N139DL

Part: SUPPORT — DAMAGED (RT WING TE FLAP) · airframe 72,644 hrs · 29,279 cycles

RIGHT WING OTBD T/E FLAP, THREE HOLES ON NR 7 SUPPORT 1-2-3 BEAM FASTNER HOLES HAS TOOLING DAMAGE. REPAIRED IAW ERA 539808-14.

Part: ANGLE — CRACKED (BS 1809) · airframe 72,644 hrs · 29,279 cycles

AT C-CHECK, BS 1809, RT OF HORIZONTAL ANGLE WL 257, BL 28, CRACKED AT FASTENER HOLE. ANGLE REPAIRED IAW SRM 53-80-08, REPAIR 10.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,460 hrs · 29,230 cycles

EMERGENCY SEAT MOUNTED LIGHT DAMAGED AT SEAT 12B. REPLACED BUMPER, SHROUD AND REPLACED THE LAMP. SYSTEM OPS NORMAL.

Part: FILTER — NOT REPORTED (ENGINE) · airframe 71,730 hrs · 29,036 cycles

THE CREW SHUTDOWN RT ENGINE IAW QRH DUE TO LOSS OF FUEL FROM RT TANK. CREW ALSO REPORTED A RT HYDRAULIC EICAS MESSAGE. REPLACED RT ENGINE FUEL FILTER. SYSTEM OPERATION IS NORMAL.

Part: SKIN — DENTED (NR 4 SLAT) · airframe 69,122 hrs · 28,291 cycles

DURING WALK AROUND, FOUND A DENT IN NR 4 SLAT ON LT WING. REPLACED THE SLAT.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 64,954 hrs · 27,122 cycles

SEAT EMERGENCY PATH LIGHTS FROM ROW 34-46AB ARE INOPERATIVE. MX RESET PIN 9 ON CONNECTOR D9048. SYS OPS IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,954 hrs · 27,122 cycles

IN SEAT EMERGENCY PATH LIGHTING ROW 34AB-46 ARE INOPERATIVE. MX REPLACED THE POWER SUPPLY. SYS OPS IS NORMAL.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE FROM ROW 34AB. MX FOUND LOOSE CONNECTOR AT SEAT 33AB. SECURED WIRE AND CONNECTOR, SYS OPS IS NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 62,220 hrs · 26,352 cycles

EMERGENCY MOUNTED LIGHTING AT SEAT 37B DAMAGED AND INOPERATIVE. MAINTENANCE SECURED LIGHT MOUNTED. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,895 hrs · 26,260 cycles

DURING INSPECTION, EMERGENCY LIGHTING WAS FOUND INOPERATIVE FROM ROW 34 TO 45 ON THE RIGHT SIDE SEATS. MAINTENANCE REPLACED THE BATTERY PACK AT ROW 45. SYSTEM OPERATION IS NORMAL.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,518 hrs · 26,517 cycles

LT WING O/B FLAP T/E UPPER SURFACE IS DELAMINATED JUST I/B OF NR 2 FLAP TRACK FAIRING AREA AND REPAIRED PER B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG 9.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,518 hrs · 26,157 cycles

RT WING O/B FLAP UPPER SURFACE IS DELAMINATED O/B OF THE NR 7 FLAP TRACK AREA AND REPAIRED PER THE B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG 9.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 61,518 hrs · 26,157 cycles

RT WING I/B MAIN FLAP O/B FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 FIG 5 .

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,518 hrs · 26,157 cycles

RT WING O/B FLAP UPPER SURFACE IS DELAMINATED AT THE NR 7 FLAP TRACK AREA AND REPAIRED PER B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG 9.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,518 hrs · 26,157 cycles

LT WING O/B FLAP UPPER SURFACE IS DELAMINATED JUST O/B OF THE NR 1 FLAP TRACK FAIRING AREA AND REPAIRED PER B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG 9.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,518 hrs · 26,157 cycles

LT WING O/B FLAP UPPER SURFACE IS DELAMINATED APPROX 50" FROM I/B END AND REPAIRED PER B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG 9.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,518 hrs · 26,157 cycles

RT WING O/B FLAP UPPER SURFACE IS DELAMINATED I/B OF THE NR 7 FLAP TRACK AREA AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-06 FIG 9 (NRC 50813).

