N804UP
Registered owner: WHEELS UP PARTNERS LLC, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| CIRCADIAN AVIATION LLC (O2GA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
LEFT ENG POWER LEVER IS DIFFICULT TO ADVANCE FWD. EXHIBITS A SPONGE LIKE FEELING. R & R THE LT ENG FUEL CONTROL UNIT. GND OPERATIONS & LEAK CHECKS WERE GOOD. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED. ACFT WAS RTS.
AUTO PROP FEATHER TEST FAIL RT & LT ENGS. LT PROP LINGERS BETWEEN 670 & 680 RPM, TORQUE BETWEEN 13.5 & 16.1. RT PROP LINGERS BETWEEN 670 & 690 RPM, TORQUE BETWEEN 12.9 & 15.2. TROUBLE SHOT THE DISCREPANCY & FOUND A FAULTY LT & RT ENG AUTO FEATHER OIL PRESS SWITCH. R & R SAME. SYS OPERATIONAL CHECK WAS GOOD. ACFT WAS RETURNED TO SERVICE.
ON FINAL APPROACH THE LT MAIN GEAR LIGHT DID NOT ILLUMINATE. THE NOSE GEAR & RT MAIN GEAR LIGHTS ILLUMINATED NORMALLY. A GO AROUND WAS INITIATED TO TROUBLESHOOT & IT WAS DETERMINED THAT THERE WAS NO GEAR UNSAFE RED INDICATED & THE GEAR WARNING HORN DID NOT SOUND WHEN EITHER THE THROTTLE WAS REDUCED OR THE FLAPS WERE EXTENDED TO THE DOWN POSITION. WAS ABLE TO VISUALLY SEE THAT THE GEAR APPEARED TO BE IN THE DOWN POSITION. PERFORMED A LOW APPROACH & HAD TOWER VERIFY THAT THE GEAR APPEARED TO BE DOWN IN THE NORMAL POSITION. A NORMAL LANDING WAS MADE WITHOUT INCIDENT. EMER VEHICLES WERE STANDING BY UPON LANDING. CONFIRMED THE LT MAIN GEAR DOWN & LOCKED INDICATOR BULB WAS INOPERATIVE. BULB WAS REPLACED & INDICATOR LIGHT OPERATIONS CHECKED GOOD. ACFT WAS RETURNED TO SERVICE.
FIRE WARNING ILLUMINATED ON PIT 34. ON DESCENT APPROX 5 MINS AFTER SELECTING TAIL DEICE THE LOWER CARGO FIRE LIGHT ILLUMINATED SECURED TAIL DEICE AND ACCOMPLISHED EMERGENCY CHECKLIST. RAN TAIL DEICE SYS AFTER SEVERAL MINS HAD LOWER CARGO IRE LIGHT ON F/O PANEL & MSG AFT D FIRE WITH VISIBLE SMOKE AN R & R AFT 2 SMOKE DETECTORS IN AFT PIT NEEDS OPS CK OPS CHECK GOOD PER 26 18 01 4 5. ***CLOSED***
AFTER ROTATION, LOWER CARGO FIRE LIGHT ILLUMINATED, MX DISPLAY INDICATED FIRE COMP C, AFTER I MINUTE INDICATION CLEARD, TEST PASSED, RETURNED TO PHL FOR CARGO PIT INSPECTION. INSPECTED COMP C, FOUND NO EVIDENCE OF FIRE OR SMOKE.
EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CK GOOD IAW MM CH 33.
INSPECTION TYPE:N/A CAPTS SEAT SLIDES AFT ON TAKEOFF ROLL. INSTALLED NEW BOTH AFT SEAT TRACKS REF EO DC8-5340-0741E SRM 53-2-3 FIG 11, REMOVED AND REPLACED CAPT SEAT PER DC8 MM 25-11-01. OPS CHECK GOOD.
INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS STAY ON WITH AC POWER ON GENERATORS. REMOVED EMERGENCY EXIT LIGHT BATTERY PACK, OPS OK.
INSPECTION TYPE:N/A ATB NO BRAKES ON LT SIDE OF A/C FROM THE CAPTS, F/O, POS, WHILE TAXING HYD BRAKE PRESS IS LOW AND FWD ACCUMULATOR IS FLAT. UPON INVESTIGATION FOUND HYD FLUID COMING OUT OF FWD BRAKE ACCUMULATOR. REMOVED AND REPLACED FWD BRAKE ACCUMULATOR IAW 32-42-04 MM. SERVICED AS REQUIRED AND SYS OPS CHECK GOOD AND LEAK CHECK GOOD.
INSPECTION TYPE:C2 FWD LOWER CARGO L36 CORRODED BETWEEN FS 620 & FS 640. REPAIR FWD LWR CARGO L36 LT IAW REO G08587 REV A & UPS EO DC8-5300-1 6674-B.
INSPECTION TYPE:C2 FS 702, STR 31 LT FRAME CRACKED AT END. REMOVED AND REPLACED FRAME IAW DAC DWG 5750365.
INSPECTION TYPE:C2 FABRICATE FRAME. FABRICATED FRAME IAW DAC DWG 9750428.
INSPECTION TYPE:C2 FASTENER HOLES AT INTERSECTION OF L34R AND FS FRAME AT STA 56 ARE CORRODED AND CRACKED. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-2.
INSPECTION TYPE:C2 NR 1 SEAT TRACK AT STA 46 IS CORRODED. REPLACED SECTION OF SEAT TRACK WITH SPLICE IAW EO DC8-5320-5167.
INSPECTION TYPE:C2 LWR FILLET AREA STA 660 L36R FITTING CRACKED. REMOVED FITTING AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C2 CRACK INDICATIONS FOUND BY NDT ON HOLE NR 9 LT. REAMED AND COINED HOLE, FABBED AND INSTALLED BUSHING IAW REO G08603.
INSPECTION TYPE:C2 CRACK INDICATIONS FOUND BY NDT ON HOLE NR 11 LT. REAMED AND COINED HOLE, FABBED AND INSTALLED BUSHING IAW REO G08603.
INSPECTION TYPE:C2 CRACK INDICATION FOUND BY NDT ON HOLE NR 10 LT. REPAIRED IAW REO - G08603 REV A.
INSPECTION TYPE:C2 CRACK INDICATIONS FOUND BY NDT ON HOLE NR 9 LT. REAMED AND COINED HOLE, FABBED AND INSTALLED BUSHING IAW REO G08603.
INSPECTION TYPE:C2 BS 683 LONGERON 36 RT SIDE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21D AND DWG 9750428.
INSPECTION TYPE:C2 BS 683 LONGERON 36 LT SIDE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND DWG 6750428.
