N8928A

Part: BATTERY — INOPERATIVE · airframe 31,223 hrs · 29,433 cycles

"ORANGE LUMINESCENT FROM ROW 1 DETACHED "DEFERED CABIN EMERGENCY LIGHTS IAW MEL 33-51-1A. PLACARD INSTALLED ENTERED INTO MMO2 PER MOC 99758\\\\\\\\\ R&R BATTERY PACK IAW CRJ-200 AMM 33-51-04, OPS TEST GOOD MMO2 UPDATED PLACARD REMOVED "

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 29,093 hrs · 26,904 cycles

FORWARD MOST EMERGENCY FLOOR TRACK LIGHT INOP R&R FLOOR TRACK LIGHT IAW AMM 33-51-01. OPS CHECK GOOD.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 27,963 hrs · 25,698 cycles

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

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,963 hrs · 25,698 cycles

PAX DOOR VENT OPENING LOWER INTERCOSTAL HAS CORROSION SPOTS ON BOTH SIDES, VIEWED WITH THE DOOR OPEN. REMOVED AND REPLACED CORRODED INTERCOSTAL IAW SRM 51-42-06. OPS CHECKS OF PAX DOOR WARNING SYSTEM ACCOMPLISHED ON W/O 1017080 - 20000-0105. S/N 7058709.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 27,963 hrs · 25,698 cycles

CARGO DOOR FWD UPPER BACK UP FITTING IS CRACKED. REMOVED AND REPLACED FWD UPPER BACK FITTING IAW SRM 51-42-10.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

REPAIR STRIP UNDER THE RT FLOOR SILL HAS CORROSION SPOTS AROUND NUTPLATES, BETWEEN FS 589 THRU FS 605, IN THE CARGO BAY. REMOVED AND REPLACED RT FLOORSILL 559+15-621 IAW SRM AND EA CRJ-253-08678. OPS CHECK GOOD IAW AMM 38-21-23 AMM 38-21-24 AND AMM 38-21-29.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 27,963 hrs · 25,698 cycles

LT WING L/E PNL 520JL OTBD RIB ATTACH ANGLE AT TRANSITION DUCT SUPPORT ASSY CRACKED IN LWR RADIUS. REMOVED AND INSTALLED NEW ATTACH ANGLE IAW SRM 51-41-02 AND 57-41-12.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 27,963 hrs · 25,698 cycles

LT MLG WHEEL WELL, BRAKE HYD BYPASS TRANSDUCER BRACKET CRACKED. REMOVED AND REPLACED LT MLG BRAKE HYD BY PASS TRANSFER BRKT IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

RBL9 SEAT TRACK HAS CORROSION BETWEEN FS409.0 TO FS409.0.0+128. REMOVED AND REPLACED SEAT TRACK AT RBL9 FROM FS409 TO FS 409+128 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

SEAT TRACK ON RBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. CORROSION ALL REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-61-44. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

SEAT TRACK ON LBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574, THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK AT LBL9 FS 559+112 AND FS 574 IAW AMM 53-01-11.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

ANGLE BRACKET ON TOP OF THE LH FLOOR SILL AT FS 574 HAS A HOLE WORN THROUGH IT, IN THE CARGO BAY. REMOVED AND REPLACE WITH NEW ANGLE BRACKET IAW SRM 51-13-01 & SRM 51-42-21.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

FLT DECK FLOOR SUPPORT ANGLE AT FS 280.0 CRACKED IN RADIUS AT LBL4. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-42-06 51-42-21 AND AMM 20-21-00.

Part: STRAP — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

FLOOR STRAP AT FS 559 HAS CORROSION BETWEEN LBL 27 AND THE LT FLOOR SILL, IN THE CABIN. REMOVED AND REPLACED FLOOR STRAP AT FS 559 LBL 27. IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

RT SIDE SEAT RAIL STICK 6 HAS MULTIPLE SPOTS OF CORROSION AND GOUGES. REMOVED AND REPLACED SIDE SEAT RAIL RT 6 IAW AMM 53-01-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

INTERCOSTAL AT FS484.0 BETWEEN RBL27 AND RT SILL HAS CRACKED INBD CLIP. REMOVED OLD AND REPLACED WITH NEW CLIP IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

RT FLOOR SEAT RAIL STICK 1 HAS MULTIPLE SPOTS OF CORROSION AND GOUGES. REMOVED AND REPLACED RT 1 FLOOR SEAT RAIL IAW AMM 53-01-11.

Part: STRAP — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

FLOOR STRAP AT FS 559 HAS CORROSION BETWEEN RBL 27 AND THE RT FLOOR SILL, IN THE CABIN. REMOVED AND REPLACED FLOOR STRAP AT FS 559 RBL 27 IAW SRM 51-42-06.

