N825AS

Part: LIGHT — MISSING (CABIN) · airframe 37,389 hrs · 33,465 cycles

SHORT PORTION OF EMERGENCY LIGHT AT 18B MISSING. SECURED EMERGENCY LIGHT IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED.

Part: SCAVENGE PUMP — FAILED (OIL SYSTEM) · airframe 33,058 hrs · 29,546 cycles

RIGHT ENGINE OIL PRESSURE MASTER CAUTION AT 18000 FT. EMERGENCY DECLARED. R & R RT LUBE AND SCAVENGE PUMP IAW AMM 79-21-01. LEAK AND OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (OIL TRANDUCER) · airframe 33,079 hrs · 29,568 cycles

CLIMBING THROUGH FL 220, RECEIVED RT ENGINE OIL PRESSURE WARNING WITH OIL PRESSURE AT 15 PSI. OIL TEMPERATURE WAS NORMAL OIL PRESS READ NORMAL AFTER DESCENT. (ACFT RETURNED TO CAE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) FOUND RT ENGINE OIL TEMPERATURE BULB PRESSURE TRANSDUCER CONNECTOR PLUGS LOOSE. TIGHTEN CONNECTOR AND PERFORMED ENGINE RUNS AT POWER OF THE DAY IAW AMM-79-31-05, ALSO R & R RT ENGINE OIL TANK PRESSURE RELIEF VALVE ASSY IAW CMM-SEI-843, OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 32,847 hrs · 29,356 cycles

SERVICE DOOR SILL FLOOR SUPPORT ANGLE CORRODED. REPAIRED IAW AMM 20-21-00-910-001 AND 20-24-00-910-802.

Part: ANGLE — CRACKED (DOOR FRAME) · airframe 32,847 hrs · 29,356 cycles

NLG CUTOUT CORNERS CRACKED AFT OF FOLLOW -UP DOOR HINGES (RADIUS). REPAIRED IAW REO 601R-53-11-0048 IAW 601R-53-11-0048, REV C.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 32,847 hrs · 29,356 cycles

SEAT TRACK FS 409+128 TO 559.0 AT RBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK IS OUT OF LIMITS IAW SRM 51-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-807 AND AMM 53-01-11-400-802.

Part: ATTACH ANGLE — CRACKED (E/E BAY BULKHEAD) · airframe 32,847 hrs · 29,356 cycles

ATTACH ANGLE CRACKED AFT EQUIPMENT BAY RT SIDE AT PRESSURE BULKHEAD ABOUT 12 INCHES BELOW ENGINE SUPPORT BEAM. REMOVED CRACKED ATTACH ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE IAW SRM 51-42-21 AND REO 601R-53-61-985.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 32,847 hrs · 29,356 cycles

SEAT TRACK FS 394 TO 409+128 AT RBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK IS OUT OF LIMITS IAW SRM 53-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 32,851 hrs · 29,361 cycles

SERVICE DOOR SILL FWD UPPER ANGLE CORRODED. R & R CORRODED ANGLE IAW DWG NR 601R38303.

Part: ATTACH ANGLE — CRACKED (E/E BAY BULKHEAD) · airframe 32,847 hrs · 29,356 cycles

ATTACH FITTING CRACKED AFT EQUIPMENT BAY LT SIDE AT PRESSURE BULKHEAD ABOVE ENGINE SUPPORT BEAM. REMOVED CRACKED ATTACH ANGLE IAW SRM 51-42-06. LOCATED SERVICEABLE ATTACH ANGLE IAW STM 51-40-11. INSTALLED ATTACH ANGLE IAW SRM 57-42-22.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 32,847 hrs · 29,356 cycles

FS 280 BEAM ATTACH ANGLE CRACKED AT RBL 9.0 INBD. REMOVED ANGLE SRM 51-42-21-00. DRILLED NEW ANGLE IAW SRM 51-40-11, ALODINED IAW SRM 51-21-11. INSTALLED ANGLE IAW SRM 51-42-21-00, 51-25-06.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 32,847 hrs · 29,356 cycles

FLOORBEAM FS 280 HAS CORROSION DAMAGE. REMOVED CORROSION IAW SRM 51-21-06. REMOVED FLOORBEAM ANGLE IAW SRM 51-42-06. DRILLED NEW ANGLE IAW SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 364-396) · airframe 32,847 hrs · 29,356 cycles

SEAT TRACK FS 364 TO 396 AT RBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK OUT OF LIMITS IAW SRM 53-21-49, FIG 101. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SERVICEABLE SEAT TRACK IAW AMM TASK 53-01-11-400-802.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 32,847 hrs · 29,356 cycles

CORROSION AROUND NUTPLATE ON FS 280.00 FLOORBEAM. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PRODCEDURES UT-3. MIN MATERIAL REMAINING IS .035".

Part: SEAT TRACK — CORRODED · airframe 32,847 hrs · 29,356 cycles

SHORT SEAT TRACK BETWEEN FLOOR PANELS 281BLF AND 281FRF HAS CORROSION. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 32,847 hrs · 29,356 cycles

RIGHT FS 484 PRESSURE FLOOR INTERCOSTAL HAS CRACKED ATTACH FITTING AT RBL 27.0. REMOVED DAMAGED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE IAW SRM AND DWG NR 601R31171.

Part: SEAT TRACK — CORRODED (BS 364-396) · airframe 32,847 hrs · 29,356 cycles

SEAT TRACK FS 364-396 AT LBL 9.0 HAS CORROSION DAMAGE. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & AMM 53-01-11-420-001.

Part: SEAT TRACK — CORRODED · airframe 32,847 hrs · 29,356 cycles

SHORT SEAT TRACK HAS CORROSION AT LBL9 BETWEEN FLOOR PANEL 281HLF AND 281BLF. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-61-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-40-802.

