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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR VJ9800462Fitting · corrodedLONGERON END FITTING AT FS 600 CORRODED BEYOND LIMIT. LOCATED, DRILLED AND DEBURRED NEW FITTING IAW DC9 SRM 51-10-4.SDR MWEA98946Linkage · disconnectedTHE STALL INDICATION FAILURE LIGHT CAME ON AUTO SPOILER DO NOT USE LIGHT WITH SMELL IN CABIN. PERFORMED AIR TURNBACK. MAINTENANCE FOUND GROUND SHIFT LINKAGE DISCONNECTED AND RECONNECTED.SDR MWEA98945Oven · dirtyTHE LEFT OVEN STARTED TO SMOKE AND FLIGHT ATTENDANT TURNED OFF. MTC CLEANED AND OPS CHECKED OVEN.SDR VJ9800461Channel · corrodedLT AFT LAV BRACKET ASSY HARDWARE AND BRACKET FOR PULLEYS ON AFT PRESSURE BULKHEAD CORRODED. FABRICATED CHANNEL REPAIR FROM EXTRUSSION S1324556 IAW DC9 SRM 53-01, FIG 1 AND 50-10-1. TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, 51-30-3, 51-30-1 AND 51-30SDR VJ9800409Skin · corrodedTRAILING EDGE SKIN OUTBOARD LOWER AFT CORNER LT ELEVATOR CORRODED BEYOND LIMIT. FABRICATED DOUBLER REPAIR, DRILLED, COUNTERSUNK, ALODINED, PRIMED AND INSTALLED DOUBLER IAW DC9 SRM 55-20-0 FIG 3, 51-30-9, 51-10-3, 51-30-8.SDR VJ9800408Skin · corrodedTRAILING EDGE SKIN LT ELEVATOR, UPPER OUTBOARD AFT CORNER CORRODED BEYOND LIMIT. FABRICATED REPAIR FROM 2024T3, .050. TREATED AND PRIMED AREA, INSTALLED DOUBLER IAW DC9 SRM 51-30-8, 51-10-3, 55-01, 55-03 FIG 14.SDR VJ9800369Access Panel · corrodedACCESS PANEL C2 DOOR, FWD SIDE, CORRODED BEYOND LIMIT AND CORROSION UNDER NUTPLATES. CUT OUT CORRODED AREA IAW DC9 SRM 51-01, FIG 1. FABRICATED REPAIR DOUBLER AND SPLICE, HEAT TREATED, PRIMED, DRILLED AND INSTALLED IAW DC9 SRM 51-10-3, 51-10-4, 51-30-1, 51-3SDR VJ9800368End Cap · corrodedEND CAPS STA 598 - 600, L30, 29L AND 29R CORRODED BEYOND LIMIT. REMOVED END CAPS AND DETERMINED CORRODED OUT OF LIMIT IAW SRM 53-01, FIG 1. DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED NEW END CAPS IAW DC9 SRM 51-10-3, 51-10-4, 51-30-2 AND 51-30-5.SDR VJ9800314Seal · chafedNR 1 ENGINE SPRING SEAL ON LOWER SURFACE APRON HAS WEAR BEYOND LIMIT DUE TO CHAFING IAW DC9 SRM 53-01, FIG 1. LOCATED, DRILLED, DEBURRED AND INSTALLED NEW SPRING SEALS IAW DC9 SRM 51-10-4 AND 51-30-5.SDR VJ9800313Shroud · chafedAPU GENERATOR ACCESS INNER ATTACH COVER OPENING HAS POPPED FASTENERS AND DEEP CHAFE MARKS BEYOND LIMIT. REMOVED SHROUD, DRILLED OFF HEAT BLANKET TO GAIN ACCESS TO WORK AREA IAW DC9 SRM 53-01, FIG 1. FABRICATED NEW SHROUD PER DC9 SRM 51-10-2, 51-10-4 AND RES SDR VJ9800312Fitting · corrodedJACKPAD STRUT CORRODED BEYOND LIMIT AT FS 996, L30. REMOVED CORROSION FROM JACKPAD FITTING AND ALODINED, PRIMED, REPAINTED, DRILLED AND DEBURRED NEW STRUT IAW DC9 SRM 51-10-3 AND 51-10-4.SDR VJ9800311Web · corrodedAFT PIT WEB CORRODED BEYOND LIMIT AT FS 996. REMOVED CORROSION, DRILLED, DEBURRED, ALODINED, AND PAINTED NEW WEBS IAW DC9 SRM 51-10-2, 51-10-3 AND 51-10-4.SDR VJ9800310Frame · corrodedFORWARD PIT FRAME, WHERE CLIP NUTS TO LOWER PART OF FRAME, CORRODED BEYOND LIMIT AT FS 579, L26R-26L. REMOVED CORROSION IAW DC9 SRM 53-01, FIG 1. FABRICATED