N807UP
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
AT CRUISE ALTITUDE, FL310 RIGHT ENGINE OIL PRESSURE DROPPED TO 111 PSI. ENGINE OIL PRESSURE RETURNED TO NORMAL DURING DESCENT WENT TO 123 PSI. ENGINE OIL LEVEL CHECKED ONCE AIRCRAFT WAS ON THE GROUND AND FOUND ENGINE TO BE CONSUMING OIL. ENGINE CHANGED.
FASTENER FOUND LOOSE IN THE RUDDER BAR BELL CRANK ATTACHMENT. ACFT WAS FERRIED FOR RUDDER BELL CRANK REPLACEMENT IAW ENGINEERING NTO. BELL CRANK WAS REPLACED & ACFT WAS RTS.
STRONG ELECTRICAL ODOR MINUTES AFTER DEPARTURE. CREW NOTICED SMOKE COMING FROM UNDERNEATH FLOOR, BETWEEN SEATS 6 & 8. AN EMER WAS DECLARED & ACFT DIVERTED. LANDING WAS UNEVENTFUL. ACCESSED & INSPECTED SURROUNDING AREA WITH NO DEFECTS NOTED. ENG GND RUNS PERFORMED WITH ENVIROMENTAL SYS ON & NO INDICATIONS OF ELEC ODOR OR SMOKE NOTED.
DURING TAXI RT BRAKE PEDAL WENT TO FLOOR & LT BRAKE PEDAL FELT SPONGY. BLED BRAKE SYS, RAN ENGS & PERFORMED TAXI CHECK WITH NO DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.
DURING CRUISE CREW SMELLED ELEC TYPE BURNING SMELL. CREW DONNED OXYGEN MASK. FEW MINUTES LATER CREW REMOVED MASK & SMELL WAS UNDETECTABLE. DURING DESCENT CREW NOTICED THE SMELL AGAIN & ELECTED TO DIVERT TO & DECLARED AN EMER. LANDING WAS UNEVENTFUL. ACFT WAS FERRIED TO SERVICE CTR FOR FURTHER TROUBLESHOOTING & IS STILL CURRENTLY IN MX. MX WAS UNABLE TO DUPLICATE OR FIND THE SOURCE OF THE BURNING SMELL. AN UNEVENTFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. FOUND AND REPLACED AN OVERHEATING CABIN PRESSURE SAFETY SOLENOID VALVE ASSEMBLY. A CORRODED LAV ELECTRICAL CONNECTOR WAS REPLACED DUE TO A CRACKED WELD ON WATER TANK. WATER TANK WAS REPLACED. SEVERAL SATISFACTORY OPERATIONAL CHECKS FLIGHT WERE PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE ON 01/08/2014 AND THE DISCREPANCY HAS NOT RE-OCCURRED. .
DURING CLIMB THROUGH 6000â CREW SMELLED AN ELEC TYPE BURNING SMELL FOLLOWED BY SLIGHT HAZE IN CABIN. ACFT DIVERTED & LANDING WAS UNEVENTFUL. FIRE TRUCKS WERE STANDING BY. MX APPLIED POWER TO ACFT & PERFORMED OPERATIONAL CHECKS OF ELEC SYS & COMPONENTS. INSPECTED ELEC EQUIPMENT UNDER CTR AISLE FLOOR. PERFORMED ENG RUNS & NO DEFECTS WERE NOTED. A MAX VERIFICATION FLIGHT WAS PERFORMED & NO DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.
INSPECTION TYPE:N/A AREA OF CORROSION CAUSING RIVET HEADS TO DEFORM ON A/C SKIN LOWER CENTERLINE LOCATED NEAR VHF BLADE ANTENNA. INSTALLED INTERIM REPAIR DOUBLER REF NRC 224311 REF E/O DC8-5330-3135 3-A FOR REPEAT INSP AND PERM REPAIR REQUIREMENTS. THIS IS A MAJOR REPAIR. TRANSFERRED TO D-389557.
INSPECTION TYPE:N/A L1 DOOR EXTREMELY HARD TO OPEN OR CLOSE. RERIGGED L-1 DOOR. OPS CHECK NORMAL.
INSPECTION TYPE:N/A DURING EMERGENCY LIGHT CHECK, EMERGENCY STANDBY LIGHTS FAILED TO ILLUMINATE. REMOVED & REPLACED EMERGENCY LIGHT BATTERY / RELAY ASSY PER MM 33-50 -01-2. OPS CHECK GOOD.
PITS 32 AND 34 CARGO DOOR INNER CRACKS. ISSUED DEFERRAL D380080 IAW EO DC8-5230-29933-A. DAMAGE CONSISTS OF 2.0" LONG CRACK LOCATED ON THE INSIDE RADIUS OF FRAME. VERIFIED ENDS OF CRACK IAW NDT MANUAL 06-10-01 MARKED ENDS. MEASURED CRACK TO BE 2.0" LONG. STOP DRILLED CRACKS IAW EO DC8-5230-29933 STEP 6 (A) 4. AFTER STOP DRILL HFEC PERFORMED, NO CRACKS FOUND. DEFERRAL WAS FOR REPEAT INSPECTIONS.
MAIN ENTRY DOOR HAD DENT WITH CREASE JUST OUTBD OF BAYONET FITTING DENT MEASURES 1.25 LENGTH BY .750 WIDE AND .150 DEEP. CON'T ON ECA FORM 011317: FABRICATED DOUBLER. COLD WORKED AREA TO PROPER LIMITS OF .0 08 IAW UPS EO DC8-5310-28745-A, APPX PARA 3. ACCOMPLISHED ADDITIONAL HFEC AFTER REWORK OF AREA-REF NDTSPM 06-10-0. NO CRACKS DETECTED IN WEB ANGLE OR INTERNAL ANGLE ALODINE AND PRIMED AREA, COMPLETED INSTALLATION.
INSPECTION TYPE:N/A NR 3 ENGINE FLAMEOUT AT CRUISE. FLT LVL 360, SPEED MACH .81, FUEL NORMAL AND BALANCED. ATTEMPTED RESTART AT FL 300 UNSUCCESSFUL. ATTEMPTED 2ND RESTART AT 16000 FT SUCCESSFUL. ENG OPERATED NORMALLY REMAINDER OF FLT. EMERGENCY WAS DECLARED. PERFORMED T/S PROCEDURE WRT MM 71-00-00-1 FIG 139 SHEET 1 & 2. FOUND NO ABNORMAL DEFECTS. REMOVED AND REPLACED NR 3 MAIN ENG FUEL FILTER WRT MM 73-10-02-4-2. NO ABNORMAL CONTAMINATION FOUND. IDLE LEAK CHECK WAS GOOD. PERFORMED HIGH POWER RUN WRT MM 71-00-00-5, ALL PARAMETERS NO DEFECTS FOUND. NO PREVIOUS HISTORY A/C OK FOR SERVICE.
THE CREW EXPERIENCED A HYDRAULIC LEAK. AFTER RUNNING THE CHECKLIST, DECLARED AN EMERGENCY AND CONTINUED TO PHL. AFTER APPROX 20 MIN IN CRUISE, LOST HYD QTY DOWN TO AUX AT THE "X" AND AIL CTRL MANUAL AND RUDDER CTRL MANUAL LTS ILLUM. RAN LOSS OF HYD FLUID/PRSR CK LIST. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP PRESSURE HOSE ASSY.
CAPTAIN'S LEFT SHOULDER HARNESS INERTIAL REEL IS STICKY. REMOVED AND REPLACED CAPTAIN'S INERTIA REEL. OPS CHECK GOOD.
INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PER 33-50-01-2, DC8 AMM. LIGHTS OP'S OK.
INSPECTION TYPE:N/A F/E PANEL EMERGENCY CONTROL LIGHT PANEL HAS 4 OR 6 LIGHTS INOP. DEF 358150 ASSIGNED. *SDR FILED OPEN* DEFERRED F/E EMERGENCY ELECT CONTROL LIGHTING PANEL REF MEL 33-1 PART REQ A 847094.
INSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN HAS DEEP GOUGE AND DENT AT STA 160 L21L TO L22L. REPAIR EXTERIOR SKIN IAW SAA EA 008-5330-01-A0966, UPS RAA DC8-53-2064 3.
INSPECTION TYPE:C2 L-1 DOOR FRAME SEGMENT CRACKED IN BAYONETTE AREA. STOP DRILLED CRACK IN FRAME SEGMENT AT L-1 DOOR IAW SRM 52-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON L-1 DOOR FRAME SEGMENT IAW SRM 52-02-02 FIG 007.
INSPECTION TYPE:C2 STA 1180 L27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED BANANA FITTING AT STA 1180 L27L IAW SRM 51-01-20D, AND SRM 51-3-2.
INSPECTION TYPE:C2 LONGERON ATTACH FITTING CRACKED AT STA 1140 L33R. REMOVED LONGERON END FITTING AT STA 1140 L33R IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED LONGERON END FITTING AT STA 1140 L33R IAW SRM 51-3-2, AND SRM 51-1-20D.
INSPECTION TYPE:C2 LONGERON ATTACH FITTING CRACKED AT STA 1140 L34R. REMOVED END FITTING AT STA 1140 L34R IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPLACEMENT END FITTING AT STA 1140 L34R IAW SRM 51-1-20D, AND DWG 475814.
INSPECTION TYPE:C2 LONGERON END FITTING CRACKED AT STA 1140 L35L. REMOVED L35L END FITTING AT STA 1140 IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED L35L END FITTING AT STA 1140 IAW SRM 51-3-2, AND SRM 51-1-20D.
INSPECTION TYPE:C2 LEFT SIDE OF RUDDER SKIN ZR 251 HAS CORROSION. REMOVED SKIN PANEL ON LEFT SIDE OF RUDDER STA ZR 251 IAW SRM 51-1-21. FABRICATED AND INSTALLED LEFT RUDDER SKIN PANEL AT STA ZR 251 IAW SRM 51-3-2, SRM 51-1-9A, AND DWG 5655077.
