# Service difficulty reports: N217JC

A list on [N217JC](https://openairdocs.org/aircraft/N217JC.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 6 · 266 reports

- [SDR SWAA2026101201027](https://openairdocs.org/sdr/SWAA2026101201027.md): Lavatory · dirty · Oct 6, 2026 · N217JC · Boeing 7377H4 · Lavatories
  > FORWARD LAV HAD A HORRIBLE ODOR. FWD LAV CLEANED IAW TTG8Q01FSWJ9.
- [SDR SWAA2026042492106](https://openairdocs.org/sdr/SWAA2026042492106.md): Girt Bar · loose · Apr 23, 2026 · N217JC · Boeing 7377H4 · Emergency Equipment
  > L1 DOOR GIRT BAR BRACKET LOOSE<[01] RE-SECURED L1 DOOR GIRT BAR BRACKET. NO OTHER DEFECTS NOTED AT THIS TIME. REF AMM 25-66-01
- [SDR SWAA2026040381804](https://openairdocs.org/sdr/SWAA2026040381804.md): Pressure Blkhd · cracked · Mar 21, 2026 · N217JC · Boeing 7377H4 · Fuselage Main, Bulkhead
  > DURING INSPECTION OF BS 1016 AFT PRESSURE BULKHEAD CENTER DOME APEX - GROUP 2; INDICATION OF A CRACK AT BL0 FASTENER DURING HFEC INSPECTION. CRACK VERIFIED POST PAINT REMOVAL AS PER NDT PART 6, 53-10-64 AND PART 6, 51-00-00, PROC 23 COMPLIED WITH. REPAIRED
- [SDR SWAA2026010858254](https://openairdocs.org/sdr/SWAA2026010858254.md): Oil System · leaking · Jan 4, 2026 · N217JC · Boeing 7377H4 · Turbine Engine Oil System
  > LOST OIL QUANTITY THEN WE LOST OIL PRESSURE ON NR 1 ENG. SHUTDOWN AND LANDED WHITE BOX CAME ON FOR THE OIL QTY AND 20 MINS LATER WENT YELLOW THEN RED ON THE OIL PRESSURE. REMOVED AND REPLACED #1 ENGINE I/A/W MT 771-00-01. REF TTG8Q015T71N FOR ACCOMPLISHMENT
- [SDR SWAA2025120240639](https://openairdocs.org/sdr/SWAA2025120240639.md): Pump · failed · Nov 29, 2025 · N217JC · Boeing 7377H4 · Engine Fuel Pump
  > AFTER EXITING RUNWAY (AFTER LANDING), NR 1 ENGINE FAILED. FAIL ON ENGINE INSTRUMENTS. NR 1 GEN OFF LINE AT SAME TIME. NR 1 ENGINE SPOOLS UP MUCH SLOWER ON TAKEOFF COMPARED TO NR 2 ENGINE. NR 1 ENG FUEL PUMP & HMU R+R PER MT 773-11-00. PS3 CONNECTOR FOUND DI
- [SDR SWAA2025120241853](https://openairdocs.org/sdr/SWAA2025120241853.md): Hmu · failed · Nov 29, 2025 · N217JC · Boeing 7377H4 · Fuel Control/Turbine Engines
  > AFTER EXITING RUNWAY (AFTER LANDING) NR 1 ENGINE FAILED. FAIL ON ENGINE INSTRUMENTS. NR 1 GEN OFF LINE AT SAME TIME. NR 1 ENGINE SPOOLS UP MUCH SLOWER ON TAKEOFF COMPARED TO NR 2 ENGINE. NR 1 ENG FUEL PUMP & HMU R & R IAW MT 773-11-00. PS3 CONNECTOR FOUND D
- [SDR SWAA2025120241854](https://openairdocs.org/sdr/SWAA2025120241854.md): Elec Connector · disconnected · Nov 29, 2025 · N217JC · Boeing 7377H4 · Engine Fuel System Wiring
  > AFTER EXITING RUNWAY, AFTER LANDING. NR 1 ENGINE FAILED. FAIL ON ENGINE INSTRUMENTS.NR 1 GEN OFF LINE AT SAME TIME. NR 1 ENGINE SPOOLS UP MUCH SLOWER ON TAKEOFF COMPARED TO NR 2 ENGINE. NR 1 ENG FUEL PUMP AND HMU R & R PER MT 773-11-00. PS3 CONNECTOR FOUND D
- [SDR SWAA2025102828365](https://openairdocs.org/sdr/SWAA2025102828365.md): Girt Bar · jammed · Oct 24, 2025 · N217JC · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR GIRT BAR JAMMED. FREED THE GIRT BAR FROM SLIDE COVER RETAINER IAW MM 25-66-02, OPS NORMAL.
