N8683B

Part: CABLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,286 hrs · 28,233 cycles

AFT 4 ROWS SEAT FLOOR EMERGENCY LIGHTS INOP REPLACED EMERGENCY FLOOR LIGHT CABLE AFT PN 5946-5 AND PN 6464-5 IAW CRJ-200 AMM 33-51-01 OPS CHECKS GOOD IAW CRJ-200 AMM 33-51-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,944 hrs · 27,881 cycles

EXIT SIGN LIGHT IN EXIT ROW NOT ILLUMINATED. R&R BATTERY PACK 2. OPS CHECK GOOD IAW AMM 33-51-04.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,347 hrs · 27,226 cycles

DURING WALK AROUND FOUND LT FWD EXT EMERGENCY EXIT LIGHT INOP. RELAMPED LT FWD EXT EMERGENCY EXIT LIGHT IAW AMM 33-51-21 OPS CHECK GOOD.

Part: SKIN — CORRODED (BS 605-621) · airframe 29,149 hrs · 27,020 cycles

AFT CARGO BETWN STA 605-621 STR 27 CORRODED. DAMAGED REMOVED IAW EA 253-08775 INSTALLED REPAIR DOUBLER& FILLER SPIGOT. DTWI C/W IAW GMM 4-06.

Part: HOUSING — CRACKED (E.E DOOR HANDLE) · airframe 29,149 hrs · 27,020 cycles

AVIONICS DOOR HANDLE HOUSING IS CRACKED. REMOVED AND REPLACED CARGO DOOR HANDLE HOUSING I.A.W. CRJ-200 AMM 52-42-03-400-801. OPS CHECKS GOOD I.A.W. CRJ-200 AMM 52-42-00-720-801 AAR SM 107

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 29,149 hrs · 27,020 cycles

FLOOR SUPPORT STRUCTURE HAS CORROSION ON R/H FLOOR SILL FROM FS559.0 TO 559.0+80 REPLACED INTERCOASTAL 559+16 - 559+32 AND REPAIRED SILL 559+32-559+80 IAW BOMBA REO 601R-53-51-374 AAR AP 308

Part: FRAME — CORRODED (BS 605) · airframe 29,149 hrs · 27,020 cycles

FS 605 FRAME CORRODED BETWEEN STRGR 24L AND 24R. FRAME 605 BETWEEN STGRS 24L AND 24R CORRODED OUT OF LIMITS IAW CRJ-200 SRM 53-61-15. REMOVED AND REPLACED 605 FRAME SECTION IAW CRJ-200 SRM 51-42-06 OPS CHECK GOOD IAW CRJ-200 AMM 34-44-01-740-801 LEAK CHECK GOOD IAW CRJ-200 AMM 21-20-00. AAR SM 107

Part: FLOOR SUPPORT — CORRODED (574-605) · airframe 29,149 hrs · 27,020 cycles

AFT CARGO FLOOR SUPPORT STRUCTURE HAS CORROSION AT LBL9.0 FWD OF FS 605.00 REMOVED AND REPLACED LBL9 FLOOR SUPPORT STATION 574 TO 605 IAW CRJ 200 SRM 51-42-06 AND BOMBARDIER REO 601R-53-61-3780 AAR SM 84

Part: FRAME — CORRODED (AFT CARGO BAY) · airframe 29,149 hrs · 27,020 cycles

AT FS574.0 BELOW FLOOR ALONG FRAME FROM STGR 25L TO STGR25R HAS MULTIPLE AREAS OF CORROSION REPAIRED FRAME 574 FROM STRINGER 25L TO 25R I.A.W. CRJ-200 SRM 53-00-15 REPAIR NO. 2 AND 51-21-06 AAR SM 84

Part: CHANNEL — BENT (BS 574) · airframe 29,149 hrs · 27,020 cycles

CARGO LOWER SURROUND FRAME 574.0 LOWER U-CHANNEL SUPPORT IS BENT AND POSSIBLY CRACKED AT AFT RIVET LOCATION. REMOVED AND REPLACED U-CHANNEL SUPPORT AT CARGO LOWER SURROUND FRAM 574-08 IAW CRJ 200 SRM 51-42-16. AAR R SM 4

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 29,149 hrs · 27,020 cycles

INTERCOSTAL FS364 TO 349 CORRODED STR 26R REMOVED CORRODED INTERCOASTAL AND REPLACED WITH NEW INTERCOASTAL IAW CRJ 200 SRM 51-42-06 51-42-21 OPS CHECKS GOOD IAW CRJ 200 AMM 52-70-08 AND 34-54-04-720-801 AAR SM 58

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 29,149 hrs · 27,020 cycles

PASSENGER DOOR HAS DRAG ANGLE CRACKED. REMOVED AND REPLACED PREVIOUSLY REPAIRED DRAG ANGLE SECTION WITH NEWDRAG ANGLE SECTION IAW CRJ 200 REO 601R-52-11-513 AAR SM 107

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 29,149 hrs · 27,020 cycles

AFT CARGO FLOOR SUPPORT LBL27.0 HAS CORROSION FROM FS605.0 TO FS 621.0 REPAIRED CARGO FLOOR SUPPORT IAW EA CRJ253-08733 AAR SM 107

