N902EV

Part: LANDING GEAR — FAILED (NOSE) · airframe 38,307 hrs · 35,320 cycles

GEAR DISAGREE AFTER TAKEOFF DURING GEAR RETRACTION. NOSE LANDING GEAR WOULD NOT RETRACT. DURING LANDING GEAR MECHANICAL AND HYDRAULIC HEALTH CHECK, FOUND NGWOFW2 OUT OF LIMITS. READJUSTED NGWOFW2 SENSOR IAW AMM. CYCLED LANDING GEAR IAW AMM MULTIPLE TIMES WITH NO "GEAR DISAGREE" EICAS MESSAGE PRESENT THROUGHOUT. OPS CHECK GOOD. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 38,307 hrs · 35,320 cycles

GEAR DISAGREE ON DEPARTURE OUT OF ORD. NOSE GEAR SHOWED RED. RETURNED TO FIELD. ADJUSTED NGWOFW2 SENSOR IAW AMM. REMOVED AND REPLACED 3A & 3B ACMP AND SELECTOR VALVE IAW AMM. CYCLED LANDING GEAR MULTIPLE TIMES IAW AMM NO DEFECTS NOTED. OPS CHECK GOOD.

Part: LANDING GEAR — SLOW · airframe 37,166 hrs · 34,419 cycles

GEAR DISAGREE WARNING AFTER TAKEOFF DURING GEAR RETRACTION. LEVELED AT SAFE ALT TO RUN QRH. JUST AFTER WE STARTED QRH GEAR WENT UP ON ITS OWN. COMPLETED QRH AND CONTINUED. GEAR OPERATED NORMALLY DURING EXTENSION. (FLT#3134) CLOSED PERFORMED FULL STRUT SERVICE IAW AMM. PASSED FUNCTIONAL FLIGHT.

Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 36,140 hrs · 33,525 cycles

ON DEPARTURE OUT OF ICT AREA, CAPTAIN SIDE YOKE LIGHT STARTED SPARKING AND POPPING WITH SUBSEQUENTLY SMOKING. SMOKE PERSISTED FOR ABOUT 5-10 MINUTES WITH SMOKE/ELECTRICAL SMELL. (FLT#3113) CLOSED DEFERRED CAPT YOKE CHART HOLDER IAW MEL.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 36,041 hrs · 33,439 cycles

GEAR DISAGREE ON TAKEOFF. NOSE GEAR WOULD NOT RETRACT. FLIGHT 3130. FO: 9/14/2018. CLOSED REMOVED AND REPLACED NLG SELECTOR VALVE IAW AMM. PERFORMED FULL SWINGS OF LANDING GEAR (NOSE AND MAIN). OPS CHECKS AND LEAK CHECKS GOOD.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 35,050 hrs · 32,559 cycles

FOUND THE FLOORBEAM ANGLE TO HAVE EXFOLIATING CORROSION AT LBL 40, BS 349. INSTALLED A NEW ANGLE IAW SRM.

Part: FRAME — CORRODED (BS 310) · airframe 35,050 hrs · 32,559 cycles

FRAME BS 310 HAS CORROSION ON THE FLANGE BETWEEN STRINGERS 3L & 4L. BLENDED THE CORROSION IAW SRM, AND REO.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 35,050 hrs · 32,559 cycles

LOWER FUSELAGE EXTERIOR SKIN HAS SEVERAL SCRATCHES AT THE LT AND RT DME ANTENNA LOCATIONS. REPAIRED THE SKIN IAW REO.

Part: DOUBLER — CORRODED (DOOR FRAME) · airframe 35,050 hrs · 32,559 cycles

DOUBLER AT SERVICE DOOR FRAME BS 349, STRINGER 18R AND DOUBLER AND LOWER FRAME BRACKET AT BS 319.7, STRINGER 18R CORRODED. REPLACED THE DOOR FRAME BRACKETS AND RESTORED FINISH TO DOUBLERS IAW SRM.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 35,050 hrs · 32,559 cycles

CORROSION AROUND MULTIPLE FASTENER HOLES ON THE FLOORBEAM, LBL 9 TO RBL 9, BS 589. INSTALLED A NEW CAP STRIP ON THE FLOORBEAM IAW SRM.

Part: FLOORBEAM — CORRODED (BS 574) · airframe 35,050 hrs · 32,559 cycles

CORROSION AROUND MULTIPLE FASTENER HOLES ON FLOORBEAM, LBL 9 TO RBL 40, BS 574. INSTALLED A NEW CAP STRIP ON THE FLOORBEAM IAW SRM.

Part: RUB STRIP — CHAFED (LT AILERON) · airframe 35,050 hrs · 32,559 cycles

LEFT AILERON UPPER AND LOWER L/E EDGES RUB STRIPS ARE CHAFED AT VARIOUS LOCATIONS. REMOVED AND REPLACED THE RUB STRIPS IAW SRM AND REO.

Part: SKIN — DENTED (BS 310) · airframe 35,050 hrs · 32,559 cycles

ONE DENT FWD OF SERVICE DOOR AT BS 310, STRINGER 16R. REPAIRED IAW SRM.

Part: SKIN — DENTED (BS 310) · airframe 35,050 hrs · 32,559 cycles

TWO DENTS FWD OF SERVICE DOOR AT BS 310, STRINGER 12R. REPAIRED IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · 31,584 cycles

LEFT OTBD FLAP VANE HAS CHAFING NEAR OTBD ACTUATOR. INSTALLED A REPAIR IAW REO.

Part: PLATE — GOUGED (RT WING TE FLAP) · 31,584 cycles

RIGHT FLAP INBOARD ROLLER GUIDE PLATE IS GOUGED. REPLACED THE ROLLER GUIDE PLATE IAW SRM.

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 32,336 hrs · 29,702 cycles

AFTER TAKE OFF SELECTED GEAR UP GOT NOSE GEAR DISAGREE WARNING FOLLOWED QRH PROCEDURE TO EXTEND LANDING GEAR. ACFT DIVERTED. ADJUSTED NLG CENTERING PROXMITY SWITCH IAW AMM 32-61-05 OPS CHECKED GOOD.

Part: SHIM — SHIFTED (BS 513) · airframe 31,229 hrs · 28,713 cycles

MIGRATING SHIM BETWEEN FS 513.00 FRAME AND RT AND LT MCG SIDE BRACE FITTING BRACKETS. COMPLIED WITH ECTC REO 601R-53-41-101-01 PERMANENT REPAIR. COMPLIED WITH ECTC EO 600-53-26-50003. COMPLIED WITH EC/TC REO 601R-53-41-101 01. VERIFIED COMPLIANCE OF ECTC REO 601R-53-41-101-01. COMPLIED WITH ECTC REO 601R-53-41-101-01 AS WRITTEN.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 31,229 hrs · 28,713 cycles

STIFFENER ON REAR PRESSURE BULKHEAD AT LBL 36, FS 621 IS CRACKED. REMOVED CRACKED STIFFNER ANGLE ON RT PRESSURE BULKHEAD AT LBL36, FS621.00 IAW SRM 51-42-06. LOCATED, DRILLED NEW STIFFNER ANGLE IAW SRM 51-40-11. INSTALLED FASTENERS AT LBL36 FS621, REF SRM 51-42-06 AND SRM 51-42-21 AND DWG NR 601R-36008.

Part: SKIN — DAMAGED (BS 589-605) · airframe 31,229 hrs · 28,713 cycles

TEMP REPAIR ON FUSELAGE SKIN AT FS 589-605, STRINGERS 21-26R. REPAIR BECOMES PERMENANT AT REV A OF REO 601-53-61-5212.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 31,229 hrs · 28,713 cycles

OTBD NUTPLATE AREA CORRODED ON FLOORBEAM CAP AT 559+80 & RBL 27. REMOVED SEAT TRACK TRACK TO FOM IAW AMM 53-01-11. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802. UPON FURTHER INVESTIGATION FLOORBEAM CAP AT FS 559.00, RBL27 WAS EXTREMELY EXFOILATED AROUND NUTPLATE LOCATION. PERFORMED SRM 53-00-43 FLOORBEAM REPAIR NR 1. COMPLIED WITH SRM 53-00-43, NR 1.

