N8836A

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 30,830 hrs · 28,825 cycles

LH, RH AND CENTER 9G BULKHEAD HAVE TOOLING MARKS AT CARGO PANEL ATTACHEMNT PANELS. REPAIRED 9G BULKHEADS IAW EO'S CL-600-2B19-53-L06370, CL-600-2B19-53-L06371 AND EO CL-600-2B19-53-L06372. WVAC STAMP

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 30,830 hrs · 28,825 cycles

LH, RH AND CENTER 9G BULKHEAD HAVE TOOLING MARKS AT CARGO PANEL ATTACHEMNT PANELS. REPAIRED 9G BULKHEADS IAW EO'S CL-600-2B19-53-L06370, CL-600-2B19-53-L06371 AND EO CL-600-2B19-53-L06372. WVAC STAMP

Part: SKIN — DENTED (LT SPOILER) · airframe 30,830 hrs · 28,825 cycles

L/WING O/B GRD SPOILER BOTTOM SKIN DENTED APPX .5 X .5 X .020. REPAIRED LH WING O/B GROUND SPOILER DENT ON BOTTOM SKIN IAW EA CRJ257-1045. WVAC STAMP

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,830 hrs · 28,825 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS 4 INDICATIONS NOTED: 1) BL 0.0 WL 134-127 4 INCHES LONG 50% FSH, 2) RBL 36.20 WL91-90 1 INCH LONG 100% FSH, 3) RBL 27.50 WL85-84 1 INCH LONG 100% FSH AND 4) BL 0.0 WL114-1104 INCHES LONG 80% FSH FAILED NDT INSPECTION. REPAIRED 621 BULKHEAD AT BL . RBL 27 AND RBL 36 IAW REO 601R 53-61-1285 REV E DATED 2016-10-31. WVAC

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 30,830 hrs · 28,825 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS DENT ON FWD SIDE BETWEEN LBL 9.50 AND LBL 18.00 WL 79 .400 BY .400 .010 DEEP. REPAIRED DENT ON REAR PRESSURE BULKHEAD FWD SIDE IAW REO 601R-53-61-7312 REV--. WEIGHT ADDED .7 LBS. WVAC STAMP

Part: PANEL — CORRODED (FUSELAGE) · airframe 30,830 hrs · 28,825 cycles

LIGHTNING DIVERTER PANEL CLIP LBL 27 JUST FWD OF F.S. 333.00 IS CORRODED LOCATED, DRILLED & INSTALLED NEW SERVICEABLE LIGHTNING DIVERTER PANEL CLIP PN# 601R52219-117 AT LBL 27 F.S. 333.00 IAW CRJ 200 SRM 51-42-13.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,604 hrs · 27,510 cycles

DURING INSPECTION FOUND R/H MID AND AFT EMERGENCY LIGHTS OUT. R/R R/H EMERGENCY LIGHTS IAW AMM 35-51-21. OPS CHECKS GOOD. P/N ON/OFF 1317 NSN ON OR OFF.

Part: SKIN — DAMAGED (LT WING) · airframe 29,479 hrs · 27,377 cycles

DURING REINSPECT OF THE LH WING PLANK ACCESS HOLE 550CB NOTED INDICATIONS AROUND THE CIRCUMFERENCE OF THE ACCESS HOLE LANDING 75% FULL SCREEN HEIGHT. FAILING NDT AREAS MARKED ON A/C. REPAIRED FUEL PANEL WING PLANK ACCESS HOLE 550CB IAW REO 601RX57-21-3020 DATED 2019-05-01 REV--.

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 29,476 hrs · 27,377 cycles

FS 621 PRESSURE BULKHEAD WEB FWD FACE HAS 7 TOOLING MARKS APPROX .1" ROUND X .001" DEEP AT WL 103, LBL 9,18,27 AND RBL 9,18,27,36. REPAIRED BULKHEAD IAW BOMBARDIER GREO 601R-53-61-2155 REV A DATED 2013-06-13.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,479 hrs · 27,377 cycles

PAX DOOR SILL LOWER ANGLE CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE SILL LOWER ANGLE IAW SRM 51-42-13, 51-42-06, AND 51-42-21.

Part: PLATE — CORRODED (RT PYLON) · airframe 29,479 hrs · 27,377 cycles

RT PYLOIN TOP INBD TRAILING EDGE BOND PLATE CORRODED. REMOVED AND REPLACED RT PYLON TOP IB BOND PLATE IAW SRM 51-42-12, BOND TEST GOOD.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,479 hrs · 27,377 cycles

SERVICE DOOR CUTOUT BOTTOM SILL ANGLE CORRODED BETWEEN FS319 AND FS349. REMOVED & REPLACED SVC DOOR BOTTOM SIL ANGLE IAW 51-42-21, 51-40-11, 51-42-13 & 51-25-00.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 29,479 hrs · 27,377 cycles

AFT EQUIPMENT COMPARTMENT FS 621.00 TO 625.00 OBLIQUE ANGLE AT STR 14L IN CRACKED. REMOVED AND REPLACED OBLIUQUE ANGLE AT STR14L IAW SRM 51-42-21 P/N 601-35012-51.

