N763DL

Part: DUCT — FAILED (NR 1 ENGINE)

ON T/O, HP DUCT BLEW CAUSING FIRE WARNING, ALT FIRE BOTTLE DISCHARGED. REPLACED ENGINE.

Part: COUNTERBALANCE — FAILED TEST (L 3 DOOR)

L-3 COUNTERBALANCE FAILED SI 72565-12. REPLACED COUNTERBALANCE.

Part: COUNTERBALANCE — FAILED (L 2 DOOR)

L-2 COUNTERBALANCE FAILED SEPICAL INSPECTION 72565-12. REPLACED COUNTERBALANCE.

Part: BATTERY — DISCHARGED (CABIN)

FWD RT FLT ATT FLASHLIGHT INOP. REPLACED BATTERY, CKS NML.

Part: CONNECTOR — DIRTY (CABIN)

DURING L/O, FOUND EMERGENCY LIGHTS, TRACK LIGHTS INOP, RT SIDE FROM 34HJ TO 41HJ. T-S PER MM. CLEANED CONNECTOR BEHIND WALL PANEL AT 41HJ, OPS CK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

EXTERIOR EMERGENCY LT AT L1 DOOR INOP. REPLACED BATTERY PACK.

Part: POWER PACK — WEAK (CABIN)

1R EMERGENCY LIGHT POWER PACK WEAK, FAILED TO ILLUMINATE. EMERGENCY LIGHTS LONGER THAN 30 SECONDS ON LAYOVER CHECK.

Part: FITTING — OUT OF POSITION (HORIZ STAB)

THE UPPER STABILIZER POWER SERVO FITTINGS ATTACHED TO THE 1860 BULKHEAD WERE ORIGINALLY MISPLACED. AFTER REALIGNMENT, THE FITTINGS' INBOARD ATTACH FASTENERS DID NOT HAVE E.D. THIS ER/A AUTHORIZES PLUGGING THE DISCREPANT HOLES AND RELOCATING THEM PER DL ERA 273641-14.

Part: CONTROLLER — FAILED (CABIN)

PASSING 17,000 FT, UNABLE TO MAINTAIN CABIN PRESSURE. WENT TO MANUAL WITH AFT OUTFLOW VALVE TO REGAIN CONTROL. REPLACED CABIN PRESSURE CONTROLLER, BITE CK OK.

Part: SPINNER — LOOSE (NR1 ENGINE)

NR 1 ENG HIGH VIB STARTED AT 2.5, THEN UP TO 4.0, NORMAL AT IDLE. VIBS FELT IN FLT DECK, NR 1 ENG SHUTDOWN AT FL 310. LANDED WITHOUT FURTHER INCIDENT. FOUND FAIRING ATTACHMENT AT SPINNER BROKEN. REPLACED SPINNER AND FAIRING, CKD CHIP DETECTORS, BORESCOPED 7TH STAGE IPC, 1ST STAGE HPT. REPLACED OIL FILTER LUBED FAN, RAN PER PFHB TEST 11 AND CKS GOOD.

Part: IDG — FAILED (NR 1 ENGINE)

ON CLIMBOUT, NR 1 GEN BREAKER OPEN LIGHT CAME ON, GENERATOR WOULD NOT PARALLEL, LANDED LGW. REPLACED NR 1 IDG, OPERATION NORMAL.

Part: FRAME SEGMENTS — CRACKED (AFT PRESS DOME)

DURING AIRCRAFT HMV IN ATL, THE FRAME SEGMENTS ON THE AFT PRESSURE DOME BETWEEN S23 AND S44 WERE FOUND WITH CRACK IN THE LOWER FLANGE RADII. THE DAMAGE WAS TRIMMED OUT, SPLICE STRAPS WERE ADDED, AND THE REPAIR AREA WAS TREATED FOR CORROSION.

Part: INTERCOSTAL — CRACKED (FS 1778-1792)

AT HMV, FOUND THE INTERCOSTAL CAP CRACKED BETWEEN FS 1778 TO FS 1792, AT LBL 40. REPLACED CAP PER SRM 51-10-05.

Part: TRUNION FITTING — RUSTY (RT MLG)

AT HMV, THE RIGHT MAIN LANDING GEAR FWD TRUNNION ATTACH FITTING WAS FOUND CORRODED AT THE FWD TRUNNION LUG AND IN AREA OF AFT LUG. REPAIRED PER SRM 57-14-00 FIG 804.

