Boeing 757-225
Service difficulty reports · 1,988
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 = '757225' 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 = '757225' 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 FDEA202003130560Support Angle · corrodedMAIN CABIN AFT DECK PLATE VIEWED FROM BELOW STA 1715 RBL 12 SUPPORT ANGLE CORRODED REMOVED AND REPLACED CORRODED ANGLE IAW BOEING DWG 146N5221 REV BSDR FDEA202003120558Seat Track · corrodedSURFACE CORROSION AT BODY STATION 118 (UNDERNEATH MAIN CARGO DECK FLOORBOARD) FLOOR SUPPORT BEAM, SECOND BEAM FROM LEFT, AROUND AND BELOW SEAT TRACK, AROUND HYLOCKS ON SEAT TRACK STANDOFF BRACKET, AND AROUND AND ON STANDOFF FOR SEAT TRACK. DOT AND STREAMSDR FDEA202003120554Shear Web · corrodedMAIN CABIN FLOOR SUPPORT, STRUCTURAL SHEAR WEB IS CORRODED AT APPROX STA 1691 APPROX LBL10 REPAIRED IAW B757-200 SRM 53-60-51-2R REPAIR 2SDR FDEA202003120553Shear Web · corrodedMAIN CABIN FLOOR SUPPORT SHEAR WEB (DECK PLATE) IS CORRODED AT APPROX STA 1686 APPROX LBL10 ALL WORK ACCOMPLISHED ON N/R N00342 IAW B757-200 SRM 53-60-51-2R REPAIR 2SDR FDEA2020031210544Shear Web · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS PITTED AT APPROX STA 1683 APPROX LBL 12.5 REPAIR ACCOMPLISHED ON N/R N00342 IAW B757-200 SRM 53-60-51-2R REPAIR 2SDR FDEA2020031210543Shear Web · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS CORRODED AT APPROX STA 1701 APPROX LBL7 REPAIR ACCOMPLISHED ON N/R N00342 IAW B757-200 SRM 53-60-51-2R REPAIR 2SDR FDEA2020031210542Shear Web · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS PITTED AT APPROX STA 1706 APPROX LBL7 ALL WORK ACCOMPLISHED ON NR N00342 IAW B757-2 SRM 53-60-51-2R REPAIR 2SDR FDEA2020031210540Nut Plate · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE AT STA 1681 APPROX RBL 23 FLOOR BOARD NUT PLATE STRIP IS CORRODED FABRICATED NUTPLATE STRIP IAW BOEING DWG 146N5693 REV C AND INSTALLED ON N/R N00334SDR FDEA2020031210539Nut Plate · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE AT STA 1681 APPROX RBL 32 FLOOR BOARD NUT PLATE STRIP IS CORRODED FABRICATED NUTPLATE STRIP IAW BOEING DWG 146N5693 REV C AND INSTALLED ON N/R N00334SDR FDEA2020031210538Shear Web · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE AT STA 1681 APPROX RBL 22 SHEAR WEB IS CORRODED REPAIR ACCOMPLISHED ON N/R N00334 IAW B757-200 SRM 53-60-51-2R REPAIR 2SDR FDEA2020031210537Shear Web · damagedMAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS CORRODED AT APPROX 1683 RBL 31 ACCOMPLISHED FEDEX EA # F-5321-T0352653, FUSELAGE - CARGO COMP FLOORS - FLOOR SUPPORT, STA 1681 - 1701, RBL 20 AND 23, EDGE DAMAGE, BLEND REPAIR. ACCOMPLISHED DOUSDR FDEA2020031210536Nut Plate · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE AT STA 1681 APPROX RBL 40 FLOOR BOARD NUTPLATE STRIP IS CORRODED ACCOMPLISHED FEDEX EA # F-5321-T0352606 FUSELAGE- CARGO COMP FLOORS - STA 1681, RBL 40, DOUBLE DRILLED HOLE, FREEZE PLUG REPAIR. ACCOMPLISHED DOUBLER REPAIRSDR FDEA202003090506Door Frame · crackedR-2 DOOR SKIN UPPER HINGE CUT OUT IS CRACKED. REPAIR