N802UP
Registered owner: WHEELS UP PARTNERS LLC, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| CIRCADIAN AVIATION LLC (O2GA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
LEFT MAIN LANDING GEAR INDICATOR LIGHT WAS INTERMETTENT ON APPROACH. DELCARED EMERGENCY. REMOVED AND REPLACED WITH A NEW UNIT, THE L/H MLG DOWNLOCK SWITCH PN ON/OFF: 101-364628-1, SN OFF: 404HE222-6, SN ON: 12394808A, IAW KA300 AMM 32-60-05. PERFORMED LANDING GEAR EXTENSION AND RETRACTION OPS CHECK WITH NO DEFECT NOTED.
AFTER DEPARTURE, EXCESSIVE AILERON INPUT REQUIRED TO MAINTAIN LEVEL FLIGHT. CREW LEVELED THE ACFT AT 3000 FT AFTER NOTIFYING ATC. CREW TRIED TO RETRIM THE ACFT SEVERAL TIMES AND DETERMINED THERE WAS AN AILERON/AILERON TRIM ISSUE. ACFT RETURNED TO DEPARTURE WHERE IT WAS JUST RELEASED FROM A SCHEDULED MAINTENANCE EVENT. LANDING WAS UNEVENTFUL. UPON FURTHER INVESTIGATION IT WAS NOTED THAT THE LT AND RT AILERONS WERE REMOVED DURING THE SCHEDULED MAINTENANCE EVENT. DURING THE LT AND RT AILERON INSTALLATION PROCESS THE INBD LOWER ATTACHED SCREWS ON EACH OF THE AILERONS DID NOT CAPTURE THE HINGE BRACKETS. REPLACED CENTER HINGE ON LT AND RT AILERONS DUE TO AILERONS NOT LINING UP ON ALL 3 HINGE ATTACH POINTS. REINSTALLED LT AND RT AILERONS. A SUCCESSFUL OPS CHECK FLIGHT WAS PERFORMED. ACFT WAS RETURNED TO SERVICE.
LEFT OTBD MLG TIRE BLEW ON LANDING. REPLACED THE LT OTBD & INBD MAIN WHEEL & TIRE ASSEMBLIES. NO FURTHER DEFECTS WERE NOTED. ACFT WAS RTS.
ON CLIMB OUT THE RT PROPELLER PITCH ANNUNCIATOR ILLUMINATED. ACFT WAS DIVERTED BACK FOR MX. TROUBLE SHOT THE DISCREPANCY & FOUND A DEFECTIVE RT PROXIMITY SWITCH. ENG RUNS WERE PERFORMED & SYS OPERATIONAL CHECKS WERE GOOD. ACFT WAS RETURNED TO SERVICE.
EMERGENCY ESCAPE SLIDE INOP, GIRT BAR CLIP BROKEN. REPLACED FWD GIRT BAR CLIP IAW DPS 1.07-2.
ESCAPE SLIDE CONTAINER CLOSURE CLIP BROKEN CONTAINER WILL NOT STAY CLOSED. M391960, DEFERRED IAW MEL 52-7-4. REMOVED SLIDE AND SECURED ENCLOSURE PLACARD INSTALLED. OPEN
INSPECTION TYPE:N/A NR 3 ENGINE FLAMED OUT. ENGINE RELIT ON IT'S OWN. PERFORMED FIRST FOUR STEPS OF DC-8 M/M 71-00-00-1 FIG 139 UP TO INSPECT FUEL FILTER. FILTER KIT ON ORDER. REPLACED NR 3 FUEL FILTER PER AMM 73-10-02-4. LEAK CHECK OK. ACCOMPLISHED STEPS 5 THRU 15. ENGINE RUN SUCCESSFUL. A/C RETURNED TO SERVICE.
INSPECTION TYPE:C2 FLOORBOARD F81 HAS ONE EACH SCREW HOLE BROKEN OUT. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-3 FIG 10, 51-1-8, 51-1-21, 51-1-16.
INSPECTION TYPE:C2 RT WING INBD SLOT VANE HAS A DEEP CHAFING MARK AT SUPPORT ANGLE AT OTBD SIDE. REMOVED AND REPLACED SUPPORT ANGLE IAW AMM, 51-1-24, 27-80-00.
INSPECTION TYPE:C2 INTERCOSTAL CRACKED AT STA -84 L21L BELOW SUB-FLOOR. REMOVED AND REPLACED INTERCOSTAL IAW, SRM, 51-1-20D ,51-1-8, 51-1-21
INSPECTION TYPE:C2 C-PIT CROSS SLIDE DOOR INTERIOR SKIN IS GOUGED, FWD LWR AREA. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM, 51-1-8, 51-1-21, 52-2-0 FIG 2.
INSPECTION TYPE:C2 D PIT STA 1360 L35L SPLICE FITTING CRACKED AND CORRODED. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SRM 51-03-01 AND 51-01-20D.
INSPECTION TYPE:C2 C PIT STA 1230 L27L ATTACH FITTING HAS CORROSION. REMOVED AND REPLACED LONGERON ATTACH FITTING IAW DC8 SRM 51-01-20D.
INSPECTION TYPE:C2 END FITTING BLOWN OUT, L30L, STA 1759 DIFFICULT ACCESS. REMOVED AND REPLACED CORRODED FITTING IAW SRM 51-1-21, 51-1-8, 51-1-24 , 51-3-0.
INSPECTION TYPE:C2 LARGE SHEAR TIE CRACKED IN RADIUS, 60 COMARTMENT CEILING, STA 1800 L4R. STOP DRILLED, FABBED AND INSTALLED REPAIR ANGLE IAW, SRM 51-1-21, 53-2 -0, 51-1-8, 53-5-03, 51-1-20D.
INSPECTION TYPE-C2 POSSIBLE CRACK IN RADIUS OF INTERCOSTAL ATTACH ANGLE, AT BOTTOM J-BEAM, AFT SIDE OF APB, 60 COMPT RT BS 1771. REMOVED INTERCOSTAL ATTACH ANGLE, FABRICATED AND INSTALLED REPLACEMENT ANGLE. IAW DWG 5773844 AND SRM 51-1-21,51-3-00 AND 51-1-20D.
INSPECTION TYPE:C2 AFT ACCESSORY COMPT STA 1580, L21L FLOORBEAM ATTACH FITTING HAS CORROSION. REMOVED AND REPLACED END FITTING IAW SRM, 51-1-8, 51-1-20D, 51-3-1.
INSPECTION TYPE:C2 RIGHT ELEVATOR UPPER SKIN IS DENTED AND GOUGED, FWD OF GEARED TAB. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 55-2-0, 55 51-1-8, 53-1-8, 55-2-0 FIG 10.
INSPECTION TYPE:C2 FLIGHT DECK STA -52 RT SIDE FRAME HAS CORROSION BY SUBFLOOR AREA. REPAIRED FLT DECK FRAME AT STA -52 AND SUBFLOOR AREA IAW EA 008- 5310-01-A1403.
INSPECTION TYPE:C2 RUDDER RT SIDE EXTERIOR SKIN HAS CORROSION, POPPED RIVETS AND BEADED SKIN IS SEPARATED. REMOVED AND REPLACED 2 RUDDER SKINS IAW DC8 SRM 51-1-21, 51-1-21A , AND51-01-22.
INSPECTION TYPE:C2 MAIN CABIN, L-15L CRACKED AT CANT FRAME STA 1746. REMOVED, FABBED AND INSTALLED LONGERON SLICE IAW SRM, 51-1-8, 53-2-2 FIG 10, 53-5-1 FIG 7, 51-1-20D.
INSPECTION TYPE:C2 COPILOT REAR LT AND RT SEAT TRACKS SHOWS ELONGATION. REMOVED AND REPLACED SEAT TRACKS IAW SRM, 51-1-20D, 51-3-1, 51-1-24 AN D 25-11-1.
INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK STA 1460, 0BL 2 EACH HOLES ELONGATED. REMOVED AND REPLACED SEAT TRACK PLUG IAW SRM, 51-3-00.
INSPECTION TYPE:C2 LEFT WING NR 1 SPOILER HINGE FITTING GOUGED NEAR STA XW38. REMOVED AND REPLACED HINGE FITTING IAW SRM, 51-1-8, 51-3-0, 51-3-2.
INSPECTION TYPE:C2 MAIN CABIN, FLOORBOARD TIEDOWN BULGED AND FASTENERS PULLING STA 350 LBL 35. REMOVED, DAMAGED RECEPTICLE, FABBED AND INSTALLED REPAIR DOUBLER ON FLOOR PANEL, INSTALLED NEW RECEPTICLE IAW SRM 51-1-8, 53-2-3 FIG 1F, 51-1 -21A, 51-1-11.
