N183GJ
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
74 reports on file, 2015-08-30 – 2025-08-23.
Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 25,350 hrs · 21,588 cycles
EMERGENCY LIGHTS ON WITH THE SWITCH IN THE OFF POSITION R/R EMERGENCY LIGHT SWITCH IAW CRJ900 ESPM 20-45-51. FAILED OPS CHECK OF EMERGENCY LIGHT SWITCH. R/R EMERGENCY LIGHTS POWER SENSE RELAY IAW CRJ900 ANN 33-51-19 FAILED OPS CHECK. R/R EMERGENCY BATT ASSYS AT POSITIONS PS36, PS37, PS38, AND PS43. PER JOBCARD 33-900-701. REQUIRES OPS CHECK AT THIS TIEM. PERFORMED OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00 OPS TEST FAIL, LIGHTS STILL ON. R/R #1 BATTERY CHARGER ASSY & BATTERY IAW AMM 33-51-17, OIPS TEST GOOD. EMERGENCY LIGHT TURN OFF AND ON WITH SWITCH.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 24,787 hrs · 21,140 cycles
DURING L/C FOUND PS37 BATTERY INOP AND EMER LIGHTS WONT TURN ON R/R PS37 IAW AMM 33-51-17 OPS CKS GOOD .
Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 24,787 hrs · 21,140 cycles
EMERGENCY EXIT LIGHTS STAYS ON WHILE SWITCH IS IN THE OFF POSITION AND COMES OFF IN THE ARM POSITION. R/R PS35 BATTERY CHARGER IAW AMM 33-51-17 OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
Part: SIGN — INOPERATIVE (ZONE 200) · airframe 24,735 hrs · 21,093 cycles
OVERWING CEILING EMERGENCY LOCATING SIGN FACING AFT IS INOP RECHARGED EMERGENCY LIGHTS BATTERIES IAW CMM 26-60-03. OPS CHECKS GOOD IAW AMM 33-51-00.
Part: LATCH — INOPERATIVE (ZONE 800) · airframe 24,638 hrs · 21,004 cycles
PASSENGER DOOR JAMMED, WOULD NOT OPEN. R/R PASSENGER DOOR (OUTER) DOOR LATCH SPIGOT ASSY IAW AMM 53-21-23. OPS CHECK GOOD
Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 24,488 hrs · 20,895 cycles
DURING WAKE-UP FOUND PAX DOOR EXTERIOR EMERGENCY LIGHT INOP, & OVERHEAD LH & RH GALLEY EXIT SIGN INOP. FOUND 0 VOLTS PRESENT ON PLUG P336 PINS 1 & 2 ON CEILING PANEL. REMOVED & REPLACED BATTERY CHARGER ASSY IN PS35 POSITION IAW 900 AMM 33-51-17. P/N ON/OFF: 11-0049, S/N ON: 26643, S/N OFF: 22000. OPS CHECK GOOD.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 24,460 hrs · 20,872 cycles
DURING LINE CHECK FOUND FWD EMERGENCY EXIT SIGN ON DIVIDER INOP. R/R PS35 BATTERY AND BATTERY CHARGER IAW J.C 33-900-701. OPS CHECK GOOD. A/C OK FOR SVC.
