N8694A

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 31,216 hrs · 28,747 cycles

EMERGENCY FLOOR PATH LIGHTING FROM ROWS 2 TO ROW 5 NOT LIGHTING UP. FOUND BROKEN CONNECTOR ON FLOOR TRACK LIGHT. REPLACED CONNECTOR, PER ESPM 20-17-00. EMERGENCY LIGHTS CHECK GOOD, PER AMM 33-51-00.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,445 hrs · 27,837 cycles

EMERGENCY FLOOR LIGHTS ROW 9 TO 13 INOP RESECURED PWR SUPPY STRIP @ AFT CABIN FLOO. OPS CHECK GOOD. C/W IAW 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 30,289 hrs · 27,675 cycles

FLOOR EMERGENCY LIGHT STRIP AT ROW 12 INOP REMOVED AND REPLACED EMREGENCY LIGHT FLOOR STRIP AT ROW 12 IAW CRJ 200 AMM 33-51-01. OPS CHECK GOOD. P/N ON/OFF 36378-2

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,136 hrs · 27,519 cycles

EMERGENCY LIGHT FULLY DRAINED IT NEED TO BE RE-CHARGED REMOVED AND REPALCED BATTERY PACK ASSY: PS4LF, PS1LF, PS2LF, PS3LF IAW CRJ 200 JOBCARD 33-900-701 OPS CHECK GOOD

Part: CABLE — DEFECTIVE (CABIN) · airframe 29,649 hrs · 27,028 cycles

FLOOR TRACK LIGHTING LAMP 9 TO 12 DS20LY IS INOP. REMOVED & REPLACED CABLE ASSY IAW ESPM 20-17-31. OPS TEST GOOD.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

FS 621 RBL WEB HAS A CRACK INDICATION NOTED AT TOP OF CARGO DOOR TRACK LBL 27 WL 130.5 .300" LONG EXTENDING UNDER CARGO DOOR TRACK. 100% FSH FAILED NDT INSP. INCLUDES 8769465/35 & 45. C/W REPAIR TO FS 621 RBL WEB AT THE TOP OF THE CARGO DOOR TRACK IAW BSC REO 601R-53-61-1541 REV F DATED 11/12/14.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

AC GROUND POWER SUB STRUCTURE CRACKED AT FWD AND AFT BOLTS. INCLUDES 876461/203. REMOVED EXTERNAL A/C POWER, RECEPTACLE, REMOVED EXTERNAL SERVICE PNL. REMOVED AND REPLACED GROUND POWER RECEPTACLE SUPPORT BRACKET. REINSTALLED POWER RECEPTACLED AND EXTERNAL SERVICE PNL. OPS CHECK GOOD IAW AMM 24-41-03-400-802, 24-41-01-400-801 & SRM 51-40-11,

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

FS 621 RPB WEB HAS 4 EA CHAFES FROM SCREWS AT WL 103 AT RBL 36, 27, 18 AND LBL 8. REPAIRED BULKHEAD IAW REO 601R-53-61-2155.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

AFT CARGO BAY FS 621 FLOOR SUPPORT AT RBL 14 HAS A HOLE THROUGH THE STRUCTURE. RECEIVED & PERFORMED THE REO 601R-53-61-7119 REV- DATE 08/28/19 FOR REPAIR AFT CARGO BAY FS 621 FLOOR SUPPORT AT RBL 14 AND PREVENT CORROSION CIC IAW SRM 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

RT FLOOR SEAT TRACK AT FS 409.0 TO 409.00+128 CORRODED. REMOVED, FABBED AND INSTALLED RH FLLOR SEAT TRACK AT FS 409 TO 409+128 IAW REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

LT FLOOR SEAT TRACK CORRODED AT FS 409.09 TO 409.00+128. REMOVED, FABBED AND INSTALLED LT SEAT TRACK ON FLOOR AT FS 409.00 TO 409+128 IAW AMM 53-01-11-400-802 AND GREO 601R-53-00-485 REV D DATED 01/29/18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

LT SIDE SEAT TRACK FS 409+32 TO 409+28 CORRODED. INCLUDES 8769461/184. REMOVED, FABRICATED AND INSTALLED SIDE SEAT TRACK FROM FS 409+32 TO FS 409+128 IAW AMM 53-01-11-400-802 AND GREO 601R-53-00-055 REVC 03/21/17.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

