N924EV

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,141 hrs · 32,042 cycles

LIGHT ON EXIT SIGN AFT INOP REMOVED & REPLACED BULB IAW AMM 33-51-14 & CMM 33-21-94

Part: DOOR FRAME — CRACKED (BS 310-349) · airframe 31,834 hrs · 30,666 cycles

PASSENGER DOOR AFT FRAME CRACKED. REMOVED AND REPLACED AFT PAX DOOR FRAME FS 349 PER CRJ 200 SRM 51-42-06 51-42-13 51-42-21 OPS CHECK GOOD PER CRJ 200 AMM 52-70-04-710-803 / 52-1-25-710-801 REF WIP STEPS 30 31- 34 FOR FURTHER OPS CHECKS AP-189

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 31,834 hrs · 30,666 cycles

LBL 27 O/B FLOOR LANDING HAS CORROSION SPOTS BETWEEN FS 605 THRU FS 621, IN THE CARGO BAY BELOW THE FLOOR REPAIRED LBL27 FLOOR BEAM FITTING AT STATION 605-621 IAW ENDEAVOR E.A. NO. CRJ253-08299 IR 1-29-19. AAR SM-107

Part: FRAME — CRACKED (BS 605) · airframe 31,834 hrs · 30,666 cycles

FRAME 605 IS CRACKED ON THE FWD SIDE JUST ABOVE AND BELOW STGR 9L, IN THE CARGO BAY. REPAIRED CRACKS ON FRAME 605 ABOVE AND BELOW STGR96 IAW BOMBARDIER REO #601R-53-61-5214.

Part: SEAT TRACK — CORRODED · airframe 31,834 hrs · 30,666 cycles

RH SEAT RAIL STICKS #3,#4,#5,#7 HAVE CORROSION. REMOVED/REPLACED SEAT TRACK STICK #3 IAW CRJ 200 AMM 53-01-11. SEAT TRACK STICK #5 IS FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-21-49, SEAT TRACK STICK #4 AND #7 HAVE NO VISUAL DAMAGE FOUND IAW CRJ 200 NDT 51-20-09 AAR SM 124.

Part: SUPPORT BRACKET — CRACKED (OVERWING) · airframe 31,834 hrs · 30,666 cycles

UPON OK TO CLOSE FOUND OVER WING SUPPORT BRACKET BETWEEN PANELS 162DL AND 162EL CRACKED. REMOVED/REPLACED BRACKET BETWEEN PNLS 162DL AND 162EL IAW CRJ 200 SRM 51-42-06 AAR SM 84

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 31,834 hrs · 30,666 cycles

BS 409 RBL 9 FLOOR SUPPORT HAS SURFACE CORROSION. REPLACED CORRODED FLOOR BEAM CAP FROM FS409-FS409-128 I.A.W. SRM 51-42-13 AND 51-42-21.

Part: ATTACH BRACKET — CRACKED (WINDOW FRAME) · airframe 31,834 hrs · 30,666 cycles

RIGHT LOWER CENTER WINDSHIELD POST ATTACH BRACKET IS CRACKED. REMOVED CRACKED FITTING AND REPLACED WITH NEW FITTING IAW CRJ 200 SRM 51-42-21 AND INSTALLED IAW CRJ 200 SRM 51-42-20 OPS TEST OF EFD #4 ACCOMPLISHED ON W/O 1016674 2000 0061 SN6882621 AAR SM 58

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 31,834 hrs · 30,666 cycles

RH MLG W/W DRAG ANGLE CRACKED. REMOVED AND REPALCED R/H MLG W/W DRAG ANGLE. IAW CRJ-200 SRM 51-42-21. AAR SM 33

Part: FITTING — GOUGED (HORIZONTAL STAB) · airframe 31,834 hrs · 30,666 cycles

HORIZONTAL STABILIZER ANTI-ROTATION DEVICE GOUGED. DRILLED UP NEW ANTI-ROTATION DEVICE FITTING IAW CRJ-200 SRM 51-41-02 ( PART REMOVED AND INSTALLED ON ROUTINE W/O 1016674 C/N 3000-0016 S/N 6882672. AAR SM 39

Part: DRAG ANGLE — CRACKED (LT MLG WW) · airframe 31,834 hrs · 30,666 cycles

LH MLG W/W DRAG ANGLE CRACKED. REMOVED AND REPLACED L/H MLG W/W DRAG ANGLE. IAW CRJ-200 SRM 51-42-21. AAR SM 33

Part: PLATE — CRACKED (CARGO DOOR) · airframe 31,834 hrs · 30,666 cycles

CARGO DOOR OPENING LOWER SILL APPEARS TO BE CRACKED AT FS 589. REMOVED DAMAGE REPLACED RIVIT, NDT FOR DAMAGE REMOVAL, ALL DAMAGE REMOVED. TREATED PRIMED TOPCOATED AREA IAW BOMBI REO 601R-53-61-433. AAR SM 107

Part: WEB — CRACKED (PAX DOOR) · airframe 31,834 hrs · 30,666 cycles

PASSENGER DOOR AFT RISER WEB CRACKED AT LWR STEP ATTACH FLANGE JOGGLED. REPAIRED WEB IAW REO # 601R-52-11-702 REV E. AAR SM 139

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 31,834 hrs · 30,666 cycles

PASSENGER DOOR INT. AFT INTERCOSTAL AT WL143.00 CRACKED IN RADIUS. REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT WL143 I.A.W. CRJ-200 SRM 51-42-21 AAR SM 33

Part: RIB — CRACKED (EXHAUST FAIRING) · airframe 31,834 hrs · 30,666 cycles

LEFT ENGINE EXHAUST FAIRING INNER RIB #1 IS CRACKED. REMOVED AND REPLACED LEFT ENGINE EXHAUST FAIRING INNER RIB (STIFFINER) I.A.W. BOMBARDIER CMM CMM 200 20-42-06 AAR SM 4

Part: BRACKET — CRACKED (HYD TRANSDUCER) · airframe 31,834 hrs · 30,666 cycles

RH MLG BAY, BRAKE HYD PRESSURE TRANSDUCER MOUNT BRACKET CRACKED. REPLACED HYD. BRACKET WITH NEW PN 601R-75-262-157 I.A.W. CRJ-200 SRM 51-42-20 AAR SM 33

Part: RIB — BENT (ACCESSORY DOOR) · airframe 31,834 hrs · 30,666 cycles

AFT ACCY. DOOR CENTER RIB BENT. REMOVED BENT CENTER RIB AND REPLACED WITH NEW CENTER RIB I.A.W. CRJ-200 51-42-06 AAR SM 58

Part: SEAT TRACK — CORRODED · airframe 31,834 hrs · 30,666 cycles

RH SEAT RAIL STICK #6 HAS CORROSION. REMOVED/REPLACED WITH NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11 AAR SM 58

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,834 hrs · 30,666 cycles

SEAT TRACK ON TOP OF RBL 27 HS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED WITH NEW SEAT TRACK I.A.W. CRJ-200 AMM 53-00-49. NEW SEAT TRACK FABBED ON W/O 1016675 1000 0130 S/N 688-2088 AAR SM 58

Part: CARGO TRACK — CORRODED (BS 559) · airframe 31,834 hrs · 30,666 cycles

SEAT TRACK ON TOP OF RBL 9 HS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED WITH NEW SEAT TRACK I.A.W. CRJ-200 AMM 53-00-49. NEW SEAT TRACK FABBED ON W/O 1016675 1000 0131 S/N 6882089 AAR SM 58

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 31,834 hrs · 30,666 cycles

SEAT TRACK ON TOP OF LBL 9 HS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REMOVED/REPLACED WITH NEW SEAT TRACK IAW CRJ 200 AMM 53-00-49 NEW SEAT TRACK FABBED ON W/O 1016675 1000 0129 SN6882087 AAR SM 58

Part: SEAT TRACK — CORRODED (BS 405-409) · airframe 31,834 hrs · 30,666 cycles

L/H SEAT TRACK STICK #2 HAS CORROSION. REMOVED AND REPLACED WITH NOW SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 31,834 hrs · 30,666 cycles

R/H SEAT TRACK STICK #4 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK I.A.W. AMM 53-01-11.

