N935EV
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.
61 reports on file, 2005-10-29 – 2014-09-23.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 20,133 hrs · 19,298 cycles
MAIN PASSENGER DOOR EXIT SIGN MISSING THE LIGHT COVER AND THE BULBS ARE ALL BLACK AND APPEAR TO BE BURNED OUT. REPLACED LIGHT COVER AND OPS CHECKED GOOD IAW AMM 33-51-19.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 18,691 hrs · 17,893 cycles
EMERGENCY LIGHTS STAY ON WHEN SWITCH IS IN AUTO COM, GROUND AT TIMES. RESET EMERGENCY LIGHT IAW AMM 33-50-00. NO FURTHER DEFECTS AT THIS TIME.
Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 18,691 hrs · 17,893 cycles
EMERGENCY LIGHT CIRCUIT BREAKER TRIPPED AT GATE . RESET CIRCUIT BREAKER IAW SL RJ-SL-20-005 IAW NO FURTHER ACTION REQUIRED .
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,691 hrs · 17,893 cycles
EMERGENCY LIGHTS ACTIVATED WHEN ARMED AND POWER ON AIRCRAFT, FOUND CIRCUIT BREAKER TRIPPED R & R BATTERY PACK ASSY AT BS 310 IAW AMM 33-51-04. R & R FWD BATTERY CHARGER ASSY AT BS 310 IAW AMM 33-51-05. OPS CHECKED GOOD.
Earlier reports · 2005–2013 · 57 reports
2013
Part: SKIN — CORRODED (LT WING) · airframe 17,449 hrs · 16,604 cycles
LEFT WING PLANK ACCESS HOLE FOR PANEL 540BB HAS AREAS OF PITTING. REPAIRED IAW EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV J. REPAIR CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (RT WING) · airframe 17,449 hrs · 16,604 cycles
RIGHT WING PLANK ACCESS HOLE FOR PANEL 640BB HAS AREAS OF PITTING. REPAIR IS CLASSIFIED AS MAJOR REPAIR. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV J.
Part: SKIN — CORRODED (RT WING) · airframe 17,449 hrs · 16,604 cycles
RIGHT WING PLANK ACCESS HOLE FOR PANEL 610AB HAS AREAS OF PITTING. REPAIR IS CLASSIFIED AS MAJOR. REPAIRED IAW EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV J.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,449 hrs · 16,604 cycles
CORROSION DAMAGE ON RT FLOOR SUPPORT FS 559.0+96. REPAIR CLASSIFIED AS MAJOR. REPAIRED IAW EC/TC REO 601R-53-00-526 01 AND REO 601R-53-00-526 REV DATED 5/22/13.
Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,449 hrs · 16,604 cycles
AFT PRESSURE BULKHEAD DAMAGE BY SCREW ON FWD FACE AT RBL 36.20. REPAIR CLASSIFIED AS MAJOR. REPAIRED IAW SRM 51-25-06-00.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,449 hrs · 16,604 cycles
FS 280 FLOORBEAM ANGLE CRACKED AT LBL 9.0 OTBD. REPAIR CLASSIFIED AS MAJOR. REPAIRED IAW REO 601R-53-11-071.
Part: BEAM — CRACKED (BS 280) · airframe 17,449 hrs · 16,604 cycles
FS 280, LT BEAM CRACKED BELOW MLG ALTERNATE EXT CABLE PULLEY BRACKET. REPAIR CLASSIFIED AS MAJOR. REPAIRED IAW REO 601R-53-11-171.
Part: BULKHEAD — PUNCTURED (BS 280) · airframe 17,449 hrs · 16,604 cycles
LEFT FS 280 BULKHEAD UPPER SKIN PUNCTURED BETWEEN LBL 27 AND LBL 36. REPAIR CLASSIFIED AS A MAJOR. REPAIRED IAW EO CL600-2B19-53-I00303A IAW NDTM PART 1, 51-20-06.
Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,449 hrs · 16,604 cycles
AFT PRESSURE BULKHEAD HAS SCREW DAMAGE TWO PLACES AT RBL 27 FWD FACE. REPAIR CLASSIFIED AS MAJOR. REPAIRED IAW SRM 51-25-06-00.
Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,449 hrs · 16,604 cycles
AFT PRESSURE BULKHEAD FWD FACE HAS SCREW DAMAGE TWO PLACES AT LBL 27.0. REPAIR CLASSIFIED AS MAJOR. REPAIRED IAW REO 601R-53-61-4921.
Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,449 hrs · 16,604 cycles
AFT PRESSURE BULKHEAD FWD FACE HAS SCREW DAMAGE AT LBL 18.0. REPAIR CLASSIFIED AS MAJOR. REPAIRED IAW SRM 51-25-06-00.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,449 hrs · 16,604 cycles
RS 280 FLOORBEAM ANGLE CRACKED AT RBL 9.0 OTBD. REPAIR CLASSIFIED AS MAJOR. REMOVED DAMAGED ANGLE AT FS 280, RBL 9 OTBD IAW SRM 51-42-06 AND 51-42-21. INSTALLED ANGLE IAW SRM 51-42-06 AND 51-42-21 AND DWG 601R31113.
Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,449 hrs · 16,604 cycles
AFT PRESSURE BULKHEAD FWD FACE HAS SCREW DAMAGE INBD OF LBL9.0 2 PLACES. REPAIR CLASSIFIED AS MAJOR. REPAIRED IAW SRM 51-25-06-00.
Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,449 hrs · 16,604 cycles
AFT PRESSURE BULKHEAD FWD FACE HAS SCREW DAMAGE AT RBL 18.0. REPAIR CLASSIFIED AS MAJOR REPAIR. REPAIRED IAW SRM 51-25-06-00.
Part: RELAY — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 16,758 hrs · 15,881 cycles
EMERGENCY LIGHT ON WITH SWITCH IN ARM, CIRCUIT BREAKER 4-C2 TRIPPED. R & R ACCESS BUSS SENSE RELAY (K1XD) IAW AMM 24-51-27. OPS CHECKED ESS RELAY GOOD IAW AMM 24-51-27-700-801. OPS CHECKED LIGHT IAW AMM 33-51-00, NO FAULTS NOTED.
Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 16,756 hrs · 15,880 cycles
EMERGENCY LIGHTS ON IN ARM POSITION. FOUND EMERGENCY LIGHT C/B C2 CBP 4 OUT, RESET AND OPS CHECK IAW AMM 33-51-04, NO FURTHER DEFECT NOTED.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 16,756 hrs · 15,880 cycles
EMERGENCY LIGHTS ARE ON WHILE EMERGENCY LIGHTS SWITCH IN COCKPIT IS IN THE ARM POSITION AND GALLEY SWITCH IS IN THE OFF POSITION. RESET C/B. PERFORMED OPS CHECK OF THE EMERGENCY LIGHTS. OPS CHECKED GOOD REF AMM 33-51-00. ACFT OK FOR SERVICE.
2012
Part: BULKHEAD — CRACKED (BS 202) · airframe 16,009 hrs · 15,092 cycles
BS 202 BULKHEAD CRACKED. REMOVED, FABRICATED AND INSTALLED PARTS IAW SRM 51-42-06, REO 601R-53-11-563 REV B, SRM 51-21-16, SRM 51-42-20, REO 601R-53-11-2380, GMM 3-3.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,251 hrs · 14,245 cycles
NR 2 EXTERNAL EMERGENCY LIGHT INOPERATIVE. RELAMPED 2 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.
Part: SIGN — BROKEN (CABIN) · airframe 14,660 hrs · 13,583 cycles
EXIT SIGN AT THE BOTTOM LEFT SIDE OF PAX ENTRANCE BROKE OFF. R & R SIGN . CHECKED GOOD IAW AMM 33-51-10.
2011
Part: LENS — UNBONDED (EMERGENCY LIGHT) · airframe 14,552 hrs · 13,467 cycles
FWD LT OVERWING EMERGENCY LENS UNBONDED. INSTALLED LENS COVER AND RESEALED ALL OTHER ON LT OF ACFT & SEALED IAW AMM 33-51-21.
Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 14,552 hrs · 13,467 cycles
THE FORWARD LEFT OVERWING EMERGENCY LIGHT IS INOPERATIVE. INSTALLED LENS & SEAL IAW AMM 33-51-21.
Part: CHARGER — INOPERATIVE (EMEGENCY LIGHTS) · airframe 13,519 hrs · 12,312 cycles
PAX DOOR EMERGENCY LIGHTS OUT. R & R NR 2 EMERGENCY BATTERY CHARGER AND BATTERY ASSY IAW AMM 33-51-05. (CLOSED)
Part: PLACARD — DETERIORATED (CABIN) · airframe 13,020 hrs · 11,764 cycles
RT OVERWING EXIT PLACARD MISSING HALF OF THE PLACARD. REPLACED RT EMERGENCY EXIT PLACARD IAW AMM 11-30-00.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,999 hrs · 11,743 cycles
RT EXTERIOR NR 4 EMERGENCY LIGHT INOP. RELAMPED RT EXTERIOR NR 4 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CK GOOD. RELAMPED RT EXTERIOR NR 4 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CK GOOD. (CLOSED)
Part: ANGLE — CRACKED (BS 589) · airframe 12,924 hrs · 11,664 cycles
CARGO FLOOR SILL SUPPORT ANGLE AT FS 589, LBL 36 IS CRACKED. INSTALLED NEW ANGLE AT FS 589 IAW SRM 51-42-21. PN 601R35011-11. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.
Part: RIB — CRACKED (RT WING) · airframe 12,924 hrs · 11,664 cycles
RT BATTERY RIB IS CRACKED ON THE AFT SIDE. INSTALLED ALL REPAIR PART IAW REO 601R-57-51-046.
Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,924 hrs · 11,664 cycles
FS 484 INTERCOSTAL CRACKED AT RBL 36 AND ANGLE FOR INTERCOSTAL IS CRACKED AT RBL 27. REPAIRED FS 484, RBL 36 AND RBL 27 CRACKS IAW REO 601R-53-41-059, REV B, PERFORMED EDDY CURRENT IAW STEP 7 OF EC/TC REO 601R-53-41-059. NO INDICATIONS NOTED. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27.00 AND BL 36.00 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.
Part: FLOORBEAM — CRACKED (BS 595) · airframe 12,924 hrs · 11,664 cycles
FLOORBEAM CAP CRACKED AT FS 595.00 ON LBL 27. REINSTALLED PLASTIC CAP TO THE NEW FLOORBEAM CAP IAW SRM 51-41-00. REMOVED FLOORBEAM CAP IAW SRM 51-42-06, 51-42-21. LOCATED, DRILLED, DEBURRED NEW FLOORBEAM CAP IAW SRM 51-42-21, 51-42-20 AND REO 601R-53-61-3778 STEP 2. INSTALLED FLOORBEAM CAP IAW SRM 51-42-21. COMPLIED WITH EC/TC REO 601R-53-61-3778 AND REO 601R-53-61-3778. APPLIED PRIMER, TOPCOAT AND CIC ON FLOORBEAM CAP IAW SRM 51-21-11. RII FOUND TO BE SATISFACTORY:
Part: ANGLE — CRACKED (BS 484) · airframe 12,924 hrs · 11,664 cycles
FS 484, INTERCOSTAL ANGLE CRACKED ON LBL 27 AND ANGLE (PREVIOUS REPAIR) AT LBL 36 IS CRACKED. REPAIRED IAW EC/TC REO 601R-53-41-059 REV B, STEPS 1-6 AND 8-11.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,924 hrs · 11,664 cycles
PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED PAX DOOR AFT DRAG ANGLE. DRILLED FITTED NEW DRAG ANGLE IAW SRM 51-40-11. INSTALLED DRAG ANGLE ONTO PAX DOOR AS REQUIRED IAW SRM 51-42-06 AND 51-42-13. CLASSIFIED AS A MINOR.
