N721DA

Part: CONNECTOR — CORRODED (NR 3 ENGINE)

NR 3 ENG FIRE INDICATION IN FLIGHT, POM PROCEDURE COMPLIED WITH. BOTH BOTTLES FIRED, CIRCUIT WOULD NOT TEST. REPLACED UPPER GAS GENERATOR AND AFT GEARBOX LOOP CONNECTORS.

Part: PROJECTOR — INOPERATIVE (CABIN)

STRONG ODOR LIKE ELECTRICAL BURNING BETWEEN FIRST CLASS AND COACH NO SMOKE NOTICED PER CREW REPORTS APPROX 10 MIN. AFTER MOVIE STARTED B ZONE PROJECTOR INOP WITH ELECTRICAL ODOR NOTICED. ODOR WAS NOTICED IN B ZONE ONLY. OPENED AND INSPECTED ALL CEILING AREAS. FOUND ODOR TO BE ISOLATED TO B ZONE PROJECTOR. REPLACED SAME.

Part: SKIN — CORRODED (BS 1693)

FUSELAGE SKIN FS 1693 STRG 38 : REPAIR FOR CORROSION CUTOUT. THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 1693 AND STRG 38. THE DAMAGED SKIN WAS CUTOUT OVER A 3.1 BY 6.8 AREA TO REMOVE THE CORROSION. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 365024-14, REV A.

Part: SPAR WEB — CRACKED (WS 77)

WING LT, REAR SPAR WEB, OWS 77 LOWER CAP ATTACHMENT, REPAIR FOR WEB CRACK. THE LT WING REAR SPAR WEB WAS FOUND WITH A .50 LONG CRACK EMANATING FROM A FASTENER HOLE ATTACHING THE WEB TO THE LOWER SPAR CAP AT OWS 77. THE WEB CRACK WAS ROUTED OUT AND AN ALUMINUM DOUBLER AND TRIPLER INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 364580-14, REV A.

Part: SKIN — CRACKED (WS 477)

FOUR FASTENER HOLES IN THE LOWER WING SKIN AT IWS 477 AND STRINGER 17 WERE FOUND CRACKED ON BOTH WINGS. THE CRACKS ARE THE SUBJECT OF SID AD 95-20-04, R1 (SID NR 57-3-2). THE CRACKED HOLES WERE OVERSIZED TO REMOVE THE CRACKS AND ALUMINUM BUSHINGS WERE INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 364606-14AD, REV B.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT SIGN AT 3-R DOOR STOP ILLUMINATION AFTER TWO MINUTES. REPLACED BATTERY PACK, CHECKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS DO NOT ILLUMINATE 16A/B AND 22H/J/ RT GALLEY LIFT AND LOWER GALLEY. REPLACED BATTERY PACK CHECKS OK.

Part: CONNECTOR — DIRTY (NR 2 ENGINE)

NR 2 ENG FIRE LOOP -A- FLICKERED SWITCHED TO -B- LOOP, 3 MIN LATER -B- LOOP CAME ON STEADY SHUT ENG DOWN, FIRED ONE BOTTLE-B- LOOP ON AT GATE. REPLACED FIRE DETECTION UNIT-B-LOOP CKS NORMAL. CLEANED ALL CONNECTIONS ON FIRE LOOPS, -A- LOOP CKS NORMAL. RAN ENG AT T/O POWER FOR 10 MINS ALL INDICATIONS NORMAL ENG OPERATION NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND ON L/O AFT EMERGENCY TRACK LIGHTS INOP. REPLACED AFT BATTERY PACK OP CKS NORMAL.

Part: SKIN — CORROSION (BS 464-488)

THE FUSELAGE LT SIDE LOWER BELLY SKIN WAS FOUND CORRODED JUST OUTBOARD OF THE LOWER CENTERLINE AT STRINGER 33 AFT OF FS 464. REMOVAL OF ALL CORROSION RESULTS IN A CUTOUT OF THE SKIN AND INTERNAL BONDED DOUBLER SIZED 7.25 WIDE BY 24.25 LONG, EXTENDING FROM FS 464 TO FS 488 FROM THE EDGE OF THE SKIN AT THE CENTERLINE OUTBOARD TO JUST BELOW STRINGER 34.

Part: BULKHEAD CAP — CRACKED (BS 449)

FS 449 BULKHEAD FOUND CRACKED IN HORIZONTAL FLANGE OF THE CAP. THE LOCATION IS FBL 19 AND EXTENDS FROM THE FORWARD EDGE, THROUGH AN EXISTING SEAL RETAINER HOLE, AND TOWARD THE CAP RADIUS. THE REPAIR WILL BE ACCOMPLISHED BY SB 093-53-233,2.A PAGES 7-9.

Part: POWER PACK — INOPERATIVE (CABIN)

DURING L/O CK, FOUND EMERGENCY LIGHTS INOP AT L-1 CABIN DOOR. REPLACED POWER PACK AT L-1 DOOR, OPS CKS OK.

Part: FRAME — CRACKED (BS 629/1605/1645)

DURING LETTER CHECK, CRACKS WERE FOUND AT WL 280.6. THE CRACKS WERE REPAIRED PER SI 7-69003-12AD.

Part: SKIN — CRACKED (RIGHT WING)

DURING LETTER CHECK, THE LOWER WING SKIN ON THE RT WING AT STR 18 RUNOUT WAS FOUND CRACKED. CRACK WAS REPAIRED PER DAL EO 7-70043-3.

Part: FLT CONTROLS — LACK OF LUBE (LT AILERON)

AIRCRAFT HARD TO ROLL RIGHT, BUT ROLLS NORMAL BACK TO THE LEFT. TURNING OFF B-AILERON SERVO INBD, CAUSED UNCOMMANDED HARD LEFT ROLL. INSPECTION OF FLT CONTROL SYSTEM FOUND EXTREME BINDING IN LINKAGE BETWEEN LEFT INBD AILERON AND WHEEL WELL. LUBED LINKAGE BEARINGS UNTIL FREE, OPERATION NORMAL.

