N719DA

Part: BULKHEAD PANEL — CRACKED (BS 1212)

THE FUSELAGE 1212 BULKHEAD PANEL WAS FOUND WITH A TYPICAL VERTICAL CRACK AS ADDRESSED BY LAC S/B 093-53-277. THE CRACK IN THIS CASE IS LOCATED AT RBL 6 AND IS APPROX 1.5 LONG. UPON REMOVAL OF THE CRACK, A SHORT FASTENER EDGE DISTANCE CONDITION RESULTED, REQUIRING AN ENLARGED CUTOUT AS SHOWN ON FIGURE 1. THE SUBJECT DAMAGE WILL BE REPAIRED AS PER LAC S/B 093-53-277 INSTRUCTIONS, EXCEPT ON THE LOWER O/B SIDE, WHERE THE REPAIR DOUBLER/TRIPLER PROFILE IS TO BE MODIFIED AS SHOWN ON FIGURE 2 TO ACCOMODATE A CABLE PASS-THROUGH CUTOUT.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY AILSE LIGHT INOP AT 16B, 22B, 27H, 21H AND 16H. REPLACED EMERGENCY POWER PACK AT CENTER GALLEY. EMERGENCY LIGHTS INOP AT RT GALLEY AND DIM IN LOWER GALLEY. REPLACED LOWER GALLEY POWER PACK.

Part: SOCKETS — SHORTED (CABIN)

EMERGENCY TRACK FLOOR LIGHTING INOP FROM RT AISLE SEAT ROW 20JH THROUGH 26JH. FOUND BULB SOCKET AT SEAT 23JH SHORTED. REPLACED SOCKET, OPS CHECKS NORMAL, DAL P/N337201959 MFG P/N08169-1. FOUND ON NR 2 LAYOVER CHECK.

Part: STRAP — DAMAGED (BS 1363)

DURING ACCOMPLISHMENT OF SI 7-69959-12AD, THE AFT WEB SPLICE STRAPS AT RBL 42.5 AND LBL 42.5 WERE CUT AT THE LOWER END TO FACILITATE INSTALLATION OF THE LOWER CAP. REPAIRED PER SRM.

Part: ENGINE — MALFUNCTIONED (NR 2)

NR 2 ENG EPR GRADUALLY ROLLED BACK ON CLIMBOUT. OTHER ENGINE PARAMETERS FOLLOWED, FUEL AMP NO HELP.

Part: FUEL FLOW REG — MALFUNCTIONED (NR 2 ENGINE)

ENG NR 2 FLAMED OUT SHORTLY AFTER TAXIING CLEAR OF RUNWAY AFTER LANDING, WAS VERY HARD TO START. REPLACED FFR ON NR 2 ENG, ENG STARTS NORMALLY. PERFORMED CKS PER PFHB, ALL CKS OK. T/O PWR REACHED WITH PLENTY OF ROOM, NO LEAKS.

Part: BATTERY PACK — DISCHARGED (R 4 DOOR)

EMERGENCY EXIT LIGHT AT R-4 DOOR IS INOP. REPLACED R4 DOOR BATTERY PACK, CHECK GOOD PER OPN.

Part: TIRE CAP — MISSING (NR 3R WHEEL)

AT ROTATION, LOUD ENGINE VIBRATION AUDIBLE. CHECKED ENGINE VIBRATION LIGHT ON PILOT ANN ON CHANNELS A AND B, SHOWED 5.0 UNITS STEADY AND AT LEVEL OFF THROTTLE BACK VIBRATIONS DROPPED TO 3.8 BOTH CNLS, SHUTDOWN ENGINE. TOWER INSPECTED RUNWAY AND FOUND LARGE PIECES OF TIRE TREAD. NR 3 ENGINE SHUTDOWN, NR 3 REAR TIRE FLAT AND CAP MISSING/DAMAGE TO RT INBD FLAP VANE AND HYD LINES RT W/W AREA. ALSO, DAMAGE TO 1ST STAGE FAN NR 3 ENGINE.

Part: BLKHD ANGLE — CRACKED (FS 1363)

THE 1641601-102 ANGLE INSTALLED AS PART OF THE FS 1363 BULKHEAD MODIFICATION PER DAL EO 7-47702-3AD WAS FOUND CRACKED AT A FASTENER HOLE DURING ROUTINE LAYOVER INSPECTIONS AND OPERATIONS. THE CRACK APPEARS TO HAVE BEEN THE RESULT OF PRELOAD, CAUSED BY A GAP BETWEEN THE ANGLE AND THE ADJACENT STIFFENER. ACCOMPLISHED REPAIRS PER DL ERA 2 73193-14AD.

