N14320

Part: SKIN — CORRODED (BS 986.5) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND CORROSION ON BONDED DOUBLER AT STA 986.5 BELOW S27L. THE AREA WAS REPAIRED IAW ECRA 5311-01372.

Part: ANGLE — CRACKED (BS 348-351 S16L) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN UPPER ANGLE AT S16L BETWEEN STA 348.2 AND 351.2. THE ANGLE WAS REPLACED IAW ECRA 5311-01375.

Part: INTERCOSTAL — CRACKED (BS 348.2 S16L) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A 5 INCH CRACK AND MISSING FASTENER HEAD IN INTERCOSTAL WEB ON STRINGER 16L AT STA 348.2. THE INTERCOSTAL WEB WAS REPLACED IAW ECRA 5311-01375.

Part: FRAME — CORRODED (BS 227.8) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND FRAME AND SUPPORTS CORRODED AT STA 227.8, LBL 5.7 TO RBL 5.7, S28L. THE AREA WAS REPAIRED IAW ECRA 5311-01373.

Part: SKIN — CORRODED (BS 967 S27L/R) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND SKIN CORRODED AT RIVET ROW, STA 967 BETWEEN STRINGERS 27R AND 27L. A REPAIR WAS INSTALLED IAW ECRA 5311-01377.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN NR 2 PYLON ACCESS PANEL 5824 CUTOUT ON UPPER FORWARD CORNER, NAC STA 258. THE CRACK WAS STOP DRILLED AND A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5430-01204.

Part: STRINGER CLIP — CRACKED (BS 348.2 S15L) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN ATTACHMENT CLIP (BROKEN FASTENER HEADS TOO) ON STRINGER 15L AT STA 348.2. THE ATTACHMENT CLIP WAS REPLACED IAW ECRA 5311-01375.

Part: ANGLE — CRACKED (BS 348-351 S16L) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN ATTACHMENT ANGLE ON STRINGER 16L BETWEEN STA 348.2 AND 351.2. THE ATTACHMENT ANGLE WAS REPLACED IAW ECRA 5311-01375.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR UPPER FRAME AT SPLICE POINT. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FRAME — CORRODED (BS 203 S28L/R) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND FRAME AND SUPPORT CORRODED AT STA 203.8, S28L TO S28R, RBL 5.7 TO LBL 5.7. THE FRAME CHORD AND SUPPORT WERE REMOVED AND REPLACED IAW SRM 51-40-02.

Part: KEELBEAM — CRACKED (BS 540) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN KEEL BEAM IN RIGHT A/C BAY AT STA 540. THE KEEL BEAM SECTION WAS REMOVED AND REPLACED IAW SRM 53-60-12, FIGURE 201, PAGE 201.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR FRAME AT FORWARD LOWER SEGMENT AT PULLEY BOLT HOLE. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN LT HORIZONTAL STABILIZER UPPER O/B CHORD AT STAB STA 101.90. THE CRACKED AREA OF CHORD WAS REMOVED AND A REPAIR WAS INSTALLED IAW IAW SRM 51-70-12.

Part: INTERCOSTAL — CRACKED (BS 290 S10R) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL ANGLE AT STA 290 BELOW S10R FORWARD OF R-1 DOOR. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02.

Part: STRINGER — CORRODED (BS 360 S25L) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND STRINGER 25L CORRODED AT STA 360. A REPAIR STRINGER SPLICE WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.

Part: ATTACH FITTING — CORRODED (BS 747) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND AFT CARGO COMPARTMENT STRINGER 26R ATTACH CLIP CORRODED AT STA 747. A NEW CLIP WAS INSTALLED IAW SRM 51-40-02.

Part: STRINGER — CORRODED (BS 986 S27L) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND HEAVY CORROSION ON STRINGER 27L AT STA 986.5. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03.

Part: FRAME — CRACKED (BS 847 S23-24R) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR CUTOUT AFT FRAME AT LOWER DOOR STOP FITTING, STA 847 BETWEEN STRINGER 23R AND 24R. THE CRACKED FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-40-02, PARAGRAPH 4 AND 7 AND BAC DRAWING 65C35243.

Part: FRAME — CORRODED (BS 500D S26L) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND FRAME CORRODED AT STA 500D, ABOVE S26L. THE FRAME WAS REPAIRED IAW SRM 53-00-07.

Part: FRAME — CORRODED (BS 500D S26-27L) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND FRAME CORRODED AT STA 500D BETWEEN STRINGERS 26L AND 27L. THE FRAME WAS REPAIRED IAW SRM 53-00-07.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN MAIN FRAME AT STA 616 JUST BELOW CABIN FLOOR, S17L. THE FRAME WAS REPAIRED IAW ECRA 5311-01158.

