N935LR

Part: NONE — NONE · airframe 37,493 hrs · 30,364 cycles

PAX DOOR EXIT SIGN HAS 3 BULBS INOP. REPLACED BULBS.

Part: NONE — NONE · airframe 37,391 hrs · 30,324 cycles

EMER LIGHTS INOP. MX ALLOWED EMER LIGHT BATTERY PACKS TO CHARGE - OP GOOD.

Part: BULB — INOPERATIVE (FLOOD LIGHT) · airframe 37,231 hrs · 30,213 cycles

ROW 18 EMER FLOODLIGHT INOP. REPLACED BULB

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,718 hrs · 29,816 cycles

OH FLOOD LIGHT ROW 15 INOP PLACED ON MEL

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,578 hrs · 29,718 cycles

CEILNG LEVEL EMER FLOODLIGHT ROW 18 INOP. RELAMPED.

Part: LAMP — INOPERATIVE (EXIT SIGN) · airframe 36,218 hrs · 29,416 cycles

SERVICE DOOR EXIT SIGN UPPER BULB INOP. RELAMPED.

Part: INTERCOSTAL — CORRODED (BS 364 S27L) · airframe 36,204 hrs · 29,453 cycles

INTERCOSTAL AT FRAME 364.00 AND STRINGER 27L CORRODED. CORRECTIVE ACTION: REPLACED INTERCOSTAL AT FRAME 364.00 AND STRINGER 27L IAW CRJ 900 SRM 51-42-06. FOR DETAILS SEE AVMAX WORKF ORDER 80909 WORK CARD 1161.

Part: SKIN — CHAFED (RT AILERON) · airframe 36,204 hrs · 29 cycles

RH AILERON CHAFED ON LEADING EDGE. CORRECTIVE ACTION: REMOVED AND REPLACED RH AILERON LEADING EDGE SKIN IAW CRJ 900 SRM 51-42-21. FOR DETAILS SEE AVMAX WORK ORDER 80909 WORK CARD 6070

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,204 hrs · 29,453 cycles

STRINGER 25R CORRODED BETWEEN F.S. 319.00 AND F.S. 349.00. CORRECTIVE ACTION: REPLACED STRINGER 25R FROM F.S. 319.00 TO F.S. 349.00 IAW CRJ 900 SRM 51-42-06. FOR DETAILS SEE AVMAX WORK ORDER 80909 WORK CARD 1158.

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 36,204 hrs · 29,453 cycles

VERTICAL STABILIZER RH FWD DRAG ANGLE CRACKED. CORRECTIVE ACTION: REAPIRED VERTICAL STABILIZER RH FWD DRAG ANGLE IAW BOMBARDIER RE NO: 670-55-31-018 REV-A DATED 2016-11-10. FOR DETAILS SEE AVMAX WORK ORDER 80909 WORK CARD 3071.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 36,204 hrs · 29,453 cycles

STRINGER 25R SPLICE AT F.S. 333.00 CORRODED. CORRECTIVE ACTION: REPLACED STINGER 25R SPLICE AT F.S. 333.00 IAW CRJ 900 SRM 51-42-06. FOR DETAILS SEE AVMAX WORK ORDER 80909 WORK CARD 1158.

Part: SKIN — CRACKED (RT NACELLE) · airframe 36,204 hrs · 29,453 cycles

RH AFT CORE COWL CRACKED AT PYLON ATTACHMENT POINT. CORRECTIVE ACTION: REPAIRED RH AFT CORE COWL IAW ENGINEERING AUTHORIZATION #: 20-20021-015 REV. B DATED 2/15/2021. FOR DETAILS SEE WORK ORDER 80909 WORK CARD 4071

Part: CHANNEL — CORRODED (ZONE 100) · airframe 36,204 hrs · 29,453 cycles

LOWER TCAS ANTENNA MOUNT DOUBLE CORRODED. CORRECTIVE ACTION: REPLACED LOWER TCAS ANTENNA MOUNT DOUBLER IAW CRJ 900 SRM 51-42-06. FOR DETAILS SEE AVAMX WORK ORDER 80909 WORK CARD 1165.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 36,204 hrs · 29,453 cycles

STRINGER 26R SPLICE HAS CORROSION AT F.S. 333.00. CORRECTIVE ACTION: REPLACED STRINGER SPLICE 26R AT F.S. 333.00 IAW CRJ 900 SRM 51-42-0. REFFER TO AVMAX W/O: 80913 W/C: 1187 FOR DETAILS.

Part: FRAME — CORRODED (ZONE 100) · airframe 36,204 hrs · 29,453 cycles

FRAME AT F.S. 319.00 CORRODED BETWEEN STRINGER 26L AND STRINGER 26R. CORRECTIVE ACTION: REPLACED FRAME AT F.S. 319.00 FROM STRINGER 23R TO STRINGER 25L IAW WITH BOMBARDIER REO#: 670-53-21-799 REV A DATED: 2016-11-27.

Part: STRINGER — CORRODED (BS 333-364 S26R) · airframe 36,204 hrs · 29,453 cycles

STRINGER 26R CORRODED BETWEEN F.S. 333.00 AND F.S. 364.00. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER 26R BEWTEEN F.S. 333.00 AND F.S. 364.00

Part: DUCT — GOUGED (THRUST REVERSER) · airframe 36,204 hrs · 29,453 cycles

LH LOWER C-DUCT FLANGE HAS 2 GOUGES AT THE 8 AND 6 O'CLOCK POSITION. CORRECTIVE ACTION: REPAIRED LH LOWER C-DUCT FLANGE GOUGES IAW MHI REO #: 690-54-23-253 DATED 2021-02-21. FOR DETAILS SEE AVMAX WORK ORDER 80909 WORK CARD 4081.

