N165GJ
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.
129 reports on file, 2007-09-19 – 2019-08-20.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,190 hrs · 24,665 cycles
CEILING EMERG FLOOD LIGHT NEAR ROW 15 INOP. R/R EMERGENCY FLOODLIGHT BULB AT ROW 15 IAW CRJ 700AMM 33-51-09 OPS CHECK GOOD.
Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 34,839 hrs · 23,779 cycles
GALLEY/SERVICE DOOR KICK ANGLE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED GALLET/SERVICE DOOR KICK ANGLE(PN:SH670-31996-3) IAW SRM 51-42-221, 51-42-06, 51-40-11, 51-41-00, 51-21-11, AND 51-25-06
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 34,839 hrs · 23,779 cycles
VERTICAL STABILIZER LT FWD AND AFT DRAG ANGLES ARE CRACKED. CORRECTIVE ACTION:. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EO C700-55MR-004-0 DATED 10 JAN 2018.
Part: ACCESS PANEL — CRACKED (PYLON) · airframe 34,839 hrs · 23,779 cycles
PYLON ACESS 443BB IS CRACKED. CORRECTIVE ACTION: REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-78-33-998 REV. B DATED 14-08-2018.2018.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 34,839 hrs · 23,779 cycles
PASSENGER DOOR AFT DRAG ANGLE CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED DAMAGED SECTION OF AFT DRAG ANGLE (P/N: 601R31772-5S) IAW SRM 52-11-04, 51-12-11, 51-42-22, 51-40-11, 51-25-06, 51-42-06, 51-42-10, AND AMM 52-11-08.
Part: WEB — CRACKED (FUSELAGE) · airframe 34,839 hrs · 23,779 cycles
FWD EQUIP COMPARTMENT FLOOR WEB LT SIDE AT FS 193.00 IS CRACKED. CORRECTIVE ACTION REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-53-11-509, REV.-E DATED 2018-02-08.
Part: BRACKET — CRACKED (LE SLAT) · airframe 34,839 hrs · 23,779 cycles
LT SLAT TRACK HOUSING BRACKET AT 1-3 IS CRACKED. CORRECTIVE ACTION: CUT AWAY DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-57-42 REV.- DATED 2019-12-02.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 34,839 hrs · 23,779 cycles
STRINGER 25R BETWEEN FS 333.00 AND FS 295.00 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED STR 25R(PN:SH670-31212-2U)IAW SRM 51-25-16, 51-42-21, 51-40-1151-41-00, 53-21-03, 51-42-06, NDT MANUAL PART 1 51-20-006.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 34,839 hrs · 23,779 cycles
FWD HYDRAULIC COMPARTMENT I/B AND O/B ACCUMULATOR BRACKETS ARE CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED I/B BRACKET(PN:CC670-75604-2) AND O/B BRACKET(PN:CC670-75604-3) IAW CRJ 700 SRM 51-42-21
Part: ACCESS PANEL — CRACKED (VERTICAL STAB) · airframe 34,839 hrs · 23,779 cycles
AFT LWR VERT. STAB. VISOR PANEL 326CR IS DAMAGED. CORRECTIVE ACTION: REPAIRED VISOR PANEL 326CR IAW REO 670-55-32-248 REV.- DATED 2019-01-13.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 34,839 hrs · 23,779 cycles
SRTINGER 26R IS CORRODED BETWEEN FS 333.00 AND FS 295.00. CORRECTIVE ACTION: REMOVED AND REPLACED STGR 26R(PN:SH670-31634-2) IAW CRJ 700 SRM 51-42--06, 51-41-00, 53-21-03, 51-24-36, 51-40-11, AND 51-.42-21.
Part: WEB — CRACKED (FUSELAGE) · airframe 34,839 hrs · 23,779 cycles
FWD EQUIP. COMPARTMENT FLOOR WEB RT SIDE AT FS 193.00 IS CRACKED. CORRECTIVE ACTION: REPAIRED FLOOR WEB BY CUTTING AWAY DAMAGE, FABRICATING AND INSTALLING REPAIR PARTS IAW REO 670-53-11-509 REV.-E DATED 2018-02-08.
Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 34,839 hrs · 23,779 cycles
RT AND LT SIDES OF FS 280.00 CROSSBEAM ARE CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED LT AND RT SIDES OF FS 280.00 CROSSBEAM (PN:CC670-34175-7S) IAW EO C700-53MR-011-0 DATED 07 JAN 2018.
Part: BEAM — CRACKED (FUSELAGE) · airframe 34,839 hrs · 23,779 cycles
FS 280 BEAM CRACKED ON LT AND RT SIDES. CORRECTIVE ACTION: REPLACED FS 280 BEAM LT AND RT IAW SRM 53-11-41 AND NDTM PART 1 51-20-006 AND E.O. C700-53MR-011 REV# 0.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 24,839 hrs · 23,779 cycles
AFT LWR WING TO BODY FAIRING SUPPORT STRUCTURE AT FS 909 AND LBL17.63 ANGLE IS CRACKED. CORRECTIVE ACTION REPAIRED SUPPORT STRUCTURE ANGLE IAW REO 670-53-82-478 REV.-A DATED 2014-11-12.