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,149 hrs · 27,020 cycles

AFT CARGO FLOOR SUPPORT STRUCTURE HAS CORROSION ON RBL9 FS559.0+112 REMOVE AND REPLACED CARGO SEAT RAIL AT FS 559+112 AND RBL 9 IAW CRJ 200 AMM 53-01-11 AAR SM 107

Part: SEAT TRACK — CORRODED (BS 449) · airframe 29,149 hrs · 27,020 cycles

DADO SEAT TRACK LH STICK #5 HAS CORROSION. SEAT TRACK STICK # 5 FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED WITH NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11 AAR SM 107

Part: FITTING — CRACKED (BS 461) · airframe 29,149 hrs · 27,020 cycles

FLOOR BEAM BATHTUB FITTING AT FS461.00 AND RBL9 IS CRACKED. REMOVED AND INSTALLED BATHTUB FITTING @ FS 461 + RBL IAW CRJ 200 SRM 51-42-06 AND 51-42-21 AAR SM 33

Part: FLOORBEAM — CRACKED (BS 484) · airframe 29,149 hrs · 27,020 cycles

FLOOR BEAM CLIP AT FS484.00 AND LBL36 IS CRACKED. REMOVED AND REPLACED CLIP IAW BOMBA REO 601R-53-41-059 REV B AAR SM 107

Part: SEAT TRACK — CORRODED (BS 449) · airframe 29,149 hrs · 27,020 cycles

LH SEAT TRACK #3 HAS CORROSION. REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11 AR SM 109

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,149 hrs · 27,020 cycles

AFT CARGO FLOOR SUPPORT STRUCTURE HAS CORROSION ON RBL9 FS559.0+96 REMOVED AND REPLACE CARGO SEAT RAIL AT FS 559+96 AND RBL 9 IAW CRJ 200 AMM 53-01-11 AAR SM 107

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 29,149 hrs · 27,020 cycles

DADO SEAT TRACK RH STICK #2 HAS CORROSION. REMOVED AND REPLACED DADO SEAT TRACK R/H # 2 IAW CRJ 200 AMM 53-01-11 AAR AP 135

Part: SEAT TRACK — CORRODED (BS 559) · airframe 29,149 hrs · 27,020 cycles

RIGHT HAND SEAT TRACK #4 HAS CORROSION. R/H SEAT TRACK # 4 WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED THE SEAT TRACK IAW CRJ 200 AMM 53-01-11.

Part: SEAT TRACK — CORRODED · airframe 29,149 hrs · 27,020 cycles

L/H FLOOR SEAT TRACK STICK 1 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK I.A.W. CRJ-200 AMM 53-01-11 AAR SM 58

Part: SEAT TRACK — CORRODED · airframe 29,149 hrs · 27,020 cycles

DADO SEAT TRACK RH STICK #4 HAS CORROSION. DADO SEAT TRACK R/H STICK WAS FOUND TO BE OUT LIMITS. REMOVED AND REPLACED DADO SEAT TRACK I.A.W. CRJ-200 AMM 53-01-11.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 29,149 hrs · 27,020 cycles

AFT CARGO FLOOR SUPPORT LBL27.0 HAS CORROSION FROM FS 574.00 TO FS605.00 REMOVED AND RE-PLACED LBL-27 FS 574.0 TO FS605 FLOOR SUPPORT I.A.W. VRJ-200 SRM 51-42-21 AAR R SM 17

Part: GUTTER — CRACKED (BS 310-349) · airframe 29,149 hrs · 27,020 cycles

PASSENGER DOOR RAIN GUTTER CRACKED AT CTR LINE OF DOOR OPENING. FWD CROWN SKIN BUTT SPLICE. REMOVED AND REPLACED RAIN GUTTER. I.A.W. CRJ-200 SRM 51-42-06 AAR SM 139

Part: SEAT TRACK — CORRODED (BS 559) · airframe 29,149 hrs · 27,020 cycles

SEAT TRACK CORRODED ON LBL 27+RBL 27 BETWEEN FS 559+80 AND FS 559+96. REMOVED AND REPLACED SEAT TRACK ON LBL 27 AND RBL 27 FROM F.S. 559+80 TO 559+96. I.A.W. CRJ-200 AMM 53-01-11 AAR SM 107

Part: SEAT TRACK — CORRODED · airframe 29,149 hrs · 27,020 cycles

DADO SEAT TRACK RH STICK #5 HAS CORROSION. REMOVED AND REPLACED UNSERVICEABLE SEAT TRACK #5 R/H SIDEWALL I.A.W. CRJ-200 AMM 53-01-11 AAR SM 58

Part: SEAT TRACK — CORRODED · airframe 29,149 hrs · 27,020 cycles

DADO SEAT TRACK LH STICK #3 HAS CORROSION. REMOVED AND REPLACED DADO SEAT TRACK L/H STICK #3 PART:601R38312-295 I.A.W. CRJ-200 AMM 53-01-11 DUE DATE: 10-12-19 AAR 527961 AAR SM 58

Part: SEAT TRACK — CORRODED · airframe 29,149 hrs · 27,020 cycles

LH SEAT TRACK #2 GOUGED AND HAS CORROSION. REPLACED SEAT TRACK I.A.W. CRJ-200 AMM 53-01-11 AAR SM 109

Part: SEAT TRACK — CORRODED · airframe 29,149 hrs · 27,020 cycles

DADO SEAT TRACK RH STICK #3 HAS CORROSION. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK I.A.W. CRJ-200 AMM 53-01-11.

