N17402, cancelled Apr 27, 2001
Service difficulty reports · 67
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 = 'N17402' AND deregistration_id = 'N17402-2001-04-27' 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 = 'N17402' AND deregistration_id = 'N17402-2001-04-27' 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 CALA9901738Battery Pack · dischargedINSPECTION FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE IN CABIN AND AT OVERWING EXITS, BOTH SIDES. MAINTENANCE REPLACED A BAD FUSE. THE BATTERY PACKS WERE REMOVED, RECHARGED, AND REINSTALLED. OPERATIONAL CHECKS WERE GOOD IAW MM 33-50-01, PAGE 201.SDR CALA9900418Skin · corrodedINSPECTION FOUND AFT LAV SERVICE PANEL AFT LOWER SKIN CORRODED. THE PANEL WAS REMOVED AND THE CORRODED INNER SKIN WAS REMOVED. A NEW SKIN AND INTERNAL AND OUTER DOUBLER WERE INSTALLED AND THE PANEL WAS REINSTALLED IAW SRM 51-10-2, PAGE 1, 51-30-2, PAGE 1 ANDSDR CALA9900417Stringer · crackedINSPECTION FOUND A 4 INCH CRACK IN STRINGER 23L BETWEEN STA 1183 AND 1161, JUST BELOW LAV SERVICE PANEL INSIDE AFT CARGO COMPARTMENT. THE CRACKED SECTION OF STRINGER WAS CUT OUT, A NEW STRINGER, DOUBLER AND FILLER COVER PLATE WERE INSTALLED IAW SRM 51-10-2 ANSDR CALA9900407Skin · crackedINSPECTION FOUND A .5 AND .375 INCH CRACK IN LT O/B AILERON LOWER SKIN WITH A BEND AT I/B EDGE. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-10-31.SDR CALA9900401Wire · brokenTHE RT FORWARD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE. THE WIRE WAS REPAIRED IAW WPM 20-10-13, PAGE 1. OPERATION OF THE EXIT LIGHT CHECKED GOOD.SDR CALA9900400Angle · crackedINSPECTION FOUND A 2.75 INCH CRACK IN LT WING REAR SPAR O/B SUPPORT ANGLE WHERE NR 2 SPOILER ACTUATOR AND FLAP DRIVE CASTING MOUNTS. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.SDR CALA9900398Bracket · crackedINSPECTION FOUND A .125 INCH CRACK AT UPPER END OF OUTBOARD BRACKET AT RT WING LEADING EDGE WHERE NR 5 L/E FLAP ACTUATOR MOUNTS. THE FASTENERS AND SUPPORT BRACKET WERE REMOVED IAW SRM 51-20-2. A NEW SUPPORT BRACKET WAS INSTALLED IAW SRM 51-10-1, PARAGRAPH 4 SDR CALA9900397Skin · debondedINSPECTION FOUND LT WING I/B MIDFLAP I/B END OF TRAILING EDGE SKIN DEBONDED. THE DEBONDED AREA WAS CUT OUT, A SKIN AND DOUBLER HOT BOND REPAIR WAS PERFORMED IAW SRM 51-40-6.SDR CALA9900396Control Tab · dentedINSPECTION FOUND THE RT ELEVATOR CONTROL TAB UPPER O/B TRAILING EDGE SKIN DENTED. THE ELEVATOR TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.SDR CALA9900387Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN LT O/B FOREFLAP I/B END CASTING AT LEADING EDGE AND TRAILING EDGE. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.SDR CALA9900386Skin · debondedINSPECTION FOUND LT I/B FOREFLAP UPPER SURFACE DEBONDED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-14.SDR CALA9900385Skin · debondedINSPECTION FOUND RT WING UPPER AND LOWER SKIN DEBONDED O/B AND AFT OF APU EXHAUST AREA. THE SKIN PANEL WAS REPAIRED IAW SRM 51-30-08 PAGE 1.SDR CALA9900384Skin · crackedINSPECTION FOUND A .3125 INCH CRACK IN RT INBOARD AFT FLAP LOWER LEADING EDGE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-02.SDR CALA9900372Wedge · debondedINSPECTION FOUND RT WING O/B MID FLAP T/E WEDGE DEBONDED. THE TRAILING WAS REMOVED AND REPLACED IAW SRM 51-30-2, PAGE 1.SDR CALA9900371Tab · dentedINSPECTION FOUND LEFT ELEVATOR CONTROL TAB LOWER O/B LEADING EDGE SKIN DENTED. THE LEFT ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.SDR CALA9900370Bulkhead Angle · crackedINSPECTION FOUND A .75 INCH CRACK IN FWD BULK VERT ANGLE AT RT WHEEL WELL BS 870 KEEL BEAM. THE FWD BULK VERT ANGLE WAS REPLACED IAW SRM 51-10-1, PAGE 4 AND 51-30-5, PAGE 1.SDR CALA9900369Pressure Deck · crackedINSPECTION FOUND A 3.5 INCH CRACK IN NOSE WHEEL WELL PRESSURE DECK AT FS 270, LBL 14. THE CRACKED AREA WAS CUT OUT, A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40-2.SDR