N902FJ

Part: BULB — BURNED OUT (ZONE 200) · airframe 46,147 hrs · 36,341 cycles

ROW 18 EMERGENCY FLOOD LIGHT BULB INOP PLACED ON MEL RELAMP, OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,709 hrs · 35,988 cycles

NLG/STEERING DISAGREE CURRENTLY TROUBLESHOOTING, FOUND NLG STRUT COLLAPSED AFTER LANDING, NEEDS A STRUT RE-PACK.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 45,482 hrs · 35,791 cycles

ALL EMER BATT LTS DRAINED/SW LEFT IN ON POSITION CREW ALOWED EMER BATTERIES TO CHARGE, OPS CK GD

Part: BULB — INOPERATIVE (ZONE 200) · airframe 45,462 hrs · 35,774 cycles

FWD ROW 13 EMER LIGHT INOP RELAMPED FWD ROW 13 EMER LIGHT OPS CHECK GOOD

Part: BULB — INOPERATIVE (ZONE 200) · airframe 45,449 hrs · 35,763 cycles

ROW 17 CEILING EMER FLOOD LIGHT INOP REPLACED BULB

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 45,372 hrs · 35,696 cycles

EMERGENCY LIGHTS INOPERATIVE. CHARGED BATTERIES, OPS CHECK GOOD

Part: NONE — NONE · airframe 44,872 hrs · 35,295 cycles

ROW 15 CEILING LEVEL FLOOD LIGHT INOP. REPLACED BULB.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 43,605 hrs · 34,387 cycles

SVC DR LWR AFT FLOODLIGHT 1 BULB OUT REPLACED BULB

Part: NONE — NONE · airframe 43,566 hrs · 34,362 cycles

EMER ZONE INDICATOR LIGHTS 1,3,9 INOP. RESECURED CONNECTOR, OPS CHK GOOD

Part: NONE — NONE · airframe 43,566 hrs · 34,362 cycles

DOOR EXIT LT FWD EDGE 1 BULB INOP. RELAMP, OPS CHK GD

Part: NONE — DAMAGED (SS 196.66) · airframe 43,564 hrs · 34,360 cycles

THE RH WING SLAT 1 RIB AT SS 196.66 WAS FOUND WITH EXISTING MATERIAL REMOVAL COMMON TO THE SLAT DISCONNECT SENSOR STRIKE PIN. PERFORMED PERMANENT REPAIR IAW SRM 57-41-12-995-801, ITEM 28B (REV. 38 DATED JUL. 25, 2020).

Part: NONE — NONE (FS280-FS319) · airframe 43,564 hrs · 34,360 cycles

A FLOOR SILL STRUCTURE WAS FOUND WITH SEVERAL DAMAGES MAKING THE SILL INOPERABLE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 53-21-45-001-A02, ITEM 1 (REV. 38 DATED JUL. 25, 2020).

Part: NONE — NONE · airframe 43,564 hrs · 34,360 cycles

THE FORWARD AND AFT SEAL CARRIERS OF THE AFT SERVICE DOOR PLUG WAS FOUND TO HAVE (2) GOUGES. PERFORMED PERMANENT REPAIR IAW CRJ7/9 IAW SRM 53-51-07-001-005-A01 FIG. 53-51-07-991-801, ITEMS 3 AND 4 (REV. 38 DATED JULY 9, 2021).

Part: NONE — NONE (SPS 43.60) · airframe 43,564 hrs · 34,360 cycles

THE L/H WING T/E STRUCTURE SUPPORT FITTING AT SPS 43.60 WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 REO 670-57-51-341 AND SRM 51-26-00, 51-12-00.

Part: NONE — CORRODED (SVC DOOR SRND ST) · airframe 43,564 hrs · 34,360 cycles

THE SERVICE DOOR SURROUND STRUCTURE SEAL STRIKER WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-21-16 AND PER CMM 516-02 FIG. 1 DETAILS.

Part: NONE — CORRODED (FS581-FS586 RBL9) · airframe 43,564 hrs · 34,360 cycles

THE CENTER FLOOR BEAM AT PAX CABIN WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-00-41-201-001-A03 (FLOORBEAMS FS 280.00 -FS 1098.20 REPAIRS), FIG. 53-00-41-995-829 (REV. 38 DATED JUL. 25, 2020).

Part: NONE — CORRODED (FS661.32-FS 661.) · airframe 43,564 hrs · 34,360 cycles

HE RBL9.00 CENTER FLOOR BEAM AT PAX CABIN WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53 -31-43-101-A03 AND 53-00-41-201-001-A03 (FLOORBEAMS FS 280.00 -FS 1098.20 REPAIRS), FIG 53-00-41-995-829 (REV. 38 DATED JUL. 25, 2020). DEFECT LOCATION: FS 661.00+32-FS 661.00+74, RBL 9.00

Part: BEAM — CORRODED (FS621-661+22.50) · airframe 43,564 hrs · 34,360 cycles

THE CENTER FLOOR BEAM WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 53-31-43, FIG. 53-31-43-991-801, ITEM 6 (REV. 38 DATED JUL. 25, 2020). DEFECT LOCATION: FS 621.00-661.00+22.50, LBL 9.00

Part: NONE — ERODED (VER STAB BULLET) · airframe 43,564 hrs · 34,360 cycles

THE VERTICAL STABILIZER BULLET FAIRING UPPER PANEL ASSEMBLY WAS FOUND HAVING EROSION DAMAGE. PERFORMED PERMANENT REPAIR JAW CRJ7/9 SRM 51-74-02-201-001-A01, (REV. DATED 7-9-2021). DEFECT LOCATION: VERTICAL STABILIZER BULLET FAIRING UPPER PANEL

Part: NONE — DENTED (FS104-1051 STR22) · airframe 43,564 hrs · 34,360 cycles

THE FUSELAGE LOWER SKIN PANEL WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ?/9 53-61-01. DEFECT LOCATION : FS 1047-FS 1051, STGR. 22L - STGR. 23L

Part: NONE — CORRODED (FS661+16FS661+32) · airframe 43,564 hrs · 34,360 cycles

THE UPPER CAP OF THE LBL9.00 CENTER FUSELAGE FLOOR BEAM BETWEEN FS661+16-FS661+32 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-31-43-001-A03, FIG. 53-61-43-991-801, ITEM 2A (REV. 33 DATED JUN. 25, 2017). DEFECT LOCATION: FS 661+16-FS661+32, LBL 9

Part: NONE — DENTED (FS278BET STGR22L) · airframe 43,564 hrs · 34,360 cycles

THE LH FUSELAGE SKIN PANEL WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 53-11-01, FIG. 53-11-01-991-806, ITEM 1 (REV. 38 DATED 9 JUL. 2021 ). DEFECT LOCATION: FS 278.00 BETWEEN STRG. 22L AND STRG. 23L

Part: NONE — NONE (LWR RH FAN COWL) · airframe 43,564 hrs · 34,360 cycles

OUTER SKIN PANEL OF THE LOWER RH FAN COWL DOOR WAS FOUND TO HAVE WEAR DAMAGE AT THE UPPER AFT CORNER. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-14-01, FIGURE 54-14-01-991-801, ITEM 1A, EA 72-2021-219.

Part: NONE — CORRODED (AFT, FS693, RBL) · airframe 43,564 hrs · 34,360 cycles

THE UPPER CAP AFT FLOOR BEAM FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 53-31-43-991-801, ITEM 7 (REV. 33 DATED JUN.25, 2017).

Part: NONE — DENTED (FS295-310 STGR18) · airframe 43,564 hrs · 34,360 cycles

LOWER FUSELAGE SKIN PANEL WAS FOUND TO HAVE A DENT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-01-001-002-A01, ITEMS 1 AND E (REV. 37 DATED 15 AUG 2019). DEFECT LOCATION: FS295.00-FS310.00 ANO STGR.18R-STGR. 19R

Part: NONE — NONE (FS661+32& STR15L) · airframe 43,564 hrs · 34,360 cycles

FOUND PREVIOUS BLENDOUTS AT FUSELAGE LH SKIN PANEL BETWEEN FS661+32 & BETWEEN STGR15L & STGR17L. PERFORMED PERMANENT REPAIR IAW CRJ?/9 SRM 53-31-01, FIG. 53-31-0.1-995-804, ITEM 1 (REV. 38 DATED 9 JUL 2021).

Part: NONE — DENTED (WS 281.50) · airframe 43,564 hrs · 34,360 cycles

THE RH WING OUTBOARD RIB AT WS 281.50 WAS FOUND WITH A DENT AT THE LOWER FLANGE OF THE RIB. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-26-01, SRM 57-53-02-101-001-A01/57-53-01-101-001

Part: NONE — CORRODED (FS581-FS586 RBL9) · airframe 43,564 hrs · 34,360 cycles

CENTER FLOOR BEAM AT PAX CABIN WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM TASK 53-00-41-201-001-A03, SRM 53-31-43-991-801, ITEMS 4 (REV.38 DATED JUL. 25, 2020).

Part: NONE — DENTED (WS.281.50) · airframe 43,564 hrs · 34,360 cycles

DENT DAMAGE WAS FOUND ON RH WING OTBD FLAP LOWER SKIN. DENT WAS LOCATED ON OTBD AFT END AT WS 281.50 & MEASURED 7.779" LONG X 3.228" WIDE X0.120". PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 57-53-01-201-001-A01 TYPE II REPAIR-OUTBOARD FLAP SKINS-FLUSH REPAIRS.

