N557NN

Part: SEAL — OUT OF POSITION (ZONE 800) · airframe 25,205 hrs · 22,489 cycles

LOUD NOISE COMING FROM PAX DOOR IN FLIGHT. FOUND SEAL OF UPPER PORTION OF PAX DOOR OUT OF RETAINER. REINSTALLED SEAL INTO RETAINER, CLEANED AND LUBRICATED DOOR SEAL IAW AMM 52-11-07-400-801-A02-PSA. PERFORMED INSPECTION OF DOOR SEAL IAW 52-11-07-210-801-A01 AND FOUND NO FURTHER DEFECTS. PERFORMED PRESSURIZATION TEST OF AIRCRAFT IAW AMM 21-31-00-910-801-A02-PSA AND TEST WAS SUCCESSFUL. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: SKIN — WORN (ZONE 600) · airframe 20,506 hrs · 18,533 cycles

WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN WAS REPAIRED PER EA 23-C9-57-1600 REV IR SECTION III - PERMANENT REPAIR, EA 23-C9-57-1627 REV IR SECTION III - PERMANENT REPAIR, EA 23-C9-57-1628 REV IR SECTION III - PERMANENT REPAIR, EA 23-C9-57-1629 REV IR SECTION III - PERMANENT REPAIR, EA 23-C9-57-1630 REV IR SECTION III - PERMANENT REPAIR

Part: WEB — CRACKED (ZONE 100) · airframe 20,506 hrs · 18,533 cycles

CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.0 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 20,506 hrs · 18,533 cycles

DURING INSPECTION OF THE TASK CARD TRFKE001WBUB:53-20-220-JIC, IT WAS DETECTED CORROSION ON KICK PLATE AT PASSENGER DOOR SURROUND STRUCTURE. KICK PLATE AT PASSENGER DOOR SURROUND STRUCTURE WAS FOUND OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01

Part: SEAL DEPRESSOR — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,506 hrs · 18,533 cycles

CORROSION ON LWR STRIKER SEAL BTW FS=319 / FS=349 AT GALLEY SERVICE DOOR SURROUND STRUCTURE. LWR STRIKER SEAL BTW FS=319 / FS=349 AT GALLEY SERVICE DOOR SURROUND STRUCTURE. WAS FOUND OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-002-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01

Part: HINGE — CORRODED (ZONE 600) · airframe 20,514 hrs · 18,539 cycles

AFTER AILERON BUSHING REMOVAL, CORROSION WAS FOUND ON OUTBOARD LUG HINGE 2 OF AILERON RH. OUTBOARD LUG HINGE 2 OF AILERON RH WAS REPAIRED PER 670-57-61-237 REV. --

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,506 hrs · 18,533 cycles

CORROSION ON INTERCOSTAL BTW FS=310 / FS=319 AND STGR 20RH AT FUSELAGE INTERNAL STRUCTURE, BELOW FLOOR. INTERCOSTAL BTW FS=310 / FS=319 AND STGR 20RH AT FUSELAGE INTERNAL STRUCTURE, BELOW FLOOR WAS EVALUATED AND FOUND OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 AND REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,514 hrs · 18,539 cycles

CORROSION ON INTERCOSTAL BTW FS=319 / FS=349 AND STGR 20RH AT FUSELAGE INTERNAL STRUCTURE, BELOW FLOOR. INTERCOSTAL BTW FS=319 / FS=349 AND STGR 20RH AT FUSELAGE INTERNAL STRUCTURE, BELOW FLOOR WAS EVALUATED AND FOUND OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 AND REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01.

Part: SKIN — DAMAGED (ZONE 200) · airframe 20,506 hrs · 18,533 cycles

LIGHTNING STRIKE (1EAS) ON FS1015.00 BTW STGR#2 TO STGR#3 LH SIDE, LIGHTNING STRIKES (1EAS) ON FS1069.00 BTW STGR#2 TO STGR#3 LH SIDE, LIGHTNING STRIKES (1EAS) BTW FS1108.00 TO FS1126.00 AND STGR#4 TO STGR#5 LH SIDE OF THE REAR FUSELAGE. LIGHTNING STRIKE (1EAS) ON FS1015.00 BTW STGR#2 TO STGR#3 LH SIDE, LIGHTNING STRIKES (1EAS) ON FS1069.00 BTW STGR#2 TO STGR#3 LH SIDE, LIGHTNING STRIKES (1EAS) BTW FS1108.00 TO FS1126.00 AND STGR#4 TO STGR#5 LH SIDE OF THE REAR FUSELAGE WERE REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03

