N702PS
Registered owner: AMERICAN AIRLINES INC, TX (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
APPR 20 MINS INTO OCF RECEIVED PROX SYS 1 FAULT STATUS MSG FOLLOWED BY GEAR AND FLAP ICONS THEN COULD HEAR GEAR TRYING TO EXTEND. PROBLEM PROGRESSIVELY BECAME MORE FREQUENT THROUGH REST OF FLIGHT AND RIGHT MLG GEAR STARTED SHOWING IN TRANSIT ON EICAS. COMMANDED EXTENSION FOR LANDING WAS NORMAL / REMOVED THE PINS FROM THE OLD TERMINAL BLOCK TM117 TO THE NEW TERMINAL BLOCK IAW TAP 3230-070-001-25-702-3 & RIL 13951. LANDING GEAR OPS CHECKED GOOD. PSEU REMOVED & REPLACED IAW 32-61-01-000/400-801.
UNCOMMANDED RELEASE OF MLG, HYDS REPRESSURIZED AND RETRACTED, RAN QRC FOR GEAR DISAGREE FOR APPROACH SUCCESSFULLY. DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL 32-30-01-2. REMOVED AND REPLACED SELECTOR VALVE IAW AMM 32̉‰32̉‰10̉‰000/400̉‰801. OPS CHECK GOOD. LEAK CHECK GOOD.
RH WING JACK POINT MISSING HELI-COIL AND NYLON PLUG. CORRECTIVE ACTION: COMPLIED WITH MHIRJ REO 670-57-22-155, REV -- DATED 2025-09-22 - TEMPORARY DISPOSITION FOR REMAINING THREADS AFTER REAMING RH WING JACKING FITTING BORE (DEVIATION TO GENERIC REO 670-57-22-004 REV-F'). REFERENCE RFTS-124472 FOR TRACKING. CC670-10126-3
R/H AILERON UPPER LEADING EDGE IS CHAFED IN SEVERAL AREAS. CORRECTIVE ACTION: PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-57-61-194 REV -C DATED 2019-01-07. CC670-1305-1,-2,-3,-4
LH SLAT TRACK 2-3 LOWER BRACKET IS BROKEN. CORRECTIVE ACTION: REMOVED AND REPLACED BRACKET ASSEMBLY IAW CRJ-700 AMM 20-21-00-910-801-A01. CC670-12065-1
CA WINDSHIELD OUTER LAYER MULTIPLE CRACKS DURING FLIGHT. PERFORMED INSTALLATION OF LH SIDE WINDOW IAW AMM 56-12-01-400-801-A01-PSA.
STEERING INOP CAUTION MSG ON DECENT. / REMOVED AND REPLACED THE PSEU IAW AMM 32-61-01-00-801-A01 ,PERFORMED FUNCTIONAL TEST OF THE NOSE WHEEL STEERING AND OPERATIONAL TEST OF THE NOSE WHEEL STEERING IAW AMM 32-51-00-720-801-A01 AND 32-51-00-710-801-A01 RESPECTIVELY ,TEST IS GOOD AT THIS TIME.
DURING CRUISE ABOUT 1HR 20MIN INTO FLIGHT AT FL330 PROS SYS FAULT 1 STATUS MSG AND RIGHT LNDING GEAR YELLOW ON LANDING GEAR DISPLAY. SLOWED TO 220KTS AND BELOW MSG WAS INTERMITTENT. FELT SHUDDERING / REMOVED AND REPLACED LANDING GEAR LEVER CONTROL IAW CRJ700 AMM 32-31-01-000/400-801-A01. REMOVED AND REPLACED PSEU IAW CRJ 700 AMM 32-61-01-000/400-801-A01. DID POWER UP TEST OF LANDING GEAR PSS IAW CRJ 700 AMM 32-61-00-740-801-A01. TEST PASSED AT THIS TIME.
FOUND THE L/H WING INBOARD LEADING EDGE SKIN TO HAVE GOUGE DAMAGE ON THE OUTBOARD END AT WS 144.94
FOUND LH SLAT #1 TO HAVE GOUGE NEAR MIDDLE ON BOTTOM SIDE.
TOTAL FUEL INDICATION DECREASED RAPIDLY DURING CLIMB / C/W EXTERNAL ZONAL INSPECTION OF A/C IAW CRJ700 AMM 05-21-00-210-802-A01. NO FUEL LEAKS NOTED. C/W OPS. TEST OF FUEL QTY. GAUGING COMPUTER IAW CRJ700 AMM 28-41-22-710-801-A01.. NO DEFECTS NOTED. DEFERRED EICAS FUEL TANK QTY. READ OUTS PER MEL 28-41-01-2 CAT B. M FUNCTION C/W. . REMOVED AND REPLACED FQGC IAW CRJ700 AMM 28-41-22-000/400-801. OPS CHECK GOOD AT THIS TIME.