Part: VANE — CHAFED (`TE FLAP) · airframe 27,963 hrs · 25,698 cycles

RIGHT INBOARD FLAP VANE IS CHAFFED IN 3 LOCATIONS ON LEADING EDGE. REMOVED 3 DAMAGED SECTIONS OF THE RIGHT INBOARD FLAP VALVE LEADING EDGE ALL INSTALLED 3 NEW SECTIONS. IAW SRM 51-42-10 AND SRM 57-52-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

FRAME 605 IS CRACKED JUST BELOW STGR 9L, IN THE CARGO BAY. REPAIRED FRAME 605 IAW REO 601R-53-61-5214 REV A.

Part: RUB STRIP — CHAFED (LT COWLING) · airframe 27,963 hrs · 25,698 cycles

LT LOWER CORE COWL LIP IS CHAFED. REMOVED AND REPLACED GWI LIP AND RUBSTRIP IAW CMM 71-12-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

RT SIDE SEAT RAIL STICK 2 HAS MULTIPLE SPOTS OF CORROSION AND GOUGES. REMOVED AND REPLACED RT SIDE SEAT RAIL STICK 2 IAW AMM 53-01-11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

FLT CONTROL CABLE FAIRLEAD SUPPORT INTERCOSTAL AT FS 484.00 BTWN LBL27 AND LBL36 INBD AND OTBD ATTACH ANGLE CLIPS CRACKED. REMOVED CRACKED CLIPS AND INSTALLED NEW IAW SRM 51-42-21 AND REO 601R-53-41-059 REV B.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

PREVIOUS REPAIR ON THE AFT PRESSURE BULKHEAD HAS A CHAFE MARK AT RBL 27, IN THE CARGO BAY. REPAIRED EXISTING DOUBLER ON AFT PRESSURE BULKHEAD AT RBL 27 IAW REO 601R-53-61-6950 IR 04/20/2019.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

PREVIOUS REPAIR ON THE AFT PRESSURE BULKHEAD HAS A CHAFE MARK AT LBL 18, IN THE CARGO BAY. REPAIRED EXISTING DOUBLER ON AFT PRESSURE BULKHEAD AT LBL 18 IAW REO 601R-53-61-6950 IR 04-20-19.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

PREVIOUS REPAIR ON THE AFT PRESSURE BULKHEAD HAS A CHAFE MARK AT RBL 36. IN THE CARGO BAY. REPAIRED PREVIOUS REPAIR AT RBL 36 AFT PRESSURE BULKHEAD IAW REO 601R-53-61-6950 IR 04/20/2019.

Part: RUB STRIP — CHAFED (RT COWLING) · airframe 27,963 hrs · 25,698 cycles

RT UPPER NOSE ACCESS COWL TRAILING EDGE HAS CHAFING DAMAGE. REMOVED AND REPLACED NOSE ACCESS COWL T/E (RUB-STRIP) IAWCMM 71-14-01.

Part: FITTING — GOUGED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

MAIN AVIONICS COMPARTMENT DOOR FWD LH FITTING ON FUSELAGE IS GOUGED. BLENDED DAMAGE IAW SRM 51-12-00 TR 51-44 NO ALLOWABLE DAMAGE LIMITS IAW SRM 53-21-23 REMOVED AND REPLACED FITTING IAW SRM 51-41-04 601R-38343-1 B94305.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 27,963 hrs · 25,698 cycles

CARGO NET TIE-DOWN FITTINGS ON TOP OF LBL 27 HAVE CORROSION BETWEEN FS 559+96 AND FS 574, IN THE CARGO BAY. (3 TOTAL) REMOVED AND REPLACED 3 EA CARGO NET TIE DOWN FITTING IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

LT SIDE SEAT RAIL STICK 3 HAS MULTIPLE SPOTS OF CORROSION AND GOUGES. REMOVED CORROSION IAW SRM 51-12-00 FOUND TO BE OUT OF LIMITS DUE TO NO BLENDING PERMITTED IN CROSS SECTION "V" IAW EO P53029 REMOVED AND REPLACED 601R-38312-1195 LT SEAT RAIL NR 3 IAW AMM 53-01-11.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 27,963 hrs · 25,698 cycles

CARGO NET TIE-DOWN FITTINGS ON TOP OF LBL 9 HAVE CORROSION BETWEEN FS 574 AND FS 605, IN THE CARGO BAY. (2 TOTAL) REMOVED AND REPLACED 2 EA CARGO NET TIE DOWN FITTING IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

RT SIDE SEAT RAIL STICK 3 HAS MULTIPLE SPOTS OF CORROSION AND GOUGES. REMOVED CORROSION IAW SRM 51-12-00 MAT.REM 0.021 MAX IS 0.09 FOUND TO BE OUT OF LIMITS IAW EO PS3029 REMOVED AND REPLACED 601R38312-1195 LT SEAT RAIL NR 3 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

