N921FJ

Part: BULB — INOPERATIVE (ZONE 200) · airframe 40,343 hrs · 32,500 cycles

MID CABIN EMER EXIT SIGN FWD LIGHT INOP REPLACED BULB

Part: TIRE — BURST (NR 3) · airframe 40,036 hrs · 32,277 cycles

#3 TIRE BURST ON ON GROUND DUE TO #4 TIRE BURST. REPLACED #3 MLG TIRE AND COMPLIED WITH BURST TIRE INSPECTION.

Part: TIRE — BURST (NR 4 MLG) · airframe 40,036 hrs · 32,277 cycles

#4 MLG TIRE BURST ON GROUND DURING TAXI, EMERGENCY DECLARED. REPLACED #4 MLG TIRE AND COMPLIED WITH TIRE BURST INSPECTION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,010 hrs · 32,259 cycles

EMER CEILING FLOOD LIGHT ROW 15 INOP. REPLACED BULB

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,010 hrs · 32,259 cycles

EMER EXIT SIGN ROW 13 LHS 1 BULB INOP. REPLACED BULB.

Part: LIGHT — MISSING (CABIN) · airframe 39,889 hrs · 32,170 cycles

FORWARD EMERGENCY PATH LIGHT STRIP MISSING.

Part: ECU — FAULTED (TE FLAPS) · airframe 39,397 hrs · 31,791 cycles

FLAPS FAIL CAUTION IN FLIGHT, EMERGENCY DECLARED. MX RE-RACKED BOTH SFECU'S, OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,376 hrs · 31,933 cycles

R/H FLOOR SEAT TRACK FROM F.S.364-477 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR SEAT TRACK FROM F.S. 364-477 IAW CRJ900 SRM 51-41-02.

Part: LIGHT — INOPERATIVE · airframe 38,759 hrs · 31,318 cycles

ROW 15 CEILNG LEVEL EMERGENCY LIGHT INOP. PLACED ON MEL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,684 hrs · 31,273 cycles

LH ROW 14 FLOOR LEVEL EXIT SIGN 1 BULB INOP. PLACED ON MEL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,573 hrs · 31,206 cycles

14A FLOOR EMERGENCY EXIT SIGN 1 BULB INOPERABLE, PLACED ON MEL.

Part: LIGHT — INOPERATIVE (ROW 11) · airframe 38,493 hrs · 31,154 cycles

ROW 11 EMERGENCY CEILING FLOOD LIGHT INOPERABLE. PLACED ON MEL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,419 hrs · 31,103 cycles

CEILING EMERGENCY LIGHT ROW 11 INOPERABLE, RELAMPED.

Part: LAMP — INOPERATIVE (EMER FLOODLIGHT) · airframe 38,344 hrs · 31,045 cycles

CEILING EMERGENCY FLOODLIGHT AT ROW 11 INOPERABLE, RELAMPED.

Part: LAMP — INOPERATIVE (FLOOD LIGHT) · airframe 38,217 hrs · 30,961 cycles

EMERGENCY CEILING FLOODLIGHT ROW 11 C INOPERABLE, RELAMPED.

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 38,172 hrs · 30,929 cycles

LT ENGINE LOWER THRUST REVERSER SKIN AND COAMING CRACKED NEAR LATCH COVER DOOR. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 4092.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 38,172 hrs · 30,929 cycles

STRINGER 24R SPLICE AT FS 333.00 CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVAMX W/O: 80889 W/C: 1236.

Part: ANGLE — CRACKED (BS 280) · airframe 38,172 hrs · 30,929 cycles

LT AND RT ANGLES AT BL 26.00 AT FS 280 ARE CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2319.

Part: SKIN — GOUGED (BS 927) · airframe 38,172 hrs · 30,929 cycles

LOWER FUSELAGE SKIN GOUGED OUT OF LIMITS BETWEEN FS 913 TO FS 927 ON EACH SIDE OF STGR 27. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/0: 80889 W/C: 1143.

Part: SEAT TRACK — CORRODED (BS 349-477) · airframe 38,172 hrs · 30,929 cycles

RT FLOOR SEAT RAIL FROM FS 349 TO FS 477 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2235.

Part: FLOORBEAM — CORRODED (BS 985) · airframe 38,172 hrs · 30,929 cycles

FLOOR SUPPORT CROSSBEAM AT FS 985 IS CORRODED BEYOND LIMITS (LOCATED BENEATH FLOORBOARD 281HLF). CORRECTIVE ACTION TO BE ACCOMPLISHED ON W/O: 80889 W/C:1223.

Part: SHIELD — GOUGED (RT NACELLE) · airframe 38,172 hrs · 30,929 cycles

RT LOWER COWLING HAS TWO GOUGES OUT OF LIMITS IN THE FIRE SHIELD. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 4082.

Part: BRACKET — CORRODED (BS 295-310) · airframe 38,172 hrs · 30,929 cycles

HYDRAULIC LINE MOUNT BRACKET ATTACHED TO STGR 26L BETWEEN FR 295 AND FR 310 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1165.

Part: CAP — CORRODED (PAX DOORWAY) · airframe 38,172 hrs · 30,929 cycles

FLOOR MID CAP AT PAX DOOR ENTRANCE IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1146.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 38,172 hrs · 30,929 cycles

RT SIDE SEAT RAIL FROM FS 847+8.40 TO FS 865 HAS SIGNS OF CORROSION IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2240.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 38,172 hrs · 30,929 cycles

LT SIDE SEAT RAIL AT FS 785 TO FS 847+8.40 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2239.

Part: FLOOR SUPPORT — CORRODED (BS 969-1098) · airframe 38,172 hrs · 30,929 cycles

RT FLOOR SILL BETWEEN FS 969 AND FS 1098 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1218.

Part: SUPPORT BRACKET — CORRODED (BS 280) · airframe 38,172 hrs · 30,929 cycles

FLOOR BOARD MOUNT ON THE AFT SIDE OF FRAME 280 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON W/O: 80889 W/C: 1169.

Part: SEAT TRACK — CORRODED (BS 661-720) · airframe 38,172 hrs · 30,929 cycles

RT SIDE SEAT RAIL FROM FS 661+90 TO FS 720.85 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2237.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 38,172 hrs · 30,929 cycles

KICK ANGLE AT PAX DOOR ENTRANCE IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 82889 W/C: 1147.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1047) · airframe 38,172 hrs · 30,929 cycles

LT FLOOR SUPPORT BEAM IS CORRODED OUT OF LIMITS BETWEEN FS 1000 AND FS 1047. CORRECTIVE ACTION TO BE ACCOMPLISHED ON W/O: 80889 W/C: 1215.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 38,172 hrs · 30,929 cycles

RT SIDE SEAT RAIL FROM FS 785 TO FS 847+8.4 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON W/O: 80889 W/C: 2241.

Part: SEAT TRACK — CORRODED (BS 847-865) · airframe 38,172 hrs · 30,929 cycles

RT SIDE SEAT RAIL FROM FS 847+40 TO FS 865 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2240.

Part: SEAT TRACK — CORRODED (BS 661) · airframe 38,172 hrs · 30,929 cycles

LT SIDE SEAT RAIL AT FS 661+16 TO FS 661+90 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2247.

Part: SEAT TRACK — CORRODED (BS 661-677) · airframe 38,172 hrs · 30,929 cycles

LT FLOOR SEAT RAIL AT FS 661+32 TO FS 677 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2254.

Part: SEAT TRACK — CORRODED (BS 661-720) · airframe 38,172 hrs · 30,929 cycles

LT SIDE SEAT RAIL FROM FS 661+90 TO FS 720.85 HAS SIGNS OF CORROSION IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON W/O: 80889 W/C: 2236.

Part: SEAT TRACK — CORRODED (BS 565-661) · airframe 38,172 hrs · 30,929 cycles

RT SIDE SEAT RAIL FROM FS 565 TO FS 661+16 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2246.

Part: SEAT TRACK — CORRODED (BS 565-661) · airframe 38,172 hrs · 30,929 cycles

LT SIDE SEAT RAIL AT FS 565 TO FS 661+16 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2245.

Part: SEAT TRACK — CORRODED (BS 847) · airframe 38,172 hrs · 30,929 cycles

LT FLOOR SEAT RAIL BETWEEN FS 847 AND 847+62 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2278.

Part: SEAT TRACK — CORRODED (BS 969-985) · airframe 38,172 hrs · 30,929 cycles

AFT LAV SEAT TRACK AT LAV MOUNT BETWEEN FS 969 TO FS 985 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2286.

Part: SEAT TRACK — CORRODED (BS 847-913) · airframe 38,172 hrs · 30,929 cycles

LT SIDE SEAT RAIL AT FS 847+40 TO FS 913 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2242.

Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 38,172 hrs · 30,929 cycles

LT SIDE SEAT RAIL AT FS 785 TO FS 847+8.40 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2239.

Part: SEAT TRACK — CORRODED (BS 477-565) · airframe 38,172 hrs · 30,929 cycles

LT SIDE SEAT RAIL FROM FS 477 TO FS 565 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2243.

Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 38,172 hrs · 30,929 cycles

LT FLOOR SEAT RAIL AT FS 847+62 TO FS 977 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2276.

Part: SEAT TRACK — CORRODED (BS 565-661) · airframe 38,172 hrs · 30,929 cycles

RT SIDE SEAT RAIL FROM FS 565 TO FS 661+16 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2246.

Part: STRINGER — CORRODED (BS 280-319) · airframe 38,172 hrs · 30,929 cycles

STRINGER 27 IS CORRODED OUT OF LIMITS BETWEEN FS 280-295, AND FS 310-319. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1166.

Part: SEAT TRACK — CORRODED (BS 847) · airframe 38,172 hrs · 30,929 cycles

RT FLOOR SEAT RAIL BETWEEN FS 847 AND FS 847+62 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2277.

Part: STRINGER — CORRODED (BS 280-349) · airframe 38,172 hrs · 30,929 cycles

STRINGER 25R IS CORRODED OUT OF LIMITS BETWEEN FR 280 AND FR 349. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1180.

Part: SEAT TRACK — CORRODED (BS 477-581) · airframe 38,172 hrs · 30,929 cycles

RT FLOOR SEAT RAIL FROM FS 477 TO FS 581 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2250.

Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 38,172 hrs · 30,929 cycles

RT FLOOR SEAT RAIL BETWEEN FS 847+62 AND FS 977 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2275.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 38,172 hrs · 30,929 cycles

RT INBOARD FWD INTERCOSTAL LOCATED BETWEEN FR 349 AND FR 364 AND STGR 27 AND STGR 26R IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1175.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 38,172 hrs · 30,929 cycles

LT FLOOR SEAT RAIL FROM FS 581 TO FS 661+32 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2251.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 38,172 hrs · 30,929 cycles

LT INBOARD FWD INTERCOSTAL LOCATED BETWEEN FR 349 AND FR 364 AND BETWEEN STGR 26L AND STGR 27 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1176.

Part: SEAT TRACK — CORRODED (BS 661) · airframe 38,172 hrs · 30,929 cycles

RT SIDE SEAT RAIL FROM FS 661+16 TO FS 661+90 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2248.

Part: SEAT TRACK — CORRODED (BS 477-581) · airframe 38,172 hrs · 30,929 cycles

LT FLOOR SEAT RAIL AT FS 477 TO FS 581 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2249.

Part: STRINGER SPLICE — CORRODED (BS 333-349) · airframe 38,172 hrs · 30,929 cycles

STRINGER 26R SPLICE IS CORRODED OUT OF LIMITS BETWEEN FR 333 AND FR 349. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1184.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 38,172 hrs · 30,929 cycles

RT INBOARD INTERCOSTAL LOCATED BETWEEN FR 349 AND FR 364, AND BETWEEN STGR 26R AND STGR 27 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1175.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 38,172 hrs · 30,929 cycles

LT INBOARD INTERCOSTAL LOCATED BETWEEN FR 349 AND FR 364 BETWEEN STGR 26L AND STGR 27 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1176.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 38,172 hrs · 30,929 cycles

RT OUTBOARD INTERCOSTAL LOCATED ON STGR 26R BETWEEN FR 349 AND FR 364 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1174.

Part: STRINGER SPLICE — CORRODED (BS 319-333) · airframe 38,172 hrs · 30,929 cycles

STRINGER 27 IS CORRODED OUT OF LIMITS UNDER STRINGER SPLICE BETWEEN FR 319 AND FR 333. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1160.

Part: SEAT TRACK — CORRODED (BS 661-677) · airframe 38,172 hrs · 30,929 cycles

RT FLOOR SEAT RAIL FROM FS 661+32 TO FS 677 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2253.

Part: STRINGER — CORRODED (BS 280-310) · airframe 38,172 hrs · 30,929 cycles

STRINGER 24R IS CORRODED OUT OF LIMITS BETWEEN FR 280 TO FR 310 AND BETWEEN FR 333 TO FR 349. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1179.

Part: SEAT TRACK — CORRODED (BS 477-581) · airframe 38,172 hrs · 30,929 cycles

RT FLOOR SEAT RAIL FROM FS 477 TO FS 581 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2250.

Part: SEAT TRACK — CORRODED (BS 661) · airframe 38,172 hrs · 30,929 cycles

RT SIDE SEAT RAIL FROM FS 661+16 TO FS 661+90 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2248.

Part: SEAT TRACK — CORRODED (BS 661-677) · airframe 38,172 hrs · 30,929 cycles

RT FLOOR SEAT RAIL FROM FS 661+32 TO FS 677 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2253.

Part: STRINGER — CORRODED (BS 280-319) · airframe 38,172 hrs · 30,929 cycles

STRINGER 27 IS CORRODED OUT OF LIMITS BETWEEN FS 280 AND FS 319. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1166.

Part: SEAT TRACK — CORRODED (BS 477-581) · airframe 38,172 hrs · 30,929 cycles

LT FLOOR SEAT RAIL FROM FS 477 TO FS 581 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2249.

Part: SEAT TRACK — CORRODED (BS 874-977) · airframe 38,172 hrs · 30,929 cycles

RT FLOOR SEAR RAIL BETWEEN FS 874+62 AND FS 977 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2275.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 38,172 hrs · 30,929 cycles

RT FLOOR SEAT RAIL AT FS 581 TO FS 661+32 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2252.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 38,172 hrs · 30,929 cycles

RT OUTBOARD INTERCOSTAL LOCATED ON STGR 26R BETWEEN FR 349 AND FR 364 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1174.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 38,172 hrs · 30,929 cycles

LT FLOOR SEAT RAIL FROM FS 581 TO FS 661+32 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2251.

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 38,172 hrs · 30,929 cycles

RT FLOOR SEAT RAIL FROM FS 581 TO FS 661+32 IS CORRODED OUT OF LIMITS IN MULTIPLE AREAS. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2252.

Part: STRINGER — CORRODED (BS 280-310) · airframe 38,172 hrs · 30,929 cycles

STRINGER 24R IS CORRODED OUT OF LIMITS BETWEEN FR 280 AND FR 310, AND BETWEEN FR 333 AND FR 349. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1179.

Part: STRINGER — CORRODED (BS 319-333) · airframe 38,172 hrs · 30,929 cycles

STRINGER 27 IS CORRODED OUT OF LIMITS BETWEEN FR 319 AND FR 333. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1160.

Part: STRINGER — CORRODED (BS 280-349) · airframe 38,172 hrs · 30,929 cycles

STRINGER 26R IS CORRODED OUT OF LIMITS BETWEEN FS 280 AND FS 349. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1182.

Part: STRINGER — CORRODED (BS 280-333) · airframe 38,172 hrs · 30,929 cycles

STRINGER 26L IS CORRODED OUT OF LIMITES BETWEEN FR 280 AND FR 333. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1164.

Part: STRINGER — CORRODED (BS 280-333) · airframe 38,172 hrs · 30,929 cycles

STRINGER 25L IS CORRODED OUT OF LIMITS BETWEEN FR 280 AND FR 333. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1162.

Part: STRINGER — CORRODED (BS 280-333) · airframe 38,172 hrs · 30,929 cycles

STRINGER 25L IS CORRODED OUT OF LIMITS BETWEEN FR 280 AND FR 333. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1162.

Part: STRINGER SPLICE — CORRODED (BS 333-349) · airframe 38,172 hrs · 30,929 cycles

STRINGER 26R SPICE IS CORRODED OUT OF LIMITS BETWEEN FR 333 AND FR 349. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1184.

Part: STRINGER — CORRODED (BS 280-349) · airframe 38,172 hrs · 30,929 cycles

STRINGER 24R HAS SIGNS OF CORROSION BETWEEN FRAME 280 AND FRAME 310 AND BETWEEN FRAME 333 AND FRAME 349. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 89889 W/C: 1179.

Part: STRINGER — CORRODED (BS 280-333) · airframe 38,172 hrs · 30,929 cycles

STRINGER 26L IS CORRODED OUT OF LIMITS BETWEEN FR 280 AND FR 333. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1164.

Part: STRINGER — CORRODED (BS 280-349) · airframe 38,172 hrs · 30,929 cycles

STRINGER 25R IS CORRODED OUT OF LIMITS BETWEEN FR 280 AND FR 349. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1180.

