N902AN
Registered owner: AMERICAN AIRLINES INC, TX (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
AIRCRAFT IN BASE MAINTENANCE: L/H FWD EMERGENCY EXIT DOOR HANDLE NEEDS NEW BUSHINGS AND NEW SCREW. MARKED WITH RED TAPE. MAINTENANCE REPLACED WITH NEW BUSHINGS AND NEW SCREW AT L/H FWD EMERGENCY EXIT DOOR HANDLE IAW AIPC 52-22-51
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: SPEED LIMIT FLAG APPEARS INTERMITTENTLY ON CAPTAIN'S PFD. WHEN THE FLAG APPEARS THE MIN MANEUVERING AMBER BAR DISAPPEARS AS WELL AS THE VERTICAL PORTION OF THE CAPTAIN'S FLIGHT DIRECTOR, WHICH THEN DISENGAGES THE AUTOPILOT. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW. REMOVED AND REPLACED LEFT (AOA)-ANGLE OF ATTACK. PER AMM 34-21-05.
AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR HARD TO OPEN. FOUND DOOR RUBBING ON METAL THRESHOLD PLATE, ADJUSTED THE LAVATORY-A DOOR THRESHOLD. PER AMM 25-40-00.
AIRCRAFT WAS GROUNDED: DURING THE LANDING ROLL AND AGAIN DURING THE TAXI, THE ANTI-SKID AND BRAKING SYSTEM HAD A TENDENCY TO SKIP AND STUTTER. PERFORMED (AACU)-ANTISKID AUTOBRAKE CONTROL UNIT BITE PER FIM 32-42-00-810-801. FOUND MULTIPLE FAULTS. REMOVE AND REPLACED AACU, PER AMM 32-42-21. PERFORMED OPERATIONAL TEST PER AMM 32-42-00 FAULTS CLEARED.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AT AFT LAVATORY OVERBOARD VENT AT BS 907 BETWEEN S21L AND S22L. REPAIRED SKIN PER SRM 53-70-01-2R-3.
AIRCRAFT IN BASE MAINTENANCE: AFT PRESSURE BULKHEAD OIL CAN DAMAGE AT BS 1016, BETWEEN S11R AND S12R. REPAIRED BULKHEAD PER SB-737-53-007051.
AIRCRAFT IN BASE MAINTENANCE: AFT PRESSURE BULKHEAD OIL CAN DAMAGE AT BS 1016, BETWEEN S1L AND S2L. REPAIRED BULKHEAD PER SB-737-53-007051.
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR TAB CONTROL MECHANISM HAS EVIDENCE OF CORROSION ON LOWER SPRING ATTACHMENT POINTS. (4 EA). REMOVED AND REPLACED RIGHT HAND HORIZONTAL STAB ELEVATOR SPRING. SUPPORT, PER PER B737-NG AMM 27-31-34. PERFORMED SATISFACTORY ELEVATOR ANDELEVATOR TRIM CONTROL SYSTEM OPERATIONAL TEST, PER B737-NG AMM 27-31-00-710-801.
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND SIDE OF FUSELAGE SKIN IS CORRODED AT AFT LAVATORY OVERBOARD VENT AREA AT STA 907 BETWEEN STR 21L AND 22L. REPAIRED LEFT HAND SIDE OF FUSELAGE SKIN IS CORRODED AT AFT LAVATORY OVERBOARD VENT AREA. PER B737 SRM 53-70-01-2R-3.
AIRCRAFT WAS NOT GROUNDED: LOWER EXIT SIGN AT 17A MISSING. REINSTALLED EXIT SIGN AT 17A AND OPERTIONAL CHECK GOOD. PER AMM 33-51-00.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER S25L AT STA 837. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-03-2R-1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN INTERCOSTAL LOCATED FROM STA 847 TO STA 867 AT S25L. REPLACED INTERCOSTAL PER AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: EES BATTERY FOUND WITH INOPERATIVE CIRCUITS. REMOVE AND REPLACED BATTERY PACK OPERTIONAL CHECK GOOD.
AIRCRAFT IN BASE MAINTENANCE: EES BATTERY PACK FOUND WITH SOME INOPERATIVE CURCUITS. REMOVE AND REPLACED BATTERY PACK, OPERTIONAL CHECK GOOD.
AIRCRAFT IN BASE MAINTENANCE: EES BATTERY PACK FOUND WITH SOME INOPERATIVE CIRCUITS. REMOVE AND REPLACED BATTERY PACK, OPERTIONAL CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTANDENT FLASHLIGHT IS FLASHING RED. REPLACED FORWARD FLIGHT ATTENDANT INBOARD FLASHLIGHT ASSEMBLY. PER AMM 25-64-00.
AIRCRAFT WAS NOT GROUNDED: EXIT SIGN OVER AFT ENTRY DOOR FELL OFF AFTER TAKEOFF. RESECURED EMERGENCY EXIT LENS AT L2 DOOR. PER AMM 33-51-01.
AIRCRAFT WAS NOT GROUNDED: FIRST CLASS LAVATORY DOOR STICKS. HARD TO OPEN AND CLOSE. ADJUSTED BOTTOM OF DOOR PER STANDARD PRACTICES.
AIRCRAFT WAS NOT GROUNDED: AFT MEGAPHONE DUE FOR MX. REMOVE AND REPLACED MEGAPHONE. PER AMM 25-64-00.
AIRCRAFT WAS NOT GROUNDED: FORWARD MEGAPHONE DUE FOR MX. REMOVE AND REPLACED MEGAPHONE. PER AMM 25-64-00.
AIRCRAFT WAS GRO UNDED: SMOKE ODOR FUMES REPORTED EVENT. ACCOMPLISHED SMOKE FUMES INITIAL TROUBLESHOOTING ODOR CARD 08L00021001. NO ODORS FOUND, NOT FAULT FOUND.
AIRCRAFT WAS GROUNBDED: 1L DOOR WAS VERY DIFFICULT FOR THE AGENT TO OPEN ON ARRIVAL. (OPEN).
