N834AY

Part: BULKHEAD WEB — CRACKED (ZONE 100) · airframe 25,056 hrs · 25,105 cycles

FOUND FS 559 RH SIDE BULKHEAD WEB OB OF RBL 9.0 WL 58.70 .300 LONG 75% FSH. FAILED NDT INSPECTION. COMPLIED WITH REPAIR TO THE 559 BULKHEAD IAW EO P53025 REO 601R-53-41- 260 REV G, 601R-53-41-609 REV D AND 601R-53-41-2856 REV--.NO DEFECTS NOTED.

Part: BULKHEAD WEB — CRACKED (AFT) · airframe 25,056 hrs · 25,105 cycles

FOUND REAR PRESSURE BULKHEAD WEB AT LBL 27.50 WL 130 HAS INDICATION NOTED TOP OF CARGO DOOR TRACK .400 LONG 80% FSH FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD AT LBL 27.50, WL 130 IAW BOMBARDIER REO 601R-53-61-1541 REV. F, DATED 2014/11/12 . THIS REPAIR HAS IN-SERVICE DEVIATION REQUIREMENTS IAW BOMBARDIER REO 601R-53-61-1541 REV. F, DATED 2014/11/12, PAGE 1A

Part: BULKHEAD WEB — CRACKED (BS 202.75) · airframe 25,056 hrs · 25,105 cycles

INDICATION NOTED AT THE FS 202.75 PRESSURE BULKHEAD AT BL 23.71 BRAKE CABLE PASS THROUGH HOLE AT THE 12 O'CLOCK APPROX. .100"" IN LENGTH VERTICALLY AND 100% FULL SCREEN HEIGHT FAILING NDT. REPAIRED FS 202.75 PRESSURE BULKHEAD AT PARKING BRAKE CABLE PASS THROUGH IAW ENDEAVOR AIR EO P53015 ON JOB 8803425/5147 THIS IS A MAJOR REPAIR. OPS CHECK GOOD.

Part: ATTACH ANGLE — CRACKED (WING) · airframe 25,056 hrs · 25,105 cycles

ATTACH ANGLE ON LEADING EDGE 530JL IS CRACKED. DRILLED & INSTALLED ANGLE 600-12045-11 IAW SRM 51-40-11 & 51-41-02.

Part: FITTING — CRACKED (FLOORBEAM) · airframe 25,056 hrs · 25,105 cycles

CABIN FLOOR BEAM FITTING CRACKED AT FS 460 OUTBD SIDE OF RBL 9.0 BEAM. REMOVED AND REPLACED FLOORBEAM FITTING IAW CRJ 200 SRM 51-42-21 AND 51-40-11.

Part: BRACKET — CRACKED (RT MLG) · airframe 25,056 hrs · 25,105 cycles

"RH MLG VOLUMETRIC FUSE MOUNT BRACKET CRACKED. "INSTALLED RH MLG VOLUMETRIC FUSE MOUNT BRACKET P/N: 601R75278-11 IAWCRJ 200 SRM 51-42-06. "

Part: STOP FITTING — CRACKED (PAX DOOR) · airframe 25,056 hrs · 25,105 cycles

"PAX DOOR UPPER STOP FITTING CRACKED AT FS 310 FRAME. REMOVED AND REPLACED UPPER STOP FITTING @ FS 310 PAX DOOR OPENING WITH PART #600-38087-31 IAW CRJ 200 SRM 57-42-21 REMOVED TAPE. "

Part: FITTING — CRACKED (WINDSHIELD) · airframe 25,056 hrs · 25,105 cycles

PILOTS WINDSHIELD SIDE POST BOTTOM AFT FITTING CRACKED P/N: 601R33235-3. REMOVED AND REPLACED PILOTS WINDSHIELD SIDE POST BOTTOM AFT FITTING IAW CRJ 200 SRM 51-40-11 AND 51-42-21.

