N304UP
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
CRACK - WEDGE, RT WING OUTBD FLAP INBD WEDGE. IAW SREO-70175-REQ001 REV.1 PERFORM REPAIR AS BELOW STEP. REMOVED THE CRACK MATERIALS AND CLEANED. MEASURE THE DAMAGE AREA ( L : 0.5", W : 0.2", D : 2 PLIES, 6.6" FROM AFT EDGE, AT INBD EDGE ). BOND THE REPAIR PLIES WITH RESIN CURED AT 200 F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. CONDITION CHECK IS SATISFACTORY.
FOUND FLOOR SUPPORT CORROSION IN THE AREA AFT OF BULK CARGO COMPARTMENT AT BS 1588 LBL 33. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV. 95.
THE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING. (REPLACE) INSTALL THE BUMPER IS FROM THE CREW ENTRY DOORWAY LINING. IAW PSDL 411T2240 SH DL REV.A AND DWG 411T2036 SH1 REV.H.
THE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING.
THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN.
**SUPPLEMENTAL SDR** CAPT #2 WINDOW CRANK IS BINDING WHEN TRYING TO OPEN FOUND AFT OUTBOARD GEARBOX TO BE SERVICEABLE, RE-INSTALLED SAME AFT OUTBOARD GEARBOX, FINISHED INSTALLING FORWARD GEARBOX AND INSTALLED A SERVICEABLE AFT INBOARD GEARBOX WITH A NEW RUBBER SPACER IN REF MM 56-11-04. L2 WINDOW OPS NORMAL REF MM 56-11-02-715-045. NO GRINDING NOISES OR BINDING OBSERVED. OK FOR SERVICE.
*** SDR FILED OPEN *** CAPT #2 WINDOW CRANK IS BINDING WHEN TRYING TO OPEN ADJUSTED AFT LINK ARM AND AFT UPPER ROLLER CLUSTER PER AMM 56-11-02. CRANK CLUTCH STILL BREAKING OVER WHEN CLOSING.
MAJOR REPAIR - GOUGES - SKIN, R/H WING NO.8 SLAT INNER SURFACE UPPER SIDE. (REPAIR) REPAIR I/A/W B767-300F (REV. 89) SRM 51-70-10-2R-4 AND 51-70-10-2R-0 PER SRM 57-43-02-2R-1 (DETAIL III).
FOUND ENTRY DOOR FWD SIDE DOORWAY LINING SPLINE - TRIM CRACK IAW AMM 52-12-02-004-001 REV.142 AND AMM 52-12-02-404-025 REV.142 REPLACED DOORWAY SPLINE TRIM. JOB COMPLETED AND CONDITION CHECK NORMAL.
FOUND ENTRY DOOR FWD SIDE DOORWAY LINING SPLINE - TRIM CRACK. OK TO WORK. OPEN
FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM. (REPLACE) OK TO WORK
FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM. (REPLACE) I.A.W AMM 52-12-02-404-025 REV.142 INSTALLED DOORWAY LINING. I.A.W AMM 33-51-01-402-030 REV.142 PERFORM EXIT SIGN LAMP TEST WAS NORMAL. JOB COMPLETED AND CONDITION CHECK NORMAL.
*SUPPLEMENTAL SDR* FAULT - CORROSION SKIN AFT CARGO COMPARTMENT LOWER AT STA 1175~STA 1197+11, S-36R. (REPAIR) ACCOMPLISHED REPAIR I.A.W UPS EO-98978-REQ1 REV.1 AND EGAT EI NO.F2024A53M-1771 REV.2. REVIEWED
CRACKED BRACKET MEC INTERIOR COMPARTMENT LH FWD UPPER FLIGHT DECK COCKPIT FLOOR BEAM SUPPORT AT STA 246 LBL 50. (REPLACE) 1.FABRICATE P/N(141T5146-16) PER BOEING DWG NO.141T5146 SH 15 REV."B";PL REV."F";PSDL REV."-"AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX CH 9.08 REV 7B REQUIREMENT. 2.INSTALLED FABRICATED PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO 141T5600 SH 2 REV.E.
CRACKED ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 LBL 60. (REPLACE) REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.89. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T5650 SH 5 REV.C. I.A.W AMM 25-59-01-404-019 REV 142 INSTALLED MAIN DECK CARGO DADO PANEL. I.A.W AMM 53-01-06-400-801 REV 142 INSTALLED FLOOR PANEL , PANEL NO:251CGF. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 RESTORED MAIN DECK CARGO HANDLING.
CRACKED ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.89. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T5650 SH 5 REV.C. I.A.W AMM 25-59-01-404-019 REV 142 INSTALLED MAIN DECK CARGO DADO PANEL. I.A.W AMM 53-01-06-400-801 REV 142 INSTALLED FLOOR PANEL, PANEL NO:252YFF. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 REMOVED MAIN DECK CARGO HANDLING.
CORROSION SKIN AFT CARGO COMPARTMENT LOWER AT STA 1175~STA 1197+11, S-36R. (REPAIR) PERFORM NDT INSPECTION I.A.W EGAT EI NO.F2024A53M-1771 SEQUENCE B PARTA STEP 1.2)~1.4)
FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231DFF, P/N: 143T5876-37. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. 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 25-57-03-404-005 AND AMM 25-57-05-404-006 AND AMM 25-57-08-404-020 AND AMM 25-58-01-404-018 REV 142 RESTOED MAIN DECK CARGO HANDLING.
FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231CFF, P/N: 143T5876-39. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. 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 25-57-02-404-016 AND AMM 25-57-03-404-005 AND AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-58-01-404-018 AND AMM 25-58-03-404-004 AND AMM 25-58-05-404-062 REV 142 RESTORED MAIN DECK CARGO HANDLING.
FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 252WFF, P/N: 146T5869-55. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. 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 25-57-02-404-016 AND AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV 142 RESTORED MAIN DECK CARGO HANDLING.
FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO.232AFF, P/N: 143T5876-40 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. 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 25-57-02-404-016 AND AMM 25-57-03-404-005 AND AMM 25-57-05-404-006 AND AMM 25-57-08-404-020 AND AMM 25-58-01-404-005 AND AMM 25-58-01-404-018 REV 142 RESTORED MAIN DECK CARGO HANDLING.
FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO.251SFF, P/N:146T5869-37 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-58-03-404-004 REV 142 RESTORED MAIN DECK CARGO HANDLING. I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.
FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO.231QFF, P/N:143T5876-19 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. 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 25-58-04-404-015 AND AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV 142 RESTORED MAIN DECK CARGO HANDLING.
*SUPPLEMENTAL SDR* FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) C/W EO-82173.
EMERGENCY LIGHT IN COCKPIT AND PRM CAME ON INFLIGHT. WE HAD NO EICAS MESSAGE. WE CYCLED THE EMERGENCY LIGHT OFF+ON SEVERAL TIMES. FINALLY THE LIGHTS WOULD STAY OFF IN THE ARMED POSITION. EMERGENCY OPERATION CHECK OK PER AMM33-51-00.
INSPECTION TYPE:N/A**ATB** **EMERGENCY DECLARED** C" HYDR SYS PRESS" CAUTION MESSAGER/R'D CENTER HYD PRESSURE SWITCH AND THEN CENTER HYD SYS OPS CHKD NML. HYD LEAK CHKD OK PER AMM 2911-09-401. AMM 05-51-33 PN ON: 211C223-534, OFF: 211C223-301 SN ON : J019718AC OF: T010980C IPC 29-11-63-05A ITEM 50
INSPECTION TYPE:C14CRACK DAMAGE WAS FOUND ON OUTBD SKIN PANEL ASSEMBLY(P/N:311T2450-25) OF NO.1 ENG PYLON ACCESS PANEL CUTOUT EDGE NEAR NAC STA 237.5.PERFORM REPAIR I.A.W BOEING SR 4-5607971815 AND UPS EO B767-5450-84881-A.