Part: SEAL — BROKEN (PBE) · airframe 31,254 hrs · 30,068 cycles

1 BROKEN PBE SEAL ON COCKPIT PBE. REPLACED PBE SEAL, NO MAINTENANCE REQUIRED AT THIS TIME. A/C OK FOR SVC.

Part: FITTING — CRACKED (OXYGEN MASK) · airframe 30,906 hrs · 29,666 cycles

DURING TROUBLESHOOTING OF O2 SERVICING MOTR REQUEST NOTED AIR FITTING ON BOTTOM OF CAPTAINS OF MASK BOX CRACKED AND LEAKING. REMOVED AND REPLACED CAPTAINS O2 MASK BOX P/N ON/OFF MXP411-3 S/N OFF SE10546 S/N ON SE07542 IAW AMM 35-11-15. NO LEAKS NOTED.

Part: OXYGEN MASK — UNWANTED DEPLOY (LAVATORY) · airframe 30,693 hrs · 29,431 cycles

LAVATORY OXYGEN MASKS DEPLOYED. RESTOWED SERVICEABLE LAVATORY OXYGEN MASK IAW AMM 35-21-09, NO DEFECTS NOTED.

Part: POST — CRACKED (BS 409) · airframe 30,480 hrs · 29,169 cycles

INBD FLANGE OF THE VERTICAL POST AT RBL 27, BS 409+128 IS CRACKED AT BOTTOM EDGE, EXTRUDING HALFWAY BETWEEN THE FIRST AND SECOND RIVET. REPAIRED THE VERTICAL POST IAW REO 601R-53-41-056. MAJOR REPAIR.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 30,277 hrs · 28,952 cycles

FO'S O2 MASK MIC INOP. REMOVED AND REPLACED FO O2 MASK P/N ON/OFF MF10-08-01 S/N OFF SE20024I S/N ON 105551T. IAW AMM 35-11-12. RECONNECTED CANNON PLUG. OPS CHECK GOOD.

Part: OXYGEN BOX — LEAKING (COCKPIT) · airframe 30,241 hrs · 28,905 cycles

FOUND THE FIRST OFFICER`S OXYGEN MASK STORAGE BOX LEAKING DURING A LEAK CHECK. R & R THE OXYGEN MASK, STORAGE BOX, AND FLEX HOSE IAW AMM 35-11-12, AND AMM 35-11-15. LEAK CHECKED GOOD.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 30,134 hrs · 28,795 cycles

CAPTAINS 02 MASK LEAKING FROM REGULATOR AT HEADSTRAP CONNECTIONS. REMOVED AND REPLACED CAPTAINS 02 MASK W/SERV ASSY IAW AMM 35-11-12-400-801. OPS AND LEAK CHECKS GOOD. P/N MF10-08-01, S/N OFF 97974, S/N ON 87575I.

Part: HYDRAULIC SYSTEM — LEAKING (NR 1) · airframe 29,924 hrs · 28,563 cycles

NR 1 HYDRAULIC LEAK. REPLACED THE EDP, PRESSURE MANIFOLD AND PRESSURE CHECK VALVE. ALL PARTS ACCOUNTED FOR IN WORK PACKAGE. YELLOW TAGS RECEIVED FOR CHECK VALVE REMOTE RECEIVING INSPECTION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,338 hrs · 27,943 cycles

FWD RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW CMM 33-52-06. OPS CHECKED GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,981 hrs · 27,556 cycles

LEFT CENTER OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 3 FUSE IN THE NR 3 BATTERY CHARGER IAW CMM 33-21-70. OPS TESTED GOOD IAW AMM 33-51-00-710-801.

Part: OXYGEN MASK — PUNCTURED (ROW 7) · airframe 28,981 hrs · 27,556 cycles

ONE OXYGEN MASK AT SEAT ROW NR 7 IS PUNCTURED. REMOVED AND REINSTALLED PSU AT ROW 7 IAW AMM 25-28-01. REMOVED AND INSTALLED ONE OXYGEN MASK AT RT SEAT ROW 7 IAW AMM 32-21-09-420-801. AAR RE-37.

Part: LATCH — INOPERATIVE (O2 MASK DOOR) · airframe 28,981 hrs · 27,556 cycles

ROW 1 RT SIDE PASSENGER OXYGEN MASK DOOR FAILED TO OPEN. REMOVED AND REPLACED THE OXYGEN MASK DOOR LATCH IAW AMM 35-21-05, OPS TESTED GOOD IAW AMM 35-20-00-710-803.

Part: SHROUD — CRACKED (APU BAY) · airframe 28,981 hrs · 27,556 cycles

APU SHROUD IS CRACKED ON AFT UPPER SIDE PANEL LANDING. REPAIRED APU SHROUD IAW REO 601R-49-11-071.

Part: FITTING — CORRODED (BS 621) · airframe 28,981 hrs · 27,556 cycles

BS 621 BULKHEAD FITTING AT LBL 9 HAS CORROSION AROUND FASTENERS. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-21, 51-42-22, AND REO 601-53-61-3778.

Part: RETAINER — CORRODED (E/E DOOR SEAL) · airframe 28,981 hrs · 27,556 cycles

DURING REMOVAL OF MAIN AVIONICS BAY DOOR SEAL, FOUND THE SEAL RETAINERS CORRODED. REMOVED AND REPLACED SEAL RETAINERS IAW SRM 51-42-06, PARA 6.

Part: FITTING — CORRODED (BS 621 BULKHEAD) · airframe 28,981 hrs · 27,556 cycles

BS 621 BULKHEAD LBL 27 FITTING HAS AREAS OF CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-21, 51-42-22, AND REO 601-53-61-3778.

Part: FITTING — CORRODED (BS 621) · airframe 28,981 hrs · 27,556 cycles

FLOORBEAM FITTING BS 621, LBL 27 IS CORRODED. REPAIRED THE FITTING IAW 253-05423, REV I/R.

Part: FLOOR SUPPORT — CORRODED (BS 574-610) · airframe 28,981 hrs · 27,556 cycles

BS 574 - 621, LBL 27 BOTH INBD AND OTBD FLOOR SUPPORT HAD SEVERAL AREAS OF CORROSION AROUND NUTPLATES. REMOVED & REPLACED THE FLOOR SUPPORT IAW REO 601R-53-61-3778, REV. A.

Part: RISER — CRACKED (PAX DOOR) · airframe 28,981 hrs · 27,556 cycles

PAX DOOR AFT RISER IS CRACKED BY LOWER STEP. REPAIRED IAW REO 601R-52-11-702 REV E 2016-08-14.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 28,981 hrs · 27,556 cycles

LOWER PAX BOTTOM STEP SWIVEL LATCH SUPPORT ANGLES 601R31902-147 AND 148 ARE CRACKED IN THE RADIUS. R&R 2 EA CRACKED SUPPORT ANGLES IAW AMM 52-11-25 PARA 7 A THRU J.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

LT SIDEWALL SEAT TRACK STICK 3 HAS CORROSION, IN CABIN FS409+18 - FS409+113. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11 TASK 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

LT SIDEWALL SEAT TRACK STICK 2 HAS CORROSION, IN CABIN. REMOVED AND REPLACED LT SIDEWALL SEAT TRACK STICK 2 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

LT SIDEWALL SEAT TRACK STICK 1 HAS CORROSION, IN CABIN. REMOVED AND REPLACED LT SIDEWALL SEAT TRACK STICK 1 IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 621) · airframe 28,981 hrs · 27,556 cycles

ANGLE CRACKED AT THE BS 621 BULKHEAD JUST BELOW FLOOR LEVEL AND JUST AFT OF THE AFT CARGO TIE DOWN. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21, & 51-42-10.

