N452XJ

Part: SKIN — DELAMINATED (AILERON) · airframe 21,509 hrs · 23,466 cycles

RT WING, RIGHT AILERON P/N 7294576-618 S/N 0266 INBOARD LEADING EDGE DELAMINATED. REPAIRED IAW EO NR S51031. COLD BOND (WET LAYUP) REPAIR IN ACCORDANCE WITH SAAB SRM 51-70-50.

Part: SKIN — DAMAGED (BS 236-251) · airframe 21,509 hrs · 23,466 cycles

ON THE RIGHT FUSELAGE, STA 236.5-251.5 AND EXTENDING 8.3 INCHES FROM SL1636, THERE IS AN EXISTING RT FUSELAGE SKIN DOUBLER REPAIR THAT IS NOT LISTED ON THE MRAL. MAP THIS REPAIR AND SEND IT TO MESABA ENGINEERING. INSPECTED THIS REPAIR AND FOUND IT AS PER EO NR S53574. REPAIR ACCEPTED AS IS, PROVIDED IT COMPLIES WITH SAAB REPAIR STATEMENT 340SDS015017.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,488 hrs · 23,447 cycles

RIGHT FORWARD GALLEY SEAT TRACK CORRODED. REPLACED SEAT TRACK P/N 7253721-459 AND PROFILE P/N 7253721-495 IAW SRM 51-40-21 AND 51-40-22.

Part: SEAT TRACK — CORRODED (BS 284) · airframe 21,488 hrs · 23,447 cycles

LEFT AND RIGHT SEAT TRACK CORRODED AT STA 284 BL0 AND BL18.3. REPAIRED SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 236-258) · airframe 21,488 hrs · 23,447 cycles

RAIL CORRODED AT STA 236 TO STA 258 BL 18.3. REPLACED RAIL P/N 7253710-131 IAW SRM 51-40-27.

Part: DETECTOR — MALFUNCTIONED (LT TAILPIPE) · airframe 20,920 hrs · 22,834 cycles

LT TAILPIPE HOT LIGHT ILLUMINATED DURING TAXI. RETURNED TO GATE. CLEANED AND RESEALED LT TAILPIPE HOT DETECTORS IAW JC 2610-302. OPS CKS GOOD. OK FOR SERVICE.

Part: HEATER — SPARKS (LT INTAKE) · airframe 20,546 hrs · 22,399 cycles

LEFT INTAKE HEAT SPARKING. AIR-TURN-BACK, SLIGHT SMOKE ODOR IN CABIN DUE TO INTAKE SMOKE INGESTION INTO BLEED SYSTEM. REMOVED AND REPLACED LOWER DUCT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,209 hrs · 22,034 cycles

ARMED LIGHT FOR EMERGENCY LIGHTS ON FLIGHT ATTENDANTS PA PANEL IS INOP. REMOVED AND REPLACED SWITCH 5LN EMERGENCY LIGHTS ALL CHECKS GOOD IAW SF340 MM CH 33-50 SEE 409 CARD 291184 AND CONT CARD 020231 FOR DETAILS. MX NOTIFIED 4632.

Part: CONNECTOR — LOOSE (NR 2 ENGINE) · airframe 19,297 hrs · 21,055 cycles

DURING CRUISE FLIGHT, THE FLIGHT CREW EXPERIENCED ILLUMINATION OF AN ENGINE IGNITION LIGHT ALONG WITH ENGINE POWER ROLL-BACK (TORQUE). IGNITION LIGHT ON NR 2 ENGINE ILLUMINATED TWICE AT 11000 FT (NO ICING CONDITION AT ALL) TORQUE AT ONE POINT WENT TO 10 PERCENT + IGNITION LIGHT EXTINGUISHED. THIS OCCURRED ONCE OR TWICE MORE DURING DESCENT. THE FLIGHT RETURNED TO DEW AND LANDED. DURING RADIO COMMUNICATION WITH PILOT, NOTED NO CHANGE IN FLIGHT CHARACTERISTICS OR CHANGE IN SOUND OF ENGINE DURING SAID EVENTS. PERFORMED PRE CHECK RUN OF ENG NO DISCREPANCY NOTED. PERFORMED PRE CHECK RUN OF ENGINE NO DISCREPANCY NOTED. PERFORMED CONTINUITY CIRCUIT CHECK OF ECU IAW GE MM 72-00-00 ENGINE TESTING NO DISCREPANCY NO

Part: ALTIMETER — STUCK (COCKPIT) · airframe 18,585 hrs · 20,224 cycles

CAPTAINS ALTIMETER SHOWING A RED FLAG AND IS STUCK IN POSITION DURING CLIMB-OUT. REMOVED AND REPLACED PILOTS ALTIMETER REF AMM 34. OPS CHECK GOOD REF AMM 34-12-05 PN OFF 622-3975-001 SN OFF 7644 SN ON 7817.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 18,028 hrs · 19,680 cycles

FAILED CAP CHECK. REPLACED BATTERY PACK.

