N334US

Part: SKIN — CRACKED (BS 727E) · airframe 54,281 hrs · 54,281 cycles

BS 727E -10 S-18R CRACKED. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 201, REPAIR 31 DEFECT SIZE: 3.25 INCH.

Part: SKIN — CRACKED (BS727) · airframe 54,281 hrs · 54,281 cycles

BS 727 S19R CRACKED. INSTALLED DOUBLER IAW 53-00-01 FIG 201, DEFECT SIZE: 1.35 INCH.

Part: INDICATOR — FAULTY (TE FLAPS)

DFW FLT1262 - DURING FINAL APPROACH TO DFW, CREW SELECTED FLAPS FROM 15 TO 25 UNITS AND NOTICED A DEVELOPING SPLIT IN THE LEFT AND RIGHT FLAP POINTERS. AT 25 UNITS, THERE WAS A NOTICEABLE SPLIT BUT NO APPARENT AIRCRAFT ROLL. CREW EXECUTED A GO-AROUND AND LANDED WITH FLAPS 15 WITHOUT FURTHER INCIDENT. SUBSEQUENT TEST AT THE GATE SHOWED THE FLAPS GOING TO 25 UNITS WITH A 3 TO 4 SPLIT, THEN 30 UNITS WITH NO SPLIT AND 40 UNITS WITH NO SPLIT. MAINTENANCE FOUND THE FLAP POSITION INDICATOR FAULTY. REPLACED INDICATOR PER MM 27-51-00 AND 27-58-01. OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (BS 727D) · airframe 54,047 hrs · 40,823 cycles

1-7/8 INCH CRACK AT BS 727D AND STRINGER 3L. REMOVED DAMAGED SKIN AND REPAIRED PER SRM 53-00-01.

Part: SKIN — CRACKED (FUSLAGE) · airframe 53,600 hrs · 40,490 cycles

A 1.5 INCH CRACK IN SKIN AND HOLE IN STRINGER 22R AT STA 727E, STR 22R. INSTALLED DOUBLER ON SKIN AND STRINGER PER SRM 53-00-01 FIG 229, DET 19 AND 53-00-03 FIG 201.

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND FUSELAGE SKIN CRACKED 1.2 INCH, STRINGER 18R AT STATION 749. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. (M)

Part: LUG — WORN (BEARING)

PIT - FOUND BEAR LUG WORN, BEARING LUG BORE WORN INSIDE DIAMETER SURFACE .75 INCH. ROTO PEENED BORE ID PER TYPE REPAIR 54-50-09 REV C. (M)

Part: SKIN — CRACKED (FUSLEAGE)

FOUND SKIN CRACKED 1 INCH, EXTERNAL FUSELAGE SKIN STATION 727D PLUS 2 AT STRINGER 19R. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)

Part: SKIN — CRACKED (FUSELAGE)

FOUND SKIN CRACKED 1.5 INCH, EXTERNAL FUSELAGE SKIN STATION 765 STRINGER 23R. INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 229. (M)

Part: CONTROLLER — OVERHEATED (OVEN TEMP)

EN ROUTE FROM CLT TO DFW, CREW REPORTED AN ELECTRICAL BURNING ODOR IN FORWARD GALLEY. OVEN, CONTROLLER AND BACKWALL OF GALLEY WAS HOT. TURNING OFF GALLEY POWER APPEARED TO BE OF SOME HELP. FLIGHT LANDED AT DFW WITHOUT FURTHER INCIDENT. MAINTENANCE IN DFW PULLED OVEN CONTROL UNIT AND FOUND UNIT TO SMELL BURNED. OPERATED GALLEY LIGHTS. NO TROUBLE FOUND. PULLED AND COLLARED OVEN AND COFFEEMAKER CIRCUIT BREAKERS. RELEASED AIRCRAFT ON MEL 25-10. THREE DAYS LATER, ON OCTOBER 13TH IN PHL, CREW REPORTED FEELING HEAT AND DETECTING ODOR IN FORWARD GALLEY AGAIN. APPEARS TO BE COMING FROM OVEN CONTROL PANEL. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY OVEN TEMP CONTROLLER. OPS CHECK GOOD. CLEARED MEL 25

