N8977A

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 24,805 hrs · 22,180 cycles

OBSERVERS OXYGEN MASK BROKEN. R & R THE OBERVER'S OXYGEN MASK IAW AMM 35-11-12. LEAK CHECKED GOOD IAW AMM 35-11-12-790-001, OPS CHECKED GOOD IAW AMM 35-10-0-710-802.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 24,596 hrs · 21,971 cycles

CAPTAIN`S FLASHLIGHT ISN'T BLINKING. REMOVED AND INSTALLED SERVICABLE CAPTAIN`S FLASHLIGHT BATTERY IAW AMM 25-61-00. OPS CHECK GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

CARGO DOOR SILL IS CORRODED AROUND NUTPLATES. CONTINUATION CARD 8797711 OP 189. R & R CARGO SILL PLATE IAW REO 601R-53-61-1574 REV B & SRM 51-42-06 21 13. REF JC 8797711 OP 150 STEPS 1 - 6 FOR WORK PERFORMED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

EXTERIOR FUSELAGE SKIN AT FS 605, APPROX 1" UNDER CARGO DOOR SCUFF PLATE IS GOUGED, APPROX 1" L X 1/8" W X .005" D WITH HIGH METAL. CONTINUATION CARD 8797711 OP 201. REPAIRED FUSELAGE SKIN IAW EA CRJ253-04007 REV A, DTA DUE WITHIN 12 MOS FROM 02 13 16 IAW NRWC 527021.

Part: RETAINER — DENTED (PAX DOOR) · airframe 23,544 hrs · 20,904 cycles

PASSENGER DOOR SEAL RETAINER AT TOP OF STEP HAS A SMALL AREA THAT IS DENTED, APPROX 1.5 X .020. R & R SEAL RETAINER ON PAX DOOR IAW REO 601R-52-11-915 & SRM 51-42-13.

Part: FITTING — CORRODED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

FLOORBEAM ATTACHMENT TO FS 621.00 REAR PRESS BULKHEAD, LBL 27, HAS MINOR CORROSION AT BOTH REAR MOST FLOORBOARD ATTACHMENT HOLES. CONTINUATION CARD 8797711 OP 162 & 183. R & R FS 621, LBL 27 FITTING IAW SRM 51-40-11, 51-42-06, 51-42-21 & AMM 20-21-00-910-801. REF JC 8797711 OP 125 STEPS 1 - 6, JC 8797711 OP 162 STEPS 7 - 12 & JC 8797711 OP 183 STEP 13 FOR WORK PERFORMED.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

RIGHT FLOOR SILL IN CARGO BAY, FS 559+80 - 621 HAS CORROSION AROUND NUTPLATES. CONTINUATION CARD 8797711 OP 169 & 194. R & R CORRODED FLOOR SILL WITH NEW SERVICEABLE FLOOR SILL IAW SRM 51-42-06 & 51-42-21. REF JC 8797711 OP 146 STEPS 1 - 6 & JC 8797711 OP 169 STEPS 7 - 12 FOR WORK PERFORMED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

FS 589 FRAME IS CORRODED AT STRINGER 27 ON FWD & AFT FACE. CONTINUATION CARD 8797711 OP 175. REMOVED CORRODED FRAME AT FS 589 & INSTALLED SERVICEABLE FRAME AT FS 589 IAW SRM 51-42-06 & 51-42-21.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

FS 605 FRAME IS CORRODED, BETWEEN STRINGERS 25L & 25R. REMOVED CORRODED FS 605 FRAME & INSTALLED SERVICEABLE FS 605 FRAME IAW SRM 51-42-06 & 51-42-21.

Part: SPLICE — BROKEN (CABIN) · airframe 23,544 hrs · 20,904 cycles

GALLEY TRIM PANEL EMER WIRE SPLICE BROKEN. REPAIRED GALLEY TRIM PANEL EMER WIRE SPLICE IAW ESPM 20-17-10. OPERATIONS CHECKED GOOD.

