N437XJ

Part: SMOKE DETECTOR — FALSE ACTIVATION (E/E BAY) · airframe 25,150 hrs · 27,845 cycles

DURING FLIGHT, AVIONICS SMOKE LIGHT CAME BUT NO SMOKE IN CABIN. AIRTURN BACK, INSPECTED AND CLEANED SMOKE DETECTOR.

Part: SKIN — DENTED (BS 363-389) · airframe 25,020 hrs · 27,700 cycles

DENT NOTED ON LT FUSELAGE BETWEEN FRAME 363 AND FRAME 389, BETWEEN STRINGER 1516 AND 1517. REPAIRED IAW S53035.

Part: SKIN — DENTED (BS 320-374) · airframe 25,020 hrs · 27,700 cycles

47 DENTS WERE FOUND IN LT FUSELAGE STA 320-374 AND 5 DENTS WERE FOUND ON RT FUSELAGE STA 365-373. REPAIRED IAW S53676.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 25,020 hrs · 27,700 cycles

NOTED DOUBLER REPAIR ABOVE PAX DOOR TO HAVE UNDERSIZED RIVETS AROUND PERIMETER OF DOUBLER. REPAIRED IAW S53679.

Part: SPAR — DENTED (VERTICAL STAB) · airframe 25,020 hrs · 27,700 cycles

DENT NOTED ON LT VERTICAL STAB AT STA 781.35 11 INCH FWD OF VERTICAL REAR SPAR. REPAIRED IAW S55017.

Part: STRUCTURE — CORRODED (BS 294) · airframe 25,020 hrs · 27,700 cycles

PREVIOUS REPAIR ON LT AISLE, JUST AFT OF WRAP-AROUND AT STA294, HAS CORROSION ON AND BELOW REPAIR. REPAIRED IAW S53342.

Part: SKIN — DENTED (RT AILERON) · airframe 25,020 hrs · 27,700 cycles

DENTS NOTED ON RT AILERON OUTBOARD LEADING EDGE, 10 AND 32.5 FROM INBD EDGE ON TOP SKIN. REPAIRED IAW S51031.

Part: SEAT TRACK — CORRODED (BS 297-303) · airframe 25,020 hrs · 27,700 cycles

CORROSION NOTED ON SEAT TRACK RAILS, LT AT STA 297- STA 303.5 BL18, WL71 AND RT AT STA 297-STA 303, BL 0, WL71. REPAIRED IAW S53342.

Part: FRAME — CHAFED (BS 363) · airframe 25,020 hrs · 27,700 cycles

CHAFE NOTED ON LT CABIN FRAME STA363 INNER FLANGE REINFORCEMENT ANGLE AT SL 1505. REPAIRED IAW S53675.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,020 hrs · 27,700 cycles

DENT NOTED IN CENTER BELLY PANEL 13 FWD OF BEACON. REPAIRED IAW S51031.

Part: STRUCTURE — CORRODED (BS 294) · airframe 25,020 hrs · 27,700 cycles

PREVIOUS REPAIR ON RT AISLE, JUST AFT OF FWD WRAP-AROUND AT STA 294, HAS CORROSION. REPAIRED IAW S53342.

Part: SMOKE DETECTOR — MALFUNCTIONED (E/E BAY) · airframe 22,072 hrs · 24,410 cycles

AVIONICS SMOKE LIGHT ILLUMINATED IN FLIGHT AND CAPTAIN DIVERTED TO MTC. SMOKE DETECTOR WAS SUBSEQUENTLY DEFERRED, MORE INFORMATION WILL BE ADDED TO THIS REPORT UPON COMPLETION OF MX.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 21,420 hrs · 23,659 cycles

