N853AS

Part: CONTROL PANEL — FAILED (INTERPHONE) · airframe 34,263 hrs · 30,828 cycles

IN CRUISE PA BUTTON WAS EXTREMELY HOT AND SMOKING WITH ELECTRICAL SMELL DIVERTED TO BHM. PASSENGER ADDRESS SYSTEM, ENROUTE TO JAN, ACFT DIVERTED DUE TO MAINTENANCE EMERGENCY ACTIONS. R & R INTERPHONE CONTROL UNIT IAW AMM 23-31-07, REF IPC 23-31-07, ITEM 5, OPS TEST GOOD DEFER CLEARED.

Part: SUPPORT BEAM — CRACKED (BS 621) · airframe 33,450 hrs · 29,989 cycles

FS 621 SUPPORT BEAM LOWER ANGLE CRACKED. R & R SUPPORT BEAM ANGLE IAW SRM 51-42-21.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,695 hrs · 29,255 cycles

EMERGENCY LIGHTS IN CENTER CABIN INOPERATIVE. REPLACED NR 2 CHARGER ASSEMBLY IAW AMM 33-51-05, AIPC 33-51-04 ITEM 78. SELF TESTED GOOD. OPS CHECK OF EMERGENCY LIGHT IN CENTER OF CABIN GOOD.

Part: SKIN — BURNED (BS 395-310) · airframe 31,973 hrs · 28,532 cycles

ONE BURN BETWEEN STRINGERS 4R-5R FS 295 - 310. REMOVED DAMAGE IAW REO 601R-53-00-115, REV.E. INSTALLED PERMANENT FASTENER AND RESTORED FINISH, REO 601R-53-00-115, REV E. TMAJOR REPAIR IAW GMM 5-3.

Part: SKIN — CRACKED · airframe 31,973 hrs · 28,532 cycles

CRACK IN SKIN PANEL AT LT TRU DOOR AFT LATCH. PERFORMED VISUAL INSPECTION, STOP DRILLED CRACK. RESTORED FINISH. WORK DONE IAW REO 601R-53-11-2381. MAJOR REPAIR IAW GMM 3-3.

Part: SKIN — DENTED (RT WING LE) · airframe 31,376 hrs · 27,931 cycles

TEMP REPAIR OF DENT IN L/E, RT SIDE L/E DENT AT WS 199.00, REFER TO REO 601 R-57-41-806. REPAIRED IAW REO 601R-57-41-853.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 31,359 hrs · 27,914 cycles

THE NR 4 EMGERGENCY BATTERY IS BELOW MIN. VOLTAGE. R & R EMERGENCY BATTERY PACK NR 4 IAW AMM 33-51-04-000-801, AMM 33-51-04-400-801. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: SKIN — DAMAGED (BS 310) · airframe 31,376 hrs · 27,931 cycles

FUSELAGE REPAIR DOUBLERS OF PAX DOOR FS 310 & S16L THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. R & R TOP DOUBLERS AND FILLERS IAW EO 600-53-0737.

Part: SKIN — NICKED (FUSELAGE) · airframe 31,376 hrs · 27,931 cycles

FUSELAGE NICKED DURING TRIMMING OF ADG DOOR. REPAIRED IAW EO CL600-2B19-53-I000399.

Part: CLAMP — CRACKED (APU FUEL SHROUD) · airframe 31,376 hrs · 27,931 cycles

PRESSURE AND BLOCKAGE TEST OF THE APU FUEL FEED LINE USING GASEOUS PRESSURE REQUIRED. FOUND SMALL CRACK UNDER UPPER CLAMP ON THE APU FUEL SHROUD IAW AMM 28-20-01-780-804. REPAIRED IAW REO 601R-28-21-004. MAJOR REPAIR.

Part: DOOR FRAME — CRACKED (BS 338) · airframe 31,359 hrs · 27,914 cycles

DOOR FRAME CRACKED AT FS 338. TRIMMED & DRILLED NEW FRAME SECTION & TOUCHED UP HOLES & EDGES IAW SRM 51-40-11-00. INSTALLED NEW FRAME SECTION IAW SRM 51-42-21-00.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 31,359 hrs · 27,914 cycles

INTERCOSTAL CRACKED INSIDE ASD ACCESS PANEL 832BR. REMOVED DAMAGED INTERCOSTAL AND DRILLED UP NEW PART IAW SRM 51-42-06-001-001 AND 51-42-13-001-001. INSTALLED INTERCOSTAL ATTACH ANGLE GF 162018 IAW SRM 51-42-06-00 & SRM 51-42-13-00. & DWG 601R31902.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,359 hrs · 27,914 cycles

CORRODED SEAT TRACK LBL9 FS 559+110 TO 559+120. REMOVED SEAT TRACK IAW SRM 51-40-11 AND INSTALLED SEAT TRACKS IAW AMM 53-01-11.

Part: DOOR — FOULED (LT OVERWING) · airframe 31,358 hrs · 27,912 cycles

LEFT OVERWING EMERGENCY OUT OF ADJUSTMENT, FAILED FUNCTION TEST. LT OVERWING EMERGENCY DOOR EXIT WAS CLEANED AND REMOVED OLD LUBE FROM LOBES. ACCOMPLISHED FUNCTIONAL CHECK. OPS CHECKED GOOD IAW AMM 51-21-00-720-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,358 hrs · 27,912 cycles

CORRODED SEAT TRACK RBL27, FS 559+72 TO 559+89. REPLACED WITH SERVICEABLE SEAT TRACK AMM 53-01-11-000-802 AND 53-1-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,359 hrs · 27,914 cycles

CORRODED SEAT TRACK RBL9 FS 559+85 TO 559+94. R & R CORRODED SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,359 hrs · 27,914 cycles

RIGHT AFT SIDE WALL SEAT TRACK FOUND CORRODED BETWEEN FS 559.00+16 - 559.00+48. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & AMM 53-01-11-400-802.