AIRCRAFT WAS GROUNDED: 1L DOOR WAS VERY DIFFICULT FOR THE AGENT TO OPEN ON ARRIVAL.**SUPPLEMENTAL REPORT FOR (AALA202404263142): ADJUSTED HORIZONTAL CONTROL ROD, OPERTIONAL CHECK GOOD NO DEFECTS NOTED AT THIS TIME. PER AMM 52-11-00-820-801**(CLOSED).
AIRCRAFT IN BASE MAINTENANCE: FOUND CRACK IN AFT LEFT HAND OF SECTION 48 JUST AFT OF BS 1138 MEASURING 2 INCHES LENGTH BY 0.063 IN WIDTH AND 0.30 IN DEPTH. ITEM MINOR IN NATURE. PERFORMED A GENERAL VISUAL INSPECTION OF AREA, FOUND DAMAGE WITHIN LIMITS. PREFORMED RESIN SWEEP PER AARD 53-00-00 AND AARD 53-70.**(CLOSED)
AIRCRAFT IN BASE MAINTENANCE: FOUND CRACK IN AFT LEFT HAND OF SECTION 48 JUST AFT OF BS 1138 MEASURING 2 INCHES LENGTH BY 0.063 IN WIDTH AND 0.30 IN DEPTH. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND BOTTOM CORNER OF (GPU)-ELECTRICAL GROUND POWER RECEPTACLE ACCESS OPENING IS CRACKED. TRIMMED OUT THE DAMAGED AREA OF (GPU) INSTALLED DOUBLER REPAIRED. PER SRM 53-10-15-1A PROCEDURE 4.
AIRCRAFT IN BASE MAINTENANCE: EXFOLIATION CORROSION IN THE ADVANCED STAGE OF DETERIORATION FOUND ON THE RIGHT HAND SIDE OF THE UPPER FORWARD TAIL CONE. LOCATED AT AFT OF RUB STRIP AND JUST UNDER HORIZONTAL STAB. ÿ½ **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).
AIRCRAFT IN BASE MAINTENANCE: EXFOLIATION CORROSION IN THE ADVANCED STAGE OF DETERIORATION FOUND ON THE RIGHT HAND SIDE OF THE UPPER FORWARD TAIL CONE. LOCATED AT AFT OF RUB STRIP AND JUST UNDER HORIZONTAL STAB. REPAIRED PER AARD 11-20-00-1 REPAIR 1.
WHILE ACCOMPLISHING WORK CARD 08C20025006 (DVI-EMERGENCY ESCAPESLIDE AND PRESSURE BOTTLE) FOUND HEAT SHRINK TUBING LOOSE AND INTERFERING WITH GIRT BAR FLOOR ATTACH FITTINGS AT R1 SLIDE. MAINTENANCE REPLACED RED HEAT SHRINK TUBING IAW AARD 25-66-00-4
AIRCRAFT WAS NOT GROUNDED: WHILE ACCOMPLISHING WORK CARD 08C20025006 (DVI-EMERGENCY ESCAPESLIDE AND PRESSURE BOTTLE) POST EO 2523J012 FOUND HEAT SHRINK TUBING MISSING ON GIRT BAR AT L2 SLIDE, MAINTENANCE REPLACED HEAT SHRINK TUBING AT L2 SLIDE IAW AARD 25-66-00-4.
AIRCRAFT WAS NOT GROUNDED: WHILE ACCOMPLISHING WORK CARD 08C20025006 (DVI-EMERGENCY ESCAPESLIDE AND PRESSURE BOTTLE) FOUND HEAT SHRINK TUBING LOOSE AND INTERFERING WITH GIRT BAR FLOOR ATTACH FITTINGS AT L1 SLIDE. MAINTENANCE REPLACE RED HEAT SHRINK TUBING IAW AARD 25-66-00-4.
AIRCRAFT WAS NOT GROUNDED: WHILE ACCOMPLISHING WORK CARD 08C20025006 (DVI-EMERGENCY ESCAPESLIDE AND PRESSURE BOTTLE) POST EO 2523J012 FOUND HEAT SHRINK TUBING MISSING ON GIRT BAR AT R2 SLIDE. MAINTENANCE REPLACED HEAT SHRINK TUBUING AT SLIDE R2 IAW AARD 25-66-00-4.
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND SIDE PASSENGER FLOOR PROXIMITY LIGHTING SEATS 21 THRU 26 ARE INOPERATIVE. RESECURED CONNECTOR D10716 PER WDM 33-51-22. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND RBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.
AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE INFLIGHT SEEMS TO STICK CLOSED NEAR LOWER AFT CORNER. TIGHTENED LOOSE SCREW ON LOWER DOOR TRIM.
AIRCRAFT IN BASE MAINTENANCE: CAPTAIN'S L2 WINDOW HARD TO CLOSE AND LOCK. REMOVED AND REINSTALLED L2 WINDOW PER AMM 56-12-11-820-801 AND AMM 56-12-400-801. ACCOMPLISHED SATISFACTORY CHECK.
AIRCRAFT IN BASE MAINTENANCE: FORWARD LEFT OVERWING EMERGENCY LIGHT IS DIM. RE-LAMPED THE FORWARD LEFT OVERWING EMERGENCY LIGHT.
AIRCRAFT IN BASE MAINTENANCE: L1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND CONNECTOR D11074 NOT PROPERLY SEATED. PROPERLY INSTALLED CONNECTOR PER WDM 33-51-12 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.
AIRCRAFT IN BASE MAINTENANCE: AFT CARGO COMPARTMENT RIGHT FLOOR TRANSITION PANEL HAS AREAS OF CORROSION ON UPPER SURFACE BETWEEN STA 727F AND STA 787 AND RIGHT BUTT LINE 30. CUT OUT CORRODED Z CHANNEL, FABRICATED 2 EACH Z CHANNELS AND 2 EACH SPLICE PLATES AND INSTALLED.
AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON FUSELAGE SUPPORT INTERCOSTAL UPPER SURFACE APPROXIMATELY BETWEEN STA 948 AND 967 AND STR 20R. REMOVED, FABRICATED, AND INSTALLED INTERCOSTAL PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: RIGHT UPPER T CHORD LOCATED STA 927 26 INCHES FROM BUTT LINE ÿ½0ÿ½ CORRODED. REMOVED FABRICATED AND REPLACED UPPER T CHORD PER SRM 53-70-51-2R-4.
AIRCRAFT IN BASE MAINTENANCE: AFT WEB LEFT SIDE FORWARD OF AFT PRESSURE BULKHEAD CORRODED LOCATED AT STA 1016 AND LEFT BUTT LINE 33. REMOVED AND REPLACED WEB PER SRM 53-70-51-01.
AIRCRAFT IN BASE MAINTENANCE: LEFT AND RIGHT UPPER T CHORD ON FLOOR SUPPORT HAS CORROSION. LOCATED BETWEEN STA 967 TO 986.5 AND RIGHT BUTT LINE 16. REMOVED AND FABRICATED COMPLETE T CHORD INCLUDING SPLICE AND INSTALLED PER SRM 53-70-51-2R-4.
AIRCRAFT IN BASE MAINTENANCE: LEFT FORWARD ENTRY DOOR LOWER SILL INBOARD FLOOR SUPPORT CORRODED LOCATED BETWEEN STA 310 AND 344 AND LEFT BUTT LINE 60. REMOVED AND REPLACED CORRODED ANGLE PER SRM 53-10-15-1A-1.
AIRCRAFT IN BASE MAINTENANCE: AFTER NDT INSPECTION (ROTO) TO EXISTING OPEN HOLES AT FLOORBEAM 986.5 UPPER VERTICAL WEB AREA FOUND 1 EA HOLE WITH CRACK INDICATION. LOCATED BETWEEN RIGHT BUTT LINES 26 AND 27. TRIMMED OUT DAMAGE AND FABRICATED DOUBLER REPAIR PER EA 339770.
AIRCRAFT IN BASE MAINTENANCE: RIGHT WEB HAS CORROSION LOCATED BETWEEN STA 786.5 TO 1016 AND LEFT BUTT LINE 33. REMOVED FABRICATED AND REPLACED WEB PER SRM 53-70-51-1A-1.
AIRCRAFT IN BASE MAINTENANCE: AFT ENTRY DOOR CUT OUT LOWER SILL WEB CORRODED LOCATED BETWEEN STA 967 TO 987 AND LEFT BUTT LINE 60. REMOVED AND REPLACED SILL PER SRM 53-70-15-1A.
AIRCRAFT IN BASE MAINTENANCE: AFT WEB RIGHT SIDE FORWARD OF AFT PRESSURE BULKHEAD CORRODED LOCATED BETWEEN 1016 AND 1036 AND RIGHT BUTT LINE 33. REMOVED AND REPLACED WEB PER SRM 53-70-51-1A.
AIRCRAFT IN BASE MAINTENANCE: LEFT INNER CHORD CORRODED LOCATED BETWEEN STA 890 TO 1006 AND LEFT BUTT LINE 60. REMOVED CORRODED CHORD AND REPLACED WITH NEW CHORD PER SRM 53-70-15-1A.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING INBOARD LEADING EDGE LOWER ATTACH STRAP LOCATED FROM WS 94.24 TO WS 156.25. REPAIRED PER DWG 112A4402 AND EA 340171.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND FLOOR SUPPORT LOCATED FROM BS 942 TO BS 967 AT RBL 24. REPLACED FLOOR SUPPORT PER SRM 51-10-02-0G.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT INNER CHORD LOCATED FROM BS 890 TO BS 1006 AT RBL 60. REPLACED CHORD PER SRM 53-70-15-1A.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND FLOOR SUPPORT LOCATED FROM BS 950 TO BS 967 AT RBL 52. REPLACED FLOOR SUPPORT PER SRM 53-70-51-1A.
AIRCRAFT IN BASE MAINTENANCE: CORROSION AROUND FASTENER HOLES IN AFT CARGO COMPARTMENT AFT BULKHEAD CENTER ACCESS PANEL LOWER SUPPORT LOCATED AT BS 947.5 FROM LBL 10 TO RBL 16. REPLACED PANEL SUPPORT ANGLE PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND FLOOR TRANSITION PANEL LOCATED BETWEEN BS 727G AND BS 787 AT LBL 26. REPLACED TRANSITION PANEL PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO FLOOR INTERCOSTAL LOCATED FROM BS 500G TO BS 500H AT S26L. REPLACED INTERCOSTAL PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME AFT SIDE ATTACH ANGLE STRINGER CLIP LOCATED AT BS 500G AND S26L. REPLACED STRINGER CLIP PER SRM 51-40-02-0G,
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT RIGHT Z CHANNEL LOCATED FROM BS 500B TO BS 500I, AT RBL 21. REPLACED ZEE CHANEL PER SRM 53-00-53 REPAIR 5.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO FLOOR STRUCTURE ZEE CHANNEL LOCATED AT BS 945.5 AND RBL 16.5. REPLACED ZEE CHANNEL PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN STUB FRAME LOCATED FROM BS 277 TO BS 344 AT RBL 60. REPLACED FRAME PER SRM 51-10-02-OG AND SRM 53-10-15-01-2 TABLE 2 FIG 3 ITEM 7.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE SUPPORT BAFFLE LOCATED FROM BS 500E TO BS 500F AT S26L. REPLACED BAFFLE PER SRM 51-40-02-0G AND SRM 51-40-05-0G.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND INNER CHORD LOCATED FROM BS 360 TO BS 270 AT LBL 60. REPLACED CHORD PER SRM 53-10-15-1A AND SRM 51-40-02.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT STRAP TEE ASSEMBLY LOCATED AT BS 887 BETWEEN LBL 14 AND RBL 14. REPLACED TEE ASSEMBLY PER SRM 51-40-02-0G AND SRM 51-40-05-0G.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R1 DOOR LOWER SILL INNER CHORD STRAP LOCATED AT BS 303 AND RBL 60. REPAIRED STRAP PER DWG 141A8316 AND SRM 51-40-02-OG.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN INTERCOSTAL LOCATED AT BS 294.5 AND BL 0. REPLACED INTERCOSTAL PER SRM 53-10-04-1A AND SRM 51-40-02G.