N825MH
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| DELTA AIR LINES, INC. (DALA) | Operator | 2009-10-27 – 2009-10-27 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2009-10-27 – 2009-10-27 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
DURING WALK AROUND FOUND PAINT LOSS OR DELAMINATION ON THE RIGHT SIDE OF TAIL. REPAIRED DELAMINATION ON THE RIGHT SIDE OF TAIL AS PER B767-400 SRM 55-30-01-2R-1 AND 51-70-10-2R (1438051)
DURING WALK AROUND FOUND PAINT LOSS OR DELAMINATION ON THE RIGHT SIDE OF TAIL. REPAIRED DELAMINATION ON THE RIGHT SIDE OF TAIL AS PER B767-400 SRM 55-30-01-2R-1 AND SRM 51-70-10 (1438045)
DURING INSPECTION NR 8 SLAT EXTERNAL LE SKIN FOUND THE BLIND RIVET HOLE CRACK AROUND OSS 439.50. THE HOLE CRACK ON NR 8 SLAT EXTERNAL LE SKIN AROUND OSS 439.50 REPAIRED AS PER B767-400 SRM 57-43-01 (1438057)
FOUND LH WING NR 3 SLAT INBD WEDGE T/E WORN. REPAIRED LT WING NR 3 SLAT INBD WEDGE T/E WORN AS PER SRM 57-43-02-2R-1 AND SRM 51-70-10 (1436450)
FOUND RT WING NR 11 SLAT UPPER SKIN FROM INBD EDGE 51 INCH AND TRAILING EDGE 10.5 INCH 01EA BULGE. REPAIRED RH WING NO.11 SLAT UPPER SKIN FROM I/B EDGE 51 INCH AND TRAILING EDGE 10.5 INCH 01EA BULGE AS PER B767-400 SRM 51-70-10 -2R-2 AND SRM 57-43-02 (1436455)
FOUND RT STRUT FORWARD MID SPAR BEWTEEN STA 221 AND STA 237 CUTOUT CRACKED. REPAIRED AS PER PRI 631935-14. (1434806)
AFT CARGO FRAME LOWER CHORD AT STA1197+154/S39L-S39R FOUND CORROSION. REPAIRED AS PER PRI 631843-14 (1431341)
AFT CARGO SKIN AT STA1197+165 TO 1197+187/S39L-S39R FOUND CORROSION. THE DAMAGED SKIN REPAIRED AS PER PRI 631872-14 (1431330)
DURING AN H-CHK AT STAG, CORROSION WAS NOTED ON THE FAIL SAFE AT BS 1197+154 BETWEEN S39L AND S39R. ER/A 631843-14 SECT. I REPAIR WAS ACCOMPLISHED. FOLLOW ON ACTION IS REQUIRED FOR DTE. ASSOCIATED ER/A 74-631843 ADDED FOR AC 1801 (1429898)
DURING H CHK AT STAG, CORROSION WAS NOTED ON THE FUSELAGE SKIN BETWEEN BS 1197+165 AND 1197+187. A REPAIR WAS INSTALLED IAW ER/A 631872-14, SECT I. FOLLOW ON ACTION IS REQUIRED FOR SECT. II REPEAT INSPECTIONS. ACCOMPLISH ER/A 631872-14 SECT. II REPEAT INSPECTIONS PRIOR TO 30,000 TOTAL A/C CYCLES, THEN REPEAT AT 9000 FLIGHT CYCLE INTERVALS THEREAFTER. (1429833)
AD / EM-EO TASK - FOUND NO.1 PYLON FWD UPPER WEB FOUND WITH AN EXISTING REPAIR AT NAC STA 221.250 TO NAC STA 237.500. REPAIRED THE WEB IAW ER/A 631985-14. (1425083)
DURING REMOVAL OF ACCESS FOR PYLON REMOVAL, FOUND THE PYLON UPER SPAR WEB HYDRAULIC LINE CUTOUT CRACKED ABOUT 0.5" AFT NAC STA 228.19. DAMAGED AREA REPAIRED IAW PRI 631750-14 . (1423385)
AFT CARGO SHEAR TIE AT BS 1562, S38 - 39L FOUND CORRODED. DAMAGED AREA REPAIRED IAW SRM 51-40-02. (1423503)
AFT CARGO ONE SHEAR TIE AT BS 1219, S39L-39R FOUND CORRODED. DAMAGED AREA REPAIRED IAW SRM 51-40-02. (1423497)
AFT CARGO SHEAR TIE AT BS 1197+154, S39L-39R FOUND CORRODED. DAMAGED AREA REPAIRED IAW SRM 51-40-02. (1423439)
AFT CARGO SHEAR TIE, BS 1518, S38-39L FOUND CORRODED. DAMAGED AREA REPAIRED IAW SRM 51-40-02. (1423433)
BULK CARGO SHEAR TIE AT BS 1417, 39L-39R FOUND CORRODED. DAMAGED AREA REPAIRED IAW SRM 53-00-07. (1423427)
AFT CARGO SHEAR TIE AT BS 1417, S38-39L FOUND CORRODED. DAMAGED AREA REPAIRED IAW SRM 51-40-02. (1423420)
BULK CARGO BAY, FOUND BS 1477, STINGER 39R CORRODED. REFER TO CPCP TASK 53-584-00. DAMAGED AREA REPAIRED IAW SRM 53-00-03. (1422037)
OPEN HOLE HFEC INSPECTION CARRIED OUT ON THE ALL FASTENER HOLES (5EA) AT THE FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER. FOUND ONE CRACK FROM THE NR 4 FASTENER HOLE. DAMAGED AREA REPAIRED IAW SRM 53-10-01. (1419957)
RIGHT FUSELAGE SKIN AT BS 1730, WL 200. FOUND FWD SKIN ABRASION. DAMAGED AREA REPAIRED IAW SRM 53-80-01 (1415504)
LEFT FUSELAGE SKIN AT BS 1730, WL 200, FOUND FWD SKIN ABRASION. DAMAGED AREA REPAIRED IAW SRM 53-80-01. (1415515)
HFEC INSPECTION CARRIED OUT ON THE LT FUSELAGE SKIN ,SECTION 48, FOUND TWO CRACKS IN STRINGER 13, BS 1654 - 1678, THE LENGTH OF CRACK IS 0.19 IN AND 0.15 INCH, THE FUSELAGE SKIN CRACK AREA WAS REPAIRED AS PER B767-400 SRM 53-80-01 (1408646)
R1 DOOR SLIDE ARMED LIGHT AT FWD F/A PANEL INOPERATIVE. R & R R1 DOOR ARMED STATUS LIGHT SWITCH ASSY AT FOWARD FAP PANEL. (1168017)
SHIP 1801 1L SLIDE IS INOP. CORRECTIVE ACTION: R/R LIGHT BOARD ASSY PER B767 AMM 52-73 OPC CHECK GOOD. (7527434)
ROW 41F-49F EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER B767-400 AMM 32-51. OPERATIONAL CHECK IS NOW NORMAL. (LP #7542926)
