N12322

Part: ANGLE — CORRODED (R1 DOOR) · airframe 68,580 hrs · 31,195 cycles

R-1 DOOR Z ANGLE HAS CORROSION STA 296. INSTALLED NEW Z ANGLE PER SRM 51-40-02.

Part: STRINGER — CORRODED (BS 357 S23R) · airframe 68,580 hrs · 31,195 cycles

CORROSION AT STA 357 STRINGER 23R REPAIRED PER ECRA 5311-01391.

Part: BRACKET — CRACKED (BS 348) · airframe 68,580 hrs · 31,195 cycles

BRACKET CRACKED AT STA 348.20 STRINGER 16L. REMOVED AND REPLACED PER ECRA 5311-01392.

Part: ANGLE — CRACKED (BS 384-351 S16L) · airframe 68,580 hrs · 31,195 cycles

ANGLE CRACKED BETWEEN STA 384.20 AND STA 351.20 STRINGER 16L. REMOVED AND REPLACED ANGLE PER ECRA 5311-01392.

Part: STRINGER — CRACKED (BS 360 S15L) · airframe 68,580 hrs · 31,195 cycles

FORWARD ENTRY STRINGER 15L AT STA 360 IS CRACKED AT FASTENER HOLES. REMOVED AND REPLACED PER ECRA 5311-01392.

Part: BRACKET — CRACKED (BS 351 S16L) · airframe 68,580 hrs · 31,195 cycles

BRACKET CRACKED AT STA 351 STRINGER 16L. REMOVED AND REPLACED BRACKET PER ECRA 5311-01392.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FORWARD ENTRY INTERCOSTAL STRINGER 15L WEB FWD SUPPORT CLIP CRACKED. REMOVED AND REPLACED PER ECRA 5311-01392.

Part: STRINGER — CRACKED (BS 360 S14L) · airframe 68,580 hrs · 31,195 cycles

FORWARD ENTRY AT AFT SIDE OF L-1 DOOR CUT OUT STRINGER 14L CRACKED AT STA 360. REMOVED AND REPLACED PER ECRA 5311-01392.

Part: STRINGER — CRACKED (BS 360) · airframe 68,580 hrs · 31,195 cycles

FORWARD ENTRY L-1 DOOR STRINGER 11L AT STA 360 CRACKED AT UPPER FLANGE. REMOVED AND REPLACED CLIP PER ECRA 5311-01392.

Part: ATTACH FITTING — CRACKED (BS 360 S11L) · airframe 68,580 hrs · 31,195 cycles

FORWARD ENTRY WEB AFT SUPPORT CLIP AT INTERCOSTAL 11L STA 360 IS CRACKED. REMOVED AND REPLACED CLIP PER ECRA 5311-01392.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE FRAME IS CRACKED AT STA 727E BETWEEN STRINGER 8L AND 9L. REPAIRED PER ECRA 5310-04697.

Part: FRAME — CRACKED (BS 887 S8-9L) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE FRAME IS CRACKED AT STA 887 BETWEEN STRINGER 8L AND 9L. REPAIRED PER ECRA 5310-04697.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE FRAME STA 887 IS CRACKED BETWEEN STRINGERS 8R AND 9R. REPAIRED PER ECRA 5310-04697.

Part: FRAME — CRACKED (BS 767 S8-9R) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE FRAME IS CRACKED AT BS 767 BETWEEN STRINGER 8R AND 9R. REPAIR DONE PER ECRA 5310-04697.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 68,580 hrs · 31,195 cycles

CABIN FRAME IS CRACKED AT STA 380 RIGHT ABOVE STRINGER 8R AT SUPPORT BRACKET. REPAIRED PER ECRA 5310-04697.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE FRAME IS CRACKED AT STA 767 BETWEEN STRINGER 8L AND 9L. REPAIR PER ECRA 5310-04697.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE CROWN INTERIOR BELT FRAME HAS CRACK AROUND FASTENER OF OVERHEAD GRILL MOUNTING BRACKET JUST ABOVE STRINGER S9L AT STA 480.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE FRAME IS CRACKED AT STA 867 BETWEEN STRINGER 8R AND 9R. REPAIR PER ECRA 5310-04697.

