N836AY

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,929 hrs · 23,971 cycles

FWD OVERWING EMERGENCY EXIT BULB IS INOP REMOVED AND REPLACED BULB IAW AMM 33-51-21 OPS CHECK GOOD

Part: BEAM — CRACKED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

FS 280 BEAM CRACKED ON LOWER SIDE OUT BOARD OF RBL 9 (TYP). REPAIRED PER GREO 601R-53-11-171 REV "D".

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

FUSELAGE SKIN CRACKED 2 PLACES AT NOSE MLG CUTOUT RADIUS @ FS 235. REPAIRED PER CREO 601R-53-11-048 REV "D".

Part: WEB — CRACKED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

FWD EQUIPMENT COMPARTMENT FLOOR-WEB CRACKED AT LT FS 191. REPAIRED PER GREO 601R-53-11-081.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

SUPPLEMENTAL INFORMATION FS 621/ LBL27 FLOORBEAM FITTING IS CORRODED. REPAIRED FLOORBEAM.

Part: SKIN — CHAFED (EXHAUST NOZZLE) · airframe 22,929 hrs · 22,927 cycles

LT ENG EXHAUST NOZZLE EXT SKIN HAS FRETTING FROM CONTACT WITH PYLON SEAL. PERFORMED EXHAUST SKIN AND DOUBLER REPAIR IAW EA #CRJ254-08921 REV A.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

AVIONICS OPENING RT INTERCOSTAL IS CORRODED BEYOND SERVICABLE LIMITS. REPLACED PART WITH NEW PART.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

ANGLE CLIP ON THE I/B SIDE OF LBL 36 AT FS 484 IS CRACKED, IN THE CABIN BELOW THE FLOOR. REPAIRED ANGLE CLIP IAW REO 601R-53-41-059 REV B.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

LT CARGO FLOOR SILL FS 574-621 CORRODED OUT OF SRM LIMITS. REMOVED AND REPLACED SILL IAW SRM 51-42-06 AND REO 601R-53-61-1574.

Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 22,929 hrs · 22,927 cycles

RT MLG BAY, HYD LINE SUPPORT BRACKET ATTACHED TO PRESSURE FLOOR SKIN AT FS 528.0 RBL25 IS CRACKED. REMOVED AND REPLACED HYD LINE SUPPORT BRACKET IAW SRM 51-42-06.

Part: RING — CHAFED (LT COWLING) · airframe 22,929 hrs · 22,927 cycles

PANEL RACK. LEFT ENGINE CORE COWL PANEL TRAILING EDGE RUB STRIP WORN. REMOVED AND REPLACED CLOSER RING AND RUB STRIP IAW CMM 71-12-01 TASK 71-12-01-300-820-A01.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 22,929 hrs · 22,927 cycles

RT WINDSHIELD SIDE POST BOTTOM O/B CLIP IS CRACKED, IN THE FLT DECK. REMOVED AND REPLACED RT WINDSHIELD SIDEPOST O/B CLIP IAW SRM 51-42-21.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 22,929 hrs · 22,927 cycles

LT WINDSHIELD SIDE POST BOTTOM O/B CLIP IS CRACKED, IN THE FLT DECK. REMOVED AND REPLACED LT WINDSHIELD O/B SIDE POST BOTTOM CLIP IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

RIGHT HAND SIDE SEAT TRACK STICK #6 HAS CORROSION. REMOVED AND REPLACED RT SIDE SEAT TRACK STICK # 6 IAW AMM 53-01-11.

Part: ANGLE — CHAFED (EXHAUST NOZZLE) · airframe 22,929 hrs · 22,927 cycles

RT ENG EXHAUST NOZZLE FWD T ANGLE EDGE MEMBER CHAFED IN SEVERAL AREAS. REPAIRED RT ENG EXHAUST NOZZLE FWD T ANGLE EDGE (LEADING EDGE) IAW CMM 78-11-00.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

LT OVERWING PNL SUPPORT BRACKET AT FS449.85 IS CRACKED. REMOVED AND REPLACED LT OVERWING PNL SUPPORT BRACKET (ANGEL) IAW SRM 51-42-06.

