N905J

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,701 hrs · 35,447 cycles

ROW 13 A FLR LVL EXIT SIGN (1) BULB INOP. REPLACED BULB

Part: NONE — NONE · airframe 44,270 hrs · 35,132 cycles

FLAP FAIL CAUTION (EMERGENCY DECLARED). RESET SFECU AND CLEARED INHIBITS, OPS CHECK GOOD.

Part: NONE — NONE · airframe 43,617 hrs · 34,656 cycles

13A EMERGENCY EXIT SIGN-1 BULB INOP. REPLACED BULB.

Part: NONE — NONE · airframe 43,617 hrs · 34,656 cycles

SERVICE DOOR EXIT SIGN-2 BULBS INOP. REPLACED BULBS.

Part: NONE — NONE · airframe 43,603 hrs · 34,646 cycles

GEAR DISAGREE WARN IN FLIGHT -EMER DECLARED. AIRCRAFT CURRENTLY OOS.

Part: NONE — CRACKED (CENTER COCKPIT-L) · airframe 43,326 hrs · 34,453 cycles

THE LBL 12.00 FLOOR BEAM (P/N: CC670-33202-15) WAS FOUND WITH A CRACK. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) A) 53-11-43-001-001-A01, FIGURE 53-11-43-991-807, ITEM 108B (REV.38 DATED JUL. 25,2020.) B) 53-11-43-201-003-A01, FIGURE 53-11-43-995-819, ITEM 33(REV 38 DATED JUL. 25, 2020).

Part: NONE — NONE (LH WING) · airframe 43,326 hrs · 34,453 cycles

SLAT TRACKS 2-1 (P/N CC670-12042-7), 2-2 (P/N CC670-12051-11) 2-3 (P/N CC670-12062-7) OF SLAT #2 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-12-00 PROCEDURES.

Part: NONE — NONE (LH WING) · airframe 43,326 hrs · 34,453 cycles

SLAT TRACK 1-1 (P/N CC670-12012-15), 1-2 (P/N CC670-12021-11) AND 1-3 (P/N CC670-12032-7) OF SLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM).51-12-00 PROCEDURES

Part: NONE — CORRODED (LH WING) · airframe 43,326 hrs · 34,453 cycles

SLAT TRACKS 2-1 (P/N CC670-12042-7), 2-2 (P/N CC670-12051-11) 2-3 (P/N CC670-12062-7) OF SLAT #2 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-12-00 PROCEDURES.

Part: NONE — CORRODED (LH WING) · airframe 43,326 hrs · 34,453 cycles

SLAT TRACKS 3-1 (P/N CC670-12072-7) AND 3-2 (CC670-12081-9) OF SLAT #3 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-12-00 PROCEDURES.

Part: NONE — CORRODED (LH WING) · airframe 43,326 hrs · 34,453 cycles

SLAT TRACKS 3-1 (P/N CC670-12072-7) AND 3-2 (CC670-12081-9) OF SLAT #3 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-12-00 PROCEDURES.

Part: NONE — NONE (LH WING) · airframe 43,326 hrs · 34,453 cycles

SLAT TRACK 1-1 (P/N CC670-12012-15), 1-2 (P/N CC670-12021-11) AND 1-3 (P/N CC670-12032-7) OF SLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM).51-12-00 PROCEDURES

Part: NONE — CORRODED (LH WING) · airframe 43,326 hrs · 34,453 cycles

SLAT TRACKS 3-1 (P/N CC670-12072-7) AND 3-2 (CC670-12081-9) OF SLAT #3 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-12-00 PROCEDURES.

Part: NONE — CORRODED (LH WING) · airframe 43,326 hrs · 34,453 cycles

SLAT TRACK 1-1 (P/N CC670-12012-15), 1-2 (P/N CC670-12021-11) AND 1-3 (P/N CC670-12032-7) OF SLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM).51-12-00 PROCEDURES

Part: NONE — NONE (PANEL 413 AT) · airframe 43,327 hrs · 34,453 cycles

THE PYLON DETACHABLE TRAILING EDGE ASSEMBLY WAS FOUND TO HAVE EROSION DAMAGE AFFECTING THE ALUMINUM MESH. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-73-00-201-009-A01, (REV. 38 DATED 7-9-2021).

Part: NONE — NONE (FS 193, STGR 16R) · airframe 43,327 hrs · 34,453 cycles

THE MAINTENANCE DISCOVERED CRACK ON THE SKIN PANEL. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-14-06, FIG. 51-14-06-991-815, 51-23-00 AND SRM 51-21-16.

Part: NONE — NONE (FS 310.00 FWD PA) · airframe 43,327 hrs · 34,453 cycles

THE PASSENGER DOOR FWD SEAL STRIKER WAS FOUND BENT COMMON TO THE OUTBOARD FLANGE OF THE STRIKER. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-23-001-001-A01, FIG 53-21-23-995-818 ITEM 1388 (REV. 38 DATED JUL. 25, 2020).

Part: NONE — NONE (FS501-661 STR19L) · airframe 43,327 hrs · 34,453 cycles

THE LOWER FUSELAGE SKIN PANEL WERE REPORTED WITH TOTAL OF FOUR ZONES WITH MULTIPLE NICK DAMAGES. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-31-01-991-806, ITEM 1, A AND B (REV. 37 DATED AUG. 15, 2019. DEFECT LOCATION: FS 501.00 -FS 661.00 AND STGR 19L -STGR 25L

Part: NONE — NONE (LH WING LE EDGE) · airframe 43,327 hrs · 34,453 cycles

THE LH WING L/E SLAT 1 T/E WEDGE WAS FOUND WITH AN EXISTING DAMAGE BLENDOUT.AT THE AFT EDGE, BETWEEN SLAT TRACK 1-2 AND SLAT TRACK 1-3. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-00-00, 51-21-16, AND 51-13-02 TABLE 1. DEFECT LOCATION: LH WING LEADING EDGE SLAT NO. 1 T/E WEDGE

Part: NONE — DENTED (LONGERON SIDE FI) · airframe 43,327 hrs · 34,453 cycles

THE LONGERON SIDE FITTING FUEL VENT AND THE WELDED TUBE ASSEMBLY WERE FOUND TO HAVE DENTS ON THE OUTER SURFACE OF THE TUBES. PERFORMED PERMANENT REPAIR IAW CRJ900 AMM 28-12-00-710-801-A01 (REV 68 DATED 9-21-2021) AND CRJ900 AIPC 28-12-91-05, FIG 5 ITEM 5 (REV 70 DATED 8-9-2021). DEFECT LOCATION: LONGERON SIDE FITTING FUEL VENT

Part: ACCESS PANEL — NONE (RH WING SLAT# 2) · airframe 43,327 hrs · 34,453 cycles

THE RH WING L/E SLAT# 2 ACCESS PANEL 63102 WAS FOUND TO HAVE AN ELONGATED FASTENER HOLE. PERFORMED PERMANENT REPAIR IAW CRJ900 IPC 57-42-32, FIG. 5, ITEM 125 (REV. 70DATED JUN. 25. 2021 ).

Part: NONE — CRACKED (LH ENG LWRTRANS) · airframe 43,227 hrs · 34,453 cycles

THE LH ENGINE LOWER TRANSCOWL INNER SKIN WAS FOUND TO HAVE 11 SMALL CRACKS. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 54-21-05-991-801, ITEMS 2&3 (REV. 38 DATED 7-6-2021). DEFECT LOCATION: LH ENGINE LOWER TRANSCOWL ASSEMBLY

Part: FLOORBEAM — CORRODED (BS 333) · airframe 43,327 hrs · 34,453 cycles

THE CROSSBEAM WAS FOUND TO HAVE SEVERE CORROSION DAMAGE ON THE UPPER FLANGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-43-001-A02, FIG. 53-21-43-991-802, ITEM 3.

Part: NONE — NONE (RH WING SLAT TRA) · airframe 43,327 hrs · 34,453 cycles

THE RH WING SLAT #3 WERE FOUND TO HAVE CORROSION DAMAGE ON BOTH THE UPPER AND LOWER SURFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG.10, ITEMS 15,AND 90 (REV. 70 DATED 10 AUG 2021). DEFECT LOCATION: RH WING-SLAT TRACKS 2-1, 2-2, AND 2-3

Part: PANEL — NONE (PNL L/E INBD RH) · airframe 43,327 hrs · 34,453 cycles

A MISS DERILLED HOLE WAS FOUND ON THE RH OUTBOARD LEADING EDGE ACESS PANEL #632EB. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 57-42-32-991-801, 29A (REV 38 DATED 9 JUL 2021). PANEL/LE INBD RH PANEL #632EB

Part: NONE — NONE (SLAT 2-1THRU 2-3) · airframe 43,327 hrs · 34,453 cycles

SLAT #2 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWERFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG.1, ITEM 45, 85, AND 105 (REV. 70 DATED 10 AUG 2021).

