N138DL

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 74,755 hrs · 30,147 cycles

EMERGENCY LIGHTS FROM ROW 12 TO CENTER LAVS ARE INOPERATIVE ON BOTH SIDES. MAINTENANCE POWER PACK WITH BLOWN FUSE, FOUND SHORT TO GROUND AT SEAT 15 LEFT AND REPINNED PLUG AT SEAT 16 LEFT. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 74,755 hrs · 30,147 cycles

EMERGENCY LIGHT AT SEAT 30 RT SIDE ARE INOPERATIVE. MAINTENANCE FOUND PIN PULLED OUT OF PLUG AND REPINNED. SYSTEM OPERATION IS NORMAL.

Part: RECEIVER — ODOR (ADF) · airframe 74,076 hrs · 29,964 cycles

PERFORMED AN AIR TURNBACK DUE TO AN ELECTRICAL BURNING ODOR THROUGHOUT THE ACFT. FOUND CIRCUIT BREAKER POSITION F6, LEFT ADF, WAS TRIPPED. VERIFIED THE ADF RECEIVER AS THE CAUSE. REPLACED THE LT ADF RECEIVER IAW AMM 34-57. INSPECTED ACFT CARGO BIN AND E/E COMPARTMENTS FOR OTHER PROBLEMS, NONE FOUND. ACFT OK FOR SERVICE.

Part: BEAM — CRACKED (WING) · airframe 71,599 hrs · 29,269 cycles

BEAM CRACKED, OTBD SIDE AT LWR FASTENER AFT OF STUD FITTING. CRACKED IN BEAM ONLY. NR 7 FLAP SUPPORT. C/W ERA 530729-14.

Part: SUPPORT BEAM — CRACKED · airframe 71,599 hrs · 29,269 cycles

MAIN OTBD SUPPORT BEAM, INBD SIDE AT NR 2 JOINT, 2 EA .3750 SIZE FASTENERS AND 1 FASTENER ON OTBD SIDE AT NR 2 JOINT, SHOW CRACK. C/W ERA 530731-14.

Part: FRAME — CRACKED (BS 859) · airframe 71,594 hrs · 29,268 cycles

FRAME CRACKED AT BS 859.5 ON RT SIDE BELOW WL 200. REPAIRED ON WC 5311-01-01195-09.

Part: OXYGEN MASK — INOPERATIVE (SEAT 34CDF) · airframe 70,443 hrs · 28,941 cycles

DURING AN EMERGENCY DESCENT, DUE TO PRESSURIZATION FAILURE, OXYGEN MASKS AT SEAT 34CDF DID NOT DROP. INSPECTED PSU AND MASK LATCH ASSEMBLY AND VERIFIED DEPLOYMENT DURING MANUAL DEPLOYMENT, AND REPACKED MASKS.

Part: BULB — BROKEN (EMERGENCY LIGHT) · airframe 68,672 hrs · 28,438 cycles

LT SIDE OF FUSELAGE, TWO EMERGENCY EXIT EXTERIOR LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND BROKEN BULB AND DAMAGED HARDWARE AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 68,463 hrs · 28,369 cycles

EMERGENCY LIGHTS AT ROW 14AB IS INOPERATIVE. MAINTENANCE REPAIRED CONNECTOR. SYSTEM OPS NORMAL. (LP 1182487)

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 68,463 hrs · 28,369 cycles

EMERGENY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. SYSTEM OPERATION IS NORMAL. (LP 1182485)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,440 hrs · 27,517 cycles

EMERGENCY LIGHTS ROW 35 AND AFT ARE INOPERATIVE. MX REPLACED THE BATTERY PACK AND CHARGER. SYS OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,652 hrs · 27,287 cycles

EMERGENCY LIGHTS AT 35A-F TO 46A-F ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER M9010 PER AMM. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 64,613 hrs · 27,269 cycles

EMERGENCY LIGHTS FROM ROW 35-47 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND BATTERY CHARGER M9010. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,174 hrs · 27,148 cycles

FOUND DURING A CHECK EMERGENCY EXIT PATHWAY LIGHTS ROW 35 AFT ARE INOPERATIVE. THE BATTERY PACK REPLACED. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,800 hrs · 27,046 cycles

EMERGENCY PATCH LIGHTING ROW 35 ON INOPERATIVE. REPLACED BATTERY CHARGER ASSY M9010 PER 767 AMM 33. OPS CHECK NORMAL OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,729 hrs · 27,026 cycles

ALL EMERGENCY LIGHT FROM ROW 35 AFT INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51.

