N974EV

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,217 hrs · 23,252 cycles

F/A REPORTS THAT EXIT SIGNS IN THE GALLEY WILL NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE SELECTED ON. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS SYS IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,137 hrs · 22,138 cycles

FOUR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R LAMPS IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 24,114 hrs · 22,114 cycles

SEAT TRACK RBL 9, CORRODED AT FS 364. REMOVED SEAT TRACK SECTION FS 364 - 398 IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-00-11-400-802.

Part: SEAT TRACK — CORRODED (BS 365-398) · airframe 24,114 hrs · 22,114 cycles

SEAT TRACK LBL 9 THAT EXTENDS FROM FS 365 TO 398 CORRODED SEVERAL AREAS. WORST CORROSION AT FS 364.00 OF TRACK. REMOVED SEAT TRACK SECTION IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,114 hrs · 22,114 cycles

BS 280 FLOORBEAM ANGLE IS CORRODED AT CENTER SECTION. REMOVED FLOORBEAM ANGLE IAW SRM 51-42-06 LOCATED HOLES IN NEW PART IAW SRM 51-40-06 TREATED PRIMED AND APPLIED TOPCOAT IAW SRM 51-25-16 AND 51-25-06. INSTALLED NEW ANGLE WET WITH SEATANT IAW SRM 51-42-06-00, 51-42-21-00 & DWG 600-34017. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,114 hrs · 22,114 cycles

BS 280 FLOORBEAM CORRODED AT CENTER SECTION. REPAIRED IAW REO 601R-53-11-2503.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 24,114 hrs · 22,114 cycles

LT SIDE SEAT TRACK THAT EXTENDS FROM FS 364.00 TO FS 409+16 IS CORRODED AT FS 383.00. INSTALLED SERVICEABLE SECTION OF LT SEAT TRACKIAW AMM 53-01-11. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REF A.

Part: SEAT TRACK — CORRODED (BS 547-559) · airframe 24,114 hrs · 22,114 cycles

LEFT SIDE SEAT TRACK THAT EXTENDS FROM FS 547.00 TO FS 559+80 IS CORRODED AT FS 559+69. INSTALLED SERVICEABLE SECTION OF LT SEAT TRACK EXTENDING FROM FS 547.00 TO FS 559.+80 IAW AMM 53-01-11. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REV A. DATED: 11/18/2011.

Part: BULKHEAD — CRACKED (AFT PBH) · airframe 24,114 hrs · 22,114 cycles

REAR PRESSURE BULKHEAD WEB FORWARD FACE IS CRACKED ABOVE CARGO DOOR AFT TRACK AREA. REPAIRED IAW REO 601-53-61-1541.

Part: SPRING — LACK OF LUBE (EMERGENCY EXIT) · airframe 24,114 hrs · 22,114 cycles

LT OVERWING EMERGENCY EXIT FAILED FUNCTION TEST IAW TASKCARD 000-52-830-104. RELEASED TENSION ON SPRINGS BY CLEANING & LUBING & REINSTALLED LT EMERGENCY EXIT DOOR LATCH SPRINGS IAW AMM 52-21-02-400-801, 12-20-02-640-802. OPS TESTED GOOD IAW AMM 52-21-00-710-801.

Part: SPRING — LACK OF LUBE (EMERGENCY EXIT) · airframe 24,114 hrs · 22,114 cycles

RT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST IAW TASKCARD 000-52-840-102. RELEASED TENSION ON SPRINGS BY CLEANING & LUBING & REINSTALLED RT EMERGENCY EXIT DOOR LATCH SPRINGS IAW AMM 52-21-02-400-801, 12-20-52-640-802. OPS TESTED GOOD IAW AMM 52-21-00-710-801.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,114 hrs · 22,114 cycles

LOWER EMERGENCY LIGHT AT PAX DOOR FAILED OPS CHECK. R & R LAMPS IN PAX DOOR LOWER EMERGENCY LIGHT IAW AMM 33-51-10-000-801 AND 33-51-10-400-801. COMPLIED WITH OPS TEST OF THE LOWER EMERGENCY LIGHT AT THE PAX DOOR IAW AMM 33-51-00-710-801, OPS TESTED GOOD.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,114 hrs · 22,114 cycles

ASD AFT DRAG ANGLE CRACKED AT PULLEY BRACKET. REPAIRED IAW REO 601R-52-11-513.