Part: NONE — NONE (FS280-FS319) · airframe 43,564 hrs · 34,360 cycles

FLOOR SILL STRUCTURE WAS FOUND WITH SEVERAL DAMAGES MAKING THE SILL INOPERABLE. PERFORMED PERMANENT REPAIR IAW CR700/900 SRM 53-21-45-001-001-A02, ITEM 31, EA 80-2021-159.

Part: NONE — NONE (INTERFACE PYLON) · airframe 43,564 hrs · 34,360 cycles

WEAR DAMAGE WAS FOUND ON THE L/H ENGINE AFT CORE COWL INBOARD SKIN, THE DAMAGE IS LOCATED AT THE INTERFACE OF THE PYLON FAIRING SEAL. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-13-00, EA 20-2021-202.

Part: NONE — NONE (FS485-517 STR24-) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE LOWER SKIN PANEL BETWEEN FS 485 -FS 517, STR 24R -STR 26R WAS FOUND WITH SIX AREAS OF DAMAGE DUE TO LIGHTNING STRIKE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01-001-003-A02, "SKIN, LOWER PANEL FS477.40 TO FS693.00 -STRUCTURAL IDENTIFICATION, EA 20-2021-197.

Part: NONE — NONE (FS285-295 STR24R) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE SKIN AT FS285.00 - FS295.00 & STGR24R - STGR26R WAS FOUND TO HAVE 3 DENTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01, FIGURE 53-21-01-991-802, ITEM 1M, EA 72-2021-210. FS28S.00 • FS295.00 & STGR2AR • STGR:26R

Part: NONE — NONE (FS295-333 STGR 2) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE LOWER SKIN PANEL WAS FOUND WITH DAMAGE BETWEEN FS295.00-FS333.00 & STGR21R, THE DAMAGE CONSISTS OF TWELVE PROTRUDING DENTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-001-002-A01, FIGURE 53-21-01-991-802, ITEM 1, EA 81-2021-089.

Part: NONE — NONE (AFT BAGGAGE BAY) · airframe 43,564 hrs · 34,360 cycles

AFT BAGGAGE BAY DOOR OUTER SKIN WAS FOUND TO HAVE EIGHT NICKS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 52-31-01-001-001-A01 FIGURE 52-31-01-991-801, ITEM 2A, EA 79-2021-266.

Part: NONE — DENTED (FS319.70 - FS333) · airframe 43,564 hrs · 34,360 cycles

LH FUSELAGE LOWER SKIN PANEL BETWEEN FS319.70 - FS333.0 & STR22L - STR23L WAS FOUND WITH TWO DENTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01, FIGURE 53-21-01-991-802, ITEM 1, EA69-2021-195.

Part: NONE — DENTED (FS1047.0- FS105) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE LOWER SKIN PANEL BETWEEN FS1047.0- FS1051.0, STR. 22L- STR. 23L WAS FOUND WITH A DENT. PERFOMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-01 , EA 20-2021-198.

Part: NONE — NONE (.FS501 & FS525) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE LH SKIN PANEL BETWEEN FS501 & FS525 AND STGR14L & STGR15L WAS FOUND TO HAVE PREVIOUS BLENDOUTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-99-804, ITEM 1, EA 85-2021-003.FS501 & FS525 / STGR14L & STGR15L

Part: NONE — DENTED (FS349-FS 364) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE LOWER SKIN PANEL WAS FOUND WITH A PROTRUDING DENT BETWEEN FS349 - FS364 AND STGR20R - STGR21R. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01, FIGURE 53-21-01-991-806, ITEM 1, EA 72-2021-205.

Part: NONE — NONE (FS661-645 / STGR) · airframe 43,327 hrs · 34,453 cycles

RH FUSELAGE SKIN PANEL WAS FOUND WITH DAMAGE BETWEEN FS 645.00 AND 661.00 AT STGR 17R. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-001-005-A01, FIGURE 53-21-01-991-805, ITEM 1A, EA.81-2021-091

Part: NONE — NONE (FS453, STGR27R -) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE LOWER SKIN PANEL AT FS453 AND STGR27R & STGR26L WAS FOUND TO HAVE A PREVIOUS BLENDOUT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-11-01, FIGURE 53-21-01-99-807, ITEM 1, EA 72-2021-218.

Part: NONE — CORRODED (FS693.00, RBL9.0) · airframe 43,564 hrs · 34,360 cycles

UPPER CAP OF THE RBL9.00 AFT FLOOR BEAM AT FS693.00 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-43-001-001-A03, FIGURE 53-31-43-991-801, ITEM 7, EA 79-2021-260.

Part: NONE — NONE (FS597-629 STGR20) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE LOWER SKIN PANEL BETWEEN FS597 & FS629 AND STGR20L & STGR22L WAS FOUND TO HAVE PREVIOUS BLENDOUTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-99-806, ITEM 1, EA 72-2021-216.

Part: NONE — NONE (FS565-581 STGR21) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE LOWER SKIN PANEL BETWEEN FS565 & FS581 AND STGR21R AND STGR22R WAS FOUND TO HAVE A PREVIOUS BLENDOUT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-99-806, ITEM 1, EA 72-2021-217.

Part: NONE — DENTED (FS278 STR 22L-23) · airframe 43,564 hrs · 34,360 cycles

LH FUSELAGE SKIN PANEL AT FS 278 BETWEEN STR 22L AND 23L WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-11-01, FIGURE53-11-01-991-806, ITEM 1, EA 69-2021-193.

Part: NONE — NONE (FS280-295 STR24R) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE SKIN LOWER PANEL BETWEEN FS280.00 -FS295.00 AND STGR24R -STGR26R WAS FOUND WITH CORROSION DAMAGE AND 4EA DENTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-001-002-A01, ITEM 1, D, E, EA 79-2021-251.

Part: NONE — DENTED (LH ENGINE) · airframe 43,564 hrs · 34,360 cycles

LH ENGINE THRUST REVERSER FORWARD CORE COWL UPPER INBOARD FACING SHEET WAS FOUND WITH (6) MINOR DENTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-23-05-001-001-A01, EA 12-2021-268.

Part: NONE — NONE (FS897-FS927 STGR) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE SKIN BETWEEN FS897.00 - FS927.00, STGR27, WAS FOUND WITH (2) PREVIOUS BLEND OUTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-01-001-003-A02, FIGURE 53-51-01-991-806, ITEM 1, D, EA 79-2021-257.

Part: NONE — DENTED (FS421-437 STR19L) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE SKIN BETWEEN FS 421 - FS 437, STR 19L - STR 20L, WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-991-859, EA 20-2021-205.

Part: NONE — NONE (DOOR DATUM 4 & 5) · airframe 43,564 hrs · 34,360 cycles

PASSENGER DOOR COMMON TO THE AIRSTAIR WAS FOUND TO HAVE CRACK, WHICH IS LOCATED UNDERNEATH THE AFT DRAG ANGLE BETWEEN THE DOOR DATUM 4 AND THE DOOR DATUM 5. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 52-11-04, FIGURE 52-11-04-991-801, ITEM 1A, EA 32-2021-024. DEFECT LOCATION: UND AFT DRAG ANGLE/DOOR DATUM 4 &5

Part: NONE — NONE (AFT CORE COWL) · airframe 43,564 hrs · 34,360 cycles

AFT CORE COWL Z STIFFENER WAS DISCOVERED WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-13-01-991-801, ITEM 31, EA 80-2021-158.

Part: NONE — NONE (FS501.00-FS533.0) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE SKIN BETWEEN FS501.00-FS533.00 AND STGR21L-STGR25L WAS FOUND TO HAVE SEVERAL NICKS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01-001-003-A02, FIGURE 53-31-01-991-806, ITEM 1, A, EA 79-2021-253.

Part: NONE — NONE (FS295-310STGR18-) · airframe 43,564 hrs · 34,360 cycles

LOWER FUSELAGE SKIN PANEL BETWEEN FS295.00 - FS310 AND STGR18R - STGR19R WAS FOUND TO HAVE A DENT. PERFORMED PERMANENT REPAIR JAW CRJ 700/900 SRM 53-21-01-001-002-A01, ITEM 1 AND E, EA 79-2021-254.

Part: NONE — NONE (FS437-FS469) · airframe 43,564 hrs · 34,360 cycles

FUSELAGE LOWER SKIN PANEL WAS FOUND WITH DAMAGE BETWEEN FS437.00-FS469.00 AND STGR23R-STGR25R, DAMAGE CONSISTS IN EIGHT NICKS THAT WERE BLENDED OUT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01, FIGURE 53-21-01-991-807, ITEM 1, EA 81-2021-088.

