Boeing 737-8
Service difficulty reports · 6,799
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 = '7378' 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 = '7378' 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 CALA2024061801844Wire · damagedREF LP 8301672. WHEN REPLACING MMR1 FOUND PUSHED BACK PIN IN MMR1 BENCHPLUG CONN D10719B POS B8. REF SSM 34-58-11 PIN IS ASSOCIATED WITH ''IR OUTPUT BUS 4'' SIGNAL.. PLUG D10719B POSITION B8 ON D10719B IS NOT P/N BACC47EF1 AND WILL REQUIRE REPLACMENT AND RE-TESDR SCNA20240806291Channel · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT FLOOR STRUCTURE LBL 25.2. ZEE CHANNEL SIDEPLATE WITH CORROSION AT SEVERAL PLACES. REPLACED FLOOR ZEE CHANNEL LH SIDE PLATE PN BAC 1496-377 FROM STA727+4" TO STA 847" LBL 21 WITH TWO REPAIR SPLICES INSTALLED FORM STA 727+6.SDR SWAA2024061801443Battery Pack · no testFLIGHTDECK EMERGENCY FLASHLIGHT DOES NOT TEST. R & R FLIGHT DECK EMERGENCY FLASHLIGHT BATTERY PER AMM 25-64-00 OPS CHECK GOOD.SDR CALA2024061701819Lavatory · fullDIVERT TO KONT DUE TO LAVS INDICATING FULL UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR. LAV INDICATION SHOWING FULL. SERVICED LAVS AND INDICATION FOLLOWED. INDICATION SHOWING EMPTY NOW. ACFT GOOD TO CONTINUE.SDR SWAA2024061401719Contact · dirtyFORWARD GALLEY OUTBOARD UNDER JUMP SEAT FLASHLIGHT WILL NOT PRESS TO TEST<[01] CLEANED CONTACTS OPS CHECKS GOOD PER AMM 25-64-00-200-801-MAX-01 (FLASHLIGHT CHECK (WITH FLASHING OR PUSH TO TEST - LED INDICATOR) - PERMANENT)]SDR CALA2024061701822Landing Gear · shearedLEFT MAIN LANDING SHEARED OFF DUE TO AIRCRAFT VEERED OF THE HARD SURFACE. ALL WORK PERFORMED BY BOEING.SDR CALA2024071001988None · noneON LIGHTNING STRIKE INSPECTION, FOUND DAMAGE ON L/H WING UPPER SURFACES AROUND STATIONS 180 AND 204, CLEANED SURFACE DIRT RESIDUE FROM THE LOCATION IAW AMM 51-21-02.SDR SWAA2024061300819Battery Pack · inoperativeRH AFT EMER LIGHTS INOP.<[01] REMOVED AND REPLACED RH AFT EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2024061300170Flashlight · unknownAFT LEFT FLASHLIGHT INOP<[01] OPS CHECKED PER AMM 25-64-00. OPS CHECK GOOD. CLEARS MELSDR SWAA2024061300820Flashlight Assy · failedAFT EMERGENCY FLASHLIGHT; CAPT SIDE; WILL NOT TEST<[01] OK TO CONTINUE PER MEL 25-64-02A SP1B;[02] REMOVED AND REPLACED BRACKET ASSY FOR AFT EMERGENCY FLASHLIGHT (CAPTAINS SIDE) PER AMM 25-64-00. OPS CHECK GOOD.SDR SWAA2024061199549Battery · failedFOUND FLIGHT DECK EMERGENCY FLASHLIGHT OUT OF BATTERY. R & R FLIGHT