Part: SKIN — DENTED (TE FLAP) · airframe 61,518 hrs · 26,157 cycles

RT WING O/B FLAP T/E LOWER SURFACE IS DENTED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-06 FIG 9.

Part: FITTING — DEFECTIVE (NR 1 PYLON) · airframe 61,524 hrs · 26,158 cycles

NR 1 PYLON UPPER LINK PITCH LOAD FITTING T-CLIPS 112T7010-13 O/B AND 112T7010-15 I/B HAVE SHORT EDGE MARGIN (NRC 52405).

Part: FITTING — DEFECTIVE (NR 2 PYLON) · airframe 61,524 hrs · 26,158 cycles

NR 2 PYLON UPPER LINK PITCH LOAD FITTING T-CLIPS 112T7010-14 O/B AND 112T7010-16 I/B HAVE SHORT EDGE MARGIN AT FASTENER HOLES (NRC 52406).

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,524 hrs · 26,158 cycles

FS 1197 + 132 LBL 22 FLOORBEAM UPPER CHORD IS CORRODED AND REPLACED PER B767-300 SRM 51-10-02 PG 2 PARA 9 AND DWG 146T1229 SH 1.

Part: SEALANT — ACTIVATED (NR 2 PYLON) · airframe 61,518 hrs · 26,157 cycles

NR 2 PYLON LWR SPAR FITTING AFT BUSHING SEALANT CRACKED AND REPAIRED PER B767-300 SRM 54-51-90 REPAIR 4 FIG 201.

Part: SEALANT — CRACKED (NR 1 PYLON) · airframe 61,518 hrs · 26,157 cycles

NR 1 PYLON UPPER SPAR FITTING AFT BUSHING SEALANT IS CRACKED AND REPAIRED PER B767-300 SRM 54-51-90 REPAIR 2 FIG 201.

Part: BUSHING — MIGRATED (NR 1 PYLON) · airframe 61,518 hrs · 26,157 cycles

NR 1 PYLON LWR AFT FITTING BUSHING MIGRATED AND REPAIRED PER B767-300 SRM 54-51-90 REPAIR 4 FIG 201.

Part: SEALANT — CRACKED (NR 2 PYLON) · airframe 61,518 hrs · 26,157 cycles

NR 2 PYLON UPPER SPAR FITTING AFT BUSHING SEALANT IS CRACKED AND REPAIRED PER B767-300 SRM 54-51-90 REPAIR 2 FIG 201.

Part: FAIRING — CRACKED (RUDDER) · airframe 61,524 hrs · 26,158 cycles

RUDDER L/E FAIRING 324KL FOUND CRACKED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT CRACKED AREA AS PER B767-300 SRM 55-40-01 REPAIR 1 AND B767-300 SRM 51-70-06 FIGURE 9.

Part: PANEL — DAMAGED (HORIZ STAB) · airframe 61,524 hrs · 26,158 cycles

RT HORIZONTIAL STAB L/E PANEL 342DR INNER SURFACE DETACHED. METAL HOT BOND REPAIR PERFORMED ON DETACHED AREA AS PER B767-300 SRM 55-10-01 REPAIR 1 FIGURE 201 AND B767-300 SRM 51-70-10 REPAIR 4 FIGURE 202.

Part: FAIRING — CRACKED (RUDDER) · airframe 61,524 hrs · 26,158 cycles

RUDDER L/E FAIRING 324ML FOUND CRACKED. COMPOSITE PREPREG REPAIR CARRIED OUT AT CRACKED AREA AS PER B767-300 SRM 55-40-01 REPAIR 1 AND B767-300 SRM 51-70-04 FIGURE 9.

Part: FASTENER — MISSING (NR 1 PYLON) · airframe 61,524 hrs · 26,158 cycles

NR 1 PYLON HAS FASTENER MISSING. FASTENER INSTALLED ACCOMPLISHED AS PER VA81913AD REV A.

