N331UP
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
132 reports on file, 2001-04-25 – 2026-08-07.
Part: FORMER — CRACKED (ZONE 600) · airframe 69,295 hrs · 23,159 cycles
CRACKED FORMER, RT WING FIXED L/E NOSE BEAM SUPPORT STRUCTURE AT STA OSS 499. REMOVE DAMAGE FORMER IAW SRM 51-40-02-0G, REV 95. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 95 AND DWG 114T2161, SH 1, REV E, & EO SREO-50900-REQ001, REV 2.
Part: FAIRING — DEBONDED (ZONE) · airframe 69,295 hrs · 23,159 cycles
DEBONDED SKIN, RT AFT WING TO BODY FAIRING EXTERNAL, PANEL 198CR. IAW SRM 52-40-02-2R-4, REF SRM 51-70-17-0G-0, & SRM 51-70-14-0G-0, REV 95. REMOVED DEBONDED MATERIAL & CLEANED. BONDED THE REPAIR PLIES WITH RESIN CURED AT 200F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. BONDED THE FOIL WITH RESIN CURED AT 200F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG IAW SRM 52-40-02-2R-4, REF SRM 51-70-17-0G-0, & SRM 51-70-14-0G-0, REV 95.
Part: COWLING — DENTED (ZONE 400) · airframe 69,295 hrs · 23,159 cycles
DENTED NR 2 ENG NOSE COWL INLET AT 7 & 5 O'CLOCK POSITIONS. CUT OUT THE DAMAGE & CLEAN, MEASURE THE CUT OUT ( (1) DIA : 1", 15.5" FROM FWD EDGE AT 7 O'CLOCK , (2) DIA : 1" , 15.3" FROM FWD EDGE AT 5 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL. BONDED THE SPACER WITH FILM ADHESIVE CURED AT 250F FOR 2 HOURS AND FILL THE CUT OUT WITH ADHESIVE CURED AT 200F FOR 1 HOUR IAW SRM 54-15-01-2R-3, REV 95. CONFIRM THAT THE ENGINE NACELLE IS ACOUSTICALLY COMPLIANT IAW SRM 54-00-00-2R-0, REV 95.
Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 69,295 hrs · 23,159 cycles
FOUND AFT CARGO FLOOR PANEL CRACKED. IAW SRM 53-00-50-2R-0 REV. 95, CUT OUT THE DAMAGE AND CLEANED. BONDED THE REPAIR PLIES WITH RESIN CURED AT 170F FOR 2 HOURS WITH A MINIMUM VACUUM OF 20 IN/HG IAW SRM 53-00-50-2R-0, REV 95.
Part: FORMER — CRACKED (ZONE 500) · airframe 69,295 hrs · 23,159 cycles
CRACKED FORMER, LT WING OTBD FXD LE NOSE SKIN SUPPORT, OSS 499.60. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G REV.95 AND DWG 114T2161 SH 1 REV. E AND EO SREO-50900-REQ001 REV2.
Part: SHAFT — CORRODED (ZONE 500 FLAP) · airframe 69,295 hrs · 23,159 cycles
FOUND LT WING OTBD FLAP NR 2 SUPPORT CRANK ARM AND INPUT SHAFT CORROSION. IAW AMM 27-51-21-024-001, REV 148, REMOVED LT WING NR 2 FLAP ACTUATOR CRANK ARM & INPUT SHAFT. IAW AMM 27-51-21-424-032, REV 148. INSTALLED LT WING NR 2 FLAP ACTUATOR CRANK ARM & INPUT SHAFT WITH NEW PARTS.
Part: SKIN — CRACKED (ZONE 200) · airframe 69,295 hrs · 23,159 cycles
MAJOR REPAIR, SKIN , DURING PERFORM T/C : EO-24301-JIC001 FOUND SKIN CRACK AT BS 1725.5 , S-7R.
Part: RING — CRACKED (ZONE 400) · airframe 69,295 hrs · 23,159 cycles
FOUND NR 1L T/R AFT CASCADE SUPPORT RING CRACK.
Part: RING — CRACKED (THRUST REVERSER) · airframe 69,295 hrs · 23,159 cycles
FOUND NR 1R T/R AFT CASCADE SUPPORT RING CRACK. COMPLETED THRUST REVERSER AFT CASCADE SUPPORT RING (ACSR) REPLACEMENT I.A.W EO-87822-REQ01R-REPL REV4.
Part: ANGLE — CRACKED (ZONE 100) · airframe 69,295 hrs · 23,159 cycles
THE BULK CARGO OTBD ANGLE AT BS 1578, RBL 80 IS CRACKED. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV.95. INSTALL NEW ANGLE IAW SRM 51-40-02-0G REV.95 AND DWG 146T5650 SH 5 REV.C.
Part: ANGLE — CRACKED (ZONE 100) · airframe 69,295 hrs · 23,159 cycles
FOUND THE FIRE DETECTION LOOP FASTENER STRIP CRACKED AT BS 1562 LBL 76 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.95. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 218T4100 SH 3 REV: B AND BOEING DWG NO: 218T4004 SH 16 REV: D.
Part: ANGLE — CRACKED (ZONE 100) · airframe 69,295 hrs · 23,159 cycles
THE BULK CARGO INBOARD ANGLE AT BS 1578, LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV.95. INSTALL NEW ANGLE IAW SRM 51-40-02-0G, REV 95 AND DWG 146T5650, SH 5, REV C.
Part: ANGLE — CRACKED (ZONE 100) · airframe 69,295 hrs · 23,159 cycles
THE BULK CARGO OUTBOARD ANGLE AT BS 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.95. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G, REV.95 AND DWG 146T5650, SH 5, REV C.
Part: FLOOR PANEL — CRACKED · airframe 69,295 hrs · 23,159 cycles
CRACKS ON THE FLOOR PANEL NO. 251XFF (P/N 146T5869-89) IN THE MAIN DECK CARGO COMPARTMENT. REMOVED THE FLOOR PANEL IAW AMM 53-01-06-000-801 REV. 148. IAW AMM 53-01-06-400-801 REV.148. INSTALLED THE FLOOR PANEL 251XFF.
Part: FORMER — CRACKED (ZONE 500) · airframe 69,295 hrs · 23,159 cycles
CRACKED FORMER , LT WING OTBD FXD LE NOSE SKIN SUPPORT, OSS 648.60. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G REV.95 AND DWG NR 114T2163 SH 1 REV. E, AND EO SREO-50900-REQ001 REV2.
