N156DL
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| DELTA AIR LINES, INC. (DALA) | Operator | on 2009-10-05 | Operator named in NTSB report |
Accident & incident history
Operated by DELTA AIR LINES INC (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.
177 reports on file, 1997-12-02 – 2023-05-03.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
TAILCONE OUTER SKIN BTWN STA 1943.5-1952: DURING CONVERSION AT IAI IN TLV, MTX FOUND SEVERAL DAMAGES AND UNDICUMENTED REPAIRS ON OUTER TAILCONE SKIN. THE FOUNDS WERE: -BLEND OUTS; - WELDING REPAIRS; - LIGHTNING STRIKES; - FASTENER REPAIRS. SOME OF THESE FOUNDING ARE NOT WITHIN TOLERANCE IAW SRM 53-80-01-1A-1 AND 53-00-01-2R-8 RPR8. THE TAILCONE SKIN IS MADE FROM 321 CRES SHEET 0.025" IN THICK IAW SRM 53-80-01 ID1.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
SECTION 43 FUSELAGE SKIN STA 669.3 BETWEEN STR 35L AND STR 36L: AN EXISTING BULGE OUT OF LIMITS ON FUSELAGE SKIN WAS REPAIRED PER SRM 53-00-01 REPAIR 8.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
SEC 43 FUSELAGE SKIN, STA 600.8 BTWN STR 32L-33L: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE DENT ON FUSELAGE SKIN LOCATED AT STA 600.8 BETWEEN STR 32L AND STR 33L. INITIAL DIMENSION OF DENTED AREA A=0.680â, Y=0.027â (A/Y=25). DENT IS OUT OF LIMITS PER SRM 53-00-01, ALLOWABLE DAMAGE 1.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
DURING AIRCRAFT CARGO CONVERSION, A 0.186" DIAMETER INITIAL FASTENER HOLE WAS MISTAKENLY DAMAGED IN THE STA 1065 BULKHEAD WEB AND NO. 6 STIFFENER. THE BULKHEAD STRUCTURE IS CLASSIFIED AS PRIMARY STRUCTURE, A PSE, AND FCBS (NOTE 1) PER REF 767-300 SRM 51-00-04, STRUCTURE CLASSIFICATION.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
ENG #2, INBD SIDE CORE COWL, S/N 0982, P/N 224M4761-513: DURING NAINTENANCE INSPECTION SHOP FOUND SEVERAL LOOSE FASTENERS IN THE EXTERNAL CORE COWL SKIN ON THE INBD SIDE OF ENF #2 BETWEEN NAC STA 303.75 TO 306.75 AT 6 O'CLOCK. AFTER REMOVING THE LOOSE FASTENERS FOUND ONE LARGE HOLE (5/16" APPROX).
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
OUTBâD FAN COWL ENG #2 S/N 0424 P/N 224-2202-507. DURING MAINTENANCE CHECK AT IAI FACILITIES, SHOP DISCOVERED THE FOLLOWING FINDINGS: DENT IN THE EXTERNAL FAN COWL SKIN, COMMON TO NAC STA 182.5. 59â AWAY FROM THE BOTTOM EDGE OF THE FAN COWL. THE FIBERS ARE DAMAGED, SO A REPAIR IS NEEDED. DIMENSIONS: MAJOR AXIS LENGTH A=0.71â. DEPTH Y=0.019â. RATIO= A/Y=37. THE DISTANCE BETWEEN THE DENT AND EXISTING REPAIR IS 6.7. LARGE UNDOCUMENTED COMPOSITE REPAIRS: I. LOCATED BETWEEN NAC 144.5 AND NAC 158.5. 16â AWAY FROM BOTTOM EDGE. AREA SIZE: 14âX52â. II. LOCATED BETWEEN NAC 166.5 AND NAC 177.5. 43 AWAY FROM BOTTOM EDGE. AREA SIZE: 11X18.5. LOCATED BETWEEN NAC 177 AND NAC 187. 32.5â AWAY FROM BOTTOM EDGE. AREA SIZE: 10âX11.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
DURING MAINTENANCE INSPECTION SHOP FOUND EXISTING LATCH REPAIR DOUBLER ON THE OUTBD CORE COWL ENG #2 B/T NAC STA 267 TO 274.5 AT 6 OâCLOCK, CENTER LATCH. DURING DISASSEMBLE THE EXISTING DOUBLER, SHOP FOUND TWO (2) ELONGATED HOLES, 1 HOLE IN DIA 0.328â AND THE SECOND ONE 0.284â DIA. IN ADDITION, THESE ELONGATED HOLES ARE COMMON TO BOTH SKIN AND INNER FRAME AND FOUND DAMAGED ON BOTH PARTS.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
FUS. SKIN, SEC 48, BT STA 1809.5 â STA 1824, ABOVE STR 22L: DURING MAINTENANCE INSPECTION SHOP FOUND UNDOCUMENTED REPAIR ON THE EXTERNAL FUS SKIN, P/N 148T3181-7. A REVIEW OF THE PREVIOUS OPERATORâS RECORDS (DAL) WAS PERFORMED AND NO DOCUMENTATION WAS FOUND. THE REPAIR APPEARS TO CONFORM TO REF /E/ REPAIR. THE SKIN IS MADE FROM 7075-T6X0.100â AND CHEM-MILLED TO 0.050â MINIMUM PER REF /C/. THE SKIN IS CLASSIFIED A PRIMARY STRUCTURE, A PSE, FCBS (NOTE 1).
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
DURING CONVERSION OF S/N 25354, MAINTENANCE WAS REQUIRED TO REPLACE ENGINE #2 INLET COWL. THE REPLACEMENT INLET COWL P/N 224-2101-563, S/N 0634RV860 PROVIDED BY COSTUMER. THE NOTED INLET COWL WAS INSTALLED ON A/C AND POLISHED. MAINTENANCE REPORTED CORROSION/PITTING ON THE INLET COWL LIP AND UNDER SEVERAL FASTENER HEADS AS REPORTED IN RFTA 02905-0244. COSTUMER REQUESTED A TIME LIMITED REPAIR APPROVAL FOR 10 FLIGHT CYCLES.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
STA 139 - ATA 180.5, BELOW WINDOWS R1 AND R1: DURING MAINTANACE INSPECTION AT IAI, SHOP FOUND TWO (2) DOCUMENTED REPAIRS AT THE NOTED LOCATION. FWD REPAIR: LIGHTNING STRIKE REPAIR AT STA 139, BELOW WINDOW R1. AFT REPAIR: A DOUBLER REPAIR ON THE EXTERNAL FUS SKIN BT BS 145.5 TO 153 RBL 34 AND 3" BELOW WINDOW R1. BOTH REPAIRS ARE DOCUMENTED IN REF. /C/ NOTE: 13.4" AFT OF THE EXITING REPAIR DOUBLER, A STRUCTURAL MODIFICATION R2 WINDOW SHOULD BE INASTALLED UNDER REF. /A/REQUIREMENTS. EXISTING DOUBLER SIZE 7.5" X 18.5".
