N2819W

Part: RACK — FAULTY (L2 DOOR) · airframe 78,516 hrs · 52,912 cycles

L2 DOOR EMERGENCY LIGHT INOP. FOUND BATTERY MOUNT RACK BAD. REPLACED BATTERY RACK AND BATTERY. CHECKS GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 78,170 hrs · 52,687 cycles

PAX SEATS 23, 24, 25, 26 EMERGENCY LIGHTS INOPERATIVE, REPAIRED PINCHED WIRING. ALL CHECKED OK.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 76,901 hrs · 51,816 cycles

CRACKS WERE FOUND IN THE WEBS AND FAIL SAFE CHORDS OF THE FS294.5 BULKHEAD. CRACKS WERE EMANATING FROM FASTENER LOCATIONS AT WL 180 AND LBL 14. ONE WEB AND THE CHORDS WEREREPLACED AND ONE OF THE WEBS WAS SPLICED. THE DAMAGE WAS FOUND AT HMV.

Part: FRAME — CRACKED (FUSELAGE) · airframe 76,901 hrs · 51,816 cycles

CRACKS WERE FOUND IN TWO LOCATIONS OF THE FS 990 FRAME. ONEWAS AT STR 28R AND THE OTHER AT STR 29R. THE CRACKS WERE CUT OUT AND A DOUBLER INSTALLED. THE DAMAGE WAS FOUND AT HMV.

Part: SKIN — CRACKED (ENTRY DOOR) · airframe 76,901 hrs · 51,816 cycles

DURING MAINTENANCE VISIT, THE FWD ENTRY DOOR WAS FOUND CRACKED AROUND THE UPPER LATCH CUTOUT. REPAIR PER ER/A 401383-14.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,901 hrs · 51,816 cycles

STRINGER 29R WAS FOUND CRACKED AT FS 950E AND 975. THE STRINGER WAS CUT AT FS 950D +10 AND REPLACED AFT TO THE MFG SPLICE LOCATION. THE DAMAGE WAS FOUND AT MV.

Part: DOOR FRAME — MISDRILLED (FUSELAGE) · airframe 76,901 hrs · 51,816 cycles

THE RT AFT ENTRY DOOR FRAME SPLICE INSTALLED PER S/B 727-53-0210 WAS FOUND TO HAVE SHORT EDGE DISTANCE. THE AREA WAS MODIFIED PER S/B AT HMV.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 76,901 hrs · 51,816 cycles

DURING OVERHAUL, THE NR 4 INBD FLAP TRACK WAS FOUND WITH WEAR AND CORROSION, WHICH WAS BEYOND ALLOWABLE LIMITS, AT THE MLG BEAM ATTACH BOLT HOLES AND SPOTFACES, SPOILER BEAM ATTACH HOLES, HINGE SUPPORT FITTING ATTACH BOLT HOLES, AND THE CLIP ASSY ATTACH BOLT HOLES. REPAIR PER ER/A 401306-14AD AND BF GOODRICH ENGINEERING REPORT 23-0776.

Part: SLAT TRACK — CORRODED (LE FLAP) · airframe 76,901 hrs · 51,816 cycles

DURING OVERHAUL THE INBD TRACK, CORROSION AND WEAR WAS FOUND, WHICH WERE BEYOND ALLOWABLE LIMITS, AT MLG BEAM ATTACH BOLT HOLE AND SPOTFACES, SPOILER BEAM ATTACH HOLES, THE MLG DOOR AFT HINGE FITTING HOLES, THE TOGGLE DETENT HOLE AND THE CLIP ASSEMBLY ATTACH BOLT HOLES. REPAIR PER ER/A 387604-14AD AND BF GOODRICH ENGINEERING REPAIR 23-0708.

