N741AX
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
AIRBORNE/PEMCO NON-ROUTINE 2387N2380 DISCREPANCY: AFT CARGO STRINGER 36R HAS CORROSION AT STA-1355. CORRECTIVE ACTION: REMOVED, FABRICATED AND REPLACED STRINGER SECTIONS IAW B767-200 SRM 51-40-02 AND SRM 53-00-03, REPAIR 2 TYPE III.
AIRBORNE/PEMCO NON-ROUTINE 2768N93 DISCREPANCY: P/R-MESA SUPPORT TASK; #2 ENGINE INLET COWL REPAIR AT 5:30 POSITION (AFT LOOKING FWD) REQUIRES ENGINEERING EVALUATION REF FVCI EO 20113-2 CORRECTIVE ACTION: COMPLIED WITH FVCI E.O. 20113-2 (ATTACHED SEE ATTACHED 8110-3)
AIRBORNE/PEMCO NON-ROUTINE DISCREPANCY: CORROSION ON AFT CARGO FRAME WEB STA-1270 AFT FACE BETWEEN STR-29R AND STR-32R. CORRECTIVE ACTION: REMOVED, FABRICATED WEB (7075-T6 .100) AND SPLICE PLATE (7075-T6 .125), INSTALLED WEB AND SPLICE PLATE. REMOVED AND REINSTALLED SEAL DEPRESSOR, DOOR STOP FITTINGS, SUPPORT BRACKETS AND "L" ANGLES AT STA-1270 STR-28R - STR-32R. ALL WORK ACCOMPLISHED IAW B767-200 SRM 51-40-02, 51-10-02, 51-40-05, 51-40-04, 51-20-01, SOPM 20-41-02 AND F.V.C E.O.#19309.
AIRBORNE/PEMCO NON-ROUTINE 2387N316 DISCREPANCY: FWD CARGO STRINGER 39R FROM FWD FACE BULKHEAD TO STA-764. CORRECTIVE ACTION: REMOVED, FABRICATED AND REPLACED STRINGER SECTION AT FWD CARGO BETWEEN STA-730 - STA-784 S-39R IAW B767-200 SRM 53-00-03 REPAIR 2. AND SRM 51-40-02.
AIRBORNE/PEMCO NON-ROUTINE 2387N2956 DISCREPANCY: SEAT TRACK FLANGE AT LBL-78 CORRODED FROM STA-1087 - STA-1109 ON I/B SIDE. CORRECTIVE ACTION: REMOVED, FABRICATED, AND INSTALLED SEAT TRACK SECTION FROM STA-1087 - STA-1109, LBL-78 IAW B767 SRM 51-40-02, 51-40-05 AND 53-00-52.
AIRBORNE/PEMCO NON-ROUTINE 2387N498 DISCREPANCY: AFT LOWER CARGO HAS CORROSION APROX. S-36 STA-1131 BELOW POWER DRIVE 1R INTERNAL. CORRECTIVE ACTION: REMOVED, FABRICATED AND INSTALLED AFT CARGO STRINGER 36R BETWEEN STA 1087 TO STA 1143 IAW B767-200 SRM 53-60-03 FIG.201, PG 201 AND B767-200 SRM 53-00-03 REPAIR 2.
AIRBORNE/PEMCO NON-ROUTINE 2387N2078 DISCREPANCY: CORROSION ON AFT CARGO DOOR SILL WEB STA-1270 - STA-1285, STR-33 R/H. CORRECTIVE ACTION: REMOVED, FABRICATED NEW WEB IAW FVCI E.O.# 19544 AND INSTALLED IAW BOEING 767-200 SRM 51-40-02.
AIRBORNE/PEMCO NON-ROUTINE 2387N3148 DISCREPANCY: AFT CARGO, STRINGER 39R AND STRINGER SPLICE CORRODED AT APPROX STA-1287 - STA-1307. CORRECTIVE ACTION: REMOVED, FABRICATED, REPLACED STRINGER AND STRINGER SPLICE AT 39R AT STATION 1287 - 1307 IAW B767-200 SRM 51-40-02, 51-40-05, AND 53-00-03 TYPE III, REPAIR 2.
AIRBORNE/PEMCO NON-ROUTINE 2387N1601 DISCREPANCY: CORROSION ON STRINGER 36L FROM STA-434 - STA-478. CORRECTIVE ACTION: REMOVED, FABRICATED, INSTALLED REPAIRS AT STA-434 - SAT-478, STR36L IAW B767-200 SRM 51-40-05, 53-00-03 REPAIR 2, E.O.#19330 REV.A AND E.O.#19365.
AIRBORNE/PEMCO NON-ROUTINE 2387N608 DISCREPANCY: EXTERNAL SKIN CORRODED BENEATH DOUBLER STATION 1285, STR-36R. CORRECTIVE ACTION: EXTERNAL FUSELAGE SKIN AT STA-1285, STR-36R REPAIR ACCOMPLISHED ON N/R CARD 2387N2744 AND E.O. PD67-53-070.
AIRBORNE/PEMCO NON-ROUTINE 2387N2744 DISCREPANCY: AFT CARGO DOOR CUT-OUT BEAR STRAP CORRODED STA-1250 - STA-1307, STR-38R - STR-31R. REQUEST EA. CORRECTIVE ACTION: COMPLIED WITH AFT CARGO DOOR CUT-OUT BEAR STRAP (REPAIR) STA-1250 - STA-1307, STR-38R - STR-31R IAW E.A.# PD67-55-070.
AIRBNORNE/PEMCO NON-ROUTINE 2387N3147 DISCREPANCY: AFT CARGO WEB BETWEEN STA-1285 - STA-1329 LBL 35-38. CORRECTIVE ACTION: REMOVED, FABRIACATED AND REPLACED AFT CARGO WEB BETWEEN STA-1285 - STA-1329 LBL 35-38 IAW B767-200 SRM 51-40-02, 53-60-53,51-30-01.
AIRBORNE/PEMCO NON-ROUTINE 2387N3163 DISCPREPANCY: AFT CARGO STRINGER 39L IS CRACKED APPROX. AT STA 1307. CORRECTIVE ACTION: REMOVED CRACKED STRINGER 39L, FABRICATED, AND INSTALLED STRINGER REPAIRS AT STA-1253 - 1275 AND STA-1307 - 1329 IAW B767-200 SRM 53-00-03. REPAIR #2 FIG. 201 SHT 5 TYPE III.
AIRBORNE/PEMCO NON-ROUTINE 2387N3078 DISCREPANCY: AFT CARGO FRAME WEB CRACKED AT STA-1153 RBL-18. CORRECTIVE ACTION: REMOVED, FABRICATED, AND INSTALLED FRAME WEB AT AFT CARGO STA-1153, RBL-44 TO LBL-44 IAW B767-200 SRM 51-40-05, 51-30-01 AND 51-40-02.
