N8783E

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,782 hrs · 29,858 cycles

EMERGENCY LIGHT SYSTEM IS BURNT OUT FROM ROW 2-6. R/R #2 CHARGER ASSY AND #2 BATTERY PACK IAW AMM 33-51-05 AND 33-51-04. OPS TEST INTERIOR AND EXTERIOR EMERGENCY LIGHTS NORMAL.

Part: FUEL LINE — FAULTY (APU) · airframe 29,912 hrs · 27,690 cycles

STRONGFUEL SMELL FROM PACKS WHEN APU IS RUNNING. REMOVED AND REPLACED APU FUEL LIKE TUBE ASSY AND RIGHT AND LEFT WATER SEPARATOR COALESCER BAG IAW CMM 49-26-43 AND AMM 21-51-13 OPS CK GOOD AT THIS TIME.

Part: RETAINER — CRACKED (LT OVERWING) · airframe 29,476 hrs · 27,244 cycles

SEAL RETAINER IS CRACKED ON LEFT HAND OVERWING ESCAPE DOOR.

Part: BEAM — CHAFED (RT WING TE FLAP) · airframe 29,476 hrs · 27,244 cycles

RH IB FLAP IB VANE ACTUATOR BEAM CHAFED UNDER ROLLER. RH I/B FLAP I/B VANE ACTUATOR BEAM REPAIRED IAW BOMBARDIER REO 601R-57-52-1979 OPS/CLEARANCE CHECK GOOD IAW CRJ 200 AMM 27-54-15-820-801 AND 27-54-00-710-801.

Part: DOUBLER — CRACKED (GROUND POWER) · airframe 29,476 hrs · 27,244 cycles

AC GROUND POWER DOOR 122BR LANDING, FWD EDGE IS MISSING. REPAIRED AC GROUND POWER DOOR 122BR LANDING, FWD EDGE I.A.W. BOMBARDIER REO 601R53-11-569

Part: SUPPORT ANGLE — CRACKED (RT ACM BAY) · airframe 29,476 hrs · 27,244 cycles

RH ACM RACK LWR PRSOV SUPPORT ANGLE CRACKED. REMOVED CRACKED SUPPORT ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-42-06

Part: BEAM — CHAFED (LT WING TE FLAP) · airframe 29,476 hrs · 27,244 cycles

LH IB FLAP OB VANE ACTUATOR BEAM CHAFED UNDER ROLLER. LH I/B FLAP O/B VANE ACTUATOR BEAM REPAIRED IAW REO 601R-57-52-1979 OPS/CLEARANCE CHECK GOOD IAW CRJ 200 AMM 27-54-15-820-801 AND 27-54-00-710-801 AAR AP 453

Part: BEAM — CHAFED (RT WING TE FLAP) · airframe 29,476 hrs · 27,244 cycles

RH IB FLAP OB VANE ACTUATOR BEAM CHAFED UNDER ROLLER. REPAIRED CHAFE UNDER ROLLER ON RH O/B VANE ACTUATOR BEAM ON I/B FLAP RH IAW BOMBARDIER REO 601R-57-52-1979 OPS/CLEARANCE CHECK GOOD IAW CRJ 200 AMM 27-54-15-820-801 AND 27-54-00-710-801

Part: BEAM — CHAFED (LT WING TE FLAP) · airframe 29,476 hrs · 27,244 cycles

LH IB FLAP IB VANE ACTUATOR BEAM CHAFED UNDER ROLLER. REPAIRED CHAFE UNDER ROLLER ON LH I/B FLAP VANE ACTUATOR BEAM IAW BOMBARDIER REO 601R-57-52-1979 OPS/CLEARANCE CHECK GOOD IAW CRJ 200 AMM 27-54-15-820-801 AND 27-54-00-710-801

Part: BEAM — CHAFED (LT WING TE FLAP) · airframe 29,476 hrs · 27,244 cycles

LH IB FLAP MID VANE ACTUATOR BEAM CHAFED UNDER ROLLER. REPAIRED CHAFE ON LH I/B FLAP MID VANE ACTUATOR BEAM UNDER ROLLER IAW REO 601R-57-52-1979 OPS/CLEARANCE CHECK GOOD IAW CRJ 200 AMM 27-54-15-820-801 AND 27-54-00-710-801 AAR SM 107

Part: BEAM — CHAFED (RT WING TE FLAP) · airframe 29,476 hrs · 27,244 cycles

RH IB FLAP MID VANE ACTUATOR BEAM CHAFED UNDER ROLLER. REPAIRED CHAFE ON RH I/B FLAP MID VANE ACTUATOR BEAM UNDER ROLLER IAW BOMBARDIER REO 601R-57-52-1979 OPS/CLEARANCE CHECK GOOD IAW CRJ 200 AMM 27-54-15-820-801 AND 27-54-00-710-801 AAR SM 107

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 29,476 hrs · 27,244 cycles

PAX DOOR UPPER EDGE MEMBER IS CRACKED AT THE AFT SIDE, UNDER TOP STEP 832ET. REPAIRED PAX DOOR UPPER EDGE MEMBER IAW REO 601R-52-11-279

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 29,476 hrs · 27,244 cycles

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

Part: SEAL — WORN (RT NACELLE) · airframe 29,476 hrs · 27,244 cycles

R/H UPPER CORE COWL T/E IS CHAFED, REMOVED OLD AND INSTALLED NEW CLOSURE RING IAW BOMBARDIER CMM 71-12-01.