Part: LANDING — CRACKED (FUSELAGE) · airframe 34,839 hrs · 23,779 cycles
ACCESS DOOR 212AR BOTTOM DOOR LANDING IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED DOOR LANDING(PN: CC670-33151-6S) IAW SRM 51-42-06, 51-42-13, 51-40-06, 51-40-11, AND 51-25-16.
Earlier reports · 2007–2018 · 113 reports
2018
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 32,357 hrs · 22,177 cycles
LEFT OVERWING EMERGENCY LIGHT LENS DETACHED. SECURED THE LENS IAW AMM 51-22-61.
Part: STRINGER — CRACKED (BS 280) · airframe 32,296 hrs · 22,134 cycles
LINTEL STRINGER 3 CRACKED AT BS 280. REPAIRED THE STRINGER IAW SB 670-BA-53-040.
2017
Part: O-RING — LEAKING (HYD SYSTEM) · airframe 30,960 hrs · 21,125 cycles
HYD SYSTEM 1 FLUID DROPPED TO 0% IN FLIGHT. FOUND A BROKEN O-RING ON PRESSURE TRANSDUCER ON THE NR 1 SYSTEM. R & R THE O-RING ON NAS1612-4. PERFORMED SERVICING OF HYD 1 SYSTEM AND CLEANED UP EVIDENCE OF HYD LEAK. RAN PUMP 1A AND 1B, OPERATED MULTIPLE HYD FUNCTIONS FOR 5 MINUTES. NO LEAKS NOTED.
Part: O-RING — LEAKING (HYD SYSTEM) · airframe 30,290 hrs · 20,623 cycles
HYDRAULIC SYSTEM 1 LOW PRESSURE CAUTION MESSAGE. FOUND A BAD O-RING AT THE NR 1 SYSTEM FORWARD FILTER PRESSURE SWITCH. REMOVED AND REPLACED THE O-RING IAW AMM 29-11-05. SERVICED THE RESERVOIR IAW AMM 12-12-29. PERFORMED HYDRAULIC NR1 LEAK CHECK. NO LEAKS NOTED
2016
Part: PIN — DETACHED (PAX DOOR) · airframe 29,364 hrs · 19,922 cycles
PAX DOOR RAIL PIN IS NOT ATTACHED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,267 hrs · 19,842 cycles
ROW 11 CEILING EMERG LIGHT INOP. DEFERRED ROW 11 CEILING EMERGENCY LIGHT PER MEL 33-51-01B CAT C.
Part: TRIM PANEL — DEFECTIVE (ESCAPE HATCH) · airframe 29,108 hrs · 19,702 cycles
CREW ESCAPE HATCH DOES NOT OPEN. R & R OUTER TRIM PANEL ASSY IAW AMM 25-15-06. R & R SEAL TRIM ASSY IAW AMM 52-22-07, FUNCTIONAL TEST OF ESCAPE HATCH IAW AMM 52-22-00 FUNCTIONAL TEST GOOD.
Part: TRACK — DIRTY (PAX DOOR) · airframe 28,974 hrs · 19,602 cycles
MAIN PAX DOOR HARD TO OPEN. CLEANED OUT DOOR TRACK AND APPLIED LUBRICANT IAW AMM 12-20-52.
Part: COVER — MISSING (CABIN) · airframe 28,205 hrs · 19,053 cycles
FORWARD FLIGHT ATTENDANT EMER LIGHT SWITCH COVER MISSING. PLACED FWD FLIGHT ATTENDANT EMER LIGHT SWITCH COVER ON NEF 25-100-39.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,814 hrs · 18,791 cycles
AFT EMER OVERHEAD LIGHT INOPERATIVE. R & R BULB IAW AMM 33-51-09. OPERATIONS CHECKED GOOD.
Part: BRACKET — BROKEN (FIRE BOTTLE) · airframe 27,787 hrs · 18,770 cycles
FIRE EXTINGUISHER HOLD DOWN BRACKET AT 17B, LATCH BROKEN. SECURED ROW 17A - B PORTABLE FIRE EXTINGUISHER BRACKET IAW AMM 25-23-01. OPERATIONS CHECKED GOOD.
Part: SERVICE DOOR — NOISY (CABIN) · airframe 27,462 hrs · 18,543 cycles
SERVICE DOOR SQUEALS IN FLIGHT. PERFORMED PRESSURIZATION OF ACFT & LEAK CHECK IAW AMM 52-00-00. LEAK CHECKED GOOD AT THIS TIME.