Part: INTERCOSTAL — CORRODED (DOOR) · airframe 22,929 hrs · 22,927 cycles

AFT EQUIPMENT BAY DOOR 2ND RIB IS BENT AND HAS BARE METAL SPOTS WITH PAINT FLAKING UP. REMOVED AND REPLACED UNSERVICEABLE WEB ON AFT ACCY BAY DOOR IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

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

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

AFT PRESSURE BULKHEAD HAS CHAFING AT 36INCHES FROM FLOOR UP ON RBL18. REPAIRED AFT PRESSURE BULKHEAD 36 ABOVE FLOOR @ RBL 18 IAW REO # 601R-53-61-6962.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

STR 3L IS CRACKED JUST AFT OF FRAME 280, IN THE CABIN. REMOVED AND REPLACED STR 3L AFT OF FRAME 280 IAW SRM 51-42-21.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

AFT PRESSURE BULKHEAD HAS CHAFIN AT 36INCHES FROM FLOOR UP ON RBL27. REPAIRED AFT PRESSURE BULHEAD 36 ABOVE FLOOR @ RBL27 IAW REO #601R-53-61-6962.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

AC RECEPTACLE BOX CRACKED AT TOP ON FUSELAGE NEED MIRROR TO SEE, INSIDE ADG COMPARTMENT. REMOVED CRACKED BOX AND INSTALLED NEW A/C RECEPTACLE BOX IAW SRM 51-42-06 AND SRM 51-42-21.

Part: TRACK — CORRODED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK @LBL9 BETWEEN FS 559+80 TO FS 559+96 IAW AMM 53-01-11.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

AFT PRESSURE BULKHEAD HAS CHAFIN AT 36INCHES FROM FLOOR UP ON RBL36. REPAIRED AFT PRESSURE BULKHEAD 36 ABOVE FLOOR @ RBL 36 IAW REO #601R-53-61-6962.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 22,929 hrs · 22,927 cycles

LT WING L/E PNL ATTACH ANGLE CRACKED IN RADIUS AT WING TRANSITION SPLICE AREA, WS149.0. REMOVED AND REPLACED CRACKED ANGLE AT WS 149.0 ON LT WING IAW SRM 51-41-02.

Part: SKIN PANEL — GOUGED (FUSELAGE) · airframe 22,929 hrs · 22,927 cycles

SUPPLEMENTAL INFORMATION EXTERNAL LOWER SKIN PANEL HAS CORROSION AND SCRIBE MARKS IN NO DAMAGE ALLOWED AREAS FS 409+64 TO 409+90: STG 20L-23R. REPAIRED EXTERNAL LOWER SKIN ALONG PANELS 191AB AND 191BB FWD MATING SURFACE INCLUDING BELLY AND FASTENER HOLES IAW EA# 253-08706 REV IR.

Part: PANEL — DAMAGED (LT COWLING) · airframe 22,929 hrs · 22,927 cycles

PANEL RACK. LEFT ENGINE COWL PANEL 432-AT TRAILING EDGE KNIFE EDGED. REMOVED AND REPLACED TRAILING EDGE ON PANEL 432AT IAW CMM 71-14-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,553 hrs · 22,528 cycles

DURING ROUTINE CHECK LH EMERGENCY LIGHT OUT (3RD BACK FROM FRONT OF AIRCRAFT). RELAMPED LH 3RD (GOING BACK) EMERGENCY LIGHT IAW AMM 33-51-21. OPC GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY) · airframe 21,373 hrs · 21,233 cycles

O2 MASK IN LAV DOWN. REINSTALLED O2 MASK IAW AMM 35-21-09. NO FURTHER ISSUES NOTED.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 21,285 hrs · 21,129 cycles