Part: DOOR — DEFORMED (RT MLG) · airframe 61,849 hrs · 26,511 cycles

RIGHT MLG TRUNNION DOOR LWR EDGE DEFORMED. REPAIRED PER ERA 496335-14.

Part: SKIN — DENTED (TE FLAP) · airframe 61,849 hrs · 26,511 cycles

INBOARD AFT FLAP LWR SURFACE DENTED. METAL HOT BOND REPAIR C/W PER B767-300 SRM 57-53-01, REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.

Part: FITTING — DAMAGED (NR 1 PYLON) · airframe 61,849 hrs · 26,511 cycles

NR 1 PYLON MIDSPAR BH FITTING HAS 10 EACH OVERSIZED FASTENERS. REPAIRED PER ERA 496325-14AD REV ORIG.

Part: FITTING — MISREPAIRED (NR 2 PYLON) · airframe 61,849 hrs · 26,511 cycles

NR 2 PYLON UPPER PITCH LOAD FITTING "T" CLIP HAS HOLE WITH SHORT EDGE DISTANCE. C/W REPAIR PER ERA 496333-14AD REV ORIG.

Part: PANEL — DEBONDED (TE FLAP) · airframe 61,849 hrs · 26,511 cycles

RT WING O/B FLAP UPPER PANEL 666KT IS DISBONDED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 201.

Part: FITTING — MISREPAIRED (NR 1 PYLON) · airframe 61,849 hrs · 26,511 cycles

LT UPPER PITCH LOAD FITTING "T" CLIP HAS SHORT EDGE DISTANCE AT FASTENER HOLE FOR NR 1 PYLON. REPAIR PER ERA 496333-14AD.

Part: FITTING — DAMAGED (NR 2 PYLON) · airframe 61,849 hrs · 26,511 cycles

NR 2 PYLON MIDSPAR BH FITTING HAS 10 EACH OVERSIZED FASTENERS. REPAIRED PER ERA 496325-14AD REV ORIG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,849 hrs · 26,511 cycles

FWD C/C FS 654+121 LBL 38 FRAME UPPER CHORD IS CORRODED BEYOND LIMITS.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,849 hrs · 26,511 cycles

LT WING O/B FLAP L/E AREA IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND 51-70-05 PAR 5A (1).

Part: SPAR — MISREPAIRED (NR 1 PYLON) · airframe 61,849 hrs · 26,511 cycles

NR 1 PYLON FWD UPPER SPAR WEB FASTENER PATTERN DOES NOT MATCH SB 767-54-0090 REV 2 FIG 10. SPAR WEB REPAIRED PER ERA 496329-14 REV ORIG.

Part: WEDGE — DENTED (TE FLAP) · airframe 61,849 hrs · 26,511 cycles

RT WING I/B T/E AFT FLAP T/E WEDGE IS DENTED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 61,849 hrs · 26,511 cycles

LT WING I/B MAIN FLAP O/B L/E FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PAR 5A (1).

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,849 hrs · 26,511 cycles

FWD C/C FS 654+121 LBL 38 FRAME UPPER CHORD IS CORRODED BEYOND LIMITS. CHORD REPLACED PER B767-300 SRM 51-10-02 AND INSTALLED PER B767-300 SRM 51-40-02.