INSPECTION TYPE:C2 MAIN CABIN FLOORBOARD CRACKED, STA 45 RBL 47. FABBED AND INSTALLED REPAIR DOUBLER IAW, SRM. 53-2-00, 53-2-3, 510108, 51-1-26, 51-1-21.
INSPECTION TYPE:C2 RIGHT WHEEL WELL AT UPPER FWD BULKHEAD, HYDRAULIC MANIFOLD PULLEY BRACKET IS CRACKED. REMOVED CRACKED FITTING, REPAIRED AND RE-INSTALLED FITTING IAW SRM 20-16-0, 51-1-8, DPS 4.706, DPS9.18.
INSPECTION TYPE:C2 COCKPIT, SECOND OBSERVER SEAT TRACKS SHOW ELONGATIONS. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-3-0, 51-1-2, 51-1-8.
INSPECTION TYPE:C2 COCKPIT SECOND OBSERVER SEAT TRACKS SHOWS ELONGATIONS. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-1-8, 51-3-0, 51-1-24.
INSPECTION TYPE:C2 PILOT REAR LT AND RT SEAT TRACKS SHOW ELONGATIONS REMOVED AND REPLACED 2 EACH SEAT TRACKS IAW SRM, 51-1-20D, 51-1-24.
INSPECTION TYPE:C2 NR 2 PYLON UPPER PANEL FRAME, WORN BEYOND LIMITS, DEEP CHAFED DAMAGE BETWEEN PANELS 293A/B AND 294A/B. FABBED AND INSTALLED NEW PANEL FRAME IAW SRM, 51-1-8, 51-1-20D, 51-1-2 1, 54-3-3 FIG 7.
INSPECTION TYPE:C2 MAIN CARGO COMP STA 980, L22R ATTACHING FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20, 51-1-20D, 51-1-8.
INSPECTION TYPE:C2 INTERIM REPAIR TO RT INBOARD FLAP AT TRAILING EDGE XM-75. REMOVED INTERIM REPAIR, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-21A, 51-1-8, 51-1-9A.
EMERGENCY EXIT LIGHT AT THE C1 DOOR HAS 2 BULBS OUT. REMOVED AND REPLACED 2 BULBS FOR THE EMERGENCY EXIT LIGHTING AS NEEDED.
EMERGENCY LIGHTS DISARM LIGHT WAS NOT ILLUMINATED. FOUND BATTERY BUS 30 AMP CURRENT LIMITER BAD. REPLACED SAME AND PERFORMED EMERGENCY LIGHT TEST IAW DC8 AMM 33-50-01-2. SYS OPS CKS NORMAL.
INSPECTION TYPE:N/A PIT 32 DOOR CRACKED. ACCOMPLISHED HFEC INSPECTION PER EO DC8-5230-28827 PAR 6 A2. ACCOMPLISHED STOP DRILL PER EO DC8-5230-28827 PAR 6 A3-A4. NEEDS HFEC. ALSO REMOVED MOUNT BOLTS & 2 EA RIVETS FOR ACCESS. PERFORMED EDDY CURRENT ON STOP DRILL. NO CRACKS NOTED.
GLARESHIELD HAS ONE EMERGENCY LIGHT INOP. RELAMPED AND TESTED IAW MM 33-13-00-2. OPS CHECK GOOD.
NR 3 ENGINE FLAME OUT. INFLIGHT RESTART ACCOMPLISHED AFTER DESCENT TO FL220. NORMAL ENGINE INDICATIONS AFTER RESTART. A/C IS CURRENTLY OUT OF SERVICE. PERFORMED DC8 MM71-00-00-1, FIG 139 AS REQUIRED. REF LP 887083/1,2,3 LOG PAGE 887084 ITEM 1,2,3. NR 3 ENGINE PERFORMANCE WAS NORMAL WITH MIN. FUEL PRESSURES MET. NO PREVIOUS FLAME OUT HISTORY. A/C OK FOR CONTINUED SERVICE.
EMERGENCY EXIT LIGHTS ARE VERY DIM AND FLIGHT DECK LIGHT GOES OUT IN APPROX 2 MINUTES. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW DC8 AMM 33-50-01-2. OPS TEST NORMAL.
INSPECTION TYPE:N/A CAPT ESCAPE ROPE DOOR LOOSE, ROPE FELL OUT. ROLLED, INSTALLED ESCAPE ROPE. RESECURED ESCAPE ROPE DOOR, OK TO CONTINUE.
INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT DISARM. RELAMPED DISARM INDICATION LIGHT. OPS CHECK OK.
INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT SWITCH HARD TO MOVE TO DISARM CHECK POSITION. REPLACED EMERGENCY EXIT LIGHT SWITCH PER IPC 33-50-00-003. OPS CHECK OK PER AMM 33-50-00-0.
INSPECTION TYPE:N/A FLIGHT LEVEL 370 .79 MACH AT CRUISE ENGINE 3 FLAMED OUT AND WITH IGNITION ON RESTARTED ALL INDICATIONS NORMAL. PERFORMED AMM 71-00-00-1 UP TO ENG RUN. SUBSEQUENT STEPS OF THE ENGINE FLAMEOUT TROUBLESHOOTING TREE ARE NOT REQUIRED DUE TO R/R OF ENGINE FEED LINE GAMMA COUPLINGS PACKINGS.
CAPTAIN'S CLEARVIEW WINDOW STUCK CLOSED. REMOVED AND REPLACED CAPT'S SLIDING WINDOW UPPER LOCK BAR W/REF TO DC8 AMM 56-10-03-5 CAPTAIN'S CLEARVIEW WINDOW OPS NORMAL.
CAPT CLEARVIEW WINDOW WILL NOT OPEN. FOUND WINDOW TRIM ON AFT OF SLIDING WINDOW JAMMING WINDOW MOTION. REMOVED WINDOW TRIM FROM AFT OF WINDOW. WINDOW OPS CK NORMAL.
INSPECTION TYPE:C3 END FITTING FOR STRINGER 51 OUTBOARD OF XRS 74 NR 2 MAIN TANK. REMOVED STRINGER END FITTING 51 AT STA XRS 74 NR 2 MAIN TANK IAW SRM 51-3-0. LOCATED, DRILLED UP AND INSTALLED END FITTING ON STRINGER 51 AT STA 74 NR 2 MAIN TANK IAW SRM 51-1-20D.
INSPECTION TYPE:C3 LT CENTER L/E UPPER RIB CRACKED AT XFS 460. STOP DRILLED CRACKED RIB AT LT L/E STA XFS 460 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE AT LT L/E RIB STA XFS 460 IAW SRM 57-02-00 FIG 002.
INSPECTION TYPE-C3 AFTER REMOVED FUSELAGE BELLY SKIN FROM FS -22 TO 70 L31L-L31R, FOUND LONGERON HAS HEAVY CORROSION AT STA 55 TO 70 L36. FABRICATED AND INSTALLED LONGERON AND END FITTING. IAW SRM 51-3-2 AND 51-1-20D.
INSPECTION TYPE-C3 STA 857 RBL 53 UPPER HORIZONTAL ATTACH ANGLE, CENTER FUEL TANK, FWD BULKHEAD HAS EXFOLIATED CORROSION. REMOVED FABRICATED AND INSTALLED SHEAR WEB ANGLE RAT WHEEL WELL, FWD BULKHEAD (CENTER FUEL TANK), STA 857 RBL 53 IAW DRAWING NR 5644011, SRM 51-3-0, AND SRM 51-1-20D.
INSPECTION TYPE:C3 LEFT CENTER LEADING EDGE UPPER RIB CRACKED AT XFS 366. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-3-3, 57-02-00, 51-1-21 AND 51-1-20D.
INSPECTION TYPE-C3 STA 1766 LONGERON 28R END FITTING CORRODED. END FITTING FOUND TO BE CORRODED AND CRACKED. REMOVED AND REPLACED STA 1766 LONGERON 28R END FITTING IAW SRM 51-1-20D, AND SRM 51-03-02 -0.
INSPECTION TYPE-C3 STA 1760 LONGERON 14R END FITTING CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 1760 LONGERON 14R IAW SRM 51-01-21, SRM 51-03-00, AND SRM 51-01-20D.
INSPECTION TYPE-C3 STA.1766 LONGERON 28R CORRODED AND CRACKED. REMOVED DAMAGED SECTION OF LONGERON 28R FROM STA 1752 TO 1766 IAW SRM 53-02-02-0 FIG 10 AND SRM 51-01-21-0. FABRICATED LONGERON SECTION AND REPAIR STRAPS IAW SRM 53-05-03-0, AND SRM 53-02-02-0 FIG 10. INSTALLED LONGERON SECTION, REPAIR STRAPS, AND REPAIR SPLICE P/N DC8-53B-009-39 IAW SRM 51-01-20D-0.
