# Service difficulty reports: N462AW

A list on [N462AW](https://openairdocs.org/aircraft/N462AW.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 4 · 197 reports

- [SDR A6WA202210208350](https://openairdocs.org/sdr/A6WA202210208350.md): Engine · failed · Oct 20, 2022 · N462AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > RIGHT ENG FAILURE ON T/O, LOST THRUST AT PROX 50FT, VIBRATIONS IN RED PERFORMED IAC SHUT ENG DOWN WITH 6 MIN. LH ENG HAD APR INCREASED LANDING WEIGHT APROX 49,000LBS. AIRCRAFT REMOVED FROM SERVICE. REF WO 319228 JOB CARD 4-R&RENG FOR REMOVAL AND REPLACEME
- [SDR A6WA202105037768](https://openairdocs.org/sdr/A6WA202105037768.md): Skin · damaged · Apr 29, 2021 · N462AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS TOP FUSELAGE FS 409.00+80 +4.5 TO 409+80+7 S0+2R TO S0.2L ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SCRIBE MARKS TOP FUSELAGE FS 409.00+80 +4.5 TO 409+80+7 S0+2R TO S0.2L,AT ORIGINAL THICKNESS OF 0.058Ï¿½ BLEND MEASURED 2.0Ï¿½L X 1.5Ï¿½W X.
- [SDR A6WA202105117775](https://openairdocs.org/sdr/A6WA202105117775.md): Skin · cracked · Apr 22, 2021 · N462AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING EDDY CURRENT INSPECTION OF CUT-LINE OF PREVIOUS REPAIR OF SKIN AT FS589.00 Ï¿½ FS621.00 BETWEEN STR 23L AND STR 27L, 1 INDICATION NOTED EMANATING FROM CUT-LINE ADJACENT TO STR 23L 1.0Ï¿½ FORWARD OF FRAME AT FS605 MEASURING 0.175" FWD OF FS605 AND BELOW
- [SDR A6WA202105077772](https://openairdocs.org/sdr/A6WA202105077772.md): Skin · corroded · Apr 22, 2021 · N462AW · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING PLANK ACCESS HOLE CUT-OUT AT PANEL 640BB HAS FRETTING CORROSION AT 2 LOCATIONS AROUND CIRCUMFERENCE. INITIATE AWAC E06/021-457 CURRENT REVISION. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED FRETTING CORROSION ON INBOARD (P1) & OUTBOARD (P2)
- [SDR A6WA202105077771](https://openairdocs.org/sdr/A6WA202105077771.md): Skin · corroded · Apr 22, 2021 · N462AW · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING PLANK ACCESS HOLE CUT-OUT AT PANEL 640CB HAS 2 INDICATIONS AT FWD I/B ARC. INITIATE AWAC E06/021-457 CURRENT REVISION. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED INDICATIONS ON INBOARD FLANGE OF PANEL 640CB ACCESS HOLE, MEASURING 6.100Ï¿½L
- [SDR A6WA202105077770](https://openairdocs.org/sdr/A6WA202105077770.md): Skin · corroded · Apr 22, 2021 · N462AW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER WING PLANK ACCESS HOLE CUT-OUT AT PANEL 540BB HAS FRETTING CORROSION AT SEVERAL LOCATIONS AROUND CIRCUMFERENCE. INITIATE AWAC E06/021-457 CURRENT REVISION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED FRETTING CORROSION ON INBOARD (P1) AND OUT
- [SDR A6WA202104307762](https://openairdocs.org/sdr/A6WA202104307762.md): Retainer · gouged · Apr 22, 2021 · N462AW · Cndair CL6002B19 · Fuselage Main, Structure
  > STRAP JUST ABOVE FRONT RIGHT WINDSHIELD OUTBOARD VERTICAL RETAINER HAS A GOUGE WL 128.85 RBL 1. AIRCRAFT REMOVED FROM SERVICE BLENDED DAMAGE TO A SMOOTH CONTOUR, PERFORMED HFEC WITH NO INDICATIONS, ROTO PEENED REWORK AREA AND APPLIED PROTECTIVE FINISH IAW
- [SDR A6WA202104307763](https://openairdocs.org/sdr/A6WA202104307763.md): Rib · corroded · Apr 21, 2021 · N462AW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RIGHT WING REAR SPAR RIB AT WS 53.60 INBOARD DOUBLER HAS CORROSION AROUND UPPER AND LOWER ELECTRICAL CONNECTOR HOLES AND AROUND NUTPLATE HOLES (3 EACH). ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM RIGHT WING REAR SPAR RIB AT WS 53.60 INBOARD D
