Boeing 757-2B7
Service difficulty reports · 3,730
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 = '7572B7' 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 = '7572B7' 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 FDEA201011084282Skin · damagedEXISTING DOUBLER REPAIR ON NR 9 SLAT INBD AND OTBD END UPPER SURFACE. COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5001 PT 1 EVALUATED REPAIR IAW EO F-5100-7-5001 ATTCHEMENT "B". REPAIR FOUND TO BE IAW SRM 51-70-10, REPAIR 2, FIG 201. REPAIR IS CLASSIFIED AS ASDR USAA2010111592608Skin Panel · delaminatedCLT - MAJOR REPAIR - C2 CHECK - VERTICAL STABILIZER SKIN PANEL 6 INCHES AFT OF AUXILIARY SPAR AT STATION 120 IS DELAMINATED. REPLACED VERTICAL STABILIZER SKIN PANEL 6 INCHES AFT OF AUXILIARY SPAR AT STATION 120 IAW BOEING 757 DRAWING 175N2001.SDR USAA2010111692612Slide · inoperativeCLT - EES - C2 CHECK - DURING A SCHEDULED DEPLOYMENT OPERATIONAL CHECK OF THE L4 DOOR SLIDE, THE LOWER AFT LIGHT DID NOT ILLUMINATE. REPLACED SLIDE IAW TASK CARD 19L80025001.SDR FDEA201011024222Seat Track · misalignedSEAT TRACK STA 377-440, LBL 25 REQUIRES CHANGE IAW CUSTOMER REQUEST. R & R SEAT TRACK STA 377-440, LBL 25 IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.SDR USAA2010111592610Stringer · corrodedCLT - MAJOR REPAIR - C2 CHECK - CORROSION ON STRINGER AT BS 1412 - BS 1440, S30. REPAIRED STRINGER AT BS 1412 - BS 1440, S30 IAW EA 102306.SDR USAA2010111592606Panel · delaminatedCLT - MAJOR REPAIR - C2 CHECK - VERTICAL STABILIZER LEFT TORQUE BOX PANEL HAS DELAMINATION. REPAIRED VERTICAL STABILIZER LEFT TORQUE BOX PANEL IAW EA 139564.SDR USAA2010111592609Wedge · delaminatedCLT - MAJOR REPAIR - C2 CHECK - LEFT WING LEADING EDGE SLAT NR 4 TRAILING EDGE WEDGE LOWER SURFACE HAS DELAMINATION. REPAIRED LEFT WING LEADING EDGE SLAT NR 4 TRAILING EDGE WEDGE LOWER SURFACE IAW B757 SRM 51-70-10.SDR USAA2010111592607Beam · crackedCLT - MAJOR REPAIR - C2 CHECK - VERTICAL STABILIZER T/E BEAM CRACKED AT STATION 90. REPAIRED VERTICAL STABILIZER T/E BEAM AT STATION 90 IAW EA 102285.SDR USAA20101026BB071Motor · burnedFLT 750 WHILE EN-ROUTE, DURING FLIGHT, SEAT 3C MOTOR OVERHEATED. HOT ACRID SMELL FROM UNDER SEAT. SPARKS FROM AREA POWER DISCONNECTED. THE FLIGHT DIVERTED TO YJT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND VACUUM MOTOR FOR LUMBAR BAGS BURNT. REMOVED AND SDR USAA20101025BB070Transceiver · inoperativeFLT 807 EN-ROUTE. THE CREW COULD NOT GET THE AIRCRAFT HF RADIOS TO TRANSMIT OR RECEIVE, REPORTING: "TRANSMISSION AND RECEPTION ON R HF AT 5547, 8843 