N8980A

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,334 hrs · 28,249 cycles

EXTERIOR EMERGENCY LIGHT BY SERVICE DOOR WOULDN`T ILLUMINATE. REMOVED & REPLACED THE EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: DOOR FRAME — CHAFED (AFT CARGO) · airframe 28,467 hrs · 26,267 cycles

DURING 5A CHECK NOTED AFT CARGO DOOR SURROUND BEAM CHAFED AFT .5"X.91" X .033" DEPTH. COMPLETED REPAIR OF CARGO DOOR TRACK BEAM ASSY. IAW EA CRJ 253-08684.

Part: WEB — CRACKED (PAX DOOR) · airframe 27,920 hrs · 25,675 cycles

PAX DOOR FWD EDGE MEMBER HAS A POSSIBLE CRACK. REPAIRED DOOR EDGE MEMBER IAW REO 601R-52-11-279.

Part: HINGE — CORRODED (LAV SERVICE) · airframe 27,920 hrs · 25,675 cycles

AFT LAV SER PNL 196AR BOTH HINGE CORRODED. REMOVED/REPLACED HINGES ON PNL 196AR IAW SRM 51-42-06 AND 51-42-06 AND 51-42-21.

Part: VANE — CRACKED (LE SLAT) · airframe 27,920 hrs · 25,675 cycles

AFTER REMOVAL OF RT INBD FLAP VANE FOUND OUTBD VANE LE CRACKED AT FASTENER HOLE. REMOVED/FABBED/INSTALLED BUTT STRAP IAW SRM 51-42-10.

Part: ATTACH BRACKET — CRACKED (RT SPOILER) · airframe 27,920 hrs · 25,675 cycles

RT FLT SPOILER O/B BOLT RETENTION ANGLE ATTACH BRACKET CRACKED. REMOVED AND REPLACED RT FLT SPOILER O/B BOLT RETENTION ANGLE ATTACH BRKT IAW SRM 51-42-06.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 27,920 hrs · 25,675 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGE DRAG ANGLE AND INSTALLED DRAG AND REPAIR ANGLE IAW R.E.O. 601R-52-11-513 TYPE 11.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 27,920 hrs · 25,675 cycles

AFT CARGO DOOR, CONNECTOR SUPPORT IS BENT AND CRACKED. REMOVED/REPLACED CONNECTOR SUPPORT ON AFT CARGO DOOR IAW SRM.

Part: SEAL — CHAFED (NOSE COWLING) · airframe 27,920 hrs · 25,675 cycles

NOSE COWL 432AB LE SEAL HAS CHAFING DAMAGE. REMOVED/REPLACED NOSE COWL 432AB LE SEAL IAW CMM 200 71-14-01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

ANGLE CLIP IS CRACKED ON THE I/B SIDE OF LBL 36 AT FS 484, IN THE CABIN BELOW THE FLOOR. REMOVED/REPLACED ANGLE CLIP AT STATION 484 LBL36 IAW REO 601R-53-41-059.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

LBL27 FLOORBEAM ATTACHMENT FITTING AT RPB HAS CORROSION. REPAIRED LBL27 FLOORBEAM ATTACHMENT FITTING IAW EA 253-07919.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

PNL 211AL AFT LATCH LWR CORNER SKIN IS CRACKED. REMOVED CRACK AND APPLIED TOPCOAT FA934 IAW EA 253-8138.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

PAX DOOR OPENING FWD UPPER STOP FITTING IS CRACKED. REMOVED CRACKED STOP FITTING AND REPLACED WITH NEW UPPER STOP FITTING IAW SRM 51-42-21.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

FRAME 333 IS CRACKED JUST BELOW AND I/B OF STGR 2L, IN THE CABIN. REPAIRED FRAME 333 CRACK DAMAGE STR 1L-2L PER EA 253-08159.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

BATHTUB FITTING IS CRACKED ON THE O/B SIDE OF LBL 9 AT FS 461, IN THE CABIN BELOW THE FLOOR. REMOVED AND REPLACED BATHTUB FITTING AT LBL 9 FS 461. IAW SRM 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

BEAM 280 IS CRACKED AT THE AFT UPPER ANGLE BETWEEN THE MLG MANUAL RELEASE CABLE PULLEY BRACKET AND PREVIOUS REPAIR, JUST O/B OF LBL 9, IN THE CABIN BELOW THE FLOOR. REPAIRED CRACKED ANGLE IAW REO 601R-53-11-136.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

SERVICE DOOR THRESHOLD HAS CORROSION AROUND FASTENER HOLES. LOCATED AND DRILLED NEW SERVICE DOOR THRESHOLD IAW SRM 51-24-16 REPLACED WITH NEW. INSTALLATION TO BE COMPLIED WITH ON W/O 1016523-2000-0056 S/N 6798600.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

FLOOR LANDING ON RBL 9 HAS CORROSION SPOTS BETWEEN FS 260 THRU FS 280,IN THE FLT DECK BELOW THE FLOOR. REMOVED AND REPLACED FLOOR LANDING ANGLE IAW SRM 51-42-06/51-42-13.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

FLOOR LANDING ON LBL 9 HAS CORROSION SPOTS BETWEEN FS 260 THRU FS 280,IN THE FLT DECK BELOW THE FLOOR. REMOVED AND REPLACED FLOOR ANGLE LANDING IAW SRM 51-42-06/51-42-13.

