N324UP
Registered owner: UNITED PARCEL SERVICE CO, KY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED PARCEL SERVICE CO. (IPXA) | Operator | on 2025-01-09 | Operator named in NTSB report |
Accident & incident history
Operated by UNITED PARCEL SERVICE CO (per NTSB report)
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.
153 reports on file, 1999-06-05 – 2025-08-19.
Part: STRUCTURE — DELAMINATED (ZONE 300) · airframe 67,716 hrs · 22,896 cycles
DELAMINATE- COMPOSITE, VERICAL STABILIZER AUXILIARY SPA AFT FSS 18.037 AREA. (RAPAIR) REQUEST UPS ENGINEERING DETERMINE MAJOR OR MINOR REPAIR.
Part: ANGLE — CRACKED (ZONE 200) · airframe 67,754 hrs · 22,910 cycles
FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G, REV 93. INSTALL NEW ANGLE IAW SRM 51-40-02-0G, REV 93 AND DWG 146T5650 SH 5, REV C.
Part: ANGLE — CRACKED (ZONE 200) · airframe 67,754 hrs · 22,910 cycles
FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. REMOVED FLOOR PANEL 252YFF I.A.W AMM 53-01-06-000-801 REV. 145, G.V.I AND CONDITION CHECK NORMAL. REMOVED FLOOR PANEL SEALANT I.A.W AMM 53-01-06-000-801 REV. 145, COMPLETED AND CONDITION CHECK NORMAL. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV.93 INSTALL NEW ANGLE IAW SRM 51-40-02-0G, REV 93 AND DWG 146T5650 SH 5, REV C.
Part: HINGE — DEFORMED (ARMING LEVER) · airframe 67,716 hrs · 22,896 cycles
FOUND THE ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY WITH DEFORM DAMAGE.
Part: BUMPER — MISSING (ZONE 800) · airframe 67,716 hrs · 22,896 cycles
FOUND CREW ENTRY DOORWAY LINING BUMPER WITH MISSING.
Part: ANGLE — CRACKED (ZONE 100) · airframe 67,716 hrs · 22,896 cycles
FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE) PAPER CHECK OK.
Part: ANGLE — CRACKED (ZONE 100) · airframe 67,716 hrs · 22,896 cycles
FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE) PAPER CHECK OK.
Part: BUMPER — MISSING (ZONE 800) · airframe 67,716 hrs · 22,896 cycles
FOUND CREW ENTRY DOORWAY LINING BUMPER WITH MISSING. INSTALLED THE BUMPER IAW DWG 411T2036, SHEET 1, REV H & PSDL 411T2240, SHEET DL, REV A.
Part: HINGE — DAMAGED (ARMING LEVER) · airframe 67,754 hrs · 22,910 cycles
FOUND THE ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY WITH DEFORM DAMAGE. REPLACED HINGE ASSY. I.A.W AMM 20-11-00-910-802 REV.146. INSTALLED PLACARD I.A.W AMM 20-10-13-964-001 REV.146. INSTALLED DOORWAY LINING OF THE ENTRY DOOR. I.A.W AMM 52-12-02-404-025 REV.146.
Part: ANGLE — CRACKED (ZONE 100) · airframe 67,716 hrs · 22,896 cycles
FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE) ATTACHMENT ARE UPLOADED.
Part: ANGLE — CRACKED (ZONE 200) · airframe 67,754 hrs · 22,910 cycles
FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. REMOVED FLOOR PANEL NO. 251CGF IAW AMM 53-01-06-000-801 REV. 145, GVI AND CONDITION CHECK NORMAL. REMOVED FLOOR PANEL SEALANT IAW AMM 53-01-06-000-801 REV. 145, COMPLETED AND CONDITION CHECK NORMAL. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV.93 INSTALL NEW ANGLE IAW SRM 51-40-02-0G REV.93 AND DWG 146T5650 SH 5, REV C INSTALLED DADO PANEL IAW AMM 25-59-01-404-019 REV. 145. INSTALLED FLOOR PANEL 251CGF IAW AMM 53-01-06-400-801, REV 145.
Part: PAWL — WORN (ZONE 800) · airframe 67,716 hrs · 22,896 cycles
THE PAWL BEHIND THE CREW ENTRY DOOR HANDLE HAS WEAR DAMAGE OK TO WORK
Part: PAWL — DAMAGED (ZONE 800) · airframe 67,754 hrs · 22,910 cycles
THE PAWL BEHIND THE CREW ENTRY DOOR HANDLE HAS WEAR DAMAGE. REMOVED THE PAWL IAW AMM 52-11-26-004-001, REV 145. INSTALLED A NEW PAWL IAW AMM 52-11-26-404-003, REV 145.
Part: SKIN PANEL — DAMAGED (ZONE 100) · airframe 67,097 hrs · 22,661 cycles
DAMAGE SKIN PANEL FROM STA. 1405 TO STA. 1540, STRINGER 38L TO 38R DUE TO TAIL STRIKE. ALL WORK COMPLETED ON ATTACHED BOEING WORK DOCUMENTS.
Part: FLOOR SUPPORT — DAMAGED (ZONE 200) · airframe 67,104 hrs · 22,663 cycles
REMOVED 5 FLOOR STRINGERS AT STA 1417- 1540 FOR FOM AREA RESTORED ON BOEING DOC REM 1 AND 2 ATTACHED. ENTIRE BOEING WORK PACKAGE WILL BE ATTACHED TO LINE ITEM 103 OF THIS WORK PACKAGE.
Part: SHEAR TIE — DAMAGED (ZONE 200) · airframe 67,104 hrs · 22,663 cycles
REMOVED 4 STRINGER SHEAR TIES AND 3 SHEAR CLIPS FROM FRAME AT STA 1439 AREA RESTORED ON REM 12, 13 & 14 (SEE ATTACHED). ENTIRE BOEING REPAIR PACKAGE ATTACHED TO LINE 103 OF THIS WORK PACKAGE.
Part: FAILSAFE — DAMAGED (ZONE 200) · airframe 67,104 hrs · 22,663 cycles
CUT OU DAMAGED SECTION OF TEE CHORD FROM FRAME AT STA 1461 PART REPLACED ON BOEING REPAIR DOC REM-14 (ATTACHED). ENTIRE BOEING WORK PACKAGE ATTACHED TO LINE ITEM 103. (PLEASE SEE BARCODE T3F18E005W6PJ - NLL 0782896)
Part: STIFFENER — DAMAGED · airframe 67,104 hrs · 22,663 cycles
REMOVED 4 VERTICAL L SHAPED STIFFNERS FROM FRAME AT STA 1502 AREA RESTORED ON BOEING DOC REM-10 & 11 (SEE ATTACHED). ENTIRE REPAIR DOCUMENTED ON LINE 103.