INSPECTION TYPE:C14CRACK DAMAGE WAS FOUND ON INBD SKIN PANEL ASSEMBLY(P/N:311T2450-25) OF NO.2 ENG PYLON ACCESS PANEL CUTOUT EDGE NEAR NAC STA237.5PERFORM REPAIR I.A.W BOEING SR 4-5608163059 AND UPS EO B767-5450-84882-A.
INSPECTION TYPE:C14CORROSION AND CRACK DAMAGE WAS FOUND ON FUSELAGE SKIN(P/N:146T3241-14) BETWEEN STA 1395-STA 1417,S-38R-S-39R.REPAIR I.A.W BOEING SRID:4-5611978450 AND UPS EO B767-5330-84909-A.
INSPECTION TYPE:N/ATHE EMERGENCY EXIT LIGHTS ACTIVATED WITH THE EMER LIGHTS SWITCH IN THE ARMED POSITION. AFTER 30 MIN, THE EMERGENCY LIGHT DE-ACTIVATEDT/S AS PER WDM 33-51-11 SHEET 1, PERFORMED OPS TEST OF EMERG LIGHT SYS SEVERAL TIMES. NO FAULTS FOUND PER AMM 33-51-00-715-001. A/C OK FOR SVC
INSPECTION TYPE:NA**ATB**NO EMERG DEC'D** A/C LANDED W-OUT INCIDENT** AIR TURN BACK: ABOVE 10,000' FEET ACCELERATING GREATER THAN 290 KTS A CONTINUOUS AIRFRAME BUFFET/VIBRATION WAS EXPERIENCED. SEEMS TO BE SPEED RELATED. SOURCE DOES NOT APPEAR TO BE ENGINE VIBRATION HOWEVER COULD NOT DETERMINE OTHERWISE #1 CONT/S PER AMM 05-51-38-202 PARA (B) (H) FOUND # R/H PACK EXHAUST DOOR ATUATOR FROZEN IN CLOSET PORTIO REMOVE AND REPLACED R/H PACK EXHAUST DOOR ACTUATOR REF B767 AMM 21-53-104-401 B767 AIR 21-53-02-01A ITEM 325
BTB 1418Z - REASON FOR BTB WHEN TAKING THE RUNWAY FOR DEPARTURE, STRONG FUMES / ODOR ENTER THE COCKPIT, SOUCE UNKNOWN AS PER AMC AND TECH SUPPORT REQUEST, PERFORMED BOTH AIR CONDITIONING SYSTEM OPERATION WITH APU OPERATION AND BOTH ENGINE RUN PER AMM21-00-00-201. AND AMM71-00-00/501. NO SMOKE AND ODOR NOTED. PHYSICALLY CHECKED BOTH WXR TRANSCEIVER AND ANT DRIVE UNIT NO ABNORMALITIES FOUND. BOTH WXR SYSTEM
INSPECTION TYPE:N/A**EMERGENCY DECLARED** - STARTED SMELLING FUMES APPRT 10000.ODORINCREAREASED IN INTINSITY AT ABOUT 8000 NO SMELE NOTICE. DENNEL O2 , SO UNABLE TO TELL IF FUMES WERE STILL PRESENT. DECLARED EMEGENCY AND LANDED. DID NOT SAY TO DETECT FUMES ON.INSPECTED ALL CARGO AREA AND MEC NIL SMELL AND EVIDENCE OF SMOKE. PERFMD SMOKE OR FUMES IN CABIN INSP PER AMM 05-51-56-201. NIL EVIDENCE OF OIL CONTAMINATION FOUND. NRT2189 D.USUI
ENTRY DOOR LIGHT ANNUNCIATOR REMAINS ILLUMINATED. DEFERRED PER MEL 52-71-1-1. VERIFIED DOOR CLOSED AND LOCKEDFOUND DOOR CLOSED SENSOR S194 BRACKET BENT. REPLACED BRACKET REF AMM 52-71-01 VERIFIED SENSOR CLEARANCE CORRECT. ALSO FOUND EXT HANDLE CAPTURE SYS EXT LOCK WORN & BINDING. REPLACED SAME AND CHECKED ADJUST PER AMM 52-12-00 D (3) OPERATED DOOR AND TESTED IND REF 52-71-00. OPS CKS NORMAL. THIS CLEARS M736591.
INSPECTION TYPE: N/A ATB. ON TAKE OFF LEFT ENGINE SURGED N1 AND N2 IND WOULD GO BLANK PERIODICALLY. FOUND LT ENGINE COMPRESSOR INLET TEMP SENSOR AT FAULT T-25 REPLACED SAME. R & R LT ENGINE T-25, PER AMM 73-21-02-401 2.
INSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS ILLUMINATED WITH EMERGENCY SWITCH IN ARMED POSITION. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY, AS PER AMM 33-51-07-402-010. PERFORMED TEST AND NO DISCREPANCIES FOUND.
INSPECTION TYPE: C13 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 972-STA 1043, RBL 33-RBL 55, PNL NR 242 TFF. FABRICATE THE REPLACEMENT FLOOR PANEL, PER EO NR B767-5320-9693-I.
INSPECTION TYPE:ETOP#1 ENG 1ST STG HPT BORO PLUG DAMAGER/R BORO PLUG B3-1 AS REQ'D I/A/W AMM 72-00-00-206-363-H00.
CABIN CREW DOOR INTERIOR HANDLE PLEXIGLASS GUARD DAMAGED. REPLACED HINGE & INTERIOR ACCESS COVER IAW AMM 52-12-02-401. OPS CHECKED GOOD.
INSPECTION TYPE:NABLOCK TURN BACK, ON TAXI OUT, EMERGENCY LIGHTS ILLUMINATED IN THE ARMED POSITION.R/R EMERGENCY BATTERY PACK PER AMM 33-51-07-022-001, TEST SATIS A/C OK TO CONTINUE. PN ON/OFF:2013-1A, SN OFF:49046, SN ON:63927. IPC 33-51-07-32 ITEM 020R.
AFTER LANDING LEFT THRUST REVERSE DID NOT OPERATE NORMALLYY COULD NOT GET OVER INTERLOCK (AFTER ABOUT 10 SEC) LEFT WENT INTO REVERSE NORMALLY. ACCOMPLISHED TASK 78-31-00-725-005-1200 THRUST REVERSER ENGINE LEFT NORMAL OPERATION AND VISUAL CHECK NO FOUND FAULT THRUST REVERSER SATIFACTORY OPERATION.
INSPECTION TYPE:N/A CREW ENTRY DOOR AIR LEAK. BOTTOM DOOR SEAL. RESULTED IN A DIVERSION.FOUND DEBRIS ON DOOR SILL. CLEARED DOOR SILL AND PRESS PER MM 05-51-02.
LEFT ENGINE FIRE LOOP 1 STATUS MESSAGE. OPEN.
DAMAGE FOUND ON THE M/D CARGO FLOOR PANEL 231JFF, FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-I.
DAMAGE WAS FOUND ON THE M/D CARGO FLOOR PANEL 232FFF. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-I.
DAMAGE ON THE MAIN DECK CARGO FLOOR PANEL 232HFF, BS 533 - 654 + 22 , RBL 55 - RBL77. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-I.