Part: SUPPORT ANGLE — CORRODED · airframe 32,847 hrs · 29,356 cycles

SERVICE DOOR SILL FLOOR SUPPORT ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-26-00. .031" OF MATERIAL REMOVED- .026" MATERIAL REMAINING. REMOVED SILL SUPPORT ANGLE IAW SRM'S 51-42-06, 51-42-21, AND 51-42-13. INSTALLED NEW ANGLE IAW SRM 51-42-21 AND 51-42-13 AND 51-42-21.

Part: SEAT TRACK — CORRODED · airframe 32,847 hrs · 29,356 cycles

SEAT TRACK HAS CORROSION AT RBL 9 AT 9G BULKHEAD. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-21-49, FIG 101. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 32,847 hrs · 29,356 cycles

LEFT FS 484 PRESSURE FLOOR INTERCOSTAL HAS CRACKED ATTACH FITTING AT LBL 27.0. REMOVED AND INSTALLED NEW ATTACH FITTING IAW SRM 51-42-21.

Part: LIGHT — DAMAGED (CABIN) · airframe 32,847 hrs · 29,356 cycles

WARDROBE FLOOR EMERGENCY FLOOD LIGHT ASSY FOUND DAMAGED AND UNSERVICABLE. R & R WITH NEW LIGHT IAW AMM 33-51-19-400-807. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801, OPS TESTED GOOD.

Part: FAIRING — ERODED (LT WING ROOT) · airframe 32,847 hrs · 29,356 cycles

LEFT WING ROOT FAIRING 191BB, ERODED AT L/E AROUND SCREW HOLES. FOUND SCREW HOLES TO HAVE PAINT DELAMINATION WITH MINOR EROSION TO L/E, REPAIRED IAW SRM 51-14-06-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,847 hrs · 29,356 cycles

CABIN FLOOR EMERGENCY LIGHT FROM ROW 4 FWD, DOES NOT ILLIMINATE AFTER CHARGE. INSTALLED NEW LIGHT UP TO ROW 10 IAW AMM 33-51-01-400-806.

Part: PROXIMITY SENSOR — OUT OF RIG (NLG) · airframe 32,202 hrs · 28,760 cycles

RECEIVED NLG DOOR DISAGREE INFLIGHT. MAIN GEAR WENT UP NOSE GEAR WOULD NOT GO UP . FOLLOWED QRH , USED MLG MANUEL RELEASE HANDLE TO LOWER GEAR & ALL INDICATIONS GREEN. ACFT RETURNED TO DEPARTURE & EMERGENCY DECLARED. R & R NLG SELECTOR VALVE IAW AMM 32-33-10. LEAK CHECKED GOOD. OPS CHECKED BAD. NLG REMAINS INOPERATIVE. FOUND NLG OLEO CENTERED & EXTENDED. PROXIMITY SENSOR OUT OF RIG, REGAPPED PROXIMITY SENSOR IAW AMM 32-61-05. PERFORMED FUNCTIONAL TEST IAW AMM 32-30-00, OPS CHECKED GOOD.

Part: DOOR — BINDING · airframe 31,242 hrs · 27,890 cycles

AIR STAIR DOOR WILL NOT OPEN ARRIVING AT GATE. OPS CHECKED PAX DOOR IAW AMM 52-11-00. NO DEFECTS NOTED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 31,014 hrs · 27,705 cycles

LT AFT EXTERNAL EMERGENCY LIGHT IS INOP. R & R LT AFT EXT EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,929 hrs · 27,624 cycles

RT AFT EXTERNAL EMERGENCY LIGHT IS INOP. R & R RT AFT EMERGENCY LIGHT BULB IAW AMM 33-51-21. OP'S CHECKED GOOD, R & R RT AFT EMERGENCY LIGHT BULB IAW AMM 33-51-21. OP'S CHECKED GOOD. (CLOSED)

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 28,505 hrs · 25,462 cycles

REMOVED FS 280 CLIPS AT LBL 9.0 INBD & OTBD IAW SRM 51-42-21. FS 280 CLIPS AT LBL 9.0 INBD & O/B REQUIRE INSTALL. J.SINGLETON 3/23/10 REINSTALLED CLIPS FS 280 & LBL 9.0 I/B, 7 OTBD IAW SRM 51-42-21, STEP 9. REPAIRED FS 280 FLOOR SUPPORT ANGLE AT LBL 9 BOTTOM IAW REO 601R-53-11-171. ALSO R & R SECTION OF UPPER ANGLE FS 280, LBL 9 IAW SRM 51-42-21 & 51-42-06. EC/TC REQUIRED FOR REO 601R-53-11-171. COMPLIED WITH EC/TC REO 601R-53-11-171 AND MET ALL THE REQUIREMENTS OF REO 601R-53-11-171.

Part: FINGER DOUBLER — CORRODED · airframe 28,505 hrs · 25,462 cycles

FINGER DOUBLER CORRODED. C/W REO 601R-53-41-666 REV A DATED NOV. 3, 2009 AS WRITTEN.

Part: POST — CRACKED (BS 409) · airframe 28,505 hrs · 25,462 cycles

FOUND FS 409+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH AT WL 64.0 AFT FLANGE RADIUS. FAILED NDT INSPECTION. LOOSENED HYD LIEN ADEL CLAMPS AT 6 LOCATIONS, ADJACENT TO FS 409+128 RBL 18 POST FOR ACCESS IAW SRM 51-41-02. RESECURED ADEL CLAMPS. REMOVED POST AT FS 409.0+128 RBL 18.0 IAW SRM 51-42-06 DRILLED/LOCATED NEW SERVICEABLE OTBD SIDE POST IAW SRM 51-40-06. INTALLED POST ASSY AT FS 409+128, RBL 18 WITH EXCEPTION OF 15 EA RIVETS AT TOP OF ASSY IAW SRM 51-42-22 AND C/W EC/TC REO 601R-53-41-889 AND MET ALL REQUIREMENTS OF REO 601R-53-41-889 REV A. INSTALLED 15 EA RIVETS AT TOP OF POST ASSY. ATTACHED HYD LINE CLAMPS TO POST IAW SRM 51-41-02.

