# Service difficulty reports: N707EV

A list on [N707EV](https://openairdocs.org/aircraft/N707EV.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 · 227 reports

- [SDR SWIA2026050176636](https://openairdocs.org/sdr/SWIA2026050176636.md): Bulkhead Web · corroded · May 1, 2026 · N707EV · Cndair CL6002C11 · Fuselage Main, Bulkhead
  > UPON REMOVAL OF THE BS 280 CROSSBEAM LT THE COCKPIT BULKHEAD LOWER WEB HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE CROSSBEAM, THE COCKPIT BULKHEAD LOWER WEB IAW SRM 53-00-00, 51-42-06, 51-42-13, 53-11-10, 51-21-11, 51-25-06, 51-42-21, 51-25-16,, AMM 25
- [SDR SWIA2026041676633](https://openairdocs.org/sdr/SWIA2026041676633.md): Post · corroded · Apr 16, 2026 · N707EV · Cndair CL6002C11 · Fuselage Main, Structure
  > FLIGHT COMPARTMENT LT DOOR POST HAS SIGNS OF CORROSION. PERFORMED REPAIR AT FLIGHT COMPARTMENT LT DOOR POST IAW SRM 53-00-00, & 51-21-11, 51-25-06, IAW AMM 20-70-00, IAW REO 670-53-11-745 REV -A, IAW REO 670-53-11-2321 REV --.
- [SDR SWIA2026030576627](https://openairdocs.org/sdr/SWIA2026030576627.md): Door Frame · gouged · Mar 5, 2026 · N707EV · Cndair CL6002C11 · Fuselage Main, Structure
  > NLG AFT DOOR CUTOUT ON LH SIDE EDGE IS GOUGED. REMOVED, EVALUATED AND REPAIRED DAMAGE ON LT SIDE EDGE AT NLG AFT DOOR CUTOUT IAW REO 670-53-11-2318 REV -- AND SRM 53-00-00.
- [SDR SWIA2026030476630](https://openairdocs.org/sdr/SWIA2026030476630.md): Frame · fom · Mar 4, 2026 · N707EV · Cndair CL6002C11 · Standard Practices/Structures
  > FRAME AT BS 333. REQUIRES CUT OUT DUE TO MULTIPLE STRINGER REPLACEMENTS. PERFOMED REPAIR AT FRAME BS 333 IAW AMM 20-70-00, SRM 51-42-06, 51-42-13, 51-42-21, IAW REO 670-53-21-799 REV -A.
- [SDR SWIA2026022776624](https://openairdocs.org/sdr/SWIA2026022776624.md): Plate · cracked · Feb 27, 2026 · N707EV · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > AFT EQUIPMENT BAY LH PROTECTIVE PLATE ABOVE COCKPIT VOICE RECORDER IS CRACKED. REMOVED AND REPAIRED DAMAGE ON AFT EQUIPMENT BAY LT PROTECTIVE ABOVE COCKPIT VOICE RECORDER IAW REO 670-53-72-037 REV --(P1) AND SRM 51-41-02, 51-11-00, REO 670-53-72-037 REV--.
- [SDR SWIA2026012776639](https://openairdocs.org/sdr/SWIA2026012776639.md): Structure · corroded · Jan 27, 2026 · N707EV · Cndair CL6002C11 · Fuselage Main, Structure
  > RBL9 SIGNS OF CORROSION FROM BS 6770 TO 693. BLENDED OUT AND EVALUATED DAMAGE ON FLOOR SUPPORT AND BULKHEAD BEAM AT RBL9 BETWEEN F.S.677 TO 693, REWORKED CONDITION IS STRUCTURALLY ACCEPTABLE IAW SRM 51-42-10, 51-42-21, 51-41-02, 53-31-43, 53-00-41, 51-42-15 A
- [SDR SWIA2026012776637](https://openairdocs.org/sdr/SWIA2026012776637.md): Support · corroded · Jan 27, 2026 · N707EV · Cndair CL6002C11 · Fuselage Main, Structure
  > MULTIPLE NUTPLATE HOLES HAVE SIGNS OF CORROSION ON LBL9 FROM FS579.00 TO FS661. REPAIRED DAMAGE AROUND NUTPLATE HOLES ON LBL 9 FROM BS 579 TO BS 661 IAW REO 670-53-31-1199, REV-P1, REV-- 1 AND SRM 53-31-43, 51-41-02, 51-42-06, 51-42-10, AMM 53-00-49.
