Douglas DC-9-32

Service difficulty reports · 12,755

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 = 'DC932'
  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 9520199923Battery Pack · dischargedDURING LINE CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD.Dec 12, 1995 · N927RC · Doug DC932 · Emergency LightingSDR MWEA95530Girt Bar Latch · fouledCREW REPORTS FORWARD ENTRANCE DOOR EVACUATION SLIDE IS DIFFICULT TO DISARM. TRIMMED CARPET AROUND FORWARD GIRT BAR LATCH.Dec 11, 1995 · N302ME · Doug DC932 · Emergency EquipmentSDR MWEA95529Intercostal · crackedDURING D-CHECK, FOUND IN E/E COMPARTMENT INTERCOSTAL AT STA 180 AND LONGERON 22L HAS CORROSION. FABRICATED INTERCOSTAL AND INSTALLED IAW SRM 53-01, PG 1.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95528Fitting · crackedDURING D-CHECK, FOUND THAT LONGERON 27R END FITTING AT STA 565 AND STA 586 IS CRACKED. INSTALLED A NEW END FITTING IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95527Fitting · corrodedDURING D-CHECK, FOUND LONGERON 26L END FITTING FROM STA 573 TO STA 604 HAD EXCESSIVE CORROSION AROUND NUTPLATE HOLE AT AFT END. INSTALLED A NEW FITTING IAW SRM 53-01, PG 1.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95526Intercostal · corrosionDURING D-CHECK, FOUND INTERCOSTAL AT LONGERON 26R HAS CORROSION FROM STA 200-STA 218 ON BOTH SURFACES IN E/E COMPARTMENT. FABRICATED A NEW INTERCOSTAL IAW SRM 53-01, PAGES 1 AND 51-60. INSTALLED INTERCOSTAL IAW SRM 53-03, PAGE 1.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95525Fitting · crackedDURING D-CHECK, FOUND LONGERON 28R END FITTING AT STA 570 IS CRACKED. INSTALLED A NEW END FITTING IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95524Fitting · crackedDURING D-CHECK, FOUND LIGHT CORROSION IN SEVERAL PLACES ON INBD SURFACE OF TRAPEZOIDAL FITTING BEHIND THE REMOVED SKI FITTING IN THE LT WHEELWELL. FOUND THE TRAPEZOIDAL FITTING TO BE CRACKED AND REPLACED IT IAW SRM 57-09, FIG 34 AND 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95523Web · corrodedDURING D-CHECK, FOUND MODERATE CORROSION AT VARIOUS LOCATIONS ALONG AFT WALL OF LT WHEELWELL WEB SKIN. REPLACED THE WEB SKIN AND T-FITTING IAW SRM 53-03, FIG 17.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA95522Angle · corrodedDURING D-CHECK, FOUND MODERATE CORROSION EVIDENT ALONG INBD EDGE OF LT WHEELWELL CUTOUT BEHIND INBD DOOR HINGE ON STRUCTURE FROM STA 699-STA 750. INSTALLED NEW ANGLE IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95521Longeron · corrodedDURING D-CHECK, FOUND RT LONGERON 20 OUTBOARD MEMBER TO BE CORRODED TO EXCESS IN ONE BOLT HOLE AND ALONG THE RADIUS OF THE ANGLE AT STA 730. REPLACED THE OUTBOARD LONGERON MEMBER IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA95520Channel · corrodedDURING D-CHECK, FOUND FLOOR PANEL CORRODED RT SIDE STA 120-STA 160. REPLACED MOST OUTBOARD HAT CHANNEL IAW SRM 53-01.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95519Doubler · crackedDURING D-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR FLOOR PAN AT STA 908. INSTALLED A REPAIR IAW SRM 53-01, FIG 2, SHEET 4.