Part: NONE — NONE (FWD PASSENGER DR) · airframe 43,327 hrs · 34,453 cycles

THE PASSENGER DOOR INNER SKIN WAS FOUND WITH A CRACK. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-24-36, 51-21-16, 51-23-00. DEFECT LOCATION: FWD PASSENGER DOOR LOWER CORNER

Part: NONE — NONE (SIDE SEAL CARRIE) · airframe 43,327 hrs · 34,453 cycles

THE FORWARD AND AFT SEAL CARRIERS OF THE AFT SERVICE DOOR PLUG WAS FOUND TO HAVE (2) CRACKS. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 52-46-07 FIG. 52-46-07-991-801, ITEM 4 AND 5 (REV. 38 DATED JUL. 9, 2021 ). DEFECT LOCATION: SIDE SEAL CAREER, AFT SERVICE DOOR PLUG

Part: NONE — NONE (FS661+16&FS661+3) · airframe 43,327 hrs · 34,453 cycles

THE UPPER CAP OF THE CENTER FUSELAGE FLOOR BEAM WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-61-43-991-801, ITEM 2A (REV. 33 DATED JUN. 25, 2017). DEFECT LOCATION: FS 661+16-FS 661+32, LBL 9

Part: NONE — NONE (SLAT 3-1THRU3-2) · airframe 43,327 hrs · 34,453 cycles

SLAT #3 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWERFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG.10, ITEM 15, 90 (REV. 70 DATED 10 AUG 2021).

Part: NONE — NONE (RH WING SLAT TRA) · airframe 43,327 hrs · 34,453 cycles

THE RH WING SLAT #1 WERE FOUND TO HAVE CORROSION DAMAGE ON BOTH THE UPPER AND LOWER SURFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG. 01, ITEMS 45, 85, AND 105 (REV. 70 DATED 10 AUG 2021). DEFECT LOCATION: RH WING-SLAT TRACKS 1-1. 1-2. AND 1-3

Part: NONE — NONE (FS875-FS920 STR1) · airframe 43,327 hrs · 34,453 cycles

THE FUSELAGE RH SKIN PANEL WAS FOUND WITH MINOR CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-51-01-001-004-A02 ITEM 1, A, AND D (REV.38 DATED 9 JUL 2021) - DEFECT LOCATION: FS 875-FS 920 AND STGR 17R - 19R

Part: NONE — NONE (FS 1000- FS 1015) · airframe 43,327 hrs · 34,453 cycles

THE FUSELAGE SKIN LOWER PANEL WAS FOUND TO HAVE A PREVIOUS BLENDOUT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-61-01-001-003-A02, FIG. 53-61-01-991-806, ITEM 1 AND ITEM F (REV.38 DATED 9 JUL 2021 ). DEFECT LOCATION: FS 1000- FS 10L5 AND STRG 25R AND STRG 26R

Part: NONE — NONE (FS 913.00 -942.0) · airframe 43,327 hrs · 34,453 cycles

THE FUSELAGE LOWER SKIN PANEL WAS FOUND WITH MINOR CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-51-01-001-003-A02 ITEM 1A, D AND E (REV.38 DATED 9 JUL2021). DEFECT LOCATIONS: FS 913.00 -942.00. STGR 20R-STGR 20L

Part: NONE — NONE (FS 847+16- FS913) · airframe 43,327 hrs · 34,453 cycles

THE FUSELAGE LH SKIN PANEL WAS FOUND WITH MINOR CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-51-01-001-002-A02 ITEM 1, C, AND D (REV.38 DATED 9 JUL 2021). DEFECT LOCATION: FS 847+16-FS 913 AND STGR 17L-STGR 20L

Part: NONE — NONE (SLAT 1-1 THRU 1-) · airframe 43,327 hrs · 34,453 cycles

SLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWERFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG.1, ITEM 45, 85, AND 105 (REV. 70 DATED 10 AUG 2021).

Part: NONE — NONE (FS1069-FS193 STR) · airframe 43,327 hrs · 34,453 cycles

A CRACK WAS DISCOVERED ON THE SKIN PANEL. PERFORMED PERMANENT REPAIR IAW CR7/9 SRM 53-11-01-991-810, ITEM 1A (CRJ7/9 REV. 38 DATED JUL 9TH, 2021).

Part: NONE — NONE (RH WING SLAT TRA) · airframe 43,327 hrs · 34,453 cycles

THE RH WING SLAT #2 WERE FOUND TO HAVE CORROSION DAMAGE ON BOTH THE UPPER AND LOWER SURFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG. 05, ITEMS 15, 85, AND 105 (REV. 70 DATED 10 AUG 2021). DEFECT LOCATION: RH WING-SLAT TRACKS 2-1, 2-2, AND 2-3

Part: NONE — NONE (STGR 20L AT FS33) · airframe 43,327 hrs · 34,453 cycles

THE LH FUSELAGE SKIN PANEL WAS FOUND WITH DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-12-00, SRM 51-40-11-001-001.

Part: NONE — DENTED (FS280-310STGR17R) · airframe 43,327 hrs · 34,453 cycles

THE FUSELAGE LOWER SKIN PANEL WAS FOUND TO HAVE THREE PROTRUDING DENTS. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-01, FIG. 53-21-01-991-802, ITEM 1 (REV. 38 DATED 25 JUL. 2020).

Part: NONE — NONE (STGR 20L AT FS 3) · airframe 43,327 hrs · 34,453 cycles

THE LOWER FUSELAGE SKIN PANEL HAD A PREVIOUS REPAIR INSTALLED PER REO 690-53-21-989 THAT CONFLICTED WITH THE OPERATOR RECOMMENDED SERVICE BULETIN 670BA-53-057 THAT INVOLVES RELOCATING THE DRAIN HOLES FORWARD AND INSTALLING TWO SMALL DOUBLERS FOR THE NEW DRAIN TUBES. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-11-01-991-802-1.

Part: NONE — NONE (FS394 & STRG20L-) · airframe 43,327 hrs · 34,453 cycles

FUSELAGE LOWER SKIN PANEL AT FS394.00 AND STGR20L -STGR21L WAS FOUND TO HAVE A PREVIOUS BLENDOUT, PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-001-006-A02, FIGURE 53-21-01-991-807, ITEM 1, C, EA 79-2021-264.

Part: NONE — NONE (WS14.50 & WS 68.) · airframe 43,327 hrs · 34,453 cycles

LH MAIN LANDING GEAR HYDRAULIC INTERFACE IN THE MLG BAY BETWEEN WS 14.50 AND WS 68.00 WAS FOUND WITH MISSING MATERIAL. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 51-13-02, EA 20-2021-214.

Part: NONE — NONE (TRAILING EDGE/SS) · airframe 43,327 hrs · 34,453 cycles

L/H WING LEADING EDGE SLAT NO. 2 TRAILING EDGE WAS FOUND WITH GOUGE DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 51-13-02, EA 69-2021-200.

Part: NONE — NONE (FS349-364 STR22R) · airframe 43,327 hrs · 34,453 cycles

FUSELAGE SKIN PANEL BETWEEN FS 349 -FS 364, STR 22R -STR 24R WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-001-006-A02, "SKIN, LOWER PANEL FS333.00 TO FS477.40" -STRUCTURAL IDENTIFICATION ADN ALLOWABLE DAMAGE, EA 20-2021-207.

Part: NONE — NONE (TE/SS416.50&SS47) · airframe 43,327 hrs · 34,453 cycles

L/H WING LEADING EDGE SLAT NO. 3 TRAILING EDGE WAS FOUND WITH GOUGE DAMAGE. PERFORMED PERMANENT REPAIR JAW CRJ 700/900 SRM 51-13-02, EA 69-2021-201.

Part: NONE — NONE · airframe 43,077 hrs · 34,271 cycles

ROW 18 EMER CEILING FLOODLIGHT INOP. RELAMPED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,876 hrs · 33,192 cycles

EMER FLOODLIGHT ROW 6-7 INOP - RELAMPED OVHD EMER FLOODLIGHT.

Part: ACCELEROMETER — FAULTED (RT ENGINE) · airframe 42,801 hrs · 34,078 cycles

RH ENGINE VIBE 3.9 AT CRUISE. CREW REPORTS AT CRUISE FLIGHT, VIBES REACHED 3.9 AND WAS STILL CLIMBING. CREW SHUT DOWN RH ENGINE IN FLIGHT, BUT RESTARTED TO HAVE TWO GENS. THEY LEFT THE ENGINE AT IDLE AND VIBES WERE AT 1.4. CREW DECLARED EMERGENCY AND RTF. DFW MX REPLACED THE VIBRATION ACCELEROMETER AND PERFORMED FCF. FCF FAILED. AIRCRAFT STILL CURRENTLY OOS IN DFW.

Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 42,766 hrs · 34,056 cycles

AFT FA FLASHLIGHT INOP. REPLACED BATTERY

Part: SEAL — LEAKING (RT PNEUMATIC SYS) · airframe 42,462 hrs · 33,825 cycles

RTF DUE TO RH ENGINE BLEED WARNING. EMER DECLARED. MX REPLACED RH DUAL HEAT XCHANGER PERISEALS AND XBLEED DUCT. OP/LEAK CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,797 hrs · 33,361 cycles

ROW 13A/C MID LEVEL EXIT SIGN BULB INOP. RELAMPED.