- [SDR SWIA2026012776634](https://openairdocs.org/sdr/SWIA2026012776634.md): Stringer · corroded · Jan 27, 2026 · N707EV · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer
  > STRINGER 19R SIGNS OF CORROSION BETWEEN BS 437 TO 453 UNDER FLOORBOARD 252CFR. REMOVED AND REPLACED STR 19R BETWEEN BS 349 TO 485 IAW SRM 53-21-03, 51-42-06, 51-42-13, 51-42-21, 51-40-11, 51-21-11, 51-25-06, 51-25-16, AMM 20-70-00 AND 21-31-00
- [SDR SWIA2026012776631](https://openairdocs.org/sdr/SWIA2026012776631.md): Stringer · corroded · Jan 27, 2026 · N707EV · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer
  > AVIONICS BAY STR 24R BETWEEN BS 333 - 364 HAS MULTIPLE SIGNS OF CORROSION. REPAIRED DAMAGE ON AVIONICS BAY STRG 24R BETWEEN FS 333 AND FS 364 IAW REO 670-53-21-2879 REV -, SRM 51-42-06, 51-21-06, 51-32-59, 53-21-03, & AMM 21-31-00.
- [SDR SWIA2026012776626](https://openairdocs.org/sdr/SWIA2026012776626.md): Floor Support · corroded · Jan 27, 2026 · N707EV · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > ON RBL9, MULTIPLE NUTPLATE HOLES HAVE SIGNS OF CORROSION FROM BS 613 TO 693. BLENDED OUT AND EVALUATED DAMAGE ON FLOOR SUPPORT AT RBL9 BETWEEN BS 613 TO 693, REWORKED CONDITION IS STRUCTURALLY ACCEPTABLE IAW SRM 51-42-10, 53-31-43, 53-00-41, 51-42-15 AND REO
- [SDR SWIA2026012276628](https://openairdocs.org/sdr/SWIA2026012276628.md): Stringer · corroded · Jan 22, 2026 · N707EV · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer
  > SIGNS OF CORROSION ON STGR 26R AT F.S.1047.0, JUST FORWARD AND TO THE RIGHT OF THE POTABLE WATER TANK. REMOVED AND REPLACED REPAIR SPLICE, REPAIR FILLER, REPAIR DOUBLER, AND INTERCOSTAL BETWEEN FS 1047 AND FS 1069 BETWEEN STRINGERS 24L AND 26R IAW SRM 53-00-0
- [SDR SWIA2026011976638](https://openairdocs.org/sdr/SWIA2026011976638.md): Stringer · corroded · Jan 19, 2026 · N707EV · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer
  > SIGNS OF CORROSION IN THE FORWARD CARGO BAY AT BS 581, STGR 22LH ON THE STRINGER FOOT. PERFORMED REPAIR IN THE FORWARD CARGO BAY AT BS 581 STGR 22L ON THE STRINGER FOOT, IAW SRM 51-42-06, SRM 53-31-03, REO 670-53-31-1210, REV - (P1), REO 670-53-31-1210, RE
- [SDR SWIA2026011976625](https://openairdocs.org/sdr/SWIA2026011976625.md): Shear Tie · corroded · Jan 19, 2026 · N707EV · Cndair CL6002C11 · Fuselage Internal Mounting Structure
  > SIGNS OF CORROSION IN THE FWD CARGO BAY AT BS 549, S26L, ON FRAME FOOT OF FRAME 549. PERFORMED REPAIR ON FWD CARGO BAY AT BS 549 ON FRAME BETWEEN STGR 26L AND STGR 26R IAW SRM 51-42-06, SRM 53-31-06, SRM 51-42-13, REO 670-53-31-1220 REV -, SRM 51-40-11, AMM
- [SDR SWIA2026011776629](https://openairdocs.org/sdr/SWIA2026011776629.md): Hinge · gouged · Jan 17, 2026 · N707EV · Cndair CL6002C11 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE HAS MULTIPLE LUGS WITH GOUGES DOWN ENTIRE LENGTH FUSELAGE SIDE. BLENDED AND REMOVED DAMAGE ON PAX DOOR HINGE LUGS IAW REO 670-53-21-582, REV -F, SRM 51-21-11, 51-25-06, 51-25-16, & AMM 52-11-00.
