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 AWXA0000411Battery Pack · dischargedEMERGENCY LIGHT OVER L-1 DOOR AND OUTSIDE R-2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY AND CHARGER OPS CHK GOODSDR AWXA0000400Wire · brokenNON ROUTINE LINE, EMERGENCY LIGHT INOP AT SEAT 3C. REPAIRED BROKEN WIRE AT CONNECTOR, OPS CHECK GOOD.SDR AWXA0000395Spar · damagedLEFT HORIZONTAL STABILIZER LEADING EDGE SPAR HAS PREVIOUS TEMPORARY REPAIR. PERFORM PERMANENT REPAIR. REMOVED LEADING EDGE, CUT OUT DAMAGED AREA FROM UPPER SPAR CHORD IAW SRM 55-10-10. FABRICATED PARTS AND INSTALLED IAW 55-10-10, 51-20-02, 51-40-02.SDR AWXA0000394Angle · crackedLEFT HORIZONTAL STABILIZER LOWER WEB ATTACH ANGLE CRACKED AT LOWER FORWARD LEADING EDGE SPAR, 4 FT FROM STABILIZER TIP. STOP DRILLED CRACK IAW SRM 55-10-09. CHECKED TERMINATION BY NDT. FABRICATED REPAIR ANGLES AND FILLERS IAW SRM 55-10-09, FIG 202. INSTALLSDR AWXA0000393Stringer · crackedRIGHT MAIN WHEEL WELL, STRINGER 18A CRACKED STA 727 FROM FASTENER HOLE TO END OF STRINGER. REMOVED AND REPLACED STRINGER 18A RIGHT CHANNEL AT FS 727, IAW SRM 51-40-02. FASTENERS SEALED IAW SRM 51-20-05.SDR AWXA0000392Seat Track · damagedSEAT TRACK GOUGED. AFTER BLEND OUT AND EVALUATION DETERMINED TRACK DAMAGE IS OUT OF LIMITS STA 368 LEFT, INBOARD. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED SECTION OF SEAT TRACK. INSTALLED SEAT TRACK IAW SRM 53-00-52, STA 340 - 420, LBL 24 - 44, LEFT ISDR AWXA0000391Seat Track · damagedSEAT TRACK GOUGED, AFTER BLEND OUT AND EVALUATION, DETERMINED TRACK DAMAGE IS OUT OF LIMITS. REMOVED DAMAGED SECTION OF SEAT TRACK BETWEEN STA 344 - 380 LEFT, IAW SRM 51-40-02. FABRICATED SECTION OF SEAT TRACK FROM BAC 1520-792. INSTALLED REPAIR SECTION IAWSDR AWXA0000390Floorbeam · corrodedCORROSION LEVEL 1, TOP OF CABIN FLOORBEAM HAS SEVERAL AREAS OF CORROSION STA 986.5 LBL 24 - 42. REMOVED AND REPLACED T CHORD FLOORBEAM, STA 986.5, LBL 24 - 42, IAW SRM 53-00-51.SDR AWXA0000389Intercostal · crackedINTERCOSTAL CRACKED AT STA 328, LBL 45. REMOVED INTERCOSTAL, REMOVED CRACKED DAMAGED AREA. FABRICATED REPAIR ANGLE IAW SRM 51-70-11. INSTALLED INTERCOSTAL AND REPAIRED ANGLE IAW SRM 51-40-02.SDR AWXA0000388Structure · corrodedCORROSION LEVEL 1, LEFT ENTRY DOOR SILL, EXFOLIATED CORROSION, SEVERAL AREAS, FS 954 - 990. REMOVED AND REPLACED AFT ENTRY MOP SILL, FS 954 - 990 IAW SRM 51-40-02.SDR AWXA0000387Skin · dentedFUSELAGE DENT, 4 AFT OF REAR CARGO DOOR. CUT OUT