Part: FLOOR SKIN — CRACKED (BS 202) · airframe 24,114 hrs · 22,114 cycles

CRACK ON FLOOR SKIN LT SIDE FWD OF FS 202. REPAIRED IAW REO 601R-53-11-081.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,488 hrs · 21,446 cycles

F/A FLASHLIGHT INOPERATIVE. R & R FA FLASHLIGHT IAW AMM 25-61-02. ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,255 hrs · 20,150 cycles

NR 8 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM 33-51-21, OPS CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED (APU FIRE) · airframe 22,227 hrs · 20,121 cycles

APU FIRE INDICATION ON LANDING FOLLOWING STRONG FUEL ODOR. EMERGENCY DECLARED. R & R APU FIRE BOTTLE AND SQUIB IAW AMM 26-22-10. OPS CHECKED GOOD.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 20,895 hrs · 18,633 cycles

FLAPS FAIL 0 DEGREE ON APPROACH, REPEAT WRITEUP. EMERGENCY DECLARED AS A PRECAUTION. ALL WORK ACCOMPLISHED. AD 2009-06-12 ACCOMPLISHED.

Part: BPSU — UNSERVICEABLE (TE FLAPS) · airframe 20,891 hrs · 18,627 cycles

ON APPROACH AFTER SELECTING FLAPS 8200 KNOTS RECEIVED FLAPS FAIL CAUTION MSG FLAPS REMAINED AT ZERO DEG C/W QRH AND NO FLAP LANDING. EMERGENCY DECLARED AS A PRECAUTION. RT BPSU REPLACED.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 20,858 hrs · 18,590 cycles

F/O FLASHLIGHT INOP. R & R FLASHLIGHT BATTERIES IAW AMM 25-61-04. OPS CHECKED GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 20,403 hrs · 18,088 cycles

CAPTAINS LT SIDE WINDOW SPIDER WEBED DESCENDING BELOW 24000 FT INTO LT (FIRE TRUCKS WERE ROLLED AS A PRECAUTION) N/C & FLT 5353 CX. REMOVED AND REPLACED CAPTAIN'S SIDE WINDOW IAW AMM 56-12-01. OPS CHECK GOOD.

Part: ANGLE — CORRODED · airframe 20,305 hrs · 17,970 cycles

WHILE PERFORMING MAINTENANCE, FOUND PAX DOOR ANGLE ASSY TO HAVE CORROSION ABOVE HINGE ON SILL. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED ANGLE IAW SRM 51-42-06, 51-42-13, & 51-42-21. INSTALLED AND SEALED ANGLE ASSY IAW 601R31527-211.

Part: PLACARD — DAMAGED (CABIN) · airframe 20,305 hrs · 17,970 cycles

PAX DOOR "EXIT" PLACARD PARTIALLY MISSING. REMOVED WORN PLACARD IAW MM 11-30-00-000-801 AND APPLIED NEW EXIT PLACARD IAW MM 11-30-00-400-801.

Part: SILL — CORRODED (BS 349) · airframe 20,305 hrs · 17,970 cycles

SERVICE DOOR SILL PLATE UPPER AFT ANGLE HAS CORROSION AT FS 349 UNDER CABIN FLOOR PANEL 232CRF. REPAIRED IAW THE REO 601R-53-21-1277.

