Boeing 757-204
Service difficulty reports · 676
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 = '757204' 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 = '757204' 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 FDEA202102160446Fill Port · corrodedR/H OVERWING FILL PORT FAILED BONDING CHECK. HAVE EVIDENCE OF CORROSION EVALUATED R/H OVERWING FILL POART IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 3, FIG 102 AND FOUND FILL PORT TO BE OUTSIDE SRM LIMITS.LIMIT OF REMAINING THICKNESS 0.240" ACTUAL=0.210". REPAIREDSDR FDEA202102160445Fill Port · corrodedL/H OVERWING FILL PORT FAILED BONDING CHECK HAS EVIDENCE OF CORROSION EVALUATED L/H OVERWING FILL POART IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 3, FIG 102 AND FOUND FILL PORT TO BE OUTSIDE SRM LIMITS. LIMIT OF REMAINING THICKNESS 0.240" ACTUAL=0.220". REPAIRED SDR FDEA202101270207Transmitter · failedDURING ARRIVAL GOT TE FLAP ASYM WHEN FLAPS SELECTED TO 5. FLAP INDICATION SHOWS BETWEEN 1 AND 5. COMPLIED WITH QRH, LANDED UNEVENTFULLY. TRAILING EDGE FLAP INDICATION SHOWING APPROXIMATELY HALF A NEEDLE WIDTH SPLIT AFTER BLOCK-IN. LEFT AND RIGHT TRAILING ESDR FDEA202101130082Door · bindingAT A/C ARRIVAL LEFT (L1) ENTRY DOOR WAS DIFFICULT TO OPEN AND DISARM. RELEASED FOR SERVICE, PER MEL: 52-11-01-A CATEGORY: B EXPIRATION: 16JAN21 "MEL 52-11-01-A: L1 DOOR/SLIDE) INOPERABLE. DEFERRED L1 ENTRY DOOR/SLIDE, REF MEL 52-11-01-A. ADJUSTED L1 PASSENGSDR FDEA202009142211Switch · out of adjustPDIS 923 52-70 1907 14SEP20 CDG OPEN U. MN CARGO DR SYS ON STATUS PAGE AFTER BLK OUT FROM BSL INFO 14SEP20 18:20. MC1 R REF TECH TIP NR 18-0045 FACT 15SEP20 09:35 CDG, AS PER FIM 52-72-00-815-802 CLEANNING CONNECTORS D7174 OF S10518 AND D7170 OF V10129. PERSDR FDEA202009032085Hose · leakingPDIS 923, 32-51, 1866, 03SEP20, AMS, OPEN U. AT APPROX 500' ON LANDING, RECEIVED 'L HYD QTY' EICAS. OBSERVED QTY SLOWLY DECREASING. AFTER LANDING RECEIVED 'L HYD SYSTEM PRESSURE' EICAS, QTY=0.16 SHGN 03SEP20 09:25. AMS U DURING T/S FOUND FLEX HYDR. HSDR FDEA2020072381577Bulb · inoperativeR1 DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED R1 DOOR SLIDE LIGHT BULB, P/N 767 . LIGHT CHECKED GOOD REF B757 AMM 33-51-06-2-1. OK FOR SERVICESDR FDEA2020040100639Girt Bar · damagedMDIS 923 52-10 1428 30MAR20 CDG OPEN U L1 DOOR DIFFICULT TO CLOSE. SHGN 30MAR20 19:13 CDG U L1 DOOR LINING REMOVED PER MM 52-11-02-04.FOR TROUBLESHOOTING PURPOSE. SHGN 30MAR20 19:19 CDG U HANDLE BOX COVER REMOVED PER MM 52-11-13-2. FOR TSDR FDEA2020012740224Skin · chafedWEAR MARK AT LEFT IN-BOARD FLAP LEADING EDGE. ALL WORK ACCOMPLISHED IAW EA F-5750-T0352020 P1 WING - FLIGHT SURFACES - LT INBOARD MAIN FLAP LEADING EDGE SKIN REPAIR.SDR FDEA202001170161Skin · corrodedPROTUDING FASTENERS APPROX AT STA-400 BETWEEN S14L ALL WORK ACCOMPLISHED IAW EA F-5330-T0351895 P1. FUSELAGE - PLATES & SKINS - CORROSION AT STA 394, STRINGER S-14L.SDR FDEA202001160150Doubler · crackedR2 DOOR UPPER HINGE CUTOUT PREVIOUS DOUBLER IS CRACKED. R2 DOOR WAS REMOVED AND REPLACED IAW AMM 52-11-01-4. OP'S