N330UP
Registered owner: C C & E I LLC, KY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE , P/N : 145T5876-81 PANEL NO : 241MFF.
AERODYNAMIC SEAL BROKEN, FWD LH ENTRY DOOR (REPLACE) 1. I.A.W AMM 52-12-01-004-001 REV. 148 REMOVE CREW ENTRY DOOR.
FOUND CRACKED ANGLE, BULK CARGO COMPT CEILING AREA, STA 1577 LBL 74 INBD SIDE. MAIN DECK CARGO FLOOR PANEL AND DADO PANEL OK TO INSTALL CHECK OK
FOUND CRACK - ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 LBL 74 OUTBD SIDE. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND DWG 146T5650 SH. 5 REV. C. JOB COMPLETED.
FOUND MAIN DECK DOORWAY LINING BROKEN TTL:1AREA.
CRACKED PANEL, LT WING L/E NO.1 SLAT LOWER SURFACE INBD CLOSURE PNL. IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.144 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6" ALL AROUND. RESULT: NO DEFECT FOUND.
FOUND THE CREW ENTRY DOOR AFT DOORWAY LINING SEAL BROKEN.
FOUND THE CREW ENTRY DOOR FORWARD DOORWAY SEAL MISSING.
ENTRY DOOR WILL NOT CLOSE UNLESS SECURE LEVER IS ALREADY IN SECURE POSITION. REMOVED AND REPLACED PAWL IAW AMM 52-11-26 OPS CHECKED GOOD.
EMERGENCY/EXIT LIGHT FORWARD OF L1 DOOR HAS DAMAGED BASE. R&R EMERGENCY LIGHT ASSY @ L1 DOOR IAW AMM 33-51-16 OPS CKS NORMAL
FAULT - FOUND NO.8 SLAT INBD MAIN TRACK DRAIN HOUSING TUBE PORT FUEL SEEPING.I.A.W. AMM 28-11-01-004-013 REV.142 REMOVED THE FUEL PANEL NO 632FB.I.A.W. AMM 28-11-11-004-023 REV.142 AND AMM 28-11-11-404-036 REV.142 REPLACED THE O-RINGS OF THE DRAIN TUBE.
FOUND MAIN DECK CARGO FLOOR PANEL CRACK AT STA 1432~1520, LBL 55~LBL 77.5, P/N: 146T5869-89. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.2. CONDITION CHECK IS SATISFACTORY. I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.
**SDR FILED OPEN** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) OKAY TO WORK
CRACK -ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL60 OUTBOARD.I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.
**SUPPLEMENTAL SDR** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDR. PREFORM MODIFICATIONS PER UPS EO-82173-JIC001.
CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 OUTBOARD I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL
*SDR FILED OPEN* CREW ENTRY DOOR HANDLE LINING PANEL (REF IPC 52-11-02-10A-140) HAS A 2Ãâ¬?X1.5Ãâ¬? HOLE IN HANDLE STOWED POSITION. ACCOMPLISHED INTERIM REPAIR PER EO-90156-REQ1. DEFER UNTIL NEXT C CHECK WITH REPEAT INSPECTIONS NOT TO EXCEED EVERY 30 DAYS.
*SUPPLEMENTAL SDR* CREW ENTRY DOOR HANDLE LINING PANEL (REF IPC 52-11-02-10A-140) HAS A 2Ãâ¬?X1.5Ãâ¬? HOLE IN HANDLE STOWED POSITION. C/W INSTALL OF DOORWAY LINING IN REF TO AMM 52-12-02. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DEFERRAL CONTROL NUMBER 2813867.
NOSE LANDING GEAR FAILED TO EXTENDED. PERFORMED FIM TASK 32-30 TREE 807.<BR><BR>STEP 1. FOUND CHECK VALVES NO.1 AND NO.4 ARE CLEANED. <BR>STEP. 2 FOUND RESTRICTIONS VALVES ON LOCK ACTUATOR ARE CLEANED.
ON ARRIVAL, PILOT REPORTED " NOSE LDG FAILED TO BE EXTENDED ON FIRST ATTEMPT. AFTER GO-AROUND AND CYCLED LDG HANDLE, ALL LDG EXTENDED NORMALLY. T/S ACC. FIM TASK AND REPLACED NOSE LDG LOCK ACTUATOR.
**SUPPLEMENTAL SDR**NOSE LANDING GEAR FAILED TO EXTENDED. R&R DOWN LOCK ACTUATOR IAW 32-34-02-004-001 AND AMM 32-34-02-404-017.