Part: LIGHT — INOPERATIVE (SEAT 10)

FOUND EMERGENCY EXIT LIGHT AT SEAT 10 ABC INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

PIT - FOUND RIGHT KEEL BEAM FORWARD OF STATION 520, WITH CORROSION 1 INCH BY 6 INCHES. CORROSION LEVEL 1, TASK NR C53-20-01. REPLACED KEEL BEAM SECTION FROM STATION 540-500 PER TYPICAL REPAIR MANUAL 53-60-09. (M)

Part: SKIN — CORRODED (FUSELAGE)

FOUND SKIN CORRODED 2 INCHES BY 1 INCH, STATION 500C PLUS 17 INCHES AT S-27R. CORROSION LEVEL 1, TASK NR C53-208-01. REMOVED RIVETS, BLENDED CORROSION, TREATED, PRIMED, PAINTED PER SRM 53-00-01 AND 53-30-01. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PIT - FOUND Z-ANGLE WITH 3 AREAS OF CORROSION, RIGHT CREASE BEAM INNER CHORD Z-STATION 947.5-986.5 PLUS 8 INCHES, 3 INCH BY 2 INCH, 2 INCHES BY 2 INCHES, 4 INCHES BY 2 INCHES. REPLACED Z-ANGLE PER SRM 53-60-15. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PIT - FOUND RIGHT CREASE BEAM INNER CHORD Z-STATION 947.5 TO 986.5 PLUS 8 INCHES, WITH THREE CORRODED AREAS OF CORROSION, 3 INCHES BY 2 INCHES, 2 INCHES BY 2 INCHES, 4 INCHES BY 2 INCHES. REPLACED Z-ANGLE PER SRM 53-60-15. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

FOUND KEELBEAM CORRODED 1 INCH BY 3 INCH AREA, FS 727 LEFT KEELBEAM. CORROSION LEVEL 1, TASK NR C53-208-01. REPLACED LEFT KEELBEAM PER TYP REPAIR 53-60-09. (M)

Part: STIFFENER — CORRODED (FUSELAGE)

PIT - FOUND STIFFENER CORRODED 2 INCHES BY 6 INCHES, STATION 1016 AT BL 0 BETWEEN PRESSURE WEB AND CHANNEL STIFFENER. KIT NR 65C28106-1 AND 65C28106-16 REPAIRED PER EO 5302V112 REV A. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

FOUND LT KEELBEAM CORRODED LOWER CHORD INBOARD SURFACE STATION 727, 1.5 INCHE LONG .050 INCH - .070 INCH DEEP. KEELBEAM INSTALLED WITH SPLICE AT STATION 540 PER TYPICAL REPAIR 53-60-09. (M)

Part: SKIN — CRACKED (PAX DOOR)

PIT - FOUND DOOR SKIN CRACKED .5 INCH LONG, MED INTERIOR EDGE OF INNER SKIN, 4TH STOP PAD SCREW HOLE. DOUBLER INSTALLED PER EA 76491. (M)

Part: PAN — CRACKED (DOOR)

FOUND DOOR PAN CRACKED .5 INCH LONG, MED DOOR PAN CRACKED AFT SIDE. DOUBLER INSTALLED PER 52-10-02/51-70-11. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

FOUND CARGO TRACK CORRODED .5 INCH BY 2 INCHES, AFT CARGO STATION 807 2 INCHES S-26R TIE DOWN TRACK. CARGO TRACK REPAIR PER SRM 53-10-53 FIG 202. (M)

Part: PRESSURE PANEL — CRACKED (FUSELAGE)

FOUND TWO CRACKS IN WEB 1 INCH EACH, PRESSURE WEB AT STATION 665 RBL 40. DOUBLERS AND FILLERS INSTALLED AT CUTOUT OF WEB PER TYP REP 53-60-04. (M)

Part: KEELBEAM — CORRODED (FUSELAGE)

FOUND LT KEEL BEAM WITH EXFOLIATION CORROSION 3 INCHES LONG BY 1 INCH WIDE, FS 500 C PLUS 18 INCHES. CORROSION LEVEL 2, TASK NR C53-208-01. INSTALLED KIT NR 65C28106-1 AND 65C28106-16 PER EO 5302V112 REV A. (M)

