N17025, cancelled Jul 11, 2003

Service difficulty reports · 48

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 = 'N17025' AND deregistration_id = 'N17025-2003-07-11'
  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 CALA9802066Skin · damagedTHE LOWER FUSELAGE BELLY SKIN WAS FOUND TO BE PUNCTURED BY GROUND EQUIPMENT AT STA 1997. THE PUNCTURED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-30-3, FIGURE 19, 53-10-3, FIGURE 1 AND 51-40-4, FIGURE 2.Nov 14, 1998 · N17025 · Boeing 747238B · Fuselage Main, Plate/SkinSDR CALA9700753Power Supply · inoperativeINSPECTION FOUND AIRCRAFT LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE POWER SUPPLY AT L-3 DOOR WAS REMOVED AND REPLACED.May 18, 1997 · N17025 · Boeing 747238B · Emergency LightingSDR CALA9700040Channel · crackedINSPECTION FOUND A .125 INCH CRACK IN AFT SUPPORT CHANNEL AT LT WING NR 4 LEADING EDGE FLAP. THE CHANNEL WAS REPAIRED IAW SRM 51-40-03, FIGURE 2.Dec 22, 1996 · N17025 · Boeing 747238B · Leading Edge DevicesSDR CALA9700038Rib · corrodedINSPECTION FOUND TOP RIB CHORD CORRODED AT LT WING LEADING EDGE, WS 614. THE RIB CHORD WAS REPAIRED IAW SRM 51-40-02, FIGURE 1.Dec 22, 1996 · N17025 · Boeing 747238B · Wing, Rib/BulkheadSDR CALA9700033Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN VERTICAL SUPPORT ANGLE OF RT WING LEADING EDGE NOSE STRUCTURE BACKING WEB AT INBOARD LEADING EDGE STA 631. THE ANGLE WAS REPLACED IAW SRM 51-10-01.Dec 22, 1996 · N17025 · Boeing 747238B · Wing Miscellaneous StructureSDR CALA9700032Chord · crackedINSPECTION FOUND A 6 INCH CRACK IN UPPER CHORD OF RT WING OUTBOARD MID FLAP OUTBOARD REAR SPAR. THE CHORD WAS REPAIRED IAW SRM 51-40-02.Dec 22, 1996 · N17025 · Boeing 747238B · Trailing Edge FlapsSDR CALA9700031Web · crackedINSPECTION FOUND A 2 INCH CRACK IN FORWARD SPAR WEB OF LT WING AT WS 780. THE WEB WAS REPAIRED IAW SRM 51-40-02, FIGURE 1.Dec 22, 1996 · N17025 · Boeing 747238B · Wing SparSDR CALA9700030Web · crackedINSPECTION FOUND A .5 INCH CRACK IN THREE LOCATIONS OF MOST INBOARD WEB OF RT WING INBOARD FOREFLAP. THE WEB WAS REPLACED IAW SRM 51-10-01, PAGE 18.Dec 22, 1996 · N17025 · Boeing 747238B · Trailing Edge FlapsSDR CALA9700028Stiffener · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FORWARD VERTICAL STIFFENER AT LT WING LEADING EDGE RIB, INBOARD LEADING EDGE STA 636.72. THE STIFFENER WAS REPLACED IAW SRM 51-10-01.Dec 22, 1996 · N17025 · Boeing 747238B · Wing Miscellaneous StructureSDR CALA9700027Chord · crackedINSPECTION FOUND AN 8 INCH CRACK IN UPPER CHORD OF LT WING OUTBOARD MID FLAP OUTBOARD REAR SPAR. THE CHORD WAS REPAIRED IAW SRM 51-40-02.Dec 22, 1996 · N17025 · Boeing 747238B · Trailing Edge FlapsSDR CALA9700034Door Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN DOOR FRAME AT BS 440, STRINGER 26R. THE DOOR FRAME WAS REPAIRED IAW SRM 52-10-02, FIGURE 2.Dec 19, 1996 · N17025 · Boeing 747238B · Passenger/Crew DoorsSDR CALA9700037Rib · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RIB CHORD AT RT WING NR 3 MAIN TANK, WS 670. THE RIB CHORD WAS REPAIRED IAW SB 57-2273.Dec 16, 