Boeing 757-2G5
Service difficulty reports · 557
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 = '7572G5' 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 = '7572G5' 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 FDEA201308101827Unknown · smokeAFTER TAKEOFF, NOTICED HAZE IN COCKPIT WHICH DEVELOPED INTO LIGHT SMOKE EMINATING FROM BEHIND THE INSTRUMENT PANEL. DECLARED AN EMERGENCY & STARTED DESCENT. PERFORMED SMOKE, FIRE, FUMES CHECKLIST. AFTER STEP 10, NOTICED LIGHT SMOKE ABATED AND LEFT RESIDUALSDR FDEA201303270674Handle · detachedCAPTAIN`S WINDOW CRANK HANDLE DETACHED. REPLACED WINDOW CRANK HARDWARE. OPS CHECKED GOOD IAW AMM 56-11-04-4.SDR FDEA201301190150Stringer Clip · crackedCRACK NOTED ON BS 487, S1R FORWARD HOLE FOR STRINGER CLIP. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-00-03 REPAIR 2 FIG 201 AND SRM 53-00-00.SDR FDEA201212294398Connector · damagedWHILE INSTALLING PANEL ON LT SIDE OF PEDESTAL REF WRI 27-60/0753. FOUND CAPT'S STICK SHAKER WIRES ARCING. CONNECTOR MSN 1299126. REMOVED SPORTS TAPE AND FOUND WIRES WERE BROKEN INSIDE CLAMP FOR BACKSHELL. PINS DO NOT COME OUT OF THIS CONNECTOR AND WIRES HASDR FDEA201212214349Slide · dislodgedL1 DOOR ESCAPE SLIDE FELL OFF OF DOOR. REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE IAW AMM 25-66-01-4. OPS CHECKED NORMAL. ACFT OK TO CONTINUE.SDR FDEA201211023816Lamp · inoperativeRT ENTRY DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED LAMP IAW MM 33-51-06-2-1. OPS CHECKED NORMAL.SDR FDEA201211013806Lamp · inoperativeRIGHT ENTRY DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. LAMPED IAW MM 33-51-06-2-1. OPS CHECKED NORMAL.SDR FDEA201211013805Lamp · inoperativeRIGHT ENTRY DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. LAMPED PER MM 33-51-06-2-1 OPS CHECKED NORMALSDR FDEA201210293773Carriage · gougedNR 3 FLAP TRACK CARRIAGE OTBD LOWER FITTING GOUGED. COMPLIED WITH EA F-2750-154109 WINGS-LT INBD FLAP CARRIAGE ASSY-GOUGE ON ROLLER SUPPORT ASSY.SDR FDEA201209233412Sensor · dirtyTAXIING INTO POSITION FOR TAKE OFF, RECEIVED LEFT FWD ENTRY DOOR EICAS MESSAGE CAME ON INTERMITTENTLY DURING TAXI BACK TO GATE. INSPECTED ENTRY DOOR, FOUND GREASE, DIRT AND DEBRIS ON PROXMITY SWITCH, CLEANED AREA , OPERATED DOOR IAW AMM 52-11-01-6 SYS CHECKESDR FDEA201208183067Spring · brokenL1 DOOR LATCH ASSY SPRING IS BROKEN. R & R L1 DOOR LATCH SPRING IAW AMM 5-11-13-2 AND OPS CHECKED PER AMM 52-11-00-5. OPS CHECKED GOOD.SDR FDEA201208163017Liner · out of positionWHEN ARMING L1 DOOR, EXCESSIVE FORCE HAD TO BE APPLIED TO GET SLIDE ARM INDICATOR TO DISPLAY. FOUND ESCAPE SLIDE ARMING TAB RUBBING ON LOWER LINING OF L1 DOOR. REF MM 52-11-02-4, ADJUSTED LOWER LINING. ALL DOOR COMPONENTS RE-INSTALLED. SLIDE ARMING TAB OPSSDR FDEA201207262684Wire · burnedBURNING RUBBER ODOR HAPPENED AFTER