Boeing 757-224

Service difficulty reports · 3,824

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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 aircraft_model_key = '757224'
  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 CALA9901121Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 377, RBL 59-61.5. THE FLOORBEAM UPPER CHORD WAS REPAIRED IAW SRM 53-10-51 AND ECRA 5321-01060.Sep 1, 1999 · N18112 · Boeing 757224 · Fuselage Main, Floor BeamSDR CALA9901110Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 324, RBL 40.75. THE INTERCOSTAL WAS REPAIRED IAW ECRA 5321-01059.Aug 31, 1999 · N18112 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA9901109Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 680 - 700, RBL 56. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-51, ECRA 5321-01061, AND BOEING DRAWING 143N5845.Aug 31, 1999 · N18112 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA9900962Chord · chafedINSPECTION FOUND LT WING/FUSELAGE CHORD CHAFED BY UNDER CARRIAGE BEAM REAR SPAR AT STA 720, WBL 70.5. THE CHORD WAS REPLACED IAW BOEING DRAWING 149N7222.Aug 4, 1999 · N13110 · Boeing 757224 · Wing Miscellaneous StructureSDR CALA9900961Skin · splitINSPECTION FOUND RT AILERON COMPOSITE PLIES SPLIT AT HINGE POINT I/B OF ACTUATOR ATTACHMENT LOWER SURFACE. THE AILERON WAS REMOVED, REPAIRED, AND REFITTED IAW SRM 51-70-17, ECRA 5751-01022, AND MM 27-11-21.Aug 4, 1999 · N13110 · Boeing 757224 · AileronsSDR CALA9900960Chord · chafedINSPECTION FOUND RT WING/FUSELAGE CHORD CHAFED AT STA 730, WBL 70.5 BY U/C BEAM REAR SPAR. THE CHORD SECTION WAS REPLACED IAW BOEING DRAWING 149N7222 AND SRM 51-50-02.Aug 4, 1999 · N13110 · Boeing 757224 · Wing Miscellaneous StructureSDR CALA9900959Beam · damagedINSPECTION FOUND IMPACT DAMAGE TO FORWARD CARGO DOOR AFT CORNER AND EDGE BEAM. THE DOOR AFT CORNER AND EDGE BEAM WERE REPLACED IAW BOEING DRAWING 143N6618, 143N6621, AND SRM 51-40-02.Aug 4, 1999 · N13110 · Boeing 757224 · Cargo/Baggage DoorsSDR CALA9900946Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1880 BETWEEN STRINGER 3 AND 4L. REPAIRED IAW ECRA 5331-01062.Aug 3, 1999 · N13110 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA9900935Skin · dentedINSPECTION FOUND LEFT LOWER FUSELAGE SKIN DENTED AT STA 1617, STRINGER 25-26L. REPAIRED IAW ECRA 5331-1061.Aug 2, 1999 · N13110 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA9900934Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 610, STRINGER 16-17L. THE SKIN WAS REPAIRED IAW ECRA 5331-01060.Aug 2, 1999 · N13110 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA9900971Support · corrodedINSPECTION FOUND THE L-4 DOOR SILL SUPPORT CORRODED BETWEEN STA 1661 AND 1680. THE DOOR SILL SUPPORT WAS REPLACED IAW BOEING DRAWING 146N8722.Jul 27, 1999 · N13110 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA9900821Wire · chafedINSPECTION FOUND GENERATOR FEEDER CABLE CHAFED AGAINST ADJACENT CLAMP AT NR 2 ENGINE PYLON AT WING LEADING EDGE. THE CHAFING CAUSED CONTACT OF WIRE CONDUCTOR TO AIRCRAFT FRAME WITH ARCING DAMAGE TO FEEDER