N936AN
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 WAS NOT GROUNDED: AFTER CABIN RH F/A INBOARD EMERGENCY FLASH LIGHT INOP. MAINTENANCE REPLACED R/H AFT FA INBOARD FLASHLIGHT BATTERY IAW AMM 25-64-00.
AIRCRAFT WAS NOT GROUNDED: AFT FA FLASH LIGHT IS DEAD. MAINTENANCE REPLACED AFT CABIN LH JUMP SEAT INBD FLASH LIGHT IAW AMM 25-64-00.
AIRCRAFT WAS GROUNDED: AT FL270 FLIGHT ATTENDANT REPORTED A MODERATE DIRTY SOCK SMELL FROM THE CENTER TO AFT FUSELAGE. ACCOMPLISHED JC 08L00021001 AND NO SMOKE OR ODOR WAS PRESENTED. SOF EVENT COULD NOT DUPLICATED AT THIS TIME. PERFORMED BOTH PACK DECONTAMINATION/ PNEUMATIC DUCT PURGING, PER AMM21-00-01. REMOVED AND REPLACED BOTH RECIRCULATION FAN FILTERS (AALA202603260375) AND (AALA202603279672), PER AMM21-25-01 (OPEN).
AIRCRAFT WAS GROUNDED: AT FL270 FLIGHT ATTENDANT REPORTED A MODERATE DIRTY SOCK SMELL FROM THE CENTER TO AFT FUSELAGE.
AIRCRAFT WAS GROUNDED: AT FL270 FLIGHT ATTENDANT REPORTED A MODERATE DIRTY SOCK SMELL FROM THE CENTER TO AFT FUSELAGE. ACCOMPLISHED JC 08L00021001 AND NO SMOKE OR ODOR WAS PRESENTED. SOF EVENT COULD NOT DUPLICATED AT THIS TIME. PERFORMED BOTH PACK DECONTAMINATION/ PNEUMATIC DUCT PURGING, PER AMM21-00-01. REMOVED AND REPLACED BOTH RECIRCULATION FAN FILTERS (AALA202603260375) AND (AALA202603279672), PER AMM21-25-01, (OPEN).
AIRCRAFT WAS GROUNDED: VOMIT SMELL COMING FROM AIRCRAFT AIR CONDITIONING SYSTEM. WHILE ACCOMPLISHING TROUBLE SHOOTING OF SOF EVENT FOUND RECIRCULATION FAN FILTERS TO BE DIRTY AND FOUND RECIRCULATION FAN INSULATION BLANKETS COVERED IN UNKNOWN LIQUID. REMOVED AND REPLACED RECIRCULATION AIR FILTERS (AALA202603109798), PER AMM 21-35-01. ALSO, RMOVED AND REPLACED INSULATION BLANKET (AALA202603100296) ON FORWARD CARGO AFT BULKHEAD, PER AARD 25-80-00-3. OPS CHECK FOR LEAK ON FORWARD GALLEY AND NO LEAK FOUND.
AIRCRAFT WAS GROUNDED: VOMIT SMELL COMING FROM AIRCRAFT AIR CONDITIONING SYSTEM. WHILE ACCOMPLISHING TROUBLE SHOOTING OF SOF EVENT FOUND RECIRCULATION FAN FILTERS TO BE DIRTY AND FOUND RECIRCULATION FAN INSULATION BLANKETS COVERED IN UNKNOWN LIQUID. REMOVED AND REPLACED RECIRCULATION AIR FILTERS (AALA202603109798), PER AMM 21-35-01. ALSO, RMOVED AND REPLACED INSULATION BLANKET (AALA202603100296) ON FORWARD CARGO AFT BULKHEAD, PER AARD 25-80-00-3. OPS CHECK FOR LEAK ON FORWARD GALLEY AND NO LEAK FOUND.
AIRCRAFT WAS NOT GROUNDED: SEAT ASSEMBLY 1BA AFT EMERGENCY LIGHT ON SEAT DOES NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY FLOOR PROXIMITY LIGHT ASSEMBLY AT SEAT 1BA. PER AMM 33-51-11. OPS CHECK GOOD AT THIS TIME.
AIRCRAFT WAS NOT GROUNDED: FORWARD SERVICE DOOR ESCAPE SLIDE IS COMING OUT OF COMPARTMENT. MAINTENANCE RE-SECURED FORWARD ESCAPE SLIDE LATCH PER AMM 25-61-00.
AIRCRAFT WAS GROUNDED: L1 DOOR GUST LOCK WILL NOT ENGAGE WHEN DOOR IS OPEN. FOUND L1 GUIDE ARM OPEN LOCK MECHANISM BROKEN. REPLACED L1 GUIDE ARM. PER AMM 52-11-21.
AIRCRAFT WAS NOT GROUNDED: LEFT HAND AFT OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED PER AMM 33-51-04. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS GROUNDED: FLIGHT ATTADNENT REPORTS MILD BURNING PLASTIC SMELL IN DESCENT IN AFT GALLEY. ACCOMPLISHED SOF J/C 08L00021001, NO FAULTS FOUND OR DAMAGE NOTED.
AIRCRAFT WAS NOT GROUNDED: AIRCRAFT LEFT, AFT DOOR 2L SLIDE IS DETACHING FROM DOOR,. RESECURE BUSTLE ON AFT L2 DOOR. PER AMM 52-13-31.
AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR IS DIFFICULT TO OPEN OR CLOSE. ADJUSTED AND LUBRICATED FORWARD LAVATORY DOOR. PER CMM 25-45-46.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: IMMEDIATELY AFTER TAKEOFF THE CONTROL CABIN TEMPERATURE BECAME EXCESSIVELY HOT AND THE CONTROL CABIN ZONE TEMP OVERHEAD LIGHT ILLUMINATED; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW.**SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: IMMEDIATELY AFTER TAKEOFF THE CONTROL CABIN TEMPERATURE BECAME EXCESSIVELY HOT AND THE CONTROL CABIN ZONE TEMP OVERHEAD LIGHT ILLUMINATED; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW.**SUPPLEMENTAL REPORT FOR (AALA202408141621): AFTER PACK INSPECTION FOUND LEFT HAND PACK SENSE LINE DISCONNECTED FROM FLOW CONTROL SHUTOFF VALVE, RECONNECTED AND TORQUED SENSE LINE, LEAKS AND OPERTIONAL CHECK GOOD PACK OPERATED NORMAL. PER AMM 21-51-01-400.**(CLOSED).
AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR IS STICKY AND HARD TO OPEN AND CLOSE. FOUND FORWARD LAVATROY DOOR LOWER DOOR SILL 2EA SCREWS STICKING UP AND LOOSE. SECURED SCREWS AS REQUIRED. OPERTIONAL CHECKED OKAY.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.
AIRCRAFT WAS NOT GROUNDED: FIRST CLASS LAVATORY DOOR DIFFICULT TO OPEN AND CLOSE. ADJUSTED FIRST CLASS LAVATORY DOOR. PER AMM 25-40-11.
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS THAT FORWARD GALLEY LAVATORY DOOR KNOB WORKS INTERMITTENTLY. FORWARD LAVATORY DOOR KNOB ADJUSTED AND CHECKS GOOD REF. AMM 25-40-11.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLOOD LIGHT IN AFT LOWER CEILING PANEL INOPEATIVE AT ROW 33 A-F. REPLACED BULB AND OPERTIONAL CHECK GOOD. PER AMM 33-51-03.
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER VISUAL INDICATION OF A CRACK IN LOWERSKIN AT STABILIZER BS 101.90 LOCATED 9 INCHES FROM THE AFT SPAR. FABRICATED DOUBLER PER SRM 55-10-01-2R REPAIR 11 INSTALLED DOUBLER. PER SRM 55-10-01-2R REPAIR 11.
AIRCRAFT IN BASE MAINTIANCE: BOTTOM OF GIRT IS WORN ON R1 SLIDE, GALLEY SERVICE DOOR. INSTALLED SLIDE ASSEMBLY. PER AMM 25-66-01.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER RIB, ON SECOND STIFFENER FROM FRONT SPAR, LOCATED AT STABILIZER STA 92.70, REPLACED RIB PER AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: UNSPECIFIED DAMAGE FOUND TO PASSENGER CABIN FLOOR WEB FROM BS 927 TO BS 947, RBL 54. REPLACED WEB PER AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER STIFFENER AT BS 663, LBL 30. REPLACED STIFFENER PER EA 351145 AND SRM 57-10-10-2R-2.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM BS 947.5 TO BS 967, LBL 51. REPLACED INTERCOSTAL PER AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT INTERCOSTAL AT BS 500D, RBL 27. REPLACED INTERCOSTAL PER SRM 51-40-02.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR BOARD SUPPORT AT BS 540, LBL 1. REPLACED FLOORBOARD SUPPORT PER AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN INTERCOSTAL FROM BS 327 TO BS 344, LBL 46. REPLACED INTERCOSTAL PER SRM 51-40-02.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN INTERCOSTAL FROM BS 312 TO BS 327, LBL 46. REPLACED INTERCOSTAL PER SRM 51-40-02.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM BS 947 TO BS 967, RBL 24.5. REPLACED INTERCOSTAL PER SRM 51-40-02.
AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN INTERCOSTAL FROM BS 294 TO BS 277, BL 0. REPLACED INTERCOSTAL PER SRM 51-40-02.
AIRCRAFT IN BASE MAINTENANCE: CRACK N FORWARD CARGO COMPARTMENT TRANSITION PANEL AT BS 500C MINUS 6 INCHES, RBL 25. REPLACED TRANSITION PANEL PER SRM 51-40-02 AND SRM 53-00-53-2R-6.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 727J AND BS 747, LBL 25. REPLACED TRANSITION PANEL PER SRM 53-00-53-1A-2 AND AARD 51-00-05-01.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL FROM BS 847 TO BS 967, RBL 52. REPLACED INTERCOSTAL PER SRM 51-40-02.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN AFT ENTRY WAY SILL INNER CHORD AT BS 947.5, RBL 55. REPLACED CHORD PER AARD 51-00-05-1.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER CHORD OF APU ENCLOSURE AT BS 1104, RBL 21. REPAIRED CHORD PER EA 351132.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD AT BS 947.5, RBL 45. REPLACED UPPER CHORD PER SRM 53-70-51-2R-5.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER CHORD OF FLOOR BEAM, AROUND LAVATORY FLOOR MOUNT, AT BS 947.5, LBL 25. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-5.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL, , CORROSION ON TRANSITION PANEL BETWEEN BS 747 AND BS 767, RBL 25. REPLACED TRANSITION PANEL PER SRM 53-00-53-1A-2 AND AARD 51-00-05-01
AIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN LOCATED AT STABILIZER STA 101.90, 9 INCHES FROM AFT SPAR. REPAIRED SKIN PER SRM 55-10-01-2R-11.
AIRCRAFT WAS NOT GROUNDED: RIGHT MAIN TANK FUEL PUMP LOW PRESSURE LIGHT WILL NOT GO OUT WHEN PUMP SWITCH IS TURNED ON.**SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).
AIRCRAFT WAS NOT GROUNDED: RIGHT MAIN TANK FUEL PUMP LOW PRESSURE LIGHT WILL NOT GO OUT WHEN PUMP SWITCH IS TURNED ON.**SUPPLEMENTAL REPORT FOR (AALA202312277774): REPLACED CONNECTOR, PIN 2 AND 3 AND BACKSHELL. PER SWPM 20-61-11 AND WDM 28-43-11. OPERATIONAL CHECK GOOD.**(CLOSED).
AIRCRAFT WAS GROUNDED: EMERGENCY DECLARED ON APPROACH TO STI DUE TO HYDRAULIC SYSTEM B LOW PRESSURE LIGHT. AIRCRAFT LANDED SAFELY AT STI WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED O-RING RIGHTHAND NUMBER 8 SPOLIER ACTUATOR FILTER CAP PER CMM 27-60-42.
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED MANUAL SYSTEM ACCESS DOOR SWITCH PER MM 32-34-00. ACCOMPLISHED FUNCTIONAL ALTERNATE LANDING GEAR TEST PER MM 32-31-51.
AIRCRAFT WAS NOT GROUNDED: LEFT AFT FUEL LOW PRESSURE LIGHT CAME ON IN FLIGHT. PRIMED LEFT AFT FUEL BOOST PUMP PER FIM 28-22-00-810-803. PUMP OPERATES NORMAL.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT NOT ARMED LIGHT HAS BULB OUT. REMOVED AND REPLACED WITH NEW BULB PER AMM 11-30-00 OPERATIONS CHECK GOOD.
