N323UP
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 | 2021-09-18 – 2021-09-18 | Operator named in NTSB report |
| UNITED PARCEL SERVICE CO | Operator | 2021-09-18 – 2021-09-18 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
CRACKED BULKHEAD OUTER CHORD STRAP AT BS 1725 S-7R. (REPAIR). COMPLETED REPAIR I.A.W EGAT WORK SHEET NO.40938 STEP D.5 AND D.6 AND D.8 AND D.10 AND D.11 AND D.13~D.19. ACCOMPLISHED UPS EO NO. EO-24301-JIC003 REV. 4 AND EGAT WORK SHEET NO. 40938.
FOUND M/D FLOOR PNL NO. 241DFF BROKEN AT STA 731 TO STA 834 LBL-65, P/N : 145T5876-63.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
BROKEN - FOUND M/D FLOOR PNL BROKEN AT STA933 TO STA980 RBL-80 P/N: 145T5876-84 , PANEL NO.242MFF. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
FOUND M/D FLOOR PNL DENT AND BROKEN AT STA 1040 TO STA 1114 LBL-45, P/N: 145T5876-43, PANEL NO 241BGF. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
BIRD STRIKE - SKIN, UPPER FACE OF L/H WING NO.4 SLAT T/E SKIN, OSS 545.75.JOB COMPLETED AND CONDITION CHECK NORMAL AND ATTACHMENT ARE UPLOADED. I.A.W AMM 27-81-02-424-099 REV.143 STEP 3A TO H (16) INSTALLED NO.4 SLAT OF THE LH WING.
FOUND M/D FLOOR PNL NO.241EFF DENT AT STA 746 TO STA 876 LBL 80, P/N:145T5876-1.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
FOUND M/D FLOOR PNL NO.241WFF DENT AT STA 980 TO STA-1114 LBL11, P/N: 145T5876-73. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
FOUND M/D FLOOR PNL NO.241BFF DISBOND AT STA 731 TO STA 834 LBL-22, P/N:145T5876-70. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
DENT - FOUND M/D FLOOR PNL NO.242FFF AT STA 834 TO STA 933 RBL -45, P/N: 145T5876-61.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
FOUND M/D FLOOR PNL DISBOND AND DENT AT STA 746 TO STA 876 RBL -80 PNL NO.242DFF, P/N: 145T5876-7. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
FOUND M/D FLOOR PNL NO.241CFF DENT AND INSERT DAMAGE AT STA 731 TO STA 834 LBL-45, P/N:145T5876-65. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
FOUND M/D FLOOR PNL DENT AND INSERT DAMAGE AT STA 988 TO STA 1114 LBL 65 PNL NO.241ZFF, P/N:145T5876-77.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
FOUND M/D FLOOR PNL NO.241GFF DENT AT STA 834 TO STA 933 LBL-22, P/N: 145T5876-59. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
FOUND FLOOR PNL NO.241QFF DENT AT STA 933 TO STA 980 LBL-80, P/N: 145T5876-78. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
FOUND THE MAIN DECK CARGO FLOOR PANEL DENT , P/N: 146T5869-134. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
FOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN. REPLACED SPLINE TRIM I.A.W AMM 52-12-02-004-001 REV.143 AND AMM 52-12-02-404-025 REV.143.
FOUND THE MAIN DECK CARGO FLOOR PANEL DENT , P/N: 146T5869-135. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.
FOUND MAIN ENTRY DOOR DOORWAY SPLINE TRIM BROKEN. (REPLACE) OK TO WORK.
CORROSION , FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R. ACCOMPLISH REPAIR PER EO-91974-REQ1 AND EGAT EI F2024A53M-2800, REV. 0 AND 1.
FOUND THE MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING WITH CRACK DAMAGE AT STA 1109 BL 0.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 90.INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 90. AND BOEING DWG NO. 457T4000 SH. 11 REV. B
FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. REVIEW COMPLETED PER EO-82173-J1C001.CONDITION CHECK OK
#2 ENG OUTBD ACCESS PANEL FOR ENG MOUNT BOLTS HAS A DAMAGED FIRE SEAL REMOVED AND REPLACED SEAL ON #2 ENG OUTBD ACCESS PANEL REF. SRM 51-40-02 AND IPC 54-52-01-19.
*SUPPLEMENTAL SDR* #2 ENG OUTBD ACCESS PANEL FOR ENG MOUNT BOLTS HAS A DAMAGED FIRE SEAL REMOVED AND REPLACED SEAL ON #2 ENG OUTBD ACCESS PANEL REF. SRM 51-40-02 AND IPC 54-52-01-19. RE-INSTALLED PANEL PER SRM 51-40-02.
