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 SWAA2017080115463Battery Pack · dischargedAFT EMERGENCY LIGHTS FAULTY. R&R BATTERY PACK PER AMM.SDR SWAA2017080115345Charger · faultyAFT EMERGENCY LIGHTS FAULTY. R&R CHARGER PER AMM.SDR SWAA2017080115344Powerpack · faultyFORWARD RT EMERGENCY LIGHTS FAULTY. R&R POWER PACK PER MM.SDR SWAA2022013188454Fairing · delaminated#3 FLAP TRACK FAIRING TAILCONE DELAMINATED BEYOND LIMITS OUTBD SIDE OF TAILCONE / R&R #3 FLAP TRACK FAIRING TAILCONE IAW AMM 27-51-18SDR SWAA2017080115327Skin · crackedEXTERNAL POWER DOOR CUTOUT CRACKED FROM LOWER FASTENER HOLE AT THE CENTER LATCH LANDING. REPAIRED CUTOUT PER SRM.SDR SWAA2022013197142Door · corrodedTOILET SERVICE DOOR HAS CORRODED HINGES. / REMOVED AND REPLACED TOILER SERVICE DOOR ASSY PER AMM 52-49-09.SDR SWAA2017071715051Bonding Wire · looseL2 DOOR EMERGENCY EVAC SLIDE BONDING WIRE LOOSE. SECURED WIRE PER MT.SDR SWAA2022012792646Balance Weight · corrodedDURING RUDDER FLIGHT CONTROL CHECKS FOUND RUDDER WEIGHT TO BE CORRODED AND HAVING VISABLE SEPERATION ON L/H SIDE. / REPLACED RUDDER WEIGHT PER CMM REF. 55-40-09SDR SWAA2017071815141Slide · low pressureL2 DOOR EMERGENCY EVAC SLIDE LOW PRESSURE. R&R SLIDE PER MT & EA.SDR SWAA2017071715102Sensor · faultyDIVERSION, ON APPROACH INTO SNA, FLAPS 5 SELECTED NO FLAP MOVEMENT OCCURRED. R&R FLAP SKEW DETECTION SENSOR PER AMM.SDR SWAA2017071314990Bulkhead · crackedBULKHEAD CRACKED AT BS 663, RBL 35. REPAIRED THE BULKHEAD IAW EA.SDR SWAA2017071314989Bulkhead · crackedBULKHEAD CRACKED AT BS 663, LBL 35. REPAIRED THE BULKHEAD IAW EA.SDR SWAA2017071314988Battery Pack · no testRIGHT AFT EMERGENCY EXIT LIGHT FAILED THE CAPACITY CHECK AT LOCATION M1672. R & R THE BATTERY PACK IAW AMM.SDR SWAA2017071214964Sign · missingR2 DOOR EMERGENCY EXIT LENS COVER MISSING. R&R SIGN ASSEMBLY PER MM.SDR SWAA2017062614611Slide · unsecureL1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.SDR SWAA2017062814629Light · inoperativeRT EMERGENCY EXIT INDICATOR LIGHT FORWARD OF OVERWING EXIT INOP. R&R LIGHT ASSEMBLY PER AMM.SDR SWAA2017062814628Connector · disconnectedLT OVERWING EMERGENCY SLIDE LIGHT INOP. RECONNECTED CONNECTOR PER WDM.SDR SWAA2017062214567Slide · out of positionR2 DOOR EMERGENCY EVAC SLIDE ASSEMBLY OUT OF POSITION. POSITIONED THE SLIDE IAW MT.SDR SWAA2017061914450Light · looseRT FLOOR LIGHT LOOSE AT ROW 11. SECURED LIGHT STRIP PER SIP.SDR SWAA2022012689641Scuff Plate · crackedAFT CARGO BAY CENTER SCUFF PLATE IS CRACKED. / AFT CARGO BAY CENTER SCUFF PLATE IS ACCOMPLISHED ON EA 1-A53-2076 REV 11 DATED 05/11/1999 88928U 13JUN17SDR SWAA2017061214242Cable · out of rigDECLARED EMERGENCY, UPON SELECTING FLAPS '1' FOR APPROACH, LEADING AND TRAILING EDGE DEVICES DID NOT MOVE. ADJUSTED CABLES WFFA AND WWFB IAW MM.SDR SWAA2017062214570Rib · crackedRIGHT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT HSS 129.5, 4TH VERTICAL STIFFENER FROM THE FRONT. REPAIRED THE RIB IAW SRM.SDR SWAA2017062614595Rib · crackedRIGHT HORIZONTAL STABILIZER SPAR RIB WEB CRACKED AT HSS 129.5, FORWARD LOWER EDGE. REPAIRED RIB IAW EA.SDR SWAA2017062614594Rib · crackedLEFT HORIZONTAL STABILIZER SPAR RIB CRACKED AT HSS 120.3, FORWARD OUTBOARD LOWER FLANGE. REPAIRED THE RIB IAW EA.SDR SWAA2017062214568Rib · crackedRIGHT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT HSS 129.5, FORWARD STIFFENER THAT ATTACHES TO FORWARD SPAR. R & R THE RIB IAW SRM.SDR SWAA2017061214254Cover · missingLT EMERGENCY DOOR PULL HANDLE COVER HOOK & LOOP MISSING. INSTALLED COVER PER AMM.SDR SWAA2017061214253Lens · discoloredRT EMERGENCY DOOR LIGHT LENS DISCOLORED. R&R LENS IAW AMM.SDR SWAA2022012589577Plate · crackedRW PANEL 651EB IB FWD WIGGLE PLATE CRACKED / REMOVED AND REPLACED R/W PANEL 651EB FWD WIGGLE PLATE IAW SRM 51-40-05-0G-0 AND SRM 51-40-02-0G-0.SDR SWAA2022012589614Brake Assy · crackedPANEL BREAK ASSY CRACKED AT BS540 LBL 0 TO LBL 25 / REMOVED & REPLACED PNL BREAK ASSY AT BS 540 LBL 0 TO LBL 25 PER SRM 51-40-02-0G-0SDR SWAA2017062114548Rib · crackedRT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STA 129.5, 3RD VERTICAL STIFFENER FROM THE FRONT. REPAIRED RIB PER SRM.SDR SWAA2017062114547Rib · crackedLT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STA 120.3, 4TH VERTICAL STIFFENER FROM THE FRONT. REPAIRED RIB PER SRM.SDR SWAA2017062114546Rib · crackedLT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STA 120.3, 3RD VERTICAL STIFFENER FROM THE FRONT CRACKED. REPAIRED RIB PER SRM.SDR SWAA2017061214256Lens · defectiveRT AFT EMERGENCY EXIT SIGN LENS MISSING DIRECTIONAL ARROW. R&R LENS PER AMM.SDR SWAA2017061214255Lens · missingLT AFT EMERGENCY EXIT SIGN LENS MISSING DIRECTIONAL ARROW. R&R LENS PER AMM.SDR SWAA2022012489541Intercostal · crackedCRACKED INTERCOSTAL AT B.S. 277-294; R.B.L 2 W.L. 208.1 / REMOVED & REPLACED INTERCOSTAL AT BS 277-294 RBL 2 WL 208.1 PER SRM 51-40-02-0G-0SDR SWAA2022012489545Floor Support · crackedCRACKED FLOOR SUPPORT AT B.S. 540; B.L. 0 - R.B.L. 25; W.L. 208.1. / REMOVED & REPLACED FLOOR SUPPORT AT BS 540. BL 0 RBL 25 WL 208.1 PER SRM 51-40-02-0G-0SDR SWAA2022012589543Service Door · corroded***CORROSION*** ON FORWARD SERVICE DOOR MOP SILL B.S. 295-333. / F.S.D MOP SILL. REMOVED CORROSION @ 2 LOCATIONS 4.4' X 0.8'; 3.1' X 1.8'. MAX MATERIAL REMOVED .012. ORIGINAL THICKNESS .080'. REMAINING THICKNESS .068' FOUND TO BE OUT OF LIMITS PER SRM 53-10-15SDR SWAA2017062114535Splice Strap · corrodedAFT CARGO BAY FLOORBOARD PANEL SPLICE STRAP CORRODED AT BS 727D+5. R&R SPLICE STRAP IAW SRM.SDR SWAA2017062114534Stringer · crackedLT WING INBOARD FIXED LEADING EDGE 1ST STRINGER FORWARD OF FRONT SPAR FROM IFSS 206 TO IFSS 227 CRACKED AT OUTBOARD FLANGE. R&R STRINGER IAW SRM.SDR SWAA2017062014505Sidewall Support · corrodedAFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 727B TO 787, LBL 24. R & R THE SIDEWALL SUPPORT IAW SRM AND DWG.SDR SWAA2017062014503Stringer Splice · corrodedAFT CARGO BAY STRINGER SPLICE CORRODED AT BS 887, STRINGER 22L. R & R THE STRINGER SPLICE IAW SRM AND DWG.SDR SWAA2017062014502Web · corrodedFORWARD CARGO DOOR SUB THRESHOLD CORRODED. R & R THE WEB IAW SRM.SDR SWAA2017062014501Sidewall Support · corrodedRIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO 500D. R & R THE SIDEWALL SUPPORT IAW SRM AND DWG.SDR SWAA2017062014500Shield · corrodedRIGHT SHIELD CORRODED BETWEEN BS 490 TO 500A. R & R THE SHIELD IAW SRM.SDR SWAA2017062014499Frame · crackedR1 DOOR FORWARD LOWER STUB FRAME CRACKED AT BS 295, WL 209. REPAIRED THE STUB FRAME IAW ER AND EA.SDR SWAA2022012489533Floor Panel · delaminatedPASS CABIN FLOOR PANEL (241ACF) UPPER SURFACE DELAMINATION. / FABRICATED NEW PASSENGER CABIN FLOOR PANEL 241ACF IAW SRM 53-00-50-2R-0 PARA 1A (NOTE) AND DWG 147A5810-13 20549U 06/07/17SDR SWAA2022012489531Floor Panel · delaminatedL/H PASS CABIN FLOOR PANEL (242VF) UPPER SURFACE DELAMINATION. / REPAIRED ALL DELAMINATION DAMAGE ON L/H PASS CABIN FLOOR PANEL 242VF IAW SRM 53-00-50-2R-1. 56749U 07JUN17SDR SWAA2022012489532Floor Panel · delaminatedL/H PASS CABIN FLOOR PANEL (241XF) UPPER SURFACE DELAMINATION. / REPAIRED UPPER SURFACE DELAMINATION ON L/H PASS CABIN FLOOR PANEL 241XF IAW SRM 53-00-50-2R-1. 56749U 07JUN17SDR SWAA2022012489523None · corroded***CORROSION*** NOTED ON AED MOP SILL (BS 947 - BS 987/ LBL 50 / WL 208). / REMOVED CORROSION ON AED MOPSILL BS 947-987 IN A 34.00' X 1.5' X 0.012'; ORIGINAL MAT THICKNESS 0.080'; REMAINING THICKNESS 0.068' FOUND TO BE OUT LIMITS; REMOVED AND REPLACED AED MOPSSDR SWAA2017062614603Floorbeam · corrodedFLOORBEAM CORRODED AT BS 986.5, BETWEEN LBL 44 TO RBL 44. REPAIRED FLOORBEAM IAW EA.
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