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 20,305 hrs · 17,970 cycles

LT FS 621 FLOOR SUPPORT ANGLE PREVIOUS REPAIR CRACKED. REPAIR OF THE DAMAGED PORTIONS OF ANGLE 601R38031-239 IS COMPLETED IAW REO 601R-53-61-117.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 20,305 hrs · 17,970 cycles

FS 621 PRESSURE BULKHEAD FWD FACE HAS 9 BROKEN ISOLATORS. FOUND 13 BROKEN ISOLATORS AND R & R THE ISOLATORS WITH NEW SERVICEABLE ISOLATORS P/B SL2337-3 IAW SRM 51-42-06. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 20,305 hrs · 17,970 cycles

LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROX .6" LONG. REPLACED CRACKED INTERCOSTAL LT SIDE AT FS 621 STR 14L IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 20,305 hrs · 17,970 cycles

CARGO FLOOR TRACK SEGMENTS AT LBL 9 AND RBL 9 CORRODED BETWEEN FS 559+80 AND FS 559+96. REMOVED 2 CORRODED CARGO TRACKS AND REPLACED 2 NEW CARGO TRACKS IAW SRM 51-41-02. THIS REPAIR REQUIRE MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 20,305 hrs · 17,970 cycles

LT CARGO FLOOR SUPPORT CAP ANGLE HAS CORROSION AROUND FASTENER HOLES OTBD SIDE OF LBL 27 BETWEEN FS 574 AND FS 621. REMOVED CORROSION FOUND IAW REO 601R-53-00-005, REPAIR STEPS 1 AND 2.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 20,305 hrs · 17,970 cycles

RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROX .5" LONG. REPLACED CRACKED INTERCOSTAL RT SIDE AT FS 621, STR 14R IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: CARGO TRACK — CORRODED (BS 605-621) · airframe 20,305 hrs · 17,970 cycles

CARGO BAGGAGE RAIL CORRODED AT LBL 9 BETWEEN FS 605 AND FS 621. REMOVED 1 CORRODED CARGO FLOOR TRACK AND REPLACED A NEW CARGO TRACKS IAW SRM 51-41-02. THIS REPAIR REQUIRE MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 364-694) · airframe 20,305 hrs · 17,970 cycles

RT SIDE FWD SECTION OF SEAT TRACK FS 364.00 TO FS 394.00 HAS SEVERAL AREAS OF CORROSION. CORRODED SECTION OF SEAT TRACK REMOVED IAW AMM 53-01-11-000-802. NEW FLOOR SEAT TRACK INSTALLED IAW AMM 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 559-574) · airframe 20,305 hrs · 17,970 cycles

CARGO BAY FLOOR TRACKS CORRODED AT LBL 9 AND RBL 9 BETWEEN FS 559+112 AND FS 574. REMOVED 2 CORRODED CARGO FLOOR TRACKS AND REPLACED 2 NEW CARGO TRACKS IAW SRM 51-41-02. THIS REPAIR REQUIRE MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)

Part: LIGHT — DAMAGED (CABIN) · airframe 20,128 hrs · 17,768 cycles

EMERGENCY EXIT FLOODLIGHT ON LT WARDROBE AT ENTRY WAY IS DAMAGED. R & R EMER EXIT FLOODLIGHT ASSY ON WARDROBE IAW AMM 33-51-10, OP'S CHECK GOOD. R & R EMERGENCY EXIT FLOODLIGHT ASSY ON WARDROBE IAW AMM 33-51-10, OP'S CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 19,779 hrs · 17,345 cycles

2ND EMERGENCY CEILING LIGHT IS INOP. R & R EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OP'S CHECKED GOOD. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,704 hrs · 17,262 cycles

3 SEGMENTS OF GREEN FLOOR LIGHTING DO NOT ILLUMINATE. OPS CHECK GOOD IAW AMM 33-51-01. (CLOSED)

Part: FRAME — CRACKED (BS 605 S18L) · airframe 19,506 hrs · 17,047 cycles

FOUND FS 605.00 FRAME CRACKED AT STRINGER 18L. REPAIRED IAW REO601R-53-61-3887.

