N403XJ

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 39,798 hrs · 40,175 cycles

LEFT GALLEY EXIT LOCATOR LIGHT INOPERATIVE DURING SCHEDULED INSPECTION. TROUBLESHOT SYS. PINNED WIRES AT CONNECTOR. OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 39,782 hrs

CARGO SMOKE LIGHT ON CWP ILLUMINATED INFLIGHT THEN CARGO, LAVATORY & AVIONICS LIGHTS ILLUMINATED ON SHUTDOWN. PERFORMED CONTINUITY CHECKS ON SYSTEM'S WIRING, NO DEFECTS NOTED. R & R AVIONICS & LAVATORY SMOKE DETECTORS FOR TROUBLESHOOTING OPERATIONS CHECK OK. WEU REPLACED FOR TROUBLESHOOTING OPERATIONS CHECKED OK ALSO PERFORMED OVERWEIGHT LANDING INSPECTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,184 hrs · 39,817 cycles

FLIGHT ATTENDANT PANEL EMERGENCY LIGHTING ARM LIGHT INOPERATIVE. RE-LAMPED THE ARM LIGHT. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — LOOSE (LT MLG) · airframe 38,827 hrs

NO LT MAIN GEAR GREEN LIGHT ON GEAR EXTENSION DECLARED EMERGENCY. FOUND LT DOWN LOCK CONNECTOR 5/6 GA LOOSE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,542 hrs

FLIGHT ATTENDANT PANEL EMERGENCY LIGHTS ARM DOES NOT ILLUMINATE WHEN ARMED.

Part: RELAY — FAILED (RT INTAKE HEAT) · airframe 38,196 hrs · 39,205 cycles

RIGHT INTAKE LIGHT REMAINS ON. R & R RIGHT INTAKE HEAT AC POWER RELAY.

Part: TRANSCEIVER — FAILED (NR 2 COMMS) · airframe 38,031 hrs

NR 2 COM BLACKED OUT, STUCK ON ONE FREQUENCY INSTALLED SERVICABLE NR 2 COM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,005 hrs · 38,527 cycles

FOUND ARM LIGHT BURNED OUT DURING EMERGENCY LIGHTING TEST. REPLACED LAMP, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,445 hrs · 38,164 cycles

F/A PANEL EMERGENCY ARMED LAMP OUT THAT WAS DISCOVERED DURING LINE MAINTENANCE. RELAMPED EMERGENCY LIGHT ARMED LIGHT ON F/A PANEL.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 36,090 hrs · 37,955 cycles

DURING SCHEDULED MAINTENANCE CHECK. CHECK OF EMERGENCY LIGHTING POWER SUPPLY; ONE POWER SUPPLY OF THE 4 ON THE AIRCRAFT FAILED THE CAPACITANCE CHECK PORTION OF THE TEST. IT WAS REMOVED FROM THE AIRCRAFT AND REPLACED WITH A SERVICEABLE ASSEMBLY.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 28,496 hrs · 31,880 cycles

DENT LOCATED IN RT FLAP ASSY TOP SKIN 19.5 INCH FROM INBOARD EDGE, 3 INCHES FROM, AFT EDGE. REPAIRED

Part: SKIN — DENTED (TE FLAP) · airframe 28,496 hrs · 31,249 cycles

DENT LOCATED IN LT FLAP ASSY 38.5 INCHES OUTBOARD FROM INBOARD EDGE ON PANEL 541AT, REPAIRED.

Part: SKIN PANEL — DENTED (T/E FLAP) · airframe 27,225 hrs · 29,768 cycles

THREE DENTS WERE FOUND ON RT FLAP UPPER SKIN PANEL 641AT FROM WS 94.5 TO WS 99. DENTS WERE REPAIRED IAW EOS57201. (S)

Part: FRAME — DAMAGED (FUSELAGE) · airframe 27,225 hrs · 29,768 cycles

UPPER FLANGE ON BOTTOM FUSELAGE FRAME STA 294, RBL 18.38. REPAIRED IAW EONRS53108. (S)