2015
Part: WHEEL — BROKEN (PAX DOOR) · airframe 26,548 hrs · 17,874 cycles
SUPPORT WHEEL ON PAX DOOR LOWER CABLE IS BROKEN. REMOVED PAX DOOR SUPPORT WHEEL ASSEMBLY & BOTTOM CABLE IAW AMM 52-11-13. VERIFIED PAX DOOR CLOSES, LATCHES & OPERATES NORMALLY. ACFT FOUND SAFE FOR FERRY FLIGHT.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,548 hrs · 17,874 cycles
RAMP REPORTS DAMAGE TO PAX DOOR CUT OUT FRAME AREA. INSPECTED & FOUND PAX DOOR SEAL AFT STRIKER & FUSELAGE SKIN AT FS 349.00, BETWEEN STRINGER 4L & 5L. COMPLIED WITH REO 670-53-22-070, DRESSED BACK DAMAGE & APPLIED SPEED TAPE. ACFT FOUND TO BE SAFE OF FERRY FLIGHT.
Part: CABLE — BROKEN (PAX DOOR) · airframe 26,223 hrs · 17,651 cycles
PASSENGER DOOR ICE BREAK CABLE IS BROKEN. R & R PAX DOOR ICE BREAK CABLE, PN 601R318127-3, IAW AMM 52-11-15.
Part: LENS — CRACKED (EXTERIOR LIGHT) · airframe 26,223 hrs · 17,651 cycles
FIVE EXTERNAL EMER LIGHT LENSES ARE CRACKED. R & R PN 9EL400042-11 IAW AMM33-51-15.
Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 26,230 hrs · 17,651 cycles
LEFT & RIGHT CROSSBEAM AT FS 2080.00 IS CRACKED. R & R LT & RT CROSSBEAM, PN CC670-34175-7S IAW SRM 51-42-13, 51-42-21, 51-42-06, 53-11-41, 51-25-16, 51-21-11, 51-25-06 & AMM 20-70-00 & 51-21-01. NDT PERFORMED, WO A15-762, DATED 14 JULY 20105.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 26,223 hrs · 17,651 cycles
MAIN AVIONIC DOOR, INTERNAL FWD SURROUND STRUCTURE INTERCOSTAL AT STRINGER 27R HAS SIGN OF CORROSION. R & R INTERCOSTAL IAW SRM 51-42-21 & 51-42-06.
Part: FASTENER — CORRODED (EMERGENCY EXIT) · airframe 26,223 hrs · 17,651 cycles
RIGHT OVERWING EMER EXIT DOOR HANDLE PIVOT MOUNTS, BRACKETS, HAVE CORRODED HARDWARE. R & R HARDWARE IAW AMM 20-21-00. WO 80302 & WC 8060.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,050 hrs · 17,531 cycles
EMERGENCY LIGHT OUT ON 4TH CEILING PANEL. DEFERRED NR 4 CEILING OVERHEAD PANEL EMER FLOODLIGHT IAW MEL 33-51-01-B CAT C.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 25,738 hrs · 17,329 cycles
ANTI-ICE DUCT WARNING MSG ON TAKEOFF. MSG RETURNED SEVERAL TIMES ON TAXI BACK. PERFORMED EVENT CHECK OF LOOPS AT SS430R. VERIFIED NO LOOPS WERE TOUCHING IAW AMM 36-21-00. DEFERRED WING ANTI-ICE MODULATING SOVS IAW MEL 30-12-01A CAT C.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,313 hrs · 17,039 cycles
CEILING EMER LIGHT INOPERATIVE. RELAMPED EMER CEILING LIGHT AT ROW 21 IAW AMM 33-51-06. OPERATIONS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,065 hrs · 16,852 cycles
THREE EMER LIGHTS INOPERATIVE. DEFERRED CABIN EMER LIGHTS IAW MEL 33-51-01A CAT A.
Part: DOOR — OBSTRUCTED (EMERGENCY EXIT) · airframe 24,910 hrs · 16,776 cycles
LOUD SQUEAL FROM RT OVERWING EXIT. REMOVED RT OVERWING EXIT DOOR, FOUND DEBRIS IN SILL AREA, REMOVED DEBRIS. REINSTALLED DOOR. PERFORMED OPERATIONS CHECK OF EXIT DOOR IAW AMM 52-21-00. PERFORMED PRESSURIZATION CHECK IAW AMM 21-31-00. NO DEFECTS NOTED AT THIS TIME.
2014
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 24,744 hrs · 16,679 cycles
LEFT SIDE EMER EXIT SIGN LOWER, HAS BULBS OUT. RELAMPED LT EMER EXIT DOOR LIGHT IAW AMM 33-51-05. OPERATIONS CHECKED GOOD AT THIS TIME.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,642 hrs · 16,607 cycles
EMERGENCY LIGHTS AT EXIT ROW LT SIDE BULBS INOPERATIVE. R & R NR 3 ESPU BATTERY CHARGER ASSEMBLY IAW AMM 33-51-07. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,291 hrs · 16,376 cycles
EMERGENCY LIGHT INOPERATIVE ROW 15. R & R LIGHT BULB ON CEILING AT ROW 15 IAW AMM 33-51-09. OPERATIONS CHECKED GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 223,867 hrs · 16,118 cycles
EMERGENCY LIGHTS WILL NOT TURN ON. R & R BATTERY PACK NR 2 IAW 33-50-14. OPERATIONS CHECKED GOOD.
