Boeing 737-7K9
Service difficulty reports · 794
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 = '7377K9' 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 = '7377K9' 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 SWAA2022020265573None · crackedVERTICAL CLIP @ 727 PANEL 193 HAS CRACK APPROX. 2.0' LONG. ; / [01] FABRICATED NEW CLIP AND INSTALLED PER SRM 51-40-02 AND 51-40-05SDR SWAA2022020265572Panel · elongatedPANEL 194E HAS SEVERAL OUT OF ROUND HOLES. ; / [01] FABRICATED NEW PANEL; BACK DRILLED HOLES PER 51-40-05; COUNTER SINK PER 51-40-08 AND APPLIED DECORATIVE FINISH PER AMM 51-21-99.SDR SWAA2022020165116Girt Bar · looseREAR ENTRY DOOR GIRT BAR DOES NOT ALIGN SECURELY IN BRACKET ; / [01] REMOVED FLOOR-MOUNTED ESCAPE SLIDE GIRT BAR<BR>BRACKET PER AMM 25-66-02; [02] FOUND 1 BOLT IN ADAPTOR PLATE TO SHORT. REPLACED BOLT AND INSTALLED ADAPTOR PLATE PER AMM 25-66-02. OPS CK GOODSDR SWAA2022012462124Retainer · crackedR/H WING #6 FLAP FAIRING OUT BOARD SEAL RETAINER CRACKED. REMOVED AND REPLACED R/H WING #6 FLAP FAIRING OUTBOARD SEAL RETAINER PER AMM 27-51-18. REMOVED AND REPLACED R/H WING #6 FLAP FAIRING OUTBOARD SEAL RETAINER PER AMM 27-51-18.SDR SWAA2022011862218Slide · out of positionSUPPLEMENTAL INFORMATION: R2 AND L2 DOORS ESCAPE SLIDE SKIRT RUB ACUFF PLATE WHEN CLOSING ; / [01] REPOSITIONED GIRT 'Z' FOLD ON L2 AND R2 DOOR SLIDES AS PER B737 AMM 25-66-01-400-804; [02] VERIFIED STEP 1SDR SWAA2022011861362Slide · out of positionR2 AND L2 DOORS ESCAPE SLIDE SKIRT RUB ACUFF PLATE WHEN CLOSING ; / [01] REPOSITIONED GIRT 'Z' FOLD ON L2 AND R2 DOOR SLIDES AS PER B737 AMM 25-66-01-400-804; [02] VERIFIED STEP 1SDR SWAA2022011861000Light · inoperativeFLIGHT DECK ENTRY EMERGENCY LIGHT INOP. ; / [01] REPLACED LAMP ON FLIGHT DECK EMERGENCY ENTRY LIGHT; PERFORMED TEST; TEST PASS. REF. TO B 737 AMM 33-51-01-960-801.; [02] VERIFIED STEP 1SDR SWAA2022011860605Drain · crackedCUSTOMER REQUEST: BS 1016 CENTER FUSELAGE DRAIN CRACKED ; / [01] REMOVED DAMAGE DRAIN AT STA 1016 ( CENTER DRAIN ) PER B737 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW DRAIN PER B737 SRM 51-40-05-0G-0; [03] VERIFIED STEPS 1 AND 2; [04] OK TO INSTALL DRAIN;SDR SWAA2022010557734Hook · looseFWD SVC DOOR GIRT BAR LOOSE IN STORAGE HOOKS ; / [01] ADJ. GIRT BAR HOOKS PER SIPSDR SWAA2022011856030Seal Plate · delaminatedLEFT VERTICAL STAB TRAILING EDGE SEAL PANEL 324ABL IS DELAMINATED AND HAS SECTIONS OF THE SEAL MISSING ; / [01] RECEIVED NEW SEAL PANEL P/N 175A1601-86; [02] OK TO INSTALL PANEL.; [03] INSTALLED NEW PANEL P/N 175A1601-86 REF B 737 SRM 51-40-02. WORK WAS ACCOMPSDR