N980EV

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,707 hrs · 29,755 cycles

LH EXTERIOR EMERGENCY LIGHT INOP REPLAMPED EMREGENCY LIGHT IAW CMM 33-52-06. OPS CHECK GOOD. P/N OFF/ON: 8GH002473-08

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 30,162 hrs · 29,184 cycles

FLOOR SUPPORT AT LBL 9 UPPER INBOARD FLANGE WAS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 409+128 - 559. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-41-2542 REV.

Part: LANDING — CORRODED (RT WING) · airframe 30,162 hrs · 29,184 cycles

RIGHT WING PLANK FUEL PANEL ACCESS HOLE NR 1, 640BB HAS MINOR CORROSION AT INBD AND OUTBD ENDS, WS 54.897 IN NON-CRITICAL ZONE. COMPLIED WITH STEPS 10 AND 11 OF REO 601R-57-21-030 REV L. GAP CHECKED GOOD.

Part: LANDING — CORRODED (LT WING) · airframe 30,162 hrs · 29,184 cycles

LEFT WING PLANK FUEL ACCESS HOLE NR 8, 540FB, HAS MINOR CORROSION ALONG FRONT OF HOLE IN CRITICAL ZONE, WS 136.676. COMPLIED WITH STEPS 10 AND 11 OF REO 601R-57-21-030 REV L. GAP CHECKED GOOD.

Part: LANDING — CORRODED (LT WING) · airframe 30,162 hrs · 29,184 cycles

LEFT WING PLANK FUEL ACCESS HOLE NR 7, 540EB, HAS MINOR CORROSION AT INBD AND OUTBD ENDS WS 116.366 IN NON-CRITICAL ZONE. COMPLIED WITH STEPS 10 AND 11 OF REO 601R-57-21-030 REV L. GAP CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 30,162 hrs · 29,184 cycles

FLOOR SUPPORT CAP ANGLE AT LBL9 HAS MULTIPLE AREAS OF CORROSION BETWEEN FS409+64 TO FS409+128. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-43.

Part: LANDING — CORRODED (ACCESS PANEL) · airframe 30,162 hrs · 29,184 cycles

LEFT WING PLANK FUEL ACCESS HOLE NR 1, 540BB, HAS MINOR CORROSION AT INBD AND OUTBD ENDS, WS 54.897 IN NON-CRITICAL ZONE. COMPLIED WITH STEPS 10 AND 11 OF REO 601R-57-21-030. GAP CHECKED GOOD.

Part: LANDING — CORRODED (RT WING) · airframe 30,162 hrs · 29,184 cycles

RIGHT WING PLANK FUEL PANEL ACCESS HOLE NR 5, 640CB HAS MINOR CORROSION ALONG BACK OF HOLE IN CRITICAL ZONE, WS 76.161.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,162 hrs · 29,184 cycles

AFT CABIN EMERGENCY LIGHTS FAIL. REMOVED AND REPLACED EMERGENCY BATTERY NR 4 IAW AMM 33-51-04-400-801. OP TEST GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 30,162 hrs · 29,184 cycles

FLOOR SUPPORT AT RBL 9 UPPER INBD FLANGE WAS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 409+128 TO 559. INSTALLED A NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-42-06, 51-42-13, 51-42-21, AND REO 601R-53-41-2537 REV--.

Part: FRAME — CORRODED (BS 589) · airframe 30,162 hrs · 29,184 cycles

AFT FUSELAGE FS 589.00 FRAME CORRODED BETWEEN STRINGERS 26R TO 21L. INCLUDES JOB 8775971 OP 318 AND 349. REMOVED AND REPLACED LOWER FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-42-06 AND 51-42-21. LEAK CHECKED GOOD.

Part: FRAME — CORRODED (BS 589) · airframe 30,162 hrs · 29,184 cycles

AFT FUSELAGE FS 589.00 FRAME CORRODED BETWEEN STRINGERS 26R TO 21L. INCLUDES JOB 8775971 OP 318 AND 349. REMOVED AND REPLACED LOWER FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-42-06 AND 51-42-21. LEAK CHECKED GOOD.

Part: RETAINER — GOUGED (PAX DOOR) · airframe 30,162 hrs · 29,184 cycles

PAX DOOR HAS 3 EA GOUGES ON TOP CENTER SEAL RETAINER, WITH DOOR OPEN. REMOVED AND REPLACED PAX DOOR UPPER SEAL RETAINER IAW BOMBARDIER GREO 601R-52-11-915 AND CRJ 200 SRM 51-42-06 AND 51-42-13. LEAK CHECK GOOD. WVAC EMP 769 STAMP

Part: FLOOR SUPPORT — CORRODED (BS 409-) · airframe 30,162 hrs · 29,184 cycles

FLOOR SUPPORT CAP ANGLE AT RBL 9 HAS MULTIPLE AREAS OF CORROSION BETWEEN BS 409 - 409+128. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-11, TR 51-42, 51-42-06, 51-42-21, 51-42-15, 51-45-00.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,162 hrs · 29,184 cycles

FOUND 9 INDICATIONS IN HEEL OF Z-MEMBER FWD FACE OF BS 621 REAR PRESSURE BULKHEAD RBL 18, WL 126 - 135, 40%FSH, BL 0 WL 126 - 135, 45% RSH, LBL 18 WL 126 - 133, 40% FSH, RBL 27.5 WL 107-109 70% FSH, RBL 18 WL 99-104 80%FSH, BL 0, WL 107-113 45% FSH, LBL 18 WL 108-110 40% FSH. REPAIRED THE BS 621 PRESSURE BULKHEAD IAW GREO 601R-53-61-1240 REV D.

Part: BRACKET — GOUGED (LT WING TE FLAPS) · airframe 30,162 hrs · 29,184 cycles

LEFT WING OTBD FLAP, O/B LUG FITTING HAS A SMALL GOUGE ON BRACKET APPX .300 X .300 X .010 DEEP. REPAIRED AREA ON THE LT WING OTBD FLAP, OTBD LUG FITTING IAW REO 601R-57-21-3105 REV--.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 30,162 hrs · 29,184 cycles

FS 280 CROSSBEAM UPPER FLANGE HAS CORROSION AT SEVERAL LOCATING BETWEEN LBL 4 TO RBL 17. ACCOMPLIISHED FS 280 REPAIR IAW REO 601R53-11-926 REV B.