Part: CROSSBEAM — CORRODED (BS 559) · airframe 31,229 hrs · 28,713 cycles

CORROSION ON CROSSBEAM 559 + 80 AND RBL 9. REMOVED CORROSION IAW SRM 51-21-06. REWORKED WITH THE ALLOWABLE DAMAGE LIMITS OF SRM 53-51-15-01 AND SRM 53-00-00-01, FIG 102.

Part: FITTING — CRACKED (BS 202) · airframe 31,229 hrs · 28,713 cycles

RIGHT WINDSHIELD CENTER POST LOWER FITTING CRACKED FS 202.75, WL 110.00. R & R CRACKED RT WINDSHIELD CENTER POST LOWER FITTING AT FS 202.75 AND WL 110.00 IAW SRM 51-42-21.

Part: BULKHEAD — CRACKED (BS 621) · airframe 31,229 hrs · 28,713 cycles

REAR PRESSURE BULKHEAD FORWARD FACE IS CRACKED AT LBL 36.20 JUST ABOVE WL 73.50, BS 621. COMPLIED WIHT EC/TC REO 601R-53-61-1285, REV D.

Part: BULKHEAD — CRACKED (BS 621) · airframe 31,229 hrs · 28,713 cycles

REAR PRESSURE BULKHEAD FORWARD FACE IS CRACKED AT BL 0.00 - 36.20 BETWEEN WL 73.50 AND WL 137.50 FS 621.00 AREA IS MARKED. COMPLIED WITH ECTC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, DATED: 10/31/2011. COMPLIED WITH REO 601R-53-61-5659. RECEIVED AND COMPLIED WITH ECTC REO 601R-53-61-56959.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 31,229 hrs · 28,713 cycles

RIGHT SIDE SEAT TRACK SEGMENT BS 409+16 - 409+112 CORRODED SEVERAL AREAS. REMOVED RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SIDE SEAT TRACK IAW AMM 53-01-11-400-802. COMPLIED WITH EC/TC REO 601R-53-00-055.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 31,229 hrs · 28,713 cycles

RT SIDE SEAT TRACK SEGMENT FS 364-409+16 CORRODED SEVERAL AREAS. REMOVED RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802. FABRICATED NEW SEAT TRACK IAW REO 601R-53-00-485. INSTALLED NEW FABRICATED RT SIDE SEAT TRACK IAW AMM 53-01-11-400-802. COMPLIED WITH EC/TC REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 31,229 hrs · 28,713 cycles

RT SIDE SEAT TRACK SEGMENT, FS 409+112-449.85 CORRODED SEVERAL AREAS. REMOVED RT SIDE SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SIDE SEAT TRACK IAW AMM 53-01-11-400-802. COMPLIED WITH EC/TC REO 601R-53-00-055.

Part: FLOOR SUPPORT — CORRODED (BS 574-589) · airframe 31,229 hrs · 28,713 cycles

CARGO RT FLOOR SILL CORRODED BETWEEN FS 574-589. REMOVED CORROSION ON RT FLOOR SILL TW FS 574-589 IAW SRM 51-21-06-00. ACCOMPLISHED CORROSION REMOVAL, BLEND OUT IAW REO 601R-53-61-5654. UPON FURTHER EVALUATION, FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS OF GEO 601R-53-00-526. RECEIVED REO 601R-53-21-5654 VERIFIED ALL STEPS WERE ACCOMPLISHED. RECEIVED AND COMPLIED WITH ECTC 601R-53-61-5654.

Part: DOOR SILL — CRACKED (BS 589) · airframe 31,229 hrs · 28,713 cycles

CARGO DOOR LOWER SILL CRACKED AT FS 589. COMPLIED WITH EC/TC REO 601R-53-61-433 AND REO 601R-53-21-433, REV C, DATED 11/23/2012 AS WRITTEN.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 31,229 hrs · 28,713 cycles

LEFT SIDE SEAT TRACK SEGMENT, BS 409+16 - 409+112 CORRODED SEVERAL AREAS. REMOVED LT SIDE SEAT TRACK IAW AMM 53-01-11-946-003. INSTALLED LT SIDE SEAT TRACK IAW AMM 53-01-11-420-802. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REV B.

Part: SEAT TRACK — CORRODED (BS 612-616) · airframe 31,229 hrs · 28,713 cycles

CORRODED SEAT TRACK SEGMENT, BS 612 - 616, LBL9. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW EC/TC REO 601R-53-00-485. INSTALLED NEW FABRICATED SEAT TRACK FS 612-616 LBL9 IAW AMM 53-00-49-400-801. COMPLIED WITH EC/TC REO 601R-53-00-485.

Part: CARGO TRACK — CORRODED (BS 584-600) · airframe 31,229 hrs · 28,713 cycles

CARGO TRACKS CORRODED ON LBL 9 AT FS 584 AND FS 600. FOUND OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-61-49, FIG 101. REMOVED THE CARGO TRACK IAW AMM 53-00-49-000-801. INSTALLED IAW AMM 53-00-49-400-801.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 31,229 hrs · 28,713 cycles

2 EA CARGO TRACKS CORRODED FROM FS 559+86-559+112, RBL9. EVALUATED 2 EA CARGO TRACKS. TRACKS AT DISCREPANT LOCATION AND FOUND OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-51-49 AND SRM 53-61-49, FIG 101. REMOVED 2 EA CORRODED CARGO TIE DOWN TRACKS AS NEEDED SRM 53-00-49-000-801. REPLACED 2 EA CARGO TIE DOWN TRACKS IAW AMM 53-00-49-400-801. COMPLIED WITH ECTC REO 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,229 hrs · 28,713 cycles

CABIN SEAT TRACK SEGMENT CORRODED BS 559+86, LBL9. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW FABRICATED SEAT TRACK FS 559+5-559+86, LBL9.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,229 hrs · 28,713 cycles

2 EA CARGO FLOOR TRACKS CORRODED FROM FS 559+86-559+122, LBL9. EVALUTED 2EA CARGO FLOOR TRACKS AT DISCREPANT LOCATIONS AND FOUND OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-51-49-01 AND 53-61-49-01, FIG 101. REMOVED 2EA CORRODED CARGO TIE DOWN TRACKS AS NEEDED REF AMM 53-00-49-000-801. REPLACED 2EA CARGO TIE DOWN TRACKS IAW AMM 53-00-49-400-801. COMPLIED WITH ECTC REO 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A.

Part: CARGO TRACK — CORRODED (BS 559-574) · airframe 31,229 hrs · 28,713 cycles

3 EA CARGO TRACKS CORRODED ON LBL 27 FROM FS 559+96-574.00. REMOVED 3 EA DISCREPANT CARGO TRACKS, ANCHOR PLATES REF: AMM 53-00*-49-000-801. INSTALLED 3 EA SERVICEABLE CARGO TRACKS IAW AMM 53-00-49-400-801. EVALUATED CORROSION DAMAGE FOR ALLOWABLE DAMAGE AND FOUND IT OUT OF THE ALLOWABLE LIMITS OF SRM 53-61-49-012, FIG 101.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 31,229 hrs · 28,713 cycles

CARGO TRACK CORRODED RBL27, FS 559+78-559+95. EVALUATED CARGO TRACK RBL27 FS 559+78-559+95 OUT OF LIMITS IAW SRM 53-61-49. REMOVED CARGO TRACK RBL27, 559+78-559+95 IAW AMM 53-00-49-000-801. FABRICATED NEW CARGO TRACK IAW EC/TC REO 601R-53-00-485. INSTALLED NEW FABRICATED CARGO TRACK IAW AMM 53-00-49-400-801. COMPLIED WITH EC/TC REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,229 hrs · 28,713 cycles

CABIN SEAT TRACK SEGMENT CORRODED BS 559+5 - 559+86, RBL9. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49, SRM 53-00-49. REMOVED SEAT TRACK IAW AMM 53-01-000-802. FABRICATED NEW SEAT TRACK IAW EC/TC REO 601R-53-00-485. INSTALLED NEW FABRICATED SEAT TRACK IAW AMM 53-01-11-400-802. COMPLIED WITH EC/TC REO 601R-53-00-485.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 31,229 hrs · 28,713 cycles

