N885AS

Part: SKIN — WORN (TE FLAP VANE) · airframe 37,117 hrs · 35,420 cycles

ALL 3 LT INBD FLAP VANE L/E SKIN SECTIONS HAVE WEAR. (C-CHECK) RO: 05/21/2019 REPLACED 3 LT INBD FLAP VANE L/E SKIN SECTIONS IAW SRM.

Part: FLAP — DENTED (RT WING) · airframe 37,117 hrs · 35,420 cycles

RT INBD. FLAP DENTED. (C-CHECK) RO: 05/21/2019 REMOVED AND REPLACED THE RT INBD FLAP IAW AMM. ALL RIGS GOOD, OPERATIONAL TEST GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,117 hrs · 35,420 cycles

INTERCOSTAL AT APPROX. FS473, BETWEEN RBL27 AND RBL36, BELOW FLOOR, HAS A CRACKED ATTACH CLIP ON THE OUTBOARD SIDE. (C-CHECK) RO: 05/21/2019 REMOVED CRACKED CLIP (ANGLE), AND INSTALLED NEW CLIP IAW REO. LEAK CHECK GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,117 hrs · 35,420 cycles

INTERCOSTAL AT APPROX. FS473, BETWEEN LBL27 AND LBL36, BELOW FLOOR, HAS A CRACKED ATTACH CLIP ON THE OUTBOARD SIDE. (C-CHECK) RO: 05/21/2019 REMOVED CRACKED CLIP (ANGLE), P/N 601R-53-41-059-1 AND INSTALLED NEW CLIP IAW REO. LEAK CHECK GOOD.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 37,117 hrs · 35,420 cycles

CORROSION ON CROSS BEAM CAP. FS.589.00, BETWEEN RBL27 AND RBL43. (C-CHECK) RO: 05/21/2019 REMOVED CROSSBEAM CAP STRIP AT FS589 BETWEEN RBL 27 AND RBL 43. AND INSTALLED NEW SERVICEABLE CROSSBEAM CAP STRIP AT FS589 BETWEEN RBL 27 AND RBL 43 IAW SRM.

Part: NOT REPORTED — DENTED (FUSELAGE) · airframe 37,117 hrs · 35,420 cycles

RT FUSELAGE FROM FS 640 TO FS 654 DENTS BETWEEN STR 21R AND STR 22R. (C-CHECK) RO: 05/21/2019 PERFORMED PERMANENT REPAIR ON RT FUSELAGE DENT #1 LOCATED AT APPROX FS645.00 BETWEEN STRINGER 21R AND 22R IAW REO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,117 hrs · 35,420 cycles

CORROSION ON EXTERNAL SKIN AT FS 409+96 BETWEEN STR 25L AND STR 25R. (C-CHECK) RO: 05/21/2019 PERFORMED PERMANENT REPAIR ON CORROSION OF EXTERNAL SKIN AT FS409.96 BETWEEN STR25L AND STR25R IAW REO. PRESSURE LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,117 hrs · 35,420 cycles

IN AVIONICS BAY, CORROSION ON AFT SIDE OF INTERCOSTAL BETWEEN FS349.00 AND FS364.00 LEFT OF STR 27. (C-CHECK) RO: 05/21/2019 REMOVED AND REPLACED INTERCOSTAL AT FS349.00 TO FS364.00 LEFT OF STR 27 IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,117 hrs · 35,420 cycles

IN AVIONICS BAY, CORROSION ACROSS INTERCOSTAL BETWEEN FS349.00 AND FS364.00 RIGHT OF STR 27. (C-CHECK) RO: 05/21/2019 REMOVED AND REPLACED INTERCOSTAL AT FS349.00 TO FS364.00 RIGHT OF STR 27 IAW SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,117 hrs · 35,420 cycles

DENTS IN SKIN AT RT FS 589 - FS605 AFT OF AIR CONDITION SERVICE PANEL. (C-CHECK) RO:05/21/2019 C/W REO REPAIR. PRESSURE AND LEAK CHECK GOOD.

Part: SKIN — DAMAGED (LT WING) · airframe 36,608 hrs · 34,845 cycles

DAMAGE TO THE LH WING PLANK LWR SKIN AT WS 148.019 LOCATED 1" FWD OF EDGE OF WING PLANK. (PERMANENT REPAIR) RO: 11/06/2018COMPLIED WITH PERMANENT REPAIR OF THE LH WING PLANK LWR SKIN AT WS 148.019 IAW REO. LEAK CHECK GOOD, NO DEFECTS FOUND.

Part: FAIRING — CHAFED (RT WING TE FLAP) · airframe 33,759 hrs · 31,664 cycles

RIGHT FLAP STUB FAIRING CHAFED. R & R RH FLAP STUB FAIRING IAW AMM. GAP CHECKED GOOD.

Part: FAIRING — CHAFED (LT WING TE FLAP) · airframe 33,759 hrs · 31,664 cycles

LEFT FLAP STUB FAIRING HAS CHAFING. R & R NEW STUB FAIRING IAW SRM & AMM. OPS CHECK GOOD.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 33,759 hrs · 31,664 cycles

SERVICE DOOR THRESHOLD PLATE HAS AREAS OF CORROSION. REMOVED AND REPLACED SERVICE DOOR THRESHOLD PLATE IAW SRM.