Part: NONE — NONE (WS 14.50) · airframe 43,564 hrs · 34,360 cycles

LH OUTER WING BAT RIB AT WS 14.50 WAS FOUND WITH A CRACK DAMAGE AND IS BEING REPLACED BY FABRICATION OF A NEW PART. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-21-12-001-001-A01, EA 20-2021-194.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,405 hrs · 34,345 cycles

EMER O/H FLOOD LT ROW 11 INOP. REPLACED BULB.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,378 hrs · 34,224 cycles

EMERGENCY CEILING FLOOD LIGHT ROW 11 INOP. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,378 hrs · 34,224 cycles

EMERGENCY CEILING FLOOD LIGHT ROW 16 INOP. RELAMPED.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 43,315 hrs · 34,175 cycles

SMOKE AFT LAV WARNING - FALSE INDICATION. INSPECTED AND PERFORMED OPS CHECK OF LAV SMOKE DETECTOR, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,261 hrs · 34,138 cycles

EMER FLOOD LIGHT ROW 6 INOP PLACED ON MEL

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,261 hrs · 34,138 cycles

EMER FLOOD LIGHT ROW 18 INOP PLACED ON MEL

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,409 hrs · 33,504 cycles

2 OH EMERG CEIL FLOOD LIGHTS INOP- PLACED ON MEL

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 39,503 hrs · 31,829 cycles

ROW 18 CEILING EMER FLOOD LIGHT INOPERABLE, PLACED ON MEL.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 41,055 hrs · 32,566 cycles

RH FIRST CLASS FACING EXIT SIGN INOP. RECONNECTED WIRE BTW ROWS 3-4 CEILING

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 40,953 hrs · 32,494 cycles

FWD CABIN EXIT SIGN INOP. CHARGED BATTERY PACKS.

Part: UNKNOWN — ODOR (CABIN) · airframe 40,940 hrs · 32,487 cycles

AFT LAV SMOKE WARNING IN FLT PLASTIC BURN SMELL. INSP BY CONTRACT MX AND DEFERRED SMOKE DET.

Part: WIRE — DISCONNECTED (CABIN) · airframe 40,873 hrs · 32,442 cycles

ROW 4 EXIT SIGN INOP RESECURED DISCONNECTED WIRE

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 40,726 hrs · 32,345 cycles

FO FLASHLIGHT INOP- REPLACED BATTERY

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 40,668 hrs · 32,302 cycles

AFT FA FLASHLIGHT INOP. REPLACED BATTERY

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,645 hrs · 32,284 cycles

ROW 14A EMER LIGHT INOP

Part: BATTERY — INOPERATIVE (FO'S FLASHLIGHT) · airframe 40,546 hrs · 32,218 cycles

FO FLASHLIGHT INOP REPLACED BATTERY

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 39,544 hrs · 31,460 cycles

ROW 18 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (ROW 22) · airframe 39,544 hrs · 31,460 cycles

ROW 22 CEILING LVL EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: SIGN — INOPERATIVE (ROW 13A) · airframe 39,120 hrs · 31,129 cycles

ROW 13A FLR LVL EMER EXIT SIGN INOP. R & R LIGHT ASSY.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 39,105 hrs · 31,119 cycles

ROW 14 A/C EMER EXIT SIGN INOP. SECURED THE CONNECTOR PLUG PIN BEHIND SIDEWALL

Part: LIGHT — INOPERATIVE (ROW 13) · airframe 39,049 hrs · 31,073 cycles

ROW 13 OVHD EMER LIGHT INOP. RELAMPED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,042 hrs · 30,312 cycles

2 AFT CABIN CEILING EMER FLOOD LTS INOP. REPLACED BULBS.

Part: DCU — MALFUNCTIONED (ELEVATOR) · airframe 37,183 hrs · 29,661 cycles

ELEVATOR SPLIT CAUTION. RERACKED DCU 1.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN)

AFT FA FLASHLIGHT INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,652 hrs · 29,247 cycles

LAST THREE CEILING EMER FLOOD LIGHTS INOP. REPLACED BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,644 hrs · 29,242 cycles

LAST THREE CEILING EMER FLOOD LIGHTS INOP. RELAMPED.

Part: STRIKER — CORRODED (BS 310-349) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

SERVICE DOOR LOWER SILL SEAL STRIKER CORRODED BEYOND REPAIRABLE LIMITS. THE SEAL STRIKER WAS REPAIRED IAW SRMS.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 35,874 hrs · 28,641 cycles

CRACK IN RADIUS OF LBL 12 COCKPIT FLOORBEAM, AFT ATTACHMENT ANGLE. REPLACED COCKPIT FLOORBEAM IAW REO 670-53-11-896.

Part: FLOOR SUPPORT — CRACKED (BS 270-280) · airframe 35,874 hrs · 28,641 cycles

THREE INCH LONG CRACK IN RADIUS OF THE RBL 12 COCKPIT FLOOR SUPPORT AFT ATTACHMENT FLANGE.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

AFT CARGO DOOR FLOOR SILL IS CORRODED IN SEVERAL LOCATIONS. REPLACED AFT CARGO DOOR FLOOR SILL IAW APPLICABLE SRM'S.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

FRAME SECTOR AT FS 319.00, STRINGER 21L - 20L, CORRODED BEYOND REPAIRABLE LIMITS. FRAME SECTOR REPLACED IAW APPLICABLE SRMS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,874 hrs · 28,641 cycles

FS 333.00 LOWER FRAME SECTOR, STR 26R - 25R, CORRODED BEYOND REPAIRABLE LIMITS. REPLACED FRAME SECTOR IAW REO 670-53-21-799 REV-A, DATED 2016-11-27.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,874 hrs · 28,641 cycles

INTERCOSTAL AT STRINGER 21L IS CORRODED AT FS 319.00. REPLACED IAW APPLICABLE SRM'S.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

FS 280.00 TRANSVERSE FLOORBEAM, COCKPIT FLOOR SUPPORT "J" ANGLE CORRODED BEYOND REPAIRABLE LIMITS. REPLACED FLOOR SUPPORT "J" ANGLE IAW APPLICABLE SRM'S

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

LBL 9, FS 364.00 - 477.00, SEAT TRACK CORRODED. FABRICATED AND INSTALLED NEW SEAT TRACK.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 35,874 hrs · 28,641 cycles

RIGHT VERTICAL FORWARD DRAG ANGLE CRACKED. REPAIRED THE DRAG ANGLE IAW REO 670-55-31-018.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,874 hrs · 28,641 cycles

FS 295.00 LOWER FRAME SECTOR, STRINGER 27 - 26R, CORRODED. REPLACED FRAME SECTOR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

STRINGER 25L BETWEEN FS 295.00 AND FS310.00 CORRODED. REPLACED STRINGER 25L.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

FLOOR SUPPORT CORRODED. THE FLOOR SUPPORT WAS REPLACED IAW SRMS.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

SERVICE DOOR FLOOR SUPPORT CORRODED. REPLACED THE FLOOR SUPPORT IAW SRMS.

Part: FRAME — CORRODED (BS 280) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

CORROSION ON THE FRAME AT BS 280 AT THE LOWER RT FLOOR SUPPORT ATTACH POINT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,874 hrs · 28,641 cycles

FRAME 333.00 BETWEEN STR 1R AND 2R CRACKED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

RT FLOOR SILL FROM FS 280 TO SERVICE DOOR HAS MULTIPLE AREA OF CORROSION.

Part: STRINGER — CORRODED (BS 295-310) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

STRINGER 26R IS CORRODED BETWEEN BS 295 AND 310.

Part: SKIN — CORRODED (BS 295-310) · corrosion level 2 · airframe 35,874 hrs · 28 cycles

FUSELAGE SKIN CORRODED BETWEEN F.S. 295 AND F.S. 310 AND BETWEEN STGR 26R AND 25R.

Part: LONGERON — CORRODED (BS 333-349) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

LONGERON 25R BETWEEN BS 333 AND 349 IS CORRODED.

Part: STRINGER — CORRODED (BS 280-310) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

STRINGER 25R BETWEEN BS 295 AND BS 310 AND 280 IS CORRODED.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

BS 280 FLOORBEAM ANGLE IS CORRODED.

Part: STRINGER SPLICE — CORRODED (BS 333) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

STRINGER SPLICE 25R AT BS 333 IS CORRODED.

Part: STRINGER SPLICE — CORRODED (BS 333) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

STRINGER SPLICE 26R AT BS 333, IS CORRODED.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 35,874 hrs · 28,641 cycles

FLOORBEAM, RBL 11.06 AT BS 280 IS CORRODED AT BOTTOM ATTACHEMENT TO THEFRAME.

Part: HINGE — GOUGED (ZONE 100) · airframe 35,874 hrs · 28,641 cycles

PASSENGER DOOR HINGE FUSELAGE SIDE IS GOUGED ON FLAT FROM ROLL PIN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,853 hrs · 28,625 cycles

ROW 18 OVERHEAD EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,269 hrs · 28,133 cycles

ROW 18 CEILING LEVEL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,269 hrs · 28,133 cycles

ROW 21 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,241 hrs · 28,106 cycles

TWO LAMPS FOUND INOPERATIVE FOR THE LT OVERWING EXIT LIGHT. REPLACED THE LAMPS.

Part: LIGHT — INOPERATIVE (ROW 15) · airframe 3,512 hrs · 28,006 cycles

ROW 15 CEILING LEVEL EMERGENCY LIGHT INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 34,489 hrs · 27,489 cycles

FWD FA'S FLASHLIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (ROW 21) · airframe 34,337 hrs · 27,367 cycles

ROW 21 CEILING LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,086 hrs · 27,151 cycles

FWD FA FLASHLIGHT INOP. PLACED ON MEL.

