N8946A

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 22,626 hrs · 22,471 cycles

PILOTS IB SEAT TRACK WEAR STRIP 1 2 AN 3 FROM FRONT RETAINING RIVETS SHEERED AND FWD SECTION OF WEAR STRIP CAN BE LIFTED UP UNBONDED. COMPLIED WITH REO 601R-53-11-1093.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 22,626 hrs · 22,471 cycles

PILOTS OTBD SEAT TRACK WEAR STRIP NR 2 AND 4 FROM FRONT RETAINING RIVETS SHEARED. COMPLIED WITH REO 601R-53-11-1093 TEMPORARY DISPOSTITION INITATED PWI WITHIN 6000 FHS SEE N705634

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 22,626 hrs · 22,471 cycles

CO PILOTS OB SEAT TRACK WEAR STRIP 4 FROM FRONT RETAINING RIVET SHEARED. COMPLIED WITH REO 601R-53-11-1093.

Part: OXYGEN MASK — NO TEST (CAPTAIN'S) · airframe 20,854 hrs · 20,570 cycles

CAPTAIN`S OXYGEN MASK FAILS TO TEST. PREFORMED AN OPS CHECK IAW AMM 35-11-12. OPS CHK GOOD. NO FURTHER DEFECTS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,088 hrs · 19,735 cycles

RIGHT WING AFT EMERGENCY LIGHT OUT. REPLACED THE LAMPS IAW AMM 33-51-21. OPS TESTED GOOD.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 20,063 hrs · 19,704 cycles

RIGHT WING INBD FLAP VANE, INBD ACCESS PANEL 684DT HAS ELONGATED SCREW HOLE. LOCATED & DRILLED A NEW ACCESS PANEL IAW SRM 51-40-11.

Part: SUPPORT — CRACKED (BS 220-235) · airframe 20,063 hrs · 19,704 cycles

PILOTS SIDE LOWER SIDE POST SUPPORT BELOW PILOT WINDOW IS CRACKED BETWEEN BS 220 AND 235, BELOW WL 110. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-42-06, AND SRM 51-42-21 AAR SM-58

Part: SKIN — CHAFED (RT WING) · airframe 20,063 hrs · 19,704 cycles

RIGHT WING LOWER SKIN CHAFED. REPAIRED THE WING SKIN IAW REO 60IR-57-21-2749.

Part: STEP — CRACKED (PAX DOOR) · airframe 20,063 hrs · 19,704 cycles

WHILE REMOVING CORROSION ON PAX DOOR STEP, FOUND A CRACK. LOCATED, AND DRILLED A NEW STEP IAW SRM 51-40-11.

Part: STIFFENER — CRACKED (EXHAUST CONE) · airframe 20,063 hrs · 19,704 cycles

NR 1 ENGINE EXHAUST CONE 436AL HAS CRACKED STIFFENER. REPAIRED THE STIFFENER IAW CMM 78-11-00, PG 6043.

Part: ATTACH ANGLE — CRACKED (BS 202) · airframe 20,063 hrs · 19,704 cycles

RIGHT WINDSHIELD SIDE SUPPORT POST, LOWER OTBD ATTACH ANGLE CRACKED. REMOVED THE ATTACH ANGLE, LOCATED, DRILLED, AND INSTALLED A NEW ATTACH ANGLE IAW SRM 51-52-21.

Part: POST — CRACKED (BS 409) · airframe 20,063 hrs · 19,704 cycles

VERTICAL POST AT LBL 27 ON THE BULKHEAD AT BS 409+128. FOUND TO HAVE A ONE INCH CRACK AT BOTTOM OF INBD CHANNEL. REPAIRED THE POST IAW REO 601R-53-41-056.

Part: ATTACH ANGLE — CRACKED (LT WINDSHIELD)

LEFT WINDSHIELD, SIDE SUPPORT POST LOWER OTBD ATTACH ANGLE CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-21.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 20,063 hrs · 19,704 cycles

INTERCOSTAL INBD ATTACH ANGLE CRACKED AT LBL 36, BS 484. REPLACED THE ATTACH ANGLE IAW SRM 51-42-21.

