N367PA, cancelled Mar 27, 2006
Service difficulty reports · 51
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 = 'N367PA' AND deregistration_id = 'N367PA-2006-03-27' 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 = 'N367PA' AND deregistration_id = 'N367PA-2006-03-27' 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 RIVA0000027Nose Cowl · crackedPSM, CRACK AT NR 3 NOSE COWL AT 12 O''CLOCK POS AT NAC STA 77.5, 6 AFT OF COWL L/E. DAMAGE AREA WAS CUT OUT OF NOSE COWL AT NAC STA 77.5. THE REP PLATE WAS FAB FROM .050 2024T-3. DRILLED EXISTING (AND REPAIRED) HOLES ONTO REP PLATE. DEBURRED ALL EDGES ON NSDR RIVA0000028Connector · damagedADW, AT T/O, A FIRE BELL, FIRE WARN LIGHT, ENG FAIL LIGHT AND GROUND FAULT LIGHT ILLUM. THE CHECKLIST WAS COMPLETED AND THE TAKEOFF WAS ABORTED. THE A/C RETURNED BACK TO THE GATE W/O INCIDENT. THE NR3 ENG. AND PYLON FIRE DETECT. SYS WERE INSP. THE NR 3 ENGSDR RIVA0000024Clamp · displacedBGR, ON CLIMBOUT, THE NR 3 ENGINE INDICATED A FIRE WARNING AT 6500 FEET. THE ENGINE WAS SECURED BY THE APPROPRIATE CHECK LIST. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS RETURNED TO BGR. AFTER LANDING, FIRE RESCUE CONFIRMED THAT THERE WAS NO FIRE. THE SDR RIVA0000023Duct · leakingBGR, ON CLIMBOUT AT 6000 FEET, THE NR 3 ENGINE INDICATED A FIRE WARNING. THE ENGINE WAS SECURED BY THE APPROPRIATE CHECKLIST. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO BGR.UPON INSPECTION, A PNEUMATIC DUCT LEAK WAS FOUND BLOWING BLEED AIR ON THESDR RIVA0000021Connector · shortedUPON APPROACH TO PIT, THE NR 3 ENGINE FIRE BELL SOUNDED WITH NO ASSOCIATED ENGINE FIRE LIGHT. THE SYSTEM TESTED NORMAL. THE NR 3 ENGINE DETECTOR GROUND LIGHT MOMENTARILY FLICKERED. AFTER LANDING, THE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED STEADILY. THE SDR RIVA0000020Fire Loop · malfunctionedYYZ - ON CLIMB-OUT AFTER TAKEOFF, THE ENGINE FIRE BELL AND LIGHT OPERATED INDICATING AN ENGINE FIRE. THE NR 3 ENGINE FIRE HANDLE WAS LIGHTED. THE EMERGENCY CHECK LIST WAS COMPLETED. THE AIRCRAFT RETURNED TO YYZ WITHOUT INCIDENT. NO FIRE WAS VISIBLE BY THE SDR RIVA0000019Duct · looseAT 110 KNOTS ON TAKEOFF, THE NR 3 FIRE LIGHT WARN BELL AND GROUND FAULT LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE AT PSM WITHOUT INCIDENT. AN AIR DUCT ON THE START VALVE WAS FOUND TO BE LOOSE. THE DUCT WAS SECURED AND SDR RIVA0000018Fire Warning · false activationPIT - AT 70 KNOTS ON TAKEOFF ROLL, THE NR 3 FIRE LIGHT, WARNING BELL AND GROUND FAULT LIGHT ILLUMINATED. THE BELL WENT OUT, AND WITH RETARDED THROTTLE, THE FIRE LIGHT EXTINGUISHED. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE AT PIT WITHOUT INCISDR RIVA0000017Csd · malfunctionedPSM - ON CLIMB-OUT, THE NR 3 CSD GENERATOR DRIVE OIL TEMPERATURE STEADILY ROSE TO APPROXIMATELY 155 DEGREES CELCIUS. AT THAT POINT, THE NR 3 GENERATOR CIRCUIT BREAKER TRIPPED. VOLTS AND FREQUENCY WERE NORMAL. THE AIRCRAFT RETURNED TO PSM WITHOUT INCIDENT. SDR RIVA0000015Skin · wornDURING C CHECK INSPECTION, IT WAS NOTED THAT THE RIGHT WING OUTBOARD FOREFLAP HAS A WEAR MARK IN SKIN AT LEADING EDGE, INBOARD OF INBOARD SEQUENCE CARRIAGE ATTACH BEARING. INSTALLED PATCH ON RIGHT WING OUTBOARD FOREFLAP LEADING EDGE (INBOARD OF INBOARD SEQUENSDR RIVA0000014Structure · crackedDURING C CHECK INSPECTION, IT WAS