N786DL

Part: POWER PACK — INOPERATIVE (CABIN)

LOWER GALLEY EMERGENCY CEILING LIGHT AND R2 DOOR EXITS AND CEILING LIGHT INOP. REPLACED 2 EACH POWER PACKS.

Part: SPAR CAP — CRACKED (BS 1043)

THE UPPER CAP OF THE CENTER WING INTERMEDIATE SPAR AT FS 1043 WAS FOUND CRACKED BEYOND LIMITS AT THE LT OUTBD END. THE CAP WAS CUT NEAR LBL 80 AND A NEW OUTBD END WAS SPLICED IN WITH 4 STEEL SPLICE ANGLES AND 2 SPLICE STRAPS. THE REPAIR WAS ACCOMPLISHED PER ER/A 365093-14, REV A.

Part: TIMER — INOPERATIVE (CABIN)

MASKS DID NOT DROP IN D-ZONE DURING OXY DROP CHECK. REPLACED SEQUENCING TIMER (P/N 25720481) OPS CHECK GOOD.

Part: FITTING — CORRODED (WS 346)

RT MLG ATTACH RIB FITTING FOUND WITH CORROSION ON FACES AND IN BORES OF MLG ATTACH LUGS. REPAIRED PER ERA 331716-14.

Part: SPAR CAP — CRACKED (WS 258)

OVERSIZED FASTENER HOLES WERE FOUND IN THE VERTICAL FLANGE OF THE LT WING LWR REAR SPAR CAP AT APPROX IWS 258. THE FASTENER FINAL DIAMETER WAS 0.3428. REPAIRED PER ERA 331709-14AD.

Part: PLUG — LOOSE (NR 3 ENGINE)

A AND B LOOP FIRE WARNING ON NR 3 ENG. FOUND BOROSCOPE PLUG LOOSE AT THE NUMBER TWO FUEL NOZZLE.

Part: SPAR — CRACKED (BS 1103)

THE CENTER WING INTERMEDIATE SPAR UPPER CAP LOCATED AT STA 1103 WAS FOUND TO HAVE A 2 INCH CRACK ON THE RT O/B SIDE. THE CRACK WAS TYPICAL OF THOSE DESCRIBED IN S/B 093-57-087, BUT IS BEYOND THE ALLOWABLE LIMITS. THIS ER/A REPAIRS THE CRACKED UPPER CAP BY CUTTING AWAY THE DAMAGED SECTION AND SPLICING A NEW SECTION IN.

Part: PRESS RELIEF VLV — CRACKED (AFT PRESS BLKHD)

ONE OF THE SIX SPOKES ON THE LT NEGATIVE PRESSURE RELIEF VALVE ON THE AFT PRESSURE BULKHEAD WAS FOUND CRACKED. THE REPAIR/ MODIFICATION WAS ACCOMPLISHED PER L-1011 S/B 093-53-249, REV 2.

Part: ENGINE — BIRD STRIKE (NR 3)

ON T/O, NUMBER 3 ENGINE INGESTED AT LEAST ONE LARGE BIRD. PERFORMED FIRST STAGE HPC BORESCOPE INSPECTION AS PER MM. ENGINE FAILED INSPECTION, WILL REQUIRE ENGINE REPLACEMENT AS PER FIM 71-99-00 AND MM.

Part: DOOR — UNLATCHED (NLG)

ON ROTATION WHEN GEAR LEVER RAISED NOTICED NOSE GEAR RED DOOR LIGHT AND RED INTRANSIT LIGHT ON. LIGHT REMAINED ON AFTER GEAR RETRACTION. LEFT NOSE GEAR DOOR WAS FOUND HANGING DOWN. RELATCHED DOOR, SECURED OK.

Part: BULKHEAD — CRACKED (BS 1212)

DURING INSPECTION PER S.I. 7-70645-12AD, THE FS 1212 BULKHEAD WAS FOUND CRACKED AT RBL 6 AND RBL 42.5. THE RBL 42.5 CRACK WILL BE REPAIRED PER THE S.I. DUE TO THE BRAKE CONTROL CABLE FITTING.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY, OPS GOOD.