Part: CAP — BROKEN (LT MLG WW)

UPON LOWERING LT GEAR LOST C-SYSTEM FLUID TO ONE-QUARTER. FOUND LEFT LANDING GEAR PHASE CONTROL MODULE CAP BROKEN. REPLACED CAP, SERVICED SYSTEM OPERATION NORMAL.

Part: SKIN — CORROSION (FS 1363-1453)

DURING INSPECTION OF THE LOWER BELLY SKIN AREA, THE LOWER FUSELAGE SKIN FROM FS 1363 TO 1453 WAS FOUND TO HAVE AREAS OF SEVERE CORROSION. ACCOMPLISHED REPAIRS PER DL ERA 270760-14.

Part: STIFFENER — CRACKED (LT HORIZ STAB)

INTERNAL STIFFENERS CRACKED LT HORIZ LE PANEL 331F, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803.

Part: STIFFENER — CRACKED (RT HORIZ STAB)

INTERNAL STIFFENERS CRACKED RT HORIZ LE PANEL 341C, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803.

Part: STIFFENER — CRACKED (RT HORIZ STAB)

INTERNAL STIFFENER CRACKED RT HORIZ LE PANEL 341D, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803.

Part: STIFFENER — CRACKED (LT HORIZ STAB)

INTERNAL STIFFENER CRACKED LT HORIZ LE PANEL 331E, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803.

Part: TEAR STRAP — CORRODED (FS 476)

SKIN BULGED/RIVETS SHEARED FS 476 STRGR 27 TO 26. FOUND DURING INITAIL INSP AT HMV. CLEANED CORROSION PER 53-31-00 FIG 801 REPAIRED TEAR STRAP PER 53-31-00 FIG 804/836.

Part: STIFFENER — CRACKED (RT HORIZ STAB)

INTERNAL STIFFENER CRACKED RT HORIZ LE PANEL 341E, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803.

Part: FLOOR SUPPORT — CORRODED (BS 689)

C-1 B/B FLOOR SUPPORT CORRODED AT LBL3 FS 689. REPAIRED PER SRM 53-23-04. FOUND AT HMV.

Part: FITTING — CORRODED (RT MLG)

RT MLG FITTING CORRODED AT RETRACT ACTUATOR FTG HOLE 17. FOUND DURING HMV/CORROSION CK. REPAIRED PER SRM 57-14-00.

Part: FITTING — CORRODED (RT MLG)

RT MLG FITTING CORRODED AT RETRACT ACTUATOR ATTACHMENT HOLES 1 TO 6. FOUND AT HVM, REPAIRED PER SRM 57-14-00.

Part: FLOORBEAM — CORRODED (FS 1505)

STA 1505 FLOORBEAM CORRODED LBL 4 ON T-CAP. FOUND AT HMV. REPAIRED PER SRM 53-23-00 FIG 801.

Part: FITTING — CORRODED (RT MLG)

RT MLG FITTING IS CORRODED ON VERTICAL WALL AREA EXPOSED BY REMOVAL OF ACTUATOR FTG. FOUND AT HMV, REPAIRED PER SRM 57-14-00.

Part: STIFFENER — CRACKED (RT HORIZ STAB)

INTERNAL STIFFENERS CRACKED RT HORIZ LE PANEL 341A. FOUND DURING HMV INITIAL. REAIRED PER SRM 55-12-00 FIG 803.

Part: WEB — CORRODED (FS 1103)

WEB CORRODED AND PITTED INTERIOR OF CTR WING AT FS 1103, BETWEEN RBL 22 AND RBL 42 WITHIN 4 INCHES OF CTR BOX UPPER SKIN FWD SIDE 4 AREAS OF CORROSION AT FASTENERS. FOUND DURING HMV/CORROSION VISIT. REPAIRED PER SRM 57-11-00 FIG 811.

Part: TEAR STRAP — DISBONDED (FS 1792)

TEAR STRAP LIFTING AFT WASTE COMPARTMENT FS 1792 AND 1809 FROM STRGR 30 TO 31, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 807.

Part: FITTING — CORRODED (LT MLG)

LT MLG RETRACT FTG CORRODED ON FACES OF FTG COMMON TO HOLES 17 THROUGH 20 AND HOLES HAVE CORROSION IN THEM. FOUND DURING HMV. REPAIRED PER SRM 57-14-00.

Part: FITTING — CORRODED (RT MLG)

RT MLG FTG CORRODED UPPER SURFACE OF LWR ATTACHMENT FOR ACTUATOR FTG. FOUND AT HMV, REPAIRED PER SRM 57-14-00.