Part: LIGHT — MISSING (CABIN)

EMERGENCY LIGHT MISSING AT SEAT 1CD. RELAMPED AND REPLACED, CHECKS GOOD.

Part: HYD LINE — LEAKING (C-HYD SYSTEM)

C-SYSTEM HYD QUANTITY DECREASED TO BELOW HALF FULL. TURNED OFF C-SYS PUMPS. FOUND LINE ABOVE C-SYSTEM RETURN FILTER LEAKING. REPLACED LINE, OPERATION NORMAL.

Part: ROLLER/BRACKET — MISSING (NR 3 TE FLAP)

ON TAKEOFF, FLAPS DID NOT COME UP BEYOND 8 DEGREES, RETURNED ATL. FOUND NR 3 RT FLAP IB ACTUATING ROLLER AND BRACKET MISSING. REPLACED ROLLER AND BRACKET INSTALLED PER ERA 272472-14. RIGGED VANE ROLLER REF MM 27-51-00.

Part: DUCT — RUPTURED (NR 3 ACM)

AT FL 370 HEARD LOUD BANG, POSSIBLY PNEU IN NATURE. CABIN PRESSURE NORMAL, ENGINE BLD CONT PANEL PSIG NORMAL. SUBSEQUENTLY C/D ZONES TURNED ICE COLD, WAS ABLE TO SUPPLY MAX HOT TEMP IN DUCT SUPPLY, BUT ZONE NEVER WARMED UP. SUSPECT POSSIBLE DUCT FAILURE. FOUND RT O/B DUCT RUPTURED ON NR 3 ACM. REPLACED SAME, OPERATION NORMAL.

Part: STRINGER SPLICE — CRACKED (FUSELAGE)

DURING ACCOMPLISHMENT OF AN INSPECTION OF THE AFT P-DOME STR SPLICE FITTING PER SI 7-66332-12 AND VA 30620, STRINGER 10 FITTING WAS FOUND TO BE CRACKED. THE SUBJECT FITTING WILL BE RELEASED ON A TIME LIMITED BASIS AND REPAIRED BY REPLACING WITH A SERVICEABLE PART, WITHIN 150 FLIGHT CYCLES OF ISSUANCE.

Part: STRINGER SPLICE — CRACKED (FUSELAGE)

THE AFT PRESSURE BULKHEAD STRINGER SPLICE FITTING PER SI 7- 66332-12 AT STR 58 FITTING, WAS FOUND TO BE CRACKED. THE FITTING WILL BE RELEASED ON A TIME LIMITED BASIS AND REPLACED WITHIN 150 FLIGHT CYCLES FROM DATE OF ISSUANCE.

Part: SKIN — CORROSION (BS 529-983)

THE FORWARD LOWER BELLY SKIN WAS FOUND WITH EXTENSIVE CORROSION BETWEEN FS 529 AND FS 983, STR 29 TO STR 42. ALSO, THERE ARE NUMEROUS EXISTING EXTERNAL REPAIRS ON THE SKIN IN THIS AREA. DUE TO THE EXTENSIVE NATURE OF THE CORROSION AND EXISTING REPAIRS, REPLACEMENT OF LARGE AREA OF THE FORWARD BELLY SKIN WILL BE REQUIRED. ACCOMPLISHED REPAIRS PER DL ERA 271106-14.

Part: FAIL-SAFE STRAP — DISBONDED (FS 1555/1575)

FAIL-SAFE STRAP DISBONDED AT FS 1555 STR 36 TO 37 AND AT FS 1575 BTWEEN STR 40 TO 41, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 830.

Part: FAIL-SAFE STRAP — DISBONDED (FS 1565-1615)

FAIL-SAFE STRAPS DISBONDED AT FS 1565 TO 1585 STG 30 TO 29. FAIL-SAFE STRAPS DISBONDED AT FS 1615 STR 30 TO 29. FAIL-SAFE STRAPS DISBONDED AT FS 1575 STR 36 TO 37. FOUND DURING HMV CORROSION INSP. REPAIRED PER SRM 53-31-00 PG 830 AND SKIN REPLACEMENT.

Part: FLOORBEAM — CORRODED (FS 1480)

FLOOR SUPPORT CAP CORRODED C2 BB FS 1480 RBL 4. REPAIRED PER SRM 53-23-00 PG 803 TO 804, FOUND AT HMV.

Part: SKIN — CORROSION (FS 1453-1655)

FUSELAGE SKIN BETWEEN FS 1453 AND FS 1655 BETWEEN STR 24 AND STR 37 REQUIRES REPLACEMENT, DUE TO EXTENSIVE CORROSION AND NUMEROUS REPAIRS. ACCOMPLISHED REPAIRS PER DL ERA 271107-14.

Part: STRINGER — CORRODED (FS 1475-1605)

STRINGER 29 CORRODED FS 1475, FS 1523 TO 1545, FS 1585, FS 1565 TO 1585, FS 1585 TO 1605. FOUND AT HMV, CORROSION SAMPLE INSP. REPLACED STRINGER PER SRM 53-13-00 PG 804.

Part: SILL — CORROSION (C-2 DOOR)

C-2 DOOR SURROUND STRUCTURE LOWER SILL OUTER CAP WAS FOUND CORRODED ON THE OUTBOARD HORIZONTAL FLANGE OF THE CAP AT STATION 1625. ACCOMPLISHED REPAIRS PER DL ERA 271113-14.

Part: SPAR CAP — CRACKED (FS 1163)

THE CENTER WING FS 1163 INTERMEDIATE SPAR UPPER CAP HAS A CRACK IN THE FWD LEFT AND RIGHT OUTBOARD ENDS. ACCOMPLISHED REPAIRS PER DL ERA 271114-14.