Part: WEDGE — DEBONDED (NR 4 SLAT) · airframe 69,295 hrs · 23,159 cycles
DEBONDED SKIN , LT WING NR 4 SLAT TE WEDGE INBD. RII COMPLETED FOR OK TO INSTALL CHECK
Part: ANTENNA — ERODED (ZONE 100) · airframe 69,295 hrs · 23,159 cycles
FOUND V.S.T HF ANTENNA (321E) EROSION. REMOVE THE EROSION MATERIALS AND CLEAN IAW SRM 55-30-01-2R-6 REFER TO SRM 51-70-07-0G-0 REV. 95. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260ðF FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG.
Part: ANGLE — CRACKED (ZONE 100) · airframe 69,295 hrs · 23,159 cycles
THE BULK CARGO INBOARD ANGLE AT BS 1578, RBL 80 IS CRACKED. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95 AND DWG 146T5650 SH 5 REV.C.
Part: HANDLE — BROKEN (ZONE 800) · airframe 68,731 hrs · 22,934 cycles
CREW DOOR INTERIOR EMERGENCY PANEL HANDLE BROKEN REMOVED AND REPLACED EMERGENCY ASSIST HANDLE PER AMM 20-11-00. THIS CLOSES DMI 2875106.
Part: COVER — BROKEN (DOOR HANDLE) · airframe 68,330 hrs · 22,788 cycles
CREW ENTRY DOOR PLUNGER HANDLE PLASTIC COVER PLATE IS BROKEN AND WILL NOT STAY DOWN. SAFETY DOOR LATCH HANDLE COVER DOES NOT APPEAR TO BE BROKEN. COVER CLOSES AND COVERS HANDLE AS INTENDED IAW 52-12-02.
Part: COVER — BENT (ZONE 800) · airframe 68,314 hrs · 22,781 cycles
SAFETY DOOR LATCH COVER WILL NO CLOSE. FOUND BENDED FLAP ON SAFETY DOOR LATCH COVER. REWORKED AND REINSTALLED PER AMM 52-12-02/401 AT REV. 147 WITH SATIS. FUNCTION IS GIVEN. COVER OPENS AND CLOSES AS DESIGNED. OK TO CONTINUE. CONFIRMED ALL TOOLS AND PARTS REMOVED FROM AIRCRAFT.
Earlier reports · 2001–2025 · 111 reports
2025
Part: SWITCH — DAMAGED (ZONE 200) · airframe 67,339 hrs · 22,366 cycles
FOUND UNARMED? KORRY SWITCH ON EMERGENCY LIGHT PANEL DAMAGED. R & R EMERGENCY LIGHT PANEL IAW AMM 33-51-08/401. OPS CHECK GOOD.
Part: ADC — INOPERATIVE (ZONE 200) · airframe 67,221 hrs · 22,314 cycles
***AIR TURN BACK*** AIRCRAFT DISPLAYED FLAP LIM & SPD LIM AT 255 KTS AND 3000 FT ON CLIMBOUT. FLAP LEVER WAS IN UP POSITION AND INDICATED UP ON FLAP INDICATOR. ++REPLACED R ADC IAW AMM 34-12-01. OPS CHECK SATISFACTORY PER AMM 34-12-00. RESEATED R SWC PER AMM 27-32-01. OPS CHECKS SATISFACTORY PER AMM 27-32-00.
2024
Part: INDICATOR — FAULTED (FUEL QTY) · airframe 64,798 hrs · 21,383 cycles
AIR TURN BACK DUE FUEL CONFIG EICAS MESSAGE AT TOP OF CLIMB (LOGPAGE ATTACHED) ACCOMPLISHED DETAILED EXTERNAL VISUAL INSPECTION FOR LEAK OF CENTER & LEFT FUEL TANK AREA. NO LEAK FOUND. ACCOMPLISHED DETAILED INTERNAL AUXILIARY CENTER TANK INSPECTION #3 RIB SEALANT AREA NO DAMAGE FOUNDED ALSO NO LEAK FOUND. CHEKCED OVERRIDE PUMP INLET SCREEN NO FOD FOUND. BOTTOM OF THE TANK NO FOD FOUND. #2 RIB NO DAMAGE NO FOD. LEFT FUEL FEED LINE PIPE WITH BOOST PUMP ON CHECKED NO LEAK. FUEL QUANTITY INDICATING SYSTEM BITE TEST (CENTER AUXILIARY (CENTER) CIRCUIT AND LEFT AND RIGHT MAIN TANK CIRCUIT TEST) PASSED PER AMM 28-41-00/501. CLOSED THE AUXILIARY TANK ACCESS DOOR PER AMM 28-11-02/401. NO FUEL LEAK.
Part: WARNING MESSAGE — ILLUMINATED (FUEL CONFIG) · airframe 64,766 hrs · 21,371 cycles
ATB, EMERGENCY DECLARED, DUE FUEL CONFIG EICAS MESSAGE AT TOP OF CLIMB DEFERRED PER EO-90886-REQ1 1 FLT CYCLE.
Part: FLOOR PANEL — DENTED (MAIN DECK CARGO) · airframe 64,707 hrs · 21,356 cycles
FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231PFF, P/N: 143T5876-67. (REPAIR). .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. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: FLOOR PANEL — DENTED (MAIN DECK CARGO) · airframe 64,707 hrs · 21,356 cycles
FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 222AFF, P/N: 141T5856-48. (REPAIR). .I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-57-02-404-016 REV 142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: FLOOR PANEL — DENTED (MAIN DECK CARGO) · airframe 64,707 hrs · 21,356 cycles
FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 222CFF, P/N: 141T5856-50. (REPAIR). I.A.W AMM 25-57-05-404-006 AND AMM 25-58-05-404-052 AND AMM 25-58-01-404-005 REV 142 RESTORED MAIN DECK CARGO HANDLING. OB COMPLETED AND CONDITION CHECK NORMAL.
Part: FLOOR PANEL — DENTED (MAIN DECK CARGO) · airframe 64,707 hrs · 21,356 cycles
FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231CFF, P/N: 143T5876-75. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.2.