Part: TRUNNION — CORROSION (RT MLG)

RT MLG TRUNNION FWD/AFT LUG FACE HAS LIGHT CORROSION. SPOT FACED 019 DEEP ON FWD FACE AFT LUG OF FWD. TRUNNION TO REMOVE CORROSION. REWORK C/W ON R/C 1488 TO 1489, WITHIN LIMITS 57-14-00.

Part: FITTING — CORROSION (LT MLG)

LT MLG AFT TRUNNION FITTING A HAS CORROSION ON AFT FACE OF FWD LUG. BURNISHED FACE TO REMOVE LIGHT CORROSION.

Part: TRUNNION — CORROSION (RT MLG)

RT LOCAL BLEND 010 TO REMOVE CORROSION. REWORKED SRM LIMITS 57-14-00, C/W ON RC 1488 TO 1489.

Part: ANGLE — CORRODED (PRESS DOME)

AFT P-DOME CIRCUMFERENTIAL ATTACH ANGLE IS CORRODED AT STRINGER 27 AND 32. FOUND AT HMV, REPAIRED PER SRM 53-12-00 FIG 801 AND SRM 53-11-00 FIG 848.

Part: FAILSAFE STRAP — DISBONDED (FS 846)

FAILSAFE STRAP DISBONDED FS 846 BETWEEN STRINGER 31 TO 30. FOUND DURING CORROSION INSP AT HMV TASK NR C-53-130-05. CLEANED CORROSION PER SRM 53-31-00 FIG 801, INSTALLED REPAIR PER 53-31-00 FIG 804.

Part: TEAR STRAP — DISBONDED (FS 703)

FAIL SAFE STRAP DISBONDED AFT OF FS 703, BETWEEN STRINGER 37 TO 38. FOUND DURING CORROSION INSP AT HMV. REPAIRED PER SRM 53-31-00 FIG 804.

Part: TEAR STRAP — DISBONDED (FS 519)

C1 B/B TEAR STRAP DISBONDED AT FS 519 BETWEEN STGRS 26 AND 27. REPAIRED PER SRM 53-30-00. FOUND AT HMV.

Part: FITTING — CORROSION (LT MLG)

LT GEAR FITTING FWD TRUNNION FWD BORE HAS CORROSION ON FWD/AFT SIDES AND CORROSION AND PITTING IN BORE. BORED LUG TO 4.218 0 TO REMOVE CORROSION. BURNISHED FACES TO REMOVE PITS PER SRM 57-14-00.

Part: FITTING — CORRODED (LT MLG)

LT GEAR FITTING AFT TRUNNION FWD BORE PITTED IN BORE. BORED LUG TO 4.7095 INCHES TO REMOVE CORROSION.

Part: FITTING — CORRODED (LT MLG)

LT GEAR FITTING FWD TRUNNION AFT BORE HAS CORROSION ON FWD FACE AND CORROSION AND PITTING IN BORE. BORED LUG TO 4.229 TO REMOVE CORROSION. BLENDED AREAS TO REMOVE MINOR CORROSION. TREATED/PAINTED PER SRM 57-14-00.

Part: SPLICE — CRACKED (FS 1705)

BLKD SPLICE TEE CRACKED LT FS 1705 WL 405 VIEWED THROUGH PANEL 313A-1 AND 311UL.

Part: TEAR STRAP — DISBONDED (FS 559)

TEAR STRAP DISBONDED AT FS 559 STRINGER 25 TO 27, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 806-807.

Part: TEAR STRAP — DISBONDED (FS 579)

TEAR STRAP DISBONDED IN C1 FS 579 STRINGER 26, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 830.

Part: TRUNNION FITTING — CORROSION (LT MLG)

LEFT GEAR FITTING AFT TRUNNION AFT BORE HAS CORROSION FWD FACE. CORR SPOT FACED .004 DEEP AND LOCALLY BLENDED AREA, REMOVED CORROSION PER SRM 57-14-00. ALL REMAINING REWORK COMPLIED WITH ON RC'S 1453/1454.

Part: TEAR STRAP — CORRODED (FS 935)

AT HMV, LWR GALLEY TEAR STRAP DISBONDED FS 935 BETWEEN STR 40 TO 45, ON FUSELAGE SKIN. REPAIRED PER SRM 53-31-00 FIG 805.

Part: TEAR STRAP — DISBONDED (BS 1393)

TEAR STRAP DISBONDED FS 1393 BETWEEN STRGR 34 TO 35. REPAIRED DURING ACCOMPLISHMENT OF LOWER SKIN REPLACEMENT FS 1363 TO FS 1453, BETWEEN STRINGERS 31 AND 36, PER DL ERA 270691-14.

