N413

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 26,549 hrs · 24,813 cycles

RIGHT ELEVATOR LIGHTNING STRIKE ON TRAILING EDGE. REPAIR OF SKINS & REPLACEMENT OF T/E EXTRUSION P/N 601R24042-1 IAW REO 601R-55-21-382 REV C.

Part: MOUNT — CRACKED (HYDRAULIC SYS) · airframe 26,549 hrs · 24,813 cycles

NR 2 HYD SYSTEM O/B CASE DRAIN FILTER MOUNT IS CRACKED. REMOVED UNSERVICEABLE NR 2 HYD SYSTEM O/B CASE DRAIN FILTER MOUNT AND REPLACED WITH SERVICEABLE MOUNT IAW CRJ 200 SRM 51-40-11, 51-42-06 AND 51-42-21.

Part: SKIN — DAMAGED (STABILIZER) · airframe 26,549 hrs · 24,813 cycles

C/W AWAC CARD 4DMI16663 REPAIR LEFT STAB LWR SKIN. REMOVED AND RE-INSTALLED NEW SERVICEABLE RIVET IAW CRJ 200 SRM 51-42-06.

Part: POST — CRACKED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

FS 409 VERT POST AT LBL & RBL 27 I/B RADIUS CRACKED FROM BOTTOM OF POST APPROX HALFWAY BETWEEN FIRST & SECOND RIVET. REPAIRED LT & RT LBL 27 POSTS I/B IAW GREO 601R-53-41-056 REV F & SNI EO K601R32209S01.

Part: SCREW — LOOSE (APU) · airframe 26,549 hrs · 24,813 cycles

APU EXHAUST HEAT SHIELD HAS 4 EACH LOOSE SCREWS. REPAIRED HEAT SHIELD SCREW HOLES 4 EA IAW REO 601R-49-81-167.

Part: FAIRING — DAMAGED (TE FLAP) · airframe 26,549 hrs · 24,813 cycles

LEFT FLAP STAB FAIRING CHAFED AND GOUGED NEW SERVICEABLE STUB FAIRING FABRICATED & INSTALLED NEW SERVICEABLE SEAL RETAINERS. REMOVED UNSERVICEABLE LEFT STUB FAIRING LOCATED, DRILLED, INSTALLED NEW SERVICEABLE LEFT STUB FAIRING ASSY IAW AMM 53-82-01 SRMS 51-24-21, 51-40-11.

Part: DOOR — CHAFED (RT MLG) · airframe 26,549 hrs · 24,813 cycles

RIGHT MLG DOOR AFT EDGE IS CHAFED. REPAIRED CHAFING ON AFT EDGE OF RIGHT MLG DOOR IAW BOMBARDIER REO 601R-32-82-366.

Part: STRUCTURE — SCRATCHED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

NICKS AND SCRATCHES FOUND ON CARGO DOOR CUTOUT FWD LIP. BLENDED & RESTORED FINISH IAW REO 601R-53-61-4839. BLENDED & RESTORED FINISH IAW REO 601R-53-61-4839.

Part: STRUCTURE — SCRATCHED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

NICKS AND SCRATCHES FOUND ON CARGO DOOR CUTOUT UPPER LIP. BLEND RESTORE FINISH IAW REO 601R-53-61-4839.

Part: PANEL — DAMAGED (LT ELEVATOR) · airframe 26,549 hrs · 24,813 cycles

LEFT ELEVATOR HINGE UNDER PANEL 334AB HAS TOOLING MARKS. REPAIRED DAMAGE IAW REO 601R-55-11-456.

Part: DOOR — OUT OF LIMITS (LT MLG) · airframe 26,549 hrs · 24,813 cycles

LEFT MLG DOOR IS OUT OF LIMITS PER AMM 32-12-01-502 ZONE E. REMOVED AND REPLACED UNSERVICEABLE LEFT MLG DOOR WITH UNSERVICEABLE LEFT MLG DOOR P/N 601R31178-169, S/N: 7863.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

FUSELAGE SKIN JUST AFT OF APU EXHAUST HAS SCREW MARKS. BLEND REPAIR IAW REO 601R-53-61-4841.

Part: COWLING — DELAMINATED (RT ENGINE) · airframe 26,549 hrs · 24,813 cycles

RIGHT UPPER CORE COWL HAS DELAMINATION ON I/B SIDE & L/E (FIRE SHIELD). REPAIRED IAW REO 601R-71-12-458.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

CENTER VERTICAL STIFFENER ON AFT SIDE OF 621 BULKHEAD CHAFED BY BLEED AIR VALVE. BLEND REPAIR IAW REO 601R-53-61-4842.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

AFT SIDE OF 621 BULKHEAD AT STR 14L ANGLE IS CRACKED. REMOVED AND REPLACED P/N 601-35012-51 IAW CRJ 200 SRM 51-40-11, 51-42-31.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,549 hrs · 24,813 cycles

FITTING AT FS 310.0 STR 17 CORRODED. REMOVED AND REPLACED FITTING P/N 601R38335-1S IAW CRJ 200 SRM 51-40-11 & 51-42-21.

