Boeing 757-26D
Service difficulty reports · 1,057
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 = '75726D' 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 = '75726D' 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 DALA2016041302917Skin · corrodedAFT FUSELAGE TAIL COMPARTMENT, BS 1883-1885, LBL10-RBL10, SKIN AND FASTENERS CORRODED. REMOVED SKIN STRAP AFT LOWER BS 1885, STR 25L TO 25R. ORIG MATERIAL THICKNESS .011" IAW DWG 148N3601, MATERIAL LOSS .025" FOUND OUT OF LIMITS IAW SRM 53-80-01, FIG 101. FASDR DALA2016041202827Power Supply · inoperativeDURING SERVICE CHECK, DR 4R, EXTERIOR EMERGENCY LIGHT NOT ILLUMINATE. TEST AND NO POWER AT L60 SOCKET IAW WDM 33-51-15, PG 4, SH2. REPLACED M736 POWER SUPPLY AND OPS CK OK IAW AMM 33-51-07.SDR DALA2016041002778Angle · corrodedCORROSION ON AFT CARGO LT INTERCOSTAL UPPER ANGLE BETWEEN BS 1480-1500, LBL 24.5 UNDER OTBD SIDE OF TRANSITION PANEL. REMOVED CORROSION ON AFT CARGO LT INTERCOSTAL UPPER ANGLE FOUND TO BE EXFOLIATED 50 PERCENT AND CRACKED OUT OF LIMITS IAW SRM 53-00-04. ALLOSDR DALA2016042003150Intercostal · corrodedCORROSION ON AFT CARGO BILGE INTERCOSTAL LOWER FLANGE BETWEEN BS 1300-1320, LBL-3. REMOVED CORROSION AT INTERCOSTAL LOWER FLANGE BETWEEN BS 1300-1320, LBL3. ORIGINAL MATTERIAL THICKNESS .032-MATTERIAL LOSS: 50 PERCNET =.016", FOUND OUT OF LIMITS IAW SRM 53-00SDR DALA2016040802776Crease Beam · corrodedUPON REMOVAL OF FLOORBOARD 230-41 IAW JIC 2020-2376 MAIN CABIN LT CREASE BEAM INBD CHORD CORRODED IN MULTIPLE SPOTS BETWEEN BS 800 AND BS 880. COMPLIED WITH ERA 544733-14, REV-0 PERMANENT REPAIR IN MAIN CABIN LT CREASE BEAM AT BS 760-898 INBD CHORD.SDR DALA2016040802773Floorbeam · corrodedCORROSION ON FLOORBEAM LOWER CHORD BS 310, LBL 51 TO LBL 60. COMPLIED WITH ERA 544723-14, REV ORIGINAL.SDR DALA2016040802728Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER TEE BS 310, LBL 17 TO LBL 21. COMPLIED WITH ERA 544722-14, REV ORIGINAL ON FUSELAGE FLOOR BEAM UPPER TEE AT BS 310.5, LBL 17-LBL 21.SDR DALA2016040502666Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK BS 1320-1350, RBL 24. BLENDED AND FOUND TO BE OUT OF LIMITS. ACCOMPLISHED PERMANENT REPAIR IAW SRM.SDR DALA2016040802774Intercostal · corrodedCORROSION ON AFT CARGO LT INTERCOSTAL UPPER ANGLE BETWEEN BS 1200 - 1220, LBL 24.5 JUST BELOW OTBD SIDE OF LT TRANSITION PANEL. REMOVED UPPER ANGLE IAW SRM 51-40-02, PG 1-10. LOCATED AND DRILLED UPPER ANGLE ON INTERCOSTAL IAW DWG 146N5390. INSTALLED