N8936A

Part: LIGHT — INOPERATIVE · airframe 31,668 hrs · 29,940 cycles

RH MIDDLE WING EMERGENCY LIGHT INOP. R&R EXTERIOR EMERGENCY LIGHT 6 IAW CRJ 200 CMM 33-52-06. OPS CHECK IS GOOD. PN ON & OFF: 8GH002473-08

Part: BATTERY — INOPERATIVE · airframe 31,424 hrs · 29,632 cycles

"LEFT HAND OVERWING EXIT LOWER LIGHT APPEARS TO BE INOPERATIVE. FOUND ON PREFLIGHT. "INSPECTED AND VERIFIED LIGHT INOP DEFFERED CABIN EMERGENCY LIGHTS IAW MEL 33-51-1A ENTERED IN MMO2 MOC NOTIFIED 4488***REMOVED & REPLACED ALL EMERGENCY BATTERY PACKS IAW AMM 33-51-04 ALL CHECKS GOOD. THIS CLEARS MEL 33-51-1A "

Part: FRAME — CORRODED (BS559) · airframe 29,738 hrs · 27,531 cycles

FS 574 FRAME IS CORRODED ON AFT FACE BETWEEN STRINGER 27 & 26R. CONTINUED FROM JOB 8793631, OP 105 FS 574 FRAME IS CORRODED ON AFT FACE BETWEEN STRINGER 27 & 26R. CONTINUATION CARD: YES, OP: 128 REPAIRED FS 574 FRAME BETWEEN STRINGER 27 & 26R IAW RE601R-53-61-7428.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 29,738 hrs · 27,531 cycles

LT CARGO FLOOR SILL CORRODED AROUND FLOOR BOARD FASTENER HOLES BETWEEN FS 574.00 AND FS 621.00. CONTINUATION CARD: YES, OP: 125 REPLACED LT CARGO FLOOR SILL BETWEEN FS 574.00 TO FS 621.00 IAW CRJ 200 SRM 51-42-06, 51-42-13, 51-42-21 AND BOMBARDIER REO# 601R-53-61-15 74 REV-B, DATED 2012-04-15.

Part: FLOOR SUPPORT — CRACKED (BS 574-621) · airframe 29,738 hrs · 27,531 cycles

UPON INSTALLATION OF AFT CARGO FLOOR SILL, FOUND ANGLE P.N. 601R35011-15 TO BE CRACKED. REMOVED & DRILL & LOCATED NEW SERVICEABLE ANGLE IAW CRJ 200 SRM 51-40-11 & INSTALLED ANGLE IAW CRJ 200 SRM 51-42-21.

Part: SUPPORT — CRACKED (BS 718) · airframe 29,738 hrs · 27,531 cycles

RT SYSTEM #2 HYDRAULIC FILTER MANIFOLD SUPPORT IN AEB IS CRACKED IN LOWER AFT CORNER. REMOVED & REPLACED RT SYSTEM #2 HYDRAULIC FILTER MANIFOLD SUPPORT IN AEB. REMOVED & INSTALLED RETURN & PRESSURE MANIFOLD ASSEMBLY IAW CRJ 200 AMM 29-11-44-000/400-801 & SRM 51-42-06. BLEED & OPERATIONS CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 29,738 hrs · 27,531 cycles

CARGO FLOOR SEAT RAIL CORRODED AT RBL 27, BETWEEN FS 559.00+80 AND FS559.00+96. REMOVED & REPLACED SEAT RAIL AT RBL 27 AT FS 559.00+80 TO FS 559.00+96 IAW CRJ 200 AMM 53-01-11-000-802/400-802. REPLACED FITTING PN CDSP1900-15 IAW AMM 25-41-01-400-806.

Part: PLATE — BENT (BS 584) · airframe 29,738 hrs · 27,531 cycles

FWD & AFT DOOR LANDINGS ON GROUND AIR DOOR BENT. REMOVED & REPLACED AFT DOOR LANDING IAW CRJ 200 SRM 51-40-11, 51-42-0651-25-01 & 51-23-00 & REPAIRED FWD LANDING IAW REO 601R-53-61-6078 REV, DATED 2018-04-06.