INSPECTION TYPE:C2 FITTING AT BS 702, L36 RT SIDE HAS CRACK. REMOVED AND REPLACED CRACK FITTING IAW DC8 SRM 51-1-20D, 51-3-1.
INSPECTION TYPE:C2 FITTING AT BS 702, L36 LT SIDE HAS CRACK. REMOVED AND REPLACED CRACKED FITTING IAW DC8 SRM 51-1-20D AND 51-3-2.
INSPECTION TYPE:C2 BS 683 BETWEEN L31 & L30R HAS CRACKED FITTING. REMOVED DAMAGED FITTING IAW DC8 SRM 51-1-20D, LOCATED DRILLED AND DEBURRED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C2 CORROSION ON LOWER SURFACE OF CABIN FLOOR PANEL BS 400 TO 480, LBL 24 IN FWD PIT. REMOVED AND REPLACED FITTINGS AND SPLICE IAW EO DC8-53202-5167, DC8 SRM 53-7-3, 51-3-0, 53-2-3, & 51-3-1F.
INSPECTION TYPE:C2 LONGERON 34 RIGHT SPLICE FITTING CRACKED AT BS 1270 IN AFT PIT. REMOVED L34R IAW DC8 SRM 51-1-21, INSTALLED NEW LONGERON IAW DC8 51-1- 21.
INSPECTION TYPE:C2 L-2 LWR FWD DOOR JAMB, CORNER CRACKED AT 3 FASTENER HOLES. TRIMMED DAMAGE, FABRICATED AND INSTALLED REPAIR PER DC8 SRM 53-2-0 FIG 18.
INSPECTION TYPE:C2 SEAT TRACK NR 6 CORRODED ON UNDERSIDE AT STA 783. REMOVED DAMAGED SECTION OF TRACK. FABRICATED NEW SECTION OF TRACK AND SPLICE IAW UPS EO NO DC8-5320-5167-6. INSTALLED TRACK AND SPLICES IAW DC-8 SRM 51-3-0.
INSPECTION TYPE:C2 SEAT TRACK NR 6 CORRODED ON UNDERSIDE AT STA 783. REMOVED DAMAGED SECTION OF TRACK. FABRICATED NEW SECTION OF TRACK AND SPLICE IAW UPS EO DC8-5320-5167-C. INSTALLED TRACK AND SPLICES IAW DC-8 SRM 51-3-0.
INSPECTION TYPE:C2 R-2 DOOR LONG 11 RT IS CRACKED. REMOVED AND REPLACED LONGERON IAW DAC DWG 3773512 AND DC8 SRM 51-1-20 AND 51-1-21.
INSPECTION TYPE:C2 FLC PIT FLOOR FITTING HAS CORROSION AT FS 296 STR 33R. REMOVED CORROSION IAW DC8 SRM 51-1-8 FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED FITTING REPAIR IAW DC8 SRM 53-2-0 PG 15/16. INSTALLED FITTING REPAIR & CLIPS AT STA 296 STR 33R IAW DC8 SRM 53-2-0 PG 15/16 & DC8 SRM 51-1-21.
INSPECTION TYPE:C2 FRAMED CRACKED AT FASTENER TO CUTOUT FS 720 RBL 24 LWR FUSE FILLET AREA. REMOVED AND REPLACED FRAME IAW DAC DWG 5750365.
INSPECTION TYPE:C2 R2 UPPER AFT DOOR JAMB CORNER CRACKED S-2. REPAIRED R2 UPPER AFT JAMB IAW DC8 SRM 53-2-0 FIG 16 SHEET 4 AND TR 53-130 & 53-131.
INSPECTION TYPE:C2 AFT LOWER CARGO STA 1150 Z-FITTING L34R AND L35R CRACKED. REMOVED CRACKED Z-FITTING, FABBED SPLICE AND DOUBLER. INSTALLED FITTING SPLICE AND DOUBLER IAW DC8 SRM 53-2-0 & DC8 SRM 51-1-8.
INSPECTION TYPE:C2 FUS STA 857, BL 60 LEFT, ANGLE CRACKED, LOWER FILLET PANEL AREA. REMOVED AND REPLACED CRACKED ANGLE IAW REO-G-08094.
INSPECTION TYPE:C2 FS 680, STR 32 LT AFT SIDE OF BULKHEAD HAS 2 CRACKS. REMOVED OLD BULKHEAD AND INSTALLED NEW BULKHEAD IAW DC8 SRM 51-1-2 D WG'S 9750428, 3750826, 4750426, 5750365, 3750447.
INSPECTION TYPE:C2 FS 717 STR 33 LT SHEAR TIE CRACKED. REMOVED AND REPLACED SHEAR TIE IAW DAC DWG 5750365.
INSPECTION TYPE:N/A AT TOP OF DESCENT, LWR CARGO FIRE LIGHT ILLUMINATED. MX DISPLAY READ "AFT D FIRE". ACCOPM CKLIST PROCEDURE, FIRE LIGHT EXTINGUISHED AND MX DISPLAY READ "AFT D INOP". MX LIGHT ALSO ILLUMINATED WHEN AFT D INOP MSG APPEARED. FOUND MX FAULT AD2318 AND AD3411 AFT CARGO PIT. AFT D INOP MSG ON CONTROL. GREEN SYST OK LIGHT ON. DEFER AFT CARGO COMP PER 26-10 FIRE DET INOP AFT PIT D.
INSPECTION TYPE:N/A TRIM AROUND FIRST OFFICER SWING WINDOW HANDLE IMPEDES OPERATION IF OPENING DURING AN EMERGENCY IS REQUIRED. SECURED TRIM AT FWD PART OF F/O'S SLIDING WINDOW, CLEARANCE NOW ALLOWS HAND TO RELEASE HANDLE IN CASE OF AN EMERGENCY EXIT REQUIRED, OK FOR SERVICE.
INSPECTION TYPE:N/A LEFT MLG W/W WEB PANEL CRACKED. *S/D* REPAIRED PER SRM 51-1-5.
INSPECTION TYPE:N/A, LEFT (CENTER FUESLAGE) PANEL CRACKED AND DELAMINATED JUST FWD OF LEFT MAIN GEAR DOOR. REMOVED PANEL. *S/D* REINSTALLED SERVICEABLE ADF PANEL PER 34-51-01.
INSPECTION TYPE:N/A, EMERGENCY LIGHTS NOT ON IN ARMED. REMOVED AND REPLACED BATTERY PACK, OP''S CHECK NORMAL. P/N ON - OFF: 5708458-503, S/N ON: FTL243, S/N OFF: 7.
