N317DL

Part: GASPER FAN — FAILED (CABIN) · airframe 55,395 hrs · 41,133 cycles

GASPER FAN C/B POPPED IN CLIMB WITH A BURNED METAL ODOR. REPLACED FAN.

Part: COFFEEMAKER — BURNED (AFT GALLEY) · airframe 55,086 hrs · 40,891 cycles

BURNING ODOR IN AFT GALLEY, TURNED GALLEY POWER OFF, ODOR WENT AWAY. REPLACED AFT GALLEY NR 2 COFFEE DISPENSER.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,775 hrs · 40,628 cycles

AFTER LANDING FWD EMERGENCY LIGHT COVER FELL ON FLOOR. REINSTALLED COVER AND LIGHT DOES NOT OPS OK. CHANGED EMERGENCY LIGHT BATTERY PACK, NO HELP. CHANGED BATTERY CHARGER, OPS CHECK OK.

Part: FRAME — CUT (FUSELAGE) · airframe 54,639 hrs · 40,518 cycles

FRAME AND REINFORCEMENT ANGLE CUT AT STA 380 TO REPLACE SECTION OF STR 17L. REPAIRED FORMER PER SRM 53-10-4 FIG 9. REPAIRED REINFORCEMENT ANGLE PER SRM 51-40-3, OK PER LIA ENGINEERING.

Part: ACTUATOR — CRACKED (LT WING) · airframe 54,627 hrs · 40,508 cycles

AFTER LANDING ROLL OUT, LOSS OF SYSTEM -A- QUANTITY PRESSURE FOUND NR 1 SPOILER ACTUATOR CRACKED. REPLACED ACTUATOR

Part: WEB — CORRODED (PRESSURE WEB) · airframe 49,676 hrs · 38,325 cycles

CORROSION WAS FOUND ON THE AFT PRESSURE DOME WEB AT BL 0. THE CORROSION WAS CUT OUT AND A REPAIR DOUBLER INSTALLED. THE DAMAGE WAS FOUND AT HMV.

Part: FITTING — CORRODED (HOR. STAB.) · airframe 49,655 hrs · 38,314 cycles

CORROSION WAS FOUND RH AND LH HORIZONTAL STABILIZER ATTACH FITTINGS ON THE FACES AND BORES. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS WERE INSTALLED PER ERA 397745-14. THE DAMAGE WAS FOUND DURING INSPECTION AT HMV.

Part: FITTING — CORRODED (FUSELAGE) · airframe 49,655 hrs · 38,314 cycles

CORROSION WAS FOUND ON THE LUG BORES AND FACES OF THE RH ANDLH HORIZONTAL STABILIZER CLEVIS ATTACH FITTINGS. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS INSTALLED.

Part: SKIN — CRACKED (FS 767) · airframe 49,655 hrs · 38,314 cycles

THE FUSELAGE SKIN SKIN JUST FWD OF FS 767 AT STR 19R UNDER THE WING-TO-BODY FAIRING WAS FOUND CRACKED. THE CRACK WAS LIMITED TO THE SKIN ONLY AND WAS CUT OUT. THE DAMAGE WAS REPAIRED WITH AN EXTERNAL DOUBLER. THE DAMAGE WAS FOUND DURING HMV.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 49,654 hrs · 38,314 cycles

THE FUSELAGE CLEVIS LUGS AND THE VERTICAL FIN ATTACHMENT LUGS WERE FOUND CORRODED IN THE BORES AND THE FACES. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS INSTALLED. THE DAMAGE WAS FOUND DURING HMV.

Part: SPAR CAP — CRACKED (WING) · airframe 49,654 hrs · 38,314 cycles

A CRACK WAS FOUND IN THE REAR SPAR UPPER CAP AT RSS 224.14. A REPAIR WAS INSTALLED PER BOEING REWORK DRAWING 65C30105. THE DAMAGE WAS FOUND DURING AN INSPECTION AT HMV.

Part: SKIN — CRACKED (SKIN) · airframe 49,654 hrs · 38,314 cycles

A CRACK WAS FOUND IN THE FUSELAGE SKIN FORWARD OF THE LOWER AFT CORNER. THE DAMAGE WAS REPAIRED PER BOEING S/B 737-53- 1083. THE DAMAGE WAS FOUND AT HMV.