LOUD RUMBLING SOUND/VIBRATION FROM UNDER NOSE DURING FLIGHT SUSPECT NOSE GEAR DOORS NOT SEATING PROPERLY. REPLACED RH NLG DOOR AND ASSOCIATED HARDWARE IAW CRJ 700 AMM 32-22-01-000/400-801.
IN CRUISE FLIGHT AT FL310 CREW GOT GEN2 CAUTION MESSAGE. CA TOOK OVER THE CONTROLS AND FO RAN THROUGH ( QRC/QRH) BUT THE MESSAGE WAS STILL THERE. APU WAS ALREADY DIFFERED SO CREW DECLARED MECHANICAL EMERGENCY. CREW DID A NORMAL LANDING IN CLT ( NO OVERWEIGHT AND NO BRACE IN CABIN). PLANE TAXIED TO GATE UNDER ITS OWN POWER TRUCKS ROLLED. NO OXYGEN, NO EMK KIT AND NO INJURIES. REMOVED AND REPLACED GCU2. OPS CHECK GOOD
FORWARD CARGO DOOR, AFT HINGE ARM HAS CHAFFING AND GOUGING
L/H SLAT TRACK 3-1 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKS
L/H SLAT TRACK 2-1HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKS
L/H SLAT TRACK 1-2 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKS
L/H SLAT TRACK 1-3 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKS
PREVIOUS REPAIR ON PAX DOOR FORMER AND PULLEY HINGE BRACKET AT FS 347.25, DATUM 4 HAS WORKING/LOOSE FASTENERS.
EA 12-2020-258 (PERMANENT REPAIR OF SERVICE DOOR HINGE ASSEMBLY) ACCOMPLISH PERMANENT REPAIR PER EA 12-2020-258.
L/H SLAT TRACK 3-3 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKS
GOUGE ON PREVIOUS REPAIR BETWEEN FS 977 - FS 985 STGR 27
HSTA JACK SCREW MOUNT FITTING HAS SIGNS OF TOOLING MARK DAMAGE NEAR RH OUTBOARD UPPER MOUNT HOLE
L/H SLAT TRACK 1-1 HAS MULTIPLE AREAS OF WEAR DAMAGE FROM UPPER AND LOWER ROLLERS AND ALSO MULTIPLE AREAS OF WEAR DAMAGE FROM RUB BLOCKS
FLOORBEAM AT LBL 27 HAS MULTIPLE SPOTS OF CORROSION FROM FS1000 TO FS1088
FLOORBEAM AT LBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM FS1000 TO FS1088
R/H OUTBD GROUND SPOILER CENTER HINGE UPPER SURFACE LEADING EDGE CRACKED.
LOWER FRAME SEGMENT FS 364 (FWD SIDE) IS CORRODED SEVERAL LOCATIONS BETWEEN STRG 25L AND STRG 25R.
FLOORBEAM AT RBL 27 HAS MULTIPLE SPOTS OF CORROSION FROM FS1000 TO FS1088.
FLOORBEAM AT RBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM FS1000 TO FS1088
L/H INBD FLAP INNER SKIN IS CHAFFED UNDER PANEL 584DB
REO 670-52-35-448(PERMANENT REPAIR) BLENDED GOUGE DAMAGE ON FWD CARGO DOOR FWD INNER ARM.
LH O/B FLAP AT WS 178 AFT HINGE POINT FITTING ON WING HAS CHAFING ON METAL
RH HSTA SCREW JACK MOUNT FITTING HAS BURRS AND SIGNS OF TOOLING DAMAGE NEAR UPPER MOUNT BOLT ATTACH POINTS.
CA SIDE WINDOW ARCING AT BOTTOM, APPROX 8-10 INCHES FROM PILLAR, CYCLED LH WINDOW HEAT, ARCING LESS INTENSE, ARCING STOPPED ONCE UNDER 15K FEET / DEFERRED LH SIDE WINDOW HEATING SYSTEM PER MEL 30-41-02 CAT A. DEACTIVATED LH SIDE WINDOW HEAT CONTROLLER BY PULLING AND COLLARING CBP-1 U10 & CBP-2 S4. PERFORMED REMOVAL OF L.H. FLIGHT COMPARTMENT SIDE WINDOW IAW CRJ 700 AMM 56-12-01-001-801-A01-PSA. INSTALLED LH FLIGHT COMPARTMENT SIDE WINDOW IAW CRJ 700 AMM 56-12-01-400-801-A01-PSA REV C UP TO STEP 5(D). OPS CHECK GOOD. STEP 5(E)-5(H) NEED TO BE C/W.COMPLIED WITH STEPS 5(E) IAW CRJ 700 AMM 56-12-01-400-801-A01-PSA. LEAK CHECK GOOD AT THIS TIME.