Part: BRACKET — CORRODED (HAND RAIL) · airframe 31,359 hrs · 27,914 cycles

PAX DOOR AFT HANDRAIL RECESS HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 AND 53-00-00. REMOVED AFT HAND RAIL RECESS BRACKET IAW SRM 51-42-06. DRILLED & INSTALLED NEW SERVICEABLE LOWER AFT HANDRAIL RECESS BRACKET IAW SRM 51-42-06 & 51-42-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,358 hrs · 27,912 cycles

CORRODED SEAT TRACK LB L9 FS 559+85 TO 559+94. FOUND OUT OF LIMITS. R & R CORRODED SEAT TRACK. INSTALLED SERVECIBLE SEAT TRACK IAW AMM 53-0-11-000-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,359 hrs · 27,914 cycles

CORRODED SEAT TRACK RBL 9 FS 559+110 TO 559+120. REMOVED SEAT TRACK IAW SRM 51-40-11 AND INSTALLED SEAT TRACK IAW AMM 53-01-11.

Part: FLOOR SUPPORT — CORRODED (BS 570) · airframe 31,359 hrs · 27,914 cycles

LT CARGO FLOOR SUPPORT CORRODED AT FS 570. REPAIRED IAW REO 61R-53-00-526.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 31,358 hrs · 27,912 cycles

LEFT FWD SIDE WALL SEAT TRACK FOUND CORRODED BETWEEN BS 409+16 - 409+80. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: SKIN — DENTED (RT WING LE) · airframe 31,376 hrs · 27,931 cycles

TEMP REPAIR OF DENT IN L/E, RT SIDE L/E DENT AT WS 199.00, REFER TO REO 601R-57-41-806. COMPLIED WITH EC/TC REO 601R-57-41-853, PERMANENT REPAIR. REPAIRED IAW AMM TASK 57-41-01-000-804 AND REO 601R-57-41-853.

Part: SKIN — DAMAGED (BS 310) · airframe 31,376 hrs · 27,931 cycles

DAMAGE TO FUSELAGE REPAIR DOUBLERS FWD OF PAX DOOR FS 310 AND S16L. REPAIRED IAW REO 601R-53-21-180.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 30,031 hrs · 26,579 cycles

RT FWD EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R RT FWD EXTERNAL EMERGENCY LIGHT BULB IAW AMM 33-51-21. OP'S CHECKED GOOD.

Part: WIRE HARNESS — MALFUNCTIONED (NLG STEERING) · airframe 29,722 hrs · 26,270 cycles

RECEIVED STEERING INOPERATIVE MESSAGE AFTER LOWERING LANDING GEAR PRIOR TO LANDING. EMERGENCY DECLARED AS A PRECAUTION. R & R NOSE WHEEL STEERING ELECTRICAL HARNESS DUE TO INTERMITTENT SHORT IAW AMM 32-61-25. ALL OPS CHECKS GOOD. SDR CLOSED.

Part: CONNECTOR — CONTAMINATED (NLG STEERING) · airframe 29,707 hrs · 26,253 cycles

NOSE WHEEL STEERING INOPERATIVE MESSAGE ON T/O ROLL, CONTINUED AND RAN QRH. DID NOT RESET. EMERGENCY DECLARED AS A PRECAUTION. VERIFIED DISCREPANCY. MDC FLAGGING RT RVDT. INPECTED RT NOSEGEAR STEERING ACTUATOR POSITION FEED BACK SENSOR. FOUND UNKNOWN LIQUID OR WATER INSIDE. CLEANED CONNECTOR W/ CONTACT CLEANER REATTACHED PLUG AND FUNCTION TESTED NOSEWHEEL STEERING SYS IAW AMM 32-51-00. ALL CHECKS OK AT THIS TIME. SDR CLOSED.

Part: BRACKET — DAMAGED (PROXIMITY SENSOR) · airframe 28,105 hrs · 24,537 cycles

AIR RETURN DUE TO GEAR UP DISAGREE MESSAGE - GEAR IN UP POSTION FOLLOWED QRH NOSE GEAR DOWN MAINS UP LANDING UP, LANDING WEIGHT 49,100, IAS 139, VSI 150 FPM. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) FLT 5101, DEL 33 MINS. R & R CENTER/EXTENDED BRACKET IAW CMM 200 32-20-01 ADJUSTED PROXIMITY SENSOR IAW AMM 32-61-05. OPS CHECK GOOD.

Part: BULKHEAD — CRACKED (BS 621) · airframe 27,288 hrs · 23,631 cycles

CRACK INDICATION NOTED AT LBL 36.20, WL 79.0, FS 621. REAR PRESSURE BULKHEAD WEB APPROX .50 IN LENGTH. VERTICALLY AT HEEL LINE 100 PERCENT FULL SCREEN HEIGHT. FAILED NDT. REPAIRED IAW REO 601R-53-1285.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 27,279 hrs · 23,623 cycles

FLOORBEAM CAP AT RBL 9 IS CORRODED AROUND NUTPLATES FROM FS 409.0 TO 409+112.

Part: FRAME — CORRODED (BS 349) · airframe 27,279 hrs · 23,623 cycles

FOUND FRAME STA 349 LOWER SECTION TO BE CORRODED AND REQUIRES REPLACEMENT. CLASSIFIED AS A MINOR REPAIR.

Part: SILL — CORRODED (BS 409-559) · airframe 27,279 hrs · 23,623 cycles

RT PRESSURE FLOOR SILL IS CORRODED AROUND NUTPLATES & SILL ANGLES ARE CORRODED AROUND FASTENERS FROM FS 409+128 TO FS 559.

Part: FRAME — CORRODED (BS 333) · airframe 27,279 hrs · 23,623 cycles

FOUND LOWER FS 333 FRAME SECTION TO BE CORRODED. REPAIRED IAW SRM.

Part: FRAME — CORRODED (BS 333) · airframe 27,279 hrs · 23,623 cycles

FOUND LOWER FS 333 FRAME SECTION CORRODED. REMOVED FRAME IAW SRM 51-42-06, 51-42-21. DRILLED & LOCATED NEW SERVICEABLE FRAME IAW SRM 51-40-06.

Part: FRAME — CORRODED (BS 349) · airframe 27,279 hrs · 23,623 cycles

FOUND FRAME BS 349 LOWER SECTION TO BE CORRODED. INSTALLED NEW FRAME IAW SRM 51-42-06 AND 51-42-21.

Part: FRAME — CORRODED (BS 319.7) · airframe 27,279 hrs · 23,623 cycles

FRAME AT FS 319.70 IS CORRODED AT LBL 26. LOCATED AND DRILLED NEW FRAME SECTION IAW SRM 51-40-11. INSTALLED NEW FRAME SECTION IAW SRM 51-42-06 AND 51-42-21.

