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 ABXA9500763Tab · delaminatedDURING C-CHECK INSPECTION, FOUND LEFT AILERON TRIM TAB DELAMINATED. REPLACED TRIM TAB IAW DC-9 MM 27-10-5.Sep 13, 1995 · N965AX · Doug DC941 · Aileron TabsSDR ABXA9500762Support · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND CRACKED FLOOR SUPPORT ON FRAME 465 AT LONGERON 29R. REPAIRED FLOOR SUPPORT IAW SUPP MM DRAWING NR K05018.Sep 13, 1995 · N965AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500761Tie · damagedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND DAMAGED AREA IN THE RADIUS OF THE SHEAR TIE STA 1056 ABOVE LONGERON 12L. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2.Sep 13, 1995 · N965AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500756Gusset · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LIGHTENING HOLE GUSSET PLATE CRACKED AT FLOORBEAM STA 180. REPLACED GUSSET IAW DC-9 SRM 51-30-5 AND ENGINEERING MEMO 95-01.Sep 12, 1995 · N965AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500759Angle · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND A CRACK IN THE UPPER AND LOWER ATTACH ANGLES ON THE APB STIFFENER AT LONGERON 15R. REPAIRED IAW DC-9 SUPP DRAWING NR K05159.Sep 11, 1995 · N965AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500758Angle · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND A CRACK IN THE ATTACH ANGLE ON APB STIFFENER BETWEEN LONGERONS 15R TO 16R. REPLACED ANGLE IAW DC-9 SUPP SRM DRAWING NR K05159.Sep 11, 1995 · N965AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500757Angle · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND A CRACK IN THE ATTACH ANGLE ON APB STIFFENER, BETWEEN LONGERONS 16L TO 17L. REPAIRED IAW DC-9 SUPP DRAWING NR K05159.Sep 9, 1995 · N965AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500760Angle · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND A CRACK IN THE ATTACH ANGLE ON APB STIFFENER BETWEEN LONGERONS 12L TO 13L. REPLACED ANGLE IAW DC-9 SRM 51-30-5 AND 51-30-2.Sep 8, 1995 · N965AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500685Eel Battery · dischargedDURING PREFLIGHT INSPECTION, FOUND THE FLIGHT COMPARTMENT EMERGENCY LIGHTS VERY DIM. REPLACED THE BATTERIES IN THE SUPPLY PACK IAW DC-9 SUPP MM 33-53-00, OPS CHECKED NORMAL.Sep 5, 1995 · N955AX · Doug DC941 · Emergency LightingSDR ABXA950684Sliding Window · out of adjustDURING POST FLIGHT INSPECTION, FOUND FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. CLEANED TRACK, REPOSITIONED OPERATING ASSEMBLY AT TOP OF WINDOW AND LUBRICATED. OPS CHECKED GOOD IAW DC-9 MM.Aug 31, 1995 · N975AX · Doug DC941 · Flight Compartment WindowsSDR ABXA9500680Wire · looseNOSE GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR, LIGHT WENT OUT. FOUND UPLOCK SENSOR GROUND WIRE LOOSE. SECURED GROUND WIRE, OPS CHECKED PROX SENSORS AND UNSAFE LIGHT IAW DC-9 SUPP MM 32-60-1. DURING GEAR SWING, ALL INDICATIONS OPS Aug 26, 1995 · N957AX · Doug DC941 · Landing Gear System WiringSDR 9513469760Bracket · crackedDURING LINE CHECK, FOUND A CRACK IN THE SHEAR CLIP ANGLE, FS 1114 AT LONGERON 15L. REPAIRED CLIP (P/N 9912246-43) PER EA 97-100866.Aug 26, 1995 · N760NW · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500678Eel Switch · defectiveDURING SERVICE CHECK, FOUND THE EMERGENCY LIGHTS INTERMITTENT IN TEST. REPLACED THE EMERGENCY LIGHT SWITCH AND OPS CHECKED GOOD IAW DC-9 SUPP MM 33-53-00.Aug 24, 1995 · N990AX · Doug DC941 · Emergency LightingSDR ABXA9500671Eel Power Supply · defectiveDURING SERVICE