Part: SPAR — MISREPAIRED (NR 2 PYLON) · airframe 61,849 hrs · 26,511 cycles

NR 2 PYLON FWD UPPER SPAR WEB FASTENER PATTERN DOES NOT MATCH SB 767-54-0090 REV 2 FIG 10. SPAR WEB REPAIRED PER ERA 496330-14 REV ORIG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,849 hrs · 26,511 cycles

FS 1197 +66 FLOOR FRAME UPPER SURFACE IS CORRODED AT RBL 42 BEYOND LIMITS OF SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,849 hrs · 26,511 cycles

FS 1197+66 FLOOR FRAME UPPER SURFACE CORRODED AT RBL 42 BEYOND LIMITS OF SRM. FLOORBEAM UPPER CHORD REPLACED PER B767-300 N SRM 51-10-02 AND INSTALLED PER B767-300 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,849 hrs · 26,511 cycles

FS 1219 FLOOR FRAME UPPER CHORD IS CORRODED AT LBL 22.5 BEYOND SRM LIMITS. FLOORBEAM UPPER CHORD REPLACED IAW B767-300 SRM 51-10-02 AND INSTALLED IAW B767-300 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,849 hrs · 26,511 cycles

FS 1219 FLOOR FRAME UPPER CHORD IS CORRODED AT BL L22.5 BEYOND SRM LIMITS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,849 hrs · 26,511 cycles

CABIN RT STA 883 BETWEEN STR 20R AND STR 21R FRAME INNER CHORD CRACK. REPAIR ACCOMPLISHED AS PER ERA 491126-14AD REV 0.

Part: RELAY — MALFUNCTIONED (FA PANEL) · airframe 60,980 hrs · 26,280 cycles

THE FLIGHT CREW REPORTED THAT SPARKS AND SMOKE WERE COMING FROM THE 2R SLIDE LIGHT. MAINTENANCE REMOVED AND REPLACED THE RELAY BEHIND THE 2R FLIGHT ATTENDANT LIGHTING CONTROL PANEL. ALL CHECKS WELL PER AMM.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 60,446 hrs · 26,137 cycles

FUSELAGE STRINGER LBL & RBL 85.9, FS 966. REPAIRED IAW ERA 481423-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,732 hrs · 25,955 cycles

FUSELAGE SKIN STA 140-152, STR 24R-27R LIGHTNING DAMAGE. REPAIRED IAW ERA 479493-14.

Part: FAILSAFE — CORRODED (BS 980) · airframe 57,054 hrs · 25,279 cycles

A CRACK INDICATION WAS FOUND ON THE RT FAIL SAFE STRAP REF ERA 481422-14AD.

Part: FAILSAFE — CORRODED (BS 960) · airframe 57,054 hrs · 25,279 cycles

A CRACK INDICATION WAS FOUND AT LWR BOLT HOLE FAIL SAFE STRAP INSP REF ERA 481421-14AD.

Part: SLIDE — OPEN (R1 DOOR) · airframe 56,217 hrs · 25,048 cycles

R1 DOOR SLIDE WOULD NOT ARM AT DEPARTURE TIME. FOUND SLIDE PACK PARTIALLY OPEN. REPLD R1 SLIDE PACK IAW AMM. OPS CKS NML.

Part: DOOR — DAMAGED (CARGO BAY) · airframe 55,923 hrs · 24,967 cycles

AFT CARGO DOOR LOWER AFT CORNER DAMAGE. REPAIRED IAW ERA 477986-14.

Part: MODULE — MISSING (PAX SEAT OXYGEN) · airframe 55,781 hrs · 24,927 cycles

DURING EA 01-477420-12 AD REV ORIG MEO1 FOUND ENTIRE O2/MASK MODULE MISSING OVER SEAT 12AB. INST O2 MASK/GEN MODULE ASSY AT 12AB

Part: SENSOR — MALFUNCTIONED (STAB TRIM) · airframe 54,634 hrs · 24,635 cycles

REJECTED TAKEOFF FOR UNSCHEDULED TRIM EICAS MSG. PERFORMED FIM AND MM TESTS OF STAB TRIM INDICATION SYSTEM. FOUND CENTER FSPM CARD WOULD NOT TEST. REPLACED CTR FSPM CA STAB RATE ISOLATES L AND C POSITION SENSORS. REPLACED R STA TRIM POSITION SENSOR. ALL POST TESTS OK PER MM.