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME FORWARD SIDE ATTACH STRINGER CLIP LOCATED AT BS 500G AND S26R. REPLACED STRINGER CLIP PER SRM 51-40-02-OG AND SRM 53-30-53.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME ATTACH STRINGER CLIP LOCATED AT BS 500I AND S26L. REPLACED STRINGER CLIP PER SRM 53-30-53 AND AND 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM UPPER T CHORD LOCATED AT BS 1016 AND RBL 33. REPAIRED T CHORD PER EA 339928 AND SRM 53-70-51-2R-4.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R1 DOOR LOWER SILL INBOARD FLOOR SUPPORT CHORD LOCATED FROM BS 298 TO BS 328 AT LBL 6.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R1 DOOR LOWER SILL INBOARD FLOOR SUPPORT CHORD LOCATED FROM BS 298 TO BS 328 AT LBL 6. REPLACED CHORD PER SRM 53-10-15-1A.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME AFT SIDE ATTACH ANGLE LOCATED AT BS 500H AND RBL 26. REPLACED ATTACH ANGLE PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME ATTACH STRINGER CLIP LOCATED AT BS 500I AND S26R. REPLACED STRINGER CLIP PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME ATTACH STRINGER CLIP LOCATED AT BS 500I AND S26R. REPLACED STRINGER CLIP PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO AFT BULKHEAD LOWER BULKHEAD TO FLOOR SUPPORT LOCATED AT STA 500I LEFT BUTT LINE 21 TO RIGHT BUTT LINE 21 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT AFT BULKHEAD RIGHT HAND ACCESS PANEL LOWER SUPPORT RAIL LOCATED AT BS 500I AND RBL 21. REPLACED RAIL ASSEMBLY PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: LEFT Z CHANNEL LOCATED AT STA 992-1016 AND 33 INCHES LEFT BUTT LINE HAS CORROSION. REMOVED AND REPLACED Z CHANNEL PER SRM 53-70-51-1A.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON WEB LOCATED FROM BS 986.5 TO BS 1016 AT LBL 33. REPAIRED WEB PER SRM 53-70-51-1A.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON INTERCOSTAL LOCATED BETWEEN BS 294.5 AND BS 312, AT LBL 12. REPLACED INTERCOSTAL PER SRM 53-10-51-1A-1.
FORWARD CARGO LEFT ZEE CHANNEL SIDE PLATE CORRODED LEFT BUTT LINE 21 FROM STA 500-500I. REMOVED AND REPLACED SIDE PLATE PER SRM 53-00-53-2R-6.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME FORWARD SIDE ATTACH ANGLE LOCATED AT BS 500H AND S26L. REPLACED ATTACH ANGLE PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME AFT SIDE ATTACH ANGLE LOCATED AT BS 500H AND S26L. REPLACED ATTACH ANGLE PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME FORWARD ATTACH ANGLE HAS CRACKS LOCATED AT STA 500G AND STR 26L. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME AFT SIDE ATTACH ANGLE LOCATED AT BS 500G AND S26R. REPLACED ATTACH ANGLE PER SRM 51-40-02-0G.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER T CHORD LOCATED AT BS 947.5 FROM LBL 27 TO RBL 27. REPAIRED T CHORD PER SRM 53-70-51-2R-5 FIG 206 ALT R2.
AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FLOOR PANEL SUPPORT ANGLE IS CRACKED LOCATED AT STA 540 AND RIGHT BUTT LINE 2. REMOVED AND REPLACED BOEING PART BREAK PER SRM 51-40-02-OG.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME FORWARD SIDE ATTACH ANGLE LOCATED AT BS 500H AND S26R. REPLACED ATTACH ANGLE PER SRM 51-40-02-0G.
AIRCRAFT WAS GROUNDED: GROUND CREW REPORTED SMOKE COMING FROM NUMBER 1 MAIN LANDING GEAR BRAKE. FOUND FLUID LEAKAGE FROM BRAKE ASSEMBLY. REMOVED AND REPLACED #1 BRAKE IAW AMM 32-41-41-401. BRAKE OPS CHECKS NORMAL WITH NO LEAKS NOTED. A/C OK FOR SERVICE.
AIRCRAFT NOT GROUNDED: PILOT REPORTS ON ILS APPROACH A/P A ENGAGED. CAPTURED G/P RWY 9R. APPROX. 2200 FEET PITCHED DOWN 8 DEGREES, THEN PITCHED UP THROUGH GLIDEPATH A/P TURNED OFF, RENGAGED, SAME THING ABOUT 1100 FEET. MAINTENANCE ACCOMPLISHED DFCS BITE AS WELL AS LAND VERIFY TEST IAW AMM 22-11-00. HUD BITE TEST ACCOMPLISHED IAW AMM 34-36-00. NO FAULTS NOTED. AUTOPILOT A AND B CHECKS NORMAL.
AIRCRAFT WAS NOT GROUNDED: 1L DOOR SLIDE STOWED IMPROPERLY. MAINTENANCE RESECURED SLIDE PER AMM 25-66-01.
AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY DOOR SLIDE FELL OUT DOOR WHEN IT WAS OPENED ON ARRIVAL. MAINTENANCE RESECURED L1 DOOR SLIDE PER MCM JOB CARD 25-94-10 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
10 MINUTES AFTER SECURING LEFT PACK IAW BLEED TRIP, QRH PROCEDURE, CABIN ALTITUDE WARNING SOUNDED. EMERGENCY DECLARED, DONNED THEIR OXYGEN MASKS AND DIVERTED FLIGHT, LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED 450 SENSOR PER AMM 36-11-05 AND REPLACED PRECOOLER CONTROL VALVE IAW AMM 36-12-02 AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 71-00-00-00.
