N835AY

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,555 hrs · 24,779 cycles

FWD MOST EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND INSTALLED THE EPSU BATTERY PACK PS1LF IAW JOB CARD 33-900-701. PERFORMED OPS CHECK. OPS CHECK GOOD. PN OFF: 2013-1A SN OFF: 103895 PN ON: 2013-1ASMI SN ON: 8724.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 22,875 hrs · 23,005 cycles

RH FLOOR SILL CORRODED FS 559+96. REMOVED AND REPLACED FLOOR SILL

Part: PLATE — CRACKED (CARGO DOOR) · airframe 22,875 hrs · 23,005 cycles

CARGO DOOR KICKPLATE CRACKED. NEW KICK PLATE LOCATED AND DRILLED I.A.W. CRJ-200 SRM 51-40-11 TR 51-42. REFER TO AAR WORK ORDER 1017193-2000-0085 S/N 7119114 FOR INSTALLATION.

Part: ANGLE — CRACKED (BS 559) · airframe 22,875 hrs · 23,005 cycles

FS 559 LNL 19 AND RBL 18 CRACKED AT LOWER CAP ANGLE. REPAIRED AND MODIFIED IAW EO P53025

Part: SKIN — GOUGED (FUSELAGE) · airframe 22,875 hrs · 23,005 cycles

445AB OUTER SKIN GOUGED AT LATTCHES. REMOVED GOUGED DOUBLER AND REPLACED WITH NEW FABRICATED DOUBLER I.A.W. CRJ-200 CMM 71-12-01.

Part: ANGLE — CORRODED (BS 409) · airframe 22,875 hrs · 23,005 cycles

FUSELAGE , FORWARD WING TO BODY FAIRING MOUNT ANGLE CORRODED RHS. REMOVED AND REPLACED FAIRING MOUNT ANGLE ON FUSELAGE AT FWD WING TO BODY IAW CRJ 200 SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 610-621) · airframe 22,875 hrs · 23,005 cycles

LBL 27 I/B AND O/B FLOOR PANEL LANDINGS HAVE CORROSION SPOTS BETWEEN FS 610 THRU FS 621, IN THE CARGO BAY. REPAIRED LBL 27 INBOARD AND OUTBOARD FLOOR PANEL LANDINGS IAW ENDEAVOR E.A NO# CRJ 253-09044 AAR SM 107

Part: STRINGER — CORRODED (BS 310-319) · airframe 22,875 hrs · 23,005 cycles

STGR 23R HAS CORROSION BETWEEN FRAMES 319.70 AND 310, IN THE FWD E & E BAY. REPAIRED IAW EA CRJ 253-08988 REV IR AAR SM 107

Part: FRAME — CRACKED (BS 333) · airframe 22,875 hrs · 23,005 cycles

FRAME FS333.0 CRACKED AT TOOLING HOLE AT LBL 5.0 ABOVE PAX DOOR. REPAIRED FRAME 333 IAW EA CRJ 253-08930 AAR R SM 4

Part: STRAP — CORRODED (BS 621-) · airframe 22,875 hrs · 23,005 cycles

FLOOR PANEL LANDING ANGLE STRIP HAS CORROSION SPOTS AT FS 621 BETWEEN LBL 27 AND THE LH FLOOR SILL, IN THE CARGO BAY. REMOVED DAMAGE IAW CRJ 200 REO 601R-53-61-117 AAR SM 58

Part: INTERCOSTAL — CORRODED (BS 310-319) · airframe 22,875 hrs · 23,005 cycles

INTERCOSTAL ON TOP OF STGR 20R HAS CORROSION BETWEEN FRAMES 310 AND 319.70, IN THE FWD E & E BAY. REMOVED AND REPLACED INTEROCASTAL ATTACHED TO STRINGER 20R IAW CRJ 200 SRM 51-42-06 AAR SM 84

Part: ANGLE — CRACKED (BS 473.15) · airframe 22,875 hrs · 23,005 cycles

ANGLE AT STA. 473.15 LH FUSELAGE SUPPORT BEAM ABOVE CTR WING IS CRACKED. REPLACED ANGLE @ STA 473.15 L/H FUSELAGE ABOVE CTR WING IAW CRJ 200 SRM 51-42-06 AND 51-42-21 AAR SM 33