Part: SENSOR — MALFUNCTIONED (STAB TRIM) · airframe 54,634 hrs · 24,635 cycles

UNSCHEDULED STAB TRIM DURING TAKEOFF AT APPROX 75 KTS. RTO, TS PER FIM 27-09-00 FIG 106A. CHECKED SAMS CHECKED FSPMS ALL CHK NORM. PERFORMED STAB TRIM CHKS FROM YOKE AND PEDESTAL PER FIM. ALL NORM. INSPECTED STAB POS XMITTER CABLES ALL PULLEYS AND CABLES APPEAR NORMAL. PERFORMED FIM AND MM TESTS OF STAB TRIM INDICATION SYSTEM. FOUND CENTER FSPM CARD WOULD NOT TEST. REPLACED CTR FSPM CA STAB RATE ISOLATES L AND C POSITION SENSORS. REPLACED R STA TRIM POSITION SENSOR. ALL POST TESTS OK PER MM.

Part: CIRCUIT CARD — INOPERATIVE · airframe 54,634 hrs · 24,635 cycles

ON TAKEOFF ROLL EXACTLY THE SAME THING HAPPENED AS PREVIOUS WRITE-UP. BRAKE TEMP NEVER ABOVE 2. PERFORMED FIM AND MM TESTS OF STAB TRIM INDICATION SYSTEM. FOUND CENTER FSPM CARD WOULD NOT TEST. REPLACED CTR FSPM CARD. STAB RATE ISOLATES L AND C POSITION SENSORS. REPLACED RT STAB TRIM POSITION SENSOR. ALL POST TESTS OK PER MM.

Part: TRIM SYSTEM — MALFUNCTIONED (STAB) · airframe 51,785 hrs · 23,646 cycles

UNSCHEDULED STAB TRIM 3X DURING T/O ROLL. RTO AND RTN GATE. NO HIST, T/S PER FIM 27-09-00 FIG 106A. SAMS AND FSPM BITE CHK GOOD. RAN STAB FROM BOTH COLUMNS AND CTR PEDESTAL FULL TRAVEL NO EICAS MSGS. ALL CHKS OK. A/C OK FOR SERVICE.

Part: LINK — DAMAGED (TE FLAP) · airframe 51,327 hrs · 23,488 cycles

TRAILING EDGE FLAP 3-10 LINKS. REPAIRED IAW EA 01-076248-12, ME07, ME08, ME09, ME10, ME11, ME12.

Part: SKIN — DAMAGED (BS 196 S21-24L) · airframe 50,552 hrs · 23,178 cycles

THE FUSELAGE SKIN WAS FOUND WITH LIGHTNING STRIKE DAMAGE AT STA 196.5 BETWEEN S-21L AND S-24L. THE DAMAGED SKIN WAS CUTOUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: WHEEL — WORN (RT NLG) · airframe 49,172 hrs · 22,744 cycles

ON TAKEOFF AT V1 SIGNIFICANT YAW-TRANSIENT EVENT AND LOUD BANG HEARD IN CABIN. SUSPECTED BLOWN TIRE. ON ARRIVAL INSPECTED ALL WHEEL ASSYS AND GEAR. RT NOSE WHEEL ASSY HAD SOME PLAY. REPLACED BOTH NOSE WHEEL ASSYS.

Part: UNKNOWN — ODOR (CABIN) · airframe 48,916 hrs · 22,669 cycles

F/ATTENDS SMELL BURNT ODOR THROUGHOUT AIRPLANE. CHKD CABIN AND GALLEY AREAS, NO NOTICEABLE ODORS FOUND. NO REPORT BY INBOUND CREW. SUSPECT ODOR INTRODUCED BY GROUND A CONDITIONING. NO TROUBLE FOUND.

Part: SKIN — GOUGED (FS 1269 S31R) · airframe 48,031 hrs · 22,421 cycles

THE FUSELAGE SKIN WAS GOUGED FORWARD OF THE C2 DOOR OPENING AT STA 1269, S31R. GOUGE AFTER BLENDING WAS 1 BY 0.8 IN. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: CONTROL PANEL — ODOR (COCKPIT) · airframe 46,953 hrs · 21,979 cycles

STRONG ELECTRICAL ODOR IN COCKPIT. REMOVED AND REPLACED OVERHEAD LIGHT SWITCH PANEL PER M/M, OPS CHECKS GOOD. REMOVED MCO/PLACARD.

