N419DA

Part: BULB — FAILED (CABIN)

ON SVC CHECK, FOUND RT R1 EMERGENCY LIGHT INOP. REPLACED BULB, OPS CK GOOD.

Part: SKIN — CRACKED (VERT STAB)

TPA LTR CHECK F-2, 1 CRACK IN VERT STAB SKIN LT SIDE AT LWR SIDE OF CUTOUT FOR ACCESS PANEL 9523. REPAIRED PER MM 54-30-0.

Part: STRINGER — CRACKED (BS 940)

STRINGER 18A CRACKED AT LWR AFT BOLT STA 940. REPAIRED PER MM 53-12-0 PG 816.

Part: BRACKET — CRACKED (NR 1 SLAT ACT)

NR 1 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED ON WEB. REPAIRED PER M/M 57-20-21 PG 812.

Part: SKIN — CRACKED (BS 231)

TWO .25 INCH CRACKS IN F/S 231 STR 21R. INSTALLED DOUBLER PER SRM 53-30-3 F 26.

Part: WEB — CRACKED (BS 1235)

TPA LTR CHECK F-2, LT TORQUE BOX VERT WEB CRACKED 1 AT STA 1235. REPAIRED PER MM 53-11-0.

Part: FRAME — CRACKED (PAX DOORWAY)

FOUND AT F-2 LTR CK, AFT ENTRY DOOR FRAME CUTOUT CRACKED LT SIDE BELOW A/C DATA PLATE. REPAIRED PER SRM 53-10-9.

Part: PRBC — INOP (NR 3 ENGINE)

AUTO PACK TRIP ON TAKEOFF. POSSIBLE COMPRESS STALL. OCCURED AFTER BRAKES RELEASE. ABORTED TAKEOFF AT 60 KTS. REPLACED NR 3 ENGINE PRBC FOR OFF IDLE STALL. RAN ENG PER PHHB, ALL INDICATIONS CKS OK. NO STALLS.

Part: STIFFENER — CRACKED (NR 3 LE SLAT)

FOUND ON F1 LETTER CK, L/E SPAR STIFFENER CRACKED AT LOWER END NR 3 SLAT O/B TRACK I/B SIDE. REPAIRED PER MM 57-20-21.

Part: SKIN — CRACKED (FUSELAGE)

A .25 INCH CRACK FUSELAGE SKIN AT FASTENER JUST AFT OF L-3 COCKPIT WINDOW. REPAIRED PER SRM 53-30-3 FIG 8.

Part: BRACKET — CRACKED (NR 1 LE SLAT ACT)

FOUND ON F1 LETTER CK, CRACK IN NR 1 SLAT ACTUATOR SUPPORT BRACKET WEB I/B SIDE. REPAIRED PER MM 57-20-21.

Part: FRAME — CRACKED (PAX DOORWAY)

FOUND ON F1 LETTER CK, AFT ENTRY DOOR FRAME CRACKED RT SIDE 10 INCHES BELOW THE TOP OF THE DOOR CUTOUT. REPAIRED PER SRM 53-10-9.

Part: ANGLE — CRACKED (NR 7 LE SLAT)

REPAIR ANGLE CRACKED NR 7 SLAT STOP PAD I/B SIDE. REPAIRED PER MM 57-54-0 PG 816.

Part: SKIN — CRACKED (RT ELEVATOR)

A .5 INCH CRACK IN RT ELEVATOR LOWER SKIN AT FWD SPAR AREA. REPAIRED PER SRM 55-20-3 FIG 4.

Part: BATTERY PACK — DISCHARGED (CABIN)

OVERHEAD EXIT SIGN EMERGENCY LIGHT INOP ON TEST AT OVERWING EXITS. REPLACED M1094 RACK AND BATTERY PACK OP CKS OK. PARTS BORROWED FROM AMERICA WEST PACK LOCATED ABOVE ROW 19 RT SIDE OF CTR DUCT.

Part: BATTERY PACK — DISCHARGED (LT OVERWING)

LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT MOST FWD INOP. REPLACED RACK AND BATTERY PACK, OP CKS OK.