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 34,050 hrs · 27,116 cycles

ROW 18 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (ROW 3) · airframe 33,852 hrs · 26,967 cycles

CEILING EMERGENCY FLOOD LIGHT ROW 3 INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,817 hrs · 26,940 cycles

FWD FA FLASHLIGHT NOT CHARGING. PLACED ON MEL.

Part: LIGHT — INOPERATIVE · airframe 33,682 hrs · 26,841 cycles

AFT TWO EMERGENCY CEILING LIGHTS INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,341 hrs · 26,599 cycles

EMERGENCY EXIT SIGN HAD ONE BULB INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,124 hrs · 26,452 cycles

OVERHEAD CENTER ISLE EMERGENCY EXIT LIGHT THREE BULBS INOPERATIVE. REPLACED THE BULBS.

Part: LIGHT — INOPERATIVE (ROW 21) · airframe 32,462 hrs · 25,934 cycles

ROW 21 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: LIGHT — NOT REPORTED (CABIN) · airframe 32,359 hrs · 25,851 cycles

EMERGENCY CEILING FLOOD LIGHT ABOVE ROW 6. PLACED ON MEL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,948 hrs · 25,538 cycles

LT ROW 14 LOWER EXIT SIGN, ONE BULB INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,948 hrs · 25,538 cycles

RT ROW 14 LOWER EXIT SIGN, ONE BULB INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,909 hrs · 25,509 cycles

EMERGENCY CEILING FLOODLIGHT ROW 18 INOPERATIVE. REPLACED BULB.

Part: CIRCUIT BOARD — FAILED (EMERGENCY LIGHT) · airframe 31,723 hrs · 25,368 cycles

ROW 14AC EXIT SIGN INOPERATIVE. MX REPLACED THE LIGHT AND PCB ASSY.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 31,658 hrs · 25,317 cycles

ROW 14 LEFT FLOOR LEVEL EMERGENCY EXIT SIGN INOPERATIVE. REPAIRED WIRE AND REPLACED CHARGER 52502.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 31,658 hrs · 25,317 cycles

ROW 14L FLOOR LEVEL EMERGENCY EXIT SIGN INOPERATIVE. CLEANED CONNECTORS ON EPSU AND CHARGER ASSY.

Part: LIGHT — INOPERATIVE (CEILING ROW 8) · airframe 31,641 hrs · 25,303 cycles

CEILING LEVEL EMERGENCY LIGHT ROW 8 INOPERATIVE.

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 31,587 hrs · 25,259 cycles

LEFT FWD EMERGENCY EXIT DOOR WOULD NOT OPEN. ADJUSTED LEFT FWD EMERGENCY DOOR.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 31,587 hrs · 25,259 cycles

RIGHT AFT EMERGENCY EXIT DOOR DIFFCULT TO OPEN. CLEANED AND LUBED RT AFT EMERGENCY DOOR,

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,281 hrs · 25,025 cycles

FLOOR LEVEL EMERGENCY EXIT SIGN ROW 14 INOPERATIVE. R & R NR 4 EMERGENCY LIGHT BATTERY PACK, OPS NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,155 hrs · 24,926 cycles

ONE BULB INOPERATIVE IN EMERGENCY EXIT SIGN ROW 14F.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,155 hrs · 24,926 cycles

ONE BULB INOPERATIVE ON EMERGENCY EXIT SIGN, ROW 14A.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,106 hrs · 24,889 cycles

ROW 14, EXIT SIGN, 3 BULBS OUT. REPLACED BULBS.

Part: FIREWALL — GOUGED (APU BAY) · airframe 31,103 hrs · 24,888 cycles

APU FIRE BULKHEAD, AFT SIDE, GOUGED IN 2 PLACES, APPROXIMATELY .030" DEEP, SIDE BY SIDE. REPAIRED IAW BSC EO CL600-2D24-53-L03549.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,019 hrs · 24,816 cycles

CEILING EMERGENCY FLOOD LIGHT EXIT ROW INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,902 hrs · 24,722 cycles

ROW 14, RIGHT EXIT SIGN, HAS ONE BULB INOPERATIVE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 30,771 hrs · 24,626 cycles

LOWER EMERGENCY EXIT SIGN 14A INOPERATIVE. REPAIRED WIRE AT CONNECTOR J552.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,750 hrs · 24,609 cycles

EMERGENCY EXIT SIGN SW ROW 14, 1 OF 5 LIGHT BULBS INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,737 hrs · 24,596 cycles

ROW 14DF FLOOR EMERGENCY EXIT SIGN, 2 BULBS INOPERATIVE. PLACED ON MEL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,737 hrs · 24,596 cycles

ROW 14AC FLOOR EMERGENCY EXIT SIGN, 2 BULBS INOPERATIVE. PLACED ON MEL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,632 hrs · 24,514 cycles

LT AFT EMERGENCY EXIT SIGN HAS ONE BULB INOPERATIVE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,605 hrs · 24,487 cycles

CEILING EMERGENCY EXIT SIGN INOPERATIVE AT ROW 4 RT. REPLACED BATTERY PACK, PS32.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,605 hrs · 24,487 cycles

CEILING EMERGENCY FLOOD LIGHTS, ROW 1, 3, 6, 9, 11 INOPERATIVE. REPLACED BATTERY PACK PS32.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,288 hrs · 21,680 cycles

LEFT AFT EXT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,941 hrs · 23,982 cycles

TWO LAMPS INOPERATIVE LT FWD OVERWING EXIT SIGN. OPEN

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,901 hrs · 23,958 cycles

EXIT SIGN 13A, 1 BULB INOPERATIVE. REPLACED BULB, OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,083 hrs · 23,314 cycles

EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 28,900 hrs · 23,147 cycles

FWD F/A FLASHLIGHT INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,845 hrs · 23,094 cycles

AFT EMERGENCY EXIT CEILING LIGHT INOPERATIVE, REPLACED THE LAMP.

Part: BATTERY — DISCHARGED · airframe 28,641 hrs · 22,930 cycles

AED BATTERY DEAD, STBY BATTERY INSTALLED. REPLACED AED BATTERY.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 28,555 hrs · 22,856 cycles

AFT FLASHLIGHT INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,431 hrs · 22,761 cycles

SEAT 14F EMERGENCY EXIT SIGN HAS ONE BULB INOPERATIVE. REPLACED THE BULB.

Part: COMPUTER — MALFUNCTIONED (LT BLEED SYS) · airframe 28,399 hrs · 22,731 cycles

LEFT BLEED DUCT WARNING IN FLIGHT. CREW DECLARED EMERGENCY. RERACKED AILC, OPS GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,170 hrs · 22,538 cycles

EMERGENCY EXIT SIGN AT ROW 14DF 1 BULB OUT.

Part: COUNTERBALANCE — DAMAGED (PAX DOOR) · airframe 27,846 hrs · 22,265 cycles

PAX DOOR COUNTERBALANCE SYSTEM DAMAGED.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 27,538 hrs · 21,988 cycles

LEFT EMERGENCY ROW LOWER EMERGENCY LIGHTS INOPERATIVE. REPLACED BULBS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,535 hrs · 21,985 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,499 hrs · 21,955 cycles

CEILING LEVEL EMERGENCY FLOODLIGHT ROW 19 INOPERATIVE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 26,610 hrs · 21,174 cycles

GALLEY EXIT LIGHTS AND SIGNS INOPERATIVE. SECURED LOOSE CONNECTOR ON NR 1 BATTERY CHARGER.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,229 hrs · 20,818 cycles

OVERWING EXIT LIGHT, ONE LAMP INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,746 hrs · 20,396 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE. CHARGED EMERGENCY EXIT LIGHTS WITH ACFT POWER.

Part: BULB — UNSECURE (EMERGENCY LIGHT) · airframe 25,550 hrs · 20,196 cycles

MID CABIN EXIT LIGHT HAS ONE BULB INOPERATIVE. MX SECURED BULB AND FOUND IT TO OPERATE NORMALLY.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 25,476 hrs · 20,139 cycles

FWD FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED BATTERY PACK.

Part: CONNECTOR — DISCONNECTED (FLASHLIGHT) · airframe 25,440 hrs · 20,109 cycles

CAPTAIN FLASHLIGHT INOPERATIVE, FOUND BATTERY CONNECTOR LOOSE. CONNECTED BATTERY TO CAPTAIN'S FLASHLIGHT, OPS GOOD.

Part: BULKHEAD — CORRODED (ZONE 100) · airframe 25,425 hrs · 20,093 cycles

FS 280.00 RT WEB HAS MINOR CORROSION. BLENDED MINOR CORROSION IAW REO 670-53-11-052.

Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,425 hrs · 20,093 cycles

FS 280 CROSSBEAM IS CORRODED BEYOND ALLOWABLE LIMITS ALONG TOP SURFACE. REPAIRED CROSSBEAM IAW SB 670BA-53-041 REV B.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 25,425 hrs · 20,093 cycles

RIGHT FLOOR SUPPORT CORRODED BETWEEN FS 280 AND 295. REPLACED RT FLOOR SUPPORT IAW SRM 51-40-06-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,425 hrs · 20,093 cycles

FS 280 LT WEB HAS MINOR CORROSION. BLENDED MINOR CORROSION IAW REPAIR EO (REO) 670-53-11-052.