Part: PLACARD — MISSING (CABIN) · airframe 19,332 hrs · 16,845 cycles

"EXIT" DECAL MISSING FROM (3RD STEP) ON AIRSTAIR DOOR END. REPLACED EXIT DECAL IAW AMM 11-30-00. (CLOSED)

Part: RESERVOIR — WORN (HYD SYSTEM) · airframe 18,749 hrs · 16,150 cycles

RECEIVED NOSE GEAR DISAGREE WARNING MSG AFTER T/O, CYCLED GEAR AND GOT GEAR DISAGREE MSG AND NOSE DOOR WARNING MSG. (EMERGENCY EQUIPMENT REQUESTED AS A PRECAUTION) (LANDING GEAR RETRACTION SYS ) REFER TO LOG PAGE 532717-3 HYD RESERVOIR, REPLACED. PERFORMED OPS CHECK, GEAR SWING IAW 32-30-00, OPS CHECK NORMAL DEFER CLEAR PLACARD REMOVED. (CLOSED)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 16,687 hrs · 13,927 cycles

FLAP FAIL CAUTION MSG ON CLIMB OF ATL AT 18800' AND LANDED AT 300FPM, EMERGENCY DECLARED. FLT 5563 DEL 32 MINS

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,684 hrs · 13,924 cycles

AFT SECTION EMERGENCY FLOOR TRACK LIGHT INOP.

Part: SKIN — CRACKED (PAX DOOR) · airframe 16,671 hrs · 13,910 cycles

PAX DOOR AFT SKIN WEB IS CRACKED IN RADIUS AT STEP 832CT AND FIXED MID STEP.

Part: BEAM — CRACKED (BS 280) · airframe 16,671 hrs · 13,910 cycles

FS 280 OTBD OF RBL 9, TRANSVERSE BEAM IS CRACKED.

Part: POST — DAMAGED (BS 409) · airframe 16,671 hrs · 13,910 cycles

FOUND FS 409.0+128 VERTICAL POST LBL 18.0 OTBD SIDE HAS INDICATION NOTED A1TWL 69.0 AFT FLANGE APPROX .2 INCH IN LENGTH 50 PERCENT FSH FAILED NDT INSP. REMOVED VERTICAL POST IAW SRM 51-42-06. FABRICATED NEW VERTICAL POST IAW SRM 51-24-16. HEAT TREATED REPAIR PART, POST FROM 7075-0 TO A T62 IAW AMS 2770. LOCATED AND DRILLED POST IAW SRM 51-40-11 AND 51-42-06. INSTALLED VERT POST IAW SRM 51-40-11 & 51-42-06.

Part: POST — DAMAGED (BS 409) · airframe 16,671 hrs · 13,910 cycles

FOUND FS 409+128 VERTICAL POST BL 0.0 LT SIDE HAS INDICATION NOTED AT WL 69.0 AFT FLANGE APPROX .2 INCH IN LENGTH 50 PERCENT FSH FAILED NDT INSP. REMOVED VERTICAL POST IAW SRM 51-42-06. FABRICATED NEW VERTICAL POST FOR AS PER SAMPLE. ALSO FABRICATED NEW VERTICAL POST DOUBLER ANGLE AS PER SAME IAW SRM 51-24-16, REF DWG 601R32208. PAINTED POSTS AND ANGLES IAW SRM 51-25-01. LOCATED AND DRILLED POST AND ANGLE IAW SRM 51-40-11 AND 51-42-06. INSTALLED POST AND ANGLE IAW SRM 51-40-11 & 51-42-06.

Part: BULKHEAD — CRACKED (BS 559) · airframe 16,671 hrs · 13,910 cycles

FS 559 BULKHEAD WEB HAS INDICATION NOTED AT RT SIDE WEB WL 59.10 INBD OF RBL 18.0 APPROX .5 INCH IN LENGTH 60 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED BULKHEAD IAW REO 601R-53-41-260, STEP S1 THRU 14.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 16,671 hrs · 13,910 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.0 INCH IN LENGTH.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,671 hrs · 13,910 cycles

REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LINTEL ATTACHMENT FITTING APPROX .1 INCH IN LENGTH 80 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED THE PRESSURE BULKHEAD WEB AT THE LINTEL ATTACHMENT FITTING IAW REO 601R-53-61-1230 REV. "D".

Part: SILL — CRACKED (FUSELAGE) · airframe 16,671 hrs · 13,910 cycles

FS 280 O/B OF LBL 9 FLOOR SILL CRACKED APPROX 1 INCH LONG. REPAIRED IAW REO 601R-53-11-136 REV A.

