N8828D

Part: ENGINE — FAILED (RIGHT) · airframe 27,035 hrs · 24,460 cycles

DURING CRUISE, HEARD A LOUD BANG FROM RT ENGINE AND THEN A LOSS OF POWER. ALSO HEARD A VERY LOUD WHINING NOISE . RECEIVED HIGH N1 VIBRATION. PULLED BACK TO IDLE AND THEN FOLLOWED QRH FOR IN FLIGHT SHUTDOWN. R&R RT ENGINE.

Part: COVER — BROKEN (CABIN) · airframe 24,520 hrs · 21,907 cycles

WHILE INSPECTING FLOOR TRACK EMER LIGHTING FOUND FLOOR TRACK LIGHTING COVER BROKEN, CRACKED & DETACHED. R & R FLOOR TRACK LIGHTING COVER IAW AMM 33-51-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 24,497 hrs · 21,884 cycles

EMERGENCY LIGHT COVER LOOSE. RESECURED EMERGENCY LIGHT COVER IAW AMM 33-51-01.

Part: BPSU — FAILED (TE FLAP) · airframe 24,006 hrs · 21,407 cycles

FLAPS FAIL CAUTION MSG. PERFORMED TROUBLESHOOTING IAW FIM CHAPTER 27-580-00 REV 47 IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC DATED APRIL 22,2014 & TS001100-2014 FIM TECHNICAL SUPPLEMENT. TROUBLE SHOT WRING IAW FIM, CHANGED RT BPSU IAW 27-51-10. FLAP FAIL CODES 12 1B, 12 2B, 25 BC. R & R RT FLAP BPSU IAW AMM 27-15-10.

Part: COVER — BROKEN (CABIN) · airframe 23,954 hrs · 21,354 cycles

FLOOR TRACK EMER LIGHT STRIP COVER & BASE IS BROKEN IN MULTIPLE PLACES. REPAIRED FLOOR TRACK EMER LIGHT STRIP IAW AMM 33-51-01. OPERATIONS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: ULB — FAILED (CVR) · airframe 23,954 hrs · 21,354 cycles

CVR ULB FAILED FUNCTIONAL TEST. R & R CVR ULB IAW AMM 23-71-03. FUNCTIONAL CHECK GOOD IAW AMM 23-71-03-720-801.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 23,943 hrs · 21,340 cycles

RIGHT WING PLANK CORRODED AT LANDING FOR PANEL 640BB AT WS 54.897. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CHAFED (RT WING) · airframe 23,945 hrs · 21,341 cycles

FOUND CHAFE DAMAGE TO THE RT WING LOWER AFT WING PLANK AT THE WING JACK POINT WS 144.00 AUX SPAR DATUM. REPAIRED IAW EA CRJ257-02801.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 23,943 hrs · 21,340 cycles

RIGHT WING PLANK CORRODED AROUND LANDING FOR FUEL ACCESS PANEL 610AB AT WS 12.245. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — DENTED (FUSELAGE) · airframe 23,945 hrs · 21,341 cycles

FOUND A DENT TO THE LT FUSELAGE SKIN AT FS 356.00 AT STRINGER 23L. REPAIRED IAW EA CRJ253-02782.

Part: SKIN — CHAFED (LT WING) · airframe 23,945 hrs · 21,341 cycles

FOUND CHAFE DAMAGE TO THE LT WING LOWER AFT WING PLANK AT THE WING JACK POINT WS 144.00, AUX SPAR DATUM. REPAIRED IAW EA CRJ257-02800.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,943 hrs · 21,340 cycles

SKIN CORRODED AT FS 605 BETWEEN STRINGER 26 & 26R MEASURING 7 INCHES X 4.5 INCHES X 0.033 INCHES DEEP. REPAIRED IAW REO 601R-53-61-5321.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 23,945 hrs · 21,341 cycles

FORWARD FACE OF FS 621 BULKHEAD CHAFED FROM SCREW HEADS IN 13 PLACES. REPAIRED IAW REO 601R-53-61-2155.

Part: SPAR — GOUGED (LT PYLON) · airframe 23,945 hrs · 21,341 cycles

LEFT ENG PYLON BOX FRAME FWD ENG YOKE MOUNT SPAR GOUGED IN THREE PLACES. REPAIRED IAW REO 601R-54-51-341.

Part: SKIN — DENTED (FUSELAGE) · airframe 23,945 hrs · 21,341 cycles

FOUND A DENT IN THE LT FUSELAGE SKIN AT FS 615.00. REPAIRED IAW EA CRJ253-02758.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,945 hrs · 21,341 cycles

FOUND CORROSION ON THE LOWER FRAME SECTOR AT FS 605.00 BETWEEN STRINGER 25R & 26L. REPAIRED IAW EA CRJ253-02772.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,945 hrs · 21,341 cycles

RIGHT OTBD CLIP OF FS 280 BULKHEAD CRACKED. REPAIRED IAW REO 601R-53-11-171.

