Boeing 737-3B7
Service difficulty reports · 4,722
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 = '7373B7' 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 = '7373B7' 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 SB04136Shutoff Valve · faultyENROUTE, AIRCRAFT EXPERIENCED A PNEUMATIC DUCT PRESSURE SPLIT OF 46 PSI RT AND 6 PSI LT. WHEN LT BLEED IS TURNED OFF, LT PRESSURE EQUALS RT AT APPROXIMATELY 36 PSI. ALTITUDE WARNING HORN SOUNDED AS CABIN GRADUALLY ASCENDED THROUGH 10,000 FEET. FLIGHT DESCENDESDR SB04134Battery Pack · dischargedBOS - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY LIGHTS, AT SEAT ROWS 17 THROUGH 20, WOULD ILLUMINATE AND THEN QUICKLY EXTINGUISH. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT CABIN. OPERATIONAL CHECK GOOD.SDR USAA040788Keelbeam · corrodedPIT Q5, KEEL BEAM, 2 INCHES X 40 INCHES AREA CORROSION; LEVEL 1 TASK NR C53-208-01, L KEEL BEAM STA 500D-540. REMOVED AND REPLACED, SPLICED IN NEW SECTION IAW TYP REP 53-60-09.SDR USAA040648Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCH, STATION 870, .5 INCH BELOW STRINGER 23R. INSTALLED DOUBLER IAW SRM 53-00-01. (M)SDR USAA040655Doubler · crackedPIT - FOUND DOUBLER AND SKIN CRACKED .75 INCH LONG, OPENING FOR ACCESS PANEL 5727L, LEFT PYLON NACELLE STATION 180 OUTBOARD SIDE. DOUBLER INSTALLED PER TYPICAL REPAIR 54-30-07. (M)SDR USAA040653Beltframe · crackedPIT - FOUND BELTFRAME CRACKED .125 INCH, IN FRAME AT FS 767 LOWER OVERHEAD BIN ATTACH POINT, RIGHT SIDE. INSTALLED REPAIR ANGLES 1 AND 2 PER TYPICAL REPAIR 53-10-20A. (M)SDR USAA040652Window Frame · crackedPIT - FOUND WINDOW FRAME CRACKED .25 INCH, UPPER OUTBOARD CORNER OF CAPTAIN WINDOW FRAME. REMOVED DAMAGE, DOUBLER INSTALLED PER SRM 53-10-01. (M)SDR USAA040646Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, STATION 945.5, .5 INCH ABOVE STRINGER 24R. INSTALLED DOUBLER IAW 53-00-01 FIG 229. (M)SDR USAA040802Skin · crackedPIT, Q5, SKIN, 6 INCH CRACK, RT PYLON LOWER PAN FROM NAC 319 AFT TO END. REMOVED AND REPLACED SKIN AND INSTALLED DOUBLER IAW SRM 51-70-13.SDR USAA040707Support Angle · corrodedSUPPORT ZEE ANGLE, .2500 INCH BY .1250 INCH AREA, CORROSION; LEVEL; TASK C53-202-1; BS 727A TO 787 AT AFT CARGO S-25R.SDR USAA040706Fitting · corrodedPIT - Q2, R-1 LUG .1250 BY .2500 INCH AREA, CORROSION; NO LEVEL OR TASK, RT HORIZ STAB R-1 LUG. CLEANED CORROSION, REMOVED AND REPLACED BUSHING, CAB PLATED IAW SRM 55-10-10, NDTM 0-4-53-10.SDR USAA040705Floor Support · corrodedPIT,Q2, FLOOR SUPPORT .1250 INCH X .2500 INCH AREA, CORROSION, LEVEL 1; TASK NR C53-107-02. FLOOR SUPPORT, BETWEEN STA 312 AND 344, APPROX. 10 INCHES LT OF CENTER. CLEANED, TREATED, PRIMED AND REPLACED FLOOR SUPPORT IAW SRM 53-10-06B.SDR USAA040677Anchor Fitting · corrodedANCHOR FITTINGS; CORROSION; LEVEL 1; TASK NR C53-107-02, ANCHOR FITTINGS AT STA 993R. REPLACED FITTINGS IAW SRM 51-10-2.SDR USAA040657Floor Support · crackedPIT - FOUND FLOOR SUPPORT HAS TWO CRACKS .25 INCH, NR 6 SLAT BOARD, 1 AT 4 INCH AND 1 AT 5 INCH OUTBOARD OF DEICING TUBE, 1 AT 5 INCH. CLEANED, TREATED AND PRIMED, REPLACED FLOOR SUPPORT. (M)SDR USAA040654Attach Angle · crackedPIT - FOUND ATTACH ANGLE CRACKED 1 INCH LONG, BS 538, STRINGER 22, PACK RAM AIR INLET AREA. FABRICATED AND INSTALLED REPAIR ANGLES PER TR 53-50-03. (M)SDR USAA040631Skin · crackedCLT - FOUND SKIN CRACKED 2.25 INCH, .5 INCH ABOVE STRINGER 25R SKIN LAP AT STATION 764. INSTALLED