Part: FITTING — BROKEN (THRUST REVERSER) · airframe 28,981 hrs · 27,556 cycles

RIGHT THRUST REVERSER TRANS COWL ANTI VIBRATION FITTING IS BROKEN OFF. REMOVED & REPLACED THE FITTING IAW CMM 20-42-10, PG 6008, & 20-42-28, PG 6003.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

A/C RECEPTACLE MOUNT BRACKET IS CRACKED. REMOVED AND REPLACED MOUNT BRACKET IAW SRM 51-42-06 AND 51-42-21.

Part: FITTING — BROKEN (THRUST REVERSER) · airframe 28,981 hrs · 27,556 cycles

LEFT TRANS COWL ANTI VIBBRATION FITTING ON TORQUE BOX AT THE 1 O`CLOCK POSITION WAS BROKEN. REMOVED & REPLACED THE FITTING IAW CMM 20-42-10, PG 6008, & 20-42-28, PG 6003.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

LT AISLE SEAT TRACK STICK 2 HAS CORROSION, IN CABIN. REMOVED AND REPLACED LT AISLE SEAT TRACK 2 IAW AMM 53-01-11-020-002 PARA 3 B, 53-01-11-420-001 PARA 2B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

RT AISLE SEAT TRACK STICK 1 HAS CORROSION AND IS CHAFED, IN CABIN. REMOVED AND REPLACED RBL 9 SEAT RAIL 1 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

RT AISLE SEAT TRACK STICK 6 HAS CORROSION, IN CABIN. REMOVED AND REPLACED RT AISLE SEAT RAIL 6 IAW AMM 53-01-11.

Part: MOUNT BRACKET — CRACKED (RT MLG WW) · airframe 28,981 hrs · 27,556 cycles

BRAKE HYD LINE MOUNT BRACKET IN RT MLG WHEEL WELL PRESS FLOOR CRACKED. REMOVED AND REPLACED BRAKE HYD LINE MOUNT BRACKET IN RT MLG WHEEL WELL IAW SRM 51-42-06.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 28,981 hrs · 27,556 cycles

PAX DOOR AFT RISER DRAG ANGLE IS CRACKED BY ASSIST MOTOR PULLEY. REMOVED AND REPLACED ANGLE, AFT RISER DRAG ANGLE, BY MOTOR ASSIST PULLEY IAW REO# 601R-52-11-513.

Part: RISER — CORRODED (PAX DOOR) · airframe 28,981 hrs · 27,556 cycles

PAX DOOR FWD RISER HAS CORROSION BY UPPER STEP. REMOVED CORROSION. ORIG MATL IS .040, REM IS .029 LOSS IS .011 OUT OF LIMITS. REPAIRED IAW REO 601R-52-11-302 SRM 51-21-06, 52-00-00.

Part: RISER — CRACKED (PAX DOOR) · airframe 28,981 hrs · 27,556 cycles

PAX DOOR FWD RISER IS CRACKED AT THIRD STEP. REPAIRED RISER IAW REO 601R-52-11-702 REV E 2016-08-14.

Part: ANGLE — CORRODED (LT MLG WW) · airframe 28,981 hrs · 27,556 cycles

LT MLG WHEEL WELL AFT BULKHEAD OTBD SIDE EDGE MEMBER IS HEAVILY CORRODED. REMOVED & REPLACED ANGLE IAW SRM 51-42-06, PG 5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

LBL 9 AT STATION 621 SEAT TRACK SECTION HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

LBL9 SEAT TRACK AT STATION 559+80 TO 559+106 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

SMALL SECTION OF SEAT TRACK ON RBL9 STATION 559+112 TO 574 HAS CORROSION AROUND FASTENERS. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

RT SIDEWALL SEAT TRACK STICK 6 HAS CORROSION, IN CABIN. REMOVED AND REPLACED RT SIDEWALL SEAT TRACK STICK 6 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

LT SIDEWALL SEAT TRACK STICK 6 HAS CORROSION, IN CABIN. REMOVED AND REPLACED LT SIDEWALL SEAT TRACK STICK 6 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

LT SIDEWALL SEAT TRACK STICK 7 HAS CORROSION, IN CABIN. REMOVED AND REPLACED LT SIDEWALL SEAT TRACK STICK 7 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

LT AISLE SEAT TRACK STICK 4 HAS CORROSION, IN CABIN. FS559+4 - FS559+86 LT AISLE SEAT TRACK STICK 4 REMOVED AND REPLACED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

RT SIDEWALL SEAT TRACK STICK 7 HAS CORROSION, IN CABIN. FS 535.02 - FS 559+79. REMOVED AND REPLACED RT SIDEWALL SEAT TRACK STICK 7 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

RT SIDEWALL SEAT TRACK STICK 2 HAS CORROSION, IN CABIN FS364 - FS409. REMOVED AND REPLACED SEAT TRACK SIDEWALL STICK 2 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

LT SIDEWALL SEAT TRACK STICK 5 HAS CORROSION, IN CABIN FS 444.02 - FS 495.98. REMOVED AND REPLACED LT SIDEWALL SEAT TRACK STICK 5 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

RT SIDEWALL SEAT TRACK STICK 5 HAS CORROSION AND IS CHAFED, IN CABIN. FS 444.02 - FS 495.98. REMOVED AND REPLACED RT SIDEWALL SEAT TRUCK STICK 5 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

RT AISLE SEAT TRACK STICK 5 HAS CORROSION AND IS CHAFED, IN CABIN. REMOVED AND REPLACED THE RT AISLE SEAT TRACK STICK 5 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

LT SIDEWALL SEAT TRACK STICK 4 HAS CORROSION, IN CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11 TASK 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,981 hrs · 27,556 cycles

RT SIDEWALL SEAT TRACK STICK 4 HAS CORROSION AND IS CHAFED, IN CABIN. FS 409+111.02 - FS 444.02. R&R RT SIDEWALL SEAT TRACK NR 4 IAW AMM 53-01-11.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 28,091 hrs · 26,557 cycles

EMERGENCY EXIT OVER SERVICE DOOR BROKEN OFF DOOR. REMOVED & REPLACED SERVICE DOOR OVERHEAD EMERGENCY EXIT SIGN IAW AMM 33-51-13 OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 27,767 hrs · 26,199 cycles

CAPTAIN FLASHLIGHT INOPERATIVE. REPLACED CAPTAIN FLASHLIGHT BATTERIES IAW AMM 25-61-00. NO FURTHER DEFECTS NOTED.

Part: WIRE — BROKEN (STAB TRIM) · airframe 26,472 hrs · 24,774 cycles

AFTER T/O THE STABILIZER TRIM WOULD NOT WORK AT ALL. TRIM BEGAN TO RUNAWAY NOSE UP CAPTAIN & F/O FOLLOWED STABILIZER TRIM RUNAWAY PROCEDURES AND PRESSED THE STAB TRIM DISCONNECT SWITCHES AFTER PULLING CB'S 2F5 4A1. THE TRIM ACTUALLY GOT WORSE REQUIRED MORE DOWNWARD PRESSURE TO HOLD LEVEL FLIGHT. ACFT RETURNED TO CAE AFTER T/O - EMERGENCY ACTIONS, UPON FURTHER INSPECTION FOUND LT STABILIZER PITCH TRIM SWITCH WIRE BROKEN AND TOUCHING ANOTHER SWITCH WIRE. R & R LT STABILIZER PITCH TRIM SWITCH IAW AMM 27-41-05, OPS CHECK GOOD.