Part: SUPPORT ANGLE — CRACKED (B 473.15) · airframe 20,063 hrs · 19,704 cycles

SUPPORT AT BS 473.15 ON THE RT UNDEFLOOR LONGERON IS CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-06.

Part: HINGE — CRACKED (CARGO THRESHOLD) · airframe 20,063 hrs · 19,704 cycles

CARGO DOOR THRESHOLD HINGED PROTECTOR PLATE, THREE PIANO HINGE SEGMENTS CRACKED AND/OR WORN AT HINGE PIN LUGS. REPLACED THE PIANO HINGES ON THE CARGO DOOR THRESHOLD PLATE IAW IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 280) · airframe 20,063 hrs · 19,704 cycles

INBD ANGLE ON STRINGER 3L IS CRACKED JUST AFT OF FRAME BS 280, IN THE CABIN. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06, AND 51-42-21.

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 20,040 hrs · 19,682 cycles

EMERGENCY LIGHTS SWITCH LIGHT, BULBS INOPERATIVE. REPLACED THE LAMPS IAW ESPM 20-24-00.

Part: LIGHT — INOPERATIVE · airframe 19,986 hrs · 19,631 cycles

FWD RT OVERWING EMERGENCY LIGHT INOP. RELAMPED FWD RT OVERWING EMERGENCY LIGHT IAW AMM 33-51-21. OPS GOOD. P/N OFF/ON: 1317

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 19,826 hrs · 19,469 cycles

CA SIDE O2 MASK LEAKS DURING TEST. R/R'D CPT SIDE O2 MASK IAW AMM 35-11-12. OPC GOOD, OK FOR SVC.

Part: OXYGEN MASK — LEAKING (FLIGHT DECK) · airframe 18,763 hrs · 18,318 cycles

OBSERVER OXYGEN MASK LEAKS. R & R THE OBSERVER`S OXYGEN MASK IAW AMM 35-11-12. PERFORMED OPS CHECK AND FOUND GOOD.

Part: DEFIBRILLATOR — INOPERATIVE (CABIN) · airframe 18,722 hrs · 18,273 cycles

BOTH DEFIBRILLATOR`S POWER INOPERATIVE NOT GREEN. REMOVED AND REPLACED IAW CRJ 200 AMM 25-60-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,608 hrs · 18,161 cycles

LEFT EMERGENCY LIGHT FWD OF EMERGENCY EXIT DOOR IS INOPERATIVE. EXTERIOR EMERGENCY LIGHT 5. REMOVED AND REPLACED THE BULBS IAW AMM 33-51-21, OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,602 hrs · 18,154 cycles

FA FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT IAW AMM 25-61-02. OK FOR SERVICE.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 18,279 hrs · 17,824 cycles

OBSERVER'S OXYGEN MASK FAILED TEST. HARNESS EITHER STAYS INFLATED OR STAYS DEFLATED. BUT IT WON'T BOTH. REMOVED & REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS TEST AND LEAK CHECKED GOOD.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 18,267 hrs · 17,814 cycles

FO OXYGEN MASK TEST FAIL. FOUND FO'S O2 MASK INOP. REMOVED FO'S 02 MASK AND SWAPPED WITH OBSERVER'S O2 MASK IAW AMM 35-11-12. PERFORMED OPS CHECK OF FO'S 02 MASK IAW AMM 35-100-00 AND 23-51-00. OPS CHECK GOOD AT THIS TIME. DEFERRED OBS O2 SYS IAW MEL 35-10-01 ENTERED ON MM02 MAINTENANCE PROCEDURES C/W PLACARD INSTALLED. REMOVED AND REPLACED OBSERVER O2 MASK IAW AMM TASK 35-11-000-802. OPS CHECKS NORMAL.

Part: DEFIBRILLATOR — INOPERATIVE (CABIN) · airframe 18,133 hrs · 17,672 cycles

AED BATTERY IS DEAD. REMOVED AND REPLACED AED IAW AMM 25-60-00. MM02.

Part: MOTOR — INOPERATIVE (PAX DOOR) · airframe 17,952 hrs · 17,497 cycles

PASSENGER DOOR DOES NOT CLOSE. REMOVED AND REPLACED PASS DOOR POWER ASSIST MOTOR IAW AMM 52-11-08. OPS CHECK OK. REMOVED AND REPLACED PASS DOOR PRESS VENT-FLAP ICE BREAK CABLE ASSY IAW AMM 52-11-15. OPS CHECK OK.