UPON LOWERING THE GEAR ON FINAL APPROACH. NOSE GEAR FAILED TO INDICATE GREEN AND GEAR DISAGREE LIGHT ILLUMINATED. AFTER ALT GEAR EXTENSION RESULTED IN SAFE GEAR INDICATING NORMAL LDG ++ REF FIM TASK 29-11FAULT TREE814 AND FIM TASK 29-11FAULT TREE 841, ADP OPS CHECKED WAS SATIS. DMI IS CLOSED AND DMI PLACARD HAS BEEN REMOVED. DMP IS REVERSED.
*ATB* CABIN ALTITUDE WARNING ALERT AT FL360 CABIN ALTITUDE AT 1600 FEET AND CLIMBING. RAN CABIN ALT CHECKLIST. DESCENDED LOWER ALTITUDE. RAN CABIN AUTOMATIC INOP CHECKLIST BECAUSE AUTO INOP ILLUMINATED RETU PREFORMED SYS TEST OF CABIN PRESSURE CONTROLLER PER FILM 21-31 FAULT TREE 803 NO CURRENT FAULTS FOUND OPS CHECK GOOD AT THIS TIME
**SUPPLEMENTAL SDR**EMERGENCY LIGHTS TURN ON INTERMITTENTLY IN ARMED POSITION. REPEAT WRITE UP LOG G11357 REPLACED EMER LIGHTING POWER SUPPLY AND BATT ASSY. SYS OPS NORMAL. REF AMM 33-51-07.
**SDR FILED OPEN**EMERGENCY LIGHTS TURN ON INTERMITTENTLY IN ARMED POSITION. REAPEAT WRITE UP LOG G11357
EMERG LIGHT NEXT TO CREW ENTRY DOOR BLINKS ON AND OFF PERFORMED OPS CHECK OF EMERGENCY LIGHT PER AMM 33-51-00. OPS CHECK GOOD. NO FAULT NOTED AT THIS TIME.
ON TAXI IN, AFTER LANDING, EMER LIGHTS CAME ON AND STAYED ON WITH SWITCH IN ARMED POSITION DISCONNECTED AND RECONNECTED EMERGENCY LIGHTING BATTERY PACK IAW MM 33-51-07. DISCONNECTED AND RECONNECTED EMERGENCY LIGHTING POWER SUPPLY IAW AMM 33-51-07. PERFORMED EMERGENCY LIGHTS FUNCTIONAL TEST AND EMERGENCY LIGHTS OPERATIONAL TEST WITH CONTROL SWITCHES. OPS CHECK GOOD. NO DEFECTS AT THIS TIME.
ATB, ON CLIMB OUT,(WXR FAIL) DISPLAYED ON BOTH CAPT AND FO ND. INTERMITTENT (WXR SYS) STATUS MESSAGE DISPLAYED. RESULTED IN AIR TURN BACK. OII 1 FOUND EVIDENCE OF ARCHING ON SOCKET 2 CONNECTOR D391C AND NO PIN RETENTION. REPLACED ALL USED SOCKETS OF CONNECTOR D391C SWPM 20-71-14. FOUND EVIDENCE OF ARCHING ON WX TRANSCEIVER PIN 2. R&R WX TRANSCEIVER MM 34-43-01. DURING OPERATIONAL TEST AT 60 MIN WX FAIL CONT MESSAGE. R&R WX RADAR CONTROL PANEL MM 34-43-02. ACCOMPLISHED OPERATIONAL TEST MM 34-43-01 FOR 90+ MINUTES NO FAULTS FOUND.
INSPECTION TYPE:N/A**ATB** AT CRUISE BOTH FMC'S LOST FP AND FROZE UP ,LOST ALL VNAV, NO INPUTS WOULD WORK.C/W'D FIM, 34-61-00-854, GROUND TEST-OPERATION-PASSED.