Part: CHILLER — ODOR (GALLEY) · airframe 44,291 hrs · 21,000 cycles

ELEC SMELL FROM AFT GALLEY AREA. FOUND SMELL FROM AFT GALLEY CHILLERS. UNABLE TO DUPLICATE.

Part: DRAG BRACE — LOOSE (LT MLG) · airframe 43,664 hrs · 20,726 cycles

LANDING GEAR UNSAFE AURAL WARNING AND GEAR DOOR LIGHT ILLUMINATED ON LANDING TOUCHDOWN. REPLACED LEFT MLG UPPER DRAG BRACE SPINDLE. INSPECTED GEAR AS PER ERA 01-0451457-14.

Part: MODULE — FAILED (TRIM CONTROL) · airframe 43,629 hrs · 20,710 cycles

UNSHEDULED STAB TRIM EICAS MESSAGE. ABORTED T/O AT 100 KTS. REPLACED LEFT STAB TRIM CONTROL MODULE BRAKE PRESSURE SWITCH.

Part: SKIN — CORRODED (BS 1219) · airframe 43,629 hrs · 20,710 cycles

FUSELAGE/SKIN/STA 1197+132 - STA 1219 BELOW S-36R CORRODED. CORROSION DAMAGE CUT OUT FROM SKIN AT LAP SLICE AND AN EXTERNAL ALUMINUM DOUBLER AND FILLER INSTALLED WITH HI-LOKS.

Part: SKIN — CORRODED (BS 1218 S-36R) · airframe 43,622 hrs · 20,707 cycles

THE FUSELAGE SKIN AT BS 1218, S-36R WAS FOUND CORRODED OVER AN APPROXIMATELY 4 INCH BY 8 INCH AREA. THE CORRODED SKIN WAS REMOVED AND A DOULBER INSTALLED.

Part: FRAME — CRACKED (BS 903.5) · airframe 43,622 hrs · 20,707 cycles

THE INNER CHORD OF THE LT STA 903.5 FRAME WAS FOUND WITH A 0.60 INCH LONG CRACK. REPAIR ANGLE INSTALLED PER ACTS PP B767-53-21657, REF ER/A 450982-14AD, AD 2003-18-10.

Part: BOLT — UNKNOWN (VERTICAL FIN) · airframe 43,622 hrs · 20,707 cycles

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

Part: FITTING — UNKNOWN (WING T/E) · airframe 43,622 hrs · 20,707 cycles

WING T/E - INBD FLAP - MAIN FLAP - COLLAR FITTING REPLACEMENT IAW EO 01-073591-12 ME12 AND ME13. C/W EO 01-073591-12 ME12 AND ME13.

Part: WIRE — BROKEN (PDU) · airframe 42,244 hrs · 20,159 cycles

UPON ARRIVAL NOTIFIED BY RAMP, WHILE UNLOADING CARGO FROM FWD CARGO COMPARTMENT, NOTICED LARGE SPARKS AND SMOKE FROM AREA AROUND NR 8 PDU ON THE LEFT SIDE. C/B FOR PDUS 2, 6, 8 LEFT POPPED. REMOVED PDU, SPLICED 7 WIRES ON P1242, ALL EXCEPT W 704-318, BRY-20 SPLICED W 704-318 BRY -20 WIRES AND ROUTED CORRECTLY. PDU CHECKS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,770 hrs · 18,390 cycles

DURING SVC CHECK FOUND LT FWD CABIN OVERHEAD EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY.

Part: BLEED VALVE — INOPERATIVE (NR 2 ENGINE) · airframe 37,580 hrs · 17,763 cycles

REJECTED TAKEOFF SHORTLY AFTER TAKEOFF POWER APPLIED. (LESS THAN 30 KTS) FOR MASTER CAUTION LIGHT AND AURAL WARNING. EICAS MSG RT ENGINE BLEED VALVE AND BLEED ANNUNCIATOR LIGHT IN OVERHEAD PANEL ILLUMINATED. REPLACED VALVE

Part: MEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 31,241 hrs · 14,696 cycles

DURING FLIGHT NR 2 ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. ENGINE SHUT DOWN, LANDED SINGLE ENGINE. CHECKED THROTTLE CABLES, ALL SECURE. REMOVED AND REPLACED MECPRE M/M. LEAK AND RUN CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,975 hrs · 14,581 cycles

