Douglas DC-9-41

Service difficulty reports · 2,671

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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 = 'DC941'
  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 ABXA9701237Trim Tab · delaminatedDURING C-CHECK, FOUND LEFT HAND AILERON TRIM TAB DELAMINATED. *S/D* REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS.Jul 10, 1997 · N956AX · Doug DC941 · Aileron TabsSDR ABXA9701235Fitting · crackedDURING C-CHECK, FOUND THE RT FLOORBEAM TO KEEL ATTACH FITTING FS 775 CRACKED. *S/D* REPLACED FITTING IAW DC9 S/B 53-80.Jul 10, 1997 · N956AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701234Cusp Web · crackedDURING C-CHECK, FOUND THE CUSP WEB CRACKED IN THREE PLACES AT STA 655 RBL 54. *S/D* REPLACED CUSP WEB IAW DC9 SRM 51-30-1.Jul 10, 1997 · N956AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701233Fitting · crackedDURING C-CHECK, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR BOTTOM INTERNAL STIFFENER AND THE FORWARD AND AFT FITTINGS CRACKED. *S/D* REPAIRED IAW DC-9 SRM 52-30-00.Jul 10, 1997 · N956AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA9701232Tab · delaminatedDURING C-CHECK, FOUND THE RIGHT ELEVATOR CONTROL TAB DELAMINATED. *S/D* REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.Jul 10, 1997 · N956AX · Doug DC941 · Elevator, Tab StructureSDR ABXA9701231Control Tab · corrodedDURING C-CHECK, FOUND THE LT ELEVATOR CONTROL TAB UPPER AND LOWER SURFACE CORRODED AT THE L/E SEAM. *S/D* REPAIRED UNIT COMPLETE.Jul 10, 1997 · N956AX · Doug DC941 · Elevator, Tab StructureSDR ABXA9701230Shear Tie · crackedDURING C-CHECK, FOUND A CRACKED SHEAR TIE AT LONG 16L AND STA 1052. *S/D* REPAIRED SHEAR TIE IAW DC9 SRM 51-30-2.Jul 10, 1997 · N956AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701229Frame · crackedDURING C-CHECK, FOUND THE CANTED FRAME AT STA 1244 CRACKED ON RT SIDE 1 FT BELOW THE SPLICE AT THE RUDDER POWER PACK LINE. REPAIRED IAW ABX REA D953-20187MR.Jul 10, 1997 · N956AX · Doug DC941 · Fuselage Main, FrameSDR ABXA9701228Fitting · crackedDURING C-CHECK, FOUND THE RT MAIN LANDING GEAR DOOR ACTUATOR ATTACH FITTING IS CRACKED. *S/D* REPLACED FITTING IAW DC9 SRM 51-30-1.Jul 10, 1997 · N956AX · Doug DC941 · Landing Gear ActuatorSDR ABXA9701385Bracket · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE SLAT CONTROL VALVE PULLEY BRACKET CORRODED AT FS 675. REPLACED SLAT CABLE PULLEY BRACKET AND RIGGED SLAT CONTROL SYSTEM IAW DC-9 MAINTENANCE MANUAL CHAPTER 27-80-2.Jul 9, 1997 · N962AX · Doug DC941 · Leading Edge Slat Control SystemSDR ABXA9701383Jamb · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT MAIN LANDING GEAR DOOR FORWARD JAMB CRACKED AT UPLOCK SWITCH. REPAIRED DOOR JAMB IAW ABX REA D953-20150.Jul 9, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701384Fitting · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT ENGINE PYLON UPPER BEAVERTAIL FITTING CORRODED. REMOVED AND REPLACED LEFT BEAVERTAIL FITTING AND REPAIRED AREA IAW ABX REA D954-20135-MR AND DC-9 SRM CHAPTER 51-30-5.Jul 8, 1997 · N962AX · Doug DC941 · Nacelle/Pylon, Attach FittingsSDR GTIA9700336Prox Sensor · failedDTW - FLT 621 - RIGHT MAIN GEAR RED LIGHT ON RETRACTION. AFTER EXTENDING GEAR, GREEN LIGHT FLASHING ON AND OFF WHILE RED FLASHED OFF AND ON. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK WARNING PROXIMITY SENSOR IAW MM 32-60-1. JACKED AND PERFORMED Jul 7, 1997 · N130NK · Doug DC941 · Landing Gear Position and WarningSDR ABXA9701193Uplock Switch · wornAFTER TAKEOFF, LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED. LANDING WAS UNEVENTFUL. REPLACED LEFT MLG UPLOCK SWITCH, OPS CHECKED GOOD IAW DC9 MM 32-60-0.Jul 2, 1997 · N971AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA9701387Fitting · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT ENGINE PYLON LOWER BEAVERTAIL FITTING CORRODED. REPAIRED LEFT LOWER BEAVERTAIL IAW ABX REA D954-20074 AND DC-9 SRM CHAPTER 53-04, FIGURE 13.Jul 1, 1997 · N962AX · Doug DC941 · Nacelle/Pylon, Attach FittingsSDR ABXA9701386Fitting · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT ENGINE PYLON LOWER BEAVERTAIL FITTING CORRODED. REPAIRED RIGHT PYLON LOWER BEAVERTAIL