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 FDEA201207162590Collar · brokenDURING PRE-DISPATCH CHECK, NOTED L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REMOVED BROKEN PIECES. REPLACED LOCKING COLLAR AND LATCHING MECHANISM ON L1 DOOR IAW MM 52-11-08-4, OPS CHECKED GOOD.SDR FDEA201207132575Mechanism · brokenDURING PRE-DISPATCH CHECK, NOTED L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REPLACED LOCKING COLLAR AND LATCHING MECHANISM ON L-1 DOOR IAW MM 52-11-08-4, OPS CHECKED GOOD IAW SAME.SDR FDEA201207072509Support Bracket · looseL1 DOOR WILL NOT CLOSE. APPEARS TO BE OUT OF RIG. FOUND BOLTS ON LOWER SUPPORT BRACKET FOR THE GUIDE ARM LOOSE ON THE L-1 DOOR. ADJUSTED BRACKET AND RETORQUED BOLTS REF AMM 52-11-04-02 AND 52-11-00-5. ACFT OK FOR SERVICE. FINAL CLOSED.SDR FDEA201206212291Rod · malfunctionedRT ENTRY DOOR SLIDE PLACARD IS PROTRUDING WHEN IN DISARM POSITION. ALL OTHER INDICATIONS SHOW SLIDE DISARMED. REMOVED LOWER AND MID INTERIOR CORES AND DOOR HANDLE REPLACED ROD ASSY AND TESTED PER MM 52-11-00-216-025. OPS CHECKED GOOD, NO RIGGING OR ADJUSSDR FDEA201206212290Slide · dislodgedLEFT ENTRY DOOR WAS DISARMED. DOOR WAS CRACKED OPEN FROM INSIDE. PERSONNEL FROM THE OUTSIDE OPENED THE DOOR FURTHER, AT WHICH TIME IT APPEARED THE DOOR CAUGHT AND THE SLIDE FELL OUT. SLIDE DID NOT FULLY DEPLOY. STILL SHOWS GREEN PRESSURE ON THE SLIDE. WSDR FDEA201206152248Elbow · leakingON TAKEOFF DISCREPANCY BETWEEN CAPTAIN`S AIRSPEED AN F/O AIRSPEED OF 40KIAS. REJECTED T/O AT 100KIAS BASED ON F/O AIRSPEED INDICATOR. CLEARED RWY & PERFORMED RTO CHECKLIST. BRAKE COOLING TIME OF 51 MIN. FOUND CAPT'S PITOT TUBE CLOGGED WITH ORGANIC MATTER. RSDR FDEA201205211913Skin · damagedEXTERNAL LOWER FUSELAGE LAVATORY SERVICE PANEL CUT OUT EDGE DOUBLER AFT/INBD CORNER BUCKLED COMPLIED WITH EA F-5330-157269 FUSELAGE PLATES AND SKIN-SECTION 41-SKIN CORROSION. REPAIR STA 418-430 S-28L REF 8100-9 DATED MAY 17, 2012. MAJOR REPAIR.SDR FDEA201205151814Structure · crackedNR 2 PYLON, HORIZ FLANGE FASTENER HOLE CRACKED IN TITANIUM RT THIRD HOLE FROM AFT BULKHEAD. REAMED HOLE TO .405 IAW EA F-5450-157204 STEP1, AND 2ND HOLE TO .437 IAW EA F-5450-157204, STEP 3, NDT CHECK FOR CRACK, NO CRACK NOTED. INSTALLED FASTNER IAW-SRM-51-40SDR FDEA201205041736Bushing · migratedNR 2 PYLON MID SPAR ATTACH FITTING LUG RT SIDE BUSHING MIGRATED. (RT SIDE) ACFT SIDE. REMOVED MIGRATED BUSHING IAW SOPM-20-50-03. NO CORROSION NOTED, MEASURED LUG BORE AND IT IS 1.8140 FOUND TO BE OVERSIZE DIAMETER IAW DWG 112N7003, HFEC INSPECTED IAW NDTM SDR FDEA201204231526Skin · damagedFOUND SCRIBE LINE AT S14R LAP JOINT FROM BS 439.094 - 445.813. REPAIR ACCOMPLISHEDIAW EA F-5330-157266. MAJOR REPAIR.SDR