N8918B

Part: FRAME — CORRODED · airframe 32,579 hrs · 31,171 cycles

FRAME 574 CORRODED AT STGR 27 REMOVED FRAME SECTOR FROM STRGR 20L TO 20R AT FS 574 IAW CRJ-200 SRM 51-42-06. INSTALLED NEW SERVICABLE FRAME SECTOR 574 FROM STRGR 20L TO 20R IAW CRJ-200 SRM 51-42-06 AND 51-42-21

Part: FRAME — CORRODED · airframe 32,579 hrs · 31,171 cycles

FRAME AT FS 409+16 IS CORRODED BETWEEN STGR 25L AND 25R. REPAIRED FUSELAGE FRAME 409+16 FRON STGR 25L TO STGR 25R IAW CRJ 200 SRM 53-00-15-02 REPAIR NO.1.

Part: STRINGER — CRACKED · airframe 32,579 hrs · 31,171 cycles

STGR 3L AT FS 379.00 IS CRACKED. COMPLIED WITH ENDEAVOR EA CRJ253-14362 REV B DATED 08/18/2022.

Part: SKIN — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR INNER SKIN IS CORRODED. INSTALLED PAX DOOR INNER SKIN IAW CRJ200 SRM 51-42-06, SRM 51-42-13, SRM 51-42-22.

Part: NONE — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR, ANGLE “C” AFT CLIP IS CORRODED. LOCATED AND DRILLED PAX DOOR NEW C ANGLE AFT CLIP P/N 601R318058-1 IAW CRJ 200 SRM 51-40-11, INSTALLED NEW C AFT CLIP IAW CRJ 200 SRM 51-42-06 AND 51-42-21

Part: BRACKET — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR, BRACKET OF DD6 FWD IS CORRODED. INSTALLED NEW FWD BRACKET P/N 601R318084-1 IAW CRJ 200 SRM 51-42-06

Part: INTERCOSTAL — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR, INTERCOSTAL OF DD7 FWD IS CORRODED. INSTALLED NEW INTERCOSTAL P/N 601R318826-1 IAW CRJ 200 SRM 51-42-06

Part: WEB — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR FWD WEB CORRODED LOCATED AND DRILLED NEW PAX DOOR FWD WEB P\N 601R317071-12 IAW CRJ 200 SRM 51-40-11, INSTALLED ATTACHING ANGLES ON FWD WEB IAW CRJ 200 SRM 51-42-06. REFERENCE JOB 81513641 OP 242 FOR INSTALLATION OF PAX DOOR FWD WEB

Part: INTERCOSTAL — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR, INTERCOSTAL OF DD6 FWD IS CORRODED. INSTALLED NEW FWD DD6 INTERCOSTAL P/N 601R31902-485 CRJ 200 SRM 51-42-06

Part: INTERCOSTAL — CRACKED · airframe 32,579 hrs · 31,171 cycles

INTERCOSTAL DD1 AT AFT SIDE FOUND TO BE CRACKED LOCATED AND DRILLED NEW PAX DOOR AFT DD1 INTERCOSTAL P/N 601R31902-318 IAW CRJ 200 SRM 51-40-11, INSTALLED NEW INTERCOSTAL IAW CRJ 200 SRM 51-42-06

Part: BRACKET — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR, BRACKET OF DD7 FWD IS CORRODED. INSTALLED NEW BRACKET P/N 601R318824-1 IAW CRJ 200 SRM 51-42-06

Part: CLEAT — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR, FS 320, HINGE SIDE, FWD CLEAT IS CORRODED. LOCATED AND DRILLED NEW CLEAT P/N 601R319034-1 IAW CRJ 200 SRM 51-40-11, INSTALLED NEW CLEAT IAW CRJ 200 SRM 51-42-06

Part: INTERCOSTAL — CORRODED · airframe 32,579 hrs · 31,171 cycles

INTERCOSTAL DD3 AFT IS CORRODED. LOCATED AND DRILLED NEW PAX DOOR AFT INTERCOSTAL DD3 P/N 601R318055-1IAW CRJ 200 SRM 51-40-11, INSTALLED NEW INTERCOSTAL IAW CRJ 200 SRM 51-42-06

Part: ANGLE — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR, ANGLE “C” IS CORRODED LOCATED AND DRILLED NEW PAX DOOR C ANGLE P/N 601R317052-1 IAW CRJ200 SRM 51-40-11 ,INSTALLED NEW C ANGLE IAW CRJ200 SRM 51-42- 21

Part: ANGLE — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR, ANGLE “C” FWD CLIP IS CORRODED. LOCATED AND DRILLED PAX DOOR C ANGLE FWD CLIP P/N 601R318058-1IAW CRJ 200 SRM 51-40-11, INSTALLED C ANGLE FWD CLIP IAW CRJ 200 SRM 51-42-06 AND 51-42 -21

Part: DOUBLER — CORRODED · airframe 32,579 hrs · 31,171 cycles

FS 338 DOUBLER, PULL IN CAM IS CRACKED REMOVED AND INSTALLED NEW SERVICEABLE DOUBLER P/N 601R318094-2 IAW CRJ -200 SRM 51-42-21-001-001-A01

Part: INTERCOSTAL — CORRODED · airframe 32,579 hrs · 31,171 cycles

INTERCOSTAL DD4 AFT IS CORRODED. LOCATED AND DRILLED NEW PAX DOOR AFT INTERCOSTAL P/N 601R31902-317A IAW CRJ 200 SRM 51-40-11, INSTALLED NEW INTERCOSTAL IAW CRJ 200 SRM 51-42-06

Part: INTERCOSTAL — CORRODED · airframe 32,579 hrs · 31,171 cycles

INTERCOSTAL DD7 AFT IS CORRODED. LOCATED AND DRILLED NEW INTERCOSTAL P/N 601R318825-1 IAW CRJ 200 SRM 51-40-11, INSTALLED NEW INTERCOSTAL IAW CRJ 200 SRM 51-42-11

Part: INTERCOSTAL — CORRODED · airframe 32,579 hrs · 31,171 cycles

INTERCOSTAL AT DD4 MID IS CORRODED. REPLACED INTERCOSTAL P/N 601R318081-1 DD4 IAW CRJ-200 SRM 51-42-06 AND 51-42-21.

Part: FORMER — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR AFT FORMER HAS MINOR CORROSION REPLACED PAX DOOR AFT FORMER PN 601R318034-5 IAW CRJ 200 SRM 51-40-11, 51-42-06 AND 51-42-21

Part: FORMER — CORRODED · airframe 32,579 hrs · 31,171 cycles

FORMER AT FS 309.00 BETWEEN DD4 AND DD5 IS CORRODED.( AFTER FURTHER INVESTIGATION THE CORRECT LOCATION FOR DEFECTIVE FORMER IS FS 313.00) REPLACED PAX DOOR FORMER P/N 601R318086-1 IAW CRJ 200 SRM 51-42-06 AND 51-40-11

Part: FRAME — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR FRAME AT FS 329 BETWEEN DD5 AND DD6 IS CORRODED REPLACED 329 STUB FRAME PN#601R318078-3 IAW CRJ 200 SRM 51-40-11 AND 51-42-06.

