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 CALA2016120501036Switch · faultyNR 4 RT MED ARM/DISARM WARNING LIGHT INOP. REPLACED SLIDE ARM SW S10225 REF MM 25-66-11, CKS GOOD.SDR FDEA201612024305Skin · dentedSIX INCH HORIZONTAL DENT ON THE RIGHT SIDE FOR THE VERTICAL STAB VSS 125. REPAIRED THE VERTICAL STAB IAW SRM 51-70-10-2R. PRIMED AND TOP COATED IAW SRM 51-70-10-2R AND AMM 51-21-10-7.SDR FDEA201611294288Skin · debondedLEFT HORIZONTAL STAB HSS 81.0 FOUND DEBONDED. REPAIRED IAW SRM 51-70-17-0G PRIMED AND TOP COATED IAW SRM 51-70-17-0G AND AMM 51-21-10-7.SDR FDEA201611294287Frame · chafedPUNCTURE ON FRAME BS 231 FORWARD ACCESSORY ACCESS DOOR CUTOUT. REMOVED DAMAGE AND INSTALLED REPAIR IAW EA F-5310-T0330045 P1.SDR FDEA201611244235Bottle · low pressureDURING A PREFLIGHT INSPECTION, FOUND LEFT ENTRY DOOR SLIDE PRESSURE NOT IN GREEN RANGE. IAW AMM 25-66-01-6.SDR CALA2016111800928Floor Support · crackedAFT CARGO BAY BS 1200 - 1220, BL 0 FLOOR SUPPORT CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-00-02 PARA 4 .SDR CALA2016111800927Intercostal · crackedMAIN CABIN AT BS 1200 - 1220 HAS A CRACKED INTERCOSTAL. REPLACED MAIN CABIN INTERCOSTAL IAW SRM 51-04-02 PARA 4.SDR CALA2016111100873Exhaust Valve · failedCABIN ALT WARNING AT FL 410 PRESSURIZATION KEPT CLIMBING UPON ARRIVAL FOUND AT THE RIGHT FWD A/C BAY A DUCT DETACHED FROM THE CABIN AIR SUPPLY CHECK VALVE. VALVE INSPECTED AND FOUND GOOD. REINSTALLED DUCT TO CHECK VALVE AND SECURED IAW AMM 21-51- 15. ADDITIONSDR CALA2016111100872Clamp · brokenAUTO 1 AND AUTO 2 COULD NOT MAINTAIN NORMAL CABIN ALT. OUTFLOW VALVE FULL CLOSE REPLACED AIR SPLY CK VLV PRECAUTIONARY; BROKEN CLAMP AROUND THE AIR SPLY CK VLV REF AMM 21-51-15.SDR FDEA201611083906Skin · puncturedTWO PUNCTURES NOTED ON LT ELEVATOR INBD UPPER SURFACE. REPAIRED IAW SRM 51-10-17, EA F-5520-T0329529. MAJOR REPAIR.SDR FDEA201610283741Transmitter · inoperativeAFTER TAKEOFF, WHEN FLAP HANDLE WAS MOVED FROM 5 TO 1 DEGREES, AN IMMEDIATE EICAS MESSAGE FOR TE FLAP ASYMETERY APPEARED AND THE FLAP GUAGE STOPPED SLIGHTLY LESS THAN 5 DEGREES WITH ASSOCIATED FLAP STOPPAGE. REMOVED AND REPLACED THE FLAP POSITION TRANSMITTSDR FDEA201610283729Girt Bar · stuckAFTER DISARMING R1 DOOR, GIRT BAR DID NOT RELEASE.SDR FDEA201610273713Seat Track · corrodedMAIN CABIN SEAT TRACK BS 345 TO 377.70 LBL 6 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. EVALUATED DAMAGE LOSS .055 FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DET I. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED SEAT TRACK IAW SRM 53-00-52-1A. SDR FDEA201610273712Seat Track · corrodedMAIN CABIN STA 345 TO 377.70 RBL 12 HAS CORROSION ON SEAT TRACK. REMOVED CORROSION IAW SRM 51-10-02. EVALUATED DAMAGE LOSS .060 FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DET I. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED SEAT TRACK IAW SRM 53-00-52-SDR FDEA201610193659Frame · gougedBS 231 FRAME BUTLINE 0 IS GOUGED. REPAIRED IAW EA F-5310-T0329105 P1.SDR FDEA201610193660Panel · delaminatedVERTICAL STAB RT SIDE PANEL HAS AREA OF DELAMINATION AT APPROX. BS 1786, FSS 170, 10 INCH AREA, EVALUATED DELAMINATION AND FOUND TO BE OUT OF LIMITS IAW SRM 55-30-01-1A FIG. 101 NOTE K. REMOVED AND REPLACED THE PANEL IAW-SRM-51-40- 02-0G AND DWG 175N2001 SHSDR FDEA201610193658Bulkhead Web · gougedAPU COMPARTMENT FWD BULKHEAD GOUGE, OUTBD OF SERVICE INTERPHONE JACK INSTALLED DOUBLER IAW-SRM-51-40-02-0G AND 53-80-08-2R, ORIG. MAT. .016, REMAINING .007, OUT OF LIMITS IAW-53-80-08-1A FIG. 101 DET.IX, THIS IS A CAT."A" REPAIR, AT 1885.2 BULKHEAD, APU COSDR FDEA201610193655Switch · failedON TAKEOFF ROLL, WITH POWER STABILIZED, AT ABOUT 50 KNOTS THE SPOILERS EICAS ALERT AND AUREL WARNING APPEARED. REJECTED TAKEOFF AND ALERT DISAPPEARED AT ABOUT 40 KNOTS. R & R SPEED BRAKE HANDLE POSITION SWITCH IAW MM 31-51-03-4, AND W/D32-42-12. OPS CHECSDR FDEA201610193654Control Module · malfunctionedDURING TAKEOFF ROLL AT ABOUT 50 KNOTS, RECEIVED A SPOILERS EICAS MESSAGE AND WARNING TONE. TAKEOFF WAS REJECTED AND SPOILERS EICAS WENT AWAY AS AIRCRAFT REACHED TAXI SPEED ON ABORT. REMOVED AND REPLACED THE SPOILER CONTROL MODULE IAW AMM 27-09-00-2, OPS CHSDR FDEA201610183648Reservoir · lowDURING POST FLIGHT WALK AROUND, FOUND RIGHT PASSENGER DOOR EMERGENCY POWER RESERVOIR AT ZERO PSI. REPLACED R2 DOOR EMERGENCY POWER ESERVIOR IAW AMM 52-11-30-4. CHECKED GOOD, ACFT OK FOR SERVICE.SDR TIPR2016101226089Skin · dentedFUSELAGE SKIN DENTED APPROXIMATELY 15 INCHES ACROSS TWO EXISTING FASTENER ROWS.SDR TIPR2016101226500Skin · gougedR2 DOOR, UPPER HINGE CUTOUT GOUGED. REPAIRED IAW SRM 52-10-02 REPAIR 1SDR FDEA201610093518Skin · dentedEXTERIOR FUSELAGE SKIN 1 EACH DENT ON FRAME AT STA 460 ABOVE STR 20L AND 1 EACH DENT STA 466 ABOVE STR 20L. BOTH DENTS ARE INSIDE THE RVSM AREA. ALL WORK ACCOMPLISHED IAW EA F-5330-T0328802 P1 FUSELAGE PLATES & SKINS. FUSELAGE SKIN REPAIR AT STA 460 BETWEENSDR CALA2016101000737Lamp · failedELECTRIC BURNING ODOR NEAR OVERWING EXIT. DISSIPATED RAPIDLY. FOUND EMERGENCY EXIT LEFT SIDE SIDE WALL LIGHTS BLACK AT THE END. REPLACED LT EMERGENCY EXIT SIDE WALL LIGHTS IAS AMM 33-21-30SDR FDEA201610073486Frame · gougedAFT CARGO COMPARTMENT STA 1320, STR 27R-28R FRAME FREE FLANGE HAS GOUGE. REMOVED GOUGE IAW-SRM-51-10-02-0G, ORIG MAT .063 MAT REMAINING .049 D=.014, FOUND TO BE OUT OF LIMITS IAW-SRM-53-00-07-1A FIG 101 DET II. REMOVED AND REPLACED FRAME, AFT PIT STA 1320, SDR FDEA201610073500Frame · corrodedBULK CARGO BAY BS 1681, FRAME CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02-0G, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG. 101, DETAIL II. REMOVED AND REPLACED THE FRAME IAW DWG 146N1024 AND SRM 51-40-02-0G. REPAIR MAJOR.SDR FDEA201610073498Stringer · corrodedAFT CARGO BS 1661-1681, STRINGER 28L CORRODED. REMOVED CORROSION