N8837B

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 31,097 hrs · 28,864 cycles

"MOST AFT FLOOR TRACK LIGHT DAMAGED "REPLACED AFT PWR CABLE AND FLEX LAMP CABLE IAW CRJ200 MM 33-51-01 OPS CHECK GOOD "REPLACED PART NUMBER: 6464-5, 36378-2

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 30,994 hrs · 28,734 cycles

FLIGHT ATTENDANT REPORTS EMERGENCY PATHWAY LIGHTING STRIP PLASTIC COVER IS NOT SECURE. R & R`D AFT END EMER, FLOOR LIGHT CABLE AND TRACK IAW AMM 33-51-04. ALL CHECKS GOOD. A/C OK FOR SVC. "

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,924 hrs · 28,648 cycles

SECTION 6CD- TO - 8CD EMERGENCY LIGHTING STRIPS ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHTING STRIPS IAW CRJ-200 AMM 33-51-01. OPS CHECK GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 30,924 hrs · 28,648 cycles

EMERGENCY LIGHT FLOOR STRIP IS DAMAGED ROW 11-12 C/D. REMOVED AND REPLACED EMERGENCY LIGHT FLOOR STRIP IAW CRJ 200 AMM 33-51-01. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (ROWS 2-3) · airframe 30,236 hrs · 27,937 cycles

FLOOR EMERGENCY LIGHT INOP @ ROW 2 + 3 P/N OFF: 36262-4 REMOVED AND REPLACED EMGERENCY TRACK LIGHT IAW CRJ200 AMM 33-51-01. OPS CHK GOOD

Part: LIGHT — INOPERATIVE (ROW 8) · airframe 29,954 hrs · 27,632 cycles

CABIN FLOOR PATH LIGHTING INOP AFT OF ROW 8. REMOVED AND REPLACED EMERGENCY LIGHT FLOOR TRACK POWER AND LIGHT STRIP IAW CRJ200 33-51-01. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,725 hrs · 27,397 cycles

AFT EMERGENCY FLOOR TRACK LIGHTING STRIP BY LAV INOP. REMOVED AND REPLACED AFT FLOOR TRACK LIGHTING STRIP PN 36378-2 IAW AMM 33-51-01. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,661 hrs · 27,325 cycles

EMERG FLOOR LIGHT TOWARDS AFT IS INOP. REPLACED AFT SECTION OF EMERG FLOOR LIGHT IAW AMM 33-51-01 OPS TEST GOOD PN ON/OFF 36378-2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,650 hrs · 27,315 cycles

CREW REPORTS @ 10CD AND 12CD EMERGENCY LIGHTING INOP. REMOVED & REPLACED FLEX LAMP WITH ARROWS @ 10CD AND 12CD P/N 36378-2 AND CABLE ASSY P/N 6464-5 PER AMM 33-51-01 ALL CHECKS GOOD.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 29,509 hrs · 27,163 cycles

AFT CARGO SCUFF PLATE CRACKED. LOCATED ADB, DRILLED IAW SRM 51-40-11 TR 51-42

Part: ACCESS PANEL — CORRODED (TAIL) · airframe 29,509 hrs · 27,163 cycles

TAIL ACCESS PANEL 361AB CORRODED OUT OF LIMITS. RECEIVED NEW PANEL AND PAINTED IAW SRM 51-25-16.

Part: STRAP — CORRODED (BS 589) · airframe 29,509 hrs · 27,163 cycles

FLOOR SUPPORT STRAP FS 589 LBL9-RBL 9 CORRODED. REMOVED AND REPLACED STRAP IAW SRM 51-42-06

Part: STRAP — CORRODED (BS 589) · airframe 29,509 hrs · 27,163 cycles

FLOOR SUPPORT STRAP FS 589 LBL9-LBL27 CORRODED. REMOVED AND REPLACED STRAP IAW SRM 51-42-06

Part: SEAT TRACK — CORRODED (BS 559) · airframe 29,509 hrs · 27,163 cycles

RIGHT AISLE SEAT TRACK NEAREST THE LAV, IS CONTAMINATED BY BLUE JUICE AND PRESUMED TO BE CORRODED. REMOVED CORROSION FROM RIGHT AISLE SEAT TRACK WHICH WAS OUT OF LIMITS IAW CRJ 200 SRM 53-21-49 REMOVED AND REPLACED WITH NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · airframe 29,509 hrs · 27,163 cycles

