N8839E

Part: BULKHEAD WEB — CRACKED (AFT CABIN) · airframe 33,622 hrs · 31,567 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS 3 CHAFED AREAS AT WL 103 RBL 36.20, RBL 27.50, AND RBL 18.00 .200 LONG BY .200 WIDE .003 DEEP. REPAIRED 3 CHAFED AREAS OF REAR PRESSURE BULKHEAD WEB AT WL 103 RBL 36.20, RBL 27.50 AND RBL 18.00, IAW REO 601R-53-61-21-55 REV A, 2013-08 -13 AND BOMBARDIER REO 601R-53-61-1285 REV E, 2016-10-13.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 33,622 hrs · 31,567 cycles

FLOORBEAM AT LBL 27 BETWEEN FS 559+16 AND FS 570 IS CORRODED. R & R UNSERVICEABLE FLOORBEAM AT LBL 27 BETWEEN 559+116 AND 570 WITH SERVICEABLE FLOORBEAM, IAW MHIRJ REO 601R-53-61-7489 REV-- DATED 2020-11-12 AND REO 601R-53-00-027 REV D DATED 26-NOV-2009.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,622 hrs · 31,567 cycles

FRAME AT FS 605 CORRODED BETWEEN STGR 25R AND STRG 24L. R & R 605 FRAME SECTION FROM 25R TO 25L, IAW ENDEAVOR EA CRJ253-10963 REV IR DATED 11-4-20, CRJ 200 SRM 51-42-06 AND 51-25-01.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 33,622 hrs · 31,567 cycles

CARGO BAY FLOORBEAM CORRODED AT LBL 27 BETWEEN FS 605 AND FS 621. REPAIRED CARGO FLOOR BEAM AT LBL 27.0 BETWEEN 605-621, IAW ENDEAVOR EA CRJ253-10960 REV IR DATED 11-2-20. THIS IS A MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,622 hrs · 31,567 cycles

SKIN DAMAGE MEASURING .750" L LOCATED AT FWD FS 672 BETWEEN STGR 27 &26L. REPAIRED SKIN DAMAGE LOCATED FWD OF 672, IAW ENDEAVOR EA CRJ253-10934 REV IR DATED 10-31-2020 THIS IS A MAJOR REPAIR.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 33,622 hrs · 31,567 cycles

CARGO BAY FLOOR SEAT RAIL BEAM CORRODED BETWEEN FS 559+112 TO 621, LBL27. REMOVED AND REPLACED FLOOR BEAM FS 559+112-FS 621, LBL 27, IAW REO 601R-57-61-3378 REV B DATED 16/12/19.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,622 hrs · 31,567 cycles

FRAME AT FS 574 CORRODED BETWEEN STGR 24R AND STRG 24L. REMOVED UNSERVICEABLE 574 FRAME AND INSTALLED SERVICEABLE 574 FRAME, IAW CRJ-200 SRM 51-42-06, 51-42-21, 51-40-11. BELOW CARGO FLOOR AIR DISTRIBUTION SYSTEM LEAK TEST GOOD, IAW CRJ 200 AMM 21-20-00-790-801.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 33,622 hrs · 31,567 cycles

CARGO BAY TRACK SEGMENTS AT FS 559+80 TO FS 559+96 AND AT LBL 27, RBL 9, AND RBL 27 CORRODED. REMOVED AND REPLACED SEAT TRACK SEGMENTS AT FS 559+80 TO FS 559+96 AT LBL 27, RBL 9 AND RBL 27, IAW CRJ 200 AMM 53-01-11-000/400-802 AND SRM 51-40-11.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,622 hrs · 31,567 cycles

FRAME AT FS 589 CORRODED BETWEEN STGR 24R AND STGR 25L. REMOVED AND REPLACED FS 589 LOWER FRAME SECTOR, IAW CRJ200 SRM 51-40-11, 51-42-00, 51-42-21.

Part: STRAP — CORRODED (CARGO BAY) · airframe 33,622 hrs · 31,567 cycles

CARGO BAY FLOOR CAP STRAP CORRODED BETWEEN LBL 9 AND LBL 27 AT FS 589. REMOVED, FABRICATED, LOCATED AND INSTALLED CARGO BAY FLOOR STRAP, IAW CRJ 200 SRM 51-42-06, 51-42-21, 51-24-36, 51-40-11 AND 51-25-00.

Part: BULKHEAD WEB — CRACKED (AFT) · airframe 33,622 hrs · 31,567 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0.0 WL 112 1.0" LONG. 100% FSH FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD, IAW CRJ 200 REO 601R-53-1285 REV E, 2016-10-31.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 33,622 hrs · 31,567 cycles

CORROSION JUST AFT OF FS 559+112 ON STGR 27 CLEAT. REMOVED, FABRICATED AND INSTALLED STR 27 CLEAT JUST AFT OF FS 559+112, IAW CRJ 200 SRM 51-24-16, 51-42-06 AND 51-42-21 REFERENCING DRAWING 601R31057 REV J FOR MAT SPEC.

Part: SUPPORT BRACKET — CRACKED (SERVICE PANEL) · airframe 33,622 hrs · 31,567 cycles

EXTERNAL SERVICES PANEL SUPPORT BRACKET CRACKED. R & R UNSERVICEABLE SUPPORT BRACKET WITH SERVICEABLE SUPPORT BRACKET, IAW 51-40-11, 51-42-06 (CRJ 200 SRM) AND AMM 24-24-01-000/400-801. NO ELECTRICAL CONNECTIONS DISTURBED (PN: 601R33003-19).