AIRCRAFT HAD ARRIVED TO MSP AFTER LANDING FLIGHT 2788 WITH PASSENGERS ON BOARD. AIRCRAFT TAXIED TO GATE AREA AND WAS WAITING AT CIRCLE 95. AIRCRAFT 8896 WAS PUSHED BACK AND LEAVING FROM B14 WHEN JET BLAST FROM THE CRJ PUSHED BAG CARTS FROM THE GOPHER AREA. ONE CART MADE CONTACT WITH THE RT SIDE OF N437XJ BELOW FO'S SIDE WINDOW. ENGINE WAS SHUTDOWN BY CREW TO AVOID A POSSIBLE PROP STRIKE WITH BAG CART. INSTALLED FLUSH REPAIR TO DAMAGE ON RT SIDE OF A/C JUST BELOW AND A FEW FEET BEHIND FO'S WINDOW IAW EO NR S53044.

Part: SEAT TRACK — CORRODED (BS 294-300) · airframe 21,019 hrs · 23,190 cycles

SEAT TRACK AT LBL 18.3, IS CORRODED OUT OF LIMITS, ON A PREVIOUS REPAIR, BETWEEN FS 294 AND 300. REMOVED AND REPLACED THE REPAIR IAW MESABA EO#S53342. REF: EAMS WORK ORDER 216320 TASK 1518.

Part: SEAT TRACK — CORRODED (BS 294-300) · airframe 21,019 hrs · 23,190 cycles

SEAT TRACK AT BL0, IS CORRODED OUT OF LIMITS, ON THE CENTER AISLE FLOORBOARD SUPPORT FLANGE, BETWEEN FS 294 AND 300. THE DAMAGED AREA HAS BEEN REPAIRED IAW MESABA EO NR S53342 REF: EAMS WORK ORDER 216320 TASK 1519.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 20,675 hrs · 22,797 cycles

FOUND EMERGENCY FLOOR TRACK LIGHTING DISCOVERED INSECURE AT THE 1A/2A AREA. UPON INSPECTION, FOUND CONNECTORS BROKEN. REPLACED EMERGENCY FLOOR TRACK LIGHTING STRIP AT ROW 2A-3A WITH SERVICEABLE UNIT, P/N 6636-2 IAW SF340MM 33-50-20.

Part: WIRE HARNESS — UNKNOWN (MLG) · airframe 20,548 hrs · 22,634 cycles

UPON GEAR EXTENSION IN EAU, LT MAIN GEAR DOWNLOCK INDICATOR DID NOT SHOW GREEN, INTRANSIT LIGHT EXTINGUISHED NORMALLY, 20 SECONDS LATER, LEFT GEAR GREEN LIGHT ILLUMINATED BY ITSELF. INSPECTED MAIN GEAR ACTUATOR AND DOWNLOCK, FOUND OK. PINNED GEAR TO INSURE DOWN AND LOCKED. REMOVED GEAR PINS. INSP A/C FOUND TO BE SAFE FOR ONE-TIME FERRY FLIGHT FROM EAU TO MSP WITH GEAR DOWN, NOT PINNED. MAX SPEED 200 KNOTS, AND FLOWN NO ICE CONDITION. REMOVED AND REPLACED LT MLG PER 32-61-05-02. GEAR SWING CHECKS GOOD.

Part: PHOTO CELL — DIRTY (SMOKE DETECTIONS) · airframe 20,105 hrs · 22,125 cycles

AVIONICS SMOKE LIGHT ILLUMINATED, DEFERRED. CLEANED THE PHOTO CELL AND THE CONNECTOR.

Part: CONNECTOR — DAMAGED (OIL TRANSDUCER) · airframe 19,955 hrs · 21,976 cycles

ENROUTE, THE CREW EXPERIENCED FLUCTUATION OF THE ENGINE OIL PRESSURE. THE CREW DIVERTED FOR MAINTENANCE ACTION WITHOUT FURTHER INCIDENT. CORRECTLY INDEXED BACKSHELL AND TIGHTENED PGB OIL TRANSDUCER CONNECTOR 3 TURNS. PERFORMED OPS RUN CHECK. GOOD. NO FLUX NOTED.

