N804DH, cancelled Sep 26, 2017
Service difficulty reports · 656
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 = 'N804DH' AND deregistration_id = 'N804DH-2017-09-26' 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 = 'N804DH' AND deregistration_id = 'N804DH-2017-09-26' 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 DHLA201100537Skin · corrodedLOWER FUSELAGE HAS CRACK IN SKIN AT STA 100 AT LONGERON 35 & 36R. CRACK IS PROBABLY INDUCED BY CORROSION. COMPLIED WITH STEPS 1-11 OF EVA D853-00412. FABRICATED FILLER, DOUBLER AND INSTALLED REPAIR. MAJOR REPAIRSDR DHLA2011F00187Skin · crackedWHILE COMPLYING WITH VISUAL WALK AROUND INSP, A CRACK WAS FOUND IN THE LOWER FUSELAGE SKIN AT STA 100.5. UPON FURTHER INVESTIGATION THE CAUSE OF THE CRACK WAS CORROSION. THE CRACK WAS ADJACENT TO ANOTHER REPAIR WHICH WAS REMOVED AND THE NEW REPAIR INCOORPERASDR DHLA201000139Wire · brokenCLIMBING OUT OF 2000 FT AFE ENG NR 4 FIRE INDICATION. COMPLETED PHASE I'S AND ENG FIRE CHECKLIST FIRED BOTH BOTTLES. EMERGENCY WAS DECLARED. AIR TURN, ACFT WAS GROUNDED. INSPECTED NR4 ENGINE AND FOUND NO EVIDENCE OF FIRE IAW MM71-00-00. R & R NR3 AND NR4 FIRSDR DHLA201000130Skin · damagedEXISTING REPAIR LOCATED ON LOWER BELLY AT FS 1400.000 L36 IN POOR CONDITION. R & R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-04-10, EVA D853-00378 REV IR DATED 09-22-10. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA ANDSDR DHLA201000120Skin · damagedEXISTING REPAIR LOCATED ON LWR BELLY AT FS 1400.000 L36 IN POOR CONDITION. R & R PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 10-04-10, EVA D853-00378 REV IR DATED 09-22-10. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA + FASDR DHLA201000129Intercostal · crackedNOSE SECTION.- INTERCOSTAL CRACKED 1" APPROX, STA - 2.000 L-30 - 33RT. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0 CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B PERFORMED STOP HOLE + FABRICATED DOUBLER (AL 2024 B 0.050") IAW SRM 53-2-0 FIG 23, SHEET 1 TR SDR DHLA201000098Intercostal · crackedNOSE SECTION.- INTERCOSTAL CRACKED 1" APPROX, STA - 2.000 L-30 - 33RT. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0 CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B PERFORMED STOP HOLE + FABRICATED DOUBLER ( AL 2024 B 0.050") IAW SRM 53-2-0 FIG 23 SHEET 1 TRSDR DHLA201000124Skin · misrepairedR & R EXISTING REPAIR ON RT RUDDER PLATING AT ZR 61.156 UTILIZING APPROVED DATA. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG. 1. REMOVED PLATING AND EXISTING NON STANDARD REPAIR IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING IAW SRM 55-6-1 FIG 1 ITEM "SDR DHLA201000115Skin · misrepairedR & R EXISTING REPAIR ON RT WING LOWER SURFACE AT XFS 566.250 UTILIZING APPROVED DATA. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 09-30-10, EVA D857-00373 REV IR DATED 09-17-10. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREASDR DHLA201000111Skin · misrepairedEXISTING REPAIR ON RT WING L/E LOWER SURFACE AT XW257.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 ATED 09-21-10, EVA D857-00367 REV IR DATED 09-14-10. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA & FABRICATED FILLER & REPAIRSDR DHLA201000107Skin · crackedR & R EXISTING REPAIR LOCATED ON RT AILERON UPPER PLATING SURFACE UTILIZING APPROVED DATA, PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 2X PAR 16D-3. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21. CUT OUT DAMAGED AREA + FABRICATED INTERNAL REPAIR DOUBLER SDR DHLA201000102Skin · misrepairedR & R EXISTING REPAIR ON RT RUDDER PLATING AT ZR 61.156 (REF REPAIR REPORT VS002) UTILIZING APPROVED DATA. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOVED PLATING AND EXISTING NON STANDARD REPAIR IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING SDR DHLA201000126Skin · deformedLEFT OTBD AILERON LOWER PLATING DEFORMED STA XA 741.000. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 4. REMOVED DEFORMED NOSE PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-3-0. FABRICATED NEW NOSE PLATING IAW SRM 57-8-1 FIG. 4 ITEM "H". CLEANED, TREATED AND PSDR DHLA201000096Skin · deformedLT OTBD AIL LWR PLATING DEFORMED STA XA 741.000 PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 4. REMOVED DEFORMED NOSE PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-3-0. FABRICATED NEW NOSE PLATING (AL2024T3 0.032") IAW SRM 57-8-1 FIG. 4 ITEM "H". CLEANED, TRESDR DHLA201000128Cargo Track · wornUPPER CARGO COMPT.-NR3 TRACK LUGS WORN (STA 1670.000 - 1702.000). PERFORMED MAJOR REPAIR IAW SRM 53-2-3, FIG 12, SHEET 1, PG 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT EXTRUSION PN S277SDR DHLA201000127Cargo Track · wornUPPER CARGO COMPT.- NR4 TRACK LUG WORN (STA 57.000 - 110.000). PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG 12, SHEET 1, PG 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT EXTRUSION PN S2772660 SDR DHLA201000114Rib · damagedREMOVE DAMAGED RIB IN RT FLAP WELL STA XW 90 AND REPAIR IAW APPROVED DATA PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 10-06-10, EVA D857-00357 REV IR DATED 09-01-10. REMOVED DAMAGED RIB & EXISTING REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED WEB SDR DHLA201000109Skin · nickedRT OTBD FLAP UPPER SKIN NICK, STA XF 227.000 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-04-10 EVA D857-00377 REV IR DATED 09-22-10. REMOVED DAMAGED PLATING AND EXISTING SPLICE IAW SRM 51-1-21, SRM 51-3-0. FABRICATED NEW PLATING SEGMENT (AL2024T3 0.071SDR DHLA201000097Seat Track · wornUPPER CARGO COMPT.- NR3 TRACK LUGS WORN STA 1670.000 - 1702.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-3, FIG 12, SHEET 1, PG 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT EXTRUSION IAW SRM SDR DHLA201000095Seat Track · wornUPPER CARGO COMPT.- NR 4 TRACK LUG WORN STA 57.000 - 110.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG. 12 SHEET 1 PG 49-50. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES IAW SRM 53-1-0 PG 1, SRM 51-3-0. FABRICATED NEW TRACK SEGMENT EXTRUSION IAW SRM 53-2-3SDR DHLA201000131Skin · corrodedFUS LWR SKIN CORRODED, STA 160.000 L-35R - L-36 PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7, SHEET 25,23,24 TR 53-203, DATED JAN 21-2008. REMOVED CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0, PG 2P. REMOVED EXISTING REPAIR NEAR CORROSDR DHLA201000118Skin · crackedRT INBD FLAP WELL.- WEB CRACKED 1" STA XF 75.000 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 10-04-10, EVA D857-00375 REV IR DATED 09-21-10. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER REPAIR STRAP IAW DWG ES-D85700375-001-D REV IR DATED 9-21-10.SDR DHLA201000110Skin · misrepairedPERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-11-10, EVA D85500374 REV IR DATED 09-28-10. REMOVED RUB PLATE IAW SRM 51-1-21. CUT OUT DAMAGED AREA + FABRICATED (3EA) FILLERS & INTERNAL REPAIR DOUBLER IAW DWG ES D85500374-001-D REV IR DATED 09-28-10. HEAT SDR DHLA201000106Skin · crackedREMOVED & REPLACED EXISTING REPAIR ON LT WING T/E AT STA XW 47.000 UTILIZING APPROVED DATA. (REF REPAIR REPORT LW011) REMOVED EXISTING REPAIR AND CUT OUT DAMAGED AREA IAW SRM 57-2-3 PAR 5. FABRICATED DOUBLER (AL7075T6 0.020") IAW SRM 57-3-3 PG 36. BONDED DOUBLSDR DHLA201000103Skin · damagedREMOVED AND REPLACED EXISTING REPAIR LOCATED ON RT HORZ STABILIZER AT XE 159.000 UTILIZING APPROVED DATA (REF REPAIR REPORT HS002) PERFORMED MAJOR REPAIR IAW SRM 55-3-1, FIG 1, SHEET 1-2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICASDR DHLA201000093Skin · corrodedFUSELAGE LOWER SKIN CORRODED STA 160.000 L-35R-L-36. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG. 7 SHEET 25,23,24 TR 53-203 DATED. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED EXISTING REPAIR NEAR CORRODED AREA SDR DHLA201000117Frame · wornNR 3 ENG LT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 203.000 (BETWEEN 6 AND 9 O'CLOCK POS) PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR10502 DATED 10-08-10, EVA D878-00368 REV IR DATED 09-15-10. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMSDR DHLA2010001416Skin · misrepairedR & R 3 EXISTING REPAIRS LOCATED ON AFT LOWER BELLY BETWEEN STA 1300-1370.000 LONGERON 36 UTILIZING APPROVED DATA. REF REPAIR REPORT F039, F040 & F041 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-05-10, EVA D853-00370 REV IR DATED 09-15-10. REMOVED EXISDR DHLA201000113Skin · delaminatedLT ELEVATOR GEARED TAB DELAMINATED. R & R LT ELEVATOR GEARED TAB IAW MM 27-30-3 PG 201-204. REFER TO NR 265752 FOR OPS CHECK.SDR DHLA201000108Frame · wornNR 2 ENG LT THRUST REVERSER STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 203.000 (BETWEEN 6 AND 9 O'CLOCK POS) PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 10486 DATED 09-29-10, EVA-D878-00372 REV IR DATED 09-16-10. CUT OUT DAMAGED AREA. FABRICATED SDR DHLA201000104Frame · wornNR 3 ENG RT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE STA YN 202.000 (BETWEEN 5 AND 6 O'CLOCK POS). PERFORMED MAJOR REPAIR IAW FORM 8110-3 NR 10471 DATED 09-22-10, EVA D878-00371 REV IR DATED 09-15-10. CUT OUT DAMAGED AREA, FABRICATED FRAME SEGMENT IASDR DHLA201000112Skin · delaminatedNR 3 LEFT SPOILER UPPER SKIN DELAMINATED R & R NR3 LT SPOILER IAW MM 27-61-1 PG 201-204. REFER TO NR 265753FOR, OPS CHECK.SDR DHLA201000125Skin · dentedRT INBD FLAP UPPER PLATING DENTED STA XW 68. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DENTED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING (AL2024T3 0.025") & BONDED DOUBLER (AL2024T3 0.020") IAW SRM 57-7-1 FIG 1 ITEM "A" & "L"SDR DHLA2010000122Skin · misrepairedINSPECT EXISTING REPAIR ON RT FUSELAGE STA FS - 17. PERFORMED MAJOR REPAIR IAW SRM 53-2-0, FIG 1 D, SHEET 3 REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21 FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG 1D, SHEET 3, SRM 53-3-3 FIG 1 ITEM "A", SRM 51-9-0 FIGSDR DHLA201000121Skin · misrepairedINSPECT EXISTING REPAIR ON FUS STA -156 FOR CONFORMITY WITH SRM, CONDITION AND SECURITY. IF REPAIR COMPLIES, NOTE DETAILS ON NON ROUTINE. IF REPAIR DOES NOT CONFORM, R & R UTILIZING APPROVED DATA. REF REPAIR REPORT (F011). STRIPPED REPAIR AREA IAW MM 51-20SDR 2010F00223Skin · damagedINSPECT EXISTING REPAIR ON FUS STA -156 FOR CONFORMITY WITH SRM, CONDITION AND SECURITY. IF REPAIR COMPLIES, NOTE DETAILS ON NON ROUTINE. IF REPAIR DOES NOT CONFORM, R & R UTILIZING APPROVED DATA. REF REPAIR REPORT (F011). STRIPPED REPAIR AREA IAW MM 51-20-0 SDR DHLA201000101Skin · dentedRT INBD FLAP UPPER PLATING DENTED STA XW 68 PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DENTED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING & BONDED DOUBLER IAW SRM 57-7-1 FIG 1, ITEM "A" & "L". BONDED BOTH PARTS WITH HYSOL IAW SDR DHLA2010000100Skin · misrepairedREMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG. 1D SHEET 3, SRM 53-3-3 FIG. 1 ITEM "A" SRM 51-9-0 FIG 68A. CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR DOUBLER IAW SRM 53-SDR DHLA201000094Skin · misrepairedPERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 1 D, SHEET 3 REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21 FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG 1D SHEET 3, SRM 53-3-3 FIG 1 ITEM "A", SRM 51-9-0 FIG 68 A CLEANED, TREATED AND PRIMED AREA & REPAIR DOUBLESDR DHLA201000071Battery Pack · inoperativeEMERGENCY LIGHT BATTERY DEAD. ACFT WAS GROUNDED. R & R EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-1, OPS CK GOOD.SDR DHLA201000068Rib · damagedON LANDING, NR8 MAIN TIRE BLEW CAUSING DAMAGE. ON POST FLIGHT INS FOUND RT WING RIB AT STA XW 90.000 DAMAGED. DEFECT RESOLUTION: REPAIRED RIB IAW EVA 085700356-001-D.SDR DHLA2010804001Skin · corrodedCORROSION CRACK DISCOVERED ON FUSELAGE EXTERIOR SKIN AT FS 120, AND LONGERON 36, EMANATING FROM FWD ADF ANTENNA. ACCOMPLISHED FUSELAGE SKIN EXTERNAL DOUBLER AND FILLER REPAIR IAW EVA D853-00319, DWG ES D853-00319-001-D, SRM, AMM, AND NDT MANUAL. REF 8110-3SDR DHLA200900055Fire Detector · false activationNR 2 ENG FIRE WARNING LIGHT AND BELL. COMPLETED ENG FIRE PHASE ONE ITEMS COMPLETED ENG FIRE CHECK LIST FIRE LIGHT OUT. INSPECTED ENG NR 2 INLET AND EXHAUST INCLUDING FAN AND CORE SECTION NO DAMAGE OR EVIDENCE OF FIRE NOTED. T/S IAW MMS 26-10-01 AND W/D 26-01SDR DHLA2009804002Skin · corrodedREFERENCE ASTAR N/R 8285-39: DURING "B" CHECK, FOUND CRACK IN FUSE SKIN AT FS 1442, BETWEEN LONGERON 35R AND 36. ACCOMPLISHED CLASS II EXTERNAL DOUBLER REPAIR FOR CORROSION REMOVAL IAW SRM 53-2-1 FIG 7 TEMP REV. 53-203, 53-2-0, AND 51-1-8. THIS IS A LIFE LISDR DHLA2000900052Bleed Valve · malfunctionedDURING CRUISE, AT 360FL, ODOR OF SMOKE IN COCKPIT. PERFORMED SMOKE SOURCE IDENTIFICATION CHECKLIST. HAD DIFFICULT TIME CONTROLLING CABIN PRESSURE IN AUTO AT ALT PRESSURE SWING 2000 FT/M UP AND DOWN EVERY 10. TRANSFERRED NR 1 ENG HP REG VALVE TO DMI NR 3567SDR DHLA200900048Pump · wornNR 4 ENG FLAMOUTED, PASSING FL350 IN CLIMB. ATTEMPTED RESTART AT FL350 UNSUCCESSFUL ATTEMPTED. ATTEMPED 2ND RESTART DURING DECENT TO CVG AT FL220. ATTEMPTED UNSECCESSFUL. OIL PRESSURE 3-5 PSI TIME OF FAILER 0430Z. LAND AT 0613. PERFORMED FAULT ISOL 51 IN MM 71SDR DHLA2008804001Skin · corrodedFUSE SKIN HAS CORROSION AT FS 100 AND BS 0. ACCOMPLISHED FUSE SKIN DOUBLER AND FILLER REPAIR IAW ASTAR EVA D853-00268 AND DWG D85300268-001-D. HFEC OF REPAIR PARTS AND DAMAGE CUT OUT AREA ON FUSELAGE ACCOMPLISHED PER STEP 6 OF LISTED EVA. NO CRACKS OR CORROSDR DHLA200900024Flashlight · inoperativeEMERGENCY FLASHLIGHT IN LAV INOP. REMOVED AND REPLACED FLASHLIGHT IAW DC-8 MMS 25-60-62, OPS CHECKS GOOD P/N 3800.SDR DHLA200800044Bulb · malfunctionedFLT NR 445, IF LIGHT OVER LIFE RAFT IN GALLEY AREA RIGHT COMP LIGHT SWITCH ILLUMINATED FOR 2 HRS THERE IS A STRONG CHEMICAL ODOR. RELAMPED IAW MM 33-13-0. OPS CHECK GOOD NO ODOR DETECTED P/N 307. A/C WAS GROUNDEDSDR DHLA200800043Light · odorFLT NR 160 WITH COMP LIGHT SWITCH ON LIGHT OVER GALLEY ON A PHOSPHOROUS ODOR WAS DETECTED WITH GALLEY POWER OFF TURNED OFF COMP LIGHT SWITCH AND ODOR DISSIPATED, NO SMOKE DETECTED. TURNED ON COMP LIGHTS INSPECTED CARGO COMP LIGHTS, NO ODOR NOTED. OPS CK GOOD
Back to N804DH, cancelled Sep 26, 2017