N110XJ

Part: WIRE — LOOSE (EMERGENCY LIGHT)

DURING INSPECTION EMERGENCY FLOOD LIGHT FOUND INOPERATIVE. FOUND DEFECTIVE SOLDER JOINT ON LAMP ASSY.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 38,014 hrs

RIGHT ENGINE ERRATIC TORQUE INDICATIONS ABORTED TAKEOFF. REMOVED AND REPLACED TORQUE INDICATOR.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,893 hrs · 41,256 cycles

CABIN EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLIES 23LN & 21LN INOP. REPLACED SUPPLIES WITH SERVICEABLE UNITS. OPS CHECK GOOD.

Part: FRAME — CHAFED · airframe 36,755 hrs · 41,100 cycles

DURING 4Y/2Y INSPECTION IN BNA, FRAME 686.888 RT SIDE OF FUSELAGE HAS BEEN CHAFED BY CARGO DOOR CABLE. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#53308. REFER EAMS WORK ORDER #212691 TASK 2505.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,263 hrs · 40,523 cycles

DURING LC1, NOTED LT AND RT AFT EXT EMERGENCY LIGHTS INOP. NOTED SEVERAL OTHER INT LIGHTS INOP ALSO. REMOVED AND REPLACED EMERGENCY SUPPLY AND BATTERY PACK 24LN. OPS CHECK GOOD. DOCUMENTED AND MM 409 237757.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 36,119 hrs · 40,349 cycles

DURING 30/12 CYC CHECK IN BNA FOUND RIGHT LOWER HORIZONTAL STAB SKIN IS DENTED AND HAS BEEN REPAIRED IAW MESABA EO S55053. DAMAGE IS 2.1 INCHES AFT OF FRONT SPAR AND 13.3 INCHES FROM I/B EOP.

Part: BATTERY PACK — FAILED (FUSELAGE) · airframe 35,868 hrs · 40,075 cycles

BATTERY PACK 61-0478-9, S/N 1875. FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 55-2198-1, UNIT PASSES, RTS 1/31/05.

Part: WIRE — BURNED (POWER SUPPLY) · airframe 35,849 hrs · 40,045 cycles

EMERGENCY POWER SUPPLY P/N 60-1321-1 S/N 16238 INSPECTION HAS BURNED WIRE INSIDE. REPAIRED GROUND WIRE. UNIT PASSES CMM CHECKS, RTS 1/25/05.

Part: ICE SHIELD — DENTED (FUSELAGE) · airframe 35,682 hrs · 39,861 cycles

DENTS DISCOVERED ON RT ICE SHIELD. MAINTENANCE CARRIED OUT REPAIR IAW MESABA EO NR S53276. REFER TO LOG PAGE 1335862 FOR ADDITIONAL INFORMATION.

Part: CIRCUIT BREAKER — FAILED (ALPHA LIGHT) · airframe 34,823 hrs · 38,949 cycles

DURING FLIGHT L ALPHA LIGHT CAME ON, RAN QRH LIGHT STAYED ON. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED CIRCUIT BREAKER 13 XA, ALL CHECKS GOOD IAW SF-340MM CH 24.

Part: RELAY — FAILED (AC POWER SYS) · airframe 34,567 hrs · 38,669 cycles

AFTER DEPARTURE FROM MSP, CREW REPORTED RT AVIONICS FAILURE. AIR RETURN TO MSP. MAINTENANCE REPLACED RELAY 4PP RT AVIONICS BUSS. CHECKS GOOD IAW CHAP 24.

Part: ENGINE — MALFUNCTIONED (LEFT)

DURING FLIGHT 3009, LT ENGINE SHOWING GRADUAL LOSS IN ITT MARGIN. LT ENGINE PLACED ON DERIVITIVE POWER FOR CONTINUED SERVICE. CTOT AND ANTI SKID SYSTEMS MUST BE OPERATIVE. MAINTENANCE PROCEDURES COMPLIED WITH FOR DERIVATIVE POWER PROGRAM. CHAP 2, SECTION 2.1 ENTERED IN MDR AND MAINTENANCE CONTROL NOTIFIED.