INSPECTION TYPE:C3 LT CENTER L/E WING RIB CRACKED AROUND FASTENER HOLE AT XFS-448. STOP DRILLED CRACK IAW SRM 57-02-00-0. FABRICATED AND INSTALLED ANGLE REPAIR LT CENTER L/E WING RIB AT XFS-448 IAW SRM 53-03-03-0 FIG 005 AND SRM 51-1-20D.
INSPECTION TYPE:C3 LEFT CENTER LEADING EDGE UPPER RIB CRACKED AT XFS 310. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00 FIG 002, 57-03-03 FIG 005 AND 51-1-20D.
INSPECTION TYPE: C3 STA.1690 LONGERON 28R END FITTING CRACKED. REMOVED AND REPLACED STA.1690 LONGERON 28R END FITTING IAW SRM 51-1 -20D AND SRM 51-03-01-0.
FOUND CORROSION BETWEEN SKIN AND DOUBLER AT L36 STA 1180, EXTERIOR BULGED. CUT OUT DAMAGED AREA AT STA 1180 L36 IAW SAA EA 008-5320-01-A0381. FABRICATED AND INSTALLED REPAIR PARTS AT STA 1180 L36 IAW SAA EA NR 008-5320-01-A0381, UPS RAA DC8-53-20581, DOUGLAS DWG 5770322, BAC MSG NR 1-221344384, AND FAA FORM 8100-9.
INSPECTION TYPE:C3 LT CENTER L/E UPPER RIB CRACKED AT XFS 491. STOP DRILLED CRACKED RIB AT LT L/E UPPER RIB AT STA XFS 491 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE AT STA XFS 491 IAW SRM 57-02-00 FIG 002.
INSPECTION TYPE: C3 STA.1690 LONGERON 26R END FITTING CRACKED. REMOVED AND REPLACED STA. 1690 LONGERON 26R END FITTING IAW SRM 51-1-20D,AND SRM 51-03-01-0.
INSPECTION TYPE:C3 LT CENTER L/E UPPER RIB CRACKED AT XFS 409. STOP DRILLED CRACKED RIB AT LT L/E RIB STA XFS 409 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE AT LT L/E RIB STA XFS 409 IAW SRM 57-02-00 FIG 002.
INSPECTION TYPE:C3 RT CENTER L/E UPPER RIB BROKEN AT XS 515. REMOVED DAMAGED AREA AT RT CENTER L/E UPPER RIB AT STA XS 515 IAW SRM 57-02-00. FABRICATED AND INSTALLED REPAIR DOUBLER AT RT WING UPPER L/E RIB AT STA XS515 IAW SRM 57-02-00 FIG 002.
INSPECTION TYPE:C3 RT CENTER L/E WING UPPER RIB HAS DEEP GOUGE AT XFS 435 BLENDED GOUGE IAW SRM 57-02-00 FIG 2 SHEET 2 (OUT OF LIMITS). FABRICATED AND INSTALLED DOUBLER IAW SRM 57-3-3 FIG 5, SRM 57-02-00 AND SRM 51-1-20D AT RT CENTER L/E UPPER RIB XFS 435.
INSPECTION TYPE:C3 RT CENTER L/E WING UPPER RIB CRACKED AT XFS.404. STOP DRILLED CRACK IAW SRM 57-02-00-0. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-02-00-0,SRM 51-1-20D, AND SRM 51-1-21 AT RT CENTER L/E UPPER RIB XFS.404.
INSPECTION TYPE:C3 BANANA FITTING CRACKED AT STA 300 L26L. REMOVED CRACKED BANANA FITTING AT STA 300 L26L IAW SRM 51-1-20D LOCATED, DRILLED, AND INSTALLED REPLACEMENT FITTING AT STA 300 L26L IAW SRM 51-3-2, DWG 3754041, AND SRM 51-1-20D.
INSPECTION TYPE-C3 FLOORBEAM TO CUSP FITTING CRACKED AT STA 280 RBL 55 REMOVED FLOORBEAM TO CUSP FITTING AT STA 280 RBL55 IAW SRM 51-1-20D LOCATED, DRILLED, AND INSTALLED FRAME FITTING TO CUSP IAW SRM 51-3-2 AND SRM 51-1-20D.
INSPECTION TYPE:C3 BROKEN FITTING ON RT W/W CEILING, FWD SIDE OF STA 960 BEAM RBL 2. REMOVED BROKEN FITTING AT STA 960 RBL 2 RT W/W IAW SRM 51-1-20D LOCATED, DRILLED UP, AND INSTALLED REPLACEMENT FITTING AT STA 960 RBL 2 RT W/W IAW SRM 51-01-24-0, AND SRM 51-1-20D.
FOUND CORROSION UNDER VERTICAL STRAP ON RT W/W FWD BULKHD (CNTR TANK) STA 857 RBL 25. REPAIRED VERTICAL STRAP WEB AT RT W/W STA 857 XCW 23 IAW SAA 008-5320-01-A0374, UPS DC8-53-20583, BAC SERV REQUEST NR 1-221600945, AND DWG 5619335 AND 5644678 REV P, AND FAA FORM 8100-9.
INSPECTION TYPE:C2 LT L/E OB UPPER RIB CRACKED AT XFS 816. STOP DRILLED CRACK ON RIB AT XFS 816 L/WING IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT L/WING STA XFS 816 IAW SRM 57-02-00 FIG 2.
LT LE OB UPPER RIB CRACKED AT XFS 808. STOP DRILLED CRACK AT RIB AT LT LE STA XFS 808 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIB AT LT WING LE STA XFS 808 IAW SRM 57-02-00 FIG 002.
INSPECTION TYPE:C2 LT OB LE UPPER RIB CRACKED AT XFS 846. STOP DRILLED CRACK ON RIB AT STA XFS 846 LT IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIB AT LT L/E STA XFS 846 IAW SRM 57-02-00 FIG 2.
INSPECTION TYPE:C2 LT L/E OB UPPER RIB CRACKED AT STA XFS 852. STOP DRILLED CRACK ON RIB AT LT L/E XFS 852 IAW SRM 57-02-00 FIG OO2. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIB AT LT L/E STA XFS 852 IAW SRM 57-02-00 FIG 2.
INSPECTION TYPE:C2 LT L/E OB UPPER RIB CRACKED AT XFS 827. STOP DRILLED CRACKED RIB AT L/WING STA XFS 827 IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT L/WING STA XFS 827 IAW SRM 57-02-00 FIG 2.
INSPECTION TYPE:C3 LT L/E LWR RIB CRACKED AT XFS 778. STOP DRILLED CRACKED RIB AT LT L/E LWR RIB STA XFS 778. FABRICATED AND INSTALLED REPAIR DOUBLER AT LT L/E RIB STA XFS 778 IAW SRM 57-02-00-0 FIG 2.
INSPECTION TYPE:C3 LT CENTER L/E UPPER RIB CRACKED AT XFS 372. STOP DRILLED CRACKED RIB AT LT L/E STA XFS 372 IAW SRM 57-02-00 FIG 005. FABRICATED AND INSTALLED REPAIR DOUBLER AT L/WING LE STA XFS 372 IAW SRM 57-02-00 FIG 005.
INSPECTION TYPE:C3 LT L/E UPPER RIB IS CRACKED AT XFS 796. STOP DRILLED CRACKED RIB AT LT L/E UPPER RIB AT STA XFS 796 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER AT LT L/E STA XFS 796 IAW SRM 57-02-00 FIG 002.
INSPECTION TYPE:C3 LT L/E UPPER RIB CRACKED AT XFS 641. STOP DRILLED CRACKED RIB AT LT L/E RIB AT STA XFS 641 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER AT LT L/E RIB STA XFS 641 IAW SRM 57-02-00 FIG 002.
INSPECTION TYPE:C3 LT OB L/E UPPER RIB CRACKED AT XFS 672. STOP DRILLED CRACKED RIB AT STA XFS 672 LT IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR ANGLE ON RIB AT LT L/E STA XFS 672 IAW SRM 57-02-00 FIG 002.
INSPECTION TYPE:C3 RT OUTBD LE WING UPPER RIB CRACKED AT XFS.591. STOP DRILLED CRACK IAW SRM 57-02-00-0. FABRICATED AND INSTALLED ANGLE R REPAIR IAW SRM 57-02-00-0 FIG 2, SRM 57-03-03-0 FIG 6 AND SRM 51-1-21D -D AT RT OUTBD LE WING UPPER RIB XFS 591.