Part: FITTING — RUSTY (RT MLG)

AT HMV, THE RIGHT MAIN GEAR FITTING AT UPPER LATERAL BRACE LUG WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 57-14-00 FIG 804.

Part: TRUNNION FITTING — RUSTY (RT MLG)

AT HMV, THE RIGHT MAIN LANDING GEAR TRUNION FITTING BETWEEN LATERAL BRACE LUGS ARE RUSTY. REPAIRED PER SRM 57-14-00 FIG 804.

Part: TEAR STRAP — DISBONDED (FS 923)

DURING HMV, FOUND TEAR STRAP AT FS 923 STR 21 AND 22 DISBONDED. REPAIRED PER SRM 53-30-00 PG 807.

Part: SKIN — CORRODED (FS 1615)

AT HMV, FOUND CORROSION ON FUSELAGE SKIN UNDER AND AROUND TEAR STAP AT FS 1615 BETWEEN STRINGERS 34-37. REMOVED LIGHT CORRROSION AND CHECKED WITHIN LIMITS PER SRM 53-31-00 FIG 801. REINSTALLED TEAR TRAP PER SRM 53-31-00 FIG 816.

Part: HINGES — RUSTY (RT MLG DOOR)

AT HMV, HINGES AND BUSHINGS THAT ARE ATTACHED RT MAIN GEAR FITTING FOR UPPER HINGE DOOR WERE FOUND CORRODED. REPAIRED PER SRM 57-14-00 FIG 804.

Part: STRINGER — CORRODED (FS 963)

AT HMV, FOUND STRINGER CORRODED INSIDE MESC FWD OF STA 963 S-34. REPLACED STRINGER SECTION PER SRM 53-13-00 PG 896.

Part: TEAR STRAP — DELAMINATED (FS 729/846)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DELAMINATED BETWEEN FS 729 AND 846 BETWEEN STRINGERS 32-31. REPAIRED PER SRM 53-31-00 FIG 804.

Part: TRUNNION FITTING — RUSTY (RT MLG)

HMV, THE RIGHT MAIN LANDING GEAR TRUNNION FITTING WAS FOUND CORRORDED BETWEEN FWD TRUNNION LUGS. REMOVED CORROSION PER SRM 57-14-00 FIG 804.

Part: STRINGER — CORRODED (FS 963)

AT HMV, FOUND FUSELAGE STRINGER 32 INSIDE MESC WITH CORROSION DAMAGE JUST FORWARD OF FS 963. REPLACED DAMAGED SECTION OF STR BETWEEN STA 933-983 PER SRM 53-13-00 PG 806.

Part: SKIN DOUBLER — CORRODED (FS 727)

AT HMV, FOUND INTERIOR FUSELAGE SKIN DOUBLER FOR SKIN SPLICE AT FS 727 AT BL-0 CORRODED. REPAIRED PER SRM 53-31-00 FIG 836.

Part: SKIN — CORRODED (FS 933)

AT HMV, THE 0.020 INCH BONDED INTERNAL SKIN WAS FOUND CORRODED AT FS 933, BETWEEN STRINGERS 30 AND 31. REPAIRED PER SRM 53-31-00 FIG 836.

Part: FLOOR SUPPORT — CORRODED (FS 888-901)

AT HMV, FOUND CABIN FLOOR SUPPORT AT FS 888-901 AT LBL 46.5 CORRODED. REPLACED SUPPORT PER SRM 51-10-05 PG.1.

Part: TEAR STRAP — LOOSE (FS 1370)

DURING HMV, A TEAR STRAP WAS FOUND LOOSE AT FS 1370 BETWEEN STR 33 AND 34. REPAIRED PER SRM 53-31-00 PG 830.

Part: SKIN — CORROSION (FS 729-846)

DURING HMV, FOUND CORROSION ON FUSELAGE SKIN BETWEEN FS 729 AND FS 846, STRINGER 332 AND 33. ROUTED OUT INTERNAL BONDED DOUBLER, AND REMOVED CORROSION AS PER SRM 53-33-00 FIG 836.

Part: DOUBLER — DISBONDED (FS 1625)

AT HMV, FOUND FUSELAGE SKIN BONDED DOUBLER AT FS 1625 JUST OUTBOARD OF STRINGER 6 DISBONDED. REPAIRED PER SRM 53-31-00 PG 960.

Part: FLOOR BEAM — CRACKED (FS 1103)

AT HMV, FOUND HORIZONAL TRUSS MEMBER AT LT FS 1103, CRACKED UPPER TAB. REPAIRED PER SRM 53-21-00 PAGES 853-855.

