Boeing 737-490
Service difficulty reports · 3,288
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 = '737490' 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 = '737490' 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 ASAA11410538Frame · crackedFRAME 400 IS CRACKED BELOW STR 8L. REPAIRED IAW EA AD20062609 400 53 124 REV A.SDR ASAA11410537Frame · crackedFRAME 380 IS CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.SDR ASAA11410536Frame · crackedTHE 867 FRAME CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.SDR ASAA11410535Frame · crackedTHE 827 FRAME IS CRACKED BELOW STR 8L. REPAIRED IAW EA AD20062609 400 53 124 REV A.SDR ASAA11410534Frame · crackedTHE 867 FRAME CRACKED BELOW STR 8L. REPAIRED IAW EA AD20062609 400 53 124 REV A.SDR ASAA11410533Frame · crackedTHE 787 FRAME IS CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.SDR ASAA11410532Frame · crackedTHE 787 FRAME CRACKED BELOW STR 8L. REPAIRED IAW EA AD20062609 400 53 124 REV A.SDR ASAA11410531Frame · crackedTHE 747 FRAME IS CRACKED BELOW STR 8L. REPAIRED IAW EA AD20062609 400 53 124 REV A.SDR ASAA11410530Frame · crackedFRAME 480 IS CRACKED BELOW STR 8L. REPAIRED IAW AD 20062609 400 53 124 REV A.SDR ASAA11410529Frame · crackedFRAME 480 CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.SDR ASAA11410528Frame · crackedFRAME 440 IS CRACKED BELOW STR 8L. REPAIRED IAW EA AD20062609 400 53 124 REV A.SDR ASAA1140527Frame · crackedFRAME 440 IS CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.SDR ASAA11410526Frame · crackedFRAME 400 IS CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.SDR ASAA11410499Sill · corrodedPASSENGER CABIN AFT WET AREA R 2 INNERCHORD (MOP SILL) CORRODED FROM 947 996. REPLACED CORROSION MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REPLACED INNERCHORD AND REINSTALLED ATTACHING PARTS IAW BA737 400 SRM 53 60 15, 51 40 05 & 51 40 02.SDR ASAA11410498Sill · corrodedPASSENGER CABIN AFT WET AREA L 2 INNER CHORD (NOP SILL) CORRODED FROM STA 947 TO 986. REMOVED CORROSION MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REPLACED INNER CHORD AND REINSTALLED ATTACHING PARTS IAW B737 400 SRM 53 60 15, 51 40 05 & 51 40 02.SDR ASAA11410525Frame · crackedFS 360 FRAME CRACKED BELOW STR 8. REPAIRED IAW ASA EA AD20062609 400 53 124.SDR ASAA11410496Web · crackedRT HORIZONTAL STAB O/B END CLOSER WEB AFT HOLES/UPPER AND LOWER FOR STAB TIP PANEL ARE ELONGATED AND CRACKED. REPLACED CLOSURE WEB FLANGE PLATE IAW SRM 51 40 02 AND BOEING DRAWING 65C25162.SDR ASAA11410477Angle · crackedFORWARD OF R1 DOOR ANGLE CRACKED ON UPPER SURFACE OF WEB ABOVE UPPER DOOR HINGE. REPLACED ANGLE IAW B737 400 SRM 51 40 02.SDR ASAA11410489Strap · crackedFLOOR STRUCTURE STABILIZATION STRAP CRACKED. NO LIMITS ALLOWED, BS 312 WL 200 LBL 11. REMOVED CRACKED STRAP, INSTALLED NEW STABILIZATION STRAP PER DWG 65 45834 AND SRM 51 40 02.SDR ASAA11410500Support Angle · crackedFOUND LEFT WING I/B TRAILING EDGE (NO STEP PNL) I/B ANGLE AFT ATTACH FASTENER HOLE OVERSIZE