Boeing 757-28A
Service difficulty reports · 2,000
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '75728A' 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 aircraft_model_key = '75728A' 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 U2RA201211150002Stringer · corrodedMAIN CABIN BS 1600-1620, STRINGER 17R, STRINGER HAS CORROSION, CORROSION LENGTH 1.6", WIDTH .8" DEPTH .016", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL .047". STRINGER REPAIRED IAW INSTRUCTIONS.SDR U2RA201211150001Retainer · crackedNR 2 ENGINE THRUST REVERSER "C" DUCT T/E UPPER FORWARD RETAINER HAS TWO CRACKS. CRACK ONE LENGTH .25" CRACK TWO LENGTH .5". REPAIRED IAW DWG 5430D1519.SDR U2RA201211140008Floor Support · corrodedFORWARD CARGO BS 640-660, RBL 2.9, FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1", DEPTH .037" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .026". FLOOR SUPPORT REPLACED IAW DWG 143N5370.SDR U2RA201211140007Floor Support · corrodedFORWARD CARGO BS 640-660, LBL 7.55", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1", DEPTH .017", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .046", FLOOR SUPPORT REPLACED IAW DWG 143N5370.SDR U2RA201211140006Floor Support · corrodedFORWARD CARGO BS 640-660 LBL 2.9", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1",DEPTH .023" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .040". FLOOR SUPPORT REPLACED IAW DWG 143N5370.SDR U2RA201211140005Frame · corrodedAFT CARGO BS 1640, STRINGER 29L TO 29R FRAME WEB HAS HEAVY CORROSION. REPLACED FROM STRINGER 24L TO S24R IAW DWG 146N1032. REF NRC HFL6086. GENERATED FROM TASK CARD 53-222-00-01.SDR U2RA201211140004Floor Support · corrodedFORWARD CARGO BS 640-660 RBL 7.55" FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1", DEPTH .018", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .045". FLOOR SUPPORT REPLACED IAW DWG 143N5370.SDR U2RA201211140003Floor Support · corrodedFORWARD CARGO BS 640-660, LBL 10.45", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5" WIDTH 1", DEPTH .029" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .034". FLOOR SUPPORT REPLACED IAW DWG 143N5370.SDR FDEA201211144005Frame · dentedAFT CARGO BAY LT SIDE FRAME BS 1480 HAS DENT ON TOP OF FRAME, BETWEEN STR 25 AND 26L. REPAIRED IAW EA : F-5310-162902. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201211144004Frame · dentedFWD CARGO BAY LT SIDE FRAME AT BS 680 HAS DENT ON TOP OF FRAME AT STR 23L. COMPLIED IAW EA: RF-5310-162903. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR U2RA201211140002Fairing · scratchedLEFT HORIZONTAL STABILIZER L/E MID FAIRING 332CL 2 EA AREAS SCRATCHED, (AREA 1 LENGTH 1.2" WIDTH .9", DEPTH .017", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .046"). (AREA 2 LENGTH 1.2", WIDTH .9", DEPTH .013" ORIGINAL MATERIAL THICKNESSSDR U2RA201211140001Doubler · corrodedNR 2 PYLON ACCESS PANEL 443LL CUT OUT SKIN DOUBLER HAS CORROSION LENGTH 2.5", WIDTH 1.1", DEPTH .065", ORIGINAL MATERIAL THICKNESS .090", REMAINING MATERIAL THICKNESS .065".SDR U2RA201211130011Floor Support · corrodedAFT CARGO BS 1450-1490, RBL 10.45", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 2.5", WIDTH 1" DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". REPAIRED IAW SRM 51-70-11.SDR U2RA201211130010Floor Support · corrodedAFT CARGO BS 1460-1490, LBL 70. 55, FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5",WIDTH 1", DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". FLOOR SUPPORT REPAIRED IAW SRM 51-70-11.SDR U2RA201211130009Floor Support · corrodedAFT CARGO BS 1350-1380, RBL 16.1", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5",WIDTH 1", DEPTH .021", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .042". FLOOR SUPPORT REPLACED5 IAW DWG 146N5417.SDR U2RA201211130008Support · corrodedAFT CARGO BS 1360-1380, LBL 2.9, FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5, WIDTH 1", DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERILA THICKNESS .025". REPLACED FLOOR SUPPORT IAW DWG 146N5417.SDR U2RA201211130007Floor Support · corrodedAFT CARGO BS 1450-1500 RBL 2.9, FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH 1" DEPTH .038" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". FLOOR SUPPORT, REPLACED IAW DWG 146N5447.SDR U2RA201211130006Floor Support · corrodedAFT CARGO BS 1460-1500, RBL 7.55" FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT AREAS, LENGTH 1.5, WIDTH 1", DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". SUPPORT REPLACED FROM STATION 1450-1500 IAW DWG 146N5447.SDR U2RA201211130005Floor Support · corrodedAFT CARGO BS 1380-1400, RBL 7.55" FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH 1", DEPTH .038", ORIGINAL MATERIAL THICKNESS .063", MATERIAL THICKNESS REMAINING .025". REPLACED SUPPORT FROM STATION 1340-1445 IAW DWG 146N5417.SDR U2RA201211130004Floor Support · corrodedAFT CARGO BS 1450-1500 RBL 2.9", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH 1", DEPTH .038" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .025". SUPPORT REPLACED IAW DWG 146N5447.SDR U2RA201211130003Floor Support · corrodedAFT CARGO BS 1360-1380 RBL 10.45", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT AREAS, LENGTH 1.5", WIDTH 1", DEPTH .035", ORIGINAL MATERIAL THICKNESS .063", REMAINING THICKNESS .028". SUPPORT REPLACED FROM STATION 1340-1445 IAW DWG 146N5417.SDR U2RA201211130002Floor Support · corrodedAFT CARGO BS 1460-1480, LBL 10.45" FLOOR SUPPORT HAS CORROSION ON AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH .5", DEPTH .038" ORIGINAL THICKNESS .063", REMAINING THICKNESS .025". SUPPORT, REPLACED IAW DWG 146N5447. REF NRC HFL5781.SDR U2RA201211130001Floor Support · corrodedAFT CARGO BS 1390-1410, RBL 2.9", FLOOR SUPPORT HAS CORROSION AT ANCHOR NUT ATTACH AREAS, LENGTH 1.5", WIDTH 1", DEPTH .014" ORIGINAL MATERIAL THICKNESS .063", REMAINING MATERIAL THICKNESS .049". SUPPORT REPLACED IAW DWG 146N5417. REF NRC HFL5880.SDR FDEA201211123948Seat Track · corrodedCABIN SEAT TRACK AT STA 365 TO 377 RBL 45 HAS CORROSION ON TRACK FLANGES. CORROSION REMOVED IAW SRM 51-10-02 REV 106. FOUND EXCEED LIMITS IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 106. SEAT TRACK SUPPORT REMOVED IAW SRM 51-40-02 REV 106. SEAT TRACK SSDR FDEA201211123956Crease Beam · corrodedBS 740 LBL 64 CREASE BEAM HAS CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 106. MATERIAL THICKNESS REMOVED 0.014 INCHES FOUND EXCEEDS LIMITS IAW SRM 53-30-13 FIG 101 ALLOWABLE DAMAGE 1 REV 106. CREASE BEAM REMOVED IAW SRM 51-40- 02 REV 106. NEW CREASE SDR FDEA201211123951Crease Beam · corrodedBS 1295 TO 1360, RBL 64 CREASE BEAM HAS CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 106. MATERIAL THICKNESS LOSS MORE THAN 50%. CREASE BEAM REMOVED IAW SRM 51-40-02 REV 106. NEW CREASE BEAM INSTALLED IAW DRAWING 146N8322 SHT 1 REV F. REPAIR CLASSIFIESDR U2RA201211120005Sill · corrodedFORWARD CARGO DOOR CUT OUT BS 560-620 LOWER SILL HAS CORROSION IN NUT PLATE AREA. LENGTH 3.2", WIDTH 1", DEPTH .042". ORIGINAL MATERIAL THICKNESS .300", REMAINING MATERIAL THICKNESS .258".SDR U2RA201211120004Nose Cowl · corrodedNR 1 ENGINE NOSE COWL FOUR O'CLOCK ARE INNER SANDWICH PANEL FOUND CORRODED. NOSE COWL REPLACED.SDR U2RA201211120003Blades · debondedNR 1 ENGINE, NR 14 FAN BLADE FOUND TAP DISPLAY MORE THAN 600 DB AT SEC "C" OUT OF LIMITS IAW SB RB211-72-9660. GENERATED FROM TASK CARD 72-136-01-01.SDR U2RA201211120002Nose Cowl · corrodedNR 1 ENGINE NOSE COWL 11 O'CLOCK POSITION AREA INNER SANDWICH PANEL FOUND CORROSION. REF NRC HFL0717, COWL REPLACED. GENERATED FROM TASK CARD 71-802-50-01.SDR U2RA201211120001Fitting · chafedNR 1 PYLON MID-BULKHEAD RT FITTING, CHAFING, LENGTH 3", WIDTH 1" DEPTH .095", ORIGINAL MATERIAL THICKNESS .388", REMAINING MATERIAL THICKNESS .293". MFG FOUND CONDITION ACCEPTABLE AS IS.SDR FDEA201211123966Seat Track · misalignedCABIN SEAT TRACK AT BS 1610, LBL 24 HAS SEAT FITTING MISMATCH. SEAT TRACK SECTION INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR 3, REV 107.SDR FDEA201211123965Seat Track · corrodedCABIN SEAT TRACK AT BS 1610 TO 1640, RBL 45 HAS CROWN CORROSION. REPLACED SEAT TRACK SECTION FABRICATED AND INSTALLED IAW SRM 53-00-52, FIG 201. REPAIR 3 REV 107. REPAIR IS MAJOR.SDR FDEA201211123964Floorbeam · corrodedCABIN, AT BS 1640 RBL 54 TO 45 FLOORBEAM HAS CORROSION. NEW FLOORBEAM INSTALLED IAW DWG 146N5089, SHT 1, REV B. REFER TO SNRM: N01086 FOR WORK DETAILS. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201211123963Seat Track · corrodedCABIN SEAT TRACK AT BS 1610 TO 1640, RBL 24 HAS CHANNEL AND CROWN CORROSION. REPLACED SEAT TRACK WITH FABRICATED SECTION AND INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR 3, REV 107. REPAIR IS MAJOR.SDR FDEA201211123962Seat Track · damagedCABIN SEAT TRACK AT BS 1524, RBL 45 HAS A DRILL HOLE ON THE CHANNEL. FOUND EXCEEDED LIMITS IAW SRM 53-00-52, FIG 101, ALLOWABLE DAMAGE 1, REV 107. SEAT TRACK REPAIR CARRIED OUT IAW SRM 53-00-52, FIG 201. REPAIR 3, REV 107 AND COMPLIED WITH PART 1 OF EA F-53SDR FDEA201211123961Deck Plate · corrodedCABIN DECK PLATE AT BS 1681 LBL 12 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3, REV AND INSTALLED IAW DWG 146N5300 SHT 