N800AY

Part: CLEAT — CRACKED · airframe 30,902 hrs · 28,823 cycles

CLEAT CRACKED COMMON TO EXTERNAL SERVICE PANEL. CA: REMOVED, LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE BRACKET, IAW CRJ200 SRM TASKS 51-42-06 AND 51-40-11.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 30,902 hrs · 28,823 cycles

FS 280 WEB IS CORRODED BETWEEN RBL 9 AND LBL 9. CA: REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B DATED 2006/05/10.

Part: FRAME — CORRODED (BS 589) · airframe 30,902 hrs · 28,823 cycles

FRAME AT FS 589 CORRODED BETWEEN STGR 24R AND STGR 24L. REMOVED AND REPLACED FRAME SECTOR, IAW CRJ 200 SRM 51-42-06 AND 51-42-21. LEAK CHECK OF MIX MANIFOLD CHECK GOOD. NO DEFECTS NOTED AT THIS TIME, IAW CRJ 200 AMM 21-20-00-790-801.

Part: CHANNEL — CORRODED (SERVICE DOOR) · airframe 30,902 hrs · 28,823 cycles

SERVICE DOOR BOTTOM CHANNELS AT CENTER SPLICE ARE CORRODED. REPLACED CORRODED SPLICE ANGLES AT SERVICE DOOR BOTTOM CHANNELS, IAW EA NR CRJ252-10846, EA NR CRJ252-10847, CRJ200 SRM'S 51-40-11-00, 51-42-06, 51-42-13.

Part: DOOR SILL — CORRODED (BS 310-349) · airframe 30,902 hrs · 28,823 cycles

PAX DOOR FLOOR SILL ANGLE IS CORRODED BETWEEN FS 310 TO FS 349. REMOVED SERVICEABLE FLOOR SILL ANGLE. LOCATED AND DRILLED FLOOR SILL ANGLE, IAW CRJ200 SRM 51-40-11.

Part: FLOORBEAM — CORRODED (BS 319) · airframe 30,902 hrs · 28,823 cycles

DOUBLER ON TOP OF FLOOR BEAM CAP AT FS 319 AT RBL 5 IS CORRODED. REMOVED AND INSTALLED NEW FABBED DOUBLER PLATE, IAW CRJ 200 SRM 51-42-13.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 30,902 hrs · 28,823 cycles

SEAT TRACK SEGMENT AT RBL 9 BETWEEN FS 409+128 TO FS 559 IS CORRODED. REMOVED AND REPLACED FABRICATED SEAT TRACK, IAW CRJ 200 MM 53-01-11-400 -802 AND REO 601R-53-00-485.

Part: SKIN — CORRODED (PAX DOOR) · airframe 30,902 hrs · 28,823 cycles

PAX DOOR INNER SKIN HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED PAX DOOR INNER SKIN, IAW CRJ200 SRM'S 51-42- 51-42-21, 51-42-10, 51-42-13 AND 51-42-22.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 30,902 hrs · 28,823 cycles

PAX DOOR INTERCOSTAL DD4 CORRODED BETWEEN FS 320.163 AND FS 338.963. INSTALLED NEW INTERCOSTAL DD4 ON PAX DOOR BETWEEN FS 320.163 AND FS 338.963, IAW CRJ200 SRM'S 51-42-06 AND 51-42-21. AFTER REMOVING CORRODED INTERCOSTAL AT DD4, IAW CRJ200 SRM'S 51-42-06 AND 51-42-21.

Part: BULKHEAD — CRACKED (BS 621) · airframe 30,902 hrs · 28,823 cycles

INDICATION NOTED AT BL 0.00, WL 114, 3.7" IN LENGTH, FS 621 REAR PRESSURE BULKHEAD. REPAIRED 621 BULKHEAD AT BL 0.00 WL 114, IAW MHIRJ REO 601R-53-61-1285, REV E DATED 10/31/16. NO DEFECTS NOTED. THIS IS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 30,902 hrs · 28,823 cycles

SEAT TRACK SEGMENT AT LBL 9 BETWEEN FS 409+128 TO FS 559 IS CORRODED. REMOVED UNSERVICEABLE SEAT TRACK. FABRICATED AND INSTALLED SERVICEABLE SEAT TRACK 9 LBL 9 BETWEEN 409 + 128-559 (FS), IAW CRJ200 AMM 53-01-11-020-002/53-01-11-400-802 AND MHIRJ REO 601R-53-00-485 REV D, DATED 2018-01-29. NO DEFECTS NOTED.

