N405AW

Part: SHUTOFF VALVE — MALFUNCTIONED (AC BAY) · airframe 41,586 hrs · 38,663 cycles

ON DEPARTURE OUT OF ATW WITH ONE PACK ON MEL THE OTHER PACK INDICATED OVERPRESSURE. THE CAPTAIN OPTED TO RETURN TO ATW. RECORDED LOGBOOK DISCREPANCY: WHEN TRANSFERRING BLEEDS, APU SELECTED RIGHT 10TH STAGE BLEEDS REMAINED CLOSED, RIGHT PACK HI PRESSURE C/W QRH CAS MIS COMP". MX REPLACED THE RH PACK PRESSURE REGULATING AND SHUTOFF VALVE.

Part: FLAP SYSTEM — MALFUNCTIONED

FLAP FAIL AT ZERO AT 8000FT ON ARRIVAL AFTER SELECTING FLAPS 8. PERFORMED RESET PER AWA SUP 98-018G. FLAPS FAILED AGAIN WHEN RETRACTING FROM 45 TO 30.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,015 hrs · 38,119 cycles

AEB STR 13L INTERCOSTAL CRACKED. REPLACED.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,015 hrs · 38,119 cycles

CARGO DOOR FWD SURROUND FRAME IS CRACKED IN THE RADIUS JUST BELOW THE FWD STOP UPPER FITTING. REPAIRED CARGO DOOR FWD SURROUND FRAME AT THE FWD UPER STOP FITTING IAW EA AWAC-CRJ252-01137 REV IR.

Part: FITTING — DAMAGED (TE FLAP) · airframe 41,015 hrs · 38,119 cycles

LEFT WING TRAILING EDGE FLAP ALIGNMENT FITTING DAMAGED. REPLACED FITTING IAW SUPP. 16-056.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 41,015 hrs · 38,119 cycles

CARGO DOOR PAN (FRAME) IS CRACKED. REPAIRED CARGO DOOR PAN IAW EA AWAC-CRJ253-01145 REV-IR .

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,015 hrs · 38,119 cycles

PAX DOOR LOWER SILL ANGLE CORRODED. REPLACED PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,015 hrs · 38,119 cycles

RIGHT FLOOR SILL CORRODED FROM FS 559.00+48 TO 559.00+80. REPAIRED RIGHT FLOOR SILL IAW REO601R-53-00-526 REV-- AND EA 253-01141.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,015 hrs · 38,119 cycles

FUSELAGE SKIN CRACKED, FS 235.00, STR 26R. REPAIRED SKIN IAW REO 601R-53-11-048 REV-D.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 41,015 hrs · 38,119 cycles

LEFT WING LEADING EDGE O/B, RIB CORRODED. REPLACED RIB IAW SRM 51-42-10, 51-42-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,015 hrs · 38,119 cycles

FLOORBEAM CAP CORRODED, FS569.00-621.00, LBL9. REPLACED CAP IAW REO 601R-53-61-3780 REV-A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,015 hrs · 38,119 cycles

CARGO DOOR FWD LOWER DOOR STOP BACKUP FITTING CRACKED. REPLACED FITTING IAW SRM 51-42-06, 51-42-21.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,015 hrs · 38,119 cycles

FLOORBEAM CAP CORRODED AT FS569.00 TO 621.00, LBL27. REPLACED CAP IAW SRM 51-42-06, 51-42-21, 51-42-22, REO 601R-53-00-005 REV-B.

Part: WEB — CRACKED (FUSELAGE) · airframe 41,015 hrs · 38,119 cycles

E&E BAY FLOOR WEB CRACKED, FS 193.00, LBL30. REPAIRED CRACK IAW REO 601R-53-11-111.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,015 hrs · 38,119 cycles

FS 621.00 FLOOR SUPPORT ANGLE AT LBL43 IS CRACKED. REPAIRED FS 621.00, LBL43 ANGLE IAW REO 601R-53-61-117 REV-E.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,015 hrs · 38,119 cycles

280 BEAM AFT ANGLE CORRODED BETWEEN LBL12 AND RBL12. REPAIRED ANGLE IAW REO 601R-53-11-926 REV-D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,015 hrs · 38,119 cycles

NLG WHEEL WELL GS 202.00 BULKHEAD RBL 9 VERTICAL POST O/B CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,015 hrs · 38,119 cycles

FS 559+80, RBL9 O/B FLOORBEAM CAP CORRODED. REPLACED BEAM CAP IAW REO 601R-53-00-005 REV-B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,015 hrs · 38,119 cycles

FS589, LBL45 CLIP UNDER CARGO DOOR FLOOR SILL IS CRACKED. REPLACED CLIP IAW SRM 51-42-06, 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,015 hrs · 38,119 cycles

AEB STR 14R OBLIQUE ANGLE CRACKED. REPLACED ANGLE IAW SRM 51-42-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,015 hrs · 38,119 cycles

AEB STR 16L INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,015 hrs · 38,119 cycles

AEB STR 14L INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,015 hrs · 38,119 cycles

AEB STR 15L INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 5142-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,015 hrs · 38,119 cycles

RT CABIN SIDE SEAT RAIL STICK 3 GOUGED AND CORRODED. REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,015 hrs · 38,119 cycles

RIGHT SIDEWALL SEAT TRACK NR 2 CORRODED. REPLACED RIGHT SIDEWALL SEAT TRACK NR 2 IAW AMM 53-01-11.

Part: BEAM — CUT (CARGO DOOR) · airframe 41,015 hrs · 38,119 cycles

CARGO DOOR BEAM HAS CUTS MADE BY ASSIST CABLES FWD AND AFT. REPLACED CARGO DOOR BEAM MEMBER IAW SRM 51-42-21.

Part: ATTACH BRACKET — CRACKED (COCKPIT) · airframe 41,015 hrs · 38,119 cycles

WINDSHIELD CENTER POST LOWER RIGHT ATTACH BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,015 hrs · 38,119 cycles

RIGHT FLOOR SEAT TRACK NR 3 CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 41,015 hrs · 38,119 cycles

CARGO DOOR INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,015 hrs · 38,119 cycles

PAX CABIN STA 280.00 AFT SIDE OF BULKHEAD AT STR 3L HAS 2 CRACKED CLIPS. REPLACED CLIPS IAW SRM 51-42-06, 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,015 hrs · 38,119 cycles

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

Part: BRACKET — CRACKED (FAIRING) · airframe 41,015 hrs · 38,119 cycles

FAIRING BRACKET CRACKED AT FS 461.00, RBL47. REPLACED BRACKET IAW SRM 51-42-06, 51-42-15.

Part: BRACKET — CRACKED (FAIRING) · airframe 41,015 hrs · 38,119 cycles

FAIRING BRACKET CRACKED AT FS449.85, RBL47. REPLACED BRACKET IAW SRM 51-42-06, 51-4215.

Part: BRACKET — CRACKED (FAIRING) · airframe 41,015 hrs · 38,119 cycles

FAIRING BRACKET CRACKED AT FS 468.00, LBL47. REPLACED BRACKET IAW SRM 51-42-06, 51-42-15.

Part: BRACKET — CRACKED (FAIRING) · airframe 41,015 hrs · 38,119 cycles

FAIRING BRACKET CRACKED AT FS 468.00, RBL47. REPLACED BRACKET IAW SRM 51-42-06, 51-42-15.

