N262QS

ATA 2530

Part: OVEN — SMOKE (GALLEY) · airframe 11,351 hrs · 7,013 cycles

APPROXIMATELY 40 MINUTES INTO FLIGHT, AFTER FLIGHT ATTENDANT STARTED USING OVEN, A STRONG ACRID ODOR ENTERED COCKPIT, ALSO NOTICED A SMOKEY HAZE IN MICROWAVE COMPARTMENT. OVEN USE WAS DISCONTINUED & ODOR DIMINISHED. R & R OVEN ASSEMBLY WITH A REPAIRED UNIT. VERIFIED OVEN HEATS UP & NO ODOR PRESENT IAW MM 20-43-00.

ATA 2820

Part: DRAIN VALVE — LEAKING (FUEL SYSTEM) · airframe 10,787 hrs · 6,668 cycles

THERE IS A STRONG FUEL ODOR IN THE AFT SERVICE COMPARTMENT. R & R AUTOMATIC DRAIN VALV E70QD. OPS & LEAK CHECKED GOOD. FUEL ODOR NO LONGER PRESENT IN AFT SERVICE COMPARTMENT IAW MM 53-80-09-710-801.

ATA 3242

Part: BRAKE PADS — WORN (MLG) · airframe 8,188 hrs · 5,038 cycles

LOSS OF BRAKE AUTHORITY. ON LANDING, THE BRAKING AUTHORITY DIMINISHED TO THE POINT OF USING FULL BRAKE. INVESTIGATED AND FOUND NR 2 AND 3 BRAKES WERE WORN BEYOND LIMITS. REMOVED NR 2 BRAKE AND INSTALLED O/H BRAKE ASSY. REMOVED NR 3 BRAKE ASSY AND INSTALLED O/H BRAKE ASSY. BLED BRAKE IAW MM 32-419. OK AT THIS TIME. TAXIED ACFT FOR FT OF BRAKES AT THIS TIME THERE ARE NO DEFECTS NOTED IAW MM 32-428, 32-400.

ATA 7261

Part: SHAFT — WORN (SUMP) · airframe 8,158 hrs · 5,021 cycles

CRUISING ALONG AT FL400 THE LT ENGINE FLAMED OUT WITH NO INDICATIONS WHAT SO EVER. HAD AN X ON THE N2 VIBRATION. ELECTED NOT TO RESTART AND DIVERTED. NO CHIP, FILTER DETECTOR MESSAGES. DISASSEMBLED FRONT SUMP & FOUND TOWERSHAFT DISENGAGED FROM BEVEL GEARSHAFT DUE TO EXCESSIVE WEAR AT BEVEL GEARSHAFT TO RETAINING BOOT INTERFACE. COMPLIED WITH SB CFE738-72-8070R1. REASSEMBLED ENGINE. COMPLIED WITH OIL FLUSH PROCEDURE SERVICED WITH OIL. NR 1 ENGINE OPS AND LEAK CHECKED GOOD. INSPECTED CHIP DETECTOR AS SATISFACTORY IAW LMM 72-06-03.

ATA 7930

Part: FCU — MALFUNCTIONED (ZONE 400) · airframe 2,824 hrs · 1,989 cycles

DURING DECENT, ELECTRICAL AND ICE PROTECT LOOK UP LIGHTS COME ON. GEN 1 AND ALT 1 FAIL LIGHTS ON. NOTICED LT OIL PRESSURE FALLING. CHECKED GUAGE, 10 PSI. DIGIT STILL GREEN BUT CHECK LIST CALLS FOR HP COCK TO BE CLOSED IF IT FALLS BELOW 25. RAN SHUTDOWN CHECK LIST. AFTER SHUTDOWN LOW OIL PRESSURE LIGHT CAME ON N1 AND N2 CONTINUED TO INDICATE DURING THE FLIGHT. INTEROGATED DEEC NR 1. FOUND FAULT FOR UNCOMMANDED SHUTDOWN. R & R LT FCU IAW MM 73-20-01 C/W ADJUSTMENT/ TEST PROCEDURES IAW MM 72-00-00. LT ENGINE OPS CHECKS AND LEAK CHECKS GOOD AT THIS TIME. R & R LT ENGINE FUEL FILTER. NO DETECTS NOTED ON FILTER. LEAK CK GOOD IAW MM 73-21-02. SUMPED LT & RT FUEL TANKS WITH NO OBVIOUS DEFECTS NOTED.

