N304AW
Service difficulty reports not matched to an aircraft · 55
They name N304AW, 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 = 'N304AW' 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.
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 = 'N304AW' AND registry_match IS NULL ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 304AW0008Battery Pack · inoperativeROWS 1-4 OF EMERGENCY LIGHTS DO NOT ILLUMINATE. REPLACED FUSES IN BATTERY PACK. OPS CHECKS GOOD PER MM 33-51-51.SDR 304AW0007Skin · lightning strikeSEVERAL LIGHTENING STRIKES IN THE CROWN OF THE FUSELAGE SKIN NEAR STATION 259 BETWEEN STR 2 AND 3 LEFT. REPAIRED IAW SRM 53-00-01 AND EA NR 53-171.SDR 304AW0006Panel · malfunctionedMODE CONTROL PANEL SWITCHES, N1, SPD, VNAV, LNAV, ALT HLD & V/S INDICATORS INOP. PLACED ON MEL 22-15-8. NOTE: MAINTENANCE INDUCED PROBLEM WHILE REPLACING ONE LIGHT BULB IN PANEL. 04/26/2004: REPLACED MCP AND OPS CHECKED PER MM 22-11-34. CLEARED MEL.SDR 304AW0005Coupler · damagedYAW DAMPER POPS DC CIRCUIT BREAKER. PLACED ON MEL 22-3-1 AND PERFORMED RUDDER PRESSURE REDUCER SYSTEM TEST PER MM 22-12-01. 04/22/2004: REPLACED YAW DAMPER COUPLER PER MM 22-12-13. SYSTEM CHECKS NORMAL PER ADJUSTMENT/TEST.SDR 304AW0004Battery · inoperativeMID CABIN EMERGENCY ESCAPE LIGHTS ALONG SEAT BOTTOMS INOP. ALSO AFT EMERGENCY FLASHLIGHT INOP. REPLACED 1 FUSE ON BATTERY PACK LOCATED ON RIGHT AFT DOOR. CABIN LIGHTS OP NORMAL. REPLACED BATTERY IN FLASHLIGHT, OPS NORMAL.SDR 304AW0003Relay · stickingCREW REPORTED THAT THE AUTOPILOT COMMAND-A WILL NOT ENGAGE UNLESS COMMAND-B IS ENGAGED FIRST. REPLACED AILERON FORCE LIMITER CLUTCH RELAY DUE TO STICKING. CHECKS OK PER MM 22-11-13.SDR 304AW0002Connector · dirtySPEED TRIM FAIL LIGHT ILLUMINATED DURING FLIGHT. PLACED ON MEL 22-10. CLEANED AND RESECURED CANNON PLUG ON FCC PER MM 22-11-33. PERFORMED BITE TEST PER MM 22-11-01. TEST PASSED. CLEARED MEL.SDR 304AW0001Computer · malfunctionedAUTO THROTTLE DISCONNECTED ON TAKEOFF ROLL. REMOVED AUTO THROTTLE COMPUTER AFTER TROUBLESHOOTING. REINSTALLED AUTO THROTTLE COMPUTER AND PERFORMED BITE TEST PER MM 22-10-04. OPS CHECKED NORMAL.SDR AWXA200200280Floorbeam · corrodedLCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AND NUTPLATES IN THE AFT CARGO COMPARTMENT AT BS 727+6, LBL 2.5. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS BEYOND LIMITS IAW B737 300 SRM 53-60-53, FIG 101, SHT 8. FABSDR AWXA200200271Skin · dentedLCQ - MAJOR REPAIR - DURING C-15 CHECK A DENT WAS FOUND ON RT HORIZONTAL STABILIZER AT STAB STA 144 MID SPAN. FABRICATED A DOUBLER, FILLER AND INSTALLED REPAIR PARTS IAW B737-300 SRM.SDR AWXA200200295Floor Support · corrodedLCQ - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT AND NUTPLATES IN THE AFT CARGO PIT AT BS 773, LBL 2.5. MAINTENANCE REMOVED NUTPLATES AND CLEANED CORROSION, FABRICATED 2 EACH REPAIR ANGLES AND INSTALLED REPAIR PARTS IAW B737SDR AWXA200200294Strap · corrodedMAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON THE RT FLOOR SUPPORT LOWER STRAP IN THE AFT CARGO COMPARTMENT AT BS 849, RBL 19. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED CORRODED STRAP AT RBL 19, BS 849, FABRICATESDR AWXA200200292Floorbeam · corrodedMAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON THE TOP OF FLOORBEAM AT BS 986.5, LBL 58. MAINTENANCE CLEANED CORROSION OFF FLOORBEAM AND FOUND MATERIAL LOSS EXCEEDING ALLOWABLE LIMITS. FABRICATED FLOORBEAM REPAIR STRAP AND INSTALLED REPAIR PART AT BSSDR AWXA200200279Floorbeam · corrodedLCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AND NUTPLATES IN THE AFT CARGO COMPARTMENT AT BS 727D+6, LBL 7.5. MAINTENANCE REMOVED CORROSION IAW B737-300 SRM 51-10-2, PG. 24, FABRICATED 2 EACH REPAIR ANGLES FROM 7075-0-.071,SDR AWXA200200278Floorbeam · corrodedLCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AND NUTPLATES IN THE AFT ACRGO COMPARTMENT AT BS 860, LBL 7.5. MAINTENANCE FABRICATED 3 EACH REPAIR ANGLES, TREATED AND PRIMED, AND INSTALLED REPAIRS IAW B737-300 SRM SDR AWXA200200277Floorbeam · corrodedLCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT BEAM IN THE AFT CARGO COMPARTMENT AT BS 860, RBL 7.5. MAINTENANCE FABRICATED 2 EACH REPAIR ANGLES, TREATED AND PRIMED ANGLES, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53SDR AWXA200200276Floorbeam · corrodedLCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AND NUTPLATE IN THE AFT CARGO COMPARTMENT AT BS 860, LBL 2.5. MAINTENANCE REMOVED THE NUTPLATE AND CLEANED CORROSION ON FLOOR SUPPORT BEAM AT FS 860, LBL 2.5 IAW 51-40-02 PG 1, 53SDR AWXA200200275Floorbeam · corrodedLCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM IN THE AFT CARGO COMPARTMENT AT BS 773, RBL 2.5. MAINTENANCE CLEANED CORROSION ON FLOOR SUPPORT BEAM AT FS 773, RBL 2.5 AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. FABRICATED 2 ESDR AWXA200200274Floorbeam · corrodedLCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON AFT CARGO PIT RT FLOOR SUPPORT BEAM BS 727D+6, RBL 7.5. MAINTENANCE REMOVED CORROSION AND MATERAIL REMAINING .039, FABRICATED 2 EACH REPAIR ANGLES FROM 7075-0.071, 7075-0-.081, HEAT TREATED IAW B737SDR AWXA200200273Floor Support · corrodedLCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON AFT CARGO PIT FLOOR SUPPORT NUT PLATE BS 860, RBL 2.5. MAINTENANCE REMOVED NUT PLATE AND CORROSION AT BS 860, RBL 2.5. MATERAIL REMAINING .031, FABRICATED 2 EACH REPAIR ANGLES, HEAT TREATED, TRIMMEDSDR AWXA200200272Floor Support · corrodedLCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATED CORROSION WAS FOUND ON AFT PIT FLOOR SUPPORT AT BS 860, LBL 12.5. MAINTENANCE CLEANED CORROSION AND FOUND MATERAIL LOSS OUT OF LIMITS. FABRICATED AND INSTALLED 2 EACH REPAIR ANGLES IAW B737-300 SRM 53-00-53, PGSDR AWXA200200270Floorbeam · crackedLCQ - MAJOR REPAIR - DURING C-15 CHECK A CRACK WAS FOUND RUNNING FROM SEAT TRACK FLOORBEAM TEE CAP LOWER EDGE TO A FASTENER HOLE ON INBOARD SIDE, BS 663.75, RBL 26. FABRICATED A REPAIR STRAP, SHIMS AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 PG 10 ANSDR AWXA200200268Frame · crackedLCQ - MAJOR REPAIR - DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND ON CABIN SIDE WALL FRAME ATTACHED TO FLOORBEAM AT BS 616, LBL 66, WL 208, LOCATED JUST BELOW FLOOR LINE UNDER THE OVERWING EMERGENCY EXIT. MAINTENANCE REMOVED INNER CHORD, FABRICATED NEW INNER SDR AWXA200200293Stringer · corrodedLCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER IN THE AFT CARGO COMPARTMENT BS 