Part: PLATE — CHAFED (FLAP FAIRING) · airframe 29,476 hrs · 27,244 cycles

FLAP FAIRING 692BB HAS CHAFFED GUIDE PLATE. REMOVED/INSTALLED NEW GUIDE PLATE ON PANEL 692BB IAW CRJ 200 SRM 51-42-06

Part: ANGLE — CRACKED (NAC PANEL) · airframe 29,476 hrs · 27,244 cycles

PYLON PANEL 422BT SEAL RETAINER IS CRACKED. REMOVED & REPLACED SEAL RETAINER IAW CMM 20-42-06.

Part: RETAINER — CRACKED (PYLON ACCESS PNL) · airframe 29,476 hrs · 27,244 cycles

PYLON ACCESS PANEL 422DB SEAL RETAINER IS CRACKED. REMOVED AND REPLACED SEAL RETAINER IAW CRJ-200 SRM-51--42-06.

Part: ANGLE — CRACKED (BS 484) · airframe 29,476 hrs · 27,244 cycles

WHILE PERFORMING INSPECTION OF PRESSURE FLOOR SKIN, NOTED ANGLE CRACKED AF FS484, LBL27 - REMOVED/REPLACED CLIP ANGLE AT FS 484 LBL 27 IAW CRJ 200 SRM 51-42-06 AND 51-42-21.

Part: ANGLE — CRACKED (BS 484) · airframe 29,476 hrs · 27,244 cycles

WHILE PERFORMING INSPECTION OF PRESSURE FLOOR SKIN, NOTED ANGLE CRACKED AF FS484, LBL27. REMOVED/REPLACED CLIP ANGLE AT FS 484 LBL 27 IAW CRJ 200 SRM 51-42-06 AND 51-42-21

Part: RETAINER — CRACKED (PYLON ACCESS PNL) · airframe 29,476 hrs · 27,244 cycles

PYLON ACCESS PANEL 422DB SEAL RETAINER IS CRACKED. REMOVED AND REPLACED SEAL RETAINER IAW SRM-51-42-06.

Part: ANGLE — CRACKED (BS 484) · airframe 29,476 hrs · 27,244 cycles

WHILE PERFORMING INSPECTION OF PRESSURE FLOOR SKIN, NOTED ANGLE AT FS484, RBL27 CRACKED. REMOVED & REPLACED CLIP ANGLE AT FS484 RBL27 IAW CRJ 200 SRM 51-42-21.

Part: STRAP — CORRODED (BS 559) · airframe 29,476 hrs · 27,244 cycles

WHILE ACCESSING INSPECTION AREA, NOTED FLOOR SUPPORT STRAP AT FS559.00 RBL36 IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT STRAP AT BS 559, RBL 36 IAW SRM 51-42-06.

Part: STRAP — CORRODED (BS 559) · airframe 29,476 hrs · 27,244 cycles

WHILE ACCESSING INSPECTION AREA, NOTED FLOOR SUPPORT STRAP AT FS559.00 LBL36 IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT STRAP @ 559 LBL 36 IAW CRJ200 SRM 51-42-06

Part: RUB STRIP — CHAFED (NAC ACCESS PANEL) · airframe 29,476 hrs · 27,244 cycles

PYLON ACCESS PANEL 412DB FIRE SHIELDS ARE CHAFED. REMOVED AND REPLACED FIRESHIELDS AND RUBSTRIPS IAW CRJ200 SRM 51-42-13

Part: RUB STRIP — CHAFED (NAC ACCESS PANEL) · airframe 29,476 hrs · 27,244 cycles

PYLON ACCESS PANEL 422DB FIRE SHIELDS ARE CHAFFED. REMOVED AND REPLACED FIRE SHIELDS AND RUBSTRIPS IAW CRJ200 SRM 51-42-13

Part: RETAINER — CRACKED (ACCESS PNL SEAL) · airframe 29,476 hrs · 27,244 cycles

PYLON ACCESS PANEL 412BT HAS CRACKED SEAL RETAINER. REMOVED AND REPLACED SEAL RETAINER IAW CRJ200 SRM 51-42-06

Part: INTERCOSTAL — CRACKED · airframe 29,476 hrs · 27,244 cycles

INTERCOSTAL JUST AFT OF EXTERNAL POWER PLUG APPEARS TO BE CRACKED AT TOOLING HOLE, LOCATED JUST I/B AND AFT OF ACCESS DOOR 122BR OPENING. - EDGE BLENDED CRACKED AREA IN AFT INTERCOSTAL AT POWER PLUG IAW CRJ 200 SRM T.R 51-44 FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-00-00 APPLIED FINISH IAW CRJ 200 SRM 51-25-16 AAR SM 33

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,297 hrs · 27,047 cycles

AFT FLOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED PS4LF BATTERY AND CHARGER IAW AMM 33-51-05. OPS CHECK GOOD.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 28,777 hrs · 26,506 cycles

