# Service difficulty reports: N974EV, cancelled Jan 16, 2023

A list on [N974EV, cancelled Jan 16, 2023](https://openairdocs.org/deregistered/N974EV-2023-01-16.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 2 · 80 reports

- [SDR ASOA2014111211632](https://openairdocs.org/sdr/ASOA2014111211632.md): Relay · failed · Nov 8, 2014 · N974EV · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN DOOR AUTOMATICLY CLOSED BY ITSELF AND IS IMPOSSIBLE TO OPEN WITH NORMAL POWER. R & R RELAY K1MB IN JUNCTION BOX 2. OPS CHECKED GOOD. ACFT OK FOR SERVICE. IAW CMM 24-00-02.
- [SDR ASOA2014072510967](https://openairdocs.org/sdr/ASOA2014072510967.md): Light · inoperative · Jul 21, 2014 · N974EV · Cndair CL6002B19 · Emergency Lighting
  > SERVICE DOOR EMERGENCY EXIT SIGN FLOOD LIGHT INOPERATIVE. 07-21-2014 R & R EMERGENCY EXIT SIGN FLOOD LIGHT IAW AMM 33-51-10. OPS CHECKED GOOD.
- [SDR ASOA2013122409691](https://openairdocs.org/sdr/ASOA2013122409691.md): Sign · inoperative · Dec 22, 2013 · N974EV · Cndair CL6002B19 · Emergency Lighting
  > F/A REPORTS THAT EXIT SIGNS IN THE GALLEY WILL NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE SELECTED ON. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS SYS IAW AMM 33-51-00. OPS CHECKED GOOD.
- [SDR ASOA2013053103741](https://openairdocs.org/sdr/ASOA2013053103741.md): Lamp · burned out · May 29, 2013 · N974EV · Cndair CL6002B19 · Emergency Lighting
  > FOUR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R LAMPS IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2013052303655](https://openairdocs.org/sdr/ASOA2013052303655.md): Seat Track · corroded · Apr 16, 2013 · N974EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 9, CORRODED AT FS 364. REMOVED SEAT TRACK SECTION FS 364 - 398 IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-00-11-400-802.
- [SDR ASOA2013052303654](https://openairdocs.org/sdr/ASOA2013052303654.md): Floorbeam · corroded · Apr 16, 2013 · N974EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 280 FLOORBEAM ANGLE IS CORRODED AT CENTER SECTION. REMOVED FLOORBEAM ANGLE IAW SRM 51-42-06 LOCATED HOLES IN NEW PART IAW SRM 51-40-06 TREATED PRIMED AND APPLIED TOPCOAT IAW SRM 51-25-16 AND 51-25-06. INSTALLED NEW ANGLE WET WITH SEATANT IAW SRM 51-42-0
- [SDR ASOA2013052303653](https://openairdocs.org/sdr/ASOA2013052303653.md): Floorbeam · corroded · Apr 16, 2013 · N974EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 280 FLOORBEAM CORRODED AT CENTER SECTION. REPAIRED IAW REO 601R-53-11-2503.
- [SDR ASOA2013052303652](https://openairdocs.org/sdr/ASOA2013052303652.md): Seat Track · corroded · Apr 16, 2013 · N974EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 9 THAT EXTENDS FROM FS 365 TO 398 CORRODED SEVERAL AREAS. WORST CORROSION AT FS 364.00 OF TRACK. REMOVED SEAT TRACK SECTION IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2013052303647](https://openairdocs.org/sdr/ASOA2013052303647.md): Seat Track · corroded · Apr 15, 2013 · N974EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT TRACK THAT EXTENDS FROM FS 364.00 TO FS 409+16 IS CORRODED AT FS 383.00. INSTALLED SERVICEABLE SECTION OF LT SEAT TRACKIAW AMM 53-01-11. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REF A.
- [SDR ASOA2013052303646](https://openairdocs.org/sdr/ASOA2013052303646.md): Seat Track · corroded · Apr 15, 2013 · N974EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK THAT EXTENDS FROM FS 547.00 TO FS 559+80 IS CORRODED AT FS 559+69. INSTALLED SERVICEABLE SECTION OF LT SEAT TRACK EXTENDING FROM FS 547.00 TO FS 559.+80 IAW AMM 53-01-11. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REV
- [SDR ASOA2013052303651](https://openairdocs.org/sdr/ASOA2013052303651.md): Bulkhead · cracked · Apr 11, 2013 · N974EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB FORWARD FACE IS CRACKED ABOVE CARGO DOOR AFT TRACK AREA. REPAIRED IAW REO 601-53-61-1541.
