N855AS

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 35,190 hrs · 32,058 cycles

CENTER CEILING EXIT SIGN MISSING RED LENS. REPLACED MISSING RED LENS ON CENTER CEILING EXIT SIGN IAW AMM 33-51-14.

Part: DOOR — LACK OF LUBE (SERVICE) · airframe 32,986 hrs · 29,736 cycles

SERVICE DOOR CANNOT BE OPENED FROM OUTSIDE. ALSO, VERY DIFFICULT TO LATCH CLOSED. CLEANED & LUBRICATED SEREVICE DOOR OUTER HANDLE & RELEASE BUTTON. OPS CHECKED GOOD REF AMM 52-41-00. ACFT OK FOR SERVICE.

Part: DOOR — UNKNOWN · airframe 32,945 hrs · 29,692 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. OUTER HANDLE JAMMED. COMPLIED WITH INSPECTION ON SERVICE DOOR - NO DEFECT NOTED IAW AMM 2-40-00. OK FOR SERVICE.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 31,297 hrs · 28,063 cycles

FLOOR LEVEL EXIT SIGN LIGHT ELECTRICAL CONNECTOR BROKEN IN THE FLIGHT ATTENDENT WARDROBE REPAIRED WIRES P23LY IAW ESPM 20-16-00. PERFORMED OPS CHECK IAW AMM 33-51-00. OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: ACM — SMOKE (RIGHT) · airframe 31,234 hrs · 27,993 cycles

AFTER TAKEOFF, SMOKE TOILET CAUTION MESSAGE, COMPLIED WITH QRH. NO VISIBLE FUMES IN FLIGHT DECK. PASSENGERS REPORTED "HAZE" AND COLOR IN CABIN. ACFT RETURNED. R & R RT ACM IAW AMM 21-51-10. OPS CHECKED GOOD IAW AMM 21-51-00. RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 31,116 hrs · 27,853 cycles

WHILE PERFORMING EMERGENCY LIGHT OPS CHECKS, FOUND BOTH AFT EXTERIOR & NR 2 CEILING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 BATTERY PACK IAW AMM 33-51-04-000-801 AND 33-51-04-400-801 SELF TEST OF BATTERY PACK & CHARGER ASSY GOOD.

Part: DOUBLER — DAMAGED (BS 349) · airframe 31,116 hrs · 27,853 cycles

INTERNAL DOUBLER AT FS 349 DAMAGED. REPAIRED IAW REO 601R-53-21-2469. MAJOR REPAIR.

Part: ANGLE — DAMAGED (BS 349) · airframe 31,116 hrs · 27,853 cycles

FOUND TWO DAMAGED HOLES ON FS 349 ATTACHMENT ANGLE. REPAIRED IAW REO 601R-53-21-2471. MAJOR REPAIR.

Part: ANGLE — CORRODED (BS 310.1) · airframe 31,116 hrs · 27,853 cycles

ANGLE CORRODED AT BS 310.1 SERVICE DOOR SURROUND. R & R ANGLE IAW SRM 51-42-21-00. MAJOR REPAIR.

Part: SEAT TRACK — CRACKED · airframe 31,116 hrs · 27,853 cycles

SEAT TRACK CRACKED. PERFORMED EDDY CURRENT INSPECTION IAW MAC NDT INSPECTION PROCEDURE 4.2 LOCATED END OF CRACK AREA. PERFORMED EDDY CURRENT INSPECTION OF CUT OUT AREA IAW BSC NDT PROGRAM MANUAL SECTION 4.2 NO INDICATIONS NOTED AT THIS TIME. COMPLIED WITH SNIEO K601R53100.

Part: ANGLE — CORRODED (BS 349) · airframe 31,116 hrs · 27,853 cycles

ANGLE AT BS 349 CORRODED. REMOVED ANGLE AND REMOVED CORROSION. FOUND TO OUT OF LIMITS IAW SRM 51-42-06, 51-21-06, AND TR 53-27 LOCATED, DRILLED AND DEBURRED NEW ANGLE IAW SRM 51-40-11L AND INSTALLED IAW SRM 51-42-06 AND 51-42-21.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 31,116 hrs · 27,853 cycles

AIRFRAME THE DOUBLER FS 319.7 - 349.00 CORRODED. REMOVED CORROSION IAW SRM 51-21-06.

Part: BRACKET — CORRODED (BS 349) · airframe 31,116 hrs · 27,853 cycles

BS 349 FOUND CORROSION ON FRAME BRACKET. REMOVED FRAME BRACKET IAW SRM 51-42-21. INSTALLED NEW BRACKET IAW SRM 51-42-21 AND DWG 601R-38303. MAJOR REPAIR.

Part: CROSSBEAM — CORRODED (BS 349) · airframe 31,116 hrs · 27,853 cycles

CROSSBEAM AT FS 349 CORRODED. REMOVED CORROSION IAW SRM 51-21-06 CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM TR 53-27, FIG 102.