Part: FASTENER — ACTIVATED (NR 1 PYLON) · airframe 61,524 hrs · 26,158 cycles

NR 1 PYLON MOD ERA 38671-14AD DWG 624T0016 SHEET 1. PRODUCTION FASTENER MISSING; PRI ISSUED NO FINAL REPAIR DATA AT THIS TIME.

Part: FASTENER — MISSING (NR 2 PYLON) · airframe 61,524 hrs · 26,158 cycles

NR 2 PYLON MOD ERA 389672-14AD DWG 624T0016 SHEET 1. PRODUCTION FASTENER MISSING; PRI ISSUED FOR WORK TO CONTINUE NO FURTHER REPAIR DATA AT THIS TIME.

Part: SPAR — MISREPAIRED (NR 1 PYLON) · airframe 61,524 hrs · 26,158 cycles

NR 1 PYLON FWD UPPER SPAR WEB; EXISTING REPAIR FASTENER PATTERN NOT SAME AS INDICATED IN SB767-54-008 REV 2 FIGURE 10. PRI REQUESTED FOR REPAIR. NO REPAIR DATA AT THIS TIME.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 61,524 hrs · 26,158 cycles

RIGHT WING I/B MAIN FLAP LEADING EDGE O/B FAIRING FOUND DELAMINATED.

Part: SPAR — MISREPAIRED (NR 1 NACELLE) · airframe 61,524 hrs · 26,158 cycles

NR 1 PYLON FWD UPPER SPAR WEB MISREPAIRED. REPAIRED PER ERA 499056-14.

Part: BULKHEAD — DAMAGED (NR 1 NACELLE) · airframe 61,524 hrs · 26,158 cycles

NR 1 PYLON MIDSPAR AFT BULKHD AREA FASTENER HOLES LARGER THAN SB 767-54-0081 REV 1 DWG 624T0016 INDICATES. REPAIRED PER ERA 499052-14AD REV ORIG.

Part: BULKHEAD — CRACKED (NR 1 PYLON) · airframe 61,524 hrs · 26,158 cycles

NR 1 PYLON AFT BULKHEAD LT MID SPAR FTG AFT BLKHD WEB NR 2 FASTENER HOLE CRACK APPROX 1/16 INCH.

Part: BULKHEAD WEB — CRACKED (NR 1 NACELLE) · airframe 61,524 hrs · 26,158 cycles

NR 1 PYLON AFT BULKHEAD LEFT MID SPAR FITTING AFT BULKHEAD WEB CRACKED APPROX 1/16". CRACK REPAIRED PER ERA 499059-14AD REV ORIG.

Part: BULKHEAD — DAMAGED (NR 2 NACELLE) · airframe 61,524 hrs · 26,158 cycles

NR 2 PYLON MIDSPAR AFT BULKHEAD AREA FASTENER HOLES LARGER THAN SB 767-54-0081 REV 1 DWG 624T0016 INDICATED. REPAIRED PER ERA 499052-14AD REV ORIG.

Part: BULKHEAD — DAMAGED (NR 1 PYLON) · airframe 61,524 hrs · 26,158 cycles

NUMBER 1 PYLON MID SPAR AFT BULKHEAD AREA EXISTING FASTENER HOLES LARGER THAN SB 767-54-0081 REV 1 DWG 624T0016 ST 1.

Part: FAIRING — CRACKED (TE FLAP) · airframe 61,524 hrs · 26,158 cycles

DURING HMV 3 VISIT FOUND RT WING INBOARD MAIN FLAP OUTBOARD LEADING EGDE FAIRING CRACKED. COMPOSITE REPAIR CARRIED OUT AS PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PAR 5.A(1).

Part: SKIN — BULGED (LE SLAT) · airframe 61,524 hrs · 26,158 cycles

RT WING 11 L/E SLAT WEDGE SKIN FOUND BULGED. HOT METAL BOND REPAIR PERFORMED ON AREA AS PER SRM 57-43-02 REPAIR 1 FIGURE 201 AND SRM 51-70-10 REPAIR 4 FIG 202.

