N7748A
Service difficulty reports · 253
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 = 'N7748A' 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 = 'N7748A' 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 SWAA2025030693489Skin · crackedCRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 25.5' FROM FWD EDGE; .75' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON RH HORIZONTAL STABILIZER LOWER SKIN STA 193.9 25.5' FROM FWD EDGE; AND INSTALLED REPAIR PARTS IAW SRM 55-10-01-2R-11SDR SWAA2025030693486Attach Angle · crackedCRACKED INTERCOSTAL UPPER ATTACH ANGLE AT AFT CABIN BS927+4 BL0 WL208. MARKED<[01] REMOVED AND REPLACED UPPER ATTACH ANGLE PN#147A5430U1 FROM BS927-BS947 AT BL0; WL208 IAW SRM 51-40-02 AND IAW DWG#147A5400 REV:-.;[02] CORRECTIVE ACTION COMPLETED.SDR SWAA2025030593487Skin · crackedCRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 25.5' FROM FWD EDGE; .3' IN LENGTH (MARKED)<[01] REMOVED THE DAMAGED PART ON LH HORIZONTAL STABILIZER LOWER SKIN STA 193.9 25.5' FROM FWD EDGE; AND INSTALLED REPAIR PARTS IAW SRM 55-10-01-2R-11;SDR SWAA2025031095377Vapor Barrier · crackedTHE L/H B.S. 663 VAPOR BARRIER HAS AN ALUMINUM FOIL PREVIOUS REPAIR LOCATED AT APPROXIMATELY LBL 55 <[01]. PREVIOUS ALUMINUM FOIL REPAIR ON L/H B.S. 663 VAPOR BARRIER LOCATED AT APPROXIMATELY LBL 55 WAS REMOVED; AND PERMANENT REPAIR WAS ACCOMPLISHED IAW SRM 5SDR SWAA2025030692615Floor Panel · pulledFLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231YF; WITH UPPER SKIN AREAS OF PULLED STRANDS; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2025030692621Floor Panel · pulledFLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241CF UPPER SKIN HAS PULLED STRANDS REPAIRED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]SDR SWAA2025030692616Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF UPPER SKIN HAS PULLED STRAINDS REPAIRED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]SDR SWAA2025030692623Floor Panel · pulledFLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241FF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030692619Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231ZF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030692620Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030692622Floor Panel · pulledFLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241EF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030692624Floor Panel · pulledFLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 242AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030592618Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF; WITH UPPER SKIN AREAS OF PULLED STRANDS; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2025031092613Attach Angle · crackedCRACKED ATTACH ANGLE AT MIDCABIN; RBL 24; STA 693; WL 203 <[01]. REMOVED AND REPLACED ATTACH ANGLE AT MIDCABIN RBL 24 BS 693 WL 203 PER SRM 51-40-02 AND DWG 273A9110 REV A;[02] VERIFIED ALL STEP; CORRECTION ACTION ITEM 1 MEASUREMENT FIELD COMPLETE; CARD COMPLSDR SWAA2025030692222Scuff Plate · crackedFSD AFT CORNER SCUFF PLATE CRACKED<[01] PROCURED SCUFF PLATE P/N 141A8431-3 LOT: 1594959-1. IAW IPC 53-13-00-13;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2025010682960Skin · pulled#1 ENG INNER INLET COWL LIPSKIN HAS ONE PULLED THROUGH FASTENER IN SEGMENT 3<[01] COMPLIED WITH EA 25-171-00023; REF TTG8Q00XYR35. THIS REMAINS ON TLD.SDR SWAA2024120273198Battery Pack · inoperativeEMERGENCY EXIT AISLE LIGHTS FROM SEAT 12C TO 20C (4EA LIGHTS) DID NOT COME ON DURING TEST.