Part: PANEL — DAMAGED (WINGLET) · airframe 23,544 hrs · 20,904 cycles

WINGLET PANEL 672AL HAS AN ELONGATED HOLE, NEEDS FURTHER INVESTIGATION. RECEIVED SERVICEABLE WINGLET PANEL 672AL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

FLOOR SEAT TRACKS ON LBL 9 & RBL 9, FS 559 - 559+96 HAVE SEVERAL AREAS OF CORROSION. R & R FLOOR SEAT TRACKS IAW AMM 53-01-11-400-802.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

ANGLE AT FS 589 BELOW CARGO SILL IS CRACKED. REMOVED CRACKED ANGLE AT FS 589. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-40-11 & 51-42-21.

Part: SEPARATOR — DAMAGED · airframe 23,544 hrs · 20,904 cycles

PANEL 412DB SEAL RETAINERS & FWD SEPARATOR KNIFE EDGED & CRACKED. R & R SEPARATOR IAW SRM 51-42-06 & REPAIRED SEAL RETAINER IAW EA CRJ254-04005 REV 1R.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

LEFT FLOORBEAM CAP HAS CORROSION AROUND FASTENER HOLES, FS 574 - 621. R & R FLOORBEAM CAP IAW SRM 51-40-11, 51-42-21 22 & 51-42-34.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

LEFT SIDE CABIN FLOOR SEAT RAIL FROM FS 409+126 - 559+4, LBL 9, HAS SEVERAL AREAS OF CORROSION. REMOVED UNSERVICEABLE FLOOR SEAT RAIL, LT SIDE. INSTALLED SERVICEABLE FLOOR SEAT RAIL, 601R31032-75, IAW AMM 53-01-11-000-802 -400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

RIGHT SIDE CABIN FLOOR SEAT RAIL FROM FS 409+126 - 559.4, RBL 9, HAS SEVERAL AREAS OF CORROSION. REMOVED UNSERVICEABLE RT FLOOR SEAT RAIL. INSTALLED SERVICEABLE FLOOR SEAT RAIL, 601R31032-75, IAW AMM 53-01-11-000-802-400-802.

Part: SKIN — CORRODED (LT WING) · airframe 23,544 hrs · 20,904 cycles

LEFT WING LOWER WING PLANK ACCESS HOLE 550AB, WS 163.000 HAS FRETTING CORROSION AT OTBD END MEASURING APPROX 0.4" LONG X 0.08" WIDE X 0.002" DEEP. REPAIRED 550AB CUT OUT IAW GREO 601R-57-21-030 REV L DATED 02 05 14. THIS IS A MAJOR REPAIR. REF TO ATTACHED REO FOR WORK PERFORMED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 23,544 hrs · 20,904 cycles

CARGO BAY SEAT TRACK ON RBL 27, FS 559+80 - 559+96 IS CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801.

Part: SKIN — CORRODED (LT WING) · airframe 23,544 hrs · 20,904 cycles

LEFT WING LOWER WING PLANK ACCESS HOLE 510AB, WS 12.245 HAS FRETTING CORROSION AT INBD & OTBD ENDS. INBD CORROSION MEASURES APPROX 6.5" LONG X 0.20" WIDE X 0.002" DEEP. OTBD CORROSION MEASURES APPROX 8.0" LONG X 0.15" WIDE X 0.002" DEEP. REPAIRED 510AB CUT OUT IAW GREO 601R-57-21-030 REV L DATED 02 05 14. THIS IS A MAJOR REPAIR. REF TO ATTACHED REO FOR WORK PERFORMED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

CARGO BAY SEAT TRACK ON RBL 9, FS 559+112 - 574 IS CORRODED. REMOVED UNSERVICEABLE & INSTALLED SERVICEABLE SEAT TARCKS IN CARGO AREA IAW AMM 53-00-49-000-801 & AMM 53-00-49-400-801.