Part: MOUNT — CRACKED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

NR 2 HYD SYSTEM RETURN FILTER MOUNT IS CRACKED. REMOVED UNSERVICEABLE NR 2 HYD SYSTEM RETURN FILTER MOUNT AND REPLACED WITH SERVICEABLE MOUNT IAW BOMBARDIER REO 601R-53-62-031 REV A.

Part: MOUNT BRACKET — CRACKED (HYD ACCUMULATOR) · airframe 26,549 hrs · 24,813 cycles

HYD ACCUMULATOR FWD O/B MOUNTING BRACKET IS CRACKED IN THE NOSE HYD COMPARTMENT. REMOVE AND REPLACED BRACKET IAW CRJ 200 SRM 51-42-21.

Part: STOP FITTING — CHAFED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

RIGHT EMERGENCY EXIT STOP FITTING CHAFED 6EA. BLENDED 6EA STOP FITTINGS ON RIGHT EMERGENCY EXIT.

Part: BRACKET — CRACKED (RT ENGINE) · airframe 26,549 hrs · 24,813 cycles

BRACKET CRACKED ON RIGHT ENGINE NOSE INLET FWD OF T/R FLEX DRIVE SHAFT BETWEEN 4 & 5 O` CLOCK POSITION. REMOVED AND REPLACED IAW CRJ 200 SRM 51-42-13.

Part: STOP FITTING — CRACKED (FUSELAGE) · corrosion level 2 · airframe 26,549 hrs · 24,813 cycles

MAIN AVIONICS DOOR STOP FITTING BACK UP STUCK ON FWD SIDE IS CORRODED. REMOVED AND REPLACED PART.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 26,549 hrs · 24,813 cycles

LEFT MLG DOOR INNER SKIN CHAFED. REMOVED & REPLACED CHAFED UPPER INNER SKIN FOUND CHAFE ON LOWER INNER SKIN FOUND WITHIN LIMITS WITH MAT LOSS OF .004, MAX ALLOWED IS .008.

Part: BRACKET — BROKEN (RT ENGINE) · airframe 26,549 hrs · 24,813 cycles

RIGHT ENGINE INLET BROKEN BRACKET FWD OF FAN INLET TEMP. REMOVED AND REPLACED BRACKET.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

2 FASTENER HOLES ON ACCESS HOLE 132AL ARE DAMAGED 12 O`C LOCK AND 3 O` CLOCK POSITION. REPAIRED PER BOMBARDIER REO 601R-53-11-162 REV B.

Part: RIB — CHAFED (TE FLAP) · airframe 26,549 hrs · 24,813 cycles

CHAFE DAMAGE LEFT I/B FLAP ON I/B END OF FLAP L/E AND SURROUNDING RIVER HEADS. REMOVED AND REPLACED DAMAGED RIB & FASTENERS IAW CRJ 200 SRM 51-42-06.

Part: MOUNT BRACKET — CRACKED (EXTERNAL POWER) · airframe 26,549 hrs · 24,813 cycles

EXTERNAL A/C POWER PLUG MOUNT IS CRACKED. REMOVED AND REPLACED MOUNT BRACKET.

Part: HANDLE — CRACKED (E&E BAY DOOR) · airframe 26,549 hrs · 24,813 cycles

MAIN AVIONICS COMPARTMENT DOOR HANDLE CRACKED. REMOVED AND REPLACED HANDLE ASSY.

Part: FITTING — DAMAGED (RT MLG TRUNNION) · airframe 26,549 hrs · 24,813 cycles

WHILE PERFORMING COLD WORKING ON RIGHT LOWER FLANGE OF MLG TRUNNION FITTING FOUND 1EA OVERSIZED FASTENERS. REPAIRED HOLE PER REO 601R-57-21-1886.

Part: SKIN — CHAFED (WING) · airframe 26,549 hrs · 24,813 cycles

BUTE DOOR 694PB HAS CHAFE SPOTS ON UPPER SIDE. REMOVE & REPLACE BUTE DOOR SKIN AIW CRJ 200 SRM 51-42-06.

Part: HINGE — GOUGED (TE FLAP) · airframe 26,549 hrs · 24,813 cycles

RIGHT OUTBD FLAP OUTBD HINGE ARM & HINGE BOX HAVE GOUGING AND FOD DAMAGE AT FLAP HINGE POINT. REPAIR IAW REO 'S 601R-57-53-971 & 601R-57-21-1888.

Part: RIB — CRACKED (LT WING) · airframe 26,549 hrs · 24,813 cycles

LEFT MLG BATT RIB CRACKED. REMOVED UNSERVICEABLE REPAIR DOUBLER WITH A SERVICEABLE REPAIR DOUBLER AND INSTALLED.

