N320UP
Registered owner: UNITED PARCEL SERVICE CO, 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
EMERGENCY DECLARED, FLAP INDICATOR DISAGREE ,RAN QRH CHECKLIST.RT TE PLAP INDICATOR EVENTUALLY UNSTUCK REMOVED AND REPLACED FLAP INDICATOR AS PER AMM 27-58-02, OPS TEST OK
CRACKED COLLAR , NR 1 PYLON AFT FAIRING AFT BULKHEAD FWD CHANNEL INBD SIDE TOTAL 2 EA. INSTALLED NEW COLLAR IAW SRM 51-40-02-0G, REV 95, & DWG 313T3380, SH 3, REV F.
FOUND ENG-1 RT THRUST REVERSER CASCADE SUPPORT RING CRACK AT 9 O'CLOCK. REFERENCED TASK T3F18E008RMGN INSTALLED THE T/R, FAN COWL AND ACCOMPLISHED THE INSTALLATION TEST.
CHAFED LONGERON, NR 1 ENG RT CORE COWL AFT LWR INNER CHORD EDGE AREA. INSTALLED A NEW LONGERON IAW SRM 51-40-02-0G REV.95 AND CMM IPL 71-13-24, REV 50.
BROKEN SEAL, NR 1 PYLON FAIRING PANEL NR 436 CR SPRING SEAL BROKEN. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 95, AND DWG 311T2570, SHT 14, REV -.
CHAFED STRIP, NR 1 ENG RT CORE COWL INNER AFT UPPER STRIP CHAFING. INSTALLED A NEW WEAR STRIP IAW SRM 51-40-02-0G, REV.95, AND CMM IPL 71-13-24 REV. 50
CHAFED EDGE, NR 2 ENG RT T/R BLOW OUT DOOR L/E AREA. INSTALL WITH DOOR ASSY IAW SRM 51-40-02-0G, REV 95, AND AIPC 78-31-51-03, REV 141 AND IPC 78-32-22 REV.96 AND AMM 78-31-19-402-008-H00, REV 147.
CHAFED DOOR , NR 1 ENG RT T/R LWR BLOW OUT DOOR L/E AREA. INSTALL WITH DOOR ASSY I.A.W SRM 51-40-02-0G REV.95 AND BOEING AIPC 78-31-51-03 REV. 141 AND ST ENGINEERING IPC 78-32-22 REV.96 AND AMM TASK 78-31-19-402-008-H00 REV: 147
CHAFED BRACKET, NR 1 ENG RT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-24 REV. 50
CHAFED BRACKET , NR 1 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-23 REV. 47
CHAFED BRACKET, NR 2 ENG, RT T/R CLOSURE DOOR T/E AREA. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND IPC 78-32-22 REV.96
DENTED SCUFF PLATE, LOWER SIDE OF BULK CARGO DOOR CUTOUT. IAW AMM 53-13-02-404-007, REV 147, TO INSTALL BULK CARGO DOOR SCUFF PLATE CENTER.
FAULT - CRACK - ANGLE, NO.2 ENG L/H T/R DRAIN TUBE SUPPORT BRACKET. (REPLACE) INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-51 REV.96
BROKEN - PAN - SEAL, R/H WING SLAT NO.7 OUTBD SIDE. IAW PL 114T3200 REV. W DWG 114T3200 SHEET 3 REV. A & AMM 20-11-00-910-802 REV. 147 TO INSTALL THE SEAL PAN PN: 114T3187-2.
CHAFING - CHANNEL , NO. 1 ENG L/H T/R AFT LWR FAIRING L/E AREA (REPLACE) INSTALL NEW CHANNEL I.A.W SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-01 REV.96
BROKEN SEAL, NR 1 ENG LT TRANSLATING COWL AFT LWR FAIRING INNER AREA. INSTALLED A NEW SEAL IAW SRM 51-40-02-0G, REV 95, AND IPC 78-32-31, REV 96.
BROKEN - CLAMP, CREW ENTRY DOOR UPPER CUTOUT AREA. (REPLACE) I.A.W SWPM 20-10-12 REV.91 REPLACED CLAMP AT CREW ENTRY UPPER CUTOUT AREA AND CONDITION CHECK NORMAL.
BROKEN CLAMP, CREW ENTRY DOOR UPPER CUTOUT AREA.
FRAYED SEAL, NR 1 ENG LT TRANSLATING COWL AFT LWR FAIRING INNER AREA. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G, REV 95,
FOUND RT WING NR 12 SLAT OTBD SIDE MAIN TRACK SKEW DETECTION BRACKET BROKEN. REPLACED IAW AMM 27-81-34-404-014, REV 147, INSTALLED RT WING NR 12 SLAT OTBD SIDE MAIN TRACK SKEW DETECTION BRACKET.
CHAFED BRACKET, NR 1 ENG LT T/R LWR CLOSURE DOOR T/E AREA. INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.95 AND IPC 78-32-21 REV.96
CRACKED COLLAR, NR 2 PYLON AFT LWR FAIRING AFT FRAME OTBD SIDE FWD SURFACE. INSTALLED NEW COLLAR IAW SRM 51-40-02-0G, REV 95, & DWG 313T3380, SH 3, REV F.
FOUND RT WING NO.12 SLAT OTBD SIDE MAIN TRACK SKEW DETECTION BRACKET BROKEN.
CHAFED QUARD, MEC DOOR CUTOUT RT AREA. INSTALLED A NEW GUARD IAW SRM 51-40-02-0G, REV 95, AND DWG 141T6300, SH 1, REV J.
LEFT WING AT LEADING EDGE SPAR AREA LWR PANEL ATTACH STRUCTURE AT NR 1 SLAT INBD DRIVE MOTOR LINK IS DEFORMED. REPAIR DAMAGE AREA IAW SRM 57-41-01-2R-4, REPAIR 4, REV 95, AND WORK SHEET 60290.
LEFT WING AT LEADING EDGE SPAR AREA LWR PANEL ATTACH STRUCTURE AT NR 2 SLAT OUTBD DRIVE MOTOR LINK IS DEFORMED. REPAIR DAMAGE AREA IAW SRM 57-41-01-2R-4, REPAIR 4, REV.95 AND WORK SHEET 60291.
NR 1 PYLON AFT LEFT SIDE FRAME WAS CHAFED. REPAIR DAMAGE AREA IAW EO-97331-REQ1 REV 1 AND EI F2026A54M-937 REV. 0.