Part: SKIN — CORRODED (LT WING) · airframe 23,544 hrs · 20,904 cycles

LEFT WING LOWER WING PLANK ACCESS HOLE 540BB, WS 54.897 HAS FRETTING CORROSION AT INBD & OTBD ENDS. INBD CORROSION MEASURES APPROX 9.75" LONG X 0.20" WIDE X 0.003" DEEP. OTBD CORROSION MEASURES APPROX 10.5" LONG X 0.20" WIDE X 0.003" DEEP. REPAIRED 540BB CUT OUT IAW GREO 601R-57-21-030 REV L DATED 02 05 14. THIS IS A MAJOR REPAIR. REF TO ATTACHED REO FOR WORK PERFORMED.

Part: FITTING — CHAFED · airframe 23,544 hrs · 20,904 cycles

PANEL 412BT FWD CLIPS CHAFED. R & R CLIPS & APPLIED NEW SILKSCREEN PLACED ON 412BT IAW AMM 11-10-03-400-801 & SRM 51-42-02.

Part: SKIN — CORRODED (RT WING) · airframe 23,544 hrs · 20,904 cycles

RIGHT WING LOWER WING PLANK ACCESS HOLE 640BB, WS 54.897, HAS FRETTING CORROSION AT INBD & OTBD ENDS. INBD CORROSION MEASURES APPROX 9" LONG X 0.15" WIDE X 0.002" DEEP. OTBD CORROSION MEASURES APPROX 11.3" LONG X 0.20" WIDE X 0.003" DEEP. REPAIRED 640BB CUT OUT IAW GREO 601R-57-21-030 REV L DATED 02 05 14. THIS IS A MAJOR REPAIR. REF TO ATTACHED REO FOR WORK PERFORMED.

Part: SKIN — CORRODED (RT WING) · airframe 23,544 hrs · 20,904 cycles

RIGHT WING LOWER WING PLANK ACCESS HOLE 640AB, WS 54.681 HAS FRETTING CORROSION AT INBD END MEASURING APPROX 6" LONG X 0.12" WIDE X 0.002" DEEP. REPAIRED 640AB CUT OUT IAW GREO 601R-57-21-030 REV L DATED 02 05 14. THIS IS A MAJOR REPAIR. REF TO ATTACHED REO FOR WORK PERFORMED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

CARGO BAY SEAT TRACK ON LBL 9, FS 613 - 621 IS CORRODED. R & R SEAT TRACK WITH SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,544 hrs · 20,904 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. PAX DOOR AFT DRAG ANGLE WAS REPAIRED IAW REO 601R-52-11-513.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,544 hrs · 20,904 cycles

FLOOR SEAT TRACKS FROM FS 349 - 409+128 HAVE SEVERAL AREAS OF CORROSION ON LBL 9 & RBL 9. FLOOR SEAT TRACKS WERE REPLACED IAW AMM 53-01-11-400-802.

Part: HOUSING — DIRTY (CABIN DOOR) · airframe 23,107 hrs · 20,475 cycles

MAIN CABIN DOOR HANDLE GETS STUCK IN THE CLOSED POSITION & FLIGHT ATTENDANT WAS NOT ABLE TO OPEN IT. WHEN FIRST OFFICER OPENED THE DOOR HE SAID IT TOOK A GREAT DEAL OF FORCE & THERE WAS A LOUD BANG, OR POP, WHEN THE PINS DISENGAGED, SEEMS TO BE INTERMITTENT. CLEANED DEBRIS OUT OF THE STOP HOUSING. PERFORMED OPERATIONS CHECK ON PAX DOOR IAW AMM 52-11-00. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: FLEX DRIVE — DAMAGED (TE FLAP) · airframe 22,884 hrs · 20,243 cycles

FLAP FAIL ON ARRIVAL, 37 DEGREES, 1800 FEET, SPEED ROUGHLY 155 - 160. R & R LT BPSU IAW AMM 27-51-10, NO FIX. R & R LT NR 1 & 2 FLEX SHAFTS, FLAP IAW AMM 27-53-10. DUE TO DAMAGE, CLEANED NR 3 & 4 FLEX SHAFTS IAW AMM 27-53-10. R & R FLAP PDU IAW AMM 27-52-01. COMPLETED RIG OF BPSU IAW AMM 27-51-10. OPERATIONS TESTED OK, NO FURTHER DEFECTS NOTED IAW AMM 27-51-00.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 22,664 hrs · 20,019 cycles

MAIN CABIN DOOR VERY HARD TO OPEN, LOUD POP WHEN HANDLE IS BROUGHT UP. LUBED MAIN PAX DOOR IAW AMM 52-10-00. OPERATIONS CHECKED GOOD.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 22,607 hrs · 19,955 cycles

INFANT LIFE VEST BAG TORN. R & R ONE INFANT LIFE VEST IAW PA 25-096A.