Part: RIB — CRACKED (RT WING) · airframe 31,116 hrs · 27,853 cycles

ON REMOVAL OF RT INBD FLAP ACTUATOR OTBD LOCATION FOUND WING RIB AT WS 130.10 CRACKED. REPAIRED IAW REO 601R-57-51-661. MAJOR REPAIR.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 31,116 hrs · 27,853 cycles

LT DME ANTENNAS CUTOUT DOUBLER HAS CRACK IN THE INBD BEND RADIUS. REMOVED LT DME ANTENNA DOUBLE IAW SRM 51-42-06. INSTALLED SERVICABLE ANTENNA DOUBLER IAW SRM 51-42-06 AND DWG 601R38502-11.

Part: BRACKET — CRACKED (BS 325) · airframe 31,100 hrs · 27,836 cycles

ANGLE BRACKET AT BS 325 S13L, CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-42-20.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 31,100 hrs · 27,836 cycles

ISOLATOR BROKEN ON AFT PRESSURE BULKHEAD. R & R DAMAGED ISOLATORS IAW SRM 51-42-13-00.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 31,116 hrs · 27,853 cycles

FLOOR SUPPORT CORRODED BS 349. REMOVED FLOOR SUPPORT FROM BS 349 - 409 IAW SRM 51-42-06 AND 51-42-20. INSTALLED IAW SRM 51-24-36, 51-40-11, 51-42-06, 51-42-13, DRW 601R31148.

Part: LIGHT — BROKEN (GALLEY) · airframe 31,100 hrs · 27,836 cycles

GALLEY CLOSE OUT PANEL HAS EMERGENCY LIGHT BASE BROKEN. R & R EMERGENCY LIGHT IAW AMM 33-51-10-000-801 AND 33-51-10-400-801. CRIMPED AND SECURED CONTACTS IAW ESPM 20-16-00. OPS TESTED IAW AMM 33-51-00-710-801 OPS TESTED GOOD.

Part: SILL — CORRODED · airframe 31,114 hrs · 27,852 cycles

SERVICE DOOR LOWER SILL CORRODED. REMOVED DOOR SILL AND TOP COVER IAW SRM 51-42-20, 51-42-36, 51-42-06, AND 51-42-13. DRILLED AND INSTALLED NEW SILL IAW SRM 51-40-11-00 AND SRM 51-42-06-00. MAJOR REPAIR.

Part: BULKHEAD — GOUGED (AFT) · airframe 31,100 hrs · 27,836 cycles

GOUGES ON AFT PRESSURE BULKHEAD. REPAIRED IAW REO 601R-53-61-2155, REV A.

Part: FITTING — GOUGED (RT WING TE FLAP) · airframe 31,114 hrs · 27,852 cycles

RT WING FLAP FITTING GOUGED. REPAIRED IAW REO 601R-57-51-143. MAJOR REPAIR.

Part: SKIN — CRACKED (LT WING) · airframe 31,114 hrs · 27,852 cycles

LT WING PLANK CRACKED. ROTO-PEENED, REWORKED AREA IAW STEP 16 OF REO 601R-57-21-130. COMPLIED WITH EC/TC REO 601R-57-21-130 AND GENERIC REO 601R-57-21-130, REV J. MAJOR REPAIR.

Part: BRACKET — CRACKED (BOX BEAM) · airframe 31,100 hrs · 27,836 cycles

BRACKET BROKEN ON TOP RT SIDE ON ENGINE BOX BEAM. R & R BRACKET IAW ARM 51-42-21 AND 51-41-02 AND DWG 600-98047.

Part: FITTING — GOUGED (LT WING TE FLAP) · airframe 31,114 hrs · 27,852 cycles

LEFT WING FLAP FITTING GOUGED. REPAIRED IAW REO 601R-57-51-143. MAJOR REPAIR.

Part: SKIN — CRACKED (RT WING) · airframe 31,114 hrs · 27,852 cycles

RT WING PLANK CRACKED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. ROTO PEENED, REWORKED AREA FOR STEP 16 OF REO 601R-57-21-130. COMPLIED WITH ECTC REO REO 601R-57-21-130-01 AND REO 601R-57-21-130, REV J.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,902 hrs · 27,633 cycles

LEFT EXTERIOR EMERGENCY LIGHT FWD OF OVER WING DOOR IS OUT. R & R NR 3 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,379 hrs · 25,070 cycles

RT SIDE AFT OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED RT SIDE AFT OVERWING EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: IDG — FAILED (NR 1) · airframe 27,427 hrs · 24,026 cycles

MODERATE VIBRATION DEVELOPED ON NR 1 ENGINE. VIBRATION FELT THROUGHOUT ENTIRE AIRFRAME AND CONTROL YOKE. VIBRATION METERS WERE IN NORMAL RANGE, GREEN ARC. ROW 10 PAX FELT & HEARD GRINDING NOISE. EMERGENCY DECLARED. SUSPECT DEFERRED ENG 1 IDG RECONNECT AND FAILURE. R & R NR 1 IDG. OPS CHECKED GOOD. NO VIBRATIONS OR NOISES HEARD INSIDE OR OUTSIDE DURING ENGINE NR 1 OPS WITH NR 1 IDG ONLINE. AC RETURNED TO SERVICE.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 27,026 hrs · 23,565 cycles

ISOLATOR ON AFT PRESSURE BULKHEAD HAS BROKEN MOUNT LOCATED BOTTOM LT BY BAGGAGE DOOR ENTRANCE. R & R ISOLATOR ON 621 BULKHEAD BOTTOM LT BY BAGGAGE DOOR ENTRANCE IAW SRM 51-42-13. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: RIB — CRACKED (LT WING) · airframe 27,026 hrs · 23,565 cycles

LEFT WING BATT RIB CRACKED IN WHEEL WELL AT WS 53.60. REPAIRED IAW AMM 57-21-30-400-801.

