N867AS

Part: SKIN — DENTED (BS 364-394) · airframe 36,471 hrs · 34,291 cycles

REF BOMBARDIER TUCSON AIR CENTER JOB# 2746375 5 DENTS ON LH FUSELAGE SKIN BETWEEN FS 364.00 AND 394.00, 14L-17L. REPAIRED IAW STS EA 48-2018-074 DATED 11/02/2018.

Part: SKIN — DENTED (RT WING SPOILER) · airframe 36,471 hrs · 34,291 cycles

REF BOMBARDIER TUCSON AIR CENTER JOB# 2746375 DENT ON TOP OUTBOARD SURFACE OF RH FLIGHT SPOILER. REPAIRED IAW EA 32-2018-222 DATED 11/05/2018.

Part: SKIN — DENTED (BS 220-280) · airframe 36,470 hrs · 34,291 cycles

REF BOMBARDIER TUCSON AIR CENTER JOB# 2746375 DENT ON LH FUSELAGE SKIN AFT OF PITOT PROBE. REPAIRED IAW WITH STS EA 30-2018-224 DATED 11/01/2018.

Part: SKIN — DAMAGED (BS 349) · airframe 36,471 hrs · 34,291 cycles

FOUND A BLEND OUT AREA ON LH FUSELAGE SKIN FWD OF FS 349.00 BETWEEN STA 18L-19L. REPAIRED PER STS EA 30-2018-227 REV -- DATED 10/25/2018

Part: FLAP — DAMAGED (LT WING) · airframe 36,028 hrs · 33,774 cycles

LEFT WING INBOARD FLAP DAMAGED ON T/E. REPLACED LEFT INBOARD FLAP ASSY IAW AMM 27-54-01-400-801.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,137 hrs · 32,745 cycles

CORROSION DAMAGE FOUND ALONG LT FLOOR SILL BETWEEN FS409.00+128-559.00. BLEND DAMAGE LT FLOOR SILL BETWEEN FS409.00+128-559.00 IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF SILL IAW BSC NDTM .43 MIN REMAINING THK OF PANEL/ANGLE PAD-UP IS .012"/.078"/.075". ORIGINAL IS .055"/.080"/.080". SOME BLENDED AREAS OF FLOOR SILL PANEL ARE OUT OF ALLOWABLE LIMITS IAW REO 601R-53-41-666. FABRICATED, LOCATED AND DRILLED REPAIR DOUBLERS FOR LT FLOOR SILL IAW REO 601R-53-41-2132 P1 DETAIL B. CUT OUT DAMAGE ON LT FLOOR SILL IAW REO 601R-53-41-2132 P1 DETAIL B. PERFORMED EDDY CURRENT INSPECTION OF SILL IAW NDTM PT 1 51-20-06. NO INDICATIONS NOTED AT THIS TIME. CUT OUT DAMAGE ON LT FLOOR SILL FS439, 449.85 AND 461 IAW REO 601R-53-41-2132 P1 DETAIL A. PERFORMED EDDY CURRENT INSPECTION OF SILL IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME. TRIMMED FUSELAGE FRAMES FS439, 461 AND 484 LT SIDE IAW REO 601R-53-41-2132.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,137 hrs · 32,745 cycles

CORROSION DAMAGE FOUND ALONG RT FLOOR SILL BETWEEN FS409.00+128-559.00. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF SILL IAW BSC NDTM .43 MIN REMAINING THK OF PANEL/ANGLE PAD-UP IS.020"/.043". ORIGINAL IS .055"/.080". REMOVED IS .035:/.018"?.037" SOME REPAIRS OF FLOOR SILL PANEL ARE OUT OF ALLOWABLE LIMITS IAW REO 601R-53-41-666. PERFORMED EDDY CURRENT INSPECTION OF SILL IAW NDTM PT 1 51-20-06. CRACK INDICATION NOTED IN FLOOR SILL PANEL FS484. CORROSION REMOVED BEYOND LIMITS OF GRE 601R-53-41-666 ON RT FLOOR SILL FS424,449,461,484 AND 529. FS484 ALSO CRACKED. COMPLIED WITH REO 601R-53-41-2129 P4 DATED 11/30/2016.

Part: CROSSBEAM — CRACKED (BS 484) · airframe 35,137 hrs · 32,745 cycles

DURING C CHECK, FOUND CROSSBEAM AT BS 484 BETWEEN LBL 27 & THE LT FLOOR SILL HAS TWO CRACKED ANGLES. REMOVED PREVIOUSLY INSTALLED REPAIR ANGLES. FABRICATED NEW REPAIR ANGLES. PERFORMED NDT. NO DEFECTS NOTED AT THIS TIME. DRILLED UP AND INSTALLED NEW ANGLES PER BOMBARDIER REO 601R-53-41-2126 REV A AND EXPRESSJET EC/TCREO 601R-53-41-2126 REV 0.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 35,137 hrs · 32,745 cycles

RIGHT SIDE SEAT TRACK BETWEEN BS 364 TO 409 HAS CORROSION. REMOVED AND INSTALLED A NEW FABRICATED SEAT TRACK IAW REO 601R-53-00-651 REV 0, EC/TC REO 601R-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 35,137 hrs · 32,745 cycles

LEFT SIDE SEAT TRACK BETWEEN BS 409+112 TO 449.85 HAS CORROSION. REMOVED AND INSTALLED A NEW FABRICATED SEAT TRACK IAW REO 601R-53-00-651 REV 0, EC/TC REO 601R-53-00-651, AMM 53-01-11-000-802 AND 53-01-11-400-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 35,137 hrs · 32,745 cycles

DURING C CHECK, FOUND THE SEAT TRACK AT BS 559+80 TO 559+96, RBL27 CORRODED. REMOVED, FABRICATED, AND INSTALLED A NEW SEAT TRACK IAW REO 601R-53-00-485, EC/TC REO 601R-53-00-485, AND AMM 53-00-49-000-801/53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 35,137 hrs · 32,745 cycles

SHORT SEAT TRACK BS 559+96 TO 559+112, LBL 9 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485, EC/TC REO 601R-53-00-485, AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 644-559) · airframe 35,137 hrs · 32,745 cycles

RIGHT SIDE SEAT TRACK BETWEEN BS 544 TO 559+80 HAS CORROSION. REMOVED AND INSTALLED A NEW FABRICATED SEAT TRACK IAW REO 601R-53-00-651 REV 0, EC/TC REO 601R-53-00-651, AMM 53-01-11-000-802 AND 53-01-11-400-801.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 35,137 hrs · 32,745 cycles

RT SIDE SEAT TRACK BETWEEN BS 409+112 TO 449.85 HAS CORROSION. REMOVED AND INSTALLED A NEW FABRICATED SEAT TRACK IAW REO 601R-53-00-651 REV 0, EC/TC REO 601R-53-00-651, AMM 53-01-11-000-802 AND 53-01-11-400-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 35,137 hrs · 32,745 cycles

DURING C CHECK, FOUND THE SEAT TRACK AT BS 559+80 TO 559+96, LBL9 CORRODED. REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 601R-53-00-485, EC/TC REO 601R-53-00-485, & AMM 53-00-49-000-801/53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 35,137 hrs · 32,745 cycles

DURING C CHECK, FOUND THE SEAT TRACK AT BS 559+80 TO 559+96, LBL 27 CORRODED. REMOVED, FABRICATED, AND INSTALLED A NEW SEAT TRACK IAW REO 601R-53-00-485, EC/TC REO 601R-53-00-485, AND AMM 53-00-49-000-801/53-00-49-400-801.