Part: SENSOR — OUT OF ADJUST (NLG STEERING) · airframe 32,974 hrs · 30,815 cycles

GEAR DISAGREE AFTER TAKEOFF, NLG DID NOT COME UP. DECLARED AN EMERGENCY & RETURNED TO THE FIELD. LANDED WITHOUT INCIDENT BUT HAD TO BE TOWED TO THE GATE DUE TO NOSE GEAR WAS TURNED. TROUBLESHOT THE SYSTEM, INSP GEAR AND SENSORS, NO DEFECTS NOTED. PSEU FLAGGING ALL PARAMETERS EXCEPT WOW 2. ADJUSTED WOW NR 1 SENSORS, SECURED LEFT WIRE HARNESS. ALL OPS CHECK GOOD. NOSE WHEEL STEERING OPS CHECKED GOOD.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 31,710 hrs · 29,452 cycles

ON DEPARTURE, GEAR DISAGREE CAUTION MSG. RETURNED TO FIELD. R & R THE NR 3A ACMP AND MLG SELECTOR VALVE, SWUNG THE GEAR NUMEROUS TIMES AFTER REPAIRS. OPS CHECKED GOOD.

Part: STRUT — DISCHARGED (NLG) · airframe 31,503 hrs · 29,223 cycles

GEAR DISAGREE NOSE GEAR CYCLED AND RUBBING SOUND HEARD. SERVICED STRUT AND CLEANED NLG UPLOCK PIN. PIN MOVES FREELY. PERFORMED EXTENSION/RETRACTION IAW AMM. OPS CHECK GOOD.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 31,170 hrs · 28,878 cycles

CABIN PRESSURE WARNING IN FLIGHT, CREW COULD NOT CONTROL THE RISE IN PRESSURE. REPLACED NR 2 OUTFLOW VALVE IAW AMM.

Part: SKIN — CHAFED (LT AILERON) · airframe 30,184 hrs · 27,740 cycles

LOWER LEFT AILERON PANEL 599AB CHAFED, C-CHECK RO 3/23/15, REPAIRED LOWER LT AILERON PANEL 599AB CHAFE REF REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 30,184 hrs · 27,740 cycles

LOWER LT AILERON PANEL 599BB CHAFED, C-CHECK, RO 3/23/15, REPAIRED LOWER LT AILERON PANEL 599BB CHAFE REF REO.

Part: FRAME — CORRODED (BS 319.7) · airframe 30,184 hrs · 27,740 cycles

FS 319.7, STRINGER 26L TO 26R FWD AND AFT SIDE HAS CORROSION. C-CHECK, RO 3/23/15. R & R THE FRAME SECTOR AT FS 319.7, STR 26L TO STR 26R IAW SRM. COMPLIED WITH FORM M-337. LEAK CHECK GOOD. COMPLIED WITH ST 51-900-1003.

Part: FRAME — CORRODED (BS 333) · airframe 30,184 hrs · 27,740 cycles

FS 333.0 AT STRINGER 26L TO 26R FWD AND AFT SIDE HAS CORROSION, C-CHECK RO 3/23/15, R & R THE LOWER SECTOR AT FS333 IAW SRM. OP CHECKS GOOD, LEAK CHECK GOOD. COMPLIED WITH ST 51-900-1003. COMPLIED WITH FORM M-337.

Part: FRAME — CORRODED (BS 349) · airframe 30,184 hrs · 27,740 cycles

FS 349.0 AT 26L TO 26R FWD AND AFT SIDE HAS CORROSION, C-CHECK, RO 3/23/15, R & R THE LOWER FRAME FS349.0 AT STR 25L TO STR 26R IAW SRM. COMPLIED WITH FORM M-337. LEAK CHECKS GOOD. COMPLIED WITH ST 51-900-1003.

Part: SEAL DEPRESSOR — CHAFED (PAX DOOR) · airframe 30,184 hrs · 27,740 cycles

PAX DOOR SEAL DEPRESSOR CHAFED ON FWD AND AFT SIDES FROM LATCH PINS, MARKED, C-CHECK, RO 3/23/15, BLENDED OUT CHAFE ON PAX DOOR SEAL DEPRESSOR ON FWD AND AFT SIDES FROM LATCH PINS. FWD SIDE OF STRIKER PLATE MEASURES .023" PROTECTOR PLATE AND ALL HARDWARE SECURELY ATTACHED, PERMANENT REPAIR FOR SURFACE DAMAGE LESS THAN .031", STEPS 1-3 MEASUREMENT CHECKED WITH DEPTH GAGE TUC4720, CAL DUE 31-DEC-2015. AFT SIDE OF STRIKER PLATE MEASURES .027" PROTECTOR PLATE AND ALL HARDWARE SECURELY ATTACHED, PERMANENT REPAIR FOR SURFACE DAMAGE IS LESS THAN .031" STEPS 1-3 MEASUREMENT CHECK WITH DEPTH GAGE TUC4720 CAL DUE 31-DEC-2015, REF REO.

Part: GATE — DENTED (PAX DOOR) · airframe 30,184 hrs · 27,740 cycles

PAX DOOR VENT FLAP DENTED FROM ICE BREAK CABLE; VISIBLE FROM EXTERIOR SURFACE, MARKED, C-CHECK RO 3/23/15, EVALUATED PAX DOOR PRESSURE DOOR? DENT AND CHAFE FROM ICE BREAK CABLE, DAMAGE EXCEEDS ALLOWABLE LIMITS, CHAFE EXTENDS INTO NO DAMAGE ZONE REF REO. PRESSURE DOOR REQUIRES REPLACEMENT, TRANS 11934346, JOB: 2752141, OP:154 FOR WORK PERFORMED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,922 hrs · 27,438 cycles

EMERGENCY LIGHTS ARE INOPERATIVE. R & R NR 2 AND NR 3 EMERGENCY LIGHT BATTERY PACKS. EMERGENCY LIGHTS OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 29,251 hrs · 26,634 cycles

REAR F/O SIDEWALL FLOOD LIGHT INOPERATIVE. FOUND BROKEN WIRE, RESOLDERED WIRE IAW ESPM. LIGHT SYSTEM OP CHECKS GOOD IAW AMM.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 29,079 hrs · 26,444 cycles

RED INDICATOR LIGHT FOR RT EMERGENCY FLASHLIGHT IN COCKPIT DOES NOT ILLUMINATE. R & R RT EMERGENCY COCKPIT FLASHLIGHT BATTERY. OPS CHECKED GOOD.