Part: CONTROL MODULE — FAILED (DEICE SYSTEM)

DURING FLIGHT 3183, LEFT INTAKE CAUTION LIGHT ILLUMINATES, MOVING POWER LEVER WILL EXTINGUISH LIGHT FOR APPROXIMATELY 2 MINUTES THEN COMES ON AGAIN. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED DEICE CONTROL MODULE (LT) P/N44730-501, S/N OFF A0072, S/N ON A00301. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOCOARSEN) · airframe 33,085 hrs · 37,002 cycles

AUTOCOURSEN LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED AUTOCOURSEN COMPUTER. P/N ON AND OFF 8542M2, SN/ON 504, S/N OFF 215

Part: GCU — FAILED (ELECTRICAL)

DURING FLIGHT 3294, ON MISSED APPROACH RT AC GEN CAUTION LIGHT ILLUMINATED, RH AC GEN WAS UNABLE TO RESET AND WAS TURNED OFF PER QRH. AIRCRAFT IN ICING CONDITIONS FOR APPROXIMATELY 10 MINUTES WITH RH AC GEN OFFLINE. MAINTENANCE REPLACED GEN, DID NOT FIX, INSTALLED ORIGINAL AC GEN INSTALLED AC GCU OPS CHECK GOOD.

Part: HINGE — LACK OF LUBE (AILERON)

DURING FLIGHT 3321, WITH AUTO-PILOT OFF, A/C HARD TO TURN TO THE LEFT. MAINTENANCE PERFORMED REQUIRED AILERON CHECKS, ALL CHECKS GOOD. LUBRICATED AILERON HINGE POINTS, FREEDOM FORCE CHECK OF PILOTS AND F/O'S CONTROL COLUMN IS GOOD.

Part: CONNECTOR — FAILED (PROP OIL PRESS)

DURING FLIGHT 3084 LT PROP OIL PSI DROPPED TO ZERO AFTER START. A/C RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED PGB OIL PRESSURE TRANSMITTER CONNECTOR PLUG 15HE. ALL CHECKS GOOD IAW SF-340, MM CHAP. 79.

Part: TRANSMITTER — MALFUNCTIONED (OIL PRESS)

DURING CRUISE ON FLIGHT 3001, LT ENGINE MASTER WARNING LIGHT FLICKERED TWICE AT CRUISE. CREW NOTED LT PROP OIL PRESSURE DROPPED FROM NORMAL RANGE TO ZERO CAUSING MASTER WARNING LIGHT TO "FLICK" ON/OFF. ENGINE /PROP RAN FINE. LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LT PROP OIL PRESS TRANSMITTER IAW MM PN IPTE119-1000-200D1, SN/ON 4181-4-428/382 SN/OFF 4487-1-38/12. OPS AND LEAK CHECK GOOD.

Part: CONNECTOR — ARCED (F/A PANEL)

FLIGHT ATTENDANT REPORTED SPARKS BEHIND FA PANEL. MX FOUND CONNECTOR PLUG ARCING TO SWITCHES. WRAPPED CONNECTOR PLUG WITH COMPRESSION TAPE. ALL CHECKS GOOD.

Part: VALVE — FAILED (LT ENGINE)

DURING FLIGHT 2868 LT AIR VALVE LIGHT ILLUMINATED. AIR RETURN TO DTW. WEATHER CONDITIONS WARRANT THE RETURN. MAINTENANCE REMOVED AND REPLACED THE LT GARRET VALVE, (SWAPPED LEFT TO RIGHT AND PROBLEM FOLLOWED) IAW SAAB MM CH 75. OPS AND SECURITY CHECK GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,893 hrs · 33,561 cycles

DURING 4K-CHECK IN CWA, LT CENTER AISLE SEAT TRACK LBL 18.3 FWD PORTION OF FLOOR BOARD FLANGE HAS CORROSION, STARTING AT APPROXIMATELY STA 297. MAINTENANCE INSTALLED NEW SECTION OF SEAT TRACK ON LT CENTER AISLE IAW EO S53060 DATED 11-07-2000.

Part: CONTROL CABLE — CORRODED (ELEVATOR) · airframe 29,893 hrs · 33,561 cycles

DURING 4K-CHECK IN CWA, LT OUTBOARD AFT ELEVATOR CABLE CORRODED. MAINTENANCE REPLACED LT OUTBOARD AFT ELEVATOR CABLE P/N 7227215-841 IAW SF340 AMM 27-31-15-4.