Part: FLOOR PANEL — DENTED (MAIN DECK CARGO) · airframe 64,707 hrs · 21,356 cycles
FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231RFF, P/N: 143T5876-58. (REPAIR). I.A.W AMM 25-57-05-404-006 AND AMM 25-58-03-404-004 AND AMM 25-58-01-404-005 REV 142 REINSTALLED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: FLOOR PANEL — DENTED (MAIN DECK CARGO) · airframe 64,707 hrs · 21,356 cycles
FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231FFF, P/N: 143T5876-85. I.A.W AMM 25-57-02-404-016 AND AMM 25-57-03-404-005 AND AMM 25-57-90-424-011 AND AMM 25-58-01-404-018 AND AMM 25-58-03-404-017 AND AMM 25-58-03-404-004 REV 142 REINSTALLED MAIN DECK CARGO HANDLING . JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: FLOOR PANEL — DENTED (MAIN DECK CARGO) · airframe 64,707 hrs · 21,356 cycles
FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 232GFF, P/N: 143T5876-82. (REPAIR). .I.A.W AMM 25-57-02-404-016 AND AMM 25-57-03-404-005 AND AMM 25-58-01-404-018 AND AMM 25-58-05-404-026 AND AMM 25-58-05-404-052 REV 142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL
Part: FLOOR PANEL — DENTED (MAIN DECK CARGO) · airframe 64,707 hrs · 21,356 cycles
FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231NFF, P/N: 143T5876-69. (REPAIR). I.A.W AMM 25-57-02-404-016 AND AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-58-05-404-052 REV 142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: NONE — NONE (NONE) · airframe 64,707 hrs · 21,356 cycles
FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. ACCOMPLISHED EO-82173-JIC001.
Part: HANDLE — INOPERATIVE (SERVICE DOOR) · airframe 64,716 hrs · 21,359 cycles
FOUND FORWARD LH ENTRY/ SVCE DOOR HANDLE MECHANISM PAWL DAMAGE. (REPLACE). I.A.W AMM 52-11-26-004-001 REV.142 AND AMM 52-11-26-404-003 REV.142 REPLACED PAWL. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: PAWL — DAMAGED (LT ENTRY DOOR) · airframe 64,707 hrs · 21,356 cycles
FOUND FORWARD LH ENTRY/ SVCE DOOR HANDLE MECHANISM PAWL DAMAGE. (REPLACE) OK TO WORK
Part: ANGLE — CRACKED (ZONE 100) · airframe 64,742 hrs · 21,367 cycles
ANGLE, L/H E/E COMPARTMENT, STA 246. (REPLACE) 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. INSTALLED FABRICATED PART I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO 141T5600 SH 2 REV.E. I.A.W AMM 20-11-00-910-802 REV.142 INTALLED COCKPIT PANEL. I..A.W AMM 25-11-03-400-801 REV 142 INSTALLED SUPERNUMERARY SEAT AND CONDITION AND CONDITION CHECK NORMAL. I.A.W AMM 25-16-01-404-019 REV.142 INSTALLED COCKPIT FLOOR MAT AT STA 246 LBL 49 AREA. JOB COMPLETED.
2023
Part: FLAP SYSTEM — WARNING MESSAGE (UNKNOWN) · airframe 63,433 hrs · 20,841 cycles
*** EMERGENCY DECLARED *** TRAILING EDGE FLAP DISAGREE EICAS CAME ON DURING APPROACH. RAN QRH PROCEDURE. PERFORMED FIM PROCEDURE 27-90-30-00. FSEU BITE PER 27-51 FAULT TREE 808. NO FAULTS FOUND. PERFORMED OPERATIONAL TEST OF TRAILING EDGE FLAPS PER AMM 27-51-00. OK FOR SERVICE.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 63,375 hrs · 20,821 cycles
*SDR FILED OPEN* L/H LEADING EDGE SLAT #6 DAMAGED. METAL TRIM PIECE FROM WING EMBEDDED IN SLAT CAUSING CRACK***SM EVAL REQ*** DEFERRED PER EO-88445. NO DMP REQUIRED.
Part: SLAT — CRACKED (NOT REPORTED) · airframe 63,595 hrs · 20,893 cycles
*SUPPLEMENTAL SDR* L/H LEADING EDGE SLAT #6 DAMAGED. METAL TRIM PIECE FROM WING EMBEDDED IN SLAT CAUSING CRACK***SM80/LMX6***HGR*** LEFT WING NO. 6 SLAT CLOSURE PANEL CRACK REPAIR. FOLLOW ON ACTION. COMPLETED EO-88445-REQ3
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 63,268 hrs · 20,775 cycles
*** SDR FILED OPEN *** LOWER AFT CARGO DOOR FORWARD FRAME DOOR LATCH GUARD BROKEN AND SEAL RETAINER BENT.***SM18/LMX8*** R&R LWR AFT CARGO DOOR FWD FRAME DOOR LATCH IAW SRM 51-40-1
Part: UNKNOWN — BROKEN (UNKNOWN) · airframe 63,272 hrs · 20,777 cycles
LOWER AFT CARGO DOOR FORWARD FRAME DOOR LATCH GUARD BROKEN AND SEAL RETAINER BENT.***SM18/LMX8*** R&R LWR AFT CARGO DOOR FWD FRAME DOOR LATCH IAW SRM 51-40-1
Part: SPRING — BROKEN (ARMING LEVER) · airframe 63,036 hrs · 20,670 cycles
*SUPPLEMENTAL SDR* MAIN ENTRY/DOOR ARMING LEVER HINGE COVER SPRING BROKEN. REPLACED MAIN ENTRY DOOR ARMING LEVER HINGE COVER SPRING PER MM 52-12-00-201. OPS CHK NML PER SAME THIS CLEARS AUTH # 2501580. REMOVED PLACARD
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,829 hrs · 20,597 cycles
*SDR FILED OPEN* MAIN ENTRY/DOOR ARMING LEVER HINGE COVER SPRING BROKEN.
Part: UNKNOWN — WARNING MESSAGE (WING) · airframe 62,325 hrs · 20,407 cycles
INSPECTION TYPE:N/A**EMERGENCY DECLARED**TRAILING EDGE FLAP DISAGREE EICAS MSG AND LIGHT APPEARD WHEN FLAPS 5 SELECTED LIGHT EXTINGUISHED WHEN ALT TRAILING EDGE SWITCH PUSHED ON APPROACHPERFORMED FSEU BITE PROCEDURE FOUND FLT 0 SEC 3 DATA MSG NO 27-51333 IAW FRM 27-51-00-815-809 BLOCK 73 R AND RED FSEU OPS CHK GOOD IAW AMM 27-51-01
Part: DOOR — INOPERATIVE (DOORS) · airframe 62,234 hrs · 20,365 cycles
INSPECTION TYPE:N/ACREW ENTRY DOOR: RH TRIM SEAL LOOSE - FALLSOUT FROM THE TOP.REPOSITIONED DISLODGED TRIM SEALS ON THE FWD SIDE OF THE CREW ENTRY DOOR IAW B767 MM 52-09-01.