16, REV C. REPAIR IS MAJOR.SDR FDEA201211123960Deck Plate · corrodedCABIN DECK PLATE AT BS 1703 TO 1710, RBL 48 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3, REV AND INSTALLED IAW DWG 146N5300, SHT 16, REV C. REPAIR IS MAJOR.SDR FDEA201211123959Floorbeam · corrodedCABIN FLOORBEAM AT BS 365, RBL 12 TO RBL 47 HAS CORROSION. CORROSION REMOVED IAW SRM 51-10-02, REV 107. FOUND OUT OF LIMIT IAW SRM 53-00-51, FIG 101 ALLOWABLE DAMAGE 1, REV 107. FLOORBEAM REMOVED IAW SRM 51-40-02, REV 107. NEW FLOORBEAM FABRICATED IAW DWSDR FDEA201211123958Seat Track · corrodedCABIN, AT BS 1615 RBL 45 SEAT TRACK HAS CORROSION IN CHANNEL. REPLACED SEAT TRACK SECTION. FABRICATED AND INSTALLED IAW SRM 53-00-52, FIG 201. REPAIR 3 REV 107. REPAIR IS MAJOR.SDR FDEA201211123957Crease Beam · corrodedCABIN CREASE BEAM ANGLE HAS CORROSION AT BS 710 TO 730 LBL 64. NEW ANGLE INSTALLED IAW DWG 143N8322, SHT 1, REV K, REPAIR CLASSIFED MAJOR IAW GMM 6-2-100.SDR FDEA201211123955Crease Beam · corrodedCABIN, BS 734 LBL 64 CREASE BEAM ANGLE HAS CORROSION. NEW ANGLE INSTALLED IAW DWG 143N8322, SHT 1, REV K. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201211123954Seat Track · damagedCABIN SEAT TRACK AT BS 418 TO 440 LBL 24 HAS SEAT FITTING DAMAGE TO CROWN. SEAT TRACK INSTALLED IAW DWG 141N5130, SHT 1, REV F. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201211123953Seat Track · damagedCABIN SEAT TRACK AT BS 418 TO STA 440 LBL 45 HAS SEAT FITTING DAMAGE TO CROWN. SEAT TRACK INSTALLED IAW DWG 141N5130, SHT 1, REV F. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201211123952Seat Track · corrodedCABIN SEAT TRACK AT BS 365 TO 377 RBL 24 HAS CORROSION ON TRACK FLANGES. NEW SEAT TRACK SUPPORT INSTALLED IAW DWG 141N5130, SHT 2, REV E. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201211123950Crease Beam · corrodedCABIN CREASE BEAM AT BS 362 TO STA 395, LBL 64 HAS CORROSION. CORROSION REMOVED IAW SRM 51-10-02, REV 107 AND FOUND OUT OF LIMIT IAW SRM 53-00-15, FIG 101 ALLOWABLE DAMAGE 1, REV 107. NEW CREASE BEAM INNER CHORD FABRICATED IAW DWG 141N8322 SHT 3, REV G. NSDR FDEA201211123949Seat Track · corrodedCABIN SEAT TRACK AT BS 377 TO 395 RBL 24 HAS CORROSION ON TRACK FLANGES. CORROSION REMOVED IAW SRM 51-10-02, REV 107. FOUND EXCEEDED LIMITS IAW SRM 53-00-52, FIG 101 ALLOWABLE DAMAGE 1, REV 107. SEAT TRACK IAW SRM 51-40-02, REV 107. NEW SEAT TRACK INSTALLSDR FDEA201211123947Seat Track · corrodedCABIN SEAT TRACK AT BS 395 TO 418 RBL 45 HAS CORROSION ON TRACK FLANGES. SEAT TRACK REPLACED IAW DWG 141N5130, SHT 2, REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201211123946Seat Track · corrodedCABIN SEAT TRACK AT BS 395 TO STA 418, RBL 24 HAS CORROSION ON TRACK FLANGES. NEW SEAT TRACK INSTALLED IAW DWG 141N5130, SHT 2, REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201211123945Seat Track · corrodedCABIN SEAT TRACK AT BS 377 TO 395 RBL 45 HAS CORROSION ON TRACK FLANGES. REPLACED IAW DWG 141N5130, SHT 2, REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
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