Boeing 737-33A

Service difficulty reports · 1,809

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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 = '73733A'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR AWXA200500471Door Frame · crackedDURING C-19 CHECK A .3125 INCH CRACK WAS FOUND ON R-1 DOOR AFT FRAME AT 3RD DOOR STOP CUTOUT FROM BOTTOM BS 329, STR 12 RT. MAINTENANCE TRIMMED OUT DAMAGE R-1 DOOR AFT FRAME AT 3RD DOOR STOP CUTOUT FROM BOTTOM BS 329, STR 12 RT; FABRICATED A REPAIR DOUBLER; IApr 1, 2005 · N174AW · Boeing 73733A · Service DoorsSDR AWXA200500470Door Frame · crackedDURING C-19 CHECK A .375 INCH CRACK WAS FOUND ON R-1 DOOR AFT FRAME AT 4TH DOOR STOP FROM BOTTOM BS 344, STR 13 RT. MAINTENANCE TRIMMED OUT DAMAGE R-1 DOOR AFT FRAME AT 4TH DOOR STOP FROM BOTTOM BS 344, STR 13 RT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIRApr 1, 2005 · N174AW · Boeing 73733A · Service DoorsSDR AWXA200500378Wire · brokenPHX - EEL - DURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT PIN FOR CONNECTOR, RETERMINATED WIRE AT PIN AT SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD.Mar 30, 2005 · N174AW · Boeing 73733A · Light System WiringSDR AWXA200500361Switch · shortedPHX - ABORTED TAKEOFF - FLT 0506 - ON TAKEOFF AT PHX EN ROUTE TO YVR UPON ADVANCING THROTTLES AND BRAKE RELEASE THE TAKEOFF CONFIGURATION WARNING HORN SOUNDED, ALL EFFORTS TO SILENCE HORN FAILED. RETURNED TO GATE. MAINTENANCE FOUND STABILIZER NOSE UP SWITCH Mar 24, 2005 · N174AW · Boeing 73733A · Central WarningSDR AWXA200500363Circuit Breaker · defectiveLAS - ABORTED TAKEOFF - FLT 0399 - ON TAKEOFF AT LAS EN ROUTE FOR DFW THE TAKEOFF CONFIGURATION WARNING HORN SOUNDED COUNTINUOUSLY, RETURNED TO GATE. MAINTENANCE REMOVED EXCESSIVE GREASE AT SWITCHED S132 AND S546, REPLACED LEADING EDGE FLAP CIRCUIT BREAKER ASMar 2, 2005 · N174AW · Boeing 73733A · Central WarningSDR AWXA200500288Battery · dischargedSMF - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT WAS NOT BLINKING. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE FORWARD GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.Mar 2, 2005 · N166AW · Boeing 73733A · Emergency EquipmentSDR AWXA200500170Battery · dischargedMAINTENANCE FOUND THE AFT GALLEY OUTBOARD EMERGENCY FLASHLIGHT INOPERATIVE. MX REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT. OPERATIONAL CHECK WAS GOOD.Feb 6, 2005 · N164AW · Boeing 73733A · Emergency EquipmentSDR AWXA200500147Indicator · malfunctionedON FINAL APPROACH, WHILE CONFIGURING FOR LANDING, FLAPS BECAME SPLIT WITH LT FLAP AT 11 DEGREES & RT FLAP AT 15 DEGREES, A SLIGHT ROLL NOTED ON CONTROLS. LE SLATS ALL NORMAL WITH GREEN LIGHTS, DECLARED EMERGENCY & LANDED WITHOUT FURTHER EVENT. MX PERFORMED AFeb 2, 2005 · N173AW · Boeing 73733A · Trailing Flap Position Indicating SystemSDR AWXA200401358Light · inoperativeDFW - EEL - DURING A-01 CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD.Dec 6, 2004 · N174AW · Boeing 73733A · Emergency LightingSDR AWXA200401364Wedge · delaminatedMCN - MAJOR REPAIR - DURING 8-DAY CHECK ,THE LOWER SURFACE OF LT WING INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED 14" FROM OUTBOARD END, BETWEEN WBL 169 AND WBL 176. MAINTENANCE CUTOUT DAMAGED AREA OF LOWER SURFACE OF LT WING INBOARD MID FLAP TNov 28, 2004 · N164AW · Boeing 73733A · Trailing Edge FlapsSDR AWXA200401363Wedge · delaminatedMCN - MAJOR REPAIR - DURING 8-DAY CHECK A DISBOND AREA WAS FOUND ON LOWER SURFACE OF LT