N808UP
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 BRAKE INOPERATIVE DURING TAXI. REPLACED THE COPILOTS SIDE MASTER CYLINDER & HOSE. TAXI CHECK COMPLIED WITH. ACFT RTS.
INSPECTION TYPE:N/A JUMP SEATER OPENED DOOR WITH RAFT ATTACHED. REPACKED EMERGENCY DOOR SLIDE AND SECURED. CHECK OK.
INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. EMERGENCY LIGHT SYSTEM OPS CKS GOOD PER MM 33-50-02-2.
A/C IS OOS DUE TO FUSELAGE DAMAGE CAUSED BY OTHER CARRIER'S BAGGAGE CART. REPAIRED PER UPS EO DC8-5330-29309-A.
INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK.
FWD LT CREW ENTRY DOOR BOTTOM BRACKET ON SLIDE CASE IS BROKEN CASE SLIDE WILL NOT CLOSE AND SECURE. DEFERRED PER MEL 34-7-4, M 372532. INSTALLED, INSTALLED EMER EVAC SLIDE PACK IAW 25-60-01-2. THIS CLEARS M-372532.
CLIMBING THRU FL250 CABIN PRSR/ALT WARNING HORN SOUNDED. CABIN ATL WAS 13000 FT AND CLIMBING AT 4000 FPM. LOCKED OUTFLOW VLV CLOSED AND TURNED BOTH PACKS TO MAX. NO OTHER LIGHTS OR INDICATIONS. WENT BACK TO AUTO AND WORKED OK. BOTH PACKS WERE AT MINIMUM AT TIME OF PROBLEM. PRESSURIZED A/C, FOUND (L) OVER-PRESS. RELIEF VALVE OPENING PREMATURELY. DEFERRED PER MEL 21-10-2, MEL NR 371331. PRESSURIZED A/C, FOUND (L) OVER-PRESS. RELIEF VALVE OPENING PREMATUREL Y. REF AMM 21-31-05-2. ADJUSTED LEFT CABIN PRESSURE SAFETY VALVE TO 1/4 TURN COUNTER CLOCKWISE TO INCREASE CRACK PRESS DIFFERENTIAL CRACK POINT. OPS CHECKS GOOD ON GROUND. M371331 CLOSED.
INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-01-2. CHECKS GOOD.
CAPTAIN'S ESCAPE ROPE COVER FELL OFF, ROPE UNCOILED. REPACKED AND STOWED ESCAPE TAPE AND REINSTALLED AND RESECURED ACCESS DOOR ON CAPTAIN'S ESCAPE ROPE, REF MM 25-60-02-2.
EMERGENCY EXIT LIGHTS WON'T CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER AMM 33-50-00-4.
INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT DISARM. REPLACED LAMP FOR "DISARM" LIGHT. OPERATION CHECK GOOD PER DC8 AMM 33-50-00.
INSPECTION TYPE:C2 CRACK ON FWD STRINGER END FITTING AT XRS 204 FROM STRINGER S-62 - S-63. REMOVED END FITTING AT STA XRS 204 S-62 - S-63 IAW SRM 51-03-02, FABRICATED AND INSTALLED END FITTING AT STA XRS 204 STRINGER S-62 TO STRINGER S-63 IAW DWG 5615767 AND SRM 51-1-20D.
INSPECTION TYPE:C2 HFEC AND VISUAL INSPECTION DETECTED A .125 INCH CRACK ON THE C-2 DOOR LWR FWD DOOR JAMB CORNER. REPAIRED C-2 DOOR LWR FWD DOOR JAMB CORNER IAW SRM 53-02-00-0 FIG 22, AND SRM TR 53-187.
INSPECTION TYPE:C2 FLOORBEAM STA 1300 RBL 12 HAS EXFOLIATION CORROSION BETWEEN FLOORBEAM AND FLOORBOARD. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER. IAW SRM 51-1-8, 53-7-3 FIG 10, 51-2-1 FIG 1 SHT 7, TR 51-130 NOTE 19.
INSPECTION TYPE:C2 STIFFENER IN RT WHEEL WELL STA 857 HAS EXFOLIATION CORROSION. REMOVED STIFFENER AT STA 857 RT WHEEL WELL IAW SRM 51-1-21. FABRICATE AND INSTALLED STIFFENER AT STA 857 RT WHEEL WELL IAW DWG 5613917-19 AND SRM 51-1-20D.
INSPECTION TYPE:C2 BULGING SKIN ON EXTERIOR OF SKIN AT STA 290 L21L AFT OF MAIN CARGO DOOR. REPAIRED FUSELAGE SKIN AT STA 290 L21L AFT OF MAIN CARGO DOOR IAW SAA EA 008-5330-01-A0883, UPS EO DC8-5330-26921-A, AND FAA FORM 8100-9.
INSPECTION TYPE:C2 CENTER WING EXTERIOR FUSELAGE -L- ANGLE CRACKED AT ST 857.125 RBL 65. REMOVED CRACKED -L- ANGLE AT STA 857.125 RBL 65 IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR -L- ANGLE AT STA 857.125 RBL 65 IAW DWG 5649893, AND SRM 51-01-20D.
FOUND 1 DOOR EMERGENCY LIGHT INOP. RELAMPED. OPS CK OK.
MAIN CARGO DOOR EXIT SLIDE FELL OUT OF HOLDER, BROKEN CLIP ON COVER EMERG ESCAPE SLIDE INOP. SLIDE REMOVED FROM DOOR AND DEFERRED IAW MEL 52-07-4 AND ASSIGNED DEFERRAL NR M330482. REPLACED DMGD CLIP ON ESCAPE SLIDE COVER PER SMR 51-01-21. RE- INSTALLED SLIDE ON A/C. THIS CLEARS M330482. OK FOR SERVICE.
EMERG EXIT LIGHTS WOULD NOT TEST. INSTALLED SERVICEABLE EMERGENCY EXIT LIGHT BATTERY PACK PER AMM. OPS CK NORMAL, P/N ON 5708458-503, S/N FTL010.
LOWER CARGO FIRE AMBER MX LIGHT CAME ON AFTER 4 HOURS OF FLIGHT (5 AND 11). PERFORMED ADJUSTMENT AND TEST PER DC-8 M/M 26-18-00-5, NO FAULTS FOUND IN MEMORY OR SIGNAL STRENGTH.
INSPECTION TYPE:N/A DURING ROUTINE MX, EMERGENCY LIGHTING WOULD NOT TEST. REMOVED AND REPLACED BATTERY PACK ASSY IAW AMM 33-50-01-2, EMERGENCY LIGHTING OPS CHECKS NORMAL.
INSP TYPE: C3, D PIT INTERGRANULAR CORROSION ON L34R STA 1412. REMOVED AND REPLACED LONGERON 34R STA 1390-1460 IAW SRM 51-1-21D.
INSPECTION TYPE: C3, LONGERON 14L CRACKED AT STA 1746. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-2-2 FIG 11 AND 51-1-20D.
INSPECTION TYPE:C3 LONGERON CRACKED 1/4 INCH LONG AT STA 1726 L15L. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED STRAPS 2 EA IAW DC-8 SRM 53-02-02, 51-1-8, 53-2-2 FIG 10 AND 51-1-20D.
INSPECTION TYPE: C3, LEFT L/E LWR RIB CRACKED AT XFS 816. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-3-0, 51-1-21 AND 51-1-20D.
INSPECTION TYPE: C3, LT WING L/E LWR RIB CRACKED AT XFS 816. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-3-0, 51-1-21, 51-1-20D AND DWG 5769471.
INSPECTION TYPE: C3, LT WING L/E AT XFS 385.000 LWR RIB CRACKED 2 INCHES LONG MIDDLE OF RIB. FABRICATED AND INSTALLED RIB FORMER AND 2 EA REPAIR ANGLES IAW DWG 5769603, SRM 51-3-2, 57-2-1 AND 51-3-2.
INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED XFS 316.000. REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2, 51-1-21, 51-1-20D AND 51-1-15.
INSPECTION TYPE: C3, LT WING L/E UPPER SKIN FASTENER HOLES CRACKED .125 INCH LONG AT XFS 450. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 57-2-1-0 AND 51-3-2.
INSPECTION TYPE:C3 LT WING L/E AT XFS 454, LWR SURFACE FASTENER HOLES ARE ELONGATED. REMOVE DAMAGE AND INSTALLED DOUBLER AND FILLER IAW EO DC-8 5720- 7767-A AND SRM 51-1-21.
INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB CRACKED AT STA XFS 438. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA REPAIR ANGLE DOUBLERS IAW SRM 53-02-00 FIG 001B, 51-1-21.
INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 408. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2, 51-1-20D AND DWG 5770375.
INSPECTION TYPE: C3, LEFT WING L/E UPPER RIB CRACKED AT XFS 391. STOP DRILLED CRACK, FABBED AND INSTALLED 2 EA DOUBLERS IAW SRM 57-2-0 FIG 2, 57-2-0, 51-1-20D, 51-1-8 AND DWG 5770087.
INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 385.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS 2 EA IAW SRM 57-2-0 FIG 018, 51-1-20D, 51-1-15 AND DWG 5770087.
INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED AT XFS 822.500 .5 INCH LONG. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2 -0, 57-2-0 FIG 2, 51-1-20D, 51-1-21 AND DWG 5769470.
INSPECTION TYPE: C3, LT WING L/E UPPER RIB CRACKED .25 INCH LONG AT XFS 809. STOP DRILLED CRACK AND FABRICATED INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.
INSPECTION TYPE:C3 LT WING L/E UPPER RIB CRACKED 1/4 INCH LONG AT XFS779. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER IAW SRM 57-2-0 FIG 2, DWG 5769470-29 AND SRM 51-1-20D,51-1-21 AND 51-1-15.
INSPECTION TYPE: C3, LEFT WING L/E UPPER RIB CRACKED 1 INCH LONG AT XFS 828.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1B, 57-2-0 FIG 2B, AND DWG'S 5769470-45, 576947U.
INSP TYPE: C3, A/C BAY L30R AT APPROX STA 38 TO STA 58 DOME NUTS UNDER LONGERON HAVE CORROSION OUT OF LIMITS AT ATTACH INTERNAL DOUBLER. R & R INTERNAL DOUBLER AT STA 38-58 L31R AND 2 EA LONGERONS AT STA 8 TO 70 L27R AND L30R IAW SRM 51-1-21 AND 51-1-20D.
INSPECTION TYPE:C3 "D" PIT BETWEEN STA 1340-1360 L30R SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-21 AND 51-1-20D.
STA 1160 SEVERE CORROSION ON BASE OF FRAME AT L33L. REMOVED, FABRICATED AND INSTALLED IAW SRM 51-1-20D, 51-1-20 D, DWG 3755842 AND SK808-785521.
INSPECTION TYPE: C3, LWR CUSP AT STA 153 RT CUSP TO FRAME FITTING AT TORQUE BOX IS CRACKED BOTH UPPER AND LWR OF CUSP, LENGTH OF FITTING. REMOVED AND REPLACED FRAME FITTING IAW SRM 51-1-21 AND 51-1-20D.
RT MLG AFT WEB CRACKED AT GEAR CUTOUT LWR CORNER OLD REPAIR CRACKED IN RADIUS. REMOVED WEB, FAB REPLACEMENT WEB AND INSTALLED IAW SRM51-1-21, 51-1-21D, SAA FAB TRAVLER NR 0001 AND 21-1-21A.
RT MLG WW FWD BULKHEAD LOWER SECTION FASTENERS HAVE MILD CORROSION IN SEVERAL PLACES RUNNING INBD TO OTBD AT SPLICE. REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW SRM 53-2-0. HFEC INSP DETECTED 3 CRACKS. FABRICATED AND INSTALLED 3 EA. REPAIR ANGLES AND 1 SPACER IAW SRO 08570009, 51-3-2, 51-1-20D, 51-1-21 AND 51-3-0.
INSPECTION TYPE:C3 C-1 CARGO FITTING CRACKED AT FS 280 L32R. FOUND ON X-RAY OF DOOR CORNER EO DC8-5330-20206-B. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-2.
LT FWD UPPER AC BAY AT APPROX STA 8 WEB IS CRACKED APPROX 4 INCH LONG IN 2 PLACES. FABRICATED AND INSTALLED 2 DOUBLERS AND REPAIR WEB IAW SRM 53-03-03-0, 53-02-00-0 FIG 001D, 53-2-0 FIG 1D 51-1-21,51-1-20D AND 51-1-21A.
INSPECTION TYPE:C3 FUSELAGE SKIN AT APROX STA 1723 L16L HAS CRACK APROX 3/4 INCH LONG. REMOVED EXISTING DOUBLER AND FINGER DOUBLER AND FABRICATED EXTERNAL DOUBLER AND INSTALLED EXISTING FINGER DOUBLER, EXTERNAL DOUBLER AND FILLER IAW DC-8 SRM 51-1-21, 51-1-20D, 53-2-1 FIG 7, 51-1-20D AND 51-1-11.
INSPECTION TYPE:C3 FUSELAGE SKIN AT APROX STA 1723 RT L16 HAS CRACK APROX. 1/2 INCH LENGTH. CUT OUT DAMAGE AND INSTALLED DOUBLER, FINGER DOUBLER FILLER AND EXTERNAL DOUBLER IAW SRM 53-02-01-0 FIG 007.
CAPTAIN'S LT SIDE WINDSHIELD CRACKED. BACK TO BLOCK. REMOVED AND REPLACED LT SIDE WINDSHIELD, WINDSHIELD HEAT CONTROLLER, LOWER POWER RELAY AND HIGH POWER RELAY IAW DC8 AMM 56-10-02-2, OPS CHECK GOOD.
F/O OXYGEN REGULATOR LEAKING. REMOVED AND REPLACED 02 BOTTLE IAW MM 12-70-01-3, NO LEAKS NOTED.
INSPECTION TYPE: C1, LT WING AT STA. XRS 74 OB SIDE STRINGER 51 END FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3704841, AND SRM. 51-1-20D
INSPECTION TYPE: C1, LT WING FITTING AT REAR SPAR AT XRS 446 AT REAR SPAR REMOVED,FABRICATED AND REPLACED FITTING I.A.W. DWG. 4640309 AND SRM. 51-1-20D
INSPECTION TYPE: C1, INTERCOSTAL ATTACH FITTING IS CRACKED AT STA. 1230 LONG. 33R REMOVED AND REPLACED FITTING IAW DWG. 4758514,AND SRM. 51-1-20D
INSPECTION TYPE: C1, REPAIR DOUBLER AT FS 237 AT LONG. 5R HAS BLIND FASTENERS AND DOES NOT COMPLY WITH SRM. PER. EO. DC8-5330-12800-D REMOVED EXISTING DOUBLER,CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED DOUBLER,FILLER,AND FINGER DOUBLER I.A.W. SRM. 53-2-1 FIG. 7
INSPECTION TYPE: C1, STATION 380-400 LONGERON 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG. 3754473 AND SRM. 51-1-20D
INSPECTION TYPE: C1, STA. 660 - 680 LONG. 11 LT SPLICE FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 5750540,AND SRM. 51-1-20D
INSPECTION TYPE: C1, RT WING CENTER LE. SUPPORT ANGLE AT XS 520 IS CRACKED. REMOVED,FABRICATED AND REPLACED ANGLE IAW DWG. 9753297,AND SRM. 51-1-20D
INSPECTION TYPE: C1, FREON SYSTEM EXHAUST DOOR AFT LOWER CORNER STA 55 HAS A STAINLESS DOUBLER, DOES NOT COMPLY IAW EO DC8-5330-12800-D, AND IS CRACKED AT STA 52. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-2-0 FIG 13, NDT VERIFIED NO CRACKS AT CUTOUTS.
INSPECTION TYPE: C1, MAIN CARGO DOOR OPENING AFT LOWER CORNER STA. 270 HAS A STAINLESS STEEL DOUBLER THAT DOES NOT COMPLY IAW DC8-5330-12800-D LONG. 20L-21L APPROX. REMOVED EXISTING REPAIR,NDT VERIFIED NO CRACKS AROUND EXISTING CUTOUT,FABRICATED DOUBLERS AND FILLER I.A.W SRO8530027
INSPECTION TYPE: C1, LT NOSE WHEEL WELL TUNNEL, PRESSURE WEB IS CORRODED BEYOND LIMITS OUTBOARD OF HEAT EXCHANGER SUPPORT BRACKET AT STA -68 AT APPROX LBL 64. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, SPLICE, DOUBLERS, FINGER DOUBLERS IAW REPAIR DWG SRO8530026 AND SRM 51-1-20D, 51-3-0.