Part: ANGLE — CRACKED (BS 449) · airframe 22,875 hrs · 23,005 cycles

ANGLE AT STA. 449.85 RH FUSELAGE SUPPORT BEAM ABOVE CTR WING IS CRACKED REPLACED ANGLE @ STA 449.85 R/H FUSELAGE ABOVE CTR WING IAW CRJ 200 SRM 51-42-06 AAR SM 33

Part: ANGLE — CRACKED (BS 449) · airframe 22,875 hrs · 23,005 cycles

ANGLE AT STA. 449.85 LH FUSELAGE SUPPORT BEAM ABOVE CTR WING IS CRACKED REPLACED ANGLE @ STA 449.85 L/H FUSELAGE ABOVE CTR WING IAW CRJ 200 SRM 51-42-06 AAR SM 33

Part: ANGLE — CRACKED (BS 461) · airframe 22,875 hrs · 23,005 cycles

ANGLE AT STA. 461.00 RH FUSELAGE SUPPORT BEAM ABOVE CTR WING IS CRACKED. ANGLE @ STA 461.00 R/H FUSELAGE ABOVE CTR WING WAS REPLACED IAW CRJ 200 SRM 51-42-06 AAR SM 33

Part: ANGLE — CRACKED (BS 473) · airframe 22,875 hrs · 23,005 cycles

ANGLE AT STA.473.15 RH FUSELAGE SUPPORT BEAM ABOVE CTR WING IS CRACKED REPLACED ANGLE @ STA 473.15 R/H FUSELAGE ABOVE CTR WING IAW CRJ 200 SRM 51-42-06 51-42-21 AAR SM 107

Part: FLOOR SUPPORT — CORRODED (BS 574-610) · airframe 22,875 hrs · 23,005 cycles

LBL 27 I/B AND O/B FLOOR PANEL LANDINGS HAS CORROSION SPOTS BETWEEN FS 574 THRU FS 610, IN THE CARGO BAY. REMOVED AND REPLACED LBL 27 I/B AND OUTBOARD FLOOR PANEL LANDINGS AND BEAM CAP BETWEEN F.S. 574 AND 610 IN THE CARGO BAY I.A.W. CRJ-200 SRM 51-42-21 AAR SM 107

Part: SUPPORT — CRACKED (CARGO DOOR TRACK) · airframe 22,875 hrs · 23,005 cycles

CARGO DOOR FWD TRACK, LOWER SUPPORT IS CRACKED AND BENT. REMOVED AND REPLACED LOWER SUPPORT IAW SRM 51-42-06 ON FWD CARGO DOOR TRACK.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 22,875 hrs · 23,005 cycles

STRINGER 3L ATTACH ANGLE CRACKED AT FS 280. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-21 AND 51-42-06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,875 hrs · 23,005 cycles

LAST AFT EMERGENCY CEILING FLOOD LIGHT INOP. REMOVED/REPLACED AFT EMERGENCY CEILING FLOOD LIGHT IAW CRJ 200 AMM 33-51-16 OPS TEST ACCOMPLISHED ON W/O 1017193 2000 0017 SN7119046 AAR R RE 13

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 22,875 hrs · 23,005 cycles

SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REMOVED AND REPLACED I.A.W. CRJ-200 AMM 53-00-49 AAR SM 58

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 22,875 hrs · 23,005 cycles

SEAT TRACK ON TOP OF RBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REMOVED AND REPLACED IAW CRJ 200 AMM 53-00-49 AAR SM 58

Part: ATTACH BRACKET — CRACKED · airframe 22,875 hrs · 23,005 cycles

ATTACH BRACKET FOR L/E PANEL 630AL IS CRACKED REMOVED AND REPLACED BRACKETS IAW CRJ 200 SRM 51-41-02. AAR SM 58

Part: RUB STRIP — WORN (NACELLE) · airframe 22,875 hrs · 23,005 cycles

RUB STRIP WORN IN SEVERAL AREAS. REMOVED AND REPLACED THE RUB STRIP ON ACCESS COWL 432AB IAW CMM 71-14-01 AAR SM 58

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,166 hrs · 22,259 cycles

EMERGENCY LIGHTS WON'T ILLUMINATE. R/R EMERGENCY BATTERY PACKS IAW AMM 33-51-04.OPS CHK'D EMERGENCY LIGHTS GOOD.NO DEFECTS NOTED.