Part: BATTERY — INOPERATIVE · airframe 41,738 hrs · 33,318 cycles

ALL EMERGENCY LIGHTS BATTERIES DRAINED- CHARGED BATTERIES

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 41,540 hrs · 33,198 cycles

FWD FA FLASHLITE WILL NOT CHARGE, PLACED ON MEL.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 41,108 hrs · 32,907 cycles

LT WING FWD OVERWING EMERGENCY LIGHT INOPERABLE. PLACED ON MEL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,831 hrs · 32,701 cycles

ROW 13A FLOOR EXIT SIGN INOPERABLE. RECHARGED #3 BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 40,831 hrs · 32,701 cycles

ROW 13F FLOOR EXIT SIGN INOPERABLE. RECHARED #3 BATTERY PACK

Part: PANEL — DETACHED (RT WING) · airframe 40,578 hrs · 32,515 cycles

RH WING MISSING PANEL UNDER SLATS, PANEL FOUND ON RUNWAY, REINSTALLED THE PANEL

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 40,460 hrs · 32,432 cycles

F/O EMER FLASHLIGHT RED LIGHT NO FLASH- REPLACED BATTERY

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,300 hrs · 32,321 cycles

OVHD EMER LIGHT AT ROW 18 INOP

Part: FLASHLIGHT — INOPERATIVE (FIRST OFFICER'S) · airframe 40,206 hrs · 32,245 cycles

FO FLASHLIGHT LED NOT FLASHING

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,713 hrs · 31,880 cycles

ROW 15 CEILING LVL EMER FLOOD LT INOP REPLACED BULB

Part: LIGHT — UNSECURE (EXIT SIGN) · airframe 38,887 hrs · 31,207 cycles

PAX DOOR EXIT SIGN LIGHTBULBS INOP. RESECURED BULB.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 37,658 hrs · 30,280 cycles

13A LOWER EMERGENCY SIGN BULB INOP. PLACED ON MEL.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 37,525 hrs · 30,177 cycles

SERVICE DOOR EMERGENCY LT BULB INOP. REPALCED BULB.

Part: PITOT SYSTEM — ERRATIC (ZONE 100) · airframe 37,352 hrs · 30,045 cycles

STBY/CA AIRSPEED IND ERRATIC/ZERO FOUND WATER IN P1 AND STBY SYSTEMS, REMOVED WATER

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 37,106 hrs · 29,846 cycles

FWD FA FLASHLIGHT INOP. PLACED ON MEL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 370,055 hrs · 29,771 cycles

ONE BULB INOP FLOOR EMER SIGN ROW 14. PLACED ON MEL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 37,005 hrs · 29,771 cycles

ONE BULB INOP FLOOR EMER SIGN ROW 13. PLACED ON MEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,842 hrs · 29,642 cycles

ROW 18 OH CEILING EMERG LT INOP. PLACED ON MEL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 36,623 hrs · 29,468 cycles

AFT FA FLASHLIGHT INOP. REPLACED BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,623 hrs · 29,468 cycles

ROW 1 OVHD EMER FLOOD LIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 36,623 hrs · 29,468 cycles

SERVICE DOOR EXIT SIGN 3 BULBS INOP. RELAMPED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,480 hrs · 29,350 cycles

THREE OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BULBS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,380 hrs · 29,269 cycles

CEILING OVERHEAD EMERGENCY LIGHT LAMP INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,380 hrs · 29,269 cycles

CEILING OVERHEAD EMERGENCY LIGHT LAMP AT ROW 1 WAS INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,380 hrs · 29,269 cycles

FWD ENTRY EXIT SIGN HAD ONE BULB INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,574 hrs · 28,656 cycles

ROW 19 OVHD EMERG FLOOD LIGHT INOP. PLACED ON MEL.

Part: STRINGER — CORRODED (BS 333-349) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

STRINGER 20R CORRODED BETWEEN BS 333 AND 349.

Part: FRAME — CRACKED (BS 333) · airframe 35,496 hrs · 28,591 cycles

BS 333 FRAME IS CRACKED BETWEEN STRINGERS 1R AND 2R.

Part: TRANSCOWL — CRACKED (THRUST REVERSER) · airframe 35,496 hrs · 28,591 cycles

LEFT HAND ENGINE UPPER TRANSCOWL HAS CRACK AT DOOR LATCH COAMING AND UPPER HAT CHANNEL MISSING.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

EXTERNAL SKIN IS CORRODED AT FS 280.00 AND STR 27.

Part: STRAP — CORRODED (FUSELAGE) · airframe 35,496 hrs · 28,591 cycles

CORROSION ON CIRCUMFERENTIAL JOINT AT FS 280.00 BETWEEN STR 23L AND 23R.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 35,496 hrs · 28,591 cycles

VERTICAL STABILIZER RT FWD DRAG ANGLE IS CRACKED.

Part: HINGE — GOUGED (PAX DOOR) · airframe 35,496 hrs · 28,591 cycles

PASSENGER DOOR HINGE (DOOR SIDE) 4 HINGE LUGS GOUGED. REPAIRED IAW REO 670-52-11-511, REV-E, DATED 2017-08-02.

Part: HINGE — GOUGED (FUSELAGE) · airframe 35,496 hrs · 28,591 cycles

PAX DOOR HINGE, FUSELAGE SIDE GOUGED ON LAST LUG. REPAIRED IAW REO 670-53-21-582 REV-F DATED 2017-08-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,496 hrs · 28,591 cycles

DENT IN FUSELAGE AT FS 485.00 STR 12L. REPAIRED FUSELAGE DENT IAW REO 690-53-31-373, REV-, DATED 2018-03-10.

Part: STRINGER — CRACKED (BS 280-295) · airframe 35,496 hrs · 28,591 cycles

PAX DOOR LINTEL STRINGER 3L IS CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

LEFT HAND SEAT TRACK, AT LBL 9, FS 847.00 & 48 - 985.00 CORRODED BEYOND REPAIRABLE LIMITS. INSTALLED NEW SERVICEABLE SEAT TRACK, IAW APPLICABLE SRM'S.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

STRINGER 21R CORRODED AT FS 320 TO FS 325.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

BS 333 FRAME IS CORRODED BETWEEN STRINGER 25 TO 27R.

Part: SEAT TRACK — CORRODED (BS 581-708) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

LEFT CABIN SEAT TRACK CORRODED, LBL 9, BS 581 TO 708.

Part: SEAT TRACK — CORRODED (BS 379-485) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

LEFT CABIN SEAT TRACK, LBL 9, BS 379 TO 485 IS CORRODED.

Part: DOUBLER — CHAFED (BS 927) · airframe 35,496 hrs · 28,591 cycles

CHAFED LOWER FUSELAGE DOUBLER AT BS 927, STRINGER 27 ON A PREVIOUSLY REPAIRED AREA.

Part: BULKHEAD WEB — CORRODED (BS 280) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

LT AND RT BS 280 BULKHEAD LOWER WEB CORRODED AT LBL 12 AND RBL 39.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

CORROSION ON INTERCOSTAL AT BS 364 BETWEEN STRINGERS 26 AND 27R.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

CORROSION ON STR 26R AT FS 280.00.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

STRINGER 27 CORRODED AT FS 280.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

STRINGER 25R CORRODED AROUND FASTENERS BETWEEN FS 280.00 AND FS 295.00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

LT NR 2 SEAT TRACK AT LBL9 IS CORRODED BETWEEN FS 485.00 AND FS 613.00.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

RT FLOOR SILL IS CORRODED AT FS 349.00.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

PASSENGER DOOR SILL ANGLE IS CORRODED BETWEEN FS 310 AND FS 349.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

INTERCOSTAL CORRODED UNDER SERVICE DOOR AT STRINGER 20R BETWEEN FS 319.70 AND FS 349.00.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,496 hrs · 28,591 cycles

CORROSION ON FRAME 349.00 FS STR 25RBL.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 35,496 hrs · 28,591 cycles

RT COCKPIT FLOORBEAM HAS 1" CRACK IN RADIUS ON AFT SIDE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,172 hrs · 28,358 cycles

CEILING EMERGENCY FLOOD LIGHT ROW 19/21 INOP. RELAMPED.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 34,457 hrs · 27,776 cycles

FWD FA FLASHLIGHT INOPERATIVE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,285 hrs · 246 cycles

FWD FA FLASHLIGHT INOP. R2 BATTERY.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 34,141 hrs · 27,517 cycles

AFT FA FLASHLIGHT INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,078 hrs · 27,466 cycles

ROW 6 CEILING EMERGENCY FLOODLIGHT INOPERATIVE. REPLACED THE LAMPS.

Part: UNKNOWN — MALFUNCTIONED (ELEVATOR) · airframe 33,863 hrs · 27,289 cycles

ELEVATOR SPLIT INDICATION IN FLIGHT.

Part: LIGHT — INOPERATIVE (ROW 8) · airframe 33,699 hrs · 27,142 cycles

ROW 8 CEILING LEVEL EMERGENCY FLOODLIGHT INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,235 hrs · 26,003 cycles

EMERGENCY EXIT SIGN ROW 13 HAD ONE BULB INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,322 hrs · 23,412 cycles

ROW 14L SIDE EMERGENCY SIGN ONE BULB INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 25,653 hrs · 419,151 cycles

FWD F/A FLASHLIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,387 hrs · 25,345 cycles

LT AFT EXIT EMERGENCY LIGHT INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 31,292 hrs · 25,268 cycles

FWD F/A FLASHLIGHT INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 31,292 hrs · 25,268 cycles

AFT F/A FLASHLIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (ROW 11) · airframe 31,139 hrs · 25,151 cycles

EMERGENCY CEILING FLOOD LIGHT AT ROW 11 INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 308,885 hrs · 24,995 cycles

AFT F/A FLASHLIGHT INOPERATIVE.

