Boeing 737-277

Service difficulty reports · 1,584

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '737277'
  ORDER BY difficulty_date DESC"

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SDR AWXA200300988Gusset · crackedDURING C-16 CHECK A 2 INCH CRACK WAS FOUND IN RADIUS OF NOSE LANDING GEAR ACTUATOR MOUNT FITTING ATTACH ANGLE. MAINTENANCE REMOVED AND REPLACED DAMAGED NOSE LANDING GEAR ACTUATOR MOUNT FITTING ATTACH ANGLE IAW B737-200 SRM 51-30-02, PG. 1, FIG. 007, & SRM 51-3Aug 13, 2003 · N186AW · Boeing 737277 · Fuselage, Landing Gear Attach FittingsSDR AWXA200300986Bracket · crackedDURING C-16 CHECK A 3/16 INCH CRACK WAS FOUND ON NR 2 SLAT INBOARD AUXILIARY TRACK CLOSE-OUT DOOR AFT SPRING ATTACH BRACKET AT WS 404.8. MAINTENANCE REMOVED AND REPLACED THE CRACKED NR 2 SLAT INBOARD AUXILIARY TRACK CLOSEOUT DOOR AFT SPRING ATTACH BRACKET AT WAug 13, 2003 · N186AW · Boeing 737277 · Trailing Edge FlapsSDR AWXA200301051Angle · crackedDURING C-16 CHECK A 1 1/8 INCH CRACK WAS FOUND ON NR 1 ENGINE RT FORWARD COWL LOWER ZEE ANGLE AT RIB 7, NAC STA 151. MAINTENANCE CUTOUT CRACK ON RIB 7; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-200 SRM 54-40-03, FIG. 001.Aug 12, 2003 · N186AW · Boeing 737277 · Nacelle/Pylon, Main FrameSDR AWXA200301042Floorbeam · crackedDURING C-16 CHECK A .5625 INCH CRACK WAS FOUND ON FLOORBEAM REPAIR BS 677, RBL 24. MAINTENANCE REMOVED REPAIR ANGLE AND 2 EACH DOUBLERS; FABRICATED A NEW REPLACEMENT REPAIR CHANNEL AND 3 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 15-5715-03240-ES2.Aug 12, 2003 · N186AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200301021Floorbeam · crackedDURING C-16 CHECK .875 INCH CRACK WAS FOUND ON PASSENGER CABIN FLOORBEAM AT BS 644, LBL 45. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM AT BS 694, LBL 45; FABRICATED A FILLER AND 3 EACH REPAIR PLATES; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-04 FIG 1 PG 1.Aug 12, 2003 · N186AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200301020Floorbeam · crackedDURING C-16 CHECK 2 EACH 1.25 INCH CRACKS WERE FOUND ON PASSENGER CABIN FLOORBEAM AT BS 674, RBL 45. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM AT BS 674, RBL 45; FABRICATED A REPAIR EXTRUSION AND 3 EACH REPAIR PLATES; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-Aug 12, 2003 · N186AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200301043Skin · crackedDURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON NR 2 ENGINE LT FORWARD COWL INNER SKIN UNDER UPPER FORWARD SAFETY LATCH. MAINTENANCE CUTOUT CRACKED SKIN ON NR 2 ENGINE LT FORWARD COWL INNER SKIN NAC STA 120 RT; FABRICATED A DOUBLER, SHIM AND FILLER; INSTALLED REAug 11, 2003 · N186AW · Boeing 737277 · Nacelle/Pylon, Plate/SkinSDR AWXA200301029Flap · debondedDURING C-16 CHECK THE UPPER SURFACE OF THE RT INBOARD FORE-FLAP WAS FOUND DISBONDING 33 INCH TO 37 INCH FROM THE OUTBOARD END. MAINTENANCE PERFORMED HONEYCOMB CORE REPAIR ON RT INBOARD FORE-FLAP IAW B737-200 SRM 51-40-20, REPAIR NR 9, FIG. 18, PG. 63-67.Aug 11, 2003 · N186AW · Boeing 737277 · Trailing Edge FlapsSDR AWXA200300908Battery · dischargedPHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD LOWER CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN THE FORWARD LOWER CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.Aug 