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 AWXA200501168Skin · delaminatedGYR - DURING C20 CHECK DISCOVERED,THE RT AFT FLAP, RT WING, ON THE INBOARD END DELAMINATED. MAINTENANCE REMOVED DAMAGED SKIN AND CORE ON THE RT AFT FLAP IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 51-70-10-2R. BOSDR AWXA200501021Switch · stuckLAS - ABORTED TAKEOFF - FLT 162 - AFTER ADVANCING THROTTLES CREW RECEIVED TAKE OFF WARNING CONFIGURATION HORN. EXITED RUNWAY AND TAXIED TO THE GATE. MAINTENANCE TROUBLESHOT AND FOUND THE STABILIZER TAKE OFF WARNING SWITCH STICKING. REMOVED AND REPLACED THE SDR AWXA200501016Battery · inoperativePHX - EEL - DURING INSPECTION DISCOVERED EMERGENCY EXIT PATHWAY LIGHTS AT ROWS 1, 2, 3, AND 4 ARE ON DIM WITH SWITCH IN OFF OR ARMED POSITION. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTER IAW MAINTENANCE MANUAL 33-51. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200500982Skin · crackedPHX - DURING 4 DAY CHECK, FOUND SKIN CRACK ON LEFT SIDE OF FUSELAGE APPROX 1' AFT AND 1' BELOW EMERGENCY LIGHT AFT OF MLG WHEEL WELL. MAINTENANCE REMOVED DAMAGED SKIN AT STA JUST FWD OF 747, STR 24L PER BOEING 737-300 SRM 51-00-01. FABRICATED DOUBLER AND INSSDR FX7A200500008Engine · overheatedENGINE NR 2 EGT REACHING 936 DEGREES AFTER TAKEOFF, IT WAS NECESSARY TO REDUCE POWER TO MAINTAIN BELOW 930 DEGREES, FIRST REDUCTION + OR - 2% N1 SECOND REDUCTION + OR - 4.5% N1, SET UP FOR 92.5% OAT 31 DEGRESS. AIRCRAFT TAKEN TO THE BLAST FENCE BY THE FLIGHT SDR AWXA200500876Skin · crackedDURING B4 CHECK, DISCOVERED CRACK IN FUSELAGE STA 947.5, STRINGER 23R, FORWARD OF THE OUTFLOW VALVE. MAINTENANCE REMOVED DAMAGED AREA AT STA 947.5, STR 23R IAW BOEING 737-300 SRM 53-00-01. FABRICATED DOUBLER IAW BOEING 737-300 SRM 53-00-01. INSTALLED FABRICSDR AWXA200500787Battery · dischargedLAS - EES - WHILE ON GROUND CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200500756Connector · dirtyON LANDING, FLAPS AT ZERO, HOT LANDING. LANDED WITHOUT FURTHER INCIDENT. CREW REPORTED FLAP PROBLEM TO TOWER PRIOR TO LANDING. CREW REQUESTED PRIORITY LANDING DUE TO FLAP PROBLEM. UPON LANDING, CREW WROTE UP FLAP INDICATOR SHOWS SPILT FLAPS AT FLAPS UP POSDR AWXA200500718Charger · inoperativeDURING C-21 CHECK EMERGENCY EXIT LIGHTS AT SEATS 1-4 INOPERATIVE AND SEAT 17 LAMP OUT. MX REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER IAW BOEING 737-300 AMM 31-51-51-962-016. OPS CHECK GOOD IAW AMERICA WEST AIRLINES TASK CARD A1C33006.SDR AWXA200500700Fitting · corrodedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND CORROSION ON LEFT MAIN LANDING GEAR STABILIZER BEAM ATTACH FITTING ON WING AT RSS 197.56. MAINTENANCE BLENDED CORROSION ON LEFT MAIN LANDING GEAR STABILIZER BEAM ATTACH FITTING AND DETERMINED TO BE OUT OF LIMITS. SDR AWXA200500699Stiffener · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK DISCOVERED 2 CRACKS .113 INCHES IN LENGTH ON ANGLE LOCATED AT BULKHEAD STA 178 LBL 5.7 WL 184. MAINTENANCE CUT OUT AND REMOVED DAMAGED AREA FROM BULKHEAD LOCATED AT STA 178. FABRICATED REPAIR ANGLES, STRAPS, FILLERS IAWSDR AWXA200500717Spar · crackedDURING C-21 CHECK, DISCOVERED RT HORIZONTAL STAB CHANNEL CRACKED ON AFT SPAR WEB AT STAB STATION 170. MX CUT OUT CRACKED SECTION ON AFT SPAR WEB AT STAB STATION 170 AND FABRICATED REPLACEMENT PARTS IAW BOEING 737-300 SRM 51-70-11-0 FIG 1. BONDED AND INSTALLESDR AWXA200500696Stiffener · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK DISCOVERED CRACK .322 INCHES LONG AT FORMED CHANNEL LOCATED AT BS 178 WL 230 RBL 17.1. MAINTENANCE REMOVED AND FABRICATED NEW CHANNEL IAW BOEING DWG 9-63089. INSTALLED FABRICATED REPAIR PARTS AT BS 178 WL 230 RBL 17.1 ISDR AWXA200500693Stiffener · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND SUPPORT ANGLE CRACKED AT BS 178 WL 230 RBL 17.1. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE AND FABRICATED SUPPORT ANGLE IAW BOEING DWG 65-17582. INSTALLED FABRICATED REPAIR PARTS AT BS 178 WL 230 RBL 17.1 IAW BOEISDR AWXA200500663Skin · crackedFUSELAGE SKIN CRACKED AT APPROXIMATELY BS 870 AND STRINGER 24R. MAINTENANCE ROUTED OUT CRACK AT BS 870 AND STRINGER 24R THEN FABRICATED DOUBLER IAW AIRBUS SRM 53-00-01 FIGURE 229. INSTALLED DOUBLER, FILLET WAS SEALED AND DOUBLER PAINTED IN REFERENCE TO AIRBUSDR AWXA200500662Skin · crackedAFT FUSELAGE FROM BS 727E TO BS 747 JUST ABOVE STRINGER 22L A 1.0 INCH SKIN CRACK WAS FOUND. MAINTENANCE REMOVED DAMAGE AREA AND OLD DOUBLER. FABRICATED REPAIR DOUBLER TRIPLER AND NEW INTERNAL LIGHT RING DOUBLER. INSTALLED FABRICATED REPAIR PARTS IAW AMERICSDR AWXA200500713Doubler · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND TOP 3 OUTBOARD SCREW HOLES ON FIRST OFFICERS NR 1 WINDOW FRAME TO HAVE EVIDENCE OF CRACKING INSIDE HOLES. MAINTENANCE REMOVED CRACKED DOUBLER IAW BOEING 737-300 SRM 53-10-01-2 FIG 210. INSTALLED REPLACEMENT DOUBLESDR AWXA200500710Skin · crackedMCN - DURING C-21 CHECK FOUND 2 CRACKS .275 INCHES IN LENGTH. BOTH CRACKS LOCATED ON THE BOTTOM OF THE NR 4 SLAT SKIN, AT SS 72 TO SS 74. MAINTENANCE CUT OUT DAMAGED AREA AT NR 4 SLAT SKIN AND FABRICATED REPAIR DOUBLER AND FILLER IAW BOEING 737-300 SRM 57-43SDR AWXA200500692Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND 3 CRACKS .271 INCHES LONG AT FRAME WEB STA 178 WL 230 RBL 17.1. MAINTENANCE REMOVED DAMAGED AREA FROM FRAME WEB STA 178 WL 230 RBL 17.1 AND FABRICATED WEB AND TAPERED SHIMS IAW BOEING 737-300 SRM 53-10-08-2 FIG 212SDR AWXA200500691Skin · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK DISCOVERED 2 CRACKS .275 INCHES LONG LOCATED AT THE BOTTOM OF THE NR 6 SLAT SKIN, SLAT STATION 307 TO SLAT STATION 309. MAINTENANCE REMOVED DAMAGED AREA FROM THE BOTTOM OF NR 6 SLAT SKIN FROM SLAT STATION 