Boeing 757-27B
Service difficulty reports · 242
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 = '75727B' 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 = '75727B' 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 FDEA201409032433Skin · damagedAPU DOOR SKIN DAMAGED ADJACENT TO DOOR 1 LATCH, NUMBERED 1 - 5 FWD TO AFT. REPAIR CUT OUT IAW EA F-5240-T0310700 REV PT 1.SDR FDEA201409032432Shear Plate · damagedIMPACT DAMAGE ON SHEAR PLATE AT MCD THRESHOLD BS 560. SHEAR PLATE REPLACED.SDR FDEA201409032430Skin · dentedNUMBER 1 SLAT HAS QTY 4 DENTS IN THE TE WEDGE TOP SKIN. REPAIRED IAW SRM 51-70-10 & 57-43-02.SDR FDEA201409032418Skin · dentedNUMBER 5 SLAT HAS QTY 7 DENTS IN THE TE WEDGE TOP SKIN REPAIRED IAW SRM 57-43-02 & 51-70-10.SDR FDEA201409022409Skin · gougedUPPER FUSELAGE BS 1320 - 1350 STRINGER 4R. SCRIBE GOUGE MARKS EVIDENT ON FUSELAGE SKIN BELOW LAP JOINT REPAIRED IAW SRM 53-00-01, SB757-53A0092 & EA F-5300-T0310858.SDR FDEA201409022408Skin · gougedUPPER FUSELAGE BS 1390 - 1410 STRINGER 4R. SCRIBE & GOUGE MARKS EVIDENT ON FUSELAGE SKIN BELOW LAP JOINT. REPAIRED IAW SRM 53-00-01 & SB 757-53A0092.SDR FDEA201409022407Skin · damagedMULTIPLE LIGHTNING STRIKES ON LOWER SKIN PANEL FROM FWD PRESS BULKHEAD BS 200 TO FWD AVIONICS BAY DOOR. REPAIR CARRIED OUT IAW EA F-5300-T0310667.SDR FDEA201409022406Skin · damagedSEVERAL LIGHTNING STRIKES FOUND ON FWD AVIONICS BAY DOOR SKIN 113AL. REPAIRED IAW EA F5240-T0310668.SDR FDEA201409022404Bracket · corrodedLEFT THS TIP BONDING POINT BRACKET FOR LT ELEVATOR FOUND IN POOR CONDITION. REPAIR CARRIED OUT TO LT THA TIP UPPER BEAM IAW EA F-5500-T0310741.SDR FDEA201409012397Angle · damagedDURING AGEING INSPECTION, REPAIR INSPECTED IAW EO-5100-7-5001 PT 1. REPAIR AT CREASE BEAM STATION 1190 STRINGER 17L FOUND NOT TO CONFORM TO SRM 51-70-12 FIG 1. OUTER ANGLE FOUND NOT BE INCORRECT GAUGE & MID ANGLE FOUND TO HAVE MECHANICAL DAMAGE MID & OUTER ASDR FDEA201408302373Angle · corrodedNUMBER 5 SLAT CORROSION ON INBD CLOSURE ANGLE REPAIRED IAW EA F-5750-T0310708.SDR FDEA201408302372Angle · corrodedNUMBER 6 SLAT INBD CLOSURE ANGLE CORRODED. REPAIRED IAW EA F-5750-T0310704.SDR FDEA201408292357Skin · puncturedLEFT INBD MAIN FLAP TE HONEYCOMB TOP SKIN PUNCTURE REPAIR IAW SRM 57-53-01 & SRM 51-70-07.SDR FDEA201408292354Bulkhead · damagedDVI OF THE ENG 2 PYLON MOUNT BULKHEAD FITTING REVEALS NICK DAMAGE EVIDENT TO THE LOWER FLANGE OTBD SIDE AFT EDGE. REPAIRED IAW SRM 51-10-02 & EA F-5440-T0310190.SDR FDEA201408272335Nut Plate · corrodedRIGHT WING OTBD FLAP STRESS PANEL NUTPLATE CORROSION IN SEVERAL PLACES. CORROSION REPAIRED IAW EA F-5750-T0310492.SDR FDEA201408272327Spar · corrodedRIGHT OTBD