Part: SEAT TRACK — CORRODED (BS 364-409) · corrosion level 2 · airframe 41,015 hrs · 38,119 cycles

L/H SEAT TRACK STICK 2 CORRODED REMOVED AND REPLACED L/H SEAT TRACK STICK 2

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 41,015 hrs · 38,119 cycles

INTERCOSTAL CRACKED AT FS484.00, LBL33. REPAIRED INTERCOSTAL IAW REO601R-53-41-059 REV-B.

Part: ANGLE — CRACKED (BS 484) · airframe 41,015 hrs · 38,119 cycles

FS484 CLIP CRACKED AT RBL33. REPLACED CLIP IAW REO601R-53-41-059 REV-B.

Part: CHANNEL — CRACKED (CARGO DOOR) · airframe 41,015 hrs · 38,119 cycles

FWD CARGO DOOR TRACK LOWER U CHANNEL HAS MULTIPLE CRACKS. REPLACED CARGO DOOR FWD TRACK LOWER U CHANNEL IAW SRM 51-42-06. *SUPPLEMENTAL INFORMATION* (DIFFICULTY DATE YEAR ENTERED IN ERROR, CHANGED FROM 2018 TO 2019)

Part: UNKNOWN — ODOR (CABIN) · airframe 40,777 hrs · 37,893 cycles

EXHAUST SMELL FROM PACS DURING APU AND ENGINE OPERATIONS, SMELL SEEMS TO BE MORE PRONOUNCED AT FRONT OF A/C.

Part: WARNING MESSAGE — ILLUMINATED (NLG) · airframe 40,706 hrs · 37,838 cycles

AFTER GEAR RETRACTION, RECEIVED NWS CAUTION MESSAGE FOLLOWED BY A GEAR DISAGREE WARNING MESSAGE. GEAR DISAGREE APPEARED FOR APPROXIMATLEY 20 SECONDS. AFTER HANDLE MOVEMENT, HANDLE MOVED AFTER 30 SECONDS. NOSE GEAR SHOWED RED. DID NOT USE MANUAL RELEASE. ALL HYDRAULICS INDICATED NORMAL.

Part: CAP — MISSING (CABIN) · airframe 37,982 hrs · 35,307 cycles

END CAP MISSING FWD END OF EMER FLOOR TRACK LIGHTS.

Part: DOUBLER — CORRODED (FUSELAGE)

AFT CARGO BAY WATER LINE MOUNT DOUBLER CORRODED AT FS 605. R & R DOUBLER AT FS 605 IAW SRM 51-42-06 & 51-42-20.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,491 hrs · 34,844 cycles

FLOORBEAM 349 VERY OTBD FLANGE HAS CORROSION, JUST INBD & AFT OF THE SERVICE DOOR OPENING. PERFORMED REPAIR TO FS 349 FLOORBEAM AT THE VERY OTBD FLANGE IAW EA AWAC-CRJ253-00154.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,491 hrs · 34,844 cycles

RIGHT SIDE OF THE E & E BAY DOOR SURROUND STRUCTURE HAS SEVERAL CORROSION SPOTS, ON BOTH THE INBD & OTBD SIDES, 80% MATERIAL LOSE. R & R INTERCOSTAL AT E & E BAY DOOR, RT SURROUND STRUCTURE IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2

RIGHT SIDE OF THE E & E BAY DOOR SURROUND STRUCTURE HAS SEVERAL CORROSION SPOTS ON BOTH THE INBD & OTBD SIDES. R & R INTERCOSTAL AT E & E BAY DOOR RT SURROUND STRUCTURE IAW SRM 51-42-06 & 51-42-21.

Part: FITTING — CRACKED (FUSELAGE)

ANGLE CLIP IS CRACKED AT THE TOP, OTBD SIDE OF RBL 27 AT FS 484, IN CABIN.

Part: SHROUD — CRACKED (RT WING) · airframe 37,491 hrs · 34,844 cycles

RIGHT WING SHROUD ASSEMBLY CRACKED BETWEEN LE INBD 620JL & CTR 630JL. REPAIRED BY REPLACEMENT OF BRACKET IAW SRM 51-41-02.

Part: SHROUD — CRACKED (LT WING) · airframe 37,491 hrs · 34,844 cycles

LEFT LE SHROUD ASSEMBLY CRACKED IN TWO PLACES BETWEEN INBD LE PANEL 520JL & 530JL. REPLACED IAW SRM 51-42-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 37,491 hrs · 34,844 cycles

BATH TUB FITTING IS CRACKED AT THE OTBD SIDE OF RBL 9, JUST AFT OF FLOORBEAM AT FS 461, IN CABIN.

Part: UNKNOWN — ODOR (CABIN) · airframe 37,344 hrs · 34,699 cycles

FLIGHT 3768, BURNING ELECTRICAL ODOR OVER ROW 12 DF, NOTICED OVERHEAD LIGHT BURNT OUT. INSPECTED & VERIFIED, NO FURTHER OR CURRENT BURNING ELECTRICAL ODOR EXISTS AT THIS TIME. ALSO FOUND NO ABNORMAL BURN INDICATIONS OR BURNED OUT LIGHT BULBS, ACFT OK FOR SERVICE.

Part: OVERHEAT LOOP — OUT OF ADJUST (LT JET PIPE) · airframe 36,927 hrs · 34,295 cycles

CONTINUOUS LEFT JET OVERHEAT CAUTION INFLIGHT. ENGINE INDICATIONS NORMAL. ADJUSTED TERMINAL ENDS FOR LEFT JET PIPE LOOP A IAW AMM 26-11-04. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 36,479 hrs · 33,860 cycles

FUEL ODOR IN COCKPIT WITH APU & PACKS SELECTED ON.

Part: LINE — LEAKING (APU FUEL) · airframe 36,474 hrs · 33,856 cycles

STRONG FUEL ODOR COMING FROM PACKS WHEN OPERATING FROM APU AIR. FOUND APU P3 SENSOR AIRLINE & FUEL CONTROL UNIT LINE CRACKED. OPERATED PACKS, NO FUEL ODOR NOTED.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 36,155 hrs · 33,566 cycles

FLOOR EMERGENCY LIGHT COVER AT 1D IS CRACKED & END CAP IS MISSING.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZ STAB) · airframe 35,330 hrs · 32,781 cycles

CLIMBING OUT OF 12,000 FT & 290KTS WITH THE AUTOPILOT ON, RECEIVED STAB & MACH TRIM CAUTION MSG AT THE AUTOPILOT. DISCONNECTED, RAN QRH & WERE ABLE TO RE-ENGAGE THE STAB & MACH TRIM, AS SOON AS WE TRIED TO TRIM THE ACFT THE STAB & MACH TRIM DISENGAGED.

Part: FLAP — FAILED (WING) · airframe 34,800 hrs · 32,272 cycles

FLAPS FAIL CAUTION MSG ON APPROACH. FAILED AT 20 DEGREE DETENT. COMPLIED WITH QRH.

Part: QUICK DISCONNECT — DISCONNECTED (NR 3 BRAKE) · airframe 33,324 hrs · 30,868 cycles

3854, RIGHT INBD BRAKE IS STICKING. BTMS SHOWS 14 FOR THAT BRAKE. ALL OTHER INDICATORS NORMAL, COMPLIED WITH QRH. FOUND NR 3 FUSE BLOWN. R & R NR 3 & NR 4 MLG TIRE ASSEMBLIES IAW AMM 32-41-01. VERIFIED SPACER & WASHER INSTALLED. FOUND NR 3 BRAKE QD DISCONNECTED. RECONNECTED QD & SPUN TIRE, TIRE SPINS FREELY. INSPECTED NR 3 BRAKE NO DISCOLORATION OR OTHER DEFECTS NOTED COMPLIED WITH TIRE BURST INSPECTION.