Part: FLOOR SUPPORT — CORRODED (BS 574-605) · airframe 29,738 hrs · 27,531 cycles

CARGO LBL 27 FLOOR BEAM CAP HAS CORROSION AROUND NUTPLATE HOLES FROM FS 574.00 TO FS 605.00. REMOVED AND REPLACED FLOORBEAM CAP FROM FS 574 - FS 621 LBL 27 IAW CRJ200 SRM 51-42-06 AND SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 29,738 hrs · 27,531 cycles

CARGO FLOOR SEAT RAIL CORRODED AT LBL 27, BETWEEN FS 559.00+80 AND FS559.00+96. REMOVED AND REPLACED SEAT TRACK AT LBL 27 FS 559+80, FS 559+96 IAW CRJ 200 AMM 53-01-11-000/400-802. REMOVED BROKEN FITTING RETAINER IAW CRJ 200 AMM 20-21-00-910-801.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 29,738 hrs · 27,531 cycles

CARGO FLOOR SEAT RAIL CORRODED AT RBL 9.0, BETWEEN FS 559.00+112 AND FS 574.00. REMOVED TAPE, REMOVED AND REPLACED CARGO FLOOR SEAT RAIL AT RBL 9.0, BETWEEN FS 559.00+112 AND FS 574.00 IAW CRJ 200 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 29,738 hrs · 27,531 cycles

CARGO FLOOR SEAT RAIL CORRODED AT LBL 9.0, BETWEEN FS 559.00+112 AND FS 574.00. REMOVED TAPE, REMOVED AND REPLACED CARGO FLOOR SEAT RAIL AT LBL 9.0, BETWEEN FS 559.00+112 AND FS 574 IAW CRJ 200 SRM 51-41-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,103 hrs · 26,850 cycles

RIGHT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 26,618 hrs · 24,208 cycles

LAV SMOKE DETECTOR WON'T TEST. R&R LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECK GOOD.

Part: ANGLE — CRACKED (RT WING) · airframe 26,538 hrs · 24,118 cycles

RT WING L/E SUPPORT STRUCTURE UPPER ANGLE AT TRANSITION DUCT SUPPORT ASSY CRACKED, WS149.0. REMOVED AND REPLACED RT WING LE SUPPORT STRUCTURE UPPER ANGLE AT TRANSITION DUCT IAW SRM 51-41-02.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 26,538 hrs · 24,118 cycles

RT WING FUEL ACCESS PANEL LAND 640BB HAS FRETTING CORROSION. REPAIRED RIGHT ACCESS PANEL LAND 640BB IAW REO 601R-57-21-030.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 26,538 hrs · 24,118 cycles

RT INBD FLAP VANE LE SKIN CHAFED AT OTBD BUMP STOP CONTACT POINT. BLENDED CHAFE FOUND TO BE OUT OF LIMITS, REMOVED & REPLACED LE IAW REO601R-57-52-004 & SRM 51-40-11 PG 1413, 51-42-10 PG 10&15.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 26,538 hrs · 24,118 cycles

LT WING FUEL ACCESS PANEL LAND 510AB HAS FRETTING CORROSION. REPAIRED LEFT WING ACCESS PANEL LAND 510AB IAW REO 601R-57-21-030.

Part: RIVET — CHAFED (BULKHEAD) · airframe 26,538 hrs · 24,118 cycles

APB SKIN AND RIVET HEADS CHAFED FROM LINER FASTENERS 14 INCHES ABOVE FLOOR LBL36 TO RBL35.5. BLENDED CHAFES AND RESTORED FINISH. REMOVED AND REPLACED DAMAGED RIVETS IAW REO GOIR-53-61-2155.

Part: ATTACH BRACKET — CRACKED (TAIL PIPE) · airframe 26,538 hrs · 24,118 cycles

LT ENGINE TAIL PIPE FAIRING 436AL FIRE DETECTION LOOP MOUNT BRACKET ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED FIRE DETECTION COOP COVER ATTACH BRACKET IAW CMM 20-41-00.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 26,538 hrs · 24,118 cycles

PASSENGER ENTRY DOOR HOIST MOTOR ATTACH ANGLE IS CRACKED AT LOWER RADIUS. REMOVED AND REPLACED PASSENGER ENTRY DOOR ATTACH ANGLE IAW SRM 51-42-21 & 51-42-06.

Part: ATTACH BRACKET — CRACKED (TAIL PIPE) · airframe 26,538 hrs · 24,118 cycles

LT ENGINE TAIL PIPE FAIRING 436AL FIRE DETECTION LOOP MOUNT BRACKET ATTACH BRACKET IS CRACKED. REMOVED AND REPLACED FIRE DETECTION COOP COVER ATTACH BRACKET IAW CMM 20-41-00.

