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 GTIA012107Seat Track · gougedFTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK X44 FROM STATION 649 TO STATION 765. INSTALLED SECTION OF SEAT TRACK FROM STA Y 649 TO Y 765 X 44 IAW SRM DC9 53-05. (M)Nov 8, 2001 · N12536 · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA012108Seat Track · gougedFTW - FOUND CORROSION, NICKS AND GOUGES AT SEAT TRACK BY 44 INCHES FROM STATION Y 532 TO STA 649. INSTALLED SECTION OF SEAT TRACK FROM STA 532 TO STA 649. (M)Nov 8, 2001 · N12536 · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA012149Skin · crackedFTW - FOUND RIGHT ENGINE NOSE COWL, CRACK IN INNER LIP SKIN AT 6:00 POSITION. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR PARTS PER DC9 SRM 51-30-2. (M)Nov 8, 2001 · N12536 · Doug DC932 · Engine Cowling SystemSDR GTIA012152Housing · crackedFTW - FOUND MAIN CABIN OVERHEAD CEILING PANEL BETWEEN ROWS, AFT 15 L/R INNER LIGHT HOUSING CRACKED. REMOVED EMERGENCY LIGHT ASSY. INSTALLED EMERGENCY LIGHT ASSY IAW MD9 33-53-00. (M)Nov 8, 2001 · N12536 · Doug DC932 · Emergency LightingSDR GTIA012153Light · missingFTW - FOUND MAIN CABIN, OVERHEAD CEILING PANEL BETWEEN ROWS 13L AND RIGHT LIGHT ASSY MISSING. REMOVED EMERGENCY LIGHT ASSY. REPAIRED WIRING. INSTALLED EMERGENCY LIGHT ASSY IAW MD9 MM 33-53-0. (M)Nov 8, 2001 · N12536 · Doug DC932 · Emergency LightingSDR 0104139916Rib · crackedDuring Hck at ATL, the pylon closing rib was found cracked at sta YN 176 LHS, at the portion of the lower cap. A new lower cap section was installed and spliced with repair angle. Material 0.040 TI-6AI-4V titanium. Repaired per EA 99-185300Nov 8, 2001 · N949N · Doug DC932 · Nacelle/Pylon, Main FrameSDR GTIA012325Rib · crackedFTW - FOUND RIGHT WING FUSELAGE MOUNTED VERTICAL RIB, INBOARD OF TRAILING EDGE FLAP HAS A .250 CRACK ON ITS LOWER EDGE. REMOVED DAMAGE PART. FORMED ANGLE FOR REPAIR ON VERTICAL RIB. INSTALLED REPAIR ANGLE IAW DC9 SRM 51-30-2. (M)Nov 7, 2001 · N12536 · Doug DC932 · Wing, Rib/BulkheadSDR GTIA012310Jackscrew · damagedFTW - ACME SCREW AND NUT END PLAY CHECK IN EXCESS OF .040, REPLACEMENT OF HORIZONTAL STAB ACTUATOR ASSY REQUIRED. REMOVED LONGITUDINAL TRIM CONTROL SYSTEM ASSY (JACKSCREW). INSTALLED JACKSCREW ASSY IAW DC9 MM 27-40-1. (M)Nov 7, 2001 · N12536 · Doug DC932 · Stabilizer Control SystemSDR AT0200018Longeron · crackedLONG 5R CRACKED AT STA 617.Nov 7, 2001 · N830AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0200017Longeron · crackedLONG 6R CRACKED AT STA 617.Nov 7, 2001 · N830AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0200016Longeron · crackedLONG 5L CRACKED AT STA 699.Nov 7, 2001 · N830AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA012193Floor Panel · damagedFTW - FOUND FORWARD GALLEY FLOOR WHEN WALKING ON SOUNDS AND FEELS LIKE SOMETHING LOOSE OR MISSING. REMOVED FLOOR. FORM NEW PANEL AND HATS. INSTALLED FLOOR PANEL IAW DC9 SRM 51-30-1. (M)Nov 7, 2001 · N12536 · Doug DC932 · Fuselage Floor PanelSDR GTIA012183Skin · damagedFTW - FOUND STATION 1143 L16, 2.5 L CREASE IN SKIN AFT OF FRAME, 2 INCH LONG SCRATCH FORWARD OF FRAME. FORMED DOUBLER IAW DC9 SRM 53-04. INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M)Nov 7, 2001 · N12536 · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA012238Floor Panel · deterioratedFTW - FOUND FORWARD GALLEY FLOOR LOOSE AND DETERIORATED. FORMED NEW PANEL, FORMED HAT