Part: COALESCER BAG — ODOR · airframe 32,837 hrs · 30,374 cycles

BURNING ODOR COMING FROM GASPERS MAINLY IN CABIN. NO SMOKE OR FLAME NOTED. R & R LT AND RT COALESCER BAGS IAW AMM 21-51-13.

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 32,837 hrs · 30,374 cycles

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

Part: UNKNOWN — ODOR (CABIN) · airframe 32,830 hrs · 30,369 cycles

AFTER ROTATION, A BURNING SMOKEY ODOR. ODOR WORSE WITH POWER CHANGES. PERFORMED ENGINE RUN AND RAN THRU DIFFERENT POWER LEVELS, PERFORMED OPS CHECK OF ACFT SYS IAW AMM 21-51-00. ALSO PERFORMED PACK BURN IAW SUPP 09-037A. OPS CHECKED GOOD. COULD NOT DUPLICATE.

Part: TORQUE TUBE — CORRODED (PAX DOOR) · airframe 32,837 hrs · 30,374 cycles

PAX DOOR UPPER TORQUE TUBE STOP LEVER IS CORRODED. REMOVED CORRODED STOP FITTING AND REPLACED WITH NEW.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,837 hrs · 30,374 cycles

RIGHT INBD FLAP VANE HAS DAMAGE ON OTBD CENTER AND R/B LEADING EDGES. BLENDED CENTER L/E TO SMOOTH CONTOUR R & R R/O AND OTBD L/E SECTION IAW REO 601R-57-52-004, REV D SRM 51-40-11, 51-21-11, 51-23-00, 51-24-16, 51-25-06, 51-25-16, 51-42-13.

Part: SKIN — CHAFED (RT AILERON) · airframe 32,837 hrs · 30,374 cycles

RIGHT AILERION UPPER L/E IS CHAFED ON INBD CENTER & OTBD AREAS. R & R RT AILERION UPPER L/E WITH NEW SERVICEABLE L/E, PN 601R-13031-166 IAW SRM 51-42-06, 51-42-13, REO 601R-57-60-013, REV A.

Part: SKIN — CORRODED (BS 333) · corrosion level 2 · airframe 32,837 hrs · 30,374 cycles

CORROSION FOUND ON FRAME 333 BETWEEN STR 25L & 25R BEYOND LIMITS. SPLICED IN NEW SECTION OF FRAME IAW STS EA 15-2013-373.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,837 hrs · 30,374 cycles

FS 280 FWD FLOORBEAM ANGLES CRACKED. R & R FS 280 RBL 9 & LBL 9 FLOORBEAM ANGLES IAW REO 601R-53-11-136, REV A & REO 601R-53-11-171, REV D.

Part: CARGO TRACK — CORRODED (BS 559-574) · corrosion level 2 · airframe 32,837 hrs · 30,374 cycles

CARGO TRACK LBL 27 AT FS 574-559+96 HAS CORROSION. R & R CARGO TRACK IAW SRM 51-41-02.

Part: CARGO TRACK — CORRODED (BS 559-621) · corrosion level 2 · airframe 32,837 hrs · 30,374 cycles

CARGO TRACK LBL 9 FS 621-559+112 CORRODED. BLENDED CORROSION AND FOUND TO BE WITHIN THE LIMITS IAW SRM 53-61-49, R & R CARGO TRACK IAW SRM 51-41-02.

Part: SEAL — CRACKED (SPOILER) · airframe 32,837 hrs · 30,374 cycles

RIGHT FLIGHT SPOILER CENTER SPRING SEAL CRACKED. R & R SEAL IAW SRM 51-42-06 AND 51-42-21.

Part: RIB — CRACKED (LT MLG WW) · airframe 32,837 hrs · 30,374 cycles

LEFT WHEEL WELL BATTERY RIB DRAG ANGLE IS CRACKED. REMOVED UNSERVICEABLE DRAG ANGLE AND INSTALLED SERVICEABLE DRAG ANGLE ON LT WHEEL WELL BATTERY RIB.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 32,837 hrs · 30,374 cycles

RIGHT WHEEL WELL BATT RIB DRAG ANGLE CRACKED. REPLACED RT WHEEL WELL BATTERY RIB DRAG ANGLE WITH SERVICEABLE DRAG ANGLE IAW SRM 52-42-21, 51-40-11, 50-42-21, 51-23-00, 51-25-16.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · corrosion level 2 · airframe 32,837 hrs · 30,374 cycles

RT FLOOR SUPPORT CORRODED FS 621 - 559+96. BLENDED IAW REO 601R-53-00-526, FOUND OUT OF LIMITS. R & R FLOOR SUPPORT.

Part: BRACKET — CRACKED (WINDSHIELD) · airframe 32,837 hrs · 30,374 cycles

RT WINDSHIELD SIDE POST SUPPORT BRACKET IS CRACKED. REPLACE PART.

Part: ANGLE — CRACKED (BS 484) · airframe 32,837 hrs · 30,374 cycles

INTERCOSTAL ANGLE CRACKED AT FS 484, RBL 27. REMOVED & REPLACED INTERCOSTAL ANGLE.

Part: THRESHOLD — CORRODED (BS 319-349) · corrosion level 2 · airframe 32,837 hrs · 30,374 cycles

SERVICE DOOR THRESHOLD & SHIM ARE CORRODED & UNSERVICEABLE. R & R THRESHOLD PLATE AND SHIM.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 32,837 hrs · 30,374 cycles

CORRODED SEAT TRACK AT RBL 9, FS 559+80. REMOVED AND REPLACED NEW SEAT TRACK.

Part: BPSU — FAILED (RT TE FLAPS) · airframe 32,676 hrs · 30,227 cycles

FLAPS FAIL CAUTION MESSAGE, RESET IAW SUPP 98-018F, FLAPS FAILED DURING 4TH CYCLE OF FLAPS . R & R RT BPSU IAW AMM 27-51-10. OPS CHECKED GOOD.

Part: ENGINE — MALFUNCTIONED · airframe 31,014 hrs · 28,634 cycles

AT 12,000 FEET IN CRUISE AIRCRAFT STARTED TO VIBRATE WITH INCREASING FREQUENCY AND INTENSITY OVER A PERIOD OF APPROXIMATELY 5-10 SECONDS, FOLLOWED BY UNCOMMANDED ENGINE SHUTDOWN. NO INDICATION OF A FIRE OR OVERTEMP. DIVERTED TO CAE. SINGLE ENGINE LANDING WAS UNEVENTFUL. REMOVED AND REPLACED ENGINE (S/N 950010) AND AWAITING FURTHER ANALYSIS. FINDINGS SO FAR SHOW NO TEMPERATURE SPIKE OR ENGINE EXCEEDANCE AND NO INDICATION OF ENGINE OIL LOSS. CHIP LIGHT WAS ON. CHIPS SENT OUT FOR ANALYSIS. ENGINE GEARBOX SCHEDULED FOR BOROSCOPE.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 30,771 hrs · 28,399 cycles

LAV BURNING SMELL NOTICED. REMOVED AND REPLACED BALLAST ASSY AND ALL LAMPS. ALSO REPAIRED GROUND TERM. SYS TEST OK PER AMM 33-25-07. NO SMELL AFTER TEST.