Part: FITTING — CRACKED (WINDOW POST) · airframe 25,056 hrs · 25,105 cycles

CO-PILOTS WINDSHIELD SIDE POST BOTTOM AFT FITTING CRACKED P/N:601R33235-4. REMOVED AND REPLACED COPILOTS WINDSHIELD SIDE POST BOTTOM AFT FITTING IAW CRJ 200 SRM 51-40-11 AND 51-42-21.

Part: ANGLE — CRACKED (SUPPORT BEAM) · airframe 25,056 hrs · 25,105 cycles

"CARGO DOOR SUPPORT BEAM BOTTOM ANGLE CRACKED AT FWD FACE OF FS 621 BULKHEAD WEB, WL 114. "REMOVED TAPE. REMOVED AND REPLACED ANGLE LOCATED ON CARGO DOOR SUPPORT BEAM BOTTOM AREA AT FWD FACE OF FS 621 BULKHEAD WEB, WL 114 IAW CRJ 200 SRM 51-42-20. "

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 23,773 hrs · 23,671 cycles

EMER LGTS BATTERY DEPLETED RECHARGED BATTERY WITH AIRCRAFT POWER IAW CMM 25-60-03 FOR 6 HOURS PERFORMED OPS TEST OF THE EMREGENCY LIGHTS IAW AMM 33-51-04 PERFORMED OPS TEST OF THE BATTERY PACK/CHARGER ASSY IAW AMM 33-51-00 OPS TEST PASSED A/C GOOD FOR SVC

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,534 hrs · 22,393 cycles

LH FWD OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED #2, PS2LF EMERGENCY BETTERY CHARGER ASSEMBLY. IAW CRJ AMM 33-51-05 OPS CHECKS GOOD AT THIS TIME.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 22,433 hrs · 22,282 cycles

LOWER AREA OF REAR PRESSURE BULKHEAD BY LBL 9.5 HAS A LARGE DENT. REPAIRED FS621 AFT PRESSURE BULKHEAD DENT @ LBL9 LWR AREA IAW REO 601R-53-61-68-78 OPERATIONAL CK OF CARGO BAY DOOR BALANCE SPRING C/W IAW AMM 52-31-08 NO DEFECTS NOTED.

Part: SEAL — WORN (RT COWLING) · airframe 22,433 hrs · 22,282 cycles

RT ENG LWR NOSE COWL TE IS KNIFE EDGED. REMOVED/REPLACED NOSE COWL T/E IAW CMM 71-14-01.

Part: STEP — CRACKED (PAX DOOR) · airframe 22,433 hrs · 22,282 cycles

PAX DOOR STAIR EDGE MEMBER CRACKED ON AFT SIDE. CUTOUT DAMAGE/REPAIRED IAW REO 601R-52-11-279.

Part: RETAINER — CRACKED (RT PYLON) · airframe 22,433 hrs · 22,282 cycles

RT PYLON PANEL 422BT SEAL RETAINER CRACKED. REMOVED AND REPLACED PANEL 422BT SEAL RETAINER IAW SRM 51-42-06.

Part: SEAL — CHAFED (TAILPIPE) · airframe 22,433 hrs · 22,282 cycles

LT TAIL PIPE FAIRING LE METAL SEAL HAS CHAFING DAMAGE. REMOVED AND REPLACED WITH NEW METAL SEAL ON LT TAIL PIPE FAIRING L/E IAW CMM 20-42-06 AND CMM 78-11-00.

Part: HINGE — CRACKED (FUSELAGE) · airframe 22,433 hrs · 22,282 cycles

AFT CARGO THRESHOLD HINGE BROKEN/CRACKED IN 2 AREAS. REMOVED/REPLACED HINGE IAW SRM 51-40-11-00 TR 51-42.