Part: FINGER DOUBLER — CORRODED (BS 409-559) · airframe 28,505 hrs · 25,462 cycles

MAIN CABIN BETWEEN FS 409+128 AND FS 559.00 PRESSURE FLOOR SILL AND FINGER DOUBLER HAVE CORROSION IN NUMEROUS AREAS ON LT SIDE. (OPEN)

Part: POST — CRACKED (BS 409) · airframe 28,505 hrs · 25,462 cycles

FOUND FS 409+128 VERTICAL POST LBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 64.0 AFT FLANGE RADIUS. FAILED NDT INSPECTION. DISCONNECTED A/C CABIN AIR DUCT. REMOVED INBD AND OTBD POST. LOCATED & DRILLED OTBD POST IAW SRM 51-42-06. LOCATED AND DRILLED INBD POST. INSTALLED INBD AND OTBD POST IAW SRM 51-42-06. PAINTED POST ASSY IAW SRM 51-25-01. INSTALLED POST IAW SRM 51-42-06. C/W EC/TC REO 601R-53-41-889 AND MET ALL REQUIREMENTS OF REO 601R-53-41-889. RECONNECTED A/C FLEX DUCT.

Part: FINGER DOUBLER — CORRODED · airframe 28,505 hrs · 25,462 cycles

FINGER DOUBLER CORRODED. C/W REO 601R-53-41-666 REV A DATED NOV. 3, 2009 AS WRITTEN.

Part: FRAME — CORRODED (BS 319 S26R) · airframe 28,505 hrs · 25,462 cycles

FRAME CORRODED AT FS 319 STG-26R FWD SIDE. UPON FURTHER INVESTIGATION FOUND FRAME AT FS 319, STA 26R FWD SIDE TO BE OUT OF LIMITS WITH .008 MATERIAL LOSS BEFORE CORROSION WAS REMOVED IAW SRM 51-21-15 AND 53-00-00. FRAME AT FS 319, STR 26R, REQUIRES REPLACEMENT. REMOVED DAMAGED FRAME AT FS 319 BETWEEN STR 24L & 24R IAW SRM 51-42-06 & SRM 51-42-21. NEW FRAME REQUIRED. INSTALLED NEW FRAME AT FS 319 BETWEEN STR 24L & 24R IAW SRMS 51-42-06 AND 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,505 hrs · 25,462 cycles

JOB 8720721, OPERATION 374 / FS 280 FLOOR SUPOORT ANGLE AT LBL 9 OTBD UNDER ALTERNET EXTENSION PULLEY BRACKET CRACKED TOP AND BOTTOM. (OPEN)

Part: SILL — CORRODED (BS 409-555) · airframe 28,505 hrs · 25,462 cycles

MAIN CABIN RT SIDE BETWEEN FS 409+128 AND FS 555.00 PRESSURE FLOOR SILL AND FINGER DOUBLER HAVE CORROSION IN NUMEROUS AREAS. (OPEN)

Part: FRAME — CORRODED (BS 364 S26R) · airframe 28,505 hrs · 25,462 cycles

FRAME CORRODED AT FS 364 STG 26R FWD SIDE. REMOVED CORROSION FROM FRAME FS 364, STR 26R ON FWD SIDE IAW SRM 51-21-06. REMOVING ONE BOLT TO ACCESS CORROSION IAW SRM 51-41-02 AND FOUND TO BE WITHIN LIMITS WITH OEM 0.080 AND MATERIAL LOSS TO BE 0.006 IAW SRM 53-21-15 AND 53-00-00. TREATMENT OF EXPOSED AREAS AND REINSTALLATION OF BOLT AT FS 364 STR 26R. ALL EXPOSED AREAS WERE TREATED IAW SRM 51-25-06 AND THE BOLT WAS INSTALLED AND TORQUED IAW SRM 51-41-04. REPAIRED AREAS REQUIRED PAINT AND DINITROL. PAINTED EXTERNAL AREAS IAW SRM 51-25-06. APPLIED DINITROL TO INTERNAL REPAIRED AREA IAW SRM 51-21-11.

Part: FLOORBEAM — CORRODED (BS 319) · airframe 28,505 hrs · 25,462 cycles

FLOOR SUPPORT ANGLE AT RBL 36 JUST AFT OF FS 319 HAS CORROSION. UPON FURTHER INVESTIGATION FOUND FLOOR SUPPORT ANGLE AT RBL 36 TO BE OUT OF LIMITS WITH 0.012 MATERIAL LOSS BEFORE CORROSION REMOVAL IAW SRM 53-21-43 AND 53-00-00. ANGLE REQUIRES REPLACEMENT. R & R SUPPORT ANGLE IAW SRM'S 51-42-06, 51-42-11 AND 51-42-21.

Part: DOOR — NO TEST (EMERGENCY EXIT) · airframe 28,505 hrs · 25,462 cycles

LEFT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST & IS CONTACTING UPPER LATCH PIN FITTING. ADJUSTED LT OVERWING EMER EXIT IAW AMM 52-21-00-820-801. LT OVERWING EMERGENCY EXIT FUNCTIONAL TEST GOOD IAW AMM 52-21-00-720-801. PRESSURIZED ACFT IAW MM 21-32-00-863-801. LEAK CHECK OF RT OVERWING LINER EXIT GOOD AT THIS TIME. STEPS 4A(4-6) STILL NEED C/W. AMM 52-21-00-720-801 STEPS 4A(4-6). SYS WORKING PROPERLY.