DAMAGED AREA, NDT PERFORMED, NO CRACKS FOUND. FABRICATED REPAIR DOUBLER FROM 2024 T3, .050. INSTALLED CONICAL WASHERS AND DOUBLER IAW SRM 53-00-01, FIG 202.SDR AWXA0000386Floor Support · corrodedCORROSION ON TOP OF CABIN FLOORBOARD SUPPORT BEAM, RBL 30 TO RBL 48, BS 960. FABRICATED AND INSTALLED FLOOR SUPPORT TOP CAP SHIM, RBL 30 TO RBL 48 BS 960, IAW SRM 53-60-51, SRM 51-20-01, SRM 51-40-02.SDR AU000911Tire · failed(AUS) LT MAIN LANDING GEAR NR 2 TIRE FAILED DUE TO FATIGUE AND SEPARATION OF THE SIDEWALL AREA. LT MLG NR 1 TIRE FAILED DUE TO OVERLOAD AS A CONSEQUENCE OF THE FAILURE OF NR 2 TIRE.SDR AWXA0000372Battery · inoperativeNON-ROUTINE LINE, OVERHEAD EMERGENCY LIGHT INOP, ROW 6L. REPLACED BATTERY POWER SUPPLY, OPS CHECK NORMAL.SDR AWXA0000371Light · brokenNON ROUTINE LINE, EMERGENCY LIGHT BROKEN AT ROW 18L. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, OPS CHK GOOD.SDR AU000451Windshield · cracked(AUS) FIRST OFFICERS NO1 WINDOW OUTER PANE CRACKED.SDR AWXA0000258Pressure Panel · crackedC-CHECK, LT WHEEL WELL PRESSURE WEB HAS 2 CRACKS STA 663 LBL 33. FAB''D DOUBLER, ANGLE, AND FILLERS FROM 2024T3 .050 AND 7075 T6 .063. TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW ER 03-5310-0090-DL1.SDR AWXA0000257Battery Pack · inoperativeC-CHECK, FWD EMERGENCY LIGHT POWER SUPPLY FOR L-1 DOOR INOP. REMOVED AND REPLACED PWR SUPPLY IAW 737 MM 33-51-51, OPS CK GOOD.SDR AWXA0000256Intercostal · crackedC-CHECK, INTERCOSTAL CRACKED AT BS 178 RBL 25 WL 16. REMOVED DAMAGED PART IAW 737 SRM 51-40-01, FAB'' D REPAIR PART FROM 2024T3 .063 IAW 737 SRM 53-10-08 FIG 204. TREATED AND PRIMED PARTS IAW 737 SRM 51-20-01, INSTALLED IAW 737 SRM 53-10-08.SDR AWXA0000255Intercostal · crackedC-CHECK, INTERCOSTAL CRACKED AT BS 178 LBL 25 WL 16. REMOVED DAMAGED INTERCOSTAL IAW 737 SRM 51-40-01, FAB''D REPAIR INTERCOSTAL FROM 2024T3 .063 QQA 250/13 IAW 737 SRM 53-10-08. FAB''D DOUBLER AND COVER PLATE FROM 2024T3 .125 QQA 250/5, FAB''D RADIUS FILLERSDR AWXA0000254Skin · crackedC-CHECK, HFEC INSPECTION DETECTED 2 INCH CRACK AT THE LOWER AFT CORNER OF R-1 DOOR CUTOUT. FAB''D, DRILLED AND INSTALLED -1, -2, AND -5 PLATES IAW 737 SRM 53-10-01 FIG 202. TREATED AND PRIMED PARTS IAW 737 SRM 51-20-01.SDR AWXA0000253Skin · crackedC-CHECK, EXTERNAL FUSLAGE FS 747 STR 21L SKIN CRACKED. REMOVED DAMAGED SECTION IAW 737 SRM 51-40-02, FAB''D DOUBLER ..090 2024T3 QQA 250/5 AND FILLER .071 2024T3 QQA250/5 IAW 737 SRM 53-00-01, TREATED AND PRIMED IAW 