Part: BRACKET — CORRODED (ZONE 100) · airframe 24,357 hrs · 20,773 cycles
CORROSION ON LIGHT BRACKET (ON FUSELAGE SKIN) AT WATER WASTE PANEL LIGHT BRACKET WAS FABRICATED PER EA CRJ953-18254 REV IR AND REPLACED PER CRJ900 AMM 38-31-08 (CONFIG A01)
Part: STOP — CRACKED (ZONE 800) · airframe 24,357 hrs · 20,773 cycles
CRACK ON AFT STOPPERS OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT AFT STOPPER OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REPLACED PER CRJ900 AMM 53-62-34 (CONFIG A01)
Part: HINGE — CRACKED (ZONE 100) · airframe 24,357 hrs · 20,773 cycles
CRACK ON FWD HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
Part: STOP — CRACKED (ZONE 800) · airframe 24,357 hrs · 20,773 cycles
CRACK ON FWD STOPPER OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD STOPPER OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REPLACED PER CRJ900 AMM 53-62-34 (CONFIG A01)
Part: HINGE — CRACKED (ZONE 100) · airframe 24,357 hrs · 20,773 cycles
CRACK ON MIDDLE HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT MID HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
Part: HINGE — CRACKED (ZONE 100) · airframe 24,357 hrs · 20,773 cycles
CRACK ON AFT HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT AFT HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 24,357 hrs · 20,773 cycles
CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE 67.5% REAR SPAR DATUM. RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
Part: ANGLE — CORRODED (ZONE 200) · airframe 24,357 hrs · 20,773 cycles
COROSION ON LOWER SILL ANGLE BTW FS 319.00/FS349.00 COROSION ON LOWER SILL ANGLE BTW FS 319.00/FS349.00 WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-002-A01 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-34-001-001-A01
Part: ANGLE — CORRODED (ZONE 200) · airframe 24,357 hrs · 20,773 cycles
DURING SILL REMOVAL IN REF NRC 093, CORROSION ON ANGLE MID CAP WAS FOUND CORROSION ON ANGLE MID CAP WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 THEREFORE WAS REPLACED ON NRC 0093
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 24,357 hrs · 20,773 cycles
CORROSION ON PASSENGER SEAT RAILS RBL9 AND LBL9 BTW FS 661.00+90 AND 693.00 AT PASSENGER CABIN. DUE TO EXCESIVE CORROSION AT SEAT TRACK 9RBL AND 9LBL OF FS 661 TO FS 693 AT PASSENGER CABIN WERE REPLACED PER CRJ-900 SRM53-21-49-101-001-A01 AND CRJ-900 AMM 53-00-49 (CONFIG A07)
Part: BEAM — CORRODED (ZONE 200) · airframe 24,357 hrs · 20,773 cycles
CORROSION ON UPPER FACE AT TRANSVERSE BEAM FS 333.00 BTW LBL 9 TO LBL 27 UPPER FACE AT TRANSVERSE BEAM FS 333.00 BTW LBL 9 TO LBL 27 WAS REPAIRED PER REO 690-53-21-1887 REV --
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 24,357 hrs · 20,773 cycles
CORROSION ON RH/LH SEAT TRACK FS349-FS379 9RBL AND FS374-FS384 9LBL AT PASSENGER CABIN CORROSION AT SEAT TRACK FS349-FS484 9RBL AND FS- 374-FS485 9LBL AT PASSENGER CABIN WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49-000-801 CONFIG A07, CRJ-900 SRM 51-41-02-001-001-A01 AND AMM 20-21-00-910-801(CONF A01)
Part: STIFFENER — CRACKED · airframe 24,357 hrs · 20,773 cycles
AFTER REMOVAL OF ACCESS PANEL 621AT CRACK WAS FOUND ON SUPPORT BRACKET CRACK ON STIFFENER SS 21.50 WAS REPAIRED PER CRJ 900 SRM 51-71-59-001-001-A01
Part: FAIRING — CORRODED (ZONE 100) · airframe 24,357 hrs · 20,773 cycles
