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 FDEA201010204117Plate · crackedFWD CARGO COMPT AFT REVEAL PLATE FOUND BOTTOM CORNER CRACKED OFF. FWD CARGO COMPT AFT BOTTOM CORNER CRACKED REVEAL PLATE R & R IAW SRM 51-40-02 REV 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201010204116Intercostal · crackedE/E COMPT INTERCOSTAL ASSY AT STA 440- STA 460 S24L FOUND CRACKED. CRACKED INTERCOSTAL FROM STA 440 TO STA 460, STR 24L R & R WORKCARD 118150066FL1R02 (SUPPORT INSTL - E1-E5 ELEX EQUIP CTR). ALTERATION IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201010124018Skin · dentedFUSELAGE SKIN DENTED STA 1340 STR 29R. EVALUATED DENT AND FOUND OUT OF LIMITS DUE TO CROSSING A FRAME IAW SRM 53- 00-01. REMOVED DAMAGED SHEAR TIE, CUT OUT DAMAGED AREA DIMS 3 3/4" X 2 1/4", FABRICATED NEW SHEAR TIE, HEAT TREATED SHEAR TIE TO 7075T-6 CONDISDR FDEA201010103984Seat Track · corrodedAT RBL 24, BL 1600- 1640 HAS HEAVY PITTING IN INBD RADIUS OF SEAT TRACK CROWN TO FLANGE. CHECKED LIMITS FOUND TRACK TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DET VII. PAGE 104. REMOVED SEAT TRACK IAW SRM 51-40-09. TRIMED NEW SEAT TRACK PER SAMPLE ISDR FDEA201009223634Skin · dentedPREVIOUS SKIN DENTED AT BS 309, S18L. ACCOMPLISHED SKIN REPAIR IAW EA F-5330-141203, BS 309, BELOW S17L. DENT WAS OUT OF LIMITS DUE TO PROXIMITY TO BS 310.5 FRAME. 2EA. SHEAR TIES WERE FABRICATED ON TRAVELERS T10/855076 AND T10/855075. MAJOR REPAIR.SDR FDEA201009213598Shear Tie · corrodedSTA 1460 FRAME SHEAR-TIE BETWEEN STRINGER 26L AND 27L CORRODED. REPLACED SHEAR TIE, FABRICATED ON TRAVELER T10/850999, IAW SRM 51-40-02/ DWG 140N2002. SHEAR TIE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, DETAIL 2, FIG 101. CORROSION REWORK; L=1.74",W=.510"SDR FDEA201009203561Gate · corrodedL2 DOOR LOWER GATE EDGE HAS CORROSION L2 DOOR LOWER GATE OUT OF LIMITS MAX DEPTH MEASURED 0.15 IAW SRM 52-10-02, FIG 101, DETAIL IV SHEET 4 OF 8 PAGE 104. REPLACED GATE IAW SRM 51-10-02. MAJOR REPAIRSDR CNMA20100031Control Module · failedAIR RETURN DUE TO SPOILERS EICAS AND MESSAGE OVERHEAD. R & R ED NR 2 PCA AND LT NR2 ISCM IAW MM 27-61 AND 27-09. OPS CHECK GOOD.SDR FDEA201009173531Floorbeam · corrodedFLOORBEAM STA 377, BL 0, RBL 10, UPPER TEE CORRODED. REMOVED CORROSION PER SRM 51-10-02. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, FIG.101, DETAIL 3. REMOVED DAMAGED AREA OF THE FLOORBEAM PER SRM 53-00- 51. FABRICATED NEW TEE AND REPAIRSDR FDEA201009163506Skin · dentedPREVIOUS SKIN DENT AT BS 668, S19R. EVALUATED DENT L=1.3 W = 1.0 D= .033 FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO SKIN SPLICE. CUT OUT DAMAGE & FABRICATED DOUBLER AND STRUCTURAL FILLER FROM .063 2024-T3 BATCH 1862687 AND SHIM .032 2024 - T3, BATCH SDR FDEA201009153533Skin · corrodedLT OTBD MAIN FLAP CORRODED ON LOWER SURFACE AT WS 409 AND WS 429. CUT OUT DAMAGED AREA