Part: SILL — CORRODED (BS 409-559) · airframe 27,279 hrs · 23,623 cycles

RT PRESSURE FLOOR SILL IS CORRODED AROUND NUTPLATES & SILL ANGLES ARE CORRODED AROUND FASTENERS FROM FS 409+128 TO FS 559.

Part: ANGLE — CRACKED (BS 589) · airframe 27,279 hrs · 23,623 cycles

FOUND ANGLE TO BE CRACKED AT FS 589, LBL 45, WL 73. DRILLED, NEW ANGLE PN 601R35011-13 IAW SRM 51-4221, STEP 5A-B. INSTALLED NEW ANGLE IAW SRM 51-42-21, STEP 9C. PRIMERED AND PAINTED FASTENER HEADS AND COLLARS IAW SRM 51-25-01, STEP 7B & E. REPAIR CLASSIFIED AS A MINOR.

Part: FRAME — CRACKED (BS 409) · airframe 27,279 hrs · 23,623 cycles

CRACK INDICATION NOTED AT FS 409+128 RBL 18 INBD & OTBD CHANNELS AT JOGGLES IN RADIUS WL 69.00. INDICATIONS APPROX .150" IN LENGTH, 78 PERCENT FULL SCREEN, FAILED NDT, AREAS MARKED ON VERT POST RADII. CLASSIFIED A MINOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 27,279 hrs · 23,623 cycles

CORROSION ON FLOORBEAM FS 589 BETWEEN LBL 9 & LBL 27 ABOVE & BELOW FLANGES AROUND NUTPLATE HOLES. REMOVED AND REPLACED WITH SERVICEABLE PARTS IAW SRM.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 27,279 hrs · 23,623 cycles

FLOORBEAM CAP FS 589 CORRODED BETWEEN LBL 9 & LBL 27. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. INSTALLED CAP IAW SRM 51-40-11, SRM 51-42-06, SRM 51-42-21 AND SRM 51-42-15.

Part: SKIN — CORRODED (PAX DOOR) · airframe 27,279 hrs · 23,623 cycles

PAX DOOR INNER SKIN IS CORRODED ON LWR AFT EDGE AT APPOX FS 342-335. FOUND OUT OF LIMITS. REPLACED CORRODED SKIN SECTION IAW REO 601R-52-11-1977.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 27,279 hrs · 23,623 cycles

PAX DOOR LOWER FWD & AFT CORNERS HAVE CORROSION UNDER FOAM RESIN. REMOVED PAX DOOR LOWER FWD AND AFT CORNERS. LOCATED AND DRILLED UP NEW LOWER FWD AND AFT CORNERS IAW SRM 51-42-06. INSTALLED NEW CORNERS IAW SRM 51-42-06/-21.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · airframe 27,279 hrs · 23,623 cycles

PAX DOOR LOWER 5 SKIN CLIPS HAVE CORROSION UNDER FOAM RESIN. R & R PAX DOOR 5 LOWER SKIN CLIPS AS REQUIRED IAW SRM 51-42-06. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)

Part: CHANNEL — CRACKED (BS 409) · airframe 27,279 hrs · 23,623 cycles

INDICATIONS NOTED AT FS 409+128 RBL 18 INBD & OTBD CHANNELS AT JOGGLES IN RADIUS WL 69.00. INDICATIONS APPROX .150 IN LENGTH 78 PERCENT FSH, FAILED NDT. INSTALLED NEW CHANNELS IAW SRM 51-42-06 AND REO 601R-53-41-889.

Part: CHANNEL — CRACKED (BS 49) · airframe 27,279 hrs · 23,623 cycles

INDICATION NOTED AT FS 49+128 BL 0.0 WL 69.0 RT CHANNEL OF VERT POST IN JOGGLE. INDICATION APPROX .10 IN LENGTH 100 PERCENT FSH, FAILED NDT. INSTALLED NEW POST AND ANGLES IAW SRM 51-42-06 AND REO 601R-53-41-889.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 27,279 hrs · 23,623 cycles

SEAT TRACK AT LBL 9 IS CORRODED BETWEEN FS 394 & 409+128. DRILLED NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED TRACK IAW AMM 53-01-11-400-802.

Part: FRAME — CRACKED (BS 718 S10L) · airframe 27,279 hrs · 23,623 cycles

FS 718 FRAME CRACKED AT S10L. PERFORMED EDDY CURRENT INSP OF FS 718 FRAME SUSPECTED AREA AT STR 10L IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME.

Part: FLOOR SUPPORT — CORRODED (BS 621) · airframe 27,279 hrs · 23,623 cycles

FS 621 BULKHEAD FLOOR SUPPORT ANGLE HAS LIGHT CORROSION FROM RBL 27-RBL 45. FOUND CORROSION TO BE PITTED AT AND AROUND FASTENER HOLES AT FS 621, RBL 27- RBL 45. AREA FOUND OUT OF LIMITS IAW SRM 51-21-06. ACCOMPLISHED STEP 1 OF REO 601R-53-61-4166. MAX MAT LOSS .004. COMPLIED WITH STEP 3 OF REO 601R-53-61-4166. PERFORMED EDDY CURRENT OF FLOOR SUPPORT REPAIR IAW NDTM 51-20-06. NO INDICATIONS NOTED. ACCOMPLISHED STEPS 2, 4, 5 AND 6 OF REO 601R-53-61-4166. REO 601R-53-61-4166 REV-- HAS BEEN ACCOMPLISHED

Part: CARGO TRACK — CORRODED (BS 559-567) · airframe 27,279 hrs · 23,623 cycles

CARGO TRACK AT LBL 9 IS CORRODED BETWEEN FS 559+100 & 567. R & R CARGO TRACK IAW SRM 51-41-04.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 27,279 hrs · 23,623 cycles

SEAT TRACK AT RBL 27 IS CORRODED BETWEEN FS 559+80 & 559+96. CLEANED SEAT TRACK IAW SRM 51-26-00. FOUND NO CORROSION.

Part: FLOOR SUPPORT — CORRODED (BS 589-615) · airframe 27,288 hrs · 23,631 cycles

LBL 9, FLOOR SUPPORT HAS LIGHT CORROSION AROUND NUTPLATES FROM FS 589-615. REMOVED FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21. LOCATED NEW FLOOR SUPPORT AND DRILLED FASTENER HOLES IAW REO 601R-53-61-3780. INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-61-3780.

