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 SWAA2022021693841Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 242VF HAS EDGE DELAMINATED. / WORK ACCOMPLISHED ON NON ROUTINE X774407 (37835-2400-0182)SDR SWAA2018062523020Structure · corrodedELECTRONIC AND EQUIPMENT COMPARTMENT CHORD CORRODED BETWEEN BS 312 TO BS 360, STR 23L. REPAIRED CHORD IAW EA.SDR SWAA2018061922896Attach Angle · crackedRT WING TRANSVERSE WEB OUTBOARD ATTACH ANGLE CRACKED AT PROGRAM ROLLER SUPPORT ARM ATTACH POINT. R&R ANGLE IAW SRM.SDR SWAA2018061922895Support Angle · crackedRT WING UPPER TRAILING EDGE SUPPORT ANGLE CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT ABOVE NR 2 PYLON AFT TIP. R&R ANGLE IAW SRM.SDR SWAA2018061922894Web · crackedRT WING TRANSVERSE WEB CRACKED AT OUTBOARD UPPER RIVET JUST INBOARD OF PROGRAM ROLLER SUPPORT ARM ATTACH POINT. R&R WEB IAW SRM.SDR SWAA2018061822845Intercostal · corrodedE/E COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS 344 TO BS 351, STR 23L. R&R INTERCOSTAL IAW SRM & DWG.SDR SWAA2022021793276Web · corroded***CORROSION*** NOTED ON AFT CABIN FLOOR WEB ASSEMBLY (BS 1020 / RBL 15 / WL 207.5). / CORROSION ON AFT CABIN FLOOR WEB ASSEMBLY AT BS 1020; RBK 15 WL 207.5 WAS REMOVED; INSPECTED AND REPAIRED IAW 1-753-32831 REV IR AND ER 18-02960 REV IRSDR SWAA2022021793278Strap · corroded***CORROSION*** NOTED ON AFT CABIN FLOOR STRAP (BS 1016 / RBL 17.5 / WL 207.5). / CORROSION ON AFT CABIN FLOOR STRAP AT BS 1016 RBL 17.5 WL 207.5 WAS REMOVED; INSPECTED AND REPAIRED IAW EA 1-753-32831 REV IR AND ER 18-02960 REV IR (ORIGINAL ATTACHED CARD T7903SDR SWAA2022021793282Floor Support · corroded***CORROSION*** CORROSION ON FWD CABIN FLOOR SUPPORT AT BS 312; LBL 55; WL 208 (MARKED) / REMOVED AND REPLACED FWD CABIN FLOOR SUPPORT AT BS 312; LBL 55; WL 208 WITH ITEM #141A5220-2 IAW SRM 51-40-02-0G-0 AND AIPC 53-42-00-29.SDR SWAA2022021793285Intercostal · crackedCRACK FOUND ON FWD CABIN INTERCOSTAL; APPROX. BS 317; RBL 31; WL 208 (MARKED) / REMOVED AND INSTALLED NEW FWD CABIN INTERCOSTAL; APPROX BS 317; RBL 31; WL 208 ITEM # 141A5410U12 IAW SRM 51-40-02-0G-0 AND DWG # 141A5410SDR SWAA2022021793800Panel · crackedLH HORIZONTAL STABILIZER LEADING EDGE PANEL 331B; LE STA 105.26 LOWER INNER CHORD CRACKED AT AFT FASTENER HOLE; MARKED. / REMOVED AND REPLACED CRACKED CHORD ON L/H HORIZ. STAB. L/E PNL 331B @ STA. 105-26; P/N: 186A1352-7 SI#: 7550352 ATAG: WN5444 IAW B737-700 SDR SWAA2022021793812Angle · corrodedAFT CARGO PIT RIGHT Z-ANGLE STA 919-925 HAS CORROSION AROUND FASTENER HOLES / REMOVED CORROSION IN AFT CARGO COMPARTMENT; R/H ZEE ANGL AT STA 919-925 IAW SRM 51-10-02-0G-0. VERIFIED LIMITS; ORIGINAL THICKNESS .040'; LOSS OF .008'; REMAINING .032' OUT OF LIMITSSDR SWAA2022021693288Floor Panel · brokenAFT CABIN FLOOR PANEL 242XF IS BROKEN / DUE TO THE EXTENT OF DAMAGE ON PANEL 242XF; REPLACED WITH NEW PANEL IAW SRM 51-10-02-0G-0 PAR 9; AIPC 53-21-00-36B AND D3 TECHNOLOGIES DRAWING D1040M0003 REV ASDR SWAA2022021693289Floor Panel · brokenAFT CABIN FLOOR PANEL 242WF IS BROKEN / DUE TO THE EXTENT OF DAMAGE ON PANEL 242 WF; REPLACED WITH NEW PANEL IAW SRM 51-10-02-0G-0 PAR 9 AND AIPC 53-21-00-36B; D3 TECHNOLOGIES DRAWING D1040M0003 REV ASDR SWAA2022021693286Floor Panel · pulledAFT CABIN FLOOR PANEL 241XF HAS PULLED UPPER SURFACE PLIES / REPAIRED PULLED UPPER SURFACE PLIES ON AFT CABIN FLOOR 241XF IAW SRM 53-00-50-5R-1. 57066U 06/08/18SDR SWAA2018061822823Strap · corrodedAFT CABIN FLOOR STRAP CORRODED AT BS 1016, RBL 3. R&R STRAP IAW SRM AND DWG.SDR SWAA2018061822822Strap · corrodedAFT CABIN FLOOR STRAP CORRODED AT BS 1016, LBL 3. R&R STRAP IAW SRM AND DWG.SDR SWAA2018061822821Web · corrodedAFT CABIN FLOOR WEB ASSEMBLY CORRODED AT BS 1020, LBL 15. R&R WEB ASSEMBLY IAW SRM & DWG.SDR SWAA2018061822820Strap · corrodedAFT CABIN FLOOR STRAP CORRODED AT BS 1016, LBL 17.5. R&R STRAP IAW SRM AND DWG.SDR SWAA2018061222713Intercostal · crackedINTERCOSTAL CRACKED AT BS 285, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.SDR SWAA2018060722603Angle · corrodedAFT CARGO PIT RT SIDE Z-ANGLE CORRODED BETWEEN BS 727C+18 TO BS 767. R&R Z ANGLE IAW SRM.SDR SWAA2022021793767Shield · corrodedFWD CARGO; SPLASH SHIELD JUST AFT OF CARGO DOOR HAS CORROSION AT STA 500 TO 500+12 RBL22 / REMOVED AND REPLACED DAMAGED SHIELD IN FWD CARGO COMPARTMENT AT STA 500 TO 500+12; RBL 22 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 BOEING DWG# 143A0080 REV- AND BOEING DSDR SWAA2022021793757Channel · crackedPASSENGER CABIN FLOOR BOARD SUPPORT CHANNEL CRACKED AT LOWER SURFACE BS 540 LBL 26'. / REMOVED AND REPLACED FLOORBOARD SUPPORT CHANNEL AT BS 540; LBL 26 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND BOEING DWG# 143A0060 REV A WN0414SDR SWAA2022021693766Strap · corrodedCABIN FLOOR STRAP AT 0BL STA 1016 END CORRODED. UNDER FLOOR PANEL 241AEF. / REMOVED CORROSION ON CABIN FLOOR STRAP AT 1016; BLO IAW SRM 51-10-02-0G-0 VERFIED LIMITS; ORIGINAL THICKNESS .071' ;LOSS OF .21: REMAINING .050' OUT OF LIMITS IAW SRM 53-70--51-1A-1. RSDR SWAA2022021693759Intercostal · crackedPASSENGER CABIN INTERCOSTAL CRAKED AT FASTENER HOLE AT BS 380 TO BS 400 BL 0. / REMOVED AND INSTALLED A NEW INTERCOSTAL ANGLE BS380 TO BS400 BLO I/A/W B737 SRM 51-40-02-0G-0 AND BOEING DRAWING 143A5410 REV BSDR SWAA2022021693760Intercostal · crackedPASSENGER CABIN INTERCOSTAL CRAKED AT FASTENER HOLE AT BS 380 TO BS 400 RBL 10. / REMOVED AND INSTALLED A NEW INTERCOSTAL ANGLE BS380 TO BS400 RBL 10 I/A/W B737 SRM 51-40-02-0G-0 AND BOEING DRAWING 143A5410 REV BSDR SWAA2018062022928Gusset · crackedFORWARD CARGO STRINGER CLIP GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM AND DWG.SDR SWAA2018061122680Gusset · crackedFORWARD CARGO STRINGER CLIP GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET IAW DWG AND SRM.SDR SWAA2018060522504Light · inoperativeLT EMERGENCY EXIT WALL LAMP INOP. R&R LAMP IAW AMM.SDR SWAA2021112393710Floor Panel · corrodedSUPPLEMENTAL INFORMATION: FWD CARGO PIT FLOOR PNL 120BF TOP SIDE CORNER EDGES LENGTH AND WIDTH OF PNL SEVERAL AREAS OF MINOR LIGHT CORROSION TOP SKIN AS MARKED / PANEL REPLACED ON NRC X774048 W/O 37835-1400-0014 COPY ATTACHEDSDR SWAA2022021793716Floor Panel · corrodedFWD CARGO PIT FLOOR PNL 120AF TOP SKIN SURFACE IN SEVERAL AREAS AS MARKED IS CORRODED / FWD CARGO FLOOR PNL 120AF TOP SKIN AREA'S OF CORROISION REPLACED FWD CARGO PNL 120AF WITH NEW PANEL P/N 453A1610-14 'A' TAG WN2350 I/A/W AIPC 25-52-10-16 ITEM 5 PG 11 SHEETSDR SWAA2022021793707Strip · corrodedFWD CARGO PIT R/H SIDE; SIDEWALL TO FLOOR PNL TRANSITION STRIP 1 EA IS CORRODED IN SEVERAL AREAS ON BOTTOM SIDE AS MARKED / REPLACED FWD CARG TRANSITION STRIP IAW AIPC 25-52-10-01 ATAG: WN8944SDR SWAA2022021793708Strip · corrodedFWD CARGO PIT L/H SIDE SIDEWALL TO FLOOR PNL TRANSITION STRIPS 2 EA; SEVERAL AREAS CORRODED ON BOTTOM SIDE AS MARKED / VERIFIED QTY (2) NEW CAP STRAPS PN453A1611-11 ATAG#A75711 PN:453A164-10 ATAG# WN2820. INSTALLED QTY(3) CAP STRIPS IAW DWG 453A1600 REV C; SRMSDR SWAA2022021793712Floor Panel · corrodedFWD CARGO PIT FLOOR PNL 120CF TOP SKIN 3EA CORNERS AS MARKED IN SEVERAL AREAS THE LENGTH AND WIDTH OF PNL CORRODED / VERIFY NEW PANEL #120CF AS P/N 453A1610-32 FWD CARGO FLOOR PANEL A-TAG WN2230 IAW AIPC 25-52-10-16 PG 3. ITEM 35 & PG 11.A-TAG WN2230SDR SWAA2022021793713Strip · corrodedAFT CARGO BAY; FLOOR CAPSTRIP MARKED R/H #1 IS CORRODED ON BOTTOM SIDE. / REPLACED AFT CARGO FLOOR CAPSTRIP R/H #1 IAW AIPC 25-52-10-02 PG 45 ATAG: Y0OO25SDR SWAA2022021793714Strip · corrodedAFT CARGO BAY; FLOOR CAPSTRIP MARKED R/H #2 IS CORRODED ON BOTTOM SIDE. / REPLACED AFT CARGO FLOOR CAPSTRIP RH#2 IAW AIPC 25-52-10-02 PG 6 ATAC:A73546SDR SWAA2022021793715Strip · corrodedAFT CARGO BAY; FLOOR CAPSTRIP MARKED R/H #3 IS CORRODED ON BOTTOM SIDE. / VERIFIED PART TO BE P/N 453A2611-3 FOR AFT CARGO FLOOR CAPSTRIP RH #3 IAW AIPC 25-52-10-02. LOCATED & DRILLED CAP STRIP IAW SRM 51-40-05-0G-0 STEP 4(A) & BOEING DWG: 453A2611 ID: 0003 RESDR SWAA2022021793717Strip · corrodedAFT CARGO BAY; FLOOR CAPSTRIP MARKED L/H CENTER IS CORRODED ON TOP AND BOTTOM SIDE. / REPLACED CAPSTRIP AT AFT CARGO L/H CENTER IAW AIPC 25-52-10-02 PG 44 ATAG: A52449SDR SWAA2022021793718Strip · corrodedAFT CARGO BAY; FLOOR CAPSTRIP MARKED L/H AFT IS CORRODED ON TOP AND BOTTOM SIDE. / REPLACED CAPSTRIP AT AFT CARGO FLOOR L/H IAW AIPC 25-52-10-02 PG 45 ATAG: WN355SDR SWAA2022021793719Strip · corrodedFWD CARGO PIT FLOOR PNL 120AF R/H FLOOR TO SIDEWALL TRANSITION STRIP AS MARKED IN SEVERAL AREAS ON BOTTOM SIDE IS CORRODED / REPLACED FWD CAP STRIP C FWD CARGO PN420AF R/H FLOOR TO SIDEWALL IAW AIAC 25-52-10-01 ATAG: A74895SDR SWAA2022021793720Strip · corrodedAFT CARGO BAY; FLOOR CAPSTRIP MARKED L/H FWD IS CORRODED ON BOTTOM SIDE. / REPLACED AFT CARGO FLOOR CAPSTRIP L/H FWD IAW AIPC 25-52-10-02 PG 45 ATAG: WN832SDR SWAA2022021793752Attach Bracket · crackedAFT CARGO; ATTACH CLIP CRACKED BELOW FLOOR LINE ON FWD SIDE OF STA 867 FRAME BETWEEN STR 26 AND 27L / REMOVED & REPLACED CLIP AFT CARGO BELOW FLOOR LINE STA 867 BETWEEN STR 26&27L IAW SRM 51-40-02-0G-0 & DWG 149A8102 REV:CSDR SWAA2022021693703Floor Panel · corrodedAFT CARGO BAY FLOOR PANEL 140DF IS CORRODED ALONG TOP EDGES. / FABRICATED NEW REPLACEMENT PANE FOR AFT CARGO PANEL 140DF IAW BOEING 737 DWG 453A2610SDR SWAA2022021693726Strap · corrodedCABIN FLOOR STRAP AT 0BL STA 1016 END CORRODED. UNDER FLOOR PANEL 241AEF. / REMOVED CORROSION ON CABIN FLOOR STRAP AT 1016; BLO IAW SRM 51-10-02-0G-0 VERFIED LIMITS; ORIGINAL THICKNESS .071' ;LOSS OF .21: REMAINING .050' OUT OF LIMITS IAW SRM 53-70--51-1A-1. RSDR SWAA2022021693745Floor Panel · looseMAIN CABIN FLOOR PANEL #222BF; JUST INSIDE THE R1 DOOR HAS THE TOP LAYER OF COMPOSITE COMING LOOSE. / REPAIRED PEELING TOP PLY AND 19 HEEL IMPUT DELAMINATIONS ON PANEL 222BF IAW SRM 53-00-50-2R-0 PARA 5.SDR SWAA2022021693742Floor Panel · looseMAIN CABIN FLOOR PANEL#222DF HAS THE TOP LAYER OF COMPOSITE COMING LOOSE. / REPAIRED TOP LAYER ON MAIN CABIN FLOOR PANEL 222DF PER B737 SRM 53-00-50-2R-1SDR SWAA2022021693740Floor Panel · looseMAIN CABIN FLOOR PANEL AT STA. 360 LH SIDE HAS THE TOP LAYER OF COMPOSITE COMING LOOSE.#231CT / EVALUATED; CLEANED; PREPPED AND REPAIRED FIBER DAMAGE AT UPPER SURFACE FWD EDGE OF FLOORBOARD 231CF IAW B737 SRM 53-00-50-2R-1; PAR 3 (A; C; E & F; - - K1; L1; M1) SDR SWAA2022021693738Floor Panel · looseMAIN CABIN FLOOR PANEL #221DF AT STA. 328 JUST INSIDE THE L1 DOOR HAS THE TOP LAYER OF COMPOSITE COMING LOOSE. / REPAIRED PANEL 221DF UPPER SURFACE DELAM IAW SRM 53-00-50-2R-0 AND 53-00-50-3R-0SDR SWAA2022021693736Floor Panel · corrodedMAIN CABIN UNDER FLOOR PANEL#221BF CORROSION POWDER IS ON TOP OF THE INTERCOSTAL AND AVIONICS TRAY. INTERCOSTAL IS LOCATED BETWEEN STA 294.5 AND 312 LBL 13' / INSTERCOSTAL AT STA 294.5 TO STA 312 LBL 13 CORRODED; REMOVED CORROSION AND VERIFIED ORIG 'T' .170' MSDR SWAA2022021693733Floor Panel · looseMAIN CABIN FLOOR PANEL #222AF AT STA. 270 HAS THE TOP LAYER OF COMPOSITE COMING LOOSE. / EVALUATED; PREPPED; CLEANED AND REPAIRED FIBER DAMAGE ON ENTIRE UPPER SURFACE ON FLOORBOARD 222AF IAW B737 SRM 53-00-50-2R-1; PAR 3 (A; C; E & F K1; L1; - M1) REV 64.
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