N511DA

Part: ANGLE — CRACKED (NR 3 SLAT) · airframe 70,711 hrs · 47,774 cycles

A 1.25 INCH VISIBLE CRACK ON NR 3 SLAT AT O/B STOP PAD. REPAIRED PER MM 57-54-0 PG 816.

Part: RIB — CRACKED (NR 7 SLAT) · airframe 70,711 hrs · 47,774 cycles

A .75 INCH CRACK IN L/E NOSE RIB OF NR 7 SLAT AT O/B SIDE OF ACTUATOR ATTACH FITTING. REPAIR PER M/M 57-54-0.

Part: ACTUATOR — LEAKING (NR 7 SLAT) · airframe 70,168 hrs · 47,426 cycles

A SYS HYD LOSS ON TAKEOFF, FOUND NR 7 LEADING EDGE SLAT ACTUATOR LEAKING FROM AFT SIDE. REPLACED NR 7 LEADING EDGE ACTUATOR.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,981 hrs · 47,305 cycles

CABIN EMERGENCY LIGHTS INOP AFT OF ROW 26. REPLACED BATTERY PACK, CKS GOOD.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 69,889 hrs · 47,238 cycles

F/A REPORTED ELECTRICAL SMELL IN AFT GALLEY. FOUND COFFEEMAKER AT FAULT. REPLACED SAME.

Part: ANGLE — CORRODED (ENGINE MOUNT)

ON HUSH-KIT MOD, FOUND LT NR 2 AFT MOUNT SUPPORT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED LT AFT MOUNT SUPPORT CHORD ANGLE WITH ONE OF NEW MFG.

Part: ANGLE — CORRODED (ENGINE MOUNT)

ON HUSH-KIT MOD, FOUND RT NR 2 ENG AFT MOUNT SUPPORT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED CHORD ANGLE WITH ONE OF NEW MFG.

Part: ANTISKID MODULE — SPLIT (RT)

WHILE STOPPED ON THE TAXI WAY DURING TAXI OUT WITH BRAKES SET. A/C STARTED TO ROLL. S/O NOTED 'B' SYSTEM PRESSURE DROPPING TO ZERO WITH BOTH HYD B LIGHTS ON. FOUND RT ANTI-SKID MODULE CASE BROKEN IN TWO AT FILTER CASE. REPLACED MODULE.

Part: SKIN — DAMAGED (RUDDER)

UPPER RUDDER DAMAGED TORN 2 INCHES BY 7 INCHES AT L/E RUDDER STA 180 TO 187. DRILLED UP REPAIR PER SRM 55-20-3 FIG 1. INSTALLED REPAIR PER SRM 55-20-3.

Part: STIFFNER — CRACKED (LE WING SPAR)

FOUND ON MV2 CK INBD AND OUTBD SPAR STIFFENERS CRACKED AT THE NUMBER 7 SLAT I/B TRACK ON THE FWD WING SPAR. REPAIRED PER MM 57-20-21.

Part: SKIN — CORRODED (BS 685)

THE LOWER SKIN OF THE STRINGER 26R SKIN LAP SPLICE WAS FOUND WITH A 5 INCH LONG AREA OF CORROSION OVER THE UPPER TWO FASTENER ROWS. THE CORRODED AREA WAS CUT AWAY AND REPAIRED WITH AN INTERNAL REPAIR DOUBLER PER ER/A 368232-14, REV A.

Part: STIFFNER — CRACKED (LE WING SPAR)

FOUND ON MV2 CK, L/E WING SPAR STIFFENER CRACKED AT THE NUMBER 7 SLAT O/B TRACK O/B SIDE. REPAIRED PER MM 57-20-21.

Part: RIB — CRACKED (NR 2 LE SLAT)

FOUND ON MV2 CK, .375 INCH CRACK ON NR 2 L/E SLAT RIB O/B OF ACTUATOR ATTACH BOLT. REPAIRED PER MM 57-54-0.

