Boeing 757-2B7
Service difficulty reports · 3,730
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 = '7572B7' 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 = '7572B7' 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 AALA201903199021Shear Tie · corrodedCORROSION FOUND ON THE SHEAR TIE AT BS 1540, BETWEEN STRINGER 28L & 29L. REPLACED THE SHEAR TIE IAW SRM 53-60-07-01-1, AND SRM 51-40-02.SDR AALA201903069010Plate · inoperativeEMERGENCY LIGHT SWITCH LIGHT PLATE WAS INOPERATIVE ON THE COCKPIT OVERHEAD PANEL. REPLACED THE EMERGENCY LIGHT SWITCH LIGHT PLATE IAW AIPC 33-13-01-02, AND AMM 33-13-01-401. PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-13-01-404-006, SUBTASK 714-009SDR AALA201903198007Skin · corrodedCORROSION FOUND ON THE FUSELAGE SKIN AT BS 1540, STRINGERS 28L - 29L. REPAIRED THE SKIN IAW SRM 53-00-01-2R-3, REPAIR 3.SDR AALA201902229020Strap · crackedCRACKED FLOORBEAM STABILIZER STRAP AT BS 377.7, LBL 24.75. REPLACED THE STRAP IAW SRM 53-10-51-2R-1.SDR AALA201902219003Stringer · corrodedCORROSION FOUND ON STRINGER 29, BETWEEN BS 1620 AND 1640. REPAIRED THE STRINGER IAW EA 289704.SDR AALA201902209014Transition Panel · corrodedCORROSION FOUND ON THE AFT CARGO RIGHT TRANSITION PANEL, BS 1440 AND 1520. REPLACED THE TRANSITION PANEL IAW SRM 53-00-53-2R-2, AND 51-40-02-0G.SDR AALA2019021539013Transition Panel · corrodedCORROSION ON THE AFT CARGO COMPARTMENT RIGHT SIDE TRANSITION PANEL BETWEEN BS 1310 AND 1380. REPLACED THE TRANSITION PANEL IAW SRM 51-40-02.SDR AALA2019021539015Floorbeam · crackedAFT CARGO BAY LEFT SLOPING FLOOREBEAM, BS 1460. REPLACED THE FLOORBEAM IAW SRM 51-40-02.SDR AALA201902119007Floor Support · corrodedCORROSION ON AFT THE AFT CARGO BAY FLOOR SUPPORT BETWEEN BS 1320 AND BS 1340, RBL 15. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.SDR AALA2019011769004Oven · odorHAD A TRANSIENT BURNING ODOR JUST AFTER TAKEOFF, SIMILAR TO OVEN TURNING ON. DISSIPATED AFTER A FEW MINUTES. PERFORMED JC 19L00021001 IAW TSI 0081377. REPLACED THE NR 2 FORWARD GALLEY OVEN IAW AMM 25-31-05. OPS CHECKED GOOD. NO ABNORMAL ODOR NOTED AT THISSDR FDEA201901100078Actuator · damagedPDIS 901 32-30 1809 10JAN19 BCN OPEN U LOGPAGES:3018949 DOORS LIGHT AT APPROX. FL 260 300 KNOTS CLIMBING EICAS DOORS LIGHT ILLUMINATED. BOTH EXTINGUISHED AS WE DECELERATED. HANDLE IN OFF POSITION. REF WRI 32-20-1821 = LEFT MAIN GEAR DOOR PROX SENSORS MAINTENANSDR FDEA201901090077Actuator · damagedPDIS 901 32-30 1807 09JAN19 BCN OPEN U LOGPAGES:3018948 DOORS LIGHT CAME ON IN CLIMB AT ABOUT 300 KTS. WENT OUT AND WE RESUMED DOOR LIGHT CAME BACK ON AND STAYED ON TILL DECELERATION BELOW 300 KTS. ''GEAR DOORS'' EICAS MESSAGE ILLUMINATE BOTH TIMES. MEL 09JAN1SDR AALA201812289001Windshield · failedFIRST OFFICER`S WINDSHIELD OUTER PANE SHATTERED. QRH CHECKLIST PERFORMED. AIRCRAFT PRESSURIZATION AND OTHER SYSTEMS WERE NORMAL AND FLIGHT CONTINUED TO DESTINATION. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE WINDSHIELD IAW STANDARD PRACTICES ANDSDR AALA201812079009Transition Panel · corrodedCORROSION WAS FOUND ON THE TRANSITION PANEL, BS 1480 - 1520, LBL 16 IN THE AFT CARGO BAY. REPAIRED THE TRANSITION PANEL IAW SRM 53-00-53-2R-2, 51-40-02, & 51-20-10.SDR AALA201812049032Torque Tube · excess playLEFT WING FLAP TORQUE TUBE AT THE TRAILING EDGE REAR SPAR AREA, BELOW THE NR 5 SPOILER HAD EXCESSIVE PLAY. REPLACED THE TORQUE TUBE AND PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW AMM 27-51-25.SDR AALA201812039002Panel · delaminatedDELAMINATED PANEL 611BB AT THE CORNER. REPAIRED THE PANEL IAW SRM 57-41-01AND B757 SRM 51-70-03.SDR AALA201811309006Collar · wornR1 DOOR HOLD OPEN COLLAR ASSEMBLY WAS WORN. REPLACED HOLD OPEN COLLAR IAW AMM 52-11-08-0047-025, 52-11-08-404-00, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.SDR AALA2018113099006Floor Support · corrodedCORROSION FOUND ON THE AFT CARGO BAY FLOOR SUPPORT, BS 1500 -1520, RBL 2.2 - 11. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53-1A , 51-20-10, & 51-40-2.SDR AALA201811299007Transition Panel · corrodedCORROSION FOUND ON THE TRANSITION PANEL, BS 1410 - 1480, LBL 16.10. REPAIRED THE TRANSITION PANEL IAW SRM 53-00-04-1A, 51-20-01, & 51-40-02.SDR AALA2018112989007Floor Panel · corrodedCORROSION FOUND ON THE RIGHT SLOPING PANEL AT BS 1300, IN THE AFT CARGO BAY. REPLACED THE PANEL IAW SRM 53-00-53-1A, AND 51-40-2.SDR AALA201811289009Stringer · crackedAIRCRAFT WAS IN BASE MAINTENANCE. CRACK FOUND ON THE AFT CARGO COMPARTMENT FLOOR STRUCTURE STRINGER LOCATED AT BS 1470, RBL 2.90. REPLACED STRINGER PER SRM 53-00-53-1A , 51-20-10 & 51-40-2.SDR AALA201811289008Stringer · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON THE AFT CARGO COMPARTMENT FLOOR STRUCTURE STRINGER AT BS 1470, LBL 7.55. REPAIRED STRINGER PER SRM 53-00-53-1A , 51-20-10 & 51-40-2.SDR AALA201811289006Stringer · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON AFT CARGO COMPARTMENT FLOOR STRINGER AT BS 1470, RBL 10.45. REPAIRED STRINGER PER SRM 53-00-53-1A , 51-20-10 & 51-40-2.SDR AALA201811289004Stringer · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON AFT CARGO COMPARTMENT FLOOR STRUCTURE STRINGER AT BS 1470, LBL 2.9. REPAIRED STRINGER PER SRM 53-00-53-1A , 51-20-10 & 51-40-2.SDR FDEA201811263393Circuit Breaker · trippedAFTER TROUBLE SHOOTING FINISHED THE LDG ALT EXT C/B POPPED OUT AGAIN DURING T/S FOUND "ALT GEAR EXTENSION CONT" C/B FAULT , C/B SWAPPED CB C41177 WITH CB C00773, P006-01//H006 CB-BTL 2 CARGO FIRE EXTINGUISHING T/S REF SDR AALA2018112769002Floor Support · corrodedCORROSION FOUND ON THE AFT CARGO BAY FLOOR SUPPORT BS 1470, RBL 7.55. REPLACED THE FLOOR SUPPORT IAW SRM 53-00-53-1A, 51-20-10, AND 51-40-2.SDR AALA201811269001Stringer · corrodedCORROSION FOUND ON STRINGER 7R, BS 1470. REPLACED THE STRINGER IAW SRM 53-00-53-1A, 51-20-10, AND 51-40-2.SDR AALA201811209003Web · crackedMAIN DECK FLOOR WEB WAS CRACKED BETWEEN BS 1620 AND 1640, BL 0. REPLACED THE WEB IAW SRM 53-00-51-2R-4.SDR AALA201811109008Skin · debondedLEFT ELEVATOR TRAILING EDGE HAS A DEBONDED AREA STARTING AT ELEVATOR STATION 160.5 GOING OUTBOARD TO ELEVATOR STATION 175. REPLACED THE ELEVATOR IAW AMM 27-31-01-401, AND TC 19L33027002.SDR AALA201811129002Floor Support · corrodedCORROSION FOUND ON THE FLOOR SUPPORT, BETWEEN BS 1300 - 1320, RBL 16. REPLACED THE FLOOR SUPPORT IAW SRM 53-00-04-1A, AND 51-40-02.SDR AALA201811069004Retainer · unsecureAIRCRAFT IN BASE MAINTENANCE: AFT CARGO DOOR CUT OUT AFT FRAME 2ND FROM THE TOP CORNER DOOR STOP ROTATES FREELY (NOT SECURED). REPLACED DOOR STOP SPRING RETAINER PER AMM 52-34-00-825-009.SDR AALA2018111209013Torque Box · delaminatedVERTICAL STABILZER LEFT FORWARD TORQUE BOX PANEL WAS DELAMINATED 3 INCHES UP FROM BOTTOM EDGE. REPLACED THE TORQUE BOX PANEL IAW SRM 51-40-02.SDR AALA201811089011Wedge · delaminatedLEFT WING NR 5 SLAT TRAILING EDGE WEDGE UPPER AND LOWER SURFACES WERE DELAMINATED. REPLACED THE SLAT IAW TC 19L51027001.SDR AALA201811019006Transition Panel · corrodedTHE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON LOWER SECTION OF TRANSITION PANEL. REPAIRED TRANSITION PANEL PER SRM 53-00-53-1A-1 FIGURE 102 AND 51-40-02.SDR AALA201811019009Support Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: L4 DOOR LOWER SILL CENTER SCUFF PLATE FORWARD SUPPORT ANGLE CORRODED AT BS 1661 AND LBL 65. REPLACED SUPPORT ANGLE PER SRM 51-40-02.SDR FDEA201810313062Flight Recorder · inoperativeFLIGHT DATA RECORDER FAILED TO TEST. REPLACED PANEL FDR SVCE INTPH IAW AMM 31-31-04-4. TESTED SYSTEMS ALL SATIS. FDR IS TESTING AND WORKING, NO EICAS MESSAGES.SDR AALA201810319006Transition Panel · corrodedCORROSION FOUND ON THE TRANSITION PANEL BETWEEN BS 1441 TO 1552, RBL 6. REPAIRED THE TRANSITION PANEL IAW SRM 53-00-53-1A, FIGURE 101, AND 51-40-02.SDR AALA201810319017Skin · crackedLEFT WING LEADING EDGE NR 2 SLAT SKIN FOUND CRACKED AT THE INBOARD TRACK COVE AREA. REPLACED THE SLAT IAW TC 