N412XJ

Part: COVER — MISSING (SWITCH) · airframe 39,624 hrs · 43,498 cycles

FLIGHT# 0130 MCO/FLL REPORT: F/A EMERGENCY PANEL, MISSSING COVER FOR PUSH BUTTON SWITCH. CORRECTIVE ACTION: FOUND AND RESECURED COVER IAW AMM 20-00-00.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 39,484 hrs · 43,390 cycles

FLIGHT# 0089 EYW/TPA REPORT: F/A EMERGENCY LIGHTS COVER CAME OFF. CORRECTIVE ACTION: RESECURED EMERGENCY LIGHT COVER ON F/A PANEL IAW SAAB AMM 33-50-00.

Part: LIGHT — LOOSE (CABIN) · airframe 39,225 hrs · 43,160 cycles

FLT 0061 FLL/MCO REPORT: EMERGENCY STRIP LIGHT ON ROW 12 LOOSE. SECURED LOOSE EMERGENCY LIGHT STRIP AS REQUIRED OPS CHECK GOOD IAW AMM 33-50-20-04 ROW 12.

Part: SWITCH — STUCK (EMERGENCY LIGHTS) · airframe 39,093 hrs · 43,014 cycles

EMERGENCY LIGHTS REMAIN ON AFTER ALL POWER REMOVED AND THE SWITCH OFF. FOUND F/A SWITCH GUARD PRESSED IN, ADJUSTED SWITCH IAW AMM 39-40-60-04. OPS CHECKED GOOD.

Part: LIGHT — DISCONNECTED (SEATS 11-12A) · airframe 39,047 hrs · 42,968 cycles

EMERGENCY LIGHT NEAR SEATS 11 - 12A DISCONNECTED. CONNECTED THE EMERGENCY LIGHT IAW AMM 33-50-20. OPS CHECKED GOOD ..

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,841 hrs · 42,756 cycles

FLIGHT 0075 MCO/EYW REPORT: EMERG LIGHT OUT AT ROW 9A INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW AMM 33-50-10-04-1. OPS CHECKS GOOD IAW AMM 33-50-00-05-1

Part: DOOR — LACK OF LUBE (MAIN CABIN) · airframe 37,699 hrs · 41,608 cycles

MAIN CABIN DOOR DIFFICULT OPEN AND DOOR STAIRS DIFFICULT TO SLIDE. LUBRICATED THE MAIN CABIN DOOR AND PERFORMED AN OPERATIONAL CHECK IAW AMM 52-10-00-05. LUBED DOOR STAIRS AND PERFORMED AN OPERATIONAL CHECK IAW AMM 52-60-00-05, NO DEFECT NOTED.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 37,501 hrs · 41,400 cycles

LEFT EMERGENCY LIGHT OVER BATTERY COMPARTMENT WIRES DISCONNECTED. SECURED THE WIRES, OPERATIONAL CHECKED GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 37,142 hrs · 41,035 cycles

FLIGHT 0082, BURNING SMELL IN FLIGHT DECK OCCURRED DURING FLIGHT. INSPECTED BOTH ENGINES NO DEFECTS NOTED. RAN AIRCRAFT AT FULL POWER WITH CREW NO BURNING SMELL NOTED. CYCLED A/C SYSTEMS WITH NO APPARENT ODOR PER AMM 72-00-00.

Part: CONNECTOR — DIRTY (CABIN) · airframe 36,000 hrs · 39,763 cycles

CREW REPORTED F/A PANEL ARM LIGHT INOPERATIVE. R & R GE85 BULB NO FIX. REMOVED LOWER TRIM PANEL TO ACCESS CONNECTOR PLUG, CLEANED AND RESEATED CONNECTOR PLUG, OPS CHECKED GOOD IAW AMM CHAPTER 33-50-00.

Part: CIRCUIT BREAKER — WEAK · airframe 35,998 hrs · 39,760 cycles

L8 CIRCUIT BREAKER, EXT CTRL, POPPED AND WOULD NOT RESET. INSP L8 CB FOUND TO BE LOOSE, WEAK. RR L8 CB IAW MM 39-10-42. OPS CK OK PN ON/OFF MS3320-5.

Part: CIRCUIT BREAKER — POPPED (EMERGENCY LIGHTS) · airframe 35,928 hrs · 39,687 cycles

L-8 CIRCUIT BREAKER POPPED IN FLIGHT. PERFORMED OPS CHECK ON EMERGENCY LIGHTING SYS IAW AMM REF 33-50-20-04. OPS CHECK NORMAL.