Part: FAIRING — DAMAGED (FUSELAGE) · airframe 19,625 hrs · 21,616 cycles

LT FAIRING PANEL 197BL SUSTAINED DEER STRIKE AND REQUIRES REPAIR. REPAIRED IAW EOS51031. THIS IS A MAJOR REPAIR.

Part: PANEL — ANIMAL STRIKE (FUSELAGE) · airframe 19,625 hrs · 21,616 cycles

PANEL 151CB HAS COMPOSITE DAMAGE FROM DEER STIKE. REPAIRED IAW EOS51031, THIS IS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,386 hrs · 21,343 cycles

DURING 4K CHECK, FOUND SEAT TRACK AT LBL 18.3, IS CORRODED OUT OF LIMITS, BETWEEN FS320 AND 321. THE DAMAGED AREA HAS BEEN REPAIRED IAW MESABA EO NR S53342. REF: EAMS WORK ORDER 214182 TASK 1519.

Part: STRUCTURE — CHAFED (RT NACELLE) · airframe 19,386 hrs · 21,343 cycles

DURING 4K CHECK IN BNA FOUND RT NACELLE LOWER DECK IS CHAFFED OUT OF LIMITS. INSTALLED DOUBLER OVER DAMAGED AREA IAW EO NR S54095. REF: EAMS WORK ORDER 214182-4511

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,386 hrs · 21,343 cycles

DURING 4K CHECK IN BNA FOUND SEAT TRACK AT LBL 18.3 IS CORRODED OUT OF LIMITS AT FS299. THE DAMAGE HAS BEEN REPAIRED IAW EO NR S53342. REF: EAMS WORK ORDER 214182 TASK 1518.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,386 hrs · 21,343 cycles

DURING 4K CHECK IN BNA FOUND SEAT TRACK AT BLO IS CORRODED OUT OF LIMITS, BETWEEN FS320 AND 321. THE DAMAGED AREA HAS BEEN REPAIRED IAW EO NR S53342. REF: EAMS WORK ORDER 214182 TASK 1519.

Part: SKIN — DENTED (HORIZ STAB) · airframe 19,386 hrs · 21,343 cycles

DURING 4K CHECK IN BNA FOUND RT HORIZONTAL STABILIZER HAS 2 DENTS LOCATED AT HS103.72 AND 102.50. THE DENTS ARE OUT OF LIMITS. INSTALLED BONDED DOUBLER OVER BOTH DAMAGED AREAS IAW EO NR S55017. REF: EAMS WORK ORDER 214182-3510.

Part: STRUCTURE — DAMAGED (LT NACELLE) · airframe 19,386 hrs · 21,343 cycles

DURING 4K CHECK IN BNA FOUND LT NACELLE LOWER DECK IS CHAFFED OUT OF LIMITS. INSTALLED DOUBLER OVER DAMAGED AREA IAW EO NR S54095. REF: EAMS WORK ORDER 214182-4516

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 19,386 hrs · 21,343 cycles

DURING 4K CHECK IN BNA, FOUND RT ELEVATOR P/N 7255201-654, SN 2046 IS DAMAGED ON THE LOWER SURFACE, 6" FORWARD OF THE TRAILING EDGE. THE ORIGINAL DAMAGE HAD BEEN TEMPORARILY REPAIRED IAW MESABA EO NR S55071. THE TEMPORARY REPAIR HAS BEEN REMOVED AND A PERMANENT REPAIR INSTALLED IAW MESABA EO NR S51031. REF: EAMS WORK ORDER 214183 TASK 3501.