Part: SELECTOR VALVE — FAULTY (MLG) · airframe 22,725 hrs · 20,144 cycles

GEAR DISAGREE WARNING MESSAGE WHEN PULLED LG DOWN ON FINAL RST RW 13 6 NM OUT AT 3000' 180 KISA. QRH COMPLETE WITH MANUAL GEAR EXTENSION FULL UP, GEAR CAME DOWN WITH ALL 3 GREEN LANDED NORMAL. R & R PSEU IAW AMM 32-61-01, NO HELP. R & R MLG SELECTOR VLV IAW AMM 32-32-10. FUNCTIONAL CHECK OF LG GOOD IAW AMM 32-30-00, ACFT OK FOR SERVICE.

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 22,115 hrs · 19,528 cycles

FO`S LIFE VEST HAS A HOLE IN BAG. R & R F/O`S LIFE VEST IAW AMM 25-61-03.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 21,476 hrs · 18,909 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,312 hrs · 18,744 cycles

FORWARD OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FWD EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 21,222 hrs · 18,659 cycles

FUSELAGE SKIN AT FS 780.00 DENTED BETWEEN S-25L AND S-26L AND CRACKED. REPAIRED IAW EA CRJ253-01255A AS APPROVED BY 8110-3 DATED FEBRUARY 1, 2013.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,222 hrs · 18,659 cycles

AFT PRESSURE BULKHEAD AT FS 621 CRACKED AT THE LINTEL FITTING LOWER EDGE. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,222 hrs · 18,659 cycles

PRESSURE BULKHEAD AT FS 202.75 AT LL 23.75 CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-563.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 21,222 hrs · 18,659 cycles

Z-STIFFENER CRACKED AT WL 47 ON AFT SIDE OF FS 202 BULKHEAD ON LEFT SIDE NEAR PARKING BRAKE CABLE FEED THRU. REPLACED IAW SRM 51-24-00.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 21,222 hrs · 18,659 cycles

DURING HEAVY CHECK RIGHT OVERWING EMERGENCY EXIT DOOR FAILED FUNCTIONAL CHECK. (AIRCRAFT WAS IN HEAVY CHECK 1/19/2013 THROUGH 2/3/2013). PERFORMED LUBE OF RT OVERWING EMERGENCY EXIT IAW CRJ 200 AMM 12-20-52 PERFORMED FUNCTIONAL CHECK OF RT EMERGENCY EXIT IAW CRJ 200 AMM 52-21-00 WITH NO DEFECT NOTED.

Part: STRIKER — DAMAGED (PAX DOOR) · airframe 27,117 hrs · 24,719 cycles

EXTREMELY HIGH PITCH NOISE COMING FROM THE MAIN CABIN DOOR IN FLIGHT. NOISE STOPPED AS WE STARTED THE DESCENT. REPAIRED PASSENGER DOOR STRIKER IN 2 SPOTS ON THE AFT PORTION IAW REO601R-53-22-033.

Part: LIGHT — SHORTED (CABIN) · airframe 21,157 hrs · 18,602 cycles

EMERGENCY LIGHT FLOOR STRIP ROW 2 SHORTED OUT. REPLACED FLOOR LIGHT STRIP IAW AMM 33-51-01.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,937 hrs · 18,382 cycles

EMERGENCY FLOOR STRIPS 6 TO 8 INOPERABLE. REMOVED AND REPLACED NR 3 INVERTER AND NR 8 FLOOR TRACK STRIP IAW AMM 33-51-07 AND AMM 33-51-01. OPS CHECK GOOD.

Part: STRIP — OUT OF POSITION (CABIN) · airframe 20,749 hrs · 18,196 cycles

ORANGE STRIP AT SEAT 8C FOR EMERGENCY EXIT FLOOR PATH LIGHTING STRIP IS LOCATED AT SEAT 10C. RELOCATED EMERGENCY ORANGE STRIP TO SEAT 8C, OPS CHECK GOOD IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,749 hrs · 18,196 cycles

FORWARD EMERGENCY LIGHT STRIP AT ROW 11 RIGHT INOPERABLE. REPLACED EMERGENCY LIGHT STRIP IAW CRJ-200 AMM 33-51-01. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (TE FLAPS) · airframe 20,471 hrs · 17,901 cycles

FLAPS FAILED AT 0' 200 KTS ON APPROACH. PERFORMED TROUBLESHOOTING PER FIM REV 43 IAW AD 2009-06-12 (H)(6)(I) AMOC DATED APRIL 2012 AND PA 27-05H. FOUND LT BPSU BAD, REMOVED AND REPLACED LT BPSU IAW CRJ 200 AMM 27-51-01. ALL CHECKED GOOD.