KHZ INOP (OCCASIONAL XMISSIONS ON 5547, WEAK)" AND "TRANSMISSION AND RECEPTION ON L HJF AT 5547, 8843 KHZ INOSDR USAA20101025BB069Coupler · inoperativePHX FLT 807 EN-ROUTE PHX TO HNL. THE CREW COULD NOT GET THE AIRCRAFT HF RADIOS TO TRANSMIT OR RECEIVE, REPORTING: "TRANSMISSION AND RECEPTION ON R HF AT 5547, 8843 KHZ INOP (OCCASIONAL XMISSIONS ON 5547, WEAK)" AND "TRANSMISSION AND RECEPTION ON L HJF AT 55SDR USAA20101025BB068Coupler · inoperativePHX FLT 807 EN-ROUTE PHX TO HNL. THE CREW COULD NOT GET THE AIRCRAFT HF RADIOS TO TRANSMIT OR RECEIVE, REPORTING: "TRANSMISSION AND RECEPTION ON R HF AT 5547, 8843 KHZ INOP (OCCASIONAL XMISSIONS ON 5547, WEAK)" AND "TRANSMISSION AND RECEPTION ON L HJF AT 55SDR USAA20101025BB067Transceiver · inoperativeFLT 807. CREW COULD NOT GET THE ACFT HF RADIOS TO TRANSMIT OR RECEIVE, REPORTING: "TRANSMISSION AND RECEPTION ON RT HF AT 5547, 8843 KHZ INOP (OCCASIONAL XMISSIONS ON 5547, WEAK)" AND "TRANSMISSION AND RECEPTION ON LT HJF AT 5547, 8843 KHZ INOP". MAINTENANCESDR FDEA201010214144Fitting · misinstalledPOTENTIAL SHORT EDGE MARGIN CONDITIONS IN THE 675N3161-11 FITTING DUE TO INCOMING FASTENER HOLE LOCATIONS AT STA 1640, S-17L- 18L. A REPAIR WAS ACCOMPLISHED ON STAM EA 757-5362-16-F2804 FOR POTENTIAL SHORT EDGE MARGIN CONDITIONS IN THE 657N3161-11 FITTING AT SDR FDEA201010214142Frame · damagedMISDRILLED HOLES COMMON TO 143N1002-18 FRAME WEB, 143N1002-9 FRAME DOUBLER AND 143N1114-3 INBD CHORD AT STA 460, BETWEEN S-13L AND S-14L. A REPAIR WAS ACCOMPLISHED ON STAM EA 757-5332-16-F2898 FOR MISDRILLED HOLES COMMON TO THE 143N1002-18 FRAME WEB, 143N1SDR FDEA201010214139Fitting · misinstalledPOTENTIAL SHORT EDGE MARGIN CONDITIONS IN 657N3161-12 FITTING DUE TO INCOMING FASTENER HOLE LOCATIONS AT STA 1640, S-17R- 18R. A REPAIR WAS ACCOMPLISHED ON STAM EA 757-5362-16-F2803, FOR POTENTIAL SHORT EDGE MARGIN CONDITIONS IN THE 657N3161-12 FITTING AT STASDR FDEA201010214138Structure · damagedSMOKE DETECTOR CUT OUTS INCORRECTLY LOCATED AT STA'S 1620, STA 1640 AND STA 1661, LBL 28.25. A REPAIR WAS ACCOMPLISHED ON STAM EA-757-5365-16-F2884, FOR THE SMOKE DETECTOR CUT OUTS INCORRECTLY LOCATED AT STA 1620, 1640, AND 1661, LBL 28.25. AN 8110-3, DATED SDR USAA20101021BB065Battery · dischargedDCA - THE FLASHLIGHT AT THE RIGHT EMERGENCY EXIT JUMPSEAT WAS INOPERATIVE. REPLACED FLASHLIGHT BATTERY.SDR USAA20101018BB064Switch · inoperativePHX - THE EMERGENCY LIGHTS AT DOORS L2 AND R2 DO NOT COME ON WHEN THE SWITCH ON THE NOSE GEAR IS USED FOR THE TEST. INSTALLED NEW SWITCH S10035 IN P-62 PANEL.SDR