N17407, cancelled Jan 18, 2002
Service difficulty reports · 68
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 = 'N17407' AND deregistration_id = 'N17407-2002-01-18' 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 = 'N17407' AND deregistration_id = 'N17407-2002-01-18' 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 CALA9900377Power Supply · inoperativeTHE INTERIOR EMERGENCY EXIT LIGHTS FOR LEFT OVERWING DOOR WOULD NOT ILLUMINATE. THE POWER SUPPLY WAS REMOVED AND REPLACED.SDR CALA9900143Battery · dischargedINSPECTION FOUND THE LT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATION CHECKED GOOD.SDR CALA9900142Duct · failedNR 3 ENG FIRE WARNING ACTIVATED AFTER T/O FROM BWI. THE A/C WAS RETURNED TO BWI WHERE IT LANDED W/O INCIDENT. MX FOUND THE PNEUMATIC DUCT LEADING TO NR 3 NOSE COWL ANTI-ICE VALVE BLOWN. THE NOSE COWL FLANGE FITTING FOR COWL ANTI-ICE INLET WAS ALSO BLOWN. TSDR CALA9900115Duct · brokenA FIRE WARNING INDICATION ON THE NR 3 ENGINE WAS RECEIVED AFTER TAKEOFF FROM BWI. CHECKLIST PROCEDURES WERE FOLLOWED, FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 3 ENGISDR CALA9802196Anti Ice Duct · brokenTHE NR 3 ENGINE FIRE WARNING LIGHT CAME ON DURING CLIMB-OUT OF IAH. THE ENGINE POWER WAS REDUCED AND THE LIGHT EXTINGUISHED. WHEN POWER WAS ADVANCED THE WARNING LIGHT CAME ON AGAIN. THE NR 3 ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT SDR CALA9802172Chord · corrodedINSPECTION FOUND AFT RT LAV FLOOR REINFORCEMENT CHORD CORRODED AT BS 1176, RBL 26. THE CORRODED AREA WAS BLENDED OUT. A FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5310-03799 AND BOEING SKETCH CAL-MIA-98-CC55TR.SDR CALA9802171Track · corrodedTHE RT WING NR 5 FLAP TRACK WAS FOUND CORRODED. THE NR 5 FLAP TRACK ASSEMBLY WAS REMOVED AND REPLACED IAW MM 27-57-31.SDR CALA9802170Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR UPPER AFT OVERCENTER STOP LOCK FITTING. THE STOP LOCK, FITTING, AND PLATE WERE REMOVED. A NEW FITTING, STOP LOCK, AND PLATE WERE INSTALLED IAW SRM 51-10-1.SDR CALA9802168Cylinder · corrodedINSPECTION FOUND THE RT MLG OUTER CYLINDER THREADS FOR GLAND NUT CORRODED. THE RT MLG WAS REMOVED AND REPLACED.SDR CALA9802167Stiffener · crackedINSPECTION FOUND A .5 INCH CRACK IN RT ELEVATOR CONTROL TAB ROD STIFFENER PLATE IN COVE AREA. THE CRACKED AREA WAS REMOVED, AN ANGLE WAS INSTALLED IAW SRM 51-20-1, PAGE 7.SDR CALA9802166Fitting · corrodedINSPECTION FOUND RT WING NR 5 FLAP TRACK FORWARD FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW BOEING DRAWING 65-19297.SDR CALA9802165Mount Pad · corrodedINSPECTION FOUND NR 5 FLAP TRACK AFT MOUNTING FLANGE ON FALSE SPAR WORN AND CORRODED. THE MOUNT PAD WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 1.SDR CALA9802164Skin · bentINSPECTION FOUND LT INBOARD FOREFLAP INBOARD MOST UPPER SKIN LOOSE AND BENT. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-3.SDR CALA9802158Power Supply · inoperativeINSPECTION FOUND LT OVERWING CABIN INTERIOR EMERGENCY LIGHT INOPERATIVE. THE POWER SUPPLY WAS REPLACED IAW MM 33-50-0.SDR CALA9802157Power Supply · inopINSPECTION FOUND RT OVERWING CABIN INTERIOR EMERGENCY LIGHT INOPERATIVE. THE POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-50-0.SDR CALA9802156Stiffener · corrodedINSPECTION FOUND THE LT WING NR 2 LE FLAP O/B HINGE CORRODED AROUND HINGE ARM BOLTS AND O/B VERTICAL STIFFENER HAD CORROSION AROUND BONDING WIRE BOLT HOLE. THE NR 2 LE FLAP WAS REPLACED IAW MM 27-81-1, PAGES 404-406.SDR CALA9802155Skin · debondedINSPECTION FOUND LT O/B AILERON TRAILING EDGE O/B CORNER DEBONDED. THE AILERON WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2, PAGE 18 AND 51-8-4.SDR CALA9802154Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1130, RBL 34. A REPAIR WAS INSTALLED IAW ECRA 5310-03790.SDR CALA9802153Angle · crackedINSPECTION FOUND A 5 INCH CRACK IN L ANGLE AT FORWARD I/B CORNER OF RT MLG WHEEL WELL, BEHIND APU, STA 870. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.SDR CALA9802152Bracket · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RT ELEVATOR NR 4 ATTACH HINGE BRACKET AT ELEVATOR STA 99.79. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2, PAGE 1, 51-10-1, AND 51-10-2.SDR CALA9802151Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN LT WING SECOND UPPER STRINGER FROM AFT SPAR AT WS 686.50. AN ANGLE REPAIR WAS WAS INSTALLED IAW EA 5762-01050.SDR CALA9802150Stringer · crackedINSPECTION FOUND A 1.5 INCH CRACK LT STRINGER 9 INSIDE VERTICAL STABILIZER AT RIB NR 8. THE CRACKED AREA WAS CUT OUT IAW SRM 55-30-4, PAGE 1. REPAIR ANGLES WERE INSTALLED IAW SRM 51-30-4 AND 51-10-2, PAGE 21.SDR CALA9802149Skin · corrodedINSPECTION FOUND LT O/B AILERON TAB LOWER SURFACE CORRODED AT O/B END AND A SMALL DEBONDED AREA. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41, PAGE 401-403.SDR CALA9802148Chord · corrodedINSPECTION FOUND CHORD CORRODED IN COCKPIT FLOOR PANEL AT F/E SEAT AFT STOP. THE CHORD WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2, PAGE 4.SDR CALA9802147Rib · crackedINSPECTION FOUND A 1.25 INCH CRACK AROUND BOLT HEADS AT UPPER AFT END OF LT WING FIXED LE RIB, WS 330. THE RIB WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2, PAGE 3, 51-40-3, 51-10-6, PAGE 1, AND 51-10-1, PAGE 1.SDR CALA9802146Skin · dentedINSPECTION FOUND RT O/B AILERON TAB UPPER SURFACE DENTED. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41.SDR CALA9802124Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT ANGLE CORRODED AT STA 420, RBL 62. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW 53-30-2 AND 51-30-2.SDR CALA9802123Web · corrodedINSPECTION FOUND WEB CORRODED WHERE R-1 FORWARD DRAIN LINE FITTING ATTACHES, FS 378. THE CORRODED AREA OF WEB WAS REMOVED IAW SRM 51-40-2. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-2, PAGE 7 AND 51-10-2, PAGE 2.SDR CALA9802122Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 LEADING EDGE FLAP ACTUATOR MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-10-2 AND 51-30-7.SDR CALA9802121Floorbeam · corrodedINSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 1110, RBL 44. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-10-8, PAGE 44.SDR CALA9802111Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN I/B AND O/B BRACKETS AT LT WING NR 2 LE FLAP ACTUATOR MOUNT. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE INSTALLED IAW SRM 51-30-2, FIGURE 1.SDR CALA9802104Chord · crackedINSPECTION FOUND A 2.25 INCH CRACK IN LT WING NR 3 SLAT AT LOWER CHORD BELOW OUTBOARD STOP PAD. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR CALA9802102Skin · corrodedINSPECTION FOUND RT FUSELAGE SKIN CORRODED AT STA 1050, STRINGER 28R. THE CORRODED AREA WAS CUT OUT, A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-10-1, 51-10-2, 53-30-3, PAGE 14.SDR CALA9802097Floorbeam · corrodedINSPECTION FOUND AFT CARGO FLOORBEAM CORRODED AT STA 1070, RBL 12 TO 48. A REPAIR WAS INSTALLED IAW SRM 53-10-8.SDR CALA9802094Angle · crackedINSPECTION FOUND CRACKS IN LOWER ANGLE AT O/B SIDE OF RIB AROUND SEVEN BOLT HEADS INSIDE LT WING LE AFT OF NR 3 LE FLAP I/B END, FS 121. THE ANGLE WAS REMOVED IAW SRM 51-30-2, PAGE 3 AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-3, 51-10-2, PAGE 12 AND 51-30-2 SDR CALA9802093Stiffener · crackedINSPECTION FOUND A .75 INCH CRACK IN LT WING RIB STIFFENER AT LOWER END, WBL 92.0. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3.SDR CALA9800361Light · inoperativeINSPECTION FOUND THE EMERGENCY EXIT LIGHT AT ROW 28 AND 29 INOPERATIVE. THE EXIT SIGN WAS REMOVED AND REPLACED. ALSO, MAINTENANCE FOUND PIN AT SIGN CANNON PLUG BENT AND BROKEN WIRING. THE PIN AND WIRING WERE REPAIRED AND OPERATION OF THE LIGHT WAS NORMAL.SDR CALA9800092Frame · crackedINSPECTION FOUND A 3.5 CRACK IN UPPER AFT CORNER OF R-1 DOOR FRAME. A REPAIR WAS FABRICATED AND INSTALLED IAW DRAWING 69-69978, SRM 57-10-02, AND ECRA 5240-01223.SDR CALA9800091Lugs · corrodedINSPECTION FOUND HORIZONTAL STABILIZER LEFT AND RIGHT BEARING SUPPORT VERTICAL LUGS CORRODED. THE LT VERTICAL LUGS WERE REWORKED IAW ECRA 5550-01033. THE RT VERTICAL LUGS WERE REWORKED IAW ECRA 5550-01141.SDR CALA9800090Skin · corrodedINSPECTION FOUND RT WING INBOARD MID-FLAP UPPER SKIN PILLOWED WITH DISHED FASTENERS IN AREA ABOVE REAR SPAR UPPER CHORD APPROXIMATELY 21 INCHES FROM INBOARD END AND EXTENDING OUTBOARD 6.5 INCHES. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRSDR CALA9800083Torus · crackedINSPECTION FOUND A 5 INCH CRACK IN INBOARD WELD SEAM OF APU TORUS ASSEMBLY. THE APU WAS REMOVED AND REPLACED IAW MM 49-10-01. LEAK AND OPERATIONAL CHECKS WERE GOOD.SDR CALA9800082Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1060, STRINGER 27L. THE CORROSION WAS REMOVED AND THE SKIN WAS REPAIRED IAW SRM 53-30-3.SDR CALA9800081Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT CLIPNUTS, STA 380, RBL 24 TO RBL 62. TWO L-ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-30-8 FIGURE 8.SDR CALA9800080Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT CLIPNUT ON UPPER FORWARD FLANGE LOWER SURFACE AT STA 328, LBL 48. THE FLOORBEAM WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 53-10-8 AND 53-20-11.SDR CALA9701252Slide · low pressureTHE CREW FOUND L-1 DOOR EMERGENCY SLIDE PRESSURE LOW. THE L-1 DOOR SLIDE WAS REMOVED AND REPLACED PER MM 25-60-15.SDR CALA9601700Angle · crackedINSPECTION FOUND RT WING NR 11 SPOILER ACTUATOR SUPPORT FITTING INBOARD ATTACH ANGLE CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.SDR CALA9601687Skin · corrodedINSPECTION FOUND SKIN CORRODED UNDER WEB IN AFT CARGO COMPARTMENT AT STA 970, STRINGER 28L. THE CORRODED AREA OF SKIN WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9601689Stringer · corrodedINSPECTION FOUND STRINGER 28L CORRODED AT STA 965 IN AFT CARGO COMPARTMENT. THE CORRODED SECTION OF STRINGER WAS CUT OUT, A REPLACEMENT STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3.SDR CALA9601697Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 3 SLAT ACTUATOR OUTBOARD ATTACH RIB. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-40-3.SDR CALA9601696Rib · crackedINSPECTION FOUND A .75 INCH CRACK IN NR 3 SLAT ACTUATOR INBOARD ATTACH RIB. A REPAIR PART WAS FABRICATED, HEAT TREATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.
Back to N17407, cancelled Jan 18, 2002