Part: SPAR WEB — CRACKED (WS 310-330)

THE RT WING REAR SPAR WEB AT THE UPPER CAP ATTACH AT IWS 310-330 AND UPPER WING SKIN HAS A CRACK. THE DAMAGE WAS REINFORCED WITH A REPAIR PLATE.

Part: FIRE WARN — MALFUNCTIONED (NR 1 ENGINE)

NR 1 ENGINE B-LOOP FIRE WARNING PLACED ON MCO BY FLIGHT CREW DURING TAXI OUT DUE TO FLICKERING. AT 17,000 FEET, NR 1 ENGINE A-LOOP STARTED FLICKERING ACCOMPANIED BY WARNING BELL AND LIGHT. ENGINE SHUT DOWN, BOTH BOTTLES DISCHARGED AND AIRCRAFT RETURNED TO JFK.

Part: BATTERY PACK — DISCHARGED (R4 DOOR)

R4 DOOR BATTERY PACK WILL NOT POWER LIGHTS. REPLACED PACK, CHECKS GOOD.

Part: OVEN — FIRE (GALLEY)

CUP COVERING EGGS IN OVEN CAUGHT FIRE IN NR 1 OVEN. FIRE EXT WITH HALON EXT.

Part: MECHANISM — JAMMED (L1 DOOR)

ON ARRIVAL, L1 DOOR WOULD NOT OPEN. FOUND SHEET METAL INSULATION SHIELD OVER DOOR RIPPED LOOSE AND JAMMING DOOR. REMOVED METAL DOOR. OPERATED NORMALLY.

Part: TRACK COVERS — CRACKED (CABIN)

FWD LT AND RT EMERGENCY TRACK LIGHT COVERS CRACKED IN FIRST CLASS. REPLACED BAD TRACK, CHECKED GOOD.

Part: HALON FIRE BOTT — DISCHARGED (LOWER GALLEY)

HALON FIRE BOTTLE ON CAPTS SIDE, USED IN LOWER GALLEY, SMALL FOOD TRAY FIRE. REPLACED HALON BOTTLE, INSPECTED OVENS AND ALL CHECK NORMAL. SUSPECT PART OF FOOD WRAPPER INADVERTENLY LEFT ON TRAY.

Part: BLKHD WEB — CRACKED (FS 1212)

THE FS 1212 BLKHD WAS FOUND WITH A 7 INCH VERTICAL CRACK AT RBL 22.5. THE CRACK WAS CUT OUT AND A REPAIR FILLER AND DOUBLER WERE INSTALLED PER DL ERA 273431-14A.

Part: FILLET PANEL — DAMAGED (LT FUS/WING)

A/C ARRIVED AT GATE WITH LEFT SIDE AFT FUSELAGE TO WING FILLET PANEL DAMAGED, 3 FT BY 5 FT SECTION WAS MISSING. REPLACED PANEL, RETURNED TO SERVICE.

Part: ACTUATOR FITTING — CORRODED (MLG)

THE RT AN LT MLG ACTUATOR ATTACH FITTING WERE FOUND WITH AREAS OF CORROSION. CORROSION WAS REMOVED FROM THE SURROUNDING AREA AND HOLE BORES OF HOLES 1, 2, 3, 4, 17 AND 19 ON THE LT FITTING. ALSO, HOLES 1, 2, 19 AND 18 ON THE RT FITTING. THE HOLES WILL BE REAMED AND BUSHED PER STANDARD SRM PRACTICES AND DL ERA 271413-14 REV B.

Part: ANGLE — CRACKED (FS 1043)

THE WING TO FUSELAGE JOINT FAIL-SAFE ANGLE AFT HOLE OF THE RT UPPER ROOT JOINT AT FS 1043, WAS OVERSIZED TO REMOVE A CRACK INDICATION. THE HOLE WILL BE TREATED FOR CORROSION AND RETURNED TO SERVICE PER DL ERA 271375-14AD.

Part: ATTACH BOLTS — IMPROPER PART (MLG)

DURING AIRCRAFT HEAVY MTC VISIT, IT WAS FOUND THAT A/C 786 WAS NOT LISTED IN THE ISSUED EFFECTIVITY IN REGARDS TO TEN BOLTS THROUGH THE VERTICAL LEG OF THE LT AND RT WING MLG ATTACH FITTINGS. THE BOLTS HAVE BEEN REPLACED WITH APPROVED SUBSTITUTES PER S/B 093-57-148.