Part: RIB — MODIFIED (LT WS 293)

REF EO 7-59089 IN COMPLIANCE OF VA 31733AT LEFT WING RIB CAP AT IWS 293, BOTTOM HOLE ON VERTICAL FLANGE CANNOT BE REAMED OR COLD WORKED, DUE TO INTERFERENCE FROM RIB CAP. CUT RIB CAP FOR TOOL CLEARANCE AND REPAIR PER SRM 57-12-00 PG805.

Part: RIB — MODIFIED (RT WS 293)

REF EO 7-59089-3 IN COMPLIANCE OF VA 31733 AT RIGHT WING IWS293 BOTTOM HOLE ON VERTICAL RIB FLANGE CANNOT BE REAMED OR COLD WORKED DUE TO INTERFERENCE TO RIB CAP. CUT RIB CAP FOR CLEARANCE AND REPAIRED PER SRM 57-12-00 P805.

Part: RIB — MODIFIED (RT WS 319)

REF EO 7-59089-3 AT RIGHT WING IWS 319 RIB CAP BOTTOM HOLE ON VERTICAL FLANGE CANNOT BE REAMED OR COLD WORKED DUE TO INTERFERENCE WITH THE RIB CAP. CUT RIB CAP AND REPAIRED PER SRM 57-12-00 PG 805.

Part: RIB — MODIFIED (LT WS 319)

REF EO 7-59089 AT LEFT WING IWS 319, BOTTOM HOLE ON VERICAL FLANGE CANNOT BE REAMED OR COLD WORKED DUE TO INTERFERENCE OF RIB CAP. CUT RIB FLANGE FOR TOOL CLEARENCE AND REPAIRED PER SRM 57-12-00 PG 805.

Part: FITTING — CORRODED (LT MLG)

DURING HMV, FOUND LT MLG SUPPORT FITTING UPPER FLANGE HOLES 1, 2, 3, 4, 5, AND 6 WERE CORRODED. REAMED HOLES 1 THROUGH 6, AND REMOVED CORROSION PER SRM 57-14-00 PG 809-811. INSTALLED BUSHINGS, TREATED AND PAINTED.

Part: P-DOME — CRACKED (P-DOME STR 43)

AT HMV, FOUND AFT P-DOME CRACKED AFT OF STRINGER 43 ATTACH FITTING UNDER Z-ANGLE. REPAIRED PER SRM 53-11-00 PG 812, 813.

Part: FLOOR BEAM — CORRODED (FS 900)

AT HMV, FOUND CABIN FLOOR SUPPORT CORRODED ON LOWER SURFACE APP FS 900 AT RBL 30. REPLACED FLOOR SUPPORT PER SRM 51-10-05.

Part: PRESSURE DECK — CORRODED (FS 349)

AT HMV, FOUND PRESSURE DECK CORRODED AFT OF STIFFENER AT FS 349, AND OUTBOARD OF BL 0 UNDER THE RT FWD LAV. REPAIRED PER SRM 53-11-00 PG 922.

Part: FLOOR BEAM — CORRODED (FS 1763)

DURRING OVERHAUL FOUND, FLOOR BEAM UPPER FLANGE TOP SURFACE CORRODED AT STA 1763, LBL 36 TO LBL 54. ALSO, SEVERAL PLACES ON LWR SURFACE AT SAME CLIP NUT HOLES. INSTALLED NEW SECTION OF T-CAP PER SRM 53-21-00 PG 849-852.

Part: FLOOR BEAM — CORRODED (FS 901-923)

AT HMV, FOUND CABIN FLOOR SUPPORT CORRODED AT LBL 30 FS 901-923. FOUND CORROSION TO BE OUT OF LIMITS, REPLACED FLOOR SUPPORT PER SRM 51-10-00 PG 1.

Part: FITTING — CORROSION (LT MLG)

DURING HMV, LT MLG RETRACT ACTUATOR FITTING HOLES 1, 2, 3, 4, 5, AND 6 FOUND TO HAVE CORROSION. REAMED HOLES 1 THROUGH 6 TO REMOVE CORROSION, AND INSTALLED BUSHINGS PER SRM 57-14-00 PGS 819 AND 820.

Part: SEAT TRACK — CORRODED (FS 1318)

AT HMV, FOUND FS 1318 CENTER INBOARD SEAT TRACK CORRODED AT FS 1318 AVBOVE HYDTRAULIC SERVICE CENTER. REPLACED TRACK PER SRM 53-21-00.