Part: CONNECTOR — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 25,515 hrs · 23,762 cycles

FLOODLIGHT AND EXIT SIGN ON WARDROBE, EXIT SIGN ON PANEL 232BZ AND EXIT SIGN ON CEILING PANEL 263HLC NEEDS TO BE TROUBLESHOT. FOUND THE EMERGENCY LIGHTS MALFUNCTION TO BE CAUSED BY THE CONNECTORS OF THE PASSENGER DOOR FLOOR LEVEL FLOODLIGHT CONNECTORS INADVERTANTLY GETTING SWAPPED WITH THE PASENGER DOOR EMERGENCY FLOODLIGHT CONNECTORS. CORRECTLY INSTALLED THE CONNECTORS OF THE EXIT SIGN AND FLOODLIGHT AND THE SYS OPS CHECKED GOOD IAW AMM 33-51-10-400-801, AMM 33-51-19-400-801 AND AMM 33-51-00-710-801.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 25,515 hrs · 23,762 cycles

FS 621, 5 EA ISOLATORS CRACKED/BROKEN. REMOVED DAMAGED 5 EA ISOLATORS AND INSTALLED NEW IAW SRM 51-42-06.

Part: BRACKET — BROKEN (LWS 66.2) · airframe 25,515 hrs · 23,762 cycles

FOUND BRACKET ASSY AT WS 66.20 UPPER ASSY BROKE ON LT WING L/E. REPLACED BRACKET ASSY AT WS 66.20, UPPER, IAW AMM 30-11-41-400-801, SUBTASK 30-11-41-420-803, C3, A-E.

Part: SKIN — CRACKED (RT WING) · airframe 25,515 hrs · 23,762 cycles

RT LOWER WING PLANK ACCESS HOLE FOR PANEL 650CB HAS AN INDICATION ON LANDING SURFACE 65 PERCENT FULL SCREEN HEIGHT. AREA MARKED ON ACFT. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV L.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 25,515 hrs · 23,762 cycles

RJ2-53-4, REV 2, PASSENGER DOOR LOWER SILL ANGLE REPLACEMENT. R & R LOWER SILL ANGLE, PN: 601R31527-221 IAW SRM 51-42-21, 51-42-06 AND 51-42-11.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 25,515 hrs · 23,762 cycles

LT PRESSURE FLOOR SILL ANGLE HAS FILIFORM CORROSION BETWEEN FS 409+128 AND FS 559, LBL 36 LBL 47 AND FLOOR SILL HAS FILIFORM CORROSION AT 1 FASTENER HOLE FS 468, LBL 43. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C DATED 11/06/2012 AS WRITTEN. COMPLIED WITH DEVIATION TO GREO 601R-53-41-666 REV C IAW REO 601R-53-41-1883 REV DATED 03/02/2015. REO 601R-53-41-1883 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: LONGERON CLIP — CRACKED (BS 499) · airframe 25,497 hrs · 23,743 cycles

LEFT LONGERON T CLEAT, PN 601R38605-3 CRACKED AT FS 499.00, LBL 47. REMOVED BROKEN CLEAT AND REPLACED WITH NEW PART IAW SRM 51-40-11 AND 51-42-21, PN: 601R38605-3, P/O:W34118.

Part: SKIN — CRACKED (RT WING) · airframe 25,515 hrs · 23,762 cycles

FOUND RT LOWER WING PLANK DRAIN HOLE WS 65.75 HAS INDICATION NOTED AT FWD EDGE OF HOLE APPROXIMATELY .100 IN LENGTH 80 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH REO 601R-57-21-2301. COLD WORKED AND FINAL REAMED FASTENER HOLES IAW SB 601R-57-044 IAW REO 601R-57-21-2301. PERFORMED SHOT/ROTO PEEN TO THE RT LOWER WING PLANK DRAIN HOLE 2.64" DIAMETER BORE AND LOWER SKIN REWORKED SURFACES IAW REO 601R-57-21-2301, REV DATED 03-07-15.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 25,515 hrs · 23,762 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT RBL 18.00, WL 111 APPROXIMATELY .500" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. DEVIATION RECEIVED AND COMPLIED WITH IN ITS ENTIRETY IAW REO 601R-53-61-5448 REV DATED 2015-02-25. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, REV D DATED 10/31/2011 AS WRITTEN. REO 601R-53-61-5448 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: FLOOR SUPPORT — CRACKED (BS 460) · airframe 25,497 hrs · 23,743 cycles

FS 460 FLOOR SUPPORT FITTING, PN 600-31068-19, CRACKED ON OTBD SIDE OF RBL 9.0. REMOVED FS 460 FLOOR SUPPORT AT RBL 9.0 IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED FS 460 FLOOR SUPPORT AT RBL 9.0 IAW SRM 51-42-06, 51-42-21 AND 51-40-11.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 25,497 hrs · 23,743 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 18.00, WL 111 APPROXIMATELY .750" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. FABRICATED REPAIR PARTS DOUBLER, TRIPLER, WEB FILLER, 2 EA SHIMS AND 2 EA SPLICE FOR FS 621, LBL 18.00. WORK PERFORMED IAW REO 601R-53-61-1285, REV D. INSTALLATION OF REINFORCING ANGLE AND SHIMS ACCOMPLISHED IAW REO 601R-53-61-5451. INSTALLED DOUBLER, TRIPLER, SHIMS, WEB FILLER AND SPLICES IAW REO 601R-53-61-1285, REV D DATED 2011/10/31. COMPLIED WITH REO:601R-53-61-5448 IN IT'S ENTIRETY. REO:601R-53-61-5448 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: SKIN — DAMAGED (RT WING) · airframe 25,515 hrs · 23,762 cycles

RIGHT WING LOWER WING PLANK HAS 1 O/S FASTENER HOLE ON STEEL STRAP, AFT HOLE, HOLE DIA IS .341". COMPLIED WITH REO 601R-57-21-2300 P1. RECEIVED PERMANENT REPAIR REO 601R-57-21-2300, REV DATED 2015-02-25. REF PRELIMINARY P1 FOR WORK PERFORMED. NO STEP CHANGES FROM PRELIMARY P1 TO PERMANENT. ALL STEPS OF PERMANENT REO ARE COMPLETE.

Part: FLOOR SUPPORT — CORRODED (BS 509-559) · airframe 25,515 hrs · 23,762 cycles

RIGHT PRESSURE FLOOR SILL HAS FILIFORM CORROSION AROUND 6 FASTENER HOLES BETWEEN FS 509+128 TO FS 559 RBL 43. BLENDED CORROSION IAW TASK REO:601R-53-41-666 IAW NDTM PT 1 51-20-06. C/W EC/TC REO:601R-53-41-666 AND REO:601R-53-41-666, REV C DATED 11/06/2012 AS WRITTEN.

Part: ANGLE — CRACKED (BS 280) · airframe 25,497 hrs · 23,743 cycles

FWD J-ANGLE ON FS 280, PN 600-34017-351 IS CRACKED. REMOVED FWD "J" ANGLE IAW SRM 51-42-06. INSTALLED NEW "J" ANGLE IAW SRM 51-42-06. LOCATED AND DRILLED NEW FWD "J" ANGLE IAW SRM 51-40-11.

Part: STIFFENER — CRACKED (BS 409) · airframe 25,497 hrs · 23,743 cycles

FS 409+128, RBL 18 OTBD VERT POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROX .250" LONG X 60 PERCENT FSH. FAILED NDT INSP. REMOVED OTBD VERTICAL POST AT FS 409+128 RBL 18 IAW SRM 51-42-06. INSTALLED RBL 18 INBD AND OTBD VERTICAL POSTS TOGETHER IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE VERT POST ASSY AT FS 409+128, RBL 18 IAW SRM CH 51-42-06 AND REO: 601R-53-41-889. COMPLIED WITH EC/TC REO: 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO:601R-53-41-889, REV A.