INSPECTION TYPE:C3 RT WING OUTBD L/E UPPER RIB CRACKED AT XFS.716. STOP DRILLED CRACK IAW SRM 57-02-00-0. FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 57-03-03-0 FIG 6, SRM 57-02-00-0 FIG 2 AND SRM 51-1-20D AT RT OUTBD L/E UPPER RIB XFS 716.
INSPECTION TYPE:C3 RT OUTBD WING L/E UPPER RIB CRACKED AT XFS.603. STOP DRILLED CRACK IAW SRM 57002-00-0 FIG 2. FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 57-03-03-0 FIG 6, SRM 57-02-00-0 FIG 2 AND SRM 51-1-20D AT RT OUTB WING L/E UPPER RIB XFS 603.
INSPECTION TYPE:C3 UPON REMOVAL OF D-PIT SCUFF PLATE, FOUND BELLY SKIN CORRODED OUT OF LIMITS AT STA 1400-1420 L31R. REMOVED AND REPLACED BELLY SKIN AT STA 1350-1490 L31L-L31R IAW SRM 51-1-21, 51-1-8, AD SRM 51-1-20D.
INSPECTION TYPE:C3 CRACKED END FITTING AT STA 70 L31R UPPER FITTING. REMOVED CRACKED END FITTING AT STA 70 L31R IAW SRM 51-3-0. FABRICATED AND INSTALLED END FITTING AT STA 70 L31R IAW SRM 51-1-20D SRM 51-3-0, AND DWG 4614397.
INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 844. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-03-03 FIG 7, 57-02-00 AND 51-1-20D.
INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 808. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-02-00-0 AND 51-1-20D.
INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE, LWR RIB CRACKED AT XFS 778. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2, 57-3-3 FIG 7 AND 51-1-21, 51-1-20D.
INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE, UPPER RIB CRACKED AT XFS 796. FABRICATE AND INSTALL REPAIR ANGLE IAW SRM 57-3-30 FIG 7 AND 51-1-20D.
INSPECTION TYPE:C3 RIGHT WING LEADING EDGE UPPER RIB CRACKED AT XFS 722. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51-1-20D AND 57-02-00-0.
INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT XFS 760. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 51-1-21, 57-2-0 FIG 2.
INSPECTION TYPE:C3 LEFT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 760. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-02-00 FIG 2 SHT 2, 57-02-00, 51-1-20D AND 51-1-21.
INSPECTION TYPE:C3 LEFT O/B LEADING EDGE UPPER RIB CRACKED XFS 597. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-02-00 FIG 2 SHT 1, 57-3-00 FIG 17, 51-1-21 AND 51-3-0.
INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT XFS 778. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-3-3 FIG 7, 53-2-0 FIG 2, 51-1-21 AND 51-1-20D.
INSPECTION TYPE:C3 LEFT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 660. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 EA REPAIR ANGLES IAW SRM 57-0-00 FIG 2 SHT 2, 57-2-0 FIG 2 SHT 2, 57-3-0 FIG 17 SHT 1.
INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 802. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-0-0 FIG 2, 57-3-3, 51-1-21 AND 51-1-20D.
INSPECTION TYPE:C2 LH OB LE, LWR RIB CRACKED AT XFS 822. STOP DRILLED CRACK ON RIB AT WING STA XFS 822 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER AT XFS 822 RIB IAW SRM 57-02-00 FIG 002.
LT OB LE LWR RIB CRACKED AT XFS 816. STOP DRILLED CRACK AT RIB L/WING LE STA XFS 816 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER AT L/WING LE RIB STA XFS 816.
INSPECTION TYPE:C3 CRACK AT STA 1741 L17R OUTER SKIN SURFACE. REPAIRED CRACKED SKIN AT STA 1741 L17R IAW SAA EA NR 008-5320-01-A0401 UPS EO DC8-5330-25029-A, BAC SERV REQUEST NR 1-223199646-2, DACO DWG 5649327 REV P, AND FAA FORM 8100-9.
INSPECTION TYPE:N/A 1 INCH CUT IN FLOOR PIT 33 STA 1020 L. PERFORMED INTERIM REPAIR REF EO DC8-5320-8724A APPENDIX A.
EMERG EXIT LIGHT ON IN FLT WILL NOT EXTINGUISH IN ARMED POS. THIS DISCREPANCY COULD NOT BE DUPLICATED ON THE GROUND. PERFORMED EMERG LIGHTING CK PER MM 33-50-02-2 WITH ALL NORMAL RESULTS.
2ND OBSERVERS SMOKE GOGGLES SCRATCHED. REPLACED SMOKE GOGGLES.
CREW REPORTED WINDOW WAS ARCING AND TURNED OFF WINDOW HEAT. 30 SECONDS LATER, WINDOW SHATTERED (CAPTAIN'S SIDE WINDOW). REMOVED AND REPLACED LEFT SIDE WINDOW PER MM 56-10-02-2. OPERATIONAL A ND LEAK CHECK NORMAL.
INSPECTION TYPE:N/A ON MAIN CARGO DOOR LATCH ACTUATING BEAM BOLT HOLE ELONGATED 3RD AFT. ACCOMPLISHED MAIN CARGO DOOR LATCH WALKING BEAM REPAIR AS PER EO DC8-5230-1803-M. DOOR OPERATES NORMAL.
INSPECTION TYPE:N/A FLT DECK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND REPAIRED WIRE TO PIN 9 OF CONNECTOR P1-1345, OP CHECK'S GOOD PER MM 33-50-01-2.
DURING CRUISE NOTICED VERY BAD BURNING SMELL COMING FROM RT SIDE OF AIRCRAFT BEHIND REAR JUMPSEATS NOT ELECTRICAL SMELL R MANIFOLD TEMP 240 C R PACK ON AND OFF NO CHANGE. LT PACK SYSTEM CKD GOOD NO SMELL. RT SYSTEM HAS OIL SMELL FOUND RT ACM BAD DEFERRED IAW MEL 21-39. PLACARD INSTALLED. GRD RAN ENGINE AT PWR PERFORMED MANIFOLD AIR ABNORMAL TEMPERATURE INDICATION TEST. FOUND L/H TEMP BULB READING LOW. FOUND SKYDROL OVER SERVICED BY APPROX.5 GALS. RAN BOTH PACKS NO ABNORMAL SMELL. TEMP O ALL WORK IAW MM 36-00-00.
EMERGENCY LIGHTS OUT, REPLACED LIGHTING BATTERY PACK, OPS NORMAL.
AT FL 370 ENGINE ANTI ICE WAS TURNED ON, SHORTLY AFTER MANIFOLD OVER TEMP LIGHT ILLUMINATED MANIFOLD TEMP (RT) REACHED RED ARC. COCKPIT FILLED WITH SMOKE AND FUMES. COMPLIED WITH CHECKLIST AND TURNED NR 3 ENG ANTI-ICE OFF. MANIFOLD TEMP RETURNED TO NORMAL. OVERTEMP LIGHT EXTINGUISHED AND SMOKE WAS EVACUATED. REMOVED AND REPLACED NR 3 ENG PRECOOLER CONTROL VALVE. LEAK CHECK OPS CHECK GOOD.
INSPECTION TYPE:C1 WING CENTER SPAR LOWER CAP AT WING STATION XCW 36 IS CRACKED. STOP DRILLED CRACK NDT VERIFIED STOPDRILLS TERMINATED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER AND REPAIR ANGLE IAW SAA SK 802-190 AND UPS EO DC8-5710-20888-A.
INSPECTION TYPE: C1, NR 4 ALT BOOST PUMP BRACKET AND STRINGER 59 END FITTING AT XW 408 ARE CRACKED. REMOVED, FABRICATED AND REPLACED FITTING AND REPLACED BRACKET IAW DWG 3645611 AND 5644972 AND SRM 51-1-20D.
INSPECTION TYPE: C1, STATION 1220 AFT SIDE BATHTUB FITTING IS CRACKED BETWEEN LONG 33R AND 32.5R IN TORQUE BOX. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D.
INSPECTION TYPE: C1, HFEC INSPECTION DETECTED A CRACK IN FITTING AT STA 1150, FWD SIDE AT LONGERON 33 RT. REMOVED AND REPLACED FITTING AT STA 1150, LONGERON 33 RT IAW SRM 51-3-2, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE: C1, RT WING INTERIOR DOUBLER CORRODED AT STALL WARNING VANE, STA XFS371- 376. REMOVED CORRODED INTERNAL DOUBLERS SRM51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG5769589, AND SRM 51-1-21, & 51-1-8.