Part: HINGE — CORRODED (PAX DOOR) · airframe 27,920 hrs · 25,675 cycles

PAX DOOR TOP STEP HINGE HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED PAX DOOR TOP STEP HINGE PN# 601R31980-63 IAW SRM 51-40-11 TR 51-42 AND SRM 51-42-06.

Part: HINGE — CORRODED (PAX DOOR) · airframe 27,920 hrs · 25,675 cycles

PAX DOOR TOP STEP HINGE FROM TOP STEP TO FUSELAGE IS CORRODED. REMOVED AND REPLACED TOP STEP TO FUSELAGE HINGE IAW SRM 51-41-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

ANGLE CLIP IS CRACKED AT THE O/B SIDE OF RBL 27 AT FS 484, IN THE CABIN BELOW THE FLOOR. REPLACED ANGLE CLIP @ RBL 27 FS 484 IAW SRM 51-42-06 AND 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

LT SIDEWALL SEAT TRACK STICK 6 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

LT AISLE SEAT TRACK STICK 1 HAS CORROSION SPOTS, IN THE CABIN. REMOVED/REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

RT SIDEWALL SEAT TRACK STICK 4 HAS CORROSION SPOTS, IN THE CABIN. REMOVED/INSTALLED REPLACEMENT SEAT TRACK NR 4 STICK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

RT SIDEWALL SEAT TRACK STICK 7 HAS CORROSION SPOTS, IN THE CABIN. REMOVED/REPLACED SIDEWALL SEAT TRACK IAW AMM 53-01-11 AND IAW SRM 51-21-06.

Part: STRAP — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

FLOOR STRAP AT FS 559 HAS CORROSION BETWEEN RBL 27 AND THE RT FLOOR SILL, IN THE CABIN BELOW THE FLOOR. REMOVED AND REPLACED WITH NEW FLOOR STRAP ON FS 559 STRAP @ RBL27 AND RT FLOOR SILL IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

LT SIDEWALL SEAT TRACK STICK 2 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED SIDEWALL SEAT TRACK IAW AMM 51-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

LT SIDEWALL SEAT TRACK STICK 3 HAS CORROSION SPOTS, IN THE CABIN. REMOVED/REPLACED SIDEWALL SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

RT SIDEWALL SEAT TRACK STICK 2 HAS CORROSION SPOTS, IN THE CABIN. REMEOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAL — CHAFED (RT COWLING) · airframe 27,920 hrs · 25,675 cycles

RT ENGINE COWL 442AT SEAL HAS KNIFE EDGE. REMOVED AND REPLACED AFT EDGE STRIP IAW CMM 71-14-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

RT SIDEWALL SEAT TRACK STICK 3 HAS CORROSION SPOTS, IN THE CABIN. REMOVED/REPLACED DAMAGED SEAT TRACK NR 3 STICK IAW AMM 53-01-11.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

RT MLG WHEEL WELL DRAG ANGLE CRACKED. REMOVED AND REPLACED IAW 51-42-21.

Part: SUPPORT FITTING — CRACKED (WINDSHIELD) · airframe 27,920 hrs · 25,675 cycles

RT WINDSHIELD SIDE POST LWR OTBD SUPPORT FITTING CRACKED. REPLACED SUPPORT FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

BATHTUB FITTING IS CRACKED ON THE O/B SIDE OF RBL 9 AT FS 461, IN THE CABIN BELOW THE FLOOR. REMOVED CRACKED BRACKET IAW SRM 51-42-06 INSTALLED NEW BRACKET AFTER LOCATING/DRILLING IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

RT SIDEWALL SEAT TRACK STICK 5 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

LT SIDEWALL SEAT TRACK STICK 4 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

LT SIDEWALL SEAT TRACK STICK 7 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

RT SIDEWALL SEAT TRACK STICK 6 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

LT AISLE SEAT TRACK STICK 2 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-12.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,920 hrs · 25,675 cycles

RT AISLE SEAT TRACK STICK 1 HAS CORROSION SPOTS, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-01-11.

