N801DH, cancelled Sep 26, 2017
Service difficulty reports · 758
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 = 'N801DH' AND deregistration_id = 'N801DH-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 = 'N801DH' AND deregistration_id = 'N801DH-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 DHLA20120519801Skin · corrodedPOSSIBLE CORROSION FOUND AT FS 102 AND LONGERON 36.SDR DHLA201000152Access Door · corrodedACCESS DOOR HAS CORROSION AT FUSELAGE STA FS 650.000 L32R - L36. PERFORMED MAJOR REPAIR IAW ASTAR EC-02354-001 AND DWG 5800471 AND WO 9735. REMOVED CORRODED ACCESS DOOR IAW DPS 3.67 AND SRM 51-3-0. REMOVED CORROSION IAW SRM 51-1-8. FOUND OUT OF LIMITS IAWSDR DHLA201000150Skin · damagedINSPECTED EXISTING REPAIR LOCATED AT FS 1890.000, L36 FOR CONDITION, SECURITY AND CONFORMITY. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 12-09-10 AND EVA D853-00384 REV "IR" DATED 11-18-10. REMOVED EXISTING REPAIR IAW SRM 51-1-21. TRIMMED OUT DAMAGED ASDR DHLA201000151Spar Cap · crackedNR 1 ALT TANK FRONT SPAR LWR CAP SPLICE CRACKED 1" STA XFS 532.000 S-64 PERFORMED MAJOR REPAIR IAW EC-02340-001, WO 9735, MESSAGE SEU-SEU-10-0074-028, DATED 11-17-10. REMOVED CRACKED SPLICE FITTING IAW JC EC-02340-001, MESSAGE SEU-10-0074-028 AND DWG 3644046.SDR DHLA201000133Finger Doubler · corrodedMAIN CARGO COMPT- FINGER DOUBLER CORRODED, STA 879.000 RB 1. 65" REMOVED CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0, PG 2P. REMOVED FINGER DOUBLER IAW SRM 51-1-21, FABRICATED FINGER DOUBLER (AL7075T6 0.050") IAW SRM 53-7-3 FIG 4, SDR DHLA201000148Skin · corrodedFUSELAGE EXTERNAL SKIN CORRODED, STA 1690.000 L28L AND CRACKED .5" ALSO PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9, DATED 11-19-10, AD2008-06-23, S/B 53A080, EVA D853-00383, REV IR DATED 11-18-10. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. REMOVED CORRSDR DHLA201000145Rib · crackedLT INBD FLAP.- RIB CRACKED AND WITH IMPROPER REPAIR, STA XW 125.000. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 2, SHEET 4, ITEM "Q". REMOVED DAMAGED RIB IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA + NEW RIB IASDR DHLA2010000149Frame · wornNR2 ENG LT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 202.000, BETWEEN 7 AND 8 O'CLOCK POS. C/A PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-29-10, EVA D878-00380, REV IR DATED 11-09-10. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGEDSDR DHLA201000147Frame · wornNR1 ENG LT T/R STRUCTURE FWD FRAME HAS EXISTING WEAR DAMAGE AT STA YN 202.000, BETWEEN 7 AND 8 O'CLOCK PERFORMED MAJOR REPAIR IAW FAA, FORM 8110-3, DATED 11-29-10, EVA D878-00382 REV IR DATED 11-09-10. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED AREA. FSDR DHLA201000146Vane · delaminatedNR 2 RT FLAP VANE DELAMINATED. R & R NEW FLAP VANE NR2 RT IAW MM 27-51-14, PG 201-203. REFER TO NR 239348 FOR OPS CHECK.SDR DHLA201000012Battery Pack · inoperativeEMERGENCY LIGHTING SYS WOULD NOT OPERATE DURING PREFLIGHT TEST. R & R BATTERY EMERGENCY RACK ASSY CHECK OPS GOOD IAW MM 33-11-0. ACFT WAS GROUNDED.SDR DHLA201000009Skin · corrodedFUSELAGE SKIN CORRODED AT FS 25.25 AND LONGERON 33R . ACCOMPLISHED MAJOR REPAIR