- [SDR ASOA2013052303650](https://openairdocs.org/sdr/ASOA2013052303650.md): Spring · lack of lube · Apr 9, 2013 · N974EV · Cndair CL6002B19 · Emergency Exits
  > RT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST IAW TASKCARD 000-52-840-102. RELEASED TENSION ON SPRINGS BY CLEANING & LUBING & REINSTALLED RT EMERGENCY EXIT DOOR LATCH SPRINGS IAW AMM 52-21-02-400-801, 12-20-52-640-802. OPS TESTED GOOD IAW AMM 52-21-00-71
- [SDR ASOA2013052303649](https://openairdocs.org/sdr/ASOA2013052303649.md): Spring · lack of lube · Apr 9, 2013 · N974EV · Cndair CL6002B19 · Emergency Exits
  > LT OVERWING EMERGENCY EXIT FAILED FUNCTION TEST IAW TASKCARD 000-52-830-104. RELEASED TENSION ON SPRINGS BY CLEANING & LUBING & REINSTALLED LT EMERGENCY EXIT DOOR LATCH SPRINGS IAW AMM 52-21-02-400-801, 12-20-02-640-802. OPS TESTED GOOD IAW AMM 52-21-00-710
- [SDR ASOA2013052303648](https://openairdocs.org/sdr/ASOA2013052303648.md): Floor Skin · cracked · Apr 6, 2013 · N974EV · Cndair CL6002B19 · Fuselage Floor Panel
  > CRACK ON FLOOR SKIN LT SIDE FWD OF FS 202. REPAIRED IAW REO 601R-53-11-081.
- [SDR ASOA2013052303645](https://openairdocs.org/sdr/ASOA2013052303645.md): Drag Angle · cracked · Apr 6, 2013 · N974EV · Cndair CL6002B19 · Passenger/Crew Doors
  > ASD AFT DRAG ANGLE CRACKED AT PULLEY BRACKET. REPAIRED IAW REO 601R-52-11-513.
- [SDR ASOA2013052303644](https://openairdocs.org/sdr/ASOA2013052303644.md): Lamp · burned out · Apr 6, 2013 · N974EV · Cndair CL6002B19 · Emergency Lighting
  > LOWER EMERGENCY LIGHT AT PAX DOOR FAILED OPS CHECK. R & R LAMPS IN PAX DOOR LOWER EMERGENCY LIGHT IAW AMM 33-51-10-000-801 AND 33-51-10-400-801. COMPLIED WITH OPS TEST OF THE LOWER EMERGENCY LIGHT AT THE PAX DOOR IAW AMM 33-51-00-710-801, OPS TESTED GOOD.
- [SDR ASOA2012122002687](https://openairdocs.org/sdr/ASOA2012122002687.md): Flashlight · inoperative · Dec 16, 2012 · N974EV · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT INOPERATIVE. R & R FA FLASHLIGHT IAW AMM 25-61-02. ACFT OK FOR SERVICE.
- [SDR ASOA201201651](https://openairdocs.org/sdr/ASOA201201651.md): Lamp · burned out · May 15, 2012 · N974EV · Cndair CL6002B19 · Emergency Lighting
  > NR 8 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM 33-51-21, OPS CHECKED GOOD.
- [SDR ASOA201201601](https://openairdocs.org/sdr/ASOA201201601.md): Warning Light · illuminated · May 7, 2012 · N974EV · Cndair CL6002B19 · Fire Detection
  > APU FIRE INDICATION ON LANDING FOLLOWING STRONG FUEL ODOR. EMERGENCY DECLARED. R & R APU FIRE BOTTLE AND SQUIB IAW AMM 26-22-10. OPS CHECKED GOOD.
- [SDR ASOA201101618](https://openairdocs.org/sdr/ASOA201101618.md): Flap System · failed · Aug 28, 2011 · N974EV · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL 0 DEGREE ON APPROACH, REPEAT WRITEUP. EMERGENCY DECLARED AS A PRECAUTION. ALL WORK ACCOMPLISHED. AD 2009-06-12 ACCOMPLISHED.