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 36,204 hrs · 29,453 cycles

VERTICAL STABILZER LH AFT DRAG ANGLE CRACKED. CORRECTIVE ACTION: REPAIRED VERTICAL STABILZER LH AFT DRAG ANGLE IAW BOMBARDIER REO#: 670-55-31-018 REV-A DATED: 2016-11-10. FOR DETAILS SEE AVMAX WORK ORDER 80909 WORK CARD 3072

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 36,204 hrs · 29,453 cycles

LH SIDE WALL SEAT TRACK CORRODED BETWEEN F.S. 573.00 AND F.S. 661.00+8.40. CORRECTIVE ACTION: REPLACED LH SIDE WALL TRACK BETWEEN F.S. 573.00 AND F.S. 661+8.40 IAW CRJ 900 AMM 53-00-49. FOR DEATIL SEE AVMAX WORK ORDER 80909 WORK CARD 2274.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,204 hrs · 29,453 cycles

LH SIDE SEAT TRACK AT F.S.661.00+16 AND F.S. 669.40 CORRODED. CORRECTIVE ACTION: CORROSION AT F.S. 661.00+16 WIHTIN LIMITS. REPLACED SEAT TRACK FROM F.S. 669.00 TO 724.00 IAW CRJ 900 AMM 53-00-49. FOR DETAILS SEE AVMAX WORK ORDER 80909 WORK CARD 2275.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,204 hrs · 29,453 cycles

LH FLOOR SEAT RAIL AT L.B.L 9.0 CORRODED BETWEEN F.S. 394.00 AND F.S. 485.00. CORRECTIVE ACTION: REPLACED LH FLOOR SEAT RAIL AT L.B.L. 9.0 FROM F.S. 394.00 TO 485.00 IAW CRJ 900 AMM 53-00-49. FOR DETAILS SEE AVMAX WORK ORDER 80909 WORK CARD 2278.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 36,204 hrs · 29,453 cycles

RH SIDE SEAT TRACK CORRODED AT F.S. 485.00 TO F.S. 581.00. CORRECTIVE ACTION: REPLACED RH SIDE SEAT TRACK FROM FRAME F.S. 485.00 TO F.S. 581.00 IAW CRJ 900 AMM 53-00-49. FOR DETAILS SEE AVMAX WORK ORDER 80909 WORK CARD 2272.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,204 hrs · 29,453 cycles

RH FLOOR SEAT RAIL AT R.B.L. 9.0 CORRODED BETWEEN F.S. 847+62 AND F.S. 969.00. CORRECTIVE ACTION: REPLACED RH FLOOR SEAT RIAL AT R.B.L 9.0 BETWEEN F.S. 847.00+62 AND F.S. 696.00 IAW CRJ 900 AMM 53-00-49. FOR DETAILS SEE AVMAX WORK ORDER 80909 WORK CARD 2283.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,204 hrs · 29,453 cycles

STRINGER 27 AT FRAME 280 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER 27 FROM F.S. 280 TO F.S. 310 IAW CRJ900 SRM 51-42-06. FOR WORK PERFORMED, REFER TO AVMAX W/O: 80909 W/C: 1193

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,204 hrs · 29,453 cycles

L/H SIDE FLOOR SEAT TRACK AT LBL9.0 AT F.S. 667 TO F.S. 661+32 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR SEAT TRACK IAW CRJ900 SRM 51-41-02. FOR WORK PERFORMED, SEE AVMAX W/O: 80909 W/C: 2270

Part: SEAT TRACK — CORRODED (CABIN) · airframe 36,204 hrs · 29,453 cycles

L/H SIDE FLOOR SEAT TRACK AT LBL 9 F.S. 865-F.S. 977 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLASED FLOOR SEAT TRACK IAW CRJ900 AMM 53-00-49. FOR WORK PERFORMED, REFER TO AVMAX W/O: 80909 W/C: 2282

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,204 hrs · 29,453 cycles

L/H FLOOR SEAT RAIL AT LBL 9 F.S. 847- F.S. 865 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT RAIL IAW CRJ900 AMM 53-00-49. FOR WORK PERFORMED, REFER TO AVMAX W/O: 80909 W/C: 2281

Part: FLOORBEAM — CORRODED (FWD CABIN) · airframe 36,204 hrs · 29,453 cycles

FWD FLOOR BOARD SUPPORT AT F.S. 280 HAS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR BOARD FWD SUPPORT AT F.S. 280 IAW CRJ900 SRM 51-42-06.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 36,201 hrs · 29,452 cycles

THIS SDR IS AN AMENDMENT TO SDR#: V0XD20211228003, CORRECTING FRAME STATION FROM 295.00 TO FRAME STATION 310.00.

Part: FRAME — CORRODED (ZONE 100) · airframe 36,201 hrs · 29,452 cycles

FRAME AT FRAME STATION 295.00 CORRODED BETWEEN STRINGERS 27 AND 26R. CORRECTIVE ACTION: REMOVED CORROSION AND EVALUATED AREA, FOUND TO BE WITHIN LIMITS, IAW BOMBARDIER REO 670-53-21-1308 DATED: 2016/09/06.

Part: FRAME — CORRODED (ZONE 100) · airframe 36,201 hrs · 29,452 cycles

FRAME AT FRAME STATION 295.00 CORRODED BETWEEN STRINGERS 27 AND 26R. CORRECTIVE ACTION: REMOVED CORROSION AND EVALUATED AREA, FOUND TO BE WITH IN LIMITS, IAW BOMBARDIER REO 670-53-21-1308 DATED: 2016/09/06.

Part: STRAP — CORRODED (ZONE 100) · airframe 36,204 hrs · 29,453 cycles

PANEL 193AB ON R/H SIDE STRAP IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED STRAP AT PANEL 193AB. REFER TO AVMAX W/O: 80989 W/C: 1184.

Part: BRACKET — CRACKED (LT WING SLAT) · airframe 36,204 hrs · 29,453 cycles

L/H WING SLAT BOX 1-3 SUPPORT BRACKET CRACKED. CORRECTIVE ACTION: REPAIRED L/H SLAT BOX 1-3 SUPPORT BRACKET IAW BOMBARDIER REO 670-57-42-577 REV --, DATED 201-12-02. FOR WORK PERFORMED, REFER TO AVMAX W/O: 80909 W/C: 5097

Part: SKIN — GOUGED (ZONE 100) · airframe 36,201 hrs · 29,452 cycles

LOWER FUSELAGE SKIN GOUGED AT FRAME STATION 913.00 AND STRINGER 27. CORRECTIVE ACTION: BLENDED DAMAGED AREA AND FOUND TO BE WITHIN LIMITS, IAW BOMBARDIER REO 670-53-00-290 REV-F DATED: 2019/04/26.