- [SDR A6WA202104307764](https://openairdocs.org/sdr/A6WA202104307764.md): Angle · corroded · Apr 21, 2021 · N462AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RIGHT WING REAR SPAR WS 53.60 INBOARD UPPER ANGLE HAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM RIGHT WING REAR SPAR WS 53.60 INBOARD UPPER ANGLE BLENDS WITHIN LIMITS IAW ASAP EA# AWAC-CRJ257-01616 REV IR DATED 4/27/2021. DTE IS C
- [SDR A6WA202104297760](https://openairdocs.org/sdr/A6WA202104297760.md): Web · corroded · Apr 21, 2021 · N462AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RIGHT WING REAR SPAR RIB AT WS 53.60 AFT UPPER ANGLE HAS CORROSION. ***AIRCRAFT WAS REMOVED FROM SERVICE*** REMOVED CORROSION ON R/H WING REAR SPAR AT WS 53.60 AFT WEB, ARE MEASURES 1.50Ï¿½L X 0.10Ï¿½W X 0.004Ï¿½D, ORIGINAL THICKNESS 0.050Ï¿½, REMAINING 0.0
- [SDR A6WA202104287759](https://openairdocs.org/sdr/A6WA202104287759.md): Rib · corroded · Apr 21, 2021 · N462AW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LEFT WING REAR SPAR RIB AT WS 48.30 HAS CORROSION BELOW UPPER LIGHTING HOLE. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON LH WING REAR SPAR AT WS 48.30 BELOW UPPER LIGHTING HOLE, MEASUREMENTS ARE 0.800"L X 0.700"W X 0.002"D. REMAINING THICKNES
- [SDR A6WA202104297761](https://openairdocs.org/sdr/A6WA202104297761.md): Angle · corroded · Apr 21, 2021 · N462AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT WING REAR SPAR AT WS 53-60 INBOARD DOUBLER/ ANGLE HAS CORROSION AROUND UPPER AND LOWER ELECTRICAL CONNECTOR HOLES. ***AIRCRAFT REMOVED FROM SERVICE*** FOUND AND BLENDED CORROSION IN 3 PLACES ON LEFT WING REAR SPAR AT WS 53-60 INBOARD ANGLE. P1) 5.800
- [SDR A6WA202105037766](https://openairdocs.org/sdr/A6WA202105037766.md): Skin · corroded · Apr 21, 2021 · N462AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION TOP FUSELAGE FS 409.00+80 +4 S 0+3L ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION TOP FUSELAGE FS 409.00+80 +4 S 0+3L, 2.5Ï¿½L X 1.0Ï¿½W X.003Ï¿½D. ORIGINAL MATERIAL 0.045Ï¿½, LOSS 0.003Ï¿½ REMAINING 0.042Ï¿½. PERFORMED HFEC WITH NO INDICA
- [SDR A6WA202105037767](https://openairdocs.org/sdr/A6WA202105037767.md): Skin · corroded · Apr 21, 2021 · N462AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION TOP FUSELAGE FS 409.00+80 +2.5 S 0+3R ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION TOP FUSELAGE FS 409.00+80 +2.5 S 0+3R, 4.0Ï¿½L X 5.0Ï¿½W X.005Ï¿½D. ORIGINAL MATERIAL 0.058Ï¿½, LOSS 0.005Ï¿½ REMAINING 0.053Ï¿½. PERFORMED HFEC WITH NO
- [SDR A6WA202105117773](https://openairdocs.org/sdr/A6WA202105117773.md): Strap · damaged · Apr 20, 2021 · N462AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RIGHT WING TIP WHERE PANEL 671JT ATTACHES HAS SCRIBE MARKS ON THE UPPER AND LOWER SURFACES, 9 AREAS IN ALL. ***AIRCRAFT REMOVED FROM SERVICE***1) LOWER RT WINGLET DOUBLER, PN 600-10380-64 REPAIRED IAW ASAP EA# AWAC-CRJ257-01620 REV A DATED 5/5/2021. FCBS IS NO
- [SDR A6WA202104287758](https://openairdocs.org/sdr/A6WA202104287758.md): Skin · dented · Apr 19, 2021 · N462AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN DENT FS 672.20+2 AND S23+3R ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT AT FS672.20+2 AND S23+2R IAW ASAP EA# AWAC CRJ253-01606 REV IR DATED 4/27/2021.