SERVICE DOOR FLOOR SUPPORT ANGLE CORRODED. REMOVED AND REPLACED SERVICE DOOR SUPPORT ANGLE PN 601R38303-253 IAW SRM 51-40-11, 51-41-02 AND 57-42-21. ADJUSTMENT CHECK GOOD.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 29,649 hrs · 27,028 cycles

PAX DOOR HANDLE HOUSING, INNER AFT ANGLE CRACKED. REMOVED AND REPLACED PAX DOOR HANDLE HOUSING INNER AFT ANGLE P/N 601R318072-1 IAW SRM 51-40-11 T/R51-42 AND SRM 51-42-06. OPS TEST GOOD.

Part: SUPPORT STRAP — CORRODED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

FLOORBOARD SUPPORT STRAP AT FS 559 LBL 36 IS CORRODED. REMOVED AND REPLACED SUPPPORT STRAP AT FLOORBOARD FS 559 LBL36 IAW SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

FS 280 CROSSMEMBER HAS 2EA CRACKED ANGLES @ LBL/RBL 9. REMOVED AND REPLACED 2EA ANGLES @ LBL/RBL 9.0 IAW BSC REO 601R-53-11-923 STEP 20 AND SRM 51-42-22 AND 51-42-21.

Part: SUPPORT STRAP — CORRODED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

FLOORBOARD SUPPORT STRAP AT F.S. 559 RBL 36 IS CORRODED. REMOVED AND REPLACED SUPPORT STRAP AT FLOOR BOARD FS 559 RBL 36 IAW SRM 51-24-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

FS 484.00 LBL 27 FLOOR SUPPORT CHANNEL ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE (CLIP) FS 484.00 LBL 27 FLOOR SUPPORT CHANNEL IAW SRM 51-42-20 AND 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

FS 484.00 RBL 27 FLOOR SUPPORT CHANNEL ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE (CLIP) FS 484.00 RBL 27 FLOOR SUPPORT CHANNEL IAW SRM 51-42-20 AND 51-42-21.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 29,649 hrs · 27,028 cycles

FWD HYD BAY, TOP BRACKET FOR COMPENSATOR BROKE. REMOVED AND REPLACED BROKEN COMEPNSATOR BRACKET WITH NEW SERVICEABLE BRACKET PN 601R75248-3 IAW SRM 51-41-02.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 29,649 hrs · 27,028 cycles

RT MLG WHEEL WELL HYD TRANSDUCER BRACKET CRACKED. REMOVED AND INSTALLED BRACKET IN RT MLG WELL IAW SRM 51-42-06.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,395 hrs · 25,709 cycles

RH WING EMERGENCY LIGHT 8 INOP REMOVED AND REPLACED BULB FOR EXTERIOR EMERGENCY LIGHT 8 IAW CRJ 200 AMM 33-51-21. OPS CHK GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 28,120 hrs · 25,420 cycles

EMERGENCY LIGHT INOPERATIVE AT FLOOR IN PASSENGER ENTRANCE BY PAX DOOR PULL HANDLE. REPAIRED WIRES TO SAID EMERGENCY LIGHT IAW ESPM 20-00-00.OPERATIONAL CHECK GOOD.

Part: POST — CRACKED (FUSELAGE) · airframe 27,855 hrs · 25,148 cycles

DURING COMPLIANCE OF T/C 53-160-604(DETAILED INSPECTION OF THE VERTICAL BEAMS ON FRAME FS 409.0+128 AND FRAME FS 559.0), NOTED FS409.0+128 LBL 18.00 IS CRACKED. OB LWR FLANGE EXTENDING UP TO AND PAST 1SR RIVET ENDING BETWEEN 1ST AND 2ND RIVET GOING UP. REPAIRED VERTICAL POST LBL 18 FS 409.0+128 OB LWR FLANGE IAW REO 601R-53-41-0056. THIS IS A MAJOR REPAIR.

Part: OXYGEN MASK — LEAKING (PORTABLE O2) · airframe 27,831 hrs · 25,119 cycles

PORTABLE O2 4LMP MASK IS LEAKING FROM GREEN INDICATOR AREA. R&R PORTABLE O2 4LPM MASK IAW AMM 35-31-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,363 hrs · 24,599 cycles

RT OVERWING EMERGENCY LIGHT NOT WORKING. REPLACED THE LAMPS AMM 33-51-21 OPS CHECKED GOOD. CLEANED THE CONTACTS IAW ESPM 20-17-10.

