# Service difficulty reports: N717JL

A list on [N717JL](https://openairdocs.org/aircraft/N717JL.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 5 · 207 reports

- [SDR DALA2026091805208](https://openairdocs.org/sdr/DALA2026091805208.md): Skin · cracked · Sep 18, 2026 · N717JL · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON SKIN AT STA Y=1076 AND LONG 14R OF AFT EXTERNAL FUSELAGE, COMPLIED WITH ER/A 635946-14TR. (1819140) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805206](https://openairdocs.org/sdr/DALA2026091805206.md): Skin · cracked · Sep 18, 2026 · N717JL · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON SKIN AT STA Y=1076 AND LONG 14R OF AFT EXTERNAL FUSELAGE, COMPLIED WITH ER/A 635946-14TR. (1818917) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805207](https://openairdocs.org/sdr/DALA2026091805207.md): Scuff Plate · cracked · Sep 17, 2026 · N717JL · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS ON AFT CARGO COMP DOOR JAMB SCUFF PLATE, COMPLIED WITH ER/A 542149-14TR. (1818676) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805205](https://openairdocs.org/sdr/DALA2026091805205.md): Skin · cracked · Sep 17, 2026 · N717JL · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > CRACK WAS FOUND AFFECTING A BUSHING INSTALLED IN THE VERTICAL STABILIZER LEADING EDGE SKIN REPAIR DOUBLER INSTALLATION LOCATED BETWEEN ZFS= 44 AND ZFS=52, HOLE #65, COMPLIED WITH ER/A 620945-14AD. (1817838) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805204](https://openairdocs.org/sdr/DALA2026091805204.md): Frame · cracked · Sep 16, 2026 · N717JL · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1200, REPAIRED FRAME PER B717-200 SRM 53-30-08-2R. (1816798) (AIRCRAFT GROUNDED).
- [SDR DALA2026092305314](https://openairdocs.org/sdr/DALA2026092305314.md): Skin · cracked · Sep 15, 2026 · N717JL · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND CRACK AT FUSELAGE RIGHT SKIN Y=1076, BETWEEN LONGERON 13R AND 14R, COMPLIED WITH ER/A 636937-14. (1816724) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805203](https://openairdocs.org/sdr/DALA2026091805203.md): Lanyard · damaged · Sep 15, 2026 · N717JL · Boeing 717200 · Passenger/Crew Doors
  > BROKEN STRANDS ON LANYARD ASSEMBLIES OF RT AND LT, R & R STRANDS IAW AMDS 5211-4002. (1814626) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805202](https://openairdocs.org/sdr/DALA2026091805202.md): Pin · damaged · Sep 15, 2026 · N717JL · Boeing 717200 · Escape Slide
  > PASSENGER DOOR EVACUATION SLIDE ARRIVED WITH VALVE RELEASE CABLE PINS NOT INSTALLED ON PARACHUTE CONE, EVACUATION SLIDE WITH TORN NYLON PARACHUTE PIN, R & R NYLON PARACHUTE AND INSTALLED PINS PER AMDS 2561-9004. (1814619) (AIRCRAFT GROUNDED).