Part: PANEL — DAMAGED (RT WING) · airframe 26,538 hrs · 24,118 cycles

RT LE PANEL 630BL HAS ELONGATED AND OVER COUNTERSUNK ATTACH FASTENERS HOLES. REMOVED AND REPLACED WITH NEW PANEL 630BL IAW SRM 51-40-11.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 26,538 hrs · 24,118 cycles

REPAIR DOUBLER ON APB RBL18.25 CHAFED FROM PANEL FASTENERS 36INCHES ABOVE FLOOR. REMOVED DAMAGED REPAIR DOUBLER FABRICATED AND INSTALLED NEW REPAIR DOUBLER ON APB, AT RBL 18.25, 36INCHES ABOVE FLOOR IAW REO 601R-53-61-1285.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 26,538 hrs · 24,118 cycles

RT MLG WHEEL WELL, DRAG ANGLE ADJACENT TO BATT RIB CRACKED. REMOVED AND REPLACED DRAG ANGLE IAW SRM 51-42-21.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 26,538 hrs · 24,118 cycles

REPAIR DOUBLER ON APB RBL35.5 CHAFED FROM PANEL FASTENERS 36 INCHES ABOVE FLOOR. REMOVED DAMAGED REPAIR DOUBLER. FABRICATED AND INSTALLED NEW REPAIR DOUBLER ON APB, REL35.5 36 INCHES ABOVE FLOOR IAW REO 601R-53-61-1285.

Part: SKIN — CORRODED (LT WING) · airframe 26,538 hrs · 24,118 cycles

LT WING FUEL ACCESS PANEL LAND 540BB HAS FRETTING CORROSION. REPAIRED LEFT WING ACCESS PANEL LAND 540BB IAW REO 601R-57-21-030.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 26,538 hrs · 24,118 cycles

REPAIR DOUBLER ON APB RBL27.75 CHAFED FROM PANEL FASTENERS 36 INCHES ABOVE FLOOR. REMOVED DAMAGED REPAIR DOUBLER. FABRICATED AND INSTALLED NEW REPAIR DOUBLER ON APB AT RBL 27.75, 36INCHES ABOVE FLOOR IAW REO 601R-53-61-1285.

Part: PLATE — CRACKED (PYLON) · airframe 26,538 hrs · 24,118 cycles

PYLON PANEL 412BB DIVIDER PLATES ARE BOTH CRACKED. REMOVE AND REPLACE 2 EACH DIVIDER PLATES ON PANEL 412BB IAW SRM 51-42-06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,687 hrs · 23,154 cycles

RT EMERGENCY LIGHT FOUND TO BE INOP DURING ROUTINE 200 JOB CARD INSPECTION OF EMERGENCY LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHT BULB IAW AMM 33-51-21-04 P/N OFF/ON WL-1317.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,669 hrs · 23,134 cycles

FLOOR EMERGENCY LIGHTS ARE INOPERATIVE FROM ROWS 6 THRU 8. REPLACED THE INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,411 hrs · 22,890 cycles

SEAT 8D EMERGENCY LIGHT OUT. R & R THE EMERGENCY LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD, OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,303 hrs · 22,739 cycles

FORWARD EMERGENCY LIGHTS NEAR MAIN AND SERVICE DOORS ARE INOPERATIVE. R & R THE BULBS AND OPS CHECKED IAW AMM 38-51-10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,043 hrs · 22,458 cycles

FLOOR EMERGENCY LIGHT STRIP IN THE MIDDLE SECTION INOPERATIVE. R & R THE EMERGENCY LIGHT STRIP IAW AMM 33-51-01, OPS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 24,789 hrs · 22,196 cycles

ROW 1 & 2 EMERGENCY LIGHTS HAS A WHITE WIRE SHOWING AND LIGHT STRIP NOT BONDED TO THE FLOOR. FOUND ROW 1 & 2 EMERGENCY FLOOR LIGHT SPLICE BROKEN. INSTALLED A NEW SPLICE IAW ESPM 20-16-00. REINSTALLED THE EMERGENCY LIGHTS IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 24,665 hrs · 22,064 cycles