Part: BULKHEAD — CHAFED (BS 621) · airframe 27,968 hrs · 25,718 cycles

REAR PRESSURE BULKHEAD HAS MULTIPLE SUPERFICIAL HARDWARE HITS & A LIGHT SUPERFICIAL SCRATCH, HITS LOCATED AT RBL 36.20, 27.50, 18.00 ON RIVET CL ONE 1.75" I/B OF RBL 9.50 CL OUTSIDE OF TOE ZONE ANOTHER 1.75" I/B OF LBL 9.50 CL OUTSIDE OF TOE ZONE SUPERFICIAL SCRATCH 3.25" BETWEEN BL 0.0-LBL 9.50 OUTSIDE HEAL/TOE ZONE ALL TO BE REPAIRED IAW REO 601R-53-61-2155 REV A REPAIRED IAW REO 601R-53-61-2155, REV A

Part: POST — CRACKED (BS 409) · airframe 27,968 hrs · 25,718 cycles

VERTICAL POST AT RBL 27, BS 409 +128 HAD A CRACK ORIGINATING AT BOTTOM OF THE INBD FLANGE & EXTENDING UP TO & PAST 1ST RIVET, ENDING APPROX BETWEEN 1ST & 2ND RIVETS. REPAIRED IAW REO 601R-53-41-056. MAJOR REPAIR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,642 hrs · 25,327 cycles

RIGHT FWD CENTER EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW CMM 33-52-07. OPS CHECKED GOOD.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 27,436 hrs · 25,106 cycles

CAPTAIN`S OXYGEN MASK HARNESS WILL NOT INFLATE. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,939 hrs · 24,565 cycles

LEFT FWD AND AFT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FWD AND AFT EMERGENC LIGHTS IAW 33-50

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 26,687 hrs · 24,298 cycles

CAPTAIN'S EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-61-00.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 26,646 hrs · 24,257 cycles

EMERGENCY LIGHT SECTION JUST AFT OF EXIT ROW NOT ILLUMINATING. REMOVED AND REPLACED THE EMERGENCY LIGHT SECTION IAW AMM 33-51-01.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 26,613 hrs · 24,217 cycles

FLOOR LIGHTING IS OUT ROW 8-10. PERFORMED VISUAL INSPECTION OF EMERGENCY LIGHT STRIP AT 9-10 C/D, FOUND STRIP CONNECTOR DISCONNECTED. ATTACHED, OPS CHECKED IAW AMM 33-51-00. OK FOR SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 26,564 hrs · 24,169 cycles

EMERGENCY LIGHTS CAME ON BRIEFLY, THEN TURNED OFF. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS OPS TESTED GOOD.

Part: WIRE SPLICE — DAMAGED (EMERGENCY LIGHT) · airframe 26,537 hrs · 24,143 cycles

FLOOR EMERGENCY LIGHTS NOT ILLUMINATED AT ROWS 9CD TO 12CD. REMOVED AND REPLACED THE CABLE SPLICE CONNECTOR IAW ESPM 20-17-10.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,012 hrs · 23,589 cycles

FO'S EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FO'S EMERG FLASHLIGHT PN ON/OFF P2-07-0001-214 IAW AMM 25-61-04. OPS CHECK GOOD.

Part: G SWITCH — INOPERATIVE (ELT) · airframe 25,964 hrs · 23,541 cycles

ELT G SWITCH INOPERATIVE. R & R THE ELT IAW AMM TASK 25-62-01-000-801. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,853 hrs · 23,427 cycles

DURING A ROUTINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. R & R THE LIGHT IAW AMM 33-51-01, OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,632 hrs · 22,157 cycles

EMERGENCY CALL LIGHT ON MID CABIN EMER EXIT LIGHT OUT, BACKSIDE ONLY. R & R CALL LIGHT MID CABIN EMER EXIT LIGHT IAW AMM 33-50-00. OPERATIONS CHECKED GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

FRAME SECTOR FS 333 IS CORRODED AT STRINGER 27. CONTINUATION CARD 8783611 OPERATIONS 302 & 311. REPLACED FRAME AT FS 333 IAW SRM 51-40-11, 51-42-06 7 51-42-21.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

FRAME SECTOR CORRODED AT FS 574, BETWEEN STRINGER 2GR & 2GL. CONTINUATION CARD 8783611 OPERATIONS 327 & 345. REMOVED FRAME SECTOR & REINSTALLED NEW SERVICEABLE FRAME SECTOR IAW SRM 51-42-06, 51-42-21, 51-42-22 & EA CRJ 253-04189 & REINFORCEMENT ANGLE, REPAIRED IAW EA CRJ 253-04199.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

RIGHT FLOOR SILL HAS SURFACE CORROSION AROUND SEVERAL FASTENER HOLES, AT APPROX FS 559+106 & ONE EACH NUTPLATE IS MISSING AT FS 559+92. CONTINUATION CARD 8783611 OPERATIONS 356. REPAIRED RT FLOOR SILL IAW REO 601R-53-00-526 REV DATED 05 22 13 & EA CRJ253-04188 REV A.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

