Boeing 737-33A
Service difficulty reports · 1,809
Newest first. General aviation reporting is voluntary.
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 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.
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
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 AWXA200400169Battery · dischargedLAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400144Wire · brokenPHX - EEL - FLIGHT CREW REPORTED ELECTRICAL WIRE FOR EMERGENCY LIGHTING BROKEN IN AFT GALLEY AT LT TRASH BIN COMPARTMENT. MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT IN AFT GALLEY; OPERATIONAL CHECK WAS GOOD.SDR SO19200405477Aileron · inoperativeIAW L/P 23142 EXCESSIVE RT ROLL AFTER T/O RETURNED WITHOUT INCIDENT, PERFORMED TROUBLESHOOTING INSPECTED LUBRICATED AND CHECKED CABLE TENSION FOR THE AILERON SYS IAW MM. OPS CHECK GOOD. PERFORMED FUNCTIONAL CHECK FLIGHT AND RETURNED AIRCRAFT TO SERVICE WITHOSDR AWXA200400137Skin · crackedPHX - MAJOR REPAIR - DURING 8-DAY CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN JUST AFT OF WING TO BODY FAIRING BETWEEN BS 727D AND 727 E, AT STR 23 LT. MAINTENANCE CUT OUT DAMAGED SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED SDR AWXA200400057Warning Horn · activatedPHX - ABORTED TAKEOFF - FLT 0429 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR ELP TAKEOFF WARNING HORN SOUNDED, REJECTED TAKEOFF AT 60 KTS. FOUND SPEED BRAKES NOT STOWED, STOWED SPEED BRAKES AND TOOK OFF WITHOUT FURTHER EVENT.SDR AWXA200400043Support · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT. MAINTENANCE REMOVED AND REPLACED LT INBOARD MIDFLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT PER AWA T/C I3R57057.SDR AWXA200400042Support · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT INBOARD FLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT. MAINTENANCE REMOVED AND REPLACED RT INBOARD FLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT PER AWA T/C I3R57057.SDR AWXA200400023Spar · delaminatedMCN - MINOR REPAIR - DURING C-18 CHECK THE RT AILERON FORWARD SPAR LOWER FLANGE WAS FOUND DELAMINATED AT ACCESS PANEL ATTACHMENT WS 430. MAINTENANCE TRIMMED OUT DAMAGE ON RT AILERON FORWARD SPAR, LOWER FLANGE; CLEANED AND PREPARED SURFACE; PERFORMED BOND REPAISDR AWXA200400008Angle · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON LT AIR CONDITIONING BAY FORWARD OUTBOARD DUCT SUPPORT (TEE ANGLE) BS 530, LBL 58, WL 156. MAINTENANCE REMOVED CRACKED TEE ANGLE BS 530, LBL 58, WL 156; FABRICATED A NEW REPLACEMENT TEE ANGLE SDR AWXA200301567Wire · brokenDEN - EEL - DURING INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 12-14 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT ROW 14 LT, OPERATIONAL CHECK OF EEL SYSTEM WAS GOOD.SDR AWXA200301566Battery · dischargedDEN - EMERGENCY EQUIPMENT - DURING INSPECTION FOUND THE EMERGENCY FLASHLIGHT IN AFT GALLEY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400009Clip · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON LT AIR CONDITIONING BAY FORWARD DUCT SUPPORT CLIP AT BS 530, LBL 56, WL 158. MAINTENANCE REMOVED CRACKED CLIP AT BS 530, LBL 56, WL 158; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-37254; INSDR AWXA200301540Bracket · crackedDURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN BRACKET FOR JUNCTION BOX J10 AT BS 380. MAINTENANCE REMOVED BRACKET FOR JUNCTION BOX J10 AT BS 380; FABRICATED A NEW REPLACEMENT BRACKET PER DWG 69-45146; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 