Part: BOLT — GALLED (ENGINE MOUNT) · airframe 28,860 hrs · 26,197 cycles

LEFT ENGINE, YOKE MOUNT BOLTS HAVE GALLING MARKS. FOUND DURING LT ENGINE CHANGE. R & R LT ENGINE YOKE MOUNT BOLTS IAW AMM.

Part: BUSHING — GALLED (ENGINE MOUNT) · airframe 28,860 hrs · 26,197 cycles

LEFT ENGINE, YOKE MOUNT LINK BUSHINGS HAVE GALLING MARKS, FOUND DURING LT ENGINE CHANGE. R & R LT ENGINE MOUNT LINK BUSHINGS IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,664 hrs · 25,981 cycles

NR 4 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.

Part: DETECTOR — FAILED (TE FLAP SYSTEM) · airframe 28,358 hrs · 25,650 cycles

FLAPS DEGRADED MESSAGE DISPLAYED WITH ERRONEOUS FLAP POSITIONS. R & R THE SKEW DETECTION UNIT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,415 hrs · 24,624 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT2902 RELAMPED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,372 hrs · 24,584 cycles

EMERGENCY EXIT SIGN AT 8F, ROW 1, OVERHEAD CEILING AT WING EXITS & ALL THREE ON LT OVERWING EXIT. FLT 2960 ALLOWED BATTERIES TO CHARGE & ALL EMERGENCY LIGHTS OPERATED NORMALLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,204 hrs · 24,408 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT#2988 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,112 hrs · 24,314 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT#2940 RELAMPED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,937 hrs · 24,118 cycles

EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. FLT#2934 CHARGED EMERGENCY BATTERIES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,674 hrs · 23,822 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#2783 RELAMPED.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 26,530 hrs · 23,664 cycles

RIGHT MLG DOOR INNER L/E SKIN CHAFED AT OTBD END. C-CHECK, REPAIRED RT MLG DOOR INNER SKIN IAW SRM AND REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,483 hrs · 23,614 cycles

THE 2ND OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 2965) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,471 hrs · 23,600 cycles

AFT EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 2980) RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,435 hrs · 23,560 cycles

ELECTRICAL SMELL IN REAR OF CABIN. (FLT 2972) INVESTIGATED SMELL IN CABIN FOUND NO SOURCE OR EVIDENCE OF BURNING, OKAY FOR CONTINUED SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,132 hrs · 23,227 cycles

NR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 2951) RELAMPED EMERGENCY LIGHT.

Part: CONTROL UNIT — FAILED (SPOILER SYS) · airframe 25,359 hrs · 22,476 cycles

AIRCRAFT ROLLED UNEXPECTEDLY 10° TO THE RIGHT, A FLIGHT SPOILER CAUTION MESSAGE DISPLAYED. (FLT 2976) REPLACED BOTH NR 1 & 2 SECUS IAW AMM PN ON/OFF: 49-164-20 S/N ON: 03129 S/N OFF: 03490 P/N ON/OFF: 49-164-20 S/N ON: 03339 S/N OFF: 03084.

Part: O-RING — BROKEN (HYDRAULIC SYS) · airframe 24,846 hrs · 21,933 cycles

HYDRAULIC 3 LOW PRESSURE. (FLT 2927) REPLACED A BROKEN PUMP O-RING AND SERVICED HYDRAULIC SYSTEM 3 TO PROPER LEVEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,262 hrs · 21,309 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2971) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,077 hrs · 21,131 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2851) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,942 hrs · 20,995 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2966) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,809 hrs · 20,863 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. (FLT 2974) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,658 hrs · 20,711 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2956) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,658 hrs · 20,711 cycles

THE LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2980) RELAMPED EMERGENCY LIGHT.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 23,184 hrs · 20,182 cycles

PAX DOOR EMERGENCY FLOOD LIGHTS INOPERATIVE. R & R FUSE IN NR 2 CHARGER ASSY IAW CMM 33-21-70, OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 22,511 hrs · 19,409 cycles

NR 3 EMERGENCY LIGHT BATTERY PACK FAILS OPS CHECK. REPLACED BATTERY NR 3 IAW AMM 33-51-04-400-801. OPS CHECK GOOD.

Part: ANGLE — CORRODED (BS 349) · airframe 22,506 hrs · 19,402 cycles

WHILE ACCESSING FOR REPAIR TO INTERCOSTAL AT FS 349 FOUND SERVICE DOOR ANGLE PN 601R38303-253 TO BE CORRDED. SERVICE DOOR FITS AND CLEARANCES CHECK GOOD IAW MM 52-41-00-220-802. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: FLOOR SUPPORT — CORRODED (BS 324-620) · airframe 22,506 hrs · 19,402 cycles

CARGO DOOR SUPPORT BEAM CAP ANGLE CORRODED AROUND FASTENER HOLES BETWEEN FS 324-620 OTBD SIDE OF LBL 27. DRILLED & LOCATED NEW PART IAW SRM 51-40-06. REMOVED ACCESS PANEL 325DL IAW AMM TASK 55-32-07-000-801. REINSTALLED PANEL 325DL IAW AMM 55-32-07-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 22,506 hrs · 19,402 cycles

FLOOR SUPPORT INTERCOSTAL J ANGLE CORRODED AT FS 349, RBL 45. REO 601R-53-21-1290 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NRI WORK CARD.