Part: MOTOR — MALFUNCTIONED (A/C SYSTEM) · airframe 19,165 hrs · 21,026 cycles

WHILE AT THE GATE AND WHILE PASSENGERS WERE BOARDING, GROUND PERSONNEL ADVISED THAT THE CARGO BIN APPEARED TO BE FILLING WITH SMOKE. CREW STARTED TO SMELL BURNING SMELL IN CABIN AT THAT TIME. DEPLANED THE AIRCRAFT AND TURNED OFF ALL ELECTRICAL POWER. THE AFT SUPP AIR COND UNIT WAS RUNNING AT THE TIME OF THE SMOKE. REPLACED NR 2 A/C MOTOR PN 1134104-1, SN ON 1404, SN OFF 2103

Part: ACCESS PANEL — CHAFED (RT TE FLAP) · airframe 17,297 hrs · 19,097 cycles

DURING 4Y/2Y CHECK FOUND RT FLAP ACCESS PANEL 641AT IS CHAFED OUT OF LIMITS ON THE INBOARD END AND HAS BEEN REPAIRED IAW MESABA EO#S57094 REF: EAMS WORK ORDER 612613 TASK 6507

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,297 hrs · 19,097 cycles

DURING 4Y/2Y CHECK IN BNA FOUND SEAT TRACK AT LBL18.3 IS CORRODED FROM FS297 TO FS319 AND HAS BEEN REPAIRED IAW MESABA EO#S53066. REF: EAMS WORKORDER 212613 TASK 2514

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,297 hrs · 19,097 cycles

DURING 4Y/2Y CHECK IN BNA FOUND SEAT TRACK AT BL 0 IS CORRODED FROM FS 297 TO FS 319 AND HAS BEEN REPAIRED IAW MESABA EO S53060. REF: EAMS WORK ORDER 212613 TASK 2513

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 17,297 hrs · 19,097 cycles

DURING 4Y/2Y CHECK IN BNA FOUND FLOOR FLANGE AT FS272 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EO#S53102. REF: EAMS WORK ORDER 212613 TASK 2517

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,297 hrs · 19,097 cycles

DURING 4Y/2Y CHECK IN BNA FOUND LAV SEAT TRACK PN 7253721-459 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-27. REF: EAMS WORK ORDER 212613 TASK 2515

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,297 hrs · 19,097 cycles

DURING 4Y/2Y CHECK IN BNA FOUND LAV SEAT TRACK PROFILE PN 7253721-495 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21. REF: EAMS WORK ORDER 212613 TASK 2526.

Part: SOCKET — INOPERATIVE (CHIP DETECTOR) · airframe 15,629 hrs · 17,280 cycles

DURING DEPARTURE WHILE LEVEL A 4000 FEET THE R-CHIP DETECT ANNUNCIATOR ILLUMINATED NUMEROUS TIMES. QRH CONSULTED ENGINE PARAMETERS NORMAL. CALLED MXCTRL, ADVISED TO RETURN. MAINTENANCE, UPON INSPECTION NOTED RT CHIP DETECTOR CONNECTOR PLUG SOCKET LOOSE. REMOVED AND REPLACED CHIP DETECTOR IAW GE 72-00-00. NO DEBEIS NOTED ON OLD CHIP DETECTOR. CLEANED AREA, RAN ENGINE AT VARIOUS POWER SETTINGS FOR 30 MINUTES NO FAULTS NOTED. S/N ON TED19434 S/N OFF TED13652.

Part: INVERTER — INOPERATIVE (NR 1) · airframe 15,118 hrs · 16,708 cycles

AFTER DEPARTURE FROM MQT INTO IMC, THE EADI'S BEGAN TO DRIFT TO THE LEFT TO APPROX 20 DEGREES OFF RUNWAY HEADING. DURING TURNOUT THE HDG FLAGGED ON BOTH EADI'S. AFTER LEVELING OFF CONFIRMED THE EADI'S WERE OFF COMPASS HEADING BY 50 DEGREES. RECEIVED RMI FLAGS ON BOTH RMI'S. TRIED THE NR 1 INVERTER, NO CHANGE. A/C DIVERTED TO ESC. MAINTENANCE REPLACED NR 1 INVERTER P/N PC251-123C, S/N OFF 9123, S/N ON 8198. NR 1 INVERTER CHECKS GOOD IAW SF340 MM CH 24. RESET NR 1 AND NR 2 AHRS COMPUTERS. NR 1 AND NR 2 AHRS CHECK GOOD IAW SF340 MM CH 34.

