N784DA

Part: INVERTER — FAILED (CABIN)

LWR GALLEY EMERG LIGHTS INOP. REPLACED INVERTER MODULE ON BACK OF BATTERY PACK, CKS OK.

Part: BLEED VALVE — MALFUNCTIONED (NR 1 ENGINE)

FIRE WARNING BOTH LOOPS, NR 1 ENG. REPLACED BLEED VALVE CKS GOOD.

Part: SPAR CAP — CRACKED (LT WING)

A FASTENER WAS FOUND CRACKED IN THE LT LOWER SPAR CAP AND SKIN. IT AND THE ADJACENT FASTENER HOLE WERE O/S. THE HOLES WERE COLD-WORKED AND INSTALLED WITH HI-LOKS.

Part: PROX LOGIC BOX — FAILED (E/E BAY)

ALL WARNING LIGHTS FAILED AS PREVIOUS LOG BOOK ENTRY, LDG GEAR, SLAT REV PRESS AND INTRANSIT LIGHTS, DOOR OPEN LIGHTS. AIR TURNBACK TO SEA, NO GREEN DOWN AND LOCK LIGHT GEAR.

Part: ACTUATOR — INOPERATIVE (L 2 DOOR)

2L DOOR ELECTRIC ACTUATION INOPERATIVE. UNABLE TO CLOSE DOOR MANUALLY. REPLACED 2L DOOR ACTUATOR ASSEMBLY, OPERATION NORMAL.

Part: FITTING — BROKEN (LT AILERON)

LEFT INBOARD AILERON POSITION INDICATOR ON SPI IS STUCK IN FULL DOWN POSITION. REPLACED LEFT INBD AILERON POSITION TRANSMITTER. ALSO, FOUND LEFT O/B ACTUATOR ATTACH FITTING HAD BROKEN LOOSE FROM AILERON. REPLACED AILERON AND ROUTED TO SHOP.

Part: BRAKES — SEIZED (RT MLG)

AFTER START BRAKES REMAINED LOCKED, ALTHOUGH HANDLE RELEASED AND LIGHT WENT OUT. FOUND NR 3 FRONT BRAKE ASSY FROZEN ON AXLE. REPLACED RT FWD MAIN GEAR AXLE, BRAKE AND WHEEL ASSY. WHEEL BEARING FAILED, DAMAGED AND CUT INTO AXLE.

Part: EEL POWER PACK — FAILED (CABIN)

DURING LAYOVER, L-4 DOOR EMERGENCY LIGHT POWER SUPPLY POPS C/B. REPLACED POWER SUPPLY AND OPERATION NORMAL.

Part: FITTING — CRACKED (AFT P-DOME)

COMPLYING WITH INSPECTION SI 7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTING CRACKED AT STRINGER NR 11. SCHEDULED THE FITTING REPLACEMENT PER DL ERA 271759-14.

Part: EEL POWER SUPPLY — INOP (L4 DOOR)

L4 DOOR EMERGENCY LIGHT INOP. REPLACED EMER LIGHT BATT PACK, DAL P/N 337001090 SN NR 54051.

Part: BLKHD FITTINGS — CRACKED (AFT PRESS BLKHD)

DURING THE ACCOMPLISHMENT OF AN INSPECTION OF THE AFT PRESSURE BULKHEAD STRINGER SPLICE FITTINGS PER SI 7-66332-12, THE STR 11 FITTING WAS FOUND TO HAVE CRACKS, IT IS 7075-T6 FORGED AL. ACCOMPLISHED REPAIRS PER DL ERA 271759-14AD.

Part: SKIN — CRACKED (NR 3 PYLON)

AT HMV, INTERFACE BOX CRACKED, NR 3 PYLON FWD END. REPAIRED PER SRM 54-11-00 PG 812.

Part: FLOORBEAM — CORRODED (FS 1523)

AT HMV, FOUND FLOORBEAM CORRODED AT FS 1525, RIGHT SIDE. REMOVED SECTION OF FLOORBEAM AT STA 1523 RT SIDE. FAB REPAIR PARTS REF SRM 53-23-00 FIG 802.

Part: FLOORBEAM — CORRODED (FS 1525)

AT HMV, C-2 CARGO COMPT FLOORBEAM FS 1525 FOUND CORRODED AT LBL 3. REPAIRED PER SRM 53-23-00 PG 803.