Part: BRACKET — BENT (NLG) · airframe 17,773 hrs · 17,322 cycles

GEAR DISAGREE ON TAKE OFF. NOSE GEAR REMAINED DOWN. QRH PERFORMED SATISFACTORILY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED TARGET AND BRACKET FOR NLG CENTERED, EXTENDED PROXIMITY SENSOR IAW CMM 32-20-04 EXTENSION AND RETRACTION OF NLG GOOD IAW AMM 32-30-00-710-802

Part: ANGLE — CRACKED (BS 621) · airframe 17,772 hrs · 17,321 cycles

LEFT BS 621 OBLIQUE ANGLE AT STRINGER 14L IS CRACKED. REMOVED & REPLACED THE ANGLE IAW SRM 51-42-06 & 51-42-21. LEAK CHECKED GOOD IAW AMM 52-31-07-720-801.

Part: ATTACH ANGLE — CRACKED (BS 621) · airframe 17,772 hrs · 17,321 cycles

THE ATTACH ANGLE AT AFT SIDE OF BS 621 BULKHEAD IS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-06.

Part: ATTACH ANGLE — CRACKED (BS 621) · airframe 17,772 hrs · 17,321 cycles

ANGLE AT AFT SIDE OF BS 621 BULKHEAD IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06.

Part: ATTACH ANGLE — CRACKED (BS 621) · airframe 17,772 hrs · 17,321 cycles

ANGLE AT AFT SIDE OF BS 621 BULKHEAD IS CRACKED. REMOVED & REPLACED THE ANGLE IAW SRM 51-42-06.

Part: ANGLE — BENT (PASSENGER DOOR) · airframe 17,772 hrs · 17,321 cycles

PAX DOOR FWD HAND RAIL STOW ANGLE MISSING. ALSO AFT HANDRAIL STOW ANGLE IS BENT. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 621) · airframe 17,772 hrs · 17,321 cycles

ANGLE AT AFT SIDE OF FS621 BULKHEAD IS CRACKED. REMOVED AND REPLACED IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 17,772 hrs · 17,321 cycles

IN AFT CARGO BAY BS 621 - 589 LBL 28 FLOOR SUPPORT CORRODED. REMOVED & REPLACED FLOOR SUPPORT IAW SRM 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 17,772 hrs · 17,321 cycles

INTERCOSTAL AT AFT SIDE OF FS621 BULKHEAD IS CRACKED. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 17,772 hrs · 17,321 cycles

INTERCOSTAL AT AFT SIDE OF BS 621 BULKHEAD IS CRACKED. REMOVED & REPLACED INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 17,772 hrs · 17,321 cycles

INTERCOSTAL AT AFT SIDE OF BS 621 BULKHEAD AND L 13 IS CRACKED. REMOVED & REPLACED INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 17,772 hrs · 17,321 cycles

IN AFT CARGO, FWD FACE OF AFT PRESSURE BULKHEAD HAS TWO ISOLATOR MOUNTS THAT ARE BROKEN. REMOVED AND REPLACED THE ISOLATOR IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 17,772 hrs · 17,321 cycles

SEAT TRACK FROM BS 409+126 - 559 HAS SEVERAL AREAS OF CORROSION AND GOUGES. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 17,772 hrs · 17,321 cycles

IN AFT CARGO BAY BS 589 - 621 LBL 9 FLOOR SUPPORT CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOOR SUPPORT IAW EA CRJ253-04792.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 17,772 hrs · 17,321 cycles

IN THE AFT CARGO BAY, BS 589 - 621 LBL 26 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW EA CRJ253-04790.

