N617DL

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 91,610 hrs · 44,270 cycles

ON SERVICE CHECK, FOUND EMERGENCY LIGHTS AT SEAT ROWS 24, 32, 37 INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51. OP CHECKED GOOD. FOUND PUSHED PINS ON SEAT 32 & 37 SECURED PINS. CHECKED GOOD IAW AMM 33-51. OK FOR SERVICE.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 89,832 hrs · 43,480 cycles

DOOR SLIDE DEPLOYED UPON OPENING AT GATE. SLIDE DID NOT INFLATE. REPLACED L1 DOOR SLIDE ASSY REF AMDS T/C. RII OF ABOVE INSTALL C/W.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 89,305 hrs · 43,245 cycles

FOUND EMERGENCY LIGHTS DAMAGED AT SEATS 25D AND 26D. REPLACED BROKEN LENS AND RECEPTACLES, OPS CHECK GOOD. OK FOR SERVICE.

Part: SKIN — CORRODED (BS 1691) · corrosion level 2 · airframe 89,299 hrs · 43,240 cycles

FUSELAGE SKIN AT BS 1691, S28R AFT LAV VENT SURROUND STRUCTURE CORRODED. REPAIRED IAW ER/A 523081-14AD, REV A.

Part: LIGHT — DAMAGED (CABIN) · airframe 88,541 hrs · 42,857 cycles

ROW 27D, AFT EMERGENCY LIGHT ASSY DAMAGED. REPLACED THE LIGHT AT SEAT 27D.

Part: SOCKET — DAMAGED (EMERGENCY LIGHT) · airframe 87,506 hrs · 42,443 cycles

DURING SERVICE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE AT ROW 4RT. REPLACED SEAT 4CD MOUNTED EMERGENCY LIGHT SOCKET, OPS CHECKS GOOD.

Part: CAP — ERODED (HORIZONTAL STAB) · airframe 86,963 hrs · 42,224 cycles

LT HORIZONTAL END CAP L/E HAS ERODED. REPAIRED.

Part: CAP — ERODED (HORIZONTAL STAB) · airframe 86,963 hrs · 42,224 cycles

LEFT HORIZONAL END CAP L/E ERODED. REPAIRED IAW SRM 51-70.

Part: SKIN — DAMAGED (BS 620) · airframe 91,522 hrs · 44,227 cycles

FUSELAGE SKIN DAMAGE AT FS 620, S-16L. DTA TRACKING LOG FOR SKIN REPAIR ACCOMPLISHED IAW ER/A 523526-14, REV B. DTA REQUIRED WITHIN 12 MONTHS OF 14-APR-2014 IAW ER/A 523526-14 REV B. ASSOCIATED ER/A 56-523526, ADDED FOR AC 0617. ER/A 523526-14, REV D IS CURRENT. THE DTA STAGE II INSPECTION THRESHOLD HAS BEEN INCORPORATED AND IS TRACKING VIA LOGPAGE 2155976. THIS LOGPAGE IS TO BE DELETED.

Part: SKIN — DENTED (BS 620) · airframe 86,514 hrs · 42,031 cycles

MAINTENANCE FOUND A DENT ON THE FUSELAGE SKIN AT BS 620, JUST ABOVE STRINGER 16L. REPAIRED IAW ERA 523526-14, REV A SECTION II.

Part: SKIN — DENTED (BS 620) · airframe 86,882 hrs · 42,188 cycles

FOUND A DENT IN THE SKIN AT BS 620 BETWEEN STRINGERS 15 - 16L. DENT IS OUTSIDE OF ALLOWABLE DAMAGE IAW SRM 53-00-01. REPAIRED IAW ERA 523526-14 REV ORIGINAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,413 hrs · 41,989 cycles

DURING WALKAROUND, FOUND AFT LAVATORY SERVICE PANEL HAS CORROSION BETWEEN DOUBLER AND SKIN. PERFORMED REPAIR IAW ERA 523081-14AD, REV ORIGINAL.