FLOORBEAM CAP CORRODED RBL9 BETWEEN 559+16 - 559+112. UPON FURTHER EVALUATION FOUND FLOORBEAM CAP TO BE OUT OF LIMITS IAW SRM 53-00-00 WITH SEVERE HEAVY CORROSION. COMPLIED WITH ECTC REO 601R-53-51-274.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 31,229 hrs · 28,713 cycles

FLOORBEAM CAP AT RBL9 SCREW HOLES CORRODED BETWEEN FRAME BS 409+9 - 409+35. BLENDED CORROISON DAMAGE IAW SRM 51-21-06. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-00-00 WITH NO MATERIAL REMAINING. REMOVED FASTENERS IN FLOORBEAM COMMON TO REPAIR IAW SRM 53-00-43, REPAIR NR 2. COMPLETED FLOORBEAM, REPAIR NR 2 IAW SRM 53-01-43. REPAIR NR 2.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 31,229 hrs · 28,713 cycles

LEFT SIDE SEAT TRACK SEGMENT FS 409+112 - 449.85 CORRODED SEVERAL AREAS. REMOVED LT SIDE SEAT TRACK IAW AMM 53-01-11-946-003. INSTALLED LT SIDE SEAT TRACK IAW AMM 53-01-11-420-001. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REV B.

Part: FITTING — GOUGED (E/E DOOR) · airframe 31,229 hrs · 28,713 cycles

MAIN AVIONICS COMPARTMENT FWD LT DOOR FITTING ON FUSELAGE IS GOUGED. BLENDED DAMAGE IAW SRM 51-12-00 BLEND AREA IS .5" WIDE X .2" T. ALL MATERIAL REMOVED IS .017" MEASURED USEING MACT 3100. SUBMITTED TO STS ENGINEERING FOR PERMANENT DISPOSITON REF SRM 51-13-00-01. COMPLIED WITH EA 32-2016-020.

Part: ANGLE — CRACKED (BS 621-625) · airframe 31,229 hrs · 28,713 cycles

ANGLE CRACKED AT FS 621-625.00 AND STR 14, LT AND RT SIDE. R & R CRACKED ANGLE AT FS 621-625.00 AND STR14 LT AND RT IAW SRM 51-42-21.

Part: FITTING — GOUGED (E/E DOOR) · airframe 31,229 hrs · 28,713 cycles

MAIN AVIONICS COMPARTMENT FWD RT DOOR FITING ON FUSELAGE IS GOUGED. NO ALLOWABLE DAMAGE. BLENDED DAMAGE IAW IAW SRM 51-12-00 BLEND AREA IS .5" WIDE X .2" TALL MATERIAL REMOVED IS .019" MEASURED USING MACT 3100. SUBMITTED TO ENGINEERING FOR PERMANENT DISPOSITON, REF SRM 51-13-00-01. COMPLIED WITH EA32-2016-020.

Part: RIB — CRACKED (LT MLG WW) · airframe 31,229 hrs · 28,713 cycles

INSIDE LT WHEEL WELL, LT BATTERY RIB CRACKED AT WS 53.60. REPAIRED BATTERU RIB ASSY IAW REO 601R-57-51-046, REV B. RECEIVED AND COMPLIED WITH ECTC REO 601R-57-51-046.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,524 hrs · 28,086 cycles

OUTSIDE FWD EMERGENCY LIGHT BURNED OUT. R & R OUTSIDE FWD EMERGENCY LIGHT BULB IAW AMM 33-51-21.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 30,076 hrs · 27,686 cycles

SECOND AFT CABIN EMERGENCY CEILING FLOOD LIGHT IS INOPERATIVE. R & R CABIN EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OP'S CHECKED GOOD.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 30,018 hrs · 27,632 cycles

LIGHTED EXIT SIGN ABOVE SERVCE DOOR DAMAGED. R & R SIGN IAW AMM 33-51-13. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 28,210 hrs · 25,918 cycles

NR 1 FWD RT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R RT NR 1 EXTERIOR EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD. SDR CLOSED.

Part: SKIN — DAMAGED (BS 589-605) · airframe 26,895 hrs · 24,612 cycles

MULTIPLE DENTS & GOUGES ON FUSELAGE SKIN & GROUND AIR DOOR, BS 589-605, S21-56R. COMPLIED WITH REO 601R-53-61-5212 AND EC/TC REO 601R-53-61-5212.

Part: BULKHEAD — CRACKED (BS 621) · airframe 26,895 hrs · 24,612 cycles

FS 621 BULKHEAD AT LBL 27.5 WL 105.43 IS CRACKED. C/W EC/TC EO 600-53-0745 AND REO 601R-53-61-1285 REV D. MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 26,895 hrs · 24,612 cycles

INTERCOSTAL AT S27R BETWEEN BS 349 & 364 IS CORRODED OUT OF LIMITS. REMOVED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED INTERCOSTAL IAW SRM 51-42-06, & 51-42-21.

Part: ANGLE — CRACKED (BS 280) · airframe 26,894 hrs · 24,611 cycles

FS 280, RBL 9.0 OTBD ANGLE IS CRACKED. FABRICATED NEW ANGLE IAW REO 601R-53-11-171 AND NOTE 9, REV D. INSTALLED IAW REO 601R-53-11-171.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 26,895 hrs · 24,612 cycles

CORROSION ON FLOOR SUPPORT AFT OF PAX DOOR AT FS 349. COMPLIED WITH REO 601R-53-00-530.

Part: FLOOR SUPPORT — CORRODED (BS 319-364) · airframe 26,894 hrs · 24,611 cycles

CORROSION ON RT FLOOR SUPPORT AT FS 319 AND BETWEEN FS 349 AND 364. CORROSION FOUND OUT OF LIMITS. REPAIRED IAW REO 601R-53-21-2520.

Part: FRAME — CORRODED (BS 319.7) · airframe 26,895 hrs · 24,612 cycles

CORROSION ON FRAME FWD FACE AT BS 319.7, BL 0, S27. REMOVEDFRAME LOWER SECTOR IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW FRAME SECTOR IAW SRM 51-40-11. INSTALLED FRAME SECTOR IAW SRM 51-42-06 AND 51-42-21.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 26,894 hrs · 24,611 cycles

FS 621, BULKHEAD HAS A .75 INCH CRACK AT RBL 27.5 JUST BELOW WL 120.43. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND REO 601R-53-61-1285, REV D.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 26,894 hrs · 24,611 cycles

FS 621, BULKHEAD HAS A .75 INCH CRACK AT LBL 27.5 JUST BELOW WL 137.5. REMOVED DAMAGE IN BULKHEAD WEB IAW REO 601R-53-61-1541.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 26,894 hrs · 24,611 cycles

FS 484 INTERCOSTAL ANGLE AT WL 72.50, LBL 27 IS CRACKED .250 INCH LONG IN UPPER RADIUS. R & R ATTACH ANGLE IAW SRM 51-42-21.

Part: POST — CRACKED (BS 409) · airframe 26,894 hrs · 24,611 cycles

FOUND FS 409.0+128, VERTICAL POST LBL 18 INBD AND OTBD SIDES HAVE INDICATIONS NOTED AT AFT FLANGE RADIUS APPROX .3 INCH IN LENGTH 50 PERCENT FSH. BOTH FAILED NDT INSPECTION. REMOVED VERTICAL POST IAW SRM 51-42-06. INSTALLED NEW POST IAW BSC REO/ECTC 601R-53-41-889 REV A AND SRM 51-42-06 AND 51-42-22.

Part: SUPPORT FITTING — CRACKED (BS 460) · airframe 26,894 hrs · 24,611 cycles

SUPPORT FITTING AT FS 460, WL 72.50, LBL 10 IS CRACKED APPROXIMATELY .750 INCH LONG IN UPPER RADIUS. REMOVED DAMAGED SUPPORT FITTING IAW SRM 51-42-06 AND 51-42-21. DRILLED NEW SUPPORT FITTING IAW SRM 51-40-11 AND INSTALLED IAW SRM 51-42-06 & 51-42-21.

