N159GJ

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,970 hrs · 24,089 cycles

STRINGER 26R HAS SIGNS OF CORROSION BETWEEN FS 280 AND FS 349. REMOVED AND REPLACED STRINGER SH670-31634-2S AND SH670-31372-4S IAW SRM 51-40-11, 51-42-06, 51-42-21, 51-15-06, 51-25-06, 51-25-21, 51-21-11, 51-26-00, 51-25-00.

Part: WEB — CRACKED (BS 193) · airframe 34,970 hrs · 24,089 cycles

FORWARD EQUIPMENT COMPARTMENT RH FLOOR WEB IS CRACKED AT F.S 193. CORRECTIVE ACTION: REPAIRED FORWARD EQUIPMENT COMPARTMENT RH FLOOR WEB AT F.S 193 IAW BOMBARDIER REO 670-53-11-509 REV. E DATED 2018-02-08 AND BOMBARDIER REO 670-53-11-1458 REV. -- DATED 2018-11-09 AND CRJ700 NDTM PART 1 51-20-006.

Part: STRAP — CRACKED (W-B FAIRING) · airframe 34,970 hrs · 24,089 cycles

AFT WING TO FUSELAGE FAIRING MID STRAP CRACKED. CORRECTIVE ACTION: FABRICATED NEW MID STRAP AND REPLACED CRACKED MID STRAP IAW BOMBARDIER DRAWING PLCC670-39171 AND CRJ700 SRM 51-42-06, 51-41-02, 51-42-10, 51-25-06 AND CRJ700 AMM 51-21-01.

Part: WEB — CRACKED (BS 193) · airframe 34,970 hrs · 24,089 cycles

FWD EQUIP. BAY FLOOR WEB AT F.S. 193.00 L/H SIDE IS CRACKED. CORRECTIVE ACTION: REPAIRED THE FWD EQUIP. BAY FLOOR WEB CRACK AT F.S 193.00, BY CUTTING OUT DAMAGE, FABRICATING AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 670-53-11-509 REV. E DATED 2018-02-08 AND 670-53-11-1458 REV.- DATED 2018-11-09.

Part: CROSSBEAM — CRACKED (BS 280) · airframe 34,970 hrs · 24,089 cycles

FUSELAGE CROSSBEAM(PN:CC670-33292-135) AT F.S. 280.00 L/H AND R/H SIDES ARE CRACKED. CORRECTIVE ACTION: REMOVE AND REPLACED F.S. 280.00 L/H AND R/H SIDES IAW CRJ 700 SRM51-21-11, 51-25-00, 51-25-16, 51-42-21, 51-42-06, 53-11-41, 25-42-18, 51-42-13, 51-40-11, 53-11-41, CRJ 700 NDT MANUAL PART 1 51-20-006, CRJ 700 AMM 20-70-00.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,970 hrs · 24,089 cycles

LH I/B FLAP BOTTOM SURFACE HAS A DENT AT W.S. 38.00 CORRECTIVE ACTION: REPAIRED L/H I/B FLAP BOTTOM SURFACE AT W.S. 38.00 IAW CRJ 700 SRM 57-52-01 REPAIR IV, 51-25-06, 51-21-11, 51-25-16, AND CRJ700 NDTM PART 1 51-20-006.

Part: STRUCTURE — CRACKED (MAIN PAX) · airframe 33,429 hrs · 23,104 cycles

PAX DOOR CRACKED. PERFORMED GVI INSPECTION FOR FURTHER DAMAGE AND CORROSION.

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 31,442 hrs · 21,592 cycles

PAX DOOR IS DIFFICULT TO OPEN. DOOR OP CHECKED GOOD IAW AMM 52-11-00.

Part: DOOR — LEAKING (MAIN PAX) · airframe 31,048 hrs · 21,289 cycles

EXTREMELY LOUD SQUEAL FROM MAIN CABIN DOOR. VERIFIED PAX DOOR CLOSED AND LATCHED.

Part: STRIKER — LEAKING (PAX DOOR SEAL) · airframe 31,042 hrs · 21,285 cycles

PAX DOOR SQUEALED. APPLIED SEALANT TO PASSENGER DOOR SEAL STRIKER PLATE IAW REO 670-53-22-011 AND PERFORMED LEAK CHECK IAW AMM 52-00-00, AND AMM 52-11-07. LEAK TEST PASSED. NO DEFECTS NOTED.

Part: DOOR — BINDING (MAIN PAX) · airframe 30,585 hrs · 20,922 cycles

MAIN CABIN DOOR DIFFICULT TO CLOSE AND LOCK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,123 hrs · 20,584 cycles

MID CABIN CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,017 hrs · 20,506 cycles

OVERHEAD EMERGENCY FLOOD LIGHT AT 2CD INOPERATIVE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,977 hrs · 20,474 cycles

ROW 12 EMERGENCY CEILING LIGHT INOPERATIVE. R & R THE BULB IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,666 hrs · 20,221 cycles

EMERGENCY EXIT FLOOD LIGHT AT ROW 11 INOPERATIVE. DEFFERED CEILING EMERGENCY FLOOD LIGHT AT ROW 11 IAW MEL 33-51-01B.

