N8938A

Part: STOWAGE BOX — LEAKING (OXYGEN MASK) · airframe 25,520 hrs · 22,887 cycles

PILOT OXYGEN MASK STOWAGE BOX TEST BUTTON LEAKING. REPLACED PILOT OXYGEN MASK STOWAGE BOX IAW AMM 35-11-15. NO LEAKS NOTED. OPS CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 8CD) · airframe 25,103 hrs · 22,456 cycles

OXYGEN MASKS IN SEAT 8 C/D ARE DEPLOYED. REPACKED THE OXYGEN MASKS FOR SEAT 8 C,D AND PERFORMED OPS CHECKED IAW AMM 35-21-09.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,644 hrs · 21,975 cycles

DURING WAKE UP CHECK, NOTED EMER FLOOR LIGHTS AT ROW 2 - 5 & LT EMER EXIT LIGHT AT ROW 7 INOPERATIVE. R & R NR 2 INVERTER WITH SERVICEABLE UNIT, PN ON & OFF 5925-7 & SN N/A IAW AMM 33-51-07-04. ALL CHECKED GOOD.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 24,590 hrs · 21,925 cycles

FLOOR EMER EXIT STRIPS, SEATS 2 - 5 NOT LIT. CONNECTED FLOOR EMER LIGHTS, CHECKED GOOD IAW AMM 33-51-01. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,437 hrs · 21,790 cycles

FLIGHT ATTENDANT EMER SWITCH TURNED ON WILL NOT ILLUMINATE, ROWS 2 - 5 ON FLOOR TRACK LIGHTING. PERFORMED ADJUSTMENT & TEST OF ROWS 2 - 5 FLOOR TRACK LIGHTING IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 24,184 hrs · 21,533 cycles

CAPTAINS SIDE OXYGEN MASK NOT TESTING PROPERLY. WHILE HOLDING PRESS TO TEST, O2 FLOW CONTINUES WHEN IT SHOULD NOT, & MARKER REMAINS YELLOW, NOT BLACK. SWAPPED CAPTAINS SIDE 02 MASK WITH OBSERVERS SIDE 02 MASK, PROBLEM FOLLOWED DEFERRED OBSERVERS MASK IAW MEL 35-10-01 CAT AN AUTHORIZATION 002843 IAW MOC 96184 PLACARD INSTALLED.. OBSERVERS SEAT IS CONSIDERED INOPERATIVE. R & R OBSERVER'S OXYGEN MASK IAW AMM 35-11-12. MM02 UPDATED & PLACARD REMOVED. THHIS CLEARS MEL 35-10-01 CONTROL 002843.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 24,104 hrs · 21,449 cycles

RIGHT FWD FUSELAGE POWER RECEPTACLE STRUCTURE CRACKED. REMOVED ACFT POWER RECEPTACLE BRACKET IAW SRM 51-42-06 & SRM 51-42-21. INSTALLED ACFT POWER RECEPTACLE BRACKET IAW SRM 51-42-06 & 54-42-21. LOCATED & DRILLED NEW AC POWER BRACKET RECEPTACLE IAW SRM 51-40-11. REMOVED AC POWER RECEPTACLE IAW AMM 24-41-03-000-802. INSTALLED SAME SERVICEABLE EXTERNAL AC POWER RECEPTACLE IAW AMM 24-41-03-400-802,. REMOVED EXTERNAL SERVICE PANEL BY REMOVING 4 SCREWS IAW SRM 51-41-02. INSTALLED EXTERNAL SERVICE PANEL BY INSTALLING 4 SCREWS IAW SRM 51-41-02. CLOSE OUT STEPS 4A & B OF AMM 24-41-03-400-802 REQUIRE COMPLETION. COMPLIED WITH CLOSEOUT STEPS 4A & B OF AMM 24-41-03-400-802. NO DEFECTS NOTED. R & R AC POWER RECEPTACLE BRACKET PN 600-33283-33 IAW SRM 51-42-06 & 51-42-21.

Part: SKIN — CHAFED (RT AILERON) · airframe 24,104 hrs · 21,449 cycles

RIGHT AILERON UPPER LE SKIN HAS 2 CHAFED AREAS AT OTBD HINGE. INBD DAMAGE MEASURES APPROX 1.2"" LONG X 0.6"" WIDE X 0.010"" DEEP. OTBD DAMAGE MEASURES APPROX .9"" LONG X 0.6"" WIDE X 0.020"" DEEP. R & R UPPER LE SKIN IAW SRM 51-42-06 & 51-42-20. LE PN CC670-13052-4. UPPER LE SKIN REQUIRES PAINT. PAINTED UPPER LE SKIN IAW SRM 51-25-01. FIVE EACH RIVETS FOUND NOT ACCEPTABLE DUE TO BEING NAILED, TO SHORT OR NOT SHOT DOWN PROPERLY. REMOVED FIVE EACH UNSERVICEABLE RIVETS & REPLACED WITH FIVE EACH NEW SERVICEABLE RIVETS IAW SRM 51-42-06. INTERNAL FASTENER NEED PAINTED. TOUCHED UP FASTENERS IAW SRM 51-25-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,104 hrs · 21,449 cycles

FS 333.00 FRAME CRACKED APPROX 2""L AT STRINGER 1L. R & R CRACKED FRAME AT FS 333, BETWEEN STRINGER 0 & STRINGER 3L IAW SRM 61-42-06 & 51-12-21. REMOVED CRACKED FRAME AT FS 333, BETWEEN STRINGER 0 & 3L IAW SRM CH 51-42-06 & SRM CH 51-42-21. REPLACE FRAME PN 601R32004-41 IAW SRM 51-42-06 & SRM 51-42-21. LOCATED & DRILLED NEW FRAME PN 601R32004-41 IAW SRM 51-40-11. BONDING WIRE N103 ON FS 333 FRAME REQUIRES INSTALLATION. UPON FURTHER INVESTIGATION, FOUND NO GND WIRES REQUIRING ATTACHMENT TO GND STUD N103 IAW WM 91EEL & 91EWL. GND STUD N103 IS INSTALLED AT FS 333, BETWEEN STRINGER 0 & 3L.