Part: FLOORBEAM — CRACKED (BS 461) · airframe 35,137 hrs · 32,745 cycles

DURING C CHECK, FOUND THE FLOORBEAM BS 461 BETWEEN LBL 9 AND LBL 18 CRACKED. CUT AWAY DAMAGE AND INSTALLED SECONDARY STRUCTURE & DOUBLER IAW EC/TC REO 601R-53-41-2128 REV A.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 35,137 hrs · 32,745 cycles

LEFT SIDE SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 6017-53-00-651 REV 0, EC/TC REO 6017-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 35,137 hrs · 32,745 cycles

RIGHT SIDE SEAT TRACK BETWEEN BS 409 TO 449.96 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-651 REV 0, ECTC REO 601R-53-00-651, AMM 53-01-000-802, AND 53-01-11-400-801.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 35,137 hrs · 32,745 cycles

RIGHT SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 6017-53-00-651 REV 0, EC/TC REO 6017-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801.

Part: SEAT TRACK — CORRODED (BS 499-590) · airframe 35,137 hrs · 32,745 cycles

LEFT SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 6017-53-00-651 REV 0, EC/TC REO 6017-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 35,137 hrs · 32,745 cycles

LEFT SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 6017-53-00-651 REV 0, EC/TC REO 6017-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 35,137 hrs · 32,745 cycles

LEFT SIDE SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 6017-53-00-651 REV 0, EC/TC REO 6017-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 35,137 hrs · 32,745 cycles

LEFT SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 6017-53-00-651 REV 0, EC/TC REO 6017-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801.

Part: RISER — CRACKED (PAX DOOR) · airframe 35,137 hrs · 32,745 cycles

DURING C CHECK, FOUND PAX DOOR AFT GAS STRUT TOP ATTACH STRUCTURE LOOSE AND CRACKED ON STRIP SKIN. TRIMMED ALL DAMAGE FOUND AND INSTALLED SECONDARY STRUCTURE/DOUBLERS PER EC/TC REO 601R52-11-2367 REV 0,EC/TC REO 601R52-11-2366 REV 0, AND EC/TC REO 601R52-11-702 REV D.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 34,565 hrs · 32,081 cycles

FA FLASHLIGHT INOPERATIVE. REPLACED THE BATTERIES AND OPS CHECKED GOOD IAW AMM 25-61-04. ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 32,236 hrs · 29,564 cycles

NR 6 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 31,974 hrs · 29,266 cycles

EXTERNAL EMERGENCY LIGHT NR 6 INOPERATIVE. RE-LAMPED IAW AMM 33-51-21. SYS OPS CHECKED GOOD. NO FURTHER ACTION.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 31,108 hrs · 28,406 cycles

LT WING LOWER WING PLANK ACCESS HOLE LAND AT FUEL PANEL 540DB CORRODED /PITTED THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED AND COMPLIED WITH GREO 601R-57-21-030. COMPLIED WITH REO 601R-57-21-030 REV L. DATED FEB.5,2014.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 31,108 hrs · 28,406 cycles

LT WING LOWER WING PLANK ACCESS HOLE LAND AT FUEL PANEL 510AB CORRODED /PITTED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED AND COMPLIED WITH GREO 601R-57-21-030. COMPLIED WITH REO 601R-57-21-030, REV C, DATED FEB 5, 2014.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 31,108 hrs · 28,406 cycles

FS 280, WEB CORRODED AT FLOOR SUPPORT FWD ANGLE BETWEEN LBL9 AND RBL9. COMPLIED WITH ECTC 601R-53-11-926 01 FABRCATED REPAIR PARTS. REMOVED LT AND RT, 4 ATTACH CLIPS AT FS280 -3 WEB FILLER, -5 REPAIR ANGLE, AND -13-5 SHIM, AILERON PULLEY BRACKETS REMOVED WORK DONE IAW REO 601R-53-11926, REV 8. INSTALLED -3 WEB FILLER , 5 REPAIR ANGLE AND -13 SHIM IAW ECTC REO 601R-53-11-26 01. COMPLIED WITH ECTC 601R-53-11-926-01.

Part: SKIN — CORRODED (SERVICE DOOR) · airframe 31,108 hrs · 28,406 cycles

SERVICE DOOR LOWER INNER SKIN HAS CORROSION SEVERAL PLACES. BLENDED CORROSION IAW SRM 51-12-00-00.

Part: ANGLE — CORRODED (BS 320-345) · airframe 31,108 hrs · 28,406 cycles

PAX DOOR LOWER SILL UPPER ANGLE CORRODED AT FS 320.00 AND FS345.00. REPAIRED IAW SRM 51-42-20-00 & DWG 601R-31527. BLENDED CORRODED AREA IAW SRM 51-12-00-00. AFTER FURTHER INVESTIGATION ANGLE REQUIRES REPLACEMENT BECAUSE ITS MORE THAN 30 PERCENT OF LENGTH, INBD SIDE, IAW SRM TR 53-27. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED PAX DOOR LWR SILL UPPER ANGLE FS 320.00 TO 345.00 IAW SRM 51-42-20-00. INSTALL NEW SERVICEABLE PAX DOOR LWR SILL UPPER ANGLE IAW DWG 601R31527 & SRM 51-42-20-00. COMPLETED INSTALLATION OF NEW SERVICEABLE PAX DOOR LWR SILL UPPER ANGLE IAW DWG 601R31527 & SRM 51-42-20-00.

Part: HINGE — GOUGED (PAX DOOR) · airframe 31,108 hrs · 28,406 cycles

PAX DOOR HINGE LUGS ARE GOUGED. REPAIRED IAW REO 601R-52-11-1347.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,108 hrs · 28,406 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT MOTOR ASSIST WHEEL PULLEY AREA. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REPAIRED IAW REO 601R-57-11-513, REV A DATED MAR 5, 2009 DWG 601R-31702. COMPLIED WITH EC/TC REO 601R-52-11-513.

Part: BULKHEAD — GOUGED (BS 621) · airframe 31,108 hrs · 28,406 cycles

F/S 621 AFT PRESSURE BULKHEAD HAS 2 NICKS BETWEEN LBL 18 - LBL 27. REMOVED DAMAGE IAW SRM 51-12-00-00. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH REO 601R-53-61-2155, REV A DATED AUG 13,2013. COMPLIED WITH EC/TC REO 601R-53-61-2155 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-2155, REV A.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 31,108 hrs · 28,406 cycles

AFT FLT DECK SUPPORT ANGLE AT BS 280 IS CORRODED. REMOVED COCKPIT FLOORBEAM ANGLE. INSTALLED NEW COCKPIT FLOORBEAM ANGLE IAW SRM 51-42-06. L

Part: SEAT TRACK — CORRODED (BS 394) · airframe 31,108 hrs · 28,406 cycles

CORRODED SEAT TRACK BS 394, RBL 9 BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394) · airframe 31,108 hrs · 28,406 cycles

CORRODED SEAT TRACK BS 394, LBL 9 BEYOND LIMITS. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: FRAME — CORRODED (BS 319) · airframe 31,108 hrs · 28,406 cycles

CORROSION AT LOWER FRAME SECTION OF BS 319.7 BETWEEN STR26-27L. REMOVED THE CORROSION IAW SRM 51-21-06. REPAIRED IAW EA 32-2014-143.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 31,108 hrs · 28,406 cycles

CORRODED SEAT TRACK BS 364, RBL 9 BEYOND LIMITS. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: CARGO TRACK — CRACKED (BS 598-605) · airframe 31,107 hrs · 28,405 cycles

CRACKED CARGO TRACK AT BS 598-605. BETWEEN LBL 42.9- 27. REMOVED AND REPLACED IAW SRM 51-42-06, 51-40-11, AND DWG 601R35031, REV AG.

