Boeing 757-23A
Service difficulty reports · 1,397
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 = '75723A' 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 = '75723A' 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 FDEA201109053667Fitting · corrodedLOWER FWD CARGO COMP LT TIE DOWN FITTING HAS CORROSION AT BS 800. TIE-DOWN FITTING REPAIRED AS PER E.A. F-5340-152555. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201108253466Skin · damagedFUSELAGE EXTERIOR SKIN SCRATCHED AT BS 1578 BETWEEN S17-18L. REPAIRED AS PER E.A. F-5330-152534. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201108253465Skin · scratchedFUSELAGE SKIN, BS 1436 S10L, SCRATCHED. REPAIR CARRIED OUT AS PER E.A. F-5330-153402. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201108233444Girt Bar · failedL-1 DOOR SLIDE WOULD NOT ARM, BINDING PIECE FELL WHEN RETURNED DISARMED. REINSTALLED L1 SLIDE GIRT BAR IAW AMM 25-66-10-2. L-1 DOOR AND SLIDE ARM-DISARM FUNCTION OPERATES NORMALLY.SDR FDEA201108223401Skin · dentedPROTRUDING DENT BS 1675 BETWEEN STRINGER'S 26L AND 27L. DENT OUT OF LIMITS IAW SRM 53-00-01. CUT OUT DAMAGED AREA IAW SRM 53-00-01, FIG 201. FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 53-00-01, FIG 201.SDR FDEA201108093143Battery Pack · failedEMERGENCY EXIT LIGHTS WILL NOT TEST. EMERGENCY EXIT BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED NORMAL. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION.SDR FDEA201108043089Splice Plate · damagedFUSELAGE BUTT JOINT SPLICE PLATE AT STA 780, STR 8L TO 9L HAS SCRIBE LINE WITH MAX DEPTH OF 0.0025". R & R IAW SRM 51-40-02, REV 103. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201108023065Indicator · reads lowON TAKEOFF ROLL F/O AIRSPEED LAGGED BADLY. INFLIGHT A/S CAME BACK TO MATCH CAPT, THEN SHOWED FAST. EVENTUALLY STABILIZED ABOUT 5KTS FAST ON FINAL. FLUSHED F/O'S PITOT SYSTEM USING AMM 34-11-00-3-0 AND REMOVED AND REPLACED RIGHT HAND ADC PER MM 34-12-01-4-0SDR FDEA201108013053Skin · damagedFUSELAGE, BUTT JOINT SPLICE PLATE AT STA 780, S8R TO 9R HAS SCRIBE LINE WITH MAX DEPTH OF 0.0038. DAMAGED BUTT JOINT SPLICE PLATE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 103. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201108013052Stringer · gougedCABIN, STRINGER 2R AT STA 417 HAS GOUGE NEAR FRAME. REPAIRED IAW EA F-5310-152522. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201108013051Stringer · damagedCABIN, STR 1 AT STA 416 HAS TOOLING MARKS IN THE SIDE OF STRINGER. REPAIRED IAW EA F-5310-152521. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201108013050Frame · damagedCABIN, STA 1280, LT FRAME HAS TOOLING MARKS BETWEEN STR 15L AND 16L ON FRAME FLANGE. DAMAGED REPAIRED IAW EA F-5310-152523. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107293028Bottle · dischargedWHEN OPENING L1 DOOR THE DOOR ASSIST BOTTLE DEPRESSURISED.SDR FDEA201107293027Bottle · dischargedWHEN OPENING L1 DOOR THE DOOR ASSIST BOTTLE DEPRESSURISED. REMOVED L1 DOOR RESERVOIR BOTTLE IAW MM 52-11-30-4. NEW RESERVOIR BOTTLE IS BAD FROM STOCK. NO SERVICABLE BOTTLES IN MEM NIS.SDR FDEA201107262998Girt Bar · dislodgedGIRT BAR FELL OUT OF BOTTOM OF DOOR L1. REFITTED AND CHECKED OK.SDR FDEA201107242926Bulb · inoperativeON SHORT FINAL, RT MAIN GEAR LIGHT WAS INOP, SHOWED UNSAFE. NO LIGHT IN GEAR HANDLE OR DISAGREE LIGHT. FLEW LOW APPROACH, HAD GEAR VISUALLY INSPECTED BY TOWER, RAN QRH, REPLACED 1 LIGHT BULB, GEAR LIGHT WORKED SHOWING SAFE GEAR, LANDED WITHOUT FURTHER ISDR FDEA201107162762Floor Panel · corrodedCABIN, DECK PLATE CORROSION, STA 1715, RBL 58 TO LBL 58. REPAIR CARRIED OUT IAW SRM 53-60-51 REPAIR 2 FIG 201, REV 103. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107162761Shim · migrated2 PYLON NACELLE BETWEEN MID BULKHEAD UPPER FLANGE AND INNER WEB SKIN AT PPSTA 174.3 FOUND WITH SHIMS MIGRATION. SHIMS R & R IAW EA F-5450-152561. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107162758Shim · migratedNR 2 NACELLE STRUT UPPER SPAR FITTING AT PPSTA 174.0 FOUND WITH OTBD SIDE HORIZ SHIMS MIGRATION. DAMAGED SHIMS R & R IAW SRM 54-50-90, REPAIR 6, FIG 201, REV 103 AND EA F-5450-152561. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107162755Shim · migratedNR 2 NACELLE STRUT BETWEEN MID BULKHEAD LOWER FLANGE AND STIFFENER AT PPSTA 174.3. FOUND WITH OTBD SHIMS MIGRATION. SHIMS R & R IAW EA F-5450-152561. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201107162751Shim · migratedNR 2 NACELLE STRUT BETWEEN MID BULKHEAD LOWER FLANGE AND STIFFENER AT PPSTA 174.3. FOUND WITH INBD SHIMS MIGRATION. R & R IAW EA F-5450-152561. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107162748Shim · migrated1 PYLON MID BULKHEAD LOWER FLANGE OUTBD AFT SIDE AT PPSTA 174.30 FOUND WITH SHIMS MIGRATION. R & R IAW SRM 54-50-90. REPAIR 7, REV. 103. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107162746Shim · migratedNR 1 PYLON MID-BULKHEAD LOWER FLANGE INBD AFT AND FWD SIDE AT PPSTA 174.30 FOUND WITH SHIMS MIGRATION. SHIMS REPLACED IAW SRM 54-50-90 REPAIR 7, REV 103. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107092620Floorbeam · corrodedCABIN, FLOORBEAM AT STA 365 RBL 58 HAS CORROSION. FLOORBEAM R & R IAW SRM 51-40-02, REV. 103. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107072603Stringer Splice · crackedCABIN, STRINGER SPLICE AT STR 18R STA 1668 TO STA 1695 HAS CRACK THROUGH STRINGER TIE STRAP FASTENER HOLE. CRACKED STRINGER SPLICE R & R IAW SRM 51-40-02, REV 103. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107052572Skin · corrodedNR 1 PYLON NAC STRUT INBD INNER SIDE SKIN AT PPSTA 144.4 - PPSTA 174.30 FOUND WITH CORROSION. SKIN R & R IAW EA 5450-152562. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107052571Skin · corrodedNR 2 PYLON NAC STRUT INBD INNER SIDE SKIN AT PP STA 136.7 - PP STA 174.30 FOUND WITH CORROSION. SKIN R & R IAW SRM 51-40-02, REV 103 AND DWG 311N5002, REV E. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107052570Skin · corrodedNR 2 PYLON NAC STRUT STRUCTURE INBD ACCESS HOLE FOR PANEL NR 443GL CUT-OUT INNER EDGES FOUND WITH CORROSION. SKIN R & R IAW SRM 51-40-02 REV.103 AND DWG 311N5002, REV E. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107052569Skin · corrodedNR 2 PYLON NAC STRUT STRUCTURE OTBD ACCESS HOLE FOR PANEL NR 443AR CUT-OUT INNER EDGES FOUND WITH CORROSION. PANEL R & R IAW EA F-5450-152563. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107052568Skin · corrodedNR 1 PYLON NAC STRUT STRUCTURE INBD ACCESS HOLE FOR PANEL NR 433GR CUT-OUT INNER EDGES FOUND WITH CORROSION. SKIN PANEL R & R IAW SRM 51-40-02 REV 103 AND EA F-5450-145386. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201107052567Skin · corrodedNR 1 PYLON NAC STRUT STRUCTURE OTBD ACCESS HOLE FOR PANEL NR 433AL CUT-OUT INNER EDGES FOUND WITH CORROSION. R & R IAW E.A. F-5450-152562. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201106292483Engine · erraticAT CRUISE FL 400, THE RT ENGINE BECAME ERRATIC WITH EPR FLUCTUATIONS BETWEEN 1.10 TO 1.29 WITH ASSOCIATED VARIATIONS IN N1 AND FUEL FLOW. TURNED AUTO THROTTLES OFF AND THE PROBLEM CONTINUED. REDUCING POWER DID NOT HELP. R & R RT(NR 2) ENGINE EEC IAW AMM 7SDR FDEA201105171850Eec · malfunctionedON DESCENT INTO MEM GOT RT ENG OIL PRESS ALERT WITH OIL PRESS ABOVE 70 PSI (RED) SHUTDOWN RT ENGINE IAW QRH. RECIEVED STATUS MESSAGES, RT ENG SEC SEL RT ENG LOW N1 R ENG OIL PRESS R ENG SPEED CARD RT ENG SEC CONT RT ENG FUEL ON SOL. INSTALLED RT ENGINE EEC SDR FDEA201105111828Spring · brokenHUB TRAINING KNOCKED GIRT BAR OFF EMERGENCY SLIDE ON L1 DOOR AGAIN. "MEL 52-11-01-A: L1 DOOR SLIDE - MISSING (IDENTIFY INOP OR MISSING)." GIRT BAR WOULD NOT ENGAGE OPERATING MECHANISM CORRECTLY, LEAF SPRINGS IN GIRT BAR BROKEN. REMOVED LI DOOR SLIDE, INSTALLESDR FDEA201104271651Fseu · bindingT/E FLAP DISAGREE "T/E FLAP DISAGREE". EICAS MSG ILLUMINATED DURING APPROACH WHILE SELECTING FLAPS FROM 5 TO 20. T/E FLAPS STUCK AT APPROX 18. RAN QRH PROCEDURES WHICH DICTATED ALT FLAP OPERATION. FLAPS MOVED TO 20 WITH ALT MODE. FLAPS LT AT 20 FOR BLOCKINSDR FDEA201103080905Skin · delaminatedDELAMINATION FOUND ON SLAT1 OTBD UPR T/E FROM OTBD END TO 250MM AND 40MM FROM T/E DIM 250MMX40MM, 15SQIN. REPAIRED IAW SRM 57-70-10CH REPAIR #4, 57-43-02 FIG 1 AND FIG 201REPAIR DOUBLER INSTALLED,SDR FDEA201102260783Skin · dentedDENT STA 1690 STRINGERS 14R - 15R. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER 2024T3, .080, STRUCTURAL FILLER 2024T3, .063. TAPERED FILLER 2024T3, .020 AND FILLER 2024T3, .071. INSTALLED REPAIR PARTS IAW EA NR F-5330-123584. CLOSED AND DEACTIVATED R4 SDR FDEA201102220693Skin · dentedDENT ON FUSELAGE IN LAP SEAM, STA 684, STR 26R. FOUND DENT OUT OF LIMITS DUE TO LOCATION ON A LAP SEAM IAW SRM 53-00-01 FIGURE 101. TRIMMED OUT DAMAGE, FABRICATED REPAIR FILLER, STRUCTURAL FILLER, DOUBLER, AND TRIPLER IAW EA F-5330-123582. INSTALLED REPAIR PASDR FDEA201102180781Spar · corrodedNR 5 SLAT FRONT SPAR HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 57-43-02. CUT OUT DAMAGED AREAS IAW SRM 51-70-11. FABRICATED REPAIR PARTS IAW SRM 51-70-11. INSTALLED REPAIR PARTS IAW