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 FDEA201906191523Strip · corrodedLT ELEV O/B AFT END CAP STRIP BULGING. FABRICATED AND REPLACED PARTS IAW GMM7-0-1001 AND BOEING DRAWING# 183N2006 AND 183N2007 AND IAW SRM51-40-02.SDR FDEA201906191489Sleeve · crackedENG #2 I/B T/R SLEEVBE CRACKED AT LOWER CORNER OF CUTOUT FOR BLOCKER DOOR #10 REPAIRED CRACKE ON ENGINE #2 LT T/R SLEEVE INNER PERFORATED SKIN AT THE BLOCKER DOOR#10 IAW EA #:F-7830-T0347748 P1. TITLE ;EXHAUST SYSTEM-TRUST REVERSER GEN- CRACK ON 2L TRANSLATINSDR FDEA201906191478Bracket · crackedRT O/B AFT FLAP, O/B AUX TRACK FAIRING BRACKET IS CRACKED REPLACED RT O/B AFT FLAP O/B AUX TRACK FAIRING BRACKET IAW SRM 51-40-02 AFTER FABRICATION OF NEW BRACKET IAW DRAWING# 113N3333 AND GMM-7-0-1001.SDR FDEA201906181532Panel · crackedSLAT #5 LOWER TRAILING EDGE SKIRT IS CRACKED. REPAIRED THE DAMAGE SLAT #5 LOWER FLEX PANEL PER SRM 57-43-02-2R, SRM 57-43-01-0I IDENTIFICATION 1, SRM 57-43-01-2R REPAIR 10 AND SRM 51-70-07-0G GENERAL AND PARAGRAPH 5(H). REPAIR 10, PARA 4(C) WITHOUT DEVITION.SDR FDEA201906181522Panel · crackedSLAT #6 LOWER TRAILING EDGE MIDDLE SKIRT IS CRACKED. REPAIRED THE DAMAGED SLAT #6 LOWER FLEX PANEL PER SRM 57-43-02-2R, SRM 57-43-01-0I IDENTIFICATION 1, SRM 57-43-01-2R REPAIR 10 AND SRM 51-70-07-0G GENERAL AND PARAGRAPH 5(H) . REPAIR 10, PARA 4(C) WITHOUT DESDR FDEA201906181511Bracket · damagedAFT CARGO DOOR AFT SIDE SEAL DEPRESSOR LOWER CORNER BRACKET IS DAMAGED FABRICATED NEW BRACKET IAW DRAWING#140N2791 REV.B AND GMM 7-0-1001 REV.156. P/N 2024T0-0402, B/N 0191818482, HEAT TREATMENT CERT # HT-19-077. BRACKET P/N:140N2791-9 AND INSTALLED IAW SRM SDR FDEA2019061751308Control Rod · out of adjustTHE SLIDE PLACARD DOES NOT COME INTO VIEW WHEN THE LEFT FORWARD DOOR IS ARMED, ADJUSTED AND LUBRICATED L1 DOOR EMERGENCY MECHANISM RETRACTABLE DOOR CONTROL ROD , SYSTEM TESTED SATISFACTORY IAW AMM 52-11-20-5, MEL CLOSED, PLACARD REMOVED, A/C OK FOR SERVSDR FDEA201906141538Strap · damagedAGING AIRCRAFT MAIN DECK BS 365.25 LBL 24.75 STABILIZER STRAP REPAIR. REPAIR REPLACED IAW EA # F-5310-T0348004 P1 AND SRM 51-00-51 REPAIR 13.SDR FDEA201906141537Strap · damagedAGING AIRCRAFT MAIN DECK BS 365-.25 LBL 45..50 STABILIZER STRAP REPAIR. REPAIR REPLACED IAW EA #F-5310-T0348004 P1 AND SRM 53-00-51 REPAIR 12.SDR FDEA201906051228Transceiver · malfunctionedRADAR NOT GIVING ACCURATE INFORMATION REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 066-50008-0406 POS: ONL SRL: 12218 TAG NBR: 2611E0 ON MPN: 066-50008-0406 CPN: 3414883 SRL: RTA4B-20922 SDR FDEA2019060311193Gcu · faultedPDIS 914 24-20 9178 30MAY19 MNL OPEN U LOGPAGES:2951455 DURING DESCENT INTO RPLL, THE FOLLOWING EICAS INDICATIONS DISPLAYED: R GEN, R BUS, R UTILITY BUS, R EEC. QRH PROCEDURE ACCOMPLISHED TO UNEVENTFUL LANDING. FACT 02JUN19 09:04 CAN U SDR FDEA2019060391194Ballscrew · damagedWHILE COMPLYING WITH TSI 27-50/5006 FOUND OVERLOAD INDICATOR POPPED ON R/H INBOARD TRANSMISSION ASSY ON INBD FLAP INPECTED BALLSCREW WITH A CHEESECLOTH