R/H WING #7 SLAT TRACK LEADING EDGE PANEL DAMAGED. REMOVE AND REPLACED LEADING EDGE SUPPORT LINK DOOR R/H INB AS PER 57-41-59 404-009, OPS CHKS GOOD-
*** SUPPLEMENTAL SDR *** CREW ENTRY DOOR ARMING LEVER HINGED COVER SPRING BROKEN REPLACED CREW ENTRY DOOR ARMING HINGE COVER REF MM 52-12-02 OPS CK GOOD THIS CLEARS DEFERRAL
CREW ENTRY DOOR ARMING LEVER HINGED COVER SPRING BROKEN DEFERRED CREW ENTRY DOOR HINGED COVER IAW MEL 52-11-2, PLACARDS INSTALLED. OPEN
INSPECTION TYPE:NA*EMERGENCY DECLARED* LEADING EDGE SLATS DISAGREE RAN CHECKLIST AND CONFIGURED SUCCESFULLYBITE CARRIED OUT IAW FIM 27-51-00-815-809 FLAPS/SLATS EXTENDED/RETRACTED WITH NO FAULTS
INSPECTION TYPE:N/ATEMP BLIND FASTENER INSTALLED FUSELAGE 8 INCH FWD OR STA 676 - 1 INCH O/B OF S39LFABRICATED REPAIR DOUBLER IAW UPS E.O.B767-5330-85085-A ON NRC 684228
TEMP BLIND FASTENER INSTALLED FUSELAGE 8" FWD OR STA 676 - 1 INCH O/B OF S39LREPAIRED IAW E.O. B767-5330-85085-B ON NRC 684229
INSPECTION TYPE:**ETOPS FILED OPEN** ON LANDING, L THRUST REV WOULD NOT DEPLOY. DEFERRED LEFT ENG T/R PER MEL 78-31-1 C/W DMP 78-31-
IFSD, ATB, EMERGENCY DECLARED, AIRCRAFT OOS, APPROXIMATELY 200' AFTER TAKE OFF, ENG STARTED TO SURGE. DURING THE CLIMB THE L ENG HAD NO RESPONSE FROM THE L THRUST LEVER. RAN APPROPRIATE CHECKLIST AND SHUTDOWN L ENG. A/C AWAITING LEFT ENG CHANGE.R/R #1 ENGINE PER AMM 71-00-02, SN OFF- 704418, SN ON- 702140 PER UPS TC 6001 & TC 6002. COMPLED WITH REVISION OF UPS EO E-7900-62890, APPX B. ENGINE TEST & LEAK CHECK GOOD.
INSPECTION TYPE: C12 DAMAGE ON MD CARGO FLOOR PANEL BETWEEN STA 510 - 620, LBL 11 - RBL 11. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320-9693-I.
INSPECTION TYPE: C12 CORROSION WAS FOUND ON FLOOR BEAM PN 146T5144-11 OF MAIN DECK FLOOR STRUCTURE AT STA 1540, RBL 60 - RBL 80. REPAIR IAW BOEING SR 3-4942408700 AND UPS EO B767-5310-79230-A.
INSPECTION TYPE:C12CORROSION WAS FOUND ON FLOOR BEAM (P/N : 146T5143-5) OF MAIN DECK FLOOR STRUCTURE AT STA 1518 , RBL 70 - RBL 90REPAIR I.A.W BOEING SR 3-4942597086 AND UPS EO B767-5310-79232-A
INSPECTION TYPE: C12 CORROSION WAS FOUND ON FLOOR BEAM PN 146T5144-11 OF MAIN DECK FLOOR STRUCTURE AT STA 1540, LBL 60 - LBL 80. REPAIR IAW BOEING SR 3-4942408700 AND UPS EO B767-5310-79230-A.
INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2011-5) ON STA 785.9 , LBL 55REAPIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.79.01 AND UPS EO B767-5740-58151-C
INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2008-11) ON STA 785.9 , LBL 33REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.79.01 AND UPS EO B767-5740-58151-C
INSPECTION TYPE: NA, ATB, NO EMERGENCY DECLARED & NO EQUIPMENT USED. T/O & 38 MINS GOT L HYD QUANTITY EICAS LT QUANTITY L HYD PRIM PUMP. EICAS LIGHT CAME ON WHEN USING SPEEDBRAKES. ARRIVED WITH ZERO FLUID IN LT SYS. NEVER LOST SYSTEM PRESSURE FOUND ELECTRO-HYD SERVO VALVE ON RUDDER RATION CHGR ACT LEAKING FROM PLUG ON SIDE OF VALVE, REF AMM 27-21-15. R & R RRCA SOLENOID VALVE, AS PER AMM 27-21-15-201. OPERATIONS CHECK OK, PER AMM 27-21-15-422-024. NO LEAK NOTED AT THIS TIME.
INSPECTION TYPE: N/A ATB- EMERGENCY DECLARED. RECEIVED FIRE WARNING BELL ON TAKE OFF ROTATION COULD NOT EXTINGUISH. R & R M1000 BELL CHIME MODULE BOARD, PER MM 31-51-04-004-133/404-014. TEST PER AMM 31-51-04-724-154. PN ON AND OFF 285T0385-5. SN OFF 01860 ON D01475. IPC REF 31-51-04-05C ITM 145.
INSPECTION TYPE:C11CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287,RBL 25, WL 159.REPAIR I.A.W UPS EO B767-5310-20118-F AND 767-300F SRM 51-70-12 GENERAL, FIGURE 1 , REV 73.01
INSPECTION TYPE:N/A ATB - DUE TO CABIN ALTITUDE. AFTER ACCOMPLISHING THE QRH PROC CABIN REMAINED UNCONTROLLABLE. PERFORMED PRESSURE CONTROLLER BITE PROCEDURE FOUND NR 2 LOW IN FLOW FAULT FIM 21-31-00-815-803/REF TS-B767-2150-00007 FOUND LEFT PACK "LO" FLOW 25% LESS THAN RIGHT PACK. REMOVED & REPLACED LEFT PACK FLOW CONTROL AND S.O. VALVE REF AMM 21-51-01-401. AFTER REPLACEMENT.
