N168GJ

Part: UNKNOWN — SMOKE (LAVATORY) · airframe 23,898 hrs · 16,190 cycles

SMOKE IN AFT LAV. PERFOMED VISUAL INSPECTIO OF AFT LAV IAW CRJ700 AMM 25-42-08 NO DEFECTS NOTED

Part: FAN — ICED (LT ENGINE) · airframe 23,898 hrs · 16,190 cycles

N1 FAN VIBRATION IN THE YELLOW, NOT CONTROLLABLE, LEFT ENGINE SHUT DOWN. AFTER AC LANDED FOUND ICE ON SEVERAL FAN BLADES. RAN ENGINE FOR VIBE TEST , AC PASSED VIBE TEST . VIBE WAS BELOW 0.1. INSPECTED FWD AND AFT FAN NO DEFCTS NOTED REF TO CRJ700 AMM 30-22-01 AND 72-21-02

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 22,465 hrs · 15,096 cycles

PAX DOOR AFT SIDE PANEL STIFFENER IS CRACKED. REMOVED AND REPLACED CRACKED STIFFENER IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,465 hrs · 15,096 cycles

LEFT BS 280 FLOORBEAM CRACKED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06.

Part: UNKNOWN — ODOR (CABIN)

SMOKE AFT LAVATORY MASTER WARNING AND ODOR OF FUMES IN THE FLIGHT DECK. PERFORMED HIGH POWER ENGINE RUNS AND PROCEDURES IAW AMM 70-00-00 NO SMOKE IN COCKPIT CABIN OR LAV DETECTED, OPS CHECKED GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: CABLE — BROKEN (PAX DOOR) · airframe 18,793 hrs · 12,406 cycles

PASSENGER DOOR WILL NOT CLOSE. FOUND ICE BREAKER CABLE BROKEN. R & R ICE BREAKER CABLE IAW AMM 52-11-15. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 18,534 hrs · 12,225 cycles

PASSENGER DOOR OUTER HANDLE CAUTION MSG. DEFERRED IAW MEL 52-70-01.

Part: TORQUE TUBE — DISCONNECTED (LE SLAT) · airframe 18,518 hrs · 12,210 cycles

SLATS FAIL, CAUTION MSG ON APPROACH, ACFT DID A GO AROUND. FOUND LT OTBD TORQUE TUBE AT WS 327.00 - 353.00, DISCONNECTED. RE-CONNECTED LT OTBD TORQUE TUBE IAW AMM 27-81-01. PERFORMED OPERATIONS CHECK IAW AMM 27-81-00. THE SLAT DISCONNECT SENSOR WAS ALSO DAMAGED DURING THIS EVENT & REPLACED IAW AMM 27-31-39. THIS ACFT WAS 3 CYCLES OUT OF HEAVY MX & THIS INCIDENT HAS BEEN REPORTED.

Part: SKIN — DENTED (PAX DOOR) · airframe 18,511 hrs · 12,207 cycles

PASSENGER DOOR DENTED ON FWD UPPER CORNER INNER SURFACE. DRESSED DENT TO ORIGINAL CONTOUR IAW REO 670-52-11-839. NDT PERFORMED, WO A15-973, DATED 21 AUG 2015.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 18,511 hrs · 12,207 cycles

MAIN AVIONICS DOOR FWD SURROUND, NR 3 INTERCOSTAL AT STRINGER 27 IS CORRODED. R & R INTERCOSTAL IAW SRM 51-42-06, 51-40-11, 51-42-21, 51-25-16, & 51-25-06.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 18,511 hrs · 12,207 cycles

MAIN AVIONICS DOOR FWD SURROUND, NR 2 INTERCOSTAL AT LT SIDE OF STRINGER 27 IS CORRODED. R & R INTERCOSTAL IAW SRM 51-42-06, 51-40-11, 51-42-21, 51-25-16, & 51-25-06. WO 80311 & WC 1112.