Part: SILL — CORRODED (BS 461-559) · airframe 22,506 hrs · 19,402 cycles

RIGHT PRESSURE SILL ANGLE CORRODED FROM FS 461.00 TO FS 559, RBL 45 UNDER CABIN FLOOR PNL 262DRF. ACFT BEING RETURNED TO SERVICE. COMPLIED WITH REO 601R-53-41-666, REV A DATED NOV 3, 2009 AS WRITTEN. RII FOUND TO BE SATSIFACTORY. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 22,506 hrs · 19,402 cycles

CARGO FLOOR SUPPORT BEAM CAP ANGLE CORRODED AROUND FASTENER HOLES BETWEEN FS 605 - FS 621 OTBD SIDE OF RBL 27. EC/TC REQUIRED. REO 601R-53-61-3961, REV -- HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORKCARD. ALL RII'S HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTOR IAW GMM 3-3, PROCEDURES PRIOR TO THE ACFT BEING RETURNED TO SERVICE. RII FOUND TO BE SATISFACTORY.

Part: ATTACH FITTING — CORRODED (DOOR SILL) · airframe 22,506 hrs · 19,402 cycles

UPON REMOVAL OF PAX DOOR SILL ANGLE, FOUND SILL ANGLE ATTACH CLEAT AT AFT END OF SILL ANGLE (FS 349) TO BE CORRODED BEYOND LIMITS. INSTALLED NWE AFT CLEAT FROM SILL ANGLE AT FS 349 IAW SRM 51-42-06 AND 51-42-21. C/W STEP 1 OF REO 601R-53-21-1300 BY FABRICATING A NEW CLEAT FROM S6144-4. PERFORMED EDDY CURRENT OF FABRICATED CLEAT TO COMPLY WITH REO 601R-53-21-1300 IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME. PAINTED PART IAW REO 601R-53-21-1300 STEP 2. COMPLIED WITH STEP 3 OF REO 601R-53-21-1300.

Part: SILL — CORRODED (BS 513-559) · airframe 22,506 hrs · 19,402 cycles

LEFT PRESSURE SILL ANGLE CORRODED FROM FS 513 TO FS 559 LBL 45 UNDER CABIN FLOOR PANEL 261DLF. COMPLIED WITH STEP 5 OF REO 6041R-53-41-1426. PERFORMED EDDY CURRENT OF LT PRESSURE SILL REPAIRED AREAS FS 513 TO FS 559 IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME. REQUIRES STEP 6 OF REO 601R-53-41-1426. COMPLIED WITH STEPS 6, 7 AND 8 OF REO 601R-53-41-1426. REPAIR COMPLETED. EC/TC REQUIRED FOR REO 601R-53-41-1426. REO 601R-53-41-1426, REV -- HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORKCARD. ALL RII'S HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTOR IAW GMM 3-3, PROCEDURES PRIOR TO THE ACFT BEING RETURNED TO SERVICE.

Part: ANGLE — CORRODED (BS 349) · airframe 22,506 hrs · 19,402 cycles

FLOOR SUPPORT INTERCOSTAL J-ANGLE CORRODED AT FS 349 RBL 45. FABRICATED REPAIR PARTS 601R-53-21-1290-1 AND 601R-53-21-1290-2.

Part: FLOORBEAM — CORRODED (BS 574-620) · airframe 22,506 hrs · 19,402 cycles

CARGO FLOORBEAM CAP ANGLE CORRODED AROUND FASTENER HOLES BETWEEN FS 574-620, OTBD SIDE OF RBL 27. REMOVED FLOORBEAM CAP ANGLE IAW SRM 51-42-21 AND SRM 51-42-22. FLOORBEAM CAP ANGLE INSTALLED.

Part: POST — CRACKED (BS 409) · airframe 22,506 hrs · 19,402 cycles

FS 409.0+128, LBL 18.0 INBD SIDE VERTICAL POST HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSPECTION. REMOVED POST ASSY IAW SRM 51-42-06. INSTALLED NEW VERT POST ASSY IAW SRM 51-40-11, SRM 51-47-06 AND REO 601R-53-41-889 REV.A.

Part: WEB — CORRODED (BS 280) · airframe 22,506 hrs · 19,402 cycles

FS 280, WEB IS CORRODED FROM LBL 9-RBL 9. REPAIRED IAW REO 601R-53-11-926.

Part: ATTACH FITTING — CORRODED (BS 349) · airframe 22,689 hrs · 19,626 cycles

FS 349 TO TRANSVERSE BEAM ATTACHMENT FITTING HAS 2 SPOTS OF MINOR CORROSION AT UPPER INBD END, WORST AREA MEASURES APPROX .4" LONG X .20" WIDE X .003" DEEP. REMOVED THE FS 349, LBL 45 TRANSVERSE BEAM ATTACH FITTING IAW SRM 51-42-21. FOUND CORROSION DAMAGE TO BE OUT OF LIMITS IAW SRM 53-21-23 & 53-00-00. PERFORMED STEP 3 OF REO EDDY CURRENT REPAIRED AREAS, NO INDICATIONS NOTED. ROTOPEENED REWORKED AREAS IAW SRM 51-24-11. INSTALLED FITTING AT FS 349, LBL 45 IAW SRM 51-42-21.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 22,506 hrs · 19,402 cycles

PAX DOOR SILL ANGLE IS CORRODED. REMOVED SILL ANGLE IAW SRM 51-42-21, 51-42-13, 51-42-06. LOCATED & DRILLED NEW SERVICEABLE SILL ANGLE IAW SRM 51-40-11. SEALED & INSTALLED NEW SILL ANGLE ASSY IAW THE SRM 51-23-00, 51-25-16, 51-42-06, 51-42-21, 51-42-11.