Part: WEB — CRACKED (BS 1303)

FOUND ON MV-2 CK, 1 INCH CRACK IN STA 1303 WEB WL 270 LBL 20 FIN STRINGER 8. REPAIRED PER SRM 53-10-4.

Part: WEB — CRACKED (BS 1303)

FOUND ON MV-2 CK, 1 INCH CRACK STA 1303 WEB WL 270 RBL 20 FIN STRINGER 8. REPAIRED PER SRM 53-10-4.

Part: FRAME — CORRODED (BS 740)

FOUND DURING MV2 CORROSION VISIT NRC 226, CORROSION AT SUPPORT FRAME FOR ACCESS PANEL 3455R AT LWR SURFACE I/B OF FWD HINGE. REPAIRED PER M/M 53-30-1 FIG 804.

Part: STRINGER — CRACKED (BS 936)

FOUND DURING MV2 CORROSION VISIT NRC 196, DURING UPPER WING INSPECTION OPERATION 5621, FOUND 1.5 INCH VISIBLE CRACK AT STR 18 A RT AT STA 936, IN LOWER FLANGE OF STR 18 A. REPAIRED PER M/M 53-12-0.

Part: SKIN — CRACKED (BS 442)

LFEC INSPECTION REVEALED A CRACK INDICATION NEAR THE LOWER FASTENER ROW OF THE LOWER SKIN AT THE STRINGER 4R SKIN LAP SPLICE NEAR FS 442. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE AT FS 442. THE CRACK WAS REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366845-14AD, REV A.

Part: SKIN — CRACKED (BS 405)

LFEC INSPECTION INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4R SKIN LAP SPLICE NEAR FS 405. HFEC INTERNAL INSPECTION OF THE SKIN LAP CONFIRMED A CRACK AT FS 405. THE CRACK WAS REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 366843-14AD, REV A.

Part: LIGHT — INOP (R1 DOOR)

R1 OVER DOOR EMER LIGHT INOP. REPLACED LIGHT, CKS GOOD.

Part: LIGHT — INOP (L2 DOOR)

L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS CHKS GOOD.

Part: HOSE — LEAKING (LT ELEVATOR)

AFTER T/O, LOST A-SYS HYD FLUID. RETURNED TO MSY. FOUND LEAKING SUPPLY LINE AT LEFT ELEVATOR PCU. REPLACED LINE.

Part: WEB — CRACKED (FUSELAGE)

FOUND AT D-1 LETTER CHECK, WEB CRACKED RT FWD LOWER AFT AIRSTAIR AREA. REPAIRED PER M/M 53-11-0.

Part: RIB — CRACKED (NR 3 LE SLAT)

A 1.5 INCH CRACK IN DOUBLER NR 3 SLAT I/B NOSE RIB AT ACTUATOR ROD END ATTACH. REPAIRED PER M/M 57-54-0.

Part: SKIN — CRACKED (R1 DOOR)

FOUND ON C2 LETTER CK, R-1 DOOR OUTER SKIN CRACKED 1 INCH UPPER FWD CORNER JUST BELOW GATE. REPAIRED PER MM 52-11-01.

Part: WIRE — CUT (CABIN)

ON L/O 2 CK, FOUND EMERGENCY TRACK LIGHTING INOP NEAR L1 DOOR. REPAIR SPLICED WIRES, OPN CKS GOOD PER M/M.

Part: HEAT MANIFOLD — BLOWN (NR 2 ENGINE)

NR 2 ENG DETECTOR ILLUM AFTER POSITIONING TO A AND TESTING LIGHT STAYED ON AND FOLLOWED BY NR 2 FIRE WARNING LIGHT. THROTTLE TO IDLE ALL INDICATIONS NORMAL AND ALL TESTS NORMAL, THROTTLE IN IDLE FOR DURATION. REPLACED NR 2 ENG FUEL HEAT MANIFOLD.

Part: TRACK LIGHT — BROKEN (CABIN)

EMERGENCY TRACK LIGHTING AT 22 RIGHT SIDE IS MISSING PARTS OF PLASTIC STRIP, RED COVER WILL NOT STAY IN. REPLACING TRACK PIECE, ALL LIGHTS SECURE AND TEST GOOD.

