Boeing 757-251
Service difficulty reports · 4,707
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 = '757251' 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 = '757251' 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 DALA1034745646Skin · crackedDURING L-CHECK FOUND NR 2 PYLON STRUT LT SKIN PANEL, CRACKED AT FWD UPPER CORNER INNER AND OUTER SKIN APPROX .5" IN LENGTH. NR 2 PYLON STRUT LT SKIN PANEL REPAIRED IAW EM 5451-01010-02C.SDR DALA1034735646Skin · crackedDURING L-CHECK FOUND NR 2 PYLON STRUT RT SKIN PANEL CRACKED FOUND AT FWD UPPER CORNER OUTER SKIN APPROX .3750" IN LENGTH. NR 2 PYLON STRUT RT SKIN PANEL REPAIRED IAW EM 5451-01010-02D.SDR DALA1102185522Tab · delaminatedLT ELEVATOR CONTROL TAB DELAMINATED APPROX 8 SQUARE INCHES. R & R RT ELEVATOR CONTROL TAB IAW AMM 27-30-03. ADJUSTMENT/TEST GOOD IAW MM 27-30-03-201 CORRECTED BY COOK 284650 STA DHN 10JAN11. REQUIRED INSP COMPLETED.SDR DALA1050735652Light · inoperativeDURING A LINE CHECK, MX FOUND THE EXTERNAL EMERGENCY LIGHT AT DOOR 4R INOPERATIVE. MX REPLACED THE LIGHT ASSY. OPS CHECK WAS GOOD.SDR DALA1101915534Floorbeam · corrodedFLOORBEAM CORRODED AT STA 365 FROM BL 0.0, TO RBL 64. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM B757-20053-00-51, FIG 101. GAINED ACCESS TO REPAIR AREA, CUT OUT DAMAGE "T" ANGLE. FABRICATED & INSTALLED REPLACEMENT "T" ANGLE, 2 EA REPAIR ANGLES ANDSDR DALA1033755654Rack · inoperativeDURING LAYOVER CHECK, FOUND AFT RIGHT LOWER EMERGENCY EXIT LIGHT L637 NOT ILLUMINATED. REPLACED RACK ASSEMBLY M737. OPS CHECK GOOD.SDR DALA1033385532Sill · corrodedDURING M-CHECK FOUND FT AFT CABIN 4L DOOR SILL HAS CORROSION BS 1640-1681 LBL54" TOP SURFACE & LWR SURFACE AT BS 1640. CLEANED OUT CORRODED AREA IAW SRM 51-10-02, DIMENSIONS L=2.6 W=2.0 D=.0205 IAW SRM 53-60-15 OUT OF LIMITS, REMOVED DOOR SILL IAW SRM 51-40-0SDR DALA1033425532Floorbeam · corrodedDURING M-CHECK, FOUND AFT CABIN FLOORBEAM BS 1640 BBL "0" TO RBL 54" CORRODED AT UPPER SKIN & LOWER SKIN SURFACE AROUND FASTENER HOLE. BLENDED OUT AREAS BEAM 1640 BBL 0 TO RBL 54 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-40-51, FIG 101, SHEET 1 AND SHEET 3, DESDR DALA1033415532Floorbeam · corrodedDURING M-CHECK FOUND AFT CABIN FLOORBEAM CORRODED AT BS 1640 LBL 54 00-51 FIG 101. REMOVED STIFFENERS AND UPPER CHORD IAW SRM 51-40 02. RECEIVED EXTRUSION IAW SRP B757-A-53-01-07-801-863A-A AND SRM 53-00-51 FIG 201 PARTS SRM 53-00-51. LOCATED AND DRILLED ALLSDR DALA1033405532Support · corrodedREMOVED