Part: BULKHEAD — CRACKED (LT MLG WW)

LT MLG WHEEL WELL AFT BULKHEAD HAS 5 CRACK BETWEEN STIFFENERS (LWR MID AREA).

Part: TEAR STRAP — DISBONDED (FS 599)

TEAR STRAP IS DISBONDED ABOVE STR 25 TO 24 AT FS 599. REPAIRED PER SRM 53-30-00. FOUND AT HMV.

Part: FORMER — CRACKED (BS 1103)

FORMER CRACKED AT STA 1103 LT SIDE W/L 198, JUST UNDER FLOOR LEVEL. REPAIRED PER SRM 53-12-00 FIG 816. FOUND AT HMV.

Part: FITTING — CORRODED (LT MLG)

LT MLG RETRACT FITTING, CORRODED HOLES 1 THROUGH 6 TO .750 TO REMOVE CORROSION. SPOT FACED NR 2 HOLE TO .060 DEEP. HOLE ID'S ARE WITHIN LIMITS PER SRM 57-14-00. CORROSION REMOVAL IN HOLES IS OK. FUTHER REPAIR COMPLETED ON JPC 032169 TRK NR MRL465. COMPLETED WITH ERA 270721-14.

Part: FORMER — CRACKED (FS 1383)

FORMER CRACKED STA 1883 AT STRINGER 19, FOUND AT HMV. REPAIRED PER SRM 53-12-00 PG 823.

Part: FITTING — CRACKED (FS 1043)

HORIZONAL TRUSS MEMBER FS 1043 LT SIDE IS CRACKED IN TWO, FOUND DURING HMV INITIAL INSP. REPAIRED PER SRM 53-21-00, PG 861-863.

Part: FITTING — CORROSION (LT MLG)

LT MLG FITTING HOLES 1 THROUGH 6 COMMON TO WING AT RETRACT FITTING ATTACH AREA ARE CORRODED. REMOVED HOLES 1 THROUGH 6 TO .750 TO REMOVE CORROSION. CORROSION REMOVED PER 54-14-00 HFEC PER SRM 57-14-00 PG 809. CAD PLATE PER PS 900-3-9, PRIMED AND PAINTED.

Part: FITTING — CORROSION (MLG)

MLG FITTING, CORROSION HOLES 17 THROUGH 20 COMMON TO WING AT THE RETRACT FITTING ATTACH AREA ARE CORRODED. REAMED HOLES 17 THROUGH 20 TO .625 TO REMOVE CORROSION. CORROSION REMOVED PER SRM 51-14-00 HFEC. ROTO PEENED PER SRM 57-14-00 PG 809. CAD PLATE PER PS 900-3-9, PRIMED AND PAINTED FITTING.

Part: FITTING — CORRODED (LT MLG)

LT MLG FITTING CORRODED ON UPPER SURFACE OF LWR RETRACT ACT ATTACHMENT. REMOVED CORROSION BY LOCAL BLEND, .020 DEEP. REMOVED CORROSION PER SRM 57-14-00, HFEC PER SRM 54-14-00 PG 809. ROTO PEENED PER SRM 57-14-00 PG 809. CAD PLATE PER PS 900-3-9, PRIMED AND PAINTED.

Part: FITTING — CORRODED (MLG)

AT HMV, MLG FITTING, CORRODED HOLES 17 THROUGH 20 COMMON TO WING AT THE RETRACT FITTING ATTACH AREA ARE CORRODED. CONTINUED ON N/R 2125. REAMED HOLES 17 TO 20 TO .625 TO REMOVE CORROSION. CORROSION REMOVAL OK PER SRM 57-14-00, HFEC PER SRM 57-14-00 CK OK. ROTO PEENED PER SRM 57-14-00 PG 809, CAD PLATED PER PS 900-3-9.

Part: LONGERON — CRACKED (FS 1123-1143)

DURING INITIAL INSPECTION FOR HMV, THE OUTBOARD FLOOR SUPPORT 'T' ANGLE WAS FOUND CRACKED AT FS 1123, 1143 RT. REPAIR PER SRM 53-21-00 FIG 825.

Part: THRESHOLD — CORRODED (R4 DOOR)

R4 DOOR LWR INNER THRESHOLD AFT CORNER FTG CORRODED. REPLACED CORNER FITTING PER SRM 51-10-05, SMALL PARTS REPLACEMENT. FOUND AT HMV.