AND WORN. ALSO POSSIBLE CRACK ABOVE THE FASTENER IN THE ANGLE. REPLACED IAW SRM 51 40 02 SEC 4 (B).SDR ASAA11410497Skate Angle · crackedPOSSIBLE CRACK ON NR 1 PYLON AFT O/B SKATE ANGLE AFT FASTENER HOLE. REPLACED NR 1 PYLON AFT O/B SKATE ANGLE PER SRM 51 40 02.SDR ASAA11410466Skin · crackedNR 1 SLAT L/E BULLNOSE SKIN LOWER SURFACE CRACKED AT CENTER AUX TRACK ATTACH AREA 1.5FT FROM AFT EDGE. REPAIRED PER SRM 57-43-01.SDR ASAA11410490Strap · crackedE & E BAY STRAP CRACKED. REPLACED STRAP PER SRM 51 40 02.SDR ASAA11410438Skin · delaminatedRT WING NR 6 UPPER COMPSITE SURFACE DELAMINATED AT I/B CORNER. REPAIRED THE DAMAGED AREA OF THE NR 6 SLAT UPPER SURFACE I/B CORNER IAW B737 400 SRM 51-70-10 REPAIR 4.SDR ASAA11410437Skin · delaminatedRT WING NR 5 SLAT UPPER COMPOSITE SURFACE DELAMINATED AT I/B CORNER. REPAIRED THE DAMAGED AREA OF THE RT WING NR 5 SLAT UPPER SURFACE I/B CORNER IAW B737 400 SRM 51-70-10 REPAIR 4.SDR ASAA11410436Skin · delaminatedRT WING NR 5 SLAT UPPER COMPSITE SURFACE DELAMINATED AT O/B CORNER. REPAIRED THE DAMAGED AREA OF THE NR 5 SLAT UPPER SURFACE O/B CORNER IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA11410435Angle · crackedFORWARD OF R/1 DOOR ANGLE CRACKED ON UPPER SURFACE OF SECOND WEB BELOW THE UPPER DOOR HINGE. REPLACED ANGLE IAW B737 400 SRM 51 40 02.SDR ASAA11410434Skin · chafedRT WING NR 4 SLAT CHAFE AT LOWER SURFACE AFT END IN NUMBEROUS PLACES. REPAIRED CHAFE DAMAGE IAW B737 400 SRM 51 70 10 REPAIR 4 PAGE 201.SDR ASAA11410433Skin · delaminatedRT WING NR 4 SLAT UPPER COMPOSITE SURFACE DELAMINATED AT I/B CORNER. REPAIRED DELAMINATION DAMAGE IAW B737 400 SRM 51 70 10 REPAIR 4 PAGE 201.SDR ASAA11410432Stringer Clip · crackedPAX CABIN STRINGER CLIP CRACKED AT STA 663.75 STR 10L. REPLACED THE STRINGER CLIP IAW B737 400 SRM 51 40 02.SDR ASAA11410431Angle · crackedFORWARD OF R1 DOOR ANGLE CRACKED ON LOWER SURFACE OF WEB BELOW THE UPPER DOOR HINGE. REPLACED ANGLE IAW B737 400 SRM 51 40 02.SDR ASAA11410430Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 380 BELOW STR 8R. REPLACED THE STRINGER CLIP IAW B737 400 SRM 51 40 02.SDR ASAA11410456Guide Arm · out of adjustF/A REPORTS THAT THE L1 DOOR IS TO CLOSE. ADJUSTED DOOR GUIDE ARM IAW AMM 52 11 00, OPS CHECK GOOD.SDR ASAA1140417Battery Pack · dischargedL1 EMERG EXIT LIGHT ON EXTERIOR INOP. L1 EMERG EXTERIOR PWR SUPPLY AND BATTERY PACK REPLACED PER 33 51 51 962 016 AND 33 51 51 962 015 M1133. OPS CHECK NORMAL.SDR ASAA11410572Structure · crackedLT WING STA WBL 135.5 RIB LOWER CHORD CRACKED BETWEEN WING STR 23. REMOVED CRACKED PORTION OF CHORD. REPAIRED CHORD IAW EA 400 57EA 06417.SDR ASAA11410359Light · inoperativeLT FORWARD OVERWING EMERGENCY EXIT IDENTIFIER HAS BULBS INOP. RELAMPED & PERFORMED GOOD OPS TEST IAW AMM 33 51 22 962 001.SDR ASAA11410356Guide Arm · out of adjustL1 DOOR WILL NOT LATCH CLOSED. UPON INSPECTION FOUND JAM NUT BACKED OFF OF GUIDE ARM. ADJUSTED L1 DOOR GUIDE ARM REF MM 52 11 00 705 007 STEPS G.