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 33,622 hrs · 31,567 cycles

LT PRESSURE FLOOR SILL CORRODED BETWEEN FS 409+128 TO FS 559. REPAIRED AREAS OF CORROSION ON LT PRESSURE FLOOR SILL BETWEEN FS 409+128 TO FS 559, IAW BOMBARDIER REO 601R-53-41-666, REV C 11/6/12.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 33,622 hrs · 31,567 cycles

RT PRESSURE FLOOR SILL CORRODED BETWEEN FS 409+128 TO FS 559. REPAIRED CORRODED RT PRESSURE FLOOR SILL BETWEEN FS 409+128 AND FS 559, IAW BOMBARDIER REO 601R-53-41-666 REV C, 2012-11-06.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,622 hrs · 31,567 cycles

FLOOR SEAT TRACK AT LBL 9.0 BETWEEN FS 559 TO FS 559+80 GOUGED IN SEVERAL LOCATIONS. REPLACED SEAT TRACK AT LBL 9 BETWEEN FS 559 TO FS 559+80, IAW BOMBARDIER REO 601R-53-00-485 AND BOMBARDIER CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802, P/N:20276-288-0-0A.

Part: ATTACH ANGLE — CRACKED (CARGO DOOR) · airframe 33,622 hrs · 31,567 cycles

FOUND CARGO DOOR SUPPORT BEAM LOWER ATTACH ANGLE IS CRACKED .500 LONG. INSTALLED CARGO DOOR SUPPORT BEAM LOWER ATTACHMENT ANGLE, IAW CRJ 200 SRM 51-42-21 (NEW), P/N: 601R35050-109.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 33,622 hrs · 31,567 cycles

FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 409.0 TO FS 409.0+128 IS GOUGED AND CHAFED. REPLACED GOUGED FLOOR SEAT TRACK.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 33,622 hrs · 31,567 cycles

PRESSURE FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 409+128 TO FS 559 GOUGED AND CHAFED. CORRECT AMM REFERENCE FOR LINE ITEM NR 2 IS CRJ 200 AMM 53-01-11-000/400 -802.

Part: SEAT TRACK — GOUGED (CABIN) · airframe 33,622 hrs · 31,567 cycles

FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 559 TO FS 559+80 GOUGED IN SEVERAL LOCATIONS. REPLACED GOUGED FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 559 AND FS 559+80, IAW REO 601R-53-00-485 REV D DATED 1/29/18, CRJ 200 AMM 53-01-11-000/ 400-802.

Part: RIVET — SHEARED (SEAT TRACK) · airframe 32,157 hrs · 29,974 cycles

PILOTS IB SEAT RAIL WEAR STRIP #3 AN #4 RIVETS SHEARED AND WEAR STRIP UNBONDED. COMPLETED TEMPORARY DISPOSITION PER REO 601R-53-11-1093 INITIATED PWI FOR PERMANENT REPAIR WITHIN 6000FHS SEE N705678.

Part: VANE — CHAFED (TE FLAP) · airframe 32,157 hrs · 29,974 cycles

RT IB FLAP VANE LEADING EDGE CHAFED @ APPROX WS 57.5 FROM CONTACT WITH FLAP VANE BUMPER ON REAR SPAR. DIMENSIONS 1.25" X .875" X .023. FLAP ASSY PN 601R14002-2, SN SB/RJ866 COMPLETED TEMPORARY REPAIR IAW REO 601R-57-52-004 ON RHIB FLAP VANE AT STA 57.5 REFERENCE NR 705673 FOR 1000 CYC PWI UNTIL REPLACEMENT IS REQUIRED.

Part: CABLE — DEFECTIVE (CABIN) · airframe 32,157 hrs · 29,974 cycles

AFT FLOOR EMERGENCY LIGHT STRIP NOT WORKING. REMOVED AND REPLACED AFT FLOOR EMERGENCY LIGHT STRIP CABLE ASSY P/N 64-64-5 IAW AMM 33-51-01. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,797 hrs · 29,600 cycles

LH AFT EMERGENCY LIGHT INOP. REMOVED & REPLACED BULB IAW AMM 33-51-21. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 31,572 hrs · 29,355 cycles

FIRST ROW FLOOR LIGHT EMER STRIP WILL NOT LIGHT. REPLACED PS1LF BATTERY CHARGER ASSY IAW AMM 33-51-05. REPLACED FIRST ROW FLOOR TRACK LIGHTING STRIP IAW AMM 33-51-01. PN BA5-0933-901. SN OFF C01087. SN ON C00494. PN 36491-1. EMERGENCY LIGHTING SYSTEM OPS CHECKS GOOD IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 31,154 hrs · 28,904 cycles

EMERGENCY FLOOR TRACK LIGHTING LAMP 2 AND LH OVERWING EXIT FLOOR PROX LIGHT IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT CHARGER, BATTERY, INVERTER, FLEX LAMP, CONNECTOR, AND CABLE IAW AMM 33-51-01, 33-51-05, AND 33-51-07. OPS CHECK GOOD.

Part: STRUCTURE — CRACKED (APU ENCLOSURE) · airframe 30,766 hrs · 28,494 cycles

APU ENCLOSURE HAS CRACKED WELDS ON UPPER AND RH SIDE OF AFT FACE AND STIFFENERS REPAIRED APU ENCLOSUE IAW BOMARDIER REO 601R-49-11-071 AAR S/M-124

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,766 hrs · 28,494 cycles

PASSENGER MAIN ENTRY DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED PASSENGER MAIN ENTRY DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513 AAR S/M-124

Part: SEAT TRACK — CORRODED · airframe 30,766 hrs · 28,494 cycles

CABIN SEAT TRACK CORRODED AT LBL9 FROM FS559-FS559+80 REMOVED AND REPLACED CABIN SEAT TRACK LBL9 FS 559-559+80 IAW CRJ 200 AMM 53-01-11 AAR SM-107

Part: SEAT TRACK — CORRODED (BS 409) · airframe 30,766 hrs · 28,494 cycles

RH AISLE SEAT TRACK STICK 3 HAS CORROSION, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK STICK #3 I.A.W. CRJ-200 AMM 53-01-11 AAR SM-107

Part: REPAIR — CRACKED (BS 559) · airframe 30,766 hrs · 28,494 cycles

WHILE REMOVING RIVETS IN FUSELAGE SKIN FOUND LOWER FLANGE OF FRAME 559+96 STRINGER 22R CRACKED REPAIRED LOWER FLANGE OF FRAME 559+96 AND STRINGER 22R IAW CRJ SRM 53-00-15. AAR S/M-124