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 28,505 hrs · 25,462 cycles

RIGHT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST. ADJUSTED RT OVERWING EMERGENCY EXIT IAW AMM 52-21-00-820-801. RT OVERWING EMER EXIT FUNCTIONAL TEST GOOD IAW AMM 52-21-00-720-801. STESP 4A(4-6) ON AMM 52-21-00-720-801. PRESSURIZED ACFT IAW MM 21-32-00-863-801. LEAK CHECK OF RT OVERWING LINER EXIT GOOD AT THIS TIME. SYS WORKING PROPERLY.

Part: BULKHEAD — CRACKED (BS 202) · airframe 27,804 hrs · 24,683 cycles

SUSPECT FS 202.00 BULKHEAD TO BE CRACKED

Part: DOOR — STUCK (MAO PAX) · airframe 27,763 hrs · 24,636 cycles

FLT 5053. PAX DOOR CAN NOT BE OPENED FROM THE OUTSIDE. THE HANDLE POPS OUT BUT WILL NOT TURN.

Part: FRAME — CRACKED (BS 559) · airframe 27,728 hrs · 24,599 cycles

FRAME CAP ANGLE LOCATED AT FS 559.00, LBL 18.00, IS CRACKED IN RADIUS. ACCOMPLISHED IAW EC/TC REO 601R-53-41-260-AND EC/TC & REO 601R-53-41-609 02

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 27,693 hrs · 24,556 cycles

FLAPS FAIL ON APPROACH AT 30, EMERGENCY DECLARED. SUSPECT SKEW DETECTION SYSTEM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,599 hrs · 24,469 cycles

TWO OUTSIDE AFT OVERWING EMERGENCY LIGHTS AND TWO CENTER EMERGENCY LIGHTS INOP.

Part: TAB — DEFECTIVE (SERVICE DOOR) · airframe 25,698 hrs · 22,668 cycles

UNABLE TO OPEN SERVICE DOOR BY USING OUTSIDE RELEASE HANDLE (TAB NOT RELEASING HANDLE).

Part: FIRE LOOP — OUT OF POSITION (ENGINE) · airframe 25,041 hrs · 22,098 cycles

CLIMBOUT APPROX 12K FT RECEIVED MASTER WARNING L 14TH DUCT WARNING. INITIALLY CAME ON, THEN WENT OUT, THEN CAME ON AGAIN. RAN QRH WARNING RETURNED. RAN QRH. (RETURN TO BTR, CAPTAIN DECLARED EMERGENCY). FLT 4816 DEL 265 MINS. INSPECTION OF LT 14TH STAGE DUCT AND BLEED LEAK DETECTION SYSTEM REVEALED LEAK DETECTION LOOP FOULING ON STRUCTURE WITHIN PYLON AREA. REPOSITION LOOP AND OPS CHECKED SYSTEM IAW AMM 36-21-00. NO FURTHER DEFECTS NOTED AT THIS TIME. (S)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

CORROSION ON FLOOR SUPPORT STA 310 TO 349 AT ASD SILL. REMOVED FASTENERS ON LOWER SILL ANGLE AND UPPER ATTACH ANGLE. REMOVED UPPER ATTACH ANGLE IAW SRM 51-42-06. REMOVED FLOOR SUPPORT ANGLE . DRILLED NEW SUPPORT ANGLE 601R31527-221 IAW SRM 51-40-11. READY TO INSTALL. INSPECTED PARTS AT FLOOR SUPPORT. OK TO INSTALL. INSTALLED ASD SILL & ANGLE FOR FLOOR SUPPORT PER SRM 51-42-06. SEALED, PRIMED, AND PAINTED ASD SILL LOWER AND UPPER ANGLES & ASSOCIATED FASTNER PER SRM 51-25-00 AND 51-23-00.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

VERTICAL BEAMS AT FS 409.0+128 (WING BOX FWD BULKHEAD) CRACKED IN THE RADIUS ON THE BOTTOM OUTBOARD SIDE AT LBL-18 AND INBOARD SIDE AT LBL 27. JOB COMPLETE. REPAIRED VERTICAL BEAMS AT FS 409.0+128 AT LBL-18 AND AT LBL-27 AS PER REO 601R-53-41-056. CUT OUT DAMAGE ON LBL 27 AND LBL 18 IAW REO 601R-53-41-08. PERFORMED EDDY CURRENT INSPECTION OF CUT LINES PER MTC REQUEST IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FABRICATED REPAIR ANGLE -5 AND FILLER -7 AT LBL 18.0 FS 409 & 128 PER REO 601R-53-41-056. PICK UP ALL HOLES ON NEW REPAIR PARTS ALL WORK IAW REO 601R-53-41-056. INSTALLED REPAIR PARTS LBL 27 & LBL 18 FILLET SEALED AND RESTORED FINISH PER REO 601R-53-41-056. JOB COMPLETE. SUPPLEMENTAL SDR CLOSED 4/28/08.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

FS 280 CLIP CRACKED AT LBL 9.0 OUTBOARD.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

CARGO COMPT DOOR TRACK CROSSBEAM HAS CRACKED ATTACH FITTING AT AFT PRESSURE BULKHEAD. REMOVED AND REPLACE ATTACH FITTING PER SRM 51-42-20.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