Part: DRAG BRACE — DAMAGED (RT MLG) · airframe 39,504 hrs · 35,746 cycles

FOUND DURING MAINTENANCE: RT MLG LOWER LINK AND BEARING ASSY BEARING DISPLACED. R & R RT MLG DRAG BRACE IAW TASK CARD 32-11-10S AND PERFORMED GEAR EXTENSTION AND RETRACTION FUNCTIONAL CHECK IAW AMM 32-30-00. OPS CHECKS GOOD LEAK CHECKS GOOD.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 35,554 hrs · 39,291 cycles

CIRCUIT BREAKER, L8, EMERGENCY AND EXTERIOR LIGHTS TRIPPED DURING FLIGHT. RESET THE CIRCUIT BREAKER. PERFORMED EMERGENCY LIGHTING OPS TEST IAW AMM 33-50-00-05-1.

Part: BULB — BURNED OUT (CONTROL PANEL) · airframe 35,527 hrs · 39,258 cycles

ON F/A LIGHT PANEL EMERGENCY LIGHT SWITCH DOES NOT ILLUMINATE ON ARM WHEN BOTH ENGINES ARE RUNNING. R & R LIGHT BULB TO F\A LIGHT PANEL EMERGENCY LIGHT SWITCH IAW AMM 33-32-10-04, PERFORMED OPS CHECK, OPS CHECK SATISFACTORY,

Part: BUTTON — BROKEN (EMERGENCY LIGHT) · airframe 35,440 hrs · 39,172 cycles

F/A PANEL EMERGENCY LIGHT SWITCH BUTTON IS BROKEN. R & R F/A PANEL EMERGENCY LIGHT SWITCH BOTTOM IAW AMM 20-10.

Part: CLAMP — BENT (BLEED SYSTEM) · airframe 35,383 hrs · 39,120 cycles

LEFT ENGINE FAILURE AND AUTO COARSENED WHILE CLIMBING THROUGH 400 FT ON TAKEOFF, LEFT ENGINE OVERTEMP LIGHT ILLUMINATED. REPLACED HP BLEED LINE CLAMP IAW AMM 36-11-00 PERFORMED BORESCOPE INSPECTION OF HOT SECTION AND POWER TURBINE MODULE IAW MM 72-00-00 AS REQUIRED IAW MM 72-00-00 SPECIAL INSPECTIONS. ALL CHECKS GOOD.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 34,997 hrs · 38,712 cycles

EMERGENCY EXIT SIGN FELL OFF DURING FLIGHT OVER EXIT DOOR 2A. R & R EMERGENCY EXIT SIGN AT EXIT DOOR 2A IAW CMM REF 25-25-15-5. OPS CHECK OK.

Part: CONTROL PANEL — MALFUNCTIONED · airframe 33,683 hrs · 37,349 cycles

LEFT ENGINE AUTOCOARSEN ON FINAL APPROACH. REPLACED CTOT PANEL OPS AND FUNCTION CHECK FLIGHT GOOD.

Part: ENGINE — OUT OF ADJUST (LEFT) · airframe 33,673 hrs · 37,338 cycles

LEFT ENGINE AUTO COARSEN ON FINAL WITH AUTO COARSEN LIGHT ILLUMINATED. PERFORMED AUTOCOARSEN SYSTEM ADJUSTMENT TEST, AUTO COARSEN SYS TEST NORMAL.

Part: ENGINE — OUT OF ADJUST (LEFT) · airframe 33,673 hrs · 37,338 cycles

LT ENGINE AUTO COARSEN ON FINAL WITH AUTO COARSEN LIGHT ILLUMINATED. PERFORMED AUTOCOARSEN SYSTEM ADJUSTMENT TEST, AUTO COARSEN SYSTEM TEST NORMAL.

Part: COMPUTER — MALFUNCTIONED · airframe 33,674 hrs · 37,339 cycles

LEFT PROPELLER AUTOCOARSEN ON FINAL APPROACH. REPLACED AUTO COARSEN COMPUTER, SWITCH, AND PRESSURE SENSOR OPS SATISFACTORY.

Part: COMPUTER — MALFUNCTIONED (ELEVATOR TRIM) · airframe 33,313 hrs · 36,884 cycles

ELEVATOR TRIM RUNAWAY WITH AUTOPILOT ENGAGED FOLLOWED BY PITCH TRIM CAUTION DISCONNECTED AUTOPILOT AND CONDITIONS PERSISTED INTERMITTENTLY. REPLACED FLIGHT CONTROL COMPUTER, NO DEFECTS NOTED. OPS CHECK GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 31,766 hrs · 35,063 cycles

EMERGENCY LIGHT SYS AT 94 AND 11A INOPERATIVE. FOUND CONNECTOR 11VP SLIGHTLY AJAR CLEANED AND RESEATED CONNECTOR.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 31,766 hrs · 35,063 cycles

EMERGENCY LIGHT SYS AT 9A AND 11A INOPERATIVE. FOUND CONNECTOR 11VP SLIGHTLY AJAR CLEANED AND RESEATED CONNECTOR PLUG. PREVIOUSLY SUBMITTED UNDER CONTROL NR 2013FA0000558, LOCKED OUT OF THE DATA BASE SUBMITTED BY SILVER AIRWAYS CORP.