AIRCRAFT IN BASE MAINTENANCE: AFT RIGHT FLIGHT ATTENDANT SEAT INBOARD FLASHLIGHT INCORRECT MAINTENANCE DUE DATE WAS WRITTEN ON THE PLACARD. EVALUATED AND INSTALLED NEW PLACARD WITH CORRECT MAINTENANCE REMOVED OLD PLACARD.
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND OUTBOARD CARRY THROUGH ANGLE FASTENER HOLES DAMAGED AT BS 887 AND RBL 45.50. REPLACED ANGLE PER SRM 51-40-02.
AIRCRAFT IN BASE MAINTENANCE: LEFT AFT LOWER FUSELAGE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FUSE ON BATTERY PACK M1670 PER AA B737 NG AMM 33-51-06.
AIRCRAFT IN BASE MAINTENANCE. LEFT AFT LOWER FUSELAGE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FUSE ON M1670 BATTERY PACK PER AMM 33-51-06.
AIRCRAFT IN BASE MAINTENANCE: LIGHT INOP AT SEAT 17 ABC. RESEATED CONNECTOR AND OPERATIONS CHECKED GOOD.
AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LEFT HAND #1 WINDOW POST CRACKED AS BS 217. REPAIRED WINDOW POST PER EO 5616J009-007.
AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK FIRST OFFICERS #1 WINDOW POST REQUIRES REINFORCING MODIFICATION / REPAIR PER EO 5616J009-008. ACCOMPLISHED REINFORCING MODIFICATION / REPAIR OF THE FIRST OFFICERS #1 WINDOW POST PER EO 5616J009-008.
AIRCRAFT IN BASE MAINTENANCE: L1 DOOR GUIDE ARM LOCKING MECHANISM NOT PROPERLY LOCKING THE DOOR IN THE OPEN POSITION. REPLACED L1 DOOR GUIDE ARM LOCKING MECHANISM PER AMM 52-11-21.
AIRCRAFT IN BASE MAINTENANCE: QTY 6 EMERGENCY LIGHT BATTERY PACKS MISSING. REPLACED BATTERY PACKS WITH NEW (AALA202112144926, AALA202201312870, AALA202201311085, AALA202201313301, AALA202201314061) IAW B737-NG AMM 33-51-06, OPS CHECK GOOD.
AIRCRAFT IN BASE MAINTENANCE: QTY 6 EMERGENCY LIGHT BATTERY PACKS MISSING. REPLACED BATTERY PACKS WITH NEW (AALA202112144926, AALA202201312870, AALA202201319505, AALA202201311085, AALA202201313301) IAW B737-NG AMM 33-51-06, OPS CHECK GOOD.
AIRCRAFT IN BASE MAINTENANCE: QTY 6 EMERGENCY LIGHT BATTERY PACKS MISSING. REPLACED BATTERY PACKS WITH NEW (AALA202112144926, AALA202201312870, AALA202201319505, AALA202201313301, AALA202201314061) IAW B737-NG AMM 33-51-06, OPS CHECK GOOD.
AIRCRAFT IN BASE MAINTENANCE: QTY 6 EMERGENCY LIGHT BATTERY PACKS MISSING. REPLACED BATTERY PACKS WITH NEW (AALA202201312870, AALA202201319505, AALA202201311085, AALA202201313301, AALA202201314061) IAW B737-NG AMM 33-51-06, OPS CHECK GOOD.
AIRCRAFT IN BASE MAINTENANCE: QTY 6 EMERGENCY LIGHT BATTERY PACKS MISSING. REPLACED BATTERY PACKS WITH NEW (AALA202112144926, AALA202201319505, AALA202201311085, AALA202201313301, AALA202201314061) IAW B737-NG AMM 33-51-06, OPS CHECK GOOD.
AIRCRAFT IN BASE MAINTENANCE: QTY 6 EMERGENCY LIGHT BATTERY PACKS MISSING. REPLACED BATTERY PACKS WITH NEW (AALA202112144926, AALA202201312870, AALA202201319505, AALA202201311085, AALA202201314061) IAW B737-NG AMM 33-51-06, OPS CHECK GOOD.
AIRCRAFT GROUNDED: LEADING EDGE DISSAGREMENT LIGHT ILLUMINATED FROM FLAPS 5 TO 10. PEFORMED GO AROUND DECLARED EMERGENCY, QRH LANDING FLAPS 15. CONT LIGHT REMAINED ILLUMINATED THROUGHOUT LANDING. MINOR SPEED DEVIATIONS WOULD ILLUMINATE GREEN LIGHT THEN BACK TO AMBER. THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED LEADING EDGE FLAP EXTEND PROXIMITY SENSOR S169 (AALA202007029014), LEADING EDGE PROXIMITY SENSOR S995 (AALA202007099005) NR 1SLAT DETENT ARM ROLLER BEARING WHICH WAS FROZEN (AALA202007099006) AND NR 4 SLAT DETENT ROLLER BEARING WHICH WAS FROZEN (AALA202007099007) AND A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT GROUNDED: LEADING EDGE DISSAGREMENT LIGHT ILLUMINATED FROM FLAPS 5 TO 10. PEFORMED GO AROUND DECLARED EMERGENCY, QRH LANDING FLAPS 15. CONT LIGHT REMAINED ILLUMINATED THROUGHOUT LANDING. MINOR SPEED DEVIATIONS WOULD ILLUMINATE GREEN LIGHT THEN BACK TO AMBER. THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED LEADING EDGE FLAP EXTEND PROXIMITY SENSOR S169, LEADING EDGE PROXIMITY SENSOR S995, NR 1 SLAT DETENT ARM ROLLER BEARING WHICH WAS FROZEN AND NR 4 SLAT DETENT ROLLER BEARING WHICH WAS FROZEN AND A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT GROUNDED: LEADING EDGE DISSAGREMENT LIGHT ILLUMINATED FROM FLAPS 5 TO 10. PEFORMED GO AROUND DECLARED EMERGENCY, QRH LANDING FLAPS 15. CONT LIGHT REMAINED ILLUMINATED THROUGHOUT LANDING. MINOR SPEED DEVIATIONS WOULD ILLUMINATE GREEN LIGHT THEN BACK TO AMBER. THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED LEADING EDGE FLAP EXTEND PROXIMITY SENSOR S169 (AALA202007029014), LEADING EDGE PROXIMITY SENSOR S995 (AALA202007099005) NR 1 SLAT DETENT ARM ROLLER BEARING WHICH WAS FROZEN (AALA202007099006) AND NR 4 SLAT DETENT ROLLER BEARING WHICH WAS FROZEN (AALA202007099007) AND A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT GROUNDED: LEADING EDGE DISSAGREMENT LIGHT ILLUMINATED FROM FLAPS 5 TO 10. PEFORMED GO AROUND DECLARED EMERGENCY, QRH LANDING FLAPS 15. CONT LIGHT REMAINED ILLUMINATED THROUGHOUT LANDING. MINOR SPEED DEVIATIONS WOULD ILLUMINATE GREEN LIGHT THEN BACK TO AMBER. THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED LEADING EDGE FLAP EXTEND PROXIMITY SENSOR S169 (AALA202007029014), LEADING EDGE PROXIMITY SENSOR S995 (AALA202007099005) NR 1SLAT DETENT ARM ROLLER BEARING WHICH WAS FROZEN (AALA202007099006) AND NR 4 SLAT DETENT ROLLER BEARING WHICH WAS FROZEN (AALA202007099007) AND A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: R1 DOOR FORWARD BOTTOM STOP BEARING PLATE IS CRACKED. REPLACED STOP BEARING PLATE PER AMM 52-41-01.
AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS #1 OB SLAT HAS BINDING & LOUD BANGING/POPPING SOUND DURING EXTENSION & RETRACTION BETWEEN 5-10 DEGREES TRAVEL. MAINTENANCE LUBED NO. 1 SLAT IAW AMM 12-22-71-604 AND 12-22-71-600. NO FURTHER NOISE FROM #1 SLAT NOTED.
AIRCRAFT WAS GROUNDED: PILOT REPORTS IN CRUISE, THE FLAP INDICATOR HAD SPLIT NEEDLES. RIGHT INDICATOR UP, LEFT INDICATED GREATER THAN UP WAS PAST THE UP INDICATION TOWARDS THE BOTTOM. FLAPS WOULD NOT EXTEND. MAINTENANCE REPORTS FSEU SHOWS FLAP 2 SKEW MAINT MSG 27-53251. REPLACED #2 FLAP SKEW SENSOR T526 IAW AMM 27-59-01. CHECKS OK.
AIRCRAFT WAS GROUNDED: PILOT REPORTS FORWARD LAV HAS AN ODOR OF RESIDUAL ELECTRIC SMOKE OR CHARING. NO EVIDENCE OF ANY ACTIVE ISSUE ON THIS FLIGHT. MAINTENANCE REMOVED AND REPLACED FWD LAV WATER HEATER IAW AMM 38-13-01. OPS CHECK GOOD.
AIRCRAFT WAS GROUNDED: EMERGENCY SLIDE ON DOOR 1L WAS REPORTED BY FLIGHT ATTENDANTS TO SLIDE DOWN ABNORMALLY ON LANDING. MAINTENANCE REPLACED SLIDE PER AMM 25-66-01.
PASSING 32000, LET FLAPS TRANSIT LIGHT ILLUMINATED WITH OVERHEAD LE DEV INDICATOR (6). AN EMERGENCY WAS DECLARED, LANDED WITHOUT INCIDENT. LIGHT WENT OUT DURING DECENT BEFORE QRH PROCEDURE RUN. NORMAL EXTENSION AND LANDING. REPLACED SL6 PROXIMITY OUTBOARD SENSOR S1004 PER AMM 27-88-11. LEADING EDGE FLAP/SLAT POSITION INDICATION SYSTEM OPERATIONS CHECK NORMAL PER AMM 27-88-00, NO FAULT NOTED. THE AIRCRAFT WAS GROUNDED.
CORROSION FOUND ON LOWER LEG OF AN INTERCOSTAL, BS 909 AND STRINGER 25L, LBL 22. REPLACED THE INTERCOSTAL IAW 51-00-05-1.
R1 DOOR STUB FRAME CRACKED AT A PREVIOUS REPAIR, BETWEEN BS 291 TO 300, STRINGERS 15R AND 17R. REPAIRED THE STUB FRAME IAW SRM 51-70-11-2R.
CRACKED CABIN ANGLE BS 540, 1 INCH OUTBOARD OF BL 0. REPLACED THE ANGLE IAW 51-00-05-1.
CRACKED CABIN ANGLE AT BS 540, LBL 1. REPLACED THE ANGLE IAW 51-00-05-1.
CORROSION FOUND ON THE FORWARD SERVICE DOOR CREASE ANGLE LOCATED BETWEEN BS 314 AND 344. INSTALLED A NEW ANGLE IAW SRM 51-40-02, 51-00-05-1, AND DRAWING 141A8310.
CORROSION FOUND ON THE FORWARD ENTRY FLOORBEAM MOUNT BS 344, LBL 60. INSTALLED A NEW MOUNT IAW 51-00-05-01 & DWG. 141A5220.
CORROSION FOUND ON THE FORWARD ENTRY WET AREA LT FLOOR ANGLE BS 342 - 350, LBL 61. INSTALLED AN NEW ANGLE IAW SRM 51-40-02, 51-00-05-1, AND DWG 141A8110.
CORROSION FOUND ON THE FLOOR SUPPORT BETWEEN BS 986, AND 1006, JUST INBORARD OF THE INTERCOSTAL AT RBL 31. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, 51-00-05-1, AND DRAWING 147A5700.
INTERCOSTAL ON THE AFT PRESSURE BULKHEAD IS CRACKED AT BS 1030 AND RBL 12. REPLACED THE INTERCOSTAL IAW 51-00-05-1 AND DRAWING 65-54862-21.
RIGHT ZEE ANGLE AT BS 992, RBL 34 TO RBL 46 CORRODED. INSTALLED A NEW ZEE ANGLE IAW 51-00-05-1 AND DRAWING 147A5710.
CORROSION FOUND ON THE ZEE ANGLE AT RBL 31 AND BETWEEN BS 986 AND 1016. REPLACED THE ANGLE IAW 51-00-05-1 AND DRAWING 147A5710.