2022
Part: FLAP — CRACKED (RH WING LE SKIN) · airframe 60,791 hrs · 19,803 cycles
INSPECTION TYPE:C12CRACK ON SEAL STRIP (P/N: 114T2800-165) OF RH WING FIXED LEADING EDGE SKIN AT OSS 514.17.REPLACE I.A.W. 767-300F SRM 51-40-02-0G REV.83.02 AND BOEING DRAWING 114T2800 SHEET 5, REV. G.
Part: FLAP — NONE (WING) · airframe 60,157 hrs · 19,529 cycles
INSPECTION TYPE:NA**EMERGENCY DECLARED** **LANDED WITHOUT INCIDENT** ON APPROACH TE FLAP DISAGREE RAN CK LIST LANDED USING ALT SYSTEMTROUBLE SHOT TE DISAGREE MSG IAW FIM27-51-00-815-810 FIG5 BLOCKS 1THRU6 ALL 3 FSPM CARFD BITE GOOD SYSTEM CHECK OK. PERFORMED OPERATION OF THE TE FLAP SYSTEM IAW AMM767 27-51-00-862-004 SYSTEM OPS CK NORMAL
2021
Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,156 hrs · 18,797 cycles
INSPECTION TYPE:N/ADURING FLIGHT EMER LIGHT SWITCH OFF OVERHEAD MOVED TO THE ON POSITION THE GUARD IS CAUSING THE SWITCH TO THE OFF POSITION (INSTEAD OF REMAINING ARMED WITH THE GUARD CLOSED)REPOSITION GUARD RING OPS TEST OK IAW B767 MM 33 50 00
Part: FSEU — MALFUNCTIONED (TE FLAPS) · airframe 57,915 hrs · 18,699 cycles
INSPECTION TYPE:N/A** EMERGENY DECLARED ** LANDED UNEVENTFULLY ** ON APPROACH UPON FLAP EXTENSION FLAP DISAGREE MSG USED ALT FLAPS TO LAND W/ FLAPS 20.PERFORMED BITE OF FSEU NO CURRENT FAULTS CHECKED FLAP HANDLE RVDT M04 M603 ANALOG INPUTS NO ERROR READINGS. REPLACED FSEU IAW MM 27-52-01-401 OPS CHECK GOOD
Part: EICAS — WARNING MESSAGE (TE FLAP CONTROL) · airframe 57,664 hrs · 18,624 cycles
INSPECTION TYPE:NA EMERG DECLARED, LANDED WITHOUT INCIDENT. NO EQUIP USED AC TAKEN OOS ON APCH TE FLAP DISAGREE MSG & LT W/FLAP HANDLE @ 5 OCCURRED WHEN MOVING FROM 1 TO 5 EICAS MSG TE FLAP DISAGREE DISPLAYED TRAILING EDGE LIGHT ON WHEN FLAPS @ POSN 5 FLAPS FAILED TO MOVE TO SELECTED POS N CHKD FLAP HANDLE RVDTS REF AMM 27 51 26. NO FAULTS FOUND. CHKD FLAP POS TRNSMTRS PER AMM 27 51 45. NO FAULTS FOUND. RPLD FLAP SLAT SHUTOFF MODULE PER AMM 27 51 48. OPER FLAPS MM 27-51-26. NO MSGS OR FAULTS. OBSVD FLAP POS TRNSMTR MEASURED VAL LIMITS ON FSEU, ALL VALUES W/IN LIMITS. OPS CHK GOOD PER MM 27-51-26 & 27-51-45.
2020
Part: SKIN — BROKEN (NR 8 SLAT) · airframe 56,654 hrs · 18,222 cycles
INSPECTION TYPE:C11, BROKEN ON RT LOWER SKIN OF NR 8 SLAT TRAILING EDGE WEDGE NEAR OSS 430. REPAIR IAW SRM 57-43-02-2R, REPAIR 1, SRM 51-70-10-2R-4, REPAIR 4, AND SRM 51-70-10-2R, REPAIR GENERAL REV.77.
Part: SKIN — BROKEN (NR 8 SLAT) · airframe 56,654 hrs · 18,222 cycles
INSPECTION TYPE:C11, BROKEN ON THE LOWER SKIN OF NR 8 SLAT TRAILING EDGE WEDGE NEAR OSS 450. REPAIR IAW SRM 57-43-02-2R, REPAIR 1, SRM 51-70-10-2R-4, REPAIR 4, AND SRM 51-70-10-2R, REPAIR GENERAL REV.77.
Part: SKIN — DENTED (BS 618) · airframe 56,654 hrs · 18,222 cycles
INSPECTION TYPE:C11, DENT WAS FOUND ON FUSELAGE SKIN, BS 618, STRINGERS 4R TO 5R. REPAIRED IAW SRM 53-00-01, REPAIR 14 , REV.77.
Part: STIFFENER — CRACKED (BS 785.) · airframe 56,654 hrs · 18,222 cycles
INSPECTION TYPE:C11, CRACK ON CENTER WING TANK STIFFENER, BS 785 , RBL 55. REPAIRED IAW SRM 57-10-10-2R-2, REPAIR 2, REV 77, AND EO B767-5740-77351-A.
2019
Part: PANEL — BROKEN (L1 DOOR) · airframe 53,953 hrs · 17,311 cycles
INSPECTION TYPE:N/A L-1 DOOR INSIDE HANDLE BUMPER BROKEN OUT OF PANEL (PANEL CRACKED AROUND BUMPER). ITEM DEFERRED REF 25-20-25-20-01. **SUPPLEMENTAL SDR** COMPLETED PERMANENT REPAIR OF DAMAGE TO L1 DOOR INTERIOR HANDLE PANEL REF AMM 25-00-00-801. IS A MINOR REPAIR. REINSTALLED IAW AMM 52-12-02. OPS CK NORMAL. THIS CLEARS M675933
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 53,307 hrs · 17,070 cycles
INSPECTION TYPE:N/A ON ARRIVAL TO ANC DESCENDING THROUGH 7000 FT RECIEVED "TE FLAP DISAGREE" EICAS MESSAGE FOLLOWED BY "TE" LIGHT DISAGREE ACTIVATED WHEN FLAPS WERE SELECTED "5" ACCOMPLISHED "TE FLAP DISAGREE CHECKLIST" WHICH LED TO "TE FLAP ASSYMETRY. EMERGENCY DECLARED. T/S IAW FIM 27-51-00-815-837 NO CURRENT FAULTS SHOW FOUND MESSAGE 27-51104 SHOP DETAILS A/S 202 OPERATED FLAPS SEVERAL TIMES OPS NORMAL AT THIS TIME.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 52,799 hrs · 16,910 cycles
INSPECTION TYPE:N/A TRAILING EDGE FLAP DISAGREE. EMERGENCY DECLARED, LANDING UNEVENTFUL.PERFORMED FLAP SLAT ELECT UNIT BITE NO FAULTS NOTED OPERATED FLAPS/SLAT SEVERAL TIMES W/NO FAULTS PER AMM FIM 27-51-00 OPS CKS OK.