Part: POST — DAMAGED (FUSELAGE) · airframe 24,104 hrs · 21,449 cycles

FS 409+128 VERTICAL POST HAS ONE INDICATION .3"" LONG BY 90% FSH ON THE BL 0.0 LT VERTICAL POST AFT RADIUS. FAILED NDT INSPECTION. REMOVED Y DUCT & UNDER FLOOR AC DUCT BY REMOVING 3 EA ADEL CLAMP, 3 EA WORM CLAMP. REINSTALLED Y DUCT & UNDER FLOOR AC DUCT BY REINSTALLING 3 EA ADEL CLAMPS, 3 EA WORM CLAMPS IAW SRM 51-41-04. REMOVED INSULATION FROM AROUND FS 409+128, BL 0. REINSTALLED INSULATION AT FS 409+128 BL 0 IAW AMM 25-81-02-400-801. REMOVED FS 409+128, BL 0 POST ASSEMBLY IAW SRM 51-42-06 & 51-42-21. OK TO INSTALL. INSTALLED NEW SERVICEABLE BL 0 POST ASSEMBLY IAW SRM 51-42-06 REO 601R-53-41-889. DRILL & LOCATED NEW SERVICEABLE BL 0 POST ASSEMBLY IAW SRM 51-42-06 & 51-42-21. PERFORMED A MAJOR REPAIR TO FS 409+128 VERTICAL POST BL 0 IAW SRM 51-42-06 & REO 601R-53-41-889.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 24,104 hrs · 21,449 cycles

INTERCOSTAL CORRODED, BETWEEN FS 333 & FS 349, STRINGER 20R. REMOVED CORRODED INTERCOSTAL IAW SRM 51-42-06 & 51-42-11. LOCATED & DRILLED NEW INTERCOSTAL IAW SRM 51-40-11. NEW INTERCOSTAL REQUIRES INSTALL. INSTALLED NEW INTERCOSTAL & INSTALLED BETWEEN FS 333.00 & FS 349.00 IAW SRM 51-42-06 & 51-42-21. NO FURTHER ACTION REQUIRED. SUMMARY STATEMENT REQUIRED.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 24,104 hrs · 21,449 cycles

SERVICE DOOR LOWER SILL ANGLE & DRAIN HOSE AFT ATTACH ANGLE CORRODED, BETWEEN FS 319 & 349, STRINGER 18R. REMOVED SERVICE LOWER SILL ANGLE BY REMOVING RIVETS, CHERRYMAX & HI-LITES IAW SRM 51-42-06/10/21. INSTALLED NEW LT WING SIDE SILL ANGLE AT SERVICE DOOR IAW SRM 51-42-06, 51-42-10, 51-42-21, 51-42-34. LOCATED & DRILLED NEW SERVICEABLE DOOR LOWER SILL ANGEL PN 601R38303-253 IAW SRM 51-40-11. REMOVED FWD & AFT STOP FITTINGS & ANGLE TO GAIN ACCESS TO SERVICE DOOR LOWER SILL ANGLE BY REMOVING BOLTS IAW SRM 51-41-02. INSTALLED FWD & AFT STOP FITTINGS & ANGLE IAW SRM 51-42-21. AFT DRAIN HOES ATTACH ANGLE REQUIRES REPLACEMENT IAW SRM 51-41-02, 51-40-11. LOCATED, DRILLED, DEBURRED & INSTALLED NEW ATTACH ANGLE FOR AFT DRAIN HOSE A SERVICE DOOR IAW SRM 51-41-02 & 51-40-11. FWD & AFT SPIGOTS FITTING FOR SERVICE DOOR NEED SAFETIED. SAFETY WIRED FWD & AFT SPIGOT FITTING FOR SERVICE DOOR IAW AMM 20-24-00-910-802. R & R SERVICE DOOR SILL LOWER ANGLE & DRAIN HOSE AFT ATTACH ANGLE IAW SRM 51-42-06, 51-42-10, 51-42-21 & 51-42-34.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,104 hrs · 21,449 cycles

PRESSURE BULKHEAD FS 202.75 AT BL 23.75, FOUND MULTIPLE INDICATIONS EXTENDING A MAXIMUM OF .45"" LONG BY 100%FSH AROUND PARKING BRAKE PASS THROUGH HOLE FROM 6 O'CLOCK POSITION TO 2 O'CLOCK POSITION. LEAKING AFT, FAILED NDT. COMPLIED WITH STEP 1 & 2 OF REO 601R-53-11-563 REV C DATED 11 21 12 REPAIR TYPE IV. COMPLIED WITH STEP 7 - 10 OF REO 601R-53-11-563 REV C DATED 11 21 12 REPAIR TYPE IV. Z MEMBER PLUS SHIMS REQUIRE INSTALL. Z MEMBER PO 604-34-012-81 & SHIMS POW36712. INSTALLED Z MEMBER, ANGLE, T MEMBER, SHIMS 13, 14, 15 & 16 IAW SRM 51-42-06, 51-42-21 & REO 601R-53-11-563 REPAIR TYPE N REV C DATED 11/21/12. LOCATED & DRILLED NEW Z ANGLE PN 604-34012-81 & RUDDER PEDAL T MEMBER PN 600-90201-113 IAW SRM 51-40-11. REPAIRED FS 202.75 BULKHEAD DAMAGE IAW REO 601R-53-11-563.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 24,104 hrs · 21,449 cycles