Part: CONTROL CABLE — BROKEN (ELEVATOR) · airframe 29,893 hrs · 33,561 cycles

DURING 4K-CHECK IN CWA, LT INBOARD AFT ELEVATOR CABLE HAS A BROKEN WIRE. MAINTENANCE REPLACED LT INBOARD AFT ELEVATOR CABLE P/N 7227215-946 IAW SF340 AMM 27-31-15-4.

Part: CONTROL CABLE — CHAFED (AILERON) · airframe 29,893 hrs · 33,561 cycles

DURING 4K-CHECK IN CWAM LT INBOARD AILERON FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE INSTALLED NEW LT I/B FWD AILERON FUSELAGE CABLE P/N 7227105-623 IAW SAAB AMM 27-11-25.

Part: CONTROL CABLE — CHAFED (ELEVATOR) · airframe 29,893 hrs · 33,561 cycles

DURING 4K-CHECK IN CWA, LT I/B ELEVATOR FWD FUSELAGE CABLE IS CHAFFED. MAINTENANCE REMOVED AND REPLACED LT I/B FWD FUSELAGE ELEVATOR CABLE PN7227705-644 IAW SF3 AMM 27-31-15.

Part: CONTROL CABLE — CHAFED (ELEVATOR) · airframe 29,893 hrs · 33,561 cycles

DURING 4K-CHECK IN CWA, LT OUTBOARD FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED LT OUTBOARD FWD ELEVATOR CABLE P/N 7227105-712, IAW SF3 AMM 27-31-15.

Part: CONTROL CABLE — CHAFED (RUDDER) · airframe 29,893 hrs · 33,561 cycles

DURING 4K-CHECK IN CWA, FOUND LT I/B FWD FUSELAGE RUDDER CIRCUIT 1 CABLE CHAFFED. MAINTENANCE REMOVED AND REPLACED LT I/B FWD FUSELAGE RUDDER PN 7227105-571 CIRCUIT 1 CABLE IAW SF3 AMM 27-21-25.

Part: CONTROL CABLE — CHAFED (RUDDER) · airframe 29,893 hrs · 33,561 cycles

DURING 4K-CHECK IN CWA, RT O/B RUDDER SYSTEM CABLE OF DUAL CIRCUIT IS CHAFFED. MAINTENANCE INSTALLED SERVICEABLE RT O/B DUAL CIRCUIT CABLE PN 7227105-562 IAW SF340 AMM 27-21-25.

Part: CONTROL CABLE — CHAFED (AILERON) · airframe 29,893 hrs · 33,561 cycles

DURING 4K-CHECK IN CWA, LT O/B AILERON FWD WING CABLE IS CHAFFED. MAINTENANCE REMOVED AND REPLACED FWD LT O/B WING CABLE PN 7227151-522 IAW SAAB 340 AMM 27-11-25.

Part: CONTROL CABLE — CHAFED (RUDDER) · airframe 29,893 hrs · 33,561 cycles

DURING 4K-CHECK IN CWA, FWD RT FUSELAGE RUDDER CIRCUIT AFT SINGLE CABLE IS CHAFFED. MAINTENANCE INSTALLED SERVICEABLE RT SINGLE AFT RUDDER CABLE PN 7227105-582 IAW SF340 AMM 27-21-25.

Part: CONTROL CABLE — CHAFED (AILERON) · airframe 29,893 hrs · 33,561 cycles

DURING 4K-CHECK IN CWA, RT O/B FWD AILERON WING CABLE IS CHAFED. MAINTENANCE REPLACED RT O/B FWD AILERON CABLE ASSEMBLY PN 7227151-522 IAW SAAB AMM 27-11-00-2.

Part: PROBE — DEFECTIVE (LT ENGINE)

DURING FLIGHT NR 3354, LT PROP OIL TEMP FLUCTUATES. AIR RETURN TO DTW. MAINTENANCE REPLACED LT ENGINE OIL TEMP PROBE IAW GE MM CHAP 79. REPLACED LT ENGINE OIL TEMP/PRESS INDICATOR IAW SAAB AMM CH 77. PERFORMED GROUND RUNS. ALL INDICATIONS NORMAL OIL QUANTITY CHECK GOOD. ENG OIL TEMP PROBE P/N 4053T73P01, S/N ON EGNAB451. ENG OIL INDICATOR P/N 522794, S/N ON 06871426.