NEW UPPSDR DALA2016040402561Skin · dentedLEFT INBD MAIN FLAP UPPER OTBD PANEL HAS CHAFE DAMAGE 0-36" FROM THE OTBD END. ACCOMPLISHED REPAIR, DAMAGE DIMENSION IS APPROXIMATELY 1" X 11" OF THE DISCREPANT AREAS ON LT INBD MAIN FLAP UPPER OTBD PANEL IAW ER/A 514121-14MA, ORIGINAL REVISION.SDR DALA2016040402560Skin · dentedLT WING INBD MAIN FLAP UPPER SURFACE HAS 2 GOUGED DENTS 53" FROM INBD END/ 19"-22" FROM T/E. ACCOMPLISHED PERMANENT REPAIR ON LT WING INBD MAIN FLAP UPPER SURFACE AT 2 EA GOUGED DENTS 53" FROM INBD END 19"-22" FROM T/E, DAMAGE AREAS MEASURED 2." DIA IAW SRM 5SDR DALA2016040102550Skin · damagedRT WING INBD MAIN FLAP UPPER SKIN HAS 2 EA CREASES 47"-49" FROM INBD END/ 18.5"-22.5" FROM T/E. ON RT WING INBD MAIN FLAP UPPER SKIN REPAIRED 2 EA CREASES 47"-49" FROM INBD END 18.5"-22.5" IAW SRM 51-70-10.SDR DALA2016040102549Skin · dentedLEFT WING INBD MAIN FLAP T/E WEDGE LOWER SKIN DENTED 63.5"-77" FROM OTBD END. ACCOMPLISHED REPAIR OT THE DISCREPANT AREA ON THE UPPER SURFACE, APPROX 1" X 10" AND THE LOWER SURFACE, APPROX 10" X14" OF THE LT WING INBD MAIN FLAP T/E WEDGE IAW SRM 51-70-10.SDR DALA2016033102483Connector · unsecure5D EMERGENCY PATH LIGHT INOPERATIVE. SECURED LIGHT CONNECTOR. OPS CK OK.SDR DALA2016050503752Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK SUPPORT BS 1640, RBL 24. REMOVED CORROSION ON SEAT TRACK SUPPORT AT BS 1640, RBL 24. MATERIAL LOSS IS .015". ORIGINAL MATERIAL THICKNESS IS .070" REF BAC1508-240/BOEING DWG 146N5126-2. FOUND TO BE OUT OF LIMIT IAW SRM 53-SDR DALA2016033102548Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK SUPPORT BS 1640, RBL 45. R & R NEW SEAT TRACK SUPPORT BETWEEN BS 1600-BS 1640, RBL 45 IAW DWG 146N5120.SDR DALA2016050503749Seat Track · gougedMAIN CABIN SEAT TRACK CROWN LBL 45 AT BS 1222 HAS A DEEP GOUGE. R & R NEW SECTION OF SEAT TRACK ON MAIN CABIN, LBL 45.5 FROM BS 1180 TO BS 1250 IAW BS SRM 53-00-52, REPAIR 3 OPTION 2. INSTALLED ID TAG IAW PS 900-5-1, NR 04.SDR IXXA20160401012Stop Fitting · defectiveL1 CREW DOOR HARD TO OPEN. INSTALLED STOP BLOCK FITTING IAW PRECISION AMM 52-12-00. OPERATIONAL CHECKED SATISFACTORY. FAULT NOT DUPLICATED. ACFT RELEASED TO SERVICE.SDR DALA2016032802349Skin · dentedRIGHT WING INBD MAIN FLAP T/E WEDGE LOWER SKIN DENTED 63.5 - 77" FROM OTBD END. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA ON RT WING INBD MAINFLAP T/E WEDGE LOWER SKIN IAW SRM 51-70-10.SDR DALA2016042903596Strap · corrodedCORROSION MAIN CABIN FLOOR STABILIZER STRAP, BS 740, LBL 26. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.SDR DALA2016032502343Seat Track · gougedMAIN CABIN SEAT TRACK CROWN LBL 45 AT BS 1545 HAS A DEEP GOUGED. BLENDED GOUGED ON MAIN CABIN SEAT TRACK CROWN AT BS 1545, LBL 45. MATERIAL LOSS OF 0.033", FOUND TO BE OUT OFF LIMITS IAW SRM 53-00-52. ALLOWABLE DAMAGE DETAIL 1., ACCOMPLISHED REPLACEMENT OF MSDR DALA2016032402333Skin · dentedRT T/E FLAP 20" FROM OTBD END 3" FROM T/E. T/E WEDGE UPPER SKIN HAS DENT. T/E WEDGE UPPER SKIN REPAIRED DENT IAW SRM.SDR DALA2016040502668Strap · crackedMAIN CABIN FLOOR STRUCTURE STABILIZER STRAP LBL 45, BS 365 CRACKED. REMOVED AND INSTALLED NEW SECCION OF STABILIZER STRAP AT MAIN CABIN FLOOR STRUCTURE STABILIZER STRAP, LBL 45, STA 365.25 TO STA 377.7 IAW SRM.SDR DALA2016040502667Strap · crackedMAIN CABIN FLOOR STRUCTURE STABILIZER STRAP BS LBL 26, BS 365 TO BS 377 CRACKED MIDSPAN. REMOVED AND INSTALLED NEW SECTION OF STABILIZER STRAP AT MAIN CABIN FLOOR STRUCTURE STABILIZER STRAP AT MAIN CABIN FLOOR STRUCTURE STABILIZER STRAP, LBL 26, BS 365.25 TO SDR DALA2016032302258Cable · out of limitsL-1 PASSENGER DOOR EMERGENCY ACTUATION CABLE SYS FAILED TRAVEL CHECK IAW CARD 5211-3001-1L, STEP 4. ADJUSTED L-1 DOOR EMERGENCY ACTUATION CABLE IAW AMM 52-11-32-404-010 PAR E 16, CABLE TRAVEL CHECK GOOD 0.95.SDR DALA2016031902176Support Strap · corrodedCORROSION ON SUPPORT STRAP BS 1681, BL0. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED.SDR DALA2016041302938Support · corrodedCORROSION ON MAIN CABIN BOX BEAM SUPPORT LBL 52, BS 1678. R & R THE SUPPORT IAW SRM'S 51-40-02, PG 31 AND 51-40-02, PG 21.SDR DALA2016031802178Stop Fitting · out of limitsDOOR R1 ESCAPE SLIDE KNUCKLE KNOCKER NOT FULLY EXTENDED WHEN DOOR ARMED. FOUND LOWER STOP THAT SETS OUT DIM, LOOSE TIGHTENED SAME IAW MM 52-11. OPS CK GOOD.SDR DALA2016031402179Charger · inoperativeEMERGENCY EXIT LIGHTS IN SEATS INOPERATIVE FROM ROWS 32-42. R & R BATTERY PACK AND CHARGER IAW AMM 33-51. OPS CK GOOD.SDR DALA2016032902430Nut · corrodedNR 6 T/E FLAP TRACK BALL NUT TRUNNION HAS CORROSION AND BOTH BALLNUT BUSHING ARE WORN OUT OF LIMITS. REMOVED RT WING NR 6 T/E FLAP BALL SCREW IAW AMM 27-51-11-029-001. INSTALLATION OF SERVICEABLE NR 6 T/E FLAP BALLSCREW AND 2 EA NEW BALLNUT BUSHINGS AND TESTSDR DALA2016032802339Ball Screw · spalledLT WING INBD FLAP OTBD BALLSCREW THREADS SPALLING AND BALLNUT GREASE FILLED WITH RUST. R & R INBD FLAP, OTBD BALLSCREW IAW AMM 