part: ANGLE — CRACKED (PAX DOOR)

PAX DOOR ANGLE CRACKED APPROX .5 INCH LONG. (M) MAINTENANCE CUT OUT DAMAGED SECTION OF ANGLE AND INSTALLED REPAIR ANGLE AND DOUBLERS IAW REO 601R-52-11-513, REV A. (K)

Part: SKIN — CRACKED (PAX DOOR)

PAX DOOR FORWARD SIDE SKIN CRACKED APPROX .4 INCH LONG. (M) MAINTENANCE CUT OUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER IAW REO 601R-52-11-702, REV A. (K)

Part: INTERCOSTAL — CRACKED (BS 484)

RIGHT FS 484 INTERCOSTAL CRACKED APPROX .1 INCH LONG AT RBL 36 FLOOR SUPPORT BEAM. (M) MAINTENANCE CUT AWAY DAMAGED FLANGE AND INSTALLED REPAIR FLANGE IAW REO 601R53-41-059, REV A AND BSC SR 601R-53-0030A. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

LEFT FS 84 INTERCOSTAL CRACKED APPROX .1 INCH LONG AT LBL 36 FLOOR SUPPORT BEAM. (M) MAINTENANCE CUT AWAY DAMAGED FLANGE AND INSTALLED REPAIR FLANGE IAW REO 601R-53-41-059, REV A AND BSC SR 601R-53-0030A. (K)

Part: ANCHOR FITTING — CRACKED (PAX DOOR)

FOUND PASSENGER DOOR AFT ANCHOR FITTING IS CRACKED. [SUP 06-11-07] REMOVED FITTING IAW CRJ AMM 52-11-17-000-804 AND INSTALLED NEW FITTING P/N 601R380741-3 IAW CRJ AMM 52-11-17-400-804. (M)

Part: ANCHOR FITTING — CRACKED (PAX DOOR)

FOUND PASSENGER DOOR FORWRAD ANCHOR FITTING IS CRACKED. [SUP 06-11-07] REMOVED AND REPLACED FORWARD ANCHOR FITTING IAW CRJ AMM 52-11-17-400-804, P/N 601R380742-3. (M)

Part: BRACKET — CRACKED (LT MLG WW)

LEFT MLG BAY HYDRAULIC TRANSDUCER BRACKET IS CRACKED. (M) [07-17-07] MAINTENANCE REMOVED AND REPLACED BRACKET, P/N 601R75262-159, IAW CRJ SRM 51-42-06. (M)

Part: BRACKET — CRACKED (RT MLG WW)

RIGHT MLG BAY HYDRAULIC TRANSDUCER BRACKET CRACKED. (M) MAINTENANCE REMOVED AND REPLACED BRACKET PN 601R75262-157 IAW SRM 51-42-06. (K)

Part: BRACKET — CRACKED (RT MLG WW)

RIGHT MLG BAY Z BRACKET FORWARD OF HYDRAULIC TRANSDUCER IS CRACKED. (M) MAINTENANCE REMOVED AND REPLACED BRACKET PN 601R75262-155 IAW SRM 51-42-06. (K)

Part: RIB — CRACKED (BATTERY BOX)

FOUND RIGHT BATTERY RIB IS CRACKED. (M) MAINTENANCE REPAIRED RT BATTERY RIB IAW EO 601R-57-51-046. (K)

Part: FIRE BOTTLE — DISCHARGED · airframe 7,450 hrs · 6,736 cycles

DURING SERVICE CHECK, FOUND ENGINE FIRE BOTTLES NR 1 AND NR 2 DISCHARGED. REMOVED AND REPLACED FIRE BOTTLES NR 1 AND NR 2 IAW CRJ 26-21-07. OPS CHECK GOOD. (K)

Part: HYDRAULIC LINE — LEAKING (NR 2 SYSTEM)