- [SDR ASOA201101617](https://openairdocs.org/sdr/ASOA201101617.md): Bpsu · unserviceable · Aug 27, 2011 · N974EV · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH AFTER SELECTING FLAPS 8200 KNOTS RECEIVED FLAPS FAIL CAUTION MSG FLAPS REMAINED AT ZERO DEG C/W QRH AND NO FLAP LANDING. EMERGENCY DECLARED AS A PRECAUTION. RT BPSU REPLACED.
- [SDR ASOA201101546](https://openairdocs.org/sdr/ASOA201101546.md): Battery · inoperative · Aug 20, 2011 · N974EV · Cndair CL6002B19 · Emergency Equipment
  > F/O FLASHLIGHT INOP. R & R FLASHLIGHT BATTERIES IAW AMM 25-61-04. OPS CHECKED GOOD.
- [SDR ASOA201101014](https://openairdocs.org/sdr/ASOA201101014.md): Window · cracked · May 8, 2011 · N974EV · Cndair CL6002B19 · Flight Compartment Windows
  > CAPTAINS LT SIDE WINDOW SPIDER WEBED DESCENDING BELOW 24000 FT INTO LT (FIRE TRUCKS WERE ROLLED AS A PRECAUTION) N/C & FLT 5353 CX. REMOVED AND REPLACED CAPTAIN'S SIDE WINDOW IAW AMM 56-12-01. OPS CHECK GOOD.
- [SDR ASOA201100846](https://openairdocs.org/sdr/ASOA201100846.md): Angle · corroded · Apr 25, 2011 · N974EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WHILE PERFORMING MAINTENANCE, FOUND PAX DOOR ANGLE ASSY TO HAVE CORROSION ABOVE HINGE ON SILL. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED ANGLE IAW SRM 51-42-06, 51-42-13, & 51-42-21. INSTALLED AND SEALED ANGLE ASSY IAW 601R31527-211.
- [SDR ASOA201100758](https://openairdocs.org/sdr/ASOA201100758.md): Isolator · broken · Apr 12, 2011 · N974EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 PRESSURE BULKHEAD FWD FACE HAS 9 BROKEN ISOLATORS. FOUND 13 BROKEN ISOLATORS AND R & R THE ISOLATORS WITH NEW SERVICEABLE ISOLATORS P/B SL2337-3 IAW SRM 51-42-06. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSI
- [SDR ASOA201100757](https://openairdocs.org/sdr/ASOA201100757.md): Floor Support · cracked · Apr 12, 2011 · N974EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FS 621 FLOOR SUPPORT ANGLE PREVIOUS REPAIR CRACKED. REPAIR OF THE DAMAGED PORTIONS OF ANGLE 601R38031-239 IS COMPLETED IAW REO 601R-53-61-117.
- [SDR ASOA201100756](https://openairdocs.org/sdr/ASOA201100756.md): Floor Support · corroded · Apr 12, 2011 · N974EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT CARGO FLOOR SUPPORT CAP ANGLE HAS CORROSION AROUND FASTENER HOLES OTBD SIDE OF LBL 27 BETWEEN FS 574 AND FS 621. REMOVED CORROSION FOUND IAW REO 601R-53-00-005, REPAIR STEPS 1 AND 2.
- [SDR ASOA201100755](https://openairdocs.org/sdr/ASOA201100755.md): Cargo Track · corroded · Apr 12, 2011 · N974EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR TRACK SEGMENTS AT LBL 9 AND RBL 9 CORRODED BETWEEN FS 559+80 AND FS 559+96. REMOVED 2 CORRODED CARGO TRACKS AND REPLACED 2 NEW CARGO TRACKS IAW SRM 51-41-02. THIS REPAIR REQUIRE MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSI
- [SDR ASOA201100754](https://openairdocs.org/sdr/ASOA201100754.md): Cargo Track · corroded · Apr 12, 2011 · N974EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO BAGGAGE RAIL CORRODED AT LBL 9 BETWEEN FS 605 AND FS 621. REMOVED 1 CORRODED CARGO FLOOR TRACK AND REPLACED A NEW CARGO TRACKS IAW SRM 51-41-02. THIS REPAIR REQUIRE MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REP
- [SDR ASOA201100753](https://openairdocs.org/sdr/ASOA201100753.md): Cargo Track · corroded · Apr 12, 2011 · N974EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO BAY FLOOR TRACKS CORRODED AT LBL 9 AND RBL 9 BETWEEN FS 559+112 AND FS 574. REMOVED 2 CORRODED CARGO FLOOR TRACKS AND REPLACED 2 NEW CARGO TRACKS IAW SRM 51-41-02. THIS REPAIR REQUIRE MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIF
- [SDR ASOA201100752](https://openairdocs.org/sdr/ASOA201100752.md): Sill · corroded · Apr 12, 2011 · N974EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL PLATE UPPER AFT ANGLE HAS CORROSION AT FS 349 UNDER CABIN FLOOR PANEL 232CRF. REPAIRED IAW THE REO 601R-53-21-1277.
