N929TW, cancelled Jun 27, 2013
Service difficulty reports · 33
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 = 'N929TW' AND deregistration_id = 'N929TW-2013-06-27' 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 = 'N929TW' AND deregistration_id = 'N929TW-2013-06-27' 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 ZW0A0213101LampTHE EMERGENCY LIGHT IN THE TAIL COMPARTMENT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 2-8-02 STL. --CLOSED--SDR ZW0A0205603Accelerometer · malfunctionedAFTER TAKEOFF YAW DAMPER OFF LT-YAW KICKS LT-RT UNSKD LANDING AFTER UNCOMMANDED RUDDER INPUT. REMOVED AND REPLACED ACCELEROMETER PER MM 22-19-01 PG 201. ACCOMPLISHED RTS PER MM 22-01-05 PG 201.SDR ZW0A0104703Wedge · damagedDURING CHECK-C MAINT THE RT WING T/E FLAP T/E WEDGE WAS DAMAGED ON THE BOTTOM SIDE APPROX 6 FT INBD OF THE OTBD END. REMOVED AND REPLACED THE OTBD 13 .75 OF TRAILING EDGE WEDGE PER SRM 57-03 FIG 9 PAGE 12.SDR ZW0A0103901Frame · crackedDURING CHECK-C MAINT FOUND AT CANTED FRAME NUMBER 1497, 11 O'CLOCK POSITION A DOUBLE ROW OF HI-LOKS WERE CRACKED OUT. INSTALLED WEB REPAIR PER SRM 51-70-11 AND SRM 53-01. INSTALLED FASTENERS PER SRM 51-30-2. STOP DRILLED CRACK.SDR ZW0A0103709Floor Support · corrodedDURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT CRACKED AT STA 1098, BETWEEN LONGERON 26R AND 25R. FLOOR SUPPORT WAS REMOVED AND SENT TO SHOP TO BE WELDED PER SSRM 53-00-106, PAGE 201. REINSTALLED PER SRM 51-30-2, FIG 1.SDR ZW0A0103708Floor Support · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 183, LBL 44. FLOOR SUPPORT REMOVED AND NEW SUPPORT FABRICATED AND INSTALLED PER SPM 6-70-1 AND SRM 51-30-2.SDR ZW0A0103707Web · corrodedDURING CHECK-C MAINT IN FWD CABIN FOUND CORROSION ON MEMBRANE AT STA 197 TO 200, UNDER FWD EDGE OF NUMBER 1 CHAIR TRACK. INSTALLED REPAIR PER SRM 51-70-4 ON MEMBRANE AT STA 197 TO 200 UNDER NUMBER 1 CHAIR TRACK. TREATED PER SRM 51-10-03 PAGE 46 ITEM 3. INSTSDR ZW0A0103706Panel · dentedDURING CHECK-C MAINT ON LT WING FOUND NUMEROUS DENTS ON TRAILING EDGE PANEL IN FRONT OF AILERON. INSTALLED NEW PANEL P/N 5812737-501 PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-02 AND ARA 17765.SDR ZW0A0103705Floorbeam · gougedDURING CHECK-C MAINT A GOUGE WAS FOUND IN THE BOTTOM FLANGE OF THE CABIN FLOORBEAM, STA 408, RBL 2 INCH. BLENDED GOUGE IN BOTTOM FLANGE OF CABIN FLOORBEAM, STA 408, RBL 2 IN. FABRICATED REPAIR ANGLE AND REPAIR STRAP AND PHENOLIC RUB STRIP PER SSRM 53-60-103,SDR ZW0A0103703Bulkhead · crackedDURING