N167GJ

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 25,715 hrs · 17,553 cycles

RIGHT EMERGENCY DOOR MESSAGE. PERFORMED AN OPS CHECK FOR THE RT EMERGENCY DOOR. OPS CHECKED GOOD IAW AMM 52-21-00.

Part: WARNING MESSAGE — ILLUMINATED (EMERGENCY EXIT) · airframe 24,070 hrs · 16,286 cycles

RIGHT EMERGENCY DOOR CAUTION MESSAGE.

Part: LIGHT — DETACHED (CABIN) · airframe 23,600 hrs · 15,935 cycles

EMERGENCY LIGHT STRIP IS DETACHED. REPAIRED IAW AMM 52-41-32. OPS CHECKED GOOD.

Part: A/C PACK — FAILED (LEFT) · airframe 23,438 hrs · 15,806 cycles

SMOKE AND FUMES VISIBLE FROM GASPERS IN FLIGHT DECK, RESIDUE FROM SMOKE IN FLIGHT DECK ALSO SEEN IN FWD CABIN FUMES LASTED FOR 4 TO 5 MINUTES. INSPECTED AND FOUND LT PACK TO BE MAKING MECHANICAL GRINDING NOISE. RAN ENGINES WITH CREW TO CONFIRM NO FURTHER ODORS OR SMOKE. DEFERRED LH PACK ON OCN 70018555 PER MEL 21-51-01B-2 CAT C

Part: ANGLE — CRACKED (PAX DOOR) · airframe 23,062 hrs · 15,525 cycles

CRACK FOUND ON PASSENGER DOOR NEAR PASSENGER DOOR ASSIST PULLEY. INSTALLED NEW PASSENGER DOOR ANGLE IAW SRM 52-11-04

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 23,062 hrs · 15,525 cycles

PASSENGER DOOR AFT SIDE PANEL STIFFNER IS CRACKED. REMOVED AND REPLACED THE STIFFNER IAW SRM 51-42-06

Part: SKIN — CORRODED (BS 333) · airframe 23,062 hrs · 15,525 cycles

LEVEL 2 CORROSION AT BS 333 CIRCULAR JOINT SPLICE AT STRINGER 26R. REMOVED AND REPLACED JOINT SPLICE IAW SRM 51-42-06.

Part: LENS — MISSING (CABIN) · airframe 21,416 hrs · 14,312 cycles

GALLEY FLOOR LOWER SERVICE DOOR EMERGENCY LENS MISSING. DEFERRED GALLEY FLOOR LEVEL EMERGENCY FLOODLIGHT LENS IAW NEF 25-100-12, CAT 1.

Part: SCREW — UNSECURE (CABIN DOOR) · airframe 21,028 hrs · 14,024 cycles

SCREW FELL OFF MAIN CABIN DOOR. RE-INSTALLED SCREW FROM PAX DOOR INSPECTION PANEL IAW AMM 20-21-00. NO DEFECTS NOTED.

Part: LIGHT — LOOSE (CABIN) · airframe 19,380 hrs · 12,815 cycles

ESCAPE PATH LIGHTING AT 2C LOOSE. SECURED ESAPE PATH LIGHTING AT 2C IAW AMM 33-51-01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 19,168 hrs · 12,657 cycles

LINTEL STRINGER 3L AT FS 280.00 IS CRACKED. CUT OUT DAMAGED AREA, FABRICATED & INSTALLED REPAIR PARTS IAW REO 670BA-53-040 REV C DATED 20 SEPT 2012, USED PNS 670BA53040K1A & 670BA. NDT PERFORMED BY CRS.

Part: SLAT — GOUGED (LT WING) · airframe 19,168 hrs · 12,657 cycles

LEFT SLAT 1, BETWEEN WS 108.00 & 128.00 IS GOUGED. REPAIRED LT SLAT 1, BETWEEN WS 108.00 & 128.00 BY CUTTING OUT DAMAGE. FABRICATING REPAIR PARTS & INSTALLING IAW REO 670-57-42-574 DATED 30 JULY 2015. NDT PERFORMED CRS.

