N416AW

Part: CONTROL UNIT — FAULTED (E/E BAY) · airframe 46,132 hrs · 44,251 cycles

FLAPS FAIL CAUT MESSAGE FLAPS FAILED AT 16K FT 250 KNOTS FAILED IN THE ZERO DEGREE POSITION. AIRCRAFT REMOVED FROM SERVICE R&R THE FECU IAW AMM 27-51-05. OPS CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL. PN:860D100-18 SN OFF:582 SN ON:923 RAH

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 46,162 hrs · 44,283 cycles

FLAPS FAIL CAUT MESSAGE FLAPS FAILED AT 16K FT 250 KNOTS FAILED IN THE ZERO DEGREE POSITION. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL ***** AIRCRAFT REMOVED FROM SERVICE ***** R&R THE FECU IAW AMM 27-51-05. OPS CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL.

Part: LANDING GEAR — WARNING MESSAGE · airframe 45,497 hrs · 43,539 cycles

AFTER T/O RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE. RAN QRH PROCEDURE MSG'S WENT AWAY. LANDING WIGHT 44, 600LBS, SMOOTH NORMAL LANDING. MSG APPEARED AFTER 2 SECONDS SELECTING GEAR. AIRCRAFT REMOVED FROM SERVICE PERFORMED GEAR SWING IAW AMM 32-30-00 OPS CHECK GOOD.

Part: SENSOR — UNKNOWN (FS628-FS648) · airframe 45,170 hrs · 43,155 cycles

PERSISTENT ANTI-ICE DUCT WARNING MESSAGE. RH FUSELAGE SHOWED RED ON THE SYNOPTIC PAGE. C/W QRH AND RETURNED TO YUL. *********AIRCRAFT REMOVED FROM SERVICE********* T/S PER MTCM 19-149. REPLACED LOOP A46WK PER AMM 36-21-04. OPS CHECK GOOD.

Part: SENSOR — UNKNOWN (FS628-FS648) · airframe 45,170 hrs · 43,155 cycles

ANTI ICE DUCT WARN MSG ******AIRCRAFT REMOVED FROM SERVICE******** T/S PER MTCM 19-149. REPLACED LOOP A46WK PER AMM 36-21-04. OPS CHECK GOOD.

Part: STRAP — OUT OF POSITION (FS 310) · airframe 44,057 hrs · 41,903 cycles

PREVIOUS REPAIR ON PASSENGER DOOR FRAME 310 .0 DAMAGE FROM INPROPER DOOR CLOSING. AIRCRAFT REMOVED FROM SERVICE. INSTALLED NEW REPAIR STRAP 601R-53-22-033-1 IAW REO 601R-53-22-033 REV -D DATE 2014/02/17 REPAIR TYPE 1 FOR FASTENER CALL OUT

Part: SKIN — NONE (BS 257 S15L) · airframe 44,057 hrs · 41,903 cycles

TEMPORARY REPAIR TO FUSELAGE SKIN AT BS 257.75, S15L. DENT MEASURES 0.55" X 0.4" X 0.004" DEPTH - HAS BEEN COMPLIED WITH IAW EA AWAC-CRJ253-01543. PERFORMED PERMANENT REPAIR AS REQUIRED ****AIRCRAFT REMOVED FROM SERVICE**** COMPLIED WITH REO 601R-53-11-3811 REV. -- DATED 2022-11-23

Part: FLOOR SUPPORT — CORRODED (BS 513-559) · corrosion level 2 · airframe 44,057 hrs · 41,903 cycles

R/H PRESSURE FLOOR SILL HAS CORROSION FROM FS 513 TO FS 559. AIRCRAFT REMOVED FROM SERVICE. REPAIRED PRESSURE FLOOR SILL REF REO 601R-53-41-3104 REV -.

Part: FLOOR SUPPORT — CORRODED (BS 439-529) · corrosion level 2 · airframe 44,057 hrs · 41,903 cycles

L/H PRESSURE FLOOR SILL CORRODED FROM FS 439 TO 529. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CORRODED AREA IAW REO 601R-53-41-3103 REV -.

Part: SKIN — DENTED (BS 605 S21-22L) · airframe 44,057 hrs · 41,903 cycles

FUSELAGE DENTED AT BS 605 S21L-22L. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE SKIN IAW REO 601R-53-61-7913, REV -.

Part: RIB — CRACKED (FLS 50.498) · airframe 44,057 hrs · 41,903 cycles

UPON REMOVAL OF THE INBOARD FLAP SEAL ON THE L/H INBOARD FLAP, A CRACK WAS FOUND ON THE FWD CHERRYMAX HOLE. ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND INSTALLED NEW RIB AT L/H INBOARD FLAP AS PER REO 601R-57-52-2472 REV -- DATED 2022-11-29

Part: SEAT — CORRODED (200 CABIN SEATS) · corrosion level 2 · airframe 44,057 hrs · 41,903 cycles

RIGHT PASSENGER SEATS THE STRUCTURE HAS EVIDENCE OF CORROSION. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE SEAT STRUCTURE IAW 926-DH124A & 926-DH224A SERIES, CMM 25-26-95.

Part: SEAT TRACK — CORRODED (200 CABIN) · corrosion level 2 · airframe 44,057 hrs · 41,903 cycles

9EA LH PASSENGER SEATS THE STRUCTURE HAS EVIDENCE OF CORROSION (MARKED) ****AIRCRAFT REMOVED FROM SERVICE ***** REPLACED PASSENGER SEAT STRUCTURE REF CRJ200 B/E AEROSPACE, 926-DH124A & 926-DH224A SERIES, CMM 25-26-95

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 44,057 hrs · 41,903 cycles

LEFT WING INBD FLAP HAS A DENT INBD BOTTOM SIDE. ACFT REMOVED FROM SERVICE. REPAIRED THE LT INBOARD FLAP LOWER SKIN IAW SRM 57-52-00, REPAIR -3, AND SRM 51-23-00.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 44,057 hrs · 41,903 cycles

RIGHT WING INBOARD FLAP THE FLAP VANE CHAFING ON THE TOP INBOAD TRAILING EDGE. ACFT REMOVED FROM SERVICE. REPAIRED THE RT WING INBOARD FLAP VANE REF REO 601R-57-52-2469 REV-.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 44,057 hrs · 41,903 cycles

LEFT WING INBOARD FLAP THE FLAP VANE IS CHAFFED ON THE TOP INBOARD TRAILING EDGE. ACFT REMOVED FROM SERVICE. REPAIRED THE LT WING INBOARD FLAP VANE IAW REO 601R-57-52-2469 REV-.

Part: STRAP — CORRODED (BS 559 LBL27-47) · corrosion level 2 · airframe 44,057 hrs · 41,903 cycles

LEFT FLOOR STRAP A BS 559 BETWEEN LBL 47 AND LBL 27 HAD CORROSION. ACFT REMOVED FROM SERVICE. REPLACE THE STRAP.

Part: IDG — FAULTED (NR 1 GENERATOR) · airframe 42,889 hrs · 40,790 cycles

IN FLIGHT RECEIVED GEN 1 CAUTION MESSAGE (APU WAS ON MEL), F/O SMELLED BURNED PLASTIC MOMENTARILY C/W QRH GEN 1 MESSAGE PERSISTED. TURNED GEN 1 TO OFF/RESET. MESSAGES RECEIVED: L WINDSHIELD & L WINDOW CAUTION, CW QRH MESSAGES CLEARED. ***AIRCRAFT REMOVED FROM SERVICE*** SERVICED #1 LH IDG AWA SUP 16-364, OPS TEST STILL REQUIRED REF 333203/2.

