Boeing 737-800
Service difficulty reports · 843
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 = '737800' 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 = '737800' 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 CALA2022032300766Rivet · missingPDA 3 RIGHT WING FIXED L/EDGE AT OUTBD END HAS ONE RIVET HEAD BROKEN OFF / MISSING AND 2 RIVETS PULLED THRU -- SEE PHOTO PHOTO ADDED REMOVED THREE LOOSE FASTENERS AND INSTALLED THREE NEW FASTENERS REF. SRM 51-40-02.SDR CALA2022032300765Probe · failedENGINE OVERTEMPERATURE (EXCEPT STARTING) EGT OVER REDLINE, NO SU RGE/STALL ENGINE 1 LEVEL OFF ENGINE PARAMETERS TURNED TO NORMAL WITH A 50F HIGHER DEFECTS NOTED. REF WDM 77-21-11-101 AND FIM 77-21 TASK 801. TEMPERATURE VARIATION FROM 2 ENGINE. AIRCRAFT RETURNESDR CALA2022032300764Hmu · failedNO 1 ENG FAILED AT 340. ATTEMPT RESTART. NOEGT NO RESTART SECTION. REPLACED GASKET REF AMM 73-21-10. RAN ENGINE NO LEAKS NOTED, BUT FUEL WAS SEEPING FROM HMU SIDE CASE COVER. REQUIRES HMU REPLACMENT. ADDED PICTURES. T/S FOUND MSG 73-21551. PERFORMED EEC BITE TSDR CALA2022032300762Proximity Sensor · failedLEADING EDGE TRANSIT LIGHT FROM FLAPS 5 TO 10 PERFORMED FSEU BITE LAST LEG FAULT FOR SL7 PROX O/B MSG: 27-81212. DURING INTIAL EVALUATION PER FIM 27-88 TASK 803 FOUND ON FULL EXTENDED SLATS S7 O/B PROX WAS SHOWING FAR INSTEAD OF NEAR REMOVED AND REPLACED #7 SLSDR CALA2022032300757Rib · crackedLEFT HORIZONTAL STABILIZER STA.101.90 RIB HAS 3/4" CRACK ON LOWER HORIZONTAL FLANGE AT VERTICAL STIFFENER # 2. (REF AAR NR 9641753) TO T7075 T6 .063", REF BHC 5602 AND OP 84, REINSTALLED REPAIR AT STA 101.90, VERTICAL STIFFNER IN REF B737-800 SRM 55-10-09-2R-5SDR CALA2022032300744Rib · crackedL/H HORIZONTAL STAB STA 101.90 RIB CRACKED AT LOWER FWD FLANGE REF AAR N/R 9642208 INSTALLED REPAIR ANGLE AT LT HORIZONTAL STAB STA 101.90 AT LOWER FWD FLANGE OF RIB REF B737 SRM 55-10-09-2R-5 FIG 205 WORK ACCOMPLISHED BY V920314SDR CALA2022032100742None · none*DECLARED EMERGENCY* LEFT WING-BODY OVERHEAT LIGHT ILLUMINATED ON GROUND ENGINES NOT RUNNING. APPROVED WITH NO FAULTS NOTED. RAN OVERHEAT TEST , NO FAULT CODE NOTED. SYS MEMORY CODE 14 (LT LE FAULT) NOTED. DISPATCH DESK: 6 NAME: SLDATE: 16-MAR-22- NOC DSDR CALA2022032100739Service Door · missingPDA 1 LAVATORY SERVICE DOOR FOUND MISSING UPON ARRIVAL IN BNA AFTER FLIGHT UA771 (DEN / BNA). DOOR (145AL)MEASURES IN EXCESS OF 150 SQ INCHES AND WILL BE DESIGNATED A CATEGORY 1. SDR #1028039 SUBMITTED AS PER GMM 02-30-95 AND ESC HAS BEEN ADVISED. SDR #1028039SDR CALA2022032100732Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED. SUPPORT TASK NSA EMX N/R 00090. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 6.14 IAW B737- ENTERED BY UAL INSPECTION U354653 3/16/22 800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORG. DATA SDR CALA2022032100731Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKEDSUPPORT TASK NSA EMX N/R 00089. REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04 IAW B737 ENTERED BY UAL INSPECTION U354653 3/16/22 -800 SRM 51-40-02 AND BAC DWG 11A2000 REV ORG. DATA SDR CALA2022032100730Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00088. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND RBL 32.40 IAW ENTERED BY UAL INSPECTION U354653 3/16/22 B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORG. SDR CALA2022032100729Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 40.87 IS CRACKED. SUPPORT TASK NSA EMX N/R 00087. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND RBL 40.87 IAWW INSPECTION U 354653 3/16/22 B737-800 SRM 51-40-02 AND BAC DWG 11A2000 REV ORG DATA WAS TRAN SSDR CALA2022032100728Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRACKED. SUPPORT TASK NSA EMX N/R 00086. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 54.60 U354653, 03/16/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R IAW B737-800 SRM 51-40-02 AND BAC DSDR CALA2022032100727Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRACKED. SUPPORT TASK NSA EMX N/R 00085. REMOVED AND REPLACED SHEAR FITTINGS AT STA 540 AND LBL 6.14 IAW ENTERED BY UAL U354653 3/16/22 B737-800 SRM 51-40-02 AND BAC SWG 11A2000 REV ORG. DATA WAS TRANSDR CALA2022032100726Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00084. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 LBL 15.04 ENTERED BY UAL INSPECTION U354653 ON 03/16/22 IAW B737-800 SRM 51-40-02 AND DWG 111A2000 REV OSDR CALA2022032100725Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00083. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 32.40 ENTERED BY UAL INSPECTION U354653 ON 03/16/22 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 RSDR CALA2022032100724Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 40.87 IS CRACKED. SUPPORT TASK NSA EMX NR 00082. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 AND LBL 40 ON 03/16/22 .87 IAW B737-800 SRM 51-40-02 AND DWG 111A2000 REV ORG. DATA WAS TRANSCRIBED FROM SDR SWAA2022032485720Sensor · faultyAFTER TAKEOFF; WITH LANDING GEAR LEVER IN UP POSITION; THE RIGHT MAIN GREEN LANDING GEAR INDICATOR LIGHT REMAINED ILLUMINATED. / [01] REMOVED AND REPLACED THE RH FORWARD MLG DOWN-AND-LOCKED SENSOR (S0073) PER AMM 32-61-31. OPS CHECK GOOD; COULD NOT DUPLICATE; SDR SWAA2022032485718Fuse · inoperativeEXTERIOR EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOP / [01] REMOVED AND REPLACED DEFECTIVE FUSE IN BATTERY PACK M1875 PER AMM 33-51-06SDR CALA2022032100721Rib · crackedR/H HORIZONTAL STAB RIB NO.1 AT STA 82.70 CRACKED AT NO.3 VERTICAL STIFFNER LOWER AREA REF AAR N/R 9642159 REMOVED NO.1 RIB AT STA 92.70 REMOVED T-SCETIOC REPAIR EXTRUSION REPAIR AT RIB NO.1 AND REINSTALLED RIB AT FR STA 92.70 REF B737 FOR HEAT TREAT AND REMOVSDR CALA2022032100720Skin · dentedREFERENCE LOG PAGE 5529746 (CLOSED).FWD CARGO DOOR CUTOUT TOP R/H AREA HAS DENT REWORKED DAMAGE IAW B SRM 53-00-01-2R-21. INSPECTION THRESHOLD OF 50000 FLIGHT CYCLES. EXTERNAL LFEC AT 3500 FLIGHT CYCLES, INTERNAL HFEC AT 3500 FLIGHT CYCLES AND EXTERNAL DV AT 3SDR CALA2022032100719Skin · dentedREF ELB LP 8128621 ITEM REPETITIVE INSP PER AMM FOUND BIRD STRIKE DENT ON LT SIDE OF FUSLAGE STA 190 WL 184 3.75IN DIA AND .160 DEEP REF AAR N/R 9641251 CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS FOR PART 2 OF THE LATEST REVISION OF ECRA 5331-02855 RESDR CALA2022032100718None · corrodedMAIN CABIN AFT WET AREA STA 986.5 FLOOR BEAM L/H JUST I/B OF L2 CREASE BEAM UPPER SURFACE CORROSION. (REF AAR NR 9641534) CABIN AFT WET AREA STA 986.5 AS PER B737-800 SRM 53-70-51-2R-4 AND EC/RA 5320-02466. REMOVED EXISTING REPAIR AT MAIN CABIN AFT WET AREA STSDR SWAA2022032385648Girt Bar · missingFWD ENTRY GIRT BAR STOP MISSING / [01] R&R FWD ENTRY GIRT BAR ASSEMBLY PER AMM 25-66-01. VERIFIED GIRT BAR ENGAGES AND LOCKS ONTO THE FLOOR.SDR CALA2022032100714Frame · crackedF/O''S UPPER OUTBOURD CORNER WINDOW FRAME IS CRACKED. LOCK FOR MX FERRY PHOTO ADDED RAMS REQUITED LOGPAGE UNLOCKED FOR UPDATE COMPLETED STEPS B1&2 OF AVO9568 REF NDT PART 6 51-00-01. CORRECTION: COMPLETED STEPS B3 & B4 OF AVO9568 REF NDT PART 6 INSPECTION EVALSDR SWAA2022032285345Bulkhead · crackedAFT CARGO PANEL 142NWB (CHIMNEY) HAS CRACK THAT WAS COVERED BY TAPE AND IS NOW CRACKED THROUGH TAPE. / [01] REMOVED AFT CARGO COMPARTMENT FORWARD BULKHEAD LINER PER AMM 25-52-18.;[02] REMOVED AFT FWD BULKHEAD CAP-STRIP FROM PANEL 142 NWB FOR REPLACEMENT WITH NSDR SWAA2022032285100Bulkhead · cracked#1 ENGINE PYLON HAS A CRACK IN THE AFT BULKHEAD AT APPROXIMATE NACELLE STATION 314.0. CRACK IS 2.75' LONG; PROPAGATES INTO A RADIUS; AND EXITS OUT THE BOTTOM EDGE OF THE BULKHEAD FRAME. / [01] CRACK CONFIRMED WITH HFEC INSPECTION USING NDT MANUAL PART 6; 51-00SDR CALA2022032100711Service Door · missingLAV SERVICE PANEL ON AFT FUSELAGE MISSING. CONFIRMED LAVATORY SERVICE DOOR IS MISSING. PERFORMED A ENHANCED ZONAL INSPECTION OF THE AFT LOWER FUSELAGE AND EMPENNAGE AREA IN REFERENCE WITH 05-42-01-210-801. NO DAMAGED NOTED. PLACING DOOR ON CDL IN REFERENCE WISDR SWAA2022032184808Mechanism · faultyFIRST OFFICER'S SLIDING WINDOW DOES NOT OPEN WHEN EMERGENCY RELEASE HANDLE IS PULLED. / [01] ADJUSTED EMERGENCY EXIT RELEASE MECHANISM PER AMM 56-12-11.SDR SWAA2022032084516Battery · faultyBOTH FWD F/A FLASHLIGHTS WILL NOT TEST. / [01] R AND R BOTH FORWARD F/A FLASHLIGHT BATTERIES + SEALS AS PER AMM 25-64-00-802 LOG PAGE # 1858729SDR SWAA2022031883960Megaphone · inoperativeAFT F/A MEGAPHONE INOP / [01] REPLACED MEGAPHONE AND OPERATION TEST IAW AMM 25-64-00. NO FURTHER DEFECTS NOTED. A/C OK FOR SERVICE.SDR SWAA2022031883939Flashlight · inoperativeBATTERIES DIED ON 2 FLASH LIGHTS IN AFT GALLEY / [01] REMOVED AND REPLACED AFT GALLEY RIGHT SIDE F/A STATION FLASH LIGHT BATTERIES AND OPS CHECKED GOOD PER AMM 25-64-00SDR SWAA2022031883450Flashlight · inoperativeAFT FLT ATTENDANT FLASHLIGHT INOP. / [01] OK TO CONTINUE PER MEL 25-12-01 SP1B.;[02] REMOVED AND REPLACED AFT RIGHT HAND OUTBOARD CLOSE TO ISLE FLT ATTENDANT FLASHLIGHT BATTERY AS PER AMM 25-64-00. OPS CHECK NORMAL AND NO DEFECTS NOTED AT THIS TIME. THIS ACTIOSDR SWAA2022031883951Guide Arm · failedFORWARD ENTRY DOOR STICKS WHILE OPENING / [01] REMOVED AND REPLACED GUIDE ARM HINGE BOLT PER MM 52?11-21. OPS NORMALSDR CALA2022031400660None · none*EMERGENCY DECLARED*AFT CAEGO PIT FIRE INDICATION IN FLIGHT. FIRE SUPRESSION DISCHARGED IN AFT PIT, PLANE LANDED IN UNDER 60 MINUTES APPLIED MEL FOLLOWED SDS FOR CIRCUIT BREAKERS RESET TO STOP FIRE APPLIED MEL 2619C AFT PIT SECURED AND TAGGED DO NOT USE INOP ASDR SWAA2022031782980Flashlight · inoperativeAFT FLASHLIGHT WILL NOT TEST / [01] OK TO CONTINUE PER MEL 25-12-01 SP1B;[02] REMOVED AND REPLACED FLASHLIGHT BATTERY PER AMM 25-64-00SDR SWAA2022031683173Retainer · out of positionFORWARD GALLEY GIRT BAR DIFFICULT TO SECURE IN UN-ARMED POSITIO. RIGHT SIDE OF RETAINING CLIP APEERS LOOSE. / [01] RE-SECURED FWD GALLEY SERVICE DOOR STOWAGE RETAINER PER MM 25-66-01SDR CALA2022031000635Screw · missingPDA 3 #2 ENGINE MISSING A SCREW FROM FWD INBOARD PYLON PANEL. REPLACED 1 MISSING SCREW AS REQURIED.SDR CALA2022031000634None · failedAIR RETURN MAX SPEED RED BLACK INDICATOR 270KTS DIRECTED BY TOMC TO SWITCH EITHER THE NAV, IRS AND OR FMC POWER SOURCES AT THE OVERHEAD PANEL TO TRY TO RESOLVE THE INACCURATE A IRSPEED BARBER PULLS INDICATIONS ON BOTH PFDS. NEED TO TS AIRSPE ED INDICATION ISSUSDR CALA2022031000633Transmitter · failedLEADING EDGE FLAPS AND SLATS DO NOT EXTEND DURING NORMAL SYSTEM OPERATION LOCKED L/P UNLOCKED TO UPDATE LOCKED DUE TO FAULT CODE 27-52261 FOUND DURING FSEU BITE PLEASE REMOVE PERFORMED FSEU BITE PROCEDURE 27-51 TASK 801 NO EXISTING FAULS AND REPLACE LEFT FLAPSDR CALA2022030900620Transducer · faultedANTI SKID INOP LIGHT CAME ON AFTER T/O RETURNED TO DENVER LIGH T WENT OUT ON APRCH IN J33 KE2,KG2.CHECK PIN CRIMPS AND PIN TENSION ON MONITOR PINS B12 