NOTED THAT THE NR 2 SLAT HAS TWO CRACKS AT EDGE OF LIGHTENING HOLES. REMOVED FASTENERS IN THE NR 2 SLAT COVE PANEL IAW B727 SRM 51-30-2. BLENDED OUT ONE CRACK IAW SRM 57-50-1, REMOVED DAMAGED AREA OF OTHER CRACK IAW SRM 51-4SDR RIVA0000016Floorbeam · corrodedDURING C CHECK INSPECTION, IT WAS NOTED THAT ON THE LOWER SURFACE ON FLOORBEAM FLANGES AT STATION 344 HAVE CORROSION THAT WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-8 FIG 1. REPAIRED CORRODED UPPER CHORD OF FUSELAGE FLOORBEAM AT STATION 344 FROM LBL 60 TO RBSDR EISA98001Engine · failedNR 2 ENGINE FAILED ON GO AROUND. REMOVED AND REPLACED NR 2 ENGINE. (M)SDR EISA97286Wire · brokenNR 2 OIL TEMP ABOVE RED LINE ON TAKEOFF ENGINE SHUTDOWN. REPAIRED BROKEN WIRE AT TEMP BULB ON NR 2 ENGINE, OPS CHECK NORMAL. (M)SDR EISA97099Receiver · inopON DEPART NR 1 VHF NAV INOP, RETURNED TO DFW. REPLACED NR 1 NAV RECEIVER. (M)SDR EISA97032Battery Pack · dischargedAFT SLIDE EMEGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. (M)SDR EISA97004Oil Press Switch · inoperativeNR 2 ENGINE OIL FILTER BYPASS/LOW PRESS LIGHT ILLUMINATED DURING FLIGHT. REMOVED AND REPLACED NR 2 LOW PRESS SWITCH. (M)SDR EISA96285Adi · inopF/O'S ADI GYRO FLAG IN VIEW IN BOTH NORMAL AND ALTERNATE. REMOVED AND REPLACED F/O'S ADI. OPS CHECK GOOD IAW MM 34-23-11. (M)SDR EISA95052Floor Beam · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR BEAM, BS 1130, LBL 10 INCHES, WL 208.1. REPAIRED PER DRAWING HSE-53-151. (Z)SDR EISA95051Beam · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON BS 1183 VERTICAL BEAM AT BL '0', WL 148. REPAIRED PER DRAWING HSE2-53-154 AND HSE2-53-150. (Z)SDR EISA95050Stringer · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON STRINGER 29R AND 30, BETWEEN BS 990 AND 1010. REPAIRED PER DRAWING HSE2-53-147 AND BOEING FAX C00-SJ0-95-0037RR. (Z)SDR EISA95049Skin · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION BULGES AT AFT LAVATORY SERVICE PANEL. REPAIRED PER SRM 51-10-1 PAGE 4. (Z)SDR EISA95048Spar · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD, STATION 223.05. REPAIRED PER DRAWING HSE2-55-146. (Z)SDR EISA95047Angle · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE, BS 970 TO BS 990, BL '0'. REPLACED PER SRM 51-10-1, PARA 4A, PAGE 4. (Z)SDR EISA95046Floor Beam · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR BEAM, BS 1030, WL 208.1, LBL 1 INCH. REPAIRED PER SRM 53-10-8, FIGURE 3. (Z)SDR EISA95045Intercostal · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON INTERCOSTAL, BS 1110 TO BS 1130, BL '0'. REPAIRED PER SRM 51-10-1. (Z)SDR EISA95044Support · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT, BSL 1110 TO BS 1030, LBL 12 INCH. REPLACED PER SRM 51-10-1 PARAGRAPH 4A, FIGURE 4. (Z)SDR EISA95043Support · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT BS 1050 TO 1070, LBL 22. REPLACED PER SRM 51-30-2. (Z)SDR EISA95042Seat Track · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON SEAT TRACK, BS 1070 TO BS 1140, WL 208.1, LBL 55 INCHES. REPAIRED PER SRM 51-10-1 PAGE 4. (Z)SDR EISA95041Seat Track · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON SEAT TRACK, BS 1090 TO BS 1140, WL 208.1, LBL 24.75. REPLACED PER SRM 51-10-1. (Z)SDR EISA95040Track · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON SEAT TRACK, BSL 1090 TO BS 