Douglas DC-9-14

Service difficulty reports · 1,736

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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 = 'DC914'
  ORDER BY difficulty_date DESC"

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SDR MWEA96604Floor Beam · corrodedDURING D-CHECK, FOUND FLOOR BEAM AT STA 801 HAS SEVERAL AREAS OF EXFOLIATION CORROSION ON UPPER FLANGE UNDER RT LAV. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 53-05 FIG 20A.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Floor BeamSDR MWEA96603Longeron · damagedDURING D-CHECK, FOUND REPAIR OF LONGERON 2L AND 2R AT STA 897 NEED EVALUATION FOR REWORK. MAINTENANCE REMOVED REPAIR ON LONGERONS 2L AND 2R AT STA 897 AND INSTALLED SPLICE REPAIR IAW SRM 53-02 FIG 2.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA96602Skin · corrodedDURING D-CHECK, FOUND E AND E COMP BELLY SKIN HAS CORROSION IN SEVERAL AREAS BETWEEN STA 110 TO 229 LONG 26 TO 26R. REMOVED AND REPLACED BELLY SKIN STA 110 TO 229 IAW SRM 51-30-2.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Plate/SkinSDR MWEA96601Panel · gougedDURING D-CHECK, FOUND LEFT WING TRAILING EDGE PANEL HAS 2 GOUGES ON THE SURFACE FWD OF THE GROUND SPOILER PANEL. MTC BLENDED GOUGES FOUND OUT OF LIMITS. INSTALLED DOUBLER REPAIR IAW SRM 57-01 FIG 2.Oct 11, 1996 · N80ME · Doug DC914 · Wing, Plate/SkinSDR MWEA96600Skin · corrodedDURING D-CHECK, FOUND AFT CARGO COMPT SKIN FROM STA 690 TO 817 LONG 26L TO 26R HAS SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED SKIN STA 690 TO 817 L26L TO 26R IAW SRM 51-30-2.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Plate/SkinSDR MWEA96599Skin · chafedDURING D-CHECK, FOUND LEFT FLAP UPPER EXTERIOR SKIN CHAFED 12 INCHES STA XFLS 273 TO 285. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 57-01.Oct 11, 1996 · N80ME · Doug DC914 · Trailing Edge FlapsSDR MWEA96598Angle · enlarged holeDURING D-CHECK, FOUND ENLARGED FASTENER HOLE ON FRAME TO SKIN ATTACH ANGLE AT STA 237, LONGERON 8R. INSTALLED FABRICATED ANGLE IAW SRM 53-03 FIG 32.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA96597Skin · corrodedDURING D-CHECK, FOUND SKIN BULGED AT STA 218, LONGERON 23R, NO CORROSION FOUND. INSTALLED DOUBLER REPAIR IAW SRM 53-04 FIG 38.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Plate/SkinSDR MWEA96596Longeron · crackedDURING D-CHECK, FOUND LONGERON 23R IS CRACKED AT STA 218. INSTALLED LONGERON IAW SRM 53-02 FIG 2.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA96595Longeron · crackedDURING D-CHECK, FOUND LONGERON 30 CRACKED AT STA 754 AFT CARGO COMPT. MAINTENANCE SPLICED IN NEW SECTION OF LONGERON IAW SRM 53-10-3.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA96594Intercostal · crackedDURING D-CHECK, FOUND INTERCOSTAL UNDER NR 2 SEAT TRACK IS CRACKED FWD OF STA 642. INSTALLED DOUBLER REPAIR IAW SRM 53-01 FIG 2.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA96593Doubler · missingDURING D-CHECK, FOUND SKIN REPAIR AT STA 110 TO 125 AND LONGERON 25R TO 26R NEED TITANIUM FINGER DOUBLER. INSTALLED REPAIR IAW SRM 53-04 FIG 26, SHEET 1.