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 ABXA9700819Support · crackedDURING C-CHECK, A FLOOR PANEL SUPPORT AT STA 680 RBL 44 WAS FOUND CRACKED. THE SUPPORT WAS REPLACED IAW DC9 SRM 51-30-5.Jan 22, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR 9701329977Longeron · crackedDURING H-CHECK, FOUND CRACK IN LONGERON 17L AT STA 1019. REPAIRED PER EA 9-112035.Jan 22, 1997 · N9341 · Doug DC931 · Fuselage Main, Longeron/StringerSDR 9701119980Fuel Transfer · malfunctionedFUEL BEGAN VENTING FROM RIGHT WING AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE BACK FLUSHED ALL THREE FUEL SYSTEMS. NO FUEL TRANSFER PROBLEMS WERE ENCOUNTERED.Jan 22, 1997 · N9344 · Doug DC931 · Aircraft Fuel Distribution SystemSDR USAAD97023Battery Pack · failedDAY - LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE BATTERY PACK. (M)Jan 21, 1997 · N922VJ · Doug DC931 · Emergency LightingSDR GTIA9700112Trim Tab · corrodedMHV - LEFT GEARED TAB HAS HONEYCOMB DAMAGE AND DELAMINATION. REPAIRED IAW SRM 55-04 PAGE 3 AND 51-70-2 PAGE 80. (M)Jan 21, 1997 · N928ML · Doug DC931 · Elevator, Tab StructureSDR ABXA9700869Rudder · corroded skinDURING C-CHECK, THE RUDDER SKIN WAS FOUND BULGED IN TWO AREAS AT THE TRAILING EDGE. THE RUDDER WAS REPLACED IAW DC9 MM.Jan 21, 1997 · N906AX · Doug DC931 · Rudder, Plate/SkinSDR ABXA9700868Torque Tube · corrodedDURING C-CHECK, THE RUDDER TORQUE TUBE WAS FOUND CORRODED. THE TORQUE TUBE WAS REPLACED IAW DC9 MM.Jan 21, 1997 · N906AX · Doug DC931 · Rudder Control SystemSDR ABXA9700861Longeron · corrodedDURING C-CHECK, THE LONGERON 27 LT AT STA 585 WAS FOUND CORRODED. THE LONGERON WAS REPLACED IAW DC9 SRM 51-30-2.Jan 21, 1997 · N906AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA9700859Fitting · crackedDURING C-CHECK, THE LONGERON 30 END FITTING AT STA 606 WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-10-5.Jan 21, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9700845Frame · crackedDURING C-CHECK, THE FRAME AT 622 AT THE OUTBOARD END WAS FOUND CRACKED. THE FRAME WAS REPAIRED IAW DC9 SRM 53-03 FIGURE 12.Jan 21, 1997 · N906AX · Doug DC931 · Fuselage Main, FrameSDR ABXA9700823Intercostal · corrodedDURING C-CHECK, AN INTERCOSTAL FROM STA 579 TO 598 LONG 28 LT WAS FOUND CORRODED. THE INTERCOSTAL WAS REPLACED IAW DC9 SRM 51-30-5.Jan 21, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9700820Support · corrodedDURING C-CHECK, A FLOOR PANEL SUPPORT AT STA 541 LONG 28 LT WAS FOUND CORRODED. THE SUPPORT WAS REPLACED IAW DC9 SRM 51-30-5.Jan 21, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR 9701049966Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT EXIT ROW 12 INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.Jan 21, 1997 · N9330 · Doug DC931 · Emergency LightingSDR USAAD97016Strut · req'd serviceFLT 972 - TOL-PIT - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO FIELD. FOUND NOSE STRUT