FOR SHARP EDGES AND FOUND UNSATISFACTORY ON TRANSMISSION #5. INSPECTED ALL OTHER TRANSMISSION ASSY'S SDR FDEA201905291180Warning System · false activationON FINAL APP. ATH. EICAS DISPLAYED TE FLAP DISAGREE (WITH FLAPS 20). RAN QRH. PERFORMED FIM 27-51 FAULT 811. UNABLE TO DUPLICATE THE FAULT FLAP SLAT ELEX UNIT 1 2 3 WITH NO EXIST FAULTS. IN FAULT HISTORY "0" - MSG 30S FLAP DISAGREE INTERM. OPERATIONAL TEST OFSDR FDEA201905101024Latch · failedDURING POST FLIGHT CHECK FOUND LATCH ON, LAVATORY ACCESS DOOR, BENEATH SINK BROKEN. IN REF TO DISC. 25-40/5348 PREVENTIVELY SET LAV TO INOP RELEASED FOR SERVICE PER MEL : 25-41-01 CATEGORY : C EXPIRATION : 19MAY19 "MEL 25-41-01: LAVATORY WASTE CONTAINER FLAPPSDR FDEA2019042290862Bracket · corrodedBS 1410, AFT CARGO DOOR, LOWER FRAME SUPPORT BRACKET HAS EXFOILIATING CORROSION, 1 INCH BY 1 INCH SIZE. BOTH SIDES OF BRACKET ARE CORRODED.SDR FDEA201904160811Crease Beam · corrodedMAIN CABIN CREASE BEAM STA. 860-880 RBL64.20 HAS CORROSION REMOVED CORR. ON CREASE BEAM STA 860-880 RBL 64.20 IAW B757 SRM 51-10-02. ORIG MAT .071 REM .051 LOSS .020 FOUND OUT OF LLIMITS IAW B757 SRM 53-30-13-1A FIG 101 DET VIII. REMOVED, FABRICATED ANDSDR FDEA201904160810Seat Track · corrodedCORROSION SEAT TRACK FLANGE MAIN CABIN STA. 1540 RBL 45.50 PERFORMED SEAT TRACK REPAIR AT RBL 45.50 BETWEEN BS 1500-1540 IAW B757 SRM 53-00-52- 2R FIG 201 REPAIR 1 OPTION1. REMOVED COR ON SEAT TRACK IAW B757 SRM 51-10-02. 100% MAT. LOSS DUE TO EXFOILATION FSDR AALA2019041189001Starter · failedAIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS AFTER APU OIL SERVICING ON ARRIVAL, APU WOULD NOT START-FAILED. SMOKE EVIDENT. APU WAS SHUTDOWN FROM NLG POSITION. MAINTENANCE REMOVED AND REPLACED APU STARTER IAW AMM 49-41-01. ON 3RD START ATTEMPT ON THE NEW STARTERSDR FDEA201903150644Transducer · out of adjustA/P ON IN VNAV, BELOW PATH, THROTTLES IDLE AIRCRAFT NOSE PITCHES DOWN RESULTING IN 6000' FPM DESCENT WITH AIRSPEED INCREASING AND SPEED BRAKES OUT. AIRCRAFT DOES NOT HONOR AIRSPEED, VNAV PATH, OR VERTICAL SPEED. AUTOPILOT DISENGAGED WITH VERY HEAVY NOSE DOWINSDR FDEA201903140643Relay · faultyPDIS 967 36-11 5155 14MAR19 TLH FACT U LOGPAGES:3073947 RIGHT ENGINE BLEED OFF. ACCOMPLISHED QRH PERFORMED AIR SUPPLY BACK PRESSURE CHECK ON RT ENGINE PNEUMATIC SYSTEM IRW 757 AMM 36-11-09-2-1; NO LEAKS OR DEFECTS FOUND. RAN BOTH ENGINES PER JRH FSDR FDEA201903130597Wire · incorrectCARGO ISOLATION SWICH OPERATION CHECK FAILED. WHEN R PACK IN STBY-W, L PACK IN AUTO AND CARGO ISOLATION SWITCH ON, LEFT PACK VALVE CLOSES AND RIGHT PACK TO HIGH FLOW. RESULT SHOULD BE LEFT PACK HIGH AND RIGHT PACK VALVE CLOSES. CARRIED OUT TROUBLESHOOTING IAW SDR AALA201903139002Autopilot Sys · malfunctionedTHE PILOT REPORTED THAT THE RT AUTOPILOT UNCOMMANDEDLY DISCONNECTED. MAINTENANCE PERFORMED AN FCC TEST THROUGH MCDP. NO FAULTS. ENGAGED THE RT AUTOPILOT AND MOVED FLIGHT CONTROLS. DID NOT DISCONNECT. NO FAULTS CAN BE DUPLICATED.SDR FDEA201903080560Retainer · corrodedLT AILERON TRAILING EDGE