AIRBORNE/PEMCO NON-ROUTINE 2387N1528 DISCREPANCY: AFT CARGO BEAR STARP CORRODED AT STA.1285 - STA-1307, STR-34R STR-35R. CORRECTIVE ACTION: BEAR STRAP FROM STA 1250 - STA-1307 AND STR-32R -STR-38R WAS REPAIRED ON N/R 2387N2744 AND IAW E.A.#PD67-53-070.
AIRBORNE/PEMCO NON-ROUTINE 2387N3013 DISCREPANCY: RIGHT WING, APPRX WS-933 UPPER SPAR T/E SPAR CORRODED. CORRECTIVE ACTION: COMPLIED WITH FLIGHT VEHICLES CONSULTING INC.. E.O.# 19552 REV.B FOR RIGHT WING , APPROX WS-933 UPPER SPAR T/E SPAR.
AIRBORNE/PEMCO NON-ROUTINE 2387N3014 DISCREPANCY: RIGHT WING STA-933 LOWER SPAR T/E SPAR CORRODED. CORRECTIVE ACTION: REPAIRED IAW F.V.C E.O.#19553 REV.IR.
AIRBORNE/PEMCO NON-ROUTINE 2387N2982 DISCREPANCY: AFT CARGO STRINGER 36R CORRODED BETWEEN STA-1373 - STA-1461. CORRECTIVE ACTION: REMOVED AND REPLACED AFT CARGO STRINGER 36R BETWEEN STA-1373 - STA-1461 IAW B767-200 SRM 53-00-03.
AIRBORNE/PEMCO NON-ROUTINE 2387N2980 DISCREPANCY: R/H WING, T/E UPPPER SPAR AT APPRX WS-442 HAS CORROSION. CORRECTIVE ACTION: REMOVED CORRSION AT R/H WING UPPER T/E SPAR WS-442 AND REPAIRED IAW E.O.#19350.
AIRBORNE/PEMCO NON-ROUTINE 2387N3191 DISCRPANCY: WHILE ACCOMPLISHING N/R 2387N2982 FOUND PREVIUOS DAMAGE AT STA-1395 - STA-1415, STR-36R. DAMAGE WAS COVERED UP WITH BONDO. CORRECTIVE ACTION: REWORKED AND REPAIRED AREA AT AFT CARGO EXTERNAL FUSELAGE SKIN BETWEEN STA-1395 - STAS-1415, STRINGER 36R IAW F.V.C E.O# 20038 REV. IR
AIRRBORNE/PEMCO NON-ROUTINE 2387N2976 DISCREPANCY: FWD CARGO STR-36L CORRODED AT APPROX STA-594. CORRECTIVE ACTION: REMOVED DAMAGED STRINGER SECTION AND INSTALLED STRINGER REPAIR AT STA-578 -STA-600 IAW SRM 53-00-03 REPAIR 2 DETAIL III.
AIRBORNE/PEMCO NON-ROUTINE 2387N2965 DISCRREPANCY: FWD CARGO STRINGER 35R CORRODED AT STA-780. CORRECTIVE ACTION: REMOVED DAMAGE STRINGER SECTION AND INSTALLED STRINGER REPAIR IAW B767-200 SRM 53-00-03 REPAIR #2 DETAIL III.
AIRBORNE/PEMCO NON-ROUTINE 2387N2950 DISCREPANCY: AFT CARGO, STR 37R HAS CORROSION AT STA.1297. CORRECTIVE ACTION: REMOVED, FABRICATED AND REPLACED 37R AT STATION 1297 IAW B767 SRM 53-00-03 REPAIR 2.
AIRBORNE/PEMCO NON-ROUTINE 2387N3021 DISCREPANCY: DURING "OK TO INSTALL" L/H AILERON FOUND CORROSION ON WING REAR SPAR UPPER CAP AT W.S.906.2 FWD OF AILERON I/B MOST HINGE FITTING. CORRECTIVE ACTION: REMOVED CORROSION ON L/H AILERON ON WING REAR UPPER SPAR CAP AT W.S. 906.2 FWD OF AILERON I/B MOST HINGE FITTING IAW SRM 57-51-02. MATERIAL 0.120, MATERIAL LOSS 0.050, REMAINING MATERIAL THICKNESS 0.070. FOUND TO BE OUT-OF-LIMITS IAW B767-200 SRM 57-51-02. REPAIRED IAW E.O.#19560.
AIRBORNE/PEMCO DISCREPANCY: CORROSION ON AFT CARGO SILL WEB STA-1270 - STA-1285, STR-33 R/H. CORRECTIVE ACTION: REMOVED, FABRICATED NEW WEB IAW FVCI E.O. 19544 AND INSTALLED IAW BOEING 767-200 SRM 51-40-02.
AIRBORNE/PEMCO NON-ROUTINE 2387N3190 DISCREPANCY: MAIN CABIN FRAME OUTTER FLANGE AT STA-1480, STR-18 R/H IS CORRODED. CORRECTIVE ACTIN: REMOVED CORROSION AT MAIN FRAME STA-1480, FOUND TO OUT-OF-LIMITS IAW SRM 53-00-07 FIG.101. REMOVED, FABRICATED AND INSTALLED NEW FRAME AT MAIN CABIN STA 1480 IAW SRM 51-40-02, TRAVELERS NR#2387N3228/NR#2387N3229.
AIRBORNE/PEMCO NON-ROUTINE 2387N318 DISCREPANCY: FWD CARGO-LOWER BILGE AREA CORRODED AT STA 698 BETWEEN S36R-S35R. CORRECTIVE ACTION: REWORKED AND REPAIRED AREA AT FWD CARGO - LOWER BILGE STA 698 S36R-S35R IAW B767-200 SRM 53-00-01 REPAIR 12.
AIRBORNE/PEMCO NON-ROUTINE 2387N314 DISCREPANCY: FWD CARGO STRINGER CORRODED, FWD OF BULHEAD STA 764 AT S36R. CORRECTIVE ACTION: REMOVED AND REPLACED DAMAGE STRINGER S36R FROM STA-638 TO STA-784 IAW B767-200SRM 53-00-03 REPAIR #2 AND E.O. 47359REA10.