11, 2003 · N180AW · Boeing 737277 · Emergency EquipmentSDR AWXA200300877Roller · out of adjustLAX - FLIGHT CONTROL - FLT 0102 - ON TAKEOFF AT LAS EN ROUTE FOR LAX AT FLAP 1 THE AIRCRAFT HAD TENDENCY TO ROLL RIGHT, 20 DEGREES LEFT AILERON NEEDED TO HOLD WINGS LEVEL. AFTER FLAPS WERE RETRACTED ROLL TO THE RIGHT STOPPED. ON APPROCH INTO LAX AT FLAP 1 AND Aug 5, 2003 · N188AW · Boeing 737277 · Leading Edge DevicesSDR AWXA200300812Bleed Valve · malfunctionedDEN - ABORTED TAKEOFF - FLT 0640 - DURING TAKEOFF ROLL AT DEN EN ROUTE FOR PHX, A LOUD "BANG" CAME FROM THE NR 1 ENGINE, REJECTED TAKEOFF, SUSPECT COMPRESSOR STALL. MAINTENANCE PERFORMED A BORESCOPE INSPECTION IAW T/C I5M72008, NO DAMAGE NOTED. REMOVED AND REPJul 18, 2003 · N182AW · Boeing 737277 · Compressor Bleed ValveSDR AWXA200300772Circuit Breaker · weakEN ROUTE FROM AUS TO PHX ALL EMERGENCY EXIT LIGHTS ILLUMINATED. EMERGENCY EXIT LIGHT WAS SWITCHED OFF TO CONSERVE BATTERY ENERGY. MAINTENANCE FOUND A WEAK EMERGENCY LIGHT SYSTEM CONTROL CIRCUIT BREAKER (5 AMP) ON THE P-18 PANEL. REMOVED AND REPLACED 5 AMP CJul 2, 2003 · N178AW · Boeing 737277 · Light System WiringSDR AWXA200300721Pump · failedON DEPARTURE, LOST A-SYSTEM HYDRAULIC PRESSURE, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. AIRCRAFT TOWED BACK TO GATE. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP HAD FAILED, REMOVED AND REPLACED PUMP. A-SYSTEM HYDRAULICS FLUSHED, OPERATIONAL Jun 20, 2003 · N184AW · Boeing 737277 · Hydraulic Pump (Electric/Engine), MainSDR AWXA200300689Light · defectiveLAS - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD.Jun 11, 2003 · N186AW · Boeing 737277 · Emergency LightingSDR AWXA200300622Circuit Breaker · intermittentEN ROUTE FROM AUS TO PHX THE EMERGENCY EXIT LIGHTS CAME ON WITH THE SWITCH IN ARMED POSITION, TURNED SWITCH OFF TO CONSERVE BATTERIES. MAINTENANCE TROUBLESHOT AND FOUND THE EMERGENCY EXIT LIGHT POWER CIRCUIT BREAKER (C250) WAS INTERMITTENT. REMOVED AND REPLAMay 29, 2003 · N189AW · Boeing 737277 · Emergency LightingSDR AWXA200300605Battery · dischargedDURING 8-DAY CHECK THE EMERGENCY EXIT LIGHT ABOVE THE R-2 DOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AT EMERGENCY EXIT LIGHT ABOVE THE R-2 DOOR, OPERATIONAL CHECK WAS GOOD.May 28, 2003 · N186AW · Boeing 737277 · Emergency LightingSDR AWXA200300606Light · brokenFLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD.May 27, 2003 · N179AW · Boeing 737277 · Emergency LightingSDR AWXA200300575Wire · brokenDURING INSPECTION MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 14 AND 19 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 14 LT, AND REPAIRED A BROKEN WIRE AT SEAT ROW 19 LT. OPERATIONAL CMay 21, 2003 · N183AW · Boeing 737277 · Light System WiringSDR AWXA200300550Transmitter · malfunctionedPHX - ABORTED TAKEOFF - FLT 0445 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR TUS, SETTING REDUCED FOR POWER 1.96, NR 2 ENGINE EPR DID NOT COME UP TO POWER, EPR STAGNATED AT 1.45 EPR WHILE THRUST LEVER ADVANCED. REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TRMay 16, 2003 · N182AW · Boeing 737277 · Engine Pressure Ratio (EPR)SDR AWXA200300687Skin · corrodedDURING C-15 CHECK CORROSION WAS FOUND ON LT WING LOWER SURFACE SKIN AT NR 2 FLAP TRACK ATTACH POINT. MAINTENANCE