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 2024F00059Frame · crackedL/H FUSELAGE FRAME AT STA 840 BETWEEN STR8L AND STR9L HAS A CRACK.SDR 2024F00058Frame · crackedR/H FUSELAGE FRAME AT STA 800 BETWEEN STR8R AND STR9R HAS A CRACK.SDR 2024F00057Frame · crackedL/H FUSELAGE FRAME AT STA800 BETWEEN STR8L AND STR9L HAS A CRACKSDR 2024F00056Frame · crackedR/H FUSELAGE FRAME AT STA760 BETWEEN STR8R AND STR9R HAS A CRACKSDR 2024F00055Frame · crackedL/H FUSELAGE FRAME AT STA 760 BETWEEN STR8L AND STR9L HAS A CRACK.SDR 2024FA0000208Frame · gougedR/H FUSELAGE INTERIOR FRAME AT STA 1280 STR14R HAS 3 GOUGE MARKS POSSIBLE INTERIOR BINS NOT PROPERLY INSTALLED.SDR FDEA202402160165Duct · damagedDURING SVC WHILE DOING A LEAK INSPECTION ON APU AREA FOUND APU SURGE DUCT CASING BROKEN AND MISSING MATERIAL RELEASED FOR SERVICE PER MEL : 49-11-01. REMOVED AND REPLACED APU PER MM 49_11_01_4_0 PERFORMED OPERATIONAL TEST ON APU PER MM 49_11_00_2_0 ALL TSDR FDEA202401250111Engine · inoperativePDIS 928 73-22 1096 25JAN24 MEM OPEN U AT CRUISE, FL360, #1 ENG EPR DID NOT INDICATE PROPERLY. THE WHITE EPR NEEDLE WAS FULL POWER ABOVE THE DIAL, THE POWER STRIP WAS ALSO WELL ABOVE THE MAX PORTION, THE N1 WAS SLOWLY DEGRADING AND WE BEGAN TSDR FDEA202401240116Lock · wornWHILE WORKING ON TSI 25-60/5212, FOUND RH DOOR ARMED LIGHT WORKING INTERMITTENTLY. RELEASED FOR SERVICE PER MEL : 25-66-05-A CATEGORY : C EXPIRATION : 03FEB24 "MEL 25-66-05-A: R1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS - INOP. REMOVED AND REPLACED FWD SDR FDEA202401190090Girt Bar · fodRIGHT ENTRY DOOR SLIDE LIGHT INOP. REPEAT GRIPE. REFER TO ATTACHED PICTURES: SLIDE ARMED THREE TIMES IN A ROW: SLIDE LIGHT COMES UP EVERY TIME. FOLLOWED FIM 25-66 FAULT TREE 802, IAW AMM 25-66-11-2 CLEARANCE DIMENSIONS WITH THE FOLLWING FINDINGS: ON FIG 20SDR FDEA202311271944Seat Track · damagedSEAT TRACK LOBE DAMAGED AT STA 582 LBL 45 MAJOR REPAIR: FABRICATED NEW SEAT TRACK BAC1520-792 7178T6511 P.O. MA6505860 , PER SAMPLE AND INSTALLED NEW SEAT TRACK STA. 440-680 LBL 45.5 , REF B757 SRM 51-40-02 AND B757 SRM SUPPLEMENT 53-10-52.SDR FDEA202305160872Module · failedPASSING 8000 FEET, GOT R HYD QTY LOW WHICH TURNED INTO R HYD SYS PRESS. CONSULTED QRH, FOLLOWED PROCEDURE, DECLARED EMERGENCY AND LANDED SAFELY. ***EMERGENCY DECLARED*** INSTALLED FILTER MODULE REF AMM 29-11-17-4. SERVICED RIGHT HYD SYSTEM REF AMM 12-12SDR FDEA202212022866None · noneDUE TO WRI 25-60/5015 AND A POSSIBLE SAFTEY CONCERN OF THE NORMAL OPERATION OF THE R1 DOOR SLIDE WHEN OPENING FROM THE EXTERIOR. R1 DOOR, TO INCLUDE THE SLIDE, IS TO BE PLACED ON MEL AND HAVE AN INSPECTION PLANNED AT AN APPROPRIATE GROUND TIME IAW AMM 52-11-SDR FDEA202212012864Control Panel · failedOVERHEAD COCKPIT EMERGENCY LIGHTS PANEL WON'T TEST IAW AMM 33-51-08-4. REMOVED AND REPLACED P5 EMEGENCY LIGHTS PANEL IAW AMM 33-51-08-4. OPS CHECKED NORMAL. ACFT OK FOR SERVICE.SDR FDEA202211302865Bulb · inoperativeL1 DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. BULB REPLACED IAW AMM 33-51-06-2-1, REV 130.9, X1.SDR FDEA202211162798Actuator · failedSELECTED FLAPS 1 AT 5500 FEET AND ABOUT 200 KNOTS. RECEIVED LE SLAT DISAGREE EICAS MESSAGE. COMPLIED WITH QRH. MESSAGE REMAINED. QRH DIRECTED US TO RUN LE SLAT ASYMMETRY QRH. COMPLIED WITH QRH. DECLARED EMERGENCY AND LANDED WITH TE FLAPS AT 20 WITH NO FURTHERSDR FDEA202211152785Bearing · misalignedAFTER LOADING, UNABLE TO LOCK MAIN CARGO DOOR, ONLY THE FWD CAM IS LOCKED, AFT CAM WOULD NOT MOVE. AMM: 52-32-00-5 DURING INSPECTION OF THE HOOK PIN, FOUND MISALIGNEMENT BETWEEN BOTH BEARING HOUSINGS, CAUSING POINT OF CONTACT AT WRONG LOCATION AND BLOCKING THSDR FDEA202211122760Bulb · inoperativeEXTERIOR EMERGENCY LIGHT (SLIDE LIGHT) DOOR 1R INOP. BULB REPLACED ACC AMM 33-51-06-2-1 (REV 130.5). OPS TEST SATIS.SDR FDEA202211042729Frame · crackedWHILE PERFORMING HFEC INSP OF FRAME WEB INBD OF STRINGER S-26L AT BODY STATION 1460, FOUND CRACK INDICATON ON INBD HOLE AT 6:O,CLOCK. ACCOMPLISHED REPAIR PER EA TF-5310-T0371176 EA TITLE: FUSELAGE - MAINFRAME - STA1460 FRAME BETWEEN S-26L AND S-27L CRACK SDR FDEA202211012702Skin · damagedWHILE WORKING #1 O/B T/R C DUCT CHANGE FOUND DAMAGE ON UPPER PORTION OF INBOARD #1 ENG FAN COWL REPAIRED IAW EA F-7110-T0371402 THIS IS A MAJOR REPAIRSDR FDEA202210242676Steering Sys · unknownAIRCRAFT PULLING LEFT DURING MOVEMENT IN ALL PHASES OF GROUND OPS. INSPECTED STEERING ACTUATOR AND LINKS IAW AMM 32-51-00-0 WITHOUT ANY DEFECT FOUND. PERFORMED STEERING TENSION IN THE CABLES NWSA / NWSB / NGPPA AND NGPPB IAW AMM 32-51-00-5-3 WITHOUT ANY SDR FDEA202206171458Hose · malfunctionedRIGHT ENGINE PROBLEM AT CRUISE. RIGHT EPR SHOWED MAX ON SCALE. FUEL FLOW APPRX 1/2 OF LEFT ENGINE. ALL RIGHT INSTRUMENTS WERE SIGNIFICANT THEN LEFT. HAD TO DESCEND FROM CRUISE F380 TO FL 320 TO HOLD AIRSPEED. HAD RIGHT SIGNIFICANT RIGHT THROTTLE VIBRATIONSDR FDEA202204120932Girt Bar · misalignedMDIS 963 52-10 7334 12APR22 PDX FACT U L-1 DOOR WILL NOT ARM FACT 12APR22 21:02 AFW U INSPECTED AND VERIFIED GIRT BAR ALLIGNMENT IN REF TO AMM 25-66-10-2. PERFORMED L1 DOOR GIRT BAR INSPECTION/CHECK IN REF TO AMM 25-66-10-2 SECTION 4. DOSDR FDEA202202240930Floorbeam · corrodedFOUND CORROSION ON FLOOR BEAM UPPER T-CHORD AT STA 880 BETWEEN RBL 45-68 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A #F-5310-T0367576 B, FLOOR BEAM ASSY , STA 879, UPPER CHORD, BL 45-68, CORROSION, REPAIR MAJOR REPAIR.SDR FDEA202202240929Floorbeam · corrodedCORROSION WERE FOUND ON FLOOR BEAM UPPER T-CHORD LOCATED STA 880 LBL 45-60 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0367576 B, FLOOR BEAM ASSY, STA 879, UPPER CHORD, BL 45-68 CORROSION, REPAIR. MAJOR REPAIRSDR FDEA202202240740Seat Track · crackedCRACK ON SEAT TRACK LOCATED STA1580-1600 RBL 45 WORK ACCOMPLISHED PER FEDEX E.A # F-5300-T0367320: SEAT TRACK AT STA 1580-1600 RBL 58.22, CRACK, PERMANENT REPAIR MAJOR REPAIRSDR FDEA202202220742Beam · elongatedFLOOR