Part: ANGLE — CORRODED (BS 319-345) · airframe 30,902 hrs · 28,823 cycles

PAX DOOR SURROUND STRUCTURE CAP ANGLE BETWEEN FS 319.70 AND FS 345 CORRODED ON MULTIPLE CROSS ANGLE. REMOVED AND REPLACED CAP ANGLE AT PAX DOOR SURROUND STRUCTURE FLOOR SILL, IAW CRJ 200 SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 497-544) · airframe 30,902 hrs · 28,823 cycles

RIGHT SIDE SEAT RAIL SEGMENT NO 6 BETWEEN FS 499 TO FS 544 IS CORRODED. REMOVED, FABRICATED AND INSTALLED RIGHT SIDE SEAT RAIL SEGMENT AT FS 497 TO FS 544, IAW MHIRJ REO 601R-53-00-055 REV C DATED 2017-03-21 REPAIR B.

Part: INTERCOSTAL — CORRODED (BS 320-338) · airframe 30,902 hrs · 28,823 cycles

PAX DOOR INTERCOSTAL DD6 CORRODED BETWEEN FS 320.163 AND 338.963. REMOVED AND REPLACED DD6 INTERCOSTAL, IAW CRJ200 SRM 51-42-06 AND 51-42-21. NO DEFECTS NOTED.

Part: FRAME — CORRODED (BS 605) · airframe 30,902 hrs · 28,823 cycles

FRAME AT FS 605 CORRODED BETWEEN STGR 18R AND STGR 24L. BLENDED AREAS ON 605 FRAME LISTED ABOVE, IAW CRJ 200 SRM 51-21-06, 53-61-15, 53-00-00 & 51-25-00. NO DEFECTS NOTED, WITHIN LIMITS.

Part: STRAP — CORRODED (BS 559) · airframe 30,902 hrs · 28,823 cycles

STRAP IS CORRODED BETWEEN LBL 36 TO LBL 27 AT FS 559. REMOVED AND REPLACED STRAP LOCATED BETWEEN LBL 36 TO LBL 27 AT FS 559, IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-40-11.

Part: FAIRING — DETACHED (RT INBOARD) · airframe 28,420 hrs · 26,152 cycles

ON DEPARTURES THROUGH 10,000 AIRCRAFT MADE A THUMP ASSOCIATED WITH A VIBRATION WHICH WAS FELT IN THE FLIGHT CONTROL, PERFORMED AN AIR RETURN TO DEPARTURE AND DISCOVERED RIGHT WING INBOARD FAIRING BROKEN/MISSING. REPLACED RH INBOARD FAIRING, OUTBOARD AND AFT FLAP ARM ASSY BRACKETS IAW ENGINEERING DRAWINGS 601R14116, 601R14100 AND SRM 51-42-13, 51-42-06, AND 51-42-14. REMOVED AND REPLACED RH INBOARD FWD AND AFT HINGE FAIRING IAW AMM 57-55-01

Part: BULKHEAD — CRACKED (BS 621) · airframe 28,041 hrs · 25,739 cycles

AFT PRESSURE BULKHEAD HAS A CRACK IN THE WEB UNDER LINER SUPPORT AT RBL 9.50 APPROX WL 78.5. DOT 262A001 REPAIRED AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1285 AND REO # 601R-53-61-6758 AAR SM-139

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,041 hrs · 25,739 cycles

EMERGENCY LIGHTS BATTERY PACK #1 IS DEAD/INOP REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK #1 IAW CRJ 200 AMM 33-51-04 OPS CHECK GOOD IAW CRJ 200 AMM 33-51-04-710-801 AAR AP 344

Part: TORQUE BOX — CRACKED (THRUST REVERSER) · airframe 28,041 hrs · 25,739 cycles

#1 ENGINE T/R TORQUE BOX CRACKED ARE HI- LITE FASTNER ON AFT FLANGE @ 6 O'CLOCK POSITION. REPAIRED CRACK IAW ENDEAVOR EA CRJ 254-07814 REV IR AAR SM-35

Part: FRAME — CRACKED (BS 333) · airframe 28,041 hrs · 25,739 cycles

FRAME BS 333 IS CRACKED JUST I/B OF STGR 2L, IN THE CABIN. REPAIRED FRAME 333 JUST I/B OF STRINGER 2L IAW CRJ 200 EA CRJ-253-07892 ARR-SM-107

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 28,041 hrs · 25,739 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513 TYPE 11 AAR SM-23

Part: LATCH — CRACKED (DOOR) · airframe 28,041 hrs · 25,739 cycles

UPPER NOSE COMPARTMENT DOOR HAS CRACK AT LATCH. REPAIRED CRACK ON UPPER NOSE COMPARTMENT DOOR IAW EA NO CRJ 253-07855 AAR SM-33

