N815SK

Part: PACKING — FAILED (NLG STRUT) · airframe 25,635 hrs · 16,041 cycles

GEAR DISAGREE AFTER TAKEOFF AND NWS IN-OP CAUTION MESSAGE. REPACKED NLG STRUT AND PERFORMED FULL STRUT SERVICE AND PERFORMED LANDING GEAR SWINGS. LEAK CHECK AND OPS CHECKED GOOD.

Part: FRAME — CORRODED (BS 349) · airframe 25,207 hrs · 15,763 cycles

AVIONICS BAY LOWER FRAME AT BS 349 CORRODED. R & R THE FRAME IAW SRM. PRESSURE CHECKS GOOD AT THIS TIME.

Part: FRAME — CORRODED (BS 333) · airframe 25,207 hrs · 15,763 cycles

AVIONICS BAY LOWER FRAME AT BS 333 CORRODED. INSTALLED A NEW FRAME IAW SRM AND REO. PRESSURIZATION CHECK GOOD AT THIS TIME.

Part: FRAME — CORRODED (BS 295) · airframe 25,207 hrs · 15,763 cycles

AVIONICS BAY LOWER FRAME AT BS 295 CORRODED. INSTALLED A NEW FRAME IAW SRM AND REO. PRESSURIZATION CHECKED GOOD.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 25,207 hrs · 15,763 cycles

INTERCOSTAL IN AVIONICS BAY BS 364 - 349, STR 27L CORRODED. R & R THE INTERCOSTAL IAW SRM. PRESSURE CHECKED GOOD.

Part: DOUBLER — CORRODED (TCAS ANTENNA) · airframe 25,207 hrs · 15,763 cycles

TCAS ANTENNA DOUBLER IN AVIONICS BAY CORRODED. R & R TCAS ANTENNA DOUBLER IAW AMM. PRESSURE CHECKED GOOD.

Part: STRINGER — CORRODED (BS 661) · airframe 25,207 hrs · 15,763 cycles

STRINGER 19R BS 661+90 CORRODED. R & R THE STRINGER IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 25,207 hrs · 15,763 cycles

CORRODED INTERCOSTAL IN AVIONICS BAY BS 364 - 349, STR 27R. R & R THE INTERCOSTAL IAW SRM. PRESSURE CHECKS GOOD AT THIS TIME.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 25,207 hrs · 15,763 cycles

PAX DOOR FWD INTERCOSTAL CORRODED. R & R IAW SRM. PRESSURE CHECK GOOD.

Part: SKIN — DENTED (NR 1 SLAT) · airframe 22,492 hrs · 13,953 cycles

RT WING L/E NR 1 SLAT HAS DENT FROM BIRDSTRIKE. DENT IS APPROXIMATELY 3 FT FROM INBD AND 2" FROM BOTTOM OF SLAT. DENT IS APPROX 2.5" IN DIAMETER AND .035" DEEP. RO: 03/27/2015, FILLED DENT IAW REO.

Part: SKIN — DENTED (RT NACELLE) · airframe 21,397 hrs · 13,218 cycles

RT ENGINE COWL IS DENTED OUT OF LIMITS. REPLACED IAW AMM.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 20,908 hrs · 12,861 cycles

FORWARD F/A FLASHLIGHT DOES NOT BLINK. R & R FWD F/A FLASHLIGHT BATTERY, OPS CHECKED GOOD IAW AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,359 hrs · 12,499 cycles

RT NR 3 OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT AFT OVERWING SECTION EMERGENCY LIGHT BULB AND CRACKED LENS COVER IAW AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,323 hrs · 12,476 cycles

RIGHT FLOOR SEAT RAIL AT FS477.00 THRU 573.00 CORRODED. C-CHECK, R & R RT FLOOR SEAT RAIL AT FS477.00 - FS 573.00 IAW AMM.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 20,323 hrs · 12,476 cycles

PAX DOOR MID-CAP ANGLE HAS CORROSION. C-CHECK, REPLACED NEW PAX DOOR MID CAP ANGLE, PN SH670-31825-7 IAW SRM.

Part: STRUCTURE — CHAFED (FUSELAGE) · airframe 20,323 hrs · 12,476 cycles

BOTTOM OF FUSELAGE CHAFED AT APPROXIMATELY FS969, STGR27, C-CHECK, BLENDED CHAFE ON FUSELAGE A FS 969, STR 27 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,323 hrs · 12,476 cycles

LT SIDE FLOOR SEAT TRACK HAS CORROSION AT APPROXIMATELY FS 612.00 ON LBL 9.00. C-CHECK, REPAIRED LT SIDE FLOOR SEAT TRACK AT APPROXIMATELY FS 612.00 ON LBL 9.00. LARGEST MATERIAL LOSS FOUND AT LOCATION "Z". STARTING GAP- 0.420", REMAINING GAP- 0.430", MATERIAL REMOVED- 0.010", WITHIN LIMITS IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,323 hrs · 12,476 cycles

SIDE SEAT RAIL HAS CORROSION AT APPROXIMATELY FS 746.00 ON STG 15L. C-CHECK, REPAIRED SIDE SEAT RAIL AT APPROXIMATELY FS 746.00 ON STG 15L. LARGEST MATERIAL LOSS FOUND AT LOACTION "Z". STARTING GAP- 0.420", REMAINING GAP- 0.459", MATERIAL REMOVED- 0.039", WITHIN LIMITS IAW REO.