Part: SEAT TRACK — CORRODED · airframe 29,149 hrs · 27,020 cycles

DADO SEAT TRACK RH STICK #7 HAS CORROSION. REMOVED AND REPLACED R/H SEAT TRACK #7 I.A.W. CRJ-200 53-00-49.

Part: FRAME — CORRODED (BS 621) · airframe 29,149 hrs · 27,020 cycles

AT FS621.0 BELOW FLOOR ALONG FRAME HAS MULTIPLE AREAS OF CORROSION FROM STGR 25L TO STGR25R REPAIRED FRAME AT STATION 621 FROM STRINGER 25L TO 25R I.A.W. CRJ-200 SRM 51-21-06. FOUND TO BE IN LIMITS. I.A.W. CRJ-200 SRM 53-00-00 FIG 102

Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,149 hrs · 27,020 cycles

FORWARD CABIN FLOOR SUPPORT -280- BEAM TOP CENTER CORRODED REMOVED AND REPLACED FWD CABIN FLOOR SUPPORT 280 BEAM, TOP CENTER ANGLES I.A.W. CRJ-200 SRM 51-42-06, 51-42-10.

Part: SEAT TRACK — CORRODED · airframe 29,149 hrs · 27,020 cycles

DADO SEAT TRACK LH STICK #2 HAS CORROSION. REMOVED AND REPLACED DADO SEAT TRACK L/H STICK #2 PART #601R38312-31 I.A.W. CRJ-200 AMM 53-01-11 AAR 517847 DUE DATE: 10/07/2019 AAR AP 468

Part: SEAT TRACK — CORRODED · airframe 29,149 hrs · 27,020 cycles

DADO SEAT TRACK RH STICK #6 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK I.A.W. CRJ-200 AMM 53-01-11 AAR AP 468

Part: FLOORBEAM — CRACKED (BS 484) · airframe 29,149 hrs · 27,020 cycles

FLOOR BEAM CLIP AT FS484.00 AND RBL27 IS CRACKED. REMOVED AND REPLACED WITH NEW CLIP AT FS 484.00 AND RBL 27 ON FLOOR BEAM IAW SRM 51-42-21.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 29,149 hrs · 27,020 cycles

FLOOR BEAM CLIP AT FS484.00 AND LBL27 IS CRACKED. REMOVED AND REPLACED ANGLE (CLIP) ON FLOOR BEAM FS 484.00 LBL 27 IAW 51-42-21.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 29,149 hrs · 27,020 cycles

LH SEAT TRACK #4 GOUGED AND HAS CORROSION. REMOVED AND REPLACED SEAT IAW CRJ 200 AMM 53-01-11 AAR SM 58

Part: SEAT TRACK — CORRODED · airframe 29,149 hrs · 27,020 cycles

RH SEAT TRACK #3 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK #3 R/H I.A.W. CRJ-200 AMM 53-01-11 SEAT TRACKWAS FABRICATED ON WORK CARD #1016950-2000-0213 .

Part: FLOORBEAM — CRACKED (BS 484) · airframe 29,149 hrs · 27,020 cycles

FLOOR BEAM CLIP AT FS484.00 AND RBL36 IS CRACKED. REMOVED CLIP AND INSTALLED NEW CLIP IAW BOMBARDIER REO 601R-53-41-059 AAR AP 377

Part: RUB STRIP — GOUGED (NR ENGINE FAN) · airframe 29,149 hrs · 27,020 cycles

#2 UPPER FAN COWL GOUGED ON AFT LIP. REMOVED ADN REPLACED RUB STRIP IAW CRJ 200 71-14-01-350-075-A01 AAR SM 58

Part: SEAT TRACK — CORRODED · airframe 29,149 hrs · 27,020 cycles

DADO SEAT TRACK LH STICK #7 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11 AAR SM 58

Part: SEAT TRACK — CORRODED · airframe 29,149 hrs · 27,020 cycles

RH SEAT TRACK #1 GOUGED AND HAS CORROSION REMOVED AND REPLACED 3 1 R/H SEAT TRACK IAW CRJ 200 AMM 53-01-11 AAR R SM 4

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 29,149 hrs · 27,020 cycles

DADO SEAT TRACK LH STICK #4 HAS CORROSION. REPLACED SEAT TRACK PART @ 601R-38312-1195 IAW CRJ 200 AMM 53-01-11 AAR SM 58

Part: BRACKET — CRACKED (BS 622) · airframe 29,149 hrs · 27,020 cycles

RPB OBLIQUE ANGLE AT STGR 15L CRACKED. REMOVED AND REPLACED ANGLE AT STRINGER 15L REAR PRESSURE BULKHEAD IAW CRJ 200 SRM 51-42-06 AAR SM 84

