N244LR

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 28,453 hrs · 21,505 cycles

ALL EMER LIGHTS INOP/BATT DRAIN/SW OFF. ALOWED BATTERIES TO CHARGE/FA SW LEFT ON

Part: FIRE LOOP — FAILED (ZONE 100) · airframe 27,123 hrs · 20,468 cycles

LH BLEED DUCT WARNING/ ANTI-ICE OFF. REPOSITIONED FIRE LOOPS PREFORMED ENG RUNS NO FURTHER DEFECT

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 26,871 hrs · 20,278 cycles

RT BLEED DUCT WARNING MESSAGE- MX SECURED A LOOSE DUCTING CLAMP

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 26,484 hrs · 19,998 cycles

LH BLEED DUCT CAUT/DEPRESSURIZATON EMER DECLARED. INSP LOOP MT142 AND ACM PRE COOLER, NO DEFECTS.

Part: LIGHT — INOPERATIVE · airframe 24,847 hrs · 18,764 cycles

CAPT.'S FLASHLIGHT RED LED INOP. PLACED ON MEL.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 23,706 hrs · 17,969 cycles

PASSENGER COMPARTMENT FLOOR PANEL 231BLF WAS FOUND TO HAVE FRAYING DAMAGE ON THE OUTER STYLE 120 FIBERGLASS SCRIM PLY. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 53-00-47, FIGURE 5E, CMM COMCMM-030, EA 72-2021-141. DEFECT LOCATION:FS280.00 - FS349.00 231BLF

Part: SKIN — CORRODED (BS927-942 S21-22) · airframe 23,706 hrs · 17,969 cycles

FUSELAGE SKIN WAS FOUND WITH CORROSION DAMAGE BETWEEN FS 927 - FS 942, STR 21R -STR 22R. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-01-101-003-A04, IPC 53-82-83 FIGURE 10, EA 20-2021-161.

Part: SKIN — DENTED (LT WING SPOILER) · airframe 23,706 hrs · 17,969 cycles

LH WING INBOARD GROUND SPOILER LOWER SKIN WAS FOUND WITH TWO DENTS AT_SPS 21.80. PERFORMED PERMANENT REPAIR JAW CRJ 700/900 SRM 57-71-02-001-001-A01, FIGURE 57-71-02-991-801, ITEM 5A, EA 79-2021-216.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1088) · airframe 23,706 hrs · 17,969 cycles

UPPER CAP OF THE RBL9.00 FLOOR BEAM BETWEEN FS1000.00 - FS1088.20 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-43-001-001-A01, FIGURE 53-61-43-991-801, ITEM 2C, EA 79-2021-212.

Part: SLAT TRACK — CORRODED (NR 3 SLAT) · airframe 23,706 hrs · 17,969 cycles

SLAT TRACK 3-2 OF THE SLAT #3 ON THE LH & RH WING WERE FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 10, ITEM 90, EA 69-2021-131

Part: SLAT TRACK — CORRODED (NR 2 SLAT) · airframe 23,706 hrs · 17,969 cycles

SLAT TRACK 2-2 OF THE SLAT #2 ON THE LH & RH WING WERE FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 5, ITEM 85, EA 69-2021-132.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 23,706 hrs · 17,969 cycles

FWD BAGGAGE COMPARTMENT FLOOR PANELS (PN - A842101-501, A842106-501 & A842103-501) WERE FOUND TO HAVE (4) DELAMINATIONS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 CMM 25-52-17, EA 12-2021-199.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1031) · airframe 23,706 hrs · 17,969 cycles

UPPER CAP OF THE LBL27.00 FLOOR BEAM BETWEEN FS1015.00 - FS1031.00 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-43-001-001-A01, FIGURE 53-61-43-991-801, ITEM 3C, EA 79-2021-211.

Part: FITTING — DAMAGED (HANDRAIL) · airframe 23,706 hrs · 17,969 cycles

FS343.04 HANDRAIL FITTING (P/N: SH670-31905-6) AND CABLE ANCHOR FITTING (P/N:SH670-31882-19) WERE FOUND TO HAVE WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-23, FIGURE 53-21-23-995-818, ITEM 758, EA 72-2021-142. DEFECT LOCATION: HANDRAIL/FS343.04 & CABLE ANCHOR/PAX DOOR

Part: SKIN — DAMAGED (BS 565 S24-25R) · airframe 23,706 hrs · 17,969 cycles

LOWER FUSELAGE SKIN PANEL WAS FOUND WITH BURN DAMAGE AT FS565.00 BETWEEN STR 24R & STR 25R. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-991-806, ITEM 1B, EA 69-2021-129.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1088) · airframe 23,706 hrs · 17,969 cycles

FLOOR BEAM BETWEEN FS1000.00 AND FS1088.00 AT LBL 9.0 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-43, FIGURE 53-31-43-991-801, ITEM 2A, EA 83-2021-034.