Part: STRIKER — DENTED (FUSELAGE) · airframe 20,323 hrs · 12,476 cycles

PASSENGER DOOR EXTERNAL SURROUND STRUCTURE AT FS 310, UPPER SECTION HAS A DENT. C-CHECK, REPAIRED PASSENGER DOOR SURROUND SEAL STRIKER IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,323 hrs · 12,476 cycles

LT SIDE FLOOR SEAT TRACK HAS CORROSION AT APPROXIMATELY FS 693.00 ON LBL 9.00. C-CHECK, REPAIRED LT SIDE FLOOR SEAT TRACK AT APPROXIMATELY FS 693.00 ON LBL 9.00. LARGEST MATERIAL LOSS FOUND AT LOCATION "Z". STARTING GAP- 0.420", REMAINING GAP- 0.429", MATERIAL REMOVED- 0.009", WITHIN LIMITS IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,323 hrs · 12,476 cycles

LEFT SIDE FLOOR SEAT TRACK HAS CORROSION AT APPROXIMATELY FS 661.00 + 82.00 ON LBL 9.00. C-CHECK, REPAIRED LT SIDE FLOOR SEAT TRACK AT APPROXIMATELY FS 661.00 + 82.00 ON LBL 9.00. LARGEST MATERIAL LOSS FOUND AT LOCATION "Z". STARTING GAP- 0.420", REMAINING GAP- 0.436", MATERIAL REMOVED- 0.016", WITHIN LIMITS IAW REO.

Part: STRIKER — DENTED (FUSELAGE) · airframe 20,323 hrs · 12,476 cycles

PASSENGER DOOR EXTERIOR SURROUND STRUCTURE AT FS 349, UPPER SECTION HAS DENT. C-CHECK, REPAIRED PASSENGER DOOR SURROUND SEAL STRIKER IAW REO.

Part: SUPPORT — CHAFED (HAND RAIL) · airframe 20,323 hrs · 12,476 cycles

PAX DOOR AFT HAND RAIL OTBD SUPPORT ARM CHAFED FROM PAX DOOR SUPPORT WHEEL. C-CHECK, BLENDED CHAFE ON PAX DOOR AFT HANDRAIL OTBD SUPPORT ARM ORIGINAL MATERIAL THICKNESS .083" REMAINING MATERIAL THICKNESS .078" MATERIAL LOSS OF .005" IS WITHIN LIMITS IAW STS EA.

Part: LEVER — CHAFED (PAX DOOR) · airframe 20,323 hrs · 12,476 cycles

PAX DOOR FWD PULL-IN LEVER CHAFED. C-CHECK, BLENDED CHAFED AREA, REQUESTED NDT FOR CRACK CHECK NO DEFECTS WERE NOTED. ORIGINAL MATERIAL THICKNESS WAS 1.700". AFTER RE-WORK MATERIAL THICKNESS IS 1.665". A TOTAL LOSS OF .035. TOTAL ALLOWABLE LOSS IS .050". PAX DOOR FWD PULL-IN LEVER FOUND TO BE WITH-IN LIMITS IAW REO.

Part: ROD — CHAFED (RT WING TE FLAP) · airframe 20,323 hrs · 12,476 cycles

RIGHT INBD FLAP VANE ACTUATOR ROD UNDER ACCESS PANEL 684CB CHAFED ON CHROME SURFACE. C-CHECK, BLENDED CHAFE ON RT INBD FLAP VANE ACTUATOR ROD UNDER PANEL 684CB, AND FOUND TO BE WITHIN LIMITS, IAW REO.

Part: ROD — CHAFED (RT WING TE FLAP) · airframe 20,323 hrs · 12,476 cycles

RIGHT INBD FLAP VANE ACTUATOR ROD UNDER ACCESS PANEL 684AB CHAFED ON CHROME SURFACE. C-CHECK, BLENDED CHAFE ON RT INBD FLAP VANE ACTUATOR ROD UNDER PANEL 684AB, AND FOUND TO BE WITHIN LIMITS IAW REO.

Part: SUPPORT ARM — CHAFED (CARGO DOOR) · airframe 20,323 hrs · 12,476 cycles

FWD BAGGAGE BAY DOOR FWD LOWER SUPPORT ARM CHAFED ON TOP SIDE. C-CHECK, BLENDED CHAFE ON FWD BAGGAGE BAY DOOR FWD LOWER SUPPORT ARM TOP SIDE IAW SRM AND STS EA.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 20,323 hrs · 12,476 cycles

PAX DOOR FWD LOWER CAM LATCH HAS CORROSION UNDERNEATH. C-CHECK, REMOVED CORROSION FROM UNDERNEATH FWD LOWER CAM LATCH OF PAX DOOR IAW SRM.

Part: ATTACH BRACKET — CRACKED (PAX DOOR) · airframe 20,323 hrs · 12,476 cycles

PAX DOOR AFT ANGLE BRACKET CRACKED NEXT TO PULL-IN CABLE ASSIST WHEEL BRACKET. C-CHECK, REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO.

Part: SUPPORT — CHAFED (PAX DOOR) · airframe 20,323 hrs · 12,476 cycles

PAX DOOR SUPPORT WHEEL CHAFED. C-CHECK, BLENDED CHAFE ON PAX DOOR SUPPORT WHEEL IAW STS EA.

Part: ROD — CHAFED (RT WING TE FLAP) · airframe 20,323 hrs · 12,476 cycles

RT INBD FLAP VANE ACTUATOR ROD UNDER ACCESS PANEL 684DB CHAFED ON CHROME SURFACE. C-CHECK, BLENDED CHAFE ON RT INBD FLAP VANE ACTUATOR ROD UNDER PANEL 684DB, AND FOUND TO BE WITHIN LIMITS IAW REO AND AMM.

Part: ENGINE — VIBRATION (LEFT) · airframe 19,941 hrs · 12,242 cycles

AT FL 380, ROUGHLY 30 SECONDS AFTER REDUCING TL TO CRUISE SETTING A SIGNIFICANT VIBRATION WAS FELT THROUGHOUT THE AIRFRAME. REPLACED LT ENGINE ASSY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,951 hrs · 11,572 cycles

NR 1 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#4503 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,822 hrs · 11,489 cycles

NR 5 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#4693 RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,723 hrs · 10,819 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 14 BURNED OUT, REPLACED LAMPS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,398 hrs · 10,612 cycles

EMERGENCY LIGHT AT ROW 8 IS BURNED OUT. (FLT 4661) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,858 hrs · 10,250 cycles

THIRD FROM REAR OVERHEAD CABIN EMERGENCY LIGHT IS BURNED OUT. (FLT 4618) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,872 hrs · 9,629 cycles

OVERWING EXIT ROW LIGHT PARTIALLY INOPERATIVE AT ROW 13 ON THE RIGHT SIDE. (FLT 4618) RELAMPED EMERGENCY LIGHTS AT FOOT LEVEL AT ROW 13C/D SIDE IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,348 hrs · 9,249 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4452) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,303 hrs · 9,218 cycles

NR 7 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4550) RELAMPED EMERGENCY LIGHT.

Part: PROXIMITY SENSOR — OUT OF RIG (PAX DOOR) · airframe 15,181 hrs · 9,128 cycles

PASSENGER DOOR LATCH CAUTION MESSAGE. GROUND DOOR WARNING WAS INTERMITTENT ABOUT 2 SECONDS. RIGGED PX101 IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,153 hrs · 9,106 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 20 IS OUT. (FLT 4557) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,093 hrs · 9,065 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 17 IS OUT. (FLT 4452) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,800 hrs · 8,873 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 17 IS OUT. (FLT 4727) RELAMPED EMERGENCY LIGHT.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LANDING GEAR) · airframe 14,436 hrs · 8,637 cycles

GEAR UP DISAGREE WARNING MESSAGE. (FLT 4467) ADJUSTED THE CLEARANCE OF PROXIMITY SENSORS PX03 AND PX11.

Part: WARNING LIGHT — FALSE INDICATION (RT A/C PACK) · airframe 14,376 hrs · 8,602 cycles

FLT 4452, RIGHT PACK FAULT. PERFORMED OPERATIONAL CHECK OF RIGHT PACK IN REFERENCE TO AMM. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,376 hrs · 8,602 cycles

FLT 4817, OVERHEAD EMERGENCY LIGHT AT ROW 17 IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,284 hrs · 8,540 cycles

ROW 17 EMERGENCY LIGHT INOPERATIVE. (FLT 4518) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,267 hrs · 8,532 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 14 IS OUT. (FLT 4680) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,832 hrs · 8,235 cycles

THE 3RD FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4479) RELAMPED EMERGENCY LIGHT.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 13,585 hrs · 8,063 cycles

F/O'S WINDSHIELD CRACKED WITH CREW REPORTING SPARKS. (FLT 4756) REPLACED RIGHT SIDE WINDSHIELD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,555 hrs · 8,038 cycles

NR 6 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4663) RELAMPED EMERGENCY LIGHT.

