Boeing 757-236
Service difficulty reports · 2,544
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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 = '757236' 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 = '757236' 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 FDEA2019032870738Shear Plate · corrodedMAIN CABIN APPROX STA 377 LBL 46-57.5 FLOOR SHEAR WEB HAS EVIDENCE OF CORROSION COMPLIED WITH FEDEX E.A. F-5310-T034031 FUSELAGE-MAINFRAME-RIGID CARGO BARRIER FLOOR SHEAR PANEL CORROSION BLEND REPAIR AT STA 377,LBL 45-LBL 58SDR FDEA2019032760720Charger · no testDURING POST FLIGHT MX WALKAROUND FOUND THE INTERIOR EMERGENCY EXIT LIGHT ABOVE THE L1 DOOR INOP. REPLACED BATTERY CHARGER CPN 3311913 AND BATTERY CPN 3301128 IN POS M731, EMERGENCY LIGHT ABOVE L1 SDR FDEA2019032760719Charger · no testDURING POST FLIGHT MX WALKAROUND FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AFT OF THE L1 DOOR . REPLACED BATTERY CHARGER CPN 3311913 AND BATTERY CPN 3301128 POS M731, EMERGENCY LIGHT AFT OF L1 SDR FDEA201903100566Skin · dentedRT FUSELAGE HAS GOUGE AT STA. 218, JUST BELOW STR. 23R EVALUATED DAMAGE AT STA 218 JUST BELOW STR 23R FOUND TO BE DENT WITH GOUGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DET III. CUTOUT DAMAGE DIM 1.6" X 1.4" AND REPAIRED IAW SRM 53-00-01-2R REPAIR SDR FDEA201903060549Girt Bar · dirtyPDIS 955 25-60 4235 06MAR19 MSP FACT U LOGPAGES:2839823 COULDN'T ARM R1 DOOR ENTRY SLIDE. FACT 06MAR19 04:14 MSP U CLEANED GIRT BAR AND GIRT BAR FLOOR FITTINGS. DOOR ARMED NORMALLY SEVERAL TIMES. M/M REF 25-66-10.SDR FDEA2019022870510Lamp · inoperativeEXTERIOR BATTERY POWERED EMERGENCY LIGHT LOCATED AFT OF R-1 MAIN ENTRY DOOR INOP. REMOVED AND REPLACED LAMP ON R1 DOOR EXTERNAL SLIDE LAMP IAW B757 AMM 33-51-06-2-1OPS CK SATIFACTORY R1 DOOR EXTERNAL SLIDE LAMP IAW B757SDR FDEA201902190451Unknown · odorAT FL 340, AIRCREW SMELLED A STRONG PUNGENT ODOR COMING FROM VENTS. IT WAS STRONG BUT NOT QUITE STRONG ENOUGH TO GO ON OXYGEN. RAN PACKS FOR 30 MINUTES AT MAX HEAT. NO UNUSUAL ODORS NOTED THROUGHOUT MAIN CARGO COMPARTMENT AND IN FLIGHT DECK. RAN BOTH ENG AT MSDR FDEA201902110373Collar · brokenDURING SVC CHECK FOUND L1 DOOR HOLD OPEN LATCH COLLAR BROKEN. REMOVED AND REPLACED L1 DOOR HOLD OPEN LATCH AND LOCKING COLLAR IAW B-757 AMM 52-11-08-8. OPS CK GOOD.SDR FDEA201901160152Fitting · lack of lubePDIS 977 25-60 3952 16JAN19 GSO OPEN U LOGPAGES:2922410 RED SLIDE ARMED INDICATOR DOES NOT EXTEND FULLY WHEN THE DOOR IS ARMED (L1 DOOR) FACT 16JAN19 14:48 ORD APPLIED DC-33 TO GIRT BAR FLOOR FITTINGS AND REPOSITIONED UPPER DOOR LINER. PERFORMED OPS. SDR FDEA201901160151Warning System · activatedPDIS 950 27-80 6538 16JAN19 LOGPAGES:3084577 WHEN CONFIGURING FOR APPROACH RECEIVED MASTER CAUTION AND EICAS MASSAGE LE SLAT DISAGREE. RAN QRH, DECLARED EMERGENCY AND LANDED FLAPS 20.SDR FDEA201901120113Wire · brokenDURING CRUISE F/O TURNMED ON FOOT HEATER AND A SPARK AND A POP WAS FOLLOWED BY ELECTRICAL SMOKE. TURNED HEATER OFF AND SMOKE DISSIPATED. FOUND WIRES TO F/O LEFT FOOT HEATER BROKEN. REPAIRED BROKEN WIRES PER SWP