Part: STRINGER — CORRODED (BS 280-310) · airframe 38,172 hrs · 30,929 cycles

STRINGER 24L IS CORRODED OUT OF LIMITS BETWEEN FR 280 AND FR 310. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1161.

Part: WINDOW POST — CRACKED (RT COCKPIT) · airframe 38,172 hrs · 30,929 cycles

RT WINDSHIELD TO SIDE WINDOW POST CRACKED AT TOP BARREL NUT. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 2302.

Part: STRINGER — CORRODED (BS 333-349) · airframe 38,172 hrs · 30,929 cycles

STRINGER 25R IS CORRODED OUT OF LIMITS BETWEEN FR 333 AND FR 349. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1185.

Part: STRINGER — CORRODED (BS 280-349) · airframe 38,172 hrs · 30,929 cycles

STRINGER 26R IS CORRODED OUT OF LIMITS BETWEEN FR 280 AND FR 349. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1182.

Part: BRACKET — CRACKED (PAX DOOR ASSIST) · airframe 38,172 hrs · 30,929 cycles

PASSENGER DOOR ASSIST MOTOR OUTBOARD BRACKET CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 8067.

Part: FRAME — CORRODED (BS 364) · airframe 38,172 hrs · 30,929 cycles

FRAME 364 IS CORRODED OUT OF LIMITS BETWEEN STGR 26L AND 26R. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1177.

Part: STRINGER SPLICE — CORRODED (BS 333-349) · airframe 38,172 hrs · 30,929 cycles

STRINGER 25R SPLICE CORRODED OUT OF LIMITS BETWEEN FR 333 AND FR 349. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 1185.

Part: WEB — CRACKED (E/E BAY) · airframe 38,172 hrs · 30,929 cycles

LT FWD EQUIPMENT COMPARTMENT FLOOR WEB IS CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/0: 80889 W/C: 2185.

Part: TRAY — CRACKED (E/E BAY) · airframe 38,172 hrs · 30,929 cycles

FWD EQUIPMENT COMPARTMENT JB6 TRAY CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C:2184.

Part: PANEL — CRACKED (RT WING LE) · airframe 38,172 hrs · 30,929 cycles

RT WING LEADING EDGE PANEL 622BR HAS A CRACK AT APPROX WS 231.23. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 6056.

Part: DRAG ANGLE — CRACKED (PAX DOOR STEP) · airframe 38,172 hrs · 30,929 cycles

PAX DOOR AFT STAIR WEB DRAG ANGLE IS CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/0: 80889 W/C: 8056.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 38,172 hrs · 30,929 cycles

AFT CARGO DOOR AFT SUPPORT DOUBLER IS CRACKED. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/0: 80889 W/C: 8065.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,500 hrs · 32,263 cycles

CLASS DIVIDER AND OVHD EMER LTS INOP

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 37,636 hrs · 30,529 cycles

SVC DOOR EMER EXIT LIGHT 1 BULB INOP- PLACED ON MEL

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 37,541 hrs · 30,459 cycles

14DF EXIT SIGN BULB INOP REPLACED BULBS

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 37,392 hrs · 30,350 cycles

CA FLASHLIGHT INOP. RELAMPED

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,144 hrs · 30,168 cycles

PAX DR FLR EXIT SIGN 1 BULB INOP- RELAMPED

Part: LIGHT — INOPERATIVE (ROW 1) · airframe 37,050 hrs · 30,099 cycles

ROW 1 CEILING LEVEL EMERG FLOOD LIGHT INOP- PLACED ON MEL

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,200 hrs · 29,443 cycles

ENTRY EMER LIGHT FLOOR LVL INOP. REPLACED LIGHT ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,635 hrs · 28,993 cycles

ROW 14DF FLOOR EMER LIGHT 1 BULB INOP. PLACED ON MEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,635 hrs · 28,993 cycles

ROW 14AC FLOOR EMER LT 2 BULBS INOP. PLACED ON MEL.

Part: SIGN — INOPERATIVE (ROW 14) · airframe 35,408 hrs · 28,823 cycles

ROW 14 D/F EMER EXIT SIGN 1 LT INOP. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,258 hrs · 27,960 cycles

ROW 14DF EXIT SIGN HAS ONE BULB INOP. PLACED ON MEL

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 34,247 hrs · 27,954 cycles

EMERG OVERHEAD FLOOD LIGHT ROW 18 INOP. PLACED ON MEL

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 33,485 hrs · 27,358 cycles

FWD FA FLASHLIGHT INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,129 hrs · 27,063 cycles

ROW 9, OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,396 hrs · 26,909 cycles

AFT FA FLASHLIGHT RED LIGHT NOT BLINKING. PLACED ON MEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,021 hrs · 32,643 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,394 hrs · 26,506 cycles

FWD LEFT & RIGHT EXT EMERG OVERWING LIGHTS INOP. REPLACED BATTERY AND CHARGER

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 32,122 hrs · 26,291 cycles

FWD FA FLASHLIGHT INOP. REPLACED BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,888 hrs · 26,092 cycles

ROW 21 CEILING EMERGENCY FLOOD LIGHT INOP. PLACED ON MEL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,085 hrs · 25,444 cycles

SEVERAL EMERGENCY FLOOD LIGHTS INOPERATIVE. REPLACED THE NR 2 BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,400 hrs · 24,890 cycles

SECOND TO AFT CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: HINGE — GOUGED (FUSELAGE) · airframe 30,179 hrs · 24,727 cycles

PASSENGER DOOR HINGE (FUSELAGE SIDE) GOUGED ON MOST AFT LANDING AND FACE APPROX .75" LONG, .060" WIDE, .100" DEEP.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 30,179 hrs · 24,727 cycles

INTERCOSTAL AT STR 20R IS CORRODED BETWEEN FS 310- FS 319.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,179 hrs · 24,727 cycles

SERVICE DOOR SILL ANGLE IS CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 319.70 TO FS 349.0.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 30,179 hrs · 24,727 cycles

AFT BAGGAGE BAY DOOR CUT OUT, FLOOR SILL CORRODED, P/N:MM670-35655-001. REMOVED AND REPLACED WITH SERVICEABLE P/N MM670-35655-001 FLOOR SILL IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 & 51-42-21-001-001-A01.

Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 30,179 hrs · 24,727 cycles

LT VERTICAL STABILIZER FORWARD DRAG ANGLE IS CRACKED.

Part: FRAME — CHAFED (FUSELAGE) · airframe 30,179 hrs · 24,727 cycles

RT SIDE AT FS 1144 FRAME IS CHAFED BY WATER INJECTION LINE AT STRINGER 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,179 hrs · 24,727 cycles

RT CABIN FLOOR TRACK SEGMENT BL9.0 FS 349-FS 421.0 IS CORRODED.

Part: STRINGER — CHAFED (BS 1144-1162) · airframe 30,179 hrs · 24,727 cycles

BS 1144 AND 1162 STRINGER 7L IS CHAFED AND SUPPORT BRACKET IS BROKEN.

Part: SIGN — INOPERATIVE (ROW 3) · airframe 29,801 hrs · 24,427 cycles

LIGHTED EXIT SIGN AT ROW 3 WAS FOUND INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,777 hrs · 24,409 cycles

ROW 3 EXIT SIGN HAD TWO BULBS INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,771 hrs · 24,404 cycles

AFT F/A FLASHLIGHT INOPERATIVE. PLACED ON MEL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,742 hrs · 24,383 cycles

ROW 3 EXIT SIGN INOPERATIVE. CHARGED THE BATTERIES

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,440 hrs · 24,168 cycles

EMERGENCY LIGHTS INOPERATIVE. CHARGED BATTERIES.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 29,416 hrs · 24,151 cycles

FWD FA FLASHLIGHT INOPERATIVE. R & R THE BATTERY.