Part: SEPARATOR — CHAFED (NACELLE) · airframe 30,162 hrs · 29,184 cycles

PANEL 422DB IS CHAFED. REMOVED AND REPLACED FWD AND AFT SEPERATORS ON PANEL 422DB IAW SRM 51-41-06.

Part: SEPARATOR — CHAFED (NACELLE) · airframe 30,162 hrs · 29,184 cycles

PANEL 422DB IS CHAFED. REMOVED AND REPLACED FWD AND AFT SEPERATORS ON PANEL 422DB IAW CRJ200 SRM 51-41-06 WVAC EMP STAMP 771

Part: STIFFENER — CHAFED (BS 621 BULKHEAD) · airframe 30,162 hrs · 29,184 cycles

FS 621 REAR PRESSURE BULKHEAD AFT VERTICAL STIFFENER AT B.L. 0 AT WL 140 IS CHAFED APROX -.5 WIDE & 0.030 DEEP. REPAIRED AREA IAW REO 601R-53-61-7060, AND GREO 601R-53-61-1523.

Part: FITTING — CRACKED (WINDOW POST) · airframe 30,162 hrs · 29,184 cycles

COPILOTS WINDSHIELD POST LOWER AFT FITTING CRACKED. INSTALLED A NEW FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (WINDOW POST) · airframe 30,162 hrs · 29,184 cycles

PILOT WINDSHIELD SIDE POST LOWER AFT FITTING CRACKED. REPLACED THE FITTING IAW SRM 51-42-21.

Part: FRAME — CRACKED (BS 333) · airframe 30,162 hrs · 29,184 cycles

FS 333 FRAME CRACKED ABOVE PAX DOOR CUTOUT BETWEEN STRINGER 0 AND 1L. LOCATED, DRILLED, AND INSTALLED A NEW SERVICEABLE FRAME SEGMENT IAW SRM 51-42-06, 51-42-21, AND 51-40-11.

Part: SEAT TRACK — CORRODED (BS 449) · airframe 30,162 hrs · 29,184 cycles

RIGHT SIDE SEAT TRACK IS CORRODED FS 449. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 30,162 hrs · 29,184 cycles

RIGHT SIDE SEAT TRACK WAS CORRODED BS 406+112 - 449. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 30,162 hrs · 29,184 cycles

LEFT SIDE SEAT TRACK IS CORRODED BS 449 - 499. INSTALLED A NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — GOUGED (BS 364-409) · airframe 30,162 hrs · 29,184 cycles

LEFT SIDE SEAT TRACK SEGMENT IS GOUGED BS 364 - 409+16. INSTALLED NEW SEAT TRACK RAIL IAW AMM 51-01-11-400-802.

Part: SEAT TRACK — DAMAGED (BS 365-400) · airframe 30,162 hrs · 29,184 cycles

SEAT TRACK, LBL 9, BETWEEN BS 365 TO 400 WAS CORRODED AND GOUGED AT MULTIPLE LOCATIONS. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 30,162 hrs · 29,184 cycles

RIGHT SIDE SEAT TRACK WAS GOUGED, BS 364 - 409+16. INSTALLED A NEW SEAT TRACK IAW AMM 51-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 30,162 hrs · 29,184 cycles

LEFT SIDE SEAT TRACK IS CORRODED FS409+112 - 449 INSTALLED NEW SEAT RAIL IAW AMM 53-01-11-400-802.

Part: BULKHEAD WEB — GOUGED (BS 621) · airframe 29,195 hrs · 28,142 cycles

SCRATCH/GOUGE/DENT NOTED ON RPB @FS621 2.25" OB OF RIVET CENTER LINE FOR LBL18.00 22" UP FROM THE FLOOR 1.5"L X 1.25"W X.025" DEPTH DEEPEST DEPTH IS AT END OF GOUGE REATHER SHARP IN NATURE COMPLIED WITH TEMP REPAIR IAW REO 601R-53-61-6808 NDT COMPLIED WITH REFERANCE NON ROUTINE 655399 FOR FINAL DISPOSITION

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 29,195 hrs · 28,142 cycles

DURING COMPLETION OF T/C53-280-607 NOTED MULTIPLE AREAS OF HARDWARE STRIKE DAMAGE TO THE RPB FWD FACE SKIN LOCATIONS LBL27.5 LBL18.0 RBL18 RBL27.5 RBL36.2 ALL ARE 30" UP FROM THE FLOOR AND IN A LINE HORIZONTALLY ALL ARE ON A RIVET LINE COMPLETED REPAIRS TO NOTED DAMAGED AREAS IAW REO601R-53-61-2155 NDT COMPLIED WITH

Part: BULKHEAD — DAMAGED (BS 621) · airframe 29,195 hrs · 28,142 cycles

DURING COMPLIANCE OF T/C 53-280-607 NOTED MULTIPLE RIVET HEAD STRIKE DAMAGE ON THE FWD FACE OF THE REAR PRESSURE BULKHEAD @FS621. LOCATIONS LBL36.20 LBL27.5 LBL18 LBL9.5 RBL18.0 RBL27.5 AND RBL36.2 ALL 13" UP FROM THE FLOOR AND IN LINE HORIZONTAL REMOVED AND REPLACED DAMAGED RIVETS IAW SRM 51-42-06

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,659 hrs · 27,542 cycles

GALLEY DOOR, EMERGENCY EXIT LIGHT, ONE BULB WAS INOPERATIVE. PERFORMED AN OPS TEST OF THE EMERGENCY LIGHT IAW AMM 33-51-00. OPS CHECKED GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,659 hrs · 27,542 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,417 hrs · 27,276 cycles

ON A ROUTINE 200 NOTICE, FIRST OFFICER`S FLASHLIGHT LED INOPERATIVE. R & R THE FLASHLIGHT IAW AMM 25-61-02. OPS CHECKED GOOD. OK FOR SERVICE.