INSPECTION TYPE:C2 RIGHT SIDE OF RUDDER SKIN ZR 271 HAS OIL CANNING. REMOVED SKIN PANEL ON RT/SIDE OF RUDDER AT ZR 271 IAW SRM 51-1-21. FABRICATED AND INSTALLED RUDDER SKIN PANEL ON RT/SIDE OF RUDDER STA ZR 271 IAW SRM 51-1-21, AND DWG 56555077.
INSPECTION TYPE:C2 HEAVY CORROSION ON TOP OF FLOORBEAM IN C-PIT TUNNEL AT STA 1300 LBL 51. REMOVED CORROSION FROM FLOORBEAM, FOUND TO BE OUT OF LIMITS IAW SRM 53-2-00. FABRICATED AND INSTALLED REPAIR ANGLES AT STA 1300 LBL 51 FLOORBEAM IAW SRM 53-2-0 FIG 1B.
INSPECTION TYPE:C2 DENTS ON NLG RT/STRUT DOOR EXTERIOR SKIN. CUT OUT DAMAGED AREA ON RT/NLG STRUT DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT/NLG STRUT DOOR IAW SRM 52-02-00 FIG 004.
INSPECTION TYPE:C2 CRACK ON EXTERIOR FUSE SKIN AT STA 1740 L19R. CUT OUT DAMAGED AREA ON FUSELAGE SKIN AT STA 1740 L19R IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AT STA 1740 L19R IAW SRM 53-02-01 FIG 7.
INSPECTION TYPE:N/A CABIN ESCAPE SLIDE WILL NOT STOW. INSTALLED RETAINING PIN IN SLIDE PER AMM 25-60-01-2.
INSPECTION TYPE:N/A ESCAPE SLIDE NOT IN DOOR. INSTALLED ESCAPE SLIDE ON DOOR IAW MM 25-60-01-2.
PILOTS OVERHEAD PANEL EMERGENCY LIGHTS DISARMED LIGHT INOP. FOUND BULB BURNED OUT. REPLACED BULB, CHECKS OK.
INSPECTION TYPE:N/A EMERGENCY ESCAPE SLIDE DEPLOYED INADVERTENTLY. DEFERRAL M340403 ASSIGNED. CLEARED MEL 52-7-4 M340403. INSPECTED AND REINSTALLED ORIGINAL DOOR SLIDE IAW AMM 25-60-01 & CHECKS OK.
EMERGENCY EXIT LTS INOP. REMOVED ADN REPLACED EMERGENCY EXIT BATT/RELAY PACK IAW MM 33-50-01-2. OPS CK GOOD.
ELECTRICAL ODOR ON F/O'S SIDE OF COCKPIT TROUBLESHOOTING IN PROGRESS COULD NOT SMELL ANY TYPE OF ELECTRICAL ODOR WHEN OPERATING ALL FOUR ENGINES.
INSPECTION TYPE:C1 WHILE ACCOMPLISHMENT OF MCD FWD HINGE REPLACEMENT AFTER REMOVAL OF THE ACTUATOR CLOSE OUT PNL FOUND A 1" CRACK ON THE FWD UPPER MAIN FRAME CRACK ON "Z" FRAME STOPPED AT EXISTING HOLE NDT HFEC CRACK TERMINATES AT EXISTING HOLE IAW NDTSPM06-10-01. FABRICATED REPAIR ANGLE AND DOUBLER IAW SRM 52-2-0 FIG 2 AND 51-3-0.
WHILE WORKING N/R 859104 FOUND LONG 31L END FITTING CRACKED. REMOVED AND REPLACED LONG END FITTING AT STA 106 IAW SRM 51-3-0 51-1-21, AND SRM 51-1-20D.
A/C COMPT LONGERON END FITTING CORRODED AROUND FASTENER HOLE AT STA 70 L32R. REMOVED AND REPLACED LONG END FITTING AT STA 70 L32R IAW SRM 57-1-20D, AND 51-3-2.
INSPECTION TYPE: C1, SKIN SPLICE AT FS 1350 INTERIOR FINGER DOUBLER HAS PITTED CORROSION FROM L31R TO L31L. REMOVED FINGER DOUBLER AT FS 1350 IAW SRM 51-1-21 AND 51-1-20D. FABRICATED AND INSTALLED FINGER DOUBLER AT FS 1350 L31L TO 31R IAW SRM 51-1-21.
INSPECTION TYPE:C1 REMOVE MAIN CARGO DOOR HINGE TO ACCOMPLISH FWD HINGE REPLACEMENT, CRACKED, FOUND DURING DOUBLER REMOVAL. REMOVED MAIN CARGO DOOR AND HINGE, MAG PARTICAL, HFEC AND FPI INSPECT IONS ACCOMPLISHED, NO CRACKS NOTED. REINSTALLED HINGE, REPLACED HINGE PINS 2 EA AND INSTALLED DOOR IAW MM 52-36-01-4, SRM 51-3-0, 51-1-21, DPS 4.704, NDTSPM 06-10-01.001 AND DPS4.707.
INSPECTION TYPE:C1 AFTER REMOVAL OF INTERCOSTAL ON N/R 858794 FS 1473 L34R FOUND CORROSION AT LONGERON UNDER STRAP REMOVED LONGERON 34R STA 1350 TO 1490 IAW DC8 SRM 53-2-2 FABRICATED AND INSTALLED LONGERON 34R AT STA 1350-1490 IAW DRWG 3646937
INSPECTION TYPE:C1 UPON REMOVAL OF D-PIT SCUFF PLATE TO FOM FOR NDT INSPECTION TO COMPLY WITH EO DC8-5330-20206 FOUND CORROSION ON FUSELAGE SKIN FS 1395 TO 1445 L34R-L32R. REMOVED AND REPLACED FUSELAGE SKIN AT STA 1395-1445 L34R-L32R IAW SRM 51-1-21, 51-1-20D AND DWG 65615372.
REPLACE SKIN PANEL AT STA 70 TO -21.92 LONG 31R-L31L. REMOVED AND REPLACED FWD BELLY SKIN AT STA -21.92 TO STA LONG 31L TO LONG 31R IAW EO DC8-5330-8942-D.
INSPECTION TYPE:C1 BATHTUB FITTING CRACKED AT C-PIT DOOR JAMB STA 1200 L33R-L34R. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 53-2-0 AND SRM 53-2-0 FIG 02G.
INSPECTION TYPE:C1 SPLICE FITTING CRACKED AT STA 610, L35L REMOVED CRACKED SPLICE FITTING AT STA 610, LONG 35L IAW SRM 51-1-20D. FABRICATED REPLACEMENT FITTING AND INSTALLED FITTING IAW DRWG 3750330
F/S 960 LBL 60 FLOORBEAM AT LIGHTING HOLE ON VERT FLANGE AT CENTER OF HOLE HAS A 5" CRACK GOING AT HORIZ ANGLE. STOP DRILLED CRACKED FLOORBEAM, FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SAA SK 807-858978 AND UPS EODC8-53-20486.
INSPECTION TYPE:C1 LONG 31R SPLICE FITTING CRACKED FROM 1040-1060. REMOVED AND REPLACED LONG SPLICE FITTING IAW SRM 53-1-0 AND 51-1-20 AT STA 1040-1060 LONG 31R.
MAIN CARGO DOOR LWR AFT CORNER, THE DOOR JAMB CORNER INTERNAL SUPPORT PLATE IS CRACKED. REMOVED FILLET IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT FILLET AT THE MAIN CARGO DOOR LWR AFT DOOR JAMB INTERNAL SUPPORT PLATE IAW DWG 5772786 AND SRM 51-3-0.
A-PIT CENTER TORQUE BOX BATHTUB FITTING AT FS 360 BETWEEN TORQUE BOX FRAME AND LONGERON34R HAS CORROSION. REMOVED CORROSION FROM BATH TUB FITTING AT STA 360 LONG 34R AND FOUND OUT OF LIMITS IAW SRM 51-1-8. REPLACED BATHTUB FITTING AT STA 360, 34R IAW 53-02-00-0 FIG 002D.
FS 1488 LONG 32L CRACKED ON BACKSIDE OF SPLICE END. REMOVED LONG 32L AND SPLICE END FITTING AT FS 1488 IAW SRM 51-1-21, FABRICATED LONG 32L AND SPLICE END FITTING IAW SRM 53-02-02 FIG 010 AND INSTALLED LONG 32L AND SPLICE END FITTING IAW SRM 51-1-21.
INSPECTION TYPE: C1, EXFOILIATED CORROSION ON VERTICAL L-FITTING FWD BULKHEAD RT NOSE TUNNEL. REMOVED VERTICAL L-FITTING, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21, DWG 4642086,S-2506104 AND 51-1-20D.
INSPECTION TYPE:C1 D-PIT FS 1473 LONG 34R LWR RETURN FLANGE ON INTERCOSTAL IN LONGERON HAS HEAVY EXFOLIATION 4.00". REMOVED INTERCOSTAL ATTACH ANGLE AT STA 1473 LONG 34R IAW SRM 51-1-20D. FABRICATED AND INSTALLED INTERCOSTAL ATTACH ANGLE AT STA 1473 LONG 34R IAW SRM 51-1-20D AND DWG 5616674.
INSPECTION TYPE:C1 HEAVY CORROSION UNDER FINGER DOUBLER LT SIDE OF COCKPIT SUBFLOOR STA -12 TO -32 REMOVED DOUBLER AT STA -12 TO -32 IAW 53-02-03 FABRICATED 3 EA FILLERS, 1 EA DOUBLER, AND 1 EA FINGER DOUBLER AND INSTALLED IAW DWG SRO 8530026 SRM 51-1-20D, AND 51-2-1
INSPECTION TYPE: C1, D-PIT DOOR AFT WEB HAS SEVERAL ELONGATED HOLES AND LITE CORROSION AROUND FASTENER. REMOVED DAMAGED WEB IAW SRM 51-1-21, FABRICATED DOOR JAMB SKIN AND WEB IAW DWG 5616674 AND SRM 51-1-21 AND INSTALLED JAMB SKIN AND WEB IAW DWG 5616674 AND SRM 53-2-0.