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95518Bracket · corrodedDURING D-CHECK, FOUND THE LEFT ELEVATOR NR 4 HINGE BRACKET AT STA XE225 HAS SPOTS OF MODERATE CORROSION OUT OF LIMITS. INSTALLED A NEW BRACKET IAW MM 20-16-0.Dec 11, 1995 · N401ME · Doug DC932 · Elevator StructureSDR MWEA95517Bracket · corrodedDURING D-CHECK, FOUND THAT THE RIGHT ELEVATOR NR 4 HINGE BRACKET AT STA XE225 HAS SPOTS OF CORROSION OUT OF LIMITS. INSTALLED NEW BRACKET IAW SB 55-31, FIG 3 AND MM 20-16-0.Dec 11, 1995 · N401ME · Doug DC932 · Elevator StructureSDR MWEA95516Skin · crackedDURING D-CHECK, FOUND A 1.1250 INCH CRACK IN SKIN RADIUS ON FORWARD END OF KEEL SKIN ATTACH ANGLE AT STA 683-STA 686 AT XCW10. FABRICATED AND INSTALLED A NEW SKIN IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA95515Intercostal · corrodedDURING D-CHECK, FOUND AFT CARGO DOOR JAMB INTERCOSTAL AT LONGERON 28R HAS MODERATE CORROSION AT LOWER FLANGE STA 889-STA 897. FABRICATED NEW INTERCOSTAL PER SRM 51-10-4 AND INSTALLED PER SRM 53-01.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95514Intercostal · corrodedDURING D-CHECK, FOUND AFT CARGO COMPARTMENT STRUCTURE DOOR JAMB INTERCOSTAL GUSSET PLATE HAS EXTENSIVE CORROSION AT STA 889-STA 897, LONGERON 29R. FABRICATED A NEW INTERCOSTAL IAW SRM 51-10-4. INSTALLED ATTACH CLIP AND INTERCOSTAL PER SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95513Skin · gougedDURING D-CHECK, FOUND A GOUGE APPROX .031 INCH ON THE INNER SKIN LOCATED BETWEEN STA 370 AND STA 389 JUST UNDER LONGERON 18R. INSTALLED A NEW SKIN PANEL IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA95512Floor Beam · gougeDURING D-CHECK, FOUND THAT THE FLOOR BEAM AT STA 408 HAS STRUCTURAL DAMAGE IN THE FORM OF A GOUGE IN THE LOWER FLANGE AND RADIUS LOCATED NEAR CENTER OF BEAM. FABRICATED AND INSTALLED REPAIR IAW SRM 53-05, FIG 86.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA95511Floor Beam · damagedDURING D-CHECK, FOUND THE FLOOR BEAM AT STA 389 HAS A DIME-SIZED HOLE IN THE LOWER FLANGE AND RADIUS LOCATED NEAR THE CENTER OF THE BEAM. FABRICATED AND INSTALLED THE REPAIR IAW SRM 53-05, FIG 86.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA95510Support · corrosionDURING D-CHECK, FOUND CENTER VERTICAL SUPPORT LOWER END EXTENSIVELY CORRODED ABOVE AFT FUSELAGE JACK SUPPORT AT STA 996. REPLACED THE HAT SECTION IAW SRM 51-10-4.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95509Fitting · exfoliatedDURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT LONGERON 22L SPLICE FITTING HAS SEVERE EXFOLIATION CORROSION AT STA 897-STA 917. INSTALLED A NEW FABRICATED PART PER SRM 53-01.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95508Fitting · corrodedDURING D-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 29R END FITTING AT STA 756 HAS EXFOLIATION CORROSION. DRILLED UP AND INSTALLED LONGERON IAW SRM 51-30 AND SRM 51-10-4.