AFT FUSELAGE PRESS BULKHEAD, APPROX 32" UP FROM FLOOR, 7 EA CHAFE & GOUGES FROM SCREWS, APPROX .180 DIA X .002 DEEP. REPAIRED AFT FUSELAGE PRESS BULKHEAD IAW REO 601R-53-61-2155. .002"" MAX MATERIAL REMOVED AT ALL LOCATIONS. SCREW LENGTHS REQUIRE ADJUSTMENT TO PREVENT FURTHER CHAFING IAW REO 601R-53-61-2155. ADJUSTED SCREW LENGTHS AS REQUIRED TO PREVENT FURTHER CHAFING ON 621 BULKHEAD IAW REO 601R-53-61-2155. COMPLIED WITH REO 601R-53-61-2155 TO REPAIR AFT BULKHEAD CHAFES & TO PREVENT FURTHER DAMAGE.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 24,104 hrs · 21,449 cycles

PASSENGER DOOR INTERNAL HANDLE HAS A CRACK. REMOVED CRACKED PAX DOOR INTERNAL HANDLE IAW AMM 52-11-21-000-801 SUB TASK 52-11-21-020-012, STEP N5. LOCATED NEW FASTENER HOLES TO NEW SERVICEABLE HANDLE IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE PAX DOOR INTERNAL HANDLE IAW AMM 52-11-21-400-801 SUB TASK 52-11-21-420-004, STEP G8. EXIT & BETA SIGN INSTALLED UPSIDE DOWN. REINSTALLED EXIT & BETA SIGN CORRECTLY IAW AMM 20-21-00-910-801. R & R PAX DOOR INTERNAL HANDLE IAW AMM 52-11-21-400-801, SUB TASK 52-11-21-420-004 STEP G 8. NO DEFECTS NOTED.

Part: POST — CRACKED (FUSELAGE) · airframe 24,104 hrs · 21,449 cycles

FS 409+128, BULKHEAD VERTICAL POSTS CRACKED AT BOTTOM INBD CORNERS LBL 27 & RBL 27. REMOVED SUPPLY AIR FILTER IAW AMM 21-24-01-000-801. REINSTALLED SUPPLY AIR FILTER IAW AMM 21-24-01-400-801. REMOVED SUPPLY AIR FILTER DUCT BY REMOVING & SCREWS FROM THE STRUCTURE. REINSTALLED SUPPLY AIR FILTER DUCT IAW AMM 21-24-01-400-801. REMOVED SUPPLY AIR FILTER DUCT SUPPORT BRACKET ASSEMBLY IAW SRM 51-42-06. REINSTALLED SUPPLY AIR DUCT BRACKET ASSEMBLY IAW SRM 51-42-06. COMPLIED WITH REO 601R-53-41-056 REV F 2011 09 02.

Part: SKIN — CORRODED (RT WING) · airframe 24,104 hrs · 21,449 cycles

RIGHT WING LOWER PLANK HAS MULTIPLE INDICATIONS NOTED NEXT TO FOOTPRINT OF DRAIN HOLE FITTING AT BOOST PUMP 55% FSH. FAILED NDT INSPECTION. COMPLIED WITH WORK PACKAGE DRAIN HOLE SURFACE INSPECTION. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-21-06. ENGINEERING REQUIRED FOR FURTHER DISPOSITION. COMPLIED WITH REO 601R-57-21-2374, NO LEAKS NOTED AT THIS TIME. REPAIRED RT WING LOWER FLANK DRAIN HOLE FITTING AT BOOST PUMP IAW REO 601R-57-21-2374. THIS IS A MAJOR REPAIR. DTA REQUIRED WITHIN 12 MONTHS OF REPAIR. RECORDED DTA ON AML, REFERENCE ATTACHED LOG PAGE 3258680. COMPLIED WITH WORK PACKAGE DRAIN HOLE SURFACE INSPECTION. REF JOB 8793815 OP 69 FOR INDICATIONS NOTED. NO OTHER INDICATIONS NOTED.

Part: WIRE — BROKEN (CABIN) · airframe 24,104 hrs · 21,449 cycles

WIRE BROKEN TO EMER EXIT LIGHT IN BOTTOM OF WARDROBE. UPON INVESTIGATION, FOUND CONNECTOR BROKE OFF END OF WIRE. INSTALLED NEW SERVICEABLE CONNECTOR FOR EMER LIGHT IAW ESPM 20-17-31. OPERATIONS TEST OF THE EMER LIGHTS DUE. OPERATIONS TEST OF EMER LIGHTS GOOD IAW AMM 33-43-00-710-801.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 24,104 hrs · 21,449 cycles

INFANT LIFE VEST OUTER PACKING IS TORN OPEN, UNSERVICEABLE. REMOVED UNSERVICEABLE INFANT LIFE VEST FROM LT FWD CLOSET. INSTALLED SERVICEABLE INFANT LIFE VEST IN LT FWD CLOSET AT PLACARD LOCATION.