Part: OXYGEN MASK — LEAKING (FIRST OFFICER'S) · airframe 21,655 hrs · 21,722 cycles

FIRST OFFICER`S MASK LEAKED AND DOES NOT SEAL ON THE FACE. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12. PERFORMED AN OPS TEST IAW 35-10-00-710-801. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: APU — UNKNOWN · airframe 21,410 hrs · 21,453 cycles

APU HAD AN UNCOMMANDED SHUTDOWN ON THE GROUND & DURING FLIGHT. NO ASSOCIATED CAUTIONS OR WARNING MESSAGES. VIBRATION FELT AT AROUND 90% RPM DURING START OF APU, JET FUEL ODOR IN THE COCKPIT AFTER SHUTDOWN DURING FLIGHT. OPS CHECKED THE APU WAS SATISFACTORY IAW AMM 49-10-00. NO FURTHER DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 21,095 hrs · 21,090 cycles

PILOT`S FLASHLIGHT, RED FLASHING LED INOPERATIVE. REMOVED AND REPLACED THE BATTERY IAW CMM 25-60-02.

Part: FLOOR SUPPORT — CORRODED · airframe 18,968 hrs · 18,792 cycles

FLOOR SUPPORT AT PAX DOOR THRESHOLD CORRODED. REMOVED IAW SRM 51-42-06, 51-42-21, 51-42-13. FABRICATED A REPLACEMENT IAW SRM 51-24-21, 51-24-36, 51-40-11. INSTALLED IAW SRM 51-42-06, 51-42-21, 51-42-13 OPS CHECKED.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 18,968 hrs · 18,792 cycles

INTERCOSTAL AT BS 621 AND STRINGER 16L IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-22 & 51-42-21.

Part: MOUNT — GOUGED (APU BAY) · airframe 18,968 hrs · 18,792 cycles

AFT ACCY COMPARTMENT, LEFT SIDE AFT APU ENCLOSURE MOUNT AROUND FASTENER HOLE AREA IS GOUGED. REMOVED AND REPLACED IAW SRM 51-42-06.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 18,968 hrs · 18,792 cycles

INTERCOSTAL AT BS 621 AND STRINGER 14L IS CRACKED. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 18,968 hrs · 18,792 cycles

INTERCOSTAL AT BS 621 AND STRINGER 15L IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.

Part: ANGLE — CRACKED (BS 621) · airframe 18,968 hrs · 18,792 cycles

ANGLE AT BS 621 AND STRINGER 14L IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 18,968 hrs · 18,792 cycles

INTERCOSTAL AT BS 621 AND STRINGER 13L IS CRACKED. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 18,968 hrs · 18,792 cycles

RT INBD LEADING EDGE OF WING, SUPPORT BRACKET AFT OF SPAR CAP IS CRACKED AT LOWER AFT CORNER. REMOVED AND REPLACED IAW CRJ 200 SRM 51-41-02, 51-42-06, AND 51-40-11.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 18,968 hrs · 18,792 cycles

AFT CARGO TRACK IS CORRODED AND GOUGED BS 559+80 - 559+96, RBL 27. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49.

Part: ATTACH ANGLE — CRACKED (BS 473) · airframe 18,968 hrs · 18,792 cycles

ATTACH ANGLE CRACKED AT BS 473 LBL 36. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-21.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 18,968 hrs · 18,792 cycles

AFT CARGO TRACK IS CORRODED AND GOUGED BS 559+80 - 559+96, RBL 9. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49 RBL-9.

Part: STRUCTURE — CRACKED (APU BAY) · airframe 18,968 hrs · 18,792 cycles

APU ENCLOSURE AFT SIDE AREAS ARE CRACKED. REPAIRED IAW REO 601R-49-11-070 REV B. REPAIREDTHE REMAINING AREAS IAW REO 601R-49-11-071.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 18,968 hrs · 18,792 cycles

MAIN CABIN SEAT TRACK IS CORRODED AND GOUGED LBL 93, BS 409+126 - 559. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409-444) · airframe 18,968 hrs · 18,792 cycles

RIGHT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED, BS 409+111 - 444. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 18,968 hrs · 18,792 cycles

LEFT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED, BS 409+112 - 449+85. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED · airframe 18,968 hrs · 18,792 cycles

LEFT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED · airframe 18,968 hrs · 18,792 cycles

LEFT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 18,968 hrs · 18,792 cycles

RIGHT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,968 hrs · 18,792 cycles

FLOORBEAM BS 280 ANGLE CRACKED LBL 9. REMOVED THE ANGLE. FABRICATED, AND INSTALLED A NEW ANGLE IAW SRM 51-24-21 AND 51-42-21.