Part: COMPUTER — FAILED (E/E BAY)

DURING FLIGHT 3372 AFTER TAKEOFF, YD OR AUTO-PILOT WOULD NOT STAY ENGAGED. F/O'S ADI SHOWED 8 DEGREE BANK TO LEFT IN STRAIGHT AND LEVEL. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 2 AHRS COMPUTER P/N 622-6190-113, S/N OFF 9285, S/N ON 248. NR 2 AHRS, OPS CHECKS GOOD IAW SF340 MM CHAP 34.

Part: BATTERY — DEFECTIVE (LT & RT)

DURING FLIGHT 2831, CREW REPORTED NO BATTERY START LIGHT WAS ON. AIR TURNBACK TO MSP. MAINTENANCE REMOVED AND REPLACED LT & RT BATTERY LT P/N 4078-7 SN/ON GO2561, RT P/N 4078-7 SN/ON EO2584 IAW TASK CARD 243401. OPS CHECK GOOD.

Part: COMPUTER — FAILED (NR 2 AHRS)

AFTER TAKEOFF FO'S EFIS WENT TO SKELETON MODE ON BOTH TUBES, ATT, PITCH, ROLL AND HDG FLAGS APPEARED, QRH COMPLETED -XSIDE DATA SELECTED. AIRCRAFT RETURNED TO MSP. MAINTENANCE COULD NOT DUPLICATE ON GROUND. REPLACED NR 2 AHRS AS PRECAUTIONARY MEASURE. SYSTEMS OPS CHECK GOOD IAW SF 340 MM.

Part: COMPUTER — FAILED (NR 2 AHRS)

RED THEN YELLOW HEADING FLAG IN FLIGHT. AC RETURNED TO MSP. MAINTENANCE REPLACED NR 2 AHRS COMPUTER. OPS CHECKS GOOD IAW SF340 MM CHAP 34.

Part: CONNECTOR — CONTAMINATED (INTAKE DEICE)

RT INTAKE HEAT LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO DTW DUE TO WEATHER. MAINTENANCE CLEANED OIL AT UPPER DUCT CANNON PLUG, GROUND RAN 30 MINUTES. ALL CHECKS GOOD. SEE 409 135155 FOR FURTHER DETAILS.

Part: TRANSMITTER — FAILED (LT PROPELLER)

LT PROP OIL PRESSURE FLUCUATES. AIR RETURN TO DTW. MAINTENANCE REPLACED LG PGD OIL TRANSMITTER. OPS CHECK GOOD.

Part: SKIN — CHAFED (LT NACELLE)

DURING HEAVY CHECK INSPECTION FOUND CHAFED SKIN ON LEFT INBOARD NACELLE SKIN. MAINTENANCE PERFORMED PERMANENT REPAIR IAW EO NR S54021.

Part: SKIN — CHAFED (RT NACELLE)

DURING HEAVY CHECK INSPECTION FOUND RIGHT INBOARD NACELLE SKIN CHAFED. MAINTENANCE PERFORMED PERMENANT REPAIR IAW EO NR S54022.

Part: SEAT TRACK — CORRODED (BS 297 - 357)

DURING HEAVY CHECK INSPECTION, FOUND CENTER FORWARD SEAT TRACK CORRODED FROM STA 297 TO 357. MAINTENANCE REPAIRED BY COMPLETING SEAT TRACK SPLICE REPAIR PER IAW EO NR S53060.

Part: POWER SUPPLY — INOP (ROW 20LN)

EMERGENCY LIGHTS ON WHEN SWITCHED IN ARMED POSITION. MAINTENANCE REPLACED POWER SUPPLY 20LN. OPS CHECKS GOOD.

Part: TRANSDUCER — FAILED (LT ENGINE)

AFTER TAKEOFF, LEFT PROP OIL INCREASED TO 150 PSI. CREW BEGAN QRH PROCEDURES AND LEFT RPM BEGAN TO FLUCTUATE AND LEFT PROP PSI BEGAN TO INCREASE. CREW ACCOMPLISHED ENGINE SHUTDOWN AS PER QRH AND LANDED IN CWA. MAINTENANCE FOUND GAUGE STUCK AT 160 PSI, REMOVED TRANSDUCER CANNON PLUG AND GAUGE DROPPED TO ZERO. MAINTENANCE REPLACED PGB TRANSDUCER. OPS CHECK DURING GROUND RUN GOOD. TEST FLIGHT REQUIRED DUE TO REPEAT LT PGB OIL PRESSURE GOING HIGHER THAN NORMAL IN FLIGHT. TEST FLIGHT SATISFACTORY, COMPLETED WALKAROUND OF AIRCRAFT. NO DEFECTS NOTED.