Part: FRAME — CRACKED (BS 867 S8-9L) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE FRAME IS CRACKED AT STA 867 BETWEEN STRINGER 8L AND 9L. REPAIRED PER ECRA 5310-04697.

Part: FRAME — CRACKED (BS 847 S8-9L) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE FRAME CRACKED AT STA 847 BETWEEN STRINGER 8L AND 9L. REPAIR PER ECRA 5310-04697.

Part: FRAME — CORRODED (BS 847) · airframe 68,580 hrs · 31,195 cycles

ABB BELTFRAME STA847 RBL8 TO LBL4 HAS CORROSION. INSTALLED NEW FRAME SECTION PER ECRA 5311-01394.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE FRAME IS CRACKED AT STA 827 BETWEEN STRINGERS 8R AND 9R. INSTALLED REPAIR DOUBLERS PER ECRA 5310-04698.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE FRAME IS CRACKED AT STA 827 BETWEEN STRINGERS 8L AND 9L. INSTALLED REPAIR DOUBLERS PER ECRA 5310-04698.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

CABIN STA 639 FRAME WEB CRACKED JUST ABOVE CABIN FLOOR. REPAIRED CRACKED WEB PER ECRA 5311-01388.

Part: STRINGER — CORRODED (BS 849 S23R) · airframe 68,580 hrs · 31,195 cycles

STA 849 STRINGER 23R CORRODED. REMOVED AND REPLACED PER SRM 53-00-03.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

CORROSION ON SUPPORT ANGLE AT STA 847 RBL 8 TO RBL 4. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02 AND SRM 51-70-11.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 68,580 hrs · 31,195 cycles

FORWARD CARGO DOOR SKIN CRACKED AT EXTERIOR HANDLE CUTOUT MARKED. INSTALLED DOUBLER, SEALED AND PAINTED PER SRM 52-00-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE SKIN HAS A 2.5 INCH CRACK AT STA 500+16 STRINGER 12L. INSTALLED REPAIR PER ECRA 5331-01385.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE AT STA 840 STRINGER 21L WAS CORRODED. REMOVED DAMAGED SECTION, FABRICATED AND VERIFIED REPAIR PART, TREATED, PRIMED AND INSTALLED IN REF TO SRM 53-00-03.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

AFT BAG BIN CUTOUT FWD FRAME CRACKED AT LOWER STOP PAD REF EA5310-04443. REMOVED AND REPLACED FRAME IN REF TO SRM 51-40-02, BOEING DRAWING 65 AND ECRA 5311-01386.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

ABB STATION 947.5 BELTFRAME HAS CORROSION LBL 4". REMOVED CORROSION, CUT OUT DAMAGE, INSTALLED FRAME REPAIR PER SRM 53-00-07 REPAIR 2 FIG 201.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

ABB WEB AT STATION 787-794 ABOVE STRINGER 25R HAS CORROSION. REMOVED AND REPLACED INTERCOSTAL IN REF TO SRM 51-40-02 AND BOEING DRAWING 65-47959.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FORWARD CARGO STRINGER 28R AT STATION 500 HAS CORROSION. REMOVED DAMAGED, FABRICATED PARTS, TREATED, PRIMED AND INSTALLED PER SRM 53-00-02 FIG 201.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 68,580 hrs · 31,195 cycles

LEFT W/W UPPER PRESSURE BULKHEAD SUPPORT STIFFENER CRACKED JUST ABOVE GEAR UP LATCH AT STATION 706. REMOVED CRACKED AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED PER SRM 51-70-11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FORWARD BAG BIN DOOR CUTOUT AFT FRAME CRACKED AT LOWER STOP PAD. REMOVED DAMAGED FRAME AND INSTALLED A NEW ONE PER SRM 51-40-02.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

