N764DA

Part: HYD LINE — CRACKED (RT WING)

DURING DESCENT, -B- HYD SYSTEM FLUID LEVEL DROPPED TO 1/4 AND RESERVOIR LOW QTY LIGHT ILLUMINATED. REPLACED -B- SYSTEM RETURN LINE AT RT INBD GROUND SPOILER PER MM. SVCD -B- SYSTEM HYD LK CK AND OPN CK NORMAL.

Part: POWER PACK — INOP (L3 DOOR)

CEILING AND EXTERIOR EMERGENCY LIGHTS AT L3 DOOR INOP. REPLACED EMERGENCY LIGHT POWER PACK AT L3 DOOR. EMERGENCY LIGHTS CHECK GOOD PER MM.

Part: SKIN — DAMAGED (LT TE FLAP)

WING, LT / OUTB'D FLAP / UPPER SKIN: DOUBLER REPAIR. THE UPPER SKIN WAS FOUND WITH MULTIPLE PUNCTURES AND DENTS DUE TO GROUND HANDLING. DAMAGE APPROX 30 SPAN WISE X 20 CHORD WISE. REPAIR CONSISTED OF TRIMMING OUT ENTIRE DAMAGE SECTION OF SKIN AND SPLICING NEW SECTION IN PLACE.

Part: DECK — CRACKED (BS 415)

THE NOSE LANDING GEAR PRESSURE DECK WAS FOUND CRACKED IN SIX LOCATIONS. THE LOCATIONS ARE FROM FS 395 TO 437, BETWEEN RBL 24 AND LBL 24. REPAIRED PER ERA 333267-14, REV A.

Part: SUPPORT — CORRODED (RT TE FLAP)

DAMAGED FASTENER HOLES WERE NOTED IN THE RT NR 4 O/B TRACK SUPPORT AT WBL 731. THE HOLE WAS OVERSIZED TO A FINAL DIAMETER OF 0.799 INCH. REWORKED PER ERA 333262-14, REV A.

Part: SKIN — MISREPAIRED (BS 1745)

AN UNIDENTIFIED SKIN REPAIR WAS FOUND AT STA 1745 AND STR 45 AND 46. THE REPAIR WAS PARTIALLY REMOVED, INSPECTIONS ACCOMPLISHED AND IMPROVEMENTS TO THE REPAIR ACCOMPLISHED. REPAIRED PER ERA 333264-14, REV A.

Part: RIB CAP — CRACK (WS 555)

LT WING UPPER RIB CAP AT IWS 555 WAS FOUND CRACKED DURING A RTN INSP OF THE CAPS. REPAIRED PER ERA 333266-14, REV A.

Part: SKIN — CORRODED (BS 930)

CORROSION WAS FOUND ON THE INTERNAL SURFACE OF THE FUSELAGE SKIN CENTERED AT STA 930 BETWEEN S30 AND S31. REPAIRED PER ERA 333238-14, REV A.

Part: SERVO — FAILED (LT AILERON)

DURING APPROACH HAD DIFFICULTY FLYING STRAIGHT WITHOUT UNUSUALLY SEVERE RT AILERON AND RUDDER INPUTS SPI SHOWED LT OUTBD AILERON STUCK AT 8 UNITS UP. MTC IN PROGRESS LT AILERON NO MOVEMENT. REPLACED LT O/B AILERON SERVO, OPS CHECKS NORMAL.

Part: POWER SUPPLY — INOP (CABIN)

EMERGENCY LIGHT POWER SUPPLY BAD, CHARGE LIGHT FLASHING. REPLACED POWER SUPPLY.

Part: BULB — FAILED (EXTERIOR)

R2 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED.

Part: BULB — FAILED (EXTERIOR)

2L EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED, OPS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FOUND DURING LAYOVER 3L DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED POWER SUPPLY.