Part: RESERVOIR — MALFUNCTIONED (HYD SYSTEM) · airframe 41,608 hrs · 39,509 cycles

OPEN WARNING MESSAGE. CW QRH. ON HYD SYNOPTIC PAGE, #3 SYS SHOWED 300PSI, 70% QUANTITY AND BOTH HYD PUMP OFF. SYS 3 HYD SWITCHES SET FOR TAKEOFF. WITH FLAPS SET TO 8D DEGREES. PUMP CB'S WERE IN. AT GATE, QUANTITY SHOWS 70%. NO OBVIOUS SIGNS OF LEAKS NOTED. ***AIRCRAFT REMOVED FROM SERVICE*** R&R #3 HYD RESERVOIR IAW AMM 29-12-30. REF TO 319015/2 FOR REST OF INSTALLATION STEPS REQUIRED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,476 hrs · 39,366 cycles

FS 220 RIGHT SIDE EXTERNAL SKIN CRACKED AFT OF NOSE GEAR CUT OUT RADIUS. AIRCRAFT REMOVED FROM SERVICE. REPAIRED FUSELAGE EXTERNAL SKIN FS 220.00 RIGHT SIDE AFT OF NOSE GEAR CUT OUT, IAW MHI RJ AVIATION REO 601R-53-11-3647.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,476 hrs · 39,366 cycles

T-CAP EXTRUSION ON LBL 27, FS 559+118 TO FS 621 IS CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T-CAP EXTRUSION ON LBL 27, FS 559+118 TO FS 621.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,476 hrs · 39,366 cycles

LBL 9, FLOOR SEAT TRACK FS 364 THRU FS 409 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT LBL 9, FS 364 THRU FS 409.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2

SEAT TRACK CORROSION AT RBL 9, FS 559+64. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT RBL 9, FS 559+64.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,476 hrs · 39,366 cycles

RT SIDEWALL SEAT TRACK FROM FS 559 TO FS 559+64 CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT SIDEWALL SEAT TRACK FROM FS 559 TO FS 559+64.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,476 hrs · 39,366 cycles

RBL 9, FLOOR SEAT TRACK FS 364 THRU FS 409 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR SEAT TRACK AT RBL 9, FS 364 THRU FS 409.

Part: DISPLAY — FAILED (COCKPIT) · airframe 39,394 hrs · 37,342 cycles

ON ARRIVAL, BOTH MFD'S FAILED, ONCE SHUTDOWN AT GATE, MFD #2 CAME BACK. (INFLIGHT AT 10000FT FAILURE OCCURRED).

Part: FLAP — FAILED (WING) · airframe 39,147 hrs · 37,106 cycles

RECEIVED FLAP FAIL CAUTION MESSAGE ON APPROACH WHILE SELECTING FLAPS 45. FLAPS FAILED AT 33 DEGREES.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 39,053 hrs · 37,018 cycles

PAX DOOR AFT DRAG ANGLE CRACKED.

Part: STRINGER — CORRODED (BS 319-349) · corrosion level 2 · airframe 39,053 hrs · 37,018 cycles

STRINGER 26R IS CORRODED BETWEEN F.S.319 AND F.S.349.

Part: STRUCTURE — GOUGED (FLAP HINGE BOX) · airframe 39,053 hrs · 37,018 cycles

R/H INBD FLAP, OUTBD HINGE BOX IS GOUGED ON INBD SIDE OF OUTBD LUG WHERE FLAP ATTACHES TO HINGE BOX.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,053 hrs · 37,018 cycles

FS 319 IS CORRODED AT STR 26R.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,053 hrs · 37,018 cycles

FS 310.00 LOWER FRAME SEGMENT IS CORRODED AT STRINGER 26R.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 39,054 hrs · 37,018 cycles

INDICATIONS NOTED AT FS 621 REAR PRESSURE BULKHEAD FWD FACE AT LBL18 WL131.9 .9" IN LENGTH AND 55% FSH. AT LBL27.5 WL131 2.9" LONG AND 100% FSH. AT LBL 27.5 WL 105 1.25" LONG AND 78% FSH. ALL FAIL NDT.

Part: SKIN — DENTED (TE FLAP) · airframe 39,053 hrs · 37,018 cycles

LEFT WING I/B FLAP LOWER SKIN DENTED WITH CREASE THROUGH DENT WS 70.00 DENT APPROX. .300" X .250" X .025" DEEP.

Part: FORMER — CORRODED (PAX DOOR) · airframe 39,054 hrs · 37,018 cycles

PAX DOOR FWD FORMER IS CORRODED UNDER PANEL 832HL.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 39,053 hrs · 37,018 cycles

LT WINDSHIELD SUPPORT ANGLE IS CRACKED BETWEEN FS 220.00 AND FS 235.00 BETWEEN STGR 11L TO 14L.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,628 hrs · 36,602 cycles

DURING SCHEDULED INSP OF AFT PRESS BULKHEAD FS621. FOUR CRACKS WERE DISCOVERED DURING EDDY CURRENT, 8 DAMAGED RIVETS DURING VISUAL, AND 7 TOOLING MARKS DURING VISUAL.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 37,273 hrs · 35,244 cycles

FO WINDSHIELD CRACKED AT 21,200'. C/W QRH. RETURNED TO CAE, LANDING OVERWEIGHT AT 48,240 LBS. LANDING WAS SMOOTH.

Part: APU — SHUTDOWN · airframe 36,076 hrs · 34,064 cycles

4108 APU AUTO SHUT DOWN ON GROUND WITH ASSOCIATED FUEL SMELL. REPLACED THE APU.

Part: DOUBLER — CRACKED (BS 409) · airframe 35,660 hrs · 33,695 cycles

INTERNAL DOUBLER COMMON TO UPPER BEACON LIGHT INSTALLATION IS CRACKED

Part: PULLEY BRACKET — DAMAGED (BS 280) · airframe 35,660 hrs · 33,695 cycles

TWO INBD BOLT HOLES FOR LANDING GEAR ALTERNATE EXTENTION PULLEY BRACKET ARE ELONGATED AT LBL 12 POST BS 280.00. REPAIRED IAW REO 601R-53-11-300- REV --.

Part: FLOOR SUPPORT — CORRODED (BS 574-601) · corrosion level 2 · airframe 35,660 hrs · 33,695 cycles

FLOOR SUPPORT HAS LIGHT CORROSION SPOTS ON THE TOP AND BOTTOM SIDE BETWEEN BS 574 - 601.00 IN THE CARGO BAY. REPAIRED IAW EA AWAC-CRJ253-00609 REV-IR.

Part: FLOOR SUPPORT — CORRODED (BS 349-365) · corrosion level 2 · airframe 35,660 hrs · 33,695 cycles

MAIN CABIN FLOOR SUPPORT CORRODED LBL43 BS 349-408.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 35,660 hrs · 33,695 cycles

1013785-1000-0065 - FLOORBEAM AT FS 280 IS CORRODED BTW RBL 9 AND LBL 9

Part: ANGLE — CORRODED (BS 319-349) · corrosion level 2 · airframe 35,660 hrs · 33,695 cycles

SERVICE DOOR CUT-OUT SILL HAS AREAS OF CORROSION FROM BS 319 - 349

Part: FITTING — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 35,660 hrs · 33,695 cycles

SERVICE DOOR LOWER SILL FITTING IS CORRODED

Part: ANGLE — CRACKED (BS 202) · airframe 35,660 hrs · 33,695 cycles

WINDSHIELD CENTER POST LOWER ANGLE BS 202.75 IS CRACKED.

