N305FE

Part: CONTROL CABLE — BROKEN (L/E SLAT) · airframe 42,139 hrs · 13,337 cycles

RIGHT WING NR 8 SLAT 2ND SLAT TRACK FROM O/B END CABLE BROKEN. REMOVED AND REPLACED CABLE PER MM 27-89-14-4.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 39,136 hrs · 12,455 cycles

CABIN - CORROSION ON FLOOR PANEL SUPPORT STRUCTURE AT BS 450, BL 0 TO LBL 28. *S/D* BLENDED OUT AS PER SRM 51-21-01 VOL II. REMOVED AND REPLACED PER SRM 51-31-01 VOL II. TOUCH UP PAINT PER SRM 51-21-01 VOL II.

Part: PLATE — CORRODED (CABIN FLOOR) · airframe 39,136 hrs · 12,455 cycles

CABIN - CORROSION ON FLOOR PANEL PLATE AT BS 420, LBL 35 TO 75. *S/D* BLENDED OUT PER SRM 51-21-01 VOL II. REMOVED AND REPLACED PER SRM 51-31-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 39,136 hrs · 12,455 cycles

CABIN - CORROSION ON FLOOR SUPPORT HAT SECTION AT BS 392, RBL 5. *S/D* REMOVED AND REPLACED HAT SECTION PER SRM 51-31-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 39,136 hrs · 12,455 cycles

CABIN - CORROSION ON FLOOR PANEL SUPPORT HAT SECTION AT BS 450 TO 460, LBL 55. *S/D* REMOVED AND REPLACED PER SRM 51-31-01 VOL II.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 39,136 hrs · 12,455 cycles

CABIN - CORROSION ON SEAT TRACK CROWN AT BS 460 TO 468, LBL 28. *S/D* REMOVED AND REPLACED PER MM 53-21-04-2, 53-70-00 FIG 1 SHT 4 VOL I.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 39,136 hrs · 12,455 cycles

CABIN - CORROSION ON FLOOR PANEL SUPPORT HAT SECTION AT BS 425 TO 460, LBL 28. *S/D* REMOVED AND REPLACED PER SRM 51-31-01 VOL II. PAINT TOUCHED UP PER SRM 51-21-02 VOL II.

Part: SKIN — CRACKED (TE FLAP) · airframe 39,136 hrs · 12,455 cycles

LEFT HAND WING - RIVETS LOOSE (APPROX 30 EA) AND SKIN CRACK AT OUTBOARD FLAP UPPER SURFACE INBOARD MIDDLE SEGMENTS AS MARKED. *S/D* REMOVED AND REPLACED PER SRM 51-35-01, 57-10-00 VOL I. PAINT TOUCHED UP PER SRM 51-21-01 VOL II.

Part: DOOR — MISSING (REFUELING)

ON POST FLIGHT FOUND LEFT WING REFUEL DOOR MISSING. REPLACED REFUELING DOOR ASSY.

Part: SENSOR — OUT OF ADJUST (LT MLG DOOR)

98-296 - AFT GEAR RETRACT, LMLG REMAIN ILLUM RED. RECYCLE GEAR 3 TIMES LIGHT REMAIN ON. DID REPOSITION OF STOP SENSOR IN LT MAIN LAND GEAR UP AND DOOR LATCH SENSOR. READJUST CLEARANCE AT TARGET AND PROXIMITY SENSOR AND THEN PERF OPER CK OF L/G SWING AS PER MM 32-34-03-2 AND 7-11-00-2, ALL FUNCTION IS GOOD. A/C OK FOR SVC.

Part: COUPLING — LEAKING (NR 3 ENGINE)

FUEL LEAKING OUT OF AFT PYLON J-BOX. RAN ENG AND INSPECT FUEL SYS AND FUEL NOZZLES, NO LEAKS NOTED. REMOVED PYLON CAPS AND SIDE PANEL TO INSPECT FUEL LINE. CAP LOOSE, NO LEAKS NOTED. FOUND DAMAGED FWD GAMMA COUPLING OF NR 3 ENGINE. REMOVED AND REPLACED BOTH SETS OF FWD ON FWD LINE AT TOP OF PYLON FWD OF PRECOOLER. LEAK AND OPS CKS OK ON ENG RUN CAPS AND PANELS SECURED.

Part: WARNING LIGHT — ILLUMINATED (AIR COND DOORS)

DURING CLIMBOUT, AIR COND DOORS LIGHT ILLUMINATED INTERMITTENTLY. AS AIRSPEED INCREASED TO 300 KTS LIGHT ILLUM, STEADY ON DESCENT, LIGHT EXTINGUISHED BELOW 250 KTS. AIRCRAFT RELEASED FOR SERVICE PER MEL/CDL 52-4 CATEGRORY C EXPIRATION, 17 JULY 96. INSPECTED ALL DOOR LATCHES AND DIMENSIONS FOUND SERVICEABLE. ADJUSTED 2 AND 3 DOOR LIMITS SWITCHES PER MM 52-42-01 PRECAUTIONARY.

Part: REVERSER HALF — MISSING (NR 2 ENGINE)

NR 2 THRUST REVERSER UNLOCK LIGHT ILLUMINATED AFTER LANDING AT ISD. FOUND NR 2 LT TRANSLATING SLEEVE MISSING FROM A/C. TRANSLATING SLEEVE WAS FOUND ON RUNWAY AFTER A/C LANDED. REPLACED NR 2 LT ENGINE THRUST REVERSER ASSY, AS PER WORK CARD NR 78T3101 AND 78T3101. NR 2 THRUST REVERSER OPS CHECK GOOD.

Part: DOOR — CRACKED (CTR MLG)

CENTER LINE GEAR R/DOOR IS CRACKED AT FWD LOWER I/B FRAME. REMOVED AND REPLACED FRAME PER SRM 51-00-00 VOL 1 PAR 2 SEC C.

Part: GEAR DOOR — CRACKED (CTR MLG)

CENTER LINE GEAR L/DOOR IS CRACKED AT FWD LOWER I/B FRAME. REMOVED AND REPLACED ANGLE PER SRM 51-00-00 VOL 1 PAR 2 SEC 3.