Part: BULKHEAD — CORRODED (FUSELAGE)

FOUND WEB CORRODED, 12 INCHES BY 6 INCHES, AFT PRESS BULKHEAD STATION 1016 LBL 4 INCHES-RBL 4 INCHS. MODIFIED PART NR INSTALLED, KIT NR 65C28106-1 AND 65C28106-16 PER EO 5302V112, REV A. (M)

Part: FRAME — CRACKED (FUSELAGE)

PIT - FOUND FRAME CRACKED 4 INCHES, STATION 500 BETWEEN STRINGER 26L-26R. INSTALLED TWO DOUBLERS PER SRM 51-70-11 FIG 1, DETAIL NR 2, PAGE 6. (M)

Part: SWITCH — FAILED (MLG)

UPON APPROACH INTO PWM, WITH GEAR HANDLE DOWN, CREW RECEIVED A RED NOSE LANDING GEAR UNSAFE LIGHT ALONG WITH ALL THREE GREEN GEAR DOWN AND LOCKED LIGHTS. CREW DECLARED AN EMERGENCY AND MANUALLY LOWERED THE NOSE LANDING GEAR. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE ACCOMPLISHED LANDING GEAR POSITION AND WARNING SYSTEM TROUBLESHOOTING PER MM 32-61-00 AND WD 32-64-01. REMOVED AND REPLACED LANDING GEAR LEVER POSITION SWITCH S78 PER MM 32-61-11. ALSO, REMOVED AND REPLACED NOSE GEAR LATCHING RELAY R374 (P/N BR20AXH5V3) AND PRINTED CIRCUIT CARD M983 (P/N 65-58250-29), AS PRECAUTIONARY, PER MM. JACKED AND OPERATIONALLY CHECKED NOSE LANDING GEAR RETRACTION AND EXTENSION SYSTEMS.

Part: SOCKET — DEFECTIVE (CABIN)

IND - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT 13ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD. (M)

Part: WIRE — BROKEN (CABIN)

PHL - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 22C INOPERATIVE. MAINTENANCE REPAIRED DAMAGED/BROKEN WIRE AT SEAT 22C. OPERATIONAL CHECK GOOD. (M)

Part: SKIN — CRACKED (FUSELAGE)

SKIN, 2.8 INCH CRACK, RIGHT SIDE STA 727E AT STR 23 RIGHT. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE)

SKIN, RIGHT SIDE STA 727E AT STR 23 RT, CRACKED. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER IAW SRM.

Part: CHARGER — FAILED (CABIN)

IND - MAINTENANCE FOUND THE EMERGENCY LIGHTS FROM SEAT ROW 5 THROUGH THE OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)

Part: WIRE — BROKEN (CABIN)

MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ON SEAT ROW 6, LEFT SIDE, INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE)

TPA - FOUND SKIN CRACKED .5 INCH, APPROXIMATE STATION 960 BETWEEN STRINGER 14 AND 15 RIGHT. REPAIRED FOB DOUBLER, FILLER, TRIPLER, FASTENERS FRO SRM 53-60-01 FIG 207. (M)

Part: BUNGEE CORD — DAMAGED (CARGO DOOR)

IND - FLT 461 - EN ROUTE FROM CLT-ORD, AT FL240, THE CABIN ALTITUDE WARNING HORN ACTIVATED AS CABIN ALTITUDE WAS AT 10,000 FT AND CLIMBING. STANDBY PRESSURIZATION WOULD NOT CONTROL CABIN AND SELECTING MANUAL SHOWED OUTFLOW VALVE FULL CLOSED. CREW SELECTED BOTH PACKS WITH ISOLATION VALVE OPEN AND CABIN STOPPED CLIMBING. FLIGHT DIVERTED TO IND AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED AND NO OXYGEN MASKS WERE DEPLOYED. MAINTENANCE FOUND THE AFT CARGO DOOR RELEASE BUNGEE LANYARD CAUGHT IN THE DOOR SEAL. REPAIRED BUNGEE LANYARD AND CHECKED DOOR AND SEAL FOR DAMAGE. NO DAMAGE FOUND. PERFORMED SINGLE PACK CONFIDENCE CHECK PER MM 21-00-05. CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULKHEAD — DENTED (FUSELAGE)

