N8970D

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,821 hrs · 28,773 cycles

FWD CEILING EMERGECNY LIGHT OUT. REMOVED AND REPLACED FORWARD CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-16. OPS CHECK GOOD.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 30,517 hrs · 28,451 cycles

LH INBD FLAP VANE CHAFED 1""L X .5""W JUST OTBD OF ACCESS PANEL 584ET. REMOVED AND REPLACED LH INBD FLAP VANE L/E SKIN IAW CRJ200 SRM TASKS 51-40-11 AND 51-42-10

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 30,517 hrs · 28,451 cycles

LH INBD FLAP VANE CHAFED 1"L X .5"W JUST INBD OF ACCESS PANEL 584DT. REMOVED AND REPLACED LH INBD FLAP VANE L/E SKIN IAW CRJ200 SRM TASKS 51-40-11 AND 51-42-10

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 30,517 hrs · 28,451 cycles

RH INBD FLAP VANE CHAFED 1"L X .5"W JUST OTBD OF ACCESS PANEL 684ET REMOVED AND REPLACED RH INBD FLAP VANE L/E SKIN IAW CRJ200 SRM TASKS 51-40-11 AND 51-42-10

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 30,517 hrs · 28,451 cycles

CARGO FLOOR BEAM (CAP) BETWEEN FS 574 AND FS 621 AT LBL 27 IS CORRODED AT SEVERAL LOCATIONS REMOVED AND REPLACED BEAM (CAP) IAW CRJ 200 SRM 51-40-11, TR51-42, 51-42-21 AND 51-42-23

Part: FLOOR SUPPORT — CORRODED (BS 569-610) · airframe 30,517 hrs · 28,451 cycles

CARGO FLOOR BEAM (CAP) BETWEEN FS 574 AND FS 621 AT LBL 27 IS CORRODED AT SEVERAL LOCATIONS REMOVED AND REPLACED BEAM (CAP) IAW CRJ 200 SRM 51-40-11, TR51-42, 51-42-21 AND 51-42-22

Part: SKIN — CORRODED (LT WING) · airframe 30,517 hrs · 28,451 cycles

LH LOWER WING PLANK ACCESS HOLE AT 540BB IS CORRODED AT SEVERAL LOCATIONS BLEND REPAIRED WING PLANK ACCESS HOLE IAW BOMBARDIER REO 601R-57-21-030 REV L, DATED 2014-02-05.

Part: SKIN — CORRODED (LT WING) · airframe 30,517 hrs · 28,451 cycles

LH LOWER WING PLANK ACCESS HOLE AT 510AB IS CORRODED AT SEVERAL LOCATIONS BLEND REPAIRED WING PLANK ACCESS HOLE IAW BOMBARDIER REO 601R-57-21-030 REV L, DATED 2014-02-05.

Part: BULKHEAD WEB — CRACKED (BS 202.75) · airframe 30,517 hrs · 28,451 cycles

FS202.75 BULKHEAD FWD SIDE @BL23.71 HAS MULTIPLE INDICATORS AROUND ENTIRE CIRCUMFERENCE OF THE PARKING BRAKE CABLE CUTOUT .15"" LONG BY 80% FSH. FAILED NDT INSPECTION COMPLIED WITH REMAINING STEPS OF REO 601R-53-11-563 REV-C. REMOVED & INSTALLED 1EA NEW BRACKET PN#600-90201-113 IAW CRJ 200 SRM 51-40-11-00 TR 51-42-06, 51-42-21 WVAC EMP #774 MTC.

Part: SEAT TRACK — CORRODED (BS 513-544) · airframe 30,517 hrs · 28,451 cycles

LH SIDE SEAT RAIL CORRODED AT 2 EA LOCATIONS BETWEEN F.S. 513 AND F.S. 544 REMOVED TAPE AND COMPLIED WITH REO 601R-53-00-055 DATED 2017-03-21 REV-C REMOVED AND INSTALLED IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802. WVAC EMP# 603145

Part: SKIN — DAMAGED (TE FLAP) · airframe 30,517 hrs · 28,451 cycles

ELONGATED RIVET HOLE FOUND AT THE INBOARD LEADING EDGE OF INBD FLAP VANE PANEL OUTBD OF ACCESS PANEL 584ET. REMOVED TAPE. REMOVED AND REPLACED DAMAGED BUTT STRAP P/N 601R14303-24 IAW CRJ 200 SRM 51-42-06 AND 51-41-02. WVAC STAMP EMP # 722 MTC

Part: SEAT TRACK — CORRODED (BS 529-559) · airframe 30,517 hrs · 28,451 cycles

RH SIDE SEAT RAIL CORRODED AT 3 EA LOCATIONS BETWEEN F.S. 559+32 AND F.S. 559+80. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK AT RBL 9 BETWEEN FS 559+80 AND FS 559+112 IAW CRJ 200 AMM 53-01-01-000-802/400-802 AND GREO 601R-53-00-485 REV D.