Part: CONNECTOR — MISSING (CABIN) · airframe 24,104 hrs · 21,449 cycles

ELECTRICAL CONNECTS FOR FLOOR TRACK EMER LIGHTS ARE MISSING IN MULTIPLE LOCATIONS. REPAIRED ELEC CONNECTORS FOR FLOOR TRACK EMER LIGHTS IAW ESPM 20-11-00. OPERATIONS TESTED GOOD IAW AMM 33-51-00-710-801.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,104 hrs · 21,449 cycles

COPILOT FLASHLIGHT IS NOT BLINKING & DOES NOT COME ON WHEN PULLED FROM HOUSING. WARDROBE FLASHLIGHT, EMER USE ONLY STRAP IS BROKEN. R & R TAMPER STRAP ON WARDROBE FLASHLIGHT IAW AMM 20-21-00-910-801, PN A1-18-1030.

Part: SEPARATOR — CHAFED (LT PYLON) · airframe 24,104 hrs · 21,449 cycles

LEFT ENG, LOWER PYLON, PN 412DB, FWD SEPARATOR IS CHAFED. R & R LT ENG, LOWER PYLON PANEL 412DB SEPARATOR WITH NEW SERVICEABLE SEPARATOR IAW SRM 51-40-11, 51-42-06 & 51-42-13.

Part: BRACKET — BROKEN (TE FLAP) · airframe 24,104 hrs · 21,449 cycles

BONDING JUMPER BRACKET BROKEN ON LT FLAP HINGE BOX, STATION 127.25. REPLACED ANGLE BRACKET, BONDING WIRE JUMPER, LT FLAP HINGE BOX, PN 600-14500-9 IAW EA CRJ257-03796 & SRM 51-42-21.

Part: FITTING — CHAFED (RT PYLON) · airframe 24,104 hrs · 21,449 cycles

RIGHT ENG UPPER PYLON, PN 422BT, TWO INBD CLIPS ARE CHAFED. REMOVED NO STEP PLACARD FOR ACCESS IAW AMM 11-20-00-000-801. APPLIED NO STEP PLACARD TO PANEL 422BT IAW AMM TASK 11-20-00-400-801. REMOVED TWO EACH UNSERVICEABLE INBD CLIPS FROM RT ENG UPPER PYLON PANEL 422BT, PN 601-37003-180 & PN 601-37003-182, IAW SRM 51-42-06. INSTALLED TWO EACH NEW SERVICEABLE INBD CLIPS, PN 601R-370003-180 & PN 601-37003-182 IAW SRM 51-42-06. REQUIRES PREP & PAINT. APPLIED PAINT IAW SRM 51-25-06. WORK SUMMARY STATEMENT REQUIRED. R & R INBD CLIPS IAW SRM 51-42-06. REPLACED PLACARD ON PANEL 422BR IAW AMM 11-20-00-400-801.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,104 hrs · 21,449 cycles

INBD & OTBD ANGLES ON INTERCOSTAL IS CRACKED AT FS 484, RBL 27 & 36. REMOVED CABLE GUIDE TO ACCESS CRACKED ANGLE FOM, BY REMOVING BOLTS & NUTS IAW SRM 51-41-00. REINSTALLED SAME SERVICEABLE CABLE GUIDE IAW AMM 20-21-00-910-801 & 20-24-00-910-801. R & R INBD ANGLE ON INTERCOSTAL AT FS 484, RBL 27 BY REMOVING & REPLACING HI-LITES IAW SRM 51-42-21 & REO 601R-53-41-059. OTBD ANGLE REQUIRES REPLACEMENT IAW EA CRJ253-03784. R & R OTBD ANGLE ON INTERCOSTAL AT FS 484, RBL 36 BY REMOVING AND REPLACING HI-LITES IAW SRM 51-42-21, TWO EACH CRJ253-03784. R & R INBD ANGLE ON INTERCOSTAL RBL 27 WITH NEW CLIP ON 601R31171-9 IAW SRM 51-42-21. FABRICATED & INSTALLED NEW CLIP AT FS 484, RBL 36 IAW EA CRJ 253-03784. REINSTALLED SERVICEABLE GUIDE ROLLER IAW AMM 20-21-00-910-801.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 24,104 hrs · 21,449 cycles

FS 280 CROSSBEAM HAS 2 ATTACH ANGLE CRACKED AT LBL 9 & RBL 9. INSTALLED TWO EACH CABLE BLOCKS, TOOL 201175 & 201174, AT FS 280 - 295 ON MLG ALT RELEASE FOR BRACKET REMOVAL TO FOM. REMOVED TWO EACH CABLE BLOCKS, TOOL 201175 & 201174, FROM MLG ALT EXTENSION CABLE. REMOVED CRACKED FS 280 RBL & LBL 9.0 OTBD CLIPS IAW SRM 51-42-21. FABRICATED NEW RBL & LBL 9, FS 280.00 ATTACH CLIPS IAW EA CRJ253-03792, STEP 1. STEPS 2 - 6 OF EACH CRJ253-03792 REQUIRED. PERFORMED EDDY CURRENT INSPECTION ON FABRICATED CLIPS IAW EA CRJ253-03792, NO INDICATIONS NOTED. STEPS 3 - 6 OF EACH CRJ253-03792 REQUIRED. COMPLIED WITH EA CRJ253-03792, STEPS 3 - 6, FABRICATE FILLERS, INSTALLATION OF CLIPS, RETSORE FINISH & CORROSION PREVENTION APPLIED. REPLACED FS 280 ATTACH ANGLES CLIPS, TWO EACH AT LBL 9 & RBL 9 OTBD IAW EA CRJ253-03792. NO FURTHER ACTION REQUIRED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,104 hrs · 21,449 cycles

FOUND REAR PRESS BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .400 IN LENGTH 70% FSH. REPAIRED FS 621 BULKHEAD WEB AT THE LINTEL ATTACHMENT FITTING IAW REO 601R-53-61-1230 REV F DATED 10 31 1. THIS IS A MAJOR REPAIR. REPEAT INSPECTION REQUIRED WITHIN 6215 FLIGHT CYCLES. CURRENT FLIGHT CYCLES ARE 21449. THIS WILL REQUIRE REP DOCUMENTATION. TRACKING THE REPEAT INSPECTION IAW FORM 908.1.

