N17410, cancelled Jul 22, 2004

Service difficulty reports · 60

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 = 'N17410' AND deregistration_id = 'N17410-2004-07-22'
  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.

SDR EISA20010151Skin · tornACCOMPLISHED SHEET METAL REPAIR AREA FORWARD OF RT OUT FLOW VALVE, STA 1166, STR. 24R.CORRECTIVE ACTION:CUT OUT DAMAGED AREA. FABRICATED DOUBLER .071 2024-T3 8" X 12" IAW B727 SRM 53-30-3, FIG. 3. TREATED & PRIMED AND INSTALLED DOUBLER IAW B727 SRM 51-10-2 & Dec 27, 2001 · N17410 · Boeing 727243 · Fuselage Main, StructureSDR EISA20010119Structure · crackedRT HORIZONTAL STAB O/B T/E CORNER IS CRACKED, TOP SIDE. FOUND DURING B-CHECK. ROUTED OUT CRACK IAW B727 SRM 55-10-1. NDT VERIFIED CRACK BEING REMOVED. FABRICATED DOUBLER AND FILLER PER EO NR 01-236. INSTALLED REPAIR PER EO 01-236 & B727 SRM 57-30-2 WITH APPRAug 29, 2001 · N17410 · Boeing 727243 · Horizontal Stabilizer StructureSDR EISA20000196Plate · misalignedPACK FAN REMAINED ON AFTER FLAPS UP. RUDDER LOAD LIMITER LIGHT REMAINED ON FOR 4 MINUTES AFTER FLAPS UP. REMOVED AND REPLACED RIVETS ON STRIKER ON INBOARD FLAP CONTROL VALVE FOLLOW UP PULLEY. OPS CHECKED INBOARD FLAP FOLLOW UP CABLES, RUDDER LOAD LIMITER INOct 28, 2000 · N17410 · Boeing 727243 · Rudder Control SystemSDR EISA2000001Receiver · shortedNR 1 NAV RECEIVER INOPERATIVE. INSTALLED SERVICEABLE NAV RECEIVER. (M)Dec 29, 1999 · N17410 · Boeing 727243 · Attitude and Direction Data SystemSDR CALA9800863Fuel Pump · failedNUMBER 2 ENGINE FAILED AT ROTATION. FOUND FUEL PUMP SHAFT SHEARED. REPLACED NUMBER 2 ENGINE FUEL PUMP AND FUEL CONTROL PER MM 71-00-67.May 14, 1998 · N17410 · Boeing 727243 · Engine Fuel PumpSDR CALA9800856Battery · dischargedEMERGENCY EXIT LIGHT OVER COCKPIT DOOR INOP. REPLACED BATTERY PACK.May 14, 1998 · N17410 · Boeing 727243 · Emergency LightingSDR CALA9800469Stiffener · crackedINSPECTION FOUND A .1562 INCH CRACK THROUGH FASTENER HOLE AT BOTTOM OF STIFFENER AT INBOARD SIDE OF LT WING LEADING EDGE RIB, WBL 92.0, ACCESS CUTOUT 6303. A REPAIR WAS INSTALLED IAW SRM 51-14-1.Mar 17, 1998 · N17410 · Boeing 727243 · Wing Miscellaneous StructureSDR CALA9800468Floor Track · corrodedINSPECTION FOUND FLOOR TRACK CORRODED AT STA 380 TO 420, RBL 25. THE TRACK WAS REMOVED AND A NEW TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-05-01 AND 51-10-01.Mar 16, 1998 · N17410 · Boeing 727243 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9800467Skin · wornINSPECTION FOUND A GROOVE WORN ON BOTTOM OF LT WING NR 7 SPOILER. THE NR 7 SPOILER WAS REMOVED AND REPLACED.Mar 16, 1998 · N17410 · Boeing 727243 · SpoilersSDR CALA9800466Window · delaminatedINSPECTION FOUND A BURNED SPOT AND A DELAMINATION BUBBLE IN R-1 WINDOW UPPER EDGE. THE R-1 WINDOW WAS REMOVED AND REPLACED IAW MM 56-11-11.Mar 16, 1998 · N17410 · Boeing 727243 · Flight Compartment WindowsSDR CALA9800465Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN J-BEAM ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. THE J-BEAM WAS REPAIRED IAW ECRA 5750-02193 AND EA 26865-5075.Mar 16, 1998 · N17410 · Boeing 727243 · Wing Miscellaneous StructureSDR CALA9800464Foreflap · damagedINSPECTION FOUND LT INBOARD FOREFLAP CRUSHED (4 AREA) AT INBOARD END. THE FOREFLAP WAS REMOVED AND REPLACED.Mar 16, 1998 · N17410 · Boeing 727243 · Trailing Edge FlapsSDR CALA9800463Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN R-1 DOOR CUTOUT AT FS 417. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5307-01141.Mar 16, 1998 · N17410 · Boeing 727243 · Fuselage Main, Plate/SkinSDR CALA9800442Skin · dentedINSPECTION FOUND LT OUTBOARD AILERON OUTBOARD UPPER TRAILING EDGE HAD A PREVIOUSLY FILLED SMALL DENT WITH FILLER BREAKING OUT. THE DENTED AREA WAS CUT OUT AND A HOT BONDED REPAIR WAS INSTALLED IAW SRM 51-40-6.Mar 13, 1998 · N17410 · Boeing 727243 · AileronsSDR CALA9800441Skin · crackedINSPECTION FOUND A .375 INCH CRACK IN LT WING FIXED LEADING EDGE CUTOUT ABOVE NR 3 SLAT OUTBOARD TRACK AREA. A SKIN FLUSH REPAIR WAS INSTALLED IAW SRM 57-30-4.Mar 13, 1998 · N17410 · Boeing 727243 · Wing, Plate/SkinSDR CALA9800440Skin · dentedINSPECTION FOUND A DENT 19.5 INCHES FROM OUTBOARD END IN LT WING NR 2 LEADING EDGE SLAT UPPER SKIN. A REPAIR WAS INSTALLED IAW SRM 57-50-3.Mar 13, 1998 · N17410 · Boeing 727243 · Leading Edge DevicesSDR CALA9800439Splice · crackedINSPECTION FOUND A 3 INCH CRACK AT SPLICE PLATE ON LOWER SURFACE OF LT WING UPPER LEADING EDGE SKIN DIRECTLY ABOVE NR 2 LEADING EDGE FLAP ACTUATOR, FSS 224. THE SPLICE PLATE WAS CUT OUT, A NEW PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-2.Mar 13, 1998 · N17410 · Boeing 727243 · Wing Miscellaneous StructureSDR CALA9800438Bracket · crackedINSPECTION FOUND A 2 INCH CRACK IN BRACKET AT AFT FACE OF LT GEAR BEAM WHERE HYDRAULIC LINES PASS THROUGH ACCESS DOOR 8405. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-0, 51-10-2, AND 51-30-2.Mar 13, 1998 · N17410 · Boeing 727243 · Wing Miscellaneous StructureSDR CALA9800437Angle · crackedINSPECTION FOUND A .5 INCH CRACK THROUGH AFT FASTENER HOLE AT REPAIR ANGLE INSIDE LT WING LEADING EDGE RIB, WS 330, AFT OF NR 4 SLAT, INBOARD END. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6.Mar 13, 1998 · N17410 · Boeing 727243 · Wing Miscellaneous StructureSDR CALA9800436Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING NR 1 SLAT LOWER LEADING EDGE SKIN TO INBOARD TRACK ATTACH BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-1.Mar 13, 1998 · N17410 · Boeing 727243 · Leading Edge DevicesSDR CALA9800435Skin · disbondedINSPECTION FOUND RT TRAILING EDGE INBOARD FOREFLAP DISBONDED IN TWO AREAS. THE FOREFLAP WAS REMOVED AND REPLACED.Mar 13, 1998 · N17410 · Boeing 727243 · Trailing Edge FlapsSDR CALA9800434Angle · crackedINSPECTION FOUND A 1.6 INCH CRACK AT BOTTOM OF LEFT CURVED SIDEWALL SUPPORT ANGLE MOUNTED TO FORWARD SIDE OF CIRCUMFERENTIAL STA 950D. A NEW SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-40-3.Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9800433Skin · corrodedINSPECTION FOUND CORROSION IN SKIN ATTACH LEG AT FORWARD SIDE OF CIRCUMFERENTIAL, BS 1148, STRINGER 28L AND 29L. THE CORROSION WAS CUT OUT IAW SRM 51-10-6. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-10-6.Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage Main, Plate/SkinSDR CALA9800432Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL UPPER SUPPORT ANGLE BETWEEN FLOORBEAM SUPPORT, STA 720 AND 720A. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9800431Skin · crackedINSPECTION FOUND A .0937 INCH CRACK AT LT WING UPPER SKIN CUTOUT FOR NR 2 SPOILER. THE FASTENERS WERE REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-4, 51-10-2, AND 57-30-2.Mar 13, 1998 · N17410 · Boeing 727243 · SpoilersSDR CALA9800430Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN FALSE SPAR LOWER ANGLE BELOW AND INBOARD OF NR 7 SPOILER ACTUATOR INBOARD COVE AREA. REPAIRED FALSE SPAR LOWER ANGLE IAW EA NR 26865-5182 AND REINSTALLED ADJACENT STRUCTURE IAW SRM 51-30-2.Mar 13, 1998 · N17410 · Boeing 727243 · SpoilersSDR CALA9800429Hinge · crackedINSPECTION FOUND A .5 INCH CRACK IN RT ELEVATOR BALANCE PANEL NR 9214 FORWARD HINGE. THE HINGE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.Mar 13, 1998 · N17410 · Boeing 727243 · Elevator StructureSDR CALA9800428Stringer · crackedINSPECTION FOUND VERTICAL STABILIZER INTERNAL COMPARTMENT NR 9 RT NR 3 STRINGER CRACKED 1 BEHIND ATTACH BOLT. REMOVED FASTENERS IAW SRM 51-30-2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-2, AND 51-40-5.Mar 13, 1998 · N17410 · Boeing 727243 · Vertical StabilizerSDR CALA9800427Stringers · crackedINSPECTION FOUND VERTICAL STABILIZER INTERNAL COMPARTMENT NR 6 RT NR 3 STRINGER AND NR 5 STRINGER CRACKED 1 BEHIND ATTACH BOLT. REMOVED FASTENERS IAW SRM 51-30-2. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-2, AND 51-40-5.Mar 13, 1998 · N17410 · Boeing 727243 · Vertical StabilizerSDR CALA9800426Gusset · crackedINSPECTION FOUND A 2 CRACK IN GUSSET ON FORWARD SIDE OF RT FUSELAGE FRAME AT STA 825, RBL 70. THE GUSSET WAS REMOVED AND A NEW ONE WAS INSTALLED IAW EA SA012-5310-01870.Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9800425Web · crackedINSPECTION FOUND A 7 CRACK JUST BELOW DRAIN CHUTE IN LT AFT LAV FLOOR WEB AT BS 1176, LBL 50. THE CRACKED SECTION OF WEB WAS REMOVED. A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-20-01.Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9800424Skin · bulgedINSPECTION FOUND RT FUSELAGE SKIN BULGED JUST AFT AND BELOW FORWARD LAV SERVICE PANEL. THE BULGED AREA WAS REMOVED. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-10-2.Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage Main, Plate/SkinSDR CALA9800423Floor Track · corrodedINSPECTION FOUND CABIN FLOOR TRACK CORRODED AT STA 1050 TO 1130, BL 25R. THE CORRODED SECTION OF FLOOR TRACK WAS REPLACED IAW SRM 53-10-5 AND 51-10-1.Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9800422Floor Track · corrodedINSPECTION FOUND CABIN FLOOR TRACK CORRODED AT STA 1100, BL 45R. THE CORRODED SECTION OF FLOOR TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-5.Mar 13, 1998 · N17410 · Boeing 727243 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9800718Battery Pack · dischargedTHE EMERGENCY EXIT SIGN IVER COCKPIT DOOR FELL OUT AND WAS FOUND INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK AND LENSE ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.Mar 12, 1998 · N17410 · Boeing 727243 · Emergency LightingSDR CALA9800421Intercostal · crackedINSPECTION FOUND A 1.25 CRACK IN SUPPORT INTERCOSTAL AT AFT BAGGAGE COMPARTMENT BETWEEN BS 1030 AND 1050 ABOVE STRINGER 25L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.Mar 12, 1998 · N17410 · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9800143Light · inoperativeINSPECTION FOUND EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. THE EXIT LIGHT WAS REMOVED AND REPLACED.Jan 31, 1998 · N17410 · Boeing 727243 · Emergency LightingSDR CALA9700787Brake Housing · crackedACFT RETURNED TO THE GATE AFTER DRAGGING THE NR 3 BRAKE DURING TAXI. THE NR 3 TIRE CAUGHT ON FIRE, FOAM WAS USED TO EXTINGUISH THE FIRE. THE NR 3 AND 4 MAIN TIRE/WHEEL