GOUGED DEPRESSOR SEAL AT MAIN DECK CGO DOOR CUTOUT AREA FWD SIDE STA 492 2EA (REPLACE) INSTALLED MAIN DECK CARGO DOOR DEPRESSOR SEAL AT FWD SIDE I.A.W AMM 20-10-00-910-802 REV.147.<
CRACKED FAIRING , INBD SIDE FWD EDGE OF LT WING NR 3 FLAP TRACK AFT FAIRING. IAW AMM 51-21-10-307-020, REV 147, REPAINTED AREA. I.A.W AMM 27-51-15-424-029 REV 147 INSTALL NO.3 FLAP AFT FAIRING. CONDITION CHECK NORMAL.
CRACKED ANGLE AT BULK CARGO, BS 1578, LBL 78, INBD. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 146T5650 SH 5 REV: C
CRACKED ANGLE, BULK CARGO BS 1578, LBL 78 OTBD. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G, REV 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95, AND DWG 146T5650, SHT 5, REV C.
BROKEN SEAL, NR 2 PYLON RT FAIRING PANEL 446CR. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 95, & DWG 311T2570, SHT 14, REV -.
CRACKED ANGLE, NR 1 PYLON AFT FAIRING AFT BULKHEAD INNER INBD. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95, AND DWG 313T3380, SHT 3, REV F.
CRACKED ANGLE, NR 2 PYLON AFT LWR FAIRING AFT FRAME OUTBD SIDE SUPPORT ANGLE. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95, AND DWG 313T3380, SHT 3, REV F.
BROKEN SEAL, NR 2 PYLON LT FAIRING PANEL 446CL AREA. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 95, & DWG 311T2570, SHT 14, REV -.
CRACKED ANGLE, LT WING L/E REFUELINGS STATION LOWER DOOR CUTOUT INBD STOP SPRING, ACCESS PANEL NR 521QB. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95, & DWG 114T2450, SHT 1, REV J.
CHAFED FIRESHIELD, NR 1 PYLON FAIRING PANEL 436BL INNER PLATE. Â INSTALLED A NEW FIRESHIELD IAW SRM 51-40-02-0G, REV 95, AND DWG 311T2570, SH 14, REV -.
CHAFED FIRESHIELD, NR 2 PYLON LT FAIRING PANEL 446BL. Â INSTALLED A NEW FIRESHIELD IAW SRM 51-40-02-0G, REV 95, AND DWG 311T2570, SH 14, REV -.
CRACK, NR 1 PYLON AFT FAIRING AFT BULKHEAD INNER OUTBD ANGLE CRACKED. INSTALLED A NEW CLIP IAW SRM 51-40-02-0G, REV 95, AND DWG 313T3380, SH 3, REV F.
CRACKED BRACKET, NR 2 PYLON AFT LWR FAIRING INBD SIDE DRAIN TUBE SUPPORT BRACKET. INSTALL NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND DWG 272T0333, SH 8, REV A.
FAULT - BENT ANGLE IN LOWER FORWARD CARGO COMPARTMENT CEILING AT STA 478-500, RBL 80 (NO.6623) (AGING AIRRCAFT INSPECTION) INSTALL NEW CLIP-ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 143T8550 SH 4 REV: -
FAULT - AFT LOWER CARGO DOOR SEAL DEPRESSOR BENT AT LOWER AFT CORNER (NO.6625) (AGING AIRCRAFT INSPECTION) INSTALL NEW DEPRESSOR SEAL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 146T8575 SH 1 REV: A, SH 2 REV: A
DEBONDED SKIN, INBD EDGE LOWER FACE OF LT WING T/E, OTBD FLAP LOWER SKIN, WBL 355. IAW CMM 57-53-51, REV 38, AND AMM 20-11-00-910-802 REV 147 INSTALLED THE OTBD FLAP INBD UPPER AND LOWER SIDE SEAL WITH RETAINER.
MAJOR REPAIR, CORROSION-FUSELAGE SKIN IMMEDIATELY SURROUNDING THE DRAIN VALVE AT STA 1410 BETWEEN S-38R AND S-39R. (REPAIR) INSTALLED BULK CARGO FLOOR PANEL IAW AMM 53-01-05-404-004 REV.1472. CONDITION CHECK NORMAL.
FAULT- CRACK- TORQUE TUBE SUPPORT BRACKET, RH WING INBD LE COMPARTMENT. Â INSTALL NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND DWG 114T1240, SH 4, REV D.
FAULT- FOUND THE LOWER RUDDER PCA LEAK. (REPLACE) AMM 27-21-02-422-038 REV 147 STEP 5A TO 5H INSTALL LOWER RUDDER PCA
FOUND SEAT TRACK ASSY INBOARD AFT INBD FWD OF CAPTAIN SEAT WORN . I.A.W AMM 25-11-01-822-095-001 REV.147 REPLACED SEAT TRACK ASSY.
FOUND MAIN DECK CARGO HANDLING BASE OF LOCK ASSY WORN TOTAL : 1EA AT BS 1000 LBL 11.50. REPLACED LOCK IAW AMM 25-58-01-004-001 AND AMM 25-58-01-404-005 REV.147.
FAULT - FOUND MAIN DECK CARGO HANDLING CL ROLLOVER RESTRAINT ASSY CRACK AT STA 654+22 BL0 . IAW AMM 25-58-03-004-001 AND AMM 25-58-03-404-004 REV.147 REPLACED CL ROLLOVER RESTRAINT ASSY .
FOUND MAIN DECK CARGO HANDLING ROLLER HOLE OF LOCK ASSY WORN TOTAL : 1EA AT STA 654+99 RBL 55.50. REPLACED IAW AMM 25-58-01-004-001 AND AMM 25-58-01-404-005 REV.147.
FAULT - FOUND MAIN DECK CARGO HANDLING SHAFT OF ROLLER RAIL ASSY WORN TOTAL: 2EA AT STA 456 ~ STA 500 LBL 77.50, LBL 55.50. I.A.W AMM 25-57-05-004-001 AND AMM 25-57-05-404-006 REV.147 REPLACED ROLLER RAIL ASSY.
DURING PERFORM J/C : MXP-57-117-00-1-JIC, FOUND LEFT WING LOWER SKIN NEAR RIB 32, WSTA 1018.2 SKIN CRACKED. ACCOMPLISHED JOB I.A.W UPS EO-97334-REQ1 REV1 2.