LOW. SERVICED NOSE STRUT PER MM. (M)Jan 20, 1997 · N934VJ · Doug DC931 · Nose/Tail Landing Gear Strut/AxleSDR GTIA9700111Frame · tornMHV - RIGHT SIDE OF COCKPIT AT FUSELAGE STATION 148 55 INCHES ABOVE FLOOR LEVEL INBOARD FLANGE OF FRAME TORN AND MISSING A 1 INCH BY 2.25 INCH SECTION. REMOVED DAMAGED AREA IAW SRM 53-03 FIG 4. FABRICATED DOUBLER AIND INSTALLED PER SRM 51-10-3, 53-03 FIG 4. Jan 20, 1997 · N928ML · Doug DC931 · Fuselage Main, FrameSDR ABXA9700867Bracket · corrodedDURING C-CHECK, THE AILERON BUS PULLEY BRACKET WAS FOUND CORRODED. THE BRACKET WAS REPLACED IAW DC9 MM 20-16-0.Jan 20, 1997 · N906AX · Doug DC931 · Aileron Control SystemSDR ABXA9700847Fitting · crackedDURING C-CHECK, THE LONGERON END FITTING AT STA 608 LONG 28 LT WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-5.Jan 20, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9700115Floor · corrodedMHV - COCKPIT FLOOR RIGHT SIDE, SMALL PAN AREA UNDER GALLEY NR 1 HAS EXFOLIATION CORROSION AT STATION 160. REMOVED DAMAGED AREA, FABRICATED NEW WEB AND INSTALLED PER SRM 53-10-1. (M)Jan 19, 1997 · N928ML · Doug DC931 · Fuselage Floor PanelSDR ABXA9700846Longeron · corrodedDURING C-CHECK, THE LONGERON FROM STA 908 TO 917 LONG 29 LT WAS FOUND CORRODED. THE LONGERON WAS REPLACED IAW DC9 SRM 53-02, FIGURE 2.Jan 19, 1997 · N906AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA9700839Frame · damagedDURING C-CHECK, THE FRAME AT STA 1059 LONGERON 20 RT WAS FOUND DAMAGED. THE FRAME WAS REPLACED IAW DC9 SRM 51-30-2.Jan 19, 1997 · N906AX · Doug DC931 · Fuselage Main, FrameSDR ABXA9700817Fitting · crackedDURING C-CHECK, A FITTING AT STA 606 AT LONG 27 LT WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-1.Jan 19, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR 9701029968Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.Jan 19, 1997 · N9332 · Doug DC931 · Emergency LightingSDR GTIA970125Panel · brokenMHV - LEFT LOWER WING PANEL NR 2114 INTERLOCK STRIP LOWER UNDERSIDE OF PANEL BROKEN. REMOVED DOUBLER, FABRICATED DOUBLER PER SRM 51-10-2. INSTALLED PER SRM 51-10-3, 51-30-2. (M)Jan 18, 1997 · N928ML · Doug DC931 · Wing, Plate/SkinSDR GTIA9700140Panel · brokenMHV - LEFT LOWER WING PANEL NR 2114 INTERLOCK STRIP LOWER UNDERSIDE OF PANEL BROKEN. REMOVED DOUBLER, FABRICATED DOUBLER PER SRM 51-10-2. INSTALLED PER SRM 51-10-3, 51-30-2. (M)Jan 18, 1997 · N928ML · Doug DC931 · Wing, Plate/SkinSDR ABXA9700870Fitting · crackedDURING C-CHECK, THE AILERON CENTER HINGE ATTACH FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 MM 27-10-1.Jan 18, 1997 · N906AX · Doug DC931 · Wing, Control Surface Attach FittingsSDR ABXA9700855Subfloor · corrodedDURING C-CHECK, THE COCKPIT SUBFLOOR, FROM STA 120 TO 160 RBL 22 TO 55, WAS FOUND CORRODED. THE SUBFLOOR WAS REPLACED IAW REA D953-17685-MR.Jan 18, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9700853Web · crackedDURING C-CHECK, THE