SUPPLEMENTAL INFORMATION. EMERGENCY FLOOR LIGHTING HAS 3 SECTIONS INOP FROM SEATS 6-8. FOUND EMERGENCY LIGHT CABLE ASSEMBLY IN FLOOR STRIP WITH BREAKS IN WIRES. INSTALLED NEW CABLE ASSY IAW AMM 33-51-01-400-808. REINSTALLED 3 FLOOR LIGHT SECTIONS IAW AMM 33-51-01-400-801. OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 28,761 hrs · 26,487 cycles

INSIDE EMERGENCY FLOOR LIGHTS CENTER SECTION IS INOPERATIVE. FOUND AND SECURED LOOSE CONNECTION AT SEAT 5C, D LOCATION IAW AMM 33-51-00. OPS CHECK GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 28,276 hrs · 25,963 cycles

EMERGENCY FLOOR LIGHTNING INOP AT EMERGENCY EXIT ROW. FOUND EMER FLOOR LIGHT LOOSE. RESECURED IAW AMM 33-51-01. OP CHECK GOOD, OK FOR SVC.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 28,078 hrs · 25,749 cycles

HAD A SMOKE TOLIET CAUTION MESSAGE AND ALARM WENT IFF, FA WENT TO THE LAVATORY TO CHECK, NO SMOKE OR FUMES WERE FOUND. PERFORMED AN OPERATIONAL TEST OF AFT LAVATORY SMOKE DETECTOR IAW AMM 26-50-00, OPS TESTED GOOD.

Part: POST — CRACKED (FUSELAGE) · airframe 27,944 hrs · 25,598 cycles

DURING COMPLIANCE OF T/C 53-160-635, NOTED VERT POST LBL 27.00 HAS A CRACK ON LWR IB FLANGE EXTENDING FROM EDGE UP TO AND PAST THE 1ST RIVET ENDING APPROX MID POINT BETWEEN 1ST AND 2ND RIVETS. REPAIRED VERT POST LBL 27.00 FS 409+128 IAW REO 601R-53-41-0056. THIS IS A MAJOR REPAIR.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 27,815 hrs · 25,453 cycles

FLOOR EMERGENCY LIGHTS INOPERATIVE. CONNECTED LIGHT AND OPS CHECKED GOOD IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (SEAT 8DC) · airframe 27,660 hrs · 25,265 cycles

SECTION OF EMERGENCY LIGHTING BY SEAT 8DC WAS FOUND INOPERATIVE. R & R THE EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CENTER CABIN) · airframe 27,626 hrs · 25,231 cycles

EMERGENCY FLOOR LIGHT IN THE MIDDLE OF THE CABIN IS NOT ILLUMINATING. PERFORMED AN OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: SEAL — DAMAGED (GALLEY DOOR) · airframe 27,563 hrs · 25,145 cycles

GALLEY DOOR SEAL HAS VENT HOLES MISSING AND VENT HOLES IN WRONG LOCATION BEING BLOCKED IAW AMM 52-41-07. ADDED VENT HOLES AND RELOCATED BLOCKED HOLES IN THE GALLEY DOOR SEAL IAW AMM 52-41-07

Part: LIGHT — UNKNOWN (CABIN) · airframe 27,080 hrs · 24,645 cycles

FLOOR LIGHTING STRIP INOP ROWS -7 AND WALL EXIT SIGN IS INOP PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT PER CRJ 200 AMM 33-51-00. OPS CHECK GOOD, NO OTHER DEFECTS NOTED AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 26,957 hrs · 24,522 cycles

DURING WAKE UP, CO PILOT EMERGENCY FLASHLIGHT WAS FOUND NOT BLINKING. BATTERY NOT CHARGING. REMOVED AND REPLACED THE BATTERY IN THE FLASHLIGHT IAW 25-61-00. OPS CHECKED GOOD.

Part: SMOKE GOGGLES — BROKEN (COCKPIT) · airframe 26,484 hrs · 24,014 cycles

CAPTAIN`S SMOKE GOGGLES BROKEN. REMOVED AND REPLACED THE SMOKE GOGGLES IAW AMM 35-11-12

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,389 hrs · 23,916 cycles

FLOOR LEVEL EXIT LIGHT NEXT TO LEFT EMERGENCY EXIT DOOR INOP. REMOVED AND REPLACED EXIT LIGHT IAW AMM 33-51-10.

Part: LIGHT — INOPERATIVE · airframe 26,345 hrs · 23,870 cycles

CENTER EMERGENCY LIGHT ON LEFT SIDE OF FUSELAGE IS OUT. REMOVED AND REPLACED THE EMERGENCY LIGHT. OPS CHECKED GOOD IAW 33-51-00-710-801.

Part: CONNECTOR — LOOSE (MICROPHONE) · airframe 26,257 hrs · 23,773 cycles

OBSERVER OXYGEN MASK MICROPHONE INOPERATIVE. CONNECTED THE CONNECTOR ON OBSERVERS O2 MASK CASE. PERFORMED AUDIO INTEGRATING SYSTEM TEST IAW 23-51-00.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEATS 2AB) · airframe 26,186 hrs · 23,695 cycles

SEATS 2A & B PASSENGER OXYGEN MASK DOOR RED TAB DOWN AND SHOWING. RESTOWED MASK IAW AMM 35-21-05. OPS CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 2CD) · airframe 26,181 hrs · 23,689 cycles

SEAT 2CD PAX OXYGEN DOOR OPENED IN FLIGHT. SECURED THE PSU DOOR CLOSED WITH TAPE. VERIFIED OXYGEN GENERATOR WAS NOT DEPLETED. RESTOWED THE MASK IAW AMM 35-21-05. OPS CHECKED GOOD.