Part: ENGINE — VIBRATION (NR 1) · airframe 23,487 hrs · 15,575 cycles
NUMBER 1 ENG N1 VIBE 1.9. INSPECTED NR 1 ENG BLADES FOR STIFFNESS CHECK & PERFORMED ENG RUN. FOUND TO HAVE 0.2 N1 VIBE AT THIS TIME IAW AMM 72-21-02. PLACED ON CARRYOVER 4239.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,101 hrs · 15,631 cycles
ROW 23 EMERGENCY FLOOD LIGHT INOPERATIVE. DEFERRED EMERGENCY FLOOD LIGHT AT ROW 23 IAW MEL 33-51-01B CAT C.
Part: PLACARD — WORN (PAX DOOR) · airframe 22,908 hrs · 15,513 cycles
PAX DOOR EXIT & OPEN PLACARDS WORN. R & R EXIT & OPEN PLACARDS IAW AMM 20-60-04.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,367 hrs · 15,367 cycles
EMERGENCY CEILING FLOOD LIGHT AT ROW 11 INOPERATIVE. DEFERRED IAW MEL 33-51-01B CAT C.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,367 hrs · 15,168 cycles
EMERGENCY CEILING FLOOD LIGHT AT ROW 11 INOPERATIVE. DEFERRED IAW MEL 33-51-01B CAT C.
2013
Part: AHRS — FAILED (NR 1) · airframe 21,322 hrs · 14,506 cycles
AHRS FAILED IN FLIGHT, R & R NR 1 AHRS IAW AMM 34-21-01. OPS CHECKED GOOD AT THIS TIME.
Part: FRAME — CORRODED (ZONE 100) · airframe 21,315 hrs · 14,501 cycles
FUSELAGE FRAME CORRODED ON FWD FACE AT BS 349, BL 0 - LBL 3. BLENDED FRAME IAW REO 670-53-21-1014, REV A. FOUND TO BE WITHIN LIMITS.
Part: STRINGER — CORRODED (BS 333-349) · airframe 21,315 hrs · 14,501 cycles
STRINGER 26R CORRODED BETWEEN BS 333 AND 349. BLENDED STRINGER. FOUND WITHIN LIMITS IAW REO 670-53-21-1013.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 21,315 hrs · 14,501 cycles
AFT CARGO BAY FLOOR SUPPORT CORRODED AT LBL 26 FROM BS 1015-1042. CUT OUT DAMAGED SECTION OF FLOOR SUPPORT. FABRICATED REPAIR AND INSTALLED IAW REO 670-53-00-029, REV A.
Part: FRAME — CORRODED (BS 310) · airframe 21,315 hrs · 14,501 cycles
FUSELAGE FRAME FS 310 BETWEEN LBL 7 AND RBL 2 CORRODED. BLENDED AREA TO WITHIN LIMITS, IAW REO 670-53-21-1015.
Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 21,315 hrs · 14,501 cycles
FS 280 FLOORBEAM CORRODED AND CRACKED. R & R FLOORBEAM IAW REO 670-53-11-047, REV E, SRM 51-21-11, 51-42-06, 51-21-16, 51-42-10, 51-42-21, AND 51-40-11. NTD PERFORMED.
Part: FLOOR SUPPORT — CRACKED (BS 268) · airframe 21,315 hrs · 14,501 cycles
COCKPIT FLOOR SUPPORT RBL 12, FS 268 IS CRACKED. CUT AND REMOVED DAMAGED SECTION OF FLOOR SUPPORT FROM FS 268 TO 280. REPLACED SUPPORT IAW REO 670-53-11-861.
Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 21,315 hrs · 14,501 cycles
COCKPIT FLOOR SUPPORT AT LBL 12, FS 268 IS CRACKED. CUT AND REMOVED DAMAGED SECTION OF FLOOR SUPPORT FROM FS 268 TO 280. REPLACED SUPPORT IAW REO 670-53-11-861.
Part: SILL — CORRODED (ZONE 100) · airframe 21,315 hrs · 14,501 cycles
RIGHT SILL, AFT OF BS 280 CORRODED. REMOVED SILL AND REPLACED WITH A SERVICEABLE SILL IAW SRM 51-42-06, 51-42-21, 51-42-13, 51-23-00, 51-40-11.
Part: FITTING — CORRODED (ZONE 200) · airframe 21,315 hrs · 14,501 cycles
CABIN RT WINDSCREEN FLOOR MOUNT FITTINGS CORRODED. R & R FITTINGS AND DOUBLERS.
Part: BULKHEAD WEB — CORRODED (ZONE 200) · airframe 21,315 hrs · 14,501 cycles
FS 280.0 BULKHEAD RT AFT LOWER WEB CORRODED. REMOVED CORRODED PORTION OF WEB. FABRICATED REPLACEMENT WEB AND STRAP, AND INSTALLED IAW REO 670-53-11-594.
Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 21,315 hrs · 14,501 cycles
FS 280 FLOORBEAM UNDERFLOOR STORAGE BOX "QUARTER TURN" ANGLE CORRODED. R & R "QUARTER TURN" ANGLE IAW SRM 51-40-11 AND 51-42-06.
