Douglas DC-9-31

Service difficulty reports · 7,433

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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 = 'DC931'
  ORDER BY difficulty_date DESC"

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SDR ABXA9801055Bulkhead Clip · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD 4TH RADIAL STIFFENER LEFT ATTACH CLIP CRACKED. REPLACED CLIP IAW DC9 SRM 51-30-1 AND 51-30-5.Oct 14, 1998 · N906AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA9801052Angle · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND SHEAR TIE REPAIR DOUBLER CRACKED AT STATION 1059 BELOW LONGERON 15 RIGHT. REPLACED ANGLE IAW DC9 SRM 53-03, AND DOUGLAS DWG 5913596.Oct 14, 1998 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR USAAD98182Door · unlatchedTOL - CAK FLT 7002, AIRCRAFT FAILED TO PRESSURIZE ON LIFT OFF. A SEVERE BUFFETING OCCURRED ON CLIMB-OUT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD CARGO DOOR OPEN. NO DAMAGE WAS NOTED TO THE AIRCRAFT AND Oct 13, 1998 · N978VJ · Doug DC931 · Cargo/Baggage DoorsSDR ABXA9801071Doubler · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND RIGHT WING REAR SPAR DOUBLER CRACKED OUTBOARD OF TRAPEZOIDAL PANEL. REPAIRED IAW ABX REA D957-25132MR.Oct 13, 1998 · N906AX · Doug DC931 · Wing Miscellaneous StructureSDR USAAD98181Indicator · malfunctionedPIT-BNA - FLT 1285 - AFTER TAKEOFF THE CAPT NOTICED THE RIGHT ENGINE OIL TEMP WAS IN THE YELLOW ARCH. POWER WAS REDUCED BUT THE TEMPERATURE CONTINUED TO CLIMB THROUGH THE RED ARCH AND OF SCALE. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE FIELD Oct 12, 1998 · N960VJ · Doug DC931 · Engine Oil TemperatureSDR TWAA9816503Membrane · puncturedDURING OP 16 MAINT CHECK, FOUND MEMBRANE BELOW FLOOR AT STA 947, RBL 50 IN, WAS PUNCTURED. REPAIRED PER SRM 53-01, FIG 2. APPLIED 2 ROWS OF RIVETS ON 0.040 DOUBLER.Oct 12, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9816502Membrane · crackedDURING OP 16 MAINT CHECK, FOUND MEMBRANE BELOW FLOOR AT STA 958, LBL 50 IN, WAS CRACKED. REPAIRED PER SRM 53-01, FIG 2. APPLIED 3 ROWS OF RIVETS ON 0.040 DOUBLER.Oct 12, 1998 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9801058Support · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE RIGHT VERTICAL FLOORBEAM SUPPORT CRACKED AT STATION 541. REPLACED RIGHT FLOORBEAM STRUT IAW DC9 SRM 51-30-2 AND 51-30-5.Oct 12, 1998 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9801051Angle · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE SHEAR TIE ON FRAME AT STATION 1109 CRACKED AT THE RIGHT VERTICAL ATTACH ANGLE. REPLACED ANGLE IAW DC9 SRM 51-30-5.Oct 12, 1998 · N906AX · Doug DC931 · Fuselage Main, FrameSDR ABXA9800913Stiffener · crackedDURING C-CHECK, FOUND VERTICAL STIFFENER CORRODED FORWARD SIDE OF WEB STATION 996 AT LONGERON 29R. REPLACED STIFFENER IAW DC-9 SRM 51-30-5.Oct 12, 1998 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9800912Skin · crackedDURING C-CHECK, EDDY CURRENT INSPECTION INDICATED TOP FUSELAGE SKIN CRACKED 18 RIGHT OF CENTER SPLICE, STATION 76. REPAIRED IAW DC-9 ABX EA 53100075-003-2.Oct 12, 1998 · N946AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA9800911Intercostal · crackedDURING C-CHECK, FOUND INTERCOSTAL AT LBL 50 STATION 718 CRACKED. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-5.Oct 12, 1998 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9800910Stiffener · crackedDURING C-CHECK, FOUND VERTICAL STIFFENER CORRODED FORWARD SIDE OF WEB STATION 996 AT LONGERON 29L. REPLACED STIFFENER IAW DC-9 SRM 51-30-5.Oct 12, 1998 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9800909Fitting · crackedDURING C-CHECK, FOUND JACK PAD FITTING CRACKED AT LONGERON 30 STATION 996. REPLACED FITTING IAW DC-9 SRM 51-30-5.Oct 12, 1998 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9800908Intercostal · crackedDURING C-CHECK, FOUND INTERCOSTAL CRACKED AFT SIDE OF STATION 37 BULKHEAD RBL 12. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 12, 1998 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9800907Jackscrew · corrodedDURING C-CHECK, FOUND HORIZONTAL STABILIZER JACK SCREW THREADS CORRODED AND PITTED. REPLACED JACK SCREW AND NUT ASSEMBLY IAW DC-9 SMM 27-40-1.Oct 12, 1998 · N946AX · Doug DC931 · Stabilizer Control SystemSDR ABXA9800906Fitting · crackedDURING C-CHECK, FOUND VENTRAL DOOR RIGHT LOWER CORNER FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-30-5 AND 51-30-1.Oct 12, 1998 · N946AX · Doug DC931 · Passenger/Crew DoorsSDR ABXA9800902Fitting · crackedDURING C-CHECK, FOUND AFT ENTRY DOOR UPPER BAYONET SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1.Oct 12, 1998 · N946AX · Doug DC931 · Passenger/Crew DoorsSDR ABXA9800901Frame · crackedDURING C CHECK, FOUND AFT ENTRY DOOR LOWER LEFT FRAME CRACKED IN LOWER POCKET. REPLACED FRAME IAW DC9 SRM 51-30-2, 51-30-1, AND 51-30-5.Oct 12, 1998 · N946AX · Doug DC931 · Passenger/Crew DoorsSDR ABXA9800900Fitting · crackedDURING C-CHECK, FOUND RIGHT INBOARD SPOILER TORSION BAR OUTBOARD SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-3 AND 51-30-5.Oct 12, 1998 · N946AX · Doug DC931 · SpoilersSDR ABXA9800899Fitting · crackedDURING C-CHECK, FOUND RIGHT OUTBOARD SPOILER TORSION BAR SUPPORT INBOARD FITTING CRACKED. REPAIRED IAW DC9 SRM 51-30-3 AND 51-30-5.Oct 12, 1998 · N946AX · Doug DC931 · SpoilersSDR ABXA9800898Frame · crackedDURING C-CHECK, FOUND LEFT WHEEL WELL MAIN FRAME STATION 718 CRACKED, EXTENDING INTO THE WEB. REPLACED FRAME IAW DC9 SRM 51-30.Oct 12, 1998 · N946AX · Doug DC931 · Fuselage Main, FrameSDR ABXA9800897Angle · crackedDURING C-CHECK, FOUND RIGHT FLAP OUTBOARD HINGE ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-31-1 AND 51-31-2.Oct 12, 1998 · N946AX · Doug DC931 · Trailing Edge FlapsSDR ABXA9800896Bulkhead Fitting · crackedDURING C-CHECK, FOUND NOSE LANDING GEAR LEFT TUNNEL VERTICAL BULKHEAD FORWARD UPPER INBOARD FITTING AT STATION 69 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-1.Oct 12, 1998 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9800895Membrane · crackedDURING C-CHECK, FOUND SUBFLOOR MEMBRANE CRACKED AT STATION 180 AND RBL 20. REPAIRED SUBFLOOR IAW DC9 SRM 53-01.Oct 12, 1998 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9800894Floorbeam · crackedDURING C-CHECK, FOUND FLOORBEAM AT STATION 996 CRACKED JUST BELOW LONGERON 18R. REPAIRED FLOORBEAM IAW DC9 SRM 51-30-5, 51-30-1 AND ABX SSRM DRAWING K05019.Oct 12, 1998 · N946AX · Doug DC931 · Fuselage Main, Floor BeamSDR ABXA9800893Longeron · crackedDURING C-CHECK, FOUND LONGERON 16L AT STATION 965 CRACKED. REPAIRED LONGERON IAW DC9 SRM 53-02.Oct 12, 1998 · N946AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA9800892Bulkhead · corrodedDURING C-CHECK, FOUND FALSE BULKHEAD, STATION 996 EXFOLIATED JUST ABOVE LONGERON 30. REPAIRED BULKHEAD IAW ABX REA D953-25069.Oct 12, 1998 · N946AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA9800891End Cap · corrodedDURING C-CHECK, FOUND LONGERON 22R END CAP CORRODED AT STATION 996. REPLACED END CAP IAW DC9 SRM 51-30-2 AND 51-30-5.Oct 12, 1998 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR USAAD98178Wire · brokenIAD-BOS - FLT 1682 - DURING CRUISE, THE FELT AN UNCOMMANDED YAW FROM THE RUDDER. THE PROBLEM CONTINUED AFTER COMPLETING THE ABNORMAL PROCEDURES FOR AN UNCOMMANDED YAW. THE AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE WIRE TO POct 10, 1998 · N991VJ · Doug DC931 · Auto Flight System WiringSDR USAAD98177Battery · dischargedIND - THE TAILCONE SLIDE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE TAILCONE EMERGENCY LIGHT BATTERY AND THE BULBS. (M)Oct 10, 1998 · N971VJ · Doug DC931 · Emergency LightingSDR ABXA9801050Frame · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE SHEAR TIE ON FRAME AT STATION 1109 CRACKED AT LEFT VERTICAL ATTACH ANGLE. REPLACED FRAME IAW DC9 SRM 51-30-2.Oct 10, 1998 · N906AX · Doug DC931 · Fuselage Main, FrameSDR ABXA9801072Longeron · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND LONGERON 4 LEFT CRACKED AT STATION 160. REPLACED LONGERON 4L AT STATION 160 IAW DC9 SRM 53-02.Oct 9, 1998 · N906AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR 9810459910Bulkhead · crackedDURING SURVEILLANCE INSPECTION, FOUND CRACK ON UPPER LEFT CORNER OF AFT PRESSURE BULKHEAD VENTRAL DOOR CUTOUT. REPAIRED PER EA 99-160501 (P/N 5910130-9).Oct 9, 1998 · N960N · Doug DC931 · Fuselage Main, BulkheadSDR USAAD98176Control Box · failedPIT - FLT 7900 - DURING MAINTENANCE TEST HOP THE NOSE LANDING GEAR GREEN LIGHT WOULD NOT ILLUMINATED DURING FLIGHT WITH ANY GEAR EXTENSION METHOD, NORMAL OR NON NORMAL. THE NOSE GEAR WAS VERIFIED DOWN AND LOCKED USING THE NOSE GEAR VIEWPORT. THE AIRCRAFT LANOct 7, 1998 · N918VJ · Doug DC931 · Landing Gear Position and WarningSDR USAAD98175Battery · dischargedIND - THE SERVICE DOOR SLIDE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE SERVICE DOOR SLIDE EMERGENCY LIGHT BATTERY. (M)Oct 7, 1998 · N965VJ · Doug DC931 · Emergency LightingSDR USAA980526Beam · corrodedPIT - DURING Q-1 CHECK, FOUND CORROSION ON LAV FLOORBEAM, 6 AREAS, .375 INCH WIDE .035 INCH DEEP AT STATION 980 RT LAV AT HOLD DOWN HOLES. (M)Oct 7, 1998 · N918VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA980486Flange · crackedPIT - DURING Q-1 CHECK, FOUND .375 INCH CRACK AT LEFT DRAG ANGLE AT FOURTH RIVET FROM AFT END ON HORIZONTAL FLANGE. FABRICATED SPLICE