Boeing 757-222
Service difficulty reports · 15,539
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 = '757222' 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 = '757222' 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 FDEA201609133208Shear Web · corrodedRIGHT CREASE BEAM WEB AT BS 967 - 975 RBL 69.5 FOUND CORROSION AROUND 3 RIVETS. REMOVED AND REPLACED IAW SRM 51-40-02-0G, REV 119.0 AND DWG 144N5140, SHEET 6. REV REPAIR CLASSIFIED AS MAJOR.SDR FDEA201609133207Crease Beam · corrodedRIGHT CREASE BEAM WEB AT BS 1439.5 RBL 67 FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-40-02-0G, REV 119.0, AND DWG 146N5590, SHT 8, REV B. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201609133206Crease Beam · corrodedRIGHT CREASE BEAM WEB AT BS 1382 - 1389 RBL 69 CORROSION. CORROSION REMOVED PER SRM 51-10-02-0G REV 118.0. REWORKED AREA EVALUATED AND FOUND CORRODED THROUGH. CREASE BEAM WEB REMOVED AT STA 1380 - 1400 PER SRM 51-40-02-0G REV 119.0. CREASE BEAM WEB FABRICSDR FDEA201609133205Crease Beam · corrodedLEFT CREASE BEAM AT BS 680 - 730 FOUND CORRODED. REPAIRED IAW SRM 51-40-02-0G REV 119.0, DWG 143N8322 SHT 1 REV K, AND 143N8322 SHT 2 REV E. REPAIR CLASSIFED AS MAJOR.SDR FDEA201609133204Crease Beam · corrodedRIGHT CREASE BEAM AT BS 680 - 730 FOUND CORRODED. REPAIRED IAW SRM 51-40-02-0G REV 119.0, DWG 143N8322 SHT 1 REV K, AND 143N8322 SHT 2 REV E. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201609113190Seat Track · chafedSEAT TRACK OTBD FLANGE AT BS 780 - 880 LBL 45.5, FOUND OVAL SHAPE CHAFED. THE SEAT TRACK WAS REMOVED IAW SRM 51-40-02-0G REV 119.0. A NEW SEAT TRACK WAS FABRICATED IAW DWG 143N5016 SHT 1 REV A AND INSTALLED IAW DWG 143N5080 SHT 5 REV A. REPAIR CLASSIFIED ASDR FDEA201609113189Seat Track · chafedCABIN SEAT TRACK INBOARD FLANGE AT STA 1420-1440 LBL 24.75 FOUND CHAFED AROUND 2 EA FASTENER HOLE. CHAFED MARK REMOVED AS PER SRM 51-10-02-0G REV 119.0. REWORKED AREA ORIGINAL 0.070" REMAINING 0.050" AND REMOVED 0.020" FOUND EXCEED 10% LIMIT PER SRM 53-00-52SDR FDEA201609113188Seat Track · chafedSEAT TRACK INBOARD FLANGE AT BS 1500-1540 LBL 24.75, FOUND CHAFED. REPAIRED IAW SRM 53-00- 52-2R REPAIR 1 OPTION 1 REV 119.0. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201609093161Access Panel · damagedRIGHT WING, TANK DRY BAY ACCESS DOOR ASSY PANEL BROKEN, OTBD WS 258.5, PN 112N8003-2 COMPLIED WITH EA F-5720-T0326684, DATED SEPT 02,2016. FUEL SYSTEMS, CELLS, TANKS, VENTS, RT WING TANK ACCESS DOOR ASSY CAT-B, MAJOR REPAIR.SDR FDEA201609093160Spar · corrodedRIGHT WING REAR SPAR AT IRSS 183, CORROSION ON AFT