Part: BEAM — CRACKED (FUSELAGE) · airframe 19,168 hrs · 12,657 cycles

FS 280.00 BEAM, LT & RT SIDES ARE CRACKED. R & R LT & RT FS 280.00 BEAM, PN CC670-34094-1 & CC670-34094-2S IAW DWG BA670-31057 REV K, DWG CC670-33052 REV E, DWG CC670-34010 REV G, DWG CC670-34117 REV B, AMM 51-21-01, 20-70-00, SRM 51-40-11, 51-25-06, 51-25-16, 51-42-13, 51-42-21, 51-42-06, & 51-21-11.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 19,168 hrs · 12,657 cycles

STRINGER SPLICE AT FS 333, STRINGER 25R IS CORRODED. R & R STRINGER SPLICE PN SH670-32429-4 IAW SRM 51-42-06, 51-42-21 & 51-25-21.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 19,168 hrs · 12,657 cycles

MAIN AVIONICS DOOR FWD SURROUND STRUCTURE, NR 2 INTERCOSTAL IS CORRODED. R & R INTERCOSTAL IAW SRM 51-42-06 & 51-42-21. WO 80306, WC 1066.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 19,168 hrs · 12,657 cycles

INTERCOSTAL NR 3, RT OF STRINGER 27, IS CORRODED. R & R INTERCOSTAL NR 3, PN SH670-32075-3 IAW SRM 51-42-06 & 51-42-20.

Part: DETECTOR LOOP — OUT OF POSITION (BLEED AIR SYS) · airframe 18,951 hrs · 12,507 cycles

LEFT BLEED DUCT CAUTION MSG IN FLIGHT. PERFORMED LEAK TEST & FOUND MT139L CHANNEL A INDICATING A FAULT. INSPECTED DETECTION LOOP A & FOUND IT CONTACTING NR 1 HYD ACCUMULATOR. REPOSITIONED IAW AMM 36-21-01. OPERATIONS CHECKED GOOD IAW AMM 36-21-00.

Part: SPRING — MISSING (CABIN DOOR) · airframe 18,922 hrs · 12,486 cycles

MAIN CABIN DOOR HANDLE MISSING SPRING. DEFERRED PAX DOOR HANDLE FLAP IAW REO 670-52-11-831. TEMP PLACARD INSTALLED.

Part: DOOR — OPEN (EXTERNAL POWER) · airframe 17,774 hrs · 11,716 cycles

GPU DOOR LEFT OPEN. INSPECTED, CLOSED & SECURED GPU DOOR IAW AMM 05-21-00. NO DEFECTS NOTED.

Part: HANDLE — ICED (PAX DOOR) · airframe 17,544 hrs · 11,567 cycles

PAX DOOR SHOWS RED ON EICAS. REMOVED ICE FROM PAX DOOR HANDLE ASSEMBLY & PERFORMED OPERATIONS CHECK IAW AMM 52-70-04. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: WHEEL — MALFUNCTIONED (PAX DOOR) · airframe 16,718 hrs · 11,024 cycles

PAX DOOR SUPPORT WHEEL DID NOT DEPLOY. COMPLIED WITH PAX DOOR SUPPORT WHEEL INSPECTION & TEST IAW AMM 52-11-13. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: AMPLIFIER — MALFUNCTIONED (CABIN) · airframe 16,126 hrs · 10,664 cycles

OVERHEAD LIGHT MID CABIN OUT, BOTH FRONT & BACK. RERACKED PA AMP IAW AMM 23-31-00. OPERATIONS CHECK NORMAL AT THIS TIME.

Part: DOOR — OPEN (GPU) · airframe 16,014 hrs · 10,594 cycles

GPU DOOR OPEN IN FLIGHT. INSPECTED GPU DOOR, NO DAMAGE NOTED, VERIFIED INSTALLATION IAW AMM 52-45-31.

Part: PLACARD — MISSING (EMERGENCY EXIT) · airframe 15,952 hrs · 10,555 cycles

FORWARD CREW EMERGENCY EXIT HATCH MISSING INSTRUCTION PLACARD. PLACED PLACARD ON NEF 25-500-3 CAT 5.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 14,378 hrs · 9,560 cycles

FLOOR SUPPORT AT LBL 12 IS CRACKED. CUT BEAM AND REMOVED 12 INCHES FROM FS 268 TO 280. INSTALLED NEW SECTION AND FABRICATED REPAIR PARTS IAW REO 670-53-11-866,

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 14,378 hrs · 9,560 cycles

FLOOR SUPPORT AT RBL 12 IS CRACKED. CUT SUPPORT AND REMOVED FROM FS 268 TO 280. INSTALLED NEW SECTION AND FABRICATED REPAIR PARTS IAW REO 670-53-11-866 AND REO 670-53-11-866, REV A.