SHIP 1801 -DIV/DE- THE CREW DECLARED AN EMERGENCY WITH ATC AND DIVERTED THE AIRCRAFT TO SNN PER THE QRH, DUE TO THE F/O R3 SIDE WINDOW SHOWING INCREASING DAMAGE FROM HEAT. THE DAMAGE INCREASED RAPIDLY AND INCLUDED GLASS LAYER RIPPLING, DISCOLORATION, AND EXTREMELY HOT TO THE TOUCH. THE LANDING WAS OVERWEIGHT BUT OTHERWISE UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE R3 WINDOW AND THE WINDOW HEAT CONTROL COMPUTER. THE WINDOW HEAT SYSTEM CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (LP #6661752)
THE EMERGENCY LIGHTS FOR ROWS 50-52AB ARE INOPERATIVE. MAINTENANCE FOUND A CONNECTOR AT 52AB TO BE DISCONNECTED. THE WIRES WERE RECONNECTED AND THE OPERATIONAL CHECK WAS GOOD IAW B767-400 AMM 33-51. (LP #6661750)
LEFT SIDE OF TAIL SHOWING PAINT LOSS OR DELAMINATION NEAR LEADING EDGE ON CAPTAINS SID. CORRECTIVE ACTION: FOUND LEFT SIDE OF TAIL DELAMINATION NEAR LEADING EDGE ON CAPTAINS SIDE AND PERFORMED INTERIM REPAIR AS PER ER/A 631907-14 (6716370)
AIRCRAFT 1801, DURING SVC, FOUND ROWS 31-38 FG EMMERGENCY LIGHTS INOP. CORRECTIVE ACTION: FOUND CONNECTOR AT 32 FG DISCONNECTED. RESECURED. ALL OPS NML. (LP 5761218)
SHIP 1801 FOUND LHW SLAT NO.3 IB INNER SURFACE WORN. CORRECTIVE ACTION: LHW SLAT NO.3 IB INNER SURFACE REPAIRED AS PER B767-400 SRM 57- 43-02-2R-1 & SRM 51-70-10-2R-4. FIG202(SHEET8) & SRM 51-70-10-2R (0351205)
SHIP 1801 FOUND OUT FLOOR BEAM STIFFENER CRAKED AS BS246 BETWEEN LBL0 AND LBL30. CORRECTIVE ACTION: THE CRACKED STIFFENER AT STA 246 REMOVED AND REPLACED AS PER B767-400 SRM 51-40-02 (0349280)
SHIP 1801 FOUND OUT AFT CARGO LH NO.1 ROLLER TRAY CRACKED AT BS1480. CORRECTIVE ACTION: THE CRACKED ROLLER TRAY APPLIED DOUBLER REPAIR AS PER B767-400 SRM 53-00-53-2R-1 (0346502)
SHIP 1801 AFTER DEPARTUREFLT CREW REPORT DOOR 2L WONT ARMED. CORRECTIVE ACTION: REMOVED FOD. PERFORM OPS CHK. DOOR OPS NML. A/C OK FOR SVC (5644364)
SHIP 1801 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS: 3. CORRECTIVE ACTION: EMERGENCY EXIT SIGN INTACT AT SAID LOCATION. GOOD FOR SVC. (0120392)
SHIP 1801 1L DOOR SHOWING OPEN. OPENED AND RESET 1L DOOR IAW AMM B767 52-11. DOOR AND INDICATIONS CHECK GOOD. (5071912)
SHIP 1801 - DIV - CREW REPORTED LOSS OF OIL FROM RIGHT ENGINE AT A RATE OF 1 QUART/30 MINUTES. OUT OF AN ABUNDANCE OF PRECAUTION, CREW DECIDED TO STOP SHORT. FLIGHT DIVERTED TO TPA. CORRECTIVE ACTION: REPLACED RIGHT ENGINE STARTER AND HYDRAULIC PUMP PER B767 AMM 72-64. NO FURTHER LEAKS FROM THOSE SEALS. FOUND OIL LEAKING FROM B AND C AND 6 O'CLOCK RECOUP DUCT. RAN ENGINE AT 80% N2 FOR 20 MINUTES, OIL CONSUMPTION WITHIN LIMITS. (LP 4535404)
SHIP 1801 -SMKE/FUME- PASSENGER ENTERTAINMENT SCREEN AT 40A SMOKING. CORRECTIVE ACTION: ITU REPLACED. (4511560)
SHIP 1801 NUMEROUS F/C RIGHT SIDE EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: REPLACED OVHD BATTERY PACK M6756 PER B767 MM 33-51 ALL LIGHTS NOW ILLUMINATE (4598064)
SHIP 1801 FA CREW WEST FACILITY EMERGENCY LIGHT ON IN BUNK WITH ESCAPE HATCH. CORRECTIVE ACTION: R/R EMERGENCY EXIT LIGHT PER B767 AMM25-29. OPS CHECK GOOD. OK FOR SVC (4722565)
SHIP 1801 FLIGHT ATTENDANTS REPORT WARM ELECTRICAL SMELL IN CREW REST COMPARTMENT. CORRECTIVE ACTION: FOUND HEATERS TO BE THE SOURCE OF ELEC SMELL. FWD TO MEL 21-66-02A. MEL PLACARD INSTALLED & "M" PROC C/W (4722506)
SHIP 1801 ON SVC CHK, FOUND EMERG LIGHT ON TEMP CONTROL PANEL & EMERG LIGHT AT ALT EXIT INOP IN LLCR. CORRECTIVE ACTION: R&R LLCR EMERGENCY POWER SUPPLY & BATTERY PER B767-400 AMM 25-29 . R&R BOTH LIGHTY ASSY PER B7676-400 AMM 25-29. OPS CHK GOOD (4722504)
SHIP 1801 -DIV- DIVERTED TO IAD DUE TO ALL LAVS INOP. CORRECTIVE ACTION: FOUND LAV TANKS FULL. SERVICED LAV TANKS. OPS CHECKS GOOD. (4714274)
SHIP 1801 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: POS 601 SLIDE INDICATOR LIGHT OK. (2755448)
SHIP 1801 - DIV - DUE TO UNRELIABLE AIRSPEED INDICATION. CORRECTIVE ACTION: R/R F/O ADM, C/W AUTOPILOT TEST AND PITOT STATIC TEST. (4159768)
SHIP 1801 -MISC/DE- CREW ELECTED DE DUE TO TE DISAGREE INDICATION DURING DESCENT. C/W QRH AND LANDED UNEVENTFULLY AT DESIRED FLAPS 20. CORRECTIVE ACTION: SUSPECTED FLAP OVERSPEED DUE TO AIRSPEED ISSUE. R/R F/O PITOT PROBE PER B767-400 AMM 34-11, OPS TEST NORMAL. FLAP SYSTEM TEST NORMAL.(4159753)
SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: 1L. REPOSITIONED LAMP, SLIDE INDICATOR LIGHT WORKING NORMALLY. B767- 400 AMM 52-71. ITEM OK .
