Boeing 737-7CT
Service difficulty reports · 2,414
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 = '7377CT' 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 = '7377CT' 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 SWAA2024050983471Battery Pack · failedBATTERY PACK M1674 FAILED CAPACITY CHECK. BATTERY PACKS M1674 AND M1675 FAILED CAPACITY CHECK.<[01] R&R BATTERY PACKS M1674 AND M1675 IAW AMM 33-51-06.SDR SWAA2024050984027Battery Pack · failedBATTERY PACK M1674 FAILED CAPACITY CHECK. BATTERY PACKS M1674 AND M1675 FAILED CAPACITY CHECK.<[01] R&R BATTERY PACKS M1674 AND M1675 IAW AMM 33-51-06.SDR SWAA2024043080548Slide · out of positionF/A REPORTS FWD SERVICE DOOR SLIDE HARD TO ARM<[01] REMOVED FWD SERVICE DOOR SLIDE AND REPOSITIONED IN SLIDE CASE PER MT 725-61-06 AND REINSTALLED PER AMM 25-66-01.SDR SWAA2024040470177Sign · brokenAFT CEILING EMERGENCY EXIT SIGN BROKEN<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLACEMENT - PERMANENT)]SDR SWAA2024032165799Doubler · crackedELECTRICAL GROUND POWER RECEPTACLE (EGPR) SURROUND DOUBLER HAS A 0.50 CRACK 2.25 INCHES BELOW CENTER LATCH RUBBING STRIP.<[01] REPAIRED DAMAGE ON EXTERNAL POWER DOOR SURROUND DOUBLER PER SRM 53-10-15-1A-4;[02] PERFORMED HIGH FREQUENCY EDDY CURRENT (HFEC) INSPESDR SWAA2024031864781Fastener · missingMISSING SLIDE FASTENER ON L1 DOOR SLIDE<[01] INSTALLED MISSING FASTENER PER AMM 20-50-11SDR SWAA2024031563927Battery Pack · inoperativeEMERGENCY LIGHTS INOP IN AFT GALLEY.<[01] R/R BATTERY PACK M1673 PER AMM 33-51-06.SDR SWAA2024031161172Sign · looseOVERHEAD EXIT SIGN OVER THE EXIT ROW IS LOOSE<[01] EXIT SIGN LIGHT ASSY WAS REMOVED FOR TROUBLESHOOTING IAW AMM 33-51-01.;[02] R/R EXIT SIGN LIGHT ASSY OVER THE EXIT ROW IAW AMM 33-51-01. OPS CHECK GOOD.SDR SWAA2024022957102Slide · dislodgedR1 DOOR SLIDE REQUIRES REPLACEMENT (DISLODGED)<[01] UPON FURTHER INSPECTION THE SLIDE WAS DETERMINED TO BE IN SERVICEABLE CONDITION. RE-INSTALLED R1 DOOR SLIDE PER AMM 25-66-00 & MT725-61-06 75351SDR SWAA2024021651671Bracket · crackedLEFT WING #2 SLAT INBOARD AUX TRACK SKIN TAB BRACKET CRACKED<[01] R&R LEFT WING #2 SLATE INBOARD AUX TRACK SKIN TAB BRACKET PER AMM 20-50-11.SDR SWAA2024021551661Battery Pack · no testEMX BATT PACK M01675 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01675 PER AMM 33-51-06SDR SWAA2024021551660Battery Pack · no testEMX BATT PACK M01672 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01672 PER AMM 33-51-06SDR SWAA2024012343553Hmu · faultedTOD AT 380; NR 1 ENG EXPERIENCED VIBRATION/SHUTTER W/ROLLBACK. ENGINE RECOVERED; THEN ANOTHER SHUDDER; THEN ROLLBACK SHUTDOWN ENGINE AND CONTINUED TO DEN. NO EGT LIMITS EXCEEDED. ON LANDING; BOTH (CONTD) (CONTD FROM ABOVE) ENGINE CONTROL LIGHTS ILLUMINATED<[01SDR SWAA2024012242478Handle · brokenL1 DOOR ASSIST HANDLE BROKEN<[01] SWAPPED ASSIST HANDLE IIN FWD LAV WITH L1 DOOR HANDLE OK TO CONT PER MEL 25-10-01 SP 1B AUTH CODE 175984;[02] INSTALLED NEW ASSIST HANDLE AT FWD LAV PER S.I.PSDR SWAA2023122133492Skirt · out of