Part: BULKHEAD — CRACKED (BS 621) · airframe 17,772 hrs · 17,321 cycles

FS 621 BULKHEAD CRACKED AROUND LINTEL FITTING. REPAIRED IAW REO 601R-53-61-1230. REV. F.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 17,772 hrs · 17,321 cycles

SEAT TRACK FROM BS 559 TO 559+80 HAS SEVERAL AREAS OF CORROSION AND GOUGES. REMOVED AND REPLACED THE SEAT TRACK AMM 53-01-11, AND AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 17,772 hrs · 17,321 cycles

SEAT TRACK FROM BS 559 TO 559+80 HAS SEVERAL AREAS OF CORROSION AND GOUGES. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11, REO 601R-53-00-485, AND AMM 53-01-11.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 17,772 hrs · 17,321 cycles

FLT CONTROL CABLE FAIRLEAD INTERCOSTAL AT BS 484, RBL 27 TO 34 INBD ATTACH ANGLE CRACKED. REMOVED & REPLACED THE ATTACH ANGLE IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 17,772 hrs · 17,321 cycles

LEFT SEAT TRACK FROM BS 409+126 TO 559 HAS SEVERAL AREAS OF CORROSION AND GOUGES. REMOVED AND REPLACED THE FLOOR SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 364-398) · airframe 17,772 hrs · 17,321 cycles

RT SEAT TRACK FROM BS 364.0 TO 398 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 398-409) · airframe 17,772 hrs · 17,321 cycles

SEAT TRACK FROM BS 398 - 409+126 HAS CORROSION. REPLACE THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 364-398) · airframe 17,772 hrs · 17,321 cycles

LEFT SEAT TRACK FROM BS 364 - 398CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,772 hrs · 17,321 cycles

LT FLOOR SEAT TRACK FROM FS398.0 TO FS409+126 HAS CORROSION. RECEIVED NEW SEAT TRACK, INSTALLED NEW LT SEAT TRACK FS 398.0 TO FS 409+126 IAW AMM 53-01-11.

Part: BRACKET — CRACKED (BS 615) · airframe 17,772 hrs · 17,321 cycles

EXTERNAL AC ELECTRICAL RECEPTACLE BRACKET IS CRACKED. REMOVED AND REPLACED DAMAGED EXTERNAL AC ELECTRICAL RECEPTACLE BRACKET IAW BOMBA REO 601R-53-11-569 AND CRJ200 SRM 51-42-21. AAR S/M-107

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 17,772 hrs · 17,321 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED CRACKED AFT DRAG ANGLE PER REO 601R-52-11-513 REV B.

Part: BULKHEAD — CRACKED (BS 202) · airframe 17,772 hrs · 17,321 cycles

BS 202.75 BULKHEAD IS CRACKED AT PARKING BRAKE CABLE. REPAIRED THE BULKHEAD IAW REO 601R-53-11-563 REV C.

Part: SEAL — BROKEN (FIRE BOTTLE) · airframe 17,753 hrs · 17,304 cycles

SEAL BROKEN ON WATER FIRE EXTINGUISHER. R & R FIRE EXTINGUISHER IAW AMM 26-23-01. OK FOR SERVICE.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 17,688 hrs · 17,239 cycles

FIRST OFFICERS O2 HARNESS ONLY INFLATES ON 1 SIDE, OTHER SIDE IS LIMP. R & R FIRST OFFICERS 02 MASK IAW AMM 35-11-12. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE O2 BOTTLE PRESS AT 1700 PSI.

Part: DOOR SEAL — DIRTY (PAX DOOR) · airframe 17,565 hrs · 17,106 cycles

ENROTE, FLIGHT ATTENDANT REPORTED HIGH PITCHED SQUEAL FROM MAIN BOARDING DOOR. CABIN ALT 2900' SOUND WENT AWAY AT D=7.2 CABIN ALT 2300. INSPECTED PAX DOOR & SEAL IAW AMM 52-11-10, FOUND NO DAMAGE ON SEAL, BUT SEAL HAD GLYCOL & DIRT. CLEANED & LUBED SEAL.

Part: DOOR — NOISY (CABIN) · airframe 17,516 hrs · 17,047 cycles

LOUD SQUEAL FROM PAX DOOR IN FLIGHT. PRESSURIZED ACFT 5.2^P COULD NOT DUPLICATE NOISE IAW 21-31-00. PERFORMED VISUAL INSPECTION OF DOOR SEAL & DOOR FRAME, NO DEFECTS NOTED.