Part: RETAINER — CRACKED (LT PYLON) · airframe 22,433 hrs · 22,282 cycles

LT PYLON PANEL 412DB SEAL RETAINER CRACKED. REMOVED/REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: PANEL — CHAFED (WING) · airframe 22,433 hrs · 22,282 cycles

SUPPLEMENTAL INFORMATION. PANEL 599CB ON THE ZONE 5 PANEL RACK HAS CHAFING. REMOVED CHAFE FOUND TO BE OUT OF LIOMITS IAW SRM 57-60-00. DRILLED AND LOCATED NEW 599CB PANEL IAW SRM 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,433 hrs · 22,282 cycles

RIGHT HAND SEAT TRACK NR 2 HAS CORROSION. REMOVED/REPLACED SEAT TRACK IAW AMM 53-01-11 SEAT TRACK FABRICATED ON CARD#6915030 1016735 2000 0162.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,433 hrs · 22,282 cycles

LEFT HAND SEAT TRACK NR 3 HAS CORROSION. REMOVED/REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,433 hrs · 22,282 cycles

RIGHT HAND SEAT TRACK NR 3 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,433 hrs · 22,282 cycles

SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574 IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,433 hrs · 22,282 cycles

RIGHT HAND SEAT TRACK NR 1 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,433 hrs · 22,282 cycles

SEAT TRACK ON TOP OF RBL 27 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 33-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,433 hrs · 22,282 cycles

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

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,433 hrs · 22,282 cycles

SEAT TRACK ON TOP OF RBL 9 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,433 hrs · 22,282 cycles

LEFT HAND SEAT TRACK NR 1 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK STICK NR 4 IAW AMM 53-01-11-420-01.

Part: SEAL — BROKEN (PBE) · airframe 21,456 hrs · 21,255 cycles

AFT PBE SEAL BROKEN. INSTALLED AFT PBE SEAL AS REQUIRED. A/C OK FOR SVC.

Part: SEAL — MISSING (PBE) · airframe 21,440 hrs · 21,238 cycles

CABIN PBE MISSING SEAL. REPLACED BROKEN SEAL ON CABIN PBE AS REQUIRED.

Part: ELT — NO TEST (CABIN) · airframe 1,990 hrs · 19,645 cycles

ELT FAILED INERTIA TEST. REMOVED AND REPLACED ELT ASSY IAW AMM 25-62-01 OPS CHECKED GOOD.

Part: FUEL — LEAKING (NR 2 ENGINE) · airframe 19,110 hrs · 18,736 cycles

NR 2 ENGINE N2 LAG BEHIND DURING START DRY MOTOR ENGINE. FLAMES REPORTED AND FUEL LEAKING. RAN THE ENGINE FIRE ON THE GROUND SEVERE OR ENG FIRE CHECKLIST. ANOTHER REPORT CAME IN THAT WE WERE STILL ON FIRE. CALLED THE FIRE TRUCKS TO TAKE A LOOK. MAINTENANCE INSPECTED TAIL PIPE FOR DAMAGE, NO DAMAGE NOTED. DRY RUN MOTOR IAW AMM 71-00-00 TO BLOW OUT RESIDUAL FUEL AND TO CHECK STARTER VALVE AND STARTER OPERATION. OPS CHECK GOOD. RAN ENGINE WITH CREW TO OPS CHECK ENGINE OPERATION IAW AMM 71-00-00. NO DEFECTS NOTED, OPS CHECK GOOD. BOTH FIRE BOTTLE DISCHARGED, REFER TO NEXT DISCREPANCY FOR CORRECTIVE ACTION.

Part: SEAL — BROKEN (FLASHLIGHT) · airframe 18,880 hrs · 18,502 cycles

FA REPORTED THE FLASHLIGHT SEAL BROKEN. REPLACED FA FLASHLIGHT SEAL, IAW AMM 25-61-02.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 18,793 hrs · 18,414 cycles

RIGHT INBD FLAP VANE CHAFED. REMOVED & REPLACED THE FLAP VANE IAW SRM 51-42-13.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,793 hrs · 18,414 cycles

WHILE REMOVING CORROSION ON LBL27 FS 605 - FS 621 FOUND CRACK ON O/B FLANGE. REPAIRED O/B FLANGE OF FITTING AT LBL27 FS 605-621 IAW EA CRJ253-05050.