Part: BULKHEAD — GOUGED (BS 621) · airframe 35,660 hrs · 33,695 cycles

FORWARD FACE OF THE AFT PRESSURE BULKHEAD HAS SEVEN AREAS THAT ARE GOUGED. REPAIRED THE PRESSURE BULKHEAD IAW GREO 601R-53-61-2155 REV-A AND REO 601R-53-61-5895.

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 35,660 hrs · 33,965 cycles

FRAME BS 605 HAS CORROSION ON THE FWD AND AFT SIDE, BETWEEN STRINGER 20 AND 23L.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 35,660 hrs · 33,695 cycles

LEFT INBOARD FLAP LOWER SKIN HAS MULTIPLE DENTS BELOW INBD LOWER ACCESS PANEL. REPAIRED THE LT WING TE FLAP LOWER SKIN IAW REO 601R-57-52-1544.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 35,660 hrs · 33,695 cycles

BS 484 FLOORBEAM ANGLE AT LBL 27 IS CRACKED. REPLACED.

Part: CARGO TRACK — CORRODED (BS 559-574) · corrosion level 2 · airframe 35,660 hrs · 33,695 cycles

CARGO TRACK ON RBL 9 BETWEEN BS 559+112 AND 574 IS CORRODED. REPAIRED.

Part: FITTING — CRACKED (BS 461) · airframe 35,660 hrs · 33,695 cycles

FLOOR SUPPORT BATHTUB FITTING AT RBL 9, BS 461 IS CRACKED. REPLACED.

Part: CLEAT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 35,660 hrs · 33,695 cycles

IN MAIN CABIN AFT PASSENGER DOOR CLEAT BS 343, LBL 38 IS CORRODED. REPAIRED.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 35,660 hrs · 33,695 cycles

BS 484 INBD FLOORBEAM ANGLE AT LBL 36 IS CRACKED. REPAIRED.

Part: FLT CONTROLS — MALFUNCTIONED · airframe 35,604 hrs · 33,642 cycles

UNCOMMANDED YAW ON DESCENT & APPROACH TO LAND WITH AUTOPILOT ENGAGED & WITH AUTOPILOT OFF.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 35,103 hrs · 33,194 cycles

F/A REPORTS PASSENGER DOOR DIFFICULT TO OPEN AND CLOSE.

Part: STRUT — LOW (NLG) · airframe 34,233 hrs · 32,405 cycles

3815,3882, AFTER TAKEOFF GEAR DISAGREE WARNING MSG & WOW INPUT CAUTION MSG DISPLAYED AFTER SELECTING GEAR LEVER UP. NOSE GEAR STAYED DOWN & INDICATED GREEN. CREW PULLED CBP2-N6 IAW QRH. SUSPECTED NLG NOT EXTENDED FULLY. SERVICED NLG SHOCK STRUT WITH OIL & NITROGEN IAW AMM 12-12-32. JACKED ACFT & SWUNG GEAR MULTIPLE TIMES. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 33,326 hrs · 31,573 cycles

AFTER DEPARTURE, RECEIVED LG DISAGREE, NLG SHOWED RED BARS. COMPLIED WITH QRH, GEAR SHOWED DOWN & LOCKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,827 hrs · 30,122 cycles

FLIGHT NR 4076 REF 261679/2. FLOOR TRACK LIGHTING AT ROW 1 INOPERATIVE. ALL OTHER EMER LIGHTS OPERATES NORMALLY. PLACARDED & PLACED ON MEL.

Part: LIGHT — MISSING (CABIN) · airframe 31,176 hrs · 29,512 cycles

LIGHT COVER FOR EMERGENCY LIGHT ARROW NEAR PAX DOOR MISSING.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,148 hrs · 29,485 cycles

FS 333 IN AVIONICS BAY HAS CORROSION.

Part: RIB — CRACKED (RT WING) · airframe 31,148 hrs · 29,485 cycles

RIGHT BATTERY RIB CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,148 hrs · 29,485 cycles

WINDSHIELD CTR POST LT LOWER CLIP CRACKED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,149 hrs · 29,485 cycles

PAX DOOR AFT DRAG ANGLE CRACKED.

Part: BRACKET — CRACKED (RT WING) · airframe 31,149 hrs · 29,485 cycles

RIGHT WING LE TRANSITION DUCT INBD BRACKET CRACKED.

Part: BRACKET — CRACKED (LT WING) · airframe 31,149 hrs · 29,485 cycles

LEFT WING LE TRANSITION DUCT OTBD BRACKET CRACKED.

Part: CLEAT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 31,148 hrs · 29,485 cycles

PAX DOOR HANDRAIL STOW CLEATS ARE CORRODED.

Part: ANGLE — CRACKED (CARGO DOOR FRAME) · airframe 31,148 hrs · 29,485 cycles

CARGO DOOR LOWER FWD STOP BRACKET LOWER FWD ANGLE CRACKED.

Part: SKIN — CRACKED (RT EXHAUST) · airframe 31,149 hrs · 29,485 cycles

RIGHT EXHAUST FAIRING SKIN CRACKED AT DRAIN FITTING.

Part: ANGLE — CRACKED (CARGO DOOR FRAME) · airframe 31,148 hrs · 29,485 cycles

CARGO DOOR LOWER AFT STOP BRACKET FWD ANGLE CRACKED.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 31,148 hrs · 29,485 cycles

TWO EACH CARGO TIE DOWNS IN CARGO BAY ON LBL 9 AT FS 574 TO 559+80 HAS CORROSION.

Part: BRACKET — CRACKED (VERTICAL STAB) · airframe 31,149 hrs · 29,485 cycles

BRACKETS ON VERTICAL STAB UNDER LT & RT LOWER VISOR PANELS ARE CRACKED.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 31,149 hrs · 29,485 cycles

CARGO DOOR LOWER SILL CRACKED AT FS 589.

Part: DRAG ANGLE — CRACKED (LT WING) · airframe 31,149 hrs · 29,485 cycles

LEFT MLG WW BATTERY RIB DRAG ANGLE CRACKED.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 31,149 hrs · 29,485 cycles

RIGHT MLG WW BATTERY RIB DRAG ANGLE CRACKED.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 31,149 hrs · 29,485 cycles

RIGHT MLG WW BRAKE TRANSDUCER BRACKET CRACKED.

Part: VANE — CHAFED (TE FLAP) · airframe 31,149 hrs · 29,485 cycles

LEFT INBD FLAP VANE LE CHAFED, MID-SECTION OUT OF LIMITS.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 28,281 hrs · 26,735 cycles

TO SHORTLY AFTER FLAP RETRACTION, "STAB AND MACH TRIM CAUTION" MSGS APPEARED AND WOULD NOT CLEAR. DIVERTED, LDG WT 38000. INTERROGATED MDC HSTCU 270, BIT 14 SET FOR DISCONNECT SWITCH. CW FIM FAULT RESET PROCEEDURE-NO FIX. RERACKED HSTCU REF AMM 27-41-01. CW FUNCTION CHECK OF HSTCU IAW 27-41-01 AND OPS CHECK OF HSTCU IAW 27-40-00.