INSPECTION TYPE: C1, LONGERON END FITTING CRACKED AT STA 690 L4L. REMOVED CRACKED END FITTING AT STA 690 L4L IAW SRM 53-2-2. REPLACED END FITTING AT STA 690 L4L IAW SRM 51-1-20 AND 51-3-0.
INSPECTION TYPE: C1, MAIN CARGO DOOR JAMB AFT LATCH SPOOL FITTING FWD ANGLE HAS INTERGRANULAR CORROSION. REMOVED AND REPLACED MCD LATCH SPOOL FITTING IAW 51-3-0, 51-3-2, 51-1-21, AND 51-3-1.
LONGERON END FITTING CRACKED AT STA 902 L7L. REMOVED AND REPLACED LONGERON END FITTING IAW 51-1-20D, 51-1-21 AND 51-3-0.
INSPECTION TYPE: C1, LONGERON END FITTING CRACKED AT STA 690 L2L. REMOVED AND REPLACED LONGERON END FITTING AT STA 690 L2L IAW SRM 53-2-2, 51-1-20D, AND 51-3-0.
INSPECTION TYPE:C1 STA 834.500 L19L FRAME TO INTERCOSTAL FITTING CRACKED. REMOVED, FABRICATED AND INSTALLED FRAME FITTING IAW 51-1-20D AND DWG 3779874.
INSPECTION TYPE: C1, FINGER DOUBLER BLOWN OUT COCKPIT SUBFLOOR AT STA -12 T0-32R REMOVED CORRODED FINGER DOUBLER IAW SRM51-1-21, FABRICATED REPLACEMENT FIGER DOUBLER AND INSTALLED IAW SRM53-03-03AND SRM 53-2-0 FIG 1F
INSPECTION TYPE:C1 FRAME TO INTERCOSTAL FITTING CRACKED STA.1160 L18R. REMOVE AND REPLACE INTERCOSTAL FITTING IAW SRM 51-3-0 AND 51-1-20D.
INSPECTION TYPE:C1 HEAVY CORROSION BETWEEN COCKPIT SUBFLOOR SKIN AND 2ND FINGER DOUBLER, SEVERAL POPPED RIVIT HEADS,-52 TO -62 LH SIDE AT CUSP. REMOVED FINGER DOUBLERAND REMOVED CORROSION .004 FROM SUBFLOOR SKIN FOUND TOBE WITHIN LIMITS. FABRICATED AND REPLACED FINGER DOUBLER. IAW SRM 51-1-21, 53-2-0, 53-3-3, 51-1-8, 51-1-15, AND 51-1-20D.
INSPECTION TYPE:C1 FRAME TO INTERCOSTAL FITTING CRACKED STA 1200 L18R REMOVED FITTING AT STA 1200 L18R IAW SRM 51-1-20D FABRICATED AND INSTALLED FITTING AT STA 122 L18R IAW SRM51-1-8 AND 51-1-20D
INSPECTION TYPE:C1 60 COMPT L17L AT 1770 HAS 6 INCH CRACK AT END FITTING. REMOVED FITTING AND SUPPORT FROM STA 1770 L17L IAW SRM 51-1-20D, FABRICATED AND INSTALLED LONGERON END SPLICE FITTING AT STA 1170 1793 IAW DWG S-1616757 AND SRM 51-1-8.
FINGER DOUBLER BLOWN OUT IN COCKPIT SUBFLOOR AT STA -67 TO -81. REMOVED FINGER DOUBLER AT STA -67 TO -81. FABRICATED FINGER DOUBLER AND INSTALLED IAW SRM 53-3-1, AND 51-1-21, 51-1-20D.
INSPECTION TYPE:C1 RIGHT AFT MAIN CABIN FS 1730 LONG 15R CRACKED LWR SIDE AT RADIUS .500" LONG. REMOVED DAMAGED AREA AT STA 1730 L15R IAW SRM 53-2-2 FIG 10. FABRICATED AND INSTALLED LONGERON SECTION AND SPLICE FITTING AT FS 1730 L15R IAW SRM 53-02-02 FIG 10 AND SRM 53-2-2 FIG 1D.
RT AFT PRESS BULKHEAD FWD SIDE CRACKED HORIZONTALLY .375 LONG AT RBL 35 AT APPROX 55 INCHES ABOVE FLOOR LINE AT EXISTING REPAIR DOUBLER. CUT OUT DAMAGED AREA ON BULKHD IAW SRM53-2-5 FIG 14A. FABRICATED FILLER AND INSTALLED IAW SRM 53-2-5 FIG 14A, LOCATION OF CRACK ON FS 1766 PRESS BULKHD WITH EXISTING REPAIR DOUBLER IS IN COMPLIANCE WITH AFT PRESS BULKHD WEB CRACK REPAIR IAW SRM 53-2-5 FIG 14A SHEET 4.
INSPECTION TYPE:C1 LEFT AFT MAIN CABIN FS 1756 LONG 14L UPPER FLANGE AT FRAME INTERSECTION CRACKED .500" LONG. REMOVED LONG SECTION AT STA 1756 LONG 14L IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR SPLICE AT STA 1756-1764 L14L IAW SRM 53-02-02 FIG 11 AND SRM 51-1-20D.
INSPECTION TYPE:C1 RIGHT AFT MAIN CABIN FS 1738 LONG 18R UPPER FLANGE TO LONG FITTING CRACKED .250" LONG. REMOVED LONGERON SPLICE FITTING IAW SRM 53-2-2 FIG 10. FABRICATED 2EA REPAIR SPLICES AND LONGERON SECTION AND INSTALLED REPAIR PARTS IAW SRM 53-2-2 FIG 10, 53-02-02 FIG 010.
LT CENTER MAIN CABIN STA 857.125 L19L INBD INTERCOSTAL ATTACH ANGLE CRACKED .500" LONG BETWEEN FASTENERS AT FRAME IN RADIUS. REMOVED ATTACH ANGLE, FABRICATED AND INSTALLED IAW SRM 51-1-20D AND DWG 3779498.
INSPECTION TYPE: C1, MAIN CABIN SEAT TRACK PLUGS HAVE CORROSION AT STA 500 BL0. REMOVED DAMAGED SEAT TRACK, FABRICATED AND INSTALLED SEAT TRACK SECTION IAW SRM 53-2-3 FIG 8A, FIG 12, AND 51-3-0.
INSPECTION TYPE:C1 FLOORBEAM CORRODED AT STA 55 BL 0, FWD SIDE, SEEN FROM A/C COMPARTMENT. REMOVED CORROSION IAW SRM 51-2-1 FIG 1 SHEET 7. FABRICATED REPAIR ANGLE DOUBLER AND FILLER IAW SRM 53-07-03 FIG 006A, AND 51-02-00-0 FIG 050. INSTALLED FILLER AND ANGLE DOUBLER IAW SRM 51-1-20D AND 51-1-15.
CRACK IN FRAME 55 A/C COMPT BETWEEN L24L AND L25L. REMOVED CRACKED FRAME AT STA 55 L24L-L25L IAW SRM 51-3-0. FABRICATED REPAIR FRAME SECTION, REPAIR ANGLES, AND FILLER IAW SRM 53-03-03 FIG3 AND 53-2-0. INSTALLED FRAME SECTION AND REPAIR ANGLES AND FILLER AT STA 55 L24L-L25L IAW SRM 51-1-20D.
INSPECTION TYPE: C1, MAIN CARGO AT FS 990 LBL45 HAS LIGHT CORROSION ON SEAT TRACK SPLICE. REMOVED, FABRICATED AND REPLACED SEAT TRACK SPLICE. IAW SRM 51-3-0, D WG 5910152, 51-3-2 AND 51-1-11.
INSPECTION TYPE:C1 MAIN CABIN IN BETWEEN FS 980-1000 RBL 60 HAS LIGHT CORROSION ON SEAT TRACK SPLICES. REMOVED, FABRICATED AND INSTALLED 2 EA. SEAT TRACK SPIICES. IAW 51-3-0 ,53-02-03 FIG 006A, AND 51-1-21.
INSPECTION TYPE:C1 MAIN CABIN SEAT TRACK PLUGS HAVE CORROSION AT STA.420 AND RBL 25. REMOVED CORROSION AND FOUND SEAT TRACK OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK,FABRICATED AND REPLACED. IAW SRM 53-02-03-0, 53-2-3 FIG 12 , 51-3-0, AND 53-21-01.
MAIN CABIN STA 680 L2R LONG SPLICE FITTING CRACKED. REMOVED AND REPLACED LONG SPLICE FITTING AT STA 680 L2R IAW SRM 51-1-20D.
INSPECTION TYPE:C1 STA 675 L2L LONGERON SPLICE FITTING CRACKED REMOVED AND REPLACED SPLICE FITTING AT STA 675 L2L IAW SRM 51-1-20D AND 51-3-0
INSPECTION TYPE:C1 STA 781 BETWEEN LONG 19R AND 18R BOOT FITTING IS CRACKED. REMOVED AND REPLACED FUSELAGE FWD CENTER SPAR FRAME FITTING (BOOT FITTING) AT STA 781 LONG 19R AND 18R IAW SAA SK 807-858138 AND UPS EO DC8-53-20482.
INSPECTION TYPE:C1 STA 675 L3L SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING AT STA 675 L3L IAW SRM 51-1-20D AND 51-3-0
STA 675 L8L LONGERON SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-21,51-1-20D AND 51-1-23.
RT WING L/E UPPER RIB CRACKED .25 INCHES LONG AT XF693. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2, DWG 5769470 AND SRM 51-1-20D.
