Boeing 737-7Q8
Service difficulty reports · 3,964
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 = '7377Q8' 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 = '7377Q8' 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 SWAA2023040413532Attach Angle · corrodedCORROSION ON AFT CARGO BAY INTERCOSTAL ATTACH ANGLE BS 767+2 WL 157 RBL 21<[01] EVALUATED CORROSION ON ATTACH ANGLE BS 767+2 RBL 21 WL 157; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] VERIFIED CORRECSDR SWAA2023040413530Intercostal · corrodedCORROSION ON AFT CARGO BAY INTERCOSTAL BS 787+9 RBL 6 WL 153<[01] EVALUATED CORROSION ON INTERCOSTAL BS 787+9 RBL 6 WL 153; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] VERIFIED CORRECTIVE ACTIONS STESDR SWAA2023040414113Angle · crackedCRACKED ATTACH ANGLE AT MID PAX CABIN BS663+28 RBL1 WL207.<[01] NOT ALLOWABLE LIMITS APPLICABLE FOR SPECIFIC LOCATION PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED ATTACH ANGLE AT MID PAX CABIN BS663+28 RBL1 WL207 I.A.W SRM 51-40SDR SWAA2023040414111Attach Angle · crackedCRACKED ATTACH ANGLE AT MID PAX CABIN BS663+30 RBL23 WL203.<[01] NOT ALLOWABLE LIMITS APPLICABLE FOR SPECIFIC LOCATION PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED ATTACH ANGLE AT MID PAX CABIN BS663+30 RBL23 WL203 I.A.W SRM 51-SDR SWAA2023040414114Floor Support · crackedCRACKED FLOOR SUPPORT AT MID CABIN BS540 LBL1 WL208.<[01] NO ALLOWABLE DAMAGE FOUND ON SRM PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C REPLACEMENT OF THE PART;[02] REMOVED DAMAGED BREAK PANEL AT STA 540 LBL 1; WL 207 IAW SRM 51-40-02-0G-0.;SDR SWAA2023040314107Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-25R RBL22. WL155. MARKED<[01] REMOVED DAMAGED SECTION OF STR 25R BS 500D+11' TO BS 540 IAW SRM 53-00-03-2R-1 REP.1;[07] HFEC INSPECTED CUTOUT AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR><BRSDR SWAA2023033013533Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACKS ON AFT CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(2) AND (4)<BR>EQUIP USED;<BR>WELDING MACHINE E10583; CAL DUE 01/2024;[02]SDR SWAA2023040413498Shield · corrodedMULTIPLE AREA OF CORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847-867.<[01] EVALUATED CORROSION ON SHIELD BS 847-867 RBL 21 WL 164; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] VERIFIED CORSDR SWAA2023040413516Nut Plate · corrodedCORROSION ON AFT CARGO BAY NUT PLATE BRACKET AT BS 787+8 RBL 19.<[01] EVALUATED CORROSION ON NUTPLATE STRIP BS 787+8 RBL 19 WL 157; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] VERIFIED CORRECTIVE ACTSDR SWAA2023040413517Shield · corrodedMULTIPLE AREA OF CORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 21 BS 767-787.<[01] EVALUATED CORROSION ON SHIELD BS 767-787 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] VERIFIED CORSDR SWAA2023040413518Support · corrodedMULTIPLE AREA OF CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727+5-767.<[01] EVALUATED CORROSION AT ALL LOCATION OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 747+10 RBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIGINAL 0.04SDR SWAA2023040413505Support · corrodedMULTIPLE AREA OF CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727+5-727E+7.<[01] EVALUATED CORROSION AT ALL LOCATION OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 727D+10 LBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIGINAL SDR SWAA2023040413519Support · corrodedMULTIPLE AREA OF CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727E+10-847.<[01] EVALUATED CORROSION AT ALL LOCATION OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 767+10 LBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIGINAL 0.SDR SWAA2023040413514Shield · corrodedMULTIPLE AREA OF CORROSION ON FWD CARGO BAY FWD DOOR SHIELD AT RBL 24 BS 420+10-420+18 WL 157.<[01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] LOCATED AND DRILLED NEW FWD DOOSDR SWAA2023040413528Shield · corrodedMULTIPLE AREA OF CORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 24 BS 480+15-500+11 WL 157.<[01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] LOCATED AND DRILLED NEW AFT DOOSDR SWAA2023040313521Stringer · crackedCRACK ON FWD CARGO BAY END OF STRINGER AT BS 540 STRINGER 23R.<[01] REQUEST NDI VERIFY CRACK IN STRINGER END;[02] ACCOMPLISHED HFEC SURFACE SCAN IAW 73 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. VERIFIED CRACK IS PRESENT IN STRINGER END; 0.5'L.<BR><BR>EQUIPMENSDR SWAA2023040313526Angle · crackedCRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH ANGLE AT LBL 24 BS 500A+19 WL 156.<[01] CRACK ON CLIP FOUND TO BE OUT OF LIMITS DUE TO NO LIMIT ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED AND REPLACED FWD CARGO BAY BAFFLE FRAME ATTSDR SWAA2023040313496Bracket · crackedCRACK ON AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+8 RBL 12.<[01] EVALUATED STIFFENER BS 907+8 RBL 12 WL 170.5; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] REMOVED DAMAGED AFT CARGO BAY WATER SERSDR SWAA2023040313529Support · corrodedMULTIPLE AREA OF CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500A+2-500C+18 WL 157.<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500C+2' REMOVED 0.015' IN AN AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TSDR SWAA2023033013492Stiffener · crackedCRACK ON AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+12 RBL 12.<[01] EVALUATED STIFFENER BS 907+12 RBL 12 WL 170.5; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[SDR SWAA2023033013504Track · crackedCRACK ON AFT CARGO BAY TRACK AT LBL 17 BS 727C.<[01] CRACK ON CARGO TRACK WAS FOUND TO BE OUT OF LIMITS.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED AFT CARGO BAY TRACK AT LBL 17 BS 727+4 - BS 867 IAW SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW AFTSDR SWAA2023032412899Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED ON ACCESS PANEL 651FB AT RT WING 2023-165233<[01] REPLACED SUPPORT BRACKET LOCATED ON ACCESS PANEL 651FB AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2710; SHEET 6; REV: B;[02] REPLACED SUPPORT BRACKET SDR SWAA2023032313017Scuff Plate · crackedCRACK ON SCUFF PLATE (CENTER) AT FWD SERVICE DOOR 2023-165240<[01] TOOL USED: DIGITAL CALIPER P/N: 500-193-30 S/N:0000293 DUE DATE: 12/OCT/23;[02] REPAIRED BY WELDING SCUFF PLATE (CENTER) AT FWD SERVICE DOOR I.A.W. BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 ANDSDR SWAA2023033012272Panel · chafedPANEL 194AR MATING SURFACE IS CHAFED.<[01] IDENTIFIED 194AR PANEL IAW SRM 53-60-70-0I-1 PARA FIGURE 2; ITEM 1; TABLE 2<BR><BR>FOUND DAMAGE TO BE WITHIN ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1 PARA 4.B.(8).<BR><BR>WILL PERFORM WORK IAW SRM 53-60-70-1A-1 PARA 2.ASDR SWAA2023032412560Skin · crackedCRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.100 INCHES 2023-165218<[01] TOOL USED: CALIPER; PN: 500-752-20; SN: B20317422; DUE DATE: 29-AUG-23.;[0SDR SWAA2023032412558Plate · crackedCRACK TRAILING EDGE CORRUGATED PLATE LOCATED ORSS 261 AT LT WING 2023-165210<[01] REPLACED CORRUGATED PLATE AND LOCATED ON ORSS 261 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 22 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] RESDR SWAA2023032412557Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS 287 LOWER SIDE RT WING 2023-165217<[01] REPLACED ANGLE AND FASTENERS LOCATED ORSS 287 LOWER SIDE RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A3700 SHEET 27 REV - ; SEE INDIVIDUAL SING-OFF BELOW.;[02] CORRECTED STEP 1<BR>SDR SWAA2023032412548Angle · crackedCRACK SUPPORT ANGLE LOCATED DEFLECTION CONTROL AT LT WING 2023-165209<[01] REPLACED NEW SUPPORT ANGLE LOCATED DEFLECTION CONTROL AT LT WING I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUSDR SWAA2023032412547Plate · corrodedCORROSION GROUND SPOILER SEAL-PLATE AT LT WING 2023-165207<[01] REPLACED PLATE LOCATE ON GROUND SPOILER AT LT WING IAW B737-700 SRM 51-10-02; Ï¿½TEM 9 AND DRAWING 115A2512 SHEET 8 REV C<BR>SEE INDIVIDUAL SING OFF BELOW.;[02] CORRECTED STEP 1. <BR>REPLACED PLATSDR SWAA2023032412546Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 375 UPPER SIDE AT LT WING 2023-165201<[01] REPLACED TRAILING EDGE ANGLE LOCATED ORSS 375 UPPER SIDE AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] TASK COMPLETED <BRSDR SWAA2023032412545Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 407 UPPER SIDE AT LT WING 2023-165200<[01] REPLACED TRAILING EDGE ANGLE LOCATED ORSS 407 UPPER SIDE AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] CORRECTED STEP 1. REPLACED TRAILING EDGE ANGLE LOCASDR SWAA2023032412553Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 459 UPPER SIDE AT RT WING 2023-165212<[01] REPLACED TRAILING