Part: BRACKET — CRACKED (LT WING) · airframe 28,041 hrs · 25,739 cycles

LEFT WING FRONT SPAR CENTER LEADING EDGE HAS CRACK ON CORNER REMOVED AND REPLACED LEFT WING FRONT SPAR CENTER LEADING EDGE BRACKET IAW CRJ 200 SRM 51-42-06

Part: FRAME — CRACKED (BS 605) · airframe 28,041 hrs · 25,739 cycles

FRAME 605 IS CRACKED ON THE FWD SIDE JUST ABOVE AND BELOW STGR 9L, IN THE CARGO BAY. REPAIRED FRAME 605 AT STGR 9L IAW BOMBARDIER REO 601-53-61-5214 AAR AP-377

Part: FLOOR SUPPORT — CORRODED (BS 260-280) · airframe 28,041 hrs · 25,739 cycles

LH FLOOR LANDING AT LBL 9 HAS CORROSION BETWEEN FS 280 AND FS 260, IN THE FLT DECK. REMOVED AND REPLACED L/H FLOOR LANDING AT LBL9 BETWEEN FS 280 & FS 260 IAW CRJ 200 SRM 51-42-21 51-42-06 AAR SM-107

Part: FLOOR SUPPORT — CORRODED (BS 260-280) · airframe 28,041 hrs · 25,739 cycles

RH FLOOR LANDING AT RBL 9 HAS CORROSION BETWEEN FS 280 AND FS 260, IN THE FLT DECK. REMOVED AND REPLACED R/H FLOOR LANDING @RBL9 BETWEEN FS 280-FS260. I.A.W. CRJ-200 SRM 51-42-06 AND 51-42-21 AAR SM-107

Part: BRACKET — CRACKED (RT WING) · airframe 28,041 hrs · 25,739 cycles

RH WING LEADING EDGE FRONT SPAR IB REFUEL BRACKET HAS A CRACK REMOVED AND REPLACED REFUEL BRACKET IAW CRJ 200 SRM 51-41-02 AND 51-42-06

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 28,041 hrs · 25,739 cycles

RIGHT WING L/E @ WS149.58 HAS CRACKED CORNER BRACKET REMOVED AND REPLACED RIGHT WING L/E CORNER BRACKET AT WS 149.58 IAW CRJ 200 SRM 51-41-02

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 28,041 hrs · 25,739 cycles

LT SIDE SEAT RAIL STICK 7 GOUGED AND CORRODED MULTIPLE AREAS. REMOVED AND REPLACE NR 7 LT SIDE RAIL IAW AMM 53-01-11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 28,041 hrs · 25,739 cycles

FLOOR ANGLE STRIP ON THE FWD SIDE OF BEAM 280 IS CRACKED IN 2 SPOTS, JUST I/B OF LBL 9 AND RBL 9, IN THE VERY FWD E & E BAY. REMOVED AND REPLACED FLOOR ANGLE IAW CRJ 200 SRM 51-42-21 AAR SM-107

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 28,041 hrs · 25,739 cycles

LH FLOOR SEAT RAIL STICK 5 GOUGED AND CORRODED SEVERAL LOCATIONS. REMOVED AND REPLACED L/H FLOOR SEAT RAIL STICK # 5 IAW CRJ 200 AMM 53-01-11 AAR SM-107

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 28,041 hrs · 25,739 cycles

LT SIDE SEAT RAIL STICK 5 GOUGED AND CORRODED MULTIPLE AREAS. REMOVED AND REPLACED NR 5 LT SEAT RAIL IAW AMM 53-01-11.

Part: SEAT TRACK — GOUGED (BS 379-409) · airframe 28,041 hrs · 25,739 cycles

LH SIDE SEAT RAIL STICK 1 GOUGED AND CORRODED MULTIPLE AREAS. REMOVED AND REPLACED SEAT RAIL IAW CRJ 200 AMM 53-01-11. AAR SM-58

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 28,041 hrs · 25,739 cycles

LH FLOOR SEAT RAIL STICK 2 GOUGED AND CORRODED. REMOVED AND REPLACED L/H FLOOR SEAT RAIL STICK # 2 IAW CRJ 200 AMM 53-01-11

Part: SEAT TRACK — CORRODED (BS 379-409) · airframe 28,041 hrs · 25,739 cycles

RH SIDE SEAT RAIL STICK 2 GOUGED AND CORRODED MULTIPLE AREAS. REMOVED AND REPLACED SEAT RAIL IAW CRJ 200 AMM 53-01-11. AAR SM-58