MAIN FLAP CORROSION ON FWD SPAR INTERNAL LOWER FLANGE. REPAIR IAW EA F-5750-T0310699.SDR FDEA201408272325Angle · corrodedLEFT OTBD FLAP CORROSION ON INTERNAL FRONT SPAR LOWER ANGLE CORROSION REMOVED IAW EA F-5750-T0310561.SDR FDEA201408272324Structure · corrodedSLAT NR 5 ON AFT FACE SPAN WISE CHORD CORRODED. SPAN WISE CHORD PN 114N3011-1 REPLACED.SDR FDEA201408262314Slat · corrodedSLAT NR 7 CORROSION ON AFT LOWER CHORD. REPAIRED IAW CMM 57-43-28.SDR FDEA201408262313Skin · corrodedSLAT NR 1 CORROSION ON NOSE SKIN LOWER SURFACE SLAT. REPAIRED IAW EA F-5750-TO310402.SDR FDEA201408122147Skin · misrepairedDURING AGEING INSPECTION EF-5100-7-5001PT1 FOUND DENT STILL APPARENT BELOW DOUBLER REPAIR IAW EA F-5330-117347. EXISTING DOUBLER REPAIR REMOVED & SKIN DENT DRESSED OUT IAW 5300. NEW DOUBLER FABRICATED & INSTALLED REPAIR AREA NOW CONFORMS TO EA F-5330-11734SDR FDEA201408022038Seat Track · crackedMCD SEAT TRACK AT BS 580 LBL 45.50 UPPER FLANGE IS CRACKED & FASTENER PULLED.SDR FDEA201408022037Splice · crackedMCD MODIFICATION FLOORBEAM COUPLER SPLICE FITTING AT BS 580 LBL 45.50 UPPER FLANGE CRACKED.SDR FDEA201407312019Skin · delaminatedNDT REPORT DELAMINATION OF LT ELEVATOR LOWER SKIN LE APPROX 1.5 IN X 0.5 IN. INVESTIGATION CARRIED OUT ON SUITABLE REPAIRS IAW SRM 55-20-01 REPAIR 1 FIG 201 TABLE 2 350 CURE REPAIR NOT AVAILABLE AT THIS LOCATION , ELEVATOR REPLACED.SDR FDEA201405100974Girt Bar · out of positionAFTER CLOSING LT ENTRY DOOR, THE ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT DID NOT ILLUMINATE. FOUND GIRT BAR OUT OF PLACE IN LT ENTRY DOOR. GIRT BAR INSTALLED, CHECKED FOR OPERATION & FOUND OK IAW AMM 25-60.SDR FDEA201311142839Socket · defectiveESCAPE SLIDE ARMED LIGHT OVER L1 IS BURNED OUT. RELEASED FOR SERVICE IAW MEL 25-66-05-A ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS INOPERATIVE. ENGAGEMENT OF SLIDE L1 HAS BEEN VISUALLY VERIFIED. AC OK FOR SERVICE BSL R BULBS CHECKED OK. FOUND BULB SUPPORT SSDR FDEA201310252614Nut · missingRIGHT AILERON OTBD PCA INPUT ROD NUT MISSING. INSTALLED NUT IAW AMM 27-11-20.SDR USAA2013112500017Floorbeam · corrodedC4 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM UPPER T CAP AT BS 345, RBL 61. REPAIRED FLOOR BEAM UPPER T CAP AT BS 345, RBL 61 IAW B757 SRM 53-00-51-2R, PROCEDURE 8, REPAIR 8.SDR FDEA201308021752Skin · dentedDENT ON LOWER FUSELAGE BS 1681-1696 BETWEEN S27-29L. FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101. TRIMMED OUT DAMAGE AREA IAW SRM 51-10-02 & EA F-5330-T0301824, REV PS PT 1, REPAIRED IAW EA F-5330-T0301824, REV PS PT 1.SDR FDEA201209143322Bulb · burned outDURING SVC, FOUND LT SLIDE EMERGENCY LIGHT INOPERATIVE. BULB REPLACED IAW