Part: SLAT TRACK — CORRODED (NR 1 SLAT) · airframe 23,706 hrs · 17,969 cycles

SLAT TRACK 1-2 OF THE SLAT #1 ON THE LH & RH WING WERE FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 1, ITEM 85, EA 69-2021-133.

Part: ACCESS PANEL — DAMAGED (LT WING TE FLAP) · airframe 23,706 hrs · 17,969 cycles

RH LOWER ACCESS PANEL 684GB BETWEEN FLS 61 & FLS 69 WAS FOUND TO HAVE WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-52-01, FIGURE 57-52-01-991-802, EA 83-2021-036. DEFECT LOCATION: RH LNBOARD FLAP, 684GB, FLS 61 TO FLS 69

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 23,706 hrs · 17,969 cycles

PASSENGER COMPARTMENT FLOOR PANEL 231BLF WAS FOUND TO HAVE FRAYING DAMAGE ON THE OUTER STYLE 120 FIBERGLASS SCRIM PLY. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 53-00-47, FIGURE 5E, ITEM 25B, CMM COMCMM-030, EA 72-2021-141.

Part: SKIN — CORRODED (BS 927-947) · airframe 23,706 hrs · 17,969 cycles

FUSELAGE SKIN WAS FOUND TO HAVE CORROSION DAMAGE BETWEEN FS927 - FS942, STR. 21R -STR. 22R. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-01-101-003-A04, EA 20-2021-161.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1031) · airframe 23,706 hrs · 17,969 cycles

THE UPPER CAP OF THE LBL27.00 FLOOR SUPPORT BETWEEN FS1015.00 - FS1031.00 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-43-001-001-A01, FIGURE 53-61-43-991-801, ITEM 3C, EA 79-2021-211.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,337 hrs · 17,703 cycles

TWO EMERGENCY EXIT LIGHTS INOP IN GALLEY. REPLACED BULBS

Part: LANDING GEAR — INOPERATIVE (NOSE) · airframe 20,535 hrs · 15,670 cycles

GEAR DISAGREE, NLG WOULD NOT RETRACT. PLACED ON MEL.

Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 20,493 hrs · 15,641 cycles

GEAR DISAGREE WARNING REPLACED LAND GEAR SELECTOR VALVE

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

PERFORMED A MAJOR REPAIR BY REMOVING TCAS ANTENNA DOUBLER AND STRINGER 27 FORWARD SECTION AT FS 295 TO FS 310. INSTALLING A NEW SERVICABLE TCAS DOUBLER P/N SH670-32364-7 AND THE SAME SERVICABLE STRINGER 27 FORWARD SECTION IAW SRM 51-40-11-001-001-A01, 51-47-06-001-001-A01 AND 51-42-06-001-001-A01. REF MWC JOB# 41523351 OP# 92.

Part: INTERCOSTAL — CHAFED (FUSELAGE) · airframe 19,016 hrs · 14,499 cycles

PERFORMED A MAJOR REPAIR BY REMOVING, FABRICATING AND INSTALLING CARGO BEAM INTERCOSTAL AT FS 1031 TO FS 1047, P/N MM670-35328, IAW SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND MM670-35328-S01. REF MWC JOB# 41523351 OP# 79.