Part: SEAT TRACK — CORRODED (BS 449-541) · airframe 29,149 hrs · 27,020 cycles

DADO SEAT TRACK LH STICK #6 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 29,149 hrs · 27,020 cycles

AFT CARGO FLOOR SUPPORT STRUCTURE HAS CORROSION ON SEAT TRACK AT FS559.0+96 LBL9. REMOVED AND REPLACED WITH NEW SEAT TRACK ON AFT CARGO TIE DOWN AT FS 559.0 LBLCRJ 200 AMM 53-00-49 AAR AP 225

Part: BRACKET — CRACKED (LT MLG WW) · airframe 29,149 hrs · 27,020 cycles

LH MLG WHEEL WELL, BRAKE HYD PRESS TRANSDUCER ATTACH BRACKET CRACKED. REMOVED AND REPLACED DEFECTIVE BRACKET WITH NEW FOR LH MLG WHEEL WELL BREAK HYD PRESS TRANSDUCER IAW CRJ 200 SRM 51-42-21 AAR SM 107

Part: SEAT TRACK — CORRODED (BS 621) · airframe 29,149 hrs · 27,020 cycles

AFT CARGO FLOOR SUPPORT STRUCTURE HAS CORROSION ON SEAT TRACK AT FS621 ON LBL9. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-00-49 AAR AP 225

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 28,755 hrs · 26,585 cycles

EMER EXT LT WONT ILLUM MX REPINNED WIRE AND INSTALLED NEW CONNECTOR

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 27,829 hrs · 25,570 cycles

INBOARD LOWER AFT CORNER OF THE VERTICAL BEAM AT BS 409+128, RBL 27 HAD A 1 INCH CRACK UP TO THE SECOND RIVET FROM THE BOTTOM. REPAIRED THE VERTICAL BEAM IAW REO 601R-53-41-056. MAJOR REPAIR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,422 hrs · 25,461 cycles

CEILING EMERGENCY FLOODLIGHT LAMPS 1 & 2 FOUND INOPERATIVE. REMOVED AND REPLACED THE LAMPS IAW AMM 33-51-16, OPS CHECKED GOOD.

Part: DIODE — FAILED · airframe 27,367 hrs · 25,075 cycles

BURNING ODOR INSIDE AIRCRAFT, POWER SURGE ON POWER UP, PFD & MFD 2 INTERMITENT, AHARS 2 INOPERATIVE, APU MADE A LOUD BANGING NOISE. INSPECTED APU, NO DEFECTS OR CDCR NOTED. USING GPU PWR, NO PWR SURGES OR CDCR ODOR NOTED. SUSPECT APU AT FAULT. SERVICED APU CORRECTLY AND REMOVED AND REPLACED APU LOAD CONTROL VALVE IAW AMM 49-51-01. OPS CHECKED GOOD.

Part: PBE — DAMAGED (COCKPIT) · airframe 26,800 hrs · 24,459 cycles

COCKPIT PBE LOST VACUUM. REMOVED AND REPLACED THE PBE IAW AMM 35-31-01.

Part: PBE — DEFECTIVE (CABIN) · airframe 26,800 hrs · 24,459 cycles

WARDROBE PBE LOST VACUUM. REMOVED AND REPLACED THE PBE IAW AMM 35-31-01.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 26,608 hrs · 24,234 cycles

EMERGENCY EXIT LIGHT AT 1AB DOES NOT ILLUMINATE. REPAIRED THE EMERGENCY EXIT SIGN HARNESS IN FRONT OF ROW 1 A/B IAW ESPM 20-17-31. REPLACED THE EXIT SIGN IAW AMM 33-51-13. OP CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 26,502 hrs · 24,126 cycles

DURING FINAL APPROACH AND AFTER LANDING GEAR EXTENSION A STEERING INOP CAUTION ILLUMINATED 10 SECONDS AFTER EXTENSION. PERFORMED GO AROUND RAISED LANDING GEAR AND PERFORMED QRH. MESSAGE CLEARED. AFTER EXTENDING GEAR A SECOND TIME FOR APPROACH, 10 SECONDS LATER "STEERING INOP ILLUMINATED. PERFORMED EMERGENCY LANDING WITH CAUTION ILLUMINATED.AFTER LANDING AND COMING TO A COMPLETE STOP, PERFORMED RESET PER CFM CHAPTER 6.CAUTION EXTINGUISHED AND WE TAXIED TO THE GATE. FLAPS AT 30. FOLLOWED FIM 32-50-00 PG114 AND AMM 32-51-00-710-802. NO MSGS POSTED. OPS CHECK NORMAL. MDC SHOWED NWS ECU FAIL PRIOR TO RESET. NO FAIL DURING TEST. MOC NOTIFIED 53430 A&P3579452.

Part: WIRE HARNESS — DAMAGED (NLG) · airframe 26,381 hrs · 23,992 cycles

NOSE GEAR DID NOT RETRACT AFTER TAKEOFF, PERFORMED QRH AND RETURNED FOR SUCCESSFUL LANDING. REMOVED AND REPLACED NLG ELECTRICAL HARNESS IAW AMM 32-61-25. OPS TESTED PROXIMITY SENSOR IAW AMM 32-61-00-710-801. NO DEFECTS AT THIS TIME. NOSE GEAR EXTENSION & RETRACTION COMPLETED IAW AMM 32-33-00. NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,366 hrs · 23,975 cycles

LEFT AND RIGHT OVERWING EXIT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-51-04, AND OPS CHECKED GOOD IAW AMM 33-51-04.