ASSEMBLIES AND BRAKES WERE REMOVED AND REPLACED. THE NR 3 BRAKE DEBOOST VALVE WAS ALSO REMay 26, 1997 · N17410 · Boeing 727243 · BrakeSDR CALA9700516Skin · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT INTERIOR SKIN CORRODED AT ANTENNA, STA 1030 TO 1050, STRINGER 29R TO 30. THE AREA WAS REPAIRED IAW SRM 51-40-3.Mar 27, 1997 · N17410 · Boeing 727243 · Fuselage Main, Plate/SkinSDR CALA9700581Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN VENTRAL STAIRWELL TORQUE BOX ANGLE AT STAIR ACTUATOR FITTING, STA 1272, RBL 22. A REPAIR WAS INSTALLED IAW BOEING DRAWING 65C27136.Mar 26, 1997 · N17410 · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9700519Skin · disbondedINSPECTION FOUND LT INBOARD MIDFLAP UPPER SURFACE OF TRAILING EDGE WEDGE DISBONDED 24 INCHES FROM INBOARD END. THE DISBONDED AREA WAS CUT OUT, CORE AND DOUBLERS WERE FABRICATED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.Mar 26, 1997 · N17410 · Boeing 727243 · Trailing Edge FlapsSDR CALA9700515Skin · corrodedINSPECTION FOUND LT FUSELAGE SKIN CORRODED AT STA 1130. THE CORRODED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1.Mar 26, 1997 · N17410 · Boeing 727243 · Fuselage Main, Plate/SkinSDR CALA9700512Spar Web · crackedINSPECTION FOUND A .75 CRACK IN WEB AT FRONT SPAR JUST OUTBOARD OF LT FORWARD TERMINAL PIN FITTING. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-40-2.Mar 26, 1997 · N17410 · Boeing 727243 · Wing SparSDR CALA9700511Skin · crackedINSPECTION FOUND A .5 INCH CRACK AT AFT OUTBOARD END OF CUTOUT FOR NR 6 SLAT OUTBOARD HOOK OF RT WING FIXED LEADING EDGE. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 57-30-4.Mar 26, 1997 · N17410 · Boeing 727224 · Wing, Plate/SkinSDR CALA9700580Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING FIXED LEADING EDGE SKIN AT NR 6 SLAT OUTBOARD TRACK CUTOUT, STA 216. THE CRACK WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5730-01489.Mar 25, 1997 · N17410 · Boeing 727243 · Wing, Plate/SkinSDR CALA9700518Skin · delaminatedINSPECTION FOUND OUTBOARD END OF LT OUTBOARD AILERON TAB DELAMINATED. THE TAB WAS REMOVED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. THE TAB WAS REINSTALLED.Mar 25, 1997 · N17410 · Boeing 727243 · Aileron TabsSDR CALA9700514Skin · disbondedINSPECTION FOUND LEFT OUTBOARD FOREFLAP DISBONDING AT INBOARD END. THE END CAP WAS REMOVED, THE DISBONDED AREA WAS CUT OUT, A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6 AND THE END CAP WAS REINSTALLED.Mar 25, 1997 · N17410 · Boeing 727243 · Trailing Edge FlapsSDR CALA9700513Rib · crackedINSPECTION FOUND A 1 INCH CRACK BETWEEN TWO AFT UPPER BOLTS OF LT WING LEADING EDGE RIB AT SLAT STA 0. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.Mar 25, 1997 · N17410 · Boeing 727243 · Wing, Rib/BulkheadSDR CAL960427Frame · crackedINSPECTION FOUND A 1.5 INCH CRACK IN AFT BAG PIT FLOOR LEVEL FRAME AT BS 1166, RBL 24. THE CRACKED AREA WAS CUT OUT. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, AND 51-30-2. (M)Feb 27, 1996 · N17410 · Boeing 727243 · Fuselage Main, FrameSDR CAL960431Floorbeam · oversized holeINSPECTION FOUND OVERSIZED HOLE ON MAIN CABIN INTERIOR FLOORBEAM AT BS 350, RBL 40. THE EFFECTED SECTION WAS REMOVED. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, 51-10-2, 51-30-8 AND MM 51-20-2. (M)Feb 25, 1996 · N17410 · Boeing 727243 · Fuselage Main, Floor Beam
Back to N17410, cancelled Jul 22, 2004