Part: INDICATOR — OUT OF ADJUST (PAX DOOR) · airframe 29,460 hrs · 20,079 cycles

LOWER WITNESS MARK ON PAX DOOR NOT ALIGNING. ADJUSTED MAIN DOOR LOWER LOCK INDICATOR ASSY IAW AMM 52-11-00 OPS AND INDICATION NORMAL.

Part: STRINGER SPLICE — CORRODED · airframe 29,209 hrs · 19,901 cycles

STRINGER SPLICE 25R SHOWING SIGNS OF CORROSION. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06, 53-21-03.

Part: STRINGER — CORRODED (BS 295-349) · airframe 29,209 hrs · 19,901 cycles

STRINGER 25R BETWEEN BS 295 - 349 SHOWING SIGNS OF CORROSION AT 6 LOCATIONS. REMOVED AND REPLACED THE STRINGER IAW SRMS 51-42-06 AND 51-25-16.

Part: AIRSTAIR — CRACKED (FWD SIDE) · airframe 29,209 hrs · 19,901 cycles

PASSENGER STAIR STRUCTURE CRACKED ON FWD SIDE OF MID STEP ASSEMBLY, LOWER AND UPPER CORNERS. REPAIRED PASSENGER DOOR STAIR STRUCTURE ON FORWARD SIDE OF MID STEP ASSEMBLY IAW REO 670-52-11-104 REV G AND SRMS 51-42-21, 51-41-00, 51-42-06 AND AMM 52-11-04

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 29,209 hrs · 19,901 cycles

RIGHT VERTICAL STABILIZER FORWARD DRAG ANGLE CRACKED. REPAIRED THE DRAG ANGLE IAW REO 670-55-31-018 REV.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 29,209 hrs · 19,901 cycles

LT VERTICAL STABILIZER FWD AND AFT DRAG ANGLES ARE CRACKED. CUTOUT DAMAGE FABRICATED AND INSTALLED REPAIR PARTS IAW REO 690-55-31-088, DATED 21 JUNE 2016, AND 690-55-31-018, DATED 16 APRIL 2016. NDT PERFORMED, PO 134-965, WO A16-1339, DATED 21 JUNE 2016.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 29,209 hrs · 19,901 cycles

STR 25R, LONGERON AT FS 333-364 HAS CORROSION BEYOND LIMITS. REPLACED STR 25R LONGERON AT FS 333-364 IAW SRM 51-42-06, REO 670-53-21-1310, REV DATE 2016-07-01.

Part: BEAM — CRACKED (PAX DOOR) · airframe 29,209 hrs · 19,901 cycles

FWD PASSENGER DOOR INTERNAL STRUCTURE BEAM IS CRACKED. R & R CRACKED BEAM IAW SRM'S 51-42-06 AND 51-42-21.

Part: PANEL — CRACKED (PAX DOOR) · airframe 29,209 hrs · 19,901 cycles

PASSENGER DOOR STAIR STRUCTURE IS CRACKED AT THE AFT SIDE OF THE MID STEP ASSEMBLY. REPAIRED CRACKED PASSENGER DOOR STAIR MID PANEL IAW REO 670-52-11-104, REV G DATED 2016-05-11 AND SRM 51-42-06.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 29,209 hrs · 19,901 cycles

FS 280, FLOORBEAM IS CRACKED ON LT SIDE AND HAS CORROSION ON THE RT SIDE. R & R FS 280 FLOORBEAM IAW SRM 53-11-41. WO 80413, WC 1081.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 29,209 hrs · 19,901 cycles

FS280 RT BULKHEAD AFT WEB IS CORRODED. REPAIRED RT WEB BY CUTTING OUT DAMAGED SECTION. FABRICATED WEB AND BUTT STRAP AND INSTALLED IAW REO 670-53-11-594, DATED 27, APR 2011. WO 80413, WC 2096.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 29,209 hrs · 19,901 cycles

PASSENGER DOOR STRINGER 3L IS CRACKED AT FS 280. CUT OUT DAMAGED AREA. REPAIRED STRINGER IAW REO 670-53-21-493, REV D, DATED 10 JUL 2015 AND SB 670BA-53-040, REV C.