Part: CABLE — BROKEN (ICE BREAKER) · airframe 22,309 hrs · 19,627 cycles

F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. FOUND ICE BREAKER CABLE ASSY BROKEN. R & R ICE BREAKER CABLE ASSY IAW AMM 52-11-15. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,555 hrs · 18,876 cycles

SERVICE DOOR EXTERNAL EMER LIGHT INOPERATIVE. R & R SERVICED DOOR EXTERNAL EMER LIGHT IAW AMM 33-51-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 21,398 hrs · 18,725 cycles

EMERGENCY LIGHT EXIT SIGN BULBS OUT. R & R EXIT SIGN BULBS ON CREW SERVICE DOOR & PAX DOOR IAW AMM 33-51-10. PERFORMED OPERATIONS CHECK, OPERATIONS CHECKED GOOD.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 20,659 hrs · 17,981 cycles

OBSERVER`S LIFE VEST HAS HOLE IN BAG. R & R OBSERVER`S LIFE VEST IAW AMM 25-61-03.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 20,656 hrs · 17,979 cycles

FORWARD FACE OF FS 621 BULKHEAD HAS MULTIPLE SCREW CHAFES. REPAIRED IAW REO 601R-53-61-2155.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 20,641 hrs · 17,968 cycles

EMERGENCY FLASH LIGHT BEHIND CAPTAIN'S SEAT SECURING STRAP BROKE. REPLACED EMERGENCY FLASHLIGHT ASSEMBLY IAW CRJ 200 AMM CHAPT 25. OPERATIONS CHECKED GOOD.

Part: LIFE VEST — DAMAGED (COCKPIT) · airframe 20,521 hrs · 17,853 cycles

OBSERVER`S LIFE VEST HAS HOLE IN BAG. R & R OBSERVER`S LIFE VEST IAW AMM 25-61-03.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 20,382 hrs · 17,716 cycles

OBSERVER & FIRST OFFICER`S LIFE VEST HAS HOLE IN BAGS. R & R OBSERVERS & FIRST OFFICER`S LIFE VEST IAW AMM 25-61-03.

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 19,975 hrs · 17,309 cycles

OBSERVER'S LIFE VEST HAS HOLES IN THE BAG. R & R OBSERVER'S LIFE VEST IAW AMM 25-61-03.

Part: CONTAINER — TORN (LIFE VEST) · airframe 19,640 hrs · 16,990 cycles

OBSERVER LIFE VEST BAG TORN.

Part: TILLER — INOPERATIVE (NLG STEERING) · airframe 19,613 hrs · 16,964 cycles

STEERING TILLER WILL NOT AUTO CENTER WHEN RELEASED. R & R NOSE WHEEL STEERING TILLER IAW AMM 32-51-01. TAXIED ACFT AROUND WITH NO DEFECTS. VERIFIED STEERING RIG IS GOOD. OK FOR SERVICE.

Part: ENGINE — FAILED (RIGHT) · airframe 19,555 hrs · 16,912 cycles

RT ENGINE FAILED ON CLIMBOUT AT APPROX 4500 FT. ENGINE APPEARED TO SEIZE. RAN QRH AND RETURNED TO DEPARTURE. R & R RT ENGINE IAW AMM 71-00-00 & CHECKLIST. OPS CHECKED GOOD, NO LEAKS.

Part: ENGINE — FAILED (RIGHT) · airframe 19,553 hrs · 16,908 cycles

SHORTLY AFTER TAKEOFF AND AT 4400 FT, RT ENGINE MADE A LOUD NOISE AND N2 WENT TO ZERO. SHORTLY AFTER, A HOT ICON POSTED. EMERGENCY DECLARED AND RETURNED TO DEPARTURE.