- [SDR A6WA202104267757](https://openairdocs.org/sdr/A6WA202104267757.md): Skin · dented · Apr 19, 2021 · N462AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN DENT FS654.50+8 STR22+3.5L ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT AT AFT FUSELAGE SKIN DENT FS654.50+8 STR22+3.5L IAW CRJ SRM 53-00-31 REPAIR #3 REV 38.
- [SDR A6WA202104267755](https://openairdocs.org/sdr/A6WA202104267755.md): Skin · dented · Apr 19, 2021 · N462AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN DENT AT FS 691.0 STR 23+2L ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED FUSELAGE DENT AT FS 691.0 STR 23+2L TO ORIGINAL CONTOUR IAW ASAP EA# AWAC-CRJ253-01607 REV IR DATED 4/21/2021.
- [SDR A6WA202104267756](https://openairdocs.org/sdr/A6WA202104267756.md): Skin · dented · Apr 19, 2021 · N462AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN DENT FS 636-638 STR 26+1.5 TO 26+3L ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED 2 DENTS TO ORIGINAL CONTOUR AT FS636-638 STR 26+1.5 TO 26+3L IAW ASAP EA# AWAC CRJ253-01609 REV IR DATED 04/21/2021.
- [SDR A6WA202104237754](https://openairdocs.org/sdr/A6WA202104237754.md): Skin · dented · Apr 19, 2021 · N462AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN DENT LH FS692.5 STR 23+4L ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT AT LH FS693.5 AND STR 23+4L IAW ASAP ENGINEERING REV IR DATED 4/21/2021
- [SDR A6WA202104237753](https://openairdocs.org/sdr/A6WA202104237753.md): Skin · dented · Apr 19, 2021 · N462AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN DENT AT FS580.0 AND STR L20+2.5. ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT AT FS580 LEFT HAND AT STR 20+2.5, PERFORMED HFEC NO INDICATIONS NOTED. REPAIR WITHIN LIMITS REF ASAP EA# AWAC-CRJ253-01608 REV A DATED 4/22/2021.
- [SDR A6WA202102017572](https://openairdocs.org/sdr/A6WA202102017572.md): Control Handle · faulted · Jan 29, 2021 · N462AW · Cndair CL6002B19 · Landing Gear Door Retract Section
  > AFTER TAKEOFF RECEIVED A SKID INBD CAUTION MSG FOLLOWED BY PARKING BRAKE SOV CAUTION MSG GEAR WOULD NOT RETRACT. Q/W QRH. AFTER SELECTING GEAR DOWN ALL MESSAGES CLEARED. NO GEAR DISAGREE MSG AND ALL INDICATIONS GREEN. GEAR HANDLE WAS IN UP FOR APPROX 7 MIN.
- [SDR A6WA2020010747096](https://openairdocs.org/sdr/A6WA2020010747096.md): Idg · malfunctioned · Jan 6, 2020 · N462AW · Cndair CL6002B19 · AC Generator-Alternator
  > SUPPLEMENTAL, RECEIVED NR 2 GEN CAUTION MESSAGE WITH DISCONNECT INDICATION, ALSO RECEIVED RIGHT WINDOW HEAT CAUTION MESSAGE AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH M ACTION FOR MEL 24-11-01-01 AND PLACED IDG GEN NR 2 ON MEL. PERFORMED FIM RESET PROCED
- [SDR A6WA2019050346594](https://openairdocs.org/sdr/A6WA2019050346594.md): Panel · damaged · May 2, 2019 · N462AW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > PANEL 342BB HAS ONE DAMAGED FASTENER HOLE.