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 26,389 hrs · 24,850 cycles

CARGO DOOR HANDLE HAS CRACK AND SIDE OF HANDLE CUTOUT. REMOVED AND REPLACED CARGO DOOR HANDLE IAW CRJ 200 SRM 51-42-21.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,389 hrs · 24,850 cycles

CAP ANGLE LBL 27 FROM 559+80 TO 559+109 HAS FLAKING CORROSION NUT FASTENERS EXTENDING FROM TOP TO BOTTOM SURFACES. REMOVED CAP ANGLE LBL 27 FROM FS 559.85 TO FS 559.00 O/B SIDE THEN INSTALLED NEW SECTION OF CAP ANGLE IAW CRJ SRM 53-00-43 B/A REO 601R-53-00-506.

Part: SKIN — CHAFED (TE FLAP) · airframe 26,389 hrs · 24,850 cycles

LEFT INBOARD FLAP INBOARD SIDE SKIN RIB HAS CHAFING DAMAGE. BLENDED CHAFE DAMAGE TO LEFT INBOARD FLAP INBOARD RIB IAW REO 601R-57-52-2007.

Part: FITTING — CHAFED (TE FLAP) · airframe 26,389 hrs · 24,850 cycles

LEFT OUTBOARD FLAP GUIDE ROLLER FITTING IS CHAFED. BLENDED CHAFED AREA ON LEFT O/B FLAP GUIDE ROLLER FITTING IAW REO 601R-57-53-963.

Part: SILL — CORRODED (FUSELAGE) · airframe 26,389 hrs · 24,850 cycles

PAX DOOR LOWER SILL HAS CORROSION ON INTERIOR AND EXTERIOR. REMOVED PAX DOOR LOWER SILL AND INSTALLED NEW SERVICEABLE LOWER SILL IAW CRJ SRM 51-42-06, 51-42-21, 51-40-11, 51-21-11.

Part: SKIN — CHAFED (RT COWLING) · airframe 26,389 hrs · 24,850 cycles

RIGHT ENGINE LOWER CORE COWL FWD INT SKIN HAS SEVERAL DENTS & CHAFING. PERFORMED DENT REPAIR & BLEND CHAFED AREA IAW REO 601R-71-12-4149 & CRJ 200 CMM 71-12-01 REPAIR SRS046 & CRJ 200 CMM 20-12-00.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 26,389 hrs · 24,850 cycles

PAX DOOR PRESSURE DOOR AFT ATTACH ANGLE P/N 601R318072-1 IS CRACKED. REPLACED UNSERVICEABLE ATTACH ANGLE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,389 hrs · 24,850 cycles

EXFOILATING CORROSION FOUND AROUND FASTENERS ON SEAT TRACK AT FS 409.00 LBL 9. REMOVE & REPLACE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 364) · corrosion level 2 · airframe 26,389 hrs · 24,850 cycles

CORROSION FOUND AROUND FASTENERS OF SEAT TRACK AT FS 364 RBL 9. REMOVE & REPLACE SEAT TRACK.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 26,389 hrs · 24,850 cycles

PAX DOOR STAIR AFT SUPPORT WEB CRACKED AT CORNER BETWEEN CENTER STEP AND STEP 832CT. REPAIRED IAW REO 601R-52-11-702 REV C.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 26,389 hrs · 24,850 cycles

CORROSION FOUND ON CARGO TIE DOWN (SEAT TRACK) ON RBL 27 FROM 559+77 TO 559+96. REMOVE & REPLACE SEAT TRACK IAW CRJ 200 SRM 51-40-11 & CRJ 200 AMM 53-01-11-000-802 & CRJ 200 AMM 53-01-11-400-802.

Part: RIVET — SHEARED (PAX DOOR) · airframe 26,389 hrs · 24,850 cycles

PAX DOOR ASSIST MOTOR LOWER ATTACH ANGLE HAS 2 EA SHEARED RIVETS ON EACH END WITH A CRACK IN SKIN UNDER ANGLE. REPLACED 2EA DAMAGED RIVETS WITH SERVICEABLE RIVETS REPAIRED CRACK IAW REO 601R-52-11-702 REV C.

Part: VANE — CRACKED (TE FLAP) · airframe 26,389 hrs · 24,850 cycles

RIGHT I/B FLAP VANE CRACKED IN 3 AREAS ON LEADING EDGE. REMOVED UNSERVICEABLE I/B AND CTR LEADING EDGE AND INSTALLED SERVICEABLE I/B AND CTR LEADING EDGE IAW CRJ 200 SRM 51-40-11/51-42-13. BLENDED CHAFE DAMAGE ON O/B LEADING EDGE AND RESTORED FINISH IAW REO 601R-57-52-001 REV C.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,389 hrs · 24,850 cycles

FS 280 FLOOR SUPPORT STRUCTURE HAS THE FOLLOWING DISCREPANCIES, FWD CAP ANGLE, AFT CAP ANGLE CRACKED, RBL 9 I/B & O/B CLIPS CRACKED. REPAIRED FWD ANGLE, AFT ANGLE, RBL 9 O/B CLIP, LBL 9 I/B & O/B CLIPS IAW REO 601R-53-11-136 REV A.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,389 hrs · 24,850 cycles

CARGO TIE DOWN TRACK ON LBL 9, 3" FWD OF THE 621 BULKHEAD HAS FLANKING CORROSION 109-3. REMOVED UNSERVICEABLE CARGO TRACK P/N 601R31032-51 AND INSTALLED A NEW SERVICEABLE CARGO TRACK ON LBL 9, 3" FWD OF THE 621 BULKHEAD IAW CRJ 200 SRM 51-41-02.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 26,389 hrs · 24,850 cycles

AFT RIGHT SIDE OF FS 280 BULKHEAD AND VERTICAL POST AT RBL 9 CHAFED. REPAIRED AFT RIGHT SIDE OF 280 BULKHEAD AND VERTICAL POST AT RBL 9 IAW REO 601R-53-11-1727.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,389 hrs · 24,850 cycles

PAX DOOR AFT DRAG ANGLE PREVIOUS REPAIR IS CRACKED IN THE RADIUS. REMOVED AND REPLACED SERVICEABLE DRAG ANGLE REPAIR IAW REO 601R-52-11-513.

Part: MOUNT BRACKET — CRACKED (HORIZ STAB) · airframe 26,389 hrs · 24,850 cycles

HORIZONTAL STAB MCU RIGHT AND LEFT LOWER MOUNT BRACKETS CRACKED. REMOVED AND REPLACED BRACKETS.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,389 hrs · 24,850 cycles

RIGHT & LEFT VOLUME METRIC FUSE SOLENOID BRACKETS CRACKED. REMOVED UNSERVICEABLE AND REPLACED WITH SERVICEABLE BRACKET P/N 601R75262-157 AND 601R7526-159 IAW CRJ 200 SRM 51-42-06.

Part: ANGLE — CRACKED (RT WING) · airframe 26,389 hrs · 24,850 cycles

INBOARD AT ANGLE FOR RIGHT WING CENTER L/E CRACKED. REMOVED AND REPLACED LEADING EDGE.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 26,389 hrs · 24,850 cycles

CORROSION AROUND 9 NUT PLATES IN LOWER CARGO DOOR SURROUND STRUCTURE. REPAIRED AREA IAW BOMBARDIER REO 601R-53-61-1574 REV A.