INSPECTION TYPE: C123, RT MLG WHEEL WELL, RT O/B PRESSURE DECK STIFFNER HAS CORROSION AT STA 880. CORROSION BEYOND LIMITS IAW DC8 SRM 53-2-0. FABRICATED & INSTALLED HAT CHANNEL, SPLICE ANGLES & STRAPS IAW REO-G07259, DC8 SRM 51-1-20D & DC8 SRM 51-1-21A. ALODINED & PRIMED IAW DC8 SRM 51-1-8.
INSPECTION TYPE: C123, AFT CARGO BAY DOOR RAMP COVER GATE FWD STOP FITTING IS CRACKED. REMOVED & REPLACED STOP FITTING, PN NR 4754061-1 IAW DC8 SRM 51-1-21.
INSPECTION TYPE: C 123 AFT CARGO BAY DOOR RAMP COVER GATE HINGES ARE CRACKED. REMOVED CRACKED HINGE IAW DC8 SRM 51-3-0. RECD NEW HINGE P#5754062-1 . LOCATED & DRILLED HOLES IAW DC8 SRM 51-1-24. INSTALLED NUT PLATES IAW DC8 SRM 51-1-21. INSTALLED HINGE IAW DC8 SRM 51-3-0.
INSPECTION TYPE: C123, FWD CARGO BAY FS 520 LONGERON 35 RT STRAP IS CORRODED. REMOVED LONGERON 35 RT STRAP IAW DC8 SRM 51-1-21. FABED STRAP IAW DAC DWG 3758450. ALODINED & PRIMED STRAP IAW DC8 SRM 51-1-8. INSTALLED STRAP IAW DC8 SRM 51-1-21.
INSPECTION TYPE: C123, CORRODED FLOOR SUPPORT FS 1700, RBL20, UNDERSIDE, AFT ACCESSORY BAY. FABBED FLOOR SUPPORT IAW DAC DWG 575032. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED FLOOR SUPPORT IAW2 DC8 SRM 51-1-20D.
INSPECTION TYPE: C123, CORRODED FLOOR SUPPORT FS 1715 BLR 28, UNDERNEATH, AFT, ACCESSORY COMP. FABED ANGLE IAW DAC DWG 575032.ALODINED & PRIMED IAW DC8 SRM 51 -1-8. INSTALLED IAW DC8 SRM 51-1-20D & 51-1-21.
INSPECTION TYPE: C 123 FLOORBEAM LOWER SURFACE CORROSION FS 680 RBL 46. REMOVED DOUBLER , MATERIAL ID FOR NEW ANGLE 7075-0 .100 PO NR 312186 IAW DAC DWG 5773275 FORMED IAW DC8 SRM 51-1-4. HEAT TREATED IAW TPS-1003. FABRICATED ANGLE IAW DAC DWG 5773275. ALODINED & PRIMED IAW DC8 SRM 51 -1-8. INSTALLED IAW DC8 SRM 51-1-20D.
INSPECTION TYPE: C123, AFT CARGO BAY, CORROSION ON UPPER FWD FLOORBEAM FLANGE AT FS 1540 RBL 50. REMOVED CORRODED SECTION OF FLOORBEAM FLANGE IAW REO G07207. ALODINED & PRIMED IAW DC8 SRM 51-1-8. PERFORMED HFEL IAW NAT SRM 06-10-01.001. NO CRACKS NOTED AT THIS TIME, FABRICATE REPAIR ANGLE IAW REO G0720 7. I NSTALLED REPAIR ANGLE IAW REO G07207.
INSPECTION TYPE: C 123 SEAT TRACK HAS SEVERAL BARE METAL AREAS, STA 680 TO 980. CLEAN BARE METAL, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-3. REPLACED & INSTALLED SEAT TRACK & CHANNEL SPLICE IAW DC8 SRM 51-3-0.
INSPECTION TYPE: C123 AFT PIT FS 1240 - 1260 CORROSION ON LOWER SURFACE OF UPPER INTERCOSTAL FLANGE AT LONGERON 33 RT. REMOVED CORRODED INTERCOSTAL, FABRICATE NEW INTERCOSTAL, LOCATED & DRILLED EXISTING FASTENERS HOLES. ALODINED & PRIMED INTERCOSTAL & INSTALLED .
INSPECTION TYPE: C123, AFT CARGO BAY FS 1160 RT FLOORBEAM END FITTING CRACKED. REMOVED FLOORBOARD STA 1000 - 1300 RT IAW DC8 SRM 51-3-0, REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D & 51-1-21. LOCATED & DRILLED NEW FITTING PN 3754946-501N. INSTALLED FITTING IAW DC8 SRM 51-1-21 & 51-1-2 0D AND REINSTALLED FLOORBOARD STA 1000 - 1300 RT IAW DC8 SRM 51-3-0.
INSPECTION TYPE: C123, AFT CARGO BAY FWD FITTING AT FS 1240 LONGERON 35 RT CRACKED. REMOVED FITTING. LOCATED & DRILLED IAW DC8 SRM 51-1-24 NEW FITTING & INSTALLED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C123, AFT ASSY COMPT STA 1560-1580 LHBL 58 UNDER FLOOR CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. REMOVED AND REPLACED SEAT TRACK STA 1470-1580 IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51 -1-8.
INSPECTION TYPE:C123, CUSP WEB STA 1580 RBL 60 HAS A CRACK. REPAIRED AREA IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.
INSPECTION TYPE: C 123 CORROSION GROUND NUT PLATES FROM STA 1580 TO 1620 BL 0 AFT ACCESSORY BAY CORRODED BEYOND LIMITS. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED & REPLACED SEAT TRACK.
INSPECTION TYPE:C 123 CORROSION ON FLOORBEAM, UPPER FLOOR SKIN & SEAT TRACK NEAR CUSP RT FS 1580 AFT ACCES BAY. SEAT TRACK CORRODED OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED CORROSION FROM FLOORBEAM & SKIN. FOUND TO BE IN LIMITS IAW DC8 SR M 53-2-0. REMOVED CORROSION FROM SEAT TRACK, FOUND TO BE OUT OF LIMITS IAW D C8 SRM 53-2-3. REMOVED & REPLACED SECTION OF TRACK FROM FS 1530 - 1580 RT.
INSPECTION TYPE: C 123 SEAT TRACK AT STA 1575 HAS CORROSION AROUND SEAT TRACK PLUG, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-3. CUT SEAT TRACK AT FS 1550 & AT PRODUCTION SPLICE AT 1590. FABBED FWD SPLICE PER DC8 SRM 53-2-3. LOCATED, DRILLED & INSTALLED NEW SECTION OF SEAT TRACK & SPLICES PER DC8 SRM 53-2-3, PARTS WERE ALODINED & PRIMED BEFORE INSTALLATION PER DC8 SRM 51-1-8.