STAB TRIM RUNAWAY TOWARDS NOSE DOWN ON SHORT FINAL / PERFORMED DFDR DOWNLOAD IAW CRJ 700 AMM 31-33-01-970-802-A01. R&R OF THE HORIZONTAL STABLIZER MOTOR CONTROL UNIT IAW CRJ700 AMM 27-42-07-000/400-801-A01, & C/W SELF TEST OF THE SSCU IAW CRJ700 AMM 27-61-05-740-801-A01 OPS CHK GOOD.
EMERGENCY DECLARED GOING INTO PWM DUE TO IB FLIGHT SPOILER MESSAGE. NO TRUCKS WERE ROLLED AND NO NEED TO BRACE. FLIGHT LANDED SAFELY AND IS ON THE PHONE WITH MX NOW / CYCLED SYSTEM CBS AND PERFORMED SPOST2 TEST IAW CRJ700 AMM 27ÃËâ61ÃËâ05ÃËâ740ÃËâ801-A03 FAULT CLEARED AND DID NOT RETURN SYSTEM SYSTEM OPS CHECKS AT THIS TIME A/C OK FOR SERVICE.
DUE TO NOSEWHEEL STEERING INOP MESSAGE CAPTAIN INFORMED OPS AND ATC OF ISSUE AND ATC DECLARED AN EMERGENCY FOR THE FLIGHT. R/R LANDING GEAR SELECTOR VALVE IAW CRJ 700 AMM 32-32-10-000/400-801. OPS CHECK GOOD AT THIS TIME.
ON TAKEOFF OUT OF TLH, CREW REPORTED A STEERING INOP MESSAGE, CREW RAN QRH. CREW THEN DECLARED AN EMERGENCY IN ORDER TO GET PRIORITY HANDLING AND THE LONG RWY (36C) IN CLT. UPON LANDING MAINTENANCE TOWED AIRCRAFT OFF TO SAFETY. CREW WAS ABLE TO RESET AND TAXI TO GATE UNDER THEIR OWN POWER. AIRCRAFT WAS NOT OVERWEIGHT, EMERGENCY VEHICLES WERE STANDING BY. STEERING INOP CAUTION MSG ON TAKE OFF IN TLH / REMOVED AND REPLACED THE STEERING WHEEL HARNESS IAW CRJ 700 AMM 32-21-01-000/400-803, OPS CHECK GOOD."
FRAME AT FS 349.00 HAS CORROSION ON THE FLANGE AT STRINGER 26R. REMOVED AND REPLACED FRAME P/N SH670-31357-5 IAW CRJ 700 SRM 51-42-06-001-001-A01.
LT FS 280 CROSSBEAM IS CORRODED. INSTALLED NEW SERVICEABLE LT FS280 FLOORBEAM IAW SB670BA-53-041 REV H DATED JUNE 14/2019.
INNER PASSENGER DOOR HANDLE CRACKED AT INNER TAPGER PIN HOLE, P/N 600-31887-15. INSTALLED NEW HANDLE IAW CRJ700 SRM 51-40-11-001-001-A01.
STRINGER 25R IS CORRODED BETWEEN FS 1051-1098. REPAIRED IAW SRM 53-00-03-201-001-A01.
STRINGER 3L, PASSENGER DOOR LINTEL IS CRACKED AT FS 283. REPAIRED PER REO 670-53-21-1793 REV-P2.
STRINGER 20R BETWEEN FS863 TO FS879 HAS CORROSION AT RIVET. REPAIRED IAW EA: 80-2020-004 REV-P4, DATED 08/25/20.
PASSENGER DOOR OUTER DOOR HANDLE IS CRACKED. INSTALLED NEW SERVICEABLE PASSENGER DOOR OUTER HANDLE, IAW CRJ700 AMM 52-11-03-400+-801-A01.
FS 1047 FRAME IS CORRODED BETWEEN STRINGER 27 AND STRINGER 26L. REPAIRED FRAME SEGMENT.
FS 1051 FRAME IS CORRODED BETWEEN STRINGER 25L AND STRINGER 25R. REPAIRED IAW STS EA 79-2020-009 REV P2 DATED 8/19/2020.
STRINGER 25R IS CORRODED BETWEEN FS319.70 AND FS333 AT NUMEROUS LOCATIONS. INSTALLED NEW STRINGER 25R, IAW CRJ700 SRM 51-42-06-001-001-A01.