CABIN PRESSURE ALT WARNING DURING CLIMB THROUGH 10,000FT. CABIN ALTITUDE WAS GREATER THAN 10,000. FOLLOWED QRH, DESCENDED DOWN TO 10,000. COULDN'T GET CABIN ALT BELOW 8900 IN MAN MODE. PUSHED THE EMERGENCY DEPRESS IAW QRH. FOUND THE OVERBOARD EXHAUST SOV DEACTIVATED IN THE OPEN POSITION. DEACTIVATED OVERBOARD EXHAUST SOV IN THE CLOSED POSITION IAW AMM 21-24-00-040-806.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 21,276 hrs · 21,121 cycles

DURING PREFLIGHT, FLIGHT ATTENDANT NOTICED THE FLASHLIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT AND HOLDER IAW CMM 25-60-02.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 19,816 hrs · 19,543 cycles

FA FLASHLIGHT NOT BLINKING. REMOVED & REPLACED THE BATTERY PACK IAW AMM 25-61-00. OPS CHECKED GOOD.

Part: OXYGEN BOTTLE — EMPTY (PORTABLE) · airframe 19,540 hrs · 19,245 cycles

DURING WAKE-UP, NOTED FWD PORTABLE OXYGEN CYLINDER. HAD 0 PSI. INSTALLED NEW SERVICEABLE PORTABLE OXYGEN BOTTLE IAW AMM 35-31-01 AND T.S. 00340R1. OPS TESTED GOOD.

Part: DEFIBRILLATOR — INOPERATIVE (CABIN) · airframe 19,132 hrs · 18,834 cycles

FA FOUND DEFIBRILLATOR INOPERATIVE. REPLACED DEFIBRILLATOR. ACFT OK FOR SERVICE.

Part: OXYGEN MASK — LEAKING (FIRST OFFICER'S) · airframe 19,132 hrs · 18,834 cycles

FIRST OFFICER`S OXYGEN MASK LEAKING. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS CHECKED GOOD.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 19,122 hrs · 18,826 cycles

LEFT WING INBD FLAP VANE LE SKIN HAS CHAFE DAMAGE FROM CENTER STOP. REPAIRED THE SKIN IAW REO 601R-57-52-004 REV -D AND SRM 57-52-00 REPAIR 1.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 19,122 hrs · 18,826 cycles

LT WING INBD FLAP VANE LE SKIN HAS CHAFE DAMAGE FROM OTBD STOP. REMOVED AND REPLACED THE SKIN IAW SRM 51-42-10, 51-40-11, AND REO 601R-57-52-004 REV -D.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,122 hrs · 18,826 cycles

WARDROBE BOTTOM EMERGENCY LIGHT INOPERATIVE. REMOVED & REPLACED THE EMERGENCY LIGHT BULBS IAW AMM 33-51-13-400-801. OPS TESTED GOOD IAW AMM 33-51-00-710-801.

Part: ANGLE — CRACKED (BS 621-625) · airframe 19,122 hrs · 18,826 cycles

BS 621 - 625 ANGLE ADJACENT TO STRINGER 14L IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06, AND 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 19,122 hrs · 18,826 cycles

BS 621 - 625 INTERCOSTAL AT STRINGER 13L AT AFT FACE OF THE BS 621 BULKHEAD IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21, 51-42-06, AND 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 19,122 hrs · 18,826 cycles

BS 621 - 625 INTERCOSTAL MEMBER STRINGER 14L AT THE AFT FACE OF THE 621 BULKHEAD IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.

Part: LATCH — INOPERATIVE (OXYGEN MASK) · airframe 19,122 hrs · 18,826 cycles

LAVATORY & FLIGHT ATTENDANT OXYGEN MASKS DID NOT DROP. REMOVED AND REPLACED THE LAVATORY AND FLIGHT ATTENDANT OXYGNE MASK CONTAINER LATCHES IAW CMM 25-28-54. DISASSEMBLY STEP 2.E.(2) AND ASSEMBLY STEP 2.D.(11), OPS TESTED GOOD IAW AMM 35-20-00-710-803 STEPS 2.D AND 3.A.