Part: FLOORBEAM — CORRODED (BS 559) · airframe 30,766 hrs · 28,494 cycles

CABIN FLOOR BEAM CORRODED AT FLOORBOARD LANDING FROM STA-559.00 TO 559+80 RBL-9 REMOVED AND REPLACED CABIN FLOOR BEAM CAP FS559.00-FS 559+8 RBL9 IAW CRJ200 SRM51-42-06 AND 51-42-21 AAR SM-107

Part: ATTACH FITTING — CRACKED (BS 202.75) · airframe 30,766 hrs · 28,494 cycles

WINDSHIELD CENTER POST LOWER INTERNAL ATTACH FITTING ON FIRST OFFICERS SIDE IS CRACKED AT FS202.75 INSTALLED NEW WINDSHIELD CENTER POST LOWER INTERNAL ATTACH FITTING IAW CRJ 200 SRM 51-42-21. AAR SM-107

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 30,766 hrs · 28,494 cycles

CABIN FLOOR BEAM CORRODED AT FLOORBOARD LANDING FROM STA-559.00 TO 559+80 RBL-9 REMOVED AND REPLACED CABIN FLOOR BEAM CAP FS559.00-FS 559+8 RBL9 IAW CRJ200 SRM51-42-06 AND 51-42-21 AAR SM-107

Part: SEAT TRACK — CORRODED · airframe 30,766 hrs · 28,494 cycles

RH SIDE SEAT RAIL STICK 6 GOUGED AND CORRODED IN MULTIPLE LOCATIONS. REMOVED AND REPLACED SIDE SEAT TRACK IAW CRJ 200 AMM 53-01-11 AAR-R S/M 17

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 30,766 hrs · 28,494 cycles

RH SIDE SEAT RAIL STICK 6 GOUGED AND CORRODED IN MULTIPLE LOCATIONS. REMOVED AND REPLACED SIDE SEAT TRACK IAW CRJ 200 AMM 53-01-11 AAR-R S/M 17

Part: ANGLE — CRACKED · airframe 30,766 hrs · 28,494 cycles

RH STGR 14 OBLIQUE ANGLE IS POSSIBLY CRACKED REMOVED AND REPLACED INTERCOASTAL IAW CRJ 200 SRM 51-42-06 51-24-21 TR 51-42 AAR SM-35

Part: ANGLE — CRACKED · airframe 30,766 hrs · 28,494 cycles

LH STGR 14 OBLIQUE ANGLE HAS POSSIBLY CRACKED REMOVED AND REPLACED WITH INTERCOASTAL IAW CRJ 200 SRM 51-42-06 51-40-11 TR 51-42 AAR SM-35

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 30,766 hrs · 28,494 cycles

L/H FLOOR SEAT TRACK FROM FS409.00+128.00 TO FS559.00 HAS CORROSION. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11 REF ACTION # 4 FOR MAT ID AAR SM-58

Part: SEAT TRACK — CORRODED (BS 554-559) · airframe 30,766 hrs · 28,494 cycles

RH SIDE SEAT RAIL STICK 7 GOUGED AND CORRODED IN MULTIPLE LOCATIONS. REMOVED AND REPLACED WITH NEW RH SIDE RAIL STICK #7 IAW CRJ 200 AMM 53-01-11. AAR SM-58

Part: SEAT TRACK — CORRODED (BS 364-405) · airframe 30,766 hrs · 28,494 cycles

RH AISLE SEAT TRACK STICK 1 HAS CORROSION, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11. AAR SM-58

Part: BRACKET — CRACKED (BS 484) · airframe 30,766 hrs · 28,494 cycles

CLIP IS CRACKED AT FS484.00 OTBD SIDE OF RBL27. REMOVED, FABRICATED AND INSTALLED NEW CLIPS. I.A.W. BOMBA REO 601R-53-41-059. AAR SM-107

Part: HINGE — CORRODED (PAX DOOR) · airframe 30,766 hrs · 28,494 cycles

PASSENGER DOOR STEP 832FT LOWER HINGE ASSEMBLY IS CORRODED. INSTALLED HINGE PN PANEL 832FT IAW CRJ 200 SRM 51-41-02. AAR SM-58

Part: OXYGEN BOTTLE — LEAKING · airframe 30,545 hrs · 28,259 cycles

DURING INSTALLATION OF 4LPM MASK TO A PORT ON BOTTLE, HISSING SOUND NOTED. BOTTLE PRESSURE BECAME TO LOW TO USE. REPLACED WITH NEW O2 BOTTLE AND O2 4LPM MASK (BLUE) IAW JOB CARD 35-900-750.

Part: PBE — UNSERVICEABLE (COCKPIT) · airframe 30,545 hrs · 28,259 cycles

FLT DECK PBE LOST VACUUM. REMOVED AND REPLACED FLT DECK PBE IAW AMM 35-30-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,209 hrs · 27,872 cycles

EMERGENCY LIGHT 8 INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB 8 IAW AMM 33-51-21. OPS CHECK OK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,726 hrs · 27,344 cycles

FWD OVERHEAD EMERGENCY LIGHT BULB INOPERATIVE. R & R THE BULB IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: EXTINGUISHER — LOW PRESSURE (CABIN) · airframe 29,241 hrs · 26,844 cycles

1 FWD F.A FIRE EXTINGSHR NOT SHOWING IN THE GREEN AREA INSTALLED NEW FIRE EXT IAW AMM 25-60-00. OPS CHECK GOOD A/C OK FOR SVC

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,800 hrs · 26,353 cycles

OVERWING EMERGENCY EXIT LIGHT ON CEILING INOPERATIVE. REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 28,450 hrs · 25,978 cycles

EMERGENCY LIGHTS ROWS 8 - 12 NOT WORKING. REPAIRED A BROKEN WIRE IAW ESPM 20-16-00. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 28,134 hrs · 25,647 cycles

EMERGENCY LIGHT INOPERATIVE. FOUND BROKEN WIRE. REPAIRED IAW ESPM 20-16-00. REPLACED THE LIGHT IAW 33-51-01 OPS CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 27,806 hrs · 25,300 cycles

FLOOR EMERGENCY LIGHT MISSING. SECURED THE IAW AMM 33-51-01.