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 20,421 hrs · 17,853 cycles

AFTER TAKEOFF, FLIGHT 4093, GEAR HANDLE IN THE UP POSITION RECEIVED A NOSE GEAR WARNING ALONG WITH GEAR DISAGREE. DID NOT DECLARE AN EMERGENCY. PERFORMED AN AIR RETURN. COMPLIED WITH PA 05-018 REV G. FOUND NLG OLEO CENTERING EXTENDED SENSOR (PS14GA) TO TARGET GAP TO BE .014 OUT OF ADJUSTMENT. ADJUSTED TO .50 .

Part: BPSU — OUT OF ADJUST (TE FLAPS) · airframe 20,258 hrs · 17,961 cycles

FLAPS FAILED AT 30 DEGREES ON APPROACH. PERFORMED TROUBLESHOOTING PER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I). AMOC DATED MARCH 27, 2009, TR NR 27-012 PER AMOC DECEMBER 18, 2009 AND PA AD27-052G. FOUND LEFT BPSU OUT OF ADJUSTMENT. ADJUSTED LEFT BPSU IAW AMM 27-51-10. OPS CHECKS GOOD AT THIS TIME, OK FOR SERVICE.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 20,258 hrs · 17,691 cycles

EMERGENCY LIGHT COVER HAS SEVERAL DAMAGED AREAS AND STRIP IS PULLING AWAY FROM FLOORBOARD IN AFT CABIN. REMOVED AND REPLACED SECTIONS OF LIGHT COVER IAW AMM 33-51-01.

Part: PBE — DAMAGED (COCKPIT) · airframe 19,770 hrs · 17,195 cycles

COCKPIT PBE IS MUSHY AND INDICATOR IS NOT LIGHT BLUE. REMOVED & REPLACED COCKPIT PBE IAW CMM PRM-01 AND AMM 35-30-00, OK FOR SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 19,290 hrs · 16,720 cycles

EMERGENCY FLOOR TRACK LIGHTING FIRST ONE DAMAGED. REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHTING STRIP IAW AMM 33-51-01.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,033 hrs · 16,458 cycles

THE 559 SEMI-PRESSURE BULKHEAD CRACKED IN WEB ANGLE AT LBL 9 AND RBL 9. REPAIRED IAW PA53-025 IAW REO 601R-53-41-260 REV E AND 601R-53-41-609 REV B.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,932 hrs · 16,362 cycles

FA FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY TO FA FLASHLIGHT IAW AMM 25-61-04. NO FIX 'VERIFIED PART EFFECTIVITY'. REMOVED AND REPLACED FA EMERGENCY FLASHLIGHT ASSY IAW AMM 25-61-04. OPC GOOD. "VERIFIED PART EFFECTIVITY".

Part: CIRCUIT BREAKER — TRIPPED (FUEL SYSTEM) · airframe 18,721 hrs · 16,157 cycles

APU XFLOW MSG FOUND CBP 1 N10 XFLOW/APU FUEL CB OUT AND PERFORMED RESET NO DEFECTS NOTED. OPS CHECK GOOD IAW AMM 28-24-01.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 18,350 hrs · 15,816 cycles

NOSE WHEEL STEERING INOP INSPECT NWS SYSTEM IAW AMM 32-51-10 AND OPS CHECKED IAW AMM 32-51-00, NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 17,181 hrs · 14,698 cycles

RIGHT WING LOWER PLANK ACCESS HOLE NR 2 FOR 610AB HAS CORROSION AT INBOARD END NOT IN CRITICAL REGION. REPAIRED RIGHT WING LOWER PLANK ACCESS HOLE NR 1 FOR 640BB AT OUTBOARD END NOT IN CRITICAL REGION IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 17,181 hrs · 14,698 cycles

THERE IS A LIFE LIMITED SKIN REPAIR BETWEEN FS 587.00 AND FS 605.00 FROM STRINGER 22R TO 26R. PERFORMED A MAJOR REPAIR TO THE FUSELAGE SKIN BETWEEN FS 587 AND FS 605 FROM STRINGER 22R TO 26R IN ACCORDANCE WITH BOMBARDIER AEROSPACE REPAIR ENGINEERING ORDER 601R-53-20147.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,181 hrs · 14,698 cycles