Part: SIGN — UNKNOWN (EMERGENCY LIGHTS) · airframe 29,416 hrs · 24,151 cycles

EMERGENCY EXIT SIGN AT ROW 4 INOPERATIVE. OPS CHECKED GOOD

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,352 hrs · 24,102 cycles

ALL OVERHEAD EMERGENCY CEILING FLOOD LIGHTS INOPERATIVE EXCEPT ROW 15. CHARGED THE BATTERIES.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,352 hrs · 24,102 cycles

EMERGENCY EXIT SIGNS AT THE RT BULKHEAD INOPERATIVE, 1ST & COA. CHARGED THE BATTERIES.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,352 hrs · 24,102 cycles

OVERHEAD FWD CEILING EMERGENCY LIGHTS & GALLEY DOOR INOPERATIVE. CHARGED THE BATTERIES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,114 hrs · 23,926 cycles

ALL EMERGENCY EXIT LIGHTS INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 29,114 hrs · 23,926 cycles

FWD F/A FLASHLIGHT INDICATOR LIGHT INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 28,926 hrs · 23,768 cycles

SEVERAL EMERGENCY LIGHTS INOPERATIVE BATTERY DRAINED. CHARGED BATTERIES.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,899 hrs · 23,745 cycles

EMERGENCY EXIT SIGN FLOOR LEVEL 14F, ONE BULB INOPERATIVE. REPLACED, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,899 hrs · 23,745 cycles

EMERGENCY EXIT SIGN FLOOR LEVEL 14A, ONE BULB INOPERATIVE. REPLACED, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 28,513 hrs · 23,453 cycles

RIGHT FWD OVERWING EMERGENCY LIGHT INOPERATIVE.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 28,281 hrs · 23,262 cycles

FWD F/A FLASHLIGHT INOPERATIVE. REPLACED BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,953 hrs · 23,010 cycles

EXIT EMERGENCY LIGHT BY PASSENGER DOOR INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 27,736 hrs · 22,845 cycles

FWD F/A FLASHLIGHT INOPERATIVE, REPLACED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,579 hrs · 22,724 cycles

LT FWD OVERWING DOOR EXIT SIGN HAS ONE BULB INOPERATIVE.

Part: LIGHT — INOPERATIVE (ROW 15) · airframe 27,579 hrs · 22,724 cycles

ROW 15 EMERGENCY CEILING LIGHT INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 27,473 hrs · 22,638 cycles

ROW 13A EMERGENCY EXIT SIGN INOPERATIVE. CHARGED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 27,473 hrs · 22,638 cycles

ROW 13F EMERGENCY EXIT SIGN INOPERATIVE. CHARGED BATTERY PACK.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 27,459 hrs · 22,628 cycles

FWD F/A'S FLASHLIGHT INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,459 hrs · 22,628 cycles

ROW 13F EMERGENCY EXIT SIGN HAS ONE BULB INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,459 hrs · 22,628 cycles

ROW 13A EMERGENCY EXIT SIGN HAS ONE BULB INOPERATIVE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,350 hrs · 22,543 cycles

14DF EMERGENCY EXIT LIGHT 1 BULB BURNED OUT. PLACED ON MEL.

Part: SIGN — DETACHED (CABIN) · airframe 27,097 hrs · 22,334 cycles

EMERGENCY FLOOR FLOOD LIGHT 14C PANEL DETATCHED. SECURED THE EMERGENCY LIGHT PANEL.

Part: LIGHT — INOPERATIVE (ROW 9) · airframe 26,427 hrs · 21,843 cycles

ROW 9 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: SHUTOFF VALVE — LEAKING (BLEED SYS) · airframe 26,371 hrs · 21,801 cycles

RETURN TO FIELD, EMERGENCY DECLARED. LT BLEED DUCT WARNING. ISOLATED LEAK BY PLACING PRSOV BLEED ON MEL.

Part: LIGHT — INOPERATIVE (ROW 6) · airframe 26,274 hrs · 21,721 cycles

CEILING EMERGENCY FLOOD LIGHT, ROW 6 INOPERATIVE, PLACED ON MEL.

Part: CRADLE — INOPERATIVE (AFT FLASHLIGHT) · airframe 26,245 hrs · 21,699 cycles

AFT F/A FLASHLIGHT CONSIDERED INOPERATIVE DUE TO HOLDER INOPERATIVE, PLACED ON MEL.

Part: BATTERY PACK — INOPERATIVE (AFT FLASHLIGHT) · airframe 26,086 hrs · 21,580 cycles

AFT F/A FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY.

Part: LIGHT — INOPERATIVE (ROW 15) · airframe 26,010 hrs · 21,528 cycles

ROW 15 EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,884 hrs · 21,433 cycles

13DF FLOOR LEVEL EMERGENCY LIGHT HAS ONE BULB INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,884 hrs · 21,433 cycles

14DF FLOOR LEVEL EMERGENCY LIGHT HAS ONE BULB INOPERATIVE.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 25,767 hrs · 21,336 cycles

AFT CABIN EMERGENCY CEILING LIGHT INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,111 hrs · 20,841 cycles

ONE BULB FOR FLOOR EMERGENCY EXIT SIGN INOPERATIVE.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 25,008 hrs · 20,750 cycles

BS 280, FLOORBEAM HAS WIDESPREAD CORROSION.

Part: BULKHEAD WEB — CORRODED (BS 280) · corrosion level 2 · airframe 25,008 hrs · 20,750 cycles

FS 280 BULKHEAD WEBS HAVE WIDESPREAD CORROSION.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · corrosion level 2 · airframe 25,008 hrs · 20,750 cycles

RIGHT FLOOR SUPPORT FROM BS 280-319 HAS SEVERAL AREAS OF CORROSION.

Part: SKIN — CHAFED (ZONE 100) · airframe 25,008 hrs · 20,750 cycles

THREE CHAFES FOUND ON LOWER EXTERNAL SKIN ALONG STRINGER 27. AT BS 913 AND BETWEEN BS 913 AND 927.

Part: SKIN — CHAFED (ZONE 100) · airframe 25,008 hrs · 20,750 cycles

THREE CHAFES FOUND ON LOWER SKIN ALONG STRINGER 27 AT BS 913 AND BETWEEN BS 913 AND BS 927.

Part: BULB — UNSECURE (EMERGENCY LIGHT) · airframe 24,591 hrs · 20,391 cycles

LIGHT OUT AT SIDEWALL EXIT TIP ROW 13A-C. MAINTENANCE SECURED BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,505 hrs · 20,318 cycles

FOUND RT LOWER EMERGENCY LIGHT WITH ONE PEANUT BULB OUT. R & R PEANUT BULB, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,505 hrs · 20,318 cycles

FOUND FWD ENTRY LOWER EMERGENCY WITH ONE PEANUT BULB OUT. R & R PEANUT BULB, OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 24,049 hrs · 19,884 cycles

FWD F/A FLASHLIGHT INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,909 hrs · 19,756 cycles

ROW 13A OVERWING EXIT SIGN HAS ONE LAMP INOPERATIVE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,539 hrs · 19,420 cycles

EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY BATTERY PACKS.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,021 hrs · 23,432 cycles

OVERHEAD EMERGENCY LIGHTS DIM. CHARGED EPSU WITH AIRCRAFT POWER.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 23,412 hrs · 19,412 cycles

ROW 1 TO ROW 11, CEILING 5 EMERGENCY LIGHTS INOPERATIVE. ALLOWED ACFT ELECTRICAL POWER TO RECHARGE EPSU, OPS NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,615 hrs · 18,604 cycles

ROW 20, EMERGENCY FLOOD LIGHT BURNED OUT. MX REPLACED BULB.

Part: STRAP — DAMAGED (RT WING) · airframe 22,376 hrs · 18,374 cycles

RT WING STRAP, FOUND 18 DISCREPANT HOLES IN COLD WORKED AND NON COLDWORKED HOLES.

Part: BRAKE — INOPERATIVE (MLG) · airframe 22,263 hrs · 18,258 cycles

OTBD BRAKES INOPERATIVE. REPLACED NR 3 & 4 BRAKES.

Part: BATTERY PACK — DISCHARGED (MEGAPHONE) · airframe 22,019 hrs · 18,026 cycles

AFT F/A MICROPHONE INOPERATIVE. MX REPLACED THE MEGAPHONE BATTERY PACK.

Part: PIN — DEFECTIVE (EMERGENCY LIGHT) · airframe 21,706 hrs · 17,727 cycles

RIGHT OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED GROUND WIRE PIN.

Part: BATTERY PACK — MISINSTALLED (CABIN) · airframe 21,501 hrs · 17,531 cycles

ROW 13 LT AND RT EMERGENCY SIGNS INOP. CORRECTLY INSTALLED NR 5 BATTERY PACK.

Part: SWITCH — DEFECTIVE (CABIN DOOR) · airframe 20,759 hrs · 16,834 cycles

MAIN CABIN DOOR WILL NOT OPEN (DUE PAX DOOR MOTOR RETRACTING DOOR). R2 SWITCH OPS NORMAL

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 20,716 hrs · 16,798 cycles

COCKPIT FLASHLIGHT INOP. REPLACED BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,648 hrs · 16,750 cycles

FLOOR LEVEL EMERGENCY EXIT SIGN AT ROW 14 INOPERATIVE UPON POST FLIGHT INSPECTION. MAINTENANCE REPLACED THE LAMPS.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 20,529 hrs · 16,630 cycles

AFT FLIGHT ATTENDANT'S FLASHLIGHT INOPERATIVE ON POST FLIGHT INSPECTION. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY PACK.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 20,279 hrs · 16,368 cycles

RTF LEFT BLEED DUCT WARNING. RESET AILC RAN ENGINES OPERATED BLEEDS, OPS CHECKED.