Part: RELAY — INTERMITTENT (MLG) · airframe 31,626 hrs · 34,886 cycles

LANDING GEAR FAILED TO RETRACT COMPLETELY ON TAKEOFF AFTER PERFORMING QRH. GEARS RETRACTED, AIRSPEED WAS BELOW 150 DURING THE PROCESS. REPLACED HYD PUMP RELAY 7ML OPS CHECK OF LANDING GEAR EXTENSION AND RETRACTION SATISFACTORY.

Part: DOOR — MISINSTALLED (EMERGENCY EXIT) · airframe 30,008 hrs · 33,106 cycles

ON PREFLIGHT NOTICED THAT THE HANDLES ON THE OVER THE WING EMERGENCY EXIT DOOR FACING THE WRONG DIRECTION. UPON INSP, FOUND OVER WING EMERGENCY DOORS TO BE SWAPPED. R & R RESPECTIVE DOOR ON CORRESPONDING SIDE. ACCORDING TO AMM 52-20.

Part: FRAME — MISREPAIRED · airframe 24,939 hrs · 27,304 cycles

PREVIOUS REPAIR TO UNDERFLOOR FRAME STA 258 CENTER FUSELAGE REQUIRES ADDITIONAL WORK. REPAIRED SECTION IAW EO NR S53108.

Part: SKIN — DENTED (CARGO DOOR) · airframe 24,939 hrs · 27,304 cycles

DENTS LOCATED IN CARGO DOOR, ONE AT 23 INCH CARGO DOOR LOWER EDGE, 9 INCHES FROM AFT EDGE. THE OTHER AT 14 INCHES FROM LOWER EDGE, 10 INCHES FROM AFT EDGE. REPAIRED IAW EO NR S52028.

Part: SKIN PANEL — DENTED (BS 300-319) · airframe 24,939 hrs · 27,304 cycles

DENTS LOCATED UNDER ICE SHIELD NR 7 AT FS 300.5 - FS 319.5, SL1615-SL1618. INSTALLED DOUBLER TRIPLER REPAIR IAW EO NR S53009.

Part: SKIN — DENTED (PAX DOOR) · airframe 24,939 hrs · 27,304 cycles

MAIN ENTRANCE DOOR HINGE, INNER CLOSING SKIN HAS A DENT. REPAIRED IAW EO NR S52093.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 23,161 hrs · 25,200 cycles

FAILED CAP CHECK PER BF GOODRICH CMM WO 418119 PN501-1712-02. REPLACED BATTERY PACK.

Part: FLOORBEAM — CORRODED (BS 258) · airframe 22,413 hrs · 24,359 cycles

DURING CHECK IN BNA, UPPER FLOOR FLANGE, AT, FS258, RT AT BLO, IS CORRODED OUT OF LIMITS. THE DAMAGE HAS BEEN REPAIRED IAW EO NR S53108. REF: EAMS WORK ORDER 214384 TASK 1520

Part: SEAT TRACK — CORRODED (BS 339) · airframe 224,132 hrs · 24,359 cycles

DURING CHECK IN BNA FOUND SEAT TRACK AT LBL 18.3, AT FS 339, IS CORRODED OUT OF LIMITS ON THE HORIZONTAL FLANGE. THE DAMAGE HAS BEEN REPAIRED IAW EO NR S53342.

Part: FLOORBEAM — CORRODED (BS 272) · airframe 22,413 hrs · 24,359 cycles

DURING CHECK IN BNA FOUND UPPER FLOOR FLANGE AT FS272 BETWEEN RBL17 AND RBL33, IS CORRODED OUT OF LIMITS. THE DAMAGE HAS BEEN REPAIRED IAW EO NR S53108.

Part: ECU — MALFUNCTIONED (RT ENGINE) · airframe 21,901 hrs · 23,787 cycles

RT ENGINE TORQUE, ITT, NG AND NP WERE FLUCTUATING WHILE CLIMBING OUT OF MSP. PERFORMED ERRATIC ENG OPERATION QRH NAD LOCKED OUT TORQUE MOTOR. SLIGHT FLUCTUATIONS CONTINUED BUT REMAINED WITHIN ENGINE OPERATING PARAMETERS. REPLACED DECU RT SIDE. PN ON 6071T20P16, SN ON ECDT1931 PN OFF 6071T20P17, SN OFF ECDT1122. OPS CHECK GOOD

Part: SKIN — PUNCTURED (RT ELEVATOR) · airframe 21,673 hrs · 23,544 cycles

HAIL CONTACT DAMAGE ON RIGHT ELEVATOR CAUSED PUNCTURE IN UPPER COMPOSITE SKIN. PUNCTURE WAS .625 IN DIA AND 4/4 LONG. LOCATED 51 INCHES FROM I/B ELEVATOR EDGE AND 8 INCHES FROM TRAILING EDGE. DAMAGE REPAIRED WITH A COLD BOND WET LAYUP IAW SAAB SRM SECTION 51-70-50 AND MESABA EO S51031.