- [SDR A6WA201904306592](https://openairdocs.org/sdr/A6WA201904306592.md): Floorbeam · cracked · Apr 29, 2019 · N462AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE FLOOR INTERCOSTAL AT FS 484 RBL 27-RBL 36 IS CRACKED AT O/B SIDE REPAIRED PRESSURE FLOOR INTERCOSTAL AT FS 484 RBL 27 - RBL 36 IAW ASAP EA#: AWAC-CRJ253-01224 REV IR
- [SDR A6WA201904306591](https://openairdocs.org/sdr/A6WA201904306591.md): Floorbeam · cracked · Apr 29, 2019 · N462AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PRESSURE FLOOR INTERCOSTAL AT FS 484 LBL27-LBL36 IS CRACKED O/B SIDE REPAIRED PRESSURE FLOOR INTERCOSTAL AT FS 484 LBL27-LBL36 IAW ASAP EA# AWAC-CRJ253-01225 REV 1R
- [SDR A6WA201904296588](https://openairdocs.org/sdr/A6WA201904296588.md): Intercostal · cracked · Apr 27, 2019 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR UPPER AFT INTERCOSTAL CRACKED REMOVED AND REPLACED PASSENGER DOOR UPPER AFT INTERCOSTAL IAW CRJ 200 SRM 51-42-06 + 51-42-21
- [SDR A6WA201904296587](https://openairdocs.org/sdr/A6WA201904296587.md): Intercostal · cracked · Apr 27, 2019 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR UPPER FOWARD INTERCOSTAL CRACKED REMOVED AND REPLACED PAX DOOR UPPER FWD INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND 51-42-21
- [SDR A6WA201904296583](https://openairdocs.org/sdr/A6WA201904296583.md): Retainer · cracked · Apr 26, 2019 · N462AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > PANEL 422AT HAS CRACKED SEAL RETAINER REPAIRED CRACKED SEAL RETAINER ON PANEL 422AT IAW CRJ 200 SRM 51-71-59
- [SDR A6WA201904296586](https://openairdocs.org/sdr/A6WA201904296586.md): Bracket · cracked · Apr 26, 2019 · N462AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT CARGO DOOR BEAM MEMBER AFT BRACKET CRACKED REMOVED AND REPLACED AFT CARGO DOOR BEAM MEMBER AFT BRAKCET IAW CRJ 200 SRM 51-42-21
- [SDR A6WA201904296585](https://openairdocs.org/sdr/A6WA201904296585.md): Intercostal · cracked · Apr 26, 2019 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BAGGAGE DOOR LINTEL INTERCOSTAL CRACKED REPAIRED LINTEL INTERCOSTAL IAW BOMBARDIER REO# 601R-53-61-1230 REV F
- [SDR A6WA20190426575](https://openairdocs.org/sdr/A6WA20190426575.md): Seat Track · corroded · Apr 25, 2019 · N462AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 SEAT TRACK CORRODED. REPLACED RBL9 SEAT TRACK #4 IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR A6WA20190426578](https://openairdocs.org/sdr/A6WA20190426578.md): Shim · damaged · Apr 25, 2019 · N462AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > GS621 APB REPAIR AT BAGGAGE DOOR LINTEL, POCKET SHIM DAMAGED AT ONE OFF NON REPAIR BLIND FASTENER USED TO ATTACH POST TO BULKHEAD LINERS. REPLACED LINTEL FITTING REPAIR POCKET SHIM IAW REO 601R-53-61-1230 REV-F.
- [SDR A6WA20190426582](https://openairdocs.org/sdr/A6WA20190426582.md): Stiffener · cracked · Apr 25, 2019 · N462AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS409+128 BULKHEAD VERTICAL POST AT LBL 18.0 O/B STIFFENER IS CRACKED AT BOTTOM FASTENER HOLE. REPAIRED VERTICAL POST STIFFENER IAW REO 601R-53-41-056 REV-E.
- [SDR A6WA20190426577](https://openairdocs.org/sdr/A6WA20190426577.md): Seat Track · corroded · Apr 25, 2019 · N462AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 SEAT TRACK #3 CORRODED. REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11-000-802, 53-01-11-400-802.
- [SDR A6WA20190426576](https://openairdocs.org/sdr/A6WA20190426576.md): Seat Track · corroded · Apr 25, 2019 · N462AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 SEAT TRACK #4 CORRODED AT FS559.00+4 TO 559.00+86. REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11-000-802, 53-01-11-400-802.
- [SDR A6WA201904296589](https://openairdocs.org/sdr/A6WA201904296589.md): Rib · cracked · Apr 24, 2019 · N462AW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RH WING LEADING EDGE 630JL RIB IS CRACKED AT WS 247.95 REMOVED AND REPLACED RH WING LEADING EDGE RIB AT WS 247-95 IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-10
- [SDR A6WA20190426580](https://openairdocs.org/sdr/A6WA20190426580.md): Vertical Support · cracked · Apr 24, 2019 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STA 409+128 VERTICAL POST CRACKED IN RADIUS. REPLACED VERTICAL POST IAW REO601R-53-41-889 REV-D AND CRJ200 SRM 51-42-06.