LT SIDE SEAT RAIL STICK 4 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

LT SIDE SEAT RAIL STICK 5 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

LT SIDE SEAT RAIL STICK 2 HAS MULTIPLE SPOTS OF CORROSION. BLENDED CORROSION IAW SRM 51-21-06 ORIG .370 REMOVED .028 REMAIN 7.342 FOUND OUT OF LIMITS IAW EO# P53029 REMOVED AND REPLACED 601R38312-295 LT SIDE SEAT RAIL STICK 2 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,963 hrs · 25,698 cycles

LT SIDE SEAT RAIL STICK 1 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED LT SIDE SEAT RAIL 1 IAW AMM 53-01-11.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 27,963 hrs · 25,698 cycles

CARGO DOOR TRACK FWD LOWER STIFFENER IS CRACKED. REMOVED UNSERVICEABLE STIFFNER INSTALLED SERVICEABLE STIFFNER IAW SRM 51-42-06 & 51-41-02.

Part: B-NUT — LOOSE (APU) · airframe 27,536 hrs · 25,254 cycles

DURING THE DESCENT WE NOTICED A STRONG FUEL ODOR IN THE FLIGHT DECK. RESECURED LOOSE B NUT ON APU FUEL FLOW PRESSURE SWITCH ALL CHECKS GOOD PER AMM 49-30-00.

Part: FLASHLIGHT — NO TEST (CABIN) · airframe 26,957 hrs · 24,627 cycles

FA EMERGENCY FLASHLIGHT BELOW THE SEAT WAS NOT TESTING CORRECTLY. RED LIGHT WAS NOT FLASHING. REMOVED AND REPLACED THE FWD FLASHLIGHT IAW AMM 25-62-02, OPS CHECKED GOOD.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 26,566 hrs · 24,190 cycles

FA EMERGENCY FLASHLIGHT STRAP WAS BROKEN. REPLACED THE STRAP IAW CMM 25-60-02.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,351 hrs · 23,962 cycles

EMERGENCY LIGHT, CABIN CEILING INOPERATIVE. R & R THE BULB IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,345 hrs · 23,956 cycles

EMERGENCY LIGHTING IS NOT ILLUMINATING LAST 3 FEET RT SIDE. REMOVED AND REPLACED THE EMRGENCY LIGHT IAW AMM 33-51-01. NO FURTHER DEFECTS FOUND. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,194 hrs · 23,771 cycles

EMERGENCY LIGHT BULBS INOPERATIVE. R & R THE BULBS IAW AMM 33-51-13. OPS CHECKED GOOD, OK FOR SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 25,878 hrs · 23,435 cycles

SMOKE TOILET CAUTION AFTER LANDING, JUST AS THE LEFT ENGINE WAS SHUT DOWN AND BLEEDS ON APU. WENT AWAY AFTER F/A WENT BACK AND LOOKED AROUND. PERFORMED EQUIVALENT SCENARIO AND OPS CHECKED LAV SMOKE DETECTOR. OPS CHECKED IAW AMM 26-16-01. COULD NOT DUPLICATE MESSAGE. OK FOR SERVICE. NO SMOKE IN LAV OR CABIN. OPS CHECKED GOOD.

Part: WIRE — SHORTED (EMERGENCY LIGHT) · airframe 25,377 hrs · 22,897 cycles

CIELING EMER EXIT SIGN INOP CREW REPORTED. FOUND SHORTED WIRE LY32A22, REPAIRED IAW ESPM 20-15-00. OPS CHECK GOOD IAW AMM 33-51-00. REF NRWC # 631494 FOR DETAILS ON WORK PERFORMED.

Part: LIGHT — DAMAGED (CABIN) · airframe 25,319 hrs · 22,836 cycles

PAX DOOR FLOOR EMERGENCY FLOODLIGHT DAMAGED AND LOOSE. REPLACED THE FLOODLIGHT ASSY IAW AMM 33-51-19. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 24,398 hrs · 21,846 cycles

CAPTAIN'S EMERGENCY FLASHLIGHT DISCHARGE INDICATOR DOES NOT FLASH. REMOVED AND REPLACED THE BATTERY IAW AMM 25-61-02. INDICATOR FLASHES, OK FOR SERVICE.

Part: PBE — UNSERVICEABLE (CABIN) · airframe 23,975 hrs · 21,405 cycles

DURING INSPECTION NOTED PBE POUCH IN FWD WARDROBE HAS LOST VACUUM SEAL. REMOVED & REPLACED FWD WARDROBE PBE IAW AMM CH 35-30-00.

Part: PBE — UNSERVICEABLE (COCKPIT) · airframe 23,975 hrs · 21,405 cycles

DURING INSPECTION NOTED PBE POUCH IN FLIGHT DECK HAS LOST VACUUM SEAL. REMOVED & REPLACED FLIGHT DECK PBE WITH SERVICEABLE UNIT IAW AMM CH 35-30-00.