Part: SKIN — DENTED (RT AILERON) · airframe 21,673 hrs · 23,544 cycles

HAIL CONTACT DAMAGE ON RIGHT AILERON CAUSED DENT IN UPPER COMPOSITE SKIN. DENT WAS .75 IN DIA AND .75 IN LENGTH AND .007 DEEP. LOCATED 67.625 INCHES FROM I/B AILERON EDGE AND 5.375 INCHES FROM TRAILING EDGE. DAMAGE REPAIRED WITH A COLD BOND WET LAYUP IAW SAAB SRM SECTION 51-70-50 AND MESABA EO S51031.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 21,673 hrs · 23,544 cycles

HAIL CONTACT DAMAGE ON LEFT ELEVATOR CAUSED DENT IN UPPER COMPOSITE SKIN. DENT WAS .5 IN DIAMETER AND .375 IN LONG AND .0055 DEEP. LOCATED 31.5 INCHES FROM O/B ELEVATOR EDGE AND 9.5 INCHES FROM TRAILING EDGE. DAMAGED REPAIRED WITH A COLD BOND WET LAYUP IN ACCORDANCE WITH SAAB SECTION 51-70-50 AND MESABA EO S51031.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 21,673 hrs · 23,544 cycles

HAIL CONTACT ON LEFT ELEVATOR CAUSED DENT IN UPPER COMPOSITE SKIN. DENT WAS 1 IN DIAMETER AND 1 IN LONG AND .165 DEEP. LOCATED 17 INCHES FROM I/B ELEVATOR EDGE AND 21 INCHES FROM TRAILING EDGE. DAMAGE REPAIRED WITH A COLD BOND WET LAYUP IAW SAAB SRM SECTION 51-70-50 AND MESABA EO S51031.

Part: WARNING LIGHT — ILLUMINATED (TAIL PIPE) · airframe 20,767 hrs · 22,489 cycles

LOW ENERGY ABORT DUE TO TAIL PIPE HOT INDICATION. NO FURTHER INFO AT THIS TIME.

Part: LIGHT — INOPERATIVE (NLG) · airframe 20,562 hrs · 22,265 cycles

NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE ON EXTENSION.

Part: RAIL — CORRODED (AIRSTAIR) · airframe 19,499 hrs · 21,148 cycles

DURING 4K INSPECTION IN BNA FOUND AIRSTAIR RAIL ASSEMBLY PN 7253710-871 IS CORRODED AND WILL BE REMOVED AND REPLACED IAW SRM 51-40-21/22. REF EAMS WORK ORDER 212166 TASK 1521.

Part: ODOR — DETECTED (CABIN) · airframe 19,443 hrs · 21,087 cycles

THE CREW REPORTED, A SLIGHT CHEMICAL SMELL RIGHT AFTER DEPARTING CRW. THE SMELL QUICKLY WENT AWAY AND MAINTENANCE WAS PERFORMED LAST NIGHT.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 18,968 hrs · 20,540 cycles

EMERGENCY POWER SUPPLY 20LN FAILED CAPACITY CHECK IAW JOB CARD 335003.

Part: SENSOR — CONTAMINATED (RT TAILPIPE) · airframe 18,672 hrs · 20,236 cycles

AFTER TAKEOFF THE RT TAIL PIPE HOT LIGHT ILLUMINATED. AIR RETURN TO MEM. MAINTENANCE APPLIED SEALENT TO TAIL PIPE SENSORS IAW SMM CHP 54-30-05-2 OPS CHECK GOOD IAW SMM CHP 26-11-00-5.

Part: SMOKE DETECTOR — MALFUNCTIONED (E/E BAY) · airframe 18,317 hrs · 19,895 cycles

AVIONICS RACK SMOKE DETECTION SYSTEM ON TAKEOFF ROLL AVIONICS SMOKE LIGHT ILLUMINATED. ABORTED TAKEOFF AT ABOUT 100 KTS, NO SMOKE NOTICED. MAINTENANCE INSPECTED TIRES AND BRAKES AFTER REJECTED TAKEOFF IAW FAXED AMM 05-50-00-6, NO SIDS NOTED. CONFIRMED AVIONICS RACK SMOKE DETECTOR LIGHT. MAINTENANCE REMOVED AND REPLACED DETECTOR. REMOVED FROM DMR, REMOVED AND REPLACED AVIONICS SMOKE DETECTOR. TESTED SMOKE DETECTOR, OPS CKS GOOD. P/N 72-111211-00, S/N OFF-A5306, S/N ON-A3732. MXC NOTIFIED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,148 hrs · 19,717 cycles

DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON SEAT TRACK VERTICAL FLANGE BL 0 STA 298 ABOVE FLOORBOARD. REPAIRED PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 18,148 hrs · 19,717 cycles

DURING 4Y/2Y INSPECTION IN BNA, NOTED 4 DENTS ON RT HORIZONTAL STABILIZER UPPER SKIN. REPAIRED 2 DENTS PER EO S55017, 2 ARE WITHIN LIMITS PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04.