AIRBORNE/PEMCO NON-ROUTINE 2768N42 DISCREPANCY: (PR 604284) BULK CARGO EXISTING REPAIR AT STA 1394 TO STA 1407 BETWEEN S25R TO 27R REQUIRES ENGINEERING EVALUATION CORRECTIVE ACTION: BULK CARGO EXISTING REPAIR @ STA 1394 TO STA 1407 BETWEEN S25R TO 27R WAS FOUND TO BE INCORRECT PER B767 SRM 53-00-01 REPAIR 33 AND CORROSION WAS FOUND ON OUTER SURFACE OF DOUBLER, TRIPLER, AND FILLER. REMOVED AND REPLACED IAW B767 SRM 53-00-01 REPAIR 33
AIRBORNE/PEMCO NON-ROUTINE 2387N2408 DISCREPANCY: FUSELAGE UPPER AND LOWER SKIN STR 36R LAP SPLICE CORRODED BETWEEN STA-566 - STA-654. CORRECTIVE ACTION: INSTALLED REPAIR AT FUSELAGE UPPER AND LOWER SKIN 36R LAP SPLICE IAW B767 SRM 53-00-01.
AIRBORNE/PEMCO NON-ROUTINE 2387N2186 DISCREPANCY: MAIN DECK STA-786 - STA-996, RBL-74.75, CORRODED SEAT TARCK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE , REMOVED DAMAGE AND INSTALLED REPAIRS IAW E.O.# CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2192 DISCREPANCY: MAIN DECK STA-786 - STA-996, LBL-54.75, CORRODED SEAT TRACK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE, REMOVED DAMAGE AND REPAIRED AT DECK STA-786 - STA-996. LBL 54.75 SEAT TARCK, O/B FLANGE L=10FT W=1.25, I/B FLANGE L=6FT W=1.40, AFT I/B FLANGE IAW BOEING 767-200 E.O. #CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2745 DISCREPANCY: AFT CARGO DOOR CUTOUT BEAR STRAP STA-1340 - STA-1360, STR-34R -STR-33R, CORRODED. CORRECTIVE ACTION: REPAIRED BEAR STRAP AT STA-1340 - 1360 FROM STR-36R - STR-33R IAW E.A. PD67-53-071 REV.NC.
AIRBORNE/PEMCO NON-ROUTINE 2387N2191 DISCREPANCY: EVALUATED DAMAGE, REMOVED DAMAGE AND REPAIRED AT MAIN DEACK STA-786 - STA-996, LBL 33, I/B FLANGE (2 EACH)L=7FT 6IN W=1.25, L=8FT 6IN W= 1.25 O/B FLANGE L=9IN W=1.25, L=6FT W=1.25 IAW E.O.#CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2190 DISCREPANCY: MAIN DECK STA-786 - STA-996, LBL 11, CORRODED SEAT TRACK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED REWORK DAMAGE AT SEAT TRACK FLANGE, FOUND TO BE OUT -OF -LIMITS, REPAIRED MAIN SEAT TRACK FLANGE I/B AND O/B AT STA 786 - STA 996, LBL 11 IAW E.O.# CS-22213-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2189 DISCREPANCY: MAIN DECK STA-786 - STA-996, RBL-11, CORRODED SEAT TRACK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE, REMOVED DAMAGE AND INSTALLED REPAIRS IAW E.O.#CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2188 DISCREPANCY: MAIN DECK STA-786 - STA-996, RBL 33, CORRODED SEAT TRACK OUT-OF-LIMITS. CORRECTIVE ACTION EVALUATED DAMAGE, REMOVED DAMAGE AND INSTALLED REPAIRS IAW E.O.#CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2187 DISCREPANCY: MAIN DECK STA-786 - STA-996, RBL 54.75, CORRODED SEAT TARCK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE, REMOVED DAMAGE AND INSTALLED REPAIRS IAW E.O.#CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2066 DISCREPANCY: FWD CARGO , STA-538, STR-34R, FRAME LOWER CHORD CORRODED. CORRECTIVE ACTION: REPAIRED DAMAGE AT FWD CARGO, STA-538, STR-34R, FRAME LOWER CHORD IAW FVCI E.O.#19319 REV.A.
AIRBORNE/PEMCO NON-ROUTINE 2378N2195 DISCREPANCY: MAIN DECK STA-996-STA-1068, RBL-74.75, CORRODED SEAT TRACK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE, REMOVED DAMAGE AND REPAIRED IAW E.O.# CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2193 DISCREPANCY: MAIN DECK, STA-786 - STA-996, LBL 74.75, CORRODED SEAT TRACK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE, REMOVED DAMAGE AND REPAIRED AT THE MAIN DECK STA-786 - STA 996, LBL 74.75 SEAT TARCK O/B FLANGE L=2FT 5IN, W=1.40IN , I/B FLANGE L=8FT W= 1.25 IAW 767-200 E.O.# CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2196 DISCREPANCY: MAIN CABIN STA-996-STA-1068, RBL-54.75, CORRORED SEAT TRACK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE, REMOVED DAMAGE , INSTALLED REPAIRS IAW E.O.# CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2197 DISCREPANCY: MAIN DECK STA-966-STA-1068, RBL-33, CORRODED SEAT TRACK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE, REMOVED DAMAGE AND INSTALLED REPAIRS IAW E.O.# CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2199 DISCREPANCY: MAIN DECK STA-996-STA-1068, LBL, CORRODED SEAT TRACK OUT OF LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE, REMOVED DAMAGE AND REPAIRED THE MAIN DECK STA-996 TO STA-1068, LBL11 SEAT TRACK, O/B FLANGE L= 6FT 7IN W= 1.25, I/B FLANGE L= 5FT 6IN W=1.25 IAW BOEING 767-200 E.O. CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2200 DISCREPANCY: EVALUATED DAMAGE, REMOVED DAMAGE AND REPAIRED THE MAIN DECK STA-996 -STA-1068, LBL-33, L= 6FT 7IN, W= 1.25IN IAW B767-200 E.O.#CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2181 DISCREPANCY: MAIN DECK STA-445 - STA-664, RBL-73.80, CORRODED SEAT TRACK OUT OF LIMITS. CORRECTIVE ACTION: REMOVED CORROSION FROM MAIN DECK STA-445-STA-664 RBL 73.80 SEAT TRACK IAW B767 SRM 51-10-02. EVALUATED LIMITS AND FOUND TO BE OUT OF LIMITS AT STA-630 RBL 73. INSTALLED SEAT TRACK REPAIR STRAP IAW B767 E.O.# 19568 REV:IR AND SRM51-40-02.
AIRBORNE/PEMCO NON-ROUTINE 2387N2461 DISCREPANCY: FWD PIT STA 583 (APPROX) S22LH CORRODED AFT DOME NUT MOUNTING PLATE. CORRECTIVE ACTION: REMOVED DOME NUT PLATES IAW B767-200 SRM 51-40-02. REMOVED CORRSION AT STA 583 LBL 90 IAW B767-200 SRM 51-10-02. PERFORM REPAIR IAW E.O. CS-22215-008.