Part: FLOORBEAM — CORRODED (BS 621) · airframe 27,279 hrs · 23,623 cycles

FS 621 BULKHEAD FLOOR SUPPORT ANGLE HAS LIGHT CORROSION FROM LBL 27- LBL 45. COMPLETED CORROSION PREVENTION AND CONTROL PROGRAM IAW SRM 51-21-00. FOUND CORROSION TO BE PITTED AT AND AROUND FASTENER HOLES. AREA FOUND OUT OF LIMITS IAW SRM 51-21-06. ACCOMPLISHED STEP 1 OF REO 601R-53-61-4166. MAX MAT LOSS .005. PERFORMED EDDY CURRENT OF FLOOR SUPPORT REPAIR IAW NDTM 51-20-06. NO INDICATIONS NOTED. ACCOMPLISHED STEPS 2, 4, 5 AND 6 OF REO 601R-53-61-4166.

Part: FLOORBEAM — CORRODED (BS 618) · airframe 27,279 hrs · 23,623 cycles

FLOORBEAM CAP AT FS 618 IS CORRODED FROM LBL 9 TO RBL 9. REMOVED DAMAGE IAW SRM 53-00-00. MAX REMOVED .003. BLENDED IAW SRM 51-12-00. PERFORMED LPI ON FLOORBEAM CAP IAW NDTM 51-20-08. NO INDICATIONS NOTED.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 27,279 hrs · 23,623 cycles

FLOORBEAM CAP AT RBL 9 IS CORRODED AROUND NUTPLATES FROM FS 409 TO 409+112. FLOORBEAM CAP IS CORRODED BEYOND LIMITS. REMOVED CAP IAW SRM 51-42-06 & 51-42-21. REPLACED CAP WITH NEW PART IAW REO 601R-53-00-433 REV.

Part: CARGO TRACK — CORRODED (BS 559-565) · airframe 27,279 hrs · 23,623 cycles

CARGO TRACK AT RBL 9 IS CORRODED BETWEEN FS 559-100 & 565. INSTALLED NEW CARGO TRACK IAW SRM 51-41-02 AND SRM 51-41-04.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 27,279 hrs · 23,623 cycles

FLOORBEAM AT LBL 12 IS CORRODED AT FS 559+104. REMOVED CORROSION APPROX .004" FROM .100". FOUND CORROSION WITHIN ALLOWABLE LIMITS IAW SRM 53-61-43 AND 53-00-00.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 27,279 hrs · 23,623 cycles

FLOORBEAM CAP AT FS 589 IS CORRODED BETWEEN RBL 27 & RBL 45. REMOVED FLOORBEAM CAP IAW SRM 51-40-11, STEP 3A. INSTALLED NEW FLOORBEAM CAP IAW SRM 51-42-06, STEP 9C.

Part: FLOORBEAM — CORRODED (BS 574) · airframe 27,279 hrs · 23,623 cycles

FLOORBEAM CAP AT FS 574 IS CORRODED BETWEEN RBL 27 & RBL 45. REMOVED MINOR CORROSION, TREATED AND PAINTED AREA IAW SRM 51-21-06.

Part: FLOOR SUPPORT — CORRODED (BS 574-619) · airframe 27,279 hrs · 23,623 cycles

RBL 9, FLOORBEAM CAP IS CORRODED BETWEEN FS 574 & 619. REMOVED FLOORBEAM CAP IAW REO 601R-53-61-3780 AND SRM 51-42-06 AND 51-42-21. REPLACED A NEW CAP IAW REO 601R-53-61-3780.

Part: BULKHEAD — CRACKED · airframe 27,279 hrs · 23,623 cycles

INDICATION NOTED AT LBL 36.20, WL 79.0 621 REAR PRESSURE BULKHEAD WEB APPROX .50 IN LENGTH VERTICALLY AT HEEL LINE 100 PERCENT FULL SCREEN HEIGHT. FAILED NDT. REMOVED ISOLATOR IAW SRM 51-42-06. INSTALLED NEW ISOLATOR IAW REO 601R-53-61-4165.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 27,279 hrs · 23,623 cycles

INDICATION NOTED AT 621 REAR PRESSURE BULKHEAD WEB AT LINTEL FITTING IN UPPER CORNER APPROX .20 IN LENGTH 100 PERCENT FULL SCREEN HEIGHT. FAILED NDT. REPAIRED BULKHEAD IAW REO 601R-53-61-1230.

Part: FLOOR SUPPORT — CORRODED (BS 574-619) · airframe 27,288 hrs · 23,631 cycles

RBL 27 FLOOR SUPPORT HAS LIGHT CORROSION AROUND NUTPLATES FROM FS 574-619. UPON REMOVAL OF CORROSION DAMAGE, FOUND BEYOND LIMITS IAW REO 601R-53-00-005. R & R FLOOR SUPPORT WITH NEW SERVICEABLE PIECE IAW SRM 51-42-21 AND 51-42-22 AND REO 601R-53-61-4174.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 27,279 hrs · 23,623 cycles

SEAT TRACK AT RBL 9 IS CORRODED BETWEEN FS 559+85 & 559+96. REMOVED AND REPLACED CORRODED SEAT TRACK IAW AMM 20-21-00-910-801.

Part: FLOOR SUPPORT — CORRODED (BS 574-615) · airframe 27,279 hrs · 23,623 cycles

LBL 27 FLOORBEAM CAP IS CORRODED BETWEEN FS 574 & 615. REMOVED FLOORBEAM CAP IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW FLOORBEAM CAP IAW REO 601R-53-61-3778, REV A AND SRM 51-42-21. INSTALLED A NEW FLOOR BEAM CAP IAW REO 601R-53-61-3778.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 27,279 hrs · 23,623 cycles

TRANSVERSE FLOORBEAM CAP AT FS 589 IS CORRODED BETWEEN RBL 9 & RBL 27. REMOVED FLOORBEAM CAP IAW SRM 51-42-06, 51-42-21, 51-42-15. DRILLED NEW FLOORBEAM CAP AND INSTALLED IAW SRM 51-40-06, 51-40-11, 51-42-15, 51-42-06, 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 27,279 hrs · 23,623 cycles

SEAT TRACK AT LBL 27 IS CORRODED BETWEEN FS 559+80 & 559+96. REMOVED CORRODED SEAT TRACK AND INSTALLED A NEW SEAT TRACK IAW SRM 51-41-02.