Part: FRAME — CORRODED (ZONE 100) · airframe 21,315 hrs · 14,501 cycles
AFT FACE OF FRAME FS 295 BETWEEN LBL 9 AND RBL 1 HAS CORROSION. CUT OUT CORRODED SECTION OF FRAME AND INSTALLED SERVICEABLE FRAME IAW REO 670-53-21-1012, REV A.
Part: CHANNEL — CORRODED (ZONE 100) · airframe 21,315 hrs · 14,501 cycles
LOWER FUSELAGE TCAS ANTENNA MOUNT CHANNEL CORRODED. R & R TCAS MOUNT CHANNEL IAW SRM 51-42-06, 51-42-21 AND 51-23-00.
Part: DOUBLER — CORRODED (FAIRING) · airframe 21,315 hrs · 14,501 cycles
AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE DOUBLER AT FS 939 CORRODED. R & R AFT WING TO FUSELAGE SUPPORT STRUCTURE DOUBLER IAW SRM 51-21-11, 51-40-11, 51-25-16, 51-25-06, 51-42-15, 51-45-00, 51-42-06, AND 51-23-00.
Part: STEP — LOOSE (PAX DOOR) · airframe 21,280 hrs · 14,477 cycles
PAX DOOR STEP HAS LOOSE AND MISSING HARWARE. REPLACED AND RETORQUED HARDWARE ON PAX DOOR IAW AMM 20-21-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,161 hrs · 14,401 cycles
RED EMERGENCY NOTIFICATION LIGHT ON AFT SIDE OF OVERBOARD EXIT SIGN AT ROW 12 DOES NOT ILLUMINATE.
Part: HOOK AND LOOP — DETACHED (EMERGENCY EXIT) · airframe 21,161 hrs · 14,401 cycles
RT SIDE OVERWING EMERGENCY EXIT COVER DOES NOT STAY IN PLACE. RESECURED HOOK AND LOOP ON EMERGENCY EXIT HANDLE AS REQUIRED.
Part: CABLE — DISLODGED (PAX DOOR) · airframe 20,389 hrs · 13,877 cycles
PAX DOOR CABLE APPEARS TO HAVE COME OFF OF PULLEY. SECURED CABLE ON PULLEY IAW 52-11-08. OP'S CHECKED GOOD.
Part: PROXIMITY SWITCH — INOPERATIVE (PAX DOOR) · airframe 20,144 hrs · 13,715 cycles
PASSENGER DOOR WARNING MESSAGE WHEN MAIN CABIN DOOR IS CLOSED. R & R PAX DOOR PROXIMITY SWITCH PX-101 IAW AMM 52-70-04, OP'S CHECKED GOOD.
Part: DOOR — LEAKING (EMERGENCY EXIT) · airframe 20,136 hrs · 13,709 cycles
RT OVERWING EMERGENCY EXIT HAS LOUD WHISTLE. INSPECTED RIGHT OVERWING EMERGENCY EXIT IAW AMM 52-21-07. OK FOR SERVICE AT THIS TIME.
Part: SEAL — DIRTY (EMERGENCY EXIT) · airframe 20,128 hrs · 13,701 cycles
A LOUD SQUEAL COMING FROM RT SIDE EMERGENCY EXIT. REMOVED DEBRIS, CLEANED AND LUBRICATED RT SIDE EMERGENCY EXIT DOOR SEAL, NO DEFECTS NOTED IAW AMM 52-21-07
Part: HANDLE — UNSECURE (PAX DOOR) · airframe 19,651 hrs · 13,382 cycles
PAX DOOR LATCH CAUTION MESSAGE IN FLIGHT, F/A REPORTED DOOR SENSOR ALIGNMENT MARKING ON PAX DOOR IS RED, PRESSURATION IS NORMAL, PAX DOOR MASTER WARNING DURING DECENT ALTERATION BETWEEN CAUTION AND WARNING MESSAGES. RAMP REPORTED HANDLE WAS AJAR UPON ARRIVAL. PERFORMED OP'S CHECK OF PAX DOOR AND WARNING SYS, NO DEFECTS NOTED AT THIS TIME IAW AMM 52-11-00 & 52-70-00.
Part: DISPLAY — INOPERATIVE (COCKPIT) · airframe 19,646 hrs · 13,379 cycles
DURING TAKEOFF ROLL CAPT'S PFD AND MFD WENT BLANK AND YDI INOPERATIVE, STAB CHAN NR 2, R REV FAULT. R & R SSPC K 126 IAW AMM 24-62-11, OP'S CHECK GOOD.
Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 19,638 hrs · 13,374 cycles
IN FLIGHT, AT 9000 FT, CLIMBING AUTO PILOT OFF AND ACFT IN NORMAL FLIGHT, PDF 1 & MFD 1 WENT TO SYMBOLOGY ONLY. YD 1 DISENGAGED, NUMEROUS STATUS MESSAGES DISPLAYED, MOMENTARY ELECTRONICS ODOR ON FLIGHT DECK. ALL SYS RETURNED TO NORMAL IN APPROX 20 SECOND. NORMAL LANDING. SWAPPED CAPT PFD TO EICAS 1 AND CAPT MFD TO EICASE 2 IAW AMM 31-61-01, ALL SCREEN OP'S CHECKED GOOD.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,162 hrs · 13,063 cycles
ROW 14 CEILING LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE.