Part: STRUCTURE — CORRODED (BS 559) · airframe 31,108 hrs · 28,406 cycles

CORROSION FOUND ALONG NUTPLATE HOLES OF RT SILL, RBL 42.90, BS 559 - 559+48. R & R RECEPTICLE L/W OTBD FLAP 2ND FROM OTBD PANEL OTBD POSIITON IAW SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 31,108 hrs · 28,406 cycles

FLOOR SUPPORT BS 574-621, LBL 27 CORRODED. REMOVED CORROSION IAW SRM 51-21-06. REPAIRED IAW REO 601R-53-00-005.

Part: STRAP — CORRODED · airframe 31,108 hrs · 28,406 cycles

FOUND FLOORBEAM CAP CORRODED SEVERELY AT BS 557 BETWEEN BL 27 AND BL 42.9. REMOVED CORRODED STRAP AND INSTALLED NEW STRAP IAW SRM 51-42-06 AND DWG 601R31025.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 31,108 hrs · 28,406 cycles

FOUND SERVICE DOOR SILL TO HAVE MULTIPLE CORROSION ALONG SILL. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED CORRODED SERVICE DOOR SILL IAW SRM 51-42-21, INSTALLED NEW SERVICEABLE DOOR SILL, LWR UPPER ANGLE IAW DWG 601R-38303 & SRM 51-42-01. REMOVED LWR DOOR STOP FITTING FWD & AFT IAW SRM 51-41-02. INSTALLED DOOR STOP FITTINGS FWD & AFT IAW AMM 51-41-02 & ADJ TEST OPS CHECK GOOD. REMOVED SERVICE DOOR SILL UPPER ANGLE IAW SRM 51-41-02 & 51-42-21. INSTALLED NEW SERVICEABLE DOOR SILL, LWR, UPPER ANGLE IAW DWG 601R38303 & SRM 51-42-21. LOCATED & DRILLED NEW SERVICEABLE LWR SILL, UPPER ANGLE, FOR SERVICE DOOR IAW DWG 601R38303.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 31,108 hrs · 28,406 cycles

FLOOR SUPPORT CORRODED BS 574- 621. REPAIRED IAW REO 601R-53-00-526.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 31,108 hrs · 28,406 cycles

FLOOR SUPPORT BS 557+80 RBL 9 CORRODED. REMOVED CORROSION IAW SRM 51-21-06. REPAIRED IAW REO 601R-53-00-005.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 31,107 hrs · 28,405 cycles

CORROSION FOUND ALONG FLOOR SUPPORT LBL42.9, BS 559-559+80. REPAIRED IAW REO 601R-53-00-526.

Part: SEAT TRACK — CORRODED (BS 557) · airframe 31,107 hrs · 28,405 cycles

SEAT TRACK, CORRODED BEYOND LIMITS AT BS 557, RBL 9 REMOVED AND REPLACED IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802, AND SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,107 hrs · 28,405 cycles

SEAT TRACK CORRODED BEYOND LIMITS AT BS 559, LBL 9.00. REMOVED AND REPLACED IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802, AND SRM 51-40-11.

Part: CONNECTOR — MISSING (EMERGENCY LIGHT) · airframe 31,108 hrs · 28,406 cycles

FWD WARDROBE UNIT EMERGENCY EXIT FLOOR LIGHT HAS TWO QUICK DISCONNECT CONNECTORS MISSING. INSTALLED NEW QUICK DISCONNECTORS ON FWD WARDROBE UNIT ON EMERGENCY EXIT FLOOR LIGHT IAW ESPM 20-16-00. COMPLIED WITH OPS TEST OF EMERGENCY LIGHT ON FWD WARDROBE IAW AMM 33-51-00-710-801, OPS TEST GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,108 hrs · 28,406 cycles

EXTERIOR EMERGENCY LIGHTS AT PAX DOOR AND SERVICE DOOR NOT WORKING. REMOVED BAD BATTERY PACK IAW AMM 33-51-04-000-801. INSTALLED A NEW BATTERY PACK IAW AMM 33-51-04-400-801 AIPC 33-51-04. COMPLIED WITH OPS CHECK OF BATTERY PACK NR 1 IAW AMM 33-51-04-740-801. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,108 hrs · 28,406 cycles

INTERIOR EMERGENCY LIGHT ON GALLEY NEXT TO SERVICE DOOR NOT WORKING. REMOVED BAD BATTERY PACK IAW AMM 33-51-04-000-801. INSTALLED A NEW BATTERY PACK IAW AMM 33-51-04-400-801 AIPC 33-51-04. COMPLIED WITH OPS CHECK OF BATTERY PACK NR 1 IAW AMM 33-51-04-740-801 OPS CHECK GOOD. R & R BATTERY PACK, SN 6431 IAW AMM 33-51-04-000/400-801. OPS CHECK GOOD, IPC 33-51-04, FIG 1, ITEM NR 17.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,353 hrs · 27,677 cycles

FOUND MULTIPLE EMERGENCY LIGHTS OUT. REMOVED DEFECTIVE EMERGENCY NR 4 BATTERY PACK AND INSTALLED SERVICEABLE IAW AMM 33-51-04. CHECKED GOOD AT THIS TIME.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,052 hrs · 27,390 cycles

RT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-51-21. SYSTEM OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,291 hrs · 25,579 cycles

NR 3 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED LAMPS. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: ANGLE — CRACKED (BS 625-640) · airframe 27,415 hrs · 24,668 cycles

SKIN TIE-IN ANGLE ESB WL 119 BETWEEN FS 625 AND 640 LBL 42 (UPPER) IS CRACKED IN AFT END RADIUS. LOCATED & DRILLED NEW ESB ANGLE IAW SRM 51-40-11. INSTALLED ESB ANGLE IAW SRM 51-42-21.

Part: BULKHEAD — CRACKED (BS 621) · airframe 27,415 hrs · 24,668 cycles

FS 621 BULKHEAD HAS MULTIPLE INDICATIONS FROM NDT AT LBL 36.2 WL 80, LBL 27.5 WL 80-111, LBL 18.0 WL 97-134.5, LBL 9.50 WL 82-134.5, BL 0 WL 83-134.5, RBL 9.50 WL 97.134.5, RBL 18.0 WL 100.134.5 AND RBL 27.5 WL 100-116. INDICATIONS ARE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-53-61-4712. SDR CLOSED.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 27,415 hrs · 24,668 cycles

LT FLOOR SILL PANELS HAVE CORROSION AROUND NUTPLATE HOLES BETWEEN FS 409+128 AND FS 559, BL 36.0 AND BL 45.0 AT WL 73.00. INSTALLED MYLAR TAPE TO LT FLOOR SILL BETWEEN FS 409.128 AND FS 559, BL 2500 TO BL 45.0 AT WL 73.0 IAW SRM 51-27-19. SDR CLOSED.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 27,415 hrs · 24,668 cycles

RT FLOOR PANELS AND FLOOR SUPPORT HAVE CORROSION BETWEEN FS 409+128 AND FS 559, BL 36.0 AND BL 45.0 AT WL 73.0. COMPLIED WITH REO 601R-53-41-1640.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 27,401 hrs · 24,652 cycles

FS 589 FLOORBEAM CAP STRIP CORRODED FROM RBL 27 TO RBL 36. OUT OF LIMITS IAW CRJ 200 53-61-43. R & R FS 589.00 FLOORBEAM CAP AT RBL 27 WITH NEW IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 27,407 hrs · 24,660 cycles

CARGO FLOOR SUPPORT RBL 36 AT FS 559+96 TO 559+112 HAS AREAS OF CORROSION. REMOVED FLOOR SUPPORT AT RBL 36 FS 559+9 TO FS 559+112 IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE RT FLOOR SUPPORT IAW SNIEO 601R31133 S03 AND REO 601R-53-51-204, REV A.