- [SDR SWAA2025090511358](https://openairdocs.org/sdr/SWAA2025090511358.md): Lens · detached · Sep 4, 2025 · N217JC · Boeing 7377H4 · Emergency Lighting
  > ROW 11F SIDEWALL LIGHT LENS FELL OFF. ATTACHED ROW 11F SIDEWALL LIGHT LENS IAW AMM 33-51-00
- [SDR SWAA2025072992996](https://openairdocs.org/sdr/SWAA2025072992996.md): Hinge · cracked · Jul 19, 2025 · N217JC · Boeing 7377H4 · Fuselage, Door Hinge
  > WATER SERVICE DOOR; AFT HINGE CRACKED. REMOVED AND REPLACED WATER SERVICE DOOR; AFT HINGE IAW SRM 51-40-02-0G-0 AND IPC 52-49-00-02.
- [SDR SWAA2025071690904](https://openairdocs.org/sdr/SWAA2025071690904.md): Girt Bar · out of adjust · Jul 13, 2025 · N217JC · Boeing 7377H4 · Emergency Equipment
  > CHECK R1 GIRT BAR PROPER FUNCTION FA REPORTS LOOSE IN HOLDER. REPAIRED PER [UNLISTED MANUAL NOT LISTED (NO REFERENCE FOUND)] TIGHTENED GIRT BAR HOLDING BRACKET IAW SIP.
- [SDR SWAA2025070788698](https://openairdocs.org/sdr/SWAA2025070788698.md): Slide · out of limits · Jul 6, 2025 · N217JC · Boeing 7377H4 · Escape Slide
  > AFTER SERVICE. DOOR SLIDE IS INDICATING IN RED. REMOVED AND REPLACED SLIDE ASSY PER M/M 25-66-01 AND MT 725-61-06.
- [SDR SWAA2025032406906](https://openairdocs.org/sdr/SWAA2025032406906.md): Handle · loose · Mar 19, 2025 · N217JC · Boeing 7377H4 · Passenger/Crew Doors
  > PAX CABIN FWD ENTRY DOOR INTERNAL HANDLE WITH LOOSE PLATE 2025-137106 <[01]. INSTALLED CORRECTLY PAX CABIN FWD ENTRY DOOR INTERNAL HANDLE PLATE IAW B737-700 AMM 52-11-31-400-802 STEP 3.G.(4) (D); [02] INSTALLED CORRECTLY PAX CABIN FWD ENTRY DOOR INTERNAL HANDL
- [SDR SWAA2025032404186](https://openairdocs.org/sdr/SWAA2025032404186.md): Slat Track · corroded · Mar 11, 2025 · N217JC · Boeing 7377H4 · Leading Edge Slat Control System
  > CORROSION ON SLAT 5 OUTBOARD MAIN TRACK ON UPPER ROLLER SURFACE AT RT WING 2025-137044 <[01]. REPLACED LEADING EDGE SLAT 5 OUTBOARD MAIN TRACK IAW B737-700 AMM 27-81-21-000-802 AND AMM 27-81-21-400-802; FOR SLATS ACTIVATION; ADJUSMENTS AND TESTS THE STEPS ARE
- [SDR SWAA2025032198532](https://openairdocs.org/sdr/SWAA2025032198532.md): Slat · cracked · Feb 22, 2025 · N217JC · Boeing 7377H4 · Trailing Edge Flap Control System
  > REPLACE SLAT 5 DUE TO CRACK ON FITTING WAS FOUND AT RT WING 2025-137023<[01] REPLACED SLAT 5 IAW B737-700 AMM 27-81-21-401-NG<BR>SEE INDIVIDUAL SIGN OFF BELLOW;[02] CORRECTED STEP 1:<BR>REPLACED SLAT 5 IAW B737-700 AMM 27-81-21-401-NG; SLAT ADJUSTMENT AND OPER
- [SDR SWAA2025032498190](https://openairdocs.org/sdr/SWAA2025032498190.md): Support Bracket · damaged · Feb 20, 2025 · N217JC · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ELONGATED HOLES ON SUPPORT BRACKETS OF BRACE SUPPORT AT RT MLG WHEEL WELL RING 2025-136995<[01] REPLACED SUPPORT BRACKETS OF BRACE SUPPORT AT RT MLG WHEEL WELL RING IAW B737-700 SRM:51-40-02 AND DWG:149A7502 SHEET 168 REV. A. SEE INDIVIDUAL SIGN OFF BELOW.;[02