REMOVED CORROSION ON LT WING LOWER SURFACE SKIN BY MACHINING A FLAT STEP; PERFORMED A HFEC INSPECTION TO VERIFY MACHINED AREA WAS NOT CRACKED; FABMay 15, 2003 · N178AW · Boeing 737277 · Wing, Plate/SkinSDR AWXA200300683Skin · crackedDURING C-15 CHECK A .375 INCH CRACK WAS FOUND AT FASTENER HOLE ON FUSELAGE SKIN, LOWER FORWARD CORNER OF R-1 DOOR CUTOUT BS 294.5. MAINTENANCE REMOVED FASTENER AT LOWER FORWARD CORNER OF R-1 DOOR CUTOUT BS 294.5; PERFORMED NDT INSPECTION TO VERIFY CRACK CONTAMay 15, 2003 · N178AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA200300686Skin · delaminatedDURING C-15 CHECK THE RT OUTBOARD HINGED FLAP TRAILING EDGE WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGE AND PERFORMED COMPOSITE REPAIR IAW BAC5514-589/5101 AND DWG 65-71930.May 14, 2003 · N178AW · Boeing 737277 · Trailing Edge FlapsSDR AWXA200300685Door Frame · crackedDURING C-15 CHECK A .25 INCH CRACK WAS FOUND ON FRAME OF R-1 DOOR AT UPPER HINGE CUTOUT. MAINTENANCE PERFORMED A HFEC INSPECTION TO VERIFY END OF CRACK; STOP DRILLED CRACK IAW B737-200 SRM 52-00-2 FIG 7 PG 32.May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, StructureSDR AWXA200300684Skin · corrodedDURING C-15 CHECK CORROSION WAS FOUND ON LOWER FUSELAGE SKIN AT BS 727-727A AND LT KEEL BEAM. MAINTENANCE REMOVED EXISTING DOUBLER & TRIPLER AND TRIMMED OUT CORRODED SKIN; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPLACEMENT DOUBLERMay 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA200300682Stringer · corrodedDURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 RT LOWER LOBE AT BS 907. MAINTENANCE REMOVED CORRODED STRINGER SPLICE AND TRIMMED AWAY CORROSION ON STRINGER 27 RT, BS 907; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-45895-3 AND A May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA200300649Frame · crackedDURING C-15 CHECK A .5000 INCH CRACK WAS FOUND ON FUSELAGE LOWER LOBE FRAME AT BS 827, LBL 22. MAINTENANCE TRIMMED OUT DAMAGE ON FUSELAGE LOWER LOBE FRAME AT BS 827, LBL 22, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED FILLER, RADIUS FMay 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA200300638Floorbeam · crackedYVR - MAJOR REPAIR - DURING C-15 CHECK A .25 INCH CRACK WAS ON FLOORBEAM WEB ANGLE AT BS 639, LBL 45.50. MAINTENANCE REMOVED DAMAGED FLOORBEAM WEB ANGLE AT BS 639, LBL 45.50; FABRICATED A NEW REPLACEMENT ANGLE AND STRAP; INSTALLED REPAIR PARTS IAW SB 737-53-1May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200300637Frame · crackedYVR - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND ON R-1 DOOR FRAME AT AFT NR 4 STOP FITTING CUTOUT. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC TO VERIFY CRACK WAS CONTAINED, ALODINED AND PRIMED IAW B737-200 SRM 51-10-2 PG 7.May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA200300636Skin · crackedYVR - MAJOR REPAIR - DURING C-15 CHECK A .25 INCH CRACK WAS FOUND AT L-1 DOOR ON THE AFT EDGE OF THE CENTER DOOR STOP ACCESS HOLE. MAINTENANCE STOP DRILLED CRACK AND PERFORMED HFEC TO VERIFY CRACK WAS CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PMay 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA200300608Floorbeam · crackedDURING C-15 CHECK A 2 INCH CRACK WAS FOUND ON TRANSVERSE FLOORBEAM WEB OUTBOARD OF LBL 45.50, BS 639. MAINTENANCE REMOVED DAMAGED ON WEB AT LBL 45.50, BS 639; FABRICATED REPAIR DOUBLERS AND A STRAP PER SB 737-53-1061 R4; INSTALLED REPAIR PARTS IAW E.R. 15-5300May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200300602Floorbeam · crackedDURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND ON FLOORBEAM WEB AT BS 639, RBL 45-50. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM; FABRICATED A FILLER, DOUBLER, AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-200 SRM 51-40-2, FIG. 1, PG. 1.May 14, 2003 · N178AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200300648Floorbeam · crackedYVR - MAJOR REPAIR - DURING C-15 CHECK 2 EACH 1INCH CRACKS WERE FOUND ON FLOORBEAM STRUCTURE AT AFT END OF AILERON TOWER SHAFT QUADRANT CUTOUT BS 676, LBL 24.5. MAINTENANCE REMOVED ANGLE AND STIFFENER AT BS 676, RBL 24.5; FABRICATED DOUBLERS; INSTALLED REPAIR May 13, 2003 · N178AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200300647Floorbeam · crackedDURING C-15 CHECK 2 EACH 1 INCH CRACKS WERE FOUND ON FLOOR BEAM UPPER STRUCTURE AT AFT END OF AILERON QUADRANT CUTOUT BS 676, RBL 24.5. MAINTENANCE CUTOUT DAMAGE ON FLOORBEAM UPPER STRUCTURE BS 676, RBL 24.5; FABRICATED 3 EACH DOUBLERS; INSTALLED REPAIR PARTMay 13, 2003 · N178AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA200300646Frame · crackedDURING C-15 CHECK A 1 INCH CRACK WAS FOUND ON MAIN WHEEL WELL UPPER COMPRESSION FRAME AT BS 663, RBL 24.5. MAINTENANCE REMOVED VERTICAL STIFFENER, WEB DOUBLER, VERTICAL ANGLE, AND FORWARD AND AFT STIFFENER BRACKETS TO FACILITATE REPAIR; CUT AND TRIMMED DAMAGEMay 13, 2003 · N178AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA200300645Panel · delaminatedDURING C-15 CHECK THE NO. 5 SPOILER WAS FOUND DELAMINATED AT THE INBOARD AFT EDGE. MAINTENANCE REMOVED AND REPLACED THE NO.5 SPOILER PANEL IAW BMM 27-62-12, PG. 401.May 13, 2003 · N178AW · Boeing 737277 · SpoilersSDR AWXA200300644Web · crackedDURING C-15 CHECK A .7500 INCH CRACK WAS FOUND ON FUSELAGE INTERIOR SHEAR WEB BELOW THE RT EMERGENCY ESCAPE HATCH CUTOUT. MAINTENANCE REMOVED DAMAGED SHEAR WEB BELOW THE RT EMERGENCY ESCAPE HATCH CUTOUT BS 616 TO BS 639, STR 27 RT; FABRICATED A NEW REPLACEMENTMay 13, 2003 · N178AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA200300643Frame · crackedDURING C-15 CHECK A .5000 INCH CRACK WAS FOUND ON RADIUS OF SIDE FRAME AT BS 597, LBL 70. MAINTENANCE TRIMMED OUT DAMAGE AT BEND OF THE FLANGE ON SIDE FRAME AT BS 597, LBL 70; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR ANGLE ANMay 13, 2003 · N178AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA200300642Frame · crackedYVR - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND ON MAIN WHEEL WELL COMPRESSION CHORD AT BS 663, LBL 24.5. MAINTENANCE REMOVED WEB STIFFENER, FLOOR BEAM FITTING, AND 2 EACH ANGLE STIFFENERS TO FACILITATE REPAIR; REMOVED DAMAGED PORTION OF UPPEMay 13, 2003 · N178AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA200300634Panel · delaminatedYVR - FLIGHT CONTROL - DURING C-15 CHECK THE NO. 8 SPOILER WAS FOUND DELAMINATED AT THE MID CENTER AFT EDGE. MAINTENANCE REMOVED AND REPLACED THE NR 8 SPOILER PANEL IAW BMM 27-62-91, PG. 401.May 13, 2003 · N178AW · Boeing 737277 · SpoilersSDR AWXA200300633Skin · delaminatedDURING C-15 CHECK THE NR 3 SLAT INBOARD END UPPER