Part: ATTACH FITTING — CORRODED (BS 280) · airframe 12,924 hrs · 11,664 cycles
FS 280, ATTACH CLIPS AT LBL 9 & RBL 9 ON INBD SIDES ARE CRACKED. FITTED, DRILLED AND RELACED BY INSTALLING ATTACH CLIP WITH SERVICEABLE PN 601R31113-57 AND 601R31113-58 IAW SRM 51-42-21 AND 51-42-06. TOUCHED UP TOP COAT ON FASTENERS AND APPLIED CORROSION PREVENTION IAW SRM 51-21-11 AND 51-25-16. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.
Part: ANGLE — CRACKED (BS 625) · airframe 12,924 hrs · 11,664 cycles
RT UPPER 625 OBLIQUE ANGLE IS CRACKED. INSTALLED NEW RT UPPER OBLIQUE ANGLE AT FS 625 IAW SRM 51-42-06. REPAIR IS CLASSIFIED AS A MINOR.
Part: LIGHT — CRACKED (CABIN) · airframe 12,924 hrs · 11,664 cycles
FLOOR TRACK LIGHT CRACKED, DETERIORATED AND DISCOLORED. REPLACED LIGHT IAW AMM 33-51-01-400-807. OPS TEST CHECKED GOOD IAW AMM 33-51-00-710-802.
Part: SWITCH — CONTAMINATED (THRUST REVERSER)
RIGHT REVERSER UNLOCK MESSAGE ON TAKEOFF. EMERGENCY DECLARED & RETURNED TO DEPARTURE. CLEANED SWITCHES, PERFORMED OPS CHECK OF THRUST REVERSER IAW AMM 71-00-00. OPS CKS GOOD.
Part: PLACARD — DETERIORATED (CABIN) · airframe 12,817 hrs · 11,541 cycles
PAX DOOR EXIT PLACARD PEELING. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-00. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-00. (CLOSED)
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,817 hrs · 11,541 cycles
NR2 CABIN CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED NR2 CABIN CEILING EMERGENCY LIGHT IAW AMM 33-51-16, OPS CHECK GOOD. RELAMPED NR2 CABIN CEILING EMERGENCY LIGHT IAW AMM 33-51-16, OPS CHECK GOOD. (CLOSED)
2010
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 12,578 hrs · 11,264 cycles
RT WINDSHIELD HEAT ARCED AND CAUSED THE WINDSHIELD TO CRACK IN FLIGHT (ENROUTE ACFT DIVERTED DUE TO MX -- EMERGENCY DECLARED AS A PRECAUTION) R & R RT WINDSHIELD IAW AMM 56-11-01. LEAK CK GOOD IAW AMM 21-32-00, WINDSHIELD HEAT OP CK GOOD IAW AMM 30-41-01. (CLOSED)
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,135 hrs · 9,556 cycles
RT WING MID EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERG LIGHT BULB IAW AMM 33-51-21.
2009
Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 10,509 hrs · 8,884 cycles
RT OVER WING AFT EMENGENCY EXIT LIGHT INOP.
Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,974 hrs · 7,322 cycles
FS 484 LBL 36 INTERCOSTAL IS CRACKED.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,974 hrs · 7,322 cycles
FLOOR ATTACH ANGLE CRACKED AT OTBD SIDE OF LBL 9 FS 280.
Part: ANGLE — CRACKED (BS 484) · airframe 8,974 hrs · 7,322 cycles
FS 484 RBL 27 ANGLE IS CRACKED.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,974 hrs · 7,322 cycles
FLOOR ATTACH ANGLE CRACKED AT OTBD SIDE OF RBL 9 FS 280.
Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 8,974 hrs · 7,322 cycles
CARGO DOOR SUPPORT BEAM BOTTOM ANGLE FS 621 CRACKED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,974 hrs · 7,322 cycles
CEILING EMERGENCY FLOODLIGHT 2ND LIGHT FROM AFT IS INOPERATIVE. REMOVED AND REPLACED 2ND EMERGENCY LIGHT ON CEILING COMING FROM AFT IAW AMM 33-51-16-400-801 AND OP CHECK OF THE LIGHT IS GOOD IAW AMM 33-51-00-710-801.
