N18513

Part: SWITCH — INOPERATIVE (LT MLG)

THE LEFT GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF FROM ABQ. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ON. THE FLIGHT WAS CONTINUED TO IAH WITH PUMPS IN HIGH AND WHEN GEAR WAS EXTENDED INDICATIONS WERE NORMAL. MAINTENANCE REPLACED THE OVERLINK SWITCH. THE GEAR WAS SIMULATED UP AND DOWN AND ALL INDICATIONS WERE NORMAL.

Part: LONGERON — CRACKED (BS 229)

INSPECTION FOUND A 3 CRACK IN LONGERON 29L AT STA 229. A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURES 17 AND 18.

Part: CABLES — OUT OF ADJUST (TAIL CONE)

THE TAILCONE PULL CHECK WAS HIGH. THE CABLES RELEASED AT 50 POUNDS AND THE CONE DID NOT DROP. MAINTENANCE FOUND AFT RT LOWER TAILCONE LATCH MECHANISM BINDING. THE TAILCONE RELEASE SYSTEM CABLES WERE RIGGED IAW CARD 08-5350-1-0007 AND OPERATION CHECKED GOOD.

Part: SHEAR TIE — CORRODED (BS 600)

INSPECTION FOUND SKIN SHEAR TIE CORRODED IN FORWARD CARGO COMPARTMENT AT BS 600, STRINGER 27R. THE SHEAR TIE WAS REMOVED IAW SRM 57-30-2. A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, 51-10-2, AND 51-30-2.

Part: ANGLE — CRACKED (BS 980)

INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF ATTACH ANGLE UPPER END AT STA 980 JUST BELOW LONGERON 15L, AFT LAV OUTBOARD WALL. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 3.

Part: LONGERON — CRACKED (BS 965)

INSPECTION FOUND LONGERON 17R CRACKED AT STA 965, RT LAV A SPLICE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 18.

Part: INTERCOSTAL — CRACKED (BS 146.5-160)

INSPECTION FOUND INTERCOSTAL CRACKED AT STA 146.5-160 BETWEEN LONGERONS 12 AND 13R. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5320-01495.

Part: CLIP — CRACKED (BS 980)

INSPECTION FOUND SKIN CLIP CRACKED AT STA 980 BETWEEN LONGERONS 14 AND 16L. THE CLIP WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 3.

Part: DOOR PAN — WORN (AFT PRESS BLKHD)

INSPECTION FOUND 15 EACH ELONGATED FASTENER HOLES ON APB UPPER DOOR PAN. THE HOLES WERE REAMED FOR SECOND OVERSIZE HILOCK IAW SRM 51-30-5.

Part: BULKHEAD WEB — BUCKLED (AFT LAVATORY)

INSPECTION FOUND THE LT ENGINE PYLON FRONT SPAR WEB(LAV BULKHEAD) BUCKLED AT BOTTOM WITH A 2 CRACK AT BOTTOM OUTBOARD CORNER. THE BULKHEAD WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Part: CLIP — CRACKED (BS 945)

INSPECTION FOUND A 3 CRACK IN SKIN CLIP AT STA 945 BETWEEN LONGERONS 14 AND 15L. A CLIP REPAIR WAS INSTALLED IAW SRM 53-03.

Part: INTERCOSTAL — CRACKED (BS 150)

INSPECTION FOUND A 4 CRACK IN INTERCOSTAL AT STA 150, LONGERON 11R. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5320-01495.

Part: STANDOFF — CORRODED (BS 207)

INSPECTION FOUND FLOOR SUPPORT STANDOFF CORRODED AT STA 207 RIGHT, BETWEEN INBOARD SEAT TRACK AND CENTER STANDOFF. THE STANDOFF WAS REMOVED AND A NEW STANDOFF WAS FABRICATED AND INSTALLED IAW SRM 51-10-3.

Part: STANDOFF — CORRODED (BS 220-229)

INSPECTION FOUND STANDOFF CORRODED AT STA 220-229 LT, TWENTY INCHES FROM CENTER. THE STANDOFF WAS REMOVED AND A NEW STANDOFF WAS FABRICATED AND INSTALLED IAW SRM 51-10-3.

Part: JAMB — CRACKED (PAX DOORWAY)

INSPECTION, FOUND A 3 CRACK IN AFT ENTRY DOOR JAMB. A WEB AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-05.

Part: BULKHEAD WEB — BUCKLED (AFT LAVATORY)

INSPECTION FOUND RT AFT LAV BULKHEAD WEB BUCKLED AT BOTTOM. A WEB AND TEE SUPPORT WERE FABRICATED AND INSTALLED IAW SRM 53-03.

Part: BULKHEAD WEB — CRACKED (AFT PRESS BLKHD)

INSPECTION FOUND A 3 CRACK IN AFT PRESSURE BULKHEAD DOOR FRAME. THE CRACK WAS LOCATED AT INBOARD END AND TOP OF DOOR JAMB ON FORWARD SIDE OF APB. THE CRACKED FRAME SECTION WAS REMOVED AND A NEW UPPER FRAME SECTION WAS INSTALLED ON DOOR JAMB IAW SRM 51-30-2.

Part: BULKHEAD WEB — CRACKED (AFT PRESS BLKHD)

INSPECTION, FOUND TWO 1.75 CRACKS IN LT AFT PRESSURE BULKHEAD DOOR CUTOUT UPPER CORNER BELOW RADIUS. REPAIRED IAW DOUGLAS DRAWING J060088.

Part: CONTROL VALVE — OUT OF ADJUST (RT BRAKE SYST)

THE AIRCRAFT WAS RETURNED TO DTW FOR REPORTS OF A RUBBER ODOR OBSERVED IN THE CABIN. THERE WERE NO VISIBLE SIGNS OF SMOKE. THE ODOR BEGAN TO DISSIPATE WITHIN THREE MINUTES. THERE WERE NO ENGINE OR AIRCRAFT SYSTEM PROBLEMS NOTED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THIS WAS THE SECOND AIR RETURN FOR THE SAME PROBLEM. THE COALESCER BAGS HAD BEEN REMOVED AND REPLACED PREVIOUSLY. TROUBLESHOOTING FOUND THE RIGHT BRAKE CONTROL VALVE OUT OF ADJUSTMENT. THE BRAKE CONTROL VALVE WAS ADJUSTED IAW MM 32-42-2. A HIGH POWER ENGINE RUN WAS PERFORMED WITH THE PACKS SET HOT AND NO ODORS WERE NOTED.

Part: SLIDE — LOW PRESSURE (L1 DOOR)

INSPECTION FOUND THE L-1 DOOR EMERGENCY SLIDE PRESSURE LOW. THE SLIDE WAS REMOVED AND REPLACED.

Part: CABLES — OUT OF RIG (TAILCONE)

HOU - THE TAILCONE EXTERIOR HANDLE FAILED TEST PULLING AT 50 POUNDS AND THE TAILCONE DID NOT PROP. THE TAILCONE WAS RIGGED AND ADJUSTED IAW WORK CARD 08-5350-1-0007. (M)

Part: CABLES — OUT OF RIG (TAILCONE)

HOU - THE TAILCONE INTERIOR RELEASE HANDLE PULLED AT 45 POUNDS AND THE TAILCONE DID NOT DROP. THE TAILCONE WAS ADJUSTED AND RIGGED IAW WORK CARD 08-5350-1-0007. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH - INSPECTION FOUND THE LT EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE POWER SUPPLY WAS REMOVED AND REPLACED AND OPERATION OF THE LIGHT WAS RESTORED. (X)