Douglas DC-9-31

Service difficulty reports · 7,433

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 = 'DC931'
  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 USAA990156Skin · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK ON SKIN AT STATION 965 LONGERON 6R. CUT OUT CRACK. INSTALLED DOUBLER PER SRM 53-04. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA990155Skin · lightning strikePIT - DURING Q-1 CHECK, FOUND .25 INCH DIAMETER LIGHTNING STRIKE IN SKIN BETWEEN STATION 560 AND 579 ABOVE LONGERON 7R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA990154Skin · lightning strikePIT - DURING Q-1 CHECK, FOUND .25 INCH DIAMETER LIGHTNING STRIKE IN SKIN AT STATION 560 LONGERON 7R. DRILLED OUT AND INSTALLED RIVET PER SRM 53-04. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA990153Longeron · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN WEB AT LEFT PYLON LOWER FLANGE STATION 1030. STOP DRILLED AND INSTALLED DOUBLER PER SRM 54-01. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Nacelle/Pylon, Longeron/StringerSDR USAA990152Longeron · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK AT LONGERON 13R STATION 965. REMOVED CRACKED LONGERON SECTION, INSTALLED NEW SECTION WITH SPLICE PER SRM 53-02 FIG 18. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990150Frame · crackedPIT - DURING Q-1 CHECK, FOUND 3 INCH CRACK CANTED BELTFRAME STATION 1074. INSTALLED DOUBLER PER SRM 53-03 FIG 30 AND EA 51559. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Main, FrameSDR USAA990149Skin · crackedPIT - DURING Q-1 CHECK, FOUND .75 INCH CRACK IN FUSELAGE SKIN AT RIGHT SIDE STATION 953 BETWEEN L14 AND L15. INSTALLED TITANIUM FINGER DOUBLER PER EA 51542. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA990148Frame · crackedPIT - DURING Q-1 CHECK, FOUDN 3 INCH CRACK AT CANTED FRAME STATION 1074, LONGERON 6 RT. INSTALLED/FABRICATED 27 DOUBLER, 11 CLIP, 23 DOUBLER. REPETITIVE INSPECTION RED EA NR 51559. TEMP REPAIR PER SRM 53-03 FIG 30. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Main, FrameSDR USAA990147Skin · lightning strikePIT - DRUING Q-1 CHECK, FOUND .25 INCH DIAMETER LIGHTNING STRIKE ON SKIN BETWEEN STATION 560-579, 2 INCHES ABOVE 7R. INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA990146Skin · crackedPIT - DURING Q-1 CHECK, FOUND .5 INCH CRACK ON SKIN AT STATION 965 BELOW 6R. INSTALLED DOUBLER PER SRM 53-04. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR EISA99032Check Valve · dirtyCREW REPORTED LEFT WING FUEL VENTING OUT OF RIGHT WING. LEAK STOPPED WHEN CENTER TANK PUMPS WERE TURNED OFF. TURN BACK TO (ACY). CHECK FUEL SYSTEM PER CROSS FEED AND TRANS TEST ML/M 28-20-00 PAGE 50/2502. OPS CHECK NORMAL AFTER FREEING CENTER TANK PUMP DISFeb 27, 1999 · N945VJ · Doug DC931 · Fuel StorageSDR TWAA9903702Window · damagedDURING OP 16 MAINT CHECK, FOUND STATIC BURNS ON RIGHT SIDE OF AIRCRAFT, CABIN WINDOWS 3, 4, 12, 30, 33 AND 35. BLENDED EACH PER SRM 53-05, FIG 3 AND ARA 16105, AND ALODINED BLEND.Feb 26, 1999 · N987Z · Doug DC931 · Passenger Compartment WindowsSDR EISA99033Gyro · failedAIR TURN BACK BUF, CAPTAIN ADI ERRATIC IN FIGHT AFTER TAKEOFF, BANK AND PITCH BOTH SHOW INCORRECT INDICATIONS. REPLACED CAPTAINS ADI AND VERTICAL