LH AISLE SEAT TRACK #1 CORRODED. REMOVED AND REPLACED STRAP IAW AMM 53-01-11-400-802

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 29,509 hrs · 27,163 cycles

PASSENGER DOOR AFT MIDDLE DRAG ANGLE CRACKED. REMOVED AND REPLACED PASSENGER DOOR AFT MIDDLE DRAG ANGLE IAW REO 601R-52-11-513 TYPE 11 AAR SM 107

Part: SEAT TRACK — CORRODED (CABIN) · airframe 29,509 hrs · 27,163 cycles

RIGHT AISLE SEAT TRACK #2 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11 AAR SM 58

Part: FLOOR SUPPORT — CORRODED (BS 610-621) · airframe 29,509 hrs · 27,163 cycles

BEAM AT RBL 9 O/B FLOOR PANEL LANDING HAS CORROSION BETWEEN FS 610 AND FS 621, IN THE CARGO BAY. REMOVED CORROSION BETWEEN FS 610 AND FS 621 IN THE CARGO BAY ON BEAM AT RBL 9 O/B FLOOR PANEL LANDING IAW CRJ 200 SRM 51-21-06 AND INSTALLED REPAIR STRAP IAW CRJ 200 BOMBARDIER EA# CRJ 253-09002..

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,490 hrs · 27,143 cycles

DURING WALK AROUND FOUND OUTSIDE FWD EMERGENCY EXIT LIGHT NOT WORKING. R/R OUTSIDE EXTERNAL FWD RT EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: LIGHT — UNKNOWN (CABIN) · airframe 29,395 hrs · 27,039 cycles

EMERGENCY ROW LIGHTING NOT ILLUMINATING DURING FLIGHT ATTENDT PRE FLIGHT INSPECTION. PERFORMED OPS CHECKS OF THE EMERGENCY LIGHTS AND VISUAL CHECK OF THE FLOOR TRACK LIGHT WITH NO DEFECTS AMM 33-50-01 AT THIS TIME.

Part: HOLDER — SPARKS (COCKPIT) · airframe 28,808 hrs · 26,418 cycles

CAPTAIN CHART HOLDER (YOKE) STARTED TO SPARK AND SMOKE. AFTER A FEW SECONDS THE LIGHT STOPPED WORKING. BOTH CHART HOLDERS ARE NOW INOP. RE-SECURED CHART HOLDER HARDWARE IAW CRJ200 T.S. 004310. RESET C/B OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,792 hrs · 26,402 cycles

DURING POST FLIGHT NOTICED EMER-LIGHTS NOT OPERATIONAL CHARGED EMERGENCY LIGHT BATTERY PACKS IAW CMM 25-60-03 REPLACED INVERTER PS3LY IAW AMM 33-51-07 OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,188 hrs · 25,751 cycles

CABIN FLOOR EMERGENCY LIGHT STRIPS OUT. REMOVED AND REPLACED SECOND TO AFT ARROW SEGMENT IAW AMM 33-51-01 OPS CHECKS GOOD AT THIS TIME.

Part: LIGHT — UNSECURE (CABIN) · airframe 28,106 hrs · 25,654 cycles

EMERGENCY FLOOR TRACK LIGHTING IN AFT MOST SECTION INOP. RESECURED AND OPS CHECKED AFT EMER FLOOR LIGHT SECTION IAW AMM 33-51-19. ALL CHECKS GOOD AT THIS TIME.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 7 C,D) · airframe 27,762 hrs · 25,306 cycles

OXYGEN MASKS AT SEATS 7 C, D, DEPLOYED. RESTOWED THE OXYGEN MASKS IAW AMM 35-20-01.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 27,723 hrs · 25,254 cycles

EMERGENCY LIGHTS AT ROW 10 INOPERATIVE. SECURED THE CONNECTOR, OPS CHECKED GOOD IAW AMM 33-51-00.