Part: SHEAR TIE — DAMAGED (ZONE 200) · airframe 67,104 hrs · 22,663 cycles
REMOVED 4 SHEAR TIES AND 3 STRINGER TIES FROM FRAME STA 1461 AREA RESTORED ON BOEING DOC REM-15 & 16 (ATTACHED). ENTIRE BOEING WORK PACKAGE WILL BE ATTACHED TO LINE ITEM 103 OF THIS WORK PACKAGE. (PLEASE SEE BARCODE T3F18E005W6PJ - NLL 0782896)
Part: STIFFENER — NOT REPORTED · airframe 67,104 hrs · 22,663 cycles
REMOVED 2 VERTICAL L SHAPED SATIN EARS FROM FRAME AT STA 1480 AREA RESTORED ON REM-12
Part: STIFFENER — DAMAGED · airframe 67,104 hrs · 22,663 cycles
REMOVE 4 DAMAGED VERTICAL L SHAPED STIFFNERS FROM FRAME AT STA 1439 4 VERTICAL STIFFENERS REPLACED ON BOEING DOCUMENT REM 8 & 13
Part: FAILSAFE — DAMAGED (ZONE 200) · airframe 67,104 hrs · 22,663 cycles
CUT OUT DAMAGED SECTION OF LOWER TEE CHORD ON FRAME AT STA 1439 PART REPLACED ON REM-13.
Part: SKIN — PILOT ERROR · airframe 67,097 hrs · 22,661 cycles
*SDR FILED OPEN* TAIL STRIKE IDENTIFIED ON WALK AROUND INSPECTION
Earlier reports · 1999–2024 · 130 reports
2024
Part: SUPPORT — BROKEN (DOOR) · airframe 64,728 hrs · 21,819 cycles
*SDR FILED OPEN* FOUND BROKEN INBOARD LEADING EDGE SUPPORT LINK DOORS (SUPPORT ASSY THAT CONNECTED TO WEB ASSY)
Part: SUPPORT — BROKEN (DOOR) · airframe 64,754 hrs · 21,828 cycles
FOUND BROKEN INBOARD LEADING EDGE SUPPORT LINK DOORS (SUPPORT ASSY THAT CONNECTED TO WEB ASSY) REMOVED THE BROKEN INBD LE SUPPORT LINK DOORS AND REPLACED NEW INBD LESUPPORT LINK DOORS PER AMM 57-41-59-401 AND OPS CHK OK
2023
Part: SKIN — CHAFED (UNKNOWN) · airframe 63,809 hrs · 21,473 cycles
*** SUPPLEMENTAL SDR *** FAULT - CHAFED - SKIN SURFACE, LOWER FUSELAGE MAIN EQUIPMENT CENTER ACCESS DOOR EXTERNAL. (AGING A/C INSPECTION) (EVALUATE) REVIEWED
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 63,804 hrs · 21,471 cycles
FAULT - CHAFED - SKIN SURFACE, LOWER FUSELAGE MAIN EQUIPMENT CENTER ACCESS DOOR EXTERNAL. (AGING A/C INSPECTION) (EVALUATE) PAPER OK
Part: STIFFENER — CRACKED (UNKNOWN) · airframe 63,804 hrs · 21,471 cycles
FAULT - STIFFENER CENTER WING FRONT SPAR CRACK IS STIFFENER AT STA 785.9 RBL 11 (REPAIR) PERFORM REPAIR I.A.W SRM 57-10-10-2R-2 REPAIR INSTRUCTIONS 4. O~Q REV.86 AND SREO-58151-REQ001 REV.1 AND SREO-76672-REF REV.1 BOEING DWG NO.111T5201 SH.2 REV.A AND BOEING DWG NO.140T0520 SH.23 REV.-. STIFFENER CENTER WING FRONT SPAR CRACK IS STIFFENER AT STA 785.9 RBL 11 (REPAIR) REVIEWED
Part: STIFFENER — CRACKED (UNKNOWN) · airframe 63,804 hrs · 21,471 cycles
FAULT - STIFFENER CENTER WING FRONT SPAR CRACK IS STIFFENER AT STA 785.9 LBL 33 (REPAIR) PERFORM REPAIR I.A.W SRM 57-10-10-2R-2 REPAIR INSTRUCTIONS 4.O~Q REV.86 AND SREO-58151-REQ001 REV.1 AND SREO-76672-REF REV.1 BOEING DWG NO.111T5202 SH.2 REV.- AND BOEING DWG NO.140T0520 SH.23 REV.-. STIFFENER CENTER WING FRONT SPAR CRACK IS STIFFENER AT STA 785.9 LBL 33 (REPAIR) REVIEWED
2022
Part: NONE — INOPERATIVE (DOORS) · airframe 61,624 hrs · 20,608 cycles
INSPECTION TYPE:N/AENTRY DOOR GASKET NOT IN TRACKACCOMPLISHED EO B767-5210-84538-A
Part: FAN — ODOR (CABIN) · airframe 61,291 hrs · 20,478 cycles
STRONG ODOR ON FINAL FWD EQIP COOLING EXH FAN STATUS AFTER LANDING. DEF FWD EQPT COOLING EXH FAN PER MEL 21-58-4-2-1 C/W DMP ACCESS FWD EQPT EXH FAN VERIFIED FAN NOISE AND SMELL PULLED P6H21/P11 P22 NO FURTHER SMELL NOTEDR/R FWD EQUIP COOLING EXHIT FAN IAW AMM 21-58-06. OPS CHECK GOOD.
2021
Part: INTERCOSTAL — CORRODED (BS 1602) · airframe 59,123 hrs · 19,753 cycles
INSPECTION TYPE:C12CORROSION WAS FOUND ON INTERCOSTAL (P/N;146T5649-7) ON MAIN DECK FLOOR NEAR STA 1602.64, LBL 54.75.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH 4, REV "A";SH 5,REV"C" AND 767-300F SRM 51-40-02 REV 80.03
Part: ANGLE — CORRODED (BS 1586.51) · airframe 59,123 hrs · 19,753 cycles
INSPECTION TYPE:C12CORROSION WAS FOUND ON CLIP(P/N:146T5619-357) ON MAIN DECK FLOOR NEAR STA 1586.51, LBL 54.75.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH 4, REV"A" AND 767-300F SRM 51-40-02 REV 80.03
Part: ANGLE — CORRODED (BS 1597) · airframe 59,123 hrs · 19,753 cycles
INSPECTION TYPE:C12CORROSION WAS FOUND ON ANGLE (P/N:146T5628-22) ON MAIN DECK FLOOR BETWEEN STA 1581.845 AND STA 1597.940, RBL 33.INSTALL NEW PART I.A.W. BOEING DWG 146T5650 SH 2, REV "A", AND 767-300F SRM 51-40-02 REV 80.03
Part: INTERCOSTAL — CORRODED (BS 1597.94) · airframe 59,123 hrs · 19,753 cycles
INSPECTION TYPE:C12CORROSION WAS FOUND ON INTERCOSTAL(P/N:146T5649-3) ON MAIN DECK FLOOR NEAR STA 1597.04, BETWEEN RBL 11 AND RBL 33.INSTALL NEW I.A.W BOEING DWG 146T5650 SH 2, REV"A" AND 767-300F SRM 51-40-02 REV 80.03.