- [SDR ASOA201100751](https://openairdocs.org/sdr/ASOA201100751.md): Seat Track · corroded · Apr 12, 2011 · N974EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE FWD SECTION OF SEAT TRACK FS 364.00 TO FS 394.00 HAS SEVERAL AREAS OF CORROSION. CORRODED SECTION OF SEAT TRACK REMOVED IAW AMM 53-01-11-000-802. NEW FLOOR SEAT TRACK INSTALLED IAW AMM 53-01-11-400-802.
- [SDR ASOA201100750](https://openairdocs.org/sdr/ASOA201100750.md): Placard · damaged · Apr 12, 2011 · N974EV · Cndair CL6002B19 · Placards and Markings
  > PAX DOOR "EXIT" PLACARD PARTIALLY MISSING. REMOVED WORN PLACARD IAW MM 11-30-00-000-801 AND APPLIED NEW EXIT PLACARD IAW MM 11-30-00-400-801.
- [SDR ASOA201100749](https://openairdocs.org/sdr/ASOA201100749.md): Intercostal · cracked · Apr 12, 2011 · N974EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROX.5" LONG. REPLACED CRACKED INTERCOSTAL RT SIDE AT FS 621, STR 14R IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED
- [SDR ASOA201100748](https://openairdocs.org/sdr/ASOA201100748.md): Intercostal · cracked · Apr 12, 2011 · N974EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROX.6" LONG. REPLACED CRACKED INTERCOSTAL LT SIDE AT FS 621 STR 14L IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED A
- [SDR ASOA201100453](https://openairdocs.org/sdr/ASOA201100453.md): Light · damaged · Mar 7, 2011 · N974EV · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT FLOODLIGHT ON LT WARDROBE AT ENTRY WAY IS DAMAGED. R & R EMER EXIT FLOODLIGHT ASSY ON WARDROBE IAW AMM 33-51-10, OP'S CHECK GOOD. R & R EMERGENCY EXIT FLOODLIGHT ASSY ON WARDROBE IAW AMM 33-51-10, OP'S CHECK GOOD.
- [SDR ASOA201100008](https://openairdocs.org/sdr/ASOA201100008.md): Bulb · burned out · Jan 1, 2011 · N974EV · Cndair CL6002B19 · Emergency Lighting
  > 2ND EMERGENCY CEILING LIGHT IS INOP. R & R EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OP'S CHECKED GOOD. (CLOSED)
- [SDR ASOA201001990](https://openairdocs.org/sdr/ASOA201001990.md): Light · inoperative · Dec 17, 2010 · N974EV · Cndair CL6002B19 · Emergency Lighting
  > 3 SEGMENTS OF GREEN FLOOR LIGHTING DO NOT ILLUMINATE. OPS CHECK GOOD IAW AMM 33-51-01. (CLOSED)
- [SDR ASOA201001767](https://openairdocs.org/sdr/ASOA201001767.md): Frame · cracked · Nov 11, 2010 · N974EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND FS 605.00 FRAME CRACKED AT STRINGER 18L. REPAIRED IAW REO601R-53-61-3887.