Part: SIGN — INOPERATIVE (CABIN) · airframe 13,555 hrs · 8,038 cycles

SIDEWALL EMERGENCY EXIT SIGN BY 13A LIGHTING IS OUT. (FLT 4765) RELAMPED EMERGENCY SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,493 hrs · 7,999 cycles

THE 3RD FROM BACK OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4701) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,401 hrs · 7,936 cycles

THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4599) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,097 hrs · 7,711 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 14 IS OUT. (FLT 4691) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,034 hrs · 7,660 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4648) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,001 hrs · 7,641 cycles

NR 6 CEILING EMERGENCY LIGHT IS OUT. (FLT 4701) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,902 hrs · 7,550 cycles

NR 6 OVERHEAD EMERGENCY LIGHT NOT ILLUMINATING. (FLT 4512) RELAMPED EMERGENCY LIGHT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 12,594 hrs · 7,351 cycles

FS 280 FLOORBEAM IS CRACKED AND CORRODED. (C-CHECK) REPLACE FLOORBEAM PER SRM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 11,589 hrs · 6,723 cycles

EMERGENCY LIGHT STRIP ON FLOOR IN GALLEY IS MISSING. (FLT 4811) REPLACED MISSING PHOTO ILLUMINESCENT STRIP AT LEFT SIDE OF GALLEY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,224 hrs · 6,497 cycles

CEILING EMERGENCY LIGHT AT ROW 17 DOES NOT LIGHT. (FLT 4849) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,176 hrs · 6,469 cycles

FORWARD EMERGENCY OVERHEAD LIGHT OUT. (FLT 4695) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,861 hrs · 5,662 cycles

SECOND TO LAST EMERGENCY CEILING LIGHT INOP. (FLT 4691) RELAMPED EMERGENCY LIGHT.

Part: ADC — MALFUNCTIONED (NR 1) · airframe 8,861 hrs · 5,074 cycles

ALTIMETER SPLIT AT CRUISE ALTITUDE. (FLT 4482) REPLACED NR 1 ADC AND NR 2 PITOT STATIC HEAD.

Part: STATIC SYSTEM — CONTAMINATED (PITOT/STATIC SYS) · airframe 8,861 hrs · 5,074 cycles

ALTIMETER SPLIT AT ALTITUDE. (FLT 4724) PURGED STATIC SYSTEM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,690 hrs · 4,986 cycles

NR 6 EMERGENCY OVERHEAD LIGHT INOP. (FLT 4783) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 8,496 hrs · 4,880 cycles

FLT 4652 - SECOND TO LAST CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. RELAMPED.

Part: BEAM — CORRODED (FUSELAGE) · airframe 7,972 hrs · 4,597 cycles

FS280 BEAM CORRODED. (C CHECK) BEAM REPLACED PER REO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,535 hrs · 4,898 cycles

RIGHT LOWER BULKHEAD WEB STIFFENING ANGLE CRACKED. (C CHECK) REPAIRED PER SRM AND AMM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 7,666 hrs · 4,432 cycles

CABIN EMERGENCY - PHOTOLUMINESCENT LIGHT STRIP OPPOSITE LAV DOOR MISSING. (FLT 4577) REPLACED PHOTOLUMINESCENT LIGHT STRIP ON LT SIDE OF GALLEY FLOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,420 hrs · 4,314 cycles

NR 6 CEILING LEVEL EMERGENCY LIGHT INOP. (FLT 4455) RELAMPED EMERGENCY LIGHT.

Part: SIGN — LOOSE (CABIN) · airframe 7,420 hrs · 4,314 cycles

EMERGENCY EXIT SIGN ABOVE THE GALLEY SERVICE DOOR LOOSE. (FLT 4455) RE-SECURED SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,942 hrs · 4,060 cycles

FLOOR LEVEL EMERGENCY LIGHT PANEL FWD OF MAIN CABIN DOOR INOP. (FLT 4662) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,942 hrs · 4,060 cycles

FORWARD EMERGENCY LIGHT PANEL BY SERVICE DOOR INOP. (FLT 4662) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 6,826 hrs · 3,995 cycles

FLT 4703 - THIRD FROM AFT EMERGENCY LIGHT INOP. RELAMPED.

Part: RELAY — FAULTY (EMERGENCY LIGHTS) · airframe 3,350 hrs · 1,943 cycles

FLT NR 4000 - THE EMERGENCY LIGHTS COME ON WHEN IN THE "ARMED" POSITION. REPLACED K135 RELAY IN JB11 IN ACCORDANCE WITH CRJ 900 MAINTENANCE MANUAL 20-00-00. CHECKS GOOD.