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 GTIA020294Latch · out of adjustDTW - FLT 9536 - FOUND LEFT LANDING GEAR UNSAFE LIGHT AND DOOR OPEN LIGHT REMAINED ON AFTER GEAR RETRACTION. GEAR RECYCLED IAW QRH SAME INDICATIONS. FOUND LEFT MAIN GEAR DOOR LATCH MECHANISM ASSEMBLY OUT OF ADJUSTMENT. ADJUSTED AND PERFORMED TEST IAW DC-9. Apr 20, 2002 · N12536 · Doug DC932 · Landing Gear Door Retract SectionSDR MWEA020300Gusset · corrodedFRAME TO STRUT GUSSET, LEFT SIDE AT STATION 965 CORRODED. -- REMOVED AND REPLACED GUSSET.Apr 19, 2002 · N301ME · Doug DC932 · Fuselage Miscellaneous StructureSDR 0201319609Shutoff Valve · failedMASTER WARNING AND CABIN PRESSURE LIGHTS ILLUMINATED AT FL350. AIRFOIL AND ENGINE ANTI-ICE WERE SELECTED ON. CABIN ALTITUDE WAS 10,000 FEET AND CLIMBING AT 1200 FPM. CREW PERFORMED AND EMERGENCY DESCENT AND SHUT OFF THE AIRFOIL ANTI-ICE AND THE PNEUMATIC CRApr 18, 2002 · N609NW · Doug DC932 · Cabin Cooling SystemSDR AT0200049Battery Pack · damagedAFT ESCAPE SLIDE EMERGENCY LIGHT DOES NOT ILLUMINATE (FOUND B5-28 BATTERY PACK NICAD BATTERY BLEW UP). REMOVED AND REPLACED B5-28 BATTERY PACK AND NICAD BATTERY. OPS CHECK GOOD IAW DC-9 MM 33-53.Apr 18, 2002 · N823AT · Doug DC932 · Emergency LightingSDR MWEA020262Microphone · dirtyCOMMUNICATIONS INTERMITTENT. -- FOUND CAPTAIN'S AND FIRST OFFICER'S MICROPHONE JACKS DIRTY. REMOVED AND REPLACED BOTH MICROPHONE JACKS IAW MM 20-50-01.Apr 17, 2002 · N202ME · Doug DC932 · Audio Integrating SystemSDR ABXA010856Fitting · crackedINTERCOSTAL ATTACH FITTING AT STATION 994 BETWEEN LONGERON 27 - 28 LEFT WAS CRACKED. REPLACED INTERCOSTAL ATTACH FITTING IAW DC-9 SRM.Apr 16, 2002 · N989AX · Doug DC932 · Fuselage Main, StructureSDR ABXA010855Longeron · crackedLONGERON 28 RIGHT AT STATION 990 WAS CRACKED FROM EXFOLIATION CORROSION. REPLACED LONGERON 28 RIGHT AT STATION 990 IAW DC-9 SRM 51-30-5.Apr 16, 2002 · N989AX · Doug DC932 · Fuselage Main, StructureSDR ABXA010854Support · crackedINTERCOSTAL ATTACH FITTING AT STATION 994 BETWEEN LONGERON 27 - 28 RIGHT WAS CRACKED AND CORRODED AROUND LOWER NUTPLATE. REPLACED INTERCOSTAL ATTACH FITTING IAW DC-9 SRM 51-30-5.Apr 16, 2002 · N989AX · Doug DC932 · Fuselage Main, StructureSDR ABXA010853Support · crackedRIGHT WING SLAT CONTROL PULLEY BRACKET SUPPORT WAS CRACKED. INSTALLED NEW PULLEY BRACKET IAW DC-9 SRM.Apr 16, 2002 · N989AX · Doug DC932 · Wing StructureSDR ABXA010852Rib · crackedLEFT WING LEADING EDGE RIB AT THE #2 SLAT TRACK, INBOARD RIB WAS CRACKED. REPAIRED RIB IAW DC-9 SRM.Apr 16, 2002 · N989AX · Doug DC932 · Wing StructureSDR ABXA010850Angle · crackedRIGHT VERTICAL STABILIZER ATTACH ANGLE WAS CRACKED ON THE AFT END. REPAIRED AREA IAW DC-9 SRM 53-05.Apr 15, 2002 · N989AX · Doug DC932 · Vertical StabilizerSDR ABXA010849Doubler · crackedLOWER FUSELAGE SKIN WAS CRACKED AT THE LEFT AFT NOSE GEAR DOOR ATTACHING CUTOUT. INSTALLED REPAIR DOUBLER AT THE AFT NOSE GEAR DOOR CUTOUT AREA IAW DC-9 SRM 53-05.Apr 15, 2002 · N989AX · Doug DC932 · Fuselage Main, StructureSDR 0201169922Acm · damagedCREW WAS UNABLE TO COOL THE CABIN DOWN WITH AIR CONDITIONING PRIOR TO DEPARTURE. THEN, DURING CLIMBOUT, CABIN DISPLAYED NONSTANDARD CLIMB PROFILE. VERY SLOW CLIMB TO ABOUT 