Part: SEAT TRACK — CORRODED (BS 529-559) · airframe 30,517 hrs · 28,451 cycles

RH SIDE SEAT RAIL CORRODED BETWEEN F.S. 529 AND F.S. 559+16 AT SEVERAL LOCATIONS. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11-000-802/400-802 AND GREO 601R-53-00-055 REV C. WVAC STAMP EMP# 717 MTC

Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 30,517 hrs · 28,451 cycles

FWD SIDE OF REAR PRESSURE BULKHEAD HAS A CREW CHAFE ON AN EXISTING REPAIR AT RBL 36 REPAIRED CHAFFED AREA ON FWD SIDE OF FS 621 BULKHEAD BY REMOVING AND REPLACING CHAFFED TRIPLER IAW BOMBARDIER REO 601R-53-61-7280 REV-- DATED 2020-01-18. TRIPLER FABRICATED FROM 2024-T3 .063"" PO# W58363. REPAIR PART AND FIELD FASTENER WEIGHT APPROX0.20LBS. WVAC EMP#

Part: SEAT TRACK — CORRODED (BS 559) · airframe 30,517 hrs · 28,451 cycles

CARGO FLOOR SEAT TRACK AT F.S. 559+112 LBL 9 IS CORRODED REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK AT FS 559+112 LBL 9 CRJ 200 AMM 53-01-11-000-802/400-802 AND GREO 601R-53-00-485 REV D. WVAC STAMP EMP# 717 MTC

Part: SEAT TRACK — CORRODED (BS 559) · airframe 30,517 hrs · 28,451 cycles

CARGO FLOOR SEAT TRACK AT FS 559+80 RBL 27 IS CORRODED REMOVED AND REPLACED CARGO FLOOR SEAT TRACK P/N 601R38779-9 AT FS 559+80 & RBL 27 IAW CRJ 200 AMM 53-01-11-400-802. REMOVED TAPE. WVAC STAMP EMP# 711 MTC

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,517 hrs · 28,451 cycles

RIGHT AILERON LEADING EDFGE ACCESS PANEL 699CB HAS 2 AREAS WITH CHAFE DAMAGE, WORST AREA MEASURES APPROX 1" X. .25" X 0.008" DEEP REPAIRED 699CB IAW CRJ 200 SRM 57-60-00, TR51-44 AND 51-25-01. WVAC STAMP EMP# 771 MTC

Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 30,517 hrs · 28,451 cycles

FWD SIDE OF REAR PRESSURE BULKHEAD HAS 10 SCREW CHAFES ON WEB BETWEEN RBL 27 TO LBL 27 AND WL 73.0 TO WL 137 REPAIRED CHAFFED AREAS ON FS 621 BULKHEAD BETWEEN RBL 27 & LBL 27 WL 73.0 TO WL 137 IAW BOMBARDIER REO'S 601R-53-61-1285 REV-E, DATED: 2016-10-31 & 601R-53-61-2155 REV-A DATED 2013-08-13. WVAC EMP# 574771

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 28,096 hrs · 25,863 cycles

FO OXYGEN MASK LEAKING AIR DISCOVERED ENROUTE. PERFORMED DETAILED INSPECTION OF THE CREW O2 FO SIDE MASK AS PER AMM 35-11-12. NO LEAK NOTED AT THIS TIME. A/C GOOD FOR SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 27,703 hrs · 25,420 cycles

KNEE LEVEL EMERGENCY EXIT SIGN IN GALLEY BY SERVICE DOOR DOESN’T LIGHT UP AT ALL. RECONNECTED CONNECTOR PERFORMED OPS CHECK IAW AMM 33-51-00 OPS CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 27,670 hrs · 25,384 cycles

EMERGENCY LIGHT ABOVE THE SERVICE DOOR HAD THE BASE & LENS BROKE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-13-400-801. OPS TESTED GOOD IAW AMM 33-51-00-710-801.

Part: BRACKET — CRACKED (FUEL FILL NECK) · airframe 27,670 hrs · 25,384 cycles

SINGLE POINT REFUEL FILL NECK SUPPORT BRACKET WAS CRACKED. REMOVED & REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06, AND SRM 51-41-02.