IAW-SRM-51-10-02-0G, AFTER BLEND OUT, FOUND TO BE OUT OF LIMITS IAW SRM, NO ALLOWABLE LIMITS NOTED, REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02-0G AND DWG 146N3600. MAJOR REPAIR.SDR FDEA201610073495Doubler · corrodedFWD CARGO BAY BS 700-720, BETWEEN STRINGERS 20-22L, LAV SERVICING DRAIN ASSEMBLY STRUCTURE HAVE AREAS OF CORROSION. REMOVED THE CORROSION, IAW-SRM-51-10-02, DOUBLER EXFOLIATED, NO LIMITS FOUND IN SRM, OUT OF LIMITS, REMOVED DOUBLER IAW-SRM-51-40-02, NEW DOSDR FDEA201610053462Skin · gougedLEFT WING INBD MAIN FLAP TOP SURFACE OTBD PANEL GOUGED. REMOVED AND REPLACED THE FLAP. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.SDR FDEA201609283380Skin · dentedLEFT WING INBD MAIN FLAP LOWER SURFACE HAS ONE DENT. REMOVED AND REPLACED THE FLAP. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.SDR CALA2016092600686Floorbeam · corrodedCORROSION ON TOP OF MAIN CABIN FLOORBEAM AT BS 1682 RBL 48 BETWEEN PRESSURE DECK AND FLOORBEAM. REMOVED CORROSION ON TEE IAW SRM 51-10-02 PARA 15 FIG 1. TEE CAP FOUND TO BE 100% MATERIAL LOSS AND OUT OF LIMITS IAW SRM 53-00-51. REMOVED AND REPLACED UP PER SDR FDEA201609223335Skin · chafedFUSELAGE EXTERNAL SKIN BS 1600 TO 1620, STRINGER 14R. BETWEEN UPPER SKIN PANEL AND LOWER SKIN PANEL. SUSPECT SHIM PRESENT AND MIGRATED. REPAIRED IAW EA F-5330-T0328680. MAJOR REPAIR.SDR FDEA201609223333Skin · scratchedFUSELAGE EXTERNAL SKIN BS 1620 - 1640 , STRINGER 14R. THERE ARE FIVE SCRATCHES FOUND BELOW THE SKIN LAP SPLICE. REPAIRED IAW EA F-5330-T0328680.SDR FDEA201609223332Skin · gougedFUSELAGE EXTERNAL SKIN BS 1600 - 1620, STRINGER 14R, THERE IS A SCRATCH FOUND BELOW THE SKIN LAP SPLICE. REPAIRED IAW EA F-5330-T0328680. REPAIR CLASSIFIED AS MAJOR.SDR CALA2016092200674Slide · damagedWHEN PERFORMING 1R ROLLER AND LATCH BEARING LUBE, FOUND 1R DOOR SLIDE COVER LATCH ASSY BROKEN AND HONEYCOMB DELAMINATED. INSTALLED SERVICEABLE 1R DOOR SLIDE BUSTLE IAW AM M 52-11-02.SDR FDEA201609203316Frame · puncturedFRAME AT BS 231, BL 0 IS PUNCTURED. REPAIRED IAW EA F-5310-T0328373 P1.SDR FDEA201609203315Skin · dentedFUSELAGE SKIN DENTED AT BS 660 - 680 STRINGERS 26 - 27L. FOUND OUT OF LIMIT AS PER SRM 53-00-01-1A REV 118.0 AND REPAIRED IAW SRM 53-00-01-2R FIG 201 REPAIR 15 REV 119.0. REPAIR CLASSIFIED AS MAJORSDR FDEA201609193312Stiffener · crackedLEFT WHEEL WELL AFT PRESSURE BULKHEAD INBD SIDE STIFFENER CRACKED. FABRICATED STIFFENER AND INSTALLED IAW SRM 51-40-02, DWG NR 144N2503 REV H, DWG PL 144N2503 REV BM.SDR FDEA201609183309Seat Track · chafedSEAT TRACK CROWN AT BS 1150 - 1170, LBL 24.75 FOUND CHAFED. CHAFES REMOVED IAW SRM 51-10-02-0G REV 118. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A REV 119. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02-0G REV 119, DWG 144N5021 SHT 1 & 3 REV A. RESDR FDEA201609183308Shim · migratedLT PYLON STRUT WING INBD SIDE LOAD FITTING AT WS313.50 FOUND WITH SHIMS MIGRATION. COMPLIED WITH EA F-5740-T0328306 P1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.SDR FDEA201609163284Skin · damagedSCRIBE LINE FOUND AT LAP SEAM S-14R, BS 1538.875-BS 1541.125. COMPLIED WITH EA TF-5330-T0328119 PT 1, FUSELAGE, PLATES AND SKIN SCRIBE LINE LRTS INSPECTIONS, S-14R-STA 1530 TO STA 1550. MAJOR REPAIR.SDR FDEA201609153266Skin · dentedLEFT INBD MAIN FLAP LOWER SURFACE APPX 10 INCHES FROM INBD EDGE AND 3 INCHES ABOVE T/E WEDGE DENTED. REPAIRED LT INBD MAIN FLAP LOWER SURFACE BY HOT-BONDING NEW CORE & DOUBLER IAW SRM 57-53-01, FIG 1 & SRM 51-70-10-2R. REPAIR NR 3 AND SRM 51-70-10-2R REPAIRSDR FDEA201609153264Handle · looseCAPTAIN`S SLIDING WINDOW WILL NOT LOCK IN CLOSED POSITION. FOUND CAPTAIN'S SLIDING WINDOW HANDLE LOOSE CAUSING LOCK FEATURE TO BE INOPERABLE. RESECURED HANDLE INTO POSITION. WINDOW OPERATES NORMAL IAW MM 56-11-02-5-0.SDR FDEA201609143232Strap · corrodedAPU AIR INLET DOOR CUT OUT, MIDDLE STRAP FOUND CORROSION AT BS 1825 STRINGERS 3 - 6R. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-80-15-1A FIG 101 TABLE 101 REV 119.0 AND REPAIR CARRIED OUT IAW SRM 53-80-15-2R FIG 202 REPAIR 1 DETAIL 1 REV 119.0. SDR FDEA201609143231Strap · corrodedAPU AIR INLET DOOR CUT OUT SUPPORT STRAP FOUND CORROSION BETWEEN BS 1790 - 1825, STRINGER 6R. APU AIR INLET DOOR CUT-OUT SUPPORT STRAP (ANGLE) CORROSION THRU FOUND OUT OF LIMIT AS PER SRM 51-10-02-0G REV 118.0 CORRODED SUPPORT STARP (ANGLE) REMOVED AND RESDR FDEA201609143230Angle · corrodedAPU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORRODED BETWEEN BS 1790 - 1825, STRINGER 3R. SUPPORT ANGLE FOUND OUT OF LIMIT AS PER SRM 51-10-02-0G REV 119.0 CORRODED SUPPORT ANGLE REMOVED AND REPLACED WITH NEW SUPPORT ANGLE IAW DWG NO 148N3105 SHT 1 REVSDR FDEA201609143229Strap · corrodedAPU AIR INLET DOOR CUT OUT- FWD STRAP CORRODED AT BS 1787, STRINGERS 3 - 6R. APU AIR INLET DOOR CUT OUT FWD STRAP CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-80-08-1A FIG 101 DETAIL 1X REV 118.0 CORRODED FWD STRAP REMOVED AND REPLACED WITH NEW FWD SDR FDEA201609143218Seat Track · chafedSEAT TRACK INBD FLANGE AT BS 1200 - 1320, LBL 24.75 CHAFED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02-0G REV 119.0, DWG 146N5133 SHT 2 REV, DWG 146N5120 SHT 28 REV A. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201609143216Warning Light · illuminatedLEFT OIL FILTER EICAS MESSAGE ILLUMINATED. COMPLIED WITH THE CHECK LIST, INFLIGHT ENGINE SHUTDOWN. DRAINED AND FLUSHED LT ENGINE MAIN OIL TANK, 3RD TIME & REPLACED MAIN ENGINE OIL FILTER IAW 79-21-05-4, 3RD TIME. R & R LT ENGINE LUBRICATION AND SCAVENGE OILSDR FDEA201609133215Door Frame · damagedAT THE FWD EQUIPMENT BAY DOOR 113AL CUT-OUT, FRAME BS 231.25 UPPER RADIUS DENTED & GOUGED, BL0. COMPLIED WITH EA, F-5310-T0328207, P1 FUSELAGE. MAINFRAME FORWARD ELECTRONIC EQUIPMENT COMPARTMENT, BS 231.25, BL0 FRAME DENT REPAIR. THIS IS A MAJOR REPAIR.
Back to Boeing 757-222