Part: ACM — INOPERATIVE (AC BAY) · airframe 26,271 hrs · 23,872 cycles

SMELL COMING FROM BACK OF AIRCRAFT. FOUND IT WAS PACK 2 OVERHEAT 120 C. DEFER RT A/C PACK PER MEL 21-51-01 CAT C. R&R FAN BYPASS CHECK VALVE IAW AMM 21-52-07 DID NOT FIX. R&R ACM IAW AMM 21-51-10. OPS CHECK GOOD IAW AMM 21-51-00 MMO2 UPDATED PLACARD REMOVED.

Part: PBE — UNSERVICEABLE · airframe 25,963 hrs · 23,555 cycles

FD AND ENTRANCE COMPARTMENT PBE'S HAVE BROKEN VACUUM SEALS. REMOVED AND REPLACED FD AND ENTRANCE COMPARTMENT PBE'S P/N'S OFF/ON MR-10047N NSN'S AS REQ'D.

Part: PROXIMITY SWITCH — DEFECTIVE (NLG) · airframe 24,519 hrs · 22,079 cycles

NOSE DOOR OPEN & GEAR DISAGREE MASTER CAUTION MSG AFTER TAKEOFF WHEN PUTTING GEAR UP. SPEED APPROX 160 KTS. R & R CENTERING PROX SWITCH & PROX SWITCH BRACKET IAW AMM 32-61-05 & AMM 32-21-01. R & R NLG HARNESS IAW AMM 32-61-25. SECURED TOW STRAP COLLAR IAW TS 000871R4. SEE CONTINUATION CARDS FOR DETAILS.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 24,359 hrs · 21,914 cycles

CAPTAIN SIDE OXYGEN MASK HAS CONTINUOUS OXYGEN FLOW EVEN WHEN NOT IN EMER SETTING. R & R CAPTAINS SIDE O2 MASK IAW AMM 35-11-1. OPERATIONS CHECKED GOOD. OK FOR SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 24,350 hrs · 21,906 cycles

SERVICE DOOR SILL ANGLE IS CORRODED. R & R SERVICE DOOR SILL ANGLE IAW SRM 51-42-21 & 51-42-06.

Part: SKIN — NOT REPORTED (LT WING) · airframe 24,350 hrs · 21,906 cycles

LEFT WING LOWER PLANK ACCESS HOLE 550BB HAS MULTIPLE INDICATIONS, 80% FULL SCREEN HEIGHT FAILING NDT. REPAIRED LT WING LOWER PLANK ACCESS HOLE 550BB IAW REO 601R-57-21-030 REV L AND 601R-57-21-2428. THIS IS A MAJOR REPAIR.

Part: SKIN — NOT REPORTED (LT WING) · airframe 24,350 hrs · 21,906 cycles

LEFT LOWER WING PLANK ACCESS HOLE 550AB HAS MULTIPLE INDICATIONS, 75% FULL SCREEN HEIGHT FAILING NDT. REPAIRED LT LOWER WING PLANK ACCESS HOLE 550AB IAW REO 601R-57-21-00 REV L & 601R-57-21-2428. THIS IS A MAJOR REPAIR.

Part: BEAM — CORRODED (FUSELAGE) · airframe 24,350 hrs · 21,906 cycles

FS 349 BEAM IS CORRODED, LOCATION IS NEAR RT FLOOR SILL ADJACENT TO SERVICE DOOR. RECEIVED FINAL EA & COMPLIED WITH EA CRJ 253-04116 REV B REPAIRING FS 349, RBL 27 - 42:50. THIS IS A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 24,350 hrs · 21,906 cycles

FOUND CORROSION ON LT FLOOR SUPPORT BEAM AT FS 349, LBL 27 - 36. CONTINUATION CARD 8768311 OP 290. REPAIRED FS 349 FLOOR SUPPORT BEAM IAW EA CRJ253-04123. THIS IS A MAJOR REPAIR.

Part: LATCH — NOT REPORTED (E&E DOOR) · airframe 24,350 hrs · 21,906 cycles

AVI DOOR HANDLE HOUSING HAS AN INDICATION NOTED ALL THE WAY AROUND BASE OF SHAFT 100% FSH. FAILED NDT INSPECTION. MAIN AVIONICS DOOR LATCH WAS REPLACED IAW AMM 52-42-00-400-801, 52-42-03-400-801 & SRM 52-42-00.

Part: RETAINER — CORRODED (WINDOW) · airframe 24,350 hrs · 21,906 cycles

PILOT SIDE WINDOW RETAINER HAS SURFACE CORROSION ALONG LOWER EDGE. REMOVED TAPE AS REQUIRED. R & R PILOT SIDE WINDOW IAW AMM 56-12-01-000 400-801. ASSOCIATED OPERATIONS & LEAK CHECKED GOOD. REF ATTACHED AMM'S FOR WORK PERFORMED.