Part: FLOORBEAM — CORRODED (FS 1480)

AT HMV, C-2 CARGO COMPT FLOORBEAM FS 1480 LBL 60 CORRODED. REMOVE CAP SECTION, FAB NEW CAP PER SRM 53-23-00 FIG 802 PG 803/804.

Part: REAR SPAR — CRACKED (CENTER WING)

WHILE ACCOMPLISHING EO 7-59040-3 STRUCTURAL MODIFICATION TO THE REAR SPAR JOINT AT THE BL 115 WING ROOT RIBS, CRACKS WERE FOUND IN THE CENTERWING REAR SPAR WEB TO BL 115 RIB WEB ATTACH ANGLE EMANATING FROM EXISTING ATTACHMENT HOLES. THE CRACKING IS PRESENT ON BOTH THE SPAR WEB AND THE RIB WEB ATTACH FLANGES. ACCOMPLISHED REPAIRS PER DL ERA 270996-14.

Part: SKIN — CORRODED (FS 1453-1815)

THE AFT BELLY SKIN WAS FOUND CORRODED AND HAD SEVERAL PREVIOUS REPAIRS REQUIRING REPLACEMENT OF THE BELLY SKIN AT FS 1453 TO 1815, DAMAGE FOUND AT HMV. REPAIRS ACCOMPLISHED PER DL ERA 270891AD.

Part: SKIN — CRACKED (RT ELEVATOR)

THE O/B L/E UPPER SIDE PANEL WAS FOUND TO BE CRACKED. REPAIRED PER SRM 55-22-00, AT HMV FOR RIGHT ELEVATOR.

Part: DOUBLER — TORN (FS 1490)

AT HMV, FOUND INTERNAL DOUBLER FOR FUS TORN AT STA 1490 BETWEEN STR 27 TO 28, C2 B/B. REMOVED DAMAGE INSTALLED DOUBLER PER SRM 53-31-00.

Part: SUPPORT — CRACKED (LBL 8.5-RBL 8.5)

AT HMV, FOUND SUPPORT CRACKED C2 B/B LBL 8.5 AND RBL 8.5. DYE PENETRANT, INSPECTED CRACKS AND STOP DRILLED BOTH CRACKS. FABRICATED NEW ANGLES, DRILLED NEW ANGLES, TREAT AND PAINTED, AND INSTALLED NEW ANGLES PER SRM 53-24-00 PG 807 FIG 805.

Part: FLOOR SUPPORT — CORRODED (FS 649)

AT HMV, FOUND FLOOR SUPPORT CORRODED FS 649 O/B. REMOVED FLOOR SUPPORT, DRILLED NEW FLOOR SUPPORT AND SPLICE ANGLE, INSTALLED PER SRM 53-23-00 FIG 802.

Part: FLOOR SUPPORT — CORRODED (FS 689)

AT HMV, FOUND FLOOR SUPPORT CORRODED, C1 B/B AT FS 69. REMOVED SUPPORT, DRILLED TREAT AND PAINTED, INSTALLED PER SRM 53-23-00 FIG 802.

Part: TEAR STRAP — DISBONDED (FS 769-789)

AT HMV, FOUND TEAR STRAP DISBONDED, AFT CORNER LOWER GALLEY AREA BETWEEN FS 769 TO 789 STA 38. CORROSION REMOVED, PER SRM 51-21-01, FOUND TO BE WITHIN LIMITS PER SRM 53-31-00 FIG 801. MFG AND INSTALLED DOUBLER PER SRM 53-31-00 FIG 804.

Part: SKIN — CRACKED (RT ELEVATOR)

THE T/E TIP SKIN WAS FOUND TO BE CRACKED ON THE LOWER SIDE. THIS WAS REPAIRED PER SRM 55-22-00 FIG 802, AT HMV FOR RT ELEVATOR.

Part: TRACK — CORRODED (FS 1445-1545)

AT HMV, FOUND CABIN SEAT TRACKS WITH CORROSION DAMAGE AT FS 1445 TO 1545. REPLACED TRACK PER SRM 53-23-00.

Part: SEAT TRACK — CORRODED (FS 1443-1545)

AT HMV, FOUND SEAT TRACK CORRODED STA 1443 TO 1545. REMOVED SEAT TRACK AND INSTALLED NEW TRACK PER SRM 53-21-00 PG 836.