FRAME, HEAT TREATED, TRIMMED, DEBURRED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-21, 51-10-4, 51-10-3 ASDR TWAA9814902Skin · crackedDURING MAINT, FOUND FIVE .250 INCH CRACKS IN FUSELAGE SKIN EXTENDING FROM RIVETS STA 170 TO 175, LONGERON 22L. REPAIRED PER SRM 53-04, FIG 12B. CHECK-C 3-2-98 STL.SDR TWAA9814503Skin · crackedFOUND 5 .250 INCH CRACKS IN FUSELAGE SKIN EXTENDING FROM RIVETS STA 170 TO 175, LONG 22L. REPAIRED PER SRM 53-04, FIG 12B.SDR CALA9801586Clip · crackedINSPECTION FOUND A 2 INCH CRACK IN SHEAR TIE CLIP AT LT AFT CABIN STA 965 UNDER LONGERON 13L. THE CRACK WAS REMOVED AND A CLIP REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 28.SDR CALA9801585Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR SKIN AT LOWER AFT CORNER. THE CRACKED AREA WAS CUT OUT AND A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 52-01, FIGURE 4.SDR CALA9801566Uplatch Mech · out of adjustTHE RT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING IAH. THE GEAR WAS CYCLED AND THE LIGHT EXTINGUISHED, BUT THE GEAR DOOR OPEN LIGHT REMAINED ON. THE AIRCRAFT WAS RETURNED TO IAH. BOTH THE LT AND RT MLG DOORS WERE DAMAGED ON LANDING.SDR CA981001010Apu · leaking(CAN) ON ENGINE START, OIL SMELL REPORTED, AFT CABIN SMOKE ALARM CAME ON. AIR CYCLE MACHINE OIL LEVEL FOUND LOW. LEFT AIR CYCLE MACHINE AND APU REPLACED, SYSTEM SERVICEABLE.SDR ABXA9800873Track · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT FLOOR TRACK IN THE AFT LOWER CARGO COMPARTMENT CORRODED AT FS 889. REPLACED FLOOR TRACK AT FS 889 IAW DC9 SRM.SDR ABXA9800872Track · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT FLOOR TRACK IN THE AFT LOWER CARGO COMPARTMENT CORRODED FROM FS 756 TO FS 855. REPLACED FLOOR TRACK FROM FS 756 TO 855 IAW DC9 SRM.SDR ABXA9800856Fitting · gougedWHILE COMPLYING WITH C-INSPECTION, FOUND A RIGHT FLAP MOVEABLE VANE PULLEY BRACKET ATTACH FITTING GOUGED AND RIVETS SHEARED. REPLACED RIGHT FLAP PULLEY BRACKET ATTACH FITTING IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR VJ9800309Frame · corrodedFORWARD PIT FRAME CORRODED BEYOND LIMIT AT FS 465, L30. REMOVED FASTENERS AND CORROSION IAW DC9 SRM 51-30-1. FABRICATED REPAIR, CLIP FILLER AND DOUBLERS IAW DC9 SRM 53-08, FIG 2A, 51-10-3, 51-30-2 AND 51-30-5. HEAT TREATED, ALODINED, PRIMED AND INSTALLED FASDR VJ9800308Angle · corrodedLOWER FORWARD AREA SKIN ATTACHMENT ANGLE AT RT NOSE WHEEL AREA HAS CORROSION BEYOND LIMIT. REMOVED CORROSION AND ATTACH ANGLE IAW DC9 SRM 51-10-3 AND SRM 53-01, FIG 1. FABRICATED REPAIR DOUBLER AND PRIMED IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2 AND 51-30-5.SDR GTIA9800100Skin · tornDTW - AT GATE, BAGGAGE CART DRIVER INTO RT AFT OF AIRCRAFT. PUNCTURE IN SIDE OF FUSELAGE JUST AFT OF BAGGAGE DOOR. PERFORMED FUSELAGE SKIN EXTERNAL RPAIR FROM FS 937 TO FS 950 BETWEEN L23R AND L26R IAW 08-98-53-012 FROM 8-28-98. DRAWING 53-98445-1 PAINTED ASDR ABXA9800871Track · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT FLOOR TRACK IN THE FORWARD LOWER CARGO COMPARTMENT CORRODED AT FS 370. REPLACED FLOOR