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 AWXA200200024Floorbeam · corrodedMCN - MAJOR REPAIR - C - DURING C-17 CHECK MAINTENANCE DISCOVERED CORROSION ON FLOORBEAM UPPER FLANGE AT BS 986, RBL 17. REMOVED DAMAGED AREA OF FLOORBEAM UPPER T-CHORD AT BS 986, FABRICATED 2 SPLICE STRAPS, REPAIR ANGLES, NEW UPPER T-CHORD AND INSTALLED REPSDR AWXA200200023Pressure Panel · crackedMCN - MAJOR REPAIR - C - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON THE LT WHEEL WELL PRESSURE WEB AT BS 664, LBL 34. MAINTENANCE CUT OUT DAMAGED AREA OF PRESSURE WEB AND PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED. FABRICATED A DOUBLER, FILSDR AUS20011277Controller · contaminated(AUS) RUDDER CONTROL SYSTEM SUBJECT TO TWO UNCOMMANDED INPUTS. INVESTIGATION FOUND EVIDENCE OF WATER/COFFEE CONTAMINATION OF THE FORWARD E&E BAY. CONTAMINATION WAS DUE TO REMOVAL OF THE AIRSTAIRS AND DRIP TRAY LOCATED ABOVE THE E&E BAY. SERVICE BULLETIN SB 7SDR AUS20011276Controller · contaminated(AUS) PRESSURISATION SYSTEM FAULTY. PASSENGER OXYGEN MASKS DEPLOYED. INVESTIGATION FOUND EVIDENCE OF WATER/COFFEE CONTAMINATION OF THE FORWARD E&E BAY. CONTAMINATION WAS DUE TO REMOVAL OF THE AIRSTAIRS AND DRIP TRAY LOCATED ABOVE THE E&E BAY. SERVICE BULLETSDR AWAX200100591Pressure Panel · crackedPHX - MAJOR REPAIR - C - CRACK FOUND LT WHEEL WELL PRESSURE WEB BS 665, WL 202.6, LBL 32, 3 INCHES LONG. MAINTENANCE TRIMMED OUT DAMAGED AREA, FABRICATED REPAIRED DOUBLERS AND INSTALLED IAW AWA ER 03-5715-01324-TB1.SDR AWXA200100525Transmitter · arcedON APPROACH T/E FLAPS LOCKED OUT AT 5 UNITS, APPROACH WAS ABORTED. CREW FOLLOWED QRH CHECKLIST. ON RETURN FLAP POS INDICATOR NEEDLES MARRIED UP, CREW SELECTED FLAPS 10 & DOWN TO 30, PERFORMED NORMAL LANDING. MX PERFORMED T/E FLAP ASYMMETRY CHECK & T/E FLAP SDR AWXA200100524Floorbeam · corrodedMCN - C18 CK - C - CORROSION FOUND ON FLOORBEAM UPPER HORIZONTAL FLANGE AT BS 1016, LBL 6, WL 208.1, BEYOND SRM LIMITS AFTER CORROSION CLEAN UP. MAINTENANCE REPAIRED THE FLOORBEAM UPPER HORIZONTAL FLANGE IAW SRM 53-00-51 FIG 203 PG 212 - 214.SDR AWXA200100154Floorbeam · corrodedMCN - C18 CK-C, CORROSION FOUND ON FLOORBEAM UPPER HORIZONTAL FLANGE AT BS 1016, LBL 6, WL 208.1, BEYOND SRM LIMITS AFTER CORROSION CLEAN UP. MAINTENANCE REPAIRED THE FLOORBEAM UPPER HORIZONTAL FLANGE IAW SRM 53-00-51 FIG 203 PG 212 - 214.SDR AWXA200100530Floorbeam · corrodedMCN - C18 CK -C- CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT BS 967, RBL 15 TO RBL 19, BEYOND SRM LIMITS. MAINTENANCE REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 SRM 53-00-51, FIG 202, PG 207 - 211.SDR AWXA200100531Stringer · corrodedMCN - C18 CK - "C" - CORROSION FOUND ON STR 28R, BS 320 TO 323, JUST FWD OF MAIN E&E COMPARTMENT DOOR, BEYOND SRM LIMITS AFTER CLEAN