N922
Registered owner: TJK ENTERPRISES LLC, MT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| WILLIAM R & KATHRYN A. RHYMER | Operator | on 1982-08-22 | Operator named in NTSB report |
Accident & incident history
Operated by WILLIAM R & KATHRYN A. RHYMER (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
37 reports on file, 2019-03-27 – 2021-06-25.
Part: INTERCOSTAL — CORRODED (BS349-364 S27L) · airframe 39,794 hrs · 31,994 cycles
FORWARD E&E BAY INTERCOSTAL CORRODED AT STGR 27L FS 349|R&R INTERCOSTAL IAW SRM 51-42-06
Part: SKIN — DENTED (BS 437 S22L) · airframe 39,794 hrs · 31,994 cycles
FUS FWD LH FS437 AREA NEAR STR 22L IS DENTED|REPAIRED SKIN STA 437 NEAR STR 27L IAW SRM 53-00-01
Part: INTERCOSTAL — CORRODED (BS 364 S27L) · airframe 39,794 hrs · 31,994 cycles
INTERCOSTAL IN E+E BAY CORRODED AT STGR 27L AT FS364 |REMOVED CORROSION ON INTERCOSTAL IN E+E BAY AT STGR 27L AT FS364 IAW SRM 51-42-06
Part: TRACK — DAMAGED (AFT CARGO DOOR) · airframe 39,794 hrs · 31,994 cycles
AFT BAGGAGE BAY FWD DOOR TRACK HAS DAMAGE AND BARE METAL|R&R AFT BAGGAGE BAY DOOR TRACK IAW REO 670-53-62-102
Part: INTERCOSTAL — CORRODED (BS 319-349 S20R) · airframe 39,794 hrs · 31,994 cycles
FWD E&E BAY INTERCOSTAL CORRODED RH SIDE FS319-FS333 STGR 20R|R&R INTERCOSTAL IAW SRM 51-42-06
Part: STRINGER — CORRODED (BS 284 S27) · airframe 39,794 hrs · 31,994 cycles
STGR 27 FWD CORRODED AT FS284| R&R STGR 27 FWD AT FS284 IAW SRM 51-42-06 AND SRM 51-42-21
Part: INTERCOSTAL — CORRODED (BS 319-333) · airframe 39,794 hrs · 31,994 cycles
FWD E&E BAY INTERCOSTAL CORRODED RH SIDE FS319-FS333|R&R INTERCOSTAL IAW SRM 51-42-06
Part: POST — CORRODED (COCKPIT DOOR) · airframe 39,794 hrs · 31,944 cycles
R/H FLIGHT COMPARTMENT DOOR POST CORRODED|R&R FABRICATED REPAIR PARTS IAW SRM 53-00-00
Part: FLOOR SUPPORT — CORRODED (BS 281 RBL 11) · airframe 39,794 hrs · 31,994 cycles
R/H FLIGHT COMPARTMENT FLOOR PANEL SUPPORT GUSSET CORRODED|R&R FLOOR SUPPORT GUSSET IAW SRM 51-42-06
Part: FRAME — CORRODED (FS310 S26L-R) · airframe 39,794 hrs · 31,994 cycles
FORWARD E&E BAY FRAME AT FS310 STGR 26L AND 26R |REMOVED AND REPAIRED FRAME SECTOR FS310 BETWEEN STGR 25R AND 25L IAW SRM 53-00-06
Earlier reports · 2019 · 27 reports
2019
Part: SEAL — TORN (EMERGENCY EXIT) · airframe 27,177 hrs · 17,910 cycles
"INITIAL INSPECTION: TORN SEAL ON FLAP FAIRING NBR. 597BB AT LH WING. AI) " "SUMMARY: SEAL ON FLAP FAIRING NBR. 597BB AT LH WING WAS CLEANED PER C RJ900 SRM 51-26-00-001-001-A01. AFTER OF CLEANNESS THE SEAL WAS INSPEC TED PER CRJ 900 SRM 51-11-00-001-001-A01 2.A. THE SEAL NO PRESENTS DAM AGE. "
Part: FLOORBEAM — CORRODED (BS 280) · airframe 27,177 hrs · 17,910 cycles
"AWR; HIDDEN CRACK: [ DURING 280 RH FLOOR BEAM REMOTION RELATED WITH NR C 00141, A STIFFENER OF COCKPIT BULKHEAD, FWD FACE WAS FOUND CRAKED ]: CRACKED STIFFENER IN STA. FS= 280 AND 26RBL AND WL= 70 AT PAX CABIN F WD WET AREA. (W1) (CPAX) " "STIFFENER IN STA. FS= 280 AND 26RBL AND WL= 70 AT PAX CABIN FWD WET AR EA WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 "
Part: FITTING — CORRODED (NLG DOOR) · airframe 27,177 hrs · 17,910 cycles
"INITIAL INSPECTION: FREE PLAY ON BOTH LOWER ROD END LINKS [LH/RH ] AT NLG AFT DOOR. (FYT) " "SUMMARY OF NRC 163: HARDWARE ON NLG AFT DOOR WERE REPLACED PER CRJ 900 AMM 32-22-05 AND ALTERNATE EXTENSION TEST AND CLEARANCE CHECK WILL BE COMPLETED WITH TASK 900-32-710-902. FREE PLAY WAS CORRECTED "