- [SDR SWAA2025032497763](https://openairdocs.org/sdr/SWAA2025032497763.md): Support Bracket · cracked · Feb 19, 2025 · N217JC · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET ON BULKHEAD BS 727 AT LEVEL STRINGER 27R AFT CARGO COMPARTMENT 2025-136984 <[01]. REPLACED SUPPORT BRACKET ON BULKHEAD BS 727 AT LEVEL STRINGER 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 144A2600 REV -: SEE IN
- [SDR SWAA2025032497125](https://openairdocs.org/sdr/SWAA2025032497125.md): Gusset · cracked · Feb 17, 2025 · N217JC · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2025-136939 <[01]. REPLACED NEW GUSSET AND FASTENERS LOCATED ON BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 143A7902 SHEET:174 REV:-. SEE INDIVIDUAL SIGN-OFF B
- [SDR SWAA2025032497128](https://openairdocs.org/sdr/SWAA2025032497128.md): Light · broken · Feb 17, 2025 · N217JC · Boeing 7377H4 · Emergency Lighting
  > BROKEN HOUSING ASSY EMERGENCY LIGHT OVERHEAD BIN BULLNOSE ROW 6 DEF AND 14 DEF 2025-136949 <[01]. REPLACED HOUSING ASSY EMERGENCY LIGHT OVERHEAD BIN BULLNOSE ROW 6 DEF AND 14 DEF IAW B737-700 AMM 33-51-03-960-802. AND OPERATIONAL TEST IAW TTG8Q004Z05 STEP 83;
- [SDR SWAA2025032497124](https://openairdocs.org/sdr/SWAA2025032497124.md): Angle · cracked · Feb 17, 2025 · N217JC · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK ON ANGLE LOCATED BS663 UPPER POSITION RBL39 AT CENTER WING BOX 2025-136945 <[01]. TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; [02] REPLACED ANGLE LOCATED BS663 UPPER POSITION BTW RBL5 TO RBL70 AT CENTER WI
- [SDR SWAA2025032497118](https://openairdocs.org/sdr/SWAA2025032497118.md): Support Angle · cracked · Feb 17, 2025 · N217JC · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS500D STR28R AFT POSITION FWD CARGO COMPARTMENT 2025-136936 <[01]. REPLACED ANGLE-SUPPORT LOCATED BS500D STR28R AFT POSITION FWD CARGO COMPARTMENT IAW B737-700 SRM:51-40-02 AND DWG 143A7902 SHET 126 REV A. SEE INDIVIDUAL SIGN OF
- [SDR SWAA2025032497123](https://openairdocs.org/sdr/SWAA2025032497123.md): Gusset · cracked · Feb 17, 2025 · N217JC · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON GUSSET LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT 2025-136940 <[01]. REPLACED GUSSET LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-40-02-0G-0 AND DWG 143A7902 SHEET:174 REV:-SEE INDIVIDUAL SIGNS OFF BELOW; [02]
- [SDR SWAA2025032497126](https://openairdocs.org/sdr/SWAA2025032497126.md): Gusset · cracked · Feb 17, 2025 · N217JC · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2025-136938 <[01]. REPLACED GUSSET AND FASTENERS LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM:51-40-02 AND DWG:143A7902 SHEET:174 REV:- SEE INDIVIDUAL SIGN OF BELOW; [02] TASK