- [SDR A6WA20190426581](https://openairdocs.org/sdr/A6WA20190426581.md): Stiffener · cracked · Apr 24, 2019 · N462AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS621.00 APB HORIZONTAL STIFFENER O/B OF LBL36.20 IS CRACKED. REPLACED STIFFENER IAW CRJ 200 SRM 51-42-06.
- [SDR A6WA20190426579](https://openairdocs.org/sdr/A6WA20190426579.md): Vertical Support · cracked · Apr 24, 2019 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STA 409+128 BL0, VERTICAL POST HAS A CRACK ON L/H SIDE AFT ANGLE, WL69. REPLACED VERTICAL POST IAW REO 601R-53-41-899 REV-D, CRJ200 SRM 51-42-06.
- [SDR A6WA201900426574](https://openairdocs.org/sdr/A6WA201900426574.md): Channel · cracked · Apr 24, 2019 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CHANNEL BEHIND HYD. SYS. 2 PRESSURE/RETURN MANIFOLD IS CRACKED. REPAIRED CHANNEL IAW REO 601R-53-62-031 REV-A.
- [SDR A6WA201904236573](https://openairdocs.org/sdr/A6WA201904236573.md): Door Frame · cracked · Apr 23, 2019 · N462AW · Cndair CL6002B19 · Fuselage Main, Structure
  > AFT CARGO DOOR CUTOUT FRAME AT STR 9L HAS 2 CRACKS. REPAIRED FRAME IAW REO 601R-53-61-5214 REV-A.
- [SDR A6WA201904226572](https://openairdocs.org/sdr/A6WA201904226572.md): Seat Track · corroded · Apr 20, 2019 · N462AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK #4 HAS CORROSION THE ENTIRE LENGTH OF THE TRACK, RBL9 REMOVED AND REPLACED #4 SEAT TRACK AT RBL 9 IAW CRJ 200 AMM 53-01-11
- [SDR A6WA201904226570](https://openairdocs.org/sdr/A6WA201904226570.md): Retainer · cracked · Apr 20, 2019 · N462AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > PANEL 442BT CRACKED SEAL RETAINER REMOVED AND REPLACED CRACKED SEAL RETAINER IAW CRJ 200 SRM 51-42-06
- [SDR A6WA201904226571](https://openairdocs.org/sdr/A6WA201904226571.md): Seat Track · corroded · Apr 20, 2019 · N462AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK #1 RBL 9 HAS CORROSION THE ENTIRE LENGTH OF THE TRACK REMOVED AND REPLACED SEAT TRACK #1 LOCATION RBL9 IAW CRJ 200 AMM 53-01-11
- [SDR A6WA201904196569](https://openairdocs.org/sdr/A6WA201904196569.md): Floor Support · cracked · Apr 19, 2019 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SUPPORT INTERCOSTAL OUTBD CLIP AT FS484 RBL 36 CRACKED. REPLACED
- [SDR A6WA201904196568](https://openairdocs.org/sdr/A6WA201904196568.md): Angle · cracked · Apr 17, 2019 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PREVIOUS REPAIR ANGLE AFT FACE OF STA 280 AND RBL 12 CRACKED. REPLACED
- [SDR A6WA201904196565](https://openairdocs.org/sdr/A6WA201904196565.md): Skin · cracked · Apr 16, 2019 · N462AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LOWER CLOSE OUT SKIN IS CRACKED UNDER TOP FOLDING STEP. REPAIRED
- [SDR A6WA201904196566](https://openairdocs.org/sdr/A6WA201904196566.md): Angle · cracked · Apr 16, 2019 · N462AW · Cndair CL6002B19 · Fuselage, Stabilizer Attach Fittings
  > RH OVER WING BL 45 FS 473 REINFORCING ANGLE CRACKED. REPLACED
- [SDR A6WA201904196567](https://openairdocs.org/sdr/A6WA201904196567.md): Angle · cracked · Apr 16, 2019 · N462AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LH OVER WING BL 45 FS 473 REINFORCING ANGLE CRACKED. REPLACED

Next page: https://openairdocs.org/aircraft/N462AW/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 = 'N462AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N462AW/reports

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