Part: STIFFENER — CRACKED (APU BAY) · airframe 27,670 hrs · 25,384 cycles

INSIDE APU ENCLOSURE FORWARD LT STIFFENER WAS CRACKED AT TOP. FABRICATED AND INSTALLED DOUBLER OF WELD CRACKS IAW EA CRJ249-07093.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 27,670 hrs · 25,384 cycles

HYD PRESSURE TRANSDUCER MOUNTING BRACKET WAS CRACKED IN THE RT MLG WHEEL WELL, ON THE PRESSURE FLOOR LOWER SURFACE. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 621-625) · airframe 27,670 hrs · 25,384 cycles

ANGLE FROM BS 621 TO 625, BS 621 BULKHEAD AFT FACE STGR 15L IS CRACKED. REMOVED THE ANGLE, FABRICATED, AND INSTALLED THE NEW ANGLE IAW SRM 51-42-21, SRM 51-40-11, AND SRM 51-24-36.

Part: STIFFENER — CRACKED (EXHAUST FAIRING) · airframe 27,670 hrs · 25,384 cycles

LEFT ENGINE EXHAUST FAIRING, CIRCUMFERENTIAL STIFFNER WAS CHAFED AND CRACKED AT THE FIVE O`CLOCK POSITION. REPAIRED THE STIFFNER IAW CMM 78-11-00-306-810-A01.

Part: SKIN — CORRODED (RT WING) · airframe 27,670 hrs · 25,384 cycles

RIGHT WING FUEL STORAGE ACCESS PANEL LANDING, AT WS 640BB HAD FRETTING CORROSION. REMOVED THE CORROSION AND RESTORED FINISH IAW REO 601R-57-21-030, REV L.

Part: SKIN — CORRODED (LT WING) · airframe 27,670 hrs · 25,384 cycles

LEFT WING FUEL STORAGE ACCESS PANEL LANDING AT WS 540BB HAD FRETTING CORROSION. REMOVED CORROSION AND RESTORED FINISH IAW REO 601R-57-21-030.

Part: OXYGEN MASK — NO TEST (FLT ATTEND) · airframe 27,670 hrs · 25,384 cycles

OXYGEN MASKS FAILED TO DEPLOY. REMOVED & REPLACED THE F/A OXYGEN MASK LATCH ASSY IAW AMM 32-21-05. OPS CHECKED GOOD.

Part: PANEL — CRACKED (PAX DOOR RISER) · airframe 27,670 hrs · 25,384 cycles

PAX DOOR AFT RISER IS CRACKED AT THE LOWER STEP CORNER. REMOVED THE CRACK.

Part: RISER — CRACKED (PAX DOOR) · airframe 27,670 hrs · 25,384 cycles

PAX DOOR AFT RISER CRACKED IN RADIUS SECOND STEP FROM THE BOTTOM. REMOVED THE CRACK. FOUND WITHIN LIMITS. IAW SRM 53-00-00.

Part: DRAG ANGLE — CRACKED (LT WING) · airframe 27,670 hrs · 25,384 cycles

LEFT WING INBD DRAG ANGLE SUPPORT STRUCTURE WAS CRACKED AT WS 48, LT MLG WW AREA. CUT OUT THE DAMAGE IAW REO 601R-57-51-046, REV B, REPAIR 2, & INSTALLED IAW REO 601R-57-51-046, REV B, REPAIR 2.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 27,670 hrs · 25,384 cycles

CARGO DOOR SILL FLAP HINGE WAS FOUND CRACKED. REMOVED AND REPLACED THE HINGE IAW SRM 51-42-06.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 27,670 hrs · 25,384 cycles

CARGO DOOR SILL FLAP CENTER HING EHAS SEVERAL CRACKED AND CORRODED LUGS. REMOVED AND REPLACED THE HINGE IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 27,670 hrs · 25,384 cycles

AT BS 280, STRINGER 3, THE ANGLES INBD AND OTBD WERE CRACKED, TWO PLACES. REMOVED AND REPLACED THE ANGLES IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 27,670 hrs · 25,384 cycles

THE ANGLE ON THE FWD SIDE OF THE BS 280 FLOORBEAM WAS CRACKED JUST INBD OF LBL 12, IN THE VERY FWD E & E BAY. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06, AND SRM 51-42-21.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 27,371 hrs · 25,082 cycles

LEFT CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED& REPLACED THE LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,268 hrs · 24,971 cycles

DURING LINE CHECK, THE EXTERIOR AND INTERIOR EMERGENCY LIGHTS DID NOT ILLUMINATE. R & R THE BATTERY PACK AT PS3LF IAW 33-900-701, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,250 hrs · 24,952 cycles

EMERGENCY LIGHTS FOUND INOPERATIVE. REPLACED AND CHARGED THE BATTERY PACKS IAW AMM 33-51-04. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,309 hrs · 23,881 cycles

OUTSIDE EMERGENCY LIGHTS BY PAX DOOR AND SERVICE DOOR FOUND INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT POSITION PS1LF IAW CARD 33-900-701, OPS CHECKED GOOD.