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 28,041 hrs · 25,739 cycles

RH SIDE FLOOR SUPPORT HAS CORROSION FS559.00 REMOVED AND REPLACED RH SIDE FLOOR SUPPORT (STRAP) IAW CRJ 200 SRM 51-42-06

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 28,041 hrs · 25,739 cycles

RT SIDE SEAT RAIL STICK 7 GOUGED AND CORRODED MULTIPLE AREAS. REMOVED AND REPLACED NR 7 RT SEAT RAIL IAW AMM 53-01-11.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 28,041 hrs · 25,739 cycles

LH SIDE FLOOR SUPPORT HAS CORROSION FS559.00 REMOVED AND REPLACED LH SIDE FLOOR SUPPORT IAW CRJ 200 SRM 51-42-06 AAR-R S/M4

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 28,041 hrs · 25,739 cycles

LH SIDE SEAT RAIL STICK 5 CORRODED MULTIPLE AREAS. REMOVED AND REPLACED SIDEWALL SEAT TRACK L/H # 5 IAW CRJ 200 AMM 53-01-11

Part: SEAL — MISSING (PBE) · airframe 27,959 hrs · 25,654 cycles

FA PBE MISSING 1 SEAL. REPLACED FA PBE MISSING SEAL IAW AMM 25-60-00.

Part: DUCT — DISPLACED (ANTI-ICE SUPPLY) · airframe 27,852 hrs · 25,514 cycles

RT 14TH DUCT WARNING MESSAGE. QRH COMPLETED. MESSAGE PERSISTED AFTER 40 SECONDS. RIGHT THRUST LEVER REDUCED TO IDLE. LANDING AT FLAPS 20, ON TOUCHDOWN. FOUND THE RT ENGINE COWL ICE, 14TH STG SUPPLY DUCT CLAMP ALIGNMENT OFF. INSTALLED THE SEAL, ALIGNED THE DUCT & SECURED THE CLAMP. PERFORMED A GROUND RUN, OPS & LEAK CHECKED GOOD. COMPLIED WITH AMM 71-00-00-4.

Part: FIRE WARNING — FALSE INDICATION (LAVATORY) · airframe 27,207 hrs · 24,821 cycles

SMOKE TOILET EICAS & WARNING HEARD, FA CHECKED THE LAVATORY. NO SMOKE NOTED. MESSAGE & WARN WENT AWAY ON ITS OWN AFTER 60 SECONDS. PERFORMED OPS CHECK OF THE LAVATORY SMOKE DETECTION SYSTEM. OPS CHECKED GOOD. NO MESSAGES NOTED. ACFT OKAY FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 27,053 hrs · 24,659 cycles

CO-PILOT`S FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT IAW AMM 25-61-00, OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 26,327 hrs · 23,889 cycles

PILOT FLASHLIGHT BATTERY DEAD. R & R THE BATTERY IAW AMM 25-61-00. OPS TESTED GOOD.

Part: OXYGEN MASK — NO TEST (FIRST OFFICER'S) · airframe 25,603 hrs · 23,107 cycles

FIRST OFFICER`S OXYGEN MASK NOT TESTING CORRECTLY. REMOVED AND REPLACED THE OXYGEN MASK STOWAGE BOX AND OXYGEN MASK IAW AMM 35-11-15, AND AMM 35-11-12. OPS & LEAK CHECKED GOOD. SERVICED CREW OXYGEN IAW AMM 12-16-35 TO 1850 PSI.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 25,281 hrs · 22,767 cycles

FOUND EMERGENCY LIGHT LEFT ON EMERGENCY LIGHTS INOPERATIVE. CHARGED THE BATTERY PACK AND PERFORMED OPS CHECK IAW AMM 33-51-00, OPS GOOD.

Part: BULKHEAD — CRACKED (BS 202) · airframe 24,448 hrs · 21,919 cycles

BRAKE CABLE PASSAGE HOLE IS CRACKED ON INBD SIDE AT BS 202.75 BL 23.71. CUT OUT DAMAGE, FABRICATED, AND INSTALLED A REPAIR IAW REO 601R-53-11-2941 AND REO 601R-53-11-563 TYPE 5 REV C. OPS CHECKED GOOD IAW AMM 32-45-00-710-801.

Part: ANGLE — CRACKED (BS 625) · airframe 24,448 hrs · 21,919 cycles

ANGLE AT BS 625 STRINGER 14L IS CRACKED. REMOVED & REPLACED IAW SRM 51-42-21 & REO 601R-53-61-5265. LEAK CHECKED GOOD IAW AMM 52-31-00-710-801.