Part: DISPLAY — INOPERATIVE (NR 1 & 2) · airframe 27,704 hrs · 25,234 cycles

MFD 1 DROPPED OFF LINE THEN AFTER 1 OR 2 MINUTES MFD2 DROPPED OFF LINE AS WELL FOR DURATION OF FLIGHT. CLEANED THE COCKPIT DISPLAY COOLING FILTER IAW AMM 21-24-15, AND REMOVED AND REPLACED THE NR 1 & 2 MFDS. PERFORMED AN OPERATIONAL TEST IAW AMM 31-61-01, AND 34-25-00, OPS TESTED GOOD. NO DEFECTS NOTED.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 26,824 hrs · 24,274 cycles

SMOKE TOILET WENT OFF FOR ABOUT 5 MINS, NOTED AFTER TURNING OFF APU GEN. PERFORMED OPS TEST OF THE LAV SMOKE DETECTION SYSTEM IAW CRJ 200 AMM 26-16-01. OPS TEST GOOD.

Part: STRUT — DISCHARGED (NLG) · airframe 26,504 hrs · 23,935 cycles

ON DEPARTURE, NOSE GEAR DID NOT FULLY RETRACT GEAR DISAGREE MASTER WARNING. FOUND NOSE STRUT SERVICED IMPROPERLY. SERVICED NLG STRUT IAW 12-710-002. PERFORMED GEAR EXTENSION & RETRACTION OK IAW AMM 32-30-00. ALL OPS AND LEAK CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,693 hrs · 23,077 cycles

EMERGENCY SWITCH LEFT ON FA PANEL EMERGENCY LIGHTS WILL NOT COME ON. CHARGED A/C BATTERIES FOR MINIMUM 6 HOURS IAW CMM 33-21-70. OPS CHECK NORMAL A/C OK FOR SVC.

Part: PBE — DAMAGED (COCKPIT) · airframe 25,618 hrs · 22,996 cycles

FOUND FLIGHT DECK PBE VACUUM SEAL DAMAGED. R&R FLIGHT DECK PBE IAW JOB CARD EE-200. P/N ON/OFF: MR-10047N

Part: PBE — DAMAGED (CABIN) · airframe 25,618 hrs · 22,996 cycles

FOUND WARDROBE PBE VACUUM SEAL DAMAGED. R&R WARDROBE PBE IAW JOB CARD EE-200. P/N ON/OFF: MR-10047N

Part: PBE — DAMAGED (CABIN) · airframe 25,618 hrs · 22,996 cycles

FOUND AFT CABIN PBE VACUUM SEAL DAMAGED. R&R AFT CABIN PBE IAW JOB CARD EE-200. P/N ON/OFF: MR-10047N

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

LOWER MID FRAME CORRODED AT FS 319.00, STRINGER 23R. REPAIR LOWER MID FRAME IAW EA CRJ253-04290.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

AIRCRAFT GND POWER RECEPTACLE STRUCTURE CRACKED. SUPPORT BRACKET CRACKED, PN 600-33283-33. CONTINUATION CARD 8783711 OP 269. REPAIRED ACFT GND POWER RECEPTACLE STRUCTURE IAW SRM 51-42-06 & 51-42-21. REPAIRED SUPPORT BRACKET, PN 600-33283-33.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

ACFT GND POWER RECEPTACLE STRUCTURE CRACKED. INTERCOSTAL CRACKED, PN 600-33283-35. CONTINUATION CARD 8783711 OP 269. REPAIRED ACFT GND POWER RECEPTACLE STRUCTURE IAW SRM 51-42-06 & 51-42-21. REPAIRED INTERCOSTAL, PN 600-33283-35.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

FS 319 FRAME HAS CORROSION AT STRINGER 27 & 23R. CONTINUATION CARD 8783711 OP 318. REMOVED & INSTALLED SERVICEABLE FRAME 319 LOWER IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

INTERCOSTAL BETWEEN FS 333 & 349, ALONG STRINGER 20R IS CORRODED. REMOVED INTERCOSTAL, FABRICATED REPLACEMENT IAW EA CRJ253-04320 & INSTALLED FABRICATED INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

INBOARD & OUTBOARD CLIPS ON AILERON CABLE INTERCOSTAL ARE CRACKED, FS 484, RBL 27 & 36. REPAIRED DAMAGE AT FS 484, RBL 27 & 36 IAW EA CRJ253-04241.