Part: RIB — CRACKED (FLAP) · airframe 76,901 hrs · 51,816 cycles

DURING SHOP VISIT THE I/B AFT CLOSEOUT RIB WAS FOUND CRACKED. THE RIB WAS REPAIRED PER 727 MM 57-52-0, FIG 808 BY REMOVING THE DAMAGE AND INSTALLING A FILLER AND DOUBLER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,786 hrs · 51,733 cycles

A 2.75 INCH LONG CRACK WAS FOUND IN THE UPPER SKIN AT THE UPPER FASTENER ROW OF THE STRINGER 26L SKIN LAP JOINT AT FS 700. THE DAMAGED SECTION OF SKIN WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOULBER PER B727 SRM 53-30-3, FIG 14 AND ER/A 379754-14.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,271 hrs · 51,405 cycles

FOUND L2 DOOR OVERHEAD EMER LIGHT INOP. REPLACED L2 DOOR OVERHEAD EMER LIGHT BATTERY PACK.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 75,510 hrs · 50,874 cycles

MEGAPHONE IN FWD CLOSET INOP. REPLACED SAME.

Part: SKIN — CRACKED (WINDOW BELT) · airframe 75,092 hrs · 50,596 cycles

A 0.5 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN EMANATING FROM THE LWR FWD CORNER OF THE L-4 WINDOW CUTOUT. REPAIR PER ERA 377485-14, REV A.

Part: BEAM — CRACKED (FUSELAGE) · airframe 75,050 hrs · 50,568 cycles

HFEC INSPECTION OF A FASTENER HOLE IN THE RBL 17.3 VERTICAL BEAM ON THE FS 1183 BULKHEAD AT WL 283 REVEALED A CRACK INDICATION. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK WITH AN ADDITIONAL INSURANCE CUT. THE HOLE WAS BUSHED AND THE NOMINAL FASTENER INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 377428-14AD.

Part: BATTERY — DISCHARGED (CABIN)

RIGHT OVERWING EMERGENCY EXIT LIGHTS FLASHING. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BATTERIES.

Part: BRACKET — CRACKED (NR 1 SLAT ACT)

INBD ATTACH BRACKET CRACKED NR 1 SLAT ACTUATOR BRKT. INSTALLED DOUBLER PER M/M 57-20-21. TPA F-1 LETTER CHECK.

Part: ACTUATOR — FAILED (NR 8 LE SLAT)

ARRIVING DFW, LOST 'A' SYS HYD. GEAR CAME DOWN NORMALLY, BUT UPON LANDING ZERO QTY AND INTERMITTENT PRESSURE UNTIL PUMP SHUT DOWN AT STOP. REMOVED AND REPLACED NR 8 SLAT ACTUATOR. REPLACED SYS 'A' FILTERS AND CASE DRAIN FILTERS. LEAK CKS GOOD. SERVICED HYD.

Part: BEAM — DAMAGED (CARGO DOOR)

C2 DOOR / UPPER PRESSURE BEAM, THE UPPER PRESSURE BEAM WAS FOUND DAMAGED DUE TO GROUND HANDLING AT THE AFT PRESSURE STOP FITTING ATTACH LOCATION. AUTHORIZED REPAIR TO TRIM AND REMOVE AFT HALF OF PRESSURE BEAM AND SPLICE-IN REPLACEMENT SECTION.

Part: COMPRESSOR — STALLED (NR 3 ENGINE)

DEPARTING DFW AFT CARGO DOOR CAME OPEN DURING ROTATION AT T/O. NUMBER 3 ENGINE PRECAUTIONARY SHUT DOWN IN FLIGHT DUE TO MULTIPLE COMPRESSOR STALLS. ONE FAN BLADE NICKED AND MINOR DAMAGE TO ACCOUSTICAL PANEL.

Part: WEB — CRACKED (BS 1271)

A TYPICAL CRACK WAS FOUND IN THE INBOARD VERTICAL WEB OF THE RT AFT ENTRY DOOR TORQUE BOX AT FS 1271. THE CRACK WAS REPAIRED PER BAC S/B 727-53-0129 AND DOCUMENTED PER ER/A 367089-14AD.