FOUND REAR PRESS BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED AT INBD LOWER CORNER, APPROX .200" IN LENGTH 90% FSH. FAILED NDT INSPECTION. CONTINUATION CARD 8783615 OP 76. REPAIRED REAR PRESS BULKHEAD AT THE LINTEL ATTACHMENT FITTING IAW REO 601R-53-61-1230, REF F DATED 10 31 11. LEAK CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,505 hrs · 22,021 cycles

48 MONTH. NR 4 EMER LIGHT BATTERY PACK INVERTER INOPERATIVE. R & R NR 4 EMER LIGHT BATTERY PACK INVERTER IAW AMM 33-51-07-400-801. OPERATIONS TESTED GOOD.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,505 hrs · 22,021 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED ABOVE PULLEY SUPPORT BRACKET. CONTINUATION CARD 8783611 OP 310. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO:601R-52-11-513 REV B DATED 2015 07 05, TYPE I REPAIR. OPERATIONS CHECKED GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

FRAME CORRODED AT FS 605 & STRINGER 27. CONTINUATION CARD 8783611 OPERATIONS 297, 298, 301, 303, & 338. REMOVED FRAME & INSTALLED NEW FRAMES IAW SRM 53-00-00, 51-40-11, 51-42-06, 51-42-20 & 51-42-21. OPERATIONS CHECKED GOOD.

Part: VANE — CHAFED (TE FLAP) · airframe 24,505 hrs · 22,021 cycles

LEFT WING INBD FLAP VANE LE CHAFED IN 3 PLACES. INBD 1.0 X 1.0 X .006 DEEP, MID 1.0 X .750 X .005 DEEP, OTBD 1.0 X .300 X .002 DEEP. CONTINUATION CARD 8783611 OPERATIONS 324. REPAIRED LT INBD FLAP VANE LE CHAFES IAW REO 601R-57-52-004 REV D DATED 2012 12 19.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

AIRCRAFT GND POWER RECEPTACLE STRUCTURE CRACKED. CONTINUATION CARD 8783611 OPERATION 322 & 346. R & R POWER RECEPTACLE BRACKET IAW SRMS 51-42-06, 51-42-21, 51-40-11 & EA CRJ253-04187.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

FOUND FS 202.75 PRESS BULKHEAD WEB AT BL 23.71 HAS INDICATION NOTED, APPROX .500 IN LENGTH 50% FSH, FAILED NDT. CONTINUATION CARD 8783615 OP 66 & 82. REPAIRED FS 202.75 PRESS BULKHEAD IAW REO 601R-53-11-563 REV C. THIS IS A MAJOR REPAIR.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

CARGO DOOR FLOOR SILL IS CORRODED AROUND MULTIPLE FASTENER HOLES. R & R CORRODED FLOOR SILL IAW REO 601R-53-61-1574 & SRM 51-40-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

OUTBOARD CLIP 1 EACH IS CRACKED ATTACHING TO FLOORBEAM AT FS 280 AT RBL 9 & LBL 9. CONTINUATION CARD 8783611 OPERATIONS 333. FABRICATED, R & R FS 280 CLIPS IAW REO 601R-53-11-926 & SRM 51-42-21.

Part: SKIN — CHAFED (RT WING) · airframe 24,505 hrs · 22,021 cycles

RIGHT WING INBD LOWER SKIN, WING PLANK, CHAFED FROM FAIRING APPROX 3.0 X .400 X .003 DEEP. REPAIRED IAW REO 601R-57-21-880 REV C DATED 2011 07 18. THIS IS A MAJOR REPAIR. REPAIR PERFORMED TO ZONE A, .010" MATERIAL REMOVED.

Part: SKIN — DAMAGED (LT WING) · airframe 24,505 hrs · 22,021 cycles

LEFT LOWER WING PLANK CUT OUT FOR FUEL PANEL 540BB, HAS FRETTING DAMAGE ON INBD SIDE, NON-CRITICAL REGION. REPAIRED FUEL PANEL 540BB WING PLANK CUT OUT IAW REO 601R-57-21-030 REV L DATED 02 05 14. THIS IS A MAJOR REPAIR.

Part: PANEL — CHAFED (LT WING) · airframe 24,505 hrs · 22,021 cycles

LEFT INBD WING, BOTTOM WING PANEL CHAFED FROM FAIRING, APPROX 1.5 X .300 X .004 DEEP. REPAIRED IAW REO 601R-57-21-880 REV C DATED 07 18 11. THIS IS A MAJOR REPAIR. REPAIR PERFORMED TO ZONE A, .030" MATERIAL REMOVED.

Part: SKIN — DAMAGED (LT WING) · airframe 24,505 hrs · 22,021 cycles

LEFT LOWER WING PLANK CUT OUT FOR FUEL PANEL 540FB, HAS FRETTING DAMAGE ON INBD & OTBD ENDS, NON-CRITICAL REGION. REPAIRED FUEL PANEL 540FB WING PLANK CUT OUT IAW REO 601R-57-21-030 REV L DATED 02 05 14. THIS IS A MAJOR REPAIR.