27-51.SDR DALA2016032402335Ball Screw · corrodedLT WING INBD MAIN FLAP INBD BALLSCREW NUT CORRODED AND BUSHINGS ARE WORN. R & R LT WING INBD MAIN FLAP INBD BALLSCREW AND 2 EA NEW BUSHINGS WILL BE ACCOMPLISHED ON T/C 2751-2538.SDR DALA2016032402334Ball Screw · corrodedNR 5 T/E FLAP BALL NUT TRUNNION HAS CORROSION AND BOTH BALL NUT BUSHINGS ARE WORN OUT OF LIMITS. R & R RT WING NR 5 T/E FLAP BALLSCREW IAW AMM 27-51. NEW BUSHINGS WILL BE ACCOMPLISHED ON T/C 271-2542.SDR DALA2016031001831Heater · failedNOTICED ORANGE GLOW ON LOWER L1 WINDOW, LT WINDOW SHATTERED, THEN LT WINDOW HEAT MSG ILLUMINATED. R & R L1 & R1 WINDSHIELD IAW AMM 56-11. C/W TORQUING AND AERODYNAMIC SEALING. ALSO R & R LT AND RT WHC IAW AMM 30-41. PERFORMED BITE, NO FAULTS AT THIS TIME, ASDR DALA2016030401793Skin · puncturedRT WING INBD MAIN FLAP UPPER SKIN PUNCTURED 62" FROM INBD END/ 13" FROM T/E. ACCOMPLISHED REPAIR OF RT WING INBD MAIN FLAP UPPER SKIN, APPROXIMATELY A .5" CIRCLE, 62" FROM THE INBD END AND 13" FROM THE T/E IAW SRM 51-70-17.SDR DALA2016030301789Counterbalance · unknownL4 DOOR COUNTER BALANCE MAKES A POPPING SOUND WHEN OPENED. R & R L-4 DOOR COUNTER BALANCE IAW AMM 52-11-11-004-001 AND 52-11-11-404-007.SDR DALA2016030301788Counterbalance · unknownL1 DOOR MAKES A POPPING SOUND WHEN DOOR IS OPENED AND CLOSED, FOUND AFTER SLIDE INSTALLATION. R & R COUNTER BALANCE AT L-1 DOOR TORQUE TUBE BODY IAW AMM 52-11-11-004-001 AND 52-11-11-404-007, OPS CHECK GOOD, NO POPPING SOUND NOTED, DOOR ADJUSTMENT, ACCOMPLISHSDR DALA2016022901622Skin · puncturedLT WING INBD MAIN FLAP UPPER SURFACE PUNCTURED 53" FROM INBD END 14" FROM T/E. ON LT WING INBD MAIN FLAP UPPER SURFACE 53" FROM INBD END 14" FROM T/E. REPAIRED IAW SRM 51-70-17, REPAIR 4B, FIG 24.SDR DALA2016022701567Floorbeam · corrodedCABIN FLOORBEAM BS 365, RBL 1 - 50, TOP SURFACE HAS CORROSION AND CUTS. BLENDED AND REMOVED CORROSION TOP SURFACE IAW SRM 53-00-51, FIG 101 ALLOWABLE DAMAGE DETAIL IV. ORIGINAL MATERIAL THICKNESS .125" IAW DWG BAC 1518-338. MATERIAL LOSS .030. FOUND OUT OFSDR DALA2016022701566Stringer · damagedWHILE WORKING, NR 100-41, FOUND DOUBLE DRILLED HOLE THRU STR 28R AT BS 1320. ACCOMPLISHED PERMANENT REPAIR ON BS 1320, STR 28R IAW ER/A 542500-14, REV ORIGINAL. TRACKING OF REPAIR TO BE ACCOMPLISHED.SDR DALA2016021000994Ball Screw · corrodedLEFT WING, OTBD FLAP, OTBD BALLSCREW NR 1 HAS CORROSION INSIDE THE BUSHING POST. PROCURED LT WING OTBB FLAP OTBD BALLSCREW NR 1 POSITION PN 7900067, SN 