N69351

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 60,159 hrs · 30,753 cycles

LAST ROW OF FLOOR PROXIMITY EMERGENCY LIGHTS INOP. REPLACED FUSES IN BATTERY CHARGER. OPS CHECK'S GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,823 hrs · 30,593 cycles

FORWARD SIDE OF STA 986 SKIN HAS CORROSION I/B OF STRINGER 27L. REPAIRED PER ECRA 5330-03781.

Part: STRINGER CLIP — CRACKED (BS 348 S15L) · airframe 59,822 hrs · 30,593 cycles

STA 348.2 STRINGER 15L LOWER STRINGER CLIP IS CRACKED. INSTALLED NEW CLIP PER SRM 51-40-05.

Part: STRAP — CORRODED (FUSELAGE) · airframe 59,823 hrs · 30,593 cycles

CORROSION ON INTERNAL BONDED STRAP BETWEEN STRINGER 27L AND 27R JUST FORWARD OF STA 986.5 FRAME. REPAIR PER ECRA 5330-03781.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,823 hrs · 30,593 cycles

FOUND CORROSION ON INTERNAL SKIN AT BS 483 LOCATED AT FORWARD CARGO DOOR CUTOUT LOWER AFT CORNER. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 59,822 hrs · 30,593 cycles

INTERCOSTAL WEB AT STA 927 TO 947 CORRODED. REMOVED DAMAGED 4 ANGLES AND INSTALLED NEW ANGLES PER SRM 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · airframe 59,823 hrs · 30,593 cycles

FOUND CORROSION AT FORWARD CARGO DOOR SILL WEB. NEW WEB WAS FABRICATED AND INSTALLED.

Part: SHEAR TIE — CORRODED (BS 927 S26-27R) · airframe 59,822 hrs · 30,593 cycles

STA 927 FRAME TO SKIN ATTACH LEG CORRODED BETWEEN STRINGER 26R AND 27R. REMOVED AND REPLACED DAMAGED FRAME SECTION PER SRM 53-00-07.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 59,823 hrs · 30,593 cycles

STA 986 STRINGER 27L CORRODED FORWARD AFT SIDE OF FRAME. REPAIRED PER ECRA 5330-03781.

Part: SHEAR TIE — CORRODED (BS 927 S26-27L) · airframe 59,822 hrs · 30,593 cycles

STA 927 FRAME TO SKIN ATTACH LEG CORRODED BETWEEN STRINGER 26L AND 27L. REMOVED AND REPLACED DAMAGED FRAME SECTION PER SRM 53-00-07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,823 hrs · 30,593 cycles

STA 986 FRAME TO SKIN ATTACHEMENT LEG CORRODED I/B OF STRINGER 27L. REMOVED AND REPLACED SHEAR TIE AT STA 986 STRINGER 27L PER SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,822 hrs · 30,593 cycles

STA 907 RBL 45 SEAT TRACK CORRODED. FABRICATED AND INSTALLED SEAT TRACK SECTION PER SRM 53-00-52.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,822 hrs · 30,593 cycles

FOUND CORROSION IN FORWARD PIT ON SKIN AND AROUND DOME NUT AT BS 500D LBL 17-21. REPAIRED PER SRM 53-00-07.

Part: STRAP — CRACKED (FUSELAGE) · airframe 59,822 hrs · 30,593 cycles

STA 348.2 STRINGER 16 LT SIDE STRAP CRACKED. REPLACED PER JOB 24-0553-8-0114 SEQ 482.

Part: FITTING — CORRODED (FUSELAGE) · airframe 59,822 hrs · 30,593 cycles

FOUND CORROSION AT FORWARD CARGO DOOR CUTOUT AT STRINGER 22R. REMOVED, FABRICATED AND INSTALLED NEW CLIP PER SRM 51-10-02.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 59,823 hrs · 30,593 cycles

FOUND CRACK ON FORWARD CARGO AFT BOTTOM DOOR STOP. REMOVED AND INSTALLED NEW FRAME AT STA 492.4 PER SRM 51-40-02.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 59,822 hrs · 30,593 cycles

ATTACHMENT CLIP CRACKED IN RADIUS AT BS 360 STRING 10L. REMOVED AND REPLACED PER ECRA 5310-04719.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,948 hrs · 30,182 cycles

RIGHT FUSELAGE SKIN CRACKED 2.125 - 3 INCHES AFT OF PREV REPAIR AT EMERGENCY LIGHT. REPAIRED PER ECRA 5330-03461 (REV A).