Part: STOP — DIRTY (PAX DOOR) · airframe 19,157 hrs · 13,060 cycles
PAX DOOR ALIGNMENT MARKS DO NOT LINE UP WITH DOOR CLOSED. CLEANED AND DRIED PIN STOPS OF PAX DOOR. CLOSED DOOR AND VERIFIED DOOR LATCH PINS ALIGN WITH GREEN INDICATOR MARKS, DOOR OPS CHECKED GOOD IAW AMM 52-11-00, OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (ROW 17) · airframe 19,147 hrs · 13,054 cycles
CEILING EMERGENCY FLOOD LIGHT IN ROW 17 INOPERATIVE.
Part: WARNING MESSAGE — ILLUMINATED (ANTI SKID SYS) · airframe 18,862 hrs · 12,873 cycles
ANTI-SKID CAUTION MESSAGE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,669 hrs · 12,744 cycles
EMERGENCY LIGHT INOPERATIVE AT ROW 10. RELAMPED AND REPLACED CEILING EMERGENCY LIGHT IAW AMM,OP'S CHECKED GOOD.
Part: PROXIMITY SENSOR — INOPERATIVE (PAX DOOR) · airframe 18,280 hrs · 12,481 cycles
PAX DOOR MASTER WARNING ON GROUND WITH DOOR CLOSED AND LOCKED. R & R PASSENGER DOOR PROXIMITY SENSOR PX101 IAW AMM 52-70-04, OP'S CHECK GOOD AT THIS TIME. NO MESSAGE AT THIS TIME.
Part: WIRE — BROKEN (DOOR WARNING) · airframe 18,270 hrs · 12,476 cycles
PAX DOOR LATCH CAUTION MESSAGE IN FLIGHT. FOUND WIRE DAH6142 BROKEN N PAX DOOR, REPAIRED WIRE DAH 6142 IAW ESPM 20-33-00. OP'S CHECK GOOD AT THIS TIME.
Part: DOOR FRAME — DIRTY (PAX DOORWAY) · airframe 18,218 hrs · 12,443 cycles
PAX DOOR LATCH CAUTION MESSAGE. CLEANED DEBRIS FROM LOWER DOOR JAM, PERFORMED OP'S CHECKED OF PAX DOOR IAW AMM 52-70-00.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,189 hrs · 12,402 cycles
EMERGENCY LIGHT ROW 9 INOPERATIVE. R & R BULB, OPS CHECKED GOOD IAW AMM 33-51-15.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,631 hrs · 12,066 cycles
CEILING EMERGENCY LIGHT AT ROW 17 INOPERATIVE. R & R LIGHT AT ROW 17 IAW AMM 33-57-09.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,596 hrs · 12,042 cycles
AFT EMERGENCY EXIT CEILING LIGHT INOPERATIVE. R & R AFT EMERGECNY CEILING LIGHT IAW AMM 33-51-09. OPS CHECKED GOOD.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 16,955 hrs · 11,616 cycles
OVERHEAD EMERGENCY LIGHT BULB OUT AT ROW 15. R & R EMERGENCY LIGHT BULB AT ROW 15 IAW AMM 33-51-09. OPS CHECKED GOOD.
Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 16,680 hrs · 11,436 cycles
PAX DOOR OUTER HANDLE CAUTION MESSAGE. DEFFERED DOOR INDICATION ON MEL 52-70-01, CAT A.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 16,407 hrs · 11,261 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 15 IS INOPERATIVE. R & R BULB IN EMERGENCY LIGHT AT ROW 15 IAW AMM 33-51-09.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,374 hrs · 11,241 cycles
OVERHEAD EMERGENCY LIGHT IN ROW 17 INOPERATIVE. IAW TELECON, DEFERRED CEILING LIGHT AT ROW 17 ON DMI 20460 IAW MEL 33-51-01B, CAT C.
2011
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 15,685 hrs · 10,823 cycles
OVERHEAD EMERGENCY LIGHT IN CABIN BURNED OUT. R & R EMERGENCY CEILING FLOOR LIGHT BETWEET ROWS 9/10 IAW AMM 33-51-09. OPS CHECKED GOOD.
Part: LIGHT — BURNED OUT · airframe 15,680 hrs · 10,819 cycles
UPPER MOST STAIR LIGHT HALF BURNED OUT. DEFFERED UPPER STAIR LIGHT IAW MEL 33-21-02, CAT D ON DMI 19383.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 15,679 hrs · 10,818 cycles
PAX DOOR MID CAP ANGLE HAS CORROSION. INSTALLED NEW MID CAP ANGLE IAW SRM 51-42-06 AND 51-42-20.