RT EMERGENCY OVERWING EXIT IDENTIFICATION INOP. REMOVED AND REPLACED RT EMERGENCY EXIT IDENTIFIER P/N 6020-5 IAW AMM 33-51-10. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 24,164 hrs · 21,563 cycles

FO'S EMERGENCY FLASHLIGHT DISCHARGED. REMOVED & REPLACED THE BATTERY PACK IAW AMM 25-61-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 23,707 hrs · 21,111 cycles

CAPTAINS FLASHLIGHT NOT BLINKING . REMOVED AND REPLACED CAPT'S EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-61-04. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,484 hrs · 20,876 cycles

LOWER EMERGENCY LIGHT AT LT EMERGENCY EXIT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-10. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 23,484 hrs · 20,876 cycles

RIGHT CABIN SEAT TRACK RBL 9 HAS CORROSION AND GOUGES IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-41-49 AND AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 23,484 hrs · 20,876 cycles

RIGHT CABIN SEAT TRACK RBL 9 HAS CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 23,484 hrs · 20,876 cycles

RIGHT CABIN SEAT TRACK RBL 9 HAS CORROSION 8 INCHES AND 39 FROM FWD END. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 23,484 hrs · 20,876 cycles

AFT PRESSURE BULKHEAD TO SKIN ATTACH CLIP CRACKED BETWEEN STA 621 AND STA 625 AT STR 15L. R & R UNSERVICEABLE ATTACH CLIP WITH A SERVICEABLE ATTACH CLIP ON AFT PRESSURE BULKHEAD TO SKIN BETWEEN STA 621 & STA 625 AT STR 15L IAW REO 601R-53-61-5265 & SRM 51-42-21.

Part: RISER — CRACKED (DOOR STEP) · airframe 23,484 hrs · 20,876 cycles

PAX DOOR STAIR RISER EDGE MEMBER BELOW UPPER FOLDING STEP CRACKED AT FWD AND AFT ENDS OF RADIUS. AFT END FOUND NOT TO BE CRACKED BY NDT TESTING IAW NDTM 51-20-06 AND REPAIRED FORWARD END IAW REO 601R-52-11-279 AAR SM-39

Part: ATTACH ANGLE — CRACKED (BS 621-625) · airframe 23,484 hrs · 20,876 cycles

AFT PRESSURE BULKHEAD TO SKIN ATTACH ANGLE CRACKED BETWEEN BS 621 - 625, STRINGER 15L. REMOVED & REPLACED THE ATTACH ANGLE IAW REO 601R-53-61-5265 & SRM 51-42-21.

Part: ATTACH ANGLE — CRACKED (BS 625) · airframe 23,484 hrs · 20,876 cycles

AFT PRESSURE BULKHEAD AFT FACE LT SIDE IN LINE WITH STRINGER 14L, BS 625.3 TO INTERCOSTAL ATTACH ANGLE CRACKED. REMOVED & REPLACED THE ATTACH ANGLE IAW SRM 51-42-06, & 51-42-21.

Part: ATTACH ANGLE — CRACKED (BS 621-625) · airframe 23,484 hrs · 20,876 cycles

AFT PRESSURE BULKHEAD TO SKIN ATTACH ANGLE CRACKED BETWEEN BS 621 - 625 AT STRINGER 13L. REMOVED & REPLACED THE ATTACH ANGLE IAW REO 601R-53-61-5265 & SRM 51-42-21.

Part: SUPPORT ANGLE — CRACKED (GROUND SPOILER) · airframe 23,484 hrs · 20,876 cycles

RIGHT WING TE INBD GROUND SPOILER SUPPORT ANGLE BENT AND CRACKED AT FREE FLANGE. WS 75.0. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-42-06.

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 23,484 hrs · 20,876 cycles

BS 621 AFT PRESSURE BULKHEAD FWD FACE DAMAGED AT RBL 17 AND WL 102. CUT OUT DAMAGE AND REPAIRED IAW REO 601R-53-61-1285.

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 23,484 hrs · 20,876 cycles

BS 621 AFT PRESSURE BULKHEAD FWD FACE DAMAGED AT RBL 26 AND WL 102. CUT OUT DAMAGE AND REPAIRED THE BULKHEAD IAW REO 601R-53-61-1285.