307 TO SLAT STASDR AWXA200500678Web · crackedDURING C-21 CHECK, FOUND FLOOR WEB CRACKED AT BS 196.5, WL 207, RIGHT BL 28. MAINTENANCE REMOVED CRACKED FLOOR WEB AT BS 196.5, WL 207, RIGHT BL 28 AND FABRICATED NEW WEB IAW BOEING 737-300 SRM 51-40-02 FIGURE 2 AND DWG 65-45833. INSTALLED FABRICATED REPAIR SDR AWXA200500677Web · crackedDURING C-21 CHECK, FOUND FLOOR WEB CRACKED AT BS 196.5, WL 207, LEFT BL 28. MAINTENANCE REMOVED CRACKED FLOOR WEB AT BS 196.5, WL 207, LEFT BL 28 AND FABRICATED NEW WEB IAW BOEING 737-300 SRM 51-40-02 FIGURE 2 AND DWG 65-45833. INSTALLED FABRICATED REPAIR PASDR FX7A200500006Warning Light · illuminatedAPU FIRE WARNING SWITCH LIGHT ILLUMINATED AND FIRE WARNING. INDICATION AFTER TAKEOFF, SHUT DOWN APU AND PERFORMED FALCON AIR EMERGENCY PROCEDURES.SDR AWXA200500741Skin · delaminatedFOUND DISBOND AREA ON UPPER SURFACE OF NR 5 SLAT, 1.75 IN FROM OUTBOARD END, FROM RT SS 252 TO RT SS 253. MAINTENANCE CUTOUT SKIN AND DISBOND CORE FROM UPPER SURFACE OF NR 5 SLAT, 1.75 IN FROM OUTBOARD END, IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 7, FIG 16. SDR AWXA200500690Bulkhead · crackedDURING C-21 CHECK FOUND A CRACK .275 INCHES IN LENGTH AT BULKHEAD WEB BS 178, WL 234, AND LBL 14. MAINTENANCE REMOVED CRACKED AREA AT BULKHEAD WEB BS 178, WL 234, LBL 14 AND FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2 FIG 209. INSTALLED FSDR AWXA200500689Frame · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND CRACK .211 INCHES LONG AT 178 BULKHEAD FRAME WEB, RBL 17, WL 182. MAINTENANCE REMOVED DAMAGED AREA AT BULKHEAD FRAME WEB 178, RBL 17, WL 182 AND FABRICATED NEW WEB IAW BOEING 737-300 SRM 53-10-08-2 FIGURE 212. INSSDR AWXA200500688Support Beam · corrodedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND CORROSION ON DIAGONAL SUPPORT BEAM BOTTOM SIDE AROUND FASTENER HOLES FROM BS 1006 TO BS 1016, RBL 6. MAINTENANCE BLENDED OUT CORROSION AT BS 1006 TO BS 1016, RBL 6 AND FOUND REMAINING MATERIAL TO BE OUT OF LIMITS. SDR AWXA200500719Door Frame · crackedDURING C-21 CHECK, FOUND CRACK .750 INCHES IN LENGTH AT FORWARD CARGO DOOR LOCATED ON FORWARD EDGE BELOW HOLD OPEN HOOK. MX REMOVED CRACKED CARGO DOOR FRAME IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. INSTALLED NEW FRAME ASSEMBLY IAW BOEING 737-300 SRM 51-40-02SDR AWXA200500687Angle · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND CRACK .5 INCH IN LENGTH AT R1 DOOR CUTOUT ANGLE ON BS 294.5 AND BS 294.6, BETWEEN STRINGER 7R AND STRINGER 8R. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 737-300 SRM 51-70-11 AND FABRICATED NEW ANGLE IAW BOEING 73SDR AWXA200500686Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND A CRACK .375 INCH AT 178 BULKHEAD WEB, WL 207, RBL 10. MAINTENANCE REMOVED DAMAGED AREA FROM 178 BULKHEAD WEB, WL 207, RBL 10 IAW BOEING 737-300 SRM 53-10-08 FIG 209. FABRICATED DOULBER AND INSTALLED REPAIR PARTS SDR AWXA200500679Reveal · corrodedDURING C-21 CHECK, CORROSION FOUND AT R1 DOOR CUTOUT ON FORWARD UPPER CORNER AT BS 300. CORROSION WAS FOUND TO BE OUT OF LIMITS AT R1 DOOR CUTOUT ON FORWARD UPPER CORNER AT BS 300 IAW BOEING 737-300 SRM 53-10-15 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEWSDR AWXA200500703Stop Fitting · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND L1 DOOR AFT UPPER CORNER STOP FITTING CRACKED .550 INCHES IN LENGTH AT STRINGER 8L AND BS 344. MAINTENANCE REMOVED THE DAMAGED L1 DOOR AFT UPPER STOP FITTING AND REPLACED IT IAW BOEING 737-300 SRM 51-40-02-0 FIGURESDR AWXA200500685Intercostal · corrodedDURING C-21 CHECK FOUND CORROSION AROUND SCREW HOLE AND UNDER 2 NUT PLATES AT AFT CARGO COMPARTMENT INTERCOSTAL PANEL BS 858, WL 150, RBL 23. MAINTENANCE BLENDED OUT CORROSION AND DETERMINED CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15. FABRSDR AWXA200500720Skin · debondedDURING C-21 FOUND DISBONDED AREA ON LOWER SURFACE OF RT INBOARD FORE FLAP 11.25 INCHES FROM INBOARD END AND 10 INCHES FROM AFT EDGE. DIMENSIONS OF THE DISBONDED AREA MEASURED 10 BY 8 INCHES MAKING IT OUT OF LIMITS IAW BOEING 737-300 SRM 57-53-021-1 FIG 101. RSDR AWXA200500702Skin · debondedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND DISBONDED AREA ON LOWER SURFACE OF LT OUTBOARD FORE FLAP 18 INCHES FROM INBOARD END FROM WBL 206.5 TO WBL 225.2. MAINTENANCE CUT OUT DISBONDED AREA ON LOWER SURFACE OF LT OUTBOARD FORE FLAP. FABRICATED REPLACEMENTSDR AWXA200500665Skin · debondedDURING C-21 CHECK, FOUND DISBONDED AREA ON LOWER SURFACE OF LT OUTBOARD AFT FLAP, 94 INCHES FROM INBOARD END. MAINTENANCE REMOVED AND CLEANED OUT DAMAGED AREA ON LOWER SURFACE OF LT OUTBOARD AFT FLAP. FABRICATED DOUBLER AND INSTALLED FABRICATED REPAIR PARTS SDR AWXA200500615Warning Light · illuminatedON TAKEOFF ROLL AT LAS EN ROUTE TO SJC AT APPROXIMATELY 80-100 KTS. PILOT REPORTED AN ENGINE OVERTEMP. MX COMPLIED WITH POWER ASSURANCE TEST IAW AWA TASK CARD F5M71003 AND POWER ASSURANCE CHECK TEST 5 AND TROUBLESHOOTING CHART 71-00-42-1 STEPS 1, 2, 3 AND 25SDR AWXA200500535Battery · dischargedMCI - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200500482Bracket · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK 2 INCH CRACK WAS FOUND AT FASTENER HOLE AND A 1 INCH CRACK WAS FOUND IN INBOARD FLANGE RADIUS OF GUSSET BRACKET AT FR 335, BETWEEN STR 17 LT AND STR 18 LT. MAINTENANCE REMOVED DAMAGED GUSSET BRACKET AT FR 335, BETWEEN STSDR AWXA200500489Clip · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .5625 INCH CRACK WAS FOUND ON FRAME ATTACH CLIP AT BS 827 BETWEEN STR 25 RT AND STR 26 RT. MAINTENANCE REMOVED CRACKED FRAME ATTACH CLIP AT BS 827 BETWEEN STR 25 RT AND STR 26 RT; FABRICATED A NEW REPLACEMENT CLIP PER SDR AWXA200500492Frame · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .375 INCH CRACK WAS FOUND IN FORWARD EDGE OF AFT CARGO DOOR AT FASTENER HOLES FOR PULLEY BRACKET BS 801. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME ON FORWARD EDGE OF AFT CARGO DOOR; FABRICATED A NEW REPLACEMENT FRAMSDR AWXA200500488Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE UPPER SURFACE OF THE NR 3 SLAT T/E WEDGE ASSEMBLY DELAMINATED AT SLAT STA 54 LT. MAINTENANCE CUT OUT DELAMINATED AREA OF NR 3 SLAT WEDGE UPPER SURFACE SKIN FROM SS 46.6 TO SS 63.3; FABRICATED A CORE FILLER AND SDR AWXA200500487Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE UPPER SURFACE OF THE NR 3 SLAT T/E WEDGE ASSEMBLY DELAMINATED AT SLAT STA 84 LT. MAINTENANCE CUT OUT DELAMINATED AREA OF NR 3 SLAT WEDGE UPPER SURFACE SKIN FROM SS 74.5 TO SS 94.4; FABRICATED A CORE FILLER AND SDR AWXA200500486Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE RIGHT TOP AFT SECTION OF RUDDER DELAMINATED AT RUDDER STA 238. MAINTENANCE REMOVED DELAMINATED SECTION OF RT TOP AFT RUDDER CONDUCTIVE FRAME; FABRICATED A NEW REPLACEMENT SECTION OF CONDUCTIVE FRAME PER DWG 65CSDR AWXA200500464Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 2 SLAT WEDGE WAS FOUND DELAMINATED ON THE UPPER & LOWER SURFACE AT OUTBOARD END BETWEEN SLAT STA 250.9 AND SLAT STA 254.4 LT. MAINTENANCE REMOVED DAMAGE IN UPPER AND LOWER SURFACE SKIN OF NR 2 SLAT WEDGE FROM SS 2SDR AWXA200500463Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 1 SLAT WEDGE WAS FOUND DELAMINATED ON THE UPPER & LOWER SURFACE AT SLAT STA 348 LT. MAINTENANCE REMOVED DAMAGE IN UPPER AND LOWER SURFACE SKIN OF NR 1 SLAT WEDGE FROM SS 343 TO SS 350 LT; FABRICATED A CORE FILLER SDR AWXA200500462Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 4 SLAT WEDGE WAS DELAMINATED AT THE BOTTOM OUTBOARD END BETWEEN SLAT STA 120-124 RT. MAINTENANCE REMOVED DAMAGE IN LOWER SURFACE SKIN OF NR 4 SLAT WEDGE; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLASDR AWXA200500490Skin · chafedMCN - MAJOR REPAIR - DURING C-19 CHECK THE LEFT INBOARD MID-FLAP LOWER SKIN WAS FOUND CHAFED AT WS 100. MAINTENANCE BLENDED OUT DAMAGE ON LEFT INBOARD MID-FLAP LOWER SKIN AT WS 100; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5753-05112-RC2.SDR AWXA200500493Skin · chafedMCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE LOWER CENTER SECTION SKIN OF THE LEFT OUTBOARD FORE-FLAP CHAFED AT WBL 298. MAINTENANCE CUT OUT CHAFED SKIN ON LOWER CENTER LT OUTBOARD FORE-FLAP AT WBL 298; FABRICATED NEW SKIN SECTION AND A DOUBLER; BONDED RESDR AWXA200500491Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK THE LT OUTBOARD FORE-FLAP WAS FOUND DELAMINATED AT THE UPPER AFT OUTBOARD CORNER. MAINTENANCE CUT OUT DAMAGE ON LT OUTBOARD FORE-FLAP AT UPPER AFT OUTBOARD CORNER BETWEEN WBL 410.11 AND WBL 413.6; FABRICATED A FILLER AND
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