Part: BRACKET — CRACKED (LT WING SLAT) · airframe 36,204 hrs · 29,453 cycles

R/H WING SLAT BOX 1-3 SUPPORT BRACKET CRACKED. CORRECTIVE ACTION: REPAIRED R/H SLAT BOX 1-3 SUPPORT BRACKET IAW BOMBARDIER REO 670-57-42-577 REV --, DATED 2016-12-02. FOR WORK PERFORMED, REFER TO AVMAX W/O: 80909 W/C: 6078

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 36,204 hrs · 29,453 cycles

STRINGER 26R SPLICE IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER 26R SPLICE IAW CRJ900 SRM 51-42-06. FOR WORK PERFORMED, REFER TO AVMAX W/O: 80909 W/C: 1178

Part: DRAIN — GOUGED (LT LOWER) · airframe 36,204 hrs · 29,453 cycles

L/H LOWER C DUCT OVERFLOW DRAIN PORT GOUGED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED L/H LOR C DUCT OVERBOARD DRAIN PORT IAW CRJ900 SRM 51-41-02. FOR WORK PERFORMED, REFER TO AVMAX W/O: 80909 W/C: 4080

Part: CHANNEL — CRACKED (WNG-BDY FAIRING) · airframe 36,204 hrs · 29,453 cycles

WING TO BODY C CHANNEL IS CRACKED ON PANEL 196DR. CORRECTIVE ACTION: REMOVED AND REPLACED C CHANNEL IAW CRJ900 SRM 51-41-02. FOR WORK PERFORMED, REFER TO AVMAX W/O: 80909 W/C:1180

Part: RETAINER — GOUGED (PAX DOOR SEAL) · airframe 36,204 hrs · 29,453 cycles

PASSENGER DOOR SEAL RETAINER GOUGED NEAR DOOR WIRING HARNESS. CORRECTIVE ACTION: REMOVED AND REPLACED PAX DOOR SAL RETAINER IAW BOMBARDIER REO 670-52-11-022 REV C, DATED 2013-02-01. REFER TO AVMAX W/O: 80909 W/C:8062

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,204 hrs · 29,453 cycles

LOWER TCAS ANTENNA BASE CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED TCAS ANTENNA BASE IAW CRJ900 SRM 51-42-06. REFER TO AVMAX W/O: 80989 W/C: 1165.

Part: STRINGER — CORRODED (BS 319-333) · airframe 36,204 hrs · 29,453 cycles

STRINGER 26R FROM F.S. 319-F.S.333 IS CORRODED BEYOND LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER 26R FROM F.S. 319 TO F.S. 333 IAW CRJ900 SRM 51-42-06. SEE AVMAX W/O: 80909 W/C: 1159 FOR WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 36,204 hrs · 29,453 cycles

INTERCOSTAL AT FRAME 364 STRINGER 27 IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL AT FRAME 364 STRINGER 27 IAW CRJ900 SRM 51-42-06. FOR WORK PERFORMED, REFER TO AVMAX W/O: 80909 W/C: 1169

Part: FRAME — CORRODED (ZONE 100) · airframe 36,204 hrs · 29,453 cycles

FRAME 349 BTWN STGR 27-26R CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED FRAME 349 IAW CRJ900 SRM 51-42-06. REFER TO AVMAX W/O: 80989 W/C: 1162.

Part: RIB — CRACKED (RT WING) · airframe 36,204 hrs · 29,453 cycles

RH WING MACHINED RIB IS CRACKED JUST I/B OF SLAT 1. REMOVED AND REPLACED MACHINED RIB IAW CRJ900 SRM 51-42-13, 51-42-06, AND 51-40-11. SEE AVMAX W/O: 80909 W/C: 6075 FOR WORK PERFORMED.

Part: LUG — CORRODED (AILERON PCU) · airframe 36,204 hrs · 29,453 cycles

LH AILERON I/B PCU O/B LUG HAS CORROSION. CORRECTIVE ACTION: PERFORMED REWORK OF THE AILERON PCU LUG IAW BOMBARDIER REO 670-57-61-107. SEE AVMAX W/O: 80909 W/C: FOR WORK PERFORMED.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 36,204 hrs · 29,453 cycles

L/H AFT VERTICAL STAB TO FUSELAGE DRAG ANGLE CRACKED . CORRECTIVE ACTION: REPAIRED L/H AFT DRAG ANGLE IAW BOMBARDIER REO 670-55-31-018 REV A, DATED 2016-11-10 REFER TO AVMAX W/O: 80989 W/C: 1184.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,204 hrs · 29,453 cycles

STRINGER 26R HAS SIGNS OF CORROSION BTWN F.S. 333 AND F.S. 364. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER 26R IAW CRJ900 SRM 51-42-06. REFER TO AVMAX W/O: 80909 W/C:1160

Part: FRAME — CORRODED (BS 280) · airframe 36,204 hrs · 29,453 cycles

CIRCUMFERENTIAL JOINT AT F.S. 280 IS CORRODED BEYOND LIMITS FROM STGR 26L TO STGR 26R. CORRECTIVE ACTION: REWORKED AREA IAW STS EA 79-2021-022 REV IR, DATED 02/03/2021.

Part: SMOKE WARNING — FALSE ACTIVATION (AFT LAVATORY) · airframe 36,201 hrs · 29,452 cycles

SMOKE AFT LAV WARNING IN FLT FALSE INDICATION. CREW VERFIED NO ACTUAL SMOKE IN LAV. A/C IS IN HEAVY CHECK, TROUBLE SHOOTING NEEDED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 36,173 hrs · 29,429 cycles

CA FLASHLIGHT INOP. R2 BATTERY

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,046 hrs · 28,598 cycles

FLOOR BEAM AT FS 680.00 RBL 9.0 IS CORRODED.

Part: FITTING — CHAFED (LT WING) · airframe 35,046 hrs · 28,598 cycles

L/H WING FITTING AT FS 797.00 IS CHAFED FWD AND AFT LUGS.

Part: BULB — INOPERATIVE (FLOOD LIGHT)

ROW 18 CEILING LEVEL FLOOD LIGHT INOP. RELAMPED.

Part: FLOORBEAM — CORRODED (BS 680) · corrosion level 2 · airframe 35,046 hrs · 28,598 cycles

WHILE PERFORMING SB670BA-53-036 FOUND CORROSION IN THE RH FLOOR BEAM AT FS680

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,782 hrs · 19,519 cycles

ROW 21 EMER FLOOD LIGHT INOP. CHARGED BATTERIES.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 34,205 hrs · 27,930 cycles

CA FLASHLIGHT INOP. PLACED ON MEL.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 34,196 hrs · 27,926 cycles

CA FLASHLIGHT INOP. PLACED ON MEL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,141 hrs · 27,888 cycles

CA FLASHLIGHT INOP. REPLACED BATTERY.

