Boeing 757-23A
Service difficulty reports · 1,397
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 = '75723A' 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 = '75723A' 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 FDEA200911204089Frame · dentedLWR FUSELAGE FS 900 WING TO BODY FRAME CORRODED AND CORRODED FASTENERS. REMOVED CORROSION AT F. STA 900 WING TO BODY FAIRING RBL 63 TO LBL 63 FOUND OUT OF LIMITS IAW SRM 53-00-71 DET. 7 , REMOVED AND REPLACED FRAME CORD IAW SRM 51-40-02 THIS IS A MAJOR "ASDR FDEA200911204100Web · crackedMAIN CARGO DECK BS 1420-1440, RBL 64, WEB CRACKED. REMOVED AND REPLACED WEB IAW SRM 51-40-02 AND 51-40-02, FABRICATED NEW WEB ON MAE TRAVELER T9/810194. REMOVED AND RE-INSTALLED SPLICES AND ANGLE 2 BS 1420-1430, S17R, RBL 64, TO FACILITATE REPAIR IAW SRM 51-4SDR FDEA200911204099Web · crackedMAIN CARGO DECK BS 1400-1420 RT SIDE BL 64 WEB CRACKED. REMOVED AND REPLACED WEB AT BS 1400-1420, RBL 64, IAW SRM 51-40-02. FABRICATED NEW WEB ON MAE TRAVELER T9/8140193, LOCATED AND DRILLED IAW SRM51-40-05. REMOVED AND RE-INSTALLED SPLICES AT BS 1400-1410, RSDR FDEA200911204092Floorbeam · corrodedMAIN CABIN FLOOR STR STA 324 RBL 39 TO 46 FLOORBEAM UPPER SURFACE HAS AREAS OF CORROSION. REMOVED FLOOR T-CHORD, AND ATTACHING PARTS, FABRICATED NEW TEE , WEB, & EXTRUSION. INSTALLED NEW TEE, NEW WEB, NEW EXTRUSION AND ATTACHING PARTS STA 324- 344, LBL 60-RSDR FDEA200911194075Intercostal · corrodedFWD CARGO BS 820 TO 839 LBL 20 INTERCOSTAL CORRODED. CORRODED INTERCOSTAL FROM BS 820 TO BS 839 REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200911194067Support Bracket · misalignedINCOMING FASTENER PATTERN ON THE FRAME ASSY DOES NOT FACILITATE INSTALLATION OF SUPPORT BRACKET ASSY FOR PULLEY INSTALLATION AT STA 1640, BETWEEN S-2L AND S-3L AT BS 1640 FRAME, BETWEEN S-2L AND S-3L, THE EXISTING SHEAR TIE HOLE PATTERN CONFLICTED WITH THE ACCSDR FDEA200911194052Flap Track · corrodedRT WING OTBD AFT FLAP SUPPORT TRACK ROLLING SURFACE AT AF STA 584.1 FOUND WITH CORROSION AND WORN MARKS. RT WING OTBD AFT FLAP SUPPORT TRACK REMOVED AND REPLACED IAW AMM 27-51-22-4, REV.5. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200911113926Crease Beam · corrodedRT CREASE BEAM STA 1240-1280 CORRODED. REMOVED CORROSION IAW SRM 53-60-13 ORIGINAL THICKNESS - .070", AFTER REWORK - .060", .010" MATERIAL REMOVED. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, DETAIL 1. REMOVED CREASE BEAM IAW SRM 51-40-02. FABRICATED NEW CRSDR FDEA200911073887Seat Track · corrodedMAIN CABIN SEAT TRACK STA 640-780 RBL 24 HAS CORROSION AND GOUGES REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK P/N BAC 1520-792, IAW SRM 53-30-52. INSTALLED NEW SEAT TRACK STA 640-780, RBL 24, IAW SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.SDR FDEA200911063880Crease Beam · corrodedMAIN CABIN STA 740-760 RT SIDE INBD CREASE BEAM CHORD HAS CORROSION. REMOVED CORROSION ON CREASE BEAM IAW SRM 53-30-13 ORIG THICKNESS .070, AFTER REWORK .006 