Part: ANGLE — CORRODED (BS 349) · airframe 22,506 hrs · 19,402 cycles

WHILE ACCESSING FOR REPAIR TO INTERCOSTAL AT FS 349 FOUND SERVICE DOOR ANGLE TO BE CORRODED. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06, 51-42-21, AND 51-42-04.

Part: BEAM — CORRODED (BS 349) · airframe 22,506 hrs · 19,402 cycles

FS 349, TRANSVERSE BEAM HAS CORROSION AT LT SIDE OTBD END, FWD FACE AND BOTTOM OF TOP LIP, MEASURES APPROX 2" LONG X 1.2" WIDE X .009" DEEP. REPAIRED IAW SRM 51-42-06 AND SRM 51-42-21. MINOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 22,506 hrs · 19,402 cycles

CARGO FLOOR SUPPORT CAP ANGLE CORRODED AROUND FASTENER HOLES BETWEEN FS 605-621 OTBD SIDE OF RBL 27. REMOVED FLOOR SUPPORT CAP IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW CAP IAW SRM 51-40-11.

Part: CARGO TRACK — CORRODED (BS 613-621) · airframe 22,506 hrs · 19,402 cycles

CARGO FLOOR BAGGAGE RAIL CORRODED BETWEEN FS 613-FS 621, LBL 9. REMOVED & REPLACED CARGO FLOOR BAGGAGE RAIL AT FS 613-621, LBL IAW SRM 51-41-02 NAD IAW SRM 53-61-49. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR SOP 5702.

Part: FLOOR SUPPORT — CORRODED (BS 574-620) · airframe 22,506 hrs · 19,402 cycles

CARGO FLOOR SUPPORT CAP ANGLE CORRODED AROUND FASTENER HOLES BETWEEN FS 574 - FS 620 OTBD SIDE OF LBL 27. R & R CARGO FLOOR SUPPORT CAP ANGLE IAW SRM 51-42-06 & 51-42-21 AND WITH REO 601R53-61-3778.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 22,506 hrs · 19,402 cycles

CABIN SEAT TRACK SEGMENT CORRODED BETWEEN FS 559+80 - FS 559+96 RBL 27. REMOVED & REPLACED CABIN SEAT TRACK SEGMENT BETWEEN FS 559+80 -559+96 AT RBL 27 IAW MM 53-01-11-000-802 & 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 22,506 hrs · 19,402 cycles

CABIN SEAT TRACK SEGMENT CORRODED AT FS 559+88 RBL 9. REMOVED & REPLACED CABIN SEAT TRACK SEGMENT AT FS 559+88 RBL 9 IAW MM 53-01-11-000-802 & 53-01-11-400-802. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 559) · airframe 22,506 hrs · 19,402 cycles

SEAT TRACK CORRODED FS 559+8-559+86 RBL 9. REMOVED CORROSION IAW SRM 51-21-06. AREA MEASURED .006" D, .1250" WIDE, 14" LONG. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00.

Part: ANGLE — CORRODED (SILL) · airframe 22,506 hrs · 19,402 cycles

RT PRESSURE SILL ANGLE CORRODED FROM FS 461.00-559, RBL 45. REMOVED CORROSION AND FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-41-43 AND REO 601R-53-41-666. REPAIRED IAW REO 610R-53-41-666.

Part: ANGLE — CORRODED (BS 513-550) · airframe 22,506 hrs · 19,402 cycles

LEFT PRESSURE SILL ANGLE CORRODED FROM FS 513 TP FS 550, LBL 45. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS IAW SRM 53-41-43 AND REO 601R-53-41-666. REPAIRED IAW REO 601R-53-41-1426.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 22,506 hrs · 19,402 cycles

CABIN FLOOR SEAT RAILS CORRODED AT LBL 9 AND RBL 9, FS 364 - FS 399. REMOVED CABIN FLOOR SEAT TRACKS AT LBL 9 & RBL 9 FS 364 - FS 399 IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE CABIN FLOOR SEAT TRACKS, PN 601R-31032-15 AT LBL 9 & RBL 9 FS 364 - FS 399 IAW AMM 53-01-11-400-802.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,506 hrs · 19,402 cycles

FS 280 FLOORBEAM UPPER J-ANGLE CRACKED AT GEAR ALTERNATE RELEASE CABLE PULLEY BRACKET OTBD OF LBL 9.0. REPAIRED IAW REO 601R-53-11-926.

Part: ANGLE — CORRODED (BS 349) · airframe 22,506 hrs · 19,402 cycles

FLOOR SUPPORT INTERCOSTAL J-ANGLE CORRODED AT FS 349, LBL 45. REMOVED ANGLE ASSY IAW SRM 51-42-21, 51-42-13 AND 51-42-06. INSTALLED ANGLE IAW SRM 51-42-06, 51-42-21, AND 51-42-13.

