Boeing 757-23A
Service difficulty reports · 1,397
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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 FDEA200903170940Floorbeam · dentedUPPER TEE OF CABIN FLOORBEAM CORRODED ON TOP AND ON LWR SURFACE UNDER ONE NUTPLATE (LBL 13) FS 365 LBL 25-RBL 5. INSTALLED UPPER TEE REPAIR IAW SRM 53-00-51 FIG 201. REPAIR NR 3. THIS IS A MAJOR REPAIR CATEGORY "A".SDR FDEA200903090873Seat Track · wornBS 377-440, LBL 24, SEAT TRACK REQUIRES REPLACEMENT PER CUSTOMER REQUEST. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK ASSY PER SRM 53-30- 52. LOCATED AND DRILLED IAW SRM 51-40-05. TREATED AND PRIMED PER SRM 51-20-01. INSTALLED NEW SEATSDR FDEA200903090872Seat Track · gougedBS 418-440, RBL 24, SEAR TRACK IS GOUGED. REMOVED DAMAGED AREA IAW SRM 53-00-53, FIG 101, DETAIL 1. GOUGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53, FIG 101, DETAIL 1. ORIGINAL MATL. .180 INCH; AFTER REWORK; .060 INCH. REMOVED SEAT TRACK, BS 418-440, RBL 2SDR FDEA200902090488Floorbeam · misrepairedEXISTING FLOORBEAM REPAIR LOCATED AT BS 1661, LBL 25-RBL 52, WL 208, UPON EVALUATION OF ATTACHMENT "B" OF EO F-5100-7-5001, PART 1, DOES NOT MEET SRM REQUIREMENTS. REPAIR ACCOMPLISHED DURING PTF CONVERSION, W/O 41399, AND MAE EA 757-5365-16- F1603, REV B. TSDR FDEA200902090487Floorbeam · misrepairedEXISTING FLOORBEAM REPAIR AT BS 1661, LBL 52, WL 208, UPON EVALUATION, OF ATTACHMENT "B" OF EO F-5100-7-5001, PART 1, REPAIR DOES NOT MEET SRM REQUIREMENTS. REPAIR ACCOMPLISHED DURING PTF CONVERSION, W/O 41399, AND MAE EA 757-5365-16- F1603, REV B. THIS SSDR FDEA200902090485Skin · damagedWS 776.5, RT WING LOWER SKIN, HAS A .185 INCH DIAMETER MIS-DRILLED HOLE IN THE -466 SKIN PANEL. REPAIRED DAMAGED AREA, WS 776.5, RT LOWER SKIN, IAW EA 757-5724-16-A1813 AND EA F- 5724-124060, DOUBLER REPAIR. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR RESDR FDEA200902040456Frame · dentedAFT CARGO COMPARTMENT FRAME AT STA 1220 STR 26R HAS DENT. REPAIRED FRAME IAW EA NR F-5310-124030 AND EA 757-5342-16-F1807. THIS REPAIR IS CATEGORY "A" MAJOR REPAIR.SDR FDEA200902040455Fitting · wornL-2 DOOR TOP DOOR STOP HOUSING AFT SIDE HAS WORN SPOT FROM CHAFING. BLENDED L2 DOOR TOP STOP FITTING, AFT SIDE, FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02 FIG 101 DET. XI. REMOVED DOOR STOP FTG IAW SRM 51-40-02. FABRICATED NEW DOOR STOP FITTING. INSTALLSDR FDEA200901280348Skin · crackedL4 DOOR INNER SKIN IS CRACKED, JUST BELOW HANDLE PAN. REPAIR ACCOMPLISHED IAW FEDEX EA F-5210-123960 AT L4 DOOR INNER SKIN. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.SDR FDEA200901270328Web · crackedR1 DOOR INNER WEB CRACKED, FWD SIDE, BELOW HANDLE. COMPLIED WITH MAE EA 757-5211-16-A1817, EA F-5210-124059, ON THE R1 DOOR, BS 332.05, AT BEAM NR 3. THIS DOUBLER REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.SDR FDEA200901230313Floorbeam · damagedEXISTING FLOORBEAM REPAIR AT BS 1640, LBL 52, WL 208, UPON EVALUATION OF EO F-5100-7-5001, PART 1, ATTACHMENT "B", DOES NOT MEET SRM REQUIREMENTS AND INTERFERES WITH PTF MODIFICATION. PERMANENT FLOORBEAM CAT "A" MAJOR REPAIRS ACCOMPLISHED PER MAE EA'S 757-536SDR FDEA200901090109Crease Beam · corrodedMAIN CABIN, STA 1220-1240, RT OTBD CREASE BEAM CHORD HAS CORROSION. COMPLIED REPAIR OF RT OTBD CREASE BEAM STA 1220-1240 IAW EA NR F-5310-123914. MAJOR REPAIR NO FOLLOW-UP REQUIRED.SDR FDEA200812175194Stringer · corrodedMAIN EQUIPMENT CENTER, ZONE 119, STA 420, S23L HAS CORROSION. REMOVED AND FABRICATED NEW STRINGER SECTION ON MAE TRAVELER NR T8/759394, DRILLED, TREATED, PRIMED AND INSTALLED NEW STRINGER SECTION ON S23L BETWEEN STA 395 TO 436 IAW SRM 51-40-02, SRM 53-00-03, SDR FDEA200812165179Crease Beam · corrodedMAIN CABIN FLOOR SUPPORT, RT CREASE BEAM, INBD CHORD, BS 600-620, HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. CORROSION OUT OF LIMITS PER SRM 53-30-13, DETAIL 2; D=.025". REMOVED AND REPLACED BS 600-620, RBL 63-70, INBD CREASE BEAM WEB, THAT WAS FABRSDR FDEA200812035072Shear Web · corrodedBS 1020, RBL 65, CREASE BEAM WEB IS CORRODED. REMOVED CORROSION, BS 1020, RBL 65, ON CREASE BEAM WEB IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13. L=.50, W=.50, D=.015. FABRICATED NEW WEB ON MAE TRAVELER T8/759905, TREATED, PRIMED WEB IAW SDR FDEA200812025046Floor Support · corrodedCABIN FLOOR, BS 310-324, RBL 43, CHANNEL IS CORRODED AROUND FASTENER HOLES. REMOVED FLOOR SUPPORT/CHANNEL IAW SRM 51-40-02. FABRICATED NEW SUPPORT/CHANNEL ON MAE TRAVELER T8/759071. TREATED, PRIMED AND TOP COATED NEW SUPPORT/CHANNEL IAW SRM 51-20-01 AND AMM SDR FDEA200812025044Floor Support · corrodedCABIN FLOOR, BS 297-310.5, RBL 30, CHANNEL CORRODED AROUND FASTENER HOLES. REMOVED FLOOR SUPPORT, BS 301-310.5, RBL 30, IAW SRM 51-40-02. FABRICATED NEW FLOOR SUPPORT (CHANNEL) ON MAE TRAVELER T8/759040. TREATED, PRIMED AND TOP COATED NEW SUPPORT/CHANNEL IASDR FDEA200812025042Floor Support · corrodedCABIN FLOOR, BS 297, RBL 20-36.2, CHANNEL IS CORRODED AROUND FASTENER HOLES. REMOVED FLOOR SUPPORT AT BS 297, RBL 20-36.2, IAW SRM 51-40-02. FABRICATED NEW SUPPORT ON MAE TRAVELER T8/759390. TREATED, PRIMED AND TOP COATED SUPPORT IAW SRM 51-20-01 AND AMM 51SDR FDEA200811184910Angle · crackedLT FUSELAGE FRAME RE-INFORCING ANGLE ( DOUBLER ) HAS A CRACK STA-700, LBL 65 WL-200. REMOVED FRAME RE-INFORCING ANGLE/DOUBLER IAW SRM 51-40-02, RECEIVED NEW ANGLE/DOUBLER AND INSTALLED IAW SRM 51-40-02AND DWG NR 143N1014. MAJOR REPAIR, NO FOLLOW-UP INSP REQUSDR FDEA200811184909Floorbeam · corrodedCABIN