CORROSION ON SETTLEMENT AREA OF THE WING TO FUSELAGE FAIRING 195AL, 195DL, 196AR AND 196DR. CORROSION ON SETTLEMENT AREA OF THE WING TO FUSELAGE FAIRING 195AL, 195DL, 196AR AND 196DR WAS EVALUATED WITHIN LIMITS PER CRJ-900 SRM 53-00-01-101-001 AND SRM 53-51-01-101-003-A04 AND PER CRJ-900 SRM 53-00-00-101-001-A01, STARP ON LANDING DOOR WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-82-55-101-002-A02 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND AREAS NOT DAMAGE ALLOWABLE WERE REPAIRED PER EA CRJ953-18253 REV IR AND EA CRJ953-18485 REV. IR
Part: ANGLE — CRACKED (ZONE 300) · airframe 24,357 hrs · 20,773 cycles
CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
Part: DOOR SILL — CORRODED (ZONE 200) · airframe 24,357 hrs · 20,773 cycles
CORROSION ON LOWER SILL AT SERVICE DOOR EXTERNAL SURROUND STRUCTURE. CORROSION ON LOWER SILL AT SERVICE DOOR EXTERNAL SURROUND STRUCTURE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
Part: DOOR SILL — CORRODED (ZONE 200) · airframe 24,357 hrs · 20,773 cycles
CORROSION ON LOWER SILL AT PASSENGER DOOR SURROUND STRUCTURE. LOWER SILL AT PASSENGER DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 24,357 hrs · 20,773 cycles
CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUMWAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
Part: DIAPHRAGM — CRACKED (ZONE 100) · airframe 24,357 hrs · 20,773 cycles
CRACK IN LH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35RBL/LBL AT LH MLG WHEEL WELL. LH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35RBL/LBL AT LH MLG WHEEL WELL WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
Part: DIAPHRAGM — CRACKED (ZONE 100) · airframe 24,357 hrs · 20,773 cycles
CRACK IN RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35RBL/LBL AT RH MLG WHEEL WELL. RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35RBL/LBL AT RH MLG WHEEL WELL WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
Part: STRUCTURE — CORRODED (STATIC WICK) · airframe 24,357 hrs · 20,773 cycles
IN REF TO: DURING INSPECTION OF THE TASK CARD 900-57-900-300 IT WAS DETECTED CORROSION ON STATIC DISCHARGE BASE (4EAS) BTW AILERON AND WING EXTENSION TRAILING EDGE WS370.25 TO WS398.939 AFT OF THE REAR SPAR AT LH/RH WING. CORROSION ON STATIC DISCHARGE BASE (4EAS) BTW AILERON AND WING EXTENSION TRAILING EDGE WS370.25 TO WS398.939 AFT OF THE REAR SPAR AT LH/RH WING WERE REPLACED PER CRJ-900 AMM 57-00-28-960-801-A02
Part: STRUCTURE — CORRODED (STATIC WICK) · airframe 24,357 hrs · 20,773 cycles
IN REF TO: DURING INSPECTION OF THE TASK CARD 900-57-900-300 IT WAS DETECTED CORROSION ON STATIC DISCHARGE BASE (4EAS) BTW AILERON AND WING EXTENSION TRAILING EDGE WS370.25 TO WS398.939 AFT OF THE REAR SPAR AT LH/RH WING. CORROSION ON STATIC DISCHARGE BASE (4EAS) BTW AILERON AND WING EXTENSION TRAILING EDGE WS370.25 TO WS398.939 AFT OF THE REAR SPAR AT LH/RH WING WERE REPLACED PER CRJ-900 AMM 57-00-28-960-801-A02
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 24,323 hrs · 20,745 cycles
EMERGENCY LIGHT AFT OF PAX DOOR INOP R/R EMERGENCY LIGHT AFT OF PAX DOOR IN REF AMM 33-51-15 P/N ON/OFF: 8GH002473-08
Earlier reports · 2015–2024 · 44 reports
2024
Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 24,098 hrs · 20,539 cycles
EMER. LTS IN LOWER FWD GALLEY AND ENTRANCE COMPARTMENT INOP. REMOVED AND REPLACED CHARGER ASSY, BATTERY PER AMM 33-51-17. ALL CHECKS GOOD. P/N OFF/ON 11-0049 S/N OFF 26323 S/N ON 26250
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 23,306 hrs · 19,824 cycles
SEAT TRACK RBL 9 FS 693- 837 IS CORRODED WITH CORRODED HARDWARE THROUGHOUT. REMOVED AND REPLACED IAW CRJ-900 SRM 53-00-49-201-002-A01.
Part: SEAT TRACK — CORRODED (BS 693-837 LBL9) · airframe 23,306 hrs · 19,824 cycles
SEAT TRACK LBL 9 FS 693- 837 IS CORRODED WITH CORRODED HARDWARE THROUGHOUT. REMOVED AND REPLACED IAW CRJ-900 SRM 53-00-49-201-002-A01.