Part: SEAT TRACK — CORRODED (BS 621) · airframe 27,415 hrs · 24,668 cycles

CARGO FLOOR SEAT TRACK AT FS 621, LBL 9 IS CORRODED. REMOVED SEAT TRACK AT FS 621 LBL 9 IAW SRM 51-41-02. APPLIED RTV157 TO NEW SEAT TRACK, AND INSTALLED IAW AMM 20-21-00-910-801.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 27,407 hrs · 24,660 cycles

FLOOR SUPPORT BEAM CAP CORRODED AROUND NUTPLATE HOLES BETWEEN FS 559+96 & FS 559+112 RBL 9. REPAIRED FLOOR SUPPORT BEAM CAP BETWEEN FS 559+96 AND FS 559+112 RBL 9 IAW REO 601R-53-00-005, REV B. SDR CLOSED.

Part: SILL — CORRODED (BS 574-621) · airframe 27,415 hrs · 24,668 cycles

CARGO DOOR SILL HAS AREAS OF CORROSION FROM FS 574 TO FS 621. REMOVED CORRODED CARGO FLOOR LANDING PLATE IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW CARGO FLOOR LANDING PLATE IAW SRM 51-42-06. SDR CLOSED.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 27,415 hrs · 24,668 cycles

FLOOR SUPPORT CORRODED AROUND NUTPLATE HOLES BETWEEN FS 574 AND 621 LBL 9. R & R FLOOR SUPPORT IAW SRM 51-42-06, 51-40-11-00 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 603-621) · airframe 27,407 hrs · 24,660 cycles

CARGO FLOOR SUPPORT RBL 36 FROM FS 603 TO FS 615 HAS AREAS OF CORROSION. REMOVED CORROSION FROM RT FLOOR SUPPORT FROM FS 603 TO 621 RBL 36 IAW SRM 51-21-06 APPROX .003. MATERIAL REMOVED FURTHER DISPOSITION REQ COMPLIED WITH REO 601R-53-61-4717.

Part: FLOOR SUPPORT — CORRODED (BS 589-605) · airframe 27,407 hrs · 24,660 cycles

FLOOR SUPPORT CAP CORRODED AROUND NUTPLATE HOLES BETWEEN FS 589 AND FS 605 RBL 27. REMOVED CORRODED FLOOR SUPPORT CAP AT RBL 27 FS 589 THROUGH FS 605 IAW SRM 51-42-06, 51-42-21. FIT, DRILLED UP FLOOR SUPPORT CAP AT RBL 27, FS 589 THROUGH FS 605, IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE CAP ANGLE IAW REO 601R-53-61-4718.

Part: STIFFENER — CRACKED (BS 621 BULKHEAD) · airframe 27,407 hrs · 24,660 cycles

FS 621 PRESSURE BULKHEAD VERTICAL STIFFENER RBL 36.20 JUST FWD OF THE TRANSVERSE BEAM HAS SIGNS OF A CRACK IN THE RADIUS APPROX 2" LONG. REPAIRED IAW REO 601R-53-61-4714, REV A. SDR CLOSED.

Part: CHANNEL — CRACKED (BS 409) · airframe 27,407 hrs · 24,660 cycles

INDICATION NOTED AT FS 409+128 WL 69.00 RBL 18 OTBD CHANNEL IN RADIUS 60 PERCENT FULL SCREEN HEIGHT APPROX .10" LENGTH VERTICALLY. FAILED NDT. R & R FS 409+128, RBL 18 INBD & OTBD POST ASSY IAW SRM 51-42-06 & REO 601R-53-41-889, REV A. SDR CLOSED.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 27,407 hrs · 24,660 cycles

SEVEN CARGO BAY LINE ISOLATORS ON THE 621 BULKHEAD CRACKED. ALL FS 621 BULKHEAD ISOLATORS R & R WITH NEW. IAW REO 601R-53-61-4712 -SDR CLOSED.

Part: POST — CRACKED (BS 409) · airframe 27,401 hrs · 24,652 cycles

INDICATION NOTED AT FS 409+128, WL 69.00, BL 0, RT CHANNEL IN RADIUS 50 PERCENT FULL SCREEN HEIGHT APROX .100 IN LENGTH VERTICALLY. FAILED NDT. REMOVED POST AT FS 409+128, BL 0 IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW POST PN 601R32208-190 AND 601R32208-132 IAW SRM 51-40-11. INSTALLED NEW POST PN 601R32208-190A ND 601R32208-132 IAW REO 601R-53-41-887 AND SRM 51-42-06. SDR CLOSED.

Part: FUEL CONTROL — FALSE INDICATION · airframe 26,997 hrs · 24,245 cycles

SUSPECT LT WING FUEL LEAK INTO CENTER TANK. ACFT DIVERTED. EMERGENCY DECLARED. PERFORMED OPS CHECKS INCLUDING FUEL COMPUTER BITE CHACK IAW AMM 28-41-16-740-801, OPS TEST OF THE REFUEL/DEFUEL SYS IAW AMM 28-25-00-710-801. OPS TEST OF FUEL MANUAL XFLOW SYS IAW AMM 78-13-00-710-801. OPS TEST OF GRAVITY XFLOW SOV IAW AMM 28-13-16-710-801. OPS TEST OF FUEL XFER SOV IAW AMM 28-13-43-710-801. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (FIRE BOTTLE) · airframe 26,727 hrs · 23,964 cycles

CARGO BOTTLE LOW MESSAGE IN FLIGHT. ENROUTE, ACFT DIVERTED, EMERGENCY DECLARED, INSPECTED COMPARTMENT, TROUBLESHOOTING PERFORMED. SECURED CARGO BOTTLE SQUIB BACK SHELL CONNECTOR AND OPS TEST IAW AMM 26-15-00. NO FURTHER DEFECT NOTED.