FLOORBEAM, STA 1661, LBL 58 TO RBL 58 HAS CORROSION AT SEVERAL PLACES. REMOVED AND REPLACED FLOORBEAM UPPER CAP AT STA 1661, LBL 58, RBL 58 IAW SRM 51-40-02 MAJOR REPAIR. NO FOLLOW-UP INSP REQUIRED.SDR FDEA200811184916Floorbeam · corrodedAFT CARGO COMPT, FLOORBEAM 1360, AT S-26L, IS CORRODED AND GOUGED. REPAIRED FLOORBEAM IAW SRM 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED AS A CAT. "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP REQUIREMENTS: INITIAL AT 37,500 FC; THEREAFTER EVERY 12,0SDR 08FDEA04918Skin · damagedPREVIOUSLY INSTALLED REPAIR, WS 823, WBL 740, TANK INTERNAL, RT WING, LOWER SURFACE, IDENTIFIED AS A TIME-LIMITED REPAIR. COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5100, PART 1. COMPLIED WITH ATTACHMENT "B" OF EO F-5100-7-5001, PART 1. REPLACED RT WING, LSDR 08FDEA04916Frame · corrodedAFT CARGO COMPT, FRAME 1360, AT S-26L, IS CORRODED AND GOUGED. REPAIRED FRAME, AFT CARGO COMPT, BS 1360, AT S-26L, IAW SRM 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED AS A CAT "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP REQUIREMENTS, INITIAL AT 37SDR 08FDEA04910Doubler · crackedLT FUSELAGE FRAME RE-INFORCING ANGLE (DOUBLER) HAS A CRACK BS-700, LBL 65 WL-200. REMOVED FRAME RE-INFORCING ANGLE/DOUBLER IAW SRM 51-40-02, RECEIVED NEW ANGLE/DOUBLER AND INSTALLED IAW SRM 51-40-02 AND DWG NR 143N1014 MAJOR REPAIR. NO FOLLOW-UP INSPECTION RSDR 08FDEA04909Floorbeam · corrodedCABIN FLOORBEAM STA 1661, LBL 58 TO RBL 58 HAS CORROSION AT SEVERAL PLACES. REMOVED AND REPLACED FLOORBEAM UPPER CAP AT STA 1661 LABL 58-RBL 58 IAW SRM 51-40-02, MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED.SDR FDEA200811124867Frame · damagedAFTER REMOVAL OF DOUBLER FROM TV MONITOR SPT AT BS 395, S-3L - S-3R, FOUND SEVERAL HOLES ON FRAME. COMPLIED WITH EA 757-2550-16-F1312, REV E, FRAME ALTERATION BS 395, B/T S-3L - S-3R. REMOVED SHEAR TIES AND STRINGER CLIPS PER EA STEP 2A1. REMOVED DAMAGE PSDR FDEA200811114855Frame · gougedAFT CARGO COMPT, BS 1480, S-23R - S-24R, BEAM HAS DEEP GOUGES. REPAIRED FRAME AFT CARGO COMPT, IAW SRM 53-00-07, REPAIR NR 5, DETAIL 3. THIS REPAIR IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP TRACKING REQUIREMENTS: INITIAL AT 37,5SDR 08FDEA04855Frame · damagedAFT CARGO COMPT, BS 1480, S-23R - S-24R, BEAM HAS DEEP GOUGES. REPAIRED FRAME/BEAM, BS 1480, S-23R - S-24R, AFT CARGO COMPT, IAW SRM 53-00-07, REPAIR NR 5, DETAIL 3. THIS REPAIR IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP TRACKISDR FDEA200811104839Skin · damagedWHILE DRILLING THE 311N5046-31 NR 1 PYLON OTBD SKIN 2 EA NUTPLATE ATTACH HOLES WERE OVERSIZED TO .250 DIA AT APPROX PPS 132 AND 1 EA HOLE WAS ELONGATED AT APPROX PPS 205.65 AND 2 EA HOLES DAMAGED IN LOWER CHORD AT PPS 174.30. COMPLIED