WITHIN LIMITS , REMOVED CORROSION ON WEB FOUND OUT OF LIMITS IAW SRM 53-30-15 FIG. 101 DET 4, ORIG. MSDR FDEA200911043851Seat Track · damagedSEAT TRACK FASTENER HOLES ELONGATED BS 1415 RBL 24.0. CHECKED LIMITS FOR SEAT TRACK BS 1415-1445,M RBL 24, AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG 101, DETAIL 4. REMOVED SEAT TRACK BS 1320-1540, RBL 24, IAW SRM 51-40-02. FEABRICATED NEW SEAT TRSDR FDEA200911043850Seat Track · corrodedMAIN CABIN SEAT TRACK RBL 24 STA 1379-1384 UPPER LOBES HAVE AREAS OF CORROSION. REMOVED CORROSION AND CHECKED LIMITS OF SEAT TRACK @ BS 1379-1384, RBL 24, AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG. 101, DETAIL 4. FABRICATED NEW SEAT TRACK ON N/R SDR FDEA200911033802Floor Support · corrodedAFT PIT FLOORBOARD SUPPORT UPPER SURFACE HAS CORROSION APPROX FROM STA 1440 TO STA 1500 AT LBL 4. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS. ORIG MAT THICKNESS 0.063 AFTER REWORK 0.042. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-83. REMOVED FLOOR SUPSDR FDEA200910313750Seat Track · corrodedMAIN CABIN SEAT TRACK STA 680-780 LBL 45 HAS CORROSION AND GOUGES. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK P/N 60-6549/24 IAW SRM 53-30-52. INSTALLED NEW SEAT TRACK STA 680-780, LBL 45, IAW SRM 53-30-52, 51-40-02. MAJOR REPAIR.SDR FDEA200910313752Floor Support · corrodedMAIN CABIN FLOOR STR AT L-1 DOOR STA 324 TO 377 LBL 60 HAS AREAS OF CORROSION AROUND NUT PLATES. REMOVED CORROSION AT FLOOR STRUCTURE FROM F STA 324 TO 377 FOUND OUT OF LIMITS IN 3 EA FLOOR SUPPORTS LBL 60 IAW SRM 53-00-04. REMOVED AND REPLACED WITH NEW FLOORSDR FDEA200910313751Seat Track · corrodedMAIN CABIN FLOOR STR STA 1620 TO 1640 LBL 24 SEAT TRACK WEB CORRODED. REMOVED CORROSION IAW SRM 51-10-02. AREA FOUND OUT OF LIMITS IAW SRM 53-00-04, FIGURE 101, DETAIL II. REMOVED ANGLE AND WEB IAW SRM 51-40-02. RECEIVED NEW ANGLE AND WEB FROM FAB SHOP TSDR FDEA200910303741Seat Track · gougedSTA 418-440, RBL 24 SEAT TRACK GOUGED REMOVED SEAT TRACK IAW SRM 51-40-00-02, FIG 101, DETAIL VII. RECEIVED NEW SEAT TRACK PN 60-6549/24. INSTALLED NEW SEAT TRACK STA 418 TO 440, RBL 24, IAW SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.SDR FDEA200910303737Seat Track · gougedSTA 418-440 RBL 45 SEAT TRACK GOUGED. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02. OLD SEAT TRACK WAS FOUND OUT OF LIMITS DUE TO GOUGE BEING MORE THAN 20% OF MATERIAL THICKNESS. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-02. TREATED AND PRIMED NEW SESTSDR FDEA200910283717Seat Track · corrodedSEAT TRACK UPPER AND LWR SURFACE CORRODED LBL 24 BS 1570-1640. REMOVED SEAT TRACK PER SRM 51-40-02 ,FABED NEW TRACK, P/N. BAC1520-792 BATCH 1544829 PER SRM 53-60-52 LOCATED END DRILLED AND INSTALLED IAW SRM 51-40-02 AND 51-20-05, THIS IS A MAJOR "A" REAPAIR NSDR CNMA20090153Window · failedF/O WINDSHIELD SHATTERED DURING FLIGHT. REMOVED AND REPLACED F/O WINDSHIELD IAW MM 56-11. (PRECAUTIONARY: REMOVED AND REPLACED HEAT CONTROL UNIT, OPS