Part: POST — CRACKED (FUSELAGE) · airframe 27,261 hrs · 24,492 cycles

LT VERTICAL POST AT BL 27.00 ON BULKHEAD AT 409.00+128 FOUND TO HAVE A 1" CRACK AT BOTTOM OF IB CHANNEL. REPAIRED LT VERTICAL POST AT LBL 27.00 FS 409.00+128 PER REO 601R-53-41-056. REPAIR ANGLE MATERIAL S6144-4.

Part: POST — CRACKED (FUSELAGE) · airframe 27,261 hrs · 24,492 cycles

RT VERTICAL POST AT BL 27.00 ON BULKHEAD AT 409.00+128 FOUND TO HAVE 7/8" CRACK AT BOTTOM OF IB CHANNEL. REPAIRED RT VERTICAL POST AT RBL 27.00 FS409+128 PER REO 601R-53-41-056. REPAIR ANGLE MATERIAL S6144-4.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 27,050 hrs · 24,272 cycles

FA FLASHLIGHT STRAP IS MISSING AND THE RED LIGHT ISN`T FLASHING. REPLACED THE FLASHLIGHT BATTERY. IAW CMM #25-60-02.

Part: EXTINGUISHER — DAMAGED (COCKPIT) · airframe 26,295 hrs · 23,452 cycles

COCKPIT PORTABLE FIRE EXTINGUISHER DISCHARGE HOSE BENT CLOSED. REMOVED AND REPLACED PORTABLE FIRE EXTINGUISHER AS PER JOB CARD 26-900-700 P/N ON/OFF - 100-9750, S/N OFF - W-950108, S/N ON - W-950665

Part: OXYGEN BOTTLE — DAMAGED (PORTABLE) · airframe 26,240 hrs · 23,389 cycles

BROKEN ON & OFF KNOB ON PORTABLE OXYGEN BOTTLE. REPLACED THE PORTABLE OXYGEN BOTTLE IAW AMM 35-30-00.

Part: FRAME — CRACKED (BS 333) · airframe 24,667 hrs · 21,799 cycles

DURING A MAINTENANCE INSPECTION, A CRACK MEASURING 0.5 WAS FOUND AT BS 333. THE CRACK WAS FOUND AT A TOOLING HOLE, WHICH MEASURES 0.25 IN DIAMETER, JUST BELOW STRINGER 1L.

Part: SENSING ELEMENT — INOPERATIVE · airframe 26,210 hrs · 23,354 cycles

14TH DUCT CAUTION DURING CLIMBOUT, RETURNED TO FIELD IAW QRH. REMOVED AND REPLACED THE SENSING ELEMENT IAW AMM 36-21-04. OPS CHECKED GOOD IAW AMM 36-21-00.

Part: HOSE — DAMAGED (OXYGEN MASK) · airframe 26,085 hrs · 23,226 cycles

PORTABLE OXYGEN BOTTLE, OXYGEN MASK HOSE DAMAGED. REMOVED & REPLACED THE OXYGEN MASK IAW AMM TS 000340R1

Part: SMOKE GOGGLES — BROKEN (COCKPIT) · airframe 23,515 hrs · 22,451 cycles

CAPTAIN`S SMOKE GOGGLES FOUND BROKEN. R & R THE GOGGLES IAW AMM 25-60-00.

Part: ACTUATOR — INOPERATIVE (TE FLAPS) · airframe 25,306 hrs · 22,443 cycles

FLAPS FAILED AT ZERO DURING DECENT. PERFORMED QRH. NO OTHER ABNORMAL EVENTS. FOUND RT OTBD FLAP, OTBD ACTUATOR LOCKED UP AT -52 C, AND NR 4 AND 5 RT FLEXSHAFTS DAMAGED. R & R THE FLAP ACTUATORS IAW AMM 27-53-05.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 25,299 hrs · 22,435 cycles