Part: FLASHLIGHT — UNSERVICEABLE (COCKPIT) · airframe 25,614 hrs · 22,746 cycles

COCKPIT FLASHLIGHTS UNSERVICEABLE. INSTALLED NEW FLASHLIGHTS IAW AMM 25-60-00. ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,777 hrs · 20,696 cycles

RIGHT NR 2 EMERGENCY LIGHT INOPERATIVE. RELAMPED RT EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 23,610 hrs · 20,492 cycles

CONTINUATION OF MWC 324 CARGO COMPARTMENT FLOORBEAM HAS CORROSION LBL 27, FS 559+112 TO FS 621.0. C/W STEPS 3 AND 4 OF REO NR 601R-53-51-138. ECTC REQUIRED FOR REO 601R-53-31-138. REO 601R-53-51-138, REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NRI WORK CARD ALL RII'S HAVE BEEN ACCOMPLISHED BY TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTOR IAW GMM 3-3 PROCEDURES, PRIOR TO THE ACFT BEING RETURNED TO SERVICE. PERFORMED AND FOUND TO BE SATIFACTORY 12/18/10" (CLOSED)

Part: SUPPORT — CRACKED (APU BAY) · airframe 23,610 hrs · 20,492 cycles

APU SUPPORT STRUCTURE AT FS 640.00, RT STG 24 SUPPORT BRACE UPPER OTBD/ CLIP CRACKED. REMOVED THE CRACKED FS 640, BROKEN CLIP IAW THE SRM 51-42-13. NEW CLIP REQUIRES LOCATION AND INSTALL IAW SRM 51-42-13. LOCATED A NEW CLIP TO THE STRUCTURE OF THE ACFT. INSTALLED THE NEW CLIP IAW SRM 51-42-13, PN 601-97060-2. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 23,610 hrs · 20,492 cycles

CARGO COMPARTMENT FLOORBEAM HAS CORROSION LBL 27, FS 559.0+112 TO FS 621.0. REMOVED CORROSION FROM FLOORBEAM LBL 27 AT STA 574-621 AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06, 53-61-43 & 53-00-00. 50 PERCENT MAT'L LOSS AT SEVERAL LOCATIONS. R & R FLOORBEAM IAW SRM 51-40-11, 51-42-21, 51-42-22, 51-42-34, 51-45-0, 51-25-06, 51-21-11, & 51-25-16 & REO 601R-53-61-3778 & 51-42-10. REPAIRED FLOORBEAM IAW REO 601R-53-51-138.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 23,610 hrs · 20,492 cycles

RT CABIN FLOOR SUPPORT STRUCTURE CORRODED AT FS 349.00, RBL 36. REMOVED LIGHT CORROSION FROM RT CABIN FLOOR SUPPORT STRUCTURE AT FS 349.00 RBL 36 IAW SRM 51-21-06, STEP 3. .004" OF MATERIAL REMOVED. TREATED AREA IAW 52-21-11 AND APPLIED PRIMER AND PAINT IAW SRM 51-25-00.

Part: FRAME — CORRODED (BS 319.7) · airframe 23,610 hrs · 20,492 cycles

FUSELAGE BELLY FRAME AT FS 319.7 HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-21-06. REMOVED APPROX .003 MATERIAL. REMOVAL WITHIN LIMITS. MINOR REPAIR IAW SOP 5702.

Part: FRAME — CORRODED (BS 349) · airframe 23,610 hrs · 20,492 cycles

FS 349.00 FRAME HAS MODERATE CORROSION ON FLANGE BETWEEN STR 26L AND 26R. MEASURES APPROX .007" DEEP. REMOVED MODERATE CORROSION IAW SRM 51-21-06. REMOVED APPROX .005. REMOVAL WITHIN LIMITS. TREATED, PRIMED & PAINTED REPAIR AREA IAW SRM 51-21-06. MINOR REPAIR IAW SOP 5702.

Part: FRAME — CORRODED (BS 364) · airframe 23,610 hrs · 20,492 cycles

FS 364.00 FRAME HAS MODERATE CORROSION ON FLANGE BETWEEN STR 26L AND 26R. MEASURES APPROX .006" DEEP. INSTALLED AVIONICS DOOR LATCH PIN PROX SWITCH MOUNTING BRACKET AND FWD CNTR LATCH FITTING IAW AMM 52-70-08-400-801 & SRM 51-41-04- & 51-42-06. REMOVED MODERATE CORROSION IAW SRM 51-21-06. REMOVED APPROX .005. REMOVAL WITHIN LIMITS. TREATED, PRIMED & PAINTED REPAIR AREA IAW SRM 51-21-06. AVIONICS COMPARTMENT DOOR WARNING SYS REQUIRES OPS CHECK. OPS TEST IS GOOD IAW AMM TASK 52-70-08-710-801.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 23,610 hrs · 20,492 cycles

INTERCOSTAL CLIP AT FS 484.00 ON TOP OF THE WING BOX BETWEEN LBL 27.00 AND LBL 36.00 IS CRACKED AT LBL 36.00. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27.0 AND BL 36.00 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 23,610 hrs · 20,492 cycles

FLOORBOARD SUPPORT STRAPS AT FS 559.00, RBL 27.00 TO RBL 36.00 AND LBL 27.00 TO 36.00 ARE CORRODED. REMOVED CORROSION FROM STRAPS IAW 51-21-06, STEP 3. TREATED, PRIMED AND TOPCOATED BOTH AREAS IAW SRM 51-21-11, 51-25-06, 51-25-16. MATERIAL THICKNESS FOR BOTH FLOORBOARD SUPPORT STRAPS IS .050 IAW SRM 53-41-43. MATERIAL LOSS FOR BOTH IS .003, REMAINING MATERIAL IS .047. BOTH STRAPS FOUND TO BE IN LIMITS IAW SRM 53-00-00. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 23,610 hrs · 20,492 cycles

INTERCOSTAL CLIP AT FS 484 ON TOP OF WING BOX BETWEEN RBL 27.00 AND RBL 36.00 IS CRACKED AT RBL 36.00. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27.0 AND BL 36.00 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 23,610 hrs · 20,492 cycles

INTERCOSTAL BETWEEN FRAMES 349 AND 364 JUST LT OF ACFT CTR LINER (STR 27) HAS MODERATE CORROSION ON FLANGE. MEASURES APPROX .006" DEEP. INSTALLED INTERCOSTAL IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 333) · airframe 23,610 hrs · 20,492 cycles

FUSELAGE BELLY FRAME AT FS 333.00 IS CORRODED IN SEVERAL AREAS. REMOVED BELLY FRAME FROM STR 23L - 23R IAW SRM 51-42-06 & 51-42-21. LOCATED, DRILLED, SEALED & INSTALLED NEW FRAME IAW SRM 51-42-06, 51-42-21. FRAME STA 333 LOWER REQ'S PAINT. TOUCHED UP REWORK AREA IAW SRM 51-25-01.

Part: INTERCOSTAL — CORRODED (BS 349-363) · airframe 23,610 hrs · 20,492 cycles

INTERCOSTAL BETWEEN FRAMES 349 AND 363 JUST RT OF ACFT CTR LINER (STR 27) HAS MODERATE CORROSION ON FLANGE MEASURES APPROX .005" DEEP. REMOVED MODERATE CORROSION IAW SRM 51-21-06. REMOVED APPROX .005. REMOVAL WITHIN LIMITS. TREATED, PRIMED AND PAINTED REPAIR AREA IAW SRM 51-21-06. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: BULKHEAD WEB — CRACKED (FUSELAGE) · airframe 23,610 hrs · 20,492 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .3" IN LENGTH 55 PERCENT FSH FAILED NDT INSP.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,610 hrs · 20,492 cycles

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

Part: SEAT TRACK — CORRODED (CABIN) · airframe 23,610 hrs · 20,492 cycles

LT AND RT FWD FLOOR SEAT TRACKS ARE CORRODED. INSTALLED A NEW SERVICEABLE LT AND RT FWD FLOOR SEAT TRACKS IAW AMM 53-01-11-400-802.