Part: ATTACH TEE — CRACKED (WS 503)

DURING AIRCRAFT HEAVY MTC VISIT, THE RIB TO TORQUE BOX VERTICAL ATTACH TEE ON THE RT WING AT IWS 503 WAS FOUND CRACKED AT SEVERAL TYPICAL LOCATIONS. THE REPLACEMENT OF THE TEE IS COVERED IN S/B 093-57-207. THE TEE HAS BEEN REPAIRED PER THIS S/B.

Part: RIB — CRACKED (WS 503)

THE LT AND RT WING RIB UPPER CAPS AT IWS 503 WERE FOUND WITH SEVERAL CRACKS IN THE TYPICAL LOCATIONS AT THE ATTACH TABS AT AIRCRAFT HMV. THESE CAPS WILL BE REPLACED PER DL ERA 271522-14.

Part: RIB — CRACKED (WS 555)

LT/RT WING RIB LOWER CAP AT IWS 555 HAVE SEVERAL CRACKS IN THE TYPICAL LOCATION AT THE ATTACH TABS. REPAIRED PER DL ERA 271518-14AD. FOUND AT HMV.

Part: RIB — CRACKED (WS 503)

THE LT WING RIB UPPER CAP AT IWS 503 HAS SEVERAL CRACKS IN THE ATTACH TABS. DUE TO STRUCTURAL CONSTRAINTS IT IS DESIRABLE TO REPLACE THE UPPER CAP RATHER THAN REPAIR SUBJECT DAMAGED PART. REPAIRED PER DL ERA 271522-14AD.

Part: SKIN — DENTED (FS 1655)

AN UNIDENTIFIED EXTERNAL SKIN REPAIR WAS REMOVED FROM FS 1655, BETWEEN STRINGERS 24 AND 25. THE REPAIR CONSISTED OF A CUTOUT APPROX 4.5 BY 4.25, A 0.032 2024-T3 DOUBLER, .070 TRIPLER AND .090 FILLER. INSTALLED PERMANENT REPAIR PER DL ERA 271459-14. FOUND AT HMV.

Part: SKIN — CRACKED (FS 328)

THE FUSELAGE SKIN WAS FOUND SLIGHTLY BULGED AROUND THE LBL 22 FS 328 NLG W/W CORNER. UPON FURTHER INSPECTION, THERE WAS SLIGHT CORROSION FOUND ON THE INNER CUTOUT DOUBLER. THE CORROSION WAS REMOVED PER SRM PROCEDURES. AFTER REMOVAL OF THE EXISTING CORNER DOUBLERS A 1.5 INCH LONG CRACK WAS FOUND EXISTING IN BOTH THE OUTER FUSELAGE SKIN AND THE INNER CUTOUT DOUBLER. THE CRACK RUNS FWD FROM THE NLG W/W CUTOUT EDGE, THROUGH FASTENER AND ENDS IN A .3125 INCH DIA STOP DRILL. REPAIRED PER DL ERA 271415-14AD. FOUND AT HMV.

Part: SKIN — CORRODED (FS 539-983)

THE FWD LWR BELLY SKIN WAS FOUND WITH EXTENSIVE CORROSION BETWEEN FS 529 AND FS 983 AND STRINGER 29 AND STRINGER 42. DUE TO THE EXTENSIVE NATURE OF THE CORROSION AND EXISTING REPAIRS, REPLACEMENT OF LARGE AREAS OF THE FWD BELLY SKIN WILL BE REQUIRED. ACCOMPLISHED REPAIRS PER DL ERA 271311-14.

Part: TRIPLER — CORRODED (GALLEY DR CUTOUT)

THE FUSELAGE LWR GALLEY DOOR TRIPLER SURROUND STRUCTURE WAS FOUND WITH SEVERE CORROSION LOCATED IN THE LWR AFT CORNER OF THE DOOR CUTOUT. FOUND AT HMV, AND REPAIRED IAW DL ERA 271379-14.