FLAPS FAIL CAUTION ON APPROACH WHEN FLAPS SELECTED TO 8 AT APPROXIMATELY 190 KIAS QRH COMPLETED. TOUCHDOWN OCCURRED AT 300 FPM PERFORMED TROUBLESHOOTING PER FIM 27-50-00 REV 5 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC LOG 16-26 DATED 5/27/2016 AND TS 00110R3 FIM TECH SUPPLEMENT. FECU FAULT CODES 5 1A,5 2A,17 1B,17 2B,5 2A,17 1B. R&R RT IB IB AND RT IB OB ACTUATORS IAW AMM 27-53-01. OPC OF FLAP SYSTEM GOOD IAW AMM 27-54-00. P/NS ON/OFF 852D100-25, S/N ON 3882, OFF 5669 FOR RT IB, S/N ON 6433, OFF 7370 FOR RT IB OB.

Part: BPSU — INOPERATIVE (TE FLAP SYSTEM) · airframe 25,298 hrs · 22,434 cycles

APPROACHING FINAL, WENT TO SELECT FLAPS 8, & FLAPS FAIL CAUTION MESSAGE. RAN APH, LANDED WITH OUT INCIDENT. REMOVED AND REPLACED THE LT BPSU IAW AMM 27-51-10.

Part: ACTUATOR — INOPERATIVE (TE FLAP SYS) · airframe 25,210 hrs · 22,341 cycles

FLAPS FAILED AT 0 DEGREES DURING APPROACH. PERFORMED TROUBLESHOOTING IAW FIM 27-50-00 REV 51 IAW AD 2009-06-12 PARA H,6,I. REMOVED AND REPLACED THE LT FLAP ACTUATORS. REPLACED THE LT NR 4 FLEXSHAFT AND RT NR 5. RIGGED AND OPS CHECKED GOOD.

Part: STOWAGE BOX — LEAKING (OXYGEN MASK) · airframe 25,025 hrs · 22,156 cycles

CAPTAIN`S OXYGEN MASK LEAKING. REMOVED AND REPLACED THE CREW OXYGEN MASK STOWAGE BOX IAW AMM 35-11-15 OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,864 hrs · 21,997 cycles

EMERGENCY LIGHT BULB BURNED OUT. R & R THE BULBS. OPS CHECK NORMAL, OK FOR SERVICE IAW AMM 33-11-05 & AMM 31-11-00.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 24,669 hrs · 21,800 cycles

LAV O2 MASK FELL DOWN, RESTOWED MASK.

Part: ATTACH ANGLE — CRACKED (BS 621) · airframe 24,667 hrs · 21,799 cycles

AFT EQUIPMENT COMPARTMENT BS 621 BULKHEAD INTERCOSTAL LT ATTACH ANGLE IS CRACKED AT STRINGER 13L. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-42-21. LEAK TESTED IAW AMM 52-31-07-720-801, STEP 3 A7(A-C).

Part: LATCH — FAILED (OXYGEN DOOR) · airframe 24,667 hrs · 21,799 cycles

DURING OPS CHECK OF OXYGEN MASK, PSU NR 5 FROM FWD ON LEFT SIDE OXYGEN DOOR FAILED TO DEPLOY. REMOVED AND REPLACED OXYGEN DOOR LATCH IAW 35-21-05 OF AMM. OPS CHECKED GOOD IAW AMM 35-20-00-710-803.

Part: SHROUD — PUNCTURED (LT WING) · airframe 24,667 hrs · 21,799 cycles

LEFT WING L/E WS 82 SHOUD IS PUNCTURED. REMOVED AND REPLACED THE SHROUD IAW SRM 51-42-13. OPS CHECKED GOOD IAW AMM 30-11-00 TASK 30-11-00-710-802 STEP 3 A-C.

Part: FRAME — CRACKED (BS 333) · airframe 24,667 hrs · 21,799 cycles

FRAME AT BS 333 BETWEEN STR 0 - 3L IS CRACKED. REPAIRED THE FRAME IAW CRJ253-04507 REV. D.

Part: STRINGER — CORRODED (BS 333-349) · airframe 24,667 hrs · 21,799 cycles

STRINGER 26R IS CORRODED IN NUMEROUS AREAS BETWEEN BS 349 & 333. REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03 AND SRM 51-25-06.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 24,667 hrs · 21,799 cycles

BS 621 STRINGER 14L INTERCOSTAL ANGLE WAS FOUND TO BE CRACKED. REMOVED AND REPLACED THE INTERCOSTAL ANGLE IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 24,667 hrs · 21,799 cycles

LEFT WING INBD FLAP VANE L/E CHAFED IN THREE PLACES INBD, CTR AND O/B AREAS. I FLAP VANE SKIN REMOVED AND REPLACED IAW REO 601R-57-52-004.