Part: BRACKET — CRACKED (LT NACELLE) · airframe 19,122 hrs · 18,826 cycles

LEFT ENGINE PDU ORANGE WIRE HARNESS BRACKET IS CRACKED. REPLACED THE BRACKETS IAW SPM 70-13-01.

Part: SEAT TRACK — CORRODED (BS 406-409) · airframe 19,122 hrs · 18,826 cycles

LEFT SIDE SEAT TRACK NR 3 FROM BS 409.0+16 TO 409+112 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11 AND REO 601R-53-00-055.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 19,122 hrs · 18,826 cycles

RIGHT NR 5 SEAT TRACK FROM BS 449.85 TO 499 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-420-001.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 19,122 hrs · 18,826 cycles

LEFT SIDE SEAT TRACK NR 5 FROM BS 449.85 TO 499 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-21-06, BA, DWG 56487 REV A, AND AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 19,122 hrs · 18,826 cycles

RBL 9 SEAT TRACK FROM BS 409+4 TO 409+126 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-21-06, 53-21-49, DWG 56487 REV A, AND AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 19,122 hrs · 18,826 cycles

RIGHT SEAT TRACK AT RBL 9 HAS CORROSION FROM BS 559 - 559+14. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-21-06, 53-21-49, DWG 56487 REV A, AND AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 19,122 hrs · 18,826 cycles

RBL 9 SEAT TRACK BETWEEN BS 409+126 AND 559+4 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-21-06, 53-21-49, DWG 56487 REV A., AND AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 400-409) · airframe 19,122 hrs · 18,826 cycles

RBL 9 SEAT TRACK BETWEEN BS 400 AND 409+4 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-21-06, 51-21-49, DWG 56487 REV.A, AND AMM 53-01-11.

Part: CHANNEL — BENT (DOOR FRAME) · airframe 19,122 hrs · 18,826 cycles

CARGO DOOR FWD FRAME LOWER AFT CHANNEL BENT BS 574. REMOVED AND REPLACED THE CHANNEL IAW SRM-51-42-06.

Part: CARGO TRACK — CORRODED (BS 583) · airframe 19,122 hrs · 18,826 cycles

LBL 9 CARGO TRACK AT BS 583 IS CORRODED. REMOVED AND REPLACED CARGO TRACK IAW AMM 53-00-49.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 19,072 hrs · 18,777 cycles

FO'S OXYGEN MASK LEAKING. SWAPPED FO'S OXYGEN MASK INTO OBSERVERS POSITION IAW AMM 35-11-12. PERFORMED OPS CHECK IAW AMM 35-10-00 + 23-53-00. OPS CHECKED GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 18,495 hrs · 18,217 cycles

EXIT SIGN ABOVE SERVICE DOOR CAME LOOSE. R & R THE EMERGENCY LIGHT IAW AMM 33-51-13. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,477 hrs · 18,203 cycles

RIGHT EXTERIOR MIDDLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND INSTALLED THE EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 18,399 hrs · 18,115 cycles

EXTERNAL EMERGENCY LIGHTS NR 3 LT & RT INOPERATIVE. MIDDLE OVERWING POSITIONS. R & R BATTERY PACK NR 3 ASSY IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 16,584 hrs · 16,268 cycles

LAVATORY SMOKE DETECTOR RESET BUTTON GREEN LIGHT WAS PUSHED IN. R & R LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 16,492 hrs · 16,166 cycles

LEFT AFT EXTERIOR OVERWING EMER LIGHT INOPERATIVE. R & R LT AFT EXTERIOR EMER LIGHT BULB & UPPER AFT LENS SCREW IAW CMM 33-41-41. OPERATIONS CHECKED GOOD AT THIS TIME IAW AMM 33-51-00. THIS CLEARS DM 001563 MM02 UPDATED PLACARD REMOVED.