DAMAGE FOUND ON THE M/D CARGO FLOOR PANEL 231GFF. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-I.
CORROSION FOUND ON THE MAIN DECK SEAT TRACK UPPER FLANGE AT BS 955 - 1112, RBL 33. REPAIRED IAW SRM 53-00-52-1A-1, DETEIL III, REV 72.01.
CORROSION FOUND ON THE MAIN DECK SEAT TRACK UPPER FLANGE AT BS 955 - 1112 , LBL 33. REPAIRED IAW SRM 53-00-52-1A-1, DETEIL III, REV 72.01.
CORROSION WAS FOUND ON THE SHEAR WEB OF FLIGHT COMPT FLOOR AT LBL 8, AND RBL 8, BS 188.18. REPAIR IAW SRM 53-10-51-1A-2, DETAIL III, REV 72.01.
A CRACK WAS FOUND ON THE SKIN AT BS 1661, STRINGER 13AR. REPAIR IAW SRM 53-80-01, REPAIR 7, REV 72.01.
A CRACK WAS FOUND ON THE STIFFENER, UPPER SIDE AT BS 785.9, RBL 11. REPAIR IAW SRM 57-10-10-2R-2, REPAIR 2, REV 72.01, AND EO B767-5740-58151-A.
A CRACK WAS FOUND ON THE STIFFENER, UPPER SIDE AT BS 785.9, LBL 11. REPAIR IAW SRM 57-10-10-2R-2, REPAIR 2, REV 72.01, AND EO B767-5740-58151-A.
INSPECTION TYPE:N/ADIVERSION - EICAS MSGS NORM ANTISKID DISPLAYED AMBER ANTISKID LIGHT ON. MSG & LIGHT ON CONTINUOUSLY FOR APPROX 2 HOURS THEN WENT OFF.PERFORMED FIM PROCEDURE 32-42-00-803. ANTISKID CONTROL UNIT SHOWED FAULTY #4 BRAKE TRANSDUCER. RELACED #4 BRAKE ANTISKID BRAKE TRANSDUCER IAW MM 32-42-06-004 OPS OK GOOD EFF 32-42-06-01-65J
LEFT INBD ELEVATOR HAS A PUNCTURE, 48 INCHES FROM INBD EDGE AND 11 INCHES FORWARD OF TRAILING EDGE. REPAIRED THE ELEVATOR SKIN IAW EO B767-5520-67648-A.
CREW ENTRY DOOR CLOSED SENSOR S194 BRACKET IS BROKEN. REPLACED THE SENSOR BRAKET. ADJUSTED AND INSTALLED THE SENSOR IAW MM 52-71-01-401. SENSOR CHECKED NORMAL IAW MM 52-71-00-735-072.
WHILE ON APPROACH WE GOT "FIRE/OVHT SYS" AND FAIL P-RESET EICAS AND LIGHT. WHEN TRANS POWER ON SHUTDOWN LIGHTS WENT AWAY. THE RT ENG OH LP 1 STATUS MSG WAS THE ONLY LOOP STATUS MSG ON IN FLT AND ON GND. THE RT ENG LP 1 OVHT DET SYS IS ON DEFERRAL REF M620477. OK TO CONTINUE. MAINT PERF BY ETOPS QUAL MECH. R&R OVHT LOOP AND CARD M689 ON H ALERT 179162 OPS NORMAL.
ENTRY DOOR ROPE PULLED OUT OF SLEEVE CONTAINER. REPLACED THE HOOK AND LOOP AT BOTTOM OF SLEEVE CONTAINER & REINSTALLED ROPE IAW MM 25-61-04.
FUSELAGE SKIN DAMAGED AT BS 449 BELOW STRINGER 36L REPAIRED IAW EO B767-5330-65478-A.
DAMAGE TO STRINGER 45L, BS 376. REPAIRED IAW EO B767-5310-65535-A
INSPECTION TYPE: C, DURING MAJOR MAINTENANCE VISIT, FOUND A DENT IN THE NR 1 ENGINE EXHAUST SLEEVE EXTERNAL SURFACE, DENT AT 1 O'CLOCK. EVALUATED DAMAGE IAW SRM 54-45-30-1A-1 , DETAIL VII REV.67.
INSPECTION TYPE: C, DURING MAJOR MAINTENANCE VISIT FOUND A DENT ON NR 1 ENGINE EXHAUST SLEEVE EXTERNAL SURFACE. DENT AT 1 O'CLOCK , NAC STA 321. EVALUATED DAMAGE IAW EO NO B767-7810-63019-A.
INSPECTION TYPE:C11, CRACK WAS FOUND ON THE LEADING EDGE SKIN OF LT WING NR 4 SLAT AT INBD TRACK AREA. REPAIR IAW SRM 57-43-01-2R-2 REPAIR 2 REV 67.00.
INSPECTION TYPE:C11, CRACK WAS FOUND ON THE LEADING EDGE SKIN OF LT WING NR 4 SLAT AT WS 590.2. REPAIR IAW SRM 57-43-01-2R-2 REPAIR 2 REV 67.00.
INSPECTION TYPE:C11, CRACK WAS FOUND ON THE LEADING EDGE SKIN OF LT WING NR 9 SLAT AT INBD TRACK AREA. REPAIR IAW SRM 57-43-01-2R-2 REPAIR 2 REV 67.00.
INSPECTION TYPE:C11, CRACK WAS FOUND ON THE STRINGER 20L AT STA 1552. REPAIR IAW SRM 53-00-03-2R-5 REPAIR 5 REV 67.00.
INSPECTION TYPE:C11, CRACK WAS FOUND ON THE STRINGER 20R AT STA 1552. REPAIR IAW SRM 53-00-03-2R-5 REPAIR 5 REV 67.00.
INSPECTION TYPE:C11, CRACK WAS FOUND ON THE STRINGER 20L AT STA 1502. REPAIR IAW SRM 53-00-03-2R-5 REPAIR 5 REV 67.00.
WHILE AT FL360, HAD A EICAS INDICATION C HYD QTY FOLLOWED AFTER DIVERTING TO TUL TO C HYD SYS PRESSURE COMPLETED SOTA CHECK LIST AND LANDED. R & R DIFFERENTIAL PRESSURE INDICTATOR. SERVICED HYDRAULIC IAW AMM 12-12-01-613, REPLACED INDICATOR IAW AMM 29-11-18. OPS CK & LEAK CHECKED GOOD.
PUNCTURED FLOORBOARD AT POS 9/10 MAIN DECK. FABRICATE A NEW FLOORBOARD IAW SREO B767-5320-9693
MCD FLOOR PANEL DENTED, FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-I.
EMERGENCY ESCAPE DESCENT DEVICE, SN 9725 DAMAGED, REQ 157852A, R & R EMERGENCY DESCENT INERTIAL DESCENT REEL REF AMM 25-61-03, SN OFF 9725, SN ON 9662, IPC 25-61-02-04-240M.
WHEN SECURING THE ACFT "ENTRY DOORS" LIGHT REMAINED ILLUMINATED. REPLACED FWD ENTRY DOOR CLOSED SENSOR BRACKET ASSY IAW MM 52-71-01. OPS CK NORMAL.
MAIN CARGO DECK FLOOR PANEL BS 668, RBL 63 HAS A HOLE. REPAIRED IAW SRM 53-00-50-2R, PARA 4.D.
EMERGENCY LIGHTING SYSTEM HAS THE LIGHTS ON WITH THE SWITCH IN THE ARM POSITION. R & R EMERGENCY BATTERY IAW MM 33-51-07. OPS CHECKED GOOD.