R2 CREASE ANGLE HAS CORROSION BETWEEN BS 887 TO 1016. REPLACED THE CREASE ANGLE IAW 51-00-05-1 AND DRAWING 147A8501.
AFT SERVICE DOOR FLOORBEAM TEE CAP CORRODED AT BS 985 BETWEEN RBL 4 AND RBL 43. REPAIRED THE FLOORBEAM IAW EA 277341, 53-00-00-7, AND SRM 53-00-51-2R.
CORROSION FOUND ON THE WEB AT BS 984, BETWEEN LBL 30 - 31. REPLACED THE WEB IAW 51-00-05-1 AND DRAWING 147A5712.
WEB AT BS 1018 HAS CORROSION AT LBL 30. INSTALLED A NEW WEB IAW 51-00-05-1, DRAWINGS 147A5700, AND 147A5712.
ZEE ANGLE AT BS 992, LBL 33 TO LBL 46 HAS CORROSION. INSTALLED A NEW ANGLE IAW 51-00-05-1, DRAWINGS 147A5710, AND 147A5700.
ZEE ANGLE AT LBL 31, BS 986 TO 1016 HAS CORROSION. INSTALLED A NEW ZEE ANGLE IAW 51-00-05-1 AND DRAWING 147A5710.
AFT ENTRY FLOOR STRUCTURE, LEFT CREASE ANGLE HAS CORROSION FROM BS 947 TO 992. REPLACED THE CREASE ANGLE IAW 51-00-05-1 AND DRAWING 147A8501.
AIRCRAFT WAS IN BASE MAINTENANCE. FLOORBOARD Z ANGLE HAS DEEP WORN SPOT AT STA 510 LBL 6. REPAIRED Z ANGLE PER SRM 53-00-53-2R-2.
CORRODED STRAP AT BS 1019 AND RBL 27 STRAP AT BS 1019. REPLACED STRAP IAW DRAWING 147A5700 AND 51-00-05-1.
CORRODED LEFT TRANSITION PANEL CHANNEL BETWEEN BS 807 TO 827. REPLACED THE CHANNEL IAW SRM 53-00-53-2R AND EA.B737-53-022404.
THE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION ON RIGHT HAND TRANSITION PANEL AT STATIONS 727A-727B. REPLACED TRANSITION PANEL PER SRM 53-00-53 AND 51-00-05-1.
INTERCOSTAL AT BS 991, LBL 32 HAS CORROSION ON UPPER SURFACE. REPLACED INTERCOSTAL IAW SRM 51-10-02, AND DRAWING 147A5705.
AIRCRAFT WAS IN BASE MAINTENANCE. STRAP IS CORRODED AT STA 1030, AND RBL 18. REPLACED STRAP PER DRAWING 147A5700 AND AARD 51-00-05-1.
CORROSION ON STRAP AT BS 1030 AND RBL 3. REPLACED STRAP IAW DRAWING 147A5700 AND 51-00-05-1.
THE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION ON R2 DOOR THRESHOLD WEB. REPLACED WEB PER 51-00-05-1, DRAWING 147A8510 AND EA 277849.
LEFT HAND TRANSITION PANEL CHANNEL CORRODED BETWEEN BS 400 AND 500L. REPLACED THE CHANNEL IAW SRM 53-00-53-2R-5.
BAFFLE BETWEEN BS 500C - 500D UNDER TRANSITION PANEL HAS CORROSION. REPLACED THE BAFFLE IAW 51-00-05-1, AND DRAWING 143A750.
BAFFLE AT BS 460-480, LBL 25 HAS CORROSION. REPLACED THE BAFFLE IAW DRAWING 143A7505, AND 51-00-05-01.
CORRODED FLOORBEAM TEE AT BS 985, LBL 4 TO LBL 51. REPAIRED THE FLOORBEAM IAW SRM 51-10-02, AND EA 277694
CORRODED AFT CARGO SHIELD, BS 847. REPLACED THE SHIELD IAW DRAWING 146A0081 AND 51-00-05-1.
CORRODED AFT CARGO SHIELD FORWARD OF DOOR OPENING. REPLACED THE SHIELD IAW DRAWING 146A8127, AND 51-00-05-1.
THE FORWARD CARGO ON THE RIGHT SIDE, THERE WAS CORROSION ON THE UPPER FLANGE OF THE INTERCOSTAL BETWEEN BS 500F-500G. REPAIRED THE INTERCOSTAL IAW SRM 51-70-13-2R-1, SRM 53-30-53-01, AND DRAWING 143A7510.
SHORT TRANSITION PANEL ANGLE BETWEEN BS 495 - 500A RIGHT CORRODED. REPLACED THE ANGLE IAW SRM 51-40-02.
RIGHT TRANSITION PANEL FROM 500A-500L HAS NUMEROUS AREAS OF CORROSION. REPLACED THE TRANSTIION PANEL IAW SRM 53-00-53-2R-5.
AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON INTER-SKIN ANTENNA DOUBLER BETWEEN STA 500 -500-A AND BETWEEN STR 28L -28R. REPLACED INTER-SKIN ANTENNA DOUBLER PER 51-00-05 AND DRAWING NUMBER 143A3230.
SHORT TRANSITION PANEL ANGLE BETWEEN BS 420 - 440 RIGHT HAS CORROSION. REPLACED TRANSITION ANGLE IAW SRM 51-40-02.
CORROSION FOUND ON THE AFT BULKHEAD TRANS ANGEL AT BS 500I. INSTALLED NEW TRANS ANGLE AND FASTENERS IAW 51-00-05-1, AND DWG:143A9485.
CORROSION ON THE NUT PLATE HOLE OF THE FLOOR SUPPORT IN FORWARD SERVICE WET AREA AT BS 325, RBL 11. REPLACED FLOOR SUPPORT IAW 51-00-05-1, AND DRAWING 141A5400.
CORRODED WEB AT BS 984, RBL 33 TO RBL 41. REPLACED THE WEB IAW DRAWING 147A5700, AND 51-00-05-1.