Part: ANTI-ICE DUCT — CRACKED (NR 2 ENGINE)

NR 2 ENG INLET AT 5:30 O'CLOCK POS. ANTI-ICE DUCT SKIN CRACKED AROUND RIVET. ACCESS THRU PANEL 311 GR-MARKED, REF NR 712. REMOVED DAMAGED AREA. FABRICATED DOUBLER SPACERS AND SHIMS PER SRM 54-34-00 FIG 804.

Part: RIB — CORROSION (WS 346)

DURING THE COMPLETION OF EO 7-56199-3AD, THE RT IWS 346 MLG ATTACH RIB UPPER I/B 1.125 HOLE WAS FOUND WITH CORROSION IN THE HOLE BORE. REPAIRED PER DL ERA 270991-14AD.

Part: SEAT TRACK — CORRODED (FS 649-749)

AT OVERHAUL THE SEAT TRACK AT STA 649-749, 1ST TRACK TO LEFT OF CENTER, WAS FOUND CORRODED. REPLACED SEAT TRACK PER SRM 5321-00 PG 836.

Part: FLOOR BEAM — CORRODED (FS 313)

FLOOR BEAM F.S. 313 CORRODED ON UPPER CAP FROM APPROX. RBL 16-LBL 16. REF TASK NR C-53-100-02. REPAIRED PER SRM 51-21-01, 53-21-00 PG 823-824.

Part: SKIN DOUBLER — CORRODED (FS 328)

AT HMV, INSPECTION FOUND .020 EDGE DOUBLER AT SKIN SPLICE BOTTOM LEFT OF STR 33 AT STA 328 CORRODED. FABRICATED NEW EDGE DOUBLER SEGMENT IAW SRM 53-31-00 PG 863 AND INSTALLED.

Part: DOUBLER — CORRODED (FS 325)

AT HMV, INSPECTION FOUND .020 BONDED DOUBLER CORRODED AT STA 325 RIGHT OF CENTERLINE. REMOVED DAMAGE SECTION OF EDGE DOUBLER AND INSTALLED REPAIR PER SRM 53-31-00 PG 863.

Part: STRAP — CORRODED (BS 1745)

FOUND DURING HMV, FAILSAFE STRAP LIFTED/CORRODED C-3 B/B FS 1745 BETWEEN STR 44 AND 45. REPAIRED PER SRM 53-31-00 FIG 801.

Part: TEAR STRAP — DISBONDED (FS 1783)

AT HMV, FOUND TEAR STRAP DISBONDED AT FS 1783 BETWEEN STR 23 THROUGH 24. REPAIRED PER SRM 53-31-00 PG 830.

Part: FRAME — CRACKED (FS 267)

AT HMV, FOUND FRAME CRACKED STA 267 RT SIDE OF E AND E ABOVE STR 9. REPAIRED PER SRM 53-12-00 FIG 805 AND DL ERA 271044-14.

Part: STRINGER — CORRODED (BS 1645-1725)

FOUND DURING HMV, C-3 B/B STRINGER CORRODED FS 1645 TO 1725 STR 39. REPLACED DAMAGED STRINGER FROM FS 1675 TO 1695 PER SRM 53-13-00 PG 806.

Part: FLOORBEAM — CORRODED (BS 1505)

AT HMV, FLOORBEAM CORRODED AFT OF FS 1505 BELOW LEFT FIXED FLOOR PANEL ABOVE STRINGER 40. REPAIRED PER SRM 53-23-00 FIG 802.

Part: STRAP — DISBONDED (FS 901-923)

AT HMV, FUSELAGE SKIN FAILSAFE STRAP WAS FOUND LIFTED AND CORRODED IN LOWER GALLEY FS 901 TO 923 STR 40 TO 45. REPAIRED STRAP AND CLEANED CORROSION PER SRM 53-31-00 FIG 804 AND 816.

Part: FAIL-SAFE STRAP — CORRODED (FS 1765-1785)

AT HMV, FOUND FAIL-SAFE STRAP CORRODED IN C3 B/B AT FS 1765 TO 1785 BETWEEN STR 42 TO 34. REPAIRED PER SRM 53-31-00.

Part: PRESSURE DECK — CRACKED (FS 1243)

ON HMV, FOUND RT PRESSURE DECK CRACKED STA 1243 6 INCHES INBD OF FRAME. REPAIRED PER SRM 53-11-00 FIG 844.