MAIN CARGO DECK FLOORBOARD 2R DAMAGED. FABRICATED NEW FLOORBOARD REF EO B767-5320-9693-H.
LT OTBD AILERON L/E SPAR UPPER SURFACE AT WS 923.34 TO 940, NINE WORN DAMAGED AREAS WERE FOUND.
EMERGENCY LIGHTS WILL NOT TEST. R & R BATTERY ASSY IAW AMM 33-51-07-022-001. OPS GOOD.
INSPECTION TYPE: C09, FOUND CORROSION ON LBL 54 SEAT TRACK AT BS 610, REPAIRED IAW SRM 53-00-52, REPAIR 9, REV 55.
INSPECTION TYPE: C09, FOUND CORROSION ON RBL 11, SEAT TRACK AT BS 530. REPAIRED IAW SRM 767-300F, SRM 53-00-52, REPAIR 9, REV 55.
INSPECTION TYPE:C09, FOUND CORROSION ON LBL 33 SEAT TRACK AT BS 621-660. REPAIRED IAW SRM 767-300F, SMR 53-00-52, REPAIR 9, REV 55.
INSPECTION TYPE: C09, FOUND CORROSION ON LBL 88.5 CARGO TRACK AT BS 507 AND SEAL PLATE AT BS 542. REPAIRED IAW EO B767-5310-49515-A.
INSPECTION TYPE: C09, FOUND CORROSION ON SEAT TRACK PLATE AT BS 654+11. REPAIRED IAW EO B767-5340-49497-A.
CORROSION ON SHEAR WEB OF SEC 41, AT BS 411, LBL 59-66. REPAIRED IAW EO NR B767-5310-49478-A.
FOUND CORROSION ON SHEAR WEB OF SEC 41, AT BS 287-368 , LBL 35-45. REPAIRED IAW EO B767-5310-49474-A.
FOUND CORROSION ON SHEAR WEB OF SEC 41, AT BS 287- 368. REPAIRED IAW EO B767-5310-49474-A
INSPECTION TYPE: C09, FOUND CORROSION ON RBL 77.5 SEAT TRACK AT BS 366-390. REPAIRED IAW EO B767-5310-49500-A.
INSPECTION TYPE: C09, FOUND CORROSION RBL 88.5 SEAT TRACK AT BS 385. REPAIRED IAW EO B767-5310-49510-A.
INSPECTION TYPE: C09, FOUND CORROSION ON RBL 74.57 SEAT TRACK AT BS 287. REPAIRED IAW EO B767-5310-49499-A.
FOUND CORROSION ON SHEAR WEB OF SEC 41, AT BS 372, LBL 81. REPAIRED IAW EO B767-5310-49477-A.
FOUND CORROSION ON SHEAR WEB OF SEC 41, AT BS 372, LBL 81. REPAIRED PER EO B767-5310-49477-A.
INSPECTION TYPE: C09, DENTS FOUND IN M/D CARGO INTERIOR FLOOR PANEL BETWEEN BS 752 AND 763, NEAR LBL 87. REPAIRED IAW EO B767-5320-9693-H.
INSPECTION TYPE: C09, MAIN DECK CARGO INTERIOR FLOOR PANEL DENTED BETWEEN BS 632 & 654+22, LBL 44-54. REPAIRED IAW EO NR B767-5320-9693-H.
RT WING NR 11 SLAT DAMAGED. REPAIRED IAW EO B757-5750-48966-A.
MAIN CARGO DECK FLOOR PANEL 14L, SECOND PANEL FROM OTBD SIDE HAS A GOUGE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H AND DWG 146T5869.
MAIN CARGO DECK FLOOR PANEL POS NR 12L HAS HOLE IN OTBD PANEL, PN 146T5869-39. FABRICATED NEW PANEL IAW EO B767-5320-9693-H AND DWG 146T5869.
MAIN CARGO DECK FLOOR PANEL AT POS 7R FWD HAS HOLE IN OTBD PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693H.
MAIN CARGO DECK POS 7L FWD FLOOR PANEL HAS A HOLE, THIRD PANEL FROM OTBD. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693H.
MAIN CARGO DECK FLOOR PANEL, POS 7R MID HAS A HOLE. FABRICATE NEW FLOOR PANEL IAW EO B767-5320-9693-H.
MAIN CARGO DECK, FLOOR PANEL AT POS 8R AFT HAS HOLE IN OTBD PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693H.
FLOOR PANEL AT POS 6R FWD HAS DENT WITH CRUSHED CORE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693H.
MAIN CARGO DECK FLOOR PANEL POS 11L HAS HOLE. COMPLIED WITH EO B767-5320-9693-H.
MAIN CARGO DECK FLOORBOARD POS 5R DENTED WITH DAMAGED CORE. FABRICATED NEW FLOORBOARD IAW EP B767-5320-9693-H.
MAIN CARGO DECK POS 5R CENTER FLOOR PANEL DENTED WITH CRUSHED CORE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693H.
MAIN CARGO DECK POS 9R AFT, HOLE IN OTBD FLOOR PANEL, COMPLIED WITH EO B767-5320-9693-H.
MAIN CARGO DECK POS 10R OTBD FLOOR PANEL GOUGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693H.
MAIN CARGO DECK POS 11R OTBD FLOOR PANEL HAS 2 INCH GOUGE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693H.
MAIN CARGO DECK FLOOR PANEL POS 10R MID OTBD HAS HOLE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693H.
FLOOR PANEL FROM OTBD HAS GOUGED. COMPLIED WITH EO B767-5320-9693, FABRICATED NEW FLOOR PANEL.
MAIN CARGO FLOOR PANEL HAS TWO PLACES OF DAMAGE ON POS 4 CTR PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693H.
MAIN CARGO DECK FLOOR PANEL POS 4R FWD APPROX 2 INCH GOUGE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
MAIN CARGO FLOOR PANEL DENTED AND PUNCTURED LBL 44, STA 647. REPAIRED REF SRM 53-00-50-2R.
NR 4 FLOOR PANEL RT MID POS HAS 1" HOLE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
MAIN CARGO FLOOR PANEL POS 4R FWD HAS 1 INCH HOLE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
MAIN CARGO DECK POS 2L FWD HOLE IN FLOOR PANEL, OTBD PANEL 4"X1" DAMAGED HONEYCOMB. REPAIRED IAW SRM 53-00-50-2R 4C.
FLOOR PANEL HAS DAMAGE AT DEF D473437 AND D473438 POS 1 ON MAIN CARGO DECK. FABRICATED FLOOR PANEL REF EO B767-5320-9693-H.
MAIN CARGO DECK POS 2L AFT HOLE IN FLOOR PANEL. REPAIRED IAW SRM 53-00-50-2R, PARA 4B.
MAIN CARGO DECK POS 2L MID 2 HOLES IN FLOOR PANEL WITHIN 2" OF EA OTHER. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
MAIN CARGO DECK POS 2L MID HOLE IN FLOOR PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
MAIN CARGO DECK FLOOR DAMAGED, POS 2L. REPAIRED IAW SRM 53-00-50.
MAIN CARGO DECK FLOOR DAMAGE, POS 1 RT. REPAIRED IAW SRM 53-00-50.
MAIN CARGO DECK FLOOR PANEL DAMAGED, POS 1. REPAIRED IAW SRM 53-00-50.
MAIN CARGO DECK FLOOR PANEL DAMAGED, POS 14 CTR, REPAIRED IAW SRM 53-00-50.