CRACKED FITTING, RT WING NR 10 SPOILER SUPPORT FITTING WS 638. REPLACED IAW AMM 27-61-01-424-019, REV 147, STEP 3A, TO 3H (11) INSTALLED NR 10 SPOILER.
SDR FILED OPEN. FULL GEAR RETRACTION TOOK 8 MINS. CLIMB STOPPED AT FL190 FOR 1 MIN AND AIRSPEED LIMITED TO 250KTS UNTIL SUCH. FULL RETRACTION TOOK UNTIL PASSING 10,000 FT. GEAR EXTENSION & FLAP EXTENSION WERE.
**SUPPLEMENTAL SDR** FULL GEAR RETRACTION TOOK 8 MINS. CLIMB STOPPED AT FL190 FOR 1 MIN AND AIRSPEED LIMITED TO 250KTS UNTIL SUCH. FULL RETRACTION TOOK UNTIL PASSING 10,000 FT. GEAR EXTENSION & FLAP EXTENSION WERE ... PERFORMED PRESSURIZATION CHECK OF CENTER HYDRAULIC SYS WITH EACH ACMP. VERIFIED PRESSURE STABILIZED AT +3000 PSI WITH EACH C ELEC 1 AND C ELEC 2 IAW AMM 29-11-00-862-013. OPS CHECK GOOD, OK FOR SERVICE.
FAULT - DENT - SURFACE, NO.2 ENG, LPT ACC MANIFOLD SURFACE, AT R/H UPPER SIDE (EVALUATE) I.A.W. CF6-80C2 ENGINE MANUAL GEK92451 REV:97 ESM72-56-06 STEP 6. A. (4), MEASURE THE DENT AREA. RESULT: OD: 2.4655", DEPTH OF DENT: 0.1310", THE RADIUS OF THE DENT: 1.23", THE DEPTH OF THE DENT IN TUBE IS WITHIN LIMITATION. JOB COMPLETED AND CONDITION CHECK NORMAL. REVIEWED
DENT - SURFACE, NO.2 ENG, LPT ACC MANIFOLD SURFACE, AT R/H UPPER SIDE (EVALUATE) OK TO WORK
APU FUEL FEED TUBE DENT STA 1629, LEFT SIDE. (TUBE PN: 346T0003-11) .I.A.W AMM 28-25-05-004-036 REV 142 AND AMM 28-25-05-404-084 REV 142 REPLACED THE TUBE, AND LEAK CHECK RESULT WAS NO LEAK FOUND.
SECTION 48, APU FUEL FEED TUBE DENT STA 1629, LEFT SIDE. (TUBE PN: 346T0003-11) (REPLACE) OK TO WORK
*** SUPPLEMENTAL SDR *** FAULT - CRACK - BRACKET, NO.1 ENGINE LH AFT LOWER LPT COOLING MANIFOLD DUCT SUPPORT AT 7:30 POS (REPLACE) 1. I.A.W. AMM 75-24-03-004-050-H00 & 75-24-03-404-037-H00, REV: 141, REPLACED THE LPTACC MANIFOLD WITH SERVICEABLE PARTS. 2. COMPLETED THIS JOB & CONDITION CHECK SATISFACTORY. 3. IPC VERIFIED AND SERVICEABLE TAG NO.:072576.
**SDR FILED OPEN**FAULT - CRACK - BRACKET, NO.1 ENGINE LH AFT LOWER LPT COOLING MANIFOLD DUCT SUPPORT AT 7:30 POS (REPLACE) OK TO WORK
*** 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) ACCMPLISHED SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R).
FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. PAPER FINAL CHECK COMPLETED.
CRACK - ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60. I.A.W AMM 53-01-06-000-801 REV.141 REMOVED MAIN DECK CARGO FLOOR PANEL AND G.V.I CHECK NORMAL.
ON DEPARTURE WITH TAKEOFF THRUST SET, STRONG SMELL OF "DIRTY SOCKS" OBSERVED UNTIL CLIMB THRUST SELECTED REVERSED DMP, AFTER R/H ENGINE CHANGE REF BARCODE (T3F18E0041NKW) DUE TO FINDINGS ON TECH ALERT BARCODE T3F18E0040D5T, OPERATED R/H PACK WITH RIGHT ENGINE BLEED AS PNEUMATIC SOURCE PER AMM 21-51-00, NO SMELL NOTED, OPS CHECK GOOD, THIS CLEARS DEFERRAL, PLACARD REMOVED
*SDR FILED OPEN* ON DEPARTURE WITH TAKEOFF THRUST SET, STRONG SMELL OF "DIRTY SOCKS" OBSERVED UNTIL CLIMB THRUST SELECTED PERFORMED HIGH POWER ENGINE RUN IN REF TO AMM 71-00-00-862. ONLY ABLE TO DUPLICATE SOCK SMELL WITH RH PACK ON, COULD NOT DUPLICATE SMELL WITH LH PACK ONLY, BEGAN PERFORMING AMM REF 05-51-56-202-001 AND AMM 21-00-21-102-030. WAS NOT ABLE TO FIND LEAK/ CONTAMINATION IN RH PACK OR RH ENGINE BLEED. PROBLEM NEEDS FURTHER TROUBLESHOOTING TO FIND SOURCE. ALL WORK DONE BY ETOPS AMT. DEFERRED RH AC PACK PER MEL 21-51-1-1. DMP ACOMPLISHED. PLACARDS APPLIED.
*** SDR FILED OPEN *** DENT AND GOUGE BETWEEN STA: 456 AND STA: 434, AT AND BELOW S -26R ***AWE - SM EVAL REQ*** **LINK 22E79** C/W EO87526-REQ2 DEFERRAL REMAINS AT THIS TIME
MCD CENTER POS 9 FLOOR BOARD DAMAGED, MARKED COMPLETE INSTALLATION OF FLOOR BOARD POS 9 REF B767 AMM 53-01-01-404 AND SREO B767-5320-9693-I
INSPECTION TYPE:ETOP, RT PACK TEMP EICAS IN FLIGHT, ACCOMPLISHED QRH PROCEDURE, EICAS AND R PACK INOP LIGHT EXTINGUISHEDPERFORMED R PACK TEMP CONTROLLER BITE TEST IAW AMM 21-51-14-705-035, NO FAULT FOUND OK TO CONTINUE IN SERVICE
INSPECTION TYPE:C13CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287,RBL25.REPAIR I.A.W UPS EO B767-5310-20118-H AND 767-300F SRM 51-70-12 GENERAL,FIGURE 1,REV 82.01.