FS 280 FRAME UPPER AFT ANGLE CRACKED AT RBL 12.0. JOB COMPLETE. STARTED REMOVING FS 280 UPPER ANGLE AT RBL 12.0 PER CRJ 200 SRM 51-42-20. REPAIRED J-ANGLE ON THE PILOT`S BULKHEAD AT FS 280.0 RT BL 9.0 IAW EO 600-53-0091. PERFORMED ET INSPECTION OF CUT LINES AT FS 280 IAW REO 601R-53-11-136 PER CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. 4/18/08. FABRICATED -3 AND -4 SPLICE ANGLES OUT OF 7075 -0 .050" BATCH 511928, PO 20040439. HEAT TREATED -3 & -4 SPLICE ANGLES TO +62 CONDITION AS PER CRJ 200 SRM 51-24-06 IAW REO 601R-53-11-136. HARDNESS TEST GOOD. FINAL TRIMMED, DRILLED, AND FINISHED -3, -4, AND -1 REPAIR PARTS IAW REO 601R-53-11-136. OK TO INSTALL. INSTALLED ALL 280 REPAIR PARTS INCLUDING RBL 9 INBOARD AND OUTBOARD CLIPS. FINISHED SURFACE AND APPLIED CIC. REINSTALLED DRIP TRAY. WORK DONE IAW REO 601R-53-11-136. JOB COMPLETE. SUPPLEMENTAL SDR CLOSED 4/21/08.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

AFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING. REPAIRS PERFORMED IN ACCORDANCE WITH REO 601R-53-61-1230.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

LEFT CABIN FLOOR SEAT RAIL STARTING AT FS 379.00 HAS CORROSION DAMAGE.

Part: SEAT TRACK — CORRODED (BS 394) · airframe 24,781 hrs · 21,854 cycles

LEFT CABIN FLOOR SEAT TRACK STARTING AT FS 394.00 HAS CORROSION DAMAGE. REMOVED CORROSION FROM SEAT TRACK. BLENDED OUT OF LIMITS PER 53-21-49.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

SURFACE CORROSION ON LT PRESSURE FLOOR LANDING FS 484.00 AT LBL 45. REMOVED PRESSURE FLOOR LANDING FS 484 LBL 45 PER SRM 53-41-45. COMPLIED WITH UT THICKNESS CHECK OF BLENDED AREAS IAW NDTM 51-20-04. FOUND BLENDED AREA MINIMUM THICKNESS TO BE .068". PERFORMED EDDY CURRENT INSPECTION OF BLENDED AREAS IAW NDTM 51-20-06. NO DEFECTS NOTED. BLENDOUT IS OUT OF LIMITS IAW SRM 53-41-45. MAPPED DAMAGE & SUBMITTED PER SRM 51-13-00. R & R FASTENERS IN BLENDED AREA PER REO 601R-53-41-714, PRIMED & PAINTED PER SRM 51-25-00. APPLIED A FILLET SEAL & CIC TO REWORK AREA. COMPLIED WITH EC/TC REO 601R-53-41-714.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

STA 280 FWD SUPPORT ANGLE HAS CORROSION.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

SURFACE CORROSION ON LEFT PRESSURE FLOOR LANDING FS 449.85 AT LBL 45. REMOVED CORROSION PER SRM 53-41-45. COMPLIED WITH UT THICKNESS CHECK IAW NDTM 51-20-04. FOUND BLENDED AREA MINIMUM THICKNESS TO BE .068". PERFORMED EDDY CURRENT INSPECTION OF BLENDED AREAS IAW NDTM 51-20-06. NO DEFECTS NOTED. BLENDOUT OUT OF LIMITS IAW SRM 53-41-45. MAPPED DAMAGE & SUBMITTED PER SRM 51-13-00. R & R FASTENERS PER REO 601R-53-41-714, PRIMED AND PAINTED PER SRM 51-25-00. APPLIED A FILLET SEAL &CIC TO REWORK AREA. COMPLIED WITH EC/TC REO 601R-53-41-714.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

AFT PRESSURE BULKHEAD CRACKED JUST ABOVE CARGO DOOR TRACK. REPAIRED PER REO 601R-53-61-1541 AND REO 601R-53-61-2599. REMOVED FASTENERS AS REQUIRED PER REO 601R-53-61-1541. CUT OUT DAMAGED AREA AS SHOWN PER REO 601R-53-61-1541. PERFORMED ET INSPECTION OF REWORKED AREA PER REO 601R-53-61-1541 IAW NDTM 51-20-06. NO DEFECTS NOTED. TOUCHED UP EDGES PER REO 601R-53-61-1541. FABRICATED DOUBLERS AND FILLERS PER REO 601R-53-61-1541. PERFORMED ET INSPECTION OF REWORKED WEB IAW CAR 38413 PER CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. OK TO INSTALL REPAIR PARTS PER REO 601R-53-61-1541. JOB COMPLETE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

RIGHT CABIN FLOOR SEAT RAIL STARTING AT FS 394.00 HAS CORROSION DAMAGE. JOB COMPLETE. BLENDED AREAS OF CORROSION STARTING AT FS 394.00 TO WITHIN LIMITS & ALODINED BLENDED AREAS PER CRJ 200 SRM 53-21-49 SP 7025126 04/18/2008. SUPPLEMENTAL SDR CLOSED 4/21/08.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

RIGHT CABIN FLOOR SEAT RAIL STARTING AT FS 379.00 HAS CORROSION DAMAGE. JOB COMPLETE. BLENDED AREAS OF CORROSION STARTING AT FS 379.00 TO WITHIN LIMITS & ALODINED BLENDED AREAS PER CRJ 200 SRM 53-21-49 SP 7025126 04/18/2008. SUPPLEMENTAL SDR CLOSED 4/21/08.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

FS 280 INBOARD BRACKET CRACKED AT LBL 9.0 (MARKED).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,781 hrs · 21,854 cycles

SEVERAL SEAT TRACKS IN CARGO COMPARTMENT HAVE CORROSION DAMAGE. JOB COMPLETE. REMOVED SEAT TRACKS AND INSTALLED NEW IAW CRJ200 SRM 53-41-49 COMPLETE. SUPPLEMENTAL SDR CLOSED 4/21/08.