CHECK, EMERGENCY LIGHTS STAYED ON WHEN SWITCH PLACED IN OFF POSITION. REPLACED EMERGENCY EXIT LIGHT SUPPLY IAW DC-9 SUPP MM 33-54-0. OPS CHECKED GOOD.Aug 14, 1995 · N975AX · Doug DC941 · Emergency LightingSDR 9512679755Fuel Control · malfunctionedDURING CLIMB, THE NR 2 ENGINE N1, N2, AND EPR INDICATORS WERE FLUCTUATING. THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL CONTROL ASSEMBLY AND TESTED THE ENGINE. ENGINE PERFORMANCE WAS SATISFACTORY, THE AIRCRAFT RETURNAug 13, 1995 · N755NW · Doug DC941 · Fuel Control/Turbine EnginesSDR 9511859753Controller · malfunctionedLOSS OF AUTO PRESSURIZATION OCCURRED AFTER TAKEOFF. FOUND CABIN PRESSURE AUTO/MANUAL CIRCUIT BREAKER POPPED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RESET CIRCUIT BREAKER. REGAINED CABIN PRESSURIZATION THROUGH MANUAL CONTROL. FLIGHT RETURNED TO DTAug 3, 1995 · N753NW · Doug DC941 · Cabin Pressure ControllerSDR ABXA9500827Fitting · crackedDURING COMPLIANCE OF AD 85-01-03, ASB 27-228, 27-229 AND EAAD 27-3209D, FOUND CRACK INDICATION ON THE RIGHT WING OUTBOARD SPOILER AFT FITTING. REPLACED SPOILER AFT DRIVE LINK IAW DC-9 MM 27-61-1, OPS CHECKED GOOD.Jul 29, 1995 · N968AX · Doug DC941 · SpoilersSDR ABXA9500669Le Skin · dentedDURING C - CHECK INSPECTION, FOUND DENT IN THE LEADING EDGE OF THE NR 3 SLAT ON THE LEFT WING. REPAIRED IAW DC-9 SRM 57-03, FIG. 14A.Jul 26, 1995 · N975AX · Doug DC941 · Leading Edge DevicesSDR ABXA9500664Angle · crackedDURING C - CHECK INSPECTION, FOUND LEFT FLAP ATTACH ANGLE FOR OUTBOARD HINGE CRACKED INSIDE THE FLAP. REPLACED ANGLE IAW DC-9 SRM 51-30-2 AND 51-30-5.Jul 26, 1995 · N975AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9500663Angle · crackedDURING C - CHECK INSPECTION, FOUND LEFT FLAP ATTACH ANGLE FOR OUTBOARD HINGE CRACKED INSIDE THE FLAP. REPLACED ANGLE IAW DC-9 SRM 51-30-2 AND 51-30-5.Jul 26, 1995 · N975AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9500668Le Skin · dentedDURING C - CHECK INSPECTION, FOUND DENT IN LEADING EDGE OF THE NR 1 SLAT ON THE LEFT WING. REPAIRED IAW DC-9 SRM 57-03, FIG. 14A.Jul 25, 1995 · N975AX · Doug DC941 · Leading Edge DevicesSDR ABXA9500667Fitting · crackedDURING C - CHECK INSPECTION, FOUND RIGHT WING SLAT ACTUATING MECHANISM INBOARD ATTACH FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.Jul 25, 1995 · N975AX · Doug DC941 · Leading Edge Slat Control SystemSDR ABXA9500655Skin · damagedDURING AIRCRAFT OUTBASED OPERATION IN OKC, THE FUSELAGE WAS DAMAGED BY THE CREW ENTRANCE STAIRS DURING SEVERE WEATHER. THE DAMAGE TO THE FUSELAGE WAS TEMPORARILY REPAIRED PER ABX REA D953-12257-MR. TEMPORARY REPAIR REPLACED 07-25-95 BY PERMANENT REPAIR IAW ABJul 25, 1995 · N971AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA9500654Skin · damagedDURING SEVERE WEATHER AND VERY HIGH WINDS, THE CREW ENTRANCE STAIRS WERE BLOWN AGAINST THE FUSELAGE PUNCTURING A HOLE IN THE SKIN BELOW THE ENTRANCE DOOR. TEMPORARY REPAIR DONE IAW ABX REA D953-12257-MR.Jul 25, 1995 · N971AX · Doug DC941 · Fuselage Main, Plate/SkinSDR 9511219755Torsion Spring · bentWHILE ON APPROACH FOR LANDING AT MBS, UNABLE TO EXTEND FLAPS FOR LANDING, HANDLE JAMMED IN THE UP POSITION. CONFERRED WITH MAINTENANCE CONTROL, UNABLE TO UNJAM. DECLARED EMERGENCY AND RETURNED TO DTW FOR A NO FLAP LANDING. NO FURTHER INCIDENTS. FOUND FLAP Jul 24, 1995 · N755NW · Doug DC941 · Trailing Edge Flap Control SystemSDR ABXA9500666Bolt · wornDURING C - CHECK INSPECTION AND COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT OUTBOARD MAIN LANDING GEAR DOOR ARM ASSEMBLY HAD EXCESSIVE PLAY. REPLACED BOLT IAW DC-9 OVERHAUL MANUAL 32-10-6.Jul 22, 1995 · N975AX · Doug DC941 · Landing Gear Door Retract SectionSDR ABXA9500665Fitting · wornDURING C - CHECK INSPECTION AND COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT OUTBOARD MAIN LANDING GEAR DOOR LINK ASSEMBLY HAD EXCESSIVE PLAY. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6.Jul 22, 1995 · N975AX · Doug DC941 · Landing Gear DoorsSDR ABXA9500795Door Jamb · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT LOWER CARGO DOOR INTERNAL WEB ON THE DOOR JAMB CORRODED. REPAIRED AFT LOWER CARGO DOOR JAMB WEB IAW ABX REA D953-11804-MR.Jul 18, 1995 · N979AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500794Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND MULTIPLE DAMAGED AND CORRODED AREAS ON THE AFT LOWER CARGO COMPARTMENT DOOR JAMB. REPAIRED DOOR JAMB IAW ABX REA D953-11800-MR.Jul 18, 1995 · N979AX · Doug DC941 · Fuselage Main, Plate/SkinSDR 9510789752Flapper Valve · lack of lubeTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER DEPARTURE. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. FOUND FLAPPER VALVE IN RIGHT HIGH TEMPERATURE SENSOR STUCK CLOSED. LUBED SWITCH, OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.Jul 14, 1995 · N752NW · Doug DC941 · Pneumatic Indicating SystemSDR ABXA9500802Hinge Fitting · wornDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT OUTBOARD FLAP HINGE FITTING BEARING HOLE ELONGATED. REPAIRED IAW ABX REA D927-12127-MR.Jul 12, 1995 · N979AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9500801Window Belt · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT WINDOW BELT AT FS 756 HAD PREVIOUS CORROSION BLEND OUTS THAT WERE BEYOND SRM LIMITS. REPAIRED RIGHT WINDOW BELT SECTION NR 27R IAW ABX REA D953-12047-MR.Jul 11, 1995 · N979AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500746Bearings · wornDURING D - CHECK INSPECTION WHILE COMPLYING WITH A.D. 91-22-07; A.S.B. 32-244, FOUND THE RIGHT OUTBOARD MAIN LANDING GEAR DOOR ACTUATING ROD ASSEMBLY HAD WORN BEARINGS. REPLACED ACTUATING ROD END AND BEARINGS IAW DC-9 M.M., CHAPTER 32-10-6.Jul 11, 1995 · N979AX · Doug DC941 · Landing Gear Door Retract SectionSDR ABXA9500577Sensor · defectiveON FINAL, AFTER NORMAL GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT CAME ON. GREEN NOSE GEAR LIGHT WENT OUT AND GEAR WARNING HORN SOUNDED. RECYCLED GEAR AND GOT NORMAL INDICATIONS. VERIFIED BROKEN WIRE ON NOSE GEAR DOWN LOCK PROXIMITY SENSOR. REPLACED SENSOR IAWJul 11, 1995 · N953AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA9500661Case · crackedDURING COMPLIANCE OF A. D. 87-11-7; A.S.B. 5676, REV. 6, FOUND THE NR 2 ENGINE COMBUSTION CHAMBER OUTER CASE CRACKED AT THE 11 O'CLOCK POSITION. REPLACED NR 2 ENGINE IAW ABX JOB CARD 7001.Jul 2, 1995 · N953AX · Doug DC941 · Turbine Engine Combustion SectionSDR ABXA9500797Le Skin · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A PREVIOUS REPAIR CORRODED AT THE LEADING EDGE OF THE RIGHT ENGINE PYLON. REPAIRED IAW ABX REA D953-11882-MR.Jun 30, 1995 · N979AX · Doug DC941 · Nacelle/Pylon, Plate/SkinSDR ABXA9500817Blkhd Tee · gougedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LOWER T-CAP GOUGED IN TWO PLACES AT LONGERON 30. REPLACED LOWER T-CAP SECTIONS IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Jun 29, 1995 · N979AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9500609Skin · damagedWHILE ACCOMPLISHING A.D. 89-06-04, FOUND THE AFT PRESSURE BULKHEAD CHAFED. REPAIRED IAW ABX REA D953-12012-MR.Jun 