N894UP
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
455 reports on file, 1995-03-13 – 2008-12-19.
Part: ATTACH ANGLE — CRACKED (LT ELEVATOR) · airframe 78,134 hrs · 25,452 cycles
INSPECTION TYPE: SV LT ELEVATOR STA 200.238 DOUBLER ATTACHED ANGLE IS CRACKED AND DENTED, REPAIRED IAW DWG 5700911 AND SRM 51-01-21.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,134 hrs · 25,452 cycles
INSPECTION TYPE:SV EVAL REPAIR DOUBLER INSTALLED AT STATION 161 UPPER SURFACE OF FUSELAGE SKIN JUST AFT OF NOSE RADOME SURVEY SEQUENCE 894-F1-43. REPAIRED IAW DC8 SRM 53-02-0 FIG 001 D SHEET 3.
Part: SKIN — CRACKED (FUSELAGE)
INSPECTION TYPE:N/A L1 DOOR HOLD OPEN LATCH AT FS 16 BETWEEN LONGERONS L-15L AND L-16L CRACK AT LOWER AFT CORNER OF PRODUCTION TRIMOUT. THE CRACK AND EXISTING STOP DRILL MEASURES 0.70 INCH LENGTH. COMPLIED WITH EO DC8-5330-31311-A.
Part: SKIN — UNKNOWN (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV INSTALL EXTERNAL SKIN DOUBLERS AT STA -88 TO -50 AND -29 TO 7 L21R. INSTALLED DOUBLERS IAW SRM DC-8 53-02-01 FIG 007.
Part: DOUBLER — UNKNOWN (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV (REPAIR STA -45 LBL 33 DOUBLE FILLER) REPAIR PER DAC DWG SR0830026 REF UPS NRC 188379. REPLACED FINGER AND SPLICE DOUBLERS IAW SR 08530026 REV A.
Part: DOUBLER — UNKNOWN (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV STA 904 OCTAGON DOUBLER REINSTALL DOUBLER. INSTALLED DOUBLER 51-01-08 AND DALFORT XEA X8-53-298.
Part: RIB — CRACKED (RT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV RT WING OUTBOARD L/E LOWER RIB CRACKED AT XFS 835. STOP DRILLED CRACK IAW SRM 57-2-0 DC8. MANUF AND INSTALLED REPAIR IAW DC8 SRM 51-1-8AND SRM DC8 SRM 51-01-20D-0.
Part: RIB — CRACKED (RT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV RT WING L/E LOWER RIB CRACKED AT XFS 829. STOP DRILLED CRACK IAW SRM 57-2-0 DC8. FABBED AND INSTALLED REPAIR IAW DC8 SRM 51-03-00-0, AND SRM 51-01-20D-0 DC8.
Part: FASTENER — DEFORMED (TE FLAP) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-28 LT WING INBOARD FLAP INBOARD EDGE WEB EXT REPAIR DOUBLER HAS 2EA DEFORMED FASTENER. REPLACED FASTENERS IAW DC8 SRM 51-01-21.
Part: DOUBLER — UNKNOWN (RT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV RIGHT LEADING EDGE DOUBLER NEEDS VALIDATION AT STA XFS 455 FAILED APPH STEP 5 894-W4-07. REPLACED DOUBLER IAW DC8 SRM 57-2-1 FIG 38.
Part: SKIN — MISREPAIRED (RT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV RT WING LEADING EDGE LOWER DOUBLER I/B SIDE OF NR 4 PYLON NEED VALIDATION AT STA XFS 500. DOES NOT MEET CRITERIA IN APPENDIX H STEP 5. 894-W4- 32 AREA PREVIOUSLY REPAIRED FEF SRM 57-3-1 T/R 57-83.
Part: SKIN — UNKNOWN (RT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV RT UPPER LEADING EDGE DOUBLER NEEDS VALIDATION AT STA 325 FAILS APPEN DIX "H" STEP 5 SURVEY SEQ 894-W4-5. REMOVED AND REPLACED REPAIR PER DC 8 SRM 57-2-1 FIG 38 TR 57-85.
Part: STOP — MISSING (NLG DOOR) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV LT FWD NLG DOOR BUFFER STOP MISSING. REPLACED FWD NLG DOOR BUFFER STOP IAW DC8 MM 32-22-01-5.
Part: STRUCTURE — MISREPAIRED (RT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV RT WING LOWER L/E DOUBLER REPAIR NEEDS VALIDATION FOR REPAIR AT STA XFS 747.600. DOES NOT MEET CRITERIA IN APPENDIX H STEP 1 SURVEY SEQ 89 4-W4-17. PREVIOUSLY REPAIRED IAW DC8 SRM 57-2-1 FIG 2H PG 15.
Part: SKIN — MISREPAIRED (NR 3 PYLON) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV RT LOWER LEADING EDGE DOUBLER I/B SIDE NR 3 PYLON AT STA XFS 225 DOES NOT MEET CRITERIA APPENDIX H STEP 5. 894-W4-31 AREA PREVIOUSLY REPAIRED FEF DC8 SRM 57-2-1 TR 57-83 FIG 14A.
Part: DOUBLER — UNKNOWN (RT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV RT UPPER LEADING DOUBLER NEEDS VALIDATION AT STA XFS627 FAIL APP H ST STEP 5 894-W4-12 REPAIRED IAW 57-2-1 AND 51-01-04.
Part: SKIN — MISREPAIRED (RT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV RT LWR LEADING EDGE DOUBLER STA XFS 524 NEEDS VALIDATION. DOES NOT MEET CRITERIA APPENDIX H STEP 5. 894-W4-19 AREA PREVIOUSLY REPAIRED & AND ADDED EXTRA ROW OF FASTENERS IAW DC8 SRM 57-2-1 TR 57-95 AND SRM 51-1-21.
Part: SKIN — MISREPAIRED (TE FLAP) · airframe 78,066 hrs · 25,409 cycles
INSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-20 LT INBOARD FLAP UPPER SURFACE AT STA XW89 DOES NOT MEET CRITERIA OF APPENDIX H. FLAP REPAIR MEETS CRITERIA TO BE IAW DC8 SRM 57-02-01-0 FIG 002Q.
Part: STRUCTURE — MISREPAIRED (WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV, L/E STATION XFS 88 DOUBLER DOES NOT MEET CRITERIA FOR APPENDIX H. REPAIR PREVIOUSLY ACCOMPLISHED PER DC8 73F SRM 57-2-1 FIG 2H CLASS B.
Part: SKIN — MISREPAIRED (TE FLAP) · airframe 78,066 hrs · 25,409 cycles
INSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-21 LT INBOARD FLAP EXTERIOR SURFACE AT STA XW1 05 DOES NOT MEET CRITERIA OF APPENDIX H. FLAP REPAIR MEETS CRITERIA TO BE IAW DC8 SRM 57-02-01-0 FIG 002Q.
Part: FLAP — MISREPAIRED (LT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-28 LT BS XW5.0 I/B FLAP WEB REPAIR DOES NOT MEET CRITERIA FOR APPENDIX H. FLAP REPLACED ON NR 188423.
Part: SKIN — MISREPAIRED (TE FLAP) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV RT FLAP UPPER EXT SURFACE BOILER PANEL DOUBLER REPAIR NEEDS VALIDATION. UPON FURTHER INVESTIGATION REPAIR DOES MEET CRITERIA OF EO DC8-5100-304 18 APPENDIX H STEP 5, NO FURTHER ACTION REQUIRED.
Part: FLAP — MISREPAIRED (RT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV RT INBOARD FLAP LOWER I/B EDGE DOUBLER IN STA 0.00 NEEDS VALIDATION, FAILED APPENDIX H STEP 5. REMOVED DOUBLER, FABBED AND INSTALLED NEW DOUBLER IAW DC8 SRM 57-2-05 AND SRM 51-1-21.
Part: DOUBLER — UNKNOWN (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV STA-53 TO -89 RBL TO RBL 42 DOUBLER NEEDS VALIDATION FOR REPAIR 894-F 3-11. REPAIRED BY SR08530026 AND SRM 53-2-1.
Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV EXT DOUBLER AFT LOWER DOOR CUTOUT BS 50.5 TO 55 L30L TO 1 INCH BELOW L 29L NEED VALIDATION FOR REPAIR. REPAIRED SRM 53-02-00 FIG 13.
Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV EXT WINDOW DOUBLER BS 1400 TO 1421 1.5 ABOVE L14R TO 1.5 BELOW L17R NEEDS VALIDATION FOR REPAIR. REPAIRED BY SRM 51-3-0 AND EO DC 5320-31585.
Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV EXT DOUBLER BS 1279.5 TO 1299.5 AT L35R CENTERLINE NEED VALIDATION FOR REPAIR REF SEQ 894-FA-57. REMOVED, FABBED AND REPLACED DOUBLER IAW BOEING ROD SKETCH 99-01-20-004 REV IR AND UPS EO DC8-53-20422.
Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV BS 659 TO 719.5 L35L TO L35R EXT DOUBLER LOWER BELLY NEED VALIDATION FOR REPAIR. REPAIRED IAW EO DC8-5300-3I587.
Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV REMOVE AND REPLACE ORIGINAL N/R 534909 LEFT LOWER CUSP MEMBRANE CRACKED, DENTED AND CORRODED BETWEEN FS 400-420. UPON INVESTIGATION FOUND DAMAGE WAS REMOVED AND VALIDATED REPAIR WAS A ACCOMPLISHED REF DC8 SRM 53-02-00 FIG 25.
Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV REMOVE AND REPLACE WITH SRM REPAIR. EFN 8941997-55. ORIGINAL N/R 5 34204 LEFT CUSP MEMBRANE CRACKED AT LBL 45 BETWEEN FS 1580-1600. REMOVED DOUBLER VERIFIED CRACK STOP DRILLED IAW SRM 53-02-00-0. REINSTALLED DOUBLER AND VERIFIED REPAIR COMPLIES WITH DC-8 SRM 53-02-00-0 FIG 23.
Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV REMOVE AND REPLACE EFN 89419971055 ORGINIAL N/R 534204 LEFT CUP MEMBRANE CRACKED AT LBL 45 BETWEEN FS 1580-1600. VERFIED REPAIR COMPLIES WITH SRM 53-02-00 FIG 23.
Part: RIB — CRACKED (LT WING LE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV EVALUATION OF N/R 535858 LT WING L/E REPAIR BETWEEN NR 1 AND 2 PYLONS TENTH RIB FROM INBOARD END IS CRACKED. REPAIR WAS ACCOMPLISHED IAW DC8 SRM 57-2-0 SHEET 2 OF 2.
Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV REMOVE REPAIR AND REPLACE WITH SRM REPAIR EFN 89419971080 ORIGINAL N/R 534358 CUSP MEMBRANE CRACKED BETWEEN LIGHTENING HOLES FS 80. UPON INVESTIGATION FOUND REPAIR MISSING ONE ROW OF FASTENERS, ADDED ROW 3 RIVETS AS IAW SRM 53-02-00. FOUND TO MEET ALL REQUIREMENTS OF OF DC8 SRM 53-02-00 FIG 25.
Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV REMOVE AND REPLACE WITH SRM REPAIR ORGINIAL N/R 534146 RIGHT CUSP MEMBRANE CRACK EXTENDING FROM STOP DRILL TO AFT OF FS 1600. INSTALLED DOUBLER AS PER SRM 51-21-01.
Part: FITTING — CRACKED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV BATH TUBE FITTINGG AT L33R-L34R IS CRACKED. REPAIR AS PER IAW DC8 SRM 51-03-02.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV FLUSH SKIN REPAIR CUT BS 88 TO 14 BETWEEN L31L AND L27L NEEDS VALIDATION. REPAIR PREVIOUSLY ACCOMPLISHED PER DC8 73F SRM 53-02-01 FIG 007.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV FUSELAGE EXTERIOR SKIN STA 50 L21R BULGING AND FASTENER HEAD SHEARED. REMOVED FASTENERS STA FS 70 TO FS 50 L19R TO L21R AND FS 50 TO FS 30 IAW DC 8 SRM 51-1-21. REMOVED DOUBLER FROM STA 7 TO STA 70 L20R-L21R. FABBED AND INSTALLED DOUBLER IAW DC8 SRM 53-03-03-0, DWG 5613861, AND SRM DC8 SRM 51-1-21.
Part: REPAIR — CORRODED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV LOWER FUSE-INT, BATHTUB FITTING REPAIR ANGLE HAS CORROSION AT FS 1180, BETWEEN L33R-L34R JUST INBOARD OF AFT CARGO DOOR CUTOUT LOWER EDGE. REPLACED REPAIR ANGLE IAW DC8 SRM 51-30-00-0-1 AND 53-02-00-0 FIG 002D.
Part: DOUBLER — GOUGED (TE FLAP) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV SURVEY SEQ 894-W4-23 RT WING INBOARD FLAP UPPER EXT SURFACE SKIN REPAIR DOUBLER EXT SURFACE GOUGED INBOARD OF BOILER PANEL AT STA XF 211. REMOVED AND REPLACED DOUBLER IAW DC-8 SRM 57-02-05 FIG 2.
Part: DOUBLER — GOUGED (TE FLAP) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV SURVEY SEQ NO 894-W4-24 RT WING INBOARD FLAP UPPER EXT SURFACE SKIN REPAIR DOUBLER EXT SURFACE GOUGED. REMOVED AND REPLACED DOUBLER IAW DC8 SRM 57-2-05 FIG 2.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV FLUSH REPAIR BS 151, 8 INCHES BELOW L21L HAS CLOSE FASTENER SPACING. ACCOMPLISHED IAW DALFORT AVIATION REPAIR XEA X8-53-706 AND REFERENCE DC8-73F SRM 53-2-0 FIG 1C PG 10 10 OF 14.
Part: FASTENER — LOOSE (LT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV SURVEY SEQ NO 894-W3-13 LT WING L/E ABOVE NR 2 PYLON AT XFS 275 SKIN REPAIR DOUBLER HAS 4 FASTENERS LOOSE AND 1 FASTENER PULLED THROUGH. REMOVED AND INSTALLED 5 NEW FASTENERS IAW DC8 SRM 51-3-0 FIG 52A.
Part: SKIN — MISREPAIRED (LT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV SURVEY SEQ NO 894-W3-03 LT WING L/E LOWER SURFACE SKIN REPAIR DOUBLER A HAS 5EA FASTENER HEADS PROTRUDING AT XFS 462.000 AFT OF SLOT DOOR. RE-COUNTERSINK HOLES AND INSTALLED SCREWS IAW DC8 SRM 51-3-0.
Part: SKIN — DAMAGED (RT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:CV EVALUATION AND DISPOSITION REPAIR SURVEY SEQUENCE NR: 894-W4-09. RIGHT UPPER LEADING EDGE DOUBLER REPAIR STA XFS 512 MISSING 8 EACH FA FASTENERS. INSTALLED FASTENERS IAW DC-8 SRM 51-03-00.
Part: FASTENER — BROKEN (LT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV SURVEY SEQ NO 894-W3-01 LT WING L/E LOWER SURFACE SKIN REPAIR DOUBLER HAS 1EA FASTENER HEAD BROKEN AT XFS 404.000 BETWEEN NR 1 AND NR 2 ENG. REPLACED FASTENER IAW UPS DC8 SRM 51-03-00.
Part: RIB — CRACKED (RT WING LE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV EVALUATION OF N/R 534213 RIGHT HAND LEADING EDGE AT STA XFS 804.00 UPPER LEFT RIB HAS A CRACK AFT END. REPAIR IS ACCOMPLISHED IAW DC8 SRM 57-2-0 FIG 2.
Part: WEB — CORRODED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 89419911026. ORIGINAL NR 303033. CORROSION REPAIR TO WEB AND ANGLE AT AFT PASS DOOR FS 1615-1625. REPAIR SATISFIES INTENT AND GUIDELINES OF DC8 SRM 53-2-0 FIG 001D. RF TS 894UP-20-20265.
Part: WEB — CORRODED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 89420061026. ORIG NR 994522 L33R STA 1 160 TO STA 1220 UPPER WEB HAS HEAVY CORROSION IN SEVERAL PLACES. REMOVED, FABBED, AND INSTALLED NEW DOUBLER AND FASTENERS IAW REO G12470.
Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV EVALUATION AND DISPOSITION REPAIR EFN 89419971107 ORIGINAL NRC 534711 R1 DOOR FORWARD DOOR JAB (FUSELAGE FRAME) REPAIR FOR ELONGATED HOLES. FABRICATED NEW INTERCOSTAL PER DAC DWG 561575700 REV EC, FABRICATED NEW FRAME DOUBLERS AND INSTALLED PER UPS DWG DC8 -53A001 REV A, EO DC8 5310-111728 B.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN89419971256 ORIG NR 535436 PREVIOUS REPAIR DOUBLER AND TRIPLER ON LONG 33L ARE CORRODED STA 1185-1295. REMOVED AND INSTALLED REPAIR DOUBLER IAW ROD SKETCH 97-05-06-006 AND SRM 51-30-01-00. ACTUAL REPAIR FOUND TO BE AT 33L STA 1185-1200.
Part: RIB — CRACKED (VERTICAL STAB) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:CV EVALUATION AND DISPOSITION REPAIR EFN89419911115. ORIGINAL N/R 480 775. VERTICAL STABILIZER L/E LOWER SECTION NR 25 RIB CRACKED AFT LT FLANGE. RFTS N894UP-9-20284 RIVETS INSTALLED IN FREE STANDING LEG OF REPAIR. REMOVED RIVETS AND INSTALLED LOCK FASTENERS IAW UPS DC-8 SRM 51-1-20D.
Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN89419971106 ORIG NR 534710 R-1 DOOR AFT DOOR JAMB REPAIR FOR ELONGATED HOLES (FUSELAGE FRAME). EXISTING REPAIR ACCOMP IAW DWG UPS DC8-53A-011A. RFTS N894UP-12-2027.
Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV EVALUATION AND DISPOSITION EFN 89419971107 ORGINIAL N/R 534711 R-1 DO OF FORWARD DOOR JAMB REPAIR FOR ELONGATED HOLES. REPAIRED BY ANGLE AND WEB REF DC8 51--21 EO DC8 5310-11728B AND DWG 53 DC8 53A-011-REV A.
Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV EVALUATION ESN 89420041016 N/R 721564 FOWARD ENTRY DOOR AFT LOWER JAMB REPAIR FOR ELONGATED HOLES. FAB NEW WEB IAW DC8 SRM 53-02-00 FIG 25 AND DC8 SRM 51-3-0.
Part: SEAT TRACK — GOUGED (BS 1470 RBL 46) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:CV EVALUATION AND DISPOSITION REPAIR EFN 89420081074. ORIGINAL N/R 14 7772 SEAT TRACK PLUG GOUGED FS 1470 RBL 46. REPAIR FOUND TO BE IAW SRM DC-8 53-2-3 FIGURE 60.
Part: FLANGE — CRACKED (RT WING) · airframe 78,066 hrs · 25,407 cycles
INSPECTION TYPE:SV RT WING LEADING EDGE AUX TANK AFT INBOARD SIDE VENT TUBE FLANGE CRACKED. REMOVED, REPAIRED, REINSTALLED FLANGE IAW DCI MM 20-12-00-2.
Part: PUMP — MALFUNCTIONED (NR 2 ENGINE)
INSPECTION TYPE:N/A AT FLT F/L 36.0 WITH BOOST OFF NR 2 ENGINE FLAMED OUT WHEN THROTTLE WAS MOVED TO IDLE. THIS WAS DURING A CONDITION FLT WITH A NEW PROCEDURE THAT THE FLT CREWS ARE FOLLOWING. A/C WAS NOT IN NORMAL FLT CONDITION WHEN THE FLAME OUT OCCURRED. REMOVED NR 2 ENG FUEL BOOST PUMP IAW MM 73-10-01-2. INSTALLED NR 2 ENG FUEL BOOST PUMP IAW MM 73-10-01-2. REQUIRES LEAK AND OPS CHECK VERIFIED VSV STATIC RIG. CHECKS GOOD. PERFORMED ENGINE RUN REF MM 71-00-00-1 AND 71-00-00-5. ENG RUN OPS GOOD.
Part: FITTING — CRACKED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 STA 280, L36 FLANGE IS CRACKED ON FITTING. REMOVED AND REPLACED STA 280/L 36 FITTING IAW SRM 51-01-24-0 AND SRM 51-03-00-0.
Part: ANGLE — CRACKED (NR 1 STUBWING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 NR 1 STUBWING INBOARD WEB "L" ANGLE CRACKED IN LOWER RADIUS. FABRICATED AND REPLACED NR 1 STUBWING INBOARD WEB L-ANGLE IAW SRM 51- 01-20D, SRM 51-03-00 AND SRM 51-1-21.
Part: FITTING — CRACKED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 TAIL 62 COMPT POGO STICK FITTING CRACKED AT FWD END. REPLACED POGO STICK SUPPORT FITTING IN 62 COMPT IAW SRM 51-03-00, SRM 51-01-21, SRM 51-01-24-0 AND SRM 51-03-01-0.
Part: SEAT TRACK — CORRODED (BS 130 RBL 30) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 CORROSION, MISSING BOLTS ON SEAT TRACK SPLICE IN A-PIT CEILING,STA 130, RBL 30. FABBED AND REPLACED SEAT TRACK SPLICE AT STA 130 AND RBL 30 IAW SRM 51 -03-00, SRM 53-02-00 FIG 1F, SRM 53-02-03 FIG 6A.
Part: RIB — GOUGED (LT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING CENTER LE INBD UPPER RIB GOUGED AT PNEUMATIC DUCT STA 494. REPAIRED LT WING CENTER LE INBD UPPER RIB AT STA XFS 494 IAW SRM 57-02-00 FIG 002, 57-03-03-0 FIG 005 AND SRM 51-1-20D.
Part: RIB — CRACKED (RWS 434) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB CRACKED XFS 434. REPAIRED RT WING CENTER LE RIB AT XFS 434 IAW SRM 57-02-00-0 FIG 002 AND SRM 57-03-03-0.
Part: RIB — CHAFED (RT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 PNEUMATIC DUCT CHAFING AT RIGHT L/E INBOARD OF SLAT DOOR STA XFS 404.000. REPAIRED RIGHT L/E INBOARD RIB AT XFS 404.000 IAW SRM 57-02-00-0, SRM 51- 01-08 AND SRM 51-03-03-01.
Part: INTERCOSTAL — CRACKED (RWS 434) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RIGHT WING CENTER L/E INTERCOSTAL CRACKED AT OUTBOARD PERI-SEAL STAND-OFF BRACKET AT XFS 434. FABRICATED AND REPLACED RIGHT WING CENTER L/E INTERCOSTAL AT XFS 434 IAW DWG 5769857 AND SRM 51-01-20D.
Part: RIB — CRACKED (RWS 458) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB CRACKED XFS 458. REPAIRED RT WING CENTER LE UPPER RIB AT XFS 458 IAW SRM 57-03-03-FIG 0 05 AND SRM 57-02-00-0 FIG 002 SHT 2.
Part: RIB — CRACKED (RWS 332) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RT WING CENTER LE LWR RIB REPAIR DOUBLER CRACKED AT XFS 332. REPAIRED RT WING CENTER LE LOWER RIB AT XFS 332 IAW SRM 57-03-03-0 AND 57-02-00-0 FIG 002.
Part: RIB — CRACKED (RWS 320) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RT WING CENTER LE LOWER RIB DOUBLER CRACKED AT XFS320. REPAIRED RT WING CENTER LE LOWER RIB AT XFS320 IAW SRM 57-03-03-0 AND SRM 57-02-00-0 FIG 002.
Part: FLOORBOARD — DAMAGED (BS 1680) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 MAIN CABIN AT STA 1680 AFT FLOORBOARD F213 HAT CHANNEL IS DAMAGED AT EDGE. FABRICATED AND REPLACED HAT CHANNEL ON FLOORBOARD F213 IAW SRM 51-02-0 FIG 52 AND 53-02-00 FIG 002.
Part: RIB — CRACKED (RWS 410) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB WORN AND GOUGED AT XFS 410. REPAIRED RT WING CENTER LE UPPER RIB AT XFS 410 IAW SRM 57-03-03-0 AND SRM 57-02-00-0 FIG 002.
Part: RIB — CRACKED (RWS 356) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB CRACKED AT XFS356. REPAIRED RT WING CENTER LE UPPER RIB AT XFS 356 IAW SRM 57-03-03 FIG 005 AND SRM 57-02-00-0 FIG 002.
Part: FRAME — CRACKED (RT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RT WING UPPER SURFACE NR 4 STUBWING INBD UPPER FRAME CRACKED, GOUGED AND CHAFED. REPAIRED RT NR 4 STUBWING INBD UPPER FRAME IAW SRM 51-01-20D, SRM 51-01 -21, SRM 57-02-00-0 FIG 002 AND DWG 5769525.
Part: DOUBLER — CRACKED (RT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RT WING CENTER LE LOWER RIB REPAIR DOUBLER CRACKED XFS 368. FABRICATED RT WING CENTER LE LOWER RIB DOUBLER AND REPLACED IAW SRM 51-01-21, SRM 57-03-03-0 AND SRM 51-01-20D.
Part: RIB — CRACKED (RWS 326) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RT WING CENTER LE LOWER RIB CRACKED AT XFS 326. REPAIRED RT WING CENTER LE LOWER RIB AT XFS 326 IAW SRM 57-03-03-0 AND SRM 57-02-00-0 FIG 002.
Part: SKIN — CRACKED (RWS 404) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RT WING CENTER LE UPPER SKIN DOUBLER CRACKED AT XFS 404. FABRICATED AND REPLACED RT CENTER LE UPPER SKIN DOUBLER IAW DWG 576989 1.
Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 A PIT STA 390, LONGERON 36 SPLICE HAS EVIDENCE OF CRACK. REPLACED LONGERON 36 SPLICE AT STA 390 IAW SRM 51-01-20.
Part: FRAME — CRACKED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 D-PIT STA 1420 LONGERON 35L, FRAME SECTION HAS CRACK PAST THE TERMINATION HOLE AT PREVIOUS REPAIR. REPAIRED FLOOR SUPPORT FRAME AT STA 1420 AND 35L IAW DC8 EO-5320-6176- C.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 FLOOR PANEL F80B HAS DENTS AND CRACKS AS MARKED. REPAIRED FLOOR PANEL F80B IAW SRM 53-02-03-0 FIG 10 AND SRM 53-02-03-0.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 FLOOR PANEL F81/F81A HAS 3 EA. DAMAGED SCREW HOLES AS MARKED. REPAIRED FLOOR PANEL F81/F81A IAW SRM 53-02-03-0 FIG 010 AND SRM 51-1-21.
Part: BELTFRAME — GOUGED (BS 1140 L21R) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 BELTFRAME END FITTING GOUGED IN MAIN CABIN STA 1140 AND L21R. FABRICATED AND REPLACED BELTFRAME END FITTING AT STA 1140 AND L21R IAW DWG 3755856, SRM 51-03-02-0, SRM 51-01-08 AND SRM 51-01-20D.
Part: GUSSET — CRACKED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 MAIN CABIN GOUGE/CRACK IN BELTFRAME GUSSET STA 1460 AND L21R. FABRICATED AND REPLACED BELTFRAME GUSSET AT STA 1460 AND L21R IAW SRM 51-21-24, DWG 5773480, SRM 51-1-8 AND SRM 51-01-20D.
Part: STRUCTURE — DAMAGED (RT MLG WW) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RIGHT GEAR DOOR SWITCH MOUNT HOLES ARE ELONGATED. REPAIRED RIGHT GEAR DOOR SWITCH HOLES IAW EO DC8-3260-16914-A AND DWG 56 53490.
Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT CUSP HEAVILY CORRODED AT STA 1000. REPAIRED LT CUSP AT STA 1000 IAW SRM 53-02-05 FIG 15.
Part: WEB — CRACKED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 D-PIT STA 1380 LONG 23L HAS 1 EA WEB WITH CRACK AT AFT EDGE. FABRICATED AND REPLACED STA 1380/LONGERON 23L WEB IAW DWG 4619815, SRM 51-01-08-0, SRM 51-01-21A AND SRM 51-01-21.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 D-PIT AT STA 1420 LONGERON 36, SHEAR TIE IS CRACKED AT OUTBD LOWER EDGE. FABRICATED AND REPLACED L36 SHEAR-TIE AND SPLICE PLATE AT STA 1420 AND LONGERON 36 IAW SRM 51--01-20D, SRM 51-01-21, SRM 53-02-10 FIG 002 B AND SRM 53-04-01 FIG 051.
Part: FITTING — CORRODED (BS 1440) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 CORROSION ON T-FITTING ON TOP OF CUSP AT STA 1440 LT. REPLACED T-FITTING AT CUSP AND STA 1440 LT IAW SRM 51-03-02, SRM 51-01-20D AND 51-03-00.
Part: FLOOR PANEL — TORN (CABIN) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 FLOOR PANEL F81B HAS 1EA SCREW HOLE TORN THROUGH EDGE. REPAIRED FLOOR PANEL F81B IAW SRM 53-02-03-0 FIG 010 AND SRM 51-1-21.
Part: FITTING — CRACKED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 MAIN CABIN BELT FRAME END FITTING INSIDE TORQUE BOX CRACKED AT INBD BOLT HOLE STA 1170 AND L21R. REMOVED AND REPLACED BELTFRAME END FITTING AT STA 1179 AND L21R IAW SRM 51-01-20D, SRM 51-01-24-0, SRM 51-03-00.
Part: FLOORBEAM — CORRODED (BS 1700) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 MAIN CABIN FLOORBEAM HAS INTERGRANULAR CORROSION, LOWER SURFACE OF UPPER AFT FLANGE STA1700 RBL 20 TO 28. REPAIRED MAIN CABIN FLOORBEAM AT STA 1700 RBL 20 TO 28 IAW EA 008- 5310-01-A1369, EO DC8-5310-29405-AAND DWG 5755032.
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 SEAT TRACK WORN LBL 61 STA 930 MAIN CABIN. REPAIRED MAIN CABIN SEAT TRACK AT STA 930 AND LBL 61 IAW SRM 51-1-8 AND SRM 53-02-03-0 FIG 006D.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RT SEAT TRACK DAMAGED RBL 46 FROM STA 380-STA 385. REPAIRED CABIN SEAT TRACK AT RBL 46 STA 380 TO STA 385 IAW SRM 53-02-0 3-FIG 006D, SRM 51-01-08, SRM 51-03-00.
Part: CHANNEL — CORRODED (FLOORBOARD) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 MAIN CABIN LAV AREA SAT 66-RBL 30, FLOORBOARD BOTTOM U-CHANNEL IS BLOWN OUT. REMOVED AND REPLACED U-CHANNEL ON FLOORBOARD IAW SRM, 53-2-3, 51-3-0, 51-1-8.
Part: FRAME — CRACKED (T/E FLAP) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT OUTBD FLAP LE SUPPORT FRAME CRACKED IN LOWER ATTACH ANGLE RADIUS INBD FROM STA 340 HINGE. FABRICATED AND REPLACED LT OUTBD FLAP LE ATTACH ANGLE INBD OF STA 34 0 IAW DWG 5655752, SRM 51-01-24, SRM 51-01-24, SRM 51-01-20D.
Part: FLOORBOARD — CORRODED (CABIN) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 MAIN CABIN COURIER AREA STA 55 AND RBL 12 FLOORBOARD SKIN CORRODED. REPAIRED FLOORBOARD AT STA 55 AND RBL 12 IAW SRM 53-02-03 FIG 10 AND DWG 5892154.
Part: LONGERON — CORRODED (BS 1766 L26L) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 MAIN CABIN AT STA 1766 LONGERON 26L END FITTING HAS AREA OF MODERATE C CORROSION. REPLACED LONGERON 26L END FITTING AT STA 1766 IAW SRM 51-01-21-0.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 CABIN STA 1130 RBL 50 SEAT TRACK SCALLOP IS GOUGED. REPLACED SEAT TRACK PLUG AT STA 1130 AND RBL 50 IAW SRM 51-03-00.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 MAIN CABIN SURFACE CORROSION ON VERTICAL FLOORBEAM SUPPORT (AFT SIDE) STA 1746 AT C/L. REPAIRED VERTICAL FLOORBEAM SUPPORT AT STA 1746 AND BL-0 BY FABRICATION AND REPLACEMENT IAW SRM 51-01-21, DWG 5773846 AND SRM 51-01-20D.
Part: SEAT TRACK — DAMAGED (BS 400-408) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RIGHT SEAT TRACK DAMAGED RBL 46 FROM STA 400 TO 408. REPLACED SEAT TRACK CHANNEL AND PLUG AT RBL 46 AND STA 400 TO 408 IAW SRM 51-03-00, SRM 53-02-03 FIG 6D, SRM 51-9-00 FIG 065.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 A PIT CARGO COMP FLOORBEAM AT STA 70, LBL 50 IS CORRODED. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR ANGLE AND FILLER IAW, SRM 51-1-8, 51-3-0, 53-2-0 FIG 1F.
Part: RIB — CRACKED (LWS 386) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING CENTER LE UPPER RIB CRACKED XFS 386. REPAIRED LT WING CENTER LE RIB AT XFS 386 IAW SRM 57-02-00 FIG 002 AND SRM 57-03-03-0 FIG 005.
Part: FITTING — CORRODED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LOWER FLOOR SUPPORT FRAME FITTING STA 200, RT TUNNEL PIT IS CORRODED. FABRICATED AND INSTALLED FITTING IAW DWG 3772922, SRM 51-01-20D, SRM 51-01-21.
Part: RIB — CRACKED (LT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER RIB CRACKED AT XFS 398. REPAIRED LEFT WING CENTER L/E UPPER RIB AT XFS 398 IAW SRM 57-02-00-0 FIG 002 AND SRM 57-03-03-0 FIG 005.
Part: FITTING — CRACKED (LT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LEFT WING CENTER L/E SLOT STRESS PANEL TO ROD END FITTING HAS 8 INCH CRACK AT OUTBOARD END. REMOVED AND REPLACED LT CENTER L/E FITTING IAW SRM 51-3-0 AND SRM 51-1- 24.
Part: SKIN — DAMAGED (LT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING CENTER LE LOWER OUTBD EXTERIOR SKIN HAS OVERSIZED SCREW HOLES AT SLOT CUTOUT. REPAIRED LT WING LE LOWER OUTBD EXTERIOR SKIN SCREW HOLES IAW SRM 57-03 -03-0 FIG 005 AND EO DC8-5720-7767-A.
Part: RIB — CRACKED (LWS 467) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING CENTER LE UPPER RIB CRACKED XFS 467. REPAIRED LT WING CENTER LE UPPER RIB AT XFS 467 IAW 57-02-00-0 FIG 002 AND SRM 57-03-03-0 FIG 005.
Part: RIB — CRACKED (LT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING CENTER LE UPPER RIB CRACKED AT XFS 434. REPAIRED LT WING CENTER LE UPPER RIB AT XFS 434 IAW SRM 57-02-00-0 FIG 002, SRM 57-03-03-0 FIG 005.
Part: RIB — CRACKED (LWS 440) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING CENTER LE UPPER RIB CRACKED XFS 440. REPAIRED LT WING CENTER LE UPPER RIB AT XS 440 IAW SRM 57-02-00-0 FIG 002 AND SRM 57-03-03-0 FIG 005.
Part: SKIN — DAMAGED (LT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LEFT WING CENTER L/E REPAIR DOUBLER HAS OVERSIZED SCREW HOLES AT OUTBOARD END OF SLOT VANE. FABRICATED AND REPLACED FILLER AND DOUBLER AT LEFT WING CENTER L/E AT OUTBOARD END OF SLOT VANE IAW EO DC8-5720-7767-A.
Part: WEB — GOUGED (STUB WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 SEVERAL DEEP GOUGES IN INBOARD WEB AT NR 1 STUB WING. REPAIRED NR 1 STUB WING INBOARD WEB IAW SRM SRM 57-02-00, DWG 9753297, SRM 51-01-08 AND SRM 51-01-21.