Part: SKIN — CRACKED (PAX DOOR) · airframe 29,209 hrs · 19,901 cycles

PASSENGER DOOR FWD INTERNAL SKIN UNDER LOWER ACCESS PANEL SHOWING SIGNS OF CORROSION NEAR NUT PLATE RECEPTACLE. PASSENGER DOOR FWD INTERNAL SKIN AT LOWER ACCESS PANEL CORRODED BEYOND LIMITS. 6 FASTER HOLES ARE ELONGATED WHERE THE STAIR STRUCTURE MATES WITH THE PASSENGER DOOR SHELL. SURFACE CORROSION ON PASSENGER DOOR WHERE THE STAIR STRUCTURE MATES WITH INNER SKIN AT THREE LOCATIONS. PASSENGER DOOR STRUCTURE GOUGED ON FWD SIDE OF BOTTOM STEP ASSEMBLY. CORROSION BEHIND PANEL 832DL ON UNDERSIDE OF SKIN. CORROSION BEHIND PANEL 832FL ON UNDERSIDE OF SKIN. CORRECTIVE ACTION: REMOVED AND REPLACED PASSENGER DOOR INTERNAL SKIN IAW SRMS 51-42-06 AND 51-42-13

Part: FIRESHIELD — GOUGED (RT COWLING) · airframe 29,209 hrs · 19,901 cycles

RIGHT, LOWER FORWARD CORE COWL HAS GOUGES IN FIRE SHIELD IN FROM OF THE DRAIN ACCESS PANEL. REPAIRED RT LOWER FORWARD CORE COWL BY FABRICATING A REPAIR DOUBLER IAW REO 670-54-23-959, REV-B DATED 2013-10-11.

Part: SKIN — DENTED (LE SLAT) · airframe 29,209 hrs · 19,901 cycles

LEFT WING SLAT HAS A DENT. REPAIRED DENT ON LT WING NR 2 SLAT L/E SKIN IAW REO 670-57-42-631 DATED 2016.

Part: CAP — CORRODED (PAX DOOR) · airframe 29,209 hrs · 19,901 cycles

PASSENGER DOOR MIDCAP AND KICK ANGLE CORRODED. CLEANED KICK ANGLE AND REPLACED MIDCAP IAW SRMS 51-40-11, 51-25-06, 51-42-06, 51-21-11, 51-26-00, 51-41-00, AND 51-25-16.

Part: FLAP — GOUGED (LT WING) · airframe 29,209 hrs · 19,901 cycles

LEFT FLAP VANE ACTUATOR INTERNAL BAY NR 2 HAS A GOUGE. BLENDED DAMAGE AREA IAW REO 670-57-52-347 DATED 2016-06-23.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 29,209 hrs · 19,901 cycles

AFT WING TO BODY CENTER STRAP AND AFT C-CHANNEL CRACKED. FABRICATED NEW WING TO BODY STRAP, REPLACED AFT C-CHANNEL AND INCORPORATED MODSUM IAW SRM'S 51-42-06, 51-25-06, 51-21-11, 51-42-15, TR51055, 51-25-01 AND MODSUM 15670538200021, REV C, DATED JUNE 8 2005.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,826 hrs · 19,623 cycles

CEILING EMER LIGHT INOPERATIVE. DEFERRED CEILING EMER FLOODLIGHT IAW MEL 33-51-01B-2A CAT C.

Part: GLOWSTRIP — UNSECURE (CABIN) · airframe 28,176 hrs · 19,184 cycles

FLOOR LEVEL PHOTO LUMINESCENT STRIP AT 18CD NOT SECURE. SECURED PHOTO LUMINESCENT STRIP AT 18 CD AS REQUIRED.

Part: CARPET — UNSECURE (CABIN) · airframe 27,762 hrs · 18,897 cycles

EXIT ROW 18CD CARPET IS IN A UNSECURE POSITION. SECURED CARPET AT ROW 18 CD IAW AMM 25-25-01. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,739 hrs · 18,135 cycles

OVERHEAD EMER FLOODLIGHT INOPERATIVE ATT ROW 2. DEFERRED CABIN EMER CEILING LIGHT IAW MEL 33-51-01B CAT C.

Part: CABLE — BROKEN (PAX DOOR) · airframe 26,579 hrs · 18,031 cycles

RAMP WORKER FOUND PAX DOOR SUPPORT WHEEL CABLE BROKEN. R & R PAX DOOR BOTTOM CABLE ASSEMBLY IAW AMM 52-11-13. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,150 hrs · 17,738 cycles

CEILING EMER LIGHT AT ROW 21 INOPERATIVE. DEFERRED ROW 21 EMER LIGHT IAW MEL 33-51-01B CAT C.

Part: COVER — LOOSE (CABIN) · airframe 25,645 hrs · 17,419 cycles

EMERGENCY FLOOR LIGHT COVER LOOSE. SECURED LOOSE COVERING ON EMER FLOOR LIGHT IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,536 hrs · 17,349 cycles

EMERGENCY EXIT CEILING LIGHT AT ROW 23 INOPERATIVE. R & R LIGHT BULB AT EMER EXIT ASSEMBLY AT ROW 23 IAW AMM 33-51-09. OPERATIONS CHECKED GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 24,821 hrs · 16,884 cycles

FS 295.00 HAS LEVEL 1 CORROSION ON STRINGER 26R. REMOVED LEVEL 1 CORROSION FROM FS 295.00 AT STRINGER 26R IAW SRM 51-21-06.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,821 hrs · 16,884 cycles