LANDING. ODOR WAS STILL THERE AFTER SHUTDOWN. DURING WALKAROUND NOTICED RT TAXI LIGHT ON, WENT UP TO THE COCKPIT AND NOTICED THAT THE SWITCH WAS IN THE OFF POSITION. CYCLED SWITCH SEVERAL TIMES AND THE LIGHT REMAINED ON.SDR FDEA201207092522Frame · dentedFRAME IS DENTED AND HOLE IS OVERSIZED AT STA 418 S-3L. REPAIR ACCOMPLISHEDSDR FDEA201207092521Frame · damagedFRAME HAS OVERSIZED HOLES AT BS 395 BETWEEN S-2R TO S-3R. REPAIR ACCOMPLISHED.SDR FDEA201207032477Unknown · odorAFTER PUSH BACK-ENGINE START; PACKS ON A STRONG FUEL ODOR THROUGHOUT COCKPIT.SDR FDEA201206272366Skin · damagedFOUND SCRIBE LINE AT S19R LAP JOINT FROM BS 762.687 TO BS 766.937 STR 19R REPAIR ACCOMPLISHED, IAW EA F-5330-160569. MAJOR REPAIR.SDR FDEA201206272365Skin · damagedFOUND SCRIBE LINE AT S19L LAP JOINT FROM BS 763 TO 768, S19L LAP JOINT, REPAIRED IAW SRM.SDR FDEA201206222301Skin · corrodedSKIN BS 1180 S17L, HAS TWO HOLES ELONGATED AND CORRODED, SKIN REPAIRED IAW EA 757-5361-16-F3800, REV A, MAJOR REPAIR.SDR FDEA201206152247Skin · damagedRT AILERON CONDUCTIVE FRAME AND UPPER SKIN DAMAGED AND HAS INCORRECTLY INSTALLED FASTENERS. REPAIRED RT AILERON CONDUCTIVE FRAME, UPPER SKIN, AND FASTENERS IAW SRM 51-70-03 AND SB 757-51-0006. MAJOR REPAIR.SDR FDEA201206072127Skin · misrepairedFUSELAGE SKIN AT BS 1470-1480 STR 22 - 23R MISREPAIRED. REPAIR ACCOMPLISHED IAW EA 757-5361-16-F3812, REV -.SDR FDEA201205251969Skin · puncturedDURING SURVEILLANCE INSPECTION, FOUND OUTWARD PUNCTURE (2 LOCATIONS 2.75 APART) ON FUSELAGE SKIN AT BS 1493 AND 1494, BETWEEN S24R AND S25R. REMOVED DAMAGE PER SRM 53-00-01, REPAIR 16, STEPS 1-3 AND SRM 51-40-02. INSTALLED REPAIR DOUBLER AND COMPLETED REPASDR FDEA201205181852Bottle · low pressureL1 DOOR ASSIST BOTTLE PRESSURE NOT IN SERVICEABLE BAND. R & R L 1 PASSENGER DOOR EMERGENCY POWER RESERVOIR REF AMM 52-11-30-4. OK FOR SERVICE.SDR FDEA201205171829Crease Beam · corrodedRT INBD CREASE BEAM CORRODED BS 1340-1380. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DETAIL VIII. R & R CREASEBEAM, BS 1290-1405, RT, IAW SRM 51-40-02, AND DWG 146N8326. MAJOR REPAIR.SDR FDEA201205161822Skin · gougedNR 2 PYLON SAIL FAIRING LOWER SKIN AFT SURF HAS CHAFE MARKS AND 2EA GOUGES. DAMAGE FOUND OUT OF LIMITS IAW SRM 54-50-70 FIG 105, FIG 101, DETAIL IV. REPAIRED IAW EA F-5450-159925.SDR FDEA201205161819Crease Beam · corrodedMAIN CABIN AREA LT SIDE BETWEEN BS 760 - 740. LBL 65 CREASE BEAM INBD CHORD CORRODED. REMOVED CREASE BEAM FOUND OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL VIII. REPLACED CREASE BEAM BS 670 - 750 IAW SRM 51-40-02 AND DWG 143N8328. MAJOR REPAIR.SDR FDEA201205151813Skin · corrodedLEFT PYLON RT SIDE BETWEEN PP STA 176 TO PP STA 144 INTERNAL SKIN WITH CORROSION.SDR FDEA201205091777Crease Beam · corrodedR2 DOOR SILL FLOOR CREASE BEAM HAS CORROSION FS 710. CLEANED UP