OF FWD FRAME OF NUMBER 2 RIGHT SIDE PASSENGER DOOR COMPLIED WITH IAW B757-200 SRM 52-10- 02 02-2R REPAIR 1. HFEC INSPECTION REQUIRED AT 50,000 TOTAL DOOR FLIGHT CYCLES OR 5,800 FLIGHT CYCLES AFTER REPAIRSDR FDEA2020030970500Seat Track · corrodedCABIN SEAT TRACK CORRODED ABS1071- BS 1075, BL LBL 24 REPAIRED SEAT TRACK IAW B757-2 SRM 53-00-52-2R REPAIR #4SDR FDEA202003050495Slat · delaminated#3 SLAT REQUIRES REPLACEMENT REMOVED AND REPLACED AND PERFORMED OPS TEST ON #3 SLAT IAW B757 AMM 27-81-02-4 OPS CHECK GOODSDR FDEA2020030540485Seat Track · gougedMAIN CABIN RH SIDE SEAT TRACK IS GOUGED BS 619, RBL 00 REPAIRED SEAT TRACK IAW FEDEX EA# F-5320-T0352523-P1 FUSELAGE AUXILIARY STRUCTURE - CABIN SEAT TYRACK STA 619 BL 0 GOUGE SPLICE REPAIRSDR FDEA2020030530481Rub Strip · crackedRIGHT WING INBD FLAP SUPPORT BRACKET HAS CRACKED RUB STRIP AT AFT TRUNNION FAIRING REMOVED ABD REPLACED RUB STRIP AT R/W I/B FLAP SUPPORT AT AFT TRUNNION FAIRING IAW BAC DWG 113N1831 REV-SRM 51-40-02SDR FDEA202003010471Balance Weight · corrodedLEFT WING,OUTBOARD AILERON,INBOARD COUNTER BALANCES,SEVERAL HAVE CORROSION AND OR FLAKING PAINT REMOVED AND REPLACED 1 CORRODED L/W O/B AILERON I/B COUNTER BALANCE IAW B757 SRM 51-60-01-OG AND 51-40-02.RESTORED FINISH ON REMAINING COUNTER BALANCES IAW B7SDR FDEA2020022870416Skin · dentedFUSELAGE SKIN REPAIR AT APPROX. STA 1600 STR 26L-29L REQ ENLARGING TO INCORPORATE OTHER DAMAGES PER EA F-5330-T0346172B ALL WORK ACCOMPLISHED IAW FEDEX EA # F5330-T0348842-P1, FUSELAGE-PLATES AND SKIN-REPAIR OF FUSELAGE SKIN DAMAGE- STA 1553 TO STA 162SDR FDEA2020022870417Skin · dentedL/H SIDE EXTERIOR FUSELAGE SKIN IS DENTED APPROX 7" AFT OF THE PILOTS SIDE SLIDING WINDOW APPROX 20" UP FROM THE FLOOR LEVEL MEASURED DENT; MINOR AXIS .500", DEPTH .010" A/Y = 50, FOUND TO BE STRUCTURALLY ACCEPTEBLE PER FEDEX E.A. # F-5330-T0352423 P1: FUSSDR FDEA2020022870415Web · dentedMAIN CABIN FLOOR BOARD SUPPORT WEB UNDER RH SEAT TRACK AT STA. 1337 RBL 25 WEB AND ATTACH ANGLE DENTED AT ATTACHING FASTENER. REMOVED, FABRICATED IAW B757-200 SRM 53-60-51-01 AND REPLACED ATTACH ANGLE IN MAIN CABIN FLOOR BOARD SUPPORT WEB UNDER R/H SEAT TRSDR FDEA202002270414Plate · corrodedMAIN CABIN RH SIDE METAL PLATE IS CORRODED UNDER THE SEAT TRACK BS 676, RBL 58 REMOVED AND REPLACED METAL PLATE UNDER THE SEAT TRACK AT BS676RBL 58 IAW VENTURA AEROSPACE DWG : 3458 REV L, B757 SRM 51-40-02-0G, B757 SRM 51-20-01-0GSDR FDEA2020022870413Web · dentedFUSELAGE MAIN CARGO DOOR INTERIOR SKIN AFT LOWER WEB HAS PROTUDING DENT. REMOVED AND REPLACED MAIN CARGO DOOR INTERIOR AFT LOWER WEB IAW B757 SRM 51-4 40 40-02, BOEING DWG 65-49309 REV D, AND B757 SRM 51-20-01SDR FDEA2020022870412Web · dentedFUSELAGE MAIN CARGO DOOR INTERIOR SKIN FWD LOWER WEB HAS A PROTUDING DENT. REMOVED AND REPLACED MAIN CARGO DOOR INTERIOR FWD LOWER WEB IAW B757 SRM 51-4 40-02, BOEING DWG 65-49309 REV D, B757 SRM 51-20-01SDR FDEA2020022870411Skin · dentedFUSELAGE EXT SKIN BETWEEN ST 1360 AND 1380 ST S20L HAS DENT REPAIRED DENT IAW FEDEX E.A.