N938UW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| American Airlines | Operator | 2018-12-31 – 2018-12-31 | Operator named in NTSB report |
| AMERICAN AIRLINES, INC. (AALA) | Operator | 2018-12-31 – 2018-12-31 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AIRCRAFT WAS NOT GROUNDED: L2 DOOR EMERGENCY SLIDE PRESSURE LOW. MAINTENANCE REPLACED DOOR SLIDE PER AMM 25-66-00.
AIRCRAFT WAS GROUNDED: CABIN PRESS LOST AT 37,000 FT EMERGENCY DECLARED. DIVERT TO HNLCABIN CLIMBED TO 10,000 DIFF PRES 7 MAX DOWN RATE. OUTFLOW VALVE, CABIN PRESSURE SELECTOR PANEL AND AUTO 1 CABIN PRESSURE CONTROLLER REPLACED. ACCOMPLISHED WORK CARD 19L21021001.
AIRCRAFT WAS GROUNDED: CABIN PRESS LOST AT 37,000 FT EMERGENCY DECLARED. DIVERT TO HNL. CABIN CLIMBED TO 10,000 DIFF PRES 7 MAX DOWN RATE. OUTFLOW VALVE, CABIN PRESSURE SELECTOR PANEL AND AUTO 1 CABIN PRESSURE CONTROLLER REPLACED. ACCOMPLISHED WORK CARD 19L21021001.
AIRCRAFT WAS GROUNDED: CABIN PRESS LOST AT 37,000 FT EMERGENCY DECLARED. DIVERT TO HNL CABIN CLIMBED TO 10,000 DIFF PRES 7 MAX DOWN RATE. OUTFLOW VALVE, CABIN PRESSURE SELECTOR PANEL AND AUTO 1 CABIN PRESSURE CONTROLLER REPLACED. ACCOMPLISHED WORK CARD 19L21021001.
AIRCRAFT WAS GROUNDED: NOSE LANDING GEAR LOWER TORSION LINK WORN AND HAS EXCESSIVE PLAY. REPLACED TORSION LINK PER AMM 32-21-09.
AIRCRAFT WAS GROUNDED: NOSE LANDING GEAR RIGHT HAND TORSION LINK APEX PIN WORN AND HAS EXCESSIVE PLAY. REPLACED APEX PIN PER AMM 32-21-09.
AIRCRAFT WAS GROUNDED: NOSE LANDING GEAR UPPER TORSION LINK WORN AND HAS EXCESSIVE PLAY. REPLACED TORSION LINK PER AMM 32-21-09.
AIRCRAFT WAS GROUNDED: MID F/A REPORTED A STRONG ELECTRICAL SMELL IN THE CABIN."R RECIRC" UPPER EICAS MESSAGE ILLUMINATED AND INOP ANNUNCIATORON R RECIRC SWITCH ILLUMINATED. REMOVED AND REPLACED CABIN AIR RECIRC FAN AND FILTER ASSY IAW AMM 21-25-01 AND 21-25-02.
AIRCRAFT WAS NOT GROUNDED: SLIDE LIGHT DISAGREES WITH DOOR SLIDE ARM. MAINTENANCE FOUND R4 LIGHT SOCKET NOT SEATED AND REINSTALLED LIGHT SOCKET AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT NOT GROUNDED: EMERGENCY PATH SAT-T-GLO STRIP INOP FROM R1 DOOR TO R2 DOOR. REPLACED EMERGENCY PATH SAT-T-GLO FROM R1 DOOR TO R2 DOOR REF DWG #19P33D1256.
AIRCRAFT WAS GROUNDED: PILOT REPORTS 2L GUST LOCK EXTREMELY STICKY. MAINTENANCE REPLACED HOLD-OPEN LOCK COLLAR ON 2L DOOR IAW AMM 52-11-08. OPS CHECK GOOD.
AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF LEFT ENGINE BLEED FAULT INDICATION. FLIGHT LANDED OVERWEIGHT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED PRSOV IAW AMM 36-11-09, WHILE TROUBLESHOOTING BLEED ISSUE FOUND FWD DUCT OF PRSOV DAMAGED AND LEAKING, REMOVED AND REPLACED FLEX JOINT DUCT ASSEMBLY IAW AMM 36-11-01. NEW JOINT DUCT ASSEMBLY WAS NOT COMPLETE ORDERED NEW PARTS FOR ASSEMBLY AND INSTALLED PRESSURE TAP ASSEMBLY IAW AMM 36-11-01. REMOVED AND REPLACED PNEUMATIC OVERTEMP LIMITING SENSOR IAW AMM 36-11-13-004. PERFORMED IDLE LEAK CHECK- NO LEAKS. PERFORMED TAKE OFF POWER TEST #13, NO FAULTS AT THIS TIME. PERFORMED TAKE OFF POWER WITH BLEEDS ON AND NO FAULTS.
AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF PRESSURIZATION ISSUE. LEFT ENGINE BLEED FAILURE AFTER RH BLEED ON MEL. MAINTENANCE REPLACED FAN AIR VALVE IAW AMM 36-11-16-404-096-001. OPS AND LEAK CHECK GOOD.
CORROSION WAS FOUND ON THE TRANSITION PANEL, BS 1480 - 1520, LBL 16 IN THE AFT CARGO BAY. REPAIRED THE TRANSITION PANEL IAW SRM 53-00-53-2R-2, 51-40-02, & 51-20-10.
DELAMINATED PANEL 611BB AT THE CORNER. REPAIRED THE PANEL IAW SRM 57-41-01AND B757 SRM 51-70-03.
R4 DOOR SLIDE BOTTLE PRESSURE WAS LOW. REPLACED THE SLIDE IAW JC 19L80025002.
AIRCRAFT WAS NOT GROUNDED: R4 DOOR SLIDE PRESSURE LOW. MAINTENANCE REPLACED R4 DOOR SLIDE/RAFT PER JOB CARD 19L80025002 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
THE AIRCRAFT WAS NOT GROUNDED. PHOTOLUMINESCENT TEST COUPON FAILED. DUE TO REPORT TO ENGINEERING THAT THE PHOTOLUMINESCENT TEST COUPON HAS FAILED ACCOMPLISH LIGHT PATH REPAIRS PER EA 280866. REPLACED FIRST CLASS RIGHT SIDE STRIPS AND BUSINESS CLASS RIGHT SIDE STRIPS TO R2 DOOR PER EA 280866. ALL PATH LIGHTING OPERATIONS CHECK GOOD.
AIRCRAFT WAS GROUNDED. DOOR L4 WINDOW PRISM CRACKED. REPLACED DOOR L4 WINDOW PRISM PER AMM 56-31-02.
AIRCRAFT IN BASE MAINTENANCE. RIGHT HAND PYLON STRUT HAS CRACK INDICATIONS AT THE INBOARD THRUST REVERSER AFT MOUNT BOTH UPPER AND LOWER FASTENER HOLES. REPAIRED RIGHT HAND PYLON STRUT PER EA 278784.
AIRCRAFT WAS NOT GROUNDED. ELECTRICAL ODOR IN BOTH THE COCKPIT AND CABIN DURING CRUISE. TURNED OFF THE ENTERTAINMENT SYSTEM AND LEFT RECIRCULATION FAN AND ODOR WENT AWAY. REMOVED AND REPLACED BURNED OUT #1 FORWARD EQUIPMENT COOLING SUPPLY FAN PER AMM 21-58-06. OPERATIONAL CHECK GOOD.
R1 DOOR WILL NOT ARM. REINSTALLED GIRT BAR IAW AMM 52-11-00-862-007. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS GROUNDED. R2 DOOR EMERGENCY EVACUATION SLIDE RESERVOIR PRESSURE IS LOW. REMOVED AND REPLACED SLIDE ASSEMBLY. OPS CHECKED GOOD.
R1 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR IS DISLODGED AND FOOT REMOVED. FOUND GIRT BAR SPRINGS FLAT ON ONE END. REMOVED AND REPLACED GIRT BAR. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.
AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHTS SWITCH GUARD TURNS SWITCH TO OFF POSITION WHEN IT IS DOWN. ADJUSTED GUARD. OPS CHECKED GOOD.
AIRCRAFT WAS NOT GROUNDED. R4 DOOR EMERGENCY EVACUATION SLIDE RESERVOIR PRESSURE IS LOW. REMOVED AND REPLACED SLIDE/RAFT IAW JOB CARD 19L80025002. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED. CORROSION ON AFT CARGO PIT INTERCOSTAL, LOWER FORWARD CORNER, AT FUSELAGE STATION 1620, S29R. REPAIRED INTERCOSTAL IAW SRM 51-70-11-0G AND SRM 51-40-02.
RIGHT EMERGENCY EXIT DOOR ESCAPE SLIDE, AFT RELEASE CABLE PIN, SAFETY STRING BROKEN. REPLACED THE PIN BREAKAWAY TIE IAW CMM 25-61-28.
CORROSION ON FUSELAGE SKIN UNDER AFT DRAIN MAST BETWEEN STRINGERS 25 - 26R. REPAIRED THE SKIN IAW SRM 53-00-01 AND SRM 51-40-02.
THE R1 DOOR SLIDE LIGHT FOUND INOPERATIVE. MAINTENANCE FOUND AND REMOVED A SMALL ALCOHOL BOTTLE STUCK UNDER THE GIRT BAR AND ACCOMPLISHED SATISFACTORY OPS CHECK.
SETTING TAKEOFF POWER WE GOT SPOILERS CAUTION AND CONFIGURATION WARNING WITH HORN. ABORTED TAKEOFF, WENT TO RUNUP AREA AND GOT THE SAME SYMPTONS WHEN THRUST IS ABOVE 1.5 EPR. AIRCRAFT WAS GROUNDED. MAINTENANCE FIXED A BROKEN WIRE AT TBL190 FOR SPOILER HANDLE SWITCH S493 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 31-51-00.
SEVERAL GROUND CREW MEMBERS OBSERVED SPARKS COMING OUT OF APU EXHAUST. AIRCRAFT WAS GROUNDED. REPLACED APU.
R1 DOOR SLIDE BELOW MINIMUM PRESSURE REQUIREMENTS. REPLACED DOOR R1 EVACUATION SLIDE.
NLG EMERGENCY EXTERIOR LIGHT TEST SWITCH INOP FOR L3 AND R3 DOORS. FLIGHT DECK AND FAP TEST CORRECTLY. REMOVED AND REPLACED CONN D40488P IAW STANDARD WIRING PRACTICES 20-60-03. OP'S CK'S GOOD. THE AIRCRAFT WAS NOT GROUNDED.
AIRCRAFT WAS NOT GROUNDED: 1R DOOR WOULD NOT ARM. FOUND DEBRIS INTERFERING WITH THE 1R GIRT BAR REMOVED DEBRIS AT 1R TRACK AND PERFORMED OPERATIONAL CHECK PER AMM 52-11-00-201 ARMED WITH NO ISSUES.
AIRCRAFT WAS GROUNDED. DOOR R4 SLIDE PRESSURE BOTTLE BELOW LIMITS. REPLACED R4 DOOR SLIDE RAFT ASSEMBLY PER JOB CARD 19L80025002.
GATE AGENT INFORMED MTC L2 DOOR GUST LOCK INOPERATIVE. REMOVED AND REPLACED L2 DOOR LOCK COLLAR IAW AMM 52-11-08-358-001. OPS CK GOOD. THE AIRCRAFT WAS GROUNDED.
FLIGHT ATTENDANT`S FLASHLIGHT WAS FOUND INOPERATIVE AT POSITION 4L. REPLACED THE BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: DOOR 1R SLIDE LIGHT DOES NOT LIGHT UP WHEN DOOR IS ARMED. REMOVED OBSTRUCTION FROM GIRT BAR.
AIRCRAFT WAS GROUNDED: LEFT AFT SERVICE DOOR INDICATOR LIGHT EICAS SHOWED OPEN.HANDLE INSIDE DRIFTS UP POSITION.LIGHT OUT WHILE WEIGHT IS APPLIED TO HANDLE.UNEVENTFUL.MAINTENANCE FOUND STOP PINS OUT OF ADJUSTMENT AND PROPERLY ADJUSTED THE STOP PINS. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
WHILE AT CRUISE, THE FLIGHT CREW REPORTED AN ACRID ODOR THROUGH OUT CABIN THAT LASTED ABOUT 5 MINUTES. FLIGHT ATTENDANT REPORTED THAT THE OVERHEAD MONITOR SMOKED WHICH RESULTED IN THE CREW TURNING OFF THE VIDEO. THE ODOR DISSIPATED. AIRCRAFT GROUNDED. MAINTENANCE REPLACED THE MONITORS AT ROW 9 AND 15 IAW AMM 23-32-00-800-802.
R1 DOOR COVER OFF AND SLIDE WOULD NOT DISARM. AIRCRAFT GROUNDED. MAINTENANCE FOUND THE AFT LEAF SPRING BINDING, STRAGHTENED SPRING AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 25-66-01. MAINTENANCE INSTALLED SLIDE COVER.
DOOR 1 RT UNABLE TO ARM. FOUND SLIDE STRAP UNDER THE GIRT BAR. STRAP WAS ADJUSTED AND A SATISFACTORY OPS CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS NOT GROUNDED: R1 DOOR GIRT BAR APPEARS LOOSE. REATTACHED R1 DOOR GIRT BAR IN THE DOOR FITTINGS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 25-66-10-201.
AIRCRAFT WAS GNDED. LT WING NR 5 SLAT HAS AREA OF DISBOND 4" FROM THE UPPER INBD EDGE. REPLACED SLAT IAW AMM 27-81-01 & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GNDED. DOOR 1L SLIDE LIGHT MISSING. INSTALLED MISSING DOOR SLIDE LENS AT THE 1L DOOR.
AIRCRAFT WAS NOT GNDED. R4 DOOR SLIDE LIGHT INOPERATIVE. INSTALLED GIRT BAR SLIDER PROXIMITY TARGET, ACTUATOR, IAW AMM TR 25-017AW. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GNDED. LENS COVER MISSING ON SLIDE ARMED INDICATOR AT DOOR 1L. REPLACED L1 SLIDE ARMED INDICATOR LIGHT LENS, OPERATIONAL CHECKED GOOD.
AIRCRAFT WAS NOT GNDED. WHEN 1R DOOR IS OPEN A LANYARD HANGS BELOW SLIDE. REPOSITIONED SLIDE LANYARD & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
NUMBER 2 ENG FAILED & SHUTDOWN ON TAKEOFF ROLL. STATUS MSG RT ENG LOW PRESS PUMP. REPLACED THE RT ENGINE FUEL FLOW GOVERNOR & HIGH PRESS FUEL PUMP. ACCOMPLISHED SATISFACTORY LEAK & OPERATIONAL CHECKS. SEE AALA201511109028 FOR ADDITIONAL PART INFORMATION.
NUMBER 2 ENG FAILED & SHUTDOWN ON TAKEOFF ROLL. STATUS MSG, RT ENG LOW PRESS PUMP. REPLACED THE RT ENG FUEL FLOW GOVERNOR & HIGH PRESS FUEL PUMP. ACCOMPLISHED SATISFACTORY LEAK & OPERATIONAL CHECKS. SEE AALA201511109005 FOR ADDITIONAL PART INFORMATION.
R1 DOOR, FITTING CAME OFF GIRT BAR. RE-INSTALLED GIRT BAR FITTING. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 26-66-10-202-039.
1R DOOR DOES NOT ARM & DISARM PROPERLY. REMOVED DEBRIS & CLEANED GIRT BAR. DOOR ARM OPERATION TESTED SATISFACTORY.
DOOR 1R WILL NOT CLOSE & CANNOT ARM. REMOVED DEBRIS FROM FLOOR & GIRT BAR RETAINER. NO FURTHER DEFECTS NOTED AMM 52-11-00-862-077.
FLIGHT 837 EN-ROUTE, ALL CREW NOTICED STRONG ODOR ESPECIALLY IN COCKPIT & NEAR 2L DOOR. FLIGHT ATTENDANT DISABLED INFLIGHT ENTERTAINMENT & SMELL DISSIPATED. COMPLIED WITH JC 19L00021001. R & R RT CABIN RECIRCULATION FAN IAW AMM 21-25-01-404-094 & 21-25-01-004-092. OPERATIONS CHECKED GOOD, NO ODOR NOTED.
TOWER FOREMAN REPORTED R1 DOOR HAS SOMETHING HANGING. SECURED BUSTLE STRAP WHEN R1 SLIDE WAS REPLACED. OK FOR SERVICE.
C1 CHECK, CORROSION ON FORWARD CARGO LEFT SIDE PANEL BETWEEN STATION 510 & 645 AT LBL 22. REPAIRED SIDE PANEL IAW SRM 53-00-53-2R-2.
C1 CHECK, CORROSION ON FORWARD CARGO LEFT SIDE PANEL BETWEEN STATION 645 & 705 AT LBL 22. REPAIRED SIDE PANEL IAW SRM 53-00-53-2R-2.
C1 CHECK, CORROSION ON SIDE PANEL BETWEEN STATION 620 & 645 AT RBL 22. REPLACED SIDE PANEL IAW SRM 53-00-53-1A-1 FIG 101 DET 1 51-40-02.
C1 CHECK, CORROSION ON FLOOR SUPPORT ANGLE AT STATION 845 BETWEEN LBL 25 & RBL 25. REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-10-02 & 51-40-02.
C1 CHECK, CORROSION ON SIDE PANEL BETWEEN STATION 645 & 705, RBL 19 & RBL 26. REPLACED SIDE PANEL IAW SRM 51-40-02.
C1 CHECK, CORROSION ON STRINGER SPLICE AT STATION 630 & RBL 7.55. REPLACED STRINGER SPLICE IAW SRM 51-40-02.
C1 CHECK, CORROSION ON FLOOR STRINGER BETWEEN STATION 640 & 660 AT RBL 2.9. REPLACED FLOOR STRINGER IAW SRM 51-40-02.
R1 DOOR FWD GIRT BAR SLIDER ASSEMBLY HAS EXCESSIVE PLAY. REPLACED BUSHING ON R1 DOOR FWD GIRT BAR SLIDER ASSEMBLY IAW SOPM 20-50-03.
FLASHLIGHT BATTERY AT L1 DOOR ATTENDANT SEAT REQUIRES REPLACEMENT. R & R FLASHLIGHT BATTERY IAW AMM 25-64-00-902-037.
C1 CHECK, R1 DOOR ASSIST BOTTLE CABLE TRAVEL TO SHORT, FAILED TEST. ADJUSTED CABLES TRAVEL IAW AMM 52-11-32-404. OPERATIONS CHECKED GOOD .940 TRAVEL.
DOOR R1 SLIDE BAR LOCK CAME OFF. REINSTALLED BAR LOCK. DOOR ARMS & DISARMS NORMAL. UPON FURTHER REVIEW, MX CONTROL REQUESTED FURTHER INSPECTION. COMPLETED THE INSPECTION & REPLACED THE GIRT BAR FOR THE DOOR R1 ESCAPE SLIDE.
NOTIFIED BY CLEANERS THAT THE GIRT BAR ON THE 1R DOOR BECAME DETACHED. FOUND GIRT BAR LOCK KNOCKED OFF GIRT BAR. RE-INSTALLED LOCK.
R1 GIRT BAR END DISENGAGED AS FROM BAR AS DOOR IS OPENED. REPLACED GIRT BAR.
RON VISIT RT INBD TE FLAP IS DELAMINATED BEHIND NR 2 ENG APPROX 9.5 INCHES FROM OTBD EDGE, 29 INCHES LONG & 7 INCHES FROM TE TO LE AT WS 369.5, BBL 70.50. REPLACED IAW JOB CARD 19L50027003.
SJU R1 DOOR GIRT BAR FWD END LOOSE. SECURED R1 DOOR GIRT BAR, R1 DOOR ARMS & DISARMS SLIDE AS REQUIRED.
FLT 1796, ENROUTE EICAS MESSAGE. TE FLAP DISAGREE WHEN FLAP 1 POSITION SELECTED. FLAPS FAILED TO MOVE TO SELECTED POSITION. ACCOMPLISHED QRH PROCEDURE. R & R FLAP LEVER POSITION TRANSMITTER. NO UNUSUAL CONDITIONS NOTED, PASSED BENCH TEST. CONTAMINATED, CLEANED & TESTED IAW MANUFACTURER`S SPECS.
PHL - FLT 1804 EN-ROUTE PHX TO PHL. FLAPS FAILED TO MOVE. TE LIGHT ON & EICAS MESSAGE TE FLAP DISAGREE DISPLAYED. FLAPS ALSO INOPERATIVE ON TE ALTN SYS. ACCOMPLISHED OPERATIONAL TEST OF THE TE EDGE FLAPS, COULD NOT DUPLICATE, INSPECTED FLAPS & NO FAULTS FOUND.