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 23,484 hrs · 20,876 cycles

BS 621 AFT PRESSURE BULKHEAD FWD FACE DAMAGED AT RBL 35 AND WL 102. CUT OUT DAMAGE AND REPAIRED THE BULKHEAD IAW REO 601R-53-61-1285.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 23,484 hrs · 20,876 cycles

RIGHT WINDSHIELD SIDE POST, LWR AFT FITTING CRACKED. REMOVED AND REPLACED THE POST, LWR AFT FITTING IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED · airframe 23,484 hrs · 20,876 cycles

LEFT SIDEWALL SEAT TRACK, HAS AREAS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11 STEP 2A 1-9.

Part: INTERCOSTAL — CHAFED (BS 559) · airframe 23,484 hrs · 20,876 cycles

INTERCOSTAL STRINGER 5L BS 559+94 IS CHAFED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 23,484 hrs · 20,876 cycles

RIGHT SIDEWALL SEAT TRACK HAS AREAS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 23,484 hrs · 20,876 cycles

RIGHT SIDEWALL SEAT TRACK, HAS AREAS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 23,484 hrs · 20,876 cycles

RIGHT SIDEWALL SEAT TRACK, HAS AREAS OF CORROSION. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 23,484 hrs · 20,876 cycles

LEFT SIDEWALL SEAT TRACK, HAS AREAS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11 STEP 2 A 1-9.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 23,484 hrs · 20,876 cycles

RIGHT SIDEWALL SEAT TRACK, HAS AREAS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 23,484 hrs · 20,876 cycles

RIGHT SIDEWALL SEAT TRACK, HAS AREAS OF CORROSION. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: BRACKET — CRACKED · airframe 23,484 hrs · 20,876 cycles

BRACKET FOR ACFT POWER RECEPTACLE IS CRACKED. REMOVED AND REPLACED POWER RECEPTACLE BRACKET IAW SRM 51-42-21, SRM 51-42-06, AND SRM 51-42-10.

Part: ANGLE — CRACKED (BS 280) · airframe 23,484 hrs · 20,876 cycles

INBOARD ANGLE ON STRINGER 3L BS 280 IS CRACKED. REMOVED & REPLACED THE ANGLE IAW SRM 51-24-36, 51-42-06, AND 51-42-21.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 23,484 hrs · 20,876 cycles

RIGHT WING L/E WS 139.54 ATTACH ANGLE CRACKED ON LWR EDGE. REMOVED AND REPLACED IAW SRM 51-40-11.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 23,484 hrs · 20,876 cycles

LEFT WING LE ATTACH BRACKET AT WS 149.5 CRACKED IN RADIUS. REMOVED AND REPLACED IAW SRM 51-41-02.

Part: OXYGEN BOTTLE — LOW PRESSURE (CABIN) · airframe 23,433 hrs · 20,823 cycles

MEDICAL O2 LOW, TANK IN FRONT OF CLOSET. R & R PORTABLE O2 BOTTLE IAW AMM 35-30-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,566 hrs · 19,944 cycles

ROW 1 FLOOR EMER LIGHT STRIP INOPERATIVE. R & R EMER FLOOR FLEXIBLE LAMP. OPERATIONS CHECKED PASSED IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 22,535 hrs · 19,919 cycles

GALLEY EMER SIGN HAS LIGHT BULB BURNED OUT. REPLACED BULB, OPERATIONS CHECKED GOOD IAW AMM 33-51-09.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 22,535 hrs · 19,919 cycles

CAPTAINS LIFE VEST PLASTIC WRAP HAS A COUPLE OF HOLES. REPLACED CAPTAINS LIFE VEST IAW AMM 25-61-03.

Part: LIGHT — BROKEN (CABIN) · airframe 22,240 hrs · 19,616 cycles

EMERGENCY LIGHT STRIP BROKEN IN SEVERAL LOCATIONS. REPAIRED EMER LIGHT FLOOR STRIP IAW AMM 33-51-01. REFER TO WORK ORDER 54670-2000-0050 FOR INSTALLATION & OPERATIONS CHECKED. CRIMPER 90 CAL DUE 6/11/15.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 22,240 hrs · 19,616 cycles

DURING CLIMB OUT, AFTER SELECTING GEAR HANDLE, GEAR DISAGREE WARNING. NOSE WHEEL INDICATED DOWN WHILE BOTH MAIN GEAR INDICATED UP. REPLACED NOSE DOOR SELECTOR VLV.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 22,237 hrs · 19,612 cycles

RIGHT WING PLANK CORRODED AROUND LANDING FOR FUEL ACCESS PANEL 650FB. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 22,237 hrs · 19,612 cycles