19L52027002.SDR AALA201810319015Window · arcedCOCKPIT R1 WINDOW HAS MOISTURE INGRESS AROUND THE PERIPHERY OF THE WINDOW WITH SIGNS OF ARCING NEAR THE BUSS BAR. REPLACED THE WINDOW IAW AMM 56-11-01-004-001.SDR AALA2018110209004Floor Support · corrodedCORROSION FOUND ON THE FLOOR SUPPORT BETWEEN BS 1300 - 1320. REPLACED THE FLOOR SUPPORT IAW SRM 53-00-04-1A, AND 51-40-02.SDR AALA2018101299020Bottle · low pressureR4 DOOR SLIDE BOTTLE PRESSURE WAS LOW. REPLACED THE SLIDE IAW JC 19L80025002.SDR AALA201809249026Panel · crackedCRACKED RIGHT LEADING EDGE WING TO BODY PANEL 192AR. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED A REPAIR TO THE WING - BODY PANEL IAW EA 285262.SDR AALA201809179031Skin · corrodedCORROSION FOUND ON THE LEFT WING INBOARD TRAILING EDGE FLAP UPPER SURFACE. THE AIRCRAFT WAS GROUNDED. REPAIRED THE FLAP IAW EA 284911.SDR AALA2018091989026Power Supply · inoperativeEXTERIOR EMERGENCY LIGHT, R1 DOOR, WOULDN'T ILLUMINATE DURNING TEST. MAINTENANCE REPLACED M730 AND M735 POWER SUPPLIES AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 31-51-00.SDR FDEA2018091432511Skin · wornRT MAIN FLAP TOP SURFACE HAS 2 WEAR MARKS OPPOSITE NR 10 SPOILER ACTUATOR. REPLACED DAMAGED REPAIR PLATE ON RT MAIN FLAP TOP SURFACE IAW SRM 57-53-01-2R REPAIR 2 FIG 201 REV 124SDR FDEA2018091432492Strap · corrodedINTERCOSTAL STRAP PUNCTURED AND CORRODED AT BS 1020 BETWEEN RBL 25 AND RBL 45. PUNCTURE DAMAGE IS NOT ALLOWED AS PER SRM 53-00-51-1A FIG 101 REV 124. FABRICATED NEW INTERCOSTAL STRAP IAW GMM 7-0-1001 REV 150 AND DRAWING 144N5081 SHEET 1 REV A INSTALLED NEW STRSDR FDEA2018091432491Bracket · crackedRT OB FLAP OB TOP TO LWR SKIN AFT BRACKET CRACKED. FABRICATED AND INSTALLED NEW BRACKET IAW GMM 7-00-1001 REV 150 AND DRAWING 113N3370 SHEET 2 REV C AND SRM 51-30-01 AND 51-40-02 REV 124.SDR FDEA2018091432490Frame · damagedFRAME 231.25 AT FWD E&E BAY DOOR HAS STRUCTURAL DAMAGE. PERFORMED REPAIR TO FRAME 231.25 IAW SRM 53-00-07-2R FIG 202 REV 125.SDR FDEA2018091432489Support Bracket · corrodedTOP LT WING WTB PANEL SUPPORT NR 4 FROM FWD REQUIRES EVALUATION AND REPROTECTION. FABRICATED WTB PANEL SUPPORT BRACKETS IAW DRAWING 149N7210 SHEET 7 REV B AND GMM 7-0-1001 USING MATERIAL 7075-T0 0.080" BN 017135193. INSTALLED BRACKETS IAW SRM 51-40-02 REV 124.SDR FDEA2018091432488Strip · corrodedLT ELEVATOR TIP UPPER AND LOWER STATIC DISCHARGE STRIP HAS SUSPECT CORROSION UNDERNEATH. UPON EVALUATION, BOTH STATIC DISCHARGE STRIPS FOUND TO BE OUT OF LIMITS IAW SRM 55-20-01 FIG 101 TABLE 1 REV124. FABRICATED NEW DISCHARGE STRIPS IAW DRAWING 183N2901 AND G
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