SHIP 1801 2L DOOR HARD TO ARM. CORRECTIVE ACTION: T/S PER FIM 52-11-00-815-804 B767-400. FOUND DEBRIS IN GIRT BAR TRACK AND LOCKING MECHANISM. CLEANED AND LUBRICATED PER B767-400 FIM 52-11-00-815-804. OPS CHK OK. (2574232)
2L DOOR WILL NOT ARM. CORRECTIVE ACTION: CYCLED DOOR & ARMING LEVER AT 2L DOOR, ARMS NML OK FOR SVC.
SHIP 1801 OUTBD OF RT MLG HAS BOLT PUNCTURE. CORRECTIVE ACTION: ARRIVAL PNL 651TB OUTBD OF RT MLG REPAIRED AS PER B767-400 SRM 57-51-01-2R-2. (9100304)
SHIP 1801 AOM REPORT R3 DOOR UNLATCHED, CORRECTIVE ACTION: R/R R3 SLIDE PER A330 M/M 2566. CLOSED R3 DOOR PER A330 M/M 52-22 (9013994)
SHIP 1801 2R DOOR DOES NOT ARM CORRECTLY, CORRECTIVE ACTION: CYCLED DOOR AND ARMS PROPERLY NO TROUBLE FOUND. (9290388)
SHIP 1801 UNABLE TO ARM 2L DOOR AT DEPT. CORRECTIVE ACTION: FOUND OUTSIDE HANDLE NOT STOWED RECYCLED DOOR AND PERFORMED OPS TEST OF ARMING SYSTEM AS PER B767-400 AMM 52-12. OPS OK. (9290358)
SHIP 1801 1R DOOR SLIDE, LIGHT BLINKS CONTINUALLY WITH DOOR ARMED. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0082:2500-0829/001 00583 PERFORMED OPS CHECK OF DOOR 1R SLIDE-RAFT ARMED WARNING SYSTEM REF B767 AMM 52-73-00. OPS NML. (2252853)
SHIP 1801 PRIOR TO PUSHBACK RT DOOR WOULDNT ARM, CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR. OPN NORMAL (8762534)
SHIP 1801 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:01L. CORRECTIVE ACTION: RE-SEATED LIGHT ASSY, OPS CKS NML. REF B767 AMM 52-71. (2158216)
SHIP 1801 AT DEPT 2L DOOR WONT ARM. CORRECTIVE ACTION: REMOVED DEBRIS FROM DPPR FITTING DOOR ARMS NORMALLY (8844142)
SHIP 1801 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: L1, CORRECTIVE ACTION: NO FAULTS NOTED. INDICATION OPERATES NORMAL. (2101180)
SHIP 1801 FLT CREW STATES 2L DOOR WONT ARM. CORRECITIVE ACTION: CYCLED 2L DOOR HANDLE, ARMS NORMALLY OK FOR SVC PER B767-400 AMM 52-11 (8324952)
SHIP 1801 -DIV- TO ELP DUE LOW ENGINE OIL QUANTITY MESSAGE ON THE #2 ENGINE. CREW SHUTDOWN THE ENGINE WHEN OIL PRESSURE REACHED 16PSI. CORRECTIVE ACTION: FOUND #6 SCAVENGE OIL LINE LOOSE, INSPECTED AND RETORQUED. INSPECTED MCD AND OIL FILTER, NO DEFECTS NOTED. PERFORMED HIGH POWER RUN. LEAK CHECK OK. (8206280)
SHIP 1801 DURING INSPECTION FOUND LOWER AFT FAIRING FLAP DRIVE ASSEMBLY CLOSE-OUT PANEL WAS WITH DELAMINATION AND CRACK DAMAGE DAMAGE. REPAIRED PER SRM 51-70. (LP 1994929)
SHIP 1801 FOUND EMERGENCY PATH LIGHTING AT ROW 37 AND 38G ARE INOPERATIVE. CORRECTIVE ACTION: FOUND CONNECTOR FOR POWER SUPPLY OFF AT ROW 38G AND RE-CONNECTED SYSTEM OPERATION IS NORMAL. (LP 7381608)
SHIP 1801 EMERGENCY LIGHTS FROM 6A TO L2 DOOR ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK. SYSTEM OPERATION IS NORMAL. (LP 7392902)
FLIGHT 8824; MSP-HNL PERFORMED AN AIR TURN BACK DUE TO 'FWD EQUIP OVERHEAT' WARNING. CORRECTIVE ACTION: REPLACED LOW FLOW SENSOR AT FORWARD RACK AND FLIGHT DECK LOW FLOW SENSOR TS0163. SYSTEM OPERATION IS NORMAL.