Part: FAIL-SAFE STRAP — CORROSION (FS 1763-1778)

AT HMV, FOUND FAIL-SAFE STRAP CORRODED C3 B/B FS 1763 TO 1778 BETWEEN STR 43 TO 45. REPAIRED PER SRM 53-31-00.

Part: P-DOME — CORRODED (FS 1809)

AT HMV, FOUND P-DOME CORRODED, LOWER WEB AFT OF FS 1809 STRINGER 1809. REMOVED CORROSION, FABRICATED NEW SECTION, AND INSTALLED PER SRM 53-11-00 FIG 848.

Part: FAILSAFE STRAP — CORRODED (BS 1403-1423)

FAILSAFE STRAP LIFTED/CORRODED C2 BB AT FS 1403 TO 1423 STR 35 AND 36, FOUND AT HMV. REPAIRED PER SRM 53-31-00.

Part: STRAP — CORRODED (FS 1725)

FAILSAFE STRAP LIFTED/CORRODED C-3 B/B FS 1725 BETWEEN STR 33 AND 34, FOUND DURING HMV. REPAIRED PER SRM 53-31-00. FIG 801.

Part: STRAP — DISBONDED (BS 1763 1778)

FOUND DURING HMV, FAILSAFE STRAP LIFTED/CORRODED C-3 B/B FS 1763 TO 1778 BETWEEN STR 43 TO 45. REPAIRED PER SRM 53-31-00 FIG 816.

Part: STRAP — CORRODED (BS 1685-1705)

FOUND DURING HMV, FAILSAFE STRAP LIFTED/CORRODED FROM FUSELAGE SKIN, FS 1685 TO 1705 BETWEEN STR 39 AND 40. REPAIRED PER SRM 53-31-00 FIG 801.

Part: STRAP — CORRODED (FS 1665-1685)

FOUND DURING HMV, FAILSAFE STRAP LIFTED FROM SKIN C-3 B/B BETWEEN FS 1665 TO 1685 STR 43 AND 44. REPAIRED PER SRM 53-31-00 PG 807.

Part: FRAME — CRACKED (BS 281)

AT HMV, FUSELAGE FRAME IN FESC LT SIDEWALL IS CRACKED AT FRAME SPLICE AT STA 281 BETWEEN STR 47 AND 48. REPAIRED PER SRM 53-12-00 FIG 814.

Part: FAILSAFE STRAP — CORRODED (FS 1525-1545)

AT HMV, FUSELAGE SKIN FAILSAFE TEAR STRAP WAS FOUND LIFTED AND CORRODED AT FS 1525 TO FS 1545 STRINGER 35. ACCOMPLISHED REPAIRS PER ERA 270891-14 REV C.

Part: INTERCOSTAL — CORRODED (FS 282-298)

AT HMV, FOUND INTERCOASTAL CORRODED BETWEEN FS 282 TO 298. FABRICATED NEW INTERCOASTAL AND INSTALLED PER SRM 51-10-05.

Part: TEAR STRAP — DISBONDED (FS 953)

AT HMV FOUND TEAR STRAP DISBONDED, AT FS 953 BETWEEN STR 37 AND 38. CLEANED AREA AND REPAIRED PER SRM 53-31-00.

Part: ANGLE — CRACKED (FS 1705)

AT HMV, INSPECTION FOUND AN ANGLE CRACKED 6 FEET AFT OF NR 2 INLET, LT SIDE, 9 O'CLOCK POSITION, ON FWD SIDE OF BULKHEAD RING. REMOVED ANGLE, FABRICATED T-ANGLE AND FILLER PER SRM 54-12-00.

Part: TEAR STRAP — DISBONDED (FS 865)

AT HMV, INSPECTION FOUND FAILSAFE STRAP DISBONDED BETWEEN STR 28 AND 29 AFT SIDE OF FORMER FS 865. CUT TEARSTRAP, REMOVED ADHESIVE, NO CORROSION FOUND. CHECKED NEGLIGIBLE DAMAGE LIMITS PER SRM AND FOUND TO BE WITHIN LIMITS REF SRM 53-31-00. INSTALLED REPAIR PER SRM 53-31-00 FIG 804.

Part: FLOOR BEAM — CORRODED (FS 1763)

AT HMV, INSPECTION FOUND CABIN FLOOR BEAM CORROSION AT F.S. 1763 AT RBL 52. REPAIRED BY REPLACING SECTION OF T CAP PER SRM 53-21-00 PG 823.