MAIN CARGO DECK FLOOR DAMAGED POS 1 LT. REPAIRED IAW SRM 53-00-50.
MAIN CARGO DECK FLOOR PANEL POS 9L DAMAGED. REPAIRED IAW SRM 53-00-50.
MAIN CARGO DECK FLOOR PANEL DAMAGED POS 6L. REPAIRED IAW SRM 53-00-50.
MAIN CARGO DECK FLOOR PANEL DAMAGED POS 5R. REPAIRED IAW SRM 53-00-50.
MAIN CARGO DECK FLOOR PANEL DAMAGED POS 10L. REPAIRED IAW SRM 53-00-50.
MAIN CARGO DECK FLOOR PANEL DAMAGED POS 12 RT. REPAIRED IAW SRM 53-00-50.
MAIN CARGO DECK FLOOR PANEL DAMAGED BS 834-930, LBL 5- 8. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
MAIN DECK FLOOR PANEL 8/9M LT DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
MAIN DECK FLOOR PANEL 9L DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
MAIN DECK FLOOR PANEL 10/11 LT DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
MAIN CARGO DECK FLOOR PANEL 4L GOUGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
INSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED AT MID AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG 5, REV 49.
INSPECTION TYPE:C, FX BS 955 RT SIDE TEE FITTING SHORT EDGE MARGIN FOUND AT HORIZ FLANGE AFT INBD AREA. FX BS 955, RT SIDE TEE FITTING SHORT EDGE MARGIN CONDITION IS STRUCTURALLY ACCEPTABLE AS A PERMANENT REPAIR. A NEW TEE FITTING REPLACE IAW EO B767-5350-17922-H, APPENDIX D, REF NRC FGN 502537 FOR DETAIL & FASTENER INSTALLED IAW HX RS R53-00-36918, REV A & EO B767-5310-41206-A.
INSPECTION TYPE:C, RT WING - NR 10 SLAT INBD NOSE INTERNAL SUPPORT RIB FOUND CRACKED AT THE FASTENER HOLE, CRACK LENGTH 0.063" APPROX. RIB AT OSS 723.9 AREA CRACK HOLE REPAIRED IAW HX RS R57-40-36912, REV A & EO B767-5750-41194-A SKIN CUT AT SAME LOCATION & REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 49, REF NRC FGN501497. THIS CLASSIFIED AS MAJOR REPAIR, RIB ORG MAT;L 7075-T7351, CRACK LENGTH 0.063" FINAL CUTOUT DIA IS 0.325" REPAIR SIZE IS 0.625" X 0.625".
INSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED AT INBD AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 49.
INSPECTION TYPE:C, RT WING- NR10 SLAT OTBD NOSE INTERNAL SUPPORT RIB FOUND CRACKED AT THE FASTENER HOLE, CRACK LENGTH 0.006" APPROX. RIB AT OSS792.94 AREA CRACK HOLE REPAIRED IAW HX RS R57-40-36912, REV A & EO B767-5750-41194-A SKIN CUT AT SAME LOCATION & REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 49, REF NRC FGN501513. THIS CLASSIFIED AS MAJOR REPAIR, RIB ORG MAT'L 7075T7351, CRACK LENGTH 0.060", FINAL CUTOUT DIA IS 0.309" REPAIR SIZE IS 0.625" X 0.625".
INSPECTION TYPE:C, RT WING L/E OSS 648.595, NR 9 SLAT OTBD ACTUATOR OTBD SUPPORT RIB FWD FLANGE LWR AREA FOUND CRACK. RT WING L/E OSS648.595 NR 9 SLAT OTBD ACTUATOR OTBD SUPT RIB FLANGE REPAIRED IAW HX RS R57-00-36911, REV A & EO B767-5710-41209-A, ORG MAT'L IS 7075T7351 CRACK LENGTH 0.75" FINAL CUTOUT SIZE 1.11"X 0.7". THIS REPAIR CLASSIFY AS MAJOR REPAIR WITH MAT'L 7075T7351 THK 1" PLATE TO 0.071" AS REPAIR FTG MAT'L 7075T6-0063" AS REPAIR FILLER, SIZE IS 6" X 3.5".
INSPECTION TYPE:C, LT WING INBD AILERON INBD SUPPORT RIB OTBD FLANGE FOUND CRACKED. LT WING INBD AILERON INBD SUPT RIB OTBD FLANGE REPAIRED IAW HX RS NR R-57-00-36909 REV A AND EO B767-5740-41154-A, ORIGINAL MATERIAL IS 7075T73 FORGING, CRK LENGTH IS 0.45", CUTOUT SIZE IS 1.7"X0.8", THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH & 10133-2001-7075T6511 AS REPAIR CLIP, REPAIR SIZE IS 1.46" X 2".
INSPECTION TYPE:C, BULK CARGO COMPT STA 1581, RT INBD CABIN LWR SPLICE ANGLE FOUND CRACKED. BULK CARGO COMPT STA 1581 RT INBD CABIN LWR SPLICE ANGLE REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 49.
INSPECTION TYPE:C, FLOOR PANEL FOUND 7EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 930 TO STA 975, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.
INSPECTION TYPE:C, FX BS 955 RT FAIL SAFE STRAP FOUND CRACK AT 5 O/C POSITION AND CORROSION FROM 6 TO 10 O/C POSITION. FUSELAGE STA 955 RT SIDE REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP REPAIRED IAW EO NO B767-5350-17922-H APPENDIX D.
INSPECTION TYPE:C, FX BS 955 RT T-FITTING FOUND CORROSION FROM 6 TO 10 O/C POSITION. T-FITTING REPLACED & INSTALLED IAW SRM 51-10-02, REV 49 & EO B767-5350-17922-H APPENDIX 'D' ORG MAT'L BAC1505-100900-7075T73511 CORROSION JUST AROUND FASTENER HOLE. A NEW FITTING REPLACEMENT MUST BE INSTALLED IAW EO B767-5350-17922-H, APPENDIX D.
INSPECTION TYPE:C, FLOOR PANEL FOUND 7EA PUNCTURES AND 3EA DENT MARKS AT STA 1540 TO STA 1598, LBL 55 TO LBL 88. FLOOR PANEL FABRICATE IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.
INSPECTION TYPE:C, FLOOR PANEL FOUND 7EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 1351 TO STA 1480, LBL 11 TO RBL 11. FLOOR PANEL FABRICATE IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.
INSPECTION TYPE:C, FLOOR PANEL FOUND 11EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 985 TO STA 1090, LB 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.
INSPECTION TYPE:C, FLOOR PANEL FOUND 8EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 873 TO STA 933 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.
INSPECTION TYPE:C, FLOOR PANEL FOUND 5EA PUNCTURES AND CRACK AT MIDDLE TOGETHER WITH DENT RUNNING THROUGH AT STA 933 TO STA 985, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.
INSPECTION TYPE:C, FLOOR PANEL FOUND BROKEN AT STA1041 TO STA1114, LBL33 TO LBL55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.
MCD FLOOR PANEL FOUND 9EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 975 TO STA 1114, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.
INSP TYPE:C RT WING - NR10 SLAT INBD NOSE SKIN AT RIVET HOLE FOUND CRACKED. SKIN REPAIR IAW SRM 57-43-01-2R2, FIG 201, REV 49 AT OSS 723.9 ORG MAT'L 7075T6-0063" CRACKED LENGTH 0.503" DAMAGE CUTOUT 8.875"X 7.25" THIS CLASSIFIED AS MAJOR REPAIR WITH MAT'L 7075T6-0071" AS REPAIR DOUBLER & 7075T6-0063" AS REPAIR PLATE, REPAIR SIZE 12"X10.25", THIS REPAIR IS ACCOMPLISHED IN ORDER TO REPAIR INTERNAL SUPPORT RIB.
INSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN AT RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/E OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, REV 49 AT OSS 641-9, ORG MAT'L 7075T6-0063" CRACK LENGTH 0.554" DAMAGE CUTOUT 8.875"X 7.375" THIS CLASSIFIED AS MAJOR REPAIR WITH MAT'L 7075T6-0071" AS REPAIR DOUBLER AND 7075T6-0063" AS REPAIR PLATE REPAIR SIZE IS 12"X10.5".
INSPECTION TYPE:C, LT BS 955 REAR SPAR BULKHEAD FITTING AREA WAS FOUND CRACKED ON 5 O/C POSITION AT FAIL SAFE STRAP APPROX .2500" IN LENGTH. FUSELAGE STA 955 LT SIDE REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-H, APPENDIX C.
INSPECTION TYPE:C, LT BS 955 REAR SPAR BULKHEAD FITTING AREA WAS FOUND CRACKED ON 4 O/C AND 5 O/C POSITION APPROX I/8" IN LENGTH AND FOUND CORROSION AROUND HOLE AT TEE FITTING. TEE FITTING REPLACED & INSTALLED IAW SRM 51-10-02, REV 49 & EO B767-5350-17922-H APPENDIX 'C' ORG MAT'L BAC1505-100900-7075T73511 CRACK LENGTH .1250" AT 4 O/C & 5 O/C POSITION CORROSION JUST AROUND FASTENER HOLE. A NEW FITTING REPLACEMENT MUST BE INSTALLED IAW EO B767-5350-17922-H, APPENDIX 'C'.
INSP TYPE:C RT WING - NR 10 SLAT OTBD NOSE SKIN AT RIVET HOLE FOUND CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 49 AT OSS 792.5 ORG MAT'L 7075T6-0063" CRACK LENGTH 0.154" DAMAGE CUTOUT 8.875" X 7.125" THIS CLASSIFIED AS MAJOR REPAIR WITH 7075T6-0071" AS REPAIR DOUBLER AND 7075T6-0063" AS REPAIR PLATE, REPAIR SIZE 12" X 10.25", THIS REPAIR IS ACCOMPLISHED IN ORDER TO REPAIR INTERNAL SUPPORT RIB.
INSPECTION TYPE:C, RT WING NR9 SLAT OTBD NOSE SKIN AT RIVET HOLE FOUND CRACKED. RT WING NR9 SLAT L/E OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 49 AT OSS641-9, ORG MAT'L 7075T6-0063" CRACK LENGTH 0.5955" DAMAGE CUTOUT IS 8.875" X 7.375". THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MAT'L 7075T6-0071" AS REPAIR DOUBLER AND 7075T6-0063" AS REPAIR PLATE REPAIR SIZE IS 12"X10.25".
INSP TYPE:C, FWD CARGO COMPT -WING CTR TANK FRONT SPAR UPPER VERTICAL STIFFENER CRACKED AT RBL32-94 & BS 785-9. STIFFENER REPAIR IAW HX RS R57-10-36906 REV A & EO B767-5710-41205-A ORG MAT'L BAC1518-749-2024T3511 CRK LENGTH 2.25" CUTOFF LENGTH 16.5" CLASSIFIED AS MAJ REPAIR WITH MAT'L BAC1518-749-2024T3511 AS REPLACE SECT 2024T351-0250 & 2024T3-0100 AS REPAIR STRAP, 7075T651 BARE 0250 AS REPLACEMENT CLEVIS PLATE, TOTAL OF REPAIR LENGTH IS 23 3/4".
INSPECTION TYPE:C, LT BS 955 REAR SPAR BULKHEAD FITTING AREA 1EA HOLE FOUND CRACK INDICATION BY ULTRASONIC METHOD. LT BS 955, REAR SPAR BULKHEAD FITTING AREA FASTENER REMOVED AND REINSTALLED IAW EO B767-5350-17922-H, APPENDIX C, FIG 6 FOR FURTHER CONFIRMATION BY NDT INSP.
INSPECTION TYPE:C, RT BS 955 REAR SPAR BULKHEAD FITTING AREA 1EA HOLE FOUND CRACK INDICATION BY ULTRASONIC METHOD. RT BS 955 REAR SPAR BULKHEAD FITTING AREA FASTENER REMOVED AND REINSTALLED IAW EO B767-5350-17922, APPENDIX D, FIG 6 FOR FURTHER CONFIRMATION BY NDT INSP.
FLOOR PANEL DAMAGED, POS 13 LT, FABRICATED NEW PANEL.
FLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-G.
PREVIOUS REPAIR FAILED ON MCD CNTR FLOORBOARD POS 9/10. REQUIRES NEW REPAIR PANEL. REPAIR IS A MAJOR REPAIR TRANSFERRED TO NRC 355064. SEE LOG PAGE 450344 FOR REMOVAL ITEM NR1.
CTR FLOORBOARD PANEL AT POS 10/11 HAS 3 HOLES ALONG WITH SEVERAL OTHER HOLES ON DEFERRAL REF D413492, D426407. REMOVED PANEL IAW AMM 53-01-05-4. REF L/P 450341/3 FOR PANEL INSTALLATION. THIS IS AS MAJOR REPAIR TRANSFERRED TO NRC 355067. ALL WORK COMPLETED ON NRC 355067. 2 DI NRS WERE ASSIGNED AND ARE ADDRESSED SEPARATELLY ON LP 450343.
2ND FROM AFT PANEL AT POSITION 5 CTR IN MCD HAS DENT RUNNING APPROX 2 FT LONG AT AFT EDGE GOING FWD AND THROUGH 2 PREVIOUS REPAIRS. (MARKED) REMOVED PANEL IAW AMM 53-01-05-4. SEE LP 450338/1 REF D413473 AND REF L/P 450342/1 FOR REMOVAL AND REINSTALL. ITEM IS A MAJOR REPAIR TRANSFERRED TO NRC 355066. FABRICATION COMPLETED ON NRC 355066.
AFT PANEL AT POSITION 5 CTR HAS A DENT, FULL LENGTH OF THE PANEL AND THROUGH A PREVIOUS REPAIR. MARKED. REMOVED FLOOR PANEL 14315876-58 IAW AMM 53-01-05-4. REFERENCE L/P 450341 ITEM 2 FOR PNL INSTALL. ITEM IS A MAJOR REPAIR TRANSFERRED TO NRC 355068. COMPLETED ALL WORK ON NRC 355068.
FLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-G.
FLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-G.
FLOOR PANEL DAMGED, REPAIRED IAW EO B767-5320-9693-G.
FLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-G.
FLOOR PANEL AT POS 9L HAS SMALL PUNCTURE. REPAIRED IAW SRM 53-00-50-2R.
FLOOR PANEL .5" HOLE ON UPPER SKIN AT POS 14 AT LBL85 THIS IS A MAJOR REPAIR. REPAIR IAW SRM 53-00-50-2R, PAR 4.
REF WAN 1628320 AND DMI D427308 NR 2 ENG INBD THRUST REVERSER BLOCKER DOOR NR 3 AND NR 4 WORN TEFLON WEAR STRIPS. REPLACED TEFLON WEAR STRIPS ON INBD T/R BLOCKER DOORS IAW MM 78-31-14- 8. CHECKED SATIS. THIS CLOSES DMI.
