N445AW

Part: DETECTOR LOOP — SHORTED (10 TH STAGE) · airframe 38,161 hrs · 37,504 cycles

WHILE ON CLIMB OUT RECEIVED RT 10TH ST DUCT MESSAGE. C/W QRH. MESSAGE REMAINED AND THEN EXTINGUISHED A FEW MINS LATER. ONCE ON GROUND, BRIEFLY APPEARED TWICE ON TAXI. ECS SYNOPTIC SHOWED RED FROM RT SOV UP TO PACK PRESSURE. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT AND FOUND RT 10TH STAGE MANIFOLD LOOP B SENSING ELEMENT A12WK SHORT TO GROUND INTERNALLY. REMOVED AND REPLACED SENSING ELEMENT A12WK, REF AMM CHAP 36. OPERATIONS CHECK GOOD AT THIS TIME.

Part: ELEMENT — SHORTED (SENSING DETECTOR) · airframe 38,161 hrs · 37,503 cycles

RECEIVED RT 10TH DUCT WARNING ON INITIAL CLIMB OUT OF ORD, RAN QRH, MESSAGE PERSISTED. SYNOPTIC PAGE SHOWED RED FROM ISOL TO THE PYLON, MESSAGE REMAINED EVEN AFTER ENGINE AND APU SHUTDOWN. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT AND FOUND SENSE ELEMENT A57WK SHORTED TO GROUND. R & R SENSE ELEMENT, IAW AMM 36-21-04. OPERATIONS CHECK GOOD.

Part: SEAT TRACK — CORRODED (FS 421-559) · corrosion level 2 · airframe 38,018 hrs · 37,342 cycles

LBL 9 FS 421 TO 559+80 SEAT TRACK CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK SEGMENT LBL 9 FS 421 TO 559+80, IAW REO 601R-53-00-764 & SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 421-559) · corrosion level 2 · airframe 38,018 hrs · 37,342 cycles

RBL 9 AT FS 421-559+80 SEAT TRACK HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK SEGMENT RBL 9 AT FS 421-559+80, IAW REO 601R-53-00-764 AND CRJ 200 SRM 51-41-02.

Part: TEE FITTING — CORRODED (BS 559) · corrosion level 2 · airframe 38,018 hrs · 37,342 cycles

RBL 9 AT FS 559+80 HAS CORROSION ON T CAP. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T CAP AT RBL 9 AT FS 559+80 TO FS 559, IAW BOMBARDIER DWG 601R3501 AND CRJ200 SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 421-559) · corrosion level 2 · airframe 38,018 hrs · 37,342 cycles

LT SIDEWALL SEAT TRACK AT FS 421 TO FS 559+80 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DAMAGED SEAT TRACK SECTION LT SIDEWALL, IAW REO 601-53-00-764.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 38,018 hrs · 37,342 cycles

RBL 9, FS 559+88, SEAT TRACK CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK SEGMENT AT RBL 9, FS 559+88.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 38,018 hrs · 37,342 cycles

LBL 9, FS 558+88 HAS CORROSION ON SEAT TRACK. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK SEGMENT AT LB L9 FS 559+88, IAW REO 601R-53-00-764 AND CRJ200 51-40-02.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 36,971 hrs · 36,314 cycles

ON CLIMBOUT RECEIVED PAX DOOR LATCH CAUTION MESSAGE INTERMITTANTLY FOR 10 MINUTES, THEN MESSAGE ON STEADY FOR 10 MINUTES, THEN MESSAGE CLEARED. AFTER CONFERRING WITH MAINTENANCE CONTROL THE DECISION WAS MADE TO RETURN TO CKB.

Part: HINGE — DAMAGED (FUSELAGE) · airframe 36,970 hrs · 36,313 cycles

FOUND PAX DOOR HINGE HALF ON FUSELAGE SIDE TO BE WORN BEYOND LIMITS.

Part: FAIRING — DAMAGED (RT ENGINE) · airframe 35,549 hrs · 34,963 cycles

DURING WALK AROUND INSPECTION OF AIRCRAFT AFTER ARRIVAL AT HANGAR, MECHANIC NOTED RT ENGINE LOWER STANG FAIRING DAMAGED AND PARTIALLY MISSING FROM AIRCRAFT. MECHANIC REMOVED AND REPLACED THE RT ENGINE LOWER STANG FAIRING PER AMM 78-34-15. NO DAMAGE NOTED TO SURROUNDING AREA. NO EVIDENCE OF ENGINE INGESTION NOTED. UNABLE TO DETERMINE CAUSE OF FAILURE. SUSPECT RT ENGINE LOWER TRANSLATING COWL MAY HAVE BEEN OPENED TO AN OVER-EXTENDED POSITION DURING PRIOR MAINTENANCE WHICH MAY HAVE DAMAGED THE FAIRING.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 34,992 hrs · 34,396 cycles

RIGHT FLOOR SUPORT CORRODED IN THE AFT CARGO BAY, BS 574 TO 621. REPAIRED THE FLOOR SUPPORT IAW EA CRJ253-01021, REV-IR.

Part: FLANGE — CRACKED (T/R TORQUE BOX) · airframe 34,992 hrs · 34,396 cycles

LEFT THRUST REVERSER TORQUE BOX FLANGE CRACKED. REPAIRED THE FLANGE IAW REO 601R-78-30-2553, REV-A.

Part: FLANGE — CRACKED (T/R TORQUE BOX) · airframe 34,992 hrs · 34,396 cycles

LEFT ENGINE THRUST REVERSER TORQUE BOX CRACKED ON THE AFT FLANGE, 6 O'CLOCK POSITION. REPAIRED THE FLANGE IAW REO 601R-78-34-2527, REV-B.

Part: BEAM — DAMAGED (CARGO DOORWAY) · airframe 34,992 hrs · 34,396 cycles

CARGO DOOR ASSIST CABLE HAS CUT INTO HORIZONTAL SUPPORT BEAM. REPLACED THE BEAM IAW SRM 51-42-21, 51-40-11, AND 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,992 hrs · 34,396 cycles

FLOORBEAM ANGLE AT BS 280, AFT SIDE, LBL 9 WAS CRACKED. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.

