N916F, cancelled Dec 30, 2015
Service difficulty reports · 20
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N916F' AND deregistration_id = 'N916F-2015-12-30' 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 n_number = 'N916F' AND deregistration_id = 'N916F-2015-12-30' 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 EIA2004042Battery · inoperativeEMERGENCY LIGHTS IN COCKPIT EXTREMELY DIM WHEN TURNED ON. REPLACED COCKPIT EMERGENCY LIGHT BATTERY PER DC9 MM 33-53-0, OPS CHECKED GOOD.SDR EIA2003057Skin · crackedFUSELAGE SKIN AT LWR AFT CORNER OF MAIN DOOR JAMB CRACKED. REPAIRED PER DC9 SRM 53-05 FIG 103 PAGE 407-418 & 420. REPAIR IS CAT-B N5343 ASSIGNED INSP WITHIN 28,000 CYCLES PER SRM 51-10-5C (EDDY CURRENT).SDR EIA2003055Crossbeam · crackedL1 DOOR CROSSBEAM 2ND FROM TOP .5 INCH CRACK AT FWD END IN RADIUS. REPAIRED L1 DOOR CROSSBEAM, BLENDED EDGE AO PART REF DC9 SRM 53-01 FIG 1, STOPPED DRILLED CRACK PER DC9 SRM 52-05 FIG 3, HF EDDY CURRENT PER DOUGLAS SOP 51-06-07, NO CRACKS NOTED.SDR ERKR200100154Frame · damagedFRAME HAS ELONGATED FASTENER HOLE, FS 303, L15 LEFT.SDR ERKR200100153Longeron · corrodedLONGERON 30 CORROSION - FS 285.SDR ERKR200100151Doubler · crackedL1 DOOR UPPER FWD CORNER INNER DOUBLER CRACK.SDR ERKR200100150Pan · crackedCRACKED INNER DOOR PAN ON AFT CARGO PIT DOOR (P/N: 5910157-5).SDR ERKR200100149Skin · damagedUPPER CARGO DOOR OUTER SKIN DAMAGED.SDR EIA2001238Doubler · crackedFOUND LEFT FORWARD ENTRANCE DOOR FORWARD UPPER CORNER INNER DOUBLER HAS TWO CRACKS FROM EDGE GOING FORWARD. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLERS AND FILLERS PER ECRA 916-53-030-2. (M)SDR EIA2001234Frame · crackedMZJ - FOUND STATION 897 LEFT L17 FRAME CRACKED. REPAIRED PER SRM 51-30-05, 53-03, FIGURE 32, SHT 5, AND 51-10-2, 51-10-3. (M)SDR EIA2001237Longeron · corrodedMZJ - FOUND CORROSION ON LONGERON 30 NEAR STATION 290. FABRICATED AND INSTALLED REPAIR STRAP ON LONGERON 30 AT STATION 290 PER ECRA 916-53-033-2. (M)SDR EIA2001015Engine · failedKFAR - RIGHT ENGINE FAILED IN FLIGHT. (M)SDR EIA2000038Brake Assy · malfunctionedSTL - FLT 460 - WHEN CHECKING LEFT BRAKE SYSTEM DURING TAXI INTO STL, LEFT BRAKE PRESS GOES TO ZERO WHEN PEDALS DEFLECTED, AND REQUIRES PUMPING UP WITH PEDALS TO REACH 3000 PSI. REPLACED LEAKING SCHRADER VALVE AND SERVICED LT BRAKE ACCUM. (M)SDR EIAA990181Seat · misinstalledMMV - DURING EVALUATION, FOUND THAT COURIER SEAT INSTALLED PER STC SA2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF FAR 25.561. COURIER SEAT IS DEACTIVATED PER EIA EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO 25-DC9-805-91, REV C. EO APSDR EIA980378Connector · dirtyABQ - ON APPROACH TO KDEN, NO SAFE GEAR DOWN INDICATION, LOW APPROACH FLOWN AND TOWER REPORTED GEAR HANGING. RETURNED TO ABQ, EMERGENCY GEAR EXTENSION CHECKLIST RUN, ACCOMPLISHED LOW APPROACH AT ABQ, AND LANDED WITH 6000 LBS FUEL. CLEANED AND RESEATED DIMMESDR EIAA970198Light · malfunctionedSTA - ABQ - LOG PAGE: F32459 - EMERGENCY EXIT LIGHTS INTERMITTENTLY ILLUMINATED IN-FLIGHT. COULD NOT DUPLICATE, CHECKED EMERGENCY BATTERY AND LIGHTS. (X)SDR EIAA96103Skin · corrodedDURING C-CHECK INSPECTION, DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE SKIN AT BS 642, LONGERON 30, BL 0.0. AFFECTED AREA WAS TRIMMED TO REMOVE CORROSION. INSTALLED INTERNAL FINGER DOUBLERS AND EXTERNAL REPAIR DOUBLERS WET WITH SEALANT AND TOP COATSDR 97ZZZM180Skin · corrodedDURNG C-CHECK INSPECTION DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE EXTERNAL SKIN AT BS 642, LONGERON 30, BL 0. THE CORRODED AREA MEASURED 5.25 INCH IN LENGTH AND 4.9 IN WIDTH. AFFECTED AREA WAS TRIMMED TO REMOVE CORROSION. INSTALLED INTERNAL FISDR 97ZZZM179Skin · corrodedDURING C-CHECK INSPECTION DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE EXTERNAL SKIN AT BS 642, LONGERON 30, BL 0. THE CORRODED AREA MEASURED 5.25 INCH IN LENGTH AND 4.9 INCH IN WIDTH. AFFECTED AREA WS TRIMMED TO REMOVE CORROSION. INSTALLED INTERNSDR EIAA9680Skin · corrodedMZJ - EXFOLIATION CORROSION WAS FOUND ON THE LOWER FUSELAGE EXTERNAL SKIIN AT BS 642, LONGERON 30, AND BL 0.000. CORRODED AREA MEASURES 5.25 INCH LONG AND 4.90 INCH WIDTH. TWO EXTERNAL FINGER REPAIR DOUBLERS FABRICATED AND INSTALLED ON TRIMMED OUT AREA. AN
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