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 FDEA201603231006Skin Panel · chafedRIGHT WING, INBD TE MAIN FLAP, UPPER OTBD PANEL, UPPER SURFACE FOUND CHAFE MARK AT 8" FROM LE, 33" FROM OTBD EDGE. DAMAGE REMOVED, CLEANED & REPAIRED DOUBLER, INSTALLED PER 250 F HOT BONDING IAW SRM 57-53-01-2R DETAIL I REV 117 & SRM 51-70-10-2R PARA 6, 7, SDR FDEA201603220982Stringer · corrodedAFT CARGO COMPARTMENT, STATION 1615, STRINGER 21L, STRINGER CORROSION. STRINGER REMOVED & REPAIR PARTS INSTALLED IAW EA F-5310-T0324239 P1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201603220981Stringer Splice · corrodedAFT CARGO COMPARTMENT, STATION 1620, STRINGER 18L, STRINGER SPLICE CORROSION OUT OF LIMIT. R & R WITH FABRICATED STRINGER SPLICE IAW EA F-5310-T0324244 P1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201603210964Skin · corrodedCORROSION ON EXTERNAL SKIN & UNDER LAP SEAM, STRINGER 19L, BS 763 - 767. ACCOMPLISHED EA F-5330-TO323948. FUSELAGE, PLATES & SKINS, FUSELAGE SKIN CORROSION REPAIR. MAJOR REPAIR.SDR FDEA201603200958Skin · dentedRIGHT WING INBD FORE FLAPS LOWER SKIN HAS DENT 28" FROM INBD. REPAIRED IAW SRM 51-70-10-2R REPAIR 4.SDR FDEA201603200959Tear Strap · corrodedAFT CARGO BAY TEAR STRAP CORRODED BS 1400, STRINGER 29R. REMOVED CORROSION IAW SRM 51-10-02. R & R TEAR STRAP IAW SRM 51-40-02-06 & DWG 146N3300. MAJOR REPAIR.SDR FDEA201603180954Frame · corrodedFRAME STATION 1400, STRINGER 27R - 25L REQUIRES REMOVAL TO FOM NR N00383. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101 DETAIL 2. R & R FRAME IAW SRM 51-40-02-00 & DWG 146N1028 AT STATION 1400, BETWEEN STRINGER 25SDR FDEA201603180952Skin Panel · delaminatedRIGHT VERTICAL STAB FIXED PANEL EXTERNAL SURFACE BETWEEN AUXILIARY SPAR & FRONT SPAR & APPROX BETWEEN FSS 220.521 & 245.652, HAS DELAMINATION. RT VERTICAL STABILIZER FXED PANEL FOUND DELAMINATED IAW SRM 55-30-01-1A FIG 101, NOT REPAIRABLE. FOUND TO BE OUT OFSDR FDEA201603180951Skin · damagedFUSELAGE SKIN EXTERNAL SURFACE HAS CREASE & DENT AT APPROX BS 605, BL0. REPAIRED FUSELAGE SKIN DENT IAW SRM 53-00-01-2R R 6 FIG 201 CAT B MAJOR REPAIR.SDR FDEA201603180947Skin · damagedINCOMING, AFT CARGO DOOR LOWER AFT CORNER IS DAMAGED. THE SKIN EDGE AT REPORTED LOCATION WAS TRIMMED OUT MORE THAN 0.100". FOUND TO BE OUT OF LIMITS IAW SRM 52-30-01-1A FIG 101 DETAIL 4. THE SKIN WAS REPAIRED IAW SRM 52-30-01-2R REP 4. IAW EA F-5230-TO3233SDR FDEA201603180946Frame · corrodedAFT PIT STATION 1580, FRAME CORRODED AT STRINGER 27L. REMOVED CORROSION IAW SRM 51-40-02-0G FOUND TO BE OUT OF LIMITS IAW SRM 53-60-07-01 FIG 101 DET 2. R&R FRAME IAW SRM 51-40-02-0G & DWG 146N1010 AT STATION 1580, FRAME STRINGER 25L - 25R. REPAIR CLASSIFIESDR FDEA201603170943Skin · dentedTHERE IS A DENT IN THE FUSELAGE SKIN, BETWEEN STATION 520 & 540, BETWEEN STRINGERS 24 & 25 LT SIDE. CHECKED LIMITS OF DENT AT STATION 520 - 540, STRINGER 24L - 25L, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A DET 3. INSTALLED DOUBLER IAW SRM 51-40-02-06 & SDR FDEA201603170938Stringer Splice · corrodedAFT CARGO COMPARTMENT, STATION 1620, STRINGER 20R, STRINGER SPLICE CORROSION.SDR FDEA201603150929Doubler · damagedFORWARD CARGO DOOR REPAIR AFT SIDE HAS GOUGES DINGS IN SKIN, BS 620, STRINGER 23R. R & R DOUBLER IAW SRM 52-30-01-2R. REPAIR NR 4 DUE TO OUT OF LIMITS IAW SRM 52-30-01-1A PG 5 FIG 101 DETAIL 4. REPAIR CLASSIFIED AS CAT B MAJOR.SDR FDEA201603150925Frame · corrodedCABIN STATION 1580, STRINGER 9R - 10R, FRAME OTBD FLANGE FOUND CORROSION. CORROSION EVALUATED & FOUND CORROSION MORE THAN 50% THROUGH. FRAME REPAIR CARRIED OUT IAW SRM 53-00-07-2R REV 117. THIS IS A CAT B REPAIR WITH A THRESHOLD OF 10000 FLIGHT CYCLES AFTERSDR FDEA201603130913Door Sill · corrodedCABIN STATION 740 - 755, L2 DOOR CUT OUT LOWER SILL, INNER CHORD FOUND CORROSION. COMPLIED WITH PART 1 OF EA F-5310-T0324494 REV A. THREE EACH FASTENER HOLES ON MED L2 LOWER MAIN SILL INNER CHORD. REPAIR CLASSIFIED AS MAJOR.
SDR FDEA201603130912Repair · debondedEXISTING REPAIR WING, THERE IS A REPAIR AT LT SIDE OUTER WING, UPPER INTER SPAR SKIN AT WS 790. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A4 PT 1 ATTACHMENT B, NO HISTORY. EXISTING REPAIR WAS EVALUATED IAW ATTACHMENT B OF EO F-5100-7-5001 A5 PT 1 SDR FDEA201603110903Frame · corrodedAFT PIT STATION 1380 FRAME CORRODED FROM RBL 2 29 TO LBL 7.55. REMOVED CORROSION IAW SRM 51-10-02-0G. CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DET 2. R & R FRAME IAW SRM 51-40-02-0G & DWG 146N1010, STATION 1380, STRINGER 25L - 27R CSDR FDEA201603100889Skin · dentedINCOMING, LT INBD FLAP, LOWER SURFACE, 12" OTBD OF CANOE & 14" FROM TE, HAS DENT. REPAIRED LT INBD FLAP, LOWER SURFACE IAW-SRM-51-70-10-2R REPAIR 4. FINAL REPAIR DIMENSIONS, 3.0" DIAMETER DOUBLER LOCATED 22.O" OTBD OF MF STATION 223.96 & 19.0" FWD OF TE. SDR FDEA201603090874Skin · delaminatedRIGHT INBD TE MAIN FLAP, UPPER OTBD ACCESS PANEL, UPPER SURFACE FOUND WITH MULTIPLE DENT MARKS & MULTIPLE DELAMINATED AREA. DAMAGED AREAS REMOVED, CLEANED & DRIED USING 150 DEG F PROCESS IAW SRM 57-53-01-2R DETAIL 1 REV 116 & SRM 57-70-10-2R REV 116. REPAIR SDR FDEA201603020804Panel · damagedPANEL RACK ZONE 60 RT WING INBD FLAP PANEL HAS TOOLING MARK ON AFT END OF PANEL, BETWEEN SCREW