CHAPTER 20-30 REFERENCING WIRING DIAGRAM 21-45-11SDR FDEA201901100082Mechanism · lack of lubeR1 DOOR LIGHT WAS INOP UPON ARRIVAL AT MCI WITH DOOR LOCKED. (GIRT BAR) LUBED R1 DOOR GIRT BAR SLIDER MECHANISM PER AMM 12-21-18-3 CYCLED DOOR ARMED LEVER SEVERAL TIMES DOOR SLIDE LIGHT OPS CHECK GOOD.SDR FDEA201901040014Gate · corrodedCORROSION ON 2L LOWER DOOR GATE FOUND OUTSIDE PERMITTED LIMITS IAW SRM 52-10-02- 1A, FIG 101, SHEET 7 , REV.125 REPLACE DOOR GATE IAW AMM 52-11-38-4 REV 122.7.SDR FDEA201901040019Slide · partial deployL1 ENTRY DOOR GIRT BAR STAYED ENGAGED. L1 DOOR ASSIST BOTTLE BLEW. SLIDE PARTIALLT DEPLOYED. AMM: 25-66-01-4. REMOVED AND REPLACED L1 DOOR SLIDE/RAFT, REF AMM 25-66-01-4. OK FOR SERVICE. REMOVED SAFETY PINS INSTALLED AT L-1 DOOR EMERGENCY POWER RESERVOIR. A/C SDR FDEA201901030011Cleat · dentedDOOR 3L CLEATS BENT ON CENTER STRINGER, REPLACE. FABRICATED NEW CLEATS FOR DOOR 3L CTR STRINGER IAW DRAWING 146N6346 REV INITIAL AND GMM 7-0-1001 REV 153. INSTALLED NEW CLEATS IAW DRAWING 146N6313 REV K AND SRM 51-40-02 REV 125.SDR FDEA201901030009Adc · failedAT 4000FT IN THE TURN TO JOIN 36L LOC THE CAPTAINS AIRSPEED BECAME UNRELIABLE. TEMP WAS 13 DEGREES C WITH ENG TAI OFF. AN EMERGENCY WAS DECLARED. ATC PROVIDED VECTORS TO ALLOW US TIME TO RUN THE AIRSPEED UNRELIABLE CHECKLIST. THE CHECKLIST WAS FOLLOWED AND DSDR FDEA201901020007Beam · corrodedLOWER CANTED BEAM UNDER WING TO BODY FAIRING 197AL B/S 1040-1060 CORRODED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-71-1A ALLOWABLE DAMAGE 1, FIG 101, DETAIL IV AND VII, REV 125. INSTALLED NEW BEAM IAW SRM 51-40-02 REV 125 AND DRAWING 149N7553 REV C.SDR FDEA2019010113624Structure · corrodedWTB. CHORD CORRODED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-71 ALLOWABLE DAMAGE 1 FIG 101 DETAIL IV AND VII REV 125 REPAIRED CHORD IAW EA F-5340-T0344282 P1.SDR FDEA201812283615Door Frame · damagedBS 231.21 BL0 FRAME DAMAGED AT FWD ACCESS DOOR LATCH FITTING. REPAIRED FRAME AT BS 231.21 B/L0 IAW SRM 53-00-07 REPAIR 7 REV 125.SDR FDEA201812283614Mount · damagedFWD LAV UPPER I/B FWD MOUNT IS DAMAGED ON FRAME B/S 297 BETWEEN S2L AND S3L, REPLACEMENT REQD. FABRICATED AND INSTALLED NEW MOUNT P/N 232N2003-4 IAW SRM 51-40-02 REV 125 AND DRAWING 232N2003 REV A.SDR FDEA2018122103566Control Panel · malfunctionedDURING TAKEOFF ROLL @ 85KTS CAPT SIDE LOST AIRSPEED AND ALTIMETER. REJECTED TAKEOFF AT 85KTS. REF MCDP GROUND TEST 04-MCP DISENG BAR TEST FAILED. REMOVED AND REPLACED AFCS MODE CONTROL PANEL REF AMM 22-11-02-2. PERFORMED MCDP GROUND TEST 04, 30 AND 40 ASDR FDEA201812193558Crease Beam · damagedCREASE BEAM WEB DAMAGED BS 1016 RBL 64 REPLACEMENT REQD. REPLACED CREASE BEAM WEB IAW SRM 53-40-13-1A REV 125 AND DRAWING.SDR FDEA201812183543Tee Fitting · corrodedKEEL BEAM WEB TEE CORRODED OUT OF LIMITS IAW SRM 53-00-71-1A FIG 101 DETAIL III AND DETAIL VII REPLACE AS REQD. KEEL BEAM TEE REPLACED IAW SRM 51-40-02 REV 125 AND DRAWING 144N8140 REV E.SDR FDEA201812183535Gate · wornWEAR MARK ON DOOR 4L LOWER GATE AFT O/B. EDGE OUTSIDE PERMITTED LIMITS IAW SRM 52-10-02-01A FIG 101 SHEET 7 REV 