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
DURING MAINTENANCE INSPECTION AT IAI FACILITIES, SHOP DISCOVERED THE FOLLOVING FINDINGS: M0547 â AN UNDOCUMENTED DOUBLER REPAIR LOCATED BETWEEN NAC STA 286.55 AND 288.95 AT 6 O'CLOCK. SIZE: 5.6"X3.6". M0592 â AN UNDOCUMENTED DOUBLER REPAIR LOCATED (TITANIUM FAIRING AREA) BETWEEN NAC STA 288.75 AND 295.25 AT 11 O'CLOCK. SIZE: 6.5"X4.5". APPARENTLY, REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH REF. /A/.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
FUSELAGE SKIN REPAIR, BETWEEN STA 157 AND STA 162, ABOVE STR-21L: DURING MAINTENANCE CHECK, IAI SHOP DISCOVERED AN EXISTING REPAIR IN FUSELAGE SKIN LOCATED AT THE NOTED AREA. THE FLUSH REPAIR IS LOCATED IN THE EXTRA CRITICAL AREA, FWD TO THE PITOT STATIC PROBE. EXISTING FLUSH DOUBLER DIAMETER: 5.0". THICKNESS: 0.080". EXISTING FILLER DIAMETER IS 1.0".
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
SEC 46 FUSELAGE SKIN, STA 1564.3, 5â ABOVE STR 16L: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE DENT ON FUSELAGE SKIN LOCATED AT STA 1264.3, 5â ABOVE STR 16L. INITIAL DIMENSION OF DENTED AREA A=0.720â, Y=0.032â (A/Y=22). DENT IS OUT OF LIMITS PER SRM 53-00-01, ALLOWABLE DAMAGE 1.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
DURING MAINTENANCE INSPECTION, SHOP FOUND A LIGHTNING ST88IKE DAMAGE ON SKIN, AT A BUTT JOINT AT THE NOTED AREA. SHOP PERFORMED 0.4"X1.0" SIZE BLEND OUT ON THE DAMAGED AREA. AFTER NDT INSPECTIONS, IT WAS FOUND THAT THE MINIMUM THICKNESS IS 0.54", AND THE NOMINAL THICKNESS IS 0.064" â 15.625% DECREASE. THE BLEND OUT IS BEYOND LIMITS OF B767-300 SRM 53-00-01 AND NO SRM REPAIR WAS FOUND.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
SEC 46, STA 1197 â 1197=22, STR 38L -38R: UNDOCUMENTED DOUBLER REPAIR FOUND NEXT TO DOCUMENTED DOUBLER BETWEEN STA 1189 â 1197=14, STR35L â 38L, DOCUMENTED ON ERA 518660-14AD.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
STA 236.5, LBL 69.25: DURING MAINTENANCE INSPECTION SHOP FOUND FLOOR BEAM AND SHEAR WEB WITH MISSING MATERIAL.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
STRUT #2, L/H, NAC STA 285.45 TO 289.95, UNDERWING FAIRING: DURING MAINTENANCE INSPECTION AT IAI FACILITIES, SHOP DISCOVERED UNDOCUMENTED DOUBLER REPAIR.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
SECTION 41 â FUSELAGE SKIN â STA 422 BETWEEN STR 31L AND STR 32L: A BULGE OUT OF LIMITS ON THE FUSELAGE SKIN WAS REPAIRED PER SRM 53-00-01 REPAIR 8
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
STRUT #2, AFT FAIRNG - TRAILING EDGE, RH AND LH, NAC STA 410 TO 413: DURING MAINTENANCE INSPECTION AT IAI FACILITES, SHOP DISCOVERED UNDOCUMENTED DOBULER REPAIR IN STRUT #2, SKIN PANELS, ON BOTH SIDES.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
EXTERNAL FUSELAGE SKIN, STA 661, STR-30R-STR-31R: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE BULGE ON FUSELAGE SKIN LOCATED AT STA 661, 2-INCH BELOW THE STR 30R. INITIAL DIMENSION OF BULGE IS A=0.57â, Y=0.0278â (A/Y=20). BULGE IS OUT OF LIMITS PER SRM 53-00-01, ALLOWABLE DAMAGE 1.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
CORE COWL, P/N 224-2302-345, S/N 1198: DURING MAINTENANCE INSPECTION AT IAI FACILITIES. AN UNDOCUMENTED DOUBLER REPAIR LOCATED BETWEEN NAC STA 280 AND 288 AT 10 O'CLOCK. SIZE: 7.4"X4.6". M0566 â A CRACK STRETCHING FROM THE FASTENER TO THE AFT EDGE OF THE EXTERNAL CORE COWL SKIN LOCATED AT NAC STA 307,8 O'CLOCK. A CRACK STRETCHING FROM THE FASTENER TO THE EDGE OF THE EXTERNAL CORE COWL (AFT FRAME) SKIN LOCATED AT NAC STA307,7 O'CLOCK.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
R/H MLG DOOR: MAINTENANCE DISCOVERED A PUNCTURE AT THE INNER SKIN OF R/H MLG DOOR IN A CRITICAL AREA (LESS THAN 10 INCHES FROM THE CENTER HINGE). SHOP REPORTED SEVERAL DAMAGES NEAR THE NOTED PUNCTURE. ALL OTHER DAMAGES WERE REPAIRED PER SRM 52-80 REQUIREMENTS.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,805 hrs · 22,478 cycles
BT STA 1518-1562, STR 38L-37R: DURING DAMAGED SHEAR TIE P/N 140T2102U585 REMOVAL IN ORDER TO INSTALL NEW SHEAR TIE SHOP MISTAKENLY DOUBLE DRILLED THE TEAR STRAP AND SKIN AT 4EA HOLES. THE ORIGINAL HOLE DIA 0.186â. THE HOLES WERE DRILLED UNTIL THE WHOLE DAMAGE WAS REMOVED, AND HFEC INSPECTION WAS PERFORMED â NO CRACK OR OTHER DAMAGE WAS FOUND. SKIN P/N 146T3240, IS MADE FROM 0.160â CLAD 2024-T3 (CHEM-MILLED OR MASHINED TO 0.056). THERE IS NO APPLICABLE REPAIR FOR THIS DAMAGE IN SRM. P/N TREE: 146T0001-632 SECT 46 ASSY; 146T0200-19 LOWER PANEL ASSY; 146T0200-7004 COMMON PT COLLECT; 146T3240-4 SKIN PANEL ASSY; 146T3003-21 STRINGER 39L; 146T3241-12 SKIN; 146T3242-11 TEAR STRAP.
