N527AU

Part: CIRCUIT CARD — UNKNOWN (E&E BAY)

PHL FLT1407 - AFTER TAKEOFF FROM PHL, CREW RECEIVED BOTH MAIN LANDING GEAR RED UNSAFE LIGHTS AFTER RAISING GEAR AND RETURNING GEAR LEVER TO OFF POSITION. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES, CONSULTED MAINTENANCE AND RETURNED TO FIELD AT PHL. FLIGHT LANDED WITH ALL THREE GEAR GREEN SAFE LIGHTS AND WITHOUT FURTHER INCIDENT. MAINTENANCE JACKED AIRCRAFT AND ACCOMPLISHED NUMEROUS GEAR SWINGS. COULD NOT DUPLICATE FAULT. AS PRECAUTIONARY, REPLACED M986 CARD PER MM 32-09-20-004-001. OPERATIONAL CHECK GOOD PER MM 32-09-20-724-031. OPERATED GEAR AFTER CARD REPLACEMENT. ALL INDICATIONS NORMAL.

Part: SLIDE — NO TEST (ZONE 200)

PHL - THE FORWARD RIGHT HAND SERVICE DOOR EMERGENCY ESCAPE SLIDE FAILED THE ANNUAL OPERATIONAL TEST WHEN IT TWISTED DURING DEPLOYMENT. MAINTENANCE REPLACED THE SLIDE. INSPECTED OK FOR SERVICE.

Part: SKIN — CRACKED (BS 727) · airframe 55,073 hrs · 33,695 cycles

FOUND 1.8750 INCH LONG CRACK IN SKIN AT STA 727 LONGERON 22L. CUT OUT CRACKED AREA/HFEC/INSTALLED DOUBLER IAW SRM 53-00-01.

Part: STRUCTURE — PUNCTURED (NR 5 SPOILER) · airframe 53,780 hrs · 53,780 cycles

OUTBOARD OF NR 5 SPOILER PUNCTURED. REMOVED DAMAGE, INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 2 INCH.

Part: SKIN — PUNCTURED (NR 5 SPOILER) · airframe 53,780 hrs · 53,780 cycles

OUTBOARD OF NR 5 SPOILER PUNCTURE. REMOVED DAMAGE INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 2 INCHES.

Part: SKIN — PUNCTURED (NR 6 SPOILER) · airframe 53,780 hrs · 53,780 cycles

NR 6 SPOILER TOP CENTER OF SPOILER PANEL PUNCTURE. MAJOR REPAIR, IAW TR 27-60-01, DEFECT SIZE: 1 INCH.

Part: SKIN — DELAMINATED (WING) · airframe 53,780 hrs · 53,780 cycles

STA WBL 170-160 AND 181 UPPER FIXED WING T/E DELAMINATED. REMOVED DAMAGE AND APPLIED A COMPOSITE REPAIR IAW EA 78270, DEFECT SIZE: 3 INCHES.

Part: REPAIR — UNKNOWN (RT ELEVATOR) · airframe 53,780 hrs · 53,780 cycles

RIGHT ELEVATOR LOWER SURFACE 9 INCHES I/B OF O/B END AND 16 INCHES AFT OF FRONT SPAR. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 2.5 INCHES.

Part: REPAIR — UNKNOWN (RT ELEVATOR) · airframe 53,780 hrs · 53,780 cycles

RIGHT ELEVATOR LOWER SURFACE 59 INCHES I/B OF O/B END AND 10 INCHES AFT OF RIGHT. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 6 INCHES.

Part: REPAIR — UNKNOWN (RT ELEVATOR) · airframe 53,780 hrs · 53,780 cycles

RIGHT ELEVATOR LOWER SURFACE 59 INCHES I/B OF O/B END AND 10 INCHES AFT OF FRONT SPAR DAMAGED. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 6 INCHES.

Part: REPAIR — UNKNOWN (RT ELEVATOR) · airframe 53,780 hrs · 53,780 cycles

RIGHT ELEVATOR, LOWER SURFACE 30 INCHES O/B OF I/B END AND 12 INCHES AFT OF RIGHT DAMAGED. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 6 INCHES.

Part: RIB — CRACKED (WING) · airframe 53,780 hrs · 53,780 cycles

IN SPAR LOWER AFT SUPPORT RIB 135.5 CRACKED. REPAIRED IAW 97467, DEFECT SIZE: 1.250 INCH.