- [SDR SWAA2025032497120](https://openairdocs.org/sdr/SWAA2025032497120.md): Stringer · cracked · Feb 17, 2025 · N217JC · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK ON STRINGER 25L LOCATED BTW BS520 TO BS540 AT FWD CARGO COMPARTMENT 2025-136937<[01] ON STEP 2: TOOL USED ULTRASONIC EQUIPMENT PN: 45MG; SN: 221859911; DUE DATE: 19 DEC 25;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE D
- [SDR SWAA2025032497127](https://openairdocs.org/sdr/SWAA2025032497127.md): Skin · cracked · Feb 17, 2025 · N217JC · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 9.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.845 INCHES. 2025-136952<[01] TOOL USED ON STEP 4 AND 5 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE
- [SDR SWAA2025032497121](https://openairdocs.org/sdr/SWAA2025032497121.md): Access Panel · cracked · Feb 17, 2025 · N217JC · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK ACCESS PANEL 667BT OB FOREFLAP AT RT WING 2025-136944<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26.;[02] REPLACED RH WING ACCESS PANEL 667BT OB MAIN FLAP IAW EA-25-157-00562 WIP1; EA-25-157-00562 WIP2;
- [SDR SWAA2025032097122](https://openairdocs.org/sdr/SWAA2025032097122.md): Tie Clip · cracked · Feb 17, 2025 · N217JC · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON TIE CLIP LOCATED BS500C AND STR19L AT FWD CARGO COMPARTMENT 2025-136941 <[01]. REPLACED TIE CLIP LOCATED BS500C AND STR19L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 143A1224 SHEET 49 REV? SEE INDIVIDUAL SIGN OFF BELOW.; [02] TAS
- [SDR SWAA2025031997117](https://openairdocs.org/sdr/SWAA2025031997117.md): Intercostal · cracked · Feb 17, 2025 · N217JC · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BTW BS500D TO BS520 STR28L FWD CARGO COMPARTMENT 2025-136935 <[01]. REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED BTW BS500D TO BS520 STRG28L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902; SHEET 126; REV A.
- [SDR SWAA2025032496586](https://openairdocs.org/sdr/SWAA2025032496586.md): Lens · broken · Feb 16, 2025 · N217JC · Boeing 7377H4 · Emergency Lighting
  > BROKEN EMERGENCY EXIT LIGHT LENS LAVATORY A AT FWD GALLEY AREA (1 EA) 2025-136886 <[01]. REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY A AT FWD GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-801; STEP 2.C.(4).; [02] TASK COMPLETED.
- [SDR SWAA2025032496597](https://openairdocs.org/sdr/SWAA2025032496597.md): Lens · broken · Feb 16, 2025 · N217JC · Boeing 7377H4 · Emergency Lighting
  > BROKEN EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) 2025-136900<[01] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) IAW B737-700 SOPM 20-50-01 REV 38; [02] CERTIFIED WORK PERFORMED.