Part: FRAME — CRACKED (RT EMER EXIT) · airframe 23,306 hrs · 19,824 cycles
R/H AFT EMERGENCY EXIT DOOR HAS A VISIBLE CRACK ABOVE AFT UPPER DUG LUG, PN# SH670-36600 SN# SB0863 REPAIRED RH AFT EMERGENCY EXIT IAW ENDEAVOR AIR EA CRJ952-16767 REV IR DATED 6/13/2024, REF, ENDEAVOR AIR DTA # 916531,
Part: DOOR — CRACKED (LT EMER EXIT) · airframe 23,306 hrs · 19,824 cycles
L/H AFT EMERGENCY EXIT DOOR HAS A VISIBLE CRACK BELOW AFT UPPER LUG, PN# SH670-36600 SN# SB0862 REPAIRED LH AFT EMERGENCY EXIT IAW ENDEAVOR AIR EA CRJ952-16766 REV IR DATED 6/13/2024, REF, ENDEAVOR AIR DTA # 916532,
2021
Part: BRACKET — CRACKED (CARGO LIGHT) · airframe 17,789 hrs · 15,125 cycles
THE CENTER CARGO COMPARTMENT LIGHT FIXTURE HAS A CRACKED BRACKET - REMOVED AND REPLACED CENTER CARGO COMPARTMENT LIGHT FIXTURE BRACKET IAW CRJ 900 SRM 51-41-02.
Part: ATTACH FITTING — CHAFED (PAX DOOR) · airframe 17,789 hrs · 15,125 cycles
PAX DOOR FORWARD LOWER TUBE ATTACHMENT FITTING CHAFFED FORWARD PULLING LEVER - REMOVED AND REPLACED PAX DOOR FWD LWR TUBE ATTACHMENT PULL-IN LEVER FITTING IAW BOMBARDIER CRJ 900 AMM 52-11-02.
Part: DOOR FRAME — NICKED (CENTER CARGO) · airframe 17,789 hrs · 15,125 cycles
CENTER BAGGAGE BAY SURROUND LOCK/LATCH RECEIVERS HAVE SMALL KNICKS FROM LATCHES JC: 900-500-810-306 - BLENDED OUT DAMAGE ON LATCH RECEIVERS OF CENTER BAGGAGE BAY SURROUND LOCK IAW CRJ 900 SRM 51-12-00 AND CHECKED LIMITS FOUND TO BE WITHIN LIMITS IAW CRJ 900 SRM 53-31-23. TREATED,PRIMED, AND APPLIED TOP COAT IAW CRJ 900 SRM 51-21-11, 21-25-06 AND 51-25-16
Part: LINTEL — CRACKED (BS 280-295 S3L) · airframe 17,789 hrs · 15,125 cycles
F.S. 280-295 DOOR LINTEL STR 3L IS CRACKED JUST AFT OF F.S. 280 - REFERANCE EO# R53568 (WILL SUBMIT ADDITIONAL FORM WITH CORRECTIVE ACTION)
Part: STRINGER SPLICE — CORRODED (BS 333 S26L) · airframe 17,789 hrs · 15,125 cycles
STRINGER SPLICE AT 26L AT FS333 IS CORRODED JC: 900-53-140-500 - REMOVED & REPLACED STGR SPLICE @ 26L @ FS333 IAW CRJ900 SRM 51-42-06
Part: STRINGER SPLICE — CORRODED (BS 333 S25L) · airframe 17,789 hrs · 15,125 cycles
STRINGER SPLICE @25L @FS333 IS CORRODED JC: 900-53-140-500 - REMOVED @ REPLACED STRG SPLICE @25L @FS333 IAW CRJ900 SRM 51-42-06.
Part: STRINGER — CORRODED (BS 295-310 S25L) · airframe 17,789 hrs · 15,125 cycles
STRINGER 25L BETWEEN FS295 AND FS310 IS CORRODED JC:900-53-140-500 - REMOVED & REPLACED STGR 25L BTW FS 280 TO FS 333 IAW CRJ 900 SRM 51-42-06- &51-42-20
Part: INTERCOSTAL — CORRODED (BS 349-364 S27R) · airframe 17,789 hrs · 15,125 cycles
INTERCOSTAL RIGHT OF STRINGER 27 BETWEEN FS.349 AND FS364 HAS CORROSION IOB CODE:900-53-140-500 - REMOVED & REPLACED RIGHT INTERCOSTAL OF STRINGER 27 BETWEEN FS349 & FS 364 IAW CRJ900 SRM51.42.06 & SRM51.42.20.