UP. MAINTENANCE REMOVED DAMAGED SECTION OF STRINGER, FABRICATED REPAIR PARTS AND INSTALLED. REFERENCE B737 SRM 51-40-02, PG 4 -SDR AWXA200100515Accessory Unit · wrong partPHX - ABORTED TAKEOFF - FLT 302 - C - ON TAKEOFF ROLL AT 110 KTS THE NR 1 THRUST REVERSER OVERHEAD LIGHT ILLUMINATED AND THE T/O WAS ABORTED. THE CREW DID USE BOTH T/R'S TO SLOW THE AIRCRAFT, FUNCTIONED NORMALLY. MAINTENANCE INSPECTED THE NR 1 T/R AND PLACEDSDR AWXA200100533Web · crackedMCN - C18 CK - "C" - CRACK FOUND ON FWD PRESS. BULKHEAD AT BS 178, RBL .7, WL 188, 1.375" LONG. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR FILLER AND DOUBLER AND INSTALLED IAW B737 SRM 53-10-08, FIG 203, PG 210 - 215.SDR AWXA200100532Floorbeam · corrodedMCN - C18 CK -C- CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT BS 294.5, RBL 45.5, BEYOND SRM LIMITS AFTER CORROSION CLEAN UP. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM FROM RBL 32 TO RBL 66, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 SRM 53-10-51, SDR AWXA200100529Floorbeam · corrodedMCN - C18 CK -C- CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT BS 312, LBL 2 TO RBL 3, BEYOND SRM LIMITS. MAINTENANCE REMOVED FLOORBEAM UPPER FLANGE FROM LBL 18 TO RBL 22, FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 SRM 53-10-51, FIG 205, PG 220 - 223.SDR AWXA200100527Floorbeam · corrodedMCN - C18 CK - C - CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT BS 312, RBL 6 TO RBL 13, WL 208, BEYOND SRM LIMITS AFTER CORROSION CLEAN UP. MAINTENANCE REMOVED DAMAGED FLOORBEAM UPPER FLANGE FROM LBL 18 TO RBL 22, FABRICATED REPAIR FLOORBEAM UPPER FLANGE ANDSDR AWXA200100523Floorbeam · corrodedMCN - C18 CK - C - CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT BS 294.5, RBL 32, BEYOND SRM LIMITS AFTER CORROSION CLEAN UP. MAINTENANCE REMOVED DAMAGED FLOORBEAM UPPER CHORD, FABRICATED AND INSTALLED FLOORBEAM UPPER CHORD IAW B737 SRM 53-10-51, FIG 205, PG SDR AWXA200100528Skin · crackedMCN - C18 CK - "C" - CRACK FOUND AT L2 DOOR UPPER HINGE CUTOUT, .300 LONG AT BS 960, STR 11L, WL 252. MAINTENANCE PERFORMED REPAIR IAW B737 SRM 53-60-01, FIG 205, PG 210 - 212.SDR AWXA200100452Flap · malfunctionedSFO - FLAP LOCKOUT - FLT 815 - C - ON APPROACH TO SFO FLAPS 5 WAS SELECTED AND THE FLAP POSITION INDICATOR NEEDLES SPLIT AT FLAPS 1 AND THE FLAPS STOPPED AT FLAPS 1. THE AIRCRAFT LANDED AT FLAPS 1 AND UPON TOUCHDOWN THE FLAPS MOVED TO FLAPS 5 AS WAS SELECTED.SDR AWXA200100451Mec · out of rigPHX - ABORTED TAKEOFF - FLT 436 - C - DURING TAKEOFF ROLL THE NR 2 ENGINE WAS SLOW TO SPOOL UP, ABOUT 6 SEC SLOWER THAN NR 1 ENGINE. PMC'S AND BLEEDS WERE ON. ALL OTHER PARAMETERS WERE NORMAL. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENASDR AWXA0002239Skin · crackedD: L1 Door fuselage cutout lower aft corner cracked 1/4" out of fastener hole BS 338C: Repaired skin at L1 door cutout lower aft corner IAW AWA ER 03-5330-01234-DD1SDR AWXA0002238Shear Tie · corrodedD: Clip corroded at BS 967 between STR 27R and 26RC: Repaired shear tie at BS 967 STR 27-26R IAW B737 SRM 53-00-07 pgs 219-221SDR M522001F00000Pressure Panel · crackedLEFT HAND W/W FUS STATION 664.0 PRESSURE WEB CRACKED IN 1 LOCATIONS LBL 34.SDR AUS20010931Wire · transposed(AUS) FLIGHT CONTROL COMPUTER TO STABILISER POSITION SENSOR WIRES TOPIN 22 AND PIN 23ON CONNECTOR D4079 CROSSED.SDR AUS20010937Windshield · cracked(AUS) NR 1 WINDSHIELD LT SIDE OUTER PANE CRACKED FOLLOWING ARCING.SDR AWXA0002191Skin · crackedD: L1 door fuselage cutout lower aft corner cracked 1/4" out of fastener hole BS338.C: Repaired skin at L1 door cutout lower aft corner IAW AWA ER 03-5330-01234-DD1SDR AWXA0002247Web · crackedD: Ultrasonic crack indication RBL 4.8 WL 214 BS 178 Bulkhead web fwd side beneath strapC: Repaired Bulkhead web IAW B737 SRM 53-10-8 pgs 286-298SDR AWXA0002194Web · crackedD: Ultrasonic crack indication RBL 4.8 WL 214 BS 178 Bulkhead web fwd side beneath strap.C: Repaired Bulkhead web IAW B737 SRM 53-11-8 pgs 286-298SDR AWXA0002222Stringer · corrodedSTRINGER 25 LT AT BS 967 CORRODED. REMOVED STRINGER AND REPLACED WITH NEW STRINGER SECTION FROM BS 967 TO 1016, IAW B737-300 SRM 51-40-02 PG 10 & 11.SDR AWXA0002228Bulkhead · gougedAFT PRESSURE BULKHEAD INNER SKIN GOUGED 1 INCH OUTBOARD OF STRINGER 22R. REPAIRED AFT PRESSURE BULKHEAD IAW AWA ER 03-5312-01242-DL2.SDR AWXA0002229Skin · crackedD: L2 door fuselage upper hinge cut out cracked BS 948C: Removed damaged area and installed repair IAW 737 SRM 53-60-01 fig 205 pgs 210-212SDR AWXA0002190Skin · crackedD: L2 door fuselage upper hinge cut out cracked BS 948C: Removed damaged area and installed repair IAW 737 SRM 53-60-01 Fig 205 pgs 210-212SDR AWXA0002077Cylinder · faultyPHX-EMERGENCY LANDING -FLT 229- ON LANDING GEAR EXTENSION THE CREW HEARD A LOUD NOISE AND THE ACFT YAWED TO THE LEFT. ALL INDICATIONS WERE NORMAL AND ALL PRESSURE OK. AS A PRECAUTION THE CREW CALLED OUT EMERGENCY EQUIPMENT AND MADE AN UNEVENTFUL LANDING. MXSDR AWXA0002248Shear Tie · corrodedSHEAR TIE CORRODED AT BS 986.5 BETWEEN STR 26R-25R. REMOVED AND REPLACED SHEAR TIE IAW B737-300 SRM 51-40-02 FIG 8 & 51-40-02 PG 3.SDR AWXA0002249Skin · corrodedD: Inner skin for potable water pan cutout BS 947-967 corrodedC: Removed & replaced inner skin IAW B737-300 SRM 51-40-02 pg 3SDR AWXA0002240Strap · corrodedD: Aft LAV service door frame inner doubler corroded at BS 967, 986.5 & 1006C: Aft LAV service door inner doubler was corroded beyond limits, repaired inner doubler IAW ER 03-5313-01234-DL2SDR AWXA0002227Stringer · corrodedD: Stringer 27L corroded at BS 948 and 1003.5C: removed, repaired and reinstalled stringer IAW B737-300 SRM 51-40-02 pgs 3-4 & 38 SRM 53-00-03 pgs 201-207SDR AWXA0002225Stringer · corrodedD: Stringer 26R BS 1006-1016 corrodedC: Removed and replaced stringer IAW 737-300 SRM 51-40-60 pgs 10&11SDR AWXA0002224Stringer · corrodedD: Stringer 27R corroded at BS 965C: Removed, repaired & reinstalled stringer 27R @ BS 907-1016 IAW boeing 737 SRM 53-00-03 pg 101-102, 53-00-03 pg 201-207, 51-20-01-pgs. 1,10 & 47 & 51-40-02 pg 3-4SDR AWXA0002223Stringer · corrodedD: BS 947 STR 26L corrodedC: Removed stringer, repaired & reinstalled stringer 26L @ BS 907-1016 IAW Boeing 737 SRM 53-00-03 pg 201-207, 51-40-02 pg 3-4, 51-20-01 pg 10 & 47 & 51-21-00 pg 1SDR AWXA0002169Stringer · corrodedD: Stringer 27R corroded at BS 965C: Removed , repaired & reinstalled stringer 27R @ BS 907-1016 IAW boeing 737 SRM 53-00-03 pg 101-102, 53-00-03 pg 201-207, 51-20-01 pgs 1,10 &47 & 51-40-02 pg 3-4SDR AWXA0002168Stringer · corrodedD: BS 947 STR 26L corrodedC: Removed stringer , repaired & reinstalled stringer 26L @ BS 907-1016 IAW Boeing 737 SRM 53-00-03 pg 201-207, 51-40-02 pg 3-4, 51-20-01 pg 10 & 47 & 51-20-00 pg 1SDR AWXA0002170Stringer · corrodedD: Stringer 26R BS 1006-1016 corrodedC: removed and replaced stringer IAW 737-300 SRM 51-40-02 pgs 10-11SDR AWXA0002233Frame · crackedRT BS 178 MAIN FRAME CHORD CRACKED AFT SIDE CENTER OF RADIUS WL 206. REMOVED CHORD P/N 65-16300-87 AND INSTALLED CHORD P/N 65-16300-302 IAW ER 03-5311-01232-JS2.SDR AWXA0002232Stiffener · crackedAFT SIDE 178 BLKHD LBL 5.7 VERTICAL TEE CRACKED 1.5 INCH INBOARD SIDE. REMOVED DAMAGE FROM VERTICAL TEE AND INSTALLED REPAIR IAW 737-300 SRM 53-10-08 PG 221-240.SDR AWXA0002221Intercostal · crackedRT INTERCOSTAL CRACKED BS 178 BLKHD, RBL 24 WL 195 CONFIRMED HFEC. REMOVED AND REPLACED INTERCOSTAL IAW B737-300 SRM 51-40-02.SDR AWXA0002234Frame · crackedLT BS 178 MAIN FRAME CHORD CRACKED AFT SIDE CENTER OF RADIUS WL 206. REMOVED CHORD P/N 65-16300-87 AND INSTALL CHORD P/N 65-16300-301.SDR AWXA0002107Intercostal · crackedD: RT Intercostal cracked BS 178 BLKHD. RBL 24 WL 195 confirmed HFECC: Removed and replaced Intercostal IAW B737-300 SRM 51-40-02 pg 22SDR AWXA0002250Pressure Panel · crackedCOCKPIT FLOOR WEB CRACKED RBL 24, WL 207, BS 180. REMOVED AND REPLACED WEB P/N 65-45833U40 IAW B737 SRM 51-40-02 PG 38 AN E/R 03-5316-01218-DD1.SDR AWXA0002243Bulkhead · crackedAFT SIDE BS 178 BLKHD WEB 2 CRACKS LBL 7 AND RBL 7 WL 184. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW B737-300 SRM 53-10-08 PG 287-291.SDR AWXA0002235Bulkhead · crackedCRACK RBL,1.5 WL 205 BS 178 BLKHD WEB FWD SIDE BENEATH ANGLE. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER IAW B737-300 SRM 53-10-08 PG 286-291.
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