Part: POST — CRACKED (BS 409) · airframe 27,026 hrs · 23,565 cycles

FOUND FS 409.0+128 VERT POST LBL 18.0 INBD AND OTBD SIDE HAVE INDICATIONS NOTED APPROX .3" IN LENGTH 50 PERCENT FSH. BOTH FAILED NDT INSP AT WL 69.0 AFT FLANGE RADIUS. APPLIED DINOTROL IAW SRM 51-21-11. EC/TC REQUIRED FOR REO 601R-53-41-889 REV A. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL REQUIREMENTS OF REO 601R-53-41-889, REV A.

Part: POST — CRACKED (BS 409) · airframe 27,026 hrs · 23,565 cycles

FOUND FS 409+128 VERTICAL POST RBL 18 OTBD SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 50 PERCENT FSH. FAILED NDT INSP AT WL 69 AFT FLANGE RADIUS. REMOVED POST IAW SRM 51-42-06. LOCATED, DRILLED & ASSEMBLED NEW POST IAW SRM 51-42-06 & REO 601R-53-41-889, REV A. INSTALLED VERT POST ASSY IAW REO 601R-53-41-889, REV A.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 27,026 hrs · 23,565 cycles

FOUND FS 409.0+128, VERTICAL POST LBL 18.0 INBD AND OTBD SIDES HAVE INDICATIONS NOTED APPROX .3" IN LENGTH 50 PERCENT FSH. BOTH FAILED NDT INSP AT WL 69.0 AFT FLANGE RADIUS. INSTALLED POST IAW SRM 51-42-06 & REO 601R-53-41-889.

Part: VERTICAL BEAM — CRACKED (BS 409 BULKHEAD) · airframe 27,026 hrs · 23,565 cycles

FS 409+128 PRESSURE BULKHEAD VERTICAL BEAMS INBD & OTBD AT LBL 36 ARE CRACKED AROUND BOTTOM FASTENER. REMOVED BEAM IAW SRM 51-42-06. FOUND TO BE CRACKED. INSTALLED NEW IAW SRM 51-42-06, 51-42-13 & REO 601R-53-41-1481.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 27,026 hrs · 23,565 cycles

FS 484, RBL 27 FLOOR SUPPORT ANGLE CRACKED. REMOVED CRACKED FLOOR SUPPORT ANGLE AND INSTALLED NEW ANGLE IAW REO 601R-53-41-059.

Part: ATTACH FITTING — CRACKED (INTERCOSTAL) · airframe 27,026 hrs · 23,565 cycles

FS 621 TO FS 625.3 INTERCOSTAL OTBD CLIPS ARE CRACKED AT STR 12R AND STR 13R. REMOVED AND INSTALLED NEW CLIPS IAW SRM 51-42-21, 51-42-06.

Part: INTERCOSTAL — CRACKED (INTERCOSTAL) · airframe 27,026 hrs · 23,565 cycles

FS 621 TO FS 625.3 INTERCOSTAL OTBD CLIP IS CRACKED AT STR 13L. REMOVED & REPLACED INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 27,026 hrs · 23,565 cycles

FOUND FS 409.0+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 50 PERCENT FSH. FAILED NDT INSP AT WS 69.0 AFT FLANGE RADIUS. REMOVED POST IAW SRM 51-42-06. LOCATED, DRILLED & ASSEMBLED NEW POST IAW SRM 51-42-06 & REO 601R-53-41-889, REV A. INSTALLED VERT POST ASSY IAW REO 601R-53-41-889, REV A.

Part: BULKHEAD — CRACKED · airframe 27,026 hrs · 23,565 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB DAMAGE IAW EC/TC 601R-53-61-1230.

Part: RIB — CRACKED (LT WING) · airframe 27,026 hrs · 23,565 cycles

LEFT WING BATTERY RIB CRACKED IN WHEEL WELL AT WS 53.60. REPAIRED IAW REO 601R-57-51-046.

Part: SKIN — CRACKED (BS 235) · airframe 27,026 hrs · 23,565 cycles

FS 235 FUSELAGE SKIN IS CRACKED .325" AT THE RT AFT CORNER CUTOUT OF THE AFT NOSE LANDING GEAR DOOR. REPAIRED IAW REO 601R-53-11-0048 REV.C.