Part: SEAT TRACK — CORRODED (BS 399.5-409) · airframe 22,506 hrs · 19,402 cycles

SEAT TRACK CORRODED AT LBL 9, FS 399.50-409+126. REMOVED CORROSION IAW SRM 51-21-06, WITHIN LIMITS IAW SRM 53-31-49, 53-21-49. MINOR REPAIR.

Part: ANGLE — CORRODED (BS 349) · airframe 22,506 hrs · 19,402 cycles

FLOOR SUPPORT INTERCOASTAL J-ANGLE CORRODED AT FS 349, RBL 45. REMOVED ANGLE IAW SRM 51-41-06, 5142-01 AND 51-41-02. FOUND ANGLE TO BE CORRODED BEYOND REPAIRABLE LIMITS IAW 53-00-00. REPAIRED IAW REO 601R-53-21-1290.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 22,506 hrs · 19,402 cycles

SEAT TRACK CORRODED AT RBL 9, FS 399.50-409+126. REPAIRED SEAT TRACK IAW SRM 53-21-49 & 53-31-49. MINOR REPAIR.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,506 hrs · 19,402 cycles

FS 280, FLOORBEAM CRACKED INBD SIDE OF RBL 9. REPAIRED IAW REO 601R-53-11-926.

Part: LIGHT — CRACKED (CABIN) · airframe 22,506 hrs · 19,402 cycles

FLOOR EXIT LIGHT ON GALLEY SIDE TRIM PANEL IS CRACKED. REPLACED LIGHT IAW MM 33-51-10-400-801.

Part: ANGLE — CRACKED (BS 621-625) · airframe 22,506 hrs · 19,402 cycles

LT SIDE FS 621-625, OBLIQUE ANGLE IS CRACKED ADJ TO STRINGER 14. REMOVED AND REPLACED RT BS 621-625 OBLIQUE ANGLE AT STR 14 IAW SRM 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)

Part: ANGLE — CRACKED (BS 621-625) · airframe 22,506 hrs · 19,402 cycles

RT BS 621-625, OBLIQUE ANGLE IS CRACKED ADJ TO STRINGER 14. REMOVED AND REPLACED RT BS 621-625 OBLIQUE ANGLE AT STR 14 IAW SRM 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 21,867 hrs · 18,672 cycles

COVER ON EMERGENCY LIGHT NEAR PAX DOOR BROKEN. REPLACED BROKEN LIGHT ASSEMBLY IAW AMM 33-51-10.

Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 18,630 hrs · 15,131 cycles

RT FS 409.0+128, RBL 18 OTBD SIDE VERTICAL POST HAS AN INDICATION NOTED APPROX .2 INCHES IN LENGTH, 60 PERCENT FSH. FAILED NDT INSPECTION AT WL 69.0. REMOVED VERTICAL SUPPORT POST ASSY ROM FS 409+128 BULKHEAD AT RBL 18.0 IAW CRJ 200 SRM CH 51-42-06. INSTALLED SERVICEABLE VERTICAL SUPPORT POST ASSY IAW CRJ 200 SRM 51-42-06 AND 51-42-22.

Part: SKIN — CRACKED (PAX DOOR) · airframe 18,640 hrs · 15,139 cycles

JOB 8752111 OPERATION 274 / PAX DOOR FWD SKIN IS CRACKED APPROX .500 INCH LONG AT HANDRAIL STOW CUP.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 18,630 hrs · 15,131 cycles

FLOORBEAM AT LBL 27.0 FROM FS 559.00+112 TO FS 621.00 NUTPLATE HOLES HAVE CORROSION AROUND THEM ON OTBD SIDE OF BEAM. COMPLIED WITH EO EC/TC REO 601R-53-61-3176 REV O AND REO 601R-53-61-3176.

Part: SKIN — CRACKED (PAX DOOR) · airframe 18,630 hrs · 15,131 cycles

PAX DOOR AFT SKIN IS CRACKED APPROX AT HANDRAIL STOW CUP. COMPLIED WITH EC/TC REO 601R-52-11-1677 AND MET ALL THE REQUIREMENTS OF REO 601R-52-11-1677. RII C/W 5300040.

Part: ANGLE — DAMAGED (BS 559) · airframe 18,630 hrs · 15,131 cycles

LT FS 559 CAP ANGLE HAS A INDICATION NOTED AT LBL 18.0 APPROX .2 INCH IN LENGTH 90 PERCENT FSH FAILED NDT INSP. C/W EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV C. REF MIC TASK RJ2-53-1 FOR WORK PERFORMED.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 18,630 hrs · 15,131 cycles

CARGO DOOR BEAM AFT BOTTOM ANGLE IS CRACKED 1/4" LONG IN OTBD RADIUS.

Part: DRAG ANGLE — DAMAGED (PAX DOOR) · airframe 18,630 hrs · 15,131 cycles

PAX DOOR AFT DRAG ANGLE CRACKED AT PULLEY APPROX 1 INCH L PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR FROM PAX DOOR AFT DRAG ANGLE AND FABRICATED AND INSTALLED A SERVICEABLE REPAIR SECTION IAW REO/ASA EC/TC REO 601R/52-11-513, STEPS 7 THRU 14.

Part: SUPPORT ANGLE — CORRODED (SERVICE DOOR) · airframe 18,630 hrs · 15,131 cycles

SERVICE DOOR LOWER FWD FRAME SUPPORT ANGLE CORRODED.

Part: DOOR — STUCK (MAIN PAX) · airframe 18,640 hrs · 15,139 cycles

JOB 8752115 OPERATION 63 / PASSENGER DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE. TROUBLESHOOTING REQUIRED. RECURRENT WRITEUP.