INSPECTION TYPE:N/A**DIVERSION** RUDDER RATIO LGT ON IN FLIGHT. EICAS MESSAGE: RUDDER RATIO DISPLAYEDT/S PER FIM 27-21-00-815-804. NO FAULTS NOTED . PERFORMED RUDDER RATIO CHANGER MODULE PER FIM 27-09-00-815-814. OPS CHECK GOOD NO FAULTS NOTED. NO PREV FLT/ CURRENT FLT FAULT HISTORY. RUDDER RATIO LIGHTS AND MESSAGE EXTINGUISHED
AIR TURNBACK, NO EMERG DECLARED. ALT DISAGREE EICAS MESSAGE PASSING 6000'MSL, ALT DIFFERENCE OF 320' BETWEEN CAPT & F/O INST,COMPLETED AIRSPEED UNRELIABLE PROCEDURE(W/ALTN AIR DATA SELECTED(CAPT SIDE), CAPT & F/O A/S & ALT COMPARISON FL 280 ALT SPLIT 300' A/S SPLIT 6 KTS.PERFORMED AOA SENSOR TEST BY ARINC 429 ANALYZER PER MM 34-12-03-401. FOUND OUT OF LIMIT AT LEFT VANE POSITION SET -10. TESTER SHOWS 349.233. ALL OTHER POSITION W/IN LIMIT. REPLACED LH AOA SENSOR & TEST OK PER MM 34-12-03-401.
ATB - IAS DISAGREE AND ALT DISAGREE EICAS MESSAGE DURING CLIMB A/S DIFERRENCE OF 10KTS BETWEEN CAPT & F/O A/S INDICATORS ALTITUDE DIFFERENCE OF 300' WHILE PASSING 10,000'MSL COMPLETED AIRSPEED UNRELIABLE QRH PROCEDURE SELECTED L ADC.REPLACED CAPT'S AUX PITOT TUBE AS PER AMM34-11-01-401 & LH ADC AS PER AMM34-12-01-401. PERFORMED CAPT'S PITOT LEAK TEST AS PER AMM34-11-00-730-811. ALL INDICATION WITHIN LIMITS. NO LEAK NOTED. CAPT'S PITOT LINE CHECKS NORMAL.
INSPECTION TYPE:N/AATB - IAS DISAGREE EICAS MESSAGE ON CLIMBOUT.CAPTS IAS APPROX 10KTS SLOWER THAN STBY AND F/O AIRSPEED INDICATORS.AFTER RUNNING AIRSPEED UNRELIABLE CHECKLIST CONFIRMED F/O AIRSPEED RELIABLE SELECTED RIGHT A/PT/S PER FIM34-12-00-00-815-804 AND FIM34-11-00-815-806 REPLACED CAPT PITOT STATIC PROBE PER MM34-11-01-401 AND TEST OK AND ADC TEST OK PER MM34-12-00-501 OK FOR SVC.
INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFENER (P/N : 111T2011-6) ON STA 785.9 , RBL 55REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01 , UPS EO B767-5740-58151-B , BOEING SRID : 3-4660367939 AND UPS EO B767-5710-76205-A
INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2008-11) ON STA 785.9 , LBL 33REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01 , UPS EO B767-5740-58151-B , BOEING SRID : 3-4660367939 AND UPS EO B767-5710-76205-A
ATB - LEFT ENGINE FIRE LOOP 1 STATUS MESSAGE CAME ON AT 17,000 FEET. T/S SYS PER FIM 26-11-00-815 FIG 104. FOUND LOOP 1 OF TS681 & TS682 CTR WIRE SHORTED OUT. R/R UPPER & LWR AFT ENG FIRE DET IAW AMM 26-11-02-401. OPS CK NORMAL.
RT PACK LIGHT OFF INOP R PACK OFF EICAS MSG NO ILLUMINATED WHEN RIGHT PACK IS OFF. TRANSFERRED TO DMI LOG PER 21-51-1-1 M662682 ASSIGNED. **SUPPLEMENTAL ETOPS **ACCOMPLISHED FIM 21 51 00 815 818 001 1 BLOCKS 1-7 AND 40 FOUND LOW LIMIT VALVE AT FAULT. REMOVED AND REPLACED RIGHT PACK LOW LIMIT VALVE WITH REF TO MM 21 51 11 201. TESTS GOOD EFF 21 51 11 01A 045. THIS CLOSES M662682.
INSPECTION TYPE:ETOP CARGO DET AIR STATUS MESSAGE DURING DE-ICE. CLEARED WITH STATUS MESSAGE CLEARING PROCEDURE. IAW FIM 26-16 TASK 815-828-002 REV 125.01 SYSTEM CHECKED, FOUND SYSTEM WORKS NORMAL.
INSPECTION TYPE: C11, A CRACK WAS FOUND ON THE BS 1809.5 BULKHEAD HORIZONTAL INNER ANGLE AT WL 257, RBL 28. REPAIRED THE BULKHEAD IAW SRM 53-80-08, REPAIR 10, REV 71, AND EO B767-5310-68300-A.
INSPECTION TYPE: C11, A DENT WAS FOUND ON THE LT WING INBD AFT FLAP LOWER SKIN AT IFS 113.75. REPAIRED IAW SRM 57-53-01, REPAIR 1, SRM 51-70-03, GENERAL, SRM 51-70-10, REPAIR 4, AND SRM 51-70-10, GENERAL, REV 71.
APU BITE MAINT MESSAGE DISPLAYED. MX MESSAGE CLEARED IAW FIM 49-11-00
LT FWD FUEL PUMP EICAS MESSAGE CAME ON TWICE ONE CLIMBOUT THROUGH 37000FT,THE OTHER TIME ON LEVEL OFF AT 41000FT. LT FWD FUEL PUMP PLACED ON MEL IAW 28-22-1-0-1. R & R IAW AMM 28-42-07. OPS CHECKED OK.
TOP SKIN DAMAGED DUE TO CHAFFING. REPAIRED IAW EO B767-5750-62533-B.
EXIT LIGHT LENS MISSING AT FWD UPPER CORNER OF MAIN ENTRY DOOR. REPLACED THE LENS IAW MM 52-12-00, AND 52-11- 02-10A.
INSPECTION TYPE: C10, CRACK ON THE CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, RBL 11. REPAIR IAW SRM 57-10-102R-2, REPAIR 2, REV 65 AND EO B767-5740-58151-A.