Part: SEAL — FROZEN (PAX DOOR) · airframe 17,427 hrs · 16,965 cycles

F/A REPORTS THAT PASSENGER DOOR MAKES LOUD SQUEELING NOISE IN FLIGHT. REMOVED ICE AND DEBRIS FROM LOWER DOOR SEAL AREA. CLEANED DOOR SEAL PRESSURIZED AIRCRAFT, REF AMM 21-32-00, NO LEAKS NOTED.

Part: CAGE — BROKEN (SMOKE DETECTOR) · airframe 17,156 hrs · 16,697 cycles

NUMBER 1 CARGO SMOKE DETECTOR CAGE IS BROKEN OFF. DEFERRED NR 1 CARGO SMOKE DETECTOR IAW MEL 26-15-11 IAW RM MOC 009350 PLACARDS INSTALLED. ENTERED INTO MM02 DDG COMPLIED WITH AMM 26-15-00-040-801. R & R NR 1 CARGO FIRE DETECTOR CAGE ASSEMBLY IAW AMM 26-15-01. OPERATIONS CHECKED GOOD. THIS CLEARS DM 9350. PLACARD REMOVED.

Part: LIGHT — UNKNOWN (CABIN) · airframe 16,722 hrs · 16,262 cycles

RECTANGULAR EMER LIGHT IN CABIN CEILING AFT MOST OVER AISLE. R & R CEILING EMER LIGHT BULB IAW 33-51-16. OK FOR SERVICE, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,209 hrs · 15,739 cycles

MID CABIN FLIGHT ATTENDANT EMERGENCY CALL & AUDIO LIGHT BURNED OUT. REPLACED MID CABIN FLIGHT ATTENDANT EMERGENCY CALL & LAVATORY LIGHTS IAW AMM 33-51-14. PERFORMED OPERATION CHECK OF LIGHTS IAW AMM 33-51-00. OPERATIONS CHECKED NORMAL AT THIS TIME, ACFT OK FOR SERVICE.

Part: COVER — MISSING (CABIN) · airframe 16,207 hrs · 15,737 cycles

WHITE & AMBER EMERGENCY BULB COVERS MISSING ON CTR EMERGENCY LIGHT. REPLACED WHITE & AMBER CAPS IAW AMM 33-51-14.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 15,611 hrs · 15,166 cycles

CAPTAINS EMERGENCY FLASHLIGHT INOPERATIVE. R & R BATTERY PACK IN CAPTAIN`S EMERGENCY FLASHLIGHT IAW AMM 25-61-04, OPERATIONS CHECKED GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 14,371 hrs · 13,964 cycles

FLIGHT 3733, FLAP FAILED ON APPROACH AT 30 DEGREES. LANDED WITH NO ISSUES. PERFORMED FLAP CONTROL LEVER SELF TEST. ALL OP CHECKED GOOD IAW AMM 27-51-01-740-801.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 14,023 hrs · 13,625 cycles

ON FLIGHT 3640 (DTW - ELM) CREW RECEIVED SPOILERON CAUTION MESSAGE. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN ELM WITHOUT FURTHER INCIDENT. MOC RESET SYSTEM WITH THE CREW PER FIM. OPS CHECKS NORMAL. OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 13,882 hrs · 13,489 cycles

ON FLIGHT 3645 ON CLIMBOUT FROM MSP RECEIVED GEAR DISAGREE MESSAGE WHEN GEAR HANDLE WAS SELECTED UP. THE MLG RETRACTED BUT THE NLG REMAINED DOWN. THE QRH WAS COMPLETED AND MANUAL EXTENSION WAS SELECTED WITH 3 GREENS. THE CREW DECLARED AN EMERGENCY. VERIFIED NO EXTERNAL LEAKS (HYDRAULIC/ NITROGEN) WITH NOSE STRUT. FLUSHED OLD FLUID FROM STRUT, SERVICED STRUT WITH NEW FLUID / NITROGEN PER AMM 12-12-32. COMPLETED PA 05-018J. (2), OPS CHECK GOOD.