Part: PIN — BROKEN (FLAP SYSTEM) · airframe 16,403 hrs · 16,073 cycles

FLAP FAIL CAUTION AT ZERO DEGREES ON AML 3224819-1. COMPLIED WITH FLAP FAIL TROUBLESHOOTING IAW TS 001100R1. AFTER PUSH BACK BOX ITEMS WHEN I ASKED FOR FLAPS 8 DEGREE BOX. FLAPS FAILED CAUTION MSG AT FLAPS 0 DEGREE. PERFORMED TROUBLESHOOTING IAW FIM CHAPTER 27-50-00 REV 48 IAW AD2009-06-12 PARAGRAPH H 6 I AMOC LOG 14-105 DATED 12/30/2014 & TS 001100R1 FIM TECHNICAL SUPPLEMENT, FAULT CODED NOTED WERE 5 1B, 5 2B, 12 2A, 13 1A, 13 2A. CHECKED CONTINUITY ON PLUG 1P2CE LT BPSU NO FAULTS NOTED. FOUND BROKEN PIN ON PLUG 1P2CE, EXTRACTED PIN FROM PLUG, CLEANED & TREATED IAW ESPM 20-17-10. R & R LT BPSU IAW AMM 27-51-00. RIGGED BOTH BPSU'S IAW AMM 27-51-10-220-802. ALL CHECKED GOOD. SEE AML 3224818-1 FOR DETAILS. FOUND BROKEN PIN IN PLUG 1P2CE LT BPSU, EXTRACTED PIN FROM 1P2CE PLUG IAW ESPM 20-17-10. CLEANED & TREATED CONNECTOR. R & R LT BPSU IAW AMM 27-51-10. RIGGED BOTH LT & RT BPSU'S IAW AMM 27-51-10-220-802. PERFORMED CONTINUITY CHECK OF PLUG 1P2CE IAW FIM 27-50-00, NO FAULTS FOUND. ALL CHECKED GOOD. SEE NRC N73465 FOR PARTS & WORK PERFORMED. SEE AML 3224819-1 FOR TROUBLESHOOTING & COMPLETION OF TS 001100R1.

Part: DOOR SEAL — DEBONDED (EMERGENCY EXIT) · airframe 16,043 hrs · 15,679 cycles

LEFT OVERWING EMER EXIT SEAL DISBONDED AT AFT UPPER SPLICE. R & R LT EMER EXIT DOOR SEAL IAW AMM 52-21-07. COMPLIED WITH OPERATIONS CHECK IAW AMM 52-21-07-710-801. NO DEFECTS NOTED.

Part: STOWAGE BOX — DAMAGED (COCKPIT) · airframe 16,043 hrs · 15,679 cycles

CO PILOTS OXYGEN MASK BOX OPENING LID IS DAMAGED. R & R CO PILOT OXYGEN MASK BOX IAW AMM 35-11-15-000-801 & 35-11-15-400-801. OPERATIONS CHECKED GOOD. SEE WIP FOR DETAILS.

Part: SKIN — GOUGED (BS 319-397) · airframe 16,025 hrs · 15,661 cycles

DURING INSPECTION MAINTENANCE FOUND THE FUSELAGE SKIN BETWEEN BS 319 - 349 S17 - 18R GOUGED. REPAIRED IAW EA CRJ 253-03179.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 15,757 hrs · 15,387 cycles

FLIGHT ATTENDANT EMER EQUIP FLASHLIGHT INOPERATIVE, NOT BLINKING. R & R FLASHLIGHT BATTERY IAW AMM 25-61-00. ACFT OK FOR SERVICE.

Part: OXYGEN BOTTLE — LOW PRESSURE · airframe 15,675 hrs · 15,312 cycles

EMERGENCY MEDICAL PORTABLE OXYGEN BOTTLE IS LOW. REPLACED O2 BOTTLE IAW AMM 35-11-03 DM 008656 CLOSED PLACARD REMOVED.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 15,450 hrs · 15,082 cycles

OBSERVER'S LIFE VEST BAG TORN. R & R OBSERVERS LIFE VEST IAW AMM 25-61-03.

