N324AW

Service difficulty reports not matched to an aircraft · 150

They name N324AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.

Query with SQL
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 n_number = 'N324AW' AND registry_match IS NULL
  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 AWXA200500978Tab · debondedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON UPPER SURFACE OF THE L/H AILERON TAB AT OUTBOARD END. MAINTENANCE REMOVED DISBONDED SKIN ON UPPER SURFACE OF THE L/H AILERON TAB AT THE OUTBOARD END IAW BOEING 737-300 SRM 51-70-07-0. BONDED FIJul 22, 2005 · N324AW · Boeing 737301 · Aileron TabsSDR AWXA200500668Sign · inoperativePHX - EEL - DURING 4 DAY CHECK, FOUND EMERGENCY EXIT SIGN AT FOWARD LOWER CORNER OF L1 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CK GOOD .Jun 7, 2005 · N324AW · Boeing 737301 · Emergency LightingSDR AWXA200500661Connector · damagedDURING C-19 CHECK, FOUND ESCAPE PATH LIGHTING HARNESS DAMAGED AT CONNECTORS AND SPLICES FROM BS 360 TO BS 947 AT LBL 26. MAINTENANCE REMOVED DAMAGED CONNECTORS AND SPLICES FROM BS 360 TO BS 947 AT LBL 26. REPLACED CONNECTORS AND SPLICES FROM BS 360 TO BS 947May 26, 2005 · N324AW · Boeing 737301 · Emergency LightingSDR AWXA200500646Intercostal · crackedMCN - MAJOR REPAIR - DURING C-19 CHEC, INTERCOSTAL FOUND CRACKED AT BODY STATION (BS) 500D THROUGH BS 520. MAINTENANCE REMOVED TOP OF INTERCOSTAL AT BS 500D-520 AND FABRICATED ATTACH ANGLE FOR TOP OF INTERCOSTAL IAW BOEING SRM 51-40-02. INSTALLED FABRICATED May 25, 2005 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500649Tab · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK, LT AILERON TAB WAS FOUND TO BE SEPARATED ALONG THE AFT EDGE NEAR THE OUTBOARD END. MAINTENANCE REMOVED ALL CONTAMINANTS AND WATER FROM DAMAGED AREA AND REPAIRED LT AILERON TAB IAW BOEING 737-300 SRM 51-70-06-0 FIG 13.May 23, 2005 · N324AW · Boeing 737301 · Aileron TabsSDR AWXA200500652Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK, 4 CRACKS EACH .3 INCH IN LENGTH FOUND ON BOTTOM OF NR 2 SLAT SKIN BELOW OUTBOARD MAIN TRACK AT SLAT STATION 228 TO SLAT STATION 232. MAINTENANCE CUT OUT AND REMOVED CRACKED SECTION OF NR 2 SLAT SKIN. FABRICATED FILLER May 22, 2005 · N324AW · Boeing 737301 · Leading Edge DevicesSDR AWXA200500651Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK, 3 CRACKS, .3' IN LENGTH EACH, FOUND ON BOTTOM NR 1 SLAT SKIN. MAINTENANCE REMOVED PREVIOUS REPAIR AND CRACKED SECTION ON NR 1 SLAT. FABRICATED FILLER AND SPLICE PLATE. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 737-May 22, 2005 · N324AW · Boeing 737301 · Leading Edge DevicesSDR AWXA200500650Wedge · debondedDURING C-19 CHECK, NR 2 SLAT WEDGE WAS FOUND TO BE DISBONDED ON TOP AND BOTTOM AT SLAT STATION 168. MAINTENANCE REMOVED DISBONDED SKIN AND CORE FROM TOP AND BOTTOM OF SLAT WEDGE. FABRICATED REPAIR CORE AND DOUBLER. BONDED REPAIR PIECES TO NR 2 SLAT WEDGE IAMay 22, 2005 · N324AW · Boeing 737301 · Leading Edge DevicesSDR AWXA200500660Channel · crackedDURING C-19 CHECK, FOUND ONE CRACK 1.1 INCH LONG ON CHANNEL LOCATED AT BS 328, LEFT BL 54, WL 208. MAINTENANCE REMOVED CRACKED CHANNEL AT BS 328, LEFT BL 54, WL 208. FABRICATED AND INSTALLED NEW CHANNEL AT BS 328, LEFT BL 54, WL 208 IAW BOEING DWG 65-45834 May 21, 2005 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200500647Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19, LT INBOARD MID FLAP TRAILING EDGE PANEL 7220 WAS FOUND DELAMINATED AT UPPER AND LOWER SURFACES, APPROX 39 INCHES FROM OUTBOARD EDGE. MAINTENANCE CUT OUT DELAMINATED SKIN AND CORE ON LT INBD MIDFLAP TRL EDGE PANEL UPPER AND LOMay 21, 2005 · N324AW · Boeing 737301 · Trailing Edge FlapsSDR AWXA200500645Structure · delaminatedDURING C-19 CHECK, THE RT OUTBOARD FLAP INBOARD LOWER CORNER WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGE ON RT OUTBOARD FLAP INBOARD LOWER CORNER, FABRICATED REPAIR CORE AND EXTERNAL DOUBLER, BONDED REPAIR PARTS TO FLAP IAW BOEING SRM 51-70-10 FIG 16.May 21, 2005 · N324AW · Boeing 737301 · Trailing Edge FlapsSDR AWXA200500244Light · inoperativePHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY LIGHT ASSEMBLY AT LOWER FORWARD CORNER OF THE RT OVERWING EMERGENCY EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD.Feb 22, 2005 · N324AW · Boeing 737301 · Emergency LightingSDR AWXA200500017Outflow Valve · malfunctionedEN ROUTE EXPERIENCED CABIN PRESSURE LOSS, DONNED O2 MASKS & EXECUTED EMERGENCY DESCENT. MANUALLY DEPLOYED CABIN O2 MASKS (MASKS WERE NOT USED), STANDBY & MANUAL DID NOT WORK, TRIED AGAIN LATER AND STANDBY DID WORK. LANDED AT PHX WITHOUT FURTHER INCIDENT, EMEJan 9, 2005 · N324AW · Boeing 737301 · Pressure Regulator/Outflow ValveSDR AWXA200401418Keelbeam · crackedMCN - MAJOR REPAIR - DURING INSPECTION PHX MAINTENANCE FOUND A 3 INCH CRACK IN LT PACK BAY FORWARD END KEEL BEAM AT BS 540, CRACK RUNS HORIZONTALLY THROUGH MACHINED STEP. AIRCRAFT WAS MAINTENANCE FERRIED TO MCN FOR REPAIR. CUTOUT DAMAGED SECTION OF KEEL BEAMDec 15, 2004 · N324AW · Boeing 737301 · Fuselage Main, KeelSDR AWXA200401396Light · shortedPHX - EEL - DURING INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT HAD SHORTED OUT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 4 L/H, OPERATIONAL CHECK WAS GOOD.Dec 14, 2004 · N324AW · Boeing 737301 · Emergency LightingSDR AWXA200401361Battery · dischargedLAS - EMERGENCY EQUIPMENT - DURING 8-DAY CHECK, THE AFT EMERGENCY FLASHLIGHT BATTERY WAS FOUND DEAD. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.Dec 7, 2004 · N324AW · Boeing 737301 · Emergency EquipmentSDR AWXA200400975Circuit Card · faultyON CLIMB OUT, ENROUTE, TAKEOFF CONFIGURATION WARNING HORN SOUNDED AT APPROXIMATELY 7000 FEET AND REMAINED ON UNTIL THROTTLES RETARDED TO IDLE, DIVERTED FOR REPAIR. MAINTENANCE REMOVED AND REPLACED AIR SENSING SQUAT SWITCH CIRCUIT CARD M0991 IAW BMM 32-09-20-72Sep 3, 2004 · N324AW · Boeing 737301 · Landing Gear Position and WarningSDR AWXA200400797Connector · damagedDURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 11 THRU 17 LT WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED DAMAGED PIN ON CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROW 12 LT; OPERATIONAL CHECK WAS GOOD.Jul 20, 2004 · N324AW · Boeing 737301 · Light System WiringSDR AWXA200400785Wire · brokenDURING 8-DAY CHECK EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 11 - 17 WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD.Jul 17, 2004 · N324AW · Boeing 737301 · Light System WiringSDR AWXA200400176Clevis · corrodedDURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER FORWARD CLEVIS, AT FORWARD LOWER FACE BS 1088, WL 256, RBL 30. MAINTENANCE REMOVED BUSHING FROM RT HORIZONTAL STABILIZER FORWARD CLEVIS; OVERSIZED CENTER SECTION CLEVIS FORWARD LOWJan 20, 2004 · N324AW · Boeing 737301 · Horizontal Stabilizer Miscellaneous StructureSDR AWXA200400128Strap · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .0156 INCH CRACK WAS FOUND ON FUSELAGE SPLICE STRAP AT BS 358, STR 28 RT, E & E COMPARTMENT. MAINTENANCE CUT OUT CRACKED SECTION OF STRAP BETWEEN STR 27 RT AND STR 28 RT AT BS 358; FABRICATED A NEW SECTION OF REPLACEMEJan 17, 2004 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400166Stringer · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 28 RT AT BS 344, AFT EDGE OF E&E BAY DOOR CUTOUT. MAINTENANCE REMOVED DAMAGED STRINGER 28 RT FROM BS 344 TO BS 360; FABRICATED A NEW REPLACEMENT STRINGER CHANNEL PER DWG 69-489Jan 16, 2004 · N324AW · Boeing 737301 · Fuselage Main, Longeron/StringerSDR AWXA200400119Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1.1875 INCH CRACK WAS FOUND ON R-2 DOOR FORWARD FRAME SURROUND WEB BELOW DOOR ASSIST HANDLE BRACKET, BS 948, RBL 62, WL 251. MAINTENANCE REMOVED CRACKED SECTION OF R-2 DOOR WEB BELOW DOOR ASSIST HANDLE BRACKET, BS 948,Jan 9, 2004 · N324AW · Boeing 737301 · Passenger/Crew DoorsSDR AWXA200400100Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727A, STR 2 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727A, STR 2 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B7Jan 9, 2004 · N324AW · Boeing 737301 · Fuselage Main, Attach FittingsSDR AWXA200400086Carriage · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON NR 8 FLAP CARRIAGE SPINDLE. MAINTENANCE REMOVED AND REPLACED NR 8 FLAP CARRIAGE SPINDLE ASSEMBLY IAW AWA T/C C3R57024.Jan 9, 2004 · N324AW · Boeing 737301 · Trailing Edge FlapsSDR AWXA200400074Web · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON L-2 DOOR FRAME SURROUND WEB AT BS 948, LBL 62, WL 251. MAINTENANCE REMOVED CRACKED L-2 DOOR FRAME SURROUND WEB AT BS 948, LBL 62, WL 251; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-52874-15; Jan 9, 2004 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400122Floor Support · corrodedDURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT UPPER TEE BETWEEN BS 1006-1016, RBL 8, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 1006 TO BS 1016, RBL 8; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT Jan 8, 2004 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400107Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF UPPER LEG ON FLOOR SUPPORT BETWEEN BS 951 AND BS 963, LBL 42. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT BETWEEN BS 951 AND BS 963, LBL 42; FABRICATED A NEW REPLACEMENT FLOOR SUPPOJan 8, 2004 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400102Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR SUPPORT UPPER INBOARD LEG BS 996-1004, LBL 14, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT BS 996-1004, LBL 14; FABRICATED A NEW REPLACEMENT SUPPORT PER DWJan 8, 2004 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400101Web · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF WEB AT R-2 DOOR LOWER SILL BS 990, RBL 49, WL 208. MAINTENANCE REMOVED CORRODED WEB BS 990, RBL 49, WL 208; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-45855; INSTALLEDJan 8, 2004 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400091Stringer · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON STRINGER 4 RT AT BS 867. MAINTENANCE REMOVED DAMAGED SECTION OF STRINGER 4 RT AT BS 867; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03 FIG 203Jan 8, 2004 · N324AW · Boeing 737301 · Fuselage Main, Longeron/StringerSDR AWXA200400118Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 500D, STR 8 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 500D, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65-35352; INSTALLED REPAIR PART IAW Jan 7, 2004 · N324AW · Boeing 737301 · Fuselage Main, Attach FittingsSDR AWXA200400112Floor Support · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON LONGITUDINAL FLOOR SUPPORT WEB BETWEEN BS 708 AND BS 709, RBL 24.75. MAINTENANCE TRIMMED OUT DAMAGE ON FLOOR SUPPORT WEB BETWEEN BS 708 AND BS 709, RBL 24.75; FABRICATED A DOUBLER AND FILLER; Jan 7, 2004 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400110Floor Support · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .625 INCH CRACK WAS FOUND ON LONGITUDINAL FLOOR SUPPORT WEB AT BS 708, LBL 24.75. MAINTENANCE TRIMMED OUT DAMAGE ON FLOOR SUPPORT WEB AT BS 708, LBL 24.75; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW AWJan 7, 2004 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400106Splice · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER SPLICE BETWEEN BS 353 AND BS 366, STR 27 LT. MAINTENANCE REMOVED CORRODED STRINGER SPLICE BETWEEN BS 353 AND BS 366, STR 27 LT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PERJan 7, 2004 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400105Splice · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER SPLICE AT BS 361, STR 26 RT. MAINTENANCE REMOVED CORRODED STRINGER SPLICE AT BS 361, STR 26 RT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-59644; INSTALLED REPAIR Jan 7, 2004 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400103Frame · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF UPPER LEG ON UPPER FRAME AT L-1 DOOR WAY BS 315-340, LBL 59, WL 209. MAINTENANCE REMOVED CORRODED UPPER FRAME AT L-1 DOOR WAY FROM BS 315 TO BS 350, LBL 59, WJan 7, 2004 · N324AW · Boeing 737301 · Fuselage Main, StructureSDR AWXA200400099Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK .375 