Part: STIFFENER — CORRODED (BS 280) · airframe 27,177 hrs · 17,910 cycles
"AWR; HIDDEN CRACK: [ DURING 280 RH FLOOR BEAM REMOTION RELATED WITH NR C 00141, A STIFFENER OF COCKPIT BULKHEAD, FWD FACE WAS FOUND CRAKED ]: CRACKED STIFFENER IN STA. FS= 280 AND 26RBL AND WL= 70 AT PAX CABIN F WD WET AREA. (W1) (CPAX) " "STIFFENER IN STA. FS= 280 AND 26RBL AND WL= 70 AT PAX CABIN FWD WET AR EA WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 "
Part: ANGLE — CORRODED (BS 310-349) · airframe 27,177 hrs · 17,910 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON MIDDLE C AP ANGLE IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LO WER SILL, FWD WET AREA. (W1) (CPAX) " "LEVEL CORROSION 2. MIDDLE CAP ANGLE IN STA. FS= 310 TO FS= 349 AND 41 LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA WAS REPLACED PER CR J 900 SRM 51-42-02-001-001-A01. "
Part: SUPPORT — CORRODED (BS 319-349) · airframe 27,177 hrs · 17,910 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON CAP ANGL E IN STA. FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOWER SI LL, FWD WET AREA. (W1) (CPAX) " "LEVEL CORROSION 2. CAP ANGLE IN STA. FS= 319 TO FS= 349 AND 44RBL AT G ALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REPLACED PER CRJ-900 S RM 51-42-06-001-001-A01 PAR 6 AND CRJ900 SRM 51-42-20-001-001-A01 PAR. 6. "
Part: SUPPORT — CORRODED (BS 319-349) · airframe 27,177 hrs · 17,910 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON SUPORT M OUNTING ANGLE IN STA. FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICE D OOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "LEVEL CORROSION 2. SUPORT MOUNTING ANGLE IN STA. FS= 319 TO FS= 349 AN D 41RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REPLACED P ER CRJ-900 SRM 51-42-06-001-001-A01 PAR 6 AND CRJ900 SRM 51-42-20-001- 001-A01 PAR. 6. "
Part: SUPPORT — CORRODED (BS 329) · airframe 27,177 hrs · 17,910 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTI ON PLATE SUPPORT IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SER VICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "SUMMARY: PROTECTION PLATE SUPPORT IN STA. FS= 329 BETWEEN 41RBL TO 44R BL WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 PAR. 6 "
Part: SUPPORT — CORRODED (BS 319-349) · airframe 27,177 hrs · 17,910 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON LOWER S RIKER IN STA. FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOW R SILL, FWD WET AREA. (W1) (CPAX) " "LEVEL CORROSION 2. LOWER STRIKER IN STA. FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA WAS REPLACED PER CRJ90 0 SRM 51-42-06-001-001-A01 PAR. 6 AND CRJ900 SRM 51-42-20-001-001-A01 "
Part: SUPPORT — CORRODED (BS 346) · airframe 27,177 hrs · 17,910 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTI ON PLATE SUPPORT IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERV ICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "LEVEL CORROSION 2. PROTECTION PLATE SUPPORT IN STA. FS= 346 BETWEEN 41 RBL TO 44RBL WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 PAR. 6 A ND CRJ900 SRM 51-42-20-001-001-A01 "
Part: FLOORBEAM — CORRODED (BS 339) · airframe 27,177 hrs · 17,910 cycles
"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTI ON PLATE SUPPORT IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERV ICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "LEVEL CORROSION 2. PROTECTION PLATE SUPPORT IN STA. FS= 339 BETWEEN 41 RBL TO 44RBL WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 PAR. 6 "