HOLES. COMPLIED WITH EA F-5750-T0323339 PT 1 DATED 02 18 16. WINGS, FLIGHT SURFACES, RT WING MAIN FLAP TOOLING MARK & BLEND. REF FAA FORM 8100-9 DATED 02 11 2016 SDR FDEA201603020758Bolt · looseFORWARD E & E COMPARTMENT, RT FWD RUDDER CONTROL QUADRANT LOWER MOUNT, THREE BOLTS PARTIAL INSTALLED FOUND DURING RUDDER SYS RIGGING. R & R IAW AMM 27-21-05 REV 114. R/H FWD RUDDER CONTROL QUADRANT BOTTOM BEARING HOUSING R & R IAW AMM 27-21-05 REV 114. RUDDESDR FDEA201603020757Regulator · damagedFLIGHT CONTROLS, DURING BUY BACK, FOUND ELEVATOR TENSION REGULATOR SPRING GUIDE BROKEN. LT SIDE ELEVATOR TENSION REGULATOR R & R IAW AMM 27-31-12 REV 115. CONTROL CABLE FOR ELEVATOR TENSION REGULATOR REMOVED & INSTALLED AFTER MX IAW AMM 27-31-12 REV 115. ADSDR CALA2016022995200Battery · dischargedEXIT SIGN ABOVE SEAT 20A INOPERATIVE. REPLACED BATTERY FOR EXIT SIGN AT SEAT 20A.SDR FDEA201602260690Skin · dentedFUSELAGE EXTERIOR SKIN RT SIDE, THERE IS AN EXISTING DENT WITH PREVIOUS OPERATOR STICKER AT BS 395 - 418, STRINGER 14 - 17. DENT FOUND OUT OF LIMITS IAW SRM 53-00-01-1A FIG 101 DET III REV 116. REPAIR CARRIED OUT IAW EA F-5330-T0323629 PART 1. FUSELAGE SKINSDR FDEA201602260691Torque Tube · looseAFTER TAKEOFF, DURING FLAP RETRACTION FROM FLAPS 1 TO FLAPS 0, HAD EICAS MESSAGE, LE FLAP ASYM, & AMBER LIGHT LE. RETURNED TO LAND IAW QRH FAULT CODE FRM 27 90 24 00. INSTALLED TORQUE TUBE COUPLER AND OPS CHECKED LEADING EDGE SLAT SYSTEM IN REF 27-81-00-5 ANSDR FDEA201602240678Skin · damagedLEFT WING, INBD MAIN FLAP UPPER INBD SKIN, EXTERIOR SURFACE FOUND 01 EA DENT & DELAMINATION MARK AT 20.5" FROM TE, 36" FROM INBD EDGE. DAMAGED AREA REMOVED, CLEANED, DRIED & REPAIR DOUBLERS INSTALLED IAW SRM 57-53-01-2R DETAIL I & SRM 51-70-10-2R REPAIR GENERSDR FDEA201602190631Bulkhead · chafedNUMBER 1 PYLON, AFT BULKHEAD LTH SIDE, LOWER CHORD CHAFED. ACCOMPLISHED EA F-5450-T0323050 PT 1. NACELLE & PYLON, WING PYLON & STRUT 1. ENG PYLON, AFT BULKHEAD OTBD LOWER CORNER, BLEND REPAIR, NACELLE STATION 203. REF FAA FORM 8100-9, DATED 02 15 16 FOR APSDR FDEA201602130535Frame · dentedINCOMING, FRAME UPPER FLANGE REPAIR BS 1620, BETWEEN STRINGER 25L - 26L, HAS DENT & CORROSION. DENT ON FRAME UPPER FLANGE IS NOT ALLOWED IAW SRM 53-00-07-1A FIG 101. R & R FRAME BS 1620 IAW SRM 51-40-02-0G. CAT A REPAIR MAJOR REPAIR.SDR FDEA201602100501Pump · crackedLEFT HYD SYS FAILURE AS CONFIGURATION FOR LANDING, HAD TO SERVICE LT HYD SYS ON PREFLIGHT DUE TO LOW FLUID, FOUND LE SLAT BYPASS VLV LEAKING. REMOVED, REPLACED & TESTED IAW MM 27-81-09-4. R & R LT SYS EDP PRESS & CASE DRAIN FILTERS IAW MM 29-11-17-4 FILTERS SDR FDEA201602100499Beam · gougedNR 1 CARGO DOOR, LOWER EDGE BEAM HAS GOUGES. NR 1 CARGO DOOR LOWER EDGE BEAM REPLACED IAW EA F-5230-T0323763 P 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201602080494A/C Pack · smokeAPPEAR TO HAVE SMOKE COMING FROM PACK ON TAKEOFF. TURNED PACKS OFF, SMOKE STOPPED. RETURNED FOR LANDING. DRAIN ALL THE ENGINE OIL AND RE-SERVICE TO A KNOWN QUANTITY. AFTER IDLE RUN THE ENGINES SERVICED OIL AS NEEDED. AFTER SEVERAL CYCLES OF IDLE, CRUISE PSDR FDEA201602050459Stop Fitting · galledCABIN L1 DOOR, FWD EDGE NR 1 - 7 STOP PINS FOUND METAL GALLING. R & R IAW AMM 52-11-00 REV 114. ADJUSTMENT CHECK CARRIED OUT IAW AMM 52-11-00 REV 114. FOUND GOOD. REPAIR CLASSIFIED AS MINOR.SDR FDEA201602050458Bearing · looseCABIN L1 DOOR, FWD EDGE LOWER LATCH CRANK FOUND LOOSEN AT SUPPORT BEARING AREA. L1 DOOR, FWD LOWER LATCH CRANK R & R IAW CMM 52-11-07 REV 114. L1 DOOR FWD LOWER LATCH CRANK SUPPORT BEARING R & R IAW SOPM 20-50-03 REV 127. ADJUSTMENT CHECK CARRIED OUT IAW AMSDR CALA2016020495086Line · leakingON THE RNWY FOR TAKEOFF, FOLLOWING ACFT REPORTED FLUID PUDDLE UNDER RT MLG & SIGNS OF VISIBLE FOG. REPLACED 2 RT NR 4 MLG BRAKE LINES WITH NEW LINES. BLEED BRAKES IAW AMM 32-41-00. OPERATIONS CHECKED GOOD.SDR FDEA201602030433Skin Panel · dentedFUSELAGE SKIN APPROX BS 752, STRINGER 25L - 26L, HAS AN OUTWARD DENT. AFTER DENT EVALUATION, IT WAS FOUND OUT OF LIMITS IAW SRM 53-00-01-2R FIG 101 DETAIL III. REPAIRED DAMAGED AREA IAW SRM 53-00-01-2R FIG 201 REPAIR 7. REPAIR IS CATEGORY B. MAJOR REPAIR.SDR FDEA201602030436Strap · corrodedAFT CARGO COMPARTMENT, LOWER LOBE SHEAR TIE HAS CORROSION, BS 1620, LBL 9. UPON EVALUATION, CORROSION WAS FOUND ON SPLICE STRAP & NOT SHEAR TIE. THERE IS NO ALLOWABLE DAMAGE IAW SRM. R & R SPLICE STRAP AT STATION 1620, STRINGER 25L - 25R IAW SRM 51-40-02-0GSDR FDEA201602010418Cable · unsecureON EXTERIOR WALK AROUND FOUND R1 DOOR WITH SLIDE RAFT HANGING OUT. REINSTALLED SLIDE RELEASE ROPE IAW AMM 25-66-01-4 & 25-66-00-5. OPERATIONS GOOD. OK FOR SERVICE.SDR FDEA201601300401Skin · dentedFUSELAGE SKIN APPROX BS 710, STRINGER 23L - 24L, HAS AN OUTWARD DENT. EVALUATED DENT, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REPAIRED SKIN IAW SRM 53-00-01-2R FIG 201 R7. THIS IS A CATEGORY B REPAIR. MAJOR REPAIR.SDR FDEA201601280360Skin Panel · debondedEXISTING REPAIR WING. THERE IS A REPAIR AT RT SIDE INBD MAIN FLAP, UPPER PANEL AT MF STATION 300. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A4 PT 1, ATTACHMENT B. HISTORY 5100-9 DATED 12 1 2006. EXISTING REPAIR WAS EVALUATED IAW ATTACHMENT B OF SDR FDEA201601280364Skin · dentedFUSELAGE SKIN DENTED, BS 780, STRINGERS 15 - 16L. EVALUATED DENT IAW SRM 53-00-01-1A FIG 101 SH 4. REPAIRED SKIN DAMAGED AREA IAW SRM 53-00-01 FIG 201 REPAIR 16. THIS IS A CATEGORY B REPAIR. DENT WAS OUT OF LIMITS IAW SRM 53-00-01-1A FIG 101 SH 4. MAJOR RSDR FDEA201601260318Skin · damagedLEFT WING, AFT OVERWING ATTACH FITTING, ABOVE FRONT SPAR & NR 4 SLAT INBD MAIN TRACK REMOVAL, FOUND OSS 346 LE FIXED RIB COMMON TO WING UPPER SKIN LE LOCK FASTENER HOLE, ONE EACH, ELONGATED. LT WING OSS 346 LE FIXED RIB COMMON TO WING UPPER SKIN LE LOCK FASTESDR FDEA201601240288Seat Track · corrodedBS 870 - 898, LBL 45.5, SEAT TRACK CROWN SUPPORT FOUND CORROSION AROUND THE BUSHING AREA. CORROSION EVALUATED & FOUND CORROSION MORE THAN 50% THROUGH EXCEED LIMIT IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 117. NEW SEAT TRACK SUPPORT FABRICATED IAW DWSDR FDEA201601220284Skin · dentedINCOMING, DENT IN FUSELAGE EXTERIOR SKIN, 18" FWD OF THE E & E BAY ENTRANCE WAY. ACCOMPLISHED EA F-5330-T0322892 PT 1. FUSELAGE PLATES & SKINS, FUSELAGE SKIN. REPAIR STATION 439 - 446, STRINGER 27L - 28L. THIS IS A CAT B REPAIR. REFERENCE FAA FORM 8100-9 SDR FDEA201601220281Floorbeam · damagedCABIN STATION 936, LBL 45.5, FLOORBEAM INNER FLANGE FOUND 01 ELONGATED FASTENER HOLE. REPAIRED IAW EA F-5310-T0322784 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201601190198Skin · dentedSKIN DENTED & CREASED AT BS 465, STRINGER 22R - 23R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REPAIRED IAW SRM 53-00-01 FIG 201 R16. THIS IS CATEGORY B REPAIR. MAJOR REPAIR.SDR FDEA201601180189Floorbeam · corrodedBS 1681, FLOORBEAM FWD FLANGE CORRODED TOPSIDE & IN FASTENER HOLES, RBL 24 - 47. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101 DET III. R & R FLOORBEAM IAW SRM 51-40-02 & DWG 146N5091 REV AG. MAJOR REPAIR CAT A RESDR FDEA201601180188Floorbeam · corrodedBS 1681 FLOORBEAM FWD FLANGE CORRODED TOPSIDE & IN FASTENER HOLES, RBL 24 - 47. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101 DET III. R & R FLOORBEAM IAW SRM 51-40-02 & DWG 146N5091 REV AG. MAJOR REPAIR CAT A REPSDR CALA2016012095010Fuel Control · faultyAT APPROX 500 FT, LT ENG 1, AUTO ACCELERATED TO FULL POWER. ATTEMPTED TO REDUCE POWER, NO RESPONSE WHEN THROTTLE RETARDED. NO RESISTANCE IN THROTTLE LEVER. ACCOMPLISHED GO AROUND, SHUTDOWN NR 1 ENG & LANDED. R & R FUEL CONTROL NR 1 ENG IAW AMM 73-21-01. ISDR CALA2016011895008Doubler · damagedL2 REPAIR DOUBLER AT UPPER HINGE CUT OUT DAMAGED. REMOVED EXISTING DAMAGED DOUBLER, AT UPPER HINGE CUT OUT ON FWD FRAME. FORMED A REPAIR ANGLE & INSTALLED.
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