Part: STRUCTURE — DAMAGED (T/E FLAP) · airframe 27,225 hrs · 29,768 cycles

FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR FASTENERS. REPLACED IAW EOS57051. (S)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,225 hrs · 29,768 cycles

CORROSION NOTED ON I/B FWD SIDE OF CENTER SEAT TRACK BL 0 STA 297-STA 303.25. REPAIRED IAW EOS53342. (S)

Part: SKIN — DAMAGED (T/E FLAP) · airframe 27,225 hrs · 29,768 cycles

DURING INSTALLATION OF RT FLAP DAMAGE OCCURRED TO THE LEADING EDGE AT WS 174.3. DAMAGE WAS REPAIRED IAW EO57204 AND EO57060. (S)

Part: SKIN — DENTED (ESCAPE HATCH) · airframe 27,225 hrs · 29,768 cycles

DENT NOTED ON FWD LT CORNER OUTER SKIN OF CREW ESCAPE HATCH. REPAIRED IAW EONRS52028. (S)

Part: SEAL — LOOSE (OVERHEAT DETECT) · airframe 26,659 hrs · 29,194 cycles

R TAILPIPE HOT INDICATION ON TAKEOFF CLIMB-OUT. RESEALED DETECTOR IAW SAAB MM 26-00-00, ALL CKS GOOD.

Part: COMPUTER — MALFUNCTIONED (NR 1 AHRS) · airframe 23,381 hrs · 25,501 cycles

ON TAKEOFF AFTER GEAR CAME UP, THE VERBAL BANK ANGLE SOUNDED CONTINUOUSLY. QRH, PROBLEM REMAINS. ALSO THE YELLOW HDG FLAG ON EHSI CAME ON BOTH CAPTAIN AND FO'S DISPLAY. RESET IAW QRH, PROBLEM REMAINS. REMOVED AND REPLACED NR 1 AHRS COMPUTER. P/N ON/OFF 622-6190-113, S/N ON 1048, S/N OFF 1314. SYSTEMS CHECK GOOD.

Part: ODOR — DETECTED (CABIN) · airframe 23,135 hrs · 25,205 cycles

CREW REPORTED THAT AFTER THE START OF THE RIGHT ENGINE THE PAX AND FA COMPLAINED OF A BURNING SMELL IN THE CABIN. NO SMOKE WAS REPORTED. RAN ENGINE WITH LP, HP ON, ALL LIGHTS ON. NO BURNING SMELL NOTED. A/C GOOD FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (AILERONS) · airframe 22,549 hrs · 24,590 cycles

DURING 4K CHECK IN BNA FOUND RT AILERON LEAKING EDGE 651DB HAS MINOR COMPOSITE DAMAGE AND HAS BEEN REPAIRED IAW MESABA EO S51031.

Part: SEAT TRACK — CORRODED (BS 297) · airframe 22,548 hrs · 24,589 cycles

DURING 4K CHECK IN BNA FOUND SEAT TRACK AT BL 0 AT FS 297, PREVIOUS REPAIR IS CORRODED OUT OF LIMITS. THE PREVIOUS REPAIR HAS BEEN REMOVED AND REPLACED IAW MESABA EO S53342.

Part: SKIN — DENTED (BS 319-390) · airframe 22,548 hrs · 24,589 cycles

DURING 4K CHECK IN BNA FOUND RT FUSELAGE IS DENTED BETWEEN FS 319 AND 390 AND BETWEEN SL1616 AND SL1620. TWO EXTERNAL DOUBLERS HAVE BEEN INSTALLED IN THE AREA IAW MESABA EO S53005.

Part: SEAT TRACK — CORRODED (BS 300-339) · airframe 22,548 hrs · 24,589 cycles

DURING 4K CHECK IN BNA FOUND SEAT TRACK AT BL 0 BETWEEN FS 300 AND 339 IS CORRODED OUT OF LIMITS. THE DAMAGED TRACK HAS BEEN REPAIRED IAW MESABA EO S53342.