BEAM UPPER T CHORD STA 1681 FOUND WITH ELONGATED HOLE AT LBL 4 AND 2EA UNUSED HOLES AT RBL 12 PERFORMED AFT DECK AND FLOOR BEAM REPAIRS PER SRM 53-60-51-2R REPAIR 2, AND REPAIR 3, FIG 201. THE REPAIRS ARE CAT. A REPAIRS, AND NO SUPPLIMENTAL INSPECTISDR FDEA202201190103Transmission · trippedTRAILING EDGE FLAP DISAGREE LIGHT AT FLAPS 20 SELECTING 25. RAN QRH & LANDED. TROUBLEHOT IAW FIM 27-51 FAULT TREE 805, NO FAULT FOUND ON FSEU 1, 2 OR 3. FOUND INTMT FAULT CODE 305 ON FSEU 1, LEG-0, NO FAULT HISTORY ON FSEU 2 & 3. LOAD INDICATOR POPPEDSDR FDEA202201080267Floorbeam · corrodedMAIN DECK SECTION 41 CROSS BEAM FOUND CORROSION AT STA345 BL0.0-LBL9.0 REPAIRED THE MAIN DECK SECTION 41 STA345 BL0.0-LBL9.0 CORRODED CROSS BEAM PER B757 SRM53-00-51-2R REPAIR11. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW WITH FEDEX GMM 6-2-100.SDR FDEA202112223121Transmitter · failedPDIS 972 27-50 7959 22DEC21 CGN FACT U TE FLAP ASYM ILLUMINATED WHEN FLAPS 1 WAS SELECTED. FOLLOWED QRH 9.1.14 LANDED AT 162 KIAS WITH NO ISSUES. PART 22DEC21 19:33 CDG U IDENTIFIED PARTS FLAP POSITION TRANSMITTER MPN: 18-1969-18 SDR FDEA202110312703Warning Message · false activationON FINAL AT 160-170 KNOTS, GOT RUDDER RATIO EICAS. HYDRAULIC PRESSURE WAS NORMAL. COMPLIED WITH QRH, AND DIVERTED DUE TO WIND LIMITATIONS. TROUBLELSHOOTING CARRIED OUT ON BOTH RRCM 'S FOUND MODULE FAULT BALL S SHOWING ON BOTH RRCM'S ACCOMPLISHED FIM 27-SDR FDEA202110272644None · noneFOUND LIGHTING STRIKE DAMAGE TO SKIN 1.5" AFT OF STA 520 2.75" IB OF STR S29L WRITTEN ON WRI 53-00-6918 WORKED ON SEQ 5 UNDER W/O 81650 CARD WRITTEN FOR RDR/SDR. REPAIRED LIGHTING STRIKE DAMAGE TO SKIN 1.5" AFT OF STA 520 2.75" I/B OF STR S29L REF 757 SRM 5SDR FDEA202110272643None · noneFOUND LIGHTING STRIKE DAMAGE ON SECTION 43, ON STA 580, 4.5" IB OF STR 29R DAMAGE WRITTEN UP ON WRI 53-00-6925 REPAIR WORKED ON SEQ 6 W/O 81650. CARD WRITTEN FOR RDR/SRD REPAIRED LIGHTING STRIKE DAMAGE ON SECTION 43 ON STA 580 4.5" I/B OF STR 29R REF 757 SRMSDR FDEA202110182646Crease Beam · corrodedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CREASE BEAM INBD CHORD CORRODED, BETWEEN STA1400 AND STA1620, RBL64.4 COMPLIED WITH FEDEX EA: F-5321-T0364905 PT1, EA TITLE: FUSELAGE - CARGO COMP FLOORS - CREASE BEAM INNER CHORD, STA1400-STA1620, RH SIDE, EXTSDR FDEA202110162545Warning Message · false activationTRAILING EDGE FLAP DISAGREE. HANDLE AT 20. INDICATOR SAID BOTH FLAPS AT 15. RAN QRH. RECONFIGURED FLAPS FROM ALT TO REGULAR AND RAISED FLAPS. OPERATED FLAPS THROUGH ALL DETENTS FOR SEVERAL CYCLES, REF MM 27-51-00-5. NO FAULTS NOTED. PERFORMED BITE CK OF ALLSDR FDEA202109172322Drive Assy · trippedON APPROACH SELECTED FLAPS 25 AND GOT TE FLAP DISAGREE. QRH AND LANDED FLAPS 20. FIM 27-51 FT 808 REV 127.2 APPLIED, FOUND RH INB FLAPDRIVE OVERLOAD POPOUT ACTUATED. FOUND SPINDEL DIRTY AND DRY. CLEANED AND LUBRICATED. FLAPS CYCLED , NO FAULTS. OK FOR SESDR FDEA202108262099Line · unsecureL1 DOOR DIFFICULT TO