Part: LATCH — MISSING (AVIONICS DOOR) · airframe 13,681 hrs · 13,268 cycles

AVIONICS DOOR LATCH MISSING. INSTALLED AVIONICS BAY DOOR LOCK ASSEMLY IAW PA 52-05.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 13,678 hrs · 13,266 cycles

FAIL FLAP STUCK AT ZERO IN AIR 200 KTS 1 HR INTO FLIGHT. 9 DEG C 3000' ON FLIGHT 3984 FROM MSP TO FWA. TROUBLESHOT FLAP FAILURE PER FIM 27-50-00. REMOVED AND REPLACED RIGHT BPSU AND FECU. REMOVED INSPECTED AND RE-INSTALLED THE LEFT AND RIGHT FLEX DRIVE SHAFTS. REMOVED AND REPLACED RIGHT WING FLAP ACTUATORS. NO FAULTS WITH SYSTEM AT THIS TIME. THIS CLEARS DM 73880 AND THE PLACARD WAS REMOVED.

Part: RESERVOIR — LEAKING (HYDRAULIC SYS) · airframe 13,617 hrs · 13,206 cycles

ON FLIGHT 4069 (MSP TO CLE) AFTER TAKEOFF LANDING GEAR DID NOT RETRACT, HYDRAULIC 3 PRESSURE WENT TO ZERO. THE CREW PERFORMED AN AIR RETURN BACK TO MSP FOR NR 3 HYDRAULIC SYSTEM FAILURE/LOSS OF PRESSURE. CREW DID DECLARED AN EMERGENCY AND LANDED WITH NO HYD SYSTEM 3 PRESSURE OVERWEIGHT LANDING AT 48,800 POUNDS LESS THEN 300 FPM. LANDING GEAR MANUAL EXTENSION WAS PULLED WITH GEAR IN DOWN POSITION. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. FOUND NR 3 HYDRAULIC RESERVOIR LEAKING. REMOVED AND REPLACED NR 3 HYDRAULIC RESERVOIR IAW 29-12-30. ALSO, COMPLIED WITH 05-51-34 (INSPECTION OF ACMP AFTER DRY OPERATION). REMOVED AND REPLACED CASE DRAIN FILTER. SWUNG GEAR 32-34-00. PERFORMED MANUAL EXTENSION IAW 32-34-00. ALL OPS CHECKS AND LEAK CHECKS GOOD. OVERWEIGHT LANDING FOUND TO BE ACCEPTABLE IAW 05-51-01. CASE DRAIN FILTER P/N AC7031F8.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 5,230 hrs · 4,289 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED CAPTAIN`S FLASHLIGHT BATTERY IAW AMM 25-61-02. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,576 hrs · 12,132 cycles

ONE OF THE EMERGENCY LIGHTS, (A LIGHT THAT IS BY A EMERGENCY EXIT PLACARD), IS BURNED OUT ON THE AIRSTAIRS. DEFERRED STAIR LIGHTS PER MEL 33-21-2(D). ENTERED INTO MM02. MXC NOTIFIED. REPLACED INOP AIRSTAIR LIGHT ASSY P/N 2AL455119-70, S/N 2609 OFF, P/N 2AL455119-70, S/N 2608 ON. PLACARD REMOVED. MM02 CLEARED MXC NOTIFIED OP'S NORMAL JOB COMPLETE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 9,017 hrs · 8,146 cycles

NR 2 EMERGENCY LIGHTS BATTERY PACK INOP. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY PACK IAW MM 33-51-04-000-801 AND -400-801.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 5,764 hrs · 4,996 cycles

FS 621 TO FS 625 LT UPPER INTERCOSTAL (OBLIQUE) ANGLE AT STRINGER 14L IS CRACKED 1.5 INCH LONG IN AFT RADIUS. DRILLED AND REMOVED FS 625 LT UPPER INTERCOSTAL ANGLE AND INSTALLED NEW INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND 51-42-21 AND BOMBARDIER REO 601R-53-61-422. WAITING MESABA EO FOR CLOSEOUT. C/W STA 621-625 INTERCOSTAL RE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

RECEIVED SMOKE TOILET INDICATION ON CLIMB-OUT BITTER HAZE SMOKE IN CABIN TO FLIGHT COMPARTMENT. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW AMM 26-10-00. OPS CHECK GOOD.