Part: INTERCOSTAL — CRACKED (BS 280 S14R) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT STA 280, S14R FORWARD OF R-1 DOOR. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SKIN — CORRODED (BS 500D) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND FUSELAGE SKIN CORRODED JUST FORWARD OF STA 500D ABOVE S27R. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND STRINGER SPLICE 27L CORRODED AT STA 360. THE CHANNEL SPLICE WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND AMM 51-31-00.

Part: STRINGER — CORRODED (BS 340-360) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND STRINGER 25R CORRODED AT STA 340-360. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, REPAIR 1, FIGURE 201, DETAIL VII.

Part: MOUNT — CRACKED (FUSELAGE) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A 1 INCH CRACK IN NR 2 VHF ANTENNA MOUNTING BRACKET AT FORWARD CARGO BIN BETWEEN S28L AND S28R. THE MOUNTING BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: RELEASE MECH — INOPERATIVE (COCKPIT WINDOW) · airframe 68,197 hrs · 30,876 cycles

THE FIRST OFFICER'S SLIDING WINDOW (R2) FAILED OPERATIONAL TEST FROM OUTSIDE THE CONTROL CABIN (WINDOW DID NOT UNLOCK AND OPEN WHEN THE EXTERNAL RELEASE HANDLE WAS PULLED). THE EMERGENCY RELEASE MECHANISM WAS LUBRICATED AND THE AREA WAS CLEANED. A FUNCTIONAL CHECK WAS GOOD IAW AMM 56-12-11.

Part: FRAME — CRACKED (BS 480 S8-9R) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 480 BETWEEN S8R AND S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669.

Part: FRAME — CRACKED (BS 867 S9R) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 867, S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669.

Part: FRAME — CRACKED (BS 767 S9R) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 767, S9R. THE FRAME WAS REPAIRED IAW ECRA 5310-04669.

Part: FRAME — CRACKED (BS 480 S8-9L) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE FRAME AT STA 480 BETWEEN S8L AND S9L. THE FRAME WAS REPAIRED IAW ECRA 5310-04669.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 328, RBL 11. THE FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: STRINGER — CRACKED (BS 500C S16L) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L JUST AFT OF STA 500C FORWARD OF WING SCANNING LIGHT HOUSING. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, PAGE 201, FIGURE 201, REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 360) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES AT STA 360, BL 0. REPAIRED IAW SRM 53-30-51.

Part: ANGLE — CORRODED (BS 907-1016) · airframe 68,198 hrs · 30,876 cycles

INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 907-1016, LBL 45. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: PIN — WORN (R1 DOOR LEVER) · airframe 64,472 hrs · 29,221 cycles

THE R-1 DOOR COULD BE CLOSED WITHOUT RELEASING THE HOLD OPEN CAM PLATE PIN. MAINTENANCE FOUND THE PIN WORN. THE DOOR RELEASE LEVER WAS REPLACED IAW MM 52-41-00. OPERATIONAL CHECKS WERE GOOD.

Part: FRAME — CORRODED (BS 927) · airframe 63,659 hrs · 28,858 cycles

INSPECTION FOUND FRAME CORRODED IN AFT BAGGAGE BIN AT FLOOR SUPPORT WEB FUSELAGE ATTACH AREA, STA 927 BETWEEN S26L AND S26R. A SHEAR TIE WAS INSTALLED IAW SRM 53-00-07.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 63,659 hrs · 28,858 cycles

INSPECTION FOUND A .5 INCH CRACK IN NR 1 PYLON SKIN AT UPPER FORWARD O/B PANEL, NAC STA 224. A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.

Part: SLIDE — TWISTED (R-1 DOOR) · airframe 62,231 hrs · 28,291 cycles

R-1 DOOR EVACUATION SLIDE FAILED TO DEPLOY PROPERLY DURING DEPLOYMENT TEST. SLIDE INFLATED EARLY CAUSING SLIDE TO INFLATE BETWEEN DOOR & DOOR OPENING NOT ALLOWING DOOR TO COMPLETELY OPEN. SLIDE DEPLOYED SIDEWAYS INSTEAD OF FLAT. SLIDE INFLATED COMPLETELY WITHIN 10 SEC. SLIDE WAS REMOVED & REPLACED. BOEING HAS SEEN PROBLEM WITH OTHER OPERATORS (SIDEWAYS OR TWISTED SLIDE DEPLOYMENT) DESCRIBED IN THEIR "FLEET TEAM DIGEST 737-FTD-25-02007". BOEING ATTRIBUTES SLIDE'S SIDEWAYS DEPLOYMENT TO ALIGNMENT(IE. POSITIONING) OF SLIDE WITHIN SLIDE COMPARTMENT ASSEMBLY (50% SLIDE FAULT AND 50% COMPARTMENT FAULT). BOEING PLANS TO INCORPORATE SEVERAL DESIGN IMPROVEMENTS TO ESCAPE SLIDE COMPARTMENT WITH RELEASE OF S/B.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND UPPER SURFACE OF O/B FLANGE OF LEFT KEELBEAM CORRODED AT STA 720. A REPAIR WAS INSTALLED IAW ECRA 5311-01177.

