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.
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
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 06FDEA0169Repair · unknownMAIN CABIN AT STA 1199 AND 1299 X-55 HAS SEAT TRACK REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 53-70-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 06FDEA0167Repair · noneCABIN - ATTIC AREA FS STA 1781 - 1821 BETWEEN STRINGER 2L - 4L FOUND WITH EXISTING SKIN DOUBLER REPAIR TAG ER/A 377652-14 REVISION 03/22/00. PREVIOUS DOUBLER REPAIR AT CABIN ATTIC FS STA 1781-1821 BETWEEN STRINGER 2L-4L EVALUATED AND FOUND REPAIR CARRIED SDR VNAA0601007Structure · lightning strikeTHE CREW REPORTED A LIGHTNING STRIKE DURING DESCENT INTO CLT. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE LT HORIZONTAL STABILIZER TIP FAIRING AND TWO STATIC WICKS. ASDR VNAA0601009Structure · lightning strikeTHE CREW REPORTED A LIGHTNING STRIKE DURING APPROACH INTO CLT. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE RADOME, LT NLG DOOR, FUSELAGE, RT ELEVATOR, RT HORIZONTAL STSDR 06FDEA0147Repair · unknownDURING AIRCRAFT'S P TO F/ACF CONVERSION FOUND: AT STA 1315-1301 STR 27-25 RT SIDE, EXISTING REPAIR ON JAMB DOOR. REMOVED EXISTING REPAIR DOUBLER, PERFORMED HFEC INSPECTION AND INSTALLED NEW REPAIR IAW SRM 5350-00 FIG 19 SH 2.SDR 06FDEA0096Repair · unknownPERFORMED INSPECTION IAW EO NR 8-5100-7-5001 P1 FOUND DOUBLER DIMENSION 4" BY 3" RT EXTERNAL FUSELAGE STA 357 LONG 31. PERFORMED INSPECTION ON REPAIR DOUBLER IAW EA NR 8-5330-93226 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1 E3, TREATESDR ASOA06075Unknown · unknownDURING C-CHECK, A SUSPECTED CRACK WAS FOUND ON THE LT SIDE OF FS 718. MAINTENANCE REPAIRED THE CRACK ON THE LT SIDE OF FS 718 IAW REO. (K)SDR 06FDEA0086Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 445, STR 17R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBER AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS SDR 06FDEA0085Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 720, STR 23L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR ISSDR 06FDEA0084Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 720, STR 28R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS SDR 06FDEA0083Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 950E, STR 29R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR ISSDR 06FDEA0082Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1130, STR 22L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR ISSDR 06FDEA0081Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED ABOVE AIRSTAIRS CONTROL PANEL WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIPSDR 06FDEA0078Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 370, STR 24L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 4, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR ISDR 06FDEA0077Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 680, STR 27R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 24, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS CLASSSDR 06FDEA0076Repair · unknownFOUND PREVIOUSLY 2 REPAIRS INSTALLED AT FWD CARGO DOOR WAS ACCOMPLISHED IAW SRM 52-00-3 FIG 3 AND 4, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR ISDR 06FDEA0075Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 300 ABOVE RT NLG DOOR WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 14, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPASDR 06FDEA0074Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 660, STR 27R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 14, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS CLASSSDR 06FDEA0073Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 970, STR 25L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 14, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS CLASSDR 06FDEA0072Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050, STR 19L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR SDR 06FDEA0071Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 500, STR 27R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 2 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR ISSDR 06FDEA0070Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 520, STR 27R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR ISDR 06FDEA0069Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 400, STR 22L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG.3 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP AND RSDR 06FDEA0068Repair · unknownFOUND PREVIOUSLY REPAIR, INSTALLED AT STA 1330 ABOVE AIRSTAIRS CUTOUT RT SIDE WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBERS AND SPACING, GENERAL WSDR 06FDEA00058Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT FWD OF NR 2 ENGINE LT SIDE WAS ACCOMPLISHED IAW SRM 51-40-2, FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP SDR 06FDEA00057Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1325 ABOVE AIRSTAIRS CUTOUT WAS ACCOMPLISHED IAW SRM 51-40-2 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSIST OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENERS SPACING AND NUMBERS, GENERAL WORKMANSSDR 06FDEA00056Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA.1323 LT SIDE BELOW PYLON TRAILING EDGE WAS ACCOMPLISHED