Part: BATTERY PACK — INOPERATIVE (MEGAPHONE) · airframe 30,606 hrs · 24,738 cycles

MEGAPHONE INOPERATIVE. R & R BATTERIES.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 30,534 hrs · 24,687 cycles

AFT F/A FLASHLIGHT INOPERATIVE.

Part: SKIN — CHAFED (BS 913) · airframe 30,488 hrs · 24,655 cycles

TWO CHAFES AT BS 913, STRINGER 27 ON FUSELAGE SKIN.

Part: FRAME — CRACKED (BS 235) · airframe 30,488 hrs · 24,655 cycles

FS 235 LT FRAME CRACKED.

Part: ANGLE — OUT OF LIMITS (BS 202) · airframe 30,488 hrs · 24,655 cycles

LEFT CAP ANGLE AT BS 202 HAS MULTIPLE OVERSIZED HOLES.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · corrosion level 2 · airframe 30,488 hrs · 24,655 cycles

RIGHT FLOOR SUPPORT IS CORRODED BETWEEN FS 280 AND 319.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 30,488 hrs · 24,655 cycles

LEFT FORWARD VERTICAL STABILIZER DRAG ANGLE IS CRACKED APPROXIMATELY 2.5" LONG.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,311 hrs · 24,522 cycles

ROW 9 CEILING LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LAMP IN THE FLOOD LIGHT ASSY.

Part: SENSOR — MALFUNCTIONED (ELEVATOR) · airframe 30,262 hrs · 24,480 cycles

ELEVATOR SPLIT CAUTION, EMERGENCY DECLARED, DIVERTED. MX FOUND IT TO BE INDICATION DUE TO POSITION CONTROL SENSOR, AOG FOR CONTROL SENSOR.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 30,211 hrs · 24,444 cycles

ALL EMERGENCY LIGHTS INOPERATIVE. MX CHARGED THE EMERGENCY BATTERIES.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,110 hrs · 24,362 cycles

SERVICE DOOR EMERGENCY EXIT SIGN INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,104 hrs · 24,359 cycles

SERVICE DOOR EMERGENCY FLOOR LEVEL FLOOD LIGHT ONE BULB INOPERATIVE. NO BULBS INOPERATIVE, OPERATIONAL CHECKED GOOD.

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 30,104 hrs · 24,359 cycles

SERVICE DOOR EMERGENCY EXIT SIGN INOPERATIVE. SECURED WIRING TO SIGN.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,262 hrs · 370,521 cycles

14DF EMERGENCY EXIT SIGN, THREE BULBS INOPERATIVE. REPLACED BULBS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,735 hrs · 24,067 cycles

3 CEILING EMERGENCY FLOOD LIGHTS INOPERATIVE. REPLACED LIGHT BULBS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,671 hrs · 24,020 cycles

MID CABIN CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. FOUND BULB INOPERATIVE, REPLACED.

Part: ACM — FAILED (NR 2) · airframe 29,511 hrs · 23,901 cycles

SMOKE IN AFT CABIN ON GROUND. NR 2 ACM FAILED.

Part: BATTERY PACK — INOPERATIVE (FWD FLASHLIGHT) · airframe 29,030 hrs · 23,539 cycles

FWD F/A FLASHLIGHT INOPERATIVE. REPLACED THE BATTERY.

Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 29,010 hrs · 23,525 cycles

GEAR DISAGREE, EMERGENCY DECLARED RETURNED TO FIELD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 28,906 hrs · 23,548 cycles

F/O'S FLASHLIGHT INOPERATIVE. R & R THE BATTERIES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,280 hrs · 22,976 cycles

ROW 14A EXIT SIGN HAS ONE LAMP INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,033 hrs · 22,758 cycles

F/O'S FLASHLIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 28,009 hrs · 22,770 cycles

ROW 18, OVERHEAD EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,949 hrs · 22,722 cycles

PAX DOOR, FLOOR LEVEL EMERGENCY LIGHT HAS ONE BULB OUT.

Part: LIGHT — INOPERATIVE (ROW 9) · airframe 27,864 hrs · 24,192 cycles

CEILING FLOOD LIGHT INOPERATIVE AT ROW 9.

Part: LENS — CRAZED (EMERGENCY LIGHT) · airframe 27,607 hrs · 22,413 cycles

FOUND LT AFT OVERWING EMERGENCY EXIT LENS CRAZED. R & R LENS.

Part: LENS — CRAZED (EMERGENCY LIGHT) · airframe 27,607 hrs · 22,413 cycles

FOUND RT FWD OVERWING EMERGENCY EXIT LENS CRAZED. R & R LENS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,469 hrs · 22,279 cycles

14AC LOW EMERGENCY EXIT LIGHT ONE BULB INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,028 hrs · 21,858 cycles

PAX DOOR FLOODLIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,028 hrs · 21,858 cycles

SERVICE DOOR FLOODLIGHT INOPERATIVE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,015 hrs · 21,842 cycles

ROW 13 ABCD EMERGENCY EXIT SIGNS WOULD NOT ILLUMINATE. R & R BATTERY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,957 hrs · 21,788 cycles

ROW 13A FLOOR LEVEL EXIT SIGN INOPERATIVE. RERACKED NR 3 ESPU PACK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,957 hrs · 21,788 cycles

ROW 13F FLOOR LEVEL EXIT SIGN INOPERATIVE. RERACKED NR 3 ESPU PACK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,311 hrs · 21,181 cycles

SERVICE DOOR EXIT LIGHT ONE BULB INOPERATIVE. REPLACED BULB.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 26,005 hrs · 20,891 cycles

AFT F/A FLASHLIGHT INOPERATIVE. REPLACED BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,511 hrs · 20,720 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. R & R AFT CEILING EMERGENCY LIGHT, OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 25,700 hrs · 220,612 cycles

FWD FA FLASHLIGHT INOPERATIVE. MX R & R BATTERIES, OPS NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,573 hrs · 20,496 cycles

EMERGENCY LIGHT 13AC INOPERATIVE. REPLACED BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,573 hrs · 20,496 cycles

LEFT ROW 13 EXIT SIGN ONE BULB INOPERATIVE. REPLACED BULB.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,573 hrs · 20,496 cycles

RT ROW 13 EXIT SIGN 1 BULB INOPERATIVE. REPLACED BULB.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 25,534 hrs · 20,458 cycles

MEGAPHONE INOPERATIVE. MX PERFORMED AN OPS CHECK. OPS CHECKED NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,498 hrs · 20,422 cycles

SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BULB.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 25,493 hrs · 20,417 cycles

FWD LT OVERWING EMERGENCY LIGHT INOPERATIVE.

Part: BULKHEAD — CORRODED (ZONE 200) · corrosion level 2 · airframe 25,488 hrs · 20,413 cycles

BS 280, BULKHEAD CORRODED LT AND RT SIDES BETWEEN LBL/RBL 11.0 AND LBL/RBL 47.0.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 3 · airframe 25,488 hrs · 20,413 cycles

BS 280 FLOORBEAM IS CORRODED IN NUMEROUS AREAS ON TOP SURFACE.

Part: FLOORBEAM — DAMAGED (ZONE 100) · airframe 25,488 hrs · 20,413 cycles

AFTER REMOVAL OF FS 280 FLOORBEAM AND LOWER WEB FOUND FOUR ELONGATED HOLES.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,397 hrs · 20,323 cycles

FWD F/A'S FLASHLIGHT BATTERY DEAD UPON PRE-FLIGHT INSPECTION. FLASHLIGHT WAS PLACED ON MEL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,246 hrs · 20,201 cycles

CEILING EMERGENCY FLOOD LIGHT INOPERATIVE ROW 18. REPLACED BULB.

Part: PIN — GALLED (HORIZ STAB) · airframe 24,539 hrs · 19,619 cycles

GALLING PREVIOUSLY FOUND ON HORIZONTAL STAB PIVOT PIN.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 24,226 hrs · 19,353 cycles

NR 2 BRAKE APPEARS TO BE INEFFECTIVE. MX TROUBLESHOOTING.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,168 hrs · 19,301 cycles

FORWARD FLIGHT ATTENDANT'S FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT.

Part: SENSOR — DIRTY (EMERGENCY EXIT) · airframe 23,864 hrs · 19,047 cycles

RIGHT FORWARD EMERGENCY EXIT DOOR INTERMITTENT CAUTION. MX CLEANED DOOR SENSOR NO FURTHER CAUTION INDICATION.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 23,822 hrs · 19,016 cycles

F/O'S FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,793 hrs · 18,985 cycles

ROW 3 CEILING LEVEL EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,563 hrs · 18,787 cycles

EMERGENCY O/H LIGHT AT ROW 3 INOP; MX IS TROUBLESHOOTING. RELAMPED EMERGENCY LIGHT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 23,526 hrs · 18,761 cycles

F/O'S FLASHLIGHT INOP; PLACED ON MEL. REMOVED AND REPLACED FLASHLIGHT BATTERIES.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,389 hrs · 18,654 cycles

ALL EMERGENCY EXIT LIGHTS INOPERATIVE. EMERGENCY EXIT LIGHT SWITCH FOUND IN THE "ON" POSITION. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT BATTERY PACKS.

Part: LIGHT — OUT OF POSITION (EXTERIOR) · airframe 23,241 hrs · 18,522 cycles

FWD RT EXT EMERGENCY EXIT LIGHT INCORRECT POSITION. CORRECTED FWD RT EXT EMERGENCY EXIT LIGHT.