Part: LATCH — LACK OF LUBE (PAX DOOR) · airframe 34,104 hrs · 27,857 cycles

PAX DOOR DIFFICULT TO OPEN. LUBED LATCH MECHANISM AND OUTER HANDLE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 34,071 hrs · 27,835 cycles

CABIN EMER LIGHTS INOP. ALLOWED BATTS TO CHARGE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,005 hrs · 27,787 cycles

ROW 15 OVERHEAD EMERG FLOOD LIGHT INOP REPLACED BULB

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 33,728 hrs · 27,572 cycles

CABIN ENTRY EXIT SIGN OUT. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,728 hrs · 27,572 cycles

CABIN EGRESS LIGHT OUT AT ROW 13AC. RELAMPED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 33,260 hrs · 27,228 cycles

GEAR DISAGREE WARNING- EMERGENCY DECLARED. TROUBLE SHOOTING.

Part: LANDING GEAR — MALFUNCTIONED · airframe 33,257 hrs · 27,225 cycles

GEAR DISAGREE IN FLIGHT- GEARS W/N RETRACT. AC OOS

Part: CAM — OUT OF ADJUST (PAX DOOR) · airframe 31,678 hrs · 26,079 cycles

PAX DOOR DIFFICULT TO OPEN. ADJUSTED THE DOOR CENTERING CAMS AND ROLLERS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,909 hrs · 25,473 cycles

CEILING ROW 18 EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,896 hrs · 25,466 cycles

ROW 14 FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. R & R THE NR 1 AND 3 BATTERY PACKS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,684 hrs · 25,308 cycles

ROW 14 LT FLOOR LEVEL EMER LIGHT INOP.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,617 hrs · 25,255 cycles

GALLEY AND ROW 13 EMERG EXIT LIGHTS INOP. CHARGED BATTERIES.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 30,484 hrs · 25,149 cycles

14A FLOOR LEVEL EXIT SIGN ONE BULB INOP.

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 30,455 hrs · 25,126 cycles

ROW 18 CEILING FLOOD LIGHT INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 30,380 hrs · 25,064 cycles

FWD FA FLASHLIGHT LED INOPERATIVE. REPLACED THE FLASHLIGHT.

Part: BULB — DIM (EMERGENCY LIGHT) · airframe 30,363 hrs · 25,051 cycles

AFT DOOR EMERGENCY LIGHTS WERE DIM . REPLACED THE LAMPS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 30,222 hrs · 24,925 cycles

AFT FACING MID CABIN EMERGENCY EXIT SIGN INOPERATIVE. CHARGED THE BATTERY PACK.

Part: SIGN — INOPERATIVE (CABIN) · airframe 30,090 hrs · 24,811 cycles

ROW 4 EMER EXIT SIGN INOP.

Part: SIGN — INOPERATIVE (CABIN) · airframe 30,090 hrs · 24,811 cycles

ROW 14DF LWR EMER EXIT SIGN INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,996 hrs · 24,729 cycles

EMER FLOOD LIGHT ROW 18 INOP. PLACED ON MEL.

Part: DOOR — BINDING (MAIN PAX) · airframe 29,857 hrs · 24,621 cycles

PAX DOOR WILL NOT OPEN. REMOVED EXCESS GREASE, OPS CHECKED NORMAL

Part: STRIP — DETERIORATED (CABIN) · airframe 29,738 hrs · 24,526 cycles

(3) PAX DOOR ILLUM STRIPS DETERIORATED. REPLACED STRIPS.

Part: LIGHT — INOPERATIVE (ROW 20) · airframe 29,562 hrs · 24,387 cycles

ROW 20 OVERHEAD EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,516 hrs · 24,348 cycles

AFT CEILING EMER FLOOD LIGHT INOP. PLACED ON MEL.

Part: PLACARD — BROKEN (SERVICE DOOR) · airframe 29,317 hrs · 24,185 cycles

SERVICE DOOR EMER EXIT PLACARD BROKEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,062 hrs · 23,994 cycles

ROW 18 CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,824 hrs · 23,817 cycles

CARGO BAY FLOORBEAM LBL 27.0 AT FS 1031.0 IS CORRODED.

Part: STRIKER — CORRODED (GALLEY DOOR) · corrosion level 2 · airframe 28,824 hrs · 23,817 cycles

GALLEY SERVICE DOOR, LOWER SEAL STRIKER HAS MINOR CORROSION AT SCREW HOLES.

Part: SKIN — GOUGED (FUSELAGE) · airframe 28,824 hrs · 23,817 cycles

AFTER REMOVING AFT CARGO DOOR FUSELAGE SCUFF PLATE, FOUND FUSELAGE SKIN TO BE GOUGED IN MULTIPLE LOCATIONS. FUSELAGE SKIN REPAIRED IAW REO 690-53-61-654, REV-, DATED 2016-12-22

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,824 hrs · 23,817 cycles

FUSELAGE FRAME, FS333.00, STRINGER 0, CRACKED. REPAIRED IAW REO 690-53-21-875, REV A, DATED 2016-12-28.

Part: DOOR SILL — CORRODED (BS 319-349) · corrosion level 2 · airframe 28,824 hrs · 23,817 cycles

GALLEY SERVICE DOOR SILL CORRODED

Part: FRAME — CRACKED (BS 235) · airframe 28,824 hrs · 23,817 cycles

RIGHT BS 235 UPPER FRAME SECTOR HAS A CRACK INDICATION 0.5" LONG ON THE FWD FACE AT STRINGER 13R FASTENER HOLE. FAILED NDT INSPECTION.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 28,824 hrs · 25,817 cycles

STRINGER 3L CRACKED AT FS 280.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 28,824 hrs · 23,817 cycles

RIGHT FLOORBEAM ANGLE CORRODED AT BS 280.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,350 hrs · 23,466 cycles

ROW 21 EMERGENCY CEILING FLOODLIGHT INOPERATIVE. REPLACED THE LAMP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,350 hrs · 23,466 cycles

ROW 18 EMERGENCY CEILING FLOODLIGHT INOPERATIVE. REPLACED THE LAMP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,269 hrs · 23,402 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,241 hrs · 23,380 cycles

FOUND ONE LAMP INOPERATIVE ROW 13A LOWER EXIT SIGN.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,015 hrs · 23,196 cycles

ROW 18 EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED THE LAMP.