Part: GUARD — BROKEN (CARGO BAY) · airframe 24,350 hrs · 21,906 cycles

CARGO COMPARTMENT FIRE EXTINGUISHER LINE GUARD BROKEN WITH MISSING HARDWARE. INSTALLED NEW SERVICEABLE CARGO COMPARTMENT FIRE EXTINGUISHING LINE GUARD WITH NEW SERVICEABLE HARDWARE IAW AMM 26-25-07-400-801.

Part: LENS — CRACKED (LT WING) · airframe 24,350 hrs · 21,906 cycles

LEFT WING NAV LIGHT LENS CRACKED. LT NAV LIGHT LENS WAS REPLACED IAW SERVICE LETTER SL0011, AMM 57-30-39-400-801 & TS 000592-2013.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 24,350 hrs · 21,906 cycles

IN PAX COMPARTMENT AT FS 379.00, THE STRINGER 3L IS CRACKED. CONTINUATION CARD 8768311 OP 273. REPAIRED STRINGER 3L IAW SRM 53-00-03 & REO 601R-53-21-2708.

Part: CLEAT — CRACKED (FUSELAGE) · airframe 24,350 hrs · 21,906 cycles

CRACKED CLEAT ON STRINGER 3R, BETWEEN FS 250 & 265. REMOVED & INSTALLED SERVICEABLE CLEAT IAW SRM 51-42-06 & EA CRJ9253-04152.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,350 hrs · 21,906 cycles

CROSS MEMBER IN CARGO BAY FROM FS 574 - 621, HAS A CRACKED CLIP AT FS 621. LOCATED, DRILLED & INSTALLED NEW SERVICEABLE CLIP, PN 601R35050-109, ON THE LOWER SIDE OF THE CARGO BAY CROSS MEMBER AT FS 621.00 IAW SRM 51-42-21.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 24,350 hrs · 21,906 cycles

FORWARD FUSE RT SIDE, FS 319.70 SERVICE DOOR SIDE SILL CLIP CORRODED. R & R SERVICE DOOR SILL BRACKET, PN 601R38335-1S, IAW SRM 51-42-21 & 51-40-11.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 24,350 hrs · 21,906 cycles

IN PAX COMPARTMENT AT FS 282.00, STRINGER 3L IS CRACKED. R & R TWO ANGLES, PN 600-31057-19 & 600-31057-20, AT FS 282, STRINGER 3L IAW SRM 51-40-00, 51-23-00, 51-25-00 & 51-21-11.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 24,350 hrs · 21,906 cycles

FORWARD FUSELAGE FS 280, LBL 9 INBD SUPPORT CLIP CRACKED. R & R SUPPORT CLIP, PN 601R31113-57 IAW SRM 51-42-06, 51-42-21 & 51-40-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 24,350 hrs · 21,906 cycles

FORWARD FUSE, RT SIDE JUST FWD OF SERVICE DOOR FRAME, SILL HAS MINOR CORROSION. SERVICEABLE FWD SERVICE DOOR FRAME SILL WAS REPLACED IAW SRM 51-42-06 & 51-40-11.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 24,310 hrs · 21,873 cycles

CAPTAIN`S LIFE VEST HAS HOLE IN BAG. R & R CAPTAIN`S LIFE VEST IAW AMM 25-61-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,768 hrs · 21,340 cycles

EMERGENCY LIGHT AT SEAT 1C INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-61-04. OPS CHECKED GOOD.

Part: SDU — ABNORMAL · airframe 23,433 hrs · 21,010 cycles

FLAPS FAILED CAUTION MESSAGE WHEN SELECTING FLAPS 20 ON GROUND. PERFORMED TROUBLESHOOTING IAW FIM, REV 44 IAW AD 2009-06-12, PARA (H)(6)(I) AMOC AND PA AD 27-052L. FOUND TO BE CAUSED BY INCORRECTLY RESET SDU. COMPLETED RESET IAW AMM 27-51-15. FLAPS SYS OPS CHECKED GOOD IAW AMM 27-51-05. OK FOR SERVICE.

Part: OXYGEN MASK — OUT OF ADJUST (CABIN) · airframe 22,736 hrs · 20,327 cycles

ON FLIGHT 4015 (YOW - DTW) CREW REPORTED DIFF PRESSURE WARNING AND SOME PAX FELT DIZZY AND LIGHT-HEADED. CREW THEN MANUALLY DEPLOYED O2 MASK BUT SEATS 8A+B O2 MASK DID NOT DEPLOY. INSPECTED AND FOUND 8 AB PASSENGER O2 MASKS NOT PROPERLY PACKAGED CAUSING O2 COMPARTMENT DOOR TO JAM. VERIFIED DOOR LATCH MECHANISM WAS ACTIVATED AT TIME OF DEPLOYMENT. RESET LATCH AND REPACKED MASKS PER CRJ 200 AMM 35-21-09. OPS TEST GOOD OF DOOR LATCH AND PAX O2 SYSTEM PER AMM 35-20-00.