Part: CONTROL VALVE — INOPERATIVE (BRAKE SYSTEM) · airframe 22,565 hrs · 17,991 cycles

FLT 2697, REPORTED NR 2 BRAKE APPEARED TO BE INOPERATIVE AND READING ZERO ON THE BRAKE TEMP MONITOR. CREW ALSO ADVISED THAT THE BRAKE WAS COLD TO THE TOUCH. R & R ANTI-SKID CONTROL VALVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,182 hrs · 17,694 cycles

LEFT FWD EMER EXIT LIGHT OUTBOARD BULB OUT. RELAMPED EMERGENCY LIGHT.

Part: PLACARD — WORN (DOOR) · airframe 22,127 hrs · 17,649 cycles

DOOR EXIT PLACARD WORN. R2 PLACARD.

Part: PLACARD — WORN (PAX DOOR) · airframe 22,127 hrs · 17,649 cycles

PAX DOOR EMERGENCY RED ARROW IS WORN. R2 PLACARD.

Part: PLACARD — WORN (PAX DOOR) · airframe 22,127 hrs · 17,649 cycles

PAX DOOR EMERGENCY RED STRIPE IS WORN. R2 PLACARD.

Part: PLACARD — WORN (PAX DOOR) · airframe 22,127 hrs · 17,649 cycles

PAX DOOR OPEN PLACARD WORN. R2 PLACARD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,936 hrs · 17,514 cycles

ASH FLIGHT 2731 REPORTED AN INOPERATIVE CABIN FLOOD LIGHT UPON TESTING IT. THE LIGHT WAS PLACED ON MEL.

Part: PLACARD — DAMAGED (ENTRY DOOR) · airframe 21,592 hrs · 17,256 cycles

MAIN ENTRY DOOR TO OPN LEFT HANDLE PUSH PLCD DAMAGED. REMOVED AND REPLACED MAIN ENTRY DOOR "TO OPEN LIFT HANDLE" PLCD.

Part: PLACARD — LOOSE (ENTRY DOOR) · airframe 21,592 hrs · 17,256 cycles

MAIN ENTRY DOOR ARROW AT OPN PLCD NEED SECURED. SECURED MAIN ENTRY DOOR ARROW AT OPN PLCD.

Part: PROXIMITY SWITCH — OUT OF ADJUST (EMERGENCY EXIT) · airframe 21,488 hrs · 17,172 cycles

RT AFT EMERGENCY EXIT CAUTION INT ON TAXI. ADJUST PROX SWITCH.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,185 hrs · 16,901 cycles

ROW 12 CELING FLOOD LIGHT INOP. REPLACED LAMP.

Part: BATTERY — DEFECTIVE (FLASHLIGHT) · airframe 21,032 hrs · 16,768 cycles

AFT F/A'S FLASHLIGHT WILL NOT CHARGE. R2 BATTERIES.

Part: BATTERY — DEFECTIVE (FLASHLIGHT) · airframe 21,032 hrs · 16,768 cycles

FWD F/A'S FLASHLIGHT WILL NOT CHARGE. R2 BATTERIES.

Part: OXYGEN BOTTLE — EMPTY (CABIN) · airframe 20,982 hrs · 16,723 cycles

AFT PORT O2 BOTTLE EMPTY. R2 PORTABLE O2 BOTTLE.

Part: FLAP — UNWANTED DEPLOY (WING) · airframe 20,982 hrs · 16,723 cycles

INADV FLAP DEPLOY TO 1 DEGREE AT 260. INSPECTED FLAPS/SLATS NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 20,940 hrs · 16,681 cycles

RT EMERGENCY DOOR LWR EXIT SIGN INOP (INTERIOR). RELAMPED EMERGENCY EXIT SIGN.

Part: PROXIMITY SENSOR — FAULTY (PAX DOOR) · airframe 20,925 hrs · 16,669 cycles

PAX DOOR OUTER HANDLE CAUTION INTERM. MX WORKING. R2 PROX SENSOR PX107 AND SPLICES 528

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,813 hrs · 16,571 cycles

ROW 7 CEILING EMER LIGHT OUT. RELAMP EMERGENCY LIGHT.

Part: SHAFT — UNSECURE (SERVICE DOOR) · airframe 16,512 hrs · 227,987 cycles

SERVICE DOOR W/N CLOSE. RE-SECURED ROLLER ARM SHAFT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,721 hrs · 16,503 cycles

CEILING EMERGENCY FLOOD LIGHT 4TH AFT INOP. RELAMPED EMERGENCY LIGHT.

Part: DOOR — OUT OF ADJUST (OVERWING EXIT) · airframe 20,698 hrs · 16,481 cycles

RT AFT OVERWING EXIT CAUTION. ADJUSTED DOOR AND PERFORMED PRESSURE CHECK OPS CHECK GOOD AND NO FURTHER FAULTS NOTED.

Part: ENGINE — VIBRATION (LEFT) · airframe 20,648 hrs · 16,431 cycles

LEFT ENG VIBE 2.0 DURING CLIMB AT FL 360; PERFORMED ENGINE BLADE INSPECTION AND BLADE SHAKE OPS GOOD ENGINE RUNS NORMAL. IDLE .03 / HIGH POWER .07.

Part: SENSOR — DIRTY (EMERGENCY EXIT) · airframe 20,598 hrs · 16,389 cycles

RIGHT AFT EMERGENCY DOOR CAUTION. CLEANED SENSOR.

Part: FIXTURE — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,544 hrs · 16,348 cycles

GALLEY LOWER EXIT LIGHT MISSING BULB SOCKET. R & R LIGHT FIXTURE.

Part: CONNECTOR — DEFECTIVE (BLEED AIR SYS) · airframe 20,321 hrs · 16,162 cycles

LEFT BLEED AIR DUCT WARN MSG - DIVERT. R2 CONNECTOR MT203P1 & INSPECT FOR LEAKS, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,303 hrs · 16,142 cycles

EXTERIOR EMERGENCY LIGHT AT PAX DOOR INOP. RE-LAMPED EMERGENCY LIGHT.

Part: SEAL — DEFECTIVE (BLEED AIR SYS) · airframe 20,279 hrs · 16,120 cycles

RTF - LT BLEED DUCT WARNING. R2 EURO SEALS BY LEFT PACK OPS & LEAK CHECKED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,265 hrs · 16,106 cycles

CAPTAINS EMERGENCY FLASHLIGHT INOP. R2 BATTERY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,274 hrs · 16,115 cycles

LT FWD EMERGENCY DOOR LIGHT HAS 1 BULB OUT. RELAMPED EMERGENCY LIGHT.

Part: SEAL — MISSING (EMERGENCY EXIT) · airframe 20,237 hrs · 16,081 cycles

LEFT FWD EMERGENCY DOOR SEAL MISSING. ADJUSTED THE SEAL.

Part: COVER — MISSING (CABIN) · airframe 20,186 hrs · 16,035 cycles

FWD EMERGENCY FLOOR LIGHT MISSING COVER. R2 FLOOD LIGHT COVER.

Part: COVER — MISSING (CABIN) · airframe 20,147 hrs · 16,006 cycles

FWD CABIN EMERGENCY EXIT FLOOR LEVEL FLOOD LIGHT MISSING COVER. R2 FLOOD LIGHT COVER.

Part: FIRE LOOP — SHORTED (LT ENGINE) · airframe 20,140 hrs · 15,998 cycles

FIRE SYS FAULT STATUS MESSAGE. MX WORKING MSG FLAGS L ENG FIRE LOOP-B SHORT CIRCUIT. R & R ENGINE FIRE HARNESS LINK ASSY BETWEEN ENGINE LOOP & JETPIPE LOOP.

Part: LANYARD — BROKEN (PAX DOOR) · airframe 20,122 hrs · 15,979 cycles

HAND RAIL PIN LANYARD BROKEN. R2 HANDRAIL PIN LANYARD ASSY.

Part: PROXIMITY SENSOR — OUT OF ADJUST (E&E DOOR) · airframe 20,102 hrs · 15,962 cycles

AVIONICS DOOR CAUTION IN FLT. ADJUSTED PX41.

Part: METERING VALVE — MALFUNCTIONED (BRAKE SYSTEM) · airframe 20,092 hrs · 15,956 cycles

BTMS 2 READING 7 AFTER LANDING. R2 NR 3 SYS BRAKE METERING VALVE.

Part: PROXIMITY SENSOR — FAULTY (E&E DOOR) · airframe 20,092 hrs · 15,956 cycles

AVIONICS DOOR CAUTION ON T/O ROLL. MX WORKING. R2 PX41 PROX SENSOR.

Part: BRAKE — MALFUNCTIONED (MLG) · airframe 20,092 hrs · 15,956 cycles

BTMS 2 AT 10 AND SMOKING DURING TAXI. R2 BRAKE AND TEMP SENSOR.

Part: CONNECTOR — DIRTY (BRAKE) · airframe 20,080 hrs · 15,942 cycles

NR 3 BTMS HIGH AT 7 REST AT 4 OR LESS. CLEANED BRAKE TEMP SENSOR CONNECTOR.