Part: RIB — CRACKED (RT WING) · airframe 27,026 hrs · 23,565 cycles

RT WING BATTERY RIB CRACKED IN WHEEL WELL AT WS 53.60. REPAIRED IAW REO 601R-57-51-046.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 27,026 hrs · 23,565 cycles

LT CABIN WINDSCREEN LIGHTED EXIT SIGN COVER IS BROKEN. REMOVED UNSERVICEABLE COVER AND REPLACED WITH NEW COVER IAW AMM 33-51-13-000-801, STEP 3A (1) AND 33-51-13-400-801 STEP 3A(4).

Part: ANGLE — CRACKED (BS 621) · airframe 27,026 hrs · 23,565 cycles

RT 621, OBLIQUE ANGLE CRACKED. R & R OBLIQUE ANGEL IAW SRM 51-40-11 AND SRM 51-42-21. PRIMED AND PAINTED AREA REQUIRED IAW SRM 51-25-01. REPAIR CLASSIFIED AS MINOR.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 26,796 hrs · 23,307 cycles

FWD BULKHEAD EMERGENCY FLOOR FLOOD LIGHT LENS BROKEN AND LIGHT INOP. R & R ENTRY FLOOD LIGHT IAW AMM 33-51-19. PERFORMED OPS TEST OF EMERGENCY EXIT LIGHTS IAW AMM 33-51-00. NO FAULTS FOUND AT THIS TIME. (CLOSED)

Part: LIGHT — MISSING (CABIN) · airframe 25,017 hrs · 21,308 cycles

F/A REPORTS RED EMERGENCY NOTIFICATION LIGHTS IN CABIN ARE MISSING, (COCKPIT TO F/A EMERGENCY CALL). REPAIRED EMERGENCY NOTIFICATION LIGHTS IAW AMM 33-51-14.

Part: LANDING GEAR — INOPERATIVE (NOSE) · airframe 23,717 hrs · 19,812 cycles

NOSE GEAR WILL NOT COME UP (EMERGENCY DECLARED -- ACFT RETURNED TO DEPARTURE AFTER T/O).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,351 hrs · 19,395 cycles

FIRST CABIN CEILING EMERGENCY LIGHT IS INOP. REFER BACK TO EO 600-33-0015.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 23,350 hrs · 19,393 cycles

CORROSION ON LBL 9 FLOOR SUPPORT BETWEEN FS 605 AND 621. OUT OF LIMIT DAMAGE. DISCREPANCY REPAIRED IAW REO 601R-53-61-3398.

Part: FLOORBEAM — CRACKED (BS 589) · airframe 23,350 hrs · 19,393 cycles

FLOOR ANGLE UNDER CARGO DOOR SILL AT FS589.00 AND LBL45 IS CRACKED (ANGLE ATTACHES FRAME TO SKIN). REMOVED AND REPLACED FLOOR ANGLE IAW SRM 51-40-11 & 51-42-21.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 23,350 hrs · 19,393 cycles

FLOOR TRANSVERSE BEAM UPPER ANGLES BETWEEN RBL9 AND LBL9AT FS 589.00 ARE CORRODED

Part: FLOORBEAM — CORRODED (BS 574) · airframe 23,350 hrs · 19,393 cycles

FLOORBEAM CAP ANGLES CORRODED AROUND SEVERAL NUTPLATES AT LBL9 AND LBL27 FS 574.00. REMOVED AND REPLACED FLOORBEAM CAP ANGLES BETWEEN FS 574 & FS 621. DAMAGE ON LBL 9 FLOORBEAM CAP WAS MOVED TO N/R 00518 ON WO 131561.

Part: SILL — CORRODED (BS 559-621) · airframe 23,350 hrs · 19,393 cycles

CORROSION AT RT CABIN FLOOR SILL FROM FS 559+80 TO FS 621.00 AROUND NUTPLATES. REMOVED AND INSTALLED NUT PLATES AFTER CLEANING CORROSION IAW REO 601R-53-00-328.

Part: PRESSURE BLKHD — CRACKED (BS 202) · airframe 23,350 hrs · 19,393 cycles

FWD PRESSURE BULKHEAD FS 202.75 CRACKED AT PARKING BRAKE CABLE CUT OUT. PERFORMED ET INSPECTION OF SUSPECT CRACK IAW NDTM 51-20-06. RECEIVED CRACK INDICATION AT -2 LOCATION COMING OUT OF THE BRAKE CABLE HOLE. MADE CUT TO REMOVED CRACKING FROM 202 BULKHEAD IAW REO 601R-33-11-563 + DEBURRED CUT LINE IAW 601R-53-11-563 (REO). FABRICATED DOUBLER -1, -2, -3, -4, -5 SHIMS AND TRIMED TO FIT STRUCTIVE & DRILLED UP ALL FASTENER HOLES TO FINAL SIZE AND DEBURRED ALL HOLES AND EDGES IAW REO 601R-53-11-563. INSTALLED T-BRACKET IAW REO 601R-53-11-563 AND SRM 51-42-06 AND INSTALLED -5 SHIM IAW REO 601R-53-11-563 AND 51-42-06.