1010, STR 27 R/H. MAINTENANCE REMOVED CORRODED STRINGER 27 R/H AT STA 1010, FABRICATED AND INSTALLED A NEW STRINGER IAW B737-300 SRM 51-10-2, PG.SDR AWXA200200269Skin · crackedLCQ - MAJOR REPAIR - DURING C-15 CHECK 3 EACH .300" CRACKS WERE FOUND ON LOWER AFT RADIUS RIVET PATTERN OF R1 DOOR CUTOUT. MAINTENANCE CUTOUT CRACKED AREA OF SKIN, PERFORMED HFEC INSPECTION TO VERIFY CRACKS WERE CONTAINED, FABRICATED 2 EACH REPAIR DOUBLERS ANDSDR AWXA200200267Skin · crackedLCQ - MAJOR REPAIR - DURING C-15 CHECK A .250 INCH CRACK WAS FOUND ON THE SKIN OF THE L2 DOOR CUTOUT AT BS 986.5, STR 8 LT. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW B737-300 SRM.SDR AWXA200200078Power Supply · failedAFT EMERGENCY EXIT LIGHTS FROM ROW 18 LT, ALL THE WAY AFT WILL NOT ILLUMINATE DURING TEST. MAINTENANCE TROUBLESHOT AND FOUND THE AFT POWER SUPPLY INOPERATIVE AT BS 947, REPLACED POWER SUPPLY IAW BMM 33-51-51, EMERGENCY EXIT LIGHTS OPERATIONALLY CHECKED GOOD.SDR AWXA0001952Crease Beam · corrodedBS 767-787 LT CREASE BEAM PANEL IS CORRODED. SHEAR WEB MADE AND INSTALLED AS PER DWG 65-55885-3, PART PAINTED AS PER MM 51-21-10 PG 701.SDR AWXA0001951Tee Chord · crackedCRACK INDICATION ON AFT CARGO DOOR LOWER AFT CORNER, LOWER WEB TO SKIN ATTACH ANGLE, CRACK, LOCATED BETWEEN TWO AFT RIVETS WEB. AFT LOWER WEB T-CHORD REPAIRED PER SB 737-52A1079/DRW 65 C25 180 + SRM 51-40-02 PG 4.SDR AWXA0001950Skin · damagedFUSELAGE SKIN HAS A NON STANDARD REPAIR AT RIVET LOCATION BS 727C AND 2 INCHES BELOW STRINGER 17L. FUSELAGE SKIN REPAIRED AT BS 727C AND 2 INCHES BELOW STR 17L PER SRM 53-00-01 FIG 203 PAGE 207.SDR AWXA0001949Stringer · crackedD: Stringer crack at STA 178. WL 207. RBL 28C: fabricated repair parts per SRM 51-70-12 Fig 1 detail 7. Installed repair parts per SRM 51-70-12 Fig 1SDR AWXA0001948Frame · crackedFUSELAGE RT SIDE CHORD AT WL 207, STA 178 CRACKED. INSTALLED NEW SIDE CHORD P/N 65-16300-87 AS PER DWG 65-16300 SHEET 4 FRAME 1-8.SDR AWXA0001947Frame · crackedFUSELAGE LT SIDE CHORD AT WL 207 STA 178 CRACKED. INSTALLED NEW 65-16300-86 SIDE CHORD AS PER DWG 65-16300 SHEET 4 FRAME 1 TO 8.SDR AWXA0001946Web · crackedD: Center Bulkhead Web Crack At Body STA .178 . WL 187. BLO.C: Remove Crack Per SRM 53-10-08 Fig 203. NDT Checked For Crack Containment. Frabricate Repair Parts and installed Per SRM 53-10-08 Fig 203SDR AWXA0001945Bulkhead · crackedWEB CRACKS AT STA 178 LBL 5.7. REMOVED FASTENERS PER SRM 51-40-2 AT REPAIR AREA. REPAIRED CRACKS PER SRM 53-10-08 FIG 209. NDT CHECKED CRACKS CONTAINMENT. FABRICATED REPAIR PARTS PER SRM 53-10-08 FIG 209 SH-3. PROTECTIVE TREATMENT FOR REPAIR PARTS PER SRMSDR AWXA0001944Web · crackedD: Web Crack on Floor Level (WL 207) At STA .178 on R/H Side RBL 28C: Removed Cracked Web, Fabricated New Web P/N 65-45833-40 Per REF DWG 65-45833, install Web Per 45-45833SDR AWXA0000365Bleed Valve · failedAIR TURNBACK, NR 1 ENGINE BLEED AIR VALVE W/N CLOSE, CURCUIT BREAKER POPPED. REMOVED AND REPLACED NR 1 ENGINE BLEED AIR REGULATOR. TT 0049297 M+E=03-3611-9-0001. RECOMMENDATION: REMAIN OPEN PENDING REVIEW OF TEARDOWN REPORT.SDR AWXA0000329Structure · crackedC-CHECK, VERT STAB UPPER RUDDER HINGE POINT RT STRUCTURE HAS CRACK AT CORNER. REMOVED DAMAGED CORNER COVER, FABRICATED