AFT BAG BIN DOOR CUTOUT AFT FRAME CRACKED AT LOWER STOP PAD. REPLACED FRAME PER EA 5310-04443, BAC DRAWING 65-47960 AND SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FWD FUSELAGE SKIN AT R-1 DOOR CUTOUT, LOWER AFT CORNER CRACKED. REMOVED DAMAGED SECTION OF SKIN, FABRICATED REPAIR PIECES, TREATED, PRIMED AND INSTALLED PER SRM 53-10-01 REPAIR 2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

LEFT INBOARD TRACK SEAT TRACK CORRODED AT STA 887 TO STA 927. REPAIRED SEAT TRACK PER SRM 53-00-52 REPAIR 3 FIG 201.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

CORROSION ON INBOARD FLANGE STRINGER 29R JUST FORWARD OF E&E DOOR CUTOUT APPROX STA 320. REMOVED AND REPLACED STRINGER REF SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

CORROSION IN CENTER OF STRINGER HAT SECTION STR 29RT APPROX STA 350 JUST BELOW FORWARDS OUTFLOW VALVE DUCT. REMOVED AND REINSTALLED STR CLIP AND SHIMS PER SRM 51-40-02. PICKER UP HOLES IN STR CAP REF 51-40-02. APPLIED EDGE SEAL REF AMM 51-31-00 APPLIED C.I.C. REF 51-20-01.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

STRINGER SPLICE IS CRACKED AT STA 907 STR 4R. REMOVED AND REPLACED STRINGER SPLICER PER SRM 51-40-02.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

STRINGER SPLICE IS CRACKED AT STA 907 STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-40-02.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

ABB BELTFRAME STA 727D AT S-27R HAS CORROSION. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED PER SRM 53-00-07 REPAIR NR 4.

Part: BEAM — CORRODED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

STA 947 BEAM CORRODED AROUND SCREW HOLES LBL 10 TO RBL 5. REPAIRED PER SRM 53-00-51.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

LEFT Z-ANGLE CORRODED AT STA 947-987. INSTALLED NEW LEFT Z-ANGLE PER SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

RIGHT O/B SEAT TRACK CORRODED STA 887 TO 927. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION PER SRM 53-00-02 REPAIR 3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FUSELAGE FRAME IS CRACKED AT STA 616 BETWEEN S7L AND S8L. REPAIRED PER SRM 53-00-07 FIG 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

STA 986.5 FLOORBEAM CORRODED RBL 22 TO LBL 9. REMOVED AND REPLACED UPPER T-CHORD PER SRM 51-40-02.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

FWD ENTRY FRAME STA 310 L ABOVE L-1 DOOR CUTOUT CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-70-11 FIG 1.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

CLIP CRACKED AT STA 578, S8L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

CLIP CRACKED AT STA 616, S6L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,580 hrs · 31,195 cycles

CLIP CRACKED AT STA 597, S8L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02.

Part: STRINGER — CORRODED (BS 500D S27R) · airframe 63,578 hrs · 28,939 cycles

INSPECTION FOUND STRINGER 27R CORRODED JUST AFT OF STA 500D. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 53-30-03.

Part: SHEAR TIE — CORRODED (BS 500 S27R) · airframe 63,578 hrs · 28,939 cycles

INSPECTION FOUND SHEAR TIE CORRODED AT STA 500 BETWEEN S26R AND S27R, RBL 8 TO RBL 16. A NEW SHEAR TIE WAS INSTALLED IAW SRM 53-00-07, FIGURE 201.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,346 hrs · 26,167 cycles

INSPECTION FOUND STRINGER 25L CORRODED AFT OF STA 967. A REPAIR WAS INSTALLED IAW SRM 53-60-03 AND 53-00-03.

Part: SKIN — CANNING (C2 DOOR) · airframe 57,345 hrs · 26,167 cycles

C2 DOOR LOWER SKIN OIL CANNED LOWER AFT. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 52-00-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,346 hrs · 26,167 cycles

INSPECTION FOUND CORROSION ALONG THE UPPER SURFACE OF THE UPPER SECTION OF THE STA 967 FLOORBEAM. THE CORRODED UPPER SECTION WAS TRIMMED OUT AND A NEW REPAIR SECTION WAS INSTALLED IAW ECRA 5311-01142.