Part: SEAT TRACK — CORRODED (BS 300-319) · airframe 22,548 hrs · 24,589 cycles

DURING 4K CHECK IN BNA FOUND SEAT TRACK AT LBL 18.3, BETWEEN FS 300 AND 319 IS CORRODED OUT OF LIMITS. THE DAMAGED SEAT TRACK HAS BEEN REMOVED AND REPLACED IAW MESABA EO S53060.

Part: FRAME — CORRODED · airframe 20,863 hrs · 22,633 cycles

IRREGULAR ROUTING DUE TO AIRFRAME CORROSSION NOTED DURING ROUTINE MAINTENANCE. NO FURTHER INFORMATION AT THIS TIME.

Part: SENSOR — DIRTY (TAIL PIPE) · airframe 20,255 hrs · 22,088 cycles

IN MEM, THE CREW ABORTED THE TAKEOFF DUE TO HIGH TAIL PIPE TEMPERATURE INDICATION. CLEANED SENSOR.

Part: SENSOR — DIRTY (RT TAIL PIPE) · airframe 20,255 hrs · 22,008 cycles

ON TAKEOFF ROLL, THE RIGHT TAIL PIPE HOT LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AT 70 KNTS WITH MINIMUM BRAKING. CLEANED SENSOR.

Part: SWITCH — BROKEN (COCKPIT) · airframe 20,247 hrs · 22,000 cycles

AIR TURNBACK- CTOT SWITCH BROKE OFF AFTER TAKEOFF. REMOVED AND REPLACED CTOT PANEL P/N BOTH 7239060-503, S/N ON 872621, S/N OFF 0339 NEEDS OPS CHECK LB 9850. OPS CHECKED CTOT SYSTEM IAW AMM CH 71-00-00-5.

Part: CONNECTOR — LOOSE (DECU)

LEFT PROP NP INDICATION WENT TO ZERO WHEN PROPS WENT TO MAX ON FINAL. AFTER LANDING IT WENT BACK TO NORMAL. MAINTENANCE COULD NOT DUPLICATE PROBLEM. UPON INSPECTION OFF LEFT ENGINE YELLOW HARNESS FOUND CONNECTOR TO DECU EXTREMELY LOOSE AND CONNECTOR TO NP SENSOR ALSO LOOSE. TIGHTENED CANNON PLUGS. OPS CHECK OK.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 18,898 hrs · 20,498 cycles

DURING SCHEDULED CAPACITY CHECK, BATTERY POWER SUPPLY P/N 3301-51, S/N 1317 FAILED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 AND UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/15/04.

Part: INDICATOR — INOPERATIVE (LT PROP RPM) · airframe 18,059 hrs · 19,610 cycles

AFTER TAKEOFF LEFT PROP RPM INDICATOR INDICATED ZERO CYCLED C/B J-8, INDICATOR STILL INDICATED ZERO. WHILE RETURNING TO DTW INDICATOR WORKED INTERMITTENTLY. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED GAUGE P/N 10223N01R00, S/N OFF 117, S/N ON BG05.

Part: MOUNT — CORRODED (LAVATORY) · airframe 17,321 hrs · 18,843 cycles

DURING 4K INSPECTION IN LCQ, FWD LAV AFT I/B MOUNT HAS EVIDENCE OF CORROSION. MAINTENANCE REMOVED CORRODED LAV MOUNT, FABRICATED NEW MOUNT AND INSTALLED, IAW MESABA EO S25063, REV 0 DATED 19 DEC 2003. A/C RELEASE DATE 12/24/03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,321 hrs · 18,843 cycles

DURING 4K INSPECTION IN LCQ, FS 620 TO FS 686, LT BL 18.3 SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SEAT TRACK SECTION FROM FS 620 - FS 686 IAW MESABA EO A53060 DATED 3 NOV 2003. A/C RELEASE DATE 12/24/03.