Part: GALLEY TRACK — CORRODED (FUSELAGE) · airframe 18,148 hrs · 19,717 cycles

DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON RT GALLEY INBOARD TRACK & PROFILE. REPLACED TRACK & PROFILE PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04.

Part: WEB — CORRODED (FWD ENTRYWAY) · airframe 18,148 hrs · 19,717 cycles

DURING 4Y/2Y INSPECTION IN BNA, NOTED FWD ENTRY WAY WEB CORRODED STA 288-294. REPLACED WEB PER SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,148 hrs · 19,717 cycles

DURING 4Y/2Y INSPECTION IN BNA, NOTED BL 0 FLOORBOARD ATTACH ANGLE CORRODED AT STA 294. FABRICATED & REPLACED ANGLE PER THE SRM. AIRCRAFT WAS RETURNED TO SERVICE 9/7/04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,148 hrs · 19,717 cycles

DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON VERTICAL FLANGE OF SEAT TRACK BL 18.3 STA 298 ABOVE FLOORBOARD. REPAIRED PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04.

Part: INDICATOR — MALFUNCTIONED (STBY ATTITUDE)

IN ROUTE TO SUX STANDBY HORIZON FLAGGED. PILOT RESET C/B. C/B POPPED AGAIN. AIRCRAFT CONTINUED ON TO SUX WHERE A/C WAS GROUNDED UNTIL REPAIRS WERE MADE. MAINTENANCE REPLACED STANDBY ATTITUDE INDICATOR P/N H341ADM2, S/N ON 5106, S/N OFF 6254. STANDBY ATT INDICATOR OPS CHECKS GOOD IAW SF 340 MM CHAP 34.

Part: COVER — DISLODGED (EMERGENCY LIGHT)

ROW 1D EMERGENCY COVER OVER HANDLE FELL OFF, NEEDS TO BE RE-SAFTIED. RE-SAFTIED RIGHT FWD EMERGENCY EXIT DOOR HANDLE AS REQUIRED, SEC CHECKS GOOD.

Part: THERMISTER — MALFUNCTIONED (LT INTAKE HEAT) · airframe 17,078 hrs · 18,568 cycles

LEFT INTAKE HEAT CYCLES ON/OFF INFLIGHT. AIR RETURN TO DTW. MX SWAPPED LEFT NORMAL THERMISTER TO NR 4 RAN FOR 20 MIN, ALL CHECKS GOOD IAW MM 30.

Part: DUCT — BURNED (AIR CONDITIONING)

DURING FLIGHT 3058 DURING TAXI, CREW REPORTED SMOKE IN CABIN. UPON INSPECTION FOUND DUCT COMING FROM SUPPLEMENTAL A/C MOTOR BURNED. NO OTHER INFORMATION AT THIS TIME.

Part: WARNING SYSTEM — ACTIVATED (RT ENGINE)

ABORTED TAKEOFF DUE TO RT TORQUE INDICATION. RESET CIRCUIT BREAKER.

Part: LIGHT — OUT OF POSITION (CABIN)

EMERGENCY FLOOR TRACK LIGHTING AT ROWS 2 AND 3 STICKS OUT ON LEFT SIDE. MAINTENANCE RESECURED EMERGENCY FLOOR TRACK LIGHTING AT ROWS 2 AND 3. ALL SECURITY CHECKS GOOD AT THIS TIME.

Part: CHIP DETECTOR — DIRTY (LT ENGINE)

AFTER STARTING LT ENGINE CHIP DETECTOR LIGHT CAME ON. REMOVED AND CLEANED CHIP DETECTOR. NO CHIPS FOUND, RAN ENGINE NO DISCREPANCIES FOUND.

Part: SENSOR — FAULTY (ENGINE)

AFTER TAKEOFF FROM DTW, FLIGHT 2755, SELECTED THE LP BLEED ON AND HAD A LT DUCT OVERTEMP LIGHT WITH A LT BLD CIGED. ORH COMPLETED. RESET AND DUCT OVERTEMP LT RE-ILLUMINATED. L HP WAS OFF AS WELL AS TEMP SELECT IN AUTO POSITION. AIR RETURN TO DTW. MAINTENANCE REPLACED TEMP SENSOR.

