N7704B
Service difficulty reports · 264
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N7704B' AND registry_match = 'registration' 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 n_number = 'N7704B' AND registry_match = 'registration' 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 SWAA2024062789402Attach Angle · crackedFWD CARGO INTERCOASTAL ATTACH ANGLE FWD OF BS 500C LBL 25 WL 152 CRACKED<[01] REMOVED AND REPLACED FWD CARGO INTERCOSTAL ATTACH ANGLE FWD OF BS 500C LBL 25 WL 152 IAW SRM 51-40-02 AND DWG 143A7505;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.SDR SWAA2024062789403Attach Angle · crackedFWD CARGO INTERCOASTAL ATTACH ANGLE FWD OF BS 500B LBL 25 WL 152 CRACKED<[01] REMOVED AND REPLACED ANGLE (CLIP) FWD OF BS 500B;LBL 25;WL 152.IAW DWG#143A7505.;[02] VERIFIED;[03] VERIFIEDSDR SWAA2024062789411Stringer · crackedAFT AREA OF FWD CARGO BS540 L/H STR 26 CRACKED<[01] ACCOMPLISHED REPAIR PER SRM 53-00-03-2R-1 REPAIR 1;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024062789178Door Frame · corrodedFWD CARGO DOOR CUTOUT SURROUND STRUCTURE UPPER WEB FOUND CORROSION AT STA: 460; BTWN STGR 17 AND 18 RH APPROX.<[01] REMOVED AND REPLACED FCD SURROUNDING STRUCTURE UPPER WEB IAW SRM 51-40-02 AND DWG # 143A8111;[02] VERIFIED STEP 2 COMPLETE.;[03] VERIFIED ALL STSDR SWAA2024062789405Channel · corrodedCORROSION FWD CARGO MOPSIL BS 460 +4 -BS 480+4 RBL28 WL 156 CORRECTION TO FAULT DESCRIPTION: CORROSION FWD CARGO SUBTHRESHOLD WEB BS 460+4 - BS 480+4 RBL28 WL156<[01] REPAIRED CORROSION BY REPLACEMENT OF FCB SUBTHRESHOLD WEB IAW SRM 51-40-02 AND DWG 143A8330; SDR SWAA2024062789406Sidewall Support · corrodedCORROSION FWD CARGO FLOOR TO SIDEWALL SUPPORT BS 460+7; BS 480+9-BS 500+10; BS 500A+6-BS 500A+18 LBL 25 WL 156<[01] REMOVED AND REPLACED FCB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02 AND DWG 143A7500 ID: 0045 REV: -;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BSDR SWAA2024062789407Sidewall Support · corrodedCORROSION FWD CARGO FLOOR TO SIDEWALL SUPPORT BS500A+2-BS500A+10; BS500B+6; BS500B+18; BS500C+2 RBL 25 WL 156<[01] REMOVED AND REPLACED R/H FLOOR TO SIDEWALL FROM BS 500A TO BS 500D IAW SRM 51-40-02 AND DWG 143A7500 ID:0045 REV: -;[02] JOB COMPLETE.SDR SWAA2024062789412Shield · corrodedCORROSION FWD CARGO AFT SHIELD BS480+18; BS500+10-500A RBL 25 WL 156<[01] REMOVED AND REPLACED FWD CARGO BAY AFT SHIELD PER SRM 51-40-02-0G-0 AND DWG#143A0080.;[02] REJECT - STEP 7; 2EA FASTENERS TTG8Q00TU9R5;[03] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPSSDR SWAA2024062689410Stringer · crackedAFT AREA OF FWD CARGO BS540 L/H STR 23 CRACKED WL 156<[01] REJECT: EA-24-153-01423-WIP1 STEP 2.<BR>FABRICATION PARTS DOES NOT MATCH THE 737-700 SRM 53-00-03 REPAIR 1;<BR>INCORRECT LOCATION OF DRAIN HOLE ON HAT-SECTION REPAIR.;[02] ACCOMPLISHED REPAIR PER SRM 5SDR SWAA2024062689399Attach Angle · crackedFWD CARGO INTERCOSTAL ATTACH ANGLE AFT OF BS 400 RBL 25 WL 152 CRACKED<[01] REMOVED AND REPLACED ON FCB INTERCOSTAL ATTACH ANGLE (CLIP) AFT OF BS400;RBL25;WL152 IAW SRM 51-40-02 AND DWG#143A7505. VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024070388880Seal · crackedRT. HORIZ STAB PANEL 343AT SLIDE SEAL (SHARK FIN) CRACKED.