Part: OXYGEN MASK — DISLODGED (SEAT 2 CD) · airframe 25,909 hrs · 23,401 cycles

ROW 2 SEATS CD OXYGEN MASK HANGING DOWN. STOWED THE OXYGEN MASK IAW AMM 35-21-09.

Part: LIGHT — MALFUNCTIONED (ROWS 6-8) · airframe 25,787 hrs · 23,274 cycles

FLOOR EMERGENCY LIGHTS OUT FROM ROWS 6-8. RESET & OPS TESTED THE EMERGENCY LIGHTS IAW AMM 33-51-00. OPS TESTED OK.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 25,769 hrs · 23,256 cycles

LIGHT, ON EMERGENCY FLASHLIGHT IN GALLEY IS NOT BLINKING. REPLACED THE BATTERY IN THE FLASHLIGHT IAW AMM 25-61-02. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,205 hrs · 22,699 cycles

RT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-51-10.

Part: BATTERY — LOOSE (CABIN) · airframe 24,716 hrs · 22,200 cycles

EMERGENCY LIGHTS MOST FORWARD OVERWING, FORWARD CEILING EXIT SIGN AND LOWER PAX DOOR OPEN ARROW LIGHTS ARE INOPERATIVE. REINSTALLED LOOSE EMERGENCY LIGHT BATTERY AT POSITION NR 2 IAW THE AMM 33-51-04. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,583 hrs · 22,053 cycles

PAX DOOR EXTERIOR E-LIGHT AND SERVICE DOOR EXTERIOR E-LIGHT WILL NOT ILLUMINATE. DIFFERED EXTERIOR E-LIGHTS IAW MEL 33-51-02. PLACARD INSTALLED. UPDATED MM02 CONTACTED MXC 95784 T/S FOUND FUSE F-2 BATTERY PACK 1 AND CR15LY AND FWD CABIN CURVED EXIT SIGN DS5LY ALL BAD. REPLACED ALL UNITS. EMERGENCY LIGHTS TEST OK IAW AMM 33-51-00. OK FOR SERVICE. REMOVED PLACARD, CLEARED MMO2.

Part: WIRE HARNESS — DEFECTIVE (LANDING GEAR) · airframe 24,578 hrs · 22,049 cycles

GEAR DISAGREE MASTER WARNING ON ROTATION. QRH COMPLETE. AFTER QRH WITH GEAR HANDLE DOWN, ALL 3 INDICATIONS WERE GREEN. RESECURED TOW GUARD, FLUSHED AND SERVICED NOSE SHOCK STRUT, REPLACED PROXIMITY SENSOR HARNESS, AND BRACKET IAW TS-000871R6, CMM 32-20-04, JOB CARD 12-710-002, AND AMM 32-61-05. NRCC 097361 AND 097356 FOR DETAILS. ALL CHECKS GOOD AT THIS TIME.

Part: STRUT — NOT REPORTED (NLG) · airframe 24,490 hrs · 21,951 cycles

GEAR DISAGREE WARNING UPON UP SELECTION. MAINS RETRACTED, NOSE STAYED DOWN. QRH COMPLETED FOLLOWED BY NORMAL LANDING. FOUND NLG STRUT TO BE INCORRECTLY SERVICED. RESERVICED NLG STRUT IAW AMM 12-12-32. PERFORMED EXTENSION & RETRACTION OF THE LANDING GEAR SYSTEM IAW AMM 32-30-00. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: SKIN — DAMAGED (RT WING) · airframe 24,487 hrs · 21,947 cycles

REPAIR DAMAGE TO RT OTBD WING LOWER SKIN AT WS 353 - 371. CONTINUATION CARD 8778316 OP 36. REPAIRED RT WING LOWER SKIN IAW 601R10871-S01 FABRICATED & BA REO 601R-57-2447 INSTALLED, REMOVAL & REPLACEMENT.

Part: SKIN — DENTED (FUSELAGE) · airframe 24,487 hrs · 21,947 cycles

FUSELAGE SKIN HAS A DENT AT FS 409+25, APPROX 1.75"L X 1.875"W X .050"D, BETWEEN STRINGERS 15R & 16R. CONTINUATION CARD 8778311 OP 294. REPAIRED SKIN DENT AT FS 409+25, BETWEEN STRINGERS 15R & 16R IAW SRM 53-00-31 REPAIR 1 FIGURE 201.

Part: HINGE — BENT (CARGO BAY) · airframe 24,487 hrs · 21,947 cycles

CENTER HINGE ON CARGO DOOR STEP PLATE IS BENT ON THE INBD & OTBD EDGES. REMOVED & INSTALLED SERVICEABLE CTR HINGE FOR CARGO DOOR STEP PLATE IAW SRM 51-40-11 & SRM 51-42-06 & APPLIED PAINT & PLACARD IAW SRM 51-25-01 & AMM 11-30-00-400-801.