SERVICE DOOR LOWER SILL IS CORRODED BETWEEN FS 319 AND FS 349. INSTALLED NEW SERVICE DOOR LOWER SILL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
PASSENGER DOOR INNER SKIN IS CORRODED BETWEEN DATUM AND DD1A FS313-FS320. INSTALLED NEW INNER SKIN P/N 601R318024-7 IAW CRJ 700/900 SRM 51-42-06-001-001-A01,51-42-13-001-001-A01,51-42-15-001-001-A01,51-42-21-001-001-A01,51-42-22-001-001-A01.
PASSENGER DOOR STEPS AFT WEB REPAIR HAS MULTIPLE CRACKS AROUND ORIGINAL SKIN FASTENER HOLES. MULTIPLE DEFORMED FASTENER HOLES, AND MULTIPLE RIVET SHOP HEADS ARE MISFORMED. REPAIRED IAW EO CL-600-2C10-52-LO0537 DATED 8-19-2020.
PASSENGER DOOR STEPS AFT WEB IS CRACKED AT LOWER STEP CORNER. COMPLIED WITH EO CL-600-2C10-52-LO6535 DATED 8-19-20 STEPS A(1-13) AND B(1-7).
RT NR 2 EXTERIOR EMERGENCY LIGHT INOP. MX REPLACED BULB IAW AMM 33-51-15-000/400-801. OPS CHECK FAILED. FOUND MULTIPLE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY NR 3 IAW AMM 33-51-17-000/400-801. OPS CHECK GOOD AT THIS TIME. (PN: AD2013-1A SN: 173877)
AFT FORMER CRACKED IN PAX DOOR. REPAIRED IAW MHIRJ REO 670-52-11-1153 P1.
EMERGENCY CEILING LIGHT OVER ROW 1 BURNT OUT. MX REPLACED THE BULB AND 2 SOCKETS IN THE J355 CONNECTOR. OPS CHECK GOOD.
TWO CEILING EMERGENCY LIGHTS INOP. FOUND BROKEN WIRE GOING TO CONNECTOR, RE-PINED BROKEN WIRE AND INSTALLED IN CONNECTOR IAW CRJ700 ESPM 20-26-03. RELAMPED CEILING EMERGENCY LIGHTS IAW CRJ700 AMM 33-51-09-960-801. OPS CHECK GOOD.
ENROUTE TO DCA CREW REPORTED A RIGHT BLEED ANTI ICE DUCT WARNING MESSAGE. CREW DECLARED EMERGENCY. CREW LANDED IN DCA WITH NO ISSUES AND FIELD EMERGENCY EQUIPMENT DID NOT RESPOND. MX REMOVED AND REPLACED RH BLEED AIR SUPPLY DUCT IAW CRJ 700 AMM. OPS CHECK GOOD FAULT CLEARED
FLIGHT ATTENDANTS REPORTED VERY STRONG ODOR IN AIRCRAFT AFTER PUSH BACK. RUN BOTH LEFT AND RIGHT ENGINE WITH CREW AND PERFORMED OPERATIONAL CHECK OF BOTH AIR CONDITIONING PACK. NO ODOR NOTED AT THIS TIME.
REMOVED AND REPLACED OVERHEAD EMERGENCY FLOODLIGHT MOLEX CONNECTOR P355. REMOVED AND REPLACED OVERHEAD EMERGENCY FLOODLIGHT BULB OVER ROW 1A. PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS, OP CHECKS GOOD.
DURING APPROACH TO PHL THE CREW RECEIVED A FLAPS FAIL AND DECLARED AN EMERGENCY. TRUCKS ROLLED. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE. THE AIRCRAFT WILL BE FERRIED TO A MAINTENANCE BASE FOR REPAIR. FOUND BOTH RT OB ACTUATORS NOT SUFFICIENTLY LUBRICATED, LUBRICATED THE RT OB ACTUATORS AND REMOVED AND REPLACED LT BPSU, OPS CHECK GOOD.
DURING LANDING, THE CREW RECEIVED A FLAPS FAIL AT 40 DEGREES. DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE WITHOUT INCIDENT. CLEARED INHIBITS AND C/W ELECTRICAL EXTENSION AND RETRACTION OF FLAP/SLAT SYS IAW AMM 27-52-00-864-801/802. OPS CHECK GOOD AT THIS TIME.