OF CHORD DIMS 33" IAW SRM 51-70-12. FABRICATED 2 ANGLES, 1 ANGLE, HEAT TREATED ANGLES TO 2024T-3 IAW FAS ENG REPORT NR 2-37153-801, REV A FABRICATED CHORD AND 1 RADIUS FILLSDR FDEA201009143389Seat Track · gougedMAIN CARGO COMPARTMENT SEAT TRACK HAS SEVERALS GOUGES AND CHAFFED MARKS BS 878 TO 900 RBL 45.50. DAMAGE TO SEAT TRACK MEASURED OUT OF LIMITS IAW SRM 53-00-52 PG102 FIG 101 DET I. REPLACED SEAT TRACK IAW SRM 51-40-02 PG 1 PAR A REPAIR CATEGORY A. MAJOR REPASDR FDEA201009113344Skin · misrepairedRT APU DOOR EXISTING FLUSH REPAIR AT BS 1957, STR 29R DOES NOT COMPLY WITH KNOWN APPROVED DATA. REMOVED EXISTING REPAIR IAW SRM 51-40-02. REPAIRED APU DOOR SKIN, RT, IAW SRM 52-40-01, FIG 201, P205, REPAIR NR 5. CAT "A" MAJOR REPAIR, NO REPETITIVE INSP REQUISDR FDEA201009083532Firewall · corrodedAPU FIREWALL REPAIR HAS SIGN OF CORROSION RBL6. REMOVED DOUBLER IAW SRM 53-80-08 AND 51-40-02, FABRICATED NEW DOUBLER FROM 6AL-4V .025 DIMS 6.2500" X 5.6250" IAW SRM 53-80-08 AND INSTALLED IAW SRM 53-80-08.SDR FDEA201009083317Fitting · misalignedAT STA 1640 LT THE 657N3161-11 FITTING HAS 2EA EXISTING SED FASTENERS AT LWR, INBD, END OF FITTING ALSO 5EA, EXISTING FASTENERS WHERE DWG SHOWS 4EA, AT LWR END OF FITTING APPROX WL 202 TO WL 208 AND JUST INBD OF THAT LOCATION 5EA EXISTING FASTENERS AT INBD, EDSDR FDEA201009083310Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER TEE CORRODED FROM BL 0 TO LBL 24.5 STA 345. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS ORIGINAL THICKNESS .125" AFTER REMOVED .106" FOUND OUT OF LIMITS IAW 53-00-51, FIG 101, DET III REMOVED FLOORBEAM AT STA 345 BET, LBL 70 SDR FDEA201008313280Ground Wire · shortedEMERGENCY LIGHT IN COCKPIT ABOVE OBSERVER SEAT INOP. INSTALLED NEW EMERGENCY POWER SUPPLY, NO HELP, FOUND SHORT TO GROUND WIRE FROM FLIGHT DECK EMERGENCY LIGHT D5264, TO PIN 12 ON POWER SUPPLY CONNECTOR D68. SHORT IS BLOWING FUSE INSIDE POWER SUPPLY. REF WSDR FDEA201008313207Gate · corrodedR2 DOOR LOWER GATE HAS CORROSION ALONG EDGE CHECKED LIMITS ON CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-02, FIG.101, DETAIL 4. MEASURED .150" MATL. LOSS. REMOVED AND REPLACED R2 DOOR GATE, LOWER, P/N 143N6106-26, BATCH 0001899033,PER SRM 51-10-02 SDR FDEA201008313204Skin · wornLT WING- INBD MAIN FLAP L/E, OTBD SIDE HAS 3 WORN SECTIONS WITH TOTAL LENGTH APPROX 20 INCHES. COMPLIED WITH EA F-5750-141199, CLEANED AREAS IAW SRM 51-10-02, OUT OF LIMITS, IAW SRM 57-53-01, FIG 101, SHEET 6. DAMAGE REPAIRED IAW SRM 57-53-01, LOCATED & DRILLSDR FDEA201008313203Floorbeam · mislocatedEXISTING FASTENER HOLE AT STA 440, BL-0, AFTSIDE OF FLOORBEAM WILL BE IN THE RADIUS ON LT SIDE OF L-0 SEAT TRACK CROWN IF DRILLED. AT STA 440, BL-0 EXISTING HOLE PLUGED AND RELOCATED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE MOD W/C NR 118350425BZSDR FDEA201008303196Floor Support · corrodedAFT CARGO