- [SDR SWIA2026011176635](https://openairdocs.org/sdr/SWIA2026011176635.md): Floorbeam · cracked · Jan 11, 2026 · N707EV · Cndair CL6002C11 · Fuselage Main, Floor Beam
  > LBL 12 COCKPIT FLOORBEAM IS CRACKED AT BS 280 ATTACH POINT. PERFORMED REPAIR ON LBL 12 COCKPIT FLOORBEAM IAW REO 670-53-11-896, REV --, AMM 20-70-00, AND SRM 51-25-16.
- [SDR SWIA2026010876641](https://openairdocs.org/sdr/SWIA2026010876641.md): Web · cracked · Jan 8, 2026 · N707EV · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > FWD EQUIPMENT COMPARTMENT LT FLOOR WEB CRACKED BY THE BRAKE ACCUMULATOR GAUGES. PERFORMED REPAIR ON FWD EQUIPTMENT COMPARTMENT LT FLOOR WEB IAW REO 670-53-11-509,REV -E, AMM 32-43-30, 20-70-00, SRM 51-42-06, AMM 32-43-16, 12-12-29.
- [SDR SWIA2026010876623](https://openairdocs.org/sdr/SWIA2026010876623.md): Web · cracked · Jan 8, 2026 · N707EV · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > FWD EQUIPMENT COMPARTMENT RT SIDE FLOOR WEB REPAIR DOUBLER UNDER ADG PUMP APPEARS TO BE CRACKED. REMOVED AND REPLACED DOUBLER AT FWD EQUIPMENT COMPARTMENT RT SIDE FLOOR WEB REPAIR UNDER ADG PUMP IAW REO 670-53-11-509 REV-E, DATE: 2018-02-08, AMM 24-23-19, &
- [SDR SWIA2025111876640](https://openairdocs.org/sdr/SWIA2025111876640.md): Skin · dented · Nov 18, 2025 · N707EV · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > COMPLY WITH PERMANENT REPAIR ON RA 78977, FOUND DENT ON EXTERIOR OF FUSELAGE AT INTERSECTION OF BS 501 AND STR 21R. COMPLIED WITH TEMPORARY REPAIR PER REO670-53-31-627 REV A. PERMANENT REPAIR DUE WITHIN 8000 FLT HRS BY 47667.7 TAT, PERFORMED DRESSBACK AND
- [SDR SWIA2025111876632](https://openairdocs.org/sdr/SWIA2025111876632.md): Skin · dented · Nov 18, 2025 · N707EV · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > FOUND DENT ON EXTERIOR OF FUSELAGE 2 INCHES FWD OF BS2 80 AND 1 INCH ABOVE STGR 26R. COMPLIED WITH TEMPORARY REPAIR PER REO 670-53-11-1678 REV A DATED 2022-06-01. PERMANENT REPAIR DUE WITHIN 8000 FLT HRS BY 47667.7 TAT, PERFORMED PERMANET REPAIR BY EVALUATIN
- [SDR SWIA202307050626](https://openairdocs.org/sdr/SWIA202307050626.md): Unknown · unknown · Jun 26, 2023 · N707EV · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > GEAR DID NOT RETRACT ON TAKE OFF. WE RECEIVED GEAR DISAGREE WARNING MSG. COMPLIED WITH QRH PROCEDURE. PROX SYS FAULT STATUS MSG WAS PRESENT WITH GEAR DOWN BUT AFTER LANDING IT EXTINGUISHED. (FLT 3200 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 2