Part: CARGO TRACK — CORRODED (BS 554-559) · airframe 18,968 hrs · 18,792 cycles

RIGHT SIDEWALL CARGO TRACK IS CORRODED AND GOUGED, BS 554 - 559+79 RBL 27. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 18,968 hrs · 18,792 cycles

MAIN CABIN SEAT TRACK IS CORRODED AND GOUGED RBL 9, BS 559 - 559+85. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 18,968 hrs · 18,792 cycles

LEFT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED, BS 364 - 409+18. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11 AND REO 601R-53-00-055 REV B.

Part: SEAT TRACK — CORRODED (BS 364-405) · airframe 18,968 hrs · 18,792 cycles

SEAT TRACK RBL 9, BS 364 - 405 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: ATTACH ANGLE — CRACKED (BS 202) · airframe 18,968 hrs · 18,792 cycles

INTERCOSTAL ATTACH ANGLE AT BS 202 IN NLG WHEEL WELL CRACKED. FABRICATED NEW ATTACH ANGLE IAW SRM 51-24-16 AND INSTALLED IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 554-559) · airframe 18,968 hrs · 18,792 cycles

LEFT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED, BS 554 - 559+79. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED · airframe 18,968 hrs · 18,792 cycles

MAIN CABIN SEAT TRACK IS CORRODED AND GOUGED RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 18,968 hrs · 18,792 cycles

RIGHT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED, BS 449+85 - 499. INSTALLED A NEW SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 405-409) · airframe 18,968 hrs · 18,792 cycles

IN MAIN CABIN, A SEAT TRACK IS CORRODED AND GOUGED LBL 9, BS 405 - 409+128. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 364-405) · airframe 18,968 hrs · 18,792 cycles

SEAT TRACK LBL 9, BS 364 - 405 CORRODED, REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 18,968 hrs · 18,792 cycles

LEFT SIDE SEAT TRACK GOUGED, BS 559 - 559+85. REMOVED & REPLACED THESEAT TRACK IAW AMM 53-01-11. AAR S/M-109.

Part: SEAT TRACK — CORRODED (BS 405-409) · airframe 18,968 hrs · 18,792 cycles

MAIN CABIN SEAT TRACK IS CORRODED AND GOUGED RBL 9, BS 405 - 409+128. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 18,968 hrs · 18,792 cycles

LEFT SIDEWALL SEAT TRACK IS CORRODED AND GOUGED, BS 364 - 409+18. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,501 hrs · 18,337 cycles

AFT CEILING EMERGENCY FLOODLIGHT INOP. REPLACED AFT CEILING EMERGENCY FLOODLIGHT LAMP P/N 1317 PER AMM 33-51-16, OPS CHECK GOOD PER AMM 33-51-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,322 hrs · 18,165 cycles

RIGHT EXTERIOR AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND INSTALLED SERVICEABLE EMERGENCY LIGHT IAW AMM 33-50-01

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 18,212 hrs · 18,056 cycles

CAPTAIN`S FLASHLIGHT NOT BLINKING, INOPERATIVE WHEN PULLED. R & R THE BATTERY PACK IAW AMM 25-61-00. OPS CHECKED GOOD, RESTOWED AND SECURED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,373 hrs · 17,195 cycles

FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. DEFERRED FLIGHT ATTENDANT FLASHLIGHT IAW MEL 25-61-04. PLACARD INSTALLED, MMO2 UPDATED & CAT C. R & R FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW AMM 25-61-00. OPERATIONS CHECKED GOOD. THIS CLEARS MEL 3262409-1 & PLACARD REMOVED.