Part: SEAL — BROKEN (PBE) · airframe 28,350 hrs · 27,203 cycles

SEAL ON CABIN PBE WAS BROKEN. REPLACED THE SEAL ON THE AFT PBE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 28,269 hrs · 27,121 cycles

FORWARD FA FLASHLIGHT, OK LIGHT NOT BLINKING AND UNIT VERY WARM TO THE TOUCH. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-61-02. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: PBE — DAMAGED · airframe 27,985 hrs · 26,782 cycles

WARDROBE PBE LOST ITS VACUUM. REMOVED AND REPLACED THE PBE IAW AMM 35-30-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,877 hrs · 26,661 cycles

LEFT FWD EMERGENCY LIGHT OUT (EXTERIOR PAX DOOR). RELAMPED LEFT FWD EMERGENCY LIGHT (EXTERIOR PAX DOOR) IAW AMM 33-51-21. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,717 hrs · 26,498 cycles

LT OVERWING EXTERIOR EMERGENCY CENTER LIGHT NR 3 INOP. R&R EXTERIOR EMERGENCY OVER WING CENTER LIGHT NR 3 IAW AMM 35-51-21. OPS CHECK GOOD.

Part: GAUGE — DAMAGED (OXYGEN BOTTLE) · airframe 26,640 hrs · 25,341 cycles

ENTRANCE AREA OXYGEN BOTTLE HAS DAMAGED GAUGE. REMOVED AND REPLACED PORTABLE OXYGEN BOTTLE IAW AMM 35-31-01.

Part: LIGHT — DAMAGED (CABIN) · airframe 26,226 hrs · 24,908 cycles

SEVERAL SECTIONS OF THE FLOOR EMERGENCY LIGHTS WERE DAMAGED. REPLACED THE LIGHTS, OPS CHECKED GOOD. IAW VCMM 33-60-13.

Part: LEAD — DISCONNECTED (EMERGENCY LIGHT) · airframe 26,225 hrs · 24,905 cycles

LEFT EMERGENCY EXIT LIGHTED SIGN INOP. CONNECTED LEFT EMERGENCY EXIT LIGHTED SIGN POWER LEADS IAW AMM 33-51-13 OPS CHECKED GOOD.

Part: SOCKET — UNSECURE (EXIT SIGN) · airframe 26,225 hrs · 24,905 cycles

AFT BLUE SOCKET ON CNT EXIT LIGHT DAMAGED. RESECURED AFT BLUE SOCKET ON CNT EXIT LIGHT IAW AMM 33-51-14.

Part: HOSE — DAMAGED (OXYGEN MASK) · airframe 26,225 hrs · 24,905 cycles

THE OBSERVER`S OXYGEN MASK HOSE DAMAGED. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12-000-801.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 25,929 hrs · 24,571 cycles

CARGO TRACK AT BS 559+64 - 559+80, LBL 9 CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,929 hrs · 24,571 cycles

I/B CLIP CRACKED CABLE GUIDE INTERCOSTAL AT 484.00 AND RBL36. COMPLIED WITH REO 601R-53-41-22090. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 25,929 hrs · 24,571 cycles

LT SKIN CRACKED AT FWD HYD COMPT CUTOUT AT FS 187.00 STR 15L. REMOVED AND REPLACED SKIN PANEL AT FS 187.00 STR 15L PER SRM 51-42-06, 51-40-11-00,51-42-13 P/N 600-33052-145, DRAWING 600-33052. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 25,929 hrs · 24,571 cycles

CORROSION FOUND ON TOP OF FLOORSILL AT FS 409.00+128- 559.00 AND LBL 36-40. REMOVED CORROSION FROM FLOORSILL IN DISCREPANT AREAS BETWEEN FS 409.00+128 AND 559.00 AND LBL 36-40 REF SRM 51-21-16. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666 REV C DATED 11-06-2012. RECEIVED AND COMPLIED WITH EC/TC REO 601R-53-41-2092. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 25,929 hrs · 24,571 cycles

CARGO FLOOR TRACK AT 559+64- 559+80 AT LBL 27 IS CORRODED. REMOVED AND REPLACED CARGO FLOOR TRACK AT FS 559+64- 559+80 IAW AMM 53-00-49-000-801 AND 53-00-49-400-801. COMPLIED WITH EC/TC REO 601R-53-00-485 AND REO 601R-53-00-485 REV B AND COMPLIED WITH EC/TC RIL 4354 REV B. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: INTERCOSTAL — CRACKED (BS 484 RBL 36)

INBOARD ANGLE CRACKED, CABLE GUIDE INTERCOSTAL AT BS 484 AND RBL 36. MAINTENANCE COMPLIED WITH REO 601R-53-41-2090

Part: SKIN — CRACKED (BS 187) · airframe 25,660 hrs · 24,269 cycles

LEFT SKIN CRACKED AT FORWARD HYDRAULIC COMPARTMENT CUT OUT BS 187 STRINGER 15L.. REMOVED AND REPLACED THE SKIN PANEL IAW SRM 51-42-06, 51-40-11-00, AND 51-42-13.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 25,660 hrs · 24,269 cycles

CARGO TRACK BS 559+64 - 559+80, LBL 9 IS CORRODED.. MAINTENANCE REMOVED AND REPLACED CARGO TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS409 - 559) · airframe 25,660 hrs · 24,269 cycles

CORROSION FOUND ON TOP OF FLOOR SUPPORT BS 409+128 - 559 AND LBL 36-40. MAINTENANCE REMOVED CORROSION IAW SRM 51-21-06. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, AND EC/TC REO 601R-53-41-2092.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 25,660 hrs · 24,269 cycles

CARGO TRACK AT 559+64 - 559+80, LBL 27 CORRODED. MAINTENANCE REMOVED AND REPLACED CARGO TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: BRACKET — DAMAGED (MLG) · airframe 25,188 hrs · 23,771 cycles

