N401AW

Part: SIGN — MISSING (CABIN) · airframe 40,235 hrs · 36,826 cycles

PASSENGER DOOR EMER EXIT SIGN MISSING.

Part: BUSHING — SCORED (RT MLG) · airframe 39,723 hrs · 36,312 cycles

RIGHT MLG FWD FACE OF MAIN FITTING BUSHING SCORED.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 39,723 hrs · 36,312 cycles

THE RT INBD FLAP VANE LE CHAFED BEYOND LIMITS AT CTR STOP.

Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 39,125 hrs · 35,724 cycles

FLIGHT NUMBER 3753. AUTOPILOT ENGAGED RECEIVED A LT WING DOWN CAUTION, DISCONNECTED AUTOPILOT. AILERON CONTROL WAS HEAVY IN BOTH DIRECTIONS. COMPLIED WITH AUTO PILOT TRIM QRH & AILERON JAMBED QRH SUSPECTED ICE & FREED JAMB. INSPECTED TED VISIBLE CONTROL CABLES OF AILERON CONTROL PATH. NO DEFECTS FOUND, COMPLIED WITH OPERATIONAL TEST OF AILERON SERVO IAW 22-11-21.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 38,263 hrs · 34,902 cycles

AFTER TAKEOFF, SELECTED GEAR UP RECEIVED GEAR DISAGREE WARNING MSG WITHIN 6 SECONDS. AFTER MSG PERSISTED FOR ONE MINUTE, BEGAN GEAR DISAGREE QRH.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 36,115 hrs · 32,882 cycles

CARGO DOOR HANDLE HOUSING CRACKED. R & R WITH SERVICEABLE HANDLE HOUSING IAW CRJ 200 SRM 51-40-11 & 51-42-21.

Part: FITTING — WORN (TE FLAP) · airframe 36,115 hrs · 32,882 cycles

RIGHT WING TE, OTBD FLAP ALIGNMENT FITTING WORN BEYOND LIMITS. R & R FITTING PN 601R10156-4 IAW CRJ 200 SRM 51-40-11 & 51-42-06.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,115 hrs · 32,882 cycles

COMPLIED WITH JOB CARD 4DMI16050 PERFORM PERMANENT REPAIR OF FUSELAGE AT FS 265 IAW REO 601R-53-11-2301. COMPLIED WITH PERMANENT REPAIR OF FUSELAGE SKIN AT FS 265 & STRINGER 25R-26R IAW REO 601R-53-11-2615 REV.

Part: PLATE — CRACKED (LT EXHAUST) · airframe 36,115 hrs · 32,882 cycles

LEFT EXHAUST FAIRING INBD NUTPLATE MOUNT PLATE CRACKED. R & R PN 228-50181-833 IAW CMM 20-42-06.

Part: SEAL DEPRESSOR — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,115 hrs · 32,882 cycles

SERVICE DOOR SILL AREA, FWD & AFT SPIGOT STOP BOLT FITTINGS & LOWER SILL AREA, SEAL DEPRESSOR CORRODED. R & R LOWER SILL SUPPORT ANGLE & DEPRESSOR WITH SERVICEABLE PARTS IAW CRJ 200 SRM 51-24-21,51-40-11, 51-42-06 & 51-42-21 & REO 601R-53-21-2502.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,115 hrs · 32,882 cycles

PASSENGER DOOR LOWER SILL HAND RAIL RELIEF BRACKETS CORRODED. R & R TWO EACH BRACKETS PN 601R31527-149 IAW CRJ 200 SRM 51-40-11 & 51-42-06.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,115 hrs · 32,882 cycles

PASSENGER DOOR LOWER SILL ANGLE CORRODED. R & R WITH SERVICEABLE PART IAW CRJ 200 SRM 51-40-11, 51-42-21 & 51-24-21.

Part: STIFFENER — CRACKED (LT EXHAUST) · airframe 36,115 hrs · 32,882 cycles

LEFT EXHAUST FAIRING STIFFENER IS CRACKED, 2ND FROM FRONT. REPAIRED STIFFENER IAW CMM 78-11-00-300-810-A01.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,115 hrs · 32,882 cycles

FRAME AT FS 319 CORRODED ON AFT SIDE BETWEEN STRINGER 26L & 26R. R & R LOWER FRAME SECTOR PN 601R32003-61 IAW CRJ 200 SRM 51-42-06, 51-42-21 & 51-40-11.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 36,115 hrs · 32,882 cycles

DRAG ANGLE IN RT MLG WW UPPER APRON CRACKED. R & R ANGLE PN 600-10389-2 IAW CRJ 200 SRM 51-40-11 & 51-42-21.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 36,115 hrs · 32,882 cycles

RIGHT WING INBD LE, OTBD ATTACH ANGLE CRACKED. R & R WITH SERVICEABLE ANGLE PN 600-12025-8 IAW CRJ 200 SRM 51-40-11 & 51-41-02.

Part: SUPPORT ANGLE — CRACKED (CARGO DOOR) · airframe 36,115 hrs · 32,882 cycles

CARGO DOOR FWD SUPPORT UPPER ANGLE CRACKED. R & R WITH SERVICEABLE ANGLE IAW CRJ 200 SRM 51-24-16, 51-40-11 & 51-42-21.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 36,115 hrs · 32,882 cycles

EXTERNAL SERVICE PANEL LOWER MOUNT BRACKET CRACKED. R & R WITH SERVICEABLE PN 601R33003-19 IAW CRJ 200 SRM 51-40-11 & 51-42-06.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 36,115 hrs · 32,882 cycles

STRINGER ATTACH CLIP AFT OF FS 280 AT STRINGER 3L CRACKED. R & R WITH SERVICEABLE CLIP IAW CRJ 200 SRM 51-24-21,51-40-11, 51-42-06 & 51-42-21.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 36,115 hrs · 32,882 cycles

CARGO FLOOR TIE DOWN TRACK AT RBL 27 & FS 559+80 IS CORRODED. R & R WITH SERVICEABLE TRACK IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 36,115 hrs · 32,882 cycles

CARGO FLOOR, TIE DOWN TRACK AT LBL 9 & FS 559+112 CORRODED. R & R WITH SERVICEABLE TRACK IAW CRJ 200SRM 51-40-11 & 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,115 hrs · 32,882 cycles

FLOOR SUPPORT SEAT RAIL AT RBL 9 FROM FS 409 TO 409+128 HAS CORROSION & GOUGES. R & R FLOOR SEAT TRACK WITH SERVICEABLE TRACK IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,115 hrs · 32,882 cycles

FLOOR SUPPORT SEAT RAIL AT LBL 9 FROM FS 409 TO 409+128 IS CORRODED. R & R SEAT TRACK AT LBL 9 WITH SERVICEABLE PART IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 36,115 hrs · 32,882 cycles

CARGO FLOOR TIE DOWN TRACK AT LBL 27 & FS 559+96 IS CORRODED. R & R WITH SERVICEABLE TRACK IAW CRJ 200 SRM 51-40-11 & AMM 53-01-11.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 36,115 hrs · 32,882 cycles

THE RBL 9 FLOOR BEAM OTBD ATTACH ANGLE AT FS 280 IS CRACKED. R & R ANGLE IAW 601R-53-11-171 REV D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 36,115 hrs · 32,882 cycles

THE INTERCOSTAL ATTACH CLIP AT FS 484 & LBL 27 ABOVE THE PRESS FLOOR IS CRACKED. R & R ATTACH CLIP IAW CRJ 200 SRM 51-40-11, 51-42-06 & 601R-53-41-059 REV B DATED 2009-09-16.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 36,115 hrs · 32,882 cycles

THE INTERCOSTAL REPAIR ATTACH CLIP AT 484 & RBL 36 ABOVE THE PRESS FLOOR IS CRACKED. R & R REPAIR ATTACH CLIP IAW 601R-53-41-059 REV B DATED 2009-09-16.