Part: BATTERY PACK — DISCHARGED (CABIN EEL)

EMERGENCY LIGHTS FORWARD OF L3 DOOR INOP. REPLACED BATTERY PACK, OPS CHECK NORMAL.

Part: BULB — FAILED (CABIN)

EMERGENCY PATH LIGHTING, ONE BULB OUT AT 21C. RELAMPED, OPS NML.

Part: FLOW REG — FAILED (NR 1 ENG FUEL)

DURING CRUISE, NR 1 ENGINE ROLLED BACK, GOT 1,000 PPH FUEL FLOW. DESCENDED TO 26,000 AND ATTEMPTED RESTART. FUEL FLOW STILL AT 1,000 PPH AT 36 PERCENT. ON ARRIVAL, FOUND EVIDENCE OF TAIL PIPE FIRE. BORESCOPED NR 1 ENG, REPLACED HP SOV, AND NR 1 FFR. PERFORMED PFHB TESTS 3, 13 AND 20. ENGINE CHECKS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

D-ZONE RT EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY AND OPERATION NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTS INOP FOR L-3 DOOR. REPLACED POWER SUPPLY.

Part: POWER SUPPLY — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT L-3 DOOR INOP. REPLACED POWER SUPPLY AND EMERGENCY LIGHTS CHECK GOOD.

Part: STRINGER — CRACKED (FS 297)

AT HMV, FOUND STRINGER CRACKED, STR 37 LOWER RADIUS AT FS 297. FABRICATED SPLICE PER SRM 53-13-00 PG 806 FIG 804, TREATED AND PAINTED AREA, INSTALLED SPLICE.

Part: REAR SPAR — CRACKED (RT WING)

DURING ACCOMPLISHMENT OF EO 7-59089-3, CRACKS WERE FOUND EMANATING FROM FOUR EXISTING FASTENER HOLES IN THE UPPER CAP, THE SPAR WEB, AND THE RIGHT WING UPPER SKIN. REPAIRS WERE ACCOMPLISHED PER DL ERA 270612-14AD.

Part: STRINGER — CRACKED (FS 297)

AT HMV, FOUND FUSELAGE STRINGER 37 WAS CRACKED IN LOWER RADIUS AT FS 297. REPAIRED PER SRM 53-13-00 PG 806 FIG 804.

Part: INLET RING — CRACKED (NR 2 ENG)

AT HMV, FOUND RING CRACKED, ON ANTI-ICE RING ON NR 2 ENG. REMOVED DAMAGED SECTION OF RING, FABRICATED REPAIR DOUBLER PER SRM 54-34-00 PG 804. INSTALLED DOUBLER PER SRM 54-34-00.

Part: INLET RING — CRACKED (NR 2 ENG)

AT HMV, FOUND RING CRACKED, INSIDE PANEL 311KC. FABRICATED REPAIR DOUBLER PER SRM 54-34-00 FIG 804, INSTALLED UPPER REPAIR, TRIMMED OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER PER ERA 270632-14.

Part: INLET RING — CRACKED (NR 2 ENGINE)

AT HMV, FOUND RING CRACKED, INSIDE PANEL 311 DR. DRILLED TACK PATTEN FOR LOWER RIVET CRACK. INSTALLED UPPER REPAIR DOUBLER. REPAIRED CRACK PER SRM 54-34-00 FIG 804.

Part: RIB — CORRODED (LANDING GEAR)

DURING HMV, THE A HOLE IN THE MLG ATTACH RIB WAS OVERSIZED TO REMOVE CORROSION. ACCOMPLISHED REPAIRS PER DL ERA 270587-14.

Part: DOUBLER — CORRODED (FS 459)

AT HMV, FOUND DOUBLER CORRODED AT STA 459 BL 0 FUSELAGE SKIN. REPLACED DAMAGED SECTION PER SRM 53-31-00.