Part: PBE — UNSERVICEABLE (CABIN) · airframe 23,975 hrs · 21,405 cycles

DURING INSPECTION NOTED PBE POUCH IN AFT CABIN HAS LOST VACUUM SEAL. REMOVED & REPLACED AFT CABIN PBE WITH SERVICEABLE UNIT IAW AMM CH 35-30-00.

Part: HARNESS — BROKEN (OXYGEN MASK) · airframe 23,538 hrs · 20,966 cycles

OBSERVER`S OXYGEN MASK IS LEAKING AIR WHEN TESTED. THE RUBBER HARNESS IS BROKEN. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS CHECKED GOOD.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 23,527 hrs · 20,954 cycles

CAPTAIN`S OXYGEN MASK HARNESS LEAKING O2. SWAPPED OBSERVER OXYGEN MASK WITH CAPTAIN`S MASK IAW AMM 35-10-01. REMOVED AND REPLACED THE OBSERVER`S OXYGEN MASK WITH PILOT MASK AND INSTALLED NEW MASK INTO THE PILOT POSITION IAW AMM 35-11-12-400-801. LEAK CHECKED GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (NLG) · airframe 23,407 hrs · 20,829 cycles

NOSE GEAR DISAGREE DURING CLIMB OUT, AIRSPEED 170KTS. NOSE GEAR STAYED DOWN AND GREEN MAIN GEAR RETRACTED NORMAL. RAN QRH GEAR EXTENDED NORMAL, NORMAL LANDING. REMOVED AND REPLACED NLG CENTERING PROXIMITY SENSOR BRACKET IAW CMM 32-20-04. REMOVED AND REINSTALLED TOW GUARD COLLAR IAW TS 00871R6 WITH CORRECT SHIMMING. PERFORMED OPS CHECKS OF NLG. ALL CHECKED GOOD.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

AFT PRESSURE BULKHEAD, FWD LOWER RT SIDE HAS SKIN GOUGED. REPAIRED APB FWD LOWER SKIN AT RBL 27.50 IAW REO 601R-53-61-2155, REO 601R-53-61-1285 REF WIP ITEM 10 LEAK CHECK GOOD IAW AMM 21-51-00-790-802, STEP 3A & 3B.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

AFT PRESSURE BULKHEAD, FWD LOWER RT SIDE HAS SKIN GOUGED. REPAIRED APB LOWER SKIN AT RBL 36.50 IAW REO 601R-53-61-2155, REO 601R-53-61-1285 REF WIP STEP 10 LEAK CHECK GOOD IAW AMM 21-51-00-790-802, STEP 3A & 3B.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

FLOORBEAM ATTACH FITTING FS 621.00, LBL9 HAS A CORRODED FASTENER HOLE OTBD FLANGE. REPAIRED FLOORBEAM ATTACH FITTING FS 621.00, LBL 9 IAW EA CRJ253-04436.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

AFT PRESSURE BULKHEAD IS CRACKED AT TOP OF CARGO DOOR AFT TRACK AT 621. REPAIRED AFT PRESSURE BULKHEAD CRACK WEB AT TOP OF CARGO DOOR AFT TRACK LBL 27.5, FS 621 IAW REO 601R-53-61-1541 AND REO 601R-53-61-5735.

Part: SKIN — CHAFED (RT AILERON) · airframe 23,294 hrs · 20,715 cycles

RIGHT AILERON UPPER L/E SKIN HAS CHAFING DAMAGE INBD AND OTBD OF CENTER HINGE. ALSO, OTBD OF OTBD HINGE. R & R RT AILERON UPPER L/E SKIN IAW SRM 51-40-11, 51-42-21, 51-42-06, AND AMM 27-15-01.

Part: MOUNT BRACKET — DAMAGED (TE FLAP VANE) · airframe 23,294 hrs · 20,715 cycles

RIGHT WING OTBD FLAP, FLAP VANE MOUNT BRACKETS HAVE HIGH METAL AT APPROXIMATELY WS 163.00 AND 170.00 AND 296.00. RIGHT WING OTBD FLAP VANE MOUNT BRACKET NR 7 OUT OF LIMITS IAW REO 601R-57-53-195, R & R WITH NEW BRACKET IAW SRM 51-42-21 AND SRM 51-42-10.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 23,294 hrs · 20,715 cycles

AT OK TO CLOSE, RT WING L/E ATTACH BRACKET AT WS 149.58 CRACKED. REMOVED CRACKED ATTACH BRACKET AND REPLACED WITH NEW BRACKET IAW SRM 51-41-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

RIGHT FLOOR SILL HAS CORROSION JUST FWD OF THE SERVICE DOOR OPENING AT FS 319.70, IN CABIN. REMOVED CORROSION ON STA 319.70 RT FLOOR SILL, OUT OF LIMITS, REMOVED AND INSTALLED NEW FLOOR SILL IAW REO 601R-53-00-530, SRM 51-40-10, SRM 51-42-20.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