Part: BULKHEAD — CRACKED (BS 202) · airframe 23,256 hrs · 20,082 cycles

SUSPECTED CRACK IN 202 BULKHEAD. COMPLIED WITH GENERIC REPAIR IAW E/C T/C REO 601R-53-11-563. CW 7027136 9-9-10. (JOB COMPLETE) SUSPECT CRACK VERIFIED BY E/C INSP, 202 BULKHEAD IS CRACKED NDTM 51-20 -06, ITEM: 3, COMPLIED WITH GENERIC REPAIR IAW E/C T/C REO 601R-53-11-563. CW 7027136 9-9-10.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,172 hrs · 19,992 cycles

RT EXTERIOR NR4 EMERGENCY LIGHT INOP. R & R NR 4 RT EMERGENCY EXTERIOR LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. R & R NR 4 RT EMERGENCY EXTERIOR LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: CHANNEL — CRACKED (BS 409) · airframe 22,570 hrs · 19,293 cycles

WHILE PERFORMING A VISUAL INSP OF THE BULKHEAD AT FS409+128, FOUND A CRACK LOCATED AT RBL 18 OTBD U CHANNEL BY LOWER AFT RADIUS GOING FROM BOTTOM EDGE TO THE LOWEST ATTACH FASTENER HOLE. (RESOLVED ON W/O: 154834 TASKCARD: N/R-00015 ) WORK COMPLETED IAW / ITEM: 1 / REPAIRED RBL 18 VERTICAL BEAM IAW EC/TC REO 601R-53-41-056. JOB COMPLETE.

Part: OXYGEN BOTTLE — LOW (PORTABLE) · airframe 22,506 hrs · 19,215 cycles

USED PORTABLE O2 BOTTLE TO BELOW LIMITS, 2ND BOTTLE WOULD NOT WORK. SERVICED BOTH PORTABLE O2 BOTTLES IAW CMM 35-31-01. OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,248 hrs · 18,918 cycles

RT EXTERNAL CTR OVERWING EMERGENCY LIGHT INOP. R& R RT EXTERNAL CTR OVERWING EMERGENCY LIGHT. ALL WORK ACCOMPLISHED IAW AMM 33-51-21.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,303 hrs · 17,919 cycles

LEFT NR 3 EXT EMERGENCY LIGHT INOP.

Part: PLACARD — DAMAGED (ASD) · airframe 20,408 hrs · 17,043 cycles

ASD STEPS DECALS "EXIT AND OPEN" ARE DAMAGED, NEED REPLACING.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 19,829 hrs · 16,514 cycles

CONTINUATION OF JOB 8746315/154, VERTICAL BULKHEAD BEAM AT FS 409+128 LBL 18.00 LOCAL TO WL 69.00 HAS AN INDICATION NOTED APPROX 0.2 INCH LONG AND SIGNAL AMPLITUDE OF 80 PERCENT FULL SCREEN HEIGHT ON THE O/B C-CHANNEL AT RADIUS APPROX .5 INCH FROM TOP.

Part: SKIN — CORRODED (FUSELAGE) · airframe 19,829 hrs · 16,514 cycles

INDICATION NOTED AT LOWER WING PLANK ACCESS HOLE 640CB WHILE PERFORMING ASA TASK NR 000-57-600-610. INDICATION APPEARS TO BE CORROSION APPROX .040 DEEP, INDICATION IS MAPPED ON AIRCRAFT. REPAIRED LOWER WING PLANK ACCESS HOLE 640CB IAW REO 601R-57-21-1033. ASA EC/TC NEEDS C/W. C/W EC/TC REO 601R-57-21-1033 IAW REO 601R-57-21-1033.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,829 hrs · 16,514 cycles

RT FS 559.0 BULKHEAD WEB HAS AN INDICATION NOTED APPROX .3 INCHES IN LENGTH, 55 PERCENT FULL SCREEN HEIGHT OTBD OF RBL 9 WL 58.70. FAILED NDT INSPECTION. REPAIRED RT FS 559 BULKHEAD CRACKED WEB AT WEB 58.70 BY INCORP REPAIR REO 601R-53-41-821 TO BOTH LT & RT OF BULKHEAD. ALTERATION TO DOUBLER 2 AND THE SHIM IS COMPLETED IAW ECT/TC REO 601R-53-41-821 AND THE SHIM IS COMPLETED IAW EC/TC REO 601R-53-41-821 AND THE ALTERATION MEETS ALL THE REQUIREMENTS OF REO 610R-53-41-821. C/W EC/TC REO 610R-53-41-260 IAW REO 610R-53-41-260 REV C.

Part: BEAM — CRACKED (FUSELAGE) · airframe 19,829 hrs · 16,514 cycles

VERTICAL BULKHEAD BEAM AT FS 409.00+128, LBL 18.00 LOCAL TO WL 69.00 HAS AN INDICATION NOTED APPROX 0.2 INCH LONG AND SIGNAL AMPLITUDE OF 80 PERCENT FULL SCREEN HEIGHT ON THE OTBD C-CHANNEL AFT RADIUS APPROX .5 INCHES BELOW TOP OF POST. REMOVED DAMAGED POST ASSY AND AIR FILTER BRACKETS IAW SRM 51-42-06. FABRICATED STIFFENER. HEAT TREATED STIFFENER IAW SRM 51-24-21 AND DWG 601R32208 AND HEAT TREATED TO AMS 2770H. LPI FABRICATED STIFFENER IAW NDM 51-20-08. NO INDICATIONS NOTED. INSTALLED POST AND AIR FILTER BRACKET IAW REO 610R-53-41-820 REV A & SRM 51-42-06.

Part: SKIN — CORRODED (WING) · airframe 19,829 hrs · 16,514 cycles

INDICATION NOTED AT LOWER WING PLANK ACCESS HOLE 640CB WHILE PERFORMING ASA TASK NR 000-57-900-610 AFT SIDE OF HOLE. INDICATION APPEARS TO BE CORROSION APPROX .040 IN DEPTH. INDICATION IS MAPED IN AIRCRAFT. REMOVED DAMAGE AT RT LOWER WING PLANK ACCESS HOLE 640CB IAW REO 601R-57-21-1033. ASA EC/TC NEEDS C/W. C/W EC/TC REO 601R-57-21-1033 IAW REO 601R-57-21-1033.

Part: SKIN — CRACKED (PAX DOOR) · airframe 19,829 hrs · 16,514 cycles

TWO CRACKS ON INNER SKIN AT PAX DOOR HANDLE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,829 hrs · 16,514 cycles

CARGO BAY SEAT TRACK BETWEEN FS 559.00+86 AND FS 574.00 AT LBL 9 CORRODED ALONG WITH HARDWARE. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 19,829 hrs · 16,514 cycles

PAX DOOR OUTER HANDLE IS CRACKED.

Part: ANGLE — CRACKED (INTERCOSTAL) · airframe 19,829 hrs · 16,514 cycles

LT FS 484 LBL 27 INTERCOSTAL ANGLE CRACKED. REMOVED AND REPLACED CRACKED INTERCOSTAL ANGLE IAW SRM 51-40-11 AND 51-42-21.

Part: SKIN — CORRODED (PAX DOOR) · airframe 19,829 hrs · 16,514 cycles

PASSENGER DOOR INNER SKIN HAS CORROSION AROUND FASTENER HOLES UNDER ACCESS PANELS 832AL, 832BL, 832CL, AND 832EL. CORROSION IS MINOR SURFACE CORROSION. REMOVED MINOR CORROSION IAW SRM 51-21-06.

Part: SKIN — CORRODED (PAX DOOR) · airframe 19,829 hrs · 16,514 cycles

PASSENGER DOOR INNER SKIN HAS CORROSION AROUND FASTENER HOLES UNDER ACCESS PNLS 832AR, 832BR, 832CR, 832ER AND 832GR. CORROSION IS MINOR SURFACE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 19,731 hrs · 16,423 cycles

ROW 8 OVERHEAD CEILING LIGHT EXIT SIGN FACING FWD INOP. FLT 5400 CX.