(1) (2)(C). DOOR FLUSHNESS AND DOOR CLEARANCE CHECKED GOOD REF MM 52 11 00 705 007 FIGURE 503. PERFORMED FORWARSDR ASAA11410355Frame · crackedBS 601 L FRAME INNER CHORD CRACKED AT LOWEST 2 EA FASTENER HOLES WL 200 MARKED. CUT OUT DAMAGE AT LOWEST 2 FASTENER HOLES AND REPAIRED CHORD IAW ASA EA 400 53EA 06253 AND ATS ER 11 04185.SDR ASAA11410354Frame · crackedBS 601 RT FRAME INNER CHORD CRACKED AT 1 EA LOWEST FASTENER HOLE WL 200. FOUND DURING NDI HEEC BOTTOM SIDE OF HOLE MARKED. CUT OUT CRACKED FASTENER HOLE AND REPAIRED IAW ASA EA 400 53EA 06258 AND ATS ER 11 04186.SDR ASAA11410358Frame · crackedBS 616 RT FRAME INNER CHORD CRACKED AT LOWEST FASTENER HOLE WL 200. FOUND DURING NDI HFEC BOTTOM POSITION OF HOLE MARKED. REPAIRED BS 616 RT FRAME INNER CHORD WL 200 PER T/C AD20102506 400 53 8 AND EA 400 53EA 06250.SDR ASAA11410344Angle · crackedRIGHT WING DOG HOUSE PANEL I/B ATTACH ANGLE COMMON TO NR 6 FLAP TRACK FAIRING CRACKED ON LOWER END. ACFT GROUNDED. REMOVED FABRICATED AND INSTALLED PANEL I/B ANGLE IAW DWG 65-69646 SRM 51-40-05 & 51-40-02.SDR ASAA11410347Unknown · malfunctionedL1 DOOR HARD TO OPEN FLIGHT ATTENDANT STATED DOOR WAS HARD TO SWING OPEN & CLOSED. PERFORMED GVI OF HINGES & SNUBBER PERFORMED FWD ENTRY DOOR TEST PER MM 51 11 00, NO DEFECTS NOTED DOOR MOVED SMOOTHLY & SNUBBER OPS NORMAL.SDR ASAA11410343Panel · crackedNR 6 FLAP TRACK FAIRING I/B PANEL CRACKED ABOVE UPPER FORWARD SCREW (NR 2 PYLON). REPLACED NR 2 PYLON PANEL.SDR ASAA11410316Battery · dischargedRT AFT AND R2 DOOR EMERGENCY LTS INOP ON TEST. REPLACED BATT M1137, OPS CHECK NORMAL.SDR ASAA11410275Battery Pack · dischargedEMERGENCY LIGHTS INOP: CENTER AISLE OVERHEAD AT WING EXITS BULLNOSE RT/SIDE ROW 20, 24, 27. R2 DOOR LT ABOVE DOOR AND EXIT R2 DOOR EXTERNAL SLIDE LIGHT. REPLACED BATTERY PACK AND CHARGER AT STATION/LOCATION M1134 AND M1197 REF AMM 33 50 00, OPS GOOD.SDR ASAA11410289Shear Tie · corrodedFORWARD CARGO SHEAR TIE AT STA 500 BETWEEN STR 28L AND 28R CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.SDR ASAA11410288Shear Tie · corrodedFORWARD CARGO SHEAR TIE AT STA 500A BETWEEN STR 27R AND 28R CORRODED. BLENDED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PART IAW B737 400 SRM 53 00 07.SDR ASAA11410285Shear Tie · corrodedFORWARD CARGO SHEAR TIE AT STA 500B BETWEEN STR 28L AND 27L CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PART IAW B737 400 SRM 53 00 07.SDR ASAA11410213Light · inoperativeEMERGENCY LIGHT EXIT LOCATOR SIGNS AT L1 DOOR RIGHT FORWARD OVERWING EXIT AND RIGHT AFT OVERWING EXIT EACH HAVE MULTIPLE LAMPS INOP. RELAMPED EMERGENCY LIGHT EXIT IDENTIFIERS AT L1 DOOR RT FWD AND RT AFT OVERWING EXITS AND TESTED PER MM 33 51 81 962 011, OPS SDR ASAA11410159Engine · surgesALMOST TO TOP OF CLIMB (18 MIN INTO FLIGHT) BOTH PILOTS HEARD AN ENGINE SURGE NR 1 N1 99% NR 2 N1 96%. NR 1 N1 CAME RIGHT DOWN TO 96%. ON APPROACH HAD A ONE THROTTLE KNOB WIDTH TO MATCH POWER (31 ENGINE THROTTLE BACK TO MATCH) SURGE WAS VERY NOTICABLE IN PAX
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