Boeing 737-33A
Service difficulty reports · 1,809
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 = '73733A' 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 = '73733A' 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 AWXA200700017Door Frame · corrodedMCN - CORROSION ON R2 DOOR CUTOUT INNER CHORD AT BS 917 - BS 1006, WL 208, RBL 45 - RBL55. REPLACED R2 DOOR CUTOUT INNER CHORD AT BS 917 - BS 1006, WL 208, RBL 45 - RBL55 IAW B737 SRM 51-40-02-0G, FIG 3, 8, 12.SDR AWXA200700016Floorbeam · corrodedMCN - CORROSION ON CABIN FLOORBEAM WEB AT BS 1016, BL 0 - LBL 20. REPLACED CABIN FLOORBEAM WEB AT BS 1016, BL 0 - LBL 20 IAW B737 SRM 51-40-02-0G, FIG 3, 8, 9, AND BOEING DWG 65C33419.SDR AWXA200700015Floorbeam · corrodedMCN - CORROSION ON CABIN FLOORBEAM STRAP AT BS 1014, RBL 4. REPLACED CABIN FLOORBEAM STRAP AT BS 1014, RBL 4 IAW B737 SRM 51-40-02-0G, FIG 3, 8, 9, AND BOEING DWG 6532677.SDR AWXA200700014Floorbeam · corrodedMCN - CORROSION ON CABIN FLOORBEAM STRAP AT BS 1014, LBL 4. REPLACED CABIN FLOORBEAM STRAP AT BS 1014, LBL 4 IAW B737 SRM 51-40-02-0G, FIG 3, 8, 9, AND BOEING DWG 65C32677.SDR AWXA200700013Floor Support · corrodedMCN - CORROSION ON CABIN DIAGONAL FLOOR SUPPORT BEAM AT BS 994, BL 13L. REPLACED CABIN DIAGONAL FLOOR SUPPORT BEAM AT BS 994, BL 13L IAW B737 SRM 51-40-02-0G, FIG 12.SDR AWXA200602091Strap · crackedMCN - MAIN CABIN FLOORBEAM STABILIZER STRAP CRACKED, BS 344, LBL 50, WL 200. REPAIRED MAIN CABIN FLOORBEAM STABILIZER STRAP, BS 344, LBL 50, WL 200 IAW B737-300 SRM 53-10-51.SDR AWXA200602084Stiffener · crackedMCN - MAIN CABIN FLOOR BEAM INTERCOSTAL (STIFFENER) CRACKED, BS 328, LBL 47, WL 208. REPLACED MAIN CABIN FLOORBEAM INTERCOSTAL (STIFFENER) CRACKED, BS 328, LBL 47, WL 208 IAW B737-300 SRM 51-40-02.SDR AWXA200602083Stiffener · crackedMCN - MAIN CABIN FLOORBEAM INTERCOSTAL (STIFFENER) CRACKED, BS 312, RBL 32, WL 208. REPLACED MAIN CABIN FLOORBEAM INTERCOSTAL (STIFFENER), BS 312, RBL 32, WL 208 IAW B737-300 SRM 51-40-05.SDR AWXA200700033Frame · crackedMCN - R-1 DOOR AFT FRAME CRACKED AT 3RD AND 4TH FROM TOP STOP PIN CUTOUTS. REPAIRED R-1 DOOR AFT FRAME CRACKED AT 3RD AND 4TH FROM TOP STOP PIN CUTOUTS IAW AWA ER 03-5240-06347.SDR AWXA200700018Door Frame · crackedMCN - CRACK ON R1 DOOR CUTOUT FORWARD UPPER FRAME AT BS 300, S10R. CRACK ON R1 DOOR CUTOUT FORWARD UPPER FRAME AT BS 300, S10R IAW B737 SRM 51-40-02-0G, FIG 3, 8.SDR AWXA200700002Beam · crackedMCN - L1 DOOR INNER LOWER FRAME, UPPER SUPPORT BEAM CRACKED, BS 344, S16L. REPAIRED L1 DOOR INNER LOWER FRAME, UPPER SUPPORT BEAM, BS 344, S16L IAW B737-300 SRM 51-70-11, FIGURE 1.SDR AWXA200700001Door Frame · crackedMCN - L1 DOOR INNER LOWER AFT FRAME CRACKED, BS 344, S16L. REPAIRED L1 DOOR INNER LOWER AFT FRAME, BS 344, S16L IAW B737-300 SRM 51-70-11 FIGURE 1.SDR AWXA200602086Shear Tie · corrodedMCN - CORROSION ON AFT CARGO COMPARTMENT SHEAR TIE, BS 947.5, S26L - S27L. REPLACED AFT CARGO COMPARTMENT SHEAR TIE, BS 947.5, S26L - S27L IAW B737-300 SRM 51-40-02.SDR AWXA200602085Stringer Clip · crackedMCN - STRINGER 2L