Part: CONNECTOR — LOOSE (ANTI-SKID SYS) · airframe 20,268 hrs · 16,356 cycles

ABORTED TAKEOFF FOR ANTI INBOARD SKID CAUTION MESSAGE / INDICATION ON EICAS. MAINTENANCE FOUND AND SECURED A LOOSE CONNECTION AT THE LEFT INBOARD WHEEL SPEED TRANSDUCER.

Part: DUCT — UNKNOWN (BLEED SYSTETM) · airframe 20,053 hrs · 16,157 cycles

AIR RETURN, EMERGENCY DECLARED, LEFT BLEED AIR DUCT WARNING. BLEEDS SHUTDOWN. MAINTENANCE REMOVED AND REPLACED 10TH STAGE CROSSOVER DUCT AND LEFT PACK BELLOWS.

Part: DOOR — BINDING (SERVICE) · airframe 19,708 hrs · 15,831 cycles

RIGHT FORWARD SERVICE DOOR HARD TO OPEN AND CLOSE. CLEANED AND LUBED DOOR.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,661 hrs · 15,787 cycles

SERVICE DOOR EMERGENCY EXIT SIGN HAD 1 BULB INOPERATIVE ON POST FLIGHT INSPECTION. THE BULB WAS PLACED ON MEL.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 19,491 hrs · 15,635 cycles

FLIGHT 2641, REPORTED AN INOPERATIVE FLASHLIGHT ON PRE FLIGHT INSPECTION. REMOVED AND REPLACED BATTERY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,334 hrs · 15,493 cycles

FLIGHT 2664, REPORTED ROW 19 EMERGENCY CEILING FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LAMP IN THE LIGHT ASSEMBLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,334 hrs · 15,493 cycles

FLIGHT 2664, REPORTED THREE EMERGENCY EXIT SIGN LAMPS AT THE SERVICE DOOR & EMERGENCY EXIT INOPERATIVE ON POST FLIGHT INSPECTION. MAINTENANCE REPLACED THE LAMPS IN THE SIGN ASSEMBLY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,194 hrs · 15,367 cycles

F/O FLASHLIGHT INOPERATIVE DUE TO INCORRECT INSTALLATION. R2 BATTERY.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 19,080 hrs · 15,260 cycles

F/O FLASHLIGHT INOP. R2 F/O FLASHLIGHT, OPS CHECK GOOD.

Part: SPAR — GOUGED (RT WING) · airframe 19,060 hrs · 15,241 cycles

RT WING AT WS 158.00 HAS GOUGE FROM TOOLING ON FWD FACE MEASURES .085"L X .085"W X .035" DEEP. REPAIRED AREA IN ACCORDANCE WITH BOMBARDIER REO 690-57-21-038.

Part: FITTING — WORN (HORIZ STAB) · airframe 19,060 hrs · 15,241 cycles

FS 280.00 THE HORIZONTAL STABILIZER PIVOT FITTING ANIT ROTATION TABS ARE WORN. BLENDED THE ANTI ROTATION TABS SMOOTH IAW RO CRJ9-55-0153, CRJP-55-0153 AND REO 690-55-11-038.

Part: DOUBLER — DEFECTIVE (FUSELAGE) · airframe 19,060 hrs · 15,241 cycles

FS 797 REINFORCING DOUBLER P/N KSH670-35824-21 FASTENER HOLE HAS NO EDGE DISTANCE DUE TO SHORT DIMENSION OF PART ISSUED. REPAIRED DOUBLER IAW BOMBARDIER REO CL600-25-L00969.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 19,060 hrs · 15,241 cycles

FS 1098.20 AFT SIDE OF PRESSURE BULKHEAD SUPPORT STRUCTURE JUST LEFT OF THE FLOATATION VALVE IS CHAFED APPROX 0.050" DEEP FROM FLOATATION VALVE HINGE PIN. REPAIRED SUPPORT STRUCTURE AND FLOATATION VALVE HINGE PIN IAW BOMBARDIER REO 690-53-61-245 AND BOMBARDIER REO 690-53-61-249.

Part: CROSSBEAM — CORRODED (FS 280) · airframe 19,060 hrs · 15,241 cycles

FS 280.00 CROSSBEAM HAS MINOR CORROSION ON TOP OF BEAM AT LBL 9. REMOVED CORROSION IAW EO CL600-2D24-53-L00952.

Part: STRIKER — DENTED (PAX DOOR) · airframe 19,060 hrs · 15,241 cycles

PAX DOOR AFT SEAL STRIKER IS DENTED AT FS 349 UPPER SECTION. REPAIRED STRIKER IAW REO 670-53-22-001. REPAIR TYPE 1.

Part: CROSSBEAM — CORRODED (FS 280) · airframe 19,060 hrs · 15,241 cycles

FS 280.00 BULKHEAD WEB HAS CORROSION OUT OF LIMITS AT RBL 10 AND RBL 20 WL 73. REMOVED AND REPLACED CROSSBEAM AND WEB IAW SRM 51-42-13-001-001, 51-42-06-001-001, 51-42-21-001-001.

Part: SKIN — DENTED (HORIZ STAB) · airframe 19,060 hrs · 15,241 cycles

HORIZONTAL STABILIZER SKIN AND RT ELEVATOR LOWER SKIN DAMAGED AT HINGE 3 OF RT ELEVATOR BY TOOLING. REPAIRED ELEVATOR LOWER FORWARD SKIN AND HORIZONTAL STAB LOWER TRAILING SKIN IN ACCORDANCE WITH ENGINEERING ORDER CL600-2D24-55-L00997.

Part: SEAT TRACK — CORRODED (BS 477.4-693) · airframe 19,060 hrs · 15,241 cycles

SEAT TRACK AT FS 477.40 TO 693.00, LBL 9.0 HAS AREAS OF LIGHT CORROSION. REMOVED CORROSION FROM CABIN FLOOR SEAT TRACK IAW REO 670-53-00-013 REV E.

Part: SEAL — BROKEN (EMERG MED KIT) · airframe 18,817 hrs · 15,004 cycles

EMK SEAL BROKEN. INSPECTED & RE-SEALED.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 18,794 hrs · 14,984 cycles

FWD F/A FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED BATTERIES.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 18,794 hrs · 240,805 cycles

FWD CABIN FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED BATTERIES

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,802 hrs · 14,990 cycles

FWD CABIN FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES. OPS CHECK IS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,748 hrs · 14,949 cycles

NR 6 CEILING EMERGENCY FLOOD LIGHT INOP. R2 LAMP IN NR 6 CEILING EMERGENCY FLOOD LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,759 hrs · 14,960 cycles

NR 6 CEILING EMERGENCY FLOOD LIGHT INOP. REPLACED LAMP IN NR 6 CEILING EMERGENCY FLOOD LIGHT.

Part: DOOR — OUT OF ADJUST (SERVICE DOOR) · airframe 18,706 hrs · 14,912 cycles

UNABLE TO CLOSE FWD SERVICE DOOR. ADJUSTED DOOR.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

AFT CENTER FUSELAGE SUSTAINED 2 OUT OF LIMITS DENTS AT FS 897-7-FS 969.00 BETWEEN STR 4L-STR 7L. C/W RO CRJ9-53-0772.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 18,680 hrs · 14,891 cycles

HORIZONTAL STABLIZER WAS REMOVED TO FACILITATE MAINTENANCE WHILE BEING SUPPORTED ONE OF THE SAWHORSES BEING USED HAD PROTRUDING HARDWARE WHICH CAUSED DAMAGE TO LEADING EDGE. C/W RO CRJ9-55-0144.

Part: SKIN — DENTED (HORIZ STAB) · airframe 18,680 hrs · 14,891 cycles

UPPER RT HORIZONTAL STAB WAS FOUND TO HAVE MULTIPLE DENTS DUE TO HAIL STORM. C/W RO CRJ9-55-0140.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

AIRCRAFT HAD MULITPLE OUT OF LIMITS DENTS ON AFT CROWN OF THE FUSELAGE BETWEEN FS 977-FS 1162, STR 7L-STR 7R DUE TO HAIL STORM. C/W REO690-53-61-206.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

SINGLE OUT OF LIMIT DENT LOCATED ON FORWARD LT FUSELAGE AT FS 235.00 BETWEEN STR 12L-STR 13L, OUT OF LIMITS DUE TO HAIL DAMAGE. C/W RO CRJ9-53-0813.