AIRCRAFT WAS GROUNDED: 10 MINUTES AFTER SECURING LEFT PACK PER BLEED TRIP, QRH PROCEDURE, CABIN ALTITUDE WARNING SOUNDED. EMERGENCY DECLARED, DONNED THEIR O2 MASKS (NO CABIN O2 MASK DEPLOYED) AND DIVERTED TO MIA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED 450 SENSOR IAW AMM 36-11-05 AND REPLACED PRECOOLER CONTROL VALVE PER AMM 36-12-02 AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 71-00-00.
AIRCRAFT WAS GROUNDED. CLIMBING THRU 15000 LEFT PACK LIGHT ILLUMINATED. PER QUICK RESPONSE HANDBOOK RESET AND LIGHT EXTINGUISHED LIGHT ILLUMINATED SECONDS LATER. FOLLOWED QRH PROCEDURES AGAIN AND LIGHT REMAINED ILLUMINATED. FLIGHT DECK EXTREMELY HOT. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO MIA WITHOUT FURTHER INCIDENT. THE FLIGHT LANDED OVERWEIGHT AND TAXIED TO THE GATE ON ITS OWN POWER. REPLACED TEMPERATURE CONTROL MODULE PER AMM 21-61-15. SEE ALSO SDR AALA201810319030 FOR CABIN TEMPERATURE INDICATOR.
AIRCRAFT WAS GROUNDED. CLIMBING THRU 15000 LEFT PACK LIGHT ILLUMINATED. PER QUICK RESPONSE HANDBOOK RESET AND LIGHT EXTINGUISHED LIGHT ILLUMINATED SECONDS LATER. FOLLOWED QRH PROCEDURES AGAIN AND LIGHT REMAINED ILLUMINATED. FLIGHT DECK EXTREMELY HOT. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO MIA WITHOUT FURTHER INCIDENT. THE FLIGHT LANDED OVERWEIGHT AND TAXIED TO THE GATE ON ITS OWN POWER. REPLACED CABIN TEMPERATURE INDICATOR PER AMM 21-61-15. SEE ALSO SDR AALA201810309020 FOR CONTROL MODULE.
AIRCRAFT WAS GROUNDED. CLIMBING THRU 15000 LEFT PACK LIGHT ILLUMINATED. PER QUICK RESPONSE HANDBOOK RESET AND LIGHT EXTINGUISHED LIGHT ILLUMINATED SECONDS LATER. FOLLOWED QRH PROCEDURES AGAIN AND LIGHT REMAINED ILLUMINATED. FLIGHT DECK EXTREMELY HOT. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO MIA WITHOUT FURTHER INCIDENT. THE FLIGHT LANDED OVERWEIGHT AND TAXIED TO THE GATE ON ITS OWN POWER. STANDBY PACK TEMPERATURE CONT VALVE LEFT HAND FOUND CONDITIONED AIR CHECK VALVE SENSE LINE LOOSE AND LEAKING. REPLACED VALVE SENSE LINE PER AMM 21-00-00. SEE ALSO SDR AALA201810319032 FOR TUBE ASSEMBLY FOR AC PACK.
AIRCRAFT WAS GROUNDED. CLIMBING THRU 15000 LEFT PACK LIGHT ILLUMINATED. PER QUICK RESPONSE HANDBOOK RESET AND LIGHT EXTINGUISHED LIGHT ILLUMINATED SECONDS LATER. FOLLOWED QRH PROCEDURES AGAIN AND LIGHT REMAINED ILLUMINATED. FLIGHT DECK EXTREMELY HOT. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO MIA WITHOUT FURTHER INCIDENT. THE FLIGHT LANDED OVERWEIGHT AND TAXIED TO THE GATE ON ITS OWN POWER. STANDBY PACK TEMPERATURE CONT VALVE LEFT HAND FOUND CONDITIONED AIR CHECK VALVE SENSE LINE LOOSE AND LEAKING. REPLACED TUBE ASSEMBLY FOR LEFT SIDE AIR CONDITIONING PACK PER AMM 21-00-00. SEE ALSO SDR AALA201810319031 FOR VALVE SENSE LINE.
AIRCRAFT WAS NOT GROUNDED. AT CRUISE FL360 "LAV SMOKE" LIGHT ILLUMINATED. "LAVS INTERMITTENTLY OCCUPIED" LIGHT EXTINGUISHED AFTER A MINUTE OR TWO (UNSURE WHICH LAVATORY MOST LIKELY LAVATORY "E"). INSPECTED ALL LAVATORY SMOKE DETECTORS. FOUND DEBRIS AT AFT RIGHT HAND LAVATORY SMOKE DETECTORS TEST BUTTON. REMOVED THE DEBRIS FROM TEST BUTTON. OPERATIONS CHECKED NORMAL. ALL SMOKE DETECTORS TESTED NORMAL PER AMM 26-14-00.
CORROSION ON THE RIGHT MAIN LANDING GEAR FORWARD TRUNNION FITTING ON THE WING LOWER OUTBOARD HOLE BORE. REPLACED THE TRUNNION FITTING IAW 51-00-05.
FORWARD GALLEY RIGHT EMERGENCY LIGHT POWER SUPPLY FAILED A FUNCTIONAL CHECK. REPLACED THE POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED GOOD.
FORWARD ENTRY DOOR EMERGENCY LIGHT WAS INOPERATIVE. FOUND THE ELECTRICAL CONNECTOR DISCONNECTED. CONNECTED THE CONNECTOR, OPS CHECKED NORMAL IAW AMM 33-51-04.
EMERGENCY EXIT LIGHT ASSEMBLY LENS AT SEAT 14DEF AT LOWER FORWARD CORNER OVER WING EXIT DOOR BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IAW AMM 33-51-04.
EMERGENCY EXIT LIGHT ASSEMBLY LENS BROKEN AT FORWARD GALLEY NEXT TO R1 DOOR. REPLACED THE EXIT LIGHT ASSEMBLY IAW AMM 33-51-01.