CHECK-C MAINT IN AFT ACCY COMPT FOUND CRACKED WEB APPROX 2 INCHES ON STA 1485 CANTED BULKHEAD, APPROX 10 O'CLOCK POSITION. STOP DRILLED CRACK. REPAIRED WEB PER SRM 53-01, PAGE 9.SDR ZW0A0103704Frame · crackedDURING CHECK-C MAINT FOUND CANTED FRAME AT STA 1463, 2 O'CLOCK POSITION, WAS CRACKED AT HI-LOKS. REPAIRED PER SRM 53-01, FIG 2 SHEET 3.SDR ZW0A0103403Fitting · crackedDURING CHECK-C MAINT THE FWD CARGO DOOR T-ANGLE WAS CRACKED APPROX 16 INCHES FWD OF AFT END AT TOP OF DOOR. REPLACED CRACKED FITTING PER SRM 51-01, PAGE 1, ITEM C.SDR ZW0A0103402Web · crackedDURING CHECK-C MAINT FOUND A CRACK IN MEMBRANE AT LONGERON 18R, STA 1302. REMOVED DAMAGED AREA AND REPAIRED PER SRM 53-01 AND 51-30-2.SDR ZW0A0103505Longeron · crackedDURING CHECK-C MAINT FOUND LONGERON 17L CRACKED AT EACH HI-LOK TO FORMER 217, AT BOTH ATTACH POINTS TO FORMER 313, AT ATTACH POINT TO FORMER STA 256, AT BOTTOM HI-LOK TO FORMER 275, AND AT HI-LOK AND CONNECTION TO FORMER 237. REPLACED LONGERON 17L FROM STA 22SDR ZW0A0103504Floorbeam · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOORBEAM, STA 218 CENTERLINE. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-01 PAGE 1.SDR ZW0A0103503Floor Support · corrodedDURING CHECK-C MAINT FOUND CABIN FLOOR SUPPORT HAD CORROSION AT STA 180, RBL 9 TO 43. REPLACED SUPPORT PER SPM 6-70-01, PAGE 3 PARAGRAPH 4.SDR ZW0A0103006Angle · corrodedDURING CHECK-C MAINT FOUND ANGLE CORRODED AT STA 1155, LONGERON 29R TO 28R, AND AT STA 1212, STRINGER 29R TO 28R. REMOVED CORRODED ANGLES AND REPLACED WITH NEW.SDR ZW0A0103005Bracket · crackedDURING CHECK-C MAINT IN THE FWD CARGO COMPT FOUND CRACK IN TRACK TO FORMER BRACKET, STA 237, FWD SIDE, BETWEEN LONGERON 27 AND 28L, AND BETWEEN LONGERON 27 AND 28R.SDR ZW0A0103004Bulkhead · wornDURING CHECK-C MAINT FOUND WORN AREA ON STRINGER 1380, BULKHEAD, UPPER LT SIDE, FWD FACE APPROX 11 O'CLOCK. INSTALLED 0.050 DOUBLER OVER RUB AREA PER SRM 53-01.SDR ZW0A0103001Doubler · crackedDURING CHECK-C MAINT FOUND OLD REPAIR ON MEMBRANE HAD CRACKED, STA 905 TO 927, LONGERON 18R. REPLACED DOUBLER PER SRM 53-01, PAGE 9.SDR ZW0A0102515Support · corrodedDURING CHECK-C MAINT FOUND CORROSION ON AFT GALLEY GIRT BAR SUPPORTS. REMOVED CORROSION ON FWD GIRT BAR SUPPORT PER SPM 6-80-01, PAGE 2. REPLACED AFT GIRT BAR SUPPORT PER SRM 51-00 PAGE 27, ITEM B. TREATED PER SRM 51-10-3 PAGE 14.SDR ZW0A0102514Rivet · crackedDURING CHECK-C MAINT ON THE INBD LT ELEVATOR, FWD OF INBD MOUNT, HAD A METAL PLATE WITH RIVET CRACKED OUT. REPLACED