SKIN WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 3 SLAT IAW AWA T/C R3M27002.May 13, 2003 · N178AW · Boeing 737277 · Leading Edge DevicesSDR AWXA200300632Slat · delaminatedDURING C-15 CHECK THE NR 5 SLAT OUTBOARD TRAILING EDGE WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 5 SLAT IAW AWA T/C R3M27008.May 13, 2003 · N178AW · Boeing 737277 · Leading Edge DevicesSDR AWXA200300630Charger · inoperativeDURING C-15 CHECK EMERGENCY LIGHT BATTERY CHARGER M1051 LOCATED IN AFT AISLE CEILING HAS NO OUTPUT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER M1051, OPERATIONAL CHECK WAS GOOD IAW AWA T/C A1C33005.May 13, 2003 · N178AW · Boeing 737277 · Emergency LightingSDR AWXA200300609Frame · crackedYVR - MAJOR REPAIR - DURING C-15 CHECK A .25 INCH CRACK WAS FOUND ON LT FUSELAGE FRAME AT BS 639. MAINTENANCE REMOVED DAMAGED SECTION OF LT FUSELAGE FRAME AT BS 639; FABRICATED SPLICE REPAIR AND NEW SECTION PER S/B 737-53-1061, INSTALLED REPAIR PARTS IAW ER 1May 13, 2003 · N178AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA200300604Web · crackedYVR - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND AT RIVET HOLE ON INTERNAL FUSELAGE CENTER WEB BS 706, BL 0. MAINTENANCE REMOVED CRACKED AREA OF CENTER WEB BS 706, BL 0; FABRICATED A NEW REPLACEMENT SECTION OF WEB AND FILLER PLATES; INSTALLED REMay 13, 2003 · N178AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA200300603Angle · crackedDURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND ON CENTER SECTION ANGLE BS 663, LBL 60. MAINTENANCE REMOVED CRACKED ANGLE AT BS 663, LBL 60; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-37422; INSTALLED REPAIR PART IAW B737-200 SRM 51-10-2, PG. 8.May 13, 2003 · N178AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA200300533Battery · defectivePHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT CIRCUIT BREAKER WAS FOUND POPPED. MAINTENANCE RESET EMERGENCY EXIT LIGHT CIRCUIT BREAKER AND REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD.May 13, 2003 · N189AW · Boeing 737277 · Emergency LightingSDR AWXA200300532Light · inoperativePHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD.May 13, 2003 · N179AW · Boeing 737277 · Emergency LightingSDR AWXA200300678Web · crackedDURING C-15 CHECK A .5 INCH CRACK WAS FOUND ON SHEAR BEAM WEB OF STR 18A LT, AFT OF BS 706 FRAME TRUNNION BEAM SUPPORT FITTING IN FORWARD OUTBOARD CORNER. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATEDMay 7, 2003 · N178AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA200300501Angle · crackedYVR - MAJOR REPAIR - DURING C-15 CHECK A 1" CRACK WAS FOUND ON VERTICAL ATTACH ANGLE BELOW CABIN FLOOR SEAT TRACK AT LBL 24.75, BS 663.75. MAINTENANCE CUTOUT DAMAGED SECTION OF CHORD AT LBL 24.75, BS 663.75; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRAApr 29, 2003 · N188AW · Boeing 737277 · Fuselage Internal Mounting StructureSDR AWXA200300500Angle · crackedDURING C-15 CHECK A 1 1/2 INCHES CRACK WAS FOUND ON VERTICAL ATTACH ANGLE BELOW CABIN SEAT TRACK AT RBL 24.75, BS 663.75. MAINTENANCE CUTOUT DAMAGED SECTION OF CHORD AT RBL 24.75, BS 663.75; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICApr 29, 2003 · N188AW · Boeing 737277 · Fuselage Internal Mounting Structure
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