C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON SERVO STAND BOX SUPPORT LOWER CHORD AT BS 1860, BL 0. REPAIRED SERVO STAND BOX SUPPORT LOWER CHORD AT BS 1860, B L0 IAW EA 505777 & 505775 & B757 SRM 51-40-02-0G.
C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON L4 DOOR CUT OUT LOWER FWD SUPPORT ANGLE AT BS 1642, LBL 63. REPLACED L4 DOOR CUT OUT LOWER FWD SUPPORT ANGLE AT BS 1642, LBL 63 IAW B757 SRM 51-10-02, 53-60-15-1A-1, 51-40-02 & DRAWING 146N8769.
C4 CHECK DELAMINATION ON NR 7 SLAT TE WEDGE INBD END LOWER SURFACE AT OSS305. REPAIRED NR 7 SLAT TE WEDGE IAW B757 SRM 51-70-06.
C4 CHECK CRACK ON INTERCOSTAL BETWEEN BS 345 TO BS 365, RBL 44. REPLACED INTERCOSTAL BETWEEN BS 345 TO BS 365, RBL 44 IAW B757 SRM 51-40-02.
C4 CHECK LEVEL 2 INTERGRANULAR CORROSION ON INTERCOSTAL AT BS 684 BETWEEN LBL 34 TO LBL 44. REPLACED INTERCOSTAL AT BS 684 BETWEEN LBL 34 TO LBL 44 IAW B757 SRM 51-40-02.
C4 CHECK CRACK ON INTERCOSTAL UPPER T CHORD BETWEEN BS 324 TO BS 345, RBL 25. REPAIRED INTERCOSTAL BETWEEN BS 324 TO BS 345, RBL 25 IAW B757 SRM 51-40-02 & DRAWING 141N5150.
DURING C4 CHECK. CABIN CREASEBEAM CORRODED BETWEEN BS 754 AND 763 AT LBL 64. REPAIRED CREASE BEAM IAW SRM 51-10-02, 53-30-13, 51-40-02, 51-70-12 & 51-20-21.
DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 377.7 AND LBL 62. R & R FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A AND 51-40-02.
DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED BETWEEN BS 395 AND 418 AT RBL 60. R & R FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02.
DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 1655 AND LBL 62. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-02, 53-60-15-1A-1, 51-40-02, 51-30-01 AND 51-20-01.
DURING C4 CHECK. CABIN SEAT TRACK CORRODED AT BS 377.7 AND LBL 44. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK IAW SRM 53-00-51-1A & 51-40-02 AND DRAWING 141N5130 & 141N5131.
DURING C4 CHECK, CABIN SEAT TRACK CORRODED AT BS 377.7 AND LBL 24. FABRICTED AND INSTALLED REPLACEMENT SEAT TRACK IAW SRM 53-00-51-1A & 51-40-02-0G AND DWG 141N5130 & 141N5131.
DURING C4 CHECK, CABIN FLOORBEAM CORRODED AT BS 377.7 AND LBL 62. REPAIRED FLOORBEAM IAW SRM 51-10-02, 53-00-51-1A & 53-00-51-2R-10.
DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 397 AND BL 0. R & R FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02.
DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED BETWEEN BS 720 AND 740 AT RBL 55. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02 AND DWG 143N5410.
DURING C4 CHECK, CREASEBEAM CORRODED AT BS 750 AND LBL 55. R & R CREASE BEAM IAW SRM 51-10-02, 51-40-02 & 53-30-13-1A AND DWG 143N8322.
DURING C4 CHECK. CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1300 AND 1350 AT LBL 56. R & R FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02 CORROSION.
DURING C4 CHECK. CABIN FLOORBEAM CORRODED BS 365 FROM BL 0 TO RBL 64. REPAIRED FLOORBEAM IAW SRM 51-10-02, 53-00-51-1A, 51-40-02-0G & 53-00-51-2R-10.
DURING C4 CHECK, FLOOR SUPPORT CORRODED BETWEEN BS 333.45 AND 365.25 RBL 62. R & R FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02.
DURING C4 CHECK, FLOOR SUPPORT ANGLE CORRODED AT BS 728 AND LBL 67. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT ANGLE IAW SRM 51-10-02, 53-00-51-1A & 51-40-02 AND DWG 143N8322.
C4 CHECK CABIN FLOOR STRUCTURE CLIP CRACKED AT BS 1320 & LBL 25. R & R CLIP IAW B757 SRM 51-40-02.
DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 1315 AND LBL 25. R & R SUPPORT IAW SRM 51-40-02, 53-00-51-1A & 51-30-01.
DURING C4 CHECK. CREASE BEAM CORRODED BETWEEN BS 680 AND 740 AT RBL 56. R & R CREASE BEAM IAW SRM 51-10-02, 53-00-51-1A & 51-40-02-0G.
DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 1675 AND LBL 62. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-02, 53-60-15-1A-1 & 51-40-02 AND DWG NR 146N8016.
DURING C4 CHECK, CABIN FLOOR SUPPORT ANGLE CRACKED BETWEEN BS 1420 AND 1440 AT BL 0. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT ANGLE IAW DWG 140N2505 AND SRM 51-40-02.
DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED BETWEEN BS 72 AND 740 AT LBL 56. R & R FLOOR SUPPORT IAW SRM 51-40-02.
DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 397 RBL 44. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02 AND DWG 141N5162.
DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED BETWEEN BS 700 AND 720 AT LBL 56. R & R FLOOR SUPPORT IAW SRM 51-40-02.
DURING C4 CHECK, CABIN FLOOR SUPPORT CORRODED BETWEEN BS 680 AND 700 LBL 56. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT IAW SRM 51-10-02 & 53-00-51-1A AND DWG 143N540.
DURING C4 CHECK, CORROSION AT CUSP WEB BETWEEN BS 1620 TO 1640, LBL 62. REPLACED CUSP WEB IAW SRM 51-10-02-OG, 53-00-51-1A, 51-30-01, 51-40-02 & DWG 146N8722.
DURING C4 CHECK. CABIN FLOOR SUPPORT WEB CORRODED BETWEEN BS 1300 AND 1320 AT RBL 55. R & R FLOOR SUPPORT WEB IAW SRM 53-60-15-1A, 51-10-02 & 51-40-02 AND DWG 146N8322.
DURING C4 CHECK. CABIN FLOOR SUPPORT CORRODED AT BS 1660 AND RBL 56. R & R FLOOR SUPPORT IAW SRM 53-60-15, 51-40-02 & 51-30-01.
DURING C4 CHECK. CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1640 AND 1682 AT LBL 56. R & R FLOOR SUPPORT IAW SRM 51-10-02, 53-60-15-1A-1, 51-40-02 & 51-40-05.
DURING C4 CHECK. CABIN FLOOR STIFFENER CRACKED AT BS 1320 AND LBL 50. R & R STIFFENER IAW SRM 51-40-02, CRACK, .5".
C4 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON R4 DOOR LOWER CUT OUT AREA FWD SILL FITTING AT BS 1650, RBL 62. REPLACED FWD SILL FITTING AT BS 1650, RBL 62 IAW B757 SRM 51-10-02, 53-00-51-1A & 51-40-02.
DURING C4 CHECK. CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1640 AND 1660 AT BL 0. R & R FLOOR SUPPORT IAW SRM 51-40-02.
DURING C4 CHECK. FLOORBEAM ANGLE CORRODED AT BS 1678 AND BLB 56. R & R FLOORBEAM ANGLE IAW SRM 51-40-02, 51-40-05 & 53-00-01.
C4 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON L4 DOOR LOWER CUT OUT AREA FWD SILL FITTING AT BS 1670, LBL 62. REPLACED FWD SILL FITTING AT BS 1670, LBL 62 IAW B757 SRM 51-10-02, 53-60-15-1A & 51-40-02.
DURING C4 CHECK. CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1660 AND 1682 AT LBL 56. R & R FLOOR SUPPORT IAW SRM 51-10-02, 51-40-02, 51-40-05 & 53-00-51-1A-1.
DURING C4 CHECK. CABIN FLOOR SUPPORT CORRODED BETWEEN BS 1660 AND 1680 AT RBL 9.5. R & R FLOOR SUPPORT IAW SRM 51-30-01 & 51-40-02 AND DWG 146N5191.
C4 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON L4 DOOR LOWER CUT OUT AREA FWD SILL FITTING AT BS 1670, LBL 62. REPLACED FWD SILL FITTING AT BS 1670, LBL 62 IAW B757 SRM 51-10-02, 53-00-51-1A & 51-40-02.
DURING C4 CHECK. CABIN SEAT TRACK CORRODED AT BS 1640 AND LBL 45.5. REPAIRED SEAT TRACK IAW SRM 51-10-02, 53-00-52-1A & 53-00-52-2R-3.
DURING C4 CHECK, FLOOR SUPPORT CORRODED BETWEEN BS 1660 AND 1680 AT BL 0. R & R FLOOR SUPPORT IAW SRM 51-40-02.
ENROUTE, WHEN STARTING A CLIMB FROM 36000 TO 38000, RT ENGINE ROLLED BACK TO IDLE. SEVERAL ATTEMPTS MADE TO RECOVER POWER UNSUCCESSFULLY. ENGINE DID NOT FLAME OUT. CONTINUED FLIGHT AT IDLE POWER, AT LOWER ALTITUDE. THE FLIGHT DECLARED AN EMERGENCY AND DIVERTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. AT 4000 FT, THERE WAS SOME RECOVERY. MAINTENANCE REPLACED RT ENGINE FUEL FLOW GOVERNOR.
EMERGENCY LIGHT AT ROW 13 LT SIDE, LOOSE. SECURED EMERGENCY LIGHT AT ROW 13.
EMERGENCY EXIT LIGHTING STRIP ON FLOOR AT ROW 10 IS LOOSE AND STICKING UP. RESECURED STRIP TO FLOOR.
CLT - EMERGENCY FLOOR MOUNTED TRACK LIGHTS LOOSE AT ROW 11-12. SECURED FLOOR TRACK LIGHT STRIP AT ROW 11-12.
PHX - L2 DOOR EMERGENCY EXIT LENS COVER FELL OFF (LENS IN FLT DECK). RE-ATTATCHED EMERGENCY EXIT LENS COVER AT L2 DOOR.
