N317CA
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
GALLEY SERVICE DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE FOUND SERVICE DOOR UPLOCK STRURT DISCONNECTED RECONNECTED UPLOCK STRUT ASSY IAW AMM 52-41-02. CHECKED GOOD. OK FOR SVC
PAX DOOR HINGE (FUSELAGE) FOUND OVERSIZED HOLES AT HINGE LINE RESULTING IN PAX DOOR NOT ALIGNING WHEN CLOSED. REQUIRED REPLACEMENT. REPLACED PAX DOOR HINGE (DFUSELAGE) ISW SRM 53-21-23.
PAX DOOR HINGE (DOOR) DURING INSTALL PIN BECAME STUCK IN PIANO HINGE ON DOOR SIDE RESULTING IN PAX DOOR NOT ALIGNING WHEN CLOSED. REQUIRES REPLACEMNET. PN: 601R318073-5 REPLACED PAX DOOR HINGE (DOOR) IAW SRM 52-11-01
AT FL 310 AND WE WERE TOLD TO DESCEND DOWN TO 11,00. WE HAD A R ENGINE FLAME OUT AND LOST OUT R ENGINE, R FADEC FAULT AND L FADEC FAULT STATUS MESSAGE CAME ON. OUR RIGHT ENGINE LIT BACK UP. R/L FADEC FAULT STATUS MSG CAME IN AND OUT ITERMITTENTLY. AFTER WE LANDED, L/R FADEC FAULT STATUS MESSAGE IS STAYING POSTED, RUD LIMIT FAULT STATUS MSG, ALONG WITH APR CMD SET CAUTION MSG. R & R RT FADEC IAW AMM 73-21-01. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME. PERFORMED POWER ASSURANCE RUNS IAW AMM 71-00-00. NO DEFECTS NOTED AT THIS TIME.
FUEL LEAK AT LH WING SLAT TRACK CANISTER NO.3 (SLAT TRACK 1-3) WS 148.00, LH MAIN FUEL TANK FRONT SPAR. SLAT TRACK CANISTER NO.3 (SLAT TRACK 1-3) WS 148.00, LH MAIN FUEL TANK FRONT SPAR WAS REPAIRED REO 670-57-- 42-19 REV --
CORROSION ON STGR 19L BTW FS364 / FS379 (CPCP) CORROSION ON STGR 19L BTW FS364 / FS379 (CPCP) WAS EVALUATED OUT LIMITS PER CRJ 700 SRM 51-10-06-001-001-A01 THEREFORE WAS REPAIRED PER CRJ-700 SRM 53-00-03-201-001-A01
CRACK IN LH FWD FUSELAGE SKIN LOCATED IN WL 79.5 AND F.S. 189.5 AT AFT LOWER CORNER OF CUTOUT ACCESS PANEL 211AL LH FWD FUSELAGE SKIN LOCATED IN WL 79.5 AND F.S. 189.5 AT AFT LOWER CORNER OF CUTOUT ACCESS PANEL 211AL WAS REPAIRED PER REO 670-53-11-2068 REV --
CORROSION ON BEAM BTW FS 985.00/ FS 1088.00 AND LBL 27 AT AFT CARGO FLOOR STRUCTURE FLOOR BEAM BTW FS 985.00/ FS 1069.75 AND LBL 27 WAS REPAIRED PER CRJ700 SRM 53-00-41-201-001-A01 AND FLOOR BEAM LBL 27 BTW FS 1069.75/FS 1088.00 WAS INSPECTED AND NO CORROSION FOUND PER CRJ 700 SRM 51-11-00-001-001-A01
IN REF TO: AFTER SEAT RAIL REMOVAL DURING NRC: 0200, CORROSION ON FLOOR BEAM RBL 9 BTW FS= 477.00/565.00 WAS FOUND. CORROSION ON FLOOR BEAM RBL 9 BTW FS= 477.00/565.00 WAS EVALUATED PER CRJ700 SRM 53-31-43-101-001-A01 THEREFORE WAS REPAIRED PER CRJ-700 SRM 53-00-41-201-001-A01.