LEFT EXTERNAL EMERGENCY LIGHTS INOP AFT OF WING. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,603 hrs · 14,401 cycles

ON SERVICE CHECK FOUND LEFT AFT EXTERIOR EMERGENCY LIGHTS INOP. R/R BATTERY PACK CHECKS GOOD

Part: POWER SUPPLY — WILL NOT TEST (CABIN) · airframe 29,881 hrs · 14,051 cycles

ON SERVICE CHECK FOUND C-ZONE SEAT MOUNTED EMERGENCY LIGHTS NOT WORKING. FOUND POWER SUPPLY NOT FUNCTIONING PROPERLY. REMOVED AND REPLACED AFT LEFT AND RIGHT. CHECKS GOOD.

Part: PIN — MISSING (NR 7 BRAKE) · airframe 28,658 hrs · 13,464 cycles

UPON ARRIVAL INTO MIA FOUND NR 7 BRAKE ANTI-ROTATION PIN MISSING AND SMALL HYDRAULIC PUDDLE BY NR 7 BRAKE AND TIRE. FOUND NR 7 BRAKE SPUN ON AXLE CAUSING DAMAGE TO ANTI SKID CONDUIT. HYDRAULIC BRAKE LINE AND NR 7 BRAKE TEMP SENSOR HARNESS PIN REF IPC 32-41-06-01 ITEM 65 FIG 01. REPLACED AFFECTED PARTS.

Part: SKIN — DENTED (BS 368)

SKIN AND STRINGER DAMAGED AT STA 368 AND STRINGER 33R. DAMAGE CONSISTS OF DENTED SKIN AND CRACKED STRINGER. ERA 333785-14.

Part: SKIN — DENTED (BS 1560)

SKIN DENTED BEYOND SRM LIMITS AT STA 1560 BETWEEN STRINGERS 20L AND 21L. ERA 333757-14 REV A.

Part: SKIN — GOUGED (BS 500)

DAMAGE TO SKIN AND TEAR STRAP AT STA 500 BETWEEN STRINGERS 38L AND 39L. DAMAGE CONSISTS OF DENTS AND GOUGES BEYOND SRM LIMITS. ERA 333770-14 REV A.

Part: SKIN — DENTED (BS 640)

A DENT WAS FOUND IN THE EXTERNAL SKIN AT STA 640 BETWEEN S31R AND S32R. THE DENT IS 2.5 BELOW AN EXISTING SRM SMALL SMALL HOLE REPAIR. REPAIRED PER ERA 330885-14.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

AFT FLOOR TRACK LIGHTS INOP FROM MIDDLE OF AFT CABIN AND BACK ON BOTH SIDES. REPLACED POWER SUPPLY, OPS CHECK GOOD.

Part: OVEN — SMOKING (FWD GALLEY)

BOTTOM OVEN IN F/C GALLEY PRODUCING SMOKE. PULLED AND COLLARED OVEN CIRCUIT BREAKER. FORWARD ITEM TO MCO. REPLACED OVEN.

Part: SLIDE — DEPLOYED (CABIN DOOR)

DOOR 2R SLIDE DEPLOYED, FLIGHT ATTENDANT REPORTED ARMING/DEARMING MECHANISM DIFFICULT TO OPERATE. FORWARD 2R SLIDE TO MCO PER MEL 52-11-04 ARMING MECHANISM CHECKS GOOD. SLIDE REPLACED ON LOG A020745004, FLT 1632 IN BOS, S/N INSTALLED PA1354, MCO AND PLACARD REMOVED.

Part: AIR DISTR — SMOKE ODOR (CABIN)

AFTER T/O, F/A REPORTED LIGHT ODOR OF SMOKE THROUGHOUT CABIN. ALSO, HEAT EMITTING FROM AREA AROUND SEAT 1F, LOWER HALF OF SIDEWALL. CHECKED ALL LIGHT BALLASTS IN AREA, NO PROBLEM FOUND. RAN PACKS AND INSPECTED AREA AROUND SEAT 1F, NO PROBLEM NOTED. RETURNED TO SERVICE.