Part: SKIN — CORRODED (BS 1701) · corrosion level 2 · airframe 89,299 hrs · 43,240 cycles

CORROSION COMMON TO FUSELAGE SKIN AT BS 1701, S28-29R. REPAIRED IAW ER/A 523081-14AD.

Part: SKIN — CORRODED (BS 1701) · corrosion level 2 · airframe 89,299 hrs · 43,240 cycles

CORROSION COMMON TO FUSELAGE SKIN AT BS 1701, S28-29R. REPAIRD IAW ER/A 523081-14AD.

Part: SKIN — CORRODED (BS 1701) · corrosion level 2 · airframe 89,299 hrs · 43,240 cycles

CORROSION COMMON TO FUSELAGE SKIN AT BS 1701, S28-29R. REPAIRED IAW ER/A 523081-14AD, REV A.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 85,474 hrs · 41,591 cycles

SEAT 29 DEF EMERGENCY PATH LIGHT INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT CONNECTOR IAW CH 20. OPS CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 83,707 hrs · 40,883 cycles

EMERGENCY LIGHT IN SEAT 5C DAMAGED. R & R LIGHT ASSY IAW AMM 33-51.

Part: STRINGER — CORRODED (BS 895 S26R) · airframe 80,775 hrs · 39,616 cycles

DURING AN AIRCRAFT MAINTENANCE VISIT CORROSION WAS DISCOVERED AT SKIN BS 895 AND STR 26R. CORROSION WAS REMOVED AND HFEC PERFORMED. NO CRACKS NOTED. FABRICATED REPAIR AND TREATED.

Part: WIRE — DAMAGED (CABIN) · airframe 80,241 hrs · 39,382 cycles

LINE MAINTENANCE FOUND EMERGENCY EXIT PATH LIGHTS AT ROWS 3, 4, 5, 6 INOPERATIVE. REPAIRED WIRE PER BOEING SPWM CHAPTER 20, OPERATION NORMAL. (2012-D0230)

Part: BATTERY — DISCHARGED (CABIN) · airframe 79,850 hrs · 39,219 cycles

DOOR 2L EXTERIOR EMERGENCY LIGHT INOP. REPLACED BATTERY PER AMM33-51-07. OPS CHECK GOOD. ATL JAN 19 206837.

Part: WIRE — DAMAGED (CABIN) · airframe 78,771 hrs · 38,778 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHT AT SEAT 25D INOPERATIVE. MAINTENANCE REPAIRED THE LIGHT WIRING. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY PACK — LOOSE (EMERGENCY LIGHT) · airframe 76,447 hrs · 37,828 cycles

DURING A-CHECK, FOUND 2 RT EXTERIOR OVERWING EMERGENCY LIGHTS DID NOT ILLUMINATE DURING TEST. SECURED LOOSE BATTERY PACK IN TRAY. ALL CHECKED GOOD.

Part: FRAME — DENTED (BS 1300 S26) · airframe 75,955 hrs · 37,564 cycles

DENT ON FRAME FLANGE STA 1300 RT STR 26. REPAIRED IAW ERA 485376-14 REV ORIG.

Part: STRUCTURE — CORRODED (BS 900 S26R) · corrosion level 2 · airframe 75,955 hrs · 37,564 cycles

FWD CARGO CORROSION, COMPT STA 900, S26R CORROSION. REPAIRED IAW ERA 485735-14 ORIG.

Part: STRUCTURE — DENTED (CARGO DOOR) · airframe 75,955 hrs · 37,564 cycles

AFT CARGO DOOR LOWER FWD CORNER HAS A PROTRUDING DENT. ACCOMPLISHED ERA 485736-14 ORIG.

Part: SHEAR TIE — CORRODED (BS 1400 S28L) · corrosion level 2 · airframe 75,955 hrs · 37,564 cycles

AFT CARGO SHEAR TIE CORRODED AFT SIDE OF FRAME STA 1400 OTBD TO S28L. REMOVED CORROSION, CHECKED LIMITS.