INSPECTION TYPE: C10, CRACK ON RT SIDE HORIZONTAL STABILIZER RIB ASSY OF WEB, P/N:182T5602-11 AT RS BS 202.105. REPAIR IAW SRM 55-10-09-2R-1, REPAIR 1, REV 65.
INSPECTION TYPE: C10, CRACK WAS FOUND ON THE STR 20R AT BS 1550. REPAIR IAW SRM 53-00-03-2R-5, REPAIR 5, REV 65.
INSPECTION TYPE:C10, CRACK WAS FOUND ON THE STR 20L AT BS 1504. REPAIR IAW SRM 53-00-03-2R-5, REPAIR 5, REV 65.
INSPECTION TYPE: C10, CRACK WAS FOUND ON THE STR 20R AT BS 1504. REPAIR IAW SRM 53-00-03-2R-5, REPAIR 5, REV 65.
INSPECTION TYPE: C10, CRACK WAS FOUND ON THE L/E SKIN OF RT WING NR 9 SLAT, PN:114T4104-54 AT LES 641, REPAIR IAW SRM 57-43-01-2R-2, REPAIR 2, REV 65.
INSPECTION TYPE:C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, LBL11. REPAIR IAW SRM 57-10-10-2R-2. REPAIR 2REV 65 AND EO B767-5740-58151-A.
INSPECTION TYPE: C10, CRACK ON INBD SIDE SKIN, PN:311T2450-23 AND DOUBLER, PN:311T2450-27 OF NR 2 ENGINE PYLON REPAIR IAW SRM:3-3530987764 WITH FAA APPROVED 8100-9 FROM DATED:27APR2016 AND EP B767-5430-60641-A.
MAIN CARGO DECK FLOOR PANEL, POSITION P7L HAS AREA OF DELAMINATION. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
EMERGENCY LIGHTS WILL NOT TEST. R & R EMERGENCY LIGHT BATTERY PACK AND TEST OK IAW MM 33-51-07-422-012.
PLASTIC EMERGENCY EXIT LIGHT COVER WILL NOT SECURE LT ASSY IAW MM 33-51-01.
LOAD CREW REPORTED AFT LOWER CARGO CEILING ANGLE SCUFF PLATE DAMAGED. AFT ONE REPAIRED IAW SRM 51-10-02-0G MINOR REPAIR, OK FOR SERIVCE.
ON PDC FOUND EMERGENCY LIGHTS BATTERY DEAD. R & R EMERGENCY LIGHTS BATTERY PACK REF MM 33-51-07-022-422, TEST GOOD IPC 33-51-07-32-020R.
EMERGENCY LIGHTS WHEN TESTED DO NOT STAY ON FOR ANY DURATION OF TIME. EMERGENCY LIGHT BATTERY PACK R & R IAW AMM 33-51-07-422-012, REV 113.
HOLE IN MAIN CARGO DECK FLOOR PANEL POS 2R. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.
RT ENGINE BLEED DUCT LEAK. TIGHTENED NR 2 BLEED INTERCONNECT DUCT CLAMPS IAW AMM 36-11-01-401, TASK 424-019-001, PAR F, SUB PAR 4. PERFORMED ENGINE GRAD RUN, N1=50 PERCENT, N2=88.4 PERCENT. NO DUCT LEAK INDICATION, LIGHT AND EICAS, OK FOR SERVICE.
DURING A C09 INSPECTION, FOUND A DENT ON LT SIDE FUSELAGE SKIN, BETWEEN BS 1491-1505, S29-30L. REPAIRED IAW SRM 53-00-01, REPAIR 14, REV 59.00.
DURING A C09 INSPECTION, CARGO FLOOR PANEL 251MFF FOUND DENTED BETWEEN BS 1208-1318, LBL 11- 33. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO 5320-9693-H.
DURING A C09 INSPECTION, FOUND A CRACK IN THE CARGO FLOOR PANEL 231HFF, BETWEEN BS 533-654+22, LBL 33-55. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.
DURING A C09 INSPECTION, FOUND A CRACK IN CARGO FLOOR PANEL 232SFF BETWEEN BS 687-764, RBL 77-88. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO NR 532-9693-H.
DURING A C09 INSPECTION, FOUND A CRACK IN CARGO FLOOR PANEL 222DFF, BETWEEN BS 285-412, RBL 77.5-88.5. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO 5320-9693-H.
DURING C09 INSPECTION, FOUND A SCRATCH ON CARGO FLOOR PANEL 251XFF BETWEEN LBL 54.75- 77. 50. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO NR 5320-9693-H.
DURING C09 INSPECTION, CARGO FLOOR PANEL 251AGF FOUND DENTED BETWEEN BS 1480-1598.97 LBL 33-55. FABRICATED THE REPLACEMENT FLOOR PANEL IAW EO 5320-9693-H.
DURING A C09 INSPECTION, FOUND A SCRATCH ON CARGO FLOOR PANEL 232LFF, BETWEEN BS 654+22-687, RBL 33-54.78. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO 5320-9693-H.
DURING C09 INSPECTION, FOUND A DENT CARGO BAY FLOOR PANEL 231GFF, BETWEEN BS 533-654+22, LBL 11-33. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO 5320-9693-H.
FLOOR PANEL HAS 1.5" X 1" PUNCTURE THRU FACE SHEET. REPAIRED IAW SRM 53-00-50-2R.
INTERCOSTAL DAMAGED, BETWEEN BS 1395-1417, S28-29L. FABRICATE IAW EO B767-531051605A.
DENT IN FUSELAGE SKIN, BETWEEN STA 1395 - 1417 AND S28-29L. REPAIR IAW EO B767-5330-51604-A.
INSPECTION TYPE: 8C, EMPENNAGE RT LOWER AIR GATE FAIRING FWD CUTOUT FAIRING SKIN PANELS FOUND WORN. RT LOWER AIR GATE FAIRING FWD CUTOUT PANELS REPAIRED SRM 53-80-012R3 FIG 201, REV 52.
INSPECTION TYPE: 8C, FUSELAGE RT BS 955 BULKHEAD SIDE FITTING. SLIGHT CORROSION IS FOUND AFTER FAIL-SAFE STRAP TRIMMED OFF AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE T-FITTING TO THE FAIL-SAFE STRAP AREA. CORROSION REMOVED IAW SRM 51-10-02 & REPROTECTED IAW SRM 51-20-01, REV 52, JUST AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE T-FITTING TO THE FAIL-SAFE STRAP AREA, ORIG MATL IS CLAD PLATE 2024T351- 0.400" SKIN PANEL-MACHINED, MATERIAL REMOVED IS DEPTH 0.021" X WIDTH 2" X LENGTH 2" WITHIN LIMIT IAW EO B767-5350-17922-J APPROX 'D'.