REPAIR COVER IAW 737 SRM 51-30-30, 51-20-02, AND 51-40-02, TREATED AND PRIMED IAW 737 SRM 51-20-06, INSTALLED IAW 737 SRM 51-40-02.SDR AWXA0000328Skin · crackedC-CHECK, CRACKS IN LOWER SKIN OF THE LEADING EDGE OF NR 2 AND NR 3 SLATS. REMOVED DAMAGED AREA IAW ER NR 3-57-55-17E, FABRICATED FILLERS FROM MAT SHT 77075 T6 X .063 QQA 250, 2 DOUBLERS FROM 2024T3 QQA 250/5, INSTALLED FILLER AND DOUBLER IAW 737 SRM 51-40-02SDR AWXA0000327Floorbeam · corrodedC-CHECK, CORROSION OUT OF LIMITS ON T-CAP AT FS 986.5 RBL 18. REMOVED DAMAGED T CAP IAW 737 SRM 51-40-02, FABRICATED T CAP FROM BAC 1505 100617/7077, IAW 737 SRM 53-00-51, TREATED AND PRIMED IAW 737 SRM 51-20-01, INSTALLED REPAIR PARTS IAW 737 SRM 53-00-51 SDR AWXA9900253Module · inopNML OPS, ELECTRICAL SMELL IN COCKPIT. UNKNOWN ELECTRICAL SMELL IN COCKPIT. INSPECTED COCKPIT, RAN ENGINES ISOLATED ODOR TO P5-9 WINDOW, PITOT HEAT MODULE. REPLACED PER MM 30-09-11. ACFT OK FOR SERVICE (TAG 014234).SDR AWXA9900157Floorbeam · corrodedFLOORBEAM UPPER CHORD CORRODED RBL 6 TO RBL 52 AT STA 294.5. FABRICATED T-CHORDS AND REPAIRED AS PER AWA ER 3-53-1529 INSTRUCTIONS.SDR AWXA9900156Floorbeam · corrodedCORROSION AROUND SCREW HOLES TOP AND BOTTOM OF UPPER TEE CHORD RBL 21-56, FRAME STA 328 RT. FABRICATED T-CHORD AND REPAIR AS PER AWA ER 3-53-1529 INSTRUCTIONS.SDR AWXA9900158Floorbeam · corrodedFLOORBEAM 986.5 REQUIRES REPAIR SPLICES IAW AWA ER 3-53-1529 DUE TO CORROSION ON T-CAP. FABRICATED T-CHORDS AND REPAIRED ANGLES PER AWA ER 3-53-1529 INSTRUCTIONS, 986.5 FLOORBEAM T-CAP REPLACED RT BL TO LT BL ALL INCLUSIVE SPLICE.SDR AWXA9700691Controller · failedSMOKE CAME OUT OF THE AFT PORTION OF THE COPILOTS FORWARD WINDOW, NEAR THE DRAIN HOSE. THE WINDOW HEAT WAS TURNED OFF AND THE SMOKE WENT AWAY. REMOVED AND REPLACED THE COPILOTS NR 1 WINDOW HEAT CONTROLLER.SDR AWXA9600787Skin · dentedDURING ROUTINE MAINTENANCE CHECK, FOUND C-2 DOOR AFT CARGO OUTER SKIN DENTED AND CREASED IN SEVERAL PLACES. REMOVED AND REPLACED C-2 DOOR OUTER SKIN IAW B737, SRM 52-30-01 AND 51-40-02. MAT ID 2024-T3 .071. FABRICATED NEW DOOR SKIN IAW B737 SRM 52-30-01.SDR AWXA960020Skin · dentedPHX - FLT NR 842 - DURING ROUTINE MAINTENANCE CHECK, FOUND FUSELAGE SKIN DENTED ACROSS STRINGER 25R, 4 FEET FORWARD OF AFT CARGO DOOR CUTOUT. OPENED UP INTERIOR FOR INSPECTION AND NO DAMAGE NOTED. FUSELAGE SKIN WITHIN LIMITS PER SRM 53-00-01, FIGURE 101. NDSDR AWXA960011Outflow Valve · failedPHX/BUR - FLT 0484 - AUTOPRESSURE INOPERATIVE AT 280 FEET CABIN ALTITUDE AT 3,000 FEET, DIFFERENTIAL PRESSURE 8.4. REMOVED AND REPLACED REAR OUTFLOW VALVE. OPS CHECKED GOOD. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. OPS CHECKED GOOD. REFERENCE CONTRSDR 96ZZZX565Controller · failedPHX/BUR - FLT 0484 - AUTOPRESSURE INOPERATIVE AT 280 FEET CABIN ALTITUDE AT 3,000 FEET, DIFFERENTIAL PRESSURE 8.4. REMOVED AND REPLACED REAR OUTFLOW VALVE. OPS CHECKED GOOD. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. OPS CHECKED GOOD. REFERENCE CONTRSDR AWXA9500820Cover · looseLAS - FLT 1512 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT COVER IN FORWARD GALLEY LOOSE. REPLACED EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. (X)
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