N416DA

Part: BEAM — CRACKED (BS 1183)

THE RBL 17.8 VERTICAL DOOR BEAM ON THE FS 1183 BULKHEAD WAS FOUND WITH A SMALL CRACK IN A FASTENER HOLE COMMON TO AN EXISTING REPAIR. THE CRACK WAS REMOVED BY OVERSIZING THE .0625 INCH FASTENER HOLE TO .296 DIA WITH AN ADDITIONAL .0625 OVERSIZE. THE CRACK WAS FOUND WITH A BOLT HOLE EDDY CURRENT INSPECTION AND IS OUTSIDE THE CRACK AREA OF AD 99-18-05. THE HOLE WAS BUSHED AND REPAIR RE-INSTALLED PER ER/A 368793-14.

Part: SPAR WEB — CRACKED (CENTER WING)

CENTER WING, REAR SPAR, WEB LBL 17, CRACK REPAIR. THE CENTER WING REAR SPAR WEB WAS FOUND WITH A .5 TYPICAL CRACK NEAR THE UPPER SPAR CAP. THE CRACK IS TYPICAL OF BAC S/B 727-57A0182. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PER ER/A 368400-14AD, REV A.

Part: WEB — CRACKED (BS 1290)

.25 INCH CRACK ON LEFT VERT TORQUE BOX WEB LWR LIGHTING HOLE STA 1290. ROUTE OUT CRACK PER MM 53-11-0.

Part: STIFFENER — CRACKED (LT WING)

2 INCH VISIBLE CRACK IN VERT SPAR STIFFENER I/B SIDE OF O/B TRACK NR 3 L/E SLAT. REPAIRED PER MM 57-20-21 P 813.

Part: STRINGER — CRACKED (BS 940)

FOUND ON F1 LETTER CK, 1 INCH CRACK IN STRINGER 18A AT STA 940 IN THE UPPER AND LOWER RADIUS RT. REPAIRED PER MM 53-12-0.

Part: STIFFENER — CRACKED (NR 7 SLAT)

L/E SPAR STIFFENER CRACKED AT NR 7 SLAT I/B TRACK O/B SIDE OF TRACK. REPAIR PER MM 57-20-21.

Part: SKIN — CRACKED (S DUCT)

.5 INCH CRACK ON DUCT HOUSING SKIN AT PANEL 9524 RT SIDE. REPAIR PER MM 54-30-0.

Part: LIGHT — BROKEN (ROW 10D)

EMERGENCY LIGHT AT SEAT 10D BROKEN. REPLACED BULBS AND LIGHT COVER ASSY.

Part: LIGHT — INOPERATIVE (R1 DOOR)

R1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY AND BATTERIES, OPS NOW OK.

Part: BATTERY — DISCHARGED (AFT AIRSTAIR)

AFT AIRSTAIR EMERG EXIT LIGHT INOP. REPLACED BATTERIES, OPS NOW OK.

Part: SKIN — CRACKED (BS 440-460)

FUSELAGE SKIN FS 440-460 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 440 AND 460. THE CRACK WAS ROUTED OUT AND REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 367248-14AD.

Part: SKIN — CRACKED (BS 481-681)

FUSELAGE SKIN FS 481-681 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 6 CRACKS IN TWO ADJACENT FRAME BAYS. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 367247-14AD.

Part: PANEL — CRACKED (RT ELEVATOR)

2 INCH CRACK NR 2 BALANCE BOARD CLOSE OUT PANEL, RT ELEVATOR. REPAIR PER SRM 55-20-3.

Part: RIB — CRACKED (RT VERT STAB)

VERTICAL FIN RIB CHORD CRACKED 1.25 INCH FIN STA 133.800, AT STR 8 ATTACH BOLT RT SIDE. REPAIR PER M/M 55-30-0 FIG 802.

Part: CLIP — CRACKED (LT VERT STAB)

1 IN CRACK IN LT VERT FIN SKIN TO RIB ATTACH CLIP, STA 180.600 ABOVE STR 10. REPAIR PER M/M 55-30-0 FIG 803.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING L/O, FOUND OVERWING EMERGENCY EXIT LIGHTS NOT ILLUM AT LT WING STA 804. REPLACED BATTERY PACK, OP CKS NORMAL.

Part: FAN — FAILED (COCKPIT)

SMOKE AND FUMES IN COCKPIT AND CABIN, RAN CK LIST AND COULD NOT FIND SOURCE. ALSO, ELECTRICAL BURNT PLASTIC SMELL. INSPECTED COALESCER BAGS, CKS GOOD. INSPECTED E & E AREA, CKS GOOD. INSPECTED GALLEY AREA, CKS GOOD. FOUND SMELL COMING FROM GASPER FAN, RAN PACKS W/ENGINES AND GASPER FAN OFF. NO BURNING SMELL. FWD GASPER FAN TO MCO PER MEL 21-00-24. PULLED AND COLLARED C/B. REPLACED GASPER FAN.