# F-5330-T0352390 TITLE: FUSELAGE - PLATES AND SKINS - FUSELAGE SKIN, STA 1360 - 1380, S20L, DENT REPAIRSDR FDEA2020022870410Closeout Panel · crackedPARTS RACK - P51 PANEL LOWER CLOSEOUT CONNECTOR PANEL IS CRACKED MULTIPLE LOCATIONS REMOVED, FABRICATED, AND INSTALLED NEW LOWER CLOSEOUT CONNECTOR PANEL IAW PARSONS DWG# 13481207 REV A AND B757 SRM 51-40-02SDR FDEA2020022860394Deck Plate · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE SHEAR WEB (DECK PLATE) IS PITTED AT APPROX STA 1701 APPROX LBL 31 REPAIRED MAIN CABIN FLOOR SUPPORT SHEAR WEB (DECK PLATE) AT STA 1701, LBL 31 IAW B757 SRM 53-60-51-2R REPAIR 2, B757 SRM 51-20-01-0G AND B757 AMM 51-21-00-SDR FDEA202002200360Skin · crackedRIGHT WING TRAILING EDGE LOWER PANEL BETWEEN #8 AND #9 SPOILERS CRACKED. REPAIRED PANEL PER B757 SRM 57-51-01-2R.SDR FDEA2020022090355Balance Weight · corrodedLEFT WING, OUTBOARD AILERON ,2EA COUNTER BALANCES HAVE FLAKING PAINT AND/OR CORROSION REMOVED AND REPLACED 2 CORRODED LEFT WING O/B AILERON COUNTER BALANCES IAW B757 SRM 51-60-01-OG AND 51-40-02.RESTORED FINISH ON OTHER 2 COUNTER BALANCES IAW B757 AMM 51SDR FDEA202002170349Support · crackedAPU FIRE BOTTLE ACCESS PANEL LH LOCK BRACKET INBD SUPPORT CRACKED REMOVED AND REPLACED LH LOCK BRACKET INBD SUPPORT PN:148N661449 AT APU FIRE BOTTLE ACCESS PANEL IAW B757 SRM 51-40-09SDR FDEA2020021870348Channel · gougedL/H MLG WHEEL WELL PANEL 197DL I/B ATTACH ANGLE GOUGED AT AFT END REPAIRED AREA PER B757 SRM 53-40-71-2R AND 51-70-11-OGSDR FDEA2020011650134Flap System · contaminatedDURING APPROACH WHEN GOING FROM FLAPS 20 TO FLAPS 25 GOT TE FLAP DISAGREE. RAN QRH. LANDED FLAPS 20, LUBRICATED THE TRAILING EDGE FLAP SYSTEM AMM 12-21-09-3. ALL GEARBOXES WERE SERVICED PROPERLY. NOTED THERE WAS WATER PRESENT IN SOME AREAS AND PUSHED OUT SDR FDEA2019120123145Skin Panel · delaminatedRIGHT HAND HORIZONTAL STABILIZER HAS A PANEL ON THE BOTTOM SIDE WITH A DELAMINATED AREA OF APPROXIMATELY 2' X 3'. AREA IS LOCATED JUST AFT OF THE LEADING EDGE AND 5' OUTBOARD OF THE FUSELAGE. REMOVED & INSTALLED NEW SKIN PANEL RT LOWER HORZ STAB IAW SRM 51-4SDR FDEA2019082191947Skin · dentedRH WING ON #7 SLAT UPPER SURFACE IB SIDE HAS A DENT. REPAIRED R/H WING #7 SLAT UPPER SURFACE I/B SIDE IAW B757 SRM 57-43-02-2R, REPAIR 1 AND AND B757 SRM 51-70-10-2R, IAW FEDEX E.A. T F-5750-T0348918 P1 WING - FLIGHT SURFACES - #7 SLAT TRAILING EDGE WEDGESDR FDEA201905161086Static Line · out of positionUPON CLOSING THE R DOOR (ENTRY), THE HANDLE WENT IN THE ARMED POSITION, BUT THE ARMED LIGHT WASNT ILLUMINATED. DOOR HANDLE JAMMED IN THE ARMED POSITION. DOOR DIDNT APPEAR TO BE CLOSED AT THE AFT SEAL. ROUTED AND STOWED EXCESS STATIC LINE FROM GIRT BAR TO ESCAPSDR FDEA2019042290861Tire · failed#6 TIRE FAILURE ON LANDING COMPLIED WITH TIRE BURST INSP PER AMM 05-51-16. NO DEFECTS NOTED EXCEPT #6 TIRE FAILURE. R&R #6 MLG WHEEL & TIRE ASSY PER AMM 32-45-01. R&R #5 MLG WHEEL & TIRE ASSY PER AMM 32-45-01.SDR FDEA201902160432Door Seal · out of positionREPEAT WRITE-UP, VERY LOUD SQUEAL FROM L1 ENTRY DOOR. INSPECTED L1 DOOR INSIDE SEAL REF AMM 52-09-01. FOUND