Part: PLUNGER — DIRTY (DOOR) · airframe 27,777 hrs · 25,527 cycles

FLT ATT UNABLE TO OPEN DOOR. HANDLE DIFFICULT TO MOVE DOWN. PLUNGER & ROLLER STICKING CLEANED PLUNGER SPRINGS & ROLLER IAW AMM 52-11-00, OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE · airframe 27,253 hrs · 24,954 cycles

FWD EMER FLASHLIGHT OUT/INOP. R&R LIGHT IAW AMM 25-61-00. OPS CHECK GOOD.

Part: PBE — DEFECTIVE (CABION) · airframe 27,022 hrs · 24,681 cycles

FLIGHT ATTEND. REPORTED THE PBE TO BE SOFT. R & R THE PBE IAW AMM 25-61-00.

Part: OXYGEN MASK — BROKEN (OBSERVER'S) · airframe 26,585 hrs · 24,213 cycles

OBSERVER`S OXYGEN MASK BROKE AT THE RED SQUEEZE TO RELEASE, AND WAS LEAKING OXYGEN. R & R THE OXYGEN MASK IAW AMM 35-11-12. OPS CHECKED THE OXYGEN SYSTEM, GOOD IAW AMM 35-10-00.

Part: CONNECTOR — DISCONNECTED (NLG) · airframe 26,426 hrs · 24,046 cycles

AFTER DEPARTURE, SELECTED GEAR UP, ANTI-SKID INBOARD CAUTION, GEAR DISAGREE WARNING, 6 SEC PARK BRAKE SOV CAUTION, PERFORMED QRH, EXTENDED AND RETURN TO DEPARTURE, ALL CAUTION & WARNING EXTINGUISHED AFTER QRH PROCEDURE. NOSE WHEEL DID NOT APPEAR OR INDICATE RETRACTION, MAINS DID INDICATE RETRACTED. CONNECTED THE ELECTRICAL CONNECTOR ON MLG SELECTOR IAW AMM 32-32-25, OPS TEST OF EXTENSION & RETRACTION OF LANDING GEAR GOOD, NO EICAS SYSTEMS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG) · airframe 26,426 hrs · 24,046 cycles

GEAR DISAGREE WARNING ON FINAL. NOSE GEAR DID NOT SHOW DOWN & LOCKED. PERFORMED QRH & NOSE GEAR SHOWED DOWN. DID NOT CYCLE THE GEAR LEVER. PERFORMED A FUNCTION TEST OF EXTENSION & RETRACTION SYSTEM IAW AMM 32-50-00, CHECKED NORMAL CHECKED NLG DOWN LOCK PROXIMITY SENSOR FOR CONDITION AND CLEARANCE IAW AMM 32-61-05. CLEARANCE GOOD. VERIFIED CHECK VALVES ON BOTH BRAKE CONTROL VALVE WERE INSTALLED PROPERLY IAW AMM 32-43-06. BLED HYD SYS IAW AMM 12-13-29. PERFORMED MULTIPLE EXTENSIONS AND RETRACTIONS OF LANDING GEAR IAW AMM 32-30-00. OPS TESTED NORMAL.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEATS 3 CD) · airframe 25,970 hrs · 23,555 cycles

DURING TAXI OUT, THE OXYGEN MASKS OVER SEATS 3 C/D DROPPED. STOWED THE OXYGEN MASKS IAW AMM 35-21-11.

Part: RESERVOIR — INOPERATIVE (HYD SYSTEM) · airframe 25,288 hrs · 22,839 cycles

AFTER TAKEOFF HYD 3 LOW PRESSURE FOLLOWED BY GEAR DISAGREE AND NOSE DOOR MASTER WARNING. REMOVED & REPLACED HYD RESERVOIR IAW AMM 29-12-30. OPS CHECK PASSED. EXTENDED AND RETRACTED GEARS IAW 32-30-00, NO LEAKS DETECTED. NO MESSAGES NOTED. ACFT OK FOR SERVICE. ALL CHECKS PASSED IAW 32-30-00. ALL QUANTITIES WERE STABLE DURING RETRACTION AND EXTENSION.

Part: B-NUT — LOOSE (VG ACTUATOR) · airframe 24,752 hrs · 22,275 cycles

STRONG ODOR OF FUEL IN CABIN & COCKPIT, BURNED MORE FUEL THAN EXPECTED ENROUTE. TROUBLESHOOT THE LEFT ENGINE FOR FUEL LEAKS FOUND A LOOSE B-NUT ON THE VARIABLE GEOMETRY ACTUATOR, AFTER TIGHTENING THE B-NUT IAW AMM 75-31-01, RAN THE FUEL PUMP AND NO LEAKS FOUND.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,539 hrs · 22,065 cycles

CO-PILOT EMEMERGENCY FLASHLIGHT NOT BLINKING. R & R CO-PILOT FLASHLIGHT IAW AMM 25-61-04 OP CHECKED GOOD.