IAW SRM 51-40-2, FIG 1, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKSDR 06FDEA00054Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 420, STR 8-9L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR ISDR 06FDEA00053Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 188 25L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENERS SPACING AND NUMBERS, GENERAL WORKMANSHIP AND REPAIR IS CLASDR IXXA06SMN010SRepair · misinstalledDURING C CHECK INSPECT, EXTERNAL FUSELAGE LT AFT HEAT EXCHANGER RT LWR CORNER HAS NON STANDARD REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05582 DATED 12-23-05 SEMAN DWG NR ED-4131 DATED 12-20-05, ED SEMAN NR 2005 1436 DATED 12-23-05. REMOVED NON STSDR QXEA200600057Unknown · corrodedPDX - BAG COMPARTMENT CORROSION AT NUT PLATE APPROXIMATELY X593 AND YL30. REPAIRED IAW DHC-8-200 SRM 51-40-11.SDR UPS06846091Repair · misrepairedINSPECTION TYPE:C3 DURING REPAIR SURVEY OF THE PRESSURIZED FUSELAGE, FOUND "A" PIT FWD AND AFT LWR DOOR CORNER REPAIRS NOT PER THE SRM REPAIRS. CUT OUT FUSELAGE SKIN AT L28R FWD AND AFT SIDE OF "A" PIT DOOR CUT OUT IAW SAA EA008-5320-01-A0008, FABRICATED AND SDR 06FDEA00042Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT NR 1 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 11, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL THICKNESS AND TYPE, FASTENERS NUMBER AND SPACING, GENERAL WORKMANSHIP, REPAIR IS CSDR 06FDEA00041Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT NR 4 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57- 50-3, FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBER AND SPACING, GENERAL WORKMANSHIP, REPAIR IS CSDR 06FDEA00040Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT NR 3 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57- 50-3, FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, TYPE, SIZE, SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBER AND SPACING, GENERAL WORKMANSHIP, REPAISDR 06FDEA00038Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 344, STR 7L WAS ACCOMPLISHED IAW EO 7-5340-7-5002 PT1, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, SHAPE, SIZE, TYPE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP, REPAIR IS SDR 06FDEA00037Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 312, STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, TYPE, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP, REPAIR IS CLASDR 06FDEA00036Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 312, STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, TYPE, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP, REPAIR IS CSDR 06FDEA00035Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 312, STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, TYPE, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP, REPAIR IS CSDR 06FDEA00034Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 227, STR20L WAS ACCOMPLISHED WITH SRM 53-30-3 FIG. 13, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, TYPE, SIZE, TYPE OF MATERIAL AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP AND REPAIR IS SDR 06FDEA00033Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT ST.312, STR.9L WAS ACCOMPLISHED WITH ISSUED EO 7-5330-7-2345, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, SHAPE, SIZE, TYPE OF MATERIAL AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR ISDR 06FDEA00032Repair · unknownFOUND EXISTING REPAIR AT STA 710, STR 26L WAS ACCOMPLISHED IAW ISSUED EA 7-5330-70412, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS WITH LOCATION, SHAPE, TYPE OF MATERIAL AND THICKNESS, FASTENERS SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR CLASSIFIED ASDR 06FDEA00030Repair · unknownDURING AIRPLANE'S CONVERSION FROM P TO F/ACF FOUND: 1EA EXISTING REPAIR ON AFT LOWER CARGO DOOR, EXTERNAL UPPER AFT SIDE (7 INCH X 5 INCH). REPAIR IS CONFORM TO SRM 52-10-00 FIG 17.SDR 06FDEA00025Repair · mismanufacturedLOWER FUSELAGE CENTER CARGO DOOR CUTOUT AFT LOWER AREA FOUND WITH EXISTING REPAIR (ER/A 361508-14). EXISTING REPAIR ON LOWER FUSELAGE CENTER CARGO DOOR CUTOUT AFT LOWER AREA EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM 53-50-00 FIGURE 16 VOLUME I. EXSDR ASOA06079Unknown · corrodedDURING C-CHECK, CORROSION WAS FOUND AT FS 280. MAINTENANCE REPAIRED THE CORRODION AT FS 280 BY INSTALLING NEW WEBS IAW SRM. (K)SDR ASOA06080Unknown · crackedDURING A C-CHECK, A SUSPECTED CRACK WAS FOUND AT FS 280, LBL9 AND RBL9. MAINTENANCE REPAIRED THE CRACK AT FS 280, LBL 9 AND RBL 9, IAW REO. (K)SDR DL76L050834Duct · unknownRT DUCT LEAK LP 1. RETURN TO BLOCK. TESTED DUCT LEAK. UNABLE TO DUPLICATE OR FIND FAULT.SDR 05FDEA04415Repair · unknownFUSELAGE FLUSH REPAIR AT BS 1150, BL0, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED SKIN PER SRM 53-30-3.SDR QXEA200501810Unknown · unknownFAT - ON TAXI FOR FLIGHT 2453 SPLR/STAB FAULT & RUD LIMIT FAULT STATUS MSGS KEEP CYCLING ON AND OFF. RETURNED TO THE GATE. REMOVED AND REPLACED ISI PER CRJ700 AMM 34-12-01-000-801-A01 AND 34-12-01-400-801-A01. PERFORMED PITOT LIN P3 CONTAMINATION REMOVAL PESDR 05FDEA04391Repair · misinstalledEVALUATED REPAIR AT BS 1050 STR 23R-24R FOUND NOT TO BE IAW SRM 53-30-3. REPLACED DOUBLER PER SRM 53-30-03 FIG 1.
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