Part: SIGN — INOPERATIVE (CABIN) · airframe 18,793 hrs · 18,414 cycles

FLOOR LEVEL EXIT SIGN AT PAX DOOR DOES NOT OPERATE WHEN TESTING EMER BATTERY PACKS 1 AND 3. PERFORMED OPS TEST OF EMERGENCY LIGHT BATTERY PACKS 1 AND 3. NO DEFECTS NOTED IAW AMM 33-51-04-740-801.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,793 hrs · 18,414 cycles

FLOORBOARD SUPPORT AT FS621 BETWEEN LBL27 AND LH SILL HAS CORROSION AROUND SCREW HOLES. REMOVED DAMAGE AND REPAIRED IAW REO 601R-53-61-117.

Part: PANEL — CRACKED (PASSENGER DOOR) · airframe 18,793 hrs · 18,414 cycles

PAX DOOR FWD RISER PANEL IS CRACKED BY THIRD STEP. COMPLIED WITH REPAIR TO THE PAX DOOR FWD SIDE PANEL IAW REO.NO:601R-52-11-702 REV. E.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,793 hrs · 18,414 cycles

FLOORBEAM FOUND CRACKED AT LBL 9 BS 280. REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED AND INSTALLED A REPAIR IAW REO 601R-53-11-136.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 18,793 hrs · 18,414 cycles

MAIN CABIN FLOORBEAM IS CORRODED BS 280 LBL 9 - RBL9. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06.

Part: BULKHEAD — CRACKED (BS 280) · airframe 18,793 hrs · 18,414 cycles

FOUND A CRACK ON THE LOWER BULKHEAD WEB RBL 9 BS 280. REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED AND INSTALLED A REPAIR IAW REO 601R-53-11-171.

Part: GUIDE PLATE — CRACKED (TE FLAP) · airframe 18,793 hrs · 18,414 cycles

RIGHT OUTBOARD FLAP, MID HINGE, OUTBOARD FAIRING GUIDE PLATE IS CRACKED. REMOVED AND REPLACED RIGHT OUTBOARD FLAP MID HINGE OUTBOARD FAIRING GUIDE PLATE IAW SRM 51-42-06 APPLIED TOP COAT IAW SRM 51-25-16.

Part: CARGO TRACK — CORRODED (BS 613-618) · airframe 18,793 hrs · 18,414 cycles

LBL 9 CARGO TRACK BETWEEN BS 613 TO 618 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. INSTALLED A REPLACEMENT CARGO TRACK IAW REO 601R-53-00-485.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 18,793 hrs · 18,414 cycles

LBL 27 CARGO TRACK BETWEEN BS 559+79 AND 559+96 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-01-11 AND REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 559-598) · airframe 18,793 hrs · 18,414 cycles

LBL 9 SEAT TRACK BETWEEN BS 559+110 TO 568 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED THE SEAT TRACK IAW REO-601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 18,793 hrs · 18,414 cycles

LEFT SIDEWALL SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485, AND SRM 53-51-49.

Part: ANGLE — CRACKED (BS 473) · airframe 18,793 hrs · 18,414 cycles

ANGLE IS CRACKED ON THE O/B SIDE OF LBL 27 AT BS 473.15, IN CABIN BELOW FLOOR. REMOVED AND INSTALLED A NEW ANGLE IAW SRM 51-42-20.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,793 hrs · 18,414 cycles

REAR PRESSURE BULKHEAD LT OBLIQUE ANGLE ON STGR14 IS CRACKED. REMOVED AND REPLACED OBLIQUE ANGLE LT SIDE OF REAR PRESSURE BULKHEAD ON STR 14L IAW SRM 51-42-21 & REO 601R-53-61-422 REV.

Part: SEAT TRACK — CORRODED (BS 554-559) · airframe 18,793 hrs · 18,414 cycles

LEFT SIDEWALL SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM-53-01-11.