Earlier reports · 1997–2020 · 154 reports
2020
Part: BATTERY PACK — INOPERATIVE (EMEGENCY LIGHTS) · airframe 121,706 hrs · 22,151 cycles
EMERGENCY EXIT LIGHT OVER WING LEFT SIDE IS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 121,706 hrs · 22,151 cycles
EMERGENCY EXIT LIGHT SIGN AT P12 INOPERATIVE. REPLACED BATTERY. SYSTEM OPERATION IS NORMAL.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 121,554 hrs · 22,121 cycles
SHIP 1506 - ATO - ON T/O ROLL, LT YAW DAMP MESSAGE & OVERHEAD LIGHT ILLUMINATED. CORRECTIVE ACTION: INITIALLY APPLIED MEL 22-21-01. DURING RON, PERFORMED SYSTEM BITE & MCDP TESTS 30 & 40. OPERATIONAL CHECK OK. LP 7043212
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 121,511 hrs · 22,113 cycles
DURING SERVICE CHECK FOUND BACK CEILING EMERGENCY LIGHTS OUT EXTENDING FROM ROW 35A INTO AFT GALLEY. REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 121,082 hrs · 22,041 cycles
EMERGENCY EXIT SIGN AFT CEILING ARE INOPERATIVE. REPLACED BATTERY M739. SYSTEM OPERATION IS NORMAL.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 121,082 hrs · 22,041 cycles
EMERGENCY LIGHTS AT 34-40AB ON CEILING ARE INOPERATIVE. REPLACED BATTERY AT M739. SYSTEM OPERATION IS NORMAL.
2019
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 120,468 hrs · 21,922 cycles
DURING SERVICE CHECK FOUND AFT 3 LEFT EXTERNAL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM OPERATION IS NORMAL.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 120,332 hrs · 21,900 cycles
EMERGENCY FLOOR PATH LGITHS ARE INOPERATIVE AT SEAT 39B. RECONNECTED LIGHT ASSEMBLY.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 120,244 hrs · 21,886 cycles
FOUND EXTERIOR EMERGENCY LIGHT LEFT SIDE L396 AND L645 NOT ILLUMINATING DURING TEST. REPLACED BATTERY PACK ON M738. SYSTEM OPERATION IS NORMAL.
Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 120,125 hrs · 21,868 cycles
#1 PYLON OB SIDE STRUT SKIN HAS 2" CRACK ABOVE 432AL. VERIFIED WITH HFEC SCAN TAG # 6741, CREATE EWO FOR REPAIR. REPAIRED #1 PYLON OB STRUT SKIN IAW ERA 581953-14 REV O. JOB COMPLETE. (LP1321034)
Part: SKIN — CRACKED (NR 1 PYLON) · airframe 120,124 hrs · 21,867 cycles
NUMBER 1 PYLON PANEL 436CR HAS HOLE ELONGATED , CRACKED ON INNER SKIN AND SPRING SEAL WORN (M) MOORE 350206 09/09/19 (ON REPAIR RACK). REPAIRED PYLON PANEL 436CR I/A/W ERA 581311-14 REV O. (LP1316822)
Part: PANEL — CORRODED (BS 1153-1175) · airframe 120,124 hrs · 21,867 cycles
ALC BILGE PNL STA 1153-1175 LBL20-RBL20 CORROSION AT NUMEROUS PLACES. REPAIR BILGE PNAL IAW ERA 581853-14 REV O.
Part: SKIN — BENT (NR 2 NACELLE) · airframe 120,124 hrs · 21,867 cycles
NO. 2 ENG OUTBD CORE COWL 1ST LATCH HAS BENT SKIN ABOVE LATCH. MARKED. NO. 2 ENG OOUBOARD CORE COWL 1ST LATCH SKIN BENT ABOVE LATCH HAS BEEN REPAIRED PER ER/A 581524-14 REV-0 JOB COMPLETE (LP1309495)
Part: SKIN — CORRODED (BS 883) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
SKIN BENEATH STUB BEAM AT RT FUSELAGE, BS 883.5 WAS CORRODED RBL 90. REPAIRED THE SKIN IAW ERA 581549-14, REV 0.
Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
HORIZONTAL STAB CENTER BOX UPPER SURFACE SKIN CORRODED, STRINGER 3, BL 0. REPAIRED THE UPPER SKIN IAW ERA 581523-14, REV 0.
Part: FLOORBEAM — CORRODED (BS 287) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION STA 287 FLOOR BEAM RBL 75 (APPROX.) UPPER SURFACE. REMOVED, LOCATED, DRILLED, DEBURD AND INSTALL NEW T-CAP AT STA 287 RBL75, ALODINE, PRIMED AND TOP COAT IAW B767-300 SRM 53-00- 51 FIG 201 REPAIR 1, SRM 51-40-02 AND SRM 51-20-01 JOB COMPLETE. (LP1305675)
Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1219, STRINGERS 34L-33L. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1219, STRINGERS 35L-34L. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1197+110, BETWEEN STRINGERS 35L AND STR 36L. FOUND TO BE OUT OF LIMITS. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1197+88, BETWEEN STRINGERS 36R AND 37R, FOUND OUT OF LIMITS. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1219, STRINGERS 37L-36L. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1197+66, STRINGERS 36R-35R CORRODED. REPLACED SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1197, STRINGERS 38R-37R. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1197+88 BETWEEN STRINGERS 35R AND 36R, FOUND OUT OF LIMITS. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1285, BETWEEN STRINGERS 36L AND 37L. FOUND TO BE OUT OF LIMITS. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1263) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1263, BETWEEN STRINGERS 38L AND 39L, FOUND OUT OF LIMITS. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION ON THE SHEAR TIE AT BS 1285, BTW STR. 35L AND STR. 36L IS OUT OF LIMITS. REPLACED SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1219, BETWEEN STRINGERS 39L AND 39R, FOUND TO BE OUT OF LIMITS. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1197+88 BTW STR 36L AND 35L IS CORRODED OUT OF LIMITS. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1197, STRINGERS 38L-39L. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1219, STRINGERS 38R-37R. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1197+66, STRINGERS 38R-37R. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1219) · airframe 120,124 hrs · 21,867 cycles
CORRODED SHEAR TIE, BS 1219, STRINGERS 36R-37R CORRODED. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
ALC SHEAR TIE AT STA. 1285, BTW STR. 37L AND STR. 38L IS FOUND TO BE OUT OF LIMITS AND REQUIRES REPLACEMENT. REMOVED, FABRICATED, AND INSTALLED NEW SHEAR TIE AT STA 1285 STR 37L TI 38L AS NEEDED I.A.W B767-300 SRM 51-40-02 PARA 4 AND 7 AND BOEING DWG 140T2102. (LP1298287)
Part: SHEAR TIE — CORRODED (BS 1307) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE AT STA. 1307, BTW STR. 37L AND STR. 36L FOUND TO BE OUT OF LIMITS. REPLACED SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR TIE AT BS 1197, STRINGERS 36R-37R. REPLACED THE SHEAR TIE.
Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION ON THE SHEAR TIE AT BS 1197+110 BETWEEN STRINGERS 38L AND 39L. FOUND TO BE OUT OF LIMITS. REPLACED THE SHEAR TIE.
Part: ANGLE — CORRODED (BS 1261-1283) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE BILGE PANEL, BS 1261 - 1283, LBL 7-33 ANGLE NR 5, UNDER NUTPLATES. FOUND OUT OF LIMITS. REPLACED THE ANGLE.
Part: SHEAR WEB — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE SHEAR WEB BETWEEN BS 1263- 1285, RBL 12, ON THE UPPER SURFACE. REPLACED THE SHEAR WEB.