Part: FITTING — CORRODED (R 4 DOOR)

R4 DOOR LWR INNER THRESHOLD FWD CORNER FTG CORRODED, FOUND DURING INITIAL INSPECTION AT HMV. REPLACED CORNER FITTING PER SRM 51-10-05.

Part: STIFFENERS — CRACKED (RT HORIZ STAB)

INTERNAL STIFFENERS CRACKED RT HORIZ LE PANEL 341F. REPAIRED PER SRM 55-12-00 FIG 803. FOUND AT HMV.

Part: STIFFENER — CRACKED (LT HORIZ STAB)

INTERNAL STIFFENERS, CRACKED LT HORIZ L/E PNL 331B. REPAIRED PER SRM 55-12-00 FIG 803.

Part: FLOORBEAM — CORRODED (FS 865)

FOUND FLOORBEAM CORRODED AT FUS STN. 865 RBL 40, CORROSION FOUND AT INITIAL INSPECTION DURING HMV. MADE FLOORBEAM REPAIR PER SRM 53-21-00 FIG 823.

Part: STIFFENERS — CRACKED (LT HORIZ STAB)

INTERNAL STIFFENERS CRACKED LT HORIZ LE PANEL 331D. REPAIRED PER SRM 55-12-00 FIG 803.

Part: STIFFENER — CRACKED (LT HORIZ STAB)

INTERNAL STIFFENER CRACKED IN LEFT HAND HORIZONTAL STABILIZER LEADING EDGE PANEL 331C. FOUND AT HMV, REPAIRED PER SRM 55-12-00 FIG 803.

Part: STIFFENERS — CRACKED (LT HORIZ STAB)

INTERNAL STIFFENERS CRACKED LT HORIZ LE PANEL 331G. REPAIRED PER SRM 55-12-00 FIG 803, FOUND AT HMV.

Part: ANTI-ICE RING — CRACKED (NR 2 ENG)

NR 2 ENGINE INLET ANTI-ICE RING DIMPLE SKIN IS CRACKED AT 1030 POSITION. REPAIRED PER SRM 54-34-00 FIG 804.

Part: STIFFENER — CRACKED (RT HORIZ STAB)

INTERNAL STIFFENERS, CRACKED RT HORIZ L/E PNL 341B. REPAIRED STIFFENERS PER SRM 55-12-00 FIG 803.

Part: FITTING — CORRODED (LT MLG)

LT MLG FITTING TRUNION FITTING HAS CORROSION ON FACE AT FWD ATTACH POINTS. REMOVED CORROSION PER SRM 51-21-02 MAX MATERIAL REMOVED .005 ROTO PEENED PER 51-21-00 CAD PLATE PER PS 900-3-9 PRIMED AND PAINTED.

Part: FRAMES — CRACKED (FUSELAGE)

AT HMV, FOUND MAIN FUSELAGE FRAMES CRACKED AT THE FOLLOWING LOCATIONS, RIGHT SIDE FS 649, 669, 680, 709, 729, 1685, 1705, THE LT SIDE, 1023, 1303, 1645, 1665, 1705. ALL CRACKS WERE AT WL 280. A SPECIAL INSPECITON FOR AIRCRAFT WITH 22,000 CYCLES AND HIGHER WAS SET UP. THIS IS THE FIRST TIME CRACKS WERE FOUND AT THESE LOCATIONS ON DL AIRCRAFT.

Part: FRAME — GOUGED (BS 1792)

STA 1792 FRAME GOUGED ON RT SIDE APPROX AT STRINGERS 23 AND 24. INSTALLED DOUBLER PER SRM 53-12-0 FIG 804.

Part: SPAR CAP — CRACKED (FS 1163)

FS 1163 UPPER T-CAP IN DRY BAY IS CRACKED ON RT SIDE OF A/C ANGLE WAS REPAIRED BY THE SRM 57-11-00 FIGURE 809. FOUND AT HMV.

Part: SKIN — CORROSION (FS 1765-1785)

FUS SKIN IS CORRODED IN C-3 B/B BETWEEN FS 1765 TO 1785 AND STR 37 TO 38. CLEANED CORROSION OUT OF LIMITS PER 53-31-00 FIG 801. CUT OUT SKIN PER SRM 53-31-00 FIG 803. DRILLED REPAIR PARTS PER SRM 53-31-00 FIG 803. TREATED/PAINTED, PARTS INSTALLED PER SRM 53-31-00 FIG 803, CMOR, EDGE SEALED REPAIR.

Part: ANGLE — CRACKED (FS 1103)

AT HMV, RT CUSP ANGLE AT FLOOR LINE CRACKED, AT ATTACH FASTENERS TO FLOORBEAMS, FS 1103, 1123, 1143. REPAIRED PER SRM 53-21-00.