Part: CANISTER — CRACKED (ZONE 500) · airframe 20,514 hrs · 18,539 cycles

CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.--

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,514 hrs · 18,539 cycles

CORROSION ON MID CAP, LOCATED BTW FS=310 / FS=349 AND LBL 40" AT FUSELAGE FLOOR STRUCTURE. NEW MID CAP, LOCATED BTW FS=310 / FS=349 AND LBL 40" AT FUSELAGE FLOOR STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,514 hrs · 18,539 cycles

CORROSION ON FLOOR BEAM LBL 9 BTW FS 1015.00- FS 1069.00. FLOOR BEAM LBL 9 BTW FS 1015.00- FS 1069.00 WAS REPAIRED PER EA 23-C9-53-1583 REV IR- SECTION III - PERMANENT REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 20,514 hrs · 18,539 cycles

SEVERAL CORROSION ON FLOOR SEAT TRACK 9LBL/9RBL FROM FS364.00 TO FS720.00 AT CABIN PAX. SEAT TRACK 9LBL/9RBL FROM FS364.00 TO FS720.00 AT CABIN PAX WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12).

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,514 hrs · 18,539 cycles

CORROSION ON SEAT RAIL BTW FS720.85 TO FS977.00 OF LBL9 (2EA) AND RBL9 (2EA). SEAT RAIL BTW FS720.85 TO FS977.00 OF LBL9 (2EA) AND RBL9 (2EA) WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12).

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 20,514 hrs · 18,539 cycles

CORROSION ON FLOOR BEAM LBL 27 BTW FS 1000.00- FS 1047.00. FLOOR BEAM LBL 27 BTW FS 1000.00- FS 1047.00 WAS REPAIRED PER EA 23-C9-53-1589 REV IR- SECTION III - PERMANENT REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,514 hrs · 18,539 cycles

CORROSION ON FLOOR BEAM RBL 9 BTW FS 1015.00- FS 1047.00. FLOOR BEAM RBL 9 BTW FS 1015.00- FS 1047.00 WAS REPAIRED PER REO 690-53-61-1278 REV. --

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,506 hrs · 18,533 cycles

CORROSION ON KICK PLATE ANGLE BTW FS=319 / FS=349 AT GALLEY SERVICE DOOR SURROUND STRUCTURE. KICK PLATE ANGLE BTW FS=319 / FS=349 AT GALLEY SERVICE DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,514 hrs · 18,539 cycles

CORROSION ON INTERCOSTAL IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 20,506 hrs · 18,533 cycles

CORROSION ON BRACKET MACHINED (8E/AS) OF FLOOR STRUCTURE AT FWD CARGO COMPARTMENT BTW. FS 517 TO FS 661 AND BTW STGR 23RH/22LH. BRACKET MACHINED (8E/AS) OF FLOOR STRUCTURE AT FWD CARGO COMPARTMENT BTW. FS 517 TO FS 661 AND BTW STGR 23RH/22LH WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-32-58-101-001-A01AND WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01, CRJ-900 SRM 51-42-16-001-001-A01 AND CRJ-900 SRM 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,514 hrs · 18,539 cycles