CABLE, CLAMP, AND ATTACH HARDWARE. THE FEEDER WIRE, CJul 7, 1999 · N13110 · Boeing 757224 · Electrical Power System WiringSDR CALA9900786Door · damagedINSPECTION FOUND IMPACT DAMAGE TO RT MLG FIXED DOOR. REPAIRED IAW SRM 52-80-02.Jul 2, 1999 · N14107 · Boeing 757224 · Landing Gear DoorsSDR CALA9900762Bearing · failedSMOKE APPEARED IN THE CABIN WITH THE RT OIL FILTER LIGHT ILLUMINATING WHILE EN ROUTE FROM EWR TO LAX. THE AIRCRAFT WAS DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND METAL IN THE NR 2 ENGINE OIL FILTER. THE NR 2 ENGINE WAS REMOVED AND RJul 2, 1999 · N19136 · Boeing 757224 · Engine (Turbine/Turboprop)SDR CALA9900765Skin · dentedINSPECTION FOUND FUSELAGE DENTED AT STA 400-420, STRINGER 16L. THE DENTED AREA WAS REPAIRED IAW SRM 53-00-01 AND ECRA 5331-01057.Jul 1, 1999 · N14107 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA9900738Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN RIGHT O/B TRAILING EDGE FLAP BY NR 10 SPOILER. THE FLAP WAS REPAIRED IAW ECRA 5731-01015.Jun 28, 1999 · N14107 · Boeing 757224 · Trailing Edge FlapsSDR CALA9900737Skin · crackedINSPECTION FOUND A 1.5 INCH CRACK IN AFT CARGO DOOR SKIN. REPAIRED IAW ECRA 5231-01015.Jun 28, 1999 · N14107 · Boeing 757224 · Cargo/Baggage DoorsSDR CALA9900732Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN LEFT O/B TRAILING EDGE FLAP BY NR 3 SPOILER. THE FLAP WAS REPAIRED IAW ECRA 5731-01015.Jun 28, 1999 · N14107 · Boeing 757224 · Trailing Edge FlapsSDR CALA9900718Fuse · blownINSPECTION FOUND THE EMERGENCY EXIT SIGN OVER L-2 DOOR INOPERATIVE. MAINTENANCE REPLACED A BLOWN FUSE IN THE BATTERY PACK AND OPERATION CHECKED GOOD.Jun 24, 1999 · N21108 · Boeing 757224 · Emergency LightingSDR CALA9900663Light · inoperativeTHE EMERGENCY PATH LIGHTING ON SEATS 11, 32, AND 34 WERE FOUND INOPERATIVE. THE MODULE AT SEAT 11 WAS TIGHTENED. THE CONNECTOR AT ROW 34 WAS RECONNECTED. THE LIGHT FIXTURE AT ROW 32 WAS REMOVED AND REPLACED. OPERATION OF THE EMERGENCY PATH LIGHTING CHECKEDJun 10, 1999 · N17105 · Boeing 757224 · Emergency LightingSDR CALA9900655Stringer · crackedINSPECTION FOUND A CRACK IN STRINGER 22L AT STA 1610-1640. A STRINGER SPLICE REPAIR WAS PERFORMED IAW SRM 53-00-03 AND ECRA 5331-01055.Jun 7, 1999 · N57111 · Boeing 757224 · Fuselage Main, Longeron/StringerSDR CALA9900659Floorbeam · corrodedINSPECTION FOUND TOP CHORD OF FLOORBEAM CORRODED AT STA 324, RBL 42. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, PAGES 216-219 AND ECRA 5321-01049.Jun 4, 1999 · N57111 · Boeing 757224 · Fuselage Main, Floor BeamSDR CALA9900494Skin · crackedAFT CARGO DOOR FORWARD CORNER SKIN (LOWER) IS CRACKED (1). REPAIRED PER SRM 5230-01464.May 7, 1999 · N12109 · Boeing 757224 · Cargo/Baggage DoorsSDR CAL9900495Skin · corrodedAFT CARGO DOOR AFT LOWER CORNER SKIN HAS DAMAGE BEYOND SRM LIMITS. REPAIRED AFT CARGO DOOR AFT LOWER SKIN PER EC/RA 5230-01464.May 7, 1999 · N12109 · Boeing 757224 · Cargo/Baggage DoorsSDR CALA9900489Frame · dentedAFT CARGO DOOR AFT CORNER IS DAMAGED BEYOND LIMITS. DAMAGED CORNER REMOVED, NEW CORNER FITTED PER SRM 