Part: PANEL — GOUGED (LT WING) · airframe 26,389 hrs · 24,850 cycles

LEFT BUTE DOOR PANEL 594PB IS GOUGED. REMOVED UNSERVICEABLE PANEL AND INSTALLED SERVICEABLE PANEL IAW CRJ 200 SRM 51-42-06, 51-40-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,389 hrs · 24,850 cycles

RIGHT FS 484 RBL 36 CLIP CRACKED. REMOVED & REPLACED PREVIOUS REPAIR CLIP AT FS 484, RBL 36 IAW REO 601R-53-41-059 REV B.

Part: RIB — CRACKED (WING) · airframe 26,389 hrs · 24,850 cycles

MLG WHEEL WELL BATT RIB CRACKED. REPAIRED MLG BATT RIB IAW REO 601R-57-51-046 REV B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,389 hrs · 24,850 cycles

LEFT FS 484 LBL 27 CLIP CRACKED. REMOVED & REPLACED CLIP AT FS 484 LBL 27.0 IAW CRJ 200 SRM 51-42-21.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 26,389 hrs · 24,850 cycles

DURING COLD WORKING PROCESS FOUND 2 EA OVERSIZED HOLES 1 EA ON LEFT & 1 EA ON RIGHT ON LOWER MLG TRUNNION FLANGE. REPAIRED DISCREPANCT HOLES IAW BOMBARDIER REO 601R-57-21-1847.

Part: RIB — CRACKED (RT WING) · airframe 26,389 hrs · 24,850 cycles

R NLG WHEEL WELL RIB CRACKED. REPAIRED R MLG WHEEL WELL RIB IAW REO 601R-57-51-046 REV B.

Part: SKIN — DENTED (FUSELAGE) · airframe 26,389 hrs · 24,850 cycles

REPAIR RIGHT FUSELAGE SKIN DENTS 601R-53-61-4672. REPAIRED RIGHT FUSELAGE SKIN BETWEEN FS 642 & FS 660 BETWEEN STR 21R & STR 22R IAW REO 601R-53-61-4742.

Part: RELAY — FAILED (ELECTRICAL SYS) · airframe 25,784 hrs · 24,260 cycles

ON TAKEOFF ROLL, RECEIVED "AC ESS BUS" CAUTION & "EMER LIGHTS ON" STATUS MESSAGE. RAN QRH, MESSAGE REMAINED. RETURNED TO DCA. NOTED NO ACCESS, BUS SYSTEMS APPEARED AFFECTED. INSTALLED NEW A/C ESSENTIAL BUS RELAY (K1XD) AND COMPLIED WITH OPS CHECKS. NO DISCREPANCIES AT THIS TIME, PER CRJ 200 AMM 24.51.27.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 23,899 hrs · 22,363 cycles

NOSE GEAR WOULD NOT RETRACT. RETURN TO DEPARTURE, LANDED AT 46000 LBS. RECEIVED NOG INDICATION AND AURAL WARNING APPROX 6 SECONDS AFTER SELECTED UP. ALSO, HAD NOSE DOOR MESSAGE. ALTERNATE EXTENSION. R & R NLG SELECTOR VALVE IAW AMM 32-33-10. OPS CHECKS GOOD. C/W

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 18,476 hrs · 17,733 cycles

LT MLG DOOR CHAFED ON FWD AND AFT EDGES, REO 601R-52-82-034 AND REO 601R-52-82-318.

Part: SKIN — DENTED (LT SPOILER) · airframe 21,510 hrs · 19,870 cycles

LT INBD GROUND SPOILER HAS DENT ON UPPER SKIN. REPAIRED LT INBD GROUND SPOILER IAW REO 601R-57-71-255.

Part: SKIN — DAMAGED (LT WING) · airframe 21,510 hrs · 19,870 cycles

LT WING CTR L/E HAS 1 EA UNSERVICEABLE COUNTERSINK ON LWR SIDE BETWEEN WS 203.23 & WS 212.81. REPAIRED IAW REO 601R-57-41-740.

Part: SKIN — CHAFED (LT AILERON) · airframe 21,510 hrs · 19,870 cycles

LT AILERON UPPER L/E SKIN IS CHAFED ON INBD AND OTBD SIDES OF CTR. REMOVED LT AILERON UPPER L/E SKIN AND REPLACED LT UPPER SKIN IAW REO 601R-57-60-013 SRM 51-42-06, 51-42-13.

Part: ANGLE — CRACKED (PAX DOOR ASSIST) · airframe 21,510 hrs · 19,870 cycles

PAX DOOR ASSIST MOTOR UPPER MOUNT ANGLE IS CRACKED ON OTBD GROUND. REMOVED CRACKED UPPER MOUNT FOR POWER ASSIST MOTOR AND INSTALLED NEW SERVICEABLE MOUNT PN 601R317745-7.

Part: ANGLE — CRACKED (LT WING) · airframe 21,510 hrs · 19,870 cycles

LT WING CENTER L/E LWR EDGING ANGLE IS CRACKED. REMOVED UNSERVICEABLE L/E LWR EDGING ANGLE AND INSTALLED SERVICEABLE L/E LWR EDGING ANGLE.

Part: PANEL — CRACKED (PAX DOOR) · airframe 21,510 hrs · 19,870 cycles

FWD PAX DOOR SIDE PANEL CRACKED AT 2ND STEP RISER. CUT OUT DAMAGE, THEN FABRICATED NEW PARTS IAW REO 601R-52-11-702, REV A.

Part: BULKHEAD — CRACKED (BS 202) · airframe 21,510 hrs · 19,870 cycles

PARKING BRAKE CABLE AS IT PASSES THROUGH THE FS202 IS CRACKED AT CUTOUT. REPAIRED FS202 BULKHEAD AT PARKING BRAKE CABLE CUTOUT IAW REO 601R-53-11-563.

Part: PANEL — CRACKED (PAX DOOR) · airframe 21,510 hrs · 19,870 cycles

AFT PAX DOOR SIDE PANEL CRACKED 2ND RISER. CUT OUT DAMAGE AND FABRICATED NEW PARTS IAW B/A 601R-52-11-702, REV A.

Part: ATTACH FITTING — CRACKED (PAX DOOR) · airframe 21,510 hrs · 19,870 cycles

UPPER AFT CORNER OF PAX DOOR HAS CRACK ON INTERNAL CLIP HOLDING SKIN TO FRAME. REMOVED CRACKED INTERNAL CLIP, OR DOUBLER AND INSTALLED NEW SERVICEABLE PAR PN 601R318094-2.

Part: LUG — CRACKED (THRUST REVERSER) · airframe 21,510 hrs · 19,870 cycles

RT THRUST REVERSER BLOCKER DOORS 1 THRU 9 HAVE WORN ATTACH HARDWARE UPON REMOVAL OF HARDWARE ON BLOCKER DOOR NR 9 FWD INBD LUG TO BE DAMAGED. R & R BLOCKER DOOR HINGE SUPPORT FITTING P/N 228-50758-809 IAW CMM 78-30-00, REPAIR NR SRS097.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 21,510 hrs · 19,870 cycles

LT SIDE INBD 484 CLIP CRACKED IN 2 PLACES IAW REO 601R-53-41-051.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 21,510 hrs · 19,870 cycles

LT INBD FLAP HAS CHAFING ON L/E OF MOVEABLE VANE (3 PLACES). REPAIRED IAW REO 601R-57-52-004.