Part: FRAME — CRACKED (BS 827) · airframe 53,780 hrs · 53,780 cycles

FOUND CRACK AT FRAME STA 827 BETWEEN S8L. FABRICATED FRAME REPAIR ANGLES AND INSTALLED PER T/R 53-10-20C, DEFECT SIZE: .125 INCH.

Part: ANGLE — CORRODED (BS 767-790) · corrosion level 1 · airframe 53,780 hrs · 53,780 cycles

FOUND CORROSION ON TRANSITION ANGLE STA 767-790 AT NUT PLATES. REMOVED CORROSION AND INSTALLED REPAIR PARTS IAW SRM 51-10-02, DEFECT SIZE: .250".

Part: FRAME — CRACKED (BS 787) · airframe 53,780 hrs · 53,780 cycles

FOUND FRAME CRACKED BS 787 BETWEEN S-8R AND S9-R AT OVERHEAD BIN ATTACH POINT. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES IAW TR 53-10-20C, DEFECT SIZE: .125".

Part: FRAME — CRACKED (BS 380) · airframe 53,780 hrs · 53,780 cycles

FOUND CRACK BS 380 BETWEEN S-8R AND S-9R AT OVERHEAD BIN LOWER ATTACH. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES IAW TR 53-10-20C, DEFECT SIZE: .125 INCH.

Part: FITTING — CRACKED (RT MLG) · airframe 53,780 hrs · 53,780 cycles

FOUND CRACK RIGHT MAIN LANDING GEAR SUPPORT FITTING AT HOLE B/2. INSTALLED REPAIR PER TR 57-40-13 REV A, DEFECT SIZE: .125".

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

AD 2005-20-03 INSP/REPAIR OF INTERCOSTALS FOUND CRACK COMMON TO MAIN ENTRY DOOR. REMOVED AND REPLACED CRACKED INTERCOSTAL WEB AND STRAP WITH FABRICATED PARTS IAW SRM 53-10-04 REPAIR DEFECT SIZE: .25.

Part: BRACKET — CRACKED (BS 480) · airframe 53,780 hrs · 53,780 cycles

FOUND CRACKED PSU RAIL BRACKET AT RT BODY STA 480. REMOVED AND REPLACED PSU RAIL BRACKET WITH FABRICATED IAW TR 53-10-20C, DEFECT SIZE: .250 INCH.

Part: DOOR FRAME — CRACKED (BS 847 S24R) · airframe 53,780 hrs · 53,780 cycles

FOUND AFT CARGO DOOR/AFT FRAME CRACKED STA 847 STR 24R. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-70-13, DEFECT SIZE: 1".

Part: FRAME — CRACKED (BS 807) · airframe 53,780 hrs · 53,780 cycles

FOUND CRACK STA 807 BETWEEN S8L-9L AT OVERHEAD BIN LOWER ATTACH POINT. REMOVED AND REPLACED FRAME SUPPORT BRACKETS IAW TR 53-10-20C, DEFECT SIZE: 1 INCH.

Part: FRAME — CRACKED (BS 480) · airframe 53,780 hrs · 53,780 cycles

FOUND FRAME CRACKED LT BODY STA 480. REMOVED AND REPLACED PSU BRACKET WITH FABRICATED PARTS IAW TR 53-10-20C, DEFECT SIZE: .250 INCH.

Part: CLIP — CRACKED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

FWD SIDE OF BS 294.5 AND STR 11L. REMOVED CRACKED CLIP, FABRICATED AND INSTALLED NEW CLIP IAW BOEING DWG 69-62054, DEFECT SIZE: .50 INCH.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

BS 312 FLOORBEAM CORRODED FROM RBL 8 TO RBL 36. MAJOR REPAIR SRM 53-10-51 FIG 201, REPAIR 5, DEFECT SIZE: .25 INCH.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

BS 907 AND STR 4R CRACKED. REMOVED OLD SPLICE AND DRILLED AND INSTALLED REPAIR PARTS IAW SRM 51-40-02, DEFECT SIZE: .50 INCH.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

AFT FACE OF E-1-3 RACK CENTER WEB CRACKED. REMOVED DAMAGED BRACKET, FABRICATED AND INSTALLED REPAIR PARTS BOEING DWG 69-42159, DEFECT SIZE: .50 INCH.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

STRINGER 15L AND BS 360 CRACKED. REMOVED AND REPLACED WITH NEW EXTENSION CHANNEL IAW DGW 65-61777, DEFECT SIZE: .25 INCH.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