Part: CLAMP — DAMAGED (BLEED DUCT) · airframe 35,321 hrs · 32,116 cycles

WHILE CLIMBING, RECEIVED LT 10TH DUCT WARNING MESSAGE. PERFORMED QRH, MESSAGE CAME BACK SEVERAL TIMES WHILE PERFORMING QRH. ONCE LT ENGINE AT IDLE POWER, MESSAGE DID NOT COME BACK. FOUND LT 10TH PRSOV CLAMP LEAKING AND DAMAGED, R & R CLAMP IAW AMM SUP 10-008, LEAK CHECKED IAW SUP 99-015, OK FOR SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 33,692 hrs · 30,519 cycles

DURING CLIMB THRU 30,000FT RECEIVED PAX DOOR OUTER HANDLE CAUTION MESSAGE. RAN QRH, MESSAGE PERSISTED. CREW DECLARED AN EMERGENCY AND DIVERTED TO CVG IAW QRH. CAUTION MESSAGE CLEARED DURING DESCENT AT APPROX 13,000FT. FLIGHT LANDED UNEVENTFULLY. ADJUSTED OUTER HANDLE PROX SENSOR S102MB IAW AMM 52-70-04. OPS CHECKED GOOD.

Part: ANTI-ICE VALVE — FAULTY (LT COWLING) · airframe 33,471 hrs · 30,310 cycles

LEFT COWL ANTI-ICE CAUTION IN FLT, WOULD NOT EXTINGUISH. COMPLIED WITH QRH. WITH SWITCH OFF MSG CLEARED. AIR RETURN DCA. REMOVED AND REPLACED LEFT COWL ANTI-ICE VALVE IAW AMM 30-22-01, OP CHECK/LEAK GOOD AT THIS TIME.

Part: DOUBLER — CRACKED (FS 202.75 BLKHD) · airframe 31,375 hrs · 28,223 cycles

FWD PRESSURE BULKHEAD STRIP, DOUBLER, 2ND RT OTBD FROM BL0.00 IS CRACKED, UPPERFWD INBD RADIUS BY WIPER MOTOR BRACKET. REPAIRED IAW REO 601R-53-11-2271, REV A.

Part: STRINGER — CRACKED (BS 439) · airframe 31,375 hrs · 28,223 cycles

STRINGER 6R IS CRACKED AFT SIDE OF FS 439.

Part: DOOR FRAME — CRACKED (FS 338) · airframe 31,375 hrs · 28,223 cycles

PAX DOOR FRAME AT FS 338.00 IS CRACKED 4" FROM BOTTOM OF FRAME. REMOVED CRACKED SECTION WHEN INSTALLED NEW SECTION IAW REO 601R-52-11-402, REV H.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 31,375 hrs · 28,223 cycles

INTERCOSTAL UNDER PAX DOOR PANEL 832BR CRACKED. REMOVED CRACKED INTERCOSTAL THEN INSTALLED NEW SERVICEABLE INTERCOSTAL.

Part: SEAT TRACK — CORRODED (BS 364-370) · corrosion level 2 · airframe 31,375 hrs · 25,223 cycles

SEAT TRACK CORRODED AT LBL9, FS 364. R & R SEAT TRACK.

Part: SKIN — CRACKED (PAX DOOR) · airframe 31,375 hrs · 28,223 cycles

PAX DOOR INTERIOR SKIN CRACKED ON AFT FRAME AT FS 338.00 AND INTERCOSTAL. REPAIRED INNER SKIN CRACK AT FS 338.00 IAW REO 601R-52-11-2009.

Part: SKIN — WORN (FS 544 -559) · airframe 31,375 hrs · 28,223 cycles

LEFT EXTERIOR FUSELAGE SKIN WHERE STUB FAIRING MAKES CONTACT IS GOUGED AND WORN, APPROX FS 544. CUT AWAY DAMAGED PORTION OF SKIN PANEL AND INSTALLED NEW SKIN SECTION AND STRAP ON LT EXTERIOR FUSELAGE SKIN IAW REO 601R-53-41-610, REV.

Part: SKIN — GOUGED (BS 544-559) · airframe 31,375 hrs · 28,223 cycles

LEFT EXTERIOR FUSELAGE SKIN & WHERE STUB FAIRING MAKES CONTACT IS GOUGED AND WORN. APPROXIMATELY FS 544.0 - 559.0. C UT AWAY DAMAGED PORTION OF SKIN PANEL AND INSTALLED NEW SKIN SECTION AND STRAP ON LT EXTERIOR FUSELAGE SKIN IAW REO 601R-53-41-610, REV.

Part: SKIN — MISINSTALLED (BS 499) · airframe 31,375 hrs · 28,223 cycles

SKIN MISREPAIRED. REPAIRED IAW REO 601R-53-41-1535, REV A.

Part: FITTING — CHAFED (RT FLAP ROLLER) · airframe 31,375 hrs · 28,223 cycles

RT OTBD FLAP ROLLER FITTING CHAFED, COMPIED WITH REO 601R-57-53-915.

Part: SKIN — CRACKED (NACELLE DOOR) · airframe 31,375 hrs · 28,223 cycles

A CRACK IN RT (FWD) CORE COWL DOOR OUTER SKIN. REMOVED DAMAGE FROM OUTER SKIN. FABRICATED DOUBLER AND SPIGOT IAW REO 601R-71-12-4095 AND CMM 71-12-01. REPAIR SRS118.

Part: STRUCTURE — CRACKED (WHEEL WELL) · airframe 31,375 hrs · 287,223 cycles

BOTH CORNERS ON MLG WW CUT CRACKED. REPAIRED CRACKS IAW REO 601R-53-11-048.

Part: SKIN — DAMAGED (FS 295) · airframe 31,375 hrs · 28,223 cycles

FUSELAGE SKIN AT FS 295.00 AND S26L. ONE LIGHTNING STRIKE 0.018" DEEP X 0.125" WIDE ON THE FUSELAGE SKIN LOCATED 3/00" AFT OF FS 295.00 + 0.156" FROM STRINGER 26L RIVET LINES REPAIRED LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT FS 295.0, STR 26L IAW REO 601R-53-21-2256, REV A.

Part: STRUCTURE — CHAFED (LT MLG DOOR) · airframe 31,375 hrs · 28,223 cycles

LEFT MLG DOOR CHAFED NEAR BRUSH, COMPLIED WITH REO 601R-52-82-330.

Part: FLOOR SUPPORT — CORRODED (FS 349-368) · airframe 31,375 hrs · 28,223 cycles

RT FS 349 CORRODED AND SILL IS SEPARATING. REMOVED UNSERVICEABLE ANGLE SUPPORT ANGLE AND UNSERVICEABLE SILL AND INSTALLED SERVICEABLE ANGLE SUPPORT AND SILL IAW SRM 51-42-06 AND REO 601R-53-21-326.

Part: FITTING — CORRODED (BS 349) · airframe 31,375 hrs · 28,223 cycles

FITTING CORRODED AT FS 349, JUST AFT OF THE SERVICE DOOR. BLENDED CORROSION IAW SRM 53-00-00 AND SRM 51-21-06. REMAINING MATERIAL IS WITHIN SERVICEABLE LIMITS IAW SRM 53-00-00.

Part: STRIKER — GOUGED (PAX DOOR) · airframe 31,375 hrs · 28,223 cycles

PAX DOOR AFT SEAL STRIKER GOUGED. REPAIRED IAW REO 601R53-22-033, REV C.

Part: FITTING — CHAFED (FLAP ROLLER) · airframe 31,375 hrs · 28,223 cycles

CHAFING AT LEFT OTBD FLAP ROLLER FITTING. OPEN

Part: SILL — CORRODED (BS 574-621) · airframe 31,375 hrs · 28,223 cycles

CARGO DOOR SILL HAS CORROSION FROM FS 574 TO FS 621 AND CORRODED NUT PLATES BLENDED CORROSION ON CARGO BAY DOOR SILL AT FS 574-FS 621 AT 12 NUT PLATE LOCATIONS FOUND TO BE WITHIN LIMITS IAW REO 601R-53-61-4379.