INSPECTION TYPE:ETOPRIGHT ENGINE EEC POWER CH "A" CIRCUIT BREAKER OPENR & R # 2 ENG EEC CH "A" RELAYS K01171 , K01039 K01174 IAW SWPM 20-81-22 NO FIX 5079816 07/24/22} RAN RT ENG 3X WITH NO FAULTS WRX AMM 71-00-00-795-034-H03 GROUND OPS CHECKS GOOD OK FOR SERVICE
INSPECTION TYPE:C12CRACK ON NOSE SKIN (P/N: 114T4105-23) OF NO.5 SLAT AT OSS 492.45REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.83.02
INSPECTION TYPE:NA** AIR TURN BACK ** L ENG BLEED OFF EICAS ILLUMINATED. L ENG BLEED OFF LIGHT REMAINED ILLUMINATED . QRH PROCEDURE COMPLETED. TURNBACK AFTER CONSULTATION WITH COMPANY. COMPANY REQUESTED CREW RETURN TO KIX TO REPAIR AIRCRAFT AND ACCOMODATE CREW.C/W AIR SUPPLY CONTROL SYSTEM BITE PER MM36-23-00-501,FOUND L PRSOV FAULT IN BITE. R/RED LH PRSOV PER MM36-11-09-201, TEST OK. NO LEAKAGE NOTED & NO FAULT FOUND IN BITE. PRECAUTIONARY REPLACED BLEED AIR CONT CARD PER MM36-11-12-401 RUN ENG PER MM71-00-00-201. ALL IND NORMAL. PN ON/OFF799801-4 SN ON
INSPECTION TYPE:NAIT TOOK SEVERAL ATTEMPTS TO PUSH YELLOW DOOR HANDLE TO PROPER POSITIONR&RED FWD ENTRY DOOR CAPTURE SYSTEM PAWL & SPRING REF IPC 52-12-25-02 ITEM 730 & 725 & ACCOMPLISHED ADJ TEST REF AMM 52-12-00 PAR D(3) & D(5)(C) OPS CK NORMAL. INTERIOR YELLOW CAPTURE HANDLE OPERATES SMOOTHLY
ATB** EMERGENCY DECLARED** LANDED UNEVENTFULLY** ON TAKEOFF ROLL JUST PRIOR TO V1 WE GOT A CONFIG LIGHT, SPEED BRAKES LIGHT GEAR NOT DOWN EICAS MESSAGE AND SPOILERS EXT EICAS MESSAGE ALONG WITH MASTER WARNING AND CAUTION LIGHTS AND HORN. ALL REMAINED ON UNTIL POWER REMOVED IN BLOCKSR&R T/O CONF CARD M620 AND WARNING CONF M983 IAW 767 AMM 31 51 04 WEU CARD TEST PASS IAW 767 AMM 31 51 04 ESR 767 IPC 31 51 04 056 490, 31 51 04 05C 05C
DUE TO INBOUND ITEM "GEAR NOT DOWN" EICAS MESSAGE. CHECKED GEAR DOWN LOCK SENSORS REF SSM 32 61 01 SH. 1 FOUND TARGET NEAR VALUES AS FOLLOWS. S236 AT 5.25 MH, S232AT 5.20 MH -S236 AT 5.25MH, S254 AT 5.23MHADJUSTED SENSORS, AFTER ADJUSTMENTS. WITH TARGET NEAR VALUES WERE AS FOLLOWS S236 AT 5.62 S232 AT5.82 MH, S258 AT5.63 MH, S254 AT5.78 ALSO CHECKED SENSOR CIRCUITS FOR SHORTS TO GND. WITH MEG OHM METER FOUND OK. REF MM 32 61 02 AND 32 61 03.
L ENG HPSOV APPEARED SHORTLY AFTER T/O FOR A FEW SECONDS THEN DISSAPPEARED FOR REMAINDER OF FLIGHT. L ENG HPSOV REMAINS ON STATUS PAGE. CONFIRMED FAULT AND DEFERRED PER MEL 36-11-2-2. C/W DMP PER DMP 36-11-2-2 AND INSTALLED PLACARD AS REQUIRED.REPLACED WITH NEW HPC IAW MM 36-11-08/4011RC IAW AMM 36-11-08 ACCOMPLISHED LEAK TEST OF HPC & DMP 36-11-2-2 REVERSED HIGH PRESSURE SHUTOFF VALUE SYS. OPS CK GOOD IAW AMM 36-11-07. 36-11-08-08.
INSPECTION TYPE: NA DURING PS1 CK FOUND EMERGENCY LIGHTS INOPERABLE. REMOVED & REPLACED EMERGENCY LIGHTS BATTERY PACK, AS PER 767 MM 33-51-07-201 TASK 022-001/TASK 422-012. OPERATIONS CK GOOD, IPC 33-51-07-41-30.
INSPECTION TYPE:C11 CRACK ON FUSELAGE SKIN AND CHORD STRAP NEAR STA 1725.5. REPAIR IAW SRID:4-4801590830, EO B767-5330-76807-A AND UPS EO B767-5330-24301-F.
INSPECTION TYPE:C11 CRACK ON FUSELAGE SKIN AND CHORD STRAP NEAR STA 1725.5. REPAIR IAW SRID:4-4801590830, EO B767-5330-76807-A AND EO B767-5330-24301-F.
INSPECTION TYPE:C11 CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2011-5) ON STA 785.9, LBL 55. REPAIR IAW SRM 57-10-10-2R-2 REPAIR 2 REV 77.00 AND EO B767-5740-76705-A.