AT 13L AND BS 360 CRACKED. REMOVED CRACKED ANGLE, REPLACED WITH NEW ANGLE IAW DWG 69-48204 AND SRM 51-10-02, DEFECT SIZE: .25 INCH.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

BS 360 S-14 LT. REMOVED AND REPLACED WITH NEW ANGLE IAW DWG 65-4566 AND SRM 51-10-02, DEFECT SIZE: .25 INCH.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

AFT FACE OF E-1-3 RACK CENTER WEB CRACKED. REMOVED DAMAGED BRACKET, FABRICATED AND INSTALLED REPAIR PARTS IAW BOEING DWG 69-42159, DEFECT SIZE: .25 INCH.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

FOUND FRAME CRACKED STA 847 BETWEEN S8R AND 9R. REPAIRED PER 53-10-20C DEFECT SIZE: .25".

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 53,780 hrs · 53,780 cycles

FOUND Z-ANGLE CORRODED STA 967-987 AT STR 17L. INSTALLED NEW Z ANGLE PER SRM 51-10-02, DEFECT SIZE: 2" BY 20".

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

FOUND ANGLE CRACKED INSIDE OF FRAME, 294.5 R AT S17R. INSTALLED NEW ANGLE IAW SRM 51-40-02, DEFECT SIZE: .25".

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

FOUND CRACK BS 343 AT STRINGER 11R. REMOVED FABRICATED AND INSTALLED TIE CLIP IAW BOEING DWG 69-38939-5 AND SRM 51-10-02, DEFECT SIZE: .025".

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

NR 2 VHF ANTENNA. REMOVE CORROSION , TREATED AND PAINTED IAW SRM 51-10-02. DEFECT SIZE: 6"X2"

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

NR 1 VHF ANTENNA. REMOVED CORROSION TREATED AND PAINTED IAW SRM 51-10-02. DEFECT SIZE: 6"X2"

Part: SKIN — CRACKED (L/E SLAT) · airframe 53,780 hrs · 53,780 cycles

LOWER SURFACE OF NR 6 SLAT, INBOARD END AT STOP PADS. REMOVED AFFECTED RIVETS, CUT OUT DAMAGE FABRICATED REPAIR PANEL AND INSTALLED IAW SRM 57-43-01 R-6. DEFECT SIZE: .250 INCH

Part: WEB — CRACKED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

BS 294.5 AND S12L WEB IS CRACKED. CUT OUT DAMAGED WEB, HFEC, FABRICATED REPLACEMENT PART AND INSTALLED IAW SRM 51-40-02. DEFECT SIZE: 1 INCH

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 53,780 hrs · 53,780 cycles

STA 957 RBL 18 TO RBL 44. REMOVED SURFACE CORROSION IAW SRM 51-10-02. DEFECT SIZE:

Part: PAN — CORRODED (FUSELAGE) · corrosion level 1 · airframe 53,780 hrs · 53,780 cycles

LEFT PAN STA 987 LBL 37 CORROSION AT NUT PLATE. BLENDED, ALODINED, PRIMED AND PAINTED IAW SRM 51-10-02. DEFECT SIZE: 1"X1.5"

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 53,780 hrs · 53,780 cycles

STA 984 AND STA967. REMOVED LIGHT CORROSION LESS THEN .002 IAW SRM 51-10-02. DEFECT SIZE: .002"

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 53,780 hrs · 53,780 cycles

T-CAP 967 CORROSION AT RBL 5 AND RBL 28. REPAIRED AND BLENDED LIGHT CORROSION IAW SRM 53-60-51. DEFECT SIZE: .002"

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 53,780 hrs · 53,780 cycles

STA 967 LBL28 TO LBL44. REMOVED LIGHT CORROSION LESS THEN .002 IAW SRM 53-60-51. DEFECT SIZE: .002

Part: WEB — CRACKED (FUSELAGE) · airframe 53,780 hrs · 53,780 cycles

BS 294.5 AND S16L CRACKED. REMOVED AND REPLACED WEB IAW SRM 51-10-02, DEFECT SIZE: .500 INCH.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 53,780 hrs · 53,780 cycles

STA 987 AND LBL 0 TO LBL 12 CORRODED. REMOVED LITE CORROSION LESS THAN .002, DEFECT SIZE: .002.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 53,780 hrs · 53,780 cycles

STA 98.7 RBL 2 TO RBL 36 CORROSION. REMOVED CORROSION IAW SRM 53-60-51, DEFECT SIZE: .002.