Part: BPSU — INOPERATIVE (TE FLAPS) · airframe 25,282 hrs · 22,798 cycles

CREW REPORTED FLAP FAIL MESSAGE AT 20 DEGREES. PERFORMED TROUBLESHOOTING IAW FIM 27-50-00 REV 51 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), . FOUND EVIDENCE OF MOISTURE INGRESS AND MODERATE CORROSION ON BPSU ELECTRICAL CONNECTOR. THIS, IN COMBINATION WITH LRU "MOST PROBABLE" MESSAGE STRING LED TO THE R & R OF THE LT BPSU IAW AMM 27-51-10. FLAPS OP CHECKED GOOD IAW AMM 27-54-00.

Part: BATTERY PACK — INOPERATIVE (EMREGENCY LIGHTS) · airframe 24,709 hrs · 22,231 cycles

EMERGENCY LIGHTS CAME ON BRIEFLY. THEN WENT OUT. REMOVED AND REPLACED ALL FOUR BATTERY PACKS IAW AMM 33-51-04. OPS CHECKED GOOD IAW AMM 33-51-04.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,933 hrs · 21,450 cycles

FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE. DEFERRED IAW MEL 25-61-04 ACT C PLACARD INSTALLED & TRANSFERRED TO MMO2. REPLACED FLIGHT ATTENDANT EMER FLASHLIGHT IAW AMM 25-61-02. OPERATIONS CHECKED GOOD. MMO2 UPDATED & PLACARD REMOVED. THIS CLEARS MEL CONTROL 3285537-1.

Part: LIGHT — WORN (CABIN) · airframe 23,780 hrs · 21,297 cycles

ALL CABIN PATH LIGHTING STAINED & WORN. DISCARDED & REPLACED ALL CABIN PATH LIGHTING IAW AMM 33-51-01-960-801 STEP 3A & 33-51-01-400-806 STEP 3A2. FOUND ON PANEL RACK. INSTALL TO BE COMPLIED WITH ON NR SN 4459697 1012648 2000-0088.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 23,780 hrs · 21,297 cycles

PASSENGER DOOR OPENING, LOWER FRAME LONGERON, LOWER ANGLE HAS CORROSION, BETWEEN FS 310 & 349, IN CABIN. R & R PAX DOOR OPENING, LOWER SILL ASSEMBLY, BETWEEN FS 310 & 349 IAW SRM 51-42-21 & SRM 51-42-20.

Part: WEB — CRACKED (PAX DOOR) · airframe 23,780 hrs · 21,297 cycles

PASSENGER DOOR UPPER WEB AFT CORNER IS CRACKED. FABRICATED, R & R REPAIR ANGLE & FILLER ON UPPER AFT WEB CORNER ON PAX DOOR IAW REO 601R-52-11-279.

Part: ANGLE — CRACKED (OAX DOOR) · airframe 23,780 hrs · 21,297 cycles

PASSENGER DOOR AFT RISER SUPPORT, ANGLE IS CRACKED AT ASSIST MOTOR GUIDE PULLEY. R & R EXISTING REPAIR IAW REO 601R-52-11-513, SRM 51-42-13 & SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,780 hrs · 21,297 cycles

RIGHT AISLE SEAT TRACK STICK 2 HAS CORROSION IN CABIN. R & R NEW RT AISLE SEAT TRACK STICK 2 IAW AMM 53-01-11 SUBTASK 53-01-11-420-001.

Part: STRIP — CORRODED (FUSELAGE) · airframe 23,780 hrs · 21,297 cycles

FLOORBOARD LANDING HAS CORROSION FS 589, LBL 9 - 27. R & R CAP STRIP IAW SRM 51-42-06.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 23,780 hrs · 21,297 cycles

FLOORBEAM ATTACHMENT LBL 27, FS 621.00 HAS A CORRODED FASTENER HOLE OTBD FLANGE. REPAIRED FLOORBEAM ATTACHMENT LBL 27, FS 621.00 IAW EA CRJ253-04058.