AIRBORNE/PEMCO NON-ROUTINE 2387N2336 DISCREPANCY: FWD CARGO STA 764-784 STR 37R, STRINGER CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER 37R BETWEEN STA 730-784 IAW B767 SRM 53-00-03 REPAIR 2 DETAIL III AND EA 47089SSR01IR.
AIRBORNE/PEMCO NON-ROUTINE 2387N2383 DISCREPANCY: L/H WHEEL WELL UPPER O/B LONGERON STA.970 CHORD CORRODED UPPER FLANGE. CORRECTIVE ACTION: REMOVED CORROSION UPPER FLANGE AT LONGERON IN WHEEL WELL UPPER O/B. REPAIRED IAW E.O. 19562.
AIRBORNE/PEMCO NON-ROUTINE 2387N2202 DISCREPANCY: MAIN DECK STA 996-1063 LBL 74.75 CORRODED SEAT TRACK OUT OF LIMITS. CORRECTIVE ACTION: REMOVED DAMAGE AND AFTER FUTHER EVALUATION OF I/B AND O/B FLANGE LBL 74.75 FROM STA 996 TO STA 1063 APPROX IS WITHIN ALLOWABLE LIMITS MAT .090, MAT REMAINING .077, MAT LOSS .013 IAW SRM 53-00-52, DETAIL III E.O.#CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2387N2066 DISCREPANCY: FWD CARGO, STA 538, STR 34R, FRAME LOWER CHORD CORRODED. CORRECTIVE ACTION: REPAIRED DAMAGE AT FWD CARGO , STA 538, STR 34R, FRAME LOWER CHORD IAW E.O.#19319 REV.A.
AIRBORNE/PEMCO NON-ROUTINE 2387N2201 DISCREPANCY: MAIN DECK STA 996-1068, LBL 54.75, CORRODED SAET TARCK OUT OF LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE, REMOVED CORROSION AND REPAIRED MAIN DECK STA 996-1068, LBL 54.75 SEAT TRACK O/B FLANGE L= 2FT 8IN, W= 1.40IN IAW BOEING 767-200 E.O.#CS-22215-009.
AIRBORNE/PEMCO NON-ROUTINE 2378N2337 DISCREPANCY: FWD CARGO STRINGER 36R CORRODED AT STA 588. CORRECTIVE ACTION: REMOVED AND REPLACED CORRODED STRINGER AT STA 588 36R IAW B767 SRM 51-40-02, 51-40-05 AND EA 47089SSR01IR.
AIRBORNE/PEMCO NON-ROUTINE 2387N1580 DISCREPANCY: STRINGER 33L STATION 720 HAS CORROSION. CORRECTIVE ACTION: REPAIRED STRINGER 33L AT FWD CARGO, STATION 720 IAW B767-200 SRM 53-00-03 AND PD67-53-066.
AIRBORNE/PEMCO NON-ROUTINE 2387N1525 DISCREPANCY: AFT CARGO FRAME CORRODED AT STA.1270, STR 29-30 R/H. CORRECTIVE ACTION: REMOVED CORROSION AT CARGO FRAME AT STA 1270, STR29-30 RH. EVALUATED REWORK AREA AND FOUND TO BE WITHIN LIMITS IAW B767-200 E.O.19364.REV IR.
AIRBORNE/PEMCO NON-ROUTINE 2387N1638 DISCREPANCY: SKIN CORRODED @ STA 1351-1373 STR 26 R/H LAP JOINT AREA. CORRECTIVE ACTION: REMOVED CORROSION @ STA 1351-1373 STR 26 R/H LAP JOINT FOUND TO BE OUT OF LIMITS IAW 53-00-01. FABRICATED REPAIR PARTS AND INSTALLED AT STA 1351-1373 STR 26 IAW E.O.# 230022.
AIRBORNE/PEMCO NON-ROUTINE 2378N342 DISCREPANCY: CORROSION ON FWD CARGO DOOR LWR SILL FRAME BETWEEN STA. 610 AND 632, STARTS ABOUT 2.5 INCHES AFT OF AFT VERTCAL ROLLER. CORRECTIVE ACTION: REMOVED AND FABRICATED ANGLE IAW B767 SRM 51-40-02 AND E.O.#14788.
AIRBORNE/PEMCO NON-ROUTINE 2387N378 DISCREPANCY: 3 GOUGES ON LH FUSALAGE OUTER SKIN AT STA 785.9 APPROX. S30L. REPAIRED L/H OUTER FUSELAGE SKIN AT STA 785.9 APPROX S30L IAW IAW EA #47359REA04.
AIRBORNE/PEMCO NON-ROUTINE 2387N375 DISCREPANCY: FWD FUSELAGE WATER DRAIN SERVICE PANEL CORRODED. CORRECTIVE ACTION: REPAIRED FWD FUSELAGE WATER DRAIN SERVICE PANEL IAW AMES EA47359REA14.
AIRBORNE/PEMCO NON-ROUTINE 2387N385 DISCREPANCY: CORROSION ON BULKHEAD STA 955 RIGHT WHEEL WELL BELOW WING SPLICE PLATE FITTING. CORRECTIVE ACTION: REMOVED CORROSION AND REPAIRED STA.955 RBL 97 CENTER AFT SPAR LOWER CHORD IAW AIRBORNE/PEMCO EA 57-67-019.
AIRBORNE/PEMCO NON-ROUTINE 2387N510 DISCREPANCY: R/H KEEL BEAM ST-676 THRU STA-1307 REQUIRES EVALUATION OF CORROSION. CORRECTIVE ACTION: COMPLIED WITH FVC E.O. 19135.
AIRBORNE/PEMCO NON-ROUTINE 2387N511 DISCREPANCEY: L/H KEEL BEAM STA-676 THRU STA-1307 REQUIRES EVALUATION OF CORROSION. CORRECTIVE ACTION: COMPLIED WITH FVC E.O.19134.
AIRBORNE/PEMCO NON-ROUTINE 2387N519 DISCREPANCY: AFT CARGO COMPARTMENT HAS CORROSION ON FUSELAGE SKIN BETWEEN BS 1518 THRU 1540, STRINGERS S30R - S31R. CORRECTIVE ACTION: REMOVED CORROSION AT CARGO COMP. ON SKIN BETWEEN STR 30 AND 31 R/H STA 1518 TO 1540 IAW B767 SRM51-10-02 AND FOUND OUT OF LIMITS IAW B767 SRM 53-00-001, INSTALLED REPAIR DOUBLER AND FILLER IAW E.O. #19125 REV.IR.