Part: CONNECTOR — DIRTY (BLEED AIR SYS) · airframe 17,311 hrs · 17,136 cycles

EMERGENCY WAS DECLARED & FLIGHT DIVERTED. DURING CLIMB OUT, A RT 14TH DUCT WARNING MSG WAS OBTAINED. IAW QRH, RT 14TH DUCT WAS CLOSED, BUT MSG STAYED ON. ENG BROUGHT TO IDLE, MSG STAYED ON. DURING MEL PROCESS, FOUND RT 14TH DUCT WARNING WOULD NOT EXTINGUISHED. IAW FIM, CLEANED CONNECTORS & SWAPPED BLCU FROM 1 TO 2, MSG CLEARED. SWAPPED BLCU BACK. OPERATIONS CHECK OF BLEED LEAK IAW AMM 36-21-10. OPERATIONS CHECKED GOOD, NO DEFECT NOTED.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 16,453 hrs · 16,249 cycles

FLAPS FAIL AT 0 DEGREES WHEN SELECTED ON APPROACH. R & R FECU IAW AMM 27-51-05. OPERATIONS CHECKED OK. R & R LT MOST OTBD FLEX SHAFT IAW AMM 27-53-10. OPERATIONS CHECKED OK. R & R LT BPSU IAW AMM 27-51-10. ALL CHECKED OK. PERFORMED DETAILED INSPECTION OF ALL LT FLEX SHAFTS IAW AMM 27-53-10. NO DAMAGE NOTED. SEE AML 3111014 FOR FURTHER DETAILS.

Part: SKIN — DENTED (FUSELAGE) · airframe 16,400 hrs · 16,199 cycles

MAINTENANCE WAS TASKED WITH PERMANENT REPAIR OF MULTIPLE DENTS IN THE AFT FUSELAGE SKIN BETWEEN FS 755.00 & 67.50% & BETWEEN STRINGERS S23L & 24R. THE DAMAGES MEASURE A MAXIMUM OF 4.00” DIA X .050” DEEP. REPAIRED IAW EA CRJ253-03514.

Part: RELAY — STUCK (AIRSTAIRS) · airframe 16,317 hrs · 16,113 cycles

PAX AIRSTAIR RETRACTED ON ITS OWN AFTER FULLY EXTENDED, CLOSED DOOR FULLY RE-OPENED DOOR STAYED DOWN. THEN AS JETWAY WAS BROUGHT TO ACFT, THE DOOR RETRACTED ON ITS SHUTDOWN ACFT, ACFT EXT POWER AIRSTAIR DOOR STAYED DOWN. AIRSTAIR MAY HAVE CONTACTED JETWAY. PAX DOOR POWER ASSIST MOTOR RUNNING CONTINUOUSLY UNCOMANDED, IN LIFT POSITION. DEFERRED PAX DOOR ASSIST SYS IAW MEL 52-11-01. ALL DDG PROCEDURES COMPLIED WITH. PLACARDS INSTALLED & MM02 UPDATED. TROUBLE SHOT & FOUND DOOR ASSIST RELAY, K1MB, STUCK CLOSED. R & R RELAY K1MB IAW ESPM 20-22-00. PAX DOOR ASSIST OPERATIONS CHECKED GOOD IAW AMM 52-11-08. THIS CLEARS DM 001497. PLACARD REMOVED & MMO2 CLEARED.

Part: OXYGEN MASK — OUT OF POSITION (COCKPIT) · airframe 16,041 hrs · 15,800 cycles

FOUND OBSERVER O2 MASK BOX IN THE IMPROPER ORIENTATION. PERFORMED RE ORIENTATION OF OBSERVER'S O2 MASK STORAGE BOX IAW AMM 35-11-15-400-801. ALL CHECKED GOOD.

Part: STRAP — DISCONNECTED (FLASHLIGHT) · airframe 15,945 hrs · 15,704 cycles

FLASHLIGHT SEAL STRAP ON FIRST OFFICER`S SIDE IS DISCONNECTED. R & R FIRST OFFICER`S EMER FLASHLIGHT TORCH SHIELD IAW AMM 25-61-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 15,912 hrs · 15,673 cycles

DURING INSPECTION MX FOUND MULTIPLE DENTS TO THE FUSELAGE SKIN BETWEEN FS 169.00 & FS 193.00 ABOVE STRINGER 23R. THE DENTS MEASURE AS FOLLOWS. A. .200” X .100” X .002” DEEP. B. .500” X .300” X .010” DEEP. C. .250” X .100” X .002” DEEP. D. .300” X .200” X .005” DEEP. E. .150” X .100” X .001” DEEP. REPAIRED IAW 253-03196.