EICAS MESSAGE FOR THE AFT CABIN TEMP INOPERATIVE. OPEN
INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** PERFORMED BORESCOPE INSPECTION #2 ENG PER PMC 6. FOUND 1ST STAGE HPT BLADE MISSING MATERIAL ON LEADING EDGE MEASURING DIMENSION GREATER THAN 5 EDGE HOLES. REFER TO AMM 72-00-00-206-363-H00 TABLE 680 FOR MAX SVCABLE LIMIT PICS EMAIL TO ENGINE.TRANSFERRED TO NON ROUTINE CARD 513828, DMI CLEARED. REMOVED ESN 704761 AND INSTALLED ESN 707222 PER UPS TC 6001 AND 6002. COMPLY WITH CURRENT REVISION OF UPS EO E-7900-62890 APPENDIX B.
PERFORMED A BORESCOPE INSPECTION ON THE NR 2 ENGINE IAW PMC 6. FOUND 1ST STAGE HPT BLADE MISSING MATERIAL ON THE LEADING EDGE, MEASURING DIMENSION GREATER THAN 5 EDGE HOLES IAW MM 72-00-00-206-363-H00, TABLE 680 FOR MAX SERVICABLE LIMITS.
ENGINE FUEL FEED SYSTEM L, FWD FUEL PUMP EICAS MSG SHOWS AND L FWD PUMP PRESS LIGHT IS ON WITH SWITCH ON. REPLACED L FWD FUEL PUMP GFI, RELAY REF FIM 28-22-00 FIG 114 & WDM 28-22-11, RELAY K10703 [TJQ 0558733 9-4-18] SYSTEM OPS CHECKS OK. REF FIM FIG 114, 28-22-00. IPC 28-22-03-410, ITEM 010.
AIR TURNBACK. AFTER TAKEOFF, THE RUDDER RATIO EICAS ILLUMINATED. FOUND THE RIGHT RUDDER RATIO CHANGER MODULE FAULTED. R & R THE MODULE IAW MM 27-09-00. OPS CHECKED GOOD IAW MM 27-21-00.
L1 DOOR INTERIOR EMERGENCY EXIT LIGHT DAMAGED. R & R THE SIGN IAW MM 33-51-01-962-028. REPAIRED THE MOUNTING BRACKET IAW EO 5210 67082 B, PARAGRAPH 6.
APU GEN OFF LIGHT, NO RESET INFIGHT TURNBACK, ONE ELECT POWER SOURCE. AHM SHOWS AT 370' APU COULDN'T MAINTAIN 95%. R & R THE APU FUEL CONTROL IAW MM 49-31-01, OPS AND LEAK CHECKED GOOD.
INSPECTION TYPE: C10, CRACK ON STIFFENER UPPER SIDE AT BS 785.9, RBL 33. REPAIR IAW SRM 57-10-10-2R-2, REPAIR 2, REV.67 AND EO B767-5740-58151-A
INSPECTION TYPE: C10, CRACK ON INBD SIDE SKIN AND DOUBLER OF THE NR 2 PYLON. REPAIRED THE PYLON IAW SR 3-3822893601 AND EO B767-5430-63695-A.
FOUND DURING PS1 CHECK, LIFE VEST OF F/O SEAT UNSERVICEABLE. R & R THE LIFE VEST IAW AMM 25-62-00 REV. 118.02.
FOUND DURING PS1 CHECK, LIFE VEST OF LT SUPERNUMERARY SEAT UNSERVICEABLE. REMOVED AND REPLACED THE LIFE VEST IAW AMM 25-62-00 REV. 118.02.
AFTER RESTORING THE CAPTAIN`S OXYGEN MASK INFLIGHT, THE MASK DOES NOT TEST CORRECTLY WHEN THE RED EMERGENCY BUTTON IS PUSHED. REPACKED CAPTS OXYGEN MASK. PERFORMED AMM TASK 35-11-00-715-224. MASK CHECKS NORMAL.
INSPECTION TYPE:C9, A THREE INCH CRACK WAS FOUND ON STRINGER 20R AT BS 1550, REPAIR IAW SR 4-2882995662 AND EO B767-5310-57269-A.
INSPECTION TYPE:C9, FOUND CRACK ON M/D CARGO FLOOR PANEL, 232FFF, AT BS 620, RBL 11- 33 FABRICATE THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.
INSPECTION TYPE:C9, FOUND CRACK ON M/D CARGO FLOOR PANEL, 242GFF AT FS 850, RBL 54.75 - RBL 74.25, FABRICATE THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.
INSPECTION TYPE: C9, FOUND CRACK ON M/D CARGO FLOOR PANEL, 232GFF AT BS 533-654+22, RBL 33-55, FABRICATE THE REPLACEMENT FLOOR PANEL IAW EO NR B767-5320-9693-H.
INSPECTION TYPE:C9, PUNCTURE HOLE DAMAGE, LENGTH=0.67", WIDTH=0.5", WAS FOUND ON SKIN OF TAIL FUSELAGE SECTION 48 AT STA 1630, BETWEEN S-36R AND S-38R. REPAIR IAW SR 3-3223765412 WITH APPROVED 8100-9 FORM DATED:22APR2015 AND EO B767-5310-57268-A.