Part: SKIN — DAMAGED (RT WING) · airframe 24,550 hrs · 21,888 cycles

RIGHT LOWER WING PLANK CUT OUT FOR PANEL 650EB, HAS FRETTING DAMAGE ON INBD & OTBD ENDS. CONTINUATION CARD 8783711 OP 293. REPAIRED WING PLANK ACCESS HOLE FOR PANEL 650EB IAW REO 601R-57-21-030 REV L.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

LEFT INTERCOSTAL CLIP IS CRACKED, BETWEEN 621 & 625, STRINGER 15L, APPROX 1.5"LONG. FOUND STRINGER 15L INTERCOSTAL CLIP NOT TO BE CRACKED, STRINGER 13 INTERCOSTAL CLIP CRACKED. REMOVED & INSTALLED SERVICEABLE CLIP, PN 601R350121-9 IAW SRM 51-42-21 & 51-42-22.

Part: SKIN — DAMAGED (LT WING) · airframe 24,550 hrs · 21,888 cycles

LEFT LOWER WING PLANK CUT OUT FOR PANEL 510AB HAS FRETTING DAMAGE ON INBD, OTBD ENDS & FWD SIDE. CONTINUATION CARD 8783711 OP 287. REPAIRED WING PLANK ACCESS HOLE FOR PANEL 510AB IAW REO:601R-57-21-030 REV L.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 24,550 hrs · 21,888 cycles

DURING INCORPORATION OF SB 601R-25-187 FOUND THE CARGO DOOR CROSS MEMBER AFT CLIP TO BE CRACKED AT FS 621.00. LOCATED, DRILLED & INSTALLED NEW SERVICEABLE CLIP AT CARGO DOOR CROSS MEMBER FS 621.00, LOWER AFT, IAW SRM 51-40-11 & 51-42-21.

Part: SKIN — DAMAGED (LT WING) · airframe 24,550 hrs · 21,888 cycles

LEFT LOWER WING PLANK CUT OUT FOR 550DB HAS FRETTING DAMAGE OTBD & FWD SIDES. CONTINUATION CARD 8783711 OP 289. REPAIRED WING PLANK ACCESS HOLE FOR PANEL 550DB IAW REO 601R-57-21-030 REV L L

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

VERTICAL STIFFENER ON AFT SIDE OF 621, BULKHEAD BL 0 IS CHAFED AT A PREVIOUS REPAIR FROM SOV. REPAIRED FS 621 AFT VERTICAL STIFFENER IAW EA CRJ 253-04262.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

INTERCOSTAL AT FS 484, LBL 27 - 36, THE INBD & OTBD CLIPS ARE CRACKED. REPAIRED INTERCOSTAL IAW EA CRJ 253-04246.

Part: PANEL — CRACKED (WING) · airframe 24,550 hrs · 21,888 cycles

PANEL 672AL HAS THREE ELONGATED HOLES. RECEIVED NEW PANEL 672AL, DRILLED, COUNTERSUNK & PAINTED NEW PANEL IAW SRM 51-40-11 & 51-25-01.

Part: SKIN — DAMAGED (LT WING) · airframe 24,550 hrs · 21,888 cycles

LEFT LOWER WING PLANK CUT OUT FOR PANEL 550AB HAS FRETTING DAMAGE ON OTBD END. CONTINUATION CARD 8783711 OP 291. REPAIRED WING PLANK ACCESS HOLE FOR PANEL 550AB IAW REO 601R-57-21-030 REV L.

Part: SKIN — DAMAGED (RT WING) · airframe 24,550 hrs · 21,888 cycles

RIGHT LOWER WING PLANK CUT FOR PANEL 650AB HAS FRETTING DAMAGE ON INBD & OTBD ENDS. CONTINUATION CARD 8783711 OP 294. REPAIRED WING PLANK ACCESS HOLE FOR PANEL 650AB IAW REO 601R-57-21-030 REV L.