NOSE GEAR DISAGREE AND THEN NOSE GEAR WARNING AFTER TAKEOFF COMPLETED "GEAR DISAGREE GEAR HANDLE UP CHECK LIST" MESSAGE CLEARED AFTER PULLING GEAR HANDLE AND LANDED NORMALLY. LANDING GEAR RETRACTION SYSTEM, ACFT RETURNED TO DEPARTURE AFTER T/O. EMERGENCY ACTIONS, FLT 4873, DEL 190 MINS. REPLACED BRACKET IAW VCMM 32-20-04. LANDING GEAR RETRACTION SYS, OPS CHECKED IAW AMM 32-30-00. PROXIMITY SENSOR PS146A ADJUSTED IAW AMM 32-61-05. DMIL A146808 CLEARED.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,395 hrs · 22,975 cycles

LIGHTED FLOOR-LEVEL EXIT SIGN INOPERATIVE AT LT EMERGENCY EXIT. R & R INVERTER IAW AMM 33-51-07. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 22,423 hrs · 20,939 cycles

AFTER TAKE OFF AND SELECTING GEAR HANDLE UP, RECEIVED LANDING GEAR DISAGREE WARNING, NOSE DOOR OPEN WARNING, WOW INPUT CAUTION, AND RATE OF DESCENT, STEERING INOPERATIVE CAUTION MESSAGES. COMPLIED WITH QHR, COMPLETED MANUAL GEAR LESS THAN 200 FPM EXTENSION PROCEDURES AND RECEIVED THREE GREEN INDICATION, LANDING NORMAL. ACFT RETURNED TO DEPARTURE. REMOVED AND REPLACED NOSE LANDING GEAR ASSY IAW AMM 32-21-01 AND 32-21-00 FIGURE 1 ITEM 20G. OPS CHECKS GOOD NO FURTHER DEFECT NOTED.

Part: PSEU — MALFUNCTIONED (MLG) · airframe 22,423 hrs · 20,939 cycles

GEAR DISAGREE MESSAGE, CLEARED AFTER MANUAL EXTENSION USED, ACFT RETURNED, R & R PSEU IAW AMM 32-61-01, AIPC 32-61-01, FIG 1, ITEM 5. PERFORMED GAP CHECKS OF NOSE GEAR OLEO AND UPLOCK SENSORS IAW AMM 32-61-05. OPS CHECKED GOOD, NO OTHER DEFECTS FOUND. ACFT OK FOR SERVICE PERFORMED FUNCTIONAL TEST OF GEAR EXTENSION/ RETRACTION SYS IAW AMM 32-30-00, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 22,134 hrs · 20,645 cycles

EMERGENCY LIGHTS ON STATUS MESSAGE WITH ACFT POWERED REGARDLESS OF GALLEY SWITCH POSITION OR COCKPIT SWITCH. ALLOW BATTERIES TO CHARGE, OPS TESTED GOOD IAW AMM 33-51-04.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,104 hrs · 20,617 cycles

EXTERNAL POWER RECEPTACLE DOOR LAND IS DAMAGED. REPAIRED IAW REO 601R-53-11-569 ( REV B), REO 601R-53-11-2551, AND REO 601R-53-11-2552 ( REV A ). MAJOR REPAIR IAW GMM 5-3.

Part: HANDLE — DIRTY (PAX DOOR) · airframe 21,538 hrs · 20,031 cycles

PAX DOOR FAILED INNER HANDLE FORCE CHECK. CLEANED ROLLER/TRACK AND CHECKED ADJ AND PERFORMED FORCE CHECK IAW AMM 52-11-25-400-803, STEP 3B(1-3) AND 4 CLOSEOUT. FORCE CHECK IS WITHIN LIMITS AND OP CHECKS GOOD AT THIS TIME NO DEFECTS NOTED.

Part: NUT PLATE — DAMAGED (RT WING) · airframe 21,538 hrs · 20,031 cycles

REMOVED DAMAGED NUTPLATE AT RWS 220 OTBD FLAP RT IAW 51-45-00-00, SRM CRJ200. INSTALLED NEW NUTPLATE IAW SRM 51-45-00-00. THIS REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 21,538 hrs · 20,031 cycles

FWD SEAT TRACK RBL 9.0 CORRODED AT BS 364. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 21,538 hrs · 20,031 cycles

FWD SEAT TRACK CORRODED ON LBL 9.0 BS 364. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,538 hrs · 20,031 cycles

REAR PRESSURE BULKHEAD FWD FACE IS CRACKED ABOVE CARGO DOOR AFT TRACK, REPAIRED IAW REO 601R-53-61-1541.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 21,538 hrs · 20,031 cycles

SEAT TRACK CORRODED AT RBL 9.0 AT BS 559 TO 574. R & R CORRODED SEAT TRACK IAW SRM 51-41-02-00 & 51-23-00-00.

Part: CARGO TRACK — CORRODED (BS 598-605) · airframe 21,538 hrs · 20,031 cycles

CARGO TRACK CORRODED AT LBL 9.0 AT BS 598 AND 605. REPLACED CORRODED CARGO TRACKS WITH SERVICEABLE ONES IAW SRM 51-41-02-00 & 51-23-00-00.

Part: CARGO TRACK — CORRODED (BS 598-605) · airframe 21,538 hrs · 20,031 cycles

CARGO TRACK CORRODED AT LBL 9.0 AT APPROX 598 AND 605. R & R CORRODED CARGO TRACK WITH SERVICEABLE IAW SRM 51-41-02-00 & 51-23-00-00.