INSPECTION TYPE: C1, INTERCOSTAL CRACKED IN MAIN CABIN SUBFLOOR, STA 1726, LBL 35. REMOVED, FABBED, AND REPLACED INTERCOSTAL IAW DWG 5755032, SRM 51-1-21, 51-1-8, 51-1-20D.
INSPECTION TYPE: C1, INTERCOSTAL ATTACH FITTING CRACKED AT STA 1240 LONG 35R REMOVED AND REPLACED FITTING IAW SRM 51-3-2, 51-1-20D.
INSPECTION TYPE: C1, LONGERON 28L CRACKED AT FRAME INTERSECTION STA 1400, CUT OUT DAMAGED LONGERON SECTION FROM 1390 TO 1410. FABRICATED REPLACEMENT LONGERON. SECTION SRM53-2-2 FIG10 AND SRO853009 AND 53-4-1 FIG44. INSTALLED 2 SPLICE FITTINGS AND LONGERON SECTION IAW SRM 51-1-20D, 51-1-21, 51-1-8
INSPECTION TYPE:C1 STATION 990 LONGERON 23R END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3753306 AND SRM 51-1-20D.
INSPECTION TYPE:C1 STATION 1170 BACKUP FITTING FWD SIDE IS CORRODED FOR FWD LOWER T-BOLT FITTING AT LONG 33R. REMOVED AND REPLACED FITTING IAW DWG 5894282 AND SRM 53-2-0 FIG 2D.
INSPECTION TYPE: C1, CORROSION ON SUBFLOOR BETWEEN WEB AND CHANNEL, MAIN CABIN STA 857 AT FUEL DUMP TORQUE TUBE. REMOVED UPPER CHANNEL IAW SRM 51-1-21. CUT OUT DAMAGED AREA. FABBED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM53-2-0 FIG23, DWG 5645332, 51-1-21, 51-1-8. REINSTALLED UPPER CHANNEL IAW SRM 51-1-21.
INSPECTION TYPE:C1 STATION 1735 LONG 15R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING AND STRAPS IAW SRM 53-2-2 FIG 10 BETWEEN STATION 1720 TO 1766.
INSPECTION TYPE:C1 CORROSION ON/AROUND MAIN CABIN SUBFLOOR FINGER DOUBLER STA 880 TO 900 RBL60-64 FINGER DOUBLER CORRODED BEYOND LIMITS. UNDERLYING STRUCTURE OK. FABBED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG 5645332, SRM 53-2-0 FIG1F, 51-1-8, 51-1-21, 51-1-20D, 51-1-11.
INSPECTION TYPE: C1, LONGERON 31 LT SPLICE FITTING CRACKED AT STA 450. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-11, 51-1-20D.
INSPECTION TYPE: C1, FINGER DOUBLER CORRODED IN COCKPIT SUBFLOOR. STA.-75 AT LT CUSP REMOVED, FABRICATED, AND REPLACED CORRODED EDGE DOUBLER IAW SRM 53-3-3 FIG.6, 51-1-8, 51-1-21, AND DWG5612298.
INSPECTION TYPE: C1, LEFT WING FLAP HINGE STATION 3 FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM 51-1-20D.
INSPECTION TYPE: C1, STATION 1770 LONG. 17L IS CRACKED REMOVED,FABRICATED AND REPLACED LONGERON IAW DWG. 5649327,AND SRM. 51-1-20D,51-1-21
INSPECTION TYPE: C1, RT HORIZONTAL STAB L/E HAS SCREWS PULLED THROUGH SKIN AT XFS 178.750. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-2-1 FIG 4.
INSPECTION TYPE: C, FUSELAGE EXTERIOR SKIN IS CRACKED AT STATION 1745 AT LONGERON 15R. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, DOUBLER, FINGER DOUBLER IAW SRM 53-2-1 FIG 7.
INSPECTION TYPE: C1, VERTICAL FIN TO FUSELAGE ATTACH ANGLE HAS POPPED RIVET, LT SIDE, STA 1766. REMOVED PAINT IAW SRM 51-20-00. FOUND CRACK, NDT VERIFIED. FABBED REPAIR ANGLE IAW SRM 53-2-5 FIG16A. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20D, 51-1-26, 51-1-11.
INSPECTION TYPE: C1, VERTICAL FIN TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1750 RT SIDE. STRIPPED PAINT IAW MM51-20-00. NDT VERIFIED CRACK. FABBED REPAIR ANGLE IAW SRM 53-2-5 FIG.16A. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20D, 51-1-11, 51-1-26.
INSPECTION TYPE:C1 STATION 1770 LONG 17R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION IAW DWG 5649327 AND SRM 51-1-20D, 51-1-21.
INSPECTION TYPE: C1, RIGHT WING LEADING EDGE LOWER RIB IS CRACKED AT FASTENER HOLE AT XFS 601. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C1 RIGHT WING FLAP HINGE 3 SUPPORT FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM 51-1-20D, 51-1-21.
INSPECTION TYPE:N/A CAPTAINS SEAT WILL NOT LOCK IN PLACE, IT SLID OUT OF POSITION AT BEGINNING OF T/O ROLL AND SETTING THE BRAKES AT ENGINE SHUTDOWN. SEAT WAS IN FALSE LOCK POSITION. REPLACED CAPTAIN'S SEAT ASSY IAW 25-11-01-2. OPS CHECK GOOD.
INSPECTION TYPE:ASV EMERGENCY LIGHT SYSTEM INOP. R&R EMERGENCY LIGHT BATTERY PACK OPS CK OK PER DC8 MM 33-50-00.
INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, LIGHTS CHECK NORMAL.
INSPECTION TYPE:C2 R1 AFT LOWER DOOR JAMB CORNER HAS CRACKED EXT FUSELAGE SKIN AT FASTENER HOLE FOUND BY EDDY CURRENT INSP. CUT OUT DAMAGE, PERFORMED EDDY CURRENT INSP AFTER DAMAGE REMOVAL IAW DOUGLAS NDT SPM 06-10-01.001, NO CRACKS NOTED. FABBED DOUBLER TRIPLER & FILLER IAW DC8 SRM 53-2-0 FIG 14.
INSPECTION TYPE:C2 FWD PIT STA 380 INTERCOSTAL ATTACH CLIP IS CRACKED L33L. REMOVED CLIP, FABBED CLIP IAW DAC DWG 5750726-93, AND INSTALLED CLIP IAW DC8 SRM 51-3-0.
INSPECTION TYPE:C2 MAIN CABIN LONG 32R END FITTING CORRODED AT FS 1760. REMOVED CORRODED FITTING IAW DC8 SRM 51-1-21, LOCATED DRILLED DEBURRED NEW FITTING IAW 53-2-0, INSTALLED FITTING IAW DC8 SRM 51-1-21 & 51-1-20D, 51-1-17.
INSPECTION TYPE:C2 CABIN STA 70 SEAT TRACK-E IS WORN. BLEND GOUGE IAW SRM 53-2-0 FIG 14. FOUND OUT OF LIMITS IAW 53-2-3. REMOVED DAMAGED SECTION AND FABBED NEW SEAT TRACK IAW DC8 SRM 53-2-3. INSTALLED NEW SEAT TRACK IAW DC8 SRM 53-2-3.
INSPECTION TYPE:C2 ACP SRM REPAIR TO SEAT TRACK AT POS 2L/3L SUPERLOCK INSTALLED IAW EO M-2550-4101. CUT OUT DAMAGED SEAT TRACK SECTION, FABBED AND DRILLED NEW SEAT TRACK SECTION AND 2 SPLICES IAW DC8 SRM 53-2-3. INSTALLED NEW SEAT TRACK SECTION, SPLICES IAW DC8 SRM 51-3-0.
INSPECTION TYPE:C2 AIR COND PRESS COMPT AT FS 56 BETWEEN L32R - 34R BETWEEN, UNDER AND AROUND SHEAR TIE SKIN IS CORRODED. REMOVED CORROSION FROM FUSELAGE SKIN, FAB NEW SECTION OF INNER DOUBLER, FAB SPLICE PLATE DOUBLER IAW DC8 53-2-0, INSTALLED INNER DOUBLER IAW DAC DWG 5613862.
INSPECTION TYPE:C2 C PIT DOOR JAMB T-ANGLE HAS CORROSION FROM STA 1250 L33R. REMOVED CORRODED T-ANGLE, LOCATED & DRILLED NEW ANGLE IAW DC8 SRM 51-1-24. INSTALLED NEW T-ANGLE IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C2 L17L END FITTING CRACKED FS 1769. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21.
INSPECTION TYPE:C2 L17R END FITTING CRACKED AT FS 1769. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21.
INSPECTION TYPE:C2 MAIN CABIN FRAME CORRODED AT FS 1740 BETWEEN L33L TO L33R. REMOVED DAMAGED SECTION OF FRAME AND SPLICED IN NEW SECTION IAW DC8 SRM 53-2-0.