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 27,790 hrs · 23,028 cycles

CEILING LEVEL EMERGENCY FLOOD LGHT ROW 18 INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,090 hrs · 22,493 cycles

ONE LAMP CENTER AISLE EXIT SIGN, ROW 13 INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,957 hrs · 22,390 cycles

EMERGENCY LIGHT FLOOR LEVEL ROW 14 INOPERATIVE.

Part: LIGHT — INOPERATIVE (ROW 14) · airframe 26,469 hrs · 22,024 cycles

EMERGENCY FLOOD LIGHT ROW 14 INOPERATIVE.

Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 26,372 hrs · 21,951 cycles

SERVICE DOOR FLOOR LEVEL EMERGENCY LIGHT BULB AND LENS MISSING. REPLACED LIGHT ASSY.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 25,835 hrs · 21,522 cycles

LEFT EXIT AFT OVERWING EMERGENCY LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (FWD CABIN) · airframe 25,819 hrs · 21,508 cycles

FORWARD LEFT EXIT EMERERGENCY LIGHT INOPERATIVE. OPEN

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 25,819 hrs · 21,508 cycles

AFT LEFT EXIT EMERGENCY LIGHT INOPERATIVE. OPEN

Part: LIGHT — INOPERATIVE (FWD CABIN) · airframe 25,819 hrs · 21,508 cycles

FORWARD RIGHT EXT EMERGENCY LIGHT INOPERATIVE. OPEN

Part: LIGHT — INOPERATIVE (ROW 20) · airframe 25,748 hrs · 21,452 cycles

ROW 20, CEILING FLOOD LIGHT INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 25,460 hrs · 21,231 cycles

AFT F/A FLASHLIGHT INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 25,460 hrs · 21,231 cycles

AFT F/A FLASHLIGHT INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,460 hrs · 21,231 cycles

ROW 13 EMERGENCY EXIT SIGN HAS ONE BULB INOPERATIVE.

Part: FLASHLIGHT — DISCHARGED (CABIN) · airframe 25,309 hrs · 21,115 cycles

FWD AND AFT F/A FLASHLIGHTS NOT CHARGED.

Part: DOOR — LACK OF LUBE (MAIN CABIN) · airframe 25,250 hrs · 21,067 cycles

MAIN CABIN DOOR HARD TO OPEN. MAINTENANCE LUBED DOOR.

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 24,766 hrs · 20,726 cycles

CEILING EMERGENCY FLOOR LIGHT ROW 18 INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 24,740 hrs · 20,698 cycles

FWD F/A'S FLASHLIGHT INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 24,507 hrs · 20,544 cycles

EMERGENCY LIGHTS INOPERATIVE SWITCH LEFT IN ARM POSSITION. RECHARGED WITH ACFT ELECTRICAL POWER.

Part: WARNING MESSAGE — ILLUMINATED (EMERGENCY EXIT) · airframe 24,205 hrs · 20,332 cycles

RIGHT WING AFT EMERGENCY DOOR CAUTION MESSAGE INTER.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 23,987 hrs · 20,177 cycles

FWD F/A FLASHLIGHT INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,709 hrs · 19,982 cycles

ROW 6 CEILING FLOOD LIGHT INOPERATIVE. REPLACED THE LAMP.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,496 hrs · 19,814 cycles

SERVICE DOOR EMERERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,496 hrs · 19,814 cycles

EMERGENCY LIGHT MAIN CABIN DOOR INOPERATIVE. MAINTENANCE REPLACED THE BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,496 hrs · 19,814 cycles

EMERGENCY LIGHT AT ROW 13 ARE INOPERATIVE. MAINTENANCE REPLACED THE BULB.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,251 hrs · 19,610 cycles

ONE LAMP INOPERATIVE ROW 13DF EXIT SIGN.

Part: FLOOR SUPPORT — CORRODED (BS 349) · corrosion level 2 · airframe 23,202 hrs · 19,570 cycles

RIGHT FLOOR SUPPORT AT BS 349 IS CORRODED OUT OF LIMITS.

Part: DOOR SILL — CORRODED (BS 310-349) · corrosion level 2 · airframe 23,202 hrs · 19,570 cycles

SERVICE DOOR SILL IS CORRODED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,202 hrs · 19,570 cycles

RT FLOOR SUPPORT CORRODED FROM FS 280-310. FOUND OUT OF LIMITS.

Part: ATTACH ANGLE — CORRODED (BS 349-364) · corrosion level 2 · airframe 23,202 hrs · 19,570 cycles

ON REMOVAL OF STRINGER 26R, FOUND ATTACH ANGLE BETWEEN BS 349 & 364 TO BE CORRODED BEYOND SRM LIMITS.

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 23,202 hrs · 19,570 cycles

STRINGER SPLICE 25R AT BS 333 CORRODED.

Part: STRINGER — CORRODED (BS 333-349) · airframe 23,202 hrs · 19,570 cycles

STRINGER 26R BS 333 - 349 CORRODED.

Part: FRAME — CORRODED (BS 295) · airframe 23,202 hrs · 19,570 cycles

FRAME BS 295 STRINGER 26L-26R CORRODED.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 23,202 hrs · 19,570 cycles

LT AND RT INTERCOSTALS AT BL 0, BS 349-364, CORRODED.

Part: FRAME — CORRODED (BS 349) · airframe 23,202 hrs · 19,570 cycles

FRAME BS 349, STRINGER 25L-25R CORRODED.

Part: STRINGER — CORRODED (BS 295-310) · airframe 23,202 hrs · 19,570 cycles

STRINGER 26R BS 310 - 295, CORRODED.

Part: STRINGER — CORRODED (BS 333-349) · airframe 23,202 hrs · 19,570 cycles

STRINGER 25R BS 349-333 CORRODED.

Part: STRINGER — CORRODED (BS 333-349) · airframe 23,202 hrs · 19,570 cycles

STRINGER 25R FS 349 - 333, CORRODED.

Part: FRAME — CORRODED (BS 310) · airframe 23,202 hrs · 19,570 cycles

FRAME AT BS 310, STRINGERS 25L-25R CORRODED.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 23,202 hrs · 19,570 cycles

VERTICAL STABILIZER FWD DRAG ANGLE IS CRACKED.