FRAME FS 605.00, STR 26L TO STR 26R IS CORRODED FWD/AFT SIDE. R & R FRAME IAW SRM 51-42-06.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

AFT PRESSURE BULKHEAD, FWD LT SIDE HAS SKIN GOUGED. REPAIRED 621 BULKHEAD LT FWD SIDE IAW REO 601R-53-61-2155, REO 601R-53-61-1285.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

FRAME 333 HAS CORROSION ON THE AFT SIDE BETWEEN STR 26L AND STR 26R, IN THE FWD ELECTRONIC EQUIPMENT BAY. REPAIRED FRAME AT STA 333, STR 26L-STR 26R IAW EA 253-04425, SM-27.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

202.75 BULKHEAD AT BL 23.7 IS CRACKED AT BRAKE CABLE PASS THROUGH. REPAIRED STA 202.75, BULKHEAD AT LBL23.7 IAW REO 601R-53-11-563.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

FRAME 319.70, TOP INBD SPLICE HAS CORROSION, JUST ABOVE THE RT FLOOR SILL AND FWD OF THE SERVICE DOOR OPENING. R & R ANGLE IAW SRM 51-42-24.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

EXTERIOR SKIN PANEL BETWEEN FS 559.0 TO FS 559.0+112 AND STR L25 AND STR R25 HAS MULTIPLE AREAS OF CORROSION ON LOWER SURFACE. REPAIRED SKIN BETWEEN FS 559 TO FS 559+112 AND STR 25R AND STR 25L IAW EA 253-04446.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

FRAME 333 BETWEEN STR 0 AND PASSENGER DOOR UPPER SILL IS CRACKED. REPAIRED FRAME IAW EA CRJ253-04426.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

FLOOR RAIL BEAM RBL9, FS 559.00+48 TO FS 559.00+80 HAS CORROSION ON THE OTBD FLANGE. R & R FLOORBEAM SECTION RBL9, FS 559.00+48 TO FS 559.00+68 IAW SRM 53-00-43. REPAIR NR 2 SM-27.

Part: FRAME — CRACKED (BS 333) · airframe 23,293 hrs · 20,715 cycles

WHILE PERFORMING A ZONE INSPECTION, IAW 53-200-08. FRAME AT BS 333 WAS FOUND CRACKED AT A TOOLING HOLE BELOW STRINGER 1L. THE TOOLING HOLE MEASURED A 0.250''DIAMETER AND THE CRACKS EMANATED UP AND DOWN FROM THE HOLE 0.125'' EACH DIRECTION. THE CRACK WAS REMOVED BY OPENING THE HOLE TO 0.499'' AND PERFORMED A NDI TO ENSURE CRACKS WERE CONTAINED. A REPAIR WAS INSTALLED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

FRAME FS 589.00 HAS CORROSION BETWEEN STR 25R AND STR 26R. R & R FRAME SECTOR IAW SRM 51-42-06 SM-24.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

RBL9, SEAT TRACK 559.00 TO 559.00+80 HAS CORROSION UPPER AND SIDE SURFACES. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. R & R SEAT TRACK IAW MM 53-01-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

ANGLE CLIP IS CRACKED ON THE INBD SIDE OF RBL 9 AND AFT SIDE OF BEAM 280, IN CABIN BELOW FLOOR. R & R CLIP IAW SRM 51-42-24 AP-104.

Part: BRACKET — CRACKED (RT WING) · airframe 23,294 hrs · 20,715 cycles

PRESSURE REFUELING BRACKET ON RT CENTER WING FRONT SPAR IS CRACKED. REMOVE RT PRESSURE REFUELING BRACKET AND INSTALLED NEW PRESSURE REFUELING BRACKET IAW SRM 51-40-11+ SRM 51-42-21, SM-27.

Part: FITTING — CRACKED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

ANGLE CLIP IS CRACKED ON THE OTBD SIDE OF LBL 9 AND AFT SIDE OF BEAM 280, IN CABIN BELOW FLOOR. R & R CLIP IAW SRM 51-42-24 AP-104.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

STRINGER CLIPS 3 LT AT FS 280 IS CRACKED. REMOVED 2 EA, NR 3 LT CRACKED STRINGER END CLIPS AT FS 280, FABRICATED, TREATED, PRIMED, AND TOP COATED AND INSTALLED 1 EA NEW CLIPS IAW SRM 51-24-16, 51-21-11, 51-25-06 AND 51-25-16, 51-42-06, 51-42-21, SM-22.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

RBL 9 SEAT TRACK, FS 409.00+128 TO FS 590.00 HAS CORROSION. R & R SEAT TRACK ON RBL9 FS 409.00 TO FS 590.00 IAW AMM 53-01-11.