Part: SKIN — CORRODED (LT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LEFT WING CENTER L/E 4 EA SCREWS PULLING AND HAVE CORROSION ON SKIN INBOARD LOWER CORNER OF SLOT VANE. REPAIRED LEFT WING CENTER L/E INBOARD LOWER CORNER OF SLOT VANE IAW EO DC8- 5720-7767-A.
Part: SKIN — CORRODED (LT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING CENTER L/E LOWER OUTBOARD. EXTERIOR SKIN GOUGED AND CORRODED AT CORNER SCREW HOLES. REPAIRED LT WING CENTER L/E LOWER OUTBOARD. EXTERIOR SKIN IAW EO DC8-5720- -A AND SRM 57-03-03-0 FIG 005.
Part: RIB — CRACKED (LWS 362) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING CENTER LE UPPER RIB CRACKED XFS 362. REPAIRED LT WING CENTER LE UPPER RIB AT XFS 362 PER SRM 57-02 00-0 FIG 002 AND SRM 57-03-03-0 FIG 005.
Part: RIB — CRACKED (LWS 350) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING CENTER LE UPPER RIB CRACKED XFS 350. REPAIRED LT WING CENTER LE UPPER RIB AT XFS 350 IAW SRM 57-02-00 FIG 0 02 AND SRM 57-03-03-0 FIG 005.
Part: FRAME — CRACKED (LT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING CENTER LE 3 INCH CRACK IN FRAME ABOVE PNEUMATIC DUCT XFS 410. REPAIRED LT WING CENTER LE AND FABRICATED INTERCOSTAL AND INSTALLED AT XFS 410 IAW DWG 57-69-589, SRM 51-01-21 AND SRM 51-01-20D.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 CABIN STA 1470 RBL46 SEAT TRACK PLUG GOUGED. REMOVED AND REPLACED SEAT TRACK PLUG AT STA 1470 AND RBL46 IAW SRM 51-03-00.
Part: VANE — DAMAGED (LT SLOT) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING CENTER LE, OUTBD END OF SLOT VANE HAS FRETTING WEAR. REPAIRED LT WING CENTER LE OUTBD END OF SLOT VANE IAW SRM 51-1-21, SRM 51-01-08, SRM 51-03-01.
Part: FITTING — CRACKED (STUB WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3, 2 CRACKED REINFORCEMENT PLATES IN NR 2 STUB WING AT SLOT ACTUATOR. REPLACED LEFT WING INBOARD SLOT ACTUATOR ATTACH FITTING IAW MM 27-80-01-2 AND SRM 51-03-00-0.
Part: ANGLE — GOUGED (LT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LEFT WING CENTER L/E OUTBOARD UPPER Z-ANGLE GOUGED AND HAS 2 EA OVERSIZED HOLES. REPAIRED LEFT WING CENTER L/E OUTBOARD Z-ANGLE IAW DWG 5769857, SRM 57-02-00-0 FIG 2A AND SRM 57-02-00 FIG 007.
Part: RIB — CRACKED (LT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING OUTBD LE UPPER RIB CRACKED JUST INBD OF ACCESS PNL 519B AT XFS 641. REPAIRED RT WING LE UPPER RIB AT XFS 641 IAW SRM 57-03-03-0 FIG 006 AND SRM 57-02-00-0 FIG 002.
Part: RIB — CRACKED (LWS 747) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING OUTBD LE UPPER RIB CRACKED JUST OUTBD OF ACCESS PNL 518C XFS 747.5. REPAIRED LT WING OUTBD LE UPPER RIB AT XFS 747.5 IAW SRM 57-02-00 FIG 002 AND DWG 5769470-27.
Part: SKIN — CRACKED (LH WING LE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING OUTBD LE 5 CRACKS AT 3 SCREW HOLES XFS 603.75 TO XFS 606.75 UPPER SURFACE INBD END, EXTERIOR SKIN. REPAIRED LT WING OUTBD LE EXTERIOR SKIN FROM XFS 603.75 TO XFS 606.75 IAW SRM 57-02-01-0 FIG 038 AND SRM 57-02-01-0.
Part: RIB — CRACKED (LT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING LE OUTBD UPPER RIB CRACKED JUST OUTBD OF ACCESS PNL 520A AT XFS 603.0. REPAIRED LT WING LE OUTBD UPPER RIB AT XFS 603.0 IAW SRM 57-02-00-0 FIG 002 AND SRM 57-03-03 FIG 006.
Part: DOOR — CRACKED (ACCESSORY BAY) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 AFT ACCESSORY COMPT DOOR (STA 1540) HAS CRACK ON CENTER AREA. REPAIRED AFT ACC COMPT DOOR IAW EO DC8-5350-7876-A.
Part: RIB — CRACKED (LT WING) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING OUTBD LE UPPER RIB CRACKED JUST ABOVE ACCESS PNL 519B XFS 653. REPAIRED RT WING LE UPPER RIB AT XFS 653 IAW SRM 57-02-00-0 FIG 002 AND SRM 57-03-03-0 FIG 006.
Part: SKIN — WORN (TE FLAP) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 DOUBLER LOOSE, WORN AND NUMEROUS SCREWS PULLING THROUGH ALONG BOTTOM EDGE OF LEFT OUTBOARD FLAP L/E BETWEEN 219 AND 340. REPAIRED BOTTOM EDGE OF OUTBOARD FLAP L/E AT STA 219 AND 340 IAW SRM 57-07 -01-0, SRM 57-02-00-0 FIG 002, SRM 57-01-08 AND SRM 51-01-21.
Part: RIB — CRACKED (LWS 816) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING OUTBD LE UPPER RIB CRACKED JUST OUTBD OF ACCESS PNL 518A XFS816.0. REPAIRED LT WING OUTBD LE UPPER RIB AT XFS816.0 IAW SRM 57-02-00 FIG 0 02 AND DWG 5769470-37.
Part: RIB — CRACKED (RWS 785) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RT WING OUTBD, L/E UPPER RIB CRACKED JUST OUTBD OF ACCESS PNL 518 B XFS785.0. REPAIRED LT WING OUTBD LE UPPER RIB AT XFS785.0 IAW SRM 57-02-0 FIG 0 02 AND DWG 5769470.
Part: RIB — CRACKED (LWS 822) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 LT WING OUTBD LE UPPER RIB CRACKED JUST OUTBD OF ACCESS PNL 517B AT XFS 822.5. REPAIRED LT WING OUTBD LE UPPER RIB AT XFS 822.5 IAW SRM 57-02-00 FIG0 02 AND DWG 5769470.
Part: GUSSET — CORRODED (SUBFLOOR) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 A/C COMPARTMENT AT SUBFLOOR CEILING STA 60 APPROX RBL 45 GUSSET AT BOTTOM OF FLOORBEAM HAS MODERATE CORROSION. FABRICATED AND REPLACED FLOORBEAM GUSSET AT STA 60 AND RBL 45 IAW SRM 51-1-8, SRM 53-02-00-0 FIG 001F AND DWG 5641543.
Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 COCKPIT OBSERVER SEAT AFT SEAT TRACK HAS ELONGATED HOLE. REMOVED AND REPLACED 2ND OBSERVERS AFT SEAT TRACK IAW SRM 51-03-00 AND SRM 51-01-24.
Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 COCKPIT FIRST OFFICERS LT AFT SEAT TRACK HAS ELONGATED HOLES. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-3-1, 51-1-20D, 51-1-8, 51 -1-24.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 COCKPIT STA 32 OBSERVERS SEAT FWD SEAT TRACK HAS ELONGATED HOLES. REPLACED 2ND OBSERVERS FWD SEAT TRACK IAW SRM 51-01-02 AND SRM 51-03-00.
Part: SEAT TRACK — WORN (COCKPIT) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 STOP HOLES WORN, ROUNDED ON PILOTS LOWER SEAT TRACKS. REMOVED AND REPLACED LOWER SEAT TRACKS IAW SRM 51-3-1, 51-1-20D, 51-1- 24, 51-1-8.
Part: SEAT TRACK — WORN (COCKPIT) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 BOTH FLOOR SEAT TRACKS WORN FOR F/E'S SEAT. REPLACED FWD AND AFT SEAT TRACKS IAW SRM 51-01-24 AND 51-03-00.
Part: SKIN — DENTED (FUSELAGE) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 RIGHT FUSELAGE DENT IN SKIN FS 176.5 AND L26R. REPAIRED RIGHT FUSELAGE DENT AT FS 176.5 AND L26R IAW EO DC8-5330-26529D.
Part: WEB — DENTED (CARGO DOOR) · airframe 77,966 hrs · 25,330 cycles
INSPECTION TYPE:C3 PIT 31 DOOR DENTED IN AREA OF UPPER HANDHOLD. REPAIRED PIT 31 DOOR IAW SRM 51-1-21, SRM 52-02-0 FIG 002 AND SRM 52-4-02 FIG 1A.
Earlier reports · 1995–2007 · 319 reports
2007
Part: BULB — INTERMITTENT (EMERGENCY LIGHT)
EMERGENCY EXIT LIGHTS DISARM IS INTERMITTENT. RELAMPED LIGHT BULB ON EMERGENCY EXIT LIGHT BULB IAW 33-10-00. OPS CHECKS GOOD.
Part: BATTERY PACK — DISCHARGED (COCKPIT)
INSPECTION TYPE:N/A EMERGENCY BATTERY PACK INOP. REPLACED EMERGENCY BATTERY PACK. OPS CHECKED NORMAL.
Part: BATTERY PACK — MALFUNCTIONED (COCKPIT)
INSPECTION TYPE:N/A BTB - EMERGENCY LIGHTS ILLUMINATED IN THE ARMED POSITION WITH A/C POWER ON. MAINTENANCE WILL REPLACE THE BATTERY/RELAY PACK ASSY AS A PRECAUTIONARY. ORDERED ON REQ A927417. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33-00-01-2.
Part: LIGHT — MALFUNCTIONED (COCKPIT)
INSPECTION TYPE:N/A BTB - AFTER TAXI, DIMMING LIGHTS NOTICED THAT EMERGENCY EXIT LIGHTING WAS ILLUMINATED IN THE ARMED POSITION WITH A/C POWER ON AIRCRAFT. RESET C/B. OPS CHECK NORMAL PER AMM 33-50-01-2.
Part: LIGHT — MALFUNCTIONED (CABIN)
INSPECTION TYPE:N/A BTB - AFTER TAXI DIMMING LIGHTS NOTICED THAT EMERGENCY EXIT LIGHTING WAS ILLUMINATED IN THE ARMED POSITION WITH A/C POWER ON AIRCRAFT. RESET C/B. OPS CHECK NORMAL PER AMM 33-50-01-2.
Part: BRAKE ASSY — BROKEN (NR 6 WHEEL)
INSPECTION TYPE:N/A BTB 20:10Z REASON FOR BTB IS BLOWN TIRE ON T/O ROLL. PERFORMED REJECTED TAKEOFF. FOUND NR 6 WHEEL ASSY BROKEN (RIM). REPLACED NR 6 BRAKE ASSY AND WHEEL ASSY PER MM 32-42-01-4 AND MM 32-40-01-2. NO OTHER DAMAGE FOUND.
2006
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW DC8 AMM 33-50-01-2, OPS CHECKS NORMAL P/N ON/OFF 5708458-503/60-1223-5.
Part: SLIDING WINDOW — LACK OF LUBE (COCKPIT)
CAPTAIN'S SLIDING WINDOW WILL NOT OPEN, IT IS BINDING ON TOP AND BOTTOM. LUBED CAPTAIN'S SLIDING WINDOW. OPS CHECK GOOD REF DC-8 MM CH 56-10- 03-5.
Part: WINDOW — STUCK (COCKPIT)
CAPT'S WINDOW WILL NOT OPEN. REMOVED PIECE OF DEBRIS FROM UPPER TRACK, LUBRICATED WINDOW. OPS CK GOOD. OK FOR SERVICE.
Part: HINGE — LACK OF LUBE (COCKPIT WINDOW)
CAPTAIN'S SLIDING WINDOW WILL NOT OPEN. LUBED UPPER WINDOW HINGE. SYSTEM GROUND CHECKED GOOD.
Part: LIGHT — INOPERATIVE (COCKPIT)
INSPECTION TYPE: NA EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01, NO HELP. FOUND TERMINAL END SHORTED AND WIRE L619GA22. EMERGENCY LIGHT OPS TEST GOOD IAW MM 33-50-01.
Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS)
INSPECTION TYPE:N/A ON PRE-DEPARTURE CHECK FOUND EMERGENCY EXIT LIGHTS WEAK. REMOVED AND REPLACED EXIT LIGHT BATTERY PACK. TESTS OK.
Part: CUSP WEB — CRACKED (FS 370-470 L21R) · airframe 77,074 hrs · 24,643 cycles
INSPECTION TYPE:C1 CUSP CORRODED AT STA 440 L21R AND POSSIBLE CRACK. HFEC INSP FOUND 1 INCH CRACK. CUT OUT DAMAGED AREA OF CUSP AT STA 370 - 479 IAW SRM 53-02-05-0 FIG 015A. INSTALLED CUSP SEGMENT AT STA 370 - 470 L21R IAW SRM 53-02-05-0 FIG 015.
Part: LONGERON — CRACKED (FS1690 L25R) · airframe 77,074 hrs · 24,643 cycles
FOUND LONGERON END FITTING CRACKED AT STA 1690 L25L. REMOVED AND REPLACED END FITTING AT STA 1690 L25L IAW SRM 51-1-20D.
Part: FITTING — CORRODED (FS 300 L34L) · airframe 77,074 hrs · 24,643 cycles
INSPECTION TYPE:C1 CORROSION BELOW A-PIT DOOR AT FS 300 L34L (BATH TUB FITTING). REMOVED BATHTUB FITTING. FABRICATED REPAIR ANGLES AND INSTALLED WITH REPLACEMENT FITTING IAW SRM 51-1-20D, 53-02-00 FIG 1F.
Part: FITTING — CRACKED (FUSELAGE) · airframe 77,074 hrs · 24,643 cycles
FOUND INTERCOSTAL TO FRAME ATTACH FITTINGS CRACKED AT STA 1220 L19R. REMOVED 2 FITTINGS AT STA 1220 L19R IAW SRM 51-1-20D. REPLACED 2 FITTINGS AT STA 1220 L19R IAW SRM 51-01-20D.
Part: DOUBLER — CRACKED (RT WING) · airframe 77,074 hrs · 24,643 cycles
INSPECTION TYPE:C1 RT WING L/E REPAIR DOUBLER CRACKED ABOVE NR 4 PYLON. REMOVED, FABRICATED AND INSTALLED DOUBLER AND INTERNAL DOUBLER IAW SRM 51-1-20D, 57-02-01A AND 51-1-26.
Part: LONGERON SPLICE — CRACKED (FS 1590 L12R) · airframe 77,074 hrs · 24,643 cycles
FOUND LONGERON SPLICE SECTION CRACKED AT FASTENER HOLE STA 1590 L12R. REMOVED AND REPLACED LONGERON SPLICE SECTION AT STA 1590 L12R IAW SRM 51-3-2 AND DWG 3773511-REV-A.
Part: LONGERON — CORRODED (FS250-290 L35R) · airframe 77,074 hrs · 24,643 cycles
INSPECTION TYPE:C1 L35R FROM FS 260 - 280 HAS COROSION. REMOVED, FABRICATED AND INSTALLED L35R IAW SRM 53-02-02-0, 51-1-20D, AND 51-1-21.
Part: LONGERON — CRACKED (FS 857 L4L) · airframe 77,074 hrs · 24,643 cycles
FOUND LONGERON END FITTING CRACKED STA 857 L4L. REMOVED AND REPLACED END FITTING AT STA 857 L4L IAW SRM 51-01-20 AND SRM 51-01-23-0.
Part: LONGERON — CORRODED (FS1655-1690 L23L) · airframe 77,074 hrs · 24,643 cycles
FOUND LONGERON 23L HAS CORROSION BETWEEN STA 1660-1665. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0 FIG 1F. CUT OUT DAMAGED AREA OF LONGERON AT STA 1655 TO 1690 L23L IAW SRM 51-1-21. FABRICATED AND INSTALLED LONGERON SPLICE SECTION AT STA 1655 TO 1690 L23L IAW SRM 53-2-2 AND 51-1-21.
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 77,074 hrs · 24,643 cycles
FWD ACCESSORY COMPT FS 660 RT SIDE OF KEEL BEAM TO FRAME ATTACH FITTING CRACKED IN INBD FLANGE LWR RADIUS. REMOVED FITTING FROM RT SIDE OF KEEL BEAM AT FS 660 FWD ACCESSORY COMPT IAW SRM 51-1-20D. LOCATED, DRILLED AND INSTALLED NEW FITTING AT STA 660 IAW SRM 51-1-20D, AND DWG 3750497U1.
Part: DOOR FRAME — CRACKED (MAIN CARGO DOOR) · airframe 770,074 hrs · 24,643 cycles
INSPECTION TYPE:C1 HFEC INSP DETECTED A .25 INCH CRACK ON THE LWR AFT CORNER OF THE MAIN DOOR JAMB. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER IAW SRM 51-1-26 AND EO DC8-5330-14483B.
Part: LONGERON — CRACKED (FS 902 L6L) · airframe 77,074 hrs · 24,643 cycles
FOUND LONGERON END FITIING CRACKED AT STA 902 L6L. REMOVED AND REPLACED END FITTING AT STA 902 L6L IAW SRM 51-01-21-0 AND SRM 51-01-23-0.
Part: BULKHEAD — CRACKED (FS 1766 L12L) · airframe 77,074 hrs · 24,643 cycles
INSPECTION TYPE:C1 AFT PRESS BULKHEAD CRACKED AT STA 1766 L12L SIDE. CUT OUT DAMAGED AREA IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED -25, -27 DOUBLERS, -9,-11, AND -19 FILLERS IAW SRM 53-2-5 FIG 14A 51-1-21, AND 51-1-20D THIS REPAIR REQUIRES MPI IAW TR SRM 53-2-5 FIG 14A, MPI NR ISSUED 18678.