FDEA201010154080Skin · misrepairedEXISTING EXTERNAL DOUBLER ON L-2 DOOR LOWER FWD HINGE CUTOFF DOES NOT MEET SRM REQUIEMENTS. ACCOMPLISHED EA F 5210-141214,DOORS L-2 DOOR OUTER SKIN EXISTING REPAIR REPLACEMENT, PN 143N6100-3, SN 000474. MAJOR REPAIR.SDR USAA2010101492286Skin Panel · delaminatedCLT - C2 - MAJOR REPAIR - DELAMINATION ON OUTER SKIN OF RIGHT VERTICAL STABILIZER FORWARD TORQUE BOX PANEL. INSTALLED SERVICEABLE RIGHT VERTICAL STABILIZER FORWARD TORQUE BOX PANEL.SDR USAA2010101492287Slat · debondedCLT - C2 - MAJOR REPAIR - AREA OF DISBOND ON NR 1 SLAT TRAILING EDGE WEDGE 41 INCHES OUTBOARD FROM THE INBOARD END & 1 INCH AFT OF THE LEADING EDGE. REPLACED NR 1 SLAT IAW B757 AMM 27-81-02-4.SDR USAA20101007BB061Air Data Module · malfunctionedFLT 1041- INDICATED AIRSPEED DROPPED ON BOTH CAPTAIN'S & 1ST OFFICER'S PANELS, WITH EICAS MESSAGES "RUDDER RATIO" & "MACH SPEED TRIM". INDICATED AIRSPEED DROPPED TO 140 KTS. ACFT CONTROL MAINTAINED WITH MANUAL PITCH & THRUST. MOMENTARY ELECTRICAL SMOKE ODORSDR USAA20101001BB060Battery Pack · dischargedPIT - AFT EMERGENCY EXIT SIGHT AT R4 DOOR WAS INOPERATIVE. REPLACED BATTERY PACK.SDR USAA2010100192183Wedge · delaminatedCLT - C2 - MAJOR REPAIR - DELAMINATION ON NR 6 SLAT TRAILING EDGE WEDGE. REPAIRED NR 6 SLAT TRAILING EDGE WEDGE IAW B757 SRM 51-70-10.SDR USAA20101001BB058Battery Pack · dischargedPIT - THE AFT EMERGENCY EXIT SIGN AT R4 DOOR WAS INOPERATIVE. REPLACED THE BATTERY PACK AT THE R4 DOOR.SDR USAA20100928BB057Fan · faultyFLT 863- DURING TAKEOFF AND INITIAL CLIMB, A ROTTEN ODOR BECAME APPARENT IN COCKPIT. CREW TURNED OFF THE LT BLEED & LT PACK. ODOR DISSIPATED. AT 5,000 FT, TURNED THEM BACK ON & ODOR RETURNED. CREW TURNED THEM BACK OFF AGAIN. TRIED AGAIN AT 20,000 FEET ANDSDR FDEA201009213594Wedge · dentedNR 1 SLAT T/E WEDGE UPPER SURFACE HAS SEVERAL DENTS REPAIRED NR 1 SLAT WS 711.5 TO 743.5 T/E WEDGE UPPER SURFACE IAW SRM 51-70-10, PN 114N4002-153A, SN A1-0616. CLASSIFED CATEGORY "A" MAJOR REPAIR.SDR FDEA201009173520Skin · dentedEXTERNAL FUSELAGE SKIN LT SIDE, STA. 980-1000 BETWEEN S-9L TO S-10L IS DENTED. DENT OUT OF LIMITS IAW SRM 53-00-01 FIG 101, DET.III, ACCOMPLISHED EA F-5330-141197 DTD 03SEP10, FUSELAGE STA. 993 SKIN DENT NEAR S-10L LAP SPLICE. PN: 144N3140.SDR FDEA201009163507Skin · damagedCUT FOUND AT S14R FROM BS 781 THROUGH BS 781,156 RUNNING VERTICAL UNDER LAP SEAM AT THE EDGE OF THE BUTT JOINT, DURING LAP SEAM INSP FOR SCRIBE LINES. ACCOMPLISHED EA F-53330-139219 FUSELAGE- PLATE/ SKIN (AD2007-19-07) EO F-5330-7-5000 SECTION 43 SKIN SCRATCH SDR