INSPECTION TYPE: 8C, FUSELAGE LT BS 955 BULKHEAD SIDE FITTING - A SLIGHTLY CORROSION IS FOUND AFTER FAIL SAFE - STRAP TRIMMED OFF AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE T-FITTING TO THE FAIL SAFE STRAP AREA. CORROSION REMOVED IAW SRM 51-10-02 & PROTECTED IAW SRM 51-20-01 REV 52 JUST AT THE INTERNAL SURFACE OF THE SKIN IN THE AREA WHERE THE T-FTG TO THE FAIL-SAFE STRAP AREA, ORIG MATL IS CLAD PLATE 2024T351-0.400" SKIN PANEL-MACHINED, MATERIAL REMOVED IS DEPTH 0.022" X WIDTH 2" X LENGTH 2" WITHIN LIMIT IAW EO B767-5350-17922-J APPX 'C'.
INSPECTION TYPE: 8C, RT WING INBD MAIN FLAP, INBD HINGE ARM FITTING FOUND CRACKED. RT WING INBD MAIN FLAP INBD HINGE ARM FITTING REPAIRED IAW SRM 57-53-02-2 REPAIR 1 FIG 201, REV 52.
INSPECTION TYPE: 8C, LEFT WING NR 3 SLAT INBD NOSE SKIN CRACKED. REPAIRED IAW SRM 57-43-01-2R2. REPAIR 2, FIG 201, REV 52. REPAIR CLASSIFIED MAJOR.
INSPECTION TYPE: 8C, EMERGENCY LIGHT DID NOT STAY ON FOR 15 MINS. EMERGENCY LIGHT BATTERY PACK REPLACED AND OPS TEST CARRIED OUT NORMAL, REF AMM 33-51-07.
INSPECTION TYPE: 8C, FUSELAGE BS 955, S22AR CRACK WAS FOUND AT RT SIDE TEE FITTING AT 9 O`CLOCK POSITION .0625" APPROX. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING AREA TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-J APPROX D, FIG 6, ORIGINAL MATERIAL IS BAC1505-100900 7075-T73511, CRACK AT 9 O`CLOCK POSITION .0625" APPROX, THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.
INSPECTION TYPE: 8C, FUSELAGE BS 955 S22AR CRACK WAS FOUND AT RT SIDE FAIL SAFE STRAP AT 9 O/C POSITION 0937" APPROX. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP IS REPAIRED IAW EO B767-5350-17922-J APPX 'D', ORIGINAL MATERIAL IS 2024T351-0750", MACHINED STRAP, CRACK AT 9 O/C POSITION .0937" APPROX, FINAL CUTOUT SIZE IS 7.75" X 2", THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.
INSPECTION TYPE: 8C, LEFT WING NR 5 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01-2R2, REPAIR 2, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR.
INSPECTION TYPE: 8C, RIGHT WING NR 8 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01-2R2, REPAIR 2, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR.
INSPECTION TYPE: 8C, LEFT WING NR 4 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01-2R2, REPAIR 2, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR.
INSPECTION TYPE: 8C, FUSELAGE BS 955, S22LA CRACK WAS FOUND AT LT SIDE TEE FITTING AT 2 O/C POSITION 3/32" APPROX FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG AREA T-FITTING. REPLACED AND INSTALLED IAW EO B767-5350-17922-J APPX 'C' FIG 6, ORIGINAL MATERIAL IS BAC1505-100900 7075-T73511, CRACK AT 2 O/C POSITION .0937" APPROX. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.
INSPECTION TYPE: 8C, FUSELAGE BS 955, S22LA CRACK WAS FOUND AT LT SIDE FAILSAFE STRAP AT 8 O`CLOCK POSITION .0937" APPROX. FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP IS REPAIRED IAW EO B767-5350-17922-J, APPROX C, ORIGINAL MATERIAL IS 2024T351-0750" MACHINED STRAP, CRACK AT 8 O`CLOCK POSITION .0937 APPROX, FINAL CUTOUT SIZE IS 7.75" X 2", THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.
INSPECTION TYPE: 8C, FX - LT BS 955 REAR SPAR BULKHEAD SIDE FITTING 1 EA FASTENER HOLE FOUND CRACK INDICATION BY ULTRASONIC METHOD FURTHER INVESTIGATION REQUIRED. FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING AT THE LOWER 3 FASTENERS ARE REMOVED AND REINSTALLED IAW EO B767-5350-17922-J APPROX 'C' FIG 6 FOR AN OPEN HOLE HFEC INSPECTION, NRC HAM502357 AND HAM502340 ARE RAISED FOR FURTHER ACTION.
INSPECTION TYPE: 8C, MAIN CARGO DECK FLOOR PANEL HAS NINE DENTS AND TWELVE PUNCTURES AT BS 412 TO 530, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.
INSPECTION TYPE: 8C, RT BS 955 REAR SPAR BULKHEAD SIDE FITTING 1 EA FASTENER HOLE FOUND CRACK INDICATION BY ULTRASONIC METHOD FURTHER INVESTIGATION REQUIRED. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING AT THE LOWER 3 FASTENERS ARE R & R IAW EO NO B767-5350-17922-J APPX 'D' FIG 6 FOR AN OPEN HOLE HFEC INSP, NRC NR HAM502332 AND HAM502324 ARE RAISED FOR FURTHER ACTION.
CAPT NR 2 SLIDING WINDOW LATCH HANDLE WILL NOT OPERATE WITHOUT DEPRESSING LATCH RELEASE BUTTON. R & R AFT STRIKER BRACKET ON CAPT NR 2 WINDOW IAW AMM 56-11-02-6. OPS CK OK.
MCD FLOOR PANEL POS 4R HAS .25" HOLE RBL 49 STA 662. REPAIRED IAW SRM 53-00-50-2R.
MCD FLOOR PANEL BS 1368 LBL 4.5 HAVE .5" REPAIRED IAW SRM 53-00-50-2R.
FLOOR PANEL POS NR 14 HAS 1.25" HOLE, RBL 49, BS 1531. REPAIRED IAW SRM 53-00-50-2R.
MAIN CARGO COMP POS 9/10 L OTBD MOST FLOOR PNL DAMAGED. FABRICATED FLOOR PANEL IAW EO B767-5320-9639.