Part: SEAT TRACK — CORRODED (BS 554-559) · airframe 18,793 hrs · 18,414 cycles

RIGHT SIDEWALL SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM-53-01-11.

Part: SEAT TRACK — CORRODED (BS 499-541) · airframe 18,793 hrs · 18,414 cycles

LEFT SIDEWALL SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11, AND SRM 53-51-49.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,793 hrs · 18,414 cycles

REAR PRESSURE BULKHEAD RH OBLIQUE ANGLE ON STGR14 IS CRACKED. REMOVED AND REPLACED OBLIQUE ANGLE RT ON STR 14R IAW SRM 51-42-21 & REO 601R-53-61-422. REV.

Part: SEAT TRACK — CORRODED (BS 499-541) · airframe 18,793 hrs · 18,414 cycles

RIGHT SIDEWALL SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM-53-01-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 18,793 hrs · 18,414 cycles

RBL 9 SEAT TRACK FROM BS 559+5 TO 559+19 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM-53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 18,793 hrs · 18,414 cycles

LEFT AISLE SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 18,793 hrs · 18,414 cycles

LEFT AISLE SEAT TRACK HAS CORROSION BS 559+4 - 559+86. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 18,793 hrs · 18,414 cycles

RIGHT SIDEWALL SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM-53-01-11.

Part: TRIPLER — GOUGED (FUSELAGE) · airframe 18,793 hrs · 18,414 cycles

AFT PRESSURE BULKHEAD PREVIOUS REPAIR AT FWD FACE 30 IN ABOVE THE FLOOR RBL 27 IS DAMAGED. REMOVED & REPLACED DAMAGED TRIPLER AT RBL 27 ON AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1285.

Part: DRAG ANGLE — CRACKED (PASSENGER DOOR) · airframe 18,793 hrs · 18,414 cycles

PAX DOOR AFT RISER DRAG ANGLE IS CRACKED BY ASSIST MOTOR PULLEY. REPAIRED THE AFT DRAG ANGLE AND RESTORED FINISH IAW REO 601R-52-11-513 AND SRM 51-25-16.

Part: TRIPLER — DAMAGED (FUSELAGE) · airframe 18,793 hrs · 18,414 cycles

AFT PRESSURE BULKHEAD PREVIOUS REPAIR AT FWD FACE LOCATED 30 IN ABOVE FLOOR RBL 18 IS DAMAGED. REMOVED & REPLACED DAMAGED REPAIR TRIPLER IAW REO 601R-53-61-1285.

Part: BRACKET — CRACKED (PASSENGER DOOR) · airframe 18,793 hrs · 18,414 cycles

PAX DOOR ASSIST MOTOR LOWER BRACKET IS CRACKED. REMOVED & REPLACED SUPPORT BRACKET IAW SRM 51-42-06.

Part: RISER — CRACKED (PASSENGER DOOR) · airframe 18,793 hrs · 18,414 cycles

PAX DOOR AFT RISER PANEL IS CRACKED BY BOTTOM STEP. REPAIRED PAX DOOR AFT SKIN PANEL IAW REO 601R-52-11-702 REV E AAR SM-14

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 18,793 hrs · 18,414 cycles

LEFT WING LE SUPPORT BRACKET AT WS 149.58 IS CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-41-02.

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 18,793 hrs · 18,414 cycles

RIGHT WING LE ATTACH BRACKET AT WS 149.58 FOUND CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-41-02 P.N. 600-12045-12. AAR EMP 25133

Part: CARGO TRACK — CORRODED (BS 559) · airframe 18,793 hrs · 18,414 cycles

LBL 9 CARGO TRACK BETWEEN BS 559+86 AND 559+95 IS CORRODED. REMOVED & REPLACED THE CARGO TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 18,793 hrs · 18,414 cycles