Part: POST — CRACKED (BS 409) · airframe 26,894 hrs · 24,611 cycles

FOUND FS 409.0+128 VERTICAL POST BL 0 HAD CRACK INDICATIONS. REMOVED POST IAW SRM 51-42-06-00, 51-42-21-00. DRILLED AND LOCATED NEW POST IAW SRM 51-40-11. INSTALLED POST IAW SRM 51-42-06, 51-42-22 AND C/W ECTC REO 601R-53-41-889.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 26,894 hrs · 24,611 cycles

FS 484, INTERCOSTAL ANGLE AT WL 72.50, RBL 9 IS CRACKED .375 INCH LONG IN UPPER RADIUS. R & R DAMAGED INTERCOSTAL ANGL IAW SRM 51-42-06.

Part: POST — CRACKED (BS 409) · airframe 26,894 hrs · 24,611 cycles

FOUND FS 409.0+128 VERTICAL POST RBL 18.0 INBD AND OTBD SIDES HAVE CRACK INDICATIONS IN AFT FLANGE RADIUS APPROX .3 INCH IN LENGTH 50 PERCENT FSH. REMOVED POST IAW SRM 51-42-06. LOCATED, DRILLED AND ASSEMBLED NEW POST IAW SRM 51-40-11, 51-42-06. INSTALLED POST IAW SRM 51-42-06, 51-42-22.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 26,894 hrs · 24,611 cycles

EMERGENCY EXIT LIGHT ON RT BOTTOM OF THE GALLEY HAS A DAMAGED FRAME WHERE ATTACHING SCREW GOES THROUGH. REMOVED AND INSTALLED A SERVICEABLE EMERGENCY EXIT LIGHT ON GALLEY SIDE PANEL IAW AMM 33-51-10-400-801 PROCEDURE 3A. OPS TESTED GOOD IAW AMM 33-51-00-710-801. DURING OPS CHECK OF THE EMERGENCY LIGHTS FOUND FLOOR LEVEL EXIT SIGN ON THE WARDROBE TO HAVE A BROKEN CONNECTOR. REPAIRED CONNECTOR BY CRIMPING A NEW PIN ONTO THE WIRE IAW ESPM 20-17-31.

Part: FRAME — CRACKED (BS 682) · airframe 26,894 hrs · 24,611 cycles

FRAME AT BS 682 HAS A DENT .060" DEEP WITH CRACK .185" LONG BETWEEN S26L - 26R. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-01. REPAIRED IAW EA 28-2014-006 AND EA 28-2014-006.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 26,894 hrs · 24,611 cycles

FS 621 BULKHEAD, FWD SIDE, ISOLATOR MOUNTS CRACKED, BROKEN OR MISSING. R & R ISOLATORS IAW SRM 51-42-13.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 26,894 hrs · 24,611 cycles

AFT PRESSURE BULKHEAD HAS TWO BROKEN ISOLATORS AT LBL 27.5. COMPLIED WITH EC/TC REO:601R-53-61-1541 AND F REO 601R-53-61-1541, REV D, REMOVED BROKEN ISOLATORS AT FS 621, LBL 27.5 AND INSTALLED NEW ISOLATORS IAW SRM 51-42-13.

Part: BULKHEAD — CRACKED (BS 621) · airframe 26,893 hrs · 24,610 cycles

AFT PRESSURE BULKHEAD HAS A 0.75 INCH CRACK AT BS 621 RBL 27.50 JUST BELOW WL 120.43. REPAIRED IAW AMM 21-51-15-400-801, AMM 49-14-01-400-801, AMM 26-25-01-400-801, AMM 26-25-01-400-802, AMM 36-11-07-400-801, & AMM TASK 21-51-00-790-801.

Part: BULKHEAD — CRACKED (AFT PRESSURE) · airframe 26,893 hrs · 24,610 cycles

AFT PRESSURE BULKHEAD HAS A TWO AND A HALF INCH CRACK AT LBL 27.5 JUST BELOW WL 120.43. FURHTER INSPECTION FOUND CRACK AT WL 105.43. REPAIRED IAW EO 600-53-0745 AND REO 601R-53-61-1285 REV D. MAJOR REPAIR.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 26,893 hrs · 24,610 cycles

AFT PRESSURE BULKHEAD HAS A 0.75 INCH CRACK AT BS 621 LBL 27.50 JUST BELOW WL 137.5. REMOVED DAMAGE IN BULKHEAD WEB IAW REO 601R-53-61-1541. COMPLIED WITH REO 601R-53-61-1541, REV D.

Part: BULKHEAD — CRACKED · airframe 26,895 hrs · 24,612 cycles

REAR PRESSURE BULKHEAD FOUND CRACKED AT LBL 27.50 JUST BELOW WL 137.5. 0.75" CRACK. REPAIRED REAR PRESSURE BULKHEAD IAW ECTC REO 601R--53-61-1541 AND ECTC REO 601R-53-61-1285.

Part: DOOR — UNKNOWN · airframe 25,219 hrs · 23,069 cycles

FRONT DOOR IS STICKING HARD TO OPEN. INSPECTED AND OP'S CHECK PAX DOOR IAW AMM 52-11-00. OP'S CHECKED GOOD.

Part: PRIORITY VALVE — UNSERVICEABLE (MLG) · airframe 23,649 hrs · 21,502 cycles

AFTER TAKE OFF AND GEAR SELECTED UP, RECEIVED GEAR DISAGREE WARNING MESSAGE WITH ASSOCIATED INDICATIONS. NOSE GEAR SHOWED RED WITH BOTH MAIN AMBER, COMPLIED WITH QRH AND RECEIVED THREE GREEN GEAR INDICATIONS. EMERGENCY DECLARED, RETURNED TO DEPARTURE FOR NORMAL LANDING. R & R NLG PRIORITY VALVE IAW AMM 32-33-15.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,561 hrs · 21,399 cycles

NR 3 EXTERIOR EMERGENCY LIGHT IS OUT. RELAMPED THE NR 3 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CK GOOD. SDR CLOSED.

Part: SEAT TRACK — CORRODED (BS 364-694) · airframe 23,329 hrs · 21,136 cycles

SEAT TRACK CORRODED FROM FS 364 TO 394 AT RBL 9.0. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 53-01-01-000-802 AND 53-01-01-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 23,329 hrs · 21,136 cycles

PASSENGER COMPARTMENT FLOOR SUPPORT AT LBL 27 HAS CORROSION FROM FS 574.09 - 621. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-51-43 AND 53-27. REMOVED FLOOR SUPPORT IAW SRM 51-42-06 & SRM 51-42-21. INSTALLED SERVICEABLE FLOOR SUPPORT IAW REO 601R-53-61-3778, REV A.

Part: FLOOR SUPPORT — CORRODED (BS 319.7-333) · airframe 23,329 hrs · 21,136 cycles

FS 319.7 TO FS 333 INBD OF RBL 9.0 FLOOR SUPPORT CORRODED. FABRICATED CAPPING PLATE IAW SNIEO 601R38778 S02. INSTALLED ABRASION RESISTANT FILM IAW SRM 51-27-19.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 23,329 hrs · 21,136 cycles

FS 484, FLOORBEAM CRACKED AT RBL 27 & RBL 35, RBL 36. REPAIRED IAW REO 601R-53-41-059.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 23,329 hrs · 21,136 cycles

PASSENGER COMPARTMENT BS 621 PRESSURE BULKHEAD WEB FWD FACE HAS FOUR CRACKED ISOLATORS. R & R DAMAGED ISOLATORS IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 23,329 hrs · 21,136 cycles

SEAT TRACK CORRODED FS 409 TO 409+128 AT RBL 9.0. R & R SEAT TRACK SEGMENT AT LBL 9.0 FROM FS 409 TO 409+128 IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 23,329 hrs · 21,136 cycles

FLOORBEAM CAP CORRODED AT FS 349 RBL 27 TO RBL 45. REPAIRED IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 23,329 hrs · 21,136 cycles

SEAT TRACK CORRODED FROM FS 364 TO 394 AT LBL 9.0. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 53-01-01-000-802 AND 53-01-01-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 23,329 hrs · 21,136 cycles