Part: SCREW — MISSING (HANDRAIL) · airframe 15,679 hrs · 10,818 cycles
PAX DOOR AFT HANDRAIL SHOULDER SCREW MISSING. INSTALLED MISSING SCREW IAW AMM 52-11-05.
Part: CABLE — BROKEN (PAX DOOR) · airframe 15,679 hrs · 10,818 cycles
PASSENGER DOOR VENT CABLE BROKE. R & R PASSENGER DOOR PRESSURE VENT FLAP CABLE IAW AMM 52-11-15.
Part: CROSSBEAM — CORRODED (BS 280) · airframe 15,679 hrs · 10,818 cycles
FRAME STATION 280, CROSSBEAM HAS CORROSION. ACCOMPLISHED CROSSBEAM 280 REPLACEMENT-SPLICE REPAIR IAW REO 670-53-470.
Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 15,679 hrs · 10,818 cycles
SERVICE DOOR MOUNTING ANGLE HAS CORROSION. R & R SERVICE DOOR ANGLE IAW SRM 51-42-06 & 51-42-21.
Part: FITTING — CORRODED (STRIKER SEAL) · airframe 15,679 hrs · 10,818 cycles
SERVICE DOOR STRIKER SEAL FITTING HAS CORROSION. R & R STRIKER SEAL FITTING IAW SRM 51-42-06 & 51-42-21.
Part: FITTING — CORRODED (BS 314) · airframe 15,679 hrs · 10,818 cycles
PASSENGER DOOR FORWARD CLOSING FITTING AT FS314.00 HAS CORROSION. R & R PASSENGER DOOR FITTING IAW SRM 51-42-06.
Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 15,679 hrs · 10,818 cycles
COCKPIT FLOOR SUPPORT ANGLE AT FS280 HAS CORROSION. REMOVED AND REINSTALLED NEW FLOOR SUPPORT ANGLE IAW SRM 51-42-06 AND 51-42-20.
Part: PROXIMITY SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 15,401 hrs · 10,638 cycles
PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE. ADJUSTED PASSENGER DOOR PROX SWITCH PX107 IAW AMM 52-70-04. OPS CHECKED GOOD.
Part: BULB — BURNED (EMERGENCY LIGHT) · airframe 15,377 hrs · 10,624 cycles
5TH CEILING EMERGENCY LIGHT INOP. R & R 5TH CEILING EMERGENCY LIGHT BULB IAW AMM 33-51-09. OPS CHECKED GOOD.
Part: WARNING MESSAGE — INTERMITTENT (PAX DOOR HANDLE) · airframe 15,377 hrs · 10,624 cycles
INTERMITTENT PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE. DEFFERED PASSENGER DOOR INDICATION IAW MEL 52-70-01, CAT A.
Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 14,982 hrs · 10,374 cycles
EMERGENCY CEILING FLOOD LIGHT INOP BETWEEN ROWS 10/11. DEFFERED CEILING EMERGENCY LIGHT BETWEEN ROWS 10 AND 11 ON DMI 22319 IAW MEL 33-51-01B. ON 7/3/2011 CLEARED DMI 22319, MEL 33-51-01B, CAT C , R & R LIGHT BULB IAW AMM 33-51-09. OPS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,904 hrs · 10,326 cycles
ROW 4 AND 17 EMERGENCY LIGHTS INOP. DEFFERED EMERGENCY CEILING FLOOD LIGHTS AT ROW 4 AND 17 IAW MEL 33-51-01B, CAT C, MX CONTROL.
Part: HANDLE — CRACKED (PAX DOOR) · airframe 14,845 hrs · 10,288 cycles
CRACK IN PASSENGER DOOR OUTER HANDLE. PERFORMED TEMP REPAIR NR 3 AND PLACED ON CARRY OVER NR 1597, REF REO 670-52-11-196. REINSPECT EVERY 100 FLIGHT HOURS REPLACE BY 1000 FLIGHT HOURS IAW MX CONTROL. PERFORMED NDT ON PASSENGER DOOR HANDLE AFTER CRACK REMOVAL IAW REO 670-52-11-196. NO DEFECTS WERE NOTED.
Part: DOOR — STUCK (EMERGENCY EXIT) · airframe 14,294 hrs · 9,943 cycles
COCKPIT EMERGENCY HATCH WILL NOT OPEN. REPOSITIONED HATCH AND PERFORMED OPS TEST OF DOOR. ALL INDICATIONS NOEMAL IAW AMM 52-22-00.
Part: TRIM PANEL — LOOSE (EMERGENCY EXIT) · airframe 14,045 hrs · 9,795 cycles
RT OVERWING EMERGENCY EXIT TRIM LOOSE. RESECURED TRIM IAW AMM 52-21-00.