AIRBORNE/PEMCO NON-ROUTINE 2387N315 DISCREPANCY: FWD CARGO LOWER BILGE CORRODED AT STA 764 BETWEEN STRINGERS 37R-37L. CORRECTIVE ACTION: COMPLIED WITH E.O. #19334.
AIRBORNE/PEMCO NON-ROUTINE 2387N1311 DISCREPANCY: AFT CARGO FLOOR TIE DOWN EXFOLIATED AT STA 1417 STR 32-33 R/H AND CORRSION BETWEEN SKIN AND STR 33 R/H. CORRECTIVE ACTION: REMOVED FLOOR TIE DOWN PER BOEING 767-200 SRM 51-40-02. REPAIRED SKIN PER FVCI E.O. #19121.
AIRBORNE/PEMCO NON-ROUTINE 2387N3100 DISCREPANCY: AFT CARGO WEB FRAME @STA 1241 HAS A PUNCTURE BETWEEN STR 36R & 36L. CORRECTION ACTION: REMOVED WEB, FABRICATED NEW WEB AND INSTALLED IAW FVCI E.O #20010.
AIRBORNE/PEMCO NON-ROUTINE 2387N515 DISCREPANCY: AFT CARGO BULK AREA HAS CORROSION ON STRUCTURES AT BS 1562 THRU 1582, STRINGERS S30R-S31R. CORRECTIVE ACTION: REPAIRED SKIN AT 1540-1582 BETWEEN STR 30R AND 36R IAW E.O. #19127 REV.C
AIRBORNE/PEMCO NON-ROUTINE 2387N2436 DISCREPANCY: FWD CARGO COMPARTMENT , FRAME AT STA. 500 HAS CORRSION BETWEEN STR 22L AND 23L. CORRECTIVE ACTION: REPAIRED IAW E.O. 14290.
AIRBORNE/PEMCO NON-ROUTINE 2387N2458 DISCREPANCY: MAIN CABIN FLOOR BEAM STA-1197, RBL-74 UPPER FLANGE CORRODED. CORRRECTIVE ACTION: REPAIRED MAIN CABIN FLOOR BEAM STA 1197, RBL 74 UPPER FLANGE IAW E.O. #19244 REV.A, AND B767-200 SRM 53-00-51 FIG. 201.
. AIRBORNE/PEMCO NON-ROUTINE DISCREPANCY: FWD CARGO, STA-538, STA-34R, FRAME LOWER CHORD CORRODED. CORRECTIVE ACTION: REPAIRED DAMAGE AT FWD CARGO STA. 538, STR 34R, FRAME LOWER CHORD IAW FVCI E.O. 19319 REV.A
AIRBORNE/PEMCO NON-ROUTINE 2387N1852 DISCREPANCY: RH WING AFT CORD CORRODED STA 1106 THRU ACCESS PANEL 643BB. CORRECTIVE ACTION: REPAIRED RH WING LOWER AFT CORD STA. 1106 IAW E.O. #19195.
AIRBORNE/PEMCO NON-ROUTINE 2387N3319 DISCREPANCY: LEFT WING LOWER AFT SKIN APPROX. WS 642 HAS FLAKING PAINT.(REQUIRES EVALUATION) CORRECTIVE ACTION: REPAIRED PANEL IAW B767-200 E.O.# 20064.
AIRBORNE/PEMCOAIR NON-ROUTINE 2387N3320 DISCREPANCY: LEFT WING LOWER AFT SKIN APPROX 950 HAS FLAKING PAINT. (REQIURES EVALUATION) REPAIRED AREA IAW E.O. #200665.
AIRBORNE/PEMCO NON-ROUTINE 2387N735 DISCREPANCY: CORROSION ON FUSALAGE SKIN UNDER LAP SEAM 7 INCHES AFT OF RIGHT MLG DOOR AFT END. CORRECTIVE ACTION: REMOVED CORROSION ON FUSALAGE SKIN UNDER LAP SEAM, 7 INCHES OF RIGHT MLG DOOR AFT END AND FOUND DAMAGE TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND FILLER IAW EO #47359REA05 AND INSTALLED REPAIR.
AIRBORNE/PEMCO NON-ROUTINE 2387N1310 DISCREPANCY: R/H WING UPPER FLANGE ,LOWER SURFACE, CORRODED AT WS 455 TO 496. CORRECTIVE ACTION: REMOVED CORROSION AND REPAIRED RH WING REAR SPAR,UPPER FLANGE WS 431.97 TO WS 532.46. EVALUATED AREA MAT.THICKNESS .200 MAT. REMOVED .054 MAT. REMAINING .141.TO BE REPAIRED E.O.# 19298 IAW B767-200 E.O. AND SRM 51-40-02.
AIRBORNE/PEMCO NON-ROUTINE 2387N1446 DISCREPANCY: AFT CARGO COMPARTMENT STA1540-1562, HAS CORROSION BETWEEN STR 38R-39R. CORRECTIVE ACTION: REPAIRED CORROSION BETWEEN STR 38R-39R AT AFT CARGO COMPARTMENT STA 1540-1562 IAW E.O.# 19126.
AIRBORNE/PEMCO NON-ROUTINE 2387N3180 DISCREPANCY: AFT CARGO INTERNAL SKIN AT STA 1241 JUST O/B OF S39R IS CORRODED. CORRECTIVE ACTION: REPAIRED AFT CARGO INTERNAL SKIN AT STA 1241 O/B OF S39R PER E.O. 20049 REV.B
AIRBORNE/PEMCO NON-ROUTINE 238N3321 DISCREPANCY: LEFT LOWER AFT SKIN AT WS 1075 HAS FLAKING PAINT.(REQUIRES EVALIUATION)CORRECTIVE ACTION: INSTALLED REPAIR ON LEFT WING LWR SKIN WS 1075 IAW B767 E.O.# 20066 REV.IR
AIRBORNE/PEMCO NON-ROUTINE 2387N905 DISCREPANCY ON AFT CARGO COMP., HAS CORROSION ON FUSELAGE SKIN BETWWEN BS 1355 THRU 1370, STRINGERS S26R - S27R. CORRECTIVE ACTIION: REMOVED CORROSION ON FUSELAGE SKIN STA. 1355-1370 STR 26R- STR27R. FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-01. REQUEST ENGINEERING ASSISTANCE WITH A REPAIR AS THE DAMAGE REPAIRED AREA AT STA 1355-1370 STR 26 R/H TO STR 30 R/H IAW B767 E.O.#20019
AIRBORNE/PEMCO NON-ROUTINE 2387N510 DISCREPANCY:ON NDT ROTOR HOLE INSPECTION, FOUND ONE HOLE ON R/H KEEL BEAM AROUND STA. 742 HAS AN INDICATION OF A CRACK. CORRECTIVE ACTION: EVALUATED AND REPAIRED AREA AT STA.742 RH KEEL BEAM IAW AMES DOCUMENT 47359REA15.