FDEA201009143370Web · damagedTHIS NON ROUTINE FOR TIME AND REPAIR TRACKING. W/C MAE MOD (43607420001 / 118350499EZ2R01). REWORK REQUIRED AT LBL 29. FLOORBEAM WEBS AT FS 1620, 1640, AND 1661. STRUCTURES MECH MIS-READ DWG 657N3374, SHT 1, AND DRILLED / CUT A2" HOLE AT LBL 29 IN FLOORBEASDR FDEA201009133357Skin · puncturedOUTER PUNCTURE ON FUSELAGE SKIN AT STA 710 BETWEEN S-26R TO S-27R EVALUATED DENT, FOUND PUNCTURE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. REPAIRED SKIN AT STA 710, BETWEEN S-26R TO S-27R IAW SRM 53-00-01, FIG 201, REPAIR 7 CLASSIFED CATEGORY "B" SDR FDEA201009093328Skin · dentedREWORK- DENT WAS FOUND ON FIRST EVALUATION TO BE OUT LIMITS, WAS RE-EVALUATED AND BLOCK 26 "CORRECTIVE ACTION" STATED TO BE FOUND WITHIN LIMITS. SECOND EVALUATION DID NOT ADDRESS FIRST EVALUATION OUT OF LIMITS CONDITION "DENT IS WITHIN .5" PROXIMITY OF SSDR FDEA201009083320Angle · corrodedINTERCOSTAL PLATE BET 29R AND S28R ON ATA 740 HAS CORROSION. (FWD CARGO). REMOVED CORROSION IAW SRM 51-10-02, BLENDED AREA STA 740, STR28R AND 29R, L=2" W=3" D=0.008 MAT ORIG .071 MAT REMAIN .063 OUT OF LIMITS IAW SRM 53-00-04, FIG 101, DET II. REMOVED ANGLE CSDR FDEA201009083315Skin · damagedSCRIBE LINE FOUND AT STA 586.375 TO 602.250 S-26L DURING LAP SEAM INSP FOR SCRIBE LINES ACCOMPLISHED EA 5330-141725. CLASSIFIED CATEGORY "A" MAJOR REPAIR.SDR FDEA201009083314Skin · damagedSCRIBE LINE FOUND AT STA 538.5 TO 539.563 S-26L DURING LAP SEAM INSP FOR SCRIBE LINES ACCOMPLISHED EA F-5330-141725. CLASSIFIED CATEGORY "A" MAJOR REPAIR.SDR FDEA201009083313Skin · damagedSCRIBE LINE FOUND AT S-26L FROM STA 529-530.438 DURING LAP SEAM INSP FOR SCRIBE LINES ACCOMPLISHED EA F-5330-141725. CLASSIFED CATEGORY "A" MAJOR REPAIR.SDR FDEA201009033270Battery Pack · misinstalledDOOR EMERGENCY LIGHT INOP INTERIOR. RELEASED FOR SERVICE IAW MEL: 33-51-01-01, CATEGORY: D EXPIRATION: 01JAN11 "MEL 33-51-01-01: INTERIOR EMERGENCY LIGHTS - INOP." FOUND BATTERY PACK NOT FULLY INSTALLED. SECURED BATTERY AND SYS OPS GOOD IAW MM 33-51-01.SDR FDEA201009033271Lamp · inoperativeR1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED R1 DOOR EMERGENCY LIGHT, OPS CHECKED GOOD, REF MM 33-51-06-2.SDR FDEA201009013233Doubler · damagedL-2 DOOR INTERNAL SKIN A DOUBLER HAS A DOUBLE DRILL HOLE AT APPRO 8" AFT OF FWD EDGE AND 27" FROM THE BOTTOM EDGE. ALL REPAIRED ACCOMPLISHED ON EA F-5210-141186, MAJOR REPAIRSDR USAA20100902BB052Bellows · failedPIT - FLT 739 EN ROUTE PHL TO PIT. AT FL 220, THE AIRCRAFT EXPERIENCED A THROTTLE SPLIT OF ABOUT FIVE INCHES BETWEEN ENGINES 