GYRO, OPERATIONS CHECK GOOD PER MM 34-00. (M)Feb 26, 1999 · N943VJ · Doug DC931 · Attitude Gyro and Indicating SystemSDR EISA990033Adi · failedCAPTAIN ADI ERRATIC IN FLIGHT AFTER TAKEOFF BANK AND PITCH BOTH SHOW INCORRECT INDICATIONS. AIR TURN BACK BUFFALO. REPLACED CAPTAINS ADI AND VERTICAL GYRO, OPS CHECK GOOD PER MM 34-00. (M)Feb 26, 1999 · N943VJ · Doug DC931 · Integrated Flight SystemSDR USAA990151Floorbeam · crackedPIT - DURING Q-1 CHECK, FOUND 1.5 INCH CRACK IN FLOORBEAM ATTACH ANGLE AND SUBFLOOR CRACKED AT STATION 130 OUTBOARD OF LEFT SEAT TRACK. INSTALLED FLOORBEAM REPAIR PER SRM 53-05 FIG 25. (M)Feb 25, 1999 · N937VJ · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA9903802Bracket · crackedDURING OP 16 MAINT CHECK, FOUND IN NLG WHEEL WELL A CRACK IN THE I/B BRACKET ON THE AFT BULKHEAD FOR HYD SWIVAL GLAND ANTI-ROTATION ARM. REMOVED CRACKED BRACKET AND FABRICATED NEW BRACKET WITH MATERIAL IDENTIFIED ON ORIGINAL BRACKET AND INSTALLED ORIGINAL FASFeb 25, 1999 · N987Z · Doug DC931 · Fuselage Miscellaneous StructureSDR 9900829903Bulkhead · crackedDURING PERIODIC CHECK, FOUND FORWARD SIDE OF AFT PRESSURE BULKHEAD RIGHT SIDE STIFFENER CRACKED ON OUTBOARD END. REPAIRED PER EA 99-163459.Feb 24, 1999 · N953N · Doug DC931 · Fuselage Main, BulkheadSDR TWAA9903804Intercostal · crackedDURING OP 16 MAINT CHECK, FOUND A CRACK IN THE INTERCOSTAL BELOW FLOORBEAM U-CHANNEL AT STA 617. REMOVED AND REPLACED CRACKED INTERCOSTAL PER SPM 6-70-01, PAGE 3, AND USED HI-LOK FASTENERS PER SPM 6-30-07, PAGE 1 AND 2.Feb 23, 1999 · N987Z · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990120Longeron · crackedPIT - DURING C-6 CHECK, FOUND LONGERON CRACKED IN HALF 2 INCHES BY 1 INCH, DISCONTINUITY AT INTERSECTION OF L5R AT STATION 639. DETECTED BY EDDY CURRENT. REPAIRED PER SRM 53-02 FIG 18. (M)Feb 22, 1999 · N932VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990119Longeron · crackedPIT - DURING C-6 CHECK, FOUND 1.5 INCH LONGERON CRACKED IN HALF LONGERON NR 4 AND NR 5 AT STATION 756 LT SIDE. INSTALLED DOUBLER PER SRM 53-02 FIG 18, 119-5572 SPLICE AND 119-5573 LONGERON. (M)Feb 22, 1999 · N932VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9903803Floor · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION AROUND THE RIVETS IN THE CENTER FLOOR PANEL, BETWEEN LAVATORIES. THE EDGE STIFFENERS WERE CRACKED AND WORN. REPLACED PANEL PER SPM 6-70-01.Feb 22, 1999 · N987Z · Doug DC931 · Fuselage Floor PanelSDR TWAA9902802Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON SEAT TRACK, LT I/B AT STA 200 TO 237. INSTALLED NEW TRACK PER SPM 6-80-01. SPLICED PER SRM 53-05, FIG 4F, PG 10G.Feb 21, 1999 · N987Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9902805Frame · crackedDURING OP 15 MAINT CHECK, FOUND CABIN WINDOW FRAME TIE CRACKED IN UPPER FWD CORNER, STA 680 ON RT SIDE. REPLACED WINDOW FRAME PER DOUGLAS PRINT NR 5912285, WITH (P/N 5912285-505).Feb 19, 1999 · N987Z · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9900023Wire · brokenDTW - EMERGENCY FLOORTRACK LIGHTING FROM 20 THE ROW TO AFT CABIN DOOR INOPERATIVE, SIX LIGHTS. REPAIRED BROKEN WIRE. OPERATION CHECK GOOD IAW DC-9 MM 33-53-00. (M)Feb 18, 1999 · N934ML · Doug DC931 · Light System WiringSDR 9900619903Skin · crackedDURING PERIODIC CHECK, FOUND FUSELAGE EXTERIOR SKIN CRACKED AT FASTENERS AT FS 69.5 BETWEEN LONGERONS 14L THRU 17L. REPLACED SKIN PER EA 99-163379.Feb 18, 1999 · N953N · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9902706Deck · crackedDURING OP 16 MAINT CHECK, FOUND UPPER PRESSURE DECK AT APPROXIMATELY STA 47.8 WITH A CRACK ABOUT 4 INCHES LONG. CONFIRMED WITH EDDY CURRENT. REPLACED Y ANGLE PER SPM 6-70-01, DRAWING 9911500, AND SRM 51-60-0, PAGE 27 ITEM E.Feb 16, 1999 · N982PS · Doug DC931 · Fuselage Miscellaneous StructureSDR 9900579963Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE.Feb 16, 1999 · N913RW · Doug DC931 · Emergency LightingSDR 9900539954Frame · crackedDURING PERIODIC CHECK, FOUND CRACKS AT FRAMES -5 AND -7 FS 83. REPAIRED PER EA 99-158010.Feb 16, 1999 · N921RW · Doug DC931 · Fuselage Main, FrameSDR 9900529903Hinge · corrodedDURING PERIODIC CHECK, FOUND HORIZONTAL STABILIZER HINGE FITTING CORRODED LEFT AND RIGHT SIDES. REPAIRED PER EA 99-163778.Feb 16, 1999 · N953N · Doug DC931 · Horizontal Stabilizer StructureSDR USAAD99027Battery · dischargedIND - THE FORWARD ENTRY DOOR, SERVICE DOOR, AND TAILCONE SLIDE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD ENTRY DOOR, SERVICE DOOR, AND TAILCONE SLIDE EMERGENCY LIGHT BATTERIES. (M)Feb 15, 1999 · N933VJ · Doug DC931 · Emergency LightingSDR TWAA9902705Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND IN CABIN THE LT O/B SEAT TRACK WITH CORROSION, STA 200 TO 207. REPAIRED PER SRM 53-05, FIG 4F, SHEET 6. REPLACED TRACK.Feb 15, 1999 · N987Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR 9900569959Power Supply · malfunctionedDURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES. OPERATIONAL CHECK NORMAL.Feb 14, 1999 · N919RW · Doug DC931 · Emergency LightingSDR TWAA9902709Casting · crackedDURING OP 16 MAINT CHECK, FOUND THE FLOOR SUPPORT CASTING CRACKED AT LOWER END, STA 680 LBL 44 IN. REMOVED OLD CASTING AND REPLACED WITH NEW CASTING PER STANDARD PROCESSES MANUAL 67-70-1.Feb 13, 1999 · N987Z · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9900020Bulb · failedLGA - FLT 381 - FIRST RED LIGHT IN GALLEY OF THE EMERGENCY TRACK FLOOR LIGHTING FAILS TO ILLUMINATE. DEFERRED MANTENANCE ITEM NR 591 ON 2/13/99. REPLACED MISSING LAMP ASSEMBLY. OPERATIONAL CHECK GOOD AIW DC9 MM 33-50-00. THIS CLEARS DEFERRED MAINTENANCE ITFeb 13, 1999 · N969ML · Doug DC931 · Emergency LightingSDR EISA99025Battery Pack · dischargedAUXILIARY (FORWARD) OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT FS 629 OVERHEAD. EMERGENCY LIGHTS OPS CHECK GOOD PER MM 33-51-01. (M)Feb 13, 1999 · N943VJ · Doug DC931 · Emergency LightingSDR USAAD99026Battery · dischargedIND - THE RIGHT NACELLE SCAN LIGHT AND THE FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE RIGHT NACELLE SCAN AND FORWARD OVERWING EMERGENCY LIGHTS. (M)Feb 12, 1999 · N928VJ · Doug DC931 · Emergency LightingSDR USAA990118Frame · crackedPIT - DURING Q-4 CHECK, FOUND 1.5 INCH CRACK AT STATION 965 BULKHEAD RT, BELTFRAME BETWEEN LONGERON 16-15. SPLICED IN NEW SECTION OF FRAME PER DACO DRAWING NR 9912243. (M)Feb 12, 1999 · N936VJ · Doug DC931 · Fuselage Main, FrameSDR USAA990117Clip · crackedPIT - DURING Q-4 CHECK, FOUND 2 INCH CRACK