EMERGENCY LIGHT ASSEMBLY AND LENS BROKEN AT SEAT ROW 14 DEF. REPLACED THE LIGHT ASSEMBLY AND LENS IAW AMM 33-51-04.
EMERGENCY LIGHT ASSEMBLY AND LENS BROKEN IN THE AFT GALLEY. REPLACED LIGHT ASSEMBLY IAW AMM 33-51-01.
EMERGENCY LIGHT ASSEMBLY AND LENS BROKEN IN THE AFT GALLEY. REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51-01.
THE AIRCRAFT WAS GROUNDED. 45 MINS INTO FLIGHT, A FUEL IMBALANCE LIGHT ILLUMINATED. AIRCRAFT INDICATED 2000LBS UNDER THE PLANNED FUEL. FUEL LEAK SUSPECTED , THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DFW WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED LEFT TANK COMPENSATOR, OPS CK GOOD PER AMM 28-41-21-400-810.
AIRCRAFT WAS NOT GROUNDED. L1 DOOR EMERGENCY EVACUATION SLIDE IS OUT OF POSITION. RE-ESTABLISHED Z FOLD ON SLIDE GIRT IAW AMM 25-66-01. OPERATIONAL CHECK GOOD.
EMERGENCY DECLARED. LANDING UNEVENTFUL. DURING APPROACH THE TRAILING EDGE FLAPS WOULD NOT EXTEND BEYON 25. DURING GO AROUND FLAPS WOULD NOT RETRACT. DIVERTED TO IAD. REMOVED AND REPLACED NR 1 FSEU IAW AMM 27-51-01 AND LEFT FLAP POSITION TRANSMITTER IAW AMM 27-58-01. OPERATIONAL CHECK NORMAL. AIRCRAFT WAS GROUNDED.
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. LANDING UNEVENTFUL. DURING APPROACH THE TRAILING EDGE FLAPS WOULD NOT EXTEND BEYON 25. DURING GO AROUND FLAPS WOULD NOT RETRACT. DIVERTED TO IAD. REMOVED AND REPLACED NR 1 FSEU IAW AMM 27-51-01 AND LEFT FLAP POSITION TRANSMITTER IAW AMM 27-58-01. OPERATIONAL CHECK NORMAL.
DURING CRUISE A BURNING TYPE ODOR WAS REPORTED THROUGHOUT THE FLIGHT DECK AND MAIN CABIN. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED FIM 21-00-00-810-806 AND VERIFIED OIL ODOR FROM NR 2 ENGINE BLEED AIR. FOUND OIL LEAKING FROM NR 2 ENGINE FUEL PUMP DRAIN PAD. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP DRIVE PAS SEALS IAW AMM 73-11-01 AND 72-60-00. LEAK AND OPS CHECKED GOOD.
VERTICAL PRESSURE WEB AT BS 663.75 IS CRACKED AT APPROXIMATELY RBL 42. REPAIRED THE BULKHEAD WEB IAW SRM 57-1010-2R-3.
AFT CARGO DOOR INTERIOR SKIN IS CRACKED AT THE LOWER, THIRD FROM FORWARD, LIGHTENING HOLE. REPAIRED THE CARGO DOOR SKIN IAW EA 262635.
L1 WINDOW POST IS CRACKED. ACCOMPLISHED DOUBLER REPAIR IAW AARD & SB 737-53-1336.
LEFT HORIZONTAL REAR SPAR UPPER CAP CORRODED. INSTALLED DOUBLER REPAIR IAW EA B737-55-035808.
EXTERNAL DOUBLER FROM STATION 351 TO 360 & STRINGERS 17 TO 19 RT REQUIRED REPLACEMENT. REPLACED DOUBLER IAW EA B737-53-035659.
AFT CARGO FLOORBOARD SPLICE AT STATION 787 CORRODED. R & R FLOORBOARD SPLICE IAW AARD 51-00-05-1.
AFT CARGO FLOORBOARD SPLICE AT STATION 887 CORRODED. R & R FLOORBOARD SPLICE IAW AARD 51-00-05-1.
ESCAPE PATH LIGHT AT ROW 30 INOPERATIVE. REPLACED LAMP FOR ESCAPE PATH LIGHT AT ROW 30. OPERATIONS CHECKED NORMAL.
ESCAPE PATH LIGHT AT ROW 18 INOPERATIVE. REPLACED LAMP FOR ESCAPE PATH LIGHT AT ROW 18. OPERATIONS CHECKED NORMAL.
FORWARD CARGO HOLE IN FLOORBOARD TRANSITION AT STRINGER 25 RT FROM STATION 500A. INSTALLED NEW TRANSITION PANEL IAW AARD 51-00-05-1 & SRM 51-20-01-0G.
CORROSION ON LOWER CTR WING SKIN AT STATION 540 & STRINGER 22 LT AT DRAG ANGLE. REMOVED CORROSION FROM LOWER CTR WING SKIN DRAG ANGLE IAW SRM 51-10-02-0G. FABRICATED FILLER SHIM & ALODINE TREATED & PAINTED.
CORROSION FOUND ON CARGO FLOOR SUPPORT STRINGER & TRACK. REMOVED CORRODED PORTION & SPLICED IN NEW PORTION IAW AARD 51-00-05-1.
MULTIPLE AREAS OF CORROSION AT AFT CARGO RT TRANSITION PANELS FROM STATIONS 727 TO 767. REMOVED CORRODED SECTION & SPLICED IN NEW SECTION IAW SRM 53-00-53-2R 6.
CORROSION ON CREASE ANGLE AT RT NR DOOR. REPLACED CREASE ANGLE IAW AARD 51-00-05-1.
MULTIPLE CARGO FLOOR SUPPORTS CORRODED AT STATION 772 AT TRANSITION STRIP. INSTALLED REPAIR DOUBLERS & STRAPS IAW EA.
WALL SUPPORT AT STATION 992 CORRODED. REPLACED WALL SUPPORT IAW AARD 51-00-05.
CORROSION ON LOWER FILLER FOR AUXILIARY POWER UNIT INLET AT STATION 1088. ACCOMPLISHED FILLER REPAIR IAW AARD 51-10-05 & DWG 148A0924.