- [SDR DALA2026070703949](https://openairdocs.org/sdr/DALA2026070703949.md): Relay · faulted · Jun 19, 2026 · N717JL · Boeing 717200 · Cabin Pressure Control System
  > ATB- DUE TO THE AIRCRAFT NOT PRESSURIZING WITH AN ASSOCIATED -ALL PACKS OFF- MESSAGE. REPLACED R2-5104 PACK SHUTDOWN/AUTO OFF RELAY AND PERFORMED VERIFICATION FLIGHT. OPS CHECK GOOD.(8318756)(AIRCRAFT GROUNDED)
- [SDR DALA2026030201423](https://openairdocs.org/sdr/DALA2026030201423.md): Skin · damaged · Feb 25, 2026 · N717JL · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / STA 229.00 AND STA 256.00, BETWEEN L-15R & L-16R / LIGHTNING STRIKES. REPAIRED PER ER/A 619580-14AD. (1467470)
- [SDR DALA2026012700604](https://openairdocs.org/sdr/DALA2026012700604.md): Skin · cracked · Jan 22, 2026 · N717JL · Boeing 717200 · Fuselage Main, Plate/Skin
  > REFERENCE ER/A 619241-14. FUSELAGE SKIN, BS 1037, L13 - 14L CRACKED. REPAIRED IAW ER/A 14-619241. (1414757)
- [SDR DALA2025110708146](https://openairdocs.org/sdr/DALA2025110708146.md): Sign · detached · Nov 3, 2025 · N717JL · Boeing 717200 · Emergency Lighting
  > SHIP 9550 FA REPORTS EXIT SIGN AT FWD FIRST CLASS CABIN DETACHED. CORRECTIVE ACTION: RESECURED HARDWARE ON EXIT SIGN. (7585210)
- [SDR DALA2025110708143](https://openairdocs.org/sdr/DALA2025110708143.md): Sign · detached · Nov 2, 2025 · N717JL · Boeing 717200 · Emergency Lighting
  > SHIP 9550 SIGN IN FIRST CLASS CABIN DETACHED FROM CEILING. CORRECTIVE ACTION: RE-ATTACHED EXIT SIGN AS REQUIRED. A/C OK FOR SVC (7585208)
- [SDR DALA2025010700132](https://openairdocs.org/sdr/DALA2025010700132.md): Light · arced · Jan 3, 2025 · N717JL · Boeing 717200 · Flight Compartment Lighting
  > LIGHT PRODUCES AN ELECTRICAL ARC WHEN THE ATTACHMENT BOLT TOUCHES THE SCREW NEXT TO THE LIGHT ATTACHMENT SOCKET. MAINTENANCE REPLACED THE F/O LIGHT ASSEMBLY PER B717 AMM 33-16. THE OPERATIONAL CHECK WAS GOOD AND THERE WAS NO LONGER ANY ARCHING. (LP #6555658)
- [SDR DALA2024120311397](https://openairdocs.org/sdr/DALA2024120311397.md): Transducer · shorted · Nov 28, 2024 · N717JL · Boeing 717200 · Stall Warning System
  > SHIP 9550 -ATB/DE- THE FLIGHT CREW RETURNED THE AIRCRAFT TO CAE AND DECLARED AN EMERGENCY DUE TO "STICK PUSHER FAIL" MESSAGE WITH AN ASSOCIATED STALL WARNING LIGHT. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE CAPTAINS CONTROL WHEEL FORCE TRANSDUCER (T2-6080)
- [SDR DALA2024112611224](https://openairdocs.org/sdr/DALA2024112611224.md): Bulkhead · cracked · Nov 6, 2024 · N717JL · Boeing 717200 · Fuselage Main, Bulkhead
  > -AD- ACCOMPLISH ER/A 619268-14AD REV A SECTION II - FUSELAGE MAIN FRAME BULKHEADS AT FS 1178, X=10 X=0.0. AFT WEB CRACKED & ELONGATED HOLE. ACCOMPLISH ER/A 619268-14AD REV A SECTION II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED.
- [SDR DALA2024101810189](https://openairdocs.org/sdr/DALA2024101810189.md): Bushing · cracked · Oct 17, 2024 · N717JL · Boeing 717200 · Vertical Stabilizer
  > CRACK ON BUSHING WAS FOUND, PREVIOUSLY TO INSTALL NEW LOWER BRACKET ON LEADING EDGE AT VERTICAL STABILIZER. SUMMARY OF NRC 00927: CRACK ON BUSHING OF VERTICAL STABILIZER L.E. ZFS=46.300 TO ZFS=52.267 WAS REPAIRED PER ER/A 620945-14 REV ORIGINAL SECTION I: PERM
- [SDR DALA2024100209619](https://openairdocs.org/sdr/DALA2024100209619.md): Vane · dented · Sep 29, 2024 · N717JL · Boeing 717200 · Trailing Edge Flaps
  > DENTS ON LH WING INBOARD FIXED FLAP VANE INTRADOS BETWEEN XV1=119 AND XV1=119+11, XV1=211-24, XV1=211-26. SUMMARY OF NRC 00172: DENTS (16 EA) ON LH WING INBOARD FIXED FLAP VANE INTRADOS BETWEEN XV1=119 AND XV1=119+11, XV1=211-24, AND XV1=211-26 WERE EVALUATED
- [SDR DALA2024091108922](https://openairdocs.org/sdr/DALA2024091108922.md): Pan · cracked · Sep 11, 2024 · N717JL · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INNER PAN FWD SIDE OF BEAM #4 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00422: INNER PAN FWD SIDE OF BEAM #4 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 619283-14, REV ORIGINAL, SECTION I, PERMANENT REPAIR. (LP #0550050)