Part: FILLER — CORRODED (BS 1601) · airframe 59,123 hrs · 19,753 cycles
INSPECTION TYPE:C12CORROSION WAS FOUND ON FILLER(P/N:146T5649-67) ON MAIN DECK FLOOR NEAR STA 1601, RBL 60.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH 5,REV"C" AND 767-300F SRM 51-40-02 REV 80.03
Part: FILLER — CORRODED (BS 1601) · airframe 59,123 hrs · 19,753 cycles
INSPECTION TYPE:C12CORROSION WAS FOUND ON FILLER (P/N:146T5609-67) ON MAIN DECK FLOOR NEAR STA 1601,LBL 60.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH 5, REV "C" AND 767-300F SRM 51-40-02 REV 80.03.
Part: CHANNEL — CORRODED (BS 1605) · airframe 59,123 hrs · 19,753 cycles
INSPECTION TYPE:C12CORROSION WAS FOUND ON MOPSILL(P/N:146T5651-15) ON MAIN DECK CARGO FLOOR STRUCTURE AT STA 1605, LBL54.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH5,REV"C" AND 767-300F SRM 51-40-02 REV 80.03
Part: FLOOR SUPPORT — CORRODED (BS 1602) · airframe 59,123 hrs · 19,753 cycles
INSPECTION TYPE:C12CORROSION WAS FOUND ON INTERCOSTAL(P/N:146T5649-8)ON MAIN DECK FLOOR NEAR STA 1602.64, RBL 54.75.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH 4, REV"A"; SH 5, REV"C" AND 767-300F SRM 51-40-02 REV 80.03.
Part: STIFFENER — CRACKED (FUEL CELL) · airframe 59,123 hrs · 19,753 cycles
INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER(P/N:111T2005-7)ON STA 785.9,LBL 11.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.80.03 AND UPS EO B767-5740-58151-C AND B767-5720-76672-A.
2020
Part: UNKNOWN — ODOR (COCKPIT) · airframe 55,508 hrs · 18,402 cycles
ON DESCENT INTO ONT PASSING THROUGH 17,000, STRONG ODOR OF BURNING RUBBER FILLED THE COCKPIT LASTED FOR APPROXIMATELY 3 MINUTES. THEN DISSIPATEDA/C POWERED FOR 24 HOURS. RAN BOTH PACKS 1 HOUR. NO ODOR DETECTED. OK PER AMM 05-51-56.
Part: PITOT TUBE — OBSTRUCTED (PITOT/STATIC SYS) · airframe 55,435 hrs · 18,369 cycles
INSPECTION TYPE:N/A**AIR TURN BACK** AIRSPEED UNRELIABLE, SINGLE AIR DATA, RUDDER RATIO, L ENG EEC, R ENG EEC, AILERON LOCKOUT.FLUSHED PITOT STATIC SYS AS PER AMM 34-11-00 FOUND DEBRIS IN FO PITOT TUBE. ACCOMPLISHED AIR DATA SYS TEST AS PER AMM 34-12-00 OPS CHECK NORMAL.
2019
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,771 hrs · 18,070 cycles
INSPECTION TYPE:C11 CRACK ON FUSELAGE SKIN (P/N: 148T3121-2) ON STA 1725.5, NEAR S-7R. REPAIR IAW EO B767-5330-24301 APPX C AND 5330-73933-A, SR:4-4555838821, AND SRM 53-80-01 REPAIR 5, REV 75.00.
Part: STIFFENER — CRACKED (NLG WW) · airframe 54,771 hrs · 18,070 cycles
INSPECTION TYPE:C11 CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287, RBL 25. REPAIR IAW EO B767-5310-20118-F AND SRM 51-70-12 GENERAL, FIGURE 1, REV 75.00.
Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 54,741 hrs · 18,059 cycles
EMERGENCY LIGHT SWITCH INOP. R&R'D CONT PNL PER AMM 33 51 08. OS CHK GOOD. IPC 32 51 08 01A, 010
Part: SEAL — OUT OF POSITION (PAX DOOR) · airframe 54,396 hrs · 17,925 cycles
MAIN ENTRY DOOR IS DIFFICULT TO LIFT AFTER FLIGHT.FOUND AFT DOOR LINER SEAL OUT OF RETAINER. REINSTALLED SEAL AND CLEANED. DOOR OPS NORMAL PER AMM 52-12-00
Part: DOOR SEAL — UNSECURE (ENTRY DOOR) · airframe 54,096 hrs · 17,821 cycles
INSPECTION TYPE:N/A CREW ENTRY DOOR SEAL (INNER) IS COMING OFF. REINSTALLED CREW ENTRY DOOR FWD INNER TRIM SEAL REF AMM 52 09 01 OPERATED DOOR SEVERAL TIMES REF AMM 52 12 00 SEAL REMAINS SECURED.
Part: DOOR SEAL — NOT SEATED (ENTRY DOOR) · airframe 53,758 hrs · 17,691 cycles
INSPECTION TYPE:N/A CREW ENTRY DOOR RUBBER SEAL WILL NOT STAY STRAIGHT WHEN CLOSING THE CREW ENTRY DOOR. RESEATED SEAL ON TRACK RE AMM 52-09-01.
Part: TRIM PANEL — UNSECURE (ENTRY DOOR) · airframe 53,485 hrs · 17,580 cycles
INSPECTION TYPE:N/A MAIN ENTRY DOOR TRIM UNDONE. HANGING LOOSE. MAIN ENTRY DOOR LINING NEW INSTALLED IAW AMM 52-12-02-400-025 REV 125.01.
2018
Part: FILLET — DAMAGED (PAX DOOR) · airframe 52,513 hrs · 17,183 cycles
DURING RAIN, NOTED WATER LEAKING INTO THE MAIN DECK FROM AROUND TOP AFT CORNER OF MAIN DECK DOOR. FOUND A SMALL GAP IN FILLET SEAL OF TOP AFT CORNER SEAL DEPRESSOR. FILLET SEAL REPAIRED IAW AMM 51-31-00-201, REV 124.03.
Part: BATTERY — DISCHARGED (COCKPIT) · airframe 52,236 hrs · 17,082 cycles
DURING PDC FOUND EMERGENCY LIGHTS INOP. R&R BATTERY IAW AMM 33-51-07-02, AND -422. OPS CHK GOOD.
2017
Part: GAS CYLINDER — INOPERATIVE (LIFE RAFT) · airframe 50,247 hrs · 16,381 cycles
LIFE RAFT GAS STOWAGE SUPPORT INOPERATIVE. REPLACED LIFE RAFT STOWAGE ASSEMBLY GAS SUPPORT STRUT OK FOR SERVICE.