Part: BRACKET — CRACKED (LT PYLON) · airframe 24,487 hrs · 21,947 cycles

BRACKET UNDER LT PYLON ACCESS PANEL 411AL IS CRACKED. CONTINUATION CARD 8778311 OP 358. REPAIRED BRACKET UNDER PANEL 411AL IAW EA CRJ254-04367.

Part: STRAP — CORRODED (FUSELAGE) · airframe 24,487 hrs · 21,947 cycles

FRAME STRAP AT FS 349, STRINGER 18R HAS CORROSION ON UPPER PORTION. CONTINUATION CARD 8778311 OPS 298 & 327. REPAIRED FRAME STRAP IAW EA CRJ253-04329.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 24,487 hrs · 21,947 cycles

621 BULKHEAD VERTICAL STIFFENER AT BL 0 IS CHAFED FROM 10TH STAGE ISOLATION VLV. REPAIRED FS 621 BULKHEAD VERTICAL STIFFENER AT BL 0 IAW EA CRJ253-04299.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,487 hrs · 21,947 cycles

FS 333.00 FRAME, BETWEEN STRINGER 0 & 1L HAS A CRACK AT THE BOTTOM OF A TOOLING HOLE 1/4" LONG. REPAIRED FRAME AT FS 333.00, BETWEEN STRINGER 0 & 1L IAW SRM 51-42-06, 51-42-21, 51-42-13 & 51-40-11. OPERATIONS CHECKED GOOD.

Part: HINGE — CORRODED (PAX DOOR) · airframe 24,487 hrs · 21,947 cycles

CORROSION FOUND ON BOTTOM PAX DOOR STEP HINGE PN 601R31980-65. R & R STEP ASSEMBLY IAW SRM 51-40-11 & 51-42-00.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 24,487 hrs · 21,947 cycles

LEFT STRINGER 3L FWD UPPER ATTACH ANGLE CRACKED & LOWER ATTACH ANGLE NOT INSTALLED JUST AFT OF FS 280. R & R STRINGER 3L ANGLES IAW SRM 51-40-11, 51-42-06, 51-42-21 & 51-25-01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,487 hrs · 21,947 cycles

FS 605, FRAME HAS CORROSION, BETWEEN STRINGER 24R & 26L & AT STRINGER 22L. R & R FS 605 FRAME SECTOR IAW SRM 51-42-06, 51-42-21 & 51-25-01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 24,487 hrs · 21,947 cycles

RIGHT STRINGER 9R, PN 601R31063-57, CRACKED AT FS 310. REPAIRED IAW SRM 53-00-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,487 hrs · 21,947 cycles

LEFT CABIN SIDE SEAT RAILS CORRODED. CONTINUATION CARD 8778311 OP 292. REPLACED CORRODED LT CABIN SIDE SEAT RAILS IAW SRM 51-40-11, 51-25-16 & AMM 53-01-11-400-802.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 24,487 hrs · 21,947 cycles

LEFT WING INBD FLAP, INBD VANE SKIN CHAFED, APPROX 1.0 X .700 X .004. R & R LT INBD FLAP VANE CAP IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,487 hrs · 21,947 cycles

CABIN RT SIDE SEAT RAILS 2 - 6 CORRODED. REPLACED RT SIDE SEAT RAILS 2 - 6, FS 409+16 - FS 559+80 IAW AMM 53-01-11-000 400-802, SRM 51-25-16 & REO 601R-53-00-55.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 24,487 hrs · 21,947 cycles

FOUND CRACK ON TOP OF CHANNEL AFT SIDE OF 202 BULKHEAD, JUST BELOW CTR POST OF WINDSHIELDS. R & R THE CRACKED FITTING AT WINDSHIELD CTR POST LT SIDE IAW SRM 51-42-21.

Part: ANGLE — CRACKED (RT WING) · airframe 24,487 hrs · 21,947 cycles

RIGHT WING LE TRANSITION, BETWEEN INBD & CTR LE OTBD, L ANGLE CRACKED. REMOVED UNSERVICEABLE L ANGLE & LOCATED, DRILLED & INSTALLED NEW SERVICEABLE L ANGLE PN 600-12045-12 ON RT WING LE, BETWEEN INBD & CTR LE IAW SRM 51-40-11 & AMM 20-21-00-910-801.

Part: TRACK — CRACKED (CARGO BAY) · airframe 24,487 hrs · 21,947 cycles

BAGGAGE BAY DOOR TRACK HAS A CHANNEL CRACKED AT FS 574, ABOVE FLOOR SILL. INSTALLED NEW CHANNEL 601R35050-25 AT FS 574 IAW SRM 51-42-06, SRM 51-40-06 & SRM 51-40-11.