INSPECTION TYPE: C1, LT AFT SERVICE DOOR AFT UPPER CORNER HAS CRACK APPROX 3/8 EMITTING FROM FASTNER. REMOVED DAMAGED AREA IAW DC8 SRM 53-02-0 FABRICATED FILLER DOUBLER AND TRIPLER IAW DC8 SRM 53-02-0 FIG 18, AND SRM 53-04-00 INSTALLED FILLER DOUBLER AND TRIPLER AT LT AFT SERVICE DOOR AFT UPPER CORNER IAW SRM 53-02-0 FIG 18
CORROSION UNDER SMALL CHAFF PAD IN C-PIT TORQUE BOX STA 1200 L34R. REMOVED CORROSION FROM UNDER CHAFF PAD IAW SRM 51-1-8 53-2-0. CORROSION OUT OF LIMITS IAW SRM 53-2-0. FABRICATED REPAIR DOUBLER AND INSTALLED DOUBLER AT STA 1200 L34R IAW SRM 51-1-8 AND DWG 3753772 AND SRM 53-2-0.
EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01.
INSPECTION TYPE:P/S FOUND EMERGENCY BATTERY INOPERATIVE DURING PERIODIC SERVICE CHECK PARA 9C. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY UNIT IAW AMM 33-50-01-2.
INSPECTION TYPE:ASV EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, EMERGENCY LIGHTS OPS CHECK NORMAL.
INSPECTION TYPE:C3 RT FWD FUSELAGE SKIN (EXTERNAL DOUBLER) IS CRACKED AT LOWER AFT CORNER OF RH AFT HEAT EXCHANGER OPENING AT STA -12 AT LONG. 27R CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED FILLER AND DOUBLER IAW UPS EO DC8-5330-4732
INSPECTION TYPE:C3 STA. 1260-1280 LONG. 36 IS CRACKED, CUTOUT DAMAGED SECTION,FABRICATED AND INSTALLED LONGERON SECTION, STRAPS,CHANNELS AND DOUBLERS IAW UPS ENGINEERING FILE NUMBER DC8-53-20339 DATED 07/13/03,AND SAA SK 807-542 REV. IR DATED 06/27/03
INSPECTION TYPE: C3, AFTER REMOVING CRACKED LONGERON END FITTING AT STATION 8 LONG 33L FOUND LONG 33L AND END FITTING AT STATION 70 FWD SIDE CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING AND REMOVED, FABRICATED AND REPLACED LONGERON 33 IAW DWG 4611067 AND DWG 3642838 AND SRM 51-1-21, 51-1-20D.
INSPECTION TYPE: C, C-PIT DOOR LOWER AFT CORNER, REMOVED EXISTING REPAIR TO ACCOMPLISH AND SATISFY REPAIR REQUIREMENTS OF SRM, FOR DOOR CORNER REPAIRS AT STATION 1220 LONG 33R. NDT VERIFIED NO CRACKS AT EXISTING CUTOUTS, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG. 22.
INSPECTION TYPE:C3 LEFT WING CENTER LE. LOWER SKIN IS CRACKED AT FASTENER HOLES AT XOLDI 6.225 STOP DRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B APPX. C
INSPECTION TYPE: C, STATION 1875 AT LONGERON 36 LARGE FITTING IS CRACKED INSIDE 62 TAIL COMPARTMENT. REMOVED AND REPLACED FITTING IAW DWG 5652580 AND SRM 51-1-20D, 51-3-0.
INSPECTION TYPE: C3, RIGHT WING LE LOWER RIB IS CRACKED AT XFS 385. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, EXTERIOR FUSELAGE KEELBEAM TO FRAME ATTACH FITTING IS CRACKED AT STA 702 RT SIDE OF KEELBEAM INSIDE STRESS PANEL AT LONG 35R. REMOVED AND REPLACED FITTING IAW DWG 4750718 AND SRM 51-1-20D.
INSPECTION TYPE: C, AFT ACCESSORY COMPT. STA. 1600-1620 AT RBL 45 SEAT TRACK REPAIR IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SEAT TRACK SECTION STATION 1590-1610 AT RBL 45, AND REPLACED SEAT TRACK SPLICE STATION 1600-1620 IAW SRM 53-2-3 FIG. 14
INSPECTION TYPE:C3 A/C BAY FORWARD BULKHEAD STA 8 LONG 33L END FITTING IS CRACKED REMOVED,FABRICATED AND REPLACED FITTING IAW DWG 4611067 AND SRM 51-1-20D.
INSPECTION TYPE:C3 A/C BAY STA 8 LONG 33L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4612650 AND SRM 51-1-20D.
INSPECTION TYPE: C, KEELBEAM TO FRAME FITTING IS CRACKED AT STA 702 LT SIDE OF KEELBEAM. REMOVED AND REPLACED FITTING IAW DWG 4750718 AND SRM 51-1-20D, 51-3-0.
INSPECTION TYPE: C, EXTERIOR FUSELAGE FRAME TO SKIN SHEAR TIE IS BROKEN,STATION 702 BETWEEN LONG. 33L TO 35L. REMOVED DAMAGED SHEAR TIE SECTION, FABRICATED AND REPLACED SHEARTIE SECTION IAW DWG. 5750365 AND SRM. 53-2-0 FIG. 2
INSPECTION TYPE: C3, RIGHT WING CENTER LE LOWER SKIN IS CRACKED JUST AFT OF IB END OF SLOT DOOR AT 225. STOPDRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW E.O. DC8-5720-4087.
INSPECTION TYPE: C3, LT IB FLAP INSIDE AT REAR SPAR ON FLAP AT XCW 64 WEB IS CRACKED IN CORNER. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILLS TERMINATE CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE:C3 RIGHT WING LE. LOWER SKIN IS CRACKED AT SCREWHOLE AT XFS 834 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED DOUBLER I.A.W. DC8-5720-4087-B
INSPECTION TYPE:C3 RIGHT WING OB. LE. LOWER SKIN IS CRACKED AT XFS 628 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. DC8-5720-4087-B
INSPECTION TYPE:C3 PRODUCTION SPLICE DOUBLER CRACKED AT XFS 710 ON RH WING LE. REMOVED,FABRICATED AND REPLACED DOUBLER I.A.W. DWG. 5769572,AND SRM. 51-1-21
INSPECTION TYPE: C, MAIN CABIN SEAT TRACK IS CRACKED AT STA 1000 AT RBL 45 REMOVED, FABRICATED AND REPLACED SEAT TRACK SECTION STATION 990 TO 1110 IAW SRM. 53-2-3 FIG. 14
INSPECTION TYPE:C3 LT WHEEL WELL AFT BULKHEAD LOWER SIDE OF CANTED WEB IS CORRODED BEYOND LIMITS STA 980-992 BETWEEN LONG 28L AND 31L CUTOUT CORRODED AREA ON BULKHEAD AND SKIN FABRICATED AND INSTALLED DOUBLER,FILLER,FINGER DOUBLERS,SKIN SEGMENT AND CANTED FRAME IAW DWG 5646444,AND EO DC8-5320-18960-A DATED 07/08/03,DC8-5330-18949- B DATED 07/08/03,SAA SK 807-683 REV. IR DATED 06/27/03
INSPECTION TYPE: C3, RIGHT WING LEADING EDGE INBOARD END OF OUTBBOARD. SLOT HAS SCREWS PULLING THRU SKIN AT XFS XOLDI 6.225. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM. 57-2-0 FIG. 2A
INSPECTION TYPE: C3, RIGHT WING LEADING EDGE ABOVE NR 3 PYLON, RIB TO WEB ATTACH ANGLE IS CRACKED AT LOWER END AT XS 256.339 APPROX. REMOVED ATTACH ANGLE, FABRICATED AND REPLACED ANGLE IAW DWG. 9753294, AND SRM. 51-1-20D
INSPECTION TYPE: C3, LEFT WING LE LOWER RIB IS CRACKED AT XFS 578.75 STOPD RILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, RIGHT WING LE. LOWER RIB IS CRACKED AT XFS 791. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, LT WING LE LOWER RIB IS CRACKED AT XFS 385, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLERS I.A.W. SRM. 57-2-0 FIG.2
INSPECTION TYPE:C3 LEFT WING LE UPPER RIB IS CRACKED AT XFS 741.25. STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, RIGHT WING LE LOWER RIB IS CRACKED AT XFS 785. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER I.A.W. SRM. 57-2-0 FIG.2
INSPECTION TYPE:C3 RIGHT WING OB. LE. LOWER RIB IS CRACKED AT XFS 728 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR ANGLE I.A.W. SRM. 57-2-0 FIG. 2
INSPECTION TYPE:C3 LEFT WING TE. VERTICLE STIFFNER IS CRACKED PAST STOPDRILL AT XW 0 REMOVED EXISTING DOUBLER,CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED FILLER AND REINSTALLED REPAIR DOUBLER I.A.W. DC8-5720-7767-A
INSPECTION TYPE: C3 HFEC INSPECTION OF THE L-1 DOOR LOWER AFT CORNER DETECTED A CRACK APPROX. .750 INCHES SKIN, STATION 60 BETWEEN LONG. 20L-21L CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED DOUBLER,TRIPLER AND FILLER I.A.W. SRM. 53-2-0 FIG. 15.
INSPECTION TYPE: C3, RT WING OUTBOARD LE LOWER RIB IS CRACKED AT XFS 816. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE: C3, RT WING L/E UPPER RIB IS CRACKED AT XFS 304. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE: C3, LT WING CENTER L/E UPPER RIBS ARE CRACKED AT XFS 366.5 AND XFS 379. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILL TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE: C, RT WING L/E LOWER RIB IS CRACKED AT XFS 741. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE: C, LEFT WING CENTER L/E UPPER RIBS ARE CRACKED AT XS 497.491 AND XS484.895. STOP DRILLED CRACKS. NDT VERIFIED CRACKS. STOPDRILL, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE: C3, RIGHT WING LE LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335 REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG.5769589,AND SRM. 51-1-20D,51-1-21
INSPECTION TYPE: C3, RIGHT WING LE LOWER RIB IS CRACKED AT XFS 747. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, RIGHT WING LE LOWER RIB IS CRACKED AT XFS 797. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, RIGHT WING IB. AILERON LOWER ACCESS PANEL NR 541 CUTOUT IS CRACKED. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED DOUBLER IAW SRM. 57-2-0 FIG. 2H.