Part: EXTINGUISHER — LOW PRESSURE (COCKPIT) · airframe 27,445 hrs · 24,936 cycles

COCKPIT FIRE EXTINGUISHER BOTTLE LOW PRESSURE. REMOVED AND REPLACED COCKPIT FIRE EXTINGUISHER IN ACCORDANCE WITH AMM 26-23-01.

Part: NOZZLE — DENTED (EXHAUST) · airframe 27,414 hrs · 24,907 cycles

FOUND A DENT AND PANEL MISSING ON TAILPIPE FAIRING ASSY. R & R TAILPIPE EXHAUST NOZZLE IAW AMM 78-11-03. OPS CHECKED GOOD.

Part: FRAME — CORRODED (BS 310) · airframe 27,376 hrs · 24,872 cycles

FRAME AT BS 310 CORRODED, STRINGER 22R - 23R. REPAIRED THE FRAME IAW EA. CRJ253-04961, REV IR.

Part: FRAME — CORRODED (BS 319) · airframe 27,376 hrs · 24,872 cycles

FRAME AT BS 319.7 ATTACH FLANGE, RADIUS WASHER, AND LOCK FASTENERS CORRODED AT STRINGER 23R. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REPAIRED THE FRAME IAW EA 253-04944.

Part: STRINGER — CORRODED (BS 349-364) · airframe 27,376 hrs · 24,872 cycles

STRINGER 26R CORRODED, BS 349 - 364. PERFORMED REPAIR TO THE STRINGER IAW EA CRJ253-04976 REV. IR.

Part: FRAME — CORRODED (BS 333) · airframe 27,376 hrs · 24,872 cycles

FRAME AT BS 333 CORRODED, STRINGERS 22 - 23R. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REPAIRED THE FRAME IAW EA CRJ253-04945.

Part: LATCH — INOPERATIVE (OXYGEN MASK DOOR) · airframe 27,376 hrs · 24,872 cycles

LAVATORY OXYGEN DOOR FAILED TO RELEASE DURING OPS CHECK. REMOVED & REPLACED THE OXYGEN MASK CONTAINER LATCH MECHANISM IAW AMM 35-21-05. OPS TESTED GOOD IAW AMM 35-20-00.

Part: BULKHEAD — CRACKED (BS 621) · airframe 27,376 hrs · 24,872 cycles

REAR PRESSURE BULKHEAD HAS A CRACK EXTENDING FROM THE TOP END OF THE CARGO DOOR TRACK APPROX 3/8" AT LBL 27.50. REPAIRED IAW REO 601R-53-61-1541.

Part: FRAME — CRACKED (BS 333) · airframe 27,376 hrs · 24,872 cycles

PAX CABIN FRAME BS 333 IS CRACKED BETWEEN STRINGERS 1 AND 2 L. REMOVED CRACK, FABRICATED, LOCATED AND DRILLED AND INSTALLED REPAIR ANGLE IAW EA CRJ253-04947 REV. B .

Part: STRINGER — CORRODED (BS 319-333) · airframe 27,376 hrs · 24,872 cycles

STRINGER 27 CORRODED, BS 319.70 - 333. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 AND 53-00-03. REPAIRED THE STRINGER IAW EA CRJ253-04948.

Part: BRACKET — CRACKED (VERTICAL STAB) · airframe 27,376 hrs · 24,872 cycles

LEFT VERTICAL STAB LOWER VISOR FAIRING BRACKET BROKEN. REMOVED AND INSTALLED WITH FABRICATED BRACKET IAW SRM 51-42-21.

Part: STRINGER — CORRODED (BS 310-333) · airframe 27,376 hrs · 24,872 cycles

STRINGER 23R CORRODED, BS 310 TO 333. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REPAIRED IAW SRM 53-00-03.

Part: FITTING — CRACKED (COCKPIT) · airframe 27,376 hrs · 24,872 cycles

FLIGHT DECK LT SIDE POST LOWER FITTING IS CRACKED. REMOVED AND REPLACED THE POST FITTING IAW SRM 51-42-21.

Part: FILLER — CHAFED (RT MLG DOOR) · airframe 27,376 hrs · 24,872 cycles

RT MLG DOOR FWD LE CHAFFED. REMOVED DAMAGED FILLER, FABRICATED NEW FILLER AND REPLACED IAW REO 601R-52-82-016.

Part: FILLER — CHAFED (LT MLG DOOR) · airframe 27,376 hrs · 24,872 cycles

LEFT MLG DOOR FWD LE CHAFED. REMOVED DAMAGE FILLER, FABRICATED NEW FILLER AND REPLACED IAW REO 601R-52-82-016.

Part: FITTING — CRACKED (COCKPIT) · airframe 27,376 hrs · 24,872 cycles

FLIGHT DECK RT SIDE POST LOWER FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-21.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 27,376 hrs · 24,872 cycles

BRAKE PRESSURE TRANSDUCERS BRACKET IN LT MLG WW IS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-22.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 27,376 hrs · 24,872 cycles

BRAKE PRESSURE TRANSDUCER BRACKET IN RT MLG WW IS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-06 AND SRM 51-42-22.

Part: SEAT TRACK — CORRODED (BS 552-559) · airframe 27,376 hrs · 24,872 cycles

LEFT SIDEWALL SEAT TRACK BETWEEN BS 552 - 559+80 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11 AND REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 27,376 hrs · 24,872 cycles

LEFT SEAT TRACK BETWEEN BS 409.0+16 TO 409.0+112 CORRDED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11 AND REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 402-409) · airframe 27,376 hrs · 24,872 cycles

LEFT SEAT TRACK FROM BS 402 TO 409+128 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11 AND REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 364-402) · airframe 27,376 hrs · 24,872 cycles

RIGHT SEAT TRACK BS 364 - 402 CORRODED. REMOVED AND REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 27,376 hrs · 24,872 cycles

RIGHT SIDEWALL SEAT TRACK BETWEEN BS 559+16 - 559+80 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-420-001.