Part: STRUT — LOW (NLG) · airframe 24,105 hrs · 21,578 cycles

UPON TAKEOFF LG RETRACT NOSE DOOR OPEN, LANDING GEAR DISAGREE, NOSE WHEEL STEERING INOPERATIVE. NOSE DOOR OPEN SOUND WAS HEARD FROM COCKPIT, LANDING GEAR MAINS WERE RETRACTED & NOSE GEAR UNSAFE. RAN QRH NOSE GEAR DISAGREEMENT SUCCESSFULLY GOT A 3 GEAR. COMPLIED WITH PA 05-018 REV K SCENARIO 1. SERVICED NOSE GEAR STRUT IAW AMM 12-12-32-601-803. PERFORMED FUNCTIONAL TEST OF THE LG EXTENSION & RETRACTION SYS IAW AMM 32-30-00-720-801. ALL CHECKED GOOD. ACFT OK FOR SERVICE.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 23,590 hrs · 21,065 cycles

DURING FLAP EXTENSION, FLAPS FAIL CAUTION MESSAGE DISPLAYED. FLAP POSITION AT FAILURE WAS 0. REPLACED LT FLAP NR 2 & 3 ACTUATORS, RT FLAP NR 1 ,2, 3 & 4 ACTUATORS. RIGGED FLAPS IAW 27-54-00-830-801. OPS CHECKED GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 23,527 hrs · 21,007 cycles

DURING APPROACH FLAPS FAIL CAUTION MESSAGE DURING INITIAL ATTEMPT TO EXTEND FLAPS. FAILED AT 0 DEG IN A LEVEL TURN AT 4000 MSL, TEMP -19 DEG C AIRSPEED 190KTS TIME IN FLIGHT 53MIN. PERFORMED TROUBLESHOOTING IAW FIM REV 4S IAW AD2009-06-12 PARAGRAPH H 6 I AMOC DATED JULY 22,2013 & PAAD27-052N. R & R LT NR 1 & NR 4 ACTUATORS IAW AMM 27-53-01 & 27-53-05. R & R LT NR 5 FLEX SHAFT IAW AMM 27-53-10. ALL OPERATIONAL & RIG CHECKED GOOD.

Part: SEAL — BROKEN (CABIN) · airframe 23,242 hrs · 20,739 cycles

EMK SEAL BROKEN. SECURED EMK SEAL, THIS CLEARS DM 19240 PLACARD REMOVED, OK FOR SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,118 hrs · 20,615 cycles

MIDDLE SECTION OF EMERGENCY LIGHTS AND OVERWING EXIT SIGN NOT ILLUMINATING. R & R INVERTER IAW AMM 33-51-07, OPS CHECKED GOOD. OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,686 hrs · 19,211 cycles

FIRST OFFICER'S EMERGENCY FLASHLIGHT INOPERABLE. REMOVED AND REPLACED FIRST OFFICER'S EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 25-60-01. OPS CHECKS GOOD.

Part: PACKING — DAMAGED (FUEL SYSTEM) · airframe 21,676 hrs · 19,202 cycles

ON FLIGHT 3774 DTW TO LAN ENGINE FLAMEOUT ON LANDING ROLLOUT. WHILE TRYING TO DEPLOY RIGHT THRUST REVERSER THE THRUST REVERSER DID NOT DEPLOY AND AT THE TIME NOTICED THE ENGINE HAD A FLAMEOUT. SECONDS LATER RIGHT ENGINE OIL PRESSURE SHOWED UP ON CD NR 1. PERFORMED OPERATIONAL CHECK OF RIGHT ENGINE IAW CRJ 200 AMM 71-00-00. ALL CHECKS GOOD. PERFORMED OPERATIONAL CHECK OF RIGHT THRUST REVERSER SYSTEM IAW CRJ200 AMM 78-30-00/. OPS CHECK GOOD. INSTALLED PERFORMED PACKING ON FUEL PUMP IAW AMM 73-20-00. INSTALLED RIGHT MAIN FUEL CONTROL IAW AMM 73-21-01. OPS CHECK & LEAK CHECKS GOOD. OK FOR SERVICE, NO LEAKS NOTED.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 21,386 hrs · 18,892 cycles

FIRST OFFICER'S & OBSERVERS LIFE VEST BAG TORN. REMOVED AND REPLACED FIRST OFFICER'S & OBSERVERS LIFE VEST IAW AMM 25-61-04.

Part: SKIN — DENTED (FUSELAGE) · airframe 21,232 hrs · 18,730 cycles

MAINTENANCE FOUND A DENT TO THE FUSELAGE SKIN AT FS 655 BETWEEN S-21L AND S-22L. THE DENT MEASURES 2.476" X 2.43" X 0.080" DEEP AND IS LOCATED WITHIN 1 INCH OF THE FRAME AT FS 654.5 AND S-22L. REPAIRED IAW EA CRJ253-00902 AND ASSOCIATED 8110-3.

Part: BATTERY — FAILED (FLASHLIGHT) · airframe 20,652 hrs · 18,147 cycles

FLIGHT ATTENDANTS EMERGENCY FLASH LIGHT BATTERY FAILS "RED" LED TEST. REMOVED AND REPLACED FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT BATTERY OP'S CHECK GOOD IAW AMM 25-61-00.