CORROSION ON HORIZONTAL STIFFENER ON AFT SIDE OF 1088 BULKHEAD. INSTALLED NEW STIFFENER IAW DWG 148A2410, 148A0924 & AARD 51-10-05-1.
CORROSION ON FLOORBEAM AT STATION 947 & RBL 27 T CAP. ACCOMPLISHED SPLICE REPAIR IAW SRM 53-70-51-2R-5.
LEFT LAP SPLICE DENTED AT STATION 933 & STRINGER 23 LT. INSTALLED DOUBLER IAW SRM 53-00-01-2R-12.
CORROSION ON VERTICAL ANGLE AT AFT SIDE AUXILIARY POWER UNIT INLET CUT OUT AT STATION 1126. INSTALLED NEW ANGLE STIFFENER IAW AARD 51-10-05-1 REPAIR 1 & DWG 148A8650.
ONE INCH CRACK IN LT HAND HORIZONTAL STABILIZER LOWER IN SPAR SKIN 18 INCHES AFT OF FRONT SPAR AT STATION 129.50. INSTALLED EXTERNAL DOUBLER IAW SRM 55-10-01-2R-11.
MIA FLIGHT ATTENDANT REPORTED LT NR 1 DOOR HANDLE HAD POPPED OUT OF STOW POSITION WITH NOTICEABLE AIR LEAK. NO COCKPIT INDICATION OF OPEN DOOR. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. MX FOUND OUTER DOOR HANDLE IN VERTICAL OPEN POSITION. REPLACED LT NR 1 DOOR HANDLE SPRING. SYS GND CHECKED NORMAL OPERATION CLOSED.
FOUND MULTIPLE EMERGENCY LIGHT SEGMENTS INOPERATIVE. REPLACED BATTERY PACK M1671. OPERATIONS CHECKED NORMAL.
FOUND MULTIPLE EMERGENCY LIGHT SEGMENTS INOPERATIVE. REPLACED BATTERY PACK M1672. OPERATIONS CHECKED NORMAL.
FOUND MULTIPLE EMERGENCY LIGHT SEGMENTS INOPERATIVE. REPLACED BATTERY PACK M1695. OPERATIONS CHECKED NORMAL.
RT SEAT TRACK AT STATION 727B, RBL 45.50, INBD FLANGE SHOWS CRACK INDICATIONS AT BOTH FASTENER HOLES. INSTALLED NEW SPLICE & ANGLE IAW ECO J1707AB CARD NR 3 & EA.
LT SEAT TRACK AT STATION 727B, LBL 45.50, INBD FLANGE SHOWS CRACK INDICATIONS AT BOTH FASTENER HOLES. INSTALLED NEW SPLICE & ANGLE IAW ECO J1707AB CARD NR 3 & EA.
LT SEAT TRACK AT STATION 727B, LBL 24.75, INBD FLANGE SHOWS CRACK INDICATIONS AT BOTH FASTENER HOLES. INSTALLED NEW SPLICE & ANGLE IAW ECO J1707AB CARD NR 3 & EA.
RT SEAT TRACK AT STATION 727B, RBL 45.50, OTBD FLANGE SHOWS CRACK INDICATIONS AT BOTH FASTENER HOLES. INSTALLED NEW SPLICE & ANGLE IAW ECO J1707AB CARD NR 3 & EA.
LT SEAT TRACK AT STATION 727B, LBL 45.50, OTBD FLANGE SHOWS CRACK INDICATIONS AT BOTH FASTENER HOLES. INSTALLED NEW SPLICE & ANGLE IAW ECO J1707AB CARD NR 3 & EA.
LT SEAT TRACK AT STATION 727B, LBL 24.75, OTBD FLANGE SHOWS CRACK INDICATIONS AT BOTH FASTENER HOLES. INSTALLED NEW SPLICE & ANGLE IAW ECO J1707AB CARD NR 3 & EA.
RT SEAT TRACK AT STATION 727B, RBL 24.75, INBD FLANGE SHOWS CRACK INDICATIONS AT BOTH FASTENER HOLES. INSTALLED NEW SPLICE & ANGLE IAW ECO J1707AB CARD NR 3 & EA.
RT SEAT TRACK AT STATION 727B, RBL 24.75, OTBD FLANGE SHOWS CRACK INDICATIONS AT BOTH FASTENER HOLES. INSTALLED NEW SPLICE & ANGLE IAW ECO J1707AB CARD NR 3 & EA.
CREW REPORTED SPARKS AND SMOKE COMING FROM BOTH SIDES OF ATC CONTROL PANEL. TURNED OFF AND SMOKE AND SPARKS IMMEDIATELY CEASED. F/O NAVIGATION AND AUDIO CONTROL PANEL LIGHTS BECAME INOPERATIVE. FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED ATC CONTROL PANEL INOPERATIVE. SYS GROUND CHECK NORMAL OPERATION.
MIA - CREW REPORTED "LE FLAPS TRANSIT" LIGHT STAYED ILLUMINATED ON CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 SLAT ACUATOR AS A PRECAUTION.
LEFT NUMBER 1 DOOR EXIT INDICATOR LIGHT NEXT TO FLIGHT ATTENDANT JUMPSEAT AND LEFT NUMBER 1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK M1675. OPS CHECK NORMAL.
INTERCOSTAL HAS CORROSION ON OUTBOARD SIDE LEFT HAND FOR AFT LAVATORY MOUNT. REPLACEMENT INTERCOSTAL INSTALLED SRM 51-10-02-OG
FORWARD CARGO DOOR HAS SKIN DAMAGE AND OLD DOUBLER INSTALLED OVER PAST DAMAGES. REMOVED THE DAMAGED DOOR SKIN AND REPLACED WITH NEW DOOR SKIN ON THE FORWARD CARGO DOOR AS PER ESO 60654.
HOLE IN LOWER FUSELAGE AT STATION 727E TO 727F BETWEEN STRINGERS 27 LEFT AND 27 RIGHT AT BUTTLINE 0. INSTALLED FLUSH REPAIR PER SRM 53-00-01-2R FIGURE 201.