INITIAL INSPECTION: CORROSION ON STGR 19R BTW FS409 / FS349 (CPCP) STGR 19R BTW FS409 / FS349 WAS REPAIRED PER CRJ-700 SRM 53-00-03-201-001-A01
WEAR WAS FOUND ON BEAM FWD AND AFT AREA AT CUTOUT OF AFT BAGGAGE BAY DOOR BEAM FWD AND AFT AREA AT CUTOUT OF AFT BAGGAGE BAY DOOR WAS REPAIRED PER EA CRJ753-18112 REV. IR
CORROSION OVER STGR 20R BTW FS 295 / FS 310 CORROSION OVER STGR 20R BTW FS 295 / FS 310 WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT LIMITS PER CRJ-700 SRM 53-21-03-101-002-A01 THEREFORE STGR 20R BTW FS 295 / FS 310 WAS REPAIRED PER CRJ700 SRM 53-00-03-201-001-A01
CORROSION OVER STGR19R BTW FS295 / FS310 STGR19R BTW FS280 / FS319 WAS REPAIRED PER CRJ700 SRM 53-00-03-201-001-A01
CORROSION WAS FOUND LOCATED IN FLOOR BEAM AT RBL 9.00 BTW FS645.00/FS661.00. FLOOR BEAM AT RBL 9.00 BTW FS645.00/FS661.00 WAS REPAIRED PER CRJ-700 SRM 53-00-41-201-001-A01
CORROSION ON BEAM BTW FS 985.00/ FS 1088.00 AND RBL 27 AT AFT CARGO FLOOR STRUCTURE BEAM BTW FS 985.00/FS1056.25 & BTW FS 1070/ FS 1088.00 WAS RE-INSPECTED, NO DAMAGE WAS FOUND PER CRJ700 SRM 51-26-00-001-001-A01 AND BEAM BTW FS1056.25/FS1074.75 WAS REPAIRED PER CRJ700 SRM 53-00-41-201-0010A01
CORROSION ON STRINGER 21R BTW FS349 TO FS 364 ON INTERNAL STRUCTURE STRINGER 21R BTW FS 339.00 TO FS 379.00 ON INTERNAL STRUCTURE WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01
INSPECTED THE L/H WING AILERON BUSHING BORE AT WS 295.50 AND FOUND DAMAGE IN THE TOP CENTER OF THE INBD BUSHING BORE - REPAIRED LH AILERON BUSHING BORE AT WS 295.50 IAW MHIRJ REO 670-57-51-456 REV A DATED 2021-11-15 WVAC EMP STAMP # 776 MTC
RH AILERON FUSELAGE O/B CABLE FRAYED IN CRITICAL FATIGUE AREA CLOSE TO AFT QUADRANT - REMOVED & REPLACED RH AILERON CABLE IAW CRJ 700 AMM 27-11-00. REMOVED & REPLACED REAR RH QUADRANT IAW CRJ 700 AMM 27-11-10. RIGGING & OPS CHECK OF AILERON TRIM SYS IS GOOD IAW CRJ 700 AMM 27-11-00. QUADRANT PN OFF/ ON: BA670-9325-7 SN OFF: 2012356 SN ON:C665697 CABLE PN OFF/ ON: BA670-93210-47 NSN
RH OUTBOARD MULT-FUNCTION SPOILERS CENTER HINGE ON LEADING EDGE IS BENT - REPAIRED RH OB MFS IAW MHIRJ REO 670-57-73-048 DATED 2021-11-17 WVAC EMP STAMP # 776 MTC
F.S. 333 FRAME IS CORRODED BETWEEN STGR 25L TO STGR 26R - FOUND OUT OF LIMITS. COMPLIED WITH STEPS CRJ-700 SRM 53-00-06-201-006-(A01) DISCONNECTED & CONNECETED LOWER ATC L-BAND IAW CRJ700 AMM 34-54-01-000/400-801(A01) PERFORMED FUNCTIONAL CHECK IAW CRJ700 34-54-04-720-801(A01). WVAC EMP # 603145
CORROSION AROUND 5TH FASTENER AFT OF FS 280 ON STRINGER 22R - REPAIRED STR 22R FROM FS 280-FS310 IAW CRJ 700 SRM 53-00-03-201-001-A01
CORROSION AROUND 5TH FASTENER AFT OF FS 280 ON STGR 23R. - REPAIRED STR 23R FROM FS 280-FS 310 IAW ENDEAVOR EA CRJ 753-12420.
LOW PRESSURE GROUND CONNECTION HAS A GOUGE ON SKIN, LOWER AFT SECTION. MARKED WITH RED TAPE - COMPLIED WITH ENDEAVOR EA CRJ753-12409, REV.B DATED 11/3/21. OPS CHECK GOOD. REMOVED RED TAPE. REMOVED AND REINSTALLED COVER AND ADAPTER IAW CRJ 700 AMM 21-20-01-000/400-801-A02.