CALA9900368Chord · crackedINSPECTION FOUND A .375 INCH AND .125 INCH CRACK AT LT WING NR 2 SLAT LOWER CHORD BELOW TELESCOPING ANT-ICE TUBE. THREE ACCESS PANELS WERE REMOVED PER SRM 51-30-2 AND THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1, PAGE 6B. AN ANGLE REPAIR DOUBLER WAS INSTALLESDR CALA9900367Chord · crackedINSPECTION FOUND A .3125 INCH CRACK AT LT WING NR 1 SLAT LOWER CHORD AT CUTOUT BELOW TELESCOPING ANTI-ICE TUBE. THE CRACK WAS STOP DRILLED AND AN ANGLE REPAIR WAS INSTALLED IAW SRM 57-30-2.SDR CALA9900366Chord · crackedINSPECTION FOUND A 3 INCH AND .375 INCH CRACK AT RT WING NR 7 SLAT LOWER CHORD. THE LOWER SLAT PANEL WAS REMOVED FOR ACCESS AND REMOVED ANGLE IAW SRM 51-30-2, PAGE 1. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-20 AND 51-30-2. REINSTALLED ACCESS PANEL IAW SRM 5SDR CALA9900365Floorbeam Web · crackedINSPECTION FOUND A 3 INCH CRACK IN FLOORBEAM WEB AT FS 294, RBL 48. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-40-2 FIGURE 1, SHEET 6.SDR CALA9900364Skin · debondedINSPECTION FOUND RT O/B FLAP AFT SEGMENT DEBONDED AT TRAILING EDGE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.SDR CALA9900363Skin · dentedINSPECTION FOUND LT O/B FLAP AFT SEGMENT UPPER SURFACE DENTED AND DEBONDED. THE FLAP WAS REPAIRED IAW SRM 51-40-6.SDR CALA9900362Skin · debondedINSPECTION FOUND LT INBOARD AFT FLAP LOWER SURFACE DEBONDED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-2.SDR CALA9801915Battery · dischargedINSPECTION FOUND RT AFT CARGO DOOR EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REPLACED AND LIGHT WAS RELAMPED.SDR CALA9801234Gear Handle · lack of lubeWHEN GEAR WAS EXTENDED ON APPROACH, CREW RECEIVED THREE GREEN AND THREE RED GEAR INDICATION LIGHTS. THE GEAR WAS CYCLED AND CREW GOT THREE GREEN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR HANDLE STICKING WHEN PULLED OUT. THE SDR CALA9800202Door Frame · crackedINSPECTION FOUND A 5 INCH CRACK IN UPPER AFT SECTION OF R-1 DOOR FRAME AT BS 410. THE CRACKED SECTION OF DOOR FRAME WAS CUTOUT IAW BOEING DRAWING 69-69978. A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-11.SDR CALA9800198Web · crackedINSPECTION FOUND A .125 CRACK IN RT MLG WHEEL WELL PRESSURE WEB AT BS 872.5, RBL 52.25. A PRESSURE WEB REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03671.SDR CALA9800191Support · crackedINSPECTION FOUND CABIN FLOOR SUPPORT WEB CRACKED .125 BEYOND STOP DRILL HOLE AT STA 303.9, LBL 45. THE FLOOR SUPPORT WEB WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, AND 51-30-1.SDR CALA9800190Stringer · corrodedINSPECTION FOUND STRINGER 27R CORRODED IN AFT CARGO COMPARTMENT BETWEEN STA 720 AND 720A. THE CORRODED SECTION OF STRINGER AND SKIN WERE REMOVED. A STRINGER REPAIR, REPAIR SPLICES, AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-3, FIGURE 1, 53-30-3,SDR CALA9800183Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 279, STRINGER 22L. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-1, FIGURE 1, 53-30-3, FIGURE 13, 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9800182Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT CLIP NUTS, STA 380 BETWEEN RBL 24 AND 45. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-8.SDR CALA9800181Skin · corrodedINSPECTION FOUND FUSELAGE SKIN TEAR STRAP CORRODED IN FORWARD CARGO COMPARTMENT AT BS 68, STRINGER 28R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-4, 51-30-8, 51-30-3, FIGURE 12, AND 51-10-2.SDR CALA9800180Support · crackedINSPECTION FOUND A 1.25 INCH CRACK IN LT ELEVATOR SUPPORT AT TRAILING EDGE OF ELEVATOR OUTBOARD OF INBOARD TRIM TAB HINGE BEARING. A 1.25 INCH CRACK WAS FOUND IN RT ELEVATOR OUTBOARD SUPPORT FOR ELEVATOR TRAILING EDGE AT TRIM TAB MOUNT AREA. THE SUPPORTS WERSDR CALA9800179Stringer · corrodedINSPECTION FOUND STRINGER 28R IN FORWARD CARGO COMPARTMENT CORRODED BETWEEN STA 680 AND 700. THE STRINGER SPLICE