SWAA2022011855694None · crackedFWD. CARGO COMPT. INTERCOSTAL/BAFFLE HAS CRACKED FWD. CLIP AT BS 400; LBL 21;(143A7502-5) ; / [01] REMOVED CLIP AT FWD CARGO COMPT. INTERCOSTAL/ BAFFLE IAW B737-700 SRM 51-40-02-0G-0; [02] LOCATED HOLES AT NEW CLIP. IAW B737-700 SRM 51-40-05-0G-0; [03] VERIFIESDR SWAA2022011953643Panel · crackedLT SIDE HORIZONTAL FUSELAGE BLADE GUIDE FOR PANEL 333AT CRACKED. ; / [01] REMOVED LT SIDE HORIZONTAL FUSELAGE BLAD GUIDE FOR PANEL 333AT IAW B737 SRM 51-40-02; [02] VERIFIED STEP M#1; [03] OK TO INSTALL NEW REPLACEMENT.; [04] INSTALLED LT SIDE HORIZONTAL FUSELSDR SWAA2022011953644Panel · crackedRT SIDE HORIZONTAL FUSELAGE BLADE GUIDE FOR PANEL 343AT CRACKED. ; / [01] REMOVED RT SIDE HORIZONTAL FUSELAGE BLADE GUIDE FOR PANEL 343AT IAW B737 SRM 51-40-02; [02] VERIFIED STEP #1; [03] OK TO INSTALL NEW REPLACEMENT; [04] INSTALLED RT SIDE HORIZONTAL FUSELASDR SWAA2022011854140Intercostal · crackedFOUND INTERCOSTAL/BAFFLE CRACKED AT FWD. CARGO COMPT. BETWEEN BS 400 & 420;LBL 21. ; / [01] REMOVED INTERCOSTAL/BAFFLE AT FWD CARGO COMPT. STA 400 AND 420;LBL 21 IAW B737-700 SRM 51-40-02-0G-0; [02] LOCTED AND DRILLED NEW INTERCOSTAL/BAFFLE; AT FWD CARGO COMPTSDR SWAA2022011853491Door · corrodedFOUND CORROSION & WORN AT L-1 DOOR CUTOUT FWD. FRAME LOWER HINGE BOX UPPER FITTING HOLE. PARTIAL REMOVED HINGE BOX AT L-1 DOOR CUTOUT FWD. FRAME LOWER. IAW SRM 51-40-02. INSTALLED EWIS PROTECTION AT L-1 DOOR CUTOUT FWD. LOWER HINGE BOX AREA DURING MAINT. IAWSDR SWAA2021122053641Engine · faultyFUEL IMBALANCE INDICATION. FUEL LEAK CONFIRMED. LEFT SIDE ; / [01] PERFORMED #1 ENGINE GVI AND ENG IDLE RUN PER AMM 71-00-00. NO LEAKS OR DEFECTS NOTED. (PER MOC SUSPECT L/H #1 MAIN TANK FUEL QUANTITY INDICATION FAULT)SDR SWAA2022011852349Rib · crackedL/W I/B FLAP L/E SECOND RIB IS CRACKED.(FROM I/B). ; / [01] REMOVED DAMAGED RIB AT L/W I/B FLAP L/E AREA UNDER PANEL #553AT; AS PER B737-7; SRM 51-40-02-0G-0.; [02] FPI ACCOMPLISHED AT IN-PROGRESS FABRICATION OF RIB AFTER ALL MACHINING IAW BOEING DRAWING # PL1SDR SWAA2021121452503Panel · elongatedPANEL 193D HAS SEVERAL HOLES ELONGATED. ; / [01] INSTALLED SERVICEABLE 193D PANEL IAW AMM 53-51-21 NO FURTHER DEFECTS NOTEDSDR SWAA2021121452504Panel · elongatedPANEL 194E HAS SEVERAL HOLES ELONGATED. ; / [01] ACQUIRED SERVICEABLE 194E PANEL AND MATCH DRILLED TO EXISTING SUPPORT STRUCTURE PER AMM 53-51-21.; [02] INSTALLED SERVICEABLE 194E PANEL IAW AMM 53-51-21 NO FURTHER DEFECTS NOTED AT THIS TIME.SDR SWAA2022011851281Bracket · crackedDORSAL FIN FWD ATTACHMENT BRACKET IS CRACKED ; / [01] REMOVED FWD ATTACHMENT BRACKET(WEB) FROM