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 SWAA2023050119326Channel · corrodedCORROSION SPOTS ON AFT CARGO COMPARTMENT ZEE CHANNEL B.S.727B - 727D RBL. 22' W.L. 156. (51-002) CORROSION SPOTS ON AFT CARGO COMPARTMENT EE CHANNEL B.S.727B - 727D RBL. 21' W.L. 156.<[01] REF TASK CARD: TTG8Q00JZHM2 FOR AFT CARGO COMPARTMENT ZEE CHANNEL AT LBSDR SWAA2023050119596Channel · corrodedCORROSION SPOTS ON AFT CARGO COMPARTMENT ZEE CNANNEL B.S. 727 727B LBL 22' W.L. 156. (51-006) CORROSION SPOTS ON AFT CARGO COMPARTMENT EE CNANNEL B.S. 727 - B.S 727B LBL 21' W.L. 152.7. (51-006)<[01] REMOVED CORROSION ON AFT CARGO COMPT BETWEEN STA 727 TO STA SDR SWAA2023050119597Channel · corrodedCORROSION SPOTS ON AFT CARGO COMPARTMENT ZEE CHANNEL B.S. 727B - 727D LBL 22' W.L. 156 (51-007) CORROSION SPOTS ON AFT CARGO COMPARTMENT EE CHANNEL B.S. 727B - 727D LBL 21' W.L. 152.7.<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT L/H ZEE CHANNEL PER REF. SRSDR SWAA2023050119598Channel · corrodedCORROSION SPOTS ON AFT CARGO COMPARTMENT ZEE CHANNEL B.S. 747 - 787 LBL 22' W.L. 156. (51-009) CORROSION SPOTS ON AFT CARGO COMPARTMENT EE CHANNEL B.S. 747 - 787 LBL 21' W.L. 152.7.<[01] REMOVED CORROSION ON AFT CARGO COMPT BETWEEN STA 747 TO STA 787 LBL 21; OSDR SWAA2023050119595Channel · corrodedCORROSION SPOTS ON AFT CARGO COMPARTMENT ZEE CHANNEL B.S. 787 - 847 LBL 22' W.L. 156. (51-010) CORROSION SPOTS ON AFT CARGO COMPARTMENT EE CHANNEL B.S. 787 - 847 LBL 21' W.L. 152.7.<[01] REMOVED CORROSION ON AFT CARGO COMPT BETWEEN STA 787 TO STA 847 LBL 21; OSDR SWAA2023050118690Strip · elongatedFOUND L/H CAP STRIPS WITH HOLES ELONGATED ON AFT CARGO; P/N453A2611-8;453A2611-10; 453A2611-4; 453A2611-13<[01] RECEIVED L/H CAP STRIPS P/N 453A2611-8; 453A2611-10; 453A2611-4; AND 453A2611-13.;[02] CORRECTION TO STEP 1; RECEIVED L/H CAP STRIPS P/N 453A2611-8 SDR SWAA2023032118763Light · brokenRIGHT OVER WING EXIT LIGHT COVER BROKEN<[01] INSTALLED NEW LIGHT COVER REF AMM 33-51-03SDR SWAA2023050118587Floor Panel · peelingFWD CABIN FLOOR PANEL 221BF UPPER SKIN SURFACE PEELING.<[01] PANEL REPLACED WITH NEW PANEL P/N141A5810-56 PER SRM 51-10-02-0G-0INSTALLATION WILL BE ACCOMPLISH ON TTG8Q00HL1CH;[02] VERIFIED STEP 1SDR SWAA2023050118589Floor Panel · peelingFWD CABIN FLOOR PANEL 221CF UPPER SKIN SURFACE PEELING.<[01] PANEL REPLACED WITH NEW PANEL P/N 141A5810-227 PER SRM 51-10-02-0G-0 INSTALLATION WILL BE ACCOMPLISH ON TTG8Q00HL1CF;[02] VERIFIED STEP 1SDR SWAA2023050118592Floor Panel · crackedFWD CABIN FLOOR PANEL 222DF UPPER SURFACE CRACKED.