Part: COVER — BROKEN (EMERGENCY LIGHTS) · airframe 24,503 hrs · 21,618 cycles

EMERGENCY LIGHT COVER (FLOOR) BROKE OFF AROUND ROW 5.

Part: PLACARD — UNSECURE (CABIN) · airframe 24,503 hrs · 21,618 cycles

FLIGHT ATTENDANT REPORTS "EXIT" PLACARD ON MAIN CABIN DOOR IS UNSECURE, FLT 4429 DEL 29 MINS.

Part: FLAP — FAILED (WING) · airframe 24,412 hrs · 21,547 cycles

ON APPROACH, FLAPS FAIL AT ZERO. EMERGENCY DECLARED. FLT 4892 CX.

Part: DOOR — BINDS (AIRSTAIR DOOR) · airframe 23,354 hrs · 20,637 cycles

UNABLE TO OPEN ASD. FLT 4306 CX.

Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 23,119 hrs · 20,428 cycles

ON COCKPIT CHECK, EMERGENCY LIGHTS WOULD NOT INDICATE ON STATUS.

Part: DOOR — BINDING (MAIN PAX) · airframe 23,105 hrs · 20,419 cycles

MAIN PAX DOOR DIFFICULT TO OPEN.

Part: DOOR — STIFF (MAIN PAX) · airframe 22,974 hrs · 20,318 cycles

PAX DOOR DIFFICULT TO OPEN, HANDLE DIFFICULT TO STOW.

Part: UNKNOWN — BINDING (PAX DOOR) · airframe 22,921 hrs · 20,275 cycles

F/A REPORTS MAIN DOOR HARD TO CLOSE AND LOCK PROPERLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,880 hrs · 20,244 cycles

CEILING EMERGENCY LIGHT ABOVE LAV DOOR INOP.

Part: DOOR — UNLOCKED (PAX DOOR) · airframe 22,264 hrs · 19,772 cycles

PAX DOOR LOCK NOT LOCKING. FLT 4273 DEL 35 MINS.

Part: FRAME — CORRODED (BS 349) · airframe 21,925 hrs · 19,517 cycles

LOWER SEGMENT OF FRAME 349 IS CORRODED. FOUND LOWER FRAME SEGMENT CORROSION TO BE OUT OF LIMITS OF THE SRM, REMOVED FRAME SECTION REF RJ200SRM 51-42-06 AND 53-00-15. INSTALLED FRAME, DRILLED AND REMOVED FRAME AND DE-BURRED IAW SRM 51-42-06 21. INSTALLED FRAME IN AIRCRAFT WET WITH SEALANT AND INSTALLED FASTENERS IN FRAME SPLICES AT S23L AND S23R REF CRJ200 SRM 51-42-21. COMPLETED INSTALLING FS 349 FRAME SEGMENT (EXCEPT FASTENERS COMMON TO SKIN) IAW SRM 51-42-06. INSTALLED FASTENERS COMMON TO SKIN REF CRJ200 SRM 51-42-06. FOUND LOWER FRAME SEGMENT CORROSION TO BE OUT OF LIMITS OF THE SRM, REMOVED FRAME SECTION REF CRJ200SRM 51-42-06 AND 53-00-15. INSTALLED FRAME, DRILLED AND REMOVED FRAME AND DE-BURRED IAW

Part: FRAME — CORRODED (BS 333) · airframe 21,925 hrs · 19,517 cycles

LOWER SEGMENT OF FRAME 333 IS CORRODED. FOUND LOWER FRAME SEGMENT CORROSION TO BE OUT OF LIMITS OF THE SRM, REMOVED FRAME SECTION REF CRJ200SRM 51-42-06 AND 53-00-15. DRILLED UP NEW SECTION OF FRAME AND TRANSFERED FAILSAFE ANGLE TO NEW FRAME REF CRJ 200 SRM 51-42-06. INSTALLED FRAME IN AIRCRAFT WET WITH SEALANT AND INSTALLED ALL FASTENERS EXCEPT THE FASTENERS THAT ARE COMMON TO THE SKIN REF CRJ200 SRM 51-42-21. INSTALLED FASTENERS COMMON TO SKIN REF CRJ200 SRM 51-42-06. COMPLIED WITH RII INSPECTION IAW SP 607 AND SRM 51-42-06. CLOSED 01/03/07.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,925 hrs · 19,517 cycles

ON CLIMBOUT STRONG ODOR POSSIBLY ACIDIC/ELECTRICAL FOR ABOUT 2 MINUTES FOLLOWED BY A COOL EXHAUST FAIL STATUS MSG. ODOR CLEARED ALMOST IMMEDIATELY AFTER.

Part: STEP — BROKEN (AIRSTAIR) · airframe 21,439 hrs · 19,143 cycles

ASD BTM STEP BROKEN.

Part: ANCHOR FITTING — CORRODED (FUSELAGE) · airframe 20,672 hrs · 18,526 cycles

CORROSION FOUND ON ASD AFT SWIVEL ANCHOR SERRATED PLATE BASE (BASE PLATE).

Part: FLOOR SUPPORT — CORRODED (BS 559-589) · airframe 20,672 hrs · 18,526 cycles

CORROSION FOUND AROUND NUTPLATES ON CARGO FLOOR ATTACH WEB AT LBL36 BETWEEN FS 559+96 AND FS 589. REPAIRED CORROSION IN CARGO BAY IAW SRM 51-21-11 AND REO 601R-53-61-1807

Part: CLIP — CRACKED (BS 454) · airframe 20,672 hrs · 18,526 cycles

LT FS STA 484 IB AND OB CLIPS APPEAR CRACKED.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 20,672 hrs · 18,526 cycles

FOUND CORROSION ON LT SIDEWALL SEAT TRACK AT FUS STA 409+16 APPROX .