MINOR CORROSION ON AUXILIARY FRAME IN FWD CARGO BAY NEAR FS 1051.30, NEAR STRINGER 13 RT. REMOVED SURFACE CORROSION, TREATED, PRIMED & PAINTED AREA IAW SRM 51-21-01.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,821 hrs · 16,884 cycles

T CAS LOWER CHANNEL BETWEEN FS 295.00 & 310.00 AT STRINGER 27 HAS LEVEL 2 CORROSION. R & R T CAS CHANNEL BETWEEN FS 295.00 & 310.00 IAW SRM 51-42-06 & 52-42-21.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 24,821 hrs · 16,884 cycles

MINOR CORROSION ON SERVICE DOOR SILL. REMOVED MINOR CORROSION ON SERVICE DOOR SILL IAW SRM 51-21-06.

Part: PLACARD — WORN (PAX DOOR) · airframe 24,821 hrs · 16,884 cycles

PAX DOOR EXIT PLACARD IS WORN. R & R PAX DOOR EXIT SIGN PLACARD IAW AMM 20-60-04.

Part: GUARD — CRACKED (PAX DOOR) · airframe 24,821 hrs · 16,884 cycles

PAX DOOR BOTTOM WEATHER CURTAIN STEP IS CRACKED. R & R PAX DOOR WEATHER GUARD IAW SRM 52-11-04.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 24,821 hrs · 16,884 cycles

MINOR CORROSION ON THE AFT CARGO DOOR SILL PLATE. BLENDED OUT CORROSION, PRIMED & PAINTED THE DOOR SILL PLATE IAW SRM 53-61-23.

Part: BEAM — CRACKED (FUSELAGE) · airframe 24,821 hrs · 16,884 cycles

280 BEAM IS CRACKED & HAS MINOR CORROSION. R & R 280 BEAM IAW SRM 53-11-41.

Part: DOOR — NOISY (GALLEY) · airframe 24,696 hrs · 16,811 cycles

LOUD WHISTLE FROM FWD GALLEY DOOR IN FLIGHT. PERFORMED INSPECTION OF GALLEY SERVICE DOOR IAW AMM 52-41-00. NO DISCREPANCIES FOUND & CLEANED SEAL.

Part: PLACARD — WORN (PAX DOOR) · airframe 24,593 hrs · 16,943 cycles

PAX DOOR OPEN PLACARD IS WORN. R & R PAX DOOR OPEN PLACARD IAW AMM 20-60-04.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 24,169 hrs · 16,499 cycles

CREW REPORTS PAX DOOR HARD TO OPEN. INSPECTED & LUBRICATED IAW AMM 52-11-00. FUNCTIONAL CHECK NORMAL. OK FOR SERVICE AT THIS TIME.

Part: ACTUATOR — FAULTY (LANDING GEAR) · airframe 23,556 hrs · 16,108 cycles

GEAR DISAGREE IN FLIGHT. R & R RETRACT ACTUATOR IAW AMM 32-32-09, OPERATIONS & LEAK CHECKED GOOD AT THIS TIME.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 22,784 hrs · 15,611 cycles

LEFT THRUST REVERSER CAUTION MESSAGE. DEFERRED LT T/R IAW MEL 78-30-01.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 22,673 hrs · 15,543 cycles

GEAR DISAGREE WARNING INDICATION OF NOSE GEAR. DEFERRED LANDING GEAR RETRACTION SYS IAW MEL 32-30-01 CAT C. FERRIED ACFT TO STL FOR REPAIR.

Part: INDICATOR — OUT OF ALIGNMENT (PAX DOOR) · airframe 22,657 hrs · 15,531 cycles

ALIGNMENT PIN AT BOTTOM OF PAX DOOR NOT LINED UP. ADJUSTED BOTTOM PAX DOOR INDICATOR IAW CRJ700 52-11-02, INDICATION LINED UP AT THIS TIME. CHECKED FOR FOD, CLOSED ACCESS DOOR COVER IAW CRJ700 IAW CRJ700 AMM 52-11-32.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 22,612 hrs · 15,505 cycles

RUDDER LIMITER FAULT STATUS MESSAGE ON TAKEOFF ROLL, ABORTED TAKEOFF. PERFORMED RUDDER LIMITER FAULT FIM TASK, NO MESSAGES NOTED AT THIS TIME IAW CRJ700 FIM 27-25-00.

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 22,594 hrs · 15,492 cycles

MAIN CABIN DOOR SEAL MAKING NOISE IN FLIGHT. PERFORMED LUBRICATION OF MAIN CABIN DOOR & VISUAL INSPECTION IAW AMM 52-11-00. NO DEFECTS NOTED AT THIS TIME.