Part: SWITCH — LOOSE (EMERGENCY LIGHTS) · airframe 50,200 hrs · 16,362 cycles
EMERGENCY EXIT LIGHT SWITCH LOOSE. SECURED THE LIGHT SWITCH IAW MM 20-11-00.
Part: ANGLE — CRACKED (NLG WW BULKHEAD) · airframe 49,933 hrs · 16,258 cycles
INSPECTION TYPE: C10, CRACK DAMAGE WAS FOUND ON THE NOSE WW AFT BULKHEAD VERTICAL ANGLE AT BS 287, LBL 25 , WL 173. REPAIR IAW EO B767-5310-20118-F, AND SRM 51-70-12, GENERAL FIGURE 1 , REV.68
Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 49,933 hrs · 16,258 cycles
INSPECTION TYPE: C10, CRACK DAMAGE WAS FOUND ON THE BULK CARGO DOOR LOWER FRAME AT BS 1439. REPAIR IAW SRID 3-3954693842 AND EO B767-5230-65178-A.
Part: STIFFENER — CRACKED (BS 785.9) · airframe 49,933 hrs · 16,258 cycles
INSPECTION TYPE: C10, CRACKED STIFFENER UPPER SIDE AT BS 785.9, RBL 33. REPAIRED IAW SRM 57-10-10-2R-2, REPAIR 2, REV 68, AND EO B767-5740-58151-A.
Part: STIFFENER — CRACKED (BS 785.9) · airframe 49,933 hrs · 16,258 cycles
INSPECTION TYPE: C10, A CRACK FOUND ON THE STIFFENER, UPPER SIDE AT BS 785.9 , RBL 55. REPAIRED IAW SRM 57-10-10-2R-2, REPAIR 2, REV 68, AND EO B767-5740-58151-A.
Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 49,622 hrs · 16,147 cycles
INSPECTION TYPE: ASE, RT ENG OTBD THRUST REVERSER FRAME HAS A BRACKET CRACKED AT ABOUT THE 9 O'CLOCK POSITION FWD OF CASCADE VANES UNDER TRANSLATING SLEEVE. ACCOMPLISHED A TEMPORARY REPAIR IAW EO 7830-64537-A.
Part: APU — INOPERATIVE · airframe 49,056 hrs · 15,927 cycles
AFTER LANDING, ATTEMPTED TO START APU. APU DID NOT START AND APU FAULT EICAS ILLUMINATED. OPEN.
2016
Part: DOOR — GOUGED (NLG) · airframe 47,160 hrs · 15,277 cycles
GOUGE IN FWD LT NLG DOOR APPROXIMATELY 15" FWD OF T/E IN CENTER, APPROXIMATELY .2812" BY .2500" EVALUATED DAMAGE INSTALLED TEMP REPAIR DEFER IAW SRM 52-80-02-1A-2, TABLE 2.
Part: DOOR — UNKNOWN (L1) · airframe 46,620 hrs · 15,099 cycles
L1 ENTRY DOOR HARD TO OPEN FROM HALF WAY TO FULL OPEN. PERFORMED OPS TEST OF CREW ENTRY DOOR, OPS CK NORMAL REF 52-12-00.
2015
Part: FLOORBOARD — DAMAGED (NOT REPORTED) · airframe 45,582 hrs · 14,747 cycles
MAIN CARGO FLOORBOARD CENTER LINE MOST AFT PANEL POS NR 10 DAMAGED. FABRICATED NEW FLOORBOARD IAW EO B767-5320-9693H.
Part: DOOR — LACK OF LUBE (CREW) · airframe 45,485 hrs · 14,720 cycles
CREW ENTRY DOOR IS HARD TO OPEN, DIFFICULT TO RAISE THROUGH THE FIRST 2 FT OF TRAVEL. LUBRICATED IAW AMM 12-21-18, REV 116.01, 10-22-15.
Part: PSEU — INOPERATIVE (LANDING GEAR) · airframe 45,264 hrs · 14,621 cycles
EMERGENCY DECLARED AT 120 KTS ON T/O ROLL WITH FLAPS 15 AND T/O POWER SET, RECEIVED GEAR NOT DOWN EICAS MESSAGE, CONFIG LIGHT AND AUDIBLE WARNING HORN. ALL REMAINED ON FOR ENTIRE LIGHT. ALL OTHER GEAR INDICATIONS WERE NORMAL. C/O FIM 31-51-00-815-812 AND PERFORMED PSEU BITE TEST IAW FIM 32-09-03-8, FIG 103, REV 115.01 07/22/15. FOUND SEVERAL FAULTS DISPLAYED. FAULT CODE: 302, 300, 286, 285, 284, 282 , 403, 402, 401, 201, 900, 901, 894, 104, 283, 301, 211 AND CARD FAULT 002. R & R PSEU IAW AMM 32-09-04-4, REV 115.02
Part: SKIN — DENTED (LT WING) · airframe 45,169 hrs · 14,593 cycles
INSPECTION TYPE: C, NINE DENTS ON LT WING INBD AFT FLAP LOWER SKIN. REPAIRED IAW SRM 57-53-01-2R-1, REPAIR 1, SRM 51-70-10-2R-4, REPAIR 3 AND SRM 51-70-10-2R-4, REPAIR 4.
Part: SKIN — DENTED (NR 4 SLAT) · airframe 45,169 hrs · 14,593 cycles
INSPECTION TYPE:C9, DENT DAMAGE ON LT WING NR 4 SLAT T/E WEDGE UPPER SKIN AT OSS 669.49. REPAIR IAW SRM 57-43-02-2R-1. REPAIR 1, SRM 51-70-10-2R-3, REPAIR 3 AND SRM 51-70-10-2R-4, REPAIR 4, REV 63.00.
Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 45,169 hrs · 14,593 cycles
INSPECTION TYPE:C9, FOUND CRACK ON CARGO FLOOR PANEL, 232EFF AT BS 511-599, RBL 77 - 88. FABRICATED THE REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-H.
Part: STRINGER — CRACKED (BS 1505) · airframe 45,169 hrs · 14,593 cycles
INSPECTION TYPE:C9, CRACK DAMAGE ON LT SIDE FUSELAGE STR S-20L AT BS 1505, REPAIR IAW SR: 3-3301589137 WITH FUSELAGE FAA APPROVED 8100-9 FORM , DATE: 21AUG2015 AND FLOOR APPROVED 8100-9 FORM , DATE : 20AUG2015 AND EO B767-5330-58475-A.
Part: CONTAINER — DAMAGED (ESCAPE ROPE) · airframe 45,103 hrs · 14,565 cycles
MAIN DOOR ESCAPE ROPE BAG IS DAMAGED, ALLOWING ROPE TO GET CAUGHT IN ENTRY DOOR. R & R THE COVER, CHECK CONDITION SATISFACTORY, OPS NORMAL, IAW AMM 25-61-02.