Part: SKIN — CRACKED (SKIN) · airframe 49,654 hrs · 38,314 cycles

THE FUSELAGE SKIN AT FS 727B AND STR 18L UNDER THE WING-TO- BODY FAIRING WAS FOUND CRACKED. THE DAMAGE WAS CUT OUT AND REPAIRED WITH AN EXTERNAL DOUBLER SIMILIAR TO THAT OF S/B 737-53-1065. THE DAMAGE WAS FOUND AT HMV.

Part: SKIN — DENTED (HORZ STAB) · airframe 49,654 hrs · 38,314 cycles

LEADING EDGE OF LT HORIZONTAL STAB HAD SKIN DENTED OUT OF LIMITS.

Part: FRAME — CRACKED (CABIN) · airframe 49,654 hrs · 38,314 cycles

CRACKS WERE FOUND AT THE BOTTOM TWO FASTENERS ON THE INNER CCHORD OF THE LEFT FS 616 FRAME AT THE OVERWING FRAME TO STUB BEAM JOINT. THE CRACKS ARE TYPICAL OF THAT SHOWN IN S/B 737-53-1182. THE CRACKS WERE CUT OUT AND REPAIRED PER S/B 737-53-1182. THE DAMAGE WAS FOUND AT HMV.

Part: LIGHT — INOP (ROW 10-16)

EMER TRACK LTS INOP SEATS ROW 10-16. REPLACED EMER TRACK LT PACK BATTERY AND CHARGER OPS NML.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING REPETITIVE INSPECTIONS PER SI 3-69482-12, THE STA 178 BULKHEAD WAS FOUND CRACKED AT LBL 5.7, WL 200. A REPAIR HAD PREVIOUSLY BEEN INSTALLED ON THE RIGHT SIDE OF THE PRESSURE BULKHEAD PER B737-200 SRM 53-10-11. UPON REMOVAL OF THIS REPAIR DOUBLER, A NEW CRACK WAS FOUND AT RBL 1, WL 188. REPAIRED PER ERA 330532-14.

Part: FITTING — CRACKED (LT MLG)

THE LEFT WING OUTBOARD AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM WAS FOUND CRACKED. THE CRACKING IS TYPICAL TO THAT DESCRIBED IN S/B 737-57-1216, REV 1. THE CRACK WILL REMAIN IN SERVICE ON A TIME LIMITED BASIS AND WILL BE REPAIRED ACCORDING TO THE S/B.

Part: ANGLE — CORRODED (BS 300)

SUPPORT ANGLE CORRODED LT SIDEWALL CABIN FLOOR SUPPORT ANGLE IS CORRODED FS 300 TO 360. STARTED REMOVAL OF CORR PER SRM 51-10-6, REMOVED SECTION OF ANGLE FOR REPAIR PER M/M 53-21-0 PG 801, DRILLED UP REPLACEMENT ANGLE. FABRICATED SPLICE ANGLE PER M/M 53-21-0PG 801. OK TO INSTALL Z-ANGLE, STARTED INSTALLATION OF NEW ANGLE AND SPLICE DOUBLER PER M/M 53-21-0 PG 801.

Part: ENGINE — TAILPIPE FIRE (NR 1)

DURING NR 1 ENG START HAD POSSIBLE TAIL PIPE FIRE AFTER ABORTED START. FIRED LEFT ENG FIRE BOTTLE. REPLACED LEFT ENG FIRE BOTTLE. PERFORMED VISUAL INSP OF NR 1 ENG, NO DEFECTS FOUND. STARTED NR 1 ENG, OPS CKS GOOD.

Part: FIRE WARNING — MALFUNCTIONED (APU)

APU FIRE WARNING ON SHORT FINAL. BOTTLE DISCHARGED PER POM. EGT INDICATED 600 DEGREES ON SHUT DOWN. INSPECTED APU, NO EVIDENCE OF FIRE. FWD APU TO MCO AND PLACARD PER MEL. NEEDS APU FIRE BOTTLE. PART TOTAL CYCLES, 25,768.

Part: BATTERY — DISCHARGED (CABIN)

AFT CABIN UPPER EMERGENCY FLASHLIGHT INOP. REPLACED BATTERIES, CHECKS NORMAL.