Part: SEAT TRACK — CORRODED (BS 402-409) · airframe 27,376 hrs · 24,872 cycles

RIGHT SEAT TRACK BS 402 - 409+128 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-420-001.

Part: FLOOR SUPPORT — CORRODED (BS 589-610) · airframe 27,376 hrs · 24,872 cycles

LBL 27 FLOOR SUPPORT HAS CORROSION ON INBD AND OTBD FLANGES BETWEEN BS 589 - 610. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO 601R-53-61-3778 REV. A AND SRM 51-42-00, 51-42-02, 51-42-22 AND 51-42-28.

Part: ELT — NO TEST (CABIN) · airframe 27,376 hrs · 24,872 cycles

ELT FAILED OPS TEST. REMOVED & REPLACED THE ELT IAW AMM 25-62-01. OPS TESTED GOOD IAW AMM 25-62-00.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 27,376 hrs · 24,872 cycles

LEFT SEAT TRACK BETWEEN BS 409.0+112 TO 449.85 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 499-552) · airframe 27,376 hrs · 24,872 cycles

LEFT SIDEWALL SEAT TRACK BETWEEN BS 499 - 552 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-420-001.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 27,376 hrs · 24,872 cycles

LEFT SIDE SEAT TRACK BETWEEN BS 364 - 409+16 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 27,376 hrs · 24,872 cycles

RIGHT SIDEWALL SEAT TRACK BS 409+112 AND 449.85 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,088 hrs · 24,587 cycles

FA FLASHLIGHT NOT CHARGING. THE LIGHT IS NOT BLINKING.

Part: OXYGEN MASK — DEFECTIVE (PORTABLE O2) · airframe 27,004 hrs · 24,494 cycles

1 EA BLUE 4LPM MASK FAILS LEAK CHECK ON 1 EA PORTABLE OXYGEN BOTTLE. R & R 1 EA 4LPM BLUE OXYGEN MASK IAW TS 000340-2012 & AMM 35-31-01.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 26,928 hrs · 24,420 cycles

EXCESSIVE CONDENSATION COMING FROM AIR VENTS IN COCKPIT. PFD DIFFULCULT TO SEE ON TAKEOFF CLEANED COALESCER SOCKS ON BOTH LT & RT WATER SEPARATORS IAW AMM 21-51-13. OPS CHECK GOOD AT THIS TIME.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 26,635 hrs · 24,121 cycles

FIRST OFFICER'S 02 MASK IS LEAKING AT HARNESS THAT INFLATES WHEN DONNING 02 MASK. FOUND DURING PREFLIGHT. SWAPPED FIRST OFFICER`S MASK WITH OBSERVER'S MASK IAW AMM 35-11-12, DEFERRING OBSERVER'S MASK IAW MEL 35-10-01. R & R OBSERVER'S 02 MASK IAW AMM 35-11-12. OPS CHECKED GOOD, OK FOR SERVICE. THIS CLEARS DI 3233124-1.

Part: INVERTER — UNSERVICEABLE (CABIN) · airframe 26,595 hrs · 24,081 cycles

DURING MORNING WAKE UP NOTED EMER LIGHTS FLOOR AT ROW 2 - 5. NR 2 INVERTER OVER ROW 5 LT SIDE WITH SERVICEABLE UNIT, PN ON & OFF 5925-7. ALL CHECKED GOOD IAW AMM 33-51-07.

Part: BUTTON — DIRTY (OXYGEN SYS) · airframe 26,592 hrs · 24,077 cycles

FIRST OFFICERS SIDE 02 MASK. PRESS TO TEST, WHEN PUSHED VLV OPENS & DOES NOT CLOSE. CLEANED & SECURED FIRST OFFICERS O2 MASK STOWAGE BOX, PUSH TO TEST BUTTON. OPERATIONS CHECKED GOOD IAW AMM 35-11-15. OK FOR SVC.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,276 hrs · 23,745 cycles

PILOT SIDE EMER FLASHLIGHT BATTERY DEAD. R & R FLASHLIGHT & HOLDER ASSEMBLY IAW AMM 25-61-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,866 hrs · 23,330 cycles

FLOOR PATH EMER LIGHTS AT ROW 6 INOPERATIVE. R & R FLOOR TRACK LIGHTING AT ROW 6 IAW AMM 33-51-01. OPERATIONS CHECKED. PN OFF & ON 36262-4.

Part: LENS — DISLODGED (CABIN) · airframe 25,635 hrs · 23,090 cycles

EMERGENCY LIGHT LENS, BY SERVICE DOOR, IS DISLODGED FROM HOUSING. SECURED EXT EMER LIGHT LENS IAW AMM 33-51-21. OK FOR SERVICE.

Part: DOOR SEAL — DAMAGED (CABIN DOOR) · airframe 25,483 hrs · 22,937 cycles

MAIN CABIN DOOR SEAL IS SQUEALING BADLY, PAXS COMPLAINING. SOME WATER CAME IN PASSING THROUGH RAIN. NOISE CAME FROM THE TOP, AFT AREA. THE WALL IS WET BY THE ACFT UNDER THE PLASTIC TRIM. SQUEAL STOPPED ONCE LEVEL. REMOVED DEBRIS & CLEANED DOOR SEAL IAW STANDARD PRACTICE IN CHAPTER. R & R PAX DOOR SEAL IAW AMM 52-11-10. LEAK & OPERATIONS CHECK GOOD AT THIS TIME. PN ON & OFF 601R31872-3.