Part: PANEL — CHAFED (WS 282-353) · airframe 31,375 hrs · 28,223 cycles

RT WING PANELS 699AB & 699BB ARE CHAFED. BLENDED RT WING PANEL 699AB AND C99BB TO SMOOTH CONTOUR IAW SRM 51-12-00, WITHIN LIMITS IAW REO 601R-57-60-020.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 31,375 hrs · 28,223 cycles

LEFT FLOOR SUPPORT HAS NUMEROUS AREAS OF CORROSION FROM FS 409+128 TO FS 559. BLENDED FLOOR SUPPORT. FOUND TO BE WITHIN LIMITS IAW SRM 53-41-45 & REO 601R-53-41-666.

Part: SILL — CORRODED (FS 409-559) · airframe 31,375 hrs · 28,223 cycles

RIGHT FLOORBOARD SILL HAS NUMEROUS AREAS OF CORRODED FROM FS 409+128 TO FS 559.0. BLENDED CORROSION ON RT FLOORBOARD SILL AT FS 409+128 TO 559 WITHIN LIMITS IAW SRM 53-41-45 AND 51-21-06. ALSO, REO 601R-53-41-666. NO DEFECTS NOTED.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 31,375 hrs · 28,223 cycles

RIGHT INBD FLAP VANE HAS CHAFING ON L/E NEAR INBD, CTR & OTBD ACTUATOR SIDE BEAM HINGE FITTINGS. RIVET FOD UNDER L/E FROM PREVIOUS SHEET METAL WORK. BLENDED CHAFED AREA ON RT INBD FLAP VANE INBD, CTR OTBD ACTUATOR SLIDE BEAM HINGE FITTINGS FOUND TO BE WITHIN LIMITS IAW REO 601R-57-52-004.

Part: SKIN — CHAFED (RT AILERON) · airframe 31,375 hrs · 28,223 cycles

RT AILERON OTBD FWD LWR EDGE CHAFED, R & R.

Part: STRUCTURE — CHAFED (RT AILERON) · airframe 31,375 hrs · 28,223 cycles

RT AILERON UPPER L/E CHAFED. BLENDED CHAFED AREA ON RT AILERON UPPER L/E WITHIN LIMITS IAW REO 601R-57-60-013.

Part: SILL — CRACKED (BS 577) · airframe 31,375 hrs · 28,223 cycles

CARGO BAY DOOR SILL STEP PLATE CRACKED ON FWD STEP. R & R CARGO BAY DOOR STEP PLATE FWD STOP IAW SRM 51-40-11 & 51-42-06.

Part: SKIN — CHAFED (WING) · airframe 31,375 hrs · 28,223 cycles

LOWER WING SKIN UNDER PANEL 193AB AT OTBD ENDS HAVE MINOR CHAFING LT AND RT. BLENDED LT AND RT LWR WING SKIN UNDER PANEL 193AB WITHIN LIMITS IAW REO 601R-57-21-880.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 31,375 hrs · 28,223 cycles

BULKHEAD HAS DRILL START NEXT TO ISOLATOR RBL 27, SECOND ROW FROM BOTTOM. REPAIRED IAW REO 601R-53-61-1285.

Part: SCUFF PLATE — CORRODED (SERVICE DOOR) · airframe 31,375 hrs · 28,223 cycles

20 EA NUTPLATES CORRODED AT SERVICE DOOR SCUFF PLATE ATTACH PARTS INSTALLED SERVICEABLE.

Part: SILL — CORRODED (BS 559-621) · airframe 31,375 hrs · 28,223 cycles

RIGHT FLOOR SILL FROM FS 599.00+80 TO FS 621.00 IS CORRODED. BLENDED CORRODED AREAS FOUND TO BE WITHIN SERVICEABLE LIMITS EXCEPT FLOOR SILL 559+84 TO 559+112 WHICH WAS R & R WITH SERVICEABLE FLOOR SILL IAW SRM 51-42-06.

Part: ANGLE — CRACKED (FS 589) · airframe 31,375 hrs · 28,223 cycles

FWD CAP DOOR STOP FITTING FWD LOWER ANGLE IS CRACKED UNDER CARGO DOOR SILL AT FS 589, STR 17 LT. R & R ANGLE.

Part: SEAT TRACK — CORRODED (FS 559-621) · airframe 31,375 hrs · 28,223 cycles

ALL SEAT TRACKS AND TIE DOWN POINTS FROM FS 559 TO 621.00 ARE CORRODED AT RBL 27, RBL 9, LBL 9 AND LBL27. BLENDED AND SMOOTHED OUT CORRODED ON SERVICEABLE CARGO TRACKS IAW SRM 51-21-06. INSTALLED SERVICEABLE SEAT TRACKS FOR SEAT TRACKS OUT OF SERVICEABLE LIMITS IAW SRM 51-40-11, 51-21-11, 51-25-06 AND 51-25-16.

Part: FLOORBEAM — CRACKED (FS 280) · airframe 31,375 hrs · 28,223 cycles

INBD FLOORBEAM AT LBL 9 AND RBL 9 AT FS 280 ARE CRACKED. R & R INBD FLOORBEAM AT FS 280 IAW SRM 51-42-21.

Part: STRUCTURE — CHAFED (LT AILERON) · airframe 31,375 hrs · 28,223 cycles

LEFT AILERON CHAFED ON LOWER L/E AT OTBD END & CTR AREA BLENDED CHAFED AREA ON LT AILERON LWR L/E IAW SRM 51-12-00, WITHIN LIMITS IAW REO 601R-57-60-020.

Part: FRAME — GOUGED (FS 499) · airframe 31,375 hrs · 28,223 cycles

FRAME FS 499 HAS GOUGES AT STR 5 RT. HAND BLENDED GOUGES AT FS 499 AT STR 5R FOUND TO BE WITHIN LIMITS ORIGINAL .050 REMOVED, .004 REMAINING .0146 USING THICKNESS TESTER IAW SRM 51-12-00, 53-41-15, 51-21-11 AND 51-25-06.

Part: SHROUD — DEBONDED (WING) · airframe 31,375 hrs · 28,223 cycles

OTBD END OF INNER SHROUD DISBONDED AND RIVET IS PULLED THROUGH. COMPLIED WITH STEPS 1-4 OF REO 601R-57-41-161.

Part: ANGLE — DENTED (APU ENCLOSURE) · airframe 31,375 hrs · 28,223 cycles

APU ENCLOSURE DOOR HAS CRACK AT TOP CENTER AT REINFORCEMENT ANGLES AND 2 DENT CORNERS. REPAIRED IAW REO 601R-49-11-070, REV A.

Part: CAM — CHAFED (LT BUTTE DOOR) · airframe 31,375 hrs · 28,223 cycles

LEFT OTBD FLAP, TWO MOST OTBD BUTE DOOR CAMS CHAFED. MEASURED CHAFING AT OTBD BUTE DOOR CAMS AND FOUND TO BE IN SERVICEABLE LIMITS IAW REO 601R-57-53-195.

Part: ANGLE — CRACKED (BS 640) · airframe 31,375 hrs · 28,223 cycles

LT OBLIQUE ANGLE IS CRACKED. REMOVED AND FABRICATED AND INSTALLED NEW SERVICEABLE LT OBLIQUE ANGLE AT FS 640 IAW 601R-53-61-100, 601R-53-61-422.

Part: ANGLE — CRACKED (BS 625) · airframe 31,375 hrs · 28,223 cycles

RT OBLIQUE ANGLE AT 625 IS CRACKED. REMOVED, FABRICATED AND INSTALLED NEW SERVICEABLE RT OBLIQUE ANGLE AT 625 IAW REO 601R-53-61-100, 601R-53-61-422.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 31,375 hrs · 28,223 cycles

RIGHT SEAT TRACK ON THE SIDEWALL HAS CORROSION AT FS 364, 379, & 409 AND CHAFED AT FS 394.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 31,375 hrs · 28,223 cycles

LEFT INBD FLAP VANE CHAFED IN 4 AREAS, C/W REO 601R-57-52-004.