CORROSION FROM SEAT TRACK SUPPORT IAW SRM 51-10-02 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101. REMOVED SEAT TRACK SUPPORT IAW SRM 51-40-02, RBL 45 STA 365-418. FABRICATED NEW SEAT TRACK TREATED, PRIMED APPLIED TOPCOAT, LOCATED AND DRILLED IAWSDR DALA1033395532Support Angle · corrodedDURING M-CHECK FOUND THRESHOLD PLATE SUPPORT ANGLE 2 EA AT BS 1640 & 1681 LBL 54 INCHES HAS CORROSION. REMOVED PLATE SUPPORT ANGLE IAW SRM 51-40-02, FABRICATED PLATE SUPPORT ANGLE AND PLATED ANGLE SUPPORT 1 EA LOCATED AND DRILLED IAW SRM 51-40-05. TREATED ANSDR DALA1033805532Sill · corrodedDURING M-CHECK FOUND L4 DOOR LOWER SILL WEB CORRODED AT STA 1640. REMOVED L-4 DOOR SILL WEB AND 5 (EACH) STIFFENERS IAW SRM 51-40-02. FABRICATED NEW L-4 DOOR SILL WEB IAW SRM 51-40-05. TREATED, PRIMED, AND APPLIED TOPCOAT IAW SRM 51-20-01 AND AMM 51-21-10. SDR DALA12011195637Skin · canningDURING LEAK CHECK, WHILE ACCOMPLISHING A REPAIR IAW EA 56-209491, REV "D", AN ADDITION DAMAGE (OIL CANNING) WAS FOUND ON THE LOWER SIDE OF THE CUT OUT AFTER EXISTING REPAIR DOUBLER REMOVED IAW WITH ER/A 486726-14, REV A.SDR DALA1034675532Web · puncturedDURING M-CHECK, FOUND APU COMPARTMENT UPPER SURFACE SKIN AT STA 1914 AND 17" LT FROM CTR WAS PUNCTURED. REMOVED DAMAGED SKIN, FABRICATED REPAIR DOUBLER . ALL WORK PERFORMED IAW SRM 51-70-10.SDR DALA1033015637Skin · damagedDURING L-CHECK WHILE WORKING EA 56-209491 SECTION IV REPAIR PART A DAMAGE REMOVAL/INSP, INSPECTORS FOUND FURTHER DAMAGE. REMOVE AND DISCARD THE EXISTNG DOUBLER CUT OUT DAMAGE APPROX 9.5 X 10" HFEC INSPECTED IAW NTM 51-00-19, PART 6 THE EDGE OF THE SKIN TRIM OSDR DALA1033005637Skin · damagedDURING L-CHECK FOUND LOWER FUSELAGE AT STA 207.1, APPROX 36" BELOW STR 20R LAP JOINT 1EA FASTENER AND ADJACENT SKIN HAS LIGHTNING STRIKE. REMOVED 1 EA FASTENER FUSELAGE AT 207.1 IAW SRM 51-40-02, HFEC IAW NTM 51-00-13 PT6, NO CRACK INDICATION NOTED. INCREASESDR DALA1032995637Skin · damagedDURING L-CHECK FOUND LOWER FUSELAGE AT STA 192.1 APPROX 27" BELOW STR 20R LAP JOINT 14 EA RIVET AND ADJACENT SKIN HAS LIGHTNING STRIKE. REMOVED 14 EA FASTNERS FUSELAGE AT 192.1 IAW SRM 51-40-02. NDT HFEC IAW NTM 51-00-16 PT6 NO CRACK INDECATION NOTED. INCREASSDR DALA1032975532Skin · dentedDURING M-CHECK FOUND APU COMPT EXTERNAL SKIN DENTED BETWEEN STA 1896.20 & STA 1918.9, BL 25.0. CHECKED DENT LIMITS, SANDED DAMAGED AREA, POTTED DENT, FABRICATED REPAIR DOUBLER, BONDED REPAIR DOUBLER,CLEANED AREA APPLIED SEALANT AROUND DOUBLER AND PRIMED.ALL