Part: SKIN — DAMAGED (LT WING) · airframe 24,550 hrs · 21,888 cycles

LEFT LOWER WING PLANK CUT PANEL 550EB HAS FRETTING DAMAGE ON OTBD & AFT SIDES. CONTINUATION CARD 8783711 OP 290 - REPAIRED WING PLANK ACCESS HOLE FOR PANEL 550EB IAW REO 601R-57-21-030 REV L.

Part: SKIN — DAMAGED (LT WING) · airframe 24,550 hrs · 21,888 cycles

LEFT LOWER WING PLANK CUT OUT FOR PANEL 550BB, HAS FRETTING DAMAGE ON INBD END. CONTINUATION CARD 8783711 OP 288. REPAIRED WING PLANK ACCCESS HOLE FOR PANEL 550BB IAW REO 601R-57-21-030 REV L.

Part: SKIN — DAMAGED (RT WING) · airframe 24,550 hrs · 21,888 cycles

RIGHT LOWER WING PLANK CUT OUT FOR PANEL 640BB HAS FRETTING DAMAGE ON INBD & OTBD ENDS. CONTINUATION CARD 8783711 OP 295. REPAIRED WING PLANK CUT OUT FOR PANEL 640BB IAW REO 601R-57-21-030 REV L.

Part: SKIN — DAMAGED (LT WING) · airframe 24,550 hrs · 21,888 cycles

LEFT LOWER WING PLANK CUT OUT FOR PANEL 540BB, HAS FRETTING DAMAGE ON INBD & OTBD ENDS. CONTINUATION CARD 8783711 OP 292. REPAIRED WING PLANK ACCESS HOLE FOR PANEL 540BB IAW REO 601R-57-21-030 REV L.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

RIGHT SIDE SEAT RAIL NR 6 HAS MINOR SURFACE CORROSION. R & R RT SIDE SEAT RAIL NR 6 IAW SRM 51-40-11, 51 -40-06, 51-42-34 & AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

RIGHT SIDE SEAT RAILS 4 & 5 CORRODED. R & R 4 & 5 RT SIDE SEAT RAILS IAW AMM 53-01-11-400-802 & REO 601R-53-00-055 REV B.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

RBL 9 BEAM CAP, BETWEEN FS 574 & 605 HAS CORROSION. R & R FLOORBEAM CAP IAW SRM 51-40-11 & 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

LEFT SIDE SEAT RAILS 4 - 7 SEVERELY CORRODED. R & R LT SIDE SEAT RAILS 4 - 7 IAW AMM 53-01-11-400-802 & REO 601R-53-00-055 REV B.

Part: STRAP — CORRODED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

FLOOR STRAP AT FS 559 IS CORRODED FROM RBL 27 - 45. R & R FLOOR STRAP AS NEEDED AT FS 559, RBL 27 - 45 IAW SRM 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

LEFT INTERCOSTAL CLIP IS CRACKED, BETWEEN FS 621 & 625 AT STRINGER 14L, 1.5"LONG. DRILL, LOCATED & INSTALLED NEW SERVICEABLE CLIP 601R350121-5 IAW SRM 51-42-21 & 51-42-22.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,550 hrs · 21,888 cycles

FS 280, RBL 9 INBD & OTBD ANGLES ARE CRACKED. REMOVED CRACKED ANGLES & INSTALLED NEW ANGLES PN 601R31113-58 IAW SRM 51-40-11, 51-42-06, 51-42-21 & 51-42-13.

Part: FLAP — MALFUNCTIONED (WING) · airframe 24,479 hrs · 21,822 cycles

FLAP FAIL AT 2 DURING AFTER LANDING CHECK 1C. PERFORMED TROUBLESHOOTING IAW FIM CHAPTER 27-50-00 REV 47 IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC DATED APRIL 22,2014 & TS 001100-204 FIM TECHNICAL SUPPLEMENT. INTERROGATED FECU IAW AMM 27-51-05 FOUND CODE 171A ON FL 21843 PROBABLE CAUSE 1 JAM 2 DIFFERENTIAL 3. UNSPEC CODE 171A ON FLIGHT LEG 21843 PROBABLE CAUSE 1 JAM 2 RT BPSU 3. WIRING RT BPSU 171A ON FLIGHT LEG 21843 PROBABLE CAUSE 1 JAM 2 RT BPSU 3. WIRING RT BPSU. OPERATIONS TEST OF SDU IAW AMM 27-51-15 GOOD. OPERATION FLAPS IAW AMM 27-54-00. OPERATIONS CHECKED GOOD. NO FURTHER PROBLEMS DETECTED AT THIS TIME. OK FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 24,455 hrs · 21,801 cycles

THE FUSELAGE SKIN BETWEEN FS 626 & FS 640 & STRINGER 19R & 20R IS DENTED 10.3 INCHES X 1.9 INCHES X 0.6 INCHES DEEP. REPAIRED IAW EA CRJ253-03074.