Part: FLOORBEAM — CORRODED (FS 1523)

FLOORBEAM AT STA 1523 CORRODED 0 BL TO 30 LBL. FOUND DURING HMV CORROSION INSP. REPAIRED PER SRM 53-23-00 FIG 802.

Part: STRINGER — CORRODED (FS 1770)

STRINGER 39 CRACKED AND CORRODED AT FS 1770, FOUND AT HMV. SPLICED IN SECTION OF NEW STRINGER PER SRM 53-13-00 PG 806.

Part: TRIPLER — CRACKED (R1 DOOR OPENING)

A CRACK WAS FOUND IN THE AFT EDGE OF THE R-1 DOOR SURROUND TRIPLER BELOW WL 220. ACCOMPLISHED REPAIRS PER DL ERA 271153-14.

Part: L/E SKIN — CRACKED (RT ELEV)

DURING SHOP INSPECTION, A GOUGE AND CRACK WAS FOUND IN A LEADING EDGE PANEL OF THE RT ELEVATOR. REPAIRED PER SRM 55-22-00 FIG 802.

Part: FRAME — DOUBLE DRILLED (FS 629/649)

AT HMV, FUSELAGE FRAME FS 629 AT STR 32 AND FS 649 AT STR 32 FOUND WITH DOUBLE DRILLED HOLE. ACCOMPLISHED REPAIR PER SRM 53-31-00.

Part: DOUBLER — CRACKED (RT ELEVATOR)

DURING SHOP INSPECTION, A DOUBLER WAS FOUND TO BE CRACKED AT THE AFT EDGE OF THE ELEVATOR TIP. A REPAIR WAS INSTALLED PER SRM 55-22-00 FIG 802.

Part: RIBS — CRACKED (RT ELEVATOR)

DURING HMV, SHOP INSPECTION, RT ELEVATOR WAS FOUND WITH CRACKING IN VERTICAL AND DIAGONAL TRUSS MEMBERS OF ELEVATOR RIBS. REPAIRS WERE ACCOMPLISHED PER L011 SB 093-55-018.

Part: FRAME — DOUBLE DRILLED (FS 569/589)

AT HMV, FUSELAGE FRAME FS 569 AT STR 36 AND FS 589 AT FS 33 FOUND WITH DOUBLE DRILLED HOLE. REPAIRED PER SRM 53-31-00 FIG 818.

Part: STRINGER — CRACKED (FS 1750)

AT HMV, STR 39 FS 1750 CRACKED. REPAIRED PER SRM 53-13-00 FIG 804.

Part: STRINGER — MISDRILLED (FS 690)

AT HMV, STRINGER FOUND MISSDRILLED, STR 40 FS 690. ROUTED OUT DAMAGE, WITHIN LIMITS PER SRM 53-13-00 PG 801, TREATED AND PAINTED.

Part: TEAR STRAP — DISBONDED (FS 1750)

AT HMV, TEAR STRAP DISBONDED FS 1750 BETWEEN STR 35 TO 36. PEELED BACK TEAR STRAP AND FOUND NO CORROSION. REPAIRED PER SRM 53-31-00 FIG 816 NOTE 6.

Part: REAR SPAR — OVERSIZED HOLES (WS 346)

DURING ACCOMPLISHMENT OF PART 5 OF EO 7-56199-3AD, HOLES WERE OVERSIZED IN SEVERAL LOCATIONS, DUE TO REMOVAL OF EXISTING LOOSE FORCE MATE BUSHINGS. WING REAR SPAR IWS 346 MLG ATTACH FITTING INBD, OUTBD, UPPER AND LOWER 1.125 INCH HOLES. REPAIRED PER DL ERA 271059-14.

Part: FLOOR BEAM — CORRODED (FS 1545)

AT HMV, CORRODED FLOOR BEAM UNDER T-CAP 2 LT OF B/L 0.0 C-2 B/B STA 1545. REPAIRED PER SRM 53-23-00, FIG 802.

Part: TEAR STRAP — CORRODED (FS 897)

AT HMV, FUSELAGE SKIN TEAR STRAP WITH CORROSION AND DISBONDED AT FS 897 BETWEEN STRINGES 40, 41 AND 42. REPAIRED PER SRM 53-31-00 PG 830.

Part: FITTING — CRACKED (NR 3 FLAP VANE)

DURING ACCOMPLISHMENT OF THE FLAP VANE FITTING REWORK PER DELA S.I. 7-65988-12AD, THE NR 3 FLAP VANE INBOARD FITTING LUG WAS FOUND CRACKED. IN ACCORDANCE WITH ALTERNATE MEANS OF COMPLIANCE LETTER ATL ACO DTD. 7/11/95, A REPLACEMENT FITTING WAS FABRICATED AND INSTALLED.

Part: STRINGER — CORRODED (FS 1605-1625)

STR 34 CORRODED FS 1605 TO 1625. FOUND AT HMV, REPAIRED PER SRM 53-13-00 PG 806.

Part: STRINGER — CORRODED (FS 1585-1625)

STR 33 CORRODED FROM FS 1585 TO 1625. FOUND AT HMV, REPAIRED BY REPLACING STRINGER PER SRM 53-13-00 PG 806.

Part: DOUBLER — DAMAGED (FS 1363)

INTERNAL DOUBLER HAS 2 INCH CUT BETWEEN STRINGER 41 AND 42 FS 1363, FOUND DURING HMV. REPAIRED PER SRM 53-31-00 FIG 836.

Part: CLIP — CORRODED (FS 1625-1645)

CLIP AND DOUBLERS CORRODED BETWEEN STRINGER 33 AND 34 UNDER FWD FRAME AND ALONG STRINGER 33. FOUND AT HMV, REPAIRED PER SRM 53-12-00 FIG 817.

Part: STRINGER — CORRODED (FS 1530-1645)

STRINGER 27 CORRODED FS 1530, 1545 TO 1585, 1523 TO 1545, 1585 TO 1605 AND 1625 TO 1645. FOUND AT HMV, REPLACED STRINGER PER SRM 53-13-00 FIG 804.