Part: ELEVATOR — DAMAGED (RIGHT) · airframe 17,935 hrs · 19,595 cycles

THE RIGHT ELEVATOR, P/N 7255201-654, S/N 2060, HAD COMPOSITE DAMAGE. REPAIRED IAW MESABA EO S51031. REF: EAMS WORK ORDER 214335 TASK 3506.

Part: ELEVATOR — DAMAGED (LEFT) · airframe 17,935 hrs · 19,595 cycles

THE LEFT ELEVATOR, P/N 7255201-655, S/N 2051, HAD COMPOSITE DAMAGE. REPAIRED IAW MESABA EO S51031. REF: EAMS WORK ORDER 214335 TASK 3505.

Part: SKIN — GOUGED (LT ELEVATOR) · airframe 17,935 hrs · 19,595 cycles

REPAIRED LT ELEVATOR TRAILING EDGE GOUGE FROM TRIM TAB OB HINGE IAW EO NR S51031 WO 214335/3505.

Part: SEAT TRACK — CORRODED (BS 294-300) · airframe 17,937 hrs · 19,596 cycles

DURING 2 YEAR CHECK IN BNA, FOUND SEAT TRACK AT LBL 18.3, BETWEEN FS 294 AND 300 IS CORRODED OUT OF LIMITS. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO NR S53342. REF: EAMS WORK ORDER 214335 TASK 1508.

Part: WEB — CORRODED (BS 288-294) · airframe 17,937 hrs · 19,596 cycles

DURING 2 YEAR CHECK IN BNA, FOUND FLOOR REINFORCEMENT WEB, BETWEEN FS 288 AND 294 IS CORRODED OUT OF LIMITS IN TWO AREAS. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO NR S53362. REF: EAMS WORK ORDER 214335 TASK 1505.

Part: SEAT TRACK — CORRODED (BS 294-300) · airframe 17,937 hrs · 19,596 cycles

DURING 2 YEAR CHECK IN BNA, FOUND SEAT TRACK AT BLO BETWEEN FS 294 AND 300 IS CORRODED OUT OF LIMITS. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO NR S53342. REF: EAMS WORK ORDER 214335 TASK 1507.

Part: CONTROLLER — MALFUNCTIONED (RT DUCT) · airframe 17,719 hrs · 19,389 cycles

THE CREW EXPERIENCED ILLUMINATION OF THE RT DUCT OVER TEMPERATURE WARNING LIGHT ON TAKEOFF. THE FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED CONTROLLER.

Part: CONTROL VALVE — MALFUNCTIONED (MLG) · airframe 15,642 hrs · 17,098 cycles

LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN INBOUND TO MCW, AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL VALVE PN HP848430-721 SN/ON 0011 SN/OFF 2054 IAW SF340 AMM 32-31-15, OPS CHECK GOOD. CYCLED GEAR 15 TIMES IN HANGER LEAK CHECK GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 15,640 hrs · 17,097 cycles

DURING 4K CHECK IN BNA, FOUND EMERGENCY POWER SUPPLY 21LN FAILED CAUSING RT AND LT HORIZONTAL SIDEWALL LIGHTS AND THE VERY FIRST FLOOR PROXIMITY ESCAPE PATH LIGHT 41LN NOT TO ILLUMINATE. REF: EAMS WO NR 212638 TASK 1508.

Part: FRAME — DENTED (FUSELAGE) · airframe 15,640 hrs · 17,097 cycles

DURING 4K CHECK IN BNA, FOUND LOWER FUSELAGE AND FRAME AT FS 686.888 JUST TO THE LEFT OF BL 0 IS DENTED, DAMAGE IS ACCEPTABLE IAW MESABA EO S53307. REF: EAMS WORK ORDER 212637 TASK 1546.