Part: SKIN — CRACKED (BS 681-740)

FUSELAGE SKIN FS 681-740 STRINGER 4R, SKIN LAP SPLICE, REPAIR FOR CRACKS. LFEC INSPECTION OF THE STRINGER 4R LAP SPLICE BETWEEN FS 681 AND 740. INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 15 CRACKS ALONG THE PANEL. THE LAP SPLICE WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS INSTALLED PER ER/A 366703-14, REV A.

Part: SKIN — CRACKED (BS 481-680)

FUSELAGE SKIN FS 481-680 STRINGER 4R SKIN LAP SPLICE, REPAIR FOR CRACKS. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 23 CRACKS ALONG THE PANEL LENGTH. THE LAP SPLICE WAS CUTOUT ALONG THE ENTIRE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS INSTALLED PER ER/A 366702-14, REV A.

Part: BATTERY PACK — DISCHARGED (CABIN)

REAR AISLE EMERGENCY EXIT SIGN BATTERY WEAK. REPLACED BATTERY PACK.

Part: FITTING — CRACKED (BS 940)

FUSELAGE RT STA 940 FITTING STRINGER 18-A, REPAIR FOR O/S HOLES. THE STATION 940 MLG FITTING AREA WAS INSPECTED PER BAC S/B 727-53-0141. CORROSION AND CRACK INDICATIONS WERE FOUND IN THE FITTING, STRINGER, AND SKIN. THE DAMAGED AREA OF SKIN WAS CUTOUT AND REPAIRED WITH A DOUBLER PER S/B 727-53-0172. THE STRINGER WAS SPLICED PER THE S/B, AND FITTING HOLES WEREOVERSIZED AND BUSHED. THE REPAIR WAS ACCOMPLISHED PER ER/A 332512-14, REV A.

Part: SKIN — CORRODED (BS 720)

FUSELAGE SKIN FS 720A-720B, STRINGER 27R-28R. REPAIR FOR CORROSION CUTOUT. THE FUSLAGE SKIN WAS FOUND CORRODED BETWEEN FS 720A AND FS 720B BETWEEN STRINGERS 27R AND 28R. THE CORROSION WAS REMOVED WITH A 3 BY 3.75 CUTOUT AND A 7.5 BY 3 CUTOUT. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER PER ER/A 366104-14, REV A.

Part: FITTING — CRACKED (BS 940)

FUSELAGE STA 940 FITTING STRINGER 18-A, REPAIR FOR O/S HOLES. THE STATION 940 MLG ATTACH FITTING WAS INSPECTED PER BAC S/B727-53-0141 (LT SIDE). TWO FASTENER HOLES COMMON TO STRINGER 18-A WERE FOUND TO HAVE CRACK INDICATIONS. THE HOLES WERE OVERSIZED TO REMOVE THE CRACK INDICATIONS, AND BUSHINGS AND OVERSIZE BOLTS WERE INSTALLED PER ER/A 366149-14.

Part: PANEL — PUNCTURE (LT ELEVATOR)

FOUND DURING MV2 CORROSION VISIT NRC 330, HOLE IN LT ELEVATOR BALANCE BOARD ACCESS PANEL NR 9119. REPAIRED PER SRM 55-20-3 FIG 1.

Part: STRAP — CRACKED (R1 DOORWAY)

THE R2 DOOR SURROUND BEAR STRAP WAS FOUND WITH A TYPICAL CRACK AT THE UPPER HINGE CUTOUT. THE CRACK WAS APPROX 2 INCHES LONG AND CONFINED TO THE BEAR STRAP ONLY. THE CRACK WAS REPAIRED WITH AN EXTERNAL DOUBLER PER BAC S/B 727-53-0136 & DOCUMENTED PER ER/A 366075-14.