Part: SKIN PANEL — CHAFED (FUSELAGE) · airframe 19,016 hrs · 14,499 cycles

FUSELAGE LOWER SKIN PANEL BETWEEN 910 TO 927 HAS SEVERAL CHAFES AT STIRINGER 27. REPAIRED FUSELAGE LOWER SKIN PANEL IAW REO 670-53-00-290 REV. E.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

FS 319.70 FRAME SECTOR FLANGE IS CORRODED BETWEEN STRINGER 27 AND 26R.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

RBL 9.0 SEAT TRACK IS CORRODED BETWEEN FS 661.00+32 AND 672.00.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

LT AND RT STRINGER 27 INTERCOSTALS ARE CORRODED BETWEEN FS 349.00 AND 364.00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

SEAT RAIL AT LBL 9, FS 661-672 IS CORRODED IN SEVERAL LOCATIONS.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

FS 333.00 FRAME SECTOR FLANGE IS CORRODED BETWEEN STRINGER 27 AND 26R.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,449 cycles

LBL 9.0 SEAT TRACK IS CORRODED BETWEEN FS 374.00 AND 483.00.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 19,016 hrs · 14,499 cycles

FS280.0 CIRCUMFRENCIAL JOINT CORRODED BETWEEN STRINGER 25R AND 26L.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

CORROSION ON STRINGER 25R FWD OF F.S. 333.00.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

STRINGER 26R HAS TWO SMALL AREAS OF CORROSION BETWEEN FS 295.00 AND 310.00.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

CORROSION ON STRINGER 25R AFT OF FS 333.00.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

CORROSION ON STRINGER 26R AFT OF FS 333.00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

SEAT RAIL AT RBL 9 IS CORRODED IN SEVERAL LOCATIONS AT FS 669.00+40.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

SEAT RAIL AT LBL 9 IS CORRODED IN SEVERAL LOCATIONS AT FS 669.00+40.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

PERFORMED A MAJOR REPAIR BY REMOVING AND INSTALLING THE FS 280.00 FORWARD FLOOR SUPPORT ANGLE P/N: CC670-34094-1S, DUE TO CORROSION. IAW SRM 51-40-11-001-001-A01, 51-40-06-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. REF MWC JOB# 41523351 OP# 128.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

SEAT RAIL AT RBL 9.0 AT APPROX FS 349.00 IS CORRODED IN SEVERAL LOCATIONS.

Part: SEAT TRACK — CORRODED (BS 477) · corrosion level 2 · airframe 19,016 hrs · 14,499 cycles

SEAT TRACK IS CORRODED IN SEVERAL LOCATIONS AT RBL 9.0 AND F.S. 477.00.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,449 cycles

FS 280 LT AND RT CROSSBEAMS CORRODED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,449 cycles

SERVICE DOOR CUT OUT MOUNTING ANGLE AND THRESHOLD BRACKET SUPPORT ANGLES ARE CORRODED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,016 hrs · 14,449 cycles

AFT CARGO DOOR CUT-OUT SILL IS CORRODED.

Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 16,447 hrs · 12,529 cycles

GEAR DISAGREE WARNING ON LANDING.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,859 hrs · 12,081 cycles

NUMEROUS EXIT LIGHTS INOPERATIVE. CHARGED THE BATTERIES.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,771 hrs · 12,013 cycles

ROW 12 EXIT SIGN INOPERATIVE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 15,684 hrs · 11,937 cycles

ROW 12 LOWER EMERGENCY EXIT SIGNS INOPERATIVE. SECURED A LOOSE CONNECTOR ON THE BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,679 hrs · 11,932 cycles

ROW 12 EMERGGENCY FLOOD LIGHT INOPERATIVE. CHARGED THE BATTERIES.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,679 hrs · 11,932 cycles

ROW 12 EMERGENCY EXIT SIGN INOPERATIVE. CHARGED THE BATTERIES.

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,604 hrs · 11,873 cycles

MULTIPLE EMER LIGHTS INOP. CHARGED BATTERIES.

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,583 hrs · 11,857 cycles

EXIT SIGN LIGHTS INOP ROWS 11 & 12 LT AND RT SIDES. CHARGED BATTERIES.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,575 hrs · 11,852 cycles

MID CABIN FLOOR AND CEILING EXIT SIGNS INOPERATIVE. CHARGED THE BATTERIES.

Part: LIGHT — INOPERATIVE (EXTEROR) · airframe 15,436 hrs · 11,734 cycles

RIGHT FWD EXTERNAL EMERGENCY LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 15,436 hrs · 11,734 cycles

LEFT MID EXTERNAL EMERGENCY LIGHT INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,430 hrs · 11,726 cycles

ROW 12 LOWER EMERGENCY EXIT SIGNS INOPERATIVE. CHARGED THE BATTERIES.