Part: INSULATION — CONTAMINATED (ZONE 800) · airframe 14,378 hrs · 9,560 cycles

RIGHT OVERWING EMERGENCY EXIT DOOR HAS 2 WET PIECES OF INSULATION. REPLACED INSULATION AND REMOVED MOISTURE IAW AMM 25-80-00.

Part: SCREW — CORRODED (EMERGENCY EXIT) · airframe 14,378 hrs · 9,560 cycles

RT OVERWING EMERGENCY EXIT DOOR HAS EIGHT CORRODED SCREWS AND NUTS ON UPPER RELEASE LATCH MECHANISM. R & R HARDWARE IAW AMM 52-21-02.

Part: PLACARD — WORN (PAX DOOR) · airframe 14,378 hrs · 9,560 cycles

PASSENGER DOOR "OPEN" AND "EXIT" PLACARDS ARE WORN. R & R THE "OPEN" AND "EXIT" PLACARDS IAW AMM 20-60-04

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,378 hrs · 9,560 cycles

QUARTER TURN STRAP ON FS 280 BEAM HAS LIGHT CORROSION. REMOVED CORROSION. TREATED, PRIMED, AND TOP-COATED IAW SRM 51-21-06, 51-21-01, 51-25-06, AND 51-25-21.

Part: FLOOR SUPPORT — CORRODED (BS 1036-1042) · airframe 14,378 hrs · 9,560 cycles

CARGO BAY FLOOR SUPPORT AT LBL 26, HAS TWO SPOTS OF CORROSION BS 1036 - 1042. REMOVED CORROSION IAW REO 670-53-61-1006.

Part: STRUCTURE — DAMAGED (DOOR FRAME) · airframe 14,378 hrs · 9,560 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. WO 80153; WC 8017.

Part: STEP — CORRODED (PAX DOOR) · airframe 14,378 hrs · 9,560 cycles

PASSENGER DOOR LOWER MID STEP HAS CORROSION AT CONNECTION TO BOTTOM STEP. REMOVED CORROSION AND BLENDED AREA AND RESTORED FINISHED IAW SRM 52-11-04, 51-21-11 AND AMM 51-21-011.

Part: LANYARD — BROKEN (PAX DOOR) · airframe 17,068 hrs · 9,336 cycles

PAX DOOR HAND RAIL QUICK RELEASE PIN LANYARD BROKEN. DEFERED PAX DOOR HANDRAIL QUICK RELEASE PIN ON OPEN CONTROL NR 28803 IAW MEL 52-11-05, CAT C.

Part: TIRE — DAMAGED (MLG) · airframe 13,746 hrs · 9,113 cycles

ATC REPORTED A POSSIBLE BLOWN TIRE ON TAKEOFF. INSPECTED NOSE AND MAIN TIRES FOR DAMAGE IAW AMM 32-41-01 & 32-41-01, NO DEFECTS NOTED AT THIS TIME.

Part: PLACARD — DAMAGED (PAX DOOR) · airframe 13,623 hrs · 9,030 cycles

PAX DOOR EXIT SIGN IS WORN. INSPECTED & FOUND PLACARD TO BE SCUFFED AND NOT WORN, CLEANED MARKS AND SCUFFS OFF OF PLACARD IAW AMM 12-21-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 13,426 hrs · 8,901 cycles

PAX DOOR INDICATION CAUTION. RESET POWER AND PERFORMED PAX DOOR WARNING SYS OP'S CHECK IAW AMM 52-70-04. OP'S CHECKED GOOD AT THIS TIME.

Part: CIRCUIT BREAKER — OPEN (EMERGENCY LIGHTS) · airframe 13,345 hrs · 8,840 cycles

EMERGENCY LIGHTS WILL NOT EXTINGUISH WHEN SWITCH IS ARMED. FOUND EMERGENCY LIGHTS CIRCUIT BREAKER OPEN, CLOSED CIRCUIT BREAKER AND PERFORMED OP'S CHECK, OP'S CHECKED GOOD IAW AMM 33-51-00, NO DEFECTS NOTED.

Part: BONDING STRAP — BROKEN (PAX DOOR) · airframe 13,367 hrs · 8,790 cycles

PAX DOOR STEP BONDING STRAP BROKEN. INSTALLED BONDING STRAP ON PAX DOOR STEP IAW 52-11-04.