SEVERAL CORROSION ON SIDE SEAT TRACK LH/RH FROM FS364.00 TO FS977.00 AT CABIN PAX. ON SIDE SECTION SEAT TRACK LH FROM FS364.00 TO FS720.85, SECTION SIDE SEAT TRACK LH FROM FS913.00 TO FS977.00 AND SECTION SIDE SEAT TRACK RH FROM FS 565.00 TO 669.40 WERE CLEANED AND NO DAMAGE FOUND PER CRJ 900 SRM 51-26-00-001-001-A01 AND SRM 51-11-00-001-001-A01, EVALUATED, ON SECTION SIDE SEAT TRACK RH FROM FS364.00 TO FS565.00, SECTION SIDE SEAT TRACK RH FROM FS669.40 TO 761.85 AND SECTION SIDE SEAT TRACK LH FROM FS744.15 TO FS913.00,THEREFORE IT IS OUT LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 SRM 53-51-49-101-001-A02 AND NEW SECTION SIDE SEAT TRACK RH FROM FS364.00 TO FS565.00, SECTION SIDE SEAT TRACK RH FROM FS669.40 TO 761.85, SECTION SIDE SEAT TRACK RH FROM FS785.15 TO FS977.00 AND SECTION SIDE SEAT TRACK LH FROM FS744.15 TO FS761.85 AND SECTION SIDE SEAT TRACK LH FROM FS785.15 TO FS913.00 WERE REPLACED PER CRJ900 AMM 53-00-49-400-801 (CONFIG A12).

Part: SKIN — SCRATCHED (BS 230-234) · airframe 20,506 hrs · 18,533 cycles

SCRATCH BTW FS230.00 TO FS234.00 AND STGR#21 TO STGR#20 LH SIDE FWD FUSELAGE. SCRATCH BTW FS230.00 TO FS234.00 AND STGR#21 TO STGR#20 LH SIDE FWD FUSELAGE WAS REPAIRED PER EA 23-C9-53-1555 REV.IR SECTION III - PERMANENT REPAIR

Part: FAIRING — ERODED (ZONE 300) · airframe 20,506 hrs · 18,533 cycles

EXTENSIVE EROSION ON UPPER FAIRING 326BT. UPPER FAIRING 326BT WAS REPAIRED PER CRJ-900 S.R.M 51-73-00-201-001-A01 PAR. 4. B IN REFERENCE TO EA 21-C9-55-976 REV. A SECTION III PERMANENT REPAIR

Part: SKIN — DENTED (ZONE 200) · airframe 20,514 hrs · 18,539 cycles

SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1144.00 TO REAR SPAR DATUM STABILIZER 67.5%. SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1144.00 TO REAR SPAR DATUM STABILIZER 67.5%. WAS REPAIRED PER EA 23-C9-53-1530 REV IR SECTION LLL - PERMANENT REPAIR.

Part: ACM — WARNING MESSAGE (RIGHT) · airframe 20,240 hrs · 18,300 cycles

LEFT BLEED DUCT WARNING MSG / PERFORMED FAULT CONFIRMATION PER B1 349536 IAW CRJ900 FIM 36-21-01-810-803-A02 STEPS 1 TO 3B. NO DEFECTS NOTED. THIS A/C HAS BEEN INSPECTED AND IS SAFE FOR FLIGHT INTENDED AS PER FERRY PERMIT NUMBER 9974. REMOVED AND REPLACED RH PLENUM IAW AMM 21-51-02-000/400-801-A02. REMOVED AND REPLACED ACM IAW AMM 21-51-08-000/400-801-A01. OPS CHECK AND LEAK CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 20,217 hrs · 18,281 cycles

AFTER LEAVING BHM THE CREW RECEIVED A LEFT BLEED WARNING MESSAGE. / NO CURRENT FAULT FOUND. IN FAULT HISTORY FOUND B1 CODE 349536. TROUBLESHOT IAW CRJ 900 FIM 36-21-01-810-813. FOUND MT137 BLEED LOOP TOUCHING AIR DISTRIBUTION DUCT. ADJUSTED DISTANCE, PRESSURIZED AIR-CONDITIONING SYSTEM & WAITED 10 MINUTES. NO WARNING OR STATUS MSG DETECTED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 20,147 hrs · 18,218 cycles

L BLEED DUCT WARNING / INTEROGATED MDC AND FOUND IT TO BE FLAGGING MT137 AT 78%. INSPECTED LOOP AND FOUND NO DAMAGE OR LEAKS IAW CRJ 900 AMM 36-21-01-810-813-A02. BLEED LEAK TEST GOOD AND AILC BITE CHECK GOOD IAW CRJ 900 AMM 36-21-00-710-801-A01 AND 30-12-12-740-801-A01.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 19,877 hrs · 17,987 cycles

AFTER FLAPS RETRACTION ON TAKEOFF IB FLT SPLRS, IB SPOILERONS, PITCH FEEL, IB GND SPOILERS CAUTION AND STAB FAULT, STAB CH 1, RUD LIMITER STAUTS MESSAGES / PERFORMED S POST 1 AND 2 IAW CRJ 900 AMM 27-61-05-740-801-A03, PERFORMED OPS CK OF THE HORIZONTAL STAB TRIM SYS IAW CRJ 900 AMM 27-40-00-710-801-A02 AND PERFORMED OPS CK OF FLAPS / SLATS SYS IAW CRJ 900 27-50-00-710-801-A02. OPS CHECK GOOD AT THIS TIME.