Part: STRUCTURE — CHAFED (RT MLG DOOR) · airframe 31,375 hrs · 28,223 cycles

RIGHT MLG DOOR CHAFED L/E BY BRUSH. C/W STEPS 6-12 REO 601R-53-82-034 BY FABRICATING NEW FILLER FOR EXISTING REPAIR.

Part: GUIDE — CHAFED (LT FLAP ROLLER) · airframe 31,375 hrs · 28,223 cycles

LT OTBD FLAP ROLLER GUIDE ON WING T/E CHAFED. C/W REO 601R-57-51-143.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 31,375 hrs · 28,223 cycles

FS 484 FLOORBEAM ANGLE CRACKED AT RBL 27-78. REPAIRED CRACKED FLOORBEAM ANGLE AT FS 484, RBL 27 IAW REO 601R-53-41-059, REV B.

Part: RIB — CRACKED (WS 53.6) · airframe 31,375 hrs · 28,223 cycles

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

Part: PANEL — CHAFED (WING) · airframe 31,375 hrs · 28,223 cycles

CHAFE ON PANEL 559AB. BLENDED CHAFED AREA IAW REO 601R-57-60-020 AND SRM 51-12-00.

Part: TARGET — LOOSE (MLG UPLOCK) · airframe 29,659 hrs · 26,414 cycles

RECEIVED GEAR DISAGREE WARNING MESSAGE ON CLIMBOUT WITHIN 10 SECONDS OF GEAR UP SELECTION. RT MLG SHOWED RED. SELECTED GEAR DOWN. C/W QRH. 3 GREEN LANDING WEIGHT 46600 NORMAL LANDING. INSPECTED AND FOUND RT MLG UPLOCK TARGET ARM LOOSE, RESECURED RT MLG TARGET ARM IAW CMM 32-30-15 AND AMM 32-32-00 OPS AND LEAK CHECKS GOOD. C/W AWAC SUPP 08-067 PSEU FAULT CODE S18 DOWN ARROW, FAR (RII YES-I-182).

Part: WIRE — LOOSE (PAX DOOR) · airframe 28,271 hrs · 24,936 cycles

RECEIVED PAX DOOR OUTER HANDLE CAUTION MSG LEVELING AT 33,000FT C/W QRH. RECEIVED MOMENTARY PAX DOOR WARNING THEN MSG CLEARED. 2 MIN LATER RECEIVED PAX DOOR OUTER HANDLE CAUTION. DURING INS OF PAX DOOR, LOOSE WIRE WAS FUND TO THE OUTER HANDLE SENSOR. REPINNED WIRE AND REPLACED CONNECTOR. OPS CKS GOOD, OK AT THIS TIME IAW AMM 52-11-03.

Part: PIPE — UNSECURE (NR 2 IDG) · airframe 27,912 hrs · 24,527 cycles

ABORTED T/O AT 60 KTS DUE TO NR 2 IDG CAUTION MESSAGE BTMS 4, 3, 5, 4. RESECURED NR 2 IDG STANDPIPE PLUG AND SERVICED OIL LEVEL IAW AMM 12-13-24. OPS AND LEAK CKS GOOD.

Part: DRAG BRACE — DEFECTIVE (NLG) · airframe 27,337 hrs · 23,936 cycles

DURING CLIMBOUT AT 17000 FT, RECEIVED WARNING GEAR DISAGREE NOSE GEAR RED LINE. PSEU BRAKOUT BOX SHOWS OUT OF LIMITS RESISTANCE FOR NLG DOWNLOCK NR 1. R & R NLG DRAG BRACE AND DOWNLOCK IAW AMM 32-00-00. OPS CK GOOD.

Part: WIRE HARNESS — DEFECTIVE (NLG) · airframe 27,328 hrs · 23,928 cycles

RECEIVED GEAR DISAGREE WARNING AT 26,000 FT. ACCOMPLISHED QRH AND NOSE GEAR INDICATED DASHED RED LINES UNTIL 10,000 FT. LANDING NORMAL. EMERGENCY LANDING DECLARED. WHILE TROUBLESHOOTING FOUND CONNECTOR PLUG BACKSHELL ON NLG HARNESS OFF CONNECTOR PLUG, R & R NLG HARNESS IAW AMM 32-61-25. OPS CK GOOD.

Part: PLATE — CORRODED (BS 320) · corrosion level 2 · airframe 23,629 hrs · 23,622 cycles

SERVICE DOOR THRESHOLD PLATE IS CORRODED BEYOND LIMITS. R & R PLATE ASSY PN 601R38957-19.

Part: SILL — CORRODED (BS 349) · corrosion level 2 · airframe 23,629 hrs · 23,622 cycles

SERVICE DOOR LOWER SILL AFT CORNER IS CORRODED ON LOWER FLANGE. R & R AFT LOWER CLIP PN 601R383382 IAW SRM 51-41-02-& 51-42-21.

Part: SILL — CORRODED (BS 319.70) · corrosion level 2 · airframe 23,629 hrs · 23,622 cycles

CORROSION FOUND AT SERVICE DOOR LWR SILL FWD CORNER ON ANGLE PN 601R38338-1. R & R WITH NEW PN 601R383381.

Part: HINGE FITTING — DAMAGED (RT WING TE FLAP) · airframe 23,629 hrs · 23,622 cycles

RT OTBD FLAP INBD HINGE BOX AFT HINGE FITTING IS DAMAGED ON AFT SIDE. REPAIRED DAMAGED AREA IAW REO 601R-57-54-161.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 23,629 hrs · 23,622 cycles

RT INBD FLAP VANE L/E IS CHAFED AT 3 LOCATIONS. R & R UNSERVICEABLE INBD FLAP VANE CHAFED SKINS (3EA) PANELS IAW SRM 51-42-13, +B/A REO NR 601R-57-52-004 REV C.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 23,629 hrs · 23,622 cycles

LT WING INBD FLAP VANE IS CHAFING AT 3 (EA) LOCATIONS AT STOP AREA. R & R UNSERVICEABLE 3 (EA) INBD FLAP VANE CHAFED SKIN PANEL IAW SRM 51-42-13 + B/A REO 601R-57-52-004 REV C.

Part: POST — CRACKED (BS 559) · airframe 23,629 hrs · 23,622 cycles

FS559 VERTICAL POSTS LBL 9 AND RBL ARE CRACKED. REPAIRED FS 559 BY INCORPORATION OF REOS 601R-53-41-260 AND 601R-53-41-609.

Part: ANGLE — CRACKED (BS 409) · airframe 23,629 hrs · 23,622 cycles

RBL 18 OTBD ANGLE FS 409.0 + 128 CRACK FROM BOTTOM OF LOWEST RIVET TO EDGE OR ANGLE. INCORPORATED REO 601R-53-41-056.

Part: ANGLE — CRACKED (BS 409) · airframe 23,629 hrs · 23,622 cycles

LBL 18.00, OTBD ANGLE FS 409.0+ 128 CRACK FROM BOTTOM OF LOWEST RIVET TO EDGE OF ANGLE. INCORPORATION REO 601R-53-41-056.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 23,629 hrs · 23,622 cycles

AT FS 311.75 FWD CORNER ANGLE CORRODED ON PAX DOOR. REMOVED CORRODED CORNER AND REPLACED WITH NEW SERVICEABLE PN 600-31998-12.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 23,629 hrs · 23,622 cycles

AT FS 347.25 AFT CORNER ON LOWER PAX DOOR SECTION CORRODED. REMOVED CORRODED CORNER ANGLE AND REPLACED WITH NEW SERVICEABLE PN 600-31998-11.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 23,629 hrs · 23,622 cycles

3RD RT SIDE SEAT TRACK CORRODED SEVERAL PLACES. R & R THIRD SIDE SEAT TRACK ON RT SIDE AT FS 409.00+16 TO 409.00 + 112.