Part: STRUCTURE — CHAFED (RT NACELLE) · airframe 15,639 hrs · 17,097 cycles

RT NACELLE ATNS 197 OB SIDE IS CHAFED AND HAS BEEN REPAIRED IAWS MESABA EO 54124 REF EAMS WORK ORDER 212637 TASK 4508.

Part: ACCESS PANEL — CHAFED (RT TE FLAP) · airframe 15,639 hrs · 17,097 cycles

RT FLAP IB END ACCESS PANEL S41AT IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO 57098 REF EAMS WORK ORDER 212638 TASK 6502.

Part: STRUCTURE — CHAFED (RT NACELLE) · airframe 15,639 hrs · 17,097 cycles

RT LOWER NACELLE DESK IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO 54095. REF EAMS WORK ORDER 212637 TASK 4507.

Part: ACCESS PANEL — CHAFED (LT TE FLAP) · airframe 15,639 hrs · 17,097 cycles

LT FLAP IB END ACCESS PANEL S41AT IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EO 57098 REF EAMS WORK ORDER 212638 TASK 5504.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,639 hrs · 17,097 cycles

SEAT TRACK AT LBL18.3 FROM FS 294 TO FS 310 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-60 REF: EAMS WORK ORDER 21-26-37 TASK 1510.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,639 hrs · 17,097 cycles

SEAT TRACK AT BL 0 FROM FS 294 TO FS 310 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-70-60. REF EAMS WORK ORDER 212637 TASK 1509.

Part: SEAT TRACK — CORRODED · airframe 15,639 hrs · 17,097 cycles

DURING 4K INSPECTION IN BNA, SEAT TRACK AT BLO FROM FS 294-FS 310 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EO NR 53309. REF: EAMS WORK ORDER #212637 TASK 1509.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,639 hrs · 17,097 cycles

DURING 4K INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 FROM FS 294-FS 310 IS CORRODED AND HAS BEEN REPAIRED IAW MESABA EO NR 212637 TASK 110.

Part: FIRE LOOP — FAULTY (RT ENGINE) · airframe 15,153 hrs · 16,575 cycles

RT ENGINE FIRE INDICATION ILLUMINATED WHEN PULLED IN TO PARK. THE CAPT PULLED THE FIRE HANDLE AND SHUT DOWN THE ENGINE. FIRE INDICATION EXTINGUISHED. THE CREW DIDN'T BLOW THE BOTTLES. REMOVED AND REPLACED RT FIRE LOOP, PN 703045. ALL CHECKS GOOD.

Part: ALTIMETER — MALFUNCTIONED (FIRST OFFICERS) · airframe 13,719 hrs · 14,986 cycles

DURING CLIMBOUT OF MSP, NOTICED THE F/O'S ALTIMETER BEGIN TO LAG ABOUT 500 FEET BEHIND THE CAPTAINS ALTIMETER. WHEN LEVELED OUT AT 7000 FEET THE F/O ALTIMETER READ ABOUT 400 FEET LOWER THAT CAPTAINS AND STANDBY ALTIMETERS. MAINTENANCE REPLACED F/O'S ALTIMETER P/N ON-OFF 64111-900-1, S/N ON 2519, S/N OFF 4069. NR 2 PITOT/STATIC SYSTEM OPS/LEAKS CHECSK GOOD IAW SF340 MM CH 34.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 13,037 hrs · 14,238 cycles

EMERGENCY POWER SUPPLY PN 3301-51 SN/1331 REPORTEDLY DO NOT HOLD CHARGE. REPLACED BATTERY ASSEMBLY 3301-31 AND UNIT PASSED CMM CHECKS ON 5/6/04. REFER TO IN HOUSE WO NR 367478 FOR ADDITIONAL DETAIL.

Part: BLADE — DAMAGED (PROPELLER) · airframe 12,799 hrs · 13,961 cycles

NR 4 LEFT PROP BLADE DAMAGED. MAINTENANCE INSPECTED AND STATED IT APPEARED THE BLADE STRUCK SOMETHING DURING THE TAXI IN FROM NR 3321. MX REPLACED LEFT PROP, LEFT PROP ASSY IAW MAL TC NR 6110-303, P/N OFF&ON R390/4-123-F/27, S/N OFF DAP1403, S/N ON DAP0099, OPS CHECK GOOD AT THIS TIME.