INSPECTION TYPE: C1, R-2 DOOR UPER AFT CORNER FOUND 1.450 INCHES AND 1.740 INCHES CRACKS IN SKIN AND LONG. 11R AT STA. 1660 CUTOUT DAMAGEIN SKIN AND STOP DRILLED CRACK IN LONG. 11R,NDT VERIFIED NO CRACKS AT CUTOUT AND STOP DRILL TERMINATES CRACK IN LONG., FABRICATED AND INSTALLED DOUBLER,TRIPLER,FILLER AND STRAP I.A.W. SRM 53-2-0 FIG. 21 AND SAA SK 808-475
INSPECTION TYPE:C1 REMOVE L-2 DOOR LOWER FWD. CORNER DOUBLER AND REPAIR PER SRM. 53-2-0 FIG. 18 CUTOUT DOES NOT CONFORM,STA. 1620 LONG. 20L. REMOVED EXISTING REPAIR,CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM.53-2-0 FIG. 18.
INSPECTION TYPE: C1, STATION 1700 LONGERON 11L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG. 4772397 AND SRM. 51-1-20D
INSPECTION TYPE: C1, HFEC INSP. OF L-1 DOOR FWD. UPPER CORNER DETECTED A CRACK COMING FROM THE EDGE OF THE CUTOUT EXTENDING FWD AND UP APPROX. 2.375 INCHES AT STA. 25 LONG. 10L REMOVED EXISTING REPAIR, CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER,TRIPLER, AND FILLER IAW SRM. 53-2-0 FIG. 15 AND SAA SK 808-031
INSPECTION TYPE:C1 STA 960-980 AT LBL 66 FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5645332 AND SRM 53-1-0, 53-2-0 FIG 1F, 51-1-21.
INSPECTION TYPE: C1, UPPER LT SIDE OF RUDDER LE. AREA HAS A 1.5 INCH CRACK AT ZR 298.1255 3.5 INCHES FWD. OF HINGE LINE STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER,CALCULATED RUDDER BALANCE,CALCULATED IN LIMITS AND UPDATED TAG WITH NEW MOMENT OF 2532.127 IN/LBS IN LIMITS,I.A.W. SRM. 55-2-0,51-4-6,51-4-8
INSPECTION TYPE: C1, AFT FUSELAGE INSIDE 60 HOLE LONG. 17R IS CRACKED AT STA. 1776 APPROX REMOVED,FABRICATED AND REPLACED LONGERON IAW SRM. 53-5-0,51-1-20D AND DWG. 5649327
INSPECTION TYPE: C1, STATION 1153 AT LONGERON 19R INSIDE HOLE HAS A CRACKED STRINGER CLIP. REMOVED AND REPLACED CLIP IAW DWG. 4750419 AND SRM. 51-1-20D
INSPECTION TYPE: C1, RT LONGERON 6R FWD OF PRESSURE BULKHEAD AT STA 1766 BRACKET IS BROKEN REMOVED,FABRICATED AND REPLACED BRACKET I.A.W. DWG.5773844 AND SRM. 51-1-20D
INSPECTION TYPE: C1, LT WING IB. FLAP OB. LOWER SKIN IS GOUGED BEYOND LIMITS APPROX 25 INCHES AFT OF LE. BETWEEN XW101 TO XW 115. REMOVED, FABRICATED AND REPLACED SKIN IAW DWG 5652281,AND SRM. 51-1-21,51-3-0
INSPECTION TYPE: C2, AT STA. 1723 CANTED FRAME, LONG.14L IS CRACKED. CUT OUT DAMAGED LONG. SECTION FABRICATED AND REPLACED LONGERON SECTION I.A.W. SRM. 53-2-03 FIG. 10
INSPECTION TYPE: C1, STA. 45-70 AT APPROX. LBL. 48 AT OVERHEAD IN AC BAY HAS A CRACKED FITTING. REMOVED,FABRICATED AND INSTALLED FITTING IAW DWG. 5890314,AND SRM 51-1-20D,51-3-0
INSPECTION TYPE: C1, MAIN CABIN AFT PRESSURE BULKHEAD IS CRACKED AT STA 1766 RBL 35 AT APPROX 66 INCHES ABOVE FLOOR LEVEL. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER IAW SRM 53-2-5 FIG 14A, FOUND TO BE WITHIN RANGE LIMITS OF PREVIOUSLY INSTALLED REPAIR IAW SRM 53-2-5 FIG 14A.
INSPECTION TYPE: C1, HFEC HOLE INSPECTION DETECTED A CRACK ON THE RT WING FORWARD LOWER SPAR BETWEEN STA. XFS 515-XFS 526.76 IN HOLE NR 8 (PG. 15 OF E.O. DC8-5710-14184-D) COINED 10 EA. HOLES IN CONDITION 1, COLD WORKED 1 HOLE IN CONDITION 2 NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED FLUSH REPAIR BUSHING IAW DWG.4709980, E.O. DC8-5710-14184APPX. E,DWG. J060232,AND SRM. 51-3-5
INSPECTION TYPE:C1 LT FUSELAGE SKIN IS DENTED AT STA 300 AT LONG 20L. REWORKED DENT, FOUND WITHIN LIMITS, NDT VERIFIED A .375 INCH CRACK AT DENTED AREA. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AROUND CUTOUT. FABRICATED AND INSTALLED DOUBLER FILLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.
INSPECTION TYPE: C1, RT WING L/E UPPER RIB IS CRACKED AT FASTENER END AT XFS 826.750. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED STACK ANGLE DOUBLER REPAIR IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE: C1, RIGHT WHEEL WELL AT STA. XW 5 AFT T-CAP STRUT FOR TE. IS CRACKED REMOVED,FABRICATED AND REPLACED STIFFENER I.A.W. 9887427,AND SRM. 51-1-20D
INSPECTION TYPE: C1, RIGHT WHEEL WELL OUTBOARD STA. 940 UPPER BEAM FITTING IS CRACKED AT LONG. 24R REMOVED AND REPLACED FITTING I.A.W. DWG 4619810,AND SRM. 51-1-20D
INSPECTION TYPE: C1, REMOVE L2 UPPER AFT CORNER STEEL DOUBLER PER EO DC8-5330-12073-H STA 1660 LONG 10L. REMOVED EXISTING REPAIR, NDT VERIFIED NO CRACKS AT EXISTING CUTOUT. FABRICATED DOUBLER AND TRIPLER, REINSTALLED FILLER AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 17.
INSPECTION TYPE:C1 TWO STOP DRILLED HOLES ON OUTER SKIN AT STA 400 LONG 30R. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.
EMERGENCY LIGHTS DISARMED LIGHT INOP WITH SWITCH DISARMED. REPAIRED BROKEN WIRE AT TERMINAL A2 ON SWITCH S1-327 REF WDM 33-50-01. OPS CHECK GOOD.
INSPECTION TYPE:PFLT EVACUATION SLIDE BAR STUCK IN THE EVAC SLIDE, UNABLE TO ARM SLIDE. REPLACED EVAC SLIDE.
INSPECTION TYPE:C2 AT STA -67 SUB FLOOR RT SIDE CORROSION AT CUSP IN FLT DECK REPAIRED SUBFLOOR AT STA -67 AT CUSP AREA DAC DWG SRO 8530026
INSPECTION TYPE:C2 FLOORBOARD STA 1040 BETWEEN RAILS E & F CORRODED REPAIRED AREA IAW DC8 SRM 53-2-3
INSPECTION TYPE: C2, MAIN CABIN STA 880 PRESSURE DECK FLOORBEAM ON TRACK G RBL 65 IS OUT OF LI MITS AND HAS BARE METAL. REPAIRED AREA IAW TSRM STD-5310-001
INSPECTION TYPE: C2, MAIN CARGO FLOOR SUPPORT AT STA 1684 LT SIDE AFT OF PANEL F210 CORRODED AROUND HOLES REMOVED SUPPORT FABBED NEW SUPPORT .