INSPECTION TYPE: C3, LEFT WING LE. UPPER RIBS ARE CRACKED AT XFS 781.25,XFS 797.5, XFS 803.75. STOP DRILLED CRACKS,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, LEFT WING LE LOWER RIB IS CRACKED AT XFS 766.25 STOPDRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, RIGHT WING LE. UPPER RIB IS CRACKED AT XFS 822. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, RIGHT WING LE. LOWER RIB IS CRACKED AT XFS 822. STOP DRILLED RIB,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, LEFT WING LE. OB. LOWER RIB IS CRACKED AT XFS 622.5 STOP DRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, LEFT WING TE. VERTICLE STIFFNER IS CRACKED TWO PLACES AT XW 11.5 REMOVED,FABRICATED AND REPLACED STIFFNER I.A.W. DWG. 9887427 AND SRM 51-1-20D.
INSPECTION TYPE: C3, RIGHT WING LE UPPER RIB IS CRACKED AT XS448 STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, RT WING LE. UPPER RIB IS CRACKED AT XFS 297. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, LEFT WING LE UPPER RIBS ARE CRACKED AT XFS 826.75,XFS 847.5 AND XFS 822.5. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILL TERMINATES CRACKS, FABRICATED AND INSTALLED DOUBLERS IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, LEFT WING OB LE LOWER RIBS ARE CRACKED AT XFS 772.5 AND XFS 822.5. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, RIGHT WING LE. LOWER RIB IS CRACKED AT XFS 622. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C3, RIGHT WING LE. UPPER RIB IS CRACKED AT XFS 872. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2
INSPECTION TYPE: C, 8 PREVIOUS BLENDOUTS BELOW C-PIT DOOR BETWEEN LONG. 34R TO 30R FROM STA. 1220 TO 1260 CUT AND REMOVED SKIN SECTION FROM STATION 1190-1230 BETWEEN LONG 29R TO 34R,NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED SKIN SECTION AND SPLICE DOUBLERS IAW DC8-5330-18928-A AND SAA SK 807-033.
INSPECTION TYPE: C, COMPLY WITH MPI P 14035: IAW M REPAIR TO AIRSTART DOOR CUTOUT AT 100Y CYCLES OR 3 MONTHS WHICHEVER COMES FIRST IAW EO DC8-5330-0793, STATION 25 TO 55 LONG. 28L-30L AT DOOR CUTOUT REMOVED EXISTING FILLERS,NDT VERIFIED NO CRACKS AT EXISTING CUTOUTS, FABRICATED AND INSTALLED DOUBLER AND FILLERS IAW DC8-5330-0795, SRO 8530020,AND SRM. 53-2-0 FIG. 13
RT MLG DOWNLOCK INDICATION INTERMITTENT. EMERGENCY DECLARED. TWO MINUTES RT MLG IND CAME ON ON ITS OWN. LANDED W/O INCIDENT, GEAR PINNED. REMOVED AND REPLACED RT MAIN LANDING GEAR DOWNLOCK SWITCH CONNECTOR PER MM CHAPTER 20, STANDARD PRACTICES CHECKS NORMAL.
INSPECTION TYPE:N/A EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACK RELAY UNIT IAW MM 33-50-01, OPS CHECKS GOOD.
INSPECTION TYPE:N/A DEPARTURE-L-2 WINDOW WOULD NOT LOCK CLOSED. LUBED PIVOT POINTS, OPS CHECKS OK.
INSPECTION TYPE:PFLT CAPTAIN SLIDING WINDOW WILL NOT OPEN. LUBED PIVOT POINTS, WINDOW NOW OPERATES NORMAL.
INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS BATTERY PACK DEAD. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECKS NORMAL.
INSPECTION TYPE: IN, FORMER CRACKED JUST INBOARD OF ACCESS PNL 523 LT WING L/E. REMOVED RIVETS IN AREA OF CRACK. FABRICATED AND DRILLED REPAIR PARTS PER SRM 57-2-0. INSTALLED FASTENERS IAW DC8 SRM 51-20-1.
INSPECTION TYPE:C2 STA 980 LBL 24 PRESSURE WEB IS CORRODED BEYOND LIMITS. REPAIRED PRESSURE WEB IAW 8110-3 APPROVED DH SK 807-306.
INSPECTION TYPE:C2 STA 980 LBL 24 T-FITTING IS CRACKED IN SUB FLOOR. REMOVED AND REPLACED FITTING IAW DWG 3640887 AND SRM 53-1-0, 51-3-1, 51-1-20D.
INSPECTION TYPE:C2 STA 1700 FLOORBEAM UPPER FLANGE IS CORRODED BEYOND LIMITS AT LBL 24. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 807-264
INSPECTION TYPE:C2 RIGHT WING LOWER SKIN IS CRACKED AT STRINGER 64 AT O/B END. REPAIRED SKIN IAW EO DC8-5730-9004 APPX E.
INSPECTION TYPE:C2 RIGHT WING I/B LOWER SKIN IS CRACKED AT XFS 570. REPAIRED SKIN IAW EO DC8-5720-7767-A.
INSPECTION TYPE:C2 STA 1772 LONG 10R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 53-1-0, 51-1-20D.
INSPECTION TYPE:C2 STA 1774 LONG 10L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 53-1-0, 51-1-20D.
INSPECTION TYPE:C2 STA 1774 LONG 17L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 53-1-0, 51-1-20D.
INSPECTION TYPE:C2 MAIN CABIN CUSP MEMBRANE IS CORRODED BEYOND LIMITS AT STA 1580 LBL 48-50. REPAIRED WEB IAW SRM 53-2-0 FIG 23.
INSPECTION TYPE:C2 RIGHT WING L/E LIFT TRANSDUCER DOUBLER IS CORRODED BEYOND LIMITS BETWEEN STA XFS 372.75 TO XFS 379.
INSPECTION TYPE:C2 STA 1040-1060 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.
INSPECTION TYPE:C2 STA 1100-1120 LBL 46 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.
INSPECTION TYPE:C2 STA 1772 LONG 17R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 53-1-0, 51-1-20D, 51-1-21.
INSPECTION TYPE:C2 STA 1100 TO 1120 RBL 24 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.
INSPECTION TYPE:C2 STA 35 FRAME ATTACH FITTING IS CORRODED BEYOND LIMITS AT LONG 21R. REMOVED AND REPLACED FITTING IAW DWG 4597643 AND SRM 53-1-0, 51-1-21, 51-3-0.
INSPECTION TYPE:C2 STA 1773 LONG 17R IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-3 FIG 5.
INSPECTION TYPE:C2 RIGHT WING INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21.
INSPECTION TYPE:C2 RIGHT HORIZONTAL STAB UPPER FORMER/CAP IS CRACKED AT XFS 47.5. REMOVED AND REPLACED CAP IAW DWG 5654549 AND SRM 55-1-0, 51-1-20D, 51-1-21, 51-3-0.
INSPECTION TYPE:C2 STA 1620 - 1660 SEAT TRACK IS CORRODED BEYOND LIMITS AT BL 0. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.
INSPECTION TYPE:C2 STA 1690 LONG 35R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-1-20D.
INSPECTION TYPE:C2 LEFT WING LOWER FRONT SPAR STRAP AND DOUBLER ARE BROKEN AT XS 520. REMOVED, FABRICATED AND REPLACED DOUBLER AND STRAP IAW SRM 57-2-1 FIG 14A.
INSPECTION TYPE:C2 STA 1690 LONG 33R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-3-1, 51-1-21.
INSPECTION TYPE:C2 STA 1580 LBL 24 FLOORBEAM IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 807-644.
INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 79 AT STRINGER 15. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.
INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 79 AT STRINGER 9. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.
INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 STRINGER 10. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.
INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT STA XRS 79. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.
INSPECTION TYPE:C2 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 678.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C2 RIGHT WING LOWER L/E SKIN IS CORRODED BEYOND LIMITS AT XFS 722. REPAIRED SKIN IAW SRM 57-2-0 FIG 2A.
INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 105 AT STRINGER 14. REPAIRED SKIN IAW SRM 57-2-1 FIG 10.
INSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN IS CRACKED AT XFS 597.5. REPAIRED SKIN IAW EO DC8-5720-4087.
INSPECTION TYPE:C2 STA 320 BANANA FITTING IS CRACKED AT 27L. REMOVED AND REPLACED FITTING IAW DWG 3754041 AND SRM 51-1-20D, 51-1-21.
INSPECTION TYPE:C2 STA 1690 LONG 22L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641326 AND SRM 51-1-20D, 51-1-21.
INSPECTION TYPE:C2 STA 1240 UPPER GUSSET IS CRACKED AT LONG 34R. REMOVED, FABRICATED AND REPLACED GUSSET IAW DWG 9758507 AND SRM 53-1-0, 51-1-20D.
INSPECTION TYPE:C2 STA 1680 FRAME IS CRACKED AT LONG 21R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.
INSPECTION TYPE:C2 COMPLY WITH EO DC8-5330-12073-A, STA 25 LONG 10L FOUND TWO SKIN CRACKS AFTER DOUBLER WAS REMOVED. REPAIRED SKIN IAW SRM 53-2-0 FIG 15.
INSPECTION TYPE:C2 STA 354 CUSP MEMBRANE IS CRACKED AT LONG 21L. REPAIRED MEMBRANE IAW SRM 53-2-0 FIG 1B.
INSPECTION TYPE:C2 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 572.5. REPAIRED SKIN IAW SRM 57-2-1 FIG 38.
INSPECTION TYPE:C2 STA 1620 LONG 20R LOWER FWD CORNER SKIN IS CRACKED AT R-2 DOOR. REPAIRED SKIN IAW SRM 53-2-0 FIG 17.
INSPECTION TYPE:C2 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 200. REPAIRED SKIN IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 397.75. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C2 STA 160 LONG 10R FUSELAGE SKIN IS CRACKED AT FWD UPPER CORNER OF R-1 DOOR OPENING. REPAIRED SKIN IAW SRM 53-2-0 FIG 14.