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 20,672 hrs · 18,526 cycles

CORROSION FOUND AT NUMEROUS LOCATION ON RT PRESSURE FLOOR DOUBLER. REPAIRED IAW REO 601R-53-41-415.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 20,672 hrs · 18,526 cycles

CORROSION FOUND AT SEVERAL LOCATIONS AT LT PRESSURE FLOOR DOUBLER. REPAIRED IAW REO 601R-53-41-414.

Part: CLIP — CRACKED (BS 484) · airframe 20,672 hrs · 18,526 cycles

FOUND RT FS 484 IB CLIP APPEARS CRACKED.

Part: SEAT TRACK — CORRODED (BS 529) · airframe 20,672 hrs · 18,526 cycles

FOUND CORROSION ON RT IB SEAT TRACK AT FS 529 APPROX.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 20,672 hrs · 18,526 cycles

FOUND CORROSION ON LT IB SEAT TRACK AT APPROX FUS STA 559+64.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,672 hrs · 18,526 cycles

FOUND STA 280 AFT FLOORBEAM ANGLE IS CRACKED OB OF LBL 9 TWO PLACES. REPAIRED IAW REO 601R-53-11-1002.

Part: BULKHEAD — CRACKED (BS 280) · airframe 20,672 hrs · 18,526 cycles

FOUND STA 280 BULKHEAD WEB IS CRACKED OB OF RBL 9. REPAIRED IAW EO 600-53-90. (CLOSED)

Part: BUSHING — UNKNOWN (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND TO BE DIFFICULT TO OPEN. MAINTENANCE REINSTALLED THE BUSHING ON THE LEFT SIDE UPPER ROLLER SUPPORT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HANDLE — OUT OF ALIGNMENT (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE AND THE HANDLE WOULD NOT PROPERLY ALIGN UPON CLOSING. MAINTENANCE ADJUSTED THE PASSENGER DOOR INNER HANDLE STOP AND THE DETENT ON THE PASSENGER DOOR RELEASE HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEERING SYS — MALFUNCTIONED (NLG)

DURING CLIMB-OUT FROM AVP-ATL, THE CREW RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH, AND THE MESSAGE WENT OUT WITH THE NWS SWITCH IN THE OFF POSITION. AN EMERGENCY WAS DECLARED AND THE EMERGENCY VEHICLES WERE DISPATCHED. THE AIRCRAFT LANDED SAFELY IN ATL, WHERE IT REGAINED NOSE WHEEL STEERING AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

FLT 4460 - DURING A HANGAR INSPECTION 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: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN ATL, THE LEFT AND RIGHT EMERGENCY LIGHTS FORWARD OF THE CENTER EMERGENCY EXITS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PLATE — CRACKED (CARGO BAY)

DURING A C-CHECK, THE CARGO DOOR FLOOR LANDING PLATE AT FS 589.00 AND FS 605.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR LANDING PLATE AT FS 589.00 AND FS 605.00 IAW EO 600-53-0117.

Part: HANDLE — CRACKED (AVIONIC BAY DOOR)

DURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE BASE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE MAIN AVIONICS BAY DOOR HANDLE ASSEMBLY.

Part: ANGLE — CRACKED (FLOOR SUPPORT) · airframe 16,968 hrs

DURING C-CHECK, THE LT AND RT SIDE FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT AND RT SIDE FLOOR SUPPORT ANGLES AT FS 621 IAW EO 600-53-0105.

Part: STEP — CRACKED (FUSELAGE) · airframe 16,968 hrs

DURING A C-CHECK, THE PASSENGER DOOR TOP STEP FORWARD IB CORNER WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP IAW MM 52-11.

Part: INVERTER — INTERMITTENT (EMERGENCY LIGHT)

FLT 4637 - DURING A GROND INSPECTION IN BTR, THE EMREGENCY FLOOR TRACK LIGHTING WOULD NOT ILLUMINATED WHEN THE EMERGENCY LIGHTS SWITCH WAS IN THE ON POSITION FOR APPROXIMATELY TEN SECONDS. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHTS BATTERY INVERTER. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

FLT 4402 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHT STRIP BETWEEN ROWS 2/4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTORS TO THE EMERGENCY FLOOR LIGHT STRIP BETWEEN ROWS 2 AND 4 LOOSE AND RECONNECTED THEM. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (RT OVERWING)

DURING A GROUND INSPECTION FOLLOWING A ROUTINE OVERNIGHT IN DFW, THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD OVERWING EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS 1 TO 5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS 1 TO 5. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — MALFUNCTIONED (CABIN)

FLT 4232 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE EMERGENCY FLOOR LIGHTS AT ROWS 2-5 AND WAS UNABLE TO FIND ANY DEFECTS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO DOOR SILL AT FS 574 AND FS 621 IAW SRM 51-00 AND SRM 53-00. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

DUIRNG A C-CHECK IN MCN, CROSS SUPPORT AT FS 589 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CROSS SUPPORT AT FS 589 BETWEEN LBL 9 AND RBL 9 IAW SRM 51-00. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOORBEAM BRACKET AT RBL 9 AND FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOORBEAM BRACKET AT RBL 9 AND FS 280 IAW SRM 51-00. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LT AND RT 9 AND 27 FLOORBEAMS BETWEEN FS 280 AND FS 379 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT 9 AND 27 FLOORBEAMS BETWEEN FS 280 AND FS 379 IAW ASA EO 600-53-0052. (M)