Part: FASTENER — CORRODED (EMERGENCY EXIT) · airframe 18,511 hrs · 12,207 cycles

LEFT & RIGHT OVERWING EMER EXITS INTERNAL RELEASE HANDLE BRACKETS HAVE CORRODED HARDWARE. R & R BRACKET HARDWARE IAW AMM 52-21-02.

Part: BEAM — CRACKED (FUSELAGE) · airframe 18,511 hrs · 12,207 cycles

RIGHT BEAM AT FS 280.00 IS CRACKED. R & R RT BEAM AT FS 280.00, PN CC670-34094-2, IAW DWG CC670-34010 REV G DATED 03-07-2007, DWG CC670-33052 REV E, DATED 01-04-2006, DWG CC670-34117, REV B DATED 07-08-2002, DWG BA670-31057, DATED 10-20-2014, MM 20-70-00, 51-21-01, SRM 51-42-13, 51-42-21, 21-42-06, 51-25-06 & 51-25-16.

Part: ESCAPE ROPE — FRAYED (CABIN) · airframe 18,511 hrs · 12,207 cycles

LEFT & RIGHT OVERWING EXIT EMER ROPE IS FRAYED. R & R LT & RT OVERWING EXIT EMER ROPES, PNS BA670-40609-1, IAW AMM 25-63-04.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 18,511 hrs · 12,207 cycles

LINTEL STRINGER 2L AT FS 280.00 IS CRACKED. FABRICATED PARTS & REPAIRED LINTEL STRINGER 3L AT FS 280.00 IAW REO 670-53-+21-493 REV D DATED 2015-07-10 & SB 670BA-53-040 REV C DATED 2012-9-20.

Part: DOOR FRAME — DAMAGED (CABIN) · airframe 18,056 hrs · 11,881 cycles

STRUCTURAL DAMAGE TO CABIN DOOR FRAME. INSPECTED ACFT & FOUND ACFT TO BE SAFE FOR A ONE TIME FERRY FLIGHT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 18,047 hrs · 11,875 cycles

PASSENGER DOOR OUTER HANDLE CAUTION MSG IN FLIGHT. DEFERRED PAX DOOR INDICATION SYS IAW MEL 52-70-01 CAT A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 18,032 hrs · 11,866 cycles

PASSENGER DOOR OUTER HANDLE CAUTION MSG. DEFERRED PAX DOOR CAUTION MSG IAW MEL 52-70-01 CAT A. ALSO DEFERRED GND VLV IAW MEL 21-24-0.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 17,993 hrs · 11,836 cycles

PASSENGER DOOR OUTER HANDLE INTERMITTENT IN FLIGHT. DEFERRED PAX DOOR OUTER HANDLE INDICATION IAW MEL 52-70-01 CAT A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 17,974 hrs · 11,825 cycles

PASSENGER DOOR OUTER HANDLE CAUTION MSG IN FLIGHT WITH PROX SYS 2 FAULT. NO CURRENT MSGS. PERFORMED OPERATIONS CHECK OF PAX DOOR OUTER HANDLE IAW AMM 52-11-03. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — UNSECURE (CABIN) · airframe 17,974 hrs · 11,825 cycles

ESCAPE PATH LIGHTING AT 1A COMING UP. SECURED ESCAPE PATH LIGHTS STRIP IAW AMM 33-51-01.

Part: UNKNOWN — INOPERATIVE (PAX DOOR) · airframe 17,871 hrs · 11,745 cycles

PASSENGER DOOR POWER ASSIST INOPERATIVE. DEFERRED IAW MEL 52-11-01A CAT C.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 17,421 hrs · 11,431 cycles

PASSENGER DOOR OUTER HANDLE CAUTION MSG. PAX DOOR PREVIOUSLY DEFERRED IAW MEL 52-70-01 CAT A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 17,408 hrs · 11,422 cycles

PASSENGER DOOR OUTER HANDLE CAUTION MSG. DEFERRED PAX DOOR OUTER HANDLE CAUTION MSG IAW MEL 52-70-01 CAT A.