Part: SENSOR — FAULTY (NR 3 BTMS) · airframe 20,069 hrs · 15,930 cycles

NR 3 BTMS ERRONEOUS INDICATION. R2 NR 3 BRAKE TEMP SENSOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,004 hrs · 15,868 cycles

ROW 12 EMER FLOOD INOP. RELAMPED EMERGENCY LIGHT.

Part: SWITCH — OUT OF RIG (PARKING BRAKE) · airframe 19,949 hrs · 15,827 cycles

ANTI-SKID INBD CAUT MSG; FLAGGING PARK BRAKE SOV AND PARK BRAKE PRESSURE SWITCH. MX TO CHECK RIGGING OR PARKING BRAKE MICRO SWITCH TO SEE IF IT GOT MISADJUSTED DURING METERING VALVE REPLACEMENT. MX T/S THE PROBLEM TO PARK BRAKE MICRO SWITCH OUT OF RIG. ADJUSTED BUT THE LOCKING RING IS MISSING IN THE MICRO SWITCH. R2 PARKING BRAKE MICRO SWITCH LOCKING RING.

Part: VALVE — MALFUNCTIONED (BRAKE) · airframe 19,945 hrs · 15,824 cycles

NR 1 BRAKE DRAGGING IND 9 ON LANDING. R&R NR 2 BRAKE METERING VALVE.

Part: CABLE — FRAYED (PAX DOOR) · airframe 19,945 hrs · 15,824 cycles

PAX DOOR RETRACT CABLE FRAYED. R2 CABLE.

Part: QUICK DISCONNECT — UNSECURE (NR 1 BRAKE) · airframe 19,945 hrs · 15,824 cycles

NR 1 BRAKE POSS DRAGGING, LT TEMPS 6/2. RE-SECURED QD AND BLED NR 1 & 2 BRAKES, PERFORMED TAXI.

Part: BRAKE — MALFUNCTIONED (NR 1) · airframe 19,945 hrs · 15,824 cycles

BRAKE TEMP 1 INDICATES 8 & DRAGGING. R2 NR 1 BRAKE, TAXI.

Part: QUICK DISCONNECT — NOT SEATED (NR 1 BRAKE) · airframe 19,941 hrs · 15,821 cycles

NUM 1 BRAKE STICKING. CLEANED AND RESEATED QD.

Part: ESCAPE HATCH — OUT OF POSITION (AFT) · airframe 19,752 hrs · 15,657 cycles

RT AFT EMERGENCY HATCH CAUTION MSG. MX REMOVED AND RE-INSTALLED DOOR. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,696 hrs · 15,609 cycles

AFT F/A FLASHLIGHT INOP. MX REPLACED BATTERY.

Part: SENSOR — MALFUNCTIONED (EMERGENCY EXIT) · airframe 19,685 hrs · 15,598 cycles

RT AFT EMERGENCY DOOR CAUTION. R&R SENSOR LEVER FOR PX12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,685 hrs · 15,598 cycles

FLOOR SUPPORT ANGLE AT STA 295 RT SIDE IS CORRODED. REPAIRED FLOOR SUPPORT ANGLE AT FS 295 STR 17 R IAW CRJ 900 SRM 51-42-06.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,685 hrs · 15,598 cycles

STR 25R CORRODED FS 333-295. REMOVED AND REPLACED STR 25R FS 280-333 IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,685 hrs · 15,598 cycles

INTERCOSTAL BELOW SERVICE DOOR FOUND STR 20R CORRODED. REMOVED AND REPLACED STR 20R IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: STAND OFF — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,685 hrs · 15,598 cycles

LWR FUSELAGE TUBING STAND OFFS AT FS 333 AND STR 25R CORRODED. REMOVED AND REPLACED 2 EA STAND OFF AT FS 303 AND STR 25R IAW CRJ 900 SRM 51-42-13 AND 51-42-06.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,685 hrs · 15,598 cycles

INTERNAL FWD JACK FITTING LT AND RT SUPPORTS CORRODED. REMOVED AND REPLACED LT AND RT INTERNAL FWD JACK FITTINGS IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,685 hrs · 15,598 cycles

FLOOR SUPPORT ANGLE AT SERVICE DOOR CORRODED AT NUT PLATE. REMOVED AND REPLACED FLOOR SUPPORT AT SERVICE DOOR IAW CRJ 900 SRM 51-42-06.

Part: STRUCTURE — CRACKED (TRANS COWL) · airframe 19,685 hrs · 15,598 cycles

1 UPPER TRANS COWL LATCH DOOR COAMING IS CRACKED. REMOVED AND REPLACED 1 UPPER TRANS COWL LATCH DOOR COAMING IAW CRJ 900 SRM 51-42-06 AND 51-42-10.

Part: SKIN — DENTED (FUSELAGE) · airframe 19,685 hrs · 15,598 cycles

FUSELAGE SKIN HAS A DENT AT FS 461 JUST BELOW STR 20R. REPAIRED FUSELAGE SKIN AT FS 461 BELOW STR 19R - 20R IAW RO CRJ9-53-0611.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,685 hrs · 15,598 cycles

INTERCOSTAL CORRODED FS 333-349 STR 20R BELOW SERVICE DOOR. REMOVED AND REPLACED INTERCOSTAL IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,685 hrs · 15,598 cycles

STR 25R AT FS 333 CORRODED. REMOVED AND REPLACED STR 25R SPLICE AT FS 333 IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,685 hrs · 15,598 cycles

LONGERON AT STR 25R CORRODED FS 333-349. REMOVED AND REPLACED LONGERON AT STR 25R FR FS 333-364 IAW CRJ SRM 51-42-06 AND 51-42-21.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,685 hrs · 15,598 cycles

STR 18R CORRODED FR FS 280-310. REMOVED AND REPLACED STR 18R IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,685 hrs · 15,598 cycles

STR 21R CORRODED FS 319-349. REMOVED AND REPLACED STR 21R IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: BAFFLE — CRACKED (THRUST REVERSER) · airframe 19,685 hrs · 15,598 cycles

1 ENG LWR TRANSCOWL HAS A CRACKED BAFFLE. REMOVED AND REPLACED BAFFLE ON 1 ENG LWR TRANSCOWL IAW CRJ 900 SRM 51-42-06 AND 51-42-07.

Part: FLOOR SKIN — CRACKED (FUSELAGE) · airframe 19,685 hrs · 15,598 cycles

EQUIP BAY LT AT FS 193.00 FLOOR CRACKED. REPAIRED FWD EQUIP BAY LT FS 193.00 FLOOR IAW RO CRJ9-53-0595.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,598 cycles

STR 26R SPLICE CORRODED AT FS 333. REMOVED AND REPLACED SPLICE AT STR 26R FS 333 IAW CRJ-900 SRM 51-42-06.

Part: STRAP — CRACKED (FUSELAGE) · airframe 19,685 hrs · 15,598 cycles

AFT WING TO BODY FUSELAGE CTR ATTACH STRAP IS CRACKED. FABRICATED CTR ATTACH STRAP IAW CRJ 900 SRM 51-40-11 AND 51-42-13 AND 51-42-06.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,685 hrs · 15,598 cycles

STR 26R CORRODED AT FS 349. REMOVED AND REPLACED STR 26R AT FS 349 IAW CRJ-900 SRM 51-42-06.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,598 cycles

STR 26R CORRODED FS 333-310. REMOVED AND REPLACED STR 26R FS 333-310 IAW CRJ -900 51-42-06.

Part: STAND OFF — CRACKED (THRUST REVERSER) · airframe 19,685 hrs · 15,598 cycles

RT TRANSCOWL I/B STANDOFF IS CRACKED. REMOVED AND REPLACED RT UPPER TRANSCOWL I/B STANDOFF IAW CRJ-900 SRM 51-42-14 AND 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,685 hrs · 15,598 cycles

RT FLOOR SEAT TRACK IS CORRDED AT STA 477-669. REMOVED AND REPLACED RT SEAT TRACK IAW CRJ 900 AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,684 hrs · 15,598 cycles

RT FLOOR SEAT TRACK IS CORRDED AT STA 280-477. REMOVED AND REPLACED SEAT TRACK AT STA 280-477 RBL 9 IAW CRJ 900 AMM 53-01-11.

Part: O-RING — LEAKING (APU) · airframe 19,603 hrs · 15,539 cycles

APU LEAKING FUEL. MX R2 FUEL FILTER BOWL O-RING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,409 hrs · 15,345 cycles

NR 3 CEILING EMERGENCY LIGHT INOP. MX RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 19,335 hrs · 15,280 cycles

NR 1 BRAKE INOP. MX VISUALLY INSP BRAKE, NO DEFECTS. PERFORMED OPS CHECK, OPS CHECK GOOD.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 19,331 hrs · 15,278 cycles

NR 1 BRAKE INOPERATIVE. PERFORMED TAXI CHECKS, OPS GOOD, BTMS INDICATION NORMAL.

Part: PROXIMITY SENSOR — DEFECTIVE (ENTRY DOOR) · airframe 19,312 hrs · 15,255 cycles

PAX DOOR HANDLE CAUTION IN FLIGHT. MX R2 PX 107.

Part: ACCUMULATOR — LOW (BRAKE SYSTEM) · airframe 19,249 hrs · 15,194 cycles

LEFT BRAKES SOFT ON LANDING, GOOD ON TAXI. MX SERVICED BRAKE ACCUMULATOR, OP CHECK GOOD.

