N571PE, cancelled Jun 23, 2017
Service difficulty reports · 21
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 = 'N571PE' AND deregistration_id = 'N571PE-2017-06-23' 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 = 'N571PE' AND deregistration_id = 'N571PE-2017-06-23' 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 CALA9700293Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN ANGLE UNDER CABIN FLOOR AT STA 297, RBL 12. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR CALA9700294Stringer · corrodedINSPECTION FOUND CORROSION IN BILGE AREA OF AFT PIT AT STA 950E, STRINGER 27R. THE CORRODED AREA WAS CUT OUT IAW SRM 53-30-3, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9700283Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED BETWEEN TIE DOWN TRACKS AND OUTBOARD TO END AT BS 348.2, LT SIDE. THE CORRODED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9700290Skin · damagedINSPECTION FOUND DAMAGE IN THE FORM OF MATERIAL LOSS ON EDGE OF SKIN AT LT SIDE OF FUSELAGE, BS 360 BETWEEN STRINGER 17L AND 18L, AT PRODUCTION JOINT. THE AREA WAS BLENDED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5330-02493 AND SRM 53-30-3.SDR CALA9700292Frame · crackedINSPECTION FOUND A CRACK IN RIGHT FRAME INBOARD FLANGE AT FIRST FASTENER HOLE BELOW FLOORBOARD ATTACH ANGLE AT BS 783.95. THE CRACK LENGTH WAS NOT IDENTIFIED, A REPAIR KIT WAS INSTALLED IAW BOEING DRAWING 65C36280-2.SDR CALA9700286Skin · bulgedINSPECTION FOUND RT WING OUTBOARD LOWER SKIN BULGED JUST AFT OF PANEL NR 7703. THE BULGED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5730-01484.SDR CALA9700282Skin · creasedINSPECTION FOUND A 6 INCH CREASE EXTENDING FORWARD OF DOUBLER IN RT AFT FUSELAGE AT BS 1152 TO 1121 BETWEEN STRINGER 22R AND 23R. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-2, 51-30-2, 53-30-3 AND 53-30-4.SDR CALA9700285Ceiling Panel · crackedINSPECTION FOUND TWO .125 INCH CRACKS AT ONE FASTENER HEAD IN NLG CEILING PANEL AT BS 276, RBL 14. THE CRACKS WERE ROUTED OUT, A FILLER AND DOUBLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9700284Ceiling Panel · crackedINSPECTION FOUND A .125 INCH CRACK AT TWO EACH FASTENER HEADS IN NLG CEILING PANEL AT BS 285, LBL 4. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9700291Skin · delaminatedINSPECTION FOUND LT OUTBOARD AILERON OUTBOARD TRAILING EDGE WEDGE DELAMINATED AND ERODED. SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-40-6.SDR CALA9700126Pulley Assy · wornNOSE GEAR FAILED TO RETRACT AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NLG DOOR FORWARD PULLEY ASSEMBLY WITH SIGNS OF CONTACTING THE PULLEY FOLLOWUP LINKAGES. THE FORWARD PULLEY ASSEMBLY WAS REMOVED ASDR CALA9600860Floor Beam · corrodedINSPECTION FOUND CORROSION ON FLOOR BEAM AT STA 1130, RT SIDE OF AIRCRAFT. THE FLOOR BEAM WAS REPAIRED IAW ECRA 5310-03297.SDR CAL960425Dnlock Switches · inoperativeIAH - FLT 1902 - THE AIRCRAFT HAD A BRIEF HISTORY OF THE NLG RED UNSAFE LIGHT REMAINING ILLUMINATED AFTER GEAR RETRACTION. THE LIGHT EXTINGUISHED WHEN GEAR WAS CYCLED. MAINTENANCE REMOVED AND REPLACED THE NLG LOCK AND POSITION SWITCHES PER MM 32-61-71, PAGE SDR CAL951128Fuse · blownFLT NR 0631 - EWR - A PREFLIGHT INSPECTION, FOUND FORWARD SECTION OF EMERGENCY TRACK LIGHTING INOPERATIVE FROM ROW 1-7. MAINTENANCE FOUND A FUSE BLOWN ON FORWARD POWER SUPPLY. THE FUSE WAS REMOVED AND REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (M)SDR CAL950167Bracket · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN RT WING, NR 5 LEADING EDGE SLAT ACTUATOR ATTACH BOLT BRACKET. A REPAIR WAS PERFORMED IAW SRM 51-30-2 AND BOEING DRAWING 65-17276. (X)SDR CAL950166Stiffener · corrodedGSO - INSPECTION FOUND CORRODED STIFFENER ON TOP OF DOG HOUSE AT BS 308. THE STIFFENER WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2 AND SRM 51-20-4. (X)SDR CAL950165Frame · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN WEB AT RT STA 760.95 OVERWING EXIT FRAME. THE CRACK WAS LOCATED AT THE FIRST HOLE UNDER FLOOR LINE. THE CRACK WAS REPAIRED BY INSTALLING A REPAIR ANGLE, FILLER, SHIMS, AND SILL SPLICE IAW BOEING DRAWING 65C36279-2. (SDR CAL950164Floor Beam · crackedGSO - INSPECTION FOUND A 1.25 INCH CRACK IN STRAP AT LOWER SIDE OF FLOOR BEAM, BS 344. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND SRM 51-30-2. (X)SDR CAL950163Angle · crackedGSO - INSPECTION FOUND A 2 INCH CRACK AT BOTH ENDS OF BOTTOM CENTER ANGLE AT FS 700. THE ANGLE WAS REMOVED AND THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1 AND SRM 51-30-2. REPAIRS WERE INSTALLED IAW SRM 51-30-2. (X)SDR CAL950162Support · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN LEFT WING LOWER TRAILING EDGE SUPPORT CHANNEL AT STATION 469. THE SUPPORT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW EX 5720C01236 AND CAL DRAWING 5720 DC8908. (Z)SDR CAL950161Support · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN LEFT WING LOWER TRAILING EDGE SUPPORT CHANNEL AT STATION 521. THE SUPPORT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW EX 5720C01236. (Z)
Back to N571PE, cancelled Jun 23, 2017