1 AND 2. THE MAX EPR ON THE RIGHT ENGINE WAS 1.19 AT THE FIREWALL. THE LEFT ENGINE HAD NORMAL READINGS. THE CREW DECLARED AN EMERGSDR FDEA201008273163Seat Track · corrodedSEAT TRACK RBL 45 STA 640-780 CORRODED AND GOUGED. REMOVED CORROSION AND GOUGES AT SEAT TRACK RBL 45 STA. 640-780 IAW SRM 51-10- 02. BLENDED AREA ORIGINAL MATERIAL=.070 IN. L=4.0 IN W=1.0 IN. D=.022 FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL VISDR FDEA201008233106Stringer · corrodedAFT CARGO PIT COMPT STA 1600-1620 S-29L STRINGER SPLICE CORRODED REMOVED CORROSION & FOUND OUT OF LIMITS IAW SRM 53-00-03 FIG 101. FURTHER INVESTIGATION 29L STRINGER IS ALSO CORRODED AND FOUND TO BE OUT OF LIMIT 100% MATERIAL LOSS. FABRICATED REPAIR STRINGESDR FDEA201008233113Frame · crackedAFTER REMOVAL OF TV MONITOR BRACKETS FOUND FRAME CRACKED STA 377-7, BETWEEN S-1 TO S-2L. CRACKED FRAME STA 377.7 S-5L TO S4R FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL I. REMOVED AND REPLACED FRAME IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJSDR FDEA201008233112Skin · dentedDENT ON LT SIDE VERT STAB FSS-146 EVALUATED 2EA DENTS ON VERT STAB STA FSS-146. DENTS WITHIN 1SQ FT OF EACH OTHER. FOUND OUT OF LIMITS IAW SRM 55-30-01, FIG 101, DETAIL III NOTE "H". REPAIRED DENTS IAW SRM 51-70-10, REPAIR 2. CLASSIFIED CATEGORY "A" MAJOR SDR FDEA201008233111Skin · dentedDENT IN LT SIDE OF VERT STAB FSS-153 EVALUATED 2EA DENTS ON STAB STAB STA FSS 153. DENTS WITHIN 1SQ FT OF EACH OTHER. FOUND OUT OF LIMITS IAW SRM 55-30-01, FIG 101, DETAIL III AND NOTE "H". REPAIRED DENTS IAW SRM51-70-10, REPAIR 2 CLASSIFIED CATEGORY "A" MAJSDR FDEA201008213086Seat Track · corrodedMAIN CABIN SEAT TRACK , STA. 1540 - 1640 RBL 25 IS GOUGED AND HAS CORROSION. BLENDED OUT CORROSION AND GOUGES THE MAX DEPTH IS .030 IN. AND IS OUT OF LIMITS IAW SRM 53-00-52 FIG.101 DETAIL 1. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02. REPAIR IS CLSDR USAA20100824BB049Fuse · blownPHL - MAINTENANCE REPORTED THE L3 DOOR EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED A BLOWN FUSE IN POWER SUPPLY. OPERATIONAL CHECK GOOD.SDR FDEA201008203063Nut Plate · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE BS 1340 - 1320 HAS NUMEROUS RUSTY NUT PLATES, LBL 7.55.SDR FDEA201008203060Seat Track · corrodedMAIN CABIN BETWEEN BS 1540 - 1640 LBL 25 SEAT TRACK WITH CORROSION AND GOUGES. BLENDED OUT GOUGES AND CORROSION AND MATERIAL REMAINING IS .085 AND IS OUT OF LIMITS IAW SRM 53-00-52 FIG 101, DETAIL 1 OF CROWN AREA. R & R SEAT TRACK IAW SRM 5I-40-02. REPAIR IS
Back to Boeing 757-2B7