METAL PLATE PER SRM 55-20-0 AND 51-30-02.SDR TWAA0105701Power Supply · dischargedTHE EGRESS LIGHTS BEHIND ROW 29 WERE FLASHING. REPLACED THE POWER SUPPLY. CHECK-C 3-30-00 STL.SDR TWAA0104401Light · intermittentTHE EMERGENCY EXIT LIGHTS AT THE REAR OF THE AIRCRAFT WERE REPORTED TO FLICKER IN FLIGHT. MAINTENANCE FOUND THE EMERGENCY LIGHTS OPERATED NORMALLY PER MAINT MANUAL 33-51-0. CHECK-C 3-30-00 STL.SDR TWAA0101003Battery · dischargedTHE FIRST CLASS OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY IN NUMBER 3 POSITION (P/N 60-0304-516B), AND REPLACED BATTERIES IN NUMBER 2 AND 3 POWER SUPPLIES (P/N 408822-101). CHECK-C 3-30-00 STL.SDR TWAA0100903Battery · overheatedWHILE AT THE GATE SMOKE WAS SEEN COMING FROM THE ELECTRONIC COMPARTMENT. SHIPS BATTERY WAS HOT TO TOUCH AND EVENTUALLY SPARKING. AMPS WERE CHARGING THEN DISCHARGING EVERY FEW SECONDS. TURNED BATTERY SWITCH OFF. REPLACED BOTH SHIPS BATTERIES (P/N 30475-002)SDR TWAA0014001Transceiver · shortedON PREFLIGHT, CREW NOTICED NUMBER 3 VHF CIRCUIT BREAKER TRIPPED. RESET CB AND A STRONG ELECTRICAL BURNING SMELL WAS NOTICED. PULLED CB E-24 AND SMELL WENT AWAY. CORRECTIONS WERE DEFERRED PER MEL. LATER THE NUMBER 3 VHF TRANSCEIVER WAS REPLACED. CHECK-C 3-SDR TWAA0012301Battery · dischargedBOTH COCKPIT EMERGENCY LIGHTS FAILED TO ILLUMINATE WHEN EMERGENCY LIGHTS WERE SWITCHED ON. REPLACED THE BATTERIES IN THE POWER SUPPLY. CHECK-C 3-30-00 STL.SDR TWAA0009502Battery Pack · inoperativeDURING ROUTINE INSPECTION, FOUND LEFT AND RIGHT AFT OVERWING EGRESS LIGHTS AND EXIT LIGHTS INOP. REPLACED BATTERY PACK. AC05 04-01-00 JFK.SDR TWAA0005104Battery Pack · wornTHE AFT CABIN EGRESS LIGHTS FROM THE AFT GALLEY TO REAR OF THE AIRCRAFT INTERMITTENTLY ILLUMINATED DURING FLIGHT. REPLACED BATTERY PACK AT ROW 29. CHECK-C 3-17-00 STL.SDR TWAA0005103Battery Pack · inoperativeTHE AFT CABIN EGRESS LIGHTS WERE ILLUMINATING. REPLACED THE BATTERY PACK AT ROW 23. CHECK-C 3-17-00 STL.SDR TWAA9814801Generator · failedAIRCRAFT WAS DISPATCHED WITH THE RT ENG GENERATOR INOPERATIVE PER MEL. AT FL310, THE APU SHUT DOWN. APU RESTARTED AT FL 240. ELECTED TO DIVERT TO MCI. THE RT ENG CSD AND GENERATOR WERE REPLACED. APU OPERATED OK. CSD MFG 696233B AND GEN MFG 976J252-8. CHSDR TWAA9806102Socket · crackedMCI - DURING MODIFICATION VISIT, FOUND LT FORWARD OVERWING EXIT FORWARD LOCK PIN SOCKET CRACKED ON THE LOWER OVERWING EXIT FRAME. REPAIRED PER SRM 53-05, FIG 32A. ACFT TT: 37,475 HOURS. ACFT TC: 34,855. (X)
Back to N929TW, cancelled Jun 27, 2013