PASSENGER COMPARTMENT FLOOR SUPPORT HAS MULTIPLE AREAS OF CORROSION AROUND FASTENER HOLES AT LBL 45 FROM FS 559+112 - 621. ON FURTHER INVESTIGATION, TOP & BOTTOM SIDES OF FLOOR SUPPORT ARE CORRODED, CORROSION FOUND TO BE OUT OF LIMITS OF SRM TR53-27. R & R FLOOR SUPORT IAW REO 601R-53-61-1574, REV B.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 23,329 hrs · 21,136 cycles

SEAT TRACK CORRODED FROM FS 394 TO 409+128 AT RBL 9.0. R & R SEAT TRACK WITH NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 23,329 hrs · 21,136 cycles

SEAT TRACK CORRODED FROM FS 409+128 TO 559 AT LBL 9.0. R & R SEAT TRACK SEGMENT AT LBL 9.0 FROM FS 409+128 TO FS 559.0 WITH NEW SERVICEABLE TRACK SEGMENT IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 23,329 hrs · 21,136 cycles

SEAT TRACK CORRODED FROM JUST FWD OF FS 409 AT LBL 9.0 (APPROX 15" LONG) R & R SEAT TRACK WITH NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 23,329 hrs · 21,136 cycles

SEAT TRACK CORRODED FROM FS 409+128 TO 559 AT RBL 9.0. REMOVED SEAT TRACK IAW SRM 51-41-02. INSTALLED NEW SERVICEABLE TRACK SEGMENT IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,329 hrs · 21,136 cycles

PASSENGER COMPARTMENT SEAT TRACK HAS SEVERAL AREAS OF CORROSION AT FS 559 - 559+80 AT RBL 9. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW IAW AMM TASK 53-01-11-400-802.

Part: WEB — CRACKED (PAX DOOR) · airframe 23,329 hrs · 21,136 cycles

PASSENGER DOOR AFT WEB IS CRACKED BETWEEN STEPS 832DT AND 832CT AND STEPS 832CT AND FIXED STEP. REPAIRED IAW ECTC REO 601R-52-11-702.

Part: WEB — CRACKED (PAX DOOR) · airframe 23,329 hrs · 21,136 cycles

PASSENGER DOOR FWD WEB IS CRACKED BETWEEN STEP 832CT AND 832DT. REPAIRED IAW REO 601R-52-11-702.

Part: ANGLE — CRACKED (BS 621-625) · airframe 23,329 hrs · 21,136 cycles

LEFT AND RIGHT FS 621-625 OBLIQUE ANGLES CRACKED. INSTALLED NEW OBLIQUE ANGLES IAW SRM 51-42-21-00.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,329 hrs · 21,136 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED IN PREVIOUSLY SPLICED SECTION. R & R PAX DOOR AFT DRAG ANGLE IAW SRM 51-42-06.

Part: RELAY — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 22,644 hrs · 20,350 cycles

EMERGENCY LIGHT STAY ON WHEN SWITCH SELECT IN ARM AND ACFT IS POWER UP. R & R AC ESSENTIAL BUSS SENSE RELAY IAW IAW AMM 24-51-27. OPS CHECKED GOOD.

Part: LANDING GEAR — LACK OF LUBE (NOSE) · airframe 22,082 hrs · 19,733 cycles

AFTER TAKEOFF, RECEIVED "GEAR DIAGREE" MESSAGE WHILE GEAR WAS COMING UP THERE WAS BUFFETING NOISES FROM NOSE GEAR AREA, DECLARED EMERGENCY AND RETURNED TO DEPARTURE. EMERGENCY DECLARED. LUBRICATED NOSE GEAR LANDING IAW AMM 12-20-32. PERFORMED NOSE EXTRENSION & RETRACTION IAW AMM 32-33-00. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,419 hrs · 19,010 cycles

LEFT SIDE MIDDLE EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LEFT SIDE MIDDLE EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD IAW AMM 33-51-21. (CLOSED)

Part: PLACARD — MISSING (PAX DOOR) · airframe 20,419 hrs · 17,908 cycles

PAX DOOR MISSING EXIT PLACARD. INSTALLED MISSING EXIT PLACARD ON PAX DOOR IN REF TO AMM CHAP 11-30-00.

Part: OIL SYSTEM — LOW (RT ENGINE) · airframe 20,290 hrs · 17,756 cycles

RT ENGINE LOW OIL PRESSURE MASTER CAUTION ON CLIMBOUT. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) PERFORMED OIL CONSUMPTION CHECK, RUN ACFT AT 85 PERCENT N1 FOR 30 MINUTES WITH NO OIL PRESSURE INDICATIONS IAW AMM 71-00-00-710-810. NO FURTHER DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,138 hrs · 17,580 cycles

EMERGENCY LIGHT ON RT SIDE (1) FWD OF DOOR INOP. RELAMPED EMERGENCY LIGHT AS REQUIRED IAW AMM 32-42-01, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,022 hrs · 17,455 cycles

RT EXTERIOR NR 3 EMERGENCY LIGHT INOP. R & R RT EXTERIOR NR3 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CK GOOD. R & R RT EXTERIOR NR3 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CK GOOD. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,909 hrs · 17,322 cycles

EXTERIOR EMERGENCY LIGHTS 7 AND 8 INOP. R & R NR4 EMERGENCY BATTERY PACK FOR LIGHTS IAW AMM 33-51-04. OPS CHECKS GOOD. NO DEFECTS NOTED. PLACARD REMOVED. DMIL CLEARED. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,903 hrs · 17,316 cycles

EXTERIOR EMERGENCY LIGHTS 7 AND 8 INOP. R & R NR4 EMERGENCY BATTERY PACK FOR LIGHTS IAW AMM 33-51-04. OPS CHECKS GOOD. NO DEFECTS NOTED. PLACARD REMOVED. DMIL CLEARED.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,780 hrs · 17,166 cycles

EXTERIOR EMERGENCY LIGHTS 7 & 8 INOPERATIVE. R & R BATTERY CHARGER NR 4 IAW AMM 33-51-05, OPS CHECK GOOD. DMIL CLEARED, PLACARD REMOVED. R & R BATTERY CHARGER NR4 IAW AMM 33-51-05, OPS CHECK GOOD. DMIL CLEARED, PLACARD REMOVED.

Part: CONTROL UNIT — FAILED (FLT SPOILERS) · airframe 19,503 hrs · 16,848 cycles

FLT SPOILERONS CAUTION MESSAGE FLT SPOILERS CAUTION MESSAGE AND INBD GROUND SPOILER FAULT MESSAGE IN FLIGHT. (EMERGENCY DECLARED) CX FOUND SECU 2 MODULE B TO HAVE MULTIPLE FAULTS IN THE FAULT LOG. R & R RELAY K4CN IAW AMM 20-42-00. R & R NR 2 SECU IAW AMM 27-61-05. FUNCTIONAL & OPS TESTS GOOD IAW AMM SUBTASK 27-61-05-710-001. (CLOSED)

Part: RELAY — FAILED (SPOILERS) · airframe 19,483 hrs · 16,823 cycles

DURING CRUISE, RECEIVED A SPOILERONS CAUTION MESSAGE ,FOLLOWED BY A FLT SPOILERS CAUTION MESSAGE FOLLOWED BY AN INBD GROUND SPOILER FAULT STATUS MESSAGE (EMERGENCY DECLARED) R & R RELAY K3CN FOR SECU POWER SUPPLY IAW ESPM 20-22-00 OPS CHECK GOOD JB-10 RETEST GOOD. (CLOSED)

Part: CLAMP — LOOSE (APU BAY) · airframe 19,266 hrs · 16,576 cycles

FLT 4964...WHILE BOARDING PAX GOT MAIN BAT CHARGER, APU BAT CHARGER, CARGO BOTTLE AND APU BOTTLE LOW INDICATIONS. UPON INSPECTION FOUND SEVERAL BLEED LEAKS. RESECURED CLAMPS AND LINES AND NO FURTHER LEAKS NOTED. OPS CHECKED MAIN AND APU CHARGERS IAW 24-32-03. OPS CHECKS GOOD. REFER TO AFDL 526613-3 FOR WORK PERFORMED ON APU BOTTLE LOW MSG.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 19,240 hrs · 16,547 cycles

NOSE GEAR DISAGREE CYCLED 5 TIMES IAW QRH, HAD TO MANUAL EXTEND, NO NOSE WHEEL STEERING ON THE GROUND. (EMERGENCY DECLARED]) R & R NOSE GEAR SELECTOR VALVE IAW AMM 32-33-10, OPS CHECK IS GOOD, LEAK CHECK GOOD.