DURING APPROACH TO PHL THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE AND DECLARED AN EMERGENCY. TRUCKS ROLLED. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE. CLEARED INHIBITS THROUGH MDC AND OPERATIONAL TEST OF THE FLAPS AND SLATS SYSTEM WAS PREFORMED IAW AMM 27-50-00-710-801 NO FURTHER DEFECTS NOTED. A/C OK FOR SERVICE
SUPPLEMENTAL INFORMATION: SECURED RH BLEED LOOP STAND OFF, TIGHTENED RH PACK PLENUM SLEEVE, REPLACED RH FLOW CONTROL VALVE FWD CONNECTOR DUCT AND CW WING A-ICE OPS CHECK. OPS AND LEAK CHECK GOOD.
THE AIRCRAFT DIVERTED AND DECLARED AN EMERGENCY DUE TO RIGHT BLEED DUCT MESSAGE. MAINTENANCE RE-POSITIONED MT204 AWAY FROM A METAL CLAMP.
CREW HAD A SMOKE BURNING ODOR WHEN THEY TURNED ON THE PACKS, MX INSPECTED AND FOUND THE RT PACK CAUSING THE ODOR.
PASSENGER DOOR OUTER HANDLE FLAP NOT FLUSH. REPOSITIONED PASSAGER DOOR OUTER HANDLE FLAP. OPS CHECKED GOOD.
BURNING ODOR IN COCKPIT AND CABIN, LEFT AIR CONDITIONING PACK INOPERABLE. REMOVED AND REPLACE THE LEFT ACM.
SLATS FAIL CAUTION MESSAGE ON APPROACH. CREW CONDUCTED A MISSED APPROACH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL TEST OF FLAPS AND SLATS SYSTEM IAW AMM. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.
EMERGENCY LIGHT LOOSE. MAINTENANCE INSPECTED, SECURED THE EMERGENCY LIGHT AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
CABIN EXIT SIGN 16F AT EMERGENCY EXIT HAD ONE BULB INOPERATIVE. MAINTENANCE INSPECTED, REPLACED THE BULB AND PERFORMED CHECKS IAW AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
F.S. 280 FWD J-ANGLE IS CORRODED BEYOND LIMITS. MAINTENANCE R & R J-ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
CREW REPORTED ACFT WOULD NOT PRESSURIZE AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND AFT CARGO DOOR NOT PROPERLY CLOSED. MAINTENANCE CLOSED AFT CARGO DOOR AND PERFORMED CHECKS IAW AMM. NO DEFECTS NOTED. ACFT RELEASED FOR SERVICE.
CREW REPORTED EMERGENCY FLOOD LIGHT OUT, 5TH FROM FRONT. R & R EMERGENCY FLOOD LIGHT BULB IAW AMM 33-51-09-000/400-801. OPS CHECK GOOD.
CREW REPORTED CABIN WOULD NOT PRESSURIZE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND AFT SECTION OF AFT CARGO DOOR NOT SEATED. MAINTENANCE PERFORMED OPS CHECK OF AFT BAGGAGE BAY DOOR IAW AMM. OPS CHECK GOOD. ACFT RELEASED FOR SERVICE.
BS 280.00 FLOORBEAM IS CRACKED AT LBL 12.5 ON TOP AND CORRODED LBL 9, RBL 28, AND RBL 36. PERFORMED A PERMANENT REPAIR IAW SRM 53-11-41-201-003-A01.
SERVICE DOOR SILL IS CORRODED AROUND FORWARD MOUNT FITTING. REMOVED AND REPLACED SERVICE DOOR SILL IAW SRM 51-40-11-001-A01, 51-42-06-001-A01, 51-25-01-001-001-A01, AND 51-21-11-001-001-A01.
RT LOWER BULKHEAD WEB AT BS 280 IS CORRODED BETWEEN RBL 39 AND RBL 46. REPAIRED IAW REO 670-53-11-594.
LT LOWER BULKHEAD WEB AT FS 280 IS CORRODED AT LBL 18 AND LBL 26. REPAIRED IAW REO 670-53-11-594.
BS 280, FORWARD J-ANGLE IS CORRODED AROUND FASTENER HOLES. R & R THE J-ANGLE IAW SRM 51-40-11-001-A01 AND 51-42-21-001-001-A01.
CREW REPORTED NOSE WHEEL STEERING INOPERATIVE CAS MESSAGE AFTER TAKEOFF. DECLARED AN EMERGENCY PRIOR TO ARRIVAL AT DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW FAULT ISOLATION MANUAL, R & R LANDING GEAR SELECTOR VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
CREW REPORTED ACFT FAILED TO PRESSURIZE DURING CLIMB THROUGH 10,000 FT. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R CABIN PRESSURE CONTROL PANEL, AND OUTFLOW VALVE. PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
CREW REPORTED ANTI-SKID FAULT STATUS MESSAGE DURING CLIMBOUT. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R ANTI-SKID OTBD CONTROL VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
LEFT EMERGENCY EXIT ROW FORWARD FLOOR PATH LIGHT CRACKED. MAINTENANCE REMOVED A 7 INCH SECTION AT 3 D/F AND A 7 INCH SECTION AT 6 ACFT AND INSTALLED TWO SECTIONS AT LT EMERGENCY EXIT ROW FORWARD PATH LIGHT CROSS SECTION. ALL WORK ACCOMPLISHED BY MAINTENANCE IAW AMM. ACFT RELEASED FOR SERVICE.