MCD FLOOR PANEL POS NR 8L HAS .5" HOLE LBL 81 STA 1012. REPAIRED IAW SRM 53-00-50-2R.
FLOOR PANEL HAS PUNCTURE, POS 2C REPAIRED IAW SRM 53-00-50-2R.
DECK FLOOR PANEL BS 749, RBL 39.0 HAS A 1.5 DIA DENT WITH PUNCTURE IN TO CORE. DAMAGE IS 1.5" DIA. REPAIRED IAW SRM 53-00-50-2R, 4D.
DAMAGE TO FLOOR PANEL POS 11R OTBD SIDE. REPAIRED IAW SRM 53-00-50-2R.
MCD FLOOR PANEL POS 9L OTBD HAS HOLE. REPAIRED IAW SRM 53-00-50-2R.
MCD FLOOR PANEL POS 2C HAS PUNCTURES. REPAIRED IAW SRM 53-00-50-2R.
FLOOR PANEL POS 2C HAS PUNCTURES. REPAIR IAW SRM 53-00-50-2R.
POS 6R HAS FLOOR PANEL DAMAGED. REPAIRED REF EO B767-5320-9693-H.
RUDDER TRIM WOULD NOT MOVE RT WITH RUDDER TRIM KNOB. TRIM AT 1.5 LT FOR LANDING-AIR TURN BACK TO DEPARTURE T/S IAW FIM 27-21-00/101, FIG 100, FOUND RUDDER TRIM ACTUATOR WOULD NOT MOVE. R & R RUDDER TRIM ACTUATOR AND SYS OPS CHECK NORMAL IAW AMM 27-21-11-2.
INSPECTION TYPE:C, MCD STA 1114 TO 1197+22 LBL 11" TO 33" FLOOR PANEL 3 PUNCTURE AND TOGETHER WITH 7 DENT MARKS. MCD FLOOR PANEL FABRICTED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.
INSPECTION TYPE:C, RT WING 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 47.
INSPECTION TYPE:C, LT WING OTBD T/E FLAP T/E WEDGE INBD AREA LWR SURFACE CRACKED. FIBERGLASS PREPREG LAYUP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5G, FIG 14, REV 47.
INSPECTION TYPE:C, MCD STA1425 TO 1522, RBL55 TO RBL77, FLOOR PANEL FND 2 PUNCTURE HOLES AND 8 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REPLACED IAW AMM 53-01-01.
INSPECTION TYPE:C, MCD STA540 TO 654+22 LBL11 TO RBL11 FLOOR PANEL FND 6 DAMAGED AND 4 DENT MARKS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.
INSPECTION TYPE:C, MCD STA 972 TO 1112, LBL 11 TO RBL 11, FLOOR PANEL FOUND 3 PUNCTURE HOLES AND TOGETHER WITH 6 DENT MARKS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.
INSPECTION TYPE:C, STA1207 TO 1351 RBL11 TO LBL11 FLOOR PANEL FND 3 DAMAGE AND 4 DENT MARKS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.
INSPECTION TYPE:C, MCD STA 1197+22 TO 1207 LBL11 TO RBL11 FLOOR PANEL FND 5 PUNCTURE HOLES AND 5 DENTS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.
INSPECTION TYPE:C, MCD STA833 TO 930 RBL11 TO LBL11 FLOOR PANEL FND 6 DAMAGE AND TOGETHER WITH 5 DENT MARKS. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REPLACED IAW AMM 53-01-01.
INSPECTION TYPE:C, MCD STA412 TO 544 LBL 77 TO LBL 88 FLOOR PANEL FOUND 4 PUNCTURE HOLES TOGETHER WITH 6 DENT. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND REPLACED IAW AMM 53-01-01.
INSPECTION TYPE:C, LT WING OTBD FLAP T/E LWR SURFACE AT 54.5" FROM OTBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 9, REV 47.
INSPECTION TYPE:C, LT WING OTBD FLAP T/E LWR SURFACE AT 127" FROM OTBD EDGE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1) FIG 9, REV 47.
INSPECTION TYPE:C, STA412 TO 544 LBL55 TO 77 MCD FLOOR PANEL FND PUNCTURE HOLES AND 5 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B77-5320-9693-G AND REPLACED IAW AMM 53-01-01.
INSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/B OTBD NOSE SKIN AT OSS641.9 AREA SKIN REPAIRED IAW SRM 57-43-01-22R FIG 201, ORG MATL IS CLAD7075T6-0.063IN, CRK LENGTH 0.244", DAMAGED CUTOUT IS 8.875" X 7.25" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH CLAD7075T6-0.071 AS REPAIR DOUBLER AND CLAD7075T6- 0.063" AS REPAIR PLATE. REPAIR SIZE IS 10.375" X 12".
INSPECTION TYPE:C RUDDER SKIN SIDE UPPER AREA DELAMINATION. GRAPHITE FABRIC PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-04, PAR 5K, REV 47.
INSPECTION TYPE:C, FUS MEC COMPT STA 246 FLOORBEAM ATTACH STIFFENER FOUND CRACK AT LBL40". FUS MEC COMPT STA 246 FLOORBEAM ATTACH STIFFENER AT LBL 40" AREA REPAIRED IAW SRM 53-10-51-2R4, FIG 201, REV 47.
D418763 MCD FLOOR PANEL DAMAGED AT POSITION 10L MFG AND INSTALLED IAW EO B767-4320-9693-G, POS 10L.
VERTICAL STAB AREA OF DELAMINATION, LEFT SIDE, FSS 195.39. REMOVED, REPAIRED AND INSTALLED PER SRM 51-40-02-OG, AND BOEING DWG 175T0000.
FLOORBOARD ON MCD CENTER POS 9 DAMAGED. FABRICATED FLOORBOARD PER EO B767-5320-9693-F.
MCD FLOOR PANEL DAMAGED POS 9. REPAIRED PER EO B767-5320-9693-F.
INSPECTION TYPE:N/A MCD POS 9 RT OUTBOARD FLOOR PANEL INTERIM REPAIR. FABRICATED FLOOR PANEL PER EO B767-5320-9693-F.
INSPECTION TYPE:PS D399756 MCD POS 9 AND 10 RT 2ND FROM O/B PANEL INTERIM REPAIR 1 HOLE .5 INCH DEEP 1.5 X 1 INCH 2-HOLES WITH CRACKS BOX APPX 1 INCH FWD AREA POS 10 SAME FLOOR PANEL. PERMANENT REPAIR AT C CHECK. REPLACED FLOOR PANEL PER EO B767-5320-9693-F.