Part: FRAME — CORRODED (BS 319) · airframe 23,350 hrs · 19,393 cycles

CORROSION ON FRAME AT FS 319.70 AND STR 27 IN BELLY OF ACFT IN AVIONICS BAY. REMOVED AND REPLACED FRAME SEGMENT AT FS319.70 BETWEEN STRINGERS 23L AND 23R AND SEALED, RESTORED A023 FINISH, THEN CIC WAS APPLIED. ALL WORK DONE IAW SRM'S 51-21-11, 51-21-16, 51-23-00, 51-41-00 AND 51-42-06.

Part: FRAME — CORRODED (BS 333) · airframe 23,350 hrs · 19,393 cycles

CORROSION ON FRAME AT FS 333.00 AND STR 27 IN BELLY OF ACFT IN AVIONICS BAY. REMOVED AND REPLACED FRAME SEGMENT AT FS 333 BETWEEN STRINGER 23L AND 23R AND SEALED, RESTORED A023 FINISH AND APPLIED CIC. ALL WORK DONE IAW SRM'S 51-21-11, 51-21-16, 51-23-00 51-41-00, 51-42-06. RII COMPLIED WITH IAW SP 607.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,350 hrs · 19,393 cycles

CORROSION ON ASD CUTOUT THRESHOLD AND FLOORBEAM IN THE AFT LWR CORNER OF CUTOUT. REPAIRED SURFACE CORROSION IAW SRM 51-42-00.

Part: FRAME — CORRODED (BS 349 S27) · airframe 23,350 hrs · 19,393 cycles

CORROSION ON FRAME AT FS 349.00 AND STR 27 IN BELLY OF ACFT IN AVIONICS BAY. REMOVED AND REPLACED FRAME SEGMENT AT FS 319.90 BETWEEN STRINGERS 23L AND 23R AND SEALED AND RESTORED A023 FINISH, THE APPLIED CIC. ALL WORK DONE IAW CRJ 200 51-42-06, 51-41-00, 51-21-11, 51-21-16, 51-23-00. RII COMPLIED WITH PER SP 607.

Part: INTERCOSTAL — NONE (FUSELAGE) · airframe 23,350 hrs · 19,393 cycles

LT E/EXIT DOOR HAS CRACKED INTERCOSTAL JUST BELOW WINDOW (MARKED). NO DAMAGE (CRACK) TO BE FOUND. REINSTALLED LEFT EMERGENCY EXIT DOOR INTERCOSTAL BELOW WINDOW PER SRM 51-42-06 JOB COMPLETED.

Part: FRAME — CRACKED (BS 640 S9R) · airframe 23,350 hrs · 19,393 cycles

FWD SIDE OF FS 640.00 FRAME AT STR 9 CUTOUT RT SIDE CRACKED APPROX .3750 INCH. PERFORMED ET INSPECTION OF STR9 CUTOUT ON RT FS 640 FRAME FWD SIDE IAW CRJ 200 NDTM 51-20-06. RECEIVED RELEVANT INDICATION APPROX 3/8" LONG. REMOVED AND REPLACED RIGHT SIDE 640 FRAME SECTION. REFER TO EC/TC SB A601R-53-059 PART B.

Part: SKIN — CRACKED (PAX DOOR) · airframe 23,350 hrs · 19,393 cycles

DOOR INNER SKIN CRACKED AT UPPER AFT CORNER UNDER UPPER STEP. COMPLIED WITH EC/TC EO600-52-43 C/W RII COMPLETED SATISFACTORILY IAW EC/TC EO600-52-43 C/W AND SP 607. PERFORMED ET INSPECTION OF CUT LINE ON ASD INNER SKIN UPPER AFT CORNER UNDER TOP STEP IAW NDTM 51-20-06. NO DEFECTS NOTED.

Part: PLACARD — PEELING (ASD) · airframe 23,350 hrs · 19,393 cycles

ON ASD STEPS INTERNAL EXIT PLACARD IS PEELING UP. REMOVED AND REPLACED EXIT PLACARD ON ASD STEP PER AMM 11-30-00.

Part: FLOORBEAM — CRACKED (BS 559) · airframe 23,350 hrs · 19,393 cycles

IN REFERENCE TO TASK CARD AWL2 53-41-201. CAP ANGLE CRACKED IN RADIUS AT LBL 18.00 AT FS 559.00

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,224 hrs · 18,306 cycles

CRACKED ANGLE AT FS 484 LT SIDE.

Part: LIGHT — DAMAGED (CABIN) · airframe 22,109 hrs · 18,200 cycles

EMERGENCY LIGHTS: FLOOR LIGHTING STRIP DAMAGED FORWARD OF RIGHT EMERGENCY EXIT.

Part: FLAP — FAILED (WING) · airframe 21,824 hrs · 17,930 cycles

FLAP FAIL ON FINAL APPROACH TO RUNWAY 27 (24DEG) MISSED APPROACH FLAPS FAIL APPROACH CW LANDED SAFELY OUT 25 ALT 2300, EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,661 hrs · 17,795 cycles

FWD OVERWING EMERGENCY LIGHT ON RT SIDE IS INOP.