Part: BLKHD SKIN — DAMAGED (BS 1365)

FOUND THAT 65 FASTENER HOLES WERE TOOL DAMAGED AT FS 1365 BULKHEAD, STR 22 TO STR 47. ACCOMPLISHED REPAIRS PER DL ERA 271346-14. REPAIRED PER ERA 271346-14.

Part: SKIN — CORRODED (FS 1453-1753)

THE AFT LOWER BELLY SKIN WAS FOUND TO BE CORRODED AT SEVERAL LOCATIONS BETWEEN FS 1453 AND FS 1753, BETWEEN STRINGERS 30 AND 36. THE FUSELAGE SKIN PANEL BETWEEN FS 1453 AND FS 1575 AND BETWEEN THE LAP JOINT AT STRINGER 24 AND STRINGER 31 IS HEAVILY CORRODED. A RUN-OUT TAB OF THE C-2 DOOR OUTER DOUBLER, AT FS 1535 BETWEEN STRINGERS 26 AND 27 WAS HEAVILY CORRODED. DUE TO THE EXTENSIVE LEVEL OF CORROSION, REPLACEMENT OF LARGE AREAS OF THE AFT SKIN IS REQUIRED. REPAIRS ACCOMPLISHED PER DL ERA 271342-14.

Part: CLIP — CORRODED (FS 809)

AT HMV, INSPECTION FOUND SKIN CLIP CORRODED AT STA 809 BETWEEN STR 30 AND 31. REMOVED DAMAGED CLIP AND INSTALLED NEW PER SRM 53-12-00 FIG 817.

Part: FITTING — CORRODED (FS 1501)

HMV - FRW AND AFT OUTFLOW VALVE SUPPORT FITTINGS CORRODED IN C-2 B/B. REPLACED P/N 1521684-101 AND 1521685-101 FITTINGS, REF DWG 1521682.

Part: CLIP — CORRODED (FS 729)

AT HMV, FOUND SKIN CLIP CORRODED STA 729 STR 31 TO 35. REMOVED OLD CLIPS AND DRILLED NEW CLIPS AND SPLICES. INSTALLED PER SRM 53-12-00 FIG 817.

Part: CLIP — CORRODED (BS 709)

AT HMV FOUND SKIN CLIP CORRODED STA 709 STR 33 TO 36. REMOVED CORRODED CLIP, DRILLED NEW CLIP AND SPLICE, AND INSTALLED PER SRM 53-12-00 FIG 817.

Part: CLIPS — CORRODED (FS 629)

AT HMV, FOUND SKIN CLIP CORRODED FS 629 STR 34 TO 35. REMOVED AND FABRICATED NEW SKIN CLIPS. INSTALLED PER SRM 53-12-00 FIG 817.

Part: CLIP — CORRODED (FS 549)

AT HMV, FOUND CLIP CORRODED FS 549 STR 34 TO 35. REMOVED DAMAGED FRAME TO SKIN CLIP AND INSTALLED NEW PER 53-12-0 FIG 817.

Part: CLIP — CORRODED (FS 829)

AT HMV, FOUND SKIN CLIPS CORRODED STA 829 STR 31 TO 33. REMOVED CORROSION, TREAT AND PAINTED, FABRICATED NEW FORMER TO SKIN REPAIR, AND INSTALLED PER SRM 53-12-00 FIG 817.

Part: FITTING — CORROSION (LT MLG)

AT HMV, LEFT MLG RETRACT ACTUATOR FITTING ATTACH POINT ON AIRCRAFT STRUCTURE FOUND WITH CORROSION DAMAGE. REPAIRED PER SRM 57-14-00 STEPS 2 TO 6.

Part: SKIN CLIP — CORRODED (BS 769)

AT HMV, FOUND CLIP CORRODED STA 769 BETWEEN STR 33 TO 35. CUT AND REMOVED CLIP, DRILLED NEW CLIP AND SPLICE STRAP, INSTALLED PER SRM 53-12-00 FIG 817.

Part: FITTING — CORRODED (RT MLG)

AT HMV, RT MLG RETRACT ACTUATOR FITTING ATTACH POINT ON AIRCRAFT STRUCTURE FOUND WITH CORROSION DAMAGE. REPAIRED PER SRM 57-14-00 STEPS 2 TO 6.