ESCAPE PATH MARKING MISSING AT R2 DOOR. MAINTENANCE INSTALLED ESCAPE PATH EXIT ARROW AND STRIPS AS REQUIRED.
L2 DOOR WON'T CLOSE, MAKES LOUD NOISE WHEN TRYING TO CLOSE. MAINTENANCE REMOVED AND REPLACED BROKEN HOLD-OPEN LOCK COLLAR.
FLT 1579, ON DESCENT, AS POWER WAS ADVANCED TO LEVEL OFF AT 12,000, ALL 3 COCKPIT OCCUPANTS NOTICED A DIRTY SOCK ODOR. AFTER ABOUT 1 MINUTE TURNED OFF RIGHT PACK. ODOR PERSISTED. TURNED OFF LEFT PACK AND ODOR DISAPPEARED QUICKLY. ODOR NOT NOTICED IN CABIN. MAINTENANCE SEALED LEFT ENGINE IP COMPRESSOR CASE SPEED SENSOR TERMINAL BLOCKS IN 3 AND 12 POSITIONS. ALSO, ACCOMPLISHED TASK TO REMOVE OIL CONTAMINATION FROM AIR CONDITIONING AND PNEUMATIC SYSTEM. RAN ENGINES AND PACKS, NO ODOR DETECTED.
FLT 1560 EN ROUTE. ENTERTAINMENT SYS WIRING SPARKING AT SEAT 12F. REMOVED & INSTALLED NEW AUDIO SYSTEM CABLE AT ROW 12DEF.
CLT - R1 DOOR EMERGENCY POWER ASSIST RESEVOIR NEEDS REMOVED AND REPLACED. REPLACED RESERVOIR.
C3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON HAT CHANNEL BETWEEN BS 1380 TO BS 1400, S23R. REPLACED HAT CHANNEL BETWEEN BS 1380 TO BS 1400, S23R IAW B757 SRM 51-40-03.
C3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WEB AT BS 1400, S27R. REPLACED WEB AT BS 1400, S27R IAW B757 SRM 51-40-02 & BOEING DRAWING 145N5401.
C3 CHECK - CRACK IN FAIL SAFE STABILIZER STRAP AT BS 365.25, LBL 20. REPAIRED FAIL SAFE STABILIZER STRAP AT BS 365.25, LBL 20 IAW EA 103639.
C3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORTS AT BS 1470 BETWEEN LBL 14 TO RBL 14. REPLACED FLOOR SUPPORTS AT BS 1470 BETWEEN LBL 14 TO RBL 14 IAW B757 SRM 51-70-11.
C3 CHECK - AREA OF DISBOND ON RIGHT INBOARD MAIN FLAP, OUTBOARD TRAILING EDGE WEDGE LOWER SURFACE APPROX 13 INCHES FROM INBOARD END & 6 INCHES FORWARD OF AFT TRAILING EDGE. REPAIRED RIGHT INBOARD MAIN FLAP, OUTBOARD TRAILING EDGE WEDGE LOWER SURFACE IAW B757 57-53-01-01 & SRM 51-70-10.
L1 DOOR ASSIST BOTTLE LOW PRESSURE. REPLACED DOOR ASSIST BOTTLE.
PHL - FLASHLIGHT NOT CHARGING L2 DOOR INBD. REMOVED AND REPLACED BATTERY PACK, F/A FLASHLIGHT L2 INBD POS CHARGING NORM.
PHL - EMERGENCY LIGHT UNARMED LIGHT ASSY BROKEN. REPLACED LIGHT PANEL ASSY CHECKS GOOD.
RON CHECK - CORROSION ON LOWER SECTION OF INTERCOSTAL BELOW AFT CARGO FLOOR BETWEEN BS 1400 TO BS 1405, RBL 3. REPLACED INTERCOSTAL BELOW AFT CARGO FLOOR BETWEEN BS 1400 TO BS 1405, RBL 3 IAW BOEING DRAWING 146N5399 & B757 SRM 51-40-02.
RON CHECK - CORROSION ON LOWER SECTION OF INTERCOSTAL BELOW AFT CARGO FLOOR BETWEEN BS 1400 TO BS 1405, LBL 3. REPLACED INTERCOSTAL BELOW AFT CARGO FLOOR BETWEEN BS 1400 TO BS 1405, LBL 3 IAW BOEING DRAWING 146N5399 & B757 SRM 51-40-02.
RON CHECK - CORROSION ON FRAME AT BS 1460 BETWEEN BBL 0 TO RBL 6 & BETWEEN S29R TO S30. REPAIRED FRAME AT BS 1460 BETWEEN BBL 0 TO RBL 6 & BETWEEN S29R TO S30 IAW EA 200659 & 103312.
FLT 1043 ENROUTE, RIGHT ENGINE OVERHEATING. THE CREW POWERED BACK THE RIGHT ENGINE AND DECLARED AN EMERGENCY. THE FLIGHT DIVERTED TO PLS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND RING SEAL CLAMP LOOSE ON HP2 DUCT OFF TAKE. REPLACED RING SEAL. OPS CHECKED OK.
CLT - C2 - MAJOR REPAIR - FASTENER SHEARED AT RIGHT PYLON OUTBOARD UPPER VERTICAL FLANGE FOR STRUT TO DIAGONAL BRACE FITTING AT PPS209.5. REPLACED DAMAGED FASTENER IAW EA 102029A.