Part: SKIN — DAMAGED (LT WING) · airframe 24,505 hrs · 22,021 cycles

LEFT LOWER WING PLANK CUT OUT FOR FUEL PANEL 550HB, INBD SIDE HAS FRETTING DAMAGE, NON-CRITICAL REGION. REPAIRED FUEL PANEL 550HB WING PLANK CUT OUT IAW REO 601R-57-21-030 REV L DATED 02 05 14. THIS IS A MAJOR REPAIR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

STRINGER 3L AT FS 379 IS CRACKED APPROX .25". REPAIRED DAMAGE IAW SRM 51-42-06, 51-42-21 & 53-00-03.

Part: SKIN — DAMAGED (RT WING) · airframe 24,505 hrs · 22,021 cycles

RIGHT LOWER WING PLANK FUEL PANEL CUT OUT FOR FUEL PANEL 640DB, HAS FRETTING DAMAGE ON INBD, OTBD & FWD EDGES. BOTH CRITICAL & NON-CRITICAL REGIONS. REPAIRED IAW REO 601R-57-21-030 REV L DATED 2014 02 05. THIS IS A MAJOR REPAIR. REFERENCE ATTACHED REO FOR WORK PERFORMED.

Part: CUP — CORRODED (PAX DOOR) · airframe 24,505 hrs · 22,021 cycles

FORWARD & AFT PAX DOOR HANDRAIL CUPS ARE CORRODED AROUND FASTENER HOLES, FS 310 & 349. REPLACED FWD & AFT PAX DOOR HANDRAIL CUPS WITH NEW SERVICEABLE CUPS IAW SRM 51-40-11, 51-42-06, 51-42-21, 51-42-13 & 51-12-00. PN REPLACED 601R31527-137 149.

Part: SKIN — DAMAGED (RT WING) · airframe 24,505 hrs · 22,021 cycles

RIGHT LOWER WING PLANK CUT OUT FOR FUEL PANEL 640BB, HAS FRETTING DAMAGE ON INBD & OTBD ENDS, NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030 REV L DATED 2014 02 05. REFER TO ATTACHED REO FOR WORK PERFORMED. THIS IS A MAJOR REPAIR.

Part: SKIN — DAMAGED (RT WING) · airframe 24,505 hrs · 22,021 cycles

RIGHT LOWER WING PLANK CUT OUT FOR FUEL PANEL 650HB, HAS FRETTING DAMAGE ON INBD SIDE, NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030 REV L DATED 2014 02 05. REFER TO ATTACHED REO FOR WORK PERFORMED. THIS IS A MAJOR REPAIR.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

FOUND REAR PRESS BULKHEAD WEB HAS 4 CHAFED AREAS, AT WL 105, LBL 27.50, LBL 18.00, RBL 27.50 & RBL 36.20, APPROX .200" LONG BY .200" WIDE & .002 DEEP. REPAIRED 4 CHAFED AREAS IAW REO 601R-53-61-2155 REV A DATED 2013 08 13. THIS IS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

LEFT SIDE SEAT RAIL SEGMENTS 2 - 7 ARE CORRODED. REPLACED CORRODED LT SIDE SEAT RAIL IAW AMM 53-01-11-400-802. ALL FABRICATED SEAT TRACKS WERE ACCOMPLISHED IAW REO:601R-53-00-55 REV B DATED 2015 08 24.

Part: PLATE — CORRODED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

ALL 5 CARGO FLOOR ANCHOR PLATES ARE CORRODED, 3 EA LBL 27 & 2 EA LBL 9. R & R WITH NEW SERVICEABLE ANCHOR PLATES, 5 TOTAL IAW SRM 51-41-02, PN 601R38663-21.

Part: CUP — CHAFED (PAX DOOR) · airframe 24,505 hrs · 22,021 cycles

PASSENGER DOOR HANDRAIL CUPS FWD & AFT ARE CHAFED ON BOTTOM SIDE. R & R FWD & AFT HANDRAIL CUPS IAW SRM 51-42-21. PN REPLACED 601R317727-1.

Part: STOP FITTING — BROKEN (RT WING) · airframe 24,505 hrs · 22,021 cycles

RIGHT BUTE DOOR 694JB HAS THE STOP BROKEN. RT BUTE DOOR STOP ON PANEL 694JB WAS R & R IAW SRM 51-42-14 & SRM 51-42-06 PT 600-10196-16.

Part: PANEL — DAMAGED (WING) · airframe 24,505 hrs · 22,021 cycles

PANEL 684BB HAS 4 ELONGATED MOUNTING SCREW HOLES. RECEIVED SERVICEABLE PANEL 684BB, LOCATED HOLES & TRANSFERRED PARTS IAW SRM 51-42-06, 51-40-06 & 51-40-11. REFERENCE PANEL BOOK FOR REMOVAL & INSTALL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

SEAT TRACK CORRODED AT RBL 9, BETWEEN FS 559+48 & 559+80. R & R SEAT TRACK IAW AMM 53-01-11-400-802 & REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

SEAT TRACK SEGMENTS 1 EA AT RBL 9 & LBL 9, BETWEEN FS 394 - FS 409+128 ARE CORRODED. R & R SEAT TRACK IAW SRM 51-40-11 & AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

ALL 7 CARGO SEAT TRACK SEGMENTS ARE CORRODED, 1 EA AT RBL 27, 2 EA AT RBL 9, 3 EA AT LBL 9 & 1 EA AT LBL 27. CONTINUATION CARD 8783611 OPERATIONS 299. R & R DAMAGED SEAT TRACKS IN CARGO BAY IAW AMM 53-01-11-400-802 & REO 601R-53-00-485.