Part: PANEL — CHAFED (LT WING) · airframe 21,510 hrs · 19,870 cycles

BUTTE DOOR PANEL NR 594PB IS CHAFED. REPAIRED BUTTE DOOR PANEL NR 594PB UAW REO 601R-57-51-491.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 21,510 hrs · 19,870 cycles

RT INBD HAS CHAFING ON L/E OF MOVEABLE VANE (3 PLACES). REPAIRED IAW REO 601R-57-52-004.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 21,510 hrs · 19,870 cycles

DAMAGED RIVET AND SKIN ON UPPER INSIDE OF PAX DOOR (MARKED). REPAIRED UPPER INSIDE SKIN OF PAX DOOR. R & R RIVET IAW REO 601R-52-11-1896.

Part: FITTING — CHAFED (RT WING TE FLAP) · airframe 21,510 hrs · 19,870 cycles

RT OTBD FLAP ROLLER FITTING CHAFED. REPAIRED IAW REO 601R-57-53-840.

Part: SKIN — DENTED (RT AILERON) · airframe 21,510 hrs · 19,870 cycles

RT AILERON LOWER SKIN IS DENTED. REPAIRED RT AILERON LOWER SKIN IAW REO 601R-57-61-318.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 21,510 hrs · 19,870 cycles

CARGO BAY SEAT TRACK (QTY 1) AT FS 559+96 AT RBL 9. R & R SEAT TRACK IAW SRM 51-42-02 & 51-40-11.

Part: RETAINER — CRACKED (PAX DOOR) · airframe 21,510 hrs · 19,870 cycles

FWD LWR CORNER OF PAX DOOR SEAL RETAINER CRACKED. R & R WITH NEW PART, PN 601R31872-2.

Part: ANGLE — CRACKED (BS 625) · airframe 21,510 hrs · 19,870 cycles

LT AND RT OBLIQUE ANGLES IN AERA ARE CRACKED FS 625.0. R & R LT AND RT OBLIQUE ANGLES AT FS 625.0 IAW REO 601R-53-61-985 REV NC, SRM 51-42-21, TOP COATED HARDWARE AND LT AND RT OBLIQUE ANGLES IAW SRM 51-25-16.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 21,510 hrs · 19,870 cycles

LT MLG DOOR L/E IS CHAFED AT 2 LOCATION. BLENDED OUT CHAFED AREAS IAW REO 601R-52-82-033 AND SRM 51-12-00.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 21,510 hrs · 19,870 cycles

CARGO BAY SEAT TRACK AT FS 559 + 112 CORRODED. R & R SEAT TRACK IAW SRM 51-42-02 AND 51-40-11.

Part: SKIN — CHAFED (MLG DOOR) · airframe 21,510 hrs · 19,870 cycles

RT MLG DOOR L/E AND T/E HAS 3EA CHAFED AREAS. REPAIRED REO 601R-52-82-016 AND SRM 52-82-00.

Part: SKIN — CHAFED (RT AILERON) · airframe 21,510 hrs · 19,870 cycles

RT AILERON UPPER L/E IS CHAFED. DEPTH OF DAMAGE IS AT ITS DEEPEST. BLENDED CHAFED DAMAGE FROM RT AILERON UPPER L/E FOUND TO BE WITHIN LIMITS, DAMAGE AT ITS DEEPEST POINT .009 ORIG THICKNESS 0.90 MATERIAL REMAINDER 0.81, IAW REO 601R-57-60-013 AND SRM 51-12-00.

Part: ANGLE — CRACKED (BS 559) · airframe 20,361 hrs · 18,668 cycles

559.0 BULKHEAD CAP ANGLE AT RBL 9.0 IS CRACKED AND INBD VERT STIFFENER AT RBL 9 IS CRACKED, REO 601R-53-41260 AND 601R-53-41-116.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 19,630 hrs · 17,905 cycles

GEAR DISSAGREE WARNING ON APPROACH, ALONG WITH NOSE DOOR OPEN WARNING. C/W QRH MANUAL EXTENSION RECEIVED ALL GREEN, LANDED WITHOUT INCIDENT. R & R NLG DOOR SELECTOR VALVE IAW AMM 32-22-20. OPS AND LEAK CHECKS GOOD.

Part: HANDLE — OUT OF ADJUST (COCKPIT) · airframe 17,465 hrs · 15,765 cycles

DURING FUNCTIONAL TEST OF CREW ESCAPE, EXTERIOR HANDLE OPERATION FORCE WAS BEYOND LIMITS. CREW EXCAPE HATCH EXTERIOR HANDLE REPLACED IAW AMM 52-22-03. OPS TEST OF THE CREW ESCAPE HATCH TRANSFEREED TO MX WORK CARD 134442-248. (K)

Part: HINGE FITTING — GOUGED (RUDDER) · airframe 17,355 hrs · 15,655 cycles

VERTICAL STAB, MID UPPER AND MID LOWER RUDDER HINGE FITTINGS ARE GOUGED. MID UPPER AND LOWER FITTINGS ON THE VERTICAL STAB REAR SPAR REPAIRED IAW REO 601R-55-31-149. (K)

Part: CROSSBEAM — CRACKED (BS 280) · airframe 17,355 hrs · 15,655 cycles

RT PILOT BULKHEAD CROSSBEAM INBD CLIP FOUND CRACKED .500 INCH. RT PILOT BULKHEAD CROSSBEAM FS 280.00, RBL 9.0, INBD CLIP REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,355 hrs · 15,655 cycles

LT SIDE PILOTS BULKHEAD CROSSBEAM FS 280.00, LBL 9.0 FOUND CRACKED .500 INCH LT SIDE PILOTS BULKHEAD CROSSBEAM FS 280.00, LBL 9.0 REPAIRED IAW REO 601R-53-11-171, REV D, SCHEME A. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,355 hrs · 15,655 cycles

RT PILOT BULKHEAD CROSSBEAM INBD CLIP FOUND CRACKED .500 INCH . RT PILOT BULKHEAD CROSSBEAM INBD CLIP REPAIRED IAW REO 601R-53-11-171, REV D. SCHEME B. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 117,355 hrs · 15,655 cycles

MWC 134442-139, "L" BRACKET ON INTERCOSTAL AT FS 484.00 RBL 36.00 IS CRACKED. "L" BRACKET ON INTERCOSTAL AT FS 484.00, RBL 36.00. REPAIRED IAW REO 601R-53-41-059, REV A. (K)

Part: BRACKET — CRACKED (BS 484) · airframe 17,355 hrs · 15,655 cycles

MWC 134442-138-"L" BRACKET ON INTERCOSTAL AT FS 484.00, RBL 27.00 CRACKED. L-BRACKET ON INTERCOSTAL FS 484.00, RBL 27.00 REPAIRED IAW SRM 51-42-21. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 17,355 hrs · 15,655 cycles

INTERCOSTAL AT FS 484.00, LBL 36.00 FOUND CRACKED. INTERCOSTAL AT FS 484.00, LBL 36.00. REPAIRED IAW REO 601R-53-41-059. (K)

Part: BRACKET — CRACKED (BS 484) · airframe 17,355 hrs · 15,655 cycles

"L" BRACKET ON INTERCOSTAL AT FS 484.00, RBL 27.00 CRACKED. "L" BRACKET AT INTERCOSTAL FS 484.00, RBL 27.00 FABRICATED AND INSTALLED IAW SRM 51-42-21. (K)