DURING MX, A GROUND LUG WAS FOUND CORRODED. SILL REPLACED IAW AMM. ACFT RELEASED FOR SERVICE.
CREW REPORTED GEAR DISAGREE AFTER TAKEOFF. CREW PERFORMED QRH, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MX INSPECTED, R & R LANDING GEAR SELECTOR VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
CREW REPORTED PREFLIGHT TEST OF EMERGENCY LIGHTS FOUND ALL GALLEY LIGHTS INOPERATIVE, ROW 1 BULKHEAD LIGHTS BOTH INOPERATIVE, ROW 3 AND 4 SOFT BULKHEAD LIGHTS INOPERATIVE, LOWER RIGHT ROW 12 A/C AND EMERGENCY EXIT CEILING LIGHT INOPERATIVE ROW 12. MX INSPECTED, R & R EMERGENCY LIGHTS BATTERIES AND PERFORMED CHECKS IAW MM. ACFT RELEASED FOR SERVICE.
DURING SCHEDULED MAINTENANCE FS 202 BULKHEAD CRACKS WERE FOUND CRACKED AT TOP OF POST. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
DURING SCHEDULED MAINTENANCE THE FS 280.0 BEAM WAS FOUND CRACKED AT THE TOP RIGHT AND LEFT LOCATIONS. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED MULTIPLE FLAP AND SLAT MESSAGES ON APPROACH. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP / SLAT SYSTEM, REMOVED AND REPLACED NUMBER ONE SFECU (SLAT / FLAP ELECTRONIC CONTROL UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.
CREW REPORTED LIGHTNING STRIKE ON RADOME IN FLIGHT. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND REMOVED AND REPLACED THE FOLLOWING COMPONENTS DUE TO LIGHTNING STRIKE DAMAGE: NOSE RADOME, WEATHER RADAR AND ONE STATIC WICK (NEAR UPPER TAIL NAV LIGHT). MAINTENANCE PERFORMED CHECKS AND AIRCRAFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS.
CREW REPORTED AIRCRAFT NEVER PRESSURIZED DURING CLIMBOUT. DIFFERENTIAL PRESSURE CLIMBED WITH AIRCRAFT. CABIN ALTITUDE CAUTION MESSAGE APPEARED, FOLLOWED BY MASTER WARNING CABIN PRESSURE. CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND AFT CARGO DOOR UNSEATED. MAINTENANCE CLOSED AFT CARGO DOOR AND PERFORMED OPERATIONAL AND PRESSURIZATION CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.
DURING SCHEDULED MAINTENANCE THE RIGHT INBOARD FLAP WAS FOUND DENTED. THE RIGHT INBOARD FLAP WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED INBOARD FLIGHT SPOILERS AND INBOARD SPOILERONS AMBER CAUTION MESSAGES ON APPROACH TO CLT. CREW LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.
CREW REPORTED RIGHT ENGINE BLEED AMBER CAS MESSAGE IN FLIGHT EN ROUTE FROM LIT TO CLT. CREW DIVERTED TO BNA AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NR 2 ACSC (AIR CONDITIONING SYSTEM CONTROLLER) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.
DURING SCHEDULED MAINTENANCE THE FS 280.0 TRANSVERSE BEAM WAS CORRODED. REPAIRS WERE MADE USING AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT RELEASED FOR SERVICE.
CREW REPORTED LOUD WIND NOISE FROM AROUND THE MAIN CABIN DOOR AFTER DEPARTURE FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, CLEANED THE MAIN CABIN DOOR SEAL AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. NO FAULTS WERE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED A STEERING INOP MESSAGE. AIRCRAFT DIVERTED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE NOSE WHEEL STEERING ELECTRONIC CONTROL UNIT USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.
AT CLT, CREW REPORTED LEFT FORWARD TWO (2) SECTIONS OF ESCAPE PATH STRIPS NOT GLOWING. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE DISCREPANT SECTIONS OF THE EMERGENCY FLOOR PATH MARKING AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.