INSPECTION TYPE:C2 MAIN CABIN LONGERON END FITTING CRACKED AT FS 1690 L26RT. REMOVED FITTING, CLEANED, ALODINED & PRIMED IAW DC8 SRM 51-1-8. LOCATED, DRILLED & DEBURRED NEW FITTING IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SRM 51-1-21, 51-1-20D & 51-1-17.
INSPECTION TYPE:C2 C3 CROSS SLIDE DOOR JAMB HAS CRACKED BANANA FITTING AT STA 1260 LONGERON L33R. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C2 C3 CROSS SLIDE DOOR LWR T-BOLT BACK UP FITTING CORRODED AT STA 1242. REMOVED CORRODED FITTING LOCATED, DRILLED UP MODIFIED FITTING AND CLIPS IAW DC8 SRM 53-2-0 FIG 2D. INSTALLED FITTING AND 2 CLIPS IAW DC8 SRM 53-2-0 FIG 2D & 51-1-20D.
INSPECTION TYPE:C2 TAIL CONE ATTACH FITTING HAS CRACK AT L10L. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21.
INSPECTION TYPE:C2 AT O/B SIDE OF LONG 24L STA 857 POSSIBLE CRACK ON LWR FLAT OF BATHTUB FITTING. NDT TO VERIFY REMOVED LONG 24 AND TRAP FITTING IAW DC8 SRM 51-1-20D. DRILLED LOCATED NEW LONG 24 IAW DC8 SRM 51-1-24. INSTALLED NEW LONGERON AND TRAP FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C2 AFT CARGO CORRODED INTERCOSTAL STR 35R AT LIGHTENING HOLE STA 1085. REMOVED CORRODED INTERCOSTAL IAW DC8 SRM 51-1-21, FABBED NEW INTERCOSTAL IAW DAC DWG 9758507, INSTALLED INTERCOSTAL IAW 51-1-21.
INSPECTION TYPE:C2 AFT SIDE OF FS 683 WEB LWR CHORD CRACKED BETWEEN LONGERON 30L AND 32L LOCATED BETWEEN WING CENTER SECTION LWR SURFACE AND FUSELAGE LWR LOBE VIEWED THROUGH REMOVED STRESS PNLS. REMOVED 1 CLIP STA 683 L30L AND 2 CLIP L30L & 31L RCD LOCATED AND DRILLED 2 NEW CLIP IAW DC8 SRM 51-1-24, INSTALLED ALL THREE CLIP IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C2 AFT PIT AFT SIDE OF Z-FITTING CORRODED AT PREV GROUND AREA. REMOVED CORRODED Z-FITTING, LOCATED DRILLED NEW FITTING AND FABBED 2 SPLICE REPAIR ANGLES. INSTALLED NEW FITTING AND SPLICE REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 2D & 51-1-20D.
INSPECTION TYPE:C2 AFT PIT STA 1220 AT L27L Z-FITTING CRACK. REMOVED FITTING, FABBED REPAIR ANGLES, LOCATED DRILLED ANGLES & FITTINGS IAW DC8 SRM 53-2-0 FIG 20. INSTALLED FITTING ANGLES IAW DC8 SRM 53-2-0 FIG 20.
INSPECTION TYPE:C2 R3 DOOR UPPER AFT CORNER HAS CRACK INDICATION FOUND BY RADIOGRAPHIC INSPECTION. REPAIRED DOOR JAMB CORNER IAW DC8 SRM 53-2-0 FIG 16.
INSPECTION TYPE:C2 R3 DOOR LOWER FORWARD CORNER HAS CRACK INDICATION FOUND BY RADIOGRAPHIC INSPECTION. REPAIRED DOOR JAMB CORNER IAW DC8 SRM 53-2-0 FIG 17.
INSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN CRACKED FS 1724 L15R. REPAIRED AREA IAW DC8 SRM 53-2-1.
INSPECTION TYPE:C2 L1 DOOR CORNER UPPER FWD DOUBLER DOES NOT MEET SRM REQUIREMENTS. REPAIRED DOOR JAMB CORNER IAW DC8 SRM 53-2-0 FIG 15.
INSPECTION TYPE:N/A EMERGENCY DISARM LIGHT WILL NOT DISARM. RELAMPED EMERGENCY DISARM LIGHT, OPS CHECK GOOD.
INSPECTION TYPE:B NR 3 ENGINE PYLON AFT SPAR TO CANTED RIB FITTING CRACKED.
INSPECTION TYPE:N/A EMERGENCY DISARM LIGHTS WILL NOT DISARM. RELAMPED EMERGENCY DISARM LIGHT. OPS CHECKS GOOD.
INSPECTION TYPE:N/A EMERGENCY LIGHT WILL NOT DISARM. RELAMPED EMERGENCY DISARM LIGHT, OPS CHECKS GOOD.
INSPECTION TYPE:N/A EMERGENCY DISARM LIGHTS WILL NOT DISARM. RELAMPED EMERGENCY DISARM LIGHT, OPS CHECKS GOOD.
INSPECTION TYPE:N/A 4 CRACKS AT AFT PRESS BULKHEAD 65.5 FROM FLOOR LBL 23 TO LBL 38. REPAIRED IAW DC-8 SRM 53-2-5/3.
INSPECTION TYPE:N/A J-BEAM CRACKED AT AFT PRESS BULKHEAD. REMOVED PREVIOUS REPAIR ANGLE ON BOTTOM FLANGE AND FASTENERS ON UPPER FLANGE FOR REPAIR 0340 . STOP DRILLED CRACK. ROUGH CUT REPAIR ANGLES AND PICKED UP EXISTING FASTENER HOLD 00340.
INSPECTION TYPE: PREFLT, FOUND DURING EMERGENCY LIGHT TEST. SWITCH INTERNALLY BAD DUE TO LIGHTS REMAIN ON WITH SWITCH ON OFF OR DISARMED POSITION. RESET TO S.W. MAKE LIGHT TO TURN OFF. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH AT OVERHEAD PANEL I/A/W WDM. 33-50-01 PAGE 4. AND PERFORMED TEST AS PER 30-50-01(MM). OPS CHECK NORMAL.
INSPECTION TYPE:N/A BTB - CREW REPORTED SMOKE IN COCKPIT. FOUND LEFT CONTROL VALVE NOT FULLY SEATED IN THE DEACTIVATION POSITION DUE TO M202903. LOCKED OUT SAME AND PRESSURIZED MANIFOLD TO VERIFY NO FLOW TO ACM.
INSPECTION TYPE:C123, STA 1120 FRAME TO CUSP FITTING IS CRACKED AT LONG 21L. REMOVED AND REPLACED FITTING IAW DWG 9755584 AND SRM 51-1-20D.
INSPECTION TYPE:C123, STA 1240 LONG 27L DOOR STOP FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755854 AND SRM 51-1-21.
INSPECTION TYPE:C123, STA -12 BL 0 PRESSURE WEB HAS A POPPED RIVET AND A CRACK. REPAIRED IAW SRO8570026.
INSPECTION TYPE:C123, STA 781 FLOORBEAM ATTACH FITTING IS CRACKED AT LBL 24. REMOVED AND REPLACED FITTING IAW DWG 4751820 AND SRM 51-1-20D.
INSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 697.5, 647.5, 635. REPAIRED IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C123, STA 460 FRAME IS CRACKED AT LONG 9R. REPAIRED IAW SRM 53-2-0 FIG 2.
INSPECTION TYPE:C123, STA 180 LONG 33L CARGO TRACK IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED IAW DWG 5759223 AND SRM 51-3-0.
INSPECTION TYPE:C123, STA 960 BL 0 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-3 FIG 8A.
INSPECTION TYPE:C123, STA 220 - 240 LONG 13R SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 5775792 AND SRM 51-1-20D.
INSPECTION TYPE:C123, LEFT WING L/E RIB ANGLE IS CRACKED AT XS 467.323. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5770170 AND SRM 51-1-20D.
INSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21, 51-1-21A.
INSPECTION TYPE:C123, LEFT WING L/E VERTICAL ANGLE IS CRACKED AT XS 256. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753294 AND SRM 51-1-20D.
INSPECTION TYPE:C123, STA 340 - 360 LONG 26L ANGLE O/B SIDE OF TORQUE BOX IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9751879 AND SRM 51-1-21A.
INSPECTION TYPE:C123, LEFT WING L/E AUX TANK RIB IS CRACKED AT XFS 13.75. REPAIRED IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C123, STA 798 FLOORBEAM LBL 50 FLOORBEAM SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3641126 AND SRM 51-1-20D.
