N578PE, cancelled Oct 24, 2002
Service difficulty reports · 54
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 = 'N578PE' AND deregistration_id = 'N578PE-2002-10-24' 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 = 'N578PE' AND deregistration_id = 'N578PE-2002-10-24' 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 CALA9800137Bracket · crackedINSPECTION FOUND, A .75 INCH CRACK IN LT WING NR 2 LEADING EDGE FLAP ACTUATOR INBOARD ATTACH BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-3, 51-10-1, AND 51-30-2.SDR CALA9800136Bracket · crackedINSPECTION FOUND A .75 IN H CRACK IN LT WING NR 1 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9800135Angle · crackedINSPECTION FOUND, A 2.25 INCH AND 1.5 INCH CRACK AT INBOARD UPSTOP AREA BELOW TELESCOPING ANTI-ICE DUCT OF LT WING NR 2 SLAT CHORD ANGLE. THE ANGLE WAS REPAIRED IAW SRM 51-40-3.SDR CALA9800715Wire · damagedINSPECTION FOUND FORWARD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND A DAMAGED WIRE AT CONNECTOR. THE WIRE WAS REPAIRED, THE LIGHT WAS RELAMPED, AND THE BATTERY PACK WAS RECHARGED. OPERATION CHECKED GOOD IAW MM 33-50.SDR CALA9800125Battery Pack · dischargedTHE EMERGENCY LIGHTING AT MID CABIN CEILING EXIT LIGHT, COCKPIT DOOR EXIT LIGHT, AND L-1 AND R-1 LOWER EXIT LIGHTS FAILED CAPACITANCE TEST. THE BATTERY PACK WAS REMOVED AND REPLACED.SDR CALA9800124Battery Pack · dischargedTHE EMERGENCY PATH LIGHTING AT FIRST CLASS SECTION AND ROWS 17 TO 22 FAILED CAPACITANCE TEST. TWO BATTERY PACKS WERE REMOVED AND REPLACED.SDR CALA9800123Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN AFT STAIRS ACTUATOR ATTACH ANGLES AT STA 1263 INSIDE RT TORQUE BULKHEAD. NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1.SDR CALA9800122Bracket · crackedINSPECTION FOUND A 1 INCH CRACK ON AFT SIDE OF AFT AIRSTAIRS ACTUATOR ATTACH BULKHEAD SUPPORT BRACKET AT STA 1263. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9800121Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD SUPPORT ANGLE OF AFT AIRSTAIRS RT SIDE STA 1273 (TORQUE BOX). ALSO, A 1 INCH CRACK WAS FOUND IN UPPER ANGLE OF AFT SIDE OF BULKHEAD IN AFT AIRSTAIR AREA ON RT SIDE AT STA 1273. NEW ANGLES WERE FABRICATED AND INSTALLSDR CALA9800120Bracket · crackedINSPECTION FOUND A 3 INCH CRACK IN INBOARD MOUNT BRACKET WHERE NR 1 SLAT ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2.SDR CALA9800119Skin · crackedINSPECTION FOUND A .1875 INCH CRACK IN LT WING TRAILING EDGE UPPER SKIN AT NR 3 SPOILER THIRD CUTOUT FROM INBOARD HINGE. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-4 AND 51-10-2.SDR CALA9800118Skin · crackedINSPECTION FOUND A .25 INCH CRACK IN LT WING TRAILING EDGE UPPER SKIN AT NR 3 SPOILER SECOND CUTOUT FROM INBOARD HINGE. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-4 AND 51-30-2.SDR CALA9800117Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN VENT BOX STRINGER INSIDE LT WING TANK ACCESS 7217, WS 656.50. A REPAIR WAS INSTALLED IAW EA 5712-01050.SDR CALA9800116Angle · crackedINSPECTION FOUND A 2 INCH CRACK THROUGH TWO FASTENER HOLES OF RIB SUPPORT ANGLE AT WING LEADING EDGE SLAT STA 0. THE RIB SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1.SDR CALA9800115Skin · crackedINSPECTION FOUND A .375 INCH CRACK IN LT WING NR 4 SLAT LOWER SKIN JUST OUTBOARD OF INBOARD TRACK AREA. THE CRACKED AREA WAS BLENDED OUT. A PATCH REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-50-1, 51-10-2, AND 57-50-3.SDR CALA9800114Angle · crackedINSPECTION FOUND A 6 INCH CRACK AT FASTENERS IN SUPPORT ANGLE INSIDE LT WING INBOARD LEADING EDGE AREA AFT OF NR 1 LEADING EDGE FLAP INBOARD END AT L/E STA 130. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1.SDR CALA9800113Skin · crackedINSPECTION FOUND A .625 INCH CRACK IN LT WING UPPER FIXED LEADING EDGE SKIN WHERE NR 3 SLAT OUTBOARD HOOK ATTACHES. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. DOUBLER, BACK STRAP, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 57-30-4 AND 51-10-2.SDR CALA9800112Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON AND AROUND NUT PLATES IN E AND E COMPARTMENT UNDER GALLEY AT STA 380. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-4, AND 51-10-1.SDR CALA9800111Angle · corrodedINSPECTION FOUND Z-ANGLE CORRODED AT STA 616 ABOVE STRINGER 26R IN FORWARD BAGGAGE BIN. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9800110Support · corrodedINSPECTION FOUND RT FLOOR SUPPORT IN FORWARD BAGGAGE BIN CORRODED FROM DTA 616 TO 660. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.SDR CALA9800109Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1030 BETWEEN STRINGERS 20-21L. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-10-6.SDR CALA9701235Prbc · brokenTHE NR 3 ENGINE EGT HIT REDLINE ON TAKEOFF ROLL. REDUCING EPR TO 1.4 FAILED TO KEEP EGT OUT OF REDLINE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FITTING ON PRBC BROKEN. THE PRBC WAS REPLACED IAW MM 75-31-13. THESDR CALA9701189Lock Actuator · inoperativeTHE NOSE GEAR DID NOT EXTEND WHEN GEAR HANDLE WAS SELECTED DOWN ON FINAL APPROACH. THE GEAR WAS CYCLED AND EXTENDED NORMALLY FOR A SAFE LANDING AT IAH. MAINTENANCE FOUND THE NLG LOCK ACTUATOR AT FAULT. THE NLG LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 3SDR CALA9701156Actuator · inoperativeTHE RT MLG WOULD NOT RETRACT WHEN GEAR HANDLE WAS PLACED IN THE UP POSITION AFTER TAKEOFF. THE SECOND OFFICER'S ANNUNCIATOR PANEL INDICATED THAT THE RIGHT GEAR DOOR WAS DOWN. A VISUAL CHECK CONFIRMED THE GEAR WAS DOWN. THE AIRCRAFT WAS RETURNED TO IAH WHERESDR CALA9700820Hyd Line · leakingTHE 'A' SYSTEM HYDRAULIC FLUID WAS LOST WHEN LANDING GEAR WAS RAISED AFTER TAKEOFF FROM MCO. THE AIRCRAFT WAS RETURNED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MX FOUND THE LT MLG DOOR ACTUATOR PRESSURE LINE LEAKING. THE PRESSURE LINE WAS REMOVED AND REPLACSDR CALA9700311Actuator · failedTHE A-HYDRAULIC SYSTEM QUANTITY WAS LOST WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG DOOR RETRACT AND EXTEND ACTUATOR FAILED. THE ACTUATOR WASSDR CALA9700177Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN CUTOUT FOR NR 3 LEADING EDGE SLAT INBOARD TRACK, LT WING. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-4.SDR CALA9601767Control Module · inoperativeTHE AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY APPROXIMATELY 10 MINUTES AFTER TAKEOFF. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM ELEVATOR CONTROL MODULE AT FAULT. THE ELEVATOR CONTROL MODULE WAS REPLACED. THE NR 1 ENGSDR CALA9600828Frame · damagedINSPECTION FOUND IMPACT DAMAGE TO FRAMES AT STA 169.8 AND 211.5, WL 170. THE FRAMES WERE REPAIRED IAW SRM 51-40-4, FIGURE 3.SDR CALA9600772Skin · puncturedINSPECTION FOUND TWO SMALL HOLES IN FUSELAGE SKIN DUE TO GROUND DAMAGE AT STA 196 AND 211.5, RT SIDE. AN INTERIM REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 1, PAGE 5. A DIP WAS ISSUED TO INSPECT REPAIR EVERY 3,000 FLIGHTS AND TO PERFORM A PERMANENT REPAIR SDR CAL960015Skin · crackedINSPECTION FOUND A .50 INCH CRACK IN L-1 DOOR INTERNAL SKIN AT TORQUE BOX CUT OUT. THE CRACKED AREA WAS BLENDED OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-00-2, SRM 51-10-1, AND SRM 51-20-4. (X)SDR CAL960034Stringer · corrodedINSPECTION FOUND STR 29R CORRODED AT SPLICE AND UNDER LEVELING COMPOUND AT CENTER OF STRINGER IN AFT CARGO BIN BS 1000. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A STRINGER SPLICE AND REPAIR DOUBLER ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND SRSDR CAL960035Stringer · corrodedINSPECTION FOUND STR 29L CORRODED AT STA 972 IN AFT PIT. THE CORROSION WAS BLENDED OUT IAW SRM 51-10-6. A REPAIR STRAP WAS FABRICATED AND INSTALLED IAW ECRA 5310-03205. (X)SDR CAL960027Strap · corrodedINSPECTION FOUND DOUBLER STRAP CORRODED AROUND C-1 ENTRANCE AT STA 560 ABOVE STR 26R. THE CORROSION WAS REMOVED IAW SRM 51-10-6, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5230-01298 AND SRM 51-30-2. (X)SDR CAL960022Support · corrodedINSPECTION FOUND FORWARD CARGO FLOOR SUPPORT STRUCTURE AT STA 640 CENTER SECTION CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6, AN 'L' ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND SRM 53-10-8. (X)SDR CAL960036Stringer · corrodedINSPECTION FOUND STR 28L CORRODED BETWEEN STA 985 AND STA 994, IN THE AFT PIT. THE CORRODED SECTION WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND MM 51-40-5. (X)SDR CAL9690026Stringer · corrodedINSPECTION FOUND STR 26R CORRODED AT STA 520 - STA 560. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, SRM 53-10-1, SRM 51-10-2, SRM 51-30-2, AND SRM 51-40-5. (X)SDR CAL960040Bulkhead Fitting · corrodedINSPECTION FOUND CORROSION IN FORWARD CARGO BS 740 BULKHEAD FITTING AT S28L. THE CORROSION WAS CLEANED AND TREATED IAW SRM 51-10-2. L-ANGLE SPLICE WAS FABRICATED AND INSTALLED IAW SRM'S 51-30-2, 53-10-3, 51-10-2, AND 51-20-4. (X)SDR CAL960039Bulkhead Fitting · corrodedINSPECTION FOUND CORROSION IN FORWARD CARGO BS 740 BULKHEAD CORNER FITTING AT S28R. A NEW STRINGER SECTION AND REPAIR SPLICE WERE INSTALLED IAW SRM 51-30-2, SRM 53-10-3, AND ECRA 5340-01256. (X)SDR CAL960038Frame · corrodedINSPECTION FOUND UPPER SURFACE OF BELT FRAME LOWER FLANGE IN AFT CARGO BIN CORRODED AT BS 990, LBL 16. THE CORROSION WAS REMOVED IAW SRM 51-10-6. (X)SDR CAL960037Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED AT FS 990 BETWEEN STR 28L AND STR 29L. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM'S 53-10-4, 51-10-1, 51-10-2, AND 51-30-2. (X)SDR CAL960030Stringer · corrodedINSPECTION FOUND STR 27L CORRODED IN AFT CARGO COMPARTMENT AT BS 1015. THE CORRODED SECTION OF STRINGER WAS REMOVED IAW SRM 51-30-2. A STRINGER REPAIR AND HAT SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2. (X)SDR CAL960029Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED BETWEEN S27R AND S28R AND STA 1010. A SHEAR TIE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, SRM 51-10-2, AND SRM 51-30-2. (X)SDR CAL960028Stringer · corrodedINSPECTION FOUND STRINGER 26R CORRODED AT STA 1166. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTALLED IAW SRM 53-10-3. (X)SDR CAL960025Frame · crackedINSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO FRAME AT STA 580 AND CENTER OF FLOOR STRUCTURE. THE CRACKED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, SRM 51-10-2, AND SRM 51-30-2. (X)SDR CAL960024Support · corrodedINSPECTION FOUND FORWARD CARGO RIGHT FLOOR SUPPORT STRUCTURE CORRODED AT BS 480 - BS 560. A REPAIR PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, SRM 53-10-1, AND SRM 51-30-2. (X)SDR CAL960023Frame · crackedINSPECTION FOUND FORWARD CARGO FRAME STA 640 CRACKED AT S29R (.50 INCH), S29L (1.5 INCHES), AND S28L (.25 INCH). A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, SRM 51-30-5, SRM 51-10-2, AND SRM 51-30-2. (X)SDR CAL960020Frame · crackedINSPECTION FOUND A .3750 INCH CRACK IN FORWARD CARGO FRAME AT STA 660, STR 28R. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-4 AND SRM 51-30-2. (X)SDR CAL960018Frame · crackedINSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO FRAME AT STA 600 AND CENTER FLOOR STRUCTURE. THE CRACKED SECTION OF FRAME WAS CUT OUT IAW SRM 51-40-3. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND SRM 51-30-2. (X)SDR CAL960017Frame · crackedINSPECTION FOUND A 2.5 INCH CRACK IN FORWARD CARGO FRAME AT STA 720, LBL 6. THE CRACKED SECTION OF FRAME WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, SRM 51-10-1, SRM 51-10-2, AND SRM 51-30-2. (X)
Back to N578PE, cancelled Oct 24, 2002