Part: MODULE — MALFUNCTIONED (CABIN PRESSURE) · airframe 22,736 hrs · 20,327 cycles

ON FLIGHT 4015 (YOW TO DTW) CREW REPORTED DIFF PRESS WARNING MSGT CLIMBING THRU 18,000 FT. QRH DIRECTED US TO SET PRESSURE CONTROL TO MANUAL AND ADJUST AS REQUIRED. UNABLE TO GAIN PRESS CNTRL, WE DESCENDED TO 10,000 FT. AFTER REPORTS OF SOME PAX FEELING LIGHT-HEADED MANUALLY DEPLOYED O2 MASKS. DELTA P GOT UP TO 9.4 BRIEFLY. AIRCRAFT DIVERTED TO BUF AND LANDED SAFELY. REMOVED AND REPLACED CABIN PRESSURE ACQUISITION MODULE. OPS CHECK GOOD IAW AMM 21-33-01. REF AML 2398854-2 FOR OSP AND S3 LEAK CHECK/TEST.

Part: FLAP SYSTEM — FAILED · airframe 22,705 hrs · 20,296 cycles

FLIGHT 3728, RECEIVED A FLAPS FAIL AT 0 DEGREE. FLAPS FAILED AT 130 KNOTS AT FLIGHT LEVEL 6,000FT. THE AIRCRAFT LANDED SAFELY. COMPLIED WITH FLAP HEALTH CHECK PE CHECKLIST PROVIDED.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 22,681 hrs · 20,274 cycles

INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED TORN INFANT LIFE VEST IN ACCORDANCE WITH PA 25-096A.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 22,667 hrs · 20,258 cycles

ON FLIGHT 4243 (BUF TO DTW) ON APPROACH INTO DTW AT 195 KNOTS FLAPS WERE SELECTED TO 20 DEGREES AND RECEIVED FLAPS FAILED MESSAGE AT 0 DEGREES. QRH COMPLETED WITH NORMAL LANDING AT FLAPS 0 DEGREES. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD 2009-06-12 PARAGRAH (H)(HG)(I), AMOC DATED DECEMBER 07,2012 AND PA AD 27-052J. COMPLIED WITH CRJ200 HEALTH CHECK IAW CHECKLIST PROVIDED. SEE NON-ROUTINE WORKCARD N38985 FOR COMPONENT REPLACEMENT AND FURTHER DETAILS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,386 hrs · 19,972 cycles

LEFT EMERGENCY LIGHT IS INOPERABLE. REMOVED AND REPLACED NR 2 BATTERY PACK IAW AMM 33-51-05. OPS CHECKS GOOD THIS CLEARS DM 74577. PLACARD REMOVED OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,385 hrs · 19,969 cycles

FORWARD OVERHEAD EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED EMERGENCY LIGHT BULB. OPS CHECK CLEARS DM.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 22,299 hrs · 19,884 cycles

FLIGHT ATTENDANT FLASHLIGHT NOT SHOWING FLASHING CHARGE LIGHT. REMOVED AND REPLACED FLIGHT ATTENDANTS FLASHLIGHT. DEFER CLEARED.

Part: LIGHT — UNKNOWN (CABIN) · airframe 22,221 hrs · 19,813 cycles

EMERGENCY FLOOR TRACK LIGHTS. REMOVED FROM MID CABIN TO AFT OF AIRCRAFT.

Part: CONTAINER — TORN (PBE) · airframe 22,126 hrs · 19,718 cycles

CAPTAIN'S PBE BAG IS TORN. REMOVED AND REPLACED FLIGHT DECK PBE BAG IAW AMM 25-61-00. OK FOR SERVICE.

Part: WIRE — SHORTED (EMERGENCY LIGHT) · airframe 21,989 hrs · 19,590 cycles

CREW REPORTED THAT OVERHEAD EXIT SIGN FACING THE FORWARD CENTER AISLE WAS INOPERATIVE. UPON INSPECTION, MAINTENANCE FOUND AND REPAIRED SHORTED WIRE AT FLIGHT ATTENDANT STATION. EMERGENCY LIGHTING OPS CHECK GOOD IAW 33-51-00.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 21,415 hrs · 19,027 cycles

ONE INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED 1 VEST IAW PA 25-096A.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 21,415 hrs · 19,027 cycles

CAPT & F/O LIFE VESTS BAGS TORN. REMOVED ADN REPLACED CAPT & F/O VESTS IAW AMM 25-61-03.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 21,008 hrs · 18,644 cycles

GEAR DISAGREE WARNING MESSAGE WHEN EXTENDING GEAR ON FINAL. HAD TO USE THE LANDING GEAR MANUAL RELEASE HANDLE TO MAKE THE GEAR SHOW 3-GREEN DOWN AND LOCKED. R & R MAIN LANDING GEAR SELECTOR VALVE IAW AMM 32-32-10. OPS CHECK IAW AMM 32-30-00. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 20,964 hrs · 18,600 cycles

GEAR DISAGREE ON FINAL INTO JFK. REPLACED MLG SELECTOR VALVE IAW AMM OPS CHECK GOOD.

Part: FLEX DRIVE — DAMAGED (TE FLAP) · airframe 20,874 hrs · 18,514 cycles

FLAP FAIL CAUTION MSG AT 0 DEG ON APPROACH. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I) AMOC DATED MARCH 27, 2009, TR #27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD 27-052G. FOUND LT NR 3 FLEX SHAFT AND RT NR 4 FLEX SHAFT DAMAGED.