Part: SKIN — DENTED (FUSELAGE) · airframe 24,455 hrs · 21,801 cycles

THE FUSELAGE SKIN HAS MULTIPLE DENTS BETWEEN FS 672 - FS 713 & STRINGER 20R - 23R. REPAIRED IAW EA CRJ253-03079.

Part: SMOKE GOGGLES — MISSING (COCKPIT) · airframe 24,342 hrs · 21,691 cycles

OBSERVER SEAT MISSING SMOKE GOGGLES. INSTALLED OBSERVER SMOKE GOGGLES IAW AMM 25-60-00. ACFT OK FOR SERVICE.

Part: LENS — MISSING (EXIT SIGN) · airframe 23,891 hrs · 21,231 cycles

WHITE LENS CAP MISSING ON OVERHEAD EMER EXIT SIGN. R & R WHITE LENS CAP IAW AMM 33-51-14.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 23,880 hrs · 21,221 cycles

CAPTAIN`S, FIRST OFFICER`S & FLIGHT ATTENDANT`S EMER FLASHLIGHTS FAIL RED LED TEST. R & R EMER FLASHLIGHT BATTERIES IAW 25-60-00.

Part: CONTAINER — TORN (LIFE VEST) · airframe 22,308 hrs · 19,692 cycles

OBSERVER'S LIFE VEST BAG TORN. R & R OBSERVER'S LIFE VEST IAW AMM 25-61-03.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,416 hrs · 18,852 cycles

RIGHT AFT EXTERNAL EMERGENCY LIGHT INOPERABLE. RELAMPED RIGHT AFT EXTERNAL EMERGENCY LIGHT IAW AMM 33-32-01. OPERATIONS CHECK GOOD AT THIS TIME.

Part: DRAIN — UNSECURE (FUEL SYSTEM) · airframe 21,409 hrs · 18,846 cycles

ON FLIGHT 4381 (LGA TO MSP) AIRCRAFT DIVERTED INTO JFK WITH A SUSPECTED FUEL LEAK. FUEL INDICATION WAS DECREASING RAPIDLY IN CRUISE FLIGHT. FUEL ON ARRIVAL INDICATION WAS DECREASING FASTER THAN NORMAL AS WELL. FUEL FLOW TO ENGINES LOOKED NORMAL. TOTAL FUEL INDICATION WOULD DROP 100LBS IN 10 SECONDS, THEN RETURN TO A NORMAL BURN. HAPPENED A FEW TIMES IN FLIGHT. BOTH TANKS EMPTIED TOGETHER, THERE WAS NO IMBALANCE. INSPECTED AND FOUND WATER DRAIN LEAKING RE-SECURED AND PERFORMED FUEL CHECK FOR PARTICLE CONTAMINATION IAW AMM 12-11-28. NO WATER OR ANY OTHER PARTICLES FOUND.

Part: VANE — CHAFED (TE FLAP) · airframe 21,265 hrs · 18,717 cycles

RIGHT INBOARD FLAP VANE CHAFED WHERE VANE HITS THE STOPS. REPAIRED IAW SRM 51-25-00/51-40-11/51-42-13.