Part: STRAP — CORRODED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

STRAP BETWEEN FLOORBEAMS AT LBL 9 & RBL 9 AT FS 617, IS CORRODED. EVALUATED CORROSION & REMOVED MINOR CORROSION IAW SRM'S 53-00-00 & 51-21-06. MATERIAL THICKNESS .050 BEGINNING, REMOVED .003, .047 REMAINING.

Part: STRAP — CORRODED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

LEFT FLOOR STRAP CORRODED FROM SILL TO LBL 36 AT FS 559. REPLACED LH FLOOR STRAP IAW SRM 51-40-06, 51-40-11 & 51-42-06, PN 601R31025-29.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

FS 461 FLOOR SUPPORT BEAM FITTING CRACKED AT OTBD SIDE OF RBL 9. REPLACED FS 461 FLOOR SUPPORT BEAM FITTING AT OTBD SIDE IAW SRM 51-42-06 & 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

STRINGER 3L AT FS 280 HAS CRACKED CLIP, AFT SIDE OF BULKHEAD. R & R CLIP IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,505 hrs · 22,021 cycles

SEAT TRACK SEGMENTS 1 EA AT RBL 9 & LBL 9, BETWEEN FS 364 - 394 ARE CORRODED. REMOVED UNSERVICEABLE SEAT TRACK & INSTALLED NEW SERVICEABLE SEAT TRACK, PN 601R3102-15, IAW AMM 53-01-11-000-802 & AMM 53-01-11-400-802.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 24,505 hrs · 22,021 cycles

PASSENGER DOOR INNER HANDLE IS CRACKED. REMOVED TAPE. REMOVED CRACKED HANDLE, LOCATED, DRILLED & INSTALLED NEW HANDLE IAW SRM 51-40-11 & 51-43-00.

Part: HINGE — CORRODED (PAX DOOR) · airframe 24,505 hrs · 22,021 cycles

PASSENGER DOOR TOP FOLDING STEP 832ET, UPPER HINGE IS CORRODED. REMOVED CORRODED UPPER HINGE FROM PAX DOOR TOP FOLDING STEP 832ET & REPLACED WITH NEW PART IAW SRM 51-41-02.

Part: FITTING — CHAFED (TE FLAP) · airframe 24,505 hrs · 22,021 cycles

RIGHT FLAP STUB FAIRING FLAP FITTING IS CHAFED OUT OF LIMITS & REQUIRES REPLACEMENT. REMOVED UNSERVICEABLE RT FLAP STUB FLAP FITTING & REPLACED WITH NEW SERVICEABLE FLAP FITTING, PN 601R10371-2, IAW SRM 51-40-11 & SRM 51-42-21.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 24,352 hrs · 21,870 cycles

FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. INSTALLED SERVICEABLE BATTERY IN FLIGHT ATTENDANT EMER FLASHLIGHT PN P4-01-0021 IAW AMM 25-61-02.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 24,334 hrs · 21,851 cycles

FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE. MOVED TO MEL LOG IAW MEL 25-61-04 IAW JD CAT C ITEM. TWO OTHER FLASHLIGHTS OPERATE NORMALLY PLACARD INSTALLED. R & R FLASHLIGHT BATTERY IAW AMM 200 25-61-04. THIS CLEARS DM 009191 & MMO2. PLACARD REMOVED, OPERATIONS CHECKED GOOD.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 23,703 hrs · 21,231 cycles

INFANT LIFE VEST HAS A HOLE IN THE PACKAGING. R & R INFANT LIFE VEST IAW PA 25-096A.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,470 hrs · 21,012 cycles

FIRST FLIGHT OF THE DAY TEST FOR EMER LIGHT ON PERFORMED & GOT NO MSG & DID NOT GET ANY OF THE INDICATIONS OF ANY LIGHTS IN CABIN. DID GET THE EMER LLS OFF CAUTION MSG. PERFORMED THE SAME TEST FROM THE FLIGHT ATTENDANT`S PANEL & DID NOT SEE ANY INDICATION. R & R ALL 4 BATTERY PACKS IAW AMM 33-51-04-400-801. OPERATIONS CHECKED GOOD ON ALL BATTERY PACKS.

Part: FLAP — OBSTRUCTED (WING) · airframe 23,059 hrs · 20,592 cycles

FLAPS FAIL CAUTION MSG. PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARAGRAPH H B I AMOC DATED JULY 22, 2013 & PHAD 20-052N. REMOVED SNOW & ICE CONTAMINATION FROM FLAPS. OPERATIONS CHECKED IAW AMM 27-54-00 NO DAMAGE NOTED.

Part: PBE — FAILED (CABIN) · airframe 22,474 hrs · 19,998 cycles

F/A PBE LOST ITS VACUUM. REPLACED F/A PBE AS REQUIRED.

Part: PBE — FAILED (COCKPIT) · airframe 22,474 hrs · 19,998 cycles

FLIGHT DECK PBE IS SOFT. REPLACED FLIGHT DECK PBE AS REQUIRED.