<[01] REMOVED AND REPLACED RT. HORIZ STAB PANEL 343AT SLIDE SEAL (SHARK FIN) IAW SRM 51-40-02 AND AIPC 55-10-52-01H;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024062888896Stiffener · deformedFLOOR SUPPORT STIFFENER SHIM WAS FOUND DEFORMED AT STA 540 BETWEEN RBL45 AND RBL63;WL208. (MARKED)<[01] REMOVED AND REPLACED FLOOR STIFFENER SUPPORT ANGLE IAW SRM 51-40-02 AND DWG 143A5240 ID:0021 REV: -;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASURESDR SWAA2024062788898Floor Support · crackedFLOOR STIFFENER SUPPORT ANGLE CRACKED AT STA685+8; RBL 24.5; WL203. (MARKED)<[01] REMOVED AND REPLACED FLOOR STIFFENER SUPPORT ANGLE AT STA 685+8; RBL 24.5; WL203 IAW SRM 51-40-02-0G-0 AND DWG 273A9110 REV A;[02] REMOVED AND REPLACED FLOOR STIFFENER SUPPORT ANSDR SWAA2024062788899Floor Support · crackedFLOOR STIFFENER SUPPORT ANGLE CRACKED AT STA540; LBL1; WL208. (MARKED)<[01] REMOVED AND REPLACED FLOOR STIFFENER SUPPORT ANGLE IAW SRM 51-40-02 AND DWG 143A5240 ID:0014 REV:;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024062688897Floor Panel · pulledFLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241CF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID:0130.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR SWAA2024062688137Floor Panel · pulledFLOOR PANEL 242BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024062688136Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024062688135Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024062688134Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241AF FLOOR PANEL HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.;[02] CORRECTION TO CORRECTIVE ACTION STEP 1: 'FABRICATION OF NEW 241AF FLOOR PANEL HAS BEEN ACCOMPLISHED IAW SRM 53SDR SWAA2024062688133Floor Panel · pulledFLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 232SF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1553922-1; INSERTS INSTALLED USING BMS5-107 LOT#AK3BA2380A/A THEN CURED UNDER HEAT LAMP MONITORED WITH THERMOMETER ASDR SWAA2024062688132Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024062687923Vapor Barrier · crackedL/H B.S. 663 VAPOR BARRIER IS CRACKED AT MID SPAN.<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024022053294Battery · inoperativeLH FWD EMERGENCY LIGHT BATTERY INOP<[01] R&R LH FWD EMERGENCY BATTERY IAW AMM 33-51-06SDR SWAA2023122033266Girt Bar · missingAFT ENTRY DOOR GIRT BAR HOLDER MISSING<[01] INSTALLED GIRT BAR STOP RING REF AMM 25-66-01 AC OK SERVICESDR SWAA2023101309429Seal · crackedLEFT HORIZONTAL FORWARD UPPER STABILIZER TO BODY SLIDING SEAL IS CRACKED.<[01] REMOVED AND REPLACED LH HORIZONTAL FORWARD UPPER STABILIZER TO BODY SLIDING SEAL PER AMM 53-31-31SDR SWAA2023081689183Slide · out of positionFWD SERVICE SLIDE DRAGS ON FLOOR WHEN OPENING DOOR.<[01] REMOVED SLIDE AND COVER. REPOSITIONED SLIDE IN COVER IAW AMM 25-66-01 AND REINSTALLED.SDR SWAA2022100452070None · out of positionROW 12 DEF FWD EMERGENCY LIGHT COVER FELL OFF / [01] REPLACED ROW 12 DEF FWD EMERGENCY LIGHT COVER PER AMM 33-51-01SDR SWAA2022091352676None · faultySMELLED FUMES & HAD SMOKE/HAZE IN CABIN / [01] T/SHOT PER FIM 21-00 TASK 806. PERFORMED CHECK OF RECIRC FAN; EQUIP COOLING FANS; TEMP SENSOR FANS ALL CK OK. HYDRAULIC SYSTEM QTY NORMAL WITH NO LEAKS. RAN BOTH ENGS AT IDLE WITH LEFT ENG BLEED/PACK OPERATING ANDSDR SWAA2022071227055Girt Bar · out of positionFWD ENTRY DOOR GIRT BAR TIGHT / [01] ADJUSTED FWD ENTRY DOOR EMERGENCY SLIDE PER AMM 25-66-01. OPS CHECK GOOD.SDR SWAA2022070120398Floor Panel · crackedCRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT 2022-266168 / [01] FABRICATED FLOOR ACCESS PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801.DWG 453A2610; SHEET 20; REV: E. USED MATERIAL: ALUMINUM SHEET 2024T3-071; PO: 2021 210316.;[02] CSDR SWAA2022070113816Clamp · looseLOOSE SLIDE COVER SERVICE DOOR GIRT BAR RETAINER CLIP AT FWD GALLEY AREA (2 EA) 2022-266153 / [01] REPLACED FASTENERS(2E/A) LOC. SLIDE COVER SERVICE DOOR GIRT BAR RETAINER CLIP AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02.;[02] REPLACED FASTENERS(2E/A) LOC. SLSDR SWAA2022070112894Lens · brokenBROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA 2022-266030 / [01] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-801;[02] CORRECTED STEP 1<BR>REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA I.A.W B737-SDR SWAA2022070112076Lens · brokenBROKEN EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA 2022-266099 / [01] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 PERFORMED OPERATIONAL TEST; IS OK;[02] REPLACED EMERGENCY EXIT LIGHT LENS LAVATSDR SWAA2022070111563Floorbeam · corrodedCORROSION FLOORBEAM ON BS 986.5 AT RBL 42 AND WL 207.54 AT PASSENGER CABIN 2022-265945 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600 D; S/N: 210138103; DUE DATE: 11-APR-23;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600 D; S/N: 210138SDR SWAA2022070111568Floorbeam · crackedCORROSION FLOORBEAM ON BS 986.5 AT LBL 42 AND WL 207.54 AT PASSENGER CABIN 2022-265946 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600 D; S/N: 210138103; DUE DATE: 11-APR-23;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600 D; S/N: 210138SDR SWAA2022070111564Plate · corrodedCORROSION FLOOR STRUCTURE PLATE BTW BS 1016 TO BS 1032 AT WL 207.54 AND LBL 3.0 AT PASSENGER CABIN 2022-265949 / [01] REPLACED PLATE AND FASTENERS LOC. FLOOR STRUCTURE BTW BS 1016 TO BS 1032 AT WL 207.54 AND LBL 3.0 AT PASSENGER CABIN IAW B737-700 DWG 147A5600SDR SWAA2022070111348Rib · crackedCRACK LEADING EDGE RIB LOCATED AT LE STA 78.29 AT LT HORIZONTAL STABILIZER 2022-266012 / [01] REPLACED RIB AND FASTENERS LEADING EDGE LOCATED AT LE STA 78.29 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND B737-700 DWG 186A1001 SHEET 10 REV A; SEE INSDR SWAA2022070111349Rib · crackedCRACK LEADING EDGE RIB LOCATED AT LE STA 123.85 AT LT HORIZONTAL STABILIZER 2022-266013 / [01] REPLACED RIB AND FASTENERS LOCATED AT LE STA 123.85 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND B737-700DWG 186A1001 SHEET 10 REV A. SEE INDIVIDUAL SIGSDR SWAA2022070111350Rib · crackedCRACK LEADING EDGE RIB LOCATED AT LE STA 105.26 AT RT HORIZONTAL STABILIZER 2022-266014 / [01] REPLACED RIB AND FASTENERS LEADING EDGE LOCATED AT LE STA 105.26 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND B737-700 DWGSDR SWAA2022070111104Access Panel · crackedCRACK ON LATCH LOCATED ON ACCESS PANEL 192CL AT LOWER FUSELAGE 2022-265989 / [01] REPLACED LATCH LOCATED ON ACCESS PANEL 192CL AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02.;[02] REPLACED LATCH LOCATED ON ACCESS PANEL 192CL AT LOWER FUSELAGE IAW B737-700 SRM 51-SDR SWAA2022070110914Shield · crackedCRACK ON AFT CARGO DOOR CUTOUT SHIELD AT LEVEL BS 492 TO BS 500A AND STRINGER 25R OF FWD CARGO COMPARTMENT 2022-265980 CRACK ON FWD CARGO DOOR CUT OUT SHIELD AT LEVEL BS 492 TO BS 500A AND STR 25R OF FWD CARGO COMPARTMENT / [01] REPLACED SHIELD AND FASTENERS LSDR SWAA2022070110586Stub Frame · crackedCRACK FRAME STUB LOCATED ON BS 294.5 AT FWD UPPER CORNER OF R1 DOOR CUT OUT AT PASSENGER CABIN 2022-265933 / [01] INSTALLED STUB FRAME; LOCATED ON BS 294.5 AT FWD UPPER CORNER OF R1 DOOR CUT OUT AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-SDR SWAA2022070110581Web · crackedCRACK FLOOR STRUCTURE WEB LOCATED BTW BS 312 TO BS 328 AT LBL 46 AT PASSENGER CABIN 2022-265925 / [01] REPLACED WEB AND FASTENERS LOC. BS 312 TO BS 328 AT LBL 46 AT PASSENGER CABIN. IAW B737-700 SRM 51-10-02 ITEM 9. DRAWING 141A5400. REV. -;[02] CORRECTED STEPSDR SWAA2022070110580Web · crackedCRACK FLOOR STRUCTURE WEB LOCATED BTW BS 328 TO BS 344 AT LBL 47 AT PASSENGER CABIN 2022-265926 / [01] REPLACED WEB AND FASTENERS LOCATED BTW BS 328 TO BS 344 AT LBL 47 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND DRAWING 141A5400. SHEET 44; REV -.;[02] COSDR SWAA2022070110583Web · crackedCRACK FLOOR STRUCTURE WEB LOCATED BTW BS 312 TO BS 328 AT RBL 31 AT PASSENGER CABIN 2022-265929 / [01] REPLACED WEB LOCATED BTW BS 312 TO BS 328 AT RBL 31 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND DWG 141A5400; SHEET 20; REV.-;[02] CORRECTED STEP 1.<BR>SDR SWAA2022070110584Web · crackedCRACK FLOOR STRUCTURE WEB BTW BS 270 TO BS 294 AT BL 0 AT PASSENGER CABIN 2022-265930 / [01] REPALCED WEB AND FASTENERS LOC. BS 270 TO BS 294 AT BL 0 AT PASSENGER CABIN. IAW B737-700 SRM 51-10-02 ITEM 9 DRAWING 141A5400. REV.-;[02] CORRECTED STEP 1.<BR>REPALCESDR SWAA2022070110579Structure · crackedCRACK INNER CHORD LOCATED ON BS 303.9 AT LEVEL STR 17L AT PASSENGER CABIN 2022-265923 / [01] REPLACED INNER CHORD AND FASTENERS LOC. BS 277 TO BS360 AT LEVEL STR 17L AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND SRM 51-40-02; DWG 141A81A8 REV. - AND DWG 140SDR SWAA2022070110582Web · brokenBROKEN FLOOR STRUCTURE WEB LOCATED BTW BS 344 TO BS 360 AT BL 0 AT PASSENGER CABIN 2022-265928 / [01] REPLACED WEB LOCATED ON FLOOR STRUCTURE BETWEEN BS 344 TO BS 360 AT BL 0 AT PASSENGER CABIN IAW SRM B737-700 51-40-02 AND SRM B737-700 51-10-02 ITEM 9 AND DWGSDR SWAA2022070110585Floorbeam · crackedCRACK FLOORBEAM LOCATED ON BS 294.5 AT RBL 52 AT PASSENGER CABIN 2022-265931 / [01] TOOL USED CALIPER P/N:500-197-30 S/N:A21042094 DUE DATE: 01-FEB-23;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[03] TOOLS USED: TEMSDR SWAA2022070110578Bracket · brokenBROKEN BRACKET STRUT FAIRING BOX AFT POSITION OUTBOARD SIDE AT LT PYLON (1 EA) 2022-265922 / [01] REPLACED BRACKET STRUT FAIRING BOX LOC. AT AFT POSITION OUTBOARD SIDE AT LT PYLON (1E/A) AND FASTENERS IAW B737-700 SRM 51-40-02 DWG #311A2683 REV. -. SEE INDIVID
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