- [SDR DALA2024090608755](https://openairdocs.org/sdr/DALA2024090608755.md): Cable · broken · Sep 5, 2024 · N717JL · Boeing 717200 · Aerodynamic Fairings
  > MAINTENANCE FOUND A BROKEN KEVLAR CABLE AT THE TAIL CONE SLIDE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00917: THE KEVLAR CABLE AT TAIL CONE SLIDE WAS REPLACED PER B717 AMM
- [SDR DALA2024090408734](https://openairdocs.org/sdr/DALA2024090408734.md): Hinge Fitting · corroded · Sep 3, 2024 · N717JL · Boeing 717200 · Trailing Edge Flaps
  > WEAR AND CORROSION ON HOLES OF LH FLAP HINGE FITTING #3. SUMMARY OF NRC 0885: CORROSION LEVEL 2. LH FLAP HINGE FITTING #3 WAS REPLACED BY A SERVICEABLE PER B717 AMM 57-55-25. (LP #0537751)
- [SDR DALA2024090408732](https://openairdocs.org/sdr/DALA2024090408732.md): Control System · out of adjust · Aug 31, 2024 · N717JL · Boeing 717200 · Stabilizer Control System
  > -AD- AMDS 2740-01114-07 STEP 6: DUE RESULT OF THE STEP 6A "ADJUST THE HORIZONTAL STABILIZER TRIM SYSTEM AND SHUTOFF CONTROL SYSTEM AMM 27-40-00 820-801. SUMMARY NRC 00298: HORIZONTAL STABILIZER TRIM SYSTEM AND SHUTOFF CONTROL SYSTEM WAS ADJUSTED PER B717-200 A
- [SDR DALA2024083008599](https://openairdocs.org/sdr/DALA2024083008599.md): Hinge Fitting · corroded · Aug 29, 2024 · N717JL · Boeing 717200 · Trailing Edge Flaps
  > CORROSION WAS FOUND ON THE LH FLAP INBOARD HINGE FITTING FASTENER HOLES (8 ATTACH POINT) IN REF NRC 258. SUMMARY OF NRC 00861: LEVEL CORROSION 2. LH FLAP INBOARD HINGE FITTING WAS REPLACED PER B717 AMM 57-55-25. (LP #0528717)
- [SDR DALA2024083008596](https://openairdocs.org/sdr/DALA2024083008596.md): Cap · cracked · Aug 28, 2024 · N717JL · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON UPPER CAP STA Y=1022 AND LONGERON #7 LH AT CABIN PAX. SUMMARY OF NRC 000367: UPPER CAP STA Y=1022 AND LONGERON #7 LH AT CABIN PAX WAS REPAIRED PER PRI 619642-14 REV 1 AND ER/A 619642-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-6196
- [SDR DALA2024083008594](https://openairdocs.org/sdr/DALA2024083008594.md): Barrel Nut · corroded · Aug 28, 2024 · N717JL · Boeing 717200 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION ON THE BARREL NUT HOLES #26, #27, #28, AND #30, STA HX 6.625 RIGHT, STABILIZER CENTER BOX. SUMMARY OF NRC 00407: BARREL NUT HOLES #26, #27, #28, AND #30, STA HX 6.625 RIGHT, STABILIZER CENTER BOX WERE REPAIRED PER ER/A 619552-14 REV ORIGINAL. ASSOCIA
- [SDR DALA2024082708491](https://openairdocs.org/sdr/DALA2024082708491.md): Door Frame · corroded · Aug 27, 2024 · N717JL · Boeing 717200 · Fuselage Main, Structure
  > AIRCRAFT 9550, CORROSION ON DOOR JAMB E/E STA Y=133 BTW LONG 29 RH TO 29 LH ALSO ON STA Y=160 FOUND PREVIUOS HOLE PLUGGED LIKE REPAIR AND NO DECAL FOUND. CORRECTIVE ACTION: CORROSION LEVEL 2 // DOOR JAMB E/E STA Y=133 BTW LONG 29 RH TO 29 LH ALSO ON STA Y=160
- [SDR DALA2024082308412](https://openairdocs.org/sdr/DALA2024082308412.md): Skin · damaged · Aug 22, 2024 · N717JL · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT 9550, LIGHTNING STRIKES ON SKIN STA Y=256, 229 AND BTW RH LONGERONS 15/16 AT EXTERNAL FUSELAGE. CORRECTIVE ACTION: SKIN STA Y=256, 229 AND BTW RH LONGERONS 15/16 AT EXTERNAL FUSELAGE WAS REPAIRED PER. PRI 619580-14 REV. 4 AND ER/A 619580-14AD REV. ORI
- [SDR DALA2024082208362](https://openairdocs.org/sdr/DALA2024082208362.md): Pan · cracked · Aug 21, 2024 · N717JL · Boeing 717200 · Fuselage Miscellaneous Structure
  > AIRCRAFT 9550, INITIAL INSPECTION: CRACK ON INNER PAN AFT SIDE ON BEAM NBR 3, NBR 4 AND NBR 5 AT AFT CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: INNER PAN AFT SIDE ON BEAM NBR 3, NBR 4 AND NBR 5 AT AFT CARGO COMPARTMENT DOOR. WAS REPAIRED PER PRI 619298-14 REV.
- [SDR DALA2024082208358](https://openairdocs.org/sdr/DALA2024082208358.md): Pan · cracked · Aug 21, 2024 · N717JL · Boeing 717200 · Fuselage Miscellaneous Structure
  > AIRCRAFT 9550, CRACK INNER PAN NEAR TO AFT STOP FITTING AND BEAM NBR 01. CORRECTIVE ACTION: INNER PAN NEAR TO AFT STOP FITTING AND BEAM NBR 01. WAS REPAIRED PER PRI 619304-14 REV. 3 AND ERA 619304-14 REV ORIGINAL SECTION I PERMANENT REPAIR ASSOCIATED ER/A 14-6
- [SDR DALA2024082008300](https://openairdocs.org/sdr/DALA2024082008300.md): Angle · cracked · Aug 20, 2024 · N717JL · Boeing 717200 · Fuselage Miscellaneous Structure
  > AIRCRAFT 9550, INITIAL INSPECTION: CRACKS ON ANGLE OF CANTED KEEL STRUCTURE ON STA Y=716 AND PROJECT LONG 27L AT LOWER CTR FUSELAGE. CORRECTIVE ACTION: ANGLE OF CANTED KEEL STRUCTURE ON STA Y=716 AND PROJECT LONG 27L AT LOWER CTR FUSELAGE WAS REPAIRED PER PRI
- [SDR DALA2024081908242](https://openairdocs.org/sdr/DALA2024081908242.md): Nut · corroded · Aug 17, 2024 · N717JL · Boeing 717200 · Horizontal Stabilizer, Spar/Rib
  > CORROSION ON NUTS INSIDE HOLES #26, #27, #28, AND #30 STA HX 6.625 RIGHT STABILIZER CENTER BOX. SUMMARY OF NRC 00494: NUTS INSIDE HOLES #26, #27, #28, AND #30 STA HX 6.625 RIGHT STABILIZER CENTER BOX WERE REPAIRED PER ER/A 619552-14 PRI REV 1. ASSOCIATED ER/A
- [SDR DALA2024081608212](https://openairdocs.org/sdr/DALA2024081608212.md): Frame · cracked · Aug 16, 2024 · N717JL · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON WEB AND CRACK ON FRAME OF AFT ACCESSORY COMPARTMENT FROM STA 1178 CANT BTW LONG 1 TO LONG 3RH TO 3LH, APPROXIMATELY. SUMMARY OF NRC 00219: WEB AND FRAME OF AFT ACCESSORY COMPARTMENT FROM STA 1178 CANT BTW LONG 1 TO LONG 3RH TO 3LH WERE REPAIRED PER PR
- [SDR DALA2024081508166](https://openairdocs.org/sdr/DALA2024081508166.md): Frame · corroded · Aug 14, 2024 · N717JL · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME STA Y=1022 BTW LONGERON 28R/L30 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00833; CORROSION LEVEL 2. CORROSION ON FRAME STA Y=1022 BTW LONGERON 28R/L30 AT AFT CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 3, PAR 5, FIGURE 20
- [SDR DALA2024081408112](https://openairdocs.org/sdr/DALA2024081408112.md): Window Frame · cracked · Aug 13, 2024 · N717JL · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON LH WINDOW FRAME (RETAINER POLISHED). SUMMARY OF NRC 00623: LH WINDOW FRAME WAS REPAIRED PER PRI 619398-14 REV 2 AND PER ER/A 619398-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-619398.
- [SDR DALA2024081308067](https://openairdocs.org/sdr/DALA2024081308067.md): Skin · corroded · Aug 13, 2024 · N717JL · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON SKIN UPPER EDGE OF LH AND RH WING REAR SPAR BTW XCW=0 TO XW=60 (THROUGH LH AND RH MLG (SPECIFICALLY XCW=30)). SUMMARY OF NRC 00169: CORROSION LEVEL 2. CORROSION ON SKIN UPPER EDGE OF LH AND RH WING REAR SPAR BTW XCW=0 TO XW=60 WAS REPAIRED PER PRI
- [SDR DALA2024081308066](https://openairdocs.org/sdr/DALA2024081308066.md): Beam · cracked · Aug 12, 2024 · N717JL · Boeing 717200 · Fuselage Main, Structure
  > CRACKS ON BEAM #6 BTW STA 180-196 AT FWD PASSENGER DOOR. SUMMARY OF NRC 00117: BEAM #6 ON STA 196 AT FWD PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 12 PAR 4 FIGURE 201. AND (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON BEAM #6 ON STA 180 A
- [SDR DALA2024080907920](https://openairdocs.org/sdr/DALA2024080907920.md): Cap · cracked · Aug 8, 2024 · N717JL · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON UPPER CAP STA Y=1022 AND LONGERON #7 RH AT CABIN PAX. SUMMARY OF NRC 00816: UPPER CAP STA Y=1022 AND LONGERON #7 RH AT CABIN PAX WAS REPAIRED PER PRI 619643-14 REV 1 AND ER/A 619643-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-61964
- [SDR DALA2024080907919](https://openairdocs.org/sdr/DALA2024080907919.md): Stabilizer · distorted · Aug 8, 2024 · N717JL · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > THE COUNTERSINK OF THE FASTENERS HOLES OF THE VERTICAL STABILIZER LEADING EDGE WERE NOTED WORN ALL AROUND EDGES BETWEEN ZFS 52.267 TO 153.938. SUMMARY OF NRC 00748: THE LEADING EDGE OF THE VERTICAL STABILIZER IS OUT OF LIMITS, AS REPAIRABLE HOLE LIMITS PER B71
- [SDR DALA2024080807881](https://openairdocs.org/sdr/DALA2024080807881.md): Angle · corroded · Aug 7, 2024 · N717JL · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP ANGLE Y=200, Y=219-224 AT PAX CABIN (W1.) SUMMARY OF NRC 00467: CORROSION LEVEL 2. CUSP ANGLE Y=200, Y=219-224 AT PAX CABIN WAS REPAIRED PER PRI 619420-14 REV 2 AND ER/A 619420-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A
- [SDR DALA2024080707852](https://openairdocs.org/sdr/DALA2024080707852.md): Intercostal · corroded · Aug 6, 2024 · N717JL · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL 29R STA Y=1002 TO Y=1005 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00332: CORROSION LEVEL 2. INTERCOSTAL 29R STA Y=1002 TO Y=1005 AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0487811)
- [SDR DALA2024080607842](https://openairdocs.org/sdr/DALA2024080607842.md): Autobrake Sys · intermittent · Aug 6, 2024 · N717JL · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME CAP STA Y=1133 AND BTW LONG 2LH TO 3LH AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00685: FRAME CAP (STIFFENER) STA Y=1133 AND BTW LONG 2LH TO 3LH AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP
- [SDR DALA2024080607841](https://openairdocs.org/sdr/DALA2024080607841.md): Skin · cracked · Aug 6, 2024 · N717JL · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS ON FUSELAGE SKIN LH SIDE BTW LONGERON 13L-14L AND STA 1022, 1037, 1087 AT AFT FUSELAGE. SUMMARY OF NRC 00046: (ET) HFEC INSPECTION WAS ACCOMPLISHED ON FUSELAGE SKIN LH SIDE BTW LONGERON 13L-14L AND STA 1037, 1087 AT AFT FUSELAGE ON STA 1037 THREE CRACKS
- [SDR DALA2024080607840](https://openairdocs.org/sdr/DALA2024080607840.md): Wing Root · corroded · Aug 5, 2024 · N717JL · Boeing 717200 · Wing, Center Box