2018
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 52,058 hrs · 16,619 cycles
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 72, EO B767-5740-58151-A, SRID: 3-4324271248 AND EO B767-5710-69910-A.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 52,058 hrs · 16,619 cycles
INSPECTION TYPE:C10, CRACK ON THE CENTER WING FRONT SPAR STIFFENER (P/N:111T2005-8) UPPER SIDE AT STA 785.9, RBL11. REPAIR IAW SRM 57-10-10-2R-2 REPAIR 2 REV 72, EO B767-5740-58151-A, SRID:3-4324271248 AND EO B767-5710-69910-A.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 52,058 hrs · 16,619 cycles
INSPECTION TYPE:C10, CRACK ON THE CENTER WING FRONT SPAR STIFFENER (P/N:111T2005-7) UPPER SIDE AT STA 785.9, LBL11. REPAIR IAW SRM 57-10-10-2R-2 REPAIR 2 REV 72, EO B767-5740-58151-A, SRID:3-4324271248 AND EO B767-5710-69910-A.
Part: STIFFENER — CRACKED (NLG WW) · airframe 52,058 hrs · 16,619 cycles
INSPECTION TYPE:C10, CRACK ON NOSE WHEEL WELL LT VERTICAL STIFFENER AT STA 287, RBL 25. REPAIR IAW EO B767-5310-63472-C AND DEVIATION SUPPORTED BY SRID:3-4324257003 AND EO B767-5310-69912-A.
Part: STIFFENER — CRACKED (NLG WW) · airframe 52,058 hrs · 16,619 cycles
INSPECTION TYPE:C10, CRACK ON NOSE WHEEL WELL LT VERTICAL STIFFENER AT STA 287, LBL 25. REPAIR IAW EO B767-5310-63472-C AND DEVIATION SUPPORTED BY SRID:3-4324257003 AND EO B767-5310-69912-A.
Part: SKIN — DENTED (BS 1480-1500) · airframe 52,058 hrs · 16,619 cycles
TWO DENTS WERE FOUND ON THE FUSELAGE SKIN BETWEEN BS 1480 AND 1500, STRINGERS 37L - 39L. REPAIRED IAW EO B767-5330-69911-A, AND SRID3-4320337669.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,902 hrs · 16,572 cycles
EMERGENCY LIGHTS INOPERATIVE. REMOVED & REPLACED THE POWER SUPPLY AND BATTERY IAW 33-51-07.
Part: SENSOR — INOPERATIVE (LANDING GEAR) · airframe 51,517 hrs · 16,435 cycles
ATB - AIR/GND DISAGREE STATUS MESSAGE APPEARED. COMMUNICATED THIS TO FLT CONTROL AND AMC. WE WERE DIRECTED BY ARTR TO RETURN TO SDF REF ALERT T 181888.ACCOMPLISHED MLG TILT SENSOR ADJ/TEST IAW AMM 32-09-07 AND AMM 32-09-03. FOUND PSEU TO FAIL R/H TILT SENSOR ST68 NEAR ON GROUND, REPLACED SENSOR 5268R GEAR TILT SENSOR PER AMM 32-09-13, SENSOR NOW SHOWS FAN ON GROUND. OPS CHKS AND TEST GOOD.
Part: TIRE — FAILED (NR 8 WHEEL) · airframe 51,508 hrs · 16,431 cycles
RIGHT REAR MAIN TIRE BLOWN DURING TAKEOFF. DECLARED EMERGENCY. R & R THE NR 8 MAIN WHEEL ASSEMBLY IAW MM 32-45-02-401.
2017
Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 49,252 hrs · 15,628 cycles
PUNCTURED BOTTOM SIDE RT OTBD FLAP 3.25" FROM L/E AND 31" FROM OTBD EDGE. REPAIRED IAW EO B767-5750-64523-A
2016
Part: SKIN — CORRODED (BS 1857) · airframe 47,026 hrs · 14,847 cycles
INSPECTION TYPE: C09. BULGE DAMAGE ON EXTERNAL SKIN OF FUSELAGE TAIL SEC 48, AT BS 1857. REPAIRED IAW SRID 4-3263483125 AND EO B767-5330-61376-A.
Part: FLOORBEAM — CRACKED (BS 246) · airframe 47,026 hrs · 14,847 cycles
INSPECTION TYPE: C09, CRACK ON FLOORBEAM BS 246, LBL 40. REPAIR IAW SRID 4-3261477562 AND EO B767-5310-61377-A.
Part: STRINGER — CRACKED (BS 1512) · airframe 47,026 hrs · 14,847 cycles
INSPECTION TYPE: C09, CRACK WAS FOUND ON THE STRINGER 20R AT BS 1512. REPAIR IAW SRM 53-00-03-2R-5 REPAIR 5 REV. 65.
Part: SUPPORT — CORRODED (APU BATTERY) · airframe 45,990 hrs · 14,476 cycles
APU BATTERY SUPPORT STRUCTURE CORRODED FROM PAST BATTERY FLUID SPILL. REPAIRED IAW EO B767-5320-59849-A.
2015
Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 44,703 hrs · 14,040 cycles
FLOOR PANEL POSITION NR 2 R DAMAGED, FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
Part: FLOOR PANEL — PUNCTURED (MAIN DECK) · airframe 44,242 hrs · 13,818 cycles
MAIN CARGO DECK POS 1, RT OTBD OUTER MOST FLOOR PANEL HAS A .5" DIA PUNCTURE IN UPPER FACE SHEET. FABRICATED NEW FLOOR PANEL IAW EO-B767-5320-9693-H.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 43,919 hrs · 13,693 cycles
MCD FLOOR FLOOR PANEL POS NR 1 LH HAS DAMAGE. REMOVED 2 AREAS OF DAMAGE UPPER FACESHEET SHEET AND CORE REPAIRED REF B767 SRM 53-00-50-2R.
Part: GCU — INOPERATIVE (LT GENERATOR) · airframe 43,691 hrs · 13,611 cycles
LT GENERATOR DISCONNECT SWITCH DRIVE INDICATION LIGHT INOPERATIVE. R & R GCU IAW AMM 24-22-02-4. OPS CHECKED OK.
Part: GUARD — BROKEN (LIGHT SWITCH)
EMERGENCY LIGHTS SWITCH WILL NOT GO IN THE ARMED POSITION WITH COVER CLOSED. R & R SWITCH GUARD, TEST GOOD MM 33-51-08-004.