Part: FRAME — CRACKED (BS 605) · airframe 34,992 hrs · 34,396 cycles

FRAME AT BS 605 OUTER FLANGE WAS CRACKED AT 2 LOCATIONS, STRINGER 9L. REPAIRED THE FRAME IAW REO 601R-53-61-5214, REV-A.

Part: SKIN — DENTED (BS 654-672) · airframe 34,992 hrs · 34,396 cycles

EXTERNAL FUSELAGE SKIN HAD A PROTRUDING DENT BETWEEN BS 654 AND 672, STRINGERS 21L TO 22L. REPAIRED THE SKIN IAW EA CRJ253-01011REV-IR

Part: SKIN — DENTED (BS 654-672) · airframe 34,992 hrs · 34,396 cycles

EXTERNAL FUSELAGE SKIN HAD A PROTRUDING DENT AT BS 654 TO 672, STRINGERS 22L TO 23L. REPAIRED THE SKIN IAW EACRJ253-01011, REV-IR.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 34,992 hrs · 34,396 cycles

RIGHT INBOARD FLAP LOWER SKIN HAS AREAS OF DENTS FROM WS 75.0 TO 50.5. REPAIRED RIGHT INBOARD FLAP LOWER SKIN IAW SRM 57-52-00.

Part: HOUSING — CRACKED (GROUND POWER) · airframe 34,992 hrs · 34,396 cycles

FOUND CRACKS ON THE POWER RECEPTACLE ATTACH HOUSING. REPLACED THE HOUSING IAW REO 601R-53-11-569 REV-B.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 34,992 hrs · 34,396 cycles

LEFT INBOARD FLAP VANE LEADING EDGE CHAFED AT WS 57.0. REPLACED THE FLAP VANE L/E SKIN IAW IAW SRM 51-42-13.

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 34,992 hrs · 34,396 cycles

FRAME BS 605 WAS FOUND CORRODED BETWEEN STRINGERS 22L AND 22R. REPLACED THE FRAME SECTION IAW SRM 51-21-06, 51-42-06, AND 53-61-15.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 34,992 hrs · 34,396 cycles

RIGHT INBD FLAP VANE L/E SKIN WAS CHAFED. REPLACED FLAP VANE IAW SRM 51-42-13.

Part: BRACKET — CRACKED · airframe 34,992 hrs · 34,396 cycles

A/C EXTERNAL SERVICE PANEL LOWER ATTACH ANGLE BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-42-06.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 34,992 hrs · 34,396 cycles

RIGHT INBD FLAP VANE SKIN WAS CHAFED. REPLACED THE FLAP VANE SKIN IAW SRM 51-42-13.

Part: FLAP — DAMAGED (LT WING) · airframe 34,992 hrs · 34,396 cycles

LT WING TE FLAP DAMAGED. REPAIRED IAW SRM 57-52-00.

Part: BRACKET — CRACKED (BS 527) · airframe 34,992 hrs · 34,396 cycles

RIGHT MLG WW TRANSDUCER BRACKET CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,296 hrs · 33,697 cycles

CLIMBING THROUGH FL210 RECEIVED ANTI ICE WARNING WITH OVERHEAT INDICATION, C/W QRH MESSAGE PERSISTED. AIR RETURNED TO ROC PER QRH, FLAPS 20 REF 45+30 KNOTS (SPEED WAS 169) NO THRUST REVERSERS AVAILABLE/FULL BRAKING. TEMPS AT GATE 8-10-5-5 LANDING WEIGHT 46,000 LBS. ANTI ICE DUCT SWITCH LIGHT OVERHEAT SECTION ILLUMINATED (WING), NO DUCT FAIL LIGHTS ILLUMINATED ON ANY SWITCH. WARNING CLEARED IN FLIGHT APPROXIMATELY 5-10 MINUTES AFTER RUNNING QRH. WHEN WARNING WAS RECEIVED 14TH STAGE SOV INDICATED OPEN, 10TH STAGE SOV INDICATED OPEN, APU LCV INDICATED CLOSED, ISOLATION VALVE CLOSED.

Part: HANDLE — DIRTY (SERVICE DOOR) · airframe 34,015 hrs · 33,381 cycles

SERVICE DOOR OUTER HANDLE WILL NOT POP OUT AND ALLOW DOOR TO OPEN. CLEANED AND LUBED OUTER HANDLE OPS CHECK GOOD AT THIS TIME REF AMM 52-41-00.

Part: UNKNOWN — LEAKING (APU) · airframe 33,342 hrs · 32,693 cycles

STRONG FUEL EXHAUST SMELL INSIDE OF ACFT REF 276650/3 APU FUEL LEAK. MAINTENANCE IS INVESTIGATING SOURCE OF SUSPECTED APU FUEL LEAK.

Part: WARNING MESSAGE — ACTIVATED (SPOILERONS) · airframe 32,965 hrs · 32,322 cycles

SPOILERON CAUTION MESSAGE IN CRUISE FLT. COMPLIED WITH QRH. LANDED AT FLAPS 20.

Part: ENGINE — FLUCTUATES (RIGHT) · airframe 31,639 hrs · 31,118 cycles

DURING CLIMB, WITH CLIMB POWER SET, N1 & N2 WILL NOT STABILIZE. N1 FLUCTUATES 88 PERCENT TO 92 PERCENT RAPIDLY ON RT ENGINE. DIVERTED AND LANDED AT APPROXIMATELY 40,000 LBS GROSS.

Part: ANGLE — CHAFED (PAX DOOR FRAME) · airframe 31,329 hrs · 30,837 cycles

WHILE PERFORMING NDT ON L1 DOOR, FOUND FRAME CHAFED UNDER FWD PULL IN LEVER. REPLACED THE L1 DOOR FRAME ANGLE IAW SRM 51-42-06, 51-42-21, EA CRJ252-00464 AND SUPPLEMENT 16-229.