LEFT WING LOWER PLANK ACCESS HOLE NR 2 FOR 510AB HAS CORROSION AT FORWARD SIDE AND OUTBOARD END IN AND OUT OF CRITICAL REGION. REPAIRED LEFT WING LOWER PLANK ACCESS HOLE NR 2 FOR 510AB AT FORWARD SIDE AND OUTBOARD END IN AND OUT OF CRITICAL REGION IAW BOMBARDIER REO 601R-57-21-030 REV H . REPAIRED AREA WILL REQUIRE A THRESHOLD INSPECTION AT 42780 FLIGHT CYCLES AND REPEATING AT 28,082 FLIGHT CYCLES IN ACCORDANCE WITH NON-DESTRUCTIVE TESTING MANUAL 57-21-149, PART 6.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 17,181 hrs · 14,698 cycles

RIGHT WING LOWER PLANK ACCESS HOLE NR 1 FOR 640BB HAS CORROSION AT OUTBOARD END NOT IN CRITICAL REGION. REPAIRED RIGHT WING LOWER PLANK ACCESS HOLE NR 1 FOR 640BB AT OUTBOARD END NOT IN CRITICAL REGION IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 17,181 hrs · 14,698 cycles

RIGHT WING LOWER PLANK ACCESS HOLE NR 6 FOR 640DB HAS CORROSION AT INBOARD END NOT IN CRITICAL REGION. REPAIRED RIGHT WING LOWER PLANK ACCESS HOLE NR 6 FOR 640DB AT INBOARD END NOT IN CRITICAL REGION IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,181 hrs · 14,698 cycles

FS 280 FORWARD FLOOR SUPPORT ANGLE P/N 600-34017-351 CORRODED. REMOVED AND REPLACED SUPPORT ANGLE IAW CRJ 200 SRM 51-42-06.

Part: BULKHEAD — CRACKED (FUSELAGE) · corrosion level 2 · airframe 17,181 hrs · 14,698 cycles

PILOT BULKHEAD AT FS 280 CRACKED BELOW FLOOR AT RBL 9 AND LBL 9, AFT FLOOR SUPPRT CRACKED AT LBL 9 AND PILOT BULKHEAD IS CORRODED AT FLOOR BETWEEN RBL 9 AND LBL 9. PILOT BULKHEAD AT FS 280 CRACKED BELOW FLOOR AT RBL 9 AND LBL 9, AFT FLOOR SUPPORT CRACKED AT LBL 9 AND PILOT BULKHEAD IS CORRODED AT FLOOR BETWEEN RBL 9 AND LBL 9.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,181 hrs · 14,698 cycles

CARGO DOOR SILL IS CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW BOMBARDIER REO 601R-53-61-1574, CRJ 200 SRM 51-40-11AND 51-42-06.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,181 hrs · 14,698 cycles

LEFT WING LOWER PLANK ACCESS HOLE NR 3 FOR 510BB HAS CORROSION AT OUTBOARD END NOT IN CRITICAL REGION. REPAIRED LEFT WING LOWER PLANK ACCESS HOLE NR 3 FOR 510BB AT OUTBOARD END NOT IN CRITICAL REGION IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,181 hrs · 14,698 cycles

LT PASSENGER COMPARTMENT SEAT SIDE RAIL CORRODED AT EMERGENCY EXIT FS 513.00. REMOVED AND REPLACED LT SIDE SEAT RAIL AT FS 513.00 IAW CRJ 200 SRM 51-41-00, 51-41-02.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 17,181 hrs · 14,698 cycles

RIGHT WING LOWER PLANK ACCESS HOLE NR 4 FOR 640AB HAS CORROSION AT INBOARD AND OUTBOARD ENDS NOT IN CRITICAL REGION. REPAIRED RIGHT WING LOWER PLANK ACCESS HOLE NR 4 FOR 640AB AT INBOARD AND OUTBOARD ENDS NOT IN CRITICAL REGION IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,181 hrs · 14,698 cycles

RT SIDE SEAT SIDE RAIL AT FS 409+57 IS CORRODED. REMOVED AND REPLACED RT SIDE SEAT RAIL FROM FS 409.00+16 TO FS 409.00+112 IAW CRJ 200 SRM 51-41-02 AND 51-41-04.

Part: SKIN — CORRODED (LLT WING) · corrosion level 2 · airframe 17,181 hrs · 14,698 cycles

LEFT WING LOWER PLANK ACCESS HOLE NR 1 FOR 540BB HAS CORROSION AT INBOARD AND OUTBOARD END NOT IN CRITICAL REGION. REPAIRED LEFT WING LOWER PLANK ACCESS HOLE NR 1 FOR 540BB AT INBOARD AND OUTBOARD END NOT IN CRITICAL REGION IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: STRUT — LOW (NLG) · airframe 17,121 hrs · 14,639 cycles

NOSE GEAR DISAGREE MSG ON T/O. SERVICED NLG STRUT IAW AMM. PERFORMED GEAR EXTENSION/RETRACTION FUNCTIONAL CHECK. OP/C GOOD. AC RELEASED FOR SERVICE.