adjustL2 DOOR SLIDE SKIRT NEEDS ADJUST. IT HITS SCUFF PLATE WHEN CLOSING DOOR<[01] ADJUSTED L2- DOOR SLIDE SKIRT AS PER AMM 25-66-01-000-801;[02] VERIFIED STEP 1SDR SWAA2023122133488Skirt · out of adjustR2 DOOR SLIDE SKIRT NEEDS ADJUST. IT HITS SCUFF PLATE WHEN CLOSING DOOR<[01] ADJUSTED R2- DOOR SLIDE SKIRT AS PER AMM 25-66-01-000-801;[02] VERIFIED STEP 1SDR SWAA2023122131831Battery Pack · inoperativeMULTIPLE EMERGENCY LIGHTS INTERIOR/EXTERIOR INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS<BR>M2335 BATTERY PACK STA 500C LEFT<BR>M1670 BATTERY PACK STA 727C LEFT<BR>M1673 BATTERY PACK STA 952 LEFT<BR>I/A/W BOEING AMM 33-51-06-960-805; OPS CHECKSDR SWAA2023122134441Battery Pack · inoperativeMULTIPLE EMERGENCY LIGHTS INTERIOR/EXTERIOR INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS<BR>M2335 BATTERY PACK STA 500C LEFT<BR>M1670 BATTERY PACK STA 727C LEFT<BR>M1673 BATTERY PACK STA 952 LEFT<BR>I/A/W BOEING AMM 33-51-06-960-805; OPS CHECKSDR SWAA2023122134442Battery Pack · inoperativeMULTIPLE EMERGENCY LIGHTS INTERIOR/EXTERIOR INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS<BR>M2335 BATTERY PACK STA 500C LEFT<BR>M1670 BATTERY PACK STA 727C LEFT<BR>M1673 BATTERY PACK STA 952 LEFT<BR>I/A/W BOEING AMM 33-51-06-960-805; OPS CHECKSDR SWAA2023122131068Light · damagedEMERGENCY LIGHT ASSEMBLY ON G4 DAMAGED<[01] REMOVED AND REPLACED LIGHT ASSEMBLY I/A/W ENCORE CMM 25-31-05; OPS CHECK FOUND NORMAL;[02] VERIFIED STEP 1SDR SWAA2023121830941Skin · handler errorPROVO TRUCK COLLIDED WITH CAPT SIDE ENTRY AFT DOOR<[01] REPAIRED ON EA 23-153-03617 (N569WN - SWA - REPAIR - SECTION 47 FUSELAGE SKIN DAMAGE BETWEEN STA 914 - 937 AND BETWEEN STR 20L AND 21L) [TTG8Q00QBG9R]SDR SWAA2023121830942Stringer · crackedREF TO LP 2398631 FOUND DAMAGE CAUSED BY PROVO TRUCK IN BETWEEN STATIONS 914-937 AND STRINGERS S-20L & S-21L LENGTH OF 7-12/32 AND WIDTH OF 15-8/32 13/64TH DEEP FOUND SHEAR TIE AT STATION 927 CRACKED BETWEEN STRINGERS S-20L & S-21L<[01] REPAIRED PER EA 23-153-SDR SWAA2023122125815Beam · corrodedMAIN CABIN AFT WET AREA FLOOR BEAM AT STA 986.5 LBL 44' HAS EXFOLIATING CORROSION THAT IS OUT OF LIMITS<[01] REPAIRED MAIN CABIN AFT WET AREA FLOOR BEAM AT STA 986.5 LBL 44' REF SRM 53-70-51-2R-6;[02] RII VERIFIED STEP 1;[03] COMPLETED SME INSPECTION OF WORKMASDR SWAA2023122125458Seal · crackedRIGHT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 343AT BLADE METAL SEAL CRACKED<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STAB UPPER GAP COVER ACCESS PANEL 343AT BLADE METAL SEAL REF SRM 51-40-02-0G-0;[02] VERIFIED STEP #1SDR SWAA2023122125459Seal · deterioratedLEFT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 332AT RUBBER SEAL DETERIORATED AND BROKEN PIECE AT END TIP.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 332AT RUBBER SEAL AS PER SRM 51-40-02-0G-0;[02] VERIFIED STEP SDR SWAA2023122125220Floor Panel · crackedMAIN CABIN FLOOR PANEL #221GF FWD SECTION TIP CRACKED<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON MAIN CABIN FLOOR PANEL 221GF AS PER B737 SRM 53-00-50-2R-6 PARAG 3-G-M; MATERIAL USED PO#1798939; PO#1690463.;[02] VERIFIED AND INSPECTED STEP #1. PSDR SWAA2023122124947Seal · crackedLEFT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 333AT BLADE SEAL CRACKED.<[01] REMOVED AND REPLACED BLADE SEAL AT LEFT HORIZONTAL STABILIZER UPPER GAP COVER PANEL REF SRM 51-40-02-0G-0;[02] VERIFIED STEP #1SDR SWAA2023122124939Floor Panel · crackedMAIN CABIN STA 540 RBL 2' FLOOR PANEL BREAK CRACK<[01] REMOVED AND REPLACED FLOOR PANEL BREAK AT MAIN CABIN STA 540 RBL 2' AS PER SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED FLOOR PANEL BREAK AT MAIN CABIN STA 540 RBL 2' AS PER SRM 51-40-02-0G-0; BOEING DWG #SDR SWAA2023122124940Floor Panel · crackedMAIN CABIN STA 540 LBL 2' FLOOR PANEL BREAK CRACK<[01] REMOVED AND REPLACED FLOOR PANEL BREAK AT MAIN CABIN STA 540 LBL 2' AS PER SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED FLOOR PANEL BREAK AT MAIN CABIN STA 540 LBL 2' AS PER SRM 51-40-02-0G-0; BOEING DWG #SDR SWAA2023122124942Floor Panel · frayedMAIN CABIN FLOOR PANEL 241ZF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 241ZF AND WILL BE INSTALLED ON T/C TTG8Q00PDXP8.;[02] VERIFIED STEP 1SDR SWAA2023122124934Floorbeam · corrodedMAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM STA 986.5 LBL 2'- 44'<[01] REMOVED NUTPLATE FOR ACCESS AS PER SRM 51-40-02-0G-0. CLEANED CORROSION AS PER SRM 51-10-02-0G-0 <BR>ORIGINAL THICKNESS 0.150'; MATERIAL REMOVED FROM LBL 2' THROUGH LBL 43: 0.001'; MATESDR SWAA2023122124936Strap · corrodedMAIN CABIN AFT WET AREA CORROSION AT FLOOR SUPPORT STRAP STA 1016+11' RBL 17'<[01] CLEANED AFT WET AREA AT FLOOR SUPPORT STRAP STA 1016+11' RBL 17'AS PER SOPM REF 20-30-03;[02] CLEANED AFT WET AREA AT FLOOR SUPPORT STRAP STA 1016+11' RBL 17'AS PER SOPM REF 20-SDR SWAA2023122124926Seal · crackedVERTICAL FIN L/H HORIZONTAL BOX HINGE CUTOUT UPPER SLIDING SEAL FWD GUIDE TRACK TIP CRACKED<[01] REMOVED AND REPLACED BOX HINGE CUTOUT UPPER SLIDING SEAL TRACK AT L/H HORIZONTAL STAB REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2023122124927Seal · crackedVERTICAL FIN R/H HORIZONTAL BOX HINGE CUTOUT UPPER SLIDING SEAL FWD GUIDE TRACK TIP CRACKED<[01] REMOVE AND REPLACE TRACK ASSY REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2023112825056Handle · looseFWD ENTRY DOOR INTERIOR HANDLE LOOSE. MOVES UP APPROX 1 DURING FLIGHT<[01] C/W GUIDE ARM ADJUSTMENT ON FWD ENTRY DOOR PER MT 752-11-01SDR SWAA2023112824735Girt Bar · out of adjustFWD ENTRY DOOR (L1) GIRT BAR WILL NOT SEAT<[01] REPACKED L1 SLIDE PER MT725-61-06. GIRT BAR STOWS PROPERLYSDR SWAA2023112724727Slide · out of limitsAFT LEFT EMERGENCY ESCAPE SLIDE PRESSURE GAUGE BELOW LIMITS.<[01] REMOVED AND REPLACED AFT ENTRY DOOR ESCAPE SLIDE REF MM 25-66-01.SDR SWAA2023122124228Scuff Plate · crackedFOUND CRACK AT AFT CARGO COMPT. AFT CORNER SCUFF PLATE.<[01] RECEIVED REPAIRED AFT CARGO COMPT AFT CORNER SCUFF PLATE FROM OUTSIDE VENDOR (PN: 146A8343-7 PO: 2043476). SCUFF PLATE WILL BE INSTALLED PER TASK CARD TTG8Q002GEYU.;[02] VERIFIED STEP 1SDR SWAA2023122124238Floor Panel · frayedMAIN CABIN FLOOR PANEL 222DF UPPER SURFACE FRAYING<[01] RECEIVED FLOOR PANEL 222DF. INSTALLATION WILL BE ACCOMPLISHED ON TASKS CARD TTG8Q00PDYQU.;[02] VERIFIED STEP 1SDR SWAA2023122124239Floor Panel · frayedMAIN CABIN FLOOR PANEL 221CF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 221CF AND WILL BE INSTALLED ON T/C TTG8Q00PDYRA;[02] VERIFIED STEP 1SDR SWAA2023122124232Intercostal · crackedMAIN CABIN RBL 12' BETWEEN STA 344-360 INTERCOSTAL CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN RBL 12' BETWEEN STA 344-360 AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED STEP 1SDR SWAA2023122124227Intercostal · crackedMAIN CABIN RBL 10' BETWEEN STA 380-400 INTERCOSTAL UPPER ANGLE CRACK<[01] REMOVED AND REPLACED INTERCOSTAL UPPER ANGLE. AS PER; SRM 51-40-02-0G-0 AND DWG 143A5400.;[02] VERIFIED STEP 1SDR SWAA2023122124233Intercostal · crackedMAIN CABIN LBL 46' BETWEEN STA 312-328 INTERCOSTAL CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN LBL 46' BETWEEN STA 312-328 AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED STEP 1SDR SWAA2023122124235Intercostal · crackedMAIN CABIN LBL 13' BETWEEN STA 380-400 INTERCOSTAL UPPER ANGLE CRACK<[01] REMOVED AND REPLACED INTERCOSTAL UPPER ANGLE AT MAIN CABIN LBL 13' BETWEEN STA 380-400. IN ACCORDING WITH SRM 51-40-02-0G-0 AND DWG 143A5400.;[02] REJECT: SEVERAL RIVETS NOT BUCK PROPERLSDR SWAA2023122124234Door Frame · crackedMAIN CABIN LH STA 303.9 INNER CHORD CRACK<[01] REMOVED AND REPLACED INNER CHORD AT MAIN CABIN L1 SRM 51-40-02-0G-0 AND DWG 141A8110;[02] VERIFIED STEP 1SDR SWAA2023122124231Intercostal · crackedMAIN CABIN BL 0' BETWEEN STA 344-360 INTERCOSTAL CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BL 0' BETWEEN STA 344-360 AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED; STEP # 1.SDR SWAA2023122124241Intercostal · crackedMAIN CABIN BL 0' BETWEEN STA 277-294.5 INTERCOSTAL CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BL 0' BETWEEN STA 277-294.5 AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED; STEP # 1.SDR SWAA2023122124230Intercostal · crackedMAIN CABIN LBL 11' BETWEEN STA 344-360 INTERCOSTAL CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN LBL 11' BETWEEN STA 344-360 AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED; STEP # 1.SDR SWAA2023122124236Intercostal · crackedMAIN CABIN BL 0' BETWEEN STA 380-400 INTERCOSTAL UPPER ANGLE CRACK<[01] REMOVED AND REPLACED INTERCOSTAL UPPER ANGLE AT MAIN CABIN BL 0' BETWEEN STA 380-400 AS PER SRM 51-40-02-0G-0 AND BOEING AIRCRAFT DWG # 143A5400.;[02] VERIFIED STEP 1SDR SWAA2023122124458Support Angle · corrodedMAIN CABIN FWD WET AREA INNER CHORD SUPPORT ANGLE LBL 60' BETWEEN STA 294.5-328 UPPER SURFACE CORROSION<[01] REMOVED AND REPLACED SUPPORT ANGLE AT MAIN CABIN FWD WET AREA INNER CHORD LBL 60' BETWEEN STA 309 TO 343 SRM 51-40-02-0G-0 AND DWG141A8110;[02] VERIFIE
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