Part: INTERCOSTAL — CORRODED (BS 1400 S28L) · corrosion level 2 · airframe 75,955 hrs · 37,564 cycles

AFT CARGO INTERCOSTAL CORRODED AT STA 1400 STR 28L. R & R INTERCOSTAL.

Part: STRINGER — CORRODED (BS 1460 S29L) · corrosion level 2 · airframe 75,955 hrs · 37,564 cycles

AFT CARGO STRINGER 29L AT STA 1460 CORRODED. REPAIRED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 680) · corrosion level 2 · airframe 75,955 hrs · 37,564 cycles

FLOORBEAM CORRODED STA 680, LBL 3. INSTALLED REPAIR ANGLES IAW ER/A 481634-14.

Part: SKIN — DENTED (BS 620 S17L) · airframe 7,955 hrs · 37,564 cycles

FUSALAGE SKIN DENT STA 620 STR 17 L. REPAIRED IAW ER/A 484848-1.

Part: STRINGER — CORRODED (BS 1600-1620) · corrosion level 2 · airframe 75,955 hrs · 37,564 cycles

AFT CARGO STRINGER 28L CORRODED ON REPAIR SECTION BETWEEN STA 1600 AND 1620. REPLACED REPAIR SECTION.

Part: FRAME — DENTED (BS 1500 S26L) · airframe 75,955 hrs · 37,564 cycles

AFT CARGO FRAME DENTED AT STA 1500, STR26L. REPAIRED IAW 53-00-07, PG201, REPAIR 5.

Part: FRAME — DENTED (BS 1340 S26R) · airframe 75,955 hrs · 37,564 cycles

FUSELAGE FRAME DENTED STA 1340 STR 26R. INSTALLED REPAIR DOUBLER IAW 53-00-07 REPAIR 5 PG 204.

Part: SKIN — CRACKED (NR 9 SLAT) · airframe 75,955 hrs · 37,564 cycles

NR 9 SLAT COVE SKIN CRACKED. REPAIRED IAW ERA 366767-14.

Part: FLOORBEAM — CORRODED (BS 377.7) · corrosion level 2 · airframe 75,955 hrs · 37,564 cycles

CABIN FLOORBEAM CORRODED AT STA 377.7 LBL 47. REPAIRED IAW ER/A 481634-14.

Part: PRESSURE PANEL — CORRODED (BS 1680-1685) · corrosion level 2 · airframe 75,955 hrs · 37,564 cycles

MAIN CABIN PRESSURE DECK HAS AREAS OF CORROSION STA 1680-1685, BL0 - RBL54 ON TOP OF EXISTING DOUBLER. REMOVED AND REPLACED DOUBLER .

Part: PRESSURE PANEL — CORRODED (BS 1680-1720) · corrosion level 2 · airframe 75,955 hrs · 37,564 cycles

CABIN SAFTEY PRESSURE DECK CORRODED AT STA 1680-1720 LBL 50. REPAIRED IAW SRM 51-60-51.

Part: PRESSURE PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 75,955 hrs · 37,564 cycles

CABIN AFT PRESSURE DECK CORRODED. INSTALLED REPAIR DOUBLER IAW SRM 51-40-02.

Part: STRINGER — CORRODED (BS 1455 S29L) · corrosion level 2 · airframe 75,955 hrs · 37,564 cycles

STR 29L CORRODED AT STA 1455. REPAIRED IAW PRI 484843-14 REVO.

Part: SKIN — DENTED (BS 364 S25R) · airframe 75,955 hrs · 37,564 cycles

DENT IN FUSELAGE AT STA 364, S25R. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW ER/A 485365-14.