Part: FLOOR BEAM — CORRODED (FS 884)

DURING OVERHAUL THE CABIN FLOOR BEAM LOWER SURFACE OF UPPER CAP WAS CORRODED AT SEVERAL FASTENER HOLES FS 884 RBL10. MANUFACTURED AND INSTALLED REPAIR PARTS PER SRM 53-21-00 PG 849-852

Part: FLOOR BEAM CAP — CORROSION (FS 1763)

DURING OVERHAUL AT STA 1763 THE FLOOR BEAM UPPER FLANGE TOP SURFACE HAD DEEP CORROSION SEVERAL PLACES LB 62 LBL 88. REMOVED AND INSTALLED T-CAP PER SRM 53-21-00 PG 849-852.

Part: FLOOR BEAM — CORRODED (FS 901)

DURING OVERHAUL, CABIN FLOOR BEAM CAP FROM RBL 42.5 TO RBL 74.5 WAS FOUND CORRODED. ALSO, CORROSION ON UNDERSIDE AT FASTENER HOLES FS 901. REMOVED CAP, INSTALLED REPAIR PER SRM 53-21-00 PG 849-852.

Part: FLOOR BEAM — CORRODED (FS 1763)

DURING HMV, FOUND CABIN FLOOR BEAM CORRODED AFT GALLEY/SERVICE CENTER, FS 1763 FROM RBL37 TO THE R-3 DOOR THRESHOLD.

Part: SKIN — DELAMINATED (FS 729-846)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRP DISBONDED AT FS 746 AND 846 BETWEEN STRINGERS 34 AND 36, ALSO AT FS 729 AND FS 846 BETWEEN STRINGERS 32-31. REPAIRED PER SRM 53-31-0 FIG 816 AND FIG 804.

Part: THRESHOLD — CORRODED (R-2 DOOR)

AT HMV, THE R-2 DDOR THRESHOLD WAS FOUND CORRODED AT THE AREAS EXPOSED BY REMOVAL OF THE FWD AND AFT ATTACH FITTING. CHECKED LIMITS AND REPAIRED PER SRM 53-15-00 FIG 808.

Part: FITTING — CORRODED (LT MLG)

AT HMV, FOUND LMLG RETRACT ACT FITTING ATTACH STRUCTURE CORRODED IN UPPER MATING SURFACE AROUND BOLT HOLES. LOCAL BLENDED SURFACES TO REMOVE CORROSION, HFEC INSPECTED ALL SURFACES AND FOUND OK. REPAIRED PER SRM 57-14-00 PG 809.

Part: TEAR STRAP — DELAMINATED (FS 903/923)

DURING HMV, FOUND TEAR STRAP DELAMINATED BETWEEN FS 903 AND 923 BETWEEN STR 28 AND 29. REPAIRED PER SRM 53-31-00 FIG 816.

Part: ANGLE — CRACKED (FS 1103)

DURING OVERHAUL, FOUND ANGLE AT STA 1103 RT SIDE, AT AFT SIDE OF FRAME AT FLOOR LINE CRACKED. REMOVED ANGLE, REPAIRED FRAME ATTACH TAB ON OUTBOARD END OF STA 1103, FRAME TO SEAT T-RACK TENSION TIE FITTING PER SRM 53-21-00 PG 853.

Part: TEARSTRAP — DELAMINATED (FS 865/883)

DURING OVERHAUL, A TEARSTRAP BETWEEN FS 865 AND 883, BETWEEN STR 34 AND 35 WAS FOUND DELAMINATED. REPAIRED PER SRM 53-31-0 FIG 816.

Part: ANGLE — CRACKED (FS 1705)

AT OVERHAUL NR 2 ENG INLET, LEFT SIDE AT 3:00 POS- FS 1705, HORIZONTAL ANGLE IS CRACKED. REPLACED TEE AND SPACER SECTION IAW SRM 54-12-00 FIG 803.

Part: ANGLE — CRACKED (FS 1705)

DURING OVERHAUL NR 2 ENG INLET DUCT, LT FS1705, 9:00 POS 'VIEWED THROUGH PANEL 311UL', BULKHEAD ANGLE CRACKED FABRICATED AND INSTALLED REPAIR TEE ANGLE AND SPACER PER SRM 54-12-00 FIG 803.