Part: CONTAINER — TORN (LIFE VEST) · airframe 22,353 hrs · 19,878 cycles

LIFE VESTS BAG TORN. R & R LIFE VEST IAW AMM 25-61-03.

Part: CONTAINER — TORN (LIFE VEST) · airframe 22,353 hrs · 19,878 cycles

LIFE VESTS BAG TORN. R & R LIFE VEST IAW AMM 25-61-03.

Part: COMPUTER — MALFUNCTIONED (GPWS) · airframe 21,768 hrs · 19,303 cycles

AT 3000' AGL AND CLIMBING AT 1500 FPM, RECEIVED A FALSE GPWS, GROUND, PROXIMITY CAUTION THEN A GPWS PULL UP WARNING. REMOVED AND REPAIRED GPWS COMPUTER IAW AMM 34-42-01. OPS CHECKED GOOD IAW AMM 34-42-01, OK FOR SERVICE.

Part: STALL WARNING — ACTIVATED (COCKPIT) · airframe 21,737 hrs · 19,270 cycles

STALL FAIL MASTER CAUTION ON CLIMBOUT, MESSAGE PERSISTED FOR DURATION OF FLIGHT.

Part: PBE — UNSERVICEABLE (COCKPIT) · airframe 21,583 hrs · 19,122 cycles

COCKPIT PBE TORN OPEN. REMOVED AND REPLACED PBE IAW AMM 35-30-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,331 hrs · 18,864 cycles

CA FLASHLIGHT INOP. REMOVED AND REPLACED CA FLASHLIGHT IAW AMM 25-61-04, OPS CHECKS GOOD.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 21,244 hrs · 18,796 cycles

INFANT LIFE VEST BAG IS TORN. REPLACED INFANT LIFE VEST IAW PA 25-096A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,052 hrs · 18,617 cycles

CLIPS CRACKED AT FS 484, LBL 36 AND FS 484, RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-41-059.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 21,052 hrs · 18,617 cycles

FS 621 BULKHEAD HAS 4 RIVET HOLES WITH DRILL STARTS. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,974 hrs · 17,563 cycles

MAIN CABIN DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECKED GOOD IAW AMM 33-51-21.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,803 hrs · 17,394 cycles

RT NR 3 EXT EMER LIGHT INOP. REMOVED AND REPLACED BULB IAW AMM 33-51-21. OPS CHECK GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,853 hrs · 16,466 cycles

FS 559 WEB CAP ANGLE CRACKED AT LBL 18 AND RBL 18. WEB CRACKED AT RBL 18. REPAIRED IAW PA53-025 IAW REO 601R-53-41-206 AND 601R-53-41-609.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 18,792 hrs · 16,455 cycles

RT ENGINE FAILURE SHORTLY AFTER TAKEOFF. LOUD POP, FOLLOWED BY ENGINE SPOOL DOWN AND R ENG OIL WARNING MSG, ITT SPIKED IN RED. REMOVED AND REPLACED RT ENGINE IAW CHECKLIST. VERIFIED PART EFFECTIVITY. ALL LEAK & OPS CHECKS GOOD PER AMM 71-00-00. ALL RUNS REQUIRED C/W IAW AMM 71-00-00, 0 OZ OIL USED POST ENGINE RUNS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,794 hrs · 16,456 cycles

LOWER EMERGENCY EXIT FLOOR PATH LIGHT INOP AT SEAT 7C. REMOVED AND REPLACED E-LIGHT STRIP IAW AMM 33-51-01. OP/CHECK GOOD AT THIS TIME. CLEARS DM 54985. VERIFIED PART EFFECTIVITY.

Part: INVERTER — DEFECTIVE (CABIN) · airframe 18,794 hrs · 16,456 cycles

FLOOR EMERGENCY LIGHTS OUT BETWEEN ROW 2 AND 5. INSPECTED FOUND PIN AT FLOOR TRACK LIGHTING 5C BROKEN. REPLACED PIGTAIL IAW ESPM 20-17-00. NO FIX. FOUND NR 2 INVERTER BAD. REMOVED AND REPLACED NR 2 EMERGENCY LIGHTS INVERTER IAW CRJ 200 AMM 33-51-07. SYSTEM OP CHECK GOOD. VERIFIED PART EFFECTIVITY. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 17,233 hrs · 14,941 cycles

ON APPROACH INTO DTW CREW DECLARED AN EMERGENCY FOR RHT 14TH STAGE DUCT WARNING. BLEED LEAK SYS OP CHECK GOOD. NO DEFECTS NOTED. NO MSGS IAW AMM 36-20-00.

Part: VANE — CORRODED (TE FLAP) · airframe 17,092 hrs · 14,813 cycles

RT INBOARD FLAP OUTBOARD FLAP VANE CAP CHAFED BEYOND LIMITS. PERFORMED A MAJOR REPAIR TO THE RIGHT INBOARD FLAP OUTBOARD FLAP VANE CAP IAW ENGINEERING ORDER 601R-57-20490A.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,092 hrs · 14,813 cycles

FUSELAGE FRAME CORRODED AT FS 605.00 FROM STR 26L TO 26R. REMOVED AND REPLACED FUSELAGE FRAME AT FS 605.0 IAW CRJ SRM 51-42-06 & 51-42-21.

