# SDR A6WA202112238044

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 23, 2021
- Submitted: December 23, 2021
- Operation: Air carrier
- Aircraft: [N435AW](https://openairdocs.org/aircraft/N435AW), registered now
- Make and model: Cndair CL6002B19
- Aircraft serial: 7724
- Aircraft time: 39,961 hours, 38,675 cycles
- System (JASC): [5532 · Vertical Stabilizer, Plate/Skin](https://openairdocs.org/jasc/5532)
- Part: None
- Part number: 60021024
- Part serial: NSN
- Condition: Gouged
- Location: Vertical Stabili
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/A6WA202112238044

## Discrepancy

MAINTENANCE FOUND 4 EACH SCRATCHES ON VERTICAL STABILIZER R/H SIDE COMMON TO ACCESS PANEL 325CR. DIMENSIONS OF SCRATCHES ARE: (P1) =  2.500"L X 0.800"W X 0.006"D AND (P2) = 3.00"L X 1.400"W X .007"D (P3) = 1.500"L X 1.300"W X .004"D (P4) = 1.500"L X .500"W X .005"D (P5) = 1.500"L X 1.00"W X .003"D. (P3) WAS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-31-31 REVISION 38. (P1,P2,P4, AND P5) ARE NOT    WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 55-31-31 REVISION 38.  ************AIRCRAFT REMOVED FROM SERVICE*************************  BLENDED DAMAGED AREAS TO A SMOOTH CONTOUR. (P1) AND (P2) BLENDS DID NOT SURPASS  REMAINING MATERIAL THICKNESS OF .093". ORIGINAL THICKNESS OF .100". (P4) AND (P5) BLENDS DID NOT SURPASS REMAINING MATERIAL THICKNESS OF .035" ORIGINAL THICKNESS OF .040." HFEC INSPECTION PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01769 REV A DATED 12/04/2021. WORK COMPLETED ON AERSALE WO #003486 CARD #20474 AT AERSALE CRS #4AER685B. N435AW TT:39,961 TC:38,675.

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