Part: FITTING — CRACKED (COCKPIT) · airframe 23,294 hrs · 20,715 cycles

LEFT WINDSHIELD SIDE POST LOWER OTBD ANGLE CLIP IS CRACKED, IN THE FLT DECK. REMOVED CRACKED LT WINDSHIELD SIDEPOST LOWER OTBD ANGLE CLIP, LOCATED, TREATED DRILLED HOLES, AND INSTALLED NEW CLIP IAW SRM 51-40-11, 51-21-11, TR 51-36, 51-42-21, SM-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

RT AISLE SEAT TRACK, STICK 2 HAS CORROSION, IN CABIN. R & R SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

LBL9 SEAT TRACK FS 409.00+128 TO FS 590.00 HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49, REMOVED SEAT TRACK IAW AMM 53-01-11 INSTALLED NEW SEAT TRACK IAW AMM 53-01-11.

Part: BEAM — CRACKED (FUSELAGE) · airframe 23,294 hrs · 20,715 cycles

BEAM 280 IS CRACKED JUST OTBD OF RBL 9, IN CABIN BELOW FLOOR. REPAIRED FLOORBEAM IAW REO 601R-53-11-171.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 23,294 hrs · 20,715 cycles

CARGO TIE DOWN TRACK RBL 27, FS 559.00+88 HAS CORROSION. REMOVED CORROSION, OUT OF LIMITS, R & R CARGO TIE DOWN, TRACK RBL 27, FS 559.00+88 IAW AMM-53-00-49, SRM 53-51-49.

Part: SEAL — MISSING (FIRE BOTTLE) · airframe 23,239 hrs · 20,663 cycles

COCKPIT FIRE EXTINGUISHER SEAL MISSING. VERIFIED FIRE EXTINGUISHER NOT DISCHARGED, RE-SEALED FIRE EXTINGUISHER IAW AMM 26-23-01.

Part: CABLE — FRAYED (PAX DOOR) · airframe 23,233 hrs · 20,657 cycles

FORWARD COUNTERBALANCE CABLE, 2ND, HAS AT LEAST 6 STRANDS BROKEN WITHIN 1 INCH SPAN AT BOTTOM CONNECTION ON PAX DOOR. REMOVED & INSTALLED FWD, 2ND COUNTERBALANCE CABLE ON PAX DOOR IAW AMM 52-11-17. ADJUSTED CABLE TENSION IAW AMM 52-11-17. OPERATIONS CHECKED GOOD.

Part: BRACKET — BENT (NLG) · airframe 23,160 hrs · 20,589 cycles

NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF, TROUBLESHOT IAW FIM 32-60-09 AND FOUND NLG OLEO CENTER/EXTENDED PROXIMITY BRACKET BENT, R+R NLG OLEO CENTER/EXTENDED PROXIMITY BRACKET IAW CMM 32-20-04. ADJUSTED PROXIITY SENSOR IAW AMM 32-61-05. PERFORMED OPS CHECK OF THE GEAR RETRACTION IAW AMM 32-30-00, OPS CHECK GOOD.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 23,038 hrs · 20,464 cycles

DENT ON THE LT FUSELAGE MEASURING 3.00 INCHES X 2.50 INCHES X .010 INCHES DEEP. REPAIRED IAW EA CRJ253-03115.

Part: SKIN — DENTED (FUSELAGE) · airframe 23,038 hrs · 20,464 cycles

THE FUSELAGE SKIN BETWEEN FS 290 & 295 AT STRINGER 17L WAS FOUND DENTED. THE DENT MEASURES 6.5 INCHES X 2.25 INCHES X 0.018 INCHES DEEP. REPAIRED IAW EA CRJ253-03119.

Part: LIGHT — BROKEN (CABIN) · airframe 22,724 hrs · 20,149 cycles

EMERGENCY FLOOR LIGHT STRIP BROKEN. R & R EMER FLOOR LIGHT STRIP IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,602 hrs · 20,028 cycles

FOUND FWD EMER FLOOR PATH LIGHTING TO BE INOPERATIVE. R & R EMER FLOOR PATH LIGHTING FWD STRIP. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,311 hrs · 19,748 cycles

BACK HALF OF EMER LIGHT STRIP IS INOPERATIVE. R & R EMER LIGHT STRIP LAMP STRIPS IAW AMM 33-51-01. REFER TO WORK ORDER 54673-2000-0050 FOR INSTALLATION & OPERATIONS CHECK OF EMER LIGHT STRIP.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,290 hrs · 19,731 cycles

FS 621 BULKHEAD LINTEL FITTING CRACKED. REPAIRED IAW REO 601R-53-61-1230.

Part: SKIN — DENTED (RUDDER) · airframe 22,290 hrs · 17,731 cycles

MAINTENANCE WAS TASKED WITH PERMANENT REPAIR OF TWO DENTS ON THE RT RUDDER SKIN. REPAIRED IAW EA CRJ255-02645.

Part: BALLAST — FAULTY (LAVATORY) · airframe 21,768 hrs · 19,224 cycles

SMOKE TOILET CAUTION MSG ON GND LAVATORY SMOKE DETECTOR SOUNDED. FAINT BURNING SMELL, QRH COMPLETED & SMOKE TOILET CAUTION MSG EXTINGUISHED. DEFERRED, R & R LAVATORY LIGHT BALLAST IAW AMM 33-25-07. OPERATIONS CHECKED GOOD MM02. UPDATED PLACARD REMOVED DMI CLEARED.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 21,768 hrs · 19,224 cycles

NOTICED AN OIL SMELL IN CABIN. R & R LT & RT COALESCE SOCKS IAW AMM 21-51-13.

Part: COVER — BROKEN (CABIN) · airframe 21,283 hrs · 18,747 cycles

CLEAR COVER FOR FIRST SECTION OF IN FLOOR EMERGENCY LIGHT BROKEN DETACHED. SECURED FLOOR COVER IAW AMM 33-51-01, OK FOR SERVICE.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 21,263 hrs · 18,729 cycles

EMERGENCY LIGHT TRACK COVER DETACHED NEAR ROW 1. SECURED EMERGENCY LIGHT TRACK COVER IAW AMM 33-51-01. SECURITY CHECKED GOOD.

Part: CONTAINER — TORN (LIFE VEST) · airframe 20,536 hrs · 17,998 cycles

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

Part: DETECTOR — FAULTY (COCKPIT) · airframe 20,413 hrs · 17,883 cycles

DIVERTED, DUE TO "DISPLAY COOL CAUTION QRH COMPLETE MESSAGE PERSISTS MUST LAND AT NEAREST SUITABLE" NO EMERGENCY DECLARED. R & R DISPLAY COOLING LOW FLOW DETECTOR IAW AMM 21-24-07. OP/C GOOD, RD 402, REMAINS OPEN.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 19,267 hrs · 16,629 cycles

FLIGHT ATTENDANT FLASHLIGHT LED INDICATOR NOT BLINKING.

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 19,978 hrs · 17,473 cycles

ON FLIGHT 3633 (MSP TO MSP) ON APPROACH HAD FLAPS FAIL AT 20 DEGREES WHEN COMMANDED TO 30. RECEIVED FLAPS FAIL EICAS MESSAGE AND FLAPS DID NOT MOVE. INDICATED AIRSPEED AT THE TIME WAS 180 KTS, 40 MINUTES INTO FLIGHT. EMERGENCY WAS DECLARED. RESET FLAPS, CYCLED 5 TIMES, OPERATIONS CHECK GOOD. DEFERRED FLAPS PER MEL 27-50-00 AND CAT II AS PER MEL 34-00-10. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED DECEMBER 07, 2012 AND PA AD27-052J. REMOVED AND REPAIRED FLAP CONTROL HANDLE IAW AMM 27-51-01 AND PERFORMED OPERATIONS CHECK. OPERATIONS CHECK GOOD. CODES: FLAP CONTROL LEVER, AIR DATA COMPUTER SIGNAL, AIRCRAFT WIRING, 19C1, 19C2, 25BC.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 19,555 hrs · 17,060 cycles

FLAPS FAIL ILLUMINATED IN FLIGHT, WHILE EXTENDING TO 30 DEGREES AT 160 KIAS. HAPPENED APPROXIMENTLY 34 MINUTES INTO FLIGHT AND OAT WAS 6 DEGREES. PERFORMED FUNCTIONAL AND OPERATIONAL TEST OF FLAPS AND CONTROL LEVER IAW. FLAPS FUNCTIONAL TEST CRJ 200 AMM 25-54-00 IAW. FLAPS OPERATIONAL TEST CRJ 200 AMM 27-54-00 AND IAW FLAP CONTROL LEVER SELF TEST CRJ 200 AMM 27-51-00. OPS TEST GOOD. THIS CLEARS DM 76459.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,376 hrs · 16,890 cycles

SEMI-PRESSURE BULKHEAD AT FS 559 CAP ANGLE AT LBL 18 FOUND CRACKED. REPAIRED IAW PA 53-025 AND BOMBARDIER REO 601R-53-41-260 AND 601R-53-41-609.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,376 hrs · 16,890 cycles

CRACK FOUND IN SEMI-PRESSURE BULKHEAD AT FS 559 CAP ANGLE AT LBL 18. REPAIRED CRACK PER PA 53-025, REO 601R-53-41-260 REV D AND REO 601R-53-41-609 REV A DEVIATION E.

Part: CONTAINER — TORN (LIFE VEST) · airframe 18,775 hrs · 16,285 cycles

ONE INFANT LIFE VEST HAS HOLE IN THE BAG. REMOVED AND REPLACED ONE INFANT LIFE VEST IAW PA 25-096A.