Part: STRAP — CORRODED (FS 1725)

AT HMV, FOUND FAILSAFE STRAP CORRODED IN C3 B/B, FS 1725 BETWEEN STR 33 AND 34. REMOVED STRAP FS 1725 FROM STR 33 TO 29. REMOVED DAMAGED, TREATED AND PAINTED PER PS 900-2 NR 5, INSTALLED PER SRM 53-31-00.

Part: HOLES — CORRODED (RT MLG)

AT HMV, FOUND HOLES CORRODED, RMLG 11-16 ACT ATTACH FITTING. REAMED HOLES TO .562 INCH, CORROSION REMOVED WITHIN LIMITS PER SRM 57-14-00. HFEC HOLED AND FACE, ROTO PEENED PER PS 900-4 NR 5. CAD PLATED PER PS 900-9 NR 4. TURNED BUSHINGS TO SIZE AND TREATED. INSTALLED BUSHING AND REAMED TO SIZE. OXIDE BLASTED, PRIMED, AND PAINTED.

Part: FITTING — CORRODED (RT MLG)

AT HMV FOUND HOLE CORRODED, 1, 2, 3, 5, 6, RMLG ACT FITTING. REAMED TO .688 INCH, CORROSION REMOVED. SPOT FACED NR 3 HOLE 1.750 INCH DIA AND .010 INCH DEEP CORROSION REMOVED. HFIC HOLES AND FACE. ROTO PEENED PER PS 900-4 NR 5. CAD PLATED PER PS 900-3-9 NR 5. HOLES AND SPOT FACE WITHIN SRM 57-14-00 LIMITS. TURNED BUSHING TO SIZE AND TREATED INSTALLED BUSHING AND REAMED TO SIZE OXIDE BLASTED, PRIMED, AND PAINTED. MFG, TREATED, INSTALLED WASHER.

Part: FAIL/SAFE STRAP — DISBONDED (FS 749-769)

DISBONDED FAIL/SAFE STRAP BETWEEN STR 37 AND 38 AND FORMER 749 AND 769. FOUND AT HMV, REPAIRED PER SRM 53-31-00.

Part: STRAP — DISBONDED (FS 789)

AT HMV, FOUND FAILSAFE STRAP DISBONDED FWD SIDE FORMER FS STA 789 BETWEEN STR 28 AND 29. REPAIRED PER SRM 53-31-00.

Part: STRINGER — CORRODED (FS 328)

AT HMV, FOUND STRINGER 33 CORRODED AT FS 328. REMOVED STRINGER FROM S278 TO 328, FABRICATED NEW STRINGER AND SECTION INSTALLED PER SRM 53-13-00.

Part: SPLICE STRAP — CORRODED (FS 328)

AT HMV, FOUND SPLICE STRAP CORRODED AT FS 328. REMOVED STRAP AT FS 300 TO 328. FABRICATED NEW STRAP, INSTALLED PER SRM 53-31-00.

Part: TEAR STRAP — LIFTED (FS 1665-1685)

AT HMV, FOUND FAILSAFE STRAP LIFTED FROM SKIN C-1 B/B BETWEEN FS 1665 TO 1685, STR 43 AND 44. REPAIRED PER SRM 51-31-00.

Part: FLOORBEAM — CORRODED (FS 297)

AT HMV, FOUND FLOORBEAM CORRODED AT STA 298 LBL 28. INSTALLED NEW CAP PER SRM 53-21-00.

Part: ACT FITTING — CORRODED (RT MLG)

AT HMV, RT MLG ACTUATOR ATTACH FITTING UPPER FLANGE HOLES 1, 2, 3, 5, 6 ARE CORRODED. REAMED HOLES TO REMOVE CORROSION, SPOTFACED, ROTOPEEND AND INSTALLED BUSHINGS PER SRM 57-14-00.

Part: FLOOR BEAM — CORRODED (FS 298)

AT HMV, INSPECTION FOUND CORROSION ON FLOOR BEAM AT FS 298 LBL 28. RII. CORRECTION: INSTALLED NEW T CAP ON NR 811.

Part: DRAIN PAN — CRACKED (GALLEY DOOR AREA)

AT HMV, FOUND MESG DRAIN PAN CRACKED AND BROKEN ABOVE DOOR TO LOWER GALLEY. PERFORMED REPAIR PER SRM 51-50-05 PG 16 TO 18.