AND B13 AT ANTISKID/AUTOBRAKE CONTROLLER D1040A CONNECTOR D11124 PINS 1 AND 3.ISSUE IS PROBABLY IN THE GEARSDR CALA2022030900617Channel · corroded(SUPPORT TASK) FLOOR SUPPORT BS 991-1015 LBL31 CORRODED IN AFT M AIN CABIN REMOVED CORRODED FLOOR SUPPORT AND INSTALLED NEW FLOOR SUPPORT P /N 147A5710U16 IAW BOEING DWG #1417A5700 REV "A". DATA WAS TRANS CRIBED FROM PAPER DOC AERSALE WO 3545 NR 25760 ACP BY MSDR CALA2022030900611Beam · corrodedMAIN CABIN AFT WET AREA STA 986.5 RBL 4" FLOOR BEAM UPPER SURFACE CORROSION (REF AAR NR 9641538) REMOVED EXISTING REPAIR AT MAIN CABIN AFT WET AREA STA 986.5 FLOOR BEAM AS PER B737-800 SRM 51-40-02 AND EC/RA #5320-02466. INSTALLED NEW T-CHORD AT MAIN CABIN AFSDR CALA2022030700564Pump · inoperativeLEFT CENTER BOOST PUMP PRESS LIGHT STAYS ON. RESET BOOST PUMP. PUMP FAILED. C.B. OUT AGAIN. C.B. OUT AND ITEM PLACED ON MEL. CAPPED. DISPATCH DESK: 29 NAME: JBDATE: 02-MAR-22- NOC DESK: 737 NAME: DZ DATE: 02-MAR-22- TOMC APPROVED. REPLACED R54 NO HELSDR CALA2022030700608None · illuminatedLEFT FWD OVERWING LIGHT ILLUMINATED ON TAKEOFF PLACED ON MEL 5215. LEFT FWD OVERWING EXIT DOOR FLIGHT LOCK SYSTEM INOP. DDP C/W. INSTALLED JUMPER 5220DD11102-5 ON PSEU CONNECTOR D10986. JUMPER MUST BE RETURNED TO YELLOW BAG LABELED PSEU JUMPERS IN THE EE BAYSDR CALA2022030700604Beam · corrodedMAIN CABIN AFT WET AREA STA 986.5 RBL 4" FLOOR BEAM UPPER SURFACE CORROSION (REF AAR NR 9641538) REMOVED EXISTING REPAIR AT MAIN CABIN AFT WET AREA STA 986.5 FLOOR BEAM AS PER B737-800 SRM 51-40-02 AND EC/RA #5320-02466. INSTALLED NEW T-CHORD AT MAIN CABIN AFSDR CALA2022030700579Brake · damaged#1 BRAKE DAMAGED DUE TO SUSPECTED WHEEL BEARING FAILURE. REPLACED NUMBER # 1 BRAKE IAW 32-41-41. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1935536 SN OFF 1388 BRAKE, MLG, CAR OFF 60-3241-9-0001 1388 ON 60-3241-9-0001 4389SDR CALA2022030700575Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRACKED. SUPPORT TASK NSA EMX NR 00091. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 RBL 54.60 IAW B737-800 SRM 51-40-02 AND DWG 111A2000 REV ORG. DATA WAS TRA NSCRIIBED FROM EMX 00091 WORK SDR CALA2022030700574Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 40.87 IS CRACKED. SUPPORT TASK NSA EMX NR 00090. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 RBL 40.87. 3/4/22 IAW B737-800 SRM 51-40-02 AND DWG 111A2000 REV ORIGINAL. DATA W AS TRANSCRIBED FROM NSSDR CALA2022030700573Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX NR 00089. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 RBL 32.40 2 IAW B737-800 SRM 51-40-02 AND DWG 111A2000 REV. ORIGINAL DATA WA S TRANSCRIBED FROM EMX 00089
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