Part: POWER UNIT — FAULTY (LAVATORY) · airframe 30,756 hrs · 28,385 cycles

STRONG BURNING SMELL EMITTING IN REAR OF A/C STRONGEST NEAR LAV. FOUND LAV LIGHT POWER UNIT BURNT. REMOVED AND REPLACED POWER UNIT REF CRJ AMM 33-25-07. OPS CHECKS GOOD AT THIS TIME. STRONG SMELL DISSIPATED.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 27,976 hrs · 25,521 cycles

LT INBD FLAP VANE L/E IS CHAFED IN 3 PLACES. REPAIRED IAW REO 601R-57-52-004.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 27,976 hrs · 25,521 cycles

RT INBD FLAP VANE L/E ARE CHAFED IN 3 PLACES. REPAIRED IAW REO 601R-57-52-004.

Part: ATTACH FITTING — BROKEN (BS 640) · airframe 27,976 hrs · 25,521 cycles

ATTACH FITTING BROKEN FOR 10TH STAGE BLEED LINE ON ENG BEAM RT SIDE TOP. R & R FITTING IAW SRM 51-42-11.

Part: BRACKET — CHAFED (BS 559) · airframe 27,976 hrs · 25,521 cycles

BRACKET APPROX FS 559+112 RT SIDE, JUST AFT OF SIDE SEAT RAIL HAS A HOLE CHAFED THROUGH. R & R BRACKET FS 559.0+112 RT SIDE, AFT OF SIDE SEAT RAIL IAW SRM 51-11-20.

Part: INTERCOSTAL — DENTED (BS 589) · airframe 27,976 hrs · 25,521 cycles

CARGO BEAM INTERCOSTAL AT LBL 27 BETWEEN BS 589-605, DENTED. R & R INTERCOSTAL IAW SRM.

Part: ANGLE — WORN (RT PYLON) · airframe 27,976 hrs · 25,521 cycles

DIVIDER GUIDE ON PANEL 422BT WORN. R & R DIVIDER GUIDE ANGLE WITH SERVICEABLE PN 601-37003-184 IAW SRM 51-42-06.

Part: BULKHEAD — CHAFED (BS 280) · airframe 27,976 hrs · 25,521 cycles

BULKHEAD BS 280 AFT SIDE IS CHAFED, RT SIDE BEHIND GALLEY. REPAIRED CHAFE DAMAGE ON 280 IAW 601R-53-11-1727.

Part: CARGO TRACK — CORRODED (BS 559-755) · airframe 27,976 hrs · 25,521 cycles

CARGO TRACK CORRODED TO CONTAIN EXFOLIATION CORROSION AROUND COUNTERSUNK SCREWS. R & R WITH SERVICEABLE CARGO TRACK.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 27,976 hrs · 25,521 cycles

RT NR 4 FLOOR SEAT TRACK CORRODED. R & R SEAT TRACK.

Part: STRUCTURE — CHAFED (RT NACELLE) · airframe 27,976 hrs · 25,521 cycles

RT ENGINE LOWER NOSE COWL AFT EDGE IS KNIFE EDGED. R & R AFT EDGE STRIP IAW CMM 71-14-01, REPAIR.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 27,976 hrs · 25,521 cycles

CRACKED INTERCOSTAL IN PAX DOOR PANEL 832BR AREA. REMOVED CRACKED PAX DOOR INTERCOSTAL AT 832 BR PANEL THEN INSTALLED NEW INTERCOSTAL AT 832 PANEL IAW SRM 51-40-11, 51-42-06.

Part: SEAT TRACK — CORRODED (BS 364) · corrosion level 2 · airframe 27,976 hrs · 25,521 cycles

LT NR1 SEAT TRACK HAS CORROSION AT FWD EDGE. R & R WITH A SERVICEABLE SEAT TRACK PIECE. LOCATED AND INSTALLED.

Part: SEAT TRACK — CORRODED (BS 399) · corrosion level 2 · airframe 27,976 hrs · 25,521 cycles

RT SEAT TRACK HAS EXFOLIATION CORROSION AT FWD EDGE. REMOVED UNSERVICEABLE RT SEAT TRACK, FABRICATED, LOCATED AND INSTALLED REPLACEMENT SEAT TRACK, STOCK PN N126-2075.

Part: ANGLE — CRACKED (BS 621) · airframe 27,976 hrs · 25,521 cycles

LEFT BS 621 OBLIQUE ANGLE CRACKED, R & R.

Part: BULKHEAD — CRACKED (BS 202) · airframe 27,976 hrs · 25,521 cycles

FS 202, BULKHEAD CRACKED AT PARKING BRAKE CABLE HOLE. REPAIRED FS 202 BULKHEAD CRACK AT PARKING BRAKE CABLE HOLE BY FULLY INCORPORATING REO 601R-53-11-563, REV A.

Part: SKIN — CHAFED (RT AILERON) · airframe 27,976 hrs · 25,521 cycles

RT AILERON LWR FIXED L/E INBD END IS CHAFED. REPAIRED IAW REO 601R-57-60-020.

Part: HINGE — GOUGED (PAX DOOR) · airframe 27,976 hrs · 25,521 cycles

PAX DOOR HINGE HALF MOUNTED FUSELAGE HAS SEVERAL GOUGES. BLENDED GOUGES ON PAX DOOR HINGE HALF OF FUSELAGE IAW SRM 51-12-00 FOUND TO BE WITHIN LIMITS IAW REO 601R-53-21-814.

Part: SKIN — CHAFED (LT AILERON) · airframe 27,976 hrs · 25,521 cycles

LT AILERON UPPER AND LOWER L/E SKIN IS CHAFED BY THE RUB SEALS. BLENDED OUT MINOR CHAFTING TO UPPER AND LOWER AILERON L/E IAW REO 601R-52-60-013 AND SRM 51-12-00. RESTORED FINISH BY ALODINE IAW SRM 51-21-11, FR PRIME IAW SRM 51-25-06 AND TOP COAT IAW SRM 51-25-16.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 27,976 hrs · 25,521 cycles

CRACKED INTERCOSTAL IN UPPER PAX DOOR NEAR HINGE IN AREA OF PANEL 832GL. GL THEN LOCATED AND INSTALLED NEW SERVICEABLE INTERCOSTAL. REMOVED CRACKED INTERCOSTAL IN UPPER FWD AREA AT PANEL 832.

Part: STIFFENER — CRACKED (RT EXHAUST) · airframe 27,976 hrs · 25,521 cycles

RT JET PIPE FAIRING HAS CRACKED STIFFENER. REMOVED UNSERVICEABLE STIFFENER ON RT JET PIPE FAIRING IAW CMM 20-421-06. LOCATED AND DRILLED SERVICEABLE STIFFENER IAW CMM 20-40-11 INSTALLED SERVICEABLE STIFFENER ON RT JET PIPE IAW CMM 20-42-06.

Part: WARNING MESSAGE — ILLUMINATED (STATIC HEAT) · airframe 26,668 hrs · 24,187 cycles

RT STATIC HEAT MSG RECEIVED IN FLIGHT, C/W`D QRH AND MESSAGE REMAINED. PERFORMED RESET PROCEDURE IAW FIM 30-30-00. OPS CK GOOD.