MAIN CARGO DECK FLOOR PANEL DAMAGED. FABRICATE A NEW FLOOR PANEL IAW EO 5320-9693-H.
FLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-H.
FLOOR PANEL DAMAGED. REPAIRED IAW -5320-9693-H.
FLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-H.
HOLE IN MCD FLOOR PANEL POS 4L AT BS 726. REPAIRED HOLE IAW SRM 53-00-2R-4B.
MAIN CARGO FLOOR PANEL DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H AND DWG 141T5856.
VERTICAL STABILIZER LT SIDE LOWER PANEL DELAMINATED.. TRANSFERRED TO NRC 529065 FOR PANEL REPLACEMENT. COMPLETED PANEL REPLACEMENT IAW EO B7U67-5530-55201-A. MAJOR REPAIR
EMERGENCY LIGHTS INTERMITTENT. WILL NOT STAY ON. R & R BATTERY PACK IAW MM 33-51-07-33-51-07-32. OPS CHECKED GOOD.
AIR TURNBACK, DURING CLIMBOUT, RT BLEED DUCT LEAK EICAS AND OVERHEAD LIGHT DISPLAYED. RAN QRH CHECKLIST. R & R RT WING/BODY DETECTOR ELEMENTS IAW MM 26-18-01-024-001-001, PERFORMED DUCT LEAK CHECK AND ELMENT SYSTEM TEST. ALL CHECKS GOOD.
RIGHT ELEVATOR LOWER SKIN PUNCTURED. REPAIRED IAW EO 5520-54318-A.
EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS EMERGENCY EXTERIOR LIGHT IAW AMM 33-51-16. OPS CHECKED GOOD.
INSPECTION TYPE:C08, DURING WORK OF SB 53-0116 & REQUIREMENT OF SB 53A0100, FOUND CORROSION DAMAGE TO SKIN COMMON TO FAILSAFE STRAP INTERFACING SURFACE FROM S-20R TO OVERWING LONGERON. CORROSION DAMAGE TO REAR SPAR SIDE FRAME FITTING COMMON TO INTERFACING SURFACE W/REAR SPAR WEB CORROSION DAMAGE TO REAR SPAR WEB COMMON TO INTERACING SURFACE W/REAR SPAR SIDE FRAME FITTING. REPAIR CORROSION IAW EO B767-5330-50717-A. B767-5310-50720-A AND B767-5710-50716-A. REPLACE THE FAILSAFE STRAP IAW EO B767-5350-50409-A, B767-5330-50723-A.
INSPECTION TYPE:C08, MAIN DECK CARGO FLOOR PANEL DENTED BETWEEN BS 1197+25 AND 1197 +45, LBL 8 - RBL 8. REPAIRED IAW EO NO B767-5320-9693-H.
INSPECTION TYPE:C08, FOUND CARGO FLOOR PANEL BETWEEN BS 998 AND 1003,BL 0 -LBL 5 DENTED. REPAIRED IAW EO B767-5320-9693-H.
INSPECTION TYPE:C08, MAIN DECK CARGO FLOOR PANEL DENTED BS 1480, RBL 54. REPAIRED IAW EO B767-5320-9693-H.
INSPECTION TYPE:C08, FOUND CARGO FLOOR PANEL DENTED BETWEEN BS 1215 AND 1294, LBL 23-31. REPAIRED IAW EO B767-5320-9693-H.
INSPECTION TYPE:C08, FOUND CARGO FLOOR PANEL DENTED BETWEEN BS 1410 AND 1473, LBL 35 - 54. REPAIRED IAW EO B767-5320-9693-H.
INSPECTION TYPE:C08, CARGO FLOOR PANEL DENTED BETWEEN BS 1520, LBL 55. REPAIRED IAW EO NO B767-5320-9693-H.
INSPECTION TYPE:C08, CARGO FLOOR PANEL DENTED BETWEEN BS 1120 AND 1180, LBL 34 - RBL 45. REPAIRED IAW EO B767-5320-9693-H.
INSPECTION TYPE:C08, CARGO FLOOR PANEL DELAMINATED BS 1480, RBL 11. REPAIRED IAW EO NR B767-5320-9693-H.
INSPECTION TYPE:C08. CARGO FLOOR PANEL DENTED BS 988 - 1004, LBL 82. REPAIRED IAW EO B767-5320-9693-H.
INSPECTION TYPE:C08, CRACK 1.1 INCHES, WAS FOUND ON STRINGER 20L BETWEEN BS 1502 AND 1518. REPAIR IAW SR 1-2419267958.
INSPECTION TYPE:C08, CRACK (0.65") WAS FOUND ON LT HORIZONTAL INNER CHORD OF STA 1809.5 BULKHEAD AT APPROX WL 257 AND LBL 28. THE CRACK WAS EXTENDED FROM THE FASTENER HOLE THRU THE EDGE OF INNER CHORD. REPAIR IAW SRM 53-80-08, REPAIR 10, REV 56.
MAIN CARGO DECK FLOOR PANEL POSITION 2L HAS .5" DIA PUNCTURE. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320-969.
