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 FDEA201011304518Cusp Web · corrodedLT SIDE CUSP WEB BETWEEN FR 1140 &FR 1160 HAS CORROSION ON UPPER SURFACE REMOVED CORROSION IAW 51-10-02 SHEAR WEB AND WEB OUT OF LIMITS IAW SRM 53-40-13 FIG-101, DETAIL III. INSTALLED NEW SHEAR WEB AND WEB ON TRAVLERS T10/858934 AND T10/858933. REINSTALLED ASDR FDEA201011304526Seat Track · corrodedSEAT TRACK AT RBL 24 AHS CORROSION ON UPPER SURFACE AT BS 365. REMOVED CORROSION ON SEAT TRACK SUPPORT AFTER BLEND OUT OF LIMITS IAW SRM 53-00-52, FIG 101 DETAIL XIK. ORGINAL MAT.080 AFTER REWORK .040 EXCEEDS REMOVE SEAT TRACK SUPPORT IAW SRM 51-40-02. FABRICSDR FDEA201011304523Seat Track · corrodedCORROSION ON SEAT TRACK STA 1640 RT SIDE AT END OF TRACK MAIN CABIN. REMOVED CORROSION ON SEAT TRACK STA 1640 RBL 45. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101, DETAIL VII. ORIG MATERIAL .070 AFTER REWORK .025. R & R SEAT TRACK IAW SRM 51-40-02. SDR NOCA07010Light · inoperativeE-PATH LIGHTS INOP BY DOOR 2L. REPLACED LIGHT AS PER MM 33-51-01, OPS CHECK OK.SDR FDEA201011294510Seat Track · corrodedSEAT TRACK CORRODED AT STA 440 RBL 24.75 ORIGINAL MATERIAL .070 REMOVED .060 REMAINING MATERIAL .010 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG. 101 DETAIL VII PAGE 104 REMOVED AND REPLACED SEAT TRACK IAW SRM 50- 40-02 PN BAC 1520-792 BATCH 0001904663 FROSDR NOCA06910Transcowl · damagedAIRCRAFT IS IN LGA AND IS ON AOG STATUS DUE TO NR 2 ENGINE T/R TRANSLATING COWL DAMAGE IN LGA IS MX REP AND CURRENTLY AT REST UPON ARRIVAL IN LGA FOUND DAMAGE TO NR 2 OUTBOARD T/R TRANSLATING SLEEVE AT THE 5 O'CLOCK POSITION DAMAGE DIMENSIONS ARE 11 INCHES IN SDR NOCA069Transcowl · damagedAIRCRAFT IS IN LGA AND IS ON AOG STATUS DUE TO NR 2 ENGINE T/R TRANSLATING COWL DAMAGE IN LGA IS MX REP AND CURRENTLY AT REST UPON ARRIVAL IN LGA FOUND DAMAGE TO NR 2 OUTBOARD T/R TRANSLATING SLEEVE AT THE 5 O'CLOCK POSITION DAMAGE DIMENSIONS ARE 11 INCHES IN SDR FDEA201011164396Floorbeam · corrodedAT STA 1681, FLOORBEAM HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE OF FLOOR. REMOVED CORROSION IAW SRM 51-10-01 FOUND FLOOR BEAM OUT OF LIMITS ORIG. MAT 0.150 AFTER BLEND OUT THE WORST SPOT 0.091 IAW SRM 53-00-51 DETAIL VI. REMOVED AND REPLACED FLOORBEASDR FDEA201011164397Floorbeam · corrodedCORROSION ON FLOORBEAM STA 1661, RBL 42, RT SIDE MAIN CABIN. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 DETAIL II FABRICATED FLOORBEAM 1661 FROM MAT BAC1518-338 BATCH 1915536 LOCATED AND DRILLED IAW SRM 51-40-05. REMOVED AND REPLACED IAW SRM 51-49-0SDR FDEA201011164398Floorbeam · corrodedCORROSION ON FLOORBEAM STA 1640, FROM RBL 62 TO LBL 62, MAIN CABIN. REMOVED CORROSION AT FLOORBEAM, STA 1640 FROM RBL 62 TO LBL 62, MAIN CABIN IAW SRM 53-00. ORIGINAL MATERIAL .130, AFTER REWORK .095, AMOUNT OF MATERIAL REMOVED TO BE IN OUT OF LIMITS IAW SRMSDR FDEA201011124325Crease Beam · corrodedCORROSION ON FLOOR STA 1345, LBL 62, MAIN CABIN. REMOVED CORROSION ON LT SIDE INBD CREASE BEAM CHORD STA 1292-1370 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL VIII. ORIG MATERIAL .070 AFTER REWORK .045. R & R CHORD IAW SRM 51-40-02. CLSDR FDEA201011064268Sensor · failedLT ENTRY DOOR SLIDE INTERMITT SLIDE INDICATOR. LIGHT FLASHED ON AND OFF WHEN F/O WENT TO DISARM SLIDE AFTER FLIGHT. R & R AFT GIRTH BAR PROX SWITCH S10215 IAW AMM 25-66-11-2. OPS CHECK GOOD. (CLOSED)SDR FDEA201011064266Cusp Web · corrodedCUSP WEB BETWEEN FR1600 AND FR1620 HAS CORROSION ON UPPER SURFACE LBL 62. REMOVED CORROSION ON WEB IAW SRM 51-10-02, CHECKED LIMITS L=4",W=3", D=.020",MAT ORIG .040 IAW SRM 53-60-13, DET VI, OUT LIMITS IAW SRM 53-60-13, PG 103, DET III, R &R WEB IAW SRM 51-4SDR FDEA201011054261Frame · gougedFRAME 1280 IS GOUGED JUST BELOW STR S-11L.SDR FDEA201011054260Seat Track · corrodedSEAT TRACK AT RBL 48 HAS CORROSION ON UPPER SURFACE AT BS 365. REMOVED CORROSION ON SEAT TRACK SUPPORT AFTER BLEND OUT OF LIMITS IAW SRM 53- 00-52 FIG 101 DETAIL VII. ORIGINAL MAT .080" AFTER REWORK .48" EXCEEDS. REMOVED SEAT TRACK SUPPORT IAW SRM 51-40-02SDR FDEA201011054259Floorbeam · corrodedBS 365, FLOORBEAM HAS CORROSION ON UPPER SURFACE FROM BL 0.0 TO RBL 65.0. AREA OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. ORIG MAT .125. AFTER REWORK .095 AREA OF DAMAGE L(.5") X W(2"). R & R UPPER T-CHORD IAW SRM 53-00-51. REPAIR NR3 FROM LBLSDR FDEA201011054258Floorbeam · corrodedBS 345 FLOORBEAM HAS CORROSION ON UPPER SURFACE AT RBL 2.0. AREA OUT OF LIMITS IAW SRM 53-00-51, FIG 101. AFTER REWORK .101, AREA OF DAMAGE L(2.5") X W(2"). R & R UPPER T-CHORD IAW SRM 53-00-51, REPAIR 3, FROM RBL 35 LBL 50. BS 345. CATEGORY "A" REPAIR. MAJOSDR FDEA201010284245Skin · dentedDENT IN FUSELAGE SKIN AT STATION 475, STR 19L. EVALUATED DENT AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101, TRIMMED OUT DAMAGE AND FABRICATED REPAIR DOUBLER AND REPAIR FILLER 2 AND STRUCTURAL FILLER IAW EA F-5330-143914. TREATED, PRIMED AND INSTALLED REPASDR FDEA201010284188Crease Beam · corrodedCORROSION STA 1180, LBL 62, W/L 208 CREASE BEAM. REMOVED AND REPLACED NEW CREASE BEAM IAW SRM 51-40-02 AND SRM 51-40-05, FABRICATED ON BATCH 0001879122, MAJOR REPAIR .SDR FDEA201010284190Structure · corrodedCORROSION BETWEEN STA 1040 AND STA 1020 RBL 62 W/L 208 4EA SPOTS MAIN CABIN. REMOVED CORROSION AT