SPAR, FOUND ON REMOVAL OF BONDING JUMPER REPLACEMENT, THE LOWER BONDING POINT. ACCOMPLISHED ON EA F-5710-T0326498, DATED AUG 02,2016. WINGS BASIC WING STRUCTURE, RT REAR SPAR WEB CORROSION AT IRSS 183, REF: FSDR FDEA201609093157Crease Beam · corrodedCABIN, LT CREASE BEAM INBD CHORD AT BS 690-740 NR 2L DOOR SILL AREA FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-40-02-0G REV 119.0, DWG 143N8322 SHT 1 REV K, AND 143N8322 SHT 2 REV E. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201609083144Skin · damagedEXTERIOR SKIN NUMEROUS SMALL NICKS AND SCRATCHES ALONG THE BELLY OF THE AIRCRAFT BETWEEN STRINGER 26 LEFT AND 26 RIGHT AT BODY STATION 680 - 700. STA 680-700 STR 26L-26R EXTERIOR SKIN NUMEROUS SMALL NICKS AND SCRATCHES REMOVED FOUND WITHIN LIMIT AS PER SSDR FDEA201609083143Skin · damagedEXTERIOR SKIN NUMEROUS SMALL NICKS AND SCRATCHES ALONG THE BELLY OF THE AIRCRAFT BETWEEN STRINGER 26 LEFT AND 26 RIGHT AT BODY STATION 700 - 720. STA 700-720 STR 26L-26R EXTERIOR SKIN NUMEROUS SMALL NICK AND SCRATCHES REMOVED FOUND WITHIN LIMIT AS PER SRM SDR FDEA201609083142Skin · damagedEXTERIOR SKIN NUMEROUS SMALL NICKS AND SCRATCHES ALONG THE BELLY OF THE AIRCRAFT BETWEEN STRINGER 26 LEFT AND 26 RIGHT AT BODY STATION 720 - 740. STA 720-740 STR 26L - 26R EXTERIOR SKIN NUMEROUS SMALL NICKS AND SCRATCHES REMOVED FOUND WITHIN LIMIT AS PERSDR CALA2016090900639Floor Support · crackedINTERCOSTAL CRACKED AT BS 1200 BL 0 AT FWD ATTACH UPPER. REMOVED AND REPLACED IAW SRM 51-40-02 PAR 4 FIG 3.SDR FDEA201609063122Panel · delaminatedDELAMINATION ON VERTICAL STABILIZER, LEFT SIDE ADJACENT TO L/E PANEL 321CL. DELAMINATION ON VERTICAL STABILIZER PANEL, LT SIDE FOUND TO BE OUT OF LIMITS IAW SRM 55-30-01-1A, FIG 101, NOTE K AND SRM 51-70-10-2R. R & R PANEL 175N2001-3 WITH O/H PANEL 175N2001-SDR FDEA201609063120Skin · chafedLEFT WING INBD MAIN FLAP, INBD NOSE SKIN, FOUND WITH DEEP SPANWISE CHAFING MARK. COMPLIED WITH PART 1 OF EA F--5750-T0326940 TITLE: WINGS - FLIGHT SURFACES - LT WING INBOARD MAIN FLAP ASSY, CHAFE DAMAGE FOUND ON LEADING EDGE SKIN BETWEEN STA 74.00 AND STA 105SDR FDEA201609033109Collar · crackedL1 GUST LOCK FAILS TO LOCK THE DOOR IN OPEN POSITION. REPLACED THE DAMAGED HOLD/OPEN LOCK TRIGGER CATCH AND THE UPPER COLLAR.SDR FDEA201608303067Floorbeam · corrodedBS 720, LBL 60 - 62 FLOORBEAM UPPER FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02-0G, REV 118.0 AND FOUND EXCEEDED LIMIT IAW SRM 53-00-51-1A, REV 118.0. COMPLIED WITH EA F-5310-T0327426. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201608283056Angle · corrodedEMPENNAGE AFTER REMOVAL OF APU INLET DOOR FOUND STRAP BETWEEN STA 1787 - 1825 AT S3R WITH CORROSION. STRAP ANGLE R & R WITH NEW ANGLE, PN: 654N0244-620 IAW DWG NR 148N3105, SHT 1, REV C. REPAIR CLASSIFIED AS MAJOR.SDR CALA2016082600591Display · failedF/O ADI DISPLAY WENT BLANK ON TAXI OUT. TCAS FAIL ALSO ON F/O SI DE ONLY. RESET FO EADI TEST NORMAL IAW MM34-22-03-864-032. RESET TCAS SYSTEM OPS TESTED NORMAL IAW MM34-45-00-501. RVSM REPORTINGSDR FDEA201608252974Floorbeam · damagedCABIN-STA 324, RBL 15-RBL 30 FOUND 02 EA ELONGATED FASTENER HOLES ON FLOORBEAM WEB. FLOORBEAM WEB REPAIRS COMPLIED WITH. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201608252973Floorbeam · damagedCABIN - STA 324, RBL 5-15 FOUND 03 EA ELONGATED FASTERNER HOLES ON FLOORBEAM WEB. FLOORBEAM WEB REPAIR, BETWEEN RBL 4 AND RBL 20 AND BETWEEN RBL 21 AND 29 COMPLIED WITH REPAIR. CLASSIFIED AS MAJOR.SDR FDEA201608252972Floorbeam · damagedCABIN, STA 324, RBL 30-70 FOUND SEVERAL ELONGATED FASTENER HOLES ON FLOORBEAM WEB. FLOORBEAM WEB REMOVED IAW SRM 51-40-02-0G, REV 118.0. NEW FLOORBEAM WEB FABRICATED AND INSTALLED IAW DWG 141N2930, SHT 2, REV F AND EA F-5310-T0327532 A PART 1, P1. REPAIR CLSDR FDEA201608232958Floorbeam · corrodedBS 1681 FLOORBEAM UPPER TEE IS CORRODED ON UNDERSIDE, LBL 60 - RBL-60. REMOVED CORROSION IAW SRM-51-10-02-0G, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG. 101, DETAIL VI. REMOVED AND REPLACED THE FLOORBEAM TEE IAW SRM 51-40-02-0G, DWG# 146N5111, AND SDR FDEA201608232957Shear Tie · corrodedAFT CARGO BS 1620, ONE SHEAR TIE CORRODED, STRINGER 29R. REMOVED THE CORROSION IAW SRM 51-10-02-0G, FOUND NO ALLOWABLE DAMAGE IN SRM. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02-0G, MAJOR REPAIR.SDR FDEA201608232956Connector · damagedDURING SERVICE CHECK, DISCOVERED EMERGENCY LIGHT TEST SWITCH ON P62 NLG PANEL INOPERATIVE. DURING TROUBLESHOOTING, FOUND LIGHT OXIDATION ON PIN SMALL C OF CONNECTOR D40488, CLEANED THE CONNECTOR. ALSO REPLACED TERMINAL ON WIRE W3054-0013-18 AT SWITCH S100SDR FDEA201608222954Battery · failedEMERGENCY POWER SUPPLY, M371 BATTERY INOPERATIVE, MEL 22AUG16 13:36, RELEASED FOR SERVICE IAW MEL: 33-51-01-01, CATEGORY: D-EXPIRATION: 19 DEC16, MEL 33-51-01-01, INTERIOR EMERGENCY LIGHTS, INOPERATIVE. MEL 33-51-02-02, ALSO APPLIES, MEL 33-51-02-02 ALSO APPLSDR FDEA201608192942Stringer · corrodedMCD BS 438, STG CORRODED AT 5L. REPAIRED STR 5L, STA 410-440, IAW-SRM-53-00-53-2R, SHEET 6, DETAIL I, FOUND TO BE OUT OF LIMITS IAW SRM-53-00-03-1A, FIG