Part: INTERCOSTAL — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR INTERCOSTAL DD2 IS CORRODED REPLACED 601R318053-3 INTERCOSTAL DD2 MID IAW CRJ-200 SRM 51-42-06 AND 51-42-21.

Part: INTERCOSTAL — CORRODED · airframe 32,579 hrs · 31,171 cycles

INTERCOSTAL AT DD2 FWD IS CORRODED. REPLACED PAX DOOR DD2 INTERCOSTAL PN 601R318051-1 IAW CRJ-200 SRM 51-42-06 AND 51-41-11

Part: FRAME — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR FRAME AT 338.9 IS CORRODED BETWEEN DD5 AND DD6. (UPON FURTHER INVESTIGATION, DISCREPANT FRAME LOCATION IS FS 318) REPLACED PAX DOOR FS318 SUB FRAME P/N 601R318038-3 IAW CRJ-200 SRM 51-40-11, 51-42-06, AND 51-42-21

Part: FORMER — CORRODED · airframe 32,579 hrs · 31,171 cycles

FORMER AT FS 311.25 FWD IS CORRODED. REPLACED PAX DOOR FWD FORMER P/N 601R318031-5 AT FS 311.00 IAW CRJ200 SRM 51-42-06 AND 51-42-21

Part: CLEAT — CORRODED · airframe 32,579 hrs · 31,171 cycles

CORRODED CLEAT ON FS329, NEEDS REPLACED NO ALLOWABLE LIMITS. REPLACED FS329 CLEAT P/N 600-31902-269 IAW CRJ-200 SRM 51-42-06 AND 51-40-11.

Part: INTERCOSTAL — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR, INTERCOSTAL (DOOR DATUM 6) CORRODED ACROSS SPAN. NTERCOSTAL DD6 IS OUT OF LIMITS. NO LIMITATIONS NOTED IN SRM. REMOVED & INSTALLED INTERCOSTAL DD6 IAW CRJ-200 SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED INTERCOSTAL P/N 601R318057-1 AND CLEAT P/N 600-31902-269 IAW CRJ-200 SRM 51-40-11.

Part: INTERCOSTAL — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR INTERCOSTAL DD5 IS CORRODED. PAX DOOR INTERCOSTAL DD5 IS OUT OF LIMITS WITH NO LIMITATIONS IN SRM. LOCATED AND DRILLED NEW ATTACH BRACKET P/N: 601R318084-2 AND NEW DD5 INTERCOSTAL P/N: 601R31902-317A IAW CRJ 200 SRM 51-40-11. REMOVED& INSTALLED NEW PAX DOOR INTERCOSTAL DD5 P/N 601R31902-317A IAW CRJ 200 SRM 51-42-06. REMOVED & INSTALLED NEW ATTACHING BRACKET P/N 601R318084-2 IAW CRJ 200 SRM 51-42-06.

Part: NONE — CRACKED · airframe 32,579 hrs · 31,171 cycles

"FOUND CRACK AT EXISTING COCKPIT FLOOR BEAM REPAIR AT LBL 12 AND F.S280 " REPAIRED IAW CRJ-900 SRM 51-40-11-001-001-A01

Part: FRAME — CORRODED · airframe 32,579 hrs · 31,171 cycles

FRAME AT F.S.319.00 IS CORRODED BETWEEN STRINGER 21L TO STRINGER 18L REMOVED AND REPLACED FRAME SECTOR AT F.S.319

Part: FRAME — CORRODED · airframe 32,579 hrs · 31,171 cycles

FRAME AT F.S.319.00 IS CORRODED BETWEEN STRINGER 25L AND 24R REMOVED AND REPLACED FRAME SECTOR AT F.S.319

Part: SEAT TRACK — CORRODED · airframe 32,579 hrs · 31,171 cycles

FLOOR SEAT TRACK AT RBL9 BETWEEN FS 364.00 AND FS 394.00 IS CORRODED. REMOVED FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 364.00 AND FS 394.00 IAW CRJ200 SRM 51-41-02. INSTALLED NEW SERVICEABLE FLOOR SEAT TRACK AT RBL9 BETWEEN FS364.00 AND FS 394.00 IAW CRJ 200 SRM 51-41-02

Part: SEAT TRACK — CORRODED · airframe 32,579 hrs · 31,171 cycles

FLOOR SEAT TRACK AT LBL9 BETWEEN FS 364.00 AND FS 394.00 IS CORRODED. REMOVED FLOOR SEAT TRACK AT LBL 9 BETWEEN FS 364.00 AND FS 394.00 IAW CRJ200 SRM 51-41-02. INSTALLED NEW SERVICEABLE FLOOR SEAT TRACK AT LBL9 BETWEEN FS364.00 AND FS 394.00 IAW CRJ 200 SRM 51-41-02

Part: STEP — CORRODED · airframe 32,579 hrs · 31,171 cycles

PAX DOOR BOTTOM STEP IS CORRODED @ NUT PLATE LOCATIONS REPAIRED PAX DOOR BOTTOM STEP IAW EA:CRJ252-14514 REV:IR DATED 09/09/2022 AND EA: CRJ252-14515 REV IR DATED 09/09/2022.

Part: WIRE — DETACHED · airframe 32,328 hrs · 30,861 cycles

EMERGENCY EXIT SIGN BY MAIN CABIN DOOR IS NOT ILLUMINATING FOUND WIRE PULLED OUT OF PLUG SPLICE ON WIRING BEHIND EXIT SIGN. REPAIRED AND PINNED WIRE PER CRJ200 ESPM 20-17-31. OPS CHECK GOOD

Part: WIRE — DAMAGED · airframe 31,594 hrs · 29,938 cycles

"EMERGENCY EXIT LIGHT AT AIR STAIRS FOUND INOP ON FLIRST FLIGHT OF DAY CHECK. INSPECTED WIRING BEHIND THE BULKHEAD FOUND DAMAGED WIRING DEFERRED CABIN EMERGENCY LIGHT IAW MEL 33-51-1A PLACARD INSTALLED MMO2 UPDATED AND MOC NOTIFIED #103005 REPAIRED WIRING EMERGENCY LTS TEST OK IAW AMM 33-51-00 REMOVED PLACARD CLEARED MMO2 MXC NOTIFIED #43294

Part: FEEDER CABLE — BROKEN (EMERGENCY LIGHT) · airframe 29,945 hrs · 27,869 cycles

EMERGENCY FLOOR TRACK LIGHTING IS OUT BETWEEN ROWS 6-8. FOUND A BROKEN CABLE AT ROW 8. REMOVED AND REPLACED CABLE, IAW CRJ 200 AMM 33-51-01 AND ESPM 20-17-31. OPS TEST GOOD. P/N OFF/ON: 5946-5.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 27,943 hrs · 25,720 cycles

L/H SEAT RAIL #2 HAS CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED L/H # 2 SEATRAIL IAW CRJ 200 AMM 53-01-11 AAR SM 107