INSPECTION TYPE:C2 STA 940 - 960 LONG 24L IS CRACKED. REPAIRED LONGERON IAW SRM 53-2-2 FIG 5.
INSPECTION TYPE:C2 STA 1600 AT LONG 20L FWD LOWER CORNER OF L-2 DOOR FUSELAGE SKIN IS CRACKED. REPAIRED SKIN IAW SRM 53-2-0 FIG 18.
INSPECTION TYPE:C2 STA 855 LT WING REAR SPAR LOWER CAP IS CRACKED FROM XCW 0 TO XCW 10. REPAIRED SPAR IAW 8110-3 APPROVED DH SK 807-357.
INSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 341. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1766 AT LONG 15R. REPAIRED SKIN IAW SRM 53-2-1 FIG 7.
INSPECTION TYPE:PFLT PIT 31 SMOKE DETECTOR FAILED AT DEPARTURE. REPLACED BATTERIES IN PIT 31 SMOKE DETECTOR FA3450 IAW MM 26-18-02. THIS CLEARS M211233, PLACARD REMOVED.
INSPECTION TYPE:N/A EMERGENCY LIGHTS DO NOT TEST. R&R'D EMERGENCY LIGHT BATTERY PACK W/ REF TO M/M 33-50-01 LIGHTS OPE RATE NORMALLY.
INSPECTION TYPE:N/A GIRTH BAR ON MAIN ENTRY DOOR WILL NOT CONNECT REPOSITIONED SLIDE AND CONNECTED BAR
INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CK NORMAL.
INSPECTION TYPE:N/A, NOTICED SLIGHT SMOKE COMING FROM PANEL AREA. TURNED LIGHTS TO LOW, NO SMOKE. REMOVED C/P ON WHITE FLOOD LIGHT REOSTAT AND SECURED. DEFERRED PER MEL 33-1, ORDERED REOSTAT.
INSPECTION TYPE:N/A, RT ELEVATOR CONTROL TAB DELAMINATED BOTTOM SIDE. REMOVED AND REPLACED RIGHT ELEVATOR GEARED TAB IAW MM 27-30-03.
INSPECTION TYPE:N/A, NO EMERGENCY LIGHTS ON BISE TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01 PG 202. OPS CHECKS GOOD.
INSPECTION TYPE:N/A, MAIN CABIN DOOR VERY HARD TO OPEN OR CLOSE. *S/D* ADJUSTED AND TESTED MAIN CABIN DOOR PER MM 52-11-01, OPS CHECK GOOD.
INSPECTION TYPE:N/A, RT WING FLAPWELL DAMAGED BY FLAP ACT LINK FAILURE. *S/D* REF DMI D178387 INTERIM REPAIR TO RT WING AUX SPAR. TRANSFERRED TO NRC 626624 C/W REPAIR PER EO DC8-5720-11513-A. OK FOR A ONE TIME FLIGHT TO DHC FOR PERMANENT REPAIR.
INSPECTION TYPE:IN, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK, ON (P/N 60-12 23-5) (S/N 321), OFF (P/N 5708458-503) (S/N 001).
INSPECTION TYPE:C-1, PERMANENT REPAIR TO AIRSTART CUTOUT (D161352) INCIDENT NR R598473 DATE OF OCCURANCE 10/22/98 ORIGINAL INCIDENT. AIRCART PULLED AWAY FROM AIRCRAFT WITH CART STILL CONNECTED. ACCOMPLISHED REPAIR IAW UPS EO DC8-5330-0793 AND UPS DC8 SRM 53-2-0 FIG 1B.
INSPECTION TYPE:C-1, RUDDER STIFFENER INSIDE L/E AT STA ZR 110 IS CRACKED. FABRICATED AND INSTALLED NEW STIFFENER (WEB) IAW DAC DWG 5656229, DC 8 SRM 51-1-20D & 51-1-21.
INSPECTION TYPE:C-1, SUPPORT WEB BENEATH 2ND RUDDER DAMPENER CRACKED IN SEVERAL PLACES STA ZR155. REMOVED AND FABBED NEW 5656229-11 WEB IAW DAC DWG 5656229. REINSTALLED RIB, WEB AND SIDE SKIN IAW DC8 SRM 51-1-21 & 51-1-20D. REINSTALLED L/E SECTION IAW DC8 SRM 51-3-0. REINSTALLED RUDDER IAW DC8 MM 27- 21-01.
INSPECTION TYPE:C-1, STRINGER-51 NR 2 MAIN O/B AT WS 74.00 REAR SPAR HAS FWD FITTING CRACKED. REPLACED CRACKED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C-1, STRINGER 51 NR 3 MAIN IB AT FS 74 REAR SPAR HAS TWO CRACKED FITTINGS. REMOVED AND REPLACED END FITTING IAW UPS DC8 SRM 51-2-20D AND DWG 3704 841.
INSPECTION TYPE:C-1, STRINGER 51 NR 3 MAIN I/B AT W/S 74.000 REAR SPAR HAS FWD AND AFT FITTINGS CRACKED. REMOVED AND REPLACED FITTINGS W/SERVICABLE PART IAW DAC DWG 5613423 AND DC8 SRM 51-1-20D.
INSPECTION TYPE:C-1 LONGERON END FITTING CRACKED L10L AFT SIDE OF FRAME 902. REMOVED AND REPLACED END FITTING IAW DC8 SRM 51-1-21.
INSPECTION TYPE:C-1, STRINGER 51 NR 2 MAIN O/B AT W/S 74.000 REAR SPAR HAS AFT FITTING CRACKED. REMOVED AND REPLACED END FITTING IAW DAC DAW 5613423 AND DC8 SRM 51-1-20 D.
INSPECTION TYPE:C-1 SPLICE FITTING FS 1050 AT LONGERON 35 RT IS CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SRM 51-3-2 AND 51-1-20D.
INSPECTION TYPE:C-1 INTERCOSTAL CRACKED AT LONGERON 35L BETWEEN FS 1080-1100. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DAC DWG 9758507 AND DC8 SRM 51-1-20D.
INSPECTION TYPE:C-1 STA 1700 LONG 24 LEFT FRAME SPLICE IS CRACKED. REMOVED FABRICATED AND INSTALLED FRAME SPLICE IAW DC8 SRM 51-1-20D, 53-5-3, DAC DWG 612142, 51-1-8 AND 51-1-20D.
INSPECTION TYPE:C-1, CORROSION ON FLOOR PANEL AT RBL 35 AT FS 350. REMOVED CORROSION, FABRICATED REPAIR DOUBLER IAW DC8 SRM 53-2-3 AND INSTALLED REPAIR.
INSPECTION TYPE:C-1, CORROSION EMITTING FROM AROUND AND UNDER NUT PLATES ON BOTTOM SIDE OF FRAME FLANGE AT STA 100 BETWEEN LONG 34R TO 36. REMOVED CORRODED MATERIAL OUT OF LIMITS. REPAIRED WITH FILLER/DOUBLER REPAIR IAW DAC DWG 9753784, 53-2-0, 51-1-8, 51-1-21 & 51-1-20D OF DC8 SRM.
INSPECTION TYPE: C1, RT W/W INBOARD DOOR, AFT CORNER OF TONGUE REPAIR. DOUBLER GOUGED AND CRACKED. REPAIRED BY FABRICATION AND INSTALLATION OF DOUBLER IAW DC 8 SRM 52- 2-0 AND DC 8 SRM 51-1-21, 51-1-20A, 51-3-0. SEALED REPAIR IAW DC8 SRM 51-1-16.
INSPECTION TYPE:C-1 FLOORBOARD CORRODED AROUND INSERT FS 1420 LBL 10. REMOVED CORROSION IAW DC8 SRM 51-1-8, CUT OUT DAMAGE AND REPAIR IAW DC 8 SRM 53-2-3 ALODINE AND PRIME REPAIR DOUBLER IAW DC8 SRM 51-1-8. INSTALLED ALL REPAIR DOUBLER IAW DC8 SRM 51-1-21A.
INSPECTION TYPE:C-1 FLOOR PANEL FS 1470 LBL 35 HAS CORROSION BULGE AROUND INSERT. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, FAB DOUBLER IAW DC8 SRM 53-2-3, INSTALL DOUBLER IAW DC8 SRM 51-1-8.
INSPECTION TYPE:C-1, SEAT TRACK AT STA 870, BL O.O CORR DOT E560. REMOVED CORROSION IAW DC8 SRM 51-1-8 NOT WITHIN LIMITS IAW DC8 SRM 5 3-2-3. REMOVED DAMAGED SECTION OF TRACK STA 850-890 IAW DC8 SRM 53- 2-3. INSTALLED NEW TRACK SECTION IAW DC8 SRM 53-2-3.
INSPECTION TYPE:C-1 FLOOR PNL 58-880 ROW A IS CRACKED AT ATTACH HOLE, HAS 2 EACH GOUGES, NUMEROUS AREAS OF BARE METAL AND CORROSION, AND MISSING/DAMAGED NON- SKID. FOUND TO BE WITHIN LIMITS IAW DC8 SRM 53-2-0 FIG LF. INSTALLED NON-SKID TAPE AS NECESSARY IAW DC8 MM 20-32-0. REMOVED AND FABRICATED FILLER AND DOUBLER IAW DC8 SRM 53-2-3. INSTALLED FILLER AND DOUBLER IAW DC8 SRM 53-2-3.
INSPECTION TYPE:C-1, MAIN CABIN RT SIDE FS 1680 BL 24 THRU 34 FLOORBEAM T-CAP CORRODED ON UNDERSIDE OF NUT PLATE. FAB NEW ANGLE IAW DOUGLAS DWG 5892151, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-3-0.
INSPECTION TYPE:C-1 FLOORBOARD CORRODED ROW-C FS880-1000. REMOVED CORROSION IAW DC8 SRM 51-1-8, REPAIR CORRODED AREA IAW DC8 SRM 53-2-3. ALODINE AND PRIME IAW DC8 SRM 51-1-8, INSTALL REPAIR DOUBLER IAW DC8 SRM 51-1-21.