Part: LIGHT — MISSING (CABIN)

EMERGENCY EXIT LIGHT APPEARS TO BE MISSING OVER ROW 2 A/C LEFT. FOUND AND REPAIRED EMERGENCY EXIT LIGHT ASSY OVER ROW 2AC. OPS CHECK GOOD.

Part: SKIN — CHAFED (BS 860-882) · airframe 53,426 hrs · 53,426 cycles

FOUND STA 860-882 UNDER DORSAL FIN CHAFED. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 53-60-01, REPAIR 9 AND EA 97194, DEFECT SIZE:.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

CLT - PILOT REPORTED THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 5, 9 AND 11 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND REMOVED AND REPLACED LOW LEVEL LAMP AT SEAT ROW 5, LEFT SIDE. OPERATIONAL CHECK OF LIGHTS GOOD.

Part: FORGING — CRACKED (FUSELAGE)

CLT - C5 - FORGING, .3 INCH, CRACKED, FWD SERVICE DOOR CUTOUT UPPER FWD UPPER CORNER. REMOVED CRACKED REVEL AND REPLACED IAW DWG NR 65-55878. (K)

Part: WIRE — BROKEN (SEAT 19ABC)

PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 19ABC INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES. OPERATIONAL CHECK GOOD.

Part: WIRE — CHAFED (EMERGENCY LIGHT)

MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT ROWS 5 THROUGH 10 AND THE OVERWING EXIT IDENTIFIERS INOPERATIVE. MAINTENANCE FOUND POWER WIRE L7012A20 CHAFED TO STRUCTURE IN CEILING AREA. REMOVED DAMAGED WIRE SEGMENT AND RETERMINATED. ALSO, REPLACED FUSE (PN 21031-0005) IN FORWARD POWER SUPPLY. OPERATIONAL CHECK OF EMERGENCY LIGHTING NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS ON SEAT ROWS 5 THROUGH 10 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT POWER SUPPLY. OPS CHECK OF EMERGENCY LIGHTS GOOD. (M)

Part: CHARGER — FAILED (EMERGENCY LIGHT)

PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 5 THROUGH 10, INCLUDING THE ARROW SIGNS, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK, P/N 2013-1A AT BODY STATION 400. OPS CHECK NORMAL. (M)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

FOUND LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE CHARGER ASSEMBLY. (M)

Part: CSD — DISCONNECTED (NR 2 ENGINE)

ON CLIMB-OUT FROM FLL, EN ROUTE TO DCA, CREW REPORTED THE NR 2 ENGINE GENERATOR TRIPPED OFF LIE AS THE NR 2 CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CREW STARTED APU AND PLACED THE APU GENERATOR ON LINE. AT FL240, THE APU SHUTDOWN WITH THE FAULT LIGHT AND THE LOW OIL PRESSURE LIGHTS ILLUMINATING. THE APU FAILED TO RESTART ON FIRST ATTEMPT AT FL250. CREW BEGAN DIVERSION PROCEDURES. AT FL140, THE APU STARTED ON SECOND ATTMEPT BUT CREW STILL ELECTED TO DIVERT TO MIA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE CSD TO BE INADVERTENTLY DISCONNECTED IN FLL. RECONNECTED NR 2 ENGINE CSD AND CHECKED OIL LEVEL. RAN ENGINE. OPERATIONAL CHECK NORMAL PER MM. THE APU WAS PLACED ON MEL.

Part: BATTERY — INOPERATIVE (AFT CABIN)

IND - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY LIGHTS, ON SEAT ROWS 16 THROUGH 22, ARE DIM. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATOINAL CHECK GOOD. (M)

Part: SMOKE — DETECTED (CABIN)

AVP - FLT 9280 - UPON LANDING AND APPLYING REVERSE THRUST, CAPTAIN WAS ADVISED THE AFT CABIN AREA FILLED WITH SMOKE (LESS THAN 10 FEET VISIBILITY) AND THE REAR LAVATORY SMOKE DETECTOR WAS SOUNDING. SMOKE DISSIPATED AFTER COMING OUT OF REVERSE THRUST AND SHUTTING OFF AIR CONDITIONING PACKS. AIRCRAFT TAXIED TO THE GATE ON ITS OWN POWER. MAINTENANCE INSPECTED INTAKE AND EXHAUST OF BOTH ENGINES. RAN BOTH PACKS USING RESPECTIVE ENGINE BLEEDS. OPERATED THRUST REVERSERS WITH PACKS RUNNING. NO EVIDENCE OF SMOKE OR SMELL IN THE CABIN OR COCKPIT. SUSPECT UREA INGESTION DURING LANDING USED FOR RUNWAY DEICING. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