IAW ABX REA D954-19607-MR.Jul 1, 1997 · N962AX · Doug DC941 · Nacelle/Pylon, Attach FittingsSDR ABXA9701388Bracket · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT LATERAL CONTROL MIXER BRACKET CRACKED AND CORRODED. REPLACED LEFT LATERAL CONTROL MIXER BRACKET IAW DC-9 MAINTENANCE MANUAL CHAPTERS 20-16-0 AND 27-61-4.Jun 27, 1997 · N962AX · Doug DC941 · Aileron Control SystemSDR ABXA9701361Fitting · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT PYLON UPPER BEAVERTAIL EXCESSIVELY CORRODED. REPAIRED RIGHT UPPER BEAVERTAIL IAW ABX REA D954-19607-MR.Jun 27, 1997 · N962AX · Doug DC941 · Nacelle/Pylon StructureSDR ABXA9701177Prox Box · dirtyLT MAIN LANDING GEAR UNSAFE (RED) LIGHT ILLUMINATED WHEN GEAR LOWERED FOR LANDING. ABNORMAL PROCEDURES FOLLOWED. RECYCLED GEAR, NO CHANGE. LANDING WAS UNEVENTFUL. CLEANED PINS AND REMOVED MOISTURE FROM PROXIMITY BOX.Jun 25, 1997 · N952AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA9701389Rib · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT WING NR 2 SLAT TRACK INBOARD RIB CRACKED AT AFT LOWER FLANGE. REPLACED NR 2 RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Jun 24, 1997 · N962AX · Doug DC941 · Wing, Rib/BulkheadSDR ABXA9701164Battery · dischargedEMERGENCY LIGHTS WENT DIM, THEN OUT. REPLACED BATTERY, OPS CHECKED GOOD IAW DC9 MM.Jun 24, 1997 · N968AX · Doug DC941 · Emergency LightingSDR ABXA9701376Skin · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND TWO FUSELAGE SKIN CRACKS AT RIVETS AT FS58 ON LEFT HAND SIDE. REPAIRED IAW DC-9 SRM CHAPTER 53-01.Jun 23, 1997 · N962AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA9701163Battery · dischargedEMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED EMERGENCY BATTERY, OPS CHECKED GOOD IAW DC9MM 33-53-0.Jun 23, 1997 · N968AX · Doug DC941 · Emergency LightingSDR ABXA9701391Rib · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT WING LEADING EDGE RIB AT STATION XIS 136 CORRODED. REPLACED WING LEADING EDGE RIB AT XIS 136 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Jun 19, 1997 · N962AX · Doug DC941 · Wing, Rib/BulkheadSDR ABXA9701157Uplimit Switch · worn hardwareRIGHT GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKE OFF AND DURING FLIGHT. GEAR UPLATCH CHECKED GOOD. REPLACED WORN HARDWARE ON RIGHT MAIN LANDING GEAR UP-LIMIT SWITCH. PERFORMED ADJUSTMENT AND TEST IAW DC9 MM 32-60-00. OPS CHECKED GOOD.Jun 19, 1997 · N964AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA9701390Bulkhead Jamb · crackedWHILE COMPLYING WITH VISUAL INSPECTION OF THE AFT PRESSURE BULKHEAD IAW AD 85-01-02 PER SB 53-137, FOUND THE BULKHEAD DOOR JAMB CRACKED JUST BELOW THE UPPER LEFT CORNER OF DOOR CUTOUT. REPLACED CRACKED DOUBLER IAW DC-9 SRM CHAPTER 51-30-5.Jun 18, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701382Jamb · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT VENTRAL DOOR JAMB FRAME CORRODED FROM FS 1133 TO FS 1163. REPLACED THE UPPER JAMB CAP AND DOOR STOP FITTINGS IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Jun 17, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701381Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 9 LEFT. REMOVED AND REPLACED CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 17, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701379Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 9 RIGHT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1.Jun 16, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701378Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 7R. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 16, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701364Former · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND A FRAME FITTING CRACKED AT FS 675 JUST INBOARD OF LEFT CANTED KEEL. REPAIRED FRAME FITTING IAW DC-9 SRM CHAPTER 53-03, FIGURE 12.Jun 16, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701380Slat · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE NR 1 LEFT SLAT CORRODED AT CENTER ATTACH FITTING. REPLACED NR 1 LEFT SLAT IAW DC-9 MAINTENANCE MANUAL, CHAPTER 27-80-1.Jun 13, 1997 · N962AX · Doug DC941 · Leading Edge DevicesSDR ABXA9701360Keelbeam · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE KEEL BEAM HAD EXCESSIVE CORROSION BLENDOUTS AT FS665.0. REPAIRED KEEL BEAM IAW ABX REA D953-19727-MR.Jun 13, 1997 · N962AX · Doug DC941 · Fuselage Main, KeelSDR ABXA9701141Battery Pack · corrodedEMERGENCY LIGHTS IN AFT OVERHEAD WEAK. CLEANED CORROSION FROM BATTERY PACK CONTACTS, OPS CHECKED GOOD.Jun 13, 1997 · N981AX · Doug DC941 · Emergency LightingSDR ABXA9701377Bulkhead Skin · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB CRACKED ON RIGHT SIDE. REPAIRED DOOR JAMB IAW DC-9 SRM CHAPTER 53-05.Jun 12, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701374Bracket · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LOWER RUDDER HINGE BRACKET CORRODED. REPLACED HINGE BRACKET IAW DC-9 MM 20-16-0.Jun 12, 1997 · N962AX · Doug DC941 · Vertical StabilizerSDR ABXA9701373Former · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND A FORMER CRACKED AT FS660 IN RIGHT CANTED KEEL AREA. REPLACED FORMER AND CLIP IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Jun 12, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701370Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 12 RIGHT. REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 10, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701369Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 14 RIGHT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 10, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701368Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 14 LEFT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 10, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701367Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 15 LEFT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 10, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701359Support · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT NOSE LANDING GEAR DOOR FORWARD FUSELAGE MOUNTED HINGE INTERIOR FITTING HAD EXFOLIATED CORROSION. REPLACED FITTING IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 10, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701139Vane · delaminatedDURING C-CHECK, FOUND THE LEFT FLAP CENTER FIXED VANE DELAMINATED OUT OF LIMITS AT THE LEADING EDGE. *S/D* REPLACED ALL HONEYCOMB CORE DOUBLERS AND SKIN.Jun 10, 1997 · N955AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9701138Fitting · crackedDURING C-CHECK, FOUND THE LT WING INBOARD SPOILER TORSION BAR SUPPORT FITTING IS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5.Jun 10, 1997 · N955AX · Doug DC941 · SpoilersSDR ABXA9701137Skin · delaminatedDURING C-CHECK, FOUND THE LT WING LOWER SURFACE OF TRAILING EDGE PANEL FORWARD OF LT MLG DELAMINATED BEYOND LIMITS. REMOVED AND REPLACED BONDED PANEL (T/E) IAW DC-9 SRM 51-30-1.Jun 10, 1997 · N955AX · Doug DC941 · Wing, Plate/SkinSDR ABXA9701136Spoiler · dentedDURING C-CHECK, FOUND THE RIGHT WING INBOARD SPOILER DENTED IN NUMEROUS PLACES ON UPPER SURFACE. *S/D* REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.Jun 10, 1997 · N955AX · Doug DC941 · SpoilersSDR ABXA9701134Connector · bentDURING CLIMB, GEAR DOOR LIGHT REMAINED ON WITH GEAR RETRACTED. RECYCLED GEAR WITH NO CHANGE. FOUND CONNECTOR P1-1154 WITH BENT PIN C. STRAIGHTENED PIN AND REINSTALLED CONNECTOR, OPS CHECKED IAW DC9 MM 32-00.Jun 10, 1997 · N956AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA9701371Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 15 RIGHT. REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 9, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR GTIA9700308Oil Filter Light · illuminatedMYR - FLT 566 - LEFT OIL STRAINER CLOGGING LIGHT CAME ON AFTER START. INSPECTED ENGINE OIL STRAINER FOR CONTAMINATION, NONE FOUND. INSPECTED ELECTRICAL CONNECT AT PRESSURE DIFFERENTIAL SWITCH, RE-SEATED. LIGHT OUT. PERFORMED ENGINE RUN, OIL STRAINER LIGHT Jun 6, 1997 · N131NK · Doug DC941 · Engine Oil Indicating SystemSDR ABXA9701114Press Panel · corrodedDURING C-CHECK, FOUND THE LOWER SURFACE OF THE LEFT MLG WHELL WELL PRESSURE PANEL CORRODED AT STA 758 AND LBL 32. REPAIRED PRESSURE PANEL IAW DC9 SRM 53-04.Jun 6, 1997 · N955AX · Doug DC941 · Fuselage Miscellaneous Structure
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