CLT - FOUND BULKHEAD WEB DENTED 3 INCHES BY .5 INCH, BS 1016 WL 156, RBL 51. DAMAGED REMOVED, INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-80-08, FIG 201. (M)

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND FUSELAGE SKIN CRACKED APPROXIMATELY .1875 INCH, BS 887, STRINGER 23R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLE WITH FILLER PER SRM 53-00-01, FIG 227. (M)

Part: SKIN — CRACKED (FUSELAGE)

CLT - FOUND CUT OUT FOR A/C HOOK CRACKED .25 INCH, AIR CONDITION GROUND CONNECTION STATION 527 STRINGER 28L. MANF STRAP .0637075T-6 AND FILLED .125 2024T-3 PER EA 66651. (M)

Part: CHARGER — FAILED (CABIN)

ALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 5 THROUGH 12 AND AT THE OVERWING. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N AD2013-1A) AND CHARGER ASSY. OPERATIONAL CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PVD - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

BOS - WHILE ACCOMPLISHING A-CHECK, MAINTENANCE FOUND THE FOLLOWING EMERGENCY LIGHTS INOPERATIVE, L1 DOOR EXTERIOR LIGHT, LEFT OVERWING EXTERIOR LIGHT, LEFT CABIN BULLNOSE LIGHTS AT SEAT ROWS 5 AND 9, LEFT CAIBN ESCAPE PATH LIGHTS AT SEAT ROWS 5 THROUGH 9 AND THE LEFT AND RIGHT CABIN ESCAPE ROW MARKER LIGHT. MAINTENANCE REMOVED AND REPLACED THE M1135 BATTERY PACK FOR ALL LIGHTS EXCEPT THE L1 DOOR EXTERIOR LIGHT. RELAMPED L1 DOOR EXTERIOR LIGHT. OPERATIONAL CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PHL - MAINTENANCE FOUND THE MID CABIN EMERGENCY LIGHTS INOPERTIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)

Part: DUCT — FAILED (COCKPIT)

PIT - FLT 1840 - AFTER PASSING 7,000 FT, A VERY LOUD BANG OCCURRED FROM BEHIND THE INSTRUMENT PANEL. HIGH PRESSURE AIR RUSHED OUT AND BLEW INSULATION THROUGH OUT THE COCKPIT. COCKPIT WAS VERY LOUD. AUTOPILOT OPERATION WAS AFFECTED AND HAD TO BE TAKEN OFF LINE. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE VISUALLY INSPECTED THE COCKPIT EXTERIOR FOR DAMAGE. NO DAMAGE WAS FOUND. PERFORMED PITOT CHECK OF PITOT SYSTEM. ALL CHECKS NORMAL. PRESSURIZED AIRCRAFT TO 3.5 PSI. NO LEAKS NOTED. INSPECTED AREA BEHIND INSTRUMENT PANEL AND FOUND THE COCKPIT AIR CONDITIONING SPLITTER DUCT CRACKED. REMOVED AND REPLACED DUCT ASSEMBLY. LEAK CHE

Part: LINE — LEAKING ('B' HYD SYSTEM)

PIT - FLT 1628 - AFTER CLIMB FROM PHL AT FL330, AIRCRAFT EXPERIENCED A COMPLETE FAILURE OF SYSTEM 'B' HYDRAULICS. CREW REPORTED ZERO PRESSURE AND QUANTITY. THE 'B' SYSTEM PUMPS WERE TURNED OFF WITHIN TWO MINUTES OF LOW PRESSURE LIGHTS. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. AIRCRAFT TAXIED TO THE GATE ON ITS POWER. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND A HYDRAULIC LINE IN THE MAIN LANDING GEAR WHEEL WELL LEAKING. REPLACE HYDRAULIC LINE. ALSO, REPLACED NR 2 ENGINE HYDRAULIC PUMP AND ALL HYDRAULIC SYSTEM FILTERS. SERVICED HYDRAULIC TO FULL. RAN ENGINE AND HYDRAULIC SYSTEM. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M)

Part: TIE CLIP — CRACKED (BS 727)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 7L, AT STATION 727D. REPLACED PART PER SRM 51-10-02. (M)

