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 AWXA0001734Bulkhead · crackedFWD BLKHD AT STA 178 HAS A CRACK INDICATION AT APPROX RBL 10 WL 234 FWD EXTERIOR SURFACE. REPAIRED IAW SRM 53-10-08 FIG 209 DETAIL 2.SDR AWXA0001733Floorbeam · corrodedFLOORBEAM AT STA 294.5 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-10-08 AND 53-10-51.SDR AWXA0001732Frame · crackedFWD BLKHD STA 178 LT SIDE CHORD CRACKED AT WL 207. REMOVED AND REPLACED CHORD IAW SRM 51-40-02.SDR AWXA0001731Frame · crackedFWD BLKHD STA 178 RT SIDE CHORD CRACKED WL 207. REMOVED AND REPLACED SIDE CHORD IAW SRM 51-40-02.SDR AWXA0001727Actuator · failedPHX - AIR TURNBACK, AFTER TAKEOFF THE FLAPS WERE RETRACTED BUT L/E FLAPS TRANSIT LIGHT ON FORWARD PANEL AND NR 1 SLAT INDICATOR ON THE OVERHEAD PANEL REMAINED ILLUMINATED. FLAPS WERE CYCLED BACK TO 1 & THEN UP SEVERAL TIMES. PILOT VISUALLY CONFIRMED THAT NR SDR AUS20010403Skin · corroded(AUS) LT AND RT WING UPPER SKIN LOWER SURFACES AND TOP STRINGERS IN AREA BETWEEN WS557 AND WS583. CORROSION ALSO EVIDENT ON RH REAR SPAR LOWER FLANGE IN AREA BETWEEN WS576 AND WS580.SDR AWXA0001691Floorbeam · corrodedTHREE SPOTS OF CORROSION ON UPPER FLANGE OF FLOORBEAM BS 294 RBL 28-31. REMOVED CORRODED SECTION; FORMED AND INSTALLED SECTION OF UPPER T-CHORD IAW B737 SRM 51-20-01 PG 1 AND 51-40-05 PG 3 AND 53-10-08 PG 12 AND 53-00-51 PG 207 AND 51-10-02 PG 2.SDR AWXA0001692Bulkhead · crackedBS 178 BLKHD WEB RBL 5 WL 200 HAS A .60 INCH CRACK EMANATING FROM BENEATH THE STRAP. CUT OUT DAMAGED WEB AREA; LOCATED, DRILLED, INSTALLED REPAIR DOUBLER AND FILLER IAW B737 SRM 53-10-08 TR 53-15 PG 1-11.SDR AWXA0001690Structure · crackedFS 837 AFT CARGO DOOR, CRACK AT LWR CROSS BEAM, LOWER TEE, VERT LEG, 3RD HI-LOK FROM END BEAM. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR FILLERS, DOUBLERS AND STRAPS IAW AWA EO 52-33-01 REV D PG 1-15.SDR AWXA0001689Stiffener · corrodedFS 294 TEE CAP STIFFENER CORRODED RBL 28-43. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED NEW TEE CAP STIFFENER IAW B737-300 SRM 51-40-02 PG 1-10.SDR AWXA0001688Web · crackedFS 178 COCKPIT FLOOR WEB CRACKED AT RBL 23 WL 207. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED NEW WEB SECTION IAW B737-300 SRM 51-40-02 PG 1-6 & 51-10-02 PG 15.SDR AWXA0001687Stiffener · corrodedFS 1153 TORQUE BOX LEFT LWR O/B EDGE OF STIFFENER. CUT OUT DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 51-70-13 FIG 1 PG 1.SDR AWXA0001686Bulkhead · crackedFS 178 BLKHD CRACKED 2 PLACES LBL 4 & 1.2, RBL 8 WL 187-188. CUT OUT DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-08 TR 53-15 PG 1-11.SDR AWXA0001685Skin · crackedAFT CARGO COMPT UPPER LINER SKIN CRACKED AT CENTER LIGHTENING HOLE. LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 51-40-02 PG 3.SDR AWXA0001684Bulkhead · crackedFS 178 BLKHD CRACK AT WL 202.5 RBL 4.8. CUT OUT DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-08 TR 53-15 PG 1-11.SDR AWXA0001683Bulkhead · crackedFS 178 BLKHD CRACKED AT WL 234.1 RBL 7.8-9.7. CUT OUT DAMAGED AREA, LOCATED, DRILLED, AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-08 PG 265-269.SDR AWXA0001682Frame · crackedFS 178 BLKHD CRACK AT WL 187-230 CENTER OF RADIUS. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SIDE CHORD IAW B737-300 SRM 51-10-02 PG 15 & 51-40-02 PG 1, 10.SDR AWXA0001681Skin · corrodedBLIND RIVET REPAIR FORWARD OF AFT PRESSURE BLKHD BS 1012 STR 23L WL 182. REMOVED DOUBLER REPAIR WITH BLIND FASTENERS; FORMED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 51-20-01, 53-00-01 FIG 202 PG 204.SDR AWXA0001680Bulkhead · crackedFS 178 BLKHD CRACK AT WL 202.4 LBL 4.5. CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 51-10-08 TR 53-15 PG 1-11.SDR AWXA0001679Floorbeam · corrodedCORROSION ON AFT CORNER OF TRACK SECTION AND UPPER FLANGE OF FLOORBEAM AT BS 294 RBL 12-14; CORROSION REMOVAL OUT OF LIMITS. REMOVED FLOORBEAM T-CAP SECTION; LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW T-CAP UPPER CORD IAW B737 SRM 51-40-05 PG 7 AND 5SDR AUS20010445Drag Brace · cracked(AUS) NOSE LANDING GEAR UPPER DRAG BRACE CRACKED AT RETRACTION ACTUATOR ATTACHMENT. CRACK WAS DETECTED VISUALLY.SDR AUS20010543Indicator · faulty(AUS) FLAP POSITION INDICATOR GAVE CONFLICTING LH AND RH FLAP POSITIONS ALTHOUGH THERE WAS NO EFFECT ON ROLL CONTROL. INSPECTION OF THE INDICATOR REVEALED MINOR FAULTS BUT THE INDICATOR WAS OK AND NOTLIKELY TO HAVE CAUSED THE FAULT.SDR AU010387Indicator · faulty(AUS) FLAP POSITION INDICATOR FAULTY.SDR AWXA0001650Bulkhead · crackedFS 178 BLKHD HAS 1 INCH CRACK AT WL 197-198 LBL 4.8. CUT OUT DAMAGED WEB; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08 TR 53-15 PG 1-11.SDR AWXA0001654Bulkhead · crackedFS 178.5 BLKHD CRACK AT WL 188 LBL 5.7. CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW AWA ER 03-5313-01109-TB1.SDR AWXA0001653Bulkhead · crackedFS 178 BLKHD HAS 1 INCH CRACK AT WL 206 RBL .6-1.8. CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-08 TR 53-15 PG 1-11.SDR AWXA0001652Bulkhead · crackedFS 178 BLKHD HAS 1.5 INCH CRACK AT WL 200.3 LBL 5. CUT OUT DAMAGD AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-10-08 TR 53-15 PG 1-11.SDR AWXA0001651Web · puncturedPUNCTURE IN VERT WEB RBL 44 FS 311.CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-11 PG 1 AND 51-20-01 PG 1 AND 51-40-02 PG 3 & 4.SDR AWXA0001649Bulkhead · canningFS 178 OIL CANNING AT WL 188-207 LBL 5 TO RBL 5. LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-08 PG 1-11.SDR AWXA0001644Bulkhead · crackedHFEC INDICATES .5 INCH CRACK EMANATING FROM BENEATH STRAP IN WEB BS 178 BLKHD RBL 6.8 WL 212.5 CONFIRMED 10X VISUAL. CUT OUT DAMAGED WEB AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B737-300 SRM 53-10-08.SDR AWXA0001629Bulkhead · crackedHFEC INDICATES CRACK AT FASTENER HOLE LBL 10 WL 234.1 BS 179 BLKHD WEB FORWARD SIDE. CUT OUT DAMAGED SKIN AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B737-300 SRM 53-10-08.SDR AWXA0001628Pressure Panel · crackedLEFT MLG W/W PRESSURE WEB CRACKED AT BS 663 APPROX BL 32. REMOVED UPPER ATTACH CHANNEL; TRIMMED OUT DAMAGED PORTION OF WEB; FABBED REPAIR -1 DOUBLER, -2 FILLER AND -3 STIFFENER; TREATED AND PRIMED REPAIR PARTS; INSTALLED REPAIR AND THE UPPER ATTACH CHANNEL IASDR AU010336Controller · faulty(AUS) DURING APPROACH FLAPS RAN TO 20 DEGREES ON SELECTION OF 25DEGREES. SELECTION TO 30 DEGREES SAW NO FURTHER MOVEMENT. INVESTIGATION COULD FIND NO FAULTS. SUSPECT CAUSED BY MOISTURE IN FLAP DRIVES.SDR AUS20010942Structure · corroded(AUS) CORROSION CONTROL INSPECTION FOUND AREAS OF LEVEL 2 CORROSION.FOUND DURING INSPECTION IAW AD/B737/52 AMDT2.SDR AU010302Spar · corroded(AUS) RT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD CORRODED AT STN 267.50. LT HORIZONTAL STABILISER REAR SPAR UPPER CHORD CORRODED AT STN 258.SDR AWXA0001532Actuator · failedIAH - EMERGENCY LANDING - 3/18/01 - EN ROUTE FROM PHX TO IAH PRIOR TO DESCENT THE L/E FLAP TRANSIT AMBER LIGHT CAME