Part: SHUTOFF VALVE — MALFUNCTIONED (AC BAY) · airframe 20,041 hrs · 17,552 cycles

AIR RETURN FOR AUTO PRESS CONTROL NOT HOLDING PSI, SWITCHED TO MANUAL, & COULD BARELY CONTROL PRESSURE. MANUAL RATE FULL INCREASE & MANUAL ALT IN DOWN POSITION VARIED BETWEEN 200-600FPM. REMOVED AND REPLACED PRSOV IAW AMM 21-51-43. PERFORMED OPS CHECK OF LT PACK IAW AMM 21-51-00. OPS CHECK GOOD. PERFORMED OPS CHECK OF CABIN PRESSURE IAW 21-31-00. OPS CHECK GOOD. OK FOR SERVICE. VERIFIED PART EFFECTIVITY.

Part: UNKNOWN — MALFUNCTIONED (RT ENGINE) · airframe 19,795 hrs · 17,361 cycles

RIGHT ENGINE WOULD NOT REDUCE TO IDLE AT ALTITUDE (310) FUEL FLOW WITH THRUST LEVERS AT STOPS WERE 550 WHILE THE LEFT ENGINE WAS 350. ALL WAS NORMAL ON APPROACH AND LANDING. PERFORMED ENG ACEL/DECL CHECK ON RT ENGINE IAW AMM 71-00-00. COULD NOT DUPLICATE DISCREPANCY.

Part: UNKNOWN — MALFUNCTIONED (SPOILER) · airframe 19,622 hrs · 17,134 cycles

FLT SPLRS FAULT IN FLIGHT RIGHT SIDE DID NOT HAVE FULL TRAVEL. PERFORM OPERATIONAL TEST OF FLT SPLRS IAW AMM 27-64-00, OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 19,238 hrs · 16,742 cycles

FS 559.0 BULKHEAD RT WEB FAILS NDT WITH AN INDICATION NOTED AT RBL 9 WL 54.10 AND RBL 18 WL 59.10 APPROX .10 INCH IN LENGTH AND 78 PERCENT FSH. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 REV E, REO 601R-53-41-609 REV B, DEVIATION "E" BSC STANDARD REPAIRS 601R-53-0114, 601R-53-0108B, AND 601R-53-0109A.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,666 hrs · 16,192 cycles

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

Part: UPLOCK — DEFECTIVE (NLG) · airframe 18,518 hrs · 16,053 cycles

GEAR DISAGREE. REMOVED AND REPLACED NOSE GEAR LANDING UPLOCK ASSY IAW AMM 32-33-05. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 18,515 hrs · 16,049 cycles

AIR RETURN FOR GEAR DISAGREE. COMPLIED WITH PA 05-18A NO DEFECTS NOTED.

Part: SWITCH — DEFECTIVE (NLG STEERING) · airframe 18,515 hrs · 16,049 cycles

CREW REPORTED NOSE WHEEL STEERING MESSAGE IN FLIGHT ON APPROACH INTO ATL, DECLARED EMERGENCY A/C LANDED WITHOUT INCIDENT. VERFIED DISCREPANCY. REMOVED AND REPLACED STEERING ARMING SWITCH PER AMM 32-51-37, AND OPS CHECK FIM 32-51-37 GOOD, OK FOR SVC.

Part: SILL — CORRODED (BS 310-349) · corrosion level 2 · airframe 17,470 hrs · 16,053 cycles

THE PAX DOOR LOWER SILL ANGLE IS CORRODED BETWEEN FS 310.00 TO FS 349.00. REMOVED AND REPLACED PAX DOOR LOWER SILL ANGLE (P/N 601R31527-221) BETWEEN FS 310.00 TO FS 349.00 IAW CRJ200 SRM 51-42-06, 51-42-21, 51-42-11, 51-42-10, AND 51-25-16.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 17,470 hrs · 16,053 cycles

CARGO TIE DOWN CORRODED AT RBL 9 BETWEEN FS 559+80 TO 559.00+96. REMOVED CORRODED TIE DOWNS AND INSTALLED SERVICEABLE TIE DOWNS IAW CRJ SRM 51-41-02 AND 51-41-04 AND AMM 53-01-11-400-802.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,470 hrs · 16,053 cycles

LBL 36 SILL HAS CORROSION AROUND 5 NUT PLATES AND 1 FASTENER BETWEEN FS 559.00+80 TO 559.00+96. REMOVED MINOR CORROSION AND TREATED AFFECTED AREA IAW BSC EO 601R-53-19823.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,470 hrs · 16,053 cycles

LBL 27.00 FLOORBEAM TOP CAP IS CORRODED FROM FS 589.00 TO FS 621.00. BLENDED CORROSION ON FLOOR SUPPORT CAP AND FITTING, FOUND TO BE OUT OF SERVICEABLE LIMITS IAW CRJ-200 SRM 53-61-43 AND 53-00-00 FIG 101. REMOVED AND INSTALLED NEW SERVICEABLE FLOOR SUPPORT CAP (P/N 601R35031-263) AND FITTING (P/N 601R35289-3) IAW CRJ-200 SRM 51-42-06, 51-42-21, 51-40-11, 51-42-22, 51-42-36, AND BSC EO 601R-53-19821.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,470 hrs · 16,053 cycles

RBL 36 DOOR SILL IS CORRODED AROUND NUT PLATES & FASTENERS BETWEEN FS 559.00+96 AND 559.00+112. REMOVED MINOR CORROSION AND TREATED AFFECTED AREA IAW BSC EO 601R-53-19823.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,470 hrs · 16,053 cycles