Part: BULKHEAD — CHAFED (BS 621) · airframe 24,667 hrs · 21,799 cycles

AFT PRESSURE BULKHEAD FWD FACE CHAFED UNDER NUTPLATE BRACKET AT LBL 9. REPAIRED AFT PRESSURE BULKHEAD IAW REO 601R-53-61-5754.

Part: LATCH — DAMAGED (DOOR) · airframe 24,667 hrs · 21,799 cycles

GROUND AIR CONNECTION DOOR LATCHES ARE HARD TO OPEN. REMOVED AND REPLACED THE LATCHES IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 24,667 hrs · 21,799 cycles

RIGHT SIDE SEAT TRACK NR 3 HAS CORROSION FROM BS 409+20 - 409+98. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 400-409) · airframe 24,667 hrs · 21,799 cycles

SEAT TRACK NR 2 BS 400 - 409.0+32 LBL 9 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: WINDOW FRAME — CRACKED · airframe 24,667 hrs · 21,799 cycles

WEB BELOW LEFT WINDSHIELD SIDE POST SUPPORT IS CRACKED. REMOVED AND REPLACED WEB BELOW LEFT WINDSHIELD SIDE POST IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 546-559) · airframe 24,667 hrs · 21,799 cycles

LEFT SIDE SEAT TRACK NR 7 HAS CORROSION FROM BS 546 TO 559+28. REMOVED & REPLACED THE SEAT TRACK AMM 53-00-11.

Part: SEAT TRACK — GOUGED (BS 409) · airframe 24,667 hrs · 21,799 cycles

SEAT TRACK NR 3 BS 409.0+40 RBL 9 IS GOUGED. REMOVED AND REPLACED THE SEAT TRACK FROM BS 394 - 409+128. IAW AMM 53-01-11-400-804.

Part: SEAT TRACK — CORRODED (BS 504-536) · airframe 24,667 hrs · 21,799 cycles

RIGHT SIDE SEAT TRACK NR 6 HAS CORROSION BS 504, 521 AND 536. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485.

Part: SEAT TRACK — GOUGED (BS 559) · airframe 24,667 hrs · 21,799 cycles

SEAT TRACK RBL 9 IS GOUGED BETWEEN BS 559 - 559 + 16. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 368-412) · airframe 24,667 hrs · 21,799 cycles

RIGHT SIDE SEAT TRACK NR 2 HAS CORROSION FROM BS 368 - 385 AND FROM BS 398 - 415. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — GOUGED (BS 409) · airframe 24,667 hrs · 21,799 cycles

SEAT TRACK NR 3 BS 409.0+84 LBL 9 IS GOUGED. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: STIFFENER — CRACKED (RT EXHAUST) · airframe 24,667 hrs · 21,799 cycles

RIGHT ENGINE EXHAUST NOZZLE HAS CRACKED 2ND STIFFENER FROM L/E AT 8 O'CLOCK POSITION. REPAIRED IAW CMM 78-11-00-300-810-A01.

Part: SEAT TRACK — CORRODED (BS 457) · airframe 24,667 hrs · 21,799 cycles

RIGHT SIDE SEAT TRACK NR 5 HAS CORROSION AT BS 457. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SKATE ANGLE — CRACKED (PAX DOOR) · airframe 24,667 hrs · 21,799 cycles

PASSENGER DOOR AFT SKATE ANGLE IS CRACKED AT ATTACH FASTENER. REMOVED & REPLACED THE AFT SKATE ANGLE IAW REO 601R-52-11-513.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,667 hrs · 21,799 cycles

PASSENGER CABIN FLOORBEAM BS 280 AFT SIDE ATTACH ANGLE IS CRACKED LBL 9 INBD SIDE. REMOVED & REPLACED CRACKED ANGLE IAW SRM 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,667 hrs · 21,799 cycles

PASSENGER CABIN FLOORBEAM BS 280 AFT SIDE ATTACH ANGLE IS CRACKED RBL 9 INBD SIDE. REMOVED & REPLACED CRACKED THE ANGLE IAW SRM 51-42-21.