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95507Fitting · crackedDURING D-CHECK, FOUND THE LEFT TRAPEZOIDAL PANEL LOWER SUPPORT FITTING CRACKED. REPLACED THE SUPPORT FITTING PER SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95506Angle · crackedDURING D-CHECK, FOUND THE VENTRAL DOOR PAN AT MIDPOINT BETWEEN THE FIXED BAYONETS IS CRACKED COMING FROM UNDER THE ANGLE INSIDE. REPAIRED THE CRACKED PAN IAW SRM 52-01 AND 51-30-2.Dec 11, 1995 · N401ME · Doug DC932 · Tail Cone DoorsSDR MWEA95505Angles · crackedDURING D-CHECK, FOUND THE VENTRAL DOOR ANGLES UPPER AND LOWER AT MIDPOINT BETWEEN THE FIXED BAYONETS ARE CRACKED. INSTALLED NEW ANGLES IAW SRM 51-30-2.Dec 11, 1995 · N401ME · Doug DC932 · Tail Cone DoorsSDR MWEA95504Angles · crackedDURING D-CHECK, FOUND THE VENTRAL DOOR ANGLES UPPER AND LOWER AT THE TOP FIXED BAYONET ARE CRACKED. INSTALLED NEW ANGLES IAW SRM 51-30-2.Dec 11, 1995 · N401ME · Doug DC932 · Tail Cone DoorsSDR MWEA95503Fitting · crackedDURING D-CHECK, FOUND THE VENTRAL DOOR TOP RIGHT STOP FITTING WAS CRACKED. INSTALLED A NEW FITTING IAW SRM 50-2-0, PAGE 1.Dec 11, 1995 · N401ME · Doug DC932 · Tail Cone DoorsSDR MWEA95502Frame · corrodedDURING D-CHECK, FOUND CORROSION ON CANTED FRAME RT SIDE AFT ACCESSORY COMPARTMENT BEHIND FDR. FABRICATED REPAIR PARTS AND INSTALLED PER 53-01, FIG 2, SHEET 4.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, FrameSDR MWEA95501Longeron · corrodedDURING D-CHECK, FOUND LONGERON 21R HAS LIGHT CORROSION LOCATED BETWEEN STA 237 AND 256. REPLACED THE LONGERON SECTION IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA95500Longeron · corrodedDURING D-CHECK, FOUND LONGERON 21R HAS CORROSION JUST AFT OF STA 218 FRAME. REPLACED LONGERON SECTION IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA95499Door Jamb · crackedDURING D-CHECK, FOUND FORWARD CARGO DOOR OPENING JAMB AT STA 370 AND 427 CRACKED AT AFT STOP. REPLACED DOOR JAMB IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95498Intercostal · dentedDURING D-CHECK, FOUND INTERCOSTAL BETWEEN STA 427 AND 446 AT LONGERON 29L HAS VARIOUS AREAS OF MILD CORROSION BEYOND LIMITS. FABRICATED A NEW INTERCOSTAL IAW 53-11-2 AND INSTALLED PER SRM 53-01.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95497Intercostal · corrodedDURING D-CHECK, FOUND VHF COMM ANTENNA INTERCOSTAL SUPPORT FROM STA 465 TO 484 BETWEEN LONGERON 29L AND 30L WITH VARIOUS AREAS OF VISIBLE MILD CORROSION. INSTALLED A NEW INTERCOSTAL IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95496Trapezoid Panel · corrodedDURING D-CHECK, FOUND SEVERE CORROSION IN THE RT TRAPEZOIDAL PANEL AT STA 718 AROUND THE TWO OUTBOARD TOP AFT BOLT HOLES. REPLACED THE TRAPEZOIDAL PANEL IAW SRM 51-30 AND 57-04, FIG 34.