FLOOR SUPPORT RBL 7.55 BETWEEN STA 1500 TO STA 1640 NUMEROUS BROKEN SCREWS, NUT PLATES AND ATTACHING RIVETS. REMOVED CORROSION ON FLOOR SUPPORT RBL 7.55, STA. 1500 - 1640 OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DETAIL V. ORIG MATERIAL .063" MAT LOSDR FDEA201008263155Gate · corrodedL-4 DOOR LOWER GATE CORRODED ALONG EDGE AND FWD POCKET INNER SURFACE. FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02 FIG. 101 DETAIL IV. REMOVED LOWER GATE FROM L-4 DOOR IAW SRM 51-40-02. REMOVED SEAL FROM GATE ASSEMBLY IAW AMM 52-09-01. RECEIVED NEW GATE ASSESDR FDEA201008263148Gate · corrodedL-2 DOOR UPPER GATE, AFT POCKETS INNER SURFACE CORRODED. REMOVED CORROSION ON L-2 DOOR UPPER GATE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02. REMOVED SEAL FOR ACCESS IAW AMM 52-09-01. REMOVED HINGE FOR ACCESS IAW SRM 51-40-02. RECEIVED NSDR FDEA201008253134Frame · gougedMAIN CABIN, FRAME BS 1280 S10-13R HAVE GOUGES. REMOVED DAMAGE AT STRG 11R- 13R IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II, REMOVED DAMAGE FRAME FROM STRG 11-13R, STOP 4(B) HFEC REWORK AREA IAW NTM 51--00-19 PH 6. NO CRACKSDR FDEA201008213088Floorbeam · corrodedSTA 365.25 FLOORBEAM HAS CORROSION ON TOP OF BEAM AND UNDERNEATH TOP OF BEAM AT SEVERAL LOCATIONS RT OF BL 0. REMOVED CORROSION IAW SRM 51-10-02. OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. REMOVED DAMAGED FROM LBL 13-RBL 68.6. FABRICATED REPAIR PARTSDR FDEA201008203057Skin · dentedAT STA 1605 STR 26L- PROTRUDING DENT, OTWD. FOUND DENT TO BE OUT OF LIMITS PER SRM 53-00-01, FIG.101,DETAIL 3,DUE TO BEING LESS THAN 3" FROM A SKIN SPLICE. ACCOMPLISHED A FUSELAGE SKIN DOUBLER REPAIR, BS 1605, BETWEEN S26L/27L, PER SRM 53-00-01, REPAIR 7. DSDR FDEA201008193052Seat Track · gougedSEAT TRACK STA.418-440 RBL.45, GOUGED. R & R SEAT TRACK BS 418-440, RBL 45, IAW SRM 51-40-02. BLENDED AREAS IAW SRM 53-00-52, FIG 101; ORIGINAL MATERIAL: .080", AFTER REWORK: .035", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7. REMOVED SEAT SDR FDEA201008193051Seat Track · gougedSEAT TRACK STA 418-440 RBL-24 GOUGED R & R SEAT TRACK, BS 418-440,RBL 24, SRM 51-40-02. BLENDED AREAS IAW SRM 53-00-52, FIG.101; ORIGINAL MATERIAL: .080", AFTER REWORK; .040", ON THE FLANGE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7. REMOVESDR FDEA201008143002Skin · dentedAT STA.1640-1660 BETWEEN STR 27 & 28R, 2 EA. PROTRUDING DENTS. OUTWARD. CONVEX CHECKED LIMITS; DENT NR 1 L=.50", W=.50", D=.043", A/Y=11 / DENT NR 2 L=.50", W= .50", D= .035", A/Y=14. FOUND BOTH DENTS TO BE OUT OF LIMITS PER SRM 53-00-01, FIG.101. REPAIRED SDR FDEA201007292725Frame · dentedSTA 1500 FRAME BETWEEN STR 26L AND 27L DENTED, GOUGED AND CORRODED. REMOVED CORROSION PER SRM 51-10-02; L=3", W=1", D=.004", WITHIN LIMITS PER SRM 53-00- 53, FIG.101. GOUGE AREA; L=1.2",W=.01", D=.003", WITHIN LIMITS PER SRM 53-00-53, FIG.101; DENT