Part: LINE — FAILED (A-HYD SYST)

20 MIN AFTER TAKEOFF FROM ABQ, HAD TOTAL LOSS OF A SYSTEM HYDRAULICS. C/W POM PROCEDURES. DIVERTED TO DFW. REPLACED BROKEN LINE TO A SYSTEM HYDRAULIC MODULE. REPLACED NR 1 ENGINE DRIVEN HYD PUMP. PRESSURE AND LEAK CHECK OK.

Part: SKIN — CRACKED (L1 DOOR)

FOUND ON E1 LETTER CK, .25 INCH CRACK IN L1 DOOR SKIN AT LOWER HINGE CUTOUT. REPAIRED PER MM 52-11-0.

Part: SKIN — CORRODED (BS 720)

CORROSION DAMAGE FOUND IN THE LWR SKIN AT APPROX FS720C+10 AT S26R. REPAIRED PER ERA 331866-14.

Part: STRINGER — CRACKED (BS 940)

SEVERAL FASTENER HOLES AT S18A AT FS 940 ON THE LT SIDE WERE FOUND CRACKED. CRACKS WERE IN THE STRINGER ONLY AND DID NOT EXTEND TO THE UNDERLYING STRUCTURE. REPAIRED PER ERA 331854-14.

Part: FRAME — CRACKED (BS 761)

WHILE PERFORMING THE REPAIR/MOD PER EO 4-61904-3AD. MAINTENANCE FOUND THE 2ND FASTENER BELOW THE FLOOR LINE TO BE AT A DIAMETER OF 0.375. REPAIRED PER ERA 331852-14AD.

Part: SKIN — CORRODED (BS 1009)

CORROSION WAS FOUND AT STA 1009 AND STR 28L ON THE INTERNAL SKIN BUTT SPLICE STRAP IN AN AREA PREVIOUSLY REPAIRED. THE PREVIOUS REPAIRS WERE REMOVED, AND RE-REPAIRED. REPAIRED PER ERA 237701-14.

Part: DOUBLER — DAMAGED (RT TE FLAP)

REPAIR DOUBLER IS CRACKED AT LWR AFT SPAR 21 AND 35 FROM I/B END. THIS DAMAGE WAS REPAIRED PER M/M 57-52-0, FIG 802. THIS DAMAGED WAS RECORDED ON N/R 007474 AND 007475.

Part: ANGLE — CRACKED (VERT STAB)

ANGLE CRACKED INSIDE OF VERT STAB 4TH BAY DOWN FROM OPENING STR 5 ON RT SIDE CRACK IS ON VERT LEG. REMOVED FASTENERS, DRILLED OP REPAIR PARTS PER MM 55-30-0 PG 802. INSTALLED DOUBLER PER MM 55-30-0 PG 802.

Part: SKIN — DAMAGED (RT TE FLAP)

COVE SKIN IS CRACKED 32 FROM I/B END. THIS DAMAGED WAS RECORRED ON SHOP N/R 007470 AND REPAIRED PER M/M 57-52-0 FIG 809.

Part: WEB — CRACKED (VERT STAB)

VERT WEB CRACKED INSIDE STABILIZER ABOVE S-DUCT STA 1303. REPAIRED PER SRM 53-10-4 FIG 17, LT AND RT SIDE.

Part: SKIN — DAMAGED (HORIZ STAB)

OUTER SKIN DAMAGED AT FASTENER HOLE ON PANEL 9115. REPAIRED PER SRM 55-30-3 FIG 3.

Part: STRINGER — CRACKED (VERTICAL STAB)

STRINGER CRACKED INSIDE VERTICAL STAB 4TH BAY UP FROM ACCESS 9504 STR 8R. STOP DRILLED CRACK, DYE CHECKED PER PS900-6-3, NR 1 FABRICATED REPAIR PER M/M 53-30-0 FIG 803. INSTALLED DOUBLER PER MM 53-30-0 FIG 803.

Part: SKIN — SEPARATED (RT ELEVATOR)

RT ELEVATOR I/B T/E SKIN, SEPARATED. DRILLED REPAIR FASTENER HOLES PER M/M 55-20-0 PG 801. INSTALLED REPAIR FASTENER PER M/M 55-20-0 PG 801.

Part: BATTERY PACK — DISCHARGE (COCKPIT)

EMERG LIGHT IN THE COCKPIT IS INOP. REPLACED BATTERY PACK ASSY AND THE BATTERIES CK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

L1, R1, L2 AND R2 DOORS EMERGENCY LIGHTS INOP. REPLACED BATT PACKS.

Part: BATTERY — DISCHARGED (CABIN)

ON S/C, FOUND AFT SECTION OF EMERGENCY ESCAPE LIGHTS INOP. REPLACED BATTER, OPS NORMAL.