INSPECTION TYPE: C2, FRAME AT FS -67 HAS CORROSION AT CUSP AREA. REMOVED ''Z'' ANGLES AND INTERCOSTAL TO GET ACCESS TO FRAME CUT OFF DAMAGED SECTION OF FRAME IAW REO-G07891 FABED -17 FRAME SECTION IAW DAC DW G 5613784 FABED -27 -25 SPLICES IAW REO G07891 HEAT TREATED FRAME SE CTION AND SPLICES IAW TPS-1003 REV A ALODINED & PRIMED FRAME SECTION AND SPLICES IAW DC8 SRM 51-1-8
INSPECTION TYPE: C2, LT AFT PRESSURE BULKHEAD CRACKED STA 1766, 11LT REPAIRED AREA IAW DAC DWG SRO 8530007
INSPECTION TYPE: C2, RT AFT PRESSURE BULKHEAD CRACKED AT STA 1766, 11RT REPAIRED AREA IAW DAC DWG SRO 8530007
INSPECTION TYPE:C2, KEELBEAM AREA BETWEEN MLG DOORS STA 830, LT ATTACH ANGLE CRACKED. FABED AND INSTALLED NEW ATTACH ANGLE IAW DAC DWG 4645535 AND DC8 SRM 51-1-20D
INSPECTION TYPE:C2 LT MLG WW CRACKED IN VERT LEG OF TRAPEZOIDAL FITTING FS 902 LONG 24 LT. STOP DRILLED CRACK IAW UPS EO DC8-5340-0748 2B CRACK CONDITION REPAI R PREVIOUSLYCOMPLIED WITH IAW UPS EO DC8-5340-0748 NO FURTHER ACTION REQUIRED AT THIS TIME
INSPECTION TYPE: C2, AFT LWR CARGO PIT FS 1180 IN CEILING. FLOORBEAM END FITTING IS CRACKED. REMOVED INTERCOSTAL AND FLOORBOARD TO GAIN ACCESS TO FASTENERS & REMOVED CRACKED FITTING LOCATED NEW FITTING PN 3754922-501 DIAW DC8 SRM 51-1-21 & 51-3-0
INSPECTION TYPE: C2, AFT CARGO PIT AT FS 1140 ABOVE LONG 36 FRAME IS CORRODED. FABBED ALODINED & PRIMED & INSTALLED -7 REPAIR ANGLE, FILLER, -3 BACK- UP ANGLE & -5 FRAME CAP IAW REO G07893 DC8 SRM 51-1-8 51-1-20D
INSPECTION TYPE: C2, AFT LWR CARGO PIT AT FS 1060 ABOVE LONG 33 RT - 36 FRAME IS CORRODED UND ER AND AROUND NUTPLATES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW 53-2-0 REMOVED FRAME CAP GUSSET & CLIP FOUND GUSSET DAMAGED, OUT OF LIMITS IAW 53-2-0 REC''''D LOCATED & DRILLED NEW FRAME CAP FAB REPAIR IAW STD 5310-602 FAB NEW GUSSET & CLIP IAW DAC DWG 9758507.
INSPECTION TYPE:N/A, EMERGENCY LIGHTS DID NOT CHECK. INSTALLED NEW EMERGENCY BATTERY PACK. ALL WORK DONE IAW MM 33-50-00.
INSPECTION TYPE:N/A, 3 INCH CRACK IN NR 2 PYLON SKATE ANGLE. *S/D* REMOVED CRACKED SKATE ANGLE. LOCATED AND DRILLED AND INSTALLED NEW SKATE ANGLE IAW DWG AND DC8 SRM 51-1-24.
INSPECTION TYPE:N/A, SMOKE CURTAIN NOT ATTACHED TO FLOOR NEAR ENTRY DOOR. SECURED SMOKE CURTAIN TO FLOOR AS REQUIRED. OK FOR SERVICE.
INSPECTION TYPE:N/A, EVACUATION SLIDE GIRT BAR COULD NOT BE INSTALLED BECAUSE OF FLOOR PANEL RAISED TO HIGH. REINSTALLED FLOOR PANEL TO BE FLUSH WITH FLOOR, OPS CHECK GOOD.
INSPECTION TYPE:N/A, ATB-LOUD HOWLING NOISE IN THE COCKPIT COMING FROM THE NOSE AREA IMPEDING COMMUNICATIONS. FOUND LEFT FAN INLET DOOR REMAINS OPEN IN FLIGHT. REPAIRED GROUND AT S3-8012. ALSO, REMOVED AND REPLACED R2-25, DOOR NOW CLOSES WITH GROUND TO FLIGHT SHIFT.
INSPECTION TYPE:N/A AT FL 310 CRUISE FLIGHT, FELT BUMP ND SHUDDER UNDER OUR FEET. PERFORM ED UPLATCH CHECK NORMAL. LOWERED GEAR, GOT AN IMMEDIATE NOSE GEAR DOWN INDICATION AND ALOT OF ABNORMAL NOISE AND SHUDDERING UNDER OUR FEET. ALL HYDRAULIC AND GEAR INDICATIONS NORMAL. NORMAL LANDING FOUND NLG ACTUATOR ATTACH FITTING BROKEN OFF OF LEFT BRACE AND APPROX 3 INCH HOLE IN BULKHEAD. BULKHEAD BEING TEMP REPAIRED AND ACTUATOR & FLEX HYD LINES REMOVED, PREPARING A/C FOR NOSE GEAR DOWN UNPRESSURISED FERRY FLIGHT. REPAIRS CARRIED OUT IAW MM 32-31-03 3B 1-15, SRM 51-01-21, DC8-5330-11499.
INSPECTION TYPE-C3, FS 55 FRAME AT LONG 24R IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED FRAME IAW SRM 53-2-0 FIG 2.
INSPECTION TYPE:C123 STA 1756 AT BLO, THE INTERNAL DOUBLER HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK 808-946.
INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK CORRODED BEYOND LIMITS, FS 320-340, RBL 24. CUT OUT DAMAGED SECTION, FABRICATED, REPLACED SEAT TRACK FS 290 TO 390, RBL 24, IAW SRM 53-2-3.
INSPECTION TYPE-C3, FS 1660 FLOORBEAM AT RBL 45 HAS DOUBLE DRILLED HOLES. REPAIRED FLOORBEAM IAW DH SK808-353.
INSPECTION TYPE-C3, FS 1110 AT LONG 21R, THE FINGER DOUBLER IS CRACKED. REMOVED, FABRICATED & REPLACED THE FINGER DOUBLER IAW DWG 5750321 AND SRM 51-1-21.
INSPECTION TYPE-C3, FS 1210 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C3, FS 1177 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C3, FS 1196 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C3, FS 1187 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C3, FS 1187 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C3, FS 1203 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C123, STA 1300 AT RBL 36, THE FLOORBEAM HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK 808-576.
INSPECTION TYPE-C123, FUSELAGE SKIN (EXT) AT STA 660 BETWEEN STR 35L-36 IS CORRODED. REPAIRED AREA IAW DH SK 808-237.
INSPECTION TYPE-C123, FLOORBEAM SUPPORT BACK-UP FITTING AT STA 280 AT STR 27R IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3754025 AND SRM 51-1-20D.
INSPECTION TYPE-C3, FLOORBEAM HAS HEAVY CORROSION ON THE UPPER FLANGE AT FS 1300, LBL 48. REPAIRED FLOORBEAM IAW DH SK808-870.
INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK AT BL 0, FS 520 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABRICATED AND REPLACED SEAT TRACK FS 450-590 IAW SRM 53-2-3.
INSPECTION TYPE:C123 STA 660 BTWN STR 35L TO 36, THE FUSELAGE SKIN IS CORRODED. REPAIRED AREA IAW DH SK 808-237.
INSPECTION TYPE:C3 FS 1580 AT LBL 48, THE FLOORBEAM UPPER FLANGE IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW DH SK808-839.
INSPECTION TYPE-C123, STA 879 AT LBL 60, THE PRESSURE WEB IS CORRODED. REPAIRED AREA IAW DK SK808-444.
INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK AT FS 1220, LBL 48 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGE, FABRICATED AND REPLACED SEAT TRACK FS 1190-1290 IAW SRM 53-2-3.
INSPECTION TYPE-C123, STA 1340 TO 1360 AT RBL 59, THE SEAT TRACK IS CORRODED OUT OF LIMITS. REPAIRED AREA IAW SRM 53-2-3.
INSPECTION TYPE-C123, STA 150 TO 180 RBL 30, THE SEAT TRACK HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-2-3 FIG 8A.
INSPECTION TYPE:C3 FUSELAGE SKIN IS CRACKED AT FS 1746, LONGERON 16R. CUT OUT DAMAGED AREA, AND REPAIRED IAW SRM 53-2-1 FIG 7.
INSPECTION TYPE:C123 SEAT TRACK BTWN STA 1660-1680 RBL 59 HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-2-3.
INSPECTION TYPE:C123 FUSELAGE EXTERIOR SKIN AT STA 1748 STR 16L IS CRACKED. REPAIRED AREA IAW SRM 53-2-1 FIG 7.