Part: RETAINER — LOOSE (LT SPOILER) · airframe 27,943 hrs · 25,720 cycles

LEFT WING FLIGHT SPOILER I/B METAL RETAINER IS LOOSE. REMOVED AND REPLACED WITH NEW RETAINER I.A.W. CRJ-200 SRM 51-42-06 AND CRJ-200 SRM 51-42-21 AAR SM 58

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 27,943 hrs · 25,720 cycles

RH WING AUX SPAR DRAG ANGLE AT WS47.61 CRACKED. REMOVED AND REPLACED R/H WING AUX SPAR DRAG ANGLE AT WS 47.61 IAW CRJ 200 SRM 51-42-21 AAR SM 107

Part: SUPPORT ANGLE — CRACKED (LT PYLON) · airframe 27,943 hrs · 25,720 cycles

LH PYLON LWR FWD ACCESS PANEL SUPPORT ANGLE CRACKED. REPAIRED CRACKED SUPPORT ANGLE ON L/H PYLON LOWER FED ACCESS PANEL IAW EA CRJ 254-08800 AAR SM 33

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 27,943 hrs · 25,720 cycles

FWD EQUIP COMPARTMENT DECK WEB CRACKED @ LH SIDE FS193. REPAIRED IAW REO 601R-53-11-081.

Part: STRAP — CORRODED (BS 559) · airframe 27,943 hrs · 25,720 cycles

FLOOR STRAP AT FS 559 HAS CORROSION BETWEEN LBL 27 AND THE LH FLOOR SILL, IN THE CABIN. REMOVED CORROSION ON FLOOR STRAP AT FS 559 LBL 27 AND L/H FLOOR SILL FOUND TO BE OUT OF LIMITS IAW CRJ 200 SRM 53-00-00 REMOVED AND REPLACED IAW CRJ 200 SRM 51-42-06 AAR SM 107

Part: RETAINER — CRACKED · airframe 27,943 hrs · 25,720 cycles

WHILE REMOVING RTV ON PNL 412AT FOUND THE PNL TO BE CRACKED. REMOVED AND REPLACED WITH NEW RETAINER IAW CRJ 200 SRM 51-42-06 AAR SM 58

Part: FLOOR SUPPORT — CORRODED (BS 574-610) · airframe 27,943 hrs · 25,720 cycles

FLOOR BEAM LBL 9 O/B PANEL LANDING HAS CORROSION SPOTS BETWEEN FS 574 THRU FS 621, IN THE CARGO BAY. REMOVED AND REPLACED FLOOR BEAM CAP IAW CRJ 200 SRM 51-42-21 51-42-2 AAR SM 17

Part: SEAT TRACK — CORRODED (BS 559) · airframe 27,943 hrs · 25,720 cycles

LH AISLE SEAT TRACK STICK 4 HAS CORROSION SPOTS BETWEEN FS 559 THRU FS 559+80, IN THE CABIN. REMOVED DAMAGE FROM L/H SIDE ISLE SEAT TRACK FS559-559+80 FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11 SRM 51-21-06 + SRM 53-21-49 ORIG T .105" REMAILING T-.077" LOSS -.028 AAR SM 33

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 27,943 hrs · 25,720 cycles

SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REMOVED DAMAGE FROM LBL9 FS 559+112 - FS 574 SEAT TRACK FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED SEATTRACK IAW AMM 53-01-11 SRM 51-21-06 AND SRM 53-21-49 ORIG T .260" REMAINING T .236 LOSS - .024" AAR SM 33

Part: SEAT TRACK — CORRODED (559) · airframe 27,943 hrs · 25,720 cycles

SEAT TRACK ON TOP OF LBL 27 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED DAMAGE FROM SEAT TRACK LBL27 FS 559+80 TO FS 559+96 FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11 SRM 51-21-06 AND SRM 53-21-49 ORIG 7 -.260" REMAINING 7-.239" LOSS - .021 AAR SM 33

Part: SEAT TRACK — CORRODED (BS 409) · airframe 27,943 hrs · 25,720 cycles

L/H SEAT RAIL #4 HAS CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED L/H # 4 SEATRAIL IAW CRJ 200 AMM 53-01-11 AAR SM 107

Part: SEAT TRACK — CORRODED (BS 409) · airframe 27,943 hrs · 25,720 cycles

L/H SEAT RAIL #3 HAS CORROSION IN SEVERAL AREAS REMOVED AND REPLACED L/H # 3 SEATRAIL IAW CRJ 200 AMM 53-01-11 AAR SM 107

Part: SEAT TRACK — CORRODED (BS 605-621) · airframe 27,943 hrs · 25,720 cycles

SEAT TRACK ON TOP OF LBL 9 HAS CORROSION JUST FWD OF FS 621, IN THE CARGO BAY. REMOVED DAMAGE FROM SEAT TRACK LBL9 FSC21. FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11, SRM 51-21-06, & SRM 53-21-49ORIG T. 105" REMAINING T-P77", LOSS -.028 AAR SM 33

Part: SEAT TRACK — CORRODED (BS 554-559) · airframe 27,943 hrs · 25,720 cycles

R/H SEAT RAIL #7 HAS CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED R/H # 7SEATRAIL IAW CRJ 200 AMM 53-01-11 AAR SM 33

Part: SEAT TRACK — CORRODED (BS 554-559) · airframe 27,943 hrs · 25,720 cycles

L/H SEAT RAIL #7 HAS CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED L/H # 7 SEAT RAIL IAW CRJ 200 AMM 53-01-11 AAR AP 189

Part: SEAT TRACK — CORRODED (BS 405-409) · airframe 27,943 hrs · 25,720 cycles

L/H SEAT TRACK #2 CORRODED IN MULTIPLE LOCATIONS. REMOVED AND REPLACED L/H # 2 SEATRAIL IAW CRJ 200 AMM 53-01-11-04 AAR AP 189

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 27,943 hrs · 25,720 cycles

RIGHT SIDE, AISLE SEAT TRACK, TRACK 3, HAS CORROSION. REMOVED CORROSION ON R/H FLOOR SEAT TRACK # 3 FOUND TO BE OUT OF LIMIT REMOVED CORRDED SEAT TRACK AND INSTALLED NEW FLOOR SEAT TRACK # 3 IAW CRJ 300 SRM 51-21-06 53-41-49 BA DWG 56487 REV A CRJ 200 AMM 53-01-11

Part: FLOORBEAM — CORRODED (BS 349) · airframe 27,943 hrs · 25,720 cycles

FLOORBEAM AT BS 349, RBL 32 - RBL 38 WAS CORRODED, FOUND OUT OF SRM LIMITS. REPAIRED THE FLOORBEAM IAW EA CRJ253-08784.