Part: BRACKET — CRACKED (DOOR TRACK) · airframe 24,667 hrs · 21,799 cycles

CARGO DOOR FORWARD TRACK LOWER BRACKET IS CRACKED. REMOVED AND REPLACED CARGO DOOR FORWARD TRACK, LOWER BRACKET IAW SRM 51-42-06.

Part: TIRE — FAILED (MLG) · airframe 24,135 hrs · 21,289 cycles

BOTH OUTSIDE MAIN TIRES BLOWN ON LANDING. REPAIRED MLG AND REPLACED BOTH MLG TIRES.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 23,634 hrs · 20,792 cycles

INBOARD GROUND SPOILER FAULT MESSAGE, INFORMATION ONLY FOLLOWED THE FAULT. RESET PROCEDURE IN CFM CHAPTER 6 FOR SPOILER FAULTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,200 hrs · 20,376 cycles

EMERGENCY CEILING LIGHT 3 INOPERABLE. CURRENTLY DEFERRED UNDER DEF-005629-2013.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,088 hrs · 20,277 cycles

AFT PRESSURE BULKHEAD AT FS 621 FOUND CRACKED IN THREE LOCATIONS AROUND FORWARD CARGO DOOR LINTEL. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: DUCT — UNSECURE (AIR DISTRIBUTION) · airframe 22,188 hrs · 19,383 cycles

BOTH PACKS ARE BLOWING HEAVY CONDENSATION OBSTRUCTING VIEW OUT WINDOW & FLIGHT CABIN GAGES. CABIN FLOOR LEVEL LIGHT IS OBSTRUCTED BY FOG. FOUND RH PACK SECONDARY OUTLET DRAIN HOSE BROKEN. REMOVED AND REPLACED HOSE IAW AMM 21-51-07. FOUND LEFT HAND DISTRIBUTION DUCT OFF THE AIR DISTRIBUTION MANIFOLD. RESECURED IAW AMM 21-21-00. OPS CHECK AND LEAK CHECK GOOD, AIRCRAFT OK FOR SERVICE.

Part: CONTAINER — TORN (LIFE VEST) · airframe 22,155 hrs · 19,351 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,005 hrs · 19,205 cycles

LEFT AFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 21,972 hrs · 19,169 cycles

FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE ROW 2-5. PERFORMED OPS CHECK OF EMERGENCY FLOOR TRACK LIGHTING IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 21,824 hrs · 19,012 cycles

FIRST OFFICER’S FLASHLIGHT RED LIGHT INDICATION. REMOVED AND REPLACED FIRST OFFICER’S FLASHLIGHT BATTERY IAW AMM 25-60-00.

Part: FUEL CELL — LEAKING (LT WING) · airframe 21,803 hrs · 18,988 cycles

ON LEFT MAIN GEAR, FUEL VISIBLY LEAKING. THERE IS A PUDDLE LOCATED UNDERNEATH TIRES. SEALED SEAM ON AFT SPAR MAIN LANDING GEAR TRUNNION IAW SRM 51-23-00-390-808. LEAK CHECKS GOOD.

Part: SIGN — DAMAGED (CABIN) · airframe 21,513 hrs · 18,715 cycles

EMERGENCY EXIT SIGN ON FWD WALL IN ENTRANCE WAY IS CRACKED AND BROKEN. REMOVED AND REPLACED LIGHT ASSY EMERGENCY EXIT E REF 33-10-00.

Part: ENGINE — VIBRATION (NR 2) · airframe 21,412 hrs · 18,619 cycles

NR 2 ENGINE VIBRATION IN CAUTION RANGE DURING CLIMB, COULD NOT MAINTAIN CLIMB, COULD NOT MAINTAIN CLIMB CARATS. RETURNED DUE TO RT ENGINE FAN VIBRATION, PULLED BACK THROTTLES AND AND VIBRATION CAME DOWN. NO EMERGENCY DECLARED, R & R ENG VIBE SIGNAL CONDITIONER AND REMOVED AND REPLACED RT ENG FAN ACCELEROMETER, OPS CHECKED GOOD IAW AMM 71-00-00.