AVI DOOR INTERCOSTAL BETWEEN STGR 27 TO 26L IS CORRODED. - REMOVED AND REPLACED AVI BAY DOOR INTERCOSTAL BETWEEN STR 27 AND 26L IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
AVI DOOR INTERCOSTAL AT STGR 27 IS CORRODED - REMOVED AND REPLACED AVI DOOR INTERCOSTAL AT STR 27 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. WVAC EMP STAMP # 776 MTC
REMOVE STGR 27 AT FS 280.00 - FS 295.00 TO FACILITATE INSTALLATION OF ANTENNA DOUBLER AT FS 295.00 - FS 310.00 - REPLACED STRINGER 27 FS 280-300 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001-A01.
AFTER DAMAGE REMOVAL ON COCKPIT DOOR POST AT RBL9 AT FLOOR LEVEL. FOUND BROKEN ANGLE (P/N CC670-33199-4) - REPLACED FS 280 ANGLE AT RBL 9 PN CC670-33199-4S IAW CRJ 700 SRM 51-42-06-001-001-A01. AND GASKET PN CC670-33467-2 IAW CRJ 700 SRM 51-42-04-001-001-A01 WVAC EMP STAMP # 794 MTC
FS 333 AND STR 26L STRINGER SPLICE IS CORRODED. - LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE STRINGER SPLICE AT FS 333 STR 26L IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. WVAC EMP STAMP # 794 MTC
F.S. 280 TO F.S. 310 STGR 26R IS CORRODED - REMOVED AND REPLACED STRINGER SEGMENT AT 26R BETWEEN FS 280 AND FS 333 IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 WVAC EMP STAMP # 776 MTC
AFTER DAMAGE REMOVED ON COCKPIT DOOR POST AT LBL 9 AT FLOOR LEVEL FOUND BROKEN ANGLE (P/N: CC670-33199-3). - REPLACED ANGLE PN CC670-33199-3 AT LBL 9 FS 280 IAW CRJ700 SRM 51-42-06-001-001-A01. WVAC EMP STAMP # 794 MTC
F.S. 280 "J" ANGLE AND FLOORBOARD FASTENERS CORRODED WITH EVIDENCE OF CORROSION BETWEEN J ANGLE AND F.S. 280 CROSSBEAM. - REMOVED AND REPLACED FS 280 J ANGLE IAW CRJ700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. WVAC EMP STAMP # 776 MTC
F.S. 280 TO F.S. 295 STGR 26L IS CORRODED - REMOVED AND REPLACED STR 26L BETWEEN FS 280 AND FS 333 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 LOCATED AND DRILLED NEW SERVICEABLE STR 26L P/N SH670-31634-1S BETWEEN FS 280 AND FS 333 IAW CRJ 700 SRM 51-40-11-001-001-A01 INSTALLED NEW SERVICEABLE STRINGER 26L BETWEEN FS 280 AND FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
F.S. 280.00 CROSSBEAM HAS CORROSION ON UPPER SURFACE MULTIPLE AREAS LBL 45.0 TO RBL 45.0 - REMOVED CORROSION ON F.S. 280 CROSSBEAM IAW CRJ 700 SRM 53-00-00-101-001-A01. FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED F.S. 280 CROSSBEAM IAW REO 670-53-11-579 REV B WVAC EMP # 56399
F.S. 280.00 CROSSBEAM HAS CORROSION ON UPPER SURFACE MULTIPLE AREAS LBL 45.0 TO RBL 45.0 - REMOVED CORROSION ON F.S. 280 CROSSBEAM IAW CRJ 700 SRM 53-00-00-101-001-A01. FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED F.S. 280 CROSSBEAM IAW REO 670-53-11-579 REV B WVAC EMP # 56399
