Douglas DC-9-33F
Service difficulty reports · 1,681
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 = '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.
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
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 EE4Y20110177Skin · crackedFUSELAGE SKIN CRACKED AT STA Y83.55 +Z42 +X10.SDR EE4Y20110138Vane · bulgedLT WING FLAP CTR FIXED VANE LOWER SKIN BULGED AT INBD AREA.SDR EE4Y20110137Fitting · crackedFOUND AT STA Y1077 BWTN LONG 25R AND 27R, FITTING CRACKED. DAMAGED PART WILL BE REPLACED IAW NRI 1-217.SDR EE4Y20110136Fitting · crackedFOUND AT MAIN CARGO DOOR LOWER JAMB, STA Y 301.5 BETWEEN LOND. 19L AND 20L, FRAME FITTING CRACKED. DAMAGED PART WILL BE REPLACED WITH NO ROUTINE ITEM 1-167.SDR EE4Y20110135Frame · crackedDURING THE INSPECTION COOOPESA FOUND AT UPPER FUSELAGE COCKPIT, STA 83.550 AT +Z42.00 AND -X 10 HORIZOLTAL FRAME CRACKED.SDR EE4Y20110134Frame · crackedDURING THE INSPECTION COOOPESA FOUND AT UPPER FUSELAGE COCKPIT, STA 83.550 AT +Z42.00 AND +X 100 HORIZOLTAL FRAME CRACKED.SDR ABXR201009250052Control Cable · corrodedDURING FERRY FLIGHT PREP FOUND CABLE 51C CORRODED FWD OF APB. R & R CABLE 51C IAW AMM.SDR ABXR201009250051Control Cable · brokenDURING FERRY FLIGHT PREP FOUND NR 1 ENGINE FWD TELESCOPING BRAIDED CABLE RUSTED, WORN, AND BROKEN STRANDS. R & R NR1 ENGINE FWD TELESCOPING GRAIDED CABLE IAW AMM.SDR ABXR201009250050Control Cable · brokenDURING FERRY FLIGHT PREP FOUND CABLE RUN 52C FOR RT THRUST REVERSER CORRODED AND BROKEN STRANDS. R & R CABLE 52C IAW AMM.SDR ABXR201009250049Control Cable · brokenDURING FERRY FLIGHT PREP FOUND THRUST REVERSER CONTROL CABLE 48C BROKEN. R & R CABLE 48C IAW AMM.SDR ABXR201009250048Control Cable · brokenDURING FERRY FLIGHT PREP FOUND NR 1 T/R SECTOR ON AFT 'P' DOME DOESN'T MOVE WITH T/R HANDLE MOVEMENT. REPLACED CABLE 47C IAW AMM.SDR ABXR201009250047Push-Pull Cable · damagedDURING FERRY FLIGHT PREP FOUND NR 2 ENGINE THROTTLE DOES NOT MOVE FROM THROTTLE LEVER. R & R NR 2 ENGINE THROTTLE PUSH PULL CABLE IAW MM.SDR ABXR201009250046Yoke · corrodedDURING FERRY FLIGHT PREP FOUND NR 2 ENGING FWD. YOKE CORRODED. R & R NR 2 ENG FWD YOKE IAW AMM.SDR ABXR201009250045Fitting · corrodedDURING FERRY FLIGHT PREP FOUND NR 2 PYLON FWD. UPPER SPLICE FITTING CORRODED. R & R NR2 PYLON FWD UPPER SPLICE FITTING IAW AMM.SDR ABXR201009250044Fitting · corrodedDURING FERRY FLIGHT PREP FOUND NR 2 PYLON FWD LOWER SPLICE FITTING CORRODED. R & R SPLICE FITTING IAW SRM.SDR ABXR201009250043Mount · corrodedDURING FERRY FLIGHT PREP FOUND NR2 PYLON AFT ENGINE MOUNT CORRODED. R AND R AFT MOUNT ASSY IAW MM.SDR ABXR201009250042Isolator · corrodedDURING FERRY FLIGHT PREP FOUND NR1 PYLON UPPER VIBRATION ISOLATOR RUSTED AND PITTED. R & R NR1 PYLON UPPER VIBRATION ISOLATOR IAW MM.SDR ABXR201009250041Isolator · corrodedDURING FERRY FLIGHT PREP FOUND NR 1 PYLON YOKE LOWER ISOLATION ABSORBER RUSTED AND PITTED. R & R LOWER ISOLATION ABSORBER IAW MM.SDR