TRACK AT FS 370 IAW DC9 SRM.SDR ABXA9800864Door · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE AFT LOWER CARGO COMPARTMENT BARRIER DOOR CORRODED. REPLACED AFT CARGO BARRIER DOOR IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR VJ9800407Rib · corrodedINNER ATTACH RIB, NR 4 FROM TOP, CORRODED BEYOND LIMIT AT LT, RT AND CENTER ATTACH POINTS. REMOVED CORROSION IAW DC9 SRM 52-01, PG 3. FORMED REPAIR ANGLES FROM 2024, .025. HEAT TREATED, LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-2A, SDR VJ9800406Rail · corrodedAFT ENTRY AIRSTAIRS CORRODED BEYOND LIMIT ON RAIL PANEL AT LT FS 1100. CUT OUT CORRODED AREA IAW DC9 SRM 51-10-3 AND 52-01. FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR ON RAIL IAW DC9 SRM 52-01 AND 52-05. FABRICATED AND INSTALLED STACKED ANGLE REPAIRSDR VJ9800405Rib · corrodedINNER ATTACHING RIB NR 5 ON AFT AIRSTAIRS CORRODED BEYOND LIMIT AT ATTACHING POINTS LT, RT AND CENTER. LT AND RT POINTS CORRODED BEYOND LIMIT IAW DC9 SRM 52-01, PG 3. FORMED REPAIR ANGLES FROM 2024T3, .025, IAW DC9 SRM 52-01, PG9. HEAT TREATED IAW SRM 51-10SDR VJ9800307Frame · corrodedFORWARD PIT FRAME CORRODED TOP AND BOTTOM AT FS 541, L27L-28L. REMOVED CORROSON IAW DC9 SRM 51-10-3, SRM 53-01, FIG 1. REMOVED FLOOR SUPPORT FROM LONGERON 24R-24L IAW DC9 SRM 51-30-2. FABRICATED FLOOR SUPPORT FROM 7075-0, .063, TREATED, LOCATED, DRILLED, PRSDR MWEA98942Skin · gougedFOUND GOUGES ON FUSELAGE SKIN LEFT SIDE BETWEEN LONGERON 18 LEFT AND 19 LEFT STATION 218. MTC BLENDED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER.SDR ABXA9800858Angle · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND THE INBOARD ATTACH ANGLE FOR THE CENTER BUTE DOOR CRACKED AT RIGHT WING STATION 164 HINGE BRACKET. REPLACED ATTACH ANGLE IAW DC9 SRM CHAPTER 51-30-01.SDR ABXA9800857Door · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT WING INBOARD BUTE DOOR CRACKED AT INBOARD CAM ROLLER. REPLACED LEFT INBOARD BUTE DOOR IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-2.SDR 9809999621Sensor · brokenDURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW PERFORMED EMERGENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOWNLOCK PROXIMITY SENSOR BROKEN. REPLACED SENSOR. ALSO RSDR VJ9800404Skin · damagedEXTERNAL REPAIR AT FS 83-55 ABOVE LT NOSE WHEEL WELL REQUIRES FLUSH REPAIR BECAUSE IT IS IN A CLASS 1 AERODYNAMIC AREA. REMOVED EXISTING DOUBLER AND FRAME FOR ACCESS IAW RES 981346. FABRICATED TITANIUM INTERNAL DOUBLER AND FLUSH FILLER FROM 2024T3. ALODINEDSDR VJ9800300Battery Pack · dischargedCEILING EMERGENCY LIGHTS INOP AT MID CABIN. REPLACED THE CEILING LIGHT BATTERY PACK ASSY.SDR VJ9800299Slide · inoperativeR-1 DOOR EVAC SLIDE ILLUMINATION LIGHTS DID NOT COME ON WHEN MX CHECKING SLIDE AFTER DEPLOY. PULLED LANDYARD AND LIGHT CAME ON. REPLACED THE SLIDE ASSY.SDR VJ9800349Frame · chafedAFT STAIR RT FRAME HAS 2 INCH GOUGE MIDWAY DOWN AND CHAFFING AGAINST FUSELAGE. OUT OF LIMIT IAW DC9 SRM 52-01, CALIPER MEASURE A NR 1729. FABRICATED REPAIR ANGLES IAW DC9 52-01, FIG 2 AND INSTALLED WITH SEALANT.SDR