Part: COVER — LOOSE (RT OVERWING DOOR) · airframe 13,110 hrs · 8,686 cycles

RT OVERWING EXIT HANDLE COVER FALLING DOWN IN FLIGHT. SECURED EXIT HANDLE COVER IAW AMM 25-26-09. OP'S CHECKED GOOD AT THIS TIME.

Part: CABLE — BROKEN (PAX DOOR) · airframe 12,020 hrs · 8,007 cycles

PAX DOOR SUPPORT WHEEL CABLE BROKEN. R & R PAX DOOR SUPPORT WHEEL CABLE, PERFORMED OP'S CHECK IAW AMM 52-11-03.

Part: SENSOR — OUT OF POSITION (LT NACELLE) · airframe 11,636 hrs · 7,754 cycles

LEFT BLEED WARNING ON EICAS DISPLAY IN FLIGHT. RAN BLEED SYS AND DUPLICATED DISC AFTER 10 MIN, LOOP MOUNT 139 WAS HITTING ON MDC, FOUND AREA OF LOOP SENSOR TOUCHING DUCT. REPOSITIONED LOOP SENSOR TOUCHING DUCT, OP'S CHECK GOOD IAW IAW AMM 21-51-00.

Part: UNKNOWN — VIBRATION (RT ENGINE) · airframe 11,112 hrs · 7,417 cycles

RT ENGINE FAN VIBRATION IN YELLOW 5.0, OBSERVED DURING FLIGHT. INSPECTED FAN BLADES, NO DEFECTS FOUND IAW AMM 72-21-02. PERFORMED FAN TRIM BALANCE , OP'S CHECKED GOOD IAW AMM 71-00-00.

Part: SAFETY VALVE — INOPERATIVE (NR 2) · airframe 10,520 hrs · 7,074 cycles

CABIN ALT MASTER WARNING. R & R SAFETY VALVE NR 2 IAW AMM 21-32-03. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — FAULTY (PAX DOOR) · airframe 10,428 hrs · 6,970 cycles

PAX DOOR OUTER HANDLE CAUTION MESSAGE ILLUMINATED. R & R PASSENGER DOOR PROXIMITY SENSOR PX107 IAW AMM 57-40-04.

Part: COVER — UNSECURE (ESCAPE ROPE) · airframe 10,370 hrs · 6,929 cycles

RT SIDE ESCAPE ROPE COVER WILL NOT STAY CLOSED. RESECURED RT ESCAPE ROPE COVER IAW AMM 25-63-01.

Part: BATTERY PACK — UNSECURE (EMERGENCY LIGHTS) · airframe 8,992 hrs · 6,043 cycles

EMERGENCY EXIT SIGN INOPERATIVE AS WELL AS CEILING EXIT SIGNS FOR PAX AND GALLEY EXIT DOORS. RESECURED NR 1 BATTERY PACK AND PERFORMED OPS CHECK OF EMERGENCY LIGHTS SYSTEM IAW AMM 33-15-17 AND 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,992 hrs · 6,042 cycles

OVERHEAD CEILING FLOOD LIGHT AT ROW 2 INOPERATIVE. REDECURED NR 1 BATTERY PACK AND PERFORMED OPS CHECK OF EMERGENCY LIGHT SYS IAW AMM 33-51-17 AND 33-51-00.

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR) · airframe 8,608 hrs · 5,813 cycles

PAX DOOR OUTER HANDLE CAUTION MESSAGE COMES ON CONTINUOUSLY (INTERMITTENT). DEFERRED PAX DOOR INDICATION IAW MEL 52-70-01 ON DMI 25383 CAT A IAW MX CONTROL.

Part: PROXIMITY SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 8,601 hrs · 5,807 cycles

PAX DOOR OUTER HANDLE CAUTION MESSAGE. ADJUSTED PAX DOOR OUTER HANDLE PROXIMITY SWITCH IAW AMM 52-70-04. OPS CHECKED GOOD.

Part: HINGE PIN — MIGRATED (PAX DOOR) · airframe 7,799 hrs · 5,296 cycles

PASSENGER DOOR TOP STEP HINGE PIN MIGRATING RESET PIN POSITION ON PASSENGER DOOR TOP STEP HINGE IAW AMM 52-11-09.

Part: SILL — CORRODED (ZONE 100) · airframe 6,901 hrs · 4,747 cycles

AFT CARGO LOWER SILL HAS CORROSION, PN MM670-35655-003. R & R THE AFT CARGO LOWER DOOR SILL PLATE IAW SRM 53-61-23.