Part: ANGLE — CORRODED (BS 319.70) · corrosion level 2 · airframe 31,329 hrs · 30,837 cycles

BS 319.70 FWD LOWER ANGLE STRIP HAS CORROSION BETWEEN STRINGERS 20 AND 22R IN THE FWD E&E BAY. REPAIRED THE ANGLE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,329 hrs · 30,837 cycles

FRAME 319.70 FWD LOWER ANGLE STRIP HAS CORROSION BETWEEN STR 22R AND 20R IN THE FWD ELECTRICAL EQUIPMENT BAY. REPAIRED CORROSION ON ANGLE AT FS 319.70 BETWEEN STR 20R AND 22R.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 31,329 hrs · 30,837 cycles

RIGHT SEAT TRACK NR 4, BS 559+04 TO FS 559+80 HAS CORROSION. REPLACED THE SEAT TRACK IAW AMM 53-01-11 AND REO 601R-53-00-485 REV-B.

Part: STIFFENER — BROKEN (APU BAY) · airframe 31,329 hrs · 30,837 cycles

APU ENCLOSURE HAS 3 EA BROKEN STIFFENERS FROM WEB. REPAIRED DAMAGED AREAS ON APU ENCLOSURE IAW SUP: NR 16-168, 16-233 AND EA AWAC-CRJ249-00467.

Part: ANGLE — CRACKED (WING TO BODY) · airframe 31,329 hrs · 30,837 cycles

LEFT WING TO FUSELAGE PANEL ATTACHING STRUCTURE BS 473.15 IS CRACKED. REPLACED ATTACH FITTING IAW SRM 51-42-10, 51-42-02.

Part: PANEL — CRACKED (PAX DOOR) · airframe 31,329 hrs · 30,837 cycles

PAX DOOR FWD RISER PANEL IS CRACKED AT THIRD STEP. REPAIRED THE RISER PANEL IAW REO 601R-52-11-702 REV-D AND SUPPLEMENT 16-223.

Part: PANEL — CRACKED (PAX DOOR) · airframe 31,329 hrs · 30,837 cycles

PAX DOOR AFT RISER PANEL IS CRACKED AT FIRST STEP. REPAIRED THE RISER PANEL IAW REO 601R-52-11-702.

Part: FITTING — CORRODED (BS 621) · corrosion level 2 · airframe 31,329 hrs · 30,837 cycles

LBL 9, BS 621 ATTACH FITTING IS CORRODED. REPAIRED THE FITTING IAW EA AWAC-CRJ253-00452.

Part: FLOOR SUPPORT — CORRODED (BS 597-609) · corrosion level 2 · airframe 31,329 hrs · 30,837 cycles

RBL 27 FLOOR SUPPORT HAS CORROSION AT BS 597 AND 609. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-21, 51-42-22, SUPPLEMENT 15-279.

Part: FITTING — CORRODED (BS 621) · corrosion level 2 · airframe 31,329 hrs · 30,837 cycles

LBL 27, BS 621ATTACH FITTING HAS CORROSION. REPAIRED THE FITTING IAW EA AWAC-CRJ253-00453.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 31,329 hrs · 30,837 cycles

RIGHT INBD FLAP LOWER SKIN CORNER HAS NNUMEROUS NICKS, SCRATCHES AND GOUGES. REPLACED THE FLAP SKIN IAW SRM 51-42-13.

Part: PANEL — CRACKED (BS 310-349) · airframe 31,329 hrs · 30,837 cycles

PAX DOOR AFT RISER PANEL IS CRACKED AT 4TH STEP

Part: SKIN — DENTED (FUSELAGE) · airframe 31,329 hrs · 30,837 cycles

FUSELAGE UPPER SKIN HAS A DENT WITH GOUGE AT FS 636 AND BETWEEN STR 0 AND 1R.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 31,329 hrs · 30,837 cycles

LEFT INBD FLAP VANE LE IS CHAFED AT THREE LOCATIONS WERE STOPS HIT THE VANE

Part: DOUBLER — CORRODED (BS 605-621) · corrosion level 2

AFT POTABLE WATER DRAIN MAST INTERNAL DOUBLER CORRODED.

Part: PANEL — CRACKED (PAX DOOR) · airframe 31,329 hrs · 30,837 cycles

PAX DOOR AFT RISER PANEL IS CRACKED AT 3RD STEP.

Part: FLOOR SUPPORT — CORRODED (BS 559-561) · corrosion level 2 · airframe 31,329 hrs · 30,837 cycles

RIGHT FLOOR SUPPORT CORRODED, BS 559+86 TO 561.

Part: FLOORBEAM — CORRODED (BS 559) · corrosion level 2 · airframe 31,329 hrs · 30,837 cycles

RBL 9 FLOORBEAM CAP HAS CORROSION AT FS 559+82.

Part: WEB — CRACKED (BS 202) · airframe 31,329 hrs · 30,837 cycles

RIGHT WINDSHIELD SIDE POST SUPPORT WEB IS CRACKED. REPLACED THE WEB IAW SRM 51-40-11, AND 51-42-06.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 31,329 hrs · 30,837 cycles

PAX DOOR INTERAL INTERCOSTAL CRACKED, BS 343 AFT SIDE OF DOOR. REPLACED THE INTERCOSTAL IAW SRM 51-42-06, 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,329 hrs · 30,837 cycles

LEFT OBLIQUE ANGLE AT STR 15L ON AFT SIDE OF REAR PRESSURE BULKHEAD FS 621.00 IS CRACKED. REPLACED OBLIQUE ANGLE AT FS 621.00 AND STR 15L ON AFT SIDE OF REAR PRESSURE BULKHEAD IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 202) · airframe 31,329 hrs · 30,837 cycles

WINDSHIELD CENTER POST A, BS 202.75 LOWER LEFT ANGLE IS CRACKED. REPLACED THE ANGLE IAW SRM 51-42-21.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 31,329 hrs · 30,837 cycles

FLOOR STRAP AT BS 559+82 CORRODED BETWEEN RBL 9 - 27. REPLACED THE STRAP IAW SRM 51-42-06.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 31,329 hrs · 30,837 cycles

FS 621.00 BULKHEAD FWD FACE IS CHAFED 5 PLACES FROM SCREW CONTACT. ALL 5 PLACES ARE 30" ABOVE FLOOR LEVEL AT LBL18, LBL27, RBL18, RBL27, RBL36. REPAIRED AFT PRESSURE BULKHEAD FWD FACE AT 5 LOCATIONS, 30" ABOVE FLOOR AT LBL18, LBL27, RBL18, RBL27, RBL36 IAW REO 601R-53-61-1285, REO 601R-53-61-2155.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,329 hrs · 30,837 cycles