AIRCRAFT WAS NOT GROUNDED. NAUSEOUS DIRTY SOCKS ODOR IN CABIN WHEN THE RIGHT PACK IS TURNED TO AUTO. CHECKED RECIRCULATION FILTERS, LEFT/RIGHT ENGINE INLETS AND APU PLENUM FOR CONTAMINATION. NONE NOTED. ACCOMPLISHED PACK 2 OPERATIONAL CHECK PER AMM 21-51-00, NO ODORS DETECTED. OPERATIONAL CHECK GOOD. (CLOSED)
AIRCRAFT WAS GROUNDED. ON TAXI IN, FLIGHT ATTENDANT REPORTED THE CEILING EMERGENCY EXIT LIGHTS AT THE AFT GALLEY ILLUMINATED. REMOVED AND REPLACED POWER SUPPLY PER AMM 33-51-06. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS NOT GROUNDED. AFT LEFT LAVATORY SMOKE DETECTOR ANNUNCIATOR AND ALARM ON. FLIGHT ATTENDANT REPORTS VICINITY OF TRASH CAN FEELS WARM. RESET SMOKE DETECTOR PER AMM 26-14-00. OPERATIONAL CHECK GOOD.
CENTER WING REAR SPAR RIGHT MAIN LANDING GEAR WHEEL WELL VERTICAL PRESSURE DECK WEB CRACKED AT FUSELAGE STATION 663.75, RBL31.83 TO RBL43.80. REPAIRED IAW SRM 57-10-10-2R-3 ALTERNATIVE 2.
LEFT MAIN LANDING GEAR WHEEL WELL VERTICAL PRESSURE DECK WEB CRACKED AT BS 663.75, LBL31.83 TO LBL43.80. REPAIRED IAW SRM 57-10-10-2R-3 ALTERNATIVE 2.
AIRCRAFT NOT GROUNDED. EMERGENCY EXIT LIGHT L1187 AT L1 DOOR IS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.
AIRCRAFT NOT GROUNDED. EMERGENCY EXIT LIGHT L1191 AT R2 DOOR IS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.
AIRCRAFT WAS GNDED. DURING TAKEOFF THE TAKEOFF CONFIGURATION WARNING LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT APPROX 105 KNOTS. ACCOMPLISHED FIM 31-51-00-810-803 & 31-51-00-810-822 WITH SATISFACTORY RESULTS.
AIRCRAFT WAS IN BASE MX. VERTICAL PRESS WEB AT FS 663.75 IS CRACKED AT APPROX RBL 44. REPAIRED WEB IAW EA 259851.
AIRCRAFT WAS IN BASE MX. RAM AIR INLET FWD FAIRING ANGLE CLIP HAS A 0.5 INCH CRACK AT OTBD LOWER END. R & R ANGLE CLIP IAW DWG 143A0060 ID 0022 & SRM 51-10-02-0G PARAGRAPH 9.
CRACK FOUND IN FIRST OFFICERS NR 3 WINDOW POST FASTENER HOLE, SECOND HOLE FROM BOTTOM. INSTALLED DOUBLER & TRIPLER REPAIR IAW ESO 61000 & AARD 53-10-00-7. ACFT IN BASE MX.
RIGHT MAIN WW FWD BULKHEAD WEB AT STATION 663.75 IS CRACKED BETWEEN RBL 31.83 & RBL 43.80. REPAIRED WEB IAW EA 253963.
FUSELAGE SKIN IS CORRODED AROUND AFT LAVATORY VENT AT STATION 907 & STRINGER 23L. ACCOMPLISHED DOUBLER REPAIR IAW EA 253938.
LEFT MAIN WW FWD BULKHEAD WEB AT STATION 663.75 IS CRACKED BETWEEN LBL 31.83 & LBL 43.80. REPAIRED WEB IAW EA 253963.
SEAT ROWS 12D - 22D & 14DC OVERHEAD LIGHTING FAILED TO ILLUMINATE. SEAT LIGHTING BETWEEN ROW 13 - 20 FAILED CAPACITY CHECK. R & R FWD POWER SUPPLY IAW AMM 33-51-06.
SEAT ROWS 12D - 22D & 14DC OVERHEAD LIGHTING FAILED TO ILLUMINATE. SEAT LIGHTING BETWEEN ROW 13 - 20 FAILED CAPACITY CHECK. R & R AFT POWER SUPPLY IAW AMM 33-51-06.
AIR INTERRUPT, DIVERTED, EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB AIRFRAME VIBRATION WAS NOTED ABOVE 250 KNOTS. UPON ARRIVAL, EXTERNAL POWER ACCESS DOOR WAS FOUND OPEN WITH HINGE CRACKED. HINGE TRIMMED & DOOR SECURED WITH SPEED TAPE IAW SRM 53-10-00-4 & FEA 18027. UPON ARRIVAL, R & R EXTERNAL POWER DOOR HINGE IAW AMM 52-49-02.
EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH PLACED LANDING GEAR LEVEL DOWN & RT MAIN GEAR GREEN LIGHT WAS NOT ILLUMINATED. REPLACED 2 LIGHT BULBS & RT GEAR GREEN LIGHT ILLUMINATED. GREEN INDICATOR LIGHTS FOR GEAR ALL NORMAL. PERFORMED VISUAL INSPECTION FOR GENERAL CONDITION ON BOTH MAIN & NLG. ACCOMPLISHED BITE ON PROXIMITY CONTROL UNIT WITH NO FAULTS FOUND IAW AMM 32-05-03.
WHEN PAINTERS REMOVED THE N DECAL THEY NOTED A DEEP SCRATCH HIDDEN UNDER THE DECAL AT STATION 917. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01-2R-3.
LIGHT CORROSION AROUND AFT LAVATORY VENT FROM BS 928 TO 930. INSTALLED DOUBLER.
CORROSION ON SKIN AT BS 928 BETWEEN LONGERONS 22 & 21 LT. INSTALLED DOUBLER.
CORROSION ON FS SKIN AT BS 928 BETWEEN LONGERONS 22 & 23 LT. INSTALLED DOUBLER.
TUL CREW REPORTED RT AFT OVERWING EMERGENCY EXIT DOOR LIGHT ILLUMINATED DURING DESCENT. FLIGHT LANDED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT FLIGHT LOCK SOLENOID ON THE RT AFT OVERWING EMERGENCY EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.
SEAT TRACK AT LEFT BUTTLINE 24.75 INBOARD AFT HOLE HAS CRACK INDICATION. REPAIRED SEAT TRACK PER EA B737-53-028811.
SEAT TRACK AT LEFT BUTTLINE 24.75 OUTBOARD AFT HOLE HAS CRACK INDICATION. REPAIRED SEAT TRACK PER EA B737-53-028811.