Part: SPOILER — DENTED (RT WING) · airframe 13,671 hrs · 11,277 cycles

A DENT WAS FOUND ON THE UPPER SURFACE OF THE RIGHT WING INBOARD GROUND SPOILER (P/N 601R10822-2). THE DENT MEASURES 1.0 X 0.875 X 0.011 DEEP; IT IS 9.5 FROM THE OUTBOARD EDGE AND 4.5 FROM THE TRAILING EDGE. REPAIRED IAW STS ENGINEERING EA 09-2011-037.

Part: SEAT TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 17,092 hrs · 14,813 cycles

CARGO TIE DOWN SEAT TRACKS CORRODED AT RBL 9 AND LBL 9 BETWEEN FS 559.00+112 - 574.00. REMOVED AND REPLACED CARGO TIE DOWN SECTIONS AT FS 559+112 TO 574 RBL 9 AND LBL 9 IAW CRJ 200 SRM 51-40-11 AND IAW CRJ AMM 53-01-11-400-802.

Part: PLATE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 17,092 hrs · 14,813 cycles

SERVICE DOOR STEP PLATE IS CORRODED. REMOVED AND REPLACED SERVICE DOOR STEP PLATE IAW CRJ-200 AMM 25-33-01-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,092 hrs · 14,813 cycles

RT SIDE SEAT TRACK FROM FS 529.00 TO 559.00+16 AND LT SIDE SEAT TRACK FROM FS 559.00 TO 559.00+80 HAVE AREAS OF CORROSION. REMOVED AND REPLACED SIDE SEAT TRACKS IAW CRJ-200 AMM 53-01-11-400-802.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,092 hrs · 14,813 cycles

LEFT WING LOWER PLANK ACCESS HOLES AT WS 12.245, WS 54.897, WS 76.161, WS 188.040, WS 209.040 AND WS 230.415 HAVE CORROSION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 17,092 hrs · 14,813 cycles

RIGHT WING LOWER PLANK ACCESS HOLES AT WS 54.897, WS 76.161, WS 116.366 AND WS 209.040 HAVE CORROSION NOT IN CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: SKIN — CORRODED (TE FLAP) · airframe 17,092 hrs · 14,813 cycles

RIGHT INBOARD FLAP LOWER SKIN IS DENTS - GOUGE .500"L X .500"W X .010"D. PERFORMED A MAJOR REPAIR TO THE RIGHT INBOARD FLAP LOWER SKIN IAW CRJ 200 SRM 57-52-00, INBOARD FLAP AND VANE - REPAIR NR 2 - FLUSH REPAIR TO INBOARD FLAP SKIN. CONTINUING AIRWORTHINESS DAMAGE TOLERANCE INSPECTION REQUIREMENTS: THE INSPECTION INTERVALS ARE 40000 FLIGHT CYCLES THRESHOLD AND 40000 FLIGHT CYCLES REPEAT. THE INSPECTION METHOD IS "SPECIAL DETAILED" (REFER TO NDTM 51-53-00-101, PART 6).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,092 hrs · 14,813 cycles

THE FLOOR SUPPORT IS CRACKED AT FS 280.00 LBL 9.0 AND THE FS 280.00 BULKHEAD WEB IS CORRODED AT THE FLOOR BETWEEN RBL 9.0 AND LBL 9.0. PERFORMED A MAJOR REPAIR TO THE 280.00 FLOOR SUPPORT AND THE BULKHEAD WEB AT FS 280.00 FROM LBL 20.75 TO RBL 20.75 IN ACCORDANCE WITH BOMBARDIER AEROSPACE REPAIR ENGINEERING ORDER 601R-53-11-926 REVISION B AND BOMBARDIER SERVICES CORPORATION STANDARD REPAIR 601R-53-0110.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,092 hrs · 14,813 cycles

CARGO DOOR FLOOR SILL PLATE HAS CORROSION ON TOP AND BOTTOM SURFACES. REMOVED AND REPLACED CARGO DOOR FLOOR SILL P/N - 601R35011-63 IAW BOMBARDIER REO 601R-53-61-1574 AND BSC STANDARD REPAIR 601R-53-0096.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 15,295 hrs · 13,111 cycles

IN THE CLIMB FROM MEM TO JAX AT FL230 THE CA SIDE WINDSHIELD STARTED TO ARC AND BEGAN TO SCORCH THE OUTSIDE PLY THE WINDSHIELD. AFTER, THE LT WINDSHIELD HEAT CAUTION MESSAGE CAME ON THE SCORCHING STOPPED. COMPLETED THE QRH AND TALKED TO DISPATCH AND MAINTENANCE, DECIDED TO TURNBACK AND HEAD TO MEMPHIS. THE EVENT OCCURRED DUE TO A FAILURE IN THE WINDSHIELD ON THE CA SIDE. MEMPHIS MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD.