Part: CONTROL COLUMN — BINDING (AILERONS) · airframe 26,482 hrs · 23,998 cycles

AILERONS BINDING AND AUDIBLE SNAP SOUND DURING FLIGHT CONTROL CHECK. BOTH CONTROL COLUMNS AND BOTH DIRECTIONS. LT COLUMN BINDING AT LT DEFLECTION, RT COLUMN BINDING MID AND 1/2 DEFLECTION. C/W PARA 4 OF GREO 601R-27-11-031 "DISPOSITION FOR ACFT DISPATCH. REWORK" CLICKING APPEARS TO COME FROM CAPT SIDE CONTROL WHEEL SHAFT INTERFACE. LOOSENED NUT AND RETORQUED TO 550 INCH LBS CLICKING NOISE STILL PRESENT. REPAIR REQUIRED IAW GREO 27-11-031 DUE TO CLICKING/NOISE FEELING COMING FROM AILERON CONTROL WHEELS. REPAIR MUST BE C/W WITHIN 500 FLT HRS.

Part: WARNING MESSAGE — ACTIVATED (AC BUSS) · airframe 25,597 hrs · 23,074 cycles

AFTER LANDING, AC BUSS 1 FAILED FOLLOWED BY AC AUTO TRANSFER FAIL FOLLOWED BY ALL ASSOCIATED NR 1 AC BUSS SYSTEM FAILUE MESSAGES. CHECKED ALL CONTACTORS-NO LOOSE WIRES. C/W OPS CKS OF A/C GENERATORS SYS IAW AMM 24-20-00, OPS CK GOOD.

Part: NONE — NONE · airframe 25,518 hrs · 22,991 cycles

FLIGHT CONTROLS FELT VERY "MUSHY" WITH A LOT OF SLACK BETWEEN YOKE INPUTS AND PLANE REACTION. UNRESPONSIVENESS OCCURRED IN BOTH PITCH AND ROLL INPUTS FROM BOTH CAPTAINS AND F/O YOKES. INSPECTED FLT CONTROL SYS IAW 27-31-00. NO FAULTS FOUND ALL WORK DONE ON W/O 157375.

Part: DISPLAY — FAILED (COCKPIT) · airframe 25,124 hrs · 22,581 cycles

WALKED ONTO ACFT, BATTERY SWITCH WAS ON. COCKPIT SMELLED OF ELECTRONICS OVERHEATING AND RED DISPLAY MESSAGE SAYING " DISPLAY TEMP" ON ED1 AND ED2 ILLUMINATED. IMMEDIATELY SHUT BATTERY OFF. R & R EFD3 AND EFD4 IAW AMM 31-61-01. OPS CK GOOD.

Part: BATTERY — ACTIVATED · airframe 25,124 hrs · 22,581 cycles

WALKED ONTO ACFT, BATTERY SWITCH WAS ON. COCKPIT SMELLED OF ELECTRONICS OVERHEATING AND RED DISPLAY MESSAGE SAYING "DISPLAY TEMP" ON ED1 AND ED2 ILLUMINATED. IMMEDIATELY SHUT BATTERY OFF. OPEN

Part: O-RING — LEAKING (LT ENGINE) · airframe 25,008 hrs · 22,467 cycles

AT CRUISE, LOW OIL PRESS MASTER WARNING MSG C/W QRH. LT ENG AT IDLE, OIL PRESS APPROX 30 PSI. REPLACED OUTER O-RING ON LT IDG CARBON SEAL AND CARBON SEAL IAW SUP 05-018C & AMM 24-11-01 REF W/C NR 2 FOR LEAK CHECK.

Part: WIRE HARNESS — DEFECTIVE (RT MLG) · airframe 24,818 hrs · 22,276 cycles

RT MAIN GEAR DISAGREE WARNING AFT TAKEOFF. RT MLG DID NOT RETRACT, COMPLIED WITH QRH. WO NR 153271, CARDS 1-6 AND 13-18. R & R RT INBD MLG HARNESS IAW SUPP 09 062B ALSO FOUND RT MLG UPLOCK TAT LOOSE RESECURED 32 32. OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 23,797 hrs · 21,232 cycles

PRESSURIZATION PROBLEM. RAPID DEPRESSURIZATION, CAUSING FIRST A CABIN PRESSURE CAUTION FOLLOWED BY A CABIN PRESSURE WARNING IN RAPID SUCCESSION.

Part: ANGLE — CRACKED (BS 559) · airframe 23,552 hrs · 20,994 cycles

PRESSURE BULKHEAD CAP ANGLE IS CRACKED IN THE RADIUS. FS 559, RBL 18. CRACK LENGTH IS .350" ANDWEB CRACKED AT FS 669 BTWN RBL 9 TO 18 CRACK LENGTH .520:. PRESSURE BULKHEAD STRUCTURE FS 559, RBL 9 TO RBL 18. REPAIRED IAW REO 601R-53-41-260, REV C AND REO 601R-53-41-609, REV A, DEVIATION D. (K)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 23,552 hrs · 20,994 cycles

CORROSION ON INTERNAL SURFACE OF LT WING L/E 520ML. CORROSION REMOVED IAW SRM 51-21-06 ON L/E 520ML. (K)

Part: VANE — DENTED (LT WING TE FLAP) · airframe 23,552 hrs · 20,994 cycles

DENT ON LT WING, INBD FLAP VANE L/E BTWN WS 75.27 TO WS 97.70 LT WING, INBD FLAP VANE L/E REPAIRED IAW SRM 57-52-00, PAGE 201. DUE TO DENT FOUND OUT OF LIMITSIAW SRM 57-52-00, FIG 101 (PAGE 102) REPAIR NR 01. (K)

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 23,552 hrs · 20,994 cycles

RT HORIZONTAL STAB L/E DAMAGED BY FOD AT RBL 18.91. CRACK LENGTH 0.500", SKIN DEPRESSION: 0.250" RT HORIZ STAB L/E REPAIRED IAW SRM 55-12-01, PAGE 201 TO 206. (K)

Part: SKIN — CORRODED (BS 280-559) · airframe 23,552 hrs · 20,994 cycles

CORROSION FOUND ON SKIN AT MANY PLACES BTWN FS 280.00 AND FS 559+80 AND BTWN LT AND RT STRINGER 6. CORROSION REMOVED IAW SRM 51-21-06. (K)

Part: HOUSING — CRACKED (E/E DOOR HANDLE) · airframe 23,552 hrs · 20,994 cycles

MAIN AVIONICS COMPARTMENT DOOR, HANDLE HOUSING CRACKED. HANDLE HOUSING REPLACED IAW SRM 51-42-06.

Part: SILL — CORRODED (BS 319-349) · corrosion level 2 · airframe 23,552 hrs · 20,994 cycles

CORROSION ON LWR SILL ANGLE OF SERVICE DOOR SURROUND BTWN FS 319 TO FS 349.00 AND STR 18 SERVICE DOOR SURROUND, LWR SILL ANGLE PN 601R38303-253. REPLACED IAW SRM 51-42-06 AND SRM 51-42-21. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 23,552 hrs · 20,994 cycles

INTERCOSTAL FS 484 UNDERFLOOR CRACKED AT RBL 27 AND RBL 36. (CRACK LENGTH 0.500") INTERCOSTAL FS 484 UNDER FLOOR AT RBL 27 AND RBL 36 REAPIRED IAW REO 601R-53-41-059, REV A. (K)

Part: CROSSBEAM — CORRODED (BS 349) · corrosion level 2 · airframe 23,552 hrs · 20,994 cycles

CORROSION ON UPPER FLANGE OF CROSSBEAM AT FS 349 AND RBL 45. CORROSION REMOVED IAW REO 601R-53-21-1047.