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,729 hrs · 27,338 cycles

INSPECTION FOUND A 1" CRACK AND BULGING IN LOWER VHF ANTENNA SKIN AT AFT SIDE, STA 500 TO 500A, S28L TO S 28R. A REPAIR WAS INSTALLED IAW ECRA 5330-03471 AND A DIP WAS ISSUED TO PERFORM AN INITIAL INSPECTION WITHIN 60,000 CYCLES AND TO ACCOMPLISH REPETITIVE INSPECTIONS AT INTERVALS NOT TO EXCEED 30,000 FLIGHT CYCLES AFTER ACCOMPLISHMENT OF INITIAL INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,473 hrs · 27,213 cycles

2.0 IN CRACK IN FUSELAGE SKIN BELOW RT EMERGENCY LIGHT AFT OF WING TO BODY FAIRING, STA 727E, S23R. SKIN REPAIRED IAW ECRA 5330-03461. DIP ISSUED TO REINSPECT REPAIR WITHIN 60,000 CYCLES AND MAKE SUBSEQUENT INSPECTIONS EVERY 25,000 CYCLES.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND A 1 INCH CRACK IN FLIGHT DECK FLOOR PANEL AT STA 257, RBL 1. REPAIRED IAW SRM 51-70-13.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND TWO 3 INCH CRACKS IN LEFT HORIZONTAL STABILIZER LOWER SKIN, SPAR STA 131 AND 140. REPAIRED IAW ECRA 5510-01616.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

MAINTENANCE DISCOVERED A SHEAR TIE CRACKED IN TWO PLACES ALONG THE FASTENERS ATTACHING IT TO THE FUSELAGE SKIN. THE CRACKS WERE LOCATED BETWEEN STRINGERS 9L AND 10L AND BETWEEN STRINGERS 10L AND 11L, STA 277. REPAIRED IAW ECRA 5311-01193.

Part: KEELBEAM — WORN (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

MAINTENANCE DISCOVERED WEAR ON THE UPPER SURFACE OF THE LEFT KEEL BEAM LOWER CHORD OUTBOARD FLANGE BETWEEN STA 712 AND 727. THE WEAR WAS CAUSED BY THE WASHERS THAT ARE INSTALLED WITH THE LOWER WHEEL WELL FAIRING PANEL ATTACH FASTENERS. REPAIRED IAW ECRA 5311-01192.

Part: SKIN — GOUGED (RT PYLON) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND RIGHT ENGINE PLYON SKIN GOUGED UNDER PANEL 5829R, NAC STA 234.25 AND 246.63. REPAIRED IAW ECRA 5431-01022.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND ATTACH ANGLES CORRODED UNDER RADAR R/T FORWARD OF STA 203.8. NEW ANGLES WERE INSTALLED IAW SRM 51-40-00 AND 51-10-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND A .5 INCH CRACK IN STRINGER S23L AT STA 1040, FORWARD OF TAIL COMPARTMENT ACCESS DOOR. REPAIRED IAW SRM 53-00-03, FIGURE 202.

Part: SKIN — CORRODED (SERVICE DOOR) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND GROUND AIR SERVICE DOOR SKIN CORRODED. THE CORRODED SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 51-10-02.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR FRAME UPPER CLOSE OUT WEB AT STA 847. A WEB REPAIR WAS INSTALLED IAW SRM 51-70-13.

Part: SKIN — GOUGED (NR 2 MIDFLAP) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND NR 2 LEFT I/B MIDFLAP SKIN FOR EXHAUST GATE CONTROL ROD ON LEADING EDGE GOUGED AT WBL 163. REPAIRED IAW ECRA 5752-01151.

