Boeing 737-3S3
Service difficulty reports · 1,209
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 = '7373S3' 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 = '7373S3' 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 AWXA200601778Floorbeam · crackedMCN - MAJOR REPAIR - MAIN CABIN LONGITUDINAL FLOORBEAM UPPER TEE CRACKED, BS 663, BS 666.5, BS 670.5 AND BS 677, LBL 24.5, WL 208.1. REPAIRED MAIN CABIN LONGITUDINAL FLOORBEAM UPPER TEE, BS 663, BS 666.5, BS 670.5 AND BS 677, LBL 24.5, WL 208.1 IAW AWA ER 03-SDR AWXA200601777Connector · brokenMCN - EEL - EMERGENCY ESCAPE PATH LEFT HARNESS HAS NUMEROUS CONNECTORS DAMAGED AND MISSING PINS. REPLACED CONNECTORS AND INSTALLED PINS ON THE LEFT EMERGENCY ESCAPE PATH HARNESS IAW BSWPM 20-42-01, 20-30-12 AND 20-90-14.SDR AWXA200601779Wire · shortedSAN - EEL - INTERIOR EMERGENCY LIGHTS LEFT SIDE ROW 12 THROUGH 18 ARE INOP. FOUND SHORTED WIRE UNDER SEAT 17A. REMOVED AND REPLACED SHORTED SECTION OF WIRE. OPS CHECK WAS GOOD.SDR AWXA200601706Skin · crackedMCM - THREE CRACKS, BOTTOM NR 4 SLAT SKIN, SLAT STA 71.4 TO 74. REPAIRED BOTTOM OF NR 4 SLAT SKIN STA 71.4 TO 74 IAW B737-300 SRM 57-43-01-2R6 FIG 201.SDR AWXA200601713Skin · crackedPHX-MAJOR REPAIR-4DAY CHECK-NR 4057771, LT FUSELAGE AFT OF WTB 8 IN. AFT OF PREVIOUS CRACK HAS ANOTHER CRACK AT STA 782 STR. 25L AT LAP JOINT. REPAIRED LT FUSELAGE AFT OF WTB AT LWR LAP SEAM STA 782 STR.25L IN REF TO SRM53-00-01 2R FIG201. SEE AWXA200601712 FSDR AWXA200601712Skin · crackedPHX-MAJOR REPAIR-4DAY CHECK-NR 4057770, LT FUSELAGE AFT OF WTB AT LWR LAP SEAM HAS A CRACK AT STA 774 STR 25L AT LAP JOINT. REPAIRED LT FUSELAGE AFT OF WTB LAP SEAM STA774 STR25L IN REF TO SRM53-00-01-2R FIG201.SDR AWXA200601711Skin · crackedMAJOR REPAIR-4DAY CHECK-NR 4057772, RT FUSELAGE AFT OF AFT CARGO DOOR HAS A CRACK (MARKED) AT STA 867 AND STR 23R. INSTALLED REPAIR DOUBLER RT FUSELAGE AFT OF AFT CARGO DOOR STA 867 STR 23R IAW SRM 53-00-01-2R 31 FIG 201 SHT 32.SDR AWXA200601761Angle · crackedCRACKED FLOOR STABILIZER UPPER ATTACH ANGLE, BS 500D- BS 520, BL 0. REPLACED FLOOR STABILIZER UPPER ATTACH ANGLE, BS 500D - BS 520, BL 0 IAW SRM 51-40-02-0G FIG 8 AND 51-40-02, FIGS 12 AND 14.SDR AWXA200601817Floorbeam · crackedMCN - MAJOR REPAIR - C-19 CHECK - FOUND CLIP CRACKED, OUTBOARD SIDE OF FLOORBEAM, BS 683.25, LBL 0.07, WL 208.1. REPLACED CLIP, OUTBOARD SIDE OF FLOORBEAM, BS 683.25, LBL 0.07, WL 208.1 IAW AWA ER 03-5360-06296-SS2.SDR AWXA200601809Crease Beam · crackedMCN - MAJOR REPAIR - LEFT CREASE BEAM CRACKED, BS 617.5, LBL 64.53, WL 208.1. REPAIRED LEFT CREASEBEAM, BS 617.5, LBL 64.53, WL 208.1 IAW AWA ER 03-5361-06297-SS1.SDR AWXA200601760Crease Beam · corrodedCRACK AT LT CREASE BEAM SHEAR WEB, BS 617.5, LBL 64.53, WL 208.1. REPLACED LT CREASE BEAM SHEAR WEB, BS 617.5, LBL 64.53, WL 208.1 IAW SRM 51-40-02-0G PAR 4 PG 1 AND 2 FIGURES 3, 6, 7 AND 8 AND DWG 65-47973 SHEETS 6 AND 57.SDR AWXA200601759Frame · corrodedCORROSION ON AFT CARGO COMPARTMENT FRAME, BS 827 BETWEEN LBL 3.00 AND RBL 3.00. REPAIRED AFT CARGO COMPARTMENT FRAME, BS 827 BETWEEN LBL 3.00 AND RBL 3.00 IAW SRM 53-00-07-2R 5 FIG 201.SDR AWXA200601812Frame · crackedMCN - MAJOR REPAIR - FORWARD CARGO COMPARTMENT DOOR OPENING FORWARD FRAME WEB CRACKED, BS 440, S24R. REPAIRED FORWARD CARGO COMPARTMENT DOOR OPENING FORWARD FRAME WEB, BS 440, S24R IAW AWA ER 03-5332-06293-ES4.SDR AWXA200601811Skin Panel · crackedMCN - MAJOR REPAIR - FUSELAGE SKIN CRACKED, BS 792, S25R. REPAIRED FUSELAGE SKIN, BS 792, S25R IAW AWA ER 03-5361-06293-ES1.SDR AWXA200601810Frame · crackedMCN - MAJOR REPAIR - FORWARD CARGO COMPARTMENT DOOR OPENING AFT FRAME WEB CRACKED, BS 492.3, S24R. REPAIRED FORWARD CARGO COMPARTMENT DOOR OPENING AFT FRAME WEB, BS 492.3, S24R IAW AWA ER 03-5332-06293-ES3.SDR AWXA200601781Skin · debondedMCN - MAJOR REPAIR - LEFT HORIZONTAL STABILIZER O/B TRAILING EDGE DISBONDED FROM TIP FAIRING TO O/B END OF ELEVATOR, STAB STATION 295.10 - 149.12. REPAIRED LEFT HORIZONTAL STABILIZER O/B TRAILING EDGE DISBONDED FROM TIP FAIRING TO O/B END OF ELEVATOR, STAB SSDR AWXA200601762Skin · debondedNR 4 SPOILER UPPER SURFACE HAS A DISBONDED AREA 55 INCHES FROM OB END. REPAIRED NR 4 SPOILER UPPER SURFACE IAW SRM 51-70-10-2R4, REPAIR 4, FIGURE 201.SDR AWXA200601741Skin · delaminatedMCN - MAJOR REPAIR - C-19 CHECK - RIGHT ELEVATOR UPPER SURFACE DELAMINATED, 32 INCHES FROM OUTBOARD END, ELEVATOR STA 181. REPAIRED RIGHT ELEVATOR UPPER SURFACE 32 INCHES FROM OUTBOARD END IAW 737-300 SRM 51-70-04-0G REPAIR 1 FIGURE 10.SDR AWXA200601807Stringer · crackedMCN - FOUND LEFT STRINGER 18A CRACKED, BS 727. REPAIRED LEFT STRINGER 18A CRACKED, BS 727 IAW ER 03-5300-06290-SS2.SDR AWXA200601786Stringer · crackedC-19 CHECK - NR 5931682, RT STRINGER 18A CRACKED, BS 727 AT IB FASTENER. REPAIRED RT STRINGER 18A, BS 727 IAW AWA ER 03-5314-06287-ES1.SDR AWXA200601780Skin · debondedMCN - MAJOR REPAIR - RIGHT HORIZONTAL STABILIZER O/B TRAILING EDGE DISBONDED FROM TIP FAIRING TO O/B END OF ELEVATOR, STAB STATION 295.10 - 149.12. REPAIRED RIGHT HORIZONTAL STABILIZER O/B TRAILING EDGE DISBONDED FROM TIP FAIRING TO O/B END OF ELEVATOR, STAB SDR AWXA200601705Skin · crackedMCN - L1 DOOR INNER SKIN CRACKED AFT SIDE AT NR 6 FROM TOP STOP PIN CUTOUT. REPAIRED L1 DOOR INNER SKIN, AFT SIDE AT NR 6 FROM STOP PIN CUTOUT, IAW B737-300 SRM 51-70-13-0G, FIG 1.SDR AWXA200601416Fan · burned outPHX - GTB - LOG - 7194805 - STARTING ENGINES AND DURING TAXI OUT FLIGHT ATTENDANT NOTIFIED THE FLIGHT DECK OF A STRONG SMOKE SMELL (LIKE ELECTRICAL OR CIGARETTE SMOKE) THROUGHOUT AFT CABIN. THE CREW RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE SDR AWXA200601352Sensor · failedCREW REPORTED THAT THE EXHAUST COOLING FAN "ORC" LIGHT BEGAN RAPID FLICKERING ON BOTH NORMAL AND ALTERNATE POSITION ABOVE FLIGHT LEVEL 300, PROBLEM STOPPED IN DESCENT BELOW FLIGHT LEVEL 300. MAINTENANCE REPLACED BOTH LOW FLOW SENSORS PER MM 21-58-43. EQUIPMESDR AWXA200601293Warning Light · unknownPHX - ATB - EQUIPMENT COOLING EXHAUST OFF LIGHT CAME ON DURING THE CLIMB OUT IN THE ALTERNATE POSITION AT CRUISE WAS STEADY OFF IN BOTH THE ALTERNATE AND NORMAL POSITION.SDR AWXA200601228Light · inoperativeSAL - FOUND EMERGENCY LIGHTS INOP. CART'S FLOURESCENT PANEL FLOOD LIGHT INOP INTERMITTENT CORRECTED BY FRIAL. RELAMPED CAPT'S FLOOD LIGHT, OPS CHECK GOOD.SDR AWXA200601004Sensor · faultyCREW REPORTED THAT DURING CRUISE EQUIPMENT COOLING EXHAUST OFF LIGHT ILLUMINATED. CREW PERFORMED QRH AND THE ALTERNATE COOLING OFF LIGHT ILLUMINATED. CREW RETURNED TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE M00100 AIR FLOSDR AWXA200601001Wire · chafedCREW REPORTED THAT ON CLIMB-OUT FROM PHX EQUIP COOLING EXHAUST OFF LIGHT ILLUMINATED. CREW FOLLOWED QRH PROCEDURES AND NOTIFIED MOC IN PHX. WHEN ALTERNATE SELECTED OFF REMAINED ILLUMINATED UNTIL DESCENT BACK TO PHX. REQUESTED RETURN TO PHX BY MOC. LANDED ISDR AWXA200600980Transmitter · out of rigPHX - FLIGHT CONTROL - FLT 0900 - LOG 7278984 - CREW REPORTED "FLAPS EXTENDING PAST 5, WHEN POSITION 5 IS SELECTED, INDICATOR IS APPROX 7. INDICATION IS VERIFIED ON FMC/CDU DEG PAGE. WITH FLAPS IN POSITION 5 FLAP SPEED INDICATION IS 170 KIAS, SHOULD BE 180 KSDR AWXA200600888Blower · failedPHX - AIR TURNBACK - FLT 790 - LG 7289346 - CREW REPORTED ALTERNATE EQUIPMENT COOLING LIGHT ILLUMINATED IN CRUISE. MAINTENANCE REMOVED AND REPLACED THE ALTERNATE COOLING BLOWER PER MM 21-58-12-4, OPS CHECK GOOD.SDR AWXA200600768Light · inoperativeDFW - EEL - NR 4095557 - DURING OVERNIGHT MAINTENANCE DISCOVERED ROW 16 SEAT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND INSTALLED NEW EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200600702Connector · disconnectedFLT 626 - CREW DECLARED EMERGENCY INOP PHX DUE TO GEAR DOWN AND GEAR WARNING LIGHTS BEING INOPERATIVE. REPORTED THAT THE AURAL GEAR WARNING OPERATED NORMALLY. MAINTENANCE TROUBLESHOT AND FOUND CONNECTOR D4262P DISCONNECTED AT THE LANDING GEAR PANEL. MAINTENSDR AWXA200600753Frame · crackedDURING CABIN MODIFICATION MAINTENANCE DISCOVERED BS 907 FRAME HAD 3 CRACKS, .75 INCHES, AT MOUNT HOLE BETWEEN STR 7R AND 8R. MAINTENANCE REMOVED DAMAGED SECTION OF FRAME AT BS 907 AT MOUNT HOLE BETWEEN STR 7R AND 8R IAW BOEING 737-300 SRM 53-00-07-2R1 FIG 201SDR AWXA200600760Frame · crackedDURING CABIN MODIFICATION MAINTENANCE DISCOVERED BS 907 FRAME HAD 4 CRACKS, .75 INCHES, AT MOUNT HOLE BETWEEN STR 7L AND 8L. MAINTENANCE REMOVED DAMAGED SECTION OF FRAME AT BS 907 AT MOUNT HOLE BETWEEN STR 7L AND 8L IAW BOEING 737-300 SRM 53-00-07-2R1 FIG 201SDR AWXA200600593Window Post · crackedDURING OVERNIGHT MX DISCOVERED POSSIBLE CRACK AT CAPTAINS SLIDING WINDOW FORWARD TOP CORNER. MX VERIFIED CRACK. CUTOUT DAMAGED PART OF CRACKED SKIN IAW BOEING 737-300 SRM 53-10-01 FIG 201. REMOVED CRACKED PART OF GUSSET IAW SRM 53-10-01 FIG 201. INSTALLED SDR AWXA200600565Blades · damagedFLT CREW REPORTED THAT ON DESCENT HEARD A LOUD THUMPING WITH VIBRATION, WERE ABLE TO STOPPED THIS BY RETARDING THE NR 1 THROTTLE. F/A REPORTED FLAMES COMING OUT OF THE NR 1 ENG TAIL PIPE. CREW REQUESTED A PRIORITY LANDING. LANDED IN IAH W/O FURTHER EVENT. SDR AWXA200600523Battery · inoperativePHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED THE ESCAPE PATH LIGHTING AT ROWS 1 THROUGH 6 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR ROW'S 1 THROUGH 6 EMERGENCY PATH LIGHTING. OPERATIONAL CHECKS WERE GOODSDR USAA920080248Skin · crackedMCN - MAJOR REPAIR - C20 CHECK - CRACKED FUSELAGE SKIN, BS 870, S24R. REPAIRED FUSELAGE SKIN, BS 870, S24R IAW B737 SRM 53-00-01-2R 31.SDR AWXA200600049Slat System · malfunctionedCREW REPORTED THAT DURING LEVEL FLIGHT, 6000'/210KTS, THE FORWARD "LE FLAPS TRANSIT" LIGHT ILLUMINATED AND THE NR 4 SLAT SHOWED FULL EXT ON THE OVERHEAD ANNUNCIATOR PANEL. CREW COMPLETED THE LEADING EDGE FLAPS TRANSIT QRH. THE TRANSIT LIGHT ON THE FWD PANEL SDR AWXA200600044Fuel Tank · leakingCREW REPORTED FLUID COMING FROM THE RIGHT WING TIP. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT KNOWN FURTHER INCIDENT. MAINTENANCE INSPECTED WHOLE RIGHT WING FUEL SYSTEM. NO DISCREPANCIES WERE NOTED. NO FURTER INFO REGARDING EVENT. HAS NOT REPEATED. REPSDR AWXA200600034Odor · detectedPHX - BURNING ODOR - FLIGHT ATTENDANTS REPORTED A RUBBER/BURNING SMELL COMING FROM ROW 10-15 AREA. MAINTENANCE INSPECTED CABIN AND FOUND NO RESIDUAL SMELLS OR ODORS.SDR AWXA200501600Skin · debondedMCN - DURING C20 CHECK DISCOVERED FIBER DAMAGE ON THE LT SIDE OF RUDDER 18" FROM THE TRAILING EDGE. MAINTENANCE REMOVED DAMAGED PLIES IAW BOEING 737-300 SRM 51-70-04-0G R1 FIG 10. BONDED REPAIR PLIES TO REPAIR AREA ON THE LT SIDE OF RUDDER IAW BOEING 737-300SDR AWXA200501599Skin · debondedMCN - DURING C20 CHECK DISCOVERED LT ELEVATOR UPPER SKIN HAD FIBER DAMAGE 46" FROM THE INBOARD EDGE OF THE ELEVATOR. MAINTENANCE REMOVED DAMAGED PLIES IAW BOEING 737-300 SRM 51-70-04-0G R1 FIG 10. BONDED REPAIR PLIES TO REPAIR AREA ON THE LT ELEVATOR UPPER SSDR AWXA200501595Filler · corrodedMCN - DURING C20 CHECK DISCOVERED CORROSION ON THE AFT CARGO LOWER SILL STRAP FROM BS 796 TO BS 812, WL 158.5 AND BL 19R. NO CORROSION REMOVAL LIMITS WERE AVAILABLE IN THE BOEING 737-300 SRM. MAINTENANCE REMOVED AND INSTALLED NEW AFT CARGO DOOR LOWER SILL STSDR AWXA200501594Strap · corrodedMCN - DURING C20 CHECK DISCOVERED CORROSION ON THE AFT CARGO LOWER SILL STRAP FROM BS 839 TO BS 851, WL 158 AND BL 19R. NO CORROSION REMOVAL LIMITS WERE AVAILABLE IN THE BOEING 737-300 SRM. MAINTENANCE REMOVED AND INSTALLED NEW AFT CARGO DOOR LOWER SILL STRASDR AWXA200501589Web · corrodedMCN - DURING C20 CHECK DISCOVERED CORROSION ON THE AFT CARGO DOOR SILL WEB FROM BS 794 TO BS 847 AND STR 25R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. MAINTENANCE REMOVED WEB AND INSTALLED NEW WEB FROM BS 794 TO BSSDR AWXA200501586Bulkhead · crackedMCN - DURING C20 CHECK DISCOVERED VERTICAL WEB CRACKED, 1.31 INCHES, FROM WL 226 TO WL 234, BS 178 AND BL 17R. MAINTENANCE REMOVED VERTICAL WEB FROM WL 226 TO WL 234, BS 178 AND BL 17R IAW BOEING 737-300 SRM 53-10-08-2R17 FIG 201. FABRICATED NEW WEB IAW BOEISDR AWXA200501602Frame · crackedMCN - DURING C29 CHECK DISCOVERED THAT THE 178 BULKHEAD SIDE CHORD WAS CRACKED, 2.0 INCHES, AT BL 31R AND WL 206. MAINTENANCE REMOVED AND INSTALLED NEW CHORD AT BL 31R AND WL 206 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 2, 8 AND 12.SDR AWXA200501604Reveal · corrodedMCN - DURING C20 CHECK DISCOVERED CORROSION ON THE AFT CARGO DOOR CUTOUT, AFT, FRAME EDGE COVER AT BS 851, FROM WL 158 TO WL 164 AND FROM BL 22R TO BL 25R. NO CORROSION REMOVAL LIMITS WERE FOUND IN THE BOEING 737-300 SRM. MAINTENANCE FABRICATED NEW REVEAL STSDR AWXA200501597Intercostal · corrodedMCN - DURING C20 CHECK DISCOVERED CORROSION ON THE AFT CARGO FLOOR INTERCOSTAL OUTBOARD SIDE FROM BS 787 TO BS 794, FROM WL 152 TO WL 158 AND BL 20.5R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-0I 1 FIG 101. MAINTENANCE REMOVED
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