Part: SILL — CORRODED (BS 409-559) · airframe 27,279 hrs · 23,623 cycles

LT PRESSURE FLOOR SILL IS CORRODED AROUND NUTPLATES AND SILL ANGLES ARE CORRODED AROUND FASTENERS FROM FS 409+128 TO FS 559. REPAIRED IAW REO 601R-53-41-666 AND DEVIATION 601R-53-41-1465.

Part: SILL — CORRODED (BS 409-559) · airframe 27,279 hrs · 23,623 cycles

RT PRESSURE FLOOR SILL IS CORRODED AROUND NUTPLATES AND SILL ANGLES ARE CORRODED AROUND FASTENERS FROM FS 409+128 TO 559. REPAIRED IAW REO 601R-53-41-666 AND REO 601R-53-41-666 REV B.

Part: FRAME — CORRODED (BS 394) · airframe 27,279 hrs · 23,623 cycles

FS 394, FRAME AFT FACE HAS CORROSION AROUND AVIONICS BAY DOOR GUIDE ATTACH BOLT AT STRINGER 26R. REMOVED CORROSION IAW 51-21-06. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 27,279 hrs · 23,623 cycles

SEAT TRACK AT RBL 9 IS CORRODED FROM FS 409+128 TO FS 559+85. R & R SEAT TRACK IAW MM 53-01-11-000-802 & 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 27,279 hrs · 23,623 cycles

SEAT TRACK AT LBL 9 ARE CORRODED FROM FS 409+128 TO FS 559+85. INSTALLED NEW TRACK IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · airframe 27,279 hrs · 23,623 cycles

FLOORBEAM CAP AT RBL 9 IS CORRODED AROUND NUTPLATES BETWEEN FS 559+80 AND FS 574. REMOVED CORRODED FLOORBEAM CAP AT RBL 9, FS 559+80 & FS 574 IAW SRM 51-42-06 & 51-42-21. INSTALLED NEW SERVICEABLE FLOORBEAM CAP IAW REO 601R-53-00-433.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 27,279 hrs · 23,623 cycles

FS 280.00, LBL 9 INBD FLOORBEAM CORNER CLIP CRACKED, RBL 9 INBD FLOORBEAM CLIP CRACKED. R & R FLOORBEAM IAW SRM 51-42-21 & 51-40-06.

Part: LIGHT — LOOSE (MAIN CABIN) · airframe 27,247 hrs · 23,590 cycles

PAX DOOR EXIT LIGHT (FLOOR LEVEL ) LOOSE. REPLACED PAX DOOR EXIT LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 26,948 hrs · 23,270 cycles

FWD EMERGENCY PHOTO LUM STRIP MISSING AT SEAT 8AB. INSTALLED NEW STRIP IAW VCMM 33-M41-10 STG. OPS CK GOOD. ITEM: 1 INSTALLED NEW STRIP IAW VCMM 33-M41-10 STG. OPS CK GOOD.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 26,948 hrs · 23,270 cycles

SMOKE CARGO WARNING MESSAGE IN FLIGHT, MSG LASTED 3 SECONDS THEN EXTINGUISHED. COMPLIED WITH INSP OF CARGO AND SMOKE DETECTIONS. C/W OPS CHECK OF CARGO SMOKE DET. C/W OPS CHECK OF CARGO SMOKE DET SYSTEM, NO DEFECTS NOTED, OK IAW AMM26-15-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,914 hrs · 23,233 cycles

F/A'S FLASHLIGHT INOPERATIVE, REPLACED WITH CAPTAINS.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 26,485 hrs · 22,772 cycles

NR 2 CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED EMERGENCY LIGHT. OPS CHECK GOOD IAW AMM 33-51-00.

Part: PLACARD — MISSING (CABIN) · airframe 25,869 hrs · 22,048 cycles

EXIT PLACARD ON ASD RELEASE HANDLE RELEASE HANDLE MISSING. R & R ASD HANDLE EXIT PLACARD IAW AMM 33-51-09. OPS CHECK GOOD. DMIL CLEARED.

Part: PLACARD — MISSING (PAX DOOR) · airframe 25,831 hrs · 22,004 cycles

EXIT PLACARD ON PASSENGER DOOR RELEASE HANDLE MISSING. REPLACED PLACARD IAW AMM 33-51-09.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 24,496 hrs · 20,469 cycles

NOSE GEAR REMAINED DOWN AND LOCKED AFTER GEAR RETRACTION. ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED. REMOVED AND REPLACED NLD CENTERED/EXTENDED PROXIMITY SENSOR BRACKET, OPERATIONAL CKS GOOD, IAW CMM 32-20-04.

Part: BULKHEAD — CRACKED (BS 202) · airframe 23,831 hrs · 19,770 cycles

POSSIBLE CRACK ON 202 BULKHEAD AT BRAKE CABLE HOLE. REMOVED Z-ANGLE AND BRACKET ON 202 BULKHEAD TO DO CUT OUT AND REPAIR. FABRICATED REPAIR PARTS AND INSTALLED PER REO 601R-53-11-563. COMPLIED WITH OPS CHECKS IAW CRJ 200 AMM 32-30-00, 32-51-00 AND 32-45-00, OPS CHECKS GOOD.

Part: FITTING — CRACKED (BS 621) · airframe 23,831 hrs · 19,770 cycles

AFT PRESSURE WEB FS 621.00 THERE IS A CRACKED FITTING AT LOWER LEFT INTERCOSTAL NR 7 AFT SIDE OF BULKHEAD. REMOVED AND REPLACED THE LT 625 INTERCOSTAL CLIP ON THE FS 621 AFT PRESSURE BULKHEAD IAW SRM 51-42-20.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,831 hrs · 19,770 cycles

CABIN SEAT TRACKS CORRODED IN SEVERAL LOCATIONS. REMOVED AND REPLACED SEAT TRACKS P/N 601R31032-15 AT RBL/LBL 9 FS 364 THRU 399 PER AMM 51-01-11-420-001 PART B. TRACK ON LBL 9 BLENDED FOUND TO BE WITH IN LIMITS. LBL 9 TRACK FINISH (A044) PER CRJ 200 SRM 53-21-49 AND 53-31-49. REPLACED SEAT TRACK AT RBL 9 F.S 399 THRU 409 + 126 PER AMM 53-00-49.