52-00-00.May 6, 1999 · N12109 · Boeing 757224 · Cargo/Baggage DoorsSDR CALA9900488Frame · dentedAFT CARGO DOOR FORWARD CORNER IS DENTED AND BEYOND SRM LIMITS. DAMAGED CORNER REMOVED, NEW CORNER FITTED PER SRM 52-00-00.May 6, 1999 · N12109 · Boeing 757224 · Cargo/Baggage DoorsSDR CALA9900450Structure · corrodedM LAVATORY AFT ATTACHMENT POINTS CORRODED. REPLACED AFT ATTACH POINTS PER SRM 51-40-01.Apr 28, 1999 · N12109 · Boeing 757224 · Fuselage Main, StructureSDR CALA9900449Structure · corrodedA LAVATORY ANCHOR POINT AT STA 353 LBL 20 CORRODED. REPLACED ANCHOR POINT PER SRM 51-10-00.Apr 28, 1999 · N12109 · Boeing 757224 · Fuselage Main, StructureSDR CALA9900448Structure · corrodedK LAVTORY AFT ATTACHMENT POINTS CORRODED. REPLACED BOTH AFT ATTACH POINTS PER SRM 51-40-01.Apr 28, 1999 · N12109 · Boeing 757224 · Fuselage Main, StructureSDR CALA9900447Intercostal · corrodedINTERCOSTAL CORRODED STATION 324 - 345 RBL 40 BETWEEN FLOORBEAMS. CORRODED INTERCOSTAL REPLACED PER DRAWING NUMBER 141N5170.Apr 28, 1999 · N12109 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA9900444Spring · wornR2 DOOR SLIDE RETAINING PIN STRING WORN. REPLACED SLIDE PACK RETAINING STRING PER AIR CRUISERS COMPANY SLIDE FOLDING PROCEDURE MM P-11883.Apr 26, 1999 · N17104 · Boeing 757224 · Emergency EquipmentSDR CALA9900405Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 600 BETWEEN STRINGERS 18L AND 19L. THE SKIN WAS REPAIRED IAW ECRA 5331-01051.Apr 14, 1999 · N17105 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA9900402Channel · crackedINSPECTION FOUND A .25 INCH CRACK IN RT MLG WHEEL WELL FORWARD SEAL RETAINER SUPPORT CHANNEL. THE SEAL RETAINER SUPPORT CHANNEL WAS REPAIRED IAW SRM 51-70-11.Apr 13, 1999 · N17105 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA9900395Panel · delaminatedINSPECTION FOUND RT WING INBOARD L/E PANEL NR 611HB DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-70-08 AND 51-41-01.Apr 13, 1999 · N17105 · Boeing 757224 · Wing, Plate/SkinSDR CALA9900394Panel · delaminatedINSPECTION FOUND LT WING PANEL NR 551BB DELAMINATED. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-70-05 AND 57-51-01.Apr 13, 1999 · N17105 · Boeing 757224 · Wing, Plate/SkinSDR CALA9900393Chord · crackedINSPECTION FOUND A 1 INCH CRACK IN LT MLG WHEEL WELL CHORD AT STA 1147. THE CHORD WAS REPLACED IAW BOEING DRAWING 149N7222.Apr 13, 1999 · N17105 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA9900392Panel · delaminatedINSPECTION FOUND LT WING LEADING EDGE PANEL NR 511DB DELAMINATED AT ATTACHMENT HOLES. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-70-04 AND MM 51-40-02.Apr 13, 1999 · N17105 · Boeing 757224 · Wing, Plate/SkinSDR CALA9900391Panel · delaminatedINSPECTION FOUND RT FIXED L/E PANEL DELAMINATED OUTBOARD OF PYLON AT WS 370. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-70-08 AND MM 51-40-02.Apr 13, 1999 · N17105 · Boeing 757224 · Wing, Plate/SkinSDR CALA9900390Panel · delaminatedINSPECTION FOUND LT FIXED L/E PANEL DELAMINATED OUTBOARD OF PYLON AT WS 320. THE PANEL WAS REMOVED, REPAIRED AND REINSTALLED IAW SRM 51-70-08 AND MM 51-40-02.Apr 13, 1999 · N17105 · Boeing 757224 · Wing, Plate/SkinSDR CALA9900383Skin · delaminatedINSPECTION FOUND LT FIXED LEADING EDGE PANEL DELAMINATED AT WS 590 BETWEEN SLATS NR 1 AND 2. THE L/E PANEL WAS REPAIRED IAW SRM 51-70-07.Apr 12, 1999 · N17105 · Boeing 757224 · Wing, Plate/SkinSDR CALA9900382Skin · gougedINSPECTION FOUND FUSELAGE SKIN GOUGED BETWEEN STA 620 AND 640 AT S16L AND S17L. AN EXTERNAL DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 204. A DIP WAS ISSUED TO INSPECT BLIND RIVETS EVERY 2500 FLIGHT CYCLES AND TO REPLACE THE REPAIR NO LATER THAN 1Apr 10, 1999 · N17105 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA9900381Skin · delaminatedINSPECTION FOUND THE LT FIXED LEADING EDGE PANEL DELAMINATED AT WS 397. THE L/E PANEL WAS REPAIRED IAW SRM 51-70-07.Apr 10, 1999 · N17105 · Boeing 757224 · Wing, Plate/SkinSDR CALA9900380Skin · gougedINSPECTION FOUND THE RT WING OUTBOARD FLAP INBOARD UPPER PANEL GOUGED BY SPOILER FITTING BOLTS. THE FLAP UPPER PANEL WAS REPAIRED IAW SRM 51-70-10, PAGE 10 AND ECRA 5753-01062.Apr 10, 1999 · N17105 · Boeing 757224 · Trailing Edge FlapsSDR CALA9900379Skin · gougedINSPECTION FOUND LT WING OUTBOARD FLAP INBOARD UPPER PANEL GOUGED BY SPOILER FITTING BOLTS. THE FLAP UPPER PANEL WAS REPAIRED IAW SRM 51-70-10, PAGE 10 AND ECRA 5753-01062.Apr 10, 1999 · N17105 · Boeing 757224 · Trailing Edge FlapsSDR CALA9900376Skin · crackedA PERMANENT FLUSH REPAIR TO FUSELAGE SKIN AT STA 595, BETWEEN S17L AND S16L WAS INSTALLED IAW ECRA 5331-01050. THE AREA HAD PREVIOUSLY BEEN REPAIRED FOR A .375 CRACK AND HAD BEEN PLACED ON DIP.Apr 9, 1999 · N17105 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA9900361Battery Pack · dischargedINSPECTION FOUND MID CABIN (ROW 28) EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK AND CHARGER WERE REMOVED AND REPLACED IAW MM 33-51-07.Apr 6, 1999 · N21108 · Boeing 757224 · Emergency LightingSDR CALA9900358Skin · damagedINSPECTION FOUND IMPACT DAMAGE TO FUSELAGE SKIN PANEL AT STA 780, STRINGER 15L. A FLUSH REPAIR WAS INSTALLED IAW SRM 53-00-01.Apr 5, 1999 · N17105 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA9900344Beam · damagedINSPECTION FOUND IMPACT DAMAGE TO AFT VERTICAL EDGE BEAM, LOWER BEAM, AFT AND FORWARD CORNER PIECES OF FORWARD CARGO DOOR. THE BEAMS AND CORNER PIECES WERE REPLACED IAW BOEING DRAWING 143N6603 AND SRM 52-3-02.Mar 31, 1999 · N17105 · Boeing 757224 · Cargo/Baggage DoorsSDR CALA9900343Beam · damagedINSPECTION FOUND IMPACT DAMAGE TO AFT CARGO DOOR LOWER EDGE BEAM AND FORWARD CORNER PIECE. THE LOWER EDGE BEAM AND FORWARD CORNER PIECE WERE REPLACED IAW BOEING DRAWING 143N6603 AND SRM 52-30-02.Mar 31, 1999 · N17105 · Boeing 757224 · Cargo/Baggage DoorsSDR CALA9900339Angle · corrodedINSPECTION FOUND AFT HOLD THRESHOLD ATTACHMENT ANGLE CORRODED AT BS 1376.5 TO 1443.5. THE ATTACHMENT ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 53-60-53.Mar 30, 1999 · N17105 · Boeing 757224 · Fuselage Miscellaneous Structure
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