Part: LENS — CRACKED (CABIN) · airframe 15,375 hrs · 15,004 cycles

SERVICE DOOR EMER EXIT LIGHT LENS CRACKED. DEFER SERVICE DOOR EMER EXIT LIGHT LENS CRACKED IAW NEF C-6, 120 DAYS.

Part: BOLT — DIRTY (CABIN DOOR) · airframe 15,067 hrs · 14,696 cycles

MAIN CABIN DOOR HANDLE WOULD NOT MOVE MORE THAN APPROXIMATELY 1/4 OF THE WAY TO RELEASE DOOR. GND OPERATIONS AGENT HAD TO ASSIST FROM THE OUTSIDE TO OPEN DOOR. PERFORMED VISUAL INSPECTION OF MAIN CABIN DOOR LINKAGES, ALL CHECKS GOOD. CLEANED & LUBED ALL DOOR SHOOT BOLTS, ROLLER & CATCH ASSEMBLIES. PERFORMED MULTIPLE OPERATIONAL TESTS, ALL CHECKS GOOD IAW AMM CH 52-11-03.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 14,795 hrs · 14,435 cycles

1 INFANT LIFE VEST BAG TORN. COMPLIED WITH PA 25-096A BY INSTALLING INFANT LIFE VESTS.

Part: SKIN — DAMAGED (RT WING) · airframe 14,726 hrs · 14,367 cycles

RIGHT WING EXTENSION LOWER SKIN & CLOSING RIB AT WS 402.9 HAD LIGHTNING DAMAGE RESULTING IN A 0.375 INCH X 0.437 INCH HOLE. REPAIRED IAW REO 601R-57-31-1219.

Part: SKIN — BURNED (RT ELEVATOR) · airframe 14,726 hrs · 14,367 cycles

LIGHTNING STRIKE TO RT ELEVATOR UPPER SKIN AT TE. REPAIRED IAW REO 601R-55-21-403.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,674 hrs · 14,311 cycles

ONE CABIN CEILING EMERGENCY FLOOD LIGHT INOPERATIVE, ABOVE SEAT ROW 5. RE LAMPED IAW AMM 33-51-16. OPERATIONS CHECKED GOOD. THIS CLEARS DM 001734, PLACARD REMOVED

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 13,325 hrs · 12,984 cycles

CAPTAIN SIDE FLASHLIGHT STRAP BROKEN. R & R CAPTAIN SIDE FLASHLIGHT STRAP IAW AMM 25-61-02.

Part: LUG — CHAFED (LT AILERON) · airframe 13,075 hrs · 12,737 cycles

LEFT AILERON OUTBOARD PCU LUG IS CHAFED ON LOWER SIDE. REPAIRED IAW BOMBARDIER REO 601R-57-61-325.

Part: SKIN — DENTED (PAX DOOR) · airframe 13,075 hrs · 12,767 cycles

MAINTENANCE FOUND THE PASSENGER DOOR OUTER SKIN TO BE DENTED IN TWO PLACES BETWEEN FS 338 AND FS 347. REPAIRED IAW EA CRJ252-01464 AND ASSOCIATED 8110-3.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 13,075 hrs · 12,737 cycles

FS 280 FLOOR SUPPORT IS CRACKED ON THE SUPPORT AND CLIPS AT RBL 9 AND LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136.

Part: STRUCTURE — SCRATCHED (FUSELAGE) · airframe 13,075 hrs · 12,737 cycles

SCRATCH MEASURING .875 X .500 X .011 DEEP AT FS 265 BETWEEN S-21L AND S-22L. REPAIRED IAW EA CRJ253-01456 AND ASSOCIATED 8110-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,075 hrs · 12,737 cycles

FLOOR SUPPORT AT LBL 27 HAS CORROSION AROUND FASTENER HOLES FROM FS 574 TO FS 621. REPAIRED IAW BOMBARDIER REO 601R-53-61-3778.