Part: SKIN — DENTED (FUSELAGE) · airframe 21,265 hrs · 18,717 cycles

SKIN DENT AT FS 700, S-21L TO S-22L MEASURING 3.54 X 1.93 X 0.118. REPAIRED IAW SRM 53-00-31 REPAIR 3.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 21,010 hrs · 18,467 cycles

RIGHT FWD OVERWING EMERGENCY LIGHT WILL NOT ILLUMINATE. REPLACED & OP CHECKED BATTERY CHARGER ASSY PS2LF IAW CRJ200 33-51-05. ALL TEST GOOD. DM 76228 CLEARED PLACARD PULLED.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,078 hrs · 175,556 cycles

LEFT AND RIGHT FORWARD EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT NR 1 CHARGER ASSEMBLY IAW AMM 33-51-04. REPLACED AND REPLACED EMERGENCY LIGHT NR 1 BATTERY IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: LANDING GEAR — WARNING MESSAGE

FLT 3666, A GEAR DISAGREE MESSAGE OCCURED DURING RETRACTION. MAINTENANCE HAS BLED SYSTEM AND RETURNED ACFT BACK TO SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,953 hrs · 16,449 cycles

THE 559 SEMI-PRESSURE BULKHEAD CRACKED IN WEB ANGLE AT LBL 18 AND RBL 18. REPAIRED IAW PINNACLE PA53-025 IAW BOMBARDIER REO 601R-53-41-260 REV E AND 601R-53-41-609 REV B.

Part: SELECTOR VALVE — DEFECTIVE (MLG) · airframe 18,953 hrs · 16,449 cycles

GEAR DISAGREE IN FLT. REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM 32-32-10. OPS CHECK GOOD. VERIFIED PARTS EFFECTIVITY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,672 hrs · 16,167 cycles

NR 4 BATTERY DEAD. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY IAW AMM 33-51-04. OPC GOOD, VERIFIED PART EFFECTIVITY.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 18,672 hrs · 16,167 cycles

NR 4 E-BATTERY CHARGER INOP. REMOVED AND REPLACED NR 4 E-BATTERY CHARGER IAW AMM 33-51-05. OPC GOOD VERIFIED PART EFFECTIVITY.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,643 hrs · 16,139 cycles

AFT PRESSURE BULKHEAD CRACKED AT FS 621 AT THE LT LINTEL FITTING CRACK 0.150 INCH LONG AT THE 10 O'CLOCK. REPAIRED IAW BOMBARDIER REO 601R53-61-1230.

Part: SKIN — DENTED (RT MLG) · airframe 7,196 hrs · 14,803 cycles

RIGHT MAIN LANDING GEAR (RT MLG) DOOR WAS FOUND DENTED ON THE LEADING EDGE, AFFECTING BOTH THE INNER AND OUTER SKINS. THE DENT MEASURES 1.095 L X 0.46 W X 0.108 D. TEMPORARY REPAIR IAW STS ENGINEERING EA 9-2011-19. REPEAT INSPECTIONS EVERY 100 FH. AT THE NEXT SCHEDULED C CHECK REMOVE AND REPLACE THE DAMAGED RT MAIN LANDING GEAR DOOR WITH A SERVICEABLE DOOR.

Part: SKIN — DENTED (SPOILER) · airframe 17,196 hrs · 14,803 cycles

THREE DENTS WERE FOUND ON THE RIGHT WING OUTBOARD GROUND SPOILER UPPER SURFACE: .50L X .50W X .003DEEP, .55L X.55W X .003DEEP, .48L X .30W X .002DEEP. TEMPORARY REPAIR IAW STS ENGINEERING EA 9-2011-21. WITHIN 1000 FLIGHT HOURS ACCOMPLISH EITHER A PERMANENT REPAIR TO THE DAMAGED SPOILER USING AN SRM OR OTHER APPROVED REPAIR, OR REMOVE AND REPLACE THE DAMAGED SPOILER WITH A SERVICEABLE UNIT USING OEM APPROVED PROCEDURES.

Part: HINGE — GOUGED (TE FLAP) · airframe 17,148 hrs · 14,766 cycles

DAMAGE WAS FOUND ON THE RIGHT WING INBOARD FLAP HINGE ATTACHMENT AT WS=80.5. DAMAGE TO THE P/N 601R14100-68 HINGE ATTACHMENT CONSISTS OF A GOUGE MEASURING 0.210 LONG BY 0.120 WIDE WITH A MAXIMUM DEPTH OF 0.041. PERMANENT REPAIR IAW STS ENGINEERING EA-09-PINN-2011-010A.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,154 hrs · 14,766 cycles