Part: FLOORBEAM — CORRODED (FS 943)

FLOORBEAM CORRODED FS 943 LBL 50 TOP OF BEAM, FOUND AT HMV. REPAIRED PER SRM 53-21-00 FIG 823.

Part: STRINGER — CORRODED (FS 559-599)

STRINGER 32 CORRODED FROM FS 559 TO FS 599, FOUND AT HMV. REPAIRED PER SRM 53-13-00.

Part: TEAR STRAP — DISBONDED (FS 1695)

TEAR STRAP DISBONDED FS 1695 BETWEEN STRINGER 29 AND 30, FOUND AT HMV. REPAIRED PER SRM 53-31-00 FIG 804.

Part: FITTING — CORRODED (L1 DOOR)

L1 DOOR FRAME STOP FITTING CORRODED FWD SIDE 2ND AND 3RD FROM BOTTOM. FOUND AT HMV, REPLACED FITTINGS PER SRM 53-15-00 FIG 805.

Part: STRINGER — CORRODED (FS 1625)

STRINGER 32 CORRODED FS 1625. FOUND AT HMV, REPAIRED PER SRM 53-13-00 PG 806.

Part: TEAR STRAP — DISBONDED (FS 759)

TEAR STRAP DISBONDED FS 759 STRINGER 26 TO 27. FOUND AT HMV, REPAIRED PER SRM 53-31-00 FIG 804.

Part: STRINGER — CORRODED (FS 1565-1585)

STRINGER 34 CORRODED FS 1565 TO 1585. FOUND AT HMV, REPLACED STRINGER PER SRM 53-13-00 PG 806.

Part: STRINGER — CRACKED (FS 789)

STRINGER 34 HAS CRACK JUST BELOW FORMER STA. 789. FOUND HMV. REPAIRED PER SRM 53-13-00. SPLICED IN NEW STRINGER SECTION.

Part: STRINGER SPLICE — IMPROPER (FS 826-869)

STR 33 HAS IMPROPER SPLICES AT STA 826 TO 869. FOUND IN HMV. REPLACED SPLICES PER SRM 53-13-00, FIG 804.

Part: TEAR STRAP — DISBONDED (FS 739)

LOWER GALLEY TEAR STRAPS DISBONDED AT FS 739 FROM STR 23 TO 24 AND 25 TO 27, FOUND AT HMV. CUT STRAP AND CLEANED CORROSION, AREA FOUND TO BE WITHIN LIMITS PER SRM 53-31-00 PG 801. DRILLED NEW SPLICE PER SRM, TREATED AND PAINTED, INSTALLED NEW SPLICE REPAIR PER SRM 53-31-00 PG 804.

Part: STRINGER — CORRODED (FS 1625-1645)

AT HMV, STR 35 CORRODED BETWEEN FS 1625 TO 1645. REPAIRED BY REPLACING SECTION OF STRINGER PER SRM 53-13-00 FIG 806.

Part: SWING LINK — LOOSE (NR 1 LE FLAP)

RT WING NR 1 FLAP I/B SWING LINK ATTACH POINT LOOSE. DISASSEMBLED AND FOUND FLAP FITTING BUSHING OUT OF LIMITS, BORED FITTING TO 1.319, MANUFACTURED BUSHING PER SRM 57-54-00.

Part: HINGE ARMS — WORN (E/E DOOR)

AT HMV, E/E DOOR LEFT AND RIGHT AFT HINGE ARMS WORN ON TOP EDGE NEAR CENTER OF ARM. REPAIRED PER SRM 52-11-00 FIG 801.

Part: TEAR STRAP — DISBONDED (FS 569-589)

TEAR STRAP BETWEEN FS 569 TO 589 BETWEEN STRINGERS 24 AND 25 DISBONDED. REPAIRED PER SRM 53-31-00 FIG 816, FOUND AT HMV.

Part: WEB — GOUGED (NR 5 TORQUE BOX)

NR 5 TORQUE BOX, FWD EDGE OF WEB PANEL GOUGED INSIDE AFT END BELOW AND AFT OF LINKAGE. FOUND DURING HMV. REPAIRED PER SRM 51-50-04, FIG 2 SHT 2. INSTALLED DOUBLER. REF NR 539.

Part: FRAME — CUT (FS 1763)

STA 1763 FRAME CAP IN C-3 CUT AT APPROX LBL 9 1/2 AND RBL 16 FOR MTC. FOUND IN HMV. REPAIRED PER SRM 53-12-00, FIG 817.

Part: SKIN — CORROSION (E/E DOOR)

E AND E DOOR, CORROSION FOUND ON FORWARD SKIN EDGE. REPAIRED PER SRM 52-11-00 FIG 802, FOUND AT HMV.

Part: TEAR STRAP — CORROSION (FS 1370)

AT HMV, TEAR STRAP DISBONDED ABOVE STR 40 AT FS 1370. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS AS PER SRM 53-31-00 FIG 801. REPAIRED PER SRM 53-31-00 FIG 804, TREATED/PAINTED PER MM 51-09-00.

Part: SKIN — CORROSION (FS 1490)

AT HMV, BONDED SKIN AT FS 1490, OUTBOARD OF STR 39 IS CORRODED. CUT OUT DAMAGE AND REPAIRED PER SRM 53-31-00 FIG 836 PG 965.

Part: SKIN STRAPS — UNBONDED (CARGO COMPT)

AT HMV, C-3 CARGO FUSELAGE SKIN, FAILSAFE STRAPS UNBONDED STA 1770 BETWEEN STR 30 AND 31 AND 37 AND 38. REPAIRED PER SRM 53-31-00, PG 830.

Part: SKIN — CORRODED (FS 1473)

AT HMV, SKIN CORRODED AND TEAR STRAP DISBONDED AT STA 1473, BETWEEN STR 26 TO 27. REPAIRED AREA PER SRM 53-31-00 FIG 836.