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727E, STR 8 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727E, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW BJan 7, 2004 · N324AW · Boeing 737301 · Fuselage Main, Attach FittingsSDR AWXA200400098Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK .1875 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727B, STR 10 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727B, STR 10 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAJan 7, 2004 · N324AW · Boeing 737301 · Fuselage Main, Attach FittingsSDR AWXA200400097Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM AT BS 296, LBL 11, WL 208. MAINTENANCE REMOVED CORRODED FLOORBEAM BS 296, LBL 11, WL 208; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW B7Jan 7, 2004 · N324AW · Boeing 737301 · Fuselage Main, Floor BeamSDR AWXA200400090Stringer Clip · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK AND CORROSION WAS FOUND ON STRINGER TIE CLIP AT BS 500C, STR 26 RT. MAINTENANCE REMOVED CRACKED & CORRODED STRINGER TIE CLIP AT BS 500C, STR 26 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; Jan 7, 2004 · N324AW · Boeing 737301 · Fuselage Main, Attach FittingsSDR AWXA200400089Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 867, STR 4 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 867, STR 4 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B73Jan 7, 2004 · N324AW · Boeing 737301 · Fuselage Main, Attach FittingsSDR AWXA200400088Intercostal · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON INTERCOSTAL WEB AFT OF FORWARD CARGO DOOR AT STR 26 RT BETWEEN BS 480 AND BS 500. MAINTENANCE REMOVED CORRODED INTERCOSTAL WEB AT STR 26 RT BETWEEN BS 480 AND BS 500; FABRICATED A NEW RJan 7, 2004 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400087Carriage · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON NR 7 FLAP CARRIAGE SPINDLE. MAINTENANCE REMOVED AND REPLACED NR 7 FLAP CARRIAGE SPINDLE ASSEMBLY IAW AWA T/C C3R57024.Jan 7, 2004 · N324AW · Boeing 737301 · Trailing Edge FlapsSDR AWXA200400083Splice · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON STRINGER SPLICE AT BS 906, STR 4 LT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE AT BS 906, STR 4 LT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-51698; INSTALLED REPAIR PART IAW BJan 7, 2004 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200400079Stringer · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK 4 EACH CRACKS WERE FOUND ON STRINGER 8 LT AT BS 380. MAINTENANCE PERFORMED HFEC INSPECTION OF CRACKS TO VERIFY CRACK ENDS; STOP DRILLED 4 EA CRACKS ON STRINGER 8 LT AT BS 380; PERFORMED HFEC INSPECTION TO VERIFY CRACKS AJan 7, 2004 · N324AW · Boeing 737301 · Fuselage Main, Longeron/StringerSDR AWXA200400078Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND ON FRAME FOOT AT BS 616, RBL 62. MAINTENANCE CUT OUT CRACK ON INNER CHORD FLANGE AT BS 616, RBL 62; PERFORMED HFEC INSPECTION TO VERIFY NO CRACK EXISTS; FABRICATED A REPAIR ANGLE AND FILLER; INJan 7, 2004 · N324AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA200400077Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND ON FRAME FOOT AT BS 616, LBL 62. MAINTENANCE CUT OUT CRACK ON INNER CHORD FLANGE AT BS 616, LBL 62; PERFORMED HFEC INSPECTION TO VERIFY NO CRACK EXISTS; FABRICATED A REPAIR ANGLE AND FILLER; INJan 7, 2004 · N324AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA200400076Stringer · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND ON STRINGER 16 RT, 5 INCHES FORWARD OF FRAME 500D. MAINTENANCE CUT OUT DAMAGED SECTION OF STRINGER 16 RT, BS 500D; FABRICATED A CHANNEL, RADIUS FILLER, AND FILLER; INSTALLED REPAIR PARTS IAW AWJan 7, 2004 · N324AW · Boeing 737301 · Fuselage Main, Longeron/StringerSDR AWXA200400075Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON FRAME BETWEEN STRINGERS 28 LT AND 28 RT, AT BS 500. MAINTENANCE REMOVED DAMAGED AREA OF FRAME BETWEEN STRINGERS 28 LT AND 28 RT, AT BS 500; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REJan 7, 2004 · N324AW · Boeing 737301 · Fuselage Main, Frame
Back to N324AW