Part: SHIELD — CRACKED (LT NACELLE) · airframe 24,448 hrs · 21,919 cycles

LEFT ENGINE UPPER CORE COWL FIRE SHIELD IS CRACKED. REPLACED FIRE SHIELD IAW CMM 71-12-01.

Part: HANDLE — CRACKED (E/E BAY DOOR) · airframe 24,448 hrs · 21,919 cycles

AVIONIC BAY DOOR HANDLE IS CRACKED, DISCOVERED DURING EDDY CURRENT SDI JC 52-800-201. REMOVED AND REPLACED THE AVIONIC BAY DOOR HANDLE IAW SRM 51-42-21. OP CHECEKD GOOD IAW 52-20-08-710-801.

Part: SEAT TRACK — DAMAGED (MAIN CABIN) · airframe 24,448 hrs · 21,919 cycles

IN THE MAIN CABIN, SEAT TRACK NR 4 HAS MULTIPLE GOUGES AND CORROSION. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-01-11.

Part: SEAT TRACK — DAMAGED (MAIN CABIN) · airframe 24,448 hrs · 21,919 cycles

MAIN CABIN SEAT TRACK NR 2 AT LBL 9 IS CORRODED AND GOUGED IN MULTIPLE AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-01-11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,448 hrs · 21,919 cycles

MAIN CABIN FLOORBEAM AT BS 280 IS CRACKED AT LBL 13. REPAIRED THE FLOORBEAM3 IAW REO 601R-53-11-171.

Part: SEAT TRACK — DAMAGED (MAIN CABIN) · airframe 24,448 hrs · 21,919 cycles

MAIN CABIN SEAT TRACK NR 5, HAS MULTIPLE GOUGES AND CORROSION. REMOVED CORROSION IAW 51-21-06, REMOVED GOUGES IAW 51-12-00. FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED, RESTORED FINISH, AND INSTALLED IAW REO 601R-53-00-4850.

Part: ANGLE — CRACKED (BS 625) · airframe 24,448 hrs · 21,919 cycles

ANGLE AT BS 625, STRINGER 15L IS CRACKED. REMOVED AND REPLACED IAW SRM 51-42-21 & REO 601R-53-61-5265.

Part: SEAT TRACK — DAMAGED (MAIN CABIN) · airframe 24,448 hrs · 21,919 cycles

MAIN CABIN SEAT TRACK NR 6 HAS MULTIPLE GOUGES AND CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49 AND REO 601R-53-00-485 REV. B.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,448 hrs · 21,919 cycles

MAIN CABIN FLOORBEAM BS 280 IS CRACKED AT RBL 13. REPAIRED THE FLOORBEAM IAW REO 601R-53-11-171.

Part: ANGLE — CRACKED (BS 625) · airframe 24,448 hrs · 21,919 cycles

ANGLE AT BS 625 STRINGER 16L IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21 & REO 601R-53-61-5265.

Part: INTERCOSTAL — CRACKED · airframe 24,448 hrs · 21,919 cycles

LEFT OBLIQUE INTERCOSTAL IS CRACKED. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-06.

Part: STIFFENER — CRACKED (EXHAUST FAIRING) · airframe 24,448 hrs · 21,919 cycles

EXHAUST FAIRING 446AL HAS CRACKED STIFFINER SECOND FROM FWD END. REPAIRED THE STIFFINER IAW CMM 78-11-00.

Part: PIN — DAMAGED (PAX DOOR HINGE) · airframe 24,448 hrs · 21,919 cycles

ENTRY DOOR HINGE ON DOOR SIDE, RETENTION PIN HOLE ON AFT SIDE ELONGATED AND RETENTION PIN BROKEN AND POSSIBLY MISSING. REPAIRED PAX DOOR HINGE RETAINING PIN HOLE PER REO 601R-52-11-2347. RETAINING PIN TO BE INSTALLED ON W/O 1013245-8000-0024 S/N 4805872. AAR EMP 8930

Part: BULKHEAD — CRACKED (BS 621) · airframe 24,448 hrs · 21,919 cycles

REAR PRESSURE BULKHEAD FORWARD FACE HAS A CRACK AT LBL 27.50 AT THE END OF THE CARGO DOOR TRACK APPROX 1/4" LONG. REPAIRED DAMAGE AND RESTORED FINISH IAW REO 601R-53-61-1541 AND SRM 51-25-16.