INSPECTION TYPE:C123, STA 798 LBL 50 ANGLE FITTING IS CRACKED BELOW FLOORBEAM. REMOVED AND REPLACED FITTING IAW DWG 3643112 AND SRM 51-1-20D, 51-1-21.
INSPECTION TYPE:C123, STA 822 LONG 22R ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4753360 AND SRM 51-1-20D.
INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 622.5. REPAIRED IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C123. STA 320 BATH TUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 35L-36. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG 2D.
INSPECTION TYPE:C123, STA 798 FLOORBEAM TO WING BOX FITTING IS CRACKED AT RBL 50. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3643112 AND SRM 51-1-20D.
INSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 591.25, 616.25, 635, 653.75. REPAIRED IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C123, LEFT WING L/E RIB IS CRACKED AT XFS 347.7. REPAIRED IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C123, STA 1070 - 1080 LONG 21R CUSP IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-5 FIG 15A.
INSPECTION TYPE:C123, STA 660 AT LONG 36 SHEAR TIE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 5616509 AND SRM 51-1-20D.
INSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED AT XFS 491.1. REPAIRED IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED AT XFS 322.7. REPAIRED IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED AT XFS 461.3. REPAIRED IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED AT XFS 354. REPAIRED IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C123, STA 280 LONG 33R BATH TUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755825, AND SRM 53-2-0 FIG 2D.
INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 828.750. REPAIRED IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C123, RIGHT WING L/E SKIN IS CRACKED AT XFS 710. REPAIRED IAW SRM 57-2-1 FIG 2H.
INSPECTION TYPE:C123, RIGHT WHEEL WELL STA 940 FITTING IS CRACKED AT RBL 63. REMOVED AND REPLACED FITTING IAW DWG 3646956 AND SRM 53-2-0 FIG 8.
INSPECTION TYPE:C123, STA 55 FRAME IS CRACKED AT LONG 24R. REPAIRED IAW SRM 53-2-0 FIG 2.
INSPECTION TYPE:C123, STA 55 FRAME IS CRACKED AT LONG 24L. REPAIRED IAW SRM 53-2-0 FIG 2.
EMERGENCY LIGHTS INOPERATIVE. FOUND SWITCH IN ON POSITION. REMOVED AND REPLACED EMERGENCY BATTERY PACK OPS CHECK OK IAW 33-50-0 2.
INSPECTION TYPE:N/A DIVERSION, CAPT EADI FAILED SMOKE IN COCKPIT. CARGO SMOKE DETECTORS BOTH ILLUMINATED AT FL 330 SMOKE IN COCKPIT. REMOVED AND REPLACED CAPT EADI, OPS CHECKS GOOD.
INSPECTION TYPE:N/A, NR 4 ENGINE FLAME-OUT FL350 1717Z OIL PRESS ZERO FLAME-OUT. INFLIGHT ENGINE START AND INFLIGHT ENGINE SHUTDOWN ACCOMPLISHED, MX CONTROL NOTIFIED. FL 310 RE-ATTEMPTED ENG START 1728Z OIL PRESS ZERO. ALL ENG PARAMETERS NORMAL, NO LIGHT OFF. ACCOMPLISHED TASKS ON ENGINE FLAME-OUT, TROUBLESHOOT ER 71-00-00, REMOV ED AND REPLACED FUEL PUMP FILTER ASSY PER 73-10-02. RUN AND LEAK CKS GOOD. ACFT REQUIRES HIGH POWER RUN 51265 REFERENCE LOG PAGE 348432 ITEM.
INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS DID NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY IAW MM 33-50-00, OPS CHECK NORMAL.
INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP ON PRE-DEPARTURE CHECK. REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33-50-01 PAGE 202.
EMERGENCY LIGHT VERY DIM. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT. OPS CHECK NORMAL PER DC8 DC8 MM 33-50-01.
EMERGENCY LIGHT VERY DIM. REPLACED EMERGENCY LIGHT BATTERY PACK AND RELAY UNIT. OPS CK NORMAL PER MM 33-50-01.
INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT'S BATT PACK. OPS CHECK GOOD.
INSPECTION TYPE-N/A, DURING EMERG LIGHTS TEST NO LIGHTS CAME ON. REMOVED AND REPLACED BATT PACK, OPS CK GOOD (P/N 5708458-503) (S/N FLT004) ON, (S/N D95) OFF.
INSPECTION TYPE-N/A, ON ARRIVAL TO SJU LOSS ON HYD PRESSURE. CHECKLIST COMPLETE, HAD TOTAL LOSS OF BRAKE PRESSURE AND DEPLOYED THE AIR BRAKE SYSTEM. REPLACED NR 2 HYD PUMP OUTLET LINE, REPLACED ENG FILTERS AND SERVICED SYS PER M/M 29-00-00 & 12-30-01, SERVICED EMERGENCY BRAKE ACC AND RAN ENGS OPS CHECK NORMAL.
EMERG LIGHTING BATTERY PACK DIMS LIGHTS WHEN ACTIVATED. REMOVED AND REPLACED BATT PACK FOR EEL PER M-M 33-50-01. OP'S CHECK GOOD.
INSPECTION TYPE:C, INTERCOSTAL AT LONG 33R BTWN STA 1160-1180 IS CRACKED AND HAS LIGHT CORROSION. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9754949 AND SRM 51-1-20D.
INSPECTION TYPE:C, FITTING AT STA 1180, LONG 35L IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758497 AND SRM 51-3-0.
INSPECTION TYPE:C, FITTING AT STA 1180, LONG 35L IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-3-0.
INSPECTION TYPE:C, FITTING AT STA 1180, LONG 35R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758496 AND SRM 51-3-0.
INSPECTION TYPE:C, FITTING AT STA 1180, LONG 33R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-3-0.
INSPECTION TYPE-C, FS 280 TO 300 LONGERON 29L CORRODED. REPAIRED IAW SRM 53-2-2 AND 53-4-1.
INSPECTION TYPE-C, FS 280 TO 300 STR 28L CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-2 AND 53-4-1.
INSPECTION TYPE-C, FRAME FITTING JUST UNDER LT CUSP CRACKED AT FS 1280. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.
INSPECTION TYPE:C, MAIN DECK FLOORBEAM SUPPORT FITTING AT STA 1200 AND STR 27R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9754024 AND SRM 51-1-20D.
INSPECTION TYPE-C, INTERCOSTAL LWR ATTACH ANGLE JUST FWD OF FS 1160 ABOVE LONG 35R CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE:C, LONGERON TO INTERCOSTAL TIE FITTING AT STA 1180 AND LONG 35R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758497 AND SRM 51-1-20D.
INSPECTION TYPE:C, STA 440-460 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-3-0.
INSPECTION TYPE:C, STA 440-460 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-3-0.
INSPECTION TYPE:C, RT LEADING EDGE BETWEEN NR 3 AND NR 4 ENG OUTBOARD SLOT ATTACH BRACKET TO STUB WING RIB IS CRACKED. REMOVED, FABRICATED AND REPLACED IAW DWG 5769857 AND SRM 51-1-21.
INSPECTION TYPE-C, FS 300 AT STR 33R FRAME FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE:C, STA 435 ABOVE STR 33L, CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5887623 AND SRM 51-3-0.
INSPECTION TYPE-C, FS 1300 TO 1320 LONG 32R FWD INTERCOSTAL ATTACH CLIP HAS EXTREME CORROSION AND AFT ATTACH CLIP IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT CLIPS IAW SRM 51-1-21 AND DWG 4758514-11 AND -12.
INSPECTION TYPE-C, RT UPPER CABIN WING BOX AREA AT FS 702.8 RBL 25 FLOORBEAM SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C, FRAME HAS HEAVY CORROSION UNDER NUT PLATE AT FS 1060 LONG 36. REPAIRED IAW DHC SK-802-676.
INSPECTION TYPE:C, LONGERON SPLICE FITTING BETWEEN STA 1040-1060 LONG 31R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-3-0.
INSPECTION TYPE-C, C PIT FLOOR TRACK SUPPORT HAS CORROSION UNDER NUT PLATES FROM FS 980 TO 1200 LONG 33L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK SUPPORT IAW SRM 51-1-21 AND DWG 5751516.
INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 622.500, REPAIRED IAW SRM 57-2-0.
INSPECTION TYPE:C, LT WING L/E RIB CRACKED ON UPPER ARM BY AFT FASTENER STA XFS 585.000, REPAIRED IAW SRM 57-2-0.
INSPECTION TYPE:C SPLICE FITTING FROM F/S 600-620 LONG 31L CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE:C, STA 980-1070 AT STR 33R, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5759229 AND SRM 51-3-0.