DOUBLER/TRIPLER AND FILLER PER SRM 53-00-01 FIG 229. (M)SDR USAA040635Rib · crackedPIT - FOUND RIB CRACKED .5 INCH, RIGHT WING AT RIB STATION 135.5, LOWER CHORD. DOUBLER INSTALLED PER EA 79058. (M)SDR DL733040901Controller · failedPASSING FL280 DEPARTING SFO HAD INERMITTENT FWD CARGO FIRE WARNING (BELL & LIGHT). BOTTLES FIRED. VERIFIED NO FIRE. REPLACED FIRE DETECTION CONTROLLER.SDR SB04125Socket · disconnectedMAINTENANCE REPORTED THE FLOOR EMERGENCY LIGHT AT SEAT ROW 22C WAS INOPERATIVE AND NOT CONNECTED TO THE SEAT. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET AT SEAT ROW 22C. OPERATIONAL CHECK GOOD.SDR SB04126Battery Pack · dischargedCLT - MAINTENANCE REPORTED THE SEAT MOUNTED AND BULL NOSE EMERGENCY ESCAPE PATH LIGHTING, IN THE MID-CABIN, INOPERATIVE. MAINTENANCE TROUBLESHOT PROBLEM TO THE MID-CABIN BATTERY PACKS. REMOVED AND REPLACED MID-CABIN BATTERY PACKS. OPERATIONAL CHECK GOOD.SDR USAA040645Keelbeam · wornPIT - FOUND KEEL BEAM .1875 INCH DIAMETER METAL WEAR AROUND FASTENER HOLES, L/N KEEL BEAM LOWER FLANGE BETWEEN BS 704-727. DOUBLER STRAP INSTALLED PER EA 79006. (M)SDR USAA040644Keelbeam · wornPIT - FOUND KEEL BEAM WITH DEEP METAL WEAR .1875 INCH AT FASTENER HOLES, KEEL BEAM LOEWR FLANGE BETWEEN BS 727-704. INSTALLED STRAP DOUBLER PER EA 79007. (M)SDR USAA040658Spar · crackedPIT - FOUND UPPER CHORD CRACKED MORE THAN .343, BUT LESS THAN .6285, NR 2 HOLE, LEFT REAR SPAR UPPER CHORD AT RSS 224.14. OVERSIZED HOLE, INSTALLED FILLER, INSTALLED WING SKIN DOUBLER PER EA 78987. (M)SDR USAA040656Fitting · crackedPIT - FOUND FITTING CRACKED .5 INCH, RT MLG SUPPORT FITTING NR 2 HOLE 5:30 POSITION. REPLACED RT MLG SUPPORT FITTING AND INSTALLED UPPER WING CHORD DOUBLER PER EO 5702V054, EA 78985 AND 78986. (M)SDR USAA040781Intercostal · damagedPIT, Q5, INTERCOSTAL, HOLE DAMAGE. LIGHTENING HOLE DAMAGE, STA 294.5 + 312 LBL 10 INCH INTERCOSTAL FLOORBEAM LIGHTENING HOLE DAMAGE. FABRICATED WEB AND INSTALLED SAME IAW 53-10-51, FIG 1, PG 17.SDR USAA040651Fitting · crackedPIT - FOUND CORNER FITTING CRACKED 5 INCHES, RIGHT TOP CORNER FITTING INSIDE HORIZ STAB INTERSECTING, PRIMARY AND THRUST BEAM. REPLACED ANGLE PER SRM 51-40-02. (M)SDR USAA040650Stringer · crackedPIT - FOUND STRINGER CRACKED 2 INCHES, STRINGER 20L, STATION 727D. DOUBLER AND TRIPLER REPAIR DOUBLERS PER SRM 53-00-01 FIG 228. (M)SDR USAA040649Skin · tornPIT - FOUND SKIN TEAR, .5 INCH ALONG 1.75 INCH OF DOOR, RIGHT AFT SERVICE DOOR OUTSIDE SKIN FORWARD SIDE EDGE FORWARD OF HANDLE. REPAIRED PER SRM 52-00-01. (M)SDR SB04124Light · unsecurePHL - PILOT REPORTED THE EMERGENCY EXIT LIGHTS ON SEAT 10A INOPERATIVE. MAINTENANCE SECURED THE EMERGENCY EXIT LIGHTS ON SEAT 10A. OPERATIONAL CHECK GOOD.SDR USAA040792Angle · corrodedPIT, Q5, KEEP REPAIR ANGLE, 20 INCH AREA, CORROSION; LEVEL 1; TASK NR C 53-208-01 R KEEL STA 520-540. INSTALLED NEW REPAIR ANGLE/ DOUBLER IAW SRM 51-70-11.SDR USAA040709Skin Panel · crackedUNSCHEDULED MAINTENANCE, KEEL BEAM SKIN PANEL, 3 INCH CRACK, BS 690 KEEL BEAM PANEL. INSTALLED DOUBLER (TEMP REPAIR) IAW SRM 53-60-12, FIG 202.SDR USAA040647Web · corrodedPIT - FOUND WEB CORRODED BETWEEN STATION 794 TO 847, BETWEEN STATION 794 TO 847. WEB AND STRAP REPLACEMENT ON AIR CARGO DOOR SILL PER DWG 65-47957. (M)SDR USAA040805Door Frame · crackedPIT, Q5, WEB FRAME, 3 INCH CRACK AT FWD ENTRY DOOR LOWER WEB FRAME FORWARD CORNER. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 52-10-02 FIG 1, SRM 51-70-11 FIG 1.SDR USAA040787Floor Support · corrodedPIT, Q5, FLOOR SUPPORT, 4 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02 FLOOR SUPPORT, STA 986.5 RT BL0. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 53-60-51.SDR USAA040797Angle · corrodedPIT, Q5, Z-ANGLE, 4 INCHES LONG, CORROSION; LEVEL 1 TASK NR C53-107-01 AFT ENT DOOR Z-ANGLE. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG.SDR USAA040824Keelbeam · crackedPIT - Q5, KEEL REPAIR ANGLE, .2500 INCH CRACK, FASTENER HOLE, STA 520 ON KEELBEAM REPAIR ANGLE RT. REPAIR ANGLES/DOUBLER INSTALLED IAW SRM 51-70-11.SDR USAASB04122Power Supply · failedPIT - FOUND MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 17 THROUGH 21 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK, P/N 2013-1A FOR AFFECTED SEAT ROWS. OPERATIONAL CHECK GOOD. (M)SDR USAA040803Skin · delaminatedPIT, Q5, TOP SKIN AND CORE BOND, 3.5 INCH AREA. DELAMINATION, NR 4 SLAT OB END TOP SURFACE. REMOVED DAMAGE, INSTALLED NEW CORE SECTION AND DOUBLER IAW SRM 51-70-10.SDR USAA040804Skin · delaminatedPIT, Q5, TOP SKIN - CORE BOND 1 INCH AREA, DELAMINATION, LT WING NR 1 SPOILER AT AFT OB CORNER - TOP SURFACE. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10.SDR USAA040808Skin · delaminatedPIT, O5, TOP SKIN- CORE BOND, 2 INCH AREA. NR 4 SLAT IB END TOP SURFACE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE AND DOUBLER IAW SRM 51-70-10.SDR USAA040702Structure · wornRUDDER, 1 INCH LENGTH, WEAR WITH KNIFE EDGING, LOWER TR EDGE. SCALED DAMAGE IAW EA79025.SDR USAA040638Skin · chafedPIT - FOUND RUDDER COMPOSITE CHAFED 1 INCH BY .125 INCH, RUDDER LOEWR LEFT EDGE 9.5 INCHES FROM TRAILING EDGE. INSTALLED REPAIR PLYS, REINSTALLED HARDWARE AND REFINISHED PER SRM 51-70-17 AND EA 79025. (M)SDR USAA040662Skin · chafedPIT - FOUND RUDDER WITH CHAFE MARKS .25 INCH BY .20 INCH, STATION 174 AT LEFT LEADING EDGE. REMOVED DAMAGE AND APPLIED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M)SDR USAA040661Skin · damagedPIT - FOUND RUDDER WITH COMPOSITE DAMAGE 4 INCH BY 5 INCH SINGLE LAYER, STATION 170 PLUS 10 INCHES FROM T/E RT SIDE. REMOVED DAMAGE AND INSTALLED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M)SDR USAA040660Skin · damagedPIT - FOUND RUDDER WITH COMPOSITE DAMAGE 5.25 INCH BY 1.5 INCH SINGLE LAYER, STATION 180 PLUS 10 INCHES FROM T/E RT SIDE. REMOVED DAMAGE AND INSTALLED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M)SDR USAA040659Structure · crackedPIT - FOUND RUDDER CRACKED 1 INCH WITH DELAMINATION, LOWER LEFT LEADING EDGE. REMOVED DAMAGE, INSTALLED REPAIR PLYS PER EA 79025, SRM 51-70-17. (M)SDR USAA040807Spar · crackedPIT, Q5, ANGLE SUPPORT .7500 INCH CRACK, VERT STAB SPAR ANGLE FOR RIB 163.90 FRONT LT SIDE. INSTALLED DOUBLER AND SHIM IAW EA 79100.SDR USAA040806Skin · debondedPIT, Q5, TOP SKIN - CORE BOND, 3 INCH X 3 INCH AREA, DEBONDED. LT IB AFT FLAP, UPPER OB T/E. REMOVED DAMAGE, INSTALLED CORE, DOUBLER IAW TR 57-53-01A, EA 79082, SRM 51-70-10.SDR USAA040700Support Angle · corrodedANGLE SUPPORT, .1250 INCH X .1250 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-202-01, BS 794, S-25R. REPLACED ANGLE IAW SRM 51-40-02.SDR USAASB04119Battery Pack · inoperativePIT - MAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK, IN FORWARD GALLEY OVERHEAD, HAS LOW CHARGE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)
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