N831MH
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
ATO - ABORTED TAKEOFF AT 80 KTS DUE TO LEFT ENGINE STALL. FOUND HMU CRACKED AND SPRAYING FUEL. REPLACED SAME AND PERFORMED BSI DUE TO REPORTED COMPRESSOR STALL WITH NO ISSUES. (8392736)(AIRCRAFT GROUNDED)
ATB- DUE TO AUTO PRESSURIZATION CONTROL INOP. REPLACED AUTO PRESSURE CONTROL MOTORS. REPLACED OUTFLOW VALVE. OPS CHECK NORMAL. (8831542) (AIRCRAFT GROUNDED)
SLIDE INDICATOR LIGHT INOP OR DAMAGED. : REPLACED DOOR 4L SLIDE LIGHT NOW OPS NORMAL. OK FOR SVC. (1596106) (AIRCRAFT GROUNDED)
NR 1 PYLON UPPER WEB INBD SKIN EDGE CRACK AT NAC STA 227. REPAIRED AS PER PRI 633072-14 (1512680)
NUMBER 1 PYLON FWD UPPER SPAR WEB POWER FEEDER CABLE CUTOUT CRACK. CORRECTIVE ACTION: REPAIRED AS PER PRI 633071-14 (1510893)
CABIN WET AREA FLOORBEAMS UPPER SURFACE FOUND CORROSION AT STA 347,RBL39. DAMAGED FLOORBEAM REPAIRED AS PER PRI 632985-14 (1510899)
DURING H CHK AT STAG, A CRACK WAS FOUND ON THE NR 1 NACELLE RT UPPER SPAR CHORD. REPAIRED IAW ER/A 633072-14AD. (AIRCRAFT GROUNDED)
CRACKS WERE NOTED ON THE #1 PYLON FWD UPPER SPAR WEB. ACCOMPLISH ER/A 633071-14AD (1508369)
VERTICAL STABILIZER AUXILIARY SPAR WEB 30IN BELOW 321D LWR EDGE FOUND CRACK. REPAIRED AS PER PRI 632961-14 (1507497)
VERTICAL STABILIZER, LT SURFACE BTW AUXILIARY SPAR AND FRONT SPAR AROUND FSS 40 FOUND BULGE. REPAIRED VERTICAL STABILIZER LT SURFACE BTW AUXILIARY SPAR AND FRONT SPAR AROUND FSS 40 IAW SRM 55-30-01-2R-1 AND SRM 51-70-10-2R-4, REV 77. (LP 1501546)
AIRCRAFT 1807, A CRACK DAMAGE WAS FOUND ON THE STIFFENER, WHICH IS LOCATED ON THE COCKPIT FLOOR BEAM AT STA 246, AT LBL 40.00. CORRECTIVE ACTION: REPLACED STIFFENER AND FABRICATED REPAIR DOUBLER AND INSTALLED PER ER/A 612861-14. (LP 1498790).
SECTION 48 RT SKIN AT BS 1730, WL 200 FOUND ABRASION. THE ABRASION ON SECTION 48 RT SKIN AT BS 1730, WL 200. REMOVED AND MEASURED: FOUND OUT OF LIMITS IAW SRM 53-80-70-1A-1, FIG 101, REV 77. DAMAGE SKIN REPAIRED IAW SRM 53-80-01-2R-3, REV 77. (LP 1495387)
CABIN SEAT TRACKS UPPER FLANGE SURFACE FOUND CORRSION AT BS 1480, RBL 54.75. THE CORROSION ON SEAT TRACK UPPER FLANGE AT BS 1480, RBL 54.75. REMOVED AND MEASURED, FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1, FIG 101, REV 77. THE DAMAGE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R-15, REV 77. (LP 1495404)
SECTION 48 LEFT SKIN AT BS 1730, WL 200 FOUND ABRASION. ABRASION ON SECTION 48 LT SKIN AT BS 1730 WL200 REMOVED AND MEASURED, FOUND OUT OF LIMIT IAW SRM 53-80-70-1A-1, FIG 101, REV 77. THE DAMAGE SKIN REPAIRED IAW SRM 53-80-01-2R-3, REV 77. (LP 1495385)
BULK CARGO SHEAR TIE FOUND CORROSION AT STA1417 BETWEEN S37L AND S36L. THE SHEAR TIE REMOVED AND REPLACED AS PER B767-400 SRM 51-40-02. (1490818)
BULK CARGO SHEAR TIE FOUND CORROSION AT BS 1417 BETWEEN S38L AND S37L, REFER TO CPCP TASK 53-584-00. CORRECTIVE ACTION: REMOVED AND REPLACED AS PER B767-400 SRM 51-40-02. (1490815)
SHIP 1807 RECIEVED MASTER WARNING WITH TAKEOFF CONFIGURATION WARNING. SAW FLAPS EICAS BUT FLAPS WERE SECURED AT 15 DETENT. CORRECTIVE ACTION: R/R FSPM M839 REF. B767/400 AMM 27-58. (6704694).