WING INBOARD MID FLAP TRAILING EDGE WEDGE 26" FROM OUTBOARD END, BETWEEN WBL 153 AND WBL 157. MAINTENANCE CUTOUT DAMAGED AREA OF LOWER SURFACE OF LT WING INBOARD MID FLAP Nov 28, 2004 · N164AW · Boeing 73733A · Trailing Edge FlapsSDR AWXA200401344Battery · dischargedPHX - EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE RED TEST LIGHT WAS NOT WORKING ON AFT CABIN EMERGENCY FLASHLIGHT, FLASHLIGHT WORKS BUT RED LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WASNov 28, 2004 · N173AW · Boeing 73733A · Emergency EquipmentSDR AWXA200401366Keelbeam · corrodedMCN - MAJOR REPAIR - DURING 8-DAY CHECK CORROSION WAS FOUND ON RT KEEL BEAM AT BS 540, STR 27 RT. MAINTENANCE CUTOUT DAMAGED AREA OF KEEL BEAM LOWER CHORD FROM BS 500A TO BS 540; FABRICATED A NEW REPLACEMENT SECTION OF KEEL BEAM CHORD, 3 EACH FILLERS, AND 2 ENov 22, 2004 · N164AW · Boeing 73733A · Fuselage Main, KeelSDR AWXA200401365Door Frame · crackedMCN - MAJOR REPAIR - DURING 8-DAY CHECK, A 1 1/2" CRACK WAS FOUND IN FORWARD EDGE OF FORWARD CARGO DOOR FRAME JUST BELOW CEILING HOOK, BS 460, STR 20 RT. MAINTENANCE REMOVED AND REPLACED FORWARD CARGO DOOR ASSEMBLY IAW T/C R8M52001.Nov 22, 2004 · N164AW · Boeing 73733A · Cargo/Baggage DoorsSDR AWXA200401362Connector · brokenDURING 8-DAY CHECK, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND INOPERATIVE. MAINTENANCE REPINNED WIRING IN CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT; OPERATIONAL CHECK WAS GOOD.Nov 22, 2004 · N164AW · Boeing 73733A · Light System WiringSDR AWXA200401319Flashlight · inoperativeLAS - EMERGENCY EQUIPMENT - DURING 4-DAY CHECK FOUND THE AFT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.Nov 22, 2004 · N175AW · Boeing 73733A · Emergency EquipmentSDR AWXA200401169Shear Tie · crackedDURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN FRAME FOOT CLIP AT BS 986, STR 25 RT. MAINTENANCE REMOVED AND REPLACED FRAME FOOT CLIP AT BS 986, STR 25 RT IAW SRM 51-40-02, FIG. 3, 4, 6, 7, AND 8.Oct 26, 2004 · N166AW · Boeing 73733A · Fuselage Main, StructureSDR AWXA200401192Wire Harness · brokenMCN - EEL - DURING C-18 CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT HARNESS DAMAGED IN SEVERAL LOCATIONS THROUGH OUT CABIN BETWEEN BS 340 AND BS 947. MAINTENANCE REPAIRED DAMAGE ON EMERGENCY ESCAPE PATH LIGHT HARNESS; OPERATIONAL CHECK WAS GOOD.Oct 23, 2004 · N168AW · Boeing 73733A · Light System WiringSDR AWXA200401175Seat Track · corrodedDURING C-18 CHECK, CORROSION WAS FOUND ON INBOARD FLANGE OF SEAT TRACK AT BS 480, RBL 45. MAINTENANCE CUTOUT DAMAGED SECTION OF SEAT TRACK FROM BS 334 TO BS 500 AT RBL 45; FABRICATED A NEW REPLACEMENT SEAT TRACK AND A FILLER; INSTALLED REPAIR PARTS IAW B737-3Oct 15, 2004 · N166AW · Boeing 73733A · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200401168Shear Tie · corrodedDURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD SIDE OF FRAME FOOT AT BS 480, BETWEEN STRINGERS 25 AND 26 LT. MAINTENANCE REMOVED SHEAR TIE, SUPPORT CLIP, AND DAMAGED SECTION OF FRAME AT BS 480, BETWEEN STRINGERS 25 AND 26 LT; FABRICATED A SHEAR TOct 15, 2004 · N166AW · Boeing 73733A · Fuselage Main, StructureSDR AWXA200401143Splice Plate · crackedDURING C-18 CHECK, A 5/16 INCH CRACK WAS FOUND IN SPLICE PLATE AT BS 348, BETWEEN STR 20 RT AND STR 21 RT. MAINTENANCE REMOVED CRACKED SPLICE PLATE AT BS 348, STR 20 - 21 RT; FABRICATED A NEW REPLACEMENT SPLICE PLATE PER DWG 65-45812; INSTALLED REPAIR PART IAOct 15, 2004 · N166AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200401142Shear Tie · crackedDURING C-18 CHECK, FOUND A 3/8 INCH CRACK IN SHEAR TIE AT BS 348, BETWEEN STR 20 RT AND STR 21 RT. MAINTENANCE REMOVED CRACKED SHEAR TIE AT BS 348, STR 20 - 21 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 65-45812; INSTALLED REPAIR PART IAW B737-300 SRMOct 15, 2004 · N166AW · Boeing 73733A · Fuselage Main, StructureSDR AWXA200401174Intercostal · crackedDURING C-18 CHECK, A 1 1/16 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 294, STR 7 L/H. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 294, STR 7 LEFT; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW ER 03-5311-04295-ES1.Oct 14, 2004 · N168AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200401172Stringer Clip · crackedDURING C-18 CHECK A .3750 INCH CRACK WAS FOUND IN STRINGER CLIP AT BS 294, STR 11 LT. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 294, STR 11 LT; FABRICATED A NEW REPLACEMENT CLIP; INSTALLED REPAIR PART IAW ER 03-5311-04295-ES1.Oct 14, 2004 · N168AW · Boeing 73733A · Fuselage Main, Attach FittingsSDR AWXA200401182Stringer Clip · crackedDURING C-18 CHECK, A 3/8 INCH CRACK WAS FOUND IN FRAME TO STRINGER ATTACH CLIP AT BS 348, STR 15 LT. MAINTENANCE REMOVED DAMAGED FRAME ATTACH CLIP AT BS 348, STR 15 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-16970; INSTALLED REPAIR PART IAW ER 03-5312-0Oct 11, 2004 · N166AW · Boeing 73733A · Fuselage Main, Attach FittingsSDR AWXA200401156Angle · crackedDURING C-18 CHECK, A 1/2 INCH CRACK WAS FOUND IN ANGLE AT LOWER FORWARD CORNER OF L-1 DOOR BS 315, STR 16 LT. MAINTENANCE REMOVED CRACKED ANGLE AT LOWER FORWARD CORNER OF L-1 DOOR BS 315, STR 16 LT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-49649; INSTALLOct 11, 2004 · N166AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200401147Fitting · corrodedDURING C-18 CHECK, CORROSION WAS FOUND ON RT MAIN LANDING GEAR (MLG) BEAM INBOARD STABILIZING AFT FITTING AT WBL 71.24. MAINTENANCE REMOVED AND REPLACED RT MLG BEAM INBOARD STABILIZING AFT FITTING IAW AMM 57-15-00, FIG 401-402.Oct 11, 2004 · N166AW · Boeing 73733A · Wing, Landing Gear Attach FittingsSDR AWXA200401183Stringer Clip · crackedDURING C-18 CHECK, A 5/16 INCH CRACK WAS FOUND IN FRAME TO STRINGER ATTACH CLIP AT BS 360, STR 11 LT. MAINTENANCE REMOVED DAMAGED FRAME ATTACH CLIP AT BS 360, STR 11 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-48985; INSTALLED REPAIR PART IAW ER 03-5312-Oct 8, 2004 · N166AW · Boeing 73733A · Fuselage Main, Attach FittingsSDR AWXA200401146Reveal · crackedDURING C-18 CHECK, A 3/4 INCH CRACK WAS FOUND IN R-1 DOOR CUTOUT AFT UPPER REVEAL BS 315 TO BS 328, STR 8 RT. MAINTENANCE REMOVED CRACKED R-1 DOOR CUTOUT AFT UPPER REVEAL; FABRICATED A NEW REPLACEMENT REVEAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FOct 7, 2004 · N166AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200401120Shear Web · crackedDURING C-18 CHECK A 2 INCH CRACK WAS FOUND IN RT SHEAR WEB FORWARD OF FRAME AT BS 580, STR 17. RT MAINTENANCE CUTOUT DAMAGE ON RT SHEAR WEB FROM BS 578 TO BS 597, STR 17 RT; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW SRM 51-70-13, FIG. Oct 7, 2004 · N166AW · Boeing 73733A · Fuselage Miscellaneous StructureSDR AWXA200401166Floorbeam · crackedDURING C-18 CHECK A 2 INCH CRACK WAS FOUND IN FLOORBEAM WEB AT BS 328, RBL 28, WL 208. MAINTENANCE CUTOUT DAMAGED AREA IN FLOORBEAM WEB AT BS 328, RBL 28; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW ER 03-5335-04295-RC1.Oct 5, 2004 · N166AW · Boeing 73733A · Fuselage Main, Floor BeamSDR AWXA200401159Skin · wornDURING C-18 CHECK, A WORN AREA WAS FOUND ON FUSELAGE SKIN WHERE VERTICAL FIN MEETS FUSELAGE AT BS 967, STR 2 LT. MAINTENANCE BLENDED DAMAGED SKIN AT BS 967, STR 2 LT; FABRICATED WEAR STRIPS PER DWG 65-45772; INSTALLED REPAIR PARTS IAW ER 03-5331-04293-RA2.Oct 5, 2004 · N166AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA200401153Seat Track · crackedDURING C-18 CHECK, A 3/8 INCH CRACK WAS FOUND IN LT INBOARD SEAT TRACK BEAM AT BS 727B, LBL 24.75. MAINTENANCE TRIMMED OUT CRACK IN LT INBOARD SEAT TRACK BEAM AT BS 727B, LBL 24.75; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED Oct 5, 2004 · N168AW · Boeing 73733A · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200401150Skin · wornDURING C-18 CHECK, A WORN AREA WAS FOUND ON DOUBLER (SKIN) WHERE VERTICAL FIN MEETS FUSELAGE BETWEEN BS 867 AND BS 887, STR 1 RT AND STR 2 RT. MAINTENANCE REMOVED WORN DOUBLER FROM BS 867 TO BS 887, STR 1 RT TO STR 2 RT; FABRICATED A NEW REPLACEMENT DOUBLER POct 5, 2004 · N166AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA200401144Stringer · corrodedDURING C-18 CHECK, CORROSION WAS FOUND ON SIDE OF STRINGER 28 RT, BETWEEN BS 312 AND BS 322. MAINTENANCE CUTOUT DAMAGED SECTION OF STRINGER 28 RT, FROM BS 312 TO BS 322; FABRICATED A REPAIR ANGLE AND CHANNEL; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03, Oct 5, 2004 · N166AW · Boeing 73733A · Fuselage Main, Longeron/StringerSDR AWXA200401199Frame · crackedDURING C-18 CHECK, A 1 1/8 INCH CRACK WAS FOUND IN UPPER FLANGE OF FRAME AT BS 344 ABOVE AND OUTBOARD OF STR 23 LT. MAINTENANCE CUTOUT DAMAGED SECTION OF FRAME FLANGE AT BS 344, FROM STR 22 LT TO STR 23 LT; FABRICATED A CHANNEL REPAIR DOUBLER; INSTALLED REPAOct 4, 2004 · N168AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA200401137Skin · crackedDURING C-18 CHECK, 2 EACH 3/4 INCH CRACKS WERE FOUND IN LOWER SKIN OF NR 1 SLAT BELOW OUTBOARD MAIN TRACK SLAT STA 355 - 357. MAINTENANCE CUTOUT DAMAGE IN NR 1 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-4Oct 4, 2004 · N168AW · Boeing 73733A · Leading Edge DevicesSDR AWXA200401127Shear Tie · crackedDURING C-18 CHECK, A 3/8 INCH CRACK WAS FOUND IN SHEAR TIE (CLIP) AT BS 294, STR 11 LT. MAINTENANCE REMOVED CRACKED CLIP AT BS 294, STR 11 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 66-14210; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12.Oct 4, 2004 · N168AW · Boeing 73733A · Fuselage Main, StructureSDR AWXA200401126Frame · crackedDURING C-18 CHECK, A 1 INCH CRACK WAS FOUND IN FRAME AT BS 294, STR 7 LT. MAINTENANCE REMOVED CRACKED FRAME AT BS 294, STR 7 LT; FABRICATED A NEW REPLACEMENT SECTION OF WEB PER DWG 65-17684; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12.Oct 4, 2004 · N168AW · Boeing 73733A · Fuselage Main, FrameSDR AWXA200401185Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 4 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 500C+5, STR 10 RT JUST ABOVE LAP SEAM. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN AT BS 500C+5, STR 10 RT AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICAOct 3, 2004 · N166AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA200401173Stringer · corrodedDURING C-18 CHECK, CORROSION WAS FOUND ON STRINGER 27 LEFT AT BS 987. MAINTENANCE REMOVED CORRODED SECTION OF STRINGER 27 LT FROM BS 967 TO BS 1006; FABRICATED A NEW REPLACEMENT STRINGER PER DWG 65-45776; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3Oct 3, 2004 · N166AW · Boeing 73733A · Fuselage Main, Longeron/StringerSDR AWXA200401171Shear Tie · corrodedDURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON SHEAR TIE AT BS 987, BETWEEN STR 26 RT AND STR 27 RT IN THE AFT CARGO COMPARTMENT. MAINTENANCE REMOVED CORRODED SHEAR TIE AT BS 987, BETWEEN STR 26 RT AND STR 27 RT; FABRICATED A NEW REPLACEMENT SHEAR TIEOct 3, 2004 · N166AW · Boeing 73733A · Fuselage Main, StructureSDR AWXA200401154Skin · crackedDURING C-18 CHECK, A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN JUST ABOVE LAP SEAM AT BS 500D+10, STR 10 RT. MAINTENANCE CUTOUT CRACK IN FUSELAGE SKIN AT BS 500D+10, STR 10 RT; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED 2 EACH Oct 3, 2004 · N166AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA200401138Skin · crackedDURING C-18 CHECK, A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN JUST ABOVE LAP SEAM AT BS 465, STR 10 RT. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN AT BS 465, STR 10 RT; FABRICATED 2 EACH FILLERS AND A DOUBLER; INSTALLED REPAIR PARTS IAW EO 5330-01003.Oct 3, 2004 · N166AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA200401191Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .0625 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 518, STR 12 LT. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN AT BS 518, STR 12 LT; FABRICATED A DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW ER 03-5300-04301-ES1.Oct 2, 2004 · N168AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA200401189Skin · crackedDURING C-18 CHECK, A 1/16 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 500C+5, STR 10 LEFT. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN AT BS 500C+5, STR 10 LT AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS, A DOUBLER AND TOct 2, 2004 · N168AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR AWXA200401181Beam · crackedDURING C-18 CHECK, A 3/8 INCH CRACK WAS FOUND ON LOWER FORWARD CORNER OF L-1 DOOR AT LOWER GATE BEAM WEB, BS 314, STR 16 LT. MAINTENANCE CUTOUT DAMAGE IN LOWER GATE BEAM WEB OF L-1 DOOR; FABRICATED A REPAIR DOUBLER AND FILLERS; INSTALLED REPAIR PARTS IAW B737-Oct 2, 2004 · N168AW · Boeing 73733A · Passenger/Crew DoorsSDR AWXA200401170Skin · crackedDURING C-18 CHECK 11 EACH CRACKS WERE FOUND IN NR 3 SLAT LOWER SKIN BETWEEN SLAT STA. 51.75 AND 74.65 LT. MAINTENANCE CUTOUT DAMAGED SECTION OF NR 3 SLAT LOWER SKIN FROM S.S. 51.75 LT TO S.S. 74.65 LT; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR POct 2, 2004 · N166AW · Boeing 73733A · Trailing Edge FlapsSDR AWXA200401165Stringer · corrodedDURING C-18 CHECK CORROSION WAS FOUND ON IB SIDE OF STRINGER 27 RT, BETWEEN BS 986 AND BS 1006. MAINTENANCE CUTOUT DAMAGE ON STRINGER 27 RT FROM BS 986 TO BS 1006; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER AND A SPLICE REPAIR; INSTALLED REPAIR PARTS IAOct 2, 2004 · N166AW · Boeing 73733A · Fuselage Main, Longeron/StringerSDR AWXA200401164Angle · corrodedDURING C-18 CHECK CORROSION WAS FOUND ON HORIZONTAL WEB ATTACH ANGLE AT BS 294, LBL 4, WL 208. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOORBEAM UPPER TEE CAP AT BS 294, FROM LBL 25 TO RBL 55; FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 2 EACH REPAIR ANGLESOct 2, 2004 · N166AW · Boeing 73733A · Fuselage, Stabilizer Attach Fittings
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