Part: BULKHEAD — DAMAGED (NR 2 PYLON) · airframe 61,524 hrs · 26,158 cycles

NR 2 PYLON MID SPAR AFT BULKHEAD AREA EXISTING FASTENER HOLES LARGER THAN SB 767-54-0081 REV 1 DWG 624T0016 ST 1 INDICATES.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,524 hrs · 26,158 cycles

CORROSION FOUND AFT CARGO INTERIOR SKIN AREA FS STA 1077 FROM STRINGER 39L TO 39R. CP53-151-02I/CP53-152-02I (NRC 51757)

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,524 hrs · 26,158 cycles

CORROSION FOUND AFT CARGO INTERIOR FUSELAGE SKIN AT FS 1077 STRINGER 39L.

Part: FRAME — CRACKED (BS 903) · airframe 61,524 hrs · 26,158 cycles

MAIN DECK BS 903 LBL 89 FRAME CRACKED. REPAIRED PER ERA 499046-14AD REV ORIG.

Part: FRAME — CRACKED (BS 903) · airframe 61,524 hrs · 26,158 cycles

MAIN DECK BS 903 RBL 89 FRAME CRACKED. REPAIRED PER ERA 499047-14AD REV ORIG SECT 1.

Part: FRAME — CRACKED (BS 883) · airframe 61,524 hrs · 26,158 cycles

MAIN DECK BS 883 RBL 89 FRAME CRACKED. REPAIR ACCOMPLISHED PER ERA 499049-14AD REV ORIG SECTION I.

Part: FRAME — CRACKED (BS 883) · airframe 61,524 hrs · 26,158 cycles

MAIN DECK BS 883 LBL 89 FOUND FRAME CRACKED. REPAIRED PER ERA 499048-14AD REV ORIG SECTION 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,524 hrs · 26,158 cycles

M/D L1 DOOR AFT CUTOUT LWR CORNER SKIN CRACKED. THE SKIN REPAIR AS PER B767-300 SRM 53-10-01 REPAIR 1 FIG 201 CAT B REPAIR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,524 hrs · 26,158 cycles

CABIN - BS 325 RBL 26-50 FLOORBEAM UPPER CHORD FOUND CORROSION CRACK. THE FLOORBEAM REPAIR AS PER B767-300 SRM 53-00-51 REPAIR 1 FIG 201 CAT A REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,524 hrs · 26,158 cycles

FUSELAGE LT STAB LWR GATE CUTOUT SKIN FOUND CRACKED. REPAIR THE SKIN AS PER B767-300 SRM 53-80-01 REPAIR 3 FIG 201 CAT A REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,524 hrs · 26,158 cycles

M/D STA 1518 BL R25 FLOORBEAM CORROSION. THE FLOORBEAM REPAIR AS PER B767-300 SRM 53-00-51 REPAIR 1 FIG 201 CAT A REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,524 hrs · 26,158 cycles

M/D STA 1518 LBL 25 FLOORBEAM CORROSION. THE FLOORBEAM REPAIR AS PER B767-300 SRM 53-00-51 REPAIR 1 FIG 201 CAT A REPAIR.

Part: CONNECTOR — LOOSE (CABIN) · airframe 61,387 hrs · 26,121 cycles

EMERGENCY AISLE LIGHT AT 28R ARE INOPERATIVE. MAINTENACE RE-SECURED CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 61,387 hrs · 26,121 cycles

EMERGENCY AISLE LIGHTS AT ROW 33L AND 33R ARE INOPERATIVE. MAINTENANCE FOUND BROKEN WIRES UNDER THE SEATS AND REPAIRED SYSTEM OPERATION IS NORMAL 2011-D1474.

Part: WIRE — BROKEN (CABIN) · airframe 61,387 hrs · 26,121 cycles

EMERGENCY LIGHTS AT ROW 33R ARE INOPERATIVE. MAINTENANCE SPLICED BROKEN WIRE. SYSTEM OPERATION IS NORMAL 2011-D1475.