Part: FLOORBEAM — CORRODED (BS 280) · airframe 27,177 hrs · 17,910 cycles
"INITIAL INSPECTION: CORROSION ON FLOOR PANEL SUPPORT ANGLE OF ACCESS P ANEL 221ALF IN STA. FS= 280 BETWEEN 11 LBL/RBL AT COCKPIT. (CPIL) TCI 53-10-219 " "SUMMARY: AREA WAS MEASURED AND FOUND WITH DIMENSIONS AS FOLLOW; ORIGIN AL THICKNESS: 0.063"" MAXIMUM DEPTH: 0.025"" THEREFORE IS OUT LIMITS PER CRJ/900 SRM 53-00-00-101-001-A01 PAR. 4 A. IT MUST BE REPLACED PER CR J900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01. // USED EQUIPMENT: DIAL INDICATOR P/N: 543-783 DATE EXP. 16/JUL/19 N/C:23 80 RCG FLOOR PANEL SUPPORT ANGLE OF ACCESS PANEL 221ALF IN STA. FS= 28 0 BETWEEN 11 LBL/RBL AT COCKPIT. WAS REPLACED PER CRJ900 SRM 51-42-06- 001-001-A01 PAR. 6. D. AND CRJ900 SRM 51-42-21-001-001-A01. PAR. 6 "
Part: STRINGER — CORRODED · airframe 27,177 hrs · 17,910 cycles
CORROSION ON STRINGER SPLICE 25RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09. STRINGER SPLICE 25RH AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-20-001-001-A01.
Part: STRINGER SPLICE — CORRODED (BS 327-337) · corrosion level 2 · airframe 27,177 hrs · 17,910 cycles
CORROSION ON STRINGER SPLICE 25LH AT MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-20-001-001-A01. "
Part: STRINGER SPLICE — CORRODED (BS 327-337) · corrosion level 2 · airframe 27,177 hrs · 17,910 cycles
"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION: CORROSION ON STRINGER SPLICE 24RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09. STRINGER SPLICE 24RH AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A01 AND CRJ900 SRM 5-42-20-001-001-A01.
Part: DOUBLER — CORRODED (BS 295-310) · airframe 27,177 hrs · 17,910 cycles
CORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. THE PRODUCTION DOUBLER WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A01 PAR. 6.
Part: STRINGER — CORRODED (BS 337-364) · airframe 27,177 hrs · 17,910 cycles
"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION. CORROSION ON STRINGER 25 RH IN STA. FS= 337 TO FS= 364 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TA SK 900-53-140-300 APPENDIX A ] TCI: 100-09 " "LEVEL CORROSION 2. STRINGER 25RH IN STA. FS= 337 TO FS= 364 AT MAIN AV IONICS COMPARTMENT WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A0 1 AND CRJ900 SRM 51-42-20-001-001-A01. "
Part: STRINGER — CORRODED (BS 280-327) · corrosion level 2 · airframe 27,177 hrs · 17,910 cycles
CORROSION ON STRINGER 25RH IN STA. FS= 280 TO FS= 327 BETWEEN AT MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-20-001-001-A01.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 27,177 hrs · 17,910 cycles
"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION: CORROSION ON INTERCOSTAL S (4 EAS) IN STA. FS= 349 TO FS= 364 BETWEEN STRG 26LH TO 26RH AT MAI N AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09 " "LEVEL CORROSION 2. INTERCOSTALS (4 EAS) IN STA. FS= 349 TO FS= 364 BET WEEN STRG 26LH TO 26RH WERE REPLACED PER CRJ-900 S.R.M. 51-42-06-001-0 01-A01 AND CRJ900 SRM 51-42-20-001-001-A01. "
Part: STRINGER SPLICE — CORRODED (BS 327-337) · corrosion level 2 · airframe 27,177 hrs · 17,910 cycles
[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION: CORROSION ON STRINGER SPLICE 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09. STRINGER SPLICE WAS REPLACED PER S.R.M. 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-20-001-001-A01.