Part: LONGERON — CRACKED (FS1746 L15R) · airframe 77,074 hrs · 24,643 cycles
INSPECTION TYPE:C1 LONGERON CRACKED AT STA 1746 L15R. REMOVED CRACKED LONGERON AT STA 1742-1766 L15R IAW SRM 53-01-21-0 FIG 10. FABRICATED AND INSTALLED LONGERON SPLICE SECTION AT STA 1742-1766 L15R IAW SRM 53-05-03-0 AND 53-02-02-0 FIG 10.
Part: SEAT TRACK — GOUGED (FS 40-160) · airframe 77,074 hrs · 24,643 cycles
FOUND GOUGE IN SEAT TRACK AT FS 70 LBL45 IN MAIN CARGO DECK. REMOVED DAMAGED SEAT TRACK AT STA 45 TO 160 IAW SRM 53-02-03 FIG 012. FABRICATED AND INSTALLED SEAT TRACK AT STA 40 TO 160 LBL 45 IAW SRM 53-2-3 AND SRM 51-3-0.
Part: LONGERON — CORRODED (FS1570-1690 L11R) · airframe 77,074 hrs · 24,643 cycles
INSPECTION TYPE:C1 RIGHT AFT SERVICE DOOR, AT UPPER TORQUE BOX ABOVE JAMB INSIDE TORQUE BOX HAS AREA OF MODERATE CORROSION. REMOVED, FABRICATED AND INSTALLED L11R PER DWG 3773512, SRM 51-1-21 AND 51-1-20D.
Part: SKIN — CRACKED (LT WING) · airframe 77,074 hrs · 24,643 cycles
INSPECTION TYPE:C1 LT UPPER WING SKIN CRACKED 1/2" LONG AT STA XCW 69.5 REAR SPAR UPPER SKIN. FABRICATED AND INSTALLED REPAIR -3 FILLER AND -5/-7 DOUBLERS LT UPPER WING SKIN AT XCW 69.5 IAW SRM 57-02-01-0, SAA EA 008-5710- A0314 DTD 2 AUG2006 AND UPS EO DC8 5730-24823A DTD 2 AUG 2006.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 77,074 hrs · 24,643 cycles
INSPECTION TYPE:C1 REMOVED STEEL DOUBLER FROM C-4 (D PIT) LWR CORNER AND REPAIRED IAW SRM 53-2-0 FIG 21 AND/OR DWG SRO8530019. REPAIRED SKIN CUT OUT IAW SAA EA 008-5330-01-A0288 AND UPS EO DC8- 5330-24691-A.
Part: SKIN — CRACKED (RT WING) · airframe 77,074 hrs · 24,643 cycles
INSPECTION TYPE:C1 RT UPPER WING SKIN CRACKED 1.5" LONG AT STA XCW 69.5 REAR SPAR SPAR UPPER SKIN. FABRICATED AND INSTALLED REPAIR -4 FILLER,-8 TRIPLER, AND -6 DOUBLER RT WING UPPER SKIN AT XCW 69.5 IAW SRM 57-02-01-0,SAA EA 008-5710-01-A0314 DTD 02 AUG 2006,AND UPS EO DC8 5730-24823-A DTD 02 AUG- 2006.
2005
Part: SPAR — CRACKED (LT WING XW736.5) · airframe 76,878 hrs · 24,497 cycles
INSPECTION TYPE:SV LT WING REAR SPAR UPPER CAP AFT FLANGE IS CRACKED APPROX. 7".(XW736.5). REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SAA SK 894-928513.
Part: SKIN — DAMAGED (LT WING)
LT UPPER WING PANEL AT T/E IN FRONT OF NR 4 SPOILER HAS SKIN ROLLED UP APPROX 18 - 24 INCHES ALONG AFT EDGE W/APPROX 30 RIVETS PULLED. ROLLED APPX 1.5 - 2 INCHES FWD AT DEEPEST SPOT. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR DOUBLER & ANGLE & SEAL PER EO DC8-5720-22601A. CK'D SPOILER OPERATION PER MM 27-61-01-2. CK'D OK. A/C OK FOR RETURN TO SERVICE.
Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)
ESCAPE SLIDE BOTTLE PRESSURE 2000 LBS. REMOVED AND REPLACED ESCAPE SLIDE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)
EMERGENCY LIGHTS INOP. RELAMPED, OPS CHECK GOOD.
2004
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER MM 25-60.
Part: SKIN — CRACKED (FUSELAGE) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, FUSELAGE SKIN CRACKED AT RIGHT AFT HEAT EXCHANGER CUTOUT STA -12, L27R. REPAIRED PER UPS EO 5330-4732D.
Part: FITTING — CORRODED (AFT LOWER CARGO) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, STATION 1200 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755841 AND SRM 53-2-0 FIG 2D.
Part: LONGERON — CRACKED (AFT FUSELAGE) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE:C2 STATION 1766 LONG 17R AND END FITTING ARE CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON AND END FITTING IAW DWG 5649327, 4772397 AND SRM 51-1-20D, 520D, 51-1-21.
Part: FITTING — CORRODED (LT WING) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE:C2 LEFT WING FLAP HINGE 98 CANOE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 5614372 AND M/M 27-51-12.
Part: FITTING — CRACKED (FUSELAGE) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE:C2 STATION 600-620 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.
Part: FITTING — CRACKED (AFT LOWER CARGO) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, STATION 1210 AFT T-BOLT BACKUP FITTINGS FWD AND AFT SIDES ARE CRACKED AT LONG 33R. REMOVED AND REPLACED FITTINGS IAW DWG 5894282 AND SRM 51-1-20D.
Part: SKIN — CRACKED (FUSELAGE) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE:C2, LEFT AFT HEAT EXCHANGER LOUVER OPENING LOWER AFT CORNER SKIN IS CRACKED AT STATION -12 AT LONG 27L. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EO DC8-5330-4732-D.
Part: FITTING — CRACKED (FUSELAGE) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, LONG 17 AND END FITTING CRACKED AT STA 1766 LT. REMOVED L17L AND END FITTING AT STA 1766-1790 (APPROX) REF SRM 51-1-21 & 51-1-20D. FABRICATED L17 FROM S1616757 EXTRUSION REF DWG 5649327. INSTALLED REPLACEMENT L17 AND NEW 4772397U1 FITTING REF SRM 51-1-21 & 51-1-20D.
Part: ATTACH ANGLE — CRACKED (WING TO BODY) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE:C2 FUSELAGE FWD CENTER SPAR FRAME TO WING ATTACH ANGLE CRACKED AT STA 759 RBL 50. REMOVED CRACKED ANGLE REF SRM 51-1-20D. FABRICATED REPLACEMENT ANGLE REF DAC DWG 3643110. INSTALLED ANGLE PER SRM 51-1-20D.
Part: ATTACH FITTING — CRACKED (FLOORBEAM) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, FLOORBEAM ATTACH FITTING IS CRACKED AT STA 781 LBL 24. REMOVED AND REPLACED FITTING IAW DWG 3755222 AND SRM 51-1-20D, 51-3-0.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, LOWER FLOORBEAM ANGLE IS CRACKED AT STATION 759 AT RBL 50. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 3643110, AND SRM 51-1-20D.
Part: FITTING — CRACKED (BOOST PUMP) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE:C2, NR 1 ALT TANK BOOST PUMP FITTING IS CRACKED AT STRINGER 58 BETWEEN XRS 463-XRS428. REMOVED AND REPLACED FITTING IAW DWG 3645611 AND SRM 51-1-20D.
Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STATION 960-980 LBL 63. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5645332 AND SRM 53-7-3 FIG 4, 51-1-20D.
Part: BRACKET — CRACKED (BOOST PUMP) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE:C2 BOOST PUMP BRACKET IS CRACKED IN NR 4 ALT BETWEEN XRS 463-XRS 428, ON STRINGER 58 AND 59. REMOVED AND REPLACED BRACKET IAW DWG 3645611 AND SRM 51-1-20D AND DWG 3645612.
Part: FITTING — CRACKED (FUSELAGE) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, STATION 1220 VERTICLE FRAME FITTING AT LONG 27R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9754024 AND SRM 51-1-21, 51-1-20D.
Part: FITTING — CRACKED (FUSLEAGE) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, LOWER CUSP FITTING CRACKED IN B-PIT TUNNEL, RIGHT SIDE, STA 560 (FRAME TO BEAM ATTACH FITTING). REMOVED CRACKED FITTING REF SRM 51-1-20D. FABRICATED REPLACEMENT FITTING PER DAC DWG 3773479. INSTALLED FITTING PER SRM 51-1-20D, 51-3-0, 51-1-8.
Part: LONGERON — CRACKED (AFT LOWER CARGO) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE:C2 STATION 1260-1280 LONGERON 35R IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 1270-1290, FABRICATED AND INSTALLED REPAIR DOUBLERS, CHANNELS, STRAP AND LONGERON SEGMENT IAW UPS ENGINEERING FILE NUMBER DC8-53-20422 AND SAA SK 894-477.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C3, STATION 1260-1280 LONG 34L IS CRACKED. REMOVED AND REPLACED LONGERON SECTION BETWEEN STATION 1270 TO 1350 IAW SRM 53-2-2 FIG 10.
Part: FITTING — CRACKED (FUSELAGE) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT 1240 AFT SIDE AT LONG 33R. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D.
Part: FITTING — CRACKED (FUSELAGE) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE:C2, C-PIT FWD DOOR JAMB FITTING CRACKED. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-21 AND 51-3-2.
Part: FITTING — CRACKED (CARGO DOOR FRAME) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE:C2, C-PIT DOOR FRAME LOWER FWD LATCH BACKUP FITTING AT STATION 1168 LONG 34R APPROX IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754930, AND SRM 51-1-20D.
Part: FITTING — CRACKED (BULKHEAD) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, STATION 1766 AFT SIDE OF BULKHEAD, FITTING TO THE LEFT OF UPPER TAIL SKID FITTING IS CRACKED AT BOTTOM J FRAME AND BULKHEAD. REMOVED AND REPLACED FITTING IAW DWG 3753645 AND SRM 51-1-20D.
Part: FITTING — CRACKED (AFT LOWER CARGO) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE:C2 STATION 1220 BANANA FITTING IS CRACKED AT LONG 34R. REMOVED AND REPLACED FITTING IAW DWG 3755847, SRM 51-1-20D, 51-3-0.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,297 hrs · 24,032 cycles
INSPECTION TYPE: C2, LONG 12 LT CRACKED AT STA 1746. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONG SECTION FROM STA 1740 TO 1766 & INSTALLED SPLICE FITTING IAW SRM 53-2-2 FIG 11.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,297 hrs · 24,032 cycles
INSPECTION TYPE:C2 STA 1756, LONG 14 LT CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONG SECTION FROM STA 1746 TO STA 1766. INSTALLED SPLICE FITTING AND STRAPS IAW SRM 53-2-2 FIG 10.
Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, LEFT HORIZONTAL STAB LEADING EDGE UPPER SKIN IS CORRODED XFS 272.5. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55-2-1 FIG 4.
Part: DOUBLER — DAMAGED (HORIZONTAL STAB) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE:C2 RIGHT UPPER HORIZONTAL STAB LEADING EDGE HAS ELONGATED HOLES BETWEEN XFS 47.5 TO XFS 110.0. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AND INTERNAL DOUBLER IAW DWG 5644330 AND SRM 55-2-1 FIG 4.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, LEFT HORIZONTAL STAB UPPER RIB IS CRACKED AT XFS 47.5. REMOVED AND REPLACED ANGLE IAW DWG 5654549 AND SRM 51-1-20D.
Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE:C2 LEFT HORIZONTAL STAB L/E IS CORRODED AT XFS 178.5. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS OR CORROSION AT CUTOUT, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 55-2-1 FIG 4.
Part: FRAME — CRACKED (AC COMPARTMENT) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, STATION 55 FRAME IS CRACKED AT LONG 24L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER AND SPLICES IAW SRM 53-2-0 FIG 2.
Part: FRAME — CRACKED (AC COMPARTMENT) · airframe 76,292 hrs · 24,032 cycles
INSPECTION TYPE: C2, STATION 55 FRAME IS CRACKED AT LONG 24R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER AND REPAIR SPLICES IAW SRM 53-2-0 FIG 2.
2003
Part: ENGINE — FLAMED OUT (NR 1)
ENGINE NR 1 FLAMED OUT AT 30,000 FT DUE TO FUEL STARVATION. DID INFLIGHT ENGINE RESTART. ENGINE WINDMILLED FOR ABOUT 2 MINUTES. OK FOR SERVICE IAW AMM 71-00-00-5 PARAGRAPH 6B ABNORMAL OPERATION. NO DEFECTS NOTED.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)
INSPECTION TYPE: ASV, EMERGENCY LIGHTS WILL NOT TEST. FOUND EMERGENCY LIGHT BATTERY DEAD. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-01, OP CHECK GOOD.
2002
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:N/A DURING BITE CHECK, EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. RECYCLED BREAKER AND CHECK AGAIN. EMERGENCY LIGHTS DID NOT ILLUMINATE SECOND TIME. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER MM 33-50-01 OPS CHECK GOOD.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,501 hrs · 23,446 cycles
INSPECTION TYPE:SP ANGLE IS CRACKED ON COCKPIT SUBFLOOR STA -100 AT RBL 32. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5616101, AND SRM 51-1-20D.
Part: FITTING — CRACKED (FUSELAGE) · airframe 75,501 hrs · 23,446 cycles
INSPECTION TYPE: SP STA. 934 FITTING IS CRACKED CENTERLINE BETWEEN MAIN GEAR DOORS REMOVED AND REPLACED FITTING I.A.W. DWG. 4646309,AND SRM. 51-1-20D
Part: FITTING — CRACKED (MGL WW) · airframe 75,501 hrs · 23,446 cycles
INSPECTION TYPE:SPV R/H WHEEL WELL TRAP FITTING CRACKED AT FWD LWR BOLT HOLES,AT STA 855 RT. REMOVED STIFFNER, HFEC INSPECTED, VERIFIED TWO EACH CRACKS IN LWR TRAP FITTING, STOP DRILLED CRACKS I.A.W E.O. DC8-57-20059, AND SK 894-566,CRACKS TERMINATE AT STOP DRILL I.A.W HFEC INSP.NDTSPM 06- 10-01.001, FABRICTED REPAIR ANGLE AND STIFFNER I.A.W SK894-566. INSTALLED REPAIR PARTS PER SRM 57-2-7, AND SK 894-566 AT ST 855-R
Part: FITTING — CRACKED (FUSELAGE) · airframe 75,501 hrs · 23,446 cycles
INSPECTION TYPE:SP STA 910 FITTING IS CRACKED CENTER LINE BETWEEN MAIN GEAR DOORS. REMOVED AND REPLACED FITTING IAW DWG 5616306 AND SRM 51-1-20D.
Part: FITTING — CRACKED (FUSELAGE) · airframe 75,501 hrs · 23,446 cycles
INSPECTION TYPE:SP STA 944 FITTING IS CRACKED CENTER LINE BETWEEN MAIN GEAR DOORS. REMOVED AND REPLACED FITTING IAW DWG 4645516, AND SRM 51-1-20D.
Part: FITTING — CRACKED (FUSELAGE) · airframe 75,501 hrs · 23,446 cycles
INSPECTION TYPE: SP STA. 954 FITTING IS CRACKED CENTERLINE BETWEEN MAIN GEAR DOORS REMOVED AND REPLACED FITTING I.A.W. DWG. 4645516,AND SRM.51-1-20D
Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)
INSPECTION TYPE:N/A LOWER CARGO COMPARTMENT FIRE LIGHT CAME ON FOR ONE MINUTE THEN WENT OUT FWD B ON DISPLAY PANEL. PERFORM OPS CK TO LOWER CARGO SMOKE DETECTOR IAW DC-8 MM 26-18-01 ADJ &TEST OK TO CONTINUE NO FAULTS FOUND.
Part: PRESSURE PANEL — CRACKED (FUSELAGE)
INSPECTION TYPE:N/A LEFT WHEEL WELL AFT FLAP ENCLOSURE, WEB ASSY ON AFT PORTION WHERE ACT RETRACTS IS CRACKED IN UPPER RADIUS. LOCATED & DRILLED NEW WEB FABRICATED NEW STIFFENER FOR SPOILER A PULLEY BRACKET ON I/B WEB PANEL, FABRICATED PER DC-8 SRM 51 W 18126. INSTALLED NEW WEB & STIFFENER PER DC8 SRM 51-1-21
Part: ANGLE — CRACKED (FUSELAGE)
INSPECTION TYPE:N/A VERTICAL ANGLE CRACKED LT MLG WHEEL WELL. LOCATED & DRILLED NEW ANGLE WA 18126. INSTALLED PER DC-8 SRM 51-1-20 & 51-1-21.
Part: ANGLE — CRACKED (FUSELAGE)
INSPECTION TYPE:N/A UPPER INBD ANGLE CRACKED LT MLG WW. REMOVED ANGLE SENT TO MANUFACTURING WP 70050 LOCATED AND DRILLED NEW ANGLE W/CREF 18126 9-5-02 INSTALLED PER DC8 SRM 51-1-20 & 51-1-21.
Part: FITTING — CRACKED (RH WING ROOT)
CRACK IN STEEL STRAP UNDER R/T ADF PNL. MILLED STEEL STRAP UNDER RT ADF (FWD) PANEL CRACKED AT STA 82.7 WHERE WING MEETS CENTER TANK BUT T L7ORT VERIFIED WITH EDDY CURRENT (SKI FITTING). R&R'D FITTING IAW DWG J060095 SRM 51-1-20D, 51-1-21,51-3-0 & 53-1-0. C/W WITH D244478.REF N/R 591533.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED TEST BATTERY & RELAY UNIT MM 33-50-01.
2001
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT COME ON WHEN ACTIVATED. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK PER DC8 MM 33-50-01. OPS OK.
Part: WINDOW — OUT OF ADJ (COCKPIT)
INSPECTION TYPE:N/A, F/O SLIDING WINDOW WOULD NOT OPEN. ADJUSTED WINDOW.