OUT OF SDR FDEA201007082415Transmitter · malfunctionedREJECTED TAKEOFF AT 100KTS. AT 80KT POWER WAS SET TO STANDARD AT APPROX 1.57 EPR. AFTER 80 KTS NR 1 ENG PWR DECREASED ABOUT 10 PERCENT. ADVANCED NR1 THRUST LEVER AND NR1 EPR WOULD NOT RECOVERED. CHECKED EJECTOR FILTER AND FOUND CLEAN. PURGED EPR LINE AND R SDR FDEA201005071484Windshield · failedCOPILOTS FWD WINDSHIELD DEVELOPED A SMALL CRACK FROM BOTTOM LT CORNER TO UPPER RT. FOLLOWED BY ARCING, A LOUD SHATTERING NOISE AND A SHATTERED OUTER PANE. REPLACED R1 WINSHIELD IAW MM 56-11-01-4. PREMATURE REMOVAL/INSTALLATION.SDR FDEA201004221356Skin · damagedC-2 DOOR LOWER AFT CORNER EXTERNAL SKIN HAS TRIM OUT FGREATER THAN .001". FABRICATED REPAIR DOUBLER FROM 2024-T3 0.071" DIMENSION 6 3/4" X 6 1/4" IAW SRM 52-30-1 FIGURE 201. TREATED AND PRIMED PARTS IAW SRM 51-20-1. INSTALLED REPAIR DOUBLER AT C-2 DOOR LOWER SDR FDEA201004221354Skin · damagedC-1 DOOR LOWER AFT CORNER EXTERNAL SKIN HAS ROUTE OUT GREATER THAN .001". CUT OUT DAMAGE DIMS 1 1/4" X 1/4" IAW SRM 52-30-1, FABRICATED REPAIR DOUBLER USING 2024T-3 .071 DIMS 5 7/8" X 5 3/4" IAW SRM 52-30-1 AND INSTALLED REPAIR DOUBLER IAW SRM 52-30-1.SDR FDEA201004221355Skin · damagedC-2 DOOR LOWER FWD CORNER EXTERNAL SKIN HAS TRIM OUT GREATER THAN .001". FABRICATED REPAIR DOUBLER FROM 2024-T3 0.071" DIMENSION 6.7500" X 6.5" IAW SRM 52-30-1, FIG 201. TREATED AND PRIMED PARTS IAW SRM 51-20-1. INSTALLED REPAIR DOUBLER AT C-2 DOOR LOWER SDR CNMA0010Engine · vibrationRT ENGINE BANK AND SHUDDER CLIMBING THROUGH 1600', N1 VIB AT 2.9 IN YELLOW ARC. LEVELED AT 1900' REDUCED POWER, VIBRATION RETURNED TO NORMAL.SDR FDEA201002230497Door Frame · crackedR1 DOOR SEAL MATING SURFACE ON FUSELAGE TOP FWD CORNER DAMAGED TRIMMED OUT BS 325.10 FRAME OTBD CHORD, REMOVED CRACK, MAINTAINED .50 R . HFEC INSPECTED TRIM OUT, NO CRACKS NOTED PERFORMED ENSURANCE CUT , FORMED BACK REMAINING PORTION IAW BAC5300, HFEC INSPECTESDR FDEA201002030313Gate · corrodedDOOR R1 LOWER GATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 ON LOWER GATE. CHECKED LIMITS IAW SRM 52-10-02, FIG. 101, DETAIL 12, AND FOUND TO BE OUT OF LIMITS; ORIGINAL MATL. .200"/ MATL. REMAINING .030". REMOVED LOWER GATE IAW AMM 52-11-38. REMOVESDR FDEA201001260266Gate · corrodedDOOR L-2 LOWER GATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02, AND FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02. REMOVED LOWER GATE IAW AMM 52-11-38. INSTALLED NEW LOWER GATE L-2 DOOR IAW AMM 52-11-38. ADJUSTMENT CHECK GOOD IAW AMM 52-11-00. CATEGORY "SDR FDEA201001200198Skin · dentedDENT AT STA 1230 BETWEEN STR 25 AND 26 LT FUSELAGE ( INB OUT WITH CREASE ) CHECKED LIMITS AND FOUND OUT OF LIMITS DUE TO CREASE. REMOVED DAMAGE IAW SRM 53-00-01.INSPECTED W/ NO CRACKS FOUND. FABRICATED DOUBLER FILLER IAW SRM 53-00-01, LOCATED AND DRILLED IAWSDR FDEA201001190183Spar · damagedLT