Part: FLOOR PANEL — CRACKED (AFT LAV) · airframe 57,345 hrs · 26,167 cycles

REMOVED AFT LAV WEBS TO FACILITATE REPAIR OF APB. REMOVED AND REPLACED WEBS PER SRM 51-10-02. CRACKED 2 X 5 INCH.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 57,346 hrs · 26,167 cycles

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 772, RBL 3 AND RBL 7. REPAIRED FLOOR SUPPORTS IAW ECRA 5320-01603.

Part: BULKHEAD — CORRODED (FUSLEAGE) · airframe 57,346 hrs · 26,167 cycles

INSPECTION FOUND CORROSION ON APB WEB FORWARD FACE IB OF S27L ALONG LOWER RIVET ROW AT STA 1016. THE CORRODED SECTION OF WEB WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-80-08 AND MFG DRAWING NR 65C28106-1.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,346 hrs · 26,167 cycles

INSPECTION FOUND KEEL BEAM LT LOWER CHORD CORRODED FROM STA 699-727. REPAIRED IAW ECRA 5310-03740.

Part: FITTING — CORRODED (NR 2 PYLON) · airframe 57,346 hrs · 26,167 cycles

INSPECTION FOUND NR 2 ENGINE PYLON OB CROSSBEAM MOUNT FITTING CORRODED. THE FITTING WAS REPAIRED IAW ECRA 5440-01235.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,346 hrs · 26,167 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986, RBL 18-42. THE CORROSION WAS REMOVED AND A STRAP WAS INSTALLED IAW SRM 53-00-51.

Part: SKIN — GOUGED (FUSELAGE) · airframe 55,992 hrs · 25,511 cycles

INSPECTION FOUND A GOUGE IN FUSELAGE SKIN AT THE FORWARD LOWER CORNER OF THE L2 DOOR, STA 965, S17L. THE GOUGE MEASURED 2 X 1.4 INCH THE AREA WAS REPAIRED IAW ECRA 5330-03257. A DIP WAS ISSUED TO ACCOMPLISH AN HFEC INSPECTION AND GV INSPECTION AT A THRESHOLD OF 60,000 TOTAL AIRFRAME CYCLES AND SUBSEQUENT INTERVALS OF 24,000 CYCLES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,992 hrs · 25,511 cycles

INSPECTION FOUND UPPER SECTION OF FLOORBEAM CORRODED AT BS 328. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01145.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,992 hrs · 25,511 cycles

INSPECTION FOUND CORROSION ALONG THE FLOORBEAM AT STA 294.5, RBL 31.5. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01147.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,993 hrs · 25,511 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 1006 FROM LBL 24 TO LBL 28. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW ECRA 5310-03851.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,993 hrs · 25,511 cycles

INSPECTION FOUND FLOORBEAM CORRODED ON TOP SIDE IN TWO PLACES AT STA 986, RBL 15-44. REPLACED T-CAP IAW ECRA 5310-03851.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,993 hrs · 25,511 cycles

INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 312, RBL 38 TO LBL 20. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,993 hrs · 25,511 cycles

INSPECTION FOUND FLOORBEAM T-CAP CORRODED ON TOP SIDE AND BOTTOM SIDE AT FS 986.5, LBL 25. THE FLOORBEAM WAS REPAIRED BY SPLICING IN A NEW SECTION IAW ECRA 5310-03851.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 55,993 hrs · 25,511 cycles

INSPECTION FOUND A 2 INCH CRACK IN PRESSURE DECK WEB AT STA 663.75 IN RT WHEEL WELL JUST O/B OF J-BOX. THE CRACKED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-60-51, PAGE 214-221.