Part: ANGLE — CORRODED · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION FOUND ON THE UNDER NUPLATES ON ANGLE THAT FASTENS TO THE BILGE PANEL AND OUT OF LIMITS AND REPLACED.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE ALC STA 1219 STR 39R-38R CORRODED. REPLACED SHEAR TIE. (LP 1289577)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2SHEAR TIE AT STA 1197+132 BTW STR 36L AND 35L IS CORRODED OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1289570)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE ALC STA 1219 STR 39L-38L CORRODED. REPLACED SHEAR TIE. (LP 1289586)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE CORRODED, JUST AFT OF FLOOR BEAM/FRAME, STA. 1197+132, BTW STR. 38L TO 39L OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1289574)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE ALC CORRODED STA 1219 STR 36L-35L. REPLACED SHEAR TIE. (LP 1289609)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE AT STA 1197+132 BTW STR 37L AND 36L IS CORRODED OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1287878)
Part: NUT PLATE — CORRODED (BS 1197) · corrosion level 2 · airframe 120,197 hrs · 21,880 cycles
CORROSION LEVEL: 2 VHF ANTENNA ATTACH NUT PLATE ASSEMBLY CORRODED INSIDE AFT CARGO COMPARTMENT STA 1197+99 BL-0 REPLACED VHF ANTENNA ATTACH NUT PLATE ASSM. IN ALC STA 1197+99 BL0 (LP 1287771)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE STA 1197+44 BTW STR 38L TO 39L REQUIRES REPLACEMENT, FOUND TO BE CORRODED OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1287883)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE IN ALC AT STA 1285, BTW STR 38L AND STR 39L IS FOUND TO BE OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1287875)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE AT STA. 1307, BTW STR. 37L AND STR. 38L IS OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1287769)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE AT STA 1197+88 BTW STR 37L AND 36L IS CORRODED OUT OF LIMITS AND REPLACED. (LP 1286674)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE AT STA 1197+88 BTW STR 37L AND 38L IS CORRODED OUT OF LIMITS AND REPLACED (LP 1286665)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE AT STA 1197+88 BTW STR 38L AND 39L IS CORRODED OUT OF LIMITS AND REQUIRES REPLACEMENT. REPLACED SHEAR TIE. (LP 1286734)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE AT STA 1197+88 BTW STR 39L AND 39R IS CORRODED OUT OF LIMITS AND REPLACED. (LP 1286738)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
LEVEL 2 CORROSION: SHEAR TIE AT STA 1197+110 B/W STR 39L AND 39R FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED SHEAR TIE AT STA 1197 + 110 BETWEEN STR 39L AND 39R (LP 1286742)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORRISION LEVEL 2: SHEAR TIE ALC STA 1197+66 STR 39L-38L CORRODED. REMOVED AND REPLACED SHEAR TIE (LP 1286748)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIE AT STA 1197+88 BTW STR 38R AND 37R IS CORRODED OUT OF LIMITS AND REPLACED. (LP 1286659)
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 SHEAR TIES ARE CORRODED, JUST AFT OF FLOORBEAM/FRAME, STA 1307, BTW STR 36L TO STR 38L FOUND TO BE OUT OF LIMITS AND REPLACED. (LP 1280171)
Part: BRACE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 120,124 hrs · 21,867 cycles
CORROSION LEVEL: 2 PANEL ATTACH CROSS BRACE HAS CORR AROUND NUT PLATE, JUST FWD OF HYD SERVICE DOOR ATTACH CROSS BRACE FOUNJD TO HAVE EXFOLIGTED CORROSION AND REPLACED. (LP 1280146)
2018
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 116,879 hrs · 21,423 cycles
DURING SERVICE CHECK FOUND PASSENGER EMERGENCY LIGHTS INOPERATIVE AT ROWS 32-40AB. REPLACED POWER SUPPLY AND BATTERY PACK. SYSTEM OPERATION IS NORMAL.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 116,879 hrs · 21,423 cycles
EMERGENCY PATH LIGHTS AT ROWS 13AB TO 21 AB GOES OFF AFTER 10 SECONDS DURING TEST. REPLACED BATTERY PACK AT POWER SUPPLY . SYSTEM OPERATION IS NORMAL. (LP 5248247)
Part: SKIN — CORRODED (BS 983) · airframe 116,673 hrs · 21,396 cycles
FOUND DURING DVI LOWER WING SKIN HAS A 1 INCH CRACK AT A FASTENER AT STA. 983 STR. 9. REPAIRED PER ERA 573238-14. (LP 5141052)
Part: SKIN — CORRODED (BS 900-962) · airframe 116,673 hrs · 21,396 cycles
LEFT WING LOWER SKIN WSTA 962.2-900.2 HAS A CRACKED FASTENER HOLE AT L-9.5. C/W ERA 573238-14. (LP 5141061)
Part: CONNECTOR — DIRTY (IDG) · airframe 116,208 hrs · 21,328 cycles
JUST AFTER TOP OF DESCENT GOT A R GEN DRIVE EICAS MESSAGE 30 SECONDS LATER ALL LIGHTS WENT OUT ON THEIR OWN WITHOUT DISCONNECT, LIGHTS CAME ON AT 10K FEET. QRH C/W AND DISCONNECTED RIGHT GENERATOR DRIVE. MAINTENANCE FOUND IDG/PRESSURE SWITCH WIRING AND SERVICE IDG MESSAGES. CLEANED CONNECTORS AND SERVICED IDG. SYSTEM OPERATION IS NORMAL.
Part: LENS — MISSING (CABIN) · airframe 115,995 hrs · 21,298 cycles
EMERGENCY EXIT LENS MISSING FORWARD LEFT AISLE FORWARD GALLEY. REPLACED LENS. SYSTEM OPERATION IS NORMAL.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 115,995 hrs · 21,298 cycles
EMERGENCY LIGHTS BY BOTH AFT LAVS ARE INOPERATIVE. CHARGER ASSEMBLY M1210. SYSTEM OPERATION NORMAL.
Part: BRAKE — OVERTEMP (NR 3) · airframe 114,775 hrs · 21,139 cycles
"BRAKE TEMP" LIGHT ON AT GEAR RETRACTION #3 BRAKE SHOWED TEMP LEVEL 5. FOUND WHEEL #3 FUSE BLOWN AND BRAKE #3 DAMAGED. INSTALLED NEW WHEEL AND BRAKE. SYSTEM OPERATION NORMAL.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 113,163 hrs · 20,911 cycles
DURING SERVICE CHECK FOUND OVERHEAD EMERGENCY EXIT SIGN LEFT SIDE AT OVERWING EXIT INOPERATIVE. FOUND POWER SUPPLY M737 BAD AND REPLACED.
Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 112,697 hrs · 20,847 cycles
RIGHT MLG WW UPPER CANTED PRESSURE DECK IS CRACKED ALONG CHEM MILL LINE APPROXIMATELY 3 FT OTBD OF KEEL. COMPLIED WITH ERA 564491.
Part: HOSE — COLLAPSED (OVERWING SLIDE) · airframe 112,697 hrs · 20,847 cycles
RIGHT OVERWING SLIDE AIR SUPPLY HOSE COLLAPSED. REPLACED OVERWING SLIDE.
2017
Part: SKIN — PUNCTURED (SPOILER) · airframe 112,697 hrs · 20,847 cycles
NR 7 SPOILER LOWER SURFACE HAS A PUNCTURE. C/W ERA 564481-14.