RIGHT WING PLANK CORROSION AROUND LANDING FOR FUEL ACCESS PANEL 650GB. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 22,237 hrs · 19,612 cycles

LEFT WING PLANK CORRODED AROUND LANDING FOR FUEL ACCESS PANEL 540BB. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 22,237 hrs · 19,612 cycles

LEFT WING PLANK CORRODED AROUND LANDING FOR FUEL ACCESS PANEL 510AB. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 22,237 hrs · 19,612 cycles

RIGHT WING PLANK CORRODED AROUND LANDING FOR FUEL ACCESS PANEL 650DB. REPAIRED IAW REO 601R-57-21-030.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 22,237 hrs · 19,612 cycles

AFT SIDE OF FS 621 CTR STIFFENER CHAFED 15 INCHES FROM TOP OF STIFFENER MEASURING 0.3" X 0.024" DEEP. REPAIRED IAW REO 601R-53-61-1523.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,237 hrs · 19,612 cycles

FORWARD PRESS BULKHEAD CRACKED AT BRAKE CABLE PASS THROUGH HOLE. REPAIRED IAW REO 601R-53-11-563.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 22,237 hrs · 19,612 cycles

CORROSION ON THE PANEL LANDING FOR PANELS 540AT & 540BT ON THE LT UPPER WING SKIN AT WS 74.15 & WS 96.34. REPAIRED IAW CRJ257-02706.

Part: HAND RAIL — LACK OF LUBE (PAX DOOR) · airframe 22,166 hrs · 19,543 cycles

FLIGHT ATTENDANT REPORTED PAX DOOR DIFFICULT TO OPERATE, SQUEAKS A LOT, HARD TO CLOSE THE HANDLE. PAX DOOR OPENS & CLOSES SMOOTHLY, INDICATION NORMAL. HANDRAIL PIVOTS SQUEAKY. CLEANED & LUBED. OPERATIONS CHECKED GOOD IAW AMM 52-11-00. DOOR MANUAL CLOSING & WITH POWER ASSIST CHECKS GOOD. ALL INDICATORS ALIGN CLOSED & EICAS INDICATION GOOD.

Part: CONTAINER — TORN (LIFE VEST) · airframe 21,361 hrs · 18,757 cycles

F/O'S LIFE VEST BAG TORN. R & R F/O'S LIFE VEST IAW AMM 25-61-03.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,304 hrs · 18,697 cycles

GEAR DISAGREE ON RETRACT HYD 3 AT 100%, 20 DEG C. DEFERRED, CLEARED GEAR DISAGREE DM 20301 IAW PA 05-018 REV K, SCENARIO NR 1. OPERATIONS CHECK OF LANDING GEAR EXTENSION & RETRACTION GOOD, THIS CLEARS DM 20301.

Part: SEAL — BROKEN (PBE) · airframe 20,817 hrs · 18,198 cycles

COCKPIT PBE PACKAGE SEAL BROKEN. R & R COCKPIT PBE IAW AMM 35-30-00, CHECKED GOOD AT THIS TIME.

Part: LUG — CORRODED (LT MLG) · corrosion level 2 · airframe 20,744 hrs · 18,126 cycles

LEFT MLG SIDE STAY INBD LUG HAS MINOR SURFACE CORROSION IN THE AREA BETWEEN THE FORWARD AND AFT BUSHINGS MEASURING 0.0005" DEEP. REPAIRED IAW SRM 51-21-06.

Part: COALESCER BAG — ODOR (CABIN) · airframe 20,531 hrs · 17,927 cycles

VERY STRONG JET FUEL ODOR IN CABIN AFTER STARTING APU. REPLACED LT COALESCER BAG IAW AMM 21-51-13, ALL CHECKED GOOD. ODOR NO LONGER NOTICEABLE. ACFT OK FOR SERVICE.

Part: WARNING HORN — NO TEST (APU FIRE) · airframe 20,509 hrs · 17,903 cycles

APU FIRE WARNING HORN WILL NOT SOUND DURING TEST.

