Douglas DC-9-33F

Service difficulty reports · 1,681

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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 = 'DC933F'
  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 ABXA9800444Window · out of adjustCAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. ADJUSTED CAPTAIN'S CLEARVIEW WINDOW IAW DC9 MM 56-10-3.Apr 28, 1998 · N932AX · Doug DC933F · Flight Compartment WindowsSDR ABXA9800420Window · stickingCAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED UPPER HINGE LOCK.Apr 28, 1998 · N932AX · Doug DC933F · Flight Compartment WindowsSDR ABXA9800419Window · stuckCAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED LINKAGE ON CAPTAIN'S CLEARVIEW WINDOW.Apr 28, 1998 · N932AX · Doug DC933F · Flight Compartment WindowsSDR ABXA9800413Shear Tie · crackedDURING C-CHECK, FOUND SHEAR-TIE CRACKED AT STATION 945 BELOW LONGERONS 14L AND 15L. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2 AND 51-30-5.Apr 28, 1998 · N934AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9800411Fitting · crackedDURING C-CHECK, FOUND FITTING CRACKED IN AFT ENTRY DOOR, RIGHT JAMB, FWD SIDE, 36 ABOVE FLOOR LINE. REPLACED FITTING IAW DC9 SRM 51-30-22 AND 51-30-5.Apr 28, 1998 · N934AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9800407Window · stuckCAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED FORWARD WINDOW AFT ADJUSTMENT ON CAPTAIN'S CLEARVIEW WINDOW.Apr 27, 1998 · N932AX · Doug DC933F · Flight Compartment WindowsSDR TWAA9807702Hinge Fitting · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LEFT WING EYEBROW CRACK INDICATION AT LOWER OUTBOARD MOUNT HOLE FOR FLAP IDLER HINGE. INSTALLED REPAIR PER ROD SKETCH 95-12-06-18, AND ARA 10991. (M)Apr 24, 1998 · N937F · Doug DC933F · Wing, Control Surface Attach FittingsSDR EIAA980174Shear Tie · crackedDURING 'C5' CHECK, FRAME SHEAR TIE CRACKED AT BS 237 BETWEEN STR 27R AND STR 28R. REPLACED SHEAR TIE PER SRM 51-10-03. (X)Apr 24, 1998 · N944F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806816Former · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT FS 1074, LONGERON 2R, FORMER FRAME UPPER CHORD CRACKED. INSTALLED NEW FORMER RING FROM LONGERON 17L TO 17R, PER SRM 51-01, PAGE 1 ITEM C. (M)Apr 22, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806620Skin · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND AFT CARGO COMPT LOWER DOOR JAM WITH CORROSION BETWEEN SKIN AND FRAME. ALSO, 3 CRACKS APPROX .25 INCH LONG FROM STATION 900 TO 917, RBL 17 INCH. REMOVED CORROSION PER SRM 51-10-3. REPLACED CORRODED PARTS PER SRM 51Apr 21, 1998 · N937F · Doug DC933F · Fuselage Main, Plate/SkinSDR TWAA9806619Former · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FORMER FRAME CRACKED AT LONGERON 14R, STATION 1074. INSTALLED NEW FORMER RING FROM L17L TO 17R PER SRM 51-01, PAGE 1 ITEM C. (M)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806618Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND XRS 485 LEFT WING LE RIB CORRODED AND CRACKED. REPLACED RIB PER SRM 51-10, PG 1 ITEM C. (M)Apr 21, 1998 · N937F · Doug DC933F · Wing, Rib/BulkheadSDR TWAA9806617Former · damagedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FIELD REPAIR AT STATION 1074, LONGERON 2R. INSTALLED NEW FORMER RING FROM L17L TO 17R, PER SRM 51-01, PAGE 1 ITEM C. (M)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806615Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING FLAP INTERIOR AT IDLER HINGE, OUTBOARD SIDE ANGLE CRACKED. REPLACED CRACKED ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M)Apr 21, 1998 · N937F · Doug DC933F · Trailing Edge FlapsSDR TWAA9806614Doubler · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 433 DOUBLER ON AFT FACE OF STUBBY FORMER, CRACKED 4 IN ABOVE FLOOR LEVEL. REPLACED DOUBLER PER SRM 51-01 PAGE 1. (M)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806613Floor Track · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR TRACK FROM STATION 180 TO 240, LBL 21 INCH. REMOVED CORRODED TRACK FROM STATION 180 TO 248. FABRICATED AND INSTALLED NEW TRACK PER SRM 53-01, PAGE 1 ITEM C. (M)Apr 21, 1998 · N937F · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9806612Former · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND IN AFT CARGO AT FS 917, ABOVE L27L, FORMER HAD .5 INCH EYEBROW CRACK ON FWD SIDE. WELDED FLOOR SUPPORT AND STRESS RELIEVED. REINSTALLED REPAIRED PART PER SSRM 