- [SDR SWIA20230627006](https://openairdocs.org/sdr/SWIA20230627006.md): Unknown · unknown · Jun 26, 2023 · N707EV · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > GEAR DID NOT RETRACT ON TAKE OFF. WE RECEIVED GEAR DISAGREE WARNING MSG. COMPLIED WITH QRH PROCEDURE. PROX SYS FAULT STATUS MSG WAS PRESENT WITH GEAR DOWN BUT AFTER LANDING IT EXTINGUISHED. (FLT 3200 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2023062603](https://openairdocs.org/sdr/SWIA2023062603.md): Unknown · did not stow · Jun 23, 2023 · N707EV · Cndair CL6002C10 · Landing Gear Door Actuator
  > DURING TAKEOFF, TRIPLE CHIME AND GEAR DISAGREE DURING GEAR RETRACTION, NOSE GEAR DID NOT SHOW RETRACTED. COMPLIED WITH QRH PROCEDURE, GEAR DISAGREE MESSAGE DISAPPEARED, THEN SHORTLY THEREAFTER PROX SYS FAULT 1 STATUS MESSAGE APPEARED. SET UP FOR EMERGENCY LAND
- [SDR SWIA202306150014](https://openairdocs.org/sdr/SWIA202306150014.md): Unknown · damaged · Jun 14, 2023 · N707EV · Cndair CL6002C10 · Fuselage Main, Frame
  > DAMAGE ON RH SIDE OF AIRCRAFT FUSELAGE BETWEEN FS333.00 AND FS349.00, BETWEEN STGR19R AND STGR21RTHIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 IS REQUIRED.REF: EAML 1156202 AND 1156470 (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202162959](https://openairdocs.org/sdr/SWIA202162959.md): None · damaged · Dec 3, 2021 · N707EV · Cndair CL6002C10 · Fuselage Structure (General)
  > REF CP 23937463 FOR ORIGINAL DISCREPANCY AND CP23943655 FOR DAMAGE DETERMINATION. FOUND TWO HOLES TO BE ELONGATED WHILE REMOVING THE PAX DOOR AFT SEAL RETAINER THIS DAMAGE HAS BEEN DETERMINED TO BE MAJOR PER GMM 3-26 REPAIR PER REO 670-52-11-1272. (FILED CL
- [SDR SWIA2021092961356](https://openairdocs.org/sdr/SWIA2021092961356.md): Terminal · loose · Sep 28, 2021 · N707EV · Cndair CL6002C10 · Ice/Rain Protection System Wiring
  > SMELL OF ELECTRICAL SMOKE DETECTED AROUND FL220. AT FL280, SMELL INTENSIFIED AND SMOKE SEEN AROUND WINDOW HEAT IN CA SIDE. (FLIGHT 3084) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 23560452 WITH THE FOLLOWING CORRECTIVE ACTION: "INSPECTED CA'S SIDE WIND
- [SDR SWIA2021092961238](https://openairdocs.org/sdr/SWIA2021092961238.md): Filter · obstructed · Sep 27, 2021 · N707EV · Cndair CL6002C10 · Air Distribution System