2014
Part: CIRCUIT CARD — INOPERATIVE (FWD EQUIP)
ETOP FWD EQUIPMENT OVERHEAT LIGHT ILLUMINATED, FOLLOWED QRH CHECK LIST LIGHT ILLUMINATED AGAIN, RETURNED TO DEPARTURE. TROUBLESHOT IAW FIM 21-58-00-815-833 BLOCKS 1, 2, 3, 4, 5 AND 28. R & R EQUIPMENT COOLING INDICATION CARD IAW AMM 21-58-24-00-001, OPS NORMAL. ACFT BACK IN SERVICE.
Part: IDG — INOPERATIVE (LT)
EMERGENCY DECLARED, LT AC BUSS OFF MESSAGE. WORKED CHECKLIST AND WAS ABLE TO RESET LT AC SYSTEM WITH APU. R & R LT ENGINE IDG IAW AMM 24-11-01. OPS AND LEAK CHECKED GOOD.
Part: CAP — OPEN (RT ENGINE OIL)
PERFORMED AN AIR TURN BACK DUE TO RT ENGINE OIL PRESSURE LOW ON CLIMBOUT. ENGINE WAS NOT SHUTDOWN. FOUND RT ENGINE OIL CAP OPEN. SERVICED RT ENGINE WITH TWO QUARTS OF OIL IAW AMM 12-13-01-613. OK FOR SERVICE.
2013
Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 40,645 hrs · 12,869 cycles
INSPECTION TYPE: C08, CHAFING ON UPPER SURFACE SKIN OF LT WING INBD AFT FLAP AT IFS 105.25. REPAIR IAW SRM 57-53-01-2R-1, FIG 201, REV 56.00 2. SRM 51-70-10-2R-4, FIG 202, SHEET 1, REV 56.00.
Part: SKIN — DAMAGED (LT WING TE FLAP)
LT WING INBD AFT FLAP LWR SKIN DAMAGED. REPAIRED IAW EO B767-5750-45073-C.
Part: FLOOR PANEL — DAMAGED
FLOOR PANEL HAS A HOLE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
Part: FLOOR PANEL — DAMAGED (CABIN)
FLOOR PANEL, POS 12R, DAMAGED. REPAIRED IAW SRM 53-00-50-2R.
Part: FLOOR PANEL — DAMAGED (MAIN DECK)
FLOOR PANEL DAMAGED, MAIN DECK POS 14 AFT. REPAIRED FLOOR IAW SRM 53-00-50-2R.
2012
Part: FLOOR PANEL — DAMAGED (MAIN CARGO)
MAIN CARGO DECK FLOOR PANEL DAMAGED, POS 7. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9693-H.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO)
FWD OTBD FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO)
MAIN CARGO DECK FLOOR PANEL, POS 4L FWD OTBD PANEL DAMAGED. FABRICATED NEW FLOOR PANEL REF B767-5320-9693-H.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO)
MAIN CARGO DECK FLOOR PANEL DAMAGED, POS 6L. FABRICATED FLOOR PANEL IAW EO B767-5320-9693-H AND B767-5320-49255-A.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO)
MAIN CARGO DECK FLOOR PANEL DAMAGED. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
Part: FLOOR PANEL — GOUGED (MAIN CARGO)
MAIN CARGO DECK FLOOR PANEL POS 5/6 FWD CENTER HAS 3 GOUGES. REPAIRED PANEL IAW SRM 53-00-50-2R.
Part: FLOOR PANEL — DAMAGED (CABIN)
FLOOR PANEL POS9 AFT CTR DAMAGED. FABICATED FLOOR PANEL IAW EO B767-5320-9693-H AND REPLACED.
Part: FLOOR PANEL — DAMAGED (CABIN)
FLOOR PANEL, POS 2L, 3RD OTBD DAMAGED. FABRICATED FLOOR PANEL IAW EO B767-5320-9693-H AND REPLACED.
Part: FLOOR PANEL — PUNCTURED (MAIN DECK)
MAIN CARGO DOOR FLOOR PANEL 4R HAS A PUNCTURE, DELAM, PN 143T5876-85. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
Part: FLOOR PANEL — DELAMINATED (MAIN CARGO DECK)
MAIN CARGO DECK FLOOR PANEL DAMAGED POS 3R CENTER. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
2011
Part: WARNING LIGHT — FALSE ACTIVATION (ANTI ICE VALVE)
LEFT ENG ANTI -ICE VALVE LIGHT ILLUMINATED WITH SWITCH ON WHEN THRUST AT IDLE. LIGHT OUT WHEN THRUST INCREASED. ANTI-ICE VALVE CHECKED, NO LEAK FOUND. FLUID CLEANED AWAY FROM PLUG.
Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 36,533 hrs · 11,324 cycles
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 50.
Part: WEDGE — DELAMINATED (LT NR 6 SLAT) · airframe 36,533 hrs · 11,324 cycles
INSPECTION TYPE:C, LT WING NR 6 SLAT T/E WEDGE UPPER SURFACE REPAIR PATCH DELAMINATED. METAL HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 8, REV 50.
Part: FLOOR PANEL — DENTED (MAIN CARGO) · airframe 36,533 hrs · 11,324 cycles
INSPECTION TYPE:C, MCD FLOOR PANEL FOUND 6 DENTS AND 9 PUNCTURES AT STA 654+22 TO STA 690 LBL 55 TO LBL 77. MCD FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-01.
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 36,533 hrs · 11,324 cycles
INSPECTION TYPE:C, MCD FLOOR PANEL FOUND 8 DENTS AND 5 PUNCTURES AT STA 654+22 TO STA 690 LBL 11 TO RBL 11. MCD FLOOR PANEL FABIRCATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-01.
Part: STIFFENER — CRACKED (BS 785.9) · airframe 36,533 hrs · 11,324 cycles
INSPECTION TYPE:C WING CENTER TANK FRONT SPAR VERTICAL STIFFENER TOP AREA FOUND CRACK JUST AT STA 785.9 LBL 10.94 WNG CTR TANK FRONT SPAR VERT STIFFENER REPAIRED PER SRM 57-10-10-2R2 REPAIR 2 FIG 201 REV 50 JUST AT STA 785.9 LBL 10.94 ORG MAT'L BAC1518-912-2024T3511 CRK LENGTH 3.25" CUT OFF LENGTH 19.5" REPAIR CLASSIFIED AS MAJOR REPAIR, MAT'L BAC1518-912-7075T6511 AS REPAIR STIFFENER SECT. CLAD 2024T3-0100IN AS REPAIR STRAPS TOTAL LENGTH 26"
Part: STIFFENER — CRACKED (WING CTR) · airframe 36,533 hrs · 11,324 cycles
INSPECTION TYPE:C, WING CENTER TANK FRONT SPAR VERTICAL STIFFENER TOP AREA FOUND CRACK JUST AT STA 785.9 RBL 10.94 STIFFENER REPAIRED IAW SRM 57-10-10-2R2, REPAIR 2, FIG 201, REV 50 AT STA 785.9 RBL 10.94 ORG MATERIAL BAC1518-912-2024T3511 CRACK LENGTH 1.2" CUT OFF LENGTH IS 19.5. REPAIR IS CLASSIFIED AS MAJOR REPAIR.