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 22,586 hrs · 15,488 cycles

NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. FERRIED ACFT TO STL FOR MX, FOUND BAD BUSHINGS ON NOSE GEAR DOOR AFT POSITION. R & R BUSHINGS IAW CRJ700 AMM 32-22-05. FOUND PX22 OUT OF ADJUSTMENT, ADJUSTED PX22 PROX SWITCH IAW CRJ700 AMM 32-61-00, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: THRUST REVERSER — MALFUNCTIONED (LT ENGINE) · airframe 22,529 hrs · 15,454 cycles

ABORTED TAKEOFF DUE TO LT THRUST REVERSER UNSAFE ON ROLLOUT. LOCKED OUT & DEFERRED LT THRUST REVERSER ON DMI IAW MEL 78-30-01 CAT C.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSER) · airframe 22,428 hrs · 15,388 cycles

LEFT THRUST REVERSER CAUTION MESSAGE AT 50 KNOTS.

Part: LANDING GEAR — MALFUNCTIONED · airframe 22,312 hrs · 15,307 cycles

LANDING GEAR WILL NOT RERACT AFTER TAKEOFF.

Part: FLAP — LACK OF LUBE (PAX DOOR VENT) · airframe 22,276 hrs · 15,280 cycles

PAX DOOR VENT FLAPPER ON HANDLE NOT FULLY CLOSED. LUBED PAX DOOR VENT FLAP IAW AMM 12-20-52. OP'S CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,115 hrs · 15,173 cycles

EMERGENCY LIGHT AT ROW 9 INOPERATIVE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,115 hrs · 15,173 cycles

OVERHEAD EMERGENCY LIGHT OUT AT ROW 9. REPLACED LAMP, OP'S CHECKED GOOD IAW AMM 33-51-09.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,064 hrs · 15,135 cycles

EMERGENCY LIGHT ABOVE ROW 2C INOPERATIVE.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 22,057 hrs · 15,129 cycles

PHOTOLUMINECENT STRIP LOOSE ON FAIRING AFT OF SERVICE DOOR. REATTACHED REFLECTIVE STRIP ON SERVICE DOOR IAW IAW 20-60-04.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 21,775 hrs · 14,940 cycles

EMERGENCY EXIT SIGN 12A-12D BULBS BURNOUT. R & R BULBS IN EXIT SIGN. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (SEAT ROW 9) · airframe 21,146 hrs · 14,545 cycles

EMERGENCY CEILING LIGHT INOPERATIVE AT ROW 9. R & R EMERGENCY LIGHT IAW AMM 33-51-09. OP'S CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,995 hrs · 14,449 cycles

EMERGENCY CEILING FLOOD LIGHT AT ROW 15 INOPERATIVE.

Part: COMPUTER — FAILED (NR 2 EFIS) · airframe 20,731 hrs · 14,263 cycles

EFIS COMPUTER MONITOR CAUTION MESSAGE, SUSPECT NR 2 WAS FAILING. R & R NR 2 AHC IAW AMM 34-21-01, OPS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,505 hrs · 16,018 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 15 INOPERATIVE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (MLG) · airframe 20,675 hrs · 14,226 cycles

GEAR DISAGREE WARNING. NOSE GEAR INDICATION WAS RED, MAIN GEAR WAS GREEN. ADJUSTED SWITCHES PX22, PX08 & PX44 IAW 32-61-05. OP'S CHECK GOOD IAW 32-30-00.

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR) · airframe 20,518 hrs · 14,127 cycles

PAX DOOR OUTER HANDLE CAUTION.

Part: PROXIMITY SWITCH — INOPERATIVE (PAX DOOR) · airframe 20,518 hrs · 14,127 cycles

PAX DOOR OUTER HANDLE CAUTION MESSAGE. R & R PAX DOOR PROXIMITY SWITCH PX107 IAW AMM 52-70-04. OP'S CHECKED GOOD.

Part: BOLT — WORN (STEERING COLLAR) · airframe 20,402 hrs · 14,053 cycles

GEAR DISAGREE WARNING MESSAGE IN FLIGHT. FOUND WORN BOLT ON NLG STEERING COLLAR, R & R BOLT IAW AMM 32-21-22, OP'S CHECKED GOOD IAW 32-30-00. RETURN TO SERVICE.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 19,786 hrs · 13,662 cycles

FLOORBEAM AT FS 280 IS CRACKED ON LEFT SIDE. REMOVED AND REPLACED FLOORBEAM AT FS 280 IAW REO 670-53-11-047

Part: SCREW — CORRODED (PAX DOOR STEP) · airframe 19,786 hrs · 13,662 cycles

PAX DOOR, TOP STEP HINGE LOWER OUTBD SCREWS ARE CORRODED AND WON'T TIGHTEN. CORRECTIVE ACTION: REMOVED AND REPLACED CORRODED/DEFECTIVE HARDWARE ON TOP STEP IAW CRJ 700 AMM 52-11-04

Part: HINGE — BENT (PAX DOOR) · airframe 19,786 hrs · 13,662 cycles

PAX DOOR TOP UPPER INBD HINGE IS BENT. R & R TOP STEP UPPER INBD HINGE IAW AMM 20-21-00.