PANEL 195DL BRACKET IS CRACKED. MARKED WITH TAPE - REMOVED CRACKED CHANNEL FROM BRACKET ("T" EXTRUSION) IAW CRJ700 SRM 51-42-10-001-A01. ALODINED AND PAINTED BARE AREAS ON BRACKET IAW CRJ700 SRM 51-21-11-081-A01 AND 51-25-06-001-A01. INSTALLED C CHANNEL ONTO STRAP IAW CRJ700 SRM 51-42-10-001-001-A01. COMPLIED WITH MODSUM IS670538200021. INSTALLED STRAP ON PANEL 195DL IAW CRJ700 AMM 53-82-83-400-803-A01. COMPLIED WITH ENDEAVOR AIR EO# R53573 REV DATE 22 FEB 18. REMOVED TAPED. WVAC EMP STAMP # 703 MTC
F.S. 280.00 CROSSBEAM HAS CORROSION ON UPPER SURFACE MULTIPLE AREAS LBL 45.0 TO RBL 45.0 - REMOVED CORROSION ON F.S. 280 CROSSBEAM IAW CRJ 700 SRM 53-00-00-101-001-A01. FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED F.S. 280 CROSSBEAM IAW REO 670-53-11-579 REV B WVAC EMP # 56399
R/H AILERON BUSHING LUGS HAVE DAMAGE ON THE INNER BORE OF THE LUG - COMPLIED WITH REO STEP 1 AND 2 OF REPAIR 6 BORE OVERSIZE OF REO 670-57-61-107 REV B DATED 2019-01-14. PERFORMED LPI ON RH AILERON CENTER HINGE 4 REWORKED BORES IAW BOMBARDIER REO 670-57-61-107 REV B DATED 2019-01-14 STEP 6(3) NO INDICATIONS NOTED AT THIS TIME REF C/O 10055521 JOB 81005551 OP 296 FOR DOCUMENTATION OF WORK PERFORMED. WVAC EMP STAMP # 703 MTC
RH FLOOR SILL RBL45.0 FS 280.00 TO FS 310.00 HAS CORROSION ON UPPER SURFACE. - R/R UNSERVICEABLE FLOOR SILL (R/H FS 280 TO FS 310) WITH A SERVICEABLE SILL IAW CRJ 700 SRM 51-42-06-001-001(A01), 51-42-13-001-001(A01), AND 51-42-21-001-001(A01). WVAC EMP STAMP #722 MTC
LH MLG SIDESTAY ACTUATOR PAINT FINISH IS DAMAGED, WITH SURFACE CORROSION. - REMOVED AND REPLACED LH MLG SIDE STAY IAW CRJ700 AMM 32-11-12-000-801-A01 AND 32-11-12-400-801-A01. LEAK AND OPS CHECKS GOOD IAW CRJ700 AMM 32-30-00-710-801-A01 AND 32-00-00-790-802-A01. WVAC EMP # 587142
LATCH MECHANISM PULL IN LEVER TORQUE TUBES CORRODED AND STOP FITTING CHAFED AND PITTED. - INSTALLED NEW PAX DOOR PULL IN LEVER TORQUE TUBE AND REINSTALLED SAME SERVICEABLE PULL IN LEVERS IAW CRJ700 AMM 52-11-02-400-806-A01. OPS CHECK GOOD. /N 601R31863-1. STOP FITTING P/N 601R38923-3 REPLACED DURING TORQUE TUBE INSTALL. WVAC EMP # 88565.
LH WHEEL WELL ACCESS PANEL 542AZ IS CORRODED AROUND NUMEROUS FASTENER HOLES. - REMOVED CORROSION ON PANEL 542AZ IAW CRJ 700 SRM 51-12-00-001-001-A01. FOUND TO BE OUT OF LIMITS. REPLACED PANEL, LOCATED, DRILLED AND DEBURRED PANEL IAW SRM 51-40-11-001-001(A01) INSTALLED PANEL IAW SRM 51-41-02-001-001-A01 & AMM 57-52-32-400-814. REPLACED 4 NUTPLATES IAW SRM 51-45-00-001-001-A01. WVAC EMP # 56339.
LATCH MECHANISM PULL IN LEVER TORQUE TUBES CORRODED AND STOP FITTING CHAFED AND PITTED. - INSTALLED NEW PAX DOOR PULL IN LEVER TORQUE TUBE AND REINSTALLED SAME SERVICEABLE PULL IN LEVERS IAW CRJ700 AMM 52-11-02-400-806-A01. OPS CHECK GOOD. /N 601R31863-1. STOP FITTING P/N 601R38923-3 REPLACED DURING TORQUE TUBE INSTALL. WVAC EMP # 88565.