WITH EA F-5450-124034 ANDSDR FDEA200811104838Skin · damagedWHILE REAMING THE -31 OTBD SKIN AND OTBD BATHTUB FITTING FOR THE NR1 PYLON SIP MOD F-5450-7-5003 A4 PT.5 1 EA. HOLE WAS OVERSIZED TO 0.390 DIA. AND COUNTERSUNK FOR A BACB30NW12K(*) X FASTENER. COMPLIED WITH EA F-5450-124034, 11/07/08 AND REPAIRED OVERSIZED HOSDR 08FDEA04839Skin · damagedWHILE DRILLING THE 311N5046-31 NR 1 PYLON OTBD SKIN 2 NUTPLATE ATTACH HOLES WERE OVERSIZED TO .250 DIAMETER AT APPROX PPS 132 AND 1 HOLE WAS ELONGATED AT APPROX PPS 205.65 AND 2 HOLES DAMAGED IN LOWER CHORD AT PPS 174.30. COMPLIED WITH FED EX EA NR F-5450-124SDR 08FDEA04838Skin · misrepairedWHILE REAMING THE -31 OTBD SKIN AND OTBD BATHTUB FITTING FOR THE NR 1 PYLON SIP MOD F- 5450-7-5003 A4 PT.5 1 HOLE WAS OVERSIZED TO 0.390 DIA AND COUNTERUNK FOR A BACB30NW12K(*) X FASTENER. COMPLIED WITH FEDEX EA NR F-5450-124034 11/07/08 AND REPAIRED OVERSIZSDR FDEA200811094822Skin · corrodedNR 2 NACELLE STRUT INTERNAL, INBD SKIN EXFOLIATED AT PP STA 166 APROX AND HAS CORROSION FROM PP STA 174-100 AT ACCESS DOORS CUT-OUTS. REMOVED AND REPLACED WITH A NEW SKIN PANEL PN 311N5046-33 "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.SDR FDEA200811094821Skin · corrodedNR1 STRUT OTBD SIDE SKIN CORRODED INSIDE ACCES PANEL 433CL REMOVED AND REPLACED WITH NEW SKIN PN 311N5046-31 IAW SRM 51-40-02 AND DWG 311N5002, "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.SDR FDEA200811094820Skin · corrodedNR 2 NACELLE STRUT, OTBD INTERNAL SKIN HAVE CORRODED SPOTS ALONG PYLON . REMOVED AND REPLACED NEW SKIN PN 311N5446-32 "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.SDR 08FDEA04822Skin · corrodedNR 2 NACELLE STRUT INTERNAL, INBD SKIN EXFOLIATED AT PP STA 166 APPROXIMATELY AND HAS CORROSION FROM PP STA 174-100 AT ACCESS DOORS CUT-OUTS. REMOVED AND REPLACED WITH A NEW SKIN PANEL P/N 311N5046-33 "A" MAJOR REPAIR. NO FOLLOW-UP INSPECTION REQUIRED.SDR 08FDEA04821Skin · corrodedNR 1 STRUT OTBD SIDE SKIN CORRODED INSIDE ACCESS PANEL 433CL. REMOVED AND REPLACED WITH NEW SKIN P/N 311N5046-31 IAW SRM 51-40-02 AND DWG 311N5002, "A" MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED.SDR 08FDEA04820Skin · corrodedNR 2 NACELLE STRUT, OTBD INTERNAL SKIN HAVE CORRODED SPOTS ALONG PYLON. REMOVED AND REPLACED NEW SKIN P/N 311N5446-32 "A" MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED.SDR FDEA200811084814Skin · corrodedNR1 STRUT CORROSION ON INNER AFT SKIN INBD SIDE. R & R INBD SIDE SKIN PANEL ASSY. IAW DWG N311N5002 AND SRM 51-40-02. OLD CONTROL NR: 08FDEA04814SDR 08FDEA04814Skin · corrodedNR 1 STRUT CORROSION ON INNER AFT SKIN INBD SIDE. REMOVED AND REPLACED INBD SIDE SKIN PANEL ASS'Y IAW DRAWING N311N5002 AND SRM 51-40-02.SDR FDEA200811064773Support Channel · corrodedFWD MAIN CABIN