Part: SEAT TRACK — CORRODED (BS 544) · corrosion level 2 · airframe 23,629 hrs · 23,622 cycles

CORROSION R & R SIDE SEAT TRACK IAW AMM. R & R SIDE SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 409-449.85) · corrosion level 2 · airframe 23,629 hrs · 23,622 cycles

4TH RT SIDE SEAT TRACK CORRODED, R & R TRACK.

Part: FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 23,629 hrs · 23,622 cycles

AT FS 320.10 TO FS 338.00 ON LOWER PAX DOOR 5 EA CLIPS CORRODED. FABRICATED AND REPALCED WITH NEW CLIPS.

Part: LINE — FAILED (APU OIL SYS) · airframe 26,004 hrs · 22,605 cycles

AFTER LANDING, APU AUTOSHUTDOWN, "APU FAULT" AND "APU OIL PSI" CAS MESSAGES, THEN CABIN FILLED WITH SMOKE. REMOVED AND REPLACED APU (FOUND APU OIL LINE BLOWN OUT OF HOUSING). (K)

Part: HYDRAULIC LINE — LEAKING (LT SPOILER) · airframe 23,996 hrs · 20,672 cycles

RECEIVED HYDRAULIC 2 LOW PRESSURE WARNING MSG ON GROUND. COMPLIED WITH QRH. ENGINE DRIVEN PUMP 2A RAN 2 MINUTES WITH QUANTITY ZERO. NOTED TEMPERATURE OF 46C. R&R LT OTBD SPOILER HOSE ASSEMBLY AND LT INBD SPOILER RETRACT HOSE ASSEMBLY IAW 51-10. R&R HYD NR 2 SYSTEM PRESSURE AND RETURN FILTER IAW 29-11. LEAK AND OPS CHECK GOOD. SERVICED NR 2 SYSTEM.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 23,877 hrs · 20,562 cycles

WHEN TURNING ON BOTH PACKS SMOKE ODOR IN COCKPIT. ACFT PARKED AT GATE AFTER PACKS TURNED OFF SMOKE ODOR SUBSIDED. INSPECTED APU AND AIR CYCLE MACHINE ACM AREA, NO FAULTS FOUND. TESTED ACM TEST CONTROL SYSTEM, AIR SYSTEM CHECKS GOOD IAW AMM 21-51-00, NO SMOKE OR ODORS NOTED.

Part: WIRE HARNESS — DAMAGED (NLG STEERING) · airframe 23,656 hrs · 20,359 cycles

DEPARTING, RETRACTIVE GEAR AND NOSE WHEEL STEERING INOP CAUTION. COMPLIED WITH QRH PROCEDURE. PERFORMED SHORT TO GROUND TEST WITH MEGGER OF NOSE WHEEL STEERING HARNESS ON GEAR FOUND MULTIPLE SHORT TO GROUND ON 500V SETTING. REPLACED HARNESS FROM CONNECTOR P4EC TO PIVOT RVDT AND SERVO VALVE IAW AMM 23-61-65. SWUNG NLG AND PERFORMED OPS CHECK OF NWC IAW 32-51-00, OPS CHECK GOOD. (K)

Part: ACTUATOR — INOPERATIVE (NLG) · airframe 23,264 hrs · 19,979 cycles

AFTER TAKEOFF RECEIVED GEAR DISAGREE MESSAGE, CYCLED GEAR PER QRH AND NOSE GEAR RETRACTED. REMOVED AND REPLACED (NLG) RETRACTION ACTUATOR, OPS CHECK GOOD IAW CRJ AMM 32-53-01. (A)

Part: ADC — FAULTED (NR 1) · airframe 23,011 hrs · 19,745 cycles

RECEIVED ADC NR 1 FAILURE INDICATION WITH MACH TRIM CAS MESSAGE DURING APPROACH. REMOVED AND REPLACED AIR DATA COMPUTER NR 1. (A)

Part: SILL — CRACKED (CARGO BAY) · airframe 22,525 hrs · 19,269 cycles

CRACK FOUND ON CARGO BAY FLOOR SILL FS 562.72-589. (M) CARGO BAY FLOOR SILL FS 562.72 TO FS 589.00 REPAIRED IAW REO 601R-53-61-690 REV D.

Part: FLOORBEAM — CORRODED (BS 589-610) · airframe 22,525 hrs · 19,269 cycles

FLOORBEAM BETWEEN FS 589 AND 610 LBL 27 IS CORRODED ALONG ANCHOR NUTS. (M) REPAIRED IAW REO 601R-53-61-2439.

Part: SILL — CORRODED (FUSELAGE) · airframe 22,525 hrs · 19,269 cycles

PAX DOOR LOWER SILL FORWARD AND AFT CLEATS CORRODED. (M) CORROSION REMOVED IAW ARM 51-21-06.

Part: BRAKE — CRACKED (MLG) · airframe 22,525 hrs · 19,269 cycles

CRACK FOUND AROUND PARKING BRAKE AT FS 202.75. - - PARKING BRAKE AT FS 202.75 REPAIRED IAW REO 601R-53-11-563. .

Part: BRACKET — CRACKED (BS 621-625) · airframe 22,525 hrs · 19,269 cycles

CRACKS FOUND ON BRACKETS ON INTERCOSTALS FS 621 TO FS 625.30 STRINGER 14 RT AND LT SIDE. (M) REPLACED BRACKET ON INTERCOSTAL FS 621.00 STR 14 RT & IAW REO 601R-53-61-100.

Part: RUB STRIP — WORN (ACCESS DOOR) · airframe 22,525 hrs · 19,269 cycles

RIGHT ENGINE TRAILING EDGE RUB STRIP IS WORN ON NOSE ACCESS COWL UPPER. (M) REPLACED IAW CMM TASK 71-14-01-300-814-A01 REPAIR SR5091.

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 22,685 hrs · 19,424 cycles

CREW ESCAPE HATCH OUTER HANDLE SHAFT CORRODED. REPLACED HANDLE ASSEMBY AND LUBED INTERIOR WITH DC33. (A)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,525 hrs · 19,269 cycles

AT FS 280, WL 73.10 BETWEEN LBL 9 AND RBL 9 FLOOR ANGLE (FWD) CRACKED, REPLACED IAW SRM 51-42-06 .

Part: RIB — CORRODED (RT WING) · airframe 22,525 hrs · 19,269 cycles

RIGHT WING INBOARD L/E OUTSIDE UPPER RIB CORRODED WS 148. CORROSION REMOVED IAW SRM 51-21-06. (M)

Part: LONGERON — CORRODED (BS 319-349) · airframe 22,525 hrs · 19,269 cycles

AT PAX DOOR, FS 319.70 TO FS 349, CORROSION WAS FOUND ON LOWER SILL LONGERON. (M) CORROSION REMOVED IAW SRM 51-21-06.

Part: RIB — CORRODED (LT WING) · corrosion level 1 · airframe 22,525 hrs · 19,269 cycles

LT INBOARD LEADING EDGE OUTBOARD SIDE UPPER RIB CORROSION. (M) CORROSION REMOVED IAW SRM 51-21-06. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,525 hrs · 19,269 cycles

FLOORBEAM 280 FOUND CRACKED AT LBL 9 AND RBL 9 WL 73.50 (2 PLACES). (M) REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B.

Part: RIB — CORRODED (RT WING) · corrosion level 1 · airframe 22,525 hrs · 19,269 cycles

FOUND CORROSION ON RIGHT OUT LE, WS 249 INBOARD SIDE UPPER RIB. (M) CORROSION REMOVED IAW SRM 51-21-06 AND TREATED IAW SRM (51-21-11) (51-25-06).