Part: RIB — CRACKED (HORIZ STAB) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND A .375 INCH CRACK IN RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: LINK — CRACKED (ENG MOUNT) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND NR 2 ENGINE AFT MOUNT HANGAR LINK CRACKED. THE LINK WAS REPLACED IAW MM 71-21-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 328-338. REPAIRED IAW SRM 53-00-52, FIGURE 202.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND MAIN CABIN FLOOR SUPPORT CORRODED ON UPPER SURFACE AT STA 294-312, RBL 12. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND MAIN CABIN FLOOR INTERCOSTAL UPPER FLANGE CORRODED AT STA 297, RBL 32. REPAIRED IAW BOEING DRAWING 65-45834 AND SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 328-360. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND FLOORBEAM CORRODED ON BOTTOM SIDE AT STA 360, BL 0. A DOUBLER WAS INSTALLED IAW SRM 53-00-51.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND A 3 INCH CRACK IN BELTFRAME AT STA 616 LEFT JUST BELOW FLOOR LINE. THE FRAME WAS REPAIRED IAW ECRA 5311-01158.

Part: ANGLE — CORRODED (R-2 DOOR) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND R-2 DOOR THRESHOLD SUPPORT ZEE ANGLE CORRODED. THE CORROSION WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 887-927. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED AT STA 285-370. THE CORRODED SECTION OF Z-ANGLE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND MAIN CABIN FLOORBEAM UPPER FLANGE CORRODED AT STA 344, LBL 10. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-51, FIGURE 206.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND MAIN CABIN FLOORBEAM UPPER FLANGE CORRODED AT STA 328, WL 208. A NEW FLOORBEAM SECTION WAS INSTALLED IAW SRM 53-10-51.

Part: ATTACH ANGLE — CORRODED (R1 DOOR FRAME) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND R-1 DOOR JAMB THRESHOLD ATTACH ANGLE CORRODED. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 982, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.

Part: ATTACH ANGLE — CORRODED (L1 DOOR) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND L-1 DOOR THRESHOLD ATTACH ANGLES CORRODED. NEW ANGLES WERE INSTALLED IAW SRM 51-40-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND RT I/B SEAT TRACK CORRODED AT STA 907-927. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52.

Part: GALLEY TRACK — CORRODED (STA 270-294) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND GALLEY TRACK CORRODED AT STA 270-294, RBL 14. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-52, PAGE 202, STEP 11 AND 12 AND SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,323 hrs · 25,618 cycles

INSPECTION FOUND UPPER FLANGE OF MAIN CABIN FLOORBEAM CORRODED AROUND THREE FLOORBOARD ATTACH HOLES AT STA 312, RBL 36. A REPAIR STRAP DOUBLER WAS INSTALLED IAW SRM 53-00-51.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 48,578 hrs · 25,224 cycles

INSPECTION FOUND A 1 INCH CRACK AND A 1.25 INCH CRACK IN LT HORIZONTAL STABILIZER LOWER INTERSPAR SKIN BETWEEN STAB STA 147 AND 157. THE SKIN WAS REPAIRED IAW ECRA 5510-01699.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 48,578 hrs · 25,224 cycles

INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L AT STA 504. REPAIRED IAW ECRA 5310-03262.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 48,578 hrs · 25,224 cycles

INSPECTION FOUND A 0.55 INCH CRACK IN STRINGER 16R AT BS 504. REPAIRED IAW ECRA 5310-03262.

Part: CONTROL PANEL — MALFUNCTIONED (FIRE DETECTION) · airframe 47,870 hrs · 24,833 cycles

THE CARGO FIRE DETECTION LOOP LIGHTS ILLUMINATED AFTER DEPARTING IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE COCKPIT FIRE SUPRESSION PANEL WAS REMOVED AND REPLACED IAW MM 26-23-10 AND 26-16-10. OPERATIONAL TESTS WERE GOOD.

Part: SKIN — CRACKED (#1 ENG PYLON) · airframe 45,809 hrs · 23,726 cycles

INSPECTION FOUND A 1" CRACK IN UPPER SURFACE OF #1 ENGINE PYLON PANEL 5727L CUTOUT. REPAIRED CRACK IAW ECRA 5430-01230, REV B.