CLOSING PANEL FWD OF FLIGHT DECK FLOORBOARD AT FS 260 IS CORRODED - R/R UNSERVICEABLE CLOSING PANEL @ FS260 WITH SERVICEABLE PANEL IAW CRJ 700 SRM 51-42-06-001-001-A01. WVAC EMP STAMP #722 MTC
R/H AND L/H 280 BULKHEAD LOWER WEB IS CORRODED. - INSTALLED, FABRICATED, LOCATED AND DRILLED NEW LOWER RH AND LH 280 BULKHEAD WEB AND SPLICE PLATE C/W HFEC OF LH / RH 280 BULKHEAD WEBS APPLIED PAINT ON RH AND LH 280 BULKHEAD WEBS IAW CRJ 700 SRM 53-11-10-201-004-A01, 53-11-10-201-A01 NOTE (YYY), 51-25-16-001-001-A01. NO INDICATIONS NOTED AT THIS TIME. WVAC EMP STAMP # 780 MTC.
FLIGHT DECK FLOOR BOARD SUPPORT ANGLE AT RBL18 AND LBL18 ARE CORRODED. - LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE RH AND LH FLIGHT DECK FLOORBOARD SUPPORT ANGLES AND GUSSETS IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. WVAC EMP # 85534
FS 280.00 FWD J-ANGLE IS CORRODED. - R/R/ UNSERVICEABLE "J" ANGLE WITH A SERVICEABLE ANGLE IAW MHIRJ REO 670-53-11-579 REV B. WVAC EMP STAMP #722 MTC
P/N: SH670-32075-4/SH670-32075-3. AVIONICS BAY DOOR SURROUND STRUCTURE, 2 EACH INTERCOSTALS LBL2 & RBL2 FORWARD OF DOOR STRUCTURE, CORRODED, FS349.00-FS364.00. - R/R UNSERVICEABLE L/H & R/H STRINGER 27 INTERCOSTALS WITH SERVICEABLE INTERCOSTALS IAW CRJ 700 SRM 51-42-06-001-001(A01) 51-40-11-001-001-(A01) AND 51-42-21-001-001(A01). WVAC EMP STAMP #722 MTC
SERVICE DOOR SEAL STRIKER HAS AN AREA OF CORROSION ON INNER SURFACE AND (3) ELONGATED HOLES WHERE STEP PLATE ATTACHES. - REMOVED SERVICE DOOR SILL STRIKER AND L ANGLE FWD OF IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. REMOVED AND INSTALLED SERVICE DOOR L ANGLE. IAW CRJ700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. REMOVED AND INSTALLED 2 EA LATCH FITTINGS IAW CRJ 700 AMM 53-21-27-000/400-802. REMOVED 4 SERVICED DOOR FITTINGS IAW CRJ 700 SRM 51-42-06-001-001-A01. INSTALLED SILL STRIKER IAW CRJ 700 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01. WVAC EMP STAMP # 722 MTC.
LH IB FLAP VANE LEADING EDGE SKIN IS CHAFED AT 3 LOCATIONS WHERE VANE CONTACTS WING TRAILING EDGE STRUCTURE. - REMOVED DAMAGE AREA ON L/H I/B FIXED LEADING EDGE FLAP VANE IAW CRJ 700 SRM 51-12-00-001-001-A01. FOUND TO BE WITHIN LIMITS. RESTORED SURFACE WITH SAME REFERENCE. REPLACED PANEL 584GT IAW SRM 51-40-11-001-001-A01 & 51-25-01-001-001-A01. REFER TO JOB 81005551 OP 77 FOR REPAIR OF PANEL 584HT. WVAC EMP # 56399
PAX DOOR INTERCOSTAL AT DD6 CORRODED. - REMOVED & REINSTALLED FORMER AT FS 329.41 BETWEEN DD5 AND DD6 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REMOVED AND REPLACED INTERCOSTAL AT DD6 IAW SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01. WVAC EMP #56399
RH MLG SIDESTAY ACTUATOR PAINT FINISH IS DAMAGED WITH SURFACE CORROSION. - REMOVED AND REPLACED RH MLG SIDE STAY IAW CRJ700 AMM 32-11-12-000-801-A01 AND 32-11-12-400-801-A01. LEAK AND OPS CHECKS GOOD IAW CRJ700 AMM'S 32-30-00-710-801-A01 AND 32-00-00-790-802-A01. WVAC EMP # 587142.