Part: LATCH — OUT OF ADJUST (COCKPIT DOOR) · airframe 18,032 hrs · 15,577 cycles

FLIGHT DECK DOOR WILL NOT STAY SHUT. 3RD WRITE UP. ADJUSTED FLIGHT DECK DOOR LATCH IAW CRJ CMM 52-51-10. OP CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 18,004 hrs · 15,545 cycles

FLOOR SUPPORT BETWEEN FS 574 AND FS 621 AT LBL 72 FOUND CORRODED. REPAIRED IAW REO 601R-53-00-005.

Part: SKIN — CHAFED (LT AILERON) · airframe 18,004 hrs · 15,545 cycles

LEFT AILERON LEADING EDGE PANEL 699AB FOUND CHAFED AT CENTER AND OUTBOARD END. REPAIRED IAW SRM 57-00-31 AND 57-60-00.

Part: SHROUD — CHAFED (RT AILERON) · airframe 18,004 hrs · 15,545 cycles

FIXED INBOARD SHROUD ON THE BOTTOM OF THE RIGHT AILERON AND REMOVABLE AILERON LEADING EDGE ARE CHAFED. REPAIRED IAW SRM 57-60-00 AND 57-00-31.

Part: SKIN — CHAFED (TE FLAP) · airframe 18,004 hrs · 15,545 cycles

LEFT OUTBOARD FLAP CHAFED ON THE LEADING EDGE OUTBOARD OF THE ROLLER BRACKET. REPAIRED IAW SRM 57-53-00.

Part: PANEL — CHAFED (LT AILERON) · airframe 18,004 hrs · 15,545 cycles

LEFT AILERON LOWER SHROUD PANEL 599BB HAS MINOR CHAFING. REPAIRED IAW SRM 57-60-00.

Part: FUEL CONTROL — LEAKING (LT ENGINE) · airframe 17,652 hrs · 15,240 cycles

LEFT ENG MFC LEAKING. REMOVED AND REPLACED LT ENG MAIN FUEL CONTROL IAW AMM 73-21-01. VERIFIED PART EFFECTIVITY, LEAK CHECK GOOD. PERFORMED ALL NECCESSARY ENGINE RUNS FOR LT MFC. REMOVED AND REPLACED IAW AMM 71-00-00 OP/C & FC GOOD.

Part: SECU — DEFECTIVE (SPOILER) · airframe 17,519 hrs · 15,061 cycles

FLT SPOILERS, SPOILERON CAUTION MSG WITH AS MISCOMP AND I/B GND SPLR FAULT. REMOVED AND REPLACED NR 2 SECU IAW AMM 27-61-05. OPS CHECK GOOD. VERIFIED PART EFFECTIVITY.

Part: FLAP — MALFUNCTIONED (WING) · airframe 16,720 hrs · 14,288 cycles

CREW GOT FLAP FAIL ON APPROACH INTO MSP, UNKNOWN IF EMERGENCY DECLARED. CLEARED FLAP FAIL IAW AD 2009-06-12 AND AD 27-052G, - OPS CHECK GOOD.

Part: ACCESS DOOR — DAMAGED (ADG) · airframe 15,451 hrs · 13,101 cycles

ADG ACCESS DOOR (122AR) INNER SURFACE ALONG THE HINGE LINE CONTACT WITH THE AIR DRIVEN GENERATOR (ADG) BLADE. THE RESULTING DAMAGE IS A 1.38 INCH LONG CUT / PENETRATION OF THE KEVLAR INNER SKIN AT THE HONEYCOMB TRANSITION TO THE DOOR EDGE (SEE FIGURE I). THE NOMEX HONEYCOMB CORE DOES NOT APPEAR CRUSHED AND A MAX PENETRATION DEPTH OF 0.25 INCH WAS RECORDED (LOCATION NOT NOTED). A TAP TEST ON THE DOOR OUTER SURFACE DID NOT IDENTIFY DELAMINATION OF THE ACCESS DOOR OUTER SKIN. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-254. AT THE NEXT C CHECK INTERVAL NOT TO EXCEED 5,000 FLIGHT HOURS ACCOMPLISH A PERMANENT REPAIR TO THE ADG ACCESS DOOR INNER SURFACE IN ACCORDANCE WITH CRJ-200 SRM 51-74-10.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 14,630 hrs · 12,297 cycles

4161 DTW MLI (8928) ENCOUNTERED HAIL INBOUND TO MLI. DAMAGE REPORTED: CA WINDSHIELD SHATTERED, IMPACT DAMAGE TO THE RADOME, ADG DOOR LEADING EDGE DAMAGE, DAMAGE TO THE ENGINE INLET COWLING, AND DENTS TO BOTH LEADING EDGES. BOMBARDIER ISSUED REO 601R-51-00-275 FOR FERRY FLIGHT TO CLE AIR SERVICES REPAIR FACILITY. ADDITIONAL INFORMATION WILL BE REPORTED ONCE THE EVALUATION AND REPAIR PLAN IS COMPLETED.