N17108

Part: STRIP — MISSING (CABIN) · airframe 39,520 hrs · 23,044 cycles

DURING MX INSPECTION TWO EMERGENCY EXIT FLOOR PROXIMITY STRIPS WERE FOUND MISSING. MX INSTALLED FLOOR PROXIMITY TERMINATING STRIPS. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · airframe 39,132 hrs · 22,781 cycles

SHV. DURING C-CK. CARGO DOOR LOWER BEAM CORRODED. REMOVED AND REPLACED CARGO DOOR LOWER BEAM IAW SRM 51-40-02. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 33,143 hrs · 18,690 cycles

LEFT WING RIB 7 CRACKED IN SEVERAL AREAS SURROUNDING THE REFUELING SHUTOFF VALVE AND DIFFUSER. CUT OUT THE CRACKED AREA. PERFORMED NDI OF CUTOUT SURROUND. FABRICATED FILLER & DOUBLER, ALODINED, APPLIED EPOXY PRIMER AND INSTALLED IAW EC5710-01226

Part: MOUNT — CRACKED (NR 1 ENGINE) · airframe 33,144 hrs · 18,690 cycles

DURING C-CHECK, FOUND THE LT LOWER NR 1 ENGINE MOUNT CRACKED AND WAS VERIFIED BY VISUAL AND EDDY CURRENT MEANS. MAINTENANCE R & R THE NR 1 ENGINE YOKE IAW EC 5450-01096. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: LIGHT — DISLODGED (CABIN) · airframe 33,099 hrs · 18,658 cycles

DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE AFT CEILING EMERGENCY EXIT LIGHT WAS COMING OUT OF ITS CASING AND WAS NOT FULLY LIT. MAINTENANCE SECURRED THE AFFECTED EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 30,931 hrs · 17,289 cycles

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGNS WOULD NOT ILLUMINATE. THE SYS WAS RESET, AND THE LIGHTS OPERATED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,830 hrs · 16,602 cycles

DURING 4A INSPECTION THE RT AFT FUSELAGE II SKIN WAS FOUND TO HAVE A SINGLE CRACK EMINATING FROM A RIVET AT FR 78 STR 5R. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 05/14/13.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,830 hrs · 16,602 cycles

DURING 4A INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE THREE CRACKS EMINATING FROM A SINGLE RIVET NEAR FR 78 STRINGERS 4L & 5L. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE AND REPAIR AUTHORIZATION 5330-02501, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 05/14/13.

Part: FLAPPER VALVE — LEAKING (ZONE 500) · airframe 29,482 hrs · 16,379 cycles

THE CREW REPORTED FUEL LEAKING FROM THE LT WING. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, R & R THE FLAPPER VALVES ON RIB 19, LEAK CHECKED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 28,816 hrs · 15,974 cycles

CREW REPORTED A LAVATORY SMOKE INDICATION ON EICAS DURING DESCENT. MESSAGE CLEARED AFTER QRH PROCEDURE. R & R LAVATORY SMOKE DETECTOR, OPS CHECKED SUCCESSFUL. APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 26,258 hrs · 14,275 cycles

DURING MX INSPECTION, THE NR 2 EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 25,736 hrs · 13,932 cycles

DURING ROUTINE MX THE RT AND LT FORWARD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 25,190 hrs · 13,522 cycles

DEN - FLIGHT 5862 THE CREW REPORTED LANDING GEAR AURAL WARNING IN FLIGHT AT 13,000 FEET WITH NO OTHER INDICATIONS. THE AIRCRAFT LANDED AT DEN WITHOUT INCIDENT WHERE MAINTENANCE OPERATIONALLY TESTED THE LANDING GEAR WARNING SYSTEM WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COMPUTER — DEFECTIVE (STALL WARNING) · airframe 24,882 hrs · 13,330 cycles

FLIGHT 2476 A/C N17108 FROM EWR AFTER TAKEOFF AND DURING CLIMB HAD SPS 1 INOP, AIR RETURNED TO EWR. MAINTENANCE REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW EMB-145XR AMM 27-36-02, OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,252 hrs · 12,884 cycles

RT EMERGENCY EXIT FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 3 INVERTER IAW EMB 145AMM 33-50-01. OPS CHECK GOOD.