Part: DEICE SYSTEM — INOPERATIVE (LT INTAKE)

DURING FLIGHT, THE LT INTAKE HEAT LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO MSP. MAINTENANCE PERFORMED OHMS CHECKS OF LT INTAKE HEAT ONLY FAULT HAS HIGH READINGS ON TEST BOX PINS G TO E AND E TO M FOUND PROBLEM TO BE DEICE MODULE REMOVED AND REPLACED DEICE MODULE PN 44730-501 SN OFF A00632 SN ON A00301 IAW ATC MM 30-21-03 OPS CHECKS GOOD.

Part: CONTROL VALVE — FAULTY (A/C SYSTEM)

DURING FLIGHT 3245, RT TEMP UNCONTROLLABLE IN AUTO AND MANUAL. DUCT OVERTEMP IN BOTH MODES. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED DUAL TEMP CONTROL VALVE P/N 78260-2, SN/ON 9807169.

Part: WIRE — DISCONNECTED (DC GENERATOR)

DURING FLIGHT 2919, LT DC GEN LIGHT ILLUMINATED IN FLT. AIR RETURN TO MSP. MAINTENANCE RESECURED WIRE AT DC GEN TERMINAL. DC GEN OPS CHECK GOOD. IAW AMM 24-30-00.

Part: ALTIMETER

DURING FLIGHT #3073, CAPT'S ALTIMETER WENT TO 7000' AND NOT BEYOND. ALTIMETER RED FLAGGED SO A/C WAS TURNED BACK TO MSP. AIR RETURN TO MSP. MAINTENANCE REPLACED #1 ALTIMETER PN 622-3975-001, SN/OFF 7937, SN/ON 7662. #1 ALTIMETER OPS CHECK GOOD IAW SF340 AMM CHAP 34.

Part: FRAME — CORRODED (FUSELAGE) · airframe 9,407 hrs · 10,374 cycles

DURING 4K INSPECTION IN CWA, FRAME AND ANGLE AT STA 258 HAS CORROSION. MAINTENANCE REMOVED CORROSION ON FRAME IAW SRM 51-70-40. REMOVED AND REPLACED ANGLE IAW SRM CHAP 51.

Part: BEAM — CORRODED (FUSELAGE) · airframe 9,407 hrs · 10,374 cycles

DURING 4K INSPECTION IN CWA, LT GALLEY BEAM STA 258 LBL 15 HAS CORROSION. MAINTENANCE REMOVED CORROSION ON GALLEY BEAM STA 258 IAW SRM 51-70-40. FOUND ATTACHING ANGLE TO BE CORRODED. REMOVED AND REPLACED ANGLE.

Part: PLATE — CORRODED · airframe 9,407 hrs · 10,374 cycles

DURING 4K INSPECTION IN CWA, PLATE FOR PANEL 122DZ TO 121EZ AND 122EZ TO 121FZ ARE CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH PLATES. REF TO 409 #138121 FOR DETAIL. A/C RELEASE DATE 8/20/02

Part: BEAM — CORRODED (FUSELAGE) · airframe 9,407 hrs · 10,374 cycles

DURING 4K INSPECTION IN CWA, RT BEAM AND ANGLE BETWEEN STA 272 AND 288 HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED ANGLE, REMOVED CORROSION AND REPAIRED BEAM IAW SRM 51-70-40.

Part: RIVET — CORRODED (FUSELAGE) · airframe 9,407 hrs · 10,374 cycles

DURING 4K INSPECTION IN CWA, WEB AT STA 294 HAS CORRODED FASTENERS. MAINTENANCE REMOVED AND REPLACED RIVETS.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 9,407 hrs · 10,374 cycles

DURING 4K INSPECTION IN CWA, LT AND RT CENTER AISLE SEAT TRACK CLIPS ARE CORRODED. MAINTENANCE REMOVED AND REPLACED CORROSION IAW SRM 51-70-40.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 9,407 hrs · 10,374 cycles

DURING 4K INSPECTION IN CWA, RT GALLEY I/B SEAT TRACK PROFILE HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-20-91.

Part: SEAT TRACK — CORRODED · airframe 9,407 hrs · 10,374 cycles

DURING 4K INSPECTION IN CWA, RH CENTER AISLE SEAT TRACK HAS LIGHT CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. REF 409 #138103 FOR DETAIL. A/C RELEASE DATE: 8/20/02.