Part: BULKHEAD WEB — CORRODED (ZONE 100)

FS 280, LT AND RT BULKHEAD LOWER WEBS CORRODED.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2

FS 280 FLOORBEAM CORRODED, & CRACKED.

Part: BLADE — VIBRATION (ENGINE) · airframe 22,367 hrs · 18,797 cycles

DURING ENGINE FAN BLADE INSPECTION, BLADE SHAKE, AND VIBRATION CHECK ENGINE RUNS COMPLIED WITH AS REQUIRED IAW AMM 72-21-02. FAN BLADE LUBRICATION COMPLIED WITH & ENGINE VIBRATION CHECK WITHIN LIMITS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,380 hrs · 18,808 cycles

CEILING EMERGENCY FLOOD LIGHT ROW 18 INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,305 hrs · 18,740 cycles

RIGHT EMERGENCY EXIT SIGN, ROW 13 HAS TWO BULBS INOPERATIVE. MAINTENANCE REPLACED THE BULBS.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 22,248 hrs · 18,695 cycles

F/A FWD FLASHLIGHT INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,223 hrs · 18,670 cycles

14F FLOOR LEVEL EMERGENCY EXIT SIGN LAMPS ARE INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,854 hrs · 18,444 cycles

SERVICE DOOR EXIT SIGN, 1 OF 5 BULBS INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,854 hrs · 18,444 cycles

ROW 14 RT EXIT SIGN HAS ONE LAMP INOPERATIVE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 21,382 hrs · 17,917 cycles

ROW 14AC EXIT SIGN ONE BULB OUT.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 21,298 hrs · 17,836 cycles

FWD F/A'S FLASHLIGHT INOPERATIVE. REPLACED BATTERIES.

Part: LIGHT — INOPERATIVE (CAIBN) · airframe 21,291 hrs · 17,828 cycles

ROW 6 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED ROW 6 CEILING EMERGENCY FLOOD LIGHT.  OPS CHECKED GOOD, NO DEFECT NOTED.

Part: FLASHLIGHT — INOPERATIVE (FWD FA) · airframe 21,136 hrs · 17,692 cycles

FWD F/A FLASHLIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 20,932 hrs · 17,524 cycles

CEILING LEVEL EMERGENCY FLOOD LIGHT ROW 18 INOPERATIVE.

Part: CAGE — BROKEN (SMOKE DETECTOR) · airframe 20,548 hrs · 17,165 cycles

AFT CARGO BAY FWD SMOKE DETECTOR CAGE BROKEN. REMOVED AND REPLACED AFT CARGO BAY FWD SMOKE DETECTOR CAGE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 20,295 hrs · 16,939 cycles

GALLEY EMERGENCY EXIT SIGN BULB, OUT. REPLACED BULB.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 19,531 hrs · 16,260 cycles

F/O FLASHLIGHT INOPERATIVE UPON PRE FLIGHT INSPECTION. REMOVED AND REPLACED F/O FLASHLIGHT.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 18,886 hrs · 15,664 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 18,172 hrs · 14,985 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE ON POST FLIGHT INSPECTION. R & R BATTERY.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 18,163 hrs · 14,978 cycles

AFT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT

Part: EXTINGUISHER — DISCHARGED (CARGO BAY) · airframe 17,920 hrs · 14,760 cycles

LOW PRESSURE CARGO FIRE BOTTLE DISCHARGED. REMOVED AND REPLACED FIRE EXTINGUISHER CONTAINER. OPS CHECKED NORMAL.

Part: EXTINGUISHER — DISCHARGED (CARGO BAY) · airframe 17,920 hrs · 14,760 cycles

HIGH PRESSURE CARGO FIRE BOTTLE DISCHARGED. REMOVED AND REPLACED FIRE EXTINGUISHER CONTAINER. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE · airframe 17,839 hrs · 14,674 cycles

AFT E/E BAY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT E/E BAY LIGHT.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 17,512 hrs · 14,384 cycles

TWO EXTERIOR LEFT EMERGENCY LIGHTS INOPERATIVE. SECURED CONNECTOR J377,

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,505 hrs · 14,378 cycles

OVERHEAD EMERGENCY LIGHT INOPERATIVE ROW 9. MX REPLACED BULB, OPS CHECKED GOOD.

Part: SKIN — CHAFED (FUSELAGE) · airframe 17,503 hrs · 14,376 cycles

LOWER FUSELAGE SKIN IS CHAFED JUST FORWARD OF FS 913.00 AT STRINGER 27. DAMAGE IS APPROX .500 LONG BY .300 WIDE, AND .022 DEEP. PERFORMED A MAJOR REPAIR TO THE FUSELAGE SKIN AT FS 913.00 ON STRINGER 27 BY BLENDING OUT THE DAMAGE IAW BOMBARDIER INC (REO) 670-53-00-014 REV.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,482 hrs · 14,355 cycles

SEVERAL EMERGENCY EXIT LIGHT BULBS IN GALLEY INOP. R2 BURNT OUT BULBS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,769 hrs · 13,714 cycles

ROW 14 FLOOR EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,769 hrs · 13,714 cycles

FLAPS FAIL CAUT IN FLT. MX CLEARED INHIBITS.

Part: PROXIMITY SENSOR — FAILED (PAX DOOR HANDLE) · airframe 16,463 hrs · 13,446 cycles

PAX DOOR OUTER HANDLE CAUTION INTERMITTENT. REMOVED AND REPLACED PROXIMITY SENSOR PX107.

Part: SENSOR — FAULTY (NR 3 BRAKE) · airframe 16,199 hrs · 13,234 cycles

NR 3 BRAKE TEMP SHOWS DASHES. R2 NR 3 BRAKE TEMP SENSOR.

Part: UNKNOWN — MALFUNCTIONED (BRAKE TEMP) · airframe 16,199 hrs · 13,234 cycles

NR 3 BRAKE TEMP ERATIC. PROPERLY C/W MEL.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 16,123 hrs · 13,162 cycles

L BLEED DUCT WARN IN FLIGHT. RESECURED MT137 AND TIGHTENED CLAMP ON ISO VALVE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,042 hrs · 13,082 cycles

WOW INPUT CAUT NLG. INSPECTED FOUND NO DEFECTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,997 hrs · 13,044 cycles

ROW 12 CEILING EMERGENCY FLOOD LT INOP. RELAMPED EMERGENCY LIGHT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 15,793 hrs · 12,864 cycles

F/O'S FLASHLIGHT INOP. R2 FLASHLIGHT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 15,760 hrs · 12,840 cycles

LIGHTED EMER EXIT SIGN 16F 1 BULB OUT. RELAMPED EMERGENCY LIGHT.