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 21,538 hrs · 20,031 cycles

LT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST. ADJUSTED DOOR WITHIN LIMITS IAW AMM 52-21-00-820-801 AND 52-21-00-720-801. ADJUSTED SERRATED PLATE AT LATCH POINT IAW AMM 52-21-00-720-801.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,166 hrs · 19,655 cycles

FWD WARDROBE EMERGENCY FLOOR FLOOD LIGHT INOPERATIVE. REPLACED LAMP AND OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BULKHEAD — CRACKED (BS 202) · airframe 20,333 hrs · 18,804 cycles

BS 202 BULKHEAD CRACKED AT PARKING BRAKE CABLE. CRACK HAS BEEN VERFIED BY NDT FABRICATED FILLERS AND DOUBLER. FABRICATED REINFORCEMENT DOUBLER. PREPARED AND INSTALLED PARTS AND FASTENERS, RESTORED FINISH AND APPLIED CIC. REF. 601R-53-11-563 REV. B. REPAIR TYPE 5. COMPLIED WITH RII GMM 3-3.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 19,685 hrs · 18,085 cycles

AFT MOST CABIN CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT EMER FLOOD LIGHT IAW AMM 33-51-16. OP'S CHECKED GOOD.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 19,563 hrs · 17,942 cycles

ONE ISOLATOR BROKEN ON CARGO COMP AFT WALL. R & R ISOLATOR IAW SRM 51-42-13-00.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 19,563 hrs · 17,942 cycles

ONE ISOLATOR BROKEN ON CARGO BAY AFT BULKHEAD AT BS 621 & RBL 9. R & R 1 EACH ISOLATOR ON AFT BULKHEAD AT 621 AT RBL9 IAW SRM 51-42-13-00.

Part: ANGLE — CRACKED (BS 559) · airframe 19,563 hrs · 17,942 cycles

CAP ANGLE IS CRACKED AT FS 559.00, LBL 18.00. FABRICATED REPAIR PARTS FOR LT SIDE IAW REO 601R-53-41-260, REV E AND REO 601R-53-41-6096, REV B. INSTALLED ALL PARTS IAW OREO 601R 53-41-260 AND 601R-53-41-609.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,563 hrs · 17,942 cycles

BETA LIGHTS AT PAX, SERVICE AND EMERGENCY EXIT DOORS INOPERATIVE. R & R BETA LIGHTS AT PAX SERVICE AND EMERGENCY EXIT DOORS WITH SERVICABLE BETA LIGHTS IAW AMM 33-51-09-000*400-801 AND 33-51-09-000/400-802 AND 20-21-00-910-801.

Part: INTERCOSTAL — CRACKED (BS 654.5-672.2) · airframe 18,711 hrs · 16,987 cycles

FOUND CRACK AT STRINGER 4L BETWEEN FS 654.50 AND FS 672.20 ON INTERCOSTAL, COMPLIED WITH EDDY CURRENT INSP TO LOCATE END OF CRACK IAW NDTM 51-20-06 AND REO 601R-53-62-205. STOP DRILLED CRACK AND REFINISHED REWORKED AREA IAW REO 601R-53-62-205.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 18,666 hrs · 16,940 cycles

ENGINE SUPPORT BEAM CENTER TOP PLATE CRACKED. REPAIRED IAW REO 601R-53-61-345, REV F.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,639 hrs · 16,906 cycles

F/A REPORTS STRONG ODOR OF FUEL IN REAR OF CABIN DURING APPROACH INTO MEM. COULD NOT DUPLICATE , INSPECTED FOR FUEL LEAKS AND ODORS FROM APU IAW AMM 49-10-00.

Part: INTERCOSTAL — CRACKED (BS 625 S14R) · airframe 17,794 hrs · 15,967 cycles

LEFT INTERCOSTAL (LT BRACKETS) CRACKED AT FS 625 AND S14R. REMOVED CRACKED BRACKET IAW SRM 51-42-21. FABRICATED PART OUT OF MATERIAL S6144-14 IAW REO 601R-53-61-100. APPLIED FINISH AND PN IAW REO 601R53-61-100. INSTALLED FABRICATED LT INTERCOSTAL AT FS 625, STR 14 L IAW REO 601R-53-61-100.

Part: INTERCOSTAL — CRACKED (BS 625 S14R) · airframe 17,794 hrs · 15,967 cycles

RIGHT INTERCOSTAL (LT BRACKET) CRACKED AT FS 625, S14R. REMOVED RT INTERCOSTAL (LT BRACKET) AT FS 625 STR 14 L IAW SRM 51-42-21. FABRICATED PART OUT OF MATERIAL S6144-14 IAW REO 601R-53-61-100. APPLIED FINISH AND PN IAW REO 601R-53-61-100. INSTALLED FABRICATED RT INTERCOSTAL AT FS 625, STR 14 R IAW REO 601R-53-61-100.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 16,824 hrs · 14,871 cycles

NR 3 AND NR 4 EMERGENCY LIGHT BATTERY PACKS NO CHARGE. R & R NR3 AND NR4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04-000-801 (REMOVAL) AND AMM 33-51-04-400-801 (INSTALLATION) OPS TEST GOOD IAW SUB TASK 33-51-04-740-005 NO OTHER DEFECTS NOTED.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 16,823 hrs · 14,870 cycles

INTERCOSTAL CRACKED INSIDE ASD AFT SIDE INSIDE PANEL 832BR. REMOVED -318 INTERCOSTAL. REMOVED -318 INTERCOSTAL IAW SRM 51-42-06. INSTALLED AND DRILL UP NEW -318. DRILLED HOLES TO CHIPS ON EACH END IAW SRM 51-40-11. CONTINUE DRILL INNER SKIN AND OUTER SKIN AND INSTALL. PICKED UP ALL FASTENER HOLES AND INSTALLED INTERCOSTAL PN 601R31902-318 INSIDE ASD AFT SIDE INSIDE PANEL 832BR IAW SRM 51-42-06 AND 51-42-20. (CLOSED)

Part: SILL — CRACKED (589) · airframe 16,823 hrs · 14,870 cycles

CLIP CRACKED UNDER CARGO DOOR SILL AT FS 589.0. REMOVED DAMAGED CLIP AT FS 589 AND DRILLED UP NEW SERVICEABLE PART IAW SRM 51-42-20 AND 51-42-06. INSTALLED NEW CLIP AT FS 589.0 IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,823 hrs · 14,870 cycles

CARGO COMPT SEAT RAIL JUST AFT OF FS 559+80 RBL 27 HAS CORROSION. DRILLED NEW SEAT TRACK & INSTALLED IAW AMM 53-01-11-400-802 M1417. INSTALLED FITTING IAW AMM TASK 25-41-01-400-806, SUBTASK 25-41-01-869-007.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,823 hrs · 14,870 cycles