  > DURING CLIMB OUT FROM DFW A VERY INTENSE ELECTRICAL BURNING SMELL ENTERED THE FLIGHT DECK. (FLIGHT 3243 - FILED CLOSED) PLEASE REFERENCE AML 743123 PLEASE REFERENCE AML 743125 PLEASE REFERENCE AML 743191 PLEASE REFERENCE AML 743202 PLEASE REFERENCE
- [SDR SWIA2021091561080](https://openairdocs.org/sdr/SWIA2021091561080.md): Doubler · cracked · Sep 10, 2021 · N707EV · Cndair CL6002C10 · Fuselage Main, Structure
  > LH UPPER TRANS COWL €“ POSSIBLE CRACK ON DOUBLER FOR FWD LATCH CUTOUT (FILED CLOSED) REMOVED AND REPLACED DOUBLER FOR FWD LATCH CUTOUT ON LH UPPER TRANSCOWL IN REFERENCE TO CRJ 700 SRM 51-42-13
- [SDR SWIA202154935](https://openairdocs.org/sdr/SWIA202154935.md): Smoke Warning · false activation · Jan 2, 2021 · N707EV · Cndair CL6002C10 · Smoke Detection
  > WHILE ON LEFT DOWNWIND, THE SMOKE AFT LAV WARNING LIGHT ILLUMINATED. WE ELECTED TO LAND AND THEN RAN THE QRH. NO EVIDENCE OF ANY SMOKE WAS FOUND. RAN THE QRH AND SECURED THE LAV AREA AND TAXIED TO PARKING WITH NO ISSUE.
- [SDR N6WA20200410701](https://openairdocs.org/sdr/N6WA20200410701.md): Frame · cracked · Apr 7, 2020 · N707EV · Cndair CL6002C10 · Fuselage Main, Frame
  > DURING SCHEDULED MAINTENANCE IN THE GOJET MAINTENANCE FACILITY IN ST LOUIS INT’L AIRPORT, ST. LOUIS, MO (STL) THE FUSELAGE FRAME UPPER SECTOR AT FS 333.00 BETWEEN S-1R AND S-2R WAS FOUND CRACKED. REPAIRED IAW STS ENGINEERING AUTHORIZATION 70-2020-066
- [SDR ASOA201809267169](https://openairdocs.org/sdr/ASOA201809267169.md): Brake · dragging · Sep 26, 2018 · N707EV · Cndair CL6002C10 · Brake
  > TYS A/C WAS LANDING WHEN THE RIGHT MAIN OUTBOARD TIRE BLEW OUT. MAINTENANCE FOUND THE NR 4 BRAKE TO BE DRAGGING. MAINTENANCE REMOVED AND REPLACED THE NR 4 BRAKE ASSEMBLY IAW AMM 32-43-26. REPLACED BOTH TIRES AND WAS RELEASED BACK TO SERVICE AFTER OPS CHECK.
- [SDR ASOA201804215108](https://openairdocs.org/sdr/ASOA201804215108.md): Bulb · inoperative · Apr 21, 2018 · N707EV · Cndair CL6002C10 · Emergency Lighting
  > PILOT REPORTED OVERHEAD EMERGENCY LIGHTS AT ROWS 9 AND 15 WERE INOPERATIVE. REMOVED AND REPLACED THE BULBS, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20161105207](https://openairdocs.org/sdr/ASOA20161105207.md): Floorbeam · corroded · Nov 5, 2016 · N707EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > DURING C CHECK, FOUND FLOORBEAM ANGLE CORRODED BEYOND LIMITS AT FS 280. REMOVED AND REPLACED FLOOBEAM ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-25-16-001-001-A01.