Part: SWITCH — DEFECTIVE (BLEED AIR)

DURING FLIGHT 2919 LEFT LP BLEED VALVE WOULD NOT STAY OPEN MORE THAN 2 MINUTES IN EITHER MANUAL OR AIR TURNBACK TO MSP. MAINTENANCE TROUBLESHOT, FOUND RIGHT DUCT OVERTEMP IN AUTO AND DUCT OVERTEMP LIGHT NOT ILLUMINATING. REPLACED DUCT TEMP SWITCHES M2035-501. OVERTEMP AND MCP LIGHT NOT ILLUMINATED.

Part: STRUCTURE — DENTED (MLG DOOR)

FOUND DURING C-CHECK, DENT ON RT NLG DOOR FORWARD CORNED. REFER TO CELSIUS W/O 1007, MESABA 409 CARD NUMBER 059525, TASKCARD 7502, AND SAAB STATEMENT 340SDS000435. MAINTENANCE REMOVED RIVITS AROUND DENENTED AIREA, REMOVED FWD INSIDE COVER PLATE IAW SRM 51-40-23. PERFORMED DOOR A ND PAN TO CONTOUR REF EO340SDS000435. NDT: NO CRACKS NOTED IAW FFV NDT006. REPAI RED ABOVE DISCREPENCY IAW SAAB EO340000435, SEE IPM FORM FOR DETAIL. PERFORMED L ANDING GEAR SWINGS, CHECKS GOOD IAW AMM 32-30-00-5.

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND DURING C-CHECK, SEAT TRACK IN GALLEY AREA ON RT SIDE CORRODED AT THE TROLLEY STORAGE AREA. REFER TO CELSIUS W/O 19007, TASK CARD 1542. MAINTENANCE REMOVED CORROSION AS REQUIRED, SRM 51-70-40. REMAINING MATERIAL WITHIN LIMITS, ALODINED, PRIMED AND PAINTED SEAT TRACK REF SRM51-20-42/43.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND DURING C-CHECK, CORROSION AT STA 294.0 LT OB CORNER AT APPROX STRING LINE 152Z. REFER TO CELSIUS TASK CARD 1533, W/O 19007. MAINTENANCE REMOVED DAMAGED ANGLES, FABRICATED NEW ANGLES PER SAMPLE IAW SRM 51-20-20, 51-20-30 TREATED, PRIMED AND TOPCOATED ANGLES IAW SRM 51-20-42/43. INSTALLED 2 EA ANGLES PER PRINCIPLES OF SRM 51-40-21/23.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND DURING C-CHECK, CORROSION ON CENTER AISLE FLOORBOARD ANGLES FROM STA 294-339. REFER TO CELSIUS TASK CARD 1539, W/O19007. MAINTENANCE REMOVED CORROSION FROM AFFECTED AREA , SRM 51-10-10 FOUND OUT OF LIMITS IAW 51-70-4, FABRICATED 2 EA. ANGLES PER SAMPLE IAW SRM 51-20-20, 51 -20-30. TREATED, PRIMED AND TOPCOATED ANGLE , AND INSTALLED 2 EA. ANGLES PER PRI NCIPLES OF SRM 51-40-21/23.

Part: STRINGER — CORRODED (FUSELAGE)

FOUND DURING C-CHECK, CORROSION ON STRINGER JUST OB OF RBL 18-3. AND AT OB LBL 18-3, STA 288.0 REFER TO CELSIUS W/0 19007, TASK CARD 1532. MAINTENANCE REMOVED CORROSION AS REQUIRED, SRM 51-70-40. REMAINING MATERIALS IS WITHIN LIMITS SRM 51-10-10. ALODINED, AREA IAW SRM 51-20-42, APPLIED PRIMER AND TOPCOAT IAW SRM 51-20-43.

Part: BRACKET — CORRODED (FUSELAGE)

FOUND DURING C-CHECK, FLOORBOARD 122EZ MOUNTING BRACKET HAS CORROSION REFER TO CELSIUS TASK 1535, W/O 19007. MAINTENANCE FABRICATED MOUNTING BRACKET, AS PER SAMPLE IAW SRM 51-20-00. ALODINED, PRIMED AND PAINTED. REFER W/O 19007, ITEM 24 FOR FLOORBOARD REPAIR.

Part: FRAME — CORRODED (FUSELAGE)

FOUND DURING C-CHECK, CORROSION ON FRAME 258.0 REFER TO CELSIUS W/O 19007 TASK CARD 1534. MAINTENANCE REMOVED CORROSION AS REQUIRED IAW SRM 51-70-40. REMAINING MATERIAL IS OUT OF LIMITS SRM 51-10-10.REMOVED DAMAGE ANGLE AND FABRICATED NEW ANGLE PER SAMPLE AND 1 EA. REPAIR DOUBLER. IAW 51-20-20. 51-20-30 LOCATED, DRILLED AND TRIMMED NEW NANGLE DOUBLER IAW SR M 51-40-40. TREATED, AND PRIMED AND TOPCOATED IAW SRM 51-20-42/43. FAY SEALED A ND INSTALLED REF SRM 51-40-21.