Part: BEAM — CORRODED (FUSELAGE) · airframe 9,407 hrs · 10,374 cycles

DURING 4K INSPECTION IN CWA, LT ANGLE BEAM BETWEEN FRAMES 258 AND 236.5 (LBL 10) HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW 51-20-41.

Part: CHANNEL — CORRODED (AIRSTAIRS) · airframe 9,407 hrs · 10,374 cycles

DURING 4K INSPECTION IN CWA, AIRSTAIR SLIDE CHANNEL HAS CORROSION. MAINTENANCE REPAIRED CORROSION IAW SRM CHAP 51.

Part: CONTROL UNIT — FAILED (COCKPIT)

DURING FLIGHT 3395, LT PROP RPM INDICATION WENT TO ZERO. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED DECU, ALSO REPLACED YELLOW HARNESS. ALL CHECKS GOOD AT THIS TIME.

Part: SKIN — DENTED (FUSELAGE)

DENT IN FUSELAGE AFT OF ICE SHIELD ABOVE STRINGER SL1622 RH SIDE.REPAIRED IAW EO S53126.

Part: GENERATOR — FAILED (LT ENGINE)

DURING FLIGHT 2978 IN MSP. LEFT AC GEN FAILED DURING CLIMB. AIR TURNBACK TO MSP. MAINTENANCE REMOVED AND REPLACED LT AC GEN P/N 31342-003, S/N ON 98029, S/N OFF 286.

Part: COMPUTER — MALFUNCTIONED (COCKPIT)

DURING FLIGHT 3399, YELLOW HEADING ON EHSI COMING ON INTERMITTENTLY DURING FLIGHT. ATTEMPTED TO SAVE SEVERAL TIMES DURING STRAIGHT AND LEVEL, NO CORRECTIONS NOTICED. MAINTENANCE REINITIALIZED BOTH AHRS SYSTEMS. ALL CHECKS GOOD IAW SF-340 MM CHAP 34.

Part: INDICATOR — ERRATIC (COCKPIT)

DURING FLIGHT 2933, LT PROP RPM INDICATION ERRATIC. INDICATION VARIES FROM ACTUAL RPM AND ZERO INTERMITTENTLY. AIR TURNBACK TO MSP. MAINTENANCE REMOVED AND REPLACED LT PROP INDICATOR P/N 522742, S/N ON 0387128, S/N OFF 9802872 IAW AMM 61-40-05-2. OPS CHECK GOOD.

Part: CHIP DETECTOR — CONTAMINATED (RT ENGINE)

RIGHT ENGINE CHIP DETECTOR LIGHT ILLUMINATED ON INITIAL CLIMBOUT. RAN QRH, ENGINE PARAMETERS WERE NORMAL. AIR RETURN TO OMA. MAINTENANCE REMOVED RIGHT ENGINE CHIP DETECTOR, INSPECTED FOUND TWO SMALL SLIVERS, PRESERVED FOR INSPECTION. REINSTALLED CHIP DETECTOR. LEAK CHECKED GOOD. AC TO BE FERRIED FROM OMA TO MSP FOR COMPLETION OF MAINTENANCE PROCEDURES. MAINTENANCE COMPLIED WITH MAINTENANCE PROCEDURES OUTLINED IN GE MM SEI 576 72-00-00. FAULT ISOLATION TABLE 104 TROUBLE 10. MATERIAL IS DETERMINED TO BE ALLOWABLE PER TABLE 104, FIG 1 & 2. OPS AND LEAK CHECK GOOD.

Part: THERMISTER — OUT OF POSITION (ANTI-ICE SYS)

FLIGHT 2800, RT INTAKE HEAT CYCLED ON DEPARTURE. FLIGHT RETURNED TO DTW. MAINTENANCE SWAPPED THERMISTORS 1 & 3, TO 4 & 5 POSITIONS. RAN AIRCRAFT ALL CHECK GOOD.