Part: ANTI-ICE VALVE — INOPERATIVE (LT WING) · airframe 23,730 hrs · 12,530 cycles

FLIGHT 2199 - BTV - FLIGHT CREW REPORTED WING ANTI-ICE FAIL ON EICAS. CREW DIVERTED TO BTV AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED LT WING ANTI-ICE VALE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PANEL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 22,571 hrs · 11,894 cycles

CARGO DOOR LT SIDE PANEL HAS MULTIPLE CORRODED NUT PLATE HOLES. FOUND SIX DAMAGED HOLES, BLENDED MINOR CORROSION ON FOUR HOLES. TWO OF THE SIX HOLES WERE OUT OF LIMITS. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED DOUBLER. WORK PERFORMED IAW EMB 145 SRM 51-10-03 AND EC5230-01235.

Part: PROXIMITY SWITCH — OUT OF ADJUST (RT MLG) · airframe 22,571 hrs · 11,894 cycles

TYS - A/C WENT OUT ON A TEST FLIGHT AFTER COMPLETING A C-CHECK INSPECTION. THE CREW GOT A LDG AIR/GND FAIL MESSAGE ON THE EICAS AND RETURN BACK TO THE HANGAR WHERE MAINTENANCE FOUND RT MLG TRAILING ARM WOW SWITCH OUT OF LIMITS. RE-ADJUSTED THE SWITCH IAW EMB 145XR AMM 32-63-05-804-A AND PERFORMED A PROX SWITCH FUNCTIONAL CHECK IAW EMB 145 XR AMM 32-63-05-700-802-A. OPS CHECK GOOD AND WAS RELEASED TO TEST FLIGHT AGAIN.

Part: BUSHING — DAMAGED (HORIZ STAB) · airframe 22,571 hrs · 11,894 cycles

TYS - A/C IS IN C-CHECK NOW. INSPECTION FOUND THE HORIZONTAL STAB RT INBOARD HINGE STATIONARY BUSHING PITTED. MAINTENANCE REMOVED AND REPLACED THE BUSHING IAW EMB145XR AMM 20-10-08 AND EC5510-01229. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: CABLE — OUT OF ADJUST (CABIN DOOR) · airframe 22,552 hrs · 11,882 cycles

THE CREW REPORTED THE MAIN CABIN DOOR WAS VERY HARD TO OPEN. MAINTENANCE INSPECTED AND ADJUSTED THE MAIN CABIN DOOR CABLES. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,527 hrs · 11,869 cycles

IAH - DURING POST FLIGHT INSPECTION THE CREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 12A WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,499 hrs · 11,855 cycles

IAH - FLIGHT 2194, THE CREW REPORTED A BURNING SMELL ORIGINATING FROM THE COFFEE POT AREA WITH BOTH POTS TURNED ON. MAINTENANCE INSPECTED BOTH COFFEEMAKERS & WIRING WITH NO DEFECTS NOTED, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ADC — FAULTY (NR 2) · airframe 21,446 hrs · 11,283 cycles

MSP FLT 2816 THE CREW REPORTED, THE FIRST OFFICER'S AIRSPEED INDICATION IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 AIR DATA COMPUTER, OPERATIONAL CHECKS WERE GOOD.

Part: FIRE LOOP — FAILED (NR 1 ENGINE) · airframe 21,251 hrs · 11,179 cycles

FLIGHT 2601 - EWR - FLIGHT CREW REPORTED E1 FIRE DETECTION FAIL AT 35000 FT, ALL OTHER INDICATION NORMAL. EWR MX REMOVED AND REPLACED E1 FIRE LOOP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — FAULTY (CABIN) · airframe 20,273 hrs · 10,660 cycles

CLE FLT 2095 THE CREW REPORTED THE EMERGENCY LIGHT AT THE FLIGHT ATTENDANT STATION DID NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE FORWARD LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 19,529 hrs · 10,271 cycles