Part: FRAME — CRACKED (PAX DOORWAY)

A .5 INCH VISIBLE CRACK AT AFT ENTRY DOOR CUTOUT LT FRAME AT 2ND FROM UPPER DOOR STOP. REPAIRED PER SRM 53-10-09.

Part: FLOORBEAM — CORROSION (BS 344)

FOUND DURING MV2 CORROSION VISIT NRC 16, CORROSION ON FLOORBEAM STA 344 BETWEEN RBL 13 AND RBL 25. REPAIRED PER SRM 53-10-8 FIG 11.

Part: FLOORBEAM — CORRODED (BS 1050)

FOUND DURING MV2 CORROSION VISIT NRC 81, CORROSION ON FLOORBEAM STA 1050 AT RBL 33. REPAIRED PER M/M 53-20-11 FIG 804A RBL 33 TO RBL 19.

Part: WEB — CRACKED (BS 1293)

RT VERTICAL TORQUE BOX WEB UPPER LIGHTENING HOLE HAS .375 INCH CRACK AT STA 1293. REPAIRED PER M/M 53-11-0 FIG 819.

Part: CHORD — CRACKED (BS 1274)

THE 65-17510-90 INNER CHORD OF THE VENTRAL STAIRWAY TORQUE BOX WAS FOUND WITH A CRACK AT FS 1274. THE CRACK IS TYPICAL OF BAC S/B 53-0129. THE CRACKED CHORD WAS REPAIRED WITH A REPAIR ANGLE AND STRAPS PER THE PROCEDURES OUTLINED IN THE BAC S/B. THE REPAIR WAS DOCUMENTED PER ER/A 365521-14AD.

Part: LIGHT — INOPERATIVE (CABIN)

OVERHEAD EMERGENCY LIGHTS AT AFT AIRSTAIRS INOP. MTC REPLACED LIGHT ASSY, OPS CKS. OK.

Part: LIGHTS — INOPERATIVE (CABIN)

FWD SECTION OF FLOOR TRACK LIGHTING IN FC INOP. REPLACED FWD AND AFT FLOOR TRACK LGT PWR SUPPLIES AND BATTS. REPAIRED CHAFFED WIRE UNDER SEAT 1 AB.

Part: RACK — INOPERATIVE (BS 800)

RT AFT OVERWING EMER EXIT LIGHT INOP. REPLACED BATT RACK, OPS NOW NML.

Part: CSD — FAILED (NR 1 ENGINE)

ON FINAL APPROACH NR 1 ENG DRIVEN GEN FAILED. AFTER LANDING NR 1 ENG FIRE WARNING ILLUMINATED AND BELL CAME ON. FIRE HANDLE WAS PULLED AND BOTH BOTTLES DISCHARGED. AFTER OPENING COWLING FOUND THE CSD AND GEN TO BE THE SOURCE OF IGNITION. REPLACED CSD AND GENERATOR, OPERATIONAL CHECK NORMAL.

Part: SEQUENCE VALVE — MALFUNCTIONED (RT MLG)

RIGHT MAIN LANDING GEAR FAILED TO EXTEND. CRANKED AS PER POM AND LANDED NORMALLY. REPLACED RIGHT MAIN GEAR SEQUENCE VALVE AND UP LOCK ACTUATOR. OPERATED LANDING GEAR SEVERAL TIMES, CKS OK.

Part: SIDE WALL — CRACKED (BS 277)

FOUND A .75 INCH CRACK AT RIGH-HAND SIDE WALL OF THE NOSE LANDING GEAR WHEELWELL. REPAIRED PER DAL ER/A 304418-14AD.

Part: TEE ANGLE — CORROSION (PANEL 3348L)

FOUND CORROSION ON ATTACH ANGLE FOR ACCESS DOOR 3348L. REPAIRED PER MM 53-30-1.