Part: SKIN — CORRODED (SERVICE DOOR) · corrosion level 1 · airframe 22,525 hrs · 19,269 cycles

SERVICE DOOR CORROSION FOUND WL 73.50, FS 319.70 TO FS 349 RBL 40. (M) SERVICE WL 73.50, FS 319.70 TO FS 349.00, RBL 40.00, CORROSION REMOVED IAW SRM 51-21-06. (K)

Part: ANGLE — CRACKED (LT WING) · airframe 22,525 hrs · 19,269 cycles

LT WING OUT AND INBOARD ANGLES AT WS 148 CRACKED 1 INCH BY 2 INCH. (M) ANGLES REPLACED IAW SRM 51-40-11.

Part: RIB — CORRODED (LT WING) · airframe 22,525 hrs · 19,269 cycles

LT SIDE OUTBOARD LEADING EDGE UPPER RIB INBOARD SIDE CORROSION. (M) LT SIDE OB LEADING EDGE UPPER RIB CORROSION REMOVED IAW SRM 51-21-06. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,525 hrs · 19,269 cycles

CROSSBEAM FS 280 LBL 9 WL 73 IS CRACKED. (M) REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B.

Part: ANGLE — CRACKED (RT WING) · airframe 22,525 hrs · 19,269 cycles

RIGHT WING AT WS 148 INBOARD AND OUTBOARD ANGLE CRACKED 1 INCH BY 2 INCH. (M) RT WING AT W/S 148 IB AND OB ANGLE REPLACED IAW SRM 51-41-02. (K)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 22,525 hrs · 19,269 cycles

FS 484, LBL 9, FLOOR SUPPORT ANGLE FOUND CRACKED LENGTH OF CRACK IS .400 INCH. FLOOR SUPPORT ANGLE AT FS 484, LBL 9 REPLACED IAW CRJ200 SRM 51-42-06 AND 51-42-20. (M)

Part: FLOORBEAM — CORRODED (BS 461) · airframe 22,525 hrs · 19,269 cycles

FS 461 RBL 9 FLOOR SUPPORT FITTING FOUND CRACKED LENGTH OF CRACK IS .400 INCH. (M) NEW FLOOR BEAM FITTING INSTALLED IAW SRM 51-42-21.

Part: DOOR — CORRODED (GROUND POWER) · airframe 22,525 hrs · 19,269 cycles

AT FS 200 INSIDE AC GROUND POWER DOOR (122BR), CORROSION WAS FOUND ON FWD SIDE. (M) CORROSION REMOVED IAW SRM 51-21-06.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 22,525 hrs · 19,269 cycles

CORROSION FOUND IN CARGO FLOOR SUPPORT STRUCTURE RBL 45 WL 73.50 FS 559 PLUS 80 FS 621. (M) CORROSION REMOVED IAW SRM 51-21-06.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 22,525 hrs · 19,269 cycles

FS 484, LBL 36 FLOOR SUPPORT ANGLE FOUND CRACKED LENGTH OF CRACK IS .880 INCH. (M) FS 484.00, LBL 36, FLOOR SUPPORT ANGLE REPAIRED IAW REO 601R-53-41-059, REV A. (K)

Part: STRUCTURE — CORRODED (SERVICE DOOR) · corrosion level 1 · airframe 21,934 hrs · 18,699 cycles

MINOR CORROSION UNDER SERVICE DOOR LOWER SEAL RETAINER. CORROSION REMOVED IAW SRM 51-21-06 WITHIN LIMIT SRM 52-00-31, FIG 101. MATERIAL REMOVED .003 INCH ORIGINAL THICKNESS .040. (K)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,934 hrs · 18,699 cycles

CRACK ON REAR PRESSURE BULKHEAD FWD FACE UNDER LINTER FITTING BRACKET. REPAIR TO REAR PRESSURE CUTOUT IAW REO 601R-53-61-1230 REV D. (K)

Part: CONNECTOR — FAILED (10TH STAGE VALVE) · airframe 20,747 hrs · 17,531 cycles

10TH STAGE ISO VALVE WILL NOT OPEN. REINSTALLED CONNECTOR ON 10TH STAGE VALVE, OPS CHECK GOOD, OK FOR SERVICE. (K)

Part: STRIP — UNKNOWN (TE FLAP)

WHEN FLAPS 45 DEGREES SELECTED A/C STARTS TO VIBRATE AND ROLL TO LEFT. DUIRNG TAKEOFF FLAPS 20 EXCESSIVE RIGHT AILERON TRIM REQUIRED. PERFORMED BLENDING OF L/E TEFLON STRIP OF FLAPS IAW SL-RJ-27-022 AMM 27-15 AND AMM 27-54-01-370-001 SECTION 8. (M)

Part: MECHANISM — LACK OF LUBE (SERVICE DOOR)

FOUND SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. LUBED UP DOOR MECHANISM, OPS CHECK GOOD IAW AMM 52-40. (M)

Part: HYDRAULIC LINE — CHAFED · airframe 18,426 hrs · 15,315 cycles

HYDRAULIC NR 1 LOW PRESSURE CAS INDICATION INFLIGHT. HYDRAULIC SYSTEM 1 QUANTITY ZERO PERCENT. REMOVED AND REPLACED HOSE ASSEMBLY ON PRESSURE SYSTEM NR IAW AMM. LEAK AND OPS CHECK GOOD. SERVICED HYDRAULIC SYSTEM NR 1 AS REQUIRED. (K)

Part: SKIN — DAMAGED · airframe 17,548 hrs · 14,476 cycles

FUSELAGE SKIN DAMAGED AT FS 310 BETWEEN STRINGERS 16L AND 17L. MAINTENANCE REMOVED DAMAGE, FABRICATED FILLER AND EXTERNAL DOUBLERS FROM 2024-T3 .050 INCH AND 2024-T3 .0063 INCH AND INSTALLED REPAIR PARTS IAW REO. (K)

Part: SKIN — UNSERVICEABLE (RT WING) · airframe 17,548 hrs · 14,476 cycles

RT IB FLAP VANE LEADING EDGE SKIN AT MID STOP MEASURES 1.1 INCH L X .30 INCH WIDE X .22 INCH DEEP. REMOVED (PN 601R1430352) RT IB FLAP VANE MID LEADING EDGE SKIN AND INSTALLED (PN 601R14303-52) RT IB FLAP VANE MID LEADING EDGE SKIN (NEW SERVICEABLE) IAW SRM. (K)

Part: MANIFOLD — MALFUNCTIONED (HYD SYSTEM)

HYDRAULIC 3B RUNS CONTINUOUSLY EVEN WITH SWITCH IN OFF POSITION AND CIRCUIT BREAKER PULLED HYDRAULIC QUANTITY DURING FLT WAS 95 PERCENT. REMOVED AND REPLACED PRESSURE MANIFOLD ASSEMBLY FOR ACMP HYD SYSTEM NR 3 A/B IAW AMM 29-12-05. (M)

Part: LATCH — OUT OF ADJUST (PAX DOOR)

ON CLIMB-OUT, PASSENGER DOOR LATCH CAUTION MESSAGE FOLLOWED BY PASSENGER DOOR WARNING. FLIGHT ATTENDANT STATED THE TWO TOP ALIGNMENT MARKS WERE OFF. REMOVED AND REPLACED AFT UPPER PASSENGER DOOR BEARING ROD. ADJUSTED DOOR LATCH MECHANISM. PERFORMED OPS AND FUNCTINAL TEST OF PASSENGER DOOR, OPS CHECK GOOD AT THIS TIME. (M)

Part: LATCH — INOPERATIVE (PAX DOOR)