FOUND ON CREW PREFLIGHT, HYD SYSTEM NR 2 QUANTITY AT ZERO APPEARS TO BE LEAKING FROM AFT EQUIPMENT BAY. ISOLATED NR 2 RESERVOIR SUCTION LINE. REMOVED AND REPLACED RIGHT ENGINE DRIVEN PUMP SUCTION LINE REF AMM 20-22-00, OPS CHECK AND LEAK CHECK GOOD. (M)

Part: PCU — MALFUNCTIONED (SPOILERONS)

SPOILERON FAULT MESSAGE IN FLIGHT. FELT MOMENTARILY DEPLOYMENT OF SPOILERON. REMOVED AND REPLACED LEFT SPOILERON INBOARD PCU IAW AMM CHAPTER 27-62-01. OPS CHECK GOOD. (M)

Part: FILTER — UNKNOWN (HYD SYSTEM)

"HYD 2 LOW" CAS MESSAGE FOLLOWED BY "EDP 2" CAS MESSAGE THEN FLUID SHOWED AERO. FOLLOWED QRH. REMOVED AND REPLACED EDP NR 2 PER AMM 29-11-01, LEAK CHECK AND FUNCTION CHECK GOOD. REMOVED AND REPLACED ALL HYDRAULIC NR 2 FILTERS PER AMM 29-11. LEAK CHECKS GOOD. SERVICE HYDRAULIC NR 2 SYSTEM. CHECKS GOOD AT THIS TIME. (M)

Part: BRACKET — BENT (PROX SENSOR) · airframe 5,224 hrs · 4,647 cycles

GEARS UP DISAGREE CAS, AFTER TAKEOFF. MLG`S INDICATED UP AND LOCKED. NLG REMAINED DOWN. FOUND PROXIMITY SENSOR BRACKET BENT REMOVED AND REPLACED PROXIMITY SENSOR BRACKET IAW MM. REINSTALLED SENSOR TO WITHIN LIMITS IAW MM. PERFORMED GEAR SWING IAW MM. GEAR SWING OPS CHECK GOOD. (K)

Part: COMPUTER — FAILED (ZONE 221) · airframe 5,151 hrs · 4,576 cycles

RT AOA HEAT FAIL MESSAGE AFTER TAKEOFF. REMOVED AND REPLACED ADHC NR 2 (AIR DATA HEAT CONTROLLER) IAW AMM. OPS TEST GOOD. (K)

Part: DUCT — CLOGGED (CABIN FAN)

ELECTRIC SMELL IN CABIN FROM ROW 9 AFT. FOUND CABIN FAN DUCT CLOGGED WITH DUST AND DEBRIS. CLEANED FAN AND DUCT ABOVE ROW 8. OPS CHECK GOOD. ALSO, FOUND BALLAST B130 ABOVE ROW 11 GROUND PIN IN CONNECTOR NOT SEATED CAUSING BALLAST INTERMITTENTLY FLICKERING. RESEATED PER PIN IAW STANDARD PRACTICES, OPS CHECK GOOD. (M)

Part: BUSHING — MIGRATED (LT MLG)

LEFT MLG FORWARD TRUNNION AFT BUSHING MIGRATED ON OUTBOARD EDGE .0015. INSTALLED NEW BUSHINGS, P/N 601R-57-21-003-41, IN FORWARD TRUNNION IAW BOMBARDIER, INC REO 601R-57-21-003-REV B. (M)

Part: SKIN — DENTED (FUSELAGE) · airframe 3,775 hrs · 3,285 cycles

2 DENTS RT SIDE AF FS409 + 32 BETWEEN STR 21R AND 22R. 3.5 INCHES LONG X 1.65 INCHES WIDE X 0.39 INCHES DEEP. 2.5 INCHES LONG X 1.5 INCHES WIDE X .022 INCHES DEEP. REPAIRED DAMAGE AT FS 409 +32 BETWEEN STR 21R AND 22R IAW SRM. (K)

Part: FLAP — MISRIGGED (WINGS)

FLAP FAIL CAS MESSAGE AT ZERO FLAPS ON CLIMB, DECLARED EMERGENCY. RE-RIGGED, FLAPS. (M)