Part: PLATE — CORRODED (ZONE 200) · airframe 25,425 hrs · 20,093 cycles

PASSENGER DOOR CUT-OUT FLOOR SUPPORT KICKPLATE ANGLE IS CORRODED BEYOND ALLOWABLE LIMITS. REPLACED PASSENGER DOOR CUT-OUT FLOOR SUPPORT KICKPLATE ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 25,425 hrs · 20,093 cycles

LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE IS CRACKED.

Part: SKIN — CORRODED (RT WING) · airframe 25,425 hrs · 20,093 cycles

RIGHT WING PLANK FASTENER HOLE HAS PITTING CORROSION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,425 hrs · 20,093 cycles

PAX DOOR LINTEL FITTING CRACKED AT FS 280.00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,327 hrs · 20,002 cycles

AFT CEILING EMERGENCY FLOODLIGHT INOPERATIVE. REPLACED LAMPS.

Part: DRAIN — CORRODED (PAX DOORWAY) · airframe 23,719 hrs · 18,666 cycles

DRAIN CORRODED AT PAX DOORWAY. PERFORM MESA ENGINEERING ORDER 9-52-0032 IN CONJUNCTION WITH AD 2010-23-14.

Part: PLACARD — MISSING (CABIN) · airframe 23,651 hrs · 18,610 cycles

PAX DOOR ARROW PLACARD MISSING, R2 PAX DOOR ARROW PLACARD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,490 hrs · 18,475 cycles

OVERHEAD CEILING EMERGENCY FLOOD LIGHT ROW 9 INOP. RELAMPED

Part: PLACARD — WORN (PAX DOOR) · airframe 22,370 hrs · 17,638 cycles

PASSENGER DOOR "EXIT" PLACARD WORN. R2 PASSENGER DOOR "EXIT" PLACARD.

Part: PLACARD — WORN (PAX DOOR) · airframe 22,370 hrs · 17,638 cycles

PASSENGER DOOR "OPEN" PLACARD WORN. R2 PASSENGER DOOR "OPEN" PLACARD.

Part: SENSOR — DEFECTIVE (PAX DOOR) · airframe 22,236 hrs · 17,534 cycles

PAX DOOR OUTER HNDL CTN IN FLT. CLEANED PX 107.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 21,854 hrs · 17,212 cycles

FWD F/A FLASHLIGHT BATTERY DEAD. REMOVED AND REPLACED THE BATTERIES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,268 hrs · 16,719 cycles

OVERHEAD EMERGENCY LIGHT INOP ROW 7. RELAMPED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (SERVICE DOOR) · airframe 21,162 hrs · 16,638 cycles

FWD SERVICE DOOR CAUTION INTERMITTENT. ADJUSTED PX 38 PROX SENSOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,124 hrs · 16,604 cycles

CEILING LEVEL EMERGENCY FLOOD LIGHT ROW 20 INOP. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,009 hrs · 16,513 cycles

EMER O/H LIGHT ROW 18 INOP. RELAMPED EMERGENCY LIGHT.

Part: STRUT — DEFECTIVE (PAX DOOR) · airframe 20,953 hrs · 16,463 cycles

PAX DOOR FALLS RAPIDLY. R2 AFT COUNTER BALANCE STRUT, OPS GOOD.

Part: MEDICAL KIT — UNSERVICEABLE (CABIN) · airframe 20,775 hrs · 16,314 cycles

EEMK KIT OPENED/USED (BRONC INHALER0). R2 EEMK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,734 hrs · 16,282 cycles

AFT F/A FLASHLIGHT INOP. R2 BATTERY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,734 hrs · 16,282 cycles

FWD F/A FLASHLIGHT LED INOP. R2 BATTERY.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,552 hrs · 16,134 cycles

FWD F/A FLASHLIGHT NOT CHARGING. R2 FLASHLIGHT.

Part: DOOR — DAMAGED (CABIN) · airframe 20,559 hrs · 16,138 cycles

DOOR STRUCK GROUND WHEN OPENED. INSPECTED DOOR, NO DAMAGE FOUND.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 20,514 hrs · 16,100 cycles

PROX SYSTEM FAULT 2-LG HANDLE FLAG IN MDC. R2 LANDING GEAR CONTROL PANEL.

Part: PSEU — MALFUNCTIONED (LANDING GEAR) · airframe 20,509 hrs · 16,097 cycles

PROX FAULT 2. RESET PSEU.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 20,432 hrs · 16,031 cycles

FIRE SYSTEM FAULT STATUS. R2 CENTER CARGO SMOKE DETECTOR.

Part: UNKNOWN — FAULTED (FIRE WARNING) · airframe 20,334 hrs · 15,955 cycles

FIRE SYS FAULT. OPS CHECKED GOOD

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,209 hrs · 15,848 cycles

CEILING EMERG LIGHT ROW 17 INOP. RELAMPED EMERGENCY LIGHT.

Part: LANYARD — LOOSE (PAX DOOR) · airframe 20,203 hrs · 15,841 cycles

MED AFT RAIL LANYARD NOT SECURE. SECURED MED AFT RAIL LANYARD.

Part: SUPPORT — SEPARATED (ENTRY DOOR) · airframe 20,203 hrs · 15,841 cycles

MED TOP STEP SUPPORT PANEL SEPARATING AT HINGE SEAM. R2 TOP STEP SUPPORT PANEL.

Part: COVER — LOOSE (OVERWING EXIT) · airframe 20,148 hrs · 15,791 cycles

RT WING REAR OVERWING EXIT HANDLE COVER NOT SECURE. SECURED OVER WING EXIT HANDLE COVER.

Part: PIN — MIGRATED (DOOR STEP) · airframe 20,091 hrs · 15,743 cycles

BOT ME STEP H-PIN MIGRATED. RE-SECURED BOT ME STEP H-PIN.

Part: DRAIN — CLOGGED (MAIN ENTRY) · airframe 20,091 hrs · 15,743 cycles

ME DOOR DRAINS CLOGGED. CLEANED THE MAIN ENTRY DOOR DRAINS.

Part: STATIC WICK — DAMAGED (LT WINGLET) · airframe 20,085 hrs · 15,738 cycles

STATIC WICK ON LT WINGLET (K) P/N 10-900-28A-2 (QTY 2) ON REQ TO CLT FOR 5/3 RON. R&R STATIC WICK.

Part: LIFE VEST — DEFECTIVE (CABIN) · airframe 20,072 hrs · 15,726 cycles

AFT F/A LIFE VEST NOT VACUUM SEALED. R2 LIFE VEST.

Part: WARNING SYSTEM — INTERMITTENT (FIRE DETECTION) · airframe 20,034 hrs · 15,696 cycles

FIRE SYS FAULT STATUS INTERMITTENT. RT ENG LOOP A. OPS CHECK GOOD.

Part: A/C PACK — SMOKE (LEFT) · airframe 18,145 hrs · 14,409 cycles

LEFT PACK SMOKING. REMOVED AND REPLACED LT A/C PACK.

Part: ACM — SEIZED (AC BAY) · airframe 19,906 hrs · 15,579 cycles

STRONG BURNING ODOR/SMOKE IN CABIN. MX REMOVED AND REPLACED ACM.

Part: LIGHT — INSTALLED (CABIN) · airframe 19,675 hrs · 15,369 cycles

SVC ENTRY LOWER FWD FLOOD LIGHT HAS BULBS OUT. MX RELAMPED, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,675 hrs · 15,369 cycles

PAX ENTRY LOWER FWD FLOOD LIGHT HAS BULBS OUT. MX RELAMPED, OPS CHECK GOOD.

Part: PLACARD — WORN (CABIN DOOR) · airframe 19,675 hrs · 15,369 cycles

PAX DOOR FLORESCENT OPEN PLACARD WORN. MX INSTALLED PLACARD.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,348 cycles

SERVICE DOOR SILL CORRODED AT SCREW HOLES. REMOVED AND REPLACED SERVICE DOOR SILL IAW CRJ 900 SRM 51-42-06 AND 51-42-13.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,654 hrs · 15,348 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT STEP AT ASSIST MOTOR. REPAIRED PAX DOOR AT STEP SKIN ASSIST MOTOR IAW CRJ 900 SRM 52-11-09.

Part: STRUCTURE — CRACKED (THRUST REVERSER) · airframe 19,654 hrs · 15,348 cycles

LT UPPER COWL SIDE DOOR COAMING IS CRACKED. REMOVED AND REPLACED LT UPPER TRANS COWL DOOR COAMING IAW CRJ 900 SRM 51-42-13.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,348 cycles

STR 26R HAS CORROSION JUST FWD OF THE E/E BAY OPENING. REMOVED AND REPLACED STR 26R FWD OF E/E BAY OPENING IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: SKIN PANEL — CRACKED (PAX DOOR) · airframe 19,654 hrs · 15,348 cycles

PAX DOOR AFT WEB (SKIN PNL) IS CRACKED. REMOVED AND REPLACED WEB (SKIN PNL) IAW CRJ 900 SRM 51-42-06 AND 51-42-07.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,348 cycles

FWD E/E BAY STRINGER/WEB (INTERCOSTAL) 20R HAS CORROSION BETWEEN FS 333 AND 319. REMOVED AND REPLACED INTERCOSTAL IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,348 cycles

RT AND LT 280 FRAME CORRODED. REPAIRED FS 280 FRAME IAW RO CRJ9-53-0584.