17,000 FEET AND AS MAX DIFFERENTIAL WAS OBTAINED CABIN CONTINUED TO CLIMB AT 1000 FPM.Apr 15, 2002 · N945N · Doug DC932 · Cabin Cooling SystemSDR MWEA020260Switch · faultyAT 90 KNOTS, THE OVERSPEED WARNING WENT OFF. REMOVED AND REPLACED CAPTAIN'S OVERSPEED WARNING SWITCH.Apr 14, 2002 · N216ME · Doug DC932 · High Speed WarningSDR MWEA020251Angle · out of toleranceANGLE IS MADE FROM TOO THIN OF MATERIAL. ANGLE IS CURRENTLY .063 AND SHOULD BE MADE FROM .071 THICK STOCK MATERIAL. STATION 155, EPC PANEL LOCATION. -- REMOVED ANGLE. DRILLED UP ANGLE AND INSTALLED.Apr 14, 2002 · N205ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020252Angle · out of toleranceANGLE IS NOT OF CORRECT THICKNESS. SHOULD BE .063 AND IS CURRENTLY MADE FROM .040. STATION 155, EPC PANEL. -- REMOVED ANGLE. DRILLED UP ANGLE AND INSTALLED.Apr 14, 2002 · N205ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020293Spar · crackedLEFT WING FLAP TRAILING EDGE SPAR WEB HAS A SMALL CRACK ORIGINATING FROM FASTENER HOLE AT STATION. CUT AND REMOVED DAMAGED WEB AREA AND REMOVED REMAINING PORTION OF DOUBLER. LOCATED, DRILLED AND DEBURRED DOUBLER AND INSTALLED.Apr 13, 2002 · N205ME · Doug DC932 · Trailing Edge FlapsSDR ABXA010851Fitting · crackedCRACK IN FITTING COMMON TO REAR SPAR, JUST BELOW THE INBOARD SPOILER/TORSION BAR. REPLACED STIFFENER AND REPAIRED AREA IAW DC-9 SRM.Apr 13, 2002 · N989AX · Doug DC932 · Wing StructureSDR MWEA020259Sensor · faultyTHE OVERSPEED WARNING WENT OFF. REJECTED TAKEOFF. REMOVED AND REPLACED OVERSPEED SENSOR, OPS CHECK OK.Apr 12, 2002 · N216ME · Doug DC932 · High Speed WarningSDR MWEA020250Cap · inadequateCOMPLY WITH CARRY OVER 2681. LOWER CAP REPAIR, LEFT WING, AT STATION 380 REQUIRES REMOVING TEMPORARY REPAIR AND INSTALLATION OF PERMANENT REPAIR. -- FABRICATED AND INSTALLED FILLERS AND REPAIR ANGLES.Apr 12, 2002 · N205ME · Doug DC932 · Wing SparSDR MWEA020249Angle · groundedANGLE FORWARD INBOARD CORNER IS GROUND OFF. LOCATED IN THE EPC PANEL. -- REMOVED AND REPLACED ANGLE.Apr 12, 2002 · N205ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020248Clip · inadequateSTATION XRS 91, STRINGER 21, STRINGER TO BULKHEAD ATTACH CLIP REMOVED TO FACILITATE OTHER MAINTENANCE. -- REMOVED AND REPLACED CLIP. NEW CLIP NEEDED DUE TO BUILD UP OF REPAIR.Apr 12, 2002 · N205ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA020247Stringer · crackedRIGHT WING STRINGER 21 HAS CORROSION PRESENT ON FORWARD LOWER LEG FROM XRS 69 THROUGH 91. FOUND CRACKS ON STRINGER. REMOVED AND REPLACED SECTION OF STRINGER. INSTALLED REPAIR SPLICES.Apr 12, 2002 · N205ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA020246Clip · corrodedRIGHT WING STATION XRS 69 CLIP BETWEEN STRINGER 18 TO 19 HAS LIGHT CORROSION. REMOVED AND REPLACED CLIP.Apr 12, 2002 · N205ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA020245Clip · corrodedRIGHT WING STATION XRS 69 CLIP BETWEEN STRINGER 20 TO 21 HAS LIGHT CORROSION. REMOVED AND REPLACED CLIP.Apr 12, 2002 · N205ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA020244Stringer · corrodedRIGHT WING STRINGER 19 HAS LIGHT CORROSION 9 INCHES INBOARD OF STATION XRS 69. FABRICATED AND INSTALLED REPAIR STRAP.Apr 12, 2002 · N205ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA020243Stringer · corrodedSTRINGER NR 20 IN RIGHT WING HAS LIGHT CORROSION 9 INCHES OUTBOARD OF STATION XRS 69. FABRICATED AND INSTALLED REPAIR STRAP AND FILLER.Apr 12, 2002 · N205ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA020242Stringer · corrodedRIGHT WING STRINGER NR 20 HAS LIGHT CORROSION 10 INCHES INBOARD OF STATION 69. FABRICATED AND INSTALLED REPAIR STRAP AND FILLER.Apr 12, 2002 · N205ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA020241Clip · corrodedLEFT WING STATION 111 STRINGER 20 THROUGH 21 OUTBOARD CLIP REMOVED TO FACILITATE OTHER MAINTENANCE. REMOVED AND REPLACED CLIP.Apr 12, 2002 · N205ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA020240Clip · corrodedLEFT WING TANK STATION XRS 111 BETWEEN STRINGER 20 AND 21 HAS LIGHT CORROSION ON INBOARD SIDE. REMOVED AND REPLACED CLIP.Apr 12, 2002 · N205ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA020239Clip · corrodedLEFT WING TANK STATION XRS 111, BOTTOM CLIP BETWEEN STRINGER 19 AND 20 HAS LIGHT CORROSION ON INBOARD SIDE. REMOVED AND REPLACED CLIP.Apr 12, 2002 · N205ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA020238Clip · inadequateLEFT WING RIB ATTACH CLIP AT BULKHEAD 69 BETWEEN STRINGERS 22 AND 23 TO FACILITATE OTHER MAINTENANCE. -- REMOVED AND REPLACED CLIP. REPLACEMENT OF CLIP WAS REQUIRED DUE TO REPAIR IN AREA.Apr 12, 2002 · N205ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA020237Clip · inadequateREMOVED ATTACH FITTING AT BULKHEAD XRS 69, BETWEEN STRINGER 21 THROUGH 22 RIGHT WING TO FACILITATE OTHER MAINTENANCE. -- NEW CLIP NEEDED DUE TO BUILD UP OF REPAIR ON STRINGER. FABRICATED AND INSTALLED CLIP.Apr 12, 2002 · N205ME · Doug DC932 · Wing, Rib/BulkheadSDR MWEA020236Clip · corrodedREMOVED LEFT WING RIB ATTACH CLIP BETWEEN STRINGERS 17 AND 18 AT STATION XRS 91 TO FACILITATE OTHER MAINTENANCE. CORROSION FOUND ON CLIP. INSTALLED REPLACEMENT CLIP.Apr 12, 2002 · N205ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA020235Stringer · corrodedRIGHT WING TANK STRINGER NR 22 HAS LIGHT CORROSION ON FORWARD SIDE JUST INBOARD AND OUTBOARD OF STATION XRS 69. REMOVED AND REPLACED STRINGER SECTIONS. FABRICATED AND INSTALLED SPLICE PIECES.Apr 12, 2002 · N205ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA020234Stringer · corrodedLEFT WING TANK STRINGER NR 12 HAS SPOTS OF LIGHT CORROSION JUST OUTBOARD OF STATION XRS 91 AND FASTENERS ON FORWARD AND AFT SIDE WITH CORROSION BETWEEN STATION XRS 91 AND 111. REMOVED FASTENERS. REMOVED CORROSION. BLENDED CORROSION FOUND ON STRINGER FORWARDApr 12, 2002 · N205ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA020233Stringer · corrodedLEFT WING TANK STRINGER 16 HAS SPOTS OF LIGHT CORROSION AND CORRODED FASTENERS ON AFT SIDE BETWEEN STATION XRS 69 AND 91. REMOVED ANGLE, HOLES IN WING SKIN ARE DAMAGED. OVERSIZED HOLES AS REQUIRED TO CLEAN UP DAMAGE. INSTALLED REPLACEMENT ANGLE. RECEIVED AApr 12, 2002 · N205ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA020232Clip · corrodedLEFT WING TANK STATION XRS 69 RIB ATTACH CLIP HAS LIGHT CORROSION ON OUTBOARD SIDE, LOCATED BETWEEN STRINGERS NR 20 AND 21. REMOVED AND REPLACED CLIP.Apr 12, 2002 · N205ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA020231Clip · corrodedLEFT WING TANK, RIB ATTACH CLIP OUTBOARD SIDE AT STATION XRS 69 ON BOTTOM END HAS LIGHT CORROSION, LOCATED BETWEEN STRINGER 18 AND 19. REMOVED AND REPLACED CLIP.Apr 12, 2002 · N205ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA020230Stringer · corrodedLEFT WING TANK STRINGER 18 HAS FASTENERS ON FORWARD END AFT SIDE WITH LIGHT CORROSION AND SPOTS OF CORROSION JUST INBOARD OF STATION XRS 91, FASTENERS ARE BETWEEN STATION XRS 69 AND 91. FABRICATED AND INSTALLED REPAIR ANGLE.Apr 12, 2002 · N205ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA020229Clip · corrodedLEFT WING TANK STATION XRS 69 RIB ATTACH CLIP HAS LIGHT CORROSION ON OUTBOARD SIDE, LOCATED BETWEEN STRINGER 19 AND 20. REMOVED AND REPLACED CLIP.Apr 12, 2002 · N205ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA020227Stringer · corrodedLEFT WING TANK STRINGER 21 HAS A SPOT OF LIGHT CORROSION ON FORWARD SIDE AT 4TH FASTENER INBOARD STATION XRS 91. FABRICATED AND INSTALLED REPAIR SPLICES AND REPLACEMENT STRINGER.Apr 12, 2002 · N205ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA020226Stringer · corrodedLEFT WING TANK STRINGER NR 22 HAS FASTENERS ON FORWARD AND AFT SIDE WITH LIGHT CORROSION AND BARE METAL ON TOP SIDE, LOCATED BETWEEN STATION XRS 69 AND 91. FABRICATED AND INSTALLED REPAIR STRAP AND FILLER.Apr 12, 2002 · N205ME · Doug DC932 · Wing, Longeron/StringerSDR MWEA020225Clip · crackedLEFT WING TANK STATION XRS 69 RIB ATTACH CLIP IS CRACKED AT STRINGER #2. -- REMOVED AND REPLACED CLIP.Apr 12, 2002 · N205ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA020296Support Bracket · corrodedFORWARD PIT LEFT AUX TANK STRUT UPPER SUPPORT BRACKET HAS EXFOLIATION AROUND A FASTENER STATION 545 LONGERON 24 LEFT. REMOVED AND REPLACED FITTING.Apr 11, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020295Skin · damagedREPLACE AFT CARGO PIT BELLY SKIN SECTION LONGERON 28 LEFT TO 28 RIGHT STATION 803 THROUGH 996 TO COMPLY WITH CARRY OVER NR 2201. REMOVED AND REPLACED SKIN.Apr 11, 2002 · N206ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA020294Longeron · crackedFORWARD PIT LONGERON 29 RIGHT IS CRACKED AT STATION 570-578. -- REMOVED, MATCH DRILLED LONGERON AS REQUIRED PER DWG # 5910068, AND INSTALLED.Apr 11, 2002 · N206ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR 0201289611Door Frame · crackedDURING CHK IN ATL, THE FORWARD UPPER CORNER OF THE CARGO DOOR JAMB WAS FOUND CRACKED .0625. THE REPAIRS WERE MADE IAW EA 96-188479.Apr 11, 2002 · N611NA · Doug DC932 · Fuselage Main, StructureSDR 0201279611Stiffener · crackedDURING AN HCK IN ATL, ONE .60 INCH LONG CRACK WAS FOUND IN THE STA 756 BULKHEAD. THE CRACK IS LOCATED IN THE UPPER END OF THE VERTICAL STIFFENER AT X=22. THIS EA 96-188473 PROVIDES REPAIR INSTRUCTIONS FOR THIS CRACK.Apr 11, 2002 · N611NA · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020258Warning System · out of adjustOVERSPEED WARNING SOUNDED. REJECTED TAKEOFF AT LESS THAN 20 KTS. DEFERRED OVERSPEED WARNING. PERFORMED ADJUSTMENT/TEST OF OVERSPEED WARNING SYSTEM. REF MM 34-10-5. NO DEFECTS NOTED.Apr 11, 2002 · N216ME · Doug DC932 · High Speed Warning
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