N540DA

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,284 hrs · 43,645 cycles

CENTER AISLE EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT, CHECKS GOOD.

Part: SKIN — CRACKED (PAX DOOR) · airframe 57,858 hrs · 43,339 cycles

THE AFT LOWER CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A 3 INCH CRACK IN THE SKIN AND BEAR STRAP. THE CRACK WAS ROUTED OUT OF THE SKIN AND BEAR STRAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 378019-14, REV A.

Part: FLOW DIVIDER — OVERHEATED (RT PACK BAY) · airframe 57,136 hrs · 42,830 cycles

CREW REPORTS SOMKE IN CABIN. REPLACED FLOW MULTIPIER.

Part: FLOORBEAM — CRACKED (BS 294.5)

THE FS 294.5 FLOORBEAM WEB AT LBL 40 WAS FOUND WITH A 7 INCH LONG CRACK RUNNING FROM A CABLE PASS THROUGH HOLE TO THE LOWER EDGE OF THE WEB AND THROUGH THE LOWER CHORD. THE LOWER CHORD WAS REPLACED. THE DAMAGED SECTION OF WEB WAS REPAIRED WITH AN ALUMINUM DOUBLER PER ER/A 368915-14, REV A.

Part: FRAME — CRACKED (BS 560)

THE FWD JAMB FRAME OF THE C1 DOOR CUTOUT FS 560 WAS FOUND WITH A 1 INCH CRACK IN THE FRAME WEB JUST BELOW THE NR 6 DOOR STOP FITTING. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH A DOUBLER PER ER/A 368895-14AD.

Part: BULKHEAD — CRACKED (BS 1183)

THE WEB OF THE FS 1183 BULKHEAD WAS FOUND WITH A .75 INCH LONG TYPICAL CRACK AT RBL 26 AND WL 169. THE CRACK IS TYPICAL OF BOEING S/B 727-53-0215. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED PER THE S/B AS DOCUMENTED IN ER/A 368897-14.

Part: BRACKET — CRACKED (CARGO DOOR)

C2 DOOR (S/N 634) HAD 2 BRACKETS BROKEN, ROD BENT, WEB DAMAGED AT LIGHTNING HOLE. REPAIRED PER SRM 52-30-20, OPS CHECK GOOD.

Part: SKIN — CRACKED (BS 660-680)

FUSELAGE SKIN FS 660-680, STRG 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 AND 680 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 660 AND 680. THE CRACK WAS CUTOUT OF THE SKIN LAP AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG. 5 AND ER/A 367800-14AD.

Part: WEB — CRACKED (BS 1263)

THE FS 1263 WEB OF THE RT LOWER VENTRAL STAIRWAY TORQUE BOX WAS FOUND WITH A TYPICAL CRACK. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED PER B727 S/B 53-0129 AND ER/A 367330-14AD.

Part: MEGAPHONE — INOPERATIVE (CABIN)

AFT CABIN MEGAPHONE INOP ON PREFLIGHT. REPLACED AFT CABIN MEGAPHONE.

Part: FRAME — CRACKED (L2 DOORWAY)

A .75 INCH VISIBLE CRACK AT L-2 DOOR FWD FRAME AT UPPER LOCK ROLLER. REPAIRED PER M/M 52-12-0.

Part: SKIN — CRACKED (BS 360-481)

LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS ALONG THE PANEL. THE SKIN LAP WAS CUT OUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367111-14AD.

Part: LINE — LOOSE (NR 1 ENGINE)

NR 1 GEN ON MCO. ON T/O FROM FLL LOST NR 2 GEN, WAS ABLE TO GET NR 2 GEN BACK ON LINE BUT LOW PRESS LIGHT WAS FLICKERING AND OIL TEMP WAS HIGH. FOUND OIL LEAK AT COOLER, TIGHTENED LINE.

Part: BATTERY PACK — DISCHARGED (EMER EXIT)

FOUND ON L/O, LT AFT EMERGENCY SLIDE LIGHT INOP. REPLACED BATT PACK, CKS GOOD.

Part: ANGLE — CRACKED (RT WING)

REF TPA LETTER CHECK D-1, SUPPORT ANGLE CRACKED AT LWR FWD SIDE OF NR 8 SPOILER ACTUATOR SUPPORT FITTING. INSTALLED DOUBLER PER M/M 57-20-22.