Part: BULKHEAD — SCRATCHED (FUSELAGE) · airframe 13,075 hrs · 12,737 cycles

FORWARD FACE OF FS 621 BULKHEAD SCRATCHED FROM SCREWS IN 6 PLACES. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: RESERVOIR — INOPERATIVE (MLG) · airframe 11,685 hrs · 11,291 cycles

ON GEAR RETRACTION, HYD 3 PRESSURE WENT TO 100 PSI. AFTER A FEW MINUTES GEAR CAME UP AND PRESSURE CAME BACK UP. RECEIVED A GEAR DISAGREE, HYD PRESSURE CAUTION, THEN ALL RETURNED TO GREEN WHEN SELECTED DOWN TURNED AMBER PRESSURE WENT TO 2100 AND GEAR WENT DOWN LOCKED PRESSURE STAYED, QUANTITY SAME AND STAYED IN GREEN. REPLACED NR 3 HYDRAULIC RESERVE IAW AMM 29-12-30. OPS AND LEAK CHECKED GOOD. SWUNG GEAR NO FAULTS FOUND PER AMM 32-30-00.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 11,673 hrs · 11,274 cycles

ON TAKEOFF ROLL AT 80 KTS, RECEIVED HYD 3 LOW PRESSURE CAUTION. CONTINUED TAKEOFF, HAD A GEAR DISAGREE CAUTION THEN GEAR UNSAFE WARNING, & NOSE DOOR WARNING. AFTER ABOUT 15 SECONDS HYD PRESSURE WAS RESTORED AND WARNINGS AND CAUTIONS CLEARED. REPLACED NR 3A HYDRAULIC PUMP IAW AMM 29-12-03 AND LANDING GEAR RETRACTION/EXTENSION CHECK DONE IAW AMM 32-30-00. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 7,778 hrs · 6,929 cycles

DURING CLIMBOUT RECEIVED SMOKE TOILET CAUTION MESSAGE. COMPLETED NON-NORMAL CHECKLIST. FA REPORTED LAV SMOKE DETECTOR WENT OFF FOR COUPLE MINUTES AND THERE WAS A MUSTY BURNING ODOR IN CABIN. NO SMOKE/FIRE IN LAV. RETURNED TO DTW AFTER CONFERRING WITH DISPATCH. SMOKE TOILET CAUTION WAS ONLY ON FOR 3-4 MINUTES THEN EXTINGUISHED (BLEEDS OFF ENG IN TO). REMOVED AND REPLACED LAV SMOKE DETECTOR IAW AMM 26-16. PN ON/OFF PU90-421R3. RAN BOTH PACKS SUPPLIED APU AND BOTH ENGINES FOR 30 MINUTES ON GROUND AND COULD NOT DUPLICATE MUSTY SCENT. OPS TEST OF SMOKE DETECTOR IAW AMM 26-61. ALL CHECKS GOOD.

Part: SMOKE DETECTOR — INTERMITTENT (LAVATORY) · airframe 5,871 hrs · 4,883 cycles

DURING CLIMB THROUGH 3500 FT, AMBER TOILET SMOKE CAUTION EICAS MESSAGE. MESSAGE WENT AWAY AFTER APPROX 20 SECONDS, VERIFIED ALL OK IN THE LAV. SYS OPS CHECK GOOD IAW FIM 26-00-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 5,748 hrs · 4,761 cycles

AFTER DEPARTURE FROM MSP THE CREW EXPERIENCED A LAVATORY SMOKE WARNING. AT APPROX 500 FT SMOKE TOILET CAUTION MESSAGE APPEARED. DURING THE NON NORMAL CHECKLIST MESSAGE DISAPPEARED. FA SAID NO SMOKE, BUT DID DETECT DE-ICE FLUID FROM DEICING. FLIGHT RETURNED TO MSP. THE CAPTAIN DID DECLARE AN EMERGENCY TO ATC AND RETURNED TO MSP LANDING WITHOUT FURTHER INCIDENT. COMPLIED WITH EO NR C25025: INSTALLATION OF COVER ON LAV AIR VENT.

Part: CONTROL SYSTEM — FAILED (TE FLAPS)

(REF NR: 05-083) FLAPS FAILED AT 8 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)