N805DH
Service difficulty reports not matched to an aircraft · 760
They name N805DH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N805DH' AND registry_match IS NULL 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 = 'N805DH' AND registry_match IS NULL 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 DHLA201100516Battery Pack · inoperativeDURING PDC CK FOUND EMERGENCY LIGHTS INOPERATIVE. ACFT WAS GROUNDED. R & R EMER LIGHTS BATTERY PACK IAW MMS 33-50-10. OPS-CK-GOOD.SDR DHLA201100048Skin · crackedLT OTBD AIL LWR NOSE PLATING CRACKED 1" STA XA 734.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0, PG 1, SRM 57-8-1, FIG 4. REMOVED DAMAGED NOSE PLATING IAW SRM 57-1-0, PG 1, SRM 51-1-21. FABRICATED NEW NOSE PLATING IAW SRM 57-8-1, FIG 4, ITEM "H". CLEANED, TRESDR DHLA201100501Skin · corrodedRUDDER LT SIDE.- SKIN CORRODED (STA ZR 150.000 - 178.000). CA-PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0, FIG 6. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0 PG 1, SSDR DHLA201100046Skin · corrodedRUDDER LT SIDE.- SKIN CORRODED STA ZR 115.000 - 150.000 GALVANIC CORROSION. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0, FIG. 6. REMOVED CORRODED PANEL PLATING IAW SRMSDR DHLA201100510Rib · crackedRT LWR SLOT DOOR NR 3 RIB CRACKED. REMOVED CRACKED RIB IAW SRM 51-1-21. CLEANED, TREATED & PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21.SDR DHLA201100507Rib · crackedLT LWR SLOT DOOR, NR 3 RIB CRACKED. REMOVED CRACKED RIB IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21. REINSTALLED LT LWR SLOT DOOR IAW MM 27-80-2, PG 203-204.SDR DHLA201100050Rib · crackedRT WING L/E- INBD LWR SLOT DOOR NR 4 RIB CRACKED. REMOVED CRACKED NR 4 DOOR RIB IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21.SDR DHLA201100047Longeron Splice · crackedAFT FUS- L17L SPLICE FITTING CRACKED .2500" STA 1766.000. PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-21, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-11SDR DHLA201100504Crank Assy · crackedRT OTBD SLOT CRANK CRACKED. REMOVED CRACKED RT OTBD SLOT CRANK IAW MM 27-80-2, PG 201. INSTALLED NEW RT OTBD SLOT CRANK AND REINSTALLED RT OTBD SLOT IAW MM 27-37-6, PG 1-2, MM 27-80-2, PG 201-203, SRM 51-1-21.SDR DHLA201100054Stiffener · crackedRUDDER L/E STIFFENER CRACKED 2" STA ZR 105.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-3-0. FABRICATED STIFFENER IAW SRM 55-6-1 PG 4. HEAT TREATED STIFFENER FROM 2024"0" TO 2024T4 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED AREA & STIFFESDR DHLA201100508Rib · crackedLT WING L/E -FORMER "L" ANGLE CRACKED 4" STA, XFS-23.750. REMOVED CRACKED FORMER IAW SRM 51-3-0 CLEANED TREATED & PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW FORMER IAW SRM 51-3-0, SRM 51-3-1.SDR DHLA201100502Skin · corrodedRT RUDDER EXT SKIN CORRODED, STA ZR 140.750 (GALVANIC CORROSION). PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1 REMOVED COROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 FIG. 6. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21SDR DHLA201100053Skin · corrodedRT RUDDER EXT SKIN CORRODED STA ZR 168.656. PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED LEVEL II CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 FIG 6. REMOVED CORRODED PANEL PLATING IAW SRM 55-1-0, PG 1, SRM 51-1-21. FABRICASDR DHLA201100045Support Angle · crackedRT NOSE WHEEL TUNNEL- SUPPORT ANGLE CRACKED STA -50.000. REMOVED SUPPORT ANGLE IAW SRM 51-3-0. FABRICATED SUPPORT ANGLE (AL2024T3 0.040") IAW SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED SUPPORT ANGLE IAW SRM 51-1-8B. INSTALLED SUPPORT ANGLE IAW SRM 51-3-0 WSDR DHLA201100043Doubler · crackedRT INBD FLAP.- FLAP JOINT RIB ANGLE DOUBLER SHOWS (2EA) CRACKS 1" AND .5". REMOVED CRACKED ANGLE DOUBLER IAW SRM 51-1-21. FABRICATED NEW ANGLE DOUBLER (AL2024T3 0.063") IAW SRM 57-2-0 FIG. 2, SHEET 2, SRM 51-9-0 FIG. 68A. CLEANED, TREATED AND PRIMED AREA + ANGSDR DHLA201100506Tab · delaminatedRUDDER TAB DELAMINATED 1", STA ZRT 108.000 LT. CUT OUT DAMAGED AREA IAW SRM 55-2-2 PG 6-4. FABRICATED DOUBLER (AL2024T3 0.016") IAW SRM 55-6-1 PG 8. CLEANED + BONDED DOUBLER IAW SRM 51-1-9 PAR 1, 2, 3, 4. PERFORMED WEIGHT & BALANCE IAW SRM 51-4-7 PG 1-2.SDR DHLA201100503Tab · delaminatedLT ELEV CONTROL TAB DELAMINATED 2" STA XET 35.000. CUT OUT DAMAGED SKIN AREA IAW SRM 55-2-2, PAR 6. FABRICATED DOUBLER (2024T3 0.012") IAW SRM 55-4-0 PG 10. CLEANED AND BONDED DOUBLER IAW SRM 51-1-9, PAR 1-3, TR 51-142. CLEANED AND PAINTED IAW SRM 51-1-8B. PESDR DHLA201100051Skin · delaminatedNR 5 RT SPOILER DELAMINATED 4". CUT OUT DAMAGED AREA IAW SRM 57-2-3, PAR 23. FABRICATED DOUBLER & CORE IAW SRM 57-7-1, PG 15. CLEANED AND BONDED DOUBLER IAW SRM 51-1-9 PAR 1,2,4, TR 51-142. REINSTALLED NR 5 RT SPOILER IAW MM 27-61-1, PG 204-206.SDR DHLA201100042Skin · wornNR 4 ENG INLET NACELLE COWL UPPER SKIN WORN STA, YN 147.000 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2, FIG 2, SHEET 1,2,3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED AREA & FABRICATED SKIN & SPLICE IAW SRM 71-5-2 FIG 2, SHEET 1,2,3. HSDR DHLA201100512Fitting · corrodedLEFT MLG WW PRESSURE PANEL AFT SIDE FITTING SHOWS INTERGRANULAR CORROSION AT BS 857.000. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED ARSDR DHLA201100052Hinge Fitting · wornVERTICAL STABILIZER REAR SPAR NR 1 HINGE FITTING SHOWS WEAR. STA ZR 103.000. PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1. REMOVED FITTING IAW M 20-16-0 PG 201-207. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. NDT INSPECTED NEW FITTING IAW NDT SPM PART 06-SDR DHLA201100044Frame · wornNR 2 ENG HALF THRUST REVERSER STRUCTURAL FWD FRAME SHOWS EXISTING WEAR DAMAGE STA YN 202.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-22-11, EVA D878-00401 REV IR DATED 04-06-11. REMOVED FASTENERS SRM 51-1-20D. CUT OUT DAMAGED AREA & FABRICATED NESDR DHLA201100509Skin · delaminatedLT WING T/E LOWER PANEL EXT SKIN DELAMINATED STA XF 339.000- 409.000. R & R LT WING T/E LOWER PANEL IAW SRM 51-3-0, 51-3-1.SDR DHLA201100505Door Frame · misrepairedREPAIR LOCATED ON C4 DOOR FRAME STA 1440.000, L 30R TO L 32R DOES NOT CONFORM , REMOVED REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED FILLER, DOUBLER, & TRIPLER IAW DWG ES D85300402-001-D, REV IR DATED 04-13-11. NDT INSPECTED CUT OUT AREA. NO CRACKS SDR DHLA201100511Skin · misrepairedSKIN MISREPAIRED. PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 05-04-11, EVA D853-00403, REV IR DATED 04-11-11. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA, FABRICATED INTERNAL FILLER, EXTERNAL FILLER, INTERNAL DOUBLER, EXTERSDR DHLA201100002Skin · crackedFUSELAGE SKIN CRACKED BETWEEN 2 FASTENERS AT FS 24.5, BETWEEN LONGERONS 31R AND 32R. ACCOMPLISHED FUSELAGE SKIN DOUBLER AND FILLER REPAIR IAW EVA D853-00398, REV IR, DWG NR D85300398-001-D REV IR, AND SRM CHAPTERS 51 & 53. FS 19.811 TO FS 42.5, LONGERON 31R SDR DHLA201000105Pan · crackedINNER PAN AT AIR START DOOR ACCESS IS DAMAGED FS. -156.000. R & R DAMAGED INNER PAN AT AIR START ACCESS DOOR IAW SRM 51-1-21 AND DWG ED-4985 DTD 09/05/09 AND IAW ASTAR EVA D853-00376 DTD 09/21/2010.SDR DHLA201000065Skin · corrodedFUSELAGE SKIN CORRODED AT FS 1281.0 AND 1260, LONGERON 36, BL 0. CUT OUT CORRODED AREAS OF SKIN THAT EXCEEDED DAMAGE LIMITATIONS. FABRICATED 2EA REPAIR FILLERS AND 1EA REPAIR DOUBLER AND INSTALLED IAW SRM 53-2-1, FIG 7, SHEETS 11, 13, 23 & 24. THIS IS A CLASDR DHLA201000016Skin · damagedACCOMPLISHED PERMANENT MAJOR REPAIR AT WING STA XFS 392.5, IAW EVA 857-00329 REV 1 AND DWG NR D85700329-001-D REV "A" APPROVED BY 8110-3 SIGNED DERT-510080-CE DTD 5-7-10. TRAX W/O 9269, N/R 005717 FOR DETAILS. ACFT WAS GROUNDED.SDR DHLA201000007Door · gougedRT OTBD WING SLOT DOOR HAS A DEEP GOUGE IN OUTER PLATING LOWER SURFACE APPROX AT WS XS 493.0. ACCOMPLISHED EXTERNAL DOUBLER REPAIR TO PN 5769946-502 SLOT DOOR IN AFFECTED AREA IAW EVA D857-00321 REV IR AND SRM 57-2-0, FIG 2A TR 57-84. REFERENCE ASSOCIATED FASDR DHLA200900053A/C Pack · odorCHEMICAL OIL ODOR COMMING FROM LT PACK. RAN LT PACK, SUSPECT WAS FROZE UP PACK. OPS CK GOOD NO DEFECT NOTED IAW MM 36-10-0.SDR 2009F00101Skin · misrepairedREMOVE EXTERNAL REPAIR DOUBLER AT FUSELAGE STATION 1750 LONGERON 34L AND REPLACE WITH REPAIR IAW APPROVED DATA. INDICATE TYPE OF REPAIR AND REINSPECTION INTERVAL IF KNOWN (MAJOR REPAIR). REMOVED EXISTING DOUBLER REPAIR, CUT OUT DAMAGED AREA AND FABRICATED RESDR 2009FA0000946Skin · damagedREMOVE EXTERNAL REPAIR AT LT MAIN LANDING GEAR DOOR CUT OUT (CRACKS IN INBD FWD CORNER) AND REPLACE WITH REPAIR IAW APPROVED DATA. INDICATE TYPE OF REPAIR AND REINSPECTION INTERVAL IF KNOWN (MAJOR REPAIR). REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER ASDR DHLA20098051Door Frame · crackedFWD SVC DOOR FWD UPPER JAMB CORNER CRACKED 1/4 INCH. C/A INSTALLED DOUBLER REPAIR IAW DWG SR08530021, SRM 53-4-1 FIG 9 ITEM D, AND AD-2000-20-08 S/BDC8-53-075.SDR DHLA20098054Door Frame · crackedMAIN CARGO DOOR LWR. JAMB CRACKED 1/2 INCH STA. 200.000 L-21L TO 22L. REF N/R 229834: CUT OUT DAMAGED SECTION AND INSTALLED REPAIR IAW DWG ED-4987 AND SRM 51-1-11,SRM 51-1-21, SRM51-1-20D,SRM 51-3-1.SDR DHLA20098053Doubler · damagedAPPEARS THAT AIRSTART NOZZLE IS HITTING HARD ON INTERNAL DOUBLER FLANGE AT STA 156.000. REMOVED EXISTING REPAIR AND REWORK. REMOVED AND REPLACED DOUBLER IAW NR D853-00271 REV IR DATED 09-09-09, DWG ED-4985 DATED 9-05-09 AND SRM 51-1-1 PG 