2014
Part: SKIN — WORN (BS 1819) · airframe 42,427 hrs · 13,123 cycles
INSPECTION C08, WEAR DAMAGE WAS FOUND ON RT SIDE FUSELAGE SKIN, BS 1819 AND BETWEEN STRINGERS 17 - 22R. REPAIRED IAW SRM 53-80-01, REPAIR 3, REV.59.00.
Part: SKIN — WORN (BS 1819) · airframe 42,427 hrs · 13,123 cycles
INSPECTION C08, WEAR DAMAGE WAS FOUND ON LT SIDE FUSELAGE SKIN, BS 1819 AND BETWEEN STRINGERS 17 - 22L. REPAIRED IAW SRM 53-80-01 REPAIR 3, REV 59.00.
2013
Part: FLOOR PANEL — DAMAGED (9L)
POS 9L FLOOR PANEL DAMAGED. REPAIR FABRICATED IAW EO B767-5320-9693-H.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO)
MCD FLOOR PANEL POS 10L HAS TEMP REPAIR REF D495255. REPAIRED IAW SRM 53-00-50-2R.
2012
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 38,027 hrs · 11,432 cycles
INSPECTION TYPE: 7C, RT WING OTBD FLAP INBD LOWER PANEL INTERNAL FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R. REPAIR 4, FIG 201, SHEET 3, REV 52.
Part: STIFFENER — CRACKED (BS 246) · airframe 38,027 hrs · 11,432 cycles
INSPECTION TYPE: 7C, FUSELAGE MAIN EQUIPMENT CENTER STA 246 LBL 40 FLOORBEAM FWD FACE STIFFENER FOUND CRACKED. REPAIRED IAW SRM 53-10-51-2R4, REPAIR 4, FIG 201, REV 52, ORIG MATL IS BAC1490-2793-7075T62, CRACK LENGTH: 1.1", WITH MATERIAL CLAD 7075T6-0063" AS REPAIR STIFFENER, CLAD 7075T6-0080" AS REPAIR DOUBLER & BAC1512-3347- 7075T6511 AS REPAIR FILLERS, REPEAT INSP AT 3,000 FLIGHT CYC OR 24 MONTHS WHICH EVER OCCURS FIRST IS REQUIRED IAW SRM 53-10-51-2R4.
Part: EADI — INOPERATIVE (CAPTAIN'S)
CAPTAIN`S ADI WENT BLANK SELECTED ALTERNATE EFI NO CHANGE. AT 6,000`, DISPLAY CAME BACK ON. STARTED ARCING, SLIGHT SMOKE ODOR UNTIL BREAKER TRIPPED. DID NOT RESET BREAKER. ADI BLANKED ON ROTATION EADI REMOVED AND VISUAL CHECK BACK SIDE WIRING. NOTHING ABNORMAL NOTED AND NO SMOKE ODOR. SUB REPLACED EADI IAW MM 34-22-03-4.
Part: EADI — SHORTED (P1 PANEL)
AIR TURNBACK, SMOKE IN COCKPIT ON ARRIVAL AFTER CREW DEBRIEFING, FOUND EADI BLANK WITH ASSOCIATED CIRCUIT BREAKER POPPED. PERFORMED WIRING CHECKED FROM EADI TO SYMBOL GENERATOR, & FROM EADI TO EFIS CONTROL PANEL AND FROM EADI TO EHSI, NOT ABNORMAL, NOTED REF WDM 34-22-14. R & R EADI IAW AMM 34-22-03-4, SATISFACTORY.
Part: SKIN — DAMAGED (LT WING TE FLAP)
LEFT WING OTBD FLAP L/E SKIN DAMAGED 35.5" FROM INBD EDGE LT WING OTBD FLAP L/E SKIN DAMAGED 35.5" FROM INBD EDGE. REPAIRED REF EO B767-5750-45780-B6C.
2011
Part: ESCAPE REEL — UNWANTED DEPLOY (COCKPIT)
DURING GROUND CHECK, EMERGENCY DESCENT DEVICE CABLE DEPLOYED. REPLACED IAW EMERGENCY DESCENT DEVICE IAW MM 25-61-03-2.
Part: ESCAPE REEL — MISSING (COCKPIT)
ESCAPE REEL SEAL MISSING. REPLACED EMERGENCY ESCAPE INERTIAL DESCENT REEL IAW AMM 25-61-03-2. THIS CLOSES DMI.
Part: BATTERY — NO TEST (L1 DOOR SLIDE)
L1 DOOR SLIDE WILL NOT TEST. DEFERRED IAW MEL 25-61-2 PLACARD INSTALLED. T/S IAW FIM 25-61-00-1, VLOCK 1. REPLACED BATTERIES. OPS CHECK GOOD IAW MM 25-61-04-5. THIS CLEARS M450817.
2010
Part: FLOOR PANEL — DAMAGED (BS 930-975) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 930 TO 975 LBL 11" TO RBL 11" FLOOR PANEL, FOUND 1 DAMAGED, 1 GOUGE & 10 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.
Part: PANEL — CRACKED (RT WING) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, RT WING NR7 SLAT CLOSURE PANEL EXISTING REPAIR PATCH CRACKED. COMPOSITE REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5H, FIG 15, REV 47.
Part: FLOOR PANEL — DAMAGED (BS 685-730) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C MCD STA 685 TO 730 LBL 11" TO RBL 11" FLOOR PANEL FOUND 1 DAMAGE, 1 GOUGE & 5 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 830-933) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 830 TO 933 LBL 11" TO RBL 11" FLOOR PANEL FOUND 1 DAMAGED & 9 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 977-1114) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 977 TO 1114 LBL 11" TO RBL 11" FLOOR PANEL FOUND 1 DAMAGE AND 11 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 1331-1480) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 1331 TO 1480 LBL 77" TO LBL 89" FLOOR PANL FOUND 1 DAMAGE & 10 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 1480-1599) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 1480 TO 1599 RBL 33" TO RBL 55" FLOOR PANEL FOUND 1 DAMAGE & 8 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.
Part: SKIN — MISREPAIRED (BS 446-461) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, SURVEY SEQUENCE NR331-F1-02 THE EXISTING REPAIR PATCH DOES NOT CORRELATE TO A SRM JUST AT BS 446 TO 461 BETWEEN STR -23R AND STR 25R. FX SKIN REPAIRED IAW HX RS R53-31-36824 REV A & EO B767-5330-39678-A. JUST AT BS446-461 BTN STR 23R & 25R ORG MAT'L IS CLAD 2024T3- 0.160" MACHINED SKIN TRIMMED OUT SIZE IS 1.875" X 1.75" THIS REPAIR CLASSIFED MAJOR REPAIR WITH CLAD 2024T3-0.071" AS REPAIR DOUBLER & CLAD 2024T3-0.063" AS REPAIR FILLER, REPAIR SIZE 14.375"X11.5".