Part: FLOOR PANEL — DENTED (CARGO DECK)
FLOOR PANEL AT POS 4 LT OTBD DENTED. NEW FLOOR PANEL REF EO B767-5320-9693B.
Part: FLOOR PANEL — DAMAGED (CARGO DECK)
MAIN CARGO FLOOR PANEL POS 5R HAS A HOLE. FABRICATED IAW B767-5320-9693-H.
Part: FLOOR PANEL — DAMAGED (CARGO DECK)
MAIN CARGO DECK POS 4L 1/2 HOLE IN FLOOR PANEL, FABRICATED IAW EO 767-5320-9696-H.
Part: FLOOR PANEL — DAMAGED (CARGO BAY)
FLOOR PANEL DAMAGED AT POS 2R OTBD PANEL, REF LOG PAGE 712639-1. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.
2010
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
REF D-4344202 POSITION 2L HAS 1 X 1 HOLE IN FLOORBOARD. REMOVED FLOOR PANEL AND MFG NEW PANEL IAW EO B767-5320-9693 AND INSTALLED IAW AMM 51-01-01.
Part: FLOOR PANEL — DAMAGED (CABIN)
REF D 434408, POSITION 2L HAS 1 X 1 HOLE IN FLOOR PANEL. REMOVED FLOOR PANEL AND MFG NEW PANEL IAW EO B767-5320-9693G AND INSTALLED IAW AMM 51-01-01.
Part: SKIN — DAMAGED (TE FLAP)
ON ARRIVAL FOUND DAMAGE TO OTBD FLAP L/E SKIN PANEL 666FT, 3.5"X0.75" LOCATED 1.5" FROM L/E OF PANEL AND 1.5" FROM OTBD EDGE OF PANEL. REPAIRED IAW SRM 57-53-01-2R FIG 201 AND SRM 51-70-03.
Part: SWITCH — LOOSE (EMERGENCY LIGHTS)
EMERGENCY EXIT LIGHT SWITCH IS LOOSE. SECURED SWITCH AS REQUIRED.
Part: UNKNOWN — ODOR (CABIN)
INSPECTION TYPE:ETOP WHEN LANDING GEAR EXTENDED APPROACH A STRONG ODOR OF BURNING RUBBER ENTERED THE COCKPIT. ODOR DISSIPATED BY LANDING. PERFORMED VISUAL INSPECTION OF INLET AND EXHAUST ON LEFT AND RIGHT PACK. RAN BOTH PACKS AT FULL HOT NO DISCREPANCIES NOTED.
2009
Part: SKIN — CRACKED (LE SLAT) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:ETOP RHW NR 9 SLAT INBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED RHW NR 9 SLAT INBD AREA AT OSS572.9 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV45 ORG MAT'L IS CLAD7075T6-0063 IN CRACK LENGTH IS 0.125IN DAMAGED CUTOUT IS 7.25 INCH BY 9 INCH. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MAT'L CLAD7075T6-0071IN AS DOUBLER, CLAD 7075T6-0063IN AS REPAIR PLATE. REPAIR SIZE 10 1/4 INCH BY 12 INCH.
Part: SKIN — CRACKED (LE SLAT) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:ETOP RHW NR 9 SLAT OTBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED RHW NR 9 SLAT OTBD AREA AT OSS641.62 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV45 ORG MAT'L IS CLAD7075T6-0063IN CRACK LENGTH IS 0.090 INCH DAMAGED CUTOUT IS 7.75 INCH BY 9 INCH THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MAT'L CLAD7075T6-0071IN AS DOUBLER CLAD7075T6-0063IN AS REPAIR PLATE. REPAIR SIZE IS 10 1/4 INCH BY 12 INCH.
Part: SKIN — CRACKED (LE SLAT) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:ETOP LHW NR 4 SLAT OTBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED LHW NR 4 SLAT OTBD AREA AT OSS641.6 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 ORG MAT'L IS CLAD7075T6-0063IN, CRACK LENGTH IS 0.125 INCH DAMAGED CUTOUT IS 7.735 INCH BY 9 INCH THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MAT'L CLAD7075T6-0071IN AS DOUBLER, CLAD 7075T6-0063IN AS REPAIR PLATE. REPAIR SIZE 10 1/4 INCH BY 12 INCH.
Part: SKIN — CRACKED (LE SLAT) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:ETOP LHW NR 4 SLAT INBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED LHW NR 4 SLAT INBD AREA AT OSS572.9 NOSE SKIN REPAIRED AS PER SRM 57-43-01 2R2 FIG 201 REV45 ORG MAT'L IS CLAD 7075T6-0063 IN, CRACK LENGTH IS 0.090IN. DAMAGED CUTOUT IS 7.375 INCH BY 9 INCH REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MAT'L CLAD 7075T6-0071N AS DOUBLER CLAD 7075T6-0063IN AS REPAIR PLATE. REPAIR SIZE IS 10 1/2 INCH BY 12 INCH.
Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C NR 1 PYLON RT INTERNAL VERTICAL FRAME UPPER ATT SUPPORT CLIP CRACKED AT NAC STA 285.45 (CRACK LENGTH 1 INCH). NR 1 PYLON RT INTERNAL VERTICAL FRAME UPPER ATT SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 JUST AT NAC STA 285.45.
Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C BULK CARGO COMPT STA 1439 LBL 24 INCH FLOOR PANEL SUPPORT FOUND CRACK (CRACK LENGTH 1.75 INCH), BULK CARGO STA 1439 LBL 22.33 INCH FLOOR SUPPORT REPAIRED AS PER SRM 51-70-11-0G FIG 1 REV 45 ORG, MATERIAL IS 7075T6-0.040IN, CRACK LENGTH 1.75 INCH, DAMAGED CUTOUT 1.875 INCH BY 1.625 INCH THIS IS CLASSIFIED A MAJOR REPAIR WITH MATERIAL 7075T6 BARE 0.040 INCH AS REPAIR ANGLE REPAIR LENGTH IS 7.75 INCH.
Part: STIFFENER — DEFORMED (FLOOR PANEL) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:6C BULK CARGO COMPT STA 1502 LBL 8 INCH FLOOR PANEL STIFFENER FOUND DEFORM. BULK CARGO COMPT STA 1502 LBL 8 INCH FLOOR PANEL STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.
Part: FRAME — CRACKED (NR 1 PYLON) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C NR 1 PYLON INTERNAL FRAME CRACKED AT NAC STA 285.45 RT SIDE, (CRACK LENGTH 2 INCHES) NR 1 PYLON INTERNAL FRAME REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 JUST AT NAC STA 285.45 RT SIDE.