INNER CHORD IAW SRM 51-10-02. ORIG. MAT. .070" IAW DWG BAC1515-551 MAT. LOSS D=.030" L=4.200 W=1.00" MAX. MAT. REMOVE ALLOWABLE IS .007", FOUND OUT LIMITS IAW SSDR FDEA201010284191Seat Track · corrodedCABIN FLOOR BS 440 TO BS 640 SEAT TRACK RBL 46 IS WORN/SCRATCH AND CORRODED IN SEVERAL PLACES AS MARK. BLENDED ARE IAW SRM 51-10-02,MAT ORIG ORIG .O70 MAT LOSS L=1.50",W=1",D=.026 OUT OF LIMITS IAW SRM 53-10-52 FIG 101 DETAIL III, REMOVED SEAT TRACK IAW SRMSDR FDEA201010284189Floorbeam · corrodedBS 324 FLOORBEAM HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEEN BL 0 AND RBL 40. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101. ORIG MATERIAL .125 AFTER REWORK .085. R & R UPPER CHORD RBL 62 TO LBL 62 IAW SRM 51-40-02. CLASSIFIED CATEGORY "ASDR NOCA06810Light · inoperativeR4 EMERGENCY EXTERIOR LIGHT INOP. RELAMPED R4 EMERGENCY LIGHT PER MM 33-51-00, OPS CHECK GOOD.SDR FDEA201010174095Relay · malfunctionedJUST AFTER TAKEOFF, APPROXIMATELY 800'AGL, RECEIVED F/O PITOT, TAT, R ENG EEC AND L ENG EEC EICAS. RAN THE QRH CHECKLIST AND RTB. ALSO L NAV PORTION OF FMS WOULD NOT FUNCTION REFERENCE WRI'S: 22-10/0799 AND 30-30/0798; SEPARATED F/O PITOT AND TAT AS SEPARASDR CNMA20100030Skin · delaminatedRT OTBD, AFT FLAP HAS 17 X 38 IN SECTION OF SKIN MISSING FROM INBD LOWER SURFACE. NO DAMAGE NOTED ON AFT FUSELAGE OR TAIL SURFACE. COMPLIED WITH R & R OF RT OTBD AFT FLAP IAW AMM 27-51-22.SDR NOCA06010Autothrottle Sys · malfunctionedREJECTED TAKEOFF, AUTOTHROTTLE ENGAGED NO AUTO THROTTLE INDICATION. REJECTED TAKEOFF AT 60 KTS. INSPECTED A/C NO ABNORMALITIES FOUND PREFORMED FIM PROCEDURES PER 22-00-02 AND 22-32-00 NO FAULTS NOTED THROUGH THE FIM PROCEDURES. DEFERRED THE THRUST MANAGEMENSDR NOCA05810Battery Pack · dischargedOVERHEAD EMERGENCY LIGHTS BY THE 3L AND 3R DOOR INOP. REPLACED EMERGENCY LIGHT BATTERY PACK AS PER MM 33-51-07, OPS CHECK OK.SDR FDEA201007152627Frame · misrepairedEXISTING FRAME REPAIR AT STA 1460 IS IAW SRM 51-70-11, FIG 1. REPAIR AND FOUND REPAIR WAS NOT COMPLIANT WITH SRM SPECIFIC REPAIR. REMOVED EXISTING IAW SRM 51-40-02. FABED REPAIR SPLICE ON STAM TRAVELER T10/844785. REPAIRED FRAME AT STA 1460 BETWEEN S-25L TOSDR 22AA201000072Engine · flamed outLT ENGINE FLAME OUT DURING CRUISE. PERFORMED IN FLIGHT START CHECK LIST, ENGINE RELIT, NO FURTHER PROBLEMS. DRAINED AND INSPECTED ALL ACFT FUEL TANKS SUMP IAW MM 12-11-03, ALSO PERFORMED LT ENGINE LP FUEL FILTERS BOWL INSP IAW MM 73-11-10. OPS CHECKED NORMAL DSDR NOCA04110Impeller · defectiveRT CENTER FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED AND EICAS MSG CTR FUEL PUMP DISPLAYED. OCCURRED ON INITIAL ROTATION. TROUBLESHOT