Part: CLIP — CORRODED (BS 849)

AT HMV, FOUND CLIP CORRODED STA 849 BETWEEN STR 31 TO 32. FABRICATED AND PAINTED NEW REPAIR, INSTALLED NEW FORMER TO CLIP REPAIR PER SRM 53-31-00 PG 817.

Part: CLIP — CORRODED (BS 569)

AT HMV, FOUND CLIP CORRODED STA 569 STR 33 TO 36. REPLACED SKIN CLIP PER SRM 53-12-00 FIG 817.

Part: CLIP — CORRODED (FS 789)

AT HMV, INSPECTION FOUND THE SKIN CLIP CORRODED AT STA 789 BETWEEN STR 33 AND 35. REMOVED DAMAGED CLIP, INSTALLED NEW PER SRM 53-12-00 FIG 817.

Part: RIB — CRACKED (WS 555)

LT/RT WING RIB UPPER CAPS AT IWS 555 HAVE SEVERAL CRACKS IN THE TYPICAL LOCATION AT THE ATTACH TABS. REPLACED CAP PER ERA 271319-14AD.

Part: HAT CHANNEL — CORRODED (CABIN)

HAR CHANNEL AT DOOR OPENING OF LT FIRST CLASS LAV IS CORRODED. REPAIRED PER SRM 53-21-00.

Part: FLOORBEAM — CORROSION (FS 295)

AT HMV, INSPECTION FOUND THE FLOORBEAM CORRODED AT FS 295 BETWEEN LBL 30 AND RBL 30. REPAIRED PER SRM 53-21-00.

Part: FLOORBEAM — CORRODED (CABIN)

AT HMV, FOUND FLOORBEAM CORRODED, AT LBL 53. REMOVED OLD CAP, TREAT AND PAINTED NEW CAP AND REPAIR ANGLES INSTALLED PER SRM 53-21-00 FIG 828.

Part: ANGLE — CRACKED (FS 1103)

FS 1103 RT SIDE FUSE FRAME ATTACH ANGLE AT FLOOR LEVEL CRACKED ON AFT SIDE OF FRAME THROUGH FASTENER HOLE, FABRICATED REPAIR ANGLE. OK TO INSTALL. REPAIRED PER SRM 53-21-00, PAGES 853-855.

Part: SUPPORT — CORRODED (FS 313-331)

AT HMV, FOUND FLOOR SUPPORT CORRODED FS 313.0 TO 331.0, RBL 28. REMOVED OLD CHANNEL AND REPLACED PER SRM 53-21-00.

Part: FITTING — CORRODED (RT MLG)

AT HMV, FOUND FITTING ON MLG RETRACT ACT CORRODED. REAMED HOLES AND BURNISHED AREA. HEFC OF AREA GOOD. MFG AND PAINTED SHIMS, INSTALLED BUSHINGS C/W ERA 271436-14. WORK DONE PER SRM 57-14-00.

Part: BULKHEAD — CRACKED (FS 328)

AFTER ACCOMPLISHMENT OF THE PERMANENT REPAIR PER ER/A226723-14, LAC DWG 1646545 AND EO 7-53207-3AD WAS ISSUED TO ACCOMPLISH REINFORCEMENT OF THE FS 328 CANTED BULKHEAD STRUCTURE ON DELTA'S ENTIRE L1011 FLEET. AFTER INSPECTION OF THE EXISTING MODIFICATIONS INSTALLED ON THE FS 328 BULKHEAD DURING HMV ON 7/95, IT WAS FOUND THAT THE EXTERNAL MODIFICATION PARTS ON THE RT SIDE DEVIATED FROM THE EO MODIFICATION. REPAIR APPROVAL PER DL ERA 271315-14AD.

Part: ANGLE — CRACKED (BS 349)

LOWER SUPPORT BEAM ATTACHED TO PRESSURE DECK CRACKED AT RBL 84 FS 349.1. REPLACED ANGLES, TEATED AND PAINTED. REINSTALLED FLOORBEAM SUPPORT STRUT PER SRM 53-21-00 PG 829.