Part: SKIN — DENTED (FS 620) · airframe 73,368 hrs · 36,261 cycles

DENT OUT OF ALLOWABLES SKIN. CUTOUT THE DENT AND INSTALL SINGLE REPAIR DOUBLER FOR BOTH DAMAGE AREAS.

Part: SKIN — CORRODED (BS 1720 S27R-29L) · airframe 73,124 hrs · 36,115 cycles

FUSELAGE SKIN FOUND WITH CORROSION AT STA 1720 BETWEEN S-27R AND S-29L. CUTOUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER/TRIPLER.

Part: CHILLER — OVERHEATED (NR 2 GALLEY) · airframe 70,683 hrs · 35,030 cycles

DURING FLIGHT, BURNING ODOR DETECTED IN FORWARD GALLEY. ALL CIRCUIT BREAKERS WERE PULLED. FOUND INSULATION INSIDE CHILLER/FREEZER MELTED AND BURNED. CHECKED POWER TO UNIT ALL 3 PHASES CHECK OK. REPLACED CHILLER/FREEZER. CHECKS GOOD. OK TO CLEAR PER MCO AND PLACARD REMOVED.

Part: SKIN — CRACKED (L1 DOOR) · airframe 66,900 hrs · 33,284 cycles

THE FUSELAGE SKIN HAD A 2 IN CRACK AT THE UPPER FORWARD CORNER OF THE L1 DOOR OPENING. THE CRACKED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED. REF. 6-089732-12AD

Part: CONNECTOR — FAULTY (RT T/E FLAP) · airframe 66,892 hrs · 33,280 cycles

ON T/O WHEN FLAPS RET FROM 5 TO 1, TE FLAPS ASSYM LIGHT AND EICAS MSG DISPLAY. RTN TO LAND. FOUND CONNECTOR D1802 ON RT FLAP POS XMITTER BAD. REPLACED PLUG AND BIN. MEGGED OUT WIRING FROM XMITTER TO FSEU. ALL CKS OK. NO HELP. REPLACED RT TE FLAP POS X-MITTER AND NULLED PER MM. FLAP SYS CKS GOOD.

Part: SLIDE — DEPLOYED (RT OVERWING) · airframe 62,245 hrs · 31,578 cycles

RT OVERWING SLIDE DEPLOYMENT OCCURRED WHILE ORF POLICE SWAT TEAM WAS TRAINING ON BOARD A/C. DEPLOYMENT WAS SUCCESSFUL.

Part: KEEPER — BROKEN (NR 1 ENGINE) · airframe 58,910 hrs · 30,275 cycles

AFT LATCH OR CORE COWL ON NR 1 ENGINE BROKEN. REPLACED LATCH CATCH NR 1 ENGINE CORE COWL AFT POSITION PER M/M.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,502 hrs · 29,726 cycles

THE FUSELAGE SKIN WAS FOUND DENTED BELOW THE C2 DOOR OPENING BETWEEN FS 1420 &1440 AND BETWEEN STRINGERS 29L & 28R. THE DENTED AREA WAS REMOVED WITH A 25.25 X 7.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385730-14, REV A.

Part: SILL — CORRODED (FUSELAGE) · airframe 57,502 hrs · 29,726 cycles

THE OUTBOAD CHORD OF THE C2 DOOR OPENING LOWER SILL WAS FOUND CORRODED. TO FACILITATE REPLACEMENT OF THE SILL CHORD, THE OUTER CHORD AND WEB OF THE FS 1440 FRAME WERE CUT NEAR THE LOWER SILL AND THE LOWER SECTIONS REMOVED. A NEW SILL CHORD WAS INSTALLED AND THE FRAME WEB AND CHORDS SPLICED BACK IN WITH ALUMINUM REPAIR DOUBLERS PER ER/A 385725-14, REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,502 hrs · 29,726 cycles

FUSELAGE SKIN WAS FOUND DENTED AND GOUGED BETWEEN FS 1380 & 1400 AND BETWEEN STRINGERS 28L & 28R. THE DAMAGE WAS REMOVED WITH A 18.75 X 12.25 INCHES CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385729-14, REV A.