PIT - FOUND SKIN CRACKED 15 INCHES BY 20 INCHES, STATION 178 BULKHEAD 7.50 RBL - 2.50 LBL, 217WL - 192WL. REPAIRED PER EO 5300V153, DOUBLER INSTALLED. (M)

Part: SKIN — CRACKED (FUSELAGE)

PIT - FOUND SKIN CRACKED 23 INCHES BY 22.5 INCHES EXIT DOUBLER, FS 294.5 STRINGER 28L-28R. DOUBLER INSTALLED PART OF EO FOR TCAS ANTENNA INSTALL PER EO 5389X717. (M)

Part: FLAP TRACK — CORRODED (T/E FLAP)

PIT - FOUND FLAP TRACK CORRODED 2 INCHES BY 3 INCH PITTING CORROSION, NR 1 FLAP TRACK, TOP AFT SECTION. CORROSION LEVEL 1. TRACK REPLACED PER EO 5796X180. (M)

Part: STRINGER — CORRODED (FUSELAGE)

PIT - FOUND STRINGER CORRODED 1 INCH BY 2 INCH, FS 325.9 AND S28R. REPLACED STRINGER PER SRM 53-00-03 FIG 201. (M)

Part: FLAP TRACK — CORRODED (T/E FLAP)

PIT - FOUND FLAP TRACK WITH PITTING CORROSION 2 INCHES BY 3 INCHES, NR 3 FLAP TRACK, TOP AFT SECTION. TRACK REPLACED PER EO 5796X180. (M)

Part: FLAP TRACK — CORRODED (T/E FLAP)

PIT - FOUND FLAP TRACK CORRODED 3 AREAS, 1 INCH BY .5 INCH, ALL FLAP TRACK ROLLER CONTACT AREAS, NR 2 FLAP TRACK. REPLACED FLAP TRACK PER EO 5796X180. (M)

Part: FLAP TRACK — CORRODED (T/E FLAP)

PIT - FOUND FLAP TRACK CORRODED, NR 1 FLAP TRACK ROLLER CONTACT AREA. CORROSION LEVEL 1. REPLACED FLAP TRACK PER EO 5796X180. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2

PIT - FOUND FLOOR SUPPORT/BEAM CORRODED 8 INCHES LONG, LEFT AFT SIDE NOSE GEAR STATION 270 BL 0 WL 217 FLOORBEAM. CORROSION LEVEL 2. INSTALLED DOUBLERS AND REPAIR ANGLES PER TYPICAL REP 53-20-08 AND EA 73795. (M)

Part: SKIN — WORN (RUDDER)

PIT - FOUND LEADING EDGE RUDDER WORN, 1 INCH BY .25 INCH, 3 LAYERS DEEP, LE L00 SIDE, 95 INCHES FROM TOP RUDDER AND 29 INCHES FROM TRAILING EDGE. REPAIR PER EA 73763. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PHL - MAINTENANCE REPORTED THE MID CABIN CEILING EMERGENCY EXIT LIGHT, RIGHT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)

Part: CIRCUIT BREAKER — FAULTY (FLT COMPT)

EWR - FLT 432 - IN PREPARATION FOR LANDING AT EWR, FROM PIT, CREW RECEIVED A RED NOSE GEAR UNSAFE LIGHT WITHOUT ANY GEAR INDICATIONS. CREW CHECKED CIRCUIT BREAKERS AND ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES. CREW RECYCLED GEAR BUT STILL ONLY THE RED NOSE GEAR UNSAFE LIGHT ILLUMINATED WITH NO OTHER LIGHTS. A/C WENT INTO HOLDING PATTERN TO TROUBLESHOOT AND MANUALLY DEPLOY THE GEAR. CREW RECHECKED CIRCUIT BREAKERS AND FOUND THE AIR/GROUND RELAY AND LIGHTS CIRCUIT BREAKER PARTIALLY POPPED (NO WHITE SHOWING). CREW RESET CIRCUIT BREAKER AND RECEIVED THREE GEAR GREEN LIGHTS. CREW RECYCLED GEAR AND FOUND OPERATION/INDICATION NORMAL. FLIGHT PROCEEDED AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECL

Part: FLAP — MALFUNCTIONED (WINGS)

ROC - FLT 582 - ON DESCENT INTO ROC FROM LGA, AT APPROXIMATELY 3,000 FEET, THE FLAP POSITION INDICATOR SHOWED A FLAP DISAGREEMENT AND THE TRAILING EDGE FLAP INDICATOR CIRCUIT BREAKER WAS POPPED. CREW ACCOMPLISHED A ZERO FLAPS LANDING AT ROC WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE TRAILING CIRCUIT BREAKER AND PERFORMED OPERATIONAL CHECK OF THE FLAPS SEVERAL TIMES. NO DEFECTS NOTED. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ROC - DURING OVERNIGHT CHECK, MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN MID/AFT AISLE BULLNOSE AREA AND EXTERIOR AFT OVERWING AREA INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN M1136 POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)

Part: HEAT EXCHANGER — FAILED (NR 1 ENGINE)

DEN - FLT 8052 - UPON CLIMB-OUT, JUST BEFORE LEVEL OFF AT FL 290, CREW WAS ALERTED TO HIGH OIL TEMPERATURE ALONG WITH A BURNING SEMLL ON THE NR 1 ENGINE. CREW ACCOMPLISHED CHECKLIST, DECLARED AN EMERGENCY AND INITIATED PROCEDURES IN SHUTTING DOWN THE NR 1 ENGINE AFTER THREE MINUTES AT IDLE. FLIGHT RETURNED TO FIELD AT DEN AND LANDED WITHOUT INCIDENT. AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. TOTAL SINGLE ENGINE TIME WAS ESTIMATED AT EIGHT TO TEN MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE FUEL/OIL HEAT EXCHANGER. RAN ENGINE AT HIGH POWER FOR TEN MINUTES. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M)

Part: FLOORBEAM — CORROSION (BS 967)

CLT - DURING Q-1 VISUAL CHECK INSPECTION, FOUND CORROSION AROUND THE NUTPLATE HOLES STATION 967 FLOORBEAM LBL 56, RBL 56 T-CAP. CORROSION CARD NR C53-107-02. INSTALLED NEW T-CAP PER REPAIR DOCUMENT 53-10-05. (M)

Part: STRUCTURE — CORRODED (BS 986.5)

CLT - DURING Q-1 VISUAL CHECK INSPECTION, FOUND .5 INCH BY .5 INCH AREA OF CORROSION BS 986.5 LBL 56 TO RBL 56 BEAM. CORROSION CARD NR C53-107-02. INSTALLED NEW T-CAP PER REPAIR DOCUMENT 53-10-05. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ALB - MAINTENANCE FOUND THE FOLLOWING EVACUATION/EXIT LIGHTS INOP. EVACUATION LIGHTS AT ROW 5 LEFT SIDE AND ROW 7 BULLNOSE, INSIDE LEFT EXIT OVERWING HATCH AND OVERWING ILLUMINATION LIGHTS ON THE LEFT SIDE. MAINTENANCE REMOVED AND REPLCED THE BATTERY PACK. OPS CHECK GOOD. (M)

Part: STRAP — OUT OF POSITION (SERVICE DOOR)

CLT - FL 1635 - CAPTAIN CONTACTED DISPATCH AND INDICATED HE NEEDED TO DIVERT DUE TO AN AFT SERVICE DOOR RESTRAINING STRAP CAUGHT OUTSIDE THE DOOR AND BANGING AGAINST THE FUSELAGE. DECISION WAS MADE TO DIVERT TO CLT. FLGHT LANDED WITHOUT FURHTER INCIDENT. MAINTENANCE PROPERLY STOWED STRAP AND CHECKED THE AFT SERVICE DOOR FOR SIGNS OF DAMAGE. NO DAMAGE NOTED. (M)

Part: AIR SENSING CARD — FAILED (NLG WW)

DCA - FLT 1764 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION. FLIGHT RETURNED TO FIELD AT DCA. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE RESET THE LATCH AND CIRCUIT BREAKER AND REPLACED THE AIR SENSING SQUAT SWITCH CARD M991. PERFORMED INTEGRITY CHECK ON GEAR HANDLE SYSTEM. OPS CHECK GOOD. (M)