INSPECTION TYPE:C11 CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2005-8) ON STA 785.9, RBL 11. REPAIR IAW SRM 57-10-10-2R-2 REPAIR 2 REV 77.00 AND EO B767-5740-76705-A.
INSPECTION TYPE:NA** SUPPLEMENTALSDR** VOICE/DATA SWITCH STARTED TO SMOKE MAINT NOTIFIED IMMEDIATLY SMOKE IN COCKPIT WAS LIGHT. GVI OF PEDESTAL CARRIED OUT FAULT ISOLATED ONLY ON VOICE/DATA SWITCH BODY THAT WAS FOUND SLIGHTLY BURNED. NO OTHER PANEL ASSY INVOLVED. A.C RELEASED IAW MEL 23-22-1A CAT C. DMI M705472 RAISED PLACARD INSTALLED AND DI LOG UPDATED.R/R ACARS SWITCHING PANEL IAW B767 AMM 23-22-05. CONNECTED TO D705473 (CIRCUIT BREAKERS). RESET CB'S G6 & G33 ON PANEL 11 & RECONNECTED D2891. OPS CK GOOD. OK FOR SERVICE
INSPECTION TYPE:N/AMAIN CARGO DECK FLOOR PANEL AT STATION 700 / POS. 4 CENTER LINE - MAIN CARGO COMPARTMENT FLOOR PANEL REPAIR - 1"X.25 HOLE IN FLOOR PANELPOTTING REPAIR COMPLIED WITH IAW SRM 53-00-50-2R
INSPECTION TYPE:N/AEMERGENCY LIGHTS INOP.R&R BATTERY CHARGER AND BATTERY IAW MM 33-51-07-201. EMERGENCY LIGHTS TEST GOOD IAW MM 33-51-00-501.
INSPECTION TYPE:N/A CAPTAIN NOTIFIED MX OF MAIN DOOR CAPTURE STIFF ( CREW ENTRY). REPLACED CREW ENTRY DOOR PANEL FOR CAPTURE REF AMM 52-12-25-822-024 AIPC 52-12-25-02 ITEM 730.
INSPECTION TYPE:N/A EMERGENCY DECLARED - C HYD SYS PRESSURE LIGHT ENROUTE. ALTERNATE GEAR EXTENSION & ALTERNATE FLAP EXTENSION FOR LANDING. FOUND C2 PRESSURE SWIFELY LEAKING AT MANIFOLD R&R DELTA P REF 29-11-18-01 # 240 LEAK CK OK. IPC 29-11-18-01 # 240
FUSELAGE SKIN DENT REPAIR AT BS 620, STRINGERS 27L TO 28L REPAIRED IAW EO B767-5330-69067-B.
INSPECTION TYPE:NA CREW ENTRY DOOR HAS 2 INCH GOUGE (INSIDE) UPPER LEFT CORNER PANEL. DEFERRED IAW EO B767-2520-72644-A C/W EO B767-2520-72644-A 6A. **SUPPLEMENTAL SDR** REPAIRED MAIN ENTRY DOOR PANEL AS REQUIRED. REF CMM CH 25-00-66. THIS CLEARS D670417.
INSPECTION TYPE:C10, DISBOND ON EXISTING REPAIR OF LT WING INBD AFT FLAP UPPER SKIN AT IFS 240.5. REPAIR IAW SRID:3-4228853096 AND EO B767-5750-68832-A.
INSPECTION TYPE:C10, CORROSION ON HOUSING (P/N:452T2136-2) AT FWD CGO COMPT PALLET LOCK SUPPORT STRUCTURE NEAR STA 535, RBL 38. INSTALL NEW PART IAW SRM 51-40-02-0G REV 71.
INSPECTION TYPE:C10, CORROSION ON HOUSING (P/N:452T2136-2) AT FWD CGO COMPT PALLET LOCK SUPPORT STRUCTURE NEAR STA 596 , RBL 37. INSTALL NEW PART IAW SRM 51-40-02-0G REV 71.
INSPECTION TYPE:C10, CORROSION ON HOUSING (P/N:452T2136-2) AT AFT CGO COMPT PALLET LOCK SUPPORT STRUCTURE NEAR STA 1322 , RBL 44.40. INSTALL NEW PART IAW SRM 51-40-02-0G REV 71.
INSPECTION TYPE:C10, CORROSION ON HOUSING (P/N:452T2136-2) AT AFT CGO COMPT PALLET LOCK SUPPORT STRUCTURE NEAR STA 1228 , RBL 44.40. INSTALL NEW PART IAW SRM 51-40-02-0G REV 71.