Part: DOOR — BINDING (MAIN PAX) · airframe 19,166 hrs · 16,453 cycles

MAIN CABIN DOOR DIFICULT TO OPEN. OPENED/ CLOSED MULITPLE TIMES " OPS TEST OF PAX DOOR" IAW AMM 52-11-00-710-801. NO TROUBLE FOUND, OK FOR SERV.

Part: WIRE HARNESS — DISCONNECTED (STALL FAIL) · airframe 18,908 hrs · 16,159 cycles

STALL FAIL MSG AFTER TAKEOFF. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED). FOUND WIRES FROM CAPTAINS STICK SHAKER MOTOR PULLED OUT OF CONNECTER. REINSTALLED WIRES IAW WM 27-35-00. NO OTHER SPS FAULTS FOUND IAW FIM 27-30-00 SPS SYS OPS CHECK NORMAL.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 18,807 hrs · 16,045 cycles

SERVICE DOOR TRIM PANEL EXIT LIGHT INOP (FWD PF DOOR). FOUND WIRING FROM EMERGENCY POWER SUPPLY SWAPPED BETWEEN VERTICAL EMERGENCY LIGHT ASSY AND HORIZONTAL LIGHT ASSY. PROPERLY SWAPPED WIRING BACK TO CORRECT LIGHT IAW AMM 33-51-00 AND COMPLIED WITH OPS TEST OF THE EMERGENCY LIGHTS IAW AMM TASK 33-51-00-710-801. NO DEFECTS FOUND.

Part: FRAME — CORRODED (BS 333) · airframe 18,807 hrs · 16,043 cycles

GENERATED FROM OP 297/FRAME SECTION 333 BETWEEN RBL 26 AND LBL 26 CORRODED FWD AND AFT SIDE. FINISH INSTALLING FRAME PN 601R32004-55. TP161741 2/13/10 (AJ 2/13/10) INSTALLED REMAINING FASTNER IN FRAME 333 AND APPLIED FINISH A023 IAW SRM 51-42-21 AND 51-21-16.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 18,807 hrs · 16,043 cycles

INTERCOSTAL AT LBL 2 BETWEEN FS 349-FS 364 IS CORRODED. REMOVED INTERCOSTAL. REMOVED GUSSETT REMOVED DOOR POSITION SWITCH SUPPORT BRACKET. REMOVED CABLE TIE STANDOFFS. DRILLED NEW INTERCOSTAL IAW SRM 51-40-11 READY TO INSTALL. INSTALLED INTERCOSTAL FASTENERS, WITH THE EXCEPTION OF 4 EACH FASTENERS AT AFT SIDE AT DOOR PROX SWITCH.

Part: SKIN SPLICE — CORRODED (BS 333) · airframe 18,807 hrs · 16,043 cycles

SKIN SPLICE DOUBLER AT FS 333 CORRODED IS SEVERAL PLACE FROM LBL24-RBL 24. REMOVED CORROSION FROM SKIN SPLICE DOUBLER AT FS 333 LBL 24-RBL 24 IAW SRM 51-12-00. REMOVE MATERIAL FOUND TO BE WITHIN LIMITS IAW SRM 51-21-31. BLENDED AREAS. COMPLETE STEP 5 B(5) PAGE 7, SRM 51-12-00 TW 161754 4. PERFORMED LPI TYPE 1 METHOD C ON BLEND AREAS OF SKIN SPLICE DOUBLER AT FS 333.00, LBL 24- RBL24 IAW SRM 51-12-00 PARA 5 B (2)(I) IAW NDTM PART 1 51-20-08 NO RELEVANT INDICATIONS NOTED AT THIS TIME.

Part: FRAME — CORRODED (BS 349) · airframe 18,807 hrs · 16,043 cycles

CORROSION FOUND ON FRAME FS 349 LBL 6 APPROX (MARKED). REMOVED FRAME. VERIFIED POSITION OF NEW FRAME AND DRILLED IAW SRM 51-40-11. INSTALLED FRAME IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 333) · airframe 18,807 hrs · 16,043 cycles

FRAME SECTION 333 BETWEEN RBL 26 AND LBL 26 CORRODED FWD AND AFT SIDE. REMOVED CORROSION ON FRAME IAW SRM 53-21-15. MECHANICALLY MEASURED FRAME 333 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-15. REMOVED FRAME. DRILLED NEW FRAME IAW SRM 51-42-06 AND 51-42-21. INSTALLED FRAME IAW SRM 51-42-06 AND 51-42-21. CONTINUED ON OP 317.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 18,807 hrs · 16,043 cycles

ALL CARGO TRACKS IN CARGE COMPARTMENT ARE CORRODED. 4 EACH BULKHEAD FITTING ASSY'S NEED INSTALLED ON CARGO FLOOR TRACKS. INSTALLED BULKHEAD FITTINGS P/N CDSP 1900-509 PO NR M0000000255 IN NEW SERVICEABLE CONDITION ON TO CARGO COMPT. SEAT TRACKS IAW AMM 20-21-00-910-004.

Part: PLATE — CORRODED (CABIN) · airframe 18,807 hrs · 16,043 cycles

NUT PLATES CORRODED FOR CARGO DOOR STEP PLATE. REMOVED 14EA NUTPLATES FOR CARGO DOOR STEP PLATE IAW SRM 51-45-00 2. INSTALLED 10EA NEW NUTPLATES FOR CARGO DOOR STEP PLATE IAW SRM 51-45-00 3. INSTALLED 4EA. NUT PLATES REF SRM 51-45-00 & SRM 51-42-15 M45.

Part: DOOR — NO TEST (EMERGENCY EXIT) · airframe 18,807 hrs · 16,043 cycles

RIGHT EMERGENCY EXIT FAILED, FUNCTIONAL CHECK. UPON INSPECTION FOUND AIRFRAME INSULATION TO BE IN DOOR FRAME. REPOSITION INSULATION AS REQUIRED. DOOR FUNCTIONAL CHECK GOOD. IAW AMM 52-21-00 TASK 52-21-00-720-801.

Part: DOOR — NO TEST (EMERGENCY EXIT) · airframe 18,807 hrs · 16,043 cycles

LEFT EMERGENCY EXIT FAILED FUNCTIONAL CHECK. UPON INSPECTION FOUND AIRFRAME INSULATION TO BE IN DOOR FRAME. REPOSITIONED INSULATION AS REQUIRED. DOOR FUNCTIONAL CHECK GOOD IAW AMM 52-21-00 TASK 52-21-00-720-801.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 18,807 hrs · 16,043 cycles

ALL SEAT TRACKS IN CARGO COMPARTMENT ARE CORRODED. REMOVED CARGO COMPARTMENT SEAT TRACK & ANCHOR FITTINGS DUE TO CORROSION. INSTALLED SERVICEABLE CARGO FLOOR TRACK PER AMM 53-01-11-400-802, 20-21-00-910-801 AND SRM 53-61-49 PO NR 7620-00001.

Part: FRAME — CORRODED (BS 349) · airframe 18,807 hrs · 16,043 cycles

CORROSION FOUND ON FRAME FS 349 LBL 6 APROX. REMOVED CORROSION ON BACK SIDE OF FRAME IAW SRM 51-21-06.