EDGE ANGLE AND FASTENERS LOCATED ORSS 459 UPPER SIDE AT RT WING IAW B737-700 SRM 51-10-02 ITEM ITEM 9 AND DRAWING # 115A3551 REV - SEE INDIVIDUAL SIGNOFFS BSDR SWAA2023032412555Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 404 UPPER SIDE AT RT WING 2023-165214<[01] REPLACED ANGLE AND FASTENERS LOCATED ORSS 404 UPPER SIDE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE AND FASDR SWAA2023032412556Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 287 UPPER SIDE AT RT WING 2023-165216<[01] REPLACED ANGLE AND FASTENERS LOCATED ORSS 287 UPPER SIDE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED ANGLE AND FSDR SWAA2023032412544Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 468 UPPER SIDE AT LT WING 2023-165199<[01] REPLACED ANGLE AND FASTENERS LOCATED ORSS 468 UPPER SIDE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OFF BELOW.;[02] CORRECTED STEP 1<BR>SDR SWAA2023032412554Angle · corrodedCORROSION TRAILING EDGE ANGLES LOCATED ORSS 416 UPPER SIDE AT RT WING 2023-165213<[01] REPLACED ANGLE AND FASTENERS LOCATED ORSS 416 UPPER SIDE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED ANGLE AND SDR SWAA2023032412559Angle · corrodedCORROSION TRAILING EDGE ANGLE LOCATED ORSS 369 UPPER SIDE AT RT WING 2023-165215<[01] REPLACED ANGLE AND FASTENERS LOCATED ORSS 369 UPPER SIDE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.;[02] REPLACED ANGLE AND FASTENERS LOCATED ORSS 369 UPPESDR SWAA2023032312217Structure · missingMISSING DOOR CUTOUT RETAINER UPPER SILL AT FWD CARGO COMPARTMENT (8 EA) 2023-165148<[01] REPLACED RETAINER LOCATED UPPER AREA DOOR CUT OUT AT LEVEL STR18R AT FWD CARGO COMPARTMENT (3 EA) IAW B737-700 SRM 51-10-02 ITEM 9.;[02] REPLACED RETAINER LOC. DOOR CUTOUTSDR 2023FA0000114Hose · wornABORTED TAKEOFF, AIRSPEED DISPLAY HOW IAS DISAGREE MESSAGE FRM 34204631. CORRECTIVE ACTION: HASE BEEN REPLACED FLEXIBLE HOSE IAW AMM 20-10-52/401 IN TEST ON GROUND OKSDR SWAA2023030211637Slide · out of adjustL1 ENTRY DOOR SLIDE FALLING OUT OF BUSTLE<[01] REINSTALLED L1 ESCAPE SLIDE AND BESSEL IAW MT 725-61-06SDR SWAA2023032411460Barrier · crackedCUSTOMER REQUEST CRACK ON VAPOR BARRIER LOCATED AT STA663 LH SIDE 2023-164955<[01] TOOL USED: CALIPER P/N: 500-193-30; S/N: 0000288; DUE DATE: 17-DEC-23.;[02] TOOL USED: HOT BONDER P/N:HCS9200B-AV S/N:18185781 DUE DATE: 24-JAN-24;[03] TOOL USED: SCALE P/N:SPX6SDR SWAA2023032411462Angle · crackedCRACK ON ANGLE LOCATED FLOOR STRUCTURE BS 695 LBL 24.75 AT CENTER SECTION 2023-164965<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FSDR SWAA2023032411463Angle · crackedCRACK ON ANGLE LOCATED FLOOR STRUCTURE BS 695 RBL 24.75 AT CENTER SECTION 2023-164966<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FSDR SWAA2023032411458Slat · crackedCRACK ON EXTERNAL SKIN LEADING EDGE LOCATED SLAT 6 ON SLAT STATION 202.45 AT RT WING 2023-164956<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 200053402 AND DUE DATE: 13-MAY-23.;[02] REMOVED AND REPLACED L/E SLAT 6 RT WING IAW B737-700 AMM 27-81-21-0SDR SWAA2023030311677Girt Bar · out of adjustFWD ENTRY DOOR; FWD GIRT- BAR FITTING LOOSE 2023-109683<[01] INSTALLED CORRECTLY FWD ENTRY DOOR; FWD GIRT- BAR FITTING AIW B737-700 AMM 25-66-02-400-801;[02] TASK COMPLETEDSDR SWAA2023030110299Battery Pack · inoperativeAFT LH EMERGENCY LIGHTS INOP<[01] RR AFT GALLEY LH EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-06SDR SWAA2023022104913Battery · faultyBOTH MEGAPHONES REQUIRE NEW BATTERIES.<[01] R&R'D BATTERIES AND INSPECTION TAG PER AMM 25-64-00SDR SWAA2023021603045Sign · out of adjustL1 AND R1 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARRROW.<[01] REMOVED AND REPLACED LENS IAW CMM 25-31-03;[02] INSPECTEDSDR SWAA2023030202324Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE LOCATED FWD FACE SUPPORT BEAM MAIN LANDING GEAR RT WING 2023-109646<[01] TOOL USED CALIPER PN 500-196-30 SN B21141563 CAL DUE DATE 30 NOV 23 AND RADIUS GAUGE PN 2204A3 SN AE-29974 CAL DUE DATE 15 JUL 23.;[02] TOOL USED: TEMPSDR SWAA2023030202325Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED WS278.5 DEFLECTION CONTROL RIB AREA RT WING 2023-109645<[01] REPLACED ANGLE TRAILING EDGE LOCATED WS278.5 DEFLECTION CONTROL RIB AREA RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] CORRECTED STEP 1. REPLACED AN
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