Part: UNKNOWN — MALFUNCTIONED (AILERON) · airframe 21,388 hrs · 18,594 cycles

AILERON TRIM INOP. DOES NOT MOVE AT ALL. RESET CB 2F7. OPS CHECK OF AILERON TRIM NORMAL IAW CRJ AMM 27-11-00.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 21,142 hrs · 18,357 cycles

EMERGENCY LIGHTS ROW 8 AND AFT INOP. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY CHARGER IAW CRJ200 AMM 33-51-05. FAULT CLEARED, OK FOR SERVICE AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,123 hrs · 18,340 cycles

EMERGENCY LIGHTS WOULD NOT ILLUMINATE. EMERGENCY LIGHTING BATTERY PACKS WERE FOUND IN A DISCHARGED STATE, AFTER CHARGING FOR SEVERAL HOURS EMERGENCY LIGHTS WERE OPS CHECKED IAW AMM 33-51-00. OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: LANDING GEAR — OBSTRUCTED (NLG) · airframe 21,044 hrs · 18,257 cycles

GEAR DISAGREE WARNING MESSAGE ON TAKEOFF. C/W PA 05-18B. OP CHECKS NORMAL. NO PSEU CODES. FOUND SLUSH AND ICE BUILDUP ON NOSE DOOR + NOSE GEAR. SYSTEM CHECKS GOOD IAW AMM 32-30-00. OK FOR SVC.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 20,935 hrs · 18,168 cycles

LANDING GEAR DISAGREE ON CLIMBOUT NOSE GEAR REMAINED DOWN AND LOCKED QRH COMPLETE. COMPLIED WITH PA05-018B, FOUND AFT CENTERING PROX SENSOR TO BE TOCHING TARGET AND ADJUSTED PROXIMITY SENSOR IAW AMM 32-51-05, THEN PERFORMED GEAR SWING IAW AMM 32-33-00, OPS CHECKED GOOD. OK FOR SERVICE

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 20,930 hrs · 18,164 cycles

NOSE GEAR DISAGREE (RETRACTION) IN FLIGHT. COMPLIED PA 05-018B FOUND AFT PROX SENSOR TO BE TOUCHING TARGET AND RE-ADJUSTED PROX SENSOR IAW AMM 32-61-05. PERFORMED GEAR SWING IAW AMM 32-33-00. OPS CHECK GOOD. OK FOR SVC.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 20,904 hrs · 18,185 cycles

FLOOR EMER LIGHT STRIP NOT WORKING FROM ROW 8 TO BACK OF AIRCRAFT. REMOVED AND REINSTALLED CONNECTOR ( NOTE- LIGHT STRIP CONNECTOR) IAW CRJ AMM 33-51-01. OPS CHECK GOOD. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,689 hrs · 19,830 cycles

AIRPLANE EMERGENCY LIGHT STRIP IS OUT. REMOVED AND REPLACED NR 4 BATTERY IAW AMM 33-51-04. OPS CHECK GOOD. VERIFIED PART EFFECTIVITY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,682 hrs · 17,929 cycles

IN FLOOR EMERGENCY LIGHTS INOP FROM ROW 2 -ROW 6. OP CHECK EMERGENCY FLOOR TRACK LT IAW AMM 33-51-01, OP CHECK GOOD. OK FOR SERVICE.

Part: WIRE — MISINSTALLED (CABIN) · airframe 20,630 hrs · 17,879 cycles

EMERGENCY EXIT FLOOR FLOOD LIGHTS AT PAX ENTRANCE ALL INOP. CORRECTED WIRING TO PASSENGER ENTRANCE EMERGENCY LIGHTS PER WDM 33-40-00 OC GOOD AMM 33-40-00. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,522 hrs · 17,783 cycles

CA FLASHLIGHT NO BLINK. REMOVED AND REPLACED CAPTAIN'S FLASHLIGHT BATTERIES IAW AMM 25-61-04. OPERATIONAL CHECK SATISFACTORY AT THIS TIME. PART EFFECTED VERIFIED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,317 hrs · 16,659 cycles

FS 559 PRESSURE BULKHEAD FOUND CRACKED ON RT SIDE 50 PERCENT FSH AT WL 59.10 APPROXIMATELY .2 INCH IN LENGTH. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 REV E, REO 601R-53-41-609 REV B AND BOMBARDIER SERVICE CORPORATION EO 601R-53-20912.