Part: CRADLE — DAMAGED (HANDSET) · airframe 14,263 hrs · 15,793 cycles

FLIGHT ATTENDANT OVERHEAD PA, CALL AND EMERGENCY STATUS LIGHTS INOP. REPLACED FLIGHT ATTENDANT HANDSET CRADLE IAW SF340 AMM CHAPTER 23/30/05/4. ALL CHECKS GOOD. P/N ON&OFF 5483-1-5, S/N OFF 1050, S/N ON 648.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 14,258 hrs · 15,790 cycles

FS 294 LT SEAT TRACK HAS CORROSION. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW EO NR S53060. A/C RELEASE DATE 2/26/04. REFER TO LOG PAGE NR 1264969 FOR ADDITIONAL INFORMATION.

Part: FRAME — GOUGED (FUSELAGE) · airframe 14,258 hrs · 15,790 cycles

FS 583.0 FRAME BETWEEN STR SL1501 AND 1601 GOUGED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED A DOUBLER REPAIR IAW EO NR S53152. A/C RELEASE DATE 2/26/04. REFER LOG PAGE NR 1264969 FOR ADDITIONAL INFORMATION.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 14,258 hrs · 15,790 cycles

FS 339 LEFT HD 11 INCHES BELOW STR SL1632 DENT FOUND TO BE OUT OF LIMITS. MX CUT OUT DAMAGED AREA FABRICATED AND INSTALLED A DOUBLER REPAIR IAW MESABA EO S53035. A/C RELEASE DATE 2/26/04.

Part: SKIN — DENTED (FUSELAGE) · airframe 14,258 hrs · 15,790 cycles

FS 317 LT FUSELAGE 6 INCHES BELOW STR SL1632 DENT OUT OF LIMITS. CUT OUT DAMAGED AREA FABRICATED AND INSTALLED A DOUBLER REPAIR IAW EO NR S53005. A/C RELEASE DATE 2/26/04. REFER TO LOG PAGE NR 1264969 FOR ADDITIONAL INFORMATION.

Part: FRAME — CORRODED (FUSELAGE) · airframe 13,084 hrs · 14,645 cycles

DURING 4K INSPECTION IN CWA, UPPER FLANGE ON BOTTOM FUSELAGE FRAME STA 294 HAS CORROSION RBL 30.5 MAINTENANCE REPAIRED DAMAGE IAW EO NR $53108. REFER TO 409 NR 192516 FOR DETAIL. A/C RELEASE DATE 7/31/03.

Part: INDICATOR — FAILED (LT ENGINE)

DURING FLIGHT 3056, CREW REPORTED LT ITT GAUGE WAS FLUCTUATING. INFLIGHT LEFT ITT GAUGE WENT TO ZERO FOR APPROXIMATELY 2 MINUTES. RETURNED TO NORMAL READING ON ITS OWN. ALL OTHER LEFT ENGINE INDICATIONS WERE NORMAL ENTIRE TIME. AIR RETURN TO MEM. MAINTENANCE PERFORMED FUNCTIONAL CHECK OF LT ITT INDICATING SYSTEM AS PER SAAB AMM 77-20-00-5. NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY AT THIS TIME.

Part: POWER SUPPLY — DEFECTIVE

During test of Emergency lighting System JC #335003, Maintenance found several lights Inop under no power conditions. Found Power supply 20LN PN 3301-51 SN/2192 at fault. Removed and replaced Power Supply PN 3301-51, SN ON 1370, SN OFF 2192. .

Part: FRAME — CORRODED (FUSELAGE) · airframe 9,031 hrs · 10,264 cycles

DURING 4K-CHECK IN CWA, FRAME AND ANGLE AT STA 258 HAS HEAVY CORROSION. COMPLETED REPAIR TO FRAME IAW EO S53102.