Part: TEAR STRAP — DISBONDED (FS 1675)

TEAR STRAP DISBONDED FS 1675 BETWEEN STRS 36 AND 37. FOUND AT HMV, REPAIRED PER SRM 53-31-00 PG 830.

Part: STRINGER — CRACKED (FS 975)

AT HMV, MESC STRINGER CRACKED AT ATR 33, FS 975. CORR: DRILLED UP NEW STRINGER AND SPLICE PER SRM 53-13-00. INSTALLED NEW STRINGER/SPLICE PER SRM 53-13-00 FIG 804.

Part: CLIP — CORRODED (FS 1645)

AT HMV, FS 1645 SKIN CLIP CORRODED BETWEEN STR 33 TO STR 35. CORR: REMOVED CLIP DETWEEN STR 33, 35. CUT NEW PIECE AND DRILLED UP. INSTALLED REPAIR PARTS PER SRM 53-12-00 PG 817.

Part: FRAME — CORRODED (FS 235)

AT HMV, FUSELAGE FRAME AT FS 235, WAS FOUND CORRODED 14 LEFT AND RIGHT AT FESC ACCESS OPENING. CLEANED CORROSION, OUT OF LIMITS PER SRM 53-12-00. INSTALLED REPAIR PER SRM 53-12-00.

Part: TEAR STRAP — DISBONDED (FS 1695)

TEAR STRAP DISBONDED FS 1695 BETWEEN STRS 35 AND 36. FOUND AT HMV, REPAIRED PER SRM 53-31-00 FIG 801.

Part: SKIN CLIPS — CORRODED (FS 1463)

AT HMV, FS 1463 SKIN CLIPS BETWEEN STR 33 AND 36 ARE CORRODED. REPAIRED PER SRM 53-12-00, FIG. 817.

Part: CLIPS — CORRODED (FS 1605)

AT HMV, SKIN CLIP CORRODED FS 1605 FROM STR 29 TO 34. FABRICATED SKIN CLIPS PER SRM 53-12-00 FIG 817, TREATED AND PAINTED. INSTALLED REPAIR PER SRM.

Part: TEAR STRAP — DISBONDED (FS 933)

AT HMV, FOUND FUSELAGE SKIN FAILSAFE TEAR STRAP DISBONDED AT FS 933 BETWEEN STRINGERS 43-44. REPAIRED PER SRM 53-31-00.

Part: TEAR STRAP — DISBONDED (FS 897)

AT HMV, TEAR STRAP DISBONDED FS 897 STR 43 TO 42, STRAP HAS CORROSION UNDERNEATH. REPAIRED PER SRM 53-31-00 PG 807 FIG 804.

Part: TEARSTRAP — DISBONDED (FS 779)

AT HMV, TEAR STRAP DISBONDED FS 779 STR 40-41. STRAP HAS CORROSION UNDERNEATH. REPAIRED PER SRM 53-31-00, FIG 804.

Part: TEAR STRAP — DISBONDED (FS 933)

AT HMV, FOUND FUSELAGE SKIN FAIL SAFE TEAR STRAP DISBONDED AT FS 933 BETWEEN STRINGERS 40-41. REPAIRED PER SRM 53-31-00.

Part: TEAR STRAP — DISBONDED (FS 933)

AT HMV, FOUND FUSELAGE SKIN FAIL SAFE TEAR STRAP DISBONDED AT FS 933 BETWEEN STRINGERS 44-45. REPAIRED PER SRM 53-31-00.

Part: SKIN — OUT OF LIMITS (FS 869-983)

AT HMV, FOUND LOWER FUSELAGE SKIN PANEL AT FS 869 TO FS 983 BETWEEN STR 32 TO 35 OUT OF LIMITS DUE TO CORROSION. REPLACED SKIN PANEL PER SRM 53-31-00 FIG 826, AND DL ERA 271106-14.

Part: TEAR STRAP — DISBONDED (FS 599)

AT HMV, TEAR STRAP DISBONDED, C-1 B/B RT SIDE, STA 599 BETWEEN STR 20 AND STR 24. REPAIRED PER SRM 53-10-00.

Part: TEAR STRAP — DISBONDED (FS 933)

AT HMV, FOUND FUSELAGE SKIN FAIL SAFE STRAP DISBONDED AT FS 933 BETWEEN STRINGERS 40 AND 41. REPAIRED PER SRM 53-31-00.

Part: FITTING — CORRODED (LT MLG)

HOLE BORE CORRODED LT MLG FITTING HOLE NR 11 FOR RETRACT ACTUATOR FITTING (FWD/LWR HOLE LOOKING OUTBD) HAS CORROSION IN BORE. DAMAGE WAS FOUND AT HMV. OPENED HOLE NR 11 TO .562 TO REMOVE CORROSION. REMOVAL OK, HEFC OK. OXIDE BLASTED AREA, ROTO-PEENED AREA, CAD PLATED AREA PER PS 900-3-9 NR 4 PRIMED AND PAINTED, SRM REF 57-14-00.

Part: SKIN — CORRODED (FS 509-529)

AT HMV, CORROSION ON C-1 B/B FUSELAGE SKIN AND SPLICE BETWEEN STR 32 AND 33 FS 509 AND 529. REMOVED CORROSION AND DRILLED UP NEW EDGE DOUBLER PER SRM 53-31-00 FIG 801. TREATED AND PAINTED PER PS 400-2-4-1 NR 2. INSTALLED FASTENERS PER SRM 53-31-00.

Part: SPAR CAP — CRACKED (FS 1163)

THE T-CAP FS 1163, CTR TANK INTERMEDIATE SPAR UPPER CAP IS CRACKED IN RADIOUS AT RT OUTBD END. ACCOMPLISHED REPAIRS PER DL ERA 271114-14.

Part: TEAR STRAP — DISBONDED (FS 519)

AT HMV, TEAR STRAP DISBONDED FWD B/B 39 AND 40 STA 519. REPAIRED TEAR STRAP AT FS 519 BETWEEN STR 39 AND 40 PER SRM 53-31-00 PG 830.

Part: SKIN — CRACKED (FUSELAGE)

FUSELAGE SKIN HAS .3750 INCH CRACK AT RT AFT PNEUMATIC GROUND CONNECTOR FLANGE CRACK LOC. AT FWD HINGE CORNER CUT-OUT. FOUND AT HMV, REPAIRED PER SRM 53-31-00, PG 923-922.

Part: FITTING — CORRODED (RT MLG)

DEEP CORROSION ON AREA EXPOSED BY RT MLG FITTING. FOUND IN HMV. REPAIRED PER SRM 57-14-00, PG 811.

Part: THRESHOLD — CORRODED (L2 DOOR)

THRESHOLD CORRODED L-2 DOOR, TOP SURFACE AT AFT END. FOUND IN HMV. REPAIRED PER SRM 51-1-05 AND LAC DRAWING 1506385 AND DRAWING 1506415.

Part: WEB — CRACKED (NR 2 ENG INLET)

AT HMV, WEB CRACKED 1.5 INCH LONG JUST AFT OF NR 2 ENG INLET RING INTERIOR TO PNL 311NL. REPAIRED PER SRM 54-34-00 FIG 804.

Part: INTERCOSTAL — CRACKED (NR 2 ENG INLET)

AT HMV, WEB CRACKED 2 INCHES LONG JUST AFT NR 2 ENG INLET RING INTERCOSTAL PNL 311DR, 4 O'CLOCK. REPAIARED PER SRM 54-34-00 FIG 804.

Part: INTERCOSTAL — CRACKED (NR 2 ENG)

AT HMV, WEB CRACKED 2 INCHES LONG JUST AFT OF NR 2 ENG INLET RING INTERCOSTAL PNL 311AR, 11 O'CLOCK. REPAIRED PER SRM 54-34-00 FIG 804.

Part: THRESHOLD — CORRODED (R 4 DOOR)

THRESHOLD CORRODED - R-1 DOOR UPPER SURFACE, FWD END, FOUND DURING HMV. REPAIRED PER SRM 53-15-00 PG 816-820.

Part: WEB — CRACKED (NR 2 ENG INLET)

AT HMV, WEB CRACKED 1 INCH LONG JUST AFT NR 2 ENG INLET RING INTERIOR TO PNL 311RL. REPAIRED PER SRM 54-34-00 FIG 804.

Part: WEB — CRACKED (NR 2 ENG INLET)

AT HMV, WEB CRACKED 3 EACH THE RIVET BUCKTAIL, EACH APPROX 1 INCH LONG JUST AFT NR 2 ENG INLET RING INTERIOR TO PNL 311DR, 3 O'CLOCK. REPAIRED PER SRM 54-34-00 FIG 804.

Part: FAIL-SAFE STRAP — DISBONDED (FS 1565)

AT HMV, FUSELAGE FAIL-SAFE STRAP DISBONDED AT STR 40 FS 1565. REPAIRED PER SRM 53-31-00.

Part: TEAR STRAP — DISBONDED (FS 1635)

AT HMV, TEAR STRAP DISBONDED FS 1635 BETWEEN STR 39 AND 40. REMOVED CORROSION AND FOUND WITHIN LIMITS PER SRM 53-31-00 FIG 801, TREATED AND PAINTED. INSTALLED TEAR STRAP REPAIR PER SRM 53-31-00 FIG 830.

Part: FLOORBEAM — CORRODED (FS 1501)

AT HMV, FLOORBEAM CORRODED FS 1501 ABOVE STR 39 BELOW CARGO TIE DOWN SUPPORT. REPAIRED PER SRM 53-23-00 FIG 802.

Part: FITTING — CORRODED (LT MLG)

FASTENER HOLES IN LT WING FOR RETRACT ACTUATOR ATTACH HOLES NR 1, 2, 3, 4, 5, AND 6 ARE CORRODED, FOUND AT HMV. REAMED HOLES TO .718 TO REMOVE CORROSION PER SRM 57-14-00. REMOVAL OK, HEFC OK. OXIDE BLASTED AREA, ROTO-PEENED AREA, CAD PLATED AREA PER PS 900-3-9 NR 4 PRIMED AND PAINTED.

Part: TEAR STRAP — DISBONDED (FS 1770)

TEAR STRAP DISBONDED FS 170 BETWEEN STR 38 AND 39. REMOVED STRAP, DRILLED STRAP AND SPLICE PER SRM 53-31-00 PG 830. INSTALLED STRAP PER SRM 53-31-00 PG 830, FOUND AT HMV.

Part: TEAR STRAP — DISBONDED (FS 1677)

AT HMV, TEAR STRAP DISBONDED FS 1677 BETWEEN STR 29 TO 31 UNDER FRAME. REPLACED STRAP PER SRM 53-31-00 PG 830.

Part: SKIN CLIP — CORRODED (FS 1523)

AT HMV - SKIN CLIP CORRODED FS 1523 AFT SIDE IN BETWEEN STR 28-27 C-2 B/B. REPAIRED PER SRM 53-12-00, FIG 804.

Part: FITTING — CORRODED (LT MLG)

AT HMV, FOUND FOLLOWING HOLES ON LT MLG RETRACT ACTUATOR FITTING. BUSHINGS ARE NOT SEATED AND HOLES CORRODED 1, 2, 3, 4, 5, 6. REPAIRED PER SRM 57-14-00 FIG 808 JPC 17.

Part: FITTING — CORRODED (LT MLG)

FASTENER HOLES CORRODED IN LT MLG RETRACT ACTUATOR FITTING. HOLES NR 7, 8, 9, 11, 12, 13, 16, FOUND IN HMV. REPAIRED PER SRM 57-14-00, FIG 808.

