Boeing 737-3S3
Service difficulty reports · 1,209
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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 = '7373S3' 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 = '7373S3' 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 AWXA0001209Door Frame · dentedFWD. CARGO DOOR, FWD DOOR FRAME DENTED 3 PLACES AT LOWER INSIDE END. REMOVED DAMAGED WEB IAW SRM 51-70-13 FIG 1; FABED REPLACEMENT PART IAW 51-70-13 FIG 1; INSTALLED REPLACEMENT PART IAW 51-70-13 FIG 1.SDR AWXA0001208Splice · crackedSIDE CHORD CRACKED FS 178 WL 207 RBL 26 AND WL 195 RBL 24. CUT OUT DAMAGED SECTION OF SIDE CHORD; DRILLED NEW CHORD; DRILLED NEW SPLICE ANGLE; FABED UPPER REPAIR SPLICE STRAP & INSTALLED IAW BOEING SB 737-53A1173 AND ER #03-5311-00340-JS2; HFEC INSPEC IAW B737SDR AWXA0001205Intercostal · crackedINTERCOSTAL CRACKED THRU FS 178 WL 195 LBL 24. CUT OUT DAMAGED SECTION OF INTERCOSTAL IAW SRM 53-10-08 FIG 207; HFEC - NO CRACKS NOTED; FABED REPAIR PARTS IAW 53-10-08 FIG 207; TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW 51-40-02SDR AWXA0001204Intercostal · crackedINTERCOSTAL CRACKED THRU FS 178 WL 195 RBL 24. CUT DAMAGED SECTION OF INTERCOSTAL IAW SRM 53-10-08; FABED REPAIR ANGLE, RADIUS BLOCK FILLER, AND FILLER IAW SRM 53-10-08 FIG 207; TREATED AND PRIMED PARTS IAW 51-20-01; INSTALLED PARTS IAW 51-40-02.SDR AWXA0001199Web · crackedFLOOR WEB CRACKED AT FS 180 WL 207 RBL 26. FABED AND INSTALLED FLOOR WEB IAW SRM 51-10-02 AND DWG 65-45833SDR AWXA0001198Web · crackedFLOOR WEB CRACKED FS 180 WL 207 LBL 26. FABED AND INSTALLED FLOOR WEB IAW SRM 51-10-02 AND BOEING DWG #65-45833SDR AWXA0001197Bulkhead · crackedBS 178 FWD PRESSURE BULKHEAD CENTER WEB RBL 5.7 HAS 1/2 INCH CRACK; WL 198-200 RBL 5.7 HAS 3/8 INCH CRACK UNDER STIFFENER. REMOVED DAMAGE AND INSTALLED DOUBLER AND REPAIR FILLERS IAW SRM 53-10-08 FIG 209; NDT VERIFIES CRACKS COMPLETELY REMOVED.SDR AWXA0001182Bulkhead · crackedCENTER WEB BULKHEAD 178 WL 200 LBL 537 HAS CRACK 3/8 INCH. REMOVED DAMAGE AND INSTALLED REPAIR IAW 53-10-08 FIG 209SDR AWXA0001166Skin · damagedUPPER EXTERNAL FUSELAGE STA 230 LBL 7 - LBL 9 LIGHTNING STATIC DMG WENT OUT OF LIMITS. CUTOUT DMG; FABED FILLERS & DOUBLERS; INSTALLED REPAIR PARTS IAW SRM 53-00-01 FIG 201.SDR AWXA0001106Connector · looseD: PHX - AIR TURNBACK - AFTER TAKEOFF NOTICED AIRCRAFT YAWING AND #1 ENGINE SURGING; STOPPED CLIMB AND #1 ENGINE CONTINUED TO SURGE; CREW FOLLOWED QRH AND INITIATED THEIR