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 SWAA2021070281174Angle · corrodedE&E BAY STA 312+9 STR 23L WL 167 ATTACHING INTERCOSTAL ANGLE CORRODED AROUND FASTENERS FWD AND AFT SIDE. REMOVED CORROSION ATTACH INTERCOSTAL ANGLE AND CHECK WITH 10X MAGNIFYING GLASS IAW SRM 51-10-02-0G-0 ITEM15. REMOVED 3EA FASTENERS TO ACCESS REPAIR AREASDR SWAA2021070281172Stringer · corrodedE&E BAY STA 312+2 STR 23L WL 167 CORRODED. REMOVED CORROSION STRINGER 23 L IAW SRM 51-10-02-0G-0 ITEM 15 AND CHECK WITH 10 X MAGNIFYING GLASS IAW SRM 51-10-02-0G-0 ITEM 15. REMOVED 4 EA FASTENERS' ON STRINGER REPAIR AREA IAW SRM 51-40-02. VERIFIED STEPS SDR SWAA2021061781448Skin · crackedLH HORIZONTAL STAB SKIN IS CRACKED ON INBD SIDE OF RIB AT STAB STA 184.70; 26' FROM FWD SPAR; .70' IN LENGTH. FABRICATED REPAIR PARTS IAW SRM 55--10-01-2R-11 & EA 21-155-01660-WIP1 P2 SERVICE BULLETIN 737-55-1096. APPLIED ALODINE AND PRIME TO REPAIR PARTS DOSDR SWAA2021061581179Light · looseFDR DOOR; EMERGENCY EXIT LIGHT ASSEMBLY IS SECURED BY ONLY 1 FASTENER. ; / REMOVED AND REPLACED AFT EMERGENCY EXIT LIGHT IAW AMM 33-51-01-960-801; OPS CHECK GOOD; COMPLETED INSPECTION CARD STEPS 1. AND 2. CORRECT REF IS AMM 33-51-01-960-802.<BR>AUDIT C/WSDR SWAA2021061481449Skin · crackedRH HORIZONTAL STAB SKIN IS CRACKED ON INBD SIDE OF RIB AT STAB STA 193.90; 16.5' FROM FWD SPAR; .80' IN LENGTH. DOT A177-001 ; / C/W ITEMS 13; 14; AND 15; RII C/W AUDIT COMPLETE; RII C/W AUDIT COMPLETESDR SWAA2021070280744Floor Panel · damagedPASSENGER CABIN 241AF, UPPER SURFACE, SEVERAL AREAS OF PULLED FACE SHEET PLIES. EVALUATED DAMAGE; FLOOR PANEL 241AF IS B.E.R. REPLACED PANEL BY FABRICATION IAW B737 SRM 53-00-50-2R-0 PAR 1A NOTE; PAR 4 TABLE 204; DWG 144A5810-127; AND BAC5085. CURED ADHESISDR SWAA2021061180733Lamp · inoperativeAFT MOST EMERGENCY LIGHT ON R/H SIDE OF FUSELAGE INOP ; / RELAMPED AFT MOST EMERGENCY LIGHT ON RIGHT SIDE OF FUSELAGE. OPS CK GOOD. PER AMM 33-51-04SDR SWAA2021070280736Rib · crackedRIGHT STAB LEADING EDGE PANEL 8TH RIB FROM INBOARD END IS CRACKED ; / [01] REMOVED RH STAB LE RIB ASSY AT LE STA 142.45 IAW SRM 51-40-02-0G-0; [02] VERIFIED NEW RIB ASSY AS P/N 186A1308-2 A TAG IE0100 PER DWG 186A1308 REV-; [03] C/W STEP 2; [04] LOCATED AND DRSDR SWAA2021070280735Rib · crackedLEFT STAB LEADING EDGE PANEL 3RD RIB FROM INBOARD END CRACKED ; / [01] REMOVED LH STAB LE RIB AT LE STA 95.96 IAW SRM 51-40-02-0G-0; [02] VERIFIED NEW RIB ASSY. AS P/N 186A1303-1 ATAG WN5727 PER DWG 186A1303 REV -; [03] C/W STEP 2; [04] LOCATED AND DRILLED NEWSDR SWAA2021070280175Attach Angle · corrodedDOT A223-011 AFT CARGO AFT BULKHEAD LOWER ATTACH ANGLE ASSY CORRODED AROUND FASTNER HOLES. STA 947.5. REMOVED CORROSION FROM AFT BULKHEAD LOWER ATTACH ANGLE IAW SRM 51-10-02-0G-0. MEASURED MATERIAL LOSS. ORIGINAL MATERIAL THICKNESS .080 LOSS OF .005 WITH SDR SWAA2021070280174Angle · corrodedDOT A223-007 AFT CARGO L/H Z ANGLE CORROSION AROUND FASTNER HOLES STA 727D TO 787. REMOVED CORROSION FROM Z ANGLE IAW SRM 51-10-02-0G-0; [02] VERIFIED LIMITS FOR LH Z ANGLE ORIGINAL THICKNESS .040 REMAINING THICKNESS .011. MATERIAL LOSS OF .029. OUT OF LIMITSDR SWAA2021070280171Angle · corrodedDOT A223-002 AFT CARGO R/H Z ANGLE CORROSION AROUND FASTNER HOLES 727E TO 767. ; / [01] REMOVED CORROSION FROM AFT CARGO RIGHT HAND Z ANGLE STA 727E TO STA 767 AND VERIFIED MATERIAL REMOVAL WITH 10X MAG. IAW SRM 51-10-02 MEASURED MATERIAL LOSS USING TOOL # 366SDR SWAA2021070280160Floor Panel · corrodedA-61 DOT 019 AFT PIT FLOOR PNL 140CF HAS CORROSION ON L/H AND R/H EDGES STA 767 TO STA 887 LBL 25 AND RBL 25 WL 155 ; / [01] VERIFIED MATERIAL AS 2024-T3-.071. IAW AMM 25-52-01-201-801. A-TAG # A53468.; [02] C/W STEP 1; [03] FABRICATED AFT PIT FLOOR PANEL 140CSDR SWAA2021070280170Floor Panel · corrodedA22-33; FWD PIT FLOOR PANEL 120AF; 3 EDGES OF UPPER SURFACE; CORROSION; (SECONDARY STRUCTURE) ; / [01] VERIFIED MATERIAL AS 2024-T3- .071.IAW AMM 25-52-01-201-801. A-TAG # A30648; [02] C/W STEP 1; [03] BEGAN FABRICATING FLOOR PANEL 140AF. IAW AMM 25-52-01-201-SDR SWAA2021070280169Floor Panel · corrodedA22-32; FWD PIT FLOOR PANEL 120CF; LEFT & RIGHT EDGES OF UPPER SURFACE CORROSION; (SECONDARY STRUCTURE) ; / [01] EVALUATED DAMGE FOUND TO BE OUT OF LIMITS DUE TO AREA BEING OVER 20' IAW SRM 53-00-53-1A-1 FIG 102; [02] VERIFIED STEP 1; [03] VERIFIED MATERIAL TOSDR SWAA2021070280164Floor Panel · corrodedA-61 DOT 018 AFT PIT FLOOR PNL 140DF HAS CORROSION ON AFT EDGE STA 947 RBL 25 TO LBL 13 WL 155 ; / [01] VERIFIED MATERIAL TO FAB NEW PANEL AS 2024-T3 .071' ATAG A30655 IAW AMM 25-52-01-201-801; [02] VERIFIED STEP 1; [03] FABRICATED NEW FLOOR PANEL 140DF IAW AMSDR SWAA2021070280163Floor Panel · corrodedA-61 DOT 017 AFT PIT FLOOR PNL 140AF HAS CORROSION AN L/E OF PNL STA 727+4' LBL 25 TO RBL 25 WL 155 AND STA 727D +6' TO STA 727D +12' RBL 25 WL 155 ; / [01] VERIFIED MATERIAL TO FABRICATE NEW FLOOR PANEL 140AF AS 2024-T3 .071' ATAG A53456 IAW AMM 25-52-01-201-SDR SWAA2021070280135Gusset · crackedFWD PIT STA 500D; STR 19L; GUSSET SUPPORRT BRACKET CRACKED IN RADIUS; DOT 19. ; / [01] REMOVED CRACKED GUSSET IAW SRM 51-40-02-0G-0; [02] VERIFIED NEW PART; GUSSET; P/N 143A9481-6; IAW BOEING DWG 143A7902 REV-<BR>ATAG A54122; [03] LOCATED AND DRILLED NEW GUSSESDR SWAA2021070280148Gusset · crackedFWD PIT STA 500D; STR 19R; GUSSET SUPPORRT BRACKET CRACKED IN RADIUS; DOT 18. ; / [01] REMOVED CRACKED SUPPORT BRACKET IAW SRM 51-40-02-0G-0; [02] VERIFIED ITEM 1; [03] NEW PART VERIFIED; GUESST P/N 143A9481-5; IAW BOEING DWG 143A7902 REV-<BR>ATAG A54119; [04]SDR SWAA2021070280144Floor Support · corrodedFWD PIT STA 492; RBL20; WL186; LONGITUDINAL FLOOR SUPPORT CORROSION. REMOVED CORROSION FROM FORWARD CARGO FLOOR TRACK AT STA 492; RBL 20 AND VERIFIED CORROSION REMOVED WITH 10X MAG. IAW SRM 51-10-02. MEASURED MATERIAL LOSS. ORIGINAL MATERIAL THICKNESS .06SDR SWAA2021070280176Angle · corrodedDOT A223-001 AFT CARGO R/H Z ANGLE CORROSION AROUND FASTNER HOLES STA 727+8 TO 727E. ; / [01] REMOVED CORROSION FROM AFT CARGO RIGHT HAND Z ANGLE STA 727+8' TO STA 727E AND VERIFIED MATERIAL REMOVAL WITH 10X MAG. IAW SRM 51-10-02 MEASURED MATERIAL LOSS USING TSDR SWAA2021070280133Channel · corrodedFWD PIT STA 500A+6-10; RBL25; WL186; Z-CHANNEL; CORROSION, REMOVED CORROSION FROM FORWARD CARGO Z ANGLE AT STA 500A+6' TO 500A+10' RBL 24 AND VERIFIED CORROSION REMOVAL WITH 10X MAG. IAW SRM 51-10-02 MEASURED MATERIAL LOSS, ORIGINAL MATERIAL THICKNESS .040 LSDR SWAA2021070280167Cap · corrodedA22-30; FWD PIT LEFT SIDEWALL TO FLOOR CAP STRIPS HAVE CORROSION; MRK'D (SECONDARY STRUCT) ; / [01] RECIEVED NEW CAP STRIPS P/N 453A1611-6 A TAG WN7868; 453A1611-11 A TAG WN0538; AND 453A1611-10 A TAG WN7837 IAW BOEING DRAWING 453A1600 CAP STRIPS WILL BE INSTASDR SWAA2021070280168Cap · corrodedA22-31; FWD PIT RIGHT SIDEWALL TO FLOOR CAP STRIPS HAVE CORROSION; MRK'D (SECONDARY STRUCT) ; / [01] RECIEVED NEW CAP STRIPS PART 453A1611-5 A TAG A54995 ANDP/N 453A1611-12 ATAG WN7839 PART TO BE INSTALLED ON TASK CARD 5330-E-16461-NG; [02] VERIFIED STEP 1 IS SDR SWAA2021060780191Latch · looseUPPER COCKPIT DOOR EMERGENCY EXIT LATCH LOOSE ; / RESET COCKPIT DOOR EMERGENCY EXIT UPPER DOOR LATCH PER AMM 52-51-08.SDR SWAA2021060779244Seal · crackedRIGHT HORIZONTAL STABILIZER TO BODY UPPER SLIDING SEAL IS CRACKED. ; / R AND R SLIDING SEAL PER M/M REF 53-31-31; R AND R SLIDING SEAL PER M/M REF 53-31-31SDR SWAA2021060779243Seal · crackedLEFT HORIZONTAL STABILIZER TO BODY UPPER SLIDING SEAL