Part: OVERHEAT — FALSE ACTIVATION (MLG) · airframe 13,973 hrs · 9,753 cycles
BRAKE OVERHEAT WARNING MESSAGE NR 1 LT OTBD. REMOVED, CLEANED, AND REPLACED NR 1 BRAKE TEMP SENSOR IAW AMM 32-46-01, SELF TEST NORMAL AT THIS TIME.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 13,939 hrs · 9,731 cycles
EMERGENCY LIGHT OVER ROW 4 AND 15 ARE NOT WORKING. RELAMPED EMERGENCY LIGHTS OVER ROW 4 AND 15 IAW AMM 33-51-09.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,244 hrs · 9,282 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 9-10 INOP. DEFERRED LIGHT IAW MEL 33-51-01B.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,543 hrs · 8,808 cycles
CEILING LEVEL EMERGENCY FLOOD LIGHT OUT 2ND LIGHT FROM AFT. R & R BULB IN EMERGENCY FLOOD LIGHT IAW AMM 33-24-01. OPS CHECK GOOD.
Part: TRIM SYSTEM — MALFUNCTIONED · airframe 12,171 hrs · 8,534 cycles
STAB TRIM RUNAWAY IN FLIGHT. DEFERED AUTOPILOT ON DMI 16728 CAT B APPROVED.
Part: GROMMET — OUT OF POSITION (BLEED AIR SYS) · airframe 12,146 hrs · 8,514 cycles
R BLEED DUCT MASTER WARNING AT 28000FT. INSPECTED DUCTING FOR LEAKS AND REPOSITIONED LOOP GROMMET AT MT145R AFTER INSP MDC MESSAGES. NO ACTIVE LEAKS FOUND. NO FURTHER MESSAGES NOTED REF TO CRJ700 FIM 36-10-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,096 hrs · 7,808 cycles
CEILING EMERGENCY FLOOD LIGHT NEAR ROW 15 INOP. DEFFERED CEILING EMERGENCY FLOOD LIGHT ON DMI NR 13478 IAW MEL 33-51-01B, CAT C.
Part: SLAT SYSTEM — MALFUNCTIONED · airframe 10,895 hrs · 7,657 cycles
SLATS FAIL. RESET SLAT ACTUATOR TRIP INDICATORS. PERFORMED OPS CHECK OF SLAT SYS. OPS CHECK GOOD IAW FIM 27-81-00.
2009
Part: ADC — MALFUNCTIONED (NR 2) · airframe 8,980 hrs · 6,271 cycles
HAD EFIS COMP MONITOR, IAS, ALT, RUDDER LIMIT, MACH TRIM FAULTS IN THAT ORDER. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER IAW AMM 34-13-01.
Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 8,945 hrs · 6,245 cycles
LT HYD LOW. REMOVED AND REPLACED NR 1 ENGINE HYD PUMP IAW AMM 29-11-01. OPS AND LEAK CHECK GOOD AT THIS TIME.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,919 hrs · 6,232 cycles
CEILING LEVEL EMERGENCY FLOORLIGHT AT 6A INOP. IAW TELECOM NR 70956 DEFERED EMERGENCY CEILING LIGHT AT 6A ON DMI NR 11098, IAW MEL 33-51-01-02A CAT C.
Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 8,868 hrs · 6,194 cycles
EMERGENCY LIGHT COVER BY SERVICE DOOR MISSING. DIFFERED EMERGENCY LIGHT COVER ON BULKHEAD BY SERVICE DOOR ON DMI NR 10146 IAW MEL 33-51-01-2B CAT C, AUTHORIZED.
Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 8,853 hrs · 6,182 cycles
GALLEY FLOOD LIGHT LENS MISSING. DEFERRED IAW MEL 33-51-01-2B.
Part: BATTERY — DISCHARGED (CABIN) · airframe 8,100 hrs · 5,635 cycles
EMERGENCY LIGHTS ON IN FLIGHT. EMERGENCY LIGHTS CAME ON IN THE FRONT OF THE ACFT CABIN AND STAYED ON FOR MUCH OF THE FLIGHT. REMOVED AND REPLACED EMERGENCY BATTERY NR 1 POSITION. OPS CHECK GOOD.
2008
Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 6,481 hrs · 4,480 cycles
FLMX-ORD. EXTERIOR EMERGENCY LENS CRACKED. INSTALLED NEW LENS IAW AMM 33-51-16.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,145 hrs · 3,553 cycles
LT WING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACE BULB.
Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 5,145 hrs · 3,553 cycles
LT WING EMERGENCY EXIT LIGHT INOP. REPLACE BULB.
Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 4,975 hrs · 3,448 cycles
EXIT ROW 12 LT LOWER EMERGENCY EXIT SIGN HAS INOP BULB. REPLACED BULB.
Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 4,766 hrs · 3,300 cycles
EMERGENCY EXIT SIGN INOP AT ROW 12 LT SIDE. REPLACED BULB.
2007
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 4,254 hrs · 2,946 cycles
EMERGENCY EXIT SIGN AT ROW 12A INOP. REPLACED BULB.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 4,249 hrs · 2,940 cycles
OVERHEAD EMERGENCY LIGHT IN CABIN INOP. REPLACED BULB
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 3,881 hrs · 2,680 cycles
RT EXTERIOR EMERGENCY LIGHT INOP OVERWING EMERGENCY EXIT. REPLACE BULB, OPS OK.