Part: INTERCOSTAL — CRACKED (BS 460) · airframe 18,434 hrs · 15,643 cycles

WHILE WORKING SB 601R-53-067 FOR THE MODIFICATION OF THE OVERWING PRESSURE FLOOR - FOUND THE INTERCOSTAL AT FS 460 RBL 9-18 CRACKED AT LOWER FLANGE. REMOVED CRACK DEBURRED AND REMOVED SHARP EDGES IAW REO 601R-53-41-1089, REV -- NDT FS460 RBL9-18 FLANGE CUTOUT IAW NDTM 51-20-06 NO DEFECTS NOTED. FABRICATED DOUBLER IAW REO 601R-53-41-1089, REV. INSTALLED DOUBLER IAW REO 601R-53-41-1089 REV

Part: FLOOR PANEL — CRACKED (BS 460) · airframe 18,434 hrs · 15,643 cycles

CRACK NOTED & MARKED ON PRESSURE FLOOR AT FS460.00 BETWEEN LBL9 & BL0.0, AFT OF INTERCOSTAL. DRILLED AND REMOVAL .250 HOLE TO REMOVE CRACK AT FS460.00 LBL 6 IAW REO 601R-53-41-082. PERFORMED ET AND PT INSP IAW REO 601R-53-41-1082 REV A DATE 09/20/09 IAW MM AND TM 51-20-06 AND 51-20-08 NO DEFECTS NOTED. TOUCHED UP REWORKED AREA (ALODINED, PRIMED AND PAINTED) WHERE .0250" HOLE IS DRILLED IAW REO 601R-53-41-1082 REV A 2009-09-20. 10/04/09.

Part: FLAP — FAILED (WING) · airframe 18,360 hrs · 15,578 cycles

FLAPS FAIL AT 0 ON APPROACH KPHF. CREW NEVER TOUCHED FLAP LEVER. EMERGENCY DECLARED.

Part: LIGHT — CRACKED (CABIN) · airframe 18,346 hrs · 15,566 cycles

LOWER EMERGENCY FLOOD LIGHT ON FWD WARDROBE CLOSET BASE IS CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,104 hrs · 15,323 cycles

AFT MOST CEILING EMERGENCY LIGHT IS INOP.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 18,038 hrs · 15,254 cycles

IN FLIGHT CARGO BOTTLE LOW INDICATION, FOLLOWED QRH AND LANDED NEAREST SUITABLE AIRPORT. AFDL#438707-2...FLT 5502 DEL 111 MINS & FLT 5502 DEL 247 MINS. EN ROUTE TO BTR A/C DIVERTED TO MEI DUE TO MTC. FIRE CREW OPENED CARGO DOOR, IT WAS DETERMINED TO BE AN INDICATION PROBLEM. CARGO COMPARTMENT FIRE EXTINGUISHING SYSTEM.

Part: COVER — MISSING (CABIN) · airframe 17,566 hrs · 14,796 cycles

REFER TO DMIL 472341-3 RT SIDE PHOTO ILLUMINESCENT COVER MISSING.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,055 hrs · 12,522 cycles

LOWER FS 280 FLOORBEAM WEB CRACKED OUTBOARD OF RBL9 (MARKED). REPAIRED DAMAGE IAW EO 600-53-90.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,055 hrs · 12,522 cycles

AAR - 1002 - FS 280 CLIP AT RBL 9 O/B IS CRACKED. REPAIRED DAMAGE TO FS 280 WEB O/B OF RBL 9 IAW EO 600-53-90 C/W. SUPPLEMENTAL SDR CLOSED 4/3/08.

Part: ANGLE — CRACKED (BS 280) · airframe 15,055 hrs · 12,522 cycles

FS 280 AFT ANGLE CRACKED JUST O/B OF LBL 9.0. COMPLIED WITH EO 600-53-0091 PER REO 601R-53-11-136 & 601R53-11-1311.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,055 hrs · 12,522 cycles

CLIP CRACKED AT FS 280, FLOOR LEVEL AT LBL 9 I/B (RESOLVED ON W/O: 82203 TASKCARD: N/R-00022). REPAIRED DAMAGED TO FS 280 WEB O/B OF LBL 9 IAW EO 600-53-90 C/W JB13225.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,055 hrs · 12,522 cycles

AAR - 1003 - FS 280 CLIP AT LBL 9 O/B IS CRACKED. CLIP IS REPLACED ON REPAIR OF FLOORBEAM ASA EC/TC REO 601R-53-21-787 MH13328. SUPPLEMENTAL SDR CLOSED 4/2/08.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,055 hrs · 12,522 cycles

CLIP CRACKED AT FS 280, FLOOR LEVEL AT RBL 9 I/B (RESOLVED ON W/O: 82203 TASKCARD: N/R-00023). REPAIRED DAMAGE TO FS 280 WEB O/B OF RBL 9 IAW EO 6+00-53-90 C/W.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 14,659 hrs · 12,203 cycles

L-ANGLE PART NUMBER 601R35050-109 CRACKED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,659 hrs · 12,203 cycles

AFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING. REF; NDTM PART 6 53-61-153.

Part: PLACARD — WORN (PAX DOOR) · airframe 14,643 hrs · 12,189 cycles

PASSENGER DOOR EXIT PLACARD IS WORN.

Part: BRACKET — CRACKED (AIRSTAIR DOOR) · airframe 14,079 hrs · 11,722 cycles

ASD AFT CABLE COUNTER BALANCE ANCHOR BRACKET CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,033 hrs · 11,681 cycles

CEILING EMERGENCY LIGHT AT SEAT 5AB INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,776 hrs · 10,703 cycles

CEILING EMERGENCY LIGHT 1EA INOP.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 12,225 hrs · 10,289 cycles

FLAPS FAIL MESSAGE AT 39 DEGREES OF TRAVEL AT 10000 FEET. EMERGENCY DECLARED.

Part: ANGLE — CRACKED (BS 625) · airframe 11,845 hrs · 9,998 cycles

RT 625 OBLIQUE IS CRACKED. REMOVED AND REPLACED CRACKED OBLIQUE ANGLE WITH SERVICEABLE PART P/N 601-35012-51 IAW CRJ 200 SRM 51-42-21. (SUPPLEMENTA-SDR CLOSED 10/3/06)

Part: ANGLE — CRACKED (BS 625) · airframe 11,845 hrs · 9,998 cycles

LT 625 OBLIQUE IS CRACKED. REMOVED LT 625 OBLIQUES AND INSTALLED A NEW 601-35012-51 PER CRJ SRM 53-61-17 AND 51-42-21, DR618 10-03-06.

Part: RIB — CRACKED (RT WING) · airframe 11,845 hrs · 9,998 cycles

RT BATTERY RIB CRACKED. REMOVED RT BATTERY RIB ACCESS COVER. REMOVED CONNECTORS J410 & J412. REMOVED REQUIRED FASTENERS FOR REPAIR. CUT OUT DAMAGED SECTION OF RT BATTERY RIB IAW REO 601R-57-51-046. DC699 9-26-06. RA313. FABRICATED -6 DOUBLER FROM SERVICEABLE PN S6144-4 IAW REO601R-57-51-046. DC699 9-26-06. RA333 FABRICATED -8 FILLER IAW REO 601R-57-51-046. DC699. OK TO ALODINE, PRIME AND PAINT -6 DOUBLER & -8 FILLER IAW REO601R-57-51-046. DC699 9-29-06. REINSTALLED CONNECTORS J410 & J412. DC699 9-29-06. RA190. OK TO INSTALL ACCESS COVER. RA190. REINSTALLED ACCESS COVER IAW CRJ SRM 51-41-04. DC699 9-29-06. RA190. COMPLIED WITH ASA REOI 601R-57-51-046 TO REPAIR RT BATTERY RIB. DG419 10-3-6. (CLOSED)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 11,845 hrs · 9,998 cycles

EXTERNAL EMERGENCY LIGHT ON RT SIDE AFT OF EMERGENCY EXIT DOOR IS INOP.

Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 11,573 hrs · 9,790 cycles

LAV SMOKE DETECTOR DID NOT GENERATE -AURAL MSG- SMOKE IN COCKPIT.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 11,332 hrs · 9,602 cycles

EMERGENCY FLOOR LEVEL EXIT SIGNS BU PAX AND SERVICE DOORS ARE INOP

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,261 hrs · 9,541 cycles

EMERGENCY EXIT FLOOD LIGHT AT PAX DOOR AND FWD FACING CURVED EMERGENCY EXIT MIDWAY DOWN AISLE ARE INOP.