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 14,784 hrs · 12,601 cycles

SELECTED GEAR DN ON APPROACH. NOSE LANDING GEAR FAILED TO EXTEND RESULTING IN GEAR DISAGREE WARNING. MTX PERFORMED THE FOLLOWING: PERFORMED FUNCTIONAL TEST OF THE LANDING GEAR EXTENSION AND RETRACTION. OPS CHECK GOOD. PERFORMED LANDING GEAR DISAGREE TEST. OPS CHECK GOOD, AND PERFORMED SYSTEM TEST OF THE LANDING GEAR PRIORITY VALVES OPS CHECK GOOD IAW AMM 32- 30-00 AML 541404. C/W PA 05-018A BY PERFORMING THE F/G OF THE LANDING GEAR EXTENSION/RETRACTION SYSTEM. OPS CHECK GOOD AND PERFORMED LANDING GEAR DISAGREE TEST. OPS CHECK GOOD AND PERFORMED SYSTEM TEST OF THE PRIORITY VALVES IAW AMM 32-30-00.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 14,554 hrs · 12,384 cycles

WHILE ON TAKEOFF ON 18R IN MEM A NORMAL TAKEOFF WAS ACCOMPLISHED. WHEN THE GEAR HANDLE WAS SELECTED UP THE CREW RECEIVED TWO CAUTION MESSAGES. PARKING BRAKE SOV AND ANTI SKID NBRD. THE QRH WAS STARTED WHEN FLIGHT CREW THEN NOTICED WHAT SOUNDED LIKE AN UNUSUAL AMOUNT OF DRAG. THE CREW THOUGHT THEY MIGHT STILL BE DOWN. CREW TOLD ATC, NEED A HEADING AND TO LEVEL AT 10000 TO WORK OUT AN ISSUE. AFTER CONFERRING WITH MX AND DISPATCH THE FLIGHT WAS RELEASED BACK TO MEM. SINCE THE QRH NEEDED THE CREW TO INCREASE THE LANDING DISTANCE BY 75 PERCENT WITH NO ANTI SKID. CREW DECIDED TO DECLARE AN EMERGENCY AND LAND ON 18C. CREW LANDED THE AIRCRAFT USING MAINLY REVERSE THRUST AND BROUGHT THE AIRCRAFT TO FULL STOP TOO, NO EVENT THEREAFTER. CREW WAS INFORMED NOTHING APPEARED WRONG WITH THE GEAR/AIRCRAFT AND THE AIRCRAFT RETURNED TO THE GATE. MTX PERFORMED GEAR SWINGS AND OPS CHECKS OF THE ANTISKID SYSTEM. BOTH OPS CHECKED GOOD.

Part: STEERING SYS — OUT OF RIG (NLG)

NOSE WHEEL STEERING INOPERATIVE MESSAGE ON APPROACH. QRH FOLLOWED MESSAGE REMAINED. LANDING UNEVENTFUL. NOSE WHEEL STEERING SYSTEM RIGGED PER BOMBARDIER AMM 32-51-01. (S)

Part: PLUG — MISSING (ENGINE OIL) · airframe 8,717 hrs · 7,304 cycles

AFTER TAKEOFF FROM SBN, THE AIRCRAFT CLIMBED TO FL290. SHORTLY AFTER REACHING CRUISE ALTITUDE, THE RIGHT ENGINE OIL PRESSURE WARNING ILLUMINATED FOLLOWED BY A DROP IN OIL PRESSURE ON THE RT OIL PRESSURE GAUGE. THE FLIGHT CREW PERFORMED THE QRH AND REDUCED POWER ON THE ENGINE. SEEING THAT THE OIL PRESSURE CONTINUED TO DROP, THE CAPTAIN ELECTED TO SHUTDOWN THE ENGINE. AN EMERGENCY WAS DECLARED AND AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE AT MSP. MAINTENANCE FOUND THAT THE AIRCRAFT HAD A MEL'D NR 2 ENGINE DRIVEN HYDRAULIC PUMP. FURTHER INVESTIGATION REVEALED THAT THE PUMP HAD NOT BEEN PROPERLY MEL'D AT SBN. OIL LOSS WAS THE RESULT OF A MISSING SPLINE PLUG AND O-RING WHICH ARE PART OF THE MEL KI

Part: FLAP SYSTEM — UNKNOWN

FLAPS FAIL, SECOND OCCURRENCE WITHIN 72 HOURS.

Part: FLAP SYSTEM — UNKNOWN

FLAPS FAIL, SECOND OCCURRENCE WITHIN 72 HOURS.

Part: FLAP SYSTEM — UNKNOWN · airframe 8,373 hrs · 7,028 cycles

FLAPS FAIL. RESET PER AD 2006-12-21.

Part: BPSU — DEFECTIVE (T/E FLAP) · airframe 6,792 hrs · 5,712 cycles

FLAP FAIL ON TAXI OUT SECOND OCCURRENCE. RETURNED TO GATE MAINTENANCE TROUBLESHOT SYSTEM PER FIM FOUND THE LT BPSU (BRAKE POSITION SENDING UNIT) BAD. REMOVED AND REPLACED BPSU AND RIGGED SYSTEM PER AMM.

Part: PSEU — MALFUNCTIONED (NLG DOOR)

UNCOMMANDED NOSE DOOR DEPLOYMENT. QRH FOLLOWED, EMERGENCY DECLARED, UNEVENTFUL LANDING. REMOVED AND REPLACED PSEU. PERFORMED GEAR SWINGS IAW AMM.