Part: WARNING SYSTEM — FALSE ACTIVATION (BTMS) · airframe 15,746 hrs · 12,828 cycles

NR 3 BTMS IND 5 AND RED W BRAKE OH WARN. RESET BTMS PER QRH.

Part: SENSOR — DEFECTIVE (BTMS) · airframe 15,746 hrs · 12,828 cycles

RT INBD BTMS ERRATIC (NR 3 BTMS SENSOR DISCONNECTED). SENSOR CLEANED NO FIX. R2 BTMS SENSOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,688 hrs · 12,774 cycles

ROW 12 CEILING LEVEL EMERGENCY FLOOD LT INOP. RELAMPED EMERGENCY LIGHT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 15,633 hrs · 12,722 cycles

AFT FA FLASHLIGHT INOP. R2 AFT FA FLASHLIGHT BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,584 hrs · 12,673 cycles

EMERGENCY LIGHT INOP UNDER FORWARD FA. R2 LAMP.

Part: HOOK — LOOSE (EMERGENCY EXIT) · airframe 15,533 hrs · 12,633 cycles

LT SIDE ROW 16 EMERGENCY HANDLE COVER LOOSE. R2 VELCRO.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 15,484 hrs · 12,596 cycles

AFT F/A EMERGENCY FLASHLIGHT NOT "BLINKING". R2 AFT F/A EMERGENCY FLASHLIGHT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 15,468 hrs · 12,579 cycles

PARKING BRAKE SOV CAUTION. PERFORMED OP CHECK OF BRAKES. NO DEFECTS.

Part: SEAL — OUT OF POSITION (WINDOW) · airframe 15,443 hrs · 12,554 cycles

ROW 20F EXTERIOR WINDOW SEAL EXTRUDING. R2 ROW 20DF WINDOW SEAL.

Part: CABLE — BROKEN (PAX DOOR) · airframe 15,424 hrs · 12,534 cycles

PAX DOOR CABLE SUSPECT BROKEN. R2 CABLE

Part: BOLT — LOOSE (LT WING) · airframe 15,368 hrs · 12,494 cycles

FUEL LK LEFT WING; TIGHTENED LOOSE BOLT AT LEFT I/B FLAP HINGE BOX, O/B FWD FITTING.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 15,367 hrs · 12,493 cycles

THE 16DF EMER EXIT HANDLE COVER LOOSE. RE-SECURED COVER.

Part: STRIP — LOOSE (SERVICE DOOR) · airframe 15,291 hrs · 12,423 cycles

SVC DOOR FLORESCENT STRIP LOOSE. RESECURED FLORESCENT STRIP.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 15,108 hrs · 12,246 cycles

FWD F/A FLASHLIGHT INOP. MX R2 BATTERY.

Part: COVER — BROKEN (HANDLE) · airframe 14,983 hrs · 12,136 cycles

HANDLE COVER RT EXIT ROW 15 BROKE. MX RE-SECURED WITH VELCRO.

Part: PLATE — BENT (DOOR) · airframe 14,969 hrs · 12,124 cycles

LOGO PLATE ON STOW STEP BENT. MX DEFERRED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,750 hrs · 11,940 cycles

AFT EMERGENCY FLOOD LIGHT INOP. MX RELAMPED EMERGENCY LIGHT.

Part: CONDUIT — TORN (SERVICE DOOR) · airframe 14,679 hrs · 11,880 cycles

SERVICE DOOR WIRE CONDUIT TORN. MX REPAIRED WIRING PROTECTION FROM SERVICE DOOR.

Part: OXYGEN MASK — DEPLOYED (LAVATORY) · airframe 14,514 hrs · 11,726 cycles

AFT LAV O2 MASK FOUND TO BE DEPLOYED. MX RESTOWED MASK.

Part: SELECTOR VALVE — INOPERATIVE (NLG) · airframe 14,514 hrs · 11,726 cycles

GEAR DISAGREE WARNING ON GEAR EXTENSION. MX R2 LANDING GEAR SELECTOR VALVE.

Part: PLACARD — DAMAGED (CABIN DOOR) · airframe 14,403 hrs · 11,636 cycles

MAIN ENTRY DOOR PLACARD "TO OPEN LIFT HANDLE" DAMAGED. MX INSTALLED NEW "TO OPEN LEFT HANDLE" MED PLACARD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,150 hrs · 11,412 cycles

ONE CENTER CEILING EMERGENCY FLOOD LIGHT INOP. MX RELAMPED EMERGENCY FLOOD LIGHT.

Part: PLACARD — DAMAGED (PAX STAIRS) · airframe 13,852 hrs · 11,160 cycles

STAIRS OPEN PLACARD DAMAGED. MX REMOVED & REPLACED OPEN PLACARD AT PAX DOOR STAIRS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,336 hrs · 10,707 cycles

AFT EMERGENCY LIGHT INOP. MX RELAMPED EMERGENCY LIGHT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 12,982 hrs · 10,419 cycles

AFT F/A FLASHLIGHT WOULD NOT CHARGE, FWD F/A FLASHLIGHT INOP. R2 FLASHLIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,804 hrs · 10,292 cycles

RIGHT LOWER EXIT SIGN INOP. REMOVED AND REPLACED LAMPS, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,815 hrs · 10,287 cycles

RT LOWER EXIT SIGN INOP. MX REMOVED AND REPLACED LAMPS, OPS CHECK GOOD.

Part: PROXIMITY SWITCH — MALFUNCTIONED (CARGO BAY) · airframe 12,223 hrs · 9,792 cycles

AFT CARGO CAUTION. DI26 NEED ADJUSTED (HAPPENED IN FLIGHT). HARNESS HAS ALREADY BEEN REPLACED. T/S TO PX 102 PROX SWITCH. R2 PX 102 ON 2/6/2010.

Part: BULB — BURNED (CABIN) · airframe 11,936 hrs · 9,541 cycles

FLT 2631 - CREW REPORTED AT 12000 FT THE FWD LAV SMOKE MASTER WARNING MESSAGE ILLUMINATED. THE NR 1 FA REPORTED THE POSSIBILITY OF A ODOR OF SMOKE OR FUMES IN THE AREA. CREW ELECTED TO RETURN TO CLT. CREW DID NOT DECLARE AN EMERGENCY. AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED BURNED CEILING BULB 1D, RAN ENGS/BLEED, NO DEFECTS.