125. REPLACE DOOR GATE IAW AMM 52-11-38-4 REV 122.7.SDR FDEA201812153506Floor Panel · dentedDENT FOUND ON FLOOR PANEL BSTA 560-680 LBL 25-45. FLOOR PANEL REPAIRED AT BSTA 560-680 LBL 25-45 IAW SRM 53-00-50-2R FIG 201 REV 125.SDR FDEA201812153503Gate · damagedWEAR MARK ON DOOR 4R LOWER GATE OUTSIDE OF ALLOWABLE LIMITS IAW SRM 52-10-02-01A FIG 101 SHEET 7 REV 125. REPLACE DOOR GATE IAW AMM 52-11-38-4 REV 122.7.SDR FDEA201812143500Gate · corrodedLOWER DOOR GATE 2R HAS CORROSION OUTSIDE ALLOWABLE LIMITS IAW SRM 52-10-02-01A FIG 101 SHEET 7 REV 125. REPLACED DOOR GATE IAW AMM 52-11-38-4 REV 122.7.SDR FDEA2018122163582Seat Track · corrodedEVIDENCE OF CORROSION ON SEAT TRK BSTA 1204-1210 RBL 58.22 CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52-1A. DETAIL VII REV 125. MAX ALLOWABLE CLEANUP LIMITS (X) = 20% THICKNESS, TRACK FLANGE THICKNESS = .0.085SDR FDEA2018120653432Warning Message · false activationPDIS 952 52-10 5943 05DEC18 MEM FACT U LOGPAGES:2924671 MOMENTARY LEFT FORWARD ENTRY DOOR EICAS DURING CRUISE AT FL 360 PRESURIZATION NORMAL. FACT 05DEC18 05:50 MEM U COMPLIED WITH FIM 52-11 FAULT TREE 802. NO VISUAL DEFECTS NOTED. OPERATSDR FDEA201812040137Angle · corrodedLT WING, RIVETS DAMAGED ON OT/BD TRAILING EDGE WEDGE OF NR 5 LE SLAT REPLACED CORRODED CLOSURE ANGLE TO SLAT NR 5 T/E WEDGE O/B END IAW EA T F-5750-T0344281 A P1 "WING -FLIGHT SURFACES-OUTBD CLOSURE ANGLE - SLAT NR 5 - CORROSION. THIS REPAIR IS CLASSIFIED AS MSDR FDEA2018122143580Seat Track · corrodedSUSPECT CORROSION AT B/S 1180-1200 LBL 24.5 CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52-1A. DETAIL VII REV 125. MAX ALLOWABLE CLEANUP LIMITS (X) = 20% THICKNESS, TRACK FLANGE THICKNESS = .0.085", MAX ALLOWABSDR FDEA201812043528Fitting · corrodedFITTING ON NR 1 CARGO DOOR CUT-OUT LOWER SILL AT BS 612.7 CORRODED. EVA AND RECTIFY FITTING ON NR 1 CARGO DOOR CUT-OUT LOWER SILL AT BS 612.7 REPLACED IAW SRM 51-40-02 REV 125.SDR FDEA201812030123Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, 22" AFT OF FRONT SPAR AT WS 204.5 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND SDR FDEA201812030122Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 269 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TOSDR FDEA201812030121Skin · corrodedRT WING, CORROSION ON UPPR SURFACE, ABOVE REAR SPAR AT WS 361 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TO SDR FDEA201812030120Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, ABOVE FRONT SPAR, WS 642 TO WS 654 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 ANSDR FDEA201812030119Skin · corrodedRT WING, CORROSION ON UPPER SURFACE, AS OF REAR SPAR WS 289-293 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUND TSDR FDEA201812030118Skin · corrodedRT WING CORROSION ON UPPR SURFACE AFT OF REAR SPAR, WS312 TO WS316 CORROSION REMOVED IAW SRM 51-10-02 REV 125, MEASURED AND EVALUATED BLEND IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101, TABLE 1 REV 125 AND FOUNSDR FDEA201812030112Skin · corrodedLT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 215 REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 