Part: FLOOR SUPPORT — CORRODED (BS 621-674) · airframe 27,943 hrs · 25,720 cycles

FLOOR SUPPORT LBL 27, INBD AND OTBD PANEL LANDINGS HAD CORRODED SPOTS BETWEEN FS 574 THRU FS 621, IN THE THE CARGO BAY. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-21 AND 51-42-22.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 27,943 hrs · 25,720 cycles

FLOOR BEAM SUPPORT ANGLE CRACKED AT FS280.00 LBL9 OTBD. REMOVED CRACKED FLOOR BEAM SUPPORT ANGLE AT F.S. 280, LBL 9 OTBD. FABRICATED AND INSTALLED NEW ANGLE I.A.W. CRJ-200 SRM 51-24-16, SRM 51-24-36, SRM 51-42-21 AND TR 51-42.

Part: SEAT TRACK — CORRODED (BS 449-541) · airframe 27,943 hrs · 25,720 cycles

RIGHT SIDE, SIDE (DADO) SEAT TRACK, STICK 6 HAS CORROSION. REMOVED AND REPLACED R/H #6. SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 27,943 hrs · 25,720 cycles

RIGHT SIDE, SIDE (DADO) SEAT TRACK, STICK 3 HAS CORROSION. REMOVED AND REPLACED R/H #3 SEAT RAIL IAW SRM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 449) · airframe 27,943 hrs · 25,720 cycles

R/H SEAT RAIL #5 HAS CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED R/H #5 SEAT RAIL. I.A.W. CRJ-200 AMM 53-01-11 AAR SM 33

Part: SEAT TRACK — CORRODED (BS 409) · airframe 27,943 hrs · 25,720 cycles

RIGHT SIDE, SIDE (DADO) SEAT TRACK, STICK 4 HAS CORROSION. REMOVED AND REPLACED #4 R/H SEAT RAIL I.A.W. CRJ-200 AMM 53-01-11 AAR SM 33

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 27,943 hrs · 25,720 cycles

FLT CONTROL CABLE FAIRLEAD SUPPORT INTERCOSTAL AT FS484.00 BTWN LBL27 AND LBL37 INBD ATTACH ANGLE CRACKED. REMOVED AND REPLACED ATTACH ANGLE ON SUPPORT INTERCOSTAL AT LBL27, F.S. 484.00 I.A.W. CRJ-200 SRM 51-42-06 AND SRM 51-42-21 AAR SM 107

Part: BULKHEAD WEB — CHAFED (BS 621) · airframe 27,943 hrs · 25,720 cycles

AFT PRESSURE BULKHEAD FWD FACE IS CHAFED AT SEVERAL AREAS. REMOVED THE CHAFE ON THE AFT PRESSURE BULKHEAD FWD FACE, FOUND WITHIN LIMITS. IAW REO 601R-53-61-2155.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 27,943 hrs · 25,720 cycles

FLOOR BEAM CLIP IS CRACKED AT FS484.00 AND RBL36. REMOVED FLOOR BEAM CLIP- FABRICATED AND INSTALLED NEW CLIP I.A.W. REO 601R-53-41-059.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 27,943 hrs · 25,720 cycles

FLT CONTROL CABLE FAIRLEAD SUPPORT INTERCOSTAL AT FS484.00 BTWN LBL27 AND LBL37 OTBD ATTACH ANGLE CRACKED. REPAIRED SUPPORT INTERCOSTAL AT LBL 37, F.S. 484 I.A.W. REO 601R-53-41-059 AND EA NO.CRJ 253-08647 AAR SM 107

Part: FLOORBEAM — CRACKED (BS 484) · airframe 27,943 hrs · 25,720 cycles

FLOOR BEAM CLIP IS CRACKED AT FS484.00 AND RBL27. REMOVED AND REPLACED FLOOR BEAM CLIP AT RBL 27, F.S. 484 I.A.W. CRJ-200 SRM 51-42-06 AND SRM 51-42-21 AAR SM 107

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 27,943 hrs · 25,720 cycles

L/H WING DRY BAY ACCESS PANEL 540CT LANDING HAS CORROSION AND A SCRATCH. REMOVED CORROSION I.A.W. CRJ-200 SRM 51-21-16 AND REMOVED SCRATCH I.A.W. CRJ-200 SRM TR #51-44, FOUND TO BE WITHIN LIMITS I.A.W. BOMBARDIER DRAWING TOLERANCE DWG NO. 601R10042 VIEW R SHEET 2 (.206" MIN REMAINING - DWG TOLERANCE MIN THICKNESS .195-.205" AAR SM 39

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · airframe 27,943 hrs · 25,720 cycles

RH FLOOR SILL HAS CORROSION SPOTS AT THE TOP AND BOTTOM SIDE BETWEEN FS 559+80 THRU FS 574, IN THE CARGO BAY. REMOVED AND REPLACED CORRODED SILL IAW CRJ 200 SRM 51-42-06 51-42-21 AND EA CRJ 253-08667 PERFORMED LAV FILL CHECK IAW CRJ 200 AMM 38-31-00-790-801 (ITEM 16 IN WIP) LEAK CHECK GOOD AAR SM 139

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 27,943 hrs · 25,720 cycles

L/H WING DRY BAY ACCESS PANEL 540BT LANDING HAS CORROSION. REMOVED CORROSION I.A.W. CRJ-200 SRM 51-21-06 AND FOUND TO BE WITHIN LIMITS I.A.W. DRAWING TOLERANCE DWG NO. 601R10042 VIEW P SHEET 2 ( .202" MIN REMAINING- DWG TOLERANCE .195"-.205" ).

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 27,943 hrs · 25,720 cycles

L/H WING DRY BAY ACCESS PANEL 540AT LANDING HAS CORROSION. REMOVED CORROSION I.A.W. CRJ-200 SRM 51-21-06 AND FOUND TO BE WITHIN LIMITS I.A.W. DRAWING TOLERANCE DWG NO. 601R10042 VIEW P SHEET 2 (.204" MIN REMAINING-DWG TOLERANCE ( .195"- .205").

Part: MOUNT FITTING — GOUGED (NR 1 ENGINE) · airframe 27,943 hrs · 25,720 cycles

NR 1 ENG FWD MOUNT, AFT UPPER FITTING HAD TWO NICKS. COMPLIED WITH REO 601R-54-51-196, REMOVED THE NICK DAMAGE BY BLENDOUT, ROTOPEENED AND RESTORE FINISH.