Part: WIRE — BROKEN (CABIN) · airframe 24,104 hrs · 21,449 cycles

EMERGENCY TRACK LIGHTING WIRING UNDER FLOORBOARD 251CLF BROKEN. R & R EMER TRACK LIGHT CONNECTOR PIN PL29LY IAW ESPM 20-17-10. OPERATIONS CHECK DUE. REF AMM 33-51-00-710-801. OPERATIONS TEST OF FLOOR TRACK EMER LIGHTING GOOD IAW AMM 33-51-00-710-801.

Part: FLOW DIVIDER — CHAFED (RT PYLON) · airframe 24,104 hrs · 21,449 cycles

RIGHT ENG LOWER PYLON, PN 422DB, FWD DIVIDER IS CHAFED. R & R DISCREPANT DIVIDER ON PANEL 422DB IAW SRM 51-42-06.

Part: SKIN — DAMAGED (FLAP FAIRING) · airframe 24,104 hrs · 21,449 cycles

THE LT FLAP STUB FAIRING IS CHAFED ON THE OUTER SKIN & FWD BRACKET IS DAMAGED. UPON FURTHER INVESTIGATION FOUND FWD FITTING ON LT WING TO BE DAMAGED, REQUIRES REPLACEMENT. REMOVED UNSERVICEABLE FITTING ON LT WING & REPLACED WITH NEW SERVICEABLE FITTING, PN 601R10371-1 IAW SRM 51-40-11 & SRM 51-42-21. REMOVED TWO EACH SERVICEABLE SEALS & TWO EACH SERVICEABLE SEAL RETAINERS FROM UNSERVICEABLE LT FLAP STUB FAIRING IAW SRM 51-42-06. LOCATED, DRILLED & INSTALLED TWO EACH SERVICEABLE SEALS & TWO EACH SERVICEABLE SEAL RETAINERS ON SERVICEABLE LT FLAP STUB FAIRING IAW SRM 51-40-11 & SRM 51-42-06. LT FLAP STUB FAIRING REQUIRES PREP & PAINT. PAINTED AS NEEDED IAW SRM 51-25-01. UPPER FWD HINGE ASSEMBLY REQUIRES LOCATED & INSTALLED ONCE BELLY FAIRING PANEL 195AL IS INSTALLED. LOCATED, DRILLED & INSTALLED NUTPLATES ON UPPER FWD HINGE ASSEMBLY IAW SRM 51-40-11 & 51-42-06. REPLACED LT FLAP STUB FAIRING WITH PN 601R31199-91. ALL WORK DONE IAW SRM 51-40-11 & 51-42-06.

Part: PANEL — CHAFED (LT COWLING) · airframe 24,104 hrs · 21,449 cycles

LEFT ENG, LOWER FAN COWL PANEL 432AB, TE IS CHAFED IN SEVERAL AREAS. R & R LT ENG LOWER FAN COWL TE IAW CMM 71-14-01-300-814-A01 REPAIR SRS091. UPON FURTHER INVESTIGATION, FOUND CHAFE DAMAGE TO BE OUT OF LIMITS OF CMM TASK 71-14-01-300-813-A01 SRS090, REQUIRES AFT EDGE STRIP REPLACEMENT. R & R TE, PN 228-50081-107 IAW CMM 71-14-01-300-814-A01 REPAIR SRS091. NEW PART REQUIRES PAINT. PREPPED & PAINTED REPAIR ON LT ENG LOWER FAN COWL TE IAW SRM 51-25-01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,104 hrs · 21,449 cycles

PASSENGER DOOR AFT SIDE DRAG ANGLE CRACKED, PREV REPAIR. FOUND PREV REPAIR TO BE 601R-52-11-513 REPAIR TYPE, DISREGARD PREV REPAIR & ACCOMPLISH 601R-52-11-513 REPAIR TYPE 11. REPAIRED AFT PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513. REMOVED PAX DOOR POWER ASSIST MOTOR IAW AMM 52-11-08-000-802. REMOVED FOR ACCESS. REINSTALLED PAX DOOR POWER ASSIST MOTOR IAW AMM 52-1-108-400-802. COMPLIANCE STATEMENT REQUIRED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW GREO 601R-53-11-513 REPAIR TYPE 2.