Part: CONTROL UNIT — UNSERVICEABLE (300) · airframe 19,664 hrs · 17,818 cycles

ON CLIMB OUT THE CREW RECEIVED MULTIPLE CAUTION MESSAGES INCLUDING BUT NOT LIMITED TOO, PITCH FEEL FAULT, IB GND SPLRS, IB FLT SPLRS, IB SPOILERONS, STAB FAULT, RUD LIMIT FAULT. REMOVED AND REPLACED THE SSCU #1 IAW CRJ 900 AMM 27-61-05-000/400-801 OPS CHECK GOOD. NO CURRENT FAULTS AT THIS TIME.

Part: NONE — UNSERVICEABLE (500) · airframe 19,241 hrs · 17,449 cycles

THE CREW RECEIVED MULTIPLE FAULT MESSAGES FOR SPOILERS, TRIM AND TO LAND WITH FLAPS AT 20. REMOVED AND REPLACED SSCU 1 IAW CRJ900 AMM 27-61-05-000/400-801. OPS CHECK GOOD.

Part: NONE — UNSERVICEABLE (700) · airframe 18,194 hrs · 16,548 cycles

PROX SYSTEM MSG AFTER GEAR RETRACTION. COMPLETED QRH AND RETURNED TO ORF. INTERROGATED CRJ 900 FIM 32-32-10-810-804 FOR B-1 CODE 007192 AND CHANGED THE LANDING GEAR SELECTOR VALVE IAW CRJ 900 AMM 32-32-10-000/400-801-A01. AFTER GEAR SWING NO FAULTS WERE NOTED. OPS CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 15,148 hrs · 13,895 cycles

ABOUT 10-15 MINUTES AFTER REACHING CRUISE ALTITUDE, THE CREW RECEIVED A WINDOW HEAT CAUTION MESSAGE. THE CA THEN NOTICED A CRACK IN THE WINDSHIELD ON THE CA SIDE. THEY DECLARED AN EMERGENCY, DESCENDED TO BELOW FL100, AND DIVERTED TO ORF SAFELY WITH NO ADDITIONAL ISSUES. EMERGENCY VEHICLES WERE ON STANDBY AND THE EMERGENCY WAS CANCELED WHEN THEY LANDED. THE AIRCRAFT DID NOT LAND OVERWEIGHT. PASSENGERS DID NOT BRACE. CAPT B-SCREEN FAULT CAUSED EMERGENCY LANDING DIVERTED TO ORF / REMOVED AND REPLACED LH SIDE WINDOW IAW CRJ 900 AMM 56-12-01-000/400-801-A01. RESISTANCE TEST GOOD. OPS TEST GOOD. LEAK CHECK STILL REQUIRED. COMPLIED WITH LEAK CHECK OF CAPT SIDE WINDOW IAW CRJ9 AMM 56-12-01-400-801 NO DEFECTS NOTED LEAK CHECK GOOD.

Part: DOOR — OUT OF ALIGNMENT (EMERGENCY EXIT) · airframe 13,752 hrs · 12,620 cycles

OVERHEAD BIN INSTALLED INCORRECTLY CAUSING INTERFERENCE WITH EMERGENCY EXIT. REMOVED AND REINSTALLED OVERHEAD STORAGE COMPARTMENT (SEAT 14 FD) BLOCKING RT FWD OVERWING EMERGENCY EXIT DOOR IAW CRJ 900 AMM 25-23-01-000/400-801-A50. NO CONTACT WITH DOOR AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 13,346 hrs · 12,252 cycles

DURING OVERNIGHT MAINTENANCE IT WAS FOUND THAT THE EMERGENCY BATTERIES WOULD NOT HOLD A CHARGE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES.