Part: DOUBLER — CORRODED (FS 629-669)

AT HMV, FOUND EDGE DOUBLER CORRODED C1 B/B RT SIDE, FROM STA 629 TO 669. CUT OUT CORRODED SECTION OF DOUBLER AND REPLACED PER SRM 53-31-00 PG 863 FIG 825.

Part: FRAME — CORRODED (FS 923)

AT HMV, FOUND FUSELAGE FRAME CORRODED, STA 923 BETWEEN STR 30 TO 31, AFT SIDE. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 53-12-00.

Part: FLOORBEAM — CORRODED (FS 1792)

AT HMV, FOUND FS 1792 CABIN FLOORBEAM CORRODED ATL LBL 55. REPAIRED PER SRM 53-21-00 PG 865-868.

Part: FRAME — CRACKED (FS 1063)

DURING HMV IN ATLANTA, INSPECTION FOUND THE FUSELAGE FRAME CRACKED AT FS 1063 RBL116,BELOW FLOOR LINE AT BOTTOM HOLE. THIS WAS REPAIRED PER SRM 53-12-00. DRILLED REPAIR DOUBLER PER SRM 53-12-00 PG 809. INSTALLED DOUBLER PER SRM 53-12-00.

Part: STRINGER — CORRODED (FS 923-983)

AT HMV, FOUND STRINGER CORRODED STR 34 AT FS 923 TO 983. DRILLED NEW STRINGER AND SPLICE, INSTALLED PER SRM 53-13-00 FROM STA 913 TO 983.

Part: CAP DOUBLERS — CUT (WS 293/319)

AT HMV, CUT EXISTING CAP AT IWS 293.58 AND 319.83 TO FACILITATE FASTENER REMOVAL. UPPER RIB CAPS, APPROX 10 INCHES FROM REAR SPAR. REF VA31744 AND EO 7-59089-3. CUT CAP AT 293.58 AND 319.83 TO FACILITATE FASTENER REMOVAL. FABRICATED DOUBLERS AS PER SRM 57-12-00 PG 805, FOR STA 293.58 AND 319.83. INSTALLED DOUBLERS PER SRM 57-12-00 PG 805.

Part: CAP — CUT (WS 293)

DURING HMV, HAD TO CUT CAP AT IWS 293.58 AND 319.83 TO FACILITATE FASTENER REMOVAL. CUT CAPS AS NECESSARY TO FACILITATE MAINTENANCE, TRIMMED AND DRILLED REPAIR DOUBLERS AS PER SRM 57-12-00 PG 805. INSTALLED REPAIR ANGLES PER SRM 57-12-00 PG 805.

Part: PANEL — CORRODED (FS 1542)

AT HMV, FOUND PANEL CORRODED, C2 C/C 1542. DRILLED NEW PANEL, REPLACED PANEL PER SRM 53-24-00.

Part: ANGLE — CRACKED (NR 2 S DUCT)

AT HMV, FOUND NR 2 ENGINE INLET STRUCTURE CRACKED INSIDE PANEL 311UL AND 311UR AT FS 1705 JUST AFT OF NR 2 INLET L/E LIP. REPAIRED PER SRM 54-12-00 FIG 803.

Part: BUSHING — WORN (NR 3 PYLON)

AT HMV, FOUND BUSHING WORN ON NR 3 PYLON O/B WING. REMOVED BUSHING AND CLEANED BORE. INSTALLED NEW BUSHING PER SRM 54-11-00 HONED BUSHING TO 2.5005, SIZE OK.

Part: BUSHING — GOUGED (NR 3 PYLON)

AT HMV, FOUND BEARING GOUGED, NR 3 PYLON MAIN ATTACH CENTER BEARING. REMOVED BUSHING AND CLEANED BORE. INSTALLED NEW BUSHING PER SRM 54-11-00. HONED BUSHING TO 2.5005, SIZE OK.