Part: GLOWSTRIP — UNSECURE (CABIN) · airframe 17,221 hrs · 11,294 cycles

EMERGENCY ILLUMINATION STRIP PEELED UP AT ROW 14CD. REATTACHED PHOTO LUMINESCENCE STRIP IAW AMM 33-51-0. NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,352 hrs · 10,738 cycles

AFT CARGO DOOR CAUTION MSG & PROX SYS FAULT 2 STATUS MSG IN FLIGHT. INSPECTED AFT CARGO DOOR FOR CLOSED & LOCKED POSITION. FOUND ACFT GOOD FOR ONE TIME FERRY FLIGHT.

Part: CONNECTOR — LOOSE (CARGO DOOR) · airframe 16,352 hrs · 10,738 cycles

AFT CARGO DOOR CAUTION MSG IN FLIGHT. INSPECTED WIRING HARNESS FROM FUSELAGE TO AFT CARGO DOOR, FOUND CONNECTOR LOOSE. TIGHTENED CONNECTOR & OPERATIONS CHECKED IAW AMM 52-70-02. OPERATIONS CHECKED NORMAL.

Part: SENSOR — FAULTY (OIL SYSTEM) · airframe 15,721 hrs · 10,332 cycles

NUMBER 1 ENG HIGH OIL TEMP IN FLIGHT, ENG SHUTDOWN. R & R NR 1 ENG OIL LEVEL & TEMP SENSOR IAW AMM 79-31-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 15,531 hrs · 10,217 cycles

PASSENGER DOOR LATCH CAUTION MSG. DEFERRED PAX DOOR INDICATION SYS IAW MEL 52-70-01 CAT A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 15,528 hrs · 10,213 cycles

PASSENGER DOOR WARNING. INSPECTED PX101, REMOVED & REINSTALLED PAX DOOR WIRING HARNESS IAW FIM 52-70-04. NO DEFECTS NOTED. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SENSOR — FAULTY (LT ENGINE) · airframe 15,427 hrs · 10,143 cycles

LEFT ENG WAS SHUT DOWN IN FLIGHT DUE TO HIGH OIL TEMP. R & R OIL LEVEL TEMP SENSOR IAW AMM 79-31-01. OPERATIONS CHECKED GOOD.

Part: ENGINE — VIBRATION (LEFT) · airframe 15,167 hrs · 9,977 cycles

LEFT ENG VIB AT 2.9 AT ONE POINT. INSPECTED ENG FAN BLADES FOR STIFFNESS & FOR ICE, SHOOK FAN BLADES & PERFORMED ENG RUN IAW AMM 72-21-02 ANS 71-00-00.

Part: INDICATION SYS — FAULTY (COCKPIT) · airframe 15,167 hrs · 9,977 cycles

N1 VIBRATION REACHED 2.6 IN FLIGHT AIR RETURN TO DEN VIBRATION 2.6. SWAPPED N1 FAN PICKUP FROM LT TO RT IAW AMM 77-11-01. PERFORMED PWR RUN WITH CREW. VIBRATION INDICATION APPEARS TO BE ERRONEOUS. ACFT SAFE FOR ONE TIME FERRY FLIGHT FROM DEN TO STL.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 15,124 hrs · 9,947 cycles

EMERGENCY EXIT LIGHT ON, WITH POWER TO ACFT SWITCH IN THE ARM POSITION & THE FLIGHT ATTENDANT SWITCH IN THE OFF POSITION. RESET CB, OPERATIONS CHECKED GOOD AT THIS TIME IAW AMM 33-51-00.