Part: BATTERY PACK — DISCHARGED (COCKPIT)
INSPECTION TYPE:IN, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK ASSEMBLY. CHECKED GOOD.
2000
Part: CIRCUIT BREAKER — FAILED (EMERGENCY LIGHTS)
INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS C/B WILL NOT RESET. *S/D* REMOVED AND REPLACED EMERGENCY EXIT LIGHT CIRCUIT BREAKER IAW DC8 MM 20-50-02.
Part: BATTERY PACK — INOPERATIVE (CABIN)
INSPECTION TYPE:N/A, AIRCRAFT EMERGENCY LIGHTING INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-30-01. OPERATED ALL LIGHTS AND WORKED PROPERLY.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, ''Z'' ANGLE CORRODED AND MISDRILLED AND HAS LOOSE RIVETS BETWEEN STA 25 AND 8 AND 10 RBL. REMOVED DAMAGED ''Z'' ANGLE, FABBED NEW ''Z'' ANGLE IAW DC8 DWG 54616573 & REO G07339. INSTALLED IAW DC8 SRM 51-1-20D.
Part: SKIN — CRACKED (CARGO DOOR) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, C-PIT DOOR LOWER CENTER SKIN CRACKED AND PEELED BACK. REMOVED DAMAGED AREA, FLATTENED OUT BEND. FABRICATED DOUBLER, ALODINED AND PRIMED THE SKIN AND THE DOUBLER, APPLIED SEALANT AND INSTALLED THE DOUBLER USING HI-LOK''S AND A CHERRY MAX.
Part: SKIN — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, RT FUSELAGE EXTERNAL SKIN AT STA 902 HAS INTERGRANULAR CORROSION BELOW CUSP LINE ADJACENT TO SKIN SPLICE. BLENDED OUT AREA IAW REO-G07351. ALODINED AND PRIMED IAW DC8 SRM 51-1 -8. INSTALLED FAST IAW DAC DWG 5750554 & DC8 SRM 51-1-20D & 51-9-0.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, SEAT TRACK ''I'' CORRODED ON BOTTOM SIDE, STA 1380 - 1540. REMOVED SEAT TRACK, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. FABRICATED AND INSTALLED NEW SEAT TRACK AT STA 1380 - 1540 WITH TWO SPLICES PER UPS EO REF DC8 5320-5167 AND DC8 SRM 51-1-24.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, AFT PIT C-3 DOOR AFT FRAME SECTION CRACKED. REMOVED SEAL RETAINER FOR FOM, FABRICATED REPAIR ANGLES IAW DC8 SRM 52- 2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES IAW DC8 SRM 52-2-0, INSTALLED HIGH-SHEAR FASTENERS IAW DC8 SRM 51-1-2 0A.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, SEAT TRACK B AT STA 1060 - 1330 HAS CORROSION UNDER O/B FLANGE. REMOVED CORROSION IAW DC8 SRM 53-2-0, FOUND OUT OF LIMITS. REMOVED DAMAGED SECTION OF TRACK, LOCATED AND DRILLED NEW SECTION IAW DC8 SRM 51-1-24. FABBED SPLICES IAW UPS EO 5320-8309. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAT TRACK SECTIONS AND SPLICES IAW UPS EO 5320-8309 & DC8 SRM 51-3-0. INSTALLED FLOOR PANEL IAW DC8 SRM 51-3-0 & 51-1-14.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, AFT PIT FS 1000 - 1020 INTERCOSTAL AT L35L CORRODED. REMOVED DAMAGED INTERCOSTAL FOR FOM. FABRICATED NEW INTERCOSTAL IAW DOUGLAS DWG NR 5779929, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, CORROSION ON INTERCOSTAL FS 1040 AT L35L. REMOVED DAMAGED INTERCOSTAL FOR FOM. FABRICATED NEW INTERCOSTAL IAW DOUGLAS DWG NR 779929, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, SEAT TRACK G SCALLOPS GOUGED BETWEEN STA 160 & STA 180. BLENDED GOUGES, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED SEAT TRACK STA 130 - 180 IAW DC8 SRM 51-3-0. LOCATED, DRILLED AND DEBURRED SEAT TRACK AND SPLICE FITTING IAW DC8 ADDUNDUM DC8-5320-5167-C. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SEAT TRACK AND FITTING IAW DC8 SRM 51-3-0.
Part: ATTACH FITTING — CORRODED (RT MLG WW) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, RIGHT W/W UPPER FWD PRESSURE WEB ATTACH FITTING IS CORRODED AND CRACKED AT HORIZONTAL PRESSURE WEB STA XCW-46-0 AND STA 857. REMOVED FS 857 BULKHEAD RT PRESSURE DOOR DRILLED UP NEW FITTING. REMOVED AND REINSTALLED FUEL DUMP DRUM FOR ACCESS. INSTALLED NEW FITTING. REINSTALLED RT PRESS DOOR RIGGED FUEL DUMP SYS ALL IAW DC8 MM 28-30- 00 & DC8 SRM 51-3-0, 51-3-2 & 51-1-20. FOR FINAL SEE OPS TASK CARD NR 142284.
Part: DOOR FRAME — CRACKED (LT MLG) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, LEFT MLG W/W DOOR CUTOUT FWD I/B FRAME HAS CRACK STA 886.0 UNDER KEEL BEAM. REMOVED CRACKED FRAME IAW DC8 SRM 51-3-2. MAT ID 7075.T6.063 IAW DAC DWG 5616306. FAB FRAME IAW DAC DWG 5616306 & DC8 SRM 51-3-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FRAME IAW DC8 SRM 51-1 -21 & DAC DWG 5616306.
Part: FRAME — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, FWD LWR PIT BETWEEN STA 280 TO 300 BETWEEN LONGERON 35R TO 34R CORRODED AT FRAME 280. REMOVED FASTENERS, FITTING, AND CORROSION. CORROSION ON FITTING OUT OF LIMITS. FAB SPLICE AND DRILLED NEW FITTING IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SPLICE AND FITTING IAW DC8 SRM 51-1-21.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, SEAT TRACK ''B'' IS WORN AND GOUGED FROM FS 610 - 850; OUT OF LIMITS RT & LT FS 620. ROUTED OUT DAMAGE RT & LT FS 620 WHERE THE TRACK WAS OUT OF LIMITS. INSTALLED 4 HOLE PLUG AND 4 HOLE CHANNEL IAW DC8 SRM 53-2-2, 53-2-3, 51-1-8 & 51-3-0.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, SEAT TRACK ''F'' IS WORN, GOUGED AND HAS BARE METAL STA 810 - 1010. BLENDED GOUGES STA 810 - 920. REMOVED AND REPLACED TRACK STA 970 - 1010 IAW DC8 SRM 53-2-3 & UPS EO DC8 5320-5167C. ALODINED AND PRIMED IAW DC 8 SRM 51-1-8.
Part: DOOR FRAME — CRACKED (RT MLG) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, RIGHT MLG W/W DOOR CUTOUT FWD I/B FRAME HAS CRACK STA 886.0 UNDER KEEL BEAM. REMOVED CRACKED FRAME IAW DC8 SRM 51-3-2. MAT ID 7075T6.063 IAW DAC DWG 5616306. FABRICATED FRAME IAW DAC DWG 5616306, HEAT TREATED FRAME FROM 0 TO T6 IAW DAC DWG 5616306 & TPS-1003 REV A. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FRAME IAW DC8 SRM 51-1-21 & DAC DWG 5616306.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, CORROSION ON INTERCOSTAL FS 1040 AT L35L. REMOVED DAMAGED INTERCOSTAL FOR FOM. FABRICATED NEW INTERCOSTAL IAW DOUGLAS DWG NR 5779929, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, CORROSION ON LINER SUPPORT ATTACH ANGLE STA 1440 - 1540 L33L. REMOVED CORRODED SUPPORT ANGLE, FABRICATED NEW ANGLE, ALODINED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21 & DOUGLAS DRAWING NR 9 759432.
Part: FRAME — CRACKED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, CRACK IN RADIUS OF PIT FRAME REPAIR AT FS 420 EXTENDING FROM LONG 25 TO 29 RT. FABBED PIT FRAME IAW DC8 DWG NR 3773159. HEAT TREAT IAW DC8 DWG NR 3773159. LOCATED AND DRILLED TRIM TO FIT IAW DC8 SRM 51-3-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21.
Part: FRAME — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, FRAME FS 80, L36 AFT SIDE CORRODED. REMOVED CORROSION FROM FRAME STA 80, L36 AND FOUND TO BE OUT OF LIMITS . FABRICATED AND INSTALLED REPAIR ANGLE, FILLER, AND DOUBLER IAW STD-53 10-082.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, CORROSION ON LINER SUPPORT ATTACH ANGLE STA 1440 - 1540 L33L. REMOVED CORRODED SUPPORT ANGLE. FABRICATED NEW ANGLE, ALODINED, PRIMED & INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21 & DOUGLAS DRAWING NR 9 759432.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, CORROSION ON FLOOR LINER SUPPORT ATTACH ANGLE BETWEEN STA 1400 - 1420 AND L33L. REMOVED CORROSION AND FOUND TO BE OUT OF LIMIT. REMOVED CORRODED SECTION OF ANGLE, FABRICATED NEW SECTION, ALODINED, PRIMED AND INSTALLED IAW DOUGLAS DRAWING NR 9759432, DC8 SRM 51-1-8 & 51-1-21.
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, KEEL BEAM RT SIDE, STA 792 FITTING IS GOUGED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0, 51-1-20D & 51-1-16.
Part: WEB — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, CORROSION INSIDE TORQUE BOX FS 280 BETWEEN LONGERONS 32R & 31R. REMOVED FITTING AND WEB AT STA 280. FABBED NEW WEB, FITTING AND WEB SPLICES IAW DC8 SRM 53-2-0 & DAC DWG 5772787. HEAT TREATED WEB IAW TPS-1003. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED WEB, FITTING AND WEB SPLICES IAW DC8 SRM 51-1-21.
Part: FITTING — CRACKED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, AFT ACCESSORY COMPARTMENT, LONGERON 35R, END FITTING IS CRACKED, STA 1610. REMOVED AND REPLACED FITTING, (P/N 4646403) IAW DC8 SRM 51-1-20D.
Part: FITTING — CRACKED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, AFT ACCESSORY COMPARTMENT LONGERON 35L END FITTING IS CRACKED STA 1610. REMOVED THE PLACED FITTING (P/N 4646403) IAW DC8 SRM 51-7-20D.
Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, T-ANGLE ATTACH BRACKET AND RIB AT STA 802 RRL 40 CORRODED. REMOVED 3641315-502 FITTING. REMOVED CORRODED DOUBLER. FAB NEW DOUBLER IAW DAC DWG 5773275. REMOVED CORROSION FROM WEB IAW DC8 SRM 51-1-8, WITHIN LIMITS IAW DC8 SRM 53-2-0. REMOVED CORROSION FROM 3641315-502, OUT OF LIMITS. LOCATED AND DRILLED NEW 3641315-502 FITTING IAW DC8 51-1-24. INSTALLED NEW DOUBLER, ATTACH ANGLE, AND FITTING IAW DC8 SRM 51-1-21 & 51-1-20D.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, CORROSION ON L28L STA 1170, LWR AFT PIT. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW DC8 SRM 51-1-8, AREA OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 53-2-2 & 51-20D. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.
Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, CABIN, ELONGATED HOLE IN FLOORBEAM AT STA 834 RBL 13. ROUTED OUT DAMAGED AREA IAW TIMCO SRM STD 5310-001 PG 6 AND MID FOR 2 REPAIR ANGLES IS 7075-0 .071 PO NR 297242 IAW TIMCO STD REPAIR MANUAL 5310-001 PG 4 & 6. FABBED 2 ANGLES AND FILLER IAW TIMCO STD REPAIR MANUAL 5310-001. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC 8 SRM 51-1-20D & REO G07360.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, CORROSION ON L28L STA 1170, LWR AFT PIT. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW DC8 SRM 51-1-8. AREA OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED REPAIR ANGLE IAW DC8 SRM 53-2-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLE IAW DC8 SRM 51-20D.
Part: FRAME — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, AFT PIT FS 1060 CORROSION ON LWR SURFACE OF UPPER FRAME FLANGE AT L36 AND L33L. REMOVED FRAME CAP, REMOVED CORROSION, AND FOUND TO BE OUT OF LIMIT. CUT OUT DAMAGED AREA OF FRAME IAW UPS EO DC8 5310-11728A. FABBED REPAIR DOUBLERS, FILLERS, STRAPS, ALODINED AND PRIMED AND INSTALLED REPAIR DOUBLERS, STRAPS, FILLERS AND FRAME CAP IAW DC8 SRM 51-1-21, 51-1-20D, 51-1-8 & UPS EO DC8 5310-11728A.
Part: FRAME — CORRODED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, AFT PIT FS 1060 CORROSION ON LWR SURFACE OF UPPER FRAME FLANGE AT L36 AND L33L. REMOVED FRAME CAP, REMOVED CORROSION & FOUND OUT OF LIMIT, CUT OUT DAMAGE AREA OF FRAME IAW UPS EO DC8 5310-11728A. FABRICATED REPAIR DOUBLERS, FILLERS, STRAPS, ALODINED, PRIMED & INSTALLED REPAIR DOUBLERS, STRAPS, FILLER, FRAME CAP IAW DC8 SRM 51-1-21, 51-1-20D, 51-1-8 & UPS EO DC8 5310-11728A.
Part: FRAME — MISDRILLED (FUSELAGE) · airframe 73,733 hrs · 22,388 cycles
INSPECTION TYPE:C2, AFT PIT FS 1040 DOUBLE DRILL HOLES AT L34L AND CORROSION ON LOWER SURFACE OF UPPER FRAME FLANGE AT L36. FRAME AND FRAME CAP OUT OF LIMITS. REMOVED FRAME FROM CUSP TO CUSP, FRAME CAP, FRAME DOUBLER ANGLE, RT SUPPORT STANTION, AND RT FLOORBEAM END FITTING. RECEIVED NEW FRAME AND FRAME CAP, LOCATED AND DRILLED. REPAIRED 2 AREAS OF FRAME SUPPORT ANGLE. INSTALLED FRAME, FRAME CAP, DOUBLER, RT FLOORBEAM END FITTING AND RT FLOOR SUPPORT STANTION.
1999
Part: BATTERY — DISCHARGED (CABIN)
EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LTS BATTERY PACK IAW MM33-50-01. SYS OPS CHECKS NORMAL P/N ON 60-1223-5 OFF 5708458-503 S/N ON 219 S/N OFF 2045.
Part: BATTERY PACK — DISCHARGED (CABIN)
WHILE PERFORMING EMERGENCY EXIT LIGHT TEST FOUND LIGHTS VERY DIM. REMOVED AND REPLACED BATT PACK. SYSTEM OPS CHECK GOOD PER MM 35-52-0.
1998
Part: TRACK — CRACKED (CARGO COMPT)
INSPECTION TYPE-C, A PIT CROSS SLIDE DOOR JAMB TORQUE BOX UPPER WEB TRACK BETWEEN STR 36 AND 32R IS CRACKED. REMOVED AND REPLACED TRACK IAW SRM 51-3-0.
Part: SEAT TRACK — CORRODED (BS 950-1010)
INSPECTION TYPE-C, SEAT TRACK AT STA 950 TO 1010 RBL 44 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW DC8-5320-8309-C.
Part: RIB — CRACKED (WS 672.5)
INSPECTION TYPE-C, RT WING L/E RIB AT FS 672.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.
Part: RIB — CRACKED (WS 616.25)
INSPECTION TYPE-C, RT WING L/E RIB AT XFS 616.25 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG.
Part: RIB — CRACKED (WS 772.5)
INSPECTION TYPE-C, L/E RIB CRACKED XFS 772.5 LT WING. REPAIRED IAW SRM 57-2-0.
Part: RIB — CRACKED (WS 803.75)
INSPECTION TYPE-C, LT WING L/E RIB CRACKED XFS 803.750 UPPER. REPAIRED IAW SRM 57-2-0.
Part: RIB — CRACKED (WS 722.5)
INSPECTION TYPE:C LT WING L/E RIB CRACKED XFS 722.500. REPAIRED IAW SRM 57-2-0.
Part: RIB — CRACKED (WS 728.75)
INSPECTION TYPE:C LT WING L/E RIB CRACKED XFS 728.750. REPAIRED IAW SRM 57-2-0.
Part: RIB — CRACKED (WS 810)
INSPECTION TYPE-C, LT WING L/E RIB CRACKED XFS 810 UPPER. REPAIRED IAW SRM 57-2-0.
Part: RIB — CRACKED (WS 816.25)
INSPECTION TYPE-C, LT WING L/E RIB CRACKED XFS 816.250 UPPER. REPAIRED IAW SRM 57-2-0.
Part: RIB — CRACKED (WS 635)
INSPECTION TYPE:C LT WING L/E RIB CRACKED XFS 635.00. REPAIRED IAW SRM 57-2-0.
Part: RIB — CRACKED (WS 628.75)
INSPECTION TYPE:C LT WING L/E UPPER RIB CRACKED AT XFS 628.75. REPAIRED IAW SRM 57-2-0.
Part: RIB — CRACKED (WS 785)
INSPECTION TYPE-C, L/E RIB CRACKED LT XFS785 UPPER RIB LT WING. REPAIRED IAW SRM 57-2-0.
Part: RIB — CRACKED (WS 622.5)
INSPECTION TYPE-C, RT WING L/E RIB AT XFS 622.5 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACKED AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.
Part: RIB — CRACKED (WS 778.75)
INSPECTION TYPE-C, RT WING L/E RIB AT XFS 778.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0.
Part: RIB — CRACKED (WS 616.25)
INSPECTION TYPE-C, LT WING L/E RIB AT XFS 616.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.
Part: RIB — CRACKED (WS 610)
INSPECTION TYPE:C LT WING UPPER L/E RIB CRACKED XFS 610.00. REPAIRED IAW SRM 57-2-0.