Part: POWER LEVER — OUT OF RIG (COCKPIT) · airframe 16,915 hrs · 18,405 cycles

DURING CLIMBOUT ON FLIGHT 2987, LT ENGINE WAS FIREWALLED FROM 17000 TO CRUISE ALTITUDE 22000. RAN APPROX 5 - 6 PERCENT LESS THAN CHARTED TORQUE. ITT WAS APPROXIMATELY 830-840. AIR RETURN TO MSP AS PER MXC, AND DISPATCH UNABLE TO MAKE CHARTED TORQUE POWER LEVER SPLIT NOTED AT MOST SETTING LEFT PL 3/4 AHEAD OF RIGHT PL. MAINTENANCE FOUND LT ENGINE OUT OF RIG. RERIGGED LT ENGINE PER SAAB AMM 76-10-00. PERFORMED GROUND RUN, FOUND NO POWER LEVER SPLIT. PERFORMED GPA, FOUND MARGIN TO BE ACCEPTABLE.

Part: BATTERY

DEAD EMERGENCY FLASHLIGHT BATTERIES. MAINTENANCE REPLACED BATTERY PN P4-01-0021. OPS CHECKS GOOD.

Part: COMPUTER — FAILED (E/E BAY)

DURING FLIGHT NR 2820, RT AHARS COMPUTER FAILED. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS COMPUTER P/N 622-6190-113, S/N ON 2247, S/N OFF 2788, SYSTEM OPS CHECK GOOD IAW SF340 MM CHAPTER 34.

Part: ACTUATOR — FAULTY (AILERON)

DURING FLIGHT 3052 MAIN AILERON TRIM RUNAWAY. LEFT WING HAD STRONG DOWNLOAD FORCES. TRIM INDICATOR INDICATED FULL-UP ON INDICATOR, UNABLE TO NEUTRALIZE FORCES WITH MAIN TRIM STANDBY TRIM WORKED. AIR RETURN TO RHI. MAINTENANCE FOUND LT AILERON TRIM ACTUATOR TO BE FAULTY. REMOVED AND REPLACED LT AILERON TRIM ACTUATOR P/N D97648, S/N OFF 96H19190, S/N ON 91K1575-127 IAW SAAB MM 27-12-10. OPS CHECK GOOD.

Part: CONTROL CABLE — CHAFED (RUDDER) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, LT FUSELAGE AFT CIRCUIT I SINGLE RUDDER CABLE CHAFED. MAINTENANCE REMOVED CABLE AND INSTALLED NEW CABLE P/N 7227105-582 IAW SAAB MM 27-21.

Part: CONTROL CABLE — CHAFED (RUDDER) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, LHOB FUSELAGE DUAL CIRCUIT I RUDDER CABLE CHAFED. MAINTENANCE REPLACED LHOB FUSELAGE DUAL CIRCUIT RUDDER CABLE P/N 7227105-562, IAW SF340 27-21-25-4.

Part: CONTROL CABLE — CHAFED (RUDDER) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, RHIB FUSELAGE DUAL CIRCUIT I RUDDER CABLE CHAFED. MAINTENANCE REPLACED RHIB FUSELAGE DUAL CIRCUIT RUDDER CABLE P/N 7227105-571 IAW SF340 27-21-25-4.

Part: CONTROL CABLE — CHAFED (RUDDER) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, RHOB FUSELAGE DUAL CIRCUIT I RUDDER CABLE CHAFED. MAINTENANCE REPLACED CABLE P/N 7227105-562 IAW SF340 27-21-25-4.

Part: CONTROL CABLE — CHAFED (RUDDER) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, LHIB FUSELAGE DUAL CIRCUIT I RUDDER CABLES CHAFED. MAINTENANCE REPLACED LHIB FUSELAGE DUAL CIRCUIT RUDDER CABLE P/N 7227105-571 IAW SF340 27-21-25-4.

Part: ANGLE — CORRODED · airframe 12,055 hrs · 13,318 cycles

Found during 4K-Check in CWA, Angle on Frame 258 corroded. Maintenance replaced Angle on Frame 258 PN 7253722-001 IAW Saab SRM 51.

Part: CONTROL CABLE — CHAFED (ELEVATOR) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, RHOB FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RHOB CABLE P/N 7227105-712 IAW SF340A MM 27-31-15.