INSPECTION TYPE:C10, CRACK ON THE CENTER WING FRONT SPAR STIFFENER (P/N:111T2008-12) UPPER SIDE AT STA 785.9 , RBL 33. REPAIR IAW SRM 57-10-10-2R-2 REPAIR 2 REV 71 AND EO B767-5740-58151-A.
INSPECTION TYPE:C10, CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287, RBL 25, WL 170. REPAIR IAW EO B767-5310-63472-C AND EGAT EI F2018A53M3009 REV 1 AND EO B767-5310-68834-A.
INSPECTION TYPE:C10, CRACK ON THE CENTER WING FRONT SPAR STIFFENER (P/N:111T2005-7) UPPER SIDE AT STA 785.9 , LBL 11. REPAIR IAW SRM 57-10-10-2R-2 REPAIR 2 REV 71 AND EO B767-5740-58151-A.
INSPECTION TYPE:C10, CRACK ON THE CENTER WING FRONT SPAR STIFFENER (P/N:111T2008-11) UPPER SIDE AT STA 785.9 , LBL 33. REPAIR IAW SRM 57-10-10-2R-2 REPAIR 2 REV 71 AND EO B767-5740-58151-A.
INSPECTION TYPE:C10, DENT ON LT WING INBD AFT FLAP UPPER SKIN AT IFS 151.25. REPAIR IAW SRM 57-53-01-2R-1 REPAIR 1 REV 71, SRM 51-70-10-2R REPAIR GENERAL REV 71.
FIRST OFFICER`S OXYGEN MASK INOPERATIVE. PROPERLY INSTALLED THE OXYGEN MASK IAW AMM 35-11-51-404. OPS CHECKED OK.
STATUS MESSAGE FOR CABIN ALTITUDE AUTO 2. OPEN.
THE NR 2 ENGINE LOWER SUPPORT LINK ON STARTER DUCT WORN. REPLACED THE SUPPORT LINK IAW AMM 80-11-05.
LEFT ENGINE FUEL FILTER EICAS, EMERGENCY DECLARED, AIR TURNBACK IAW FIM 73-11-00-815. R & R THE LT ENGINE FUEL FILTER & DIFFERENTIAL PRESSURE SWITCH IAW AMM 73-34-01-024, & 73-11-02-004.
MAIN ENTRY DOOR HARD TO OPEN AND CLOSE. FOUND AFT RETAINER SEAL RUBBING DOOR. REPLACED FWD AND AFT RETAINER SEAL IAW AMM 52-11-01.
INSPECTION TYPE: C, DURING MAJOR MAINTENANCE VISIT 6995 FOUND DENT AT BULK CARGO DOOR FWD LOWER CORNER WITHIN ALLOWABLE DAMAGE, REF EGAT NRC FFU05019 EVALUATED DAMAGE IAW SRM 52-30-01-1A-1, DETAIL VI REV 65.00 INFORMATION SUBMITTED FOR ADM DENT WITHIN ALLOWABLE DAMAGE LIMIT.
MCD FLOOR PANEL, POSITION 4 CENTER PANEL DAMAGED, PN 143T5876-87. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693I.
INSPECTION TYPE:ETOP, AIR TURNBACK DUE TO RT FMC FAIL, EICAS CANT DNL EICAS DISPLAY, RT IRS ON DC F/O RMI FAIL, LOWER EICAS BLANK F/O FLT DIR, MAP AND VTR, VOR/ DME FOUND C/B C307, 115VAC BUS RT SECT 2 IN P6 PANEL POP. RAN BOTH ENGINES AND BITE CK BPCU NO FAULTS FOUND. PARTS ON ORDER REF REQ E146509 FC, 1071953. C/W ITEM T169552, 5OOV & 1KV MEG OHMED HARNESS TO GROUND AND TO EACH OTHER AT A2-B2-C2, ALL SHOW 999M OHMS. R & R C/B C307 OPS. GOOD AT THIS TIME.
REMOVED ROPE FWD ENTRY DOOR EMERGENCY/ESCAPE AND CHANNEL DUE TO ROPE & COVER RIPPED AND FRAYED. R & R ROPE CHANNEL EMERGENCY ESCAPE IAW AMM 25-61-04, PN ON 416T1601-6, SN ON TAG 058615A.
INSPECTION TYPE: 7C, LT WING INBD AFT FLAP UPPER SURFACE DENT. METAL HOT BOND REPAIR PERFORMED IAW EO B767-5750-47346-A AND HAECO RS R-57-57-37356, REV A.
INSPECTION TYPE: 7C, LT WING INBD AFT FLAP UPPER SURFACE DENT. METAL HOT BOND REPAIR PERFORMED IAW EO B767-5750-47346-A AND HEACO RS R-57-57-37356, REV A.