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA96592Longeron · damagedDURING D-CHECK, FOUND PREVIOUS REPAIR AT STA 544 TO 558, LONGERON 176 TO 186 THAT NEEDS REWORK. INSTALLED DOUBLER REPAIR IAW SRM 53-04 FIG 22.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA96591Seat Track · corrosionDURING D-CHECK, FOUND CABIN SEAT TRACK NR 3 HAS CORROSION AT STA 294 BEYOND LIMITS AND CABIN SEAT TRACK NR 1 HAS CORROSION AT STA 408 BEYOND LIMITS. INSTALLED REPAIR ON BOTH SEAT TRACKS IAW SRM 53-04 FIG 4.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA96590Skin · corrodedDURING D-CHECK, FOUND AFT CARGO COMPT BELLY SKIN CORRODED TO EXCESS STA 660 AND 649, LONGERON 28L AND 27L. INSTALLED DOUBLER REPAIR IAW SRM 53-04 FIG 38.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Plate/SkinSDR MWEA96589Skin · corrodedDURING D-CHECK, FOUND CORROSION ON SKIN IN FWD CARGO COMPT STA 305 TO 313, LONGERON 24R TO 26R. INSTALLED LONGERON SPLICE REPAIRS AND DOUBLER REPAIRS IAW SRM 53-04.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Plate/SkinSDR MWEA96588Bracket · crackedDURING D-CHECK, FOUND LT FLAP TRAILING EDGE NR 3 OUTBD END RIB FWD UPPER BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-30-2.Oct 11, 1996 · N80ME · Doug DC914 · Trailing Edge FlapsSDR MWEA96587Skin · wrinkledDURING D-CK, FOUND LT FLAP TRAILING EDGE NR 3 COUNTERSUNK HOLE ON UPPER SURFACE DAMAGED AND SKIN WRINKLED. INSTALLED DOUBLER REPAIR IAW SRM 57-01 FIG 2.Oct 11, 1996 · N80ME · Doug DC914 · Trailing Edge FlapsSDR MWEA96586Panel · crackedDURING D-CHECK, FOUND PRESSURE PANEL SKIN IN NOSE WHEEL WELL CRACKED STA 83 AND LT CUSP LINE 5 INCHES IN LENGTH, RT CUSP LINE 2 PLACES STA 83. INSTALLED DOUBLER REPAIR IAW DAC SB53-187.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA96585Rib · crackedDURING D-CHECK, FOUND VERTICAL STAB LEADING EDGE STA ZV147 UPPER RIB CRACKED AT AFT END. FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 55-01 FIG 2, SHEET 3.Oct 11, 1996 · N80ME · Doug DC914 · Vertical Stabilizer, Spar/RibSDR MWEA96584Skin · crackedDURING D-CHECK, FOUND SKIN CRACK AT STA 930 AND LONGERON 3L, .625 INCH IN LENGTH. INSTALLED DOUBLER REPAIR IAW SRM 53-04 FIG 38.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Plate/SkinSDR MWEA96583Strap · crackedDURING D-CHECK, FOUND CRACK IN STRAP ALONG FWD EDGE OF MAIN CABIN ENTRY DOOR OUTER PAN BELOW NR 2 STOP FITTING. FABRICATED AND INSTALLED REPAIR IAW SRM 52-01 FIG 2.Oct 11, 1996 · N80ME · Doug DC914 · Passenger/Crew DoorsSDR MWEA96582Floor Beam · corrodedDURING D-CHECK, FOUND FLOOR BEAM AT STA 801 HAS SEVERAL AREAS OF EXFOLIATION CORROSION AROUND NUTPLATES ON UPPER ANGLE OF FLOOR BEAM. FABRICATED AND INSTALLED REPAIR IAW SRM 53-05, FIG 20M.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Floor BeamSDR MWEA96581Bulkhead Doubler · missingDURING D-CHECK, FOUND PART OF FINGER DOUBLER MISSING ON FWD SIDE OF AFT PRESSURE BULKHEAD AT 10 O'CLOCK POSITION NEAR DOOR JAMB. FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 53-01.