Part: VANE — CHAFED (TE FLAP) · airframe 23,360 hrs · 20,842 cycles

LEFT WING INBD FLAP VANE LE CHAFED IN 3 PLACES, INBD 1" X .750 X .004 DEEP, MID 1.0 X .600 X .004 DEEP, OTBD 1" X .500 X .003 DEEP. CONTINUATION CARD 8798011 OP 153. REPAIRED LT INBD FLAP VANE LE CHAFES IAW REO 601R-57-52-004 REV D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

FS 574 FRAME IS CORRODED AT STRINGER 26R. CONTINUATION CARD 8798011 OP 162, 172, & 174. R & R FRAME AT FS 574 IAW SRM 51-40-06, 51-42-21, 51-40-11. IAW JC 8798011 OPS 150, 162, 172 & 174 FOR WORK PERFORMED & EA CRJ253-04084.

Part: LIGHT — NOT REPORTED (CABIN) · airframe 23,360 hrs · 20,842 cycles

LIGHT TRACKS 9, 5 & 8 ON THE LT SIDE REQUIRE REPLACEMENT. R & R FLOOR LIGHTS 9, 5 & 8 ON LT SIDE IAW AMM 33-51-01-400-806. OPERATIONS CHECKED GOOD.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

FOUND REAR PRESS BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130, APPROX .500" IN LENGTH 90% FSH, FAILED NDT INSPECTION. CONTINUATION CARD 8798015 OP 33. REPAIRED REAR PRESS BULKHEAD WEB AT FS 621 IAW REO 601R-53-61-1541 REF F DATED 2014 11 12. THIS IS A MAJOR REPAIR.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

PRESSURE BULKHEAD AT FS 621 - 625.3, AT STRINGER 13L & 14L, HAS CRACKED INTERCOSTAL CLIPS, INSPECTED IAW REO 601R-53-61-5230 & IS DUE RE-INSPECT OF BULKHEAD CAP ANGLE & INTERCOSTAL CLIPS AT INTERVALS NOT TO EXCEED 1200 FH & TO BE REPAIRED AT OR BEFORE 5000 FH. CONTINUATION CARD 8798016 OP 9. REPLACED INTERCOSTAL CLIPS IAW SRM 51-42-21 & 51-42-06. REFERENCE MWC JOB 8798016 OPERATIONS 6 & 9 FOR WORK PERFORMED.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

FS 621 BULKHEAD FWD FACE HAS MULTIPLE CHAFES, FROM PANEL SCREWS ON SKIN, RIVET HEADS & Z MEMBER. CONTINUATION CARD 8798011 OP 207. REPAIRED CHAFES ON FS 621 BULKHEAD FWD FACE & Z MEMBER IAW REO 601R-53-61-2155 & SRM 51-12-00. THIS IS A MAJOR REPAIR.

Part: POST — DAMAGED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

FS 409+128, BL 0 LT VERTICAL POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69, .250" LONG BY GREATER THAN 50% FSH. FAILED NDT INSPECTION. CONTINUATION CARD 8798015 OP 42. REPLACED VERTICAL POST AT FS 409+128, BL 0 LT SIDE IAW SRM 51-42-06, 51-40-11, 51-42-22, & REO 601R-53-41-8889 REV A.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

PASSENGER DOOR FLOOR SILL ANGLE IS CORRODED. REPLACED PAX DOOR FLOOR SILL ANGLE WITH SERVICEABLE SILL ANGLE IAW SRM 51-42-06.

Part: WEB — CRACKED (PAX DOOR) · airframe 23,360 hrs · 20,842 cycles

PASSENGER DOOR FWD WEB STAIR STRUCTURE CRACKED AT CORNER FOR MID-STEP. CONTINUATION CARD 8798011 OP 163. REPAIRED PAX DOOR FWD WEB IAW REO 601R-52-11-702 REV C DATED 03 09 10. REF JC 8798011 OPS 79 & 163 STEPS 1 - 11 FOR WORK PERFORMED.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

FS 310 FRAME FWD, UPPER STOP BRACKET FOR PAX DOOR IS CRACKED, BELOW STOP BOLT LUG. R & R UPPER STOP BRACKET, STOP, SHIMS & BOLTS IAW SRM 51-42-21, 51-40-11 & AMM 20-21-00-910-801 & 20-24-00-910-803. OPERATIONS TESTED GOOD IAW AMM 52-11-25-710-801.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 23,360 hrs · 20,842 cycles

PASSENGER DOOR OUTER HANDLE IS CRACKED. CONTINUATION CARD 8798011 OP 205. REPLACED PAX DOOR OUTER HANDLE IAW SB 601R-52-119 & EO P52034.

Part: SKIN — GOUGED (PAX DOOR) · airframe 23,360 hrs · 20,842 cycles

PASSENGER DOOR INNER SKIN IS GOUGED AT THE OUTER HANDLE FWD LINK ARM ATTACH FITTING. REPAIRED PAX DOOR INNER SKIN GOUGE IAW EA CRJ252-04087.