<[01] 01 - REMOVED AND REPLACED BATTERY PACKS AT SEAT 7A AND 17A PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)] OPS CHECK GOOD.SDR SWAA2024112561830Heater · smokeON FINAL CAPTAIN WINDOW POPPED WITH SPARKS AND SMOKE. TURNED OFF ALL WINDOW HEAT AND CONTINUED. CHECKLIST COMPLETED ON GROUND. COULD NOT TELL WHICH WINDOW IT WAS BUT IT WAS AT THE CORNER OF EITHER THE FRONT OR SIDE WINDOW CAPT SIDE<[01] INSPECTED L-1AND L-2 WISDR SWAA2024111860603Slide · out of positionR2 AND L2 DOOR SLIDES PREVENT DOORS CLOSING. POSSIBLE MANUFACTURING ISSUE WITH THE 5A3307-9 SLIDES THAT WERE INSTALLED AFTER THE EVACUATION. THE GIRT SKIRT WAS TOO LONG AND HAD BEEN REINFORCED WITH A RUBBERIZED COATING THAT WAS STIFF ENOUGH TO PREVENT THE DOORSDR SWAA2024111258016Skin · crackedRIGHT INBOARD AFT FLAP HAS A 3' HORIZONTAL CRACK AND HAS A DENT 40' FROM INBOARD EDGE AND 1/2' FROM LEADING EDGE.<[01] REMOVED AND REPLACED RIGHT HAND INBOARD AFTFLAP; RIG AND OPS CHECK GOOD IAW AMM 27-51-12;[02] C/W INSPECTION OF RIG AND OPS CHECK GOOD IAW AMSDR SWAA2024111157219Fairing · delaminatedRIGHT WING TO BODY 194CR PANEL HAS 3' AREA OF DELAMINATION (12.5' FROM INBOARD EDGE AND 11.5' FROM AFT EDGE)<[01] REMOVED AND REPLACED PANEL # 194CR PER M/M 53-51-21;[02] REMOVED AND REPLACED PANEL # 194CR PER M/M 53-51-21SDR SWAA2024111157217Skin · crackedRIGHT INBOARD AFT FLAP HAS A 3' HORIZONTAL CRACK AND HAS A DENT 40' FROM INBOARD EDGE AND 1/2' FROM LEADING EDGE<[01] CW EA 24-127-03094SDR SWAA2024110857534Tire · blown#3 MAIN TIRE BLOWN ON TAKEOFF AND LOST ENG HYD PUMP AND A SYS QUANT<[01] REMOVED AND REPLACED #3 AND #4 WHEEL AND TIRE ASSEMBLIES PER AMM 32-45-11. ALL OTHER WORK COMPLETED ON<BR> W.O. # 86751574SDR SWAA2024081626271Vapor Barrier · cracked6 INCH CRACK FOUND IN LH WHEEL WELL AREA ON REAR VAPOR BARRIER. CRACK IS LOCATED BEHIND SYSTEM A HYDRAULIC PRESSURE MODULE.<[01] COMPLIED WITH EA# M-21-157-00675SDR SWAA2024053091464Lens · missingFLIGHT ATTENDANT REPORTS EMERGENCY EXIT SIGN MISSING ON OVER WING EXIT CAPTS SIDE<[01] INSTALLED NEW EMERGENCY EXIT LIGHT LENS ON CAPT?S SIDE OVER WING EXIT SIGN PER AMM 33-51-01SDR SWAA2024022354815Engine · flamed outON TAXI FOR TAKEOFF; REPORT OF LEFT ENGINE FLAME IN FRONT OF ENGINE SHOOTING OUT BACK OF ENGINE & AN ASSOCIATED BOOM SOUND. FLAME AND BOOM CONFIRMED BY GROUND CREW. NO EGT RISE NO ABNORMAL ENGINE PARAMETERS NOTED. ENGINE SHUT DOWN FOR TAXI TO GATE.<[01] R&R #1SDR SWAA2024012242426Sump · leaking#1 ENGINE TAILPIPE FIRE AND FLAME REPORTED BY A/C BEHIND FLIGHT.OILY SMELL IN CABIN-SHUT ENGINE DOWN PER QRH<[01] ACCOMPLISHED INSPECTION OF #1 ENGINE AND FOUND OIL LEAK COMING FROM AFT SUMP (OVERBOARD DRAIN) PER POWER PLANT ENGINEERING OIL CONSUMPTION IS WITHSDR SWAA2024011640609Light · inoperativeFLOOR PATH LIGHTING; AIRCRAFT RIGHT; 1ST HALF INOP.<[01] REMOVED AND REPLACED FLOOR PATH LIGHTING (PHOTOLUMINESCENT STRIP) RIGHT HAND 1ST HALF PER AMM 33-51-15.SDR SWAA2024011240342Sign · brokenAFT GALLEY EXIT SIGN BROKEN<[01] REPLACED MISSING SCREWS AND REINSTALLED EXIT SIGN PER AMM 33-51-01; OPS CHECK NORMAL.SDR SWAA2023101109019Sensor · faultyPACKS AIR FLOW VERY LOW AT TIMES BLOWING WARM AIR GRD AND IN FLIGHT UNABLE TO COOL AIRCRAFT SUFFICIENT FLIGHT ATTENDANTS REPORTS ODOR OUT OF THE FWD AIR OUTLET ;..<[01] R+R LT AND RT COALESCER BAGS REF M/M 21-51-05 REPLACED CONTROL CABIN TEMP SENSOR FILTER REFSDR SWAA2023041929147Lens · out of adjustEXIT SIGN LENS ABOVE AFT SERVICE DOOR (F/O SIDE) LOOSE<[01] ADJUSTED AND REATTACHED IAW SIP; NO FURTHER DEFECTS NOTED.SDR SWAA2023020992394Floor Panel · deterioratedDETERIORATED CLIP NUT FLOOR PANEL 221BF AND 221DF FWD GALLEY AND LAV 2022-708801<[01] REPLACED CLIP NUT FLOOR PANEL 221BF AND 221DF FWD GALLEY AND LAV IAW B737-700 AMM 53-21-00-400-801 STEP 3 F (10) (C) (D);[02] REPLACED CLIP NUT FLOOR PANEL 221BF AND 221DF FWSDR SWAA2023021092002Plate · elongatedREJECT ELONGATED HOLE 2EA PLATES LOCATE RBL 27 RH VAPOR BARRIER AT MAIN WHEEL WELL COMPARTMENT 2022-708792<[01] MADE PLATES (2E/A) LOCATED RBL 27 RH VAPOR BARRIER AT MAIN WHEEL WELL COMPARTMENT I.A.W B737-700 SRM 51-40-05 AND DWG 111A1511 SHEET: 9 REV:-MATERIASDR SWAA2023020991724Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS312 TO BS328 RBL32 AT FWD GALLEY AREA 2022-708790<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS312 AND BS328 RBL32 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG# 141A5SDR SWAA2023021091459Scuff Plate · crackedCRACK ON FWD SERVICE DOOR SCUFF PLATE 2022-708780<[01] TOOL USED DIGITAL CALIPER P/N:500-193-30;S/N:0000293;DUE DATE:12/OCT/23.;[02] REPAIRED FWD SERVICE DOOR SCUFF PLATE I.A.W. BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975 SEE INDIVIDUAL SIGNOFFS BELSDR SWAA2023021090014Stringer · brokenBROKEN STRINGER CLIP ASSEMBLY WIRE SUPPORT AT FWD CARG O COMPARTMENT (4EA) 2022-708759<[01] REPLACED STRINGER CLIP ASSEMBLY WIRE SUPPORT AT FWD CARGO COMPARTMENT (4EA) IAW SWPM 20-10-12;[02] REPLACED STRINGER CLIP ASSEMBLY WIRE SUPPORT AT FWD CARGO COMPARTMENTSDR SWAA2023021090013Stringer · brokenBROKEN STRINGER CLIP ASSEMBLY WIRE SUPPORT STA 480 STR 24L AT FWD CARGO COMPARTMENT 2022-708758<[01] REPLACED STRINGER CLIP ASSEMBLY WIRE SUPPORT STA 480 STR 24L AT FWD CARGO COMPARTMENT IAW B737-700 SWPM-20-10-12;[02] CERTIFIED WORK PERFORMED.SDR SWAA2023021089329Support · corrodedCORROSION SUPPORT ZEE LOCATED BS887 TO BS947.5 AT RBL 21 AND WL 178 AFT CARGO COMPARTMENT 2022-708726<[01] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BS887 TO BS947.5 AT RBL 21 AND WL 178 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 AND DWGSDR SWAA2023021089341Support · corrodedCORROSION SUPPORT ZEE LOCATED BS727 TO BS767 AT RBL21 AND WL157 AFT CARGO COMPARTMENT 2022-708723<[01] TOOL USED DIGITAL CALIPER P/N: 500-752-20; S/N: A21034751; DUE DATE: 01-MAR-23.;[02] REPLACED SUPPORT ZEE LOCATED BS727 TO BS767 AT RBL21 AND WL157 AFT CARGOSDR SWAA2023021089331Beam · corrodedCORROSION ON FLOOR BEAM LOCATED BS 986.5 LBL 46 WL 208.1 AT AFT GALLEY AREA 2022-708734<[01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101V022235; DUE DATE: 03 AUG 23;[02] TOOL USED: P/N FPK-PRO-104; S/N PRO-3446; DUE DATE 12/JAN/23;[03] PERFSDR SWAA2023021089332Beam · corrodedCORROSION ON FLOOR BEAM LOCATED BS 986.5 RBL 46 WL 208.1 AT AFT GALLEY AREA 2022-708736<[01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101V022235; DUE DATE: 03 AUG 23;[02] TOOL USED: P/N FPK-PRO-104; S/N PRO-3446; DUE DATE 12/JAN/23;[03] REPASDR SWAA2023021089327Angle · crackedCRACK ANGLE LOCATED BETWEEN BS907 TO BS927 AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT 2022-708728<[01] REPLACED ANGLE LOCATED BETWEEN BS907 TO BS927 AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 147A722SDR SWAA2023021089334Angle · crackedCRACK ANGLE LOCATED BS827 AT LEVEL STR 25R AFT CARGO COMPARTMENT 2022-708737<[01] REPLACED ANGLE LOCATED BS827 AT LEVEL STR 25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DRAWING 146A0081; SHEET 32; REV- DRAWING 146A8120; SHEET 37; REV -.<BR>SEE INDIVIDUASDR SWAA2023021089342Angle · crackedCRACK ANGLE LOCATED BS807 AT LEVEL STR25R AFT CARGO COMPARTMENT 2022-708735<[01] REPLACED ANGLE LOCATED BS807AT LEVEL STR 25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DRAWING 146A0081; SHEET 32 REV- DRAWING 146A8120; SHEET 37; REV -<BR>SEE INDIVIDUAL SISDR SWAA2023021089328Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BS927 TO BS947.5 AT RBL21 AFT CARGO COMPARTMENT 2022-708727<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 927 TO BS 947.5 AT RBL 21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 147A7500 SHEET 27 REV -. SEE INDIVIDUAL SSDR SWAA2023021089339Support · corrodedCORROSION SUPPORT ZEE LOCATED BS727 TO BS847 AT LBL21 AND WL157 AFT CARGO COMPARTMENT 2022-708724<[01] REPLACED SUPPORT ZEE LOCTED BS727 TO BS847 AT LBL21 AND WL157 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG#146A7502 REV:- SEE INDIVIDUAL SIGNOFFS<SDR SWAA2023021089337Intercostal · corrodedCORROSION WEB - INTERCOSTAL LOCATED BS767 TO BS787 AT RBL21 AND WL 157 AFT CARGO COMPARTMENT 2022-708725<[01] REPLACED WEB - INTERCOSTAL(SHIELD) AND FASTENERS LOCATED BS767 TO BS787 AT RBL21 AND WL 157 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40SDR SWAA2023021089322Rib · crackedCRACK ACCESS PANEL 321A RIB 8 AT DORSAL FIN VERTICAL STABILIZER 2022-708720<[01] REPLACED ANGLE RIB 8 AT DORSAL FIN VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A1008. SHEET 2 REV: C;[02] REPLACED ANGLE RIB 8 AT DORSAL FIN VERTICAL STABILIZER IAW BSDR SWAA2023021089336Fitting · corrodedCORROSION ON DRAG BRACE FITTING RT AFT SPAR FWD OUTBOARD POSITION ON VERTICAL STABILIZER 2022-708741<[01] REPLACED DRAG BRACE FITTING RT AFT SPAR FWD OUTBOARD POSITION ON VERTICAL STABILIZER IAW SRM B737-700 51-40-02; SRM B737-700 51-10-02 PARAGRAPH 9 AND DRAWSDR SWAA2023020989320Floor Panel · brokenBROKEN FLOOR PANEL 221BF AT FWD WET AREA 2022-708713<[01] REPLACED FLOOR PANEL 221BF AT FWD WET AREA IAW B737-700-AMM 53-21-00-400-801 PREVIOUS COMPLETED WITH TTG8Q00G7U15;[02] REPLACED FLOOR PANEL 221BF AT FWD WET AREA IAW B737-700-AMM 53-21-00-400-801 PREVIO
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