Part: BUSHING — WORN (NR 3 PYLON)

AT HMV, NR 3 PYLON O/B WING, PYLON MAIN ATTACH I/B BUSHING WAS WORN BEYOND LIMITS. REPAIRED PER SRM 54-11-00. ALSO, O/B WING, PYLON MAIN ATTACH CENTER BEARING IS GOUGED. REPAIRED PER SRM 54-11-00.

Part: DOUBLER — CORRODED (BS 1453-1625)

AT HMV, FOUND CENTER STRAP CORRODED, AT C2 B/B STR NR 3, FROM FS 1453 TO FS 1625. REMOVED CENTER STRAP. MFG NEW SPLICE DOUBLER AS PER SRM 53-31-00 FIG 825. INSTALLED NEW STRAP ON NR 1391.

Part: LONGERON — CRACKED (FS 1860)

DURING HMV, THE OUTER CAP ANGLE OF THE LT UPPER LONGERON IN THE FUSELAGE AFTER BODY AT APPROX STA 1860 AND WL 328 WAS FOUND CRACKED IN THE RADIUS. THE CRACK EXTENDS FROM THE AFT END OF THE PART FWD APPROX 6 INCHES ALONG THE RADIUS. REPAIRED PER DL ERA 270462-14AD.

Part: PANEL — CRACKED (NR 1 PYLON)

DURING HMV, FOUND PYLON STRUCTURE AT AFT O/B CORNER FASTENER FOR FWD PYLON PANEL 451TZ IS CRACKED. WELDED THE CRACK PER SRM 54-11-00 PG 812.

Part: FITTING — CORRODED (LT MLG)

AT HMV, FOUND FITTING CORRODED, LEFT MLG UPPER HOLES AT NR 1 TO 6 ATTACH POINT FOR RETRACT ACT FITTING. REAMED HOLES TO REMOVE CORROSION. INSTALLED BUSHING, PER SRM 57-14-00.

Part: HOLE — CORRODED (RT MLG)

AT HMV, FOUND HOLE CORRODED/PITTED. FITTING FOR RT MLG ACT. REAMED HOLE TO .690, TURNED BUSHING TO SIZE AND CAD PLATED PER PS 900-3-9, PRIMED HOLE PER PS 900-3-6, INSTALLED BUSHING PER SRM 57-14-00.

Part: FITTING — DAMAGED (LT MLG)

DURING HMV, FOUND FITTING ON LT MLG DAMAGED AT LOWER HOLES 17 TO 20. REAMED HOLES TO .625 TO REMOVE DAMAGE. DID HFEC CHECK, PRIMED HOLES AND INSTALLED BUSHINGS AS PER SRM 57-11-00.

Part: FLOORBEAM — CORRODED (BS 901)

AT HMV, FOUND FLOORBEAM CORRODED FS 901 LBL 68 TO LBL 92 TASK NR C-53-100-02. REMOVED DAMAGED AREA PER SRM 53-21-00 PG 849 TO 852. DYE PENETRANT CHECKED, CUT AREA PER PS 900-6-3 NR 1. NO CRACKES FOUND ON DYE CHECK. FABRACATED NEW CAP, INSTALLED NEW T-CAP PER SRM 53-21-00 PG 849 TO 852.

Part: FORMER — CORRODED (BS 1809)

P-DOME FORMER STA 1809 Z ANGLE AFT OF STR 42 CORRODED. REMOVED CORRODED SECTION OF FORMER, FABRICATED NEW FORMER SEGMENT DOUBLER AND INSTALLED PER SRM 53-11-00 FIG 809.

Part: DOUBLER — CORRODED (BS 1685-1705)

AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED, AT STA 1685 THRU 1705. MFG NEW SLICE DOUBLER PER SRM 53-31-00 AND INSTALLED ON NR 1391.

Part: DOUBLER — CORRODED (BS 1625-1645)

AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED AT STA 1625 TO 1645. MFG NEW SPLICE DOUBLER PER SRM 53-31-00 AND INSTALLED ON NR 1391.