VJ9800288Taxi Light · smokingDURING TAKEOFF, AT MSL 1000, FLIGHT CREW OBTAINED A FAINT SMELL OF SMOKE AND ELECTED TO RETURN TO IAD MAINTENANCE BASE. INSPECTION OF AIRCRAFT INDICATED SMOKE MAY HAVE EMANATED FROM TAXI LIGHT GROUND WIRE. REPLACED RT NOSE TAXI LIGHT AND OPS CHECKED GOOD.SDR 9809949623Sensor · brokenNOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CAPTAIN DECLARED AN EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. NOSE GEAR WAS PINNED ON RUNWAY AND AIRCRAFT WAS TOWED TO GATE. MAINTENANCE FOUND NOSE GEAR DOWNLOCK PROXIMITY SENSOR BROKEN.SDR VJ9800293Flange · corrodedNLG AFT DOOR FUSELAGE FLANGE CORRODED BEYOND LIMIT AT BS 105, BL 10R. REMOVED FLANGE AND ORDER NEW PART IAW DC9 SRM 53-05. DRILLED HOLES IAW DC9 SRM 51-10-4. PRIMED IAW DC9 SRM 51-10-3 AND INSTALLED FRAME IAW DC9 SRM 51-30-1, 51-30-2, 51-30-5, 51-30-8 AND 5SDR VJ9800287Batteries · dischargedMAIN CABIN DOOR PORTABLE EMERGENCY LIGHTS INOP. REPLACED NICAD BATTERIES; OPS CHECKED GOOD IAW MM 33-50.SDR CALA9801496Switch · inoperativeTHE RT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR HANDLE WAS IN THE UP POSITION AND THE GEAR DOOR OPEN LIGHT WAS EXTINGUISHED. CYCLING THE GEAR DID NOT HELP. THE FLIGHT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE RT UPSDR VJ9800426Bracket · corrodedFWD PIT FS 484 LONG 27R-28R FRAME BRACKET CORRODED. REMOVED FRAME BRACKET IN FWD BS 484 BETWEEN STR 27R AND 28R IAW SRM 51-30-1. REMOVED CORROSION ON BRACKET ORIGINAL THICKNESS .130. REMOVED .033 IAW AERO CARP MICROMETER NR A-1729, FOUND TO BE OUT OF LIMITSSDR VJ9800425Floor · corrodedFLOORBOARD NR 34 HAS CORROSION AROUND EDGES, CHAFED MARKS ON HAT CHANNEL AND BROKEN AT FASTENER ON PREVIOUS REPAIR CRACK. BLENDED CHAFED AREAS AND REMOVED CORROSION IAW SRM 53-01 FIG 1 IN LIMITS. REMOVED PREVIOUS REPAIR AND FOUND TO BE CORRODED BEYOND LIMITSSDR VJ9800424Skin · lightning strikeFWD FUSELAGE RT SIDE FS 110 HAS LIGHTENING STRIKE. BLENDED AREA IAW SRM 53-04 FIG 38 FOUND TO BE OUT OF LIMITS IAW SRM 53-04 FIG 38, 53-01 FIG 1. REMOVED OUT OF LIMITS AREA, FABBED REPAIR DOUBLER FROM .032 TITANIUM. DRILLED, COUNTERSUNK, DEBURRED, TREATED, SDR VJ9800305Fitting · corrodedLT AND RT LOWER FLOOR SUPPORT FITTINGS ARE CORRODED FS 238 BETWEEN LOG 27 AND 28 IN FWD CARGO COMPT. REMOVED EXISTING FITTINGS, REMOVED AND BLENDEDCORROSION PER DC-9 SRM 51-10-3. CORROSION BEYOND LIMITS PER DC-9 SRM 53-01 FIG 1. REPLACED EXISTING FITTINGS WSDR VJ9800292Intercostal · corrodedHORIZONTAL INTERCOASTAL CORRODED BEYOND LIMIT AT FS 600-610, L16, AN FS 710, L16. REMOVED CORROSION IAW DC9 SRM 51-30-3. LOSS LIMITS IAW DC9 SRM 53-01, FIG 1. CUT, TRIMMED AND FABRICATED INTERCOASTAL FROM 7075-0, 040, IAW DC9 SRM 53-11-3, FIG 1. HEAT TREATSDR VJ9800291Hat Channel · corrodedCABIN FLOORBOARD CORRODED BEYOND LIMIT AROUND SCREW HOLES, HAT CHANNELS AND CHAFED IN CONTACT AREA AT STA 160 - 200, LBL 0 - 44. REMOVED CORROSION IAW DC9 SRM 51-10-3, 53-01. FABRICATED FLOORBOARD FROM 7075T6, .025 IAW DC9 SRM 53-21-0. FABRICATED 4 EACH HAT
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