Part: SEAT TRACK — CORRODED (BS 449) · airframe 27,943 hrs · 25,720 cycles

L/H SEAT RAIL #5 HAS CORROSION IN SEVERAL AREAS. REMOVED UNSERVICEABLE THE LT SEAT TRACK #5, AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 27,943 hrs · 25,720 cycles

SEAT TRACK ON TOP OF RBL 27 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 27,943 hrs · 25,720 cycles

RIGHT SIDE AISLE SEAT TRACK NR 1 HAD CORROSION. REMOVED CORROSION IAW SRM 51-21-06, FOUND OUT OF LIMITS. IAW SRM 53-21-49. REMOVED AND REPLACED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 430-550) · airframe 27,943 hrs · 25,720 cycles

LT SEAT TRACK SCRATCHED BS 550 AND 430. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: STRAP — CORRODED (BS 559) · airframe 27,943 hrs · 25,720 cycles

FLOOR STRAP AT BS 559 HAD CORROSION BETWEEN RBL 27 AND THE RT FLOOR SUPPORT, IN THE CABIN. REMOVED AND REPLACED THE FLOOR STRAP IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 27,943 hrs · 25,720 cycles

L/H SEAT TRACK NR 6 HAS CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 27,943 hrs · 25,720 cycles

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

Part: SEAT TRACK — CORRODED (CABIN) · airframe 27,943 hrs · 25,720 cycles

RIGHT SIDE, AISLE SEAT TRACK 4 HAD CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: FITTING — CRACKED (BS 461) · airframe 27,943 hrs · 25,720 cycles

BATHTUB FITTING AT BS 461 AND RBL9 WAS CRACKED. REPLACED THE BATHTUB FITTING IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 27,943 hrs · 25,720 cycles

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

Part: ACCESS PANEL — CHAFED · airframe 27,943 hrs · 25,720 cycles

L/H NOSE ACCESS COWL 432AB HAS AFT TRAILING EDGE CHAFED. REMOVED AND REPLACED WITH NEW TRAILING EDGE AFT OF L/H NOSE ACCESS COWL 432AB IAW CMM 71-14-01.

Part: COVER — CRACKED (APU ENCLOSURE) · airframe 27,943 hrs · 25,720 cycles

APU ENCLOSURE COVER IS CRACKED AT TOP CENTER. WELDED PERMANENT REPAIR TO APU ENCLOSURE COVER CRACK AT TOP CENTER IAW BOMBARDIER REO 601R-49-11-070 REV "B" AAR CP 17

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 27,943 hrs · 25,720 cycles

LEFT WING LEADING EDGE, INBOARD ATTACH ANGLE, ON FRONT SPAR IS CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-41-02 AND 51-41-04.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 27,943 hrs · 25,720 cycles

RIGHT WING LEADING EDGE, OUTBOARD ATTACH ANGLE, ON FRONT SPAR IS CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-41-02.

Part: INTERCOSTAL — DENTED (E/E BAY DOOR) · airframe 27,943 hrs · 25,720 cycles

AFT EQUIPMENT COMPARTMENT DOOR CTR INTERCOSTAL DAMAGED. REMOVED DAMAGE AFT EQUIPMENT COMPARTMENT DOOR INTERCOSTAL INSTALLED NEW INTERCOSTAL I.A.W. CRJ-200 SRM 51-42-06 AAR SM 107

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 27,532 hrs · 25,271 cycles

EMER LTS ONLY STAY ON FOR 2 SECONDS WHEN PUT IN ON POSITION CHARGED EMERGENCY LIGHTS FOR 4 HRS TEST GOOD PER AMM 33-51-00 OK FOR SERVICE

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 27,368 hrs · 25,096 cycles

FS 409.0+128 VERTICAL POST LBL 18.00 LWR O/B ANGLE CRACKED, FROM LWR EDGE EXTENDING UP TO AND PAST 1ST RIVET BUT ENDING BETWEEN 1ST AND 2ND RIVET CRACKED ANGLE AT FS409.0+128 VERTICAL POST LBL 18 LWR O/B REPAIRED BY 1 VISION UNDER W.O. #2553 PER REO 601R-53-41-056. SEE CONT. CARD FOR DTAILS

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 27,368 hrs · 25,096 cycles

FS409+128 VERT POST RBL 27.00 LWR IB ANGLE CRACKED FROM EDGE EXTENDING UP TO AND PAST 1ST RIVET, ENDING BETWEEN 1ST AND 2ND RIVET. CRACKED ANGLE AT FS409+128 VERT POST RBL 27 LWR I/B REPAIRED BY 1 VISI ON UNDER WO# 2553 IAW REO 601R-53-41-056. SEE CONT CARD FOR DETAILS

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 27,368 hrs · 25,096 cycles

FS409+128 VERT POST RBL 18 LWR OB ANGLE CRACKED REPAIR COMPLETED BY 1 VISION REPAIR STATION 10VR169C ON WO#2553 PER REO 601R-53-41-056

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 27,368 hrs · 25,096 cycles

FS409+128 VERT POST LBL 27.00 LWR IB ANGLE CRACKED REPAIR COMPLETED BY 1 VISION REPAIR STATIN 10VR169C ON WO#2553 PER REO 601R-53-41-056

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,679 hrs · 24,326 cycles

EXTERIOR EMERGENCY LIGHTS DS5LF AND DS8LF WILL NOT WORK. REPLACED EMERGENCY LIGHT BATTERY PACK PS3LF IAW AMM 33-51-04 AND OPS CHECKS GOOD IAW AMM 33-51-04.

Part: WIRE — BROKEN (FLASHLIGHT) · airframe 26,631 hrs · 24,273 cycles

PILOT FLASHLIGHT NOT FLASHING. FOUND A BROKEN WIRE. R & R THE FLASHLIGHT IAW AMM 25-61-04, OK FOR SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 24,271 hrs · 21,772 cycles

FA FLASHLIGHT LED LIGHT INOPERATIVE. R & R THE FLASHLIGHT ASSY IAW AMM 25-61-02. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — OUT OF LIMITS (NLG) · airframe 25,615 hrs · 22,706 cycles

NOSE GEAR DOOR WARNING ILLUMINATED IN FLIGHT AT 20,000 FT. DISENGAGE CAME ON BREIFLY ONCE AGAIN WITH GEAR DOWN THEN EXTINGUISHED. REMAINDED OFF. FOUND THE PROXIMITY SENSOR TO BE OUT OF LIMITS AT 0.60 INCHES. ADJUSTED THE SENSOR IAW AMM 32-61-05. SENSOR CHECKED GOOD, DOOR FUNCTIONS NORMAL. ACFT OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,883 hrs · 22,418 cycles

EXTERIOR EMERGENCY LIGHT 5 INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21.

Part: WIRE — BROKEN (CABIN) · airframe 24,633 hrs · 22,150 cycles

BROKEN WHITE WIRE FOR EMER LIGHTS IN FA JUMPSEAT COMPARTMENT. R&R SPLICE FOR EMER LIGHT IN FA COMPARTMENT IAW ESPM 20-16-00.

Part: SENSOR — INOPERATIVE (NLG) · airframe 24,554 hrs · 22,059 cycles

HAD A NOSE GEAR DISAGREE WARNING LIGHT AT 18000 FT, RAN THE CHECK LIST AND ALL INDICATIONS WERE NORMAL. NORMAL INDICATIONS PRIOR AS WELL. RETURNED TO DEPARTURE, AND LANDED WITH NORMAL INDICATIONS. REMOVED & REPLACED PS1GA NLG HARNESS IAW AMM 32-61-25, OPS CHECKED GOOD IAW AMM 32-61-00.

Part: SELECTOR VALVE — INOPERATIVE (NLG) · airframe 24,543 hrs · 22,047 cycles

NOSE GEAR DOORS OPEN ON THEIR OWN AFTER HYDRAULICS ARE TURNED OFF. REMOVED AND REPLACED THE NLG CHECK VALVE IAW AMM 32-22-25. OPS AND LEAK CHECKED GOOD. REMOVED AND REPLACED NLG DOOR SELECTOR VALVE IAW AMM 32-22-20. OPS AND LEAK CHECKED GOOD.