LT SIDE SEAT RAIL STRUCTURE SECTION BELOW LT OVERWING EMERGENCY EXIT IS CORRODED. REMOVED AND REPLACED SEAT RAIL IAW CRJ AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,470 hrs · 16,053 cycles

RT SIDE SEAT RAIL STRUCTURE SECTION BELOW RT OVERWING EMERGENCY EXIT IS CORRODED. REMOVED AND REPLACED SEAT RAIL IAW CRJ AMM 53-01-11-400-802.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,470 hrs · 16,053 cycles

THE PAX DOOR LOWER SILL ANGLE IS CORRODED BETWEEN FS 310.00 TO FS 349.00. REMOVED AND REPLACED PAX DOOR LOWER SILL ANGLE (P/N 601R31527-221) BETWEEN FS 310.00 TO FS 349.00 IAW CRJ 200 SRM 51-42-06, 51-42-21, 51-42-11, 51-42-10, AND 51-25-16.

Part: WEB — CRACKED (FUSELAGE) · airframe 17,470 hrs · 16,053 cycles

FS 280.00 AFT "J" ANGLE AND WEB CRACKED AT SEVERAL LOCATIONS O/B OF RBL 9. REPAIRED FS 280.00 "J" ANGLE AND WEB IAW BOMBARDIER REO 601R-53-11-137 REV A, BOMBARDIER REO 601R-53-11-171 REV D AND BOMBARDIER SERVICES STANDARD REPAIRS 601R-53-0057B AND 601R-53-0097.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 17,470 hrs · 16,053 cycles

CARGO TIE DOWN CORRODED AT LBL 9 BETWEEN FS 559.0+80 TO 559.0+96. REMOVED CORRODED CARGO TIE DOWN AND INSTALLED A SERVICEABLE TIE DOWN IAW CRJ 200 AMM 53-01-11-400-802.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,470 hrs · 16,053 cycles

FS 202.75 BULKHEAD AT PARK BRAKE CABLE PASS THROUGH HOLE FAILS NDTM WITH AN INDICATION ON I/B SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT APPROXIMATELY .3 INCH LONG. COMPLIED WITH PERMANENT REPAIR OF FS 202.75 BULKHEAD AT PARKING BRAKE CABLE PASS THROUGH HOLE IAW BOMBARDIER REO 601R-53-11-563 AND BSC STANDARD REPAIR 601R-53-0101A.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 17,470 hrs · 16,053 cycles

CARGO TIE DOWNS CORRODED AT RBL 9 AND LBL 9 BETWEEN FS 559.00+112 AND 574.00. REMOVED CORRODED TIE DOWNS AND INSTALLED SERVICEABLE TIE DOWNS IAW CRJ SRM 51-41-02 AND 51-41-04.

Part: WARNING SYSTEM — ACTIVATED (THRUST REVERSER) · airframe 17,286 hrs · 14,911 cycles

RIGHT T/R UNLOCKED MESSAGE IN FLIGHT. INSPECTED AND FOUND RT THRUST REVERSER DEFERRED IAW MEL 78-30-01 AUTH NR 28649 TO BE DONE CORRECTLY IAW 78-30-00-040-802. OK FOR SERVICE.

Part: SWITCH — JAMMED (COCKPIT) · airframe 16,844 hrs · 14,474 cycles

CREW RECEIVED A STAB TRIM/MACH TRIM CAUTION MESSAGE ON CLIMBOUT AT 5000 FT AND WERE UNABLE TO RESET. RETURNED TO IND. UPON ARRIVAL MAINTENANCE VERIFIED DISCREPANCY AND FOUND F/O'S DISCONNECT SWITCH JAMMED WHICH WAS VERIFIED THROUGH MDC CODE 270 BIT 14. CLEANED SWITCH AND PERFORMED SYSTEM OPERATIONAL CHECKS IAW AMM 27-41-00.

Part: WINDSHIELD — FIRE (COCKPIT) · airframe 6,978 hrs · 5,978 cycles

CLIMBING THROUGH 17000 FT CAPTAIN SMELLED SMOKE. A FEW SECONDS LATER FLAMES AND SMOKE STARTED SHOOTING OUT OF THE LOWER LEFT WINDSHIELD. WINDSHIELD HEAT SELECTED TO OFF AT THIS TIME FLAMES AND SPARKS STOPPED. EMERGENCY DECLARED AND RETURNED AT AVL (DEPARTURE AIRFIELD). MAINTENANCE INSPECTED AIRCRAFT DETERMINED CAPTAINS WINDSHIELD HEAT FAILED. REMOVED AND REPLACED CAPTAINS FRONT WINDSHIELD

Part: ODOR — DETECTED (LAVATORY)

AMMONIA ODOR/SMOKE COMING FROM LAV REPORTED BY F/A. PERFORMED COMPLETE INSPECTION OF ENTIRE LAV SYSTEM FLUSHED LAV HOLDING TANK TWICE RESERVICED WITH BLUE JUICE. COMPLETE EXTENSIVE GROUND RUN A/C RELEASED FOR FLIGHT. (M)