Part: FITTING — CRACKED (AFT BULKHEAD) · airframe 23,552 hrs · 20,994 cycles

CRACK ON REAR PRESSURE BULKHEAD WEB AT LINTEL FITTING CRACK LENGTH .500. REAR PRESSURE BULKHEAD WEB AT LINTEL FITTING REPAIRED IAW REO 601R-53-61-1230, REV D. (K)

Part: RIB — CORRODED (RT WING) · airframe 23,552 hrs · 20,994 cycles

RT WING OTBD RIB AFT UPPER FLANGE VIA PANEL 640BT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-2006. (K)

Part: SILL — CORRODED (BS 310-349) · corrosion level 2 · airframe 23,552 hrs · 200,994 cycles

PASSENGER ENTRY, LOWER SILL CORRODED. LWR SILL REPLACED IAW SRM 51-42-06 AND REO 601R-52-11-577. (K)

Part: ACCESS PANEL — CORRODED · corrosion level 1 · airframe 23,552 hrs · 20,994 cycles

CORROSION AROUND SCREW HOLES ON INTERNAL SIDE OF ACCESS PANEL 650KB ON INTERNAL SIDE OF ACCESS PANEL 650KB, CORROSION AROUND SCREW HOLES REMOVED IAW SRM 51-21-06 WITHIN LIMIT IAW SRM 51-21-00. (K)

Part: CROSSBEAM — CRACKED (BS 280) · airframe 23,552 hrs · 20,994 cycles

FOUR CLIPS CRACKED ON CROSSBEAM FS 280 AT LBL 9 AND RBL 9. FOUR CLIPS REPLACED ON CROSSBEAM FS 280 AT LBL 9 AT RBL 9 IAW SRM 51-42-21 AND SRM 51-42-06. CLIP AT FS 280, RBL 9 OTBD SIDE REPLACED IAW REO 601R-53-11-171, REV D. (K)

Part: ANGLE — CRACKED (BS 559) · airframe 23,552 hrs · 20,994 cycles

PRESSURE BULKHEAD CAP ANGLE IS CRACKED IN THE RADIUS FS 559.00, LBL18, CRACK LENGTH .350" PRESSURE BULKHEAD CAP ANGLE REPAIRED IAW REO 601R-53-41-260, REV C. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,552 hrs · 20,994 cycles

FLOORBEAM LWR FLANGE CRACKED AT FS 280, RBL 9, CRACK LENGTH 1.20". REPAIR PERFORMED IAW REO 601R-53-11-171, REV D. ANGLE FILLER FABRICATED IAW REO 601R-53-11-171, REV D. (K)

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 1 · airframe 23,552 hrs · 20,994 cycles

CORROSION AT FUEL ACCESS PANEL HSG 550AB IN NON CRITICAL REGION. CORROSION REMOVED IN NON CRITICAL REGION AT FUEL ACCESS PANEL 550AB IAW EOE06/021/457, REV A AND REO 601R-57-21-030, REV 6. (K)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 1 · airframe 23,552 hrs · 20,994 cycles

CORROSION AT FUEL ACCESS PANEL HSG 640EB IN NON CRITICAL REGION. CORROSION REMOVED IN NON CRITICAL REGION AT FUEL ACCESS PANEL 640EB IAW EO E06/021/457 REV A AND REO 601R-57-21-030. (K)

Part: PLATE — CORRODED (BS 574-621) · corrosion level 1 · airframe 23,552 hrs · 20,994 cycles

CARGO DOOR NET TIE DOWN STRUCTURE (PLATES) (3X) UPPER SURFACE BTWN FS 621 AND FS 574 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-06. (K)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 23,552 hrs · 20,994 cycles

REPLACEMENT OF FWD UPPER CORNER COVER (PAX DOOR) DUE TO CRACK FOUND DURING INCORPORATION OF EO E07/027/452, REO 601R-52-11-827 AND REO 601R-52-11-159, REV B. FWD UPPER CORNER COVER OF PAX DOOR REPLACED IAW SRM 51-42-13. (K)

Part: RIB — CORRODED (LT WING) · corrosion level 1 · airframe 23,552 hrs · 20,994 cycles

LT WING L/E RIBS AT WS 139.54, WS 149.58, WS 247.95 AND WS 252.87 FRETTING CORROSION FOUND. CORROSION REMOVED ON LT WING, L/E RIBS IAW SRM 51-21-06. (K)

Part: SILL — CRACKED (BS 589) · airframe 23,552 hrs · 20,994 cycles

CARGO DOOR FLOOR SILL LANDING PLATE CRACKED AT FS 589.00 RIVET HOLE. GARGO DOOR FLOOR SILL LANDING PLATE REPAIRED AT FS 589.00 RIVET HOLE IAW REO 601R-53-61-433 REV NC. (K)

Part: WIRE HARNESS — OUT OF POSITION (DOOR PROX) · airframe 23,004 hrs · 20,460 cycles

ON INITIAL CLIMBOUT APPROX 2000 FT "PAX DOOR OUT HANDLE" CAUTION MESSAGE APPEARED. WHILE COMPLYING WITH QRH PAGE 3, PAX DOOR WOAR MESSAGE APPEARED. QRH FOR PAX DOOR MESSAGE, LANDED AT NEAREST SUITABLE AIRPORT. LANDED OVERWEIGHT APPROX 50K LBS. UNABLE TO DUPLICATE WARNINGS, INSPECTED DOOR NO DEFECTS NOTED, INSPECTED PROXIMITY SWITCH NO DEFECTS NOTED, ACFT NO DEFECTS PSEU FAULTED DOOR PROX SWITCH, SHOWED OPEN WHEN CLOSED. DOOR PHYSICALLY OPERATES OK BUT INDICATIONS ARE INOP. PSEU SHOWS A FAULTY PSI MB + PS2MB, ADJUSTED AND REROUTED WIRE HARNESS PROX SWITCHES. OPS CHECK GOOD, IAW AMM 52-70-04. (K)

Part: ANGLE — CRACKED (BS 621) · airframe 22,860 hrs · 20,317 cycles

MWC 136500-10- CARGO DOOR CAMTRACK CROSSMEMBER, LOWER ANGLE AT AFT BULKHEAD CRACKED. LOWER ANGLE AT CARGO DOOR CAMTRACK CROSSMEMBER FABRICATED IAW SRM 51-24-36 AND INSTALLED IAW SRM 51-42-21. (K)

Part: LINE — DAMAGED (HYD SYSTEM) · airframe 22,690 hrs · 20,147 cycles

IN CRUISE, HYD 1 LOW PRESSURE CAUTION MESSAGE. PERFORMED QRH. DIVERTED, ENGINE DRIVEN PUMP RAN APPROX 1 HOUR AND 5 MIN AT 0 PSI, QUANTITY 0. SWEDGED AND REPAIRED DAMAGED NR 1 HYD PRESSURE LINE FOR EXTERNAL HYD POWER IAW AMM 20-22-00. OPS CHECK GOOD AND LEAK CK GOOD. (K)

Part: CHECK VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 22,648 hrs · 20,101 cycles