DOSAL FIN REF B737-700 SRM 51-40-02-0G-0; [02] INSTALLED BRACKET AT FWD DORSAL FIN IAW B737 SRM 51-40-02; [03] PART TRANSACTION ONLY; [04] VERIFIED INSTALLATION OF NSDR SWAA2022011850322Intercostal · crackedMAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN BS 312 AND 328 LBL 34' CRACKED. REMOVED INTERCOSTAL AT MAIN CABIN FWD WET AREA STS 312 AND 328 LBL 44 IAW SRM 51-40-02-0G-0; [02] REMOVE MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 312 AND STA 328 LBL; [03] VERSDR SWAA2022011850324Intercostal · crackedMAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 328 AND STA 344 LBL 34' CRACKED ; MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 328 AND STA 344 LBL 46' CRACKED / [01] REMOVED AT MAIN CABIN WET AREA INTERCOSTAL BETWEEN STA 328 344LBL 46' IAW B737-7 SRM 51-40-SDR SWAA2022011850325Intercostal · crackedMAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 277 AND STA 294.5 RBL 12' CRACKED ; MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 277 AND STA 294.5 BL 0 CRACKED / [01] REMOVED DAMAGED INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN STA 277 AND STA 294.5 RBL 1SDR SWAA2022011850323Intercostal · crackedMAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 312 AND STA 328 RBL 30' CRACKED ; / [01] REMOVED INTERCOSTAL AT MAIN CABIN FWD WET AREA STA 312 AND 328 RBL. 30 IAW B 737-700 SRM 51-40-02-0G-0; [02] VERIFIED STEP 1; [03] OK TO INSTALL INTERCOSTAL; [04] INSTALLESDR SWAA2022011850326Gusset · crackedFWD CARGO COMPT STA 500D STR 18 R/H GUSSET CRACKED ; / [01] REMOVED R/H GUSSET AT FWD CARGO COMPT STA 500D STR 18 IAW B737-700 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED HOLES AT NEW GUSSET AT FWD CARGO COMPT SAT 500D STR 18 R/H. IAW B737-700 SRM 51-40-05-0G-SDR SWAA2022011850283Floor Panel · frayedMAIN CABIN; FLOOR PNL 242 AF HAS FRAYED FIBERS GLASS ON TOP SURFACE ; / [01] RECEIVED SERVICEABLE FLOOR PANEL 242AF. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q0097DKZ; [02] VERIFIED STEP 1SDR SWAA2022011850286Floor Panel · frayedMAIN CABIN FLOOR PNL 241 AF FRAYED FIBER GLASS ON TOP SURFACE ; / [01] REMOVED CABIN FLOOR PANEL 241AF IN REF B737-700 AMM- 53-21-00-000-801; [02] VERIFIED STEP 1. OK TO INSTALL PNL 241AF; [03] INSTALLED CABIN FLOOR PANEL 241AF IN REF B737-700 AMM-53-21-00-400SDR SWAA2022011850288Battery · inoperativeL2 MEGAPHONE BATTERIES INOP ; / [01] REMOVED AND REPLACED L2 MEGAPHONE BATTERIES AS PER BOEING AMM 25-64-00-900-804.; [02] VERIFIED STEP 1SDR SWAA2022011850295Battery · inoperativeL1 WINDSCREEN BOTH FLASHLIGHT BATTERIES INOP ; / [01] REMOVED AND REPLACED L1 WINDSCREEN BOTH