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 19,494 hrs · 16,848 cycles

OBSERVERS LIFE VEST HAS HOLE IN PACKAGE. R & R OBSERVERS LIFE VEST IAW AMM 25-61-03.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,294 hrs · 16,654 cycles

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

Part: DOOR — FROZEN (CABIN) · airframe 18,971 hrs · 16,347 cycles

MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN. TOOK OVER 5 MINS TO OPEN. ALL THREE CREW MEMBERS AND GROUND CREW TOOK TURNS BEFORE THE LATCH RELEASED. FOUND EVIDENCE OF DOOR FROZEN SHUT. REMOVED ICE AND WATER FROM PASSENGER DOOR. PERFORMED SEVERAL OPERATIONS CHECKS PER AMM 52-10-00, OF OPENING AND CLOSING PASSENGER DOOR WITH NO PROBLEMS.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 18,640 hrs · 16,035 cycles

OBSERVER LIFE VEST COVER TORN. REMOVED AND REPLACED OBSERVER LIFE VEST COVER IAW AMM 25-61-03.

Part: SEAT BELT — DEFECTIVE (FA SEAT) · airframe 18,498 hrs · 15,996 cycles

F/A JUMP SEAT SEATBELT WILL NOT BUCKLE. REMOVED AND REPLACED F/A JUMP SEAT BELT IAW CMM 25-22-04 THIS CLEARS DM 76056.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,447 hrs · 15,839 cycles

EMERGENCY LIGHTS WERE SELECTED TO ON WHEN CREW ARRIVED AT THE AIRCRAFT. EMERGENCY LIGHTS DO NOT ILLUMINATE AT THIS TIME. REPLACED BATTERY PACKS IAW AMM 33-51-04. OPERATIONAL CHECKS GOOD IAW AMM 33-51-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,919 hrs · 15,310 cycles

RIGHT SIDE SEAT RAIL NR 5 CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-00-005.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 17,485 hrs · 14,887 cycles

OBSERVERS LIFE VEST PROTECTIVE BAG IS BUSTED OPEN. REMOVED AND REPLACED OBSERVERS LIFE VEST IAW AMM 25-61-03.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,213 hrs · 14,635 cycles

LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT HAS CORROSION AT WS 12.245 IN NON-CRITICAL REGION. WS 54.681 CORRODED IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,213 hrs · 14,635 cycles

LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 136.676 CORRODED IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · corrosion level 2 · airframe 17,213 hrs · 14,635 cycles

CARGO FLOOR SUPPORT CORRODED FROM FS 589 TO 621. REPAIRED IAW REO 601R-53-00-005.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,213 hrs · 14,635 cycles

LEFT WING PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 163 CORRODED IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 17,213 hrs · 14,635 cycles

FS 621 INTERCOSTAL CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-61-985.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,213 hrs · 14,635 cycles

LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 76.161 HAS CORROSION IN NON-CRITICAL AREA 0.001" AND AT WS 95.95 (HOLE 6) HAS CORROSION IN CRITICAL AREA. REPAIRED IAW REO 601R-57-21-030 REV H.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · corrosion level 2 · airframe 17,213 hrs · 14,635 cycles

FS 280 BULKHEAD FLOOR SUPPORT CRACKED JUST OUTBOARD OF LBL 9. FORWARD FLOOR SUPPORT CORRODED BETWEEN LBL 9 AND RBL 9 AROUND NUT PLATES. ATTACHMENT CLIPS CRACKED AT LBL 9 AND RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136 AND 601R-53-11-171.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,213 hrs · 14,635 cycles

RBL 27 FS 484 INBOARD AND OUTBOARD INTERCOSTAL CLIPS CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-41-059 REV B.