101, SHEET 1, CAT-A, MAJOR REPAIR.SDR FDEA201608192941Aileron · damagedLT AILERON UPPER COAT INBD SIDE CHIPPED COMPOSITE. LT AILERON REPAIRED AS REQUIRED IAW-SRM-51-70-04 PARA. 5G, FIG 9, AILERON REBALANCE ACCOMPLISHED ON NR N00658, FOR WEIGHT ADDED AT REPAIR, DAMAGE LOCATION, WING STA 670.266-673.266, PN:113N7100-64, SN:32942SDR FDEA201608172900Skin · damagedFUSELAGE EXTERIOR SKIN THERE ARE NUMEROUS LIGHTNING STRIKES AT BS 680 - 740 STRINGERS 27 - 28L. COMPLIED WITH EA F-5330-T0327528, PART 1. REPAIR RIVETS AND LIGHTNING DAMAGES ON FUSELAGE SKIN PANEL BETWEEN STA 680-STA 716 AND S-27L-S-28L. REPAIR CLASSIFIED ASDR FDEA201608152891Shear Tie · corrodedAFT FUSELAGE SKIN HAS A BULGED AREA BS 1540 STRINGER 28R. FOUND SHEAR TIE CORRODED. REMOVED IAW SRM 51-40-02-OG, FABRICATED IAW B DWG 140N2002, REV B , HEAT TREATED IAW FORM FAS 0119, REV O AND INSTALLED SHEAR TIE IAW DWG 140N2002, REV B AND SRM 51-40-02-OGSDR FDEA201608152890Spar · gougedHORIZONTAL STAB RIGHT SIDE AUX SPAR BETWEEN RIB 2 & 3 AUX SPAR FOUND ONE DENT WITH A GOUGE. COMPLIED WITH EA F-5510-T0327452. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201608152888Spar · gougedHORIZONTAL STABILIZER RT SIDE AUXILIARY SPAR BETWEEN RIB 2 & 3. EXISTING REPAIR DOUBLER FOUND WITH 1 EA GOUGE. RT HORIZONTAL
STABILIZER AUXILIARY SPAR BETWEEN RIB 2 & 3 EXISTING REPAIR DOUBLER WITH 01 EA GOUGE, COMPLIED WITH EA F-5510-T0327452, PART 1, TITLESDR FDEA201608132886Slat System · malfunctionedAFTER TAKEOFF, RECEIVED A LE SLAT ASYM EICAS MESSAGE AND LEADING EDGE ANUNCIATOR, WHEN FLAPS WERE SELECTED FROM FLAPS 1 TO THE UP POSITION. COMPLIED WITH QRH PROCEDURE, RETUNED TO DEPARTURE. RECONNECTED RT LEADING EDGE SLAT DRIVE COUPLING TO ANGLE GEARBOXSDR FDEA201608122883Skin · corrodedFUSELAGE SKIN, STA 1681.8-1701 B/T S26R-S29R HAS CORROSION AROUND CUTOUT OF LAV SERVICE PAN. ACCOMPLISHED EA F-5330-T0327322, FUSELAGE-PLATES & SKINS. AFT LAVATORY SERVICE DOOR CUTOUT SKIN REPAIR BETWEEN STA 1675-1710 AND STR 25R-S29L, THIS IS A CAT-B, REPAISDR FDEA201608112861Skin · damagedLEFT WING OTBD MAIN FLAPS HAS HAIL DAMAGE, SOME WITH CRACKS AND DISBONDING. REPAIRED LT WING OTBD MAIN FLAP IAW SRM-51-70-17-0G, COMPLIED WITH EA F-5750-T0327099, TITLED: WINGS, FLIGHT SURFACES, LT OTBD MAIN FLAP REPAIRS RSC TRACKING, CAT A, MAJOR REPAIR.SDR FDEA201608092849Skin · corrodedCORROSION AT LAP SEAM STRINGER 19L, BS 740 - 770. REPAIRED IAW EA F-5330-T0327352. MAJOR REPAIR.SDR TIPR2016090826428Stringer · corrodedSTRINGER 29R AT BS 1681 CORRODED. STRINGER REPLACED IAW SRM 53-00-03.SDR FDEA201608052824Pitot Tube · damagedBIRDSTRIKE ON DEPARTURE. LOST ALL AIRSPEED INDICATIONS AND ASSOCIATED ITEMS ON F/O'S SIDE. R & R F/O'S