Part: PRESSURE PANEL — CRACKED (STA) · airframe 55,992 hrs · 25,511 cycles

INSPECTION FOUND CRACKS IN PRESSURE DECK WEB AT STA 665 TO 675, RBL 35 TO 45. A WEB STIFFENER WAS INSTALLED IAW ECRA 5312-01022.

Part: SILL — CORRODED (PAX DOOR) · airframe 55,992 hrs · 25,511 cycles

INSPECTION FOUND THE L-1 DOOR LOWER SILL CORRODED AT BS 314, LBL 57. THE DOOR SILL WAS REPAIRED IAW ECRA 5312-01146.

Part: STRINGER — CORRODED (BS 727D-827) · airframe 53,124 hrs · 24,119 cycles

INSPECTION FOUND STRINGER 26L CORRODED IN AFT BAGGAGE BIN AT BS 727D-827. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPAIR SPLICES WERE INSTALLED IAW ECRA 5311-01119.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 53,124 hrs · 24,119 cycles

INSPECTION FOUND AFT BAGGAGE BIN LT TIE DOWN TRACK CORRODED AT STA 727C-947. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-53, FIGURE 202.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 53,124 hrs · 24,119 cycles

INSPECTION FOUND A 4 INCH CRACK AT ATTACH POINT OF RIGHT TIE DOWN TRACK, STA 747. A NEW SECTION OF TIE DOWN TRACK WAS SPLICED.

Part: STRINGER — CORRODED (STA 1006-1016) · airframe 53,124 hrs · 24,119 cycles

INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016 IN AFT EQUIPMENT BAY. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: OVEN — SMOKE (GALLEY) · airframe 47,653 hrs · 21,736 cycles

AFT GALLEY OVEN STARTED SMOKING. FLIGHT ATTENDANT PULLED CIRCUIT BREAKER. NO EVIDENCE OF FIRE. MAINTENANCE INSPECTED OVEN SYSTEM AND COULD NOT DUPLICATE THE PROBLEM.

Part: CHARGER — INOPERATIVE (GALLEY DOOR)

INSPECTION FOUND FORWARD GALLEY SERVICE DOOR SLIDE LIGHT ASSEMBLY INOPERATIVE. MAINTENANCE FOUND CHARGER ASSEMBLY INOPERATIVE. THE CHARGER ASSEMBLY WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 312 FROM RBL 36 TO LBL 18. THE CORRODED SECTION OF FLOORBEAM WAS REPLACED IAW SRM 53-10-51.

Part: STRINGER — CRACKED (BS 500C)

INSPECTION FOUND A 1 CRACK IN STRINGER 16R AT STA 500C. THE STRINGER SECTION WAS REPLACED IAW SRM 53-00-03, FIGURE 201.

Part: WEB — CRACKED (BS 950)

INSPECTION FOUND A 2 CRACK IN WEB BELOW R-2 DOOR ASSIST HANDLE AT STA 950, S11R AND A 2 CRACK WAS FOUND IN WEB BELOW L-2 DOOR ASSIST HANDLE AT STA 950, S11L. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 51-70-13.

Part: SKIN — DENTED (CARGO DOOR)

INSPECTION FOUND C-1 DOOR EXTERNAL SKIN DENTED. THE DENTED AREAS WERE CUT OUT AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 52-00-01, FIGURE 203.

Part: SKIN — WORN (BS 867 - 907)

INSPECTION FOUND FUSELAGE CROWN SKIN WORN BY DORSAL FIN AT STA 867-907. THE WORN AREA WAS REMOVED AND A SKIN REPAIR WAS INSTALLED IAW SRM 53-00-01.

Part: SEAT TRACK — CORRODED (BS 328 - 344)

INSPECTION FOUND CABIN SEAT TRACK CORRODED AT STA 328-344, RBL 42. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52, FIGURE 202 AND 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1016)

INSPECTION FOUND RT AND LT AFT LAV FLOORBEAMS CORRODED AT STA 1016, RBL 6.5 AND LBL 28. THE FLOORBEAM UPPER CHORD SECTIONS WERE REPLACED IAW ECRA 5310-03851.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 344 FROM RBL 18 TO LBL 48. A NEW FLOORBEAM UPPER CHORD WAS INSTALLED IAW SRM 53-10-51, FIGURE 205.