SEAT TRACK AT STATION 727B LEFT BUTTLINE 24.75 OUTBOARD FORWARD HOLE HAS CRACK INDICATION. REPAIRED SEAT TRACK PER EA B737-53-028811.
SEAT TRACK AT LEFT BUTTLINE 24.75 INBOARD FORWARD HOLE HAS CRACK INDICATION. REPAIRED SEAT TRACK PER EA B737-53-028811.
DFW - CREW REPORTED FLAP ASYMMETRY INDICATION. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP SLAT ELECTRONICS UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.
CORROSION IN AFT CARGO DOOR JAMB LOWER ENTRY WEB. REPLACED WEB PER AARD 51-10-05 AND BOEING DWG 146A8123.
FORWARD CARGO DOOR HAS NICK IN EDGE OF OUTER DOOR SKIN BELOW NUMBER 2 BEAM. INSTALLED A DOUBLER REPAIR TO OUTER SKIN FORWARD EDGE AT NUMBER 2 BEAM PER EA COMP-52-022492 AND SRM 52-00-01-2R 2.
FORWARD CARGO DOOR EXTERNAL SKIN HAS DEEP LONG SCRATCHES LOCATED BELOW HANDLE NUMBER 4. REMOVED SKIN AND INSTALLED NEW SKIN PER ESO 60654.
AFT CABIN WET AREA CORRODED AT RIGHT BUTTLINE 29 AND STATION 1016+2. INSTALLED REPAIR DOUBLER PER SRM 51-70-13-R1 AND 54-40-02 AND EA.
AFT CARGO DOOR EXTERNAL SKIN SURFACE HAS SHALLOW 1 INCH DENT ABOVE DOUBLE ROW OF RIVETS. REMOVED DAMAGED SKIN AND REPLACED WITH NEW SKIN PER ESO 60651.
FORWARD CARGO DOOR EXTERNAL SKIN HAS DEEP LONG SCRATCHES LOCATED BELOW HANDLE NUMBER 4. REMOVED DAMAGED OUTER SKIN AND INSTALLED A NEW OUTER SKIN PER ESO 60654.
RIGHT TRANSITION PANEL FROM STATIONS 767 TO 787 CORRODED. REPLACED TRANSITION PANEL PER AARD 51-10-05.
INTERIM REPAIR INSTALLED AT STATION 500D, STRINGER 22 RIGHT. REMOVED AND REPLACED DOUBLER PER EA B737-53-022403 AND SRM 53-00-01-2R-1.
FRAME CRACKED AT AIR CONDITIONING SUPPORT FITTING AT STATION 380.STRINGER 9 RIGHT. INSTALLED REPAIR ANGLE PER ECO J1159-0007.
E&E ACCESS DOORSKIN SCRATCHED AND SAND PITTED FORWARD TO AFT. REMOVED AND INSTALLED NEW SKIN PER EA COMP-52-022392.
CRACKED INTERCOSTAL AT STATIONS 312 TO 328 44 LEFT BUTTLINE. REPLACED INTERCOSTAL PER AARD 51-0-05-1.
CRACKED INTERCOSTAL AT STATIONS 312 TO 328, RIGHT BUTTLINE 32. REPLACED INTERCOSTAL PER AARD 51-0-05-1.
AUXILIARY POWER UNIT COMPARTMENT INLET CUTOUT AT STATION 1125, VERTICAL STIFFENER IS CORRODED. INSTALLED VERTICAL STIFFENER AT STATION 1125 INLET CUTOUT PER AARD 51-10-05 REPAIR 1 AND BOEING DRAWING 148A8650.
CARGO FLOOR SUPPORT FORWARD BAFFLE CLIP CRACKED AT LEFT TRANSITION PANEL AND STATION 500F. REPLACED BAFFLE CLIPS PER EA B737-53-022292.
CARGO FLOOR SUPPORT AFT AND FORWARD BAFFLE CLIPS CRACKED AT LEFT TRANSITION PANEL AND STATION 500G. REPLACED BAFFLE CLIPS PER EA B737-53-022292.
CARGO FLOOR SUPPORT AFT AND FORWARD BAFFLE CLIPS CRACKED AT RIGHT TRANSITION PANEL AND STATION 500H. REPLACED BAFFLE CLIPS PER EA B737-53-022292.
CARGO FLOOR SUPPORT AFT AND FORWARD BAFFLE CLIPS CRACKED AT RIGHT TRANSITION PANEL AND STATION 500G. REPLACED BAFFLE CLIPS PER EA B737-53-022292.
CARGO FLOOR SUPPORT AFT AND FORWARD BAFFLE CLIPS CRACKED AT LEFT TRANSITION PANEL AND STATION 500H. REPLACED BAFFLE CLIPS PER EA B737-53-022292.
AUXILIARY POWER UNIT COMPARTMENT, HORIZONTAL STIFFENER FROM STATIONS 1088 TO 1138 IS CORRODED AT INLET CUTOUT LOWER END. INSTALLED LOWER HORIZONTAL STIFFENER FROM STATIONS 1088 TO 1138 IN AUXILIARY POWER UNIT COMPARTMENT INLET CUTOUT PER AARD 51-10-05 REPAIR 1 AND BOEING DRAWING 148A8650.
CARGO FLOOR SUPPORT FORWARD BAFFLE CLIP CRACKED AT RIGHT TRANSITION PANEL AND STATION 500F. REPLACED BAFFLE CLIPS PER EA B737-53-022292.
VERTICAL FRAME AT STATION 291.5 HAS DOUBLE DRILLED HOLE ABOVE CREASE ANGLE. INSTALLED FREEZE PLUG PER EA.
EDDY CURRENT INSPECTION INDICATES A CRACK AT STATION 400 LEFT FRAME AT AIR CONDITIONING SUPPORT ATTACH FITTING. INSTALLED REPAIR DOUBLER/ANGLES A &AND B PER ECO J1159AD CARD 0006.
CABIN FLOOR INTERCOSTAL FROM STATIONS 328 TO 344 CRACKED AT CLIP NUT HOLES. REMOVED AND REPLACED INTERCOSTAL PER AARD 51-10-05 AND BOEING DRAWING 1415400.