Part: SKIN — CRACKED (VERT STAB)

A .1875 INCH CRACK IN SKIN RT LOWER FWD CORNER OF VERTICAL STAB SADDLE PLATE CUTOUT (PANEL 9501). INSTALLED DOUBLER PER M/M54-30-0 FIG 802.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON S/C, FOUND LT AND RT FWD DOOR EXTEROIR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, OPS NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT)

COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY.

Part: BATTERIES — DISCHARGED (CABIN)

EMERG LIGHTS ABOVE AFT AIRSTAIRS INOP. REPLACED BATTERIES.

Part: BATTERY PACK — DISCHARGED (CABIN)

ELECTRICAL COMPARTMENT EMERGENCY LIGHT INOP. REPLACED BATT, PACK.

Part: ACM — CONTAMINATED (RT PACK)

SMOKE IN CABIN DURING CRUISE FLT. INSPECTED CABIN NR 1 AND 2 ENGINES AND LEFT AND RIGHT PACKS. FOUND WATER IN RIGHT ACM OIL. REPLACED RIGHT ACM AND COALESCER, OPS CK NORMAL.

Part: FLOOR BEAM — CORRODED (BS 1030)

FOUND CORROSION ON FLOOR BEAM, STA 1030 UPPER FLANGE FASTENER HOLES AT LBL 0 AND LBL 9. REPAIRED PER M/M 53-20-11 PG 811B.

Part: FLOOR BEAM — CORRODED (BS 1070)

FOUND CORROSION 0N TOP OF FLOOR BEAM AT STA 1070, RBL 44 TO RBL 58. REPAIRED PER M/M 53-20-11 FIG 804A.

Part: SEAL — TORN (CARGO DOOR)

AT FLIGHT LEVEL 290 LOUD RUMBLE FOLLOWED BY RAPID RISE IN CABIN ALT. BOTH OUTFLOW VALVES CLOSED AND FLT LEVEL 220, CABIN STILL CLIMBING SLOWLY. DESCENDED TO 10,000 FT TO MAINTAIN PRESS. FOUND FWD CARGO DOOR SEAL DAMAGE AND OUT OF RETAINER. REPLACED DOOR SEAL AND CABIN PRESS NORMAL.

Part: WEB — CRACKED (BS 1235/1263)

FOUND ON C1 LETTER CK, TORQUE BOX WEB CRACKED .50 INCH AT STA 1235, LT, AND .1250 INCH AT STA 1263 RT. REPAIRED PER MM 53-11-0.

Part: ANGLE — CRACKED (NR 7 SLAT)

FOUND ON C1 LETTER CK, FOUND 1.25 INCH CRACK AT NR 7 SLAT I/B TRACK BOX INBD ANGLE. REPAIRED PER MM 57-20-21.

Part: WINSHIELD — DELAMINATED (LT COCKPIT)

CAPT WINDSCREEN DELAMINATED, RETARDS VISION. REPLACED WINDSCREEN.

Part: WEB — CRACKED (BS 1213)

1) 1 INCH CRACK UPPER END OF VERTICAL TORQUE BOX WEB ABOVE AIRSTAIR CLOSEOUT PANEL STA 1213 LT. 2) .50 INCH CRACK UPPER END OF VERTICAL TORQUE BOX WEB ABOVE AIRSTAIR CLOSEOUT PANEL STA 1213 RT. FOUND AT B-2 LTR CK. REPAIRED PER MM 53-11-0.

Part: BRACKET — CRACKED (LE WING)

ATTACH BRACKET CRACKED - NR 1 L/E FLAP ACTUATOR, LOWER CORNER. FOUND AT LTR CHECK, REPAIRED PE MM 57-20-21.

Part: SKIN — CRACKED (NR 3 SLAT)

NR 3 L/E SLAT COVE SKIN LOWER ATTACH ANGLE CRACKED BELOW THERMAL ANTI-ICE (TAI) DUCT. FOUND AT LTR CHECK. REPAIRED PER MM 57-54-0.

Part: SKIN — CRACKED (WS 463)

2.25 INCH CRACK IN WING L/E SKIN AT WS 463.0 AFT OF NR 5 SLAT ABOVE REFUELING PANEL. FOUND AT B2 LTR CK. REPAIRED PER MM 57-20-21.

Part: SKIN — CRACKED (NR 7 LE SLAT)

NR 7 SLAT DOUBLER CRACKED BELOW I/B STOP PAD. FOUND DURING B-2 LTR CK TPAMM. REPAIRED PER MM 57-54-0.

Part: STRINGER — CORRODED (FS 1010-1017)

CORROSION ON OB SIDE OF STGR 29L STA 1010 TO 1017, OB SIDE OF STGR 29L IS CRACKED AT STA 1012. REPAIRED PER SRM 53-10-3.

Part: COWLING — DAMAGED (NR 1 ENG)

NOSE COWL NR 1 ENG WAS FOUND WITH TIME LIMITED REPAIR AT 6 O'CLOCK POSITION. THE COWL WAS REPAIRED PER SRM 54-30-3.