- [SDR ASOA201001515](https://openairdocs.org/sdr/ASOA201001515.md): Placard · missing · Oct 7, 2010 · N974EV · Cndair CL6002B19 · Placards and Markings
  > "EXIT" DECAL MISSING FROM (3RD STEP) ON AIRSTAIR DOOR END. REPLACED EXIT DECAL IAW AMM 11-30-00. (CLOSED)
- [SDR ASOA201000924](https://openairdocs.org/sdr/ASOA201000924.md): Reservoir · worn · Jun 12, 2010 · N974EV · Cndair CL6002B19 · Hydraulic Reservoir, Main
  > RECEIVED NOSE GEAR DISAGREE WARNING MSG AFTER T/O, CYCLED GEAR AND GOT GEAR DISAGREE MSG AND NOSE DOOR WARNING MSG. (EMERGENCY EQUIPMENT REQUESTED AS A PRECAUTION) (LANDING GEAR RETRACTION SYS) REFER TO LOG PAGE 532717-3 HYD RESERVOIR, REPLACED. PERFORMED
- [SDR ASOA200900574](https://openairdocs.org/sdr/ASOA200900574.md): Warning System · activated · May 19, 2009 · N974EV · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAP FAIL CAUTION MSG ON CLIMB OF ATL AT 18800' AND LANDED AT 300FPM, EMERGENCY DECLARED. FLT 5563 DEL 32 MINS
- [SDR ASOA200900560](https://openairdocs.org/sdr/ASOA200900560.md): Light · inoperative · May 15, 2009 · N974EV · Cndair CL6002B19 · Emergency Lighting
  > AFT SECTION EMERGENCY FLOOR TRACK LIGHT INOP.
- [SDR ASOA200900526](https://openairdocs.org/sdr/ASOA200900526.md): Skin · cracked · Apr 29, 2009 · N974EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT SKIN WEB IS CRACKED IN RADIUS AT STEP 832CT AND FIXED MID STEP.
- [SDR ASOA200900486](https://openairdocs.org/sdr/ASOA200900486.md): Beam · cracked · Apr 23, 2009 · N974EV · Doug DC983 · Fuselage Main, Structure
  > FS 280 OTBD OF RBL 9, TRANSVERSE BEAM IS CRACKED.
- [SDR ASOA200900476](https://openairdocs.org/sdr/ASOA200900476.md): Post · damaged · Apr 22, 2009 · N974EV · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND FS 409.0+128 VERTICAL POST LBL 18.0 OTBD SIDE HAS INDICATION NOTED A1TWL 69.0 AFT FLANGE APPROX.2 INCH IN LENGTH 50 PERCENT FSH FAILED NDT INSP. REMOVED VERTICAL POST IAW SRM 51-42-06. FABRICATED NEW VERTICAL POST IAW SRM 51-24-16. HEAT TREATED REPAIR
- [SDR ASOA200900475](https://openairdocs.org/sdr/ASOA200900475.md): Post · damaged · Apr 22, 2009 · N974EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND FS 409+128 VERTICAL POST BL 0.0 LT SIDE HAS INDICATION NOTED AT WL 69.0 AFT FLANGE APPROX.2 INCH IN LENGTH 50 PERCENT FSH FAILED NDT INSP. REMOVED VERTICAL POST IAW SRM 51-42-06. FABRICATED NEW VERTICAL POST FOR AS PER SAMPLE. ALSO FABRICATED NEW VER
- [SDR ASOA200900495](https://openairdocs.org/sdr/ASOA200900495.md): Bulkhead · cracked · Apr 21, 2009 · N974EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LINTEL ATTACHMENT FITTING APPROX.1 INCH IN LENGTH 80 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED THE PRESSURE BULKHEAD WEB AT THE LINTEL ATTACHMENT FITTING IAW REO 601R-53-61-1230 REV. "D".
- [SDR ASOA200900494](https://openairdocs.org/sdr/ASOA200900494.md): Bulkhead · cracked · Apr 21, 2009 · N974EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 559 BULKHEAD WEB HAS INDICATION NOTED AT RT SIDE WEB WL 59.10 INBD OF RBL 18.0 APPROX.5 INCH IN LENGTH 60 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED BULKHEAD IAW REO 601R-53-41-260, STEP S1 THRU 14.
- [SDR ASOA200900474](https://openairdocs.org/sdr/ASOA200900474.md): Support Beam · cracked · Apr 21, 2009 · N974EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.0 INCH IN LENGTH.

Next page: https://openairdocs.org/deregistered/N974EV-2023-01-16/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 = 'N974EV' AND deregistration_id = 'N974EV-2023-01-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N974EV-2023-01-16/reports

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