737 SRM 51-20-01, INSTALLED IAW 51-40-02.SDR AWXA0000243Frame · corrodedC-CHECK, LEVEL 1 CORROSION AFT PRESS BULKHEAD CHORD AT RBL 2 IN BILGE AREA. REMOVED DAMAGED CHORD SEGMENT AND REPAIRED IAW ER 03-5312-00075-022 AND 737 SRM 53-80-08 FIG 206.SDR AWXA0000242Stiffener · corrodedC-CHECK, LEVEL 1 CORROSION FS 1016 AFT PRESS BULKHEAD BELOW FLOOR ON STIFFENER AT CENTERLINE RT SIDE. REMOVED DAMAGED AREA, FABRICATED STIFFENER AND FILLER FROM SHT 2024 T3 .040 QQA250/5, TREATED, PRIMED, AND INSTALLED IAW 737 SRMS 51-70-11 FIG 1, 51-20-01, ASDR AWXA0000241Bulkhead · corrodedC-CHECK, LEVEL 1 CORROSION AFT PRESSURE BULKHEAD BELOW BL 0 TO RBL 3. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS FROM 2024 T3 .032 IAW 737 SRM 53-80-08 FIG 201. INSTALLED PARTS IAW 737 SRM 53-80-08.SDR AWXA0000240Skin · delaminatedC-CHECK, LT WING I/B MID FLAP HAS AREA OF DELAMINATION 36 INCHES I/B FROM O/B END AND 2.5 INCHES UP FROM T/E UPPER AND LOWER SURFACE. REMOVED DELAMINATED SECTION, POTTED CORE DAMAGE AND FABRICATED DOUBLER IAW 737 SRM 57-53-00 AND 51-70-10 BONDED USING HOT BONSDR AWXA0000239Floorbeam · crackedC-CHECK, REPAIR DOUBLER ON AFT FACE OF FLOORBEAM AT BS 520 LBL 45.5 CRACKED IN RADIUS .5 INCH. REMOVED DAMAGED DOUBLER AND REPAIRED IAW AWA EO 53-14-12.SDR AWXA0000238Floorbeam · corrodedC-CHECK, FLOOR SUPPORT AT FS 950 LBL 50 - LBL 20 CORRODED AT FASTENER HOLES. REMOVED AND REPLACED DAMAGED PARTS IAW 737 SRM 51-40-02, FABRICATED SUPPORT FROM BAC 1506-43 7050 T76511, SHIM 7075T6 .080 IAW 737 SRM 51-40-02, TREATED AND PRIMED IAW 737 SRM 53-60-SDR AWXA0000237Floorbeam · corrodedC-CHECK, TOP SURFACE OF FLOOR SUPPORT BEAM FROM FS 1016 LBL 5 TO FS 986 LBL 20 HAS EXFOLIATED CORROSION. REMOVED AND REPLACED FLOOR SUPPORT IAW 737 SRM 51-40-02, FABRICATED REPAIR PARTS IAW 737 SRM 51-20-02 FROM 2024T3 .063 7075T6 .125, TREATED AND PRIMED IAWSDR AWXA0000236Floorbeam · corrodedC-CHECK, STA 1016 FLOORBEAM UPPER T FLANGE CORRODED AT LBL 5. CUT OUT DAMAGED AREA IAW 737 SRM 53-00-5, FABRICATED REPAIR SECTION FROM (BAC 1505-100617 7075T73), TREATED AND PRIMED IAW 737 SRM 51-20-01, INSTALLED IAW 737 SRM 51-40-02, PARTS ALODINED AND PRIMESDR AWXA0000235Floorbeam · corrodedC-CHECK, FS 967 RBL 44 UPPER T-CAP CORRODED. CUT OUT DAMAGED AREA 737 SRM 53-30-51, FABRICATED REPAIR PARTS IAW 737 SRM 53-30-51, INSTALLED PARTS IAW 737 SRM 53-30-51 FIG 202, MAT''L USED ANGLE, BAC 1490-2887 7075T6 FILLER .125 7075 T6.SDR AWXA0000234Floorbeam · corrodedC-CHECK, FLOORBEAM AT BS 967 RBL 6 CORRODED. CUT OUT DAMAGED AREA, FABRICATED REPLACEMENT PARTS IAW 737 SRM 53-00-51, TREATED AND PRIMED IAW 737 SRM 51-20-02, INSTALLED REPAIR PARTS IAW 737 SRM 51-40-02, MAT USED: SUPPORT ANGLE BAC 1505-100617, STRAPS .063 QSDR AWXA0000233Floorbeam · corrodedC-CHECK, FLOORBEAM FS 1006 CORRODED AT FASTENER HOLE RBL 12. REMOVED DAMAGED AREA IAW 737 SRM 53-00-51 FIG 202, FABRICATED REPAIR STRAP FROM .125 7075 T6, ALODINED AND PRIMED STRAP, INSTALLED STRAP IAW 737 SRM 53-00-51 FIG 202.SDR AWXA0000232Threshold · corrodedC-CHECK, L-2 DOOR MOP SILL ANGLE HAS EXFOLIATING INTERGRANULAR CORROSION AT DOOR THRESHOLD AREA. REMOVED AND REPLACED L-2 MOPSILL IAW 737 SRM 51-40-02 AND SRM 51-20-02 (NEW PART).SDR AWXA0000231Skin · crackedC-CHECK, L-1 DOOR LOWER HINGE CUTOUT IN FUSELAGE SKIN HAS VISUAL INDICATION OF CRACK. HFEC INSP IAW 737 NTM PT 6, STOP DRILLED .25 INCH CRACK IAW 737 SRM 53-10-01, FABRICATED REINFORCING PLATE DOUBLER FROM SHT 301 1/2H .063, INSTALLED IAW 737 SRM 51-40-21 ANDSDR AWXA0000230Floorbeam · corrodedC-CHECK, FLOORBEAM AT 986.5 TOP T-ANGLE CORRODED FROM RBL 20 TO LBL 20 (PREVIOUS REPAIR). REMOVED DAMAGED SECTION IAW 737 SRM 53-00-51, FABRICATED PART AND INSTALLED IAW 737 SRM 53-00-51 AND 51-40-02, ALODINED AND PRIMED PARTS IAW 737 SRM 51-10-02, MAT USED: SDR AWXA0000210Circuit Breaker · failedCO-PILOTS FWD WINDOW HT OVERHEATS AND POPS C/B. HISTORY: WINDOW AND PITOT HEAT MODULE WAS REMOVED AND REPLACED FOR LP 7366891 AND RERACKED FOR LP 636890 ON PREVIOUS FLIGHTS 30 MAR00. CHECKED WINDOW ELEMENT FOR RESISTANCE AND CORRECT INSTALLATION, OK. REPLASDR AU000399Post · cracked(AUS) LT COCKPIT C-D WINDOW POST CRACKED. CRACK LENGTH 6.35MM (0.25IN). FOUND DURING INSPECTION IAW ER B73-53-10-6 (AD/B737/12).SDR AU000122Post · cracked(AUS) LT C/D WINDOW POST CRACKED. CRACK LENGTH 6.35MM (0.25IN). FOUND DURING INSPECTION IAW ER B73-53-10-16.SDR AU000145Structure · corroded(AUS) LEVEL 2 CORROSION FOUND AS A RESULT OF AD/B737/52 AMDT6.SDR AWXA0000066Light · inoperativeNON-ROUTINE LINE, EMERGENCY LIGHTING. EMERGENCY EXIT PATH WAY SIGN HAS INOP LIGHTS, AT L-2 DOORWAY. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY, OPS CHECK GOOD.SDR AWXA0000051Intercostal · crackedC-CHECK, MAIN CABIN, FWD AND ABOVE L-1 ENTRY FS 303 STR 4L INTERCOSTAL WEB AND SPLICE STRAP WERE CRACKED. REMOVED INTERCOSTAL WEB AND SPLICE STRAP IAW 737 SRM 51-40-2, FABRICATED WEB FRM ( 7075T6.090 R676547) AND STRAP FROM 7075T6 .063 R 6565687) IAW 737 SRM SDR AWXA0000050Skin · crackedC-CHECK, FUSELAGE SKIN HAD SUSPECTED CRACK 2 INCHES BELOW STR 25R, EXTENDING FROM STA 727D + 2 AFT 3 TO 727 D+5. REMOVED DAMAGED AREA PER 737 SRM 53-00-01, NDT HFEC AROUND CUT-OUT IAW B737 NTM PT 6, 51-00-01. NO FURTHER CRACKS. FABRICATED REPAIR DOUBLER IAWSDR AWXA0000049Floorbeam · corrodedC-CHECK CORROSION LEVEL 1, FLOORBEAM AT STA 328 RBL 25 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA IAW 737SRM 53-30-51, FABRICATED REPAIR PARTS FROM (7075T6 .071 R672214 QQA 250/135, 7075T6 .100 QQA 250/13 R684229 AND 7075T .080 QQA 250/13E R692255). ISDR AWXA0000048Floorbeam · corrodedC-CHECK CORROSION LEVEL 1, FLOORBEAM AT BS 294.5 LBL 10, CORROSION OUT OF LIMITS. REMOVED DAMAGED SECTION OF T CHORD IAW 737 SRM 53-10-51. FABRICATED REPAIR PARTS IAW 737 SRM 53-10-17 FRM (T BAC 505-101303 7075T6 R678532, AND BAC1490 2865 7075 T6 .071 R6722SDR AWXA0000047Skin · crackedC-CHECK, FOUND CRACK, EXTERNAL DOOR PERIMETER SKIN AT R-1 DOOR AFT LOWER CORNER HAS A 1.5 CRACK EXTENDING FROM TOP CORNER. CUT OUT DAMAGED AREA IAW 737 SRM 53-10-01, HFEC IAW B737 51-00-00 FIG 23. NO CRACKS NOTED, FABRICATED REPAIR PARTS PER TRAVELERS IAW 73SDR AWXA0000046Intercostal · crackedC-CHECK, FOUND CRACK, STA 328 LBL 47 (CABIN AREA) TOP OF FLOOR SUPPORT BEAM IS CRACKED AND PEICE MISSING. REMOVED DAMAGED INTERCOSTAL AND ANGLE IAW 737 SRM 51-40-02. FABRICATED REPLACEMENT INTERCOSTAL AND ANGLE IAW 373 SRM 53-10-51 FIG 1 FRM (7075 T-6 SDR AWXA0000042Accessory Unit · failedAIR-TURNBACK, WING-TO-BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT AND FLICKERED ON TAKEOFF, WENT OUT UPON RETURN TO PHX. REMOVED AND REPLACED COMPARTMENT OVERHEAT M237 UNIT. OPS CHECK GOOD. A/C HAD EXACT MALFUNCTION (INFO ONLY), QRH PROCEDURES WERE FOLLOWED UNSDR AWXA0000022Warning System · malfunctionedABORTED TAKEOFF LP 7575554, REJECTED TAKEOFF AT 80KTS, SHAKER BEGAN AT APPROX 60KTS AND CEASED AFTER DECELERATION BELOW 60KTS. FOUND FLAP POSITION, N1, AND N2 FAULTS ON BOTH STALL WARNING COMPUTERS. CLEARED MEMORY AND PERFORMED STALL WARNING SYSTEM ADJ/TEST,SDR AWXA0000018Generator · malfunctionedDIVERSION FOR ELECTRICAL PWR LOSS, REF LP 7583866, APPROX 1.4 HRS INTO FLIGHT NR 1 EFIS SCREENS WENT BLANK, STBY PWR AC BUS WENT TO ZERO VOLTS, ZERO FREQS, PRESSURIZATION FAILED; AFTER 5 SECS IT ALL CAME BACK, NR 1 BUS ALSO FLICKERED OFF. REPLACED TRANSFER R
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