Part: ACCESS PANEL — DAMAGED (ELEVATOR) · airframe 17,213 hrs · 14,635 cycles

ELONGATED HOLE COMMON TO THE PCU ACCESS PANEL, THE LOWER SKIN DOUBLER, AND LOWER STRINGER 3 AS SHOWN IN FIGURE 1. THE HOLE WAS CLEANED UP TO A CLEAN AND ROUND DIAMETER OF 0.281. REPAIRED IAW PINNACLE EA CRJ255-00462 AND ASSOCIATED 8110-3 DATE 3/29/12.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 17,213 hrs · 14,635 cycles

FS 621 BULKHEAD WEB GOUGED IN 10 PLACES ABOVE WL 73.5 BETWEEN RBL 36.2 AND LBL 36.2. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 17,213 hrs · 14,635 cycles

RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 54.897 HAS CORROSION IN THE NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: QUICK DISCONNECT — OUT OF POSITION (BRAKE SYSTEM) · airframe 16,698 hrs · 14,163 cycles

RIGHT OUTBOARD BRAKE IS INOPERATIVE. AFTER LANDING BTMS SHOWS 1 WHEN THE REST OF THE BRAKES ARE 4'S & ON INSPECTION THE REST OF THE BRAKES ARE TOO HOT TO TOUCH & RT OUTBOARD IS ICE COLD. BRAKE PINS ON RT O/B BRAKE NOT MOVING WHEN BRAKES APPLIED. DISCONNECTED AND RECONNECTED HYD LINE TO RT O/B BRAKE IAW AMM 32-43-26. BRAKE PINS MOVE NOW WHEN BRAKES ARE APPLIED. A/C OK FOR SERVICE.

Part: SPOILER — UNWANTED DEPLOY (WING) · airframe 15,845 hrs · 13,314 cycles

FLT AND GRND SPLR UNCOMMANDED DEPLOY. DIR BB STILL IN WORK. FLT RECORDER DOWNLOAD IS BEING EVALUATED BY BOMBARDIER.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 15,275 hrs · 12,795 cycles

RT GEAR DISAGREE ON CLIMBOUT. DEFERRED PER MEL 32-30-01 AUTH 41781.

Part: UNKNOWN — MALFUNCTIONED (RT MLG) · airframe 15,191 hrs · 12,718 cycles

ON APPROACH CREW REPORTED GEAR DISAGREE RIGHT MAIN LANDING GEAR WOULD NOT GO DOWN & LOCK UNTIL IT WAS CYCLED THE SECOND TIME, DEFERRED MLG RETRACTION SYSTEM IAW MEL 32-30-01 DM-41017.

Part: BUSHING — WORN (ELEVATOR) · airframe 14,682 hrs · 12,248 cycles

CREW REPORTS A INFLIGHT AIRFRAME VIBRATION. UPON INSPECTION, MAINTENANCE FOUND THE RT ELEVATOR PCU LINGAGE BUSHINGS WORN P/N: 600-10300-563. MAINTENANCE REPLACED ALL BUSHINGS AND BOTH ELEVATORS PASSED BACKLASH.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,365 hrs · 11,960 cycles

A 0.312 INCH CRACK FOUND IN FS 621 AFT PRESSURE BULKHEAD AT WL 131.8, LBL 28.0. FERRY FLIGHT FROM TYS TO MEM IAW BOMBARDIER REO 601R-53-61-3868 WHERE A PERMANENT REPAIR WAS ACCOMPLISHED IAW BOMBARDIER GREO 601R-53-61-1541.

Part: DUCT — LOOSE (AC SYSTEM) · airframe 14,006 hrs · 11,590 cycles

DISPLAY COOL CAUTION QRH COMPLETE. MESSAGE STAYED, FOUND DUCT ON MANIFOLD LOOSE RE-ATTACHED DUCT DISPLAY COOL FANS. OP CHECK GOOD IAW AMM 21-24-19. OK FOR SERVICE.

Part: FLAP SYSTEM — INOPERATIVE (TE FLAPS) · airframe 3,730 hrs · 2,758 cycles

FLAP FAILURE CAUTION MESSAGE, FLAPS FAILED AT 20 DEGREES. PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM IAW AMM 27-51-00. OPS CHECK GOOD, OK FOR SERVICE.