Part: SKIN — DENTED (FUSELAGE) · airframe 15,912 hrs · 15,673 cycles

FUSELAGE SKIN DENTED AT FS 620 AT THE CARGO DOOR LOWER CORNER AT STRINGER 17L. REPAIRED IAW REO 601R-53-00-34.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 15,912 hrs · 15,673 cycles

FS 202.75 AT BRAKE CABLE PASS THROUGH CRACKED. REPAIRED IAW REO 601R-53-11-563.

Part: CLAMP — DISPLACED (HEAT EXCHANGER) · airframe 15,908 hrs · 15,669 cycles

DURING TROUBLESHOOTING FOUND DISPLACED HEAT EXCHANGER CLAMP, DUCT ON LT AIR CONDITIONING PACK. CREW RECEIVED A CARGO OVERHEAT MESSAGE, FIRE BOTTLE BLEW, CA CALLED OUT THE EMERGENCY SERVICES. CUSTOMERS DEPLANED- NO ISSUES. RESECURED, REPLACED, HEAT EXCHANGER DUCT CLAMP IAW AMM 21-51-10. OP CHECKS AND LEAK CHECKS GOOD. OK FOR SERVICE.

Part: SIGN — MISSING (CABIN) · airframe 15,801 hrs · 15,548 cycles

EMERGENCY EXIT SIGN IS MISSING AT MAIN CABIN DOOR. R & R EMER EXIT FLOOD LIGHT AT PAX DOOR IAW AMM 33-51-19. OPERATIONS CHECKED GOOD. PN ON & OFF BR 9279-232 PART NOT SERIALIZED.

Part: PISTON — DAMAGED (NLG) · airframe 15,416 hrs · 15,171 cycles

GEAR DISAGREE UP & NOSE DOOR WARNINGS AFTER TAKEOFF. NOSE GEAR DOWN, MAIN GEARS UP TIME INTERVAL 6 SEC. GEAR LEVER WAS NOT MOVED WITHIN 30 SECONDS OF THE ORIGINAL SELECTION, MANUAL OPERATING SYS WAS NOT MOVED. LANDED AT 47,000 & MINIMAL DESCENT RATE. R & R NLG SLIDING PISTON & AXLE ASSEMBLY IAW AMM 32-21-30, DUE TO DAMAGE TO PISTON. PERFORMED EXTENSION & RETRACTION CHECK IAW AMM 32-30-00. GEAR SWINGS SATISFACTORY REFERENCE NRWC N62201 FOR MAINTENANCE DETAILS.

Part: PISTON — INOPERATIVE (NLG) · airframe 15,390 hrs · 15,145 cycles

PILOT REPORTS A GEAR DISAGREE MSG AFTER TAKEOFF FOLLOWED WITH A NOSE DOOR WARNING. HE STATED THAT THE NLG TOOK 3 -4 MINUTES TO COME UP & THE MSGS WENT AWAY. ACFT LANDED WITH NO INCIDENT. NO EMER WAS DECLARED. GEAR DISAGREE UP & NOSE DOOR WARNING AFTER TAKEOFF. NOSE GEAR DOWN & MAIN GEAR UP. TIME INTERVAL WAS 6 SECONDS. GEAR LEVER WAS NOT MOVED WITHIN 30 SECONDS OF ORIGINAL SELECTIONS. MANUAL OPERATING SYS WAS NOT MOVED. LANDED AT 47000 POUNDS AND THEY LANDED AT MINIMAL DESCENT RATE. REPAIRED & REPLACED SLIDING PISTON MEMBER IAW AMM 32-21-30. ALL CHECKED GOOD AT THIS TIME.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LANDING GEAR) · airframe 15,389 hrs · 15,144 cycles

NOSE DOOR OPEN MASTER WARNING IN CRUISE 6000 FT 250 KNTS. FOLLOWED QRH GEAR DOWN 3 GREEN WITH NO FURTHER MSG. RECEIVED A GEAR DISAGREE FOR JUST A FEW SECONDS AFTER RETRACTION THAT CLEARED WITHIN 3 - 5 SHOWING THE NOSE GEAR RED BUT IT CLEARED WITH NO REMAINING. FOUND PROX SENSORS PS18GA + PS19GA OUT OF LIMITS ADJUSTED IAW AMM 32-61-05. PERFORMED FUNCTIONAL TEST OF LG EXT & RETRACTION. ALL PUMPS UP 13 SEC, DWN 12 SEC, 3A UP 16 SEC, DWN 16 SEC, 3B 18 SEC & DWN 18 SEC. OPERATIONS CHECKED GOOD IAW 32-30-00. IAW FIM NO LEAKS FOUND FOR NOSE GEAR AREA IAW AMM 32-00-00. OK FOR SERVICE. SEE CONTINUATION CARDS N63638 + N61501.