TABLE 1 REV 125, AND FSDR FDEA201812030111Skin · corrodedLT WING, CORROSION ON UPPER SURFACE, ABOVE REAR SPAR AT WS 300 REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUT IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 AND SRM 57-20-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 TABLE 1 REV 125, AND FOSDR FDEA201812030110Skin · corrodedLT WING UPPER TE, EVIDENCE OF CORROSION ADJACENT TO FASTENER HEADS AT AREA 5 INCHES AFT OF REAR SPAR AND 67 INCHES OUTBOARD OF WING ROOT FAIRING 195AL REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUT IAW SRM 57-20-01-1A ALLOWABLE DASDR FDEA201811300155Skin · corrodedLT WING, UPPER SURFACE RSS 170 TO RSS 200 AT WING SKIN AND TRAILING EDGE PANEL JOING SUSPECT CORROSION. COROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE OF LIMITS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 1 REV 125. REPAIR CARRIED OUT IAW EA #F-573SDR FDEA201811300109Skin · corrodedPLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS.748 TO WS761, 2 INCHES FWD OF REAR SPAR AND TRILING EDGE PANEL JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 4 REV 125 ANSDR FDEA201811300108Skin · corrodedPLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS 791 TO WS 806, 7 INCHES AFT OF FRONT SPAR AND LEADING EDGE JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125. MEASURED AND EVALUATED BLEND OUTS IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 1, FIG 101 TABLE SDR FDEA201811300107Skin · corrodedPLEASE EVALUATE EXISTING BLENDS ON LT WING UPPER SURFACE AT WS 791 TO WS 806, 7 INCHES AFT OF FRONT SPAR AND LEADING EDGE JOINT REMOVED CORROSION IAW SRM 51-10-02 REV 125 EVALUATED BLEND OUT AND FOUND AREA TO BE OUT OF LIMITS IAW DUE TO LOCATION OF DAMAGE IAW SDR FDEA201811300005Crease Beam · corrodedEVIDENCE OF CORROSION ON CREASE BEAM BS907-936 RBL64. CORROSION REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-40-13-1A ALLOWABLE DAMAGE FIG 101 REV 125 AT BS 936 RBL 64. CREASE BEAM INBOARD CHORD REPLACED IAW SRM 51-40-02 REV 125, DRAWING 144N5152 DRAWING SDR FDEA201811300004Crease Beam · corrodedEVIDENCE OF CORROSION ON CREASE BEAM BSTA 1052-1180 RBL 64 CORROSION REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-40-13-1A ALLOWABLE DAMAGE FIG 101 REV 125 AT BS 1052 AND BS 1145 RBL 64. CREASE BEAM INBOARD CHORD REPLACED IAW SRM 51-40-02 REV 125, DRAWINGSDR FDEA201811303401Floor Panel · crackedFLOOR PANEL CRACKED 252MUF FLOOR PANEL REPAIRED IAW SRM 53-00-50 FIG 201 RPR # 00001. SHEET 001.SDR FDEA201811303581Seat Track · corrodedEVIDENCE OF CORROSION ON SEAT TRK BS1180-1200 RBL 47 CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52-1A. DETAIL VII REV 125. MAX ALLOWABLE CLEANUP LIMITS (X) = 20% THICKNESS, TRACK FLANGE THICKNESS = .0.085", MASDR FDEA2018122103579Seat Track · corrodedEVIDENCE OF CORROSION ON SEAT TRK BS1188-1200 LBL 45 CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52-1A. DETAIL VII REV 125. MAX ALLOWABLE CLEANUP LIMITS (X) = 20% THICKNESS, TRACK FLANGE THICKNESS = .0.085", MA
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