WOSDR DALA1032915507Coffeemaker · contaminatedEN ROUTE FLIGHT ATTENDANT REPORTED FUME/SMOKE IN AFT GALLEY. SMELLED LIKE PLASTIC. CREW SECURED POWER TO AFT GALLEY. FLIGHT ATTENDANT FOUND PLASTIC GLOVES NEAR COFFEE MAKER. FLIGHT ATTENDANT REMOVED GLOVES. OPS CHECK NORMAL. GALLEY POWER OPS NORMAL. (20SDR DALA1033795532Sill · corrodedDURING M-CHECK FOUND AFT CBN 4R SILL HAS CORROSION BS 1640-1681 RBL 54 BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15 BS 1640 TO 1660. REMOVED 2 EA SUPPORTS IAW SRM 51-40-02. FABRICATED 2 EA SUPPORTS TREATED, PRIMED & PAINTED DOOR SILLS IAWSDR DALA1032725532Support · corrodedDURING “M” CHECK FOUND SEAT TRACK SUPPORT BET STA 365 & 377 RBL 24 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101, FABRICATED NEW SEAT TRACK SUPPORT IAW TRAVELLER T10/859329 P/N DA-141N5131-4-20.TREATED ANDSDR DALA1032595532Floorbeam · corrodedDURING M-CHECK, FOUND FLOORBEAM STA 365 UPPER CORD FROM BL0 TO RBL 60 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 DIM. L=44" W=2" D=.065" ORIG MAT .130" FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51, REMOVED FLOORBEAM REPAIR IAW SRM 51-40-02 FABRICATED NEWSDR DALA1032735637Wedge · delaminatedDURING L-CHECK FOUND RT WING NR6 SLAT UPPER WEDGE AREA INBD SIDE DELAMINATED. FOUND DURING TAP TEST. SANDED & CLEANED AREA, BONDED REPAIR, SANDED EXCESS SMOOTH & PRIMED IAW SRM 51-70-10 REP IAW 4 FIG 202 IAW WC 5742-01022-02F. PAINTED AREA IAW MM 51-21-10. SDR DALA1034705533Floorbeam · corrodedDURING M-CHECK FOUND MAIN CABIN FLOORBEAM CORRODED ON UPPER SURFACE OF REPAIR CHORD EXTENDING ONTO ORIGINAL CHORD ON BOTH ENDS, STA 345, RBL 36 TO LBL 18. REMOVED CORRODED EXISTING REPAIR FLOORBEAM STA 345 CUT OUT FLOORBEAM FROM LBL 53 TO RBL 36, FABRICATESDR DALA1034335533Floor Panel · corrodedDURING M-CHECK FOUND MAIN CABIN AFT DECK PLATE UPPER SURFACE CORRODED. STA 1680-1720, BL 0-RBL 54. REMOVED CORROSION IAW SRM 53-00-51, PG 103, DETAIL III. ORIGINAL THICKNESS .071 IAW SRM 53-60-51, PG 7. MAIN CABIN AFT DECK PLATE UPPER SURFACE FOUND TO BE WISDR DALA1031235532Support · corrodedDURING L-CHECK FOUND CORROSION ON SEAT TRACK SUPPORT AT BS 324 TO BS 418 RBL 0. REPAIRED PER SRM 51-40-05, SRM 51-21-02, SRM 51-120-01.SDR DALA1034345533Seat Track · gougedDURING M-CHECK, FOUND MAIN CABIN SEAT TRACK GOUGED BEYOND ALLOWABLE LIMITS, BETWEEN STA 1502 TO STA 1504, RT OTBD SEAT TRACK. R & R 1EA SEAT TRACK AND 1EA SPLICE FROM STA 1490 TO 1540, IAW SRM 53-00-52, REPAIR NR3, FIG 201, ON RBL 45.SDR