Part: BEAM — CRACKED (FUSELAGE) · airframe 23,780 hrs · 21,297 cycles

BEAM 280 IS CRACKED JUST OTBD OF LBL 9, LOWER SIDE, BELOW FLOOR. PERFORMED REPAIR TO THE CRACK IN FS 280 BEAM AT LBL 9 IAW REO 601R-53-11-171.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,780 hrs · 21,297 cycles

FORWARD FACE AT LINTEL FITTING BULKHEAD WEB CRACKED AT INBD EDGE. REPAIRED FWD FACE AT LINTEL FITTING BULKHEAD WEB IAW REO 601R-53-61-1230.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 23,780 hrs · 21,297 cycles

LEFT OVERWING EMER EXIT HANDLE FAILED FUNCTIONAL CHECK. LUBED OVERWING LT EXIT DOOR IAW AMM 12-20-52, FUNCTIONAL TEST OF LT OVERWING EXIT DOOR GOOD IAW AMM 52-21-00-710-801.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 23,780 hrs · 21,297 cycles

LEFT INTERCOSTAL AT STRINGER L14 & AFT SIDE OF FS 621 BULKHEAD IS CRACKED. REMOVED INTERCOSTAL L14, STATION 621 & INSTALLED NEW INTERCOSTAL IAW SRM 51-42-21 AP-208.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 23,780 hrs · 21,297 cycles

LEFT INTERCOSTAL AT STRINGER L13 & AFT SIDE OF FS 621 BULKHEAD IS CRACKED. REMOVED INTERCOSTAL, INSTALLED NEW INTERCOSTAL L13, STATION 621 IAW SRM 51-42-21 AP-208.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 23,780 hrs · 21,297 cycles

LEFT INTERCOSTAL AT STRINGER L 16 & AFT SIDE OF FS 621, BULKHEAD IS CRACKED. REMOVED L 16 INTERCOSTAL & INSTALLED NEW INTERCOSTAL IAW SRM 51-42-21.

Part: ESCAPE HATCH — LACK OF LUBE (COCKPIT) · airframe 23,780 hrs · 21,297 cycles

FUNCTIONAL TEST OF THE CREW ESCAPE HATCH FAILED. LUBE CREW ESCAPE HATCH IAW AMM 12-20-52. FUNCTIONAL TEST OF CREW ESCAPE HATCH GOOD IAW AMM 52-22-00-720-801.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 23,780 hrs · 21,297 cycles

LEFT INTERCOSTAL AT STRINGER L15 & AFT SIDE OF FS 621 BULKHEAD IS CRACKED. REMOVED INTERCOSTAL LT L15, STATION 621 & INSTALLED NEW INTERCOSTAL IAW SRM 51-42-21 AP-208.

Part: TRACK — DAMAGED (CABIN) · airframe 23,682 hrs · 21,194 cycles

REFLECTIVE FLOOR TRACK ON FWD RT SIDE OF CABIN DAMAGED. R & R DAMAGED SECTION OF REFLECTIVE FLOOR TRACK IAW AMM 33-51-01. PN OFF & ON PL22-300LH00.

Part: BRAKE — JAMMED (MLG) · airframe 23,277 hrs · 20,789 cycles

RIGHT MAIN BRAKES SMOKE, BOTH BRAKES T INDICATING 6 - 7, USED COCKPIT FIRE EXTINGUISHER. DURING TAXI FELT BRAKES DRAGGING. INSPECTED RT MAIN BRAKES IAW AMM 32-43-00. FOUND OTBD BRAKE TO BE JAMMED. R & R BOTH MLG BRAKES IAW AMM 32-43-26. OPERATIONS CHECKED NORMAL. R & R BOTH RT MWA IAW AMM 32-41-01. VERIFIED SPACERS INSTALLED.

Part: OXYGEN MASK — FAILED · airframe 23,085 hrs · 20,587 cycles

ONE PORTABLE O2 MASK, RED, FAILED TO INFLATE. R & R ONE PORTABLE O2 MASK, RED, IAW AMM 35-31-01.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 22,888 hrs · 20,401 cycles

FUEL ODOR IN BLEEDS ON BOTH APU & ENGINE BLEEDS. MORE NOTICEABLE WHEN RAISING CABIN TEMPERATURE. R & R, LT & RT COALESCER SOCKS IAW AMM 21-51-13 IAW SMOKE & FUMES WORK SCOPE. FLIGHT CREW OPERATE ENGINES & PACKS FOR 30 MINUTES, ALL CHECKED GOOD. AIRCRAFT OK FOR SERVICE.

