N187GJ
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.
31 reports on file, 2015-12-09 – 2025-08-25.
Part: LUG — CORRODED (ZONE 500) · airframe 27,296 hrs · 22,059 cycles
THE L/H AILERON PCU LUG L2 HAS CORROSION INSIDE THE BORE FOR THE BUSHING COMPLIED WITH REPAIR TO RTM AILERON CENTRE HINGE FITTING LUGS IAW BOMBARDIER REO 670-57-61-237 REV-- DATED 2017-07-25.
Part: FITTING — OUT OF LIMITS (ZONE 600) · airframe 27,296 hrs · 22,059 cycles
"ON THE RH AILERON, FOUND BOTH CENTER UPPER LUG BORE DIAMETERS TO BE OUT OF LIMITS. IB LUG IS .986"" AND OB LUG IS .985"", NOMINAL LIMIT IS .975 +- .0005 REPAIRED OVERSIZED BORES AND PITTING CORROSION TO THE AILERON ACTUATOR CENTER HINGE FITTING LUGS AT AIL STA 338.424 AND 342.123 RHS IAW MHIRJ REO 690-57-61-417 REV -- DATED 2025-08-21. AILERON P/N 601R13400-2 S/N SB0052. "
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 27,296 hrs · 22,059 cycles
LEFT F.S.280 CROSSBEAM APPEARS TO BE CORRODED ON AFT EDGE UNDER CAP ANGLE, LBL11. REMOVED LH FS280 BULKHEAD CROSSBEAM BETWEEN BL 0 TO RBL37, IAW CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-13-001-001-A01. INSTALLED NEW SERVICEABLE LH FS 280 (PN: CC670-34094JP-1S) BULKHEAD CROSSBEAM BETWEEN BL 0 TO LBL37, IAW CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-13-001-001-A01.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 27,296 hrs · 22,059 cycles
R/H F.S.280 CROSSBEAM APPEARS TO BE CORRODED ON AFT EDGE UNDER CAP ANGLE, RBL 11. REMOVED RH FS280 BULKHEAD CROSSBEAM BETWEEN BL 0 TO RBL37, IAW CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE RH FS280 BULKHEAD CROSSBEAM (PN: CC670-34094JP-2S) BETWEEN BL 0 TO RBL37, IAW CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: LUG — CRACKED (ZONE 800) · airframe 27,296 hrs · 22,059 cycles
RIGHT AFT OVERWING EMERGENCY EXIT DOOR S/N SB0739 HAS POSSIBLE CRACK AROUND TOP ALIGNMENT LUG. REPAIRED CRACK TO OVERWING EMERGENCY EXIT DOOR S/N SB0739 TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER) IAW MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-06.
Part: ANGLE — CORRODED (ZONE 800) · airframe 27,296 hrs · 22,059 cycles
AFT BELLY FAIRNG SUPPORT STRUCTURE F.S.881 IS CORRODED AT STGR 27. REMOVED CORROSION FROM AFT BELLY FAIRNG SUPPORT STRUCTURE BS 881 AT S27 IAW SRM 51-21-06-001-001-A01 PER SRM 53-82-55-101-001-A02 ANGLE IS OUT OF LIMITS ON MULTIPLE ELEMENTS & REQUIRES ENGINEERING REC'D & CW EA CRJ953-19900 REV IR & CRJ953-19901 REV IR. FABRICATED ANGLE IAW SRM 51-24-21-001-001-A01, 51-24-36-001-001-A01, 51-40-11-001-001-A01 AND DWG SH690-39337 REV-NC. FABRICATED PART. INSTALLED 4EA NUT PLATES AT NEW FABRICATED ANGLE FROM AFT BELLY FAIRNG SUPPORT BS 881 AT S27 IAW SRM 51-42-06-001-001-A01. INSTALLED RIVETS IN ANGLE IAW SRM 51-42-06-001-001-A01. APPLIED SEALANT PAD AT REPAIR AREA IAW AMM 51-23-00-390-820-A01.
Earlier reports · 2015–2024 · 25 reports
2024
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 24,619 hrs · 19,824 cycles
L/H AFT EMERGENCY DOOR HAS A VISIBLE CRACK BELOW UPPER AFT LUG. REPAIRED IAW ENDEAVOR EA CRJ952-16409 REV IR DATED 4/29/2024.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 24,619 hrs · 19,824 cycles
R/H FWD EMERGENCY DOOR HAS A VISIBLE CRACK BELOW UPPER AFT LUG. REPAIRED IAW ENDEAVOR EA CRJ952-16408 REV IR DATED 4/27/2024.