INSPECTION TYPE: C123, FS 878, FLOORBEAM HAS CORROSION BETWEEN SEAT TRACKS F AND G TOP SIDE. FOUND TO BE CORRODED OUT OF LIMITS, TRIMMED OUT DAMAGED AREAS, INSTALLED REPAIR IAW REO-G07202.
INSPECTION TYPE: C 123 INTERCOSTAL CRACKED. REMOVED INTERCOSTAL IAW DC8 SRM 51-1-21. MATERIAL ID .040 7075-0 P/O NR 318790. HEAT TREATED TO .040 7075-T6 IAW DAC DWG NR 5755032. FAB IAW SRM 51-1 -21 BY INSTALLING RIVETS ON FWD SIDE OF INTERCOSTAL.
INSPECTION TYPE:C123, RT AFT SERVICE DOOR HAS A CRACK INTERCOSTAL. STOP DRILLED CRACK AND REPAIRED AREA IAW DC8 SRM 52-2-0.
INSPECTION TYPE: C123, FLOOR PANEL, STA 580 - 759 HAS CORROSION ON UPPER SKIN. REMOVED CORROSION, FOUND OUT OF LIMITS FROM FS 620 - 759 IAW 53-20-0 FIG 1F. REPLACE FLOOR PANEL PN 52772658-15300. DRILLED IAW 51-1-21. ALODINED & PRIMED IAW DC8 SRM 51-1-8. FLOORBOARD TO BE INSTALLED ON UPS T/C NR 0452, TIMCO OPS 34.
INSPECTION TYPE: C123, FLOORBEAM BRACKET STA 1700, LBL 30, CORRODED. REMOVED BRACKET, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FORMED BRACKET IAW DAC DWG NR 5755032. LOADED, DRILLED & DEBURRED IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C123 LOWER AFT CARGO BAY GILLINER SUPPORT & CARGO TRACK CORRODED AT BS 1000 - 1140. REMOVED CORRODED CARGO TRACK, DRILLED & COUNTERSUNK NEW CARGO TRACK AND INSTALLED IAW DC8 SRM 51-3-2, 51-1-22 & 51-3-0.
INSPECTION TYPE: C123, WING SKIN AT STRINGER 64 END FITTING ON LT WING HAS CRACKS AT MOST OUTBOARD AND INBOARD HOLES. FABBED DOUBLER & FILLER IAW EO DC8 5730-9004-D. ALODINED & PRIMED I AW DC8 SRM 51-1-8, INSTALLED DOUBLER, FILLER & LONICALS IAW DC8 SRM 51-1-20D & 51-1-8.
INSPECTION TYPE: C123, RT UPPER HORIZONTAL FILLET PANEL IS CHAFED. REMOVED DAMAGE, FOUND TO EXCEED LIMITS PER DC8 SRM 55-2-0. FABBED DOUBLER PER DC8 SRM 55-2-0. ALODINED & PRIMED PER DC8 SRM 51-1-8. INSTALLED PER DC8 SRM 51-1-21.
INSPECTION TYPE: C123, LT O/B AILERON I/B HINGE FITTING IS CRACKED. REMOVED & REPLACED FITTING IAW DC8 SRM 51-1-21 & 51-3-0.
INSPECTION TYPE: C123, MAIN CARGO DOOR AFT TORQUE BOX FRAME IS DAMAGED. REMOVED LOWER WEB INTERCOSTALS AT LONGERON 16 & 17 LT & LWR FRAME FITTING. FABED UPPER AND LOWER REPAIR ANGLE, FILLERS AND TRIMMED OUT DAMAGE IAW REO-G0 7188 REV B. INSTALLED UPPER & LOWER REPAIR ANGLES, FILLERS IAW REO G07 188 REV B. REINSTALLED LOWER FRAME FITTING, LOWER WEB & INTERCOSTALS IAW DC8 SRM 51-2-0, 51-1-20D, & 51-1-21.
INSPECTION TYPE: C123, CARGO DOOR FWD TORQUE BOX FWD FRAME IS DAMAGED. REMOVED LOWER TORQUE BOX WEB & INTERCOSTAL, TRIMMED OUT DAMAGE & PLUGGED DISCREPANT HOLES IAW REO-G07197. FABBED UPPER & LOWER REPAIR DOUBLERS, REPAIR ANGLE & FILLERS IAW REO G07197. ALODINED & PRIMED IAW DC8 S RM 51-1-8. INSTALLED UPPER & LWR REPAIR DOUBLERS; REPAIR ANGLE & FILLERS IAW REO-G07197 & DC8 SRM 51-1-20D, 51-1-21.
INSPECTION TYPE: C123, INSIDE VENT STAB LOWER ACCESS HOLE FUSELAGE BACKSTRAP DOUBLER HAS AREAS OF EXCESSIVE CORROSION.
INSPECTION TYPE: C 123 RUDDER LEADING EDGE ATTACH ANGLE CRACKED AT 2 RT 284.750. REMOVED CRACKED ANGLE. MATERIAL VERIFICATION PO NR 318067 7075-0.071 IAW DC8 SR M55-5-0. MATERIAL FABRICATION OF NEW ATTACH ANGLE IAW DC8 SRM 55-5-0.HEAT TREAT VERIFICATION 7075-0 TO 7075T-6 (READING 83.5) IAW TPS 1003 R EV A. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW ANGLE IAW D C8 SRM 51-3-0 & 51 -1-21.
INSPECTION TYPE: C123, FINGER DOUBLER FWD OF STA 940 CRACKED AROUND RIVET. REMOVED AND REPLACED FINGER DOUBLER IAW REO-G07215. REMOVED CORROSION IAW DC8 SRM 51-1-8. REMAINING MATERIAL ACCEPTABLE IAW REO-G07215. ALODINED & PRIMED IAW DC8 SRM 51-1-8.
INSPECTION TYPE: C123, LONGERON 29 RT, AT FS 420 - 440 CORRODED. REMOVED CORROSION FROM LONGERON, FOUND OUT OF LIMITS. FABED NEW LONGERON IAW DC8 SR M 53-4-1, TRIMMED & DRILLED (2) LONGERON SPLICES IAW DC8 SRM 53-2-2. ALODINE & PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONGERON & SPLICES IA W DC8 SRM 51-1-21D. REMOVED & REINSTALLED SKIN TIES FS 420 FOR FOM IAW DC 8 SRM 51-1-21D.