Part: ACCESSORY UNIT — MALFUNCTIONED (LANDING GEAR)

ON GEAR RETRACTION, THE RIGHT GEAR RED LANDING GEAR DISAGREEMENT LIGHT REMAINED ILLUMINATED AND REMAINED ILLUMINATED UNTIL GEAR EXTENDED FOR LANDING. PERFORMED OPERATION TEST OF UPLOCK SENSORS PER MM 32-61-811, REPLACED LANDING GEAR ACCESSSORY UNIT PER 32-09-121, CLEANED ALL SENSORS, OPERATION NORMAL.

Part: SKIN — CRACKED (LT AILERON)

DURING INSPECTION, LEFT WING O/B AILERON WAS FOUND WITH LOWER OUTBOARD SKIN CRACKED. REPAIRED PER MM 57-51-0 PG 801.

Part: ANGLE — CRACKED (NR1 LE SLAT)

ATTACH ANGLE BROKEN NR 1 L.E. FLAP ACTUATOR BOX. FOUND DURING B-1 LTR CK TPAMM. REPAIRED PER MM 57-20-21.

Part: ANGLE — CRACKED (NR 2 LE SLAT)

FOUND DURING B-1 LETTER CHECK - .50 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTATCH ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0.

Part: STIFFENER — CRACKED (RT WING FWD SPAR)

FOUND DURING B-1 LETTER CHECK - 1 INCH CRACK LWR END SPAR STIFFENER AT NR 6 L/E SLAT I/B TRACK I/B ANGLE. REPLACED PER MM 57-20-21.

Part: SKIN — CORRODED (FS 720)

DURING INSPECTION, THE RAM AIR ACTUATOR ACCESS DOOR CUTOUT WAS FOUND TO HAVE CORROSION ON THE ATTACH FLANGE IN THE LT AFT CORNER. IN ACCORDANCE WITH FAA/DER FORM 8110-3, DATED 1-17-96, THE DAMAGE HAS BEEN BLENDED TO 0.59 MINIMUM FLANGE THICKNESS.

Part: SKIN — CORRODED (BS 1005)

BELLY SKIN WAS CORRODED REQUIRING A 1 INCH BY 4 INCH CUTOUT OF THE SKIN. THE STA 1009 BUTT SPLICE IS AFT OF THE CUTOUT AND FORWARD OF AN EXISTING REPAIR. REPAIRED PER SRM 53-30-3 FIG 3A.

Part: EEL HARNESS — DAMAGE (CENTER CARGO DR)

CENTER CARGO EMERGENCY LIGHT INOP. REPLACED RACK AND REPAIRED DAMAGED WIRE HARNESS, OPERATION NORMAL.

Part: EEL PWR SUPPLY — FAILED (CABIN)

DURING DEPARTURE CHECK, EMERGENCY TRACK LIGHT IN FWD CABIN DO NOT TEST. REPLACED BATTERY PACK M9026, OPERATION NORMAL.

Part: ANGLE — CRACKED (FS 1183)

FOUND DURING A-2 LETTER CHECK, CRACK IN ANGLE BL 8 LEFT STATION 1183 ON I/B RADIUS AT BOTTOM OF BULKHEAD SUPPORT ANGLE. REPAIRED PER MM 53-11-0.

Part: ANGLE — CRACKED (RT WING)

FOUND DURING A-2 LETTER CHECK, 1 INCH CRACK NR 11 SPOILER ACTUATOR SUPPORT FITTING I/B ATTACH ANGLE BELOW SUPPORT FITTING MOUNT BOLT. REPAIRED PER SRM 57-50-6 FIG 7.

Part: RIB — CRACKED (NR 2 LE SLAT)

FOUND DURING A-2 LETTER CHECK, .25 INCH CRACK NR 2 L/E SLAT ACT ATTACH I/B RIB. REPAIRED PER MM 57-54-0.