Part: STRUCTURE — DENTED (LE SLAT) · airframe 18,680 hrs · 14,891 cycles

FIVE DENTS LOCATED ON RT WING L/E SLAT BETWEEN SS58-75-SS92.00 OUT OF LIMITS. C/W RO CRJ9-57-0344.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

DENT LOCATED AT FS 1000-1015 BETWEEN STR 7L-8L OUT OF LIMITS. C/W RO CRJ9-53-0780.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

SINGLE OUT OF LIMIT DENT LOCATED ON AFT LT FUSELAGE CENTER UPPER SKIN AT FS 942.00-FS 969.00 BETWEEN STR 0-3R. C/W RO CRJ9-53-0781.

Part: SKIN — DENTED (HORIZ STAB) · airframe 18,680 hrs · 14,891 cycles

LT UPPER HORIZONTAL STABLIZER WAS FOUND TO HAVE MULTIPLE OUT OF LIMITS DENTS DUE TO HAIL STORM. C/W RO CRJ9-55-0141.

Part: SLAT — DENTED (RT WING) · airframe 18,680 hrs · 14,891 cycles

ONE OUT OF LIMIT DENT ON NR 2 RHS. PERMANENT REPAIR FOR 1 OFF DENT ON NR 2 RHS BETWEEN SS315.75 &TRACK 2-3. C/W RO CRJ9-57-0330, TASK MRO 18134.

Part: SLAT — DENTED (LT WING) · airframe 18,680 hrs · 14,891 cycles

ONE OUT OF LIMIT DENT ON NR 3 LHS. PERMANENT REPAIR FOR 1 OFF DENT ON NR 3 LHS SLAT BETWEEN SS339.00 &TRACK 3-2. C/W RO CRJ9-57-0329, TASK MRO 18140.

Part: SKIN — DEFECTIVE (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

FOUR REDUNDANT HOLES FOUND IN REPLACEMENT SKIN PANEL P/N SH670-330013-13 LOCATED AT FS 506.125 BETWEEN STR 5L-6L(2) AND STR 5R-6R(2). C/W RO CRJ9-53-0830, TASK MRO 18396.

Part: SLAT — DENTED (LT WING) · airframe 18,680 hrs · 14,891 cycles

ONE OUT OF LIMIT DENT ON NR 1 LHS. PERMANENT REPAIR FOR 1 OFF DENT ON NR 1 LHS SLAT BETWEEN SS82.00 & SS92.20. C/W RO CRJ9-57-0328, TASK MRO 18142.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

MULTIPLE DENTS DRILLED HOLES ON STR 1R BETWEEN FS 453-FS 469. C/W RO CRJ9-53-0833, TASK MRO 18406.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

ONE DAMAGE HOLE IN UPPER FRAME SECTION AT FS 409.00 AND ANGLE VHF ANTENNA, RT LOWER HOLE. DISCREPANT HOLE OPENED TO.216 C/W RO CRJ9-53-0811, TASK MRO 18321.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

MULTIPLE DOUBLE DRILLED HOLES IN STR 1R BETWEEN FS 333-FS 477. C/W RO CRJ9-53-0832, TASK MRO 18406.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

MULTIPLE DENTS LOCATED AT FS 295.00-331.00 STR 05RT. C/W RO CRJ9-53-0812, TASK MRO 18322.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

MULTIPLE DENTS FOUND ON LT FUSELAGE SKIN. C/W RO 690-53-00-182.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

FOUND DAMAGE TO FUSELAGE SKIN AT FS 410 TO FS 418 BETWEEN STRINGERS 9L AND 13. C/W RO 690-53-21-292.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

DENT AT FS 236 FOUND TO BE OUT OF LIMITS. C/W RO CRJ9-53-0776.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

FOUND DAMAGE TO FUSELAGE FWD BARREL SIDE SKIN AT FS 501 STRINGER 12L AND FS 661+74 STRINGER 13L. C/W MESA RO 690-53-31-104.

Part: SKIN PANEL — DAMAGED (EMERGENCY EXIT) · airframe 18,680 hrs · 14,891 cycles

DAMAGE FOUND TO LT EMERGENCY EXIT DOOR SKIN PANEL. C/W RO 690-52-21-008.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

TWO (2) DENTS ON LT APRON SKIN BETWEEN FS 801.25 AND FS 830.40. C/W RO 690-53-42-003.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

DENTS AT CENTER FUSELAGE UPPER SKIN AT FS 942- FS 969, STINGER 0-3R. DAMAGE CAUSED BY WEATHER EVENT WHILE A/C WAS AT JETWAY REO 690-53-51-049 REV B. C/W RO CRJ9-53-0781.

Part: SKIN PANEL — DAMAGED (GALLEY DOOR) · airframe 18,680 hrs · 14,891 cycles

SPLICE REPAIR TO GALLEY DOOR OUTBOARD SKIN PANEL. C/W RO CRJ9-52-0460.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

FOUND DAMAGE TO FRAME OUTER FLANGE AT FS 409 STRINGERS 2 TO 3, LT. C/W RO 690-53-21-285.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

FOUND DAMAGE TO CENTER FUSELAGE RT SKIN BETWEEN FS 708 AND FS 720.85 AT STRINGER 10R. C/W RO 690-53-41-031.

Part: SKIN — DENTED (HORIZ STAB) · airframe 18,680 hrs · 14,891 cycles

FOUR DENTS ON RT HORIZONTAL STAB LEADING EDGE. C/W RO 690-55-12-061.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,680 hrs · 14,891 cycles

FOUND DAMAGE TO FUSELAGE SKIN AT FS 196.25 BETWEEN STRINGERS 14L AND 16L IN RVSM AREA. C/W MESA RO# 690-53-11-339.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,575 hrs · 14,809 cycles

OVERHEAD EMERGENCY LIGHT ROW 20 INOP. RELAMPED EMERGENCY LIGHT.

Part: HANDLE — UNSECURE (DOOR) · airframe 18,554 hrs · 14,791 cycles

PROX SYS FAULT 2. FOUND DOOR HANDLE INCORRECTLY STOWED, RESTOWED HANDLE.

Part: WARNING SYSTEM — FALSE ACTIVATION (DOOR) · airframe 18,461 hrs · 14,705 cycles

PROX SYS 2 FAULT. CYCLED DOOR.

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 18,444 hrs · 14,695 cycles

OBS O2 MASK BROKEN. O2 MASK PN:MC10-35-101 IN STOCK ALL STATIONS RONS IN CLT 7/18.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 18,425 hrs · 14,681 cycles

UNCOMMANDED SPD BUG CHANGE WITH AUTO PILOT ON CLIMB. PLACED ON MEL. RERACKED FCC 1 AND 2

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,412 hrs · 14,669 cycles

FWD ENTRY FWD UPPER EMERGENCY LIGHT HAS 1 BULB OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,233 hrs · 14,518 cycles

SERVICE DOOR AFT EMERGENCY LIGHT BULB OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,128 hrs · 14,421 cycles

THE 16A SIDE EMERGENCY LIGHT ASSY- 1 BULB OUT. RELAMPED 16A SIDEWALL EXIT SIGN.

Part: CABLE — FRAYED (PAX DOOR) · airframe 18,122 hrs · 14,416 cycles

PAX DOOR ASSIST CABLE FRAYED. R2 CABLE.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 18,116 hrs · 14,409 cycles

LT ENG BLEED CAUTION AFTER TO. ENG BLEEDS OPS NORMAL NFAR.

Part: COVER — MISSING (CABIN) · airframe 18,110 hrs · 14,402 cycles

EMERGENCY LIGHT COVER AT GALLEY DOOR MISSING. INSTALLED REPLACEMENT COVER.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 18,057 hrs · 14,354 cycles

FLOOR LEVEL EXIT SIGN AT ROW 16F 1 BULB. R2 BULB.

Part: ENGINE — VIBRATION (NR 1) · airframe 18,032 hrs · 14,327 cycles

ENG 1 N1 VIBE AT 2.0 IN CRUISE. SHOOK BLADES, ENG RUN AT .4MILS.

Part: SENSOR — MALFUNCTIONED (NR 3 BRAKE TEMP) · airframe 17,963 hrs · 14,268 cycles

INTERMIT BRAKE OVERHEAT WARNING NR 3. R&R NR 3 BRAKE TEMP SENSOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,934 hrs · 14,242 cycles

NR 8 CEILING EMER FLOOD LIGHT OUT. R2 BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,934 hrs · 14,242 cycles

NR 5 CEILING FLOOD LIGHT OUT. R2 BULB.

Part: PITOT TUBE — DENTED (NR 1) · airframe 17,431 hrs · 13,787 cycles

NR 1 PITOT TUBE INLET DENTED. MX REMOVED AND REPLACED NR 1 PITOT TUBE ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,400 hrs · 13,760 cycles

ROW 4 CEILING LEVEL [EMERGENCY] FLOOD LIGHT INOP. MX RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,400 hrs · 13,760 cycles

ROW 20 CEILING LEVEL [EMERGENCY] FLOOD LIGHT INOP. MX RELAMPED.