Part: TIE CLIP — CRACKED (BS 727)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 4R, STRINGER 5R AT BS 727B. REPLACED PART PER SRM 51-10-02. (M)

Part: CHANNEL — CRACKED (BS 520)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .20 CRACK AND CORROSION BS 520 VHF NR 2 COMM ANTENNA MOUNT CHANNEL. REMOVED AND REPLACED CHANNEL PER SB 737-53-1159 FIG 1 STEP 1. (M)

Part: FLOORBEAM — CRACKED (BS 520)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH LONG CRACK IN FLOORBEAM STATION 520 RBL 25. INSTALLED DOUBLERS AND FILLERS PER SB 737-53-1120 FIG 28 EA 63326. (M)

Part: ANGLE — CRACKED (BS 616)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .10 INCH CRACK AT LOWER FAST OF INNER CHORD ANGLE BS 616 WL 201 LT SIDE. REPAIRED PER TR 53-10-23 AND EA 63358 INSTALLED FILLER AND DOUBLER. (M)

Part: FLOORBEAM — CRACKED (BS 520)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .20 INCH CRACK STATION 520 LBL 25 FLOORBEAM. INSTALLED DOUBLER AND REPAIR ANGLES PER EA 63326, SB 737-53-1120. (M)

Part: TIE CLIP — CRACKED (BS 727)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 7L BS 727D. REPAIRED PER SRM 51-10-02. (M)

Part: STRINGER — CRACKED (BS 908)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .10 INCH CRACK BETWEEN RIVETS BS 908 STRINGER 4L. INSTALLED NEW TIE CLIP PER SRM 51-10-00. (M)

Part: FRAME — CORRODED (BS 500)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 6 INCH BY 6 INCH AREA OF CORROSION AT STRINGER 27L BS 500D CARGO FLOOR LEVEL FRAME. CORROSION TASK NR C 53-208-01. FABRICATED REPAIR PER SRM 53-00-07. (M)

Part: TIE CLIP — CRACKED (BS 597)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 16L, AT BS 597. REPLACED PART PER SRM 51-10-02. (M)

Part: TIE CLIP — CRACKED (BS 727E)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 5R STRINGER 7R AT BS 727E. REPAIRED PER SRM 51-10-02. (M)

Part: TIE CLIP — CRACKED (BS 727C)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 4R, STRINGER 5R, STRINGER 6R AND STRINGER 7R BS 727C. REPAIRED PER SRM 51-10-02. (M)

Part: TIE CLIP — CRACKED (BS 727B)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 4R BS 727B. REPAIRED PER SRM 51-10-02. (M)

Part: TIE CLIP — CRACKED (BS 727)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 7L, STRINGER 8L BS 727B. REPAIRED PER SRM 51-10-02. (M)

Part: TIE CLIP — CRACK (BS 727A)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 8R BS 727A. REPAIRED PER SRM 51-10-02. (M)

Part: FLOORBEAM — CRACKED (BS 520)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH LONG CRACK IN FLOORBEAM STATION 520 RBL 45. INSTALLED DOUBLERS AND FILLERS PER SB 737-53-1120 AND EA 63326. (M)

Part: STRINGER — CRACKED (BS 908)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STRINGER SPLICE BS 908 STRINGER 4R. INSTALLED NEW SPLICE PER SRM 51-10-02 AND 51-40-02. (M)

Part: BULKHEAD CHORD — CRACKED (BS 727)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK STATION 727 LBL 29 WL 153.5 BULKHEAD LOWER PRIMARY CHORD. INSTALLED REPAIR DOUBLER ANGLE, FILLER AND VERTICAL STIFFENER PER EA 63469. (M)

Part: TIE CLIP — CRACKED (BS 616)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 4L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-00. (M)

Part: SKIN — CRACKED (BS 380)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AFT EDGE OF EQUIPMENT COOLING DUCT STATION 380 FUSELAGE SKIN. INSTALLED EXTERNAL DOUBLER PER BOEING DRAWING 65C33930. (M)

Part: STRINGER — CRACKED (BS 908)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BETWEEN RIVETS BS 908 STRINGER 4R. INSTALLED NEW TIE CLIP PER SRM 51-10-00. (M)