CARGO SEAT RAIL AT FUSELAGE STA 559+80 AND LBL 27 HAS CORROSION. REMOVED AND INSTALLED NEW TRACK SEGMENT AT STA 559 + 80 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,823 hrs · 14,870 cycles

CARGO COMPT SEAT RAIL JUST AFT OF FUS STA 559+80 AT RBL 9 HAS CORROSION. FOUND CORROSION OUT OF LIMITS IAW SRM 53-21-49 AND 53-61-49. R & R SEAT RAIL SECTION IAW AMM 53-01-11.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 16,823 hrs · 14,870 cycles

FLOORBEAM HAS MINOR CORROSION AT LBL 27 BETWEEN FS 574.0 AND FS 621.0 AS MARKED. REMOVED NUT PLATES FROM FLOORBEAM CAP AT LBL27 AND FS576. 579, 585, 591, 597, 603,609 BLENDED CORROSION OUT OF LIMITS AT 5 LOCATIONS REF SRM 51-21-06. REPLACED LBL27 FLOORBEAM CAP. REMOVED LBL27 FLOORBEAM AND DRILLED UP NEW SERVICABLE PART IAW SRM 51-42-06 AND 51-42-21 AND REO 601R-53-61-3778. COMPLETE INSTALLATION OF NUTPLATES AND FLOOR SUPPORT CAPS. COMPLETED INSTALLATION OF NUTPLATES AND STARTED INSTALLATION OF FLOOR SUPPORT CAP IAW REO 601R-53-61-3778. COMPLETE INSTALL OF FLOOR SUPPORT CAP. COMPLETED INSTALLATION OF FLOORBEAM CAP LBL27 AT FS 574 AND 621 IAW REO 601R-53-61-3778 COMPLIED WITH EC/TC REO 601R-53-61-3778 AND GREO 601R-53-61-3778 REV. (CLOSED)

Part: SILL — CRACKED (BS 605) · airframe 16,823 hrs · 14,870 cycles

CLIP CRACKED UNDER CARGO DOOR SILL AT FS 605.0. REMOVED DAMAGED CLIP AT FS 6050 AND DRILLED UP NEW SERVICEABLE PART IAW SRM 51-42-21 AND 51-42-06. INSTALLED NEW CLIP AT FS 605.0 IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,823 hrs · 14,870 cycles

CARGO COMPT SEAT RAIL JUST AFT OF FUSELAGE STA 559+80 AT LBL 9 HAS CORROSION. EVALUATED, FOUND CORROSION OUT OF LIMITS IAW SRM 53-21-49 AND 53-61-49. R & R SEAT RAIL SECTION IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,823 hrs · 14,870 cycles

CARGO COMPT SEAT RAIL AT STA 559+112 LBL 9 HAS CORROSION. FOUND CORROSION OUT OF LIMITS IAW SRM 53-21-49 AND 53-61-49. R & R SEAT RAIL SECTION IAW AMM 53-01-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 16,823 hrs · 14,870 cycles

INTERCOSTAL CRACKED RT OVERWING BELOW EMERGENCY EXIT FWD SIDE RT. REMOVED INTERCOSTAL AT FS 449.85 BELOW RT EMERGENCY EXIT IAW SRM 51-42-06. DRILL AND INSTALL NEW SERVICEABLE INTERCOSTAL. FABRICATED NEW PART FROM S6144-33. EXTRUDED ANDGLE IAW STEP 1 OF RE0 601R-53-82-396. PERFOMRED EDDY CURRENT INSP IAW RED 601R-53--82-396 SND NDTM 51-20-06 ON FABRICATED ANGLE. NO CRACK NOTED. COMPLIED WITH STEPS 3 AND 4 OF RE0601R-53-82-396. AND INSTALLED NEW INTERCOSTAL IAW SRB 51-42-06.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 16,232 hrs · 14,172 cycles

TAKEOFF, RECEIVED WOW INPUT CAUTION THAT LASTED A FEW SECONDS. IT THEN CAME ON AND OFF ABOUT 6 MORE TIMES FOR VARIOUS LENGTHS OF TIME AND AT VARIOUS ALTITUDES. RON QRH (EMERGENCY DECLARED -- TRUCKS STANDING BY AS A PRECAUTION) FOUND LT MLG OTBD PROXIMITY SENSOR OUT OF LIMIT. ADJUST LT MLG OTBD PROX SENSOR IAW AMM 32-61-20. OPS CHECK IS GOOD IAW AMM 32-61-00. (CLOSED)

Part: WATER HEATER — CONTAMINATED (POTABLE WATER) · airframe 16,099 hrs · 14,017 cycles

FA REPORTS CHEMICAL ODOR/ TASTE FROM POTABLE WATER. ALSO REPORTED BY PASSENGERS. DRAINED FWD POTABLE WATER AND SERVICED IAW AMM 12-18-38. (SDR CLOSED)

Part: WARNING LIGHT — ILLUMINATED (NLG) · airframe 15,254 hrs · 13,053 cycles

NOSE GEAR DISAGREE ON GEAR RETRACTION. EMERGENCY DECLARED - ACFT RETURNED TO DEPARTURE AFTER T/O.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 14,805 hrs · 12,563 cycles

CAPTAINS FLASHLIGHT INOP.

Part: BEAM — CRACKED (FS 280)

FS 280 BEAM IS CRACKED OTBD OF RBL 9 BLEOW BOTTOM (2) FASTENERS THAT CONNECT FS 280 BEAM TO RBL 11 VERTICAL BEAM. (K)

Part: WEB — CRACKED (PAX DOOR)

PAX DOOR FWD WEB IS CRACKED IN ZONE 2. REMOVED CRACKED SUCTIONS OF FWD WEB PAX DOOR AND REPAIRED IAW REO 601R-52-11-702, REV A STEPS 1-10, 15. STEPS 13, 14 AND 17 ARE N/A. AREA REQUIRES SEALANT AND PAINT. SEALED AND CLEANED IAW REO 601R-52-702.