Part: FRAME — CORRODED (BS 333) · airframe 23,831 hrs · 19,770 cycles

CORROSION FOUND ON FRAME FUS STA 333 AT STRINGER 24R. REMOVED 1 EA RIVET, REMOVED CORROSION AND REINSTALLED 1 EA RIVET IAW SRM 53-21-15 AND 51-42-06.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,831 hrs · 19,770 cycles

IN REFERENCE TO TASK CARD AWL2 53-41-201. FRAME CAP ANGLE BEND RADIUS CRACKED BELOW VERTICAL BEAM AT LBL 18.00 AND RBL 18.00 LOCATED AT FS 559.00. REPAIRED 601R-53-41-559 LBL & RBL IAW REO 601R-53-41-260.

Part: DRAG ANGLE — CRACKED (ASD) · airframe 23,831 hrs · 19,770 cycles

ASD AFT SIDEWALL DRAG ANGLE CRACKED. COMPLIED WITH REO 601R-52-11-513 FOR DRAG ANGLE REPAIR. JOB COMPLETE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,831 hrs · 19,770 cycles

EMERGENCY EXIT LIGHT AT ASD INOP. REPLACED EMERGENCY LIGHT AT ASD IAW AMM 33-51-19. COMPLIED WITH CHECK OK. NO DEFECTS FOUND. JOB COMPLETE

Part: UNKNOWN — ODOR (CABIN) · airframe 22,270 hrs · 18,260 cycles

HAD ELECTRIC BURNING ODOR IN FLIGHT (ATL-SRY). DIVERTED INTO KCRW UPON LANDING F/A TOLD US THE INDICATOR LIGHTS FOR THE POT-WATER WERE OFF AND COFFEE POT WAS INOP. CAPTAINS MFD FLICKERED 3 TIMES IN FLIGHT. ENROUTE TO SYR A/C DIVERTED TO CRW DUE TO MTC, EMERGENCY DECLARED. POTABLE WATER SYSTEMS, LAVATORY POTABLE WATER CONSIDERED INOPERATIVE AND SINK PLACARED.

Part: SIGN — DAMAGED (EMERGENCY LIGHT) · airframe 21,935 hrs · 17,955 cycles

EXIT SIGN BY SERVICE DOOR OUT / DAMAGED. R&R EXIT SIGN ASSY AT TOP SERVICE DOOR IAW CRJ 200 AMM 33-51-13. OPS CHECK GOOD.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 21,792 hrs · 17,823 cycles

PAX DOOR HANDLE BROKEN COMPLETELY SHEARED OFF. GATE RETURN. R&R PAX DOOR OUTER HANDLE IAW AMM 52-11-03.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 2,123,544 hrs · 17,348 cycles

EMERGENCY FLOOR TRACK LIGHTING LAMPS ROWS 9 TO 12 AND LT AND RT AFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED NR 4 AFT BATTERY PACK ASSEMBLY AND BATTERY CHARGER ASSEMBLY IAW CRJ 200 AMM 33-51-04. OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: LATCH — OUT OF ADJUST (PAX DOOR) · airframe 21,153 hrs · 17,272 cycles

PASSENGER DOOR HARD TO OPEN. FLT 4608 DEL 35 MINS. ADJUSTED DOOR LATCH CAM SPIGOTS IAW AMM 52-11-00. PASSENGER DOOR OPENS AND CLOSES NORMALLY. NO DEFECTS NOTED. ACFT OK FOR SERVICE. (S)

Part: DOOR — STIFF (MAIN PAX) · airframe 21,152 hrs · 17,271 cycles

PASSENGER DOOR HARD TO OPEN, HANDLE OPERATES OK. DOOR REQUIRES HARD PUSH TO OPEN. OPERATED PASSENGER DOOR. DIDN`T FIND ANY FAULTS. OPS CHECK GOOD IAW CRF-200 AMM 52-11-00. (S)

Part: DOOR — STIFF (MAIN PAX) · airframe 2,115,252 hrs · 17,271 cycles

PAX DOOR HARD TO OPEN. HANDLE OPERATES OK, DOOR REQUIRES HARD PUSH TO OPEN. PERFORMED OPS CHECK OF PAX DOOR PER AMM 52-10-00. NO DEFECT NOTED. (B)

Part: MECHANISM — LACK OF LUBE (DOOR HANDLE) · airframe 2,112,016 hrs · 17,248 cycles

PAX DOOR VERY DIFFICULT TO OPEN AND CLOSE. LUBRICATED PAX DOOR LATCH MECHANISM, OPS CHECK GOOD IAW CRJ-200 AMM 52-11-02. ---[SDR CLOSED](B)

Part: DOOR — OBSTRUCTED (PAX DOOR) · airframe 21,049 hrs · 17,182 cycles

MAIN PAX DOOR STILL STICKING IN CLOSED POSITION, REQUIRES EXCESSIVE FORCE TO OPEN. FOUND BOTTLE CAP IN DOOR FRAME. REMOVED CAP, OPS CHECK GOOD REF CRJ-200MM 52-11-0.

Part: DOOR — BINDING (ASD) · airframe 20,951 hrs · 17,100 cycles

ASD HARD TO OPEN.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 20,930 hrs · 17,078 cycles

MAIN DOOR DIFFICULT TO OPEN. FLT 4653 DEL 20 MINS.

Part: HANDLE — BINDING (PAX DOOR) · airframe 20,928 hrs · 17,077 cycles

F/A UNABLE TO CLOSE PAX DOOR HANDLE, CAN ONLY BE CLOSE FROM OUTSIDE.

Part: HANDLE — STIFF (PAX DOOR) · airframe 20,271 hrs · 16,525 cycles

PAX DOOR OUTER HANDLE VERY HARD TO STOW FROM INSIDE.

Part: LIGHT — MISSING (CABIN) · airframe 20,226 hrs · 16,483 cycles

1 EMERGENCY LIGHT STRIP ON FLOOR MISSING.

Part: DOOR — JAMMED (PAX DOOR) · airframe 19,922 hrs · 16,229 cycles

PASSENGER DOOR HANDLE WILL NOT STOW FROM INSIDE. ALSO PASSENGER DOOR WILL NOT OPEN FROM INSIDE. DOOR IS JAMMED CLOSED. FLT 4705 DEL 38 MINS.