AND 1 INCH CRACK ON SKIN CLIP AT STATION 980 BETWEEN LONGERONS 16-14 RT. REPAIRED PER DACO DRAWING 9958238. (M)Feb 12, 1999 · N936VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990116Pan · crackedPIT - DURING Q-4 CHECK, FOUND 3 INCH LONG CRACK AT FORWARD LOWER CORNER PAN SECTION AT HINGE CUTOUT. REPAIRED WITH IDENTICAL PART NR 591412161N PER DACO DWG J060213. (M)Feb 12, 1999 · N936VJ · Doug DC931 · Passenger/Crew DoorsSDR USAA990115Beam · crackedPIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN MAIN ENTRANCE DOOR BEAM NR 6. INSTALLED DOUBLER AND REPAIRED PER EA 51375. (M)Feb 12, 1999 · N936VJ · Doug DC931 · Passenger/Crew DoorsSDR USAA990114Longeron · crackedPIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK AT UPPER AND LOWER HAT SECTION OF LONGERON AT STATION 965 LONGER 16 RT. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIG 18. (M)Feb 12, 1999 · N936VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990113Pan · crackedPIT - DURING Q-4 CHECK, FOUND .375 INCH CRACK AT FORWARD CARGO DOOR OUTER PAN AT LOWER STOP RADIUS FORWARD SIDE. ROUTED CRACK AND INSTALLED TWO 'L' DOUBLERS PER EA 51383. (M)Feb 12, 1999 · N936VJ · Doug DC931 · Cargo/Baggage DoorsSDR USAA990112Bulkhead Frame · crackedPIT - DURING Q-4 CHECK, FOUND 1.5 INCH CRACK AT STATION 965 BULKHEAD BELTFRAME OUTBOARD LONGERONS 16-17 LEFT. SPLICED IN A NEW SECTION OF FRAME PER DACO DRAWING NR 9912243. (M)Feb 12, 1999 · N936VJ · Doug DC931 · Fuselage Main, BulkheadSDR USAA990111Skin · crackedPIT - DURING Q-4 CHECK, FOUND .5625 INCH CRACK IN SKIN AT MED NEAR HANDLE CUTOUT AT STATION 179, Z=33.75. INSTALLED REPAIR DOUBLER PER 51395. (M)Feb 12, 1999 · N936VJ · Doug DC931 · Passenger/Crew DoorsSDR USAA990110Longeron · crackedPIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK, .25 INCH CRACK AND 4 INCH CRACK AT LONGERON 17 BETWEEN STATION 756-775. SPLICED IN NEW SECTION OF SKIN PER EA NR 51416. (M)Feb 12, 1999 · N936VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990109Bulkhead Web · crackedPIT - DURING Q-4 CHECK, FOUND 2 INCH CRACK AT STATION 965 BULKHEAD LEFT WEB. REPLACED WEB PER DACO DRAWING 9912243. (M)Feb 12, 1999 · N936VJ · Doug DC931 · Fuselage Main, BulkheadSDR USAA990108Longeron · crackedPIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN UPPER AND LOWER HAT SECTION OF LONGERON 16 LEFT STATION 965. MANUFACTURED REPAIR PIECES, LONGERON SPLICES PER SRM 53-02 FIG 18. (M)Feb 12, 1999 · N936VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990107Longeron · crackedPIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN UPPER AND LOWER HAT SECTION OF LONGERON 17 LEFT STATION 965. MANUFACTURED REPAIR PIECES, LONGERON SPLICES PER SRM 53-02 FIG 18. (M)Feb 12, 1999 · N936VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990106Longeron · crackedPIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK AT UPPER AND LOWER HAT CHANNEL OF LONGERON AT STATION 965 LONGERON 17 RT. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 18. (M)Feb 12, 1999 · N936VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9902403Power Supply · inopTHE AFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 6-25-98 STL.Feb 12, 1999 · N989Z · Doug DC931 · Emergency Lighting
Back to Douglas DC-9-31