RT CTR FUEL PUMP PER FIM 28-22-00. REMOVED AND REPLACED RT CTR OVERRIDE PUMP MOTOR IMPELLER IAW AMM 28-22-03-004-027 AND 28-SDR CNMA20100025Lever · out of adjustR-1 DOOR EMERGENCY ESCAPE SLIDE BLEW (REF OAI W/C 75TC-0893) R&R R-1 DOOR EMERGENCY ESCAPE SLIDE IAW MM 25-66 & OAI W/C 75TC-0893. CHECKED R-1 DOOR EMERGENCY MECHANISM IAW MM 52-11-20, FOUND MODE SELECTOR LEVER OUT OF ADJUSTMENT, ALSO RETRACTABLE DOOR (KNUCKLESDR NOCA04010Circuit Breaker · pulledLEFT FWD FUEL BOOST PUMP C/B POPPED. C/B INADVERTENTLY PULLED DURING PREVIOUS MAINTENANCE RESET BREAKER, OPS CHECK GOOD.SDR FDEA201005201593Floor Support · corrodedAFT CARGO COMPARTMENT FS 1600 FLOOR SUPPORT FRAME CORRODED IN NUMEROUS AREA. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. FABRICATED REPAIR ANGLE TRAV T10/814423, IAW EA F-5310-139137. INSTALLED FUSELAGE FRAME INNER CHORDSDR FDEA201005191579Frame · damagedSTA 640, ABOVE STR 26L FRAME HAS A ELONGATED HOLE AT STA 640 ABOVE STR 26L FRAME REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE P TO F CONVERSION ON MAE MOD W/C NR 118250068DSSR06 AND MAE EA NR 757- 5332-16-F2479, REV A, DATED JAN 5, 2010. THIS NONSDR FDEA201005191578Stringer Clip · missingSTRINGER CLIPS MISSING AT STA 395-418, 3R AND 6R AT STA 395-418, STR 3R AND 6R, STRINGER REPAIR/CLIP INSTALLATION WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE P TO F CONVERSION, ON WORK MAE W/C 118450525AZD, AND MAE EA NR 757-5311-16-F2612 DATED APRIL 9, SDR FDEA201005181571Structure · unknownUNABLE TO INSTALL 657N4422-1 GUTTER ASSY DUE TO 2EA. 4.60"X7.10" RECTANGULAR CUT OUTS, COMMON TO THE AFT SHEAR DECK AT BS 1710-1720, RBL 40 TO RBL 10. BS 1710 -1720, RBL 10 TO RBL 40, A WEB REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSDR FDEA201005181570Fitting · damagedPOTENTIAL SHORT EDGE MARGIN CONDITIONS IN THE 657N3161-12 FITTING DUE TO INCOMING FASTENER HOLE LOCATIONS AT BS 1640, BETWEEN S17R/ 18R. BS 1640, BETWEEN S17R/ 18R, POTENTIAL SHORT EDGE MARGIN CONDITION COMMON TO THE 657N3161-12 FITTING, DUE TO INCOMING FASTSDR FDEA201005181568Fitting · misinstalledPOTENTIAL SHORT EDGE MARGIN CONDITIONS IN THE 657N3161-11 FITTING DUE TO INCOMING FASTNER HOLE LOCATIONS AT STA 1640 BETWEEN STR 14L & STR 18L STA 1640, BETWEEN STR 14L & 18L - POTENTIAL SHORT EDGE MARGIN CONDITION COMMON TO THE 657N3161-11 FITTING DUE TO INSDR 22AA201000071Bulb · failedLEFT GEAR DOWN LIGHT FAILED TO ILLUMINATE WITH GEAR HANDLE DOWN. RELAMPED LT LANDING INDICATOR LAMPS AND RESECURED SOCKET INDICATOR IAW AMM 33-14-00, PERFORMED SYS OPERATIONS IAW AMM 32-61-00 SYS OPS CKD OK.SDR FDEA201005081487Frame · gougedFUSELAGE FRAME INNER CHORD GOUGED