Part: UPLOCK SENSOR — OUT OF ADJUST (MLG) · airframe 25,151 hrs · 22,581 cycles

AFTER TAKEOFF, DURING GEAR RETRACTION RT MLG DISAGREE WARNING MESSAGE & RT MAIN GEAR LIGHT SHOWED RED UNSAFE. COMPLETED QRH FOR LG, EXTENDED GEAR WITH EMERGENCY HANDLE, ALL GEAR DOWN & LOCKED, GREEN RETURNED. TROUBLESHOT IAW FIM 32-60-05 & FOUND RT MLG UPLOCK SENSOR OUT OF ADJUSTMENT. MEASURES .069" IAW AMM 32-32-05 ADJUSTED TO WITHIN LIMITS .035-.045 AT .035". OPERATIONS CHECKED SEVERAL TIMES WITH NO DEFECTS NOTED.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 24,898 hrs · 22,313 cycles

SMOKE TOILET CAUTION MESSAGE WITH SMOKE DETECTOR ALARM AFTER MAIN CABIN DOOR CLOSED. LAV SMOKE DETECTOR OPS CK GOOD MM 26-16-00, OK FOR SERVICE.

Part: SMOKE DETECTOR — OUT OF ADJUST (LAVATORY) · airframe 24,803 hrs · 22,217 cycles

AT GATE, SMOKE TOILET CAUTION. ADJUST & TEST OF LAVATORY SMOKE DETECTOR GOOD IAW AMM 26-16-00. NO MSG, OK FOR SERVICE.

Part: LENS — UNSECURE (CABIN) · airframe 24,714 hrs · 22,129 cycles

PASSENGER DOOR EMER EXIT LIGHT LENS FALLING OUT. SECURED AS REQUIRED.

Part: LIGHT — DISLODGED (EXTERIOR) · airframe 24,502 hrs · 21,918 cycles

GALLEY DOOR EMER LIGHT HAS BEEN DISLODGED FROM ITS HOUSING. SECURED LOOSE GLASS ON EXTERIOR EMER LIGHT COVER NEAR SERVICE DOOR IAW AMM 33-51-21.

Part: LIGHT — BROKEN (CABIN) · airframe 24,396 hrs · 21,815 cycles

LIGHTS 6 - 8 ARE BROKEN ON EMER FLOOR LIGHT STRIP. R & R FLOOR TRACK EMER LIGHT STRIP 6 -8 IAW AMM 33-51-01. OPERATIONS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: CONNECTOR — BROKEN (CABIN) · airframe 24,396 hrs · 21,815 cycles

ONE EACH BROKEN CONNECTOR ON EMER LIGHT STRIP NEAR OVERWING EXIT LOCATION. REPAIRED CONNECTOR IAW ESPM 20-17-31. OPERATIONS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 24,394 hrs · 21,813 cycles

SEVEN CHAFE MARKS ON FWD SIDE OF FS 621 BULKHEAD. REPAIRED IAW REO 601R-53-61-2155 & REO 601R-53-61-5370.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 24,394 hrs · 21,813 cycles

LEFT WING LOWER PLANK FUEL ACCESS PANEL 550BB AT WS 54.897 CUT OUT CORRODED 0.003 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 24,394 hrs · 21,813 cycles

LEFT WING LOWER PLANK FUEL ACCESS PANEL 550HB AT WS 294.048 CUT OUT CORRODED 0.002 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 24,394 hrs · 21,813 cycles

SEVEN SCREW MARKS WERE FOUND ON THE FWD FACE OF THE FS 621 BULKHEAD. REPAIRED IAW REO 601R-53-61-5370.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,394 hrs · 21,813 cycles

INBOARD & OUTBOARD CLIPS FOR FLOOR SUPPORT BEAM AT FS 280 RBL 9 CRACKED. REPAIRED IAW REO 601R-53-11-171.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,394 hrs · 21,813 cycles

INBOARD & OUTBOARD CLIPS ARE CRACKED AT FLOOR SUPPORT BEAM AT FS 280 AT LBL 9. REPAIRED IAW REO 601R-53-11-171.

Part: SHAFT — DIRTY (ESCAPE HATCH) · airframe 24,232 hrs · 21,657 cycles

CREW ESCAPE HATCH EXTERIOR HANDLE WON'T POP UP WHEN PUSH DEPRESSED. FOUND EXTERNAL HANDLE SHAFT DIRTY. CLEANED & LUBED HANDLE AS REQUIRED. OPERATIONS CHECKED IAW MTCM 000-52-830-702.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 24,099 hrs · 21,526 cycles

FLOOR LEVEL EMER FLOOD LIGHT ON LT GALLEY FWD NEAR PAX DOOR IS INOPERATIVE. NOTE LIGHTING BOARD ASSEMBLY IS GOOD IAW BENCH TEST. R & R P9LY CONNECTOR BEHIND LT WARDROBE. OPERATIONS CHECKED GOOD FOR LIGHT ASSEMBLY IAW AMM 33-51-00.

Part: LIGHT — CRACKED (CABIN) · airframe 23,870 hrs · 15,189 cycles

ENTRY DOOR EMER EXIT LIGHT ASSEMBLY & LENS CRACKED. NEF C-6, 120 DAYS. MORE INFORMATION TO COME.

Part: SEAL — MISSING (MEDICAL KIT) · airframe 23,709 hrs · 21,131 cycles

BOTH SEALS ON EMERGENCY MEDICAL KIT MISSING. R & R EMERGENCY MEDICAL KIT IAW AMM 20-00-00.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 23,191 hrs · 20,631 cycles

FLAP FAIL ON DESCENT INTO DTW ABOUT 6000 FEET 200KB. PERFORMED TROUBLE SHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARA H 6 I AMOC DATED JULY 22,2013 & PA AD 27-052N. FOR FECU & LT BPSU R & R, WORK PERFORMED SEE NRCC N60561, N60584, N60600, N60598 & N50826. ALL CHECKED GOOD, OK FOR SERVICE.

Part: SEAL — FAILED (PBE) · airframe 22,200 hrs · 19,638 cycles

FLIGHT DECK PBE VACUUM SEAL BAD. INSPECTED AND FOUND TO BE SERVICEABLE IAW AMM 35-30-00.