INSPECTION TYPE:C1, LONGERON END FITTING IS CRACKED L-10R FWD SIDE OF FRAME 680. REMOVED CRACKED FITTING. RECEIVED, LOCATED AND DRILLED NEW FITTING AT STA 680 AND L-10R IAW DC-8 SRM 51-3-2. INSTALLED FITTING IAW DC- 8 SRM 51-1-20D. TORQUED BOLT IAW DC-8 SRM 51-3-1.
INSPECTION TYPE:C1, LONGERON END FITTING IS CRACKED L4L FWD SIDE OF FRAME 680. REMOVED CRACKED FITTING. RECEIVED NEW FITTING (P/N 3779762-501N). LOCATED DRILLED AND DEBURRED FITTING. INSTALLED NEW FITTING, TORQUED BOLT.
INSPECTION TYPE:C-1, CROSS SLIDE RAMP MOUNT ATTACH FIG CRACKED FS 340 ABOVE L 35L. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC8-SRM 53-2-0 & 51-1-20D.
INSPECTION TYPE:C1, LONGERON END FITTING IS CRACKED L6L FWD SIDE OF FRAME 680. REMOVED CRACKED FITTING. RECEIVED NEW FITTING (P/N 3779762-501N). LOCATED DRILLED AND DEBURRED NEW FITTING. INSTALLED NEW FITTING, TORQUED BOLT.
INSPECTION TYPE:C1, INTERCOSTAL FITTING FWD SIDE OF FS 1140 FRAME ABOUT I/B HALF OF LONGERON 33 RT IS CRACKED. REMOVED CRACKED FITTING, RECEIVED NEW FITTING (P/N 4758514-521N). LOCATED, DRILLED AND DEBURRED NEW FITTING. INSTALLED NEW FITTING.
INSPECTION TYPE:C, INTERCOSTAL FITTING, AT FS 1228 ABOVE O/B HALF OF LONGERON 33 RT IS CRACKED ON UPPER AFT LEG. REMOVED INTERCOSTAL FITTING IAW DC-8 SRM 51-1-20D, RECEIVED FITTING NR 4758514-519N PO NR 294625 AND DRILLED UP IAW DC-8 SRM 51-1-20D, INSTALLED FITTING IAW DC-8 SRM 51-1-20D.
INSPECTION TYPE:C-1, BANANA FITTING FS 1220 LONGERON 29-33 RT IS CRACKED. REMOVED OLD FITTING. RECEIVED NEW FITTING, DRILLED HOLES, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C-1, BANANA FITTING FS 1228 LONGERON 29-33 RT IS CRACKED. REMOVED OLD FITTING, RECEIVED NEW FITTING. DRILLED HOLES, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C1, LONGERON 36 AT FS 1270 SPLICE FITTING IS CRACKED. RECEIVED, LOCATED AND DRILLED NEW LONGERON SPLICE FITTING (P/N 375922 2-1) IAW DC-8 SRM 51-3-2. INSTALLED NEW FITTING IAW DAC DWG NR 5750322.
INSPECTION TYPE:C-1, LONG 24R FITTING AT STA 920 IS CRACKED ON AFT SIDE DOT L122. REMOVED FABRICATED AND INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, DC8 SRM 51-3-0, 51-1-20D. INSTALLED SPOILER PULLEY BRACKET AND UPLOCK ASSEMBLY IAW DC8 SRM 51-3-0 AND MM 32-31-03.
REPAIR TO FUSELAGE SKIN FS 558-582, LONGERON 35L-35R. COMPLIED WITH EO 5330-10147A INTERM REPAIR. REMOVED SURFACE CORROISION TRANSFERED TO DEFERAL LIST.
INSPECTION TYPE-N/A, CORROSION FOUND DURING INSPECTION. BULGE IN SKIN AFT OF NR 2 PIT DOOR CREATING HOLE IN FUSELAGE. CLEANED CORROSION PER SRM 53-2-0, TREATED AND PAINTED. COMPLIED WITH E/O 5330-10147A.
INSPECTION TYPE-N/A JUST PRIOR TO TAXI OUT, EMERGENCY LTS ON WITH SW IN ARM POSITION. REMOVED AND REPLACED EMERGENCY BATTERY PACK. ALSO, FOUND PIN PUSHED BACK ON CONNECTOR. REPAIRED PIN EMERGENCY LTS, OPS CHECKED GOOD PER MM 33-50-00.
INSPECTION TYPE-N/A, ON LANDING THRUST REVERSERS WOULD NOT DEPLOY. THRUST REVERSER HYDRAULIC VALVE C/B POPPED. REMOVED AND REPLACED T/R HYD S/O VALVE ASSY PER DC8 MM 78-37-03, SYS OPS CKS NORMALLY. INSPECTED TIRES AND BRAKES AND FOUND ALL TO BE OK FOR CONTINUED SERVICE, (P/N 146505-15) (S/N 7593EA) ON.
INSPECTION TYPE-C/CK, FS 1160 LONGERON 35RD FRAME HAS CORROSION UNDER N/PS TO LONG 34 LEFT. REPAIRED FRAME FS 1160 IAW REO 03609, INSTALLED REPAIR IAW DC8 SRM SD51-1-20D AND SD51-1-21 AND DC8 SRM D51-3-0.
INSPECTION TYPE-C/CK, MAIN CARGO FRAME AT FS 822 HAS EDGE DAMAGE AT L10R. BLENDED OUT DRILLED DAMAGE AND FABRICATED REPAIR STRAP IAW REO 03634, PERFORMED HFEC IAW MIL-STD-271F AND FOUND NO CRACKS. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED REPAIR STRAP IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-C/CK, CORROSION ON FUSE FRAME UPPER FLANGE AT FS 1060 L33L AND 33R AROUND NUT PLATES AND UNDER NYLON SPACER. FABRICATED CAP DOUBLERS, REPAIR ANGLE STRAP AND FREEZE PLUGS IAW REO 03614, INSTALLED 3 FREEZE PLUGS IAW DC8 SRM SD51-1-25, ALODINED AND PRIMED ALL PARTS AS REQUIRED IAW DC8 SRM D51-1-8D, REINSTALLED SUB- STRUCTURE IAW DC8 SRM 51-1-2D AND 51-1-21 AND 51-3-0.
INSPECTION TYPE-C/CK, MAIN CARGO FRAME AT FS 600 HAS EDGE DAMAGE L8L. BONDED DAMAGED AREA IAW REO 03633, FABRICATED REPAIR ANGLE AND STRAPS IAW DC8 SRM D53-2-0D AND SDR EO 013633, TREATED AND PRIMED REPAIR PARTS AND REPAIRD AREA IAW DC8 SRM D51-1-D8, INSTALLED REPAIR IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-C/CK, CRACKED FITTING ON MAIN CARGO DOOR AT APPROX FS 140 AND L8L. MCD ACTUATOR AND WIRING DISCONNECTED FOR FOM TO BE REINSTALLED ON UPS NR 702904. RECEIVED NEW FITTING PE4R EO DC8 5300 9641B, DRILLED NEW FITTING IAW DC8 SRM 51-3-2D, ALODINED AND PRIMED FITTING IAW DC8 SRM 51-1-8, INSTALLED FITTING CORNER SECTION AND WEB IAW DC8 SRM D51-1-2D1 AND 51-3-0.
INSPECTION TYPE-C/CK, LONGERON 20 RIGHT IS CRACKED AT FS 230. REMOVED CRACKED PORTION OF HAT CHANNEL PER REO 03621 DEBURRED ALL EDGES MFG REPAIR ANGLE FROM EXT PER REO 036921 AND HFEC CK OF REMAINING CHANNEL TO INSURE COMPLETE CRACK REMOVAL PER REO 03621, ALODINED REPAIR ANGLE AND A/C STRUCTURE PER DC8 SRM 51-1-8, PRIMED PAST AND A/C STRUCTURE IAW DC8 SRM 51-1-8, INSTALLED ANGLE WITH 14 LOCKS.
INSPECTION TYPE-C/CK, LONGERON END FITTING STATION 1690 LONGERON 21 RIGHT IS CRACKED. REMOVED FITTING, INSTALLED NEW FITTING IAW 51-1-20D AND 51-3-1 ALODINED AND PRIMED IAW DC8 SRM 51-1-8.
INSPECTION TYPE-C/CK, LOWER ACTUATOR MOUNT CORRODED ON REAR SPAR, XW 98. REMOVED AND REPLACED MOUNT IAW DC8 MM 20-16-00 AND DAC DWG 5641112.
INSPECTION TYPE-C/CK, LEFT HAND STA 98 LOWER SUPPORT FITTING OUTBOARD STUD MOUNTING HOLE H AS PITTING CORROSION. REPAIRED IAW REO 03417 REV A, FASTENERS TO BE INSTALLED ON UPS NR 70 7586.
INSPECTION TYPE-C/CK, UPPER RIB CRACKED AT T/E OF L/E BETWEEN NR 1 AND NR 2 PYLON OUTBOARD XRS 364. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0.
INSPECTION TYPE-C/CK, REPAIR IS CRACKED ON INTERNALS L/E SECTION BETWEEN NR 1 AND NR 2 PYLONS AT I/B END OF SLOT DOOR. REPAIRED IAW 57-2-1 BY FABBING NEW DOUBLER, INSTALLED IAW DC8 51-30- 0 AND 57-2-1 ALODINED AND DPRIMED AS REQUIRED IAW DC8 SRM D51-1-8.
INSPECTION TYPE:C/CK, UPPER RIB CRACKED AT T/E OF L/E BETWEEN NR 1 AND NR 2 PYLON OUTBOARD XRS 364. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0.
INSPECTION TYPE-C/CK, LONGERON 33A HAS PITTED CORROSION, FROM FUSELAGE STATION 280 TO FUSELAGE STATION 340. MECHANICALLY REMOVED CORROSION IAW ENGINEERING FILE NUMBER DC8- 53-1920.