Part: HOUSING — CRACKED (E/E BAY DOOR) · airframe 17,789 hrs · 15,125 cycles
AVIONICS BAY DOR HANDLE HOUSING CRACKED, VERIFIED BY NDT JC: 900-52-810-901 - REPLACED AVIONICS BAY DOOR HANDLE HOUSING IAW CRJ900 SRM 51-42-00 AND CRJ900 AMM 52-42-03
Part: SEAT TRACK — CRACKED (BS 881) · airframe 17,789 hrs · 15,125 cycles
LH SIDE AT FS 881 HAS DAMAGE BELOW SIDE SEAT TRACK 900-53-900-120 - REPAIRED PER EA NO CRJ953-11812 REV IR ISSUE DATE 7/11/2021 TO SEAT SIDE TRACK AT FS 881
Part: SKIN — GOUGED (LT NACELLE) · airframe 17,789 hrs · 15,125 cycles
LEFT ENGINE LOWER AFT COWL HAS MULTIPLE GOUGES AND CHAFFED SPOTS JC:900 54-900-102 - REPAIRED DAMAGE AREAS TO L/H ENGINE LOWER AFT COWL IAW CRJ900 EANO. CRJ 954-11856
Part: HINGE FITTING — GOUGED (RT AILERON) · airframe 17,789 hrs · 15,125 cycles
R/H AILERON 1/B PCU HINGE ATTACH POINT GOUGED 900-27-650-100 - REPAIRED RH AILERON I/B PCU HINGE ATTATCH POINT IAW BOMBA RED #690-57-51-228 REV-- DATED 7-9-2021
Part: INTERCOSTAL — CORRODED (BS 349-364 S27L) · airframe 17,789 hrs · 15,125 cycles
INTERCOSTAL LEFT OF STRINGER 27 BETWEEN FS349 & FS364 HAS CORROSION JC: 900-53-140-500 - REMOVED & REPLACED INTERCOSTAL LEFT OF STGR27 BTW FS349 & FS364 IAW CRJ900 SRM 51-42-06 & 51-42-20
Part: SKIN — GOUGED (RT NACELLE) · airframe 17,789 hrs · 15,125 cycles
RIGHT ENGINE LOWER AFT COWL HAS MULTIPLE CHAFED SPOTS AND GOUGES JC:900-54-900-102 - REPAIRED R/H ENGINE LOWER AFT CORE COWL IAW BOMBARDIER REO670-54-23-959 REV E, AND CRJ900 SRM 54-23-00.
Part: WEB — CRACKED (PAX DOOR) · airframe 17,789 hrs · 15,125 cycles
PAX. DOOR WEB IS CRACKED AT AFT DRAG ANGLE F.S 347.25. J/C 900-52-830-500 - REPAIRED PAX DOOR WEB IAW F.A CRJ952-11843 REV IR ISSUE DATE 06-24-21
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 17,789 hrs · 15,125 cycles
PAX DOOR AFT DRAG ANGLE CRACKED JC:900-52-830-300 - REPAIRED PAX DOOR AFT DRAG ANGLE IAW CRJ900 REO-670-52-11-077 REV G
Part: SKIN — DENTED (CARGO DOOR) · airframe 17,789 hrs · 15,125 cycles
CENTER CARGO BAY DOOR OUTER SKIN IS DENTED. J/C 900-52-810304 - REPAIRED DAMAGE ON CENTER CARGO BAY DOOR OUTER SKIN IAW CRJ900 EA CRJ9 53-11845 REV IR.