TO FUSE SKIN, FS 24.0 TO 70.0, L33R TO L36R IAW EVA D853-00327 & DWG D85300327-001-D. SEE NR 00007 FOR REPAIR DETAILS. REV IR DATED 4/8/10, DWG NO D85300327-001-D REV IR DATED 4/1SDR DHLA201000001Battery Pack · dischargedEMERGENCY LIGHTING DIM DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY. OPS CHECK OK IAW MM 33-50-00 & 33-50-1. ACFT WAS GROUNDED.SDR DHLA2009801004Heat Exchanger · crackedFROM N/R 235627- N/R 236921 REF LT PRIMARY HEAT EXCHANGER AFT LOWER CORNER CRACKED 3/4", STA 12. WHILE PERFORMING INSPECTION OF THIS COMPLETED ITEM, QC REP NOTED 1 IN PROCESS INSPECTION NDT C/W 2 HI-LOCKS NOT TORQUED OR WITNESSED BY Q.C + 3 HI LOCK PULLED ON SDR DHLA2009801006Angle · corrodedLT MLG WW ANGLE CORRODED, STA XCW 46.000 (NEAR REAR SPAR UPPER PART) PERFORMED MAJOR REPAIR IAW BOEING MSG NR SEU XXX-09-0024-02B DATED 04-20-09, SRM 57-1-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG.16. REMOVED CSDR DHLA2009801008Skin · corrodedNR 4 STUB WING UPPER EXTERNAL SKIN CORRODED, STA.XFS 530.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3,09191 DATED 04-30-09, EVA DB57-00258 REV IR DATED 04-22-09, DWG ED9935 DATED 04-16-09. REMOVED FASTENERS IAW SRM 51-3-0, SRM 51-1-21, SRM 51-1-700. REMOSDR DHLA2009801010Skin · damagedRT WING CTR L/E REPAIR DOUBLER HOLES ELONGATED, STA X0LDO 67.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 09175 DATED 04-28-09, EVA DE53-00257 REV IR DATED 04-21-09, DWG ED 4934 DATED 04-15-09. REMOVED DAMAGED REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-2SDR DHLA2009801005Spar Cap · crackedLT LWR WING FRONT SPAR CAP AT L/E ATTACH HOLE SHOWS A 0.500 INCH LENGTH CRACK, STA XFE 523.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 05-7-09, EVA D857-00261 REV IA DATED 04-27-09, REPAIR SKETCH 200904200125 DWG J060232, JCT04316 REMSDR DHLA2009801003Heat Exchanger · crackedLT PRIMARY HEAT EXCHANGER AFT LWR CORNER CRACKED 3/7 INCH STA-12.000 L-27L TO 28L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 09181 DATED 04-29-09 EVD DB53-00256 REV IR DATED 04-21-09 SEMAN DWG NR ED-4933 DATED 04-13-09. REMOVED FASTENERS IAW SRM 51-1-21SDR DHLA2009801013Skin · misrepairedLT INBD FLAP UPPER SKIN REPAIR IMPROPER, STA XW 106.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1 PG 2. REMOVED PLATING WITH IMPROPER REPAIR IAW SRM 57-1-0 PG 1, SRM 51-1-2. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG 1 PG 2 ITEM D. CLEANEDSDR DHLA2009801012Skin · delaminatedNR 3 RT SPOILER PANEL EXTERNAL SKIN DELAMINATED (STA XRS 162.000 - 230.000). CUT OUT DELAMINATED AREA IAW SRM 57-2-3 PG 33 FIG 4D PAR 23. FABRICATED REPAIR PLUG AND CORE IAW SRM 57-1-1 PG 15,SRM 57-2-3 PAR.23.6,SRM 57-2-0 PAR. 4. PERFORMED CLEANING IAW SRMSDR DHLA2009801011Cargo Track · wornUPPER CARGO COMPARTMENT NR 5 TRACK SEGMENT LUGS WORN STA 1680.000-1700.000. MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-3 FIG. 14 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 TRASDR DHLA2009801009Vane · delaminatedNR 3 LT FLAP VANE INTERNAL SKIN DELAMINATED (STA XF 160.000 - 213.000). REMOVED AND REPLACED NR 3 FLAP VANE IAW MM 27-51-14 PG 201-203.SDR DHLA2009801002Skin · delaminatedRT WING, PANEL NR 577A EXTERNAL