Part: FLOORBEAM — CORRODED (BS 294.5)

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 294.5, RBL 54 TO LBL 24. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51, FIGURE 205.

Part: SKIN — CRACKED (WINDOW FRAME)

INSPECTION FOUND A 1 INCH CRACK IN CAPTAIN'S L-1 WINDOW FRAME SKIN. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02833.

Part: FLOORBEAM — CORRODED (BS 986)

INSPECTION FOUND FLOORBEAM CAP IN AFT LEFT LAV AREA CORRODED AT STA 986. REPAIRED IAW ECRA 5310-03851.

Part: TRANS CYLINDER — INOPERATIVE (NLG)

WHEN GEAR HANDLE WAS SELECTED DOWN ON APPROACH, THE GEAR DID NOT EXTEND ON INITIAL ATTEMPT. THE GEAR WAS CYCLED AND EXTENDED NORMALLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NLG TRANSFER CYLINDER AND NLG MODULAR PACKAGE WERE REMOVED AND REPLACED IAW MM 32-33-31 AND 32-33-41. A LANDING GEAR EXTENSION AND RETRACTION TEST WAS PERFORMED IAW MM 32-33-00 AND OPERATION CHECKED GOOD.

Part: SKIN — CRACKED (NR 2 PYLON)

INSPECTION FOUND TWO 1/2 CRACK IN #2 PYLON SKIN ON OUTBOARD SIDE AT PANEL #5824 CUTOUT. THE CRACKS WERE STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5430-01204.

Part: OIL LINE — LEAKING (OIL COOLER)

THE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO AND THE OIL PRESSURE BEGAN TO DROP AFTER TAKEOFF FROM CLE. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LINE TO FUEL/OIL COOLER LOOSE AND LEAKING. THE LINE WAS TIGHTENED AND THE NR 1 ENGINE WAS SERVICED WITH OIL. THE ENGINE WAS RUN AT FULL POWER AND NO LEAKS WERE NOTED.

Part: ACTUATOR — INOPERATIVE (NLG)

EWR - FLT 0744 - THE LANDING GEAR WOULD NOT EXTEND INITIALLY ON APPROACH TO EWR. THE GEAR DID NOT MOVE AND THERE WERE NO WARNING LIGHTS. THE GEAR HANDLE WAS CYCLED, AND THE GEAR EXTENDED WITH A LOUD BANG AFTER FIVE SECONDS. MAINTENANCE FOUND THE NLG RETRACT ACTUATOR AT FAULT. THE NLG RETRACT ACTUATOR WAS REMOVED AND REPLACED. THE NOSE GEAR HYDRAULIC MODULE, NLG HYDRAULIC TRANSFER CYLINDER, AND NLG LOCK ACTUATOR WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. LEAK AND OPERATIONAL CHECKS WERE GOOD. (X)

Part: FRAME — CRACKED (NLG)

EWR - FLT 1827 - MAINTENANCE FOUND NLG TRUNNION LOOSE, FURTHER INSPECTION FOUND NLG 'A' FRAME CRACKED. REMOVED AND REPLACED UPPER NLG DRAG BRACE PN NR 65-80051-20. (Z)

Part: GEAR HANDLE — DIRTY (COCKPIT)

IAH - FLT 1485 - WHEN THROTTLES WERE RETARDED WITH FLAPS EXTENDED, THE HORN WOULD NOT SILENCE. THE LANDING GEAR WAS LOWERED WITH 3 GREEN AND 3 RED GEAR LIGHTS ILLUMINATING. A 'TOO LOW' GEAR ALERT WAS ALSO RECEIVED. THE GEAR WAS CYCLED AND INDICATIONS WERE NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DEBRIS STICKING IN GEAR HANDLE. THE GEAR HANDLE WAS CLEANED AND LUBRICATED AND OPERATION CHECKED GOOD. (X)