Part: SEAT TRACK — CORRODED (BS 379-477 RBL 9) · airframe 17,789 hrs · 15,125 cycles
RBL 9 #3 FLOOR SEAT RAIL HAS MULTIPLE SPOTS OF CORROSION. J/C 900-53-900-101 - REMOVED AND REPLACED PBL 9 #3 SEAT RAIL I.A.W. REO BOMBARDIER REO 670-53-00-589 A REPAIR B REV-A DATED 7/14/2020
Part: SEAT TRACK — CORRODED (BS 379-573 LBL 9) · airframe 17,789 hrs · 15,125 cycles
LBL 9 #2,3 FLOOR SEAT RAILS HAS MULTIPLE SPOTS OF CORROSION. J/C 900-53-900-101 - REMOVED CORROSION IAW CRJ-900 SRM 51-21-06 FOUND TO BE WITHIN LIMITS IAW CRJ-900 SRM 53-31-49
Part: SKIN — CRACKED (BS 453 S22-23L) · airframe 17,789 hrs · 15,125 cycles
INBOUND WALK - FUSELAGE SKIN DENT AT FS453 AND BETWEEN STR22L AND STR23 L NEEDS EVALUATED DIDN'T SEE ON "SCRATCH/DENT" LOG. - REPAIRED DAMAGE ON FUSELAGE SKIN IAW EA CRJ953-11755
Part: HOUSING — CRACKED (POWER RECEPTICAL) · airframe 17,789 hrs · 15,125 cycles
EXTERNAL POWER RECEPTACLE HOUSING IS CRACKED JC 900-24-900-902 - REMOVED AND REPLACED WITH NEW EXTERNAL POWER RECEPTACLE HOUSING IAW CRJ 900 REO 670-53-11-029C
Part: SKIN — GOUGED (BS 379 S21-23R) · airframe 17,789 hrs · 15,125 cycles
TOILET SERVICE DOOR AT FS365.00 IS HITTING THE FUSELAGE AND GOUGING IT. 900-53-900-105 - REWORK AND BLENDED IAW EA CRJ953-11795 REV IR
Part: DOOR — UNSECURE (BS 349) · airframe 17,789 hrs · 15,125 cycles
POTABLE WATER SERVICE DOOR AT FS349 IS HITTING THE FUSELAGE AND GOUGING IT. 900-53-900-105 - REWORK AREA IAW EANO. CRJ953-11796 REV IR ISSUE 6-19-21
2020
Part: CHARGER — INOPERATIVE (CABIN) · airframe 17,012 hrs · 14,355 cycles
EMERGENCY EXIT LIGHTS BETWEEN 4C + 5C ARE OUT. SIGN DOES NOT ILLUMINATE. REMOVED AND REPLACED BATTERY CHARGER IAW AMM 33-51-17. REMOVED AND REPLACED BATTERY ASSY IAW JOBCARD 33-900-701. OPS CHECK GOOD. SEE NRWC 748905 FOR DETAILS. PLACARD REMOVED MOC THIS CLEARS 3651514-1.
2019
Part: SIGN — UNSECURE (CABIN) · airframe 15,559 hrs · 13,054 cycles
PAX DOOR EXIT SIGN FELL OFF. REINSTALLED MID CABIN EXIT SIGN IAW AMM 33-51-05 NO DAMAGE TO EXIT SIGN.
2017
Part: DOOR — UNKNOWN (MAIN CABIN) · airframe 11,979 hrs · 10,126 cycles
MAIN CABIN DOOR OUTSIDE HANDLE WILL NOT CLOSE. PERFORMED AN OPS CHECK OF THE CABIN DOOR IAW IAW 52-11-00. NO DEFECTS NOTED.
Part: HANDLE — UNKNOWN (PAX DOOR) · airframe 11,979 hrs · 10,126 cycles
MAIN CABIN DOOR OUTSIDE HANDLE WILL NOT CLOSE. PERFORMED AN OPS CHECK IAW 52-11-00. NO DEFECTS NOTED.
Part: PANEL — CRACKED (PAX DOOR) · airframe 11,973 hrs · 10,122 cycles
PASSENGER DOOR FWD SIDE PANEL HAS TWO CRACKS AT STEP MOUNTING FLANGE. FABRICATED REPLACEMENT ANGLES AND DOUBLER. REPAIRED IAW REO 670-52-11-104, REV H, SRM 51-42-21, AND SRM 51-42-06.
Part: PANEL — CRACKED (PAX DOOR) · airframe 11,973 hrs · 10,122 cycles
PASSENGER DOOR FWD STAIR PANEL CRACKED. ACCOMPLISHED A PERMANENT REPAIR IAW REO 670-52-11-848, REV A. FABRICATED AND INSTALLED REPAIR PARTS.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 11,973 hrs · 10,122 cycles
PASSENGER DOOR AFT DRAG ANGLE CRACKED. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-42-06, 51-40-11, 51-42-22, AND 51-25-16.
Part: WEB — CRACKED (PAX DOOR) · airframe 11,973 hrs · 10,122 cycles
PASSENGER DOOR AFT WEB BENEATH AFT DRAG ANGLE CRACKED. REMOVED AND REPLACED THE WEB BENEATH AFT DRAG ANGLE IAW SRM 51-42-22, 51-42-21, 51-42-10, 51-42-06, 52-11-04, 51-11-04, AND 51-25-16.
Part: CROSSBEAM — CRACKED (BS 280) · airframe 11,973 hrs · 10,122 cycles
F.S. 280.00 CROSS BEAM LEFT HAND SIDE IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED F.S. 280.00 CROSSBEAM(PN:CC670-34094-1) IAW CRJ 900 SRM 51-25-16, 51-40-11, 51-42-21, 51-42-13, 51-21-11, 51-42-06, 551-40-11, AND CRJ 900 AMM 20-70-00.
Part: LIGHT — MISSING (ROW 12) · airframe 11,973 hrs · 10,122 cycles
EMERGENCY FLOOR PATH LIGHTING STRIP MISSING FROM ROW 12 ON RH SIDE. CORRECTIVE ACTION: INSTALLED MISSING EMERGENCY FLOOR PATH LIGHTING STRIP (PN:PL1600LH07) AT ROW 12 ON RH SIDE IAW CRJ900 AMM 33-51-01.
Part: BRACKET — CRACKED (LT WING) · airframe 11,973 hrs · 10,122 cycles
LH SLAT TRACK 1-3 HOUSING BRACKET CRACKED. CORRECTIVE ACTION: REPIARED LH SLAT TRACK 1-3 HOUSING BRACKET IAW BOMBARDIER REO 670-57-42-577 RED -- DATED 2016-12-02.
2016
Part: SEAL — DIRTY (PAX DOOR) · airframe 9,718 hrs · 8,366 cycles
PAX DOOR SQUEALS IN FLIGHT. CLEANED AND LUBED DOOR SEAL IAW AMM 52-10-00. OPS CHECKED GOOD.
Part: CABLE — BENT (DOOR HINGE) · airframe 9,229 hrs · 8,021 cycles
PAX DOOR HINGE BOLT CABLE IS BENT. REMOVED AND REPLACED HINGE BOLT CABLES. OPS CHECK GOOD AT THIS TIME IAW AMM 52-11-17.
Part: TRIM SWITCH — DIRTY (STABILIZER) · airframe 8,902 hrs · 7,763 cycles
ELEVATOR TRIM INOPERATIVE, CAPTAIN SIDE STABILIZER TRIM SWITCH IS INTTERMITTENT. CLEANED AND OPS CHECK F/O SIDE STABILIZER TRIM SWITCH IAW AMM 27-41-05 AND 27-40-00. F/O SIDE OPS CHECK GOOD AT THIS TIME. OPERATIONS F/O IS TO BE THE FLYING PILOT. ACFT IS SAFE FOR A 1 TIME FERRY FLIGHT. CAPT SIDE STABILIZER TRIM IS INOPERATIVE.
2015
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 7,174 hrs · 6,404 cycles
PASSENGER DOOR OUTER CAUTION ON CLOSURE. DEFERRED PAX DOOR INDICATION IAW MEL 52-70-01.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,740 hrs · 6,062 cycles
LOWER SERVICE DOOR EMER LIGHT INOPERATIVE. DEFERRED IAW MEL 23-51-01-3A.