Part: ANGLE — CRACKED (BS 621-625) · airframe 8,974 hrs · 7,322 cycles
LT 621-625 OBLIQUE ANGLE IS CRACKED. REMOVED ANGLE IAW SRM 52-40-06. REINSTALLED WITH NEW 601-35012-51 ANGLE IAW SRM 51-42-06.
Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 8,954 hrs · 7,306 cycles
FLT 5268--DEPARTING ATL RETRACTED GEAR AND GOT A NOSE WHEEL DISAGREE WARNING MSG. COMPLIED WITH QRH AND PLANE WAS CHANGING PITCH AND CREW FELT THE NOSE WHEEL GEAR FLAPPING IN WIND. HYDRAULICS APPEARED NORMAL, CONTINUED WITH QRH AND PRIOR TO PULLING GEAR HANDLE THE GEAR CORRECTED ITSELF. LOWERED GEAR NORMALLY AND LANDED OVERWEIGHT AT 48000 LBS. EMERGENCY DECLARED, ACFT RETURNED AFTER T/O. REMOVED AND REPLACED NOSE GEAR SELECTOR VALVE IAW AMM 32-22-20. OPS CHECK GOOD. C/W OVERWEIGHT LANDING INSP IAW AMM 05-51-01 SP 625.
2008
Part: ENGINE — FAILED (LEFT) · airframe 7,585 hrs · 6,080 cycles
L ENG OIL PRESS MSG DURING FLT--ENROUTE TO PHF A/C DIVERTED TO CAE DUE TO MTC--EMERGENCY DECLARED, FLT 4898 DEL 169 MINS REMOVED AND REPLACED LT ENGINE ASSY IAW AMM 71-00-00 LEAK AND OPS CHECK GOOD NO DEFECTS NOTED. (B)
Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 6,760 hrs · 5,380 cycles
FLAP FAIL MSG AT 0 DEGREES ON APPROACH. EMERGENCY TRUCKS ON STANDBY AS A PRECATION. FLT 4781 DEL 593 MINS AND ON 1/21 FLTS 4717, 4414 CX.
2007
Part: FITTING — CRACKED (FUSELAGE) · airframe 4,593 hrs · 3,677 cycles
CLIP CRACKED UNER CARGO DOOR THRESHOLD AT FS 589.00. [SUP 05-09-07] INSTALLED 4EA LOCK FASTENERS THROUGH FS 589.00 FRAME AND CLIP. PRESSURIZATION CHECK GOOD IAW CRJ MM 21-31-00. NO DEFECTS NOTED AT THIS TIME.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,468 hrs · 3,575 cycles
FOUND LT FORWARD MOST EXTERNAL EMERGENCY LIGHT INOP.
2006
Part: UNKNOWN — ODOR (CABIN) · airframe 3,987 hrs · 3,221 cycles
DURING DESCENT INTO ATL TRANSFERRED THE PACKS TO THE APU AND IMMEDIATELY NOTICED A BURNING ODOR. TRACES OF SMOKE WERE VISABLE IN THE COCKPIT AND RECEIVED A SMOKE TOILET CAUTION. NO EXCESS SMOKE WAS OBSERVED IN THE LAV. SHUT OFF THE PACKS, SMOKE DISSIPATED. EMERGENCY DECLARED, TRUCKS REQUESTED TO BE ON STANDBY AS A PRECATION.
Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 3,815 hrs · 3,091 cycles
NWS INOP MESSAGE IN FLIGHT.
Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 3,810 hrs · 3,087 cycles
ON TAKEOFF, AFTER GEAR RETRACTION, RECEIVED -STEERING INOP- MSG. EN ROUTE TO JAN A/C DIVERTED TO BTR DUE TO MTC.
2005
Part: DOOR — MALFUNCTIONED (PAX DOOR)
DURING A GROUND INSPECTION IN OAK, THE PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE CYCLED THE PASSENGER DOOR. NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
Part: LIGHT — INOPERATIVE (EXTERIOR)
DURING A HANGAR INSPECTION IN BTR, THE AFT EMERGENCY LIGHT ON THE LEFT SIDE OF THE FUSELAGE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT EMERGENCY LIGHT ON THE LEFT SIDE OF THE FUSELAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)