Part: CONTROL CABLE — CHAFED (ELEVATOR) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, LHIB FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REPLACED LHIB ELEVATOR CABLE P/N 7227705-644 IAW SF 340A MM 27-31-15, FOR RIGGING SEE 409 024307.

Part: CHANNEL — CORRODED · airframe 12,055 hrs · 13,318 cycles

Found during 4K-Check in CWA, beam between LBL12-19 and Sta 258-254 is corroded. Maintenance Replaced channel PN 7253721-413 between Sta 258-254.

Part: ANGLE — CORRODED · airframe 12,055 hrs · 13,318 cycles

Found during 4K-Check in CWA, Angle between Frame 237 and 258 is corroded. Maintenance installed new Angle at Frame 237 and 258. IAW Saab SRM 51 PN 7253721-447

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, FOUND CORROSION IN CARGO SEAT TRACK BL 0 BETWEEN STA 640 - 687. MAINTENANCE REMOVED AND REPLACED SEAT TRACK SECTION IAW EO S53060, BETWEEN STA 619 - 687.

Part: CONTROL CABLE — CHAFED (ELEVATOR) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, RHIB FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED I/B CABLE P/N 7227705-644 IAW SF340A MM 27-31-15.

Part: CONTROL CABLE — CHAFED (ELEVATOR) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, LHOB FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REPLACED LHOB ELEVATOR CABLE P/N 7227105-712 IAW SF340 AMM 27-31-15 FOR RIGGING SEE 409 024307.

Part: CONTROL CABLE — CHAFED (AILERON) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, LHOB FWD FUSELAGE AILERON CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED LHOB FWD FUSELAGE AILERON P/N 7227105-613. FOR RIG AND OPS CHECK SEE 409 024306.

Part: CONTROL CABLE — CHAFED (AILERON) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, LT AND RT FWD FUSELAGE AILERON CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED LHIB FWD FUSELAGE AILERON CABLE IAW SF3 AMM 27-11-25 P/N 7227105-623. FOR RIG AND OPS CHECK SEE 409 024306.

Part: STRUCTURE — CHAFED (RT NACELLE) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, RT NACELLE LOWER I/B CHAFED AT STA 227. REPAIRED IAW SAAB STATEMENT 340 SDS002027, EO S54055. MAINTENANCE REPAIRED CHAFED AREA IAW SAAB STATEMENT.

Part: CONTROL CABLE — CHAFED (AILERON) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, RHOB FWD FUSELAGE AILERON CABLE CHAFED. REMOVED AND REPLACED CABLE IAW SF3 AMM 27-11-25. P/N ON 7227105-624 FOR RIG AND OPS CHECK SEE 409 024306.

Part: CONTROL CABLE — CHAFED (AILERON) · airframe 12,055 hrs · 13,318 cycles

FOUND DURING 4K-CHECK IN CWA, RHIB FWD FUSELAGE AILERON CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RHIB FWD FUSELAGE AILERON CABLE IAW SF3 AMM 27-11-25 P/N ON 7227105-614. FOR RIG AND OPS CHECK SEE 409 024306.

Part: ANGLE — CORRODED · airframe 12,055 hrs · 13,318 cycles

During 4K-Check, Angle on beam between Sta 272-287 RBL 10 is corroded. Maintenance removed and replaced Angle PN 7253720-337 IAW SRM Chap. 51.

Part: FRAME — CORRODED · airframe 12,055 hrs · 13,318 cycles

Found during 4K-Check, corrosion on Frame Sta 225. Completed repair IAW Saab Statement #340SDS002013. Rev A EO S53097. Maintenance completed repairs IAW Saab Statement 340SDS0021 dated 2001-06-27

Part: BEAM — CORRODED · airframe 12,055 hrs · 13,318 cycles

Found during 4K-Check, Beam between Sta 272-287 LBL11 is corroded. Maintenance removed and replaced beam PN 7253720-325 IAW SRM Chap 51. Refer to 409 #024452.