2023
Part: LIGHT — INOPERATIVE · airframe 22,833 hrs · 18,302 cycles
EXTERIOR OVERWING EMERGENCY EXIT LIGHT ON LEFT SIDE INOP R/R DS101 OVERWING EMERGENCY EXIT LIGHT IAW CRJ-900 AMM 33-51-15. GROUND WIRE WAS FOUND PULLED OUT OF PIN, RE-CRIMPED GROUND PIN IAW CRJ-900 ESPM 20-16-05. OPS CHECK GOOD. EMERGENCY LIGHT PN ON/OFF: 2LA006954-00. PIN PN ON/OFF: 00110410002
Part: LAMP — INOPERATIVE · airframe 22,325 hrs · 17,859 cycles
LEFT OVERWING FAIRING EMERGENCY LIGHT WAS BURNT OUT. R/R BULB IAW AMM 33-51-15. OPC GOOD. P/N OFF/ON: 8GH005123-06
2022
Part: FLOORBEAM — CORRODED (BS 280 BL0-LBL9) · airframe 20,133 hrs · 16,067 cycles
280 FLOOR BEAM IS CORRODED BETWEEN LBL9-BL0. MEASURING 3.5" X 1.25" X .062" DEEP. THIS IS BEYOND SRM LIMITS. - REMOVE AND REPLACE FLOOR BEAM. THIS WAS FOUND WHILE COMPLETING TASK CARD 900-53-130-300.
2021
Part: BRACKET — CRACKED · airframe 20,133 hrs · 16,067 cycles
MAIN LANDING GEAR SIDE STAY FITTING L/H LOWER BRACKET CRACK J/C:900-57-510-500 - REMOVED AND REPLACED PN CC670-39025-1 ON LH MAIN LANDING GEAR IAW CRJ 900 SRM 51-42-06 AND 53-83-85
Part: SKIN — GOUGED · airframe 20,133 hrs · 16,067 cycles
AFT LOWER SKIN HAS 2EA GAUGES BTW F.S 927.00 & F.S 913.00 STRG 27 - REPAIRED AFT LOWER SKIN BTW F.S 913.00 & F.S 927.00, STRG 27, IAW BOMBARDIER REO#670-53-00-290
Part: ANGLE — CORRODED · airframe 20,133 hrs · 16,067 cycles
GALLEY SERVICE DOOR SILL STRUCTURE IS CORRODED ON TWO PLACES DOT#-CA-009 J/C:900-53-230-500 - EVALUATED AREA REMOVED CORROSION IAW CRJ900 SRM 51-21-06 REPAIRED AREA IAW BOMBARDIER EA# CRJ953-12534
Part: HANDLE — CRACKED · airframe 20,133 hrs · 16,067 cycles
PAX DOOR-DOOR HANDLE- "PUSH IN" FLAP HAS A CRACK IN THE CORNER OF IT JC:900-52-830-300 EMP#:290BA - RMOVED AND REPLACED PAX DOOR-DOOR HANDLE- "PUSH IN" FLAP I.A.W. CRJ900 SRM 51-42-06
2019
Part: PROTECTOR — CRACKED (CARGO DOOR) · airframe 180,617 hrs · 14,291 cycles
CENTER BAG BAY DOOR FWD COUNTER BALANCE ARM UPPER HARNESS PROTECTOR CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED CENTER BAG BAY DOOR HARNESS PROTECTOR (P/N:LE670-39725-1) IAW AMM 20-21-00.
2018
Part: LONGERON — CORRODED (BS 333-364) · airframe 15,484 hrs · 12,239 cycles
LONGERON BETWEEN BS 333 AND 364 IS CORRODED. REMOVED AND REPLACED THE LONGERON IAW SRM 51-42-02, 51-42-06, 51-5-42-21, 51-40-11, AND 51-42-13.
Part: STRINGER — CORRODED (BS 333-349) · airframe 15,484 hrs · 12,239 cycles
STRINGER 26R BETWEEN BS 333 AND 349 IS CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-02, 51-42-03, 51-42-21, 51-40-11, AND 51-42-13.