Part: BRACKET — BENT (NLG) · airframe 15,059 hrs · 14,817 cycles

WITH SELECTION OF LG LEVER TO UP POSITION MASTER WARNING LIGHT ILLUMINATED. GEAR DISAGREE & NOSE DOOR OPEN MSG APPEARED ON EICAS. RAN QRH PROCEDURE, PUT GEAR HANDLE DOWN. BOTH MAIN GEARS EXTENDED NORMALLY & LANDING ACCOMPLISHED NORMALLY. FOUND NLG OLEO CENTERED & EXTENDED PROX SWITCH BRACKET BENT. R & R NLG OLEO CTR EXTENDED PROX SWITCH BRACKET IAW CMM 32-20-04. ADJUSTED PROX SWITCH PS14GA IAW AMM 32-61-05. PERFORMED OPERATIONS CHECK OF GEAR EXTENSION IAW AMM 32-30-00. OPERATIONS CHECKED GOOD COMPLIED WITH PA 05-018 REV K SCENARIO 1.

Part: FIRST AID KIT — UNSERVICEABLE (CABIN) · airframe 14,920 hrs · 14,675 cycles

BROKEN SEAL ON MED KIT. R & R FIRST AID KIT IAW AMM 25-61-06. OFF PN 70004-00, SN 0265, ON PN 70004-00 & SN MEM050109-2.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 13,614 hrs · 13,373 cycles

WHILE HAND FLYING AND GOING FLAPS 30 TO 45, EXPERIENCED AN AGRESSIVE ROLL TO THE LEFT. COUNTERED IT WITH CONTROL INPUTS UNTIL AILERON TRIM IN. ROLL GREAT ENOUGH TO BANK ACFT 35 DEG -40 DEG LT WING DOWN. PERFORMED ABBREVIATED "ROLL WITH FLAPS DEPLOYED" WORKSCOPE IAW ENGINEERING, INCLUDING A DVI OF FLAPS, VANES AND SYMETRY. DVI FOR DIRT, GRIT, GRIME, GREASE AND DAMAGE AND PAINT FLAKING AND SEALANT. NO SIGNIFICANT FINDINGS NOTED. PERFORMED FLAP SYSTEM EXTEND/RETRACT TEST IAW 27-53-00. FLAPS EXTENDED AND RETRACTED SMOOTHLY AND EVENLY. ACFT OK FOR SERVICE.

Part: BEAM — CRACKED (FUSELAGE) · airframe 12,837 hrs · 12,580 cycles

OUTBOARD SIDE OF VERTICAL BEAM AT FS 409+128 AND RBL 18 IS CRACKED NEAR BOTTOM OF THE POST. REPAIRED IAW BOMBARDIER REO 601R-53-41-1672.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,837 hrs · 12,580 cycles

CABIN FLOOR SUPPORT STRUCTURE IS CRACKED WHERE IS ATTACHES TO THE FS 280 BULKHEAD OUTBOARD OF RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136 AND 601R-53-11-171.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 12,837 hrs · 12,580 cycles

FS 621 BULKHEAD FORWARD FACE HAS CHAFE DAMAGE ON SKIN AT MULITPLE LOCATIONS BETWEEN LBL 18 AND RBL 33. REPAIRED IAW BOMBARDIER REO 601R-53-61-4857.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,837 hrs · 12,580 cycles

CABIN FLOOR SUPPORT STRUCTURE IS CRACKED WHERE IT ATTACHES TO THE FS 280 BULKHEAD OUTBOARD OF LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 12,837 hrs · 12,580 cycles

RIGHT WING PLUG SPAR EXTENSION HAS 2 DRILL STARTS OUTBOARD OF WS 353 3 STRINGER FWD OF REAR SPAR LOWER SIDE, 0.159" DIAMETER AND 0.012" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-1892.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,837 hrs · 12,580 cycles

BOTH CLIPS AT FS 484, LBL 27 AND LBL 36 ARE CRACKED. REPAIRED IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,838 hrs · 12,580 cycles

OUTBOARD CLIP AT FS 484 AND RBL 36 IS CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-41-059.