Part: LIGHT — INOP (L2 DOOR)

L2 DOOR EMERG EXIT LIGHT INOP. REPLACED LIGHT ASSY.

Part: SKIN — DENTED (BS 295)

THE FUSELAGE SKIN WAS BADLY DENTED AT FS 295 BETWEEN STR 12L AND 13L DUE TO A BIRD STRIKE. THE DAMAGED AREA WAS CUTOUT AND REPAIRED PER THE B727 SRM 53-30-3, FIG 1 WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER. THE REPAIR WAS DOCUMENTED PER ER/A 365361-14 WHICH ADDED A DTA REQUIREMENT TO THE REPAIR.

Part: WEB — CRACKED (BS 870)

DURING INSTALLATION OF PREVENTATIVE MOD ON THE LHS KEEL BEAM PER SB727-53-0208 (EO 4-64433-3), A CRACK WAS FOUND IN THE WEB JUST ABOVE THE VERT FLANGE OF THE KEEL BEAM. REPAIRED PER ERA 331201-14.

Part: SKIN — CRACKED (BS 304)

DURING INSPECTION PER EO4-60829-3, A CRACK WAS FOUND IN THE SKIN AND DOUBLER IN THE TYP LOCATION AS WELL AS A CRACK IN THE STRAP, BUT ONE FASTENER ROW HIGHER THAN TYP. REPAIRED PER ERA 331195-14.

Part: SKIN — CRACKED (NR 4 LE SLAT)

NUMBER 4 L/E SLAT HAD A CRACK FROM THE FENCE MOUNTING BOLT HOLE. INSTALLED A REPAIR DOUBLER PER M/M 57-54-0.

Part: LIGHT — DAMAGED (CABIN)

EMERGENCY TRACK LIGHTING STRIP AT 22DEF, TRACK COVER AND WIRING DAMAGED. REPLACED APPROX 30 INCHES OF LIGHT TRACK INVOLVING 4 RED LIGHTS. REPLACING 1 BULB HOLDER REPAIRED DAMAGED WIRING. INSTALLED 4 NEW RED LENS.

Part: BATTERY PACK — DISCHARGED (CABIN)

RT CARGO DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AT M957, OPS CHKS GOOD.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHT OUT AT ROW 16. REPLACED BATTERY AND RACK.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHT ABOVE L1 DOOR INOP. REPLACED BATTERIES.

Part: WEB — CRACKED (BS 1243)

A .75 INCH CRACK AT LIGHTNING HOLE STATION 1243 LT, LOWER TORQUE BOX WEB. INSTALLED DOUBLER PER MM 53-11-0 PG 828.

Part: BATTERY PACK — DISCHARGED (CABIN)

OVERWING EXIT LIGHT AT AFT CARGO DOOR INOP. REPLACED BATTERY CARTRIDGE, OPS CHECK GOOD.

Part: ANGLE — CRACKED (NR 1 LE SLAT)

FOUND ON C-2 LETTER CHECK, NR 1 SLAT COVE SKIN ATTACH ANGLE CRACKED BELOW THE ANTI-ICE DUCT. REPAIRED PER M/M 57-54-0.

Part: STRINGER — CRACKED (VERT STAB)

FOUND ON C-2 LETTER CHECK, VERT STAB STRINGER CRACKED RT SIDE TAIL CRAWLWAY, FOURTH BAY UP. REPAIRED PER M/M 53-30-0.

Part: RIB — CRACKED (NR 6 LE SLAT)

THE I/B ACTUATOR RIB WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0 FIG 804, FOR NR 6 L/E SLAT PANEL.

Part: RIB — CRACKED (NR 6 LE SLAT)

THE NR 9 RIB WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0 FIG 804, FOR NR 6 L/E SLAT PANEL.

Part: RIB — CRACKED (NR 6 LE SLAT)

THE O/B ACTUATOR RIB WAS FOUND TO BE CRACKED IN 2 PLACES. REPAIRED PER M/M 57-54-0 FIGS 804 AND 814, FOR NR 6 L/E SLAT PANEL.

Part: RIB — CRACKED (NR 4 LE SLAT)

DURING INSPECTION, NR 4 L/E SLAT WAS FOUND WITH FOUR CRACKED/DAMAGED LEADING EDGE SUPPORT RIBS. REPAIRED PER MM 57-54-0.