CHECK OF DOOR GOOD IAW AMM 52-11-01-4.SDR FDEA2019122653301Sensor · dirtyDURING SERVICE CHECK, 1L MAIN ENTRY DOOR GIRT BAR OPERATIONAL CHECK FAILED ("SLIDE" LIGHT DO NOT COME ON). CLEANED BOTH 1L DOOR PROXIMITY SENSORS AND INSPECTED IAW AMM 25-66-10-2-0, OPERATED GIRT BAR BY ARMING AND DESARMING THE SLIDE SEVERAL TIME, "SLIDE" SDR FDEA2019122313278Frame · corrodedLT ELEVATOR OUTBOARD UPPER AND LOWER CONDUCTIVE FRAME ARE CORRODED. REPLACED LT ELEVATOR UPPER AND LOWER CONDUCTIVE FRAMES IAW SRM 55-20-01 AND 55-20-01-2R WITH EA F-2730-T0351345 STATIC BASE AND WICK REMOVED AND INSTALLED IAW AMM 23-61-01-2. FINISH RESTORSDR FDEA201912173250Floor Panel · damagedAFT PIT FLOOR PANEL 161AF HAS 1EA A PUNCTURE FABRICATED NEW FLOOR PANEL 161AF IAW BOEING PL 453N1270 BN-REVSDR FDEA201912173249Floor Panel · damagedAFT CARGO FLOOR PANEL 161BF HAS 1EA PUNCTURE FABRICATED AFT CARGO FLOOR PANEL 161BF IAW B757 SRM 53-60-53 AND BOEING PL 453N1270 REV BN PARTMARKED IAW BAC5307SDR FDEA2019121753246Guide · crackedLEFT WING ,OUTBOARD FLAP,AFTFLAP,INBOARD TRACK,GUIDE CRACKED. REPAIRED LEFT WING ,OUTBOARD FLAP,AFT FLAP,INBOARD TRACK,GUIDE CRACKED BY REMOVING DAMAGE AND APPLYING HOT BOND FIBERGLASS OVERLAY REPAIRS IN 2 EACH AREAS ,CURING,SHAPING AND RESTORING FINISH IASDR FDEA2019121303219Floorboard · damagedAFT MAIN CARGO FLOORBOARD P.NO 11864182-40 DAMAGED. REPAIRED FLOOR BOARD IAW B757-2 SRM 53-00-50-2RSDR FDEA2019121303218Floorboard · damagedAFT MAIN CABIN FLOORBOARD P.NO 11864182-42 DAMAGED. REPAIRED FLOOR BOARD IAW B757-2 SRM 53-00-50-2RSDR FDEA201912043178Panel · crackedRT WING T/E WIGGLE PANEL IS CRACKED AT APPROX WSTA 335. REMOVED AND REPLACED WIGGLE PANEL AT RT WING T/E AT APPROX WSTA335 PER SRM 51-40-02-0G APPLIED PROTECTIVE FINISH PER SRM 51-20-01-0G.SDR FDEA2019111542963Mechanism · wornPDIS 923 32-51 1126 14NOV19 CDG OPEN U LOGPAGES:2940898 WHILE TAXING AC STEERS LEFT . DOES NOT STEER STRAIGHT . REMOVED AND REPLACED NOSE WHEEL STEERING SUMMING MECHANISM INPUT LEVER AND SHAFTSDR FDEA2019111542962Frame · dentedAFT PIT FRAME BENT B.S.1420 BETWEEN STR 23L AND 24L. BS1420, STR 23L STR 24L REPAIRED FRAME AT STA 1420 STR23L-STR24L IAW FDX E.A.#F-5310-T0350569SDR FDEA2019111542961Plate · cracked#1 ENG O/B CORE COWL L/E PLATE CRACKED AT LWR END REMOVED AND REPLACED FILLER PER FEDEX EA # F7110-T0350560P1SDR FDEA2019111192914Battery Pack · failedMDIS 925 33-50 8137 09NOV19 DAY FACT U L1 DOOR AND LEFT SLIDE LIGHT INOP R/I 09NOV19 02:04 DAY U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 2013-1A POS: 1 SRL: 72660 TAG NBR: H733SDR FDEA201910172712Governor · failedPDIS 927 76-10 5586 17OCT19 LGG FACT U LOGPAGES:3009818 ON TAKEOFF WITH INITIAL POWER SETTING OF APPROX 1.1 EPR, THE LEFT ENGINE IS SLOW TO ACCELERATE AND HAS TO BE PUSHED UP ABOUT A HALF KNOB WIDTH MORE THAN THE RIGHT THROTTLE. WHEN EPR'S STSDR FDEA201910172677Lamp · inoperativeNOSE GEAR LIGHT DID NOT ILLUMINATE WHEN GEAR WAS DOWN AND LOCKED. NOSE GEAR LIGHT DID NOT TEST. VERIFIED LIGHTS WOULD NOT TEST FOR NOSE GEAR LIGHT. RE-LAMPED PER SWPM 20-84-15 AND