WAS REMOVED AND A STRINGER SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-30-02, 51-10-2, AND MM 51-20-11.SDR CALA9800178Skin · crackedINSPECTION FOUND A 5.25 INCH CRACK IN FUSELAGE SKIN AT STA 510 BETWEEN STRINGER 25 AND 26R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. THE DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-8 AND 51-30-3.SDR CALA9800177Support · crackedINSPECTION FOUND A 1.5 INCH CRACK ON UPPER FLANGE OF CABIN FLOOR SUPPORT THREE INCHES AFT OF FLOORBEAM AT STA 294.5, RBL 45. THE FLOOR SUPPORT WAS REMOVED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1, 51-10-1, 51-40-3, FIGURE 3, ANSDR CALA9700977Sequence Valve · leakingTHE SYSTEM-A HYDRAULIC FAILURE LIGHTS ILLUMINATED ON CO-PILOT PANEL AFTER GEAR RETRACTION. ALSO, THE A-SYSTEM HYDRAULIC LOW PRESSURE LIGHTS ON SECOND OFFICER'S PANEL ILLUMINATED WITH THE ELEVATOR LOW PRESSURE LIGHT ILLUMINATING MOMENTARILY. THE GEAR WAS LOWESDR CALA9700796Hyd Module · crackedTHE AIRCRAFT WAS DIVERTED TO PHX, AFTER LOSING THE A-HYDRAULIC SYSTEM FLUID QUANTITY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULIC MODULE FITTING CRACKED. THE A-SYSTEM HYDRAULIC MODULE WAS REMOVED AND REPLACED. IN ADDITIONSDR CAL960373Flex Hose · leakingFLT NR 477 - TPA - A/C LOST THE 'B' SYS HYD FLUID IN FLT. THE LOSS WAS ACCOMPANIED BY FLICKERING 'B' SYS HYD LOW PRESS LIGHTS. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MX FOUND THE HYD PRESS FLEX HOSE FROM THE NR 2 ESDR CAL960251Angle · corrodedSTATION 31J - INSPECTION FOUND CORROSION AT BOTTOM OF FLOOR BEAM AT GILL SUPPORT FRAME ANGLE IN AFT CARGO PIT AT BS 1168, RBL 55. THE CORRODED AREA OF ANGLE WAS CUT OUT. A NEW ANGLE AND DOUBLER ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-20-2, ANSDR CAL960266Floor Pan · corrodedINSPECTION FOUND CENTER OF LT AFT LAV FLOOR PAN CORRODED AT BS 1140 TO BS 1176. THE CORROSION WAS REMOVED FROM THE FLOOR PAN. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 51-20-4. (X)SDR CAL960272Channel Support · corrodedSTATION 31J - INSPECTION FOUND CORROSION ON CHANNEL SUPPORT AT BS 803, BL 0. THE CORROSION WAS REMOVED AND A 'T' ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4. (M)SDR CAL960271Panel Support · corrodedSTATION 31J - INSPECTION FOUND LOWER FUSELAGE PANEL SUPPORT CORRODED AT BS 880, LBL 9 AND RBL 9. THE CORRODED AREA WAS CUT OUT. REPAIR ANGLES AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3. (M)SDR CAL960274Flap Track · corrodedSTATION 31J - INSPECTION FOUND CORROSION AT RIGHT MLG BEAM INBOARD FLAP INBOARD TRACK ATTACH POINT. THE AREA WAS REPAIRED IAW ECRA 5750-02438. (M)SDR CAL960273Beam · corrodedINSPECTION FOUND CORROSION ON LT MLG BEAM LOWER FLANGE AT INBOARD FLAP INBOARD TRACK ATTACH POINT. A REPAIR WAS PERFORMED IAW ECRA 5750-02437 AND SRM 51-10-6 AD SRM 51-10-2. (X)SDR CAL960269Floor Beam · corrodedSTATION 31J - INSPECTION FOUND ELONGATED HOLES AND PITTING CORROSION IN FLOOR BEAM AND SEAT TRACK AT BS 1010, RBL 55. THE AREA OF ELONGATED HOLES WAS CUT OUT. REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1. (M)SDR CAL960265Floor Beam · corrodedINSPECTION FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 1110, RBL 26 TO RBL 44. THE CORRODED SECTION OF FLOOR BEAM UPPER CHORD WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, SRM 51-10-2, AND MM 51-20-151. (X)SDR CAL960258Support · corrodedSTATION 31J - INSPECTION FOUND FUSELAGE PANEL SUPPORT CORRODED BELOW ANCHOR NUT AT BS 813, RBL 9 BETWEEN HEAT EXCHANGERS. THE CORRODED AREA WAS CUT OUT, TWO 'L' ANGLES AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-0SDR CAL960257Support · corrodedSTATION 31J - INSPECTION FOUND FUSELAGE PANEL SUPPORT CORRODED BELOW ANCHOR NUT AT BS 813, LBL 9 BETWEEN LEFT AND RIGHT HEAT EXCHANGER. THE CORROSION WAS REMOVED IAW SRM 51-10-2, AN 'L' ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20
Back to N17402, cancelled Apr 27, 2001