N7747C
Service difficulty reports · 170
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 = 'N7747C' 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 = 'N7747C' 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 SWAA2026101921101Scuff Plate · crackedR1 ENTRYWAY SCUFF PLATE WAS CRACKED IN THE AFT CORNER. C/W 26-153-02762 R1 GALLEY DOOR LOWER MAIN SILL SCUFF PLATE CRACK TIME LIMITED.SDR SWAA2026101978282Slide · out of positionR2 DOOR SLIDE GIRT BAR WEBBING DRAGGING AGAINST AIRCRAFT PREVENTING DOOR CLOSURE. REPOSITIONED SLIDE PACK IN COVER IAW AMM 25-66-01 AND MT 725-61-06.SDR SWAA2026060107107Seal · crackedR/H HORIZONTAL STAB UPPER SLIDING SEAL CRACKED. REPLACED TEH RIGHT UPPER SLIDING SEAL PER AMM 53-31-31.SDR SWAA2025101423670Light · inoperativeAIRCRAFT RIGHT OVERWING EXIT LIGHT INOP AT 12DEF; & 20 DEF ALSO INOP. OK TO CONTINUE PER MEL 33-2-03. SP-1B. PERFORMED OPS TEST OF EMERGENCY LIGHTS OPS TEST GOOD PER AMM 33-51-00.SDR SWAA2025051971578Light · inoperativeINOP AFT SERVICE DOOR EMERGENCY LIGHT AT PASSENGER CABIN. REPLACED AFT SERVICE DOOR EMERGENCY LIGHT ON HEADER PANEL AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 STEP 2.C.(1)(A) AND 2.C.(1)(C) THRU 2.C.(2);(3);(4) TEST IS OK.SDR SWAA2025051957390Bracket · crackedMAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL0 TO LBL 24.75. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED MAIN CABIN FLOOR STRUCTURE AT STA 540 BL0 TO LBL 24.75 IAW B737-700 SRM 51-40-02-0G AND DWG: 143A0060 SHEET: 46 REV: -.SDR SWAA2025051957392Bracket · crackedMAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540 BL0 TO RBL 24.75. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED MAIN CABIN FLOOR STRUCTURE AT STA 540 BL0 TO RBL 24.75 IAW B737-700 SRM 51-40-02-0G AND DWG: 143A0060 SHEET: 46 REV: -.SDR SWAA2025051957378Access Panel · crackedCRACK SEAL - PLATE ACCESS PANEL 333AT AT LT HORIZONTAL STAB 2025-250486<[01] REPLACED BLADE ON ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 186A3101 SHEET: 19 REV - ; FOR INSTALLATION SEE FAULT TTG8Q00ZFCLW;[SDR SWAA2025051957380Rib · crackedCRACK LEADING EDGE RIB LOCATED LE STA 95.96 AT RT HORIZONTAL STABILIZER. REPLACED RIB LOCATED LE STA 95.96 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02-0G PARAGRAPH 9; SRM 51-40-02-0G AND DWG: 186A1001; SHEET: 19; REV: -.SDR SWAA2025051957381Access Panel · crackedCRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER 2025-250492<[01] REPLACED LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG:186A1001 SHEET: 19; REV:SDR SWAA2025052157374Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED AFT UPPER AREA OUTBOARD THRUST REVERSER ON ENGINE 2 2025-250468 <[01]. REPLACED SUPPORT BRACKET LOCATED AFT UPPER AREA OUTBOARD THRUST REVERSER ON ENGINE 2 IAW B737-700 SRM 51-10-02 AND DWG 315A2104 SHEET 21 REV -. TOOL USED CALISDR SWAA2025051957370Cargo Track · crackedCRACK TRACK RBBL 13.84 LOCATED BS 747 TO BS 767 AFT CARGO COMPARTMENT 2025-250476<[01] TOOL USED ON STEP 5 AND 6: EDDY CURRENT EQUIPMENT P/N: NORTE 600D; S/N: 240525411; DUE DATE: 13-NOV-25.;[02] PERFORMED REPAIR ON TRACK LOCATED ON RBL 13.84 BETWEEN BS 727 ANSDR SWAA2025051957377Support Web · crackedCRACK SUPPORT WEB LOC INBOARD FAN COWL ON ENGINE 1 2025-250482<[01] REPLACED SUPPORT WEB LOC INBOARD FAN COWL ON ENGINE 1 IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G PARAGRAPH 9 AND GOODRICH AEROSTRUCTURES CMM 71-13-30 REV 31; IPL FIGURE 4; SHEET 5.;[02] REPSDR SWAA2025051957369Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BS927 TO BS947.5 AND S-25R AT AFT CARGO COMPARTMENT 2025-250464<[01] REPLACED WEB - INTERCOSTAL LOCATED BS927 TO BS947.5 AND S-25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9. AND DRAWING # 147A7500 SHEET 27 REV: -SDR SWAA2025051957375Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS 827 AND S-25R AT AFT CARGO COMPARTMENT 2025-250480<[01] REPLACED ANGLE - SUPPORT LOCATED BS 827 AND S-25R AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 DWG 146A8120 SHEET 37 REV. - <BR><BR>SEE INDIVIDSDR SWAA2025051957376Angle · corrodedCORROSION ANGLE LOCATED BTW BS 767 TO BS787 AND S-25R WL 156 AT AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BTW BS 767 TO BS787 AND S-25R WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081 SHEET 31 REV-.SDR SWAA2025052057360Stub Frame · crackedAFTER REMOVE SEAL DEPRESSOR CRACK INDICATION FOUND ON STUB FRAME LOCATED ON BS 296.5 BTW STR 8 TO S-9R AT FWD GALLEY DOOR AREA. CRACK LENGTH : 0.395 INCHES APPROX AT PASSENGER CABIN. 2025-250429<[01] REPLACED STUB FRAME AND FASTENERS LOCATED ON BS 294.5 AT FWDSDR SWAA2025052057358Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED IRSS 140 AT LT WING 2025-250435<[01] REPLACED ANGLE TRAILING EDGE LOCATED IRSS 140 AT LT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2000 SHEET 21 REV ?-? <BR><BR>MEASURE OF CRACK IS L: 0.500 IN. TOOL USED DIGITSDR SWAA2025051957354Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BETWEEN BS291.5 AND BS 294.5 STRINGER 17R PASSENGER CABIN 2025-250425<[01] TOOK MEASURES OF CRACK LOCATED ON ANGLE BTW BS291.5 TO BS294.5 STR17R IS: 1.235' REFER TO FAULT TTG8Q00ZS5VD WHERE ANGLE WAS REPLACED;[02] CORRECTED STEP 1:<SDR SWAA2025051957359Access Panel · damagedELONGATED HOLES ON INTERNAL PLATE ACCESS PANEL 644BB FLAP SUPPORT FAIRING 8 AT RT WING 2025-250434<[01] REPLACED INTERNAL PLATE ACCESS PANEL 644BB FLAP SUPPORT FAIRING 8 AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.;[02] REPLACED INTERNAL PLATESDR SWAA2025051957351Reveal · crackedCRACK REVEAL LOCATED BS 299 BETWEEN STRINGER 8R AND STRINGER 9R PASSENGER CABIN 2025-250423<[01] REPLACED REVEAL AND FASTENERS LOCATED BS 299 BETWEEN STRINGER 8R AND STRINGER 9R AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG# 141A8370; SHEET 9; RESDR SWAA2025051957352Pressure Deck · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.750 IN. APPROX. PERFORMED PERMANENT REPAIR LOCATED ON HORIZONTAL PRESSURE DECK WEB BTW LBL 30 TO LBL 60 STA 663 TO STA 675 MAIN WHEEL WELL SDR SWAA2025051957355Angle · crackedCRACK INDICATION IN UPPER FASTENER HOLE LOCATED AT BS 727 FRAME INNER CHORD AT S-18A RIGHT SIDE CRACK DIRECTION 3 O CLOCK AND 9 O CLOCK AFT CARGO COMPARTMENT. REPLACED UPPER FITTING AND FASTENERS LOCATED AT BS 727 FRAME INNER CHORD AT S-18A RIGHT SIDE IAW B73SDR SWAA2025051957356Fitting · crackedCRACK INDICATION IN LOWER FASTENER HOLE LOCATED AT BS 727 FRAME INNER CHORD AT S-18A RIGHT SIDE.CRACK DIRECTION 3 O CLOCK AND 9 O CLOCK AFT CARGO COMPARTMENT. REPLACED LOWER FITTING AND FASTENERS LOCATED AT BS 727 FRAME INNER CHORD AT S-18A RIGHT SIDE IAW B73SDR SWAA2025051957357Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 217 AT LT WING. REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE AT LEVEL IRSS 217 AT LT WING IAW B737-700 SRM 51-40-02 AT MEASURES OF CRACK ARE: L= 0.750' DWG 115A2001 SHEET: 45 REV: -.SDR SWAA2025051957342Tie Clip · crackedCRACK TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN. REPLACED TIE CLIP AND FASTENERS LOCATED STA277 AND STR10R PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET:18 REV:-.SDR SWAA2025051923776Gland Nut · debondedCUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP IB EDGE AT LT WING 2025-250385<[01] TOOL USED: CALIPER PN: 500-196-30; SN: B23373747; DUE DATE: 26-JAN-26.;[02] TOOL USED STEP 3: ULTRASONIC EQUIPMENT; P/N: BONDMA600D; S/N: 230106912; DUE DATE: 05 FEB 26.;SDR SWAA2025051957322Floor Support · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400 AND LBL13 PASSENGER CABIN 2025-250326<[01] REPLACED ANGLE AND FASTENERS FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400 AND LBL13 PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; DSDR SWAA2025051957324Floor Support · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400 AND RBL10 PASSENGER CABIN 2025-250327<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400 AND RBL10 AT PASSENGER CABIN AND FASTENERS IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 SDR SWAA2025051957323Lens · brokenBROKEN EMERGENCY LIGHT LENS LAV A AT FWD GALLEY AREA. REPLACED EMERGENCY LIGHT LENS LAV A AT FWD GALLEY AREA I.A.W. B737-700 AMM 33-51-01-960-801 STEP 2. C. ITEM (1) (A) AND ITEM (4).SDR SWAA2025052057301Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED STA312 TO STA328 AND LBL45 FWD GALLEY AND LAV 2025-250259 <[01]. REPLACED NEW WEB - INTERCOSTAL FLOOR STRUCTURE AND FASTENERS LOCATED STA312 TO STA328 AND LBL45 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 AND DWSDR SWAA2025051957300Web · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED STA344 TO STA360 AND BL0 FWD GALLEY AND LAV 2025-250263<[01] REPLACED INTERCOSTAL FLOOR STRUCTURE LOCATED STA344 TO STA360 AND BL0 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET 32 REV ?-? SDR SWAA2025051957310Floor Support · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND BL0 PASSENGER CABIN 2025-250280<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED STA 695 AND BL0 PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 273A9110 SHEET 6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[0SDR SWAA2025051957309Web · corrodedCORROSION WEB LOCATED BETWEEN 1006 PLUS 12INCH LBL6 AND WL208 AT PASSENGER CABIN 2025-250276 CORROSION WEB LOCATED BETWEEN BS1006 PLUS 12INCH LBL6 AND WL208 AT PASSENGER CABIN<[01] REPLACED WEB LOCATED BETWEEN 1006 TO BS 1040 AND BL0 TO LBL35 AND WL208 AT PASSSDR SWAA2025051957299Stub Frame · crackedCRACK STUB FRAME LOCATED ON BS 294.5 AND RBL53 LOWER POSITION AT FWD GALLEY AREA 2025-250257<[01] ON STEP 7 AND 8. PERFORMED PERMANENT REPAIR ON STUB FRAME LOCATED ON BS294.5 AND RBL53 LOWER POSITION AT FWD GALLEY AREA I.A.W. B737-700 SRM 53-10-15-2R-7.SDR SWAA2025051957298Angle · crackedCRACK INNER CHORD LOCATED STA 303.9 AND LBL 55 AND WL 208.1 AT FWD GALLEY AND LAV. REPLACED INNER CHORD AND FASTENERS LOCATED STA 270 TO STA 360 AND LBL 55 AND WL 208.1 AT FWD GALLEY AND LAV I.A.W B737-700 SRM 51-40-02 DWG 141A8110 SHEET 9 REV. A AND 51-10-02SDR SWAA2025051922939Frame · corrodedCORROSION FRAME ON BS 303.9 AND LBL52 WL210 FWD GALLEY AND LAV. PERFORMED REPAIR ON FRAME LOCATED BS 303.9 LBL 55 WL 208.3 AT FWD GALLEY AREA IAW EA 25-153-01057-WIP1.SDR SWAA2025052022382Support Angle · crackedCRACK SLAT 2 SUPPORT ANGLE ON OUTBOUND AUXILIARY TRACK AT LT WING (2 EA) 2025-250126<[01] REPLACED SUPPORT ANGLE ON SLAT 2 OUTBOUND AUXILIARY TRACK AT LT WING (2 EA) IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 MEASURES OF CRACK L:2.040? TOOL USED DIGITALSDR SWAA2025051957256Floor Panel · delaminatedDELAMINATED FLOOR PANEL 232SF AT PASSENGER CABIN 2025-250108<[01] TOOL USED: CALIPER:P/N:500-193-30;S/N: B20189571; DUE DATE: 06-JUN-25;[02] TOOL USED: HOT BONDER: P/N: HCS9200B-AV; S/N: 18185781; DUE DATE: 22-FEB-26;[03] TOOL USED: SCALE P/N: CR5200; S/N: 834SDR SWAA2025051957254Floor Panel · crackedCRACK FLOOR PANEL 242AF AT PASSENGER CABIN 2025-250106<[01] TOOL USED: CALIPER :P/N:500-193-30;S/N: B20189571; DUE DATE: 06-JUN-25;[02] TOOL USED: HOT BONDER: P/N: HCS9200B-AV; S/N: 18185781; DUE DATE: 22-FEB-26;[03] TOOL USED: SCALE P/N: CR5200; S/N: 83431108SDR SWAA2025051957258Vapor Barrier · crackedCRACK VAPOR BARRIER LOCATED BS663.75 ON LBL 31 AT MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER LOCATED BS663.75 ON LBL 31 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2025051957261Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING 2025-250130<[01] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9. AND SRM B737-700 51-40-02 AND DRAWING # 115A2930 SHEET 6 REV: -.;[02] TASK COMPLETEDSDR SWAA2025051957260Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING 2025-250129<[01] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9. AND SRM B737-700 51-40-02 AND DRAWING # 115A2930 SHEET 6 REV: -.;[02] TASK COMPLETEDSDR SWAA2025051957252Light · deterioratedDETERIORATED PHOTOLUMINESCENT STRIP LT SIDE AT PASSENGER CABIN (5EA) 2025-250104<[01] REPLACED PHOTOLUMINESCENT STRIP LT SIDE AT PASSENGER CABIN (5EA) IAW B737-700 AMM-33-51-15-400-802;[02] CERTIFIED CORRECTIVE ACTION STEP 1SDR SWAA2025051957253Light · deterioratedDETERIORATED PHOTOLUMINESCENT STRIP RT SIDE AT PASSENGER CABIN (6EA). REPLACED PHOTOLUMINESCENT STRIP RT SIDE AT PASSENGER CABIN (6EA) IAW B737-700 AMM 33-51-15-400-802.SDR SWAA2025051957248Vapor Barrier · crackedCRACK VAPOR BARRIER LOCATED BS663.75 ON RBL 39 AT MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR BARRIER LOCATED BS663.75 ON RBL 39 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2025031104131Pin · missingR1 ESCAPE SLIDE PIN MISSING.<[01] REINSTALLED PIN ON R1 SLIDE AND C/W MT 725-61-06SDR SWAA2024092039060Bottle · low pressureL1 DOOR SLIDE GAUGE IS IN THE RED<[01] INSPECTED L1 DOOR SLIDE PER AMM 25-66-01. L1 DOOR SLIDE IS IN SERVICEABLE CONDITION.SDR SWAA2024013046190Idg · inoperative#2 SOURCE LIGHT ILLUMINATED ALONG WITH #2 GENERATOR DRIVE LIGHT. FOLLOWED QRH PROCEDURES AND DISCONNECTED #2 GENERATOR.<[01] REMOVED AND REPLACED #2 IDG IAW AMM 24-11-11SDR SWAA2023090596924Handle · damagedCREW REPORTS R1 DOOR HANDLE COVER LOOSE<[01] RE-SECURED R1 DOOR HANDLE COVER PLATE AND STUD WITH EPOXY AND REINSTALLED BACK ON HANDLE REF STANDARD INDUSTRY PRACTICE.
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