Part: QUICK DISCONNECT — BROKEN (NR 2 BRAKE) · airframe 19,256 hrs · 15,201 cycles

NR 2 BRAKE LINE QD BROKEN. MX REPLACED THE NR 2 BRAKE LINE AND BLED BRAKES.

Part: LINE — OUT OF LIMITS (NR 3 BRAKE) · airframe 19,256 hrs · 15,201 cycles

LT BRAKES VERY SOFT ON LANDING. MX REPLACED THE NR 3 BRAKE LINE AND BLED BRAKES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,211 hrs · 15,160 cycles

ROW 7 EMERGENCY FLOOD LIGHT INOP. MX RELAMPED.

Part: LENS — MISSING (CABIN) · airframe 19,211 hrs · 15,160 cycles

F/A'S CNTR ISL EMERGENCY CALL LIGHT LENS MISSING. MX FOUND AND RE-INSTALLED LENS.

Part: WARNING SYSTEM — MALFUNCTIONED (CABIN DOOR) · airframe 19,192 hrs · 15,144 cycles

MAIN CABIN DOOR WARNING ON GROUND. MX REMOVED AND REPLACED PX101, OPS NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 19,150 hrs · 15,112 cycles

PAX DOOR TO OPEN PLACARD DAMAGED STILL LEGIBLE. MX REPLACED PLACARD.

Part: PLACARD — DAMAGED (CABIN) · airframe 19,150 hrs · 15,112 cycles

MED EXIT PLACARD DAMAGED. MX REMOVED AND REPLACED MED EXIT PLACARD NO OTHER DEFECTS NOTED.

Part: PLACARD — UNKNOWN (CABIN) · airframe 19,150 hrs · 15,112 cycles

PAX DOOR OPEN PLCD. MX REPLACED PLACARD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 19,131 hrs · 15,096 cycles

CAPT FLASHLIGHT LED NOT FLASHING. MX REPLACED FLASHLIGHT.

Part: SENSOR — INTERMITTENT (CABIN DOOR) · airframe 19,088 hrs · 15,059 cycles

MAIN CABIN DOOR HANDLE SENSOR INTERMITTENT. MX OPS CHECK DOOR, NO DEFECT NOTED.

Part: LENS — MISSING (CABIN) · airframe 18,804 hrs · 14,825 cycles

RT FWD EXT EMERGENCY EXIT LIGHT COVER MISSING. MX REPLACED THE LENS.

Part: SENSOR — DIRTY (EMERGENCY EXIT) · airframe 18,767 hrs · 14,806 cycles

RT FWD EMERGENCY DOOR CAUTION INTERMITTENT [ON] GROUND (UNKNOWN IF IN MOTION OR AT GATE). MX CLEANED SENSOR.

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 18,679 hrs · 14,735 cycles

EXCESSIVE ROLL 45 DEGREES UNCOMMANDED [AFTER] T/O. MX REMOVED AND REPLACED AIL/RUD TRIM CTL PNL.

Part: YAW DAMPER — MALFUNCTIONED (RUDDER) · airframe 18,657 hrs · 14,717 cycles

EXCESSIVE RUDDER BUMP IN CRUISE FLT. MX R2 YAW DAMP ACTUATOR NR 1.

Part: CIRCUIT CARD — FAULTY (E&E BAY) · airframe 18,657 hrs · 14,717 cycles

RUDDER MOVING LT AND RT W/AP OFF. MX REMOVED AND REPLACED BOTH HIRF CARDS. LIGHT/HIRF PROTECTION: P/N 822-0287-201; S/N 13HRD. LIGHT/HIRF PROTECTION: P/N 822-0332-201; S/N 13LHX.

Part: COMPUTER — MALFUNCTIONED (NR 1) · airframe 18,670 hrs · 14,724 cycles

UNCOMMANDED RUDDER MOVEMENT IN FLT. MX REPLACED FCC 1.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 18,666 hrs · 14,717 cycles

RT PACK FAIL SMOKE. R2 ACM.

Part: UNKNOWN — SMOKE (COCKPIT & CABIN) · airframe 18,666 hrs · 14,717 cycles

SMOKE IN CABIN AND COCKPIT ON FINAL. RAN ENGINES, RAN PACKS, CANNOT DUPLICATE.

Part: UNKNOWN — SMOKE (CABIN & COCKPIT) · airframe 18,666 hrs · 14,717 cycles

SMOKE IN CABIN AND COCKPIT. PERFORMED OPS CHECK OF BLEED SYS ENGINE AND PACKS OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,630 hrs · 14,680 cycles

FWD EMERGENCY LIGHT RIGHT SIDE INOP. REMOVED AND REPLACED EMERGENCY LIGHT.

Part: LENS — MISSING (CABIN) · airframe 18,530 hrs · 14,591 cycles

SERVICE DOOR EMERGENCY EXIT SIGN LENS MISSING. MX REPLACED LENS.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 18,244 hrs · 14,329 cycles

CAPTAIN’S FLASHLIGHT LED NOT FLASHING. R & R BATTERY.

Part: LENS — MISSING (CABIN) · airframe 18,211 hrs · 14,305 cycles

MID CABIN EXIT LIGHT AFT RED LENS MISSING. MX REPLACED LENS.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,904 hrs · 14,027 cycles

AFT FA FLASHLIGHT INOP. R2 ASSY

Part: LENS — MISSING (EXIT SIGN) · airframe 17,580 hrs · 13,733 cycles

RED LENS COVER O/H EMERGENCY SIGN MISSING. R2 LENS.

Part: SENSOR — OUT OF ADJUST (PAX DOOR WARNING) · airframe 17,338 hrs · 13,530 cycles

RIGHT AFT EMERGENCY DOOR CAUTION. ADJUSTED PX7.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,692 hrs · 12,964 cycles

ASH FLT 2836 YYC-PHX. UPON PREFLIGHT INSPECTION CREW FOUND EMERGENCY LIGHTS INOP. CREW RECHARGED BATTERIES. MX VERIFIED AND OPS CHECK GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 16,658 hrs · 12,933 cycles

ASH FLT 2658 CLT-BDL. CREW REPORTED BURNING ELECTRICAL SMELL IN COCKPIT AND FORWARD GALLEY. MX INSPECTED AND FOUND NO EVIDENCE OF SMOKE FUMES.

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 14,709 hrs · 11,451 cycles

ASH FLT 2627 CLT-SAV. CREW RETURNED TO THE FIELD DUE TO NLG HAD A GEAR DISAGREE MESSAGE ON RETRACTION. MX ADJUSTED NOSE WOW SWITCHES AND TARGETS.

Part: LENS — MISSING (CABIN) · airframe 14,407 hrs · 11,200 cycles

ASH FLT 2807 PHX-SNA. EMERGENCY EXIT LIGHT LENS ROW 15 A-C MISSING. MX FOUND LENS AND RE-INSTALLED LENS.

Part: SEAL — DIRTY (PAX DOOR)

ASH FLT 2766 PHX-SAT - PASSENGER DOOR NOISY WITH A VISUAL GAP IN THE UPPER LT CORNER. INSPECTED AND CLEANED DOOR AND SEAL. OPS GOOD. (S)

Part: ELBOW — LEAKING (LT BLEED SYS)

ASH FLT 2679 CLT-SAT - LT BLEED DUCT CAUTION, LT BLEED DUCT WARNING. NO PACK PRESSURE AFTER RUNNING OF BLEED DUCT PROCEDURES. REMOVED AND REPLACED MT138 CONNECTOR ELBOW. (S)

Part: PROXIMITY SWITCH — OUT OF ADJUST (EMERGENCY EXIT) · airframe 13,244 hrs · 10,302 cycles

ASH FLT 2732 PHX-LGB. RIGHT AFT EMERGENCY DOOR CAUTION INTERMITTENT. MX ADJUSTED PROX SWITCH.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,942 hrs · 10,046 cycles

ASH FLT 2683 CLT-MEM. ROW 12 CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED, OPS GOOD.

Part: LATCH — LACK OF LUBE (COCKPIT DOOR) · airframe 12,347 hrs · 9,572 cycles

ASH FLT 2724 LAS - COCKPIT DOOR DEAD BOLT STICKEY. MX LUBED LATCH, OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,338 hrs · 9,566 cycles

ASH FLT 2704 PHX - MAIN CABIN DOOR EMERGENCY EXIT LIGHT INOP. MX RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 1,190 hrs · 9,207 cycles

ASH FLT 2601 CLT-IAH - AFT EMERGENCY CEILING FLOODLIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,483 hrs · 7,988 cycles

ASH 2678 CLT. EMERGENCY LIGHTS TURN ON WHEN SELECTED TO ARMED. MX REMOVED AND REPLACED PCB5 IN JB-11. NO FURTHER DEFECTS NOTED.

Part: CAM — OUT OF ADJUST (PAX DOOR) · airframe 10,331 hrs · 7,865 cycles

ASH 2730 DSM - PAX DOOR WILL NOT OPEN. MX ADJUSTED FWD AND AFT SPIGOTS AND CLEARANCE CAMS.

Part: UNKNOWN — UNKNOWN (RUDDER TRIM) · airframe 9,857 hrs · 7,497 cycles

ASH 2693 CLT - TAKEOFF CONFIGURATION ADVISORY MESSAGE WHEN TAKING RUNWAY. UPON ARRIVAL AT GATE CREW NOTICED THE RUDDER TRIM OUT OF THE GREEN. MX PERFORMED AN OPERATIONAL CHECK OF THE RUDDER AND PERFORMED TAKE OFF CONFIGURATION CHECK WITH RUDDER IN GREEN. NO DEFECTS NOTED.