Part: COALESCER BAG — ODOR (AC BAY) · airframe 22,892 hrs · 20,406 cycles

FUEL ODOR IN BLEEDS ON BOTH APU & ENG BLEEDS. MORE NOTICEABLE WHEN RAISING CABIN TEMP. R & R LT & RT COALESCER SOCKS IAW AMM 21-51-13, IAW SMOKE& FUMES WORK SCOPE. FLIGHT CREW OPERATED ENGS & PACKS FOR 30 MINUTES, ALL CHECKED GOOD. ACFT OK FOR SERVICE.

Part: COLLAR — MIGRATED (NLG) · airframe 22,693 hrs · 20,193 cycles

GEAR DISAGREE MASTER WARNING WITH NOSE DOOR MASTER WARNING ON TAKEOFF. QRH COMPLETED, NOSE GEAR DOWN & GREEN MAINS UP NO OVERWEIGHT LANDING. FOUND TOW GUARD TOW BAR LESS COLLAR MIGRATED. REMOVED & REINSTALLED TOW BAR LESS COLLAR IAW WITH PA 32-066C. SEE NON-ROUTINE CARD N78199 FOR FURTHER DETAILS. FOUND & REPLACED OLEO STRUT EXTENDED & CENTERED SENSOR BRACKET BENT PN APM16215-105 EXP.

Part: LIFE VEST — WRONG PART (COCKPIT) · airframe 22,494 hrs · 19,979 cycles

F/O'S LIFE VEST WRONG TYPE. R & R F/O'S LIFE VEST WITH PROPER TYPE, REF AMM 25-61-03.

Part: DOOR — NOISY (SERVICE DOOR) · airframe 22,350 hrs · 19,818 cycles

LOUD SQUEAL FROM SERVICE DOOR IN FLIGHT, ALL PRESS INDICATIONS NORMAL & SQUEAL WENT AWAY AT DP OF 7.1. PERFORMED VISUAL INSPECTION OF SERVICE DOOR SEAL IAW AMM 52-41-07, NO DEFECTS NOTED. PERFORMED OPERATIONS TEST OF CABIN PRESSURIZATION SYS IAW AMM 21-31-00, NO LEAKS NOTED. ACFT OK FOR SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 21,464 hrs · 18,907 cycles

NOSE GEAR DOOR OPEN WARNING MSG WITH ASSOCIATED GEAR DISAGREE AFTER TAKEOFF ON RETRACTION WITHIN 2 SECONDS. CAPTAIN FOLLOWED QRH & RETURNED. GEAR DOOR & DISAGREE MSGS WENT OUT ON EXTENSION & LANDED NORMALLY. AN EMER WAS NOT DECLARED. FOUND PROX SWITCH PS14GA OUT OF LIMITS. ADJUSTED INTO LIMITS IAW AMM 32-61-05. OPERATIONS CHECKED LANDING EXTENSION & RETRACTION IAW AMM 32-33-00. OPERATIONS CHECKED NORMAL OK FOR SERVICE.

Part: COVER — MISSING (EXIT SIGN) · airframe 21,328 hrs · 18,772 cycles

AMBER COVER ON MID CABIN OVERHEAD EXIT SIGN IS MISSING ON AFT SIDE. REPLACED MISSING AMBER LIGHT COVER ON AFT EXIT SIGN IAW AMM 33-51-14, OK FOR SERVICE.

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 20,829 hrs · 18,278 cycles

AFT PRESS BULKHEAD CTR VERTICAL STIFFENER HAS CHAFING DAMAGE. REPAIRED IAW REO 601R-53-61-1523.

Part: ECS — CONTAMINATED (AC BAY) · airframe 20,487 hrs · 17,938 cycles

TAKE OFF ROLL, THICK WHITE SMOKE OBSERVED IN COCKPIT & CABIN AS REPORTED BY FLIGHT ATTENDANT, NO OTHER. ABNORMAL INDICATIONS, SMOKE SMELLED LIKE BURNING, DE-ICING FLUID. EXAMINATION OF DISC, RESIDUAL SMELL ON CABIN & GVI OF ECS SYS INDICATES THAT SUSPECTED DE-ICING FLUID CONTAMINATION OCCURRED PRIOR TO TAKEOFF. R & R RT & LT COALESCER ELEMENTS IAW AMM 21-51-13. OPERATIONS CHECKED GOOD, NO SMELL OR SMOKE NOTED AFTER 2+ OPERATION CYCLES UNDER APU & ENG PNEUMATIC FEED, ACFT OK FOR SERVICE.

Part: CONTAINER — TORN (LIFE VEST) · airframe 19,862 hrs · 17,329 cycles

F/O LIFE VEST BAG TORN. R & R F/O LIFE VEST IAW AMM 25-61-03.