Part: WINDOW — CRACKED (COCKPIT) · airframe 11,360 hrs · 9,036 cycles

ASH FLT 2638 CLT-ORF CREW REPORTED DURING FLT THE F/O SIDE WINDOW STARTED TO ARC IN THE LOWER CORNER, THEN THE WINDOW SHATTERED. CREW ELECTED TO RETURN TO CLT. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MX REPLACED WINDOW.

Part: LIGHT — LOOSE (CABIN) · airframe 9,935 hrs · 7,857 cycles

ASH FLT 2607 CLT-IAH. PILOT REPORTED THAT THE CENTER CEILING EMERGENCY FLOOD LIGHT IS INOPERATIVE. MX RESECURED LIGHT BULB, OPS CHECKED GOOD.

Part: PACKING — DAMAGED (NR 2 EDP) · airframe 9,794 hrs · 7,744 cycles

IN-FLIGHT NR 2 ENG SHUTDOWN ON APPROACH DUE TO LOW OIL PRESSURE. OIL QUANTITY DROPPED TO 15 PERCENT. MX REPLACED PACKINGS AT NR 2 EDP LEAK CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

ASH FLT 2831 PHX-TUS. EMERGENCY FLOOD LIGHT 3RD FROM AFT INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECK GOOD. (S)

Part: COVER — LOOSE (EMERGENCY EXIT)

ASH FLT 2877 PHX-ELP. THE 16F EMERGENCY EXIT HANDLE WILL NOT STOW. RE-SECURED THE DOOR HANDLE COVER. (B)

Part: ACM — MALFUNCTIONED (NR 2) · airframe 8,236 hrs · 6,564 cycles

ASH FLT 2698 BNA-CLT. SMOKE IN CABIN ON LANDING. REMOVED AND REPLACED NR 2 ACM.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 8,104 hrs · 6,447 cycles

ASH FLT 2608 CLT-SDF - FORWARD F/A FLASHLIGHT WILL NOT CHARGE. REMOVED AND REPLACED FLASHLIGHT, OP CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED · airframe 6,707 hrs · 5,288 cycles

ASH FLT 2674 CLT - RUDDER LIMIT STATUS MESSAGE. MX PERFORMED S POST, OPS CK GOOD.

Part: COUNTERBALANCE — OUT OF ADJUST (PAX DOOR) · airframe 5,498 hrs · 4,273 cycles

ASH 2627 CLT - PAX DOOR HARD TO OPEN. ADJUSTED COUNTER BALANCE.

Part: WARNING SYSTEM — MALFUNCTIONED (STABILIZER SYS) · airframe 4,451 hrs · 3,399 cycles

ASH 2979 OKC. PITCH FEEL FAULT STATUS. CONTRACT MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (STABILIZER SYS) · airframe 4,387 hrs · 3,352 cycles

ASH 2866 PHX. AIRCRAFT HAD AN PITCH FEEL CAUTION MESSAGE. MX RESET THE SSCU'S.

Part: CONTROL UNIT — MALFUNCTIONED (NR 1) · airframe 4,381 hrs · 3,348 cycles

ASH 2936 TUS. PITCH FEEL CAUTION. MX REMOVED AND REPLACED SSCU1.

Part: WARNING SYSTEM — MALFUNCTIONED (STABILIZER SYS) · airframe 4,373 hrs · 3,340 cycles

ASH 2639 GSO. PITCH FEEL FAULT STATUS. PERFORMED SPOST1/2 WITH FLIGHT CREW. NO FURTHER DEFECTS NOTED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 3,662 hrs · 2,775 cycles

ASH 5032 CLT - PITCH FEEL FAULT STATUS. MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER SYS) · airframe 3,644 hrs · 2,775 cycles

ASH 6090 CLT - STAB/SPOILER STATUS MESSAGE. MX REPLACED THE SSCU.

Part: WARNING SYSTEM — MALFUNCTIONED (HORIZ STAB) · airframe 3,495 hrs · 2,636 cycles

ASH 5017 CLT - PITCH FEEL STATUS MSG. MX RESET THE SYSTEM.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 3,495 hrs · 2,636 cycles

ASH 5020 CLT - PITCH FEEL STATUS MESSAGE. MX RESET THE SYSTEM.

Part: TRIM SWITCH — LACK OF LUBE (COCKPIT) · airframe 3,081 hrs · 2,312 cycles

ASH 6309 PHX - AILERON TRIM SWITCH WON'T MOVE TO LEFT. MX CLEANED AND LUBE SWITCH. OP'S CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (L/E SLAT) · airframe 2,857 hrs · 2,129 cycles

ASH 6486 PHX - MACH TRIM FAULT AND STAB FAULT DURING CLIMB-OUT AND INTERMITTENT SLAT FAULT MSG IN FLIGHT. MX REPLACED NR 1 SSCU AND PLACED SLAT DISCONNECT SYSTEM ON MEL. ACFT CONTINUED OPERATIONS. MX CND.

Part: STATUS MESSAGE — ILLUMINATED (SLATS) · airframe 2,850 hrs · 2,123 cycles

ASH 6301 PHX - SLAT FAULT STATUS MSG. MX CND.

Part: LIMITER — UNKNOWN (RUDDER) · airframe 2,421 hrs · 1,792 cycles

ASH 6094 PHX - RUDDER LIMIT FAULT STATUS MESSAGE. MX RESET THE SYSTEM.

Part: TRU — SMOKE · airframe 1,594 hrs · 1,116 cycles

ASH 6443 PHX, SMOKE WAS COMING FROM THE NOSE AREA. MAINTENANCE REPLACED THE TRU.

Part: LIMITER — WARNING MESSAGE (RUDDER) · airframe 1,559 hrs · 1,090 cycles

ASH 2611 CLT - RUDDER LIMIT FAULT STATUS MESSAGE. MAINTENANCE REMOVED AND REPLACED RTL RVDT.

Part: SENSOR — OUT OF ADJUST (EMERGENCY DOOR) · airframe 913 hrs · 625 cycles

ASH 6092 PHX - RT FWD EMERGENCY DOOR CAUTION MESSAGE. MX INSPECTED AND FOUND DOOR TO BE SECURE BUT EXPERIENCED AN INDICATION PROBLEM. MX ADJUSTED DOOR SENSOR.