INSPECTION TYPE: C 123 LONGERON 27 RT AT FS 420 - 440 CORRODED. REMOVED CORROSION FROM LONGERON AND FOUND OUT OF LIMITS. REMOVED LONGERON 27 RT FS 410 - 450. FABRICATED NEW LONGERON IAW DC8 SRM 53-4-1. TRIMMED & DRILLED (2) LONGERON SPLICES IAW DC8 SRM 53-2-2. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONGERON & SPLICED IAW DC8 SRM 51-1-21D. RMVD & REINSTALLED SKIN TIES FS 420 FOR FOM IAW DC8 SRM 51-1-21D.
INSPECTION TYPE :C123, BETWEEN STA 440 TO 460, LONG 27 LT CRACKED. REMOVED LONGERON SPLICE. ORDERED NEW PART, RECEIVED LONGERON SPLICE 4646163- 501N, DRILLED NEW SPLICE AND INSTALLED NEW SPLICE.
INSPECTION TYPE: C123, AFT CARGO BAY, FS 1240 FITTING AT LONGERON 35 RT CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D. LOCATED & DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D.
INSPECTION TYPE: C 123 CORROSION ON FLOOR PANEL, RT FS 1560 RBL 40 AFT ACC BAY, REMOVED CORRODED FLOOR PANEL. RECEIVED NEW FLOOR PANEL P/N 52772658-15300, S/N TAG 00428628 LOCATED DRILLED & COUNTERSUNK EXISTING HOLES IAW DC8 SRM51 -1-22 & 51-3-2. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC 8 SRM 51-3-0. SEE UPS NR 111574. TIMCO''S NR 21324 FOR PARTS TAG.
INSPECTION TYPE:C123 CORROSION AROUND BEAR STRAP RETAINER THROUGH FLOORBOARD AT STA 1595, RBL 35. REMOVED CORRODED SECTION OF FLOOR PANEL. LOCATED NEW FLOOR PANEL, DRILLED & COUNTERSUNK EXISTING FASTENER HOLES IAW DC8 SRM 51-1-22 & 51-3-2. FAB REPAIR SPLICE ANGLES IAW DC8 SRM 53-11-3. ALODINED & PRIMED IAW DC8 S RM 51-1-8. INSTALLED FLOOR PANEL & SPLICE ANGLES IAW DC8 SRM 51-3-0.
INSPECTION TYPE: C123, FWD CARGO BAY AT FS 500 - 520 INTERCOSTAL AT LONGERON 33 RT IS CORRODED. CORROSION BEYOND LIMITS IAW DC8 SR7 53-7-0.REMOVED INTERCOSTAL FROM A/C.
INSPECTION TYPE: C 123 LONGERON 27 RT SPLICE FITTING CORRODEDAT FS 440 - 460. RMVD CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED SPLICE FITTING IAW DC8 SRM 51-1-20D & 51-1-21. RECEIVED NEW PART, DRILLED & REAMED SPLICE FITTING IAW DC8 SRM 51-1-24. INSTALLED SPLICE FITTING IAW DC8 SRM 51-1-20 D.
INSPECTION TYPE: C 123 MAIN CABIN FLOORBOARD AT STA 1000 TO 1300. FLOORBOARD NR 2 HAS NUMEROUS AREAS OF CORROSION. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW DC8 SRM 51-1-8. MATERIAL ID 7075-T6 .071 IAW DC8 SRM 53-7-2 PO 313574. FABBED DOUBLERS IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED PER DC8 SRM 51-1-21.
INSPECTION TYPE: C123, CRACK IN MLG PRESSURE DECK AT FS 860 LBL63. STOP DRILLED CRACK IAW DC8 SRM 53-2-0. FABRICATED REPAIR ANGLE IAW REO-G07210 REV A. LOCATED, DRILLED & DEBURRED IAW DC8 SRM 51-1-29. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1- 20D.
INSPECTION TYPE: C123, CRACK IN MLG PRESSURE DECK AT STA 860 RBL 63 REPAIRED AREA IAW REO-G07239. ALODINED & PRIMED IAW DC8 SRM 51-1-8.
INSPECTION TYPE: C123, SEAT TRACK HAS SEVERAL BARE METAL AREAS STA 680 - 980. SEAT TRACK FOUND TO BE CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK STA 680 - 980 IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.
INSPECTION TYPE:C123, CORROSION ON MAIN FRAME FWD FACE FS380 L27R. REMOVED FASTENERS IAW DC8 SRM 51-1-20D, REMOVED CORROSION, ALODINED AND PRIMED AREA IAW DC8 SRM 51-1-8. INSTALLED FASTENERS IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C123, CORROSION ON MAIN FRAME FS 420 L27L FWD FACE. REMOVED FASTENERS, REMOVED CORROSION, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FASTENERS IAW DC8 SRM 51-1-21D.
INSPECTION TYPE:C123 CORROSION ON ATTACHMENT FITTING MAIN FRAME FS 400 L26R-28R. REPAIRED MAIN FRAME FS 400 L26R-28R BY THE FABRICATION AND INSTALLATION OF FRAME FITTING IAW DAC DWG 3773159 & DC8 SRM 51-1-20D.
INSPECTION TYPE: C 123 CORROSION ON ATTACHMENT FITTING AFT FACE OF MAIN FRAME FS 360 LONGERON 28 RT - 26 RT. REMOVED FITTING, REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND OUT OF LIMITS. MATERIAL ID 071 7075.0 IAW DAC DWG 3750999, FAB ANGLE IAW DAC DWG 3750999. HEAT TREATED IAW TPS 1003 REVA, TRIMMED & DRILLED IAW DAC DWG 375099, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED FITTING DC8 SRM 51-1- 20D.
INSPECTION TYPE: C123, AFT CARGO BAY FS 1200 BATH TUB FITTING AT LONGERON 36 - 35 RT CORRODED. REMOVED CORRODED, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED TWO FITTINGS IAW D C8 SRM 51-1-20D, MATERIAL ID FOR DOUBLER 10136-3005 PO 301430 IAW DC8 SRM 53-2-0. RECEIVED NEW FITTING PN 3755845-1, LOCATED & DRILLED FITTING IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.
INSPECTION TYPE: C123, MAIN CABIN STA 1700 FLOOR SUPPORT CRACKED. REMOVED & REPLACED FLOOR SUPPORT IAW DOUGLAS DWG 5755032. ALODINED & PRIMED IAW DC8 SRM 51-1-8.