AT 16,000 FEET AFTER DEPARTURE FROM GPT, CREW REPORTED LEFT ENGINE OIL PRESSURE DROPPED TO ZERO AND THEN DISPLAYED DASHES. FUEL FEED TEMPERATURE ALSO DISPLAYED DASHES. CREW RETURNED TO GPT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND THE LEFT ENGINE 6TH STAGE BLEED AIR DUCT AFT OF THE OIL TANK TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE AND PERFORMED CHECKS. ALL WORK WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
AT CLT, CREW REPORTED A POSSIBLE LIGHTNING STRIKE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RADOME AND THE LOWER TAIL NAVIGATION LIGHT ASSEMBLY. MAINTENANCE REPAIRED A DAMAGED RIVET ON THE LEFT WING. CHECKS WERE PERFORMED. ALL WORK WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS AND REO. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED THE NOSE GEAR WOULD NOT RETRACT, A GEAR DISAGREE CAS MESSAGE AND A PROXIMITY SYSTEM FAULT 1 STATUS MESSAGE AFTER TAKEOFF FROM DAY. AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE NLG LOWER TORQUE-LINK AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED A LEFT ENGINE ANTI ICE CAS MESSAGE. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT USING THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REMOVED AND REPLACED THE LEFT ANTI ICE MODULATING VALVE AND CHECKED AIRCRAFT PER THE AIRCRAFT MAINTENANCE MANUAL. THE AIRCRAFT WAS RELEASED FOR SERVICE.
ON TAKEOFF FROM CLT THE CREW RECEIVED A BRAKE OVERHEAT MESSAGE. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT USING THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REMOVED AND REPLACED THE TEMPERATURE SENSOR TO THE RIGHT OUTBOARD BRAKE. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUAL AND THE AIRCRAFT RELEASED FOR SERVICE.
CREW REPORTED A RIGHT ENGINE BLEED AMBER CAS MESSAGE AND A RIGHT ENGINE COWL MESSAGE AFTER TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE THE FAULT. MAINTENANCE SWAPPED THE RIGHT PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) WITH THE LEFT PRSOV FOR TROUBLESHOOTING PURPOSES AND PERFORMED OPERATIONAL CHECKS IAW THE AIRCRAFT MAINTENANCE MANUAL. NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. NO FURTHER DEFECTS HAVE BEEN NOTED SINCE THE FLIGHT.
CREW REPORTED A SERVICE PANEL DOOR LEFT OPEN. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE SERVICE PANEL DOOR OPEN. MAINTENANCE SECURED THE DOOR CLOSED. NO DEFECTS OR DAMAGE AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED THE GROUND COMMUNICATION DOOR LEFT OPEN AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. MAINTENANCE PERFORMED OPS CHECKS AND CLOSED DOOR. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED A GROUND POWER DOOR LEFT OPEN AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND EXTERNAL POWER DOOR OPEN. MAINTENANCE SECURED DOOR CLOSED. NO DEFECTS OR DAMAGE NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.
LEFT HAND LOWER WEB AT BULKHEAD FS 280, WL 73 IS CORRODED AT VARIOUS AREAS; THE BIGGEST BEING 4"L X 1.5"W. MAINTENANCE PERFORMED REPAIR TO LOWER LEFT HAND BULKHEAD FS 280 IN ACCORDANCE WITH REO 670-53-11-052.
FS 280 FRAME, AT WL 73 IS CRACKED BETWEEN RBL 9 AND RBL 18 APPROXIMATELY .5 INCH L, AT UPPER AFT CHANNEL. MAINTENANCE REMOVED AND REPLACED FRAME AT WL 73 FS 280 AS REQUIRED IN ACCORDANCE WITH THE AIRCRAFT STRUCTURE REPAIR MANUAL 51-42-06-001-001-A01.
FS 280 FRAME, AT WL 73 IS CORRODED FROM LBL 45 TO RBL 9. MAINTENANCE REMOVED AND REPLACED FRAME AT WL 73 FS 280 AS REQUIRED IN ACCORDANCE WITH THE AIRCRAFT STRUCTURE REPAIR MANUAL 51-42-06-001-001-A01.
RIGHT HAND LOWER WEB (AFT) AT FS 280 IS CORRODED IN MULTIPLE AREAS BEYOND REPAIRABLE LIMITS AND REQUIRES REPLACEMENT. MAINTENANCE PERFORMED REPAIR TO LOWER RIGHT HAND BULKHEAD FS 280 IN ACCORDANCE WITH REO 670-53-11-052.