FLIGHT 2447 - EWR - DURING LANDING, FLIGHT CREW REPORTED AUTO PRESSURIZATION FAIL. EWR MX REMOVED AND REPLACED DIGITAL AUTO PRESSURIZATION CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 19,529 hrs · 10,271 cycles

FLIGHT 2447 - EWR - DURING LANDING, FLIGHT CREW REPORTED AUTO PRESSURIZATION FAIL. EWR MX REMOVED AND REPLACED DIGITAL AUTO PRESSURIZATION CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (E&E BAY) · airframe 17,902 hrs · 9,411 cycles

IAH - FLIGHT 3048, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON CLIMB. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONICS UNIT (LGEU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,888 hrs · 9,403 cycles

EMERGENCY LIGHTS AT ROW 12 SIDEWALL PANELS & OVERHEAD PANEL INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW EMB 145XR AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,816 hrs · 9,364 cycles

IAH - DURING MX INSPECTION THE RT LOWER EMERGENCY EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. MX R&R THE AFFECTED EMERGENCY EXIT SIGN, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,749 hrs · 9,326 cycles

SHV DURING C-CHECK. LT OMEGA BEAM CORROSION BTW. FR. 23-24. REPAIRED LT OMEGA BEAM BTW FR. 23-24 IAW EMB 145 SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,749 hrs · 9,326 cycles

SHV DURING C-CHECK. LT OMEGA BEAM HAS CORROSION AT FR. 29. REPAIRED LT OMEGA BEAM AT FR. 29 IAW EMB 145 SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — MISSING (RT ELEVATOR) · airframe 17,749 hrs · 9,326 cycles

SHV-DURING C-CHECK RT ELEVATOR TIP FAIRING AFT UPPER NUT PLATE MISSING. (DAMAGED RIVET HOLES) MX REPAIRED RT ELEVATOR TIP ATTACHMENT AT AFT O/B END UPPER AREA AT NUTPLATE HOLE IAW PRINCIPALS EC 5520-01167 ORIG. MX COMPLETED REPAIR OF RT ELEVATOR TIP FAIRING UPPER NUTPLATE HOLE IAW EC5520-01170. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 300) · airframe 17,749 hrs · 9,326 cycles

SHV-DURING C-CHECK LT HORIZONTAL STAB L?E UPPER SURFACE HAS MULTIPLE RIVETS WITH CORROSION. MX REMOVED CORROSION IAW EC5510-01199 ORIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — DAMAGED (ZONE 300) · airframe 17,749 hrs · 9,326 cycles

SHV-DURING C-CHECK RT HORIZONTAL STAB L/E AT LOWER I/B CORNER HAS 1 TOOLING MARK. MX BLENDED OUT TOOLING MARKS IAW SRM 51-10-03 PER EC5510-01199 ORIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 17,749 hrs · 9,326 cycles

SHV-DURING C-CHECK RT HORIZONTAL STAB L/E UPPER SURFACE HAS MULTIPLE RIVETS WITH CORROSION. (MARKED) MX REMOVED CORROSION IAW EC5510-01199 ORIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTAKE — CORRODED (RT ENGINE) · airframe 17,749 hrs · 9,326 cycles

RT ENGINE AIR INTAKE HAS VARIOUS MOUNTING BOLT HOLES THAT ARE CORRODED. REPAIRED RT ENGINE AIR INTAKE MOUNT HOLES IAW EC5420-01158. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)

IAH - FLIGHT 2259 - DURING CRUISE, THE CREW REPORTED THAT THE AIRCRAFT CABIN RATE OF CHANGE BECAME ERRATIC. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE DIGITAL PRESSURE CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,862 hrs · 8,319 cycles

DURING ROUTINE MAINTENANCE, MX FOUND RIGHT HAND LOWER EMERGENCY LIGHT AT ESCAPE HATCH INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT IAW EMB AMM 33-50-13 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,568 hrs · 8,165 cycles

IAH - FLIGHT 2832 DURING POST FLIGHT INSPECTION THE CREW REPORTED THE MID CABIN CEILING EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (SPOILER SYSTEM) · airframe 15,419 hrs · 8,090 cycles