Part: ANGLE — CORRODED (FS 1565)

AT HMV, ANGLE CORRODED IN BETWEEN STR 28-29, FS 1565 C-2 B/B. REPAIRED PER SRM 53-12-00, FIG 804.

Part: SKIN CLIP — CORRODED (FS 1565)

AT HMV - SKIN CLIP CORRODED IN BETWEEN STR 33-34 FS 1565 AFT C-2 B/B. REPAIRED PER SRM 53-12-00, FIG 817.

Part: SKIN CLIP — CORRODED (FS 1565)

AT HMV - SKIN CLIP CORRODED IN BETWEEN STR 33-32 FS 1565 AFT SIDE C-2. REPAIRED PER SRM 53-12-00 FIG 817.

Part: FITTING — CORRODED (LT MLG)

AT HMV - LT MLG FITTING FLANGE FOR RETRACT ACTUATOR LOWER SURFACE IS CORRODED. REPAIRED PER SRM 57-14-00, FIG 804.

Part: FAILSAFE STRAP — UNBONDED (FS 1755)

FAILSAFE STRAP UNBONDED C3 B/B STA 1755 BETWEEN STR 35 AND 36 AND 38 TO 40, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 830.

Part: FITTING — CORRODED (LT MLG)

AT HMV, LT MLG FITTING CORRODED ON UPPER WING LOWER SURFACE. CORR: REPAIRED PER SRM 57-14-00, FIG 804.

Part: SUPPORT — CORRODED (FS 1545)

FLOOR SUPPORT LOWER SECTION CORRODED ABOVE STR 33 FS 1545 C-2 B/B AT HMV. REPAIRED PER SRM 53-23-00, FIG 802.

Part: BULKHEAD — CRACKED (FS 1363)

REF EO 07-69959-12 OPN 0205 HFEC INSP LT FS 1363 BULKHEAD. CRACK INDICATION BETWEEN NR 4 AND 5 BULKHEAD WEB STIFFENERS INBD IND, FOUND AT HMV. REPLACED BULKHEAD PER ERA 271056-14 REV B.

Part: TEAR STRAP — DISBONDED (FS 579)

TEAR STRAP - DISBONDED IN C-1 BB AT FS 579 FROM STA 34 TO STA 37, FOUND AT HMV. REPAIRED PER SRM 53-31-00.

Part: FITTING — CORRODED (LT MLG)

LEFT MLG FITTING I/B SURFACE CORRODED. FOUND AT HMV, REPAIRED PER SRM 57-14-00, FIG 804.

Part: FITTING — CORRODED (LT MLG)

HOLES CORRODED IN LT MLG FITTING FOR RETRACT ACTUATOR. HOLES NR 9, 14, 15, 16, FOUND IN HMV. REPAIRED PER SRM 57-14-00, FIG 804.

Part: FLOORBEAM — CORRODED (FS 901)

TOP OF FLOORBEAM IS CORRODED IN SEVERAL PLACES, FS 901 FROM LBL 60 TO RBL 60. REMOVED OLD FLOORBEAM, CUT NEW BEAM, DRILLED HOLES, TREATED AND PAINTED PER SRM 53-21-00 PG 849.

Part: FORMER — CRACKED (FS 769)

FORMER CRACKED AT STA 769 STRINGER 40. FOUND IN HMV. REPAIRED PER SRM 53-12-00, PG 823-824.

Part: TEAR STRAP — DISBONDED (FS 1695)

AT HMV - TEAR STRAP DISBONDED FS 1695 BETWEEN STR 29 AND 3. CORR: REPAIRED PER SRM 53-31-00.

Part: FITTING — CORRODED (LT MLG)

AT HMV, LT MLG RETRACT SUPPORT FITTING IS CORRODED MANY AREAS, ALL SURFACES. REPAIRED PER SRM 57-14-00 FIG 808 JPC 17.

Part: LUGS — CORRODED (LT MLG)

BOTH LUGS ON LT MLG RETRACT ACTUATOR FITTING ARE CORRODED, FOUND AT HMV. REPAIRED PER SRM 57-14-00 FIG 808 JPC 17.

Part: FITTING — CORRODED (LT MLG)

FASTENER HOLES NR 17, 18, 19, 20 ARE CORRODED AND HOLES NR 19, 20 HAVE DAMAGED BUSHINGS. REPAIRED PER SRM 57-14-00 FIG 808. FOUND DURING HMV, FOR LEFT MLG ATTACH FITTING.

Part: FLOORBEAM — CORRODED (FS 1463)

AT HMV, FLOORBEAM CORRODED FS 1463 RT SIDE BELOW CARGO TIE DOWN ABOVE STR 27. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-23-00 FIG 801. REMOVED CORRODED BEAM AND INSTALLED REPLACEMENT BEAM PER LAC DWG NR 1505121.

Part: FLOOR SUPPORT — CORRODED (FS 1565)

AT HMV, FLOOR SUPPORT CORRODED 4 RBL FS 1565. REMOVED CORROSION, OUT OF LIMITS PER SRM 53-23-00 FIG 802. DRILLED UP AND INSTALLED NEW FLOOR SUPPORT PER SRM 53-23-00.

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

AT HMV, TEAR STRAPS DISBONDED AT STR 29 AND 27 BETWEEN STA 923 AND 903. REPAIRED PER SRM 53-31-00.

Part: FAIL-SAFE STRAP — DISBONDED (FS 1575)

STRAP DISBONDED, FUSELAGE FAIL-SAFE STRAP DISBONDED ABOVE STR 40 FS 1575. REPAIRED PER SRM 53-31-00 PG 830.

Part: FORMER — CRACKED (FS 1063)

AT HMV, FORMER CRACKED LOCATED FS 1063, 1 INCH ABOVE FLOOR LBL. REPAIRED PER SRM 53-12-00 FIG 816.

Part: TEAR STRAP — DISBONDED (FS 599)

AT HMV, TEAR STRAP DISBONDED IN C-1 B/B AT FS 599 BETWEEN STR 35 AND 36. REPAIRED PER SRM 53-31-00.