INSPECTION TYPE:C, HORZ STAB RT LOWER AIRGATE FAIRING CUTOUT FWD SKIN PANELS FOUND CRACKED. HORZ STAB RT LOWER AIRGATE FAIRING CUTOUT FWD SKIN PANEL REPAIRED IAW SRM 53-80-01-2R3, REPAIR 3, FIG 201, REV49. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.
INSPECTION TYPE:7C, LT 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 49.
INSPECTION TYPE:7C, 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 49.
INSPECTION TYPE:C, MCD FLOOR PANEL FOUND DEEP GOUGE RUN THROUGH TOGETHER WITH 5 DENTS MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.
INSPECTION TYPE:C, MCD FLOOR PANEL FOUND 8 DENTS AND 7 PUNCTURES AT STA 833 TO 930 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.
INSPECTION TYPE:C, DMI D449761 - MAIN CARGO POSITION 6R OTBD FLOOR PANEL INTERIM REPAIR. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.
INSPECTION TYPE:C, FX - WING CTR TANK FRONT SPAR VERTICAL STIFFENER UPPER AREA FOUND CRACK JUST AT STA 785.9, RBL 10.94. STIFFENER REPAIR IAW HX RS R57-10-37013, REV A & EO B767-5710-42201-A AT STA 785.9 RBL 10.94, ORG MAT;L BAC1518-749-2024T3511, CRK LENGTH IS 1" CUT OFF LENGTH IS 19.5", THIS CLASSIFIED AS MAJOR REPAIR WITH MAT'L BAC1518-749-2024T3511 STIFFENER REPLACE SECT, 2024T351-0250IN & 2024T3-0100IN STRAP & 7075T651BARE0250IN CLEVIS PLATE, TOTAL L 24"
INSPECTION TYPE:C, MAIN EQUIPMENT CTR STA 246, LBL 40 FLOORBEAM VERTICAL STIFFENER FOUND CRACK. STIFFENER REPAIRED IAW SRM 53-10-51-2R4 REPAIR 4, FIG 201, REV 49. ORG MATL BAC1490-2793-7075T62 CRK LENGTH 1.1" REPAIR CLASSIFIED AS MAJOR REPAIR REPEAT INSP AT 3000 FLT CYCLES OR 24 MONTHS WHICH EVER OCCUR FIRST IS REQUIRED IAW SRM 53-10-51-2R4. REPAIR 4, FIG 201, REV 49 REPAIR LENGTH IS 14.6".
INSPECTION TYPE:N/A FLOORBOARD DAMAGED POS 2R. FABRICATED NEW PANEL IAW EO B767-5320-9693-F.
INSPECTION TYPE:N/A D-403978 MAIN CARGO DECK POS 2R FLOOR PANEL INTERIM REPAIR. REPLACED PANEL PER EO767-5320-9693-F.
INSPECTION TYPE:6C OUTER CYLINDER INNER WALL FOUND SEVERAL AREA CHIPPED. RT MLG OUTER CYLINDER INNER WALL NICK MARKS REPAIR CUTOUT AS PER HX RS R32-11-36300 AND IPXA EO C-3210-33050-A.
INSPECTION TYPE:C BULK CARGO STA 1502 RBL 14 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1502 RBL 14 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.
BULK CARGO STA 1518 LBL 14 INCHES FLR WEB FWD SIDE ATT STIFFENER BENT. BULK CARGO STA 1518 LBL 14 INCHES FLOOR WEB FWD SIDE ATT STIFFENER REPLACED PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.
INSPECTION TYPE:C FUSELAGE SURVEY SEQ 323-F1-04 BETWEEN BS 1427 TO BS 1435.25 AND STA 24L - 26L. AT BULK CARGO DOOR AREA PATCH FOUND. (REPAIR CURRENTLY WITH SURVEY SEQ 323-F1-05). SURVEY SEQ 323-F1-05 AT BULK CARGO DOOR SKIN REPAIRED CURRENTLY WITH SURVEY SEQ 323-F1-04 AT BETWEEN BS 1427 TO BS 1444 AND STR 24L - 26L AREA AS PER HX RS R52-36-36298, THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 2024T3 . 080" & REPAIR SIZE 14.2" X 16.5" , REFER HX NRC 50798 FOR WORKING DETAIL.
INSPECTION TYPE:C FUSELAGE SURVEY SEQ 323-F1-05 BETWEEN BS 1436.55 TO BS 1443.55 STR 24L TO 26L AT BULK CARGO DOOR SKIN AREA PATCH FOUND, NOT CORRELATED TO SRM. SURVEY SEQ 323-F1-05 AT BULK CARGO DOOR SKIN REPAIRED AT BETWEEN BS 1427 TO BS 1444 AND STR 24L - 26L AREA AS PER HX RS R52-36-36298. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 2024T3.080" & REPAIR SIZE 14.2" X 16.5".
INSPECTION TYPE:C EMP - VERTICAL STAB LT LWR EXTERIOR SURFACE AREA DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 201 REV 43.
INSPECTION TYPE:6C LT WING - NR 5 SPOILER PANEL FWD O/B CORNER DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-04 PARA 5G FIG 9 REV 43.
INSPECTION TYPE:C MEC- BS 246 CABIN FLOORBEAM FWD FACE L/G ALTERNATE DRIVE MOTOR SUPPORT ANGLE CRACKED AT LBL 25. (CRACK 1 INCH LENGTH). MEC- BS 246 CABIN FLOORBEAM FWD FACE L/G ALTERNATE DRIVE MOTOR SUPPORT ANGLE REPLACED AS PER SRM 51-10-02 AND SRM 51-40-02 REV 43 JUST AT LBL 25.