LT PACK HI TEMP AFTER EXITING RUNWAY ALL TEMP IND NORMAL. BURNING ODOR IN COCKPIT. UPON BOARDING ACFT, OBSERVED NO BURNING ODOR. STARTED APU AND SELECTED RT PACK ON, INSP CB`S INSTRUMENTS AND COCKPIT LIGHTING, VERIFIED WINDOW HEAT AND FANS OP NORMAL. SELECTED LT PACK ON AND RECEIVED LT PACK HIGH TEMP. REPLACED LT FAN BYPASS CHECK VALVE IAW AMM. OPS CHECK GOOD. (K)

Part: TIRE — FAILED (MLG) · airframe 22,648 hrs · 20,101 cycles

190919 - NR 3 MAIN TIRE BLOW/SHREDDED FWD ON POST FLIGHT, RT INBD FLAP AND BUTE DOOR SHOW DAMAGE FROM TIRE DEBRIS. INSPECTED RT INBD FLAP AND ACFT FLAP DAMAGE FOUND TO BE OUT OF LIMITS REF BUT 2+3+4. REF 190919/1 RT INBD FLAP LOWER SURFACE HAS 4 DENTS NO LOOSE RIVETS, NO CRACKS NO CREASES, FLAPS OPERATE NORMALLY MAX DEPTH 404 INCHES. RT INBD FLAP WAS REPLACED. (K)

Part: PSU — DETACHED (ROW 8A&C) · airframe 19,837 hrs · 17,414 cycles

PSU AND OXYGEN MASK UNIT DETACHED FROM ROW 8A AND C. RESECURED PSU, COMPLIED WITH OPS CHECK OF PSU ABOVE SEATS 8A AND 8C, OPS CHECK GOOD IAW AMM 25-20. PSU PROPERLY INSTALLED AT THIS TIME. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

RECEIVED SMOKE CARGO WARNING DURING TAXI OUT, MESSAGE LIT FOR 5 SECONDS AND EXTINGUISHED RAMP INSPECTED CARGO BAY AND FOUND NO EVIDENCE OF SMOKE AND FIRE. DEACTIVATED BOTH CARGO SMOKE DETECTORS IAW AMM 26-15-00-040-801. (M)

Part: DUCT — CRACKED (APU) · airframe 17,339 hrs · 15,014 cycles

INSPECTED APU AND FOUND UPPER AND LOWER INTAKE DUCTS CRACKED BEYOND LIMITS IAW AMM 49-14-01. REMOVED AND REPLACED UPPER AND LOWER APU INTAKE DUCTS. OPERATIONAL CHECK GOOD IAW 49-52-01. UPPER DUCT, TSN 7728, LOWER DUCT, TSN 11740. (K)

Part: DUCT — CRACKED (APU) · airframe 17,339 hrs · 15,014 cycles

INSPECTED APU AND FOUND UPPER AND LOWER INTAKE DUCTS CRACKED BEYOND LIMITS IAW AMM 49-14-01. REMOVED AND REPLACED UPPER AND LOWER APU INTAKE DUCTS. OPERATIONAL CHECK GOOD IAW 49-52-01. UPPER DUCT TSN = 7728, LOWER DUCT TSN = 11740.

Part: COVER — DISLODGED (OXYGEN MASK) · airframe 16,830 hrs · 14,537 cycles

OXYGEN MASKS COVERS FELL FROM SEATS 4 AND 5 (A) AND (C). RESECURED PSU COVERS AT SEATS 4 AND 5 IAW AMM. (K)

Part: IDG — UNDERSERVICED (ENGINE) · airframe 15,135 hrs · 12,925 cycles

ON DEPARTURE IDG NR2 ILLUMINTED AND CLEARED (IDG NR 1 ALREADY ON MEL). SERVICED IDG NR 2 IAW AMM. OPS CHECK GOOD. NO LEAKS NOTED. (K)

Part: RHEOSTAT — FAULTY (FLOOD LIGHT) · airframe 14,185 hrs · 12,051 cycles

WHEN F/O SELECTED FLOOD LIGHTS ON, SMOKE ERUPTED FROM BEHIND SW PANEL FLOOD LABEL DSTLA ON FO`S SIDE PANEL AND CBP3 C1 POPPED AND WAS NOT RESET. INSPECTED AND FOUND FO`S FLOOD LIGHT RHEOSTAT FAULTED. NO OTHER SYS AFFECTED. (K)

Part: VANE — WORN (RT TE FLAP)

RIGHT OUTBOARD FLAP VANE, OUTBOARD FLAP VANE FITTING WORN EVEN WITH LEADING EDGE OF VANE .030 INCH IS MINIMUM CLEARANCE ALLOWED PER BOMBARDIER, INC REO 601R-57-53-195. REMOVED OLD VANE FITTING FROM RIGHT OUTBOARD FLAP AS WS 296.073 AND INSTALLED NEW VANE FITTING P/N 601R14560-6 IAW BOMBARDIER, INC REOS 601R-57-53-019 AND 601R-57-53-195. (M)

Part: VANE — WORN (RT TE FLAP) · airframe 13,573 hrs · 11,501 cycles

RT OB FLAP VANE, OB FLAP VANE FITTING WORN EVEN WORN LEADING EDGE OF VANE .030 INCH IS MINIMUM CLEARANCE ALLOWED IAW REO. REMOVED OLD VANE FITTING FROM RT OB FLAP AS WS296.073 AND INSTALLED NEW VANE FITTING IAW REO. (K)

Part: RIB — CRACKED (FS 523.8)

RIGHT MLG WHEEL WELL BATTERY RIB AT WS 48.30, FS 523.8 IS CRACKED AT UPPER RADIUS APPROX 1.25 INCH LONG. REPAIRED IAW REO 601R-57-51-046 REV B. (M)

Part: RIB — CRACKED (LT FS 523.8) · airframe 13,573 hrs · 11,501 cycles

LT MLG WHEEL WELL BATT RIB AT WS 48.30, FS 523.8 IS CRACKED AT UPPER RADIUS APPROX 1.25 INCH LONG. REPAIRED IAW REO. (K)

Part: ANGLE — CRACKED (FS 484,LBL 27) · airframe 13,573 hrs · 11,501 cycles

LT FS 484, LBL27, ANGLE IS CRACKED APPROX 1.25 INCH L THRU THICKNESS OF MATERIAL AT UPPER END OF RADIUS. REMOVED CRACKED ANGLE, FABED NEW ANGLE FROM ANGLE TO SMPLE AND INSTALLED IAW SRM. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 13,573 hrs · 11,501 cycles

FS 280, RBL 9, IB CLIP ANGLE IS CRACKED 1 INCH LONG. REMOVED AND REPLACED FS 280, RBL9, IB CLIP IAW SRM. (K)

Part: CLIP — CRACKED (LBL 9, IB)

FS 280, LBL 9, IB CLIP ANGLE IS CRACKED, 1 INCH LONG. REMOVED AND REPLACED FS 280, LBL 9, IB CLIP IAW SRM. (K)

Part: ANGLE — CRACKED (LBL 9 OB) · airframe 13,573 hrs · 11,501 cycles

FS 280, LBL 9, CLIP ANGLE IS CRACKED, 1 INCH LONG. REMOVED AND REPLACED CLIP ANGLE FS 280, LBL 9, OB, IAW SRM. (K)