Part: WIRE — BROKEN (CABIN) · airframe 61,387 hrs · 26,121 cycles

EMERGENCY LIGHTS AT SEAT 37L AND 37R ARE INOPERATIVE. MAINTENANCE SPLICED BROKEN WIRES AT ROW 37L AND 37R. SYSTEM OPERATION IS NORMAL 2011-D1472.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,593 hrs · 25,363 cycles

FUSELAGE SKIN FS 1197+132 TO 1219, S-39L TO S-39R. REPAIRED IAW ERA 491074-14.

Part: STRUCTURE — DAMAGED (AILERON) · airframe 51,989 hrs · 23,509 cycles

RIGHT INBOARD AILERON HOLE REPAIRED IAW SRM 51-70-17 WITH REF SRM 57-60-01. C/W SRM 51-70-17.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 51,867 hrs · 23,457 cycles

FUSELAGE BS 1809.5 BULKHEAD OUTER CHORD REPAIR IAW EO 01-074914-12 ME08 RH. C/W 01-074914-12 ME08 RH.

Part: INDICATOR — HOT (COCKPIT) · airframe 49,637 hrs · 22,721 cycles

EN ROUTE AT FL350 HAD STRONG BURNING SMELL IN COCKPIT. AT ABOUT THAT TIME CAPTS VSI BLANKED. ODOR SUBSIDED AND 5 MINUTES OR SO VSI DISPLAY RETURNED. CONTINUED TO HAVE VERY LIGHT BURNING ODOR. SEEMED TO BE MORE OR SLIGHTLY STRONGER ODOR WHEN ENGINES ACCELERATE. NO C/B`S POPPED. REMOVED CAPTS VSI INDICATOR AND FOUND IT TO BE VERY HOT WITH A BURNING ODOR COMING FROM INDICATOR. REMOVED AND REPLACED SAME.

Part: SLIDE — UNWANTED DEPLOY (RT OVERWING) · airframe 48,684 hrs · 22,338 cycles

RIGHT OVERWING SLIDE DEPLOYMENT, C/W OP 7838 AND REPLACE OFF WING SLIDE AFTER DEPLOYMENT.

Part: FAN — WORN (CABIN) · airframe 48,417 hrs · 22,241 cycles

ELECTRICAL BURNING ODOR IN COCKPIT. ON DESCENT INTO LBB, GOT FWD EQ EXH FAN STATUS MSG. INSPECTED FAN AND E AND E AREA. FOUND NO EVIDENCE OF FUMES OR BURNING SMELL. FWD EQ EXH FAN TO MCO PER MEL 21-58-04B. REPLACED FWD EQUIP SUPPLY FAN 1 PER AMM. OPS NML. NO MSGS. EI OPS NML. FAN REMOVED SMELLED BURNED AND INTERNAL BEARINGS LOOSE/WORN OUT. OK FOR SVC.

Part: LINK — UNKNOWN (TE FLAP) · airframe 48,030 hrs · 22,129 cycles

WING FLAP LINKS REPLACED IAW EA 01-076248-12, ME07, ME08, ME09, ME10, ME11, ME12.

Part: PROJECTOR — ODOR (CABIN) · airframe 45,093 hrs · 21,074 cycles

F/A REPORTED ON OVERHEATING SMELL COMING FROM THE VIDEO ENTERTAINMENT COMPARTMENT. ALL CABIN SEATING, READING LIGHTS REPORTED INOP DUE TO PESS SYSTEM SHUT OFF. CABIN CREW REPORTED SULFER SMELL AROUND NR 4 VIDEO PROJECTOR. INSPECTED VIDEO PROJECTOR AND OVERHEAD CEILING AREA. NO TROUBLE FOUND. OPERATED PES 1 HOUR PLUS WITH NO OVERHEATING OR UNUSUAL SMELLS.