REF WAN 1628319 AND DMI D427307 NR2 ENG OTBD THRUST REVERSER BLOCKER DOORS NR 2 AND NR 3 HAVE WORN TEFLON WEAR STRIPS. REPLACED TEFLON WEAR STRIPS ON OTBD T/R BLOCKER DOORS NR 2 AND NR3 IAW MM 78-31-14-8. CHECKED SATIS. THIS CLOSES DMI.
SEAT TRACK DAMAGED STA 1415, RBL 77.5. REPAIRED IAW EO B767-5310-37995-A.
INSPECTION TYPE:N/A RT O/B GROUND SPOILER LWR SURFACE REPAIR. REPAIRED PER EO B767-5750-32318-B.
INSPECTION TYPE:N/A RT WING - I/B AFT FLAP, TRAILING EDGE WEDGE UPPER SKIN, EXISTING REPAIR DOUBLER FOUND DISBOND, REF SURVEY SEQ 304-W4-02. SRM 51-70-10 REPAIR 4 FIG 202 REV 43.
INSPECTION TYPE:7C FX - STA 1353-1366 STR - 14R FOUND A DRILLED HOLE AT THE RADIUS. FX - STA 1353-1366 STR - 14R REPAIRED AS PER SRM 53-00-03-2R1 FIG 201, SUBSEQUENCE INSPECTION REQUIRED AS PER SRM 53-00-03-2R1, FIG 201, SHEET 10 TABLE V. THIS IS CLASSIFIED AS MAJOR REPAIR WITH MATERIAL BAC1498-203-7075T62, REPAIR SIZE 13 INCH LENGTH.
INSPECTION TYPE:7C M/DECK STA 676 STR R5-R6 FRAME WEB FOUND CRACK. M/DECK STA 676 STR R5-R6 FRAME WEB REPAIRED AS PER SRM 53-00-07-2R1 FIG 201.
INSPECTION TYPE:C LT WING - I/B MAIN FLAP LOWER ACCESS PNL, FOUND DISBOND. SRM 51-70-10 REPAIR 4 FIG 203 REV 43.
INSPECTION TYPE:C M/DECK - STA 796, WL 196, LBL 33 FUEL TANK FWD UPPER CHORD FOUND CRACK 2.25 INCHES. FUEL TANK FRONT SPAR STIFFENER REPAIRED AS PER HX RS R57-11-36259 JUST AT STA 786, LBL 33, BETWEEN WL 173 AND 196. THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 2024T351-4000INX6000IN AND 2024T351-0250IN, REPAIR SIZE IS 23 INCH LENGTH X 3.5 INCH WIDTH REF UPS EO B767-5710-32138-A.
INSPECTION TYPE:7C MCD - STA 760 LBL 5 FLOOR PANEL FOUND DENT MARK. FLOOR PANEL REPAIR AS PER SRM 53-00-50-2R.
INSPECTION TYPE:C RT WING - L/E LES 732 FIXED L/E SUPPORT UPPER AFT SUPPORT BRACKET FOUND CRACKED (1.2 INCH). RT WING - L/E LES 732 FIXED L/E SUPPORT UPPER AFT SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:C RT WING- L/E LES 548 L/E SUPPORT UPPER FWD FRONT SPAR SUPPORT BRACKET FOUND CRACKED (1 INCH LENGTH). RT WING - L/E LES 548 L/E SUPPORT UPPER FWD FRONT SPAR SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:C LT WING - I/B AFT FLAP T/E WEDGE UPPER SKIN EXISTING REPAIR DOUBLER FOUND DISBOND, REF SURVEY SEQ 304-W3-08. SRM 51-70-10 REPAIR 4 FIG 202 REV 43.
INSPECTION TYPE:7C FX - MEC COMPT STA 246 RBL 10 MAIN DECK FLOORBEAM ATT CLIP FOUND CRACK. FX - MEC COMPT STA 246 RBL 10 MAIN DECK FLOORBEAM ATT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:C RT WING - O/B FLAP LOWER FWD ACCESS PNL DOUBLER DISBOND FOUND, REF SURVEY SEQ 304-W4-05. SRM REV 43, 51-70-10, REPAIR 4 FIG 201.
INSPECTION TYPE:C LT WING - I/B AFT FLAP T/E WEDGE UPPER SKIN EXISTING REPAIR DOUBLER FOUND DISBOND, REF SURVEY SEQ 304-W3-09. SRM 51-70-10 REPAIR 4 FIG 201 REV 43.
INSPECTION TYPE:C LT WING - I/B AFT FLAP T/E WEDGE UPPER SKIN EXISTING REPAIR DOUBLER FOUND TOO CLOSE AND DISBOND, REF SURVEY SEQ 304-W3-06 TO 07. SRM 51-70-10 REPAIR 4 FIG 201 REV 43.
INSPECTION TYPE:C LT WING - I/B AFT FLAP T/E WEDGE UPPER SKIN, EXISTING REPAIR DOUBLER FOUND DISBOND REF SURVEY SEQ 304-W3-04. SRM 51-70-10, REPAIR 4 FIG 202 REV 43.
INSPECTION TYPE:7C MCD - POSITION 7, FLOOR PANEL FOUND HOLE 1 X .25 INCH APPROX. FLOOR PANEL REPAIR AS PER SRM 53-00-50-2R.
INSPECTION TYPE:C RT WING MAIN FLAP SUPPORT HINGE FITTING FOUND CRACK. RT WING MAIN FLAP SUPPORT HINGE FITTING REPAIRED PER SRM 57-53-02-2R1 FIG 201.
INSPECTION TYPE:C LT WING O/B FLAP T/E WEDGE LOWER SKIN EXISTING REPAIR FOUND DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A (1).
INSPECTION TYPE:C FX MEC STA 246 LBL 25 MAIN DECK FLOOR SUPPORT CLIP FOUND CRACK (1 INCH LENGTH). FX MEC STA 246 LBL 25 MAIN DECK FLOOR SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:C FX - BS 365 TO 393 BETWEEN STR 32R AND 33R EXISTING REPAIR DOUBLER FOUND BLIND FASTENERS INSTALLED REFER TO SURVEY SEQUENCE 304-F1-01. FX - BS 365 TO 393 BETWEEN STR 32R AND 33R SKIN REPAIRED AS PER SRM 53-00-01-2R1 FIG 201, SUBSEQUENT INSPECTION IS REQUIRED AS PER SRM 53-00-01-2R1 FIG 201 SHEET 9 TABLE V REF UPS MPI P20274.
INSPECTION TYPE:C FX - BS 654 TO 654+22 BETWEEN STR 25L AND 26L EXISTING REPAIR CAN'T DETERMINE THE REPAIR CONFIGURATION AS PER SRM REFER TO SURVEY SEQ 304-F1-03. FX - BS 654 TO 654+22 BETWEEN STR 25L AND 26L SKIN REPAIRED AS PER HX RS R53-30-36256. THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 2024T3-0100IN AND 2024T3-0125IN, REPAIR SIZE IS 14 X 14.5 INCHES, REF UPS EO B767-5330-32137-A.
INSPECTION TYPE:C FX MEC STA 246 LBL 50 MAIN DECK FLOOR SUPPORT CLIP FOUND CRACK (1 INCH LENGTH). FX MEC STA 246 LBL 50 MAIN DECK FLOOR SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:7C MCD - POSITION 2R, FLOOR PANEL FOUND HOLED. FLOOR PANEL REPAIR AS PER SRM 53-00-50-2R.