Part: ANGLE — CORRODED · airframe 9,031 hrs · 10,264 cycles

Found during 4K-check in CWA, Frame and Angle at Sta 258 has heavy corrosion. Maintenance installed new Angle PN 7253722-001 and completed Frame repair IAW SRM 53-70-30-5.

Part: SEAT TRACK · airframe 9,031 hrs · 10,264 cycles

During 4K-check in CWA, LH Center Aisle seat track LBL 18.3 has heavy corrosion at Sta 297. Maintnenance repaired Seat Track IAW SR 53-70-60-2.Completed MAL EO S53060.

Part: CONTROL CABLE — CHAFED (RUDDER) · airframe 9,031 hrs · 10,264 cycles

DURING 4K-CHECK IN CWA, RT O/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MAINTENANCE INSTALLED RT O/B RUDDER CABLE P/N 7227105-562, IAW SF3 AMM 27-21-25.

Part: CONTROL CABLE — CHAFED (RUDDER) · airframe 9,031 hrs · 10,264 cycles

FOUND DURING 4K-CHECK IN CWA, LT O/B RUDDER CABLE OF DUAL CIRCUIT I IS CHAFED. MAINTENANCE REPLACED LT O/B RUDDER CABLE IN DUAL CIRCUIT I IAW SAAB AMM 27-21-25-4 P/N 7227105-562.

Part: ANGLE — CORRODED · airframe 9,031 hrs · 10,264 cycles

During 4K-check in CWA, Angle on Frame 272 is corroded between RH Galley Seat Track and RH Fwd Emergency Exit. Maintenance replaced Angle PN 7253721-471 on Frame 272 RH Galley Seat Track and RH Fwd Emergency Exit IAW Saab SRM 51.

Part: BEAM — CORRODED · airframe 9,031 hrs · 10,264 cycles

During 4K-check in CWA, LH Beam between Frame Sta 272 and 288 has heavy corrosion. Maintenance replaced LH Beam PN 7253720-325 between Frame Sta 272 and 288 IAW Saab SRM 51.

Part: CONTROL CABLE — CHAFED (RUDDER) · airframe 9,031 hrs · 10,264 cycles

DURING 4K-CHECK IN CWA, RT RUDDER AFT SINGLE CABLE OF CIRCUIT I IS CHAFED. MAINTENANCE REPLACED RT RUDDER AFT SINGLE CABLE P/N 7227105-582 OF CIRCUIT I IAW SF340 AMM 27-21-25.

Part: CONTROL CABLE — CHAFED (AILERON) · airframe 9,031 hrs · 10,264 cycles

DURING 4K-CHECK IN CWA, RT I/B AILERON FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED RT I/B AILERON FWD FUSELAGE CABLE WITH NEW CABLE P/N 7227105-614 IAW SF340 AMM 27-11-25-4.

Part: CONTROL CABLE — CHAFED (ELEVATOR) · airframe 9,031 hrs · 10,264 cycles

DURING 4K-CHECK, FOUND LT ELEVATOR FWD I/B FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED LT I/B FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED LT I/B FWD 7227705-643 P/N 7227705-643 IAW SF340 MM 27-31-15.

Part: CONTROL CABLE — CHAFED (AILERON) · airframe 9,031 hrs · 10,264 cycles

DURING 4K-CHECK, FOUND LT AILERON FWD O/B FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED LT O/B AILERON FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED LT AILERON FWD O/B FUSELAGE CABLE WITH NEW CABLE P/N 7227105-613.

Part: CONTROL CABLE — CHAFED (ELEVATOR) · airframe 9,031 hrs · 10,264 cycles

FOUND DURING 4K-CHECK IN CWA, RT O/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED RT O/B FWD ELEVATOR CABLE P/N 7227105-712 IAW SF340 AMM 27-31-15.