Part: STRAP — CRACKED (NR 1 PYLON) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND A 6 INCH CRACK IN O/B STRAP ON NR 1 PYLON AT STA 363.5. INSTALLED SPLICE STRAPS IAW ECRA 5421-01002.

Part: STRAP — CRACKED (NR 1 PYLON) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND A 6 INCH CRACK IN I/B STRAP ON NR 1 PYLON AT STA 363.5. REPAIRED IAW ECRA 5421-01002.

Part: WEB — CRACKED (NR 1 PYLON) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND A 3 INCH CRACK IN WEB AT NR 1 PYLON STRUT. REPAIRED IAW ECRA 5421-01002.

Part: SKIN — GOUGED (FUSELAGE) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 727D + 8, LBL 2. THE GOUGED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202.

Part: STRAP — BROKEN (FUSELAGE) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND STRAP BROKEN ON BOTTOM OF BEAMS AT STA 312-328, RBL 42. THE STRAP WAS REPAIRED IAW SRM 53-10-51.

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND A 2 INCH CRACK IN NR 1 PYLON FORWARD FITTING AT LOWER I/B CORNER. THE NR 1 PYLON FORWARD FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND HAT CHANNEL FOR ANTENNA CORRODED AT STA 727D +12, S27L. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-02.

Part: SKIN — GOUGED (FUSELAGE) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND LOWER FUSELAGE SKIN GOUGED AT STA 314, S27L. A DOUBLER WAS INSTALLED IAW SRM 53-00-01.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND ATTACH ANGLE AND FLANGES ON ATTACH ANGLE CORRODED AT FORWARD SIDE APB STA 1016, BL 0. THE CORRODED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW EA 5310-04045.

Part: STRAP — CORRODED (FUSELAGE) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND FORWARD SIDE OF LOWER ATTACH STRAP CORRODED AT STA 1016 BETWEEN STRINGER 26 AND 27. THE ATTACH STRAP WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND A .5 INCH CRACK IN MAIN FRAME AT STA 616 AT RT SIDE BELOW FLOOR LINE. A STIFFENER WAS INSTALLED IAW ECRA 5311-01158.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND SEAT TRACK CORRODED AT STA 277-294, RBL 43. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: WEB — GOUGED (FUSELAGE) · airframe 57,453 hrs · 26,066 cycles

INSPECTION FOUND WEB GOUGED IN PIT ON FORWARD CARGO DOOR JAMB AT S26R. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-00.

Part: FLOORBEAM — CORRODED (STA) · airframe 56,163 hrs · 25,427 cycles

I-BEAM AT STATION 986.5 AFT GALLEY HAS CORROSION THROUGHOUT ENTIRE LENGTH MARKER (8 INCHES). REMOVED CORROSION, REPAIRED FLOORBEAM PER SRM 53-30-51.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 56,163 hrs · 25,427 cycles

INSPECTION FOUND A PUNCTURE IN FUSELAGE TAIL SECTION SKIN AT STA 1043, BL 0. A DOUBLER WAS INSTALLED IAW SRM 53-00-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,163 hrs · 25,427 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016 FROM RBL 10 TO LBL 35. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS PERFORMED IAW SRM 53-00-51, FIGURE 202.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,652 hrs · 25,196 cycles

INSPECTION FOUND A CRACK IN PRESSURE DECK WEB AT STA 663, LBL 32. THE AREA WAS REPAIRED IAW SRM 53-60-51, FIGURE 203 AND ECRA 5310-04317.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 55,652 hrs · 25,196 cycles

INSPECTION FOUND A CRACK IN THE PRESSURE DECK WEB AT STA 665 - 675, RBL 35 - 45. THE CRACK WAS ESTIMATED TO BE .5 - .75 INCH LONG. THE AREA WAS REPAIRED IAW SRM 53-60-51, FIGURE 203 AND ECRA 5310-04316.