SECTION. INSTALLED FLOOR PANEL IAW DC9 SRM 51-30-1. (M)Nov 7, 2001 · N12536 · Doug DC932 · Fuselage Floor PanelSDR GTIA012237Skin · dentedFTW - DENT LEFT FUSELAGE STATION 207, JUST ABOVE CUSP. FABRICATE DOUBLER REPAIR. INSTALLED NEW DOUBLER REPAIR IAW DC9 SRM 53-04. (M)Nov 7, 2001 · N12536 · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA012230Floorboard · damagedFTW - RIGHT INBOARD FLOORBOARD NR 5 FROM STATION 579-617 HAS EDGES BROKEN, ELONGATED HOLES AND INSULATION TORN. FORMED NEW PNL IAW DC9 SRM 53-24-0. (M)Nov 7, 2001 · N12536 · Doug DC932 · Fuselage Floor PanelSDR GTIA012229Floorboard · corrodedFTW - FOUND RIGHT INBOARD FLOORBOARD NR 2 FROM STATION 237-313, PREVIOUS REPAIR AT CORNER PEELING OFF HAS CORROSION AND GOUGES. FABRICATED REPAIR DOUBLERS AND FILLER. INSTALLED DOUBLER AND FILLER IAW DC9 SRM 51-30-2. (M)Nov 7, 2001 · N12536 · Doug DC932 · Fuselage Floor PanelSDR GTIA012093Skin · delaminatedFTW - FOUND RIGHT WING, INBOARD AILERON TAB, INBOARD CORNER UPPER SIDE DELAMINATION, 1.500 INCH SPAN BY 1 INCH, CHORD. REMOVED DAMAGE TO AILERON TAB. REPAIR TAB PER DC9 MD80 SRM 57-04. (M)Nov 7, 2001 · N12536 · Doug DC932 · Aileron TabsSDR GTIA012102Web · crackedFTW - FOUND LEFT POWER PLANT NOSE COWL AFT INNER SECTION CRACK. REMOVED CRACKED WEB DOUBLER FROM NOSE COWL. FABRICATED NEW DOUBLER AND WEB. INSTALLED DOUBLER ON WEB. INSTALLED WEB PER DC9 SRM 51-30-2. (M)Nov 7, 2001 · N12536 · Doug DC932 · Engine Cowling SystemSDR GTIA012135Floorboard · damagedFTW - FOUND RIGHT INBOARD FLOORBOARD NR 3 FROM STA Y314 TO STA Y329 HAS BROKEN EDGE (FWD ONE) AND STIFFENERS CRACKED. FORMED DOUBLER FOR RIGHT INBOARD FLOORBOARD. STOP DRILLED CRACKS, ROUNDED OUT CRACK IN STIFFENER. INSTALLED FORMED DOUBLER IAW DC9 IAW SRM Nov 7, 2001 · N12536 · Doug DC932 · Fuselage Floor PanelSDR GTIA012136Floorboard · damagedFTW - FOUND RIGHT OUTBOARD FLOORBOARD NR 2 FROM STATION 237 TO STATION 313 HAS CORROSION, ELONGATED HOLES AND EDGES BROKEN OFF. FABRICATED REPAIR DOUBLER FOR ELONGATED HOLES. FABRICATED REPAIR DOUBLER FOR BROKEN EDGES. INSTALLED REPAIR DOUBLER FOR ELONGATEDNov 7, 2001 · N12536 · Doug DC932 · Fuselage Floor PanelSDR GTIA012138Floorboard · damagedFTW - FOUND RIGHT INBOARD FLOORBOARD NR 10 FROM STATION 639 TO 680 HAS EDGES BROKEN OFF. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-05. (M)Nov 7, 2001 · N12536 · Doug DC932 · Fuselage Floor PanelSDR GTIA012217Skin · crackedFTW - FOUND RUDDER RIGHT LOWER SKIN CRACKED AT FASTENER ON RIB LOCATION NR 12. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR IAW DC9 SRM 55-03. (M)Nov 6, 2001 · N12536 · Doug DC932 · Rudder, Plate/SkinSDR GTIA012255Skin · crackedFTW - FOUND RUDDER RIGHT LOWER SKIN CRACKED AT FASTENER ON RIB LOCATION NR 11. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR IAW DC9 SRM 5-03. (M)Nov 6, 2001 · N12536 · Doug DC932 · Rudder, Plate/SkinSDR GTIA012173Rib · crackedFTW - FOUND RIGHT SIDE, FUSELAGE AREA, INBOARD OF NR 1 SLAT HAS A VERTICAL RIB, BENT AND CRACKED. REMOVED DAMAGED RIB. FORMED NEW RIB. HEAT TREATED RIB TO T-6 CONDITION. INSTALLED FORMED RIB IAW DC9 SRM 51-30-3. (M)Nov 6, 2001 · N12536 · Doug DC932 · Wing, Rib/BulkheadSDR GTIA012172Skin · dentedFTW - FOUND STATION 231 L17-18 LEFT, DENT IN SKIN. FORMED INTERNAL DOUBLER. INSTALLED DOUBLER IAW MD80 SRM 53-04. (M)Nov 6, 2001 · N12536 · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA012100Doubler · improperFTW - FOUND STATION 148 RIGHT HAS A DEN AS MARKED AROUND 02 BLOW OUT DISK. UPON FURTHER EVALUATION FOUND PRODUCTION INTERNAL DOUBLER HAVE NO CONTOUR. FABRICATE NEW INTERNAL DOUBLER. INSTALLED NEW INTERNAL DOUBLER IAW DC9 SRM 51-30-1. (M)Nov 6, 2001 · N12536 · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA012101Skin · crackedFTW - FOUND RUDDER LEFT UPPER SKIN CRACKED AT FASTENER ON RIB LOCATION NR 21. TRIMMED OUT CRACKED SKIN WITH CIRCULAR CUTOUT. FORMED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER IAW DC9 SRM 55-03. (M)Nov 6, 2001 · N12536 · Doug DC932 · Rudder, Plate/SkinSDR GTIA012111Panel · crackedFTW - FOUND RIGHT TRAPEZOIDAL PANEL CRACKED AT FASTENER LOCATIONS NR 8 AND NR 9. REMOVED DAMAGE. FABRICATED ANGLES AND FILLER. INSTALLED REPAIR ANGLES AND FILLER PER DC9 SRM 51-30-5. (M)Nov 6, 2001 · N12536 · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA011420Skin · dentedLEFT HAND ELEVATOR CONTROL TAB UPPER SURFACE HAS A DENT BETWEEN THE NR 3 AND NR 4 HINGE POINTS, .75 BY .5 INCH. FABRICATED CORE, FILLER AND DOUBLER. HOT BONDED REPAIR AND REPAINTED TRIM TAB. PERFORMED WEIGHT AND BALANCE.Nov 6, 2001 · N207ME · Doug DC932 · Elevator, Tab StructureSDR MWEA011421Skin · corrodedCORROSION ON INNER FUSELAGE SKIN ST STATION 889 AND 897 ON RIGHT HAND SIDE OF INTERCOSTAL AFT PIT. REMOVED, FABRICATED AND INSTALLED DOUBLER.Nov 6, 2001 · N207ME · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA012320Skin · crackedFTW - FOUND LEFT WING FIXED FLAP VANE HAS A CRACK AT STATION XTE 206. LOCATE AND DRILL NEW (SKIN FIXED COVER). INSTALLED SKIN ASSEMBLIES PER SRM DC9 MD80 51-30-1. (M)Nov 5, 2001 · N12536 · Doug DC932 · Trailing Edge FlapsSDR GTIA012094Vane · gougedFTW - FOUND RIGHT WING FIXED FLAP VANE HAS A GOUGE AT STATION XTE 206 (OUTBOARD SURFACE). BLEND OUT LEADING EDGE COVER AND FOUND IT OUT OF LIMITS. LOCATE AND DRILL DOUBLER AND FILLER. INSTALLED REPAIR PARTS IAW DC9 SRM 51-30-2. (M)Nov 5, 2001 · N12536 · Doug DC932 · Trailing Edge FlapsSDR CA011121016Heat Exchanger · separated(CAN) UNABLE TO MAINTAIN CABIN PRESSURE WITH R/H PACK ONLY. LT PACK ON DEVIATION. FOUND HEAT EXCHANGER SEPARATED AT THE EXCHANGER. RE-SECURED AND PACKS OPERATED NORMALLY.Nov 1, 2001 · Doug DC932 · Humidity Control SystemSDR MWEA011416Strap · corrodedCORROSION ON STRAP IN LONGERON 23 LEFT AT STATION 945 AFT PIT. BLENDED, FABRICATED AND INSTALLED LONGERON.Nov 1, 2001 · N207ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA011415Longeron · corrodedCORROSION ON LONGERON 21 LEFT AT STATION 990 AFT PIT. BLENDED, DRILLED, LOCATED AND INSTALLED NEW LONGERON.Nov 1, 2001 · N207ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA011414Longeron · crackedSTATION 1087 LONGERON 7 RIGHT IS CRACKED. FABRICATED AND INSTALLED NEW LONGERON AND LONGERON SPLICE.Oct 30, 2001 · N207ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA011413Longeron · crackedSTATION 1087 LONGERON 7 LEFT IS CRACKED. REMOVED, FABRICATED AND INSTALLED LONGERON.Oct 30, 2001 · N207ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA011411Doubler · crackedTWO AREAS OF CRACKS AROUND FASTENERS ON WINDOW INNER DOUBLER AT STATION 654 LOWER RIGHT CORNER AND AT STATION 643 UPPER LEFT CORNER OF DOUBLER. FABRICATED AND INSTALLED DOUBLERS.Oct 30, 2001 · N207ME · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA010587Skin · corrodedSKIN BULGED FROM CORROSION AT FORWARD LOWER CARGO DOOR CUTOUT