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, BulkheadSDR MWEA96580Bulkhead · scratchDURING D-CHECK, FOUND SMALL SCRATCH ON FWD SIDE OF AFT PRESSURE BULKHEAD FIVE INCHES ABOVE FLOOR LEVEL BLENDED BEYOND LIMITS. INSTALLED REPAIR IAW DAC TELEX SVC-ORD-0246/DMF.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, BulkheadSDR MWEA96579Skin · crackedDURING D-CHECK, FOUND AFT CARGO COMPT SIDE SKIN CRACKED AT STA 817 RT SIDE LONGERON 22R, 8 INCHES IN LENGTH. INSTALLED REPAIR IAW DAC TELEX SVC-ORD-0232/RAK.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Plate/SkinSDR MWEA96578Fitting · crackedDURING D-CHECK, FOUND RT WING UPPER OUTBD SKIN FITTINGS AT STA XRS 164 NEAR REAR SPAR ARE CRACKED. MAINTENANCE FABRICATED AND INSTALLED NEW FITTINGS IAW DAC DRAWING 4913298, 4911461, AND SRM 57-01.Oct 11, 1996 · N80ME · Doug DC914 · Wing Miscellaneous StructureSDR MWEA96577Fitting · crackedDURING D-CHECK, FOUND LT FLAP OUTBD HINGE FITTING MOUNT INBD AND OUTBD RIBS CRACKED. REPLACED CRACKED FITTINGS IAW SRM 57-30-2 AND SRM 51-30.Oct 11, 1996 · N80ME · Doug DC914 · Trailing Edge FlapsSDR MWEA96576Angle · corrodedDURING D-CHECK, FOUND FLOOR BEAM UPPER CAP ANGLE CORRODED BEYOND LIMITS. INSTALLED NEW CAP ANGLE IAW SRM 53-01.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA96575Longeron · corrodedDURING D-CHECK, FOUND LONGERON 29L AT STA 500 CORRODED BEYOND LIMITS. REPLACED LONGERON IAW SRM 51-30.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA96574Fitting · crackedDURING D-CHECK, FOUND LONGERON 26L END FITTING CRACKED AT STA 470. REPLACED END FITTING IAW SRM 51-30-2.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA96573Longeron · crackedDURING D-CHECK, FOUND LONGERON 30 CRACKED AT STA 229, 365 AND 435. INSTALLED LONGERON SECTION STA 229 TO 465 IAW SRM 51-30-5.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA96572Longeron · crackedDURING D-CHECK, FOUND LONGERON 29L CRACKED AT STA 474 AND 303. INSTALLED NEW LONGERON SECTION IAW SRM 51-30-5.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA96571Intercostal · crackedDURING D-CHECK, FOUND FLOOR BEAM INTERCOSTAL CRACKED AT STA 360 AND 371 AND A/C CENTER LINE. INSTALLED DOUBLER REPAIR IAW SRM 53-01.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA96570Longeron · corrodedDURING D-CHECK, FOUND CORROSION ON LONGERON 27R AT STA 132 TO 140, 142 TO 144, 148 TO 154 BEYOND LIMITS. INSTALLED SECTION OF LONGERON IAW 53-02, FIG 4.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA96569Door Pan · corrodedDURING D-CHECK, FOUND E AND E DOOR JAMB PAN HAS CORROSION IN SEVERAL AREAS. MAINTENANCE REPLACED DOOR JAMB PAN IAW SRM 51-10-3 AND 51-30.Oct 11, 1996 · N80ME · Doug DC914 · Electrical/Electronic Compartment DoorsSDR MWEA96568Skin · corrodedDURING D-CK, FOUND LT ELEVATOR SKIN HAS SURFACE CORROSION AT OUTBD END. INSTALLED DOUBLER REPAIR IAW SRM 55-03 FIG 15.Oct 11, 1996 · N80ME · Doug DC914 · Elevator, Plate/SkinSDR MWEA96567Skin · damagedDURING D-CK, FOUND FWD CARGO BELLY SKIN STA 229 THROUGH 484 LONG 26L, 26R HAS EXISTING SCAB PATCH REPAIRS AT FIVE ANTENNA LOCATIONS. REPLACED BELLY SKIN STA 229 THROUGH 484, LONG 226L, 26R IAW SRM 53-01.