Part: FITTING — CRACKED (WINDOW POST) · airframe 24,448 hrs · 21,919 cycles

CO-PILOTS WINDSHIELD SIDE POST LOWER AFT FITTING CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (WINDOW POST) · airframe 24,448 hrs · 21,919 cycles

PILOTS WINDSHIELD SIDE POST LOWER AFT FITTING CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-21.

Part: NOSE COWL — CHAFED (LT ENGINE) · airframe 24,448 hrs · 21,919 cycles

LEFT ENGINE UPPER NOSE COWL T/E CHAFED. REMOVED & REPLACE T/E STRIP IAW CMM 71-14-01-99F-020-A01.

Part: SEAL — WORN (EXHAUST FAIRING) · airframe 24,448 hrs · 21,919 cycles

LEFT ENGINE EXHAUST FAIRING FWD SEALS WORN. REPLACED WORN SEALS IAW CMM 78-11-00, 20-42-06, & 20-42-20.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 24,363 hrs · 21,835 cycles

AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. AN EMERGENCY WAS DECLARED. FOUND AFT CARGO DOOR OPEN AT TOP OF DOOR WHEN ACFT ARRIVED BACK AT GATE, HANDLE WAS STOWED. ACFT PRESSURIZED WITHOUT DEFECT IAW AMM 21-31-10

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 22,183 hrs · 19,601 cycles

INFANT LIFE VEST EXPIRES 1-2016, BAG TORN OPEN. R & R INFANT LIFE VEST IAW AMM 25-61-03.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,152 hrs · 19,565 cycles

ALL EMER LIGHTS ARE INOPERATIVE. R & R ALL 4 EMER BATTERY PACKS IAW AMM 33-51-04. OPERATIONS CHECK PASSED.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 22,106 hrs · 19,523 cycles

FLAPS FAIL, FAILED TO SET FOR TAKEOFF. PERFORMED TROUBLESHOOTING IAW FIM CHAPTER 27-50-00 REV 47 IAW AD 2009-06-12 PARAGRAPH H 6 I. AMOC DATED APRIL 22, 2014 & TS 001100-2014 FIM TECHNICAL SUPPLEMENT. FOUND 2 CB'S PULLED, CBP-1 B5 PDU1 & CBP-2 B5 PDU2. RESET THE ABOVE CB'S & RESET SKEW DETECTION UNIT IAW AMM 27-51-15. FLAPS CYCLED 3 TIMES, NO DEFECTS NOTED. FLAPS OPERATIONS CHECKED GOOD IAW AMM 27-54-00.

Part: FITTING — OUT OF ADJUST (EMERGENCY EXIT) · airframe 21,447 hrs · 18,864 cycles

RIGHT OVERWING EMER EXIT FAILED FUNCTIONAL TEST. PERFORMED ADJUSTMENT OF TWO RT UPPER DOOR LATCH FITTINGS IAW AMM 52-21-00. FUNCTIONAL CHECKED GOOD, NO DEFECTS NOTED IAW AMM 52-21-00-720-801.

Part: FITTING — OUT OF ADJUST (EMERGENCY EXIT) · airframe 21,447 hrs · 18,864 cycles

LEFT OVERWING EMER EXIT FAILED FUNCTIONAL TEST. PERFORMED ADJUSTMENT OF THE TWO UPPER DOOR LATCH FITTINGS IAW AMM 52-21-00. FUNCTIONAL CHECKED GOOD, NO DEFECTS NOTED IAW AMM 52-21-00-720-801.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 21,442 hrs · 18,860 cycles

LEFT WING LOWER PLANK AT LANDING FOR FUEL PANEL 510AB CORRODED 0.007 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 21,442 hrs · 18,860 cycles

RIGHT WING LOWER PLANK LANDING FOR PANEL 640DB CORRODED. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 21,442 hrs · 18,860 cycles

RIGHT WING LOWER PLANK LANDING FOR FUEL ACCESS PANEL 640CB CORRODED 0.003 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 21,442 hrs · 18,860 cycles

RIGHT WING LOWER PLANK LANDING FOR FUEL ACCESS PANEL 650 AB & WS 163 FOUND CORRODED. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 21,442 hrs · 18,860 cycles

LEFT WING LOWER PLANK AT LANDING FOR FUEL ACCESS PANEL 550BB CORRODED 0.004 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 21,442 hrs · 18,860 cycles

LEFT WING LOWER PLANK AT LANDING FOR FUEL ACCESS PANEL 550AB CORRODED 0.005 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 21,442 hrs · 18,860 cycles

RIGHT WING LOWER PLANK LANDING FOR FUEL ACCESS PANEL 640 EB & WS 116.366 FOUND CORRODED. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 21,442 hrs · 18,860 cycles

RIGHT WING LOWER PLANK LANDING FOR FUEL ACCESS PANEL 640 FB & WS 136.676 FOUND CORRODED. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 21,442 hrs · 18,860 cycles

LEFT WING LOWER PLANK LANDING FOR FUEL ACCESS PANEL 540AB CORRODED 0.003 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.