Part: THRESHOLD — CORROSION (L 3 DOOR)

L-3 DOOR LWR INNER THRESHOLD PLATE IS CORRODED IN SEVERAL PLACES. CLEANED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-15-00 FIG 808. REMANUFACTURED THRESHOLD PLATE.

Part: DOOR FRAME — CORROSION (L 4 DOOR)

L-4 DOOR FRAME LWR AFT CORNER IS CORRODED. CORROSION OUT OF LIMITS. REMOVED LWR FITTING, DRILLED UP FITTING AND INSTALLED AS PER SRM 53-15-00 FIG 809.

Part: THRESHOLD — CORRODED (L 4 DOOR)

L-4 DOOR EDGE LWR INNER THRESHOLD PLATE IS CORRODED IN SEVERAL PLACES. CORROSION OUT OF LIMITS. REMOVED LWR INNER THRESHOLD PLATE, DRILLED UP NEW THRESHOLD PLATE, TREATED, PAINTED PER SRM 53-150-00.

Part: THRESHOLD — CORROSION (L 1 DOOR)

L-1 DOOR INNER LWR THRESHOLD PLATE HAS CORROSION IN SEVERAL PLACES. REMOVED CORROSION, WITHIN LIMITS PER SRM 53-15-00, LIMITS CK OK. TREATED AND PAINTED, REINSTALLED FASTENERS.

Part: FITTING — CORRODED (L3 DOOR)

L3 DOOR LWR INNER THRESHOLD FWD CORNER FITTING IS CORRODED. CLEANED CORROSION PER SRM 53-15-00 FIG 809, TREATED AND PAINTED.

Part: FITTING — CORRODED (R 3 DOOR SILL)

DURING INITIAL INSPECTION FOR OVERHAUL, THE AFT LOWER CORNER FITTING WAS FOUND TO BE CORRODED IN THE R-3 DOORWAY. THE PART WAS REPLACED BY A DELTA MANUFACTURED FITTING NR 1549499-103.

Part: SUPPORT — CORRODED (FS 253)

DURING OVERHAUL INITIAL INSPECTION, THE FWD LT LAV DOORWAY THRESHOLD HAT CHANNEL WAS FOUND CORRODED. REPLACED HAT CHANNEL WITH STAINLESS STEEL HAT PER SRM 53-21-00 FIG 826.

Part: FITTING — CORRODED (L-3 DOOR)

L3 DOOR LWR INNER THRESHOLD AFT CORNER FITTING IS CORRODED. CORRODED BEYOND LIMIT, REMOVED FITTING AND REMOVED AFT GIRT BAR LATCH FOR ACCESS.

Part: FLOORBEAM — CORRODED (FS 901)

HEAVY CORROSION ON THE FS 901 FLOORBEAM IN FRONT OF THE CART STORAGE AREA AT THE NR 2 CROSS AISLE. TYPICAL PROBLEM AT OVERHAUL. REPAIRED PER SRM 53-21-00 FIG 823.

Part: SKIN — BULGED (FS 479)

EXTERIOR SKIN, BULGED AND A RIVET IS SHEARED AT STA 479 BETWEEN STR 39 TO 40, JUST BELOW PURGE LINES. REMOVED FIX FLR PURGE LINES AND LWR ANGLE. OPENED/REMOVED CORROSION ON INNER SKIN PER SRM 900-2-4-1. CUT OUT GOUGE AND DYE CKD AREA FOR EXTERNAL REPAIR, NO CRACKS FOUND PER ERA 270810-14, TREAT/PAINTED AREA.

Part: FAIL-SAFE STRAP — CORRODED (FS 943)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 943 IN BETWEEN STR 42 TO 43. NO CORROSION FOUND, REPAIRED PER SRM 53-31-00 PG 830.

Part: FAIL-SAFE STRAP — CORROSION (FS 901)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 901 IN BETWEEN STR 42 TO 43. REMOVED GLUE/LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1, PAINTED PER PS 900-3-6. REINSTALLED STRAP PER SRM 53-31-00.

Part: TEAR STRAP — DISBONDED (FS 579)

C-1 BB TEAR STRAP AT FS 579 BETWEEN STGRS 37 AND 38 IS DISBONDED. REPAIRED PER SRM 53-30-00. FOUND AT HMV.

Part: STRAP — DISBONDED (FS 829)

FUSELAGE FAIL-SAFE STRAP IS DISBONDED AFT OF FS 829 IN BETWEEN STR 29 TO 28. REPAIRED PER SRM 53-30-00. FOUND AT HMV.

