Boeing 737-7BD
Service difficulty reports · 7,528
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 = '7377BD' 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 = '7377BD' 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 SWAA2022041981670Skin Panel · crackedCRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 AND 16 INCH. FROM FRONT SPAR. CRACK LENGTH = 1.5 INCH. APPROX. 2022-121967 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N:N500X1693P030457;CAL DUE DASDR SWAA2022041981666Panel · brokenBROKEN ACCESS PANEL 621GB LEADING EDGE SPRING ON LATCH RT WING 2022-121941 / [01] REMOVED AND REPLACED SPRING ON LATCH RT WING LEADING EDGE ACCESS PANEL 621GB IAW CMM 52-49-01;[02] CORRECTED STEP 1 <BR>REMOVED AND REPLACED SPRING ON LATCH RT WING LEADING EDGE SDR SWAA2022041981667Slat · crackedCRACK SLAT 7 LOWER SURFACE NOSE SKIN ACTUATOR RIB AROUND FASTENERS SLAT STATION 322.71 AT RT WING 2022-121938 / [01] TOOL USED : EDDY CURRENT TOOL; P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 02 JUN 22.;[02] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC SDR SWAA2022041981193Bulkhead · crackedCRACK BULKHEAD PANEL 142NWA (SHROUD PANEL ) AFT CARGO COMPARTMENT 2022-121901 / [01] TOOL USED CALIPER P/N:500-197-30 S/N:15259471 DIE DATE:10DEC22;[02] REPAIRED BULKHEAD PANEL 142NWA (SHROUD PANEL) AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01- 300-805 PSDR SWAA2022022376251Light · inoperative*CUSTOMER WALK* L-1 DOOR EMERGENCY LIGHT INOP (D.C). / [01] RELAMPED L-1 DOOR EMERGENCY LIGHT AS PER B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1SDR SWAA2022022375355Light · inoperativeFWD ENTRY AREA POWER SUPPLY/BATTERY PACK M1675 INOP. / [01] REMOVED BATTERY PACK AND POWER SUPPLY(M1675) PER B737 AMM 33-51-06-960-805 & 33-51-06-960-806.;[02] INSTALLED POWER SUPPLY AND BATTERY PACK; PERFORMED OPERATIONAL TEST; TEST PASS. REF. TO B 737 AMM 33SDR SWAA2022021673145Light · inoperativeCUSTOMER WALK- RT OVER WING EMERGENCY EXIT LOWER FWD EXIT SIGN UPPER BULB INOP. / [01] RELAMPED RT OVER WING EMERGENCY EXIT LOWER SIGN UPPER BULB AS PER REF. B737 AMM 33-51-01-960-801. TEST OK;[02] VERIFIED STEP 1SDR SWAA2022021673105Light · missingL2 DOOR EMERGENCY EXIT SIGN MISSING DIRECTION ARROW. / [01] REMOVED AND REPLACED L2 DOOR EMERGENCY EXIT SIGN LENS REF AMM 33-51-01.;[02] C/WSDR SWAA2022021672383Light · looseSMALL PLASTIC EXIT SIGN/ PLACARD NEXT TO AFT SERVICE DOOR IS LOOSE / [01] R&R AFT SERVICE DOOR EXIT SIGN COVER PER AMM 33-51-01SDR SWAA2022021670864Light · failedFLIGHT DECK EMERGENCY DOME LIGHT DOES NOT ILLUMINATE DURING EMERGENCY LIGHT OPERATIONAL TEST. / [01] RE-LAMPED FLIGHT DECK EMERGENCY DOME LIGHT PER AMM 33-14-00-00-801 AND AMM 33-14-00-400-801. OPS CHECK GOOD.;[02] VERIFIED CORRECTIVE ACTION 1; OPS CHECK GOOD.SDR SWAA2022022170107Panel · crackedDURING FLAP SKEW CHECKS FOUND PANEL 193CL WITH SURFACE CRACK / [01] PREPARED AREA FER REPAIR WITH SURFACE CRACK AT FOUND PANEL # 193CL AS PER B737 SRM 53-40-70-2R-1;[02] VERIFIED STEP #1.;[03] OK TO APPLY REPAIR.;[04] REPAIRED DAMAGED AREA AT FOUND PANEL # 193SDR SWAA2022021669614Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M2335 INOP / [01] REMOVED AND REPLACED BATTERY PACK M2335 AND PERFORMED GOOD INSTALLATION TEST AS PER AMM TASK 33-51-06-960-805.;[02] COMPLETED STEP 1;[03] OK TO CLOSE RETURN AIR GRILLE AT STA 500C LH;[04] CLOSDR SWAA2022021069608Light · inoperativeRIGHT OVER-WING EMERGENCY EXIT WINDOW LIGHT INOP ; / [01] REMOVED AND REPLACED RIGHT EMERGENCY EXIT WINDOW LIGHT LAMP AND FUSE PER AMM 33-21-00 OPS CHECK GOODSDR SWAA2022022866416Skin · crackedCRACK FOUND, LT HORIZONTAL STAB LOWER SKIN HSS 193.90; 16' FROM FWD SPAR AT I/B ROW OF FASTENERS. CRACK LENGTH: 1.125'. STRIPPED PAINT ON STAB IAW AMM 51-21-11-150-810; REMOVED FASTENERS IAW SRM 51-40-02-0G-0; PERFORMED CUTOUT OF DAMAGE IAW SRM 55-10-01-2R-SDR SWAA2022022866422Doubler · crackedCRACK FOUND, RT HORIONTAL STAB HSS 193.90; I/B ROW;16" FROM FWD SPAR. LENGTH OF CRACK 1'. STRIPPED PAINT ON LOWER SKIN IAW AMM 51-21-11-150-810; REMOVED FASTENERS IAW SRM 51-40-02-0G-0. PERFORMED CUTOUT OF DAMAGE IAW SRM 55-10-01-2R-11 & 51-10-02-0G-0. PSDR SWAA2022021665106Handle · crackedFWD ENTRY DOOR AFT SIDEWALL ASSIST HANDLE BASE IS CRACKED. / [01] REPLACED FWD ENTRY DOOR AFT SIDEWALL ASSIST HANDLE BASE AND INSTALLED IAW AMM 25-21-31-420-802.;[02] VERIFIED REPLACED FWD ENTRY DOOR AFT SIDEWALL ASSIST HANDLE BASE AND INSTALLED IAW AMM 25-21-SDR SWAA2022021664927Gusset · crackedFWD CARGO BAY GUSSET IS CRACKED AT BS 500D COMMON TO STR19R WL 192 / [01] UPDATED MEASUREMENT TABLE;[02] LOCATED AND DRILLED NEW FWD CARGO BAY GUSSET AT BS 500D STR 19R WL 192 IAW DWG 143A7902 AND SRM 51-40-05-0G-0 OK TO INSTALL;[03] PRIOR TO LOCATE AND DRILL;SDR SWAA2022022165107Stiffener · crackedRIGHT HORIZONTAL STABILIZER STA.129.50 RIB 5 STIFFENER # 3 HAS A CRACK AT LOWER RADIUS. / [01] CUT AND REMOVED THE DAMAGE FROM THE VERTICAL STIFFENER #3OF THE. RIB #5 AS PER B 737 -700 SRM 55-10-09-2R-4 REPAIR 4[13] INSTALLED REPAIR AT RH HORIZONTAL STABILIZERSDR SWAA2022020164914Battery Pack · failedAFT R/H EMERGENCY BATTERY PACK FAILED CAPACITY TEST. ; / [01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.SDR SWAA2022020164915Battery Pack · failedR/H OVERWING EMERGENCY BATTERY PACK FAILED CAPACITY TEST. ; / [01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.SDR SWAA2022021764781Floor Panel · delaminatedCABIN FLOOR PANEL 242AF DELAMINATED AT AFT O/B CORNER / [01] REMOVED THE DELAMINATION FACESHEET PLIES AND PREPARED AREA TO APPLY THE REPAIR PLIES. REF B737-700 SRM 53-00-50-2R-9 PARAGRAPH 3 AND SRM 53-00-50-2R-0 PARAGRAPH 5.;[02] VERIFIED STEP 1;[03] APPLIED TSDR SWAA2022013164614Light · inoperativeLEFT OVER WING EMERGENCY LIGHT INOP / [01] RE-LAMPED REF AMM 33-51-04 OPS CHECK GOODSDR SWAA2022013164775Panel · cracked194 E PANEL TRAILING EDGE HAS 3 EACH HOLES WITH CRACKS ; / [01] DRILLED; AND PREPARED NEW PANEL; [02] INSTALLED PANEL PER AMM 53-51-21SDR SWAA2022013164776Panel · cracked193D PANEL TRAILING EDGE HAS 3 EACH HOLES WITH CRACKS AND SERVAL COUNTERSUNK WITH EXCESSIVE WEAR ; / [01] DRILLED; TRIMMED AND PREPARED HOLE IN NEW PANEL; [02] INSTALLED PANEL 193D PER AMM 53-51-21SDR SWAA2022021664192Support · corrodedCORROSION ON FCB FLOOR TO SIDEWALL SUPPORT FROM STA 400+2 TO STA 400+10; RBL 24; WL 156. / [01] EVALUATED CORROSION AT ALL LOCATIONS ON FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 400+10 RBL 24 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1SDR SWAA2022021664193Shield · corrodedCORROSION ON FCB DOOR CUTOUT AFT SHIELD FROM STA 480+15 TO STA 500+15; RBL 