29, 1995 · N951AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9500813Seal Depressor · damagedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT FORWARD ENTRY DOOR SEAL DEPRESSOR DAMAGED AT LONGERON 10L. REPLACED SEAL DEPRESSOR IAW DC-9 SRM CHAPTER 51-30-2.Jun 27, 1995 · N979AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500800Jamb · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD ENTRY DOOR JAMB INNER SKIN CRACKED AT LONGERON 11L. REPAIRED ENTRY DOOR JAMB INNER SKIN IAW ABX REA D953-11995-MR.Jun 27, 1995 · N979AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500799Jamb · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT AND RIGHT VENTRAL STAIRWAY JAMBS CRACKED AT EXISTING REPAIRS. REPAIRED VENTRAL STAIRWAY JAMBS IAW ABX REA D953-11964-MR.Jun 23, 1995 · N979AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500790Spar Cap · damagedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A PREVIOUS REPAIR ON THE RIGHT WING REAR SPAR AT WS 164.0. REMOVED REPAIR, INSPECTED AREA IAW ASB 57-146. REPAIRED AREA IAW ABX REA D957-11745-MR.Jun 22, 1995 · N979AX · Doug DC941 · Wing SparSDR ABXA9500826Skin · no edge distantDURING D-CHECK ACCEPTANCE INSPECTION WHILE REPLACING THE RIGHT WINDOW BELT PANEL, FROM FS 541 TO 643, FOUND THE PANEL HAD NO EDGE DISTANCE ON ONE FASTENER IN THE LOWER AFT CORNER. REPAIRED IAW ABX REA D953-11945-MR.Jun 21, 1995 · N979AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA9500653Skin · crackedDURING PRE-FLIGHT INSPECTION, FOUND THE MAIN ENTRY DOOR HAD A ONE INCH CRACK ON THE LOWER FORWARD CORNER AND A DEEP GOUGE FIVE INCHES ABOVE IT. REPAIRED IAW ABX REA D952-11953-MR.Jun 21, 1995 · N970AX · Doug DC941 · Passenger/Crew DoorsSDR 9510009755Strut · deflatedNOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM TUS. FLIGHT CONTINUED TO PHX AND LANDED WITHOUT INCIDENT. EMERGENCY EQUIPMENT WAS CALLED OUT ON STANDBY AS A PRECAUTION. FOUND NOSE STRUT UNDERSERVICED, SERVICED STRUT TO PROPER LEVELS. OPERATIONAL CHEJun 21, 1995 · N755NW · Doug DC941 · Nose/Tail Landing Gear Strut/AxleSDR ABXA9500798Web · damagedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, WHILE REPLACING THE LEFT CUSP WEB AT FS 1041, THE WEB WAS CUT SHORT OF REQUIRED INSTALLATION UNDER THE FRAME FOOT, STA 1041 LEFT SIDE. REPAIRED CUSP WEB IAW ABX REA D953-11947-MR.Jun 20, 1995 · N979AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500562Roller · out of adjustDURING PREFLIGHT INSPECTION, FOUND CAPTAIN'S SLIDING WINDOW WOULD NOT OPEN. FOUND LOWER ROLLER OUT OF TRACK. REALIGNED ROLLER. CAPTAIN'S WINDOW OPS CHECKED GOOD IAW DC-9 M.M.Jun 20, 1995 · N965AX · Doug DC941 · Flight Compartment WindowsSDR 9510989755Longeron · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 30 AT FS 794. REPAIRED LONGERON AND SKIN PER EA 97-98403.Jun 20, 1995 · N755NW · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA9500559Eel Battery · dischargedDURING PREDEPARTURE CHECK, FOUND EMERGENCY LIGHTS DIM. REPLACED NICAD BATTERIES IN EMERGENCY LIGHTS POWER SUPPLY IAW DC-9 SUPP MM 33-50-0. OPS CHECKED GOOD.Jun 19, 1995 · N956AX · Doug DC941 · Emergency LightingSDR ABXA9600358Drain Boss · crackedDURING COMPLIANCE OF AD 87-11-07; PRATT AND WHITNEY ASB 5676, FOUND THE NR 1 ENGINE AFT DRAIN BOSS HAD A CRACK INDICATION. REPLACED THE NR 1 ENGINE IAW ABX J7001 CARD. REPAIRED ENGINE IAW PRATT AND WHITNEY OVERHAUL MANUAL AND ABX GMM, CHAPTER 4.Jun 18, 1995 · N966AX · Doug DC941 · Turbine Engine Combustion Section
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