Part: COVER — MISSING (CABIN) · airframe 14,243 hrs · 9,416 cycles

FLOOR LEVEL EMERGENCY FLOOD LIGHT MISSING COVER. DEFERRED IAW MEL 33-51-01C.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 13,580 hrs · 8,995 cycles

COCKPIT FLOORBEAM CRACKED. COMPLIED WITH REO 670-53-11-864. NDT PERFORMED. NO DEFECTS NOTED. PERFORMED REPAIR ON FLOORBEAM IAW REO 670-53-11-864.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 13,580 hrs · 8,995 cycles

12R COCKPIT FLOORBEAM CRACKED. COMPLIED WITH REO 670-53-11-864 DATED 8 OCT 2013. NDT WAS PERFORMED. NO DEFECTS NOTED.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 13,580 hrs · 8,995 cycles

COCKPIT FLOOR SUPPORT AT LBL 12, FS 268 IS CRACKED. CUT SUPPORT AND REMOVED 12 INCHES FROM FS 268 TO 280. INSTALLED NEW SUPPORT SECTION, AND FABRICATED REPAIR PARTS IAW REO 670-53-11-864.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 13,580 hrs · 8,995 cycles

COCKPIT FLOOR SUPPORT AT RBL 12, FS 268 IS CRACKED. CUT SUPPORT AND REMOVED 12 INCHES FROM FS 268 TO 280. INSTALLED NEW SUPPORT SECTION AND FABRICATED REPAIR PARTS IAW REO 670-53-11-864.

Part: STRUCTURE — DAMAGED (DOOR FRAME) · airframe 13,580 hrs · 8,995 cycles

PASSENGER DOOR LOWER SURROUND STRUCTURE HAS TWO DAMAGED RIVETS ON THE FWD LOWER AND AFT LOWER CORNER CAPS. R & R RIVETS IAW SRM 51-42-10.

Part: BONDING JUMPER — BROKEN (PAX DOOR) · airframe 13,279 hrs · 8,790 cycles

PAX DOOR BONDING JUMPER IS BROKEN. R & R PAX DOOR BONDING JUMPER WIRE IAW 51-80-00.

Part: PLACARD — WORN (PAX DOOR) · airframe 13,279 hrs · 8,790 cycles

PAX DOOR OPEN PLACARD IS WORN.

Part: LIGHT — MISSING (GALLEY) · airframe 12,772 hrs · 8,470 cycles

EMERGENCY LIGHTS MISSING FROM GALLEY BULKHEAD. REPLACED EMERGENCY LIGHTS IN GALLEY BULKHEAD IAW 33-51-11. OP'S CHECKED GOOD AT THIS TIME.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 12,352 hrs · 8,205 cycles

EMERGENCY FLOOD LIGHT COVER BY SERVICE DOOR MISSING.

Part: HINGE PIN — BACKED OUT (PAX DOOR) · airframe 12,305 hrs · 8,177 cycles

HINGE PIN ON PAX DOOR COMING OUT. INSTALLED HINGE PIN ON PAX DOOR IAW AMM 52-11-04.

Part: BALLAST — BURNED (CABIN LIGHTS) · airframe 11,410 hrs · 7,609 cycles

ELECTRICAL ODOR, & BURNING PLASTIC ODOR OBSERVED IN AFT CABIN. REPLACED AFT BALLAST IAW REO 670-33-25-001.

Part: LIGHT — UNKNOWN (CABIN) · airframe 11,362 hrs · 7,579 cycles

EMERGENCY LIGHT INOPERATIVE. PERFORMED OPS CHECK ON EMERGENCY LIGHTING SYS IAW AMM 33-51-03, CHECKED GOOD AT THIS TIME.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 10,465 hrs · 7,004 cycles

EMERGENCY LIGHTS COVER IN GALLEY MISSING.

Part: PLACARD — TORN (CABIN) · airframe 9,867 hrs · 6,618 cycles

PASSENGER DOOR OPEN PLACARD TORN. R & R PASSENGER DOOR OPEN PLACARD IAW AMM 20-60-04.