Part: ENGINE — LEAKING (NR 2) · airframe 53,463 hrs · 24,218 cycles

SMOKE ENTERED THE COCKPIT AND CABIN AFTER TAKEOFF FROM ORD. ISOLATING THE PACKS DID NOT HELP. THE AIRCRAFT WAS RETURNED TO ORD WHERE IT LANDED WITHOUT INCIDENT. A BORESCOPE OF THE NR 2 ENGINE HPC SECOND STAGE FOUND THE AREA WET WITH OIL. THE VSV WAS ALSO FOUND TO BE WET WITH OIL. A NR 2 ENGINE CHANGE WILL BE PERFORMED.

Part: WEB — CRACKED (C-2 DOOR) · airframe 53,065 hrs · 24,048 cycles

INSPECTION FOUND A 0.137" CRACK IN INTERIOR WEB AT HANDLE CUTOUT OF AFT BAGGAGE BIN DOOR. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01015.

Part: ACM — LEAKING (R/H PACK) · airframe 53,044 hrs · 24,037 cycles

SMOKE WAS REPORTED IN THE CABIN AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OIL RESIDUE FROM R/H ACM IN DUCTWORK. THE R/H ACM WAS REMOVED AND REPLACED. HOT CYCLES WERE RUN ON R/H PACK FOR 20 MINUTES IAW MM 21-51-11 AND ALL CHECKED GOOD. BOTH COALESCER BAGS WERE REMOVED AND REPLACED.

Part: SELECTOR VALVE — INOPERATIVE (LANDING GEAR) · airframe 51,581 hrs · 23,379 cycles

THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM CLE. QRH WAS COMPLETED AND THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND THE LANDING GEAR SELECTOR VALVE AT FAULT. THE LG SELECTOR VALVE WAS REMOVED AND REPLACED IAW MM 32-31-51. LEAK AND OPERATIONAL CHECKS WERE GOOD. THE GROUND SPOILER INTERLOCK VALVE CABLE WAS ALSO REMOVED AND REPLACED IAW MM 27-62-51 DUE TO BINDING.

Part: SKIN — GOUGED (R-1 DOOR)

INSPECTION FOUND R-1 DOOR SKIN GOUGED JUST ABOVE LOWER HINGE ARM. THE GOUGED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 52-00-01.

Part: SEAT TRACK — CORRODED (BS 942)

INSPECTION FOUND CABIN SEAT TRACK CORRODED AT BS 942, LBL 25. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-00-52.

Part: FLOORBEAM — CORRODED (BS 986.5)

INSPECTION FOUND CABIN FLOORBEAM CORRODED AROUND NUTPLATE HOLES AT BS 986.5. THE CORRODED UPPER PART OF BEAM WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5310-03851.

Part: FLOORBEAM — CORRODED (BS 947&967)

INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 947, LBL 10 TO RBL 10 AND AT STA 967. NEW UPPER CHORDS WERE INSTALLED IAW SRM 53-00-51 AND ECRA 5310-03851.

Part: FLOORBEAM — CORRODED (BS 294)

INSPECTION FOUND TOP OF FLOORBEAM CORRODED AT STA 294, BL 0 TO LBL 45. A NEW T-CHORD AND SPLICES WERE INSTALLED IAW SRM 53-10-08.

Part: SKIN — WORN (BS 867-887)

THE FORWARD DORSAL FIN FAIRING CAUSED CHAFING WEAR ON UPPER FUSELAGE SKIN IN TWO AREAS AT STA 867-887, RBL 1-11 AND LBL 1-11. THE WORN SECTIONS OF SKIN WERE REMOVED AND REPAIRS WERE INSTALLED IAW SRM 53-00-01, FIGURE 201.

Part: FRAME — CRACKED (R-1 DOORWAY)

INSPECTION FOUND A .5 INCH CRACK BETWEEN TWO FASTENERS OF FORWARD LOWER R-1 DOOR FRAME. A DOUBLER AND FILLERS WERE INSTALLED IAW SRM 51-70-11.

Part: FLOORBEAM — CORRODED (BS 312)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 45. A NEW FLOORBEAM WAS INSTALLED IAW SRM 53-10-51.

Part: STARTER GEAR — FAILED (NR 1 GEARBOX)

THE NR 1 ENGINE STOPPED WHILE EN ROUTE FROM SAL TO IAH. THE AIRCRAFT WAS DIVERTED TO MID WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. ACCESSORY GEARBOX DISASSEMBLY REVEALED STARTER GEAR FAILURE.