Part: STIFFENER — CRACKED (BS 409) · airframe 25,497 hrs · 23,743 cycles

FS 409+128, RBL 18 INBD VERT POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69, APPROX .250" LONG X 60% FSH. FAILED NDT INSP. REMOVED 409+128 RBL 18 VERT POST IAW SRM 51-42-06. INSTALLED RBL 18 INBD AND OTBD VERTICAL POSTS TOGETHER IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE VERT POST ASSY AT FS 409+128, RBL 18 IAW SRM CH 51-42-06 AND REO: 601R-53-41-889. COMPLIED WITH EC/TC REO: 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO:601R-53-41-889, REV A.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,497 hrs · 23,743 cycles

FS 280 BEAM IS CRACKED BETWEEN 2 RIVETS AT UPPER FLANGE JUST OTBD OF LBL 9. REPAIRED FS 280 BEAM IAW REO:601R-53-11-138 AND EC/TC REO:601R-53-11-138.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 25,497 hrs · 23,743 cycles

CLIP ATTACHING TO INTERCOSTAL AT FS 484 AT LBL 27 IS CRACKED. LOCATED AND DRILLED -17 CLIP. BEGAN INSTALL IAW SRM 51-42-21. COMPLETED INSTALL OF -17 CLIP IAW SRM 51-42-21.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 25,497 hrs · 23,743 cycles

CLIP ATTACHING TO INTERCOSTAL AT FS 484 AT RBL 27 IS CRACKED. LOCATED AND DRILLED -9 CLIP. BEGAN INSTALL IAW SRM 51-42-21. COMPLETED INSTALL OF -9 CLIP IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 25,497 hrs · 23,743 cycles

RIGHT AISLE SEAT TRACK FROM FS 409 TO FS 409+112 IS CORRODED. REMOVED DAMAGED SEAT TRACK AT FS 409 TO FS 409+112 AT RBL 9. DRILLED AND INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-000-802, 53-01-11-400-802 AND SRM 51-40-11.

Part: SKIN — DAMAGED (TAILCONE) · airframe 25,515 hrs · 23,762 cycles

LIGHTING DAMAGE TO TAIL CONE. INTERM REPAIR CW IAW EA 12-2014-251. PERMANENT REPAIR REQUIRED. REPAIRED TAIL CONE IAW SUPPLEMENT AMM 53-84-00.

Part: ANGLE — MISSING (ACCESS DOOR) · airframe 25,515 hrs · 23,762 cycles

RAMP REPORTED DAMAGE TO GROUND AIR ACCESS DOOR. MISSING FWD CLIP AND FASTNERS. EA 12-2014-218 CW GOOD FOR 1560 FLT HRS. PERMANENT REPAIR REQUIRED. INSTALLED NEW SERVICEABLE CLIP IAW SRM 51-42-06.

Part: STATIC WICK — LOOSE (HORIZONTAL STAB) · airframe 25,515 hrs · 23,762 cycles

HORIZONTAL STAB T/E LT OTBD STATIC WICK BASE LOOSE. EO 600-57-0321 TEMP REPAIR WAS CW. PERMANMENT REPAIR REQUIRED. REPAIRED LT HORIZONTAL OTBD STATIC BASE IAW AMM SUPPLEMENT 23-61-01-1 AND DOCUMENT 701569, SECTION 5.4. PAINTED REPAIRED AREA ON LT OTBD STATIC WICK BASE IAW SRM 51-25-01.

Part: DOOR — STUCK (MAIN PAX) · airframe 21,258 hrs · 19,512 cycles

IT WAS VERY HARD TO OPEN THE MAIN DOOR , ONCED OPENED THE DOOR STAY UP AND WOULD NOT GO DOWN. HAD TO FORCE IT DOWN FOR A WHILE TO MAKE IT STAY OPEN. R & R PAX DOOR CLOSE SWITCH S11MB IAW SPM 20-24-00. OPS CHECKED GOOD IAW AMM 52-11-08. OK FOR SERVICE.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 21,252 hrs · 19,506 cycles

PAX DOOR FWD UPPER CORNER OTBD ANGLE IS CORRODED BEYOND LIMITS. REMOVED & INSTALLED NEW ANGLE IAW SRM 51-42-06.

Part: POST — CRACKED (BS 409) · airframe 21,252 hrs · 19,506 cycles

FOUND FS 409+128 VERTICAL POST BL 0 HAVE CRACK INDICATIONS NOTED APPROX .2 INCHES IN LENGTH 50 PERCENT AND 60 PERCENT FSH AT AFT FLANGE RADIOUS WL 69.0 BOTH FAILED NDT INSPECTION. REMOVED VERTICAL POSTS IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW POST IAW SRM 51-40-11. COMPLIED WITH REO 601R-53-41-889.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 21,252 hrs · 19,506 cycles

FOUND CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED APPROX .3" IN LENGTH. REMOVED DAMAGED ANGLE AND INSTALLED IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 21,252 hrs · 19,506 cycles

LIGHT CORROSION ON CENTER AISLE, RT SIDE SEAT TRACK AT FS 364-409+32. INSTALLED NEW AND SERVICEABLE SEAT TRACK AT RBL 9 FROM FS 364 TO 394 IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 21,252 hrs · 19,506 cycles

LIGHT CORROSION ON CENTER AISLE LT SIDE SEAT TRACK AT FS 364.00. INSTALLED NEW SEAT TRACK FS 364 TO 394 IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 21,246 hrs · 19,499 cycles

FS 621 FLOOR SUPPORT ANGLE CRACKED. REPAIRED DAMAGED PORTIONS OF ANGLE, COMPLETED IAW REO 601R-53-61-117.

Part: ANCHOR FITTING — CORRODED (BS 574-605) · airframe 21,252 hrs · 19,506 cycles

CARGO BAY FLOOR ANCHOR PLATE CORRODED BETWEEN FS 574-FS 605, LBL 9. INSTALLED NEW ANCHOR PLATE IAW SRM 51-41-02 AND 51-41-04.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 21,246 hrs · 19,499 cycles

CARGO TRACK CORRODED BETWEEN 559+80 - 559+96. INSTALLED CARGO TRACK IAW SRM 51-41-02 AND 51-41-04.

Part: SEAT TRACK — CORRODED (BS 559-567) · airframe 21,246 hrs · 19,499 cycles

CARGO TRACK CORRODED BETWEEN FS 559+96 -567, RBL 9. INSTALLED NEW CARGO TRACK IAW SRM 51-41-02 AND 51-41-04.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 21,246 hrs · 19,499 cycles

CARGO TRACK CORRODED FS 559+80 - 559+96, LBL 9. INSTALLED NEW CARGO TRACK IAW SRM 51-41-02 AND 51-41-04.

Part: SEAT TRACK — CORRODED (BS 621) · airframe 21,252 hrs · 19,506 cycles

CARGO TRACK CORRODED AT FS 621, LBL 9. INSTALLED NEW CARGO TRACK IAW SRM 51-41-02 AND 51-41-04.

Part: ANGLE — CRACKED (BS 621-625) · airframe 21,246 hrs · 19,499 cycles

FS 621-625 OBLIQUE ANGLE CRACKED AT STR 14L IN AFT EQUIPMENT BAY. REMOVED LT OBLIQUE ANGLE IAW SRM 51-42-21. LOCATED AND DRILLED NEW OBLIQUE ANGLE IAW SRM 51-40-11 AND INSTALLED IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559-567) · airframe 21,252 hrs · 19,506 cycles

CARGO TRACK CORRODED BETWEEN FS 559+96 -567, LBL 9. INSTALLED A NEW CARGO TRACK IAW SRM 51-41-02 AND 51-41-04.

Part: BRACKET — CORRODED (BS 319.7) · airframe 21,252 hrs · 19,506 cycles

SERVICE DOOR SILL BRACKET AT FS 319.7 HAS MINOR SURFACE CORROSION. REMOVED BRACKET IAW SRM 51-42-21. LOCATED, DRILLED AND INSTALLED NEW BRACKET IAW SRM 51-40-11 AND 51-42-21.

Part: SILL — CORRODED (BS 319.7) · airframe 21,252 hrs · 19,506 cycles

SERVICE DOOR SILL HAS MINOR SURFACE CORROSION AT FS 319.7. REMOVED SERVICE DOOR SILL IAW SRM 51-42-21. LOCATED AND DRILLED NEW SILL AND DOUBLER IAW SRM 521-40-11. INSTALLED NEW SILL AND DOUBLER IAW SRM 51-42-06 AND 51-42-21.

Part: ANGLE — CRACKED (BS 621-625) · airframe 21,246 hrs · 19,499 cycles

FS 621-625 OBLIQUE ANGLE CRACKED AT STR 14R IN AFT EQUIPMENT BAY. REMOVED OBLIQUE ANGLE IAW SRM 51-42-21. LOCATED AND DRILLED NEW OBLIQUE ANGLE IAW SRM 51-40-11 AND INSTALLED IAW SRM 51-42-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,246 hrs · 19,499 cycles

PAX DOOR EXTERIOR LIGHT INOPERATIVE. R & R EXTERIOR EMERGENCY LIGHT AT PAX DOOR IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,736 hrs · 18,935 cycles

FWD EMERGENCY LIGHT INOPERATIVE. LAMPED EMERGENCY LIGHT IAW AMM 33-10-00.

Part: BULKHEAD — CRACKED · airframe 20,254 hrs · 18,403 cycles

ON EDDY CURRENT INSPECTION OF THE AFT PRESSURE BULKHEAD IAW NDTM 51-61-153, RECEIVED CRACK INDICATIONS AT LBL 27 JUST ABOVE THE DOOR TRACK AT THE ZEE MEMBER HEEL LINE. INSTALLED ALL REPAIR PARTS IAW REO 601R-53-61-1541.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,042 hrs · 18,163 cycles

RT FUSELAGE AFT EMERGENCY LIGHT INOPERATIVE. RELAMPED RT FUSELAGE AFT EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 20,012 hrs · 18,127 cycles

EXTERIOR EMERGENCY LIGHT NR 3 DOES NOT WORK. CLEANED LIGHT SOCKET BASE IAW CLEANED LIGHT BASE ASSY IAW AMM 20-10-00, OPS CHECKED GOOD IAW AMM 33-51-00-710-804.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,678 hrs · 17,755 cycles

SERVICE DOOR LOWER EMERGENCY EXIT LIGHT HAS SEVERAL INOPERATIVE BULBS. RELAMPED EMERGENCY EXIT LIGHT IAW AMM 35-51-10, OP'S CHECKED GOOD.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,600 hrs · 17,675 cycles

CRACK FOUND ON PAX DOOR AFT DRAG ANGLE. INSPECTED IAW REO 601R-52-11-1360 02. NO FURTHER DEFECT NOTED AT THIS TIME .

Part: SIGN — BROKEN (CABIN) · airframe 19,272 hrs · 17,318 cycles

PASSENGER DOOR EXIT SIGN COVER IS BROKEN. R & R PASSENGER DOOR FLOOR LEVEL EMERGENCY LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,272 hrs · 17,318 cycles

CRACK ON PAX DOOR AFT DRAG ANGLE AT ASSIST PULLEY BRACKET DUE RE-INSPECT. COMPLIED WITH RE-INSPECT OF CRACK ON PAX DOOR AFT DRAG ANGLE AT ASSIST PULLEY BRACKET IAW REO 601R-52-11-1360.

Part: BULKHEAD WEB — CRACKED (BS 559) · airframe 19,241 hrs · 17,282 cycles

FOUND FS 559 RT SIDE BULKHEAD WEB HAS A CRACK INDICATION APPROX .4" IN LENGTH 55 PERCENT FSH AT WL 59.10 INBD OF RBL 18.0. FAILED NDT INSPECTION. REPAIRED IAW EC/TC REO 601R-53-41-260 & REO 601R-53-41-260, REV E.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,429 hrs · 16,403 cycles

2 PAX DOOR AFT DRAG ANGLE CRACKED. COMPLIED WITH REINSPECT OF THE PAX DOOR AFT DRAG ANGLE CRACK IAW REO 601R-52-11-1360 02. NO ADDITONAL DEFECTS NOTED AT THIS TIME. (OPEN)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,272 hrs · 16,226 cycles

CRACK FOUND ON PAX DOOR ON AFT DRAG ANGLE AT ASSIST PULLEY BRACKET. R & R IAW REO 670-52-11-072, REV E.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 18,272 hrs · 16,226 cycles

CRACK FOUND ON PAX DOOR EDGE MEMBER AFT SIDE UNDER TOP STEP. ITEM MOVED MCOL 640009-1 OPERATE IAW REO 601R-52-11-1360 04 ZONE 5 TEMP DISPOSITION IS VALID FOR 1500 FLT HRS WITH REINSPECTION EVERY 200 FLT HRS FOR ANY DAMAGE PROPAGATION MCC ADVISED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,272 hrs · 16,226 cycles

CRACK FOUND ON PAX DOOR ON AFT DRAG ANGLE AT MOTOR ASSIST PULLEY BRACKET. OPERATE IAW REO EC/TC 601R-52-11-1360 02, ZONE 3 TEMP DISPOSITION IS VALID FOR 1500 FLT HRS WITH REINSPECT EVERY 200 FLT HRS FOR ANY DAMAGE PROPAGATION MCC ADVICED.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 18,265 hrs · 16,217 cycles

CRACK FOUND ON PAX DOOR EDGE MEMBER AFT SIDE UNDER TOP STEP. REPAIRED IAW REO 601R-52-11-2050.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,498 hrs · 15,277 cycles

CEILING EMERGENCY LIGHT 2ND FROM REAR IS INOP. RELAMPED CEILING EMERGENCY LIGHT 2ND FROM REAR IAW VCMM 33-22-89. OPS CK GOOD. RELAMPED CEILING EMERGENCY LIGHT 2ND FROM REAR IAW VCMM 33-22-89. OPS CK GOOD. (CLOSED)

Part: BRACKET — UNSERVICEABLE (NLG) · airframe 17,496 hrs · 15,276 cycles

GEAR DISAGREE AFTER TAKEOFF NOSE GEAR REMAINED DOWN COMPLIED WITH QRH ALL INDICATIONS NORMAL EXCEPT NOSE DOOR OPEN MESSAGE AIRCRAFT OPERATED ON CONTAMINATED RUNWAY AND TAXI WAY WITH SNOW POST FLIGHT REVEILS ICE ON PROX SENSORS. ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED. R & R NLG WOW SENSOR BRACKET IAW CMM 32-20-04 PERFORMED 3 GEAR SWINGS OPS CK AND RIGGING GOOD NOFURTHER DEFECTS AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,584 hrs · 14,213 cycles

AFT EMERGENCY LIGHT OVERWING ON LT & RT SIDE INOP. R & R AFT EMERGENCY LIGHT LAMPS RT & LT SIDE IAW AMM 33-51-21-400-801, OPS CK'S GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,584 hrs · 14,213 cycles

2 EA EMERGENCY LIGHTS IN CEILING INOP. R & R FLOODLIGHT, CEILING EMERGENCY LAMPS IAW AMM 33-51-16-400-801 AT NR 2 AND NR 4 POSITION. OP'S CK NEGATIVE. DURING FURTHER TROUBLESHOOTING DISCOVERED NR 4 EMERGENCY POWER PACK FAILURE, SWAPPED POWER PACK FOR TROUBLESHOOTING AND CONFIRMED OPERATION OF NR 2 & NR 4 EMERGENCY CEILING LIGHTS, OPS CK NORMAL. R & R NR 4 EMERGENCY POWER PACK IAW 33-51-04-800-801, ALL EMERGENCY LIGHTS ON POWER PACK NR4 OPS CK NORMAL EXCEPT NR 4 CEILING LIGHT FURTHER TROUBLESHOOTING REQUIRED. OPENED AND OK TO CLOSE PANEL 273LC AND CEILING PANELS AT FS424.00L. FOUND BROKEN WIRE LY43A22N BEHIND LAVATORY LIGHT BRACKET. REPAIRED IAW ESPM 20-16 OPS CHECK EMERGENCY LIGHTS WIRE GOOD IAW AMM 33-51-00-710-801. OPS CHECK LAVATORY LIGHTS GOOD IAW AMM 33-25-00-710-801. (OPEN)

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 16,551 hrs · 14,175 cycles

REAR PRESSURE BULKHEAD WEB AT FS 621.00 IS CRACKED ABOVE LINTEL ATTACH POINT. AREA IS MARKED. REPAIRED IAW EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND THE REPAIR COMPLIES WITH THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230, REV D.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 16,551 hrs · 14,175 cycles

FS409 + 128 LBL 18.00 VERTICAL BEAM OTBD SIDE LOWER ATTACH FASTNER HOLE CRACKED PROPAGATING INTO RADIUS OF BEAM APPROX ".500"L. REPAIRED IAW EC/TC REO 601R-53-41-1056. COMPLIED WITH EC/TC REO 601R-53-41-056, IAW REO 601R-53-41-056, REV E.