Part: RELEASE PIN — BROKEN (CABIN DOOR) · airframe 17,266 hrs · 13,646 cycles

PAX DOOR HANDRAIL PIN LANYARD BROKEN. MX REMOVED AND REPLACED PAX DOOR HANDRAIL PIN/LANYARD ASSY.

Part: FLAP — DENTED (RIGHT) · airframe 17,212 hrs · 13,597 cycles

RIGHT I/B FLAP DENT. MAINTENANCE R2 I/B FLAP C/W ELECTRICAL & MECHANICAL RIG OPS CHECKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,176 hrs · 13,571 cycles

CABIN CEILING EMERGENCY LIGHT ROW 23 INOP. MX RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,176 hrs · 13,571 cycles

CABIN CEILING EMERGENCY LIGHT ROW 7 INOP. MX RELAMPED EMERGENCY LIGHT.

Part: SENSOR — FAULTY (MLG) · airframe 17,084 hrs · 13,490 cycles

NR 3 BTMS BRAKE OVERHEAT WARNING IN FLIGHT. MX REPLACED SENSOR.

Part: WARNING SYSTEM — MALFUNCTIONED (PAX DOOR) · airframe 17,002 hrs · 13,424 cycles

PROX SYS FAULT 2 STATUS MSG-PAX DOOR. MX CYCLED PAX DOOR, FAULT CLEARED, NFAR.

Part: SPRING — BROKEN (HAND RAIL) · airframe 16,875 hrs · 13,323 cycles

MAIN ENTRY DOOR FWD HAND RAIL BUMPER SPRING BROKEN. MX REPLACED WITH NEW BUMPER SPRING AND HARDWARE.

Part: PLACARD — MISSING (CABIN) · airframe 16,756 hrs · 13,211 cycles

"TO OPEN" PLACARD MISSING FROM MED STAIRS. MX INSTALLED NEW "TO OPEN" PLACARD ON MAIN ENTRY DOOR STAIRS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,667 hrs · 13,141 cycles

NR 4 OVERHEAD EMERGENCY LIGHT INOP. MX RELAMPED.

Part: BLEED VALVE — LEAKING (NR 2 ENGINE) · airframe 16,487 hrs · 12,981 cycles

RIGHT ENGINE FLUID LEAK. MX REPLACED THE OBV.

Part: MOTOR — MALFUNCTIONED (CABIN DOOR) · airframe 16,350 hrs · 12,865 cycles

PAX DOOR ASSIST CABLE BROKEN. MX R2 PAX DOOR ASSIST MOTOR & FWD GAS STRUT OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,302 hrs · 12,824 cycles

2 NON SEQUENTIAL O/H FLOOD LIGHTS INOP. MX RELAMPED.

Part: PLACARD — MISSING (CABIN) · airframe 16,256 hrs · 12,787 cycles

MAIN PAX DOOR EXIT MISSING PLACARD. MX R2 PLACARD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 16,065 hrs · 12,635 cycles

FWD ATT FLASHLIGHT INDICATOR INOP. MX R2 BATTERY.

Part: SEAL — DIRTY (PAX DOOR) · airframe 15,852 hrs · 12,446 cycles

PAX DOOR SQUEALING. INSPECTED AND CLEANED LUBE SEAL.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 15,769 hrs · 12,373 cycles

CAPTAIN'S FLASHLIGHT INOP. REPLACED BATTERY.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 15,697 hrs · 12,312 cycles

F/O'S FLASHLIGHT INOP. MX REPLACED F/O'S FLASHLIGHT AMM 25-61-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,631 hrs · 12,253 cycles

ROW 20 OVERHEAD EMERGENCY FLOOD INOP. MX RELAMPED.

Part: ESCAPE HATCH — LACK OF LUBE · airframe 15,442 hrs · 12,084 cycles

ESCAPE HATCH WHISTLING AT ALTITUDE. LUBED HATCH

Part: LENS — WRONG PART (CABIN) · airframe 15,413 hrs · 12,062 cycles

OVERHEAD EXIT ROW LIGHT WRONG COLOR FWD. REPLACED RED LENS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,353 hrs · 12,004 cycles

EMERGENCY LIGHTS INOP. CHARGED EMERGENCY BATTERIES, LIGHTS OP GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,146 hrs · 11,832 cycles

ROW 17 EMERGENCY FLOOD LIGHT OUT. MX REPLACED ROW 17 EMERGENCY FLOOD LIGHT BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,053 hrs · 11,761 cycles

ROW 15 FLOOR LEVEL EXIT SIGN HAS 1 BULB OUT. RELAMPED EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,896 hrs · 11,614 cycles

ROW 7 EMERGENCY FLOOD LIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,834 hrs · 11,551 cycles

THIRD AISLE EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: TIRE — SEPARATED (NLG) · airframe 14,782 hrs · 11,512 cycles

RIGHT NLG TIRE TREAD SEPARATED. REMOVED AND REPLACED BOTH NLG WHEELS.

Part: POWER SUPPLY — LOOSE (CABIN) · airframe 13,057 hrs · 10,072 cycles

ASH FLT 2838 PHX - BUR - AFT 3 EMERGENCY LIGHTS IN THE AFT ON THE CEILING INOP. MAINTENANCE SECURED POWER SUPPLY UNIT.

Part: LAMP — INOPERATIVE (CABIN LIGHTS)

FLT 2719 - AFT CEILING LIGHT INOPERATIVE. MX RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

CREW REPORTED EMERGENCY EXIT LIGHT AT 16A AND AN EMERGENCY EXIT LIGHT AT ROW 7 INOPERATIVE. MX RELAMPED. (K)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ASH FLT 2679 CLT-SAT. EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. (S)

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS)

ASH FLT 2934 FAT-PHX. SERVICE DOOR EXIT LIGHT INOP. MX CLEANED CONNECTORS--LIGHT OPS GOOD. (B)

Part: STRUCTURE — CRACKED (RT MLG DOOR) · airframe 10,856 hrs · 8,339 cycles

FOUND RT MLG DOOR CROSS MEMBER CRACKED AND SEVERAL LOOSE RIVETS ON INNER SKIN LEADING EDGE NEXT TO FWD HINGE. REPLACED MLG DOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,527 hrs · 8,097 cycles

ASH FLT 2653 CLT-PNS. ROW 17 CEILING EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: WARNING MESSAGE — ILLUMINATED · airframe 9,673 hrs · 7,395 cycles

ASH FLT 2665 - INBOUND TO CLT, PITCH FEEL CAUTION MESSAGE. MX PERFORMED AN S-POST TEST, FAULTS CLEARED. NO DEFECTS NOTED.

Part: A/C PACK — SMOKE (RIGHT) · airframe 8,686 hrs · 6,581 cycles

ASH 2615 CLT - CAPTAIN REPORTED SMOKE IN THE CABIN. MX PLACED THE RT PACK ON MEL.

Part: STRIP — LOOSE (CABIN) · airframe 7,536 hrs · 5,638 cycles

ASH 2602 CLT. EMERGENCY FLOOR STRIP ROW 16 NOT SECURE. MX SECURED STRIP.

Part: GARLOCK SEAL — LEAKING (NR 1 ENGINE) · airframe 7,530 hrs · 5,631 cycles

ASH 9390 BWI - THE A/C DIVERTED TO IAD DUE TO THE NR 1 ENGINE OIL LOW. ENGINE SHUT DOWN DURING FLIGHT. MX REMOVED AND REPLACED EDP GARLOCK SEAL O-RING.

Part: UNKNOWN — UNKNOWN (SPOILERS) · airframe 7,050 hrs · 5,228 cycles

ASH 2664 CLT - SPOILER/STAB FAULT. PERFORMED SPOST W/FLIGHT CREW. NO FURTHER DEFECTS NOTED.

Part: SKIN — CORRODED (RT WING) · airframe 6,985 hrs · 5,179 cycles

CORROSION DAMAGE (3 OFF AREAS), 0.026 INCH MAX DEPTH TO RT WING LOWER PLANK FUEL TANK ACCESS PANEL AT LOWER PANEL LOCATION 541AB. THE DAMAGE MEASURE 1/10" WIDE IN FWD AND AFT DAMAGED AREAS. REPAIRED DAMAGE.

Part: COMPUTER — FAULTY (STALL WARNING) · airframe 6,719 hrs · 4,965 cycles

ASH 2662 CLT. PITCH FEEL FAULT/SSCU 2 FAULT STATUS. MX REMOVED AND REPLACED STALL PROTECTION COMPUTER. NO FURTHER DEFECTS NOTED.