<[01] RECEIVED NEW CABIN FLOOR PANEL P/N 141A5810-185; NEW FLOOR 222 DF TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00HL1C3;[02] VERIFIED RECEIVING PANEL AND TO BE INSTALLED T/C <BR> TTG8Q00HL1C3.SDR SWAA2023050118602Floor Panel · peelingFWD CABIN FLOOR PANEL 231CF UPPER SKIN SURFACE PEELING.<[01] APPLIED THE GLASS FABRIC REPAIR PLIES AT DAMAGED AREA ON FWD CABIN FLOOR PANEL 231CF UPPER SKIN. REF B737 SRM 53-00-50-2R-1 PARAGRAPH 3. MATERIAL USED GLASS FIBER PLIES PO#: 1690463 AND RESIN EPOCASTSDR SWAA2023050118440Intercostal · corrodedCORROSION....CABIN FLOOR INTER COSTAL @ STA 344 - STA 360; BL 0; WL 208.1 CRACKED. (18-067)<[01] INSTALLED CABIN FLOOR INTERCOSTAL AT STA 344 TO STA 360; BL 0; AS PER SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED CABIN FLOOR INTERCOSTAL @ STA 344 - STA 360; BL SDR SWAA2023050118445Intercostal · elongatedR/H CABIN FLOOR INTERCOSTAL @ STA 312 - STA 328; RBL 30.5; WL 208.1 HOLES ELONGATED. (18-070)<[01] REMOVED AND REPLACED CABIN FLOOR INTERCOSTAL @ STA 312 - STA 328; RBL 30.5; AS PER SRM 51-40-02-0G-0 AND DWB 141A5400.;[02] VERIFIED REMOVE AND REPLACE INTERCOSTSDR SWAA2023050118591Floor Panel · corrodedCORROSION....FWD CABIN FLOOR PANEL 222DF INSERTS HAS CORROSION.<[01] NEW CABIN FLOOR PANEL 222 DF RECEIVED ON CUSTOMER BAR CODE TTG8Q00JY244;[02] VERIFIED PANEL RECEIVED ON T/C TTG8Q00JY244.SDR SWAA2023050118598Floor Panel · corrodedCORROSION....L/H FWD CABIN FLOOR PANEL 221DF INSERTS HAS CORROSION.<[01] PANEL REPLACED WITH NEW PANEL P/N 141A5810-59 INSTALLATION WILL BE ACCOMPLISH ON TTG8Q00HL1CD;[02] VERIFIED STEP 1SDR SWAA2023050118599Floor Panel · corrodedCORROSION....R/H FWD CABIN FLOOR PANEL 222BF INSERTS HAS CORROSION.<[01] REMOVED AND REPLACED CORRODED INSERTS AT R/H FWD CABIN FLOOR PANEL 222BF PER SRM 53-00-50-2R-0;[02] VERIFIED AND INSPECTED STEP #1. REMOVED AND REPLACED CORRODED INSERTS AT R/H FWD CABIN SDR SWAA2023050118438Fitting · corrodedCORROSION....L/H CABIN FLOOR GRIT BAR SUPPORT FITTING @ STA 312; LBL 59; WL 208.1 FASTENER HOLES HAS CORROSION. (18-065)<[01] REMOVED AND REPLACED L/H CABIN FLOOR GRIT BAR SUPPORT FITTING @ STA 312; LBL 59; WL 208.1 AS PER SRM 51-40-02-0G-0.;[02] VERIFIED FITTSDR SWAA2023050118439Fitting · corrodedCORROSION....L/H CABIN FLOOR GRIT BAR SUPPORT FITTING @ STA 344; LBL 59; WL 208.1 FASTENER HOLES HAS CORROSION. (18-066)<[01] REMOVED AND REPLACED L/H CABIN FLOOR GRIT BAR SUPPORT FITTING @ STA 344; LBL 59; WL 208.1 AS PER SRM 51-40-02-0G-0.;[02] VERIFIED FITTSDR SWAA2023050118211Floor Panel · peelingAFT CABIN FLOOR PANEL 241UF UPPER SKIN SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 241UF; P/N 146A5810-54; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00HPNN7;[02] VERIFIED RECEIVING OF PART.SDR SWAA2023050118209Floor Panel · crackedAFT CABIN FLOOR PANEL 241WF LOWER SKIN SURFACE HAS CRACK.<[01] FAULT RESOLVED ON ANOTHER FAULT; SEE TTG8Q00JXDYJ.;[02] FAULT RESOLVED ON ANOTHER FAULT; SEE TTG8Q00JXDYJSDR SWAA2023050118208Floor Panel · peelingAFT CABIN FLOOR PANEL 242QF UPPER SKIN SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL P/N146A5810-13; NEW FLOOR PANEL 242 QF TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00HPNNB;[02] VERIFIED RECEIVING NEW PANEL AND TO BE INSTALLED ON T/C TTG8Q00HPNNB.SDR SWAA2023050118206Floor Panel · peelingAFT CABIN FLOOR ACCESS PANEL 242PF UPPER SKIN SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL P/N 146A5810-103; NEW FLOOR PANEL 242PF ; TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00HPNND;[02] VERIFIED STEP 1 FLOOR PANEL RECEIVED AND TRANSFER OF INSTALLATIOSDR SWAA2023050118210Floor Panel · crackedAFT CABIN FLOOR PANEL 241VF LOWER SKIN SURFACE HAS SEVERAL CRACKS.<[01] RECEIVED NEW CABIN FLOOR PANEL P/N 146A5810-103; NEW FLOOR PANEL 241 VF; TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00HPNN5;[02] VERIFIED PART RECEIVED AND TRANSFER OF INSTALLATION.SDR SWAA2023050118429Web · corroded*CORROSION** CABIN PASSENGER AFT WET AREA STA986 LBL 60 WEB HAS CORROSION DOT EV54 CORROSION IS ON UPPER FLANGE LBL 43 STA 986.5<[01] ACOMPLISHED EA M-21-153-00612 CORROSION BLENDOUT EXTENDED ALLOWABLE LIMITS ON STA. 986.5 RBL 43; ALL WORK STEPS C/W.;[02] VERISDR SWAA2023050118417Floorbeam · corroded*CORROSION** CABIN PASSENGER AFT WET AREA STA 986 RBL 60 -6' WEB HAS CORROSION CORROSION IS ON UPPER CHORD OF FLOOR BEAM 986.5 RBL 43<[01] FOUND EXFOLIATE CORROSION ON FLOOR BEAM AT STA. 986.5; IS OUT OF LIMITS PER RE.F SRM 53-70-51-1A-1; AND CUT OUT DAMAGE ARSDR SWAA2023050118184Floor Panel · crackedPASSENGER CABIN FLOOR ACCESS PANEL 242BF FWD EDGE CRACKED. (234-01)<[01] VERIFIED REPAIR OF FLOORBOARD PNL 242BF PER SRM 53-00-00-50-2R-4 AND REPLACEMENT OF INSERTS PER SRM 53-00-50-2R-0SDR SWAA2023050118176Floor Panel · crackedLH PASSENGER CABIN FLOOR ACCESS PANEL 231YF CRACKED. (234-08)<[01] APPLIED REPAIR IN DAMAGED AREA AT LH PASSENGER CABIN FLOOR ACCESS PANEL 231YF. REF B737 SRM 53-00-50-2R-0 MATERIAL USED CLOTH PO#1690463; RESIN PO# 1799598;[02] VERIFIED REPAIRSDR SWAA2023050118193Panel · elongatedL/H HORIZONTAL STAB ACCESS PANEL 333AT FASTENER HOLE ELONGATED.<[01] FABRICATED PANEL 333AT IN REF TO B737 DRAWING 186A3101; SRM 51-40-05-0G-0; AMM 51-21-41-370-802; AND AMM 51-21-73-370-803;[02] RII. VERIFIED FABRICATED PANEL 333AT IN REF TO B737 DRAWING 186ASDR SWAA2023050117997Fitting · crackedL/W REAR SPAR PANEL 551GB WIGGLE FITTING CRACKED INB OF FLAP TRACK NO-3 MKD DPT<[01] REMOVED AND REPLACED L/W REAR SPAR PANEL 551GB WIGGLE FITTING CRACKED INB OF FLAP TRACK NO-3 AS PER SRM 51-40-02-0G-0.;[02] CORRECTION TO STEP 1;<BR>REMOVED AND REPLACED L/W RSDR SWAA2023050118185Floor Panel · deterioratedLH PASSENGER CABIN FLOOR AFT WET AREA ACCESS PANEL 241ZF WITH UPPER SURFACE MATERIAL DETERIORATED. (234-10)<[01] RECEIVED NEW CABIN FLOOR PANEL P/N 815A0044-7; NEW CABIN FLOOR PANEL 241 ZF TO BE INSTALLED ON CUSTOMER BARCODE TTG8Q00HL13B;[02] VERIFIED RECEIVINSDR SWAA2023042818186Floor Panel · crackedRH PASSENGER CABIN FLOOR AFT WET AREA ACCESS PANEL 242TF CRACKED AND HAVING UPPER SURFACE MATERIAL DETERIORATED. (234-09)<[01] RECEIVED NEW CABIN FLOOR PANEL P/N 147A5810-94; NEW FLOOR PANE 242 TF TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00HL1BM;[02] CORRECTISDR SWAA2023050117290Stiffener · crackedL/H HORIZONTAL STAB @ STA 129.50 RIB #5 STIFFENER #3 CRACKED.<[01] INSTALLED L/H HORIZONTAL MACHINE IN SPAR RIB STIFFENER REPAIR AT RIB # 5; STIFFENER # 3 PER REF. SRM 55-10-09-2R-4; REP. 4; MIXED SEALANT 0870B002BM654SKN40 AT 23:00; ON 3/31/23 SQUEEZE OUT ANDSDR SWAA2023050117473Web · crackedCRACK FOUND AT HORIZONTAL PRESSURE DECK WEB STA 663; RBL-42. CRACK LENGTH : 0.265' CRACK FOUND AT HORIONTAL PRESSURE DECK WEB STA 663 RBL-42. CRACK LENGTH : 0.265'<[01] REMOVED AND INSTALLED NEW REPAIR PARTS AT STA 663 RBL 42 ON PREASSURE DECK WEB AND STIFFNERSDR SWAA2023050116654Panel · crackedR/H WING LOWER ACCESS PANEL 661CB LOWER SKIN SURFACE FASTENER HOLES HAS CRACKS. (18-027)<[01] PREPARED REPAIR AND REPAIRED R/H WING ACCESS PANEL 661 CB .AS PER B737 SRM 51-70-04 -2R-9 PARAGRAPH.4 .MATERIAL USED PO.1738579 AND PO.1800550. APPLIED PRIMER PANEL 6SDR SWAA2023050116652Panel · crackedLOWER FUSELAGE ACCESS PANEL 193D LOWER SKIN SURFACE HAS CRACKS AT SEVERAL FASTENER HOLES. (18-021)<[01] RECIEVED NEW PART# 149A7653-5 PO# 2012626. REF TASK TTG8Q00HL105 FOR PANEL INSTALLATION;[02] VERIFIED STEP 1.SDR SWAA2023042826086Attach Angle · crackedWING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE RBL42 HAS CRACK<[01] REMOVED AND INSTALLED NEW FABRICATED ATTACH ANGLE AT VAPOR BARRIER ON RBL 42 AT STA 663 AS PER REPAIR REFERENCE SRM 51-10-10-2R-5 AND DW 111A1000.;[02] VERIFIED REPAIRSDR SWAA2023042826087Attach Angle · crackedWING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE LBL42 CRACK<[01] REMOVED; FABRICATED AND INSTALLED NEW REPAIR AT VAPOR BARRIER ATTACH ANGLE ON STA 663 LBL42 AS PER REPAIR REFERENCE (SRM 57-10-10-2R-5) AND DW 111A1000.;[02] VERIFIED REPAIRSDR SWAA2023042824861Attach Angle · crackedWING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE LBL8 CRACK CORRECTION RBL 8<[01] FAULT WAS RESOLVED ON ANOTHER FAULT TTG8Q00JUVMQ.;[02] FAULT WAS RESOLVED ON ANOTHER FAULT TTG8Q00JUVMQ.SDR SWAA2023042816646Girt Bar · out of adjustR1 SLIDE DOOR FWD GIRT RETAINER SUPPORT BAR IS LOOSE.<[01] CONFORMED R-1 DOOR FWD GIRT BAR RETAINER CLIP AS PER AMM 25-66-01-200-802 STEP 3.B.(F)4)B);[02] VERIFIED STEP 1.SDR SWAA2023042816645Cover · damagedR1 SLIDE DOOR AT FWD/UPPER SLIDE COVER HAS BAREMETAL COMPOSITE AREA MISSING PAINT<[01] PAINTED R1 SLIDE DOOR AT FWD/UPPER SLIDE COVER ASPER B737-700 AMM 25-00-370-801;[02] VERIFIED PAINTSDR SWAA2023042816647Slide · damagedR2 SLIDE DOOR LOWER HORIZONTAL FRAME/AFT IS MISSING.<[01] REMOVED DAMAGED RUBSTRIP FROM R2 DOOR SLIDE PER REF. SRM 51-40-02-0G-0; LOCATE AND DRILL NEW RUBSTRIP PER REF. SRM 51-40-05-0G-0 AND INSTALLED NEW RUBSTRIP ON R2 DOOR SLIDE PER REF. SRM SRM 51-40-02-0G-SDR SWAA2023031415999Motor · inoperativeSTAB TRIM INOP ON BOTH CAPTS & F/O SIDE THUMB SWITCH.<[01] R & R?DSTAB TRIM MOTOR PER MM 27-41-71.SDR SWAA2023032312723Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS807 AT LEVEL STR26R AND RBL36 AT AFT CARGO COMPARTMENT 2023-116991<[01] REPLACED ANGLE - SUPPORT LOCATED BS807 AT LEVEL STR26R AND RBL36 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; DWG 146A8120 SHEET 31 REV- AND DSDR SWAA2023030812709Slide · lowR1 ESCAPE SLIDE PRESSURE GAUGE BELOW GREEN<[01] REMOVED AND REPLACED FWD SERVICE DOOR SLIDE IAW AMM 25-66-01. REF TASKCARD TTG8Q00J9N8ZSDR SWAA2023030812654Battery · faultyBOTH FWD EMERGENCY FLASHLIGHTS REQUIRE BATTERY REPLACEMENT.<[01] R+R BOTH FWD EMERGENCY FLASHLIGHT BATTERIES IAW AMM 25-64-00. OPC GOOD.SDR SWAA2023030712401Girt Bar · out of adjustL1 GIRT BAR HARD TO ENGAGE<[01] ADJUSTED L-1 DOOR GIRT BAR CATCH. OPS CHECK GOOD PER AMM 25-66-00SDR SWAA2023032304774Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 RBL 8.283 AT PASSENGER CABIN 2023-116966<[01] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 RBL 8.283 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEESDR SWAA2023032304775Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13.24 AT PASSENGER CABIN 2023-116968<[01] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13.24 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 6 REV-. SEE SDR SWAA2023032304777Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN AT PASSENGER CABIN 2023-116967<[01] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWGSDR SWAA2023032304399Angle · crackedCRACK ANGLE - CLIP LOCATED BS 480 FWD FACE STR 26L AT FWD CARGO COMPARTMENT 2023-116961<[01] REPLACED ANGLE - CLIP LOCATED BS 480 FWD FACE STR 26L AT FWD CARGO COMPARTMENT AND FASTENER IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG143A1220 SHEET 30
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