Part: FITTING — UNKNOWN (TE FLAP) · airframe 43,466 hrs · 20,459 cycles

WING TRAILING EDGE I/B FLAP, MAIN FLAP COLLAR FITTING REPLACEMENT IAW EO 01-073591-12 ME12 AND ME13. C/W EO 01-073591-12 ME12 AND ME13.

Part: BOLT — UNKNOWN (VERTICAL STAB) · airframe 43,466 hrs · 20,459 cycles

JOINT BARREL NUT/BOLT ASSEMBLY OF VERTICAL FIN REPLACEMENT IAW EO 01-074297-12 ME05. C/W EO 01-074297-12 ME05.

Part: DOOR — MISSING (NR 2 NACELLE) · airframe 40,191 hrs · 19,076 cycles

ON ARRIVAL FOUND MISSING BLOW OUT PANEL ON NR 2 ENGINE INBOARD PYLON. PANEL SIZE APPROX 9 INCHS DIAMETER. INSTALLED NEW ACCESS DOOR NR 2 PYLON INBOARD.

Part: WIRE — TORN (EMERGENCY LIGHT) · airframe 34,952 hrs · 16,500 cycles

A 2R LAV EMERGENCY EXIT RED LIGHT WIRING TORN FROM WALL BY PAX. REPAIRED WIRING AND INSTALLED NEW EMERGENCY EXIT RED LIGHT.

Part: LIGHT — INOPERATIVE (RT FUSELAGE) · airframe 34,469 hrs · 16,263 cycles

EMERGENCY LIGHT INOPERATIVE ON RT SIDE AFT OF FLAPS. REPLACED SOCKET OPS CK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,961 hrs · 16,031 cycles

R1 EMERGANCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY. AND POWER SUPPLY.

Part: DUCT — WORN (#2 ENGINE) · airframe 33,524 hrs · 15,810 cycles

AIR TURN BACK RT ENG OVERHEAT MSG AFTER TAKEOFF. FOUND 8TH STAGE DUCT SEPERATED ON NO.2 ENG. REPLCD DUCT BETWEEN CK VLV AND PRECOOLER.

Part: BOLT — LOOSE (FUEL PUMP) · airframe 32,621 hrs · 15,363 cycles

PILOT REPORT, SUSPECTED FUEL LEAK RIGHT ENGINE FUEL FLOW NORMAL IN FLIGHT -5700PPH, NO VISUAL LEAKAGE NOTED REQ'D REBALANCING 3 TIME IN FLIGHT. FOUND BOLTS LOOSE ON FUEL PUMP TO MEC TUBE AT MEC. REPLACED GASKETS AND RETORQUED BOLTS (P/N 731203193) GASKET TUBE (P/N 9378M10G07).

Part: SENSOR — FAILED (NLG) · airframe 28,660 hrs · 13,458 cycles

REPEAT WRITE UP - AFTER TAKEOFF CONFIG FLAPS MSG WITH ASSOCIATED NOSE AIR/GRD DISAGREE. PSEU FAULTED TARGET 266. CLEANED SENSOR/TARGET, PERFORMED BIT ON PSEU, OPS CHECK WAS NORMAL PER FIM BOTH TARGETS CHECKED NORMAL 244 AND 266. ALSO SLUGGED THE TARGET TO SIMULATE NOSE GEAR EXTENSION. ALSO CHECKED NORMAL. FOUND NOSE GEAR SENSOR S266 DAMAGED. REPLACED S266 PER M/M.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 27,292 hrs · 12,804 cycles

ON LAYOVER, FOUND EXIT IDENTIFIER ABOVE L-1 DOOR INOP. REPLACED POWER SUPPY DUE TO PIN 9 ON CONNECTOR BENT BACK.