Part: ATTACH BRACKET — CRACKED (BS 484) · airframe 17,355 hrs · 15,655 cycles

"L" BRACKET ON INTERCOSTAL AT FS 484.00, RBL 36.00 IS CRACKED. L-BRACKET ON INTERCOSTAL AT FS 484.00, RBL 36.00 REPAIRED IAW REO 601R-53-41-059, REV A. (K)

Part: CROSSBEAM — CRACKED (BS 280) · airframe 17,355 hrs · 15,655 cycles

RT SIDE PILOTS BULKHEAD CROSSBEAM FS 280.00, RBL 9.0 IS CRACKED. RT SIDE PILOTS BULKHEAD CROSSBEAM FS 280.00, RBL 9 REPAIRED IAW REO 601R-53-11-171, REV D. (K)

Part: SUPPORT BRACKET — CRACKED (BS 193) · airframe 17,355 hrs · 15,655 cycles

EXTERNAL AC ELECTRICAL PLUG SURROUNDING SKIN CRACKED (CRACK LENGTH IS .800) A/C SUPPORT BRACKET REPLACED IAW SRM 51-42-06 AND SRM 51-42-21. (K)

Part: POWER SUPPLY — DEFECTIVE (LAVATORY) · airframe 17,264 hrs · 15,566 cycles

VANITY LIGHT IN LAVATORY OUT OF SERVICE WITH BURNING SMELL. REMOVED AND REPLACED LAVATORY VANITY PWR SUPPLY UNIT. OPS CK GOOD IAW AMM 33-25-07.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,827 hrs · 15,154 cycles

MWC 15 FS 621 PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING IS CRACKED. PERFORMED A REPAIR BY CUTTING OUT SECTION OF WEB, FABRICATING AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 601R-53-61-1230 REV D.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 12,377 hrs · 10,895 cycles

LT LOWER WING PLANK FUEL ACCESS PANEL CUTOUT FOR FUEL PNL 540 CB HAS CORROSION IN NON-CRITICAL AREA APPROX 6.0 INCHES DEEP AND .020 WIDE. (K) [SUP 05-17-07] MAINTENANCE REPAIRED CORROSION BY BLENDING OUT CORROSION. PERFORMED NDT, ROTO PEENED AREA, SANDED REWORKED AREAS TO A SURFACE FINISH OF 63 MICRO INCHES. APPLIED CONVERSION COATING AND FUEL TANK COATING IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)

Part: SUPPORT — CRACKED (BS 718) · airframe 12,377 hrs · 10,895 cycles

INTERCOSTAL SUPPORT FOR THE NR 2 HYDRAULIC PRESSURE/RETURN FILTERS IS CRACKED APPROX .2 INCH AT THE LOWER AFT CORNER. (K) [SUP 05-09-07] MAINTENANCE REPAIRED SUPPORT IAW BSC EO 601R-53-11285 BY CUTTING OUT DAMAGE, LPI TO ENSURE CRACK REMOVED, PRIME AND PAINT. (M)

Part: SUPPORT — CRACKED (FUSLEAGE) · airframe 12,377 hrs · 10,895 cycles

INTERCOSTAL SUPPORT FOR THE NR 1 HYDRAULIC PRESSURE/RETURN FILTERS AS CRACKED APPROX .2 INCH AT THE LOWER AFT CORNER. (K) [SUP 05-09-07] MAINTENANCE REPAIRED SUPPORT IAW BSC EO 601R-53-11285 BY CUTTING OUT CRACK, LPI TO ENSURE CRACK REMOVED, PRIME AND PAINT. (M)

Part: FRAME — CRACKED (FS 617)

FOUND FRAME CLIP AT FS 617 AT LBL 9 IS CRACKED .25 INCH CRACK IN RADIUS. MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

CARGO DOOR SUPPORT BEAM LOWER ANGLE THAT ATTACHES TO REAR PRESSURE BULKHEAD IS CRACKED .4 INCH IN LENGTH. MAINTENANCE REMOVED AND REPLACED CARGO DOOR SUPPORT BEAM LOWER ANGLE IAW CRJ 200 SRM 51-42-21. (M)

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 12,337 hrs · 10,895 cycles

FS 409.0 + 128.0 VERTICAL BEAM AT RBL 27.0 IS CRACKED .4 INCH. (K) [SUP 05-09-07] MAINTENANCE TRIMMED OUT DAMAGED AREA, PERFORMED EDDY CURRENT, FABRICATED REPAIR ANGLE AND INSTALLED IAW BOMBARDIER REO 601R-53-41-056 REV E AND BSC EO 601R-53-11286. (M)

Part: CHANNEL — CRACKED (CARGO DOOR) · airframe 12,377 hrs · 10,895 cycles

CARGO DOOR FWD TRUCK BOTTOM U-CHANNEL CRACKED APPROX .1 INCH LONG. (K) [SUP 05-09-07] MAINTENANCE REMOVED AND REPLACED CARGO DOOR FORWARD U-CHANNEL IAW CRJ 200 SRM 51-42-06. (M)

Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 12,377 hrs · 10,895 cycles

HYDRAULIC LINE SUPPORT BRACKET (ASSY PN 601R75262-153) CRACKED APPROX .1 INCH LONG IN CEILING RT WHEEL WELL FWD OF TRANSDUCER BRACKET. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-153 IAW CRJ 200 SRM 51-40-06. (M)

Part: CHANNEL — CRACKED (RT MLG WW) · airframe 12,377 hrs · 10,895 cycles

HYDRAULIC TRANSDUCER HOT CHANNEL (ASSY PN 601R75262-157) CRACKED APPROX 1 INCH LONG IN CEILING RT WHEEL WELL. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-157 IAW BSC STANDARD REPAIR 601R-53-0044E. (M)

Part: CHANNEL — CRACKED (LT MLG WW) · airframe 12,377 hrs · 10,895 cycles

HYDRAULIC TRANSDUCER HOT CHANNEL (ASSY PN 601R75262-159) CRACKED APPROX .1 INCH LONG IN CEILING LT WHEEL WELL. (K) [SUP 05-09-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-159 IAW BSC STANDARD REPAIR 601R-53-0044E. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 123,377 hrs · 10,895 cycles

LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. (K) [SUP 05-09-07] MAINTENANCE REMOVED AND REPLACED LEFT FS 625 INTERCOSTAL AT STRINGER 14L IAW CRJ200 SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,377 hrs · 10,895 cycles

RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX .8 INCHES LONG. (K) [SUP 05-09-07] MAINTENANCE REMOVED AND REPLACED RIGHT FS 625 INTERCOSTAL AT STRINGER 14R IAW CRJ 200 SRM 51-42-06. (M)

Part: BRAKE ASSY — DAMAGED (NR 3 POSITION)

NR 3 BRAKE LOCKED UP AFTER EXITING RUNWAY BTMS INDICATES 13. INSPECTED AND FOUND HYDRAULIC BRAKE COUPLING NR 3 LOOSE AND THREADS DAMAGED. C/W INSP OF MLG, TIRE, BRAKES, AND AXLE IAW AMM. REMOVED AND REPLACED NR3 HYD BRAKE COUPLING AND NR 3 BRAKE ASSY. (K)

Part: SKIN — DAMAGED (FS)

LEFT SIDE AFT FUSELAGE SKIN DAMAGED BETWEEN FS 574-621, STRINGERS 17L-19L. MEASURES 2 INCH LONG BY 1 INCH WIDE BY .096 INCH DEEP. INSTALLED EXTERNAL DOUBLER AND TRIPLER TO DAMAGED FUSELAGE SKIN IAW BOMBARDIER, INCH REO 601R-53-61-1039. (M)