CREW REPORTED THE NR 2 HYDRAULIC SYSTEM FLUID QUANTITY WENT TO 0 PERCENT IN FLIGHT ALONG WITH LOW PRESSURE CAS MESSAGES DURING DESCENT. CREW DECLARED AN EMERGENCY AND LANDED IN SAV WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 2 HYDRAULIC PRESSURE LINE CHAFED AND LEAKING. MAINTENANCE REMOVED AND REPLACED THE NR 2 HYDRAULIC SYSTEM PRESSURE LINE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED THE PANEL FLOODLIGHT SHORTED/SMOKED AND POPPED THE CIRCUIT BREAKER AFTER TAKEFOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE COCKPIT FLOODLIGHT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE ALSO REPLACED THE FLOOD POTENTIOMETER IN ACCORDANCE WITH THE CMM 33-12-16. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED A LOUD SQUEAL FROM RIGHT FRONT NOSE AREA. AIRCRAFT RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE FOUND GROUND SERVICE DOOR OPEN. MAINTENANCE INSPECTED AREA AND SECURED DOOR. AIRCRAFT WAS RELEASED FOR SERVICE.
CREW REPORTED LIGHTNING STRIKE. EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS WERE PERFORMED. PAINT DAMAGE NOTED AND REPAIRED ON NOSE, RADOME AND VHF 2 ANTENNA. THE AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE.
CREW REPORTED A BIRD STRIKE ABOVE RT WINDSHIELD. AREA WAS INSPECTED AND CLEANED. NO DAMAGE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE.
AFTER LANDING CREW REPORTED LIGHTNING STRIKE. EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS WERE PERFORMED. DAMAGE WAS FOUND ON LEFT ELEVATOR TIP FAIRING AND A STATIC WICK BASE. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED TO SERVICE.
AFTER LANDING THE CREW REPORTED THE CAPTAIN'S HEADING INFO WAS UNRELIABLE. MAINTENANCE DISCOVERED EVIDENCE OF LIGHTNING STRIKE DAMAGE ON THE LT WINGLET. EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS WERE PERFORMED. ADDITIONAL LIGHTNING STRIKE DAMAGE WAS FOUND TO THE RT AOA PROBE, LT FLUX VALVE, AND SEVERAL RIVETS ON THE RIGHT SIDE OF THE FUSELAGE. A DENT IN THE RT ELEVATOR LOWER SKIN WAS ALSO DISCOVERED. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
DURING CLIMBOUT THE CREW REPORTED THE AC POWER ACCESS DOOR WAS OPEN. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE DOOR AND FOUND NO DEFECTS. THE DOOR WAS PROPERLY SECURED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
DURING CLIMBOUT THE CREW REPORTED AN OPEN ACCESS DOOR. THE FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AC ELECTRICAL GROUND POWER DOOR OPEN. THE DOOR AND FUSELAGE WERE INSPECTED AND NO DISCREPANCIES WERE FOUND. THE DOOR WAS PROPERLY SECURED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
THE LT NOSE LANDING GEAR DOOR WAS DAMAGED WHEN HIT BY A TOWBAR. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND PERFORMED TEMPORARY REPAIRS IAW REO 670-52-81-015 AND SRM 52-81-02. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.
DURING A SCHEDULED INSPECTION THE RT OUTBOARD MULTI FUNCTION SPOILER CENTER HINGE FITTING ASSEMBLY WAS FOUND CRACKED. MAINTENANCE REMOVED & REPLACED THE HINGE FITTING ASSEMBLY IAW CRJ 700 AMM 57-73-27-000-801-A01 AND 57-73-27-400-801-A01. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.
DURING A ROUTINE INSPECTION, IN ACCORDANCE WITH BOMBARDIER AMM 57-73-27-220-802, MAINTENANCE FOUND THAT THE RIGHT HAND INBOARD SPOILER HINGE FITTING WAS CRACKED. MAINTENANCE IS CURRENTLY PERFORMING SERVICE BULLETIN 670BA-57-006, REPLACEMENT OF HINGE FITTING.
DURING CLIMBOUT, THE CREW RECEIVED A MACH AND STAB TRIM FAIL INDICATION AND RETURNED TO CLT. MAINTENANCE INSPECTED AND RESET CIRCUIT BREAKERS CBP-1, F-1, P-2, R-4, R-3, AND F-1 AND THE MESSAGE CLEARED. THEN MAINTENANCE ALSO PERFORMED OPERATIONAL CHECKS ON THE STAB TRIM IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 27-140-120. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.
FLIGHT 2292 RETURNED TO GATE WITH ANTI ICE DUCT MESSAGE, BLEED LOOP FAIL. MAINTENANCE INSPECTED AND REPLACED THE GROUND AIR CONNECTION GASKET IN ACCORDANCE WITH THE BOMBARDIER MAINTENANCE MANUAL 36-17-01-400-801-A01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RELEASED FOR SERVICE.