Part: DOOR — STUCK (PAX DOOR) · airframe 18,629 hrs · 15,130 cycles

PAX DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE.

Part: DOOR — FAULTY (PAX DOOR) · airframe 18,604 hrs · 15,108 cycles

FWD PASSENGER DOOR WILL NOT OPEN FROM THE INSIDE THE HANDLE WILL NOT GO ALL THE WAY UP.

Part: DOOR — STUCK (MAIN PAX) · airframe 18,577 hrs · 15,084 cycles

PASSENGER DOOR IS VERY DIFFICULT TO OPEN. THE FLIGHT ATTENDANT WAS UNABLE TO OPEN IT.

Part: DOOR — STUCK (MAIN PAX) · airframe 18,577 hrs · 15,084 cycles

PAX DOOR DIFFICULT TO OPEN AFTER LANDING, FLT 5003 DEL 22 MINS.

Part: UNKNOWN — ACTIVATED (AILERON) · airframe 18,203 hrs · 14,726 cycles

REFF AFDL 440826 ITEM 2 - RUDDER AND AILERON TRIM RUNAWAY ON CLIMBOUT. EMERGENCY DECLARED. A/C RETURNED TO ATL AFTER T/O. FLT 5418 DEL 131 MINS.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,375 hrs · 13,972 cycles

FLIGHT ATTENDANT FLASHLIGHT INOP.

Part: CIRCUIT BREAKER — MALFUNCTIONED (COCKPIT) · airframe 17,209 hrs · 13,820 cycles

FAA STATES THAT EMERGENCY LIGHTS FOR EXIT DID NOT ILLUMINATE DURING APPROACH. CONFIRMED ON GROUND THAT LIGHTS DID NOT ILLUMINATE IN THE ARMED POSITION. RESET CIRCUIT BREAKER C2 ON PANEL NR 4. PERFORMED OPS CHECK OF EMERGENCY LIGHTS. OPS CHECK GOOD. IAW CRJ 200 AMM 33-50-00.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 16,153 hrs · 12,882 cycles

RT OVERWING EMERGENCY LIGHT INOP.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,573 hrs · 12,409 cycles

GALLEY DOOR EMERGENCY SIGN HAS BULBS INOP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 14,740 hrs · 11,598 cycles

CAPTAIN'S FLASHLIGHT INOP.

Part: ANGLE — CRACKED (BS 280) · airframe 14,577 hrs · 11,427 cycles

FOUND FS 280 AT RBL 9 O/B ANGLE IS CRACKED.

Part: ANGLE — CRACKED (BS 280) · airframe 14,577 hrs · 11,427 cycles

FOUND FS 280 AT LBL 9 I/B AND O/B ANGLES ARE CRACKED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 14,577 hrs · 11,427 cycles

RIGHT BONDED SKIN DOUBLER CRACKED BETWEEN STRINGER NR 9 AND NR 12 UNDERNEATH 640 DOUBLER. [06-12-07] COMPLED WITH EC/TC ASA REO 601R-53-61-506 REV C. ON RT SIDE.

Part: ANGLE — CRACKED (BS 484) · airframe 14,577 hrs · 11,427 cycles

RBL 36 FS 484 ANGLE IS CRACKED. [06-12-07] REMOVED CRACKED ANGLE FROM FS 484 RBL 36 IAW REO 601R-53-41-059 DUPLICATED NEW ANGLE, PER REO 601R-53-41-059. OK TO LPI. COMPLIED WITH LPI OF MANUFACTURED ANGLE IAW REO 601R-53-41-059 AND NDTM 51-20-08. NO DEFECTS NOTED. INSTALLED NEW ANGLE AND COMPLETED REPAIR IAW REO 601R-53-41-059. LEAK CHECK GOOD IAW CRJ MM 21-31-00.

Part: PLACARD — WORN (CABIN) · airframe 14,139 hrs · 10,994 cycles

ASD -EXIT- PLACARD WORN.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,080 hrs · 10,937 cycles

EXTERIOR EMERGENCY FWD OVERWING LIGHT INOP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,035 hrs · 10,899 cycles

FOUND LT AFT EXT O/W EMERGENCY LIGHT INOP.

Part: LIGHT — BROKEN (CABIN) · airframe 13,554 hrs · 10,487 cycles

EMERGENCY LIGHT AT 6D BROKEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,481 hrs · 9,594 cycles

EMERGENCY LIGHT IN CEILING ABOVE SEATS IN ROW 10 IS OUT.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 12,276 hrs · 9,432 cycles

RT EXT SERVICE DOOR EMERGENCY LIGHT INOP.

Part: ANCHOR FITTING — CRACKED (FUSELAGE)

DURING A HANGAR INSPECTION, THE PASSENGER DOOR AFT ANCHOR FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR AFT ANCHOR FITTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: HANDLE — CRACKED (FUSELAGE)

DURING A HANGAR INSPECTION, THE PASSENGER DOOR EXTERNAL HANDLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EXTERNAL HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE RETRACTING LEVER. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOODLIGHT ON THE FORWARD WINDSCREEN BY THE FLIGHT ATTENDANTS STATION WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY FLOOD LIGHT ON THE FORWARD WINDSCREEN BY THE FLIGHT ATTENDANTS STATION. (M)

Part: VANE — MALFUNCTIONED (STALL WARNING)

DURING TAKEOFF, THE STALL WARNING SYSTEM ACTIVATED EXCEPT THE PUSHER. THE AIRCRAFT DID NOT STALL. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT AOA VANE AND ALSO THE STALL PROTECTION COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: COVER — CRACKED (EXIT SIGN)

DURING A C-CHECK IN MCN, THE LT FORWARD EMERGENCY EXIT SIGN COVER BY THE WARDROBE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD EMERGENCY EXIT SIGN COVER BY THE WARDROBE. OPERATIONAL CHECKS GOOD. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING (C) CHECK, THE RT SIDE FS 484 INTERCOSTAL AT BL 36 AND THE CLIP AT BL27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT SIDE FS 484 INTERCOSTAL AT BL 36 AND THE CLIP AT BL 27 IAW EO 600-53-0098.