Part: POST — DAMAGED (FUSELAGE) · airframe 21,104 hrs · 21,449 cycles

FS 409+128, VERTICAL POSTS HAVE ONE EACH INDICATION .2" LONG BY 95% FSH ON THE BL 0.0 RT VERTICAL POST AFT RADIUS, RBL 18.0 OTBD VERTICAL POST .25" LONG BY 95% FSH AFT RADIUS, INBD VERTICAL POST .3" LONG BY 98% FSH AFT RADIUS. FAILED NDT INSPECTION. REINSTALLED OVERBOARD EXHAUST VLV IAW AMM 21-24-34-400-801. REMOVED INSULATION FROM AROUND FS 409+128 RBL 18. REINSTALLED INSULATION AT RBL 18 IAW AMM 25-81-02-400-801. REMOVED FS 409+128 RBL 18 POST ASSEMBLY. INSTALLED NEW SERVICEABLE POST ASSEMBLY IAW SRM 51-42-06, REO 601R-53-41-889. DRILL LOCATED NEW SERVICEABLE RBL 18 POST ASSEMBLY IAW SRM 51-42-06. OPERATIONS CHECK OF OVERBOARD EXHAUST VLV REQUIRED, REF TASK 21-24-34-710-801. OPERATIONS TESTED GOOD IAW AMM 21-24-34-710-801. DRILLED, LOCATED & INSTALLED NEW SERVICEABLE POST AT RBL 18 IAW SRM 51-42-06 & REO 601R-53-41-889. NO FURTHER ACTION REQUIRED.

Part: COWLING — CHAFED (RT ENGINE) · airframe 24,104 hrs · 21,449 cycles

RIGHT ENG UPPER FAN COWL HAS SEVERAL CHAFED AREAS ALONG TE. R & R RT ENG UPPER FAN COWL TE IAW CMM 71-41-01-300-814-A01 REPAIR SRS091. UPON FURTHER INVESTIGATION, FOUND CHAFE DAMAGE TO BE OUT OF LIMITS OF CMM TASK 71-14-01-300-813-A01 SRS090. REQUIRES AFT EDGE STRIP REPLACEMENT. INSTALLED NEW AFT EDGE STRIP ON RT ENG UPPER FAN COWL. WORK PERFORMED IAW CMM TASK 71-14-01-300-814-A01 REPAIR SRS091. APPLY EXTERNAL TOPCOAT TO REPAIR AREA. PREPPED & APPLIED TOPCOAT TO REPAIRED AREA ON RT UPPER EDGE COWL TE IAW SRM 51-25-01.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 24,104 hrs · 21,449 cycles

RIGHT MLG WW HYD TRANSDUCER BRACKET CRACKED. R & R RT MLG WW HYD TRANSDUCER BRACKET IAW SRM 51-42-06 & SRM 51-40-11.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 24,104 hrs · 21,449 cycles

FORWARD LT SIDE OF FUSELAGE, STRINGER 3L, CRACKED AT FS 280. REMOVED LT FWD STRINGER 31 AT FS 280 IAW SRM 51-42-06 & 51-42-21. DRILLED NEW SERVICEABLE STRINGER 3L CLIP IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE CLIP IAW SRM 51-42-06 & 51-42-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,104 hrs · 21,449 cycles

FOUND REAR PRESS BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130, APPROX .500 INCHES IN LENGTH 50% FSH. FAILED NDT INSPECTION. REPAIRED CRACK IN FS 621, REAR PRESS BULKHEAD WEB AT LBL 27.50, WL 130 IAW REO 601R-53-61-1541 REV F DATED 11 12 14.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,423 hrs · 20,742 cycles

EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE IN ROWS 5. PLACED EMER FLOOR TRACK LIGHTING AT ROW 5 ON DEFERRAL IAW MEL 33-51-17. REPLACED EMER LIGHT LAMP STRAP IAW 33-51-01. OPERATIONS CHECKED GOOD. OK FOR SERVICE. THIS CLEARS DM 1267, MM02 UPDATED & PLACARD REMOVED.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 23,283 hrs · 20,587 cycles

FLOOR LEVEL EMER LIGHT STRIP HAS DAMAGED CONNECTOR, MALE, SIDE OF THE TWO WIRES THAT COME THROUGH THE FLOORBOARD. AFT PORTION OF EMER LIGHT STRIP NEEDS REINSTALLED. FOUND NO DAMAGE TO CONNECTOR, PIN WAS BENT. STRAIGHTENED PIN, RECONNECTED WIRES & REINSTALLED AFT PORTION OF EMER LIGHT STRIP FLOOR LEVEL IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG) · airframe 23,041 hrs · 20,331 cycles

RIGHT MLG AFTER GEAR DISAGREE MASTER CAUTION QRH COMPLETE. DURING TROUBLESHOOTING FOR DISC 1 ON AML 3180474 FOUND RT MLG UPLOCK TARGET LOOSE. REFER TO CORRECTIVE ACTION NR 2 ON AML 3180474 PREFORMED GEAR SWING CHECK IAW AMM 32-30-00. OPERATIONS CHECKED GOOD, OK FOR SERVICE. ADDED ADDITIONAL WASHER TO THE RT MLG UPLOCK IAW CMM 32-30-15, ADJUSTED PROX SENSOR ON RT MLG UPLOCK IAW AMM 32-61-05. PSEU CORRELATION CHECKED GOOD. ACFT REQUIRE GEAR SWING REFER TO DISC 1 1 ON AML 3180474 NO CODES WERE FOUND IN THE PSEU.

Part: SKIN — DENTED (FUSELAGE) · airframe 22,570 hrs · 19,868 cycles

DENT WAS NOTED IN THE FUSELAGE SKIN BETWEEN FS 582 & FS 588 STRINGER 20L & 21L MEASURING 6 INCHES X 1 INCH X 0.010 INCHES DEEP. REPAIRED IAW EA CRJ253-02952.