CHECK GOOD IAW MM 30-41, DUE TO THE R-1 WINDSHIELD BEING REPLACED).SDR FDEA200910263677Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 345, LBL 45, HAS AREA OF CORRORSION. REMOVED CORROSION, FABRICATED TEE CHORD STRAPS ON MAE TRAV 3 T9/806490, AND FABRICATED ANGLES ON MAE TRAV T9/806501, INSTALLED TEE CHORD, ANGLES, STRAPS REPAIR PARTS STA 345, LBL 54- RBL 37, IAWSDR FDEA200910263674Floorbeam · corrodedMAIN CABIN FLOORBEAM BS 340 LBL 20 TO 27 HAS AREA OF CORROSION (OUT OF LIMITS). REMOVED FLOOR SUPPORT IAW SRM 51-40-02. FABRICATED FLOOR SUPPORT ON MAE TRAV NR T9\807944. INSTALLED FLOOR SUPPORT MCD STA 333-340, LBL 20-31 IAW SRM 51-40-02.SDR FDEA200910263673Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 340 LBL 32 TO 37 HAS AREA OF CORRODED OUT OF LIMITS. REMOVED CORROSION MCD STR STA 340 LBL 32-37 IAW SRM 51-10-02 CHECKED LIMITS. ORIG MAT THICKNESS = .032, AFTER REWORK MAT THICKNESS .018, MAT LOSS= .012 FOUND TO BE OUT OF LIMITS IAWSDR FDEA200910263672Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 340 LBL 29 TO 32 HAS AREA OF CORRODED OUT OF LIMITS. REMOVED CORROSION FROM FLOORBEAM IAW SRM 51-10-02. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04. REMOVED 4EA. NUTPLATES, 2EA. BRACKETS, AND FLOORBEAM IAW SRM 51-SDR FDEA200910263671Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 333 LBL 38 TO 44 HAS AREAS OF CORRODED OUT OF LIMITS IAW SRM 53-00-04. REMOVED FLOOR SUPPORT, BS 324-345, AND 2EA SUPPORT BRACKETS, BS 324, LBL 38 AND 40, IAW SRM 51-40-02. RECEIVED NEW FLOOR SUPPORT, BS 324-345, LBL 38-40, PN 141N51SDR FDEA200910263670Floor Support · corrodedMAIN CABIN FLOOR SUPPORT STA 324 TO 345 LBL 20 HAS AREAS OF CORRODED OUT OF LIMITS. REMOVED CORROSION FROM MCD FLOOR STRUCTURE, BS 324-345, LBL 20, IAW SRM 51-10-02. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-04; ORIG. MATL. THICKNESS; .055SDR FDEA200910263669Door Frame · corrodedAUXILLARY POWER UNIT INTAKE DOOR FWD & LOWER FRAME HAS CORROSION (OUT OF LIMITS) REMOVED CORROSION, CHECKED LIMITS APU INTAKE DOOR FRAME .090 ORIG THICKNESS, MAT LOSS .025 OUT OF LIMITS, LWR FRAME ORIG THICKNESS .080 MAT LOSS .020 FOUND OUT OF LIMITS IAW SDR FDEA200910263668Support · corrodedAFT PIT LT TRANSISTION PANEL SUPPORT WEB IS CORRODED BETWEEN STA 1480 TO STA. 1500 AT S-26L OUT OF LIMITS. REMOVED SUPPORT ANGLE AND WEB IAW SRM 51-40-02. FABRICATED SUPPORT ANGLE AND WEB ON MAE TRAV NR T9/808232, T9/808163. INSTALLED SUPPORT ANGLE AND WESDR FDEA200910203616Seat Track · corrodedSEAT TRACK CORRODED LBL 44, BS 1600-1640. REMOVED CORROSION MULTIPLE AREAS, BS 1600-1640, LBL 45, AT CROWN. MAX CLEANUP TOP SURFACE OF TRACK; MAT. LOSS= .022", L=.250", W=.500" 2 BS 1612. FOUD TO BE OUT LIMITS PER SRM 53-00-52. FLAGE MAX. CLEANUP; MAT. LOSDR FDEA200910203614Seat Track · corrodedMAIN CABIN SEAT TRACK RBL 24 CORROSION FROM STA 1180 TO 1280 (OUT OF LIMITS). REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK P/N 1520-792 IAW SRM 53-60-52, 51-10-02. INSTALLED SEAT TRACK