LEFT WING LOWER PLANK ACCESS HOLE NR 1 FOR 540BB AND NR 11 FOR 550CB HAVE CORROSION AT INBOARD AND OUTBOARD ENDS NOT IN CRITICAL REGION. REPAIRED RIGHT WING LOWER PLANK ACCESS HOLE NR 1 FOR 540BB AND NR 11 FOR 550CB AT INBOARD RADII IN THE NONCRITICAL REGIONS IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,154 hrs · 14,766 cycles

SUPPORT FITTING AT FS 319.70 RBL 36 IS CORRODED. REMOVED AND REPLACED JOINT ANGLE FITTING AT FS 319.70 RBL 36 IAW CRJ-200 SRM 51-42-21 AND 51-42-06.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 17,154 hrs · 14,766 cycles

FS 621 PRESSURE BULKHEAD IS CHAFED 0.004 INCH DEEP AT LBL 36.20 AND WL 100.00. PERFORMED A MAJOR REPAIR AT FS 621.00 ON PRESSURE BULKHEAD AT LBL 36.20 AND WL 100.00 BY MANUFACTURING DOUBLERS, FILLER, AND INSTALLING REPAIR PARTS IAW REO 601R-53-61-1285 REV B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,154 hrs · 14,766 cycles

LT AND RT SIDE SEAT TRACK CORRODED BETWEEN FS 449 AND 473 UNDER OVERWING EMERGENCY EXIT DOOR CUTOUTS. REMOVED AND REPLACED LT AND RT SIDE SEAT TRACK BETWEEN FS 449 AND 473 IAW CRJ 200 AMM 53-01-11-400-802.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,154 hrs · 14,766 cycles

FS 202.75 PRESSURE BULKHEAD IS CRACKED AT BRAKE CABLE PASS-THRU HOLE. REPAIRED 202.75 PRESSURE BULKHEAD IAW REO 601R-53-11-563 AND BSC STANDARD REPAIR 601R-53-0101A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,154 hrs · 14,766 cycles

FLOOR SUPPORT ANGLES AT FS 280 LBL 27 TO RBL 27 HAS MULTIPLE AREAS OF CORROSION. REPAIRED FLOOR SUPPORT ANGLES AT FS 280 LBL 27 TO RBL 27 IAW BOMBARDIER REO 601R-53-11-136 AND BSC SR 601R-53-0097A.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,154 hrs · 14,766 cycles

FWD J-ANGLE AT FS 280 RBL 9 TO LBL 9 HAS SEVERE CORROSION. REMOVED AND REPLACED FWD J-ANGLE AT FS 280 RBL 9 TO LBL 9 IAW CRJ 200 SRM 51-42-06.

Part: SENSOR — FAILED (LT ENGINE) · airframe 15,076 hrs · 12,768 cycles

DURING CLIMBOUT OF KRDU THE FLIGHT CREW NOTICED THE LT ENGINE OIL TEMPERATURE WAS INDICATING HIGH. THE FLIGHT CREW REDUCED POWER ON THE ENGINE WHICH CAUSED A REDUCTION IN THE OIL TEMPERATURE TO THE TOP OF THE AMBER LIMIT. THE FLIGHT CREW PERFORMED THE QRH AND REQUESTED TO DIVERT TO TYS. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KTYS. COMPANY MAINTENANCE DETERMINED THAT THE ENGINE OIL WAS OVERSERVICED DUE TO A FAILED HIGH LEVEL SENSOR IN THE REMOTE OIL SERVICING SYSTEM. THE REMOTE SERVICING SYSTEM WAS DEFERRED, ENGINE OIL DRAINED TO NORMAL LEVEL AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 8,092 hrs · 6,663 cycles

RECEIVED FLAP FAILURE MESSAGE ON APPROACH DECLARED EMERGENCY FOLLOWED QRH LANDED WITHOUT INCIDENT. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21

Part: PRIORITY VALVE — FAILED (LT MLG)

LEFT MAIN GEAR FAILED TO EXTEND WHEN GEAR SELECTED DOWN. EMERGENCY DECLARED, QRH PROCEDUERS FOLLOWED WITH UNEVENTFUL LANDING. REMOVED AND REPLACED MAIN LANDING GAR PRIORITY VALVE IAW AMM 32-32-15. (M)