TIE CLIP CRACKED, BS 639. REPLACED STRINGER 2L TIE CLIP, BS 639 IAW B737-300 SRM 51-40-02.SDR AWXA200700019Pressure Panel · crackedMCN - MAJOR REPAIR - C-21 CHECK - CRACK ON LEFT WHEEL WELL WEB AT BS 727, S18AL. REPLACED LEFT WHEEL WELL WEB AT BS 727, S18AL IAW AWA ER 03-5312-06353-SS1.SDR AWXA200602094Wedge · debondedMCN - RIGHT WING NR 5 SLAT WEDGE DEBONDED, SS 248.9 - SS 254.4. REPAIRED RIGHT WING NR 5 SLAT WEDGE, SS 248.9 - SS 254.4 IAW B737-300 SRM 51-70-10.SDR AWXA200602092Skin · crackedMCN - RIGHT WING NR 4 SLAT LOWER SURFACE SKIN CRACKED, SS 61 AND SS 62.2. REPAIRED RIGHT WING NR 4 SLAT LOWER SURFACE SKIN, SS 61 AND SS 62.2 IAW B737-300 SRM 57-43-01.SDR AWXA200700048Stringer · crackedMAJOR REPAIR - C-21 CHECK - NR 5917219, RT MAIN LANDING GEAR WHEEL WELL STRINGER 18A WEB CRACKED, BS 727. REPAIRED RT MAIN LANDING GEAR WHEEL WELL STRINGER 18A WEB, BS 727 IAW AWA ER 03-5361-07007-SS1.SDR AWXA200700047Fitting · crackedMAJOR REPAIR - C-21 CHECK - NR 5916816, LT WING MAIN LANDING GEAR SUPPORT BEAM OB FITTING CRACKED, WBL 147. REPLACED LT WING MAIN LANDING GEAR SUPPORT BEAM OB FITTING, WBL 147 IAW AWA ER 03-5726-06347-SS2.SDR AWXA200602093Skin · delaminatedMCN - LEFT WING OUTBOARD FORE FLAP UPPER SKIN DELAMINATED, WBL 203.69. REPAIRED LEFT WING OUTBOARD FORE FLAP UPPER SKIN, WBL 203.69 IAW B737-300 SRM 51-70-10.SDR AWXA200602011Actuator · failedDFW - ATB - DURING CLIMB-OUT OF DFW, THE A/C REQUIRED EXCESSIVE RUDDER INPUT TO MAINTAIN STRAIGHT FLIGHT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DFW. THE PAX DID NOT BRACE. MX REMOVED AND REPLACED THE RUDDER TRIM ACTUATOR. THIS DID NOT CORRECT THE SDR AWXA200602005Rib · crackedPHX - LEFT WING LEADING EDGE SEAL RIB FORWARD OUTBOARD LOWER FLANGE CRACKED, LEADING EDGE STATION 219. REPAIRED LEFT WING LEADING EDGE SEAL RIB FORWARD OUTBOARD LOWER FLANGE LEADING EDGE STATION 219 IAW AWA ER 03-5741-06337-SS1.SDR AWXA200601700Skin · delaminatedPHX - MAJOR REPAIR - RIGHT WING OUTBOARD AFT FLAP INBOARD END IS DELAMINATED, WBL 204.40. REPLACED RIGHT WING OUTBOARD AFT FLAP IAW TASK CARD R3M27034.SDR AWXA200601684Door · crackedDFW - LEFT WING KRUEGER FLAP DOOR CRACKED, WS 135.7202. REPLACED LEFT WING KRUEGER FLAP DOOR, WS 135.7202 IAW B737-300 AMM 27-81-14-2.SDR AWXA200601554Skin · crackedPHX - 2 INCH FUSELAGE CRACK RT WTB 2 INCH AFT OF EMERGENCY EXIT LIGHT AT LAP CUTOUT SEAM. REPAIRED SKIN CRACK RT WTB 26 INCHES AFT OF EMERGENCY EXIT PER SRM 53-00-01-2R, FIG 201.SDR AWXA200601526Skin · crackedPHX - SKIN CRACK AT STA 727 E, AND STR 24, APPROX 2" LONG ON LT SIDE OF A/C. REPAIRED IAW ER NR 03-5361-06193-ES1, AND SRM 53-00-01, REPAIR 31.SDR AWXA200601189Coalescer Bag · odorLAS - ODOR - FLT 835 - CUSTOMER COMPLAINTS, FOUL ODOR STILL PERVASIVE THROUGHOUT CABIN AND MINIMAL AIR CIRCULATION. MAINTENANCE REPLACED BOTH THE LEFT AND RIGHT COALESCER BAGS.SDR AWXA200601186Odor · detectedODOR FWD CABIN AND THROUGH OUT AFT.SDR AWXA200601188Odor · detectedMINIMAL AIRFLOW THROUGH GASPERS AND A FOUL ODOR THROUGH-OUT CABIN, REPORTED AND VERIFIED BY CREW. AFT LAV'S SERVICED AS REQUIRED AND DEODORIZED, AIR FLOW FROM GASPERS NORMAL AT THIS TIME.SDR AWXA200601033Battery · dischargedPHX - EEL - LOG 7260323 - CREW REPORTED THAT FORWARD VERTICALLY MOUNTED EMERGENCY FLASHLIGHT RED LIGHT WAS NOT BLINKING. MAINTENANCE REPLACED BATTERY IN THE FORWARD VERTICALLY MOUNTED FLASHLIGHT. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200600981Pin · pulledPHX - EEL - NR 4080561 - DURING OVERNIGHT INSPECTION MAINTENANCE REPORTED THAT THE LT AFT GALLEY, AISLE EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. FOUND WIRES PULLED OUT OF BAYONET. MAINTENANCE RE-SECURED PINS INTO THE CONNECTOR. LIGHT OPERATIONAL CHECKS WERESDR AWXA200600885Skin · crackedPHX - MAJOR REPAIR - LT FUSELAGE AFT AND BELOW EXISTING REPAIR CRACKED, 1.9 INCHES, AT BS 727E AND STR 24L. MAINTENANCE REMOVED DAMAGED AREA AND INSTALLED FABRICATED DOUBLER AT BS 727E AND STR 24L IAW BOEING 737-300 SRM 53-00-01-2R.SDR AWXA200600886Skin · crackedPHX - MAJOR REPAIR - FLT 277 - LG 4058471 - DURING OVERNIGHT MAINTENANCE, DISCOVERED CRACK ON LT FUSELAGE AFT OF EXISTING REPAIR CRACKED APPROX 1 INCH LONG STATION 743 STRINGER 23L. MAINTENANCE REMOVED DAMAGED AREA AND INSTALLED FABRICATED DOUBLER IAW SRM 53-SDR AWXA200600872Outflow Valve · obstructedABQ - DIVERSION - FLT 484 - CREW REPORTED THAT WHILE AT FL350, CABIN BEGAN TO CLIMB AND DIFF PRESSURE BEGAN TO DROP. COULD NOT CONTROL CABIN ALTITUDE WITH ALL STANDBY PROCEDURES. DIVERTED TO ABQ AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND INSULATIONSDR AWXA200600830Indicator · inoperativeLAS - ABORTED TAKEOFF - FLT 0110 - DURING TAKE OFF ROLL CREW REPORTED THAT THEY LOST THE F/O'S AIRSPEED INDICATION. ABORTED TAKEOFF AT APPROX 90 KNOTS AND RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE F/O'S AIRSPEED INDICATOR IAW BOEINSDR AWXA200600742Tire · damagedCREW REPORTED THAT AFTER TAKEOFF FELT VIBRATION IN YOKE AND PEDALS TILL APPROX 60 KTS. VIBRATION WAS NOT NOTICED ON TAKEOFF. MAINTENANCE FOUND THE LT NOSE TIRE WAS OUT OF ROUND. REMOVED AND REPLACED THE LT NOSE WHEEL IAW AWA TASK CARD R4N32009.SDR AWXA200600670Wire · brokenDFW - EEL - NR 4097136 - DURING OVERNIGHT INSPECTION DISCOVERED THE ESCAPE PATH LIGHTS AT ROWS 21L AND 23L WERE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES ON ESCAPE PATH LIGHTS AT ROWS 21L AND 23L. OPERATIONAL CHECKS WERE GOOD.SDR AWXA200600661Battery · failedBUR - EEL - CREW REPORTED THAT ONE FORWARD EMERGENCY FLASHLIGHT WAS NOT CHARGING. DEFERRAL WAS ISSUED FOR THE FORWARD CABIN FLASHLIGHT. IN PHX, MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD AND DEFERSDR AWXA200600665Light · intermittentLAS - FLT 0554 - FLIGHT ATTENDANTS REPORTED SEEING SPARKS AROUND AIR VENTS ON THE RT SIDEWALL BETWEEN ROWS 11 AND 12. MAINTENANCE INSPECTED WIRING IN THE OVERHEAD PANELS FROM ROW 10 TO ROW 14 FOR DEFECTS. NO DEFECTS WERE NOTED. REMOVED AND REPLACED THE RT SSDR AWXA200600619Switch · faultyPHX - FLT 790 - CREW REPORTED RECEIVING THE TAKEOFF CONFIG WARNING HORN AT 80-81% ON TAKEOFF ROLL. REPORTED NO SYSTEMS FOUND OUT OF PLACE. LOW