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95495Doubler · corrodedDURING D-CHECK, FOUND THE RT ALTERNATE STATIC PORT SUPPORT DOUBLER AT STA 341 BETWEEN LONGERONS 26R AND 27R WAS CORRODED BEYOND LIMITS. INSTALLED A NEW STATIC PORT DOUBLER IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95494Doubler · corrodedDURING D-CHECK, FOUND ANTENNA SUPPORT DOUBLER AT STA 325 BETWEEN LONGERON 30L AND 29L CORRODED BEYOND LIMITS. FABRICATED A NEW DOUBLER PER SRM 53-01, PG 1 AND INSTALLED PER SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95493Skin · corrosionDURING D-CHECK, FOUND AFT CARGO OPENING UNDER EXTERNAL SCUFF PLATE AT STA 917 SKIN AND INTERNAL DOUBLER HAVE CORROSION BULGE BETWEEN LAYERS. FABRICATED DOUBLER AND INSTALLED IAW ROD SKETCH 95-11-06-007.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA95492Pan · corrodedDURING D-CHECK, FOUND AFT CARGO DOOR PAN LOWER SECTION CORRODED. REPAIRED THE LOWER DOOR PAN SECTION IAW SRM 53-05, FIG 44.Dec 11, 1995 · N401ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA95491Longeron · corrodedDURING D-CHECK, FOUND LIGHT CORROSION ON LONGERON 29R IN KEEL AREA UNDER THE AUXILIARY HYD RESERVOIR AND ON KEEL WEB. NEW LONGERON WAS INSTALLED IAW SRM 51-10-3.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA95490Longeron · corrodedDURING D-CHECK, FOUND LIGHT CORROSION AND BARE METAL ALONG LONGERON 29L IN KEEL AREA AT STA 658-676. A NEW LONGERON WAS INSTALLED IAW SRM 51-10-3.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA95489Fitting · crackedDURING D-CHECK, FOUND LT FLAP TRACK LOWER ATTACH FITTING IS CRACKED. DRILLED UP AND INSTALLED NEW FITTING IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Trailing Edge FlapsSDR MWEA95488Bracket · corrodedDURING D-CHECK, FOUND LOWER RUDDER DAMPER IDLER ARM MOUNT BRACKET HAD HEAVY CORROSION. REPLACED BRACKET IAW MM 20-16-0.Dec 11, 1995 · N401ME · Doug DC932 · Rudder Control SystemSDR MWEA95487Blkhd Clip · crackedDURING D-CHECK, FOUND A CLIP CRACKED IN THE RT LAV PRESSURE BULKHEAD AT Z34, STA 996. FABRICATED A NEW CLIP IAW THE SRM 53-01 AND INSTALLED IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA95486Pan · corrodedDURING D-CHECK, FOUND FORWARD CARGO DOOR SILL PAN CORRODED. SPLICED IN A NEW SECTION OF FORWARD CARGO DOOR PAN IAW SRM 53-05, FIG 44.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95485Pan · crackedDURING D-CHECK, FOUND AFT CARGO DOOR BOTTOM PAN CRACKED IN TWO AREAS. REPAIRED PAN PER SERVICE RE-WORK DRAWING NR 5934142.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95484Doubler · crackedDURING D-CHECK, FOUND THE AFT CARGO DOOR REPAIR WAS CRACKED ON THE FORWARD SIDE AT THE BAYONET. FABRICATED A DOUBLER PER SRM 51-10 AND INSTALLED IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA95483Skin · dentedDURING D-CHECK, FOUND THE FUSELAGE SKIN IN FRONT OF THE FORWARD CARGO DOOR AND AROUND THE STATIC PORT AREA HAS MULTIPLE DENTS THAT ARE OUT OF SRM LIMITS. INSTALLED A NEW SKIN PANEL IAW SRM 51-30 FROM STA 229-589, LONGERON 18R-26R.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA95482Skin · dentedDURING D-CHECK, FOUND THAT THE FUSELAGE FORWARD LOWER SKIN HAS MULTIPLE DENTS AND PULLED RIVETS FROM STA 229 TO 589 FROM LONGERON 26L TO 26R. REPLACED THE FORWARD LOWER SKIN IAW SRM 51-30.Dec 11, 1995 · N401ME · Doug DC932 · Fuselage Main, Plate/Skin
Back to Douglas DC-9-32