Part: HANDLE — STUCK (PAX DOOR) · airframe 19,711 hrs · 16,053 cycles

F/A REPORTS, CABIN DOOR HANDLE WOULD NOT GO ALL THE WAY UP. TOOK 4X TO GET DOOR OPEN.

Part: HANDLE — STUCK (PAX DOOR) · airframe 19,704 hrs · 16,048 cycles

CABIN DOOR HANDLE WILL NOT GO UP IN ORDER TO OPEN. FLT 4509 DEL 22 MINS.

Part: HANDLE — STIFF (PAX DOOR) · airframe 19,697 hrs · 16,042 cycles

MAIN AIRSTAIR DOOR HARD TO OPEN. WITH AP SHOWING 0.0 (AIRCRAFT DEPESSURIZED) THERE IS A PRESSURIZATION SPIKE & IT TAKES ABOUT 20 SECONDS FOR F/A TO OPEN THE DOOR. THE F/A STATED THAT THE HANDLE WON'T PULL FULLY UP.

Part: STOP PIN — CORRODED (ESCAPE HATCH) · airframe 19,622 hrs · 15,988 cycles

CORROSION ON COCKPIT ROOF CREW ESCAPE HATCH HINGE ARM STOP PINS. STOP PINS REMOVED IAW SRM 51-21-06 PINS STEEL SERVICABAE.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 19,622 hrs · 15,988 cycles

CORROSION FOUND ON TOP OF SEAT RAIL BETWEEN FS 364 AND 15.409 + 128 AT RBL 9 AND LBL 9. REMOVED CORROSION ON TOP OF SEAT RAIL BTW FS 364 & 409 + 128 AT RBL 9 & CBL 9 AS PER SRM 51-21-06 ALODINE APPLIED AS PER 51-21-11

Part: HANDLE — CRACKED (PAX DOOR) · airframe 19,622 hrs · 15,988 cycles

PAX DOOR INNER HANDLE CRACKED. NEW PAX DOOR INNER HANDLE INSTALL IAW SRM 51-41-04.

Part: SILL — CORRODED (BS 599) · airframe 19,622 hrs · 15,988 cycles

CORROSION FOUND ON LEFT FLOOR SILL BETWEEN FS 599 + 80 AND FS 559 + 112 RBL 45. REMOVED CORROSION AS PER IAW SRM 51-21-06 APLY FINISH CODE AS PER IAW SRM 51-21-16 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 53-00-00

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,622 hrs · 15,988 cycles

CRACK FOUND ON ANGLE AT FS 280 RBL 9 OUTBOARD. REF: REO 601R-53-00-027. NEW ANGLE AT FS 280 RBL 9 OUTBOARD INSTALL IAW SRM 51-42-20. SUPPLEMENTAL - SDR CLOSED 09/12/07.

Part: SHAFT — CORRODED (ESCAPE HATCH) · airframe 19,622 hrs · 15,988 cycles

CREW ESCAPE HATCH OUTER HANDLE SHAFT CORRODED. CREW ESCAPE HATCH REMOVED AND REPLACED AS PER CMM 52-22-03 - CREW ESCAPE HATCH HANDLE OPS TEST C/O IAW 52-22-03.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 19,622 hrs · 15,988 cycles

PRESSURE FLOOR FS 484.00 RIGHT BOTH ANGLE OF INTERCOSTAL FOUND CRACKED. REPAIRED AS PER REO 601R-53-41-059-REV-A

Part: LIGHT — BROKEN (CABIN) · airframe 19,622 hrs · 15,988 cycles

FLOOR EMERGENCY LIGHTS BROKEN BETWEEN ROWS 2 AND 3.

Part: STEP — CRACKED (AIRSTAIR DOOR) · airframe 18,227 hrs · 14,877 cycles

ASD BOTTOM STEP IS CRACKED.

Part: BUSHING — BROKEN (E/E BAY DOOR) · airframe 17,293 hrs · 14,145 cycles

FWD AVIONICS BAY DOOR HANDLE BUSHING IS BROKEN ALL THE WAY AROUND IT'S CIRCUMFERENCE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,399 hrs · 13,435 cycles

FIRST EXTERNAL EMERGENCY LIGHT FORWARD OF LT OVERWING EXIT INOP.

Part: ECU — MALFUNCTIONED (NLG STEERING)

DURING CLIMB-OUT FROM VLD-ATL, THE CREW RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH, AND REQUESTED EMERGENCY VEHICLES BE DISPATCHED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE RECALIBRATED THE NOSE WHEEL STEERING ECU WITH THE CURRENT RVDT VALUES IAW CRJ 200 AMM 32-51-00. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ENGINE — MALFUNCTIONED (LEFT)

DURING CLIMB, CREW RECEIVED A LT ENGINE LOW OIL PRESSURE WARNING TRIPLE CHIME, AND AN EICAS MESSAGE THAT WENT OUT IMMEDIATELY AFTER IT ILLUMINATED. THE LEFT ENGINE OIL PRESSURE INDICATION FLUCTUATED BETWEEN 20 TO 45 PSI. THE QRH WAS COMPLIED WITH AND THE LEFT THRUST LEVER WAS BROUGHT TO IDLE WHICH STABILIZED THE OIL PRESSURE AT 40 PSI. THE AIRCRAFT WAS PREPARED FOR A SINGLE ENGINE LANDING. EMERGENCY DECLARED. ARCFT DIVERTED INTO MCN, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. OPS CHECKS GOOD AIRCRAFT OK FOR SERVICE. LL CARBON SEALS IN THE ACCESSORY GEARBOX WERE FOUND TO BE LEAKING. MAINTENANCE REMOVED AND REPLACED ENGINE CARBON SEALS. (M)

Part: THRUST REVERSER — MALFUNCTIONED (LEFT)

FLT 4802 - DURING CRUISE FROM CVG-IAH, AT APPROXIMATELY 24,000 FEET, THE CREW RECEIVED A L REV UNLOCKED AMBER MESSAGE ALONG WITH AN ASSOCIATED REV AMBER ICON ON THE L N1 GAUGE AND THE LEFT EMER STOW SWITCH LIGHT ILLUMINATED. THE LEFT THRUST REVERSER HAD AUTOMATICALLY RETARDED AND THE CREW REDUCED THE RIGHT ENGINE TO IDLE IN COMPLIANCE WITH THE QRH FOR THE REMAINDER OF THE FLIGHT. AN EMERGENCY WAS DECLARED. WHEN DESCENDING AT APPROXIMATELY 8,000 FEET ALL ELECTRONIC INDICATIONS EXTINGUISHED. THE AIRCRAFT LANDED SAFELY IN IAH. MAINTENANCE PERFORMED GROUND POWER RUN-UPS WITH THE CREW WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ANGLE — CRACKED (BS 280)