INSPECTION TYPE:PS D399757 MCD POS 12 RT 2ND FROM O/B FLOOR PANEL INTERIM REPAIR PERMANENT REPAIR AT C-CHECK. REPLACED FLOOR PANEL PER EO B767-5320-9693-F.
INSPECTION TYPE:N/A RT INBOARD T/E FLAP WEDGE UPPER SURFACE HAS DENT. C/W EO B767-5750-30772B AND B767 SRM 57-53-01-2R TAP CHECK GOOD. PAINTED SEALED MAJOR REPAIR COMPLETE.
INSPECTION TYPE: N/A INSTALL DOUBLER AND TRIPLER REF RCD 261 TO LWR SURFACE RT WING T/E WEDGE. C/W EO B767-5750-30772B.
INSPECTION TYPE:C M/D STA 754 RBL 11 SEAT TRACK CROWN WORN. M/D - CARGO TRACK SECTIONAL REPLACED FROM STA 709 TO STA 785 RBL 11 AND REPAIRED AS PER SRM 53-00-52-2R REPAIR 9 FIG 201.
INSPECTION TYPE:C FX- INTERNAL AREA STA 246 LBL 50 CABIN FLOORBEAM ATTACHMENT STIFFENER FOUND CRACK. CRACK LENGTH 0.75 INCH. FX- STA 246 LBL 50 CABIN FLOORBEAM ATTACHMENT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
FWD PIT DOOR AFT EDGE DAMAGE.
INSPECTION TYPE:ETOP DIVERSION - UNABLE TO MAINTAIN CABIN PRESSURIZATION. REPLACED CABIN PRESSURE SELECTOR PANEL PER AMM 21-31-01-4. AUTO TEST AND MANUAL TEST NORMAL, NO FAULTS AT PRESSURE CONTROLLERS WITH REFERENCE TO FIM 21-31-00.
INSPECTION TYPE:N/A FLOOR PANEL 3 PUNCTURES. REPAIRED PER EO B767-5320-31943-A.
INSPECTION TYPE:ETOP EICAS MSG MAIN BATTERY CHARGER DISPLAYED. BATTERY DISCHARGE LIGHT DID NOT ILLUMINATE. SWAPPED APU BATTERY CHARGER WITH MAIN BATTERY CHARGER IAW 24-31-02-4 & 24-31-05-4. MAIN BATTERY CHARGER OPS NORMAL.
INSPECTION TYPE:ETOP TAXIING INTO EWR RAMP NR 5 BRAKE ASSY INTERNALLY FAILED CAUSING LOW LEVEL HYD FLUID FIRE DUE TO CRACKED PUCK ASSEMBLY. PERFORMED HIGH ENERGY STOP/HEAT DAMAGE CONDITION INSPECTION IAW MM REF 05-51-14-2, NO FIRE DAMAGE NOTED ON ALL ADJACENT A/C STRUCTURES AND ASSEMBLIES.
INSPECTION TYPE:ETOP TSLV = 4514 - DIVERSION - POSSIBLE BIRD INGESTION THROUGH RIGHT ENGINE. THE CREW NOTICED AN UNUSUAL VIBRATION & REQUESTED TO SPEAK TO ACMX. DIVERTED TO SJO. PERFORMED FIM 71-05-00/101 AND REPLACED FAN BLADES 15-16-34 PER MM 72-00-00-6. PERFORMED ENGINE TEST 5 & 6 PER MM 71-00-00-5. ALL CHECKS NORMAL.
FOUND RT I/B AFT FLAP HAS 3.5" DENT WITH DELAMINATED. REPAIRED IAW 51-20-10-2 AND 51-70-10-2R.
R2 WINDOW HAS 4 INCH AREA OF DELAMINATED ALONG UPPER EDGE. OK PER 767 MM 56-11-00-6 PG 1 ITEM 6F.
ETOP FWD EQUIP EXHAUST FAN EICAS MSG, ELEC SMELL IN COCKPIT. FOUND CB H21 PANEL P6-4 TRIPPED. RESET CB, TRIPPED AGAIN. A/C RELEASED PER MEL 21-58-4-2-1. FAN ELECTRICALLY DISCONNECTED AND CB TAGGED. LP 532788 FUNCTION CK WAS SATIS. FOUND REMOVAL & INSTALLATION LABEL ATTACHED TO THIS LP. LABEL REMOVED. PLACARD WAS REMOVED.
MAIN CABIN DOOR INOPERABLE.
INFLIGHT SHUTDOWN DUE TO FUEL IMBALANCE RT ENGINE SHUT DOWN PER CHECKLIST RETURNED TO LOUISVILLE FUEL LEAKING INTERNALLY IN HMU AND COMING OUT BOTTOM CHANNEL A AND CHANNEL B CANNON PLUG PLATE. REMOVED HMU UP TO STEP 6 IAW M/M REF 73-21-14-4. INSTALLED HMU NR 2 PER MM 73-21-14-4. RAN ENGINE, ALL CHECKS NORMAL. NO LEAKS NOTED.
INSPECTION TYPE:N/A INBOUND LOG WRITE UP: CENTER HYDRAULIC QUANTITY DECREASED TO .31. SYSTEM DEPRESSURIZED AND LEAK CONTINUED. SPOILER ACTUATOR PANEL NR 9, FOUND SAFETY WIRE ON CAP, PT 1542661 IPC REF 27-61-02-01 WAS BROKEN AND CAP WAS LOOSE. REMOVED AND REPLACED O-RING P/N NAS1602-910 & SECURED FILTER CAP.
INSPECTION TYPE:C, EMERGENCY EXIT MARKINGS OUTSIDE OF FIRST OFFICERS R2 SLIDING WINDOW HAS PULL DECAL DETERIORATED. FAA REQUIRED. INSPECTED DECAL AND FOUND REPLACEMENT DECAL (P/N BAC27N84-0059) ALREADY INSTALLED.
AIR TURN BACK-LOSS OF HYDRUALIC QUANTITY HYD QTY READS ZERO HYD QTY LGT ILLUM, EICAS MSG DISPLAYED L HYD QTY HYDRAULIC LOW PRESS ON. FOUND BROKEN PACKING ON RT ELEV PCU LEFT SYS. REPLACED PACKING LEAK CK'D RAN LEFT ENG CYCLED FLIGHT CONTROLS ALL SYSTEM'S CK NORMAL, OKAY FOR SERVICE.