FLASHLIGHT BATTERIES AS PER BOEING AMM 25-64-00-900-806; [02] VERIFIED STEP 1SDR SWAA2022011850285Stringer · corrodedCORROSION FWD CARGO L-26 STRINGER TO FRAME AT BS 540. REMOVED CORROSION S26L, BS 540 FOUND OUT LIMITS IAW B737-700 SRM 51-10-02, ORIG. MAT.: 0.045'; MAT. REMOVED:0.035'; REMAINING MAT. : 0.015'; FOUND OUT OF LIMITS IAW SRM 53-00-03-1A-1, TABLE 101. CUT-OUTSDR SWAA2022011850281Stringer · corrodedCORROSION FWD CARGO R-27 STRINGER TO FRAME AT BS 540. REMOVED FASTENERS TO GAIN ACCESS AT FWD CARGO R-27 STRINGER TO FRAME AT BS 540 IAW B737-700 SRM 51-40-02-0G-0. CLEANED AREA AT FWD CARGO R-27 STRINGER TO FRAME AT BS 540 FOUND CRACKED IAW SRM 53-00-03-1A-SDR SWAA2022011850306Bracket · crackedAFT CARGO RT BS 727D S25 SIDEWALL SUPPORT CRACKED. REMOVED RT SIDEWALL SUPPORT ANGLE IAW SRM 51-40-02-0G-0. FABRICATED SIDEWALL SUPPORT BRACKET IAW DR 146A9403, LOCATED AND DRILLED HOLES IN SIDEWALL SUPPORT BRACKET IAW SRM 51-40-05. TREATED AND PRIMED NSDR SWAA2022011850307Channel · corrodedAFT CARGO COMP L/H BETWEEN STA 747 AND STA 847 ZEE CHANNEL UPPER SURFACE SEVERAL AREA WITH CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G-0-A00248. PERFORMED UT THICKNESS INSP. ON REWORKED AREA IAW NDT PART 4 51-00-00 PROC. 3. MIN THICKNESS .029'. ORIGSDR SWAA2022011850280Stringer · corrodedFW CARGO R-26 STRINGER TO FRAME BS 540. CLEANED AREA AT FWD CARGO R-26 STRINGER TO FRAME BS 540. FOUND WITH CRACK. IAW SRM 53-00-03-1A-1. REMOVED CORROSION AT STR. 26R; BS 540, ORIGINAL MAT.: 0.040'; MAT. REMOVED 0.035'; REMAINING MAT 0.005', FOUND OUT OF LSDR SWAA2022011849843Floor Panel · frayedMAIN CABIN FLOOR PANEL 241ACF UPPER SURFACE FRAYING ; / [01] PARTIALLY FABRICATED PASSENGER CABIN FLOOR PANEL 241ACF REF B-737-700 SRM-53-00-50-1A-1 PENDING INSERTS INSTALLATION.; [02] VERIFIED FABRICATED PASSENGERS CABIN FLOOR PANEL 241ACF REF B-737-700 SRM-5SDR SWAA2022011849845Floor Panel · frayedMAIN CABIN FLOOR PANEL 241ADF UPPER SURFACE FRAYING ; / [01] PARTIALLY FABRICATED PASSENGERS CABIN FLOOR PANEL 241ADF REF B-737-700 SRM-53-00-50-1A-1 PENDING INSTALLATION; [02] CORRECTION TO STEP 1: PARTIALLY FABRICATED PASSENGER CABIN FLOOR PANEL 241ADF REF BSDR SWAA2022011849846Floor Panel · frayedMAIN CABIN FLOOR PANEL 241XF UPPER SURFACE FRAYING ; / [01] PARTIALLY FABRICATED PASSENGER FLOOR PANEL 241XF REF B-737-700 SRM-53-00-50-1A-1 PENDING INSERTS INSTALLATION.; [02] VERIFIED FABRICATED PASSENGERS CABIN FLOOR PANEL 241XF REF B-737-700 SRM-53-0050-1ASDR SWAA2022011849847Floor Panel · frayedMAIN CABIN FLOOR PANEL 241AAF UPPER SURFACE FRAYING ; / [01] PARTIALLY FABRICATED PASSENGERS