RIGHT WING TO FUSELAGE PANEL ATTACHING STRUCTURE AT FS 473.15 IS CRACKED. REPLACED ANGLE AT RT FS 473.15 AND RBL 45 IAW SRM 51-42-06,51-42-21.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,329 hrs · 30,837 cycles

PASSENGER DOOR CUTOUT UPPER SILL, FWD END, ATTACH ANGLE IS CRACKED AT FS 280.00, STR 3L. REPLACED ATTACH ANGLE AT PAC DOOR CUTOUT UPPER SILL FORWARD END AT FS 280.00 AND STR 3L IAW SRM 51-42-06,51-42-21.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,329 hrs · 30,837 cycles

PAX DOOR AFT DRAG ANGLE CRACKED BY ASSIST MOTOR PULLEY. REPAIRED THE PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,329 hrs · 30,837 cycles

LT WING TO FUSELAGE PANEL ATTACHING STRUCTURE AT FS 449.85 IS CRACKED. REPLACED ANGLE AT FS 449.85 LT SIDE LBL45 IAW SRM 515-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,329 hrs · 30,837 cycles

RIGHT WING TO FUSELAGE PANEL ATTACHING STRUCTURE AT FS 449.85 IS CRACKED. REPLACED ANGLE AT FS 449.85, RBL45 IAW SRM 51-42-06.

Part: ANGLE — CRACKED (WING TO BODY) · airframe 31,329 hrs · 30,837 cycles

LEFT WING TO FUSELAGE PANEL ATTACHING STRUCTURE AT BS 461 IS CRACKED. REPLACED THE ANGLE IAW SRM 51-42-06.

Part: ANGLE — CRACKED (WING TO BODY) · airframe 31,329 hrs · 30,837 cycles

RIGHT WING TO FUSELAGE PANEL ATTACHING STRUCTURE AT BS 481.15 IS CRACKED. REPLACED THE ANGLE IAW SRM 51-42-06.

Part: FRAME — CRACKED (BS 333) · airframe 31,329 hrs · 30,837 cycles

BS 333 AT STRINGER 1L FRAME IS CRACKED. REPLACED THE FRAME IAW SRM 51-42-06, 51-42-21.

Part: DOUBLER — CORRODED (BS 409) · corrosion level 2 · airframe 31,329 hrs · 30,837 cycles

ACFT BELLY INSIDE SKIN DOUBLER HAS CORROSION, BETWEEN BS 409+32 TO 409+16 AND STRINGERS 25 - 26L IN THE FWD E & E BAY. REPLACED THE SKIN DOUBLER AND FILLER IAW EC 601R-53-4534.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 31,329 hrs · 30,837 cycles

FORWARD CARGO DOOR TRACK LOWER AFT U CHANNEL IS CRACKED. REPLACED FWD CARGO DOOR AFT TRACK LOWER U-CHANNEL IAW SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,329 hrs · 30,837 cycles

PILOTS WINDSHIELD SIDE POST LOWER OTBD CLIP IS CRACKED. REPLACED PILOTS SIDE POST OTBD LOWER CLIP IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,329 hrs · 30,837 cycles

COPILOTS WINDSHIELD SIDE POST LOWER OTBD CLIP IS CRACKED. REPLACED COPILOTS WINDSHIELD SIDE POST LOWER OTBD CLIP IAW SRM 51-42-21.

Part: GENERATOR — FAILED (NR 1 ENGINE) · airframe 30,056 hrs · 29,649 cycles

GENERATOR ! OFF CAUTION MSG ON TAKEOFF ROLL AT 40 KTS, ABORTED. BTMS READS 2, 2, 2, 2. R & R GEN 1 IAW AMM 24-11-01. OPERATIONS & LEAK CHECKS GOOD. REMOVED MEL & REMOVED PLACARD.

Part: LIGHT — FAILED (CABIN) · airframe 28,160 hrs · 27,852 cycles

EMERGENCY LIGHT AT PAX DOOR INOPERATIVE. INSPECTED & VERIFIED POWER TO LIGHT IS AVAILABLE & ASSEMBLY BULBS ARE GOOD. ASSEMBLY BAD.

Part: UNKNOWN — ODOR

AT 1000 FT AGL ACFT SHUTTERED & HAD A LOUD VIBRATING NOISE THROUGH PACKS WITH BURNING SMELL, ALSO HAD BURNING SMELL ON BLEED XFER AT GATE. INSPECTED & OPERATED BOTH PACKS IAW AMM 21-50-00, NO BURNING SMELL NOTED. LT PACK OPERATES NORMAL, NO DEFECT NOTED. FOUND RT PACK TEMP UNCONTROLLABLE IN AUTO. RT PACK MEL, INSPECTED RT PACK, NO LOOSE DUCTING OR CONNECTORS NOTED. PERFORMED OPERATIONS TEST OF RT PACK, OPERATIONS CHECKED GOOD IAW AMM 21-51-00. INSPECTED & CLEANED HIGH PRESS WATER SEPARATOR IAW SUPP 11-039B, NO DEFECTS NOTED. INSPECTED DRAIN LINES FOR LOW PRESS WATER SEPARATOR FOR FOREIGN MATTER IAW AMM 21-51-13, NO DEFECTS NOTED. OPERATIONS CHECKED RT PACK CONTROL SYS IAW AMM 21-60, OPERATION IS NORMAL. INSPECTED APU INTAKE FOR BIRD INGESTION IAW AMM 49-14-00, NO EVIDENCE NOTED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,607 hrs · 26,373 cycles

CARGO DOOR FWD DOOR STOP LOWER CLIP CRACKED.

Part: DOOR SILL — CORRODED (PAX DOORWAY) · corrosion level 2 · airframe 26,607 hrs · 26,373 cycles

PAX DOOR SILL CORRODED AROUND GROUND TERMINALS & CONNECTOR.

