Boeing 737-79P
Service difficulty reports · 2,376
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 = '73779P' 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 = '73779P' 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 SWAA2023121807972Floor Panel · peelingFWD CABIN FLOOR PANEL 222BF UPPER SKIN SURFACE PEELING.<[01] RECEIVED NEW FLOOR PANEL 222DF; PANEL WILL BE INSTALLED ON TT8Q00NEUM1.;[02] VERIFIED STEP 1SDR SWAA2023121807962Floor Panel · crackedFWD CABIN FLOOR PANEL 221BF LOWER SKIN SURFACE HAS SEVERAL CRACKS.<[01] RECEIVED FWD FLOOR PANEL #221BF WILL BE INSTALLED ON TTG8Q00NEV42;[02] VERIFIED STEP 1SDR SWAA2023121807963Floor Panel · peelingFWD CABIN FLOOR PANEL 221FF UPPER SKIN SURFACE PEELING.<[01] RECEIVED NEW FLOOR PANEL AFT 242PF PANEL WILL BE INSTALL ON TTG8Q00NEV3U;[02] VERIFIED STEP 1SDR SWAA2023121807973Floor Panel · crackedFWD CABIN FLOOR PANEL 221EF UPPER SKIN SURFACE CRACKED.<[01] RECEIVED FWD FLOOR PANEL #221EF WILL BE INSTALLED ON TTG8Q00NEV3W;[02] VERIFIED STEP 1SDR SWAA2023121807974Floor Panel · peelingFWD CABIN FLOOR PANEL 221GF UPPER SKIN SURFACE PEELING.<[01] RECEIVED NEW FLOOR PANEL AFT 242PF PANEL WILL BE INSTALL ON TTG8Q00NEV3S;[02] VERIFIED STEP 1SDR SWAA2023121807975Floor Panel · peelingFWD CABIN FLOOR PANEL 231AF UPPER SKIN SURFACE PEELING.<[01] RECEIVED FWD CABIN FLOOR PANEL#231AF WILL BE INSTALLED ON TTG8Q00NEV3L;[02] VERIFIED STEP 1SDR SWAA2023121807976Floor Panel · crackedFWD CABIN FLOOR PANEL 231AF UPPER SKIN SURFACE CRACKED.<[01] FAULT WILL BE RESOLVED ON ITEM TTG8Q00NUPDY;[02] TTG8Q00NUPDY IS IN THE SAME AREA OF CRACKSDR SWAA2023121807965Floor Panel · peelingFWD CABIN FLOOR PANEL 221CF UPPER SKIN SURFACE PEELING.<[01] RECEIVED NEW FLOOR PANEL 221 CF; PANEL WILL BE INSTALLED ON R/C TTG8Q00NEV40;[02] VERIFIED 1.SDR SWAA2023121807978Floor Panel · peelingFWD CABIN FLOOR PANEL 232BF UPPER SKIN SURFACE PEELING.<[01] RECEIVED NEW FLOOR PANEL AFT 232BF PANEL WILL BE INSTALL ON TTG8Q00NEUVW;[02] VERIFIED STEP 1.SDR SWAA2023121807966Floor Panel · peelingFWD CABIN FLOOR PANEL 221DF UPPER SKIN SURFACE PEELING. RECIEVED NEW CABIN FLOOR PANEL 221DF. INSTALLATION OF FWD WET AREA FLOOR PANEL 221DF ACCOMPLISHED ON CUSTOMER TASK CARD TTG8Q00NEV3Y.SDR SWAA2023121807968Floor Panel · peelingAFT CABIN FLOOR PANEL 242RF UPPER SKIN SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANE 242 RF; P/N 815A0044-4; NEW FLOOR PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00NEV34;[02] VERIFIED STEP 1SDR SWAA2023121807979Floor Panel · crackedAFT CABIN FLOOR PANEL 241ZF LOWER SKIN SURFACE HAS CRACKS.<[01] RECEIVED NEW CABIN FLOOR PANEL P/N 815A0044-7; NEW FLOOR PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00NEUU2;[02] VERIFIED FINAL CORRECTIVE ACTION.SDR SWAA2023121807981Floor Panel · peelingAFT CABIN FLOOR PANEL 242VF UPPER SKIN SURFACE PEELING.<[01] FAULT WILL BE RESOLVED ON ITEM TTG8Q00NUPK8;[02] REJECTED 242VF HAS SEVERAL DAMAGED INSERTS. [TTG8Q00NUPK8] THESE FAULTS ARE NOT THE SAME.;[03] PANEL 242VF WILL BE REPLACED ON ITEM TTG8Q00NUPK8;[04] SDR SWAA2023101608720Battery · inoperativeAFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHTS ARE NOT FLASHING. ( 2 EA. REQUIRED)<[01] REPLACED BATTERY'S AT AFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHTS (2EA) AS PER AMM 25-64-00-900-806;[02] VERIFIED STEP 1.SDR SWAA2023121807788Handle · out of adjustC/R R-2DOOR HANDLE; CHECK TORQUE; SEEMS LOW.<[01] ADJUSTED R-2 DOOR HANDLE AND CHECKED TORQUE<BR>REF B737-700 AMM 52-41-00-820-802;[02] ACCOMPLISHED GALLEY SERVICE DOOR (SOFT UNLATCHING ADJUSTMENT) AT R-2 DOOR<BR>REF B737-700 AMM 52-41-00-820-802SDR SWAA2023101707853Battery Pack · inoperativeEMERGENCY LIGHT INOP FOR POWER SUPPLY/BATTERY PACK M1673<[01] REMOVE & REPLACE BATTERY PACK M1673 PER B737 AMM 33-51-06-960-805. PERFORM TEST OF BATTERY PACK OER B737 AMM 33-51-06-960-805 TEST PASSED;[02] VERIFIED STEP # 1SDR SWAA2023121807529Bracket · crackedLT WING FIXED T/E LATERAL SEAL SUPPORT PANEL O/B BRACKET AT APPROX ORSS 282 I/B SIDE OF DEFLECTION CONTROL RIB IS CRACKED. 124-O04<[01] REMOVED AND REPLACED DAMAGED BRACKET AT LT WING FIXED T/E APPROX ORSS 282 I/B SIDE SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVSDR SWAA2023120507120Skin · crackedCRACK FOUND AT RT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 ; 16.5' FROM FRONT SPAR; I/B ROW. CRACK LENGTH 1.281' CRACK FOUND AT RT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 16.5' FROM FRONT SPAR I/B ROW. CRACK LENGTH 1'<[01] PERFORMED SME SDR SWAA2023120507110Beam · elongatedRIGHT WING TRAILING EDGE STRUCTURE - DEFLECTION CONTROL RIB AND SUPPORT BEAM ATTACHMENT COTTER PINED BOLTS HAVE ELONGATED HOLES.<[01] REMOVED AND REPLACED UPPER BEAM AT RIGHT WING DEFLECTION CONTROL RIB IN REF B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING #115SDR SWAA2023100506809Lamp · inoperativeL/H OVERWING EXIT SIDEWALL LIGHT INOP<[01] RELAMPED PER AMM 33-51-01SDR SWAA2023100506814Light · delaminatedAFT GALLEY ENTRY AREA L/H AND R/H ESCAPE PATH STRIPS DELAMINATED<[01] R&R CABIN PHOTOLUMINESCENT STRIPS PER AMM 33-51-15SDR SWAA2023101704639Flap · delaminatedLEFT WING O/B AFT FLAP I/B UPPER TRAILING EDGE TIP DELAMINATED DOT 223-LWAF2.<[01] FINAL STATEMENT: ACCOMPLISHED UT DISBOND INSP. ON UPPER SKIN AT LEFT WING O/B AFT I/B TRAILING EDGE IAW B737 NDT PART 1; 51-04-00 AND PART 4; 51-00-05. DISBOND NOTED; DAMAGE SIZSDR SWAA2023101704304Flap · delaminatedLEFT WING OUB AFT FLAP INB END LOWER TRAILING EDGE TIP DELAMINATED MKD DOT<[01] FINAL STATEMENT: REMOVED AND REPLACED L/H O/B AFT FLAP REF AMM 27-51-22-000-81 AND 27-51-22-400-801;[02] FINAL INSPECTION; LEFT O/B AFT FLAP REPLACED.SDR SWAA2023092603524Light · inoperativeEMERGENCY EXIT LIGHT ON L/H OWE FWD OF WINDOW LIGHT INOP<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY EXIT LIGHT ON FWD SIDE OF L/H OWE WINDOW LIGHT IAW AMM 33-51-03-960-801.;[02] JOB COMPLETE.SDR SWAA2023092603526Light · inoperativeBULLNOSE EMERGENCY EXIT LIGHT INOP AT SEAT ROW 4ABC<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF BULLNOSE EMERGENCY EXIT LIGHT AT SEAT ROW 4ABC IAW AMM 33-51-03-960-801.;[02] JOB COMPLETE.SDR SWAA2023092603525Light · inoperativeEMERGENCY EXIT LIGHT IN BETWEEN FWD RECESSED CEILING LIGHTS INOP<[01] RELAMPED AND PERFORMED GOOD INSTALLATION TEST OF FWD RECESSED CEILING EMERGENCY EXIT LIGHT IAW AMM 33-51-03-960-801.;[02] JOB COMPLETE.SDR SWAA2023092603523Light · inoperativeEMERGENCY EXIT AREA LIGHT AT SEAT ROW 16FED IS INOP<[01] REMOVED AND REPLACED AREA LIGHT LAMP AT SEAT ROW 16FED OPS CHECK GOOD IAW AMM 33-51-03-960-801.;[02] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.SDR SWAA2023092603382Light · brokenLWH OVERWING EXIT LIGHT FWD OF DOOR CUTOUT IS BROKEN.<[01] REPLACED LWH OVERWING EXIT LIGHT FWD OF DOOR AND GOOD OPERATIONAL TEST PER AMM 33-51-01-960-802.;[02] VERIFIEDSDR SWAA2023092503079Clamp · did not stowFWD ENTRY DOOR SLIDE IS DIFFICULT TO ARM<[01] REPLACED SLIDE CLAMP ASSY PER AMM 25-66-00SDR SWAA2023101902467Battery Pack · inoperativeINOP LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA (2 EA) 2023-578129<[01] REPLACED ON LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA (2 EA) IAW B737-700 AMM 33-51-06-960-805 TEST OK. SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED STEP 1 COMPLETEDSDR SWAA2023101902466Battery Pack · inoperativeINOP LOWERED CEILING PANEL BATTERY PACK AT AFT GALLEY AREA (2 EA) 2023-578130<[01] REPLACED ON LOWERED CEILING PANEL BATTERY PACK AT AFT GALLEY AREA (2 EA) IAW B737-700 AMM 33-51-06-960-805 TEST;[02] CORRECTED STEP 1 REPLACED ON LOWERED CEILING PANEL BATTERY PSDR SWAA2023101602510Floor Panel · crackedAFT CARGO COMPARTMENT PANEL 142KW IS CRACKED AT EDGE(MARKED)<[01] RECIEVED NEW AFT CARGO PANEL # 142KW; WILL BE INSTALLED ON TASK CARD# TTG8Q00MVWFY.;[02] FINAL INSPECTION; RECIEVED NEW AFT CARGO PANEL; WILL BE INSTALLED ON TASK CARD# TTG8Q00MVWFY.SDR SWAA2023092101771Light · inoperativeEMERGENCY EXIT AREA LIGHT IN RIGHT OVERWING ESCAPE HATCH INOP<[01] RELAMPED EMERGENCY EXIT AREA LIGHT IN RIGHT OVERWING ESCAPE HATCH AND TESTED GOOD IAW AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2023101901474Connector · cutCUT ON GALLEY 4 EMERGENCY LIGHT CONNECTOR AT AFT GALLEY AREA 2023-578091<[01] REPAIRED WIRES (2 E/A) OF THE EXIT INDICATOR LIGHT AT AFT GALLEY 4 I.A.W SWPM 20-30-12 AND WDM 33-51-21-11.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED STEP 1 COMPLETEDSDR SWAA2023101901471Support Bracket · crackedCRACK SUPPORT BRACKET BS 277 STR 10R AT FWD GALLEY AREA 2023-578080<[01] REPLACED SUPPORT BRACKET (TIE CLIP) LOCATED BS277 STR 10R AT FWD GALLEY AREA AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 141A1110 SHEET: 18 REV: - SEE INDIVIDUAL SIGN OFF BELOW;[02SDR SWAA2023102001468Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE AT ORSS 239 AT LT WING 2023-578052<[01] REPLACED CORRUGATED PLATE TRAILING EDGE AT ORSS 239 AT LT WING IAW B737-700 SRM-51-40-02 AND DWG-115A2781 REV: -;[02] REPLACED CORRUGATED PLATE TRAILING EDGE AT ORSS 239 AT LT WING IASDR SWAA2023102001470Plate · elongatedELONGATED HOLE TRAILING EDGE CORRUGATED PLATE LOCATED ORSS 261 RT WING 2023-578079<[01] REPLACED CORRUGATED PLATE LOCATED ORSS 261 RT WING I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG# 115A2001; SHEET 32; REV.-.;[02] CORRECTIVE ACTION CERTIFIEDSDR SWAA2023102001467Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AR AT LOWER FUSELAGE 2023-578039<[01] TOOL USED:CALIPER PN: 500-197-30 SN: A18135081; DUE DATE: 21-JUL-24.;[02] TOOL USED HOT BONDER P/N HCS9000B-AV S/N 18185761 DUE DATE 24/SEP/23;[03] TOOL USED SCALE P/N:SPX621 S/N 8340225489 DUE SDR SWAA2023102000766Web · crackedCRACK WEB ON INTERNAL AREA INBOARD FAN COWL ON ENGINE 1 2023-578017<[01] REPLACED WEB ON INTERNAL AREA INBOARD FAN COWL ON ENGINE 1; I.A.W. B737-700 SRM 51-40-02; AND GOODRICH AEROSTRUCTURES CMM 71-13-30; PAGE 10066. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACESDR SWAA2023102000378Angle · crackedCRACK ANGLE LEADING EDGE LOC BS 1016 AND BTW STR 3L TO STR 3R AT VERTICAL STABILIZER 2023-578002<[01] REPLACE ANGLE LEADING EDGE AND FASTENERS LOC BS 1016 AND BTW STR 3L TO STR 3R AT VERTICAL STABILIZER SI IAW B737-700 SRM 51-40-02 DWG 176A3101 REV. - SEE INDISDR SWAA2023102000367Angle · crackedCRACK ANGLE BTW BS 907 TO BS 927 RBL 13.84 AFT CARGO COMPARTMENT 2023-577965<[01] REPLACED ANGLE BTW BS 907 TO BS 927 RBL 13.84 ; S25R TO S27R AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02-0G-0. SRM 51-10-02 AND DWG 147A7221 SHEET 17 REV. D;[02] STEP 1 COSDR SWAA2023102003661Support · wornWEAR ON CHANNEL SUPPORT BTW BS 747 TO BS 767 LBL 13.90 AFT CARGO COMPARTMENT 2023-577968<[01] TOOL P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 12-MAR-24.;[02] REPAIRED CHANNEL SUPPORT BTW BS 747 TO BS 767 LBL 13.90 AFT CARGO COMPARTMENT I.A.W B737-700 SRSDR SWAA2023102003068Angle · wornWEAR BODY FAIRING T ANGLE LOCATED BTW BS663.75 TO BS685 AND LBL28 AT LOWER FUSELAGE 2023-577976<[01] REPLACED T ANGLE LOCATED BTW BS663.75 TO BS685 AND LBL28 AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 DWG 149A7216 SHEET 7 REV. A SEE INDIVSDR SWAA2023101700420Panel · elongatedLEADING EDGE PANEL 521CB HAS MULTIPLE ELONGATED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #521CB AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 SRM 51-70-04-2R-9 PARAG (4-D-M) AND B737 SRM 51-70-04-2R-0 PARAG (4-L-M-N). MATERIAL USED SDR SWAA2023101700424Panel · elongatedLEADING EDGE PANEL 511AT HAS ELONGATED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #511AT AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 SRM 51-70-04-2R-9 PARAG (4-D-M) AND B737 SRM 51-70-04-2R-0 PARAG (4-L-M-N). MATERIAL USED PO#179112SDR SWAA2023101700425Panel · elongatedLEADING EDGE PANEL 521FB HAS ELONGATED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #521FB AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 SRM 51-70-04-2R-9 PARAG (4-D-M) AND B737 SRM 51-70-04-2R-0 PARAG (4-L-M-N). MATERIAL USED PO#179112SDR SWAA2023092699962Panel · crackedCRACKED BREAK PANEL STA 540; RBL 1; WL 208.<[01] UPDATED TABLE;[02] COMPLETED STEPS 1-2; OK TO INSTALL STEP 3.;[03] REMOVED & INSTALLED NEW BREAK PANEL AT BS 540 RBL 1 WL 208 PER SRM 5140-02-0G-0 AND SRM 51-40-05-0G-0 AND BOEING DWG 143A5240SDR SWAA2023092699961Panel · crackedCRACKED BREAK PANEL STA 540; LBL 1; WL 208.<[01] COMPLETED STEPS 1-2; OK TO INSTALL STEP 3.;[02] REMOVED AND REPLACED BREAK PANEL AT BS 540 LBL 1 WL 208 PER SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-00 AND DWG # 143A5240SDR SWAA2023091499908Light · inoperativeFWD ENTRY DOOR FWD WALL EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED FWD ENTRY DOOR FWD WALL EXIT SIGN PER AMM 33-51-01.OPS CHECK GOOD.SDR SWAA2023102099583Floor Support · corrodedCORROSION FLOOR STRUCTURE INNER CHORD LOCATED BS986.5 RBL 60 AND WL 208.1 AFT GALLEY AND LAV 2023-577884<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] REPLACED INNER CHORD LOCATED BS887 + 6 INCHES TO BS1006
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