1140, WL 208.1, LBL 45.5. REPLACED PER SRM 53-10-5, FIGURE 7. (Z)SDR EISA95039Angle · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE, BS 1138 TO BS 1158, WL 208.1. REPAIRED PER SRM 51-10-1. (Z)SDR EISA95038Support · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT, BS 1110 TO 1130, LBL 12, WL 208.1. REPAIRED PER SRM 51-10-1. (Z)SDR EISA95037Floor Beam · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR BEAM, BS 1110, WL 208.1. REPAIRED PER SRM 53-10-8, FIGURE 3. (Z)SDR EISA95036Support · crackedDURING A SCHEDULED C-CHECK, FOUND A CRACK IN THE FLOOR ANGLE SUPPORT, BS 760.95, WL 208.1, LBL 5. REPAIRED PER SRM 51-40-3, FIGURE 1, SHEET 4. (Z)SDR EISA95035Chord · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON CHORD AT BS 1176.9, WL 208.1 LBL 58 INCHES. REPAIRED PER BOEING SB 727-53-0184 AND DRAWING HSE2-53-149. (Z)SDR EISA95034Angle · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE, BETWEEN BS 312 AND BS 344, WL 208.1, LBL 62 INCHES. REPAIRED PER SRM 51-40-3. (Z)SDR EISA95033Skin · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON FUSELAGE SKIN, BS 484 BETWEEN STRINGER 28L AND 28R. REPAIRED PER DRAWING HSE 2-53-153. (Z)SDR EISA95032End Fitting · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON STRINGER END FITTING, STRINGER 28R, BS 1183. REPLACED PER SRM 51-10-1 PAGE 4. (Z)SDR EISA95031Intercostal · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON INTERCOSTAL BETWEEN BS 1050 AND 1090, LBL 24 INCHES, WL 20 INCHES. REPLACED PER SRM 51-10-1, PAGE 4. (Z)SDR EISA95030Frame · damagedDURING A SCHEDULED C-CHECK, FOUND A HOLE IN THE AFT CARGO COMPARTMENT DOOR FRAME, BS 990, STRINGER 24R. REPAIRED PER SRM 51-40-7 FIGURE 3. (Z)SDR EISA95029Longeron · crackedDURING A SCHEDULED C-CHECK, FOUND A CRACK IN LONGERON, BS 970 TO BS 990, STRINGER 29R. REPAIRED PER SRM 53-10-8. (Z)SDR EISA95028Channel · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION BULGE FROM BS 990 TO BS 1010, STRINGER 27R. REPAIRED PER SRM 51-10-1. (Z)SDR EISA95027Stringer · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON STRINGER 29R AT BS 950D TO 950E. REPAIRED PER BOEING FAX, C00 SJO-95-0037RR. (Z)SDR EISA95026Longeron · bentDURING A SCHEDULED C-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT LONGERONS BENT BETWEEN BS 950F TO BS 970, STRINGER 29L TO 30. REPAIRED PER SRM 53-10-5 FIGURE 6, PAGE 17 (Z)SDR EISA95025Angle · crackedDURING A SCHEDULED C-CHECK, FOUND AFT CARGO COMPARTMENT RIB REINFORCEMENT SECTION CRACKED BETWEEN BS 950 F TO 970, STRINGER 30. REPAIRED PER SRM 51-10-1, PARAGRAPH AA, PAGE 4. (Z)SDR EISA95024Angles · dentedDURING A SCHEDULED C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT ANGLES DENTED FROM BS 560 TO 580, STRINGER 29L TO 29R. REPAIRED PER SRM 51-40-1, FIGURE 1. (Z)SDR EISA95023Angle · crackedDURING A SCHEDULED C-CHECK, FOUND FLOOR SUPPORT ANGLE CRACKED, BS 410 WL 166.1, RBL 38 INCHES. REPAIRED PER SRM 51-40-4. (Z)SDR EISA95022Skin · damagedDURING A SCHEDULED C-CHECK, FOUND FORWARD CARGO COMPARTMENT DOOR FRAME AND SKIN DAMAGED, LOWER AFT CORNER. REPAIRED PER SRM 52-00-3 FIGURE 1. (Z)SDR EISA95021Beltframe · corrodedDURING A SCHEDULED C-CHECK, FOUND CORROSION ON FUSELAGE FRAME, BS 344 AT STRINGER 23R. REPAIRED PER SRM 53-10-4, FIGURE 1. (Z)
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