Part: RIB — CRACKED (WS 835)
INSPECTION TYPE-C, LT WING L/E RIB CRACKED UPPER XFS 835. REPAIRED IAW SRM 57-2-0.
Part: RIB — CRACKED (WS 660)
INSPECTION TYPE-C3, RT WING L/E RIB AT XFS 660.0 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.
Part: RIB — CRACKED (WS 741.25)
INSPECTION TYPE:C LT WING L/E RIB CRACKED XFS 741.25. REPAIRED IAW SRM 57-2-0.
Part: SKIN — CRACKED (BS 55)
INSPECTION TYPE-C, LT FUSELAGE SKIN AT STA 55 AT STR 21R IS CRACKED AT THE DOUBLER. REPAIRED IAW DC8-5330-0793-I.
Part: SKIN — CRACKED (WS 433)
INSPECTION TYPE-C, RT WING L/E UPPER SKIN AT THE SPAR AT XS 433 HAS INTERGRANULAR CORROSION AND IS CRACKED. REPAIRED IAW SRM 57-2-1.
Part: SKIN — CRACKED (WS 485)
INSPECTION TYPE-C, RT WING L/E UPPER SKIN AT XW 485 IS CRACKED IN 3 PLACES. REPAIRED IAW SRM 57-2-1.
Part: SKIN — CRACKED (WS 210)
INSPECTION TYPE-C, RT WING L/E UPPER SKIN AT XFS 210 CRACKED. REPAIRED IAW SRM 57-2-0.
Part: BATTERY PACK — DISCHARGED (CABIN)
INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY BATT PACK, SYSTEM OPS CHECK OK.
1997
Part: STIFFENER — CORRODED (BS 8)
INSPECTION TYPE:D, VERTICAL STIFFENER AFT SIDE OF F/S 8 ABOVE LONGERON 28R EXFOLIATED. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-3-1 FIG 3, 51-1-8, 52-2-0 FIG 2, AND 51-1-20.
Part: FRAME — DAMAGED (BS 380)
INSPECTION TYPE:D, 2 HOLES IN FRAME F/S 380 AT LONGERON 11R. REPAIRED PER DHC SK-894-561 (REF ENRG FILE NR DC8-53-1820A).
Part: FRAME — DRILL MARKS (BS 280)
INSPECTION TYPE:D, 3 DRILL START BLEND OUTS ON FRAME F/S 280 I/B FLANGE WENT BEYOND ALLOWABLE LIMITS BETWEEN LONGERONS 19R AND 20R (REF N/R 535529). FABRICATED AND INSTALLED REPAIR PARTS IAW DHC SK-894-529 AND SRM 51-1-20 (REF UPS ENRG FILE NR DC8-53-1819).
Part: FLOORBEAM — CORRODED (BS 902)
INSPECTION TYPE:D, MAIN CABIN FLOORBEAM F/S 902 LBL 48 FWD LOWER FLANGE CORRODED BEYOND LIMITS REF N/R 535880. FABRICATED AND INSTALLED TWO SPLICES AND REPAIR IAW DHC SK 894-763A.
Part: FITTING — CRACKED (BS 1150)
INSPECTION TYPE:D, FITTING CRACKED AT F/S 1150 BETWEEN LONGERONS 33R AND 31R. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 3755847.
Part: LONGERON — CRACKED (BS 260)
INSPECTION TYPE:D, LONGERON 35L CRACKED AT F/S 260. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DWG 9754913, SRM 53-2-2 FIG 10, 51-1-20D.
Part: SKIN — CORRODED (BS 8)
INSPECTION TYPE:D, F/S 8 CHORD AT LONGERON 30R HAS A DOUBLE DRILLED HOLE AND FUSELAGE SKIN IS CORRODED BEYOND ALLOWABLE LIMITS FROM F/S 10 TO 20 BETWEEN LONGERONS 29R AND 30R REF N/RS 535460 AND 535722. REPAIRED PER DHC SK 894-722 REF UPS ENRG FILE NR DC8-53-1830.
Part: FITTING — CRACKED (BS 1270)
INSPECTION TYPE:D, LONG 31L F/S 1270 PRODUCTION SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-1-0 AND 51-1-21.
Part: INTERCOSTAL — CORRODED (BS 980-1000)
INSPECTION TYPE:D, INTERCOSTAL AT LONGERON 30R F/S 980-1000 IS CORRODED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-20D AND DWG 3644359.
Part: FITTING — CRACKED (FS 280)
INSPECTION TYPE:D, FRAME TO CUSP ATTACH FITTING CRACKED AT F/S 280 LONG 21L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 53-01-0 AND DWG 3773075.
Part: JAMB — CRACKED (BS 270)
INSPECTION TYPE:D, MAIN CARGO DOOR JAMB LOWER AFT SEAL PAN AT F/S 270 IS CRACKED. REMOVED, FABRICATED, AND INSTALLED LOWER AFT SEAL IAW DWG 5772787, AND SRM 51-1-21.
Part: CUSP — CORRODED (BS 1240-1260)
INSPECTION TYPE:D, LEFT CUSP HAS SEVERE CORROSION ON UPPER FLANGE FS 1240 TO 1260. REMOVED DAMAGED SECTION OF CUSP FROM FS 1250-1290, FABRICATED AND INSTALLED REPLACEMENT SECTION, AND SPLICE IAW SRM 53-2-5 FIG 15.
Part: STRINGER — CRACKED (BS 1270)
INSPECTION TYPE:D, STR 35L UPPER OUTBOARD FLANGE HAS A CRACK APPROX .6 LONG AT FS 1270. REMOVED DAMAGED SECTION FROM FS 1270-1290, FABRICATED AND INSTALLED REPLACEMENT SECTION, AND SPLICES IAW SRM 53-2-2 FIG 10, 51-1-20D AND DHC SK-894-978 (REF UPS ENRG FILE NR DC8-53-1815).
Part: LONGERON — CORRODED (BS 1180-1200)
INSPECTION TYPE:D, LONG 33L LWR FLANGE HAS EXFOLIATION CORROSION BETWEEN F/S 1180 TO 1200. FABRICATED AND INSTALLED REPAIR ANGLE IAW DHC SK-894-955 REF UPS ENRG FILE NR DC8-53-1811.
Part: SPLICE — CORRODED (BS 1268-1280)
INSPECTION TYPE:D, FACTORY SPLICE AT LONGERON 35L FS 1260-1280 IS CORRODED ON TOP IN THE CENTER. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE IAW DWG 3759258, SRM 51-1-20D.
Part: SHEAR TIE — CORRODED (BS 1230)
INSPECTION TYPE:D, SHEAR TIE BATH TUB FITTING F/S 1230 LONG 35R TO 36 CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 53-1-0, 51-1-20, 53-2-0, 51-1-8.
Part: FRAME — CORRODED (BS 1260)
INSPECTION TYPE:D, CORROSION REMOVAL WENT OUT OF LIMITS ON THE BOTTOM OF THE FRAME STA 1260 BETWEEN STR 35L AND 36 ( REF. N/R 535920 ). TREATED AND PRIMED AREA IAW SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-2-0.
Part: FITTING — CORRODED (BS 1160)
INSPECTION TYPE:D, FITTING AT F/S 1160 L-34R HAS CORROSION OUT OF LIMITS. REMOVED AND REPLACED FITTING PER SRM 51-1-20.
Part: DOUBLER — CORRODED (C3 CARGO DOOR)
INSPECTION TYPE:D, C-3 CARGO DOOR INTERNAL DOUBLER HAS CORROSION AND OUT OF LIMITS. FABRICATED INTERNAL DOUBLER FROM F/S 1120 TO 1260 BETWEEN STR 35L TO 26R PER DOUG DWG 9754924. DOUBLER INSTALLED ON NR 535897.
Part: PRESSURE PANEL — CORRODED (BS 12)
INSPECTION TYPE:D, F/S -12 NOSE WHEEL WELL PRESURE PANEL RBL 35, CORROSION OUT OF LIMITS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER DHC SK-894-737 (REF UPS ENRG FILE NR DC8-53-1807) AND SRM 51-1-21.
Part: CLIP — CRACKED (BS 1240)
INSPECTION TYPE:D, FRAME TO STR ATTACH CLIP CRACKED AT STR 35R F/S 1240. REMOVED AND REPLACED FITTING IAW SRM 53-1-0 AND 51-1-20.
Part: CLIP — CRACKED (BS 1150)
INSPECTION TYPE:D, FRAME CLIP CRACKED F/S 1150 LONG 35L. REMOVED AND REPLACED CLIP PER SRM 51-1-20D.
Part: SHEAR TIE — CORRODED (BS 1160)
INSPECTION TYPE:D, SHEAR TIE CORRODED F/S 1160 BETWEEN LONG 33L AND 34L. REMOVED AND REPLACED FITTING IAW SRM 53-1-0 AND 51-1-21.
Part: FITTING — CRACKED (BS 1690)
INSPECTION TYPE:D, LONGERON 34L END SPLICE FITTING CRACKED F/S 1690. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.
Part: FITTING — CRACKED (BS 1690)
INSPECTION TYPE-D, LONGERON 36 END FITTING CRACKED FS 1690 FWD SIDE. REMOVED AND REPLACED FITTING IAW SRM 53-1-0 AND 51-1-29D.
Part: SHEAR TIE — CORRODED (BS 1230)
INSPECTION TYPE:D, SHEAR TIE BATH TUB FITTING F/S 1230 LONG 35L TO 36 CRACKED AND CORRODED. REMOVED AND REPLACED FITTING IAW SRM 53-1-0, 51-1-20, 53-2-0 FIG 2D.
Part: FRAME — OPEN HOLE (BS 1340)
INSPECTION TYPE:D, HOLE IN FRAME F/S 1340 AT LONGERON 6R. PLUGGED 2 HOLES IN FRAME, FABRICATED AND INSTALLED REPAIR ANGLE IAW DHC SK-894-629 (REF UPS ENRG FILE NR DC8-53-1796) AND SRM 51-1-20D.
Part: RIB — CRACKED (LT WING)
INSPECTION TYPE-D, LT WING LEADING EDGE BETWEEN NR 1 AND NR 2 PYLONS 7TH RIB FROM THE O/B END IS CRACKED. FABRICATED AND INSTALLED REPAIR IAW SRM 57-2-0, 57-3-3, 51-1-21, AND 51-1-20D.
Part: FRAME — DAMAGED (BS 940)
INSPECTION TYPE:D, FRAME F/S 940 AT LONGERON 12R HAS DEEP DRILL START. REPAIRED IAW DHC SK-894-585 (REF UPS ENRG FILE NR DC8-53-1794).
Part: FITTING — CRACKED (BS 1140)
INSPECTION TYPE:D, F/S 1140 LONG 33R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 53-1-0.
Part: LONGERON — CORRODED (BS 980)
INSPECTION TYPE:D, CORROSION FOUND AT CHORD F/S 980 LONGERON 35L AND 35R. REMOVED CORROSION, REPAIRED IAW DHC SK-894-844 (REF UPS ENRG FILE NR DC8-53-1805).
Part: SEAT TRACK — CORRODED (BS 1548-1560)
INSPECTION TYPE:D, SEAT TRACK CORRODED FROM F/S 1548 TO 1560 BL 0. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS FROM F/S 1530 TO 1610 IAW SRM 51-1-20D, 51-3-0, AND DC8-5320-5167C.
Part: FLOORBEAM — CORRODED (BS 1580)
INSPECTION TYPE:D, F/S 1580 RBL 52-0 FLOORBEAM FWD TAB WAS CORRODED BEYOND LIMITS (REF N/R 535310). REPAIRED IAW DHC SK-894-310A (REF UPS ENRG FILE NR DC8-53-1814).
Part: DOUBLER — CRACKED (NR 3 PYLON)
INSPECTION TYPE:D, NR 3 PYLON TO LWR WING DOUBLER HAS A .75 INCH CRACK AT WING FRONT SPAR LWR CAP 18 INBD OF PYLON. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR PARTS IAW DHC SK-894-812 (REF UPS ENRG FILE NR DC8-57-0781).
Part: LONGERON — CRACKED (BS 240-260)
INSPECTION TYPE:D, LONG 36 BETWEEB F/S 240-260 CRACKED. REMOVED AND REPLACED LONG 36 RT SIDE HALF IAW SRM 53-2-0 FIG1F, AND 51-1-29D.
Part: FITTING — CRACKED (BS 1210)
INSPECTION TYPE-D, FS 1210 RT SIDE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER DWG 3754918 AND SRM 51-1-20.
Part: STRINGER — CORRODED (BS 320-340)
INSPECTION TYPE:D, F/S 320 TO 340 STR 35L IS CORRODED BEYOND LIMITS (REF NR 534887). REMOVED AND REPLACED LONG 35L IAW SRM 53-2-0 FIG 1 AND 51-1-29D.
Part: FRAME — MISS DRILLED (BS 130)
INSPECTION TYPE:D, FUSELAGE FRAME F/S 130 HAS NUMEROUS DOUBLE DRILLED, ENLONGATED, AND HOLES WITH SHORT E.D. (CARGO LINER ATTACH HOLES). REMOVED, FABRICATED AND INSTALLED FRAME IAW SRM 51-1-20 AND DHC SK- 894-514 (REF UPS ENRG FILE NR DC8-53-1790).
Part: DOUBLER — CORRODED (BS 220)
INSPECTION TYPE-D, INTERNAL TITANIUM DOUBLER AT FS 220 TO 260 LONG 31R TO 35L HAS HEAVY CORROSION. FABRICATED, REPLACEMENT DOUBLER PER DOUGLAS DWG 9754011.
Part: DOUBLER — CORRODED (BS 350-450)
INSPECTION TYPE:D, FINGER DOUBLER AT F/S 350 TO 450 LONGERON 31L HAS LIGHT TO HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 53-4-1, 51-1-20, AND 51-10-2.
Part: DOOR FRAME — MISS DRILLED (BS 120-130)
INSPECTION TYPE:D, MAIN CARGO DOOR FRAME WEB F/S 120-130 FWD OF MCD, HAS NUMEROUS DOUBLE DRILLED HOLES ( CARGO LINER ATTACH HOLES ). REMOVED, FABRICATED AND INSTALLED WEB AT STA 120 TO 130 LT BETWEEN STR 8 TO 17 LT IAW SRM 53-4-1, AND 51-1-21.
Part: DOUBLER — CORRODED (BS 190-350)
INSPECTION TYPE:D, FINGER DOUBLER AT F/S 190 TO 350 LONG 31L HAS LIGHT TO HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 51-1-8, 51-1-20D.
Part: FITTING — CRACKED (BS 860)
INSPECTION TYPE-D, INTERCOSTAL END FITTING CRACKED STA 860 LONG 18L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 4750420.
Part: DOUBLER — CRACKED (RT HORIZ STAB)
INSPECTION TYPE-D, RT INBD HORIZONTAL L/E INBD SECTION DOUBLER CRACKED. REMOVED FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND 55-3-1.
Part: FITTING — CORRODED (BS 879.375)
INSPECTION TYPE-D, FUSELAGE FRAME FITTING FS 879.375 SEVERLY CORRODED AT LONGERON 24L IN LT MLG W/W. REMOVED AND REPLACED FITTING PER SRM 53-2-0 FIG 8.
Part: DOUBLER — CORRODED (BS 1050-1115)
INSPECTION TYPE-D, FINGER DOUBLER CORRODED FS 1050 TO 1115 LONGERON 21R. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-4-1 AND 51-1-8.
Part: SUPPORT — CORRODED (BS 140)
INSPECTION TYPE-D, AFTER REMOVAL OF STA 140 STR 27R FLOOR SUPPORT TIE FITTING, THE FLOOR SUPPORT BEAM (P/N 3773077-510) WAS FOUND TO BE CORRODED BEYOND LIMITS PER SRM 53-2-0. FABRICATED, AND INSTALLED NEW STRUT IAW SRM 51-1-20D AND DWG 3773077.
Part: FITTING — CORRODED (BS 1690)
INSPECTION TYPE-D, FS 1690 LONG 32L IS CORRODED, FITTING. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-29D.
Part: FLOORBEAM — CRACKED (BS 920)
INSPECTION TYPE:D, FLOORBEAM F/S 920 CRACKED ON LOWER FLANGE IN RADIUS AT LBL 68. REF UPS N/R 534617. REPAIRED IAW DHC SK-894-617 (REF UPS ENRG FILE NR DC8-53-1806).
Part: DOUBLER — CORRODED (BS 70)
INSPECTION TYPE-D, DOUBLER PLATE FS 70 FROM LONG 27R TO 29R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED DOUBLER PLATE IAW SRM 53-3-3, 51-1-21, AND DWG 3615624.
Part: DOUBLER — CRACKED (WS 246.5-250)
INSPECTION TYPE:D, RT L/E STUB WING AT NR 3 PYLON INTERIOR DOUBLER AND ANGLE CRACKED BETWEEN STA XS 246.5 AND 250. REMOVED AND REPLACED ANGLE SUPPORT AND DOUBLER IAW SRM 51-1-20.
Part: FRAME — DAMAGED (FS 1100)
INSPECTION TYPE:D, FUSELAGE FRAME, STA 1100 HAS 10 LIGHT DRILL STARTS, LT SIDE, AND AT THE BOTTOM HAS 1 HOLE WITH TOO LITTLE EDGE DISTANCE BLENDED DRILL STARTS (9) IAW SRM 53-2-0. PLUGGED ONE DRILL START WITH RIVET IAW SRM 51-1-21. REMOVED DAMAGED Z-FRAME SECTION IAW SRM 53-2-0 FIG 2. FABRICATED AND INSTALLED REPLACEMENT Z-FRAME IAW SRM 53-2-0 FIG 2 AND DHC SK-894-702 (REF UPS ENGR FILE NR DC8-53-1818).
Part: DOUBLER — CORRODED (BS 900)
INSPECTION TYPE-D, DOUBLER HAS CORROSION APPROX FS 900 ABOVE LONG 24 O/B TOP RT MLG WW. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-20, 51-1-20D, 53-2-0.