Part: BRACKET — DAMAGED (NLG) · airframe 12,834 hrs · 12,576 cycles

ON FLIGHT 4058 (DTW TO BHM) ON DEPARTURE RECEIVED NOSE DOOR OPEN AND LANDING GEAR UNSAFE MASTER WARNINGS OCCURED AFTER GEAR RETRACTION ON TAKEOFF/CLIMB. NOSE GEAR SHOWED IN DOWN POSITION RAN QRH AND ALL 3 LANDING GEAR SHOWED IN DOWN POSITION WITH GREEN COLOR. COMPLY WITH PA 05-018 REV J. PERFORMED AIR RETURN TO DTW. REPLACED NOSE GEAR CENTERED/EXTENDED PROXIMITY SENSOR BRACKET. RERIGGED NOSE GEAR CENTERED/EXTENDED PROXIMITY SENSOR. REPLACED NOSE GEAR CENTERED/EXTENDED PROXIMITY SENSOR TARGET. PERFORMED GEAR EXTENSION/RETRACTION CHECKS. ALL REFERENCE CRJ 200 CMM 32-20-04 CRJ 200 AMM 32-61-05 AND 32-61-05 AND 32-30-00. COMPLIED WITH PA05-018 REV J SCENARIO 1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,095 hrs · 11,819 cycles

FORWARD AISLE EMERGENCY LIGHT INOP. REPLACED BULB. PN 1317. REF CRJ 200 AMM CH 33-50-00.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,602 hrs · 11,289 cycles

FOUND LEFT AND RIGHT AFT OVERWING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER ASSY AT PS41L PN OFF/ON BA5-0933-901 SN OFF UNK SN ON CO1475, REF AMM 33-51-05. REPLACED BATTERY PACK PN OFF/ON AD-2013-1A SN OFF 74974 SN ON 68804 REF 33-51-01. OPS CHECKS GOOD, REF MM409A: 060549, 060546 FOR DETAILS.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 10,398 hrs · 9,827 cycles

RT OVERWING EMERGENCY LIGHT INOP. RELAMPED PN 1317 IN REF TO AMM 33-51-21. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,398 hrs · 9,827 cycles

LT OVERWING EMERGENCY LIGHT INOP. RELAMPED PN 1317 IN REF TO AMM 33-51-21. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — MISALIGNED (MLG) · airframe 9,946 hrs · 9,305 cycles

AFTER TAKEOFF, RECEIVED A GEAR DISAGREE WARNING, RT MAIN GEAR SHOWED RED. COMPLETED NON-NORMAL CHECKLIST, RETURNED TO DEPARTURE. RESECURED RT MLG UPLOCK TARGET AND ADJUSTED SENSOR TO TARGET GAP IAW AMM 32-61-05. PERFORMED GEAR SWINGS WITH PUMP 3A, HYD PRESSURE GOOD 3B HYD PRESSURE GOOD AND BOTH PUMPS 3A AND 3B, HYD PRESSURE GOOD IAW AMM 32-30-00.

Part: BRACKET — DAMAGED (CENTERING CAM) · airframe 7,958 hrs · 7,146 cycles

ON CLIMB OUT, DURING RETRACTION OF LANDING GEAR NOSE WHEEL DID RETRACT NOSE DOOR OPEN AND GEAR DISAGREE MESSAGE. COMPLETED THE EMERGENCY/NON-NORMAL PROCEDURE IN THE POM AND GEAR LOCKED DOWN SHOWED 3 GREEN. CONTACTED DISPATCH AND MX CONTROL, AND DECIDED TO RETURN TO DEPARTURE. R & R BRACKET FOR CENTERING CAM SENSOR IAW AMM 32-61-25 READJUSTED SENSOR IAW AMM 32-61-05 PERFORMED OPS CHECK OF EXTENSION AND RETRACTION SYS IAW CRJ 200 32-30-00 PN OFF/ON 16215-105 ALL CHECKS GOOD AT THIS TIME.