HORZ STAB L/E DAMAGED. REPAIR WAS ACCOMPLISHED IAW MAE EA NR 757-5510-16 A1923. CLASSIFIED AS A, "INTERIM" REPAIR, MAJOR.SDR FDEA201001070041Skin · corrodedFOUND DENTED AREA WITH LIGHTENING STRIKE IN THE CTR & SEVERAL PIN HOLE PITS SURROUNDING THE AREA AT S14R BS 1247.5 IN LAP SEAM AREA. LENGTH OF DAMAGE .156, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01. DRILLED OUT DAMAGE WITH A .159 DRILL BIT IAW SRM 53-00-01SDR FDEA201001050013Support Bracket · corrodedR3 DOOR FWD HINGE SUPPORT BRACKET LWR SURFACE CORRODED STA 1326, RBL 60. REMOVED SUPPORT BRACKET- TEE AND WEB IAW SRM 51-40-02. FABRICATED NEW BRACKET IAW SRM 51-30-01. INSTALLED NEW BRACKET AND WEB ASSY AT STA 1326, RBL 60. IAW SRM 561-40-02. CATEGORY "A',SDR FDEA200912114417Skin · crackedFASTNER HOLE AT STA 1481 S-26L IS CRACKED. REMOVED DAMAGE SKIN IAW SRM 53-00-01. FABRICATED DOUBLER PN NR 2024-T3-.063, FILLER PN NR 2024-T3-.050 IAW SRM 53-00-01. INSTALLED DOUBLER AND FILLER ON FUSE SKIN STA 1477- 1484, S26L, AND CLIP STA 1480, IAW SRM 5SDR FDEA200912084386Strap · corrodedAPU INTAKE DOOR AFT FRAME LWR CORNER HAS CORROSION. REMOVED UPPER STRAP APU AFT FRAME FOUND TO BE OUT OF LIMITS IAW SRM 53-80-08, REMOVED LOWER STRAP ALSO. FABED ON MAE TRAV NR T9/808706, TRAV NR T9/808707. INSTALLED NEW UPPER AND LWR STRAPS AND ATTACHING SDR FDEA200912074368Attach Angle · corrodedTHE CHANNEL CLIP, PN 146N8769-24, AND ATTACHING ANGLE, PN 146N8722-41, IN THE R4 DOOR LWR SILL, ARE CORRODED BEYOUND ALLOWABLE LIMITS AND BS 1645. THE CHANNEL CLIP. PN 146N8769-24 AND ANGLE, PN 146N8722-41, WERE REMOVED AND REPLACED AT BS 1645, R4 DOOR LWR SDR FDEA200912074367Channel · corrodedTHE 143N8328-60 CHANNEL IS CORRODED AT BS 1663, R4 DOOR LWR SILL. THE CHANNEL PN 143N8328-60 WAS REMOVED AND REPLACED AT BS 1663, R4 DOOR LWR SILL, IAW SRM 51-40-02. ORIG MATL THICKNESS; .063", AFTER REWORK; .031". FOUND OUT OF LIMITS IAW SRM 53-60-15. THISSDR FDEA200912074366Stiffener · corrodedTHE 146N8722-60 STIFFNER IS CORRODED AT R4 DOOR LWR SILL, BS 1661. THE STIFFNER PN 146N8722-60 WAS REMOVED AND REPLACED AT R4 DOOR LWR SILL, BS 1661. IAW SRM 51-40-02. ORIG MATL THICKNESS; .071", AFTER REWORK; .046". OUT OF LIMITS IAW SRM 53-60-15. THIS REPASDR FDEA200911204105Seat Track · crackedWEB BENEATH LBL 45 SEAT TRACK CRACKED ON BOTTOM FLANGE, STA 660 TO 680. REMOVED WEB AND SPLICE PLATE IAW SRM 51-40-02, FABRICATED NEW WEB IAW DWG 140N2506 AND SPLICE PLATE IAW DWG 140N2505, TREATED AND PRIMED AND TOP COATED IAW SRM 51-20-01 AND AMM 51-21-01. ISDR FDEA200911204090Frame · corrodedRT LWR FUSELAGE WING TO BODY FAIRING FRAME FS 900 CORRODED WITH CORRODED FASTENERS. REMOVED CORROSION WING TO BODY FRAME STA. 900 FOUND OUT OF LIMITS IAW SRM 53-00-71 DET. 7 REPLACED FRAME, DRILLED AND INSTALLED IAW SRM 51-40-02 THIS IS A MAJOR "A" REPAIR NO
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