AIRBORNE/PEMCO NON-ROUTINE 2387N1133 DISCREPANCY: FWD CARGO COMPARTMENT, HAS CORROSION ON THE UPPER SURFACE OF THE AFT BULKHEAD LOWER CORD AT BS 784-785.9, BETWEEN STRINGERS S235R-S37R. CORRECTIVE ACTION: COMPLIED WITH EO# 19197.
AIRBORNE/PEMCO NON-ROUTINE 2387N1133 DISCREPANCY: FWD CARGO COMPARTMENT, HAS CORROSION ON THE UPPER SURFACE OF THE AFT BULKHEAD LOWER CORD AT BS 784-785.9, BETWEEN STRINGERS S235R-S37R. CORRECTIVE ACTION: COMPLIED WITH EO# 19197.
AIRBORNE/PEMCO NON-ROUTINE 2387N1268:MCC CUT-OUT LOWER LATCH CAM PINS FITTING HOLES INSIDE CORROSION CORRECTIVE ACTION: MDCD LATCH PIN FITTINGS REPAIRED PER EO#19398
AIRBORNE/PEMCO NON-ROUTINE 2387N514 DISCREPANCY: AFT CARGO BULK AREA, HAVE CORROSION ON SKIN AT BS 1540 THRU 1562, STRINGERS S28R-S29R CORRECTIVE ACTION: REPAIRED AFT CARGO BULK AREA SKIN AT B$ 1540-1562 IAW EO CONTROL # 19124
AIRBORNE/PEMCO NON-ROUTINE 2387N497 DISCREPANCY: AFT LOWER CARGO HAS CORROSION APROX S-35R STA. 1241 BELOW BODY DOOR OPEN PANEL INTERNAL CORRECTIVE ACTION: INSTALLED FILLER, DOUBLER & TRIPLER AFT LOWER CARGO APROX S355R STA 1241 BELOW BODY DOOR OPEN PANEL INTERNAL IAW EO# 19555
AIRBORNE/PEMCO NON-ROUTINE 2387N1921 DISCREPANCY: LH OTBD T/E FLAP, SUPPORT NO. 1 GOUGED, INBD ANGLED LEG, OTBD EDGE, FWD OF FLAP ATTACHMENT LUG. CORRECTIVE ACTION: REAIR DAMAGE (GOUGE) ON LH OTBD T/E FLAP SUPPORT #1 IAW EO # CONTROL 20089 REV. IR
AIRBORNE/PEMCO NON-ROUTINE 2387N1269 DISCREPANCY: MCC DOOR CUT-OUT LOWER SILL LATCH CAM PINS FITTING HAVE WEAR MARKS CORRECTIVE ACTION: MDCD LATCH CAM PIN FITTINGS REPAIRED PER EO# 19398
AIRBORNE/PEMCO NON-ROUTINE 2387N1046 DISCREPANCY: STA. 1417, STRGS 29L TO 33L BULK CARGO DOOR CUT OUT AT FUSELAGE SIDE HAS MULTIPLE AREAS OF CORROSION. CORRECTIVE ACTION: WORK ACCOMPLISHED IAW EA# 47359REA04 REV. IR
AIRBORNE/PEMCO NON-ROUTINE 2387N1312 DISCREPANCY: MAIN CARGO DOOR, SKIN IN AREA OF SCUFF PLATE HAS NUMEROUS AREAS OF CORROSION CORRECTIVE ACTION: REPAIR CORRODED AREA IAW E.O.# 19165 @MCCD SCUFF PLATE AREA
AIRBORNE/PEMCO NON-ROUTINE 2387N55 DISCREPANCY: CORROSION ON LWR EXTERNAL FUSELAGE SKIN STA. 390 STR. 39L CORRECTIVE ACTION: INSTALLED REPAIR ON LOWER EXTERNAL FUSELAGE SKIN STA 390 S39L IAW B767 RES#14409, EO# 43759REA02
AIRBORNE/PEMCO NON-ROUTINE 2387N1322 DISCREPANCY: LEFT WING ROOT HAVE CORROSION ON EXT. FUSELAGE UNDER PANEL 191GL, APPROX. BS 944, WS 0.0 (MARKED) CORRECTIVE ACTION: REMOVED FASTENERS OF AFFECTED AREA. REMOVED CORROSION FLAP PEENED SURFACE IN AREAS 1,2, AND 3, TREATED + PRIMED SURFACE. RE-INSTALLED OR REPLACED ALL REMOVED FASTENERS ALL WORK ACCOMPLISHED IAW F.V.C. EO 19137 AND BOEING DRAWING 145T0083 AND B767-200 SRM 51-40-02 SRM 51-20-01 SRM 51-10-02
AIRBORNE/PEMCO NON-ROUTINE 2387N2677 DISCREPANCY:MCC DOOR CUTOUT LOWER SILL LATCH CAM PIN FITTINGS HAVE CORROSION IN PIN BORES AT STA. 544 CORRECTIVE ACTION: MCC DOOR CUTOUT LOWER SILL LATCH CAM FITTINGS REWORKED IAW ENGINEERING ORDER NO. 19398
AIRBORNE/PEMCO NON-ROUTINE DISCREPANCY: R/H LANDING GEAR, LONGERON I/B CHORD, UPPER O/B FACE AT APPROX STA 970-977 CORRODED. CORRECTIVE ACTION: INSTALLED REPAIR STRAP IA EO CONTROL # 19558
AIRBORNE/PEMCO NON-ROUTINE 2387N736 DISCREPANCY: FWD CARGO COMPARTMENT, OUTER CORD OF LWR SILL FASTENER LOCATION CORRODED AT FS 610, STRINGERS S-32R. PEMCO ENG. SVC. REQUEST NO.: RES 14415: FWD LWR CARGO DOOR BEAM HAS CORROSION ON UPPER AND LWR FLANGES. REQUEST ENGINEERING ASSISTANCE IN REPAIR EVALUATION. STRUCTURE ID SRM 53-30-15, ALLOWABLE DAMAGE SRM 53-00-15. ENGINEERING DISPOSITION: ACCOMPLISH REPAIR PER FVCI EO 19320 REV. A. A COPY OF THE FAA APPROVAL (8110-3) IS ATTACHED AIRBORNE/PEMCO NON-ROUTINE 2387N736 CORRECTIVE ACTION: COMPLIED WITH EO 19320 FAA 8110-3 #19320 DATE: NOVEMBER 13, 2019
AIRBORNE/PEMCO NON-ROUTINE 2387N1106 DISCREPANCY: (722109) CORROSION ON SKIN, INTERNAL SIDE STA. 1263-1285 STR. 36-37 R/H CORRECTIVE ACTION: REMOVED & REPLACED DAMAGED SHEAR TIE @ STA 1285, BETWEEN S37R-S36R IAW B767 SRM 51-40-02. REPAIR DOUBLER & TRIPLER FROM STA 1250 TO STA 1307, S38R TO S31R WAS INSTALLED ON NR#2387N2744 IA EA# PD67-53-070. DAMGED STRINGER S36R WAS REPLACED ON NR#2387N2380IAW B767 SRM 51-40-02 & 53-00-03 REPAIR #2
AIRBORNE/PEMCO NON-ROUTINE 2387N2400 DISCREPANCY: P/R-AFT CARGO STR 34R BS1339 HAS CORROSION DAMAGE CORRECTIVE ACTION: REMOVED & INSTALLED NEW STRINGER SECTION FOR 34R FROM STA1241 TO STA 1379 IAW B767 SRM 51-40-02 & 53-00-03 REPAIR #2
LEFT ENGINE SHUTDOWN IN FLIGHT DUE TO VIBRATION.
