Douglas DC-8-62F
Service difficulty reports · 1,163
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 = 'DC862F' 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 = 'DC862F' 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 IXXA060233SFrame · misdrilledDURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 822.5 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060232SFrame · misdrilledDURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 1120 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060231SFrame · misdrilledDURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 1060 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060229SFrame · misdrilledDURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 960 LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060228SFrame · misdrilledDURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 940 LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060227SFrame · misdrilledDURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 900 TO 902 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060226SFrame · misdrilledDURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 880 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060225SFrame · misdrilledDURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 857.1 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060224SFrame · misdrilledDURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION 864.5 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060223SFrame · misdrilledDURING ROUTINE C CHECK FOUND DOUBLE DRILLED HOLE AT STATION 822.5 LONGERON 14 LEFT. REPAIRED FRAME PER ALL APPLICABLE DATA.SDR IXXA060222SIntercostal · corrodedDURING ROUTINE C CHECK FOUND CORRODED INTERCOSTAL FROM STATION Y702.75 TO Y717.75 AT LONGERON 20 LEFT. REPLACED INTERCOSTAL PER ALL APPLICABLE DATA.SDR IXXA060230SFrame · misdrilledDURING ROUTINE C-CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 1000 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060362SPanel · bulgedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE221 TO XE272 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060361SPanel · bulgedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE77 TO XE149 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060360SPanel · bulgedDURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE221 TO XE272 BULGED AND RIVET SHEARED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060318SPanel · bulgedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE28.843 TO XE77 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060317SPanel · bulgedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE77 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060316SPanel · bulgedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE221 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060315SPanel · bulgedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE221 TO XE272 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060314SPanel · bulgedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE272 TO XE312.5 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060313SPanel · bulgedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE77 TO XE28.843 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060312SPanel · bulgedDURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE149 TO XE77 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060311SPanel · bulgedDURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE149 TO XE272 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060310SPanel · bulgedDURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE SECTION BETWEEN STATION XE272 TO XE312 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060309SSkin · corrodedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER UPPER SKIN FROM FRONT SPAR TO REAR SPAR AT STATION XE28.843 CORRODED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060308Panel · bulgedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE77 TO XE28.843 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060307SPanel · bulgedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE272 TO XE312.5 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060306SPanel · bulgedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE149 TO XE221 BULGED AND DENTED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060305SPanel · bulgedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE221 TO XE272 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060304SPanel · bulgedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE272 TO XE312.5 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060303SPanel · bulgedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE221 BULGED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060302SPanel · bulgedLEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE77 BULGED AND DENTED. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060449SSkin · scratchedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE LOWER SKIN SCRATCHED AT STATION XFS139.250. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA0400020OLinkage · looseDURING FLIGHT CABIN CLIMBING AT 1000' PER MINUTE- AIRCRAFT ALTITUDE FL200- UNALBE TO CAUSE CABIN TO DESCEND TO NORMAL ALTITUDE- CROSSFEED OPEN. MAINTENANCE INSPECTED PNEUMATIC DUCTING AND PERFORMED LEAKS CHECK. NO DEFECTS NOTED. MAINTENANCE THEN PERFORMED GROUSDR IXXA0400011OFan · burned outDURING CRUISE FROM WSAP TO RJTY, SMOKE WAS IN COCKPIT. CREW TURNED OFF BOTH RECIRC FANS AND SMOKE CLEARED. CREW CONTINUED TO RJTY AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WHEN MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENASDR IXXA0400012OSwitch · brokenDURING CRUISE FROM WSAP TO RJTY, DOORS NOT LATCHED LIGHT CAME ON. BOTH ALTERNATE LIGHTS STAYED OUT. MAINTENANCE REMOVED AND REPLACED RIGHT LATCH DOOR SWITCH PER ALL APPLICABLE MANUALS OPERATIONAL CHECK GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE.SDR ARWA20050202Line · leakingDURING CRUISE LOST HYDRAULIC QUANTITY TO STAND PIPE. PERFORMED EMERGENCY/ABNORMAL CHECK LIST. FOUND ONE HYDRAULIC LINE, ENGINE NR 3, TO ENGINE LINE OPERATIONAL CHECK AND LEAK CHECK OK IN ACCORDANCE WITH MM 29-00-00.SDR IXXA0300084OCompressor · stalledON TAKE OFF FROM TAPA AT 115KTS NR 3 ENGINE COMPRESSOR STALLED AND POWER ROLLED BACK. CREW REJECTED TAKE OFF. 1 TIRE WAS FLAT AND THERMALED 3 MAIN ON RIGHT GEAR. MAINTENANCE INSPECTED NR 3 ENGINE FOR FOD/BIRD STRIKE PER ALL APPLICABLE MANUALS, AND NO DEFECTS SDR ARWA20031203Warning Light · illuminatedAFTER TAKEOFF OUT OF KMIA VENT DOOR WARNING LIGHT CAME ON & CABIN PRESS WAS UNABLE TO BE MAINTAINED.SDR ARWA20031102Wheel · shearedON POST-FLIGHT FOUND NR 3 MAIN WHEEL SHEARED OFF. REMOVED AND REPLACED NR 3 MAIN WHEEL ASSEMBLY IAW MM 32-40-1. ALSO, REMOVED AND REPLACED NR 4 MAIN WHEEL ASSEMBLY IAW MM 32-40-1.SDR GKZR200471C01Skin · corrodedFINGER DOUBLER ON PRESSURE WEB STA 188 TO 208 RBL 28 HAS CORROSION AND RIVET HEADS SHEARED. REMOVED CORROSION, CUT OUT DAMAGED AREA, FABRICATED FILLER, FINGER DOUBLER 2 EACH AND PLATE IAW DC8 SRM 53-2-0. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED ALL SDR ARWA20030802Proximity Switch · inoperativeGEAR NOT LATCHED; LIGHT ILLUMINATED AFTER GEAR UP. FOLLOWED ABNORMAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED PROXIMITY SWITCH BOX SYSTEM BITE TEST NORMAL AND OPERATIONAL CHECK NORMAL WITH GEAR SWING IAW MM 32-60-0.SDR ARWA20030707Proximity Switch · dirtyGEAR NOT LATCHED LIGHT CAME ON IN FLIGHT AND STAYED ON ALL THE TIME. LUBED UPLATCHED MAIN & NOSE GEAR MECHANISM IAW MM 12-81-1; CLEANED ALL PROXIMITY SWITCHES IAW MM 20-50-1. OPERATIONAL CHECK FOUND NORMAL IAW MM 32-30-0. SEVERAL GEAR SWING PERFORMED.SDR ARWA20030501Compressor · stalledNR 1 ENGINE COMPRESSOR STALLED, REDUCED POWER 1.50 EPR, N1 TACH FLUX AND MAX "O". OIL TEMP INCREASING. ENGINE SHUT DOWN 05:30Z WINDMILLING OIL PRESSURE 16 PSI. NOTE: PRELIMINARY INSPECTION REVEAL C1 BEARING FAILURE. CORRECTIVE ACTION:SDR ARWA20030403Arm · brokenAFTER GEAR RETRACTION NOISE AND VIBRATION FROM NOSE GEAR AREA. POST FLIGHT INSPECTION FOUND GEAR DOOR ARM BROKEN WITH DAMAGE TO FUSELAGE AT DOOR HINGE AREA. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER REPAIR IAW DC8 SRM 53-2-1 FIG 7 PAGE 111. REMOVED AND RESDR ARWA20030320Frame · crackedDURING C-CHECK THE FOLLOWING WAS FOUND; FS 1606 AFT PRESSURE BULKHEAD TEE CAP WITH 8 INCH CRACK BTW L-9L AND L12L. CUT LONGERONS 11L, 12L AND 13L AND REMOVED SPLICES (OPEN), CUT DAMAGED AREA OF FRAME IAW DC8 SRM 53-2-0, PREPARED NEW FRAME SEGMENT IAW BOEING ASDR ARWA20030319Door Frame · damagedDURING C-CHECK THE FOLLOWING WAS FOUND; MAIN CARGO COMPARTMENT DOOR JAMB UPPER WEB BROKEN STA 360, L-6L. CUT OUT DAMAGED AREA IAW DC8 SRM 53-2-0, FABRICATED FILLER AND DOUBLER IAW DC8 SRM 53-2-0, PRIMED FILLER AND DOUBLER IAW DC8 SRM 51-1-8 AND INSTALLED FILLSDR ARWA20030318Skin · damagedDURING C-CHECK THE FOLLOWING WAS FOUND; FUSELAGE EXTERIOR STA 1280, BTW L29R AND L31R SKIN WITH NICKS. TRIMMED OUT DAMAGE AREA IAW AS ELEVEN INC DRAWING AS11490 SHEET 1 OF 2 AND 2 OF 2, DATED 02/19/03; FABRICATED FILLER, DOUBLER AND TRIPLER IAW AS ELEVEN INC SDR ARWA20030317Cargo Track · corrodedDURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; MAIN CARGO COMPARTMENT STA 740, RBL 45, TRACK WITH CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3, CUT AWAY DAMAGED SECTION OF TRACK AND FABRICATED SPLICES IAW DSDR ARWA20030316Pressure Panel · crackedDURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; LT MAIN LANDING GEAR W/W UPPER SURFACE WITH 0.750 INCH CRACK, STA 934. DRILLED A STOP HOLE AT END OF CRACK IAW DC8 SRM 53-2-0, FABRICATED DOUBLER IAW DC8 SRM 53-2-0, PRIMED DOUBLER IAW DC8 SRM 51-1-8 AND INST
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