Part: FLAP — FAILED (WING) · airframe 18,446 hrs · 15,275 cycles

REPEAT FLAP SYSTEM FAILURE, FLAPS FAILED AT ZERO ON APPROACH INTO ROC ON 3/23/08, FERRIED TO ATL 3/24/08; REFER TO DEFECT 373059-3.

Part: FLAP — FAILED (WING) · airframe 18,415 hrs · 15,249 cycles

FLAP FAIL AT 200 KTS AT ZERO DEGREES WHEN SELECTING 8. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. EMERGENCY DECLARED. FLT 4568 DEL 279 MINS. (SKEW DETECTION SYSTEM) LUBED, RESHIMED AND RIGGED FLAP ACTUATORS NR 1-8. REMOVED AND REPLACED LT AND RT INB FLAP'S. FLAP SYSTEM OP CHECKS GOOD MESSAGE CLEARED IAW AMM 27-53-01.

Part: DETECTOR — MALFUNCTIONED (TE FLAPS) · airframe 18,332 hrs · 15,175 cycles

FLAPS FAIL AT 0, EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION, FLT 4902 CX. DURING FERRY FLT NR 9953 GRR-ATL, EMERGENCY EQUIPMENT WAS ALSO REQUESTED TO BE ON STANDBY INTO ATL. REMOVED AND REPLACED SKEW DETECTOR AND ADJUSTED LT O/B BPSU AS REQUIRED, OP CHECK GOOD AT THIS TIME.

Part: FLAP SYSTEM — FAILED (NR 3) · airframe 18,308 hrs · 15,156 cycles

NR 3 FLAP FAIL, EMERGENCY DECLARED.

Part: FLAP — FAILED (WING) · airframe 18,284 hrs · 15,136 cycles

ON APPROACH TO LGA SELECTED FLAPS TO 8 AND RECEIVED FLAP FAIL CAUTION MSG. EN ROUTE TO LGA A/C DIVERTED TO JFK AFTER T/O. EMERGENCY TRUCKS ROLLED. FLTS 4298, 4765 CX.

Part: FLAP — FAILED (WING) · airframe 18,275 hrs · 15,130 cycles

FLAP FAIL ON VISUAL APPROACH. FLT 4585 DEL 132 MINS -NC FLT 4585 CX. FAILED AT 0 DEG WHEN SELECTING 8. TOWER ROLLED THE FIRE TRUCKS AND AMBULANCE FOR SAFETY. REMOVED AND REPLACED FLAPS SCEW DETECTION UNIT ASSY IAW AMM 27-51-15. OP'S CHECK GOOD. DML CLEARED PLACARD REMOVED.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 17,459 hrs · 14,458 cycles

FLAPS FAIL AT 8 ON APPROACH COMPLIED WITH QRH. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY. FLT 4576 CX AND ON 10/20 FLT 4572 CX.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 16,071 hrs · 13,397 cycles

CAPT FWD WINDSHIELD CRACKED AND ARCHING DURING DESCENT AND SHATTERED BEFORE LANDING. EMERGENCY DECLARED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 16,034 hrs · 13,369 cycles

FLOOR SUPPORT STRINGER AT PAX DOOR OPENING STA 310 TO 349 LEFT CORRODED. REMOVED CENTER TITANIUM FLOOR SUPPORT ANGLE, DOOR PROX SWITCH SENSOR, FWD AND AFT HANDRAIL FITTINGS & BONDING WIRE CONNECTIONS, & BLENDED CORROSION OUT OF LIMITS OF CRJ 200 SRM 53-00-00 ON FLOOR SUPPORT STRINGER. FLOOR SUPPORT STRINGER REQUIRES REMOVE & REPLACE. FINISHED REMOVING FLOOR SUPPORT STRINGER, LOCATED HOLES & DRILLED NEW STRINGER, STARTED INSTALLING TOP FLOOR SUPPORT, IAW SRM 51-40-11/ 51-42-06. INSTALLED BONDING WIRES AND PROX SWITCH OPS CK GOOD IAW CRJ 200 AMM 52-70-00 AND WDM 20-00-00

Part: ANGLE — CORRODED (BS 349) · airframe 16,034 hrs · 13,369 cycles

CORROSION AT FS 349 RBL 37 SERVICE DOOR AFT ANGLE.

Part: ANGLE — CORRODED (BS 349) · airframe 16,034 hrs · 13,369 cycles

CORROSION AT FS 349 LBL 37 ASD AFT ANGLE. REMOVED TEFLON STRIP AND REMOVED CORROSION AT FS349 LBL37 ASD AFT ANGLE. DAMAGE WITHIN LIMITS. TREATED PRIMED AND PAINTED.REINSTALLED TEFLON STRIP. WORK DONE IAW CRJ 200 SRM 51-21-06 AND 51-42-13.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,034 hrs · 13,369 cycles

CORROSION FOUND ON FWD SUPPORT FLOOR ANGLE OF THE 280. REMOVED FWD 280 FLOOR SUPOPRT AGNLE DUE TO CORROSION ALL WORK DONE IAW CRJ 200 SRM 51-42-06. REMOVED AND REPLACED FWD FLOOR SUPPORT ANGLE ON 280 IAW REO 601R-53-11-926. TASK COMPLETED ON TASK CARD N/R-00169.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,034 hrs · 13,369 cycles

STA 280 AFT FLOOR SUPPORT ANGLE HAS SURFACE CORROSION AT BL 0. ALL WORK DONE IAW REO 601R-53-11-926

Part: FRAME — CRACKED (BS 640) · airframe 16,034 hrs · 13,369 cycles

LEFT SIDE 640 FRAME CRACKED FWD SIDE BETWEEN STR 9 AND ENGINE SUPPORT BEAM WEB AFT OF ENGINE SUPPORT BEAM UPPER OUTBOARD ATTACH ANGLE.

Part: FLOORBEAM — CRACKED (BS 461) · airframe 16,034 hrs · 13,369 cycles

STA 461 FLOORBEAM FITTING CRACKED RBL 9 OUTBOARD SIDE. INSTALLED NEW FITTING COMPLETE WITH LOCK FASTENERS IAW CRJ 200 SRM 51-42-21 .

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 16,034 hrs · 13,369 cycles

STA 484 RBL 36 INTERCOSTAL REPAIR ANGLE CRACKED IN RADIUS.

Part: FLOORBEAM — CRACKED (BS 461) · airframe 16,034 hrs · 13,369 cycles

FLOORBEAM FITTING CRACKED AT UPPER AFT CORNER STA 461 RBL 9 INBOARD FITTING. (SUPPLEMENTAL 28 MARCH 07) INSTALLED NEW REPLACEMENT FITTING IAW SRM 51-42-21.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 16,034 hrs · 13,369 cycles

EMERGENCY LIGHT COVER ON F/A STATION DAMAGED (MARKED).

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 16,034 hrs · 13,369 cycles

EMERGENCY EXIT LIGHT COVER ABOVE SERVICE DOOR CRACKED (MARKED).

Part: PLACARD — WORN (PAX DOOR EXIT) · airframe 16,034 hrs · 13,369 cycles

PAX DOOR -EXIT- PLACARD WORN. REPAIRED IAW ALL REFERENCE MATERIAL.