LEFT UPPER FUSELAGE SKIN AT STA 1660 BETWEEN S3L AND S4L AS MARKED POINT FOUND CRACK. C/W ERA 586296-14 (LP 1543070)
CORROSION LEVEL: 2 CORROSION FOUND ON THE BOTTOM SURFACE OF THE STRINGER 39L , BETWEEN STA 1197+193 AND STA 1197+218 IN AFT CARGO. C/W ERA 585883-14 (LP 1543064)
CORROSION LEVEL: 2 WING CENTER SECTION UPPER SURFACE AT STA 955 RBL 76 FOUND CORROSION C/W ERA 585848-14 (LP 1543055)
THE SCRATCH OF THE LH SIDE FUSELAGE SKIN AFT L-3 PASSENGER ENTRY DOOR AT STA 1537, BETWEEN S-21L AND S-22L FOUND OVER THE LIMIT. C/W ERA 38217-14 (LP 1540988)
THE AUXILIARY SPAR WEB AROUND THE SCREW HOLE WHERE IT ABOVE THE LH SIDE AUX SPAR CHORD AT APPROXIMATELY FSS 193 FOUND CRACK. REPAIRED PER ERA 585991-14 (LP 15411190)
LH SIDE VERTICAL STABILIZER SKIN BETWEEN AUX SPAR AND FRONT SPAR AT STA FSS 220 TO STA FSS 245 FOUND DELAMINATION. REPAIRED PER ERA 585841-14 (LP 1540339)
RH SIDE FUSELAGE SKIN AT BS STA 1725.5, NEAR THE S-7R AS MARKED POINT FOUND CRACK. REPAIRED PER SRM 53-80-01 (LP 1540356)
LH SIDE INTERNAL SKIN OF THE VERTICAL STABILIZER FOUND DELAMINATION AT FSS 170 TO FSS 220. 19 NICH AFT OF THE AUX FRONT SPAR. REPAIRED PER ERA 585841-14 (LP 1540344)
LH SIDE VERTICAL STABILIZER SKIN BETWEEN AUX SPAR AND FRONT SPAR AT STA FSS 245 TO STA FSS 270 FOUND DELAMINATION. C/W ERA585841. (LP 1540341)
CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE AND VERTICAL SURFACE FOUND CORROSION IN AFT CARGO AT STA 1197+209, BETWEEN S-39R AND S-39L. FOUND OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1538173)
FWD GALLEY AREA FLOOR SUPPORT STRUCTURE AT STA246 RBL 63 FOUND CRACK ON LOWER WEB. REPAIRED PER ERA 586031-14. (LP 1536093)
CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACK AT STA 1480 RBL 54.75 FOUND CORROSION OUT OF LIMITS. REPLACED SEAT TRACK. (LP 1536081)
NO.1 PYLON WIRE BUNDLE WEB CUTOUT AT NAC STA255 FOUND CRACK. C/W REPAIRED PER ERA585803-14 (LP 1533339)
CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE AND VERTICAL SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+132,BETWEEN S-39R AND S- 39L FOUND OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1533335)
#2 ENG PYLON STRUT UPPER WEB I/B WIRING CUT OUT FOUND CRACKED AT NAC STA223 TO NAC STA235. (LP 1533329)
CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+231,BETWEEN S-39L AND S-39R OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1533285)
CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE AND VERTICAL SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+168,BETWEEN S-39R AND S-39 OUT OF LIMITS. REPLACED SHEAR TIE.
CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+231,BETWEEN S-39L AND S-39R OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1533276)
CORROSION LEVEL: 2 FOUND CORROSION ON THE UPPER SURFACE AND VERTICAL SURFACE OF THE SHEAR TIE IN AFT CARGO AT STA 1197+88,BETWEEN S- 39R AND S-38R OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1532432)
CORROSION LEVEL: 2 FOUND CORROSION ON THE UPPER SURFACE AND VERTICAL SURFACE OF THE SHEAR TIE IN AFT CARGO AT STA 1197+66,BETWEEN S- 39L AND S-39R OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1532460)
CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE AND VERTICAL SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+132,BETWEEN S-38R AND S- 39R OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1532538)
CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE AND VERTICAL SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+110,BETWEEN S-38R AND S- 39R AND FOUND OUT OF LIMJITS. REPLACED THE SHEAR TIE. (LP 1532522)
CORROSION LEVEL: 2 FOUND CORROSION ON THE UPPER SURFACE AND VERTICAL SURFACE OF THE SHEAR TIE IN AFT CARGO AT STA 1197+88,BETWEEN S- 39R AND S-39L OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1532474)
CORROSION LEVEL: 2 FOUND CORROSION ON THE UPPER SURFACE AND VERTICAL SURFACE OF THE SHEAR TIE IN AFT CARGO AT STA 1197+66,BETWEEN S- 39L AND S-38L. FOUND OUT OF LIMITS AND REPLACED SHEAR TIE. (LP 1532204)
CORROSION LEVEL: 2 THE SHEAR TIE UPPER SURFACE FOUND CORROSION IN AFT CARGO AT STA1263,BETWEEN S-39L AND S-39R OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1532409)
DURING INSPECTION STAG FOR MAINTENANCE H CHECK FOUND CRACK COMMON TO THE #2 PYLON UPPER SPAR WEB AT NAC STA 221.25-237 AT POWER FEEDER CABLE CUTOUT TO THE INBOARD FORWARD NUTPLATE. C/W ERA 585804-14. (LP 1531838)