Part: STRINGER — CORRODED (BS 295-310) · airframe 15,484 hrs · 12,239 cycles
STRINGER 25R BETWEEN BS 295 AND 310 WAS CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-02, 51-42-06, 51-42-21, 51-40-11, AND 51-42-13.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 15,484 hrs · 12,239 cycles
RIGHT HAND FLOOR SILL AT FS 280.00 IS CORRODED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-53-21-139 REV B DATED 2017-04-03.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,484 hrs · 12,239 cycles
BS 280 FLOORBEAM ANGLE CRACKED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-20, 51-21-0051-25-06, 51-40-11, 51-42-43, 51-42-06, AND 51-21-11.
Part: WEB — CRACKED (DOOR STEP) · airframe 15,484 hrs · 12,239 cycles
PASSENGER DOOR AFT STAIR WEB IS CRACKED IN TWO SPOTS. CUT OUT DAMAGE AND FABRICATED A DOUBLER AND FILLER AND INSTALLED IAW SRM 51-42-06, AND 52-11-04.
Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 15,484 hrs · 12,239 cycles
INTERCOSTAL ON PAX DOOR INTERNAL STRUCTURE FOUND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, 51-40-11, AND 51-42-21.
Part: SKIN — CRACKED (PAX DOOR) · airframe 15,484 hrs · 12,239 cycles
PAX DOOR AFT PULL-IN-CAM DOUBLER INSIDE PANEL 832AR AND INNER SKIN AT FWD PULL-IN-CAM DOUBLER INSIDE PANEL 832AL HAVE CRACKS. REPLACED PAX DOOR AFT PULL-IN-CAM DOUBLER AND FWD PULL-IN-CAM DOUBLER SKIN IAW SRM 51-42-22, 51-40-11, 51-42-06, 51-42-21, 51-42-13, 51-41-02, 51-42-10 AND AMM 52-11-05, 52-11-04, 52-11-13, 52-11-08, 52-11-02, 52-11-07.
2017
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 12,961 hrs · 10,196 cycles
EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED. CHARGED FOR SIX HOURS OPS NORMAL IAW AMM 33-51-17.
2016
Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 12,835 hrs · 10,107 cycles
RIGHT WINDOW HEAT CAUTION MESSAGE IN FLIGHT. EMERGENCY DELARED. REMOVED AND REPLACED RIGHT WINDOW TEMP CONTROLER IAW AMM 30-41-06
Part: LIGHT — UNKNOWN (CABIN) · airframe 12,835 hrs · 10,107 cycles
EXIT LIGHT ON MAIN CABIN DOOR INOPERATIVE. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD.
Part: INDICATION SYS — FAULTY (PAX DOOR) · airframe 10,734 hrs · 8,508 cycles
PASSENGER DOOR LATCH MSG. DEFERRED PAX DOOR LATCH INDICATING SYS IAW MEL 52-70-01 CAT A.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 10,709 hrs · 8,488 cycles
PASSENGER DOOR LATCH CAUTION. DEFERRED PAX DOOR INDICATION SYS IAW MEL 52-70-01 CAT A.
Part: TARGET — OBSTRUCTED (PAX DOOR) · airframe 10,436 hrs · 8,282 cycles
PASSENGER DOOR LATCH CAUTION INTERMITTENT SEVERAL TIMES IN FLIGHT. INSPECTED PAX DOOR LATCH PROX SWITCH PX107, FOUND UNCURED SEALANT OBSTRUCTING TARGET PLATE. REMOVED SEALANT AS REQUIRED, PERFORMED OPERATIONS CHECK OF DOOR WARNING SYS. OPERATIONS CHECKED GOOD IAW AMM 52-70-04.
2015
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,241 hrs · 8,138 cycles
PASSENGER DOOR OUTER HANDLE, CAUTION MSG ALONG WITH PROX SYS 2 FAULT STATUS MSG IN FLIGHT. PERFORMED SHAKEDOWN & SECURITY CHECK OF PAX DOOR WARNING & INSPECTION OF WIRING OF PAX DOOR IAW AMM 52-11-00. PERFORMED OPERATIONS CHECK OF PAX DOOR IAW 52-11-00. NO DEFECTS NOTED AT THIS TIME.