Part: TEAR STRAP — DISBONDED (FS 599)

C-1 BB TEAR STRAP AT FS 599 BETWEEN STGRS 38 AND 39 IS DISBONDED, UNDER AIR DUCT. REPAIRED PER SRM 53-30-00.

Part: TEAR STRAP — DISBONDED (FS 599)

C-1 BB TEAR STRAP AT FS 599 AND STGRS 27 AND 28 IS DISBONDED UNDER DUCT. REPAIRED PER SRM 53-30-00.

Part: FAIL-SAFE STRAP — CORROSION (FS 901)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 901 IN BETWEEN STR 41 TO 42. REMOVED GLUE AND LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1, PAINTED PER PS 900-3-6, REINSTALLED STRAP PER SRM 53-31-00.

Part: TEAR STRAP — DISBONDED (STA 519)

TEAR STRAP AT STA 519 AND STGRS 25 AND 26 IS DISBONDED. REPAIRED PER SRM 53-30-00. FOUND AT HMV.

Part: FAIL-SAFE STRAP — CORROSION (FS 923)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF 923 IN BETWEEN STR 39 TO 40. REMOVED GLUE AND LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1 PAINTED PER 900-3-6. REPAIRED PER SRM 53-31-00.

Part: FAIL-SAFE STRAP — CORRODED (FS 901)

FUSELAGE FAIL-SAFE IS DISBONDED FS 901 IN BETWEEN STR 29 TO 28. REMOVED GLUE AND LIGHT SURFACE CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED AND PAINTED PER PS 900-3-6. INSTALLED REPAIR PER SRM 53-31-00 FIG 804.

Part: FAIL-SAFE STRAP — CORROSION (FR 923)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 923 IN BETWEEN STR 41 TO 42. REMOVED GLUE AND LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1 AND PAINTED PS 900-3-6. REPAIRED PER SRM 53-31-00.

Part: FAIL-SAFE STRAP — CORRODED (FS 943)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 943 IN BETWEEN STR 40 TO 41. NO CORROSION FOUND, REPAIRED PER SRM 53-31-00 PG 830.

Part: TEAR STRAP — DISBONDED (FS 699)

C-1 BB TEAR STRAP AT FS 699 AND STGR 36 IS DISBONDED. REPAIRED PER SRM 53-30-00. FOUND AT HMV.

Part: STRAP — DISBONDED (FS 829)

FUSELAGE FAIL-SAFE STRAP IS DISBONDED AFT OF FS 829 IN BETWEEN STR 28 TO 27. REPAIRED PER SRM 53-30-00. FOUND AT HMV.

Part: FAIL-SAFE STRAP — CORROSION (FS 923)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 923 IN BETWEEN STR 42 TO 43. REMOVED GLUE AND LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1, PAINTED PER PS 900-3-6. REPAIRED PER SRM 53-31-00.

Part: FAIL-SAFE STRAP — CORRODED (FS 883)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 883 IN BETWEEN STR 44 TO 45. REMOVED GLUE AND LIGHT SURFACE CORROSION FROM DISBONDED AREA, TREATED, PAINTED AS PER PS 900-3-6. INSTALLED REPAIR PER SRM 53-31-00 FIG 804.

Part: FAIL-SAFE STRAP — CORROSION (FS 901)

AT HMV, FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 901 IN BETWEEN STR 43 TO 44. REPAIRED PER SRM 53-31-00 PG 809.

Part: FAIL-SAFE STRAP — CORRODED (FS 943)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 943 IN BETWEEN STR 44 TO 45. NO CORROSION FOUND, REPAIRED PER SRM 53-31-00 PG 830.

Part: FAIL-SAFE STRAP — CORROSION (FS 749)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 749 IN BETWEEN STR 24 TO 23. REMOVED CORROSION, CKD LIMITS PER SRM 53-31-00 FIG 801 PG 801, FOUND SKIN WITHIN LIMITS. FABRICATED AND DRILLED UP REPAIR DOUBLER PER SRM 53-31-00 FIG 804, INSTALL PER SRM 53-31-00 FIG 804, TREATED AND PAINTED.

Part: FAIL-SAFE STRAP — CORROSION (FS 943)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 943 IN BETWEEN STR 43 TO 44. NO CORROSION FOUND, REPAIRED PER SRM 53-31-00 PG 830.

Part: FAIL-SAFE STRAP — CORROSION (FS 901)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 901 BETWEEN STR 40 TO 41. REMOVED GLUE AND LIGHT CORROSION UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1, PAINTED PER 900-3-6, REINSTALLED STRAP PER SRM 53-31-00.