Part: STIFFENER — DEFORMED (FLOOR PANEL) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:6C BULK CARGO COMPT STA 1480 LBL 8 INCH FLOOR PANEL STIFFENER FOUND DEFORM. BULK CARGO COMPT STA 1480 LBL 8 INCH FLOOR PANEL STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.
Part: STIFFENER — DEFORMED (FLOOR PANEL) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:6C BULK CARGO COMPT STA 1480 RBL 8 INCH FLOOR PANEL STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1480 RBL 8 INCH FLOOR PANEL STIFFENER REPLACE AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.
Part: STIFFENER — DEFORMED (CARGO BAY) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:6C BULK CARGO COMPT STA 1439 LBL 24 INCH STIFFENER FOUND DEFORM. BULK CARGO COMPT STA 1439 LBL 24 INCH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.
Part: STIFFENER — DEFORMED (CARGO BAY) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C BULK CARGO COMPT STA 1502 LBL 16 INCH FLOOR PANEL STIFFENER FOUND DEFORM. STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.
Part: PANEL — DAMAGED (RT WING TE FLAP) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C RT WING I/B MAIN FLAP O/B EDGE UPPER SURFACE FOUND CHAFE. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5H REV 45.
Part: SLAT — CHAFED (RT WING) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C RHW - NR 9 SLAT OTBD UPPER EDGE FOUND CHAFE. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REV 45, REPAIR 4, FIG 202 SHEET 8.
Part: FAIRING — DELAMINATED (LT WING) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C LT WING O/B FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5C FIG 2 REV 45.
Part: PANEL — DAMAGED (LT WING TE FLAP) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C LT WING I/B MAIN FLAP O/B EDGE UPPER SURFACE FOUND CHAFED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5H REV 45.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 1425 TO 1540, LBL 55 TO LBL 77. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGE AT STA 654+22 TO 690 RBL 33 TO RBL 55. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53- 01-01.
Part: FAIRING — DELAMINATED (RT WING) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-02 PAR 5C FIG 2 REV 45.
Part: BRACKET — CRACKED (LT WING) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C LT WING L/E LES 155 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET FOUND CRACKED (1.125 INCH). LT WING L/E LES 155 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 412 TO 540, LBL 11 TO RBL 11. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.
Part: PANEL — DELAMINATED (LT ELEVATOR) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C LEFT I/B ELEVATOR UPPER SURFACE O/B T/E AREA DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PAR 4A FIG 10 REV 45.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 412 TO 540, RBL 33 TO RBL 55. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.
Part: SLAT — CHAFED (LT WING) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C LEFT WING NR 4 SLAT I/B UPPER EDGE FOUND CHAFE. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10, REV 45 REPAIR 4 FIG 202 SHEET 8 AND SHEET 9 NOTES.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 283 TO 412, RBL 33 TO RBL 55. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.
Part: ANGLE — CRACKED (BS 1087) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:6C AFT CARGO COMPT STA 1087 RBL 24 BELOW FLOOR CLIP FOUND CRACK. AFT CARGO COMPT STA 1087 RBL 24 BELOW FLOOR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 1197+108 TO 1263, RBL 77 TO RBL 88. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.
Part: FITTING — CRACKED (CARGO BAY) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C AFT CARGO STA 1087 LBL 24 BELOW FLOOR CLIP FOUND CRACK (CRACK LENGTH 0.75 INCH). AFT CARGO STA 1087 LBL 24 BELOW FLOOR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.
Part: DOUBLER — DELAMINATED (TE FLAP) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C LHW INBD AFT FLAP UPPER SURFACE OTBD T/E AREA DELAMINATED FOUND ON EXISTING REPAIR PATCH. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REV 45, REPAIR 4 FIG 201 SHEET 1.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 833 TO 930, LBL 11 TO RBL 11. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53- 01-01.
Part: WEB — CRACKED (LE SLAT) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C LEFT WING NR 3 SLAT O/B NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED (CRACK 0.090 INCH). LEFT WING NR 3 SLAT O/B AREA AT OSS792.3 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45, ORG MATERIAL IS CLAD 7075T6-0.063IN, CRACK LENGTH 0.090 INCH DAMAGED CUTOUT 7 X 9 INCHES, THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL CLAD 7075T6-0.071IN AS DOUBLER, CLAD 7075T6-0.063IN AS REPAIR PLATE, REPAIR SIZE 10 X 12.125 INCHES.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C AFT BULK CARGO STA 1562-1582 LBL 75 INCH FLOORBEAM ANGLE FOUND CRACK (CRACK LENGTH 1.375 INCH), AFT BULK CARGO STA 1562-1582 LBL 75 INCH FLOORBEAM ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.
Part: FITTING — CRACKED (FUSELAGE) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C MEC COMPT STA 246 LBL 50 FLOORBEAM CLIP FOUND CRACKED CRACK 0.875 INCH. MEC COMPT STA 246 LBL 50 FLOORBEAM CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.
Part: FITTING — CRACKED (FUSELAGE) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C MEC COMPT STA 246 RBL 10 FLOORBEAM CLIP FOUND CRACK (CRACK LENGTH 1.5 INCH). MEC COMPT STA 246 RBL 10 FLOORBEAM CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C AFT BULK CARGO STA 1562-1582 RBL 76 INCH FLOORBEAM ANGLE FOUND CRACK (CRACK LENGTH 0.25 I NCH), AFT BULK CARGO STA 1562-1582 RBL 76 FLOORBEAM ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45
Part: WEB — CRACKED (LE SLAT) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C LEFT WING NR 3 SLAT I/B NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED (CRACK .0625 INCH). LEFT WING NR 3 SLAT I/B AREA AT OSS724.24 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45 ORG MATERIAL IS CLAD 7075T6-0.063IN, CRACK LENGTH IS .0625 INCHES DAMAGED CUTOUT IS 7.125 X 9 INCHES THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL CLAD 7075T6-0.071IN AS DOUBLER CLAD 7075T6-0.063IN AS REPAIR PLATE, REPAIR SIZE 10.25 X 12.125 INCHES.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C AFT BULK CARGO STA 1562-1582 LBL 76 INCH FLOORBEAM ANGLE FOUND CRACK (CRACK LENGTH 0.5 INCH), AFT BULK CARGO STA 1562-1582 LBL 76 FLOORBEAM ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.