CLT - C2 - MAJOR REPAIR - DELAMINATION ON APU TAIL CONE INTERIOR SKIN PANEL AT BS1990, BL 0. REPAIRED APU TAIL CONE INTERIOR SKIN PANEL AT BS 1990, BL 0 IAW EA 132039.
CLT - C2 - MAJOR REPAIR - CORROSION ON LOWER SURFACE OF CREASE BEAM WEB & T-ANGLE BETWEEN BS 1330 TO BS 1335, S17R, RBL 65. REPLACED CREASE BEAM CHORD BETWEEN BS 1330 TO BS 1335, S17R, RBL 65 IAW B757 DRAWING 146N8322.
CLT - C2 - MAJOR REPAIR - CORROSION ON LOWER SURFACE OF CREASE BEAM WEB AT BS 1330, S17R, RBL 65. REPLACED CREASE BEAM WEB AT BS 1330, S17R, RBL 65 IAW BOEING DRAWING 143N8322.
PHL - THE R3 DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE WAS LOW. MAINTENANCE REPLACED THE EMERGENCY ESCAPE SLIDE AT DOOR R3. OK FOR SERVICE.
PHL - THE EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE AT DOOR R3 WAS LOW. MAINTENANCE REPLACED THE R3 DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE.
FLL - EMERGENCY EXIT SIGN AT LEFT AFT DOOR INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY.
LOCATION: BETWEEN FR 16 AND 17 AND -Y50 REMOVED AND REPLACED FLOORBEAM AND BRACE IAW SRM 51-72-00; CORR TASK JA-220-53500; LEVEL 1 DEFECT SIZE: 5 SQ. IN.
INBOARD FOREFLAP, TRAILING EDGE, BOTTOM SIDE, 12 INCHES OUTBOARD OF AFT FLAP CUTOUT CHAFED. CUT OUT DAMAGE, HONEYCOMB REPAIR WITH DOUBLERS PER SRM 51-70-10, DEFECT SIZE: 1 INCH.
TOP CHORD OF FLOOR FRAME 1640 AT LBL 57 CORRODED; CORR TASK JL-58-53516L LEVEL 1. SPLICED IN NEW UPPER T-CAP CHORD & ANGLE DOUBLERS PER TYP REP 53-15-01; SRM 51-40-02; DEFECT SIZE: 2 X 2 INCHES.
SPORADIC CORROSION BETWEEN STA 1681 & 1720 AND FROM LBL 51 - RBL 51 CORRODED. MANUFACTURED FLOOR WEB PER DWG 146N5300; CORR TASK C53-251-03; LEVEL 1, DEFECT SIZE: 5 SQ INCHES.
STA 1661 LBL 4 TOP SIDE OF BEAM AROUND HOLE CORRODED. REPLACED CAP OF FLOORBEAM PER TR 53-15-01, DEFECT SIZE: 1 X 2 INCHES.
RIGHT CREASE BEAM BETWEEN CHORD & WEB AT STA 1636 CORRODED. REMOVED & REPLACED WEB PER SRM 51-40-02. CORR TASK JA-58-53516, LEVEL 1, DEFECT SIZE: 1 X 3 INCHES.
INBOARD OF AFT LEFT DOOR SILL BETWEEN STA 1640-1660 OF FLOOR STRUCTURE CORRODED. REMOVED & REPLACED PART PER SRM 51-40-01, DEFECT SIZE: 2 X 2 INCHES.
OUTBOARD END OF SLAT COVE PANEL CRACKED. FABRICATED NEW COVE PANEL ABOUT 27 INCHES LONG PER BOEING DWG 114N4003, DEFECT SIZE: 1 INCH.
RIGHT AFT DOOR SILL STA 1660-1680 CORRODED. REMOVED & REPLACED WITH NEW WEB PER SRM 51-40-00; CORR TASK JL-90-0900; LEVEL 1, DEFECT SIZE: 9 X 1.5 INCHES.
ANGLE AT STA 300-377 RBL 61 CORRODED. FABRICATED & INSTALLED NEW ANGLE PER BAC DWG 141N8322; CORR TASK JL-43-53501; LEVEL 1, DEFECT SIZE: 1.5 X 9 INCHES.
NUMEROUS AREAS AROUND SCREW HOLES, TOP OF FLOORBEAM STA 377.7 CORRODED. INSTALLED T-CAP & SPLICE ANGLES PER SRM 53-00-51; CORR TASK JL-46-53500; LEVEL 1 DEFECT SIZE: 2.75 INCHES.
BETWEEN STA 324-327 RBL 60 CORRODED. REMOVED & REPLACED 2 CREASE BEAMS PER SRM 51-40-02; CORR TASK JL-46-53500, LEVEL 1, DEFECT SIZE: 120 SQ INCHES.
FWD END SEAT TRACK LBL 45.5 AT STA 377.7 CORRODED. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER DWG 141N5131 & SRM 51-70-12, DEFECT SIZE: 1.5 INCH X 5 FEET.
LEFT DOOR SILL AFT WEB & SUPPORT CLIP, BETWEEN STA 1660-1681 CORRODED. REMOVED CORROSON PER SRM 53-60-15, TREATED & PRIMED, FAB'D NEW SUPPORT CLIP. CORR TASK JL-58-53516, DEFECT SIZE: 1 X 1 INCH.