LT- INTERCOSTAL PLATE ABOVE FLIGHT CONTROL PULLEYS AT LBL 24.75 BAE STA 333.45 AND STA 350.00 IS CORRODED . REMOVED AND REPLACED FLOOR SUPPORT PN 141N5170-30 IAW SRM 51-40-02 FROM STA 324.0 - 345.0 LBL 24.75 "A" MAJOR REPAIR NO FOLLOW-UP REQUIRESDR 08FDEA04773Floor Support · corrodedFWD MAIN CABIN LT, INTERCOSTAL PLATE ABOVE FLIGHT CONTROL PULLEYS AT LBL 24.75 BS 333.45 AND STA 350.00 IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT P/N 141N5170-30 IAW SRM 51-40-02 FROM STA 324.0 - 345.0 LBL 24.75 "A" MAJOR REPAIR NO FOLLOW-UP REQUIRED.SDR FDEA200811054763Frame · damagedAFTER REMOVAL OF DOUBLER FROM TV MONITOR SUPPORT AT BS 1000, FOUND SEVERAL HOLES IN FRAME. REMOVED DAMAGED SECTION OF FRAME, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS, BS 1000, S-5L-R, IAW SRM 53-00-07, REPAIR NR 3. THIS REPAIR IS CLASSIFIED AS A CAT.SDR 08FDEA04763Frame · damagedAFTER REMOVAL OF DOUBLER FROM TV MONITOR SUPPORT AT BS 1000, FOUND SEVERAL HOLES IN FRAME. REMOVED DAMAGED SECTION OF FRAME, FABBED REPAIR PARTS AND INSTALLED REPAIR PARTS, BS 1000, S-5L - S-5R, IAW SRM 53-00-07, REPAIR NR 3. THIS REPAIR IS CLASSIFIED AS A CSDR 08FDEA04760Skin · corrodedNR 1 PYLON INBD AFT 311N5046-34 SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. REMOVED AND INSTALLED REPAIRED NR 1 PYLON INBD AFT SKIN PANEL ASSY IAW DWG 311N5002 AND SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKISDR 08FDEA04714Skin · chafedRT WING O/B MAIN FLAP O/B L/E CORNER HAS 4 INCH CHAFF MARK (FROM LOWER WING PANEL). DEFECT REPAIRED IAW EA F-5750-120571. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200811044713Web · damagedNR 2 PYLON CENTER WEB BETWEEN PPS 146-154 HAS HEAT DAMAGE. PREFORMED HARDNESS TEST ON NR 2 PYLON CENTER WEB IAW SRM 51-20-02, FIG 3 AND FOUND TO BE ABOVE LIMITS. COMPLIED WITH F-5450-123904A DATED 09/03/08. THIS IS CAT "A" REPAIR . "MAJOR REPAIR"SDR FDEA200811044712Web · wornNR 2 PYLON UPPER WEB AT PPS 146-154 HAS WORN AREA CAUSED BY LOOSE SUPPORT BRACKETS. BLENDED DAMAGED WORN AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL III COMPLIED WITH EA F-5450-123904A DATED 09/03/08. THIS IS A CAT "A" REPAIR. "SDR FDEA200810314649Frame · dentedFWD CARGO PIT, BS 720, AT S-23L, FRAME IS DENTED ON TOP SIDE. REPAIRED FRAME IAW SRM 53-00-07, REPAIR NR 5. REPAIR PARTS FABRICATED AND INSTALLED IAW SRM 51-40-02 AND 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR WITH THE FOSDR 08FDEA04649Frame · dentedFWD CARGO PIT, BS 720, AT S-23L, FRAME IS DENTED ON TOP SIDE. REPAIRED BS 720 FRAME AT S-23L, IAW SRM 53-00-07, REPAIR NR 5. REPAIR PARTS FABRICATED ON MAE TRAVELER T8/763002 AND INSTALLED IAW SRM 51-40-02 AND 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED
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