Part: HINGE — CORRODED (FUSELAGE STEP)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP HINGE BETWEEN FS 310 AND FS 349 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PASSENGER DOOR TOP STEP HINGE BETWEEN FS 310.00 AND FS 349 IAW SRM 51-00. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOORBEAM AT LBL 27 AND FS 589 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT FLOORBEAM AT LBL 27 AND FS 589 IAW SRM 51-00 AND SRM 53-00. (M)

Part: STRINGER — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE STRINGER UNDER THE WATER TANK AT FS 589 AND FS 620 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE STRINGER UNDER THE WATER TANK AT FS 589 AND FS 620 IAW SRM 51-00. (M)

Part: STRINGER — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE SERVICE DOOR SILL STRINGER BETWEEN FS 310 AND FS 349 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE SERVICE DOOR SILL STRINGER BETWEEN FS 310 AND FS 349 IAW SRM 51-00. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT FRAME FS 640 BETWEEN STRINGERS 9 AND 12 AND BETWEEN 13 AND 14 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT FRAME FS 640 BETWEEN STRINGERS 9 AND 12 AND BETWEEN 13 AND 14 IAW ASA EO 600-53-0069 AND ASA EO 600-53-0088. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURNG A C-CHECK IN MCN, THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT ANGLE BRACKETS BELOW THE ENGINE SUPPORT BEAM IAW SRM 51-00. (M)

Part: SUPPORT — CRACKED (ENGINE)

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

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

FLT 4766 - DURING GROUND INSPECTION AT DFW, THE FORWARD SEGMENT OF EMERGENCY LIGHTS WERE SLOW TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK NORMAL. AIRCRAFT OK FOR SERVICE. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, FRAME 71B WAS FOUND CRACKED ON BOTH THE LEFT AND RIGHT SIDES BETWEEN STRINGERS 10-12. MAINTENANCE REPAIRED THE CRACKED FRAME IAW ASA EO 600-53-0067. THIS EO INCLUDES REPAIR SPECIFICATIONS FOR FS 718 CRACKS ON CRJ200 AIRCRAFT USING REO 601R-53-61-193, REO 601R-53-61-492, SRM 51-00 REV 14, AND SRM 53-00 REV 14 AS REF. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A HANGER INSPECTION, THE SECOND, FROM FORWARD, EMERGENCY LIGHTING STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE EMERGENCY STRIP LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: GCU — FAILED (RIGHT)

FLT 4592 - DURING FLIGHT FROM ATL TO ISP, WITH HAVING THE AUXILIARY POWER UNIT PREVIOUSLY DEFERRED, THE RIGHT INTERGRATED DRIVE GENERATOR FAILED. AN EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED AND LANDED SAFELY IN RDU. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE GENERATOR CONTROL UNIT (P/N 720846D) AND THE RIGHT ENGINE INTERGRATED DRIVE GENERATOR (P/N 755469E). OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING C-CHECK INSPECTION IN MCN, THE FORWARD ENTRY SIDEWALL EMERGENCY EXIT LIGHT WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT LIGHT BULB. NO OTHER DAMAGE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONTROLLER — INOPERATIVE (BLEED LEAK)

FLT 4101 - CREW RECEIVED A RIGHT ENGINE 14TH STAGE BLEED WARNING. CAPTAIN STARTED RETURNING TO ATL, WARNING WENT AWAY. MESSAGE THEN CAME BACK ON. CAPTAIN HAD TO SHUT ENGINE DOWN PER THE POH AND DIVERTED AIRCRAFT TO HSV. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE BLEED LEAK CONTROLLER. OPERATIONAL CHECKS AND BLEED LEAK INDICATION WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BLEEDER PORT — BROKEN (BRAKE ASSY)

FLT 4551 - ON APPROACH TO ATLANTA WHEN LANDING GEAR WAS SELECTED DOWN, CREW RECEIVED A 'HYDRAULIC 2 LOW PRESSURE' CAPTION ON THE EICAS. A GO-AROUND WAS COMPLETED. AN EMERGENCY WAS DECLARED AS A PRECAUTION DUE TO THE LOSS OF OUTBOARD BRAKES. AIRCRAFT LANDED SAFELY. MAINTENANCE REPLACED THE NR 2 HYDRAULIC PUMP AND INVESTIGATION SHOWED THE RIGHT OUTBOARD BRAKE BLEEDER PORT WAS BROKEN OFF FROM THE AIRCRAFT. THIS REQUIRED REPLACEMENT OF THE BRAKE ASSEMBLY. (X)

Part: WHEEL — DEFECTIVE (MLG)

MAIN WHEEL SUB-ASSEMBLY FOUND CRACKED AT TIRE CHANGE. THIS IS A NEW AIRCRAFT APPROXIMATELY 1200 CYCLES ON WHEEL ASSY. MAINTENANCE REPLACED THE MAIN WHEEL ASSY, P/N 5010571-1 AND S/N MAR98-1715, REMOVED FROM THE LEFT INBOARD POSITION. MAINTENANCE IS CURRENTLY WAITING ON REPLACEMENT PART FROM A/C BRAKING SYSTEMS (WHEEL TIRE DIVISION). (M)

Part: WINDOW — CRACKED (COCKPIT)

ATL/SWF - FLT 7810 - EN ROUTE AT 33,000 FEET, THE LT WINDOW BEGAN TO CRACK (FORWARD RT CORNER). CREW DECLARED AN EMERGENCY AND DIVERTED INTO ROA WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. THE WINDOW CONTINUED TO CRACK DURING DESCENT DOWN REPLACED THE WINDOW. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. TAT: 1,965.5 HOURS. (X)