Part: BEAM — CRACKED (FUSELAGE) · airframe 16,671 hrs · 13,910 cycles

FS 280 O/B OF LBL 9 TRANSVERSE BEAM CRACKED APPROX .5 INCH LONG. REPAIRED BEAM IAW EO 600-53-0090.

Part: SILL — CRACKED (FUSELAGE) · airframe 16,671 hrs · 13,910 cycles

FS 280 O/B OF RBL 9 FLOOR SILL CRACKED AT 2 EA FASTENER HOLES APPROX .5 INCH LONG. REPAIRED IAW REO 601R-53-11-136 REV A.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 16,671 hrs · 13,910 cycles

FS 280 O/B RBL 9 FLOOR SUPPORT ATTACH FITTING CRACKED. REMOVED & REPLACED SUPPORT ATTACH FITTING & FABRICATED NEW ATTACH FITTING IAW REO 601R-53-11-171.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 16,671 hrs · 13,910 cycles

FS 621-625 INTERCOSTAL, OBLIQUE RT SIDE CRACKED 1" LONG. REMOVED AND REPLACED UPPER INTERCOSTAL IAW SRM 51-42-21.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 16,671 hrs · 13,910 cycles

PASSENGER DOOR FWD AND AFT ANCHOR FITTING ARE CRACKED. REMOVED THE PAX DOOR FWD/AFT ANCHOR FITTING ASSY AND INSTALLED NEW SERVICEABLE ANCHOR FITTING, P/N 601R380741-3 AND 601R380742-3 TO THE FWD AND AFT SIDE OF THE PAX DOOR IAW MM 52-11-17-400-804.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 16,671 hrs · 13,910 cycles

FS 621-625 INTERCOSTAL, OBLIQUE LT SIDE CRACKED APPROX 3/4 INCH LONG. REMOVED AND REPLACED UPPER INTERCOSTAL IAW SRM 51-42-21.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 16,671 hrs · 13,910 cycles

EMERGENCY LIGHT TRIM PANEL ON GALLEY HAS A BROKEN LENS.

Part: ANGLE — CRACKED (BS 700) · airframe 16,671 hrs · 13,910 cycles

ANGLE AT FS 700.00 AFT EQUIP BAY DOOR CUTOUT ON RT SIDE IS CRACKED. REMOVED ANGLE IAW SRM 51-42-06. FABRICATED NEW ANGLE 601-35013-30 PER DWG 60L35013. INSTALLED ANGEL IAW SRM 51-42-06.

Part: LIGHT — DAMAGED (CABIN) · airframe 16,671 hrs · 13,910 cycles

TRACK LIGHTING NEAR 1AB DAMAGED.

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 16,520 hrs · 13,762 cycles

ON APPROACH NOSE GEAR DID NOT COME DOWN. RAN QRH WITH 3B/2B NOSE GEAR CAME DOWN. EMERGENCY VEHICLES REQUESTED AS A PRECAUTION. FLT 4974, 4931, 5515, 5613 CX.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 14,712 hrs · 12,130 cycles

LEFT FUSELAGE FWD OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT FUSELAGE FWD OVERWING EMERGENCY LIGHT IAW CRJ 200 AMM 33-51-00. (B)

Part: WARNING LIGHT — ILLUMINATED · airframe 14,240 hrs · 11,721 cycles

STALL FAIL CAUTION MESSAGE APPEARED AFTER TAKEOFF AND REMAINED ON FOR ENTIRE FLIGHT, EN ROUTE TO ATL A/C DIVERTED TO CVG DUE TO MTC. THE TOWER DECLARED AN EMERGENCY AND ROLLED EMERGENCY VEHICLES AS A PRECAUTION, FLT 4451 DEL 245 MINS.

Part: DRAG ANGLE — CRACKED (DOOR) · airframe 13,804 hrs · 11,353 cycles

ASD AFT DRAG ANGLE CRACKED.

Part: ENGINE — VIBRATION (NR 1) · airframe 13,434 hrs · 11,047 cycles

AT 27000 FT W/ ANTI ICE ON HEAVY VIBRATION IN ENG NR 1 (OVER 3.5) DESCENED TO 24000 NR 2 STARTED VIBRATION FOR 15 SEC. EN ROUTE TO ATL A/C DIVERTED TO CAE DUE TO MTC. EMERGENCY DECLARED.