Part: BRACKET — DAMAGED (NLG) · airframe 21,592 hrs · 19,022 cycles

ON FLIGHT 3667 (DTW TO CTL) PERFORMED AIR RETURN TO DTW DUE TO NOSE DOOR OPEN AND GEAR DISAGREE MESSAGE. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NOSE LANDING GEAR CENTERED /EXTENDED PROXIMITY SENSOR BRACKET IAW DOWTY CMM 32-20-04. RE-INSTALLED PROXIMITY SENSOR IAW 32-61-05. PERFORMED EXTENSION/RETRACTION CHECK IAW AMM 32-30-00. ALL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,164 hrs · 18,607 cycles

CEILING EMERGENCY FLOOD LIGHT INOPERABLE. REMOVED AND REPLACED EXIT LIGHT BATTERY PACK IAW AMM 33-51-04. SYSTEM OPS CHECK GOOD. THIS CLEARS DEFERRAL 00035 PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,164 hrs · 18,607 cycles

CEILING EMERGENCY EXIT SIGN LIGHT INOPERABLE AT EMERGENCY EXIT ROW. REMOVED AND REPLACED WHITE LENS CAP. OP CHECKS GOOD, DM 00035 CLEARED.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 20,696 hrs · 18,107 cycles

INFANT LIFE VEST BAG OPEN. REPLACE DAMAGED INFANT LIFE VEST IAW CMM 25-60-15.

Part: CONNECTOR — LOOSE (CABIN) · airframe 20,671 hrs · 18,081 cycles

EMERGENCY FLOOR TRACK LIGHTING FROM ROW 9 AND UP INOP. RE-SECURED FLOOR TRACK LIGHTING CONNECTOR AT LAVATORY IAW AMM 33-51-04. ALL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 20,377 hrs · 17,815 cycles

EMERGENCY LIGHTS INOPERATIVE. FOUND SWITCHES LEFT ON. ALLOWED TO CHARGE FOR 20 MINS, OPS CHECKED GOOD OKAY FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 19,819 hrs · 17,273 cycles

ON TAKEOFF ROLL, IDG CAUTION MESSAGE ILLUMINATED AND EXTINGUISHED 2 SECONDS LATER. TAKEOFF CONTINUED ON CLIMBOUT THROUGH 100 FT GEN 2 AND MACH TRIM CAUTION MESSAGES ILLUMINATED FOLLOWED QRH PROCEDURES CAUTION MESSAGES EXTINGUISHED UPON COMPLETION OF QRH. SERVICED IDGS IAW AMM 12-13-24. OPS CHECKED IAW AMM 24-11-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 19,272 hrs · 16,727 cycles

REAR HALF OF FLOOR EMERGENCY LIGHTS INOP. INSPECTED REAR HALF OF FLOOR EMERGENCY LIGHTS IAW AMM 33-50-00. P ROBLEM COULD NOT BE DUPLICATED. OPS CHECK GOOD. A/C OK FOR SVC AT THIS TIME.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,014 hrs · 16,469 cycles

FS 559 SEMI-PRESSURE BULKHEAD CAP ANGLE AT LBL 18 AND AT CHEM-MILLED AREA AT RBL 18 FOUND CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-41-206 REV E AND REO 601R-53-41-609 REV B.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 18,845 hrs · 16,308 cycles

EMERGENCY LIGHTS SMALL FLOOR STRIP INOP. REMOVED AND REPLACED FLOOR EMERGENCY LIGHTS CONNECTOR CABLE FOR ROWS 6, 7, 8 IAW AMM 33-51-01. VERIFIED PART EFFECTIVITY. OPC GOOD. OK FOR SVC.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 18,845 hrs · 16,308 cycles

EMERGENCY LIGHT INOPERATIVE AFT OF EMERGENCY EXIT. RESECURED CONNECTOR, OPS CHECKED GOOD IAW AMM 33-50-00. OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 18,845 hrs · 16,308 cycles

EMERGENCY TRACK FLOOR LIGHTING INOP AFT OF EMERGENCY EXIT ROW ALL THE WAY BACK. RESECURED CONNECTOR O/C GOOD AMM 33-50-00. OK FOR SVC.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,744 hrs · 16,206 cycles

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

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 17,616 hrs · 15,184 cycles

LT WINDSHIELD, OUTER LAYER CRACKED AT FL230. CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE POINT. LT WINDSHIELD REPLACED IAW AMM 56-11-01.

Part: CARGO TRACK — CORRODED (BS 559-621) · corrosion level 2 · airframe 17,458 hrs · 14,993 cycles

CARGO TIE DOWN SEAT TRACKS CORRODED BETWEEN FUSELAGE STATION 559.00+80 TO 559.00+96 AT RIGHT BUTT LINE 27, BETWEEN FUSELAGE STATION 605.00 TO 621.00 AT LEFT BUTT LINE 9 AND BETWEEN FUSELAGE STATION 559.00+80 TO 559.00+96 AT LEFT BUTT LINE 9 AND RIGHT BUTT LINE 9. REMOVED AND REPLACED CARGO TIE DOWN SEAT TRACK IAW CRJ AMM 20-21-00-910-801.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,458 hrs · 14,993 cycles

FS 280.00 BULKHEAD CROSSOVER WEB IS CRACKED AT THE LOWER RADIUS OUTBOARD OF RBL 9 AND LBL 9 AND ITS AFT J-ANGLE IS CRACKED. REPAIRED FS 280.00 FLOOR SUPPORT TRANSVERSE BEAM IAW BOMBARDIER REO 601R-53-11-926 REV B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,458 hrs · 14,993 cycles

CARGO TIE DOWN SEAT TRACK CORRODED BETWEEN FS 559.00+80 TO FS 559+96 AT RBL 27.0, FS 605.00 TO 621.00 AT LBL 9.0 AND FS 559.00+80 TO 559.00+96 AT LBL 9.0 AND RBL 9.0. REMOVED AND REPLACED CARGO TIE DOWN SEAT TRACK IAW CRJ AMM 20-21-00-910-801.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,458 hrs · 14,993 cycles