Part: SKIN — DENTED (FUSELAGE) · airframe 22,570 hrs · 19,868 cycles

MAINTENANCE FOUND TWO DENTS IN THE FUSELAGE SKIN BETWEEN FS 667 & 681 BETWEEN STRINGER 18L & 19L. THE FWD DENT MEASURES 3.00 INCHES X 1.0 INCHES X 0.002 INCHES DEEP & THE AFT DENT MEASURES 8.0 INCHES X 1.25 INCHES X 0.005 INCHES DEEP. REPAIRED IAW EA CRJ253-02947.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,489 hrs · 19,776 cycles

DURING ROUTINE CHECK FOUND SEVERAL EXTERIOR & INTERIOR EMER LIGHTS OUT. R & R NR 1 & NR 4 EMER BATTERY PACKS IAW AMM 33-51-04. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 22,309 hrs · 19,586 cycles

BULKHEAD EMERGENCY LIGHT LENS CRACKED. R & R LENS IAW CMM 33-21-38.

Part: SMOKE GOGGLES — INOPERATIVE (COCKPIT) · airframe 22,281 hrs · 19,560 cycles

OBSERVERS SMOKE GOGGLES INOPERATIVE. R & R OBSERVERS GOGGLES IAW AMM 25-61-00. MM02 UPDATED & PLACARD REMOVED.

Part: SMOKE GOGGLES — DEFECTIVE (COCKPIT) · airframe 22,281 hrs · 19,560 cycles

CAPTAINS SMOKE GOGGLES ELASTIC ADJUSTABLE STRAP WORN OUT. SWAPPED OBSERVERS WITH CAPTAINS SEAT SMOKE GOGGLES. DEFER OBSERVERS IAW MEL 25-12-11 IAW MOC JD, ADDED TO MEL LOGBOOK, PLACARD INSTALLED.

Part: PBE — DAMAGED (COCKPIT) · airframe 22,243 hrs · 19,522 cycles

TWO PBE'S DAMAGED. R & R COCKPIT PBE & GALLEY CLOSET PBE IAW AMM 35-30-00.

Part: PBE — DAMAGED (CABIN) · airframe 20,541 hrs · 17,859 cycles

CREW REPORTS DAMAGE PBE. R & R PBE IAW AMM 25-61-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 20,487 hrs · 17,801 cycles

FLIGHT SPOILER FAULT STATUS MESSAGE READ-441, COMPLIED WITH READ-441. SPOILER FAULT STATUS MESSAGE IAW FIM 27-60-00. NO SPOILER FAULT STATUS MESSAGE INDICATED AT THIS TIME. OK FOR SERVICE.

Part: VALVE — MALFUNCTIONED (NLG) · airframe 20,341 hrs · 17,649 cycles

NOSE GEAR DISAGREE MASTER WARNING, RIGHT AFTER TAKEOFF, QRH FOLLOWED, ALL GEAR DOORS DOWN AND LOCKED R & R NLG SELECTOR VALVE IAW AMM 32-33-10, ALSO R & R NLG PRIORITY VALVE IAW AMM 32-333-15. PERF EXT & RETRACTION CHECK IAW AMM 32-30-00, ALL CHECKS GOOD, SEE NON ROUTINE CARD S53789 FOR DETAILS. C/W PA 05-018J, SCENARIO NR 1, NO FURTHER MX ACTIONS REQUIRED. COMPLETED HYD PORTION CHECKS OF PA, SERVICED NOSE STRUT IAW AMM 12-12-32-610-803, ALL OPS CHECKS GOOD, ACFT OK FOR SERVICE.

Part: SECU — FAULTY (SPOILER) · airframe 19,905 hrs · 17,225 cycles

UNCOMMANDED LEFT FLIGHT SPOILER RETRACTION IN FLIGHT WITH SPOILERS EXTENDED IN DESCENT. LEFT SPOILER RETRACTED, DEPLOYED AND RETRACTED RAPIDLY (3 TIMES) IN 2 SECONDS - ROLLING THE AIRCRAFT VIOLENTLY 10/30/ APPROXIMATELY 40 DEGREES TO RIGHT. FLIGHT SPOILER CAUTION THEN DISPLAYED. REMOVED AND REPLACED NR 1 SECU IAW AMM 27-61-05, OPERATIONS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,803 hrs · 17,126 cycles

EMERGENCY FLOOR FLOOD LIGHT AT SERVICE DOOR HAS 2 BULBS OUT, 3 REMAIN. REMOVED AND REPLACED BULBS FOR CABIN EMERGENCY LIGHT IAW AMM 33-51-12. OPS CHECK GOOD. THIS CLEARS DM, PLACARD REMOVED.

Part: COALESCER BAG — ODOR (AC BAY) · airframe 19,572 hrs · 16,897 cycles

ON FLIGHT 3864 (AZO TO DTW) PASSENGER'S NOTICE A SMELL OF BURNING PLASTIC AROUND ROW 5, EN ROUTE. FLIGHT ATTENDENT CONFIRMS THE SMELL. AIRCRAFT CONTINUED AND LANDED IN DTW. REMOVED AND REPLACED LEFT AND RIGHT COALESCER BAGS IAW AMM 21-51-13. OK FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,544 hrs · 16,867 cycles

FS 559 SEMI-PRESSURE BULKHEAD CRACKED. REPAIRED IAW PA 53-025 AND BOMBARDIER REOS 601R-53-41-260 AND 601R-53-41-609.

Part: BATTERY PACK — DISCONNECTED (FLASHLIGHT) · airframe 19,149 hrs · 16,474 cycles

F/A FLASHLIGHT INOP. CONNECTED BATTERY PACK & OPS CHECKED IAW CRJ200AMM 25-61-04. OPS CHECKS GOOD, OK FOR SERVICE. THIS CLEARS DM 72601, PLACARD REMOVED.