Part: SKIN — PUNCTURED (MLG DOOR) · airframe 112,697 hrs · 20,847 cycles
LEFT MAIN LANDING GEAR DOOR HAS A PUNCTURE ON THE INNER SKIN NEXT TO THE CENTER HINGE BEAM. COMPLIED WITH ERA 564260-14.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 110,432 hrs · 20,523 cycles
LAVATORY R1 SMOKE DETECTOR AT FLIGHT ATTENDANT PANEL, L1 DOOR ON AND FLASHING CAME ON 5 MINUTES PRIOR TO LANDING NO EVIDENCE OF FIRE. RESET SMOKE DETECTOR AND PERFORMED OPS CHECK. SYSTEM OPERATION IS NORMAL.
Part: VENT — CORRODED (BS 1574) · airframe 109,865 hrs · 20,430 cycles
LEFT AFT LAVATORY VENT BS 1574 HAS CORROSION. COMPLIED WITH ERA 557063-14.
2016
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 108,274 hrs · 20,173 cycles
L3 DOOR EXTERIOR EMERGENCY LIGHT IS INOPERATIVE AND RELAMPED. SYSTEM OPERATION IS NORMAL.
Part: LIGHT — DISCONNECTED (CABIN) · airframe 104,512 hrs · 19,596 cycles
EMERGENCY LIGHTS AT SEAT 36B ARE INOPERATIVE. MAINTENANCE RECONNECTED THE LIGHT ASSEMBLY AND TESTED. SYS OPERATION IS NORMAL.
2015
Part: SKIN — DAMAGED (LT WING) · airframe 103,807 hrs · 19,484 cycles
LEFT WING WINGLET DOUBLER/TRIPLER REPAIR HOLE "M" AT WS 990.2 HAS TOOLING DAMAGE. REPAIRED IAW ERA 541225-14.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,921 hrs · 19,215 cycles
EXIT SIGN AT DOOR L1 AND R1 IS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY MODULE M1208. SYSTEM OPERATION IS NORMAL.
2013
Part: FLOORBEAM — CORRODED (BS 1197) · corrosion level 2 · airframe 94,778 hrs · 18,208 cycles
AFT CARGO FLOORBEAM FOUND CORRODED AT BS 1197 BETWEEN S36-37L. REPAIRED IAW ERA 518660-14.
Part: FRAME — CRACKED (BS 883) · airframe 94,778 hrs · 18,208 cycles
BS 883.5, RBL 89 FRAME INNER ANGLE FOUND CRACKED AT TRANSITION RADIUS.
Part: FRAME — CRACKED (BULKHEAD) · airframe 94,758 hrs · 18,203 cycles
BS 18095 BULKHEAD LT FWD OUTER FRAME, TWO CRACKS FOUND AT STR 7L, REPAIRED IAW SRM 53-80-08.
Part: FLOORBEAM — CORRODED (BS 1461) · airframe 94,758 hrs · 18,203 cycles
BS 1461, RBL 30 TO LBL 20, FLOORBEAM LOWER FLANGE CORRODED. REPAIRED BY ERA 518646-14.
Part: FAILSAFE — CRACKED (BULKHEAD) · airframe 94,758 hrs · 18,203 cycles
LEFT BS 955 REAR SPAR BULKHEAD FITTING HAS TWO CRACKS FOUND AT FAILSAFE STRAP. REPAIRED IAW ERA 515822-14AD.
Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 94,778 hrs · 18,208 cycles
BULK CARGO BAY CEILING FLOORBEAM HAS SEVERAL ANCHOR NUTS CORRODED AT BS 1480, RBL 11-36.
Part: FLOORBEAM — CORRODED (BS 1461) · airframe 94,758 hrs · 18,203 cycles
BS 1461, WL 190, RBL 32 - 52 FLOORBEAM FOUND CORRODED. REWORKED IAW SRM 53-00-51.
Part: FITTING — CRACKED (BS 955) · airframe 94,758 hrs · 18,203 cycles
LEFT BS 955 REAR SPAR BULKHEAD FITTING AREA HAS TWO CRACKS. REPLACED IAW ERA 515822-14AD.
Part: SEAT TRACK — CORRODED (BS 898-950) · corrosion level 2 · airframe 94,758 hrs · 18,203 cycles
BS 898-950, WL 200, LBL 89 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52.
Part: SEAT TRACK — CORRODED (BS 970-999) · corrosion level 2 · airframe 94,758 hrs · 18,203 cycles
BS 970-999, WL 200, LBL 89 SEAT TRACK CROWN CORRODED. REPAIRED IAW SRM 53-00-52.
Part: SEAT TRACK — CORRODED (BS 1065) · corrosion level 2 · airframe 94,778 hrs · 18,208 cycles
MAIN DECK BS 1065, WL 200, LBL 89 SEAT TRACK CROWN CORRODED. REPAIRED IAW SRM 53-00-52.
Part: FRAME — CRACKED (BS 955) · airframe 94,778 hrs · 18,208 cycles
RIGHT BS 955 REAR SPAR BEHIND FITTING AREA FOUND CRACKED AT TEE FITTING.
Part: FLOORBEAM — CORRODED (BS 1461) · corrosion level 2 · airframe 94,778 hrs · 18,208 cycles
BULK CARGO CEILING FLOORBEAM FOUND CORRODED AT SEVERAL ANCHOR NUTS BS 1461 RBL 30- LBL 20. REPAIRED IAW ERA 518646-14.
Part: FLOORBEAM — CORRODED (BS 654) · corrosion level 2 · airframe 94,758 hrs · 18,203 cycles
CORROSION ON BS 654+66, WL 200, LBL 28 FLOORBEAM. REPAIRED IAW SRM 53-00-51.
Part: FLOORBEAM — CORRODED (BS 654) · corrosion level 2 · airframe 94,758 hrs · 18,203 cycles
CORROSION FOUND ON FLOORBEAM BS 654 WL 200, RBL 21-29, FLOORBEAM REPAIRED IAW SRM 53-00-51.
Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 94,758 hrs · 18,203 cycles
CORROISION ON BS 1480 LB L28 FLOORBEAM. REPAIRED IAW SRM 53-00-51.
Part: FLOORBEAM — CORRODED (BS 654) · corrosion level 2 · airframe 94,778 hrs · 18,208 cycles
BS 654+121, WL 200, RBL 35-50 UPPER FLOORBEAM SURFACE FOUND CORRODED. REPAIRED IAW SRM 53-00-51.
Part: FLOORBEAM — MISREPAIRED (BS 654) · airframe 94,778 hrs · 18,208 cycles
MAIN DECK BS 654+44, RBL 23 AND LBL 21 FLOORBEAM MISREPAIRED. REPAIRED IAW SRM 53-00-51.
Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 94,778 hrs · 18,208 cycles
FLOORBEAM UPPER TEE CORRODED. REPAIRED IAW SRM 53-00-51.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,133 hrs · 17,511 cycles
FOUND OVERHEAD EMERGENCY LIGHTS AT SEAT 36GF INOPERATIVE. THE LIGHT ASSEMBLY WAS DAMAGED AND REPLACED. SYSTEM OPERATION IS NORMAL.