Part: SKIN — CRACKED (NR 4 LE SLAT)

DURING INSPECTION, NR 4 L/E SLAT OUTER SKIN WAS FOUND CRACKED AT FENCE ATTACH MOUNT HOLE. REPAIRED SKIN PER MM 57-54-0 FIG 813.

Part: RIB — CRACKED (NR 6 LE SLAT)

DURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH NR 1 L/E SUPPORT RIB CRACKED. REPAIRED PER MM 57-54-0.

Part: FRAME — CORROSION (FS 1166)

THE BS 1166 FRAME WAS FOUND CORRODED NEAR STRINGER 29R. THE REMOVED SECTION OF FRAME WAS TOO LARGE TO REPAIR PER THE B727 SRM. THE FRAME WEB IS MANUFACTURED FROM 0.063 CLAD 7075-T6. ALSO, THERE IS A FACTORY INSTALLED 0.050 CLAD 7075-T6 BONDED DOUBLER INSTALLED AT THIS LOCATION. THE REPAIR WILL REQUIRE INSTALLATION OF TWO 0.040 TI-6AL-4V DOUBLERS AND ONE 0.071 CLAD 7075-T6 REPAIR ANGLE. THIS REPAIR MAINTAINS THE PREVENTATIVE MODIFICATION PREVIOUSLY ACCOMPLISHED AT STR 28R PER EO 4-59823-3AD, WHICH PROVIDES TERMINATING ACTION FOR THE REPETITIVE INSPECTIONS MANDATED BY AD 92-12-03.

Part: KEEL BEAM — CORRODED (BS 950)

DURING INSPECTION, THE OUTBD FLANGE OF THE RT KEEL BEAM, STR 29R WAS FOUND WITH CORROSION AT STA 950. DUE TO INTERFERENCE ITEMS IT WAS NECESSARY TO CUT THE FUSELAGE SKIN TO REMOVE THE CORRODED FLANGE. REPAIR DOUBLERS AND STRAPS WERE INSTALLED IN ACCORDANCE WITH FAA/DER FORM 8110-3, DER DESIGNATION SO-831, DATED 01-19-96.

Part: STRINGER — CRACKED (FS 950-990)

DURING INSPECTION, CORROSION WAS REMOVED BY BLENDING AND SPOT FACING IN SEVERAL LOCATIONS ON THE UPPER SURFACE OF THE O/B AND I/B SKIN FLANGES, STRINGER 29L BETWEEN STA 950 AND STA 970. MINIMUM REMAINING FLANGE THICKNESS WAS .100. ALL CORROSION BLENDS ARE CONSIDERED ACCEPTABLE AS PERMANENT REPAIRS. ALSO, THE STRINGER REQUIRES SPLICING BETWEEN STA 950F AND 970, DUE TO CRACKING AND EXTENSIVE CORROSION BETWEEN STA 970 AND 990. THERE IS AN EXISTING SPLICE LOCATED AT STA 990 PLUS 10. THIS REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FAA/DER FORM 8110-3, DL ERA 303010 REV A.

Part: FLOOR PAN — CRACKED (BS 1183)

FOUND ON MV1 CHECK, LT AND RT LAV FLOOR PAN DITCHING SEAL PANEL CRACKED, VIEWED FROM BAG BIN FWD OF 1183. REPAIRED PER M/M 53-0-11.

Part: RIB — CRACKED (NR 6 LE SLAT)

UPON ROUTINE INSPECTION, A CRACK WAS FOUND ON 2ND RIB FROM I/B END. REPAIRED AS PER SRM 57-50-3 FIG 9, FOR NR L/E SLAT.

Part: BATTERY — DISCHARGED (CABIN)

AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERY, CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

LT AND RT LOWER OVERWING EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS EACH SIDE. RT SIDE CKS NORMAL. LT SIDE FORWARD TO MCO.