1,13,17.SDR DHLA20098052Longeron · damagedFUSELAGE STA 1749 LONGERON HAS RT EXISTING REPAIR IN POOR CONDITION. REM AND REP WITH PERMANENT TYPE REPAIR IAW APPROVED DATA. INDICATS REINSPECTION INTERVAL IF REQUIRED. REMOVED EXISTING REPAIR AND INSTALLED FABRICATED REPAIR DOUBLER IAW SRM 53-2-1, FIG 7 SDR 2009F00103Door Frame · damagedFUSELAGE STATION 1660 LONGERON 15 RT. REMOVE AND REPLACE THIS REPAIR AT R-2 AFT DOOR JAMB WITH REPAIR IAW APPROVED DATA. INDICATE REINSPECTION INTERVAL IF REQUIRED. (MAJOR REPAIR)SDR 2009F00102Tab · delaminatedRT ELEVATOR GEARED TAB IS DELAMINATED.SDR DHLA2009805303Skin · cracked1 1/8 INCH CRACK ON FUSELAGE TAIL SECTION RT SIDE AT STA.1746.00,SR17R-S18R.SDR DHLA2009805302Link · crackedRIGHT WING AT STATION XW97 FLAP DRIVE LINK ASSY HAVE CRACK AT ACTUATOR HOOK UP END.SDR DHL200800093Connector · malfunctionedFIRE WARNING LIGHT ON AND FIRE BELL RINGING NR 3 ENG. SWITCHED TO B LOOP LIGHT AND BELL WENT OUT. DEFERRED NR 3 ENG A LOOP PER EML 26-2-3 CAT C PLACARD ISN`T DMI 33371. A/C WAS GROUNDED FLIGHT 445. P/N CHANGED CONNECTOR 878238-02.SDR DHL2008805532Fitting · crackedCENTER WING REAR SPAR UPPER CAP FITTING CRACKED STA 857.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D AND SRM 51-3-1 (TORQUE).SDR DHL2008805533Stiffener · corrodedRT MLG W/W STIFFENER CORRODED AT STA 857.000. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18 AND FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED ANGLE IAW SRM 51-1-20D, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLSDR DHL2008805506Skin · damagedLT WING INBD L/E LWR SURFACE HAS ELONGATED HOLES AT STA XILD 42. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-24-08, EVA D853-00046, DWG AF12-57-101 REV IR DATED 02-22-08. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTION IAW DWGSDR DHL2008805537Cargo Track · wornUPPER CARGO COMPT NR 7 TRACK LUG WORN (STA 290.000 - 340.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-3 PG 49-50. REMOVED TRACK DAMAGED SEGMENT IAW SRM 53-2-3. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM SDR DHL2008805536Cargo Track · wornUPPER CARGO COMPT NR 3 TRACK LUG WORN (STA 590.000 - 620.000) MAJOR REPAIR. CUT OUT TRACK SEGMENT AND FABRICATED (3EA) SPLICES (AL7075T6 0.100", 0.125" AND 0.160") IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. SDR DHL2008805534Rib · wornLT MLG W/W DOOR UPLATCH RAIL RIB WORN AT STA 890.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00840-001D, DWG DOUGLAS NR 5653490. REMOVED WORN RIB IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLEDSDR DHL2008805502Angle · corrodedCORROSION AT RT VERT STAB TO FUSELAGE JOINT LWR ANGLE, STA 1800.000 L-2R - L-3R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 16A SHEET 1, 2. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SSDR DHL2008805511Flap · damagedRT OUTBD FLAP L/E PLATING HOLES ELONGATED (STA XF 325.000 - 243.000). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-12-08, ASTAR EVA D857-00049 REV IR DATED 03-12-08, SEMAN DWG NR ED-4719 DATED 02-25-08. PERFORMED NDT INSP OF DAMAGED AREA IAW DC8 NDT S
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