LEFT BUTT LINE 27.0 FS 605.00 TO FS 621.00 OUTBOARD SIDE FLOORBEAM FLANGE HAS CORROSION. REPAIRED IAW BSC EO 601R-53-20572A.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 17,458 hrs · 14,993 cycles

WHILE ACCOMPLISHING THE REPAIR OF THE INTERCOSTAL AT FS 484.00 LBL 36, A DOUBLE-DRILLED HOLE WAS DRILLED INTO THE PRESSURE BOX BEAM. REPAIRED DAMAGE AT FS 484 LBL 36 IAW BSC EO 601R-53-20536

Part: SKIN — CORRODED (BS 559) · corrosion level 2 · airframe 17,458 hrs · 14,993 cycles

EXTERNAL FUSELAGE SKIN HAS MINOR CORROSION AROUND FASTENERS AT FUSELAGE STATION 559.00+48 BETWEEN STRINGERS 25 LEFT AND 25 RIGHT. REMOVED CORROSION IN ACCORDANCE WITH ENGINEERING ORDER 601R-53-20528.

Part: SKIN — DENTED (TE FLAP) · airframe 17,458 hrs · 14,993 cycles

LT INBOARD FLAP HAS DENT WITH GOUGE ON LOWER SKIN. REPAIRED LT INBOARD FLAP LOWER SKIN IAW BSC EO 601R-57-20551.

Part: FASTENER — CORRODED (TE FLAP) · corrosion level 2 · airframe 17,458 hrs · 14,993 cycles

RT AND LT OUTBOARD FLAP MID HINGE ATTACH HARDWARE CORRODED. INSTALLED NEW HARDWARE IAW CRJ200 AMM 57-53-02-400-803.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,458 hrs · 14,993 cycles

CARGO TIE DOWN SEAT TRACKS CORRODED AT LBL 9.0 AND RBL 9.0 FORWARD OF FS 579.00. INSTALLED NEW CARGO TIE DOWN TRACKS AT AFFECTED LOCATIONS IAW CRJ200 SRM 51-41-04-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,458 hrs · 14,993 cycles

FUSELAGE STATION 333.00 STRINGER 27 HAS MINOR CORROSION. REPAIRED IAW BSC EO 601R-53-20561.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,458 hrs · 14,993 cycles

FS 202.75 PRESSURE BULKHEAD FAILED EDDY CURRENT INSPECTION AT PARKING BRAKE CABLE PASS THROUGH HOLE AT WL 69.684 AND LBL 23.71. INDICATION ON INBOARD SIDE .5"L AND CRACK .6"L AT 1" BELOW FROM A .25"D TOOLING HOLE. REPAIRED FS 202.75 PRESSURE BULKHEAD IAW BSC EO 601R-53-20540A.

Part: SILL — CORRODED (BS 574-621) · corrosion level 2 · airframe 17,458 hrs · 14,993 cycles

CARGO DOOR SILL CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-45-06.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,458 hrs · 14,993 cycles

FS 280.00 FORWARD J-ANGLE CORRODED. INSTALLED NEW J-ANGLE IAW CRJ200 SRM 51-42-08.

Part: STRUT — LOW (NLG) · airframe 17,352 hrs · 14,923 cycles

GEAR DISAGREE. C/W PA 05-018A. PERFORMED FULL NOSE GEAR SERVICE IAW AMM 12-12-32. GEAR RETRACTION SYSTEM TEST OK.

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 17,352 hrs · 14,923 cycles

GEAR DISAGREE. ADJUSTED NLG OLEO EXT/ CTR PROX SWITCH IAW AMM 32-61-05 OK FOR SERVICE SEE DISC NR 2 FOR OPS CHECK FOR GEAR. PERFORMED GEAR SWING IAW AMM 32-30-00 OPS CHECK GOOD OK FOR SERVICE. RECORDED PSEU CODES AS FOLLOWS FLT LEG NR 1 S23 FAR, FLT LEG NR 2 23 FAR, FLT LEG NR 3 S23FAR, S35 FAR, S21 FAR, S22 FAR, S30 FAR, S31 FAR, S32 FAR, DI 14 ON, DI 15 ON.

Part: IDG — LACK OF LUBE (NR 2) · airframe 17,359 hrs · 14,896 cycles

GEN 2 CAME OFF LINE AROUND 80 KIAS SVC NR 2 IDG IAW AMM 12-12-24 OPC OF GEN 2 GOOD. OK FOR SERVICE.

Part: SEAL — MISSING (RT WING) · airframe 16,810 hrs · 14,365 cycles

RIGHT WING TRAILING EDGE P/N 601R10336-130 RAZOR SEAL UNDER THE FLIGHT SPOILER WAS FOUND WITH A PORTION MISSING. THE MISSING PORTION MEASURES 7.88 INCHES IN LENGTH WITH NO OBVIOUS ORIGIN FOR THE DISCREPANCY VISIBLE. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-192 FLY ON 3700 FH WITHIN WHICH TIME RIGHT WING TRAILING EDGE P/N 601R10336-130 RAZOR SEAL MUST BE REPLACED WITH A SERVICEABLE SEAL. REPEAT INSPECTION EVERY 600 FH.

Part: BPSU — FAILED (TE FLAP) · airframe 16,529 hrs · 14,091 cycles

FLAPS FAIL AT 11 DEGREES CLIMBING OUT OFF DTW 170 KNOTS 2000FT. 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. REMOVED AND REPLACED RT BPSU IAW CRJ 200 AMM 27-51-10. OPC GOOD. OK FOR SERVICE. FECU FLIGHT LEG 14129, LRU LOG-RT BPSU, FECU, RT BPSU WIRING. FAULT LOG-5 1A,52 A,12 1B, 12 2B.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS)

ON APPROACH WHEN FLAPS SELECTED DOWN, RECEIVED (FLAPS FAIL) MESSAGE. QRH FOLLOWED WITH UNEVENTFUL LANDING. FLAP SYS RESET AND PLACED ON 72 HOUR WATCH IAW AD2006-12-21. (K)