Part: FITTING — CRACKED (FUSELAGE) · airframe 19,654 hrs · 15,348 cycles

PAX DOOR LINTEL FITTING CRACKED AT FS 280 STR 3L. REPAIRED LINTEL FITTING AT FS 280 STR 3L IAW RO CRJ 9-53-0581.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,348 cycles

FLOOR SILL AT FS 280 CORRODED RT SIDE. REPAIRED FLOOR SILL AT FS 280 RT SIDE IAW RO CRJ-9-53-0606.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,348 cycles

FWD E/E BAY STR 25R HAS CORROSION BETWEEN FRAME FS 333 AND 319. REMOVED AND REPLACED STR 25R AT STA 319-333 IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,348 cycles

FWD E/E BAY SPLICE ON 26R HAS CORROSION BETWEEN FRAME FS 333 AND 319. REMOVED AND REPLACED SPLICE AT STR 26R STA 319-333 IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,348 cycles

STR 21R AT CONNECTOR HAS CORROSION BETWEEN FS 349 AND 364. REMOVED AND REPLACED STR 21R AT STA 349-364 IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,348 cycles

FWD E/E BAY STR 26 R HAS CORROSION BETWEEN FRAME FS 333 AND 319. REMOVED AND REPLACED STR 26R AT STA 319-333 IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,348 cycles

FWD E/E BAY SPLICE ON STR 25R HAS CORROSION BETWEEN FRAME 333 AND 319. REMOVED AND REPLACED SPLICE AT STR 25R STA 319-333 IAW CRL 900 SRM 51-42-06 AND 51-42-21.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,348 cycles

FWD E/E BAY FRAME FS 295 HAS CORROSION AT BOTTOM SIDE FR STR 27 TO 25R. REMOVED AND REPLACED FRAME AT STA 295 STR 27-25R IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,348 cycles

LT DIAPHRAM JUST FWD OF E/E BAY OPENING JUST LT OF STR 27 HAS CORROSION. REMOVED AND REPLACED LT DIAPHRAM STA 364 STR 27 IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,655 hrs · 15,348 cycles

FWD E/E BAY STR 24R HAS CORROSION BETWEEN FRAMES 310 AND 295. REMOVED AND REPLACED STR 24 R STA 310 295 IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,248 cycles

FWD E/E BAY STR 19 R HAS CORROSION BETWEEN FRAMES FS 295 AND 280. REMOVED AND REPLACED STR 19R STA 280-295 IAW CRJ 900 SRM 51-42-06 AND 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,354 hrs · 15,348 cycles

RT FLOOR SEAT TRACK CORRODED AT STA 661.00-752.00 RBL 9.00. REMOVED AND REPLACED SEAT TRACK AT STA 661.00-752.00 RBL 9.00 IAW CRJ 900 AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,654 hrs · 15,348 cycles

RT SEAT TRACK CORRODED AT STA 349-453 RBL 9.00. REMOVED AND REPLACED SEAT TRACK AT STA 349.00-453.00 RBL 9.00 IAW CRJ 900 AMM 53-00-49.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 19,607 hrs · 15,313 cycles

CAPT FLASHLIGHT INOP. MX REPLACED FLASHLIGHT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,607 hrs · 15,313 cycles

F/O FLASHLIGHT INOP. MX R2 BATTERY.

Part: COVER — MISSING (CABIN) · airframe 19,546 hrs · 15,259 cycles

FWD EMERGENCY FLOODLIGHT COVER MISSING. MX REPLACED COVER.

Part: COVER — BROKEN (CABIN) · airframe 19,546 hrs · 15,259 cycles

FLIGHT ATTENDANT EMERGENCY SWITCH LIGHT COVER BROKEN. MX REPLACED COVER.

Part: PLACARD — MISSING (MAIN CABIN DOOR) · airframe 19,399 hrs · 15,149 cycles

PAX DOOR 1ST STEP EXIT SIGN MISSING. MX REPLACED PLACARD.

Part: BRAKE SYS — MALFUNCTIONED (RT MLG) · airframe 19,352 hrs · 15,115 cycles

RTG LEFT BRAKE FEELS MUSHY. TAXI CHECK / BRAKE OPS NORMAL, NO DEFECTS.

Part: WARNING SYSTEM — MALFUNCTIONED (SERVICE DOOR) · airframe 19,110 hrs · 14,925 cycles

PROX SYSTEM FAULT 2. MX CYCLED SERVICE DOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,021 hrs · 14,854 cycles

EMERGENCY EXIT FLOOD LIGHT AT ROW 20 INOP. MX RELAMPED EMERGENCY LIGHT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,927 hrs · 14,771 cycles

FWD F/A FLASHLIGHT INOP. MX R2 BATTERY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,746 hrs · 14,632 cycles

EMERGENCY LIGHTS ARE DIM IN CABIN. MX CHARGED BATTERIES.

Part: ACTUATOR — LEAKING (NR 1 ENGINE) · airframe 18,585 hrs · 14,517 cycles

LT ENGINE FUEL LEAK. MX R2 NR 1 ENG SLAVE VG ACTUATOR.

Part: CHARGER — DEFECTIVE (CABIN) · airframe 18,516 hrs · 14,468 cycles

CEILING EMERGENCY FLOOD LIGHTS AT ROW 4 AND 5. MX R2 NR 2 BATTERY AND CHARGER, OPS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,487 hrs · 14,447 cycles

THE 3RD EMERGENCY EXIT FLOOD LIGHT INOP. R2 NR 2 BATTERY PACK AND CHARGER, OPS GOOD.

Part: SEAL — MISSING (PAX DOOR) · airframe 18,482 hrs · 14,444 cycles

PAX DOOR WEATHER SEAL MISSING. REMOVED AND REPLACED SEAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,364 hrs · 14,372 cycles

AFT CABIN OVERHEAD EMERGENCY LAMP OUT. MX REPLACED THE LAMP.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,012 hrs · 14,085 cycles

FWD F/A FLASHLIGHT NOT CHARGING; REMOVED AND REPLACED FLASHLIGHT, OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,943 hrs · 14,033 cycles

AFT FLASHLIGHT INOP, AFT FLASHLIGHT WON`T HOLD A CHARGE. R2 FLASHLIGHT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,649 hrs · 13,777 cycles

FWD F/A EMERGENCY FLASHLIGHT INOP. REPLACED THE FORWARD F/A FLASHLIGHT.

Part: FAN BLADE — LACK OF LUBE (LT ENGINE) · airframe 17,278 hrs · 13,461 cycles

ON CLIMBOUT IN MEMPHIS LEFT ENGINE VIBRATION WAS HIGH 1.6MILS BUT IN THE GREEN BAND AT CRUISE WHEN POWER REDUCED VIB WENT TO 1.8. CREW WAS ABLE TO KEEP THE VIB IN THE GREEN DURING THE FLIGHT. THE FLIGHT ATTENDANTS CALLED TO ASK ABOUT THE VIBRATION AND THE LOUD NOISE LEVEL. CREW REFERRED TO THE QRH AND CONTINUED THE FLIGHT, NO SHUT DOWN WAS NECESSARY. CONTACTED DISPATCH BY ARINC AND INFORMED DISPATCH OF THE SITUATION. ON DESCENT INTO PHX, WHEN REDUCED POWER THE VIB WENT TO 3.0. AS THE ENGINE WAS NOT NORMAL. ELECTED TO DECLARE AN EMERGENCY AS A PRECAUTION. FAS PAX AND PHX OPS WERE NOTIFIED AND LANDED WITHOUT FURTHER INCIDENT. MX SENT AC TO HANGER, C/W FAN BLADE LUBE. ENG RUN OPS CHECK GOOD.

Part: DOOR — ICED (NLG) · airframe 17,228 hrs · 13,417 cycles

DE-ICED ON TAXI OUT. ON TAKEOFF GOT NOSE DOOR OPEN MASTER WARNING MSG WHEN RETRACTING GEAR. COMPLETED CHECK LISTS, TALKED TO COMPANY/MX, AND RETURNED TO FIELD PER CHECK LIST. REMOVED ICE FROM AFT NOSE DOOR, OPS CHECK GOOD.

Part: GLOWSTRIP — MISSING (CABIN)

ASH FLT 2836 PHX. RT FLOOR PANEL EMERGENCY LIGHTING SECTION MISSING. CHANGED PHOTO ILLUMINESCENT STRIP. (S)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,850 hrs · 9,946 cycles

ASH FLT 2934 FAT-PHX. CABIN CEILING LEVEL EMERGENCY FLOOD LIGHT 1 BULB INOPERATIVE. RELAMPED EMERGENCY LIGHT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,798 hrs · 9,129 cycles

ASH FLT 2821 PHX - EMERGENCY EXIT OVERHEAD FLOOD LIGHT INOPERATIVE. MX RELAMPED.

Part: WARNING LIGHT — ILLUMINATED · airframe 11,630 hrs · 8,996 cycles

ASH FLT 9701 LAS-LAS - LOW FUEL CAUTION MSG AFTER T/O. MX IS CURRENTLY TROUBLESHOOTING THE SYSTEM.