Part: WIRE — PULLED (CABIN) · airframe 87,615 hrs · 17,334 cycles
EMERGENCY LIGHTS AT SET 20AB ARE INOPERATIVE. MAINTENANCE FOUND WIRE PULLED FROM CONNECTOR AND RE-TERMINATED.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 87,096 hrs · 17,272 cycles
EMERGENCY ESCAPE PATH LIGHTS AT SEAT 38F ARE INOPERATIVE. MAINTENANCE PLUGGED IN CONNECTOR. SYSTEM OPERATION IS NORMAL.
2011
Part: PIN — DEFECTIVE (CABIN) · airframe 85,836 hrs · 17,123 cycles
EMERGENCY RED LIGHTS AT DOOR R1 ARE INOPERATIVE. MAINTENANCE REPLACED THE PIN IN THE CONNECTOR. SYSTEM OPERATION IS NORMAL.
Part: WIRE — BROKEN (CABIN) · airframe 85,504 hrs · 17,086 cycles
EMERGENCY LIGHTS AT SEAT 40B ARE INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN AND REPAIRED. SYSTEM OPERATION IS NORMAL.
Part: FAN — DAMAGED (CABIN) · airframe 83,239 hrs · 16,818 cycles
FLIGHT RETURNED TO THE GATE DUE TO A STRONG SULFUR SMELL IN THE CABIN. MAINTENANCE FOUND A DAMAGED IMPELLER ON THE RIGHT RECIRCULATION FAN RESULTING FROM CHECK VALVE FLAPPER DOOR FAILURE POSITIONED AT THE LOWER PLENUM FOR RECIRCULATION AIRFILTER. THE RIGHT RECIRCULATION FAN AND CHECK VALVE WERE REPLACED PER AMM. SYSTEM OPERATION IS NORMAL.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,110 hrs · 16,799 cycles
EMERGENCY LIGHTS ROWS 32-40AB ARE INOPERATIVE. MX REPLACED THE BATTERY CHARGER AT SEAT 38F. SYS OPS IS NORMAL.
2010
Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 81,320 hrs · 16,586 cycles
EMERGENCY PATH LIGHTS ARE SEAT 32AB ARE INOPERATIVE. MAINTENANCE REPLACED THE WALL CONNECTOR. SYSTEM OPERATION IS NORMAL. (2010-D1244) (DL76G102842).
Part: COFFEEMAKER — BURNED (GALLEY) · airframe 81,052 hrs · 16,554 cycles
COFFEEMAKER ON RT SIDE 407 EMITS SMOKE AND ELECTRICAL ODOR. CIRCUIT BREAKER PULLED FWD TO NEF, IMX REPLACED R2 COFFEEMAKER. SYS OPS IS NORMAL.
2009
Part: DRAIN — CLOGGED (EXTERIOR) · airframe 77,275 hrs · 16,087 cycles
BROWNISH SEMI SOLID PRODUCT CAME OUT NEAR 1L DOOR. DRAIN CLOGGED BELOW FLOOR LEVEL. SOLID ON FLOOR CLEANED WITH ABSORBENT FROM UPK KIT. DRAIN CLOGGED BELOW FLOOR LEVEL. BLOCKED OFF GALLEY DRAIN AND FIRST CLASS SINK SHUT OFF. FWD TO MCO AND PLACARD PER MEL 38-10-01A. CHECKED AND REMOVED DEBRIS FROM DRAIN LINES AT F/C SIDE AND F DRAIN GALLEY. CHECKED OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.
Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 76,565 hrs · 16,004 cycles
NOSE WHEEL STEERING WILL NOT STEER TO RIGHT DURING T/O OFF ROLL. REMOVED AND REPLACED STEERING METERING ASSY PER AMM. OPS AND LEAK CHECKS GOOD. MF P/N 3790037-108. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.
Part: STARTER — MALFUNCTIONED (NR 2 ENGINE) · airframe 76,565 hrs · 16,004 cycles
NR 2 START VALVE DID NOT OPEN ON CROSS BLEED OR APU START. CYCLED C/B START CONT R D-20 AS PER MC STILL DID NOT OPEN. REPLACED NR 2 ENG STARTER, RAN ENG AT GATE WITH NO PROBLEMS. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.
Part: PUMP — MALFUNCTIONED (NR 1 FUEL BOOST) · airframe 73,902 hrs · 15,704 cycles
AT FL340 DURING A CROSS FEED OPS TO CORRECT MINOR FUEL IMBALANCE THE LEFT ENG ROLLED BACK TO 52 PERCENT N1. LEFT MAIN BOOST PUMP WERE TURNED BACK ON AND X-FEED VLV CLOSED. ACFT RETRIMMED AND A/T ARM SW TURNED OFF. INITIALLY ENG WAS UNRESPONSIVE TO CHANGES IN THROTTLE POS. REFERRED TO QRH FOR ENG SURGE/STALL AS THROTTLE WAS RETARDED ENG INDICATIONS FOLLOWED NORMALLY. ALLOWED ENG TO IDLE FOR 2 MINS THEN SLOWLY ADVANCED PWR TO CRUISE THRUST. ALL INDICATIONS NORMAL. PERFORMED SUCTION TEST. ALL OK. REPLACING ENG FUEL PUMP AND PERFORMING HIGH POWER RUN. MAINTENANCE IN PROGRESS.
Part: LEAD — MISINSTALLED (NR 2 GENERATOR) · airframe 73,781 hrs · 15,690 cycles
ON RIGHT ENGINE START UP HAD FOLLOWING ELECTRICAL SYSTEM INDICATIONS RT AC BUSS OFF EICAS ON OVERHEAD R BUS TIE ISLN RBUS OFF AND RT GENERATOR CONTROL OFF. BIT BPCU FAULT WAS DP TRIP MAIN BUSS/OVERLAP ZONE. REPLACED BPCU AND RT GCU. RAN ENG NO HELP. REINSTALLED ORIGINALS. SAME MSG ON NEW BPCU. CLEARED FAULTS. FOUND RT ENG GENERATOR FEEDER LEADS PHASE A AND B SWAPPED. SWAPPED LEADS AND RAN ENG. OPS NML NO MSGS.
Part: FEEDER CABLE — DAMAGED (RT GENERATOR) · airframe 73,772 hrs · 15,689 cycles
RIGHT GENERATOR WILL NOT PICK UP BUSS, RTB, FOUND A AND B FEEDER CABLES SWAPPED AT IDG GIT BPCU FAULT WAS DP TRIP MAIN BUS/OVERLAP ZONE. REPLACED BPCU AND RT GCU. RAN ENG NO HELP. REINSTALLED ORIGINALS. SAME MSG ON NEW BPCU. CLEARED FAULTS. 185173 ROUND RT EN GENERATOR FEEDER LEADS PHASE A AND B SWAPPED. SWAPPED LEAD AND RAN ENG. OPS NML NO MSGS.
Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 73,381 hrs · 15,644 cycles
LEFT AFT MAIN FUEL PUMP LIGHT ILLUMINATED AFTER START. FOUND LT AFT MAIN PUMP CB POPPED. ACFT RELEASED AS T/S PER FIM 28-22-00-101 FIG 106A. REMOVED AND REPLACED LT AFT MAIN FUEL PUMP PER AMM. C/W CDCCL REQUIREMENTS FOR AIRWORTHINESS LIMITATION PRECAUTIONS LISTED IN AMM. BOOST PUMP OPN NML. REMOVED MCO/PLAC. PUMP P/N INST MPN 5006003D.
2008
Part: OVEN — FOD (FWD GALLEY) · airframe 73,060 hrs · 15,608 cycles
F/A IN FWD GALLEY REPORTED A LITTLE SMOKE/ELECTRICAL BURNING SMELL COMING FROM OVEN LOCATION 407. REMOVED PAPER LABEL FROM OVEN RACK. OPERATED OVEN WITH NO SMELL OR SMOKE.
Part: IDG — INTERMITTENT (NR 1 ENGINE) · airframe 72,504 hrs · 15,516 cycles
RTB DUE WHILE TAXIING FOR TAKEOFF THE LEFT ENGINE GEN DRIVE LIGHT CAME ON INTERMITTENLY WITH THE ASSOCIATED LEFT GEN DRIVE EICAS MESSAGE. REPLACED NR 1 ENG IDG AS PER AMM OP AND LEAK CKS OK MFG P/N 729825E.
Part: ENGINE — FAILED (NR 1) · airframe 68,904 hrs · 15,110 cycles
ENGINE FAILED BORO-ENGINE REPLACED.
2007
Part: FLOORBEAM — CORRODED (BS 645) · airframe 67,767 hrs · 14,975 cycles
FWD CARGO STATION 645+110 LBL 41 CARGO FLOOR BEAM UPPER CHORD CORRODED. REPAIRED ON NR APP509288 PER 53-00-07D FIGURE 801DAT HMV3/PSV17.
Part: SWITCH — FAILED (NR 2 ENGINE) · airframe 67,468 hrs · 14,940 cycles
AIR TURN BACK, DUE TO RT ENG FUEL FILTER MESSAGE. FOUND FUEL DP SWITCH BAD, REF IPC 73-34-01-06 NR 55J.
Part: FLOORBEAM — CORRODED (BS 1197) · airframe 67,468 hrs · 14,940 cycles
FOUND STA 1197+44 LBL 5 AND LBL 18 CARGO FLOORBEAM TOP SURFACE CORRODED. BEAM REPLACED PER SRM 53-00-07.
Part: FLOORBEAM — CORRODED (BS 654) · airframe 67,468 hrs · 14,940 cycles
FLOORBEAM STA654+110 LBL40"AREA CORRODED. REPLACED FLOORBEAM PER SRM 51-40-02.
Part: FLOORBEAM — CORRODED (BS 1197) · airframe 67,468 hrs · 14,940 cycles
AFT COMPARTMENT STATION 1197 AT LBL 22 CARGO LOWER FLOORBEAM TOP SURFACE CORRODED. REPAIRED PER 53-00-07 REPAIR 4 FIGURE 201 ON NON ROUTINE AMW512514.
Part: FLOORBEAM — CORRODED (BS 1197) · airframe 67,468 hrs · 14,940 cycles
AFT COMPARTMENT STATION 1197+44 LBL 43 FLOORBEAM CORRODED TOP SIDE. REPAIRED PER 53-00-07 REPAIR 4 FIGURE 201 ON NON ROUTINE AMW516960.
Part: FLOORBEAM — CORRODED (BS 654) · airframe 67,468 hrs · 14,940 cycles
FLOORBEAM CORRODED. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-00-51D.
Part: FLOORBEAM — CORRODED (BS 654) · airframe 67,468 hrs · 14,940 cycles
FLOORBEAM CORRODED. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-00-51.
Part: FLOORBEAM — CORRODED (BS 654+88) · airframe 67,468 hrs · 14,940 cycles
FLOORBEAM CORRODED. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-0051D.
Part: FLOORBEAM — CORRODED (BS 654) · airframe 67,468 hrs · 14,940 cycles
FLOORBEAM FOUND CORRODED. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM 53-51D.
Part: FLOORBEAM — CORRODED (BS 325 RBL26-54) · airframe 67,468 hrs · 14,940 cycles
FLOORBEAM UPPER CHORD FOUND CORROSION AT BS 325 RBL 26-54. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-51D.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,198 hrs · 14,791 cycles
ALL AFT UPPER EMERGENCY LIGHTS INOP. REPLACED AFT BATTERY CHARGER LIGHTS CK GOOD.
Part: AUDIO VIDEO UNIT — MALFUNCTIONED (CABIN) · airframe 65,139 hrs · 14,660 cycles
ENT SYS SHUTOFF AND BACK ON BY ITSELF. F/A INVESTIGATED AND DETECTED HOT ELECTRICAL SMELL. TURNED SYS OFF AND SMELL DISSIPATED. PULLED CB T9/T8 AS PRECAUTION. RESET CBS AND TURNED ON SYS. VMOD IMMEDIATELY EMITTED STRONG ODOR COOLING FAN NOISY AND COOLING VENTS PARTIALLY BLOCKED. REPLACED VMOD IFE SYS CKS OK. NO FURTHER ODOR NOTED. COOLING AIRFLOW UNRESTRICTED.
Part: LINE — CLOGGED (NR 1 ENGINE) · airframe 64,341 hrs · 14,560 cycles
NO THROTTLE RESPONCE TO THROTTLE MOVEMENT AFTER ENG START. ALL PARAMETERS NORMAL. FOUND BURNER PRESSURE SENSE LINE CLOGGED. CLEARED LINE, OPS CK NORMAL.
2006
Part: SPRING — BROKEN (L1 DOOR) · airframe 62,459 hrs · 14,324 cycles
L1 DOOR COUNTER BALANCE SPRING BROKEN. ITEM FORWARDED TO MCO. REMOVED L1 DOOR COUNTER BAL. INSTALLED L1 DOOR COUNTER BALANCE ASSY PER MM. REPLACED L1 DOOR ROTOR ACTUATOR PER MM. MCO/PLAC REMOVED.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,357 hrs · 14,199 cycles
EMERGENCY LIGHT AFT OF LEFT WING INOP. RELAMPED, CKS GOOD.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 61,124 hrs · 14,173 cycles
EXTERIOR EMERGENCY LIGHTS INOP AT L2 DOOR AND FIRST LIGHT AFT OF LT WING. RELAMPED, CHECKS GOOD.
Part: SHUTOFF VALVE — FAULTED (NR 1 ENGINE) · airframe 60,823 hrs · 14,135 cycles
AFTER ENGINE START LEFT ENGINE BLEED WOULD NOT OPEN. BITE CHECK ASCM - FAULTED L PRSOV. RESET BLEED AIR AND ASCM RAN ENGINE AT GATE PER PFHB. LEFT ENGINE BLEED AIR CHECKS NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,545 hrs · 14,101 cycles
EXTERIOR EMERGENCY LIGHTS AT LEFT AFT DOOR INOP. REPLACED EMERGENCY LIGHTS BATTERY PACK AT M738. EMERGENCY LIGHTS CHECK GOOD.