ON AND REMAINED ILLUMINATED; THE CREW LANDED IN IAH W/ FLAPS 15 PER THE QRH. MAINTENANCE FOUND THE SLAT CONTROL VALVE CABLE TENSIONS HIGH AND ASDR AUS20010532Turbine · failed(AUS) APU TURBINE WHEEL DISINTEGRATED. SUSPECT CAUSED WAS A BI-HUBFAILURE OF THE TURBINE WHEEL DUE TO UNDETECTABLE HANIUM OXIDE INCLUSION FORMED DURING THE CASTING PROCESS.SDR AWXA0001484Engine · malfunctionedPHX - EMERGENCY LANDING - 3/5/01 - INBOUND TO PHX THE AIRCRAFT WAS DESCENDING AT 210 KTS AS DIRECTED BY THE FMC, THE CREW SELECTED 250 KTS MANUALLY AND THE AIRCRAFT YAWED TO THE RIGHT; THE FIRST OFFICER REPORTED NR 2 ENGINE FAILURE. THE CREW THEN STARTED TO GSDR AWXA0001483Fire Loop · out of positionPHX - AIR TURNBACK - 3/5/01 - ON CLIMBOUT AT FL270 W/ FULL POWER, THE RT WING BODY OVERHEAT LIGHT ILLUMINATED; W/ THE ISOLATION VALVE CLOSED AND RIGHT BLEED OFF THE LIGHT EXTINGUISHED. MAINTENANCE TROUBLESHOT AND FOUND FIRE LOOP IN NR 2 PYLON TO CLOSE TO THE SDR AUS20010664Roller · seized(AUS) PASSENGER DOOR R1 SEQUENCING CAM ROLLER SEIZED AND DISINTEGRATEDPREVENTING CORRECT OPERATION OF DOOR.SDR AUS20010533Turbine · failed(AUS) APU TURBINE WHEEL DISINTEGRATED. SUSPECT CAUSED BY TENSILEOVERLOAD ORIGINATING FROM AN UNDETECTABLE SINGLE HAFNIUM OXIDEDROSS CASTING INCLUSION.SDR AWXA0001454Anti-Ice Valve · failedPHX - AIR TURNBACK - 2/26/01 - EN ROUTE FROM PHX TO DEN WHEN THE LEFT ENGINE ANTI-ICE WAS SELECTED ON THE BLUE LIGHT REMAINED BRIGHT WITH NO INCREASE IN N2; THE AIRCRAFT RETURNED TO PHX. IN PHX MAINTENANCE TROUBLESHOT AND FOUND THE ANTI-ICE VALVE HAD FAILED ISDR AWXA0001413Door · not closedPHX - ABORTED TAKEOFF - 2/19/01 - AT START OF POWER UP FOR TAKEOFF ROLL THE FWD CARGO DOOR ANNUNCIATOR LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO GATE. AT THE GATE A LARGE PIECE OF BAGGAGE WAS FOUND ON TOP OF THE INSIDE DOOR HANDSDR AUS20010547Control Cable · failed(AUS) NR 3 FLIGHT SPOILER CONTROL CABLE BROKEN IN THE AREA OF WBL 73.00LT. THE CABLE FAILED APPROXIMATELY 203.2MM (8IN) OUTBOARD OF THETURNBARREL. THE FAILURE WAS A RESULT OF RUST (CORROSION) AND WEAR SUSPECT DUE TO INADEQUATE REAPPLICATION OF PROTECTIVE INHIBSDR AWXA0001297Skin · crackedR-1 DOOR FRAME LOWER AFT CORNER SKIN IS CRACKED; EMINATING FROM FASTENER TRAVELING TOWARD RADIUS. STOP DRILLED CRACK; FABED REPAIR DOUBLERS; DRILLED, TREATED, PRIMED, AND INSTALLED IAW B737-300 SRM 53-10-01 PG 204.SDR AWXA0001296Skin · chafedRT WING O/B MID FLAP HAS A CHAFED AREA AT I/B FLAP TRACK ON LOWER SKIN. REPAIRED IAW AWA ER 03-5754-01027.SDR AWXA0001295Skin · chafedLT WING O/B MID FLAP HAS A CHAFED AREA AT I/B FLAP TRACK ON LOWER SKIN. REPAIRED IAW AWA ER 03-5754-01027.SDR AWXA0001294Doubler · crackedCRACK IN RT WING INBOARD L/E SKIN JUST ABOVE INBOARD END OF L/E FLAP SEAL DOOR. CUT OUT CRACKED AREA; HFEC PERFORMED; FABED FILLER AND INTERNAL DOUBLER; INSTALLED IAW AWA ER 03-5741-01027-SS1 AND B737-300 SRM 57-41-01.SDR AWXA0001293Floor Support · damagedSUSPECT CRACK IN LEFT W/W AT STA 664.75 BL 33 UPPER PRESSURE PANEL. HFEC PERFORMED; CUTOUT DAMAGED AREA; FABED REPAIR DOUBLER, FILLER AND STIFFENER; INSTALLED IAW AWA ER 03-5710-01025-JS1 AND B737-300 SRM 51-00-00 FIG 23, 51-10-02, 51-20-01.SDR AWXA0001292Skin · crackedL-2 DOOR UPPER HINGE CUTOUT SKIN IS CRACKED.CUTOUT DAMAGED FUSELAGE SKIN; FABED REPAIR DOUBLER AND FILLER; DRILLED ATTACHMENT LOCATIONS; TREATED AND PRIMED REPAIR PARTS; INSTALLED REPAIR IAW B737 SRM 53-60-01 FIG 205.
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