Part: WEB — CRACKED (PAX DOOR)

PAX DOOR AFT WEB IS CRACKED IN ZONES 2,3. REMOVED CRACKED SUCTIONS OF AFT WEB PAX DOOR AND REPAIRED IAW REO. AREA REAUIRES SEALANT AND PAINT. SEALED AND CLEANED IAW REO 601R-52-11-702, REV A STEPS 11 AND 12. PAINTED IAW SRM 51-25-01. (K)

Part: ANGLE — CRACKED (FUSELAGE)

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.5 INCHES. REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET IAW SRM 51-92-21. (K)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,826 hrs · 10,685 cycles

JOB 8775921 OPERATION 154 RT FLOOR SUPPORT ANGLE AT FS 621 AND LBL 36 HAS A 1" CRACK.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,826 hrs · 10,685 cycles

JOB 8775921 OPERATION 165 FOUND INBD AND OTBD CLIP ANGLES AT FS 280 AND RBL 9 TO BE CRACKED. SUP 9/11/08 - REMOVED INBD AND OTBD CLIPS AT FS 280 RBL 9 IAW CRJ 200, SRM 51-42-06 AND 51-42-21. INBD AND OTBD CLIPS REQUIRE INSTALL. INSTALLED NEW INBD ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. RBL 9 FS 280.00. REPLACED OTBD SLIP ANGLE FS 280.00, RBL 9 9AW, CRJ 200 SRM 51-42-06 AND 51-42-21.(K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,826 hrs · 10,685 cycles

JOB 8775921 OPERATION 144 PAX DOOR AFT DRAG ANGLE IS CRACKED. RESOLVED ON W/O 98579 TASKCARD NR 00181. C/A REPAIRED PAX DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513. SEAL AND PAINT REQUIRED. SEALED PNL IAW CRJ 200 MM 51-23-00. PAINTED IAW CRJ 200 SRM 51-25-01. WORK PERFORMED IAW ASA EC/TX REO 601R-52-11-513.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,826 hrs · 10,685 cycles

JOB 8775921 OPERATION 155 FS 621 FLOOR SUPPORT ANGLE ON LT SIDE AT LBL 36 HAS A 1" CRACK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 12,826 hrs · 10,685 cycles

JOB 8775921 OPERATION 153 FLOOR SUPPORT BEAM LBL 27 HAS MINOR CORROSION NUTPLATES FROM FS 621 TO FS 574. SUP 9/11/2008 - AFTER FURTHER INVESTIGATION FOUND ALL CORROSION N LBL 27, FS 574-621 AROUND NUTPLATES TO BE WITHIN REPAIRABLE LIMITS EXCEPT 1 AREA AT FS 615. BLENDED ALL OTHER AREAS TO REMOVED CORROSION. APPLIED ALODINE, PRIME AND PAINT. ALL WORK PERFORMED IAW REO 601R-53-00-005. REPLACEMENT OF AFT FITTING AT LBL 27 FS 605-621 DUE TO DAMAGE BEYOND REAPAIRABLE LIMITS. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,826 hrs · 10,685 cycles

JOB 8775921 OPERATION 166 FOUND INBD AND OTBD CLIP ANGLES AT FS 280 AND LBL 9 CRACKED. SUP - REMOVED INBD AND OTBD CLIPS AT FS 280 IAW CRJ 200 SRM 51-42-21 AND 51-42-06. INSTALLED NEW SERVICEABLE CLIP ON OTBD SIDE OF LBL 9 IAW CRJ 200 SRM 51-42-21. CLIP ANGLE ON INBD SIDE OF LBL 9 REQURIES INSTALL. INSTALLED NEW ANGLE ON INBD SIDE OF LBL 9 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,826 hrs · 10,685 cycles

JOB 8775921 OPERATION 43 LT AND RT FS 621 TO 625 OBLIQUE ANGLES IN THE AFT EQUIPMENT BAY ARE CRACKED 1 IN LONG IN AFT RADIUS. REMOVED CRACKED LT AND RT FS 621.00 TO 625.00, OBLIQUE ANGLES AND INSTALLED NEW SERVICEABLE LT AND RT OBLIQUE ANGLES IAW CRJ 200 SRM 51-42-21. SUP CLOSED 9/11/08. (K)

Part: LIGHT — BROKEN (CABIN) · airframe 12,531 hrs · 10,417 cycles

EMERGENCY EXIT LIGHT ASSY AT CABIN ENTRY BULKHEAD BROKEN AND HANGING BY WIRES. CHANGED EMERGENCY PATH LIGHT ASSY AT THE ENTRY BULKHEAD IAW CRJ 200 AMM 33-51-01. LIGHT OPS CHECK GOOD. (S)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,466 hrs · 10,357 cycles

AFT TWO EMERGENCY LIGHTS IN THE CEILING INOP RELAMPED AFT TWO EMERGENCY LIGHTS IA 33-51-16.

Part: SEAL — OUT OF POSITION (PAX DOOR) · airframe 11,787 hrs · 9,801 cycles

CLIMBING OUT THRU 17000 MCD SEAL BLEW OUT AND CABIN PRESSURIZATION WAS LOST. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DESCENT PERFORMED TO A LOWER ALTITUDE. REMOVED AND REPLACED PASSENGER DOOR SEAL IAW CRJ200 AMM 52-11-10, OPS CHECK GOOD. SDR CLOSED.

Part: FLAP — FAILED (WING) · airframe 11,592 hrs · 9,644 cycles

FLAP FAIL AT ZERO ON APPROACH. EMERGENCY EQUIPMENT ON STANDBY.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 9,935 hrs · 8,307 cycles

F/A'S FLASHLIGHT IS INOP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 9,643 hrs · 8,092 cycles

CAPT'S FLASHLIGHT INOP.

Part: LANDING GEAR — INOPERATIVE (NOSE) · airframe 9,583 hrs · 8,048 cycles

AFTER T/O NOSE GEAR WOULD NOT COME UP AFTER SELECTED IN THE UP POSITION, NOSE WHEEL STEERING INOP ON LANDING, A/C RETURNED TO MCN AFTER TAKEOFF. EMERGENCY DECLARED.