PERFORMED PSEU BITE PER FIM 32-09 FIG 104. AND ALL TESTS PASSED. OK FOR SDR FDEA201910122614Adc · malfunctionedTE FLAP DISAGREE EICAS MESSAGE DISPLAYED GOING FROM FLAPS 20 TO FLAPS 25, RAN QRH CHECKLIST, LANDED FLAPS 20. ACCOMPLISHED FIM 27-51-FAULT TREE 810, REMOVED AND REPLACED THE LEFT ADC IAW AMM 34-12-01-4. ALL TESTS PASSED.SDR FDEA201909242336Hydraulic Line · leakingAT 3000', 170KT IAS, PUT GEAR HANDLE DOWN AND FLAPS TO 20 FOR BEFORE LANDING CHECK LIST. NOSE GEAR DID NOT GO DOWN (NO LIGHT) AND LEFT HYDRAULIC SYSTEM PRESSURE EICAS WITH GEAR DISAGREE MSG. COMPLIED WITH QRH, EMERGENCY DECLARED. FOUND NOSE GEAR STEERING PRESSSDR FDEA201907161620Metering Valve · malfunctionedDURING TAXI WITH NO TILLER AND NO RUDDER INPUT, A/C VEERS TO RIGHT UNSAFE IAW FIM 32-51 FAULT TREE 802 CHECKED ALL WHEELS TIRE PRESS FOUND ALL NORMAL NEXT SHIFT WILL CONTINUE T/S PERFORMED T/S ON NOSE WHEEL STEERING SYSTEM AND FOUND NOSE GEAR 3 DEGREES OFF FROSDR FDEA201905241157Sensor · out of adjustEICAS R FWD ENT DOOR CLIMBING THROUGH FL100. PRESSURIZATION NORMAL PERFORMED FIM 52-71 FAULT TREE 802 AND FIM 32-09 FAULT TREE 804 PSEU BITE TEST. NO FAULTS OBSERVED. ACFT RELEASED FOR FLIGHT CREATE MTSI 52-70/5222: R1 DOOR EICAS MSG PERFORMED DOOR WARNING SYSSDR FDEA201905161085Plate · corrodedCORROSION FOUND ON RT AILERON CONDUCTIVE PLATE. REPLACED CONDUCTIVE PLATE IAW DRAWINGS 113N7108,012N8509,SDR FDEA201905161084Plate · corrodedLT AILERON INBOARD AND OUTBOARD STATIC DISCHARGER BASES FAILED BONDING TEST REMOVED STATIC DISCHARGER BASES, ON REMOVAL OF OUTBOARD STATIC DISCHARGER BASE CONDUCTIVE PLATE FOUND TO BE CORRODED. REPLACED I/B AND OUTBOARD STATIC DISCHARGER BASES IAW SRM 51-40-SDR FDEA201905151075Outflow Valve · malfunctionedOUT FLOW VALVE FAILS TO OPEN ON MANUAL MODE OUTFLOW VALVE PN = 606832-18 SN = 74-1960. REPLACED OUTFLOW VALVE IAW AMM 21-31-03 OUTFLOW VALVE PN ON = 606832-14 SN ON = 24-502 BN ON = 92705156G8 TAG ON = 5156G8.SDR FDEA201905101021Gate · corrodedDOOR 1L LOWER GATE CORRODED OUTSIDE PERMITTED LIMITS IAW SRM 52-10-02-1A FIG 101 SHEET 7 DETAIL XI MIN THICKNESS ALLOWABLE 0.050" REMAINING THICKNESS AT BLENDOUT 0.010" INSTALLED NEW DOOR GATE IAW AMM 52-11-38.SDR FDEA201905071012Frame Splice · damagedFRAME SPLICE DAMAGED B/S 1480 STR25R-26R REPLACED FRAME SPLICE IAW SRM 51-40-02.SDR FDEA201905061008Floorbeam · crackedSTA 580 FLOORBEAM CRACKED - LBL45 , UPPER CORD AFT FLANGE. COMPLIED WITH EA F- 5310 - T0346588 P1 TITLE : FUSELAGE MAINFRAME STA.580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.SDR FDEA201905030992Gate · corrodedDOOR 2R LOWER GATE CORRODED EVALUATE. EVALUATED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02-01A FIG 101 SHEET 7 DETAIL XII. REPLACED DOOR GATE IAW AMM 52-11-38.SDR FDEA201905020982Support Bracket · crackedFWD CARGO DOOR FWD EDGE FRAME UPPER CORNER SUPPORT BRACKET IS CRACKED INSTALLED NEW BRACKET IAW SRM 51-40-02.SDR FDEA201905010978Support Bracket · dentedAFT CARGO DOOR FWD FRAME SUPPORT BRACKET (3RD FROM TOP ) IS DENTED. REPLACED AFT CARGO DOOR FWD FRAME SUPPORT BRACKET