Part: STEP — BROKEN (AIRSTAIR DOOR) · airframe 15,552 hrs · 13,007 cycles

ASD BTM STEP BROKEN AT ATTACH BRACKET.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,402 hrs · 12,890 cycles

EXT EMERGENCY LIGHT NEXT TO PAX DOOR INOP.

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 15,266 hrs · 12,788 cycles

RIGHT & LEFT FS 625 CLIPS CRACKED.

Part: FRAME — CRACKED (BS 280) · airframe 15,266 hrs · 12,788 cycles

THE 280 FRAME CRACKED AT BL 12 RT, LOWER LEG. REPAIRED 280 FRAME AT BL 12 RT LOWER LEG IAW EO 600-53-0090.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 15,266 hrs · 12,788 cycles

LEFT BL 8 AND 10 280 ATTACH CLIPS CRACKED. *S/D* REMOVED AND REPLACED LEFT BL 8 AND 10 280 CLIPS, ALL WORK DONE IAW CRJ 200 SRM 51-42-20 DK 7022603 11-12-06 JOB COMPLETE.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 15,266 hrs · 12,788 cycles

RT BL 8 AND 10 280 ATTACH CLIPS CRACKED. S/D REPAIRED DAMAGE TO RT BL 8 AND 10 280 ATTACH CLIPS BY FABRICATING NEW CLIPS IAW EO 600-53-90.

Part: STEP — BROKEN (PAX DOOR)

FLT 4741 - DURING A GROUND INSPECTION IN ABE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR IAW CRJ200 AMM 52-11-04. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LENS — CRACKED (EMERGENCY LIGHT)

DURING A C-CHECK IN MCN, THE BASE AND LENS ON THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. OPS CHECKS GOOD. (M)

Part: HANDLE — CRACKED (E/E BAY DOOR)

DURING A C-CHECK, THE AVIONICS BAY DOOR OUTER HANDLE CUP WAS FOUND CRACKED AROUND THE HANDLE BOSS. MAINTENANCE REMOVED AND REPLACED THE AVIONICS BAY DOOR HANDLE ASSEMBLY IAW AMM AND SRM. OPS CHECK GOOD. (K)

Part: BRACKET — MISALIGNED (EMERGENCY EXIT)

DURING A C-CHECK IN MCN, THE RIGHT EMERGENCY EXIT DOOR FAILED THE FUNCTIONAL TEST. MAINTENANCE ADJUSTED THE DOOR MOUNTING BRACKETS ON THE RIGHT EMERGENCY EXIT. OPERATIONAL CHECKS GOOD. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE ATTACH CLIP AT FS 484, LBL 30 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ATTACH CLIP AT FS 484, LBL 30 IAW ASA EO 600-53-0098. (M)

Part: BRACKET — CRACKED (RAM AIR DUCT)

DURING A C-CHECK IN MCN, THE RAM AIR SPIDER DUCT UPPER BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RAM AIR SPIDER DUCT UPPER BRACKET IN THE AFT EQUIPMENT BAY. (M)

Part: ANCHOR FITTING — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE AFT CABLE ANCHOR MOUNT FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFT CABLE ANCHOR MOUNT FITTING ON THE PASSENGER DOOR IAW CRJ AMM 52-00-00. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN LOOSE FROM THE ACTUATOR ROD. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP IAW CRJ-200 SRM 51-42. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072B. (M)

Part: PLATE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR LANDING PLATE WAS FOUND TO BE CRACKED AT RIVET FS 605. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR LANDING PLATE AT FS 605 IAW ASA EO 600-53-0117. (M)

Part: RIB — CRACKED (LT WING)

DURING A C-CHECK IN MCN, THE LEFT BATTERY RIB AT THE UPPER CORNER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT BATTRY RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CLIP AT FS 484, LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIP AT FS 484, LBL 36 IAW ASA EO 600-53-0098. (M)

Part: LIGHT — CRACKED (GALLEY)

DURING A C-CHECK IN MCN, THE BASE AND LENS ON THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. (M)

Part: BRACKET — MISALIGNED (EMERGENCY EXIT)

DURING A C-CHECK IN MCN, THE LEFT EMERGENCY EXIT DOOR FAILED THE FUNCTIONAL TEST. MAINTENANCE ADJUSTED THE DOOR MOUNTING BRACKETS ON THE LEFT EMERGENCY EXIT. OPS CHECKS GOOD. (M)

Part: HYDRAULIC SYSTEM — LEAKING (NR 1)

DURING CRUISE FROM ATL-FNT, THE CREW NOTICED THE NR 1 HYDRAULIC SYSTEM QUANTITY HAD FALLEN TO 45 PERCENT. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT DIVERTED TO CVG AND LANDED SAFELY. MAINTENANCE INSPECTED AND SERVICED THE NR 1 HYDRAULIC SYSTEM. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING HANGAR MAINTENANCE IN BTR, THE LEFT EXTERIOR SECOND EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT EXTERIOR SECOND EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WARNING SYSTEM — FALSE ACTIVATION (FUEL SYSTEM)

FLT 4722 - DURING CLIMB-OUT FROM ATW-ATL, THE CREW NOTICED A FUEL DISCREPANCY AND LOSS OF 1,800 LBS WITH A CONINUING LOSS OF 10 LBS PER SECOND ACCOMPANIED BY SPORADIC FUEL TOTALIZER READINGS. AN EMERGENCY WAS DECLARED. FUEL LOSS READINGS CONTINUED TO FLUCTUATE BETWEEN 10 LBS PER SECOND TO 500 LBS PER MINUTE. THE AIRCRAFT DIVERTED TO ORD AND LANDED SAFELY. MX CHECKED FOR LOGGED FAULTS. NO FAULTS WERE FOUND AND THEN RESET THE FUEL COMPUTER. ALL READINGS WERE NORMAL. MAINTENANCE ALSO SUMPED THE FUEL TANKS FOR WATER. NO FAULT CODES WERE FOUND ON THE FUEL QUANTITY GAUGING COMPUTER OR THE MX DIAGONISTIC COMPUTER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR) · airframe 10,181 hrs

DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4755 - DURING A GROUND INSPECTION IN DFW, THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM THE FRONT EMERGENCY CEILING LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN BTR, THE RIGHT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE FIRST FIVE SEGMENTS OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOR TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE FIRST FIVE SEGMENTS OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOR TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE EMERGENCY CEILING LIGHT AT ROW TEN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW TEN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY IAW AMM 21-52-00. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

DURING DESCENT, AT APPROXIMATELY 10,000 FEET AND 25D KIAS, THE FIRST OFFICERS WINDSHIELD (THIRD WINDOW FROM THE LEFT) SHATTERED. THE CAPTAIN PERFORMED THE ABNORMAL PROCEDURES CHECKLIST FROM THE QRH. AN EMERGENCY WAS DECLARED, BUT LATER CANCELED BY THE CAPTAIN. THE INNER WINDOW PANE REMAINED IN TACT AND NO GLASS ENTERED THE COCKPIT. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE SHATTERED WINDSHIELD. LEAK CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: BULB — BURNED OUT (CABIN)

DURING A SCHEDULED INSPECTION IN XNA, THE FORWARD CABIN OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT OVERHEAD EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING A SCHEDULED INSPECTION IN XNA, THE THIRD EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE THIRD EXTERIOR EMERGENCY LIGHT WHICH WAS BURNED OUT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4787 - DURING SCHEDULED INSPECTION IN XNA, THE NR 3 CABIN OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 OVERHEAD EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)