Part: INTERCOSTAL — CORRODED (BS 364 S27) · airframe 19,786 hrs · 13,662 cycles

INTERCOSTAL AT STGR 27 AT FS 364 HAS CORROSION. R & R INTERCOSTAL IAW SRM 51-42-20.

Part: WARNING LIGHT — ILLUMINATED (LT MLG) · airframe 194,544 hrs · 13,437 cycles

BRAKE OVERHEAT WARNING MESSAGE IN FLIGHT, DIVERTED IAW LT INBD BRAKE TEMP INDICATION IRRATIC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,359 hrs · 13,380 cycles

EMERGENCY CEILING FLOOD LIGHT ROW 14 INOPERATIVE.

Part: LIGHT — UNSECURE (CABIN) · airframe 19,258 hrs · 13,317 cycles

FLOOR LIGHTING STRIP AT 12C & 12D IS LOOSE. OP'S CHECKED GOOD, SECURED IAW AMM 33-51-01.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 19,054 hrs · 13,182 cycles

HYDRAULIC ENGINE DRIVEN PUMP 2A MASTER CAUTION LIGHT. R & R NR 2 HYD PUMP IAW AMM 29-11-01, LK AND OPS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,896 hrs · 13,077 cycles

CEILING EMERGENCY LIGHT NR 5 INOPERATIVE. REPLACED CEILING EMERGENCY LIGHT IAW AMM 33-51-09, OK FOR SERVICE AT THIS TIME.

Part: RESERVOIR — LEAKING (HYD SYSTEM) · airframe 18,888 hrs · 13,071 cycles

HYD 3 LOW PRESSURE CAUTION MESSAGE IN FLIGHT. INSPECTED NR 3 HYD SYSTEM, FOUND SEVERE LEAKAGE COMING FROM NR 3 HYD RESERVIOR, R & R NR 3 HYD RESERVIOR IAW AMM 29-12-30, OP'S AND LEAK CHECK GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,800 hrs · 13,006 cycles

CEILING LEVEL EMERGENCY LIGHT AT ROW 9 INOPERATIVE.

Part: BOLT — OUT OF ADJUST (PAX DOOR) · airframe 18,502 hrs · 12,804 cycles

PAX DOOR LOWER GREEN ALIGNMENT PINS DO NOT LINE UP. ADJUSTED PAX DOOR INNER HANDLE STOP BOLT IAW AMM 52-11-02.

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG) · airframe 18,432 hrs · 12,756 cycles

GEAR DISAGREE MASTER WARNING. ADJUSTED LT LVDT PROXIMITY SENSOR, OPS CHECKED GOOD IAW AMM 32-61-05/32-61-00/32-30-00.

Part: PLACARD — MISSING (CABIN) · airframe 18,431 hrs · 12,755 cycles

EMERGENCY EXIT PLACARD MISSING FROM LT EXIT ROW TRAY TABLE. INSTALLED EMERGENCY PLACARD IAW AMM 20-60-04.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 18,307 hrs · 12,673 cycles

LENS FOR OVERWING EXIT SIGN NEEDS TO BE REATTACHED. REATTACHED EXIT SIGN COVER.

Part: BULB — BURNED (EMERGENCY LIGHT) · airframe 18,130 hrs · 12,558 cycles

EMERGENCY LIGHT AT ROW 15 (OVERHEAD FLOOD) INOPERATIVE. R & R LIGHT BULB AT ROW 15 IAW AMM 33-51-09.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 18,028 hrs · 12,489 cycles

OVERHEAD EMERGENCY LIGHT, ROW 17, BULB IS OUT. REPLACED BULB AT ROW 17 IAW AMM 33-51-09.

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 17,397 hrs · 12,088 cycles

LEFT EMERGENCY EXIT DOOR ROPE COVER FALLING DOWN IN FLIGHT. R & R HOOK AND LOOP TAPE ON LEFT EMERGENCY EXIT DOOR ROPE COVER IAW AMM 25-26-09.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,159 hrs · 11,935 cycles

AFT CEILING EMERGENCY LIGHT BULB BURNED OUT. R & R BULB IAW AMM 33-51-09, OPS TESTED GOOD.

Part: COVER — BROKEN (ASSIST SWITCH) · airframe 17,083 hrs · 11,883 cycles

PAX DOOR ASSIST SWITCH COVER BROKEN. PLACED PAX DOOR ASSIST COVER ON NEF 25-100-39 CONTROL NR 10875 CAT 3.

Part: MOTOR — FAULTY (PAX DOOR) · airframe 16,542 hrs · 11,521 cycles

PAX DOOR INTERMITTINTLY FREE FALLS WHEN OPENED. R & R DOOR MOTOR IAW AMM 52-11-08.

Part: CABLE — UNSECURE (PAX DOOR) · airframe 16,542 hrs · 11,521 cycles

RAMP REPORTS PAX DOOR FREE FALLS. RESECURED POWER ASSIST CABLE IAW AMM 52-11-08. OPS CHECK GOOD AT THIS TIME.

Part: BULB — BURNED (LAV CALL LIGHT) · airframe 16,361 hrs · 11,409 cycles

F/A REPORTS LAV CALL LIGHT OUT OF SERVICE. REPLACED LIGHT BULB OPS CHECKED GOOD IAW AMM 33-51-07.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,328 hrs · 11,384 cycles

BOTH RT AND LT EMERGENCY EXIT SIGNS LIGHT BULBS BURNED OUT. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD AT THIS TIME.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,190 hrs · 11,296 cycles

MID CABIN CEILING, RED F/A CALL LIGHT IS BURNED OUT. R & R MID CABIN CEILING, RED F/A CALL LIGHT IAW AMM 33-51-07. OPS CHECKED GOOD AT THIS TIME.

Part: BULB — BURNED (EMERGENCY LIGHT) · airframe 16,190 hrs · 11,296 cycles

MID CABIN CEILING, RED F/A CALL LIGHT IS BURNED OUT. R & R MIDCABIN CEILING, RED F/A CALL LIGHT IAW AMM 33-51-07. OPS CHECKED GOOD AT THIS TIME.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 16,190 hrs · 11,296 cycles

3 EMERGENCY LIGHTS IN THE CABIN ARE INOPERATIVE. R & R BULBS AS NEEDED, R & R EPSU IAW AMM 33-51-17. OPS CHECKED GOOD.

Part: COVER — UNSECURE (EMERGENCY EXIT) · airframe 16,155 hrs · 11,274 cycles

RT OVERWING EMERGENCY EXIT DOOR LATCH COVER UNSECURE. RESECURED OVERWING EMERGENCY EXIT DOOR LATCH IAW AMM 25-26-09.

Part: MOTOR — MALFUNCTIONED (DOOR ASSIST) · airframe 15,841 hrs · 11,076 cycles

PASSENGER DOOR ASSIST MOTOR SEEMS TO BE RUNNING WHEN DOOR IS CLOSED. DEFFERED PASSENGER DOOR POWER ASSIST SYS IAW MEL 52-11-01, CAT C TICKET 22813 IAW MX CONTROL.

Part: PLACARD — WORN (CABIN) · airframe 15,381 hrs · 10,796 cycles

PAX DOOR OPEN PLACARD WORN. R/R PAX DOOR OPEN PLACARD IAW AMM 20-60-04.

Part: PLACARD — WORN (CABIN) · airframe 15,381 hrs · 10,796 cycles

PAX DOOR EXIT PLACARD IS WORN. R & R PAX DOOR EXIT PLACARD IAW AMM 20-60-04.

Part: PROXIMITY SWITCH — FAILED (PAX DOOR) · airframe 15,254 hrs · 10,716 cycles

PAX DOOR OUTER HANDLE CAUTION MSG CAME ON THEN OFF SEVERAL TIMES IN FLIGHT. DEFFERED MESSAGE ON DMI 23535 IAW MEL 52-70-01, CAT A AUTHORIZED. R & R PROX SWITCH PX107 IAW AMM 52-70-04. OPS CHECKED BGOOD, CLEARED DMI 23535.

Part: GATE — OUT OF ADJUST (PAX DOOR) · airframe 15,050 hrs · 10,592 cycles

OUTER FLAP ON PAX DOOR NOT CLOSING. ADJUSTED PAX DOOR HANDLE FLAP IAW AMM 52-11-00

Part: POWER CABLE — UNSECURE (PAX DOOR) · airframe 15,014 hrs · 10,572 cycles

MAIN CABIN DOOR OPENS ABRUPTLY AND SLAMS DOWN. RESECURED AND ADJUSTED POWER ASSIST CABLE ON THE MAIN CABIN DOOR IAW IAW AMM 52-11-08 OK FOR SERVICE AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,928 hrs · 10,526 cycles

EMERGENCY LIGHT AT CEILING ROW 4 INOP. DEFERRED LIGHT AT ROW 4 IAW MEL 33-51-01B, CAT C ON DMI 24265.

Part: SEAT — OUT OF POSITION (CABIN) · airframe 14,637 hrs · 10,349 cycles

ROW 11 SEATS ARE BLOCKING THE EMERGENCY EXIT DOORS. REPOSITIONED ROW 11 PAX SEATS IAW AMM 25-21-01.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 14,421 hrs · 10,200 cycles

PASSENGER DOOR KICK ANGLE CORRODED. REMOVED, LOCATED, DRILLED AND INSTALLED NEW PASSENGER DOOR KICK ANGLE IAW SRM 53-21-23, SRM 51-42-06, SRM 51-40-11. W/C 2117.

Part: BONDING JUMPER — CORRODED (ZONE 500) · airframe 14,421 hrs · 10,200 cycles

(V0XR) LT WING NR 5 FLAP HINGE BOX FWD BONDING JUMPER LOWER HARDWARE CORRODED. R & R FWD LWR BONDING JUMPER AND HARDWARE IAW AMM 51-80-00, TASK 51-80-00-910-810. W/C 5053.