BETWEEN STATION 386 AND 391. REPAIRED SKIN IAW DC-9 SRM.Oct 26, 2001 · N983AX · Doug DC932 · Fuselage Structure (General)SDR ABXA010586Doubler · crackedRIGHT WINDOW DOUBLER CRACKED IN THE UPPER FORWARD CORNER OF WINDOW AT STATION 658. REPAIRED CRACK IAW DC-9 SSRM K07226.Oct 26, 2001 · N983AX · Doug DC932 · Fuselage Structure (General)SDR ABXA010585Doubler · crackedLEFT WINDOW DOUBLER CRACKED IN THE UPPER FORWARD CORNER OF WINDOW AT STATION 699. REPAIRED CRACK IAW DC-9 SSRM K07226.Oct 26, 2001 · N983AX · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA011408Transmitter · failedAT FL330 THE LEFT ENGINE EPR GAUGE FROZE, ALL OTHER INDICATIONS NORMAL - N1, N2, EGT. CHECKED PT2 AND PT7 LINES FOR BLOCKAGE AND LEAK CHECKED FROM ENGINE TO TRANSMITTER, REFERENCE DC9 MAINTENANCE MANUAL 77-11-0. MEGGED ALL WIRES, DID A THOROUGH INSPECTION OF COct 26, 2001 · N215ME · Doug DC932 · Engine Pressure Ratio (EPR)SDR AT0200014Skin · crackedAFT SKIN OF FUSELAGE BUTT SPLICER HAS CRACK BETWEEN LONG 18L AND 19L STA 996. CUT OUT DAMAGED AREA. INSPECTED IAW DC9/MD80 NDT MM 7-1 FIG 8. NO CRACK INDICATIONS NOTED. INSTALLED DOUBLER REPAIR AT AFT SKIN FUSELAGE BUTT SPLICE PER DC9 SRM 53-04 FIG 18.Oct 24, 2001 · N867AT · Doug DC932 · Fuselage Main, Plate/SkinSDR 0103929607Angle · crackedDuring Hck at ATL Base Maintenance, an existing repair angle was found cracked at sta 176 RHS at the aft portion of the lower cap of the pylon closing rib. Also, the lower cap was found trimmed at this location. The existing repair angle was removed and discarOct 24, 2001 · N607NW · Doug DC932 · Nacelle/Pylon, Main FrameSDR AT0200015Skin · crackedFWD PASSENGER DOOR TOP, FWD DOOR JAMB CORNER CRACKED, IND AT 2 PLACES. OUTER/INNER SKIN, INNER CRACK IS ABOUT 1 INCH LONG. TRIMMED OUT CRACK AREA. INSTALLED REPAIR AT FWD PASS DOOR IAW BOEING MESSAGE CQT-ORL-01-005521. LEAK CK GOOD IAW DC9 MM 21-31-0.Oct 22, 2001 · N867AT · Doug DC932 · Fuselage Main, Plate/SkinSDR 0103919604Doubler · damagedWhile stationed at Dothan for an HCK, and in conjunction with a lower skin panel replacement per reference, a pre-existing corner repair was removed. Upon removal of the existing repair doubler, damage was found. Repaired per EA. 96-186757. Material .050" 2014Oct 22, 2001 · N604NW · Doug DC932 · Fuselage Main, Plate/SkinSDR 0103699920Motor · leakingON CLIMBOUT, THE PRIMARY TRIM CONTROL AND BOTH YOKE SWITCHES WERE INOPERATIVE. CREW RESET THE CIRCUIT BREAKERS AND CHECKED THE CUTOUT WITH NO HELP. ALTERNATE TRIM VIA AUTOPILOT DID OPERATE NORMALLY. FLIGHT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE FOUNOct 22, 2001 · N942N · Doug DC932 · Stabilizer ActuatorSDR 0103909607Angle · crackedDuring Hck in ATL, an existing repair angle was found cracked on the sta 1076 frame at the longeron 2R. The repair angle was removed and replaced with an identical repair. The repair angle was installed because a B/P 0.25 inch hole used to attach th 5910090-73Oct 18, 2001 · N607NW · Doug DC932 · Fuselage Main, StructureSDR MWEA011403Duct · crackedLOUD (RUSHING AIR) SOUND FROM AFT CABIN AREA. ALSO RIGHT TEMP CONTROL VALVE WHEN FULL HOT, BUT CABIN TEMP SHOWS FULL COLD. TEMP MODULATION (MANUAL MODE) HAS NO EFFECT. FOUND RIGHT TEMP CONTROL VALVE OUTLET DUCT CRACKED AND COUPLING HOSE DETERIORATED. INSTAOct 18, 2001 · N401ME · Doug DC932 · Air Distribution System
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