Part: PCU — MALFUNCTIONED (SPOILER SYS) · airframe 6,715 hrs · 4,963 cycles

ASH 2833 OAK. CAPTAIN REPORTED A I/B SPOILERON AND I/B FLT SPOILER CAUTION MESSAGE IN FLIGHT. MX REMOVED AND REPLACED RIGHT INBOARD MFSPCU.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER SYS) · airframe 6,703 hrs · 4,952 cycles

ASH 2946 SEA. INBOARD FLT SPLR AND INBOARD SPLRON CAUTION MESSAGES. RESET SSCU'S OPS GOOD.

Part: CAUTION MESSAGE — ILLUMINATED · airframe 6,628 hrs · 4,896 cycles

ASH 2661 CLT. PILOT REPORTED INBOARD FLIGHT SPOILERS AND INBOARD SPOILERON CAUTION MSG. MX PERFORMED SPOST.

Part: CAUTION MESSAGE — ILLUMINATED · airframe 6,628 hrs · 4,896 cycles

ASH 2661 CLT. INBOARDD FLT SPOILERS AND INBOARD FLT SPOILERON CAUTION MESSAGE. MX RESET THE SYSTEM.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILERON SYS) · airframe 6,446 hrs · 4,746 cycles

ASH 2626 CLT. INBOARD FLIGHT SPOILERONS CAUTION MESSAGE. MX RESET THE SYSTEM.

Part: SPOILER SYS — MALFUNCTIONED · airframe 6,317 hrs · 4,637 cycles

ASH 5039 CLT - GLD NOT ARMED CAUTION ON FINAL. MX PERFORMED OPERATIONAL CHECKS OF SPOILER SYSTEM. NO DEFECTS NOTED.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 6,275 hrs · 4,602 cycles

ASH 5081 ALB - INBD RT SPOILERS AND INBD FLIGHT SPOILERS CAUTION MSG. MX RESET.

Part: SENSOR — FAULTY (L/E SLAT) · airframe 6,124 hrs · 4,481 cycles

ASH 5080 CLT. SLAT FAULT STATUS MESSAGE. MX PLACED THE SYSTEM ON MEL MX R2 LT INBD DISCONNECT SENSOR AND SWAPPED SFECU'S. OP'S CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (L/E SLAT SYS) · airframe 6,618 hrs · 4,476 cycles

ASH 5087 DTW - SLATS FAULT STATUS MSG. MAINTENANCE COULD NOT DUPLICATE.

Part: WIRE — DAMAGED (L/E SLAT) · airframe 6,077 hrs · 4,445 cycles

ASH 6309 PHX - SLAT FAULT STATUS MESSAGE. MX PLACED SYSTEM ON DEFERRAL. MX REPAIRED WIRE.

Part: ADC — MALFUNCTIONED (NR 1) · airframe 5,582 hrs · 4,071 cycles

ASH 5053 CLT - EICAS DISPLAYED SPOILER/STAB FAULT. RUDDER LIMIT FAULT. LT AND RT FADEC FAULT. AIRSPEED, ALTITUDE AND VERTICAL SPEED WARNING. MX RE-RACKED THE NR 1 ADC AND FAULTS CLEARED. SYSTEMS OP CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — MALFUNCTIONED (SLATS) · airframe 5,574 hrs · 4,063 cycles

ASH 5084 CLT. SLAT FAULT STATUS MESSAGE INTERMITTENT IN FLIGHT. MAINTENANCE REMOVED AND REPLACED RT SLAT DISCONNECT SENSOR.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 5,543 hrs · 4,035 cycles

ASH 5098 CLT - FLAPS 1/2 SPEED. MX CLEARED SFECU1 INHIBITS. NO FURTHER ACTION REQUIRED.

Part: STATUS MESSAGE — ILLUMINATED · airframe 5,496 hrs · 4,001 cycles

ASH 6090 PHX. SFECU 2 STATUS MSG. MX C/W SPOST TEST. OP'S CHECK GOOD, ACFT CONTINUED OPERATIONS.

Part: BONDING STRAP — BROKEN · airframe 5,437 hrs · 3,955 cycles

LEFT INBOARD SPOILER BONDING STRAP BROKEN. MAINTENANCE REMOVED AND REPLACED BONDING STRAP.

Part: ACTUATOR — WARNING MESSAGE · airframe 5,037 hrs · 3,634 cycles

ASH 6154 PHX - PITCH FEEL CAUTION MESSAGE. MX R&R PITCH FEEL ACTUATOR NR 2.

Part: UNKNOWN — UNKNOWN · airframe 5,024 hrs · 3,625 cycles

ASH 6428 PHX - PITCH FEEL CAUTION MESSAGE. MX PERFORMED THE SPOST RESET PROCEDURE. OP'S CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 4,994 hrs · 3,599 cycles

AFT INTERIOR AND EXTERIOR LIGHTS FLASHING. MX REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 4,882 hrs · 3,501 cycles

ASH 6336 MEM - SSCU1 FAIL. PERFORMED SPOST1 W/FLIGHT CREW. NO FURTHER DEFECTS NOTED.

Part: LIMITER — FAULTED (RUDDER) · airframe 4,882 hrs · 3,501 cycles

ASH 5085 GSO, RUDDER LIMIT FAULT. MAINTENANCE PERFORMED SPOST. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 4,790 hrs · 3,421 cycles

ASH 6530 PHX - RT REAR EMER LIGHTS FLICKERING. MX CND.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 4,722 hrs · 3,367 cycles

ASH 6263 PHX - PILOT REPORTED NWS INOP ON LANDING. STOPPED ON TAXI-WAY AND COULD NOT RESET PER THE CFM. HAD GROUND TOW TO GATE. CONTRACT MAINTENANCE RESET THE NWS. OPERATIONAL CHECK NORMAL.

Part: SEAL — BROKEN · airframe 4,726 hrs · 3,363 cycles

ASH 6090 PHX - AFT EEMK SEAL WAS BROKEN. MAINTENANCE INVENTORIED AND RESEALED THE EEMK.

Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 4,726 hrs · 3,363 cycles

MEGAPHONE WAS INOP. MAINTENANCE REPLACED THE BATTERY AND OPS CHECKED GOOD.

Part: APU — UNKNOWN (APU BAY) · airframe 4,277 hrs · 3,027 cycles

ASH 2642 CLT - FIRE/SMOKE IN FWD LAV. MAINTENANCE REMOVED AND REPLACED APU.

Part: APU — OVERSERVICED (APU) · airframe 4,166 hrs · 2,947 cycles

ASH 6093 PHX, STRONG ODOR IN CABIN WITH PACKS RUNNING. DRAINED AND SERVICED APU OIL TO PROPER LEVEL. PERFORMED SYSTEMS OPERATIONAL CHECKS WITH NO DEFECTS NOTED.

Part: PLUG — MISSING (ENGINE) · airframe 3,822 hrs · 2,702 cycles

ASH 6085 MEM - E1 ROLL BACK TO IDLE DURING FLIGHT. ENGINE RECOVERED ITSELF AFTER A FEW MINUTES AND CONTINUED TO PHX NORMALLY. FOUND BOROSCOPE PLUG MISSING INSTALLED AND PERFORMED POWER RUNS OPS CHK GOOD.

Part: CIRCUIT BOARD — FAILED (EMERGENCY LIGHT) · airframe 3,331 hrs · 2,355 cycles

ASH 6213 PHX. EMERGENCY LIGHT SYSTEM TO BE CYCLING ON AND OFF WHEN IN THE ARMED POSITION. MX REMOVED AND REPLACED THE NR 5 PRINTED CIRCUIT CARD AT J11 AND THE SYSTEM FUNCTIONED NORMALLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 1,305 hrs · 983 cycles

THE PRIOR CREW LEFT THE EMERGENCY LIGHTS ON. MAINTENANCE REPLACED THE BATTERY PACKS. OPS CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED (EMERGENCY DOOR) · airframe 299 hrs · 247 cycles

ASH 6410 PHX-COS. THE CREW REPORTED A LEFT EMERGENCY DOOR CAUTION MESSAGE. THE DOOR WAS CHECKED FOR SECURITY WITH NO DEFECTS NOTED AND THE INDICATION SYSTEM WAS DEFERRED. RESECURED TARGET. OPS CHECK GOOD, NO PARTS USED.

Part: DOOR — DAMAGED (EMERGENCY EXIT) · airframe 96 hrs · 89 cycles

ASH 6433 PHX. CREW REPORTED THE LT FWD EMERGENCY EXIT MESSAGE ON THE ECIAS SCREEN. MX REMOVED AND INSTALLED THE DOOR OPS GOOD. NO PARTS USED.