RETURN TO PHX; ABOUT 10 MIN. LATER THE PMC (POWER MANAGEMENT COMPUTER) INOP LIGHT ILLUMINSDR AWXA0001033Seat Track · crackedSEAT TRACK ATTACH FRAME AT STA 727A TO 727B WL 207 RBL 45 CRACKED. REPAIRED IAW AWA ER 03-5310-00335-JS2SDR AWXA0001028Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA 294 LBL 3 FOUND DURING CPCP INSPECTION EVALUATED AS LEVEL 1. CORROSION REMOVAL IAW SRM BEYOND LIMITS; REPAIRED FLOORBEAM IAW SRM 53-10-51 PG 220-222 FIG 205 SHT.3-4; PREPPED AND PAINTED IAW MM51-21-00SDR AWXA0001027Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA 328 LBL 49 AND GOUGES IN FLOORBEAM UPPER CHORD AT RBL 22 AND 35; FOUND DURING CPCP INSPECTION EVALUATED AT LEVEL 1 CORROSION. CORROSION REMOVAL IAW SRM BEYOND LIMITS, GOUGES CLEANED UP IAW SRM 53-10-51 BEYOND LIMITS; REPAIRED FLOOSDR AWXA0001001Frame · crackedD: SEVERAL CRACKS FOUND BS 178 WL 185, 195, AND 207 AT AND BETWEEN LEFT AND RIGHT BL 5.6 AND 24.00 IN SIDE CHORDS, WEB AND FLOOR PANEL STRUCTUREC: REPAIRED ALL IAW EO 53-12-07SDR AWXA0001000Skin · damagedFUSELAGE SKIN FOUND DAMAGD STA 500A STR 3L. FABED AND INSTALLED REPAIR PARTS IAW SRM 53-00-01 FIG 202SDR AWXA0000997Skin · damagedD; FUSELAGE SKIN FOUND DAMAGD STA 500A STR 31C: FABED AND INSTALLED REPAIR IAW SRM 53-00-01 FIG 202SDR AWXA0000998Frame · crackedSEVERAL CRACKS FOUND BS 178 WL 185, 195, 207 AT AND BETWEEN LEFT AND RIGHT BL 5.6 AND 24.00 IN SIDE CHORDS, WEB AND FLOOR PANEL STRUCTURE. REPAIRED ALL IAW EO 53-12-07.SDR 20001212SH013Spring · brokenSPRINGS, PN 669-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM CAUSING THE UNIT TO BIND AND JAM. POSSIBLE CAUSE, IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE AND INCREASED SPRING COIL STRESSES. SPRINGS, PN 69-77855-1, ARE TO BE REPLACED WITH PN 69-77855-2 SSDR AWXA0000191Skin · crackedC-CHECK, L-1 DOOR CUTOUT LWR AFT CORNER FUSELAGE SKIN GOUGED AND CRACKED. COMPLIED WITH REPAIR IAW AWA ER 03-5331-00055-DL1. CUT OUT DAMAGE, HFEC INSP C/W IAW B737 NTM PT 6, INSTALLED REPAIR DOUBLER, IAW BAC DWG6527257AND EO 53-44-01 REV B (PERMANENT REPAIR)SDR AWXA0000190Floorbeam · corrodedC-CHECK, CORROSION ON UPPER T CHORD OF FLOORBEAM AT FS 947 RBL 20 OUT OF LIMITS. REMOVED DAMAGED AREA IAW 737 SRM 53-00-51, FABRICATED REPAIR PARTS FROM (T-CHORD BAC 1505 -100617 7075T6, SUPPORT ANGLE BAC 1490-2236 7075T6, STRAPS .063 AND .071 7075T6). TREATSDR AWXA0000189Threshold · corrodedC-CHECK, L-2 DOOR MOP SILL CORRODED OUT OF LIMITS AT STA 957. REMOVED AND REPLACED MOP SILL IAW 737 SRM 51-40-02 (NEW PART).SDR AWXA0000188Threshold · corrodedC-CHECK, CORROSION LEVEL 1, R-2 MOP SILL CORRODED AROUND FASTENER HOLE AT FS 993 RBL 50. REMOVED AND REPLACED MOP SILL PAN IAW 737 SRM 51-40-02 (NEW PART).SDR AWXA0000187Skin · crackedC-CHECK, FUSELAGE SKIN CRACKED AT R-1 DOOR AFT LOWER CORNER. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLERS AND FILLERS, INSTALLED PARTS IAW 737 SRM 53-10-01 FIG 202. MATERIAL USED (2024T3 .063 R681615, 2024T3 .090 R710338 IAW 737 SRM 53-10-01). ALODINED AND PRSDR AWXA0000106Sensor · failedON FINAL APPROACH, RIGHT MAIN LANDING GEAR ANNUNCIATED UNSAFE (RED). AIRCRAFT WAS CONFIGURED FOR LANDING. DID FLY-BY AND LINED UP FOR FINAL LANDING, THEN GREEN GEAR SAFE LIGHT CAME ON. REPLACED DOWN LOCK SENSOR S-73. CHECKED GEAR RETRACTION SEVERAL TIMES, SDR AWXA0000089Skin · crackedR-1 DOOR FUSELAGE CUTOUT, AFT LOWER CORNER HAD .5 INCH CRACK IN CENTER OF RADIUS. STOP DRILLED CRACK AND OPENED HOLE TO .250 IAW 53-10-01. HFEC PART IAW 737 SRM 51-00-00 FIG 20, FABRICATED DOUBLER AND TRIPLER FRM (2024T3 .063 QQA 250-5 R699111) AND INSTALLEDSDR AWXA0000088Sill · corrodedR-1 DOOR SILL CORRODED FS 294.5 - 344. REMOVED AND REPLACED DOOR R-1 MOP SILL IAW 737 SRM 51-40-02 (NEW PART).SDR AWXA0000087Floorbeam · corrodedFLOORBEAM CORRODED BEYOND LIMITS AT TOP CAP STA 294.5 AT LBL 8. REMOVED DAMAGED UPPER CHORD IAW 737 SRM 53-10-51, FABRICATED SPLICE ANGLE FROM (BAC 14902734 7075T6 R673166), FLOORBEAM FROM (AND10136-2404 7075T6 R745841), INSTALLED SPLICE ANGLES AND FLOORBEAM USDR AWXA0000086Floorbeam · corrodedFLOORBEAM UPPER T CAP CORRODED BEYOND LIMITS AT STA 328 RBL 24.5 TO 60. REMOVED T CAP, FABRICATED REPAIR PARTS FROM (PINALCO 7075T6R696065), ANGLE FROM ( BAC 14902734 7075T6 R673166), 4 ANGLES FROM (BAC 14902738 7075 T6 R697241), AND RADIUS BLOCK (.125 7075SDR AWXA0000080Stringer · crackedCRACK IN STRINGERS 15 L/R AT STA 500B. REMOVED DAMAGED STRINGER SECTIONS IAW 737 SRM 53-00-03 AND 51-40-2. FABRICATED STRINGER SECTION FRM (BAC 1498-138 7075T6 X .063 QQA250/13 R626130) AND SPLICE FRM (BAC1498-132 7075T6 QQA250/13 X .063 R430819). TREATED ASDR AWXA0000079Clip · crackedSTRINGER CLIP CRACKED AT STA 706, STR 8R.. REMOVED AND REPLACED CRACKED CLIP IAW 737 SRM 51-20-02 AND 51-40-03 (NEW PART).SDR AWXA0000078Angle · corrodedAFTER BLEND OUT ON MOPSILL L-1 (REF NR 5282040 ZN ID SEQ 55) FOUND AREA OUT OF LIMITS AT FS 327. REMOVED DAMAGED PART, FABRICATED REPAIR DOUBLER FRM (7075T6 .100 QQA 250/13 R663458) IAW