Part: SPOILER SYS — MALFUNCTIONED · airframe 13,291 hrs · 12,198 cycles

FLIGHT SPOILERS MESSAGE EN ROUTE. THE CREW DECLARED AN EMERGENCY AS PRECAUTION BUT CREW WERE NOT NEEDED. THEY LANDED AND TAXIED TO A GATE WITHOUT INCIDENT. PERFORMED SPOST 2 IAW CRJ 900 AMM 27-61-05-740-801-A03. TEST GOOD. PERFORMED OPS CHECK OF THE MFS ACTUATOR IAW CRJ 900 AMM 27-62-01-710-801-A01. OPS CHECK GOOD. NO OTHER DEFECTS NOTED.

Part: SENSOR — FAILED (ICE DETECTION) · airframe 12,768 hrs · 11,737 cycles

CREW RECEIVED LEFT AND RIGHT WING ANTI ICE CAUTION MESSAGES. DELCARED EMERGENCY AND DIVERTED. FOUND LOOSE WIRES(W3 AND GROUND) ON LH OB WING ANTI ICE SENSOR. PERFORMED REPAIR OF THE LH OUTBOARD WING ANTI ICE SENSOR. PERFORMED OPS CHECK OF THE WING ANTI-ICE FROM LEFT AND RIGHT MODE IAW CRJ 900 AMM. OPS CHECK GOOD AT THIS TIME. THIS CLEARS MEL

Part: ANGLE — CRACKED (BS 1200) · airframe 12,607 hrs · 11,599 cycles

LT AFT VERTICAL DRAG ANGLE IS CRACKED FS 1200. COMPLIED WITH REO 670-55-31-018 REV A. APPLIED TOPCOAT IAW SRM 51-25-01-001-001-A01.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 12,607 hrs · 11,599 cycles

RH AFT VERTICAL DRAG ANGLE IS CRACKED FS 1200. 12/14/19 (PCC) M/A: 1. N/A C/A: 1. COMPLIED WITH BOMBARDIER REO 670-55-31-018 REV A DATED 2016-11-10. 12/19/19 M/A: 2. REPAIR REQUIRES TOPCOAT UP PAINT. 12/19/19 C/A: 2. APPLIED TOPCOAT IAW CRJ 900 SRM 51-25-01-001-001-A01. 12/19/19 (12/21/19 AS)

Part: UNKNOWN — ODOR (CABIN) · airframe 5,490 hrs · 5,063 cycles

BURNING ODOR AND SMOKE AROUND ROW 8. MAINTENANCE PERFORMED OPS CHECK, NO DEFECTS FOUND.

Part: BLADE — DAMAGED (LT ENGINE) · airframe 4,726 hrs · 4,365 cycles

BIRD STRIKE DAMAGE TO LEFT ENGINE. REMOVED AND REPLACED FAN BLADES NUMBERS 6 AND 20. OPS CHECK GOOD IAW AMM. RELEASED FOR SERVICE.

Part: ENGINE — BIRD INGESTION (LEFT) · airframe 4,726 hrs · 4,365 cycles

BIRD STRIKE DAMAGE TO LEFT ENGINE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 3,309 hrs · 3,102 cycles

CREW REPORTED EMERGENCY LIGHTS ABOVE ROW 14 AND 15 AND ALONG THE WALL AND OUTSIDE OF PLANE NOT WORKING. MAINTENANCE TROUBLESHOT, R & R NR 4 EMERGENCY LIGHTS BATTERY PACK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 3,309 hrs · 3,102 cycles

CREW REPORTED EMERGENCY LIGHTS ABOVE ROW 14 AND 15 AND ALONG THE WALL AND OUTSIDE OF PLANE NOT WORKING. MAINTENANCE TROUBLESHOT, R & R NR 3 EMERGENCY LIGHTS BATTERY PACK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SENSOR — FAILED (ANTI-ICE SYS) · airframe 667 hrs · 666 cycles

CREW REPORTED WING ANTI-ICE CAUTION MESSAGE AND WING ANTI-ICE FAULT STATUS MESSAGE AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT INBD TEMPERATURE SENSOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.