N137DL

Part: WIRE HARNESS — PINCHED · airframe 69,086 hrs · 28,747 cycles

F/A REPORTED AFTER LANDING "SPARKS" CAME OUT OF FWD BULKHEAD AT SEATS 1E, F AND THEN THE IFES FOR E & F ROWS WENT BLANK. MAINTENACE INSPECTED MONITORS & SEAT BOX AT 1E&F. NO DAMAGE NOTED. NO ODOR OF FIRE AROUND 1E&F. FOUND POWER HARNESS PINCHED UNDER SEAT 1E. SHIELDING AND COPPER WIRE IS EXPOSED. REPLACED SEAT TO SEAT. OPS CHECKED NORMAL.

Part: NUT — LOOSE (SLAT STOP) · airframe 64,553 hrs · 27,434 cycles

FOUND NR 1 SLAT INBD SLAT TRACK DOWN STOP NUT LOOSE. C/W EA 01-469704-03AD OPN 2201, NO DEFECTS NOTED. REPLACED DOWNSTOP ATTACH BOLT NUT IAW B767 AMM 27-81-34-404-014 STEP D (3)(D)1-3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,348 hrs · 26,552 cycles

CABIN: STA 903.5 FRAME INNER CHORD FOUND CRACKED TRANSITION RADIUS AT RBL 90. STA 903.5 FRAME CRACKED INNER CHORD REPAIRED IAW ER/A 490891-14AD REV ORIGINAL.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 61,348 hrs · 26,552 cycles

AFT CARGO: STA 1351 BETWEEN STR 26R AND 27R FRAME WEB FOUND PUNCTURE (DENT 0.7" WITH 0.4" CRACKED ). STA 1351 BETWEEN STR 26R AND 27R FRAME WEB PUNTURED AREA TRIMMED-OUT AND REPAIRED IAW ER/A 490897-14 REV ORIGINAL.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 61,348 hrs · 26,552 cycles

AFT CARGO FLOORBEAM AT STA 1197, INNER CHORD FOUND CORRODED AT LBL 13.0 AND LBL 42.0. AFT CARGO FLOORBEAM AT STA 1197 INNER CHORD TRIMMED BETWEEN BL 0 TO LBL 44 AND REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 4, OTIS.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 61,348 hrs · 26,552 cycles

CABIN AT STA 287, RBL 60.75 FLOORBEAM UPPER HORIZ FLANGE FOUND CORRODED. CORROSION FOUND ON EXISTING REPAIRED TEE :EXISTING REPAIRED TEE WITH CORROSION REMOVED AND NEW TEE FABRICATED AND INSTALLED IAW SRM 53-00-51, FIG 201, REPAIR 1 OTIS. AREA REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201 OTIS.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 61,348 hrs · 26,552 cycles

CABIN : STA 325, RBL 26.0, FLOORBEAM UPPER HORIZ FLANGE FOUND CORRODED. STA 325 FLOORBEAM UPPER HORIZ CORRODED FLANGE TRIMMED BET RBL 12.0 TO RBL 45.5 AND REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201, OTIS.

Part: FAILSAFE — CRACKED (BS 955 BULKHEAD) · airframe 61,348 hrs · 26,552 cycles

DURING ACCOMPLISHMENT INSP IAW DAL OPN 8701AD FOUND BS 955 REAR SPAR BULKHEAD LT SIDE FAIL SAFE STRAP, PN 145T2524-23, FOUND CRACKED. REAR SPAR BULKHEAD LT SIDE CRACKED FAIL SAFE STRAP REPAIRED IAW ER/A490874-14AD, REV ORIGINAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,849 hrs · 26,422 cycles

FOUND AT A CHECK EMERGENCY LIGHTS AFT ARE INOPERATIVE. MX REPLACED THE BATTERY CHARGER. SYS OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 60,168 hrs · 26,230 cycles

EMERGENCY LIGHTS ROWS 34 - 43 INOP. REPLACED BATTERY CHARGER PER AMM 33-50-00. OPS CHECK GOOD. (DL76S103008)

Part: SKIN — DAMAGED (BS 522 S11L) · airframe 57,441 hrs · 25,520 cycles

FUSELAGE STA 522, S-11L, SKIN AND TEAR STRIP DAMAGE REPAIRED IAW ERA 479184-14.