Part: STEP — CRACKED (PAX DOOR) · airframe 9,790 hrs · 6,566 cycles

PASSENGER DOOR, AFT SIDE STEPS HAS 1 CRACK ON ANGLE ZONE 3.

Part: COVER — INOPERATIVE (EMERGENCY EXIT) · airframe 9,641 hrs · 6,463 cycles

RT OVERWING EXIT HANDLE COVER WILL NOT CLOSE. REPLACED RT OVER WING HANDLE COVER IAW AMM 25-26-09. OPS CHECKED GOOD.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 9,308 hrs · 6,239 cycles

EXIT LIGHT COVER BY GALLEY DOOR, MISSING. OPEN

Part: WARNING MESSAGE — FALSE INDICATION (PAX DOOR) · airframe 9,216 hrs · 6,171 cycles

PAX DOOR OUTER HANDLE CAUTION MESSAGE. PERFORMED OPS CHECK OF PAX DOOR WARNING SYS, OPS CHECKED GOOD AT THIS TIME IAW AMM 52-70-04.

Part: PROXIMITY SENSOR — FAULTY (PAX DOOR) · airframe 8,690 hrs · 5,822 cycles

PASSENGER DOOR CAUTION MESSAGE ASSOCIATED WITH PROX FAULT SYS 1. R & R PASSENGER DOOR PROX SENSOR PX101 IAW AMM 52-70-04. OPS CHECKED GOOD AT THIS TIME.

Part: WIRE — BROKEN (PAX DOOR) · airframe 8,595 hrs · 5,767 cycles

BROKEN WIRE ON PAX DOOR ARM. R & R SUPPORT WHEEL CABLE IAW AMM 52-11-13.

Part: SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 8,588 hrs · 5,763 cycles

PAX DOOR WARNING MESSAGE ON GROUND. ADJUSTED PX101 IAW AMM 52-70-04.

Part: WARNING LIGHT — ILLUMINATED (DOOR) · airframe 8,552 hrs · 5,741 cycles

PAX HANDLE DOOR CAUTION IN FLIGHT. PASSENGER DOOR WARNING ON THE GROUND WITH THE DOOR CLOSED AND SECURED. INSPECTED PAX DOOR SENSORS AND WIRING, NO DEFECTS NOTED. CLEANED SENSORS, PERFORMED OPERATIONAL CHECK OF DOOR AND WARNING SYS IAW AMM 52-70-00 AND 52-70-04. OPS GOOD.

Part: CABLE — BROKEN (PAX DOOR) · airframe 8,219 hrs · 5,537 cycles

PAX DOOR CABLE BROKE. R & R DOOR ASSIST MOTOR AND INSTALLED IAW AMM 52-11-08.

Part: ESCAPE ROPE — FRAYED · airframe 7,856 hrs · 5,310 cycles

LT AND RT OVERWING EMERGENCY ESCAPE ROPES ARE FRAYED. R & R LT AND RT EMERGENCY ESCAPE ROPES IAW AMM 25-63-04.

Part: PAD — WORN (SERVICE DOOR) · airframe 7,856 hrs · 6,310 cycles

SERVICE DOOR UPPER BUMP STOP RUBBER PAD WORN. R & R WORN PAD IAW AMM 52-41-02.

Part: CABLE — FRAYED (PAX DOOR) · airframe 7,856 hrs · 5,310 cycles

PAX DOOR SUPPORT WHEEL CABLE FRAYED. R & R PAX DOOR SUPPORT WHEEL BOTTOM CABLE IAW AMM 52-11-13.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 7,856 hrs · 5,310 cycles

FS 280 FLOORBEAM HAS CORROSION LT OF COCKPIT DOOR. R & R FLOORBEAM IAW SMR 51-42-06.

