Boeing 737-76N
Service difficulty reports · 4,807
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 = '73776N' 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 = '73776N' 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 SWAA2023120715977Flap · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE OB SIDE AT LT WING 2023-681914<[01] TOOL USED; CALIPER PN: 500-197-30; SN: 15120589; DUE DATE: 13-FEB-24.;[02] TOOL USED; POSITECTOR PN: DF 631235; SN: AE-406428; DUE DATE: 18- AUG-24; HOT BONDSDR SWAA2023101911495Cover · brokenFWD LOWER EXIT SIGN COVER BROKEN.<[01] SECURED COVER AS REQ PER SIP.SDR SWAA2023101109745Girt Bar · exposedAFT LEFT SERVICE DOOR SLIDE EXPOSED<[01] ADJUSTED AFT SERVICE DOOR SLIDE GIRT BAR AND FLAP; REF AMM 25-66-01. A/C OK FOR SERVICESDR SWAA2023092704419Panel · brokenKEEL BEAM PANEL 192 E; FWD RIGHT ATTACHMENT BRACKET BROKEN<[01] REMOVED AND REPLACED KEEL BEAM PANEL 192E; FWD R/H ATTACHMENT BRACKET REF SRM 51-40-02;[02] C/WSDR SWAA2023092603196Cowling · cracked#1 ENGINE INBD FAN COWL HAS A 3 INCH CRACK 2.5 INCHES FWD OF TRAILING EDGE AND 4 INCHES UP FROM LOWER EDGE<[01] REMOVED AND REPLACED #1 ENGINE INBD FAN COWL. REF:AMM 71-11-02SDR SWAA2023092503200Handle · looseFWD ENTRY FWD BULKHEAD ASSIST HANDLE IS LOOSE<[01] RESECURED FWD ENTRY FWD BULKHEAD ASSIST HANDLE IN REF AMM 20-50-11SDR SWAA2023092503201Girt Bar · out of adjustFWD ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] READJUSTED FWD ENTRY DOOR SLIDE GIRT BAR IN REF AMM 25-66-01SDR SWAA2023092503202Handle · looseFWD SERVICE DOOR LINER ASSIST HANDLE IS LOOSE<[01] RESECURED FWD SERVICE DOOR LINER ASSIST HANDLE IN REF AMM 20-50-11SDR SWAA2023092502397Strut · delaminatedLEFT ENGINE - AFT ACOUSTICAL PANEL INB OF THE 6 OCLOCK STRUT DELAMINATED.<[01] R/R LEFT ENG AFT ACOUSTICAL PANEL INB OF THE 6 O?CLOCK STRUT PER AMM 72-23-02SDR SWAA2023091399935Slide · out of positionR1 DOOR SLIDE FELL OUT OF PACK<[01] REF. LOG PAGE 2425862 .R1 DOOR SLIDE FELL OUT OF PACK.<BR>REINSTALLED SF(R1) SLIDE PER MT 725-61-06SDR SWAA2023092798845Flange · damagedOUT OF ROUND HOLE WITH ADJACENT GOUGE TO FLANGE SURFACE; LH HORIZONTAL STAB RIB AT STAB STA 129.50; LOWER OB FLANGE 23.5' FROM FWD EDGE.<[01] REPAIRED DAMAGE IAW EA 23-155-02777SDR SWAA2023090596835Slide · detachedSLIDE IN FWD SERVICED DOOR FELL OUT OF COMPARTMENT<[01] REINSTALLED SLIDE PER MT 725-61-06SDR SWAA2023092696053Web · corrodedFCB SUB THRESHHOLD WEB IS CORRODED FROM BS 480+1 - 460+11; RBL 32; WL 32 CORRECT WL 157<[01] UPDATED STEP 5;[02] UPDATED STEP 6;[03] UPDATED STEP 6 AND 7;[04] SRM 53-30-15-1A-1 FOUND TO BE APPLICABLE; BLENDED MULTIPLE CORROSION AT FBC SUB THRESHOLD WEB BS 480+SDR SWAA2023092695807Scuff Plate · crackedAFT CARGO BAY; AFT CORNER SCUFF PLATE CRACKED<[01] UPDATED STEP 5.;[02] COMPLETED STEP 5.;[03] COMPLETED STEP 6.;[04] REMOVED PROTECTIVE COATINGS FROM SCUFF PLATE PRIOR TO WELDING PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2) AND SOPM 20-30-02. WELDED