SPEED REJECTION NO MORE THAN 20 KTS. AUTO THROTTLE WAS NOT YET ACTIVATED. CREW ABORTED TAKEOFF AND RETURNED TO THSDR AWXA200600623Adc · faultedLAS - ABORTED TAKEOFF - FLT 839 - CREW REPORTED THAT DURING TAKEOFF THE F/O'S AIRSPEED INDICATOR FAILED AT 80 KNOTS ON TAKEOFF ROLL. CREW RETURNED TO THE GATE WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE F/O'S AIR DATA COMPUTER IAW AMERICA WESSDR AWXA200600462Smoke Detector · faultyELP - FALSE FIRE WARNING - CREW REPORTED THAT AT GATE WITH THE APU RUNNING RECEIVED AN AFT CARGO FIRE INDICATION. CREW FOLLOWED QRH PROCEDURES AND EVACUATED AIRCRAFT AT GATE, L2 DOOR SLIDE WAS DEPLOYED AND REMAINING PASSENGERS EVACUATED AIRCRAFT. FIRE BOTTLESDR AWXA200600531Skin · crackedMCN - DURING C22 CHECK DISCOVERED FUSELAGE SKIN CRACKED AT STR 22R AND BS 727E. MAINTENANCE TRIMMED OUT DAMAGE IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-06062-RC2. FABRICATED DOUBLER, TRIPLER, FILLER, TEAR STRAP INTERNAL DOUBLER AND TAPERED FILSDR AWXA200600527Rib · crackedMCN - DURING C22 CHECK DISCOVERED LOWER CHORD OF STAB STA 138.7 RIB, CRACKED .7 INCHES AT FORWARD ATTACH POINT OF THE LT HORIZONTAL STABILIZER. MAINTENANCE REMOVED DAMAGED SECTION OF CHORD IAW BOEING 737-300 SRM 55-10-09-2R2 FIG 201. FABRICATED FILLER AND RESDR AWXA200600406Slide · unknownPHX - EES - DURING SCHEDULED DEPLOYMENT OF THE R-1 DOOR, THE SLIDE ENDED UP NOT BEING PERPENDICULAR TO THE AIRCRAFT, THE SLIDE CAME OUT TWISTED. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR SLIDE IAW AMERICA WEST AIRLINES TASK CARD R1C25001. UNABLE TO DUPLISDR AWXA200600520Support Angle · corrodedMCN - MAJOR REPAIR - DURING C22 CHECK DISCOVERED LEVEL 2 EXFOLIATION CORROSION ON LOWER SURFACE OF THRESHOLD SUPPORT ANGLE FROM BS 947 TO BS 967, BL 55R AND WL 207. CORROSION WAS REMOVED AND RE-WORK WAS FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-1SDR AWXA200600384Steering Sys · malfunctionedPHX - ABORTED TAKEOFF - FLT 206 - DURING TAKEOFF CREW REPORTED THAT WITH ENGINE POWER EVEN AND STABLE, THE AIRCRAFT VEERED TO LEFT. RIGHT RUDDER INPUT WAS NOT EFFECTIVE. AIRCRAFT CONTINUED TO VEER LEFT. CREW ABORTED TAKEOFF AT 50 KNOTS. RETURNED TO THE GATSDR AWXA200600383Skin · crackedDURING C19 CHECK DISCOVERED FUSELAGE SKIN CRACKED AT THE R-2 DOOR CUT OUT, LOWER FORWARD CORNER AT BS 960. MX REPAIRED THE R2 DOOR CUTOUT IAW AWA ER NR 03-5361-06054-RC1. REPAIRED R2 DOOR BY TRIMMING OUT THE NEW DAMAGE ON THE R2 DOOR OPENING. FABRICATED DOUSDR AWXA200600344Skin · crackedMCN - DURING C19 CHECK DISCOVERED FUSELAGE SKIN CRACKED, 6 INCHES, ON THE LEFT SIDE WINDOW BELT JUST FWD OF STA 520 STR 12L. MAINTENANCE REPAIRED PER AMERICA WEST ENGINEERING REPAIR NR 03-5331-06031-221.SDR AWXA200600583Stringer Clip · crackedMCN - DURING C22 CHECK DISCOVERED STRINGER CLIP AT BS 947 STR 22L CRACKED, 0.350 INCHES. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 947 STR 22L IAW BOEING 737-300V SRM 51-40-02-0G PARA E FIG 8. FABRICATED STRINGER CLIP IAW BOIENG 737-300 SRM 51-30-01-0G
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