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,352 hrs · 11,662 cycles

ROW 12 AND 13 FLOOR LEVEL EXIT SIGNS INOP. ALLOWED BATTERIES TO CHARGE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,317 hrs · 11,632 cycles

ROW 12 AND 13 FLOOR LEVEL EXIT SIGNS INOPERATIVE. CHARGED BATTERIES

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,234 hrs · 11,564 cycles

ROW 12 LOWER EXIT SIGNS, LEFT AND RIGHT, INOPERATIVE. CHARGED THE BATTERIES.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 15,201 hrs · 11,540 cycles

CAPTAIN'S FLASHLIGHT INOPERATIVE. REPLACED THE BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 14,932 hrs · 11,322 cycles

EMERGENCY EXIT LIGHTS AT ROW 12 INOP. RECHARGED BATTERY PACKS.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 14,737 hrs · 11,171 cycles

50 PERCENT OF CABIN EMERGENCY LIGHTS FOUND INOPERATIVE. R & R THE FA PANEL EMERGENCY LIGHT SWITCH.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,669 hrs · 11,114 cycles

MID CABIN FWD FACING EXIT SIGN INOPERATIVE. REPLACED THE NR 2 BATTERY

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,669 hrs · 11,114 cycles

ROW 13 LT & RT EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED THE NR 2 BATTERY.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 14,286 hrs · 10,795 cycles

FWD FA FLASHLIGHT INOP. PLACED ON MEL.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 13,231 hrs · 10,042 cycles

FWD FA'S FLASHLIGHT INOP. REPLACED BATTERY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,571 hrs · 9,553 cycles

SERVICE DOOR LOWER EMERGENCY FLOOD LIGHT HAD TWO BULBS INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,571 hrs · 9,553 cycles

PAX DOOR LOWER EMERGENCY FLOOD LIGHT HAD TWO BULBS INOPERATIVE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 12,442 hrs · 9,461 cycles

GEAR DISAGREE WARNING ON GEAR EXTENSION.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,264 hrs · 9,661 cycles

BOTH SIDE ROW 13 EMERGENCY EXIT SIGNS INOPERATIVE. MAINTENANCE TROUBLESHOOTING.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 12,210 hrs · 9,290 cycles

FS 280.00 LT CROSSBEAM IS CORRODED IN CENTER AREA.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 12,210 hrs · 9,290 cycles

FS 280.00 RT CROSSBEAM IS CORRODED AT LBL 12.00.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 11,962 hrs · 9,087 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. REPLACED BATTERIES, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,147 hrs · 8,432 cycles

GALLEY EXIT SIGN 1 BULB INOPERATIVE.

Part: BULB — INOPERATIVE (GALLEY LIGHT) · airframe 11,154 hrs · 8,437 cycles

FORWARD GALLEY LIGHT INOPERATIVE FOUND TO BE FAULTY LIGHT BULB. REMOVED AND REPLACED THE BULB & OPS CHECKED GOOD

Part: ACM — FAILED (LEFT) · airframe 10,924 hrs · 8,259 cycles

SMOKE IN CABIN AND FLIGHT DECK AFTER NR 1 ENGINE START. EMERGENCY DE-BOARDING OF PASSENGERS ON THE RAMP AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT TO LT ACM AND PLACED LT PACK ON MEL.

Part: BATTERY PACK — INOPERATIVE (FWD FLASHLIGHT) · airframe 9,835 hrs · 7,398 cycles

CAPTAIN FLASHLIGHT INOPERATIVE DURING ROUTINE MAINTENANCE OPERATIONAL TEST. FLASHLIGHT BATTERY REPLACED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 9,061 hrs · 6,848 cycles

F/O FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT.

Part: BATTERY PACK — INOPERATIVE (FWD FLASHLIGHT) · airframe 8,863 hrs · 6,703 cycles

FWD F/A FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-60-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 8,478 hrs · 6,473 cycles

EMERGENCY EXIT LIGHT INOPERTIVE. CHANGED BATTERIES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,204 hrs · 6,287 cycles

RT FWD EXIT EMERGENCY LIGHT INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 8,204 hrs · 6,287 cycles

RT REAR EXT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS, OPS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,249 hrs · 5,594 cycles

CABIN DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 5,035 hrs · 3,716 cycles

FWD F/A FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 4,984 hrs · 3,676 cycles

FORWARD F/A FLASHLIGHT INOPERATIVE. SECURED END CAP ON FLASHLIGHT