Part: STRUT — LOW (NLG) · airframe 24,391 hrs · 21,889 cycles

ROTATION WHEN OFF AFTER 30 SEC GEAR INDICATION DISAGREED AND FLASHING WITH NOSE GEAR INDICATION YELLOW. CHECKED S21 PROXIMITY SENSORS. FOUND GAP TO BE .043, WITHIN LIMITS. SERVICED NOSE STRUT IAW AMM 12-12-32-610-803. PERFORMED RETRACTION AND EXTENSION CHECK IAW AMM 32-30-00, NO DEFECTS NOTED. ONLY CODE IN PSEU WAS S21 NEAR.

Part: LIGHT — DETACHED (SEAT 1C) · airframe 24,166 hrs · 21,660 cycles

EMERGENCY LIGHT DETACHED NEXT TO SEAT 1C. REPLACED THE EMERGECY LIGHT IAW 33-51-01.

Part: PROXIMITY SENSOR — OUT OF RIG (MLG) · airframe 23,890 hrs · 21,382 cycles

GEAR DISAGREE WARNING MESSAGE AT BELOW 1000FT AFTER TAKEOFF. PERFORMED QRH. RETURN TO DEPARTURE. INTERROGATED PSEU AND FOUND CODE FOR LT MLG S20 LG UPLOCK FAR. ACCOMPLISHED FUNCTIONAL CHECK OF EXT AND RETRACTION SYSTEM. DUPLICATED MESSAGE ON RETRACTION. FOUND S20.O26 OUT OF RIG. ADJUSTED S20 IAW AMM 32-32-05-400-801. FUNCTIONAL TESTED NUMEROUS TIMES IAW 32-30-00-720-801 WITH NO FAULTS OR GEAR DISAGREE. PSEU MEMORY RESET.

Part: SELECTOR VALVE — INOPERATIVE (ZONE 700) · airframe 23,886 hrs · 21,379 cycles

ON TAKEOFF GEAR DISAGREE WARNING MESSAGE (LEFT MAIN) CHECKLIST CLEARED MESSAGE, NORMAL LANDING AND NORMAL STEERING DEFER L/G RETRACTION SYS IAW MEL 32-30-01. (M) PROCEDURES C/W MOC NOTIFIED (96169) ENTERED INTO MM02, PLACARDED PER THE MEL REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE FUNCTIONAL TEST OF THE LANDING GEAR EXTENSION AND RETRACTION SYS NORMAL. THIS CLEARS CONTROL #3347413-1. PLACARD REMOVED, MM02 UPDATED, MOC NOTIFIED 95794

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 23,818 hrs · 21,317 cycles

OBSERVORS 02 MASK FAILS TO TEST CORRECTLY. REMOVED AND REPLACED THE OXYGEN STORAGE BOX IAW AMM 35-11-15 AND R & R THE OXYGEN MASK IAW AMM 35-11-12 OPS AND LEAKS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 23,507 hrs · 20,992 cycles

EMERGENCY LIGHT BY SERVICE DOOR INOPERATIVE BROKEN. R & R NR 1 EMERGENCY BATTERY PACK IAW AMM 33-51-04. OPS TEST GOOD. R & R SERVICE DOOR LAMP ASSY IAW AMM 33-51-13. OPS TEST GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN CARGO AREA CORROSION ON FLOORBOARD SUPPORT STA 615, RBL 27. REPAIRED FLOORBOARD SUPPORT STA 615, RBL 27 IAW EA CRJ253-04538.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

APB IS CRACKED AT LBL 27.5 AND APPROXIMATELY WL 130, JUST ABOVE CARGO DOOR TRACK. REPAIRED APB AT LBL 27.5 APPROXIMATELY WL 130 IAW REO 601R-53-61-1541.

Part: SKIN — CRACKED (PAX DOOR) · airframe 23,487 hrs · 20,973 cycles

PASSENGER DOOR INNER SKIN CRACKED AT FASTENER HOLE BELOW AFT DRAG ANGLE AND ASSIST MOTOR CABLE PULLEY BRACKET. REPAIRED PASSENGER DOOR INNER SKIN BELOW AFT DRAG ANGLE AND ASSIST MOTOR CABLE PULLEY BRACKET IAW EA CRJ252-04537.

Part: HINGE FITTING — FAILED (RUDDER) · airframe 23,487 hrs · 20,973 cycles

RUDDER LOWER CENTER HINGE BEARING FAILED PROOF LOAD. R & R RUDDER LOWER CENTER HINGE FITTING IAW RIL 0602.

Part: LATCH — DEFECTIVE (OXYGEN MASK) · airframe 23,487 hrs · 20,973 cycles

LAVATORY OXYGEN MASK LATCH WILL NOT DEPLOY. R & R LAV OXYGEN MASK LATCH IAW AMM 35-21-05. OPS TEST OF LAV OXYGEN SYSTEM GOOD IAW AMM 35-20-00.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,487 hrs · 20,973 cycles

PASSENGER ENTRY DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED PASSENGER ENTRY DOOR AFT DRAG ANGLE IAW REO NR 601R-52-11-513.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

FS 202.75 BULKHEAD IS CRACKED AT THE PARKING BREAK PASS THROUGH. REPAIRED FS 202.75 BULKHEAD AT THE PARKING BRAKE PASS THROUGH IAW REO 601R-53-11-563, REV C.

Part: ANGLE — CRACKED (RT PYLON) · airframe 23,487 hrs · 20,973 cycles

RIGHT PYLON UPPER PANEL 422AT ANGLE CRACKED. R & R RT PYLON UPPER PANEL 422AT ANGLE AND SEAL IAW SRM 51-42-06 AND AMM 54-63-01 SM-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN MAIN CABIN LT SIDEWALL SEAT RAIL NR 6 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R SEAT RAIL NR 6 IAW REO-601R-53-00-055 AND AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

RIGHT FLOOR SEAT TRACK, STICK NR 2, HAS GOUGES AND CORROSION RBL9. R & R SEAT TRACK STICK NR 2 RBL 9 IAW AMM-53-01-11-420-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN MAIN CABIN, RT SEAT TRACK HAS CORROSION AND IS GOUGED AT STA 559 TO 559+80, RBL9. R & R SEAT TRACK FROM STA 559 TO 559+80 RBL9 IAW REO-601R-53-00-485 AND AMM 53-01-11.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 23,487 hrs · 20,973 cycles

IN CARGO AREA, CARGO TRACK IS CORRODED AND GOUGED STA 559+90, LBL9. R & R SEAT TRACK AT STA 559+90 LBL9 IAW REO-601R-53-00-485 AND AMM 53-01-11.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