Part: STRINGER — CORRODED (BS 337-364) · airframe 27,177 hrs · 17,910 cycles
"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION. CORROSION ON STRINGER 26 RH IN STA. FS= 337 TO FS= 364 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TA SK 900-53-140-300 APPENDIX A ] TCI: 100-09 " "LEVEL CORROSION 2. STRINGER 26RH IN STA. FS= 337 TO FS= 364 AT MAIN A VIONICS COMPARTMENT WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A 01 AND CRJ900 SRM 51-42-20-001-001-A01. "
Part: INTERCOSTAL — CORRODED (BS 649-364) · airframe 27,177 hrs · 17,910 cycles
"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION: CORROSION ON INTERCOSTAL S (4 EAS) IN STA. FS= 349 TO FS= 364 BETWEEN STRG 26LH TO 26RH AT MAI N AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09 " "LEVEL CORROSION 2. INTERCOSTALS (4 EAS) IN STA. FS= 349 TO FS= 364 BET WEEN STRG 26LH TO 26RH WERE REPLACED PER CRJ-900 S.R.M. 51-42-06-001-0 01-A01 AND CRJ900 SRM 51-42-20-001-001-A01. "
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 27,177 hrs · 17,910 cycles
"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION: CORROSION ON INTERCOSTAL S (4 EAS) IN STA. FS= 349 TO FS= 364 BETWEEN STRG 26LH TO 26RH AT MAI N AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09 " "LEVEL CORROSION 2. INTERCOSTALS (4 EAS) IN STA. FS= 349 TO FS= 364 BET WEEN STRG 26LH TO 26RH WERE REPLACED PER CRJ-900 S.R.M. 51-42-06-001-0 01-A01 AND CRJ900 SRM 51-42-20-001-001-A01. "
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 27,177 hrs · 17,910 cycles
"[ IN REFERENCE NRC 0046 ] INITIAL INSPECTION: CORROSION ON INTERCOSTAL S (4 EAS) IN STA. FS= 349 TO FS= 364 BETWEEN STRG 26LH TO 26RH AT MAI N AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09 " "LEVEL CORROSION 2. INTERCOSTALS (4 EAS) IN STA. FS= 349 TO FS= 364 BET WEEN STRG 26LH TO 26RH WERE REPLACED PER CRJ-900 S.R.M. 51-42-06-001-0 01-A01 AND CRJ900 SRM 51-42-20-001-001-A01. "
Part: FRAME — CORRODED (BS 349) · airframe 27,177 hrs · 17,910 cycles
CORROSION ON FRAME FS= 349 BETWEEN STRG 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TAS K 900-53-140-300 APPENDIX A ] TCI: 100-09, CORROSION ON FRAME FS= 349 BETWEEN STRG 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ-900 SRM 53-00-06-201-005-A01 AND SRM 51-21-06-001-001-A01.
Part: PLATE — CORRODED (BS 322) · airframe 27,177 hrs · 17,910 cycles
WR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBL TO 4RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) LEVEL CORROSION 2; PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41 RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 PAR. 6
Part: TRIPLER — GOUGED (BS 917-919) · airframe 27,177 hrs · 17,910 cycles
INITIAL INSPECTION: GOUGE ON PREVIOUS REPAIR TRIPLER IN STA. FS= 917 TO FS= 919.5 NEAR STGR 27 AT FUSELAGE SKIN. (FUS) SKIN TO STA. FS= 917 TO FS= 919.5 NEAR STGR 27 AT FUSELAGE SKIN WAS REPAIRED, PER CRJ-900 REO 670-53-00-290 REV.F