INSPECTION TYPE: 7C, RT WING INBD MAIN FLAP T/E FIXED PANEL LOWER SURFACE DELAMINATED AT NR 1 SUPPORT ARM AREA COUNT FROM INBD COMPOSITE WET LAY UP. REPAIR CARRIED OUT IAW SRM 51-70-17, PAR 4A (1) FIG 10, REV 52.
INSPECTION TYPE: 7C, LT WING NR 1 SLAT OTBD UPPER SURFACE FOUND DELAM. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 2 AND SHEET 3, REV 52.
INSPECTION TYPE: 7C RT WING INBD MAIN FLAP AFT T/E PANEL LOWER SURFACE DELAMINATED AT NR 2 SUPPORT ARM AREA COUT FROM INBD COMPOSITE WET LAY UP. REPAIR CARRIED OUT IAW SRM 51-70-17 PAR 4A (1) FIG 10, REV 52.
INSPECTION TYPE: 7C, RT WING INBD MAIN FLAP T/E FIXED PANEL LOWER SURFACE DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-17 PAR4A (1) FIG 10, REV 52.
INSPECTION TYPE: 7C, RT W INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A(1). FIG 5, REV 52.
INSPECTION TYPE:7C, LT WING OTBD T/E FLAP, T/E WEDGE, UPPER SURFACE MID AREA DELAMINATED AT 213" FROM INBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 9, REV 52.
INSPECTION TYPE: 7C, LT WING INBD AFT FLAP LOWER SURFACE DENTED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 1, REV 52.
INSPECTION TYPE: 7C, RT WING INBD AFT FLAP LOWER SURFACE DENTED. METAL HOT BOND REPAIR PERFORMED IAW EO B767-5750-47345-A AND RS R-57-57-37355, REV A.
INSPECTION TYPE: 7C, RT WING OTBD FLAP T/E WEDGE UPPER SURFACE MID AREA DELAMINATED FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 9, REV 52.
INSPECTION TYPE: 7C, RT WING INBD AFT FLAP LOWER SURFACE DENTED. METAL HOT BOND REPAIR PERFORMED IAW EO B767-5750-47345-A AND RS R-57-57-37355, REV A.
INSPECTION TYPE: 7C, LT WING OTBD FLAP T/E WEDGE UPPER SURFACE MID AREA DELAMINATED AT 174" FROM INBD EDGE FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1), FIG 9, REV 52.
INSPECTION TYPE: 7C, LT WING NR 4 SLAT INBD NOSE SKIN REPAIR FREEZE PLUG FOUND LOOSE. LT WING NR 4 SLAT INBD NOSE SKIN REPAIRD IAW SRM 57-43-01-2R2, REPAIR 2, FIG 201, REV 52 AT 0SS572.5, ORIGINAL MATERIAL 7075T6-0063" CUTOUT SIZE 8.875"X7.375" REPAIR IS CLASSIFIED A MAJOR REPAIR WITH MATERIAL 7075T6-0071" REPAIR DOUBLERS AND 7075T6-0063" REPAIR PLATE REPAIR SIZE IS 12" X 10.5".
INSPECTION TYPE: 7C, RT WING NR 10 SLAT OTBD NOSE SKIN REPAIR FREEZE PLUG FOUND LOOSE. RT WING NR 10 SLAT OTBD NOSE SKIN REPAIRD IAW SRM 57-43-01-2R2. REPAIR 2, FIG 201, REV 52, JUST AT OSS 792.5 ORIGINAL MATERIAL 7075T6-0063" CUTOUT SIZE 8.875"X7.25" REPAIR IS CLASSIFIED A MAJOR REPAIR WITH MATERIAL 7075T6-0071" REPAIR DOUBLERS AND 7075T6-0063" AS REPAIR PLATE REPAIR SIZE IS 12" X 10.375".
FLOORBOARD DAMAGED AT STA 1019 1" DIA HOLE 27.5" AFT OF L/E AND 6" INBD OF OTBD EDGE. REPAIRED IAW SRM 53-00-50-2R FILL AND REPAIR PLIES.
INSPECTION TYPE: ETOP DIVERSION - DUE TO OIL LEAK FROM APU LOW OIL PRESS SWITCH. ONE ADP ON DEFERRAL. ALSO RECEIVED APU FAULT LIGHT AND EICAS MSG. APU WOULD NOT RESTART. R & R APU LOW OIL PRESS SWITCH.
DIVERSION - EICAS MSG FLAP/SLAT ELEC DISPLAYED AFTER TAKEOFF. T/S C/O IAW FIM 29-51-00, FIG 114, SH 1 BLOCK 1 & 21. NO FAULTS NOTED, SYS OK. FIM REV 48.