CUSP WEB AT STA 239 RBL 54 WAS FOUND CRACKED. THE CUSP WEB WAS REPAIRED IAW DC9 SRM 51-30-2.Jan 18, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9700852Web · corrodedDURING C-CHECK, THE CUSP WEB AT STA 230 TO 237 RBL 54 WAS FOUND CORRODED. THE CUSP WEB WAS REPLACED IAW DC9 SRM.Jan 18, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9700818Blkhd Stiffener · crackedDURING C-CHECK, A STIFFENER ON THE FORWARD BULKHEAD OF AFT LOWER CARGO WAS FOUND CRACKED. THE STIFFENER WAS REPLACED IAW DC9 SRM 51-30-5.Jan 18, 1997 · N906AX · Doug DC931 · Fuselage Main, BulkheadSDR 97ZZZM207Switch · frozenFLT 840 - AFT CARGO DOOR LIGHT ON AT TAXI. FOUND SWITCH FROZEN, FREED SWITCH. OPS CHECK GOOD IAW 52-31-0. (M)Jan 18, 1997 · N969ML · Doug DC931 · Door Warning SystemSDR 9701609977Pressure Panel · crackedDURING H-CHECK, FOUND A CRACK IN NOSE WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 83. REPAIRED PER EA 99-112013.Jan 18, 1997 · N9341 · Doug DC931 · Fuselage Miscellaneous StructureSDR 9701189977Pressure Web · crackedDURING PERIODIC CHECK, FOUND PRESSURE PANEL CRACKED ABOVE FITTING AT FS 83 IN NOSE WHEEL WELL. INSTALLED REPAIR DOUBLER PER EA 99-112013.Jan 18, 1997 · N9341 · Doug DC931 · Fuselage Miscellaneous StructureSDR 9701179977Longeron · crackedDURING PERIODIC CHECK, FOUND LONGERON 30 SPLICE JOINT AT FS 551 CRACKED AT BOTH ENDS. REMOVED AND REPLACED SPLICE PER EA 99-112011.Jan 18, 1997 · N9341 · Doug DC931 · Fuselage Main, Longeron/StringerSDR 9701009966Wire · brokenDURING LINE MAINTENANCE INSPECTION, FOUND AFT TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRING BEHIND LIGHT ASSEMBLY, OPERATIONAL CHECK NORMAL.Jan 18, 1997 · N9330 · Doug DC931 · Light System WiringSDR 9700879927Retract Mech · malfunctionedAFTER DEPARTURE, THE LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. PERFORMED COCKPIT OPERATING MANUAL PROCEDURE. GEAR EXTENDED AND FLIGHT RETURNED TO ATL FOR NORMAL LANDING. MAINTENANCE REPLACED THE LEFT UP AND DOWN LOCK SWITCHES, LEFT GEAR RETRACT ACTUATOR,Jan 18, 1997 · N8920E · Doug DC931 · Landing Gear Retraction/Extension SystemSDR USAAD97017Slide · leakingBOS - DURING OPERATIONAL CHECK OF ENTRY DOOR ESCAPE SLIDE, FOUND THAT SLIDE INFLATED PROPERLY, BUT FAILED TO HOLD PRESSURE. SLIDE WAS REPLACED, AND TWO ADDITIONAL SLIDES ARE SCHEDULED TO BE CHECKED. (M)Jan 17, 1997 · N938VJ · Doug DC931 · Escape SlideSDR GTIA970117Stiffener · crackedMHV - LEFT WING TO FUSELAGE FILLET FAIRING STIFFENER IS CRACKED. REMOVED OLD STIFFENER, FABRICATED NEW STIFFENER PER SRM 53-50-0, FABRICATED PATCH PER SRM 55-01 INSTALLED PER SRM 51-30-3. (M)Jan 17, 1997 · N928ML · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9700120Skin · corrodedMHV - RT WING UPPER SKIN TO AFT SPAR END CAP HAS BULGING AND CORROSION EMITTING AT LOWER SURFACE XRS 152. TWO INCH SQUARE AREA APPROXIMATELY. REMOVED CORROSION, TRIM AND BLENDED AREA IAW EA 5730-96-001, PER