Part: TRIM SWITCH — OBSTRUCTED (COCKPIT) · airframe 20,326 hrs · 18,921 cycles

STAB TRIM CH1 KEEPS DISCONNECTING DURING CLIMB OUT AND RANDOMLY THROUGHOUT FLIGHT. RECONNECTS AND THEN DISCONNECTS. UPON INSPECTION OF PILOTS PITCH TRIM SWITCH, FOUND DEBRIS BETWEEN CONTACT POINTS; CLEANED DEBRIS IAW AMM 27-41-05. PERFORMED OPS CHECK OF HSTS IAW AMM 27-40-00. OPS CHECK GOOD. OK FOR SVC AT THIS TIME.

Part: SKIN — DENTED (FUSELAGE) · airframe 19,448 hrs · 16,892 cycles

MAINTENANCE FOUND TWO DENT TO THE FUSELAGE SKIN BETWEEN FS 349 AND FS 364 AND S-23R AND S-24R, MEASURING 3" X 2.4" X 0.044" DEEP AND 1.10" X 1.0" X 0.007" DEEP. REPAIRED IAW EA CRJ253-01126 AS APPROVED BY ASSOCIATED 8110-3.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,448 hrs · 16,892 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,956 hrs · 16,383 cycles

NR 3 EMERGENCY LIGHT BATTERY INOPERATIVE, WILL NOT HOLD CHARGE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY, OPS CHECKED GOOD IAW AMM 33-51-04.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,868 hrs · 16,298 cycles

CRACK FOUND ABOVE AFT CARGO DOOR TRACK ON AFT PRESSURE BULKHEAD MEASURING 1/4 INCH LENGTH. REPAIRED IAW BOMBARDIER REO 601R-53-61-1541.

Part: PLACARD — TORN (COCKPIT) · airframe 18,811 hrs · 16,241 cycles

FLIGHT SAFETY WARNING PLACARD RIPPED OFF FIRST OFFICERS SIDE. REPLACED PLACARD IAW PA11030.

Part: WINDOW — CRACKED (COCKPIT) · airframe 18,271 hrs · 15,721 cycles

RIGHT SIDE WINDOW SHATTERED IN FLT. REPLACED RT WINDOW, REMOVED AND REPLACED RT SIDE WINDOW HEAT CONTROLLER IAW CRJ200AMM 30-41-01. REQUIRES OPERATIONAL TEST. REFER TO AML 2241815 DISCR NR 2.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,096 hrs · 15,545 cycles

FOUND THE FUSELAGE SKIN TO BE DENTED BETWEEN FS 625 AND FS 640 AND BETWEEN S-20L AND S-21L. THE DENT WAS MEASURED TO BE 9.375 X 5.25 X 0.255 DEEP. REPAIRED IAW EA CRJ253-00427B AS AUTHORIZED BY 8110-3 DATED 3/23/12.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 17,882 hrs · 15,326 cycles

FS 621 BULKHEAD AFT VERTICAL STIFFENER AT BL 0 CHAFED. REPAIRED IAW BOMBARDIER REO 601R-53-61-1523.

Part: STIFFENER — CHAFED (BS 621 BULKHEAD) · airframe 17,882 hrs · 15,326 cycles

FS 621 BULKHEAD AFT VERTICAL STIFFENER CHAFED AT BL0. REPAIRED IAW REO 601R-53-61-1523.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,724 hrs · 15,223 cycles

F/A FLASHLIGHT INOP. REMOVED AND REPLACED FA FLASHLIGHT IAW CRJ200 AMM 25-60-11, OPS CHECK GOOD. OK FOR SVC.

Part: RESERVOIR — DEFECTIVE (HYDRAULIC SYS) · airframe 17,604 hrs · 15,058 cycles

AIR RETURN, GEAR DISAGREE UP ONCE WE SELECTED GEAR UP AFTER TAKEOFF (ABOUT 20 SC.), ALSO HAD HYD 3 LO PRESS CAUTION MSG ( NOTICED THAT THE HYD 3 PRESSURE WAS AT 1100 PSI). COMPLIED WITH PA05-018B GAR DISAGREE EVENT PROCEDURES. R&R NR 3 HYD SYS FLUID RESERVOIR IAW AMM 29-12-30. LEAK CHECK GOOD. LANDING GEAR RETRACTION AND EXTENSION SYS FC NORMAL IAW AMM 32-30-00. PART EFFECTIVITY VERIFIED.