Part: TIE CLIP — CRACKED (BS 727B)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 5R BS 727B. REPAIRED PER SRM 51-10-02. (M)

Part: TIE CLIP — CRACKED (BS 639)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN TIE CLIP BS 639 STRINGER 4L. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)

Part: TIE CLIP — CRACKED (BS 727)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP BS 727A STRINGER 2L. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)

Part: SHEAR TIE — CRACKED (BS 948)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STATION 948 STRINGER 27R SHEAR TIE. REMOVED AND REPLACED PER SRM 51-10-02. (M)

Part: TIE CLIP — CRACKED (BS 727)

CLT - DURNIG Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP BS 727C STRINGER 6L, STRINGER 7L, STRINGER 8L. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)

Part: TIE CLIP — CRACKED (BS 639)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN TIE CLIP STRINGER 4R AT BS 639. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)

Part: ANGLE — CRACKED (BS 616)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .10 INCH CRACK AT LOWER FASTENER OF INNER CHORD ANGLE BS 616 WL 201 RT SIDE. REPAIRED PER TR 53-10-23 AND EA 63358 INSTALLED FILLER AND DOUBLER. (M)

Part: TIE CLIP — CRACK (BS 727)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 5R AT BS 727D. REPAIRED PER SRM 51-10-02. (M)

Part: TIE CLIP — CRACKED (BS 727)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN TIE CLIP STRINGER 8R, AT BS 727A. REPLACED PART PER SRM 51-10-02. (M)

Part: FLOORBEAM — CRACKED (BS 520)

CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 1 INCH LONG CRACK IN FLOORBEAM STATION 520 LBL 45. INSTALLED DOUBLERS AND FILLERS PER S/ 737-53-1120 EA 63326. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PHL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT ROWS 4ABC THROUGH 9ABC INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN OVERHEAD AT ROW 10ABC. OPS CHECK GOOD. (M)

Part: ACM — FAILED (RT AIR COND BAY)

PIT - FL 358 - EN ROUTE FROM DCA TO MCI AT FL 350, ALTITUDE WARNING HORN SOUNDED. NO OTHER COCKPIT INDICATIONS WERE ILLUMINATED. COCKPIT CABIN INDICATOR SHOWED CABIN AT 10,000 FEET AND RISING. EMERGENCY DESCENT WAS MADE AND THE FLIGHT DIVERTED TO PIT. DEPLOYMENT OF OXYGEN MASKS WAS NOT NECESSARY. THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT AIR CYCLE MACHINE. OPS CHECK AND LEAK CHECK OK. (M)

Part: BATTERY PACK — DISCHARGED (BS 634)

FLT NR 1191 - PHL - MAINTENANCE FOUND L2 DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP. MAINTENANCE REPLACED THE BATTERY PACK. (M)

Part: HYD PUMP — FAILED (NR 2 ENGINE)

IND - FLIGHT NR 0133 - RIGHT ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED AND B-SYSTEM HYDRAULIC QUANTITY DROPPED TO ONE QUARTER. FLIGHT DIVERTED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND SERVICED HYDRAULICS. OPS/LEAK CHECKED GOOD. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

LGA - THE INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTING BATTERY PACK FOR ROW 12 TO 16. OPERATIONS CHECKED GOOD. (M)

Part: DOOR — AJAR (CARGO COMPT)

PHL - FLT NR 1487 - RETURN TO FIELD DUE TO THE AFT CARGO DOOR LIGHT ILLUMINATING. MAINTENANCE FOUND THE REAR CARGO DOOR AJAR. VISUAL AND MECHANICAL INSPECTION CHECKS GOOD. NO DEFECTS OR LIGHT MALFUNCTION NOTED. (M)

Part: INTERCOSTAL — CORROSION (BS 312 - 328)

INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 16 INCH CORROSION BS 312 TO BS 328 RBL 12. REPLACED WITH PREFAB INTERCOSTAL SRM 51-10-01. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)

Part: SUPPORT — CORRODED (BS 986.5 - 1006)

INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 CORRODED SCREW HOLES RT AFT LAVATORY FLOOR SUPPORT BS 986.5 PLUS 7 INCHES TO 1006 36 INCHES RBL. FABRICATED NEW SUPPORT SRM 51-10-02 PG 15. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)