INSPECTION TYPE:7C MCD - POSITION 5, FLOOR PANEL FOUND DAMAGE. FLOOR PANEL REPAIR AS PER SRM 53-00-50-2R.
INSPECTION TYPE:7C MCD - POSITION 2L, CENTER FLOOR BOARD HAS 1 INCH HOLE. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R.
INSPECTION TYPE:C AFT CARGO COMPT - STA 1087 RBL 25 BELOW FLOOR CLIP FOUND CRACK (CRACK .8750 INCH LENGTH). AFT CARGO COMPT - STA 1087 RBL 25 BELOW FLOOR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:C AFT CARGO COMPT - STA 1087 LBL 25 BELOW FLOOR CLIP FOUND CRACK. (.8750 INCH LENGTH). AFT CARGO COMPT - STA 1087 LBL 25 BELOW FLOOR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
INSPECTION TYPE:7C MCD - POSITION 6, LEFT AND LEFT OF CENTER FLOOR PANEL FOUND HOLE. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R.
INSPECTION TYPE:7C DMI D390721, MCD POSITION 5C HAS A .5 INCH HOLE IN THE CENTER (STA 700 RBL 5) FLOOR PANEL. REPAIRED AS PER SRM 53-00-50-2R.
INSPECTION TYPE:N/A RT O/B FLAP LWR SKIN DELAMINATION D368856. REPAIRED IAW SRM 51-70-10-2R.
INSPECTION TYPE:N/A LOSS OF CENTER HYD QTY & CENTER HYD PRESSURE. CREW DECLARED EMERGENCY. NOSE WHEEL STEERING WAS AVAILABLE AND TAXIIED TO GATE UNASSISTED. VERIFIED HYD LEAK AT NR 9 SPOILER ACT HOUSING CAP. FOUND O-RING UNDER CAP FLAT AND BROKEN, REF IPC 27-61-02 FIG 51. REPLACED O-RING. LEAK CHECK OK OF SPOILER. SERVICED CENTER HYD SYSTEM TO FULL. ON ARRIVAL A/C HYD WAS AT 20 PERCENT.
INSPECTION TYPE:N/A BTB - HYDRAULIC FLUID LEAK AND SMALL FIRE FROM BROKEN NR 8 BRAKE ASSY. REPLACED NR 8 BRAKE ASSY PER AMM 32-41-08-4. REMOVED BRAKE IS COMPLETELY BROKEN. NEW BRAKE OPERATION CHECKS GOOD. NR 8 MAIN WHEEL AXLE CONDITION IS GOOD.
INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT SWITCH GUARD IS CRACKED IN THE CENTER. REMOVED AND REPLACED SWITCH GUARD IAW AMM 33-51-08-4.
INSPECTION TYPE:ETOP PILOT REPORTED IDLE DISAGREE & LT ENG W/NOT RESPOND TO THROTTLE INPUT DURING TURBULENCE. TAT=32,220 TAC=10,447 TEC=8138 TET=27155 TSR=14222. *SUPPLEMENTAL ETOPS* REPLACED LEFT ENGINE ECU IAW 73-21-15-4. SYSTEM OPS CHECK NORMAL. OK TO CONTINUE.
4TH INERTIAL REEL FROM FWD INOP. REMOVED AND REPLACED INERTIAL REEL IAW MM 25-61-03-2. GROUND OPS CHECKED GOOD.
INSPECTION TYPE: N/A LT WING OB T/E FLAP DELAMINATED. A/C FERRIED TO HEAVY MX FACILITY FOR REPAIR. RMVD LW OB FLAP IAW 27-51-20-4. RMVD LW OB FLAP OB TE DEFLECTION CNTRL CARRIAGE FR DMGD FLAP & INSTLLD RPLCMNT FLAP IAW MM 27-51-24-4. RMVD LW OB FLAP IB/OB AFT FAIRING SCTN FR DMGD FLAP & INSTLLD RPLCMNT FLAP IAW 27-51-16-4. OK TO INSTLL RPLCMNT FLAP. INSTLLD RPLCMNT FLAP IAW MM 27-51-20-4. FUNC TESTED GOOD PER MM 27-51-20-4.
EMERGENCY LIGHTS GO OUT AFTER A FEW SECONDS WHEN SELECTED TO ON. REPLACED BATTERY, OPS GOOD.
EMERGENCY LIGHTS GO OUT AFTER A FEW SECONDS WHEN SELECTED TO ON. REPLACED BATTERY, OPS GOOD.
LOUD THUMP HEARD AT 27,000 FT ALT. UPON ARRIVAL FOUND LT AIR CON BAY DOOR MISSING WITH SURROUNDING DAMAGE, LEFT ECS BAY DOOR (193NL) MISSING & DAMAGED THE AIRCRAFT UPON ITS DEPARTURE. FOLLOWING ITEMS ARE OPENED AGAINST THE DOOR & DAMAGE. ACCOMPLISHED EO B767-5100-18952.
LT WING L/E CRACK IN FIBERGLASS SKIN ON SLAT CLOSURE PANEL. FOUND S MALL DENT WITH CRACKS LOWER LEADING EDGE OF LEFT WING NEAR FUSELAGE. TRIMED DAMAGE REA OUT PER SRM 51 70 AND EO B767 5750 15568-B (AS REF FOR GAP).
INSPECTION TYPE: C4, WHILE WORKING BS 246 FLOORBEAM INSPECTION IAW S/B767-53-0093 FOUND STIFFENER CRACKED AT BS 246. LBL40, WL 200. REMOVED CRACKED PART. REPAIRED BY FABRICATION AND INSTALLATION OF NE W PART PER S/B 767-53-0093, GOODRICH ER 032003 AND FAA 8110-3 FORM S IGNED 14APRIL2003
INSPECTION TYPE:N/A, PILOT REPORT - FLAPS WILL NOT RETRACT PAST 20 DEGREES. *S/D* PERFORMED FIM 27-51-00 FIG 114B. PERFORMED BITE ON FSEU AND FSPM''S, NO PROBLEMS FOUND. PERFORMED OPERATIONAL CHECK OF FLAPS SEVERAL TIMES, NO PROBLEMS FOUND. OK TO CONTINUE IN SERVICE.
INSPECTION TYPE-N/A, LOUD AIR LEAK FOUND AT ENTRY DOOR. REMOVED DEBRIS FROM SILL/SEAL AREA, OK FOR CONTINUED OPS.
LANDED 6R. BRAKING ACTION FAIR TO POOR. AFTER SLOWING TO TAXI SPEED, CAME OUT OF REVERSE. RT REVERSER DID NOT STOW. ADVANCED THROTTLES TO MAINTAIN SPEED. LOST DIRECTIONAL CONTROL, STAYED ON RUNWAY, NO DAMAGE. IT WAS NECESSARY TO BE TOWED DUE TO SLICK SURFACES. RESET REVERSER RELAY MODULE. RAN RT ENG, DEPLOYED REVERSER SEVERAL TIMES. OPS CHECK NORMAL.
FORWARD ENTRY DOOR ESCAPE ROPE TANGLED, WILL NOT DEPLOY. ROPE REINSTALLED BY BOEING DURING EO B767-3350-8522 UNDER BOEING 337 FORM FOR SB 767-33-0065 EMERGENCY LIGHT RELOCATION.
INSPECTION, REJECTED TAKEOFF DUE TO GEN OFF LIGHT ILLUMINATED AND ACCOMPANIED BY GEN DRIVE LIGHT ILLUMINATED AS WELL. CHECKED AND SERVICED IDG, RAN ENGINE AND CHECKS NORMAL.