Part: GAUGE — FAILED (COCKPIT)

WHILE EN ROUTE AT 16,000 FT, NOTICED THE LEFT PROP OIL PRESSURE INDICATING 160 PSI, COMPLETED QRH. MONITORED PROP OIL PRESSURE WAS FLUCTUATING UP TO 190 PSI. DIVERTED TO MKG. MAINTENANCE INSPECTED LT PGB OIL SYSTEM, RAN A/C AT HIGH POWER SETTING TO DUPLICATE PROBLEM, INSTALLED NEW RT GAUGE. ALL CHECKS NORMAL.

Part: WEU — FAILED (CARGO COMPT)

CARGO SMOKE ANNUN ILLUMINATED SIX MINUTES AFTER TAKEOFF AROUND 6000 FEET. ILLUMINATED INTERMITTENTLY FOUR TIMES THEN REMAINED OFF FOR THE REMAINING TRIP BACK TO DTW. MAINTENANCE REPLACED WEU. ALL WORK DONE IAW SAAB 340 MM. ALL CHECKS GOOD.

Part: SMOKE DETECTOR — CONTAMINATED (CARGO COMPT)

CARGO SMOKE ANNUN ILLUMINATED, DURING GROUND OPERATIONS. RETURNED TO GATE. MAINTENANCE REPLACED CARGO SMOKE DETECTOR, SUSPECTED ANTS IN DETECTOR CAUSING FAULT. OPS CHECK GOOD.

Part: VALVE — FAILED (RT ENGINE)

RIGHT INTAKE LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO MSP. MAINTENANCE CANNOT DUPLICATE PROBLEM. FOLLOWING FLIGHT REPLACED START AIR VALVE IAW CT7 MM 75-00-00 PG 403-404 A/B, OPS CHECK GOOD.

Part: SWIVEL — LEAKING (RIGHT MLG)

AFTER TAKEOFF FROM FORT DODGE, GEAR WAS SELECTED UP FOLLOWED BY A HYDRAULIC CAUTION LIGHT, HYDRAULIC QUANTITY WAS NEAR RED LINE AND MAIN ACCUMULATOR WAS AT ZERO. CREW FOLLOWED QRH , UPON ARRIVAL AND SHUTDOWN IN MCW, NOTED HYDRAULIC FLUID PUDDLING UNDER RIGHT MAIN WHEEL WELL. MAINTENANCE REPLACED SWIVEL ON DRAG STRUT. PERFROMED ALL LEAK AND OPS CHECKS PER AMM 32-34-00, ALL OPS AND LEAKS CHECKS GOOD.

Part: BULB — FAILED (CABIN)

DURING INSPECTION 4C, EMERGENCY LIGHT INOP. REPLACED LAMP, OPS CHECK GOOD.

Part: BULB — FAILED (CABIN)

DURING INSPECTION, EMERGENCY EXIT SIGN AT SEAT 1A INOP. MAINTENANCE RELAMPED, ALL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

DURING INSPECTIO, EMERGENCY OVERHEAD LIGHTS INOP AT 2A, 6C/D AND 8C/D. MAINTENANCE RELAMPED. ALL CHECKS GOOD.

Part: VALVE — FAILED (LT ENGINE)

DURING FLIGHT, LEFT AIR VALVE ILLUMINATED WHEN SWITCH TURNED ON, NO TORQUE DROP OR ITT RISE NOTED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED LEFT ENGINE START BLEED AIR VALVE. OPS CHECK FOR 15 MINUTES GOOD. ALL IAW GE MM.

Part: VALVE — FAILED (LT BLEED AIR)

DURING FLIGHT, LEFT AIR VALVE LIGHT ILLUMINATED. CREW PERFORMED ALL APPROPRIATE CHECKS, STILL INOP. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED LEFT ENGINE AIR BLEED SHUT OFF VALVE. ALL IAW GE MM, OPS CHECK GOOD ON THE GROUND.

Part: CHIP LIGHT — ILLUMINATED (LT ENGINE)

LEFT ENGINE CHIP DETECTION LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT RETURNED TO DTW. MAINTENANCE REMOVED CHIP DETECTOR AND FOUND CHIP TO BE ALLOWABLE PLATING MATERIAL. RAN AIRCRAFT, ALL CHECKS GOOD.