Part: RIB — CRACKED (RT WING) · airframe 21,442 hrs · 18,860 cycles

RIGHT WW OTBD BATTERY RIB CRACKED. REPAIRED IAW REO 601R-57-51-046.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 21,442 hrs · 18,860 cycles

FS 621 BULKHEAD STIFFENER AT BL 0 CHAFED FROM VLV. REPAIRED IAW REO 601R-53-61-1523.

Part: ACCESS PANEL — CHAFED (RT AILERON) · airframe 21,442 hrs · 18,860 cycles

RIGHT AILERON ACCESS PANEL 699AB CHAFED. REPAIRED IAW SRM 57-60-00.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 21,442 hrs · 18,860 cycles

FS 621 BULKHEAD FWD FACE CHAFED IN MULTIPLE LOCATIONS BETWEEN LBL 24 & RBL 36.2, WL 87.10 & WL 126.43. REPAIRED IAW REO 601R-53-61-2155.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,045 hrs · 18,462 cycles

RIGHT EMER LIGHT NR 4 INOPERATIVE, EXTERIOR RT AFT. R & R RT AFT EXTERNAL EMER LIGHT IAW AMM 33-51-21. OPERATIONS CHECKED GOOD. THIS CLEARS DM 05211, PLACARD REMOVED.

Part: LENS — CRACKED (EXIT SIGN) · airframe 21,040 hrs · 18,458 cycles

EXIT SIGN LENS ON LT WINDSCREEN & ABOVE SERVICE DOOR ARE CRACKED. REPLACE EXIT SIGN LENS.

Part: LANDING GEAR — OBSTRUCTED (MAIN) · airframe 20,605 hrs · 18,015 cycles

GEAR UP DISAGREE, RAN THE QRH CHECKLIST & RECEIVED 3 GREEN RETURNED TO DTW, 2 MAIN GEAR SHOWED DOWN WHEN HANDLE SELECTED UP. COMPLIED WITH PA 05-018 REV K SCENARIO 1. REMOVED SNOW & ICE CONTAMINATION. PERFORMED GEAR SWINGS IAW AMM 32-30-00. CHECKED RIGGING OF $18 & $20 IAW AMM 32-61-05, ALL CHECKED GOOD, SEE N24204 FOR GVI & SNOW.

Part: ANGLE — CRACKED (BS 559) · airframe 19,357 hrs · 16,795 cycles

CRACK FOUND IN CAP ANGLE FS 559 RBL 18. REPAIRED IAW PA 53-025C, AND REOS 601R-53-41260, 601R-53-41-609, AND 601R-53-41-1707.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 18,765 hrs · 16,207 cycles

DURING ROUTINE LINE MAINTENANCE AT EWR MAINTENANCE FOUND CHAFE DAMAGE TO THE CARGO DOOR OUTER SKIN, AT THE TOP OF THE DOOR. REPAIRED IAW EA CRJ252-01332 AND ASSOCIATED 8110-3.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,765 hrs · 16,207 cycles

AFT PRESSURE BULKHEAD AT FS 621 FOUND CRACKED BEHIND INBOARD UPPER CORNER OF THE MACHINED FITTING ATTACHED TO THE CARGO DOOR LINTEL MEASURING 0.1" IN LENGTH. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,765 hrs · 16,207 cycles

AFT BLUE CALL LIGHT ON CENTER CABIN EMERGENCY EXIT SIGN IS INOPERABLE. REMOVED AND REPLACED BULB PN 6839 AS REQUIRED. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,692 hrs · 16,137 cycles

FLIGHT ATTENDANT'S FLASHLIGHT INOPERABLE. REMOVED AND REPLACED FLIGHT ATTENDANT'S FLASHLIGHT BATTERY IAW AMM 25-61-00. OPS CHECK GOOD. THIS CLEARS DI#001931, REMOVED FROM MM02.

Part: TARGET — LOOSE (LT MLG) · airframe 18,392 hrs · 15,833 cycles

ON APPROACH INTO DTW (FLIGHT 3867) RECEIVED FLIGHT GEAR DISAGREE MESSAGE FOR THE LEFT MAIN GEAR RED NOSE AND RIGHT MAIN UP RAN. CYCLED GEAR ONCE AND RECEIVED 3 GREEN NORMAL AND LANDED AT DTW. FOUND LEFT MAIN LANDING GEAR UPLOCK TARGET LOOSE. RE-ADJUSTED TARGET AND INSTALLED WASHER IAW CMM 32-30-15. PERFORMED GEAR RETRACTION EXTENSION IAW AMM 32-30-00. OPS CHECK GOOD.