INSPECTION TYPE: C123, AFT CARGO BAY FS 1020. CORROSION ON LOWER SURFACE OF UPPER FRAME FLANGE FROM LONGERON 36 - 35 LT. REMOVED CORROSION, FOUND TO BE BEYOND LIMITS IAW DC8 SRM 53-2-0. RMVD FRAME CAP FOR FOM, REMOVED DAMAGE IAW DWG DC8 53-0229. FABED REPAIR ANGLE & FILLERS IAW DWG DC8 53-0229. REMOVED CORROSION FROM FRAME CAP. FOUND TO BE BEYOND LIMITS IAW DC8 SRM 5 1-2-0, DRILLED NEW FRAME CAP PN 5764343-505 & INSTALLED IAW DC8 SRM 51-1-20, 51-1-24 & DWG DC8 53-0229.
INSPECTION TYPE: C123, SEAT TRACK AT STA 1700 HAS A BROKEN OUT SCALLOP. REMOVED & REPLACED SEAT TRACK IAW EO DC8 5320-5167. DRILLED & DEBURRED IAW EO DC8 5320-5167.
INSPECTION TYPE: C123, PAX DOOR LOWER AFT CORNER FRAME AT FS 195, 2 INCHES ABOVE CUSP IS CRACKED . FABED UPPER & LOWER FRAME SECTIONS, SPLICE ANGLE IAW DAC DWG 570 5596 & REO-07171. FABED ANGLE IAW DAC DWG 5750085. HEAT TREATED FRAME SECTIONS, SPLICE ANGLE, ANGLE IAW TPS-1003 REV A. FABED SPLICE PLATE & SHIM IAW REO-G07171. INSTALLED FRAME SECTIONS, SPLICE ANGLE, SPLICE PLATE & SHIM IAW DC8 SRM 51-1-21, 51-1-20D.
INSPECTION TYPE: C123, AFT CARGO BAY FS 1140 FRAME CAP & FRAME HAS CORROSION, ELONGATED AND DOUBLE DRILL HOLES FROM LONGERON 34 RT - 34 LT. REMOVED CORROSION & DAMAGE IAW REO-G07193, FABED REPAIR ANGLES & FRAME CAP IAW REO-G07193 & DAC DWG 5755600. ALODINED & PRIMED IAW DC8 S RM 51-1-8. INSTALLED REPAIR ANGLES, FRAME CAP & INTERCOSTAL FITTING S IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C123 STA 851 LT SIDE OF KEEL BEAM NR 6. KEEL SUPPORT ANGLE CRACKED ON AFT SIDE I/B LOWER RADIUS. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0 & 51-1-20D.
INSPECTION TYPE:C123 RT FWD GALLEY DOOR AFT LOWER CORNER SKIN CRACKED PAST STOP DRILL. D O5T P-768. PERFORMED HFEZ IAW NDT SPM 06-10-001 TO FIND END OF CRACK. ROUTED OUT DAMAGE IAW DC8 SRM 53-2-0 FIG 14. FABBED REPAIR DOUBLER, TRIPLER AND FILLER IAW DC8 SRM 53-2-0 FIG 14. ALODINED AND PRIMED IAW DC8 SRM 51 -1-8. INSTALLED DOUBLER, TRIPLER AND FILLER WITH HI-LOKS IAW DC8 SRM 5 1-1-20D & 53-2-0 FIG 14.
INSPECTION TYPE:C123 FRAME AND WEB HAVE DOUBLE DRILLED HOLES AND FRAME IS CRACKED AT STA 1400 BETWEEN STR 33R & 34R. REMOVED DAMAGED AREA IAW DC8 SRM 53-2-0. MAT ID FOR DOUBLER .037 7075-T 6 IAW DOUGLAS DWG 5616674 PO 316935. FABBED DOUBLER IAW DC8 SRM 53-2-0 FIG 1D. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLERS IAW DC8 SRM 51-1-21, 51-1-20D.
INSPECTION TYPE:C123, FLOORBEAM UNDER FLOOR LT STA 1700 LBL 30 HAS CORROSION AT C TRACK ATTACHMENT DOT P142. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED REPAIR ANGLES AND FILLER IAW REO-G07178. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D.
INSPECTION TYPE:C123, FLOOR ANGLE ATTACH BRACKET CORRODED OUT AT FS 1750 BL 0. REMOVED OLD BRACKET AT FS 1750 BL 0 AND REPLACED WITH NEW BRACKET (P/N 5773846-59) UPS TAG 786954.
INSPECTION TYPE:C123 AFT PIT SMOKE BARRIER ATTACH ANGLES CORRODED AND MISSING NUT PLATES. REMOVED CORROSION, FOUND ANGLE TO BE OUT OF LIMITS. FABBED NEW ANGLES IAW DC-8 DAC DWG 9893785. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, AND INSTALLED NUT PLATES IAW 51-1-21.
INSPECTION TYPE:C123 (P4735) RE-INSPECT CLASS II REPAIR AT SKIN AND RIVETS FS 1400 AFT BOTTOM RT FUS SKIN (PER SRM 51-5-5). REMOVED EXISTING DOUBLER. REMOVED CRACK AREA IN SKIN. FABRICATED FILLER, REPAIR DOUBLER, TRIPLER. ALODINED, PRIMED AND INSTALLED FILLERS DOUBLER AND TRIPLER.
INSPECTION TYPE-C CK, 2 Z-FITTINGS AND STA 1180 AND 1200 L33R TO L34R INSTALLED NOT PER SRM. FABBED 2 501 FITTING IAW DAC DWG 3755841, LOCATED AND DRILLED FITTINGS IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 53-2-0 AND 51-1-20D.
INSPECTION TYPE-C CK, LONG 35R AND 34R ZEE FITTING AT FS 1200 HAS CORROSION. REMOVED CORRODED FITTING, ALODINED AND PRIMED ZEE FITTING. INSTALLED FITTINGS IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-C CK, NR 2 BACK-UP FITTING CORRODED. REMOVED FITTING, FABBED FITTING IAW DAC 3754930. TRIMMED FITTING IAW DC8 SRM 53-2-0 FIG 2D. DRILLED FITTING AND CLIPS TO FIT IAW DC8 SRM 5 1-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED WITH HI-LOKS IAW DC8 SRM 51-1-20D.
INSPECTION TYPE C-CK, FS 300 BETWEEN LONG 36 AND 35L HAS CRACKED FITTING. REMOVED FITTING IAW DC8 SRM 52-1-20D, RECEIVED AND CUT FITTING AS NEEDED FOR REPLACEMENT IAW DC8 SRM 52-2-0 FIG 2D. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-C-CK, AFT SIDE OF STA 350, L36 TO L35L FITTING CRACKED. REMOVED FITTING, DRILLED AND INSTALLED NEW ONE IAW DC8 SRM 53-2-0 AND 51-1-21.