Part: CIRCUIT BREAKER — UNKNOWN (NLG STEERING) · airframe 8,990 hrs · 7,604 cycles

RECEIVED -STEERING INOP- CAUTION MESSAGE AFTER GEAR RETRACTION. RAN QRH, LANDED WITH NWS OFF. RESET BREAKERS ON GROUND AND NWS RESET. TAXIED TO GATE AS NORMAL. EMERGENCY DECLARD. FLTS 4423, 4430 CX.

Part: SIGN — INOPERATIVE (CABIN) · airframe 8,638 hrs · 7,342 cycles

SERVICE DOOR EMERGENCY EXIT SIGN HAS BULBS BURNT OUT.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 8,355 hrs · 7,120 cycles

FS 484 CLIP O/B SIDE OF LBL 27 CRACKED.

Part: BEAM — CRACKED · airframe 8,355 hrs · 7,120 cycles

LEFT LOWER O/B ENGINE BEAM CRACKED. REPAIRED IAW ALL SRMS.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,355 hrs · 7,120 cycles

APU LINEAR ACTUATOR INTERCOSTAL CRACKED. UPON FURTHER INVESTIGATION FOUND TO BE A DEEP NICK NOT CRACKED. REMOVED DEEP NICK PER PROCEDURE COVERED IN CRJ SRM 51-12-00 ALLOWABLE DAMAGE AND TREATMENT OF NICKS & SCRATCHES. REMOVAL OF DAMAGE DOES NOT DECREASE THE THICKNESS OR CROSS-SECTION AREA BY 10%. DAMAGE REMOVED WAS ON THE EDGE AND MINIMAL METAL WAS REMOVED BY A ROTARY FILE TO REMOVE THE NICK. MH715. REQUIRES LPI TO INSURE THAT DAMAGE WAS REMOVED. REF W/C 400 OF THIS WORK ORDER FOR LPI. MH715 11-02-06 APPLIED ALODINE, PRIMED, TOPCOATED IAW CRJ SRM 51-25-16. MH715 11-02-06. (CLOSED 11/06/06)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,355 hrs · 7,120 cycles

FS 484 INTERCOSTAL CRACKED AT I/B SIDE OF LBL 36.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,355 hrs · 7,120 cycles

FS 484 INTERCOSTAL CRACKED AT I/B SIDE OF RBL 36.

Part: FRAME — CRACKED (BS 640) · airframe 8,355 hrs · 7,120 cycles

RIGHT 640.00 FRAME DOUBLER AT BL 45 CRACKED. REPAIRED IAW ALL APPROPRIATE REPAIR MANUALS.

Part: BEAM — CRACKED (ENGINE MOUNT) · airframe 8,355 hrs · 7,120 cycles

LEFT AND RIGHT LWR OUTBOARD ENGINE BEAM CRACKED. REPAIRED IAW ALL SRMS.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 8,355 hrs · 7,120 cycles

AFT PAX DOOR ANCHOR FITTING CRACKED; REFER TO DML 065626. REMOVED PAX DOOR AFT ANCHOR FITTING AS REQUIRED IAW CRJ 200 AMM 52-11-17. OK TO INSTALL NEW ANCHOR FITTING. INSTALLED NEW ANCHOR FITTING FOR AFT OF PAX DOOR AS REQUIRED IAW CRJ 200 AMM 52-11-17. INSTALLED SERVICEABLE P/N 601R38074-5, PO ASA070. (CLOSED 11/06/06)

Part: RIB — CRACKED (RT WING) · airframe 8,355 hrs · 7,120 cycles

RIGHT BATTERY RIB CRACKED. REPAIRED IAW ALL REPAIR MANUALS.

Part: ANGLE — CRACKED (BS 625) · airframe 8,355 hrs · 7,120 cycles

RIGHT AND LEFT 625.00 OBLIQUE ANGLES CRACKED. REMOVED RT & LT CRACKED OBLIQUE ANGLES. INSTALLED NEW RT AND LT OBLIQUE ANGLES PN 601-35012-51 & PN 601-35012-52 IAW CRJ 200 SRM 51-42-21. (CLOSED 11/01/06)

Part: ANCHOR FITTING — CRACKED (ASD) · airframe 8,316 hrs · 7,090 cycles

AFT ASD ANCHOR FITTING CRACKED. CRACK IS .547 INCH.

Part: ATTACH FITTING — CRACKED (AIR STAIR DOOR) · airframe 7,998 hrs · 6,840 cycles

AFT ASD ANCHOR FITTING CRACKED. REFER TO REO 601R-52-11-1091. RE INSPECT EVERY 50 HRS, NOT TO EXCEED 500 HRS. PREVIOUS DAMAGE WAS .5 INCH, FOUND TO HAVE MIGRATED TO .520. IF IT IS FOUND TO MIGRATE PAST THIS DIMENSION, CALL BOMBARDIER IMMEDIATELY.

Part: ANCHOR FITTING — CRACKED (AFT ASD) · airframe 7,973 hrs · 6,814 cycles

AFT ASD ANCHOR FITTING CRACKED.

Part: ANCHOR FITTING — CRACKED (AIRSTAIRS) · airframe 7,494 hrs · 6,415 cycles

ASD AFT COUNTER BALANCE ANCHOR BRACKET CRACKED.

Part: PLACARD — UNKNOWN (AIRSTAIRS) · airframe 7,494 hrs · 6,415 cycles

ASD EXIT PLACARD NEEDS REPLACED.

Part: TIRE — CUT (LT MLG) · airframe 8,324 hrs · 7,095 cycles

LT IB MAIN TIRE CUT, FLT 4229 DEL 17 MINS, NC.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING A GROUND INSPECTION IN CAE, THE FORWARD LEFT EXTERNAL EMERGENCY LIGHT ASSEMBLY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD LEFT EXTERNAL EMERGENCY LIGHT ASSEMBLY LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)