CRACKED RADIUSDR SWAA2023092695808Retainer · crackedL/W T/E PANEL 551GB AFT SEAL RETAINER IS CRACKED<[01] REPLACED L/W T/E PANEL 551GB AFT SEAL RETAINER PER AMM 20-50-11.;[02] CORRECTION: REPLACED L/W T/E PANEL 551GB AFT SEAL RETAINER PER AMM 20-50-11.;[03] CORRECTION: REPLACED L/W T/E PANEL 551GB AFT SEAL RETASDR SWAA2023092695562Stringer · crackedCRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-22R WL172. MARKED<[01] UPDATED STEPS 2-3;[02] UPDATED STEPS 6-8;[03] PARTIAL STEPS 6-7-8;[04] PARTIAL UPDATE STEPS 6 AND 7;[05] COMPLETED STEP 7 AND 8.;[06] STEP 3 COMPLETE;[07] REMOVED DAMAGED STR SECTION SDR SWAA2023092695564Frame · corrodedCORROSION ON FRAME CHORD AT AREA AFT OF FWD CARGO BAY BS500D RBL8 WL151.<[01] VERIFIED CORROSION REMOVED; THE REQUESTED NDT INSPECTIONS IS FOR ENGINEERING SUPPORT.;[02] COMPLETED STEP 6.;[03] REJECTED: SEE TTG8Q00NJT8E AND TTG8Q00NJTH5;[04] ACCOMPLISHED EA 23-SDR SWAA2023092695362Rib · crackedLH HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 111.10; 3RD VERTICAL STIFFENER IS CRACKED.<[01] UPDATED STEP 2;[02] REPAIRED L/H HORIZONTAL STABILIZER INSPAR RIB; (STAB. STA. 111.10) 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4.;[03] VERIFIED STEPS SDR SWAA2023092695363Rib · crackedLEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED.<[01] SRM 55-10-09-2R-4 STEP 4. E. INSPECTION FOUND DAMAGE ADJACENT TO REPAIR AREA; GENERATED TTG8Q00NBZEC; SEE SUB-STEP 9.;[02] REPAIR OF L/H HORIZONTASDR SWAA2023092695561Skin · crackedLH HORIZONTAL STABILIZER LOWER SKIN - .7' CRACK FOUND 27' FROM FWD EDGE AT RIB STA 184.70<[01] REPAIRED PER EA 23-155-02717 WITH REPETITIVE INSPECTION PROGRAM DEFINED IN EA 23-155-02717-INSP.';[02] TASK CARD COMPLETE.SDR SWAA2023092695565Skin · crackedLH HORIZONTAL STABILIZER LOWER SKIN - .7' CRACK FOUND 18' FROM FWD EDGE AT RIB STA 193.90<[01] REFER TO FAULT TTG8Q00N5DVD WHERE EA 23-155-02717 WAS ADDED AS A SUBTASK;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023092695356Panel · crackedWING CENTER SECTION HAS A CRACKED BREAK PANEL AT BS 540; LBL 1; WL 207<[01] UPDATED STEPS 1;2;[02] UPDATED STEP 3;[03] UPDATED STEP 3 ADDED REFERENCE;[04] CERTIFIED CHANGE TO STEP 3;[05] UDATED STEP 4 INSTALLED BREAK PANEL;[06] UPDATED MEASUREMENT TABLE;[07] USDR SWAA2023092695361Attach Angle · crackedWING CENTER SECTION HAS A CRACKED CABLE INTERCOSTAL ATTACH ANGLE AT BS 685+7; RBL 24; WL 203<[01] UPDATED STEPS 1-4;[02] INSTALLED NEW ANGLE AT BS 685+7; RBL 24; WL 203 PER SRM 51-40-02-0G-0 AND DWG 273A9110;[03] VERIFIED CORRECTIVE ACTION #2.<BR>VERIFIED MEASSDR SWAA2023092695357Attach Angle · crackedWING CENTER SECTION HAS A CRACKED CABLE INTERCOSTAL ATTACH ANGLE AT BS 685+7; LBL 24; WL 203<[01] UPDATED STEPS 1-4;[02] INSTALLED NEW ANGLE AT BS 685+7; LBL 24; WL 203 PER SRM 51-40-02-0G-0 AND DWG 273A9110;[03] VERIFIED CORRECTIVE ACTION #2.<BR>VERIFIED MEASSDR SWAA2023083095224Battery Pack · inoperativeSEVERAL EMERGENCY LIGHTS INOP IN FWD CABIN AREA<[01] REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK AT POSITION M1675 PER AMM 33-51-06SDR SWAA2023092695144Frame · crackedFED CUTOUT SURROUND STRUCTURE - CRACK ON UPPER CHORD FRAME ASSY BS 312 STR-5L<[01] REQUEST NDI TO VERIFY CRACK AND IF CRACKED MARK ENDS OF CRACK BS 312 STR 5L UPPER RADIUS OF FRAME;[02] ACCOMPLISHED HFEC SURFACE SCAN IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDSDR SWAA2023092694709Pressure Deck · crackedHORIZONTAL PRESSURE DECK CRACKED BS664.5; WL 202; LBL52 APPROX 1 INCH IN LENGTH. MARKED WITH BLACK SHARPIE.<[01] REPAIRED HORIZONTAL BEADED PRESSURE DECK WEB BETWEEN STA 663.75 TO 675 LBL 30 TO LBL 60 PER SRM 53-40-51-2R-2. FIG. 203.;[02] VERIFIED CORRECTIVE ASDR SWAA2023092894696Web · crackedRIGHT WING T/E ORSS 280 TRANSVERSE WEB O/B L-CLIP ATTACHED TO DEFLECTION CONTROL RIB IS CRACKED<[01] PARTIAL UPDATE STEPS 1 AND 2;[02] COMPLETED STEPS 1 AND 2;[03] TASK COMPLETE.SDR SWAA2023092694697Retainer · crackedRIGHT WING T/E VERTICAL SEAL RETAINER IS CRACKED AT ORSS 268 JUST ABOVE AFT PYLON FAIRING TIP<[01] REMOVED AND REPLACED RIGHT WING T/E VERTICAL SEAL RETAINER IAW SRM 51-40-02-0G-0;[02] JOB COMPLETE.;[03] VERIFIED MEASUREMENTS.SDR SWAA2023082392824Battery Pack · inoperativeLEFT OVERWING INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP<[01] REPLACED BATTERY PACK PER AMM 33-51-06. OPS CHECK GOODSDR SWAA2023082309217Charger · inoperativeTHREE EMERGENCY AISLE LIGHTS F/O SIDE ROW 13-19 INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND BATTERY CHARGER M1672 IAW AMM 33-51-06 REF LOG PAGE 2378348SDR SWAA2023082391753Battery · inoperativeTHREE EMERGENCY AISLE LIGHTS F/O SIDE ROW 13-19 INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND BATTERY CHARGER M1672 PER AMM 33-51-06 REF LOG PAGE 2378348.SDR SWAA2023081688964Valve · overservicedDURING DESCENT AT APPROXIMATELY 27;000 FEET CREW NOTICE ABNORMAL SMELL THROUGHOUT COCKPIT AND CABIN. SMELL DESCRIBED AS WAXY OR OILY.<[01] COMPLIED WITH SMOKE AND FUMES CONDITIONAL INSPECTION PER MM O5-51-56. FOUND A HYD SYSTEM SERVICED T0 96% AND B SYSTEM AT SDR SWAA2023081588694Strip · loosePHOTOLUMINESCENT STRIPS FROM OVERWING EXIT ROWS HAVE BECOME LOOSE AND DETACHED<[01] REATTACHED PHOTOLUMINESCENT STRIPS AT EMERGENCY EXIT ROWS PER SIPSDR SWAA2023081487361Battery Pack · inoperativeEMERGENCY LIGHT AT ROW 6 DEF FOUND INOP<[01] R&R FWD EMERGENCY BATTERY PACK PER AMM 33-51-06. EMERGENCY LIGHT AT ROW 6 DEF OPS CHECK GOOD.SDR SWAA2023081487088Girt Bar · looseF/A REPORTS L1 GIRT BAR LOOSE<[01] RESECURED GIRT BAR BRACKET PER SIPSDR SWAA2023080886946Oil Cooler · leakingAPU AUTO SHUTDOWN EN ROUTE<[01] FOUND OIL LEAK AT APU OIL COOLER; R&R APU OIL COOLER IAW AMM 49-91-41; OPS CHECK GOODSDR SWAA2023073183567Light · inoperativeFWD GALLEY EMERGENCY LIGHT INOP<[01] R&R FWD GALLEY EMERGENCY LIGHT PER AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2023072882753Rod · brokenL/H WING TRAILING EDGE; AFT OF PYLON; SHELF SUPPORT ROD BROKEN.<[01] REMOVED AND REPLACED ROD ASSY PER SOPM 20-50-01. CLEARANCE CHECK GOODSDR SWAA2023071176849Windshield · crackedR1 WINDSHIELD OUTTER PANE CRACKED<[01] RAR FO WINDSHIELD IAW AMM 56-11-11. ACCOMPLISHED UP TO STEP H(9) OPS CHECK OF PRESSURIZATION. PENDING SEALANT APPLICATION. PENDING STEP H(10) AND DOWN.;[02] FINISHED INSTALLING R1 WINDOW AND OPS CHECKS GOOD IAW AMM 56-11-SDR SWAA2023062972699Lens · out of positionEXIT LIGHT LENS HANGING OUT OF BIN BULLNOSE OVER SEAT 18 FED<[01] FOUND AREA LIGHT ASSY AT SEAT ROW 18DEF LOOSE ON BACK OF BULLNOSE PANEL. APPLIED ADHESIVE REF BOEING DWG 412A1605; SHEET 6; FLAGNOTES 6 AND 7; AND REINSTALLED LIGHT LENS PER AMM 33-51-03-960-801SDR SWAA2023062972698Sign · inoperativeFWD LAV EXIT LIGHT HAS 1 INOP SEGMENT FWD LAV EXIT LIGHT HAS 1 INOP SEGMENT.<[01] RELAMPED AND TESTED FORWARD LAVATORY EMERGENCY EXIT SIGN PER AMM 33-51-01-960-801; NO FURTHER DEFECTS NOTED.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2023062872173Lens · brokenEMERGENCE EXIT LIGHTS IDENTIFIERS LENS AT FWD LAV A AND LEFT HAND FWD OWE DOOR BROKEN.<[01] REMOVED AND REPLACED LH FWD OWE DOOR EMERGENCY LIGHT IDENTIFIER LENS AND FWD LAV A EMERGENCY EXIT LIGHT ASSY PER AMM 33-51-14-960-801 AND AMM 33-51-14-960-802. OPS CHECSDR SWAA2023062872652Light · brokenEMERGENCE EXIT LIGHTS IDENTIFIERS LENS AT FWD LAV A AND LEFT HAND FWD OWE DOOR BROKEN.<[01] REMOVED AND REPLACED LH FWD OWE DOOR EMERGENCY LIGHT IDENTIFIER LENS AND FWD LAV A EMERGENCY EXIT LIGHT ASSY PER AMM 33-51-14-960-801 AND AMM 33-51-14-960-802. OPS CHECSDR SWAA2023062871041Lamp · missingEMERGENCY LITS MISSING BULBS AT L1/L2 LINING DOOR SIGN; L/H OVERWING EXIT SIGN<[01] RELAMPED EMERGENCY LIGTHS BULBS AT L1/L2 LINING DOORS SIGN AND LH OVERWING EXIT AND PERFORMED A GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.;[02] CERTIFIED ACTION 1.;[03] VSDR SWAA2023062061057Slide · detachedFWD SERVICE DOOR EMERGENCY IS DETACHED<[01] REINSTALLED FORWARD SERVICE DOOR SLIDE PER MT 725-61-06.SDR SWAA2023061960454Battery Pack · inoperativeFWD RH EMER LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK IAW 33-51-06. OPS CHECKED GOOD AT THIS TIME.SDR SWAA2023070559605Fastener · crackedCRACKED AFT SEAT TRACK FASTENER AT PASSENGER CABIN BS727B LB25 WL208.<[01] REMOVED AND REPLACED CRACKED FASTENERS AT B/S 727B LBL25 IAW SRM 51-40-02 AS SHOWN IN IPC 53-41-11 ITEM 11 AND DWG 146A5300 REV:A;[02] CERTIFIED CORRECTIVE ACTION.;[03] VERIFIED CORRECTSDR SWAA2023061659896Slide · out of toleranceFWD SERVICE DOOR SLIDE GAUGE NEEDLE IN RED BAND.<[01] REMOVED SLIDE PER MT 725-61-06.;[02] INSTALLED FWD SERVICE SLIDE PER MT 725-61-06. CKS OK.SDR SWAA2023070558758Intercostal · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 500D-520; BLO; WL 208<[01] REMOVED & REPLACED INTERCOSTAL UPPER ATTACH ANGLE BS 500D-520 BL 0 WL 208.1 PER SRM 51-40-02-0G-0 ; SRM 51-40-05-0G-0 AND BOEING DWG# 143A5400;[02] VERIFIED CORRECTION ACTION ITEM 1.;[03] VE
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