Part: PANEL — CRACKED (PAX DOOR) · airframe 6,901 hrs · 4,747 cycles

PASSENGER DOOR FWD SIDE PANEL CRACKED ZONE 2 & 3, REPAIRED PASSENGER DOOR FWD SIDE PANEL IAW REO 670-52-11-104 REV F.

Part: PANEL — CRACKED (PAX DOOR) · airframe 6,901 hrs · 4,747 cycles

PASSENGER DOOR AFT SIDE PANEL CRACKED ZONE 3, REPAIRED PASSENGER DOOR AFT SIDE PANEL IAW REO 670-52-11-104, REV F.

Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 6,901 hrs · 4,747 cycles

FWD CARGO DOOR LOWER SEAL RETAINER DAMAGED, PN LE670-39644-1. BLENDED OUT TO SMOOTH CONTOUR IAW REO 670-52-35-127.

Part: ANGLE — CORRODED (ZONE 100) · airframe 6,901 hrs · 4,747 cycles

PASSENGER DOOR THRESHOLD MID-CAP ANGLE CORRODED, PN SH670-31825-7. R & R PASSENGER DOOR THRESHOLD MID-CAP ANGLE IAW SRM 51-41-02.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 6,901 hrs · 4,747 cycles

FLOOR PANEL 242 BRF, PN SH670-32571-35, HAS SOFT SPOT. FABRICATED REPAIR DOUBLER IAW SRM 53-00-47.

Part: BRACKET — CRACKED (ZONE 200) · airframe 6,901 hrs · 4,747 cycles

AFT ACCESSORY COMPARTMENT, RT SIDE, WL 97.50, STR NR8, WATER INJECTION LINE HOLDING BRACKET IS BROKEN, FUS STA 1070.70. REMOVED, FABRICATED AND INSTALLED BRACKET, PN MM670-97111-007 IAW SRM 51-40-00.

Part: SILL — CORRODED (ZONE 100) · airframe 6,901 hrs · 4,747 cycles

MAIN CABIN STA 280-319.7, RT SILL CORRODED, PN SH670-32172-9. R & R RT SILL STA 280-319.7.

Part: PLACARD — MISSING (CABIN) · airframe 6,901 hrs · 4,747 cycles

SEVERAL PLACARDS MISSING FROM PASSENGER DOOR. INSTALLED MISSING PLACARDS IAW AMM 20-60-04.

Part: BRACKET — CRACKED (BS 1070.2) · airframe 6,901 hrs · 4,747 cycles

AFT ACCESSORY COMPARTMENT, RT SIDE, WL 97.50, FUS STA 1070.20, WATER INJECTION LINE HOLDING BRACKET AT AT STR 6 IS CRACKED. REMOVED, FABRICATED AND INSTALLED BRACKET PN MM670-97107-003 IAW SRM 51-40-00.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 6,901 hrs · 4,747 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED PASSENGER DOOR AFT DRAG ANGLE IAW SRM 52-11-04.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 5,724 hrs · 4,001 cycles

ANTI-ICE DUCT MASTER WARNING. PERFORMED ANTI-ICE DUCT WARNING FIM TASK NO FAULTS NOTED AT THIS TIME IAW FIM 30-11-00.

Part: REFLECTOR — MISSING (AIRSTAIR DOOR) · airframe 4,622 hrs · 3,238 cycles

REFLECTIVE STRIP ON AIRSTAIR DOOR MISSING. DEFERRED REFLECTIVE STRIP PER MEL 33-51-01G.

Part: ESCAPE ROPE — FRAYED (EMERGENCY EXIT) · airframe 2,294 hrs · 1,669 cycles

BOTH EMERGENCY EXIT ROPES ON OVERWING EXITS IN CABIN FRAYED. INSTALLED NEW ROPES IAW CRJ 700 AMM 25-63-04

Part: CONNECTOR — LOOSE (RT ENGINE) · airframe 1,365 hrs · 1,017 cycles

RT FIRE FAIL CAUTION MESSAGE. INSPECTED UPPER AND LWR FIRE DET RAILS FOUND LOOSE CONNECTOR ON LOWER RAIL ON RT ENGINE RESECURED. OPS CHECKED FIRE DET SYS IAW AMM 26-11-00.

Part: INTERPHONE — INOPERATIVE (CABIN) · airframe 927 hrs · 695 cycles

FWD F/A HANDPHONE EMERGENCY AURAL INOP. PERFORMED CHECK OF EMERGENCY FUNCTION IAW M/M 23-31-30 OPS OK.