Part: PIN — BENT (ESCAPE SLIDE) · airframe 52,159 hrs · 27,155 cycles

AFTER TAXI IN LEFT EMERGENCY ESCAPE TEST LIGHT (P61) ON ALL THE TIME. REPLACED P61 PANEL, NO HELP. RE-INSTALLED ORIG. REPLACED RELAY K10486, NO HELP. RE-INSTALLED SIDEWALL AND BOTH HATCHES, REMOVED FOR ACCESS TO P78 PANEL. INSPECTED CANNON PLUG ON PRESSURE BOTTLE FOR EMERGENCY ESCAPE FOUND PIN BENT. STRAIGHTEN PIN, OPS TEST NORMAL. NO MESSAGES.

Part: ODOR — DETECTED (CABIN) · airframe 51,987 hrs · 27,077 cycles

FUMES REPORTED FROM REAR OF CABIN. INSPECTED AFT GALLEY AREA, NO PROBLEM FOUND INCLUDING COFFEEMAKERS AND POTABLE WATER COMPRESSOR.

Part: SKIN — MISDRILLED (FS 445, S-28) · airframe 51,466 hrs · 26,841 cycles

FUSELAGE / SKIN / FS 440-456 / STRG. 28L-28R : TOOLING DAMAGE REPAIR THE FUSELAGE SKIN WAS GOUGED AND MISDRILLED DURING REPLACEMENT OF A TCAS ANTENNA BETWEEN FS 440 & 456 AND BETWEEN STRINGERS 28L & 28R. THE DAMAGE WAS REMOVED WITH A 15" X 13" CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 381547-14, REV A.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 51,438 hrs · 26,828 cycles

RT ENG SEC CONTROL STATUS MSG THEN AFTER LEVEL OFF RT ENG STATOR CAUTION MSG, ENG SHUTDOWN. C/A REPLACED ENGINE, FCU, &EEC PER MM,PERFORMED TEST 7 14 AND 15 FROM PFHB. OPS CHKD AND LEAK CHKD OK

Part: INVERTER — FAILED (E&E COMPT)

STRONG ELECTRICAL ODOR THROUGHOUT A/C. EICAS STATUS MSG FWD EQUIP DET 2. EQUIP COOLING TEST. FUEL QUANTITY BITE. STANDBY INVERTER. DIVERTED TO KSAV. DETERMINED THE SOURCE OF SMOKE/ELECTRICAL ODOR TO BE THE STATIC INVERTER. REPLACED SAME. OPN CKS NORMAL. NO ODOR NOTED. REPLACED THE FWD EQUIP DET LIGHT ASSY. SYSTEM CKS NORMAL.

Part: FAN — FAILED (RT CABIN)

ELECTRICAL SMELL IN CABIN. REPLACED RIGHT RECIRC FAN FOR PRODUCING ODOR.

Part: KEEL BEAM — CORRODED (BS 1390)

THE STRG 29L KEEL CHORD WAS FOUND CORRODED BETWEEN STA 1390 AND 1400. THE CHORD WAS CUT AT STA 1390 AND THE AFT END REMOVED. A NEW SECTION OF CHORD WAS SPLICE IN WITH STEEL REPAIR ANGLES PER ER/A 364526-14, REV C.

Part: DUCT — OIL CONTAM (LT PACK)

AT FL 410 AFTER 1 HR OF FLT SMOKE APPEARED IN CABIN WITH FWD AND AFT SMOKE DET SOUNDING. TURNED OFF LT PACK WITH NO IMPROVEMENT. AFTER 2-3 MINS TURNED OFF RT PACK SEEMED TO GET WORSE. DIVERTED TO ABQ. ATL DELTA NORTH FOUND OIL IN LT PACK DUCTING. REPLACED ACM, HEAT EXHANGER, REHEATER AND CONDENSER. CKS GOOD ON EXTENDED ENG RUN.