Part: CABLE — FRAYED (PAX DOOR) · airframe 7,856 hrs · 5,310 cycles

PAX DOOR VENT ICE BREAK CABLE FRAYED. R & R PAX DOOR VENT ICE BREAK CABLE IAW AMM 52-11-15.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 7,856 hrs · 5,310 cycles

PAX DOOR AFT SIDE STAIR STRUCTURE HAS A CRACK IN ZONE 5. REPAIRED AFT SIDE DOOR REF REO 670-52-11-104, REV F.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 7,856 hrs · 5,310 cycles

FS 280 COCKPIT FLOORBEAM ANGLE CORRODED. R & R COCKPIT FLOORBEAM ANGLE IAW SRM 51-42-06.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 7,856 hrs · 5,310 cycles

PAX DOOR MID CAP ANGLE HAS CORROSION (LEVEL 2). R & R PAX DOOR MID CAP ANGLE IAW SRM 51-40-11 AND 51-42-13.

Part: SAFETY VALVE — FAILED · airframe 7,128 hrs · 4,859 cycles

LEFT ENGINE BLEED DUCT WARNING MESSAGE OCCURRED AT 27,500 FT. CABIN ALTITUDE CAUTION MESSAGE AND MASKS DEPLOYED OCCURRED AT 29,500 FT. CABIN ALTITUDE CLIMBED AT 3,000 FT PER MIN, LOSS OF PRESSURIZATION, SMOKE IN CABIN AT 10,000 FT. OPS CHECKED NR 1 BLEED NO DEFECTS NOTED. R & R THE NR 2 SAFETY VALVE. PRESSURIZED ACFT NO DEFECTS NOTED IAW AMM 21-32-03. REF W/O 7036-1 THRU 7036-36 FOR OXEGEN GENERATOR REMOVAL AND REPLACEMENT.

Part: REFLECTOR — LOOSE (CABIN) · airframe 7,116 hrs · 4,851 cycles

SERVICE DOOR REFLECTIVE STRIP LOOSE. REATTACHED GALLEY SERVICE DOOR REFLECTIVE STRIP IAW CRJ700 AMM 25-56-07

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 5,635 hrs · 3,908 cycles

STEERING INOP CAUTION MESSAGE IN FLIGHT. PERFORMED NWS SYS RESET, OPS TEST OF NWS SYS TEST GOOD AT THIS TIME. NO FURTHER DEFECTS OR MESSAGES AT THIS TIME. IAW FIM 32-50-00.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 2,637 hrs · 1,841 cycles

RT LOWER EXIT SIGN BY GALLEY DOOR MISSING COVER. DEFFERRED COVER IAW MEL 33-51-01C CAT C DMI 13582.

Part: MANIFOLD — MALFUNCTIONED (NLG STEERING) · airframe 2,033 hrs · 1,424 cycles

STEERING INOP CAUTION MESSAGE IN FLIGHT. REMOVED AND REPLACED NLG STEERING MANIFOLD ASSY IAW AMM 32-51-50. OPS AND LEAK CHECK GOOD AT THIS TIME.

Part: LIGHT — MISSING (CABIN) · airframe 1,917 hrs · 1,332 cycles

THE COVER ON THE FLOOR LEVEL EMERGENCY EXIT LIGHT BY THE SERVICE DOOR IS MISSING. DEFFERED FLOOR LEVEL EMERGENCY FLOOD LIGHT NEAR GALLEY SERVICE DOOR IAW 33-51-01-2B DMI 9875 CAT C AUTH BY MX CONTROLLER ZACH STILLMAN

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 1,398 hrs · 971 cycles

FLOOD LIGHT LENS COVER MISSING. DEFFERED IAW MEL 33-51-01-2B CAT C DMI NR 9361. PLACARDS INSTALLED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 536 hrs · 381 cycles

FLOODLIGHT LENS NEAR SERVICE DOOR MISSING. DEFERRED LENS IAW MEL 33-51-01-2B.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 467 hrs · 337 cycles

SERVICE DOOR LOWER EMERGENCY EXIT LIGHT COVER MISSING. DEFERRED IAW NEF 25-100-12.