SRM 51-70-13. ALODINED AND PRIMED IAW 737 SRM 51-20-0. INSTALLED DOUBLESDR AWXA0000077Frame · corrodedFLOORBEAM TOP CAP CORRODED BEYOND LIMITS STA 312, LBL 45 TO RBL 10. CHORD REMOVED IAW 737 SRM 51-40-02. FABRICATED CHORD IAW 737 SRM 53-10-51 FIG 1 DETAIL V AND FIG 205 DETAIL 1/2 (MATERIAL SUBSTITUTION IAW 737 SRM 53-10-51 FIG 205 TABLE II PART 1 FLAG NOTE SDR AWXA0001175Skin · damagedTEMPORARY REPAIR DOUBLER INSTALLED AT STA 727 STR 21L. REMOVED TEMP. REPAIR; HFEC IAW B737 NTM PT.6, 51-00-00 FIG 23 - NO CRACKS NOTED; FABED REPAIR DOUBLER; INSTALLED CONICAL WASHERS; SEALED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG 202 AND 51-40-02SDR AWXA9900476Indicator · failedAIR TURN-BACK, NR 1 ENG OIL PRESS BELOW 20 PSI, OIL TEMP NML. RETURNED TO PHX PER MX. REPLACED OIL PRESS INDICATOR PER BMM 79-32-02 P401 LK AND OPS CK GOOD. OTHER PARTS CHANGED, UNIT, LUBRICATING. A/C HAS EXPERIENCED SEVERAL OIL PRESS FLUX PROBLEMS, 3 OIL SDR AWXA9900474Seat Track · damagedSEAT TRACK STA 520-634 WENT OUT OF LIMITS LBL 45. REMOVED DAMAGED SEAT TRACK PER SRM 51-40-02. FABRICATED AND INSTALLED REPLACEMENT PER SRM 53-00-52 MAT'L BAC 1520841 7178T6511 QQA-200/13C R65996, TREATED AND PRIMED.SDR AWXA9900473Stringer · crackedFWD CABIN FS 344 STR 8A RT CRACKED. REMOVED DAMAGED SECTION PER SRM 51-40-02. FABRICATED REPLACEMENT PART FRM CLAD 7075T6 QQA250/13 R642745 PER SRM 53-10-30 FIG 1. TREATED AND PRIMED PER 51-20-02. INSTALLED PER SRM 51-40-02.SDR AWXA9900472Skin · gougedRIGHT WING OTBD FORE FLAP GOUGED AT INBD UPPER SURFACE. REMOVED EXISTING DAMAGED REPAIR. FABRICATED REPAIR DOUBLER PER SRM 57-33-01 FRM .032 301 1/2 HARD R602099--CAD PLATED PER SOPM 20-42-01. INSTALLED REPAIR PER SRM 51-40-02.SDR AWXA9900436Wire · brokenROW 8L EMERGENCY AISLE LIGHT INOP. REPAIRED BROKEN WIRE.SDR AWXA9900432Warning System · activatedTAKEOFF CONFIGURATION WARNING DURING T/O ROLL, ABORTED T/O PRIOR TO 70KTS. AIRCRAFT CONFIG WAS NML FOR T/O CONDITIONS. ACCOMPLISHED TAKEOFF WARNING SYS TEST, NO DEFECTS NOTED. SAME PROBLEM OCCURED 4 NOV 99 AT DFW. CYCLED FLIGHT CONTROLS, CHECKED GOOD. NO SDR AWXA9900413Bulkhead · crackedC-CHECK, CABIN STA 663.75 LBL 32, WHEEL WELL PRESSURE DECK HAD 1 .4375 CRACK. HFEC VERIFIED CRACK. REMOVED DAMAGED AREA, FABRICATED DOUBLER, TREATED, PRIMED, AND INSTALLED PARTS PER ER 03-5310-99288-EY1. FABRICATED REPAIR DOUBLER FROM 2024T3 X .050 R700212,SDR AWXA9900412Seat Track · corrodedC-CHECK, CORROSION ON SEAT TRACK AT RIGHT OUTBD FS 500B-500D OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK PER SRM 51-40-02, FABRICATED SEAT TRACK FROM BAC 1520-792/7178T6 PER SRM 53-30-52 R659935, TREATED AND PRIMED PER SRM 51-20-01 AND INSTALLED PER SRM 51-40-SDR AWXA9900411Skin · creasedC-CHECK, TWO SMALL DENTS 5 FEET FWD OF FWD CARGO DOOR, FS 380 STR 24R. CREASE IN BOTTOM OF DENTS OUT OF LIMITS. REMOVED DAMAGE, NDT REVEALED NO CRACKS. FABRICATED REPAIR PARTS FROM 2024T3 X.063 R699111 2024T3 X.050 R697963. INSTALLED CONICAL WASHERS, ALODSDR AWXA9900410Skin · gougedC-CHECK, RIGHT O/B MID FLAP AT I/B TRACK IS GOUGED ON LWR L/E SURFACE. REMOVED DAMAGED AREA, FABRICATED REPLACEMENT DOUBLER FROM .032301 CRES 1/2 HARD MATERIAL, IAW SRM 57-53-01. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED DOUBLER IAW SRM 57-53-01.SDR AWXA9900409Skin · crackedC-CHECK, CRACK IN FUSLAGE SKIN AT LWR AFT CORNER OF R1 DOOR HAD CRACKS EXTENDING FROM 2 FASTENER HOLES. REMOVED FASTENERS AND REAMED HOLES TO .25 IAW SRM 53-10-01, HFEC REVEALED INTERIOR CRACKS, EXTERIOR CRACKS ARE CONTAINED AT FASTENER HOLES. INSTALLED FLUSSDR AWXA9900408Intercostal · corrodedC-CHECK, AFT PIT STA 787-793, STR 25R INTERCOSTAL HAD CORROSION ON UPPER FLANGE AT NUT PLATE ATTACH AREAS. REMOVED CORRODED INTERCOSTAL, FABRICATED, TREATED, AND PRIMED REPAIR PART AND INSTALLED PER SRM 53-60-15, 51-40-12 AND 51-10-1.SDR AWXA9900336Fan · failedDURING DESCENT, FA REPORTED ELECTRICAL SMELL IN AFT GALLEY, CYCLING RECIRC FAN MADE DIFFERENCE INSTANTLY. REPLACED RECIRC FAN PER MM 21-21-22 PG 401. NONE RELATED RECOMMENDATION.SDR AWXA9900317Yaw Coupler · failedLATERAL SIDE MOTION WAS NOTICED IN AIRFRAME NO CHANGE WITH AUTO PILOT, PMCS, AND YAW DAMPNER OFF. REMOVED AND REPLACED YAW DAMPNER COUPLER, MEL CLEARED.SDR AWXA9900162Pump · leakedAIR TURN BACK, HYD FLUID LOSS ME PN 03-2914-9-0003. LOSS OF 'A' SYS HYD FLUID RETURN TO PHX. FOUND A LEAK ON THE PRESSURE SIDE OF THE ELECTRIC HYD PUMP. REMOVED AND REPLACED PUMP, OPS AND LEAK CK GOOD.SDR AWXA9900069Panel · leakingEMERGENCY LANDING, INFLIGHT RIGHT WING FUEL LEAK. NON REV PILOT REPORTED FLUID LEAK ON RT WING UNDETERMINED QTY, TYPE, AND SOURCE. CAPTAIN INITIATED AN EMERGENCY LANDING. REMOVED AND REPLACED UPPER PANEL ON WING JUST AFT OF PYLON, LEAK CK GOOD, NO LEAKS.SDR AWXA9900010Skin · crackedFUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUT OUT FROM AFT EDGE TO FASTENER AND BEYOND. REPAIRED FUSELAGE SKIN PER S/B 737-53-1117.
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