INSPECTION TYPE-C/CK, LEFT MAIN LANDING GEAR OUTBOARD AUX SPAR HAS ELONGATED HOLES ON VERTICAL UPPER AND LOWER HORIZONTAL FLANGES. REPAIRED IAW REO 03047 BY INSTALLING REPAIR BUSHINGS IAW DC8 SRM 51-1-25.
INSPECTION TYPE:C/CK, STRINGER END FITTING IS CRACKED AT APPROX XRS 365-370 LOWER STRINGER 66 LEFT WING. REMOVED CRACKED END FITTING AND INSTALLED NEW FITTING IAW DC8 SRM 51-3-2 AND 51-1-21.
INSPECTION TYPE-C/CK, DOUBLER ON AFT LOWER SKIN STA 1490 TO 1690 (P/N 5619907), CORRODED. REMOVED AND REPLACED INNER DOUBLER (P/N 561990) IAW DC8 SRM 51-3-2 AND 51-1-21.
INSPECTION TYPE-C/CK, UPPER PRESSURE PANEL AND FLOOR TO LONGERON 24 LEFT SUPPPORT FITTING AT FS 920 IS BARELY CORRODED AT AFT SIDE. REMOVED CORRODED FITTING, DRILLED NEW SUPPORT FITTING IAW DC8 SRM D51-1-20D AND 51-3-2 AND 51-1-24 AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.
INSPECTION TYPE:C/CK CENTER WING LOWER REAR SPAR CAP CRACKED, BETWEEN 2 FASTENERS IN AFT TANG, 32 IN RIGHT OF KEEL BEAM. PERFORMED HFEC INSPECTION IAW MIL S 271F AND FOUND CRACK BETWEEN 2 FASTENERS HOLES, FABRICATED REPAIR PARTS IAW REO 03412 AND DAC DWG 9 887385 AND DC8 SRM 53-2-0. INSTALLED REPAIR PARTSW IAW DC8 SRM 51-1-20D AND 51-1-21 AND REO 03412.
INSPECTION TYPE-C/CK, CENTER WING LOWER REAR SPAR CAP CRACKED BETWEEN 2 FASTENRS IN AFT TANG 32 RT OF KEEL BEAM. PERFORMED HFEC INSP IAW MIL-S-271F AND FOUND CRACK. FABRICATED REPAIR ANGLE FROM 7075-T6511 PO 111040, IAW REO 03412 AND DC8 SRM 51-9- 0. CUT OUT WEB TO ACCESS REAR SPAR AREA, FABBED WEB FILLER AND DOUBLER IAW DC8 SRM 53-2-0. LOCATED AND DRILLED REPAIR ANGLE IAW DC8 SRM 51-1-24, ALDOINED AND PRIMED REPAIR PARTS IAW DC8 SRM 51-1-8, INSTALLED REPAIR PARTS IAW SRM 51-1-20D, 51-1-21, AND REO 03412.
INSPECTION TYPE-C/CK, RIGHT HAND HORIZONTAL STABILIZER INBOARD VERTICAL WEB SUPPORT CRACKED FWD ON FRONT SPAR AT STA XAR O. STOP DRILLED CRACK, FABBED REPAIR ANGLE IAW DC8 SRM 55-2-0, INSTALLED REPAIR ANGLE IAW DC8 SRM 51-3-0, ALODINED AND PRIMED AS NECESSARY IAW DC8 SRM 51-1-8.
INSPECTION TYPE-C/CK, BOTH STRINGER SPLICE FITTING CRACKED AT STR 51 ON OUTBOARD SIDE OF RIB AT XRS 74.869 IN NR 3 MAIN TANK. REMOVED CRACKED FITTING, NEW ONES FABBED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.
INSPECTION TYPE-C/CK, RBL 22 TO RBC AT STA TO FLOORBEAM CORRODED. REPAIRED IAW REO 03525 BY INSTALLING FLOORBEAM CAP. REPAIRED IAW REO 0 3525 AND SRM 51-1-2D.
INSPECTION TYPE-C/CK, FWD CROSS SLIDE DOOR FWD TRACK HAS CORROSION EMITTING FROM REPAIR. REMOVED TRACK ANGLE, DRILLED COUNTER SUNK AND INSTALLED NEW TANK IAW DC8 SRM 51-3-0 AND 51-1-24.
INSPECTION TYPE-C/CK, STA 70 RBL 15 SEAT TRACK MISSING FASTENERS, CORROSION AT NUT PLATES. REPAIRED IAW REO 03618, REPLACED SECTION OF SEAT TRACK IAW SRM 51-1-20D.
INSPECTION TYPE-C/CK, NUMEROUS AREAS OF HEAVY CORROSION ON BELLY SKIN FUSELAGE STAION 190 TO 450. REMOVED SKIN AND DOUBLERS, INSTALLED NEW SKIN IAW DC8 SRM 51-1-2 1 AND 51-1-20D AND 51-1-22. ALL AREAS REQUIRED CORROSION PROTECTION IAW DC8 SRM 51-1-8.
INSPECTION TYPE-C/CK, FWD SERVICE DOOR DOOR JAM WEBBING AFT END HAS 3 CRACKED PLACES AT FUSELAGE STATION 200 BETWEEN LONGERON 13 RT AND 14, AND RT 17. REMOVED WEB AND FABRICATED IAW DAC DRAWING 5615700, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D.
INSPECTION TYPE-C/CK, LONGERON 20 RIGHT END FITTING AT FUSELAGE STATION 220 IS CRACKED ON UPPER FLANGE. LOCATED DRILLED END FITTING IN PLACE ON A/C IAW DC8 SRM 51-1-24 MANUFACTURED FILLER MAT ID 7075 T6 .050 PO 222933, DRILL FILLER TO MATCH END, ALODINED AND PRIMED FITTING AND FILLER IAW DC8 51-1-8, INSTALLED END FITTING AND FILLER WITH SEALANT IAW DC8 SRM 51-1-11 AND 51-1-20D AND 51-1-21.
INSPECTION TYPE:N/A, EMERGENCY LIGHTS ILLUMINATED INFLIGHT WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK. EMERGENCY LIGHTS WORK FINE ON THE GROUND.
INSPECTION TYPE-A+, RECIR FAN FAILED, FILLED AIR COND BAY WITH SMOKE. FLT CREW AND JUMP SEATERS EVACUATED TILL LOCATION OF SMOKE WAS FOUND. PULLED AND COLLARED RECIRC, FAN, C/IS DEFERRED RECIRC FAN PER MEL 21-16 M-112173.
CREW REPORTED, NR 2 ENGINE INFLIGHT SHUT-DOWN - FLAMEOUT - TOP OF DESCENT FL 360, UNABLE TO RESTART. NR 2 ENG F/F TRANSMITTER SEAL DEFECTIVE. REPLACED SEAL.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND BOLT FRAME HAS .75 INCH LONG CRACK AT FS 80 LONGERON 21R. REPAIRED FRAME PER SRM 53-2-0 FIG 2.
WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION CRK AT LT VERT STAB TO FUSELAGE ATTACH ANGLE. REPAIRED PER UPS EO.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 AND NR 3 WING FRONT SPAR PYLON SUPPORT FITTINGS CRACKED. REPLACED FITTINGS PER UPS EO.
CREW REPORTED, AFTER TAKEOFF FROM HONOLULU ON GEAR RETRACTION, GEAR DOOR LIGHT ON FWD PANEL REMAINED ON, ALT LIGHTS OUT. RECYCLE GEAR, SAME RESULTS, UPLATCH CHECK LIGHT WENT OUT AND REMAINED OUT. REPLACED RT AND LT GEAR DOOR PROX SWITCHES AND WIRING. PERFORMED GEAR RETRACTION TEST AND UPLATCH TEST IAW M/M 32-31-04, ALL OPS CHECKS OK.
CREW REPORTED WITH LANDING GEAR HANDLE IN UP POSITION, DOOR NOT LATCHED LIGHT STAYED ON. LIGHT ON F.E. PANEL WAS NOT ON. CYCLED GEAR TWICE-NO HELP. PLACED GEAR IN UPLATCH POSITION AND LIGHT WENT OUT GIVING A GOOD UPLATCH CHECK. MAINTENANCE DEFERRED PER MEL 32-8 (M-99951).
CREW REPORTED, WITH LANDING GEAR HANDLE IN THE UP POSITION, THE DOOR NOT LATCH LIGHT STAYED ON AND AFT LIGHT ON FE PANEL WERE NOT ON. CYCLED GEAR TWICE, NO HELP. PLACED GEAR IN UP LATCH POSITION AND LIGHT WENT OUT GIVING A GOOD UP LATCH CHECK. REPLACED LEFT AND RIGHT GEAR DOOR PROX SWITCHES AND FOUND BROKEN SPLICE ON LT PROX SWITCH. SYSTEM OPS CHECKS GOOD PER DC8 MM 32-31-04 PAGE 503 B.
CREW REPORTED, DOORS NOT LATCHED LIGHT CAME ON DURING UPLATCH CHECK, LIGHT WENT OUT AFTER GEAR RECYCLED. MAINTENANCE PERFORMED UPLATCH CHECK IAW MM 32-31-04, OPS CK NORMAL. FOUND GEAR HANDLE STICKY AND CLEANED AND LUBED GEAR HANDLE.
AFTER TAKEOFF, THE GEAR NOT LATCHED LIGHT ILLUMINATED. PERFORMED THE CHECKLIST AND SHORTLY THEREAFTER THE DOORS NOT LATCHED LIGHT ILLUMINATED, FINISHED CHECKLIST. PROCEEDED TO DESTINATION AT MACH .65. INSPECTED SYSTEM, FOUND NO DEFECTS. LUBED LANDING GEAR AND UPLOCKS. PERFORMED SEVERAL GEAR SWINGS AND OPERATED NORMALLY IAW M/M 32-33-00.
DURING B CHECK, MAINTENANCE REPORTED NR 3 AND NR 4 J-BEAM AT AFT PRESSURE BULKHEAD CRACKED. INSTALLED REPAIR PER UPS EO DC8-5310-6715A.