Part: FRAME — CORRODED (FUSELAGE)

FOUND DURING C-CHECK, CORROSION ON FRAME RBL 18.3 BETWEEN STRINGERS 272.0 AND 288.0. REFER TO CELSIUS W/O 19007, TASK CARD 1531. MAINTENANCE REMOVED CORROSION AS REQUIRED SRM 51-70-40. REMAINING MATERIAL IS OUT OF LIMIT SRM 51-10-10. REMOVED DAMAGED ANGLE, FABRICATED PER SAMPLE NEWANGLE, IAW SRM 51-20-20, 51-20-30. LOCATED, DRILLED AND TRIMMED NEW ANGLE IAW SRM 51-40-40, TREATED, PRIMED AND TOPCOATED IAW SRM 51-20-42/43, FAY SEALED AND IN STALLED REF SRM 51-40-21.

Part: SHIELD — DENTED (FUSELAGE)

FOUND DURING C-CHECK, SEVERAL DENTS AFT OF LT ICE SHEILD AT FUSELAGE STA 350.0 REFER TO CELSIUS W/O 19007, TASK CARD 2530, AND SAAB STATEMENT 340SDS000435. MAINTENANCE CHECKED LIMIT, FOUND DENTS OUT OF ALLOWABLE LIMIT, DISTANCE BETWEEN DENTS LESS THAN 4XL IAW SAAB SRM 51-10-10. NO CRACKS NOTED IAW FFVNDT006. DENTS ARE ACCEPTED AS IS, NO FURTHER ACTION NECESSARY IAW SAAB STAEMENT 340SDS000435.

Part: WEB — CORRODED (FUSELAGE)

FOUND DURING C-CHECK, WEB AT STA 294 CORRODED. REFER TO CELSIUS TASK CARD 1530, W/0 19007. MAINTENANCE REMOVED DAMAGE WEB AS REQUIRED IAW 51-40-21. NEW WEB DRILLED AND COUNTER SUNK HOLES IAW SRM 51-40-21. NEW WEB INSTALLED IAW SRM 51-40-21/23/50. WEB REINFORCEMENT PN 7253-721-439, NSN.

Part: SHIELD — DENTED (FUSELAGE)

FOUND DURING C-CHECK, SEVERAL DENTS AFT OF RT ICE SHIELD AT FUSELAGE STA 339.0 TO STA 363.0 REFER TO CELSIUS W/O 19007, TASK CARD 2523, AND SAAB STATEMENT 340SDS000435. MAINTENANCE FOUND DENTS OUT OF ALLOWABLE LIMIT DISTANCE BETWEEN DENTS LESS THAN 4X L IAW SAAB SRM 51-10-10. FABRICATED REPAIR DOUBLER/TRIPLER PER PRINCIPLES OF SRM 53-70-10. ALODINED, PRIMED AND TOPCOATED PER SRM 51-20-42/43, INSTALLED DOUBLER AND TRIPLER REF SAAB SRM 53-70-10. REMAINING DENTS ARE ACCEPTED AS IS IAW SAAB STAEMENT 340SDS000435.

Part: SKIN — DENTED (FUSELAGE)

FOUND DURING C-CHECK, DENT AT STA 393.0 ON RT FUSELAGE. REFER TO CELSIUS W/O19007, TASK CARD 2524, AND SAAB STATEMENT 340SDS000435. MAINTENANCE CHECKED LIMIT, FOUND DENT OUT OF ALLOWABLE LIMIT IAW SAAB SRM 51-10-10. DENT TYPE I AREA II, NO CRACKS NOTED IAW FFVNDT006. DENT IS ACCEPTED AS IS NO FURTHER NECESSARY IAW SAAB STATEMENT 340SDS000435.

Part: VIBRATION — DETECTED (AILERON)

VIOLENT SHAKING OF A/C FELT BY ALL CREW MEMBERS AND PASSENGERS. OCCURRED IN TURNS A/S 160KTS ON CLIMBING OUT OF DTW 2ND PT INTO APN CLEAN CONFIG. MX INSPECTED A/C AND OPENED PANELS 152BB, 151DB, 631AT, 531AT, ALL CHECKS GOOD. REMOVED AND REINSTALLED RT AND LT CENTERING SPRING MECHANISM ROD HARDWARE. ALL CHECKS GOOD. TEST FLIGHT IS SATISFACTORY. PERFORMED POST FLIGHT WALK, ALL CHECKS GOOD. PLANE IS SAFE TO RETURN TO SERVICE.