Part: FIRE BOTTLE — LOW PRESSURE (COCKPIT) · airframe 18,294 hrs · 15,738 cycles

DURING ROUTINE CHECK FOUND FLIGHT DECK PORTABLE FIRE EXTINGUISHER CHARGE LOW. REPLACED FLIGHT DECK PORTABLE FIRE EXTINGUISHER IAW CRJ 200 AMM 26-23-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,187 hrs · 15,637 cycles

LBL 27 IN CARGO AREA HAS CORROSION AROUND SCREW HOLES UPON CORROSION REMOVAL, FLOORBEAM FOUND TO BE OUT OF LIMITS. REPAIRED IAW BOMBARDIER REO 601R-53-61-3778.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 18,187 hrs · 15,637 cycles

AFT PRESSURE BULKHEAD (FS 621) FORWARD FACE HAS CHAFES AT LBL 8 - 13" ABOVE FLOOR, LBL 27, LBL 18, LBL 8, LBL 9, RBL 18, RBL 27, AND RBL 36 AT 30" ABOVE THE FLOOR. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: GLOWSTRIP — WORN (CABIN) · airframe 17,820 hrs · 15,267 cycles

8AB PHOTOLUMINESCENT STRIPS WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS AT 8AB IAW AMM 33-51-01.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 16,966 hrs · 14,459 cycles

ABORTED T/O FOR WING ANTI ICE CAUTION. PLACED ON MEL.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 16,552 hrs · 14,102 cycles

IN FLIGHT ON DESCENT BETWEEN 12000FT AND 4000FT WITH ENGINES AT FLT IDLE 'LOW PRESS' CAUTION POSTED. FUEL SYNOPTIC PAGE SHOWED SEGMENT AFTER FILTER IN YELLOW. OPS CHECKED IAW CRJ AMM 73-31-06. OPS CHECKS NORMAL AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,494 hrs · 14,038 cycles

"L FUEL LO PRESS" CAUTION FOR APPROX 2 MINUTES ON DESCENT. RAN QRH. ENGINE INDICATIONS NORMAL. OPS CHECKED "L FUEL LO PRESS" IAW CRJ AMM 28-23-01. NO DEFECTS NOTED. OPS CHECKS NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (FUEL SYSTEM) · airframe 16,380 hrs · 13,885 cycles

LEFT LOW FUEL PRESSURE CAUTION ILLUMINATES WHEN THRUST LEVERS ARE SET TO IDLE DURING FLIGHT. OPC OF LT FUEL LOW PRESS IAW AMM 73-31-06. OPC NORMAL, A/C OK FOR SERVICE.

Part: WARNING LIGHT — FALSE INDICATION (LT ENGINE) · airframe 16,231 hrs · 13,737 cycles

LEFT ENGINE FUEL LOW PRESSURE IN FLIGHT CAUTION AT FLIGHT IDLE. COULD NOT DUPLICATE DISCREPANCY DO FAULT FOUND, MSG CLEARED. OPS CHECK GOOD IAW AMM 28-42-04. A/C OK FOR SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 16,192 hrs · 13,695 cycles

DURING DESCENT AT 26,000FT WITH N1 AT 50 PERCENT GOT FUEL LO PRESS MSG EVENTUALLY CLEARED. PER FIM : VERIFIED LT ENG FUEL SOV IS IN OPEN POS IAW AMM 28-21-07. AC OK FOR SERVICE.

Part: SKIN — DENTED (SPOILER) · airframe 14,366 hrs · 11,969 cycles

RT INBOARD GROUND SPOILER UPPER SKIN HAS SEVERAL DENTS ON THE INBOARD CHEM-MILLED AREA, NONE GREATER THAN .009 DEEP. PERFORMED A MAJOR REPAIR TO THE RT WING INBOARD GROUND SPOILER IAW BOMBARDIER SERVICES CORPORATION ENGINEERING ORDER 601R-57-19976.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,850 hrs · 3,627 cycles

FLAP FAILURE INDICATION AFTER PUSHBACK. SYSTEM RESET AND PLACED ON 72 HOUR WATCH IAW AD 2006-12-21.

Part: CONTROL SYSTEM — FAILED (TE FLAPS)

(REF NR: 05-065) FLAPS FAILED AT 30 ON APPROACH. RESET SYSTEM, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. (K)