Part: ACM — ODOR (RIGHT) · airframe 11,459 hrs · 8,854 cycles

ASH FLT 2610 SRQ-CLT - RT PACK AUTO FAIL CAUTION MESSAGE ALONG WITH SMOKE AND ODOR IN THE CABIN. REMOVED AND REPLACED RT ACM, OPS NORMAL.

Part: HINGE PIN — DAMAGED (LT NLG DOOR) · airframe 11,256 hrs · 8,643 cycles

ASH 2610 CLT-MYR - AIRCRAFT RETURNED TO FIELD DUE TO NLG DOOR WARNING AFTER RETRACTION. MX REMOVED AND REPLACED LT SPADE DOOR HINGE PIN.

Part: HANDLE — SEPARATED (EMERGENCY EXIT) · airframe 10,507 hrs · 8,020 cycles

ASH 2946 RNO - 16DF EMERGENCY EXIT HANDLE COVER CAME OFF. MX REPAIRED HANDLE.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 10,028 hrs · 7,665 cycles

ASH 2829 PHX - CREW REPORTED THE OVERWING EMERGENCY EXIT DOOR AT 15A THE DOOR HANDLE COVER AS LOOSE. MX REPLACED THE VELCRO AND RESECURED COVER.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 9,973 hrs · 7,619 cycles

ASH 2892 TUS - ROW 15D/F OVERWING EMERGENCY EXIT HANDLE INTERIOR COVER LOOSE. MX RESECURED COVER.

Part: SENSOR — MALFUNCTIONED (RT ENGINE) · airframe 9,955 hrs · 7,599 cycles

ASH 2941 TUS - RT ENGINE FLAMED OUT DURING TAXI. MX REMOVED AND REPLACED THE N2 SENSOR AND NO DEFECTS NOTED ON BORESCOPE.

Part: CONTROL UNIT — MALFUNCTIONED (SLAT SYSTEM) · airframe 9,535 hrs · 7,274 cycles

ASH 6225 PHX. SLAT 1/2 SPEED FAULT STATUS MESSAGE. MX REMOVED AND REPLACED NR 1 SFECU.

Part: PACKING — DEFECTIVE (RT BRAKE) · airframe 9,949 hrs · 7,218 cycles

ASH 2920 PHX. RIGHT BRAKE LEAKING FLUID AND SMOKING. SMOKE WAS DUE TO FLUID LEAKING ONTO HOT BRAKE. MX REPLACED BLEEDER PACKING.

Part: CONTROL UNIT — WARNING MESSAGE (SPOILERS) · airframe 9,187 hrs · 7,023 cycles

ASH 2709 PHX. SPOILER STAB FAULT AND SLATS HALFSPEED STATUS MESSAGE. MX REPLACED SFECU.

Part: WARNING SYSTEM — MALFUNCTIONED (STABILIZER SYS) · airframe 9,177 hrs · 7,015 cycles

ASH 2931 PHX. CREW REPORTED PITCH FEEL FAULT STATUS. MX RESET SYS.

Part: WARNING LIGHT — ILLUMINATED · airframe 9,077 hrs · 6,936 cycles

ASH 2601 GSO. SLATS HALF SPEED. MX CND. OP'S CHECK GOOD.

Part: SLAT — MALFUNCTIONED (WING) · airframe 9,039 hrs · 6,905 cycles

ASH 2829 PHX. CAPTAIN REPORTED SLATS 1/2 SPEED. MX PLACED SUB SYSTEM ON MEL. MX CND.

Part: SLAT — MALFUNCTIONED (WING) · airframe 8,982 hrs · 6,859 cycles

ASH 5001 ILM. REPORTED SLATS 1/2 SPEED. MX CLEARED INHIBITS, NO OTHER FAULTS NOTED.

Part: WARNING SYSTEM — MALFUNCTIONED (FUEL CONTROL) · airframe 8,897 hrs · 6,798 cycles

ASH 5024 MEM - "RTG" CREW REPORTED RT FADEC FAULT WITH ITT GOING SLOWLY TO THE RED AT 917 CELSIUS. CONTRACT MX PERFORMED AN IDLE RUN FOLLOWED BY A POWER RUN TO FULL TAKEOFF POWER WITH CREW AND NO FAULTS FOUND. AC RETURNED TO SERVICE.

Part: ENGINE — FLAMED OUT (RIGHT) · airframe 8,819 hrs · 6,745 cycles

ASH 5008 CLT - AC "RTG" DUE TO RT ENGINE FLAME OUT. CAPTAIN INDICATED 747 IN FRONT OF HIM CAUSED FLAME OUT AND POWER RUNS WERE NORMAL. BORESCOPE INDICATED NO DEFECTS.

Part: ECU — MALFUNCTIONED (L/E SLAT) · airframe 8,756 hrs · 6,703 cycles

ASH 2469 LAS - SLAT FAULTS CAUTION MSG. MX CLEARED SFECU INHIBITS.

Part: SLAT — MALFUNCTIONED (WING) · airframe 8,708 hrs · 6,669 cycles

ASH 2886 CLT - SLATS HALF SPEED. MX RESET THE SYSTEM.

Part: SPOILER — MALFUNCTIONED (WING) · airframe 8,700 hrs · 6,658 cycles

ASH 2830 LAS - CAPTAIN REPORTED SPOILERS WERE EXTENDED. MX OP'S CHECKED AND FOUND NO DEFECTS. ACFT CONTINUED OPERATIONS.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 8,675 hrs · 6,644 cycles

ASH 2818 PHX - CAPTAIN REPORTED OUTBOARD SPOILERON AND OUTBD SPOILER CAUTION MESSAGE. MX RESET THE SYSTEM AND PERFORMED SPOST 1 AND 2.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 8,659 hrs · 6,630 cycles

ASH 2880 RNO - CAPTAIN REPORTED OUTBOARD SPOILERON AND OUTBOARD FLIGHT SPOILER CAUTION MESSAGE. MX RESET THE SYSTEM AND PERFORMED SPOST 1 AND 2.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 8,643 hrs · 6,624 cycles

ASH 6277 LAS - CAPTAIN REPORTED OUTBOARD FLIGHT SPOILER/SPOILERON CAUTION MSG. MX RESET THE SYSTEM.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 8,639 hrs · 8,621 cycles

ASH 6476 PHX - OUTBOARD SPOILERS AND OUTBOARD SPOILERONS CAUTION MESSAGE. MX PERFORMED SYSTEM RESET AND FAULTS CLEARED.

Part: CAUTION MESSAGE — FALSE ACTIVATION · airframe 8,561 hrs · 6,561 cycles

ASH 5006 CLT - OTBD FLIGHT SPOILERS/SPOILERONS CAUTION. MX PERFORMED SPOST. NO FURTHER DEFECTS NOTED.

Part: CAUTION MESSAGE — NONE · airframe 8,528 hrs · 6,530 cycles

ASH 5074 CLT - O/B FLT SPOILERS AND O/B FLT SPOILERON CAUTION MESSAGE. MX RESET THE SYSTEM.

Part: CAUTION MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 8,464 hrs · 6,475 cycles

ASH 5098 CLT - OB SPOILERONS AND OB FLIGHT SPOILERS FAULT CAUTION MESSAGE ON FINAL. MX RESET.

Part: PITOT LINE — CONTAMINATED · airframe 8,367 hrs · 6,403 cycles

ASH 6127 YEG - THE CREW ABORTED THE TAKEOFF ROLL DUE TO A STALL FAIL CAUTION MESSAGE. MX DRAINED THE PITOT/STATIC LINE TRAPS AND THE CREW PERFORMED A HIGH SPEED TAXI CHECK, SYSTEM OPERATING NORMALLY.

Part: CAUTION MESSAGE — ILLUMINATED · airframe 8,240 hrs · 6,385 cycles

ASH 6162 PHX - OTBD SPOILERON AND OTBD FLT SPLR CAUTION MESSAGES. MX PERFORMED SPOST TEST. OP'S CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (L/E SLAT) · airframe 8,294 hrs · 6,348 cycles

SLAT FAULT STATUS MESSAGE. MX RESET SYSTEM.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILERON) · airframe 8,075 hrs · 6,143 cycles

ASH 5029 CLT - OB FLT SPOILERS AND OB FLT SPOILERON CAUTION MESSAGE. MX RESET THE SYSTEM.

Part: CAUTION MESSAGE — ILLUMINATED · airframe 8,076 hrs · 6,143 cycles

ASH RON CLT. O/B SPOILERONS AND O/B FLIGHT SPOILERS FAULT CAUTION MESSAGE ON FINAL. MX RESET THE SYSTEM.

Part: SLAT SYSTEM — MALFUNCTIONED (LE SLATS) · airframe 8,054 hrs · 6,129 cycles

ASH 5001 ILM - SLATS 1/2 SPEED. MX CLEARED INHIBITS. NO FURTHER FAULTS NOTED. ACFT CONTINUED OPERATIONS.