SOME LOCATIONS OUT OFF TRACK, RESECURED AND PERFORMED OPS CHECK, OPS CHECK GOOD, SEAL AND DOOR IN NORMAL CONDITION. ACFT OK FOR SERVICE,SDR FDEA201901220192Latch · unlatchedRIGHT ENTRY DOOR LATCH CAME OUT OF LATCHED IN-FLIGHT ON ITS OWN PERFORMED OPS TEST OF R1 DOOR REF MM 52-11-00-2 DOOR CLOSES AND LOCKS WITH NO DEFECTS NOTED INSPECTED DOOR AND FOUND NO VISUAL DEFECTS NO HISTORY FOR 90 DAYS A/C OK FOR SERVICE.SDR FDEA201811273376Light · inoperativeON APPROACH TO RUNWAY 27 KMEM, WHEN LANDING GEAR SELECTED DOWN, THE LEFT GEAR DOWN GREEN LIGHT DID NOT ILLUMINATE. DECLARED AN EMERGENCY WITH KMEM ATC, MADE LOW PASS TO ALLOW TOWER TO VISUALLY VERIFY ALL GEAR NORMAL. NORMAL LANDING AFTER VERIFYING GEAR DOWNSDR FDEA201810283046Acm · seizedON TAXI OUT, THERE GRINDING NOISE AND SMOKE BELLOWING OUT OF THE GASPERS. THE CREW TURNED OFF THE LEFT PACK AND RAN THE SMOKE AND FIRE, FUMES CHECKLIST. THE SMOKE CLEARED. CFR CHECK OUT THE AIRCRAFT. NO FIRE DETECTED. TAXI BACK TO GATE. COMPLIED WITH SMOKE/FUMSDR FDEA201806221563Warning System · false activationGND PROX SYS FAULT AND BOTH FO PFD AND ND DISPLAYED RED X TERR SYS STATUS MSG ON BLOCK IN. RECYCLED DCU CIRCUIT BREAKER REF AMM 34-22-01-4-99. SYSTEM CHECKS NORMAL.SDR FDEA201806051393Skin · debondedRT INBD FWD FLAP UPPER SURFACE HAS A DISBONDED COMPOSITE REPAIR. REPAIRED RT INBD FWD FLAP UPPER SURFACE IAW SRM 51-71-10-2R REPAIR 4 & 57-53-01-2R FIG 201 DET I.SDR FDEA2018053141315Skin · damagedSKIN DAMAGED, BS 1500 AND 1560, STRINGERS 1L AND 2L. REPAIRED IAW EA F-2560-T0339100, B P2.SDR FDEA201803250779Sensor · dirtyDURING DESCENT THRU FL 280, RECIEVED A LEFT DOOR EICAS. NO HISTORY NOTED, PERFORMED AN ADJUSTMENT TEST OF THE DOOR, CLEANED THE SENSOR. DOOR WARNING & INDICATION CHECKED GOOD.SDR FDEA201802080327Frame · gougedPUNCTURE AT FRAME STA 1440 AT STR 25L AFT CARGO. ALL WORK ACCOMPLISHED ON EA F-5310-T0338309 P1. FRAME INBOARD CHORD REPAIR BETWEEN STRINGERS S-23L AND S-26L.SDR FDEA201709122478Bulb · inoperativeL1 DOOR EMERGENCY SLIDE LIGHT (EXTERIOR) INOPERATIVE. REMOVED BULB AND CLEANED SOCKET. INSTALLED A NEW BULB IAW MM 33-51-06-2-1. OPS CHECKED NORMAL.SDR FDEA201706011553Lamp · inoperativeCOCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE DURING TEST. REPLACED THE LAMPS AND OPS CHECKED NORMAL IAW MM 33-51-09-3. ACFT OK FOR SERVICE.SDR FDEA201705071371Girt Bar · out of adjustFOUND R1 DOOR NOT ARMING SMOOTHLY. DURING MX INSPECTION, FOUND THE GIRT BAR SLIDE LEATHER BLOCKING THE R1 DOOR ARMING ROD FROM MOVING. REMOVED THE GIRT BAR CENTER ALIGNMENT PLATE AND REPOSITIONED LEATHER THEN REINSTALLED CENTER ALIGNMENT PLATE ON R1 DOORSDR FDEA201705041352Bottle · low pressureFOUND L1 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED L1 DOOR SLIDE ASSY IAW AMM 25-66-01-4. OPS CHECKED GOOD.SDR FDEA201705021340Pivot · crackedLEFT MAIN LANDING GEAR BEAM RETRACT ACTUATOR LINK PIVOT SHAFT AFT END HAS CIRCUMFERENTIAL CRACKED. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR BEAM RETRACT ACTUATOR LINK PIVOT SHAFT, REFERENCE 32-32-01-4
Back to Boeing 757-225