EWR/CLT- FLT 3068 - UNCOMMANDED SPOILER INDICATION IN FLIGHT. CLT MX REPAIRED A BROKEN WIRE AT C/P P1167 PIN A. OPS CHECKS WERE GOOD IAW EMB 145 AMM 27-63-01. A/C WAS RELEASED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,100 hrs · 7,924 cycles

TYS - DURING ROUTINE MX THE FWD CEILING EMERGENCY LIGHT WAS FOUND INOP. MX REMOVED AND REPLACED THE LAMPS IAW 145XR AMM 33-50-06 AND OPS CHECKED GOOD. A/C WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (LT WING) · airframe 14,900 hrs · 7,834 cycles

IAH - FLIGHT 2392, THE CREW REPORTED A SPOILER FAIL WITH A SPOILER OPEN INDICATION WITH THE SPOILERS CLOSED. THE CREW PERFORMED AN EMERGENCY DESCENT, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE ON THE LEFT HAND INBOARD SPOILER PROXIMITY SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 14,626 hrs · 7,693 cycles

DURING ROUTINE MAINTENANCE, THE SMALL EMERGENCY EXIT SIGN ON THE RIGHT OVERWING EXIT WOULD NOT TEST. MAINTENANCE PERFORMED A ELECTRICAL RESET AND OPERATIONAL CHECKS WERE GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,722 hrs · 7,203 cycles

EMERGENCY LIGHT IN CEILING BY ROW 17A INOP. REPLACED LIGHT BULB IAW EMB 145 AMM 33-50-04, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,398 hrs · 7,030 cycles

IAH - FLIGHT 2713, DURING PREFLIGHT INSPECTION, THE GALLEY EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 12,089 hrs · 6,335 cycles

IAH - DURING PREFLIGHT INSPECTION, A CABIN EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (RT.AILERON) · airframe 10,875 hrs · 5,680 cycles

CREW REPORTED, TO KEEP AIRCRAFT LEVEL NEEDED CONSIDERABLE AILERON TO THE LEFT. MAINTENANCE FOUND THE RIGHT AILERON PCA ROD BRACKET TO BE CRACKED ON THE AILERON. REMOVED AND REPLACED RIGHT AILERON IAW EMB145MM NR 27-10-00, AILERON PRIMARY MECHANICAL CONTROL ADJUSTMENT CHECKS GOOD IAW EMB145 MM NR 27-11-00-700-801-A. AIRCRAFT TEST FLOWN SATISFACTORILY AND RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,784 hrs · 5,629 cycles

IAH - FLIGHT 2583, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 9,619 hrs · 5,040 cycles

PAX DOOR IS HARD TO OPEN. ADJUSTED BOTTOM ROLLERS AND LUBED DOOR SEAL IAW EMB145 GMM 52-18-00. OPS CHECK GOOD AND AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: CABLE — OUT OF ADJUST (PAX DOOR) · airframe 9,606 hrs · 5,033 cycles

CLE FLIGHT 2100, THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND ADJUSTED THE MAIN CABIN DOOR CABLES. OPERATIONAL CHECKS WERE GOOD.

Part: SEAL — SWOLLEN (PAX DOOR) · airframe 8,977 hrs · 4,704 cycles

CLE FLIGHT 2718 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND REPLACED THE MAIN CABIN DOOR PROFILE SEAL. OPERATIONAL CHECKS WERE GOOD.

Part: PRESSURE VALVE — FAILED (NR 1 ENGINE OIL) · airframe 7,298 hrs · 3,819 cycles

FLIGHT 2567 - EWR TO FPO - DURING CRUISE, ENGINE NR 1 OIL QUANTITY DROP FROM 8 QTS TO 5 QTS IN A LITTLE OVER ONE HOUR. CREW DIVERTED FLIGHT TO RIC. RIC MAINTENANCE REMOVED AND REPLACED OIL PRESS RELIEF VALVE AND SERVICE ENGINE NR 1. OPERATIONAL CHECK AND LEAK TEST WERE PERFORMED SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT.