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 USAA051259Intercostal · corrodedFOUND INTERCOSTAL CORRODED, BS 328-344 RBL 12. REMOVED CORROSION AND TREATED IAW SRM 53-10-51-1A-1, DEFECT SIZE: .25".SDR SB05140Wire · brokenCLT - PILOT REPORTED THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 5, 9 AND 11 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND REMOVED AND REPLACED LOW LEVEL LAMP AT SEAT ROW 5, LEFT SIDE. OPERATIONAL CHECK OF LIGHTS GOOD.SDR SB05138Outflow Valve · faultyBWI - FLT1243 - DURING CRUISE, CREW REPORTED A LOUD BUZZING NOISE COMING FROM CABIN AND ALMOST INSTANTLY FELT PRESSURE IN THEIR EARS. CREW FOUND CABIN PRESSURE CLIMBING 3,000 TO 4,000 FT PER MINUTE. OUTFLOW VALVE WAS CLOSED PER PROCEDURES WITH NO AFFECT ON PSDR USAA051249Crease Beam · corrodedFOUND CORROSION TOP SURFACE OF S-17L CREASE BEAM WEB; BETWEEN BS 727B AND 727C. REMOVED FASTENERS IN AREA, REMOVED SURF CORROSION, TREATED AND PRIMED, INSTALLED FASTENERS IAW SRM 53-60-13, DEFECT SIZE: 2" BY 1" BY 0.002" CORRODED AREA.SDR SB05136Selector Panel · sticksDURING CRUISE, AT FL350, NOTICED CABIN ALT STARTED TO CLIMB. CREW DONNED OXYGEN MASKS & STARTED DESCENT. PAX O2 MASKS DROPPED AT FL140. STANDBY PRESSURIZATION DID NOT WORK, F/O SWITCHED TO MANUAL. AFTER CABIN ALT RESTORED, F/O SWITCHED BACK TO STANDBY & ISDR SB05135Wire · damagedMAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT 14ABC INOPERATIVE. MAINTENANCE REPAIRED THE WIRING AT SEAT 14ABC. OPERATIONAL CHECK GOOD.SDR USAA051212Skin · crackedIN LOWER SKIN OF NR 5 SLAT AT RIVET, ADJACENT TO SLAT ACTUATOR CRACKED. INSTALLED A 30.25 X 3.75 INCH REPAIR DOUBLER ON LOWER SKIN AT CENTER OF SLAT, IAW 57-43-01, DEFECT SIZE: .250 INCH.SDR USAA200510002Skin · crackedA 1.375 INCH CRACK FOUND AT STA 727E AT STRINGER 21 LEFT. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 201.SDR SB05133Battery Pack · dischargedCLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT POWER SOURCE BATTERY WAS WEAK IN THE FORWARD CABIN. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN BATTERY PACK. OPERATIONAL CHECK GOOD.SDR SB05132Connector · damagedCLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS AT THE FORWARD ENTRY AND SERVICE DOORS AND SEAT ROWS 1 THROUGH 4 WERE INOPERATIVE. MAINTENANCE FOUND 2 PINS BACKED OUT OF CONNECTOR D9021J. REMOVED AND REPLACED CONNECTOR. ALSO, FOUND FORWARD ENTRY DOOR ISDR AWXA200501241Skin · damagedFLT 391 - CREW DISCOVERED DAMAGE TO TAIL SECTION DURING POST FLT INSPECTION. DAMAGE IS BELIEVED TO BE DUE TO TAIL STRIKE ON PREVIOUS TAKE OFF. MX R & R AFT BELLY SKIN FROM BS 908-1016 AND FROM STR 25L-25R IAW BOEING 737-300 SMR 51-40-02. REMOVED, FABED & INSSDR AWXA200600254Door · damagedPHX - DISCOVERED PREVIOUS BLEND OUT AT STA 1088, ABOVE THE FORWARD RT CORNER OF THE APU DOOR. WAS DETERMINED TO BE CHAFFING DAMAGE ABOUT 6" AFT OF STA 1088 AT STR 20R. DEEP BLENDED OUT AREA WAS NOT COVERED IN THE BOEING 737-300 SRM. MAINTENANCE CLEANED AND SDR SB05128Actuator · faultyPHL - FLT1243 - ON APPROACH TO PHL, WHEN AUTO PILOT WAS MANUALLY DISCONNECTED AT 1,000 FT AGL, THE AIRCRAFT ROLLED TO THE LEFT. AILERON TRIM SYSTEM WAS FOUND TO BE INTERMITTENT. BOTH THE CAPTAIN AND FIRST OFFICER WERE REQUIRED TO REGAIN LEVEL FLIGHT. CREW NSDR AWXA200501188Skin · crackedPHX - FLT 289 - ON GROUND IN PHX, REPORTED POSSIBLE TAIL STRIKE. MAINTENANCE DISCOVERED FUSELAGE CRACK 1 INCH LONG AT STATION 727D STRINGER S-23L AND AFT GALLEY DRAIN MAST DAMAGED. MAINTENANCE REMOVED DAMAGED AREA AT BS 727D AND BS 996 IAW BOEING 737-300 SRMSDR USAA051170Skin · crackedFOUND FUSELAGE STATION 727, STRINGER 22L CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 DETAIL X DEFECT SIZE: 1.5".SDR SB05120Outflow Valve · failedEN ROUTE AT CRUISE, CREW NOTICED PRESSURIZATION CHANGE AS CABIN CLIMBED AT 2,000 FPM. NO LIGHTS, NO WARNING AND NO OBVIOUS REASON FOR PROBLEM. PACKS OPERATING NORMALLY & HIGH MODE HAD NO EFFECT. CREW INITIATED DESCENT & CABIN REACHED A MAX OF ABOUT 8,000 FTSDR SB05119Adc · failedCLT FLT448 ON TAKEOFF ROLL, WITH FIRST OFFICER FLYING, THE FIRST OFFICER LOST AIRSPEED INDICATOR, ALTIMETER AND VERTICAL SPEED. AFTER TRANSFER OF CONTROLS TO CAPTAIN, THE FLIGHT RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DESDR AWXA200501089Battery · inoperativePHX - EEL - CREW REPORTED TO MAINTENANCE THE FORWARD GALLEY FLASH LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200501093Terminal Block · inoperativeLAS - DIVERSION - FLT 0282 - DURING CRUISE, EN ROUTE TO SJC, CREW REPORTED THE NR 2 ENGINE EGT WAS FLUCTUATING IN CRUISE WITH ALL OTHER ENGINE PARAMETERS BEING NORMAL. AIRCRAFT DIVERTED INTO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLASDR SB05116Bracket · missingORD - PILOT REPORTED MISSING HARDWARE FOR THE FORWARD BRACKET OF THE R2 SERVICE DOOR ESCAPE SLIDE. MAINTENANCE REPLACED MISSING HARDWARE FOR THE FORWARD BRACKET OF THE R2 SERVICE DOOR ESCAPE SLIDE.SDR USAA051066Skin · crackedCRACK IN FUSELAGE SKIN BS 754, S25L. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER PER SRM 53-00-01 FIG 249. DEFECT SIZE: 4.5 INCH CRACK IN FUSELAGE SKIN.SDR USAA051067Skin · cracked15.5 INCHES AFT OF BS 727D, S23L (2) 16.5 INCHES AFT OF BS 727D, S-22L, REMOVED DAMAGE, FAB AND INST DOUBLER, INC 2 CRACKS AND 2 PREEX REPAIRS TO 1 DOUBLER REP IAW 53-00-01 FIG 201. DEFECT SIZE: (1) 15.5 INCHES AFT OF BS 727D, S-23-L, (2) 16.5 INCHES AFT OF BSDR SB05106Battery Pack · dischargedCLT - MAINTENANCE REPORTED THE FORWARD RIGHT EMERGENCY LIGHT AT THE SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.SDR USAA200508004Skin · crackedCRACK AT BS867 JUST BELOW S-23R. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01 FIG 201, DETAIL X.SDR USAA051063Skin · chafedLOCATION: BS 869- BS 887 ACTION: REMOVED DAMAGE, INSTALLED TRIPLER IAW EA 96764 DEFECT SIZE: APPX 18 INCH AREA OF CHAFING ON SKIN BELOW DORSAL FIN TIP CONTACT AREA, BOTH SIDESSDR SB05101Warning Light · false indicationCLT - UPON LOWERING LANDING GEAR, CREW RECEIVED A GEAR INDICATION OF 3 GREEN AND 3 RED. CREW ACCOMPLISHED A GO-AROUND, CYCLED THE GEAR AND RECEIVED A NORMAL GEAR INDICATION OF 3 GREEN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE JACKED AIRCRAFT AND SDR USAA051062Keelbeam · corrodedSTA 520 S-28/KEEL BEAM. REMOVED DAMAGED, INSTALL FILLERS, SHIMS AND REPAIR ANGLE IAW EA 96839, DEFECT SIZE: 1 X 3.SDR SB05099Socket · failedMAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 15L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET. OPERATIONAL CHECK GOOD.SDR USAA051054Skin · crackedCLT - FOUND SKIN CRACKED 12 INCHES, IMMEDIATELY AFT OF SLAT ACTUATOR. REMOVED DAMAGE AND INSTALLED SPACER AND DOUBLER IAW SRM 57-43-01. (M)SDR USAA051053Wedge · dentedCLT - FOUND WEDGE WITH DENT 4 INCH BY 5 INCH, BOTTOM OF THE WEDGE AT THE OUTBOARD TRAILING EDGE. REMOVED DAMAGE, INSTALLED A NEW CORE AND DOUBLER IAW EA 96745. (M)SDR USAA051052Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, OUTBOARD LOWER SKIN OF NR 6 SLAT. INSTALLED DOUBLER IAW SRM 57-43-01. (M)SDR SB05098Battery Pack · dischargedPIT - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 11-16, LEFT-HAND SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.SDR SB05097Charger · inoperativeMAINTENANCE REPORTED THE BATTERY CHARGER FOR THE AFT ENTRY DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD.SDR USAA051030Skin · damagedCLT - Q6 - PYLON SKIN, 1.3 INCH, GROOVE IB SIDE OF NR 2 ENGINE PYLON AT WING L/E JUNCTION. REPAIRED IAW TYPICAL REPAIR IAW TR. (K)SDR SB05095Light · brokenCLT - THE AISLE EMERGENCY EXIT LIGHT WAS FOUND BROKEN. MAINTENANCE REPLACED THE EMERGENCY EXIT IDENTIFIER AND A FUSE IN THE BATTERY PACK. OPERATIONALLY CHECKS OK.SDR USAA051011Keelbeam · wornCLT - FOUND CHORD WITH 60 INCHES OF WEAR, KEEL BEAM LEFT OUTBOARD FLANGE STATION 664-727. REMOVED DAMAGED AREAS, FABRICATED AND INSTALLED FILLER PLUGS IAW EA 96777.SDR USAA051010Support Beam · corrodedCLT - Q6 - LT MLG SUPPORT BEAM OB LUG FACE AND HEAVY WEAR/ MATERIAL LOSS ON IB LUG FACE 2 INCH X 2 INCH TYPICAL. LT MLG SUPPORT BEAM; STABILIZER BEAM FITTING ASSY. CLEANED AND TREATED CORROSION, INSTALLED BUSHINGS IAW SRM. (K)SDR USAA051009Keelbeam · corrodedCLT - Q6 - ANGLE, ON KEELBEAM COMPOSITE SKIN ATTACH ANGLE HAS FRETTING WORN INTO IT, 5 INCHES X 1 INCH. CORROSION, STA 673, STA 678, LBL 8. REMOVED CORROSION, BLENDED, AND TREATED IAW SRM, DWG. (K)SDR USAA051008Angle · corrodedCLT - Q6 - ANGLE, KEEL BEAM HAS FRETTING WEAR ON IT 17 IN X 1 INCH, CORRODED, STA 727-710, LBL 8. REMOVED SURF CORROSION, BLENDED AND TREATED IAW SRM, DWG. (K)SDR USAA051000Channel · corrodedCLT - FOUND HAT SECTION CHANNEL CORRODED 6 INCH AREA, STATION 500-500A, BL 0. REMOVED DAMAGED HAT SECTION, REMOVED LIGHT SURFACE CORROSION INSTALLED NEW HAT SECTION CHANNEL. (M)SDR USAA051001Shear Tie · corrodedCLT - FOUND SHEAR TIE CORRODED .5 INCH BY 2 INCH, RBL 3, BETWEEN BS 727A AND 727B FRAMES AFT CARGO AREA. CORROSION LEVEL 1. DEFECTIVE PART REPLACED WITH IDENTICAL PART, IAW BOEING DWG 69-40710 AND SRM 51-10-02. (M)SDR USAA051002Stringer · crackedCLT - FOUND STRINGER .5 INCH CRACK, FUSELAGE STATION 500A STRINGER 8L. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-00-03 FIG 203. (M)SDR USAA051006Skin · crackedCLT - Q6 - SKIN, 1.50 INCH CRACK. 1.25 INCH FWD OF REAR SPAR, SPAR STA 124 TO 55-123.6. HORIZONTAL STABILIZER. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW EA. (K)SDR USAA051005Skin · crackedCLT - Q6 - LOWER SKIN, 1.7 INCH CRACK LOWER SKIN APPROX STAB STA 129 AT AFT SPAR, HORIZONTAL STAB. REPAIRED AND INSTALLED DOUBLER AND FILLER IAW EA. (K)SDR USAA200508003Skin · crackedA 2 INCH CRACK BETWEEN BS 753.5 & BS 755.5 AT S-21R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201 REPAIR 31.SDR SB05093Battery Pack · dischargedCLT - MAINTENANCE REPORTED THE AFT LEFT-HAND INTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT STATION 753L. OPERATIONAL CHECK GOOD.SDR SB05091Odor · detectedDCA FLT1285 DUE TO AN INOPERATIVE APU, A GROUND AIRSTART WAS ACCOMPLISHED PRIOR TO DEPARTURE IN SYR. AN OBNOXIOUS ODOR BECAME PRESENT IN THE COCKPIT AND CABIN SHORTLY THEREAFTER. AFTER DEPARTURE, THE CAPTAIN SENT AN ACAR'S MESSAGE STATING THE ODOR CLEARED SDR USAA050996Skin · crackedCLT - FOUND SKIN CRACKED 1.75 INCH, FS 727, STRINGER 20L. INSTALLED DOUBLER AND TRIPLER AND FILLERS IAW SRM 53-00-01 FIG 201. (M)SDR USAA050994Skin · dentedCLT - FOUND SKIN DENTED 5 INCHES LONG, .0200 INCHES WIDE AND .002 INCHES DEEP, FUSELAGE STATION 328 BETWEEN STRINGERS 20 AND 21 LEFT. INSTALLED DOUBLER AND TRIPLER IAW SRM 53-00-01 FIG 201. (M)SDR USAA050990Support · crackedCLT, Q6, PSU SUPPORT RAIL, 2 CRACKS, .1250 INCH, .1875 INCH, CRACK, BS 727D BETWEEN S8L AND 9L. DAMAGE REMOVED, INSTALLED REPAIR ANGLES IAW SRM. (K)
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