Part: PRESSURE PANEL — CRACKED (BS 499) · airframe 16,551 hrs · 14,175 cycles

PRESSURE FLOOR SUSPECTED CRACK AT APPROX RBL 30R, FS 499.00. PERFORMED EDDY CURRENT INSP OF SUSPECTED CRACK ON PRESSURE FLOOR. NO INDICATIONS NOTED AT THIS TIME.

Part: PLACARD — WORN (ESCAPE HATCH) · airframe 16,551 hrs · 14,175 cycles

ALL EMERGENCY CREW ESCAPE PLACARDS ARE WORN AND UNREADABLE. R & R ALL EMERGENCY CREW ESCAPE PLACARDS, ALL WORK DONE IAW AMM 20-60-11-400-801-A01.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 16,551 hrs · 14,175 cycles

REQUEST NDT ON PRESSURE FLOOR FOR POSSIBLE CRACK AT APPROX RBL 30R, FS 499.00.

Part: FRAME — CORRODED (BS 333) · airframe 16,551 hrs · 14,175 cycles

CORROSION FOUND AT FS 333 BETWEEN STR 26L AND 27 FOUND ON FRAME. REMOVED CORROSION FROM FRAME BETWEEN STR 26L AND 26R IAW SRM 51-21-06. AT FS 333. PERFORMED THICKNESS INSPECTION OF BLEND AREA ON ANGLE AT FS 333.00 BETWEEN S26 AND S27L IAW MAC NDT INSP PROCEDURE UT-3 MINIMUM MATERIAL REMAINING IS .047". FRAME SECTOR NOMINAL THICKNESS IS .050. REMOVED DAMAGE IS LESS THAN 10 PERCENT. WITHIN SERVICABLE LIMITS IAW SRM 53-21-15 & 53-00-00. INSTALLED FASTENERS AND APPLIED A023 TOP COAT FINISH IAW B/P 601R31022 REV B.

Part: DOOR — FAILED (AIRSTAIR) · airframe 16,551 hrs · 14,175 cycles

ASD FAILED OPS CHECK DOOR WOULD NOT OPEN WITHIN 10 SECONDS WITH WEIGHT ADDED. PERFORMED ADJUSTMENT OF THE PASSENGER DOOR COUNTER BALANCE IAW AMM TASK 52-11-17-820-801 & PERFORMED FUNCTIONAL CHECK OF DOOR IAW AMM 52-11-00-720-802 FUNCTIONAL CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,424 hrs · 14,023 cycles

CTR AILE FWD FACING OVERHEAD EMERGENY EXIT LIGHT INOP. (RESOLVED ON W/O: 155107 TASKCARD: N/R-00006 ) R & R EMERGENCY BATTERY IAW AMM 33-51-04. OP CK GOOD, ITEM: 1, R & R EMERGENCY BATTERY IAW AMM 33-51-04. OP CK GOOD. (CLOSED)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,424 hrs · 14,023 cycles

LT/RT FWD EXT EMERG OVERWING LIGHTS INOP. (RESOLVED ON W/O: 155107 TASKCARD: N/R-00009 ) R & R EMERGENCY BATTERY IAW AMM 33-51-04. OPS CK GOOD. R & R EMERGENCY BATTERY IAW AMM 33-51-04. OP CK GOOD. (CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,342 hrs · 13,925 cycles

SERVICE DOOR FLOOR EMERGENCY EXIT SIGN HAS SEVERAL LAMPS INOP. RELAMPED G1 FLOOR LEVEL EMERGENCY EXIT SIGN FLOODLIGHT. OPS CHECK GOOD. RELAMPED G1 FLOOR LEVEL EMERGENCY EXIT SIGN FLOODLIGHT. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,223 hrs · 12,691 cycles

EMERGENCY LIGHTS INOPERATIVE.

Part: LANDING GEAR — WARNING MESSAGE · airframe 15,246 hrs · 12,719 cycles

FLT 5428, GEAR DISAGREE MSG ILLUMINATED AFTER TAKE OFF DURING LDG GEAR RETRACTION WITH THE GEAR HANDLE UP. THE NOSE GEAR ETCAS INDICATION REMAINED WHITE BOXED UP. GEAR EXTENDED NORMAL. EMERGENCY DECLARED AS A PRECAUTION, AIRCRAFT RETURNED AFTER T/O.

Part: LIGHT — BROKEN (CABIN) · airframe 14,897 hrs · 12,366 cycles

OUTBOARD EMERGENCY LIGHT ON FLIGHT ATTENDANTS WARDROBE BASE BROKEN.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 13,857 hrs · 11,374 cycles

EXTERIOR SERVICE DOOR EMERGENCY LIGHT INOP.

Part: ANGLE — CRACKED (BS 484) · airframe 1,250,217 hrs · 10,169 cycles

FS 484 ANGLE IS CRACKED AT THE INBOARD SIDE OF LBL 36. REMOVED CABLE GUIDE BRACKETS FOR ACCESS TO REPAIR BY REMOVING BOLTS, NUTS, WASHERS AND COTTERPINS. REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE ANGLE IAW REO 601R-53-41-059 AND REO 601R-53-41-734. INSTALLED SAME SERVICEABLE CABLE GUIDE BRACKETS IAW SRM 51-41-04. COMPLIED WITH REO 601R-53-41-059.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 1,250,217 hrs · 10,169 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX .5" LONG. REMOVED AND REPLACED CARGO DOOR SUPPORT BEAM LOWER ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-21. (B)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 1,250,217 hrs · 10,169 cycles

SUPPORT ANGLE AT FS 280, RBL 9, INBD AND OTBD ARE CRACKED. REMOVED PSU PNL 11AB, 2AB AND 3AB IAW AMM 25-28-01-000-803. PSU PANELS 11AB, 2AB, AND 3AB REQUIRE REINSTALL. PSU PANEL 1AB, 2AB AND 3AB REINSTALLED PSU PANELS 1AB, 2AB AND 3AB IAW AMM 25-28-01-400-803 OPS CKS DUE. TEST POF PSU PPANEL 1AB 2AB AND 3AB IAW MM 33-24-00-710-801, 23-31-00-710-801, 33-22-00-710-801, AND 35-20-00-710-803 NO DEFECTS NOTED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 1,250,217 hrs · 10,169 cycles

SUPPORT ANGLES AT FS 280, LBL 9, INBD AND OTBD ARE CRACKED. REMOVED BOTH I/B AND O/B SUPPORT ANGLES AT FS 280 LBL 9 IAW SRM 51-42-06 AND 51-42-21. LOCATED AND STARTED TO INSTALL BOTH I/B AND O/B SUPPORT ANGLES AT FS 280 LBL 9 IAW SRM 51-42-06 AND 51-42-21. COMPLETED INSTALLATION IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 484) · airframe 1,250,217 hrs · 10,169 cycles

FS 484 ANGLE IS CRACKED AT THE OUTBOARD SIDE OF LBL 27. REMOVED AND REPLACED CRACKED ANGLE IAW REO 601R-53-41-059 WITH NEW SERVICEABLE PART. COMPLIED WITH REO 601R-53-41-059 STEP 1 THRU 5. RII COMPLIED WITH 5300040.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 12,502 hrs · 10,169 cycles