RIGHT SIDEWALL SEAT TRACK HAS CORROSION. REMOVED AND REPLACE THE SEAT TRACK IAW AMM-53-01-11.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 18,793 hrs · 18,414 cycles

LEFT SIDEWALL SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 18,793 hrs · 18,414 cycles

RIGHT SIDEWALL SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: FLOOR SUPPORT — CORRODED (BS 341-349) · airframe 18,793 hrs · 18,414 cycles

IN MAIN CABIN FLOOR SUPPORT BS 349 - 341, LBL 36 HAS CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,793 hrs · 18,414 cycles

LT SIDEWALL SEAT TRACK STICK 2 HAS CORROSION, IN CABIN. REMOVED AND REPLACED LT NR 2 SIDEWALL SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 18,793 hrs · 18,414 cycles

LEFT SIDEWALL SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 18,793 hrs · 18,414 cycles

RIGHT SIDEWALL SEAT TRACK HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: OXYGEN MASK — MALFUNCTIONED (CABIN) · airframe 18,793 hrs · 18,414 cycles

MASKS 11A AND 11B DID NOT DROP DURING OPS. PERFORMED OPS TEST OF THE PASSENGER OXYGEN SYSTEM IAW AMM 35-20-00-710-803. NO DEFECTS NOTED.

Part: OXYGEN MASK — MALFUNCTIONED (CABIN) · airframe 18,793 hrs · 18,414 cycles

OXYGEN MASKS 12A AND 12B DID NOT DROP DURING OPS. PERFORMED OPS TEST OF THE PASSENGER OXYGEN SYSTEM IAW AMM 35-20-00-710-803. NO DEFECTS NOTED.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 18,780 hrs · 18,401 cycles

CAPTAIN`S OXYGEN MASK LEAKING. REMOVED & REPLACED THE OXYGEN MASK IAW AMM 35-11-12.

Part: SWIVEL — BROKEN (PAX DOOR) · airframe 18,533 hrs · 18,159 cycles

RAMP REPORTED PAX DOOR WOULD NOT OPEN, FOUND FWD SWIVEL LEVER BROKE (COUNTER BALANCE). R & R THE PAX DOOR COUNTERBALANCE FWD SWIVEL LEVER IAW AMM 52-11-17 OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 18,139 hrs · 17,738 cycles

F/A REPORTS MAIN CABIN DOOR HANDLE IS DIFFICULT TO CLOSE. CLEANED AND LUBED PAX DOOR IAW AMM 52-11-00 AND OPS TEST OK AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 18,076 hrs · 17,671 cycles

FIRST OFFICERS EMER FLASHLIGHT LED IS NOT BLINKING. R & R FIRST OFFICERS EMER FLASHLIGHT BATTERY IAW CMM 25-60-02.

Part: BEARING — DEFECTIVE (CABIN DOOR) · airframe 17,961 hrs · 17,547 cycles

MAIN CABIN DOOR HANDLE WILL NOT CLOSE. REPLACED FWD & LWR ROD BEARING IAW AMM 52-11-00. ALL CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE · airframe 16,487 hrs · 16,056 cycles

FOUND EMER FLASHLIGHT RED LIGHT NOT FLASHING & PROTECTIVE STRAP BROKEN. R & R BATTERY PACK IN EMER FLASHLIGHT. REPLACED BROKEN STRAP ALL IAW AMM 25-61-00. OPERATIONS CHECKED GOOD.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 16,468 hrs · 16,031 cycles

FOUND INFANT LIFE VEST BAG TORN. R & R INFANT LIFE VEST IAW AMM 25-60-00. OK FOR SERVICE.