Part: PANEL — CRACKED (PAX DOOR) · airframe 26,607 hrs · 26,373 cycles

COMPLIED WITH AWAC CARD 4DMI17146 REPAIR PAX DOOR AFT SIDE PNL 601R-52-11-2178.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 26,607 hrs · 26,373 cycles

PAX DOOR ASSIST MOTOR MOUNT BRACKET CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,607 hrs · 26,373 cycles

LT OBLIQUE ANGLE AT FS 625.30 IS CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,607 hrs · 26,373 cycles

RT OBLIQUE ANGLE AT FS 625.30 IS CRACKED.

Part: ATTACH FITTING — CRACKED (CARGO DOOR) · airframe 26,607 hrs · 26,373 cycles

CARGO DOOR FWD ATTACH FITTING CRACKED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,607 hrs · 26,373 cycles

RT BRACKET TRANS. BRACKET IS CRACKED.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 26,607 hrs · 26,373 cycles

RT WING LE REFUEL PORT MOUNT, OTBD ATTACHMENT BRACKET CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,607 hrs · 26,373 cycles

FS 280 INBD & OTBD CLIPS CRACKED ON RBL 9.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 26,607 hrs · 26,373 cycles

LEFT BRAKE TRANSDUCER BRACKET CRACKED IN LT MLG WW.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,607 hrs · 26,373 cycles

FS 280 INBD & OTBD CLIPS CRACKED AT LBL 9.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,607 hrs · 26,373 cycles

CARGO FLOOR TRACK ON LBL 9 AT FS 559+96 IS CORRODED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,607 hrs · 26,373 cycles

FS 484 CLIP ON LBL 27 CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,607 hrs · 26,373 cycles

FS 484 CLIP CRACKED AT RBL 27.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,607 hrs · 26,373 cycles

NUMBER 2 LT SIDE SEAT TRACK IS CORRODED AT FS 409+20 - 409+99.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,607 hrs · 26,373 cycles

CARGO FLOOR TRACK AT LBL 9 & FS 574 CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,607 hrs · 26,373 cycles

FLOOR SEAT TRACK ON LBL 9 AT FS 349 CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,607 hrs · 26,373 cycles

SEAT TRACK AT RBL 9 AT FS 349 IS CORRODED.

Part: CHANNEL — INOPERATIVE (HORIZ STAB) · airframe 26,140 hrs · 25,939 cycles

STAB CHANNEL 2 INOPERATIVE.

Part: AILERON SYS — MALFUNCTIONED · airframe 24,692 hrs · 24,516 cycles

WITH AUTOPILOT ON, RECEIVED UNCOMMANDED LT ROLL WHILE BEING VECTORED FOR APPROACH WITH FLAPS 8. DISCONNECTED AUTOPILOT AND ROLL CONTROL VERY STIFF AND HEAVY. AILERON TRIM CAUTION ON PFD ASSOCIATED WITH UNCOMMANDED ROLL. COMPLIED WITH OPS TEST OF AILERON CONTROL SYS IAW AMM 27-11-00 AND OPS TEST OF AILERON DISCONNECT SYS IAW AMM 27-13-00, OPS CHECKED GOOD, NO ABNORMALITIES FOUND WITH AILERON MOVEMENT, ACFT OK FOR SERVICE.

Part: SENSOR — MALFUNCTIONED (LT ENGINE) · airframe 24,586 hrs · 24,411 cycles

DURNING DECENT, RECEIVED INTERMITTENT LT 14 STG DUCT WARNING MESSAGE. AFTER SEVERAL MINUTES OF INTERMITTENT MESSAGES, MESSAGE REMAINED ON UNTIL DESCENDING BELOW 8000 FT. CREW PERFORMED QRH & DECLARED AN EMERGENCY. R & R LT ENGINE PYLON SENSOR ELEMENT IAW AMM 36-21- 04. OPS CHECKED GOOD.

Part: SKIN — DENTED (RT WING) · airframe 21,763 hrs · 21,706 cycles

RIGHT CENTER WING LOWER SKIN HAS A DENT AFT OF REFUEL RECEPTACLE DOOR. FOUND TO BE WITHIN LIMITS IAW REO 601R-57-11-060.

Part: THRESHOLD — CORRODED (FS 310-349) · airframe 21,763 hrs · 21,706 cycles

SERVICE DOOR THRESHOLD CORRODED. REMOVED UNSERVICEABLE SERVICE DOOR THRESHOLD AND REPLACED WITH SERVICEABLE DOOR THRESHOLD IAW SRM 51-41-02.

Part: SKIN — GOUGED (FS 559) · airframe 21,763 hrs · 21,706 cycles

LEFT FUSELAGE SKIN GOUGED JUST FWD OF FS 559.0 CUT OUT DAMAGED AREA, NDT, FABRICATE AND INSTALL REPAIR PARTS IAW REO 601R-53-41-610, REV, SRM 51-21-11, 51-25-06, 51-25-16, 51-42-06, 51-41-02, 51-42-13, 51-41-00.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 21,963 hrs · 21,706 cycles

LEFT INBD FLAP VANE L/E CHAFED FOUR SPOTS. REPAIRED CHAFED AREAS AT OTBD AND CENTER LOCATION ON LT INBD FLAP VANE L/E IAW REO 601R-57-52-004, REV C. R & R LT INBD FLAP VANE INBD L/E SKIN IAW SRM 51-42-13.

Part: FLOOR SUPPORT — CORRODED (FS 574-612) · airframe 21,763 hrs · 21,706 cycles

FLOOR SUPPORT CORRODED FOUND AROUND SCREW HOLES ON TOP OF CAP ON LBL 27 BETWEEN FS 574 & FS 621. R & R WITH SERVICEABLE FLOOR SUPPORT CAP IAW REO 601R-53-61-3778.

Part: RETAINER — CRACKED (NACELLE) · airframe 21,763 hrs · 21,706 cycles

PANEL 422BT, AFT DIVIDER PANEL RETAINER CRACKED. REMOVED UNSERVICEABLE AFT DIVIDER ON PANEL 422BT AND REPLACED WITH SERVICEABLE DIVIDER 601R37003-180 IAW SRM 51-42-06.