4114, REMOVAL, INSTALLATION, AND OPS CHECK COMPLIED WITH ON NR 2751-2538. REMOVED LT WING OTBD FLAP OTBD BASDR DALA2016020901019Skin · damagedRT WING INBD FLAP PANEL NR 655BT HAS HONEYCOMB DAMAGE ON EDGE OF LOWER SECTION. REPAIRED PANEL 655BT RT WING INBD FLAP IAW SRM 51-70-10. SEALANT IAW SRM 51-21-05.SDR DALA2016020401033Skin · damagedRT WING INBD MAIN FLAP UPPER SKIN PANEL, INNER HONEYCOMB EDGES DAMAGED AT NUMEROUS LOCATIONS ON RT WING. SKIN PANEL REPAIRED IAW SRM 51-70-10.SDR DALA2016030401791Frame · corrodedCORROSION ON FUSELAGE FRAME AT AFT CARGO COMPARTMENT, BS 1320, FWD SIDE, BETWEEN STR 27R AND 28R. REMOVED CORROSION ON FRAME AT BS 1320, STR 27R-28R IAW SRM 53-00-07, FIG 101. ORIGINAL MATERIAL THICKNESS .071" IAW SRM 53-60-07, FIG 1 AND DWG 146N1028. MATERSDR DALA2016020301027Frame · dentedTHREE DENTS ON FWD CARGO LT FRAME UPPER FLANGE AT BS 660 BETWEEN STR 23L AND 25L. DENTS NOT ALLOWED AND FOUND OUT OF LIMITS IAW SRM 53-00-07 ALLOWABLE DAMAGE 1. REPAIRED THE FRAMEIAW SRM 53-00-07, REPAIR 5, FIG 201.SDR DALA2016021801377Connector · inoperativeLOWER RED STROBE LIGHT HAS CORROSION ON JACK AND MATING CONNECTOR. R & R LWR RED STROBE LT ASSY AND HARNESS IAW AMMS 33-44-02-002-007 AND 33-44-02-402-012, OPS CHECK DUE. OPS CHECK GOOD LOWER ANTI-COLLISION LIGHT IAW AMM 33-44-02-712-014.SDR DALA2016012600666Frame · dentedTWO DENTS ON FWD CARGO LT FRAME AT BS 580 BETWEEN STRINGERS 23-25L. TRIMMED-OUT THE DENTS AT FWD CARGO FRAME IAW SRM 53-00-07, REPAIR 5, PG 201. REPAIRED IAW SRM 53-00-07, REPAIR 5.SDR DALA2016012600639Floorbeam · corrodedCABIN FLOORBEAM, BS 377.7/LBL 61-RBL10, TOP SURFACE CORRODED AND HAS TOOLING MARKS/CUTS CP53-221-01L. REMOVED CORROSION ON FLOORBEAM TOP SURFACE AT BS 377.7, LBL 61 TO RBL 10 IAW SRM 53-00-51, FIG 101. ORIG MAT .125", MATERIAL LOSS AT LBL 20 TO LBL61 MEASURESDR DALA2016012100511Frame · dentedTWO DENTS ON AFT CARGO FUSELAGE FRAME AT BS 1400 AT AND JUST BELOW STR 23L. NO DENTS ALLOWED ON FRAME FLANGE IAW SRM 53-00-07, FIG 101, ALLOWABLE DAMAGE 1. REPAIRED FRAME AT BS 1400 BELOW STR 23L IAW SRM 53-00-07, REPAIR 5. REPAIR IS PERMANENT CAT "B" ZONE 1SDR DALA2016012200533Frame · corrodedAFT CARGO BS 1540 BETWEEN STR 28R-29R, FRAME FWD SIDE HAS CORROSION AT PREVIOUS BLEND AND CORROSION AT AFT SIDE SHEAR TIE. R & R SHEAR TIE AT BS 1540 BETWEEN STR 28R-29R IN REF TO SRM 51-40-02, PAGE 4-7. DWG NR 140N2002, ORIGINAL MATERIAL ON THE FRAME BS 154
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