INSPECTION TYPE-C123, STA 1040 TO 1060 AT STR 35R, THE STR SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750545 AND SRM 51-1-20D.
INSPECTION TYPE:C3 SEAT TRACK AT FS 1440, LBL 44 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABIRCATED, AND INSTALLED SEAT TRACK IAW EO DC8-5320-5167C AND SRM 53-2-3 FIG. 8A.
INSPECTION TYPE:C3 FS 1260 AT LONGERON 27R, THE FLOORBEAM SUPPORT IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED FLOORBEAM SUPPORT IAW DWG 3773077 AND SRM 51-1-20D.
INSPECTION TYPE:C3 FLOORBEAM SUPPORT AT FS 1220 IS CORRODED OUT OF LIMITS. REMOVED, FABRICATED, AND REPLACED SUPPORT IAW DWG 9754002 AND SRM 51-1-20D.
INSPECTION TYPE:C3 FS 1100 FRAME CAP LONGERON 31R TO 32R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED CAP IAW 53-2-0.
INSPECTION TYPE:C3 FS 1020 FRAME AT LONGERON 33L IS CORRODED BEYOND LIMITS. CUT OUT DAMAGE, AND REPAIRED IAW SRM 53-2-0.
INSPECTION TYPE:C3 FLOORBEAM SUPPORT ANGLE CORRODED BEYOND LIMITS, FS 1380 AT LONGERON 27R. REMOVED, FABRICATED, AND REPLACED SUPPORT IAW DWG 3773077 AND SRM 51-1-20D.
INSPECTION TYPE:C3 FS 1040 FRAME, BETWEEN LONGERON 31R AND 32R, IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABRICATED, AND REPAIRED IAW SRM 53-2-0.
INSPECTION TYPE:C3 FS 500 FRAME AT LONGERON 7L IS CORRODED OUT OF LIMITS. REPAIRED FRAME IAW SRM 53-2-0.
INSPECTION TYPE-C2, FS 740 TO 880, RBL 60 THE SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK FROM FS 710 TO 910, RBL 60, FABRICATED & REPLACED THE SEAT TRACK IAW SRM 53-2-3 FIG 2.
INSPECTION TYPE:C3 NR 2 MAIN TANK, INBD SIDE OF THE XRS 74 BULKHEAD, THE FWD STR 51 END FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.
INSPECTION TYPE-C3, RT I/B AILERON IS CRACKED, TOP O/B END UNDER THE WEIGHT COVER. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-0 FIG 2A.
INSPECTION TYPE-C123, RT WING AUX TANK L/E AT FS 115.122 HAS HEAVY CORROSION THAT IS OUT OF LIMITS, (SPAR CAP). REMOVED AND REPLACED CAP IAW 9751082 AND SRM 51-1-20D.
INSPECTION TYPE-C123, THE NR 3 MAIN TANK I/B SIDE OF THE XRS74 RIB, THE STR 51 FWD END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.
INSPECTION TYPE-C123, NR 3 MAIN TANK O/B SIDE OF THE XRS 74 RIB, THE STRINGER AFT END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.
INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK AT FS 1140 TO 1100, BL 0, IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABRICATED, AND REPLACED SEAT TRACK FS 1070 TO 1150, BL 0, IAW SRM 53-2-3.
INSPECTION TYPE-C123, RT WING L/E AT STA FS 564 AND 571 THE LWR I/B SKIN DOUBLER IS CRACKED IN 3 PLACES. REPAIRED AREA IAW SRM 57-3-3 FIG 6.
INSPECTION TYPE-C3, LT WING L/E OUTBOARD ATTACH CLIP AT FS 520.168 IS CRACKED. REMOVED, FABRICATED AND REPLACED CLIP IAW DWG 5769580 AND SRM 51-3-0.
INSPECTION TYPE-C3, RT WING L/E RIB AT FS 766.25 IS CRACKED BETWEEN THE AFT LWR TWO FASTENERS. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.
INSPECTION TYPE-C3, LT WING L/E RIB AT FS 354 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 56-2-0.
INSPECTION TYPE-C3, RT WING L/E RIB AT FS 741.25 IS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.
INSPECTION TYPE-C3, RT WING L/E RIB AT FS 760 IS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.
INSPECTION TYPE-C3, LT WING L/E RIB AT FS 372.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.
INSPECTION TYPE-C3, RT WING L/E RIB AT FS 738.75 IS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.
INSPECTION TYPE-C3, RT WING L/E RIB AT FS 760.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.
INSPECTION TYPE-C123, STA 590 AT RBL 24 THE SEAT TRACK SPLICE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED SPLICE FITTING IAW SRM 53-2-3 FIG 6A.
INSPECTION TYPE-C3, RT WING L/E RIB AT XS 484.895 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW SRM 57-2-0.
INSPECTION TYPE-C123, STA 1036 RBL 24, THE SEAT TRACK HAS HEAVY CORROSION, ALSO AT STA 990. REMOVED AND REPLACED SEAT TRACK FROM STA 990 TO 1050 IAW SRM 53-2-3 FIG 8A.
INSPECTION TYPE-C123, STA 1480 AT BL 0, THE SEAT TRACK HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-2-3 FIG 8A.
INSPECTION TYPE-C123, STA 630 AT RBL 59, THE SEAT TRACK HAS HEAVY CORROSION. REPAIRED AREA IAW SRM 53-7-3 FIG 2.
INSPECTION TYPE:C3 FS 1306, BL 0, THE MAIN CABIN SEAT TRACK HAS HEAVY CORROSION. CUT OUT DAMAGED SECTION, FABRICATED, AND REPLACED SEAT TRACK FS 1290-1430, BL0 IAW SRM 53-2-3.
INSPECTION TYPE:C3 SUPPORT FITTING AT FS 1220, LONGERON 21R IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3754025 AND SRM 51-1-20D.
INSPECTION TYPE-C3, LONGERON END FITTING AT FS 1690, LONG 26L IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.
INSPECTION TYPE:C3 FS 1160, LONGERON 27R, THE FITTING IS CRACKED AND CORRODED. REMOVED, FABRICATED, AND REPLACED THE FITTING IAW DWG 3754025 AND SRM 51-1-20D.
INSPECTION TYPE-C123, STA 798 AT STR 13L, THE TIE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4751642 AND SRM 51-1-20D.
INSPECTION TYPE-C123, FLOORBEAM SUPPORT FITTING AT STA 280 RT SIDE IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9754024 AND SRM 51-1-20D.
INSPECTION TYPE-C123, STA 1220 ABOVE STR 27R THE FLOORBEAM SUPPORT BRACE IS CRACKED. REMOVED AND REPLACED BRACE IAW DWG 9754024 AND SRM 51-1-20D.
INSPECTION TYPE-C123, LT O/B LOWER L/E RIB IS CRACKED AT STA FS 622.500. REPAIRED AREA IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE-C3, FS 857 AT LONG 19L THE TIE FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C3, FS 902 AT LONG 19R THE TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C123, RT WING L/E RIB AT STA 520.168 IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE-C3, LT WING L/E LWR SKIN DOUBLER IS CRACKED AT FS 570, AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21.
INSPECTION TYPE-C3, LT WING L/E RIB AT FS 822.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 1B.
INSPECTION TYPE-C3, LT WING L/E RIB AT FS 716.25 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 1B.
INSPECTION TYPE-C3, LT WING L/E RIB AT FS 728.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 1B.
INSPECTION TYPE-C3, LT WING L/E RIB AT FS 753.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 1B.
INSPECTION TYPE-C3, LT WING L/E RIB AT FS 785 IS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 1B.
INSPECTION TYPE-C3, FLOORBEAM ATTACH ANGLE IS CRACKED AT FS 702, RBL 24. REMOVED AND REPLACED THE FITTING IAW SRM 51-3-0.
INSPECTION TYPE:C3 FS 1020 FRAME BETWEEN LONGERON 32R AND 35R IS CORRODED OUT OF LIMITS. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53-2-0 FIG 2.
INSPECTION TYPE:C3 LONGERON 31L SPLICE FITTING CRACKED AT FS 200-220. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE:C3 SEAT TRACK HAS HEAVY CORROSION AT FS 500 LBL 50. CUT OUT DAMAGED SECTION, FABRICATED, AND REPLACED SEAT TRACK IAW SRM 52-2-3 FS 490 TO 580.
INSPECTION TYPE-C3, LONG 1 END FITTING IS CRACKED AT FS 857. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.