DURING CLIMB-OUT, AMBER DOOR LATCH CAS MESSAGE, FOLLOWED QRH. AT APPROXIMATELY FL20.0 RED PASSENGER DOOR MESSAGE ILLUMINATED FOLLOWED QRH DIVERTED. INSPECTED DOOR ALIGNMENT PINS AND INTERROGATED PSEU. FOUND 3 FAULTS ON PSEU. DOOR CLOSES AND LOCKS NORMALLY. PRESSURIZED CABIN TO 5 PSID. ADJUSTED PASSENGER DOOR OUTER HANDLE IAW 52-11-03. OPS CHECK GOOD. (M)

Part: FIRE LOOP — MALFUNCTIONED (LT ENG PYLON)

LEFT 14TH STAGE DUCT FAIL WARNING MESSAGE IN FLIGHT. REMAINED ILLUMINATED AFTER ENGINE SHUTDOWN 45 MINUTES. REMOVED AND REPLACED LEFT 14TH STAGE LOOP PYLON, OPS CHECK GOOD. (M)

Part: YOKE — LOOSE (COCKPIT)

CHECKED THAT PLAY EVIDENT IN CONTROL YOKE PITCH AXIS IS WITHIN ACCEPTABLE LIMITS. COMPLIED WITH AMM TASK 27-32-00-720-801. FOUND CONTROL YOKE BACKLASH AT .28 DEGREES. BACKLASH LIMITS ACCEPTABLE. (M)

Part: WARNING LIGHT — FALSE ACTIVATION (MLG)

GEAR DISAGREE AFTER RETRACTION ON CLIMB-OUT. NO OTHER WARNINGS OR CAUTIONS. RAN CHECKLIST FOR GEAR UP DISAGREE. EXTENDED GEAR RECEIVED 3 GREEN LANDED AT 49400, NO OTHER PROBLEMS. PERFORMED OPS CHECKS IAW AMM 32-30-00. CYCLED GEAR NUMEROUS TIMES, COULD NOT DUPLICATE. OPS CHECK GOOD AT THIS TIME. CHECKED ALL PSEU INPUTS CODES, NO FAULTS FOUND. AIRCRAFT OK FOR SERVICE. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

RIGHT FUSELAGE SKIN AT FS 409-116 STRINGER 23R HAS LIGHTNING DAMAGE AND A TEMPORARY REPAIR INSTALLED IAW BOMBARDIER, INC REO 601R-53-00-084 REV A. CUT OUT DAMAGED SECTION OF SKIN. PERFORMED EDDY CURRENT OF CUTOUT, FABRICATED REPAIR DOUBLER FROM 2024 T3 .063 AND REPAIR FILLER FROM 2024 T3 .063. INSTALLED FILLER AND DOUBLER IAW WVAC EO 601R-53-4380 REV A. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

RT FUSELAGE SKIN AT STATION 310 BETWEEN STRINGERS 24R AND 25R HAS LIGHTNING DAMAGE WITH A TEMPORARY REPAIR INSTALLED IAW BOMBARDIER, INC REO 601R-53-00-084 REV A. REMOVED TEMPORARY REPAIR, CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER FROM 2024T3 .063 INCH WVAC PO NR 27603/1 AND INSTALLED IAW WVAC EO 601R-53-4387A. (M)

Part: STRINGER — DAMAGED (FUSELAGE)

FOUND FS 300.8, STRINGER 24R, STRINGER HAS .097 INCH HOLE DRILLED THROUGH LOWER EDGE. TRIMMED OUT DAMAGE ON STRINGER 24R AT FS 300.8. CUT OUT DAMAGED SECTION OF SKIN, FABRICATED A FILLER FROM 2024 T3 .063 INCH WVAC PO NR 27603/1 AND INSTALLED IAW WVAC EO 601R-53-4387A. REF AWAC WO55526 MWC31 FOR INSTALL OF DOUBLER. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

RT FUSELAGE SKIN AT FS 409 AND 64 STRINGER 23R HAS LIGHTNING DAMAGE AND A TEMPORARY REPAIR IAW MFG REO 601R-53-00-084 REV A. REMOVED TEMPORARY REPAIR, CUT OUT DAMAGED SECTION OF SKIN FABRICATED FILLER FROM 2024-T3 .050 INCH WVAC PO NR 296691 FABRICATED DOUBLER FROM 2024T-42. .063 INCH WVAC PO NR 169562 AND INSTALLED IAW CRJ200 SRM 53-00-31 REPAIR NR 1 AND WVAC EO 601R-53-4381.

Part: BEAM — DAMAGED (LT WING) · airframe 12,343 hrs · 9,826 cycles

LT OB FLAP HAS THE OB HING BEAM DAMAGED BY A SCREW BETWEEN THE HINGE AND THE FITTING. CLEANED DAMAGED AREA, BLENDED SMOOTH, PERFORMED ROTO/FLAP PEEN OF REPAIR AREA, ALODINED AND TREATED IAW ORIGINAL CONFIGURATION IAW WVAC EO 601R-57-4391.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

RIGHT FUSELAGE SKIN AT STATION 379 STRINGER HAS LIGHTNING DAMAGE AND PREVIOUS REPAIR BLENDED IN EXCESS OF 10 PERCENT MATERIAL THICKNESS. CUT OUT DAMAGED SECTION OF FUSELAGE SKIN, FABRICATED REPAIR DOUBLERS FROM 2024 T3 .063 INCH WVAC PO NR 27603/1 AND INSTALLED IAW WVAC EO 601R-53-8386. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 12,343 hrs · 9,826 cycles

RT FUSELAGE SKIN AT FS409 AND 48 STRINGER 23R HAS LIGHTNING DAMAGE WITH A TEMPORARY REPAIR IAW MFG REO 601R-53-00-084 REV A. REMOVED TEMPORARY REPAIR, CUT OUT DAMAGED SECTION OF FUSELAGE SKIN, FABRICATED REPAIR DOUBLER FROM 2024-T42 .063 INCH PO NR 169562 AND INSTALLED IAW CRJ200 SRM 53-00-31 REPAIR NR 1 AND WVAC EO 601R-53-4381.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 12,343 hrs · 9,826 cycles

RT FUSELAGE SKIN AT FS 680.5 STRINGER 24R HAS LIGHTNING DAMAGE AND TEMPORARY REPAIR IAW REO 601R-53-00-084 REV. A. REMOVED DAMAGED AREA OF SKIN, FABRICATED FILLER AND A DOUBLER FROM 2024-T3 .063 INCH WVAC PO NR 27603/1, INSTALLED IAW WVAC 601R-53-4388.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

THE RIGHT FUSELAGE SKIN AT FS 272 STRINGER 24R HAS LIGHTNING STRIKE DAMAGE WITH A TEMPORARY REPAIR INSTALLED IAW BOMBARDIER, INC REO 601R-53-00-084 REV A. REMOVED TEMPORARY REPAIR, CUT OUT DAMAGED SECTION OF FUSELAGE SKIN. FABRICATED REPAIR DOUBLER AND FILLER FROM 2024 T42 .063 INCH WVAC PO NR 16956/2 AND INSTALLED IAW WVAC EO 601R-53-4379. (M)

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM)

ON TAKEOFF, NR 2 HYDRAULIC SYSTEM QUANTITY DECREASED TO 0 PERCENT, NR 2 EDP, RAN 11 MINUTES AT 0 PERCENT RETURNED TO LNK. REMOVED AND REPLACED NR 2 SYSTEM HYD FILL LINE. (M)

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM)

HYD 2 LOW PRESS EICAS MESSAGE IN FLIGHT, HYD PAGE INDICATES 0 PERCENT QUANTITY, EDP NR 2 RAN FOR 45 MINUTES WITH ZERO QUANTITY, DIVERTED TO LNK. REPLACED NR 2 EDP AND EDP PSI LINE AT PYLON. CHECK HYD FILTER FOR METAL. NONE NOTED. BLEED SYSTEM. LEAK AND OPS CHECK GOOD. (M)

Part: FRAME — CRACKED (FUSELAGE)

FS 718 FRAME WAS FOUND CRACKED BELOW STRINGER 11, LEFT REPAIRED FRAME IAW WVAC EO 601R-53-3636 AND BOMBARDIER REO 601R-53-61-193 REV A. (M)