Part: TRIM SYSTEM — MALFUNCTIONED (AILERON) · airframe 21,424 hrs · 17,552 cycles

A/C YAWED EXCESSIVELY TO THE RIGHT DURING FLIGHT, THE A/C WOULD NOT STAY TRIMMED. AFTER ENGAGING THE AUTOPILOT, THE AUTOPILOT HAD DIFFICULTY MAINTAINING THE FLIGHT CONTROL INPUTS. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. (AILERON TRIM SYSTEM)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,254 hrs · 16,533 cycles

EN ROUTE THE COVER ON ONE OF THE FLOOR EMERGENCY LIGHTS CAME OFF AND IT STOPPED WORKING.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,166 hrs · 15,625 cycles

EMERGENCY LIGHT TRACK ROW 2 TO 5 AND FLOOR PROXIMITY EXIT SIGN INOP.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 19,156 hrs · 15,616 cycles

CROSS FLOORBEAM CORRODED AT FS 349, RBL 36, ATTACHED TO SERVICE DOOR. 10-11-07 ALODINE APPLIED IAW SRM 51-21-11 AND PRIMER DONE IAW SRM 51-25-06. PAINTED IAW SRM 51-25-16, MATERIAL THICKNESS: 0.080 MATERIAL REMOVED: 0.006, WITHIN LIMITS AS PER SRM: 53-00-00 FIG 101.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 19,156 hrs · 15,616 cycles

FLOORBEAM ANGLE ON AFT SIDE OF CROSSBEAM FS 349.00 RBL 36 IS CORRODED. 10-16-07 CORROSION ON FLOOR SUPPORT ANGLE ON AFT SIDE OF CROSS BEAM FS 349.00 RBL 36 REMOVED IAW SRM 51-21-06, ANGLE REMOVED IAW SRM 51-42-06. REFER TO W/C 2000-32 FOR FABRICATION OF FLOOR SUPPORT ANGLE AT FS 349.00 RBL 36 FABRICATED PART FLOOR SUPPORT AT FS 349.00 RBL 36.00 INSTALLED IAW SRM 51-42-06. MATERIAL THICKNESS 0.063. MATERIAL REMOVED 0.020. BEYOND SRM LIMITS 53-00-00 FIG 101.

Part: ANGLE — CORRODED (BS 349) · airframe 19,156 hrs · 15,616 cycles

ANGLE 601R38983-13 AT FS 349.0 RBL 36 CORRODED OUT OF LIMITS. FABRICATION OF A NEW ANGLE REQUIRED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 19,156 hrs · 15,616 cycles

FLOORBEAM CRACK AT FS 280.00 RBL 9.5. 10-11-07 FLOORBEAM REPLACED IAW REO 601R-53-11-171 REV D.

Part: SKIN — CRACKED (PAX DOOR) · airframe 19,156 hrs · 15,616 cycles

SUSPECTED CRACK ON VERTICAL SKIN OF PAX DOOR STEP 832 AT. 10-11-07 HFEC PERFORMED, CRACK CONFIRMED AND MARILED ON THE PART. CRACK ON VERTICAL SKIN OF PAX DOOR STEP 832 AT REPAIRED IAW SRM 51-12-00 FIG 7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,156 hrs · 15,616 cycles

ETNRC - FOUND CORROSION ON CROSSBEAM AT 281 JLE POSITION (CARGO) FLOOR ATTACHMENT HOLE. 10-11-07 CORROSION ON CROSS BEAM REMOVED IAW SRM 51-21-06, ALODINE APPLIED IAW SRM 51-21-11, PRIMER APPLIED IAW SRM 51-25-06 AND WHITE TOPCOUT APPLIED IAW SRM 51-25-16 MATERIAL THICKNESS: 0.120 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 1.

Part: FRAME — CORRODED (BS 333) · airframe 19,156 hrs · 15,616 cycles

LOWER FRAME SEGMENT BETWEEN STR 23R-23L, FS 333.00 IS CORRODED. 10-9-07 CORROSION REMOVED AT LOWER FRAME SEGMENT 333.00 BETWEEN S23R-23L IAW SRM 51-21-06. RIVETS REPLACED IAW SRM 51-42-06. MATERIAL THICKNESS: 0.050 MATERIAL REMOVED: 0.001 WITHIN LIMITS AS PER SRM: 53-00-00.

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 19,156 hrs · 15,616 cycles

ON REAR PRESSURE BULKHEAD AFT SIDE AT FS 621.00 LBL 46.00 WL 93.00 AND RBL 46.00 WL 93.00 ANGLES FOUND CRACKED. BOTH CRACKED ANGLES OF F/S 621.00 AFT SIDE REMOVED AS PER SRM 51-42-20. NEW ANGLES FABRICATED AS PER SRM 51-24-16 AND TREATED AS PER SRM 51-21-11 AND 51-25-06 FABRICATED ANGLE INSTALLED AS PER SRM 51-42-20.

Part: BULKHEAD — CRACKED (BS 621) · airframe 19,156 hrs · 15,616 cycles

ON REAR PRESSURE BULKHEAD AR FS 621.00 RBL 36 MOUNT ISOLATOR BRACKET FOUND CRACKED. REPLACE ON REAR PRESSURE BULKHEAD AT FS 621.00 RBL 36, MOUNT ISOLATOR BRACKET REMOVED AND REPLACED IAW SRM 51-2-13.

