N306WA, cancelled May 4, 2007
Service difficulty reports · 23
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N306WA' AND deregistration_id = 'N306WA-2007-05-04' 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 n_number = 'N306WA' AND deregistration_id = 'N306WA-2007-05-04' 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 DL733060250Stiffener · crackedDURING ACCOMPLISHMENT OF 05-086589-12AD, THE WING CENTER SECTION REAR SPAR STIFFENER AT LBL 6.15 WAS FOUND CRACKED. REPLACED REAR SPAR STIFFENER.SDR DL733050148Skin · crackedTHE FUSELAGE SKIN WAS FOUND WITH A 4 INCH CRACK AT FS 870 JUST ABOVE THE BONDED DOUBLER MILL LINE AT STRINGER 23R. THE CRACK IS TYPICAL OF AD 2004-18-06. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-300 SSDR DL733030081Coffeemaker · odorFLT ATTENDANT VERBAL REPORT, LT AFT GALLEY COFFEEMAKER HAS ELECTRIC ODOR. REPLACED COFFEEMAKER, OPS CHECK NORMAL. NO ODOR.SDR DL733021369Attach Fitting · corrodedCORROSION WAS FOUND ON THE AFT FACE OF THE #3 LUG AND THE FORWARD FACE OF THE #6 LUG OF THE VERTICAL STABILIZER FIN ATTACH LUGS. THE CORROSION WAS REMOVED AND NEW BUSHINGS INSTALLED. THE DAMAGE WAS FOUND AT HMV.SDR DL733021368Skin Panel · crackedSEVERAL CRACKS WERE FOUND IN THE KEEL BEAM LOWER SKIN PANEL FROM FS 661 TO FS 727. THE SKIN PANEL WAS REPLACED PER S/B 737-53-1104. THE DAMAGE WAS FOUND AT HMV.SDR DL733021367Fitting · corrodedCORROSION WAS FOUND IN THE LUB BORE OF THE LHS FORWARD CLEVIS LUG. THE LUG BORE WAS OVERSIZED TO 1.4385" AND AN OVERSIZED BUSHING WAS INSTALLED. THE DAMAGE WAS FOUND AT HMV.SDR DL733021366Wedge · delaminatedRH INBD MID FLAP T/E WEDGE DISBONDED. REPAIRED PER ER/A 418047-14.SDR DL733021365Wedge · delaminatedTE WEDGE DISBONDED. REPAIRED PER ER/A 418046-14.SDR DL733021347Beam · wornWORN AREAS WERE FOUND ON THE CROWN BEAM LUG BORES OF THE #1 AND #2 PYLONS. THE BORES WERE OVERSIZED TO 3.100" AND 3.102 RESPECTIVELY. REPAIR BUSHINGS WERE INSTALLED. THE DAMAGE WAS FOUND AT HMV.SDR DL733021346Spar · damagedWHILE REPLACING THE MLG BEAM SUPPORT FITTING A FASTENER HOLE WAS DAMAGED IN THE REAR SPAR CHORD AND REAR SPAR WEB. THE HOLE WAS OVERSIZED AND A REPAIR BUSHING INSTALLED.SDR DL733021059Skin · delaminatedRT WING INBOARD MID FLAP WEDGE IS DISBONDED. REPAIR PER ER/A 417696-14.SDR DL733021057Wedge · damagedDAMAGE TO LT WING INBOARD MID FLAP WEDGE. REPAIR PER ER/A 417684-14.SDR DL733010042Frame · crackedINSPECTIONS OF THE FS 178 BULKHEAD PER AD 200-05-29 REVEALED A 2 INCH CRACK IN THE RT SIDE CHORD AT WL 207. THE DAMAGED CHORD WAS REMOVED AND A NEW SECTION INSTALLED TO ELIMINATE THE CRACK CONDITION. THE REPAIR WAS ACCOMPLISHED PER ER/A 379675-14AD, REV A.SDR DL733002248Generator · failedFLT1799/16 SLC-COS. DURING DESCENT FROM FL370 RT GEN DROPPED OFFLINE, 10 SEC LATER LT GEN DROPPED OFFLINE. UNABLE TO RESET GENERATORS PER POM. DID NOT START APU. CONCLUDED DESCENT AND APPROACH. REPLACED NR 1 GCU PER MM. MCO''D NR 2 GENERATOR PER MEL 24-0SDR DL733000730Slide · deployedTHE R-1 DOOR SLIDE WAS INADVERTENTLY DEPLOYED. SLIDE INFLATED AND DEPLOYED CORRECTLY.SDR DL733992711Socket · failedELECTRICAL SMELL IN CABIN. FOUND FLUORESCENT OVERHEAD LIGHT TUBE FWD SOCKET AT 13 A, B, C MELTING. REMOVED LIGHT TUBE AND REPLACED SOCKET.SDR DL733991658Reverse Light · illuminatedNR 2 ENG REV LIGHT CAME ON DURING TAKEOFF. ABORTED TAKE OFF JUST UNDER 100 KTS. LOCKED OUT NR 2 ENG REV PER MEL 78-00-02. MCO - CLEANED CONNECTORS. UNABLE TO DUPLICATE, REMOVED.SDR DL733991265Smoke Detector · failedLAV SMOKE FALSE ALARM. ACTIVATED TWICE IN FLIGHT. CIRCUIT BREAKER PULLED TO SILENCE ALARM. REPLACED FWD SMOKE DETECTOR.SDR DL733982662Skin · damagedDURING INSPECTION OF C1 DOOR CUTOUT SKIN AN EXISTING REPAIR WAS REMOVED FOR INSPECTABILITY OF THE AREA. REPAIRED AND REWORKED PER ERA 332586-14.SDR DL733982661Skin · crackedFUSE SKIN FOUND CRACKED AT BS 727E, S23L. DAMAGE REMOVAL RESULTED IN A 4.75 BY 2 INCH CUT OUT. REPAIRED PER ERA 332622-14.SDR DL733982660Web · crackedCRACK WAS FOUND DURING INSPECTION PER EO 5-70166-3 IN THE WEB AT BS 727, S18A (LHS). THE CRACK EXCEEDED EO/SB LIMITS. REPAIRED PER ERA 332607-14.SDR DL733982646Bulkhead Web · crackedDURING ACCOMPLISHMENT OF SI 5-69482-12, SEVERAL CRACKS WERE DISCOVERED ON THE FWD FACE OF THE BS 178 BLKD. REPAIRED PER ERA 332599-14.SDR DL733961361Window · crackedSEAT 10A PSGR CABIN WINDOW HAS SEVERAL CIRCULAR CRACKS ON OUTER WINDOW. WINDOW CRACKED AT SEAT 10F DURING PRESSURE CK FOR BROKEN WINDOW AT 10A. CABIN WAS PRESSURIZED TO 4.2 PSI, CABIN RATE OF CLIMB UP AND DOWN NEVER EXCEEDED 1,000 FPM.
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