DALA1032095645Connector · looseDURING LAYOVER CHECK FOUND SEAT-MOUNTED EMERGENCY ESCAPE PATH LIGHTS AT SEATS 19C AND 21C INOPERATIVE. SECURED LIGHT ASSEMBLY ELECTRICAL CONNECTOR. REF ADDL LOG PAGE 0286534. (2010-00854)SDR DALA1031355523Scuff Plate · corrodedDURING L-CHECK FOUND CORROSION ON L2 DOOR SCUFF PLATE TO FLOOR PANEL SUPPORT Z-ANGLE. REPAIRED PER ERA 486856-14 REV 0.SDR DALA1031345523Floorbeam · corrodedDURING L-CHECK FOUND CORROSION ON FLOORBEAM UPPER CAP AT BS 1640 RBL 53 TO BL 0. REPAIRED PER ERA 486850-14 REV 0.SDR DALA1035325537Seat Track · gougedDURING M-CHECK, FOUND LT OTBD SEAT TRACK BETWEEN STA 1468 TO 1470, GOUGED BEYOND ALLOWABLE LIMITS. R & R SEAT TRACK SECTION SPLICE, AT STA 1450 TO 1540, REF SRM 53-00-52, REPAIR 3, LBL 45.SDR DALA1035125533Seat Track · gougedDURING M-CHECK FOUND LT OTBD SEAT TRACK BETWEEN STA 1468 TO 1470 GOUGED BEYOND ALLOWABLE LIMITS. R & R SEAT TRACK SECTION SPLICE, AT STA 1450 TO 1540, REF SRM 53-00-52, REPAIR 3, LBL 45.SDR DALA1034325533Floorbeam · corrodedDURING M-CHECK FOUND RT NLG W/W TUNNEL, STA 365, LBL 24 TO RBL 24, FLOORBEAM HAS CORROSION. FABRICATED REPLACEMENT CHORD, 02 EA REPAIR ANGLES, AND 02 EA REPAIR STRAPS, TO FLOORBEAM 70 IAW SRM 53-00-51, REPAIR 3, PAGE 203, FIG 201. TREATED AND PRIMED REPLACEMESDR DALA1032905523Sill · corrodedDURING LINE CHECK, FOUND L2 DOOR UPPER SURFACE OF THE LOWER MAIN SILL INNER CHORD BETWEEN BS 704-711, AT WL 208.10 WAS FOUND CORRODED. SECTION I OF ER/A 486856-14 ISSUED FOR CORROSION REPAIR AT L2 DOOR UPPER SURFACE OF LOWER MAIN SILL INNER CHORD BETWEEN BS 70SDR DALA1031335523Intercostal · corrodedDURING L-CHECK FOUND CORROSION ON INTERCOSTAL AT BS 1660 TO BS 1680 BL 0. REPAIRED PER SRM 51-40-02, SRM 53-00-51.SDR DALA1032065655Power Supply · inoperativeDURING A LINE CHECK, MAINTENANCE FOUND THE AFT LEFT OVERWING EMERGENCY EXIT LIGHT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD. (2010-00851)SDR DALA1031215523Floor Support · corrodedDURING L-CHECK FOUND CORROSION ON MAIN CABIN FLOOR SUPPORT CHANNEL AT BS 1640 TO BS 1661 BL 0. REPAIRED PER SRM 51-40-02.SDR DALA1031205523Floor Support · corrodedDURING L-CHECK FOUND CORROSION ON R4 DOOR THRESHOLD SUPPORT STRUCTURE ASSEMBLY BS 1640 TO BS 1680. REMOVED AND REPLACED PER SRM 51-40-02.SDR DALA1031195523Floor Support · corrodedDURING L-CHECK FOUND CORROSION ON MAIN CABIN FLOOR SUPPORT CHANNEL AT BS 1661 - BS 1671 LBL 58. REPAIRED PER SRM 51-40-02 PAGES 1-12, SRM 53-00-51- PAGE 101 TO 103.SDR DALA1031225532Skin · damagedDURING M-CHECK SCRIBE LINE DAMAGE FOUND AT S-14R LAP SPLICE FROM BS 1598.75 TO BS 1605.812, WITH (D MIN)=.156" AND (D MAX)=.313"N/R 200/10. SCRIBE LINE DAMAGE FOUND AT S-14R LAP SPLICE FROM BS 1598.750TO BS 1605.812, WITH (D MIN)=.156" AND (D MAX)=.313". THESDR DALA1030985532Skin · damagedDURING M-CHECK SCRIBE LINE DAMAGE FOUND AT S-14R LAP SPLICE FROM BS 1598.75TO BS 1605.812, WITH (D MIN)=.156" AND (D MAX)=.313" N/R 200/10. DFRD BY BROWN III (D_MIN)=.156" AND (D_MAX)=.313".FOLLOWING NDT INSP TO DETECT CRACKS WERE ACCOMPLISHED: LOCAL SURFACE HSDR DALA1030975532Skin · damagedDURING M-CHECK SCRIBE LINE DAMAGE FOUND AT S-20R LAP SPLICE FROM BS 1452.062 TO BS 1453.687, WITH (D MIN) =.031" AND (D MAX) =.219" N/R 100/12. TASK ELAPSE TIME HRS: 0000.0 RII: N SCRIBE LINE DAMAGE FOUND AT S-20R LAPSPLICE FROM BS 1452.062TO BS 1453.687, WITHSDR DALA1030965532Floorbeam · corrodedDURING M-CHECK FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 377 LBL 60. REPAIRED PER SRM 53-00-51 FIGURE 201, SRM 51-40-05, SRM 51-20-01 & SRM 51-40-02.SDR DALA1030815638Light · inoperativeDURING A LINE CHECK, MAINTENANCE FOUND THE SEAT 1B (AFT) EMERGENCY PATH LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD. (2010-00843)SDR DALA1030705523Floorbeam · corrodedDURING L-CHECK FOUND CORROSION ON MAIN CABIN FLOORBEAM UPPER CAP UNDER FLOOR PANEL 104C AND 107A FROM BL 0 TO RBL 53. REPAIRED PER SRM 53-60-51 DETAIL 111 PAGE 7, DWG 148N216, SRM 51-40-02 PAGE 7.SDR DALA1030955523Fitting · corrodedDURING L-CHECK FOUND EXFOLIATION CORROSION ON STRINGER END FITTING AT BULKHEAD BS 1720 S17R APPROXIMATELY 6 FROM FUSELAGE. REPAIRED PER SRM 51-40-02 PAGE 7.SDR DALA1030675523Skin · crackedDURING L-CHECK FOUND CRACK IN LEFT WING NR 2 LEADING EDGE SLATE LOWER SKIN JUST FORWARD ON OUTBOARD MAIN SLAT TRACK. REPAIRED PER SRM 57-70-13 PAGES 1 & 2.SDR DALA1030665523Skin · crackedDURING L CHECK FOUND CRACK IN LEFT WING NR 3 LEADING EDGE SLAT LOWER SKIN JUST FORWARD OF OUTBOARD MAIN SLAT TRACK. REPAIRED PER SRM 57-70-13 PAGES 1 & 2.SDR DALA1030655523Skin · damagedDURING L-CHECK FOUND DAMAGE AND DELAMINATION ON RIGHT WING AILERON INBOARD LOWER SURFACE. REPAIRED PER SRM 57-60-01 & SRM 51-60-01.SDR DALA1031315523Floorbeam · corrodedDURING L-CHECK FOUND CORROSION ON MAIN CABIN FLOORBEAM AT BS 1661 LBL 58. REPAIRED PER SRM 53-00-51 PAGE 101 TO PAGE 103, SRM 53-10-51 PAGE 6, DWG BAC1518-338 REV C, SRM 51-40-02 PAGE 1-10, SRM 53-00-51.
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