INSPECTION TYPE:PS1, EMERGENCY EXIT LIGHT ASSY TABS TO HOLD LIGHT COVER ON WORN. R & R EMERGENCY LIGHT ASSY IAW MM 33-51-01-2.
INSPECTION TYPE:C, NR 1 PYLON INTERNAL LT SIDE BS 285.45 VERTICAL FRAME CRACK NR1 PYLON INTERNAL LT SIDE BS285.45 VERTICAL FRAME REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02.
INSPECTION TYPE:C, MCD STA 540 TO 654+22 LBL 33 TO LBL 55, FLOOR PANEL FOUND 1EA DAMAGED AND 4 DENTS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REINSTALLED IAW AMM 53-01-01.
INSPECTION TYPE:C, MCD STA 540 TO 654+22, LBL 11 TO RBL 11 FLOOR PANEL FOUND 4 DAMAGED & 10 DENT FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REINSTALLED IAW AMM 53-01-01.
INSPECTION TYPE:C, MCD STA 540 TO 654+22, LBL 11 TO LBL 33, FLOOR PANEL, FOUND 1 DAMAGED & 9 DENT. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REINSTALLED IAW AMM 53-01-01.
INSPECTION TYPE:C, MCD STA 930 TO 977, RBL11 TO RBL33, FLOOR PANEL FOUND CRACK FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REINSTALLED IAW AMM 53-01-01.
INSPECTION TYPE:C, LT WING INBD MAIN FLAP L/E FOUND DELAMINATION COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5.
INSPECTION TYPE:C, MCD STA540 TO 654+22 LBL 55 TO LBL 77 FLOOR PANEL FOUND 1 DAMAGED & 6 DENTS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REINSTALLED IAW AMM 53-01-01.
INSPECTION TYPE:C, SURVEY SEQUENCE NR 330-F1-02 THE EXISTING REPAIR DOES NOT CORRLATE TO A SRM JUST AT BS 328 TO BS 345 BETWEEN S35R AND S37R SURVEY SEQ NR 330-F1-02, FX SKIN REPAIRED IAW R53-31-36782 & EO B767-5330-38845 JUST AT BS328 TO BS345 BTN STR35R & STR37R THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MATL CLAD2024T3-0090" AS REPAIR DOUBLER, FINAL CUTOUT SIZE IS 3" X 3.8", REPAIR SIZE 13.25" X 11.125" REPEAT INSP THEREAFTER, 9000 FLIGHT CYCLES.
INSPECTION TYPE:C, RT WING NR 7 SLAT T/E WEDGE FOUND CHAFED. METAL HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 8.
INSPECTION TYPE:C, MEC COMPT STA 246 FLOORBEAM ATT STIFFENER FOUND CRACK AT LBL40" MEC COMPT BS 246 LBL40" FLOORBEAM ATT STIFFENER REPAIRED IAW SRM 53-10-51-2R4, FIG 201, ORG MATL IS BAC1490-2793-7075T62, CRK LENGTH IS 1", THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL 7075T6-0063" AS STIFFENER. REPEAT INSP AT 3000 FLIGHT CYCLES OR 24 MONTHS WHICH EVER OCCURS FIRST IS REQUIRED. REPAIR LENGTH IS 14.5"
INSPECTION TYPE:C, SURVEY SEQUENCE NR 330-F1-01 THE EXISTING REPAIR DOES NOT CORRELATE TO A SRM JUST AT BS 143 TO BS 164 BETWEEN S21R AND S27R SURVEY SEQ 330-F1-01 FX SKIN REPAIRED IAW R53-11-36792 & EO B767-5330-38856 JUST AT BS143 TO BS164 BTN STR21R & STR27R THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MATL CLAD2024T3-0071" AS REPAIR DOUBLER, FINAL CUTOUT SIZE IS 9" X 4.15" REPAIR SIZE 21" X 12" REPEAT INSP THEREAFTER 12000 FLIGHT CYCLES INTERVALS.
INSPECTION TYPE:C, DMI D423950 - E/E BAY ACCESS DOOR CRACK - INTERIM REPAIR E/E BAY ACCESS DOOR PREVIOUS CRACK AREA BLENDED DEPTH 0.20" AND LENGTH IS 1" IS ACCEPTACBLE IAW HX RS R52-00-36779 AND EO B767-5240-38816.