STA 1180-1280, RBL 24, IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA200910203617Seat Track · corrodedSEAT TRACK CORRODED LBL 44, BS 1600-1640.SDR FDEA200910163593Floor Support · corrodedMAIN CABIN FLOOR STR STA 307 RBL 4 HAS AREA OF CORR. (OUT OF LIMITS) BLEND OUT AREA IN FLOOR SUPPORT STRAP, MAT. BEFORE .100 AFTER REWORK .088 FOUND OUT OF LIMITS IAW SRM 53-0004 FIG. 101 DET. 2, REPLACED WITH NEW FABRICATED STRAP IAW SRM 51-40-02 THIS IS ASDR FDEA200910163596Intercostal · corrodedMAIN CABIN STA 680-700 LT SIDE AT DOOR 2L STRUCTURE INTERCOSTAL HAS CORROSION. (OUT OF LIMITS) REMOVED CORROSION FROM MCD, BS 680-700, LHS, AT L2 DOOR STRUCTURE IAW SRM 51-10-02. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15. ORIGINAL MATERIALSDR FDEA200910163594Crease Beam · corrodedMAIN CABIN STA 660-680 LT SIDE INBD CREASE BEAM CORD HAS CORROSION (OUT OF LIMITS). REMOVED CORROSION BS 66-680, LBL 63, FOUND OUT OF LIMITS IAW SRM 53-30-15, FIG. 101, 45 PERCENT THROUGH MATL. REMOVED CREASE BEAM, BS 565-755, LBL 63. FABRICATED NEW CREASE BSDR FDEA200910163592Crease Beam · corrodedLT CREASE BEAM CORRODED BS 1320-1360. REMOVED CORROSION IAW SRM 53-60-15 ORIG MAT .100, MAT LOSS .012 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15 FIG.101 DET 3, REMOVED AND REPLACED CREASE BEAM STA 1290-1370, LBL 58 IAW SRM 51-40-02, MAJOR A REPAIR.SDR FDEA200910153586Floor Support · corrodedMAIN CABIN FLOOR STR STA 354, RBL 45 HAS AREA OF CORROSION (OUT OF LIMITS). REMOVED FLOOR SUPPORT BS 345-365, RBL 45, IAW SRM 51-40-02. REMOVED STIFFNERS AND NUTPLATES IAW SRM 51-40-02. CHECKED LIMITS OF SUPPORT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04,SDR FDEA200910153585Floor Support · corrodedMAIN CABIN FLOOR STR STA 326, RBL 5 HAS AREA OF CORROSION. (OUT OF LIMITS) REMOVED FLOOR SUPPORT BS 324-345, RBL5 IAW SRM 51-40-02. CHECKED LIMITS & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04, FIG. 101, DETAIL 2. ORIG THICKNESS; .100" AFTER REWORK; .085" SDR FDEA200910153584Floor Support · corrodedMAIN CABIN FLOOR STR AT R-1 DOOR STA 324 TO 345 RBL 60 HAS AREA OF CORROSION AROUND NUT PLATES. (OUT OF LIMITS) CHECKED LIMITS ON FLOOR SUPPORT ORIG. .050" AFTER REWORK .041AND FOUND OUT OF LIMITS IAW SRM 53-00-04. REMOVED FLOOR SUPPORT AND STIFFENER STA. 3SDR FDEA200910153583Floor Support · corrodedMAIN CABIN FLOOR STR STA 330, BL0 TO RBL25 HAS AREAS OF CORROSION AROUND NUT PLATES. (OUT OF LIMITS) REMOVED FLOOR SUPPORT IAW SRM 51-40-02. FABRICATED ON MAE TRAV NR T9/808384. INSTALLED NEW FLOOR SUPPORT AND T-CHORD STA 330, RBL 4-25, IAW SRM 51-40-02. SDR FDEA200910153582Floor Support · corrodedMAIN CABIN FLOOR STR 307, RBL 45 HAS AREA OF CORROSION AROUND NUT PLATES. (OUT OF LIMITS) REMOVED CORROSION ON FLOOR SUPPORT, BS 297-310, RBL 42, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04, FIG 101, DETAIL 2. MATERIAL LOSS OF .015". REMOVED 4EA. STIFFNESDR FDEA200910153581Crease Beam · corrodedRT CREASE BEAM UPPER SURFACE CORRODED, BS 1440-1460. (OUT