Part: FLOORBEAM — CORRODED (FS 1763)

AT HMV, FOUND FLOORBEAM CORRODED AT FS 1763 RBL 52. REMOVED BEAM, FABRICATED, DRILLED UP AND INSTALLED REPAIR PER SRM 53-21-00 PG 823.

Part: TEAR STRAP — DISBODED (FS 729-709)

AT HMV, INSPECTION FOUND THE FAIL STRAP BETWEEN FORMER FS 729 TO 709 AT STR 29 DISBONDED. REMOVED CORROSION PER SRM 51-21-01, WITHIN NEGLIGIBLE LIMITS PER SRM 53-31-00 FIG 801. TREATED AND PAINTED PER SRM 51-21-02, REPAIRED PER SRM 53-31-00 FIG 804.

Part: ANGLE — CRACKED (FS 1705)

AT HMV, INSPECTION FOUND AN ANGLE CRACKED 6 FT AFT OF THE NR 2 INLET FS 1705, 3 0'CLOCK POSITION, INSIDE OVAL ACCESS OPENING. REMOVED CRACKED ANGLE, FABRICATED T-ANGLE AND FILLER PER SRM 54-12-00 PG 805.

Part: FAILSAFE STRAP — DISBONDED (FS 933)

FAILSAFE STRAP DISBONDED BETWEEN STR 37-38 AT F.S. 933. FOUND AT HMV, REPAIRED PER SRM 53-31-00 FIG 816.

Part: ANTI-ICE BAFFLE — CRACKED (NR 2 ENGINE)

NR 2 ENG INLET ANTI-ICE BAFFLE IS CRACKED AT 7:00 O'CLOCK POS. REPAIRED PER SRM 54-34-00 FIG 804. FOUND AT HMV.

Part: STRINGER — CORROSION (FS 328)

AT HMV, INSPECTION FOUND STRINGER 33 CORRODED AT FS 328. REMOVED STR FROM STA 278 TO 328, FABRICATED NEW STRINGER SECTION AND SPLICE IAW SRM 53-13-00 PG 806 FIG 804.

Part: FLOORBEAM — CORRODED (FUSELAGE)

AT HMV, FOUND FLOORBEAM CORRODED AT 8.328, LBL 30. REMOVED BEAM FROM LBL 48 TO I/B END, FABRICATED DRILLED UP AND INSTALLED NEW BEAM, PER SRM 53-21-00 PG 823.

Part: FITTING — CORRODED (RT MLG)

AT HMV, FOUND FITTING CORRODED, AT I/B SIDE RMLG HOLE 17-20. REAMED HOLES TO .625 INCH, CORROSION REMOVED WITHIN LIMITS. HFEC OF FACE AND HOLES, REOPENED PER PS 900-4-5, CAD PLATED PER PS 900-3-9 NR 4. TURNED BUSHING TO SIZE AND TREATED, INSTALLED BUSHING AND REAMED TO SIZE. OXIDE BLASTED. PRIMED AND PAINTED. PER SRM 57-14-00.

Part: FITTING — CORRODED (RT MLG)

AT HMV, FOUND FITTING CORRODED, I/B RMLG ACT FITTING FLANGE. MACHINED TO .030 INCH FROM VERTICAL FACE IM\N LOWER AREA. LOCAL BLENDED SMALL AREA. PER SRM 57-14-00 PG 811. CORROSION REMOVED, HFEC OF FITTING, ROTO PEENED PER PS 900-4 NR 5. CAD PLATED PER PS 900-3-9 NR 4. OXIDE BLASTED, PRIMED, AND PAINTED. MFG AND TREATED SHIM. INSTALLED SHIM PER SRM 57-14-00.

Part: RIB — CRACKED (FS 1705)

AT HMV, FOUND RIB CRACKED STA 1705 ABOVE STR 39. FABRICATED NEW DOUBLER, DRILLED UP REPAIR, AND INSTALLED REPAIR PER SRM 53-12-00 FIG 608.

Part: TEAR STRAP — DISBONDED (FS 579)

AT HMV, FOUND C1 B/B TEAR STRAP DISBONDED, FS 579 BETWEEN STRINGERS 38-39. SAME COND FS 659 BETWEEN STRINGERS 42 AND 44. REPAIRED PER SRM 53-31-00 PG 830.