CLOSE AND ARM FOUND EMERGENCY SLIDE STATIC LINE LOOSE AND BUCKLE DANGLING CAUSING INTERFERENCE. REPOSITIONED IAW AMM 25-66-01-4. OPS TEST OKAY.SDR FDEA202108232074Ram Air Turb · failedTEST FLIGHT- RAT WOULD NOT DEPLOY WITH BOTH SPEED CAD C/B PULLED. REMOVED AND REPLACED LEFT AND RIGHT ENG SPEED CARDS IAW AMM 77-12-03-4, PERFORMED RAT AUTO DROP TEST IAW AMM 29-21-00-5, TEST PASSED.SDR FDEA202108222070Strut · damagedDURING C CHECK FOUND BURN DAMAGE ON RH SIDE OF NR 2 PYLON INSTALLED DOUBLER REPAIR PER EA F-5450-T0363070P1.SDR FDEA202108101999Floor Panel · crackedMAIN DECK FLOOR PANEL 251MVF HAS CRACK (ADJACENT R4 DOOR). DOT 136-58 FABRICATED MAIN DECK FLOOR PANEL 251MVF ON VTMAE TRAVELER # T21/1565102 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.SDR FDEA202107261863Seat Track · corrodedFOUND CORROSION ON SEAT TRACK CROWN AT STA 1630 RBL 24.5 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52-2R OPTION 1 FIG 201SDR FDEA202107261862Seat Track · corrodedFOUND CORROSION ON SEAT TRACK CROWN AT STA 1640 LBL 48 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52-2R OPTION 1 FIG 201SDR FDEA202107261861Seat Track · crackedFOUND CRACKED SEAT TRACK FLANGE BETWEEN STA 1580-1600 LBL 58.22 PERFORMED SEAT TRACK REPAIR PER SRM 53-00-52 2R OPTION 1 FIG 201SDR FDEA202107231845Girt Bar · dirtyFORWARD ENTRY DOOR WILL NOT ARM. DOOR 1RH GIRT BAR MECHANISM INSPECTION PERFORMED I.A.W. AMM 52-11-25-5. FLOOR FITTINGS INSPECTED AND CLEANED. GIRT BAR RIPOSITIONED IN CORRECT POSITION AND GIRT BAR LEVER CHECKED FOR PROPER OPERATION SEVERAL TIME, SATISFACTSDR FDEA202107151791Truck · damagedANTISKID MSG AFTER TAKEOFF, SUSPECT DUE TO DAMAGE #3 TIRE. R/R L/H MAIN TRUCK IAW AMM 32-11-17-004-0001.SDR FDEA202107071697Battery Pack · inoperativeRIGHT SIDE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND TESTED OK IAW AMM: 33-51-07-2-2.SDR FDEA202106251590Attach Fitting · crackedCHECK FOUND RH WING OUTBOARD DRAG FITTING NO. 4# FASTENER HOLE CRACKED REPLACED THE RH WING OUTBOARD DRAG FITTING PER EA:F-5740-T0361981 P1, EA TITLE: WINGS - ATTACH FITTINGS - CRACK FINDING IN RH WING DRAG FITTING NO.4# FASTENER HOLE, THIS IS CAT B REPAISDR FDEA202106151543Skin · dentedFUSELAGE SKIN EXTERNAL SURFACE FOUND 1EA DENT AT STA1480 - STA1500, S23R - S24R REPAIRED THE DENT AT FUSELAGE SKIN EXTERNAL SURFACE STA1480 - STA1500, S23R - S24R PER EA F-5330-168309 A P4, EA TITLE: FUSELAGE - PLATE AND SKIN - SKIN PANEL DOUBLER REPAIR BESDR FDEA202106141536Cargo Track · crackedMAIN CARGO COMPARTMENT TRACK BEAM CRACKED AT STA1460 - STA1480, RBL45.5 REPAIRED THE CRACKED TRACK BEAM AT MAIN CARGO COMPT. STA1460 - STA1480, RBL45.5 PER B757 SRM51-40-02 & SRM53-00-52-2R REPAIR.1. THIS IS CATEGORY A REPAIR, NO ADDITIONAL INSPECTIONS REQSDR FDEA202105231364Fairing · cracked#2 ENG PYLON O/B LOWER FLEXABLE FAIRING CLOSEOUT PANEL IS CRACKED ABOVE EXHAUST NOZZLE REMOVED AND REPLACED PANEL PER DWG # 311N5137
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