- [SDR ASOA201610250615](https://openairdocs.org/sdr/ASOA201610250615.md): Battery · discharged · Oct 25, 2016 · N707EV · Cndair CL6002C10 · Emergency Lighting
  > CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT TURN ON. THE EMERGENCY LIGHT SYSTEM WAS CHARGED AND FAULT NO LONGER EXIST. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA2016051914841](https://openairdocs.org/sdr/ASOA2016051914841.md): Fitting · cracked · May 19, 2016 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WHILE WORKING INTERCOSTAL REPAIR AT FS 280, FS 265, RBL1, FOUND FWD JACK FITTING TO BE CRACKED. REMOVED LT & RT ANGLE FROM FS 280.00 AND FROM LT & RT SUPPORTS BETWEEN FS 265.00 & FS 280.00 REF: SRM 51-42-21-001-001 A01 PART REMOVED TO FOM RT ANGLE AT RBL1- FS
- [SDR ASOA2016051614859](https://openairdocs.org/sdr/ASOA2016051614859.md): Retainer · corroded · May 16, 2016 · N707EV · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOOR SEAL RETAINER AREAS HAS EXFOLICATED CORROSION. REMOVED DOOR SEAL, DAMAGED IAW AMM 52-42-07-000-801-A01. INSTALLED NEW AVIONICS DOOR SEAL IAW AMM 52-42-07-400-801-A01. REMOVED 4 EA CORRODED SEAL RETAINERS IAW 51-42-06-001-001-A01. INSTALL
- [SDR ASOA2016051614855](https://openairdocs.org/sdr/ASOA2016051614855.md): Support · cracked · May 16, 2016 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING REPAIR OF AFT BAGAGE BAY DOOR SILL STRUCTURE FOUND THE MACHINED FITTING SUPPORTING THE SILL AT FS101.5, CRACKED. REMOVED MACHINED FITTING. FITTING SPLICE, AND STRINGER CLIP IAW SRM 51-42-21-001-001-A01. LOCATED FASTENER HOLES IN NEW SERVICABLE MACHIN
- [SDR ASOA2016050214854](https://openairdocs.org/sdr/ASOA2016050214854.md): Floor Support · corroded · May 2, 2016 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON LT FLOOR SILL AT FS 761.93 & 785.07. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EA 32-2016-079. RECIEVED & COMPLIED WITH EC/TC EA 32-2016-079.
- [SDR ASOA2016042914853](https://openairdocs.org/sdr/ASOA2016042914853.md): Frame · corroded · Apr 29, 2016 · N707EV · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION WAS DISCOVERED ON LT FUSELAGE FRAME 549 BELOW FLOOR SILL. RECEIVED REO 670-53-31-367. REO 53-31-367 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.
- [SDR ASOA2016042514858](https://openairdocs.org/sdr/ASOA2016042514858.md): Intercostal · corroded · Apr 25, 2016 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL LBL1 FS 280-265 HAS CORROSION, NOSE JACK FITTING. REMOVED INTERCOSTAL SUPPORT LBL1 BETWEEN FS280.00 AND FS265.00 REF SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-0001-001-A01. STARTED DRILLING UP SERIVCABLE INTERCOSTAL AT LBL1 BET
- [SDR ASOA2016042514852](https://openairdocs.org/sdr/ASOA2016042514852.md): Floor Support · corroded · Apr 25, 2016 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON RBL9 FLOORBEAM AT FS 1015.00, SAND 1031.00. REMOVED CORROSION ON RBL9, FLOORBEAM AT FS 1015.00 AND 1031.00 IAW SRM 51-21-06-001-001 A01. REPAIRED FLOORBEAM IAW SRM 53-00-41-201-001-A01-GIG 53-00-41-991-830 & EO 700-53-0309, REV 0. STARTED
- [SDR ASOA2016042514851](https://openairdocs.org/sdr/ASOA2016042514851.md): Floor Support · corroded · Apr 25, 2016 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON LBL 27 FLOOR SUPPORT AT BS 1000, 1015, 1031. REMOVED CORROSION ON LBL27, FLOOR SUPPORT IAW SRM 51-21-06-001-001-A01. REPAIRED FLOOR SUPPORT IAW SRM 53-00-41-201-001-A01. FIG 53-00-41-991-830 & EO 700-53-03-08, REV 0.