Part: FLEX DRIVE — DIRTY (TE FLAP) · airframe 20,811 hrs · 18,446 cycles

ON APPROACH INTO DTW FLAPS FAIL HAPPENED AT 0 DEGREES WHEN TRYING TO SELECT TO 20 DEGREES. JAM CODES HAVE BEEN DOCUMENTED AND SENT TO MOTOR GROUP AIRSPEED 190 KTS. PERFORMED FLAP FLEX SHAFT CLEAN & LUBE IAW FLAP LUBE CHECKLIST. OK FOR SERVICE, OP CHECK GOOD.

Part: FLAP — FAILED (WING) · airframe 20,811 hrs · 18,446 cycles

8683B FLT 4185-02 ORF-DTW ON APPROACH INTO DTW FLAPS FAIL HAPPENED AT 0 DEGREES WHEN TRYING TO SELECT TO 20 DEGREES. JAM CODES HAVE BEEN DOCUMENTED AND SENT TO MOTOR GROUP AIRSPEED 190 KTS. APPROXIMATE TIME INTO FLIGHT 1 HR 30 MINS 19 DEGREES.

Part: WINDOW — BROKEN (COCKPIT) · airframe 19,700 hrs · 17,447 cycles

RIGHT SIDE WINDOW SHATTERED ON INSIDE DURING CLIMBOUT AT APROX 18,500. EMERGENCY DECLARED. FLIGHT DIVERTED TO DTW FOR UNSCHEDULED LANDING. MAINTENANCE REMOVED AND REPLACED RT SIDE WINDOW IAW AMM 56-12-01. OPC GOOD, A/C OK FOR SVC.

Part: WARNING SYSTEM — ACTIVATED (LAVATORY) · airframe 19,021 hrs · 16,784 cycles

SMOKE IN LAV MSG. EMERGENCY DECLARED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 8,937 hrs · 16,699 cycles

FS 559.00 BULKHEAD WEB FOUND CRACKED AND REQUIRES REPAIR. REPAIRED FS 559.00 BULKHEAD WEB LAW BOMBARDIER REO 601R-53-41-260 REV E AND BOMBARDIER REO 601 R-53-41-609 REV B, DEVIATION E.

Part: SERVICE DOOR — DAMAGED (AFT LAVATORY) · airframe 18,415 hrs · 16,202 cycles

AFT LAVATORY SERVICE DOOR PANEL 196AR AFT EDGE WAS FOUND WITH IMPACT DAMAGE. THE DAMAGE IS LOCATED 0.75 INCH ABOVE THE LOWER DOOR LATCH AND MEASURES 1.5 INCHES ALONG THE AFT EDGE AND 0.50 INCH WIDTH. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-247, REPEAT INSPECTIONS EVERY 500 FLIGHT HOURS. AT THE NEXT C CHECK NOT TO EXCEED 5,000 FLIGHT HOURS, ACCOMPLISH A PERMANENT REPAIR IN ACCORDANCE WITH SRM 51-74-10.

Part: ACTUATOR — FAILED (TE FLAPS)

FLAP FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RAI FLAP ACTUATOR IAW AMM 27-53-01.

Part: ACTUATOR — FAILED (TE FLAPS)

FLAP FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RAI FLAP ACTUATOR IAW AMM 27-53-01.

Part: ACTUATOR — FAILED (TE FLAPS)

FLAP FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RAI FLAP ACTUATOR IAW AMM 27-53-01.

Part: ACTUATOR — FAILED (TE FLAPS)

FLAP FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RAI FLAP ACTUATOR IAW AMM 27-53-01.

Part: ACTUATOR — FAILED (TE FLAPS)

FLAP FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RAI FLAP ACTUATOR IAW AMM 27-53-01.

Part: ACTUATOR — FAILED (TE FLAPS)

FLAP FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RAI FLAP ACTUATOR IAW AMM 27-53-01.

Part: ACTUATOR — FAILED (TE FLAPS)

FLAP FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RAI FLAP ACTUATOR IAW AMM 27-53-01.

Part: ACTUATOR — FAILED (TE FLAPS)

FLAP FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RAI FLAP ACTUATOR IAW AMM 27-53-01.

Part: DOOR — STUCK (EMERGENCY EXIT) · airframe 10,702 hrs · 9,298 cycles

RIGHT SIDE EMERGENCY OVERWING EXIT JAMMED. OPERATIONALLY CHECKED GOOD RIGHT SIDE OVERWING EXIT IAW AIRCRAFT MAINTENANCE MANUAL (AMM) 52-20-00.

Part: G SWITCH — FAILED (ELT) · airframe 7,000 hrs · 6,276 cycles

ELT FAILS G-SWITCH TEST. REMOVED IN ACCORDANCE WITH PA 25-048D AND FAR 91.207 FOR REPAIR. UNIT MUST BE REPAIRED AND REINSTALLED WITHIN 90 DAYS. REMOVED ELT FOR MAINTENANCE IN ACCORDANCE WITH FAR 91.207.