Part: CONTROL CABLE — BROKEN (FLT SPOILER)

FIVE UNITS OF RUDDER LEFT RUDDER TRIM WAS REQUIRED TO COUNTER ADVERSE ROLL TO RIGHT WITH SPEED BRAKES AT FLIGHT DETENT WHILE ON DESCENT INTO LAX. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 FLIGHT SPOILER CABLE NUMBER WSA2-3 BROKEN. THE CABLE WAS REPLACED AND THE FLIGHT SPOILERS WERE RIGGED IAW MM 27-61-00. OPERATIONAL CHECKS WERE GOOD.

Part: APU — LEAKING OIL (AFT FUSELAGE)

CLE - FLT 0258 - THE APU AUTOMATICALLY SHUT DOWN AFTER TAKEOFF FROM LAX. THERE WERE NO ABNORMAL INDICATIONS OR LIGHTS. THE AIRCRAFT CONTINUED FLIGHT TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE CIRCUIT BREAKER ON ACCESSORY UNIT. THE APU WAS STARTED AND FULLY LOADED WITH NORMAL EGT, VOLTS, AND FREQUENCIES EXHIBITED. PRIOR TO BOARDING FOR NEXT FLIGHT, THE APU AUTOMATICALLY SHUT DOWN AGAIN, AND EMITTED SMOKE INTO THE CABIN. MAINTENANCE FOUND EVIDENCE OF AN INTERNAL APU OIL LEAK. THE APU OIL LEVEL WAS FOUR QUARTS LOW. THE APU WAS PLACARDED INOPERATIVE, PENDING REMOVAL AND REPLACEMENT. (X)

Part: APU — LOW ON OIL (A/C TAIL)

ATL - FLT 1424 - WHILE OPERATING THE APU WITH THE NR 1 GENERATOR PLACARDED INOPERATIVE, THE APU FAILED ON TAKEOFF AND COULD NOT BE RESET. THE ACFT WAS RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU LOW ON OIL. THE APU OIL LEVEL WAS SERVICED TO FULL AND THE APU WAS RESET. OPERATIONAL CHECKS WERE GOOD. IN ADDITION, THE NR 1 CSD OIL LEVEL WAS CHECKED AND FOUND GOOD. THE CSD WAS RESET. THE ENGINE WAS RUN AND THE GENERATOR CAME ON-LINE. VOLTAGE AND FREQUENCIES CHECKED GOOD AND THE GENERATOR PLACARD WAS REMOVED.

Part: BATTERY PACK — DISCHARGED (CABIN)

GSO - THE R-2 DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE R-2 DOOR EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-51 AND OPERATION OF THE EMERGENCY LIGHT WAS RESTORED. (M)

Part: KEEL BEAM — CRACKED (BS 727)

GSO - INSPECTION FOUND A 1.5 INCH CRACK AND CORROSION ON LT KEEL BEAM AT BS 727. AN ANGLE AND EXTERNAL STRAP REPAIR WAS INSTALLED IAW ECRA 5310-03224. (X)

Part: SKIN — DENTED (C-2 DOOR)

GSO - INSPECTION FOUND C-2 DOOR EXTERIOR SKIN HAD DENTS, GOUGES, AND NICKS. THE DAMAGED SECTION OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 52-00-01. (X)

Part: ANGLES — CORRODED (BS 967)

IAH - INSPECTION FOUND CORROSION ON FLOOR BEAM SUPPORT ANGLES AT STATION 967 AND RBL 18.0, RBL 5.0, LBL 4.5, AND LBL 27.5. THE FLOOR SUPPORT ANGLES WERE REPAIRED IAW SRM 53-00-51 AND ECRA 5310-03152. (M)

Part: ANGLE — CORRODED (BS 1014)

IAH - INSPECTION FOUND WALL SUPPORT ANGLE CORRODED AT STATION 1014, LBL 4.54. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-40-2. (M)

Part: ANGLE — CORRODED (BS 1014)

IAH - INSPECTION FOUND WALL SUPPORT ANGLE CORRODED AT STATION 1014, RBL 4.54. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-40-2. (M)

Part: FLOOR BEAM — CORRODED (BS 1016)

IAH - INSPECTION FOUND CORROSION ON TOP OF FLOOR BEAM AT STATION 1016, LBL 5.5. THE FLOOR BEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 202 AND ECRA 5310-03151. (M)

Part: FLOOR BEAM — CORRODED (BS 986-1006)

IAH - INSPECTION FOUND CORROSION ON FLOOR BEAM OF L-2 DOOR THRESHOLD AT STATION 986-1006. THE AREA WAS REPAIRED IAW SRM 51-40-01. (M)

Part: SLIDE — FELL OFF (L-1 DOOR)

IAH - FLT 0717 - L1 DOOR SLIDE FELL OFF DOOR AT PUSH BACK REINSTALLED SLIDE ASSY. (W)