PITOT TUBE REF 34-11-01-4, THROUGH STEP 29, STEP 30, LEAKAGE TEST NEEDS ACCOMPLISHED. PERFORMED PITOT LEAK CHECK OF F/O'S PITOT TUBE IAW AMM 34-11-01-5. SDR FDEA201608042815Gate · corrodedMAIN DECK FWD RT SERVICE DOOR LOWER GATE IS CORRODED ACROSS LOWER SURFACE. REMOVED AND REPLACED THE GATE IAW-SRM-52-11-38-4.SDR FDEA201608042814Gate · corrodedL1 DOOR LOWER GATE CORRODED ON LOWER SIDE. REMOVED AND REPLACED THE GATE IAW AMM-52-11-38-4.SDR FDEA201608042813Stringer · corrodedMAIN CARGO DECK BS 438 STRINGER 6L CORRODED. REMOVED AND REPLACED THE STRINGER FROM BS 380-440 IAW SRM-51-40-02-0G. MAJOR REPAIR.SDR FDEA201608042812Gate · gougedR4 DOOR HAS GOUGES ON MATING AREA AS MARKS. REMOVED AND REPLACED R4 DOOR LWR GATE ASSY IAW AMM-52-11-38-4, ADJUSTED THE DOOR IAW AMM-52-11-00-5.SDR FDEA201608042811Warning System · false activationON FINAL APPROACH, WHEN SELECTING FLAPS FROM 20 TO 25 RECEIVED A T/E FLAP DISAGREE, COMPLETED QRH PROCEDURE. PERFORMED FLAPS 20 LANDING. CONTINUED PROBLEM ON GROUND. TROUBLESHOT IAW FIM 27-51 FAULT TREES 808 AND 803, COMPLYING WITH FSEU BITE PROCEDURES. SDR FDEA201608032789Door Frame · gougedFWD E & E CUT OUT FWD DOOR FRAME GOUGED BY DOOR LOCK PIN. COMPLIED WITH EA F-5310-T0327174. BS 231.25, BL0 FRAME DENT, REPAIR. THIS IS A MAJOR REPAIR. PERFORMED SATISFACTORY. OPS CHECK FORWARD ELECTRONIC EQUIPMENT DOOR SENSOR IAW AMM 52-71-00-5.SDR FDEA201608032781Seat Track · corrodedSEAT TRACK BOTTOM AT BS 699.5 RBL 24.75, FOUND CORRODED. CORROSION EXCEEDS LIMIT IAW SRM 53-00-52-1A, REV 118.0. SEAT TRACK REMOVED AT STA 699- STA 780, RBL 24.75 IAW SRM 51-40-02-0G, REV 118.0, NEW SEAT TRACK FABRICATED IAW DWG 143N5085, SHT 2, REV B AND INSDR FDEA201608022756Ecu · failedAPU SHUTDOWN IN FLIGHT WITH FAULT LIGHT. ATTEMPTED ONE RESTART, THEN RETURNED TO DEPARTURE DUE TO SINGLE GENERATOR OPS. R & R ECU. ACCOMPLISHED 3 NORMAL SUCESSFUL STARTS WITH APU PNEUMATIC AND ELECTRICAL SYSTEMS, OPS CHECKING NORMAL.SDR FDEA201608022754Door Sill · corrodedAFT CARGO COMPARTMENT, STA 1440-1460, 27R CARGO DOOR CUT LOWER SILL WEB CORROSION. SILL WEB R & R WITH NEW FABRICATED LOWER SILL WEB IAW DWG 146N8522, SHT 1, REV E. NEW LOWER SILL WEB FABRICATED IAW DWG 146N8522, SHT 1, REV C. REPAIR CLASSIFIED MAJOR IAW GMSDR FDEA201608022742Skin · corrodedLEFT WING, AFTER REMOVAL, UPPER SKIN UPPER SURFACE OVERWING FILL PORT CUTOUT FOUND CORRODED AT MATING AREA TO ADAPTER. LT WING AFTER REMOVAL UPPER SKIN SURFACE OVERWING FILL PORT CUTOUT COMPLIED WITH EA F-5730-T0327055 P1. LT WING SKIN UPPER SURFACE CORROSIO
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