IAW SRM51-40-02. NEW PART FABRICATED IAW DRAWING 140N2791 REV B. AND GMM 7-0-1001.SDR FDEA201904290967Floorbeam · corrodedCORROSION FOUND STA 1681 RBL 13 FLOORBEAM UNDER LIP OF THE TOP "T" CAP. COMPLIED WITH EA F-5310-T0346723 P1. TITLE: FUSELAGE-MAINFRAME - CORROSION ON STA 1681 FLOORBEAM UPPER CHORD, REINFORCING REPAIR, BL 0 TO RBL 45.7.SDR FDEA201904290966Shear Web · corrodedCORROSION FOUND ON SHEAR WEB MAIN CARGO CABIN STA 1701 LBL 55.0. REMOVED CORROSION AT SHEAR WEB STA 1701 LBL 55.00 IAW SRM 51-10-02-OG ORIGINAL MAT. 0.071",MATERIAL REMAINING 0.038",MATERIAL LOSS 0.033",EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-5SDR FDEA201904290965Shear Web · corrodedCORROSION FOUND ON FLOOR SHEAR WEB MAIN CARGO CABIN STA 1688 LBL 57. REMOVED CORROSION AT FLOOR SHEAR WEB STA 1688 LBL 57 IAW SRM 51-10-02-OG ORIGINAL MAT. 0.071", MATERIAL REMAINING 0.058", MATERIAL LOSS 0.013", EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW SRSDR FDEA201904290964Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE STA 1640 RBL 45.5 MAIN CARGO CABIN. REMOVED CORROSION AT SEAT TRACK FLANGE STA 1640 RBL 45.5, IAW SRM 51-10-02-OG EVALUATED AREA DAMAGE, ORIGINAL MAT. 0.070", REMAINING MAT. 0.035",MAT LOSS 0.035" FOUND TO BE OUT LIMITS IAW SRM SDR FDEA201904261090Skin Panel · delaminatedDELAMINATION FOUND AT RT HORUZONTAL STABILIZER LWR. SKIN EXISTING REPAIR AREA. RT HORIZONTAL STABILIZER LOWER SKIN PANEL 185N4001-2, REPLACED IAW DRAWINGS 185N7001, 185N2001, 185N5003, 185N5004 AND SRM 51-40-02.SDR FDEA201904260934Shear Web · corrodedCORROSION SHEAR WEB AFT WEB AREA STA 1681 RBL 32. REMOVED CORROSION ON SHEAR WEB IAW SRM 51-10-02-0G. EVALUATED DAMAGED AREA, FOUND TO BE OUT LIMITS IAW SRM 53-00 00-51-1A,FIG 101, DETAIL III. CUT OUT DAMAGED AREA, FABRICATED, LOCATED, DRILLED, AND INSSDR FDEA201904260933Floorbeam · corrodedCORROSION T CAP FLOOR BEAM MAIN CABIN STA 1681 RBL 32.0 COMPLIED WITH FEDEX EA # F-5310-T0346723 P1.SDR FDEA201904260932Deck Plate · corrodedCORROSION ON EXISTING REPAIR FLOOR WEB MAIN CABIN STA 1716 FROM RBL 45 TO BLO. COMPLIED WITH EA F-5310-T0346613 P1.SDR FDEA201904260930Floor Support · corrodedAFT FLOOR SUPPORT CORRODED BETWEEN BS 1661-1668. BL 0. INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02SDR FDEA201904260928Floor Panel · dentedFLOOR PANEL 242XBF DAMAGED UPON INSPECTION PANEL IS WITHIN REPAIR LIMITS IAW SRM 53-00-50-1A REPAIRED FLOOR PANEL 242XBF IAW SRM 53-00-50-2RSDR FDEA201904181082Strap · corrodedLOWER SECTION 48 DOOR 313AL DOOR FITTINGS AND FRAME ARE CORRODED AT B.S 1885.2 REPLACED 4 GUSSETS P/N 148N6614-7, 148N6614-8, 148N6614-9 ,148N6614-10 AND FABRICATED AND REPLACED STRAP P/N 148N6613-2. AT BS 1885.2 IAW SRM 51-40-02 BOEING DRAWINGS 148N8402, SDR FDEA201904171104Skirt · crackedNR 6 LE SLAT, TRAILING EDGE SKIRT DAMAGED AND CRACKED REPAIRED IAW SRM 57-43-01-2R & SRM 51-70-07 GENERAL. REPAIR TRACKING ON EA F-5750-T0346875 A WINGS - FLIGHT CONTROL SURFACES - SLAT#6 - CLOSURE PANELS - DAMAGED HOLES - RCS TRACKING.
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