Part: RIB — CRACKED (NR 2 SLAT)

DURING SHOP INSPECTION, THE 4TH RIB FOR I/B END WAS FOUND CRACKED. THE RIB WAS REPAIRED PER SRM 57-54-00. THE LOWER COVE PANEL ATTACH ANGLE UNDERNEATH THE I/B UPSTOP WAS FOUND TO HAVE A CRACK. THE ANGLE WAS REPAIRED PER SRM 57-54-0 FIG 812, FOR NR 2 L/E SLAT.

Part: BEAM — CRACKED (FS 1273)

AT A LETTER CHECK IN TPA, A .50 INCH CRACK WAS FOUND IN THE UPPER TRANSVERSE BEAM GUSSET ANGLE AT F.S. 1273. ALSO, A .75 INCH CRACK IN THE ACCOMPANYING UPPER TRANSVERSE BEAM AT F.S. 1273. THE DAMAGED PARTS WILL BE REPLACED IN ACCORDANCE WITH B727 S/B 53-0129 REV. 4.

Part: ANGLE — CRACKED (NR 2 LE SLAT)

CRACK, 25 INCHES, NR 2 SLAT INBOARD UPSTOP PAD. FOUND AT C-1 LTR CK. SLAT WAS REPLACED AND ROUTED TO SHOP.

Part: RIB — CRACKED (NR 6 LE SLAT)

NR 6 SLAT HAS .50 INCH CRACK INBOARD OF ACTUATOR ATTACH POINT AT FORWARD RIB. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-54-0.

Part: ACTUATOR — CRACKED (NR 7 LE FLAP)

ON APPROACH, LOST SYSTEM A HYDRAULICS. LANDED ATL AND FOUND NR 7 SLAT ACTUATOR CRACKED. REPLACED ACTUATOR, OPERATION NORMAL.

Part: WEB — CRACKED (AFT STAIRWELL)

DURING LETTER CHECK, FOUND .625 INCH AND 1 INCH CRACKS AT LIGHTNING HOLE AFT STAIRWELL TORQUE BOX STRUCTURE RT LOWER WEB. REPAIRED PER MM 53-11-00.

Part: ANGLE — CRACKED (NR 7 LE SLAT)

NR 7 SLAT LWR SKIN ATTACH ANGLE CRACKED .25 INCH AT 2 PLACES AT ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0 PG 807. DAMAGE FOUND AT LETTER CHECK.

Part: SKIN — CRACKED (RT ELEV)

DURING LETTER CHECK, FOUND .75 INCH CRACK ON EXISTING REPAIR DOUBLER ON RIGHT ELEVATOR LOWER SKIN JUST OUTBOARD OF TAB. REPLACED DOUBLER PER SRM 53-20-3.

Part: ANGLE — CRACKED (FS 1273)

DURING INSPECTION, THE RT TORQUE BOX UPPER TRANSVERSE BEAM GUSSET ANGLE AT FS 1273 WAS FOUND CRACKED. THE ANGLE WAS REPLACED IN ACCORDANCE WITH B727 SB 53-0129 REV 4.

Part: FRAME — CRACKED (FS 913.5)

FOUND ON LETTER CK, STA 913.5 CRACKED BEHIND RADIUS BLOCK FUS FRAME AT MLG UPLOCK ASSY. REPAIRED, INSTALLED DOUBLER PER M/M 53-11-0 PG 834 - 837.

Part: LE RIB — CRACKED (NR 5 LE SLAT)

NBR 5 SLAT I/B L/E RIB AT ACTUATOR CRACKED .1250 INCH AT L/E. STOPPED DRILLED PER M/M57-54-0 PG 803. DAMAGE FOUND AT LETTER CHECK.

Part: ANGLE — CRACKED (NR 1 LE SLAT)

DURING LETTER CHECK, FOUND NR 1 L/E SLAT WITH SLAT ACTUATOR I/B ATTACH ANGLE CRACKED. REPAIRED PER MM 57-20-21 PG 812.

Part: SKIN — DENTED (NR 8 SLAT LE)

DURING SHOP INSPECTION, RIGHT WING NR 8 SLAT WAS FOUND WITH THE LEADING EDGE SKIN DENTED AT 51 INCHES TO 57 INCHES FROM THE I/B END OF SLAT. REPAIRED PER SRM 57-50-3 FIG 1.