Part: LINE — LEAKING (CREW O2) · airframe 53,582 hrs · 24,299 cycles

CREW OXYGEN PRESSURE DROPPED TO 10 PSI. FOUND BAD O2 LINE BEHIND F/O OXYGEN MASK CONTAINER. REPLACED LINE AND CREW O2 BOTTLE. LEAK CHECK GOOD.

Part: LINK — DAMAGED (T/E FLAP) · airframe 51,819 hrs · 23,680 cycles

T/E FLAP 3-10 LINKS REPAIRED IAW EA 01-076248-12, ME07, ME08, ME09, ME10, ME11, ME12.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 51,391 hrs · 23,511 cycles

EMERGENCY LIGHT INOP AT SEAT 14F AND 10F. REPAIRED WIRES, OPS CK OK.

Part: ENGINE — FAILED (NR 2) · airframe 51,176 hrs · 23,433 cycles

ADVANCED THROTTLES ON T/O AND GOT A LOUD POP FROM RT ENGINE REMOVED AND REPLACED NR 2 ENG IAW TRANS 1T145.

Part: SKIN — GOUGED (FUSELAGE) · airframe 47,608 hrs · 22,209 cycles

FUSELAGE SKIN HAS A DENT AND GOUGE AT S38R AT FS 368. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: BULKHEAD — UNKNOWN (BS 287 LBL25) · airframe 47,476 hrs · 22,158 cycles

FUSELAGE NLG WHEEL WELL AFT BULKHEAD STA 287, LBL 25 CHORD, WL 173. REPAIRED IAW ERA 458240-14AD.

Part: PACKING — LEAKING (NR 2 ENGINE) · airframe 44,920 hrs · 21,199 cycles

RIGHT ENGINE LOST OIL QTY IN FLIGHT. REPLACED STARTER SHAFT PACKING.

Part: WIRE — SHORTED (CABIN) · airframe 40,735 hrs · 19,325 cycles

RED EMERGENCY LIGHTS AT 25AB INOP. FOUND WIRING SHORTED AT PAX SEAT 25AB BETWEEN LWR SIDEWALL PANEL AND SEAT TRACK. REPLACED BLOWN FUSES IN M9009 AND M9010 ESCAPE PATH PWR SUPPLIES. REINSTALLED ALL LWR KICK PNLS. EMERGENCY LIGHTS ESCAPE PATH SYS OP CHECKS GOOD PER AMM. REPAIRED WIRING PER CHAP 20.

Part: CONTROLLER — MALFUNCTIONED (TE FLAPS) · airframe 36,540 hrs · 17,202 cycles

ON APPROACH IN ATL, FLAPS WOULD NOT EXTEND PAST 25 WITH 30 SELECTED. FLAPS WOULD NOT RETRACT ON GO AROUND. LANDED WITH FLAPS AT 20 PER NON-NORMAL PROCEDURE. BITE OF FSEU PER FIM HAD NO FAULTS, RAN AND INSPECTED FLAPS SEVERAL CYCLES WITH NO STATUS MESSAGES OR FAULTS.

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 35,975 hrs · 16,927 cycles

PYLON NR 1 ENGINE FWD UPPER SPAR WEB CRACKED, REPAIRED THE FWD UPPER SPAR WEB. THE CUTOUT SIZE WAS ENLARGER TO REMOVE THE CRACK AND EXISING NUTPLATE LOCATIONS AT THE CUTOUT CORNERS. THE AREA WAS MODIFIED PER THE REQUIREMENTS OF BAC S/B 767-54-0090 AND DOCUMENTED PER ER/A 383905-14.

Part: CABLE — SHORTED (_AFT FUS) · airframe 35,070 hrs · 16,486 cycles

APU GENERATOR FEEDER CABLE SHORTED ABOVE WATER TANK @STA 16 00. ARCHING AND SOME HEAT DAMAGE TO AREA. CA RPLD FEEDER CABLE AND PERFORMED C/W EO 1-74974-3 REV B / FEEDER CABLE MODIFICATION. REPAIRED DAMAGED FEEDER CABLE STANDOFF BRACKET AT STA. 1582 PER SRM 51-70

Part: FLAP — MALFUNCTIONED (WING) · airframe 34,806 hrs · 16,355 cycles

ON APPROACH TRAILING EDGE FLAP DISAGREE EICAS WITH T/E FLAP. SHUT DOWN STATUS MSG LANDED WITH FLAPS AT 23 DEG. T/S PER FIM 27-51-00 FIG 114B. SYS TEST NORMAL. MSG CLEARED, NO FAULTS.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,750 hrs · 15,845 cycles