LEFT ENGINE SHUTDOWN IN FLIGHT DUE TO A VIBRATION. ACCOMPLISHED FIM 71-05 FT 814, NO METAL PARTICLES FOUND IN THE INLET OR EXHAUST AREAS, NO COMTAMINATION FOUND ON THE MASTER CHIP DETECTOR. ACCOMPLISHED LT ENGINE BORESCOPE INSPECTION OF THE LPC, HPC, HPT BLADES, COMBUSTOR AND FUEL NOZZLES IAW 72-00-00 AND FIM 71-05 - TREE 814. NO DEFECTS NOTED. DURING TROUBLESHOOTING IAW FIM 71-05 TREE 814, FOUND THE LEFT ENGINE RT PYLON CONNECTOR D4223P CONTAMINATED WITH HYDRAULIC FLUID. CLEANED AREA AND REMOVED & REPLACED THE CONNECTOR IAW SWPM 20-63-00, 20-10-04, WD 2233-11, 71-S1-11, 73-34-11, 75-32-12, AND 77-31-11. CONTINUITY AND INSULATION CHECKED OK. ACCOMPLIASHED A LT ENGINE VIBRATION SURVEY TEST IAW AMM 71-00-00, OPS CHECKED GOOD. REMOVED AND REPLACED THE VIBRATION SIGNAL CONDITIONING UNIT IAW AMM 72-31-03. ACCOMPLISHED SYSTEM OPS CHECK, NORMAL IAW 77-31-03, AND 77-31-00. ACCOMPLISHED AN ENGINE IDLE RUN FOR VIBRATION, OPS CHECK FAILED. TROUBLESHOT SYSTEM IAW FIM 71-05 FT 814. FOUND PYLON CONNECTION D4223P CONTAMINATED.
AFT CARGO BAY INTERNAL SKIN CORRODED BS 1351 STRINGER 29R.
BULK CARGO DOOR CORRODED BS 1461, S30 - 31L.
LOWER FUSELAGE SKIN CRACKED BS 1562 - 1640, STRINGER 24L.
AFT CARGO BAY SECTION 46, STRINGER 36R, BS 1219 CORRODED.
FWD CARGO BAY STRINGER 35R SHOWS CORROSION BS 742.
FWD CARGO BAY FRAME BS 676, UPPER ANGLE LBL 29, LBL 36 LBL4, RBL 35 CORRODED.
FWD CARGO BAY STRINGERS 37L SHOWS CORROSION.
LT WING NR 4 OTBD SLAT LOWER SKIN DENTED 6, WS 538.2-WS 564.2.
AFT CARGO BAY SECTION 46 STRINGER 26R, BS 1461 SHOWS CORROSION.
AFT CARGO DOOR LOWER FRAME WEB CORRODED BS 1345 S34R.
AFT CARGO BAY SECTION 46, FLOOR SUPPORT EXTRUSION BROKEN BS 1439, LBL 30.
AFT CARGO BAY SECTION 46, WEB SHOWS CORROSION BS 1263, RBL 70 S34R.
AFT CARGO BAY SECTION 46, STRINGER AND SPLICE 37R SHOW CORROSION BETWEEN BS 1285 - 1307.
AFT CARGO BAY SECTION 46.- STRINGER 39R AND ANGLES SHOW CORROSION BS 1373.
AFT CARGO BAY SECTION 46. FLOOR SUPPORT EXTRUSION SHOWS CORROSION BS 1430, LBL 20.
AFT CARGO BAY SECTION 46 STRINGER AND SPLICE 39R SHOW CORROSION BS 1307.
AFT CARGO BAY SECTION 46, STRINGER 36R SHOWS CORROSION BS 1417.
AFT CARGO BAY SECTION 46, WEB SHOWS CORROSION BS 1263 - 1270.
AFT CARGO BAY SECTION 46, STRINGER 36R AND ANGLES CORRODED BETWEEN BS 1285 - 1307.
LOWER FUSELAGE EXTERIOR LOWER SKIN SHOWS CORROSION BS 1480 - 1510.5 S36L.
LOWER FUSELAGE EXTERIOR SKIN SHOWS CORROSION BS 1480 - 1510 S33R.
CENTER HYD SYSTEM FLUID QUANTITY LOSS, FRM CODE 29-90-11-43.
DURING ROUTINE C CHECK INSPECTION, RIGHT FUSELAGE OVERWING EXIT HATCH LOWER SILL INNER CHORD CRACKED 0.200 INCH AT STA 883.5. REF N/R 0251
DURING ROUTINE C CHECK INSPECTION, MAIN CARGO DECK SECTION 45 - WEB AREA CRACKED 10 STA 1000 TO STA 1020 LBL 25.0 REF N/R 0356
DURING ROUTINE C CHECK INSPECTION, AFT CARGO COMPARTMENT STRINGER SHOWS CORROSION AT STA 1398 S25R REF N/R 0206.
DURING ROUTINE C CHECK INSPECTION, LEFT FUSELAGE OVERWING EXIT HATCH LOWER SILL INNER CHORD CRACKED 0.250 INCH AT STA 883.5 REF. N/R 0250.
DURING ROUTINE C CHECK INSPECTION, LEFT WING T/E RIB POST CRACKED AT WS 906.20 REF N/R 0327
DURING ROUTINE C CHECK INSPECTION, AFT CARGO COMPARTMENT REAR STRAP SHOWS CORROSION STA 1395 S25RH REF N/R 0205.
RIGHT KICK LOAD FITTING CORRODED. R & R RIGHT KICK LOAD FITTING IAW SRM 51-40-02 AND 57-10-10, FIG 201.