Part: SKIN — CREASED (FS 349-409)

DURING HMV INSPECTION, THE FUSELAGE SKIN AFT OF THE L1 DOOR AT WL 200 FROM FS 349 TO FS 409 WAS FOUND WITH A CREASE. THE MAXIMUM DEPTH OF THE CREASE IS .045, AND THERE IS NO DAMAGE TO THE UNDERLYING STRUCTURE. ACCOMPLISHED REPAIRS PER DL ERA 271317-14.

Part: SPAR — CRACKED (BS 1043)

STA 1043 WING CTR SECTION INTERMEDIATE SPAR IS CRACKED AT THE UPPER CAP ON THE LT END. REPAIRED PER SRM 57-11-00.

Part: ACT FITTING — CORRODED (MLG)

AT HMV, FOUND FITTING CORRODED MLG RETRACT ACT. REAMED HOLES, SPOTFACED AND BLENDED AROUND HOLES. HFEC OF AREA OK. MFG AND PAINTED SHIMS, INSTALLED BUSHINGS PER ERA 271436-14, C/W SRM 57-14-00 FIG 805.

Part: TEAR STRAP — DISBONDED (BS 649-669)

AT HMV, FOUND TEAR STRAP DISBONDED STA 649 TO 669 STR 38. TEAR STRAP REMOVED PER ERA 271311-14.

Part: FLOORBEAM — CORRODED (FS 901)

FLOORBEAM UPPER CAP CORRODED MANY AREAS STA 901 FROM RBL 116 TO LBL 116. ACCOMPLISHED REPAIRS PER SRM 53-21-00 PG 849 FIG 823. FOUND AT HMV.

Part: TRACK — CORRODED (MID GALLEY)

AT HMV, FOUND SEAT TRACK CORRODED AT MID GALLEY ATTACH. REMOVED TRACK AND REPLACED PER SRM 53-21-00 PG 836.

Part: TEAR STRAP — LIFTED (FS 549-569)

AT HMV, FOUND TEAR STRAP LIFTED, C1 BB FS 549 TO 569, STR 25 TO 27. REPAIRED PER SRM 53-31-00 FIG 816.

Part: TEAR STRAP — DISBONDED (BS 629)

AT HMV, FOUND TEAR STRAP DISBONDED STA 629 STR 34. TEAR STRAP REMOVED PER ERA 271311-14.

Part: TEAR STRAP — DELAMINATED (STR 38)

AT HMV, FOUND TEAR STRAP DELAMINATED AT STRINGER 38. REPAIRED PER SRM 53-31-00 PG 803.

Part: CLIP — CORRODED (FS 480)

AT HMV, FOUND CLIP CORRODED STR 33 TO 36 FS 480. REPLACED SKIN CLIP PER SRM 53-12-0 FIG 817.

Part: NOSE COWL — CRACKED (BS 1705)

AT HMV, FOUND NOSE COWL CRACKED AT STA 1705, NR 2 INTAKE. REMOVED OLD ANGLE, AND FABRICATED NEW. INSTALLED PER SRM 54-12-00 PG 806.

Part: CLIP — CORRODED (FS 669)

AT HMV, INSPECTION FOUND SKIN CLIPS CORRODED AT STA 669 AFT SIDE BETWEEN STR 34 AND 35. ACCOMPLISHED REPAIRS PER SRM 53-12-00 FIG 817.

Part: DOUBLER — CORRODED (FS 1792-1809)

FAIL-SAFE STRAP DISBONDED AFT WASTE TANK COMPT. FAIL-SAFE STRAP DISBONDED AND BULKLED UP BETWEEN FS 1792 AND 1809. REMOVED STRAP DOUBLER AND REMOVED CORROSION, REPAIRED PER SRM 53-31-00.

Part: CLIP — CORRODED (BS 746)

AT HMV, FOUND CLIPS CORRODED FS 746 BETWEEN STR 32 AND 33. REMOVED DAMAGED FORM TO CLIP, FABRICATED CLIP AND SPLICE STRAP, INSTALLED REPAIR PER SRM 53-13-00 FIG 817.

Part: CLIP — CORRODED (BS 589)

AT HMV, FOUND FS 589 FRAME TO SKIN ATTACH CLIP CORRODED BETWEEN STRINGERS 34-36. REPAIRED PER SRM 53-12-00, FIG 817.