Part: CONTAINER — TORN (LIFE VESWT) · airframe 19,862 hrs · 17,329 cycles

F/O LIFE VEST BAG TORN. R & R F/O LIFE VEST IAW AMM 25-61-03.

Part: FLAP — MALFUNCTIONED (WING) · airframe 19,151 hrs · 16,643 cycles

ON FLIGHT 3711 (BWI TO RDU) ON APPROACH INTO RDU RECEIVED FLAP FAIL AT 30 AT 170 KTS. AIRCRAFT LANDED SAFELY. RESET FLAPS PER OA AD27-052K AND DEFERRED PER MEL 27-50-00 FOR 10 CYLCES. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIMREV44 IAW AD 2009-06-12 PARA H6I AMOC DATED DEC 7, 2012 ANDPA AD 27-052K. REMOVED AND REPLACED FECU.

Part: BEAM — CRACKED (FUSELAGE) · airframe 19,123 hrs · 16,617 cycles

FS 409+128 BULKHEAD VERTICAL BEAM AT LBL 27 INBOARD STIFFENER AT LOWER FASTENER HOLE CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-41-056.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,123 hrs · 16,617 cycles

FS 559 SEMI-PRESSURE BULKHEAD CAP ANGLE CRACKED AT RBL 18 AND LBL 18. REPAIRED IAW PA 53-025C AND BOMBARDIER REO 601R-53-41-260 AND 601R-53-41-609.

Part: UNKNOWN — OUT OF ADJUST (RT ENGINE) · airframe 18,878 hrs · 16,383 cycles

ON FLIGHT 4187 (MSP TO YYZ) CREW REPORTED THAT NR 2 ENGINE N1 TAKES MORE THAN 10 SEC TO REACH 50% ON TAKEOFF. THEY ABORTED TAKEOFF AT 20 KNOTS AND AIRCRAFT RETURNED TO THE GATE. ADJUSTED RIGHT ENGINE IDLE SPEED TO LIMITS IAW AMM 71-00-00. COMPLETED RIGHT ENGINE ACCELERATION CHECK IAW AMM 71-00-00. ACCELERATION TIME WITHIN LIMITS.

Part: DOOR — NONE (PAX) · airframe 18,162 hrs · 15,673 cycles

PAX DOOR IS VERY DIFFICULT TO OPEN FROM THE OUTSIDE. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-10-00. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,093 hrs · 15,606 cycles

REAR UPPER CABIN EMERGENCY LIGHT INOPERATIVE. LAMPED LIGHT.

Part: SWITCH — DIRTY (THRUST REVERSER) · airframe 18,026 hrs · 15,547 cycles

LEFT THRUST REVERSER WOULD NOT STOW. CLEANED STOW AND DEPLOY SWITCH IAW AMM 20-10-00. PERFORMED OPS CHECK IAW AMM 78-30-00. OPS CHECK GOOD NO DEFECT NOTED.

Part: THRUST REVERSER — MALFUNCTIONED (LEFT) · airframe 17,973 hrs · 15,491 cycles

LEFT THRUST REVERSER INOPERATIVE. PERFORMED OPS CHECK OF LEFT HAND THRUST REVERSER IAW AMM 78-30-00. AIRCRAFT OK FOR SERVICE.

Part: CONTAINER — TORN (LIFE VEST) · airframe 17,966 hrs · 15,485 cycles

CAPTAIN'S LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN'S LIFE VEST IAW AMM 25-61-03.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · corrosion level 2 · airframe 17,239 hrs · 14,745 cycles

FLOOR SUPPORT AT FS 280 IS CRACKED AT UPPER AND LOWER RBL 9 AND CORRODED ON UPPER FLANGE BETWEEN RBL 9 AND LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-171, 601R-53-11-137, 601R-53-11-138.

Part: BONDING JUMPER — SHORTED (ANTI-ICE SYS) · airframe 17,929 hrs · 15,090 cycles

ANTI-ICE DUCT WARNING MESSAGE ON CLIMBOUT. FOUND SEVERAL LT LEADING STUD GROMMETS, SEVERAL THERMAL SW'S, AND OUTB PICCOLO BONDING WIRE SHORTED. NON-ROUTINE CARD N30477 AND N30497. SYSTEM OPC GOOD IAW AMM 30-11-00. FOUND LT OTBD L/E PICCOLO TUBE BONDING WIRE INCORRECTLY ROUTED. REROUTED BONDING STRAP IAW ESPM 20-15-00. OPC SYSTEM SEVERAL TIMES. ANTI-ICE SYSTEM OPC GOOD IAW AMM 30-11-05.