Part: WEB — CRACKED (PAX DOOR) · airframe 19,156 hrs · 15,616 cycles

PAX DOOR IN AREA OF ACCESS PANEL 832AL WEB FOUND CRACK. 10-16-07 REPAIRED CRACK FOUND IN PAX DOOR IN AREA OF ACCESS PANEL 832AL WEB AS PER 51-12-11 FIG 6.

Part: FRAME — CORRODED (BS 349 S23LR) · airframe 19,156 hrs · 15,616 cycles

ETNRC - FS 349.00, BETWEEN STR 23R - 23L, LOWER FRAME SEGMENT IS CORRODED. 10-11-07 CORROSION REMOVED AT FS 349.00 BTW STR 23R - 23L IAW SRM 51-21-06 RIVETS REPLACED & IAW SRM 51-42-06 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.002 WITHIN LIMITS AS PER SRM: 53-00-00.

Part: FRAME — CORRODED (BS 364) · airframe 19,156 hrs · 15,616 cycles

CORROSION FOUND ON FRAME 364.00 AROUND RIVET OF INTERCOSTAL SKIN BETWEEN STR 26 RT & STR 27 RT. 10-9-07 CORROSION REMOVED ON FRAME 364 AROUND RIVET OF INTERCOSTAL & SKIN BTW STR 26 & 27 RT IAW SRM 51-21-06 RIVETS REPLACED IAW SRM 51-42-06 MATERIAL THICKNESS: 0.050. MATERIAL REMOVED: 0.001 WITHIN LIMITS AS PER SRM: 53-00-00

Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 19,156 hrs · 15,616 cycles

ETNRC - LEFT AND RIGHT SEAT TRACKS CORRODED BETWEEN FS 349 TO FS 409 AT LBL 9 AND RBL 9. 10-16-07 REPLACED CORRODED SEAT RAILS AS PER SRM 51-41-02.

Part: FLOOR SUPPORT — UNKNOWN (FUSELAGE) · airframe 19,156 hrs · 15,616 cycles

QTY (4) FLOOR SUPPORT ANGLE UNDER CROSS BEAM AT FS 280.00 RBL 9 AND LBL 9.

Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 19,156 hrs · 15,616 cycles

ETNRC - PAX DOOR HANDLE BETA LIGHT INOP. BETA LIGHT PAX DOOR REPLACED IAW AMM 33-51-09-000-801 FUNCTIONAL TEST OF THE DOOR EXIT SIGN BETA LIGHT IAW AMM 33-51-09-720-801.

Part: SEAT TRACK — CORRODED (BS 559-621) · airframe 19,156 hrs · 15,616 cycles

MANY SEAT RAILS AND BAGGAGE RAILS CORRODED BETWEEN FS 559+80 TO 621.00. 10-9-07 REPLACED CORRODED RAILS AND BAGGAGE RAILS BTWN FS 559 80 TO FS 621.00 AS PER SRM 51-42-02

Part: FITTING — CRACKED (FLOORBEAM) · airframe 19,156 hrs · 15,616 cycles

FITTING OF PRESSURE FLOORBEAM AT FS AND RBL 9 CRACK. 10-9-07 FITTING OF PRESSURE FLOORBEAM AT FS 461 RBL 9 REPLACED IAW SRM 51-42-21

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 19,156 hrs · 15,616 cycles

ETNRC - FLOOR ANGLE CORRODED LT AND RT BETWEEN FS 409 + 128 TO FS 559.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 19,034 hrs · 15,519 cycles

ON PREFLIGHT INSPECTION F/A FOUND FLASHLIGHT ON F/A AREA DEAD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,034 hrs · 15,519 cycles

NR 6, 7, 8 FLOOR TRACK LIGHTS AND RIGHT OVERWING FLOOR EXIT LIGHT INOP.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,333 hrs · 14,937 cycles

AFT PRESSURE BULKHEAD HAS CRACK INDICATION AT LBL 27.5 AND APPROX WL 132.

Part: FRAME — CRACKED (BS 640) · airframe 16,881 hrs · 13,845 cycles

INSP OF FS 640 FRAME AT BL45 BETWEEN STR 9 AND 12. FOUND A CRACK ON THE LEFT FS 640 FRAME. REPAIRED / MODIFIED LT AND RT FRAME 640 BETWEEN STR 9 AND 12 REF S.B. 601R-53-061 APPENDIX B. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,485 hrs · 13,522 cycles

EMERGENCY TRACK LIGHTING CRACKED AND NOT ILLUMINATING

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,330 hrs · 13,399 cycles

EMERGENCY LIGHTS IN ROWS 6 THROUGH 8 ARE INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,977 hrs · 13,099 cycles

LEFT WING LWR EMERGENCY LIGHT INOP.