INSPECTION TYPE:C LT WING - I/B AILERON FWD UPPER L/E FAIRING CHAFE DAMAGED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4G FIG 18.
INSPECTION TYPE:C BULK CARGO STA 1518 RBL 9 FLOOR WEB FWD SIDE ATT STIFFENER BENT. BULK CARGO STA 1518 RBL 9 FLOOR WEB FWD SIDE ATT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.
INSPECTION TYPE:C BULK CARGO STA 1480 LBL 9 FLOOR WEB FWD SIDE ATT STIFFENER BENT. BULK CARGO STA 1480 LBL 9 FLOOR WEB FWD SIDE ATT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.
INSPECTION TYPE:C BULK CARGO STA 1439 LBL 16 FLOOR WEB FWD SIDE ATT STIFFENER BENT. BULK CARGO STA 1439 LBL 16 FLOOR WEB FWD SIDE ATT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.
INSPECTION TYPE:C BULK CARGO STA 1502 LBL 20 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1502 LBL 20 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.
INSPECTION TYPE:C BULK CARGO STA 1480 LBL 14 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1480 LBL 14 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.
INSPECTION TYPE:C BULK CARGO STA 1439 LBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1439 LBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.
INSPECTION TYPE:C BULK CARGO STA 1502 RBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1502 RBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.
INSPECTION TYPE:C BULK CARGO STA 1439 RBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1439 RBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.
INSPECTION TYPE:C BULK CARGO STA 1461 LBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1461 LBL 9 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.
INSPECTION TYPE:C BULK CARGO STA 1439 LBL 22 FLOOR WEB FWD SIDE ATTACH STIFFENER BENT. BULK CARGO STA 1439 LBL 22 FLOOR WEB FWD SIDE ATTACH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.
INSPECTION TYPE:N/A D396289 - 1 HOLE FOUND AT 7TH FLOOR PANEL FROM LT POS 12R ZONE 2 (PUNCTURE .75 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.
1 HOLE 5TH FLOOR PANEL FROM LT SIDE POS 4L ZONE 2. FLOOR PANEL REPLACED AND INSTALLED AS PER EO B767-5320-9693-E.
INSPECTION TYPE:N/A FX - THE UPPER GPS ANTENNA NOT INSTALLED AT THE CORRECT LOCATION. FUSELAGE THE UPPER GPS ANTENNA EXISTING CUTOUT REPAIRED AT BS 654+33 BL 0 AS PER RS R53-00-36295 REV A. REPEAT INSPECTION IS REQUIRED AS PER HX RS R53-00-36295 REV A SHEET 2. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH .125 INCH DOUBLER REPAIR SIZE 6.5" X 11.5", REF IPXA EO B767-5330-33047-A.
INSPECTION TYPE:C D396293 - 1 HOLE FOUND AT 3RD FLOOR PANEL FROM LT SIDE POS 2L ZONE 2 (PUNCTURE .5 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.
1 HOLE 5TH FLOOR PANEL FROM LT SIDE POS 5R ZONE 2. FLOOR PANEL REPLACED AND INSTALLED AS PER EO B767-5320-9693-E.
INSPECTION TYPE:C DMI D396284 - 1 HOLE FOUND AT 7TH FLOOR PANEL LT SIDE POS 9R ZONE 1 (PUNCTURE .75 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.
INSPECTION TYPE:C DIM D396283 - 1 HOLE FOUND AT 8TH FLOOR PANEL FROM LT SIDE POS 8R ZONE 2 (PUNCTURE 1 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.
INSPECTION TYPE:C DMI D396290 - 1 HOLE FOUND AT 8TH FLOOR PANEL FROM LT SIDE POS 12R ZONE 2 (PUNCTURE 1 INCH DIA.) FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.
INSPECTION TYPE:C DMI D396287 - 1 HOLE FOUND AT 5TH FLOOR PANEL FROM LT SIDE POS 12R ZONE 1 (PUNCTURE .75 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.
INSPECTION TYPE:C DMI D396285 - 1 HOLE FOUND AT 1ST FLOOR PANEL FROM LT SIDE POS 12L ZONE 1 (PUNCTURE 1 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.
INSPECTION TYPE:C DMI D396292 - 1 HOLE AT 5TH FLOOR PANEL FROM LT SIDE POS 2R ZONE 2 (PUNCTURE 1 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.
INSPECTION TYPE:C DMI D396280 - 1 HOLE FOUND AT 7TH FLOOR PANEL FROM LT SIDE POS 6R ZONE 2 (PUNCTURE .5 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.
INSPECTION TYPE:C DMI D396282 - 1 HOLE FOUND AT 5TH FLOOR PANEL FROM LT SIDE POS 8R ZONE 2 (PUNCTURE .5 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.
POS 8R FLOOR PANEL HAS 6 DENTS. FLOOR PANEL REPLACED AND INSTALLED AS PER EO B767-5320-9693-E.
1 HOLE 1ST PANEL FROM LT SIDE POS 2L ZONE 1. FLOOR PANEL REPLACED AND INSTALLED AS PER EO B747-5320-9693-E.
1 HOLE 5TH FLOOR PANEL FROM LT SIDE POS 6R. FLOOR PANEL REPLACED AND INSTALLED AS PER EO B767-5320-9693-E.
INSPECTION TYPE:C RT WING - O/B FLAP I/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A FIG 10 REV 43.