Part: SEAT TRACK — CORRODED (BS 349)

AT HMV, FOUND SEAT TRACK CORRODED, STA 349. CLEANED CORROSION FOUND OUT OF LIMITS, INSTALLED NEW TRACK PER SRM 53-21-00, PG 836.

Part: NOSE COWL — DAMAGED (FS 1705)

AT HMV, FOUND NOSE COWL HAD TIME LIMITED REPAIR. REMOVED OLD ANGLE. DRILLED NEW ANGLE AND INSTALLED PER SRM 54-12-00, FIG 803.

Part: CLIP — CORRODED (FS 866)

AT HMV, FOUND CLIPS CORRODED FS 866 FRAME BETWEEN STR 34 TO 35. REPAIRED PER SRM 53-12-00 FIG 817.

Part: NOSE COWL — CRACKED (NR 2 ENGINE)

AT HMV, FOUND NOSE COWL CRACKED RT UPPER FWD ACCESS NR 2 INLET. REMOVED FASTENERS FABRICATED REPAIR. DYE CHECKED AND INSTALLED REPAIR PER SRM 54-34-00 FIG 804.

Part: SKIN — DENTED (FS 509)

FUSELAGE SKIN DENTED FS 509 STRINGER 33 AND 34. REMOVED DAMAGED SKIN, DRILLED UP DOUBLERS FILLER REPAIRED PER ERA 271314-14. FOUND AT HMV.

Part: CLIP — CORRODED (FS 669)

AT HMV, INSPECTION FOUND SKIN CLIP CORRODED AT STA 669 FWD SIDE OF CLIP BETWEEN STR 34 AND 35. ACCOMPLISHED REPAIRS PER SRM 53-12-00 FIG 801.

Part: SEAT TRACK — CORRODED (BS 349)

AT HMV, FOUND SEAT TRACK CORRODED STA 349. REPLACED SECTION OF TRACK PER SRM 53-21-00 PG 836.

Part: SEAT TRACK — CORRODED (BS 749-846)

AT HMV, FOUND SEAT TRACK CORRODED STR 749 TO 846. REMOVED OLD SEAT TRACK, AND DRILLED NEW. INSTALLED TRACK PER SRM 53-21-00 PG 836.

Part: FLOOR SUPPORT — CORRODED (FS 1545)

FLOOR SUPPORT CORRODED C-2 B/B FS 1545 LBL 33. REMOVED FIXED FLOOR PANEL, INSTALLED NEW FLOOR SUPPORT PER SRM 53-23-00.

Part: SUPPORT — CORRODED (FS 1463)

FLOOR SUPPORT CORRODED C-2 BB FS 1463 RBL 10 TO RT FIXED FLOOR PANEL. ACCOMPLISHED REPAIRS PER SRM 53-23-00, FIG 801 AND 803.

Part: SUPPORT — CORRODED (FS 1463)

AT HMV, FOUND FLOOR SUPPORT CORRODED C2 B/B STA 1463 STR 35. REMOVED OLD SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT PER SRM 53-23-00 FIG 803.

Part: FLOOR SUPPORT — CORRODED (FS 1545)

FLOOR SUPPORT DAMAGED C-2 B/B FS 1545 LBL 50. REMOVED FLOOR SUPPORT, INSTALLED NEW FLOOR SUPPORT PER SRM 53-23-00. FOUND AT HMV.

Part: SUPPORT — CORRODED (FS 1565)

AT HMV, FOUND FLOOR SUPPORT CORRODED C2 B/B FS 1565 LBL 5. REMOVED OLD SUPPORT, FABRICATED NEW SUPPORT AND SPLICES, AND INSTALLED PER SRM 53-23-00 PG 803.

Part: CLIPS — CORRODED (BS 1463)

AT HMV, FOUND SKIN CLIPS CORRODED IN C2 BB AFT OF STA 1463 BETWEEN STR 33 AND 35. REPAIRED PER SRM 53-13-00 FIG 817.

Part: FRAME — CORROSION (FS 1585)

AT HMV, FOUND FRAME CORRODED. C2 BB STR 32-33 FS 1585. CLEANED CORROSION, REMOVED OLD DAMAGED PART. INSTALLED NEW REPAIR PER SRM 53-12-00, FIG 817.