Part: ECU — MALFUNCTIONED (SLAT/FLAP SYS) · airframe 7,859 hrs · 5,967 cycles

ASH 5001 ILM - SPOILER STAB FAULT AND RUDDER LIMIT FAULT. MX CLEARED INHIBITS AND SWAPPED SFECU'S. OP'S CHECK GOOD. ACFT CONTINUED OPERATIONS.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 7,853 hrs · 5,965 cycles

ASH 5049 ILM - SPOILER STAB, PITCH FEEL, RUDDER LIMIT, FLAPS 1/2 SPEED. CLEARED INHIBITS. OP'S CHECK GOOD.

Part: DOOR — DISLODGED (EMERGENCY EXIT) · airframe 7,799 hrs · 5,924 cycles

ASH 5079 CLT - ABORTED TAKEOFF DUE TO LT OVERWING EMERGENCY EXIT CAUTION. MX RESEATED LT OVERWING EMERGENCY EXIT DOOR. OP'S CHECK GOOD.

Part: CAUTION MESSAGE — ILLUMINATED (THRUST REVERSER) · airframe 7,779 hrs · 5,905 cycles

ASH 5081 ALB - REJECTED TAKEOFF DUE TO LT THRUST REVERSER UNSAFE CAUTION MESSAGE DURING TAKEOFF ROLL. MAINTENANCE REPLACED RELAY.

Part: LIMITER — FAULTED (RUDDER) · airframe 7,697 hrs · 5,842 cycles

ASH 6528 PHX - RUDDER LIMIT FAULT STATUS MESSAGE. MX REMOVED AND REPLACED NR 1 RTL.

Part: ACTUATOR — FAULTED (RUDDER) · airframe 7,695 hrs · 5,843 cycles

ASH 6486 MEM - CAPTAIN REPORTED A RUDDER LIMIT FAULT STATUS MESSAGE UPON ARRIVAL INTO PHX. MX R2 NR 1 RTL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 7,662 hrs · 5,820 cycles

ASH 5033 ILM - CAPTAIN REPORTED RT ENG LEAKING FUEL FROM DRAIN. MX COULD NOT DUPLICATE AND ONLY FOUND 2 DRIPS FROM DRAIN, WHICH WAS WITHIN LIMITS. ACT CONTINUED OPERATIONS.

Part: LIMITER — FAULTED (RUDDER) · airframe 7,656 hrs · 5,815 cycles

ASH 5040 CLT - RUDDER LIMIT FAULT. MX PERFORMED SPOST 1 AND 2. NO FURTHER DEFECTS NOTED.

Part: LIMITER — FAULTED (RUDDER) · airframe 7,641 hrs · 5,800 cycles

ASH 5083 PVD - RUDDER LIMIT FAULT. PERFORMED SPOST 2 W/FLIGHT CREW. NO FURTHER FAULTS NOTED.

Part: LIMITER — FAULTED (RUDDER) · airframe 3,244 hrs · 2,296 cycles

ASH 6075 IAH, RUDDER LIMIT FAULT STATUS MESSAGE. MX RESET SYSTEM. PERFOMED SPOST 1 AND 2. OP'S CHECK GOOD.

Part: LIMITER — FAULTED (RUDDER) · airframe 7,570 hrs · 5,736 cycles

ASH 6486 MEM - CAPTAIN REPORTED A RUDDER LIMIT FAULT STATUS MESSAGE UPON ARRIVAL INTO PHX. MX RESET THE SYSTEM AND PERFORMED SPOST. OP'S CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED · airframe 7,498 hrs · 5,674 cycles

ASH 5012 CLT - FLAP FAULT STATUS MESSAGE. MAINTENANCE RESET SEFCU'S. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 7,432 hrs · 5,619 cycles

ASH 6443 SAT - SPOILER/STAB, RUDDER LIMIT AND PITCH FEEL FAULTS. MAINTENANCE REMOVED AND REPLACED NR 2 SFECU.

Part: LIMITER — FAULTED (RUDDER) · airframe 7,432 hrs · 5,619 cycles

ASH 6443 PHX - 1/2 SPEED STATUS MSG, SPOILER STAB FAULT, PITCH FEEL FAULT AND RUDDER LIMITER FAULT. MAINTENANCE CLEARED INHIBITS AND OPS CHECK. COULD NOT DUPLICATE THE FAULT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,396 hrs · 5,596 cycles

ASH 6416 PHX - AFT CEILING EMERGENCY LIGHT INOP. MX RELAMPED.

Part: PBE — TRIPPED (COCKPIT) · airframe 7,353 hrs · 5,561 cycles

ASH 6193 TUS - CAPTAIN REPORTED FLIGHT ATT PBE VSI POP-IT IS PROTRUDING. MX REPLACED THE PBE, ACFT CONTINUED OPERATIONS.

Part: SEAL — BROKEN (PBE) · airframe 7,309 hrs · 5,529 cycles

ASH 5021 CLT - FORWARD CABIN PBE SEALS BROKEN. MX INSPECTED THE PBE WITH NO DEFECTS NOTED AND RESEALED.

Part: ACM — OVERHEATED (LEFT) · airframe 6,908 hrs · 5,216 cycles

ASH 6526 PVR - SMOKE IN THE COCKPIT AND THE LT PACK WENT TO 98° C. MAINTENANCE MEL'D LT AIR CONDITION PACK. MX REMOVED AND REPLACED AIR CYCLE MACHINE.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 6,757 hrs · 5,118 cycles

ASH 6183 PHX, NR 2 ENGINE FLAMED OUT ON TAXI OUT PREVIOUSLY DSM. ALL INSPECTIONS CHECKED GOOD PER FIM AND GE.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR HANDLE) · airframe 5,919 hrs · 4,505 cycles

ASH 6141 PHX - PAX DOOR OUTER HANDLE CAUTION MESSAGE. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO OVERHEAT) · airframe 5,914 hrs · 4,503 cycles

ASH 6644 PHX - AIRCRAFT INDICATED AN AFT CARGO OVERHEAT MESSAGE. MX INSPECTED THE BAY FOR OVERHEAT CONDITIONS, NONE WERE FOUND, RESET SYSTEM WITH NO FURTHER MSG NOTED.

Part: SEAL — DAMAGED (PAX DOOR) · airframe 5,732 hrs · 4,373 cycles

ASH 6579 PHX - MAIN PASSENGER DOOR SEAM/SEAL DAMAGED. MAINTENANCE REMOVED AND REPLACED THE SEAL/RETAINER.

Part: SMOKE — DETECTED (CABIN) · airframe 4,857 hrs · 3,767 cycles

ASH 6424 PHX-DSM. CAPT REPORTED SMOKE IN CABIN ON GROUND. MX RAN PACKS AND FOUND NO DEFECTS. MX RETURNED THE A/C TO SERVICE.

Part: SMOKE — DETECTED (CABIN) · airframe 4,837 hrs · 3,748 cycles

CAPTAIN REPORTED SMOKE IN CABIN ON GROUND WITH FORWARD AND AFT LAV SMOKE MASTER WARNING. CONTRACT MX INSPECTED AFT EQUIPMENT BAY EQUIPMENT AND DUCTING FOR INTEGRITY AND FOUND NO DEFECTS, INSPECTED AND OPS CHECKED BOTH FORWARD AND AFT LAV SMOKE DETECTORS AND OPS CHECKED NORMAL. PERFORMED APU NORMAL START AND LT & RT PACK OPERATION WITH NO REPEAT OF CABIN SMOKE. ACCOMPLISHED TWICE WITH NO REPEAT, NO FAULTS FOUND RETURNED TO SERVICE.

Part: CONTROLLER — UNCONTROLLABLE (CABIN PRESSURE) · airframe 3,977 hrs · 3,154 cycles

ASH 6931 MZT-LAX, THE CREW RETURNED THE AIRCRAFT TO THE FIELD DUE TO LOSS OF CABIN PRESSURIZATION CONTROL. MAINTENANCE IS CURRENTLY TROUBLESHOOTING. 11/27/04 MAINTENANCE REPLACED NR 1 CABIN PRESSURE CONTROLLER. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 3,539 hrs · 2,863 cycles

CENTER AISLE EMERGENCY EXIT LENS COVER WAS MISSING. MAINTENANCE REPLACED THE LENS COVER.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 3,533 hrs · 2,853 cycles

ASH 6451 PHX, OVERHEAD EMERGENCY LIGHT SIGN BETWEEN THE EXIT ROWS HAS A RED LENS MISSING. MX REPLACED THE RED LENS COVER.

Part: ODOR — DETECTED (CABIN) · airframe 22,252 hrs · 1,983 cycles

RETURNED TO FIELD DUE TO A REPORT OF A SMOKEY/OILY ODOR IN THE CABIN. IN THE COCKPIT THE LAV SMOKE WARNING MESSAGES WERE DISPLAYED. MX WAS CALLED. MX CONFIRMED THE PRESENCE OF THE ODOR, BUT WAS UNABLE TO DUPLICATE THE PROBLEM WHILE RUNNING THE ENGINES. MX COULD NOT DUPLICATE. NO PARTS USED

Part: ISOLATION VALVE — MALFUNCTIONED (THRUST REVERSER)

FLT 6747 - PHX-TUS - CAPTAIN ABORTED TAKEOFF DUE TO LEFT REVERSER UNSAFE CAUTION. MAINTENANCE TROUBLESHOT TO ISO CONTROL VALVE, R2 ISO CONTROL VALVE OPS CHECK GOOD. (M)