AND REPAIRED PER SRM 53-05 FIG 23A - 501 CONFIG. (M)Oct 7, 1998 · N918VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA980485Pan · crackedPIT - DURING Q-1 CHECK, FOUND .25 INCH LONG CRACK AT FORWARD CARGO DOOR PAN RADIUS ADJACENT TO NR 5 DOOR STOP AT BLIND NUT HOLE. INSTALLED DOUBLER PER EA 50572. (M)Oct 7, 1998 · N918VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9816314Longeron · crackedDURING OP 16 MAINT CHECK, FOUND RT LAV STA 980 LONGERON 14R WITH 2 IN CRACK IN FORMER FOOT. REPAIRED PER MO72J14H, DRAWING J060119, AND ARA 15706.Oct 7, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9816313Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LT LAV STA 980 LONGERON 14L WITH 2 IN CRACK IN FORMER FOOT. REPLACED CRACKED FORMER WITH DAC P/N J060119-17 FORMER PER MO72J14 PHASE G, AND ARA 15706.Oct 7, 1998 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9816311Former · crackedDURING OP 16 MAINT CHECK, FOUND STA 996 FORMER RING FOOT CRACKED ABOVE AND BELOW LONGERON 19L. REMOVED AND REPLACED FORMER RING FOOT SECTION WITH NEW SECTION PART A5910163-79 PER SRM 51-31-0, AND TWA STANDARD PROCEDURES.Oct 7, 1998 · N988Z · Doug DC931 · Fuselage Main, FrameSDR 9810769935Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FIRST CLASS SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL.Oct 7, 1998 · N1332U · Doug DC931 · Emergency LightingSDR USAAD98185Power Supply · inoperableDAY - THE RIGHT NACELLE EMERGENCY LIGHT WAS INOPERABLE. MAINTENANCE REPLACED THE RIGHT NACELLE EMERGENCY LIGHT POWER SUPPLY. (X)Oct 6, 1998 · N958VJ · Doug DC931 · Emergency LightingSDR USAAD98174Battery · dischargedPIT - THE LEFT AND RIGHT NACELLE EMERGENCY LIGHTS WERE INOPERABLE. MAINTENANCE REPLACED THE NACELLE LIGHT EMERGENCY LIGHT BATTERY PACKS. (X)Oct 6, 1998 · N958VJ · Doug DC931 · Emergency LightingSDR ABXA9801069Panel · delaminatedWHILE COMPLYING WITH D-INSPECTION, FOUND THE LEFT WING OUTBOARD TRAILING EDGE PANEL DELAMINATED. REPLACED PANEL IAW DC9 SRM.Oct 6, 1998 · N906AX · Doug DC931 · Wing, Plate/SkinSDR TWAA9816103Former · crackedDURING OP 16 MAINT CHECK, FOUND CRACK AT BOTTOM FWD SIDE OF FORMER RING BELOW CABIN FLOOR STA 658 LT. REPAIRED PER SRM 53-03, FIG 16. INSTALLED DOUBLER WITH HI-LOKS AS REQUIRED.Oct 5, 1998 · N988Z · Doug DC931 · Fuselage Main, FrameSDR EISA98245Battery · dischargedGALLEY DOOR EMERGENCY LIGHT ON SLIDE PACK INOP. GENERATED FROM MAINTENANCE REPORT. REMOVED AND REPLACED BATTERY PACK. (M)Oct 4, 1998 · N945VJ · Doug DC931 · Emergency LightingSDR USAAD98169Switch · failedCLT-BNA - FLT 899 - AFTER TAKEOFF, THE CABIN PRESSURE CONTROL FAILED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MANUAL, AUTO CONTROL SWITCH IN THE PEDESTAL. (M)Oct 2, 1998 · N974VJ · Doug DC931 · Cabin Pressure Control SystemSDR TWAA9816312Buklhead Web · crackedDURING OP 16 MAINT CHECK, FOUND AT RT FUSELAGE BULKHEAD WEB AT STA 965.091, PYLON FROM SPAR LOWER CAP, HIGH FREQ EDDY CURRENT INDICATED CRACK IN LOWER OTBD BOLT HOLE. REAMED HOLE SIZE TO .02807 AND ELIMINATED.Oct 1, 1998 · N988Z · Doug DC931 · Fuselage Main, Bulkhead
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