Part: CLIP — CRACKED (RBL9,OB) · airframe 13,573 hrs · 11,501 cycles

FS 280, RBL 9, OB, CLIP ANGLE IS CRACKED 1 INCH LONG. REMOVED AND REPLACED ANGLE IAW EO AND SRM. (K)

Part: SKIN — CHAFED (LT WING FLAP) · airframe 13,573 hrs · 11,501 cycles

LT WING IB FLAP, IB END AT FLAP STA 50.498 IB BELOW THE LEADING EDGE IS CHAFED FROM THE STUB FAIRING. CHAFE MEASURES 1.50 INCH LONG X .50 INCH WIDE X .035 INCH DEEP. (K)

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 13,573 hrs · 11,501 cycles

LT WING IB FLAP INNER SKIN IS DENTED BETWEEN FLAP STATION 142 AND 147 AT THE INTERCOSTAL SPAR AREA. DEN MEASURES .850 INCH LT X .800 INCH X .067 INCH DEEP. PERFORMED REPAIR BY CUTTING OUT DAMAGE AND INSTALLING 11.5 INCH X 3 INCH FLUSH REPAIR IAW SRM REPAIR AND EO. (K)

Part: FITTING — LOOSE (HZ STAB) · airframe 13,573 hrs · 11,501 cycles

HORIZONTAL STABILIZER FORWARD STEADY FITTING HAS 6 LOOSE MOUNT BOLTS. REMOVED BOLTS, VISUALLY INSPECTED HARDWARE AND HOLES, REINSTALLED BOLTS AND TORQUED IAW AMM. (K)

Part: POTENTIOMETER — FAILED (COCKPIT)

IN CRUISE FIGHT ED1, ED2, FMS 1 AND 2, RTU 1 AND 2, AND STANDBY RTU DISPLAY ALL WENT BLANK. REMOVED AND REPLACED CENTER PEDESTAL LIGHTING PANEL DISPLAY KNOB POTENTIOMETER. OPS CHECK GOOD IAW AMM 33-12-19. (M)

Part: CONNECTOR — DIRTY (NR 1 ENGINE) · airframe 12,085 hrs · 10,207 cycles

ENGINE NR 1 READS 0 PERCENT IN FLIGHT, ALL OTHER PARAMETERS NORMAL. CLEANED ALL CONNECTOR PLUGS, NR 1 ALTERNATOR AND SOCKET GROUND RAN TO TAKEOFF POWER, OPS CHECK GOOD. NO DEFECTS NOTED IAW AMM.

Part: CONTROLLER — FAILED (AOA HEAT) · airframe 11,870 hrs · 10,020 cycles

RT AOA, RT TAT, RT STATIC, RT PITOT AFTER TAKEOFF RETURNED IAW DISPATCH. REMOVED AND REPLACED RT AIR DATA SENSOR HEAT CONTROLLER IAW MM 30-31-15, OPS CHECK GOOD.

Part: SKIN — CORRODED (LT WING)

LT WING LOWER SKIN PLANK HAS CORROSION AT PANEL OPENING 540CB, FORWARD AND AFT OF PANEL OPENING. PERFORMED A MAJOR REPAIR BY BLENDING OUT CORROSION AND TREATING METAL IAW REO 601R-57-21-030. (M)

Part: SKIN — SCRATCHED (FUSELAGE)

LEFT SIDE FUSELAGE SKIN SCRATCHES FS 280 TO FS 295, STRINGER 25L TO STRINGER 26L. PERFORMED A MAJOR REPAIR BY CUTTING OUT DAMAGED SECTION OF SKIN, COMPLYING WITH HFEC TO ENSURE CRACK EXIST AND INSTALLING A NON-FLUSH PATCH IAW CRJ SRM 53-00-31 REPAIR NR 1 REO 601R-53-21-410 REV A. (M)

Part: BRACKET — CRACKED (FUSELAGE)

FOUND CRACKED BRACKETS, QTY 2, AT FS 484 RIGHT FUSELAGE, FLOOR LEVEL. REMOVED AND FABRICATED TWO BRACKETS AS PER SAMPLE MATERAL 6144-13 (2024-T42.050) WVAC PO 27909/1 IAW WVAC EO601R-53-4502 RT SIDE FS 484 RBL 9 AND RBL 27 AND INSTALLED SAME BRACKETS IAW WVAC EO 601R-53-4502 ALL STOPS COMPLIED WITH. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FOUND FLOOR STRUCTURE CRACKED AT FS 621, LT AND RT SIDE ANGLE, P/N 601R35032-239. PERFORMED A MAJOR REPAIR BY CUTTING AWAY DAMAGES PORTION OF ANGLE AND INSTALLING REPAIR ANGLE AND STRAP IAW BOMBARDIE REO 601R-53-61-117 REV C. (M)

Part: GCU — FAILED (ADG)

PERFORM ADG DEPLOYMENT TEST FLIGHT. ADG FAILED TO POWER AC ESS BUS TEST FLIGHT UNSATISFACTORY. REPLACED GCU, (S/N OFF: 0212, S/N ON: 0290). COMPLETED TEST FLIGHT REQUIREMENTS. NO DEFECTS NOTED. GCU COMPONENT REPAIR SHOP TEAR-DOWN FINDINGS, NO FAULT FOUND (NFF).

Part: A/C PACK — LEAKING (NR 2)

F/A REPORTED SMOKE IN CABIN. NOTICED TEMPERATURE RISING. PACK NR 2 SELECTED MANUALLY. REDUCED TEMP PACK, ODOR AND SMOKE SUBSIDED. GROUND RAN A/C NR 1 AND NR 2 PACKS. OPS NORMAL. NR 2 PACK SHOWS EVIDENCE OF OIL LEAKAGE. PLACED PACK ON MEL.

Part: SMOKE — DETECTED (CABIN)

SMOKE TOILET CAUTION MESSAGE ON APPROACH INTO DENVER WITH PACKS SWITCHED TO APU. FLIGHT ATTENDANT SAW SMALL AMOUNT OF SMOKE ALONG FLOOR. ALSO, REPORTED OIL SMELL IN/NEAR LAVATORY. OPS CHECK GOOD ON GROUND. COULD NOT DUPLICATE. OK FOR SERVICE AT THIS TIME. (M)

Part: WINDOW — FAILED (COCKPIT) · airframe 6,103 hrs · 5,012 cycles

PILOTS SIDE WINDOW SHATTERED IN FLIGHT MAINTENANCE REMOVED AND REPLACED PILOT 'B' SCREEN. OPERATIONAL AND PRESSURIZATION CHECK GOOD. (M)

Part: TORQUE LINK — DISCONNECTED (NLG)

UPON DEPARTING OUT OF DENT, GEAR RETRACTION, GEAR DISAGREE WOW INPUT AND WOW OUTPUT MESSAGE MAINTENANCE FOUND NLG SCISSORS (TORQUE LINKS) DISCONNECTED. UPPER TORQUE LINK DAMAGED. INSPECTED GEAR. REPAIRED DAMAGE TO SCISSOR. PERFORMED GEAR SWINGS. (M)

Part: TRANSDUCER — FAILED (RT ENGINE) · airframe 4,345 hrs · 3,671 cycles

ZERO OIL PRESSURE ON RT ENGINE DURING FLIGHT. NO ASSOCIATED MESSAGES. ALL OTHER ENGINE INDICATIONS WERE NORMAL. NO LOW OIL PRESSURE LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RT ENGINE OIL PRESSURE TRANSDUCER.