CABIN FLOOR PANEL 241AAF REF B-737-700 SRM-53-0050-1A-1 PENDING INSERTS INSTALLATION; [02] VERIFIED FABRICATED PASSENGERS CABIN FLOOR PANEL 241AAF REF B-737-700 SRM-53SDR SWAA2021120749978Panel · corrodedL/W FUEL PANEL 534BB INNER SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G-0. FOUND WITHIN LIMITS IAW SRM 57-20-01-2R-1, FIG 203, DETAIL B-B. TREATED REWORKED AREA OF PANEL IAW SRM 51-10-02-0G-0.SDR SWAA2022011949609Angle · brokenPANEL 423BL HAS SHIM BROKEN INSIDE PANEL DOOR. ; / [01] RREMOVED ANGLE (SHIM) AT PANEL 423BL REF B 737-700 SRM 51-40-02; [02] THE ANGLE SHIM P/N: 314-2215-3; WAS REPLACED ON N/R 4000/0009; W/O: 2018123; BARCODE: TTG8Q009M4UD.; [03] VERIFIED STEPS 1 AND 2SDR SWAA2022011849610Doubler · crackedEXTERNAL POWER RECEPTACLE DOOR LOWER CUT OUT SKIN DOUBLER IS CRACKED. PROTECTED EWIS AREA AT EXTERNAL POWER RECEPTACLE DOOR. IAW AMM 20-60-07-913-801. REMOVED DOOR PANEL 114 AR FOR GAIN ACCESS. IAW SRM 51-40-02-0G-0. REMOVED THE INITIAL RUBBING BLOCK; THE LASDR SWAA2022011948202Skin · crackedRT WING LOWER SURFACE L/E; #6 SLAT NOSE SKIN AT ACTUATOR RIBS. CRACK AROUND FASTENER SKIN. CRACK CONFIRMED IAW NDTM PART 6;51-00-00 PROCEDURE 23. CRACK FOUND AT 2ND FWD O/B FASTENER. CRACK LENGTH :0.157. REMOVED INBD CENTER, OTBD COVE SKIN & PARTIAL FLEX SSDR SWAA2021100625871Panel · elongated194E PNL HAS 3 ELONGATED FASTENER HOLES ON LEADING EDGE LEFT SIDE ; / [01] INSTALLED NEW PANEL PER 53-51-21SDR SWAA2021100625872Panel · cracked194E PNL HAS 1 CRACKED FASTENER HOLE ON THE TRAILING EDGE ; / [01] INSTALLED NEW PANEL PER 53-51-21SDR SWAA2021100625873Panel · elongated193D PNL HAS 6 ELONGATED FASTENER HOLES ; / [01] INSTALLED NEW 193D PANEL PER AMM 53-51-21SDR SWAA2021100625874Panel · cracked193D PNL HAS 2 CRACKED AND DIMPLED FASTENER HOLES ; / [01] INSTALLED NEW 193D PANEL PER AMM 53-51-21SDR SWAA2021100625875Panel · corroded193D PANEL HAS EXISTING REPAIR THAT IS PITTED ; / [01] INSTALLED NEW 193D PANEL PER AMM 53-51-21SDR SWAA2021091546435Battery Pack · inoperativeMID CABIN EMERGENCY LIGHTS ALSO LEFT AND RIGHT GROUND ILLUMINATION LIGHTS INOP ; EQUIPMENT # M1670 POWER SUPPLY / [01] REPLACED BATTERY PACK AT STATION 727C LT SIDE PER AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2021091416438Lanyard · brokenAFT CARGO DOOR ASSIST LANYARD BROKEN ; / [01] REBUILT AFT CARGO DOOR ASSIST LANYARD PER AMM 52-31-00SDR SWAA2021061482596Skin · crackedRAMP REPORTED A CRACK IN THE EXTERNAL POWER DOOR CUTOUT. / PERFORMED REPAIR 4--ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER PER SRM 53-10-15-2R-4
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