Part: BULKHEAD WEB — CRACKED (BS 1183)

FOUND CRACK AT RBL 27 OF BS 1183 BULKHEAD WEB. THE DAMAGE CONSISTED OF A .75 INCH CRACK AT WL 170. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECIFIED BY S/B 727-53-171. REPAIRED PER B727 SRM 53-10-9, FIG. 4.

Part: BULB — FAILED (AFT RT SLIDE)

ON LAYOVER, FOUND RIGHT AFT SLIDE LIGHT INOP. RELAMPED SAME, CHECKS GOOD.

Part: ACT ANGLE — CRACKED (NR 8 SLAT)

NR 8 SLAT ACTUATOR INBOARD ATTACH ANGLE CRACKED. REPAIR PER M/M 57-20-21.

Part: WEB — CRACKED (BS 1263)

.3750 INCH CRACK IN LIGHTNING HOLE OF LT LOWER TORQUE BOX WEB, STA 1263, TOP HOLE. REPAIR PER M/M 53-11-0.

Part: SWIVEL FITTING — OUT OF ADJUST (MLG DOOR)

MLG SPAR BEING CHAFED BY STRUT DOOR SIDE BRACE SWIVEL FITTING. REWORK PER M/M 57-43-0.

Part: ACT SUPPORT — CRACKED (NR 8 SLAT ACT)

FOUND TWO-INCH CRACK IN NR 8 SLAT OUTBOARD ACTUATOR SUPPORT WHILE SHOWING MAINTENANCE LOCATION OF CRACK AT INBOARD SUPPORT. REPAIR PER M/M 57-20-21.

Part: BATTERY PACK — DISCHARGED (CABIN)

TWO AISLE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPS CK GOOD.

Part: ANGLE — CRACKED (NR 2 LE FLAP)

FOUND ON B2 LETTER CHECK, CRACK IN NR 2 SLAT TAI DUCT CUTOUT. REPAIRED PER MM 57-54-0.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

EMERG LIGHT, F/C BULLNOSE INOP. REPLACED BATTERY AND RACK, OPERATION NORMAL.

Part: ANGLE — CRACKED (NR 6 LE FLAP)

LOWER ANGLE CRACKED AT RIB NR 7 LOCATION. REPAIRED PER B-727 M/M 57-54-0 FIG 805A, FOR RT WING NR 6 L/E SLAT. FOUND DURING SHOP INSPECTION.

Part: RIB — CRACKED (NR 6 LE FLAP)

NR 13 RIB CRACKED AT LOWER ANGLE LOCATION. REPAIRED PER B-727 M/M 57-54-0 FIG 814, FOR RT WING NR 6 L/E SLAT. FOUND AT SHOP INSPECTION.

Part: ANGLE — CRACKED (NR 6 LE FLAP)

RIB NR 11 CRACKED AT LOWER ANGLE. REPAIRED PER B-727 M/M 57-54-0 FIG 814, FOR RT WING NR 6 L/E SLAT. FOUND DURING SHOP INSPECTION.

Part: ANGLE — CRACKED (NR 6 LE FLAP)

RIB NR 7 CRACKED AT LWR ANGLE. REPAIRED PER B-727 M/M 57-54-0 FIG 814, FOR RT WING NR 6 L/E SLAT DURING SHOP INSPECTION.

Part: SPAR — CRACKED (NR 6 LE SLAT)

DURING SHOP INSPECTION, RT WING NR 6 L/E SLAT WAS FOUND WITH THE SPAR CRACKED AT THE CUTOUT FOR THE ANTI-ICE T-DUCT. REPAIRED PER MM 57-54-0 FIG 810.

Part: RIB — CRACKED (NR 6 LE FLAP)

DOUBLER FOR O/B ACTUATOR RIB CRACKED. REPLACED DOUBLER PER B-727 M/M 57-54-0 FIG 804, FOR RT WING NR 6 L/E SLAT. FOUND DURING SHOP INSPECTION.