- [SDR SWAA2025032496584](https://openairdocs.org/sdr/SWAA2025032496584.md): Light · broken · Feb 15, 2025 · N217JC · Boeing 7377H4 · Emergency Lighting
  > BROKEN FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA) 2025-136877 <[01]. REPLACED FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802; [02] REPLACED FLOOR PROXIMITY LIGHTING P
- [SDR SWAA2025032496581](https://openairdocs.org/sdr/SWAA2025032496581.md): Rib · cracked · Feb 15, 2025 · N217JC · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK FRONT SPAR INSPAR RIB 4 AT RT HORIZONTAL STABILIZER 2025-136863<[01] TOOL USED ON STEP 3: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 05-AUG-25.;[02] TOOL USED ON STEP 4: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 05-AUG-25
- [SDR SWAA2025032496430](https://openairdocs.org/sdr/SWAA2025032496430.md): Rib · cracked · Feb 15, 2025 · N217JC · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK RIB ON ACCESS PANEL 331B LEADING EDGE STA 105.26 LT HORIZONTAL STAB 2025-136851<[01] REPLACED RIB LOCATED ON ACCESS PANEL 331B LEADING EDGE STA 105.26 LT HORIZONTAL STAB IAW B737-700 SRM 51-40-02; DWG 186A1304; SHEET: 1; REV:-. AND DWG 1810A1001; SHEET:
- [SDR SWAA2025032496433](https://openairdocs.org/sdr/SWAA2025032496433.md): Rib · cracked · Feb 15, 2025 · N217JC · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK RIB ON ACCESS PANEL 341B LE STA95.96 AT RT HORIZONTAL STABILIZER 2025-136853 <[01]. REPLACED RIB ON ACCESS PANEL 341B LE STA95.96 AT RT HORIZONTAL STABILIZER IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING# 186A1001 REV:A; SEE INDIVIDUAL SIGNOFF BELOW.; [02
- [SDR SWAA2025032496208](https://openairdocs.org/sdr/SWAA2025032496208.md): Support Angle · cracked · Feb 14, 2025 · N217JC · Boeing 7377H4 · Aerodynamic Fairings
  > CRACK ON SUPPORT ANGLE FWD BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19R LOWER FUSELAGE 2025-136785<[01] REPLACED SUPPORT ANGLE LOCATED AT FWD BODY FAIRING STRUCTURE BS 500D BETWEEN STRINGER 19R AND STRINGER 20 LOWER FUSELAGE IAW B737-700 SRM 51-40-02;
- [SDR SWAA2025032495999](https://openairdocs.org/sdr/SWAA2025032495999.md): Fairing · damaged · Feb 13, 2025 · N217JC · Boeing 7377H4 · Trailing Edge Flaps
  > ELONGATED HOLE ACCESS PANEL 544CL FLAP SUPPORT FAIRING 1 AT LT WING 2025-136774<[01] REPLACED ACCESS PANEL 544CL FLAP SUPPORT FAIRING 1 AT LT WING I.A.W. B737-800 AMM 27-51-28-400-802 STEP 5.H. (4). THE INSTALLATION IS DOCUMENTED ON TTG8Q00Y0Q6F;[02] CERTIFIED
- [SDR SWAA2025032495332](https://openairdocs.org/sdr/SWAA2025032495332.md): Pressure Deck · cracked · Feb 12, 2025 · N217JC · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK ON HORIZONTAL PRESSURE DECK WEB BS 665 AND LBL 33 AT CENTER SECTION 2025-136659 <[01]. TOOL USED ON STEP 5 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 60009161631 DUE DATE: 11-MAR-25; [02] REPAIRED HORIZONTAL PRESSURE DECK WEB BS 663 TO BS 675 AND LBL 24
- [SDR SWAA2025032495545](https://openairdocs.org/sdr/SWAA2025032495545.md): Frame · cracked · Feb 12, 2025 · N217JC · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON FRAME BS 259.5 BETWEEN STRINGER 8R AND STRINGER 9R AT PASSENGER CABIN 2025-136683 <[01]. TOOL USED ON STEP 4 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 60009161631 DUE DATE: 11-MAR-25; [02] REPAIRED FRAME - WEB AT BSTA 259.5 - BTW WL 240 & WL 280 AN
- [SDR SWAA2025032495546](https://openairdocs.org/sdr/SWAA2025032495546.md): Frame · cracked · Feb 12, 2025 · N217JC · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME BS 259.5 BETWEEN STRINGER 8L TO STRINGER 9L AT PASSENGER CABIN 2025-136687 <[01].TOOL USED ON STEP 4 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25; [02] REPAIRED FRAME - WEB AT BSTA 259.5 - BTW WL 240 & WL 280 AND BTW L
- [SDR SWAA2025032495330](https://openairdocs.org/sdr/SWAA2025032495330.md): Floorbeam · cracked · Feb 12, 2025 · N217JC · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN 2025-136657<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN. IAW B737-700 SRM 51-40-02-0G AND DWG NO: 143A0060 SHEET:
- [SDR SWAA2025032495331](https://openairdocs.org/sdr/SWAA2025032495331.md): Panel · cracked · Feb 12, 2025 · N217JC · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN 2025-136658<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN. IAW B737-700 SRM 51-40-02 AND DWG NO: 143A
- [SDR SWAA2025032495333](https://openairdocs.org/sdr/SWAA2025032495333.md): Floorbeam · cracked · Feb 12, 2025 · N217JC · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK ON LOWER ANGLE FLOOR STRUCTURE BS 695 AND LBL 24.75 AT CENTER SECTION 2025-136665<[01] REPLACED ANGLE FLOOR STRUCTURE BS 695 AND LBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-40-02 AND DWG:111A6000;SHEET:244;REV:-;AND DWG:273A9110;SHEET:6;REV:A. SEE IN
- [SDR SWAA2025032495547](https://openairdocs.org/sdr/SWAA2025032495547.md): Support Angle · cracked · Feb 12, 2025 · N217JC · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE BS 294.5 AND STRINGER 13L AT PASSENGER CABIN 2025-136699<[01] REPLACED SUPPORT ANGLE BS 294.5 AND STRINGER 13L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1311 SHEET 1 REV: C. SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED CO
- [SDR SWAA2025032408753](https://openairdocs.org/sdr/SWAA2025032408753.md): Stringer · cracked · Feb 12, 2025 · N217JC · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK ON SUPPORT ANGLE BS 294.5 AND STRINGER 13L AT PASSENGER CABIN 2025-136699<[01] REPLACED SUPPORT ANGLE BS 294.5 AND STRINGER 13L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1311 SHEET 1 REV: C. SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED CO
- [SDR SWAA2025032494666](https://openairdocs.org/sdr/SWAA2025032494666.md): Skin · cracked · Feb 10, 2025 · N217JC · Boeing 7377H4 · Leading Edge Devices
  > CRACK LEADING EDGE SLAT NOSE LOWER SKIN LOCATED SLAT 5 STATION 85.19 AT RT WING. 2025-136590<[01] TOOL USED P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 14-APR-25.;[02] RESOLVED ON OTHER FAULT:TTG8Q00YVYMD;[03] CORRECTED STEP 2: SLAT WILL BE REPLACED ON T
- [SDR SWAA2024082729375](https://openairdocs.org/sdr/SWAA2024082729375.md): Battery Pack · no test · Aug 23, 2024 · N217JC · Boeing 7377H4 · Emergency Lighting
  > EMX BATT PACK M01675 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATT PACK M01675 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
- [SDR SWAA2023121330545](https://openairdocs.org/sdr/SWAA2023121330545.md): Girt Bar · out of adjust · Dec 11, 2023 · N217JC · Boeing 7377H4 · Emergency Equipment
  > FWD GALLEY SERVICE DOOR GIRT BAR WILL NOT SECURE IN THE UNARMED POSITION<[01] ADJUSTED HOOKS THAT HOLD THE FWD GALLEY SERVICE DOOR GRIT BAR AS PER AMM 25-66-02.
- [SDR SWAA2023112724596](https://openairdocs.org/sdr/SWAA2023112724596.md): Girt Bar · out of adjust · Nov 22, 2023 · N217JC · Boeing 7377H4 · Emergency Equipment
  > FORWARD SERVICE DOOR GIRT BAR WILL NOT STOW.<[01] RE-ALIGN GIRT BAR PER AMM 25-66-01 ON FWD SERVICE DOOR.
- [SDR SWAA2023110317240](https://openairdocs.org/sdr/SWAA2023110317240.md): Slide · out of limits · Nov 2, 2023 · N217JC · Boeing 7377H4 · Escape Slide
  > AFT SVC EVAC. SLIDE IS OVER PRESSURE.<[01] REMOVED AND REPLACED AFT SVC SLIDE PER AMM 25-66-01 AND MT 725-61-01. E34824
- [SDR SWAA2023090898240](https://openairdocs.org/sdr/SWAA2023090898240.md): Nut · broken · Sep 7, 2023 · N217JC · Boeing 7377H4 · Service Doors
  > FWD SERVICE DOOR ASSIST HANDLE BROKEN.<[01] REPLACED FWD SERVICE DOOR ASSIST HANDLE NUT IAW AMM 52-11-31.<BR>WORK PERFORMED BY E20763.

Next page: https://openairdocs.org/aircraft/N217JC/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N217JC' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N217JC/reports

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