AND CHECKED LIMITS, CREASE BEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13 FIG 101 SHEET 5, REMOVED CREASE BEAM IAW SRM 51-40-02. LOCATED AND DRILLED NEW CREASE BEAM IAW SRM 51-40-05, INSTALLED NESDR FDEA201205071760Skin · misrepairedFWD CARGO DOOR INNER SKIN NEAR BOTTOM MISREPAIRED. REPAIRED IAW SRM 52-30-01, FIG 1, DETAIL 1 AND 51-70-13 AND 51-40-02. MAJOR REPAIR .SDR FDEA201205031724Stringer · crackedUPON REMOVAL OF STRUCTURE FOUND STRINGER 26R AT BS 1675 CRACKED. CRACKED. REMOVED DAMAGE PER SRM 51-10-02. OUT OF LIMITS PER SRM 53-00-03, PAGE 102, FIG. 101, DETAIL 1. REMOVED STRINGER PER SRM 51-40-02. FABRICATED NEW STRINGER SECTION AND SPLICE PER SRM 53-SDR FDEA201205031725Skin · misrepairedSKIN AT BS 1670, STR 22R-23R MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 102, REPAIR NR 16.SDR FDEA201205031723Floorbeam · bentMAIN DECK BS 879 FLOORBEAM BENT. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, PAGE 101. R & R FLOORBEAM IAW ENGINEERING DWG 143N5072, AND SRM 51-40-02. MAJOR REPAIR.SDR FDEA201205021711Seat Track · corrodedSEAT TRACK BS 1540 TO 1600 CORRODED, RBL 45.50. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. R & R SEAT TRACK IAW SRM 51-40-02 AND DWG 146N5125. MAJOR REPAIR.SDR FDEA201205021710Seat Track · crackedSEAT TRACK, APPROX STA 879, INBD UPPER FLANGE CRACKED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, PG 101 AND 105. DETAIL X, R & R SEAT TRACK IAW ENG DWG 143N5106 AND SRM 51-40-02.SDR FDEA201204271654Slide · unwanted deployLEFT DOOR SLIDE DEPLOYED ON DOOR OPENING . INSPECTING AND DISCONNECTING THE LT DOOR EMERGENCY EVACUATION SLIDE IAW MM 25-66-00-0. REMOVED SLIDE AND STOW BEHIND THE RCB. FOUND GIRT BAR SPRINGS WEAK, R & R GIRT BAR ASSY. COMPLETED AND VERIFIED INSTALLATION
SDR FDEA201204261626Door Frame · gougedL2 DOOR JAMB FWD FRAME IS GOUGED CHAFED 2 PLACES FS 680 PLUS 5 ABOVE FLOOR LINE. REMOVED AND REPLACED DOOR FRAME IAW DRAWING 143N8313 P1, REV. L, AND SRM 51-40-02. MAJOR REPAIR.SDR FDEA201204241557Crease Beam · corrodedAPPROX STA 755 RT INBD CREASE BEAM CHORD CORRODED. REMOVED CORROSION IAW SRM 51-10-02, CHECK LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM53-30-13, FIG 101, DET VII. REMOVED CREASE BEAM IAW SRM 51-40-02, FABRICATED CREASE BEAM FROM BAC1515-553 IAW SRM 53-30-1SDR FDEA201204231527Frame · corrodedFRAME FLANGE CORRODED AT BS 1605, RBL 24. REMOVED DAMAGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, PG 103, FIG 101 DETAIL V. LOCATED, DRILLED AND INSTALLED NEW SUPPORT IAW SRM 51-40-05.SDR CA120423014Monitor · inoperative(CAN) ABOUT AN HOUR FROM DESTINATION THE PILOTS SMELLED AN ELECTRICAL ODOR IN THE COCKPIT FOR A SHORT DURATION. THERE WERE NO ABNORMAL INDICATIONS AND THE ODOR DISSIPATED QUICKLY. THE CAPTAIN ASKED THE F/A IF THEY SMELLED ANYTHING AND THEY REPORTED THAT THEYSDR FDEA201204211516Crease Beam · corrodedS17R BS 450-630 INNER CHORD CORRODED. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL .090", REMOVED MATERIAL .011", MATERIAL REMAINING .079". FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL VIII, PAGE 105. REMOVED CREASE BEAM IAW SRM 51-SDR FDEA201204201510Frame · chafedFOUND FRAME CHAFED BS 1600 BETWEEN S3 AND 4L. REPAIRED FRAME IAW SRM 53-00-07, FIG 201, REPAIR 3SDR FDEA201204171461Stringer · crackedCRACKED STRINGER 14L AT UPPER FLANGE ON FRAME BS 1440. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, PG 102, DETAIL 1. REMOVED DAMAGED STRINGER SECTION AND INSTALLED REPAIR FROM STA 1420-1460 IAW SRM 53-00-03, FIG 201 AND DWG 140N1530.SDR FDEA201204171462Floorbeam · corrodedFLOORBEAM BS 740 LBL 14 UPPER TEE CORRODED. FLOORBEAM FOUND OUT OF LIMITS IAW SRM 53-00-1, FIG 101, DETAIL II AND III. ORIGINAL MATERIAL .125 AFTER REWORK .070. R & R FLOORBEAM IAW SRM 51-40-02 AND DWG 143N5016, SH 5. MAJOR REPAIR.SDR FDEA201204091328Seat Track · gougedRBL 25 SEAT TRACK GOUGED ON TOP AND INSIDE SURFACE, BS 1180 - 1280. REMOVED DAMAGE IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-52, PAGE 102, FIG 101, DETAIL 1 FABRICATED NEW SEAT TRACK IAW SRM 53-60-52, 51-10-02, 53-00-52 AND BAC 1520-792A. INSTALLESDR FDEA201204061280Crease Beam · corrodedMAIN DECK LEFT CREASE BEAM BS 900 TO 1040 HAS SURFACE CORROSION. CLEANED IAW SRM 51-10-02 & CHECKED LIMITS IAW SRM 53-40-13, FIG 101, ORIGINAL MATERIAL THICKNESS .063", AFTER REWORK .018", REMAINING MATERIAL THICKNESS .045", FOUND TO BE OUT OF LIMISDR FDEA201204051274Seat Track · damagedSEAT TRACK HAS 2 BROKEN LOBES AT BS 1220 RBL 45. FOUND OUT OF LIMITS IAW SRM 53-00-52 REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK IAW SRM 53-60-52 PAGE 2 FIG 1 DETAIL 1 AND DRAWING 146N5133. INSTALLED SEAT TRACK IAW SRM 51-40-02 AND DRAWISDR FDEA201204021251Seat Track · corrodedMAIN CABIN SEAT TRACK RBL 25 BETWEEN BS 1320 -1340 CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL VII, PG 104. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK IAW SRM 51-10-02 AND 53-60-52, FSDR FDEA201204021254Seat Track · corrodedLBL 45 SEAT TRACK CORRODED BS 1620-1640. REMOVED CORROSION FROM SEAT TRACK STA 1620-1640. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL VII. R & R SEAT TRACK IAW SRM 53-00-52. MAJOR REPAIR.SDR FDEA201204021232Skin · delaminatedFUSELAGE SKIN DELAMINATED. REPAIRED WITH A BONDED FILLER AND DOUBLER IAW SRM 51-70-10. MAJOR REPAIRSDR FDEA201204021231Skin · puncturedVERTICAL STAB SKIN AT BS1898 PUNCTURED. REMOVED DAMAGE, CLEANED, PREPPED AND BONDED REPAIR AREA, FINISHED SANDED, PER SRM 51-71-00. TREATED AND PRIMED PER SRM 51-20-01. SEALED PER SRM 51-71-00. BONDED DOUBLER REPAIR IS AT BL0, BS 1898, ON SKIN. MAJOR R
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