Part: TEAR STRAP — UNBONDED (FS 1433)

AT HMV, FOUND TEAR STRAP DISBONDED, C2 B/B FS 1413 BETWEEN STRINGER 30-31. REPAIRED PER SRM 53-31-00 PG 801.

Part: T-CAP — CORRODED (FS 1525)

AT HMV, FOUND CAP CORRODED, C2 FLOOR T-CAP STR 1525 RBL 10 LBL 25. DRILLED AND INSTALLLED NEW T-CAP PER SRM 53-20-00.

Part: SEAT TRACK — CORRODED (FS 1545-1665)

AT HMV, INSPECTION FOUND SEAT TRACKS CORRODED AT STA 1545-1665 LBL 75. REPAIRED PER SRM 53-21-00.

Part: FLOORBEAM — CORRODED (FS 297)

AT HMV, FOUND FLOORBEAM CORRODED AT FS 297 RBL 30 TO 36 FWD GALLEY. CLEANED CORROSION, DAMAGE OUT OF LIMITS, CUT AND DRILLED NEW CAP. FABRICATED PARTS PAINTED AND INSTALLED PER SRM 53-21-00.

Part: INLET — CRACKED (NR 2 ENGINE)

AT HMV, FOUND SKIN CRACKED, AT NR 2 ENG INLET, ANTI-ICE DUCT. TRIMMED OUT DAMAGE, FABRACATED AND DRILLED FILLERS, AND INSTALLED REPAIR PER SRM 54-34-00 FIG 804.

Part: FLOORBEAM — CORRODED (BS 1521)

AT HMV, FLOORBEAM CORRODED AT FS 1521 ABOVE STRINGER 33. REPAIRED PER SRM 53-23-00 FIG 802.

Part: RIB — CRACKED (FS 1685)

AT HMV, FOUND RIB CRACKED STA 1865 ABOVE STR 39. FABRICATED DOUBLER, DRILLED REPAIR, AND INSTALLED PER SRM 53-12-00 PG 806.

Part: TEAR STRAP — LOOSE (FS 1685)

DURING HMV, INSPECTION FOUND A TEAR STRAP LOOSE BETWEEN STA 1685 AND 1705 BETWEEN STR 39 AND 40. AREA CLEANED, SEALED AND RIVETED DOWN PER SRM 53-31-00 FIG 804.

Part: FLOOR BEAM — CORRODED (FS 297)

ON HMV, FLOOR BEAM CORRODED F/S 279 AT RBL 30-36. REPAIRED PER SRM 53-21-00.

Part: FITTING — CORRODED (RT MLG)

FITTING CORRODED, RT MLG CORRODED AT UPPER SIDE OF LOWER SUPPORT FOR RETRACT ACTUATOR, FOUND AT HMV. MACHINED .030 FROM FACE TO REMOVE CORROSION, WITHIN LIMITS OF SRM 57-14-00. HFEC OF SUPPORT FITTING FOUND NO CRACKS. ROTO-PEENED PER PS 900-4-5, CAD PLATED PER 900-3-9 NR 4, OXIDE BLASTED, PRIMED AND PAINTED.

Part: ANTI-ICE DUCT — CRACKED (NR 2 ENGINE)

NR 2 ENG INLET AT 5:30 O'CLOCK POSITION; ANTI-ICE DUCT SKIN CRACKED AROUND RIVET. ACCESS THRU PANEL 311GR-MARKED. REMOVED DAMAGED AREA. FABRICATED NEW REPAIR DOUBLERS PER SRM 54-34-00 FIG 804.

Part: FITTING — CORRODED (RT MLG)

AT HMV, FOUND HOLE CORRODED. NR 4 HOLE RMLG UPPER FLANGE FOR ACT ATTACHED FITTING. REAMED HOLE TO .718 INCH, CORROSION REMOVED. SPOT FACED .750 INCH DIA AND .025 INCH. CORROSION REMOVED. HFEC FOUND OK. ROTO PEENED PER PS 900-4 NR 5. CAD PLATED PER 900-3-9 NR 4, WITHIN SRM 57-14-00 LIMITS. TURNED BUSHINGS TO SIZE TREATED. INSTALLED BUSHING AND REAMED TO SIZE. OXIDE BLASTED, PRIME, AND PAINTED. MFG AND TREATED WASHER, INSTALLED WASHER.