Part: FAIL-SAFE STRAP — CORROSION (FS 923)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 923 IN BETWEEN STR 43 TO 44. REMOVED GLUE AND LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1 PAINTED PER PS 900-3-6, REPAIRED PER SRM 53-31-00.

Part: FAIL-SAFE STRAP — CORROSION (FS 923)

FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 923 IN BETWEEN STR 40 TO 41. REMOVED GLUE AND LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1 PAINTED PER PS 900-3-6, REPAIRED PER SRM 53-31-00.

Part: SKIN DOUBLER — CRACKED (NR 3 EXCHANGER)

AT HMV, PNL DOUBLER CRACKED UPPER FWD CORNER FOR NR 3 HEAT EXCHANGER. REPAIRED PER SRM 53-31-00 FIG 834.

Part: FAIL-SAFE STRAP — CORROSION (FS 809)

FUS FAIL-SAFE STRAP IS DISBONDED AFT OF FS 809 IN BETWEEN STR 30 TO 29. CORROSION REMOVED WITHIN LIMITS PER SRM 53-31-00 PG 801 FIG 801. TREATED/PAINTED PER PS 900-3-6, INSTALL PER SRM 53-31-00 PG 830.

Part: FAIL-SAFE STRAP — CORROSION (FS 729)

FUS FAIL-SAFE STRAP IS DISBONDED AFT OF FS 729 IN BETWEEN STR 29 TO 28. VERIFIED NO CORROSION EXISTS. REPAIRED PER SRM 53-31-00 PG 830.

Part: FLOORBEAM — CORRODED (FS 1605)

TOP OF FLOORBEAM CORRODED STA 1605 LBL 3 TO 9. REMOVED DAMAGED AREA AND FABRICATED NEW CAP PER SRM 53-23-00 FIG 802.

Part: TEAR STRAP — DISBONDED (FS 1615)

TEAR STRAP DISBONDED AT FS 1615 BETWEEN STRINGER 39 AND 40. REPAIRED PER SRM 53-31-00 PG 30, FOUND AT HMV.

Part: SKIN — CORROSION (BS 1433)

SKIN CORRODED AT STA 1433 BETWEEN STR 32 TO 33 AT TEAR STRAP. C-2 B/B DOUBLE SKIN REPLACEMENT ACCOMPLISHED ON N/R 1978 AND ERA 270691-14.

Part: TEAR STRAP — BULGED (BS 1575)

TEAR STRAP BULGED STA 1575 BETWEEN STR 39 TO 40. REMOVED CORROSION UNDER TEAR STRAP. CHECKED LIMITS PER SRM 53-31-00 FIG 801, LIMITS CHECKED OK. TREATED AND PAINTED PER PS 900-3-6 AND FABRICATED SPLICE DOUBLER PER SRM 53-31-00.

Part: PRESSURE DECK — CRACKED (FS 1243)

PRESSURE DECK CRACKED RIGHT WHEEL WELL FS 1243 RBL 115 AT EXPANSION JOINT. REPAIRED PER SRM 53-11-00 FIG 844.

Part: TEAR STRAP — CORRODED (FS 1423-1443)

TEAR STRAP BETWEEN STA 1423 AND 1443 AT STR NR 27 IS DISBONDED AT BOTH SIDES OF STRINGER C-2 B/B. REMOVED CORROSION, WITHIN LIMITS PER SRM 53-31-00-801, TREATED/PAINTED. REPAIRED TEAR STRAP PER SRM 53-31-00 FIG 804.

Part: TEAR STRAP — DISBONDED (FS 1373)

TEAR STRAP DISBONDED STA 1373 ABOVE AND BELOW STR 40. REMOVED FASTENERS, CUT TEAR STRAP AND CLEANED CORROSION PER SRM 51-21-01, WITHIN LIMITS PER SRM 53-31-00. REPAIRED PER SRM 53-31-00 PG 830.

Part: SKIN — CRACKED (RT ELEVATOR)

TEMPORARY REPAIR INSTALLED ON RT ELEVATOR LOWER OTBD END. REPLACED WITH PERMANENT REPAIR PER SRM 55-22-00 FIG 802 WHICH REQUIRES AN MRR.

Part: ENGINE — BIRD STRIKE (NR 3)

ON TAKEOFF, NR 3 ENGINE INGESTED A SEA GULL WITH RESULTING COMPRESSOR STALLS, FLIGHT RETURNED TO PDX AFTER NR 3 ENGINE WAS SHUT DOWN. ENGINE WAS REPLACED DUE TO COMPRESSOR DAMAGE.