6 &SDR AWXA200301605Floorbeam · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND AT RT CENTER FLOORBEAM T-CAP ANGLE BS 540, BL-0. MAINTENANCE REMOVED CRACKED T-CAP ANGLE AT BS 540, BL-0; FABRICATED A NEW REPLACEMENT T-CAP ANGLE PER DWG 65-52894; INSTALLED REPAIR PART IAW B737SDR AWXA200301598Floorbeam · debondedMCN - MAJOR REPAIR - DURING C-18 CHECK THE CENTER LT FLOORBEAM T-CAP ANGLE WAS DISBONDED AT BS 540, LBL 22. MAINTENANCE REMOVED CRACKED T-CAP ANGLE AT BS 540, LBL 22; FABRICATED A NEW REPLACEMENT T-CAP ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FSDR AWXA200301579Intercostal · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND ON L-1 DOOR FORWARD INTERCOSTAL AT BS 294.5, STR 12 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT L-1 DOOR BS 294.5, STR 12 LT; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART SDR AWXA200301521Pump · failedEN ROUTE FROM PHX TO PDX B-SYSTEM HYD OVERHEAT LIGHT ILLUMINATED, FOLLOWED CHECKLIST TO CLEAR DISCREPANCY, OVERHEAT LIGHT REMAINED ON, DIVERTED TO LAS. MAINTENANCE REMOVED AND REPLACED B-SYSTEM ELECTRIC MOTOR DRIVEN HYDRAULIC PUMP IAW R4M29002 (PUMP WAS BORROSDR AWXA200301595Stringer · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON STRINGER 16 LT AT LIGHT ASSEMBLY BS 500C. MAINTENANCE TRIMMED OUT CRACK ON STRINGER 16 LT AT LIGHT ASSEMBLY BS 500C; FABRICATED A REPAIR CHANNEL AND RADIUS FILLER; INSTALLED REPAIR PART IAW AWSDR AWXA200301586Stringer · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .2500 INCH CRACK WAS FOUND ON STRINGER 16 RT AT LIGHT ASSEMBLY BS 500C. MAINTENANCE REMOVED DAMAGE FROM END OF STRINGER 16 RT AT BS 500C; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A RADIUS FILLER ASDR AWXA200301542Stringer Clip · crackedDURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN STRINGER CLIP BS 520, STR 14 LT. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 520, STR 14 LT; RECEIVED A NEW REPLACEMENT STRINGER CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 45 & 64, FIG 12 & 14SDR AWXA200400058Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK FOUND THE NR 3 SLAT OUTBOARD END UPPER WEDGE SKIN DELAMINATED. MAINTENANCE CUT OUT DELAMINATED AREA NR 3 SLAT OUTBOARD END UPPER WEDGE SKIN; CLEANED AND PREPARED AREA; FABRICATED REPAIR DOUBLERS; INSTALLED BOND REPAIR IASDR AWXA200400004Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM AT FASTENER HOLE BS 344, RBL 7. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM CHORD; FABRICATED A NEW REPLACEMENT SECTION OF CHORD, 2 EACH REPAIR ANGLES, & 3 EACH WEB STIFFSDR AWXA200301592Skin · delaminatedDURING C-18 CHECK THE NR 1 SLAT TRAILING EDGE WEDGE UPPER SKIN WAS FOUND DELAMINATED AT OUTBOARD MAIN TRACK. MAINTENANCE REMOVED DAMAGED NR 1 SLAT TRAILING EDGE WEDGE UPPER SKIN; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10SDR AWXA200301591Skin · delaminatedDURING C-18 CHECK THE NR 1 SLAT TRAILING EDGE UPPER SKIN WAS FOUND DELAMINATED AT OUTBOARD AUXILIARY TRACK. MAINTENANCE REMOVED DAMAGED NR 1 SLAT TRAILING EDGE UPPER SKIN; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, FIG. SDR AWXA200301589Wedge · delaminatedDURING C-18 CHECK THE NR 5 SLAT OB END UPPER WEDGE TRAILING EDGE SKIN WAS FOUND DELAMINATED AROUND PREVIOUS REPAIR. MAINTENANCE REMOVED PREVIOUS REPAIR AND DELAMINATED SKIN; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW 737-300 SRM 51-70-10, FIG.SDR AWXA200301577Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .0625 INCH CRACK WAS FOUND COMING FROM FASTENER HOLE ON FUSELAGE SKIN AT BS 958, STR 16-17 LT, WL 215. MAINTENANCE REMOVED FASTENER AND PERFORMED HFEC INSPECTION TO VERIFY CRACK END, STOP DRILLED CRACK AND RE-ACCOMPLISSDR AWXA200301541Stringer Clip · crackedDURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER CLIP BS 847, STR 10 LT. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 847, STR 10 LT; RECEIVED A NEW REPLACEMENT STRINGER CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 45 & 64, FIG 12 & 1SDR AWXA200400010Channel · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON NR 3 FLAP TRACK FAIRING SPRING DOOR ANCHOR BRACKET (CHANNEL) WBL 197 LT. MAINTENANCE REMOVED CRACKED NR 3 FLAP TRACK FAIRING SPRING DOOR CHANNEL AT WBL 197 LT; FABRICATED A NEW REPLACEMENT SDR AWXA200400005Plate · chafedMCN - MINOR REPAIR - DURING C-18 CHECK FOUND INSPECTION COVER IN LT FLAP WELL CHAFING ON LT OUTBOARD FORE FLAP JUST OUTBOARD OF NR 3 FLAP TRACK WS 205 LT. MAINTENANCE REMOVED CHAFED INSPECTION PLATE LT FLAP WELL WS 205 LT; FABRICATED A NEW REPLACEMENT PLATE; SDR AWXA200301647Intercostal · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT INTERCOSTAL (WEB) BETWEEN BS 847 AND BS 867, RBL 21 AT DOOR CUTOUT FRAME. MAINTENANCE CUT OUT CORRODED WEB BETWEEN BS 847 AND BS 867, RBL 21; FABRICATED A NEW REPLSDR AWXA200301643Support Angle · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND ON SUPPORT ANGLE BS 295.5, STR 7 RT. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE BS 295.5, STR 7 RT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-45807; INSTALLED REPAIR PART IAW B737-300 SRM SDR AWXA200301585Attach Angle · crackedMAJOR REPAIR - DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND ON FRAME ATTACH ANGLE AT BS 294.5, STR 13 LT MAINTENANCE REMOVED CRACKED FRAME ATTACH ANGLE AT BS 294.5, STR 13 LT; FABRICATED A NEW REPLACEMENT ANGLE IAW DWG 65-1633; INSTALLED REPAIR PART IAW B737SDR AWXA200301580Stiffener · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON LOWER LEG OF STIFFENER INSIDE THE NR 3 FLAP TRACK FAIRING, NEAR AFT END OF FAIRING WBL 191. MAINTENANCE REMOVED CRACKED STIFFENER AT WBL 191; FABRICATED A NEW REPLACEMENT STIFFENER; INSTALLEDSDR AWXA200301575Shear Tie · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON L-1 DOOR (INTERIOR) FORWARD INTERCOSTAL CLIP (SHEAR TIE) AT BS 294.5, STR 11 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL SHEAR TIE AT L-1 DOOR BS 294.5, STR 11 LT; FABRICATED A NEW REPLACEMENSDR AWXA200301543Intercostal · crackedDURING C-18 CHECK A .625 INCH CRACK WAS FOUND IN FORWARD INTERCOSTAL AT L-1 DOOR OPENING BS 294.5, STR 11 LT. MAINTENANCE REMOVED CRACKED FORWARD INTERCOSTAL AT L-1 DOOR OPENING BS 294.5, STR 11 LT; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 66-14208; ISDR AWXA200400011Channel · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON NR 6 FLAP TRACK FAIRING SPRING DOOR ANCHOR BRACKET (CHANNEL) WBL 197 RT. MAINTENANCE REMOVED CRACKED NR 6 FLAP TRACK FAIRING SPRING DOOR CHANNEL AT WBL 197 RT; FABRICATED A NEW REPLACEMENT SDR AWXA200301642Angle · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A 1.25 INCH CRACK WAS FOUND ON LT WING LEADING EDGE BRACKET (Z-ANGLE) INSIDE PANEL 5748, WS 191. MAINTENANCE REMOVED CRACKED Z-ANGLE WS 191, UPON REMOVAL OF ANGLE FOUND LOWER SKIN CRACKED. REMOVED CRACKED SECTION OF SKISDR AWXA200301641Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .125 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB, AFT SIDE AT RBL 75, WL 187. MAINTENANCE CUT OUT CRACKED