Part: TRUNNION — DAMAGED (LT MLG) · airframe 21,763 hrs · 21,706 cycles

LEFT LOWER AFT, LOWER FLANGE OF MLG TRUNNION FITTING HAS ONE OVERSIZE HOLE. REPAIRED HOLE ON LT LOWER MLG TRUNNION FLANG IAW REO 601R-57-21-1699, REV.

Part: PANEL — DAMAGED (NACELLE) · airframe 21,763 hrs · 21,706 cycles

PANEL NR422 DB DIVIDER PANEL KNIFE EDGED. REMOVED UNSERVICEABLE DIVIDERS AND REPLACED WITH SERVICEABLE IAW SRM 51-42-06.

Part: SKIN — GOUGED (FS 310) · airframe 21,763 hrs · 21,706 cycles

PAX DOOR CUT OUT FWD SEAL STRIKER AT FS 310.00 IS GOUGED. C/W REO 601R-53-22-033, REV C BY TRIMMING OUT DAMAGE & INSTALLING STRAP DOUBLER.

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 21,763 hrs · 21,706 cycles

CARGO DOOR OUTER HANDLE CRACKED. R & R CARGO DOOR OUTER HANDLE IAW SRM 51-42-21.

Part: STIFFENER — CRACKED (LT EXHAUST DUCT) · airframe 21,763 hrs · 21,706 cycles

LEFT JET PIPE FWD STIFFENER AT 3 O`CLOCK POSITION IS CRACKED BEYOND STOP DRILL. REPAIRED LT JET PIPE FWD STIFFENER AT 3 O`CLOCK POSITION IAW CMM 78-11-00, SRS 042.

Part: SUPPORT BRACKET — CRACKED (FS 718-755) · airframe 21,763 hrs · 21,706 cycles

HYS SYSTEM NR 1 ACMP CASE DRAIN FILTER SUPPORT BRACKET CRACKD AND WARPED. R & R BRACKET IAW SRM 51-42-06.

Part: ADC — MALFUNCTIONED (NR 2) · airframe 18,043 hrs · 17,840 cycles

IN CRUISE, AT 25,000 FT AND 300 KNTS, ADC 2 FAILED. R & R ADC NR2 IAW AMM 34-13-01, OPS CK AND LEAK CK GOOD AT THIS TIME.

Part: SENSOR — MALFUNCTIONED (MLG) · airframe 20,138 hrs · 20,079 cycles

AFTER LANDING GEAR UP- RECEIVED ANTI SKID INBD CAUTION MESSAGE, FOLLOWED BY PARKING BRAKE SOV MESSAGE FOLLOWED BY A GEAR DISAGREE WARNING MESSAGE, LT MAIN GEAR INDICATED DOWN AND LOCKED WHILE THE NOSE AND RT MAIN INDICATED UP AND LOCKED. QRH PERFORMED QRH, RETUREND TO DEPARTURE. ADJUSTED LOCK SENSORS ON MLG.

Part: DUCT — DISCONNECTED · airframe 17,945 hrs · 17,727 cycles

RT 10TH STAGE DUCT WARNING MESSAGE. CLEARED WHEN TURNING OFF RT PACK. INSP AND FOUND DISCONNECTED DUCT BETWEEN PRECOOLER AND HEAT EXCHANGER ON RT PACK. REPLACED SEAT AND CLAMP IAW AMM 21-51-07. OPS CK GOOD.

Part: HANDLE — BINDING (SERVICE DOOR) · airframe 17,501 hrs · 17,250 cycles

F/A UNABLE TO OPEN SERVICE DOOR FROM INSIDE OR OUTSIDE. INSPECTED AND CLEANED SERVICE DOOR HANDLE. DOOR OPERATES NORMALLY FROM INSIDE OR OUT.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 17,206 hrs · 16,925 cycles

PAX DOOR DRAG ANGLE AFT SECTION CRACKED. REMOVED CRACKED AFT DRAG ANGLE SECTION AND INSTALLED NEW SECTION OF DRAG ANGLE IAW REO 601R-52-11-513, REV A.

Part: BULKHEAD — DAMAGED (BS 280) · airframe 17,206 hrs · 16,925 cycles

RT FS280 BULKHEAD HAS A CREASE ON AFT SIDE MEASURING 20" IN LENGTH, CREASE STARTS @ 45" ABOVE FLOOR LEVEL ON INBD SIDE AND PROTRUDES DOWN AND OTBD. REPAIRED RT FS 280 BULKHEAD WEB IAW REO 601R-53-11-1954.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 17,206 hrs · 16,925 cycles

PAX DOOR OUTER HANDLE CRACKED. R & R WITH NEW SERVICEABLE OUTER HANDLE IAW AMM 52-11-03.

Part: FRAME — CRACKED (BS 559) · airframe 17,206 hrs · 16,925 cycles

FOUND RBL 9 CRACKED INBD SIDE FROM LOWEST RIVET TO EDGE OF POST REPAIR BY INCORPORATION OF REO 601R-53-41-260, REV D, 601R-53-41-609, REV B & REO 601R-53-41-1116, REV A TO LT AND RT SIDES, LBL 27 TO RBL.

Part: BULKHEAD — CHAFED (BS 280) · airframe 17,206 hrs · 16,925 cycles

RT FS 280 BULKHEAD HAS 2 EA AREAS OF CHAFING ON INBD AFT SIDE. 1 MEASURES 2" LENGTH & 2ND MEASURES 1.5" IN LENGTH AT IS 21" FROM FLOOR. REPAIRED FS280 BULKHEAD @ RBL 11.00 BETWEEN STR 13A & STR 14A IAW REO 601R-53-11-1727.

Part: BRACKET — CRACKED (RT WING) · airframe 17,206 hrs · 16,925 cycles

RT INBD FLAP INBD HINGE MIDDLE INBD FLAP FAIRING BRACKET/ANGLE CRACKED. R & R WITH DUPLICATED PART IAW SRM.

Part: PANEL — CHAFED (LT PYLON) · airframe 17,206 hrs · 16,925 cycles

CHAFE ON EDGE AT PANEL 412DB DIVIDERS. R & R PANLE 412DB DIVIDERS.

Part: ANGLE — CRACKED (RT WING) · airframe 17,206 hrs · 16,925 cycles

RT INBD FLAP HINGE OTBD FAIRING ANGLE ON INBD HINGE CRACKED REF 16 SRM 57-21-55. R & R WITH DUPLICATED PART IAW SRM.

Part: CHANNEL — CHAFED (RT PYLON) · airframe 17,206 hrs · 16,925 cycles

PANEL 422DB DIVIDERS CHAFED. R & R DIVIDERS ON PANEL 422DB.

Part: CHANNEL — CHAFED (LT PYLON) · airframe 17,206 hrs · 16,925 cycles

LT PYLON PANEL 412BT DIVIDER CHANNELS ARE CHAFED. R & R DIVIDER CHANELS ON PANEL 412BT.

Part: SKIN — CHAFED (RUDDER) · airframe 17,206 hrs · 16,925 cycles

RUDDER L/E SKIN IS CHAFED. REPAIRED DAMAGE ON RUDDER L/E SKINS IAW SRM 55-40-00.

Part: FITTING — CRACKED (BS 461) · airframe 17,206 hrs · 16,925 cycles

FITTING AT RBL 9 AND FS 641.00 CRACKED FITTING CHANGED IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 621) · airframe 17,206 hrs · 16,925 cycles

RT OBLIQUE ANGLE CRACKED. R & R RT OBLIQUE ANGLE IAW SRM 51-42-06, SRM 51-42-21 AND REV 601R-53-61-422.

Part: ATTACH FITTING — CORRODED (BS 484) · airframe 17,206 hrs · 16,925 cycles

LT INBD 484.00 CLIP IS CRACKED. R & R ANGLE IAW SRM 51-42-21 AND 51-23-00.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,206 hrs · 16,925 cycles

FLOOR ANGLE AT FS 280 IS CRCKED JUST OTBD OF LBL 9.0. REPAIRED FS280 AFT FLOOR SUPPORT ANGLE IAW REO 601R-53-11-138.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,206 hrs · 16,925 cycles

CLIP AT RBL9 AND FS 280 IS CRACKED. LOCATED ON OTBD SIDE OF RBL9.0. R & R CLIP AT FS280 OTBD SIDE OF RBL9.0 IAW SRM 51-42-21.

Part: PRESSURE BLKHD — CRACKED (BS 202.75) · airframe 17,206 hrs · 16,925 cycles

CRACK ON BULKHEAD AT FS202 AT PARKING BRAKE FEED THROUGH REPAIRED CRACKED FS202, BULKHEAD AT BL 23.71 IAW REO 601R-53-11-563.

Part: RIB — CRACKED (LT WING) · airframe 17,206 hrs · 16,925 cycles

LT BATT RIB CRACKED AT WS 53.60, REO 601R-57-51-046 CARRIED OUT.

Part: CHANNEL — CRACKED (RT NACELLE) · airframe 12,441 hrs · 12,203 cycles

RT ENGINE UPPER CORE COWL AFT U CHANNEL IB SIDE CRACKED. RT ENGINE UPPER CORE COWL AFT U CHANNEL IB SIDE REPAIRED IAW SHORTS CMM 20-12-00. (K)

Part: SUPPORT BRACKET — CRACKED (BS 531) · airframe 12,441 hrs · 12,203 cycles

LT WHEEL WELL HYDRAULIC SUPPORT BRACKET AT FS 531.75, BTW LBL 18-27 IS CRACKED LENGTH OF CRACK IS 0.350". LT WHEEL WELL HYDRAULIC SUPPORT BRACKET AT FS 531.75 BTW LBL 18-27, IS REPLACED IAW CRJ 200 SRM 51-42-06. (K)

Part: CROSSBEAM — CRACKED (BS 280) · airframe 12,441 hrs · 12,203 cycles

FS 280.00, LBL 9.0, WL 70.00 CROSS BEAM CRACKED IN THE LOWER RADIUS. FS 280, LBL9, WL 70.00. CROSSBEAM CUTOUT IAW REO 601R-53-11-171, REV D. (K)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 12,441 hrs · 12,203 cycles

FS 280, RBL 9.00, WL 71.00 IB CLIP CRACKED. FS 280, RBL 9, WL 71.00 IB CLIP REPLACED IAW CRJ 200, SRM 51-42-06 AND 51-42-20. (K)

Part: CROSSBEAM — CRACKED (BS 280) · airframe 12,441 hrs · 12,203 cycles

FS 280.00, RBL 9.00, WL 70.00, CROSS BEAM IS CRACKED IN THE LOWER RADIUS. CROSSBEAM AT FS 280.00, RBL 9.0, WL 70.00. REPAIRED IAW REO 601R-43-11-171, REV D. (K)

Part: SUPPORT — CRACKED (BS 280) · airframe 12,441 hrs · 12,203 cycles

FS 280.00 LBL 9.0, WL 71.00 IB SUPPORT CLIP IS CRACKED. IB SUPPORT CLIP AT FS 280.00, LBL 9.00, WL 71.00. REPLACED IAW REO 601R-53-11-171, REV D. (K)

Part: SUPPORT BRACKET — CRACKED (BS 523) · airframe 12,441 hrs · 12,203 cycles

RT WHEEL WELL HYDRAULIC SUPPORT BRACKET AT FS 523.60 IS CRACKED. RT WHEEL WELL HYDRAULIC SUPPORT BRACKET AT FS 523.60 IS REPLACED IAW CRJ 200, SRM 51-42-06. (K)

Part: SILL — CRACKED (BS 574) · airframe 12,441 hrs · 12,203 cycles

CRACK FOUND ON CARGO BAY FLOOR SILL FS 574, LBL 45. ON CARGO BAY FLOOR SILL FS 574, LBL45 CRACK IS REPAIRED IAW REO 601R53-61-1741. (K)

Part: SILL — CRACKED (BS 589) · airframe 12,441 hrs · 12,203 cycles

CRACK FOUND ON LOWER SILL OF CARGO DOOR FS 589, LBL 45. ON LOWER SILL OF CARGO DOOR FS 589 LBL45, CRACK IS REPAIRED IAW REO 601R-53-61-433. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,441 hrs · 12,203 cycles

CRACK FOUND IN THE AFT DRAG ANGLE OF THE PAX DOOR STAIR ASSY LENGTH OF CRACK 1.50". DRAG ANGLE OF THE PAX DOOR STAIR ASSY, AFT SIDE, REPAIRED IAW CRJ 200 REO 601R 52-11-513. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,441 hrs · 12,203 cycles

INTERCOSTAL CLIP FS 484 LBL 27 CRACKED. NEW INTERCOSTAL CLIP INSTALLED FS 484, LBL 27 IAW CRJ 200 SRM 51-42-21. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,441 hrs · 12,203 cycles

INTERCOSTAL AT FS 484, RBL 36 CRACKED. INTERCOSTAL AT FS 484, RBL 36 REPAIRED IAW CRJ 200, REO 601R-53-41-059 REV A. (K)

Part: SUPPORT BRACKET — CRACKED (BS 529)

RT WHEEL HYDRAULIC SUPPORT BRACKET AT FS 529.98, BTW RBL 18-27 IS CRACKED. CRACK LENGTH IS .250 INCH. NEW RT WHEEL WELL HYDRAULIC SUPPORT BRACKET INSTALLED AT FS 529.98 BTW RBL 18-27 IAW CRJ 200 SRM 51-42-06. (K)

Part: WIRE HARNESS — DAMAGED (NR 1 ENGINE) · airframe 12,310 hrs · 12,103 cycles

ENG NR 1 SHUTDOWN IN FLIGHT, NO ASSOCIATED EICAS MESSAGES ILLUMINATED BEFORE SHUTDOWN. THRUST LEVERS WERE ABOVE IDLE AT APPROXIMATELY 80%. RAN QRH, TRIED TO RELIGHT. ENG RELIT FOR 15-20 SECONDS THEN GOT LOW OIL PRESSURE RED WARNING. DID PRECAUTIONARY SHUTDOWN. ENG WAS SHUTDOWN FOR APPROXIMATELY 15 MINUTES. REF W/O 127068 FOR WORK PERFORMED CLEANED BROWN HARNESS AND T2 SENSOR. R&R RT ENGINE BROWN HARNESS IAW AMM 73-21. OPS CHECK GOOD. REMOVED PLACARD & MEL.

Part: COALESCER BAG — ODOR (RIGHT)

ODOR AND HAZE DETECTED IN CABIN, SMOKE TOILET CASS MESSAGE NO VISIBLE SIGN OF SMOKE IN LAV. TURNED OFF RIGHT PACK AND CASS MESSAGE WENT AWAY AS DID HAZE AND ODOR. TROUBLESHOT PER FIM, 79-20-0. REMOVED AND REPLACED COALESCER SOCKS ON LT AND RT SIDE. OPS CHECK OF PACK GOOD. NO ODOR OR HAZE NOTED. (M)

Part: FIRE BOTTLE — UNKNOWN (RT) · airframe 9,676 hrs · 9,547 cycles

MAINTENANCE REPORTED RT ENGINE BOTTLE NR 2 PUS-TO DISCHARGE GREEN PUSHBUTTON WOULD NOT ILLUMINATE WHEN TESTED. REMOVED AND REPLACED RT ENGINE FIRE BOTTLE FIRE BOTTLE. OPS CHECK GOOD. (K)

Part: RECORDER — MALFUNCTIONED (COCKPIT V R) · airframe 8,021 hrs · 7,926 cycles

WOW OUTPUT CAUTION IN FLIGHT, AS WELL AS WOW OUTPUT CAUTION PROX SYSTEM FAULT, WOW OUTPUT FAIL. REMOVED AND REPLACED CVR IAW AMM 23-71-01, OPS CHECK GOOD AT THIS TIME PERFORMED TEST OF PSEU IAW AMM. OPS CHECK GOOD. CRV FIXED THE PSEU AND WOW PROBLEM. (K)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FOUND LEFT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. MAINTENANCE CUT AWAY DAMAGED SECTION OF ANGLE. FABRICATED STRAP FROM 7024-73 .090. LOCATED AND DRILLED ANGLE. REPAIR ANGLE AND STRAP IAW BSC REO 601R-53-61-117 STEPS 1/2. COMPLETED REPAIR IAW REO 601R-53-61-117 STEPS 3-7 BY INSTALLING REPAIR ANGLES AND FASTENERS WET. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FOUND RIGHT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. COMPLETED REPAIR IAW BSC REO 601R-53-61-117 STEPS 2-7 BY FINISHING CUTLINES, INSTALLING REPAIR ANGLES AND FASTENERS WET. UP TO LEAK CHECK. LEAK CHECK GOOD IAW CRJ AMM TASK 21-32-00-863-801. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FOUND INTERCOSTAL ATTACH FLANGE IS CRACKED .3 INCH AT FS 484, LBL 36, WL 73. CUT AWAY DAMAGED FLANGE FABRICATED REPAIR ANGLE USING 56144-14 PREFORMED ANGLE 2024-T42-063 WET INSTALLED ANGLE AIW REO 601R-53-41-059. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

LEFT FS 621 TO 625 INTERCOSTAL ANGLE (OBLIQUE) CRACKED. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED AN NEW SERVICEABLE ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

FOUND RT FS 621 TO 625 INTERCOSTAL OBLIQUE ANGLE OBLIQUE CRACKED. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED A NEW ANGLE P/N 601-35012-52 IAW CRJ SRM 51-42-06. (M)

Part: TUNING UNIT — FAILED (COCKPIT)

STRONG ELECTRICAL ODOR ON FLIGHT DECK ON DESCENT INTO SAVE BACKUP RTU BACKLIGHTING AND RTU INOPERATIVE. REMOVED AND REPLACED BACKUP TUNING UNIT. TEST GOOD IAW AMM. REMOVED OFF MEL. NO FURTHR OCCURRENCES. (M)

Part: ENGINE — MALFUNCTIONED (NR 2)

NR 2 ENGINE ONLY PRODUCED 50 PERCENT POWER. ABORTED TAKEOFF AT 60 KNOTS. ALMOST NO BREAKING USED, MAX 2 PERFORMED POWER ASSURANCE CHECK IAW AMM 71-00-00-710-804. PERFORMED CHECKS WITHIN LIMITS. COULD NOT DUPLICATE PROBLEM. (M)