  > CORROSION ON LH CENTER WING UPPER SURFACE (WING BOX) BTW STGR 6-5 AND STGR 5-4 PAX CABIN. SUMMARY OF NRC 00693: CORROSION LEVEL 2. CORROSION ON LH CENTER WING UPPER SURFACE (WING BOX) BTW STGR 6-5 AND STGR 5-4 PAX CABIN WAS REPAIRED PER PRI 619399-14 REV 3 AND
- [SDR DALA2024080507763](https://openairdocs.org/sdr/DALA2024080507763.md): Skin · cracked · Aug 2, 2024 · N717JL · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS ON FUSELAGE SKIN RH SIDE BTW LONGERON 13R-14R AND STA 1116, 1144, LONGERON 7R AND STA 1022 AT AFT FUSELAGE. SUMMARY OF NRC 00047: FUSELAGE SKIN RH SIDE BTW LONGERON 13R-14R AND STA 1116, 1144, LONGERON 7R AND STA 1022 AT AFT FUSELAGE WAS REPAIRED PER PR
- [SDR DALA2024080507762](https://openairdocs.org/sdr/DALA2024080507762.md): Frame · cracked · Aug 2, 2024 · N717JL · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON MAIN FRAME STA Y=1037 LONGERON 17L AT PAX CABIN. SUMMARY OF NRC 00354: MAIN FRAME STA Y=1037 LONGERON 17L AT PAX CABIN WAS REPAIRED PER PRI 619352-14 REV 1 AND ERA 619352-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-619352 ADDED FO
- [SDR DALA2024080507761](https://openairdocs.org/sdr/DALA2024080507761.md): Longeron · cracked · Aug 2, 2024 · N717JL · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKS ON LONGERONS 3, 4, 5, 6, AND 17 LH STA Y=1022 AT CABIN PAX. SUMMARY OF NRC 00371: LONGERON 3 BTW STA Y=1012 TO STA Y=1027 LH, LONGERON 4 BTW STA Y=1011 TO STA Y=1053 LH, LONGERON 5 BTW STA Y=1012 TO STA Y=1053 LH, LONGERON 6 BTW STA Y=1013 TO STA Y=1053
- [SDR DALA2024073007625](https://openairdocs.org/sdr/DALA2024073007625.md): Frame · damaged · Jul 30, 2024 · N717JL · Boeing 717200 · Fuselage Main, Frame
  > NICKS ON FRAME STA Y=351 BTW LONGERON 17R / L18R. SUMMARY OF NRC 00711: FRAME'S STA Y=351 BTW LONGERON 17R / L18R WAS REPAIRED PER B717-200 SRM 53-00-07-2R PROCEDURE 1 REPAIR 1. (LP #0473575)
- [SDR DALA2024073007624](https://openairdocs.org/sdr/DALA2024073007624.md): Longeron · cracked · Jul 29, 2024 · N717JL · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKS ON LONGERONS 3, 4, 5, 6, AND 8 RH STA Y=1022 AT CABIN PAX. SUMMARY OF NRC 00370: LONGERONS 3, 4, 5, 6, AND 8 RH STA Y=1022 AT CABIN PAX WERE REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2 FIG.201. (LP #0473110)
- [SDR DALA2024072907540](https://openairdocs.org/sdr/DALA2024072907540.md): Cusp Web · corroded · Jul 28, 2024 · N717JL · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB BTW STA Y=579/598 AND STA X=-45 AT PAX CABIN. SUMMARY OF NRC 00453: CUSP WEB BTW STA Y=579/598 AND STA X=-45 AT PAX CABIN WAS FABRICATED PER B717 SRM 53-00-55-2R-4 AND REPLACED PER B717 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #0471
- [SDR DALA2024072907538](https://openairdocs.org/sdr/DALA2024072907538.md): Cusp Web · cracked · Jul 27, 2024 · N717JL · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK WAS FOUND AFTER REMOVED CUSP WEB BTW STA Y=218 TO STA Y=238, -X=56 TO -X=44 AT CABIN PAX. SUMMARY OF NRC 00820: CUSP WEB BTW STA Y=218 TO STA Y=238, -X=56 TO -X=44 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG 203. (LP #0468164)

Next page: https://openairdocs.org/aircraft/N717JL/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 = 'N717JL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N717JL/reports

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