STA 1280 ABOVE S13R. FRAME REPAIR AT STA 1280 ABOVE STR 13R, INNER CHORD WAS ACCOMPLISHED IAW F-5310-139133. REPAIR ANGLE FABRICATED ON TRAVLER T10/815580 IAW SRM 51-70-11. REF FAA FORM 8100-9 DATED MAY 11, 2010. - FIRST SSDR FDEA201005061469Support · misalignedAFT OXYGEN CYLINDER AT STA -680 TO 700 DOES NOT HAVE SUFFICIENT CLEARANCE BETWEEN CYLINDER AND ADJACENT STRUCTURES AFT OXYGEN CYL AT STA 680 TO 700 CLEARANCE BETWEEN CYL AND ADJACENT STRUCTURES REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING ACCOMPLISHMSDR NOCA03710Battery Pack · dischargedEMERGENCY LIGHTS OUT AT 11DEF 2 EXIT SIGNS BY DOOR 2R AND EXTERIOR LIGHT AT R2. ACCOMPLISHED FIM TASK 33-51-00, REPLACED BATTERY PACK/CHARGER AS PER MM 33-51-07.SDR NOCA03610Battery Pack · dischargedEMERGENCY EXTERIOR EXIT LIGHTS INOP DOOR 1L/4L/2R/3R INTERIOR LIGHTS INOP 1AC-3AC AND 22FED-29FED AND INTERIOR EXIT SIGN AT EMERGENCY EXIT DOOR 3R. TROUBLESHOT PER FIM 33-51-00 REPLACED BATTERY PACK/CHARGER AT 1L AND 3R AS PER MM 33-51-07.SDR NOCA03410Battery Pack · dischargedEMERGENCY LIGHTS INOP OVER SEATS 1AC 3AC. REPLACED BATTERY PACK AS PER MM 33-51-07.SDR NOCA03310Battery Pack · dischargedSEVERAL EMERGENCY LIGHTS OUT ON RIGHT SIDE OF A/C AT RIGHT EMERGENCY EXIT DOOR. REPLACED BATTERY PACK AT R3 DOOR, CHECK GOOD PER MM 33-51-07.SDR NOCA03210Battery Pack · dischargedTHE 1R EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY PACK AS PER MM 33-51-07.SDR FDEA201004211267Frame · corrodedAFT FUSELAGE ACCESS DOOR (313AL) CUTOUT, AFT FRAME, BS 1882, HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02, FIG. 101, DETAIL 4, PAGE 104; ORIGINAL MATERIAL THICKNESS: .120", REMAINING MATERIAL AFTER REWIRK: .115"; L=2",W=.400",D=.005"SDR FDEA201004141192Frame · crackedFRAME AT STA 395.5, STR 6R IS CRACKED AT STRINGER CLIP HOLE. CRACK ON FRAME BS 395, S6R, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG.101, NOTE "A". FABRICATED NEW FRAME SEGMENT ON TRAVELER NR T10/828685. INSTALLED NEW FRAME SEGMENT AT BS 395, S4-10R, ISDR FDEA201004071094Skin · gougedFUSELAGE EXTERNAL SKIN HAS A GOUGED ON, TWO (2) PLACES APPROX 12 INCHES IN LENGTH BET FS 760 TO 800, S3R TO S4R. FUSELAGE SKIN WAS REPAIRED ON MAE N/R 43024770001 IAW MAE EA NR 757-5331-16-F2493, DATED JAN 15 2010, REV - TITLE, 2 GOUGES ON THE CROWN SKIN AT SDR FDEA201003311038Skin · corrodedINTERIOR SKIN CORRODED AT STA. 836 BETWEEN STR 16L AND 17L JUST ABOVE CREASE BEAM DAMAGE ON SKIN STA 836 BETWEEN STR 16L & 17L AND FOUND OUT OF LIMITS IAW SRM 53-00-01 DET II P. 104 FIG 101. ORIG MAT .060 REMOVED .045 MAT REMAINING .015. REPAIRED SKIN STA 83
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