Part: FRAME — CRACKED (FUSELAGE)

RIGHT FRAME IS CRACKED IN RADIUS AT STRINGER 10, CRACK LENGTH IS APPROX .6 INCHES. PERFORMED PART C OF SB 601R-53-061 REV A. (M)

Part: FRAME — CRACKED (FUSELAGE)

RIGHT FS 718 FRAME FLANGE BELOW STRINGER 11 IS CRACKED INCORPORATED CANDAIR REO 601R-53-61-193 REV A AND WVAC EO 601R-53-3636. (M)

Part: SKIN — CORRODED (RT WING)

RIGHT WING FUEL PANEL ACCESS HOLES 610AB, 610BB, 640AB, 640CB, 640EB, AND 650DB HAVE MINOR CORROSION. COMPLIED WITH BOMBARDIER AEROSPACE, CANDAIR REGIONAL JET, SB 601R-57-030 REV O AND BOMBARDIER REO 601R-57-21-030. (M)

Part: SKIN — CORRODED (LT WING)

LEFT WING FUEL ACCESS PANEL HOLES 540CB, 540DB, 540EB, 550AB, 550BB, 550FBM ABD 550GB HAVE MINOR CORROSION COMPLIED WITH BOMBARDIER AEROSPACE, CANDAIR REGIONAL JET, SB 601R-57-030 REV O, AND BOMARDIER REO 601R-57-21-030. (M)

Part: ANGLE — CRACKED (FUSELAGE)

RIGHT SIDE FLOOR SUPPORT ANGLE 621 CRACKED OUT AND REMOVED FS 621 ANGLE. FITTED AND DRILLED -2 ANGLE AND -4 ANGLE. INSTALLED REPAIRED ANGLE. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

LEFT SIDE FLOOR SUPPORT ANGLE 621 CRACKED. CUT AND REMOVED CRACKED FLOOR SUPPORT ANGLE AT FS 621, LEFT SIDE. FITTED AND DRILLED NEW REPAIR ANGLES. INSTALLED REPAIR ANGLES AND STRUT P-5. (M)

Part: FRAME — CRACKED (FUSELAGE)

FOUND FS 640 FRAME LEFT IS CRACKED IN RADIUS AT STRINGER 11. REPAIRED FS 640 FRAME IAW SERVICE BULLETIN 601R-53-061. REV A BY COMPLYING WITH PART C OF SERVICE BULLETIN. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND FS 625 RIGHT OBLIQUE ANGLE. REMOVED AND REPLACED ANGLE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND FS 625 LEFT OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE. (M)

Part: SWITCH — FAILED (ROTORY COOL)

DISPLAY COOL MESSAGE IN FLIGHT MAINTENANCE REMOVED AND REPLACED DISPLAY COOL ROTARY SWITCH. OPERATIONAL CHECK GOOD. (M)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 7,978 hrs · 6,186 cycles

AFTER TAKEOFF RIGHT HAND AOA HEAT AMBER MESSAGE FOLLOWED BY LEFT HAND AOA HEAT AMBER MESSAGE. MAINTENANCE DEPOWERED AND REPOWERED AIRCRAFT OPS CHECK GOOD IAW AMM 30-31-15-710.

Part: OIL SYSTEM — OVERSERVICED (NR 2 ENGINE) · airframe 7,518 hrs · 5,795 cycles

NR 2 ENGINE HIGH OIL TEMP, PRECAUTIONARY ENGINE SHUTDOWN, NR 2 ENGINE OIL TEMP 158 DEGREES, PSI 40. MAINTENANCE INSPECTED AND FOUND NR 2 ENGINE OIL OVERSERVICED. REMOVED EXCESS OIL, GROUND RAN AIRCRAFT, OPERATIONAL CHECK GOOD.

Part: SHUTOFF VALVE — FAILED (RT ENGINE) · airframe 7,337 hrs · 5,645 cycles

IN-FLIGHT WITH RIGHT PACK SELECTED ON AND RIGHT 10TH STAGE BLEED SELECTED ON, RIGHT PACK INOP ECS PAGE SHOWED RT PACK AND 10TH STAGE VALVE CLOSED. CABIN TEMP TOO HIGH, ACFT RETURNED TO DEN. MAINTENANCE REPLACED RIGHT 10TH STAGE BLEED VALVE.

Part: WARNING — ACTIVATED (PAX DOOR)

FLT 5617 - MEM - PASSENGER DOOR LATCH CAUTION CASS, FOLLOWED BY PASSENGER DOOR WARNING CASS. PERFORMED OPS CHECK NUMEROUS TIMES, COULD NOT DUPLICATE. (M)

Part: DOOR — OUT OF ADJUST (PASSENGER COMPT)

MEM - FLT 5617 - PASSENGER DOOR CAUTION ILLUMINATED AFTER TAKEOFF, RETURNED TO MEMPHIS. AFTER LANDING, COULD NOT CLOSE DOOR PROPERLY. RE-ADJUSTED REAR SPIGOT TO OBTAIN PROPER GAP PER AMM. (X)

Part: TIRE — FAILED (NLG)

JAN - FLT 5520 - ON LANDING, NOSE TIRE BLEW WITH VIBRATION AND CLUNKING NOISE IN WHEELWELL. REMOVED AND REPLACED NOSE TIRE. INSPECTED UNDERSIDE OF AIRCRAFT AND NOSE GEAR WHEELWELL. NO DEFECTS NOTED. (X)

Part: LATCH MECH — NOT LATCHED (PASSENGER DOOR)

DEN - FLT 5558 - IN CLIMB EDI MSG. DOOR LATCH CAUTION. SHORTLY FOLLOWED BY EDI MSG DOOR LATCH WARNING. F/A CONFIRMED TOP TWO LATCHES NOT ALIGNED. PERFORMED OPS CHECK IAW MM, CHECKS GOOD. WILL PERFORM TEST FLIGHT. TEST FLIGHT SUCCESSFUL. (X)

Part: LATCH — OUT OF ADJUST (PASSENGER DOOR)

DEN - FLT 5618 - PASSENGER DOOR LATCH CAS MESSAGE. PERFORMED PASSENGER DOOR FUNCTIONAL TEST. MOVED AFT UPPER LATCH DOWN ONE SERRATION. DOOR OPS CHECK GOOD. (X)

Part: BPSU — FAILED (TE FLAPS)

DEN/MEM - FLT 5616 - 'FLAP FAIL' CAUTION AT 29,000 FEET. CRUISE FLIGHT WITH NO FLAP SELECTION. LANDING MADE WITH ZERO FLAPS AT 174 KNOTS. FERRIED AIRCRAFT TO DEN. REMOVED AND REPLACED LEFT BRAKE POSITION SENSOR UNIT (BPSU). PART TOTAL CYCLES: 230. (X)

Part: INDICATION — MALFUNCTIONED (TE FLAPS)

MSN/DEN - FLT 5537 - 'FLAP FAIL' MESSAGE IN CRUISE AT 35,000 FEET. NO SELECTION HAD BEEN MADE, LANDING SPEED 167 KNOTS WITH ZERO FLAPS. C/W SUPPLEMENT 98-18. NO TWISTING OF FLAPS EVIDENT. CLEARED FAULT BY DEPOWERING A/C, CYCLED FLAPS NUMEROUS TIMES. NO FURTHER DISCREPANCIES. TEST FLIGHT COMPLETED SATISFACTORILY. (X)

Part: MASK — DEPLOYED (CABIN)

MEM - FLT 7615 - UPON ARRIVAL AT AIRCRAFT, FOUND ALL PASSENGER OXYGEN MASKS DEPLOYED. RE-STOWED ALL OXYGEN MASKS AND PEFORMED OPERATIONAL CHECK OF OXYGEN MASKS, PERFORMED IAW CRJ MM 35-21-09. NO DEFECTS NOTED. (X)