DECK EMERGENCY FLASHLIGHT PER AMM 25-64-00SDR SWAA2024061099640Flashlight · unsecureCAPTAINS AFT I/B AND FO'S AFT I/B FLASHLIGHTS DO NOT TEST PROPERLY. ADJUSTED FLASHLIGHT AND TESTED GOOD PER M/M 25-64-00.SDR SWAA2024061099193Unknown · unknownLOUD THUD AT 120 KNOTS ON T/O ROLL FOLLOWED BY HEAVY VIBRATIONS UNTIL GEAR RETRACTION. GEAR EXTENSION; LANDING AND ROLLOUT ALL NORMAL.<[01] INSP NLG PER AMM 32-21-00. NO DEFECTS. JACKED NLG PER AMM 07-10-03 AND CHECKED WHEELS FOR COND PER AMM 32-45-00.. NO DEFSDR SWAA2024060798832Cover · delaminated#1 ENGINE I/B PYLON HINGE BEAM FAIRING AERODYNAMIC SEAL COVER SECTION FLAPPING IN THE BREEZE #1 ENGINE HINGE BEAM FAIRING BLADE SEAL SAIL CLOTH COVER DELAMINATED/FRAYED TSR# 2024003859<[01] ACCOMPLISHED REPAIR PER EA 24-154-01540SDR CALA2024061701805Coffeemaker · damagedCOFFEE MAKER 105 IN FWD GALLEY FULLY DETACHED AND FELL ON FLOOR DURING TAKEOFF. PLACING INOP COFFEE MAKER ON DEFERRAL IAW NEF 2500BD REF ECRA 2530-04524 LOG PAGE 8193684 FOR BEING REMOVED. COFFEEMAKER REMOVED. COFFEE REMOVED COFFEE MAKER M & E . TWEAKED THE SDR CALA2024061001759Coffeemaker · noneFWD GALLEY (G1) COFFEE MAKER #105 REMOVED, PLACING REMOVED COFFEEMAKER 105 FWD GALLEY ON DIP IAW ECRA 2530-04524 PART 1. ACCOMPLISHED WATER & C/B SECURED. PERFORM PERM REPAIR PER PART 3 WITHIN 10 DAYS CARRIED DIRECTLY BY TOMC TOMC-APPROVAL FROM SC1ELBYC.SDR CALA2024061001751Wire · shortedLE FLAP TRANSIT LIGHT AT 15000 MAINTENANCE MESSAGE: 27-81213 LE SLAT 7 INBOARD SENSOR SIGNAL [HISTORY]. NO CURRENT FAULT; BUT BITE CHECK INDICATES MOST ORIGINAL: FLIGHT CREW INDICATES THAT SLAT #7 WOULD NOT RETRACT SEE LOG PAGE HISTORY #8134788. FIM TASK WORKSDR SWAA2024062597988Attach Bracket · cracked(A204 DOT 19) AFT CARGO. STA 867; LBL 12; LAV BULKHEAD SUPPORT ATTACH BRACKET IS CRACKED AT CARGO FLOOR; FLOOR LINE<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-D00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]<BR>TAG: A2425SDR SWAA2024062597987Shield · corroded(A204 DOT 18) AFT CARGO STA 847+13; RBL 21; WL 162; SPLASH SHIELD UPPER SURFACE HAS CORROSION AT NUTPLATE HOLE.<[01] REMOVED CORROSION ACCOMPLISHED 10X MAG ALL CORROSION WAS REMOVED IAW SRM 51-10-02;VERIFIED ORIG .050'; LOSS .010'; REMAINING .040' FOUND TO BE SDR SWAA2024062597986Shield · corroded(A204 DOT 17) AFT CARGO STA 767 TO 787; RBL 21; WL 160; FLOOR SPLASH SHIELD HAS CORROSION ON UPPER AND LOWER SURFACE<[01] 01 - REMOVED AND REPLACED PER [SRM 53-00-53-1A-2-D00297 (PERMANENT (NON-DENT DAMAGE TYPES))];[02] AUDIT C/WSDR SWAA2024062597985Angle · corroded(A204 DOT 16) AFT CARGO STA 747 TO 787; LBL 21; WL 160; Z-ANGLE HAS CORROSION ON UPPER SURFACE.<[01] REMOVED DAMAGE FROM LH ZEE ANGLE STA 727-847 AND REPAIRED ON FAULT TTG8Q00TQT5Y PER SRM 53-00-53-2R-5;[02] VERIFIED ITEM 1<BR>C/WSDR SWAA2024062597984Angle · corroded(A204 DOT 15) AFT CARGO; STA 747 TO 767; RBL 21; WL 160; Z-ANGLE BAFFLE IS CORRODED ON LOWER SURFACE AT NUTPLATE HOLES<[01] REMOVED BAFFLE AND BLENDED CORROSION FOUND A LOSS OF .007' REMAINING WAS .025' FOUND TO BE OUT OF LIMITS RECEIVED NEW BAFFLE PN 146A7500SDR SWAA2024062597982Angle · corroded(A204 DOT 13) AFT CARGO STA 727I+4 TO 727J+20; LBL 21; WL 160; Z-ANGLE HAS CORROSION ON UPPER SURFACE.<[01] REMOVED DAMAGE FROM LH ZEE ANGLE STA 727-847 AND REPAIRED ON FAULT TTG8Q00TQT5Y PER SRM 53-00-53-2R-5;[02] VERIFIED C/WSDR SWAA2024062597981Angle · corroded(A204 DOT 12) AFT CARGO STA 727I+2 TO 727J+18; RBL 21; WL 160; Z-ANGLE HAS CORROSION ON UPPER SURFACE<[01] TTG8Q00TQT9A;[02] BLENDED CORROSION ON AFT CARGO STA 727I+2 TO 727J+18; RBL 21; WL 160; Z-ANGLE VERIFIED ORG 'T' .040 REMAINING 'T' .034 LOSS OF .006 FOUSDR SWAA2024062597973Angle · corroded(A204 DOT 11) AFT CARGO STA 727G TO 727 I; LBL 21; WL 160; Z-ANGLE HAS CORROSION ON UPPER SURFACE.<[01] REMOVED DAMAGE FROM LH ZEE ANGLE STA 727-847 AND REPAIRED ON FAULT TTG8Q00TQT5Y PER SRM 53-00-53-2R-5;[02] VERIFIED ITEM 1<BR>C/WSDR SWAA2024062597972Angle · corroded(A204 DOT 10) AFT CARGO STA 727G+8 TO 727I; RBL 21; WL 160; Z-ANGLE HAS CORROSION ON UPPER SURFACE.<[01] BLENDED CORROSION ON AFT CARGO STA 727G+8 TO 727I; RBL 21; WL 160; Z-ANGLE. VERIFIED ORG 'T' .040 REMAINING 'T' .034 LOSS OF .006 FOUND TO BE OUT OF LIMITSSDR SWAA2024062597967Angle · corroded(A204 DOT 4) AFT CARGO STA 727E +18 TO 727F+20; LBL 21; WATER LINE 160; Z-ANGLE HAS CORROSION ON UPPER SURFACE<[01] REMOVED ; FABRICATED NEW Z ANGLE AND INSTALLED I.A.W. SRM 53-00-53-2R-5;[02] VERIFIED ORIG .040'; LOSS .008'; REMAINING .032' FOUND TO BE OUT OFSDR SWAA2024060698101Panel · crackedAFT CRAGO PIT (LEFT SIDE) FOUND CRACKS ON PANEL 141DW<[01] REMOVED AND REPLACED AFT CARGO PIT PANEL 141DW PER AMM 50-12-01.SDR SWAA2024062597813Skin · damagedDOT A24-1 RH WING L/E NUMBER 5 SLAT UPPER SKIN CREASED AT CENTER OF SLAT AT UPPER CHORD.<[01] REMOVED AND INSTALLED SERVICEABLE #5 SLAT ASSY PER AMM 27-81-21-401. ADJUSTMENTS AND OPS CHECKS GOOD.;[02] VERIFIED C/WSDR SWAA2024062497572Floor Panel · crackedFWD PIT PANEL 122XAC IS CRACKED. A177-007<[01] VERIFIED AND REPLACED FWD CARGO CEILING SHROUD 122XAC ON PARTS RACK IAW IPC 50-10-03-51.;[02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2024062497581Floor Panel · crackedFWD PIT PANEL 121XBC IS CRACKED. A177-009<[01] REMOVED DAMAGED AREAS; FABRICATED AND INSTALLED REPAIR PATCH AT FWD PIT PANEL 121XBC I.A.W AMM 50-10-01-300-804;[02] VERIFIED ITEM 1<BR>C/WSDR SWAA2024062497582Floor Panel · crackedFWD PIT PANEL 122XFC IS CRACKED. A177-016<[01] DAMAGE REMOVED FROM PNL 122XFC AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED FOR PNL 122XFC IAW AMM 50-10-01-300-804;[02] VERIFIED ITEM 1<BR>C/WSDR SWAA2024062497584Floor Panel · corrodedFWD PIT PANEL 120DF IS CORRODED. A177-017<[01] 01 - REMOVED AND REPLACED PER [AMM 50-10-04-401-MAX (CARGO COMPARTMENT FLOOR PANEL - REMOVAL/INSTALLATION - PERMANENT)];[02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2024062497585Panel · corrodedFWD PIT PANEL 120AF IS CORRODED. A177-019<[01] C/WSDR SWAA2024062497586Scuff Plate · crackedFWD CARGO DOOR SURROUND; FWD CORNER SCUFF PLATE IS CRACKED FWD CARGO DOOR SURROUND FWD CORNER SCUFF PLATE IS CRACKED<[01] FWD CARGO DOOR SURROUND; FWD CORNER SCUFF PLATE REPAIRED ON BACKSHOP W/O# 45805-1000-0001 IAW SRM 53-30-15-2R-1;[02] VERIFIED STEP 1<BR>AUSDR SWAA2024062497976Shield · corrodedA225-002 FWD CARGO RH AFT SHIELD BS500 + 10' TO 500A RBL 25' WL 156 HAS AREAS OF CORROSION<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-D00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]<BR>FWD CARGO RH AFT SHIELD BS500 + 10'SDR SWAA2024062497979Support Angle · corrodedA225-005 FWD CARGO AFT BLKD LOWER SUPPORT ANGLE BS 500I CORRODED FROM RLB 20' TO LBL 20' WL 156.<[01] REMOVED; REPAIRED; AND REINSTALLED FWD CARGO AFT BLKD LOWER SUPPORT ANGLE AT STA 500I IAW EA 24-153-01577;[02] COMPLETE<BR>AUDIT C/WSDR UIEA2024052300425Keelbeam · damagedLOWER FUSELAGE AREA UNDER LOWER WING-TO-BODY FAIRING BETWEEN STA 727 AND STA 727C, LEVEL OF STR27L KEEL BEAM, WITH CORROSION.(<P>REPLACED KEEL BEAM SECTION FROM STA 727 TO STA 727C STR 27L IAW B737-800 BCF SRM 51-10-02-0G-0 PARAG 9 AND BOEING DWG: 146A7810 SHESDR UIEA2024052300426Cargo Track · crackedLOWER FUSELAGE, FORWARD CARGO COMPARTMENT , FLOOR STRUCTURE AREA,STA 460, RBL 14", TIE DOWN TRACK WITH CRACK(<P>REPLACED TIE DOWN TRACK SECTION P/N BAC1520-1397-7050 FROM STA 400 TO STA 513 WITH THE INSTALLATION OF A SPLICED REPAIR FROM STA 509 TO STA 517 RBL SDR UIEA2024052400436Floor Support · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT, FLOOR STRUCTURE AREA, FROM STA 727+10" TO STA 793, LBL 3" FLOOR SUPPORT CHANNEL WITH CORROSION AT SEVERAL PLACES(<P>REPLACED FLOOR BEAM SUPPORT RAIL CHANNEL P/N: BAC1509-100146 FROM STA 727+10" TO STA 797.5" WITH TWO SPLICSDR UIEA2024052800464Skin · damagedEXTERNAL FUSELAGE STA 844 STR18R+5" SKIN PANEL WITH SCRATCH.(<P>PERFORMED BLEND OUT REPAIR AND FOUND STRUCTURALLY ACCEPTABLE TO BOEING IAW COOPESA EO N°: COO-EO-2024-20121-R00 DATED MAY/08/2024 AND BOEING MESSAGE COO-TLS-24-0107-0413 DATED MAY/08/24. DOCUMENTSDR UIEA2024052800465Angle · wornEMPENNAGE VERTICAL FIN TO BODY INTERFACE LEFT CLOSURE ANGLE WORN FROM STA 1088 TO STA 1138.(<P>REPLACED LEFT CLOSURE ANGLE P/N: 148A8310-3 ATTACHED WITH SOLID RIVETS AND HI-LOKS IAW B737-800 BCF SRM 51-10-02-0G-0 PARAG 9, 51-40-02-0G-0 PARAG 4B AND 51-40-02-0GSDR UIEA2024052900466Skin · damagedUPPER FUSELAGE RIGHT AUTOMATIC OVERWING EXIT DOOR OUTER SKIN WITH SCRATCH AT STA 635 ON LEVEL STR 14R-15R.(<P>PERFOMED BLEND OUT ON OVERWING EXIT DOOR OUTER SKIN DUE TO SCRATCH AND FOUND WITHIN FLIGHT OPERATION LIMITS AREA B IAW B737-800BCF SRM 52-20-01-1A-1 PSDR SWAA2024060697374Connector · damagedFOUND DAMAGED WIRE SEAT ROW 15ABC FWD BIN; 2 INCHES BEHIND CONNECTOR D14702<[01] STEP 2 COMPLETE. TERMINATED WIRES W3142-0576-16 AND W3142-0577-16 AT CONNECTOR D14702 IAW WDM 33-51-13 AND SWPM 20-60-02 AND PERFORMED GOOD TEST PER AMM 33-51-00-710-801.;[02] VERSDR SWAA2024060497778Handle · out of adjustFORWARD ENTRY DOOR ASSIST HANDLE NOT ON/CONNECTED PROPERLY<[01] RE-SECURED FWD ENTRY DOOR ASSIST HANDLE IAW AMM 52-11-31SDR SCNA20240604250Bottle · low pressureL1 DOOR SLIDE CYLINDER PRESSURE INDICATOR NEEDLE IS IN THE NO-GO BAND. REMOVED AND REPLACED L1 DOOR SLIDE ASSEMBLY IAW B737-800BCF AMM 25-66-01.SDR SWAA2024060397503Flashlight · no testAFT GALLEY EMERGENCY FLASHLIGHT INOP<[01] REMOVED AND REPLACED AFT GALLEY EMERGENCY FLASHLIGHT REF AMM 25-64-00SDR SCNA20240603248Bracket · looseR1 GIRT BAR BRACKET LOOSE. FOUND RIVET MISSING IN GIRT BAR RETAINER CLIP. INSTALLED NEW RIVET. REF. AMM 70-10-12 & AMM 25-66-00. OK FOR SERVICE.SDR SWAA2024060397073Light · inoperativeRH AFT EXTERIOR EMERGENCY EXIT WINDOW LIGHT OUT<[01] R/R RH AFT EXTERIOR EMERGENCY EXIT WINDOWS LIGHT PER AMM 33-51-04SDR SWAA2024060397075Battery Pack · inoperativeR1 DOOR INTERIOR/EXTERIOR EMERGENCY LIGHTS INOP.<[01] R/R FWD ENTRY DOOR BATTERY PACK ASSEMBLY PER AMM 33-51-06. OPS CHECK SAT.
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