INSPECTION TYPE-C3, LONG 22L END FITTING AT FS 300 IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C3, HEAVY EXFOLIATION CORROSION ON FITTING AT FS 1754, BL 0. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE:C3, CUSP ANGLE AT FS 1150, RT SIDE IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FS 1110 TO 1270, FABRICATED AND REPLACED CUSP IAW SRM 53-2-5 FIG 15A.
INSPECTION TYPE-C3, LONG 9R END FITTING IS CRACKED AT FS 678. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C3, STIFFENER ATTACH ANGLE CRACKED ON VERTICAL FLANGE, AFT SIDE OF THE FS 600 FRAME, AT LONG 19R. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5648817 AND SRM 51-1-20D AND 1-1-21.
INSPECTION TYPE-C3, LONG 31L SPLICE FITTING IS CRACKED AT FS 610. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C3, FS 857, RT SIDE OF THE KEEL BEAM, THE ANGLE IS CRACKED. REPAIRED ANGLE IAW SRM 53-2-0.
INSPECTION TYPE:C123 RT FLOORBEAM ATTACH SPLICE AT STA 1660 IS CRACKED. REMOVED, FABRICATED AND REPLACED SPLICE IAW 3751193 AND SRM 51-1- 20D.
INSPECTION TYPE-C3 LONG 31R SPLICE FITTING IS CRACKED AT FS 610. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D.
INSPECTION TYPE-C3, LONG 31R SPLICE FITTING AT FS 1050 IS CRACKED IN 2 PLACES. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
INSPECTION TYPE:C3 EXFOLIATING CORROSION ON LONGERON 33L AT FS 1675. CUT OUT DAMAGED SECTION, FABRICATED AND SPLICED IN LONGERON 33L, IAW SRM 53-2-2 FIG 8.
INSPECTION TYPE-C3, RT WING LWR L/E SKIN AT FS 572.5 IS CRACKED AT THE SCREW HOLE. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4097-B.
INSPECTION TYPE-C3, FS 621 BULKEAD WEB IS CRACKED ABOVE LONG 27L. REPAIRED BULKHEAD WEB IAW SRM 53-2-0 FIG 23.
INSPECTION TYPE-C3, RT WING LWR L/E SKIN AT THE FWD I/B CORNER OF THE O/B SLOT IS CRACKED, STA XOLDI 6.225. REPAIRED SKIN IAW EO DC8-5720-4087-B.
INSPECTION TYPE-C3, LT WING L/E LWR SKIN AT FS 572.5 IS CRACKED AT THE DRAIN HOLE. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087-B.
INSPECTION TYPE-C3, FS 641 BETWEEN LONG 26L AND 27L, THE SHEAR TIE IS CRACKED. CUT OUT DAMAGED SHEAR TIE AND REPAIRED IAW SRM 53-2-0 FIG 2A.
INSPECTION TYPE-C3, RT WING L/E UPPER SKIN, JUST I/B OF THE I/B SLOT IS CRACKED, APPROX STA FS 209. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-7767-A.
INSPECTION TYPE-C3, FS 641 BETWEEN LONG 26R AND 27R, THE SHEAR TIE IS CRACKED. CUT OUT DAMAGED SHEAR TIE AND REPAIRED IAW SRM 53-2-0 FIG 2B.
INSPECTION TYPE-C3, LT WING L/E LWR SKIN AT FS 304.5 IS CRACKED AT 1 FASTENER. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087-B.
INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK, FS 900 TO 960, RBL 45, IS CORRODED OUT OF LIMITS. CUT OUT DAMAGED SECTION, FABRICATED, AND REPLACED SEAT TRACK FS 870 - 990 IAW SRM 53-2-3.
INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK, UPPER FLANGE, LWR SURFACE, FS 1050-1150, RBL 58, IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION, FABRICATED, AND REPLACED SEAT TRACK FS 1050 TO 1170 IAW SRM 53-2-3.
AT FL 330 OBSERVED THE MASTER WARNING LIGHT ON. NO OTHER INDICATIONS ABNORMAL. CHECKED SHORT CIRCUT NR 4 DID NOT TEST IN EITHER POSITION THE WARNING LIGHT CAME ON AGAIN, CHOOSE TO SHUT DOWN NR 4. UNABLE TO DETERMINE IF FIRE EXISTS. AFTER SHUT DOWN NR 4 MAN AIR OVER TEMP LIGHT ILLUM, THEN EXTING ABOUT 20 SEC LATER RT MAN TEMP (SEE HARD COPY). VISUALLY INSP NR 4 ENG PNUE DUCTING FOR COND AND SEC NO DEFECTS. REMOVED AND REPLACED ALL CORE SECTION FIRE DETECTION LOOPS. ALSO REMOVED AND REPLACED WIRE HARNESS FROM PYLON TO ENG, RAN ENGINE AT HIGH POWER AND SYSTEM OPS CK'D GOOD.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND LONGERON 34LT SPLICE FITTING CRACKED AT F/S 1350. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED SPLICE FITTING IAW DC8 SRM 53-2-2 FIG 10, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND CORROSION ON STRAP AT LONGERON 31LT F/S 1165. REMOVED CORRODED SECTION OF STRAP BELOW LONGERON 31LT F/S 1154 TO 1188, DRILLED, TREATED, PRIMED AND INSTALLED NEW SECTION OF STA, REPAIR DOUBLERS AND INTERNAL STRAPS, IAW DAX FAX FILE 97-10-02-011, FAX ACTION NR 346127 AND SKETCH NR5750322 UPS EO DC8-53-2006.
INSPECTION TYPE-C, FOUND FUSE SKIN TO RT WHEEL WELL OTBD BULKHEAD ATTACH ANGLE CORRODED. REMOVED CORRODED ANGLE, FABRICATED, DRILLED, TREATED, PRIME AND INSTALLED NEW ATTACH ANGLE IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21, 51-3-0.
INSPECTION TYPE-C, FOUND CORROSION ON LONGERON 32 LT END FITTING JUST FWD OF FS 70. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND T BOLT FITTING CORRODED ON LOWER SURFACE F/S 1170 (C PIT DOOR). REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-20D.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND C PIT DOOR T BOLT FITTING CORRODED AT F/S 1194. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-3-0.
INSPECTION TYPE-C, FOUND FITTING CORRODED AT FS 1160 BETWEEN LONGERON 36 AND 35 RT. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND T BOLT FITTING CORRODED F/S 1178 (C PIT DOOR). REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-20D.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND GUSSET (FRAME TO INTERCOSTAL TIE PLATE) CRACKED AT F/S 1260 ABOVE LONGERON 33RT. REMOVED CRACKED TIE PLATE, FABRICATED NEW PLATE, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-3-0.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND CORROSION ON C PIT DOOR T BOLT FITTING F/S 1202. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21, 51-3-0.
INSPECTION TYPE-C, FOUND SPLICE FITTING CRACKED AFT OF FS 1690 AT LONGERON 30 LT. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-N/A, FOUND LONGERON 32 RT CRACKED AT BOLT HOLE APPROX FS 1240. REMOVED LONGERON SECTION FROM FS 1230 TO 1350, DRILLED NEW SECTION OF LONGERON, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-1-0 51-1-8, 51-1-20D, 51-1-21.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND CORROSION ON FRAME F/S 1240 ABOVE LONGERON 33RT. REMOVED CORRODED SECTION OF FRAME, FABRICATED NEW SECTION OF FRAME AND REPAIR SPLICES, DRILLED, TREATED, PRIMED AND INSTALLED FRAME AND REPAIR SPLICES IAW DC8 SRM 53-2-0 FIG 2, 51-1-8, 51-1-21.
INSPECTION TYPE-C, FOUND LONGERON 32 LT FITTING CORRODED AFT OF FS 1690. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-C, FOUND INTERCOSTAL TO FRAME SUPPORT BRACKET CRACKED AT FS 1138 ABOVE LONGERON 35 LT. REMOVED CRACKED BRACKET, DRILLED, TREATED, PRIMED AND INSTALLED NEW BRACKET IAW DC8 SRM 53-1-0, 51-1-8, 51-1-20D.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND LONGERON 35RT SPLICE FITTING CRACKED F/S 1260 TO 1280. REMOVED CRACKED SPLICE FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-8, 53-1-0, 51-1-20D.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND CORROSION ON LONGERON 36 SPLICE FITTING F/S 1270. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW SPLICE FITTING IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D.
INSPECTION TYPE-C, FOUND FITTING CRACKED AT LONGERON 35 RT FS 1152. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND LONGERON 35RT SPLICE FITTING CRACKED AT F/S 1350. REMOVED CRACKED SPLICE FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW SPLICE FITTING IAW DC8 SRM 53-1-0, 53-2-2, 53-2-0, 51-1-20D, 51-1-8.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND LONGERON FITTING CRACKED, F/S 1180 BETWEEN LONGERONS 34 AND 35 RT. REMOVED CRACKED FITTING, FABRICATED SPLICE FOR NEW FITTING, DRILLED NEW FITTING AND SPLICE, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0 FIG 2D, 51-1-20D, 51-1-8.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND LONGERON 35LT SPLICE FITTING CRACKED AT F/S 1350. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW SPLICE FITTING IAW DC8 SRM 53-1-0, 53-2-2, 53-2-0, 51-1-20D, 51-1-21.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND LONGERON 32LT SPLICE FITTING CRACKED AT F/S 1350. REMOVED CRACKED SPLICE FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW SPLICE FITTING IAW DC8 SRM 53-1-0, 53-2-2, 53-2-0, 51-1-20D, 51-1-8.
INSPECTION TYPE-N/A, FOUND LONGERON 36 CRACKED FS 1270 TO 1276. REMOVED LONGERON SECTION FROM FS 1260 TO 1350, DRILLED, TREATED, PRIMED AND INSTALLED NEW SECTION OF LONGERON IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-N/A, FOUND LONGERON 35 RT CRACKED FS 1270 TO 1275.5. REMOVED LONGERON SECTION FROM FS 1260 TO 1350, DRILLED, TREATED, PRIMED AND INSTALLED NEW SECTION OF LONGERON IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-C, FOUND INTERCOSTAL TO FRAME SUPPORT BRACKET CRACKED AT FS 1142 ABOVE LONGERON 35 LT. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-20D.
INSPECTION TYPE-C, FOUND CORROSION ON FRAME FS 70 AT LONGERON 33 LT. REMOVED CORRODED SECTION OF FRAME, FABRICATED NEW FRAME SECTION, SPLICE ANGLES, REPAIR DOUBLER, DRILLED ALL NEW PARTS, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-5, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-N/A, FOUND LONERON 33 RT SPLICE FITTING CRACKED AT FS 1490. REMOVED CRACKED SPLICE FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW SPLICE FITTING IAW DC8 SRM 53-1-9, 51-1-8, 51-1-20D, 51-1-21.
INSPECTION TYPE-N/A, FOUND LONGERON 33 LT SPLICE FITTING CRACKED FS 1490. REMOVED CRACKED SPLICE FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW SPLICE FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-20D, 51-1-21.
INSPECTION TYPE-C, FOUND FITTING CRACKED OUTBOARD SIDE OF LT WING FLAP STA 410 SUPPORT FITTING. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC-8 SRM 51-1-8, 51-3-0.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND REINFORCEMENT PLATE ON BOTTOM OF LOWER FRONT SPAR CRACKED AT STA XW408. FABRICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DACO SERVICE REWORK DRAWING SR08570014 AND DC8 SRM 57-1-8, 51-1-21 AND 51-3-0 UPS EO DC8-54-0043.
INSPECTION TYPE-C, FOUND CORROSION ON FITTING AT LONGERON 36, FS 1684. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21.
INSPECTION TYPE-C, FOUND 1 CRACK IN LONGERON 33 RT FS 1640. REMOVED DAMAGED SECTION OF LONGERON, DRILLED, TREATED, PRIMED AND INSTALLED NEW SECTION OF LONGERON AND REPAIR SPLICE IAW DC8 SRM 53-2-2, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-C, FOUND LEADING EDGE ATTACH ANGLE CRACKED AT INBD END OF LEADING EDGE EXTENSION ABOVE NR 1 PYLON. REMOVED CRACKED ANGLE, FABRICATED, DRILLED, TREATED, PRIMED AND INSTALLED ATTACH ANGLE IAW DC8 SRM 57-2-0, 51-1-8, 51-1-21, 51-3-0.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND STATION ARM SLOT ACTUATOR PANEL HAS 1 CRACK AT FASTENER HOLE APPROX XFS 420, FWD OF UPPER FWD WING SPAR. REMOVED CRACKED PANEL, FABRICATED, DRILLED, TREATED, PRIME AND INSTALLED NEW PANEL IAW DC8 SRM 57-1-0, 51-1-8, 51-1-21.
INSPECTION TYPE:C, DURING C-CHECK INSPECTION, FOUND CORROSION ON FLOORBEAM TO INTERCOSTAL TIE BRACKET AT FS 40 BL 28.5 RT. REMOVED TIE BRACKET, REMOVED CORROSION FROM FLOORBEAM, FABRICATED NEW TIE BRACKET, DRILLED, TREATED, PRIMED AND INSTALLED TIE BRACKET IAW DC8 SRM 51-1-8, 51-1-21.
INSPECTION TYPE-C, FOUND LT WING INBD SLOT STATIONARY PANEL CRACKED AT STA XFS254. REMOVED CRACKED PANEL, FABRICATED NEW PANEL, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 57-2-0, 51-1-8, 51-1-21, 51-3-0.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND SPLICE FITTING CRACKED F/S 1270 AT LONGERON 30LT. REMOVED CRACKED SPLICE FITTING, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW SPLICE FITTING IAW DC8 SRM 53-2-0, 51-1-8, 51-1-20D.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND AREA'S OF CORROSION ON INNER SKIN F/S 1050 TO 1350, LONGERON 31LT TO 31RT. REMOVED OUTER AND INNER SKIN F/S 1050 TO 1350 LONGERON 31LT TO 31RT. DRILLED, TREATED, PRIMED AND INSTALLED NEW INNER AND OUTER SKIN IAW DC8 SRM 53-1-0, 51-1-8, 51-1-20D, 51-1-21, 51-3-0.
INSPECTION TYPE-N/A, FOUND CORROSION ON VERTICAL SUPPORT FWD LEG FS 1537.5 FOR CAMLOCK. REMOVED CORRODED SECTION OF VERTICAL SUPPORT, FABRICATED NEW SECTION OF VERTICAL SUPPORT AND REPAIR SPLICES, DRILLED SUPPORT, REPAIR SPLICES, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-8, 51-1-21.
INSPECTION TYPE-C, FOUND PRODUCTION SPLICE FITTING CORRODED AT FS 1690 LONGERON 32 LT REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21, 51-1-20D
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND CORROSION ON LOWER INBD LEG OF FITTING AT F/S 1160 BETWEEN LONG 30 AND 31 LT. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-2-0 FIG 20, 51-1-20D, 51-1-8.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND MAIN CARGO DOOR, UPPER DOOR JAMB (SKIN) COVER ON FUSELAGE CRACKED AT LONGERON 8, F/S 180. FABRICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-0, 51-1-4, 51-1-8, 51-1-21.
INSPECTION TYPE-C, FOUND LT WING INBD SLOT PANEL CRACKED AT STA XW196. REMOVED CRACKED SLOT PANEL, FITTED, DRILLED, TREATED, PRIMED AND INSTALLED NEW SLOT PANEL IAW DC8 SRM 57-2-0, 51-3-0.
INSPECTION TYPE-C, FOUND CORROSION ON PRODUCTION SPLICE FITTING FS 1690 LONGERON 34 RT. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-21, 51-1-20D.
INSPECTION TYPE-C, FOUND RT MLG W/W UPPER BULKHEAD ATTACH ANGLE CRACKED FS 861, BL 47 RT. REMOVED CRACKED ATTACH ANGLE, FABRICATED NEW ATTACH ANGLE, DRILLED, TREATED, PRIME AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-21, 51-1-8, 51-1-20D.
INSPECTION TYPE-C, FOUND CORROSION BEHIND LONGERON 31RT, FRAME TO LONGERON ATTACH CLIPS AT FS 55. REMOVED CLIPS, REMOVED CORROSION FROM FRAME WITHIN LIMITS IAW DC8 SRM 53-2-0 FIG F. FABRICATED NEW ATTACH CLIPS, DRILLED, TREATED PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-20D, 53-1-0.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND CORROSION ON LONGERON 24RT AT F/S 898-900. REMOVED LONGERON 24RT, FITTED, DRILLED, TREATED, PRIMED AND INSTALLED LONGERON 24RT IAW DOUGLAS LONGERON REPLACEMENT GUIDE, AND DC8 SRM 51-1-8, 51-1-21, 51-1-20D, 51-3-0.
INSPECTION TYPE-N/A, FOUND RT LOWER CUSP FITTING CRACKED FS 1580. REMOVED CRACKED CUSP FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 53-1-0, 51-1-8, 51-1-20D, 51-3-0.
INSPECTION TYPE-C, FOUND LONGERON END FITTING CORRODED AT FS 70 LONGERON 33 LT. REMOVED CORRODED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 51-1-21, 53-1-0.
INSPECTION TYPE-C, FOUND FRAME TO CUSP ATTACH CLIP CORRODED FS 140 AT LONGERON 21 RT. REMOVED CORRODED ATTACH CLIP, FABRICATED NEW ATTACH CLIP, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-20D.
INSPECTION TYPE-C, FOUND LT WING INBD FLAP 2 AND 24 CRACK IN UPPER OTBD SKIN APPROX STA XW125. REMOVED CRACKED SKIN, FABRICATED NEW SKIN, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 57-1-0, 51-1-8, 51-1-21.
INSPECTION TYPE-C, FOUND CORROSION ON LONGERON 31 RT, FS 35 BEHIND ATTACH CLIP ON FRAME. REMOVED ATTACH CLIP, REMOVED CORROSION FROM FRAME IAW DC8 SRM 51-1-8, FABRICATED NEW ATTACH CLIPS, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-20D, 53-2-0.
DURING C-CHECK INSPECTION, FOUND LT WING LEAKING EDGE CRACKED AT STA XFS 198, 29 FWD OF UPPER WING FRONT SPAR. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW UPS EO DC8-5720-7767-A AND DC8 SRM 51-1-21 AND 51-1-8.
INSPECTION TYPE-C, FOUND RT WING INBD FLAP AFT LOWER ATTACH ANGLE CRACKED AT OTBD RIB STA XW 138. REMOVED CRACKED ATTACH ANGLE, FABRICATED NEW ATTACH ANGLE, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-21 AND DACO DWG 5652396.
INSPECTION TYPE-C, FOUND LT WING INBD SLOT PANEL, OTBD SPLICE PAN ANGLE CRACKED AT AFT END, STA XW 223. REMOVED CRACKED PAN ANGLE, DRILLED, TREATED, PRIMED AND INSTALL NEW PAN ANGLE IAW DC8 SRM 57-1-0, 51-1-8, 51-1-21.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND 2 CRACKS ON LT WING AT XRS90 BETWEEN CENTER SPAR AND STRINGER 9. REMOVED DAMAGED AREAS, FABRICATED REPAIR DOUBLER AND FILLERS, DRILLED, TREATED, PRIMED AND INSTALLED DOUBLER AND FILLERS IAW DC8 SRM 57-2-1 FIG 10, 51-1-8, 51-1-20D.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND RE MLG TORQUE TUBE SUPPORT FITTING CRACKED AT F/S 902 AND 878. REMOVED MLG TORQUE TUBE SUPPORT FITTING, FITTED NEW TORQUE TUBE SUPPORT FITTING, DRILLED, TREATED AND INSTALLED IAW UPS E.O. DC8-5340-0748-F.
INSPECTION TYPE-N/A, FOUND LT WING UPPER INBD SLOT PANEL CRACKED .75 LONG AT STA XFS220. REMOVED CRACKED SLOT PANEL, DRILLED, TREATED, PRIMED AND INSTALLED NEW SLOT PANEL IAW DC8 SRM 57-1-0, 51-1-8, 51-3-0, 51-1-21.
INSPECTION TYPE-N/A, FOUND RT WING INBD FLAP OTBD RIB (END CAP) CRACKED AT LOWER ANGLE STA XW138. REMOVED CRACKED END CAP, FABRICATED NEW END CAP, DRILLED, TREATED, PRIMED AND INSTALLED END CAP IAW DC8 SRM 57-1-0, 51-1-8, 51-1-21, 51-3-0.
INSPECTION TYPE-C, FOUND LT WING INBD FLAP OTBD LOWER INTERCONNECT PANEL ATTACH ANGLE CRACKED AT AFT END STA XW138. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0, 51-1-20D, 51-1-8.
INSPECTION TYPE-C, FOUND ATTACH FITTING AT STA 880 ABOVE LONGERON 24 RT. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FITTING, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 53-1-0, 51-1-8, 51-3-0, 51-1-20D.
INSPECTION TYPE:C DURING C CHECK INSPECTION, FOUND AREAS'S OF EXTERNAL SKIN BULGING AND RIVETS PULLING THROUGH SKIN F/S 1620 TO 1690 LONGERON 31 RT TO 31 LT. REMOVED SKIN FROM F/S 1480 TO 1690, REMOVED CORROSION FROM AREA, DRILLED, TREATED, PRIMED AND INSTALLED NEW SKIN AND FINGER DOUBLER AND INNER DOUBLERS IAW DC8 SRM 51-1-8, 53-2-0, 51-1-21, 51-1-20D.
INSPECTION TYPE-C, FOUND RT WING INBD FLAP LOWER ATTACH ANGLE CRACKED AT OTBD RIB STA XW 138. REMOVED CRACKED ATTACH ANGLE, FABRICATED NEW ATTACH ANGLE, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC8 SRM 57-1-0, 51-1-8, 51-1-21.
DURING C-CHECK INSPECTION, FOUND FLOOR TRACK TANGS OUT OF LIMITS ON PREVIOUS PLUG REPAIR COMPT 4 BL 45 LT FS 560. REMOVED DAMAGED PLUG, DRILLED, TREATED, PRIMED AND INSTALLED NEW PLUG IN TRACK IAW DC8 SRM 53-2-3 FIG 6 D, 51-1-8, 51-3-0.
DURING C-CHECK INSPECTION, FOUND FLOOR TRACK TANG OUT OF LIMITS COMPT 17 BL 24 LT STA 1485. REMOVED DAMAGED SECTION OF TRACK, DRILLED, TREATED, PRIMED, AND INSTALLED TRACK PLUG IAW DC8 SRM 53-2-3 FIG 6D, 51-1-8, 51-3-0.
INSPECTION TYPE:N/A, EMERG EXIT LIGHTS DID NOT ILLUMINATE DURING PREFLIGHT CHECK BY CREW. REPLACED EMERG BATTERY PACK, OPS CKD NORMAL. (P/N 5708458-503), (S/N 10389) ON, (S/N 32) OFF.
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED WING FRONT SPAR PYLON SUPPORT FITTING REPLACEMENT. REWORKED NR 2 AND NR 3 PYLON FOOTSTOOL FITTING IAW UPS EO DC8-57-0641.
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED WING FRONT SPAR PYLON SUPPORT FITTING REPLACEMENT. REWORKED NR 2 AND NR 3 PYLON FOOTSTOOL FITTING T-DOUBLER/SKATE ANGLE IAW UPS EO DC8-57-061.
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED C-4 DOOR CUTOUT, FWD UPPER CORNER CRACKED APPROX .25 INCH LONG. FABRICATED REPAIR USING 7075-T6 AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-21, AND 51-1-20D.
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED R-1 DOOR FRAME FUSELAGE SKIN CRACKED ON LOWER AFT CORNER. FABRICATED FILLER, DOUBLER, TRIPLER AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-21, AND 51-1-21D.
PILOT REPORTED DOORS NOT LATCHED LIGHT ON AFTER TAKEOFF. RECYCLE GEAR AND OK. PERFORMED PULL TEST OF DOORS, OPS CK GOOD. CLEARED CANNON PLUGS ON DOOR SWITCHES.
WHILE ON GROUND MAINTENANCE FOUND EMERERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK.
WHILE IN CLIMBOUT FROM SEOUL TO ANCHORAGE, DOOR AND GEAR NOT LATCHED ILLUMINATED PASSING 15,000 FEET. AFTER SUCCESSFUL UPLATCH CHECK, EXECUTED PROCEDURES IAW QUICK REFERENCE HANDBOOK. LIGHTS REMAINED ILLUMINATED. GEAR AND DOOR CHECK PERFORMED REVEALED NR 3 MAIN TIRE TORN AND FLAT, TOUCHES INSIDE WELL. REPAIRED AND CHECKED IAW M/M 32-31-03.
MAINTENANCE REPORTED FLIGHT DECK EMERGENCY LIGHT INOP (DOME LIGHT). RELAMPED, OPS CHECK NORMAL.