DURING A C-CHECK IN HOT, THE LEFT OUTBOARD FS 280 ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD FS 280 ANGLE IAW CRJ200 SRM 51-42-21 AND 51-42-02. (M)

Part: RIB — CRACKED (LT WING)

DURING A C-CHECK IN HOT, THE LEFT BATT RIB ASSY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT BATT RIB ASSY AT WS 53.60 IAW ASA EO 600-57-039A. (M)

Part: DOOR FRAME — CRACKED (BS 338.9)

DURING A C-CHECK IN HOT, THE PASSENGER DOOR FRAME AND INNER SKIN AT FS 338.90, DOOR DATUM 1 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR FRAME AND INNER SKIN AT FS 338.90, DOOR DATUM 1 IAW ASA EO 600-52-0130. (M)

Part: BPSU — MALFUNCTIONED (T/E FLAP)

FLT 4563 - DURING FINAL APPROACH INTO XNA FROM ATL, THE CREW SELECTED THE FLAPS TO FIRTY FIVE DEGREES FROM THIRTY AND RECEIVED A FLAPS FAIL MESSAGE. THE AIRCRAFT PERFORMED A GO AROUND AND COMPLIED WITH THE QRH. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN XNA. MAINTENANCE REMOVED AND REPLACED THE BRAKE POSITION SENSOR UNIT, BPSU, AND THE POWER DRIVE UNIT. MAINTENANCE ALSO PERFORMED A TORQUE CHECK OF THE ACTUATORS. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN BTR, AN EMERGENCY FLOOR TRACK LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR TRACK FLEX LAMP STRIP AT THE FRONT END. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION IN ELP, THE BOTTOM STEP SUPPORT FITTING 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. (M)

Part: STEP — BROKEN (PAX DOOR) · airframe 12,486 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 IAW AMM 52-11.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING A GROUND INSPECTION, THE LT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (CABIN)

FLT 4583 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS TWO THROUGH SEVEN WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE EMERGENCY FLOOR LIGHT CONNECTORS BETWEEN ROWS TWO THROUGH SEVEN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD INTERCOSTAL SUPPORT BRACKET AT FS 484, RBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT OUTBOARD INTERCOSTAL SUPPORT BRACKET AT FS 484, RBL 36 IAW ASA EO 600-53-0137. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CABLE INTERCOSTAL BRACKETS AT FS 484, LBL 27 AND LBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CABLE INTERCOSTAL BRACKETS AT FS 484, LBL 27 AND RBL 36 IAW ASA EO 600-53-0098. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD FLOORBEAM CLIP AT FS 280, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLOORBEAM CLIP AT FS 280, RBL 9 IAW SRM 51-42-21. (M)

Part: ATTACH BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT INBOARD FLOORBEAM INTERCOSTAL ATTACH CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INBOARD FLOORBEAM INTERCOSTAL ATTACH CLIPS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-42-20. (M)

Part: FLOOR SUPPORT — CRACKED (FUSLEAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT AFT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: PLATE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO THRESHOLD FLOOR LANDING PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTNENANCE REPAIRED THE CARGO THRESHOLD FLOOR LANDING PLATE IAW ASA EO 600-53-0117. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE TOP AND LOWER STEPS ON THE PASSENGER DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP AND LOWER STEPS ON THE PASSENGER DOOR. (M)

Part: SUPPORT BEAM — CRACKED (ENGINE)

DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER CENTER UNDER THE FIRE LOOP BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER CENTER UNDER THE FIRE LOOP BRACKET IAW ASA EO 600-53-0072. (M)

Part: STEP — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONTROL HANDLE — MALFUNCTIONED (COCKPIT)

FLT 4531 - DURING APPROACH INTO ATL FROM FAY, AFTER EXTENDING THE LANDING GEAR, THE CREW RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES. THE CREW COMPLIED WITH QRH PROCEDURES AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE GEAR HANDLE ASSEMBLY AND PERFORMED TEN GEAR SWINGS WITHOUT ANY DEFECTS NOTED. OPS CHECKS GOOD. AIRCRAFT OK SERVICE. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

FLT 4726 - DURING A GROUND INSPECTION IN MSY, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MAIN AIRCRAFT BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (CABIN)

FLT 4425 - DURING A GROUND INSPECTION IN ATL, THE FORWARD EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOR FLEX LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING C-CHECK INSPECTION IN MCN, THE FIRST FLOOR TRACK EMERGENCY LIGHTING STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE SECTION OF EMERGENCY LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING C-CHECK INSPECTION IN MCN, A CRACK FOUND ON FRAME STATION 640 BETWEEN STRINGERS 13 RIGHT AND 14 RIGHT. MAINTENANCE REPAIRED THE CRACKED FRAME IAW ASA EO 600-53-0076. (M)

Part: CONNECTOR — DIRTY (CABIN)

FLT 4515 - DURING GROUN INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THAT ONE STRAP OF EMERGENCY FLOOR LEVEL LIGHTING WAS INOPERATIVE. MAINTENANCE CLEANED THE CONNECTOR ON THE INOPERATIVE STRIP OF EMERGENCY LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — BURNED OUT (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4632 - DURING GROUND INSPECTION IN ATL, EMERGENCY FLOOR LIGHTING WAS INOPERATIVE FROM ROW 8 AFT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING CABLE ASSEMBLY AND THE FLOOR LIGHTING STRIPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4519 - DURING GROUND INSPECTION IN ATL, CREW OBSERVED SEVERAL FLOOR EMERGENCY LIGHTS WERE BURNED OUT. MAINTENANCE REMOVED AND REPLACED SEVERAL FLOOR LIGHTS STRIPS WITH BURNED OUT BULBS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — CONTAMINATED (CABIN)

DURING GROUND INSPECTION IN ATL, CREW REPORTED RIGHT SIDE EMERGENCY STRIP LIGHTING INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED WATER FROM CONNECTION. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FLT 4587 - CREW REPORTED EMERGENCY LIGHTS CAME ON IN-FLIGHT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY UNIT. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X)