Part: UNKNOWN — MALFUNCTIONED (SPOILER SYS) · airframe 9,558 hrs · 7,261 cycles

ASH 2809 JFK. INBOARD FLIGHT SPOILERS/SPOILERONS CAUTION. PERFORMED SPOST2 WITH FLIGHT CREW. NO FURTHER DEFECTS NOTED.

Part: CONTROL UNIT — UNKNOWN (SPOILERS) · airframe 11,814 hrs · 11,042 cycles

ASH 2946 PHX. INBOARD FLT SPOILER CAUTION IN FLIGHT. MX PERFORMED SSCU TEST, OPS CHECKED GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 9,380 hrs · 7,121 cycles

ASH 2652 BWI. INBOARD FLT SPOILER AND INBOARD FLT SPOILERON CAUTION MESSAGES. MX RESET THE SYSTEM AND NO FURTHER ACTION WAS REQUIRED.

Part: WARNING SYSTEM — MALFUNCTIONED (STABILIZER SYS) · airframe 9,363 hrs · 7,109 cycles

ASH 2686 MCI. PILOT REPORTED STAB FAULT STATUS MSG. MX RESET AND PERFORMED S-POST.

Part: STATUS MESSAGE — ILLUMINATED · airframe 9,245 hrs · 7,019 cycles

ASH 2829 PHX. PILOT REPORTED STAB FAULT STATUS MSG. MX RESET.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,185 hrs · 6,970 cycles

ASH 2681 CLT - OVERHEAD EMERGENCY LIGHT FWD OF EXIT ROW INOP. MX RELAMPED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 9,027 hrs · 6,845 cycles

ASH 2634 IAH. CREW ABORTED TAKEOFF AND RTG DUE TO AVIONICS DOOR CAUTION MESSAGE. MOC PLACED ON MEL WITH CREW. OP'S CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED · airframe 8,943 hrs · 6,774 cycles

ASH 6132 CLT - GLD NOT ARMED CAUTION ON FINAL. MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.

Part: SENSOR — DIRTY (E/E BAY DOOR) · airframe 8,897 hrs · 6,728 cycles

ASH 5091 TRI - ABORTED TAKEOFF DUE TO AVIONIC DOOR CAUTION MESSAGE. MX CLEANED THE SENSORS.

Part: WARNING SYSTEM — ACTIVATED (SPOILER SYS) · airframe 8,849 hrs · 6,688 cycles

ASH 2882 ELP - CAPTAIN REPORTED INBD FLT SPOILER AND INBD SPOILERON CAUTION IN FLIGHT. MX PERFORMED SPOST 1 AND 2.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 8,835 hrs · 6,676 cycles

ASH 2819 PHX - INBD FLT SPOILERS AND INBD FLT SPOILERON CAUTION. MX RESET THE SYSTEM.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 8,834 hrs · 6,675 cycles

ASH 2775 PHX - IB SPOILERS AND IB SPOILERON CAUTION MESSAGE. MX RESET THE SYSTEM.

Part: WARNING SYSTEM — MALFUNCTIONED (STABILIZER) · airframe 8,557 hrs · 6,620 cycles

ASH 2881 PHX - STAB FAULT STATUS MESSAGE. MX RESET THE SYSTEM.

Part: ECU — MALFUNCTIONED (SLAT/FLAP) · airframe 8,675 hrs · 6,553 cycles

ASH 5070 CMH - THE CREW REPORTED A SLATS 1/2 SPEED STATUS MESSAGE. MAINTENANCE REMOVED AND REPLACED THE SLAT/FLAP ELECTRONIC CONTROL UNIT.

Part: STATUS MESSAGE — NONE · airframe 8,493 hrs · 6,016 cycles

ASH 6132 PHX - STAB FAULT STATUS. MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (E/E BAY DOOR) · airframe 8,258 hrs · 6,311 cycles

ASH 6185 OKC - ABORTED TAKEOFF DUE TO AN AVIONICS BAY DOOR CAUTION. DEFERRED DOOR INDICATION.

Part: CIRCUIT BREAKER — TRIPPED (CABIN) · airframe 8,343 hrs · 6,290 cycles

ASH 6550 ONT. SMOKE SMELL COMING FROM FWD LAV AREA. MX FOUND C/B POPPED FOR SIDEWALL LIGHTING. MX RESET C/B AND INSPECTED. NO SMELL OF SMOKE NOTED.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 8,268 hrs · 6,234 cycles

ASH 6357 RNO - GROUND LIFT DUMP UNSAFE MESSAGE. MX PERFORMED S-POST, FAULT CLEARED. NO FURTHER ACTIONS REQURIED.

Part: LIMITER — MALFUNCTIONED (RUDDER) · airframe 8,702 hrs · 6,178 cycles

ASH 5058 GSO - RUDDER TRAVEL LIMITER FAULT. MX RESET SYSTEM. OP'S CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 8,121 hrs · 6,117 cycles

ASH 5080 CLT - AVIONICS DOOR CAUTION. DEFERRED DOOR INDICATION. OP'S CHECK GOOD.

Part: COVER — MISSING (EMERGENCY EXIT) · airframe 7,988 hrs · 6,008 cycles

ASH 5022 CLT - ROW 15 A EMERGENCY EXIT WINDOW MISSING HANDLE COVER. MX REPLACED THE COVER.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,454 hrs · 5,397 cycles

EMERGENCY EXIT LIGHT OVER THE SERVICE DOOR WAS INOP. MAINTENANCE REPLACED THE LIGHT ASSEMBLY.

Part: PROXIMITY SENSOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 7,414 hrs · 5,564 cycles

ASH 6449 FAT - RT AFT EMERGENCY DOOR CAUTION MESSAGE. MX CURRENTLY INVESTIGATING. MX ADJUSTED PROX SENSOR. OPS CHECK GOOD.

Part: DOOR — UNSECURE (EMERGENCY EXT) · airframe 7,406 hrs · 5,557 cycles

ASH 6435 PHX - RT EMERGENCY DOOR CAUTION MESSAGE. MAINTENANCE REMOVED DOOR AND REINSTALLED DOOR. NO DEFECT NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 7,352 hrs · 5,508 cycles

ASH 6094 COS - RT AFT EMERGENCY DOOR CAUTION MESSAGE. MAINTENANCE INSPECTED AND FOUND DOOR TO BE SECURE AND INDICATIONS NORMAL.

Part: ODOR — DETECTED (CABIN) · airframe 7,133 hrs · 5,337 cycles

ASH 6437 BOI, BURNING ODOR IN THE CABIN WITH A/C STARTED. CONTRACT MAINTENANCE PERFORMED OPERATIONAL CHECKS OF APU AND ELECTRICAL SYSTEMS. NO DEFECTS NOTED.

Part: STRUT — UNDERSERVICED (NLG) · airframe 6,715 hrs · 5,015 cycles

ASH 6330 PHX - ABORTED TAKEOFF DUE TO EXCESSIVE NOSE WHEEL SHIMMY. HIGH ENERGY STOP WITHIN LIMITS AND MX RE-SERVICED THE NLG STRUT.

Part: PROXIMITY SENSOR — DIRTY (E/E BAY DOOR) · airframe 6,589 hrs · 4,931 cycles

ASH 6438 PHX - AVIONICS BAY DOOR OPEN INDICATION ON TAKEOFF. CLEANED PROX SENSORS.

Part: ACM — SMOKE (RIGHT) · airframe 6,578 hrs · 4,918 cycles

ASH 6185 MEM - EVACUATED THE AIRCRAFT DUE TO SMOKE IN THE CABIN WITH A RT PACK OVERHEAT. MAINTENANCE REMOVED AND REPLACED RT ACM OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (RADIO ALTIMETER) · airframe 4,888 hrs · 3,745 cycles

ASH 6555 DEN-PHX. ABORTED TAKEOFF FOR GLD UNSAFE MASTER CAUTION MESSAGE. MAINTENANCE INTERROGATED THE MDC AND IT FLAGGED THE NR 1 RADIO ALTIMETER. MAINTENANCE PLACED THE RADIO ALTIMETER ON MEL AND NO FURTHER DEFECTS WERE NOTED. MAINTENANCE RESECURED LOOSE RAD ALT PLUG AND OPS CHECKED GOOD.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 4,615 hrs · 3,558 cycles

ASH 6398 PHX-MEM. RETURNED TO THE FIELD DUE TO A GEAR DISAGREE MESSAGE AFTER TAKEOFF. MAINTENANCE REPLACED GEAR SELECTOR VALVE. A/C RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 2,208 hrs · 1,537 cycles

CREW REPORTED THE CEILING LIGHT 3RD ROW FLOODLIGHT INOP. MAINTENANCE PLACED THE ITEM ON MEL. 10/18/04 MAINTENANCE RE-INSTALLED CONNECTOR AND OPS CHECKED GOOD.

Part: SENSOR — FAILED (NR 2 ENG N2)

ABORTED TAKEOFF DUE TO A RIGHT FADEC CAUTION MESSAGE FOLLOWED BY A RIGHT ENGINE FLAMEOUT. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE RIGHT ENGINE N2 SPEED SENSOR AND OPERATIONAL CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)