IS CRACKED. ; / REMOVED & REPLACED L/H UPPER SLIDING SEAL PER AMM 53-31-31; REMOVED & REPLACED L/H UPPER SLIDING SEAL PER AMM 53-31-31SDR SWAA2021060778182Rib · crackedRH HORIZONTAL LEADING EDGE RIB; 4TH FROM INBD; AT STAB STA 105.26; IS CRACKED IN RADIUS. REMOVED RIB IAW SRM 51-40-02-0G. REMOVED AND REPLACED RH HORIZONTAL STAB LEADING EDGE RIB 4TH FROM INBD AT STAB STA 105.26 IAW DRAWING 186A1001 REV- SRM 51-40-05-0G SRMSDR SWAA2021060178144Light · looseESCAPE LIGHTING ON FLOOR NEXT TO ROW8 LEFT SIDE IS LOOSE. ; / SECURED FLOOR PATH ESCAPE LIGHTING STRIP NEAR ROW 8 PER S.I.P.SDR SWAA2021060178112Lens · missingEXIT LIGHT COVER MISSING AT LEFT BASE OF RIGHT OVERWING EXIT. ; / REPLACED LIGHTED SIGN LENS AT OVERWING R/H EMERGENCY IAW AMM 33-51-01. A/C OK FOR SERVICE.SDR SWAA2021061577739Stiffener · crackedLEFT HORIZONTAL STAB RIB ASSY 5 STAB STA 129.50 STIFFENER 3 HAS A CRACK DOT A-21-21 ; / REPAIRED L\H STAB RIB 129.5 IAW SRM 55-10-09-2R-5; VERIFIED ITEM 22; AUDIT C/WSDR SWAA2021060178179Isolator · brokenR1 DOOR AFT UPPER SLIDE MOUNT ISOLATOR IS BROKEN; MARKED. A177-006 ; / REPLACED R1 SERVICE DR UPPER SLIDE MOUNT ISOLATOR IAW SRM 51-40-02-OG-O; ALL WORK C/W<BR>AUDIT C/WSDR SWAA2021060178178Isolator · brokenR1 DOOR FWD UPPER SLIDE MOUNT ISOLATOR IS BROKEN; MARKED. A177-005 ; / REMOVED AND REPLACED R1 DR FWD MOUNT ISOLATOR IAW SRM 51-40-02-OG-O; C/W; AUDIT C/WSDR SWAA2021061577730Shield · corrodedAFT CARGO COMPT. SHIELD AT STA 767 - 787; RBL 25; WL 156 HAS CORROSION AT FASTENER HOLES DOT A-21-15 ; / INSTALLED NEW ZEE SHIELD IAW B737-700 SRM 51-40-05 AND BAC DWG 146A0081 REV.-; ALL STEPS C/W; OUT OF SEQUENCE; VERIFIED OK TO INSTALL FOR STEP 5; VERIFIED SDR SWAA2021061577003Attach Angle · crackedDOT 45-005; PANEL 651FB OUTBOARD ATTACH ANGLE; FORWARD ATTACH POINT; ATTACH BRACKET COMMON TO WING IS CRACKED IN HALF. ; / REMOVED AND REPLACED PANEL 651FB OUTBOARD ATTACH ANGLE COMMON TO WING WITH P/N 115A5552-2 A52333 IAW SRM 51-40-02-0G-0; VERIFIED ITEM 1.<SDR SWAA2021061576678Attach Angle · crackedDOT 45-002; RH RIB DEFLECTOR; INBOARD ATTACH ANGLE IS CRACKED AT LOWER FASTENER HOLE COMMON TO RIB DEFLECTOR. ; / REMOVED CRACKED ANGLE IAW SRM 51-40-02-0G-0 FIGURE 8. VERIFIED NEW CLIP P/N115A6260-2 TAG# 52109 IAW DWG 115A6200 REV .B VERIFIED STEP 2 IS COMPLESDR SWAA2021061576684Bulkhead Web · crackedR/H STA 663 LOWER VAPOR BARRIER WEB CRACKED BETWEEN RBL 30 AND RBL45 REQUIRES PERMANENT REPAIR ; / REPAIRED CRACKS IN R/H STA 663 VAPOR BARRIER FROM