Boeing 737-8H4
Service difficulty reports · 24,314
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 = '7378H4' 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 = '7378H4' 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 SWAA2026102171174Support Angle · crackedCRACKED SUPPORT ANGLE, BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, DWG-143A5400, SHT 154, REV -, & DWG 143A5400, SHT 201, REV -.SDR SWAA2026102117802Support Angle · crackedCRACKED RT WING SUPPORT ANGLE FIXED T/E, ORSS 261 + 16. REPLACED THE SUPPORT ANGLE & FASTENERS IAW SRM 51-40-02, & DWG 115A6200, SHT 17, REV A.SDR SWAA2026100782166Access Panel · crackedCRACKED ACCESS PANEL 544BB, INTERNAL SKIN, LT WING. REPAIRED THE ACCESS PANEL SKIN IAW EA 26-157-02598, AND EA 26-157-02598-WIP1.SDR SWAA2026092397319Battery Pack · inoperativeALL INTERIOR CEILING L/H EXIT LIGHTS DO NOT ILLUMINATE AFT OF OVERWING EXIT ROWS AND MID & AFT LEFT EXTERIOR OVERWING TO NOT ILLUMINATE. R & R M1670 EMERGENCY BATTERY IAW AMM 33-51-06-960-805, OPS CHKD GOOD.SDR SWAA2026092374315Battery Pack · inoperativeALL INTERIOR CEILING RT EXIT LIGHTS DO NOT ILLUMINATE AFT OF OVERWING EXIT ROWS AND MID AND AFT RT EXTERIOR OVER WING TO NOT ILLUMINATE. REMOVED AND REPLACED M1671 EMERGENCY BATTERY PER AMM 33-51-06-960-805. OPS CHECK GOOD.SDR SWAA2026092146823Fastener · missingLEFT ELEVATOR OTBD BALANCE WEIGHT INNER MOST TRIM WEIGHT MISSING INBD ATTACH HARDWARE. INSTALLED FASTENER IAW SRM 51-61-04, AND SRM 51-40-02-0G-0-B00387.SDR SWAA2026092107806Fitting · looseFED AFT GIRT BAR FITTING LOOSE. TIGHTENED LOOSE SCREWS COMMON TO FED AFT GIRT BAR FITTING IAW AMM 25-66-02-400-801.SDR SWAA2026102134422Shield · corrodedCORRODED SHIELD PLATE, BTWN BS 767 - 787, STRINGER 25R FAULT WAS RESOLVED ON ANOTHER FAULT, SEE FAULT TTG8Q01ECET5.SDR SWAA2026102120545Pin · deformedDEFORMED PLATING ON LOWER ATTACHMENT PIN CENTER SECTION REAR SPAR LUG AT RT HORIZONTAL STAB. REPLACED ONLY THE LOWER ATTACHMENT PIN CENTER SECTION REAR SPAR LUG IAW AMM 27-41-11-400-801, & AMM 27-41-11-400-801. FOR INSTALLATION LOWER PIN SEE TTG8R007BQES.SDR SWAA2026102174565Strap · corrodedCORRODED STRAP, BTWN BS 787 - 794.3, RBL 20, WL 156.1 IN THE AFT CARGO BAY. REPLACED THE STRAP IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 146A0081, SHT 49, REV A.SDR SWAA2026101493635Access Panel · delaminatedDELAMINATED ACCESS PANEL 194CR ON BODY FAIRING. REPAIRED THE ACCESS PANEL ON THE BODY FAIRING IAW SRM 51-70-04-2R-2, REPAIR 2.SDR SWAA2026100616799Light · deterioratedDETERIORATED PHOTO LUMINESCENT STRIPS. REPLACED PHOTO LUMINESCENT STRIPS IAW AMM 33-51-15- 960-801, AND DWG 33510503, SHEET 14, AND 5, REV B.SDR SWAA2026092275476Battery · inoperativeFOUR EMERGENCY FLASHLIGHTS LOCATED UNDER AFT JUMP SEATS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT BATTERIES IAW CMM 25-60-02.SDR SWAA2026092128212Battery Pack · inoperativeSEVERAL EXTERIOR AND INTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED & REPLACED THE BATTERY PACKS AT THE M2816, M1670, M1671, M1694, M2335, M1673, & M1672 IAW AMM 33-51-06-960-805. PERFORMED SATISFACTORY OPS CHECK IAW B737 AMM 33-51-06-960-805.SDR SWAA2026092120268Indicator · trippedFLAPS LOCKED 15, COMMANDED 30_ PERFORMED FSEU BITE WITH NO CURRENT FAULTS FOUND. FOUND #1 FLAP DRIVE TRANSMISSION TORQUE INDICATOR POPPED. PERFORMED FSEU BITE WITH NO CURRENT FAULTS FOUND. INSPECTED FLAP TRANSMISSION TORQUE TRIP INDICATORS AND FOUND #1 FLAP DRSDR SWAA2026102118881Frame · crackedCRACKED FRAME, BS 312, STR 5 - 6L IN THE FWD GALLEY AREA. PERFORMED A REPAIR TO THE FRAME IAW M-22-153-01244.SDR SWAA2026102164313Light · deterioratedDETERIORATED PHOTOLUMINESCENT STRIP ALONG PAX CABIN. REPLACED THE PHOTOLUMINESCENT STRIP IAW AMM 33-51-15-400-802, STEP 1.E.(2), & (5).SDR SWAA2026100572681Stub Frame · crackedCRACKED R1 DOOR STUB FRAME, 0.1" ABOVE SEAL DEPRESSOR, LENGTH: 1.5". REMOVED AND REPLACED R1 DOOR UPPER STUB FRAME IAW SRM 51-40-02 AND DWG 141A8370, REV D, STEP 2, ITEM 1.SDR SWAA2026092152602Collar · missingG1 GALLEY ASSIST HANDLE MISSING 1 COLLAR. REPLACED THE G1 GALLEY ASSIST HANDLE COLLAR IAW AMM 52-41-31-400-802.SDR SWAA2026091834486Attach Angle · crackedBS 663 VAPOR BARRIER UPPER ATTACH ANGLE WAS CRACKED, RBL 9, WL 165 (SEGMENT 3).SDR SWAA2026091886713Attach Angle · crackedRIGHT BS 663 VAPOR BARRIER UPPER ATTACH ANGLE FOUND CRACKED, RBL 34 ,WL 165 (SEGMENT 1).SDR SWAA2026091838814Slide · exposedFWD ENTRY ESCAPE SLIDE HANGING OUT. TUCKED IN ESCAPE SLIDE EXCESS MATERIAL IAW AMM 25-66-00. DID NOT REMOVE OR OPEN SLIDE.SDR SWAA2026091898603Fitting · looseL-2 DOOR AFT GIRT BAR FITTING IS LOOSE L-2 DOOR AFT GIRT BAR FITTING IS LOOSE. TIGHTENED LOOSE L-2 GIRT BAR FITTING IAW AMM 25-66-02-400-801. OPS CHECK GOOD.SDR SWAA2026091846474Attach Angle · crackedLEFT BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT APPROXIMATELY LBL 9 WL 165 (SEGMENT 3).SDR SWAA2026102182814Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BTWN BL 0 - RBL 24.75, WL 208.1. REPLACED CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 146A0060, SHT 36, REV A.SDR SWAA2026102142829Skin · debondedDEBONDED LT WING, OTBD AFT FLAP. PERFORMED INTERIM REPAIR ON THE LT WING, OTBD AFT FLAP IAW SRM 57-53-01-2R-16, REPAIR 16. REQUIRED TAP-TEST INSPECTIONS EVERY 6875 FLIGHT CYCLES OR 30 MONTHS WHICHEVER COMES FIRST.SDR SWAA2026102131160Skin · debondedDEBONDED RT WING OTBD AFT FLAP. PERFORMED INTERIM REPAIR ON RT WING OTBD AFT FLAP IAW SRM 57-53-01-2R-16, REPAIR 16. REQUIRED TAP-TEST INSPECTIONS EVERY 6875 FLIGHT CYCLES OR 30 MONTHS WHICHEVER COMES FIRST.SDR SWAA2026102131381Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500I - 520, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A5400, SHT 201, REV -.SDR SWAA2026102189368Access Panel · damagedELONGATED HOLES ON THE LT WING ACCESS PANEL 561BB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026102192801Access Panel · damagedELONGATED HOLES ON THE LT WING ACCESS PANEL 561CB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026101979648Angle · crackedCRACKED ANGLE ON LINING ACCESS PANEL 844AW ON THE AFT SERVICE DOOR. REPLACED THE ANGLE IAW SOPM-20-50-12, REV 58, & DWG-411A2114-43B, SHEET 26, REV C.SDR SWAA2026101699512Support · corrodedCORRODED SUPPORT ZEE, BTWN BS 727 - 847, WL 156, LBL 21 AFT CARGO BAY. REPAIRED THE SUPPORT ZEE IAW SRM 51-40-02, SRM 53-00-53-2R-6, DWG 146A7500, SHEET 233, REV -, & DWG 142A7502, SHEET 31, REV -.SDR SWAA2026101625780Support · corrodedCORROSION ON SUPPORT ZEE, BS 727 - 767, WL 156, RBL 21 IN THE AFT CARGO BAY. REPAIRED THE SUPPORT ZEE IAW SRM 53-00-53-2R-5, REPAIR 5, TABLE 201.SDR SWAA2026101636643Shield · corrodedCORROSION ON SHIELD PLATE, BTWN BS 847 - 867, WL 156, RBL 20. REPLACED THE SHIELD PLATE IAW SRM 51-40-02-0G-0, & DRAWING 146A0081-10E.SDR SWAA2026101495249Shield · corrodedCORRODED SHIELD PLATE, BS 767 - 787, RBL 21, WL 156. REPLACED THE SHIELD PLATE AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 146A0081, SHEET 49, REV A.SDR SWAA2026101453554Strap · corrodedCORRODED STRAP, BS 767 - 787, WL 156, RBL 21 & LBL 21. REPLACED THE STRAP IAW SRM 51-10-02-0G-0, ITEM 9.SDR SWAA2026100561009Plate · crackedCRACKED PLATE ON THE OTBD AFT FLAP TRACK SUPPORT. THE REPLACEMENT OF PLATE ON O/B AFT FLAP TRACK SUPPORT AREA 3 AT LT AFT FLAP IS NOT NECCESARY DUE TO WAS OBTAINED A SERVICIABLE O/B AFT FLAP ON FAULT TTG8Q01E9Y2E.SDR SWAA2026091706067Inlet · crackedOTS-#2 ENGINE INLET COWL CRACKED_ VERIFIED CRACK AND MARKED ENDS. CRACK MEASURES 3.0IN LONG. REF NDT PART 6 51-00-00. PROCEDURE 23. REMOVED AND REPLACED #2 ENG INLET COWL PER 7111-E-17634-NG (AD - REP - INLET COWL AND CRUSHABLE WEAR SPACERS) TTG8Q01EKLT2 OPS SDR SWAA2026102100595Tie Clip · crackedCRACK TIE CLIP, BS 500H, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE TIE CLIP & FASTENERS IAW SRM 51-40-02, & DWG 143A1233, SHT 29, REV -.SDR SWAA2026102142780Stub Frame · crackedCRACK INDICATION ON STUB FRAME BTWN BS 294.5 & 296.5, STRINGER 8R & 9R ON THE FWD GALLEY DOOR AREA . REPLACED THE STUB FRAME IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, DWG 141A8370, SHT 10, REV -, & DWG 141A8380, SHT 21, REV -.SDR SWAA2026102193815Web · corrodedCORROSION SHIELD WEB LOCATED BTWN BS 767 - 794.3, WL 156, RBL 22 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB IAW SRM 51-10-02, ITEM 9, & DWG 146A0081, REV A,SDR SWAA2026102141257Cover · crackedCRACKED COVER ON AFT SERVICE DOOR NEXT TO THE INTERNAL HANDLE. REPLACED THE COVER IAW AMM 52-41-31-401. THE INSTALLATION ACCOMPLISH ON TTG8Q01DTL16.SDR SWAA2026102191104Crossbeam · crackedCRACKED CROSSBEAM, BS 540, LBL 24.75 - 44.5. REPLACED THE CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A5240, SHT 12, REV-.SDR SWAA2026102153730Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500H, STRINGER 26R. REPLACED THE SUPPORT ANGLE, & FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHT 152, REV -.SDR SWAA2026102180435Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BL 0 - LBL 24.75. REPLACED THE CROSSBEAM IAW SRM 51-10-02, ITEM 9, & DWG 143A0060, REV-. SSDR SWAA2026101493719Support Bracket · crackedCRACKED SUPPORT BRACKET, BS 540, RBL 6 IN THE AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET IAW SRM 51-10-02.SDR SWAA2026101492487Support Bracket · crackedCRACKED SUPPORT BRACKET, BS 540, LBL 6. REPLACED SUPPORT BRACKET IAW SRM 51-10-02.SDR SWAA2026100550157Blade · crackedCRACKED ACCESS PANEL 333AB BLADE ASSY AT LT HORIZONTAL STAB. REPLACED THE BLADE ASSY ON ACCESS PANEL 333AB IAW SRM 51-40-02, & SRM 51-10-02, ITEM 9.SDR SWAA2026100539644Fastener · pulledNR 1 ENGINE INLET COWL HAS MULTIPLE FASTENERS PULLING THROUGH BETWEEN 11 O'CLOCK AND 1 O'CLOCK POSITIONS. REMOVED AND REPLACED THE NR 1 ENGINE INLET COWL IAW SOPM 20-50-01.SDR SWAA2026100524039Vapor Barrier · crackedCRACK FOUND AT THE VAPOR BARRIER, BS 663, WL 165, LBL 25. REPAIRED IAW AMM 51-21-99-300-802.
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