Douglas DC-9-41
Service difficulty reports · 2,671
Newest first. General aviation reporting is voluntary.
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.
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
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 9624569760Floorbeam · corrodedDURING H-CHECK, FOUND CORROSION IN THE FS 1041 FLOORBEAM CHORD, RIGHT SIDE. REPAIRED CHORD (P/N 9912243-55) PER EA 97-111768.SDR 9624559760Longeron · corrodedDURING H-CHECK, FOUND CORROSION AT LONGERON 30 AT FS 794. REPAIRED LONGERON (P/N 5924878-501) PER EA 97-111762.SDR 9624549760Bulkhead Panel · crackedDURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 108, LEFT AND RIGHT SIDES, AT BOTH THE INBOARD AND OUTBOARD VERTICAL BEAM ATTACH FITTINGS. REPAIRED PANEL (P/N 9910073-313) PER EA 97-111754.SDR ABXA9700323Bulkhead Web · damagedDURING C-CHECK, THE AFT PRESSURE BULKHEAD WEB WAS FOUND DAMAGED AT LONGERON 271LT. REPAIRED IAW REA D953-17185-MR.SDR ABXA9700322Driver Link · crackedDURING C-CHECK, THE RT ENGINE THRUST REVERSER UPPER OUTBOARD DRIVER LINK WAS FOUND CRACKED. REPLACED DRIVER LINK IAW DC-9 M.M. 78-31-5.SDR ABXA9700321Angle · crackedDURING C-CHECK, THE RT PYLON LOWER ATTACH ANGLE WAS FOUND CRACKED AT STA 1056. REPAIRED IAW DC-9 SRM 54-04.SDR ABXA9700320Bulkhead · crackedDURING C-CHECK, THE BULKHEAD AT STA 1041 WAS FOUND CRACKED ON THE RT SIDE AT ENGINE MOUNT SPAR. REPAIRED IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.SDR ABXA9700319Bulkhead · crackedDURING C-CHECK, THE BULKHEAD AT STA 1072 WAS FOUND CRACKED ON THE RT SIDE OF THE DOOR JAMB 24 FROM FLOOR. REPAIRED IAW REA D953-17165MR.SDR ABXA9700318Bulkhead · crackedDURING C-CHECK, THE BULKHEAD AT STA 76 WAS FOUND CRACKED NEXT TO RT CUSP. REPAIRED IAW REA D953-17160.SDR ABXA9700317Frame · crackedDURING C-CHECK, THE STA 1185 FRAME WAS FOUND CRACKED AT LONGERON 3 RT. REPAIRED IAW SSRM DWG NR K05159.SDR ABXA9700316Frame · crackedDURING C-CHECK, THE STA 1185 FRAME WAS FOUND CRACKED AT LONGERON 6RT. REPAIRED IAW SRM DWG NR K051-59.SDR ABXA9700315Frame · crackedDURING C-CHECK, THE STA 1231 FRAME WAS FOUND CRACKED AT LONGERON 2 RT. REPAIRED IAW DC-9 SRM 51-10-2 AND 51-10-5.SDR ABXA9700314Tee Cap · corrodedDURING C-CHECK, THE STA 110 TEE CAP WAS FOUND CORRODED AT LONGERON 25RT. REPAIRED IAW REA D953-17189.SDR ABXA9700311Blkhd Door Jamb · crackedDURING C-CHECK, THE AFT PRESSURE BULKHEAD LT VENTRAL DOOR JAMB CORNER WAS FOUND CRACKED BEYOND A PREVIOUS STOP DRILL. REPAIRED IAW REA D953-17172SB.SDR ABXA9600657Bulb · failedCOCKPIT EMERGENCY LIGHTS, LEFT BULB INOPERATIVE. RELAMPED COCKPIT EMERGENCY LIGHT, LEFT BULB IAW DC-9 M.M. OPS CHECK GOOD.SDR ABXA9600656Bulb · failedEMERGENCY LIGHTING WILL NOT COME ON IN THE ARMED (ON) POSITION. RELAMPED AND REPLACED BATTERIES, OPS CHECK GOOD.SDR 9624219753Press Panel · crackedDURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 83 LEFT AND RIGHT SIDES. REPAIRED PANEL (P/N 9910073-313) PER EA 97-111775.SDR 9623579753Press Panel · crackedDURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR HORIZONTAL PRESSURE PANEL AT FS 108, LEFT AND RIGHT SIDES AT THE INBOARD AND OUTBOARD VERTICAL SUPPORTS. REPAIRED PANEL (P/N 9910073-313) PER EA 97-111757.SDR ABXA9700313Tab · delaminatedDURING C-CHECK, THE LEFT AILERON CONTROL TAB WAS FOUND DELAMINATED. REPLACED AILERON CONTROL TAB IAW DC-9 M.M 27-10-2.SDR ABXA9700312Vane · delaminatedDURING C-CHECK, THE LEFT FLAP OUTBOARD FIXED VANE WAS FOUND DELAMINATED. REPLACED OUTBOARD FIXED VANE IAW DC-9 MM 27-51-3.SDR ABXA9600654Bulb · defectiveFIRST OFFICERS EMERGENCY LIGHTING INOPERATIVE. RELAMPED, OPS CHECKED GOOD PER DC-9 MM 33-10-0.SDR ABXA9700701Angle · crackedDURING ACCEPTANCE INSPECTION FOUND THE LEFT ENGINE PYLON TO FUSELAGE ATTACH ANGLE CRACKED IN TWO PLACES. REPAIRED LEFT PYLON ATTACH ANGLE IAW ABX REA D954-16868-MR.SDR ABXA9700696Bulkhead Clip · crackedDURING ACCEPTANCE INSPECTION FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 16L. REMOVED AND REPLACED END CLIPS AT LONGERON 16L IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR TWAA9613004Light · inoperativeSTL - EMERGENCY ESCAPE PAHT LIGHTING ILLUMINATED DURING FLIGHT. CLEANED MOISTURE FROM LIGHT TRACK, OPERATIONAL CHECK NORMAL. (M)SDR 96NK213AClamp · looseREF MRR NR 96NK213. LOG/ITEM NR 027691/M293. IN-FLIGHT, BOTH SMOKE DETECTORS WENT OFF. FINDINGS: AFTER INSP, TESTS, AND INVESTIGATION OF CAUSE, FOUND PNEUMATIC DUCTING CLAMP CAME LOOSE AND CAUSED INSTALLATION TO SEPARATE AND AIRBORNE DUST ENTERED THE AIR CSDR 96NK213Pack · smokingLOG PAGE NR 028018. ITEM NR P287. AT 18,000 FEET IN DESCENT, BOTH SMOKE DETECTORS WENT OFF. COULD SMELL ELECTRICAL SMOKE (STINKY AND HAZY IN BACK). INSPECTION THE SUSPECT LOCATION OF THE SMOKE-RUNNING RIGHT PACK, BLEW SMOKE FROM PACK. ITEM DEFERRED BY WANESDR 9624529760Floorbeam · corrodedDURING H-CHECK, FOUND CORROSION IN THE FS 1056 FLOORBEAM LEFT SIDE. REPAIRED BEAM (P/N 9958187) PER EA 97-111777.SDR 9622809753Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON THE FRAME ATTACH FITTING AT THE LOWER FORWARD CORNER OF THE GALLEY SERVICE DOOR. REPLACED FITTING PER SRM 51-30-5.SDR ABXA9700711Spar Cap · corrodedDURING ACCEPTANCE INSPECTION, FOUND THE VERTICAL STABILIZER REAR SPAR CAPS CORRODED AT STATIONS ZRS 4, 8 AND 10. REPAIRED VERTICAL STAB REAR SPAR CAPS IAW ABX REA D957-16873-MR.SDR ABXA9700699Angle · crackedDURING ACCEPTANCE INSPECTION, FOUND THE RIGHT ENGINE PYLON UPPER FUSELAGE ATTACH ANGLE CRACKED. REPLACED THE RT UPPER PYLON TO FUSELAGE ATTACH ANGLE IAW DC-9 SRM CHAPTER 51-30-2 AND 51-30-5 AND REPAIRED ONE CRACK IAW ABX REA D954-16695-MR.SDR 9622829754Battery Pack · dischargedDURING LINE CHECK, FOUND LEFT FORWARD AND RIGHT REAR OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS, OPERATIONAL CHECK OK.SDR 9624519760Bulkhead Panel · crackedDURING LINE CHECK, FOUND A 3 INCH CRACK IN THE SLANTED PRESSURE PANEL TO FUSELAGE ATTACH ANGLE APPROXIMATELY LBL 24 ABOVE THE REAR SPAR. REPAIRED ANGLE (P/N 9923419-9) PER EA 97-111746.SDR 9622339755Temp Sensor · malfunctionedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING TAKEOFF. FOLLOWED COM AND LIGHT WENT OUT. FLIGHT RETURNED TO HOU AND LANDED WITHOUT INCIDENT. REPLACED TAIL COMPARTMENT SENSOR AND RIGHT COALESCER BAG. RAN AIRCRAFT TO FULL POWER, OPERATIONAL CHECKSDR ABXA9700712Skin · erodedDURING ACCEPTANCE INSPECTION, FOUND THE LEFT HORIZONTAL STABILIZER LEADING EDGE SKINS ERODED. REPAIRED LEFT HORIZONTAL STAB LEADING EDGE SKINS IAW ABX