INSPECTION TYPE-C-3, AFT CARGO STA 1160 FWD DOOR LWR JAMB HAS CORROSION. REMOVED FITTING, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0, REVEL NEW FITTING (P/N 3757794-504). LOCATED AND DRILLED FITTING IAW DC8 SRM 51-1-2 4. INSTALLED FITTING IAW DC8 SRM 51-1-200.
INSPECTION TYPE-C CK, FITTING AT LONGERON 26L AT FS 320 CRACKED IN RADIUS AT CROSS SLIDE DOOR BUMPER STOP. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. DRILLED AND LOCATED NEW FITTING IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-C CK, LONG 26L AND STA 300 FITTING IS CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, RECEIVED, LOCATED AND DRILLED FITTING IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE C-CK, FS 340 AT LONG 31L FITTING HAS CRACK. REMOVED FITTING AND FOUND TO BE CRACKED IAW 51-1-20D. RECEIVED, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-1-24 AND 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-C CK, SEAT TRACK D HAS AREAS OF CORR FROM 1240 TO 1400. REMOVED AND REPLACED SEAT TRACK IAW DC8 SRM 51-1-8, 52-2-3, 51-3-0 FROM STA 1330 TO 1270.
INSPECTION TYPE-C CK, LONG 33 R AND 34 R FS 1180 HAS TWO FITTING CRACKED. REMOVED FITTING, FABRICATED NEW DOUBLERS, ALODINED AND PRIMED IAW DC8 S RM 51-1-8. INSTALLED DOUBLERS AND FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-C CK, REMOVE FITTING (P/N 3755847-1) TO FOM. REMOVED FITTING, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. RECEIVED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND DAC DWG 3755847. INSTALLED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-C CK, REMOVE FITTING (P/N 36755847-2) TO FOM. REMOVED FITTING, FITTING FOUND TO BE CRACKED, RECEIVED AND INSTALLED NEW FITTING IAW DC8-SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-C CK, STA 55 LONG 30 R HAS CORROSION EMITTING FROM DOME NUT. REMOVED CORRODED DOME NUT IAW DC8 SRM 51-1-21. REMOVED CORROSION FROM L30 R AND STA 35. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED LONG 30R FS 8 TO FS 70. REMOVED INTERCOSTAL AND END FITTING L30R STA 8 TO 26 TO FOM RECEIVED LOCATED AND DRILLED LONG IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONG AND END FITTING IAW 51-1-21.
INSPECTION TYPE-C CK, AFT LOWER CARGO AT STATION 1200, L32R FITTING CRACKED. REMOVED FITTING, FABBED FITTING, DRILLED FITTING AND CLIPS TO FIT ALODINED, PRIMED AND INSTALLED.
INSPECTION TYPE-C CK, AFT PIT FWD DOOR TORQUE BOX FITTING CRACKED AND CORRODED STA 1168 BETWEEN LONG 32R AND 33R. REMOVED CRACKED AND CORRODED FAB BACK-UP FITTING ON PRINTED OP 50002 IAW DAC DWG 375493. RECVD REPAIR FITTING, DRILLED UP IAW DC8 SRM 51-1-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D.
INSPECTION TYPE-C CK, RT WW/ I/B FALSE SPAR AREA WEB CRACKED. FAB WEB IAW DOUGLAS DWG 5643117 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-3-0.
INSPECTION TYPE-C CK, AFT PIT FWD DOOR TORQUE BOX FITTING IS CORRODED STA 1160 BETWEEN LONG 32R AND 33R. REMOVED FITTING, REVD FITTING, FABBED DOUBLERS AND CUT FITTING, ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51-1-8, 55-2-0. INSTALLED IAW DC8 SRM 54-1-20D AND 51-3-0.
INSPECTION TYPE-N/A, EMER EXIT LIGHTS INOP. REMOVED AND REPLACED EMER BATT PACK, OP'S NORMAL (S/N 1125) OFF, (S/N 321) ON, (P/N 60-122 3-5) ON, (P/N 5708458-503) OFF.
INSPECTION TYPE-C/CK, RT MLG WHEEL WELL FRAME CRACKED AT STA 660. *S/D* REMOVED CRACKED FRAME FABRICATED AND INSTALLED NEW FRAME IAW DWG 50F3403, 51-1-8, DWG 564304.
INSPECTION TYPE-C/CK, AFT ACCESS COMPTD BETWEEN STA 1680 AND 1690, L33R CORRODED. REMOVED AND REPLACED LONGERON SECTION IAW DC8 SRM 53-2-2 FIG 8.
INSPECTION TYPE C-CK, FRAME TO CUSP FITTING AT STA 380 HAS A CRACK IN LEG, FRAME TO LOWER CUSP TO FLOORBEAM RT SIDE. REMOVED CUSP FITTING, FABBED NEW CUSP FITTING PER REO-02928 AND DAC DWG 3773479. ALODINED AND PRIMED FITTING IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D.
INSPECTION TYPE-C/CK, CABIN FLOORBEAM FS 900 AT SEAT TRACK B-UPPER CHORD CRACKED AND CORRODED AT FASTENERS LOWER SIDE. REMOVED BOLT FROM SEAT TRACK, REMOVED CORROSION AND ALODINED AND PRIMED IAW SRM 51-1-8 AND DREO 08-02908 AND INSTALLED BOLT IAW DC8 SRM D51-3-0.
INSPECTION TYPE C/CK, CABIN FLOORBEAM BOTTOM SIDE OF UPPER CHORD AT SEAT TRACK CRACKED AT FASTENERS. REMOVED FASTENERS, REMOVED CORROSION IAW DC8 SRM 51-1-8. PERFORMED DYE PEN TEST ON FLOORBEAM, FOUND NO CRACKS. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW DC8 SRM 51-3-0.
INSPECTION TYPE-C/CK, CABIN FLOORBEAM FS 900 AT SEAT TRACK C, UPPER CHORD CRACKED AND CORRODED AT FASTENERS LOWER SIDE. REMOVED CORROSION DYE PEN AREA WITH NO CRACK NOTED IAW DC8 SRM D51-1- 8 AND MIL S 271F, ALODINED AND PRIMED IAW DC8 SRM 51-1-8D AND REO O 072909.
INSPECTION TYPE-C/CK, CABIN FLOORBEAM STA 700 BOTTOM SIDE OF UPPER CHORD AT SEAT TRACK-G CRACK AT FASTENERS. REMOVED FASTENERS, REMOVED CORROSION IAW DC8 SRM 51-1-8. PERFORMED DYE PEN TEST ON FLOORBEAM, FOUND NO CRACKS. ALODINED AND PRIMED AREA IAW DC8 SRM D51-1-8. INSTALLED FASTENERS IAW DC8 SRM D51-3-0.