CORROSION AROUND INBD FITTING ON LT FAILSAFE AND GOUGES ON OTBD SIDE OF FAILSAFE . REPAIR AND TERMINATING ACTION ACCOMPLISHED ON REA 46963REA03 AND 46963REA01.
RIGHT FAILSAFE CRACKED, FOUND ON EDDY CURRENT, VERIFIED WITH BORESCOPE. R AND R RT SIDE FAILSAFE IAW REA'S 46963REA07 AND 46725ORD01.
DURING INSPECTION, FOUND REAR SPAR WEB CORRODED UNDER RT FORK. REPAIRED IAW SRM AND REA 46963REA10.
DURING C-CHECK FOUND TEE FITTING CORRODED IN LT WW. R & R TEE FITTING IAW SRM AND REA 46963REA03.
DURING C CHECK, FOUND TEE FITTING CORRODED IN RT WW. R & R TEE FITTING IAW REA 46963REA-07.
DURING C-CHECK FOUND LT FAILSAFE HAS .4" CRACK. FAILSAFE REPAIRED ON N0N-ROUTINE 0004 AND REA 46963REA03.
DURING C-CHECK FOUND RT FAILSAFE CRACKED 3.4". R & R RT FAILSAFE IAW REA 46963REA02 AND REA 46963REA07.
DURING C-CHECK FOUND RT FAILSAFE UPPER OTBD KICK FITTING BLEEDING RUST. KICK FITTING R & R ON NON-ROUTINE 0045.
DURING INSPECTION, FOUND RT PICKLE FORK INBD LEG BLENDED BEYOND LIMITS. REPAIRED IAW REA 46963REA11.
DURING INSPECTION FOUND CENTER WING REAR SPAR CORRODED AT STA 955 INBD OF PICKLE FORK. REPAIRED IAW SRM AND REA 46963REA12.
DURING INSP FOUND INTERNAL FUSELAGE SKIN CORRODED AT STA 960, S19R. REPAIRED IAW REA 46963REA06 AND 46963REA09.
DURING C-CHECK FOUND LT PRESSURE WEB DRAIN BASE CORRODED. R & R DRAIN BASE IAW SRM.
DURING C-CHECK FOUND STRINGER 19L CORRODED AT STA 960. FABRICATED STRINGER IAW DWG AND WILL BE INSTALLED IAW REA 46963REA03.
DURING INSPECTION FOUND RT FORK LOWER FWD FACE CORRODED. REPAIRED CORRODED AREAS IAW SRM AND REA 46963REA03 AND 46963REA11.
DURING C-CHECK FOUND SKIN CORRODED AFT OF FAILSFE COMMON TO TRIM OUT. REPAIRED CORROSION IAW REA 46963REA04 AND 46963REA08.
DURING C-CHECK FOUND LEFT FAILSAFE OPEN HOLE INSPECTION, LOWER 2 HOLES CRACKED. FAILSAFE REPAIRED ON N0N-ROUTINE 0004 AND IAW REA 46963REA03.
DURING C-CHECK FOUND .25" CRACK IN DRAIN TUBE STA 955. R & R DRAIN TUBE IAW SRM.
STRONG ODOR FROM PACKS ON DESCENT TO MIA. THIN SMOKY HAZE IN SUPERNUMERARY COMPARTMENT - SET OFF SMOKE DETECTORS. SMOKY HAZE SPREAD THROUGHOUT AIRCRAFT. MAINTENANCE FOUND THE RAM AIR EXIT DOOR CLOSED IN ALL MODES. THE RAM AIR EXIT DOOR ACTUATOR WAS REPLACED AND TESTED NORMALLY PER THE AMM.
INSTALLED DOUBLER REPAIR NR 2 ENGINE STRUT MID TORQUE BOX AT ACCESS PANEL 446AL PER REFERENCE AAR RES-WI NR 2003761-23 DATED 6/27/2011 AND FAA FORM 8110-3 DATED JULY 8, 2011 BY DER DERT-605410NM.
RIGHT WING ROOT UPPER SURFACE FAIRING SUPPORT BRACKET CORRODED. REPLACED CORRODED BRACKET.
LEFT WING UPPER AFT COVE PANEL SUPPORT OUTBOARD FLANGE CORRODED. REPLACED CORRODED SUPPORT.
INSTALLED MAJOR STRINGER SPLICE REPAIR AT BS 1397-BS 1417 S39L PER B767 SRM 51-50-02, 53-01-02, 51-10-02 AND 52-20-02.
INSTALLED DOUBLER AND TRIPLER SKIN REPAIR AT BS 1725.5 S7R PER B767 SRM 53-80-01.
L ENG FIRE LP2 STATUS MSG INTERMITTENT. INSP L ENG FIRE LOOPS CONNECTION, INSULATOR, AND LOOPS FOR CHAFING, FOUND OK. PERFORMED LOOP TEST PER AMM 26-11-00-5, CHECKED OK. UNABLE TO DUPLICATE.
TWO CRACKS ON LEFT SIDE OF FUSELAGE, 2.75 INCHES LONG TOTAL, FS 1659 AT S12L. VERIFIED WITH ET (CRACKS 2 EACH APPROX 1.375 INCH LONG). REPAIR NOTED AREA IAW B767 SRM 53-00-01 FIG 201.
CAPTAIN'S SHOULDER HARNESS WOULD NOT FULLY EXTEND, UNABLE TO REACH LANDING GEAR HANDLE WITH SHOULDER HARNESS ON. REPLACED CAPTAIN SEAT INERTIAL REEL & RESTRAINT ASSY, AS PER B767 AMM 25-11-01-2.
WITH RIGHT HP BLEED CLOSED PER MEL PROCEDURES, CONTINUED TO GET A BLEED VALVE OFF EICAS MSG. CREW FOLLOWED THE ENGINE BLEED VALVE NON NORMAL PROCEDURES. RETURNED TO AIRPORT. FOUND TERMINAL BROKEN AT NR 1 HIGH STAGE VALVE POSITION, REPAIRED TERMINAL IAW 20-00-00.
STA MIA, ON WALKAROUND MAINTENANCE FOUND CIRCULAR PANEL ON OUTBOARD SIDE OF NR 2 PYLON MISSING. DEFERRED DI 61151. CLEARED DI, INSTALLED NEW CIRCULAR ACCESS PANEL ON OUTBOARD SIDE OF NR 2 PYLON. (A)
STA MIA, ON WALKAROUND, MAINTENANCE FOUND CIRCULAR PANEL ON NR 2 PYLON OUTBOARD SIDE MISSING. DEFERRED DI 61119. CLEARED DI, INSTALLED NEW PANEL ON NR 2 PYLON. (A)