Part: ACTUATOR — FAILED (RT MLG)

ON LANDING WHEN LANDING GEAR WAS EXTENDED FOR LANDING THE HYDRAULIC LIGHT WENT ON AND 2 GREEN LIGHTS CAME ON. QRH PROCEDURES USED TO EXTEND GEAR. LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR RETRACT ACTUATOR. ALL IAW SAAB AMM CH 32. ALL CHECKS GOOD.

Part: EHSI — FAILED (RT COCKPIT)

DURING FLIGHT, RIGHT HSI INOP. SCREEN IS BLACK. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED RIGHT EHSI, SYSTEM OPS GOOD.

Part: SWITCH — DIRTY (CABIN)

DURING FLIGHT, THE EMERGENCY LIGHTS CAME ON IN THE ARMED POSITION. MAINTENACE CLEANED FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH BY DOOR. OPS CHECK GOOD.

Part: BULB — FAILED (CABIN)

DURING INSPECTION, SEAT 6A OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD.

Part: BULB — FAILED (CABIN)

DURING INSPECTION, EMERGENCY OVERHEAD LIGHTS INOP AT ROW 8 C/D AND 9A. MAINTENANCE RELAMPED BOTH OVERHEAD EMERGENCY LIGHTS. ALL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

DURING INSPECTION, ONE FLOOR TRACK EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. ALL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

DURING INSPECTION, ONE OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT. ALL CHECKS GOOD.

Part: BULB — FAILED (CABIN)

DURING INSPECTION, ROW 8D EMERGENCY LIGHT FOUND INOPERABLE. MAINTENANCE RE-LAMPED EMERGENCY LIGHT AT 8D. ALL CHECKS GOOD. (X)

Part: BULB — FAILED (CABIN)

DURING INSPECTION, ONE EMERGENCY LIGHT OUT AT SEAT 2A. MAINTENANCE REPLACED LAMP. ALL CHECKS GOOD. (M)

Part: BULB — FAILED (CABIN)

DURING INSPECTION, ROW 9A EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. (M)

Part: BULB — FAILED (CABIN)

DURING INSPECTION, ROW 6 OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. (M)

Part: WINDSHIELD — SHATTERED (RT COCKPIT)

FLT 3432 - DURING CRUISE, THE RIGHT OUTSIDE FRONT WINDSHIELD SHATTERED. MAINTENANCE REPLACED FIRST OFFICER'S FRONT WINDSHIELD. ALL CHECKS GOOD. (X)

Part: ENGINE — FAILED (LEFT)

FLT 3025 - IN FLIGHT THE LEFT ENGINE OIL PRESSURE DROPPED, FOLLOWED BY CWP WARNING LIGHT. RAN QR PLUS 1 ENGINES AND SHUT DOWN ENGINE. DIVERTED TO IND AND LANDED. MAINTENANCE REPLACED LEFT ENGINE. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

DURING INSPECTION, TWO EMERGENCY LIGHTS WERE FOUND INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. (M)

Part: BULB — FAILED (CABIN)

DURING INSPECTION, FLOOR EMERGENCY EXIT LIGHT AND TWO EMERGENCY OVERHEAD LIGHTS WERE FOUND TO BE INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. (M)

Part: BULB — FAILED (CABIN)

DURING INSPECTION, FLOOR EMERGENCY EXIT LIGHT AND TWO EMERGENCY OVERHEAD LIGHTS WERE FOUND TO BE INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. REFERENCE MALA975407.

Part: DE-ICE MODULE — FAILED (RIGHT)

FLT 2942 - RIGHT INTAKE HEAT LIGHT CYCLED ON AND OFF DURING FLIGHT. AIRCRAFT WAS HEADED FOR ICING CONDITIONS, SO THEY RETURNED TO DTW. MAINTENANCE REMOVED AND REPLACED RIGHT DE-ICE MODULE. OPS AND SECURITY CHECK GOOD. (M)

Part: BLADE — CRACKED (OUTER SLEEVE)

DURING INSPECTION FOR OVERHAUL, FOUND OUTER SLEEVE CRACKED WHERE PTFE TAPE FITS. PROPELLER HAD BEEN REMOVED FOR ROUTINE MAINTENANCE.