INSPECTION TYPE:6C MAIN DECK FLOOR SUPPORT ATT ANGLE FOUND CRACKED JUST AT STA 1575 LBL 75-76. MAIN DECK FLOOR SUPPORT ATT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT STA 1575 LBL 75-76.
INSPECTION TYPE:C LT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG FLANGE FOUND CRACKED (CRACK I/B FLANGE 1.125 INCH AND O/B FLANGE 1 INCH). LT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 43. THIS IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL AND 10134-2007-7075T6511, REPAIR SIZE 2 X 2 INCHES.
INSPECTION TYPE:C D396288 - 1 HOLE FOUND AT 5TH FLOOR PANEL FROM LT SIDE POS 12R ZONE 1 (PUNCTURE .5 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.
INSPECTION TYPE:6C SURVEY SEQUENCE 323-F1-03 BETWEEN BS 1197+110 TO BS 1197+130 AND STR 24R-26R AREA SKIN REPAIR IS NOT CORRELATED TO SRM. SKIN REPAIRED AS PER HX RS 53-60-36299 REV A. REPEAT INSP IS REQUIRED AS PER HX RS 53-60-36299 REV A. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH DOUBLER 2024T3.125" AND STRUCTURAL FILLER 2024T3.100", REPAIR SIZE 22.75" X 26.5" AND REFER EO B767-5330- 33048-A.
INSPECTION TYPE:C DMI D396295 - 3 HOLES FOUND AT 3RD FLOOR PANEL FROM LT SIDE POS 4L ZONE 2 (ALL PUNCTURE .5 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.
INSPECTION TYPE:C DMI D396291 - 1 HOLE FOUND AT 1ST FLOOR PANEL FROM LT SIDE POS 13 ZONE 2 (PUNCTURE .75 INCH DIA). FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R REV 43 FIG 201.
INSPECTION TYPE:C CTR TANK FRONT SPAR STIFFENER UPPER END AT LBL 10 FOUND CRACK (CRACK 2.125 INCH LENGTH). FWD CARGO COMPT WING CTR TANK FRONT STIFFENER AT LBL 10 WL 178.96, APPROX REPAIRED AS PER HX RS R57-11-36294 REV A. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH REPAIR STRAP 202473 .250" & .100" WITH REPAIR LENGTH 19.25" IPXA EO B767-5710-33014-A.
INSPECTION TYPE:C MAIN DECK FLOOR SUPPORT ATT ANGLE FOUND CRACKED JUST AT STA 1575 RBL 75-76 (CRACK 1.5 INCH LENGTH). MAIN DECK FLOOR SUPPORT ATT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.
INSPECTION TYPE:6C FX - SURVEY SEQUENCE 323-F1-02 A PROTRUDING HEAD FASTENER AREA DENT AND 2 LOC. DENT CLOSE TO THE EXISTING FLUSH REPAIR FOUND. SURVEY SEQUENCE 323-F1-02 LOCATION A FASTENER REMOVED AND REPLACED AS PER HX RS R53-31-36297 REV A. EXTERNAL AND INTERNAL DETAIL VISUAL INSPECTION AND HFEC INSPECTION CARRIED OUT AS PER HX RS R53-31-36297 REV A. NIL DEFECT FOUND CRACK FREE. THIS REPAIR CLASSIFIED AS A CATEGORY A REPAIR. REF IPXA EO B767-5330-33045-A.
INSPECTION TYPE:C AFT CARGO DOOR MANUAL DRIVE SYS CHK FOUND FWD PDU EXCESSIVE MOVEMENT CAUSED THE PDU MOUNTING UPR STRUCTURE CRACKED. (CRACK 1.25 INCH LENGTH). AFT CARGO DOOR PDU MOUNTING UPPER WEB AND DOUBLER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43. (WEB P/N: 143T6312-502).
INSPECTION TYPE:N/A SEAT TRACK DAMAGED AT STA 1518 RBL 33. REPAIRED PER EO B767-5310-32616-B.
INSPECTION TYPE:6C DMI NR D395403, MAIN CARGO AFTER CENTER OF POS 4 HAS 2 EACH 2 INCH CRACK IN FL FLOOR PANEL. FLOOR PANEL REPLACED AND INSTALLED AS PER EO B767-5320-9693-E.
INSPECTION TYPE:N/A MAIN CARGO DOOR FLOORBOARD PANEL DAMAGED AT POS 13 REF D 392745. REMOVED FLOOR PANEL FOR REPAIR/REPLACEMENT. REMOVED AND REPLACED POS 13 FLOOR PANEL PER EO B767-5330-9693 APPX B. THIS CLEARS D 392745.
INSPECTION TYPE:N/A CENTERLINE FLOOR PANEL CRACKED AT POSITION 8. REMOVED PANEL AND ROUTED TO SHEET METAL FOR REPAIR. INSTALLED CENTERLINE FLOORBOARD PANEL AT POS NR 8 ON MCD PER EO B767-5320-9693E.