SRM 51-20-0, 51-30-2, 51-30-8, 57-09 FIG 12. (M)Jan 17, 1997 · N928ML · Doug DC931 · Wing, Plate/SkinSDR ABXA9700865Angle · crackedDURING C-CHECK, THE LOWER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC9 SRM 54-04, FIGURE 10.Jan 17, 1997 · N906AX · Doug DC931 · Nacelle/Pylon StructureSDR ABXA9700863Fitting · crackedDURING C-CHECK, THE FLOOR SUPPORT VERTICAL FITTING AT STA 680 LBL 43 WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-2.Jan 17, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9700860Intercostal · damagedDURING C-CHECK, THE INTERCOSTAL AT STA 392 LONGERON 15 RT WAS FOUND DAMAGED. THE INTERCOSTAL WAS REPAIRED IAW DC9 SRM 53-11-2.Jan 17, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9700854Subfloor · crackedDURING C-CHECK, THE UPPER CARGO SUBFLOOR WAS FOUND CRACKED IN NUMEROUS PLACES. THE SUBFLOOR WAS REPAIRED IAW DC9 SRM 53-01.Jan 17, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9700851Web · crackedDURING C-CHECK, THE CUSP WEB AT STA 237 RBL 54 WAS FOUND DAMAGED. THE CUSP WEB WAS REPLACED IAW DC9 SRM.Jan 17, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9700850Web · crackedDURING C-CHECK, THE CUSP WEB AT STA 218 RBL 54 WAS FOUND CORRODED. THE CUSP WEB WAS REPLACED IAW DC9 SRM.Jan 17, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9700849Web · crackedDURING C-CHECK, THE CUSP WEB AT STA 218 TO 237 RBL 54 LOWER SIDE WAS FOUND CORRODED. THE CUSP WEB WAS REPLACED IAW DC9 SRM.Jan 17, 1997 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR 97ZZZM228Trap Panel · crackedDTW - ULTRASONIC AND EDDY CURRENT INDICATION CRACK EMANATING FROM NR 9 ATTACH HOLE IN UPPER AFT HORIZONTAL FLANGE OF LT TRAP PANEL. CRACK LENGTH APPROX 1 INCH. REPAIR ACCOMPLISHED IAW SB 53-182 AND DOUGLAS STRUCTURAL REPAIR MANUAL (SRM) 57-09 FIGURE 7A AND EJan 17, 1997 · N934ML · Doug DC931 · Wing Miscellaneous StructureSDR 9701619977Pressure Panel · crackedDURING H-CHECK, FOUND CRACK IN NOSE WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 110. REPAIRED PER EA 99-112012.Jan 17, 1997 · N9341 · Doug DC931 · Fuselage Miscellaneous StructureSDR 9701209959Pressure Web · crackedDURING PERIODIC CHECK, FOUND PRESSURE PANEL CRACKED AT FS 83. INSTALLED REPAIR DOUBLERS PER EA 99-111996.Jan 17, 1997 · N919RW · Doug DC931 · Fuselage Miscellaneous StructureSDR 9701199959Pressure Web · crackedDURING PERIODIC CHECK, FOUND PRESSURE PANEL CRACKED AT FS 110 AT INBOARD AND OUTBOARD VERTICAL FRAMES ON RIGHT SIDE. INSTALLED REPAIR DOUBLER AND FILLER PER EA 99-112010.Jan 17, 1997 · N919RW · Doug DC931 · Fuselage Miscellaneous StructureSDR 9701169977Bulkhead · crackedDURING PERIODIC CHECK, FOUND PRESSURE PANEL CRACKED AT FS 110 ABOVE INBOARD VERTICAL SUPPORT FITTING IN NOSE WHEEL WELL. INSTALLED REPAIR DOUBLER PER EA 99-112012.Jan 17, 1997 · N9341 · Doug DC931 · Fuselage Main, Bulkhead
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