Part: PRESSURE DECK — CRACKED (NLG WW)

AT HMV, FOUND 2 INCH CRACK IN NLG WHEEL WELL PRESSURE DECK AT CEILING TO SIDEWALL, WEB LT FS 409. DYE PENETRANT, INSP SHOWS VISIBLE CRACK. STOP DRILLED BOTH ENDS, FABRICATED NEW DOUBLER, INSTALLED DOUBLER PER SRM 53-11-00.

Part: FLOORBEAM — CORRODED (FS 328)

AT HMV, FOUND FLOORBEAM CORRODED AT FS 328 RBL 24 AT TIE DOWN. REMOVED BEAM FROM RBL 10 TO RBL 69. DRILLED UP NEW BEAM AND SPLICE ANGLES, INSTALLED NEW BEAM PER SRM 53-21-00 FIG 815.

Part: FLOORBEAM — MISDRILLED (BS 1605)

AT HMV, FLOORBEAM T-CAP WAS FOUND MISSDRILLED AND 2 HOLES PLUGGED IN SPLICE AT FS 1605 AT RBL 5. REMOVED DAMAGED CAP AND INSTALLED REPAIR PER SRM 53-23-00 PG 803.

Part: SEAT TRACK — CORRODED (FS 297-313)

AT HMV, INSPECTION FOUND CORROSION ON FLANGES OF SEAT TRACK BETWEEN FS 297 TO 313 RBL 30, FWD GALLEY. REPLACED SEAT TRACK PER SRM 53-21-00 PG 836-840.

Part: SKIN — CORRODED (FS 1645-1665)

AT HMV, FOUND SKIN CORROSION, STA 1645-1665, AND AROUND TEAR STRAPS. ACCOMPLISHED REPAIRS PER DL ERA 270891-14.

Part: SKIN — CRACKED (FUSELAGE)

AT HMV, INSPECTION FOUND THE FUSELAGE SKIN CRACKED 2 INCHES LONG AT THE AFT GROUND CONDITIONED AIR CUTOUT AT THE HINGE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-31-00 FIG 828.

Part: SEAT TRACK — CORRODED (FS 649-749)

ON HMV, SEAT TRACK CORRODED STA 649 TO 749, 2ND FROM LT SIDE. REPLACED SEAT TRACK PER SRM 53-23-00.

Part: SKIN — CRACKED (C-2 DOOR)

FOUND DURING HMV, BOTTOM LIP OF C-2 DOOR CRACKED IN CENTER. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER REF 52-11-00 FIG 804. INSTALLED REPAIR PER SRM 52-11-00 PG 804 FIG 804.

Part: ANGLE — WORN (RT MLG TRUNNION)

AT HMV, FOUND VERTICAL ANGLE WORN DOWN, AFT OF RM6 TRUNNION OUT BD EDGE OF TRIANGULAR PANEL. CUT OUT, DRILLED UP AND PAINTED NEW ANGLE, INSTALLED PER SRM 57-22-00.

Part: SKIN — CORRODED (FS 1645-1665)

AT HMV, FOUND SKIN CORRODED, STA 1645 TO 1665. REPAIRED PER SRM 53-31-00 FIG 804.

Part: SEAT TRACK — CORRODED (FS 1103-1203)

ON HMV, FOUND SEAT TRACK CORRODED STA 1103 - 203 RT OUTBOARD TRACK CORRODED AT SEVERAL LOCATIONS FULL LENGTH OF TRACK. INSTALLED NEW TRACK PER SRM 53-21-00.

Part: SKIN — CRACKED (FS 775)

TA HMV FOUND FUSELAGE SKIN CRACKED AND DENTED, AT FS 775 APPROX BETWEEN STRINGERS 20-21. CUTOUT AND DYE CHECKED AREA, ALL DAMAGE REMOVED. FABRICATED DAMPER AND INSTALLED PER SRM 53-31-00 FIG 811.

Part: FRAMES — CRACKED (FUSELAGE)

DURING SPECIAL INSPECTION, CRACKS WERE FOUND IN MAIN FUSELAGE FRAMES AT RT SIDE FS 649, 669, AND 689. ALL CRACKS WERE AT WL 280. THESE CRACKS WERE FOUND AS A RESULT OF A SPECIAL INSPECTION FOR AIRCRAFT WITH 22,000 CYCLES AND HIGHER. THIS IS THE FIRST TIME CRACKS WERE FOUND AT THESE LOCATIONS ON DL AIRCRAFT. REPAIRS WERE PERFORMED PER DL ERA 270665.