Part: CONTROL CABLE — CHAFED (ELEVATOR) · airframe 9,031 hrs · 10,264 cycles

DURING 4K-CHECK IN CWA, FOUND RT I/B ELEVATOR FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED RT I/B FWD FUSELAGE CABLE P/N 7227705-643, IAW SF340 AMM 27-31-15.

Part: CONTROL CABLE — CHAFED (AILERON) · airframe 9,031 hrs · 10,264 cycles

DURING 4K-CHECK IN CWA, RT O/B AILERON FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED RT O/B FWD FUSELAGE CABLE WITH NEW CABLE P/N 7227105-624 IAW SF 340 AMM 27-11-25-4.

Part: CONTROL CABLE — CHAFED (AILERON) · airframe 9,031 hrs · 10,264 cycles

DURING 4K-CHECK IN CWA, LT I/B AILERON FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED LT I/B AILERON FWD FUSELAGE CABLE P/N 7227105-621/623 IAW SF340 AMM 27-11-25.

Part: CONTROL CABLE — CHAFED (ELEVATOR) · airframe 9,031 hrs · 10,264 cycles

DURING 4K-CHECK IN CWA, LT ELEVATOR FWD O/B FUSELAGE CABLE IS CHAFED. MAINTENANCE REPLACED LT ELEVATOR FWD FUSELAGE CABLE REPLACED IAW SF340 AMM 27-31-15.

Part: SEAT TRACK — CORRODED · airframe 9,031 hrs · 10,264 cycles

During 4K-check in CWA, LH Center Aisle Seat Track LBL18.3 has out of limits of pitting corrosion approximately Sta 649-686.88. Maintenance replaced Seat Track section between Sta 618.88 to 686.88 IAW EO#S53060.

Part: SEAT TRACK — CORRODED · airframe 9,031 hrs · 10,264 cycles

During 4K-check in CWA, LH Center Aisle Seat Track LBL18.3 has corrosion that is out of limits from approximatelyu Sta 680 to 649 IAW Saab SR 53-70-60. Maintenance replaced Seat Track Section in Aft end of Left Center Aisle IAW S53060. Seat Track PN 7253799-459.

Part: MODULE — FAILED (RT ENGINE)

DURING FLIGHT 2934, IN ICING CONDITIONS, RT INTAKE LIGHT ILLUMINATED. QRH PROCEDURE FOLLOWED, BUT NO FIX, UNDER DIRECTION OF MX CONTROL, RT INTAKE CIRCUIT BREAKER CYCLED, BUT NO FIX. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED DE-ICE CONTROL MODULE P/N 44730-501, S/N OFF A00072, S/N ON A000281 IAW ACTMM 30-21-03. OPS CHECK GOOD.

Part: GENERATOR — FAILED (RIGHT)

RIGHT AC GENERATOR CAUTION LIGHT CYCLES ON AND OFF ABOUT EVERY 6 SECONDS WITH ANIT-ICE ON. PROBLEM PERSISTED AFTER ORH RECYCLING. MAINTENANCE REPLACED RIGHT AC GEN P/N 31342-001, S/N ON 755, SN OFF 98046. ALL CHECKS GOOD AT THIS TIME.

Part: VALVE — FAILED (MLG)

CVG - FLT 3345 - ON APPROACH TO CVG, GEAR WAS SELECTED DOWN TRANSIT LIGHT CAME ON AND NEVER WENT OUT. NO WHEEL SHOWED DOWN AND LOCKED, HYDRAULIC PUMP RAN CONTINUOUSLY. RETRACTED GEAR AND IT LOCKED IN UP POSITION, PUMP STOPPED. PUT GEAR HANDLE DOWN SAME RESULT AS BEFORE, ALL HYDRAULIC PRESSURES AND QUANTITIES WERE NORMAL. MX SAID TO PULL AND RESET LANDING CONTROL CB, THIS GAVE NORMAL 3 GREEN INDICATION. MAINTENANCE REPLACED LANDING GEAR CONTROL VALVE. ALL CHECKS GOOD. (M)