Part: SILL — CORRODED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

RIGHT FLOOR SILL IN CARGO COMPARTMENT HAS CORROSION FROM FS 559+80 TO 621. REPAIRED IAW REO 601R-53-00-515.

Part: RIB — CRACKED (RT WING) · airframe 26,549 hrs · 24,813 cycles

RIGHT MLG BATT RIB IS CRACKED. REPAIRED PER REO 601R-57-51-046 REPAIR 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

TOP OF FS 280 FLOORBEAM CAP IS CORRODED. REPLACED FS 280 FLOORBEAM CAP.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

PAX FS 280 CLIPS ARE CRACKED UPPER O/B LBL 9 & RBL 9. FABRICATED & INSTALLED SERVICEABLE O/B LBL 9 & RBL 9 CLIPS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

280 I/B RBL 9 & LBL 9 CLIPS ARE CRACKED. FABRICATED & INSTALLED SERVICEABLE RBL 9 & LBL 9 I/B CLIPS.

Part: RIVET — POPPED (FLOOR SUPPORT) · airframe 26,549 hrs · 24,813 cycles

FS 280 FLOOR SUPPORT STRUCTURE LBL 9 FWD TB ANGLE ABOVE HAS POPPED RIVET HEAD AND ON UNDER DRIVEN RIVET NEXT TO IT HEAD IS NOT SEATED ON ANGLE.

Part: BRACKET — CRACKED (RT MLG) · airframe 26,549 hrs · 24,813 cycles

RIGHT MLG BRAKE VOLUMETRIC FUSE TRANSDUCER MOUNT BRACKET IS CRACKED. REMOVED AND REPLACED UNSERVICEABLE RIGHT MLG BRAKE VOLUMETRIC FUSE TRANSDUCER MOUNT BRACKET WITH SERVICEABLE MOUNT BRACKET P/N 601R75262-157.

Part: MOUNT BRACKET — CRACKED (LT MLG) · airframe 26,549 hrs · 24,813 cycles

LEFT MLG BRAKE VOLUMETRIC FUSE TRANSDUCER MOUNT BRACKET IS CRACKED. REMOVED AND REPLACED UNSERVICEABLE LEFT MLG BRAKE VOLUMETRIC FUSE TRANSDUCER MOUNT BRACKET WITH SERVICEABLE MOUNT BRACKET P/N 601R75262-159.

Part: RIVET — SHEARED (CARGO BAY) · airframe 26,549 hrs · 24,813 cycles

CARGO BAY NET TIE DOWN SUPPORT ANGLE AS IT ATTACHES TO 621 BULKHEAD HAS SHEARED OFF RIVETS (2EA). REPLACED RIVETS IAW CRJ 200 SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

CLIP UNDER CARGO DOOR SILL BENEATH AFT CARGO DOOR STOP AT FS 605 IS CRACKED. REMOVED & REPLACED CLIP IAW CRJ 200 SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

PAX PRESSURE FLOOR FS 484.0 CLIP ANGLES CRACKED UPPER I/B LBL 27 AND UPPER O/B LBL 36. REMOVED AND REPLACED 484.0 CLIP ANGLES ON UPPER I/B LBL 27 & UPPER O/B LBL 36.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,549 hrs · 24,813 cycles

SEAT TRACK IN CARGO COMPARTMENT AT RBL 9 FROM 559+86 TO 559+96 (APPROX) IS CORRODED. REMOVE AND REPLACE CORRODED SEAT TRACK FROM FS 559 +96 TO 559 +96 (APPROX).

Part: STRUCTURE — GOUGED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

RIGHT AFT SIDE FS 280 AT RBL 9 APPROX 12 INCHES UP FROM FLOOR GOUGED 2 LOCATIONS FROM FWD GALLEY DOOR. REPAIRED RIGHT AFT SIDE FS 280 AFT RBL 9 IAW REO 601R-53-71-1727.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

PAX PRESSURE FLOOR FS 484.0 CLIP ANGLE IS CRACKED UPPER I/B RBL 27. REMOVED AND REPLACED FS 484.0 CLIP ANGLE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,549 hrs · 24,813 cycles

CORROSION FOUND ON RIGHT PAX SEAT RAIL AT FS 364.00 FOUND TO BE OUT OF LIMITS DEPTH OF DAMAGE 024" MAX ALLOWED 020". REMOVED AND REPLACED PAX SEAT RAIL BETWEEN FS 349.00 & FS 379.00 IAW CRJ 200 AMM 53-01-11-000-802, CRJ 200 AMM 53-01-11-400-802 & CRJ 200 SRM 51-40-11.

Part: COWLING — DENTED (RT ENGINE) · airframe 26,549 hrs · 24,813 cycles

TWO DENTS & 1 HOLE FOUND ON RIGHT LWR CORE COWL BETWEEN 2ND & 3RD BEAMS ON I/B SIDE. PERFORM REPAIR IAW CRJ 200 CMM 71-12-01 REPAIR SRS 021.