SHIP 1807 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:606. CORRECTIVE ACTION: SECURED 3R EXIT SIGN COVER ALL CKS NRML (0795707)
1807 EMER LIGHTS RT AFT COLUMN INOP. CORRECTIVE ACTION: RPLCD CHARGER & BATTERY (M734) PER 767-400 AMM 33-51-07 TEST OK (4001705)
SHIP 1807 DURING SVC FOUND EMERG LIGHT INOP FROM SEAT 50 TO 56. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERY PACK M734 AFT RIGHT PER B767 AMM 33 -51 OPS OK (5657768)
SHIP 1807 3L MAIN DOOR ARMED INDICATOR STAYS ILLUM AT FAP & DOOR. CORRECTIVE ACTION: RR PSEU PER B767400 MM 3209 3L DOOR ARMED INDICATION CKS GOOD PER B767400 MM 6273 MEL/PLAC RMVD (5749429)
SHIP 1807 3L MAIN DOOR ARMED INDICATOR STAYS ILLUM AT FAP & DOOR. CORRECTIVE ACTION: RR PSEU PER B767400 MM 3209 3L DOOR ARMED INDICATION CKS GOOD PER B767400 MM 6273 MEL/PLAC RMVD (5749428)
SHIP 1807 -MISC/DE- CTR HYD SYS QUANTITY DECREASED DURING FLIGHT. QRH C/W AND FLIGHT CONTINUED TO DESTINATION. EMERGENCY DECLARED FOR LONGER RUNWAY. A/C TAXIED TO GATE UNDER OWN POWER. CORRECTIVE ACTION: REPLACED C1 AND C2 ELEC HYD PUMPS. CHECKED FILTERS AND REPLACED ADP FILTER DUE TO DPI EXTENDED. (LP 5632878)
SHIP 1807 -GEAR- ALTERNATE GEAR EXTEND SYSTEM USED TO LOWER LANDING GEAR DUE TO CTR HYD SYSTEM QUANTITY LOSS. CORRECTIVE ACTION: REPLACED INBOARD ALTN DRIVE SLAT MOTOR, AND OUTBOARD SLAT PDU CONTROL VALVE MODULE. (LP 5632858)
AIRCRAFT 1807, ON SVC CK FOUND EMERGENCY LIGHTS ON LEFT FRONT ROW MONUMENT AND SEATS 1-5 INOP. CORRECTIVE ACTION: FOUND WIRE W820-124-20 BROKEN AT D96121P, REPLACED SOCKET. (LP 5632865)
SHIP 1807 PRIOR TO PUSH ALL SLIDE LIGHTS WENT OUT, PURSER PANEL DOOR LIGHTS WENT OUT. ELECTRICAL BURNING SMELL AND DOORS ARMED WARN CIRCUIT BREAKER POPPED. CORRECTIVE ACTION: T/S PER B767-400 WDM 52-73-11 AND FOUND L1 DOOR SLIDE INDICATOR RECEPTACLE SHORTED OUT. REMOVED AND REPLACED L1 ALARM SIGNAL MODULE IAW B767-400 AMM 52-73. OPS CHECK GOOD. CYCLED ARM/DISARM L1 DOOR HANDLE AND VERIFIED DOORS ARMED WARNING CIRCUIT BREAKER DID NOT POP. A/C OK FOR SERVICE (5393458)
SHIP 1807 L1 DOOR SLIDE LIGHT INOP. CORRECTIVE ACTION: REPLACED SLIDE LIGHT NOW OPS NML REF B767-400 AMM 52-72 (5036242)
SHIP 1807 LH ELEVATOR, TRAILING EDGE WEDGE WITH HOLE AT ELEV STA 200.46 + 11.800 INCHES. CORRECTIVE ACTION: LH OUTBOARD ELEVATOR, CRACK WAS EVALUATED AND REQUIRE REPAIR AS PER B767-400 SRM 55-20-01-1A-1 FIG. 101 TABLE 1 NOTE B. REV 68 MAY-16-23 OUTBOARD ELEVATOR UPPER SKIN TO LOWER SKIN WERE REPAIRED AS PER B767-400 SRM 51-70-04 (0043676)
SHIP 1807 ERA 612861-14 ISSUED FOR REPAIR AND BLIND RIVET INSTL TO FLOOR B EAM STIFFENER AT STA 246, LBL 40. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: ACCOMPLISH ERA 612861-14 SECTION II INSPECTIONS EVERY 1500 CYCLE S AFTER SECTION 1, OR EVERY 456 DAYS, FIRST TO OCCUR.ACCOMPLISH SECTION III PERMANENT REPAIR THE FIRST OF EITHER: NEXT HCK OR 3 000 FLIGHT CYCLES OR 912 DAYS AFTER SECTION I. (0036179)
SHIP 1807 DURING C2 VISIT AT MEX, FUSELAGE DENT DAMAGE WAS NOTED AT STA 1502, STR 31L. CORRECTIVE ACTION: ACCOMPLISH ER/A 612802-14 SECTION II REPEAT INSPECTIONS WITHIN 30,000 TOTAL FLIGHT CYCLES (0032561)
SHIP 1807 DAMAGE PREVIOUSLY EVALUATED BY DELTA UNDER LOG 8209111. SCRATCH ON LH FUSELAGE SKIN AT STA 1538 AND STGR 35. CORRECTIVE ACTION: PERMANENT REPAIR ON LH FUSELAGE SKIN BETWEEN STA 1540 AND STGR 35 LH WAS PERFORMED PER ER/A 612712-14AD (0046915)
SHIP 1807 ERA 612712-14AD ISSUED FOR SKIN REPAIR TO STA 1540, STRINGERS 34 L - 37L, FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: ACCOMPLISH ERA 612712-14AD SECTION II AT 30000 TOTAL FLIGHT CYCL ES ON THE AIRFRAME, THEN EVERY 3000 FLIGHT CYCLES THERAFTER ASSOCIATED ER/A 00-612712 (0026607)
SHIP 1807 DAMAGE PREVIOUSLY EVALUATED BY DELTA UNDER LOG 8209109. DENT ON LH FUSELAGE SKIN AT STA1499 AND 1.500" ABOVE STGR 31. CORRECTIVE ACTION: PERMANENT REPAIR ON LH FUSELAGE SKIN AT STA1499 AD 1.500" ABOVE STGR 31, WAS PERFORMED PER ER/A 612802-14 (0044908)
SHIP 1807 CABIN FLOOR STRUCTURE SECTION 41. FRONT FACE OF FLOOR BEAM STA 246 WITH STIFFENER BROKEN LBL 40. CORRECTIVE ACTION: CABIN FLOOR STRUCTURE SECTION 41 FRONT FACE OF FLOOR BEAM STA 246 LBL 40. STIFFENER WAS REPLACED I.A.W B 767-400 ER/A 612861- 14 (0044905)
SHIP 1807 EXTERNAL SKIN WITH PROTUDING DENT BETWEEN STA 1329 AND 1351 &S- 35L AND S34L. CORRECTIVE ACTION: EXTERNAL SKIN, STA 1329 AND 1351, STGR 35L AND 34L WAS REPAIRED I.A.W B767-400 SRM 53-00-01-2R- 29. ALSO INTERVAL INSPECTION 9.000 FC EXTERNAL DETAIL INSPECTION I.A.W. B767-400 SRM 53-00-01-2R-29 TABLE V A REV. 68.00 MAY 16/23 DECAL MONITOR ESTABLISHED. (0034381)
SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:602. CORRECTIVE ACTION: REPLACED MISSING LENS CAP - OPS NML. REF B767-400 AMM 52-71. MEL AND PLAC RMVD.
SHIP 1807 ROW 50AB TO 54AB EMERG PATH LIGHTS INOP. CORRECTIVE ACTION: FOUND CONNECTOR AT ROW 55AB OFF, RESECURED SAME OPS CKS OK (4465207)
SHIP 1807 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:000. CORRECTIVE ACTION: R/R LIGHT ASSY (MPN: 52-0385-501) & OPS CHK NML PER B767-400 AMM 52-73. MEL CLEARED & PLAC REMOVED. (2912565)
SHIP 1807 -ATB -TO LHR DUE TO RIGHT ENGINE OIL FILTER STATUS MESSAGE. CORRECTIVE ACTION: T/S PER B767-400FIM, OIL FILTER AND MASTER CHIP DETECTOR CHECK OK-NO DEBRIS NOTED. FORWARD MESSAGE TO MEL. REPLACED OIL PRESS SWITCH, OPS CHK GOOD. (4964861)
SHIP 1807 DURING DESCENT @ 8000 ENG AND WING ANTI ICE WAS SELECTED ON. SHORTLY AFTER FUMES WERE EXPERIENCED ON THE FLIGHT DECK. CORRECTIVE ACTION: NO GO ODI. AS REQUESTED BY MCC. PERFORMED ENGINE RUN WITH BOTH ENGINES, PACKS ON AND WING AND THERMAL ENGINE ANTI ICE ON. NO ABNORMAL SMELL OR FUMES NOTED. IN FLIGHT DECK AND CABIN. B767- 400 AMM 71-00-00-862-020-H03 AND 30-11 AND 30-21. (4964810)
AIRCRAFT 1807, 4L DOOR INDICATION. CORRECTIVE ACTION: REPLACED PSEU. (LP 4872932)
SHIP 1807 OVERHEAD COCKPIT ENTRY LIGHT/EMER LIGHT INOP. CORRECTIVE ACTION: FOUND BATTERIES DEAD. REPLACED BATTERIES. OVERHEAD COCKPIT EMER LIGHT NOW CKS GOOD PER AMM 33-51 (4714397)
SHIP 1807 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: TESTED 2L SLIDE LIGHT. WHEN TESTED ARMED LIGHT COMES ON AT 2L AND FWD FA PANEL. WHEN 2L ARMED , ARM LIGHT ILLUMINATED. REF B767 AMM 52-73. MEL/PLAC RMVD (2749568)
SHIP 1807 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:602. CORRECTIVE ACTION: FOUND SLIDE LENS DISCARDED FROM HOUSING. RE-INSTALLED LENS. OPS CHECKED GOOD NOW. (2739453)
SHIP 1807 E-PATH LIGHTS INOP FROM ROW 33G TO 38G. CORRECTIVE ACTION: REPLACED BATTERY AT 35 RIGHT REF B767 AMM 33-51 OPS OK (9890228)
SHIP 1807 AT PUSHBACK WHEN ARMING DOORS, C/B T35 POPPED. CORRECTIVE ACTION: RE LAMPED & RE SEATED INDICATOR ON R-1 DOOR. OPERATIONALLY CHECKED ALL PASSENGER SERVICE DOORS PER B767-400 AMM 52-11. NO DISCREPANCIES NOTED. (4638561)
SHIP 1807 R1 DOOR ARM LIGHT INOP. CORRECTIVE ACTION: RESEATED AND CLEANED LED CONNECTIONS. R1 ARMED LIGHT NOW CHECKS GOOD. MEL AND PLACARD REMOVED. (4126086)
SHIP 3L SYMBOL ON EXIT LIGHTING UPSIDE DOWN. 1807CORRECTIVE ACTION: EXIT SIGN ADJUSTED. OPS TEST OK. REF. B767-400 AMM 33-51. (2660582)
SHIP 1807 3L SYMBOL ON EXIT LIGHTING UPSIDE DOWN. CORRECTIVE ACTION: EXIT SIGN ADJUSTED. OPS TEST OK. REF. AMM B767-400 AMM 33-51. (2660581)
SHIP 1807 1R DOOR 'SLIDE' STATUS WARNING LIGHT LENS MISSING. CORRECTIVE ACTION: RPLD 'SLIDE' LENS. OPN GOOD AT 1R DOOR. REF B767-400 AMM 52-73 (9683192)
MULTIPLE INTERIOR EMERGENCY LIGHTS (SEAT, CEILING + OVERHEAD EXIT LIGHTS ) INOP ON RH SIDE. FOUND CIRCUIT BREAKERS P25 P27 OUT. RESET CIRCUIT BREAKERS , EMERGENCY LIGHTS. OPS CHECK GOOD.
SHIP 1807 SEAT MOUNTED EMERGENCY LIGHT OUT LEFT ROW FROM SEAT 33-38. CORRECTIVE ACTION: R/R POWER SUPPLY (M737) BATTERY PER B767-400 AMM 33-51.OPS CKD OK. (9509950)
SHIP 1807 REF SERVICE CHECK L3 EXTERNAL EMERGENCY LIGHT INOP. CORRECTIVE ACTION: BULB REPLACED NO HELP. HOLDER CHECKED FOUND OK BATTERY PACK REMOVED PLUG CLEANED FUSE X3 REPLACED FUNCTION CHECKED EMERGENCY LIGHTS ALL OPS NML IAW B767-400 AMM 33-51-07-962-024-01 A/C OK (9408925)
SHIP 1807 DURING SVC CHECK FOUND EMER LIGHTS INOP AISLE 41-49 A/B. T/S PER B767-400 FIM 3-51-00-815-803 AND WDM 33-51-19. REPLACED BATTERY AND PWR SUPPLY M7236 (ROW 43 AB). (9391696)
SHIP 1807 4L DOOR WOULD NOT ARM. CORRECTIVE ACTION: CYCLED DOOR ARMING LEVER SEVERAL TIMES OPS CKS GOOD IAW B764 52-12 A/C OK FOR SVC. (9088364)
SHIP 1807, SUPPLEMENTAL INFORMATION, -ATO- @ 55 KNOTS DUE TO RT FWD (R1) SERVICE DOOR OPEN INDICATION. CORRECTIVE ACTION: DEFERRED PER MEL 52-71-01-REPLACED RIGHT FWD ENTRY DOOR PROX SENSOR "S196". (6099772)
SHIP 1807 ON TO ROLL AT 75 KTS R FWD ENT DOOR EICAS MESSAGE ILLUMINATED FO R1 SEC THEN DISAPEARED ON CLIMB PRESSURIZATION NORMAL. IT RESET OUR OUT TIME ON ACARS. CORRECTIVE ACTION: PERF DOOR WARNING SENSOR TEST PER B767-400 AMM 52-71 AND ALL NML (6099742)
SHIP 1807 MULTIPLE EMERGENCY LIGHTS OUT @ ROW 1, ROW 31, AND DOORS L3 & R3, CORRECTIVE ACTION: R/R EMER LIGHT POWER SUPPLY +BATTERY @ ROW1, R/R BATTERY @ ROW31 , R/R BATTERY @ AFT RH FA SEAT REF B767 AMM 33-51. OPS CHECK GOOD. (6099706)
SHIP 1807 PANEL @ 3R DOOR CAME LOOSE. CORRECTIVE ACTION: RESECURED 3DR DOOR SLIDE BUSTLE PER B767-400 AMM 25-66. OK FOR SVC (8626130)
SHIP 1807 4L DOOR WILL NOT ARM. CORRECTIVE ACTION: GREASED GIRT BAR ARMING MECHANISM. 4L DOOR ARMS NORMALLY IAW B767-400 AMM 12-21 (8209158)
WHILE WORKING SVC CK FOUND SECTION OF EMERGENCY LIGHTS OUT FROM 6A- L2 DOOR. R/R EMERGENCY LIGHT BATTERY PACK IN CEILING ABOVE SEAT 7A PER B767-400 AMM 33-51. OPS CKS GOOD. (LP# 8115134)
SHIP 1807 MAINTENANCE FOUND L/H NO.4 SLAT TRAINING EDGE LOWER SURFACE SCRATCH AT 53 INCHES TO O/B EDGE. CORRECTIVE ACTION: REPAIRED PER SRM 51-70-10. (LP 1946360)
SHIP 1807 DURING CABIN EMERGENCY LIGHTS TEST MAINTENANCE FOUND AISLE LIGHTS INOPERATIVE FROM SEAT 35F TO 38F. CORRECTIVE ACTION: REPLACED CHARGER ASSEMBLY. SYSTEM OPERATION IS NORMAL. (LP 8009162)
SHIP 1807 ON TAKE OFF, HAD AVER BRIEF RIGHT FORWARD ENTRY DOOR MESSAGE, THAN OFF FOR DURATION OF FLIGHT. SYSTEM RESTORED ITSELF. AS A PRECAUTION CLEANED DOOR SENSOR AT R1 DOOR. SYSTEM OPERATION IS NORMAL. (LP 7573712)
MAINTENANCE FOUND R4 DOOR EXTERNAL EMERGENCY LIGHTS INOPERATIVE. FUSE IN POWER SUPPLY M0734 WAS REPLACED. SYSTEM OPERATION IS NORMAL. (LP 6225956)
ATB DUE TO GEAR DISAGREE INDICATION ON CLIMB OUT. CORRECTIVE ACTION: REPLACED MAIN LANDING GEAR SELECTOR BYPASS VALVE. JACKED AIRCRAFT AND PERFORMED GEAR SWING. SYSTEM OPERATION IS NORMAL.
ATB RETURNED TO DTW DUE TO MAIN LANDING GEAR DISAGREE INDICATION WITH GEAR HANDLE UP. BIT PSEU. ACTIVE FAULT NOTED FOR LEFT LATCHED LOCK SENSOR S238. SENSOR AND TARGET FOULED WITH GREASE. REPLACED S238 AND PSEU PER ATLMA. PERFORMED GEAR SWING. SYSTEM OPERATION IS NORMAL.
CREW REPORTS L1 SLIDE LIGHT EXTINGUISHED DURING FLIGHT. CORRECTIVE ACTION: MAINTENANCE TIGHTENED SLIDE LIGHT SCREWS. SYSTEM OPERATION IS NORMAL.
AFT LOWER CREW REST EMERGENCY LIGHTS ARE INOPERATIVE. CORRECTIVE ACTION: MAINTENANCE FOUND BATTERY MISSING FROM POWER SUPPLY AND REPLACED. SYSTEM OPERATION IS NORMAL.
DOOR 3 LEFT EXIT SIGNAL LIGHT AFT WALL INOPERATIVE. (EMERGENCY LIGHT). REPLACED LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.
FOUND LLCR THE EMERGENCY LIGHT BATTERY FAULT. REPLACED BATTERY. SYSTEM OPERATION NORMAL.
NO.2 PYLON AFT FAIRING I/B ACCESS DOOR L/E FOUND EROSION. REPAIRED PER SRM 51-70-04. (LP 1330747)
MTC TASK-AFT CARGO ROLLER TRAY AT STA1153 AND LBL 6.5 FOUND CORROSION. REPAIRED THE AFT CARGO ROLLER TRAY AT STA1153 AND LBL 6.5 AS PER PRI 581515-14 REV.0&B767-400 SRM 53-00-53 REPAIR 1 REV.58 09/05 /2019.THE PRI 581515-14 REV.0 COMPLETED AND COMPLIED WITH ER/A 581515-14 REV.ORIGINAL. (LP1320688)
MTC TASK-#10 SLAT L/E SKIN FASTENER AROUND FOUND CRACK AT WS772. THE #10 SLAT L/E SKIN FASTENER AROUND CRACK AT WS772 REPAIRED AS PER B767-400 SRM 57-43-01 REPAIR 2 REV.58 09/05/2019. (LP1317342)
MTC TASK-#10 SLAT L/E SKIN FASTENER AROUND FOUND CRACK AT WS 694. THE #10 SLAT L/E SKIN FASTENER AROUND CRACK AT WS694 REPAIRED AS PER B767-400 SRM57-43-01 REPAIR 2 REV.58. (LP1317340)
NR 4 SLAT L/E UPPER SURFACE AT WS 616.2-642.2 FOUND CRACKED. THE SLAT L/E UPPER SURFACE WAS REPAIRED IAW SRM 57-43-01 REPAIR 2 REV.58.
NR 4 SLAT L/E UPPER SURFACE AT WS 538.2-564.2 FOUND CRACKED. THE SLAT L/E UPPER SURFACE WAS REPAIRED IAW SRM 57-43-01, REPAIR 2, REV.58.
FOUND ONE CRACK AT FWD OUTER CHORD AT S-7R STA1809, LENGTH IS 5MM,AS REMARKED. PERFORMED THE REPAIR CRACK FWD OUTER CHORD AT S-7R STA1809 IAW W/C 5310-01380-06 AND B767-400 SRM 53-80-08 REPAIR 9,REV.58 09/05/2019.PLS DO A SUPPLEMENTAL INSPECTION AS PER B767-400 SRM53-80-08 REPAIR 9,TABLE 202 FOR INSPECTION DETAIL. (LP1307005)
MTC TASK-PASSENGER CABIN FWD SERVICE DOOR R1 LOWER SILL TEE SUPPORT FOUND CORROSION.REFER TO CPCP TASK 53-674-00. TEE SPPORT AT CABIN FWD SERVICE DOOR R1 LOWER SILL CORROSION REMOVED AND THE CORROSION THROUGH THE WHOLE SECTION FOUND OUT OF LIMIT AS PER B767-400 SRM 53-00-15 REV.58 09/05/2019.THE DAMAGE TEE SUPPORT REPLACED AS PER B767-400 SRM51-40-02 REV.58 09/05/2019. (LP1303957)
MTC TASK-PASSENGER CABIN AFT SERVICE DOOR LOWER SILL TEE SUPPORT FOUND CORROSION.REFER TO CPCP TASK 53-716-00. THE TEE SUPPORT AT CABIN AFT SERVICE DOOR LOWER SILL CORROSION REMOVED AND EVALUATED AS PER B767-400 SRM 51-10-02 AND SRM 53-00-15 REV.58 09/05/2019 FOUND THE MAX.OF CLEAN UP IS 0.100", THE ORIGINAL THICKNESS IS 0.100",IT IS OUT OF LIMIT AS PER B767-400 SRM 53-00-15 REV.58 09/05/2019.THE DAMAGE TEE SUPPORT REPLACED WITH A FABRICATE TEE SUPPORT WHICH MAKE FROM AND10136-2401 7075-T6511 EXTROSION AS PER B767-400 SRM51-40-02 REV.58 09/05/2019 AND PRI 581541-14 REV.0.COMPARED WITH ER/A 581541-14 REV.ORIGINAL,FOUND NO DEVIATION. (LP1301538)
CORROSION LEVEL: 2 BULK CARGO SHEAR TIE AT STA1540 BETWEEN S-38R TO S-39R FOUND CORROSION. REPLACED SHEAR TIE.
CORRISION LEVEL 2: AFT CARGO SHEAR TIE AT STA1197+88 BETWEEN S-39L TO S- 39R FOUND CORROSION AND REPLACED. (LP 1288190)
CORRISION LEVEL 2: AFT CARGO SHEAR TIE AT STA 1219 BETWEEN S-39L TO S-39R FOUND CORROSION OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1288057)
CORROSION LEVEL 2 BULK CARGO SHEAR TIE AT STA1417 BETWEEN S-37R TO S-38R FOUND CORROSION AND REPLACED. (LP 1288087)
CORRISION LEVEL 2: -AFT CARGO SHEAR TIE AT STA1197+165 BETWEEN S-38R TO S- 39R FOUND CORROSION OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1288175)
CORROSION LEVEL: 2 CABIN FLOOR SUPPORT STRUCTURE AT STA 1518 RBL44 FOUND CORROSION ON INTERCOSTAL THE CORROSION AT FLOORBEAM STA1518 RBL 44 REMOVED AND FOUND OUT OF LIMIT AND REPAIRED. (LP 1284828)
FOUND ONE CRACK AT STA287 BETWEEN WL185 AND WL 159 AT RT VERTICAL STIFFENER, LENGTH IS 5MM, AS REMARKED REPAIRED THE CRACKED AT STA287 BTW WL185 AND WL 159 ON RT VERTICAL STIFFENER. (LP1276566)
RIGHT INBOARD SIDE OF #1 ENG THRUST REVERSER WIRE MESH CLOTH DAMAGE 12 " X 9 " C/W E/RA 569315-14. (LP 5553050)
EMERGENCY LIGHTS BATTERY PACK M736 FAILED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.
SHIP 1807 - ATO - DUE TO WIND SHEAR WARNING AT 70 KIAS. CORRECTIVE ACTION: MAINTENANCE C/W NO GO ODI PROCEDURES. WEATHER RADAR TRANSCEIVER DID NOT TEST CORRECTLY AND WAS REPLACED. SYSTEM OPERATION IS NORMAL.
DURING CLIMB OUT, FUEL WAS REPORTED BEING DUMPED OUT OF THE LEFT WING DURING A LEFT TURN. ELECTED TO RETURN TO DEPARTURE. DECLARED AN EMERGENCY AND LANDED . FOUND LEFT PRESSURE RELIEF VALVE TRIPPED. R & R THE LEFT WING PRESSURE RELIEF VALVE IAW AMM 28-13, OPS AND LEAK CHECKED GOOD.
EMERGENCY LIGHTS, ROWS 22-29 RT SIDE ARE INOPERATIVE. FOUND THE POWER SUPPLY M732 BATTERY PACK PLUGGED INTO WRONG SEAT 21FG . CONNECTED TO THE CORRECT SEAT 22FG AND ALL CHECKED NORMAL.
COCKPIT DOOR WONT TEST. PERFORM AN OPS TEST IAW AMM 52-51. CHECKED GOOD.
EMERGENCY LIGHTS ON SEAT 25GF, 26GF, 27GF INOP. RELAMPED EMERGENCY LIGHTS ON SEAT 25GF, 26GF, 27GF NO HELP. MX REMOVED AND REPLACED EMER PWR SUP AND BATTY PER AMM 25-29 NO HELP. T/S PER WDM 33-51-18 SHEET 1 FOUND CONNECTOR BETWEEN SEATS 24GFAND 25GF DISCONNECTED. RECONNECTED. OPS CHKS OK. OK FOR SVC.
FLIGHT DECK DOOR AUTOMATIC LOCKING SYSTEM INOPERATIVE. RESET SYSTEM IAW IAW AMM 52-51. SYSTEM OPS NORMAL. OK FOR SERVICE.
2R AND 3R EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R THE CHARGER AND BATTERY.
EMERGENCY LIGHTS 30AB-37AB COME ON THEN ALMOST IMMEDIATELY GO OUT. R&R BATTERY PACK AND CHARGER AT SEAT 32 AS PER AIM 33-50.
DURING SERVICE CHECK FOUND EMERGENCY LIGHTS INOPERATIVE AT ROWS 30-37 A & B. R & R THE BATTERY PACK 7236.
EMERGENCY EXIT SIGN COVER LOOSE. REPLACED EMERG EXIT SIGN AT LOC 602.
EMERGENCY LIGHTS INOPERATIVE FROM SEAT 22GF. REPLACED BATTERY CHARGER IAW AMM 33-51.
EXTERNAL FUSELAGE SKIN BELOW FWD APU CUTOUT AT BS 1725, S7R FOUND CRACKED. REPAIRED IAW ER/A 522047-14, PRI, REV 0.
FWD CARGO BS 424, STRINGER 38L FOUND CORRODED. REPAIRED IAW ER/A 522048-14, PRI REV 0.
ULTRASONIC INSPECTION CARRIED OUT, FOUND CRACK AT LT BS 955 FAILSAFE STRAP. WORK ACCOMPLISHED IAW ER/A 5521704-14AD, PRI, REV O, REV1, REV2. ER/A 521704-14AD REV ORIGINAL COMPARED AND COMPLIED WITH.
A CRACK WAS FOUND ON THE FUSELAGE SKIN AT BS 1725, S7R. SKIN REPAIRED IAW SECT I OF ERA 522047-14.
SEAT 4A EMER PATH LIGHT INOPERATIVE. R & R THE EMERGENCY PATH LIGHT ASSY. FWD SIDE AT SEAT 4A. OPS CHECKED NORMAL.
THE 4L AND 4R EMERGENCY PATH EXIT LIGHTS INOP. REPLACED PWR SUPP AND BATT AT 4R F/A SEAT AND TESTED PER B767400 M/M 33-51. MFG NBR S283W603-2. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS
FLIGHT ATTENDANTS REPORTED LOUD BANG NOISE DURING TAXI IN AT R3. MAINTENANCE FOUND ADP FAILED AND DAMAGED TO FUSE AND COMPOSITE PANLS. ALL REPAIRED ON N/R CARD 1-5 PER ERA 497833-14 REV A FILE CODE 53-31.
MAINTENANCE FOUND ONE EMERGENCY LIGHT IN LOWER CREW REST FLIGHT ATTENDANT CONTROL PANEL INOPERATIVE. FORWARDED TO MCO33-51-01C. LOWER FLIGHT ATTENDANT CREW REST EMERGENCY LIGHTS OPERATE/TEST NORMAL WHEN REFERENCING STC APPROVED DOCUMENT TTF-07T048-40. OK FOR SERVICE. REMOVED MCO AND PLACARD.
DURING ACCOMPLISHMENT OF THE DAILY RELIABILITY CHECK, MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 16FG THROUGH 21FG INOPERATIVE. MAINTENANCE RESEATED THE CONNECTOR AT SEAT 16FG. OPERATIONAL CHECK WAS NORMAL.
MAINTENANCE FOUND THE L4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT SOCKET AND THE OPERATIONAL CHECK WAS GOOD.
LT WING NR 3 FLAP TRACK AFT FLAP FAIRING SUPPORT FITTING CRACKED. REPAIR C/W PER ERA 490810-14AD.
EMERGENCY EXIT SIGN AT DOOR 3R IS INOPERATIVE. MX REPLACED THE LENS. SYS OPS IS NORMAL.
A HINT OF SMOKE AND BURNING ODOR CAME FROM THE LT FWD OVERHEAD ENTRY LIGHT. THE F/A TURNED OFF THE LIGHT SWITCH AND THE ODOR AND SMOKE DISAPPEARED IMMEDIATELY. MX FOUND AN ISO SHORT BETWEEN J14 TO J1. THE DAMAGED PIN, NR43 IN J1 CONNECTOR OF F/A PANEL, WAS REPLACED ALONG WITH THE ENTRY LIGHT SOCKET. SYS OPERATION IS NORMAL.
EMERGENCY PATH LIGHT AT SEAT 15A IS INOPERATIVE. MX FOUND LIGHT BULB MISSING AND REPLACED. SYS OPS IS NORMAL.
EMERGENCY EXIT SIGNS AT DOOR R4 IS INOPERATIVE. MX REPAIRED WIRE. SYS OPERATION IS NORMAL.
EMERGENCY EXIT SIGNS AT DOOR L4 DOOR ARE INOPERATIVE. MX FOUND WIRE W0836 BROKEN AT DOOR R4 AND REPAIRED. SYS OPS IS NORMAL.
RTB DUE TO LT IDG FAILED MIP. REMOVED AND REPLACED NR 1 IDG IAW AMM OPS AND LEAK CHECK OKC/W ETOPS PDC. CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.
DURING CRUISE NR 1 ENG READING 5 QTS ON ARRIVAL LHR ENG REQUIRED 10 QTS, T/S IN PROGRESS. NR 1 ENGINE LUBE AND SCAVENGE PUMP REMOVED AND REPLACED DUE HIGH OIL CONSUMPTION AND OIL LEAKS FOUND AROUND CORE AREA. PIPING AND CONNECTIONS CHECKED FOR SECURITY. ENGINE OIL SERVICED TO FULL.
DURING CLIMBOUT OF JFK HAD NR 2 ENG OVERHEAT LIGHT. LIGHT GOES OUT WITH THROTTLE REDUCTION RETURNING TO JFK FOR REPAIRS. PERFORMED DETAILED INSP OF PNEUMATIC SYS IAW FIM 26-11-14. LEAK CHECKED PNEUMATIC SYS ON RT ENG. FOUND PRSOV CLAMP LOOSE - 1 1/2 TURN OF DUCT ABOVE PRSOV.3/4 TURN. PERFORMED T/O PWR RUN 6 M, OPS CHECKS OK. MCC NOTIFIED, OK FOR SERVICE.
RTB, DUE AFTER PUSHBACK F/O PFD SHOWED 0 MAGENTA FOR A/S AND 0 MAGENTA FOR ALTITUDE MCP AND CAPTS PFD SHOWED CORRECT NUMBERS. ALSO PFD SHOWED A/S AND ALT AT 0 /C FWD TO MCO RT FCC. REPLACED RT FCC.
APU HAS NO AIR FOR PNEU. INSPECTED APU AND FOUND PNEU DUCT PULLED AWAY FROM APU HOUSING. REMOVED APU PER AMM. INSTALLED APU PER AMM, OPS AND LEAK CHECK OK.
DURING OPS 5003 BORO FOUND 1 EACH 1ST STAGE NGV DAMAGED BEYOND M/M LIMITS.
RTB - TAXI OUT LT FWD FUEL PUMP FAILED. RETURNED FOR ADDITIONAL FUEL.
GEAR DISAGREE PLUS GEAR DOORS ADVISORY MSG AFTER T/O. CYCLED BUT NO HELP, WITH GEAR DOWN, GEAR DOORS ADVISORY MESSAGE REMAINS. CLOSED DOORS WITH DOOR CLOSE SWITCH. CYCLED GEAR HANDLE, DOORS OPEN AND WILL NOT CLOSE UNLESS WITH MTC SWITCH. NO HYD TO DOOR ACTUATOR EXTEND SIDE. NO POWER AT SAFETY VALVE. FOUND RELAY K10365 BAD. REPLACED RELAY. GOOD POWER AT VALVE BUT DOORS STILL INOP WITH GEAR HANDLE. JACKED ACFT AND PERFORMED GEAR SWING PER AMM. CHECKS GOOD SEVERAL TIMES.
REPLACE RT ENG DUE TO FAILED BORO 50131. COMP INNER LINER AXIAL CRACKS. ON 25 CYCLE FLYBACK, REPLACED ENGINE.
EMERGENCY LIGHT ASSY AT SEATS 26R, 32L, 43R DAMAGED. REMOVED AND REPLACED BROKEN EMERGENCY LIGHT ASSY AT SEATS 26R,32L,43R. OPS CK GOOD IAW B767 MM 33-51-01.
BATTERY PACK (EMERG) M1208 FAILED DEEP CYCLE/REMOVED BAD BATTERY AND REPLACED WITH SERVICABLE EMERG MIZOT, OPS CHECK GOOD IAW B767 MM 33-51-07.
PASSENGER OXYGEN SYSTEM FAILS MANUAL DEPLOYMENT CHECK. REMOVED AND REPLACED K466 RELAY IAW BOEING SWP 20-81-11 PASSENGER OXYGEN SYSTEM MANUAL DEPLOYMENT TEST. OPS CHECKS GOOD IAW B767 MM 35-21-00-705-054.
EMERGENCY LIGHT BATTERY PACK MG757 FAILED DEEP CYCLE. REMOVED AND REPLACED (MG757) EMERG BATTERY PACK. OPS CHECK GOOD IAW B767 MM 33-51-07.
EMERGENCY BATTERY PACK M737 FAILS DEEP CYCLE. REMOVED AND REPLACED (M737) EMERGENCY BATTERY PACK. OPS CK GOOD IAW MM 33-51-07.
EMERGENCY BATTERY PACK M738 FAILS DEEP CYCLE. REMOVED AND REPLACED M738 EMERGENCY BATTERY PACK OPS CK GOOD IAW B767 MM33-51-07 .
EMERGENCY BATTERY PACK M1210 FAILS DEEP CYCLE. REMOVED AND REPLACED M1210 EMERGENCY BATTERY PACK. OPS CK GOOD IAW B767 MM 33-51-07 .
EMERGENCY BATTERY PACK M730 FAILS DEEP CYCLE. REMOVED AND REPLACED M730 EMERGENCY BATTERY PACK. OPS CK GOOD IAW B767 MM 33-51-07 .
RTB - DOOR SEAL LOOSE 4L DOOR. CKD PRESS SEAL DOOR 4L OK, REPOSITIONED COVER DOOR SEAL 4L.
ON PUSHBACK, TOWBAR BOLT AND TOW LUG SUSTAINED DAMAGE. REMOVED TOWBAR FITTINGS FROM NOSE GEAR. INSTALLED NEW TOW BAR FITTING PER AMM FIT CK OK.
REAR SMOKE ALARM WENT OFF IN FLT, TESTED SMOKE ALARM SYSTEM. TESTED OK. NO PROBLEMS FOUND.
APU AUTO SHUT DOWN 2 TIMES WHEN APPLYING APU ELECT. APU FAULTED MSG 49-27250 LUBE MODULE FILTER SHOWS CLOGGED. PULLED CHIP DETECTORS AND FILTER FOUND METAL AND OIL SMELLS BURNED. FWD TO MCO AND PLAC 49-00-01A. REPLACED APU PER MM.
IDLE DISAGREE MSG, FWD TO MCO AND PLACARD RT ENG IN MIN GND IDLE INOP PER MEL 73-21-08A. REPLACED NR 2 HMU PER MM, NO HELP. REPLACED K433 AND K1026R, NO HELP. FOUND K433 NOT ENGAGING. REPLACED EEC DISCREETS GE CARD ENG, OPS CHECKS OK.
APU BLEED VALVE MSG ILLUMINATED AFTER APU SHUT DOWN. CYCLED C/B P11-S23 APU BLEED VALVE C/B. STARTED APU. APU BLEED VALVE OP CHECKS GOOD.
L START VALVE WOULD NOT OPEN, RTB. REPLACED START VALVE NR 1 ENG PER AMM MCO/PLAC REMOVED.
ON TAXI, RT ENGINE N1 IDLE 42 PCT N2 80 PCT. TS PER FIMM FOUND RT ENG EPCS PAGE SHOWS FLT IDLE DISCREET LASBLE 275 41CO FLT IDLE ON GRD TS AND FOUND CARD M644 BAD, SAME OPS GOOD MCO PLACARD REMOVED.
REMOVED ENTERTAINMENT BOX 12F BURNING ELECTRICAL ODOR. INSTALLED DOWNLOADED AVU AT 12FG PER M/M.
AT FL330, 5 MINS INTO CRUISE, CABIN FILLED WITH SMOKE. A/C DIVERTED INTO OAK AND LANDED WITHOUT INCIDENT. FOUND LEFT ACM FAILED. FWD TO MCO AND PLACARD PER MEL 21-51-01.
ATB - FUMES NOTED IN COCKPIT AND 1ST CLASS IN CLIMB. REPLACED FWD EQUIPMENT COOLING FAN.
T/E FLAP ASYM EICAS MSG, LT FLAP READS 4 RT FLAP READS UP. ADJUSTED NR 5 POSITION TRANSMITTER PER MM.
L/E SLAT ASYM MSG CAME ON AFTER T/O FLAPS SELECTED. FOUND A CONTROL ROD AT NR 7 SLAT DAMAGED. REPLACED SAME.
ON DESCENT AFTER ADDING POWER FROM IDLE A BURNING SMELL LIKE BURNING POPCORN / RUBBER WAS NOTICED IN THE COCKPIT. AFTER LANDING GOING FROM IDLE TO REVERSE THE SMELL RETURNED AND WAS ALSO NOTICED IN FIRST CLASS BUT NOT IN THE MAIN CABIN. INSPECTED ENG INLETS FOR OIL. NO OIL FOUND. OIL CONSUMPTION WITHIN LIMITS. RAN APU PNEUMATICS AND PACKS. NO SMELLS NOTED. IFE SYSTEM ON AND NO SMELLS OR STATUS MSG. OPERATED GALLEY EQUIPMENT, NO SMELLS NOTED.
ON DESCENT WITH THRUST LEVERS AT IDLE STRANGE SMELL PERMEATED COCKPIT. REFERENCE PREVIOUS WRITE UP. RAN ENGINES AT TAKEOFF PWR FOR 5 MINS WITH BOTH PACKS OPERATING. ALSO RAN EACH ENGINE INDIVIDUALLY AT TAKEOFF WITH CORRESPONDING PACK OPERATING. NO SMELL NOTED. RAN EACH ENGINE IN REVERSE THRUST. NO SMELL NOTED. CANNOT DUPLICATE PROBLEM.
ATER T/O FLT ATTENDANT REPORTED NO VIDEO AVAILABLE. TRIED RESETTING THE SYSTEM A COUPLE OF TIMES AND NO HELP. ABOUT 3 HRS INTO FLIGHT THE FLT ATTENDANTS REPORTED A STRANGE ODOR POSSIBLE ELECTRICAL NEAR SEATS 6A/B, APPEARED TO COME FROM OVERHEAD AREA. POWER WAS REMOVED FROM PAX READING LIGHTS AT THE F/A VIDEO CONSOLE. ODOR DISSIPATED. POWER SWITCH LEFT OFF FOR REMAINDER OF FLIGHT. FWD TO MCO AND PLAC IFE ENT DUE TO BOOTUP PROBLEMS. NO SOURCE OF STRANGE ODOR NOTICED. INSPECTED OVERHEAD FLUORESENTS, INDIV SEAT PCUS, SIDEWALL LIGHTS, READING LIGHTS, O2 GEN IN FWD AREA 1-10.
ON APPROACH TO FLL WITH FLAPS 20 GOT L/E SLAT ASYM. DUE TO LONG RUNWAY UNAVAIL FLL AND FLAPS 20 REQUIREMENT FOR LANDING DIVERTED TO MIA. PSEU FAULTED TARGET FOR NR 8 SLAT OUTBD SENSOR. INSPECTED TARGET AND FOUND MISSING. REPLACED TARGET FOR SENSOR 238, OPS CHECK OK.
MID GALLEY EMERGENCY PATH LIGHT MISSING LENS. INSTALLED LENS, OPS CHECK OK.
AT 2000 FEET RIGHT ENG ROLLED BACK HAD HIGH FUEL FLOW AND HIGH VIBS ENG NOT RESPONDING TO THROTTLE INPUTS. AFTER LANDING ENG SHUTDOWN DUE HIGH VIBS. METAL FOUND IN TAILPIPE. REPLACED ENGINE.
THE FUSELAGE SKIN WAS DENTED BY GROUND EQUIPMENT NEAR FS 1367 AND STRINGER 29R. THE DAMAGE WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 088020-14, REV B.
BATTERY PACK FUSES BLOWN, EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY.
ON LAYOVER, NR 2 ENGINE CASE DRAIN HYD FILTER MODULE LINE LEAKING. FOUND LINE BROKEN BEND REF IPC 29-11-75-14 ITEM 357. REPLACED SAME.
L/E SLAT ASYMMETRY ILLUMINATED ON LANDING ROLLOUT. FOUND TARGET MISSING FROM NR 4 SLAT. FLEET PROBLEM. BOLT SHEARED, BEARING AND TARGET LOST. INSTALLED TARGET, OPS CHECK GOOD.
TE FLAP DISAGREE ON TAKEOFF. FLAPS STOPPED RETRACTING AT 10DEG. FLAPS EXTENDED TO 20 DEG. WITH ALTN FLAPS SYSTEM. FOUND ROTARY ACTUATOR BRAKE TRIPPED ON RT OUTBOARD FLAP GEAR BOX ROTARY FLAP ACTUATOR ON INBOARD SIDE TRIPPED. REPLACED ROTARY ACTUATOR MFR. NBR. 256T6200-4 ETOPS CATEGORY ''B'': DIVERSION OR TURNBACK
ATB DUE TO ELECTRICAL PWR FAIL IN FLT WITH THE FOLLOWING C/B POPPED ON P-6 PANEL-DC STBY-BAT BUS DIST-L GEN CONT UNIT-RAT MANUAL AND THE ASSOCIATED ALERTS. BPCU BITE FAULTED LT GCU CODE 24-30101 PER FIM. REPLACED LT GCU, GROUND TEST OK PER FIM USING WDM ISOLATED, VISUALLY INSP SHOOK DOWN AND MEGGED ALL RELATED WIRING TO THE FOUR POPPED C/B. NO SHORTS OR WIRING DAMAGE FOUND. INSP WIRING HARNESS IN P6 PANEL AND AB INSP CARD FILES FOR CHAFING, NONE FOUND. REPLACED STBY PWR RELAY K 109 STBY PWR CB A2 AND MAIN BATT CHGR DEPLOYED STOWED RAT SEVERAL TIMES TO VERIFY NML OPS RAN BOTH.