53-00-106. (M)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806611Former · damagedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FORMER FRAME FIELD REPAIR INSTALLED AT FS 1074, LONGERON 3L. INSTALLED NEW FORMER RING FROM L17L TO 17R, PER SRM 51-01, PAGE 1 ITEM C. (M)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806610Former · damagedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FORMER FRAME WITH FIELD REPAIR INSTALLED AT FS 1074, LONGERON 3R. INSTALLED NEW FORMER RING FROM LONGERON 17L TO 17R, PER SRM 51-01, PAGE 1 ITEM C. (M)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806609Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LEFT WING XRS 490, LE RIB CRACKED. REPLACED RIB PER SRM 51-01, PAGE 1 ITEM C. (M)Apr 21, 1998 · N937F · Doug DC933F · Wing, Rib/BulkheadSDR TWAA9806608Floor Track · wornMCI - DURING OP 16 MAINTENANCE CHECK AT RBL 8 INCH BS 269 HAS FLOOR TRACK WITH EXCESS METAL REMOVED BEYOND LIMITS TO CLEAN UP CORROSION. REPLACED SECTION OF TRACK PER SRM 53-05, PG 10G VIEW A. (M)Apr 21, 1998 · N937F · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9806607Frame · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 433 STUBBY FRAME CRACKED 3 INCHES ABOVE FLOOR. REPLACED FRAME PER SRM 51-01, PAGE 1 ITEM C. (M)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Main, FrameSDR TWAA9806606Skin · dentedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND DENT IN UPPER FUSELAGE SKIN, 1.5 INCH BY 1.5 INCH BY .080 DEEP AT FS 225, ON STRINGER 11L. REPAIRED DENT PER SRM 53-04 FIG 38. (M)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Main, Plate/SkinSDR TWAA9806513Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING TE FLAP INTERIOR AT IDLER HINGE, INBD ANGLE CRACKED AT TWO PLACES. REPLACED CRACKED ANGLE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Trailing Edge FlapsSDR TWAA9806416Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING XRS 490 LE RIB CRACKED. REPLACED RIB PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Wing, Rib/BulkheadSDR TWAA9806415Former · damagedMCI - DURING OP 16 MAINTENANCE CHECK FOUND FS 1074 LONGERON 2R FORMER RING FROM L17L TO 17R WITH FIELD REPAIR INSTALLED. INSTALLED NEW FORMER RING FROM LONGERON 17L TO 17R PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806414Casting · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING TE REAR SPAR NR 2 FLAP HINGE CASTING, UPPER INBD AND OTBD MOUNT HOLES WITH CORROSION ABOVE HOLES. REMOVED CORROSION. STOP DRILLED CRACK WITH .25 INCH. INSTALLED FILLER IN BLENDED OUT AREA. INSTALLED DOUBLApr 21, 1998 · N937F · Doug DC933F · Wing, Control Surface Attach FittingsSDR TWAA9806411Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING FLAP INTERIOR AT IDLER HINGE, INBD ANGLE CRACKED AT 2 PLACES. REPLACED CRACKED ANGLE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Trailing Edge FlapsSDR TWAA9806404Skin · dentedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND UPPER FUSELAGE DENT IN SKIN 1.50 INCH BY 1.50 INCH BY .080 INCH DEEP AT FS 225 ON STR 11L. REPAIRED DENT PER SRM 53-04 FIG 38. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Main, Plate/SkinSDR TWAA9806403Frame · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 433 STUBBY FRAME CRACKED 3 INCHES ABOVE FLOOR. REPLACED FRAME PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Main, FrameSDR TWAA9806402Floor Track · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, RBL 8 IN SGTA 269 FOUND FLOOR TRACK WITH EXCESS METAL REMOVED BEYOND LIMITS TO CLEAN UP CORROSION. REPLACED SECTION OF TRACK PER SRM 53-05 PG 10G, VIEW A. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9806310Frame · damagedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 1074 LONGERON 3R FORMER FRAME WITH A FIELD REPAIR INSTALLED. INSTALLED NEW FORMER RING FROM LONGERON 17L TO LONGERON 17R PER SRM 51-01 PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Main, FrameSDR TWAA9806309Frame · damagedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 1074 LONGERON 3L FORMER FRAME WITH FIELD REPAIR INSTALLED. INSTALLED NEW FORMER RING FROM LONGERON 17L TO LONGERON 17R PER SRM 51-01 PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Main, FrameSDR TWAA9806308Former · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 917 ABOVE LONGERON 27L, FORMER HAS .50 INCH EYEBROW CRACK ON FORWARD SIDE. WELDED FLOOR SUPPORT AND STRESS RELIEVED. REINSTALLED REPAIRED PER SSRM 53-00-106. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806307Floor Track · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR TRACK FROM STA 180 TO STA 240, 21 INCHES LBL. REMOVED CORRODED TRACK FROM STA 180 TO STA 248. FABRICATED AND INSTALLED NEW TRACK PER SRM 53-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66Apr 21, 1998 · N937F · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9806306Doubler · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 433 DOUBLER ON AFT FACE OF STUBBY FORMER CRACKED 4 INCHES ABOVE FLOOR LEVEL. REPLACED DOUBLER PER SRM 51-01 PG 1. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806305Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING FLAP INTERIOR AT IDLER HINGE, OTBD SIDE ANGLE CRACKED. REPLACED CRACKED ANGLE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Trailing Edge FlapsSDR TWAA9806304Rib · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND XRS 485 LT WING LE RIB CORRODED AND CRACKED. REPLACED RIB PER SRM 51-10 PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Wing, Rib/BulkheadSDR TWAA9806303Frame · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FORMER FRAME CRACKED AT LONGERON 14R, STA 1074. INSTALLED NEW FORMER RING FROM LONGERONS 17L TO 17R PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 21, 1998 · N937F · Doug DC933F · Fuselage Main, FrameSDR TWAA9806302Jamb · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND AFT CARGO BIN LOWER DOOR JAMB CORROSION BETWEEN SKIN AND FRAME AND 3 EACH CRACKS APPROXIMATELY .25 INCH LONG FROM STA 900 TO STA 917, 17 INCHES RBL. REMOVED CORROSION PER 51-10-3. REPLACED CORRODED PARTS PER 51-01 Apr 21, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9800361Battery Pack · dischargedCOCKPIT EMERGENCY LIGHTS WERE DIM. REPLACED BATTERY PACK.Apr 20, 1998 · N930AX · Doug DC933F · Emergency LightingSDR EIAA980147Wheel · crackedNR 2 MAIN TIRE, WHEEL RIM CRACKED AND TIRE DEFLATED, DEBRIS SEVERED BOTH HYDRAULIC LINES. REMOVED AND REPLACED NR 2 TIRE AND BRAKE ASSY IAW MM 32-40-1 AND 32-42-1. REPLACED BOTH BRAKE HYD LINES. CHECKED GEAR, FLAP AND ENGINE FOR FOD DAMAGE, NONE NOTED. (M)Apr 19, 1998 · N933F · Doug DC933F · Wheel/Ski/FloatSDR TWAA9806605Former · bentMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FORMER BENT AT FS 522, BETWEEN LONGERON 18R AND 17R. REPAIRED PER SRM 53-03, PAGE 5. 'Z' FRAME FLANGE REPAIR INSTALLED. (M)Apr 16, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806604Floor Track · corrodedDURING OP 16 MAINTENANCE CHECK, FOUND FLOOR TRACK CORROSION AT FS 198 TO 237, RBL 21 TO 26. REMOVED CORROSION PER 51-10-3. REINSTALLED TRACK PER MM 53-40-1 PAGE 201. (M)Apr 16, 1998 · N937F · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9806603Skin · delaminatedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON LEFT TE FLAP, THIRD TE FLAP SECTION DELAMINATED ON LOWER FWD END. REPAIRED PER SRM 51-01 AND STANDARD PRACTICES. (M)Apr 16, 1998 · N937F · Doug DC933F · Trailing Edge FlapsSDR TWAA9806602Former · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT FS 484, A FORMER CRACKED AT TOP AREA OF WINDOW BELT, RT SIDE. REPLACED FORMER PER SRM 53-03, FIG 32. (M)Apr 16, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806408Former · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 484 FORMER CRACKED AT TOP AREA OF WINDOW BELT, RT SIDE. REPLACED FORMER PER SRM 53-03, FIG 32. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 16, 1998 · N937F · Doug DC933F · Fuselage Miscellaneous StructureSDR TWAA9806407Skin · delaminatedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT TE FLAP, THIRD TE FLAP SECTION, DELAMINATED ON LOWER FORWARD END. REPAIRED IN SHOP PER SRM 51-01, AND STANDARD PROCESSES. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 16, 1998 · N937F · Doug DC933F · Trailing Edge FlapsSDR TWAA9806406Floor Track · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 198 FLOOR TRACK WITH CORROSION RBL 21 TO RBL 26. REMOVED CORROSION PER 51-10-3. REINSTALLED TRACK PER MM 53-40-1 PG 201. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 16, 1998 · N937F · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9806405Frame · bentMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 522 FORMER BENT BETWEEN LONGERON 18R AND LONGERON 17R. REPAIRED PER SRM 53-03, PAGE 5. Z-FRAME FLANGE REPAIR INSTALLED. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)Apr 16, 1998 · N937F · Doug DC933F · Fuselage Main, Frame
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