Part: DETECTOR — FAULTY (TE FLAP) · airframe 16,362 hrs · 15,912 cycles

FLAPS FAIL MSG. DURING AFTER START PROCEDURE WHEN FLAPS WERE SELECTED TO 20 DEGREES. PERFORMED R & R OF SKEW DETECTION UNIT IAW AMM 27-51-15. OPERATIONS TESTED GOOD IAW AMM 27-51-15. PERFORMED TROUBLESHOOTING IAW FIM CHAPTER 27-50-00 REV 48 IAW AD 1009 - 06 -12 PARAGRAPH H B I, AMOC LOG 14-105 DATED 12 30 2014 & TS 00100R1 FIM TECHNICAL SUPPLEMENT. FAULT CODES 51A, 111A,121B, 122B, 52A, 112A, 121A, 131B, 111B, 112B, 112B, 122A & 131A. SUSPECT SDU WAS NOT RESET AFTER BITE TEST IAW MEL 27-51-1A.

Part: OXYGEN MASK — MALFUNCTIONED (COCKPIT) · airframe 16,356 hrs · 15,906 cycles

CAPTAINS O2 MASK INTO FREE FLOW & WILL NOT SHUTOFF. EMER FLOW & 100% WERE CHECKED & DO NOT SEEM TO AFFECT FREE FLOW. PERFORMED OPERATIONS CHECK OF CREW O2 SYSTEM IAW AMM 35-10-00. OPERATIONS CHECKED GOOD.

Part: BRACKET — DAMAGED (LANDING GEAR) · airframe 16,341 hrs · 15,891 cycles

JUST AFTER SELECTING THE LANDING GEAR LEVER TO THE UP POSITION, AFTER TAKEOFF, RECEIVED A GEAR DISAGREE ALONG WITH A NOSE DOOR OPEN WARNING MSG. MAIN GEAR WAS INDICATING UP WITH THE NOSE GEAR STILL IN THE DOWN & LOCKED POSITION. REFERENCED QRH, RELEASED THE GEAR. REPLACED BRACKET FOR PROX SENSOR PS14GA PN ON & OFF 16215-105. ADJUSTED PROX SENSOR PS14GA IAW 32-61-05. PREFORMED OPERATIONS CHECK IAW 32-33-00, ALL CHECKED GOOD SEE NR CONTINUATION CARDS FOR DETAILS.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 15,822 hrs · 15,369 cycles

FS 621 PRESS BULKHEAD HAS 6 CHAFED AREAS FROM SCREWS BETWEEN LBL 27.5 & RBL 36.2 AT WL 103.75. REPAIRED IAW REO 601R-53-61-2155.

Part: STRIKER — DAMAGED (CABIN DOOR) · airframe 15,444 hrs · 14,995 cycles

MAIN CABIN DOOR SEAL LEAKING. REPAIRED DOOR SEAL STRIKER FORE & AFT IAW NRC N55807 & N55809 FOR DETAILS. SEAL LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 15,405 hrs · 14,957 cycles

NUMBER 2 LIGHT BULB ON THE EMER EXIT SIGN BY SERVICE DOOR. INSTALLED NEW BULB PN OL3071BPEGPL IAW AMM 33-51-13, OPERATIONS CHECKED GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 15,114 hrs · 14,674 cycles

ON PREFLIGHT FLIGHT ATTENDANT REPORTED PHOTO ILLUMINES CTR STRIP FLOOR AT 8AB MISSING. INSTALLED NEW FLOOR EMER STRIP AT 8AB IAW AMM 33-51-01, OK FOR SERVICE.

Part: LIFE VEST — DAMAGED (CABIN) · airframe 13,658 hrs · 13,260 cycles

FOUND TWO INFANT LIFE VESTS DAMAGED. R & R LIFE VESTS IAW PA 25-096A.

Part: PRIORITY VALVE — MALFUNCTIONED (LANDING GEAR) · airframe 13,181 hrs · 12,794 cycles

AFTER TAKEOFF WHEN GEAR WAS SELECTED UP, RECEIVED MASTER WARNING GEAR DISAGREE, AND NOSE DOOR WARNING, RAN QRH SELECTED GEAR DOWN AND GEAR INDICATED NORMALLY. REMOVED AND REPLACED NLG SELECTOR VALVE IAW 32-33-10. REMOVED AND REPLACED NLG PRIORITY VALVE IAW 32-33-15. REMOVED AND REPLACED MLG PRIORITY VALVE IAW 32-32-15. OPERATIONS CHECK OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM GOOD IAW 32-30-00. COMPLETED PA 05-018 REV J SCENARIO 1 PER MOTR GROUP.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 12,975 hrs · 12,594 cycles

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

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 12,815 hrs · 12,441 cycles

OBSERVER LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED OBSERVER LIFE VEST IAW AMM 25-61-03.