Part: INTERCOSTAL — CORROSION (BS 967 - 986.5)

INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND INTERCOSTAL, 3 SCREW HOLES CORRODED BS 967 TO 986.5 18 INCHES LBL. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL, SRM 51-10-02 PG 15. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)

Part: SEAT TRACK — CORROSION (BS 360)

INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION 1 INCH BY 2 INCH SEAT TRACK AT STA 360 RBL 54. FABRICATED NEW SEAT TRACK SRM 51-10-02 PG 15. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)

Part: KEEL BEAM — CORRODED (BS 506)

INT - DURING Q-5 CHECK INSPECTION, FOUND 1 INCH SQ CORRODED AREA S28R RT KEEL BEAM STA 506 O/B SIDE. INSTALLED REPAIR ANGLE EA 39374. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (W)

Part: SUPPORT — CORRODED (986.5)

INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 4 CORRODED SCREW HOLES, RT AFT LAVATORY FLOOR SUPPORT BS 986.5 PLUS 7 INCHES TO 1006 13 INCHES RBL. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW ONE, SRM 51-10-02 PG 15. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)

Part: INTERCOSTAL — CORRODED (BS 986.5 - 1006)

INT - DURING Q-5 CHECK INSPECTION, FOUND INTERCOSTAL, 2 CORRODED SCREW HOLES BS 986.5 TO BS 1006 13 INCHES LBL. FABRICATED NEW INTERCOSTAL SRM 51-10-02 PG 15. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)

Part: SEAT TRACK — CORRODED (BS 340)

INT - DURING Q-5 VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION .5 INCH BY 2 INCH, SEAT TRACK STA 340 RBL 45. INSTALLED NEW SECTION OF SEAT TRACK SRM 53-00-52 FIG 202. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)

Part: FLOOR PAN — CORRODED (BS 1016)

INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 10 INCHES BY 10 INCHES CORROSION AREA ON FLOOR PAN AT LT LAVATORY DUMP CHUTE CUTOUT BS 1016 LBL 5. INSTALLED WEB SKIN REPAIR SRM 51-70-13 FIG 1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)

Part: FLOORBEAM — CORRODED (BS 986.5)

INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORRODED SCREW HOLE FLOORBEAM BS 986.5, 43 INCHES LBL. INSTALLED UPPER T-CAP REPAIR, ENTIRE LENGTH TR 53-10-05. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)

Part: SUPPORT — CORRODED (BS 1006-1016)

INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 3 INCH AND 1 INCH BY 6 INCH AREA CORRODED TOP OF FLOOR SUPPORT BS 1006 TO 1016, 36 INCHES LBL. FABRICATED NEW WEB AND SUPPORT ANGLE, SRM 51-10-1, SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)

Part: SHIM — CORROSION (FWD BULKHEAD)

INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SHIM AT I/B END OF AFT LT LAVATORY FORWARD BULKHEAD WALL SUPPORT HAS CORRODED SCREW HOLE. INSTALLED NEW INTERCOSTAL/SHIM. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)

Part: INTERCOSTAL — CORRODED (BS 1006-1016)

INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORRODED AREA AND 2 CORRODED SCREW HOLES AFT LT LAVATORY DOORWAY, BS 1006 TO 1016. INSTALLED NEW INTERCOSTAL SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)

Part: SUPPORT — CORRODED (BS 1006 - 1016)

INT - DURING Q-5 CHECK INSPECTION, FOUND 2 INCHES BY 6 INCHES CORRODED AREA, BS 1006 TO 1016 RT AFT LAVATORY DOORWAY FLOOR SUPPORT. INSTALLED NEW INTERCOSTAL SUPPORT SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W)

Part: DOOR — NOT LOCKED (E/E BAY)

MCO - FLT 682 - UNABLE TO PRESSURIZE ACFT AFTER TAKEOFF. FLIGHT RETURNED TO MCO WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE FOUND FWD ELECTRICS BY DOOR UNLATCHED. CLOSED AND SECURED DOOR. SYSTEM CHECKS NORMAL. (W)