REA D955-16859-MR.SDR ABXA9700700Angle · crackedDURING ACCEPTANCE INSPECTION, FOUND THE RIGHT ENGINE PYLON UPPER FUSELAGE ATTACH ANGLE CRACKED AT FS 1095. REPAIRED THE RIGHT PYLON UPPER ATTACH ANGLE IAW ABX REA NR D954-16695-MR.SDR ABXA9700695Bulkhead Clip · crackedDURING ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 15L. REPLACED END CLIP AT LONGERON 15L IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR ABXA9700710Keel Beam · corrodedDURING ACCEPTANCE INSPECTION, FOUND THE BUTT LINE O KEEL BEAM UPPER CAP SEVERELY CORRODED AT FS 660. REPAIRED KEEL BEAM UPPER CAP IAW ABX REA D953-16673-MR.SDR ABXA9700713Rib · crackedDURING ACCEPTANCE INSPECTION, FOUND THE OUTBOARD LEFT WING LEADING EDGE RIB AT SLAT TRACK NR 10 CRACKED. REMOVED AND REPLACED LEADING EDGE RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR ABXA9700702Panel · corrodedDURING ACCEPTANCE INSPECTION, FOUND THE RIGHT WING LOWER TRAILING EDGE BONDED PANEL JUST INBOARD OF MLG CORRODED. REPLACED RIGHT WING LOWER INBOARD TRAILING EDGE PANEL IAW DC9 SRM 51-30-1.SDR ABXA9700705Jamb · crackedDURING ACCEPTANCE INSPECTION, FOUND THE RIGHT MLG WHEEL WELL DOOR JAMB CRACKED INBOARD OF HYDRAULIC SUMP JAR. REPAIRED RIGHT MLG DOOR JAMB IAW ABX REA D953-16723.SDR ABXA9700704Panel · delaminatedDURING ACCEPTANCE INSPECTION, FOUND THE RIGHT WING OUTBOARD TRAILING EDGE PANEL FORWARD OF AILERON DELAMINATED AND CORRODED. REPLACED RIGHT WING OUTBOARD TRAILING EDGE PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR ABXA9700703Panel · delaminatedWHILE COMPLYING WITH ACCEPTANCE INSPECTION, FOUND THE RIGHT WING UPPER TRAILING EDGE BONDED PANEL FORWARD OF AILERON DELAMINATED AND CORRODED. REMOVED AND REPLACED RIGHT WING TRAILING EDGE PANEL IAW DC-9 CHAPTERS 51-30-1 AND 51-30-2.SDR ABXA9700884Spoiler · corrodedTHE RIGHT WING OUTBOARD SPOILER HAD SEVERAL AREAS OF CORROSION. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.SDR ABXA9700709Spar Car · corrodedDURING ACCEPTANCE INSPECTION, FOUND THE LEFT WING REAR TEE CAP DOUBLER CORRODED. REPAIRED LEFT WING REAR SPAR CAP IAW ABX REA D957-16504-MR.SDR ABXA9700877Spoiler · corrodedTHE RIGHT OUTBOARD SPOILER HAD WIDESPREAD CORROSION. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN IAW DC-9 SRM.SDR ABXA9700714Rib · crackedDURING ACCEPTANCE INSPECTION, FOUND THE LEFT WING LEADING EDGE RIB AT SLAT TRACK NR 2 CRACKED. REMOVED AND REPLACED RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR ABXA9700708Spar Cap · corrodedDURING ACCEPTANCE INSPECTION, FOUND THE RIGHT WING UPPER SPAR CAPS CORRODED ON THE AFT TANG AT WS XRS 137. REPAIRED IAW ABX REA 957-16496-MR.SDR ABXA9700707Spar Cap · corrodedDURING ACCEPTANCE INSPECTION FOUND THE LEFT WING UPPER SPAR CAPS CORRODED ON THE AFT TANG AT WS XRS 137. REPAIRED IAW ABX REA D957-16496-MR.SDR ABXA9600638Power Supply · defectiveCREW REPORTED, THE EMERGENCY LIGHTS COME ON WHEN FLYING THROUGH TURBULENCE. REPLACED EMERGENCY LIGHT POWER SUPPLY.SDR ABXA9700219Bushings · wornDURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR HAS PLAY AT HINGE. REPLACED RIGHT MAIN LANDING GEAR OUTBOARD DOOR HINGE BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-10. BUSHINGS MANUFACTURED ON SHOP TRAVELER NR 43224.
Back to Douglas DC-9-41