LIGHTED EXIT SIGN ON WARDROBE HAS BROKEN ELECTRICAL CONNECTION CIRCUIT P9LY/J9LY. INSTALLED NEW P9LY/J9LY WARDROBE EMERGENCY LIGHT CONNECTORS IAW EESPM 20-17-10 AND WDM 33-51-00. WARDROBE EMERGENCY LIGHTS OP TEST REQUIRED. OPS TEST GOOD AT THIS TIME IAW AMM 33-51-00-710-801. (B)

Part: HANDLE — NO TEST (PAX DOOR) · airframe 1,250,217 hrs · 10,169 cycles

EMERGENCY HANDLE OF THE PAX DOOR FAILS FORCE TEST. LUBED PAX DOOR IAW AMM 12-20-52-640-810. PERFORMED FUNCTIONAL TEST OF PAX DOOR INNER HANDLE TEST GOOD AT THIS TIME IAW AMM 52-11-00-720-802.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 12,502 hrs · 10,169 cycles

THE PAX DOOR EXTERIOR HANDLE AND FLAPPER ARE CRACKED. REMOVED HANDLE AND REPLACED IAW AMM 52-11-03-400-802 AND SB 601R-52-119. ACCOMPLISH CLOSEOUT SECTION C AND INSTALLED PROXIMITY SWITCH TARGET ON DOOR HANDLE. (B)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,641 hrs · 8,653 cycles

FOUR INCH SECTION OF EMERGENCY FLOOR LIGHTING SYSTEM INOP AT ROW 12. 10-18-07 REPLACED LIGHTED EMERG FLOOR STRIP AT ROW 12 IAW CRJ200 AMM 33-51-01. OPS CHECK GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 9,544 hrs · 7,818 cycles

FLAPS FAIL AT 0. EMERGENCY DECLARED.

Part: UNKNOWN — UNKNOWN (THRUST REVERSERS) · airframe 9,339 hrs · 7,671 cycles

RIGHT REV UNLOCK MSG IN FLIGHT AT FL260. EN ROUTE TO ATL A/C DIVERTED TO MDT DUE TO MTC EMERGENCY DECLARED. (THRUST REVERSER SYSTEMS).

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 9,324 hrs · 7,661 cycles

RECEIVED FLAPS FAIL WHEN SELECTING FLAPS FROM 0 TO 8 DEGREES. EMERGENCY DECLARED.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 8,905 hrs · 7,348 cycles

FLAPS FAIL MSG WHEN SELECTING 8 DEGREES. TOWER DECLARED AN EMERGENCY.

Part: STEP — CRACKED (AIRSTAIRS) · airframe 7,784 hrs · 6,514 cycles

BOTTOM STEP OF AIRSTAIR CRACKED WHERE ARM ATTACHES TO IT.

Part: RIB — CRACKED · airframe 7,735 hrs · 6,468 cycles

FOUND RT BATT RIB CRACKED.

Part: HINGE — CORRODED (PAX DOOR) · airframe 7,735 hrs · 6,468 cycles

PAX DOOR TOP STEP UPPER HINGE CORRODED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,735 hrs · 6,468 cycles

FLOOR SUPPORT ANGLE AT FS 621 & LBL 36 IS CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,735 hrs · 6,468 cycles

484 ANGLE AT RBL 36 IS CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,735 hrs · 6,468 cycles

FS 484 ANGLE CRACKED AT RBL 27.0.

Part: FITTING — CRACKED (PAX DOOR) · airframe 7,736 hrs · 6,468 cycles

AFT PAX DOOR ANCHOR FITTING CRACKED REF DML 73089.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,736 hrs · 6,468 cycles

RIGHT HAND 621 OBLIQUE ANGLE CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,736 hrs · 6,468 cycles

LEFT HAND 621 OBLIQUE ANGLE CRACKED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,736 hrs · 6,468 cycles

RANRC 123 PAX DOOR AFT DRAG ANGLE CRACKED.

Part: SMOKE — DETECTED (COCKPIT) · airframe 7,642 hrs · 6,390 cycles

SMOKE IN COCKPIT ON DESCENT INTO MSY CAPT TURNED OFF THE LT PACK AND THE RT PACK IS DEFERRED AND AFTER ARRIVING AT GATE SHUT ACFT DOWN AND RIBBON OF SMOKE WAS COMING FROM CAPTAINS O2 MASK BOX. NO SMOKE IN CABIN.

Part: MOUNT — CRACKED (AFT AIRSTAIRS) · airframe 7,636 hrs · 6,386 cycles

ASD AFT ANCHOR MOUNT CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,554 hrs · 6,315 cycles

RT AFT EXTERNAL EMERGENCY LIGHT INOP.

Part: STEP — SEPARATED (AFT SERVICE DOOR) · airframe 7,322 hrs · 6,137 cycles

ASD BOTTOM STEP SEPARATED AT ATTACHED STAY ROD BRACKET TO STEP COMPOSITE.

Part: COVER — MISSING (CABIN)

DURING A GROUND INSPECTION IN CAE, THE LOWER OUTBAORD EMERGENCY EXIT SIGN, NEAR THE PASSENGER DOOR, WAS FOUND TO BE MISSING THE COVER. MAINTENANCE REPLACED THE LOWER OUTBOARD EMERGENCY EXIT SIGN COVER, NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

DURING CLIMB-OUT FROM ATW-ATL, AT APPROXIMATELY 20,000 FEET, THE CREW RECEIVED A RIGHT REVERSER UNLOCKED CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO ATW, WHERE IT LANDED SAFELY. MAINTENANCE PERFORMED OPERATIONAL TESTS OF THRUST REVERSER SYSTEM IAW CRJ-200 AMM 71-00-00-710-806. NO DEFECTS WERE NOTED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS)

DURING A GROUND INSPECTION, THE FWD CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: BATTERY PACK — MISINSTALLED (EMERGENCY LIGHTS)

DURING A GROUND INSPECTION, THE LT AND RT EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE EMERGENCY BATTERY PACK AND CHARGER AND FOUND IT INSTALLED INCORRECTLY. REINSTALLED BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN SHV, THE FORWARD CABIN EMERGENCY LIGHT AND RIGHT WING FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE WILL REMOVE AND REPLACE THE LAMPS IN THE FORWARD CABIN EMERGENCY LIGHT ASSEMBLY AND THE RIGHT WING FORWARD EMERGENCY LIGHT. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4260 - DURING A GROUND INSPECTION IN VPS, THE EMERGENCY LIGHT, ABOVE ROW 2, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT, ABOVE ROW 2. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

FLT 4490 - DURING CRUISE FROM XNA-CVG, AT APPROX 25,000 FEET, THE CREW RECEIVED A RIGHT REVERSER UNLOCKED CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED INTO EVV, WHERE IT LANDED SAFELY. OUTSTATION MAINTENANCE DEACTIVATED THE RIGHT THRUST REVERSER IAW MEL NR 78-30-01. MAINTENANCE REACTIVATED THE RIGHT THRUST REVERSER BY REINSTALLING THE BLEED LINE AND CONNECTORS. OPERATIONAL CHECKS WERE GOOD AND NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY CEILING LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW 10. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: RESERVOIR — LEAKING (NR 3 HYD SYS)

FLT 4777 - DURING APPROACH INTO DFW FROM ORD, THE CREW RECEIVED A HYDRAULIC THREE LOW PRESSUER CAUTION LIGHT WHEN THE GEAR HANDLE WAS LOWERED, FOLLOWED BY A GEAR DISAGREE WARNING. THE NOSE GEAR INDICATED DOWN AND LOCKED WITH THE MAINS UNSAFE. THE AIRCRAFT PERFORMED A GO-AROUND AND THE QRH WAS COMPLIED WITH. THE NR 3 HYDRAULIC SYSTEM FLUID LEVEL WAS AT FIVE PERCENT AND THE PRESSURE INDICATED 100 PSI. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ORD. DURING SERVICING OF THE NR 3 HYDRAULIC SYSTEM, MAINTENANCE OBSERVED A LEAK FROM THE NR 3 HYDRAULIC RESERVOIR, REMOVED AND REPLACED IT. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)