Part: WIRE — CHAFED (EXHAUST NOZZLE)

FLIGHT 2907 RT INTAKE HEAT INTERMITTANT. WORKED WELL ON THE GROUND, CAME ON ABOUT 10 MINUTES INTO THE FLIGHT. AIR RETURN TO DTW. MAINTENANCE TROUBLESHOT FOUND CHAFED WIRE ON EXHAUST NOZZLE, REPAIRED WIRE, REPLACED DEICE CONTROL MODULE AS A PRECAUTIONARY MEASURE. P/N 44730-501, S/N OFF L248371, S/N ON A00021, RAN AIRCRAFT 1 HOUR. NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (CABIN)

FOUND DURING C-CHECK, CORROSION ON BL 0 SEAT TRACK STA 294 - 370. REFER TO CELSIUS TASK CARD 1540, W/O19161, AND SAAB STATEMENT 340SDS000642. MAINTENANCE REMOVED CORROSION FROM BL 0 SEAT TRACK STA 360 - 294 AS MARKED IAW SRM 51-10-30. REMAINING MATERIAL IS OUT OF LIMITS REF: SRM 51-10-10. CLEANED, PRIMER AND PAINTED CENTER FLANGES IAW SRM 51-20-43. DAMAGE IS ACCEPTED AS IS REF SAAB EO340SDS000642. COMPLIED WITH STEP 1.3 THRU 1.32 REF SAAB EO340SDS000642.

Part: SEAT TRACK — CORRODED (CABIN)

FOUND DURING C-CHECK, CORROSION ON SEAT TRACK LBL, STA 294 - 370. REFER TO CELSIUS W/O 19161, TASK CARD 1539 AND SAAB STATEMENT 340 SDS000642. MAINTENANCE REMOVED CORROSION FROM SEAT TRACK 18.3 LBL STA 370 - 294 AS MARKED, IAW SRM 51-10-30. REMAINING MATERIAL IS OUT OF LIMITS REF SRM 51-10-10. DAMAGE IS ACCEPTED AS IS REF. SAAB EO340SDS000642, COMPLIED WITH STEP 1.3 THRU 1.32 REF SAAB E0SDS000642, CLEANED, PRIMERED AND PAINTED CENTER FLANGES IAW SRM 51-20-43.

Part: FLOOR SUPPORT — CORRODED (CABIN)

FOUND DURING C-CHECK, CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN FRAMES AT STA 258 - 272. REFER TO CELSIUS W/0 19161, TASK CARD 1541. MAINTENANCE BLENDED OUT CORROSION ON CHANNEL, AREA SMOOTHED IAW SRM 51-10-30. CHANNEL ALODINED IAW SRM 51-20-42. NEGLIGABLE MATERIAL REMOVED WITHIN LIMITS REF: SRM 51-10-10, TOPCOATED TO BLENDED AREA, APPLIED TO CHANNEL IAW SRM 51-20-43.

Part: NOZZLE — FAILED (EXHAUST)

ENROUTE FROM ABR TO ATY LT INTAKE HEAT INOPERATIVE. DIVERTED TO MSP DUE TO WEATHER CONDITIONS. MAINTENANCE REPLACED LEFT EXHAUST NOZZLE PN NF24668-057. OPS CHECK GOOD. REFER 409 CARD 034278 FOR DETAILS. INSTALLED LT NACELLE OBFWD KIDNEY PANEL (DISC 2).

Part: GENERATOR — INOPERATIVE (DC SYSTEM)

DC GENERATOR (LT) INOP. MAINTENANCE REPLACED PDU, RAN A/C OPS CHECK GOOD.

Part: RELAY — MALFUNCTIONED (EFIS TUBE)

AFTER TAKEOFF, THE LEFT SIDE EFIS TUBES WENT BLANK WHEN THE GEAR WAS COMING UP AND THE HYDRAULIC PUMP WAS OPERATING. EFIS TUBES COME BACK ON AFTER HYDRAULIC PUMP SHUT OFF. MAINTENANCE REPLACED LEFT BARR RELAY 73 PC.

Part: GENERATOR — FAILED (LEFT)

LEFT AC GEN CAUTION LIGHT ON, PERFORMED QRH PROCEDURES. AC GEN REMAINED INOP. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED LT AC GEN. RAN AIRCRAFT OPS CHECK GOOD IAW SAAB MM 24-00-00.

Part: CONNECTOR — LOOSE (CARGO SMOKE DET)

CARGO SMOKE LIGHT ILLUMINATED ON THE GROUND, NO INDICATION OF SMOKE, DUST ETC IN CARGO HOLD. MAINTENANCE CLEANED AND RESECURED FORWARD SMOKE DETECTOR CANNON PLUG, OPS CHECK GOOD.