OF LIMITS) REMOVED CORROSION FROM RT CREASE BEAM, BS 1405-1680, IAW SRM 51-40-02. EXFOLIATION CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FIG 101, .060" MATERIAL LOSS. FABRICATED NEW CRSDR FDEA200910153579Floor Support · corrodedMAIN CABIN FLOOR STR STA 310 TO 324 LBL 20 HAS AREA OF CORROSION AROUND NUT PLATES. (OUT OF LIMITS) REMOVED FLOOR SUPPORT IAW SRM 51-40-02. FABRICATED NEW IAW SRM 51-10-02. INSTALLED FLOOR SUPPORT AND ANGLES STA 310-324, LBL 20, IAW SRM 51-40-02. CATEGORY SDR FDEA200910143575Crease Beam · corrodedMAIN CABIN STA 740-760 LT SIDE INBD CREASE BEAM WEB HAS CORROSION DOT NR 122-43. FOUND TO BE OUT OF LIMITS PER SRM 53-30-13, FABRICATED NEW CREASE BEAM. LOCATED, DRILLED, TREATED AND PRIMED NEW CREASE BEAM PER SRM 51-20-01 / 51-21-00-7. INSTALLED NEW CREASSDR FDEA200910143572Floor Support · corrodedMAIN CABIN FLOOR STR STA 299, RBL 30 HAS AREA OF CORROSION. (OUT OF LIMITS) REMOVED 7EA BRACKET/CLIP STA 299, RBL 20-35 ON FLOOR SUPPORT IAW SRM 53-40-02. CHECKED LIMITS FOR SUPPORT ORIG .050" LOSS .015 REMAINING .035 AND FOUND OUT OF LIMITS IAW SRM 53-00-04SDR FDEA200910143571Floor Support · corrodedMAIN CABIN FLOOR STA 310.5 TO 324 RBL 30 HAS AREAS OF CORROSION AROUND NUT PLATES. (OUT OF LIMIT) REMOVED FLOOR SUPPORT (CHANNEL) IAW SRM 51-40-02. FABRICATED IAW SRM 51-10-02. INSTALLED NEW FLOOR SUPPORT (CHANNEL) STA 310-324, RBL 24, IAW SRM 51-40-02. SDR FDEA200910143570Floor Support · corrodedMAIN CABIN FLOOR STR 310.5 TO 324.0 RBL 45 HAS AREAS OF CORR AROUND NUT PLATES. (OUT OF LIMITS) REMOVED FLOOR SUPPORT IAW SRM 51-40-02. FABRICATED ON MAE TRAV NR T9/811142. INSTALLED NEW FLOOR SUPPORT AND STIFFENERS STA 310-324, RBL 45, IAW SRM 51-40-02. CSDR FDEA200910133551Crease Beam · corrodedLT CREASE BEAM CORRODED AT UPPER AND LWR SURFACE, BS 1540-BS1620 (OUT OF LIMITS). REMOVED CORROSION IAW SRM 51-10-02. ORIG MATERIAL THICKNESS; .070", AFTER REWORK; .059". FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FIG 101. REMOVED LH CREASE BEAM, BS 1370-1SDR FDEA200910133550Crease Beam · corrodedMAIN CABIN, STA 480, RT SIDE CREASE BEAM CHORD HAS CORROSION (OUT OF LIMITS). REMOVED CORROSION AND CHECKED LIMITS IAW SRM 51-10-02/53-30-13. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG.101,DETAIL 3 AT BS 450-665, RBL 60. ORIGINAL MATERIAL THICKNESS- .070SDR FDEA200910133549Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 365, RBL 24 TO 60 UPPER SURFACE CORRODED. BLENDED AREA IAW SRM 51-10-01 ORIG MAT .125 AFTER REWORK .108 OUT OF LIMITS IAW SRM 53-00-51, REMOVED DAMAGED AREA IAW SRM 53-00-51 REPAIR NR 3 , FABRICATED NEW CHORD FROM MAT ID NR BAC 1505-1SDR FDEA200910123543Floorbeam · corrodedMAIN CABIN FLOORBEAM, STA 440, LBL 62 HAS CORROSION AROUND SCREW HOLE. REMOVED CORROSION IAW SRM 53-00-51 2 BS 440, LBL 62, AND FOUND TO BE OUT OF LIMITS. ORIGINAL MATERIAL: .120", AFTER REWORK: .098". REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-02. THIS RE
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