1996 · N17025 · Boeing 747238B · Wing, Rib/BulkheadSDR CALA9700036Frame · crackedINSPECTION FOUND A .75 INCH CRACK IN FRAME WEB AT STRINGER 24R AND A .75 INCH CRACK WAS FOUND IN FRAME WEB AT STRINGER 24L, BS 800. THE WEBS WERE REPAIRED IAW SRM 53-10-04, FIGURE 84.Dec 16, 1996 · N17025 · Boeing 747238B · Fuselage Main, FrameSDR CALA9700035Web · crackedINSPECTION FOUND A .75 INCH CRACK IN WEB AT BS 1650, STRINGER 24L. THE WEB WAS REPAIRED IAW SRM 53-10-04, FIGURE 84.Dec 16, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous StructureSDR CALA9700029Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN RIB TOP AREA OF LT WING INBOARD LEADING EDGE STA 628. THE RIB WAS REPAIRED IAW SRM 51-40-02.Dec 12, 1996 · N17025 · Boeing 747238B · Wing, Rib/BulkheadSDR CALA9700039Doubler · crackedINSPECTION FOUND A .25 INCH CRACK IN DOUBLER AT BS 400 BULKHEAD AFT FACE, WL 120, RBL 40. A REPAIR WAS ACCOMPLISHED IAW SRM 53-10-04, FIGURE 37.Dec 11, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous StructureSDR CALA9601841Web · crackedINSPECTION FOUND A 3.5 INCH CRACK IN BEAM WEB AT BS 980, STRINGER 5R. THE WEB WAS REPLACED IAW SRM 51-10-01.Dec 5, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous StructureSDR CALA9601840Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1367, RBL 11 TO RBL 33. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-01.Dec 4, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous StructureSDR CALA9601839Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1280, LBL 11 TO RBL 11. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-01.Dec 4, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous StructureSDR CALA9601838Angle · corrodedINSPECTION FOUND ANGLE CORRODED AT BS 480, LBL 89. THE ANGLE WAS REPLACED IAW SRM 51-10-01.Dec 4, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous StructureSDR CALA9601837Support · corrodedINSPECTION FOUND LATERAL FLOOR SUPPORT CORRODED AT BS 1300, RBL 11 TO 33. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-01.Dec 4, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous StructureSDR CALA9601833Fittings · corrodedINSPECTION FOUND STRINGER END FITTINGS CORRODED AT BS 2360, S49L, S50L, S51L, S48R AND S51R. THE STRINGER END FITTINGS WERE REPLACED IAW SRM 51-10-01.Dec 3, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous StructureSDR CALA9601836Support Plate · corrodedINSPECTION FOUND FLOOR SUPPORT PLATE CORRODED AT BS 1259, RBL 11 TO 33. THE FLOOR SUPPORT PLATE WAS REPLACED IAW SRM 51-10-01.Nov 29, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous StructureSDR CALA9601835Support · corrodedINSPECTION FOUND TWO FLOOR SUPPORTS CORRODED AT BS 1259, LBL 33 TO RBL 11. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-10-01.Nov 29, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous StructureSDR CALA9601834Support · corrodedINSPECTION FOUND TWO FLOOR SUPPORTS CORRODED AT BS 765 TO 880, LBL 36. THE CORROSION WAS REMOVED AND TREATED, THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-10-01 AND 51-10-02.Nov 22, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous StructureSDR CALA9700006Stringer · crackedINSPECTION FOUND CRACKS IN STRINGER 2R AND 2AR AT BS 741. THERE WERE A TOTAL OF FOUR CRACKS MEASURING 2.5, 1.18, 1.38, AND 0.62 LONG. THE STRINGERS WERE REPAIRED IAW ECRA 5310-03383.Nov 9, 1996 · N17025 · Boeing 747238B · Fuselage Main, Longeron/StringerSDR CALA9700007Skin · corrodedINSPECTION FOUND CORROSION IN SKIN LAP SPLICE AT SEVERAL LOCATIONS FROM BS 520 TO 741, STRINGER 6L. THE SKIN WAS REPAIRED IAW ECRA 5330-02472.Nov 8, 1996 · N17025 · Boeing 747238B · Fuselage Main, Plate/SkinSDR CALA9700015Fitting · crackedINSPECTION FOUND SPLICE FITTING AND UPPER SPLICE PLATE CRACKED AT LT WING REAR SPAR. THE CRACKS WERE 0.040 AND .25 INCH LONG. THE SPLICE PLATE AND SPLICE FITTING WERE REPLACED IAW EA 5710-01199 AND BOEING SB 57-2110.Nov 7, 1996 · N17025 · Boeing 747238B · Wing SparSDR CALA9700003Doubler · corrodedINSPECTION FOUND CORROSION ON LT WING OUTBOARD TRAILING EDGE MID FLAP OUTBOARD DOUBLER. THE DOUBLER WAS REPAIRED IAW ECRA 5750-02581.Nov 7, 1996 · N17025 · Boeing 747238B · Trailing Edge FlapsSDR CALA9700002Lug · wornINSPECTION FOUND LT WING NR 4 MOVEABLE FLAP TRACK FAIRING DRIVE ARM LOWER OUTBOARD HINGE OUTBOARD LUG WORN. THE WORN AREA WAS REPAIRED IAW ECRA 5750-02580.Nov 7, 1996 · N17025 · Boeing 747238B · Trailing Edge FlapsSDR CALA9700001Frame · crackedINSPECTION FOUND A 1.75 INCH CRACK IN RT FRAME AT BS 220, STRINGER 32A. THE FRAME WAS REPAIRED IAW ECRA 5310-03374.Nov 7, 1996 · N17025 · Boeing 747238B · Fuselage Main, FrameSDR CALA9700022Stringer · crackedINSPECTION FOUND A .125 INCH CRACK IN STRINGER 3R AT MAIN DECK BS 2180 TO 2190. THE STRINGER WAS REPAIRED IAW SRM 53-10-03, FIGURE 6.Nov 6, 1996 · N17025 · Boeing 747238B · Fuselage Main, Longeron/StringerSDR CALA9700017Stringer · crackedINSPECTION FOUND A 1 INCH CRACK IN STRINGER 9R AT BS 990 MANUFACTURING SPLICE LOCATION. THE STRINGER WAS REPAIRED IAW ECRA 5310-03384.Nov 6, 1996 · N17025 · Boeing 747238B · Fuselage Main, Longeron/StringerSDR CALA9700016Skin · crackedINSPECTION FOUND A 0.040 CRACK AT THE RT WING EXTERNAL SPLICE FITTING AND A .1875 INCH CRACK AT THE MATING STRUCTURE WING CENTER SECTION UPPER SKIN PANEL. THE SPLICE FITTING WAS REPLACED IAW EA 5710-01199. THE SKIN PANEL WAS REPAIRED IAW ECRA 5710-01769.Nov 6, 1996 · N17025 · Boeing 747238B · Wing, Plate/SkinSDR CALA9700005Stringer · crackedINSPECTION FOUND A 0.87 INCH CRACK AT INBOARD VERTICAL FLANGE FASTENER HOLE OF STRINGER 9R AT THE MANUFACTURING SPLICE LOCATION, BS 1740. THE STRINGER WAS REPAIRED IAW ECRA 5310-03373.Nov 6, 1996 · N17025 · Boeing 747238B · Fuselage Main, Longeron/StringerSDR CALA9700024Skin · delaminatedINSPECTION FOUND LT WING INBOARD MID FLAP PANEL NR 577KT SKIN DELAMINATED. A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-06, FIGURE 15.Nov 5, 1996 · N17025 · Boeing 747238B · Trailing Edge FlapsSDR CALA9700014Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FRAME AT MAIN DECK BS 360, LT SIDE, BETWEEN STRINGER 15 AND 16. THE FRAME WAS REPAIRED IAW ECRA 5310-03376.Nov 4, 1996 · N17025 · Boeing 747238B · Fuselage Main, FrameSDR CALA9700012Frame · crackedINSPECTION FOUND A .75 INCH CRACK IN FRAME AT BS 360 ON RT SIDE, STRINGER 14E. THE FRAME WAS REPAIRED IAW ECRA 5310-03375.Nov 4, 1996 · N17025 · Boeing 747238B · Fuselage Main, FrameSDR CALA9700025Fitting · corrodedINSPECTION FOUND LT AND RT WING TO BODY KICK FITTINGS CORRODED. THE BODY KICK FITTINGS WERE REPAIRED IAW ECRA 5340-01283.Nov 1, 1996 · N17025 · Boeing 747238B · Wing, Fuselage Attach FittingsSDR CALA9700021Spar Web · crackedINSPECTION FOUND A .1875 INCH CRACK AT FASTENER HOLE OF NR 2 PYLON WING FRONT SPAR VERTICAL WEB AT INBOARD NACELLE RIB POST ATTACH AREA, WS 688. THE FRONT SPAR VERTICAL WEB WAS REPAIRED PER BOEING DRAWING 112U8040, FCD 5710-01758 AND SRM 51-10-01.Nov 1, 1996 · N17025 · Boeing 747238B · Wing SparSDR CALA9700004Splice · crackedINSPECTION FOUND STRINGER SPLICE CORRODED WITH A 1.8 INCH CRACK ALONG FLANGE AT BS 1480, STRINGER 1L. THE STRINGER SPLICE WAS REPLACED IAW ECRA 5310-03380.Nov 1, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous StructureSDR CALA9700026Skin · corrodedINSPECTION FOUND CORROSION AT RT WING LOWER SKIN FORWARD OF FRONT SPAR LOWER CHORD AND EXTENDING AFT OF FRONT SPAR BETWEEN WS 1454 AND WS 1548. THE AREA WAS REPAIRED IAW ECRA 5710-01766.Oct 31, 1996 · N17025 · Boeing 747238B · Wing, Plate/SkinSDR CALA9700018Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD SHEAR TIE AT LT WING NR 2 MAIN TANK WS 670, UPPER STRINGER 27 AND A .5 INCH CRACK WAS FOUND AT SHEAR TIE OF RIB CHORD, LOWER STRINGER 19. THE RIB CHORD AT UPPER STRINGER 27 WAS REPAIRED IAW SB 57-2273. THE RIB CHORDOct 28, 1996 · N17025 · Boeing 747238B · Wing, Rib/BulkheadSDR CALA9700013Frame · crackedINSPECTION FOUND A 2 INCH CRACK IN FRAME AT THE OUTBOARD FRAME WEB BETWEEN STRINGER 26R AND 27AR, BS 280. THE FRAME WAS REPAIRED IAW ECRA 5310-03370.Oct 28, 1996 · N17025 · Boeing 747238B · Fuselage Main, FrameSDR CALA9700011Frame · crackedINSPECTION FOUND A .75 INCH CRACK IN FRAME AT BS 380, STRINGER 23R. THE FRAME WAS REPAIRED IAW ECRA 5310-03367.Oct 28, 1996 · N17025 · Boeing 747238B · Fuselage Main, FrameSDR CALA9700023Bulkhead Chord · crackedINSPECTION FOUND A .125 INCH CRACK AT FASTENER HOLE COMMON TO THE AFT BULKHEAD VERTICAL CHORD LT FITTING OF NR 2 PYLON. THE CHORD ASSEMBLY WAS REPLACED IAW BOEING DRAWING 65B90413 AND SRM 51-10-01.Oct 26, 1996 · N17025 · Boeing 747238B · Nacelle/Pylon, Bulkhead/FirewallSDR CALA9700020Bulkhead · crackedINSPECTION FOUND A .125 INCH CRACK AT NR 3 PYLON FASTENER HOLE COMMON TO THE AFT BULKHEAD VERTICAL CHORD LT FITTING. THE NR 3 PYLON LT BULKHEAD ASSEMBLY WAS REPLACED IAW SRM 51-10-01 AND BOEING DRAWING 65B90413.Oct 26, 1996 · N17025 · Boeing 747238B · Nacelle/Pylon, Bulkhead/FirewallSDR CALA9700019Bulkhead · crackedINSPECTION FOUND A 2 INCH CRACK AT UPPER POSITION OF NR 4 PYLON AFT BULKHEAD INBOARD CHORD. THE CHORD AND AFT BULKHEAD ASSEMBLY WERE REPLACED IAW SRM 57-10-01 AND SB 747-54A2159.Oct 26, 1996 · N17025 · Boeing 747238B · Nacelle/Pylon, Bulkhead/Firewall
Back to N17025, cancelled Jul 11, 2003