THE WEB AND LOCAL REINFORCING DOUBLER OF THE LBL 24 LONGITUDINAL FLOORBEAM WAS FOUND CRACKED NEAR AT FS 680. THE CRACKED REINFORCING DOUBLER WAS REMOVED AND WEB CRACK TRIMMED OUT. A NEW REINFORCING DOUBLER WAS INSTALLED AND AN ALUMINUM REPAIR DOUBLER. THE UPPER CAP OF THE FLOORBEAM WAS REINFORCED PER BAC S/B 737-57-1139. THE REPAIR WAS PER ER/A 382279-14AD, REV A.

Part: SOCKET — DEFECTIVE (EXTERIOR) · airframe 33,303 hrs · 15,631 cycles

SLIDE EMERGENCY LIGHT INOP LEFT AFT CABIN DOOR EXTERIOR. REPLACED POWER SUPPLY, NO HELP. REPLACED SOCKET ASSY, OPS CHECKS OK.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY SEAT TRACK LIGHTS INOP MID AFT LEFT AND AFT RIGHT SECTIONS. REPLACED POWER SUPPLY.

Part: LAMP — FAILED (COCKPIT)

LEFT AFT DOOR ARMED LIGHT ON LT FWD ATTND PANEL FAILED TO TEST. RELAMPED, OPS CKS GOOD.

Part: FITTING — LEAKING (NR 1 ENGINE)

AT TOP OF DESCENT, NR 1 ENGINE ROLLED BACK AND OIL PRESSURE STARTED TO DECAY WITH N1 AND N2 STILL INDICATING DOUBLE DIGITS. REPLACED T-BONE FITTING AT 10 O'CLOCK POSITION.

Part: SKIN — GOUGED (BS 1461)

FUSELAGE/SKIN, BULK CARGO DOOR SURROUND FS 146. REPAIR FOR EDGED GOUGES. THE FUSELAGE SKIN AND UNDERLYING BEAR STRAP AT THE FWD EDGE OF THE BULK CARGO DOOR OPENING WAS DAMAGED BY GROUND EQUIP. THE DAMAGED AREAS WERE TRIMMED OUT FROM THE EDGE AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER AND TRIPLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 365124-14, REV C.

Part: SKIN — DELAMINATED (NR 1 LE SLAT)

NR 1 L/E SLAT T/E WEDGE WAS FOUND TO HAVE THE UPPERR SKIN DAMAGED AT A LOCATIONS WHICH IS APPROX 24 INCHES FROM THE OUTBD EDGE AND RUNS APPROX 2 INCHES FWD FROM THE AFT EDGE. REPAIRED PER ERA 364811-14AD.

Part: MOUNT — LOOSE (NR 2 ENGINE)

DURING LETTER CHECK NR 34 WRITTEN, GAP BETWEEN FWD ENG MOUNT AND AND PYLON. REMOVED ENG PER 1T147, INSPECTED ON NR 34 AND NO DAMAGE FOUND TO MOUNTS. REPLACED ALL MOUNT NUTS, REINSTALLED SAME ENG.

Part: AILERON — LIGHTNING STRIKE (LT WING)

DURING LETTER CHECK INSP, FOUND L/WING ODBD AILERON EVIDENCE OF LIGHTNING STRIKE INSTALLED PERMANENT REPAIR AS PER SRM 57-60-02 FIG 201, BALANCE NOT CHANGED REF 51-60-01, PAINTED REPAIR ON LEFT AILERON.

Part: SKIN — LIGHTNING STRIKE (FWD FUS)

FOUND DURING LETTER CHECK INSP, LIGHTNING STRIKE FOREWARD OF RIGHT LOWER PITOT TUBE ON FUSE SKIN BLENDED DAMAGE PER SRM 53-00-01 DYE CHK OK, TREATED AREA AND REPAINTED.

Part: SKIN — LIGHTNING STRIKE (FWD FUS)

DURING LETTER CHECK INSP, FOUND 10 LIGHTNING STRIKES ON A/C BELLY (STARTING JUST AFT OF NOSE GEAR TO SECOND BODY DRAIN AFT OF E AND E COMPT AT 6 O'CLOCK POS) FUSELAGE SKIN BLENDED DAMAGE PER SRM 53-00-01, DYE CHECK OK. TREATED AREAS W/ALODINE.