SEAL RETAINERS PN=133N1799-23 & 133N1799-25 ARE CORROED AND REQUIRE FABRICATION PER CUSTOMER REQUEST PERFORMED THE FABRICATION OF THE LT AILERON TRAILING EDGE SEAL RETAINERS PN=133N1799-23 & 133N1799-25 PER CUSTOMER REQUEST AND GMM-7-0SDR FDEA201903070557Panel · corrodedENGINE NR 2, OUTBOARD THRUST REVERSER UPPER TRACK BEAM SUPPORT PANEL HAS DAMAGE. REPAIR CARRIED OUT IAW EM 78-31-28-300-085 AND EA # F-7833-T0345330 PART 1, TITLE EXHAUST SYSTEM- TR STRUCTURE/SLEEVE-ENG NR 2 RT THRUST REVERSER- UPPER BIFURCATION PLATE CORROSIOSDR FDEA201903040534Bracket · crackedBRACKET ON AFT SIDE OF BULK CARGO B.STA 1640 FLOORBEAM AT LBL 14 IS BROKEN. BRACKET REPLACED IAW SRM 51-40-02, DRAWING NUMBERS 417N2312,146N1023 AND GMM 7-0-1001.SDR FDEA201903040535Bracket · dentedFWD CARGO DOOR AFT SEAL DEPRESSOR LOWER ANGLE SUPPORT DENTED/DAMAGED. FABRICATED AND INSTALLED NEW BRACKET IAW SRM 51-40-02, DRAWINGS # 140N2791,146N6603 AND GMM 7-0-1001.SDR FDEA201903040536Retainer · crackedRT OUTBOARD FLAP SEAL RETAINER CRACKED AT OUTBOARD END. REPLACED SEAL RETAINER IAW SRM 51-40-02.SDR FDEA201903040533Attach Bolt · looseRT WING, NR 7 & NR 8 FLAP TRACKS LOOSE AT AFT ATTACH POINTS. REPLACED NR 7 & NR 8 FLAP TRACK, AFT ATTACH BOLTS IAW AMM 27-51-15.SDR FDEA201903040532Attach Bolt · looseLT WING, NR 1 & NR 2 FLAP TRACKS LOOSE AT AFT ATTACH POINTS. REPLACED NR 1 & NR 2 FLAP TRACK, AFT ATTACH BOLTS IAW AMM 27-51-15.SDR FDEA201903010523Floor Panel · gougedAPPROX 27 GOUGES ON AFT CARGO FLOOR PANEL WHICH IS ADJACENT TO THE AFT CARGO DOOR GOUGE FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-53-1A FIG 101 DETAIL V SHEET 5. CARGO FLOOR PANEL REPLACED IAW GMM 7-00-1001 AND DRAWING # 454N1805.SDR FDEA201903010522Floor Panel · gougedGOUGE ON AFT CARGO FLOOR PANEL AT BS 1329 RBL 9 GOUGE FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-53-1A FIG 101 DETAIL V SHEET 5. CARGO FLOOR PANEL REPLACED IAW GMM 7-00-1001 AND DRAWING # 453N1805.SDR FDEA201902250498Floor Panel · gougedGOUGE FOUND ON FORWARD CARGO FLOOR PANEL AT BS 673 LBL 4 GOUGE FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-53-1A FIG 101 DETAIL V SHEET 5. CARGO FLOOR PANEL REPLACED IAW GMM 7-00-1001 AND DRAWING 454N8105.SDR FDEA201902250500Floor Panel · gougedGOUGE FOUND ON FORWARD CARGO FLOOR PANEL AT BS 721 RBL 1 GOUGE FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-53-1A FIG 101 DETAIL V SHEET 5. CARGO FLOOR PANEL REPLACED IAW GMM 7-00-1001 AND DRAWING # 454N8105.SDR FDEA201902250499Floor Panel · gougedGOUGE FOUND ON FORWARD CARGO FLOOR PANEL AT BS 720 LBL 11.5 GOUGE FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-53-1A FIG 101 DETAIL V SHEET 5. CARGO FLOOR PANEL REPLACED IAW GMM 7-00-1001 AND DRAWING # 454N8105.SDR FDEA201902210473Frame · gougedPUNCTURE HOLE FOUND ON FRAME AT B/S 231.25 BL0. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101 SHEET 1. REPAIRED FRAME IAW SRM 53-00-07-2R REPAIR 7 PARA 5 REV 126.SDR FDEA201902200521Channel · dentedDENT FOUND ON AFT CARGO RT Z CHANNEL AT B.STA 1337 PUNCTURE FOUND IN SMALL DENT, REMOVED ALL DAMAGE AND REPAIRED AREA IAW SRM 53-00-53-1A FIG 101 NOTE D.SDR FDEA201902200461Floorboard · damagedFLOORBOARD 242MCF DAMAGED. REPAIRED FLOOR PANEL 242MCF IAW SRM 53-00-50-2R FIG.201.SDR FDEA201902190551Bracket · crackedCRACKED STANDOFF BRACKET INSIDE APU PLENUM BRACKET FABRICATED AND REPLACED IAW GMM 7-0-1001, DRAWING 353N4010-134 AND SRM 51-40-02.SDR FDEA201902180556Wedge · delaminatedNR 4 EDGE SLAT HAS DELAMINATION ON TRAILING EDGE WEDGE. REPAIRED SLAT NR 4 IAW SRM 51-70-10-2R & EA F-5750-T0345329 P1 WINGS - FLIGHT SURFACES - SLAT NR 4 - TRAILING EDGE WEDGE - DISBOND - RSC TRACKING. THIS IS A MAJOR REPAIR.SDR FDEA201902180552Panel · crackedNR 4 LE SLAT, IN/BD TRACK COVER/ PANEL CRACKED. REPLACED COVER/PANEL IAW SRM 51-40-02 AND DRAWING NUMBER 114N4143.SDR FDEA201902150417Computer · malfunctionedWITH R A/P ON, A/C WENT FROM A 2000 FPM TO A 4500 FPM RATE OF DESCENT. APPROACHING LEVEL OFF ALT PF CLCK IS OFF A/P AND HAND FLEW REMAINDER OF ARRIVAL AND APPROACH REPEAT GRIPE ON A/P SYSTEM. IDENTIFIED PARTS FLT MGMT COMPUTER MPN: 4052506-955 CPN: 3414772 QTSDR FDEA201902150416Autoland Sys · malfunctionedPDIS 968 22-20 4737 14FEB19 TLV FACT U LOGPAGES:3011346 3011350 REPEAT EVENT: IN VNAV PATH @ 350, DECENDING TO 210, ACT WENT FROM VNAV PATH TO VNAV SPEED AND PITCHED DOWN AGRESSIVLEY TO 10 DEG NOSE LOW AND OVER 7000FPM DESCENT. DURING DESCENSDR AALA201902159002Flashlight · inoperativeFLIGHT ATTENDANT FLASHLIGHT AT THE L2 DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT IAW 25-64-00.SDR FDEA2019021430395Handle · obstructedCOULD NOT ARM SLIDE ON RIGHT HAND ENTRY DOOR. RELOCATED CORD DIDN'T LET CLOSE PROPERLY, OPERATE DOOR SEVERAL TIMES , OPS CKS NORMAL REF AMM 52-11-01-6.SDR FDEA201902010241Leaf Spring · wornTHE LEAF SPRINGS ON THE ESCAPE SLIDE GIRT BAR AT DOOR 1R ARE WORN. REPLACED LEAF SPRINGS IAW SRM 51-40-02 AND REF IPC 25-66-05-05 .SDR FDEA201812203567Lamp · inoperative"SLIDE" LIGHT ON RT ENTRY DOOR DOES NOT COME ON WHEN DOOR IS ARMED. RELAMPED R1 DOOR "SLIDE" LT PER SMP AND B757 WDM 25-66-1. OPENED/CLOSED DOOR SEVERAL TIMES, AND SDR AALA201812049039Bottle · low pressureTHE L1 DOOR HAD LOW BOTTLE PRESSURE. MAINTENANCE REPLACED THE L1 DOOR SLIDE IAW JC 19L80025002, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.SDR AALA201810089031Slide · low pressureTHE AIRCRAFT WAS NOT GROUNDED. R1 DOOR SLIDE BELOW PRESSURE LIMITS. REPLACED SLIDE PER JOB CARD 19L80025002.SDR FDEA2018092102640Pump · malfunctionedRT HYD ENG PUMP EICAS DURING FLIGHT AUTO EVENT RECORDED IN FLIGHT SHOWING RIGHT SYSTEM HYDRAULIC PRESSURE AT 1070 PSI, WHILE LEFT SYSTEM WAS AT 2980 PSI, AND CENTER SYSTEM AT 3120 PSI. CRANKED NR 2 ENGINE AT THE GATE AS PER JET RUN-UP HANDBOOK, AND PRESSURE ROSDR U2RA201809190001Oven · smokeAFT GALLEY LEFT HAND NR 3 OVEN SMOKING WHEN IN USE. CIRCUIT BREAKER PULLED. OVEN PLACED ON NON-ESSENTIAL FURNISHING DEFERRED MAINTENANCE ITEM, IN ACCORDANCE WITH NEF MANUAL 25-20-01.
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