Part: WEB — CRACKED (LE SLAT) · airframe 32,134 hrs · 9,846 cycles
INSPECTION TYPE:C RIGHT WING NR 10 SLAT I/B NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED (CRACK 0.090 INCH). RIGHT WING NR 10 SLAT I/B AREA AT OSS724.24 NOSE SKIN REPAIRED AS PER SRM 57- 43-01-2R2 FIG 201 REV 45 ORG. MATERIAL IS CLAD 7075T6-0.063IN, CRACK LENGTH IS 0.090 INCH, DAMAGED CUTOUT IS 7.125 X 9 INCHES. THIS CLASSIFIED A MAJOR REPAIR WITH MATERIAL CLAD 7075T6-0.071IN AS DOUBLER, CLAD 7075T6-0.063IN AS REPAIR PLATE, REPAIR SIZE IS 10.25 X 12.125 INCHES.
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
INSPECTION TYPE:N/A POS 9 RBL 5 STATION 1134 DAMAGED 1.7 X 1.2 PUNCTURE. REPAIRED PER EO B767-5320-32928-A.
Part: FLOOR PANEL — DAMAGED (FUSELAGE)
INSPECTION TYPE:N/A POS 9R RBL 8 STATION 1160 DAMAGED 1 INCH CUTOUT. REPAIRED PER EO B767-5320-32929-A.
2008
Part: UNKNOWN — NOISY (NLG)
INSPECTION TYPE:N/A 30 SECS AFTER GEAR RETRACTION THERE WAS A NOISE UNDER C/P SIMILAR TO A COMPRESSOR STALL WITH NO OTHER INDICATIONS. DURING DESCENT FROM FL 390 PASSING FL 390 PASSING FL 250 SAME SOUND WAS HEARD THROTTLES AT IDLE. CREW REQUESTED EMERGENCY EQUIPMENT BE STANDING BY PERFORMED DVI OF NOSE AREA PNEUMATIC DUCT WORK & ASSOCIATED AREAS, NO DEFECTS NOTED. PRESSURIZED A/C TO ALLOWABLE GROUND LIMITS IAW B767 MM 05-51-24-2. REPEATED SEVERAL TIMES. COULD NOT DUPLICATE ON GROUND AT THIS TIME. OK FOR CONTINUED SERVICE.
Part: LIGHT — INOPERATIVE (CABIN)
INSPECTION TYPE:ETOP ENTRY DOOR EMERGENCY LIGHT IS OUT. REMOVED AND REPLACED EMERGENCY DOOR LIGHT PER MM 33-51-03-2.
2007
Part: CHARGER — UNKNOWN (MAIN BATTERY)
INSPECTION TYPE:ETOP AT ENG SHUTDOWN RECEIVED ADVISORY LEVEL EICAS MESSAGE "MAIN BAT CHGR". ACCOMPLISHED FIM PROCEDURE 31-41-00/101 SYSTEM CHECKS OK.
2005
Part: WINDOW — SMOKE (COCKPIT)
STRONG ODOR & SMOKE IN COCKPIT. CREW DECLARED AN EMERGENCY. T/S - FOUND SMOKE COMING FROM F/O FRONT WINDOW ELECT. CONNECTOR ON AFT LWR CORNER OF WINDOW. F/O FRONT WINDOW REPLACED IAW MM 56-11-01 WINDOW HEATING SYS TEST PERFORMED IAW 30-41-00-5. ALL OPS OK NO EICAS OR INOP IND'S SHOWN ALSO NO MORE SMOKE PRESENT. NOTE: WINDOW HEAT CONTROL UNIT REPLACED. REF LP 372441 ITEM 1. ALSO REPLACED WIRE & CONNECTOR ASSY REFER WDM 30-41-12 SH. 2.
Part: A/C PACK — MALFUNCTIONED (RIGHT)
INSPECTION TYPE: ETOP IN FLT FL350 M80 AFTER AND DURING TRANSMITTING NOTICE ACRID ODOR IN COCKPIT, NO OTHER INDICATIONS NOTED. COULD NOT ISOLATE OR IDENTIFY SOURCE OF ODOR 1 PACK OPS, PRIOR TO COAST OUT HF COULD NOT BE OPERATED FOR 45 MINS EVENTUALLY TO WORK, SUSPECTED FUMES. RT PACK TEMP RUNS CONTINOUS. DEFER RT PACK IAW MEL 21-51-1-0-1. M311331 REMOVED AND REPLACED RT PACK TEMP CONTROL VALVE IAW AMM 21-51-12-4. THIS CLEARS DMI M311331.
2003
Part: WIRE — FAULTY (RT ENGINE)
INSPECTION TYPE: N/A FIRE PROTECTION SYSTEM FAIL LIGHT ILLUMINATED. EICAS MSG: FIRE/OVHT SYS DISPLAYED. EICAS STATUS MSG: R ENG FIRE LP1 DISPLAYED. INDICATION APPEARED ON SHORT FINAL TO LANDING. TESTED SYSTEM, INDICATION EXTINGUISHED. REPLACED ALL WIRING FOR RT ENG OVERHEAT DETECTION AND FIRE DETECTION FROM FIREWALL TO DETECTOR IAW WDM 26-11-02 AND 26-11-21 AND EO M2000-7 889-5.
Part: PROXIMITY SENSOR — INOPERATIVE (L/E SLATS)
INSPECTION TYPE: ETOP, DIVERTED DUE TO EICAS MSG, L/E SLAT ASYM DISPLAYED, L/E LIGHT ILLUM WITH FLAP LEVER UP. EICAS MSG ILLUMINATED MULTIPLE TIMES. PSEU BITE TEST CARRIED OUT IAW FIM 32-09-03. OUTBOARD N010 PROX SENSOR 296 INDICATES INOP, PROX SENSOR REPLACED AND TESTED IAW AMM 27-88-01.
Part: FIRE DETECTOR — FALSE INDICATION (MAIN CARGO)
MAIN CARGO FIRE INDICATED, EICAS AND BELL ON T/O ROLL MOMENTARLY AT 80 KTS, THEN EXTINGUISHED. OCCURRED AFTER LANDING AND REMAINED ON BUT NO SMOKE OR FIRE PRESENT. FOUND SHRED OF SAFETY WIRE AROUND DIODE CR2 IN APU/CARGO FIRE CONT MODULE PNL AND REMOVED SAFETY WIRE SHRED. PRECAUTION REMOVED AND REPLACED AFOLTS CARD M2026 AND MAIN CARGO FIRE WARNING TEST OK PER MM 26-15-00. P/N OFF/ON 285N0028-36, S/N OFF D12060, S/N ON D10143.
1999
Part: HOUSING — BENT (CABIN)
EMERGENCY DESCENT, DEVICE HOUSING BENT, FOUND DURING ROUTINE MAINT CK OF S/N AND P/N, PREVENTED DESCENT DEVICE FROM BEING RELEASED. STRAIGHTENED HOUSING.
Part: THERMOCOUPLER — INOPERATIVE (APU)
INSPECTION TYPE:ETOP APU AIR INOP. *S/D* PERFORMED ECU BITE, FOUND NR 2 EGT LRU FAULT. REMOVED AND REPLACED RT SIDE THERMOCOUPLERS PER B767 MM 49-71-01 PAGE 401. APU CHECKS NORMAL.