Part: VANE — CHAFED (TE FLAP) · airframe 23,360 hrs · 20,842 cycles

RIGHT WING INBD FLAP VANE CHAFED IN 2 PLACES, INBD 1.0"" X .675 X .003 DEEP, MID 1.0"" X .500 X .003 DEEP. CONTINUATION CARD 8798011 OP 164. BLENDED CHAFE ON RT FLAP VANE INBD LOCATION IAW REO 601R-57-52-004. REPLACED SKIN ON MID LOCATION IAW SRM 51-40-11 & 51-42-13.

Part: POST — DAMAGED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

FS 409+128, LBL 18, OTBD VERTICAL POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69, .250" LONG BY GREATER THAN 50% FSH. FAILED NDT INSPECTION. CONTINUATION CARD 8798015 OP 41. R & R INBD & OTBD FS 409+128, LBL 18, VERTICAL POST, STIFFENERS IAW SRMS 51-41-02 & 53-41-19 & REO 601R-53-41-889. THIS IS A MAJOR REPAIR.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

FORWARD SIDE OF FS 621, BULKHEAD HAS 2 GOUGES INBD OF J6CD, TOP SECTION OF BULKHEAD APPROX 1"" LONG X .010"" DEEP. REPAIRED FS 621 BULKHEAD IAW REO 601R-53-61-5661.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

RIGHT FLOOR SEAT TRACKS AT RBL 9 SECTION 1 - 4 ARE CORRODED. R & R RT FLOOR SEAT TRACKS AT RBL 9, SECTION 1-4, IAW AMM 53-01-11-000-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

LEFT SIDE FLOOR SEAT TRACKS AT LBL 9 ARE CORRODED SECTION 1 - 4. R & R LT SIDE FLOOR SEAT TRACKS IAW AMM 53-01-11-400-802.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

FS 280 SUPPORT ANGLE CRACKED AT LBL 9 OTBD SIDE. R & R SUPPORT ANGLE FS 280, LBL 9, OTBD SIDE IAW SRM 51-40-11 & 51-42-21.

Part: HOUSING — DAMAGED (E&E DOOR) · airframe 23,360 hrs · 20,842 cycles

AVI DOOR HANDLE HOUSING HAS AN INDICATION NOTED ALL THE WAY AROUND BASE OF SHAFT 100% FSH. FAILED NDT INSPECTION, CONTINUATION CARD 8798011 OP 169. R & R AVI DOOR HANDLE HOUSING ASSEMBLY, PN H3445-5 IAW SRM 51-42-21. REF 8798011 OPERATIONS 154 & 169 FOR DETAILS OF WORK. ALL OPERATIONS CHECKED GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

ON AFT CARGO FWD DOOR TRACK, AN INTERCOSTAL IS CRACKED. REPLACED CRACKED INTERCOSTAL ON AFT CARGO FWD DOOR TRACK WITH SERVICEABLE INTERCOSTAL IAW SRM 51-42-06, 51-25-16 & AMM 20-21-00-910-801.

Part: INTERCOSTAL — DAMAGED (DOOR) · airframe 23,360 hrs · 20,842 cycles

AFT EQUIPMENT BAY DOOR INTERNAL INTERCOSTAL IS BENT & DAMAGED. REPLACED AFT EQUIPMENT BAY DOOR INTERNAL INTERCOSTAL IAW SRM 51-42-06 & 51-40-11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 23,360 hrs · 20,842 cycles

ANGLE IS CRACKED AT STRINGER 3L, FS 280. R & R FS 280, STRINGER 3L CLIPS IAW SRM 51-42-06 & 51-42-21.

Part: STRUCTURE — CONTAMINATED (APU BAY) · airframe 23,330 hrs · 20,807 cycles

ON CLIMB OUT AT APPROX 20,000 FT, SMELLED BURNING ODOR IN FLIGHT DECK. FLIGHT ATTENDANT SMELLED IT IN GALLEY AS WELL. AS SHE WALKED TOWARD THE REAR OF THE ACFT, SMELL GREW WEAKER, BLEEDS WERE ON & ENGS ANTI-ICE OFF. SUSPECT APU OILS WHERE OVER SERVICED, OIL FOUND IN APU ENCLOSURE. CLEANED OIL FROM ENCLOSURE, SERVICED APU OILS IAW AMM 12-13-49. PERFORMED HIGH POWER RUN FOR 20 MINS WITH BLEEDS ON ENG, NO SMOKE OR SMELL ODOR. WORK PERFORMED IAW AMM 71-00-00. ACFT OK FOR SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 23,118 hrs · 20,586 cycles

FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING RED. DEFERRED FLIGHT ATTENDANT FLASHLIGHT IAW MEL 25-61-04. ENTERED INTO MM O2 & PLACARD INSTALLED. REPLACED FLIGHT ATTENDANT EMER FLASHLIGHT BATTERY & OPERATIONS CHECKED GOOD IAW AMM 25-61-04.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,194 hrs · 19,639 cycles

EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY NR 4 BATTERY CHARGER IAW AMM 33-51-05 AND BATTERY PACK IAW AMM 33-51-04. ALL CHECKED GOOD.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 22,193 hrs · 19,638 cycles

FLAP FAILED AT TAKEOFF 170KT AT 20 DEGREES AT 1.5 MIN. RETURNED TO FIELD. PERFORMED RESET & MESSAGE CLEARED. TROUBLESHOT IAW 27-50-00. R & R FECU IAW AMM 27-51-05. ALL CHECKED GOOD.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 22,171 hrs · 19,609 cycles

FLAPS FAIL CAUTION CAME ON DURING CRUISE, 20 MIN INTO FLIGHT, -40C, 0 FLAP INDICATION, 295 KTS, FLAPS STOPPED, CLEAR SKY. FROM MM02 MEL CONTROL 001050 FLAP FAIL CAUTION. RESET FLAP SYS UNDER MOC DIRECTION IAW FIM, RESET PROCEDURES, MSG NO LONGER REMAINS, CYCLED FLAPS 5 TIMES & PROBLEM DID NOT REOCCUR. DEFERRED FLAP SYS IAW MEL 27-50-00 CAT A UNDER DIRECTION OF MOC TC 4488. ENTERED ITEM IN MM02 PLACARD INSTALLED. PERFORMED TROUBLESHOOTING IAW FIM REV 48 IAW AD 2009-06-12 PARAGRAPH H 6 I, AMOC LOG 14-105 DATED 12 30 2014. INTERROGATED FECU FOR FAULT HISTORY, WHICH FLAGGED THE RT BPSU. PERFORMED CHECK OF WIRING HARNESS TO RT BPSU, NO DEFECTS NOTED IAW FIM 27-50-00. REPLACED RT BPSU IAW AMM 27-51-10. PN OFF 855D100-11, PN ON 855D100-15, SN OFF 2291 & SN ON1965. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 21,430 hrs · 18,881 cycles

COAT CLOSET FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERY IAW AMM 25-61-01. OPERATIONS CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 20,903 hrs · 18,348 cycles

SEAT 1C EMER LIGHTING STRIP IS COMING UP & APPEARS TO BE BROKEN. FOUND RT EMER FLOOR STRIP TO BE DAMAGED 5 INCHES AT FWD END NEXT TO 1C SEAT. DEFERRED IAW MEL 33-51-18, CAT C MM02 UPDATED, PLACARD INSTALLED, ACFT OK FOR SVC. R & R RT FWD EMER FLOOR STRIP IAW CMM 33-51-01. ALL CHECKED GOOD. THIS CLEARS DM 005164, PLACARD REMOVED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,712 hrs · 18,155 cycles

VERY SLIGHT ELEC SMELL IN FLIGHT DECK, DOES NOT SEEM TO BE FROM FRESH AIR VENT. LT SIDE WINDSHIELD WIPER MOVED OFF PARK ABOUT 3 TO 4 INCHES TO THE LT DURING FLIGHT NO FURTHER MOVEMENT NO ASSOC CB POPPED. INSPECTED LT WINDSHIELD WIPER SYS, WIPER & WIPER ARM TO CONVERTER SECURITY CHECKS GOOD, NO UNUSUAL PLAY NOTED. OPERATIONS CHECK OF WIPER SYS GOOD IAW AMM 30-42-00, PARK POSITION CHECKED GOOD. INSPECTED CAPTAIN'S & FIRST OFFICER'S WINDSHIELD WIPER & STALL PANELS FOR POSSIBLE ARCING, NO DEFECTS NOTED. ACFT POWERED UP ALONG WITH APU & BLEEDS ON FOR OVER 1 HR, NO UNUSUAL ODORS DETECTED. COULD NOT DUPLICATE PROBLEM.

Part: SIGN — CRACKED (CABIN) · airframe 20,700 hrs · 18,144 cycles

SERVICE DOOR HANDLE EXIT SIGN CRACKED. R & R SERVICE DOOR EMERGENCY EXIT BETA LIGHT IAW AMM 33-51-09.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,617 hrs · 18,051 cycles

FS 202 BULKHEAD CRACKED AT BRAKE CABLE PASS THROUGH HOLE. REPAIRED IAW REO 601R-53-11-563.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 20,617 hrs · 18,051 cycles

FS 621 BULKHEAD HAS 14 MARKS & 7 DAMAGED RIVET HEADS FROM SCREW. REPAIRED IAW REO 601R-53-61-2155.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,052 hrs · 17,513 cycles

FWD CABIN CEILING EMERGENCY LIGHT INOPERATIVE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,995 hrs · 17,456 cycles

NR 4 CABIN CEILING LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE. R & R NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD IAW AMM 33-51-04.