Part: CLIP — CRACKED (FLOOR SUPPORT) · airframe 7,617 hrs · 6,425 cycles

FLOOR SUPPORT BEAM CLIP AS FS280, LBL 9.0, OB IS CRACKED IN RADIUS APPROX 0.30. REMOVED AND REPLACED ANGLE P/N 601R31113-57 IAW CRJ 200 SRM 51-42-06, 51-42-21 AND BRAS EO 601R-53-6212. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FLOOR SUPPORT ANGLE AT FS 621 LHS IS CRACKED AT LBL 41.5 APPROX 1 INCH. REPAIRED BY REMOVING DAMAGE, FABRICATING STRAP, INSTALLING STRAP AND ANGLES P/N 601R-53-61-117-1 AND 601R-53-61-117-3 IAW BOMBARDIER, INC REO 601R-53-61-117 REV C. (M)

Part: CLIP — CRACKED (FLOOR SUPPORT) · airframe 7,617 hrs · 6,425 cycles

FLOOR SUPPORT BEAM CLIP AT FS 280, RBL 9 OB IS CRACKED IN RADIUS APPROX 0.52 INCH. (K)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FLOOR SUPPORT ANGLE AT FS 621 RT IS CRACKED AT RBL 41 APPROX 70 INCHES. REPAIRED BY REMOVING DAMAGE, FABRICATING STRAP, INSTALLING STRAP AND ANGLES P/N 601R-53-61-117-2 AND 601R-53-61-117-4 IAW BOMBARDIER, INC REO 601R-53-61-117 REV C. (M)

Part: CLIP — CRACKED (FLOOR SUPPORT) · airframe 7,617 hrs · 6,425 cycles

FLOOR SUPPORT BEAM CLIP AT FS484, LBL 36, IS CRACKED FROM TOP RIVET HOLE TO EDGE APPROX. (0.30 INCH). (K)

Part: CLIP — CRACKED (FLOOR SUPPORT)

FLOOR SUPPORT BEAM CLIP AT FS 280, RBL 9 IB IS CRACKED IN RADIUS APPROX ( 0.50 INCH). (K)

Part: CLIP — CRACKED (FLOOR SUPPORT) · airframe 7,617 hrs · 6,425 cycles

FLOOR SUPPORT BEAM CLIP AT FS 280, LBL 9, IB IS CRACKED IN RADIUS APPROX (0.33 INCH). (K)

Part: CLIP — CRACKED (FLOORBEAM)

FLOORBEAM CLIP AT FS 280, LBL 9, INBOARD IS CRACKED IN RADIUS APPROX 33 INCHES. REMOVED AND REPLACED ANGLE P/N 601R31113-57 IAW SRJ SRM 51-42-06, 51-42-21 AND BRAS EO 601R-53-6212. (M)

Part: DRAG ANGLE — CRACKED (PAX DOOR)

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED 1 INCH LONG AT THE MOTOR CABLE PULLEY BRACKET. PERFORMED REPAIR TO PASSENGER DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513 REV A. (M)

Part: ANGLE — CRACKED (FUSELAGE)

RIGHT FS 625.0 OBLIQUE ANGLE CRACKED .5 INCH LONG. S/D - INSTALLED NEW ANGLE AT FS 625 RT P/N 601-35012-52. (M)

Part: ANGLE — CRACKED (FUSELAGE)

LEFT FS 625 OBLIQUE ANGLE CRACKED .5 INCH LONG. S/D - INSTALL NEW ANGLE P/N 601-35012-51 AT LEFT FS 625 IAW CRJ 200 SRM 51-42-06. (M)

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 6,708 hrs · 5,642 cycles

IN-FLIGHT RECEIVED SPOILERON CASS MESSAGE. REMOVED AND REPLACED NR 1 SECU, OPS CHECK GOOD IAW 27-61-00.

Part: BRACKET — DAMAGED (NLG SENSOR) · airframe 6,527 hrs · 5,491 cycles

NOSE GEAR DOOR/ DISAGREE ON WITH GEAR HANDLE UP. NOSE GEAR DOWN, MAINS UP. REPLACED NOSE GEAR BRACKET WITH NOSE GEAR EXT AND PROXIMITY SENSOR IAW CMM 32-61-05 PERFORMED NOSE GEAR SWING. OPS CHECK GOOD.

Part: WARNING LIGHT — FALSE INDICATION (AOA HEAT)

IN FLIGHT RIGHT AOA HEAT CAUTION, COMPLIED WITH QRH. COMPLIED WITH OPS CHECK OF RIGHT AOA HEAT CONFIRMED THAT VANE IS HEATING AND CHECKED WIRING TO HEAT CONTROLLER. COULD NOT DUPLICATE IAW AMM 30-30-00. (M)

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB)

STAB TRIM YELLOW CAUTION MESSAGE WOULD NOT RESET PER QRH. MACH TRIM YELLOW CAUTION MESSAGE WOULD NOT RESET PRE QRH. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNIT IAW 27-41-01, GROUND OPS CHECK GOOD. (M)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

FOUND STAB TRIM YELLOW CAUTION MESSAGE WOULD NOT RESET FOR QRH. MACH TRIM YELLOW CAUTION MESSAGE WOULD NOT RESET PER QRH. (M)

Part: CONTROL UNIT — MALFUNCTIONED (E/E BAY)

STAB TRIM CHANNEL 1 DISCONNECT WHEN YOKE TRIM SWITCH ENGAGED FROM EITHER SIDE. FERRIED TO DEN. REMOVED AND REPLACED HORIZ STAB P/N 8396-2 S/N 827, AND MCU P/N 7062-3 P/N 849, IAW AMM 27-42-01. OPS CHECK GOOD. REPORT CONFIRMED FAULT REMOVED REPLACED CH1 RVDT. REMOVED AND REPLACED DEFECTIVE RESISTOR, IC, DIODE AND INDUCTOR. (M)

Part: IDG — INTERMITTENT (NR 2)

INTERMITTENT IDG 2 CAS MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF MESSAGE CLEARED. BRAKE TEMP REMAIN IN NORMAL RANGE. COMPLIED WITH 'CM' ACTION. PLACARDED AND PLACED ON MEL. SERVICED NR 2 IDG AND RECONNECTED, CHECKS OK. REMOED FROM MEL. (M)

Part: ENGINE — FAILED (NR 1)

NR 1 ENGINE OIL PRESSURE WENT TO ZERO IN FLIGHT. SHUT DOWN NR 1 ENGINE IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE. OPERATIONAL CHECK NORMAL. INVESTIGATION CONTINUES. AIRCRAFT RETURNED TO SERVICE. (M)

Part: OIL COOLER — LEAKS (NR 1 ENGINE)

LOW OIL PRESSURE ON NR 1 ENGINE REQUIRED PRECAUTIONARY SHUT-DOWN. (OIL LIGHT ILLUMINATED AND PRESSURE DROPPED SLOWLY TO 40 PSI AND SHUT-DOWN WAS INITIATED.) MASTER WARNING FLASHED WITHOUT CAPTION. REMOVED AND REPLACED OIL COOLER IAW MM. GROUND RAN AIRCRAFT. OPS CHECK AND LEAK CHECK GOOD, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TOTAL CYCLES, 12,113. (X)