Part: STRINGER — CORRODED (BS 1625-1645)

DURING HMV, FOUND STRINGER 33 CORRODED BETWEEN STA 1625 AND 1645. REMOVED STRINGER SECTION, DRILLED UP NEW STRINGER SECTION AND INSTALLED STRINGER PER SRM 53-13-00 PG 806.

Part: CHANNEL — CORRODED (NR 5 LAV)

AT HMV, FOUND CHANNEL CORRODED AT NR 5 LAV AT ENTRY. REPLACED HAT CHANNEL PER SRM 53-21-00 PG 859-860.

Part: DOUBLER — CORRODED (BS 1792-1801)

AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED, AT STA 1792 TO 1801. MFG NEW DOUBLER PER SRM 53-31-00 AND INSTALLED ON NR 1391.

Part: FORMER — CORRODED (PRESS DOME)

DURING HMV, FOUND P-DOME FORMER AFT OF STR 24 WHERE IT ATTACHES TO 1809 Z ANGLE TO BE CORRODED. REMOVED CORROSION , OUT OF LIMITS. REPAIRED AS PER SRM 53-11-00 FIG 809.

Part: DOUBLER — CORRODED (FS 1665-1685)

AT HMV, INSPECTION FOUND THE INTERNAL SPLICE DOUBLER CORRODED AT STA 1665 TO 1685, LOWER CENTER FUSELAGE SKIN. REPAIRED PER SRM 53-31-00 FIG 825 SH 4.

Part: DOUBLER — CORRODED (BS 1745-1765)

AT HMV, FOUND SPLICE DOUBLER CORRODED AT STA 1745 TO 1765, LT STRINGER 33. MFG NEW SPLICE DOUBLER PER SRM 53-31-00 FIG 825 AND INSTALLED ON NR 1391.

Part: FLOORBEAM — CORRODED (FS 1665)

AT HMV, FOUND FLOORBEAM CORRODED AT STA 1665 FROM DOOR SILL I/B 24 INCHES. REPLACED DAMAGED SECTION OF T-CAP PER SRM 53-23-00 PG 803.

Part: FLOORBEAM — CORRODED (FS 1685)

AT HMV, FOUND FLOORBEAM UPPER CAP AT FS 1685 WITH CORROSION DAMAGE AT DOOR SILL TO LEFT SIDE SEAT TIE DOWN TRACK. TRIMMED OUT DAMAGED SECTION A RBL 3.5 PER SRM 53-23-00 FIG 802. FABRICATED NEW FLOOR CAP, INSTALLED REPAIR PER SRM 53-23-00.

Part: DOUBLER — CORRODED (BS 1765-1783)

AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED, AT STA 1765 TO 1783. MFG NEW SPLICE DOUBLER, AND INSTALLED ON N/R 1391. PER SRM 53-31-00.

Part: CHANNEL — CORRODED (NR 3 AFT LAV)

AT HMV, FOUND CHANNEL CORRODED, LOWER CHANNEL AT AFT NR 3 AFT LAV TASK NR 53-100-02. INSTALLED NEW CHANNEL PER SRM 53-21-00 PG 859.

Part: CHANNEL — CORRODED (NR 4 AFT LAV)

AT HMV, FOUND CHANNEL CORRODED, LOWER CHANNEL AT ENTRY TO NR 4 LAV, TASK NR C-53-100-02. REPLACED CHANNEL.

Part: FLOORBEAM — CORRODED (FS 281)

AT HMV, INSPECTION FOUND HEAVY CORROSION ON FLOORBEAM AT FS 281 ON ALMOST THE ENTIRE UPPER CAP. REPAIRED BY REPLACING UPPER T-CAP PER SRM 53-21-00.

Part: FLOORBEAM — CORRODED (FS 1725)

AT HMV, INSPECTION FOUND FLOORBEAM CORRODED AT FS 1725, AREAS OF CORROSION FROM LBL 59 TO RBL 59. REPLACED SECTION OF T-ANGLE PER SRM 53-21-00.