Part: SWITCH — DEFECTIVE (BLEED AIR SYS) · airframe 17,929 hrs · 15,090 cycles

ON DEP WITH WING ANTI ICE OFF, GOT ANTI ICE DUCT WARNING, MSG THEN WENT AWAY. LATER WITH IT ON NORM IT CAME BACK, ALSO IN STBY MODE, ALL LEFT LEADING EDGE. FOUND LT O/B SECTION LEAK DET CIRCUIT SHORTING WHEN HOT. REMOVED AND REPLACED ALL O/B SWITCHES & OP CHECK GOOD IAW AMM 36-21-00. LT WING OVERHEAT WARNING MESSAGE INFLIGHT. T/S SYSTEM FOUND LT LEADING EDGE OUTBOARD CIRCUIT HAVING HIGH RESISTANCE CHECKED FOR WIRING. WIRING CHECKED GOOD. REMOVED AND REPLACED S27WK. SYSTEM OPC GOOD IAW AMM 36-21-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 16,854 hrs · 14,264 cycles

F/O'S EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED F/O FLASHLIGHT BATTERY IAW AMM 25-60-00. OPS CHECK GOOD.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,874 hrs · 12,529 cycles

DEEP CORROSION, PITTING, OF SERVICE DOOR SILL PLATE ASSY. REMOVED AND REPLACED SERVICE DOOR SILL PLATE IAW AMM 25-33-01.

Part: DOOR — DENTED (CABIN) · airframe 14,532 hrs · 12,217 cycles

MULTIPLE DENT DAMAGE (3 PLACES WITHIN CLOSE PROXIMITY OF EACH OTHER) FOUND TO PAX DOOR OUTER SKIN BETWEEN FS 338.96 AND FS 347.27 AND BETWEEN DOOR DATUM NR 5 AND NR 6. DENT DIMENSIONS ARE AS FOLLOWS: DENT 'A': 0,50"L X 0,50"W X 0.008" DEEP, DENT 'B': 2,25"L X 1,375"W X 0.062" DEEP, DENT 'C': 0.50"L X 0,50"W X 0.005" DEEP. TEMPORARY REPAIR AND FLY ON IAW BOMBARDIER RE0601R-52-11-1881A INSPECTION INTERVALS EVERY 300 FH FLY ON FOR 3600 FH WITHIN WHICH TIME A PERMANENT REPAIR WILL BE MADE.

Part: SMOKE WARNING — ACTIVATED (LAVATORY) · airframe 6,158 hrs · 4,906 cycles

TOILET SMOKE MESSAGE AFTER TAKEOFF, PILOT DELCARED EMERGENCY, PERFORMED QRH, LANDING UNEVENTFULL. DEFERRED APU IAW MEL.

Part: ACM — CONTAMINATED · airframe 6,052 hrs · 4,827 cycles

AIR RETURN TO SWF, AFTER RECEIVING SMOKE TOILET MESSAGE ON TAKEOFF. GROUND RUNS AND OPERATIONAL CHECKS OF ACM SYSTEM PERFORMED NO DEFECTS. DETERMINED TO BE RESIDUAL DE-ICE FLUID INTO ACM SYSTEM.

Part: ADG — DEPLOYED (ELECTRICAL SYS) · airframe 3,967 hrs · 3,117 cycles

IN CRUISE FLIGHT FROM DWT TO TYS, THE FLIGHT CREW DETECTED A VIBRATION COMING FROM THE NOSE AREA OF THE AIRCRAFT. NO ABNORMAL INDICATIONS WERE DISPLAYED ON ECAIS. THE FLIGHT ATTENDANT REPORTED THAT THERE WAS NO UNUSUAL NOISE OR VIBRATION IN THE CABIN. THE FLIGHT CREW ELECTED TO CONTINUE THE APPROACH INTO TYS, A MAJOR REPAIR BASE FOR THE AIRLINE. ATC WAS NOTIFIED AND AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE AT TYSON-MCGEE. MAINTENANCE DISCOVERED THE AIR DRIVEN GENERATOR PARTIALLY DEPLOYED. THE ADG WAS INSPECTED, TESTED AND RESTOWED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 3,647 hrs · 2,847 cycles

IN CRUISE RECEIVED STAB/MACH TRIM MESSAGE WITH DISCONNECT. QRH PERFORMED EMERGENCY DECLARED WITH UNEVENTFUL LANDING. SYSTEM RESET FOLLOWING MFG FIM, OPERATIONALLY CHECKED GOOD.