Part: BATTERY PACK — INTERMITTENT (EMERGENCY LIGHT) · airframe 19,977 hrs · 17,439 cycles

FIRST CEILING EMERGENCY LIGHT INTERMITTENT. REPLACED EMERGENCY NR 1 BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,895 hrs · 17,350 cycles

FIRST CEILING EMERGENCY LIGHT IS INOPERATIVE. FOUND NR 1 BATTERY CHARGER HAD BLOWN FUSE. R & R CHARGER IAW AMM 33-51-05. OPS CHECKED GOOD. R & R LIGHT IAW AMM 33-51-16.

Part: LIFE VEST — DAMAGED (COCKPIT) · airframe 19,776 hrs · 17,226 cycles

PILOT LIFE VEST BAD HAS A HOLE. R & R LIFE VEST AMM 25-61-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,623 hrs · 17,078 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,534 hrs · 16,995 cycles

FORWARD EMERGENCY CEILING FLOOD LIGHT NEAR ROW 2 IS INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,432 hrs · 16,894 cycles

NR 1 CEILING EMERGENCY LIGHT INOPERATIVE.

Part: SKIN — DENTED (BS 364) · airframe 19,314 hrs · 16,785 cycles

MX FOUND A DENT IN THE LT FUSELAGE SKIN AT FS 364 BETWEEN STRINGERS 15-16L . REPAIRED IAW EA CRJ253-01675 AND ASSOCIATED 8110-3.

Part: TRANSPONDER — UNKNOWN (ATC) · airframe 19,241 hrs · 16,713 cycles

F/O`S ATC TRANSPONDER IS FLAGGED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,175 hrs · 16,647 cycles

REFER MEL #8682 CEILING EMERGENCY FLOOR LIGHT INOP. INSTALLED SERVICEABLE BATTERY ASSY, BATTERY CHARGER NO FIX, RE-INSTALLED ORIGINAL BATTERY AND CHARGER BAD CHARGER FROM STOCK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,125 hrs · 16,597 cycles

1ST CEILING EMERGENCY FLOODLIGHT IS INOPERABLE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 18,987 hrs · 16,462 cycles

PILOTS LEFT EXTENSION EMERGENCY LIGHT INOPERABLE. REMOVED & REPLACED LEFT EMERGENCY LIGHT IAW AMM 33-50-00. OPERATIONAL CHECK GOOD.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 18,722 hrs · 16,206 cycles

INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED INFANT LIFE VEST IAW PA 25-096A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,586 hrs · 16,070 cycles

FORWARD OVERHEAD CENTER AISLE EMERGENCY LIGHT IS INOPERABLE. CURRENTLY DEFERRED UNDER DEF-002355-2013.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 18,316 hrs · 15,805 cycles

CURVED MID CABIN E-LIGHT SIGN IS INOP. ALSO PAX ENTRANCE EXIT SIGN & FOUND LIGHT ON AFT SIDE OF WARDROBE INOP & RIGHT WING FWD EXTERNAL E-LIGHT INOP. REMOVED AND REPLACED CHARGER ASSEMBLY NR 2 & 3 IAW AMM 33-51-05, OPS TEST GOOD IAW AMM 33-51-04-740-801.

Part: CHARGER — INOPERATIVE (FLASHLIGHT) · airframe 18,401 hrs · 15,883 cycles

THE NR 1 CEILING LEVEL EMERGENCY FLASHLIGHT IS INOPERATIVE, REMAINING THREE OPERATIVE. REPLACED NR 1 BATTERY CHARGER ASSY PER AMM 33-51-05 THIS CLEARS DM75789. OPS CHECKS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,270 hrs · 15,760 cycles

FS 280 FLOORBEAM CORRODED ON UPPER LBL 3 TO RBL 3. CORROSION REMOVED IAW SRM 53-00-00.

Part: FLOORBEAM — CRACKED (FUSELAGE)

FOUND CRACK IN WEB OF FLOORBEAM AT FS 280 BY LOWER CAP AT LBL 14 AND RBL 14. ALSO FOUND 1 EACH OVERSIZE HOLE IN THE O/B ATTACH CLIP ON LEFT BL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-171 REVISION D.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 17,697 hrs · 15,179 cycles

FLIGHT ATTENDANT POSITION FLASHLIGHT STRAP BROKEN AND RED LED NOT FLASHING. MAINTENANCE REPLACED BATTERY AND STRAP AND OPS CHECKED GOOD IAW AMM 25-61-00-719-801.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 17,497 hrs · 14,976 cycles