RBL30-RBL45. IAW B737-700 SRM 57-10-10-2R-10;SRM 51-70-04-2R-10; SRM 51-70-04-2R-0.; VERIFIED ITEM 3 AND 4; AUDSDR SWAA2021061576681Bulkhead Web · crackedL/H STA 663 LOWER VAPOR BARRIER WEB CRACKED BETWEEN LBL 30 AND LBL 40 REQUIRES PERMANENT REPAIR ; / REPAIRED CRACKS IN L/H STA. 663 VAPOR BARRIER FROM LBL30-LBL40. IAW B737-700 SRM57-10-10-2R-2; SRM51-70-04-2R-10; SRM51-70-04-2R-0; VERIFIED ITEMS 3 AND 4; AUDISDR SWAA2021051068978Power Supply · faultyCEILING EXIT SIGN @ OVERWING EXIT FLICKERS ON & OFF DURING FLIGHT ; / REMOVED & REPLACED POWER SUPPLY IAW AMM 33-51-06 OPERATIONAL CHECKS GOODSDR SWAA2021042967293Lamp · inoperativeLEFT GROUND EMERGENCY FLOOD LIGHT INOP ; / RELAMPED LEFT GROUND EMERGENCY FLOOD LIGHT PER AMM 33-51-04.SDR SWAA2021042966858Lamp · inoperativeLEFT GROUND EMERGENCY FLOOD LIGHT INOP / RELAMPED LEFT GROUND EMERGENCY FLOOD LIGHT REF AMM 33-51-04SDR SWAA2021042665587Light · displacedFLIGHT ATTENDANTS REPORTED LUMINESCENT STRIPS ON CABIN FLOOR BOWED UP AT ROW EIGHT. REPORTED BOTH STRIPS WERE A TRIP HAZARD. AFTER FLIGHT; BOTH STRIPS CARPETING WERE FLAT ON THE FLOOR. RESECURED LUMINESCENT STRIPS ON CABIN FLOOR ROW EIGHT PER SIPSDR SWAA2021042665340Battery · dischargedAED HAS LOW BATTERY REPACED AED IAW AMM 256900960802 PN OFF 2560000201 SN OFF B11L03093 PN ON 256001201 SN ON BI6G05047SDR SWAA2021042365156Module · inoperativeFO EFIS CONTROL PANEL BACK LIGHTS INOP. / FOUND C/B C3 ON EMER/FO LIGHTING PANEL POPPED R&R MODULE LIGHT MODULE P3-4 ON F/O SIDE PER AMM 33-11-00 OPS CHECK GOOD.SDR SWAA2021042064430Structure · damagedRH HORIZONTAL TIP FWD SECTION HOLES ELONGATED. REPLACED FWD SECTION OF TIP PER SRM 514002.SDR SWAA2021041564199Light · loosePHOTO ILLUMINCENT FLOOR LIGHTING FIRST OFFICERS SIDE; LOOSE AT ROW 9 / REMOVED DEBRI FROM UNDER PHOTO ILLUMINCENT FLOOR STRIP @ ROW 9 ON F/O SIDE; RESECURED PHOTO ILLUMINCENT STRIP @ 9D PER SIPSDR SWAA2021040560497Slide · out of positionFORWARD ENTRY GIRT BAR HARD TO ARM. / REPOSITIONED SLIDE (FWD ENTRY DOOR) PER MT 725-61-06. VERIFIED GIRT BAR ARMS PROPERLYSDR SWAA2021032257394Sign · detachedAFT EXIT SIGN (AFT GALLY) DETATCHED FROM CIELING / RESECURED AFT GALLY EMERGENCY EXIT SIGN IAW AMM 33-51-01SDR SWAA2021031756176Light · inoperativeCAPTAIN SIDE OVERWING EXIT LIGHT INOP / RELAMPED OPS NORMAL 33-51-21SDR SWAA2021031755684Lens · missingEMERGENCY EXIT LIGHT COVER FELL OFF L/H SIDE O/WING EXIT / INSTALLED LIGHT LENS PER AMM 33-51-01
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