Part: STRINGER — CRACKED (VERT STAB)

FOUND AT C2 LETTER CHECK, .5 INCH CRACK IN VERT STAB S-7L, INSIDE VERT STAB CRAWLWAY THIRD BULKHEAD ABOVE OPENING. REPAIRED PER M/M 55-30-0 .

Part: STRINGER — CRACKED (VERT STAB)

FOUND AT C2 LETTER CHECK, .75 INCH CRACK IN VERT STAB S-9L, INSIDE VERT STAB CRAWLWAY, FOURTH BULKHEAD ABOVE OPENING. REPAIRED PER M/M 55-30-0.

Part: FRAME — CRACKED (SERVICE DOOR)

FOUND ON MV1 CK, .5 INCH VISABLE CRACK RT FWD SERVICE DOOR FRAME FROM UNDER LOWER AFT DOOR STOP CASTING. ALSO, CASTING IS CRACKED. INSTALLED FRAME SPLICE AND REPLACED CASTING PER M/M 52-12-0 PG 806.

Part: UPLOCK ACTUATOR — MALFUNCTIONED (NLG)

AFTER GEAR EXTENSION, 'A' HYD QTY WENT TO ZERO (NOSE GEAR REQUIRED MANUAL EXTENSION). POM PROCEDURES COMPLIED WITH AND A FLAP 15 LDG ACCOMPLISHED. REPLACED NOSE GEARLOCK ACTUATOR PER M/M. SERVICED HYD FLUID, RETRACTED NOSE GEAR SEVERAL TIMES AND OPS NORMAL. INDICATES NORMAL, NO LEAK FOUND.

Part: TEMP CONTROLLER — SHORTED (LT PACK)

ON TAXI OUT, LEFT MIX VALVE INDICATOR WAS SPORADIC IN AUTO, INOP IN MANUAL. LOUD SPARK AND SMELL FROM AIR CONDITION F/E PANEL. FOUND LT PACK TEMP CONTROLLER AT FAULT. REPLACED CONTROLLER, OP CKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERG TRACK LIGHTING INOP IN AFT CABIN. REPLACED BATT PACK, CK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT SIDE AFT OVERWING EXTERIOR EMERGENCY LIGHT INOP. REPLACED BATT PACK AT M954, LIGHT CKS GOOD.

Part: SKIN — DAMAGED (RT ELEVATOR)

DURING SHOP INSPECTION, RIGHT ELEVATOR WAS REPAIRED FOR SKIN DAMAGE PER SRM 55-20-3, REF DL ERA 303316-14.

Part: ANGLE — CRACKED (NR 5 LE SLAT)

.25 INCH CRACK, NR 5 SLAT, LWR COVE SKIN ATTACH ANGLE BELOW O/B STOP PAD. FOUND AT A-2 LTR, CK. REPAIRED PER MM 57-54-0.

Part: ANGLE — CRACKED (NR 8 LE SLAT)

.25 INCH CRACK, NR 8 SLAT, LWR COVE SKIN ATTACH ANGLE BELOW TAIL DUCT AT PREVIOUS DOUBLER. FOUND AT A-2 LTR CK. REPAIRED PER MM 57-54-0.

Part: BEAM — CRACKED (FS 1263)

THE RIGHT HAND TORQUE BOX FWD TRANSVERSE BEAM AT FS 1263 WAS FOUND CRACKED. THE ER/A WILL REPLACE THE DAMAGED PLACE IN ACCORDANCE WITH S/B 53-0129.

Part: SKIN — CRACKED (NR 1 LE SLAT)

FOUND DURING A-1 LETTER CHECK, .5 INCH CRACK NR 1 L/E SLAT AFT SKIN ATTACH ANGLE AT I/B UPSTOP PAD. REPAIRED PER MM 57-54-0 PAR 5A.

Part: REGULATOR — FAULTY (E/E COMPARTMENT)

DURING CRUISE, WITH NR 2 GENERATOR INOP NR 3 BUS-TIE BREAKER TRIPPED. DIVERTED FLIGTH TO DFW. FOUND NR 3 VOLTAGE REGULATOR FAULTY. REPLACED REGULATOR OPERATION NORMAL.