FRAME CRACKED AT AIR CONDITIONING SUPPORT FITTING STATION 500A R. ACCOMPLISHED NESTED ANGLE REPAIR PER ESO J1159AD.
CABIN FLOOR INTERCOSTAL FROM STATION 277 TO 291.5 CRACKED AT BOTH CLIP NUT HOLES. REMOVED AND REPLACED INTERCOSTAL PER AARD 51-10-05 AND BOEING DRAWING 1415400.
FRAME CRACKED AT AIR CONDITIONING SUPPORT FITTING STATION 500C-R. ACCOMPLISHED NESTED ANGLE REPAIR PER ECO J1159AD-0007.
EDDY CURRENT INSPECTION INDICATES A CRACK AT STATION 380 LEFT AT AIR CONDITIONING SUPPORT ATTACH FITTING. INSTALLED REPAIR DOUBLER/ANGLES A AND B PER ECO J1159AD 0006.
CREASE ANGLE CORRODED AT FORWARD SERVICE DOOR THRESHOLD STATIONS 312 TO 328. INSTALLED NEW CREASE ANGLE PER AARD 51-10-05-1 AND BOEING DRAWING 141A8310.
EDDY CURRENT INSPECTION INDICATES A CRACK AT STATION 440 LEFT FRAME AT AIR CONDITIONING SUPPORT ATTACH FITTING. INSTALLED REPAIR DOUBLER/ANGLES A AND B PER ECO J1159AD 0006.
INTERIM DOUBLER REPAIR PERFORMED TO DENT WITH GOUGE BETWEEN AT STATIONS 887 TO 907 STRINGERS 22 AND 23 LEFT. PERMANENT REPAIR DOUBLER INSTALLED PER EA B737-55-022588.
BULKHEAD VAPOR BARRIER STIFFENER ANGLE CRACKED. REMOVED AND REPLACED STIFFENER ANGLE PER SRM 51-10-2, AARD 51-00-05-1 AND EA B737-57-018937.
CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK.
ORD - CREW REPORTED LEFT WING TO BODY OVERHEAT LIGHT ILLUMINATED WITH APU AND WING ANTI ICE OFF AT THE TIME. ACCOMPLISHED QRH PROCEDURES AND LIGHT WENT OFF AFTER LEFT PACK SHUT OFF. AFTER INITIAL DESCENT LIGHT CAME BACK ON AND WOULD NOT GO OUT. EMERGENCY DECLARED FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND PYLON STRUT WIRE BUNDLE SENSOR DAMAGED. REPLACED M1761 SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.
FRAME CRACKED AT AIR CONDITIONING SUPPORT FITTING STATION 727B-R. ACCOMPLISHED NESTED ANGLE REPAIR PER ECO J1159AD-0007.
FRAME CRACKED AT AIR CONDITIONING SUPPORT STATION 440 R. ACCOMPLISHED NESTED ANGLE REPAIR PER ECO J1159AD.
FRAME CRACKED AT AIR CONDITIONING SUPPORT FITTING STATION 480 R. ACCOMPLISHED NESTED REPAIR ANGLE PER ECO J1159AD.
RIGHT NUMBER 1 DOOR STUB FRAME CRACKED AT STATION 294 AT FLOOR LINE. INSTALLED REPAIR PER SRM 51-70-11.
RIGHT AFT OVERWING EXIT SIGN BROKEN AND MISSING LENS. REPLACED LIGHT ASSEMBLY FOR RIGHT AFT OVERWING EXIT SIGN. OPS CHECK NORMAL.
SKIN DAMAGED ON FORWARD CARGO DOOR. INSTALLED NEW SKIN ON FORWARD CARGO DOOR AS PER ESO 60654.
EMERGENCY LIGHT AT LEFT FORWARD SLIDE INOPERATIVE. REPLACED LAMP.
INTERCOSTAL AT STATION 312 TO 328 CRACKED. INSTALLED NEW INTERCOSTAL PER SRM 53-10-04.
IAD - INFLIGHT MIA-DCA. ANTI-SKID FAULT LIGHT ILLUMINATED AFTER GEAR RETRACTION ON TAKEOFF. EMERGENCY DECLARED, LANDED IAD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ANTI-SKID AUTO BRAKE CONTROLLER AND LEFT ALTERNATE CONTROL VALVE V125.
DFW - SEAT MOUNTED ESCAPE PATH LIGHTING AT SEAT 19D INOPERATIVE. REPAIRED BROKEN WIRE IN SIDEWALL.
DFW - SEAT MOUNTED ESCAPE PATH LIGHTING AT SEAT 10D INOPERATIVE. REPAIRED LOOSE CONNECTOR FOR SEAT MOUNTED ESCAPE PATH LIGHTING AT SEAT 10D.
TUL - EMERGENCY LIGHTS AT MID COACH CLASS INOPERATIVE. REPLACED BATTERY PACK AT SEAT 19A FOR EMERGENCY LIGHTS AT MID COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - EMERGENCY EXIT FLOOD LIGHT AT SEAT ROW 14A INOPERATIVE. RELAMPED EMERGENCY EXIT FLOOD LIGHT AT SEAT ROW 14A. SYSTEM GROUND CHECKED NORMAL OPERATION.
MIA - EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION.
MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.
MIA - EMERGENCY LIGHT AT SEAT 22D HAS MISSING LENS COVER. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.
MIA - EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION.
MIA - EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. REPINNED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION.
MIA - EMERGENCY LIGHT AT AFT LEFT OVERWING INOPERATIVE. REPLACED BATTERY PACK M1670 FOR EMERGENCY LIGHT AT AFT LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.
TUL BATTERY PACK FOR LEFT HAND EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT STATION NUMBER 575 FOR LEFT HAND EMERGENCY OVERWING EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)
DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEATS 13D AND 21D INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEATS 13D AND 21D. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - AFT SEAT MOUNTED EMERGENCY LIGHTS AT ROW 12 HAS ONE LAMP INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 17D HAS ONE LAMP INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION.
DFW - CABIN PRESSURIZATION PROBLEMS DURING CLIMB. REPEAT PROBLEM. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. LEFT HAND PACK WAS PLACARD INOPERATIVE DURING BOTH EVENTS. FOUND LOWER ELECTRICAL ACCESSORY COMPARTMENT (E&E COMPARTMENT) DOOR LEAKING. REPAIRED LOWER E AND E DOOR SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION.