N601XJ

Part: TIE CLIP — CRACKED (LEFT) · airframe 24,396 hrs · 25,157 cycles

LH FS484 I/B O/B CLIP ARE CRACKED REMOVED AND REPLACED CLIP

Part: BULKHEAD — DAMAGED (BS 621) · airframe 24,396 hrs · 25,157 cycles

FS 621 BULKHEAD FWD FACE MULTIPLE SCREW SHANK MARKS ON SKIN AND REVIT HEADS. REPAIRED FS621 BULKHEAD IAW MHI BJ REO#601R53-61-7579

Part: PROXIMITY SENSOR — FAILED (LT MLG) · airframe 21,943 hrs · 22,340 cycles

LEFT MAIN GEAR DISAGREE AFTER TAKEOFF. UPON RETURNING TO SLC WE GOT ALL THREE LANDING GEAR DOWN AND LOCKED. (FLT # 4305) CLOSED REMOVED AND REPLACED THE LEFT HAND GEAR UPLOCK PROXIMITY SENSOR S20 (PS11GA), PERFORMED A FUNCTIONAL TEST OF THE LANDING GEAR EXTENSION/RETRACTION SYSTEM IAW AMM GEAR FUNCTIONAL CHECKS ARE GOOD.

Part: SEAL — LEAKING (PAX DOOR) · airframe 20,656 hrs · 20,946 cycles

LOUD SQUEAL IN FLT AND PRESSURIZATION PROBLEMS. RECEIVED CABIN ALTITUDE WARNING, PERFORMED AN EMERGENCY DESCENT AND DROPPED MASKS. LOUD SQUEAL NEAR MAIN CABIN DOOR. CLEANED AND LUBRICATED MCD SEAL IAW AMM. PERFORMED PRESSURIZATION TEST IAW AMM. OPS AND LEAK CHECKED GOOD.

Part: STRUT — DISCHARGED (NLG) · airframe 18,048 hrs · 18,117 cycles

AIRCRAFT RETURNED TO THE FIELD WITH A GEAR DISAGREE AND INTERMITTENT STEERING . COMPLIED WITH QRH AND MANUALLY EXTENDED GEAR. SERVICED NLG AND PERFORMED EXTENSION AND RETRACTION CHECK AS REQUIRED. NO OTHER DEFECTS NOTED.

Part: BULKHEAD — CRACKED (BS 621) · airframe 16,855 hrs · 16,857 cycles

DURING EDDY CURRENT INSPECTION OF THE REAR PRESSURE BULKHEAD FORWARD FACE, A CRACK INDICATION AT WL 86.5, RBL 27.5, APPROXIMATELY 0.534" IN LENGTH. REPAIRED FS 621 BULKHEAD AT WS 86.5, RBL 27.5 IAW REO. C/W ALL STEPS OF PERMANENT REPAIR. LEAK CHECK GOOD.

Part: SWITCH — DEFECTIVE (PAX DOOR) · airframe 15,162 hrs · 15,188 cycles

PASSENGER DOOR WAS FULLY OPEN & JET BRIDGE ATTACHED. PAX DOOR THEN BEGAN TO CLOSE WITHOUT POWER DOOR ASSIST SWITCH MANIPULATION. PULLED CBS P1 F1+ F2 IAW MOC TO STOP DOOR FROM CLOSING. R & R PAX DOOR ASSIST SWITCH IAW ESPM 20-24-00. OPERATIONS CHECKED GOOD IAW AMM 52-11-00. ACFT OK FOR SVC.

Part: TRIPLER — GOUGED (FUSELAGE) · airframe 14,391 hrs · 14,403 cycles

REPAIR TRIPLER AT FS 589 - 605 BETWEEN STRINGER 21R & 26R FOUND GOUGED. R & R IAW EA CRJ253-02662.

Part: SELECTOR VALVE — FAULTY (NLG) · airframe 14,209 hrs · 14,230 cycles

GEAR DISAGREE UPON LG EXTENSION. NOSE GEAR DID NOT EXTEND. DID NOT SOUND LIKE NOSE DOORS OPENED QRH COMPLETE. MANUAL EXTENSION HANDLE DROPPED NOSE GEAR AFTER ONE CYCLING ATTEMPTED FAILED NOSE DOORS CLOSED PROPERLY & NOSE WHEEL STEERING WORKED. R & R NLG SELECTOR VLV FUNCTIONAL TEST CHECKED GOOD IAW AMM 32-22-20.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 14,181 hrs · 14,205 cycles

AFT LT PHOTO LUMINESCENT STRIP IS DISPLACED & CRACKED ON CORNER. RECEIVED SERVICEABLE PHOTO LUMINESCENT STRIP, IAW WORK CARD 54523-2000-0073.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 14,164 hrs · 14,192 cycles

LOOSE LG DOOR CUT OUT IS CRACKED AT AFT RT CORNER 0.25 INCHES. REPAIRED IAW REO 601R-53-11-048.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 14,164 hrs · 14,192 cycles

LEFT INBD FLAP VANE HAS 3 CHAFED AREAS ON LE SKIN. REPAIRED IAW REO 601R-57-52-0004.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,164 hrs · 14,192 cycles

PAX DOOR PROX SENSOR HAS CORROSION AROUND HOLE IN FLOOR SUPPORT AT LBL 36 AT FS 339. REPAIRED IAW SRM 51-42-06, 51-42-13 & 51-42-21.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 14,164 hrs · 14,192 cycles

LEFT INBD FLAP HAS 3 EACH CHAFE MARKS ON VANE LE SKIN. INBD SECTION BLENDED 1.2" X 0.5" X 0.018" DEEP, CTR SECTION REPLACED, OTBD BLENDED 1.8" X 0.5" X0.014" DEEP. REPAIRED IAW REO 601R-57-52-004.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 14,164 hrs · 14,192 cycles

LBL 27 FLOORBEAM INBD & OTBD INTERCOSTAL BETWEEN FS 574 & FS 589 HAS NUMEROUS OVERSIZED HOLES, CLEANED UP TO 0.247" - 0.262" DIAMETER. REPAIRED IAW REO 601R-53-00-005 & 601R-53-61-3780.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 14,164 hrs · 14,192 cycles

LIGHTNING BURN AT FS 358 & STRINGER 27. THE BURN MARK WAS REMOVED BY BLENDING WITH FINAL BLEND DIMENSIONS OF 4.5” X 3.5” X 0.029” DEEP. REPAIRED IAW EA CRJ253-02470.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 14,164 hrs · 14,192 cycles

FS 621 BULKHEAD FWD FACE CHAFED IN MULTIPLE LOCATIONS FROM WL 86.5 TO WL 10.35 & LBL 27.5 TO RBL 27.5. REPAIRED IAW REO 601R-53-61-2155.

Part: ELT — FAILED · airframe 14,104 hrs · 14,133 cycles

ELT FAILS G SWITCH TEST. DEFERRED ELT IAW MEL 25-62-01 CAT A PER MOC GF AUTH 003545, MM02 UPDATED & PLACARD INSTALLED. REMOVED ELT IAW DDG 25-62-01.

Part: SKIN — DENTED (RUDDER) · airframe 12,399 hrs · 12,443 cycles

2 SMALL DENTS ON THE LEFT RUDDER SKIN. THE DENTS MEASURE 1.0 IN DIA X .019 DEEP AND .50 IN DIA X .006 DEEP. REPAIRED IAW EA CRJ255-01566 AND ASSOCIATED 8110-3.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 12,399 hrs · 12,443 cycles

RIGHT WING ACCESS PANEL 640BB CUTOUT LANDING IS CHAFED AND PITTED. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,399 hrs · 12,443 cycles

FLOOR CLIP AT FS 280 JUST OUTBOARD OF LBL 9 FOUND CRACKED. REPAIRED IAW SRM 51-42-06/51-42-21.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 12,399 hrs · 12,443 cycles

FUSELAGE SKIN FROM FS 589 - FS 603, S22R - S26R HAS MULTIPLE DENTS. REPAIRED IAW EA CRJ253-01552 AND ASSOCIATED 8110-3.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 12,399 hrs · 12,443 cycles

LEFT WING ACCESS PANEL 540BB CUTOUT LANDING IS CHAFED AND PITTED. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: BULKHEAD — SCRATCHED (FUSELAGE) · airframe 12,399 hrs · 12,443 cycles

SCRATCHES ON FS 621 BULKHEAD. REPAIRED IAW BOMBARDIER REO 601R-53-61-4901.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 12,399 hrs · 12,443 cycles

FS 621 BULKHEAD HAD SCREW GOUGES FROM CARGO LINER. REPAIRED IAW BOMBARDIER REO 601R-53-61-4901.

Part: BULKHEAD — SCRATCHED (FUSELAGE) · airframe 12,399 hrs · 12,443 cycles

FS 621 BUKLHEAD HAS MINOR SCRATCHES FROM CARGO LINER SCREWS. REPAIRED IAW BOMBARDIER REO 601R-53-61-4901.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 12,204 hrs · 12,248 cycles

FLIGHT ATTENDANT'S LIFE VEST BAG IS TORN. REMOVED AND REPLACED FLIGHT ATTENDANT'S LIFE VEST IN ACCORDANCE WITH AMM 25-61-03.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 12,092 hrs · 12,139 cycles

FIRST OFFICER'S LIFE VEST HAS A TEAR IN BAG. REMOVED AND REPLACED FIRST OFFICER'S LIFE VEST IAW AMM 25-61-03.

Part: SIGN — CRACKED (CABIN) · airframe 12,062 hrs · 12,113 cycles

EXIT SIGN ABOVE SERVICE DOOR CRACKED. REMOVED AND REPLACED EXIT SIGN IAW AMM 33-21-38.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 11,315 hrs · 11,351 cycles

EXIT ROW GLOW STRIP MISSING ON LEFT SIDE EXIT ROW 8. REPLACED MISSING GLOW STRIP IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 10,558 hrs · 10,497 cycles

RT OVERWING EMERGENCY EXIT EXTERNAL LIGHT (FWD) INOP. RELAMPED FWD RT WING EMERGENCY EXIT EXTERNAL LIGHT BULB P/N 1317.

Part: SELECTOR VALVE — INOPERATIVE (NLG) · airframe 8,409 hrs · 8,017 cycles

AFTER GEAR UP SELECTION, EICAS RED NOSE DOOR OPEN LIGHT ILLUMINATED. NOTICED AIR NOISE AND FOLLOWED NON-NORMAL PROCEDURES. SELECTED GEAR DOWN AND NOSE DOOR OPEN MESSAGE WENT OUT AND THEN REAPPEARED. CONTACTED ATC TO RETURN TO DEPARTURE. THE CREW THEN CONTACTED DISPATCH AND MX CONTROL TO INFORM THEM OF THE EICAS WARNING. THE RETURN TO DEPARTURE, OCCURRED UNEVENTFULLY. FOUND CLOSED SOLENOID OF NOSE GEAR DOOR SELECTOR VALVE BAD. R & R NLG DOOR SELECTOR VALVE IAW MM 32-22-00. ALL CKS GOOD IAW MM 32-22. PN ON/OFF 750006000, S/N ON 0780T, S/N OFF 0796T.

Part: PCU — MISRIGGED (SPOILERS) · airframe 1,888 hrs · 1,803 cycles

ON TAKEOFF ROLL, CONFIGURATION, SPOILERS MESSAGE APPEARED. ABORTED TAKEOFF. FOUND LT INBOARD SPOILER PCU SLIGHTLY OUT OF RIG, ADJUSTED SPOILER IAW AMM.

Part: PROXIMITY SWITCH — MALFUNCTIONED (MLG) · airframe 1,249 hrs · 1,207 cycles

AFTER TAKEOFF OUT OF MSP BROUGHT GEAR UP AFTER GEAR WAS RETRACTED GOT A NOSE DOOR MESSAGE AND GEAR DISAGREE LIGHT MESSAGE. COMPLETED REPLACEMENT OF NOSE OLEO CENTERED/EXTENDED BRACKET, PROX SWITCH AND SETTING OF GAP OF PROX SWITCH WITH GEAR SWINGS. OPS CHECK GOOD OF EXTENSION/RETRACTION.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG DOOR) · airframe 1,037 hrs · 989 cycles

NOSE DOOR OPEN LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO MSP. PROX SENSOR GAP OUT OF LIMITS. ADJUSTED GAP TO WITHIN LIMITS. REF: CRJ AMM 32-61-05. PERFORMED GEAR SWINGS. REF: CRJ AMM 32-30-00. OPS CHECK GOOD.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 439 hrs · 421 cycles

CREW REPORTED THAT THEY LOST NR 2 HYDRAULIC QUANTITY INFLIGHT AND DIVERTED TO ABE FOR RUNWAY REQUIREMENTS. REPLACED EDP.

Part: ODOR — DETECTED (APU) · airframe 432 hrs · 415 cycles

APU AUTO SHUT DOWN INFLIGHT HAD A BRIEF STRONG BURNING ODOR IN COCKPIT IT WENT AWAY AS SOON AS APU STOPPED. DEFERRED APU PER MLE 49-10.