Part: WEB — MISDRILLED (BS 120-130)
INSPECTION TYPE:D, THE INBD WEB FS 120 TO 130, JUST ABOVE MCD FLOOR HAS 8 LIGHT AND 1 DEEP DRILL STARTS. REMOVED AND REPLACED WEB AT F/S 120 TO 130 LT BETWEEN STRINGER 17L TO 21L IAW DWG 5772878 AND SRM 51-1-20.
Part: FRAME — MISS DRILLED (BS 1240)
INSPECTION TYPE:D, MAIN CABIN BELLFRAME HAS 1 HOLE WITH NO E.D. AND 5 DRILL STARTS FS 1240 L-21L TO L-7L. BLENDED AREAS IAW SRM 53-2-0, FABRICATED AND INSTALLED FRAME AND SPLICES FROM L-18L TO L-21L IAW SRM 53-2-0 AND DHC SK-894-702-1 (REF UPS ENRG FILE NR DC8-53-1818).
Part: DOUBLER — CORRODED (BS 1688)
INSPECTION TYPE:D, F/S 1688 JUST ABOVE LONG 22L THE INTERNAL DOUBLER IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-4-1, 51-1-21, 51-1-20D, 51-1-11, 51-3-1.
Part: RIB — CRACKED (LT WING WING)
INSPECTION TYPE-D, LT WING L/E BETWEEN NR 1 AND NR 2 PYLONS, 10TH RIB FROM INBD END IS CRACKED. FABRICATED AND INSTALLED REPAIR IAW SRM 55-2-0.
Part: FRAME — DRILL MARKS (BS 560)
INSPECTION TYPE:D, 11 EA DRILL STARTS IN FRAME F/S 560 RT SIDE OF CENTER BETWEEN STR 21 AND 6R. BLENDED DRILL STARTS, CUT OUT AREAS (THAT WENT BEYOND LIMITS) AT L-18R TO 21R AND 5R TO 6R AND 8R TO 9R. FABRICATED AND INSTALLED FRAME SEGMENT AND SPLICE ANGLES IAW SRM 53-2-0 FIG 2, 51-1-20D.
Part: FRAME — DAMAGED (BS 1380)
INSPECTION TYPE:D, 1 HOLE IN FRAME F/S 1380 STR 21R. INSTALLED REPAIR IAW DHC SK-894-702 REF UPS ENRG FILE NR DC8-53-1818.
Part: INTERCOSTAL — CRACKED (BS 320-340)
INSPECTION TYPE-D, FUSELAGE INTERCOSTAL FS 320 TO 340 AT LONG-11R IS BENT AND CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PER SRM 53-01-0 AND 51-1-2.
Part: FRAME — CORRODED (BS 240)
INSPECTION TYPE-D, FUSELAGE FRAME 240 AND LONGERON 35L IS EXFOLIATED FWD SIDE OF FRAME. CUT OUT DAMAGE, FABRICATED FRAME SPLICE AND SPLICE FORMER AND INSTALLED IAW SRM 53-2-0 FIG 2 AND 51-1-20D.
Part: CHANNEL — CORRODED (BS 1240)
INSPECTION TYPE-D, T-CHANNEL ON TOP OF LONGERON 35L AFT OF FRAME 1240 IS CORRODED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT CHANNEL PER SRM 53-4-1 AND DWG 9750425 AND SRM 51-1-20.
Part: FITTING — CRACKED (BS 1170)
INSPECTION TYPE-D, FS 1170 RT SIDE FRAME CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754032 AND SRM 51-1-20.
Part: FITTING — CRACKED (BS 1226)
INSPECTION TYPE:D, F/S 1226 RT SIDE CUSP TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED FRAME FITTING IAW SRM 53-1-0, 51-1-20D AND DOUG DWG 3754047.
Part: FITTING — CRACKED (BS 1186)
INSPECTION TYPE:, F/S 1186 RT SIDE CUSP TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-20D, 53-1-0, AND DOUG DWG 3754032.
Part: SKIN — CRACKED (LT WING)
INSPECTION TYPE:D, LT WING L/E (STUB WING) ABOVE NR 1 PYLON HAS AN 8 INCH CRACK ON THE INBOARD UPPER ATTACH FLANGE. STOP DRILLED CRACK AND REINSTALLED EXISTING REPAIR REF SRM 57-2-6 FIG 1, 51-1-21, AND 51-1-20D.
Part: FITTING — CRACKED (BS 1140)
INSPECTION TYPE-D, FS 1140 RT SIDE CUSP TO FRAME FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-1-20D.
Part: BULKHEAD BEAM — CORRODED (BS 1754)
INSPECTION TYPE-D, CORROSION REMOVAL ON AFT PRESSURE BLKHD VERT BEAM AT FS 1754 BL 0 TO LBL 2 IS OUT OF LIMITS AND HAS CRACK AT BOTTOM FASTENER HOLE TO EOP (REF N/R 535205). FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIG 1B, 51-1-20, 51-1-21, AND DHC SK 894-205 (REF UPS ENGR FILE NR DC8-53-1778).
Part: ANGLE — CORRODED (BS 1600)
INSPECTION TYPE-D, LT UPPER CUSP WEB TIE ANGLE HAS SHEARED RIVETS AND LIGHT CORROSION AT FS 1600. CORROSION REMOVAL BEYOND LIMITS. REMOVED DAMAGED TIE, FABRICATED AND INSTALLED REPLACEMENT TIE IAW SRM 51-1-21, AND 51-1-8.
Part: SKIN — CRACKED (BS 1760)
INSPECTION TYPE:D HFEC INSP, CONFIRMS VISUAL CRACK INDICATION F/S 1760 AT 17L. CRACK IS .75 LONG AND EMANATES FROM FASTENER. REPAIRED IAW DHC SK-894-415A (REF UPS ENRG FILE NR DC8-53-1808).
Part: SUPPORT — CORRODED (BS 1745-1751)
INSPECTION TYPE-D, MAIN CABIN FLOOR SUPPORT FS 1745 TO 1751 RBL 10 HAS EXFOLIATION CORROSION. REMOVED FLOOR SUPPORT, FABRICATED, AND INSTALLED REPLACEMENT IAW SRM 51-2-0, DWG 5755032, 51-1-21 AND 51-3-0.
Part: SUPPORT — CORRODED (BS 980)
INSPECTION TYPE:D, F/S 980 AFT SIDE FRAME SUPPORT EXFOLIATED BETWEEN LONG 35L AND 35R. REMOVED FRAME SUPPORT PER SRM 51-1-20D, FABRICATED AND INSTALLED REPLACEMENT FRAME SUPPORT IAW DWG 5751945, SRM 51-1-20D.
Part: SHEAR TIE — CORRODED (BS 55)
INSPECTION TYPE-D, FS 55 FROM LONG 34R TO 34L HAS HEAVY CORROSION, SHEAR TIE. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 53-3-3, 51-1-8 AND 51-1-21.
Part: ANGLE — CRACKED (CTR WING TANK)
INSPECTION TYPE-D, L-ANGLE JUST FWD OF RT W/W ON EXTERIOR OF CENTER WING TANK CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW ANGLE IAW SRM 57-2-0 FIG 1B.
Part: SEAT TRACK — CORRODED (BS 1036)
INSPECTION TYPE:D, SEAT TRACK IS CORRODED FROM STA 1036-1056 LBL24. REMOVED AND REPLACED SEAT TRACK PER UPS EO DC8-5320-5167-C AND SRM 53-7-3.
Part: FITTING — CORRODED (BS 1690)
INSPECTION TYPE:D, FS 1690 AFT SIDE OF FRAME, LONGERON 30L END FITTING CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-8.
Part: FITTING — CORRODED (FS 920)
INSPECTION TYPE:D, FUSELAGE FITTING FS 920 SEVERELY CORRODED AT LONGERON 24L IN LT M/L/G W/W. REMOVED AND REPLACED FITTING PER SRM 53-2-0 FIG 8.
Part: GUSSET — CORRODED (BS 1240)
INSPECTION TYPE:D, FRAME TO LONGERON GUSSET FS 1240 LONG 35R CORRODED. REMOVED, FABRICATED AND INSTALLED REPAIR GUSSET IAW SRM 51-1-20, 51- 1-8, AND 51-1-20D.
Part: FITTING — CRACKED (BS 1180)
INSPECTION TYPE-D, FITTING (P/N 375842-505) IS CRACKED AT STA 1180 ABOVE LONG 28L. REMOVED FITTING, FABRICATED AND INSTALLED REPAIR DOUBLER AND INSTALLED NEW FITTING IAW SRM 51-1-20, 53-2-0 FIG 2D.
Part: FITTING — CORRODED (BS 940)
INSPECTION TYPE:D, FUSELAGE FRAME FITTING FS 940 SEVERELY CORRODED AT LONGERON 24L IN LT MLG W/W. REMOVED AND REPLACED FITTING PER SRM 53-2-0 FIG 8.
Part: FLOOR SUPPORT — CORRODED (BS 1746-1766)
INSPECTION TYPE:D, MAIN CABIN FLOOR SUPPORT HAS MODERATE CORROSION F/S 1746 TO 1766 LBL 30. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SUPPORT IAW SRM 51-3-0, 53-7-3.
Part: SUPPORT — CORRODED (BS 1735)
INSPECTION TYPE-D, FS 1735 BETWEEN LBL 18 AND RBL 18 FLOOR SUPPORT ANGLE IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 51-1-2, 51-1-20D, AND DWG 5755032.
Part: FITTING — CRACKED (BS 1230)
INSPECTION TYPE:D, FITTING CRACKED AFT OF FRAME 1230 O/B OF LONGERON 35L. REMOVED, FABRICATED, AND INSTALLED FITTING IAW SRM 51-1-20, 51-1-20D, AND DOUG DWG 3758570.
Part: SEAT TRACK — CORRODED (BS 1746-1755)
INSPECTION TYPE:D, MAIN CABIN HAS MODERATE CORROSION ON SEAT TRACK STA 1746-1755 AT BL 0. REMOVED, FABRICATED AND INSTALLED U CHANNELS TO SEAT TRACK IAW SRM 51-1-21 AND 53-1-0.
Part: FITTING — CRACKED (BS 1150)
INSPECTION TYPE-D, FITTING UPPER FLANGE CRACKED INBD OF LONG 33R FWD OF FRAME 1150. REMOVED AND REPLACED WITH NEW FITTING IAW SRM 51-1-11 AND 51-1-20D.
Part: FITTING — CORRODED (BS 879)
INSPECTION TYPE-D, FITTING HAS EXFOLIATION CORROSION RT W/W FS 879 ABOVE LONG 24 FWD SIDE. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 8 AND 51-1-20.
Part: STIFFENER — CORROSION (BS 960-980)
INSPECTION TYPE:D, MAIN CABIN SUB FLOOR FS 960-980, LBL 24 PRESSURE PANEL STIFFENER FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-3-0.
Part: FITTING — CORRODED (BS 960)
INSPECTION TYPE:D, MAIN CABIN SUB FLOOR, FS 960-980 LBL 48, PRESURE PANEL STIFFENER FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, AND 51-3-0.
Part: RIB — CRACKED (WS 341.5)
INSPECTION TYPE:D, RT WING L/E SECTION BETWEEN PYLONS STA XFS 341.5 THE LOWER L/E RIB IS CRACKED IN CENTER. FABRICATED AND INSTALLED REPAIR IAW SRM 57-2-0 AND 51-1-20D.
Part: SPLICE — CRACKED (WS 74.8 R)
INSPECTION TYPE-D, NR 3 MAIN STA XRS 74.869 STR 51, THE FWD STRINGER SPLICE IS CRACKED IN 3 PLACES. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-1-20, 51-3-0, 57-1-0.
Part: RIB — CRACKED (RT WING)
INSPECTION TYPE:D, RT WING L/E SECTION BETWEEN PYLONS HAS 4 UPPER L/E RIBS CRACKED AT THE AFT END. FABRICATED AND INSTALLED REPAIR PART PER SRM 57-2-0 FIG 2 AND 57-3-3.
Part: DOUBLER — CORRODED (BS 900-920)
INSPECTION TYPE:D, FS 900-920 RBL 59-65 FINGER DOUBLER HAS CORROSION THROUGHOUT. REMOVED, FABRICATED, AND INSTALLED FINGER DOUBLER PER SRM 53-4-1 AND 51-1-21 AND DWG 5645332.
Part: CUSP — CORRODED (BS 1316-1320)
INSPECTION TYPE:D, LT CUSP LOWER SIDE EXFOLIATED F/S 1316 TO 1320. REMOVED DAMAGED SECTION FROM FS 1290-1370, FABRICATED AND INSTALLED REPLACEMENT SECTION, DOUBLERS, AND SPLICES IAW SRM 53-2-5 FIG 15, 51-1-20D, 51-1-11.
Part: RIB — CRACKED (WS 250.08)
INSPECTION TYPE:D, LEFT WING L/E SECTION OVER NR 3 PYLON, L/E RIB IS CRACKED, AT LWR END JUST OB OF STA XS 250.089. FABRICATED AND INSTALLED REPAIR IAW SRM 57-2-0.
Part: FITTING — CORRODED (BS 680)
INSPECTION TYPE:D, SUB FLOOR, AT FS 680 LBL 6, HAS CORROSION REMOVAL OUT OF LIMITS. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 10 AND 51-1-20.
Part: DOUBLER — CORRODED (BS 1460)
INSPECTION TYPE:D, LONGERON 31L FINGER DOUBLER EXFOLIATED, FS 1460-1480. REMOVED, FABRICATED, AND INSTALLED FINGER DOUBLER REPAIR IAW SRM 51- 1-21, 51-1-8, 51-1-20, AND 51-1-20D.
Part: DOUBLER — CORRODED (BS 920-940)
INSPECTION TYPE:D, MAIN CABIN SUB FLOOR, FS 920-940 RBL 3 TO LBL3, FINGER DOUBLER IS BULDGING WITH CORROSION ON UNDERSIDE AND HAS 1 SHEARED RIVET. REMOVED, FABRICATED, AND INSTALLED FINGER DOUBLER PER SRM 53-4-1 AND 51-1-20.
Part: DOUBLER — CRACKED (WS 250.089)
INSPECTION TYPE:D, L/WING IB SLOT FRAME DOUBLER CRACKED, BETWEEN STA XS 246.519 AND XS 250.089. REMOVED SKIN PER SRM 51-1-20. FABRICATED DOUBLER PER SRM 57-3-0 AND INSTALLED DOUBLER AND SKIN PER SRM 51-1-20 AND 51-1-21.
Part: SPLICE — CRACKED (BS 380-400)
INSPECTION TYPE:D, LONGERON 31L SPLICE BETWEEN FS 380-400 CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20.
Part: FRAME — CORRODED (BS 1080)
INSPECTION TYPE:D, F/S 1080 FRAME WEB FWD SIDE EXFOLIATED OUTBOARD OF LONG 35R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIG1F, 51-1-29D, AND 51-1-21.
Part: SPLICE — CRACKED (BS 1050)
INSPECTION TYPE-D, LONG 31R SPLICE FITTING CRACKED FS 1050. REMOVED AND INSTALLED REPLACEMENT FITTING PER SRM 51-1-20D.
Part: STRINGER — CORRODED (BS 100-140)
INSPECTION TYPE:D, FS 100-140 STR 36 HAS SEVERE CORROSION. REMOVED, FABRICATED, AND INSTALLED LONG IAW SRM 53-2-2 FIG 10, 51-1-20, 53-2-0, AND 51-1-8.
Part: FITTING — CORRODED (BS 70)
INSPECTION TYPE-D, FS 70 AFT SIDE, STR 34R END FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0, 51-3-1.
Part: SHEAR TIE — CORRODED (BS 280)
INSPECTION TYPE-D, FS 280 BTWN STR 34L AND 35L SKIN AND SHEAR TIE FITTING HAVE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, SKIN REPLACED ON N/R 534855.
Part: GUSSET — CORROSION (BS 220)
INSPECTION TYPE:D, FLOORBEAM TO FRAME TIE GUSSET HAS SEVERE CORROSION AT FS 220 STR 27R. FABRICATED AND INSTALLED REPLACEMENT GUSSET IAW SRM 53-4-3, 51-1-8, AND 51-1-20.
Part: FRAME — CORRODED (BS 420)
INSPECTION TYPE-D, FRAME CORRODED AT STA 420, LONGERON 35L. REMOVED CORROSION AND DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0 FIG 2, 51-1-8.
Part: FITTING — CORRODED (BS 960)
INSPECTION TYPE-D, EXFOLIATION CORROSION ON AFT SIDE OF FRAME FITTING FS 960 LT WW O/B AFT ABOVE LONG 24. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 8 AND 51-1-20.
Part: GUSSET — CORRODED (BS 140)
INSPECTION TYPE-D, FS 140 AT STR 27R FLOOR SUPPORT TIE FITTING TO FRAME HAS SEVERE CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT GUSSET IAW SRM 53-1-0.
Part: CUSP — CORRODED (BS 1154)
INSPECTION TYPE-D, FUSELAGE LT CUSP BOTTOM SIDE EXFOLIATED FS 1154. REMOVED CUSP FROM FS 1130 TO 1170, FABRICATED AND INSTALLED REPAIR PART AND DOUBLERS IAW SRM 53-2-5 FIG 15, 51-1-20D. CUT AND SPLICED FRAME FS 1140 LT IAW SRM 53-2-0 FIG 2.
Part: INTERCOSTAL — CORRODED (BS 980)
INSPECTION TYPE:D, INTERCOSTAL EXFOLIATED AFT OF FRAME 980 AT LONG 35L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-4-1 AND 51-1-20D.
Part: STRINGER — CORROSION (BS 140-148)
INSPECTION TYPE:D, FS 140-148 STR 36 IS CRACKED IN 2 PLACES DUE TO CORROSION. REMOVED, FABRICATED, AND INSTALLED LONGERON SECTION W/SPLICE FROM FS 130-150 IAW SRM 51-1-20, 53-2-2 FIG 10, 53-2-0, AND 51-1-8.