Part: STEP — BROKEN (DOOR)

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

Part: STEP — BROKEN (PAX DOOR)

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

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

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

Part: DOOR — UNKNOWN (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE OPENED AND CLOSED THE PASSENGER DOOR. NO DEFECTS NOTED. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOOR FRAME — CRACKED (BS 338)

DURING A C-CHECK IN HTO, THE FS 338 PASSENGER DOOR FRAME WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 338 PASSENGER DOOR FRAME IAW BOMBARDIER REO 601R-52-11-402. (M)

Part: BPSU — MALFUNCTIONED (TE FLAPS)

FLT 4386 - DURING APPROACH INTO CVG FROM MHT, THE CREW RECEIVED A FLAPS FAIL MESSAGE WITH THE FLAPS SELECTED TO EIGHT DEGREES. EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE REMOVED AND REPLACED THE LEFT BRAKE POSITION SENSOR UNIT (BPSU) AND THE FLAPS POWER DRIVE UNIT (PDU). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS CAME ON WITH THE SWITCH IN THE OFF AND ARMED POSITIONS. MAINTENANCE FOUND CIRCUIT BREAKER P4-C2 POPPED AND THE EMERGENCY LIGHTS BATTERY PACKS LOW RESULTING FROM BOTH MAIN AND AUXILIARY POWER UNIT BATTERIES BEING DISCONNECTED WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE RESET CIRCUIT BREAKER P4-C2 AND ALSO RECHARGED THE BATTERY PACKS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HANDLE — STUCK (PAX DOOR) · airframe 11,892 hrs

DURING A GROUND INSPECTION, THE OUTSIDE HANDLE TO THE PASSENGER DOOR WOULD NOT COME OUT MAKING IT DIFFICULT TO OPEN THE DOOR. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS ON THE PASSENGER DOOR. NO DEFECTS WERE NOTED.

Part: HANDLE — BINDING (PAX DOOR)

FLT 4425 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

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

Part: SILL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72-589 IAW ASA EO 600-53-0095. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

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

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE ELFT AND RIGHT CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 280, LBL 9 AND RLB 9. (M)

Part: SUPPORT BEAM — CRACKED (CENTER ENGINE)

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

Part: LENS — CRACKED (EMERGENCY LIGHT)

DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR. (M)

Part: LENS — CRACKED (EMERGENCY LIGHT)

DURING A C-CHECK IN MCN, THE FORAWRD CEILING EMERGENCY EXIT LIGHT LENS WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD CEILING EMERGENCY EXI LIGHT LENS. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REPAIRED THE PASSENGER DOOR BOTTOM STEP IAW SRM 51-74-06. (M)

Part: LIGHT — CRACKED (GALLEY)

DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE SERVICE DOOR. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4725 - DURING A GROUND INSPECTION IN DFW, THE THIRD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE THIRD EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN IAH, THE FLOOR EMERGENCY LIGHT STRIP IN THE FORWARD SECTION WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE ORANGE FLOOR EMERGENCY LIGHT STRIP IN THE FORWARD SECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ENGINE — BIRD INGESTION (RIGHT)

DURING TAKEOFF, AT APPROX 4,000 A BIRD WAS INGESTED INTO THE RIGHT ENGINE AND IT SHUT DOWN. THE CREW COMPLIED WITH QRH PROCEDURES, DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4580 - DURING GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR TRACK LIGHTING IN THE FORWARD SECTION WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR FLEXIBLE LAMP STRIP BETWEEN ROWS 2 THROUGH 5. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CABLE — DEFECTIVE (CABIN)

FLT 4427 - DURING GROUND INSPECTION IN XNA, THE FLOOR EMERGENCY LIGHTS AT ROWS 1-5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLOOR EMERGENCY LIGHT TRACK CABLE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS WILL ARM BUT WHEN SELECTED 'ON' THE LIGHTS WILL NOT ILLUMINATE AND THE STATUS MESSAGES DOES NOT APPEAR. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDOW — FAILED (COCKPIT)

FLT 4756 - ON DEPARTURE FROM DSM TO ATL, THE CAPTAINS SIDE WINDOW SHATTERED. CREW DECLARED AN EMERGENCY AND DESCENDED TO 10,000 FEET. CREW RETURNED AIRCRAFT TO DSM AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT SIDE WINDOW. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FLT 4726 - CAE-DFW - CREW REPORTED THAT THE LEFT SIDE CAPTAIN''S WINDSHIELD CRACKED. CREW SLOWED AIRCRAFT SPEED AND ALERTED AIR TRAFFIC CONTROL OF NECESSARY LOWER ALTITUDE. ATC DECLARED EMERGENCY ON CREWS BEHALF. AIRCRAFT CONTINUED FLIGHT AND LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED CAPTAINS SIDE WINDOW. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — INOPERATIVE (BRAKE SENSOR)

FLT 4538 - CLIMBING THROUGH 21,000 FEET, CREW RECEIVED A FLAP FAIL MESSAGE. CREW PERFORMED FLAPS FAIL PROCEDURE AND CALLED ATL FLIGHT CONTROL. CREW THEN DECLARED AN EMERGENCY AND RETURNED TO ATL. CAPTAIN SAFELY PERFORMED A ZERO DEGREE FLAP LANDING. MAINTENANCE REMOVED AND REPLACED THE LEFT FLAP BRAKE SENSOR CONNECTOR PINS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)