FDEA201204121380Skin · damagedFOUND VERTICAL CUT ON SKIN PANEL AT BS 661 S26R, LEADING INTO BUTT JOINT, REMAINING ON LOWER SKIN SURFACE. ACCOMPLISHED EA F-5330-157270. "MAJOR REPAIR".SDR FDEA201204071286Skin · dentedFUSELAGE SKIN DENTED FWD OF AFT PRESSURE BULKHEAD BS 1720, S24-25R.SDR FDEA201204031238Control Valve · inoperativeRT PACK TRIPPED OFF ON DECENT LEAVING FL 350 (LT PACK IS STILL MEL'D) FOLLOWED QRH, EMERG DECENT TO 10,000", RT PACK CYCLED ON AND OFF REST OF FLIGHT. REMOVED AND REPLACED RIGHT PACK FLOW CONTROL AND SHUTOFF VALVE IAW MM 21-51-01-2 AND REMOVED AND REPLACED SDR FDEA201204031241Stringer · gougedRIGHT UPPER LOBE OF R4 DOOR, STA 1681.8. GOUGED ALONG STRINGER 13R. COMPLIED WITH EA F-5310-157257. MAJOR REPAIR.SDR FDEA201203231085Skin · misrepairedFUSELAGE SKIN MISREPAIRED AT BS 760-780 BETWEEN S16-17L. REPAIRED ON STAM 47461010001 AND STAM EA 757- 5331-16 -F3678, REV. MAJOR REPAIR.SDR FDEA201203231084Skin · dentedLEFT LOWER EXTERNAL FUSELAGE AT BS 760 S18L DENTED. REPAIRED STAM 47461000001 AND STAM EA 757-5331-16-F3678. MAJOR REPAIR.SDR FDEA201203130925Panel · damagedNR 1 PYLON DOOR CUTOUT FOR DOOR PANEL 433LR HAS MISSING MATERIAL IN UPPER AFT CORNER. REPAIRED IAW EA F-5450-157272.SDR FDEA201203130920Skin · dentedSKIN AT BS 1871 AT S-21-L DENTED A=2.65 Y=.010 A/Y=265, DENT OUT OF LIMITS DUE TO AXIS ON STRINGER,IAW-SRM-53-00-01 FIG 101, DET III. ACCOMPLISHED EA F-5330-157262. CAT A, MAJOR REPAIR.SDR FDEA201203130919Panel · corrodedNR 2 PYLON CUTOUT FOR PANEL 443LL HAS CORROSION IN UPPER AFT CORNER. COMPLIED WITH EA F-5450-159901, CAT."A" MAJOR REPAIR.SDR FDEA201203130918Skin · misrepairedNR 2 PYLON OTBD SKIN HAS AN EXISTING REPAIR THAT EXCEEDS LIMITS OF SB 757-54-0022. R & R NR 2 PYLON OTBD SKIN IAW EA F-5450-159905. MAJOR REPAIR.SDR FDEA201203090850Skin · dentedSKIN AT BS 1862 S21L, DENTED. ACCOMPLISHED EA F-5330-157239. MAJOR REPAIR.SDR FDEA201203090856Floorbeam · corrodedBS 310, FLOORBEAM CAP CORRODED LBL 62-RBL 62. REMOVED CORROSION IAW-SRM-51-10-02, CHECKED LIMITS IAW-SRM-53-00-01 PG 101-103. DETAIL II AND III, ORIGINAL MAT THICKNESS .100, D=.027 L=1.1 W=1.3, FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM UPPER TEE CAP, INSSDR FDEA201203050784Skin · corrodedCORROSION ON LOWER OUTSIDE SKIN BS 660 S26 - 30L. REMOVED CORROSION IAW SRM 51-10-02 ORIGINAL MATERIAL .063, REMAINING .052. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETIAL II. REPAIRED IAW SRM 51-40-02. MAJOR REPAIRSDR FDEA201203050785Spar · corrodedLEFT WING REAR SPAR HAS CORROSION. BLEND LIMIT TOLERENCES HAVE BEEN EXCEEDED IAW EA F-2822-7-5009, PT3, STEP B1 ACCOMPLISHED EA F-5710-156998 STEPS 1 THRU 5.SDR FDEA201202290707Skin · damagedFOUND MULTIPLE TOOLING MARKS, FAIRING CONTACT AREA OF LAP SEAM AT S-20L BS 1326-1332. ACCOMPLISHED EA F-5330-157215. MAJOR REPAIR.SDR FDEA201202230674Skin · delaminatedLT INBD AFT T/E FLAP LOWER SKIN HAS PREVIOUS REPAIR THAT IS CRACKING. REPAIRED LT INBD AFT T/E FLAP LOWER SKIN IAW SRM 51-70-06. REF EA F-5750-157259 ISSUED FOR TRACKING-WINGS -FLIGHT SURFACES -EO F-5100-7-5001 LT INBD AFT FLAP-RSC REPAIR TRACKING. MAJOR RESDR FDEA201202220645Skin · misrepairedFUSELAGE SKIN BS 700 BETWEEN S24-26R MISREPAIRED. REPAIRED IAW EA F-5330-157216SDR FDEA201202220643Support Beam · corrodedNLG STRUCTURE UPPER SUPPORT BEAM STA 345 HAS CORROSION FWD AND AFT SIDES. REMOVED NLG UPPER SUPPORT BEAM IAW SRM 51-40-02 AT STA 345. COMPLIED WITH EA F-5310-157258. INSTALLED NLG UPPER SUPPORT BEAM IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201202180613Skin · dentedEXTERNAL FUSELAGE SKIN BS 470 BETWEEN S21-22R DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101 DETAIL III. REPAIRED DENT IAW SRM 53-00-01, FIG 201 REPAIR 3 REF SRM 53-00-01, FIG 201. REPAIR 17 NOTE "D" CATEGORY "B" MAJOR REPAIR.SDR FDEA201202150584Skin · misrepairedFUSELAGE SKIN BS 1720 TO 1726, S16 TO 17L MISREPAIRED. REPAIRED IAW EA F-5330-157000.SDR FDEA201202150583Beam · corrodedSTA 377 BL-0 NOSE WHEEL WELL UPPER TORQUE BOX BEAM CORRODED. REMOVED CORROSION AT STA 377 BL-0. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-04, FIG 101 DETAIL IV, COMPLIED WITH EA F5310-157249. FUSELAGE MAIN FRAME - SECT 41 STA 377.5 NOSE WHEEL WELL TOP PANEL SDR FDEA201202140577Skin · misrepairedCARGO DOOR INNER SKIN MISREPAIRED. REPAIRED IAW SRM 51-70-13 FIG 1, & EA F5230-157271. MAJOR REPAIR.SDR FDEA201202130569Door Frame · corrodedL2 DOOR CUT OUT LOWER FWD FRAME INNER CHORD CORRODED. REMOVED CORROSION IAW SRM 51-10-02 BLENDED AREA MEASURES L= 3.0 W= 1.5 D= .018 ORIGINAL MATERIAL .080, .062 REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL II PG 103. REMOVED AND RSDR FDEA201202110547Frame · damagedRIGHT UPPER LOBE FUSELAGE BS 1140 HAS FOUR ELONGATED HOLES AT BS 1140, STR 16R, STRINGER REPAIR WAS ACCOMPLISHED, ON STAM NR 47327410001 AND STAM EA 757-5341-16-F3583, REV -, DATED FEB 11, 2012. "MAJOR REPAIR."SDR FDEA201202090537Skin · corrodedFOUND CORROSION ON LAP SEAM AT S20L, BS 1334.5. REPAIRED IAW EA F-5330-157215. MAJOR REPAIR.SDR FDEA201202080520Skin · damagedFOUND SCRIBE LINE AT S-26L FROM BS 659.812 TO BB 661 IN LAP JOINT. COMPLIED WITH EA F-5330-156930, REV A, "FUSELAGE PLATES AND SKINS- AD 2007-19-07/ EO F-5330-7-5000 SCRIBE LINE FINDINGS BETWEEN STA 659 TO STA 663 AT THE S-26L LAP SPLICE. "MAJOR REPAIR"SDR FDEA201202080519Skin · damagedFOUND SCRIBE LINE AT S26L FROM BS 661.156 TO BS 662.312 IN LAP JOINT. COMPLIED WITH EA