INSPECTION TYPE-C, RMLG W/W O/B FWD CORNER AT FS 880, FWD LWR SIDE OF FITTING HAS HEAVY CORROSION LONGERON 24. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE:C, LT WING L/E UPPER RIB ATTACH CLIP CRACKED AT STA XOLDI 6.225. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT CLIP IAW SRM 51-1-20D AND DWG 5769857.
INSPECTION TYPE:C, THE RIGHT OUTBOARD SLOT OUTBOARD UPPER CLOSURE RIB IS CRACKED. REMOVED AND REPLACED CLOSURE RIB IAW DWG 5769857 AND SRM 51-1-20D.
INSPECTION TYPE:C, LT WING L/E LWR SURFACE HAS HEAVY CORROSION 3 INCHES AFT OF L/E AT STA XFS710.000. REPAIRED AREA IAW SRM ADDENDUM DC8-5720-4087-A.
INSPECTION TYPE:C, FRAME AT LWR FLANGE AT STA 1580 HAS HEAVY CORROSION BETWEEN LONG 35L - 35R. REPAIRED AREA BY REPLACEMENT AND SPLICING IAW SRM 53-2-0 FIG 2.
INSPECTION TYPE:C, STA 660 AT STR 22R, THE FRAME HAS A 3 INCH CRACK. REMOVED, FABRICATED AND REPLACED FRAME CAP IAW DWG 3646688 AND SRM 51-1-20D.
INSPECTION TYPE:C, F/S 640 BETWEEN STR 26L-27L - SHEAR TIE HAS 3 CRACK. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-2-0 FIG 2B.
INSPECTION TYPE:C, F/S 640 BETWEEN STR 26R-27R - SHEAR TIE IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SHEAR TIE IAW SRM 53-2-0.
INSPECTION TYPE-C, FRAME LWR FLANGE AT STA 1600, HAS CORROSION AT LONGERON 34L TO 34R. REPAIRED AREA IAW DWG 2641520 AND SRM 53-2-0 FIG 2.
INSPECTION TYPE-C, NR 2 TO NR 4 LEFT HAND LEADING EDGE SPAR ATTACHMENT HOLES HAVE CRACKS. REAMED HOLES 2 + 3 TO .500 REAMED HOLE 4 TO .747 NO CRACKS NOTED. FABRICATED AND INSTALLED BUSHINGS ANGLE DOUBLERS, FILLERS AND STRESS COI NED ALL HOLES IAW DAC DWG J060232 AND REO 02487 ANAD DPS 3.67-56
INSPECTION TYPE-C, NR 2 TO 5 HOLES HAVE CRACKS ON RT L/E SPAR ATTACHMENT HOLE INB OF NR 4 PYLON REAMED HOLES 2, 4, 5 TO .500 AND NR 3 HOLE TO .747, NO CRACKS NOTED. FABRICATED AND INSTALLED BUSHINGS, STRAPS, FILLERS AND ANGLES IAW DAC DW G J06032 AND DC8 SRM 51-9-0 AND REO 02493.
INSPECTION TYPE-C, NR 2 MAIN TANK ACCESS PLATE 505F LAND IS CRACKED AT FASTENERS LOCATION MARKED IN RED. REMOVED FASTENERS, REMOVED DAMAGED AREA OF LAND, FABED DOUBLER AND FILLER IAW DC8 SRM 57-2-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED REPAIR IAW DC8 SRM 51-1-21 AND 57-2-1.
INSPECTION TYPE-C, CRACK INDICATIONS NOTED HOLE F IN SPAR, HOLES C AND D IN SKIN/SPAR INTERFACE OF RT WING C/W S/B 57 88 PER UPS EO DC8 5730.
INSPECTION TYPE-N/A, EMERGENCY LIGHTS WEAK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK.
CGN - ON CLIMBOUT, RT MAIN LANDING GEAR DOOR ACTUATOR SWIVEL GLAND SHAFT WAS FOUND TO HAVE SHEARED AND MIGRATED OUT, JAMMING THE DOOR SEQUENCING MECHANISM DURING GEAR RETRACTION, CAUSING THE RT MAIN LANDING GEAR DOOR FILLET TO CONTACT NR 3 FWD AND AFT TIRES. RT MAIN LANDING GEAR DOOR REPAIRED AND INSTALLED IAW MM 32-12-01. NEW MAIN LANDING GEAR DOOR ACTUATOR, CONTROL VALVE, SWIVEL GLAND SHAFT AND ADJUSTABLE LINK ASSY INSTALLED IAW MM 32-32-01 (02). OPERATION AND INDICATION NORMAL ON GEAR SWING.
WHILE IN C CHECK, MAINTENANCE FOUND NR 5 FLAP VANES DELAMINATED ON LEFT AND RIGHT WINGS. REPLACED VANE ASSYS PER MM 27-51-14.
WHILE IN C CHECK, MAINTENANCE FOUND NR 3 LEFT AND RIGHT FLAP VANES DELAMINATED. REPLACED VANE ASSYS PER MM 27-51-14.
WHILE IN C CHECK, MAINTENANCE FOUND FINGER DOUBLER CRACKED AT FS 178, LONGERON 31L. REPLACED FINGER DOUBLER SECTION PER SRM 51-1-20D.
WHILE IN C CHECK, MAINTENANCE FOUND LONGERON FITTING CRACKED AT FS 680, LONGERON 11R. REPLACED FITTING PER SRM 51-1-20D.
WHILE IN C CHECK, MAINTENANCE FOUND VERTICAL STAB LEADING EDGE, 4 RIBS CRACKED AT STA ZFS 217, ZFS 36, ZFS 104, AND ZFS 123. REPAIRED RIBS PER SRM 55-2-0.
WHILE IN C CHECK, MAINTENANCE FOUND CASTING HAS .5 INCH LONG CRACK AT FS 200, LONGERON 26R. REPLACED CASTING PER SRM 51-1-20D.
WHILE IN C CHECK, MAINTENANCE FOUND LEFT WING STRINGER END FITTING CRACKED AT STA XW 463 AFT OF CENTER SPAR UPPER. REPLACED FITTING PER SRM 51-1-20D.
WHILE IN C CHECK, MAINTENANCE FOUND CRACK AT THE NR 1 PYLON FORWARD HOLE OF THE INBD. SKATE ANGLE LOWER FRONT SPAR.
WHILE IN C CHECK, MAINTENANCE FOUND WEBBING CRACKED AT LONG 21R, FS 1572 AND FS 1592. REPAIRED LONGERON WEB PER SRM 53-2-0.
WHILE IN C-CHECK, MAINTENANCE FOUND LEFT AND RIGHT PRIMARY HEAT EXCHANGER EXHAUST ON LOWER FUSE SKIN DOUBLER CUTOUTS CRACKED AT AFT LOWER CORNERS. REPAIRED PER UPS DC8-5330-4732-0.
WHILE IN C CHECK, MAINTENANCE FOUND LONGERON 1R END FITTING CRACKED AT FS 857. REPLACED FITTING PER SRM 51-1-20D.
WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 29R END FITTING, FS 70. REPLACED FITTING PER SRM 51-1-20D, 51-3-0.
WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM SIDE OF DOUBLER, AT RT SIDE OF FLIGHT DECK SUB FLOOR, FS -86. REPLACED DOUBLER PER SRM 53-01-0, 51-1-20D.
WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION AND DELAMINATION ON LWR VERTICAL STAB L/E BOTTOM SPLICES. REPLACED SPLICE STRAPS (2EA) PER SRM 51-1-9.
WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME FITTING, LONGERON 21L, FS 717. REPLACED FITTING PER SRM 51-1-20D.
WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON END FITTING, LONGERON 24R, FS 70. REPLACED FITTING PER SRM 51-1-20D, 51-1-21.
WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON END FITTING, LONGERON 36, FS 70 TO 80. REPLACED FITTING PER SRM 51-1-20D.
WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 34R END FITTING, FS 70. REPLACED FITTNG PER SRM 51-1-20D.
WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON END FITTING, LONGERON 31R, FS 70. REPLACED FITTING PER SRM 51-1-20D.
WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON DOUBLER JOINING FLOOR TO FUSELAGE, FS -80 TO -70 LT. REPLACED DOUBLER PER SRM 51-1-21.
WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FRAME FITTING, FS 1270 TO 1280, LONGERON 33R. REPLACED FITTING PER SRM 51-1-20D.
WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 28L, FS 1085. INSTALLED REPAIR PER SRM 53-2-2.
WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION AFT BB LT TUNNEL ON BELT FRAME SPLICE, BS 1080 LONGERON 24L. REPLACED SPLICE PER SRM 51-1-20D.