Part: FLOOR BEAM — CORRODED (FS 1745)

DURING OVERHAUL AT CABIN AFT GALLEY/SERVICE CTR, UNDER FLOOR AREA, TOP OF FS1745 FLOOR BEAM, CORROSION AROUND FASTENER HOLE AT RBL53. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-21-00 PG 865-868.

Part: THRESHOLD — CORRODED (R-1 DOOR)

AT HMV, CORROSION WAS FOUND ON BOTTOM SURFACE OF R-1 DOOR THRESHOLD PLATE AROUND DRAIN OPENINGS AND UNDER THE AFT GIRT BAR RECEPTACLE, FS 328 TO 369 WL 200. REPAIRED PER SRM 53-15-00 PG 816.

Part: FLOOR BEAM — CORRODED (FS 315)

AT HMV, FOUND CABIN FLOOR BEAM CORRODED ON UPPER SURFACE AT FS 315 FROM CENTER LINE TO DOOR (L-1). FOUND TO BE OUT OF LIMITS PER SRM 53-21-00. REPAIRED PER SRM 53-21-00 PG 868.

Part: FLOOR BEAM — CORRODED (FS 281)

DURING OVERHAUL, CORROSION WAS FOUND ON FLOOR BEAM AT FS 281 LT SIDE ALONG TOP SURFACE FROM DOOR TO AFT CENTERLINE. REMOVED DAMAGED SECTION AND INSTALLED NEW T-SECTION PER SRM 53-21-00 PG 849-852

Part: FORMER — CORRODED (FS 267)

AT HMV, FORMER WAS FOUND CORRODED AT FS 267, BELOW STR 21 JUST OUTBOARD OF NR 3 RAM AIR INLET SCOOP (AFT SIDE). REMOVED DAMAGED SECTION OF FRAME ANGLE, AND INSTALLED REPAIR PER SRM 53-12-00 FIG 805.

Part: SEAT TRACK — CORRODED (FS 1665-1745)

DURING OVERHAUL THE SEAT TRACK THAT RUNS FROM FS 1665 FS 1745 AT RBL 22 WAS FOUND CORRODED. REPLACED SECTION OF TRACK PER SRM 53-21-00 PG 836.

Part: TEAR STRAP — DISBONDED (FS619/BL12L)

AT HMV, FOUND FUSELAGE SKIN TEAR STRAP DISBONDED AT FS 619 AT BL 12L. NO CORROSION FOUND IN AREA, REPAIRED STRAP PER SRM 53-31-00 FIG 816.

Part: TEAR STRAP — UNBONDED (FS 1675)

DURING HMV, FOUND TEAR STRAP UNBONDED AT FS 1675 BETWEEN STR 44 AND 45. REPAIRED PER SRM 53-31-00 PG 830.

Part: FITTING — CORROSION (RT MLG)

DURING HMV, RT MLG RETRACT ACTUATOR FITTING FOUND TO HAVE CORROSION ON FWD AND AFT FACES AND HOLES 1, 2, AND 4. BURNISHED FITTING FACES AND MACHINED HOLES TO REMOVE CORROSION AS PER SRM 57-14-00. INSTALLED CAD PLATED BUSHINGS.

Part: TEAR STRAP — UNBONDED (FS 1715)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 1715 BETWEEN STRINGERS 44 AND 45. REPAIRED PER SRM 53-31-00.

Part: TEAR STRAP — CORRODED (FS 933)

DURING OVERHAUL, FOUND TEAR STRAP DISBONDED BETWEEN STA 943-923, BETWEEN STR 35 & 36. CUT TEAR STRAP, CLEANED CORROSION AND REPAIRED PER SRM 53-31-00 PG 801.

Part: TEAR STRAP — DISBONDED (FS 659 BL10R)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 659 AT BL 10R. REPAIRED PER SRM 53-31-00 PG 816.

Part: TEAR STRAP — DISBONDED (FS 659 BL6L)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 659 AT BL 6L. REPAIRED PER SRM 53-31-00 PG 816.

Part: THRESHOLD — CORRODED (R1 DOOR)

AT HMV, THE R-1 DOOR THRESHOLD PANEL WAS FOUND WITH CORROSION DAMAGE AT THE FWD AND AFT DRAIN HOLES. REPAIRED PER SRM 53-15-00 PG 816-820.

Part: TEAR STRAP — DISBONDED (FS 639 BL 10R)

AT HMV, FOUND SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 639 AT BL 10R. REPAIRED PER SRM 553-31-00 PG. 810.