SKIN DELAMINATED. REMOVED AND REPLACED WING PANEL NR 577A IAW SRM 51-3-0, SRM 51-3-1.SDR DHLA2009801001Skin · delaminatedLT WING PANEL EXT SKIN DELAMINATED (STA XW 0 - XW 37.000). REMOVED AND REPLACED DELAMINATED LT WING PANEL IAW SRM 51-3-0 SRM 51-3-1.SDR DHLA2009801007Doubler · brokenFUSELAGE NOSE SECTION, INTERNAL DOUBLER BROKEN AT STA 156.00, L-36 (REF ACCESS NR 2). MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 09218 DATED 05-11-09, EVA DB53-00259 REV IR DATED 04-22-09, SEMAN DWG ED 4932 DATED 04-14-09. CUT DAMAGED SECTISDR DHLA200800099Battery · dischargedEMERG LTS BATTERY DISCHARGED REPLACED BATTERY PACK FOR EMER LTS PER MM 33-50-01 CHECKS SERV. N/A FLT NR. ACFT WAS GROUNDEDSDR DHLA200800098Battery Pack · dischargedEMERG LTS BATTERY DISCHARGED. REPLACED BATTERY PACK FOR EMER LTS PER MM 33-50-01 CHECKS SERV. NO FLT NR. ACFT WAS GROUNDED.SDR DHLA200700070Engine · shutdownIN CRUISE FL 360 FELT A/C SHUDDER AND VIBRATION FOUND NR 3 ENGINE SPOOLING DOWN ATTEMPTED RELIGHT EGT 565 ENGINE N1 WOULD NOT ACCELERATE N2 MAX 70. VIBRATION NOTED DURING DECELERATION AND ADVANCE OF THRUST LEVER PRECAUTIONARY SHUTDOWN ACCOMPLISHED A WINDMILLISDR DHL2007801540Spar Cap · crackedLT LWR WING FRONT SPAR CAP CRACKED 1.250" APPROXIMATELY AT STA XFS 520.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 11-20-07, BOEING MSG NR 1-653039342-4 DATED 10-22-07, BOEING SKETCH JO060232, JCT04316, EVA D857-00022 REV IR DATED 10-SDR DHL2007801541Skin · corrodedAFT CARGO COMPT SKIN CORRODED STA 1200.000 L-36 TO L-35L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-15-07, EVA D853-00021 REV "B" DATED 11-15-07. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. SDR DHL2007801539Skin · crackedNR 4 ENG NACELLE INLET COWL LT EXTERNAL SKIN CRACKED 1" STA YN 132.000 AT 9 O'CLOCK POS. (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-16-07, EVA B271-00015 REV IR DATED 10-12-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-21A, CUT OUTSDR DHL2007801533Skin · damagedITEM REF. NR. 101138: UPPER RUDDER T/E BROKEN AT STA ZR 335.250 (FIBERGLASS) DAMAGE CAUSED BY SEMAN. STAGGERED CUT BACK BY A/2" TO A INCH PER PLY FROM THE CRACK THROUGH ALL DAMAGED PLIES OF THE CLOTH IAW SRM 51-1-19 PG 3. REPLACED THE CUT OUT CLOTH WITH A NESDR DHL2007801526Skin · delaminatedRT WING LWR T/E PANEL INTERNAL/EXTERNAL SKIN DELAMINATED (STA XF 409.000 - XRS 456.000). REMOVED AND REPLACED RT WING T/E LWR PANEL (STA XF 409.000 - XRS 456.000) IAW SRM 51-3-0, SRM 51-3-1.SDR DHL2007801538Skin · crackedLT WING MAIN TANK NR 1 LWR SIDE CRACKED 1" STA XRS 84.000 S-59. PERFORMED MAJOR REPAIR IAW MSG NR 1-654248500-2 DATED 10-19-07, SRM 57-2-2 FIG 3D SHEET 1, 2, 3, TR NR 57-86 DATED 05-15-01. REMOVED EXISTING CLIPS AND CUT OUT DAMAGED STRINGER SEGMENT IAW MSG NSDR DHL2007801535Frame · crackedMAIN CARGO COMPT FRAME SEGMENT CRACKED 5" STA 240.000 L20R TO L21R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 2.6. REMOVED DAMAGED FRAME SEGMENT, SPLICES AND EXISTING ANGLES IAW SRM 51-1-20D. FABRICATED NEW FRAME SEGMENT P/N S2537716 IAW SRM 53-2-0SDR DHL2007801536Skin · corrodedAFT ACCY COMPT SKIN CORRODED STA 1690.000 - 1700.000 L-30L TO L-32R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-13-07, ENGINEERING VARIATION AUTHORIZATION NR D853-00024 REV IR DATED 11-06-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. REMOVEDSDR DHL2007801534Structure · damagedINSPECT REPAIR AT FUSELAGE STA 280 LONGERON 29R PER INSPECTION REQUIREMENTS OF DC8 SRM 53-2-1 CLASS II TYPE REPAIR. REPAIR ACCOMPLISHED AUG 94. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-12-07, ENGINEERING VARIATION AUTHORIZATION NR D853-00023 REVSDR DHL2007801528Structure · damagedLT INNER WING OUTBD EXTENDED LEADING EDGE SLOT LWR PLATING ELONGATED HOLES AT STA XILD 42.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 11-12-07, ENGINEERING VARIATION AUTHORIZATION NR D857-00020 REV IR DATED 10-20-07. REMOVED FASTENERSSDR DHL2007801523Skin · crackedLT RUDDER SKIN CRACKED 5" AT STA ZR 335.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21, SRM 51-1-21A. FABRICATED PLATING AND BONDED DOUBLER BOTH FROM AL 2024T3 0.016" IAW SRSDR DHL2007801522Skin · deformedRT RUDDER SKIN DEFORMED AT STA ZR 335.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1 PG 2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21, SRM 51-1-21A. FABRICATED PLATING AND BONDED DOUBLER BOTH FROM IAW SRM 55-6-1 FIG 1 PG 2SDR DHL2007801532Skin · damagedRUDDER TIP SKIN BROKEN AT STA ZR 335.250 (DAMAGE CAUSED BY SEMAN). REMOVED BROKEN TIP IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TIP IAW SRM 51-1-21A. REFER TO JC EC-00592-001 (WO 2624) FOR FABRICATION AND NR 101137 FOSDR DHL2007801520Skin · wornNR 1 ENG NACELLE INLET COWL UPPER SKIN WORN STA YN 150.000 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION. FABRICATED NEW SKIN (AL2024T3 0.080") AND SPLICSDR DHL2007801521Skin · wornNR 2 ENG NACELLE INLET COWL UPPER SKIN WORN AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN (AL2024T3 0.080") AND SPLICE (STEEL TYPSDR DHL2007801529Fitting · crackedMAIN CARGO COMPT SERVICE DOOR JAMB FITTING CRACKED 1" AT STA 1118.528 L11R. 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, SRM 51-3-0, SRM 51-3-1.SDR DHL2007801512Skin · delaminatedRT WING ACCESS DOOR NR 577B INTERNAL SKIN DELAMINATED (STA XA 650.000 - 670.000). REMOVED AND REPLACED DOOR ASSY IAW SRM 51-3-0, SRM 51-3-1.SDR DHL2007801524Support · crackedNR 7 LT AILERON HINGE SUPPORT CRACKED. REMOVED AND REPLACED NR 7 LT AIL HINGE SUPPORT IAW MM 20-16-0 PG 201-207, OHM 27-2-3A. REFER TO NR 130478 FOR OPS CHECK AND NR 130141 FOR LT OUTBD AIL REMOVAL/REINSTALLATION.SDR DHL2007801510Skin · delaminatedLT WING UPPER PANEL EXTERNAL SKIN DELAMINATED (STA XW 0 - 33.000). REMOVED AND REPLACED LT WING UPPER PANEL ASSY IAW SRM 51-3-0, SRM 51-3-1.SDR DHL2007801513Fitting · crackedLT WING CTR L/E UPPER INTERNAL SPLICE FITTING CRACKED 3" AT STA XOLDI 6.2246. REMOVED SPLICE FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-21, SRM 51-1-20DSDR DHL2007801515Skin · damagedINSPECT REPAIR AT FUSELAGE STA 490 L-23R PER INSPECTION REQUIREMENTS OF DC8 SRM 53-2-1 CLASS II TYPE REPAIR. REPAIR ACCOMPLISHED AT AIR CANADA AUG 94. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 2. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21.
Back to N801DH, cancelled Sep 26, 2017