SRM 51-70-11.SDR FDEA201102170593Skin · corrodedUPON REMOVAL OF DAMAGED STRINGER, FOUND PITTING CORROSION ON SKIN, BENEATH S28L AT STA 480, IMMEDIATELY AFT OF FRAME.SDR FDEA201102140562Channel · corrodedCORROSION INSIDE CHANNEL - STR 28L, STA 480, IMMEDIATELY AFT OF FRAME. REMOVED DAMAGED PORTION OF STRINGER DIM 9 1/4 LONG IAW B757 SRM 53-00-03. FIG 201. FABRICATED PORTION OF STRINGER IAW SRM 53-30-03 FIG 201. INSTALLED NEW PORTION OF STRINGER AND SPLICESDR FDEA201012184716Slide · failedWHEN ACFT BLOCKED IN RAMP, OPENED L1 DOOR BEFORE IT WAS DE-ARMED AND BLEW BOTTLE. SLIDE LANDED ON STAIRS BUT DID NOT DEPLOY. RELEASED FOR SERVICE IAW MEL: 52-11-01-A. L1 DOOR SLIDE - MISSING, SLIDE DID NOT DEPLOY, FOUND BOTH MAGNETS (TARGETS) AND SLID THEM SDR FDEA201012094622Support · chafedLT WING- L/E WING APPROX W/S 240 - L/E DUCT SUPPORT CHAFING INTO VERTICAL SUPPORT. REMOVED & INSTALLED NEW STIFFNER IAW SRM 51-40-02. RECIEVED NEW STIFFNER ON TR T10/861406. P/N 112N2038-79. NO NOTED DAMAGE TO BRACKET. MAJOR REPAIR.SDR FDEA201012064598Skin · wornLT WING OTBD MAIN FLAP L/E INBD SIDE HAS A WORN SECTION APPROX 10" LONG . EVALUATED LT WING OTBD MAIN FLAP AND FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01, PG 106, DETAIL VI. R & R L/E SKIN IAW SRM 51-40-02. CLASSIFIED CATEGORY "A". MAJOR REPAIR.SDR FDEA201011264496Skin · dentedEXTERNAL FUSELAGE SKIN STA 1720-1740 BETWEEN S-25R TO S-16R HAS DENT AT LAP SEAM. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO LAP SEAM. REPAIRED DENT IAW EA F-5330-143218. CLASSIFIED CATEGORY "A" MAJOR REPAIR.SDR FDEA201011184419Skin · damagedLT WING AILERON OTBD AREA LWR SURFACE PUNCTURED THRU SKIN DIAMETER OF HOLE 0.250 BY 1"X1" REPAIRED LT WING AILERON OTBD AREA IAW SRM 51-70-17 SB 757-51-0006 IAW SRM 57-60- 01. FINAL DIAMENTION OF REPAIR 5"X4" AND LOCATED AT THE IM EDGE OF STATIC FRAME REF ESDR FDEA201011184421Wedge · chafedNR 6 SLAT T/E WEDGE UNDER SKIN HAS CHAFE MARKS, REPAIRED NR6 SLAT T/E IAW SRM 51-70-10 IAW SRM 57-43-02. DAMAGE WAS LOCATED AT STA 177.5, APPROX 3" FWD OF T/E. REF EA F-5750-143211. CLASSIFIED CAT "A" MAJOR REPAIR.SDR FDEA201011184420Skin · damagedLT WING NR 2 SLAT HAS NUMEROUS CHAFED MARKS ALONG BOTTOM SKIN AFT EDGE REPAIRED LT WING NR 2 SLAT IAW SRM 51-70-10 IAW SRM 57-43-02 DAMAGE LOCATED AT STA 652.50 APPROX 1" FWD OF T/E SLAT REPAIR DIAM. 1"X1.5". REF EA F-5750-142276. CLASSIFIED CAT "A" MAJOR REPASDR FDEA201011064264Battery Pack · failedDURING TEST OF EMERGENCY EXIT LIGHTS, THE LIGHTS ABOVE THE R-1 DOOR AND COCKPIT DOOR COME ON DIM FOR A FEW SECONDS AND THEN GO OUT. VERIFIED BATTERY DISCHARGED. HAD GOOD POWER, 28VDC, AT PIN 2 ON C/P D66 FOR CHARGER. SUSPECT BAD CHARGER. R & R CHARGER ASDR FDEA201011054257Battery Pack · failedON PRE-DEPARTURE CHECK FOUND THE FLIGHT DECK COCKPIT DOOR EMERGENCY EXIT LIGHT TO BE INOP. R & R BATTERY PACK IAW AMM REF 33-51-00-5-0. OPS CK WAS NORMAL. PREMATURE REMOVAL/INSTALLATION. R & R BATTERY PACK IAW AMM REF 33-51-00-5-0, OPS CK WAS NORMAL.
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