JASC 5101

Service difficulty reports · 482

Reports filed under 5101 · Aircraft Structures, 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 jasc_code = '5101'
  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.

SDR 06FDEA1061Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 67 TO FR 68, FS 3620 TO FS 3670, STR 47 TO STR 47 AND BELOW BULK CARGO DOOR. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FMar 14, 2006 · N426FE · Airbus A310203SDR 06FDEA1059Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 60 TO FR 60, FS 3249 TO FS 3249, STR 39 TO STR 41, AND FWD OF AFT CARGO DOOR CUTOUT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT. INSPECTION NEED EVMar 14, 2006 · N426FE · Airbus A310203SDR 06FDEA1058Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 37 TO FR 38.2, FS 2029 TO FS 2082, STR 26 TO STR 26. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICMar 14, 2006 · N426FE · Airbus A310203SDR 06FDEA1057Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 38.1 TO FR 38.2, FS 2135 TO FS 2188, STR 46 TO STR 47, ON CUTOUT OF POTABLE WATER SERVICE PANEL. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTIMar 14, 2006 · N426FE · Airbus A310203SDR 06FDEA1055Repair · noneCOMPLY WITH AGING 9-AGING-INSP. PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT HAND SIDE AT FR 16A TO 16A, FS 1260 TO FS 1285 AND 150CM BELOW R1 DOOR. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIMar 14, 2006 · N426FE · Airbus A310203SDR 06FDEA0961Repair · unknownLOWER FUSELAGE FOUND EXTERNAL DOUBLER ON RT STA 1039 TO 1059 BETWEEN LONG 40 TO 42. REMOVED AND REPLACED REPAIR IAW SRM 53-20-00 FIG 6 VOL 1, FABRICATED PARTS IAW DETAIL PARTS TRAVELER N01173 AND SRM 53-20-00 FIG 6 VOL 1.Mar 7, 2006 · N563FE · Doug DC1010SDR 06FDEA0960Doubler · unknownREPLACE FWD AND AFT UPPER MCD CUTOUT DOUBLERS. FABRICATED, ALODINED AND PRIMERED UPPER MCD CUTOUT DOUBLER PER FED EX SRM 53- 30-2, 51-30-5.Mar 7, 2006 · N485FE · Boeing 727200SDR 06FDEA0952Repair · unknownFWD CARGO COMPT THERE IS A REPAIR ON LONG BETWEEN STA 869-889. REMOVED SPLICE AT STA 889 IAW SRM 51-33-00 VOL 2. INSTALLED NEW LONG SPLICE IAW SRM 53-10-00 FIG 2 VOL 1 AND ACCOMPLISH EA 8-5310-95690.Mar 6, 2006 · N563FE · Doug DC1010SDR 06FDEA0951Repair · unknownCNT CARGO COMPT HAS A SPLICE REPAIR ON LONG 51 LT BETWEEN STA 1741 AND 1761. FITTED NEW SPLICE IAW SRM 53-10-00 FIG 2 SHT 1 VOL 1 AND EA 8-5310-95690, FAB PART IAW DETAIL PART TRAVELER N01187 AND SRM 53-10-00 VOL 1.Mar 6, 2006 · N563FE · Doug DC1010SDR 06FDEA0895Bolt · misinstalledDISCREPANCY FUSELAGE STA 275 FWD PRESSURE BULKHEAD DURING VISUAL INSP IAW EA NR 8-5310-79443B P2 FOUND INSTALLED BOLT INSTEAD OF LOCK FASTENERS. REMOVED MECH ASSY STEERING IAW MM 20-50-02-2 ACCOMPLISHED EA NR8-5310-79443B. REINSTALLED MECH AND PERFORMED TESMar 2, 2006 · N68056 · Doug DC1010SDR 06FDEA0878Repair · noneFOUND REPAIR AT STA 990 STR 27R, REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 7-5310-27778. REPAIR CLASSIFIED AS MAJOR.Feb 28, 2006 · N275FE · Boeing 727200SDR 06FDEA0877Repair · noneFOUND REPAIR LOCATED AT STA 700 STR 28L REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 7-5310-02879.Feb 28, 2006 · N275FE · Boeing 727200SDR 06FDEA0876Repair · noneFOUND REPAIR LOCATED AT STA 1130 STR 5L, REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 7-5330-56270.Feb 28, 2006 · N275FE · Boeing 727200SDR 06FDEA0875Repair · noneFOUND REPAIR LOCATED AT STA 630 STR 27L REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION, AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 5330-B27- 20619. REPAIR CLASSIFIED AS Feb 28, 2006 · N275FE · Boeing 727200SDR 06FDEA0873Repair · noneFOUND REPAIR LOCATED AT STA 400 STR 15L REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 7-5330-70501. REPAIR IS CLASSIFIED AS MAJOR.Feb 28, 2006 · N275FE · Boeing 727200SDR 06FDEA0872Repair · noneFOUND REPAIR LOCATED AT STA 380 STR 15L REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR ACCOMPLISHED USING FAA APPROVED DATA ON FEDEX EA 7-5330-70501. REPAIR IS CLASSIFIED AS MAJOR.Feb 28, 2006 · N275FE · Boeing 727200SDR 06FDEA0841Repair · unknownEXTERNAL DOUBLER REPAIR APPROX 8 X 12 INCHES. LT AFT FUSELAGE STA 1050 STRINGER 19L TO 20L. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ALL WORK ACCOMPLISHED IAW FED EX EA 7-5330-96607Feb 24, 2006 · N492FE · Boeing 727200SDR 06FDEA0837Repair · unknownEXISTING REPAIR LT SIDE NOSE SECTION STA 295-313 Z-30. REMOVED REPAIR DOUBLER IAW SRM 51-35-01 VOL 2, REMOVED SEALANT AND FR PRIMER IAW SRM 51-41-01 VOL 2. PERFORMED NDI ON INTERNAL FRAME NO CRACK FOUND. FOUND CRACK ON SKIN LONG .5 INCH AT STA 298. REMOVEDFeb 24, 2006 · N563FE · Doug DC1010SDR 06FDEA0835Repair · noneMAIN CARGO COMPT STA 989-1109 X-47.5 FOUND EXISTING SEAT TRACK SPLICE REPAIR. PERFORMED INSPECTION ON SEAT TRACK SPLICE REPAIR AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.Feb 24, 2006 · N68054 · Doug DC1010SDR 06FDEA0833Repair · unknownSTA 715 BETWEEN LONGERONS 11-13 RT FOUND FRAME REPAIR. PERFORMED EA 8-5330-95683.Feb 24, 2006 · N68054 · Doug DC1010SDR 06FDEA0832Repair · unknownSTA 735 BETWEEN LONGERONS 11-13 RT FOUND FRAME REPAIR. PERFORMED EA 8-5330-95683.Feb 24, 2006 · N68054 · Doug DC1010SDR 06FDEA0822Repair · unknownFLUSH REPAIR AT FUSELAGE SKIN FROM STA 515 TO STA 525 AT LONG 17 LT. PERFORMED INSPECTION FOUND REPAIR IN COMPLIANCE WITH CRITERIA REQUEST BY EO8- 5100-7-5001 P1 AND EA 8-5330-94664.Feb 24, 2006 · N68054 · Doug DC1010SDR 06FDEA0818Repair · unknownMAIN CABIN CTR FUSELAGE L-3 FWD DOOR JAMB HAS AN EXTERNAL DOUBLER REPAIR BOTTOM PART STA 1256 DIM 7 X 10 INCH. REMOVED AND REPLACED BOLTS WITH HLT 436-6 IAW SRM 51-33-01 PAGE 6-10 VOL 2 AND SRM 53-50-00 FIG 19 VOL 1.Feb 24, 2006 · N563FE · Doug DC1010SDR DHL2006804551Repair · misinstalledINSPECT PREVIOUS REPAIRS AT STR 36 STA 310 AND 280 TO ENSURE IT COMPLIES WITH SRM. DOCUMENT ON THIS NON ROUTINE (REFERENCE ATTACHED AIR CANADA N/R 907). IF REPAIR IS NOT IN CONFORMANCE WITH THE SRM OR IN POOR CONDITION, REWORK PER SRM OR APPROVED DATA.CORR.: VFeb 16, 2006 · N804DH · Doug DC873FSDR IXXA06SMN063SNone · noneDURING C CHECK, INSTALLATION OF DOUBLER ON FS 188.000 L-1 TO L-2R REQUIRED DUE TO SEXTANT EQUIPMENT REMOVAL. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06029 DATED 01-23-06, SEMAN DWG ED-4167 DATE 01-21-06, EO SEMAN # 2006100 DATE 01-23-06. REMOVED EXISTINFeb 16, 2006 · N722CX · Doug DC872SDR 06FDEA0642Repair · noneFOUND REPAIR LOCATED LT PAX DOOR L1. EXTERNAL DOUBLER LWR AFT CORNER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIR ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR WAS PREVIOUSLY ACCOMPLISHED RAS/AS/027/2006 REPAIR EVALUATED Feb 10, 2006 · N430FE · Airbus A310SDR 06FDEA0631Repair · unknownEXTERNAL DOUBLE REPAIR APPROX 5" BY 7" RT LWR FUSE STA 1152 TO STA 1160 STRINGER 29R. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED & REPLACED EXTERNAL DOUBLER AT STA 1060 TO STFeb 9, 2006 · N488FE · Boeing 727227SDR 06FDEA0597Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1158, STR 30 WAS DETERMINED TO BE ACCOMPLISHED IAW EO 7-2500-7-2348, ITEM 12, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERFeb 8, 2006 · N487FE · Boeing 727227SDR DHL2006804539Door · scheduled maintPERFORM PREVENTATIVE MODIFICATION TO FWD LOWER CORNER OF L1 DOOR IAW AD2000-20-08, SB DC8 53-075, SR 085300021. (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2000-20-08, SB DC8 53-075, DOUGLAS DRAWING SR08530021, 5750776. REMOVED FASTENERS IAW SRM 51-1-21. Feb 7, 2006 · N804DH · Doug DC873FSDR 06FDEA0569Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 360, STR 13L WAS DETERMINED TO BE ACCOMPLISHED IAW E.O. 7-5100-7-2307F, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAFeb 7, 2006 · N487FE · Boeing 727200SDR 06FDEA0568Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050, STR 27L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3, FIG 3, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE AND SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENEFeb 7, 2006 · N487FE · Boeing 727200SDR 06FDEA0566Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 1050, STR 27R WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE AND SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENEFeb 7, 2006 · N487FE · Boeing 727200SDR 06FDEA0565Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT FWD END OF AFT AIRSTAIRS CUTOUT WAS DETERMINED TO BE ACCOMPLISHED IAW SR27-53-024, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, Feb 7, 2006 · N487FE · Boeing 727200SDR 06FDEA0564Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT AFT CUT OUT AFT AIRSTAIRS WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 51-10-1 AND SRM 51-30-1, PARA F, BASED ON AN EXTERNAL VISUAL EVAULATION, CONSISTS OF LOCATION, SIZE AND SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER Feb 7, 2006 · N487FE · Boeing 727200SDR DHL2006804536Door · nonePERFORM PREVENTATIVE MODIFICATION TO THE AFT UPPER L1 DOOR CORNER IAW AD2000-20-08, S/B 53-075 AND DWG SR085300021. PERFORMED MAJOR REPAIR IAW AD2000-20-08, SB 53-075, DOUGLAS DRAWING SR08530021, 5750776. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED REPAIRFeb 6, 2006 · N804DH · Doug DC873FSDR 06FDEA0549Repair · unknownEXISTING DOUBLER REPAIR APPROX 11" BY 19", RT LWR FUSELAGE STA 680 TO 692 STRINGER 27R TO 28R REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED REPAIR DOUBLER PER SRM 53Feb 6, 2006 · N492FE · Boeing 727227SDR 06FDEA0523Repair · noneCOMPLY WITH AGING 9-AGING-INSP REV POS PT1. FOUND REPAIR LOCATED LT FS 1305, FR16A ON THE AFT L1 DOOR FRAME EXT DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVAFeb 3, 2006 · N430FE · Airbus A310203SDR 06FDEA0522Repair · noneCOMPLY WITH AGING 9-AGING-INSP REV POS PT1. FOUND REPAIR LOCATED LT FS 1184, FR14 ON THE FWD L1 DOOR FRAME EXT DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALFeb 3, 2006 · N430FE · Airbus A310203SDR 06FDEA0520Repair · noneCOMPLY WITH AGING 9-AGING-INSP REV POS PT1. FOUND REPAIR LOCATED RT FS 3567 - FS 3587, FR66, STR 32 - STR 33 EXT DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVFeb 3, 2006 · N430FE · Airbus A310203SDR 06FDEA0518Repair · noneCOMPLY WITH AGING 9-AGING-INSP REV POS PT1. FOUND REPAIR LOCATED RT FS 766 - FS 794, FR 1 - FR 2 EXT DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND Feb 3, 2006 · N430FE · Airbus A310203SDR DHL2006804529Repair · misinstalledNOSE SECTION FUSELAGE EXTERNAL POWER RECEPTACLE ACCESS DOOR JAMB UPPER CORNER HAS NON STANDARD REPAIR STA 30.000 STA 36.000 L-31 L-32R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-31-06 DWG AA66-53-R03 REV IR DATED 01-16-06. REMOVED EXFeb 3, 2006 · N804DH · Doug DC873FSDR 06FDEA0529Repair · misinstalledFOUND REPAIR LOCATED ON LT INBD FLAP, LT WS 134-182. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX EA 6-5710-95695 REPAIR EVALUATFeb 3, 2006 · N430FE · Airbus A310SDR 06FDEA0526Repair · misinstalledFOUND REPAIR LOCATED ON L/H INBD FLAP, LT WS128-WS176. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX E:A: 6-5710-95695 REPAIR EVALFeb 3, 2006 · N430FE · Airbus A310SDR 06FDEA0510Repair · misinstalledEXTERIOR FUSELAGE SKIN STA 740 BETWEEN L44R-L45R HAS NON-SRM REPAIR. SRM REPAIR ACCOMPLISHED ON FEDEX NR N00765. MAJOR REPAIRFeb 3, 2006 · N68050 · Doug MD1010FSDR 06FDEA0509Repair · misinstalledEXTERIOR FUSELAGE SKIN STA 760 BETWEEN L44R-L45R HAS NON-SRM REPAIR.Feb 3, 2006 · N68050 · Doug MD1010FSDR 06FDEA0508Repair · unknownSKIN REPAIR DOUBLER, 15" X 10" LOCATED AT BS 367-378, STR 27L, REQUIRES EVALUATION TO DETERMINE IF THE REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA. REINSTALLED PER E.O. 7-3450-7-3393Feb 2, 2006 · N485FE · Boeing 727200SDR 06FDEA0499Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT FS 500 STR.30 WAS ACCOMPLISHED IAW SRM 53-30- 3, FIG. 24 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION OF THE REPAIR, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE, THICKNESS, GENERAL WORKMANSHFeb 2, 2006 · N273FE · Boeing 727200SDR 06FDEA0482Skin · noneACCESS SEC 48 EXTERNAL SKIN BS 1326 - 1342 RT SIDE STR 4 - 7 FOR REPAIR OF VERTICAL FIN SKIN REPAIR. REMOVED SEC 48 SKIN AT BS 1326-1342 AND INSTALLED REPAIR PER FED-EX EA 7-5330-96576.Feb 1, 2006 · N490FE · Boeing 727200SDR USAA060183Panel · corroded51A PANEL CORROSION. REPAIRED IAW PER TR 53-02-01, DEFECT SIZE: 10 X 12 INCH.Feb 1, 2006 · N677UW · Airbus A330323SDR 06FDEA0430Skin · unknownDURING ACCESS FOR STR 30 REPAIR, (CUSTOMER CARD N00999), UPON REMOVAL OF EXISTING REPAIR DOUBLER BS 1165 - 1183 RBL 12 - LBL 10 FOUND ORIGINAL SKIN HAS CUTOUT BS 1175 - 1183 RBL 1 - 6.5 AND BS 1183 LWR CHORD CUTOUT IN A 1 X 2 INCH AREA. ALL WORK WAS ACCOMPLISHJan 30, 2006 · N191FE · Boeing 727100
Back to JASC 5101