Part: FITTING — CRACKED (BS 153)
INSPECTION TYPE-D, FS 153 AT RT CUSP TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
Part: FRAME — CRACKED (BS 117)
INSPECTION TYPE:D, FUSELAGE FRAME AT F/S 117, JUST BELOW AND FWD OF THE CENTER WINDSHIELD RT POST IS CRACKED IN THE OUTBD FLANGE RADIUS. THE CRACK IS APPROX .8 LONG. STOP DRILLED CRACK, INSTALLED REPAIR ANGLES IAW SRM 51-1-20D, 51-1-21 51-1-8, AND 51-1-11.
Part: INTERCOSTAL — EXFOLIATED (BS 998)
INSPECTION TYPE:D, F/S 998 LONG 27R INTERCOSTAL EXFOLIATED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 53-1-0, 51-1-20, AND DWG 5640915.
Part: CUSP — CORRODED (BS 320-350)
INSPECTION TYPE:D F/S 320-350 LT CUSP LOWER SURFACE HAS HEAVY CORROSION. REMOVED DAMAGED SECTION F/S 330 TO 370, FABRICATED AND INSTALLED REPAIR SECTION IAW SRM 53-2-5 FIG 15, 53-2-0 FIG 2, 51-1-20.
Part: INTERCOSTAL — CORRODED (BS 1100-1120)
INSPECTION TYPE:D, UPPER AND LOWER FLANGES OF INTERCOSTAL CORRODED AT FS 1100 TO 1120 LONGERON 33R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-21, 51-1-20D AND 51-1-30.
Part: FRAME — CORROSION (BS 500)
INSPECTION TYPE:D, FRAME FWD SURFACE HAS MODERATE CORROSION AT FS 500 ABOVE LONGERON 32R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PART IAW SRM 51-1-8, 53-2-0, 51-1-20.
Part: FITTING — CORRODED (BS 70)
INSPECTION TYPE:D, FS 70 AFT SIDE STR 25R END FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 53-1-0, 51-1-21, 51-1-20D, AND 51-3-0.
Part: FITTING — CORRODED (BS 1200)
INSPECTION TYPE-D, FLOORBEAM END FITTING ABOVE C-3 DOOR FS 1200 EXFOLIATED. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D.
Part: FRAME — CORRODED (BS 1050)
INSPECTION TYPE-D, FRAME CAP FS 1050 AFT LOWER SIDE EXFOLIATED AT 2 NUT PLATES BETWEEN LONG 36 AND 35L. REMOVED DAMAGE, FABRICATED AND INSTALLED ANGLE AND STRAP IAW SRM 53-2-0, AND 51-1-20.
Part: LONGERON — CRACKED (BS 1656)
INSPECTION TYPE:D, F/S 1656 LONGERON 33R IS CRACKED AT ATTACH FITTING. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21, 53-2-2 FIG 10 AND 51-1-20.
Part: SKIN — CORRODED (BS 220-270)
INSPECTION TYPE:D, F/S 220-270 BETWEEN STR 31L-31R SKIN AND INTERNAL DOUBLER HAVE NUMEROUS AREAS OF MODERATE CORROSION. REMOVED AND REPLACED SKIN FS 190-450 LONG 31L TO 31R PER UPS E.O. DC8-5330-7427-B, SRM 51-1-29D, 51-1-21, 51-3-0, AND 51-1-11.
Part: PIN — CRACKED (LT MLG)
INSPECTION TYPE:D, ULTRASONIC INSPECTION DETECTED A CRACK ON THE MAIN LANDING GEAR BOGIE PIVOT PIN. REMOVED AND REPLACED BOGIE PIVOT PIN IAW M/M 32-11-05.
Part: ANGLE — CORRODED (BS 1340)
INSPECTION TYPE-D, FS 1340 RT SIDE AT FLOOR LEVEL DOOR JAMB TIE ANGLE HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED DOOR ANGLE IAW SRM 53-4-3, 51-1-21.
Part: FRAME — CORRODED (BS 940)
INSPECTION TYPE-D, FS 940 FRAME LT SIDE BELOW FLOOR HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED FRAME SECTION IAW DHC SK-894-614, REF UPS ENRG FILE NR DC8-53-1771, SRM 51-1-20, 53-2-0.
Part: FITTING — CRACKED (BS 902)
INSPECTION TYPE:D, FS 902 FWD SIDE AT STR 18R - INTERCOSTAL TIE FITTING CRACKED. REMOVED, FABRICATED, AND INSTALLED FITTING IAW SRM 51-1-20, 53-1-0, AND DOUGLAS DWG 4750423.
Part: FRAME — CORROSION (BS 940)
INSPECTION TYPE:D, FS 940 FRAME RT SIDE BELOW FLOOR HAS HEAVY CORROSION AT BOTTOM. REMOVED AND REPLACED FRAME IAW DOUG DWG 5751966 AND SRM 53-1-0, 51-1-1, 51-1-20, AND DHC SK-894-616 REF UPS ENRG FILE NR DC8-53- 1772.
Part: CHANNEL WEB — CORRODED (BS 1740)
INSPECTION TYPE-D, MAIN DECK FLOOR CHANNEL AND WEB BETWEEN LBL 7 TO 20 FS 1740 HAS MODERATE CORROSION ON UPPER AND LOWER SURFACE. REMOVED FLOOR CHANNEL AND WEB AND COLLAR PLATE, FABRICATED REPLACEMENT PARTS PER SRM 53-1-0 AND INSTALLED PARTS IAW SRM 51-1-21, 53-1-0.
Part: FITTING — CORRODED (BS 895)
INSPECTION TYPE:D, FS 895 TIE ANGLE TO FRAME AND SKIN HAS HEAVY CORROSION LEFT SIDE BELOW FLOOR. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
Part: FITTING — CORRODED (BS 857)
INSPECTION TYPE:D, FS 857 FWD SIDE AT STR 19R, 2 INTERCOSTAL ATTACH FITTINGS ARE CRACKED AND 1 CORRODED. REMOVED, FABRICATED, AND INSTALLED ATTACH FITTINGS IAW DOUG DWG 4750423, SRM 53-1-0, 53-2-0 FIG 1F, 51-1-8, AND 51-1-20. (1 FITTING WITHIN LIMITS)
Part: CUSP — CORRODED (BS 1152)
INSPECTION TYPE:D, F/S 1152 RT CUSP ANGLE HAS HEAVY CORROSION EXTENDING UNDER FRAME FITTING. REMOVED DAMAGED SECTION OF CUSP FS 1180-1250, FABRICATED AND INSTALLED RELACEMENT SECTION OF CUSP, DOUBLERS, AND SPLICE IAW SRM 53-2-5 FIG 15A, 51-1-21D. (WORKED WIYH N/R 534806)
Part: INTERCOSTAL — CRACKED (BS 857)
INSPECTION TYPE:D, FS 857 AFT SIDE AT STR 19R, INTERCOSTAL TIE FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DOUG DWG 4750423, SRM 53-1-0, 51-1-8, 51-1-20.
Part: ANGLE — CORRODED (BS 902)
INSPECTION TYPE-D, FS 902 RBL 59 TO 63 FRAME TO FUSELAGE TIE ANGLE HAS HEAVY CORROSION BELOW FLOOR AFT SIDE. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
Part: ANGLE — CRACKED (HORIZ STAB)
INSPECTION TYPE-D, LT HORZ STAB L/E REPAIR ANGLE CRACKED AT STA FXS53.7. REMOVED, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 55-2-0 AND 51-1-20D.
Part: SPLICE — CRACKED (BS 440-460)
INSPECTION TYPE:D, FS 440-460 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED IAW SRM 51-1-20D.
Part: SKIN — CORRODED (BS 1690-1700)
INSPECTION TYPE:D, FS 1690-1700 BETWEEN STR 30R-32R, SKIN INTERNALLY HAS LARGE AREA OF CORROSION. REMOVED AND REPLACED SKIN FROM STA 1690-1890 LONG 28L-28R IAW DWG 5649329 AND SRM 51-1-21, 51-1-20D, AND 51-1-8.
Part: SUPPORT FITTING — CRACKED (BS 280)
INSPECTION TYPE-D, C-1 CARGO PIT AT FS 280 RT SIDE FLOORBEAM SUPPORT FITTING ABOVE STR 27R IS CRACKED AND CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 9754024 AND SRM 51-1-20D.
Part: CHORD — CORRODED (BS 70)
INSPECTION TYPE-D, FS 70 CHORD (AFT) AT STR 27R TO 35R HAS HEAVY CORROSION. REMOVED SECTION OF AFT CHORD FROM BTWN LONG 32 TO 33R TO LONG 21R, FABRICATED REPAIR PARTS AND EXTERNAL DOUBLER AND INSTALLED IAW SRM 53-2-5 FIG 8C-2, 51-1-21, 51-1-20D AND 51-3-1.
Part: ANGLE — CORRODED (BS 1740)
INSPECTION TYPE:D, FS 1740 FLOORBEAM ANGLE HAS HEAVY CORROSION AT RBL 20-30. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-1-20 AND DWG 5755032.
Part: SPLICE — CRACKED (BS 220-200)
INSPECTION TYPE:D, FS 200-220 STR 31L, SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING PER SRM 51-1-20 AND 53-10-1.
Part: SHEAR TIE — CRACKED (BS 270)
INSPECTION TYPE-D, FS 270 BETWEEN STR 32R AND 33R SHEAR TIE IS CRACKED IN 2 PLACES. REMOVED CRACKED FITTING AND INSTALLED NEW IAW SRM 53-20-0.
Part: SPLICE — CRACKED (BS 440-460)
INSPECTION TYPE:D, FS 460-440 STR 31L SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D.
Part: TORQUE TUBE — CRACKED (RT WING)
INSPECTION TYPE:D, RT WING L/E SECTION BETWEEN PYLONS, O/B SLOT TORQUE TUBE AT I/B END IS CRACKED IN HALF. REMOVED AND REPLACED CRANK IAW SRM 51-1-21.
Part: LONGERON — CORRODED (BS 55-70)
INSPECTION TYPE-D, FS 55 TO 70 STR 36 IS CORRODED ON ALL SIDES. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON FS 55 TO 70 IAW SRM 51-1-21.
Part: FRAME — CRACKED (BS 660)
INSPECTION TYPE:D, FS 660 ABOVE STR 23R FRAME HAS 4 CRACK IN RADIUS. REMOVED FRAME CLIP, FABRICATED AND INSTALLED REPLACEMENT IAW SRM 53-1-0 AND 51-1-20.
Part: FITTING — CORRODED (BS 70)
INSPECTION TYPE-D, FS 70 FWD SIDE LONGERON END FITTING AT 34R IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0, 51-3-1, 51-1-21.
Part: FITTING — CORRODED (BS 70)
INSPECTION TYPE-D, FS 70 FWD SIDE AT LONG 33R END FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-0 AND 51-3-1.
Part: FITTING — CORRODED (BS 70)
INSPECTION TYPE-D, FS 70 FWD SIDE LONG 30R END FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0, 51-3-1.
Part: CHORD — CORRODED (BS 70)
INSPECTION TYPE-D, FS 70 CHORD BTWN STR 31R TO 35R HAS SEVERE CORROSION, METAL SEPARATION FWD CHORD. REMOVED SECTION OF CHORD, FABRICATED AND INSTALLED REPAIR PARTS AND EXTERNAL DOUBLER IAW SRM 53-2-5 FIG 8 C-2, 51-1-20D, 51-1-21, AND 51-3-1.
Part: SKIN — SCRATCHED (FUSELAGE)
INSPECTION TYPE-D, EXTERIOR FUSELAGE JUST AFT OF LT AFT SERVICE DOOR HAS TWO DEEP SCRATCHES. HFEC INSPECTED, NO CRACKS NOTED. REMOVED EXISTING REPAIR DOUBLER, HFEC INSPECTED, NO CRACKS IN REPAIR AREA AFTER DOUBLER REMOVAL. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED SKIN AND DOUBLER STRAP PER DHC SK-894-274 (REF UPS EO DC8-5330-9253-A), SRM 51-1-20D, 51-1-20, 51-1-11.
Part: LONGERON — CORRODED (BS 55-70)
INSPECTION TYPE-D, FS 55 TO 70 STR 35R HAS FLAKING CORROSION ON AFT END. REMOVED, FABRICATED, AND INSTALLED LONGERON FROM FS 55 TO 70 PER SRM 51-1-21, AND 53-3-1.
1996
Part: LIFE RAFT — DEPLOYED (CABIN)
INSPECTION TYPE-N/A, AFT LIFE RAFT PARTIALLY DEPLOYED. REMOVED AND REPLACED AFT LIFE RAFT ASSY UNDER COURIER SEATS.
Part: DOOR SLIDE — LOW PRESS (ENTRY DOOR)
INSPECTION TYPE-N/A, MAIN ENTRY DOOR ESCAPE SLIDE PRESSURE LOW SEE REQ A446735. REMOVED AND REPLACED MAIN ENTRY DOOR ESCAPE SLIDE ON 5156100-4DG.
Part: ATTACH STUD — SHEARED (LT MLG)
INSPECTION TYPE: DLY. LEFT MLG DOWNLOCK ACTUATOR GEAR ATTACH STUD SHEARED (EXTEND-RETRACT) D113074. TRANSFERRED TO NRC 352009/009N. FABRICATED BUSHING AND INSTALLED BUSHING AND NEW STUD PER XEA-X8-32-1063. REINSTALLED ACTUATOR, ADJUSTED. OPS CK OK PER M/M 32-32-02.
Part: LIFE RAFT ELT — INOP (CABIN)
ELT BEACON RECEIVED ON 121.5 FOR ENTIRE FLIGHT. SUSPECT ELT IN AIRCRAFT LIFE RAFTS HAS GONE OFF. REMOVED AND REPLACED BOTH 6 MAN LIFE RAFTS. P/N OFF 600-107RB, S/N OFF 6523, P/N ON 600-107RB, S/N ON E-125, P/N OFF 600-107RB, S/N OFF 6538, P/N ON 600-107RB, S/N ON F-172.
Part: SKIN — CRACKED (FUSELAGE)
WHILE IN FOR B-CHECK, MAINTENANCE REPORTED CORROSION 4.375 CRACK COMING FROM RIVET AT LOWER RT SIDE OF FUSELAGE AFT OF NOSE W/W. REPAIR PENDING.
1995
Part: SKIN — CRACKED (FUSELAGE)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND AFT SERVICE DOOR FWD LOWER CORNER ON FUSELAGE SKIN CUTOUT IS CRACKED. REPAIRED PER UPS EO DC8-5310-7402-A.
Part: FRAME — CORROSION (FS 67)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON BELT FRAME STA 67, BETWEEN LONGERONS 17L TO 21L. REPAIRED PER UPS EO DC8-5310-7429-A.
Part: SKIN — CORROSION (FS 400)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION BULGE ON FUSELAGE SKIN AND DOUBLER, STA 400 LONGERON 36. REPAIRED PER UPS EO DC8-5330-7427-A.
Part: FRAME — CORROSION (FS 77)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON BELT FRAME STA 77, BETWEEN LONGERONS 17L TO 21L. REPAIRED PER UPS EO DC8-5310-7428-A.
Part: FRAME — CORROSION (FS 52)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LOWER FWD SIDE OF BELT FRAME FS 52, LBL 52 AND FLOORBEAM. REPAIRED PER UPS EO DC8-5310-6902-A.
Part: FITTING — CRACKED (BS 52)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE END FITTING AT STATION 52 AND LONGERON 8L. MAINTENANCE REPLACED THE FITTING PER SRM 51-1-21.
Part: FRAME — CORRODED (BS 62)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FRAME AT STATION 62 BETWEEN LONGERONS 17L - 21L. MAINTENANCE REPLACED FRAME PER SRM 51-1-20D.
Part: FRAME — CORRODED (BS 1580)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE BOLT FRAME AT STATION 1580 AND LONGERON 21L UPPER SIDE. MAINTENANCE REPAIRED THE FRAME PER SRM 53-2-0 FIGURE 2.
Part: BRACKETS — CRACKED (FWD ENTRY DOOR)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE EVACUATION SLIDE MOUNT BRACKETS. MAINTENANCE FABRICATED AND REPLACED THE BRACKETS PER SRM 51-1-4 AND 51-1-21.
Part: FITTING — CORRODED (BS 1580)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT ASSEMBLY COMPARTMENT FLOORBEAM END FITTING AT STATION 1580. MAINTENANCE REPLACED THE FITTING PER SRM 51-3-0.
Part: FLOOR BEAM — CORRODED (FS 1620)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION DAMAGE ON AFT SIDE OF FLOORBEAM AND FITTING, FS 1620 LT CUSP. REPLACED FITTING PER SRM 51-1-20D.
Part: SEAT TRACK — CORRODED (CABIN)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT NR 7 SEAT TRACK FWD END OF COMPARTMENT NR 15 AND AFT END OF COMPARTMENT NR 14. REPLACED SEAT TRACK PLUGS PER SRM 53-2-3.
Part: FRAME — CORRODED (FS 1640)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION DAMAGE AT FWD SIDE OF BOLT FRAME DOUBLER FS 1640, FROM LONGERONS 25R-27R. REPLACED FRAME DOUBLER PER SRM 51-1-20D.
Part: SKIN — CRACKED (SERV DR CUTOUT)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND AFT SERVICE DOOR FWD LOWER CORNER ON FUSELAGE SKIN CUT OUT IS CRACKED. REPAIRED PER UPS EO DC8-5310-7402-A.
Part: FITTING — CORROSION (FS 1690)
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION DAMAGE ON LONGERON 33L FITTING, FS 1690. REPLACED FITTING PER SM 51-1-20D, SRM 51-1-21 AND SRM 51-3-0.
Part: J BEAM — CRACKED (AFT PRESS BLKHD)
DURING B-CHECK, MAINTENANCE REPORTED TOP J-BEAM ON AFT PRESS BULKHEAD LT O/B END HAS CRACK ON TOP FLANGE AND LOWER FLANGE. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-5310-6598B.
Part: EEL BATTERY PACK — DISCHARGED (FLIGHT DECK)
MAINTENANCE REPORTED EMER. EXIT LIGHTS INOP. REPLACED BATTERY PACK, OPS CHECK GOOD.