INSPECTION TYPE:N/A RT WING NR 7 SLAT 3EA BRACKET NR 10, 11, 12 FOUND CRACK. CRACK LENGTH .5 INCH APPROX. RT WING NR 7 SLAT 3EA BRACKET NR 10, 11, 12 REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:C RT WING FRONT SPAR AREA LES 680 D-NOSE WEB FOUND CRACK (CRACK LENGTH .5 INCH). D-NOSE WEB REPAIRED AS PER SRM 57-41-13-2R3 FIG 201 REPAIR 3.
INSPECTION TYPE:N/A LT WING NR 6 SLAT INNER LOWER NR 5 AND NR 8 BRACKET FOUND CRACK 2EA CRACK LENGTH .5 INCH APPROX. TWO BRACKETS REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:N/A CABIN STA 246 LBL 50 FLOORBEAM ATT STIFFENER CRACKED. CRACK LENGTH 1 INCH. DEFECTIVE STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:N/A CABIN STA 246 RBL 10 FLOORBEAM ATT STIFFENER CRACKED. CRACK LENGTH 1 INCH. DEFECTIVE STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02.
INSPECTION TYPE:N/A LT WING I/B MAIN FLAP AFT FLAP I/B SUPPORT FITTING FOUND CRACK. CRACK LENGTH .5 INCH APPROX. HINGE FITTING REPAIRED AS PER SRM 57-53-02-2R1 FIG 201.
INSPECTION TYPE:N/A CABIN STA 240 LBL 25 FLOORBEAM ATT STIFFENER CRACKED. CRACK LENGTH 1 INCH. DEFECTIVE STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:N/A EMP - JACKSCREW COMPARTMENT RT STA 1767.25 (STR 22) SUPPORT BRACKET FOUND CRACK. CRACK LENGTH .5 INCH APPROX. SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:N/A AFT CARGO COMPT STA 1324 FLOOR SUPPORT BEAM UPPER WEB FOUND CRACKED. CRACK LENGTH 1 INCH APPROX. FLOOR SUPPORT BEAM UPPER WEB REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:C AFT CARGO COMPT STA 1087 RBL 25 UNDER FLOOR BRACKET FOUND CRACK (CRACK LENGTH 1 INCH). BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:N/A DMID383810 - RT WING L/E SKIN GOUGE TEMP REPAIR I/B NR 2 ENG ABOVE KRUEGER FLAP. RT WING L/E SKIN AT BETWEEN ISS337.6-345.5 AREA SKIN REPAIRED AS PER RS R57-41-36117 & UPS EO B767-5730-30466-A.
INSPECTION TYPE:ETOP APU BLEED INOP DEFERRED M 356254. T/S PER FIM APU BITE SHOWED PT SENSOR WITH MINIFLAG 14. REMOVED AND REPLACED FLOW SENSING MODULE PER MM 49-53-08-4. OPS AND BITE CHECK GOOD. THIS CLEARS M356254.
INSPECTION TYPE:N/A THE EMERGENCY EXIT LIGHT SWITCH DOES NOT RETURN TO THE ARMED POSITION WHEN THE SWITCH CAP IS CLOSED. REMOVED AND REPLACED EMERGENCY LIGHT PANEL ASSY IAW AMM 33-50-00. OPS CHECKS OK.
INSPECTION TYPE:N/A DIVERSION - ALL 3 ILS SYSTEMS INOP. REPLACED ILS CONTROL PANEL PER AMM 34-31-02-4. OPS CHECKS GOOD.
WEATHER FAIL ON HSI, BOTH SIDE (INTERMITTENT). T/S PERFORMED ACC TO FIM 34-43-001 FIG 103, NO FAULT FOUND. SYST WORKS PROPERLY. WEATHER RADAR DRIVE UNIT AND TRANS. REPLACED BY AMM 34-43-05-4, TRANSC P/N OFF 622-5432-101 S/N OFF: 2904 S/N ON: 2108 P/N ON: 622-5432-109 S/N OFF: 6086 S/N ON: 7508.
INSPECTION TYPE:N/A, F/O SMOKE GOGGLES CRACKED. INSTALLED NEW SET OF SMOKE GOGGLES.
AT FL 330 RT ENG COMPRESSOR STALLED. 1ST STALL RT ENG VIB WAS 3.2 / 2ND VIB WAS 5.0. ENG THRUST WAS RETARDED TO IDLE. ON SHUTDOWN ENG READINGS WERE N1L 28.3 R28.7 EGTL 411 R480 N2L 69.0 R 72.0 FFL 1.3 R1. 5. R/R NR 2 ENG PER TC 6002 AND TC 6001. NO DEFECTS NOTED. OPS CK GOOD.
INSPECTION TYPE:N/A PILOT REP, FWD ENTRY DOOR SQUEALING. BUILT UP THRESHOLD AND PRESSURIZED A/C LEAK CHECKS GOOD.