Part: TEAR STRAP — DISBONDED (FS 699)

DURING HMV, FOUND TEAR STRAP DISBONDED AT FS 699 BL-14L AND BL-6L. REPAIRED PER SRM 53-31-00 FIG 816.

Part: STRINGER — CORROSSION (FS 963)

DURING HMV, FOUND STRINGER AND SKIN CORROSION AT FS 963 STR 32 AND 34 IN THE MESC. REPAIRED PER SRM 53-13-00 PAGE 806.

Part: TEAR STRAP — DISBONDED (FS 699)

AT HMV, FOUND FUSELAGE SKIN TEAR STRAP DISBONDED AT FS 699 BL-36R. REPAIRED PER SRM 53-31-00 FIG 816.

Part: SKIN — CORRODED (FS BL 22R)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP CORRODED AT FS 679 AT BL 22R. REPAIRED PER SRM 53-31-00 PG 830.

Part: STIFFENER — CORRODED (PRESS BLKHD)

DURING OVERHAUL AFT P DOME STIFFENER IS CORRODED FROM WHERE IT TIES TO STR 41 TO HALF WAY UP STIFFENER. REMOVED CORRODED SECTION, INSTALLED STIFFENER SECTION AND SPLICE PER SRM 53-11-00 FIG 809.

Part: TEAR STRAP — DISBONDED (FS 579/BL26L)

AT HMV, FUSELAGE SKIN FAIL/SAFE TEAR STRAP WAS FOUND DISBONDED AT FS 579 AT STR 26L. REPAIRED PER SRM 53-31-00 PG806.

Part: TEAR STRAP — DISBONDED (FS 679 BL 26L)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 679 AT BL 26L. REPAIRED PER SRM 53-31-00.

Part: TEAR STRAP — DISBONDED (FS BL 12L)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 679, BL 12L. REPAIRED PER SRM 53-31-00.

Part: STRINGER — CORRODED (FS 963-983)

AT HMV, FOUND STRINGER 33 WITH CORROSION DAMAGE AT FS 983 AND 963. ALSO, LIGHT CORROSION ON FS 963 FRAME, JUST INBOARD OF STRINGER 34. REPAIRED PER SRM 53-13-00 PG 806.

Part: TEAR STRAP — DISBONDED (FS 719/BL20L)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 719 AT BL 20L. REPAIRED PER SRM 53-31-00 FIG 816.

Part: TEAR STRAP — DISBONDED (FS 679 BL 12L)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 679 BL 6R. REPAIRED PER SRM 53-31-00 PG 830.

Part: TEAR STRAP — DISBONDED (FS 639)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 639 AT BL 31R. REPAIRED PER SRM 53-31-00.

Part: STIFFENER — CORRODED (PRESS BLKHD)

DURING OVERHAUL AT AFT P-DOME, STIFFENER IS CORRODED ON LWR END WHERE IT TIES TO STR 25. REMOVED CORROSION AND INSTALLED STIFFENER AND SPLICE PER SRM 53-11-00 FIG 809.

Part: TEAR STRAP — DISBONDED (FS 719/BL12L)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 719 BL 12L. REPAIRED PER SRM 53-31-00 PG 816.

Part: TEAR STRAP — DISBONDED (FS 679 BL 10R)

AT HMV, FOUND FUSELAGE SKN FAIL/SAFE TEAR STRAP DISBONDED AT FS 679 AT BL 10R. REPAIRED PER SRM 53-31-00 PG 816.

Part: TEAR STRAP — DISBONDED (FS 719/ BL36L)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 719 AT BL36L. REPAIRED PER SRM 53-31-00 PG 816.

Part: TEAR STRAP — DISBONDED (FS719/BL44B)

AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 719 BL44R. REPAIRED PER SRM 53-31-00 FIG 816.

Part: SKIN — CRACKED (LT FLAP VANE)

NR 1 LEFT FLAP VANE UPPER SKIN CRACKED IN TWO PLACES UNDER BOTH RUB STRIPS. REMOVED DAMAGED SKIN SECTION, MFG AND INSTALLED SPLICE REPAIR AND DOUBLERS PER SRM 57-53-00 FIG 815. DAMAGE FOUND AT HMV.

Part: SKIN — CORRODED (FS 679 BL 28R)

AT HMV, FOUND CORROSION DAMAGE TO FUSELAGE SKIN UNDER FAIL/SAFE STRAP AT FS 679 BL 28R. REPAIRED PER SRM 53-31-00 PG 830.