INSPECTION TYPE-C/CK, LONGERON SPLICE CRACKED AT 3 LT JUST FWD OF STA 1060. REMOVED CRACKED FITTING, CLEANED AREA, RECEIVED NEW SPLICE. INSTALLED NEW SPLICE FITTING IAW DC8 51-1-8 AND 51-1-20D.
INSPECTION TYPE-C/CK, FLOORBEAM EXPANSION JOINT FITTING CRACKED FS 717, LBL 24, AFT SIDE. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0.
INSPECTION TYPE C-CK, BETWEEN STA 100 AND STA 120 LONG 27R CORRODED AT SKIN AREA. REMOVED CORRODED LONGERON END FITTING, HEAT TREATED FITTING IAW DAC DWG 4649643, TRIMMED, DRILLED NEW FITTING IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED PANEL IAW DC8 SRM 51 -3-0.
INSPECTION TYPE C-CK, FLOORBEAM EXPANSION JOINT FITTING CRACKED, FS 749, LBL 24, FWD SIDE. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0.
INSPECTION TYPE C-CK, FLOORBEAM EXPANSION JOINT FITTING CRACKED WHERE ATTACHED TO SEAT TRA CK AFT ATTACH BOLT FS 759, RBL 24. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0.
INSPECTION TYPE C-CK, FLOORBEAM EXPANSION JOINT FITTING CRACKED, FS 700, LBL 24. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0.
INSPECTION TYPE-C/CK, MISSING FASTENERS LEFT UPPER LEADING EDGE SLOT OUT BOARD END ABOVE NR 1 PYLON. REMOVED LEFT UPPER LEADING EDGE OUTBOARD SLOT VANE TO FOM. REMOVED DOUBLER AND FILLER, FABRICATED DOUBLER IAW REO 02867 REV A, ALODINED AND PRIMED ALL PARTS IAW DC8 SRM D51-1-8D. INSTALLED DOUBLER AND FI LLER IAW DC8 SRM 51-1-20D, 51-1-21 AND 51-3- 0. INSTALLED LEFT UPPER LEADING EDGE SLOT VANE IAW DC8 SRM 51-3-0.
INSPECTION TYPE-C/CK, FS 857 FLOORBEAM HAS FITTING CORROSION IN AREAS WHERE FLOORBOARDS CONTACT BEAM. BLENDED CORROSION IAW DC8 SRM D51-1-8. REMOVED PULLEY BRACKET, FABRICATED ANGLE AND FILLER IAW REO 02906, ALODINED AND PRIMED REPAIR ANGLE FILLER AND FLOORBEAM IAW UPS DC8 SRM 51-1-8, INSTALLED REPAIR ANGLE AND FILLER IAW REO 02906 AND DC8 SRM D51-1-21 AND 51-1-20D. REINSTALLED PULLEY BRACKET IAW DC8 SRM 51-3-0.
INSPECTION TYPE-C/CK, STA 340 RIGHT SIDE AT CUSP, CORROSION AROUND AND UNDER FRAME ATTACH FITTING. REMOVED WEB CUSP FITTING AND L-ANGLE TO GET ACCESS TO CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED L-ANGLE CUSP FITTING AND WEB AND BOLTS AND HI-LOKS IAW DC8 SRM 51-3-0 AND D51 1 20D.
INSPECTION TYPE-C/CK, NR 1 PYLON I/B DRAG ANGLE CRACKED EXTENDING APPROX .25 INCH PAST STOP DRILL HOLE. STOP DRILL END OF CRACK .250 AND POLISH TO 32 MICRO INCH FINISH. VERIFIED AND MARKED END OF CRACK UTILIZING HFEC. STOP DRILLED CRACK AS MARKED BY NOT VERIFIED CRACKS ENDS AT STOP DRILLED UTILIZING HFEC.
CREW REPORTED, LOSS OF ALL GENS IN FLIGHT, ACCOMPLISHED QRH CHECKLIST AND GOT ALL 4 BACK ON LINE. REMOVED AND REPLACED BUSS PROTECTION PANEL. RAN ALL 4 ENG AND ACCOM PREF CHECK, ALL OPS CHECK OK.
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND DELAMINATION AT THE INBOARD LOWER SIDE OF THE LEFT WING, NR 1 SPOILER. MAINTENANCE REPLACED THE SPOILER IAW MM 27-61-01.
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE LOWER INBOARD SIDE LEFT WING NR 4 SPOILER. MAINTENANCE REPLACED THE SPOILER PER MM 27-61-01.
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE MAIN LANDING GEAR WHEELWELL CEILING WEB AT STATION 960 AND LONGERON 22L. MAINTENANCE REPAIRED THE DAMAGE PER UPS EO DC8-5310-7346-A.
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT HAND WING NR 4 SPOILER OUTBOARD ATTACH FITTING. MAINTENANCE REPLACED THE FITTING WITH SPOILER ASSEMBLY PER MM 27-61-01.
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A 1.5 INCH CRACK ON THE FUSELAGE SKIN UPPER RADIUS OF THE LEFT AFT SERVICE DOOR CUTOUT. MAINTENANCE REPAIRED THE DAMAGE PER UPS EO DC8-5330-7309-A.
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND 2 CRACKS UNDER THE LEFT AFT PACK COOLING DOOR LOWER AFT CORNER. MAINTENANCE REPAIRED THE DAMAGED AREA PER UPS EO DC8-5330-4732-A.
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT HAND WING LEADING EDGE UPPER RIB AT STATION XFS 691. MAINTENANCE REPAIRED THE RIB PER SRM 57-00-00 FIGURE 801.
WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE WEBBING AT STATION 1580, AFT OF FLOOR SUPPORT ATTACH ANGLE LEFT HAND SIDE IN AFT ACCY COMPARTMENT. MAINTENANCE REPAIRED THE WEB PER SRM 53-2-0.
WHILE ON GROUND IN ONTARIO, MAINTENANCE FOUND BATTERY WOULD LIGHT EMERGENCY LIGHT FOR A FEW SECONDS THEN LIGHTS WOULD GO DEAD. REPLACED BATTERY PACK.
PILOT REPORTED DOORS NOT LATCHED LIGHT REMAINED ON THROUGHOUT FLIGHT; CHECKLIST COMPLIED WITH; LT ALTERNATE MAIN GEAR DOOR WARNING LIGHT ILLUMINATED. ADJUSTED LEFT MAIN GEAR DOOR PRELOAD PER MM 32-31-05, STEP 32.