Part: FLOOR PANEL — DAMAGED (BS 540-654) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 540 TO 654+22, LBL 11" TO LBL 33" FLOOR PANEL FOUND 1 DAMAGE AND 8 DENT MARKS. FLOOR PNL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 1114-1197) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 1114 TO 1197+22 LBL 11" TO RBL 11" FLOOR PANEL FOUND 2 DAMAGES AND 10 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 685-764) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 685 TO 764, RBL 77" TO RBL 89" FLOOR PANEL FOUND 1 DAMAGE & 6 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 1087-1197) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 1087 TO 1197+22 LBL 77" TO LBL 89" FLOOR PANEL FOUND 1 DAMAGE AND 6 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 984-1087) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 984 TO 1087 LBL 77" TO LBL 89" FLOOR PANEL FOUND 1 DAMAGED & 8 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 412-550) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 412 TO 550 LBL 77" TO LBL 89" FLOOR PANEL FOUND 3 DAMAGES & 15 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 412-540) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 412 TO 540 LBL 11" TO RBL 11" FLOOR PANEL FOUND 1 DAMAGE & 9 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 540-654) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 540 TO 654+22 RBL 55" TO RBL 77" FLOOR PANEL FOUND 1 DAMAGE & 10 DENT MARKS, FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 281-412) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 281 TO 412 RBL 77" TO RBL 89" FLOOR PANEL FOUND 1 DAMAGED & 8 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 412-540) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 412 TO 540 RBL 33" TO RBL 55" FLOOR PANEL FOUND 1 DAMAGES & 7 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DAMAGED (BS 654-685) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, MCD STA 654+22 TO 685 LBL 11" TO RBL 11" FLOOR PANEL FOUND 3 DAMAGES, 1 GOUGED AND 9 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.
Part: STIFFENER — CRACKED (BS 785.9) · airframe 33,572 hrs · 9,902 cycles
INSPECTION TYPE:C, FWD CARGO COMPT WING CTR TANK FRONT SPAR UPPER VERTICAL STIFFENER FOUND CRACK AT STA 785.9, LBL 32.94 AREA. FWD CARGO BAY WING CTR TANK FRONT SPAR UPPER VERTICAL STIFFENER REPAIRED IAW R57-10-36821 & EO B767-5710-39644 JUST AT STA 785.9 LBL 32.94, CRACK LENGTH 3.5", CUTOFF LENGTH 16.5" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL BAC1518-749-2024T3511 AS REPLACEMENT SECTION. TOTAL OF REPAIR LENGTH 22.5"
Part: CONTROL PANEL — INOPERATIVE (ANTI ICE SYS)
INSPECTION TYPE:E, TOP ENG ANTI ICE SELECTED AND SWITCH WOULD NOT STAY DEPRESSED. R & R KERRY SWITCH FOR RT ENG A/I, NO HELP. R & R ANTI ICE CONTROL PANEL, ROBBED PANEL REF MM 30 11 01, 4 MFG SWPM 20 84 18.
2009
Part: CDU — BURNED (LT FMC)
PRIOR TO TAKEOFF HEARD A CRACKLING NOISE AND SMELLED ELECTRICAL BURNING RECEIVED A "L FMC FAIL IN EICAS" AND LOST THE R FMC CDU. CDU BREAKER OPENED AND WOULD NOT RESET. IDENTIFIED RT CDU HAD A BURNED ODOR REPLACED CDU PER MM 34-61-02-2. REPLACED LT FMC PER MM 34-61-01-4. OPS GOOD.
Part: SKIN — DENTED (RT WING TE FLAP)
RT INBD AFT FLAP UPPER SKIN HAS 4 DENTS CLASSIFIED AS A MAJOR REPAIR. REPAIRED IAW EO B767-5750-31777 AND SRM 51-70-10 REPAIR 2. INTERIM REPAIR D-392146.
2008
Part: SUPPORT CHANNEL — CRACKED (AFT CARGO BAY) · airframe 28,530 hrs · 8,242 cycles
INSPECTION TYPE:N/A APU DUCT SUPPORT CHANNEL CRACK FOUND AT STA 1153 TO 1175 LBL 75 AREA CRACK LENGTH .25 INCH APPROX. NEW CHANNEL REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 28,530 hrs · 8,242 cycles
INSPECTION TYPE:N/A MAIN DECK FLOORBEAM ATTACH STIFFENER AT TWO SURFACE STA 246 RBL 10 CRACK FOUND, CRACK LENGTH 1.25 INCH. MAIN DECK FLOORBEAM ATTACH STIFFENER AT FWD SURFACE STA 246 RBL 10" REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.
Part: SPAR — CRACKED (RT WING) · airframe 28,530 hrs · 8,242 cycles
INSPECTION TYPE:N/A RT WING ILES677 FRONT SPAR D-NOSE I/B FOUND CRACK AS MARKED CRACK LENGTH .75 INCH. RT WING ILES677 FRONT SPAR D-NOSE BEAM WEB REPAIRED AS PER SRM 57-41-13-2R FIG 201.
Part: BEAM — CRACKED (LT WING) · airframe 28,530 hrs · 8,242 cycles
INSPECTION TYPE:N/A LT WING L/E LES670 FWD NOSE BEAM LWR WEB CRACK CRACK LENGTH 1.25 INCH. LT WING L/E LES670 FWD NOSE BEAM WEB LOWER AREA REPAIRED AS PER SRM 57-41-13-2R FIG 201.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 28,530 hrs · 8,242 cycles
INSPECTION TYPE:N/A MAIN DECK FLOORBEAM ATTACH STIFFENER AT STA 246 LBL 26 CRACK FOUND CRACK LENGTH .75 INCH APPROX. MAIN DECK STA 246 LBL 26 FLOORBEAM ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 28,530 hrs · 8,242 cycles
INSPECTION TYPE:N/A MAIN DECK FLOORBEAM ATTACH STIFFENER AT STA 246 LBL 50 CRACK FOUND CRACK LENGTH .875 INCH. MAIN DECK STA 246 LBL 50 FLOORBEAM ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.
Part: CHANNEL — CRACKED (LT WING) · airframe 28,530 hrs · 8,242 cycles
INSPECTION TYPE:N/A LT WING LANDING GEAR W/W 551CB PANEL ATTACHMENT CHANNEL FOUND CRACK AS MARKED, CRACK LENGTH .75 INCH. LT WING LANDING GEAR W/W 551CB PANEL ATTACHMENT CHANNEL REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.