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 12,709 hrs · 12,337 cycles

RIGHT WING PLANK ACCESS HOLE FOR PANEL 640BB CORRODED. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 12,436 hrs · 12,073 cycles

ON FLIGHT 3729 (ALB - DTW) FLAPS FAILED AT ZERO ON APPROACH INTO DTW. AIRCRAFT LANDED SAFELY. PERFORMED TROUBLESHOOTING PER BOMBARDEIR FIM REVISION 43 IAW AD 2009-06-12 PARAGRAPH(H)(6)(I), AMOC DATED APRIL 19, 2012 AND PA AD27-052H. RIGGED FLAPS. REPLACED STALL PROTECTION COMPUTER.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 11,117 hrs · 10,623 cycles

RIGHT WING AFT EMERGENCY LIGHT INOP. RELAMPED BULB, P/N ON & OFF 1317 IAW CRJ200 AMM 33-51-21. OPS CHECK GOOD.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 10,331 hrs · 9,688 cycles

EMERGENCY LIGHT ON STATUS MESSAGE ILLUMINATED IN FLIGHT. F/A CONFIRMS EMERGENCY LIGHTS ILLUMINATED. R & R SENSE RELAY K1XF. PERFORMED OPS CHECKS OF EMERGENCY LIGHTING SYSTEM, ALL CHECKED GOOD IAW AMM 24-21-27.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,879 hrs · 7,048 cycles

NR 3 CEILING EMERGENCY FLOODLIGHT INOP. RELAMPED NR 3 CEILING EMERGENCY LIGHT BULB. OPS CK GOOD PN 1317.

Part: SKIN — DENTED (FUSELAGE) · airframe 7,715 hrs · 6,893 cycles

THE ACFT WAS PUSHED BACK INTO A BAGGAGE CART WHICH CAUSED A DENT TO THE LT FUSELAGE SKIN 9.75" LONG X 8.0" WIDTH WITH A MAX DEPTH OF 0.125 INCH. THE DENT WAS SMOOTH, WITH NO EVIDENCE OF SKIN CRACKING AND THE INTERNAL STRUCTURE WAS DISPLACED, BUT THERE WAS NO BUCKLING OR CRACKING. EVEN SO, BBD DETERMINED THE DAMAGE WAS BEYOND FLYABLE LIMITS. ACCOMPLISH REPAIR IAW REO 601R-53-51-105 DATED 21JAN2010.

Part: APU — ODOR · airframe 5,636 hrs · 4,718 cycles

FIRST ATTEMPT AT TURNING ON THE APU DURING APPROACH WAS UNSUCCESSFUL, SECOND ATTEMPT TO START THE APU WAS SUCCESSFUL BUT AFTER ONE MINUTE OF USE A VERY STRONG JET FUEL ODOR AS DETECTED IN THE CABIN AND FLIGHT DECK. FLIGHT CREW DONNED OXYGEN MASK AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MX COMPLETE PACK BURN AND DEFERRED PER MEL 49-10-1C, PULLED AND COLLARED CB N12 AND S3 TRANSFERRED TO MM02, MXC 17754 NOTIFIED PERFORMED OPS CK 3 TIMES. APU START NORMALLY, NO DEFECTS THIS TIME.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 4,378 hrs · 3,505 cycles

FLAPS FAILED WHEN SELECTED FROM 20 TO 30 ON APPROACH. SYSTEM RESET AND PLACED ON SEVENTY TWO HOUR WATCH PER AD 2006-12-21.