Part: CONTROL CABLE — CHAFED (RUDDER) · airframe 12,055 hrs · 13,318 cycles

DURING 4K-CHECK, RT FUSELAGE AFT CIRCUIT I SINGLE RUDDER CABLE CHAFED. MAINTENANCE REMOVED CABLE AND INSTALLED NEW P/N 7227105-582 IAW SAAB MM 27-21-25. SEE 409 24308 FOR RIGGING.

Part: DRAIN VALVE — FAILED (LT ENGINE)

DURING TAKEOFF, NOTICED LEFT ENGINE TORQUE NOT DEVELOPING FULL POWER. RAMP AGENT NOTICED LT EPA CAN SPRAYING FUEL. MX FOUND FUEL LEAKING FROM O/S DRAIN VALVE. REPLACED O/S DRAIN VALVE, GROUND RAN ENGINE TORQUE STILL A PROBLEM. REPLACED LT HMUPN 6068T72P18, OPS CHECK GOOD.

Part: AIRSPEED IND — FAILED (LT COCKPIT)

LT AIRSPEED IND DEAD. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED AIRSPEED IND, OPS CHECKS GOOD.

Part: RETRACT MECH — LACK OF LUBE (LANDING GEAR)

UPON GEAR RETRACTION AFTER TAKEOFF, GEAR WOULD NOT RETRACT. MAINTENANCE COMPLETED SEVERAL GEAR SWINGS. CLEANED AND LUBED GEAR SWITCHES. OPS CHECKS GOOD.

Part: INDICATOR — FAILED (LT PROP OIL TEMP)

ON CLIMBOUT, THE LEFT PROP OIL TEMP DROPPED BELOW GREEN ARC TO ABOUT 35 DEGREES. RESET CIRCUIT BREAKER, IT THEN DROPPED TO 25 DEGREES AND STAYED THERE UNTIL LANDING BACK IN MSP. MAINTENANCE REPLACED LEFT PROP OIL PRESS/TEMP INDICATOR, OPS CHECK GOOD.

Part: BULB — FAILED (FUSELAGE)

DURING INSPECTION, LEFT EXTERNAL EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. OPS CHECKS GOOD.

Part: BALLAST — FAILED (LAVATORY)

INBOUND FOUND LAV SMOKE LIGHT ILLUMINATED. MAINTENANCE REPLACED LAV LIGHT BALLAST. OPS CHECKS GOOD.

Part: SKIN — DENTED (BS 341-359)

DURING 4K CHECK, FOUND DENTS AND SEVERE OIL CANNING BETWEEN STATIONS 341 AND 359 FROM WL 100 TO WL 88. THESE DENTS ARE ON THE RIGHT SIDE OF THE AIRCRAFT. MAINTENANCE REPAIRED THIS AREA WITH A DOUBLER/TRIPLER OVERLAP REPAIR AND BONDED TO THE FUSELAGE SKIN. COMPLETED WITH ACCORDANCE TO SAAB SRM 57-70-10.

Part: STRUT — REQ'D SERV (LT MLG)

FLT 3006 - DID AN AIR TURNBACK TO DTW AFTER LIFTOFF GOT CONFIGURATION WARNING LIGHT, ICE PROTECTION AND OAT CAUTION LIGHT. MAINTENANCE SERVICED LEFT MAIN STRUT, VERIFIED PROPER OPERATION AT OAT HEAT AND TCAS. ALL CHECKS GOOD. (M)

Part: RT UNIT — FAILED (FWD FUSELAGE)

FLT 2907 - EN ROUTE, THE WEATHER RADAR SYSTEM STOPPED WORKING. THE CREW RESET THE CIRCUIT BREAKER AND IT BEGAN TO WORK INTERMITTENTLY. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE WEATHER RADAR R/T. ALL CHECKS SATISFACTORY. (X)

Part: CONNECTOR — LOOSE (CABIN)

FLT 3311 - DURING THE PRE-FLIGHT INSPECTION IN DTW, THE EMERGENCY EXIT LIGHT ABOVE THE FLIGHT ATTENDANT'S SEAT WAS FOUND INOPERATIVE. MAINTENANCE RESECURED LOOSE PLUG WIRES AT PLUG 465VP. ALL CHECKS SATISFACTORY. (X)