ABXR201009250040Mount · corrodedDURING FERRY FLIGHT FLIGHT, PREP FOUND NR1 PYLON AFT MOUNT RECEIVER RUSTED AND PITTED. R & R NR1 PYLON AFT MOUNT IAW MM.SDR ABXR2010092400039Link · corrodedDURING FERRY FLIGHT, PREP FOUND NR1 PYLON AFT MOUNT UPPER INBD "H" DOG BONE AND OTBD BOLT RUSTY. R & R BOLT AND MOUNT LINK IAW MM.SDR Y2PA2010042310007Connector · looseON FINAL APPROACH LT MLG INDICATIONS WERE ABNORMAL. GREEN "GEAR DOWN" LIGHT EXTINGUISHED. THE RED "GEAR UNSAFE" LIGHT WAS MOMENTARILY FLICKERING. ELECTED TO EXECUTE GO-AROUND TO RUN APPROPRIATE COM PROCEDURES. PROCEEDED TO HOLD. GOT THE GEAR DOWN WITH 3 GREEN SDR Y2PA2010032410002Landing Gear · malfunctionedGEAR HANDLE WOULD NOT RELEASE FROM UP POSITION. PERFORMED EMERGENCY GEAR EXTENSION CHECKLIST AND LANDED WITHOUT INCIDENT. ACFT STOPPED ON RUNWAY AND MX PINNED LANDING GEAR AND SECURED MAIN GEAR DOORS TO PREVENT ADDITIONAL DAMAGE FROM CONTACT WITH GROUND. ACFTSDR ABXR200912180053Bulkhead · corrodedDURING A ROUTINE HEAVY MX INSP EVENT AFT PRESSURE BULKHEAD WEB CORRODED AT THE 6:00 POSITION. FABRICATED AND REASSEMBLED FALSE BULKHEAD WEB IAW SRM 53-11-3. ITEM WAS RETURNED TO SERVICE.SDR ABXR200912180052Panel · corrodedDURING A ROUTINE HEAVY MX INSP EVENT RT WING T/E PANEL HAS 3 AREAS OF CORROSION/DELAMINATION ALONG THE T/E OF THE PANEL. REMOVED UPPER SKIN AND HONEY COMB CORE, CLEANED CORROSION AND SKIN IAW SRM 51-70-2. ITEM WAS RETURNED TO SERVICE.SDR ABXR200912180051Fitting · corrodedDURING A ROUTINE HEAVY MX INSP EVENT RT FLAP INBD HINGE, FWD HINGE HALF HAS RUST BLEED FROM UPPER 2 SPAR ATTACH BOLTS. RT FWD INBD FLAP HINGE FITTING WAS REPLACED IAW AMM 57-40-1. ITEM WAS RETURNED TO SERVICE.SDR ABXR200912180050Bulkhead · corrodedDURING A HEAVY ROUTINE MX INSP THE AFT PRESSURE BULKHEAD HAD CORROSION BETWEEN LONGERONS 25R TO 29R. REPAIRED AFT PRESSURE BULKHEAD IAW SRM 53-05, PARAGRAPH 116. ITEM WAS RETURNED TO SERVICE.SDR ABXR200912180049Structure · crackedDURING A HEAVY MX VISIT CRACK INDICATION WITH EDDY CURRENT VERT STAB L/E UPPER SECTION. STOP DRILLED CRACK IAW SRM 55-02 FIG 27. FABRICATED REPAIR PARTS OUT OF 2024-T3 .050 AND .040. ITEM RETURNED TO SERVICE.SDR ABXR200912180048Rib · crackedDURING A ROUTINE HEAVY MX VISIT HAD CRACK INDICATION AT A FASTENER FOR 2 EACH RIBS ON THE RT SIDE OF THE LWR SECTION OF THE VERTICLE STAB. STOP DRILLED CRACK IAW SRM 55-02, FIG 27, FABRICATED REPAIR DOUBLERS USING .0407075-T6 IAW SRM 55-31-00. ITEM WAS RETURSDR ABXR200912170047Beam · crackedDURING A ROUTINE HEAVY MX VISIT THE AFT LWR CARGO DOOR BEAM END FITTING, 2ND BEAM FROM FWD END IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-30-05. ITEM RETURNED TO SERVICE.SDR ABXR200912170046Beam · crackedDURING A HEAVY MX THE AFTR LWR CARGO DOOR HAS CRACKED BEAM END FITTING. INSTALLED NEW FITTING IAW SRM 51-30-05. ITEM WAS RETURNED TO SERVICE.SDR ABXR200912170045Skin · chafedDURING A ROUTINE HEAVY MX VISIT FOUND 2 (EA) CHAFE MARKS IN VERTICLE STAB RT SIDE. (TOP/FWD) REMOVED AND REPLACED SKIN WITH RIVITS IAW SRM 51-30-2 AND HILOCKS IAW SRM 51-30-5. ITEM RETURNED TO SERVICE.SDR ABXR200912170044Stud · corrodedDURING A ROUTINE HEAVY MX VISIT LT FLAP INBD HINGE UPPER OTBD BLEEDING RUST. INBD STUDS REPLACED IAW AMM 57-40-1 AND REPAIRED HINGE IAW OVERHAUL MM 27-50-5. ITEM RETURNED TO SERVICE.SDR ABXR200912170043Tab · corrodedDURING A ROUTINE MX VISIT, LT ELEVATOR CONTROL TAB WAS FOUND TO HAVE SURFACE CORROSION ON THE LWR SIDE. INSTALLED NEW ELEVATOR CONTROL TAB IAW AMM 27-30-3. ITEM WAS RETURNED TO SERVICE.SDR ABXR200912170042Rib · corrodedDURING A ROUTINE HEAVY MX INSP EVENT THE LT WING T/E RIB AT STA XRS 133 WAS FOUND EXFOLIATED. REPAIRED RIB BY SPLICING IN NEW SECTION AND INSTALLING DOUBLER IAW SRM 57-3, SHT 2. INSTALLED FASTENERS IAW SRM 51-30-2 AND 51-30-5.SDR ABXA080176Battery · dischargedCOCKPIT EMERGENCY LIGHTS WOULD NOT COME ON DURING TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00. (A)SDR ABXA080123Wire · brokenAFTER LANDING AT ILN, FIRST OFFICER'S MAP LIGHT SPARKED AND SMOKED WHEN TURNED ON. TURNED OFF LIGHT, SMOKE AND SPARKS STOPPED. REPAIRED BROKEN WIRE FROM FIRST OFFICER'S MAP LIGHT. OPS CHECK GOOD IAW DC9 AMM 33-00-00.SDR ABXA080109Limit Switch · faultyOPERATION OF ALTERNATE LONGITUDINAL TRIM SWITCHES CAUSES ONE 5 AMP CIRCUIT BREAKER TO TRIP. ALSO THERE IS A BURNT SMELL PRESENT. VERIFIED BAD ALTERNATE LONGITUDINAL TRIM MOTOR DOWN LIMIT SWITCH. REPLACED LIMIT SWITCH IAW DC9 AMM 27-40-10-2.SDR ABXR080086Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159.SDR ABXR080085Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 50. REPAIRED IAW DC9 SSRM DWG K05159.SDR ABXR080082Rib · crackedRIB CRACKED AT FASTENER LEFT SIDE VERT STABILIZER LEADING EDGE ZFS 93. REPAIRED RIB IAW DC9 SRM D05159.SDR ABXR080084Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT VERT STAB LEADING EDGE ZFS 43. REPAIRED IAW DC9 SSRM DWG K05159.SDR ABXR080081Rib · crackedRIB CRACKED AT FASTENER LEFT SIDE OF VERTICAL STAB LEADING EDGE XFS 148. REPAIRED IAW DC9 SSRM DWG K05159.SDR ABXR080078Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 50. REPAIRED IAW DC9 SSRM DWG K05159.SDR ABXR080077Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 43. REPAIRED IAW DC9 SSRM DWG K05159.SDR ABXR080076Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159.SDR ABXR080075Rib · crackedRIB CRACKED AT FASTENER RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 23. REPAIRED IAW DC9 SSRM DWG K05159.SDR ABXR080083Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159.SDR ABXR080080Rib · crackedRIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 74. REPAIRED LEFT AND RIGHT RIBS IAW DC9 SSRM K05159.SDR ABXR080079Rib · crackedRIB CRACKED AT FASTENER RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 80. REPAIRED RIB IAW DC9 SSRM K05159.SDR ABXR080074Frame · crackedFRAME AT STA 1168 AT APPROX 3 O'CLOCK POSITION WAS CRACKED. REPAIRED AREA IAW DC9 SRM 53-01, FIG 2.
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