F-5330-156930, REV A, FUSELAGE-PLATES AND SKINS-AD 2007-19-07/ EO F-5330-7-5000 SCRIBE LINE FINDINGS BETWEEN STA 659 TO STA 663 AT THE S-26L LAP SPLICE. "MAJOR REPAIR"SDR FDEA201202030465Beam · corrodedNOSE LANDING GEAR STRUCTURE UPPER SUPPORT BEAM STA 360 HAS CORROSION FWD AND AFT SIDES. COMPLIED WITH EA F-5310-157209. MAJOR REPAIR.SDR FDEA201202030464Skin · buckledEXTERNAL SKIN STA 1720 - 1740 BETWEEN S-27L TO S-29L BUCKLING. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET III. ACCOMPLISHED EA F-5330-159906. MAJOR REPAIR.SDR FDEA201202030442Crease Beam · corrodedCABIN CREASE BEAM WEB AT BS 1360 TO 1380 CORRODED. R & R IAW SRM 51-40-02 REV 105. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201202020441Door · misrepairedCARGO DOOR MISREPAIRED. REPAIRED IAW SRM 52-30-01, REPAIR 4, PG 201, FIG 201. CATEGORY "B" MAJOR REPAIR.SDR FDEA201202020439Skin · misrepairedCARGO DOOR MISREPAIRED. REPAIR ACCOMPLISHED EA F-5230-157264. MAJOR REPAIR.SDR FDEA201202010424Skin · misrepairedFUSELAGE SKIN BS 1681 TO 1661, S-5 TO S-6R MISREPAIRED. REPAIRED IAW EA F-5330-157251. MAJOR REPAIR.SDR FDEA201202010420Stringer · gougedFWD PIT STA 620-640 S-25R, UPPER AND LOWER SIDES OF STRINGER GOUGED. BLENDED STRINGER IAW-SRM-51-10-02, ORIG MAT .080 REMAINING .062, OUT OF LIMITS IAW-SRM-53-00-03, FIG 101, DET II. R & R STRINGER CAT "A", MAJOR. REPAIR.SDR FDEA201201310405Web · damagedAFT FLOOR WEB HAS A ROW OF DOUBLE DRILLED HOLES AT BL 0, STA 1681-1701. REPAIRED FLOOR WEB IAW SRM 53-60-51 PAGE 201 FIG. 201. MAJOR REPAIR.SDR FDEA201201270354Stringer Clip · damagedSTRINGER CLIP AT STA 1640,STR 26R HAS A OVERSIZED FASTENER HOLE. REPAIRED IAW EA NR 757-5361-16-F3621 REV AND STAM NR 47327520001 REF 8110-3.SDR FDEA201201260345Skin · damagedFOUND SCRIBE LINE IN BUTT JOINT AT STA 781 BETWEEN S-6R TO S-10R ACCOMPLISHED EA F-5330-157233, FUSELAGE-PLATES AND SKINS (AD 2007-19-07) EO F-5330-7-5000 PT 3 BUTT JOINT SCRIBE LINE AT STA 781 BETWEEN S-6R TO S-10R. MAJOR REPAIR.SDR FDEA201201230309Floorbeam · corrodedFLOORBEAM AT STA 345, RBL 12 TO LBL 30, REPAIR STRAP IS CORRODED. REMOVED CORRODED STRAP IAW SRM 51-40-02. FABRIRICATED NEW STRAP OUT OF 7075-T6 MAT, IAW SRM 53-00-51.TREATED PRIMED AND PAINTED PER AMM 20-50-14, 20-44-04. INSTALLED FABRICATED STRAP PER SRMSDR FDEA201201220304Stringer · damagedSTRINGER 6R HAS DOUBLE DRILLED HOLE AT STA 418. REMOVED STRINGER IAW SRM 51-40-02 INSTALLED NEW STRINGER IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201201220303Floorbeam · damagedSTA 1681, FLOORBEAM HAS 2 EA DOUBLE DRILLED HOLES NEAR BL-0. FOUND WHILE ACCOMMPLISHING DECK PLATE REPAIR. R & R FLOORBEAM IAW SRM 51-40-02. MAJOR REPAIR.
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