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Plate/SkinSDR MWEA96566Blkhd Stiffener · crackedDURING D-CK, FOUND CRACKED STIFFENER ON AFT SIDE OF AFT PRESSURE BULKHEAD JUST BELOW DOOR JAMB. INSTALLED STIFFENER IAW SRM 53-01.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, BulkheadSDR MWEA96565Blkhd Stiffener · crackedDURING D-CK, FOUND CRACK IN STIFFENER, AFT SIDE OF AFT PRESSURE BULKHEAD AT FOUR O'CLOCK POSITION JUST OUTBD OF DOOR JAMB APPROX .25 INCH IN LENGTH. INSTALLED DOUBLE ANGLE REPAIR IAW SRM 53-01, SHEET 4.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, BulkheadSDR MWEA96564Trap Panel · crackedDURING D-CK, FOUND RT TRAPEZOIDAL PANEL FWD FLANGE HAS A CRACK THAT EXTENDS AFT THROUGH THE FOURTH FASTENER APPROX .125 INCH. INSTALLED DOUBLER REPAIR IAW SRM 57-09, FIG 6 AND DAC TELEX SVC-MSP-0789.Oct 11, 1996 · N80ME · Doug DC914 · Wing Miscellaneous StructureSDR MWEA96563Frame · crackedDURING D-CK, FOUND FRAME CRACKED AT CANTED STA 925, LONGERON 13R. INSTALLED FRAME REPAIR IAW SRM 53-01 FIG 2.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, FrameSDR MWEA96562Clip · crackedDURING D-CK, FOUND FRAME TO SKIN ATTACH CLIP CRACKED AT STA 916 BETWEEN LONGERON 16R AND 17R. REPLACED SHEAR CLIP IAW SRM 51-30-01, FIG 1.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA96561Frame · crackedDURING D-CK, FOUND FRAME CRACKED AT STA 904, LONGERON 25L. INSTALLED FRAME REPAIR IAW SRM 53-01 FIG 2.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, FrameSDR MWEA96560Longeron · damagedDURING D-CK, FOUND LONGERON 8R LOWER FLANGE DAMAGED AT STA 916 AFT ACCESSORY. SPLICED IN SECTION OF LONGERON 8R IAW SRM 53-02 FIG 2A.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA96559Longeron · crackedDURING D-CK, FOUND LONGERON 11R CRACKED AT STA 880. INSTALLED NEW SECTION OF LONGERON 11R IAW SRM 53-02, FIG 2.Oct 11, 1996 · N80MKE · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA96558Rib · crackedDURING D-CK, FOUND LEADING EDGE SECTION ON LT WING HAS TWO CRACKED RIBS, 6TH FROM INBD END AND MOST OUTBOARD. BOTH CRACKED AT UPPER ENDS. INSTALLED DOUBLE ANGLE REPAIR IAW SRM 57-01 FIG 2, SHEET 3.Oct 11, 1996 · N80ME · Doug DC914 · Wing, Rib/BulkheadSDR MWEA96557Skin · crackedDURING D-CK, FOUND LT WING LEADING EDGE SECTION NR 2 HAS .5 INCH CRACK IN AIR EXIT DUCT ON INNER SKIN. INSTALLED REPAIR IAW SRM 57-06, FIG 1.Oct 11, 1996 · N80ME · Doug DC914 · Wing, Plate/SkinSDR MWEA96556Web · crackedDURING D-CK, FOUND WEB IN KEEL AREA BETWEEN STA 508 TO 523 BULGED AND CRACKED, LONG 30. FABRICATED AND INSTALLED WEB SECTION IAW SRM 51-30-2.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA96555Fitting · corrodedDURING D-CK, FOUND IN FWD KEEL AREA LONGERON 27L, 28L, 29L, END FITTINGS HAVE HEAVY CORROSION. REPLACED L27L, 28L, 29L END FITTINGS IAW SRM 51-10-4 AND 51-30.Oct 11, 1996 · N80ME · Doug DC914 · Fuselage Miscellaneous Structure
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