PASSENGER CABIN, S-3L BRACKET CRACKED AT FS 280. R & R PASSENGER CABIN STRINGER 3L BRACKETS AT FS 280 IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN MAIN CABIN LT SEAT TRACK HAS CORROSION AND IS GOUGED, STA 559 TO 559+80, LBL9. R & R SEAT TRACK FROM STA 559 TO 559+80 LBL9 IAW REO-601R-53-00-485 AND AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN MAIN CABIN LT SIDEWALL SEAT RAIL NR 7 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R SIDEWALL SEAT RAIL NR 7 IAW REO-601R-53-00-055 AND AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN MAIN CABIN, RT SIDEWALL SEAT RAIL NR 6 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R SEAT RAIL NR 6 IAW REO-601R-53-00-055 AND AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN MAIN CABIN, RT SIDEWALL SEAT RAIL NR 4 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R SEAT RAIL IAW REO-601R-53-00-055 AND AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

LT 1 SEAT TRACK FROM FS 364.0 TO FS 400 HAS CORROSION. R & R SEAT TRACK STICK 1 IAW AMM-53-01-11-420-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN MAIN CABIN RT SIDEWALL SEAT RAIL NR 5 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R SEAT RAIL NR 5 IAW AMM-53-01-11-420-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN MAIN CABIN, RT SIDEWALL SEAT RAIL NR 2 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R SEAT NR 2 TRACK IAW AMM-53-01-11-420-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN MAIN CABIN RT SIDEWALL SEAT RAIL NR 3 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R SEAT RAIL NR 3 IAW AMM-53-01-11-420-001.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

SINGLE POINT REFUEL RECEPTACLE MOUNT OTBD STRUCTURE IS CRACKED. R & R REFUEL RECEPTACLE MOUNTING OTBD BRACKET IAW SRM 51-42-06 & 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN MAIN CABIN LT SIDEWALL SEAT RAIL NR 3 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R SEAT RAIL NR 3 IAW AMM-53-01-11-420-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN MAIN CABIN LT SIDEWALL SEAT RAIL NR 2 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R SEAT RAIL NR 2 IAW AMM-53-01-11-420-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN MAIN CABIN LT SIDEWALL SEAT RAIL NR 4 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R SEAT RAIL NR 4 IAW AMM-53-01-11-420-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

IN MAIN CABIN LT SIDEWALL SEAT RAIL NR 5 HAS MULTIPLE AREAS OF CORROSION AND GOUGES. R & R SEAT RAIL NR 5 IAW AMM-53-01-11-420-001.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

RIGHT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE FS 470.00 IS CRACKED. R & R ATTACH STRUCTURE AT IAW SRM-51-42-21.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

RIGHT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE FS 476.00 IS CRACKED. R & R ATTACH STRUCTURE AT FS 476 IAW SRM-51-42-21.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 23,487 hrs · 20,973 cycles

LEFT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE FS 470.00 IS CRACKED. R & R ATTACH STRUCTURE AT FS 470 IAW SRM-51-42-21.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 22,332 hrs · 19,821 cycles

WHEN AT IDLE OR CLOSE TO IDLE THRUST DURING DESCENT, CABIN PRESS RATE CLIMBED AT 1000 FPM FOR APPROXIMATELY 5 TO 10 SECONDS BEFORE STABILIZING. THIS HAPPENED EVERY TIME THRUST WAS AT OR NEAR IDLE. PERFORMED OPERATIONS CHECK OF THE PRESSURIZATION CONTROLS IAW AMM 21-31-00, OPERATIONS CHECKED GOOD. PERFORMED FUNCTIONAL TEST OF CABIN PRESS CONTROLLER IAW AMM 21-31-16, FUNCTIONAL CHECK GOOD. OK FOR SERVICE NO DEFECTS NOTED.

Part: LENS — CRACKED (CABIN) · airframe 22,273 hrs · 19,758 cycles

231 BLC EMER EXIT LIGHT LENS CRACKED. R & R EMER EXIT LIGHT LENS ON PANEL 231 BLC IAW AMM 33-51-14.

Part: SKIN — DENTED (FUSELAGE) · airframe 22,266 hrs · 19,750 cycles

MULTIPLE DENTS TO THE FUSELAGE SKIN WITH TWO DENTS BETWEEN FS 605 & FS 615, STRINGER 23R & STRINGER 25R BEING CREASED. REPAIRED IAW EA CRJ253-02541.

Part: SKIN — DENTED (FUSELAGE) · airframe 22,266 hrs · 19,750 cycles

MULTIPLE DENTS TO THE FUSELAGE SKIN. THERE ARE 7 DENTS BETWEEN FS 589 & FS 605 & STRINGER 22R & STRINGER 25R, WITH A MAX DIAMETER OF 0.6” & A MAX DEPTH OF 0.007” DEEP. REPAIRED IAW EA CRJ253-02524.

Part: STIFFENER — DAMAGED (LT PYLON) · airframe 22,266 hrs · 19,760 cycles

ELONGATED FASTENER HOLE ON THE LT PYLON UPPER STIFFENER WITH A FASTENER HOLE NOMINAL DIAMETER OF .215”. REPAIRED IAW EA CRJ254-02532.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 22,266 hrs · 19,750 cycles

FS 621 BULKHEAD HAS MULTIPLE SCREW MARKS ON FWD SIDE BETWEEN LBL 36.2 & RBL 36.2. REPAIRED IAW REO 601R-53-61-2155.

Part: SEAL — MISSING (FIRST AID KIT) · airframe 22,015 hrs · 19,502 cycles

FIRST AID KIT MISSING COPPER SEAL & BAND AIDS. REPLACED FIRST AID KIT IAW PA 25-194.

Part: STRUT — DEFECTIVE (NLG) · airframe 27,867 hrs · 19,353 cycles

AFTER TAKEOFF WITH GEAR SELECTED TO RETRACT, RECEIVED NOSE GEAR DISAGREE WITH A NOSE GEAR DOOR OPEN WARNING. ALL THREE GEAR INDICATED GREEN. MAX SPEED WAS 200KIAS CREW FOLLOWED QRH & RETURNED TO CVG. ATC DECLARED AN EMERGENCY. CREW LANDED & TAXIED SAFELY TO THE GATE. DURING CREW DEBRIEF CAPTAIN STATED THAT ON TOUCHDOWN THE ACFT WANTED TO VEER TO THE RT, BUT SHORTLY AFTER ROLL OUT STEERING CENTERED & WORKED NORMALLY. R & R NLG LOWER SHOCK STRUT IAW AMM 32-21-25. EXTENSION & RETRACTION OPERATIONS CHECKED GOOD AT THIS TIME.