Part: SILL — CORRODED (ZONE 200) · airframe 14,421 hrs · 10,200 cycles

(V0XR) AFT BAGGAGE BAY DOOR LOWER SILL CORRODED. SILL R & R IAW SRM 53-61-23 AND STANDARD PRACTICES. REF THE FOLLOWING HOLES AND C-SINK, IAW 51-41-00, 51-42-00, HARDWARE INSTALLATION IAW 51-42-00, SEALING IAW 51-23-00, METAL FINISHING IAW 51-21-16, AND PAINTING IAW 51-25-21 (AFT BAGGAGE BAY DOOR, LOWER).

Part: MOUNT — CORRODED (ZONE 200) · airframe 14,421 hrs · 10,200 cycles

(V0XR) GALLEY MOUNT CORRODED AT RBL 6 FS 315. R & R GALLEY MOUNT IAW SRM 51-42-21. W/C 2105.

Part: BULKHEAD — CORRODED (ZONE 200) · airframe 14,421 hrs · 10,200 cycles

(V0XR) LOWER AFT FACING OF THE BULKHEAD AFT AT FS 280.00, RT WEB CORRODED. REMOVED AND INSTALLED RT LWR WEB BULKHEAD FS280 IAW SRM 53-11-10.

Part: FITTING — CORRODED (ZONE 200) · airframe 14,421 hrs · 10,200 cycles

PAX DOOR CLOSING FITTING APPROX FS 325 CORRODED. R & R DOOR CLOSING FITTING PN SH670-31840-3. IAW SRM 53-21-23, SRM 51-40-11, SRM 51-41-02, SRM 51-42-06 (PAX DOOR FS 325) W/C 2106.

Part: BULKHEAD — CORRODED (ZONE 200) · airframe 14,421 hrs · 10,200 cycles

(V0XR) LOWER AFT FACING OF THE BULKHEAD AT FS280.00 LT WEB CORRODED. REMOVED AND INSTALLED LWR BULHEAD WEB FS280.00 IAW SRM 53-11-00.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 14,421 hrs · 10,200 cycles

(V0XR) FLOOR SUPPORT, FS 280, RBL 9 TO LBL 9 CORRODED BEYOND LIMITS. REMOVED AND INSTALLED FLOOR ANGLE SUPPORT FS278, RBL9.00 TO LBL 9.00 IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 14,421 hrs · 10,200 cycles

(V0XR) 280 BEAM IS CORRODED. ACCOMP GENERIC REPAIR FOR CROSSBEAM 280.00 REPLACEMENT-SPLICE IAW REO NR 670-53-11-047.

Part: SUPPORT ANGLE — CORRODED (ZONE 200) · airframe 14,421 hrs · 10,200 cycles

(V0XR) PAX DOOR MID CAP SUPPORT ANGLE CORRODED. R & R PAX DOOR MIDCAP IAW SRM 51-41-02, SRM 53-21-23, SRM 51-40-11.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,334 hrs · 10,105 cycles

(V0XR) 280 BLO FLOOR SUPPORT CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR SUPPORT ANGLE FS 280 IAW SRM 51-42-06. W/C 1042

Part: SILL — CORRODED (ZONE 100) · airframe 14,334 hrs · 10,105 cycles

(V0XR) SILL STRUCTURE RT FS280 TO FS319 CORRODED BEYOND LIMITS. R & R RT SILL FS280 TO FS319 IAW SRM 51-42-06. W/C 1050

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,334 hrs · 10,105 cycles

(V0XR) STA 280 CROSSBEAM CORRODED BEYOND LIMITS. ACCOMPLISH GENERIC REPAIR FOR CROSSBEAM 280.00. REPLACEMENT SPLICE IAW REO 670-53-11-047.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,007 hrs · 8,505 cycles

EMERGENCY LIGHTS DON'T WORK. PERFORMED OPS CHECK OF EMERGENCY LIGHT SYSTEM IAW AMM 33-51-00.

Part: CONTROL UNIT — MALFUNCTIONED (SLATS) · airframe 10,265 hrs · 7,307 cycles

SLATS FAIL ON EICAS DURING APPROACH TO LANDING. REPLACED NR 1 SFECU IAW MM 27-51-05.

Part: LANDING GEAR — MALFUNCTIONED · airframe 8,436 hrs · 5,992 cycles

GEAR DIDN'T RETRACT AFTER TAKEOFF, GEAR DISAGREE WARNING MESSAGE. DEFERRED LG RETRACT SYS IAW MEL 32-30-01-2 CAT A, DMI NR 8653.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 2,931 hrs · 2,140 cycles

CABIN EMERGENCY LIGHTS CEILING LEVEL LIGHT SIGN INOP. REPLACED NR 3 BATTERY PACK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 1,967 hrs · 1,435 cycles

MX-STL-EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BULB.