Part: SPLICE PLATE — CORRODED (STA 858) · airframe 45,809 hrs · 23,726 cycles

INSPECTION FOUND AFT CARGO PIT CENTER FLOOR SPLICE PLATE CORRODED AT STA 858. THE CENTER FLOOR SPLICE WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SKIN — CRACKED (#6 SLAT) · airframe 45,809 hrs · 23,726 cycles

INSPECTION FOUND A 2" CRACK IN #6 LEADING EDGE SLAT SKIN AT EDGE OF RIVET HOLE ON SLAT LOWER SIDE BY I/B AUX TRACK. A REPAIR WAS INSTALLED IAW SRM 57-43-01, FIGURE 206.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 45,809 hrs · 23,726 cycles

INSPECTION FOUND FORWARD BAGGAGE BIN FLOOR NUT PLATE STRIP CORRODED AT STA 500D. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02.

Part: FRAME — CORRODED (STA 867) · airframe 45,809 hrs · 23,726 cycles

INSPECTION FOUND FRAME CORRODED AT STA 867 BETWEEN STRINGERS 27L AND 27R. THE CORRODED SECTION OF FRAME WAS REMOVED AND A SHEAR TIE AND FILLER WERE INSTALLED IAW SRM 53-00-07, FIGURE 208.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 39,668 hrs · 20,410 cycles

INSPECTION FOUND THREE 1 INCH CRACKS AT LIGHTENING HOLES IN C-1 DOOR INNER SKIN. REPAIRED IAW ECRA 5230-01548.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,661 hrs · 20,405 cycles

INSPECTION FOUND CABIN FLOORBEAM UPPER CAP CORRODED AT NUT PLATE AT STA 986.5. A NEW T CAP AND SPLICE REPAIR WAS INSTALLED IAW ECRA 5321-01052.

Part: ATTACH FITTING — CRACKED (LT & RT MLG) · airframe 39,668 hrs · 20,410 cycles

INSPECTION FOUND THE LT AND RT MLG AFT FALSE SPAR O/B ATTACH FITTINGS CRACKED. BOTH CRACKS WERE 2 INCHES LONG. THE ATTACH FITTINGS WERE REMOVED AND REPLACED IAW ECRA 5740-01423, REV B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,668 hrs · 20,410 cycles

INSPECTION FOUND SEAT TRACK CORRODED IN RT FORWARD GALLEY AREA BETWEEN BS 277 AND 294. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 39,668 hrs · 20,410 cycles

INSPECTION FOUND AFT PRESSURE BULKHEAD STIFFENER CORRODED BELOW LAVS AT BS 1016, BL 0. THE CORRODED SECTION WAS CUT OUT AND A NEW SECTION WAS INSTALLED WITH DOUBLERS IAW SRM 53-80-08 AND 51-70-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,668 hrs · 20,410 cycles

INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT GALLEY AREA, BS 907 - 947. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-00-52.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 39,668 hrs · 20,410 cycles

INSPECTION FOUND A .5 INCH CRACK AT RIVET HOLES OF NR 3 SLAT PANEL ON I/B SIDE OF PANEL. FILLER AND DOUBLER WERE INSTALLED IAW BOEING DRAWING 65C30133.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 39,668 hrs · 20,410 cycles

INSPECTION FOUND APB CENTER STIFFENER BELOW LAVS CORRODED NEAR BS 1016 BULKHEAD, BL 0. REPAIRED IAW SRM 53-80-08 AND 51-70-11.

Part: SKIN — CRACKED (NR 1 ENG PYLON)

INSPECTION FOUND A .5 INCH CRACK COMING FROM CUTOUT FOR PANEL 5724 ON INBOARD SKIN OF NR 1 ENGINE PYLON. REPAIRED IAW ECRA 5430-01204.

Part: FLOORBEAM — CORRODED (BS 986.5)

INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AROUND NUT PLATES AT STA 986.5 FROM BL 0 TO LBL 50. THE UPPER CHORD OF FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03450 AND SRM 53-00-51.

Part: SENSOR — OUT OF ADJUST (LANDING GEAR)

AFTER TAKEOFF, CREW COULD NOT RETRACT MLG. DIVERTED TO CRP. INSPECTION FOUND GROUND SPOILER INTERLOCK VALVE CABLE OUT OF RIG. RIGGED PER MM 32-09-01 PG 502 AND FOUND AIR SAFETY SENSOR NOT LINED UP WITH TARGET. ADJUSTED PER MM 32-09-01 AND DID GEAR SWING SEVERAL TIMES WITH NO FAULTS.