Part: UNKNOWN — SMOKE (CABIN) · airframe 17,107 hrs · 14,626 cycles

GATE RETURN: F/A REPORTED SMOKE IN CABIN WITH ELECTRICAL SMELL. MAINTENANCE C/W WORK SCOPE FOR SMOKE IN CABIN. NO DEFECTS FOUND. PERFORMED HIGH POWER ENG RUN W/PACKS ON; PERFORMED APU RUN W/PACKS ON; NO SMOKE IN CABIN. PERFORMED OPC OF PACKS IAW AMM 21-51-00. OPC GOOD. REF TL-218787-2011.

Part: FUEL CONTROL — OUT OF RIG (RT ENGINE) · airframe 16,919 hrs · 14,406 cycles

CREW STATES THAT WHEN THE RIGHT TR WAS STOWED THE ENG FLAMED OUT. AFTER LANDING IN DTW FROM CWA RE-RIGGED RIGHT ENG. FUEL CONTROL IAW AMM 73-20-00 & RERIGGED RIGHT ENG THROTTLE GEARBOX IAW AMM 72-60-00 ALL SYSTEMS OP'S CHECKED GOOD. AWAITING RESULTS OF DFDR DOWNLOAD.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 16,652 hrs · 14,166 cycles

ON APPROACH INTO INDY CREW GOT GEAR DISAGREE RHT MLG WOULD NOT GO DOWN & LOCK ON FIRST ATTEMPT CREW CYCLED GEAR HANDLE & ALL 3 GEAR INDICATED DOWN & LOCKED. A/C LANDED WITHOUT FURTHER INCIDENT. DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL 32-30-01 DM-44803.

Part: O-RING — TORN (APU) · airframe 16,330 hrs · 13,861 cycles

FUEL FUMES IN COCKPIT/CABIN ON APU BLEED VERIFIED THAT THE APU FUEL CONTROL FILTER BOWL O-RING WAS TORN. REPLACED IAW AMM 49-10-00. LEAK CHECK GOOD. COMPLIED WITH WORKSCOPE IAW CHECKLIST PROVIDED.

Part: SCAVENGE PUMP — SHEARED (OIL SYSTEM) · airframe 15,659 hrs · 13,234 cycles

EN ROUTE TO KSYR AT FL230 THE LEFT ENGINE OIL PRESSURE WARNING ILLUMINATED. THE ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT WAS VECTORED INTO KSYR AND AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE. CFR INSPECTED THE AIRCRAFT AND FOUND NO DAMAGE OR FIRE. MAINTENANCE TROUBLESHOT AND FOUND THE LUBE AND SCAVENGE PUMP SHAFT SHEARED. MAINTENANCE IS STILL IN WORK.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 12,838 hrs · 10,550 cycles

ON APPROACH INTO KMEM, THE FLIGHT CREW HEARD A LOUD POPPING NOISE BEHIND THE CAPTAIN'S SEAT, FOLLOWED BY A BURNING SMELL. NO SMOKE WAS NOTED AT THAT TIME SO A NORMAL APPROACH AND LANDING WAS MADE. ON LANDING ROLLOUT THE CREW DETECTED WHAT APPEARED TO BE SMOKE BEHIND THE CAPTAIN'S SEAT. SINCE IT APPEARED TO BE DISSIPATING, THE CAPTAIN ELECTED TO TAXI TO THE GATE AND DEPLANE THE PASSENGERS NORMALLY. NO EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED THE COCKPIT ELECTRICAL SYSTEM IN ACCORDANCE WITH AMM 24-20-00. GROUND RUNS AND INSPECTION OF THE ECS BLEED SYSTEM WERE NORMAL AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS SCHEDULED FOR A FUNCTIONAL CHECK FLIGHT. THE FCF WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 4,041 hrs · 3,302 cycles

FLAP FAIL AT 20 DEGREES ON APPROACH. PERFORMED QRH. LANDING UNEVENTFUL. PERFORMED AD98-20-01, MONITOR FLAPS FOR 72 CALENDAR HOURS.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 3,698 hrs · 2,879 cycles

FLAPS FAILED ON APPROACH, FOLLOWED QRH WITH UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR MONITOR PER AD 98-20-01.

Part: CONTROL SYSTEM — MALFUNCTIONED (LE FLAPS) · airframe 3,459 hrs · 2,694 cycles

FLAPS FAILED AT 20 DEG ON APPROACH. PERFORMED AD 98-20-01, UNDER 72 HOURS MONITORING FOR FLAPS FAIL MESSAGES.

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS)

FLAPS FAILED AFTER LANDING WHEN SELECTED UP DURING TAXI. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)