Part: SHAFT — MALFUNCTIONED (TE FLAP) · airframe 21,797 hrs · 19,284 cycles

FLAPS FAILED AT 30 WITH HANDLE AT 45. INSPECTED FLAPS, RESET & DEFERRED. PREFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD2009-06-12 PARAGRAPH H G I AMBC DATED JULY 22, 2013 & PA AD27-05-052N. PREFORMED LUBE OF RT FLAP SYS IAW CHECKLIST. R & R NR 3 & NR 5 RT FLAP FLEX SHAFTS IAW AMM 27-53-10. R & R FLAP CONTROL LEVER IAW AMM 27-51-01. ALL CHECKED GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 21,418 hrs · 18,930 cycles

FLAP FAILED AT 45 DEGREES ON GROUND, DURING FLAP RETRACTION FROM 45 DEGREES TO 0 DEGREES WITH OAT OF 20 DEGREES C. RESET FLAP SYSTEM AND PERFORMED FIVE CONSECUTIVE FLAP CYCLES, MAINTENANCE PERFORMED IAW FIM 27-50-00. PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12, PARA H, 6, I, AND PA AD 27-052M. CODES 52B; 19C1; 19C2; 25BC; 31BC; 33BC. PERFORMED SELF-TEST OF THE FLAP CONTROL LEVER IAW AMM 27-51-01-740-801. ALL CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED (SPOILERS) · airframe 20,868 hrs · 18,393 cycles

FLIGHT SPOILERS FAULT STATUS MESSAGE IN FLIGHT DESCENDING THROUGH 18,00 FL MESSAGE SPREARED WHILE USING THE FLIGHT SPOILERS AT 330 KNOTS . ON FLIGHT CONTROL PAGE THE LT FLIGHT SPOILER BOX SHOWED WHITE, FLIGHT SPOILERS OPERATED NORMALLY. RESET FLIGHT SPOILER SYS AND OPS CHECK IT IAW AMM 27-61-00. OPS CHECKED GOOD AT THIS TIME.

Part: LIGHT — UNSECURE (CABIN) · airframe 20,840 hrs · 18,364 cycles

TRACK LIGHTING UNSECURED AT ROW 8C. SECURED TRACK LIGHTS IAW AMM 33-51-01.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,751 hrs · 18,278 cycles

EMERGENCY LIGHT MID SECTION INOPERATIVE. R & R NR 3 INVERTER IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: PBE — OUT OF LIMITS (COCKPIT) · airframe 20,636 hrs · 18,161 cycles

BLUE DOT ON COCKPIT PBE IS NOT BLUE. REPLACED COCKPIT PBE IAW MM 35-30-00. SECURITY SEALS INSTALLED.

Part: TERMINAL — DAMAGED (CABIN) · airframe 20,539 hrs · 18,061 cycles

EMERGENCY FLOOR TRACK LIGHTING AT AFT CABIN LAVATORY AREA NEEDS CONNECTOR PIN. REPAIR AT LIGHTING TERMINATING PIGTAIL INSTALLED NEW TERMINAL IAW ESPM 20-17-10, OPERATIONS CHECK OF LIGHTING, GOOD.

Part: COVER — BROKEN (CABIN) · airframe 20,258 hrs · 17,764 cycles

ON FLIGHT 3948 (YYZ TO DTW) CREW REPORTED A PROBLEM WITH THE FLOOR LEVEL EMERGENCY LIGHTING STRIP. TRACK LIGHTING COVER BROKE OFF IN ROW 9. REPLACED DAMAGED FLOOR TRACK LIGHTING IAW CRJ 200 AMM CH 33-51-01. RE-ATTACHED FLOOR TRACKS.

Part: SEAL — MISSING (FIRE BOTTLE) · airframe 19,715 hrs · 17,205 cycles

MISSING SEAL ON FIRE EXTINGUISHER FLIGHT DECK. REMOVED AND REPLACED SEAL ON FIRE EXTINGUISHER AS REQUIRED IAW AMM 26-23-01. OK FOR SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,302 hrs · 16,802 cycles

CRACK FOUND IN CAP ANGLES AT FS 559 RBL 18 AND LBL 18. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 AND REO 601R-53-41-609.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,302 hrs · 16,802 cycles

AFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING OF FS 621 BULKHEAD. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,224 hrs · 16,720 cycles

EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BULB IAW AMM 33-51-21. ALL CHECKED GOOD.

Part: LENS — DAMAGED (LT WING) · airframe 18,584 hrs · 16,089 cycles

PERFORM TEMP REPAIR TO LT NAV LENS IAW REO 601R-57-32-001. PERFORMED TEMP REPAIR TO LT NAV LENS IAW REO 601R-57-32-001.

Part: LIFE VEST — DAMAGED (COCKPIT) · airframe 18,584 hrs · 16,089 cycles

F/O, F/A & OBSV LIFE VEST DAMAGED. REMOVED AND REPLACED F/O, F/A & OBSV LIFE VEST IAW AMM 25-61-03.

Part: CONNECTOR — LOOSE (WINDOW HEAT) · airframe 18,391 hrs · 15,908 cycles

AIR RETURN FOR L WINDOW HEAT CAUTION MSG INTERMITTENT IN FLIGHT. RESECURED CONNECTOR IN REF AMM 30-41-01. MSG DID NOT DUPLICATE. PERFORMED OPS CHECK GOOD AT THIS TIME. A/C OK FOR SVC.

Part: TRIM SYSTEM — MALFUNCTIONED (AILERON) · airframe 18,273 hrs · 15,797 cycles

AILERON TRIM INOP. RESET C/B ON CBP-2 F7 AILERON TRIM IAW AMM 27-12-01. OPS CHECKS GOOD IAW AMM 27-12-00. OK FOR SVC.

Part: CONTROL UNIT — DEFECTIVE (HORIZ STAB) · airframe 17,737 hrs · 15,259 cycles

HSTCU STAB CH1 AND CH2 BREAKERS POPPED ON APU START. TRIED TO RESET BUT BOTH POP BACK OUT. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. OP CHECK GOOD. VERIFIED PART EFFECVITY. OK FOR SVC.

Part: COWLING — MISSING (RT ENGINE) · airframe 15,269 hrs · 12,923 cycles

ON POST FLIGHT WALKAROUND INSPECTION AT KMSP, THE FIRST OFFICER NOTICED THE LOWER ENGINE COWLING WAS MISSING FROM THE RIGHT ENGINE. THE SUBJECT COWLING WAS IN PLACE AT KTYS THE DEPARTURE AIRPORT. MAINTENANCE WAS NOTIFIED AND THE COWL WAS REPLACED.

Part: LIGHT — SHORTED (COCKPIT) · airframe 9,850 hrs · 8,034 cycles

CAPTAIN SIDE FLOOD LIGHT RHEOSTAT SMOKED WHEN ADJUSTED. REPLACED SHORTED LIGHT ASSEMBLY. OPERATION NORMAL IAW AIRCRAFT MAINTENANCE MANUAL 33-11-00.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 6,247 hrs · 5,021 cycles

FLAP FAILURE ON TAXI IN WHEN TRYING TO RETRACT FLAPS. SYSTEM RESET AND PLACED UNDER 72 HOUR WATCH PER AD 2006-12-21.

Part: FLAP — MALFUNCTIONED (WING) · airframe 4,868 hrs · 3,880 cycles

FLAP FAILURE AT 20, FOLLOWED QRH, DECLARED EMERGENCY. UNEVENTFUL LANDING. FLAPS RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.

Part: FLAP SYSTEM — FAILED (WINGS) · airframe 3,757 hrs · 3,021 cycles

FLAPS FAIL ON APPROACH.