FIRST OFFICER`S FLASHLIGHT IS INOPERATIVE. REPLACED BATTERY PACK IAW AMM 25-61-01.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 17,250 hrs · 14,741 cycles

PASSENGER’S PERSONAL PORTABLE 02 DISCHARGED, CREW DECLARED AN EMERGENCY. CREW REPORTS SMOKE IN CABIN. NO FIRE REPORTED. OUTSTATION MX IS NOW INSPECTING AC AND FOUND PHOTOLUMINESCENT FLOOR STRIP HAS BURN MARK AT CENTER AISLE AT ROW 7 1IN BY 1/8IN. REMOVED AND REPLACED PHOTO EMER FLOOR LT STRIP AT SEAT 7 ON A/B SIDE OF AISLE IAW AMM 33-51-01. OP CHECK GOOD. THIS CLEARS DM X62216, PLACARD REMOVED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,129 hrs · 14,630 cycles

FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IS NOT WORKING. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW AMM 25-61-04. OPS CHECK GOOD. OK FOR SERVICE.

Part: SWITCH — FAULTY (NR 2 WOW) · airframe 16,106 hrs · 13,642 cycles

WOW INPUT CAUTION MESSAGE ON EICAS. REMOVED AND REPLACED NR 2 WOW SWITCH IAW AMM 32-61-05.

Part: ELEVATOR — WORN (ELEVATOR) · airframe 14,671 hrs · 12,298 cycles

AIRCRAFT EXPERIENCED MODERATE TO LOW VIBRATION IN CRUISE AT 280-300 KNOTS. NO ABNORMAL INDICATIONS. MAINTENANCE FOUND RT ELEVATOR BOLTS AND BUSHINGS WORN TOO LIMITS (P/N HTS22-DU5-22 AND NAS538B7P13).

Part: BOLT — LOOSE (LG DOOR) · airframe 14,353 hrs · 12,020 cycles

EXPERIENCED "FLUTTER"/VIBRATIONS IN THE AIRFRAME DURING CLIMBOUT AND CRUISE. THIS WAS NOT ASSOCIATED WITH TURBULANCE. IT IS MORE PRONOUNCED AT CLIMBOUT THAN CRUISE VIBRATIONS ARE PRESENT EVEN WITH AUTO PILOT DISENGAGED. VIBRATIONS LAST 3-5 SECONDS. INSP EXTERIOR OF AIRCRAFT FOR LOOSE PANELS, MISSING SEALENT. NO DEFECTS NOTED. INSP ACFT BELLY FAIRINGS SECURITY NO DEFECTS NOTED. FOUND LANDING GEAR AFT DOOR (SPADE DOOR) RT ATTACH HARDWARE LOOSE. RE-SECURED SPADE DOOR BOLT IAW CRJ AMM 20-21-00. OK FOR SERVICE.

Part: HANDLE — CRACKED (E&E DOOR) · airframe 14,360 hrs · 12,002 cycles

MAIN AVIONICS COMPARTMENT DOOR HANDLE, P/N H3445-3, HOUSING WAS FOUND CRACKED AT GSP. FERRY FLIGHT FROM GSP TO MEM IAW PINNACLE PA 52-052 WHERE DOOR HANDLE WAS REPLACED IAW CRJ 200 AMM 52-42-03.

Part: RESERVOIR — BYPASSING (HYD SYSTEM) · airframe 11,380 hrs · 9,138 cycles

GEAR DISAGREE ON APPROACH. REMOVED AND REPLACED HYD RESERVOIR AND PERFORMED GEAR SWINGS.

Part: SELECTOR VALVE — BYPASSING (NLG) · airframe 18,192 hrs · 15,652 cycles

WHILE ON THE VISUAL APPROACH INTO RWY 13 IN BIS ABOUT SEVEN MILES OUT THE NOSE GEAR FAILED TO EXTEND PROPERLY AND WE RECEIVED THE ASSOCIATED "GEAR DISAGREE" WARNINGS. WE ABORTED THE APPROACH AND REQUESTED AN EXTENDED DOWNWIND LEG, WHILE GOING THROUGH THE QRH. REMOVED AND REPLACED NLG SELECTOR VALVE IAW AMM AND OPS CHECK OF EXT/ RET.

Part: UNKNOWN — UNKNOWN (LAVATORY) · airframe 5,902 hrs · 4,590 cycles

SMOKE IN TOILET CAUTION MSG DURING TAKEOFF. LANDING UNEVENTFUL. PERFORMED OPERATIONAL CHECK OF LAVATORY SMOKE DETECTOR IAW BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 26-16-00, OPERATIONALLY CHECKS GOOD.

Part: CONTROL SYSTEM — FAILED (TE FLAPS)

(REF NR: 05-101) FLAP FAILURE MESSAGE ON TAXI. RESET SYSTEM PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. (K)