Part: LOGIC CARD — INOPERATIVE (RT MLG)

THE RT MLG RED LIGHT REMAINED ON AFTER GEAR RETRACTION. WHEN THE GEAR WAS CYCLED BOTH THE MAIN GEAR RED AND GREEN LIGHTS ILLUMINATED. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND THE M986 LANDING GEAR LOGIC CARD AT FAULT. THE M986 LOGIC CARD WAS REPLACED. A LANDING GEAR EXTEND AND RETRACT TEST WAS PERFORMED WITH GEAR OPERATION AND INDICATIONS CHECKING GOOD.

Part: INTERCOSTAL — CORRODED (BS 950)

HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT STATION 950 BETWEEN RBL 47 AND 55. THE INTERCOSTAL WAS REPLACED IAW ECRA 5310-03258. (M)

Part: INTERCOSTAL — CORRODED (BS 950)

HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT STATION 950 BETWEEN RBL 25 AND RBL 40. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03258. (M)

Part: INTERCOSTAL — CORRODED (BS 950)

HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT STATION 950 FROM LBL 17 TO 25. THE INTERCOSTAL WAS REPLACED IAW ECRA 5310-03258. (M)

Part: FLOOR SUPPORT — CORRODED (BS 291-312)

HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN BS 291 AND 312, 12 INCHES RIGHT OF CENTERLINE. AN INTERCOSTAL WAS FABICATED AND INSTALLED IAW ECRA 5310-03258. (M)

Part: FLOOR SUPPORT — CORRODED (BS 328-344)

HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN BS 328 AND 344, 12 INCHES LEFT OF CENTERLINE. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03258. (M)

Part: FLOOR SUPPORT — CORRODED (BS 344-360)

HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN BS 344 AND 360, 14 INCHES LEFT OF CENTERLINE. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03258. (M0

Part: ANGLE — CORRODED (R-1 DOOR)

HOU - INSPECTION FOUND Z-ANGLE CORRODED AT R-1 DOOR. THE CORROSION WAS REMOVED IAW SRM 51-10-02. (M)

Part: FLOOR SUPPORT — CORRODED (BS 312-328)

HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN BS 312 AND 328, 12 INCHES LEFT OF CENTERLINE. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03258. (M)

Part: FLOORBEAM — CORRODED (BS 986.5)

HOU - INSPECTION FOUND FLOORBEAM CORRODED AT STATION 986.5. THE FLOORBEAM WAS REPLACED IAW SRM 53-00-51. (M)

Part: INTERCOSTAL — CORRODED (BS 950)

HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT STATION 950 BETWEEN RBL 8 AND 18. THE INTERCOSTAL WAS REPLACED IAW ECRA 5310-03258. (M)

Part: ANGLE — CORRODED (L-1 DOOR)

HOU - INSPECTION CORROSION ON Z-ANGLE AT L-1 DOOR. THE ANGLE WAS REPLACED IAW SRM 51-10-02. (M)

Part: FLOORBEAM — CORRODED (BS 344)

HOU - INSPECTION FOUND FLOORBEAM CORRODED AT BS 344 ON LEFT AND RIGHT SIDE. A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 53-10-51. (M)

Part: SKIN — DAMAGED (BS 500)

FLT NR 1627 - EWR - FUSELAGE SKIN DAMAGED AT FS 500. REPAIRED AREA PER SRM 53-00-01 PG 204/206 SRM 53-00-07 PG 212/214 AND 51-70-11 PG 116. (M)

Part: TOGGLES — BENT (LT TE FOREFLAP)

CLE - FLT 0150 - AIRCRAFT BEGAN TO ROLL WHEN FLAPS WERE EXTENDED ON FINAL APPROACH TO CLE. FOUR UNITS OF RIGHT AILERON WITH RUDDER TRIM AT ONE UNIT RIGHT WAS REQUIRED TO MAINTAIN CONTROL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT OUTBOARD FOREFLAP TOGGLES BENT. BOTH THE INBOARD AND OUTBOARD TOGGLES WERE REPLACED PER MM 27-51-47. THE FLAPS WERE CYCLED THROUGH FULL RANGE AND ALL OPERATION WAS NORMAL. (X)