Part: DOUBLER — CORRODED (BS 1778-1792)

AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED, AT STA 1778 TO 1792. MFG NEW DOUBLER PER SRM 53-31-00 AND INSTALLED ON NR 1391.

Part: CHANNEL — CORRODED (BS 1809)

DURING HMV, P-DOME Z CHANNEL AT STA 1809 STR 40 TO SPLICE AT STR 29 FOUND TO BE CORRODED. REMOVED Z ANGLE FROM STRINGER 22 TO 44, FABRICATED SPLICE DOUBLER AS PER SRM 53-11-00 PG 946, AND INSTALLED AS PER SRM 53-11-00 FIG 848.

Part: DOUBLER — CORRODED (BS 1645-1665)

AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED, AT STA 1645 TO 1665. MFG NEW SPLICE DOUBLER PER SRM 53-31-00, AND INSTALLED ON NR 1391.

Part: FORMER — CORRODED (PRESS DOME)

DURING HMV, FOUND P-DOME FORMER IN CENTER OF P-DOME CORRODED, AREA WHERE ATTACHES TO 1809 Z ANGLE. REMOVED CORRODED SECTION OF FORMER, FABRICATED NEW FORMER AND INSTALLED PER SRM 53-11-00 FIG 809.

Part: DOUBLER — CORRODED (BS 1705-1725)

AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED, AT STA 1705 THRU 1725. MFG NEW SPLICE DOUBLER PER SRM 53-31-00 AND INSTALLED ON NR 1391.

Part: CHANNEL — CORRODED (BS 1809)

DURING HMV, Z CHANNEL AT STA 1809 STR 24 FOUND TO BE CORRODED. REMOVED Z ANGLE FROM STR 44 TO 22, CUT AND DRILLED NEW Z ANGLE AND SPLICE DOUBLER, INSTALLED PER SRM 53-11-00 FIG 848.

Part: SKIN — CORRODED (FS 967)

AT HMV, INSPECTION FOUND SKIN CORRODED FS 967 BL 3L IN THE MESC. ROUTED OUT DAMAGE AND FABRICATED REPAIR DOUBLER PER SRM 53-31-00 FIG 836.

Part: CENTER STRAP — CORRODED (FS 479)

AT HMV, INSPECTION FOUND CENTER STRAP CORRODED IN C-1 B/B AT LT SIDE OF STR 33, STA 479. REPLACED DAMAGED SECTION OF STRAP PER SRM 53-31-00 FIG 822.

Part: FLOOR BEAM — CORRODED (FS 901)

AT HMV, FOUND FLOORBEAM CORRODED, AT FS 901 RBL 65 TO 71, TASK NR C-53-100-02. TRIMMED FLOORBEAM UPPER FLANGE, INSTALLED REPAIR PER SRM 53-21-00 PG 849 TO 852.

Part: CHANNEL — CORRODED (NR 2 AFT LAV)

AT HMV, FOUND CHANNEL CORRODED AT BOTTOM OPENING OF NR 2 AFT LAV. INSTALLED NEW CHANNEL PER SRM 53-21-00.

Part: CENTER STRAP — CORRODED (FS 539)

AT HMV, INSPECTION FOUND CENTER STRAP CORRODED IN C-1 B/B AT RT SIDE STR 33, STA 539 TO 549. REPLACED SECTION OF SPLICE STRAP PER SRM 53-31-00 FIG 822.

Part: TEAR STRAP — DISBONDED (BS 639)

AT HMV, FOUND C1 B/B TEAR STRAP DISBONDED AT STR 34 TO 35 STA 639. CLEANED AREA, NO CORROSION FOUND. INSTALLED REPAIR PER SRM 53-31-00 PG 830.