2005
Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 58,526 hrs · 13,844 cycles
RADAR DISPLAY SHOWING NOTHING BUT GREEN AND YELLOW ON SCREEN REGARDLESS OF TILT. REMOVED AND REPLACED R/T IAW MM, ALL OPS CHECK OK.
Part: ANTENNA — FAILED (WX RADAR SYS) · airframe 58,506 hrs · 13,841 cycles
WXR RADAR INOP ANTENNA FAULT MESSAGE RIGHT HALF DISPLAY BLANK WITH NO WXR. REMOVED AND REPLACED WXR ANTENNA ASY IAW M/M OPS CHECKS GOOD.
Part: ADC — FAILED (LEFT) · airframe 58,069 hrs · 13,781 cycles
L ADC COMPUTER FAILED. LGW MTCCA, REPLACED L ADC A/C MM 34-12-01-404-006. OPS CHKS SATISFACTORY.
Part: SKIN — DAMAGED (LT AILERON) · airframe 57,568 hrs · 13,716 cycles
SPARE REMOVED FROM A/C 1506. LT OTBD AILERON UPPER SKIN, LOWER SKIN, CORE AND TAILING EDGE WEDGE DAMAGED AT WS 1025. A NEW SECTION OF CORE WAS INSTALLED, UPPER AND LOWER SKINS REPAIRED WITH REPAIR PLIES AND ADDED PLIES AND TRAILING EDGE WEDGE SPLICED IN.
2004
Part: CONTROLLER — FAILED (E/E BAY) · airframe 52,497 hrs · 12,948 cycles
CAPT FWD WINDSHIELD STARTED TO SMOKE ACCOMPANIED WITH FUMES. BOTTOM LEFT CONNECTOR MELTED, FOUND J5 CONNECTOR AT L1 WINDOW BURNT, WINDOW NOT DAMAGED. REPLACED WINDSHIELD HEAT CONTROLLER.
2003
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 47,986 hrs · 12,232 cycles
COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSY.
2002
Part: SENSOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 43,628 hrs · 11,493 cycles
RIGHT ENGINE SLOW TO SPOOL DOWN FROM CRUISE POWER TO IDLE SETTING. TOOK ABOUT 20-30 SECS FOR ENGINE TO SPOOL DOWN. EMERGENCY EQUIPMENT CALLED OUT, BUT NO EMERGENCY DECLARED. NR 2 ENG CIT SENSOR REMOVED. REPLACED NR 2 ENGINE CIT SENS PER M/M. LEAK CKS OK, PERFORMED TEST 2 AND 3 PER PFHB TESTS.
Part: ENGINE — VIBRATION (NR 2) · airframe 42,876 hrs · 11,343 cycles
ON TAKEOFF ROLL, THE RIGHT ENGINE VIB INDICATED A 5.0 (LPT). TAKEOFF ABORTED AT 80 KNOTS INDICATED AIRSPEED. ALL OTHER ENGINE PARAMETERS ARE NORMAL. T/S PER FIM 71-05-00. CHIP DET CHECKED, CLEANED ACCEL CONNECTOR, LUBED FAN BLADES. PERFORMED VIBRATION SURVEY R/U PER PFHB. ALL VIBS WITHIN LIMITS.
2001
Part: IDG — MALFUNCTIONED (LT ENGINE) · airframe 41,762 hrs · 11,165 cycles
FLT 83/17 NCE/JFK DIVERTED YQX DUE APU FAULTED. AFTER IT WAS STARTED DUE THE LT IDG DRIVE LIGHT AND THE LT IDG WAS DISCONNECTED. A/C LANDED SAFELY AT YQX. THE APU WAS SERVICED AND THE LT IDG WAS PLACED ON MCO. A/C RELEASED PER MEL.
Part: COVER — TORN (LIFE VEST) · airframe 40,951 hrs · 11,032 cycles
FOUND 65 LIFE VEST PROTECTIVE COVERS TORN THROUGH OUT THE CABIN. REPLACED 65 LIFE VESTS THROUGH OUT THE CABIN AS REQUIRED.
Part: FITTING — CRACKED (NR 1 PYLON) · airframe 40,868 hrs · 11,019 cycles
THE INBOARD FITTING ON THE NR 1 PYLON WAS FOUND WITH CRACKS IN THE TYPICAL LOCATION AS SHOWN IN S/B 767-54-0081.
Part: RADAR — FAILED (WEATHER RADAR) · airframe 39,459 hrs · 10,816 cycles
AIR TURN BACK WEATHER RADAR INOP WEATHER RADAR FAULT ON. REPLACED R/T AND ANTENNA PER M/M POS CHECKS GOOD
Part: IDG — FAILED (NR 2 ENGINE) · airframe 38,483 hrs · 10,658 cycles
RIGHT GEN DRIVE LIGHT FLICKERED TWICE, 30 MIN LATER LIGHT ON STEADY. IAW POM, DISCONNECTED RT GEN DRIVE. APU STARTED AT FL310. REMOVED AND REPLACED RT IDG. RUNUP AND OPS CHECK OK.
2000
Part: COMPRESSOR — INOPERATIVE (FUSELAGE) · airframe 35,160 hrs · 10,090 cycles
PRIOR TO BOARDING STRONG SMELLY SMOKE POSSIBLE ELECTRICAL WAS NOTED BY FLT ATTENDANT IN RT REAR OF CABIN. FOUND WATER COMPRESSOR FROZEN AND C/B POPPED AND MELTED PLASTIC INSIDE HOUSING. REPLACED COMPRESSOR.
Part: BATTERY — OVERHEATED (APU) · airframe 35,148 hrs · 10,087 cycles
APU BATTERY SMOKING. REPLACED BATTERY, OPS NORMAL.
1999
Part: FAN — FAILED (CARGO BAY)
FWD EQUIP EX FAN STATUS MSG PRECEDED BY SOUND OF MOTOR WINDING DOWN AND SMOKE IN COCKPIT. C/B H-20 OPENED/POPPED. SMOKE DISSIPATED.
Part: WIRE — SHORTED (FWD GALLEY)
ELECTRICAL ARC NOTED SEVERAL TIMES IN FORWARD GALLEY RT SIDE NEAR DRAIN SHUT-OFF VALVE. FOUND FEEDER WIRE TO FWD GALLEY SUPPLY SIDE RIBBON HEATER B109 SHORTED TO GALLEY STRUCTURE. REPAIRED AND REROUTED WIRE, TRIM REINSTALLED IPC REF 30-71-02 PG 106 SHEET 1.
1998
Part: SKIN — DAMAGED (BS 22)
THE FUSELAGE SKIN SUFFERED A LIGHTNING STRIKE AT A SKIN LAP SPLICE AT STA 220 AND WL 188. THE DAMAGE RESULTED IN A SMALL (APPROX 1) CUTOUT IN THE UPPER SKIN PANEL OF THE SKIN LAP. THE DAMAGE WAS REPAIRED WITH A DOUBLER INSTALLED PER THE B767 SRM 53-00-01, FIG 201 AND DOCUMENTED PER ER/A 363602-14.
1997
Part: POWER SUPPLY — INOPERATIVE (CABIN)
DURING SERVICE CHECK, F/C AND B/C EMERGENCY LIGHTS FAILED TEST. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATION TEST SATISFACTORY.