AMM 33-51-06-2-1 REV 103.2. OP TESTED GOOD IAW AMM 33-51-00-0, REV 103.2.SDR FDEA201207162591Duct · leakingIN CLIMB, PASSING FL 300 AT CLIMB POWER EICAS MSG "LT ENGINE OVERHEAT" COMPLIED WITH QRH. ENGINE WAS AT IDLE WITH LIGHT REMAINING ON. IN PROCESS OF ABOUT TO SHUTDOWN ENGINE LIGHT EXTINGUISHED. LT ENGINE REMAINED AT IDLE UNTIL TAXI-IN AND SHUTDOWN. LEFT ENSDR FDEA201206232329Bulb · burned outRT DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. BULB REPLACED IAW AMM 33-51-06-2-1. LIGHT TESTED SATISFACTORY.SDR FDEA201109213996Warning Light · illuminatedAFTER PUSH BACK COMPLETE LT FWD ENTRY DOOR EICAS ILLUMINATED. RELEASED FOR SERVICE IAW MEL: 52-71-01SDR FDEA201109023633Slide · dislodgedUPON ARRIVAL TO ACFT, FOUND THE L1 DOOR BLOWN. THE L1 EMERGENCY SLIDE HANGING OUT. R & R L1 DOOR ESCAPE SLIDE. REF AMM 25-66-01-4. ACFT OK FOR SERVICE.SDR FDEA201108073129Skin · corrodedUPON REMOVAL OF APU INLET STRAP, FOUND SKIN CORRODED STA 1780, STR 5-6 RIGHT. REMOVED SKIN SECTION IAW SRM 51-40-2. LOCATED, DRILLED, AND DEBURRED NEW SKIN IAW SRM 51-40-5. INSTALLED NEW SKIN IAW SRM 51-40-2, REV 103.SDR FDEA201102030465Warning Message · illuminatedDURING FLIGHT, RECEIVED A "L ENG BLEED OFF" EICAS. SUSPECT PRSOV AND SENSOR.SDR FDEA201011194435Slide · unwanted deployUPON ARRIVAL OF ACFT, CREW INADVERTINLY DEPLOYED L1 DOOR ASSIST BOTTLE AND L1 DOOR EVACTUATION SLIDE BY MISTAKE. REPLACED L1 DOOR ESCAPE SLIDE IN REF AMM 25-66-01-4. ALSO INSTALLED NEW GIRT BAR PROXIMITY SWITCH MAGNET IAW AMM 25-66-11-2. OPS CHECK OK ATSDR FDEA200905271803Clamp · looseON CLIMBOUT PASSING 30000 FT, RECEIVED LT ENG OVERHEAT, PULLED THRUST LEVER BACK AND WARNING EXTINGUISHED. INSPECTED ENG FOR EVIDENCE OF DUCT LEAKS. FOUND FOIL WRAP MISSING FROM IP DUCT IN STRUT. DUCT CLAMP WAS NOT TIGHT. TIGHTENED CLAMP NEEDS ENG RUN. SDR FDEA200809213956Duct · leakingDURING CLIMB PASSING FL180, EICAS MESSAGE DISPLAYS L ENG OVHT ALL OTHER ENG INDICATIONS WERE NORMAL. RETARDED L THROTTLE AND TURNED OFF L BLEED AIR. AFTER APPROXIMATELY 2 MIN THE EICAS MESSAGE WENT AWAY. DECLARED EMERGENCY AND LANDED WITH L ENG AT IDLE. COSDR 08FDEA03956Engine · false indicationDURING CLIMB PASSING FL180 EICAS MESSAGE DISPLAYS L ENG OVHT ALL OTHER ENG INDICATIONS WERE NORMAL. RETARDED L THROTTLE AND TURNED OFF L BLEED AIR. AFTER APPROXIMATELY 2 MIN THE EICAS MESSAGE WENT AWAY. DECLARED EMERGENCY AND LANDED WITH L ENG AT IDLE. COMPSDR 08FDEA03374Floorbeam · corrodedCORROSION FOUND ON FLOORBEAM AT STA 365, RBL 3 TO RBL 51. EVALUATE AND RECTIFY. REPAIR CARRIED OUT ON FLOORBEAM UPPER CHORD AT STATION 365 BETWEEN RBL 3 AND RBL 51 IN ACCORDANCE WITH B 757-200 SRM 53-00-51 FIGURE 201 REPAIR 1, REVISION 93. REPAIR IS CLASSIFSDR 08FDEA03215Spar · corrodedUNDOCUMENTED BLEND REPAIR FOUND ON THE AFT SIDE OF THE LT WING REAR SPAR WEB AT RSS 183. EVALUATE AND RECTIFY. LEFT WING REAR SPAR WEB CORROSION BLEND REPAIR CARRIED OUT IAW EA F-5710-118827 DATED MAY 24 2008. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-02-100.SDR 08FDEA02810Skin · corrodedSURFACE CORROSION FOUND ON PYLON NUMBER TWO LEFT SIDE INNER SKIN FORWARD OF ACCESS PANEL 443LL, PPS 126 TO PPS 181. EVALUATE AND RECTIFY. REPLACED LEFT SIDE INNER SKIN FORWARD OF ACCESS PANEL 443LL OF PYLON NUMBER TWO IN ACCORDANCE WITH BOEING DRAWING 311SDR 08FDEA02809Skin · corrodedSURFACE CORROSION FOUND ON PYLON NUMBER ONE LEFT SIDE INNER SKIN AFT OF ACCESS PANEL 433CL. EVALUATE AND RECTIFY. REPLACED LEFT SIDE INNER SKIN AFT OF ACCESS PANEL 433CL OF PYLON NUMBER ONE IN ACCORDANCE WITH BOEING DRAWING 311N5046, BOEING DRAWING 311N5002,SDR 08FDEA02354Panel · corrodedPYLON NUMBER TWO RIGHT SIDE STRUT SKIN CUTOUT AT ACCESS PANEL 443AR FOUND CORROSION, FROM PPS100 TO PPS126. EVALUATE AND RECTIFY. REPLACED PYLON NUMBER TWO STRUT SKIN CUTOUT PANEL 443AR IN ACCORDANCE WITH BOEING DRAWING 311N5002 ID0014, SRM 51-10-02 REV SDR 08FDEA02353Panel · corrodedPYLON NUMBER ONE RIGHT SIDE SKIN CUTOUT AT ACCESS PANEL 433GR FOUND CORROSION, FROM PPS 100 TO PPS 120. EVALUATE AND RECTIFY. REPLACED PYLON NUMBER ONE SKIN CUTOUT PANEL 433GR IN ACCORDANCE WITH BOEING DRAWING 311N5002 AND SRM 51-10-02 REV 93.SDR 08FDEA01978Skin Panel · corrodedCORROSION ON PYLON NUMBER ONE LT INNER STRUT SKIN NEAR ACCESS PANEL 433BL CUTOUT, PPS 124.76. EVALUATE AND RECTIFY. REPLACED PYLON NUMBER ONE LT INNER STRUT SKIN NEAR ACCESS PANEL 433BL CUTOUT IN ACCORDANCE WITH BOEING DRAWING 311N5002 ID 0013 REVISION E, 31SDR 08FDEA01977Skin Panel · corrodedSURFACE CORROSION ON PYLON NUMBER TWO LEFT SIDE PANEL INNER SKIN FORWARD OF ACCESS PANEL 443HL, PPS 124 TO PPS 200. EVALUATE AND RECTIFY. PYLON NUMBER TWO LEFT SIDE SKIN PANEL LOCATED FORWARD OF ACCESS PANEL 443HL REPLACED IN ACCORDANCE WITH BOEING DRAWSDR 08FDEA01976Skin · corrodedCORROSION FOUND ON PYLON NUMBER ONE INNER STRUT SKIN NEAR ACCESS PANEL 433JR CUTOUT, PPS 162.8. EVALUATE AND RECTIFY. PYLON NUMBER ONE RIGHT SIDE PANEL SKIN NEAR ACCESS PANEL 433JR CUTOUT REPLACED IN ACCORDANCE WITH BOEING DRAWING 311N5002 ID 0014 REVISION ESDR 08FDEA01821Skin · corrodedPYLON NUMBER TWO INNER SKIN OF ACCESS PANEL 443BR FOUND WITH SURFACE CORROSION, FROM PPS 126 TO PPS 151. EVALUATE AND RECTIFY. PYLON NUMBER TWO INNER SKIN OF ACCESS PANEL 443BR, REPAIRED BY AERO MECHANICAL INDUSTRIES INC. (AMII) IN ACCORDANCE WITH EA NR F
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