- [SDR ASOA2016042514850](https://openairdocs.org/sdr/ASOA2016042514850.md): Floorbeam · corroded · Apr 25, 2016 · N707EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORRISON FOUND ON LBL 9, FLOORBEAM AT FS 1031.00. REMOVED CORROSION ON LBL9 FLOOR BEAM AT FS 1031.00 IAW SRM 51-21-06-001-001, A01. REMOVED DAMAGED SECTION OF FLOORBEAM & TRIMMED TO FIT NEW SECTION OF FLOORBEAM, FS 1031, LBL9 REF REO 670-53-00-029 AND EC/TC
- [SDR ASOA2016042514849](https://openairdocs.org/sdr/ASOA2016042514849.md): Frame · corroded · Apr 25, 2016 · N707EV · Cndair CL6002C10 · Fuselage Main, Frame
  > 349 FRAME HAS CORROSION LBL2-STR 26R. REMOVED RT SIDE SEAT RAIL AT FS 565-677 IAW AMM 53-00-49-000-801-A01. INSTALLED NEW RT SIDE SEAT RAIL AT FS 565-677 IAW AMM 53-00-49-400-801-A02. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M.
- [SDR ASOA2016042514846](https://openairdocs.org/sdr/ASOA2016042514846.md): Intercostal · corroded · Apr 25, 2016 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED FS 349-364, LBL2. REMOVED INTERCOSTAL AT 349-364 LBL2 IAW SRM 51-42-06-001-001 A01 & 51-42-21-001-001 A01. DRILLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001, A01 & 51-42-21-001-001 A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001 A
- [SDR ASOA2016042514845](https://openairdocs.org/sdr/ASOA2016042514845.md): Intercostal · corroded · Apr 25, 2016 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL RBL1 FS 280-265 HAS CORROSION, AT NOSE JACK FITTING. REMOVED INTERCOSTAL RBL1, BETWEEN FS 265.00 AND 280.00, REF SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. STARTED DRILLING UP NEW RBL-1, INTERCOSTAL FS 280- FS 265 RE
- [SDR ASOA2016042514819](https://openairdocs.org/sdr/ASOA2016042514819.md): Structure · corroded · Apr 25, 2016 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PACKER CORRODED AT RBL 9, FS 333.00. R & R PACKER AT RBL 9, FS 333.0 IAW AMM 51-42-06-001-001 A01.
- [SDR ASOA2016042514818](https://openairdocs.org/sdr/ASOA2016042514818.md): Intercostal · corroded · Apr 25, 2016 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED FS 349-364, RBL2. REMOVED INTERCOSTAL AT 349-364, RBL2 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. DRILLED NEW INTERCOSTAL IAW SRM 700 51-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-
- [SDR ASOA2016042514817](https://openairdocs.org/sdr/ASOA2016042514817.md): Floorbeam · corroded · Apr 25, 2016 · N707EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > AVIONIC BAY CRAWL WAY FLOOR SUPPORT HAS CORROSION AT FS 280. REMOVED CORRODED CRAWLWAY SUPPORT IAW SRM 57-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED NEW CRAWLWAY SUPPORT IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01, DWG CC670-34256.
- [SDR ASOA2016042514816](https://openairdocs.org/sdr/ASOA2016042514816.md): Support · cracked · Apr 25, 2016 · N707EV · Cndair CL6002C10 · Wing Miscellaneous Structure
  > CRACK FOUND ON LT AFT WING TO FUSELAGE FAIRING SUPPORT DIAPHRAGM LBL17.63, FS 923.00. REPAIRED WING TO FUSELAGE AFT FAIRING SUPPORT FS 909.00, LBL 17.63 OR RBL 17.63 IAW REO 670-53-82-478, REV A.
- [SDR ASOA2016042214848](https://openairdocs.org/sdr/ASOA2016042214848.md): Seat Track · corroded · Apr 22, 2016 · N707EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK FS 565 - FS 677 HAS CORROSION DAMAGE. REMOVED RT SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A01. INSTALLED NEW RT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A02. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV M.

Next page: https://openairdocs.org/aircraft/N707EV/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 = 'N707EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N707EV/reports

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