REF LOG PAGE 842810ITEM 3 DI 392745 MC FLOOR PANEL AT POS 13 DAMAGED. FABRICATED NEW FLOOR PANEL PER EO B767-5320-9693E
INSPECTION TYPE:N/A RIGHT I/B MAIN FLAP DENTED OUT OF SRM LIMITS. REPAIRED PER EO B767-5750-30895-A.
INSPECTION TYPE:N/A, NR 1 BRAKE FIRE ON ARRIVAL, FUSE PLUGS MELTED. CFR WAS CALLED DUE TO FIRE.
INSPECTION TYPE:N/A L1 DOOR EMERGENCY EXIT LIGHT HOLDING BRACKET NEEDS RE-SECURED. RE-SECURED LIGHT ASSY USING STANDARD MX PRACTICES, CHAP 20.
INSPECTION TYPE:ETOP ATB - EICAS MSG R GEN DRIVE DISPL, GEN DRIVE LIGHT ILLUMINATED, GEN DRIVE DISCONNECTED. SERVICED OIL TO PROPER LEVEL, RECONNECTED NR 2, IDG RAN ENGINE. OPS CHECKS GOOD.
INSPECTION TYPE:N/A EMERGENCY LIGHTS SWITCH ON OVERHEAD PANEL DOES NOT WORK PROPERLY. OPS CHECK EMERGENCY LIGHT SWITCH IAW MM 33-51-00, OPS CHECK GOOD.
LEFT SUPERNUMARY SEAT INTERTIAL RESTRAINT INOP. REMOVED AND REPLACED RESTRAINT IAW MM 25-11-00-6. OPS CK NORMAL.
INSPECTION TYPE:N/A LEFT WING I/B AILERON I/B HINGE SUPPORT FRAME CRACKED BETWEEN UPPER TWO FASTENER HOLES AND OUT TO THE LOWER FASTENER EDGE. REPAIRED LEFT WING INBOARD AILERON INBOARD HINGE SUPPORT FRAME PER EO B767-5740-27949-A.
INSPECTION TYPE:ETOP NO APU BLEED AIR. BTB FOR EXTERNAL AIR CART. C/O OPERATIONAL TEST OF APU BLEED AIR IAW AMM 49-52-00-00. FOUND SATISFACTORY.
INSPECTION TYPE:C SEAT TRACK FLANGES GOUGED AT BS 632-654+20 RBL 54 WL 200. REMOVED AND REPLACED SEAT TRACK SECTION BS 621-654+55 RBL 54 IAW ER 07 07-1909 AND SRM 53-00-52-2R 9 FIG 201.
INSPECTION TYPE:ETOP ON TAKEOFF ROLL OUT OF CGN AIRCRAFT A SLIGHT ODOR OF RUBBER AND VIBRATION IN THE NOSE WHEEL THAT STARTED SLIGHT AND BECAME MODERATE TO S EVERE. CREW REQUEST EMERGENCY SUPPORT UPON LANDING IN EWR FOR SUSPECTED BLOWN NOSE TIRE. AIRCRAFT LANDED WITHOUT INCIDENT IN EWR. MX FOUND LT AND RT NOSE TIRE PROPERLY INSTALLED AND SERVICED. HOWEVER BOTH TIRES WHERE SEVERLY OUT OF ROUND. REMOVED AND REPLACED BOTH TIRE ASSY. AIRCRAFT DEPARTED AND LANDED IN SDF WITH NO FURTHER REPORT.
INSPECTION TYPE:C3 NR 9 SLAT OB DRIVE ARM OB RIB AT OFSS 651 IS CRACKED ON FORWARD FLANGE. REPAIRED NR 9 SLAT OB DRIVE ARM OB RIB AT OFSS 651 IAW GOODRICH ER NR 03-3162
INSPECTION TYPE:PFLT SKIN BUCKLED AT NOSE JACK POINT STA 287. REMOVED FASTENERS THROUGH SKIN IN DENTED AREA IAW SRM 51-40-02. INSTALLED 90 PERCENT OF FASTNERS THAT WERE REMOVED AT BX 287 NOSE JACK POINT IN DENTED AREA IAW SRM 51-40-02. REMAINING FASTENERS FOUND TO BE COMMON TO FRAME REPAIR AT BS 287.
WHEN CHECKING FLIGHT CONTROLS BEFORE ENGINE START, THE RIGHT OUTBOARD AILERON STUCK IN THE FULL UP POSITION WITH CONTROL YOKE IN NEUTRAL. ORDERED RIGHT AILERON (OUTBOARD) INBD PCA. EMP 25110 ACCOMPLISHED FIM B-767 27-11-00 NO PROBLEMS FOUND PCU OPERATE NORMALLY. LUBRICATED AILERON HINGES FOR PRECAUTIONARY SYSTEM 1 CHECKS NORMAL A/C OK FOR SERVICE (NO EICAS MESSAGES FOUND)
CENTER HYDRAULIC QTY DECREASED TO 0.07. SYSTEM DEPRESSURIZED AND LEAK CONTINUED. ***MRR FILED AS OPEN*** AWAITING LOG PAGE CORRECTIVE ACTION ENTRIES FOUND SPOILER ACTUTATOR LEAKING AT PLUG BELOW SERVO VALVE ON ACTUATOR JUST OUTBOARD OF INBOARD AILERON. REPLACED O-RINGS & SERVICED CENTER HYD SYSTEM. OP''S CHK''S OK. - NO LEAKS.