Part: TEAR STRAP — DISBONDED (FS 759)

AT HMV, TEAR STRAP DISBONDED BETWEEN STR 28 AND 29 STA 759. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS AS PER SRM 53-31-00 PG 801. DRILLED UP TEAR STRAP SPLICE REPAIR AS PER SRM 53-31-00 FIG 816. INSTALLED TEAR STRAP SPLICE, TREATED/PAINTED REPAIR AREA.

Part: TEAR STRAP — DISBONDED (FS 739)

AT HMV, TEAR STRAP DISBONDED AT STA 739 BETWEEN STR 38-39. CORR: REMOVED TEAR STRAP AND REMOVED CORROSION. TREATED/PAINTED. REPAIRED PER SRM 53-31-00 FIG 816.

Part: FLOOR BEAM — CORROSION (FS 861)

AT HMV, TOP OF FLOOR BEAM IS CORRODED AT FS 861 LBL 50. CORR: TRIMMED CORRODED FLANGE AS PER SRM 53-21-00 FIG 823. INSTALLED REPAIR ANGLES PER SRM 53-21-00 FIG 823.

Part: TEAR STRAP — DISBONDED (FS 1480-1501)

AT HMV, TEAR STRAP DISBONDED AT FS 1480 TO 1501 BETWEEN STR 38 AND 39. REPAIRED PER SRM 53-31-00 PG 830.

Part: FLOORBEAM — CRACKED (FS 349)

AT HMV, FLOOR FRAME CRACKED AT FS 349 LBL 105 BELOW CABIN FLOOR AT WL 180. REPAIRED PER SRM 53-21-00 FIG 817.

Part: TEAR STRAP — DISBONDED (FS 779)

AT HMV, TEAR STRAP DISBONDED AT STA 779 BETWEEN STR 31 TO 32. DRILLED TEAR STRAP AS PER SRM 53-31-00 FIG 816. REPAIRED AREA AS PER SRM 53-31-00 FIG 816.

Part: FAILSAFE STRAP — UNBONDED (FS 1784)

FAILSAFE STRAP UNBONDED C3 B/B STA 1784 BETWEEN STR 35 TO 40, FOUND AT HMV. REPAIRED PER SRM 53-31-00 FIG 804.

Part: FITTING — CORRODED (RT MLG)

AT HMV, CORROSION ON LOWER SURFACE AND 45 DEGREE SURFACE JUST ABOVE ON MLG RETRACT ACTUATOR FITTING. REWORKED PER SRM 57-14-00 JPC 18.

Part: TEAR STRAPS — DISBONDED (FS 559)

AT HMV - TEAR STRAPS DISBONDED BETWEEN STR 40 AND 41, STA 559, ALSO BETWEEN STR 38-39 AND STR 39-40. REPAIRED PER SRM 53-31-00, PG 830.

Part: FITTING BUSHING — MIGRATED (RT MLG)

BUSHING MIGRATED IN RT MLG FITTING FWD TRUNNION, AFT LUG BUSHING. FOUND IN HMV. REPAIRED PER SRM 57-14-00, FIG 802, PG 803.

Part: TEAR STRAPS — DISBONDED (FS 599/589-569)

TEAR STRAPS DISBONDED BETWEEN STR 37 AND 38 STA 599. TEAR STRAPS DISBONDED BETWEEN STA 589 TO 569 BETWEEN STR 40 AND 41, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PAGES 801 AND 807.

Part: TEAR STRAPS — DISBONDED (FS 659/679)

AT HMV, TEAR STRAPS DISBONDED BETWEEN STR 39 AND 40 STA 659 AND 679. REPAIRED PER SRM 53-31-00 PAGE 830.

Part: FITTING — CORRODED (RT MLG)

AT HMV, CORROSION INSIDE SEVERAL ATTACH HOLES ON MLG RETRACT ACTUATOR FITTING. REWORKED PER SRM 57-14-00 JPC 18.

Part: FITTING — MIGRATED BUSHING (RT MLG)

BUSHING MIGRATED ON THE RT MLG ACTUATOR FITTING, FWD LUG FWD SIDE, FOUND AT HMV. REWORKED ER SRM 57-14-00 .

Part: FITTING — CORRODED (RT MLG)

AT HMV, CORROSION ON OUTBD SURFACE OF MLG RETRACT ACTUATOR FITTING. REWORKED PER SRM 57-14-00 JPC 18.

Part: TEAR STRAPS — DISBONDED (FS 559)

AT HMV - TEAR STRAPS DISBONDED FROM STR 34 TO STR 37. CORR: REPAIRED PER SRM 53-31-00, PG. 830.

Part: FITTING — CORRODED (RT MLG)

AT HMV, CORROSION ON TOP SURFACE OF MLG RETRACT ACTUATOR FITTING. REWORKED PER SRM 57-14-00 JPC 18.

Part: PANEL — DELAMINATED (SPOILER)

THE SPOILER PANEL HAD 2 AREAS OF DELAMINATION. THE DELAMINATED AREAS WERE REPAIRED PER SRM 57-52-00, FOUND AT HMV.

Part: TEAR STRAP — DISBONDED (FS 897)

AT HMV, TEAR STRAP DISBONDED FS 897 STR 43 TO 44, STRAP HAS CORROSION UNDERNEATH. REMOVED CORROSION, FOUND WITHIN LIMITS PER SRM 53-31-00 PG 801, REPAIRED PER SRM 53-31-00 PG 830 FIG 816.

Part: DRAIN — PLUGGED (MID GALLEY)

DRAIN ON CAPTS SIDE IN MID GALLEY STOPPED UP AND WATER SEEPED INTO SERVICE OUTLET. OUTLET BEGAN TO SMOKE, SHUT OFF ALL GALLEY POWER AND PULLED C/B. CLEARED DRAIN LINE AND REPLACED OUTLET RECEPTACLE.