Part: CONTAINER — TORN (LIFE VEST) · airframe 20,265 hrs · 17,699 cycles

CAPTAIN AND FIRST OFFICER’S LIFE VEST BAGS TORN. REMOVED AND REPLACED CAPTAIN AND FIRST OFFICER’S LIFE VEST IAW AMM 25-61-03.

Part: BPSU — OUT OF TOLERANCE (TE FLAP) · airframe 18,290 hrs · 15,604 cycles

FLAPS FAIL AT 20. PLACARD INSTALLED. PERFORMED T/S PER BOMB FIM REV 39. IAW AD 2009-06-12 TP (H) (6) (I), AMOC DATED MARCH 27, 2009 TR # 27-012 PER AMOC DATED DEC 18,2009 & PPAD 27-052G. PERFORMED MEG CHECK OF RT BPSU WIRE HARNESS & RT BPS INTERNAL WIRING PER FIM 27-50-00. FOUND LT & RT BPSU OUT OF TOLERANCE. RIGGED BOTH BPSU IAW AMM 27-51-10. OPS CHECK GOOD @ THIS TIME DM# X62946 CLOSED PLACARD REMOVED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,070 hrs · 15,381 cycles

RIGHT SIDE SEAT TRACK RAIL HAS EVIDENCE OF CORROSION. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,070 hrs · 15,381 cycles

LEFT SEAT RAIL HAS CORROSION. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,070 hrs · 15,381 cycles

LEFT SIDE SEAT RAIL CORRODED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,070 hrs · 15,381 cycles

LEFT SIDE SEAT RAIL HAS CORROSION. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,070 hrs · 15,381 cycles

LEFT SIDE SEAT RAIL HAS CORROSION. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,070 hrs · 15,383 cycles

LEFT SIDE SEAT RAIL HAS EVIDENCE OF CORROSION. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,070 hrs · 15,381 cycles

RIGHT SEAT TRACK HAS EVIDENCE OF CORROSION. REPAIRED IAW AMM 53-01-11.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 17,660 hrs · 15,024 cycles

FUEL IMBALANCE WOULD NOT TRANSFER APP 1300 LBS. OPC FUEL CROSSFLOW IAW AMM 28-13-45. OPC NORMAL. OPC GRAVITY FLOW IAW AMM 28-13-16. OPC NORMAL. A/C OK FOR SERVICE.

Part: PRIORITY VALVE — INOPERATIVE (NLG) · airframe 15,814 hrs · 13,273 cycles

NOSE DOOR OPEN AND GEAR DISAGREE WARNING WHEN GEAR WAS RETRACTED AFTER DEPARTURE PERFORMED QRH (AIR RETURN). C/W PA05-018A BY R/R NLG PRIORITY VALVE RECORDING CODES AND PERFORMING NLG AND MLG SWINGING, SEE CORRECTIVE ACTION AML 600469 BLOCK NR 1, A/C OK FOR SERVICE.

Part: A/C PACK — CONTAMINATED (LEFT) · airframe 15,826 hrs · 13,257 cycles

THE "AIR RETURN FOR SMOKE IN COCKPIT" FOUND TO BE DEICE FLUID CONTAMINATING THE LT PACK AFTER DEICING, DEFERRED PER MEL 21-51-11.

Part: SKIN PANEL — CRACKED (ELEVATOR) · airframe 15,214 hrs · 12,655 cycles

LIGHTNING STRIKE BURNED RIVET IN UPPER SKIN PANEL AT ES 29.27, 3.5 INCHES FROM ELEVATOR AFT EDGE AND 16.0 INCHES FROM INBOARD EDGE. INSPECTION REVEALED CRACKING IN THE SKIN FROM THE RIVER AFT 0.30 INCHES LONG. REMOVED AND REPLACED ELEVATOR.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 15,159 hrs · 12,602 cycles

NOSE GEAR DISAGREE. DEFERED PER MEL 32-30-01.

Part: RAMP — CORRODED (GALLEY) · corrosion level 2 · airframe 15,094 hrs · 12,550 cycles

SERVICE DOOR GALLEY CART RAMP CORROSION FOUND. REMOVED AND REPLACED SERVICE DOOR GALLEY CART RAMP.

Part: OIL SYSTEM — LEAKING (APU) · airframe 13,307 hrs · 10,877 cycles

FLIGHT CREW RECEIVED AN LAV SMOKE WARNING AFTER THE BLEED AIR SYSTEM WAS TRANSFERRED TO THE APU. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE DETERMINED THAT THE APU WAS LEAKING OIL. THE APU WAS REPLACED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OIL SYSTEM — LEAKING (APU) · airframe 13,302 hrs · 10,875 cycles

FLIGHT 4377 BNA/MEM - AT THE GATE WHEN BLEEDS WHERE TURNED ON CREW RECEIVED "LAV SMOKE" WARNING WITH VISIBLE SMOKE IN THE LAV AREA. MAINTENANCE INSPECTED AND FOUND THE APU TO BE LEAKING OIL CAUSING THE SMOKE. APU WAS DEFERRED PER MEL 49-10-11.

Part: FITTING — DAMAGED (ELEVATOR) · airframe 8,405 hrs · 6,768 cycles

LEFT ELEVATOR NR 3 PCU FITTING -LINK ATTACHMENT, LOWER LOCK FASTENER IS SHEARED. REPLACED THE HI-LITE TO LINK ASSY.