24; WL 156. / [01] EVALUATED CORROSION ON SHIELD BS 480+15 RBL 24 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFSDR SWAA2022021664190Support · corrodedCORROSION ON FCB FLOOR TO SIDEWALL SUPPORT FROM STA 500A+6 TO STA 500C+15; RBL 24; WL 156. / [01] EVALUATED CORROSION AT ALL LOCATIONS ON FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 500B+10 RBL 24 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 ISDR SWAA2022021664191Support · corrodedCORROSION ON FCB FLOOR TO SIDEWALL SUPPORT FROM STA 400+2 TO STA 500C+15; LBL 24; WL 156. / [01] EVALUATED CORROSION AT ALL LOCATIONS ON FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 500A+10 LBL 24 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 INSDR SWAA2022021664006Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS540 S-25R WL155. MARKED / [01] UPDATED MEASUREMENT TABLE;[02] REMOVED DAMAGED STRINGER SECTION FCB BS500D+10 TO BS540 STR-25R WL153; AND PERFORMED VISUAL INSPECTION ON REPAIR AREA IN NOT ADITIONAL DAMAGE NOTED; IAW SRM 53-SDR SWAA2022021664007Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS540 S-26R WL153. MARKED / [01] VERIFIED APPLICABILITY OF SRM 53-+00-03-2R-1 TO BE CORRECT AND UPDATED MEASUREMENT TABLE;[;[13] INSTALLED NEW STRINGER SECTION AT AREA AFT GCB BS 540 S-26R WL153 PER SRM 51-40-02-0G-0; SRM 53SDR SWAA2022021664008Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS540 S-26L WL153. MARKED / [01] VERIFIED APPLICABILITY OF SRM 53-00-03-2R-1 TO BE CORRECT AND UPDATED MEASUREMENT TABLE;[02] REMOVED DAMAGED STRINGER SECTION FCB BS500D+10 TO BS540 STR-26L WL153; AND PERFORMED VISUAL INSPECSDR SWAA2022021664025Angle · crackedCRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS918 RBL13. MARKED. / [01] REMOVED WATER SERVICE PANEL; AFT SUPPORT ANGLE; BS 918 RBL13; IAW SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED; NEW WATER SERVICE ANGLE BS 918 RBL13; IAW 51-40-05-0G-0SDR SWAA2022021663999Web · corrodedCORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY RBL26; BS807; BS807+4; BS807+6; BS807+16; BS827; BS827+9. MARKED. / [01] EVALUATED CORROSION ON WEB AT ALL LOCATION; FOUND DEEPEST LOCATION TO BE AT BS 807 RBL 26 WL 157; FOUND 0.015 REMOVED FROM ORIG 0.045 IN 1'XSDR SWAA2022021664009Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727B -BS807 LBL21. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATION; FOUND DEEPEST LOCATION TO BE AT BS 747+10 LBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREAS FOSDR SWAA2022021664010Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727B - BS767 RBL21. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATION; FOUND DEEPEST LOCATION TO BE AT BS 727D+10 RBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREAS SDR SWAA2022021664016Cargo Track · corrodedCORROSION ON TRACK AT AFT CARGO BAY RBL13 BS767+6; BS787+2 - BS867. MARKED. / [01] EVALUATED CORROSION ON TRACK AT ALL LOCATION; FOUND DEEPEST LOCATION TO BE AT BS 767+6 RBL 13 WL 156; FOUND 0.030 REMOVED FROM ORIG 0.071 IN 1'X1' AREAS FOUND TO BE OUT OF LIMITSDR SWAA2022022163778Skin · crackedCRACK FOUND AT LH HORIZ.STAB LWR SKIN STA 193.90 ; I/B FASTENER ROW; 16' FROM FWD SPAR. CRACK LENGTH : 1'. CRACK FOUND AT LH HORI.STAB LWR SKIN STA 193.90 I/B FASTENER ROW 16' FROM FWD SPAR. CRACK LENGTH : 1'. / [01] REMOVED LEADING EDGE AT LH HORIZONTAL FOR ASDR SWAA2022021763779Vapor Barrier · crackedC/R R/T STA 663 VAPOR BARRIER CRACKED / [01] CLEANED AND STOP DRILL CRACK AREA AT R/H VAPOR BARRIER AS PER BOEING 737 SRM 51-70-04-2R-10 REPAIR 10;[02] PERFORMED DRY PROCESS AT R/H VAPOR BARRIER AS PER BOEING 737 SRM51-70-04-2R-10 REPAIR 10;[03] VERIFIED STEPSSDR SWAA2022021663752Stiffener · crackedL /H HORZ STAB RIB AT STAB STA. 129.50 HAS A CRACK AT THE 4TH STIFFENER FROM THE FRONT / [01] VERIFIED APPLICABILITY OF SRM 55-10-09-2R-4.[13] FABRICATED REPAIR PARTS; T-SECTION 7075-T76511 0.063' THICK LOT # 1430775-2; ANGLE BAC1490 7075-T62 0.063' THICK LOT SDR SWAA2022012763617None · cracked193 D PANEL LEFT HAND T CLIP CRACKED / [01] INSTALLED T- CLIP THAT WAS FABRICATED PER EA 22-153-00243 PER SRM 51-40-02SDR SWAA2022021663267Barrier · delaminatedBS 663 VAPOR BARRIER BULKHEAD DELAMINATING REPAIR NOTED RBL 39 WL 159 / [01] IDENTIFIED PART MATERIAL IAW SRM 57-10-10-0I-2 FIG 2 TABLE 2 ITEM 4.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-10-10-1A-2 PARA 4D(1).<BR>DAMAGE WILL BE REPAIRED IAW SRMSDR SWAA2022021663269Web · delaminatedBS 663 BULKHEAD DELAMINATED REPAIR AT LBL 39 WL 159 / [01] IDENTIFIED MATERIAL OF VAPOR BARRIER WEB IAW SRM 57-10-10-0I-2 FIGURE 1 AND 2; ITEM# 4; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PARA 4.D(1)<BR><BR>REPAIR TO BE ACCSDR SWAA2022012663290Panel · cracked194E PANEL HAS 3 EACH HOLES ON LEADING EDGE OF PANEL THAT HAVE CRACKING ON BACKSIDE OF PANEL ; 194E PANEL HAS 3 EACH HOLES ON LEADING EDGE OF PANEL THAT HAVE CRACKING ON ACKSIDE OF PANEL / [01] REMOVED AND REPLACED PANEL REF AMM 53-51-21.SDR SWAA2022012663291Panel · cracked193D PANEL HAS 6 OVERSIZED HOLES ON TRAILING EDGE OF PANEL WITH EVIDENCE OF CRACKING ON BACKSIDE OF PANEL ; 193D PANEL HAS 6 OVERSIZED HOLES ON TRAILING EDGE OF PANEL WITH EVIDENCE OF CRACKING ON ACKSIDE OF PANEL / [01] REMOVED AND REPLACED PANEL REF AMM 53-51SDR SWAA2022021663004Floor Panel · warpedCOCKPIT FLOOR PANEL 211AF IS WARPED AND WORN. / [01] NO ALLOWABLE LIMITS FOR PANEL 211AF FOUND FOR WARPED AND WORN DAMAGE ON SRM PART TO BE REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] FABRICATED; APPLIED CHEMICAL CONVERSION COAT AND PRIMED NEW FLIGHT DECK FLSDR SWAA2022012562830Slide · out of adjustAFT SERVICE DOOR SLIDE CROOKED IN CASE ; / [01] REPOSITIONED AFT SERVICE DOOR SLIDE ON DOOR PER M.M. 25-66-01.SDR SWAA2022012462661Handle · brokenAFT GALLEY SERVICE DOOR ASSIST HANDLE BROKEN ; / [01] REMOVED AND REPLACED HANDLE PER AMM 52-41-00SDR SWAA2022012462770Bracket · cracked193D STATION 727 CRACKED BRACKET. ; 193D STATION 727 LEFT VERTICAL WE RACKET AND T-CLIP CRACKED. / [01] SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)SDR SWAA2022012662495Battery · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1668 ; EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1668 ARE INOP / [01] PARTIAL UPDATE TO STEP 1; [02] REPLACED M1668 BATTERY AND PERFORMED SATISFACTORY TEST OF REPLACEMENT BATTERY PER AMM 33-51-06-96SDR SWAA2022012662496Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1673 ARE INOP ; / [01] REPLACED AND PERFORMED GOOD TEST OF EMERGENCY LIGHT BATTERY PACK; M1673 PER AMM 33-51-06-960-805.; [02] VERIFIED CORRECTIVE ACTION 1
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