Part: LIGHT — BROKEN (PAX DOOR) · airframe 11,261 hrs · 9,541 cycles

EMERGENCY LIGHT AT BOARDING DOOR BROKEN.

Part: STEP — CRACKED (AIRSTAIR) · airframe 11,165 hrs · 9,456 cycles

BOTTOM AIRSTAIR STEP CRACKED ON SIDE. FLT 4621 DEL 115 MINS & INBOUND FLT 4621 DEL 260 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,928 hrs · 9,254 cycles

FOUND FWD OVHD INTERIOR EMERGENCY LIGHT INOP.

Part: ATTACH FITTING — CRACKED (AFT SERVICE DOOR) · airframe 10,641 hrs · 9,034 cycles

ASD AFT ANCHOR FITTING CRACKED.

Part: STEP — CRACKED (AIRSTAIR DOOR)

DURING A HANGAR INSPECTION IN MCN, THE AIRSTAIR DOOR BOTTOM STEP WAS FOUND TO BE CRACKED AT THE ATTACHED BRACKET STAY ROD. MAINTENANCE REMOVED AND REPLACED THE AIR STAIR DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FAIRING — DAMAGED (RT WING)

DURING TAKEOFF, TOWER INFORMED CREW THAT TIRE DEBRIS WAS NOTIED ON RUNWAY AFTER DEPARTURE. THERE WERE NO INDICATIONS OF ENGINE DAMAGE AND AC CONTINUED. EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS PRECAUTION. AC LANDED SAFELY. UPON TOUCHDOWN, FIRE AND RESCUE CONFIRMED IB RT MAIN TIRE WAS SHREDDED. MAINT REMOVED AND REPLACED RT MLG IB AND OB WHEEL AND TIRE ASSEMBLIES. ALSO, FOUND RT IB FLAP ASSEMBLY, RT WING TRAILING EDGE FAIRING AND RT SIDE AFT BELLY FARING DAMAGED. MAINTENANCE REMOVED AND REPLACED RT IB FLAP ASSY AND T WING T/E FAIRING. MAINT REPAIRED THE RT SIDE AFT BELLY FAIRING IAW SRM. OPS CHECKS GOOD. AC OK FOR SERVICE. (K)

Part: TIRE — SEPARATED

DURING TAKEOFF, TOWER INFORMED CREW THAT TIRE DEBRIS WAS NOTICED ON RUNWAY AFTER DEPARTURE. THERE WERE NO INDICATIONS OF ENGINE DAMAGE AND AC CONTINUED. EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS PRECAUTION. AC LANDED SAFELY. UPON TOUCHDOWN, FIRE AND RESCUE CONFIRMED IB RT MAIN TIRE WAS SHREDED. MAINT REMOVED AND REPLACED RT MLG IB AND OB WHEEL AND TIRE ASSEMBLIES. ALSO, FOUND RT IB FLAP ASSEMBLY, RT WING TRAILING EDGE FAIRING AND RT SIDE AFT BELLY FARING DAMAGED. MAINTENANCE REMOVED AND REPLACED RT IB FLAP ASSY AND RT WING T/E FAIRING. MAINT REPAIRED THE RT SIDE AFT BELLY FAIRING IAW SRM. OPS CHECKS GOOD AC OK FOR SERVICE. (K)

Part: FAIRING — DAMAGED (FUSELAGE)

DURING TAKEOFF, TOWER INFORMED CREW THAT TIRE DEBRIS WAS NOTICED ON RUNWAY AFTER DEPARTURE. THERE WERE NO INDICATIONS OF ENGINE DAMAGE AND AC CONTINUED. EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS PRECAUTION. AC LANDED SAFELY. UPON TOUCHDOWN, FIRE AND RESCUE CONFIMED IB RT MAIN TIRE WAS SHREDDED. MAINT REMOVED AND REPLACED RT MLG IB AND OB WHEEL AND TIRE ASSEMBLIES. ALSO, FOUND RT IB FLAP ASSEMBLY, RT WING T/E FAIRING AND RT SIDE AFT BELLY FARING DAMAGED. MAINTENANCE REMOVED AND REPLACED RT IB FLAP ASSY AND RT WING TRAILING EDGE FAIRING. MAINT REPAIRED THE RT SIDE AFT BELLY FAIRING IAW SRM. OPS CHECK GOOD. AC OK FOR SERVICE. (K)

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN CVG, THE EMERGENCY LIGHTS WOULD ONLY TEST FOR A FEW SECONDS. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, AN EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN AN EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR IAW AMM. (K)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE THIRD EXTERIOR EMERGENCY LIGHT ON THE LT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE THIRD EXTERIOR EMERGENCY LIGHT ON THE LT SIDE. OPS CHECK GOOD. AIRCRAFT OF FOR SERVICE. (K)

Part: SILL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL AT FS 562.72 - FS 589 UNDER THE FORWARD LATCH ANGLE 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: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 484 LEFT/RIGHT INTERCOSTALS, BL 27 TO 36 AND THE RIGHT INBOARD CLIP WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 484 LT/RT INTERCOSTALS, BL 27 TO 36 AND REMOVING AND REPLACING THE RIGHT INBOARD CLIP IAW ASA EO 600-53-0098. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 LT/RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AT BL 36.20 LT/RT IAW ASA EO 600-53-0073. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE OUTBOARD FS 280 LEFT CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE OUTBOARD FS 280 LT CLIP. (M)

Part: LENS — CRACKED (CABIN)

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

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCJHN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

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

Part: NUT — MISSING (CABIN)

DURING A GROUND INSPECTION, THE FORWARD EMERGENCY FLOOR LEVEL FLOODLIGHT BY THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A NUT MISSING ON THE GROUND STUD TO THE FORWARD EMERGENCY FLOOR LEVEL FLOODLIGHT BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: WIRE — PINCHED (CABIN)

DURING A GROUND INSPECTION, THE LOWER FORWARD EMERGENCY LIGHT ON THE BULKHEAD BY THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A WIRE TO THE LOWER FORWARD EMERGENCY LIGHT ON THE BULKHEAD BY THE PASSENGER DOOR PINCHED BY A TIE WRAP CAUSING THE WIRE TO PULL LOOSE FROM ITS CONNECTION. MAINTENANCE REMOVED THE TIE WRAP AND RESECURED THE CONNECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE, THE EMERGENCY EXIT LIGHT NEAR THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP NEAR THE SERVICE DOOR. OPERATIONAL CHECKS GOOD AIRCRAFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 6,725 hrs

DURING HANGAR MAINTENANCE, THE EMERGENCY EXIT LIGHT NEAR THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE MID CABIN OVERHEAD EMERGENCY EXIT SIGN AND THE FLOOR LEVEL FLOODLIGHT BY THE PASSENGER DOOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY CHARGER FOR THE MID CABIN. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: HINGE — BROKEN (DOOR STEP)

FLT 4573 - DURING A GROUND INSPECTION IN DFW, THE TOP STEP HINGE ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE TOP STEP HINGE ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LENS — BROKEN (EMERGENCY LIGHT)

FLT 4269 - DURING A GROUND INSPECTION IN DFW, THE EMEGENCY EXIT ILGHT AT THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS AT THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX STAIRS)

DURING A C-CHECK IN MCN, THE TOP AND BOTTOM STEPS ON THE PASSENGER DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP AND BOTTOM STEPS ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A C-CHECK IN MCN, THE FLOOR EMERGENCY FLOOR LIGHT NEAR THE FLIGHT ATTENDANTS STATION WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLOOR EMERGENCY FLOOR LIGHT LAMP NEAR THE FLIGHT ATTENDANTS STATION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (FUSELAGE)

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

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN BTR, THE LOWER EMERGENCY LIGHT AT THE PASSENGER DOOR ENTRANCE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LOWER EMERGENCY LIGHT LAMP AT THE PASSENGER DOOR ENTRANCE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (EMERGENCY EXIT)

FLT 4415 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMPS BY THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

FLT 4071 - DURING GROUND INSPECTION IN DFW, THE RIGHT WING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)