Part: HINGE FITTING — CRACKED (TE FLAP) · airframe 28,530 hrs · 8,242 cycles
INSPECTION TYPE:N/A RT WING I/B MAIN FLAP AFT I/B HINGE FITTING CRACK CRACK LENGTH .9375 INCH APPROX. RT WING I/B MAIN FLAP AFT FLAP I/B HINGE FITTING REPLACED AS PER SRM 57-53-02-2R FIG 201.
Part: HINGE FITTING — CRACKED (TE FLAP) · airframe 28,530 hrs · 8,242 cycles
INSPECTION TYPE:N/A LT WING I/B MAIN FLAP AFT FLAP I/B HINGE FITTING CRACK. CRACK LENGTH .875 INCH APPROX. LT WING I/B MAIN FLAP AFT FLAP I/B HINGE FITTING REPAIRED AS PER SRM 57-53-02-2R FIG 201.
Part: SUPPORT FITTING — CRACKED (CARGO BAY) · airframe 28,530 hrs · 8,242 cycles
INSPECTION TYPE:N/A AFT CARGO COMPT STA 1086 RBL 26 PARTITION FRAME BOTTOM SUPPORT CLIP CRACKED, CRACK LENGTH .75 INCH. SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
Part: PANEL — DAMAGED (L/E SLAT)
LEFT INBOARD L/E SLAT CLOSURE PANEL DAMAGED BEYOND LIMITS. REPAIRED NR 6 L/E SLAT CLOSURE PANEL TORN OFF AREA IAW SRM 57-43-01-2R, REPAIR 3 TABLE 1 WET LAYUP 200DF CURE METHOD. SLAT OPERATION TEST SATISFACTORY IAW AMM 27-81-00-05. ACFT OK FOR SERVICE.
2007
Part: O-RING — FAILED (NR 9 SPOILER)
C HYD QTY EICAS MSG, TURNED INTO A C HYD FLUID TOTAL LOSS. CREW TURNED CENTER PUMPS OFF TO SEE IF FLUID WOULD STILL BE LOST. THE FLUID QTY CONTINUED TO GO DOWN. THIS STARTED ABOUT 75 MILES FROM SDF. FOUND NR 9 SPOILER FILTER PLUG O-RING BLOWN, SEE IPC 27-61-02 AS PER MM 27-91-02-4. REMOVED PLUG AND REPLACED O-RING AND TIGHTENED, LEAK CHECKS OK. RAN ALL FH. CONTROLS THROUGH SEVERAL TIMES.
Part: DOWNLOCK — INOPERATIVE (MLG)
REROUTED TO DFW WITH GEAR DOWN AT 265 KT SW IND LEFT MAIN GEAR WOULD NOT RETRACT. WITH GEAR HANDLE IN UP POSITION - ALL LIGHTS OUT, WITH HANDLE IN OFF POSITION GREEN LIGHT ILLUM. RECYCLED GEAR, SAME IND AT 205 KNOTS IND. REMOVED GEAR PIN FROM LEFT MAIN GEAR FWD OVERCENTER LINK OK TO CONTINUE AIRSPEED UNDER 270 REF AMM 05-51-07-2 AND A/C AOM.
Part: UNKNOWN — MALFUNCTIONED (COOLING SYSTEM)
INSPECTION TYPE:ETOP BTB - EQUIPMENT COOLING INOP IN AUTO AND STANDBY. T/S SYSTEM PER FIM 21-56-00 FIG 116, NO DEFECTS NOTED. OK TO CONTINUE.
Part: CHARGER — INOPERATIVE (MAIN BATTERY)
INSPECTION TYPE:ETOP MAIN BATTERY CHARGER STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED MAIN BATTERY CHARGER IAW MM 24-31-02-4 AND MAIN BATTERY IAW MM 24-30-01-4 SYSTEM CHECKS GOOD IAW BOTH.
2005
Part: LINE — CRACKED (HYD SYSTEM)
ON APPROACH, LOST LEFT HYDRAULIC PRESSURE RAN HYDRAULIC SYSTEM PRESSURE CHECKLIST. ON T/S FOUND HYD PRESSURE FROM L SYST ACMP TO PRESS/CASE DRAIN MODULE, RIGID LINE WITH CRACK REMOVED AND REPLACED RIGID HYD LINE IAW GMM 5- 9-1. SYSTEM CHK CARRIED OUT IAW AMM 29-11-00-2 AND SERVICE IAW 12-12-0 1-3.
2003
Part: INDICATOR — INOPERATIVE (CAPT'S IVSI/TCAS)
INSPECTION TYPE: ETOP DIVERSION, CAPTIANS VERTICAL SPEED FLAG IN VIEW ALT AIR DATA DOESN'T CORRECT. (TCAS FLAG IN VSI ALSO IN VIEW) REPLACED CAPTAIN'S VSI PER MM 34-22-06-4 & 34-45-00-5. OPS CHK NORMAL.
2002
Part: LINKAGE — BROKEN (NR 2 ENGINE)
INSPECTION TYPE:ETOP COMPRESSOR STALL ON T/O AFTER V1. ALL ENGINE INDICATIONS NORMAL UNTIL IDLE POWER DESCENT. THEN NUMBER 2 ENGINE VIBRATION SHOWED 4.4 - 4.8 UNITS. FOUND 5TH STAGE VSV LEVER ARM BROKEN OFF AT APPROX 7 O'CLOCK POSITION. REMOVED AND REPLACED RT ENGINE PER TC 6002 AND 6001 REF ENG OPS CHECKS AND LEAK CHECK NORMAL. PN OFF CF6- 80C2B6F609, SN OFF 704924. AC DOWNGRADED TO NON-ETOPS DUE TO RT ENGINE CHANGE.
2001
Part: STRAP — CRACKED (02 BOTTLES)
DURING MAINT INSP FOUND 02 BOTTLE STRAP CRACKED. R&R 02 BOTTLE STRAP
Part: LIGHT — INOPERATIVE (COCKPIT)
INSPECTION TYPE:N/A EMER EXIT LIGHT ON FLIGHT DECK ILLUM WITH OVRHD EMER LIGHTS SW IN AR MED. WOULD NOT EXTINGUISH UNLESS SW IS MOVED TO OFF POSITION. LIGHTI NG LIGHTING WENT OUT DURING CRUISE WITH SW IN ARM. IN DESCENT MALFUN CTION RE-OCCURED REMOVED AND REPLACED EMERG EXIT LIGHT SW PANEL ASSY CHECKS GOOD