Part: SKIN — DENTED (RT WING) · airframe 18,320 hrs · 15,730 cycles

DENT (6.5" LX 5.5" W X 0.380" DEEP) TO RT WING FIXED LEADING EDGE (PIN: 601R120161-4 REF) BETWEEN WS 131.80-WS 139.54 DUE TO A BIRD STRIKE. NO DAMAGE TO FASTENERS OR UNDERLYING STRUCTURE. TEMPORARY REPAIR IAW SRM 57-41-31 AND SRM 51-12-00. GOOD TO NEXT C CHECK WHERE A PERMANENT SRM REPAIR OR REPLACEMENT WILL BE PERFORMED.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO)

ON APPROACH INTO DTW RECEIVED "CARGO SMOKE" MASTER WARNING, QRH FOLLOWED. BOTTLES DISCHARGED, DECLARED EMERGENCY FOLLOWED BY UNEVENTFUL LANDING. ACFT INSPECTED BY EMERGENCY VEHICLES WITH NO FIRE OR SMOKE FOUND "FALSE WARNING". REMOVED AND REPLACED THE CARGO FORWARD DETECTOR IAW BOMBARDIER AMM. OPERATIONALLY CHECKED GOOD. (S)

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY)

ON APPROACH INTO DTW RECEIVED "CARGO SMOKE" MASTER WARNING. QRH FOLLOWED, BOTTLES DISCHARGED. EMERGENCY FOLLOWED BY UNEVENTFUL LANDING. ACFT INSPECTED BY EMERGENCY VEHICLES WITH NO FIRE OR SMOKE FOUND "FALSE WARNING". REMOVED AND REPLACED THE CARGO FORWARD DETECTOR IAW BOMBARDIER AMM. OPERATIONALLY CHECKED GOOD. (S)

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY)

RECEIVED CARGO SMOKE MESSAGE AT GATE, DETERMINED AFTER INSPECTION TO BE A FALSE WARNING. POWER RESET TO DATA CONCENTRATOR UNIT (DCU) AND PERFORMED OPERATIONAL CHECK OF CARGO DETECTION SYSTEM IAW BOMBARDIER AMM. NO DEFECTS FOUND. (S)

Part: DETECTION SYS — FALSE ACTIVATION (CARGO SMOKE)

RECEIVED CARGO SMOKE MESSAGE AT GATE, DETERMINED AFTER INSPECTION TO BE A FALSE WARNING. POWER RESET TO DATA CONCENTRATOR UNIT (DCU) AND PERFORMED OPERATIONAL CHECK OF CARGO DETECTON SYSTEM IAW AMM. NO DEFECTS FOUND. (S)

Part: BPSU — MALFUNCTIONED (TE FLAPS)

RECEIVED "FLAP FAIL" MESSAGE ON APPROACH, QRH FOLLOWED WITH UNEVENTFUL LANDING. REMOVED AND REPLACED THE RT BRAKE POSITION SENSING UNIT (BPSU) AND RIGGED FLAPS IAW AMM. (A)

Part: FCU — MALFUNCTIONED (TE FLAPS)

FLAP FAILURE MESSAGE ON TAKEOFF, QRH FOLLOWED, DECLARED EMERGENCY AND RETURNED TO THE AIRPORT. MAINTENANCE INSPECTED FLAP CONTROL SYSTEM AND FOUND A FAILURE WITH THE FLAP ELECTRONIC CONTROL UNIT (FECU). FECU REPLACED PER BOMBARDIER AMM 27-50-00. (S)

Part: FLAP SYSTEM — FAILED · airframe 10,436 hrs · 8,714 cycles

FLAPS FAIL, SECOND OCCURANCE WITHIN 72 HOURS.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT)

ON FINAL APPROACH, A LARGE POPPING NOISE CAME FROM THE FCP PANEL. SHORTLY AFTER IT STARTED TO VENT SMOKE BETWEEN NAV AND ALT BUTTON. CREW DECLARED EMERGENCY, FOLLOWED QRH PROCEDURES, LANDED NO FURTHER INCIDENT. REMOVED AND REPLACED FCP IAW AMM 22-11-07. COMPLIED WITH ALL FUNCTIONAL CHECKS IAW 22-11-07, OPS CHECK GOOD. OK FOR SERVICE. (M)