Part: UNKNOWN — ODOR (CABIN) · airframe 13,427 hrs · 11,040 cycles

F/A AND PASSENGERS REPORTED MOMENTARY ELECTRICAL BURNING SMELL AT 7A/B IN FLIGHT. APU NOT RUNNING, WING AND COWL ANTI-ICE ON. NO SMELL IN LAV OR COCKPIT. FLT 4673 DEL 60 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,277 hrs · 10,138 cycles

1ST AND 2ND FROM FRONT CEILING EMERGENCY LIGHTS INOP.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 12,220 hrs · 10,087 cycles

CORROSION ALONG FWD RIGHT WALL OF CARGO BAY (MARKED).

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 12,220 hrs · 10,087 cycles

ENGINE SUPPORT BEAM CRACKED ON UPPER WEB AT APPROXX RBL 9.0. [SUP 05-08-07] REPAIRED ENGINE SUPPORT BEAM IAW ASAS T/C EO 600-53-169 AND REO'S 601R-53-61-2152 AND REO 601R-53-61-870.

Part: STRUCTURE — CRACKED (WING) · airframe 12,220 hrs · 10,087 cycles

RANRC 356. POSSIBLE CRACK FOUND AT AFT FASTENER HOLE FOR LT DRAIN NEXT TO BOOST PUMP IN CANISTER. [07-23-07] REPAIRED IAW ALL SRM AND EO`S.

Part: STEP — CRACKED (PAX DOOR) · airframe 12,220 hrs · 10,087 cycles

PAX DOOR TOP STEP CRACKED ON AFT AND FWD SIDE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,220 hrs · 10,087 cycles

FS 484 AT LBL 36 INTERCOSTAL IS CRACKED AT TOP O/B RIVET. REMOVED DAMAGE PORTION OF INTERCOSTAL AT FS 484/LBL 36 PER REO 601R-53-41-059. FABRICATED REPAIR ANGLE FROM 2024-T3 .063 PO 9345-1 PER REO 601R-53-41-059. FOR LPI REFER TO W/C 410 (BOTH REPAIR ANGLE AND CUTLINE) INSTALLED REPAIR ANGLE IAW REO 601R-53-41-059. SUPPLEMENTAL - SDR CLOSED 05/01/07.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,220 hrs · 10,087 cycles

FS 484 AT RBL 27 INTERCOSTAL IS CRACKED IN RADIUS. REMOVED CRACKED CLIP AT FSA 484 RBL 27 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 BHS1124 4-25-07. DUPLICATED INTERCOSTAL IAW CRJ SRM 53-41-43 USING PREFORMED ANGLE P/N 56144-3, INSTALLED ANGLE IAW CRJ SRM 51-42-20. SUPPLEMENTAL - SDR CLOSED 05/01/07.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,220 hrs · 10,087 cycles

FS 484 AT RBL 36 INTERCOSTAL IS CRACKED AT TOP O/B RIVET. REMOVED CRACKED CLIP AT FS 484 RBL 36 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 (1127/RA334) DUPLICATED CRACKED CLIP USING 2024T3.063 ALUMINUM IAW CRJ SRM 51-24-21. INSTALLED CLIP IAW CRJ SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 05/01/07.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,352 hrs · 9,453 cycles

RIGHT SIDE FUSELAGE FWD EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,352 hrs · 9,453 cycles

LEFT SIDE FUSELAGE AFT EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,352 hrs · 9,453 cycles

RIGHT SIDE FUSELAGE AFT EMERGENCY LIGHT INOP.

Part: BATTERY PACK — DISCHARGED (FUSELAGE)

DURING A GROUND INSPECTION, THE EMERGENCY LIGHT SWITCH WAS FOUND LT ON, WITH NO POWER ON THE AIRCRAFT AND THE EMERGENCY LIGHTS DEAD. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT, NEAR THE SERVICE DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT, NEAR THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: PLACARD — FADED (PAX DOOR)

DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR EXIT PLACARD WAS FOUND TO NEED REPLACING. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EXIT PLACARD. (M)