ATA 3240

Part: BRAKE SYS — WARNING LIGHT (MLG) · airframe 7,972 hrs · 4,915 cycles

AT FL400 AMBER "BRAKE" ANNUNCIATOR ILLUMINATED, AND RT BRAKE MINELCO.

ATA 3240

Part: CONTROL UNIT — INOPERATIVE (BRAKE SYSTEM) · airframe 7,972 hrs · 4,915 cycles

AT FL400 AMBER "BRAKE" ANNUNCIATOR ILLUMINATED, AND RT BRAKE MINELCO. REMOVED NR 1 BSCU AND INSTALLED AND INSPECTED BSCU IAW MM 32-445 PERFOMRED AN OPS CHECK REF MM 32-446.

ATA 3150

Part: WARNING SYSTEM — MALFUNCTIONED · airframe 7,046 hrs · 4,381 cycles

ON TAKEOFF, RED DOORS MASTER WARNING ILLUMINATED WITH AUDIBLE BELL, EXTINGUISHED IT 3 TIMES AND WOULD ILLUMINATE WITH GONG AGAIN. 4TH TRY IT EXTINGUISHGED AND WE LANDED WITHOUT INCIDENT. SMOOTH LANDING. LANDING WEIGHT 35200 LBS, 700 OVER MAX LANDING WEIGHT. RATE OF DECENT WAS LESS THAN 200 FT PER MINUTE.

ATA 5270

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 6,558 hrs · 4,084 cycles

DURING T/O ROLL, DOOR WARNING LIGHT ILLUMINATED ALONG WITH MASTER WARNING LIGHT. DURING ABORT LIGHT EXTINGUISHED. CHECKED SWTICHED PAX DOOR, ALL WITH IN TOLERANCE. CHECKED SWITCHES AT BAGGAGE DOOR, HAD TO ADJUST THE SWITCHES CALLED LMCC WITH RESULTS WORK PERFORMED IAW MM 52-700 FOR DETAILS REFER TO FAS WO 09-732

ATA 3260

Part: PROXIMITY SENSOR — INOPERATIVE (MLG DOOR) · airframe 5,155 hrs · 3,208 cycles

LANDING GEAR WAS EXTENDED USING ABNORMAL GEAR EXTENSION CHECKLIST BECAUSE, UPON TAKEOFF AT GEAR RETRACTION NEITHER MAIN GEAR CAME UP. REMOVED LT GEAR DOOR PROX SWITCH PN 803682, SN1408 INSTALLED PN 84799031 SN 2047. REMOVED RT GEAR DOOR PROX SWITCH PN 803682 SN 1401 INSTALLED PN - 803682 SN 1131. REMOVED PCB (417JE) PN F422 SN 5303 INSTALLED PN 12-337-39 SN 333. REMOVED RELAY (5OYGM) PN F302-122 NSN INSTALLED PN F302-122 NSN. ALL CHECKS PERFORMED IAW THE MM 32-300 AND 32-002 WITH NO DEFECTS NOTED AT THIS TIME.

ATA 3230

Part: LANDING GEAR — MALFUNCTIONED · airframe 5,152 hrs · 3,205 cycles

LANDING GEAR WOULD NOT EXTEND AFTER SELECTING GEAR HANDLE DOWN. AFTER APPROXIMATELY 2-3 MIN, MAIN GEAR ANNUNCIATOR ILLUMINATED BUT NOSE GEAR DID NOT EXTEND. USED MANUAL GEAR EXTENSION TO EXTEND NOSE GEAR. CHECKED ALL PROX SWITCHES FOR GAP DIMENSIONS. ACCOMPLISHED LANDING GEAR FUNCTIONAL TEST IAW MM 32-300 AND 32-302. TESTED ALL PROX SWITCHES PER MM 32-605. NO FURTHER DEFECTS NOTED AT THIS TIME.