Part: ACM — MALFUNCTIONED (RIGHT) · airframe 26,675 hrs · 12,518 cycles

WITH LT PACK INOPERATIVE ON MCO - RT PACK WILL NOT COOL AIRCRAFT IN FLIGHT RETURNED TO MCO - REPLACED ACM, OPS CHECK GOOD

Part: LIGHT — SHORTED (1R DOOR)

INBOARD WRITE UP / ALL SLIDE LIGHTS INOP AFTER PUSHBACK. FOUND POPPED C/B. FOUND 1R DOOR CAUSING C/B T-35 (DOOR ARM WARNING) TO POP. RESET C/B, SMELLED HEAVY ELECTICAL SMELL. MTC STILL IN WORK, FOUND LIGHT ASSY SHORTED AT 1R AND PSEU CARD NR 6 FAULTY. REPLACED LIGHT ASSY AND CARD, OPS CHECK NORMAL.

Part: AIR DISTRIBUTION — ODOR (CABIN)

FUMES FILLED CABIN DURING T/O ROLL, SMELLED LIKE O/HEATED OVEN OR BURNING PAPER DID NOT SMELL LIKE ELECT. SMOKE ALARMS IN AFT LAVS WENT ON. SMELL DISAPATED TEMPORARILY RTND ON LDG. RAN ENGS AT T/O PWR W/ACFT PACKS ON; NO SMOKE OR ODOR NOTICED IN CABIN. REPLACED RECIRC FILTERS, CHKD ALL LAV TRASH CONTAINERS AND FIRE EXTINGUISHER CKD, ALL COFFEEMAKERS AND OVENS. NO PROBLEMS NOTED, ACFT OK FOR SERVICE.

Part: SKIN — DENTED (BS 1368)

THE RT SIDE FUSELAGE SKIN WAS FOUND WITH A DEEP DENT AT FS 1368 AT THE HORIZONTAL INTERCOSTAL MIDWAY BETWEEN STRINGERS 30R AND 31R. THE DAMAGE REQUIRES REMOVAL, REQUIRING A CUTOUT SIZED APPROX 3.5 FWD/AFT BY 2.50 UP/DOWN. THE INTERNAL INTERCOSTAL IS NOT REPORTED DAMAGED. THE DAMGE WILL BE REPAIRED PER ER/A 361326-14 REVISION 'B'.

Part: SKIN — DENTED (BS 544)

THE RT SIDE FUSELAGE SKIN WAS FOUND WITH A DEEP DENT JUST FORWARD OF FS 544 BETWEEN STRINGERS 36R AND 37R BELOW THE SKIN LAP JOINT. THE DAMAGE REQUIRES REMOVAL, REQUIRING A CUTOUT SIZED APPROX 3.0 FWD/AFT BY 4.0 UP/DOWN. IN ADDITION, TWO SMALL EDGE SECTIONS SIZED 0.50 BY 0.50 OF THE FS 544 FRAME INTERNAL TEAR STRAP REQUIRED CUTOUT AT THE UPPER AND LOWER AFT CORNERS OF THE SKIN CUTOUT. THE DAMAGE WILL BE REPAIRED PER ER/A 361325-14 'A'.

Part: COFFEE MAKER — FAILED (MID GALLEY)

TEN MINUTES AFTER FLIGHT ATTENDANT REPORTED ELECTRICAL SMOKE SMELL IN RIGHT GALLEY, BOTH MID AND AFT CABIN LAV SMOKE DETECTORS ACTIVATED IN FLT. NO DETECTABLE SMOKE OR FIRE, TURNED UTILITY BUSES OFF FOR REMAINDER OF FLT. REPLACED INBD COFFEE MAKER MID GALLEY DUE TO BURNT ELECTRICAL ODOR FROM COFFEE MAKER. IN ADDITION, INSPECTED A/C CEILING AREA RAN REC FANS, CHECKED ALL VCR'S, OPENED AND INSPECTED ALL MID GALLEY ELECT PANELS AND ALL OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

A SECTION OF EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING TEST. REPLACED POWER SUPPLY M738, OPS CHECK GOOD.

Part: PITOT PROBE — CLOGGED (FWD FUSELAGE)

AT V1 PLUS 3 KNOTS, LOST CAPTS A/S, ALTITUDE, AND HAD L AND REEC WARNING. RETURNED TO ATL. FOUND CAPTAIN'S PITOT PROBE PARTIALLY PLUGGED, REPLACED PROBE, OPERATION NORMAL.