Part: CENTER STRAP — CORRODED (FS 679-709)

AT HMV, INSPECTION FOUND CENTER STRAP CORRODED IN C-1 B/B AT STR 33, STA 679 TO 709. REPLACED INTERNAL SPLICE STRAP PER SRM 53-31-00 FIG 822.

Part: DOUBLER — CORRODED (FS 943-983)

AT HMV, INSPECTION FOUND INTERNAL DOUBLER CORRODED ON BOTH SIDES OF STR 33 FROM FS 943 TO 983, LOWER FUSELAGE SKIN. MADE NEW REPLACEMENT INTERNAL SPLICE STRAP AS PER SRM 53-31-00 FIG 822.

Part: CHANNEL — CORRODED (NR 1 AFT LAV)

AT HMV, FOUND CHANNEL CORRODED AT OPENING TO NR 1 AFT LAV. INSTALLED NEW HAT CHANNEL, PER SRM 53-21-00 PG 859-860.

Part: TEAR STRAP — DISBONDED (BS 911)

AT HMV, INSPECTION FOUND A TEAR STRAP DISBONDED IN C-1 BAG BIN AT STA 911 BETWEEN STR 34 TO 35. CLEANED CORROSION AND INSTALLED REPAIR PER SRM 53-31-00 PG 830.

Part: TEAR STRAP — DISBONDED (BS 699)

AT HMV, INSPECTION FOUND TEAR STRAP DISBONDED IN C-1 B/B AT STA 699 BETWEEN STR 34 TO 35. INSTALLED REPAIR PER SRM 53-31-00 PG 830.

Part: CENTER STRAP — CORRODED (FS 901)

AT HMV, INSPECTION FOUND CENTER STRAP CORRODED IN C-1 B/B AT STR 33, STA 901 TO 943. MADE NEW REPLACEMENT INTERNAL SPLICE STRAP AS PER SRM 53-31-00 FIG 822.

Part: CENTER STRAP — CORRODED (FS 499)

AT HMV, INSPECTION FOUND CENTER STRAP CORRODED IN C-1 B/B AT LT AND RT SIDE OF STR 33, STA 499. REPLACED DAMAGED SECTION OF STRAP PER SRM 53-31-00 FIG 822.

Part: TEAR STRAP — DISBONDED (BS 875)

AT HMV, INSPECTION FOUND A TEAR STRAP DISBONDED IN THE C-1 B/B BETWEEN STR 34 TO 35 STA875. INSTALLED REPAIR PER SRM 53-31-00 PG 830.

Part: TEAR STRAP — DISBONDED (BS 894)

AT HMV, INSPECTION FOUND TEAR STRAP DISBONDED IN C-1 B/B BETWEEN STR 34 TO 36 AT STA 894. INSTALLED REPAIR PER SRM 53-31-00.

Part: CENTER STRAP — CORRODED (FS 886)

AT HMV, INSPECTION FOUND CENTER STRAP CORRODED IN C-1 B/B AT STR 33, STA 886 TO 901. REPLACED INTERNAL STRAP AS PER SRM 53-31-00 FIG 822.

Part: SKIN — CORROSION (RT TE FLAP VANE)

DURING HMV, CORROSION WAS FOUND ON NR 4 FLAP VANE UPPER SKIN. REMOVED CORROSION PER SRM 51-21-01 PAGE 61.

Part: SKIN — DELAMINATED (NR 2 SPOILER)

AT HMV, FOUND UNDERSIDE OF NR 2 SPOILER HAD GOUGES. REPAIRED PER SRM 57-52-00. ALSO, FOUND CORROSION AND CRACK ON LOWER SIDE JUST ABOVE SEAL. REPAIRED PER SRM 57-52-00.

Part: CENTER STRAP — CORRODED (FS 609-649)

AT HMV, FOUND CENTER STRAP CORRODED FROM FS 609 TO FS 649. MADE NEW STRAP PER AND INSTALLED PER SRM 53-31-00.