Part: RIB — CRACKED (NR 6 LE FLAP)

DOUBLER FOR I/B ACTUATOR RIB CRACKED. REPLACED DOUBLER PER B-727 M/M 57-54-0 FIG 804, FOR RT WING NR 6 L/E SLAT. FOUND DURING SHOP INSPECTION.

Part: RIB — CRACKED (NR 4 SLAT)

DURING SHOP INSP, RIBS 12 WAS FOUND TO BE CRACKED. REPAIRED PER SRM 57-54-0 FIG 804, FOR LT WING NR 4 SLAT.

Part: RIBS — CRACKED (NR 4 SLAT)

DURING SHOP INSP, RIBS 2, 8, 9, 21 WERE FOUND TO BE CRACKED. REPAIRED RIBS PER SRM 57-54-0 FIG 814. DURING SHOP INSPECTION OF NR 4 L/E SLAT.

Part: RIB — CRACKED (NR 4 SLAT)

DURING SHOP INSP, NR 18 RIB WAS FOUND CRACKED. REPAIRED PER SRM 57-50-3 FIG 9, FOR LEFT WING NR 4 L/E SLAT.

Part: SKIN — CORRODED (FS 680 STR 27R)

DURING INSPECTION AT LETTER CHECK, CORROSION WAS FOUND ON THE SKIN AND STRINGER AT STATION 680, STR 27R. AN EXISTING REPAIR DOUBLER WAS ALSO REMOVED FROM THE SKIN AT STR 28R. THE SKIN CUTOUT AT STR 27R IS APPROXIMATELY 4.375 INCH BY 1.75 INCH AND THE CUTOUT AT STR28 R IS 2 INCHES BY 1.375 INCH. PER B727 SRM 53-10-3, FIG. 1, THE EXISTING REPAIR WAS REPLACED WITH A LARGER REPAIR TO COVER BOTH DAMAGED AREAS.

Part: BEAM — CRACKED (FS 1273 RT TORQ)

DURING LETTER CHECK INSPECTION, THE RT UPPER TORQUE BOX UPPER AFT TRANSVERSE BEAM AND GUSSET ANGLE AT FS 1273 WERE FOUND CRACKED. PER BAC S/B 727-53-0129, REV A, BOTH THE BEAM AND GUSSET ANGLE WERE REPLACED.

Part: SLAT — CRACKED (NR 4)

2 INCH SPIDER CRACK ON IB LWR CORNER OF NR 4 LE FLAP. FOUND DURING B-1 LETTER CHECK TPAMM. REPAIRED PER MM 57-53-0 PG 804.

Part: WEB — CRACKED (48 SEC R/H SIDE)

2 LIGHTNING HOLES HAVE .25 INCH CRACKS IN FLANGE AT VERT WEB BELOW AIRSTAIR ACT. FOUND DURING B-1 LETTER CHECK TPAMM. REPAIRED PER MM 53-11-0 PG 828.

Part: SLAT ANGLE — CRACKED (NR 6 O/B)

FOUND ON LTR CK, NR 6 POS L/E SLAT S/N BN105 HAS A 2 INCH CRACK AT O/B STOP PAD LWR COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54-0 PG 816.

Part: FOREFLAP — CRACKED (NR 4)

1 INCH CRACK ON NR 4 FOREFLAP ABOVE NR 8 FLAP TRACK. FOUND DURING B-1 LETTER CHECK TPAMM. REPAIRED PER MM 57-50-4 FIG 1.

Part: TUBE — CRACKED (RT WING)

DURING CRUISE, NR 3 FUEL QTY WAS DROPPING AT 2,500 LBS PER HOUR WITHOUT BURNING FROM THAT TANK. VISUALLY CHECKED NR 3 AT CRUISE ALTITUDE AND COULD SEE A STREAM OF FUEL VAPORS OFF THE RIGHT WING. LANDED DFW. FOUND CRACKED FUEL TUBE. REPLACED TUBE AND RETURNED TO SERVICE.