SECTION OF BS 178 BULKHEAD WEB AT RBL 75, WL 187; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST;SDR AWXA200301597Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .125 INCH CRACK WAS FOUND ON BS 178 BULKHEAD CHORD AT AFT CENTER OF RADIUS RBL 29, WL 207. MAINTENANCE REMOVED CRACKED CHORD AT RBL 29, WL 207; FABRICATED A NEW REPLACEMENT CHORD; INSTALLED REPAIR PART IAW B737-300 SRMSDR AWXA200301596Intercostal · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON INTERCOSTAL WEB AT BS 277, STR 14 RT. MAINTENANCE REMOVED CRACKED INTERCOSTAL WEB AT BS 277, STR 14 RT; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-45807; INSTALLED REPAIR PART IAW B7SDR AWXA200301581Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .125 INCH CRACK WAS FOUND ON BULKHEAD VERTICAL BEAM WEB BETWEEN BS 178 AND BS 179.5, LBL 5.7, WL 178. MAINTENANCE CUT OUT CRACKED AREA OF BULKHEAD WEB BETWEEN BS 178 AND BS 179.5, LBL 5.7, WL 178; FABRICATED A NEW REPLSDR AWXA200301578Web · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD VERTICAL BEAM WEB AT BS 181, RBL 17.1, WL 182. MAINTENANCE REMOVED DAMAGED AREA OF VERTICAL BEAM WEB AT BS 181, RBL 17.1, WL 182; FABRICATED NEW REPLACEMENT SECTION OF WEB AND SDR AWXA200301528Panel · debondedDURING C-18 CHECK FOUND PREVIOUS REPAIR DISBONDED AT OUTBOARD UPPER SURFACE OF NR 4 SPOILER FROM WBL 174.75 TO WBL 107.75. MAINTENANCE REMOVED PREVIOUS REPAIR AT OUTBOARD UPPER SURFACE OF NR 4 SPOILER FROM WBL 174.75 TO WBL 107.75; PERPARED SURFACE AND APPLIESDR AWXA200301527Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD FORWARD FACE WEB AT BUTTON HEAD HI-LOK HOLES AT 6 O'CLOCK POSITION WL 234 LBL 9 AND LBL 11. MAINTENANCE CUT OUT DAMAGE ON BS 178 BULKHEAD FORWARD FACE WEB AT WL 234 LBL 9 AND LSDR AWXA200400003Plate · chafedMCN - MINOR REPAIR - DURING C-18 CHECK FOUND INSPECTION COVER AT INBOARD END OF RT OUTBOARD FLAP WELL CHAFED WS 205 RT. MAINTENANCE REMOVED CHAFED INSPECTION PLATE AT INBOARD END OF RT OUTBOARD FLAP WELL WS 205 RT; FABRICATED A NEW REPLACEMENT PLATE; INSTALLESDR AWXA200301640Support Angle · crackedMCN - MINOR REPAIR - DURING C-18 CHECK A 1.25 INCH CRACK WAS FOUND ON ANGLE AT RT WING INBOARD UPPER TRAILING EDGE PANEL, JUST INBOARD OF NR 5 SPOILER AT WBL 71.24. MAINTENANCE STOP DRILLED CRACK ON ANGLE AT RT WING INBOARD UPPER TRAILING EDGE PANEL WBL 71.24SDR AWXA200301593Skin · debondedDURING C-18 CHECK FOUND THE NR 2 LEADING EDGE SLAT DISBONDED AT OUTBOARD CORNER. MAINTENANCE CUTOUT DAMAGED AREA NR 2 LEADING EDGE SLAT AT OB CORNER; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, FIG. 16, PG. 67-69.SDR AWXA200301583Structure · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .0625 INCH CRACK WAS FOUND ON RT OUTBOARD MIDFLAP LEADING EDGE AT OPENING FOR EXHAUST GATE ACTUATING ROD, WBL 210. MAINTENANCE TRIMMED OUT CRACK ON RT OUTBOARD MIDFLAP LEADING EDGE WBL 210 IAW B737-300 SRM 57-53-01 FIGSDR AWXA200301576Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON FUSELAGE SKIN BONDED DOUBLER AT R-1 DOOR LOWER HINGE CUTOUT AT BS 295, STR 15 RT. MAINTENANCE REMOVED CRACKED SKIN AT R-1 DOOR LOWER HINGE CUTOUT AT BS 295, STR 15 RT; FABRICATED A DOUBLER & SDR AWXA200301639Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .0625 INCH CRACK WAS FOUND IN CENTER AFT SECTION OF LT OVERWING EMERGENCY EXIT DOOR BS 638, LBL 60. MAINTENANCE TRIMMED OUT CRACK IAW B737-300 SRM 52-20-01 FIG 101, PG SHEET 3; PERFORMED A HFEC INSPECTION TO VERIFY NO
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