THE SHEAR TIE UPPER SURFACE AND VERTICAL SURFACE FOUND CORROSION IN AFT CARGO AT STA1197+168,BETWEEN S-39L AND S- 38L. LOG-PAGE UPDATED MEASURED THE CLEAN UP SHEAR TIE DEPTH IS 0.006" REMAIN THICKNESS IS 0.034" THE ORIGINAL THICKNESS IS 0.040" ALLOWABLE DAMAGE .IS 10% ORIGINAL THICKNESS AND FOUND OUT OF LIMIT AS PER B767-400 SRM 53-00-07 ALLOWABLE DAMAGE .2 RELEASE:59.00 DATE:19 DEC 19. REMOVED AND REPLACED THE SHEAR TIE AS PER B767-400 SRM 51-40-02 (1531454)
FOUND CORROSION ON THE UPPER SURFACE AND VERTICAL SURFACE OF THE SHEAR TIE IN AFT CARGO AT STA 1197+88,BETWEEN S- 39L AND S-38L. LOG-PAGE UPDATED MEASURED THE CLEAN UP SHEAR TIE DEPTH IS 0.007".REMAIN THICKNESS IS 0.033" THE ORIGINAL THICKNESS IS .0.040" ALLOWABLE DAMAGE IS .10% ORIGINAL THICKNESS AND FOUND OUT OF LIMIT AS PER B767-400 SRM 53-00-07 ALLOWABLE DAMAGE .2 RELEASE:59.00 DATE:19 DEC 19. AND REMOVED AND REPLACED THE SHEAR TIE AS PER B767-400 SRM 51-40 -02 RELEASE (1531429)
DURING HEAVY CHECK A CRACK WAS NOTED ON STRUT #2 FWD UPPER SPAR. REFER TO ERA 585799-14AD. (LP 1528295)
DURING INSPECTION MAINTENANCE FOUND #1 PYLON FWD UPPER SPAR WEB A TNAC STATION 221.25-237.5 AT POWER FEEDER CABLE CUTOUT CRACKED. REPAIRED PER ERA 585803-14. (LP 1528007)
EXT EMER LET @ DOOR 4L INOP C/A REP PWR SUPPLY & BATT PACK M739 REF B767-400 M/M 33-51. LT OPS CK GOOD. (6221800)
4L OVERHEAD EMERGENCY EXIT LIGHT AND EMERGENCY LIGHT OUTSIDE 4L DOOR INOP R/R BATTERY AND CHARGER IAW B767 AMM 33-51 AT 4R DOOR NO HELP R/R BATT PACK FOR 4L DOOR IAW B767-400 AMM 33-51 AND RELAMPED EXT LIGHT OPS CK GOOD (6389839)
IMMEDIATELY AFTER T/O F/A CALLED COCKPIT TO SAY THEY HAD A BURNING ODOR. INVESTIGATION FOUND L1 SUPPLEMENTAL HEAT VERY HOT. ODOR DISAPPEARED AFTER A FEW MINS. T/S C/O, SLIGHT ELECTRICAL SMELL NOTED FROM DOOR L1 SUPPLEMENTAL FLOOR HEATER. CONNECTOR AND WIRING INSPECTED WITH NIL FAULTS NOTED. L1 DOOR HEATER DEFERRED PER MEL 21-45-03, M PROC COMPLIED WITH, CBS D1 & D2 P36 PULLED AND COLLARED. PLACARD INSTALLED. AS A PRECAUTION BOTH PACKS RAN, RE-CIRC FANS, ALL LIGHTS IN GALLEY & FWD CABIN INSPECTED. GALLEY OVENS & CHILLERS, ALL IFE MONITORS CHECKED WITH NIL FAULTS NOTED. R/R L1 ENTRY DOOR HEATER PER B767-400 21-45 OPS CHK NML A/C OK FOR SVC PLACARD AND MEL RMVD. (LP6556016)
ATB - FIRST OFFICER PITOT HEAT FAILED AFTER TAKEOFF ROTATION. MAINTENANCE REPLACED PROBE AND SYSTEM OPERATION CHECKS NORMAL. AIRCRAFT RTS.
SLIGHT ELECTRICAL BURNING ODOR DETECTED IN AFT GALLEY. DISSIPATED AFTER GALLEY LIGHTS WERE LOWERED REMOVED, CLEANED AND INSPECTED AFT GALLEY VENT FILTERS FLOW NORMAL. INSPECTED RECIRC. FAN FILTERS AND ASSOCIATED COMPONENTS. NO DEFECTS NOTED. NO ABNORMAL SMELLS NOTED NOTIFIED OPS CHECKED ALL AFT GALLEY COFFEEMAKERS NO DEFECTS NOTED.
SHIP 1801 - ATO - CREW REPORTED WINDSHEAR WARNING AT 70KTS AND EXECUTED REJECTED TAKE-OFF. CORRECTIVE ACTION: CREW TESTED WEATHER RADAR AND ALL CHECKED GOOD. CONTINUED IN DEPARTURE SEQUENCE AND PERFORMED NORMAL TAKE-OFF.
EXIT LIGHTS BY 4L DOOR INOPERATIVE. REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.
SHIP 1801 - ABORTED TAKEOFF AT 90 KNOTS DUE TO AUDIBLE WINDSHEAR. CORRECTIVE ACTION: REPLACED WEATHER RADAR TRANSCEIVER. PERFORMED HIGH ENERGY STOP INSPECTION.
DURING SERVICE VISIT IN ATL, HEAVY CORROSION FOUND ON BELLY SKIN AT STA 1081 C/W ERA 572350-14.
DURING SERVICE CHECK ON WALK AROUND FOUND TWO CRACKS ON LOWER SKIN JUST AFT OF MAIN GEAR DOOR, BELLY SKIN. REPAIRED DAMAGED SKIN IAW ERA 572350-14.
FUSELAGE EXTERNAL SKIN WAS DENTED AT BS 1551, BETWEEN STRINGERS 23L AND 24L. THE DENT WAS OUT OF LIMITS. REPAIRED IAW SRM 53-00-01, AND ERA 568948-14.
FOUND THE CABIN FLOORBEAM LOWER TEE FASTENER HOLE CORRODED AT BS 1439, LBL 35. REPAIRED IAW ERA 568917-14.
DURING PERFORMANCE OF AMDS CARD 5312-01170-05, UT INSPECTION ON THE BS 955 FAILSAFE STRAP, FOUND A CRACK INDICATION. REPAIRED IAW 5312-01170-10A-02.
DURING PERFORMANCE OF AMDS CARD 5312-01170-05, HFEC OPEN HOLE AND HFEC SURFACE INSPECTION ON THE BS 955 FAILSAFE STRAP FOUND CRACKED. REPAIRED IAW ERA 568799-14.
DURING PERFORMANCE OF AMDS CARD 5312-01170-05, HFEC OPEN HOLE INSPECTION, ON THE BS 955 FAIL SAFE STRAP AT THE LWR OF THE THREE FASTENER HOLES FOUND LOWEST HOLE TO BE CRACK AT 2 O'CLOCK AND 7 O'CLOCK. C/W ERA 568799-14.
AFT CARGO BAY, FOUND TWO SHEAR TIES CORRODED AT BS 1285 BETWEEN STRINGER 39L AND 38R, FOUND OUT OF LIMITS AND REPLACED IAW SRM 51-40-02, AND 53-00-07.