Part: AIR DISTR — SMOKE (CABIN)

OIL SMELL AND SMOKE IN CABIN AT ALTITUDE. C/W INSPECTION OF DUCTING AND CONTAMINATION REMOVAL PER B757 M/M 21-00-01-02 PAGES 201 THROUGH 204. OPERATION OF PNEUMATICS SYSTEM NOW CHECKS NORMAL. ALSO, RENDERED APU INOPERATIVE PER ATLMA UNDER MEL 49-00-01A.

Part: PACK — MALFUNCTIONED (LEFT)

ON CLIMB FROM FL370 TO FL410, GOT SMOKE AND ODOR IN CABIN. SMOKE DETECTORS ACTUATED. DESCENDED TO FL370 AND TURNED OFF LT BLEED AND LT PACK. SMOKE CLEARED QUICKLY. CONTINUED FLIGHT WITH LT BLEED AND LT PACK OFF. PROBLEM ISOLATED TO LT PACK. DISPATCHED WITH LT PACK ON MEL 21-51-01. MAINTENANCE RAN ENGINE AND BLEED SYSTEM, ALL CHECKED GOOD. MEL REMOVED AND NO FURTHER PROBLEMS.

Part: ENGINE — FAILED (NR 1)

DURING DESCENT, ENG ANTI-ICE TURNED ON CABIN FILLED WITH LIGHT SMOKE AND ODOR, FWD LAV AND AFT LAV SMOKE ALARMS WENT OFF. TURNED OFF ACTIVE AND CLOSED LT ENG BLEED VLV, SMOKE ALARM WENT AWAY. REPLACED NR 1 LT ENG.

Part: PACK — MALFUNCTIONED (LEFT)

SMOKE IN CABIN AND COCKPIT AFTER SEA DEPARTURE. AIR TURNBACK TO SEA. FOUND LT PACK OVERTEMP IN AUTO MODE WAS OK IN MANUAL MODE FWD LT PACK AUTO MODE INOP PER MEL 21-51-03B.

Part: OVEN — DIRTY (GALLEY)

FWD GALLEY FWD OVEN CAUSES ODOR OF HOT INSULATION. SET OFF F/C LAV SMOKE ALARM AND CAUSED FUMES IN COCKPIT. INSPECTED OVENS, REMOVED BURNED STRING FROM FWD F/C OVEN AND RAN BOTH, CK OK NO ODOR NOTED.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY ESCAPE PATH LIGHTS INOP AT LEFT WING EXIT DOOR. REPLACED POWER SUPPLY.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

AISLE EMERGENCY LIGHT ABOVE 34DEF INOP. REPLACED POWER SUPPLY, CKS GOOD.

Part: FAN — FAILED (CABIN)

RIGHT RECIRC EICAS MSG, CABIN FILLED WITH SMOKE, DIVERTED TO MCI. DEACTIVATED RT RECIRC FAN BY PULLING C/BS. FWD TO MCO AND PLCRD PER MEL 21-25-01A. RAN ENGS AND BOTH PACKS, NO SMOKE PRESENT.

Part: TE WEDGE — DELAMINATED (NR 10 LE SLAT)

T/E WEDGE CRACKED AND DELAMINATED. REPLACED T/E WEDGE PER SRM 57-43-02, DURING SHOP INSPECTION FOR NR 10 L/E SLAT.

Part: SKIN — DAMAGED (RT TE FLAP)

FOUND DURING LETTER CHECK, TWO HOLES IN THE UPPER SURFACE OF THE RT I/B AFT FLAP AT O/B END. REPAIRED PER SRM 57-53-01.

Part: SKIN — DAMAGED (RT TE FLAP)

FOUND DURING LETTER CHECK, HOLE IN LOWER SURFACE OF RIGHT I/B AFT FLAP. REPAIRED PER SRM 57-53-01.