Part: MODULE — FAILED (DEICE CONTROL)

RIGHT INTAKE ANNUNCIATOR ILLUMINATED IN FLIGHT, RESET SWITCH IT REMAINED ILLUMINATED UNTIL CREW RETURNED BACK TO MSP. MAINTENANCE REPLACED DEICE CONTROL MODULE, OPS CHECKS GOOD.

Part: CONTROL LEVER — MALFUNCTIONED (COCKPIT)

FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED ON LIFT OFF. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED CONTROL QUADRANT. ALL CHECKS GOOD.

Part: GPU PLUG — SMOKING (FUSELAGE)

GROUND CREW REPORTED SMOKE FROM GPU PLUG AFTER IT WAS DISCONNECTED, SHUT DOWN AND HAD PLUG LOOKED AT. MAINTENANCE INSPECTED AFT RT ELECTRICAL COMPARTMENT, BATTERY COMPARTMENT, GPU PLUG AREA. STARTED AS AGAIN WITH POWER CART, NO DEFECTS NOTED. STARTED AIRCRAFT AGAIN WITH BATTERY POWER, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: TIRE — FAILED (RT MLG)

BLEW RIGHT OUTBOARD TIRE ON LANDING. MAINTENANCE REPLACED RT OUTBOARD AND INBOARD TIRES AND RT OUTBOARD BRAKE ASSEMBLY. ALL CHECKS GOOD.

Part: PUMP — FAILED (HYD SYSTEM)

ON TAKEOFF OUT OF MSP, HYD PUMP WOULD NOT WORK IN OVERRIDE MODE. AFTER GOING THROUGH QRH IT OPERATED AGAIN. ON LANDING IN MSP, OVERRIDE MODE WOULD NOT WORK UNTIL JUST REACHING THE GATE. MAINTENANCE REPLACED HYD PUMP PER SF340 AMM 29-10-10. PERFORMED FUNCTIONAL CHECKS OF HYD PUMP. OPS AND LEAK CHECKS GOOD. SERVICED HYD.

Part: PUMP — FAILED (HYD SYSTEM)

GEAR DID NOT RETRACT UNTIL HYD PUMP SWITCH WAS SELECTED TO OVERRIDE, PUMP WORKS PROPERLY IN THE OVERRIDE POSITION. MAINTENANCE CONTROL DEFERRED AUTO PUMP CONTROL SYSTEM. MAINTENANCE REPLACED HYD PUMP PER SR340 AMM 29-10-10. OPS AND LEAK CHECKS GOOD.

Part: DE-ICE LIGHT — ILLUMINATED (RT ENGINE)

DURING CLIMB, RIGHT ENGINE INTAKE CAUTION LIGHT ILLUMINATED. COMPLIED WITH QRH AND RETURNED TO MSP. MAINTENANCE TROUBLESHOT SYSTEM IAW SAAB AMM 30-20-00, NO FAULT FOUND.

Part: INLET DUCT — FAILED (LT ENGINE)

DURING CRUISE, THE LEFT ENGINE INTAKE CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED LEFT LOWER INLET DUCT. OPS CHECK GOOD.

Part: SIGN — FAILED (CABIN)

DURING INSPECTION, FOUND EMERGENCY EXIT LIGHT 6D INOP. MAINTENANCE INSTALLED SERVICABLE EXIT SIGN AT ROW 6 DE. ALL CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING INSPECTION, EMERGENCY LIGHT AT MAIN CAIBN DOOR IS INOP. MAINTENANCE REPLACED POWER PACK. ALL CHECKS GOOD. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

DURING INSPECTION, FOUND EMERGENCY LIGHT OUT AT MAIN CABIN DOOR. MAINTENANCE REPLACED POWER SUPPLY. OPS CHECK GOOD. (X)

Part: CHIP LIGHT — ILLUMINATED (LT ENGINE)

FLT 3310 - AFTER TAKEOFF, THE LEFT ENGINE CHIP DETECTOR ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE INSPECTED SCAVENGE SCREENS AND FOUND NO DEBRIS. COMPLETED ALL APPLICABLE STEPS IAW GEMM 72-00-00. ENGINE RUN AND ALL CHECKS GOOD. (M)

Part: O-RING — FAILED (RT GEARBOX)

DTW - FLT 3112 - AFTER DEPARTURE, A STRONG SMELL OF FUEL WAS NOTED, ISOLATED TO THE RIGHT BLEED. AIRCRAFT RETURNED TO DTW WITH NO INCIDENTS. MAINTENANCE REMOVED AND REPLACED RIGHT ACCESSORY GEARBOX O-RINGS. SECURITY AND LEAKS CHECKS GOOD. (X)