Part: CLIP — CRACKED (FUSELAGE)

DURING A (C) CHECK, THE RT IB CLIP AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT IB CLIP AT FS 280.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 625. (M)

Part: HANDLE — CRACKED (E/E BAY DOOR)

DURING (C) CHECK, THE AVIONICS DOOR HANDLE BASE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AVIONICS DOOR HANDLE ASSEMBLY.

Part: CAM ROD — BINDING (PAX DOOR)

FLT 4389 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE ADJUSTED AND LUBRICATED THE CAM ROD AT THE UPPER ROLLER ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HANDLE — MALFUNCTIONED (PAX DOOR)

DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS VERY DIFFICULT TO CLOSE AND STOW THE OUTER HANDLE. MAINTENANCE OPENED AND CLOSED THE MAIN PASSENGER DOOR TEN TIMES WITH NO FAULTS FOUND. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FLT 4596 - DURING CRUISE FROM YOW-ATL, AT APPROXIMATELY 35,000 FT THE RIGHT WINDSHIELD SHATTERED. PRESSURIZATION REMAINED NORMAL, THE QRH WAS COMPLIED WITH AND THE AIRCRAFT DESCENDED TO 10,000 FEET. AN EMERGENCY WAS DECLARED AND THE ARICRAFT DIVERTED TO TRI, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT WINDSHIELD. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SENSOR — INOPERATIVE (BRAKE POSITION)

FLT 4783 - DURING APPROACH FROM DFW-AMA, THE CREW SELECTED THE FLAPS TO EIGHT DEGREES AND RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW ABORTED THE APPROACH TO COMPLY WITH THE QRH, PERFORMED A GO AROUND AND REQUESTED EMERGENCY VEHICLES BE ON STAND-BY. THE TOWER DECLARED AN EMERGENCY AS PRECAUTIONARY MEASURE AND THE AIRCRAFT LANDED SAFELY IN AMA. MAINTENANCE REMOVED AND REPLACED THE LEFT BRAKE POSITION SENSOR UNIT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SWITCH — INOPERATIVE (COCKPIT)

DURING CLIMB-OUT FROM ATL-MTY, AFTER ROTATION THE CREW RECEIVED STABILIZER AND MACH TRIM WARNINGS. THE CREW COMPLIED WITH THE ABNORMAL CHECKLIST WITHOUT ANY EFFECTS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS STABILIZER DISCONNECT SWITCH AND THE HORIZONTAL STABILIZER TRIM CONTROL UNIT, P/N 7060-8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ANCHOR — CRACKED (PAX DOOR)

DURING A HANGAR INSPECTION IN MCN, THE FORWARD ADN AFT ANCHORS ON THE PASSENGER DOOR WERE FOUND TO BE CRACKED. MAINTENANCE WILL MONITOR CRACK AND REPLACE ANCHORS WITHIN 100 FLIGHT HOURS PER REO 601R-52-11-272. (M)

Part: CONTROL VALVE — INOPERATIVE (APU)

FLT 4770 - DURING CRUISE FLIGHT FROM ILM-ATL, WHILE DESCENDING THROUGH 20,000 FEET AND AFTER RETARDING THE POWER TO 50 PERCENT N1, AN ODOR OF SMOKE OCCURRED IN THE COCKPIT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LOAD CONTROL VALVE IN THE AUXILIARY POWER UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ODOR — DETECTED (COCKPIT)

FLT 4769 - DURING CRUISE FLIGHT FROM ATL-ILM, WHILE DESCENDING THROUGH 19,000 FEET AND AFTER RETARDING THE POWER TO 50 PERCENT N1, A STRONG BURNING ODOR OCCURRED IN TEH COCKPIT. THE AIRCRAFT LANDED SAFELY IN ILM. MAINTENANCE INSPECTED BOTH PACKS AND HAD THE CREW OPERATE THE AIRCRAFT. NO SMOKE ODOR COULD BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ODOR — DETECTED (CABIN)

FLT 4359 - DURING CRUISE AND BEGINNING OF DESCENT INTO ATL, AFTER THE RETARDING THE POWER THE ADVANCING IT AGAIN, A METALLIC/ELECTRICAL TYPE ODOR WAS EMITTED THROUGHOUT THE AIRCRAFT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE PERFORMED HIGH POWER ENGINE RUNS, INSPECTED THE AVIONICS AND AUXILIARY POWER UNIT BAYS. NO ABNORMAL ODORS REOCCURRED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONTROL UNIT — FAULTY (TE FLAPS)

AFTER TAKEOFF, THE FLAPS DID NOT COME UP ABOVE SIX DEGREES. CAPTAIN PERFORMED APPROPRIATED CHECKLIST AND THE DECISION WAS MADE TO DIVERT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED OVERWEIGHT. MAINTENANCE COMPLIED WITH THE OVERWEIGHT LANDING INSPECTION WITH NO DEFECT NOTED. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT DUE TO INTERNAL FAILURE FAULT CODE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — BURNED OUT (FUSELAGE)

DURING GROUND INSPECTION IN ATL, THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT RIGHT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)