3 EACH SCRATCHES WITH DENTS IN FUSELAGE SKIN AT STATION 321 AND STRINGER 3 LEFT. INSTALLED REPAIR PER SRM 53-00-01-2R REPAIR 1.
LEFT INBOARD INTERCOSTAL HAS CORROSION NEAR FLOOR MOUNTS. INTERCOSTAL INSTALLED PER SRM 51-10-02-OG.
RIGHT OVERWING HATCH LOWER EXIT MARKER MISSING LENS. REPLACED LENS FOR RIGHT OVERWING HATCH LOWER EXIT MARKER, OPS CHECKS NORMAL.
INFLIGHT MIA TO IAH. CREW REPORTED EQUIPMENT COOLING EXHAUST INDICATION ON DURING FLIGHT. LANDED TPA WITHOUT INCIDENT. RE-INSTALLED EQUIPMENT COOLING SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION.
MIA - CREW REPORTED VIBRATION IN FLIGHT. EMERGENCY DECLARED, RETURNED MIA WITHOUT INCIDENT. UPON ARRIVAL FOUND ELECTRICAL GROUND POWER RECEPTACLE DOOR OPEN. INSPECTED AND CLOSED DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY LIGHT AT SEAT 20D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20D.
DFW - EMERGENCY LIGHT AT SEAT 20D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 20D.
DFW - EMERGENCY LIGHT AT SEAT 20D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20D.
MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 20C INOPERATIVE. REPLACED LAMP AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPERATION.
LGA - EMERGENCY LIGHT EXIT SIGN AT AFT GALLEY DOOR CRACKED. REPLACED EXIT LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
LAX INFLIGHT T437/24APR DFW TO SNA - CREW REPORTED AMBER LEADING EDGE FLAP INDICATION WITH AMBER NUMBER THREE SLATS TRANSIT LIGHT. FLIGHT DIVERTED TO LAX. LANDED WITHOUT INCIDENT. REPLACED SLAT NUMBER THREE INBOARD PROXIMITY SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY LIGHT AT FORWARD EXIT OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD EXIT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY LIGHT AT SEAT 7D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.
TUL - EMERGENCY LIGHTS AT AFT RIGHT COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT RIGHT COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
TUL - EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
MIA - EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT NUMBER TWO DOOR AFT BULKHEAD MISSING. REPLACED EMERGENCY LIGHT ASSEMBLY AT RIGHT NUMBER TWO DOOR AFT BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.
SKB - LEFT NUMBER ONE DOOR SLIDE UNSUCCESSFULLY DEPLOYED. REPACKED SLIDE AND REINSTALLED SLIDE TO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
TUL - EMERGENCY RIGHT AFT SERVICE DOOR SLIDE DID NOT DEPLOY AUTOMATICALLY WHEN DOOR WAS OPENED DURING CHECK. DID DEPLOY MANUALLY. REPLACED EMERGENCY RIGHT HAND AFT SERVICE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.
TUL - BATTERY PACK FOR CABIN EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT M1671 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
TUL - RIGHT HAND EMERGENCY EXIT LIGHT BATTERY PACK FAILED 15 MINUTE TEST PER CARD 2311. REPLACED BATTERY PACK FOR RIGHT HAND EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
BOS - SEAT MOUNTED EMERGENCY LIGHTS FROM 7D THROUGH 11D INOPERATIVE. REPLACED FLOOR MOUNTED BATTERY PACK FORWARD OF SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION.
MIA T651/24 EN ROUTE MIA-BGI 30 KNOT AIRSPEED SPLIT NOTICED ON TAKEOFF ROLL. CAPTAINS AIRSPEED INDICATED 60 KNOTS AND FIRST OFFICERS AIRSPEED INDICATED 90 KNOTS. REPLACED CAPTAINS PITOT TUBE. SYSTEM GROUND CHECKED NORMAL OPERATION.
TECHNICIAN OBSERVED EMERGENCY ESCAPE SLIDE FAILED TO DEPLOY PROPERLY. SLIDE WAS TIED IN A KNOT AFTER INFLATION. BOTTLE PRESSURE WAS GOOD, EVERYTHING ELSE APPEARED TO BE NORMAL. REPLACED SLIDE PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
ENROUTE MIA-PHL, AFTER TAKEOFF, NR 1 ENGINE OIL QUANTITY DROPPED RAPIDLY TO THREE QUARTS AND NR 2 ENGINE OIL QUANTITY DROPPED TO 6 QUARTS. POWER WAS REDUCED AND QUANTITIES REMAINED AT 5 QUARTS AND 8 RESPECTIVELY. EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO MIA WITHOUT FURTHER INCIDENT. CHECKED ENGINE OIL QUANTITY FOR BOTH ENGINES. LT ENGINE READS ELEVEN AND RT ENGINE READS THIRTEEN. SERVICED BOTH ENGINES. CHECKED BOTH ENGINES FOR LEAKS AND FOUND NONE. CLEANED BOTH ENGINE OIL QUANTITY TRANSMITTER CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
EN ROUTE AT 37,000 FT, THE L2 WINDOW CRACKED AND SPARKED UNTIL WINDOW HEAT WAS TURNED OFF. RETURNED AND LANDED DFW WITHOUT INCIDENT. INSTALLED L2 WINDOW ASSEMBLY AND RIGGED FOR PROPER FIT AND CLOSURE. INSTALLED NEW WINDOW HEAT CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
TUL - LIGHTNING STRIKE NR 4 LEFT CABIN WINDOW FRAME. INSTALLED NEW WINDOW FRAME PER SRM 51-10-02-0. (X)
TUL - LIGHTNING STRIKE NR 10 LT WINDOW FRAME. INSTALLED NEW WINDOW FRAME PER SRM 51-10-02-0. (X)
TUL - LIGHTNING STRIKE NR 9 LEFT CABIN WINDOW. INSTALLED NEW WINDOW FRAME PER SRM 51-10-02-0. (X)