AFT CARGO BAY SHEAR TIE WAS CORRODED AT BS 1307, STRINGERS 39L TO 39R. FOUND OUT OF LIMITS. REPLACED IAW SRM 53-00-07, AND 51-40-02.
MFEC INSPECTION FOUND ONE CRACK, APPROXIMATELY 0.80 IN LENGTH ON THE NOSE WHEEL WELL LT VERTICAL STIFFENER AT BS 287, WL 159 TO WL 185. THE STIFFENER WAS REPAIRED.
DURING AN MFEC INSPECTION, FOUND ONE CRACK APPROXIMATELY .0.80 IN LENGTH, ON THE NOSE WHEEL WELL RT VERTICAL STIFFENER AT BS 287, WL159 TO WL 185. REPAIRED.
DURING A SERVICE CHECK, FOUND THE EMERGENCY LIGHTS OUT AT 23R TO 27R. FOUND THE CONNECTOR AT SEAT 23FG DISCONNECTED. CONNECTED THE CONNECTOR AND OPS CHECKED GOOD.
EMERGENCY R3 DOOR HANDLE BROKEN. INSTALLED AN ASSIST HANDLE. CHECKED NORMAL. OK FOR SERVICE.
DURING A SERVICE CHECK, FOUND THE EMERGENCY LIGHT BENEATH THE STAIRS INOPERATIVE. ALL BULBS BURNED OUT. REPLACED THE BULBS IAW AMM 33-51 OPS NORMAL.
R4 DOOR SLIDE INDICATIOR INOPERATIVE. CLEANED DEBRI FROM DOOR FRAME SURROUNDING AND OPERATED DOOR, LIGHT WORKS OK, INDICATIONS ARE OK. ARMED AND DISARMED OK.
R4 DOOR INTERIOR FRAME APPEARS TO BE BENT. LOWER PART OF DOOR APPEARS TO BE DAMAGED. FOUND THE BUSTLE NOT ALIGNED WITH DOOR, ALIGNED THE BUSTLE, DOOR WORKS NORMAL. OK FOR SERVICE.
R4 DOOR SLIDE ARMED LIGHT INOPERATIVE. THE SLIDE ARMED LIGHT CHECKED. TROUBLESHOT IAW FIM 52-73, SSM 52-73, SM 32-09-01, AND SSM 32-09. REPLACED THE LAMP, OPS CHECKED OK. (3950481).
R4 DOOR WOULD NOT ARM. THE DOOR WAS INSPECTED AND DEBRIS FOUND OBSTRUCTING THE GIRT BAR FITTING. THE DEBRIS WAS REMOVED AND ARM/DISARM LEVER CYCLED MULTIPLE TIMES, NORMAL, OPERATES FREELY. SYSTEM SERVICEABLE.
L2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE FUSE IN THE BATTERY PACK SUPPLY IAW WDM 33-51.
EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS 900. ALL EMERGENCY LIGHTS AND SIGNS OPS NML AT THIS TIME. EXIT LIGHT IN CREW REST RELAMPED.
THE L3 DOOR EMERGENCY LIGHTS ARE INOPERATIVE. R & R THE POWER SUPPLY.
FWD TRUNNION BEARING STRESS STRAP HOLE TOOLING DAMAGED. REPAIRED PER SECTION 1 ER/A 557794-14AD.
FOUND PLENUM CRACKED. REPLACED LT PLENUM (FAN INLET DIFFUSER HOUSING) PER WORKCARD 2151-4303.
FOUND ON SERVICE CHECK. INTERIOR EMERGENCY LIGHT LENS DAMAGED 2 EA LOC 603. REPLACED LENS.
FOUND ON SERVICE CHECK. EMERGENCY LIGHT ASSY DAMAGED AT DOOR 1R. REPLACED LENS ASSY. OPS CK GOOD.
EMERGENCY LIGHT LENS MISSING FROM CONTROL PANEL. REPLACED THE LENS IAW AMM 33-51.
DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE AND EXIT SIGNS AFT GALLEY OVERHEAD INOPERATIVE. FOUND HARNESS PLUG LOOSE UNDER SEAT 15FG. SECURED SAME AND FOUND C/P ON POWER SUPPLY M1210 LOOSE. SECURED SAME.
AFT CARGO BAY BS 1197+185, S39R INNER SKIN FOUND BULGED. REPAIRED IAW PRI 524527-14, REV 0 & REV 1. PRI 524527-14, REV 0 & REV 1.
AFT CARGO BAY BETWEEN BS 1197+132 -1197+154 S39R, FOUND CORRODED. ACCOMPLISHED REPAIR IAW PRI 524527-14, REV 0 & REV 1. PRI 524527-14, REV 0 & REV 1.
HFEC OPEN HOLE INSPECTION CARRIED OUT, FOUND HOLE, ONE CRACK ON RT SIDE BS 955, FAILSAFE STRAP AT LOWER OF THE THREE FASTENER HOLES. REPAIRED IAW PRI 524525-14AD, REV O AND REV 1. PRI 524525-14AD, REV 0 AND REV 1.
FOUND SURFACE CORROSION ON UPPER EXTERNAL SURFACE OF HORIZONTAL STABILIZER CENTER SECTION BETWEEN 1725-1809, RBL5. REPAIR IAW PRI 524542-14, REV 0, 1 & 2. PRI 524542-14, REV 0, 1 & 2.
AFT CARGO BAY BETWEEN BS 1197+132-1197+154 S37R, FOUND CORRODED. REPAIRED IAW PRI 524527-14, REV 0 & REV 1. PRI 524527-14, REV 0 & REV 1.
AFTER AN HFEC INSPECTION, FOUND A CRACK INDICATION ON BS 1809 BULKHEAD, RT FWD OUTER FRAME BETWEEN STRINGERS 6 - 7R. REPAIRED IAW SRM 53-80-08, REPAIR 9.
ON SERVICE CHECK, FOUND EMERGENCY LIGHTS ON SEAT 30 A/B THRU 42 A/B INOPERATIVE. RT AND RT CHARGER AT SEAT 32 A/B, PN 0717-02-030, LIGHT CHECKED GOOD.
EMGENCY LIGHT BATTERY PACK FAILED TEST IAW CHECK 74. R & R BATTERY PACK M1208 IAW AMM 33-51-07, OPS OK.
EMERGENCY LIGHTS AT ROW 20AB THRU 27AB ARE INOPERATIVE. BATTERY CHARGER REPLACED. SYSTEM OPS NORMAL.
EMERGENCY EXIT SIGN NEAR 30AB/L3 DOOR DIM. MAINTENANCE FOUND BATTERY AT CHARGER M7236 WEAK AND REPLACED BATTERY. SYSTEM OPERATION IS NORMAL.
BATTERY PACK M732 FAILED AND REPLACED. SYS OPS NORMAL.
DURING OPS 6803, FOUND EMERGENCY PATH BATTERY MOUNT CAMLOCK BROKEN ON POWER SUPPLY M6758. REPLACED POWER SUPPLY. SYSTEM OPERATION IS NORMAL.
DURING OPS 6803 BATTERY PACKS M730 M6756 M736 M737 M738 FAILED. REPLACED. SYSTEM OPERATION IS NORMAL.
DURING DRC MAINTENANCE FOUND L1 R1 DOOR EMERGENCY LIGHTS INOPERATIVE. POWER SUPPLY MODULE AT L1 DOOR WAS REPLACED. SYSTEM OPERATION IS NORMAL.
EMERGENCY PATH LIGHTS AT ROWS 21-27 ARE INOPERATIVE. MAINTENANCE FOUND CONNECTOR D21160 LOOSE AND RE-SECURED. SYSTEM OPERATION IS NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS
ON DRC MAINTENANCE FOUND THE EMERGENCY LIGHTS AT ROW 30AB - 44AB HAD A BATTERY FAULT AND REPLACED THE BATTERY. SYSTEM OPERATION IS NORMAL.
MAINTENANCE FOUND THE EMERGENCY ESCAPE LIGHTS AT DOOR 3L, THE AISLE EXIT SIGN, AND OUTSIDE FUSELAGE LIGHTS ALL TO BE DIM. AFTER CLEANING BULB AND SOCKET OUTSIDE OF DOOR L3 THE OPERATION OF THE LIGHTS WAS NORMAL.
FUSELAGE SKIN DENTED AT FS 1506 & 1514. REPAIRED IAW ERA 482800-14AD.
AFTER T/O RECEIVED RT HPSOV EICAS MSG. UNABLE TO RESET. RETURN TO ATL DUE TO GATE AND CREW AVAILABILITY. FWD TO MCO /PLAC PER MEL 36-11-02 HPSOV LOCKED CLOSED NR 2 ENG (ODI 2010-D0925) (DL764101994).
DIVERSION DUE TO ODOR IN AFT CABIN. MX IN PROGRESS.
DURING THE PUSH BACK, SMOKE ENTERED THE CABIN. RETURN TO GATE. AMM 21-00-21-102-001. NO SMOKE OR OIL ODOR FELT IN THE CABIN. CAUSE OF SMOKE DETERMINED TO BE THE APU. LOSS OF OIL FROM APU NOTED.
FLIGHT 130/27 ATB TO ATL - DUE TO CTR SYS HYD QUANTITY DROPPING. NO FURTHER INFO AT THIS TIME. FOUND O-RING LEAKING AT THE FILTER PLUG OF THE NR 4 SPOILER ACTUATOR. REPLACED O-RING, LEAK CKS OK.
MODE C REPORTED INOP BY BOTH GROUND AND TOWER. TCAS CHECKS GOOD. PERFORMED TEST OF BOTH ATC TRANSPONDERS. NO DEFECTS. ALL CHECKS NORMAL. OK FOR SERVICE, TESTED WITH ATC.
ACFT RTB AFTER CREW REPORTED YSM AND F/O DISPLAY TRU STATUS MESSAGES. CREW LEFT RUNWAY AND RETURNED TO GATE IN ORDER TO ATTEMPT RESET AND THEN PLACE ITEMS ON FLIGHT CREW PLACARD AS PER MCC TLX. THIS MSG COULD APPEAR IF ACFT ON BATTERY POWER ONLY FOR 1 MIN. ACFT DOWN POWERED MCDP MSG CLEARED AND STS M CLEARED. MCO AND PLACARD REMOVED.
NUMEROUS ABNORMAL CAUTION MSGS ON TAXI OUT. DOOR MSG BULK CARGO. CLEARED ALL MSG. REPLACED PSEU, BIT CK OK. NO ABNORMAL CAUTION MSG OK FOR SVC.
LEFT VHF PANEL STARTED DISPLAYING FAIL INTERMITTENTLY THEN CONTINUOUSLY. RESET CB, FAIL WENT AWAY BUT COULD NOT TRANSMIT OR RECEIVE ON VHF OR STACOM. RT VHF AND STACOM WAS ABLE TO RECEIVE BUT NOT TRANSMIT. AFTER 10 MIN, RT VHF COULD TRANSMIT ON A HANDFULL OF FREQUENCIES ACARS COULD RECEIVE, BUT NOT TRANSMIT. ACARS AND ATC INTERMITTENT. OPN OF ALL RADIOS NORMAL ON GROUND IN GRU. SWAPPED LT AND CENTER TRANSCEIVER AND LT AND CENTER RTPS AS PRE-CAUTION. CLEANED LT/RT VHF ANTENNA CONNECTORS. PERFORMED LIGHTNING STRIKE AND OVWT LDG INSPECTION ATC/VHF/SATOM/ACARS ALL TESTS NORMAL.
BATTERY CHARGER M7236 STA 1197 PLUS 77 LBL 94 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER M7236 DURING HMV 1 AT TIMCO IN GSO ON NR 44974.
BATTERY CHARGER M730 STA 401 RBL 95 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER OPS CK GOOD. REPLACED DURING HMV1 ON N/R 44971 AT TIMCO IN GSO.
BATTERY CHARGER M7235 STA 654A PLUS 33 LBL 94 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER M7235 ON NR 44972, DURING HMV AT TIMCO IN GSO.
BATTERY CHARGER M6759 STA 841 LBL 94 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER DURING HMV 1 AT TIMCO AT GSO ON NR 44973.
BATTERY AT CHARGER M12 STA 1545 RBL 53 BATTERY WON`T CHARGE. REMOVED AND REPLACED BATTERY, DURING HMV1 AT TIMCO IN GSO ON NR 44981.
BATTERY CHARGER M1208 STA 284 LBL 53 INOP. REMOVED AND REPLACE BATTERY CHARGER ON N/R 44980 DURING HMV1 AT TIMCO IN GSO.
BATTERY CHARGER M734 STA 1384 RBL 95 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER M734 ON NR 44975, DURING HMV 1 AT TIMCO IN GSO.
FAS REPORTED A SCREECHING SOUND WHEN STARTING FWD NR 1 OVEN. SUBSEQUENT HOT ELECTRICAL SMELL IN FWD GALLEY. FWD OVENS WERE SHUT OFF AND SMELL DISSIPATED. NR 1 OVEN IS BELIEVED TO BE SOURCE OF ODOR. PULLED FWD GALLEY U-33 CIRCUIT BREAKER AS PRECAUTION. RESET U-33 BREAKER FWD TO MCO NR 1 OVEN PER MEL 25-20-01H. NIS HNL - NDS 250007390. W/GALLEY PWR ON, ELECTRICAL SMELL NOTED. REPLACED NR 1 OVEN FWD GALLEY FOR PRECAUTION DUE TO HOT ELECTRIC SMELL AND SCRATCHING SOUND WHEN OVEN WAS TURNED ON OVEN CKS OK. MCO/PLAC REMOVED. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.
ELEC ODOR IN COCKPIT AT FLT 350 AND .80 MACH WITH EQUIP COOLING FAN STATUS MSG. REPLACED FWD EQUIP COOLING EXHAUST FAN PER M/M. MCO/PLAC RMVD.
DURING TAXI FOR T/O, EICAS MESSAGE RT HYD QTY ON STATUS PAGE. RT HYD SYS IND 1.02. FWD TO MCO AND PLACARD PER MEL 29-33-02. PERFORM REP CK RT HYD QTY CKS FULL, NO MSGS AND NO DISCREPANCIES NOTED RT HYD QTY SYS NORMAL MCO/PLAC REMOVED.
CTR HYD QTY DROPPED TO .29 INFLIGHT. MX IN WORK, FOUND NR 4 SPOILER LEAKING LEFT WING. SERVICE HYD SYSTEM. REPLACED O-RING ON NR 4 SPOILER ACTUATOR. LEAK CHECKED OK. CHECKED DIFFERENTIAL FILTER INDICATING ON CENTER ACMPS BOTH CHECK OK. CYCLED SPOILERS CONTROL SURFACES, NO FURTHER LEAK NOTED.
LEFT ENG START VLV WILL NOT OPEN. DEFERRED PER MEL 80-00-02, REPLACED NR 1 ENG START VLV, LEAK CHECK OK. OPS CHECKS OK.
CENTER HYD QTY WENT TO ZERO AFTER ENGINE START. REPLACED HYD QTY MONITOR UNIT. CHECKS GOOD, MCO PLACARD REMOVED.
R BLEED OFF LIGHT WOULD NOT EXTINGUISH. BIT ASCTU FAULTED R SIDE 36-13205 DID NOT SHOW ON LEFT RESEATED CONNECTOR PRSOV. RAN ENGINE, ALL PNEU OPS NORMAL.
SMOKE FUMES IN THE CABIN. RT RECIRC FAN AND FWD IFE COOLING STATUS MESSAGE. ACCOMPLISHED SMOKE REMOVAL CHECKLIST AND SMOKE DISSIPATED. RT RECIRC FAN C/B POPPED INFLT. REPLACED FAN.
TWO OVERHEAD EXIT LIGHTS INOPERATIVE. RELAMPED SAME.
BOTH HF RADIOS UNABLE TO TRANSMIT, AUDIO OK. RESET C/B`S SEVERAL TIMES, NO HELP. REPLACED NR 2 HF COUPLER.
ON PREFLIGHT FOUND NOSE GEAR RETRACT CYLINDER RAM CRACKED AT ROD END ATTACH POINT. REPLACED NOSE GEAR RETRACT CYCLINDER BORROWED FROM AA, S/N ON 00196, S/N OFF 00822, ASSY NR 273T4112-4.
EMERGENCY LIGHTS ON SEATS 17AB THRU 25AB INOP. SEATS ONLY LEFT SIDE. FOUND PWR SUPPLY M 6759 AT FAULT. REPLACED SAME, CHECKS GOOD.
ENTERTAINMENT POWER UNIT UNDER SEAT 11D WARM TO THE TOUCH WITH NOTICEABLE ODOR. SHUTDOWN THE ENTERTAINMENT SYS UNIT UNDER 11D. REPLACED 11 CDE AVU LOADED SOFTWARE, CHECKS OK .
AT CRUISE L GEN CONT TRIPPED OCCURRED WHILE TRYING TO ELECTRICALLY OPEN EN CHANCED COCKPIT DOOR. STARTED APU THEN REFERRED TO QRH. RESET WAS SUCCESSFUL EXCEPT L BUS TIE REMAINED OPEN. GEN OPERATED NORMALLY FOR REMAINDER OF FLIGHT. ALL BITE ON BPCU L AND R GCUS, NO FAULTS. RESET LT BUS TIE. ACCOMPLISHED ENGINE RUN. ELEC LOADS AND VALUES NORMAL. APPLIED FULL ELEC LOAD. NO FURTHER TRIPS NOTED.
ALTERNATE SLAT INBOARD ELECTRIC ACTUATOR POPPED C/B. REPLACED SLAT PDU INBD ELECT MOTOR. OPS CHECK NORMAL.
THE 29AB EMERGENCY LIGHT INOP. INSTALLED BULBS AND LENS COVER, OPS CHECK GOOD.
AT FL 370 LOST F/D - AUTOTHROTTLES AND A/P LATER WE GOT L/E SLAT DISAGREE CAUTION MSG ALONG WITH NUMEROUS ADVISORY MSGS. AILERON LOCKOUT AND STBY BUS OFF, ALSO NOTICED THAT DC STBY BUS C/B AND BUS DISTR C/B HAD POPPED AFTER LANDING. ONCE ON GROUND MTC RESET CBS, ALL MSGS CLEARED. INSPECTED BATTERY AND CHARGER, CKS OK. INSPECTED RELAYS K105-K109 CKS OK. BPCU SHOWED NO FAULTS. REPLACED BPCU AS PRECAUTIONARY. MTC FERRIED TO ATL ON 9936. REPLACED OVERHEAD PANEL, K109Â¥ K106 AND K104 RELAYS STDBY POWER FOR PRECAUTION.