PAX DOOR FRAME AT FS327-763 BETWEEN DD6 AND DD7. LIGHTENING HOLE GOUGED AND DEFORMED. - REMOVED & REPLACED FRAME AT FS 327.763 BETWEEN DD6 & DD7 IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. REMOVED & REPLACED INNER COSTAL DD7 IAW SRM SAME REFERENCES
PAX DOOR FRAME AT FS327-763 BETWEEN DD6 AND DD7. LIGHTENING HOLE GOUGED AND DEFORMED. - REMOVED & REPLACED FRAME AT FS 327.763 BETWEEN DD6 & DD7 IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. REMOVED & REPLACED INNER COSTAL DD7 IAW SRM SAME REFERENCES
TWO FORWARD EMERGENCY CEILING LIGHT BULBS INOP. REMOVED AND REPLACED BOTH CEILING LIGHT BULBS, IAW CRJ 700 AMM 33-51-09. PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS, IAW CRJ 700 AMM 33-51-00. OPS CHECK GOOD. P/N:OFF/ON 1317 (X2).
PASSENGER DOOR AFT CAM FITTING CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED PASSENGER DOOR AFT CAM FITTING IAW SRM 51-42-21, 51-40-11, 51-21-11 AND 51-25-06
LT SIDE SEAT RAIL AT FRAME STATION 708.00 HAVE SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED LT SIDE SEAT RAIL AT FS 708.00 IAW SRM 51-41-02.
PAX DOOR INNER SKIN IS CORRODED. REMOVED AND REPLACED THE DOOR INNER SKIN IAW SRM 51-42-06, 51-42-12, 51-42-21, 51-42-22, 51-42-02, AND REO 670-52-11-1010.
PAX DOOR INNER STRUCTURE FORMER UNDER PANEL 832FL WAS CORRODED. REMOVED AND REPLACED THE FORMER IAW SRM 51-42-06, AND 51-42-21.
PASSENGER DOOR INNER SKIN IS CRACKED AT FASTNER HOLE FOR ACCESS PANEL 832DL. REMOVED AND REPLACED SKIN IAW SRM 51-42-22, 51-42-06, 51-41-02, 51-40-11, AMM 52-11-02, 52-11-13, 52-11-05, 52-11-07, 52-11-00 AND REO 670-52-11-1008.
PASSENGER DOOR INTERNAL STRUCTURE INTERCOSTAL DAMAGED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21.
PASSENGER DOOR VENT PANEL SURROUND STRUCTURE AFT ANGLE CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06.
PASSENGER DOOR POWER ASSIST MOTOR MOUNT BRACKET CRACKED. REMOVED AND REPLACED THE MOUNT BRACKET IAW SRM 51-42-06, AND 51-42-13.
PASSENGER DOOR VENT PANEL HINGE FWD ROD ATTACH FITTING IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED FLAP VENT ASSY IAW CRJ 700 AMM 52-11-15 AND CRJ 700 SRM 51-42-21.
STRINGER 25R HAS SIGNS OF CORROSION FROM BS 319 TO 333. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06, 51-26-00, 53-21-03, 51-41-02, 51-42-21, 53-00-03, 51-21-11, 51-25-06, 51-25-16, 51-40-11, 53-00-06, REO 670-53-21-1508 P1, AND NDTM PART01 51-20-006-250.
STRINGER 27 IS CORRODED BETWEEN BS 280 AND 295. REMOVED AND REPLACED THE STRINGER IAW SRM 51-25-00, 51-21-11, 51-25-16, 51-40-11, 51-26-00, 515-23-03, AND AMM 34-43-03.
STRINGER 26R IS CORRODED BETWEEN BS 310 AND 319. REMOVED AND REPLACED THE STRINGER IAW SRM 51-21-03, 51-42-06, 51-42-20, 51-40-11, 51-21-11, AND 51-25-16.
STRINGER 26L IS CORRODED BETWEEN BS 280 AND 295. REMOVED AND REPLACED THE STRINGER IAW SRM 51-25-00, 51-21-11, 51-25-16, 51-40-11, 51-26-00, 515-23-03, AND AMM 34-43-03.
PAX DOOR SURROUND MID CAP HAS SIGNS OF CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED IAW SRM 51-42-01.
FWD CARGO, CARGO TRACK HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 51-42-06, 51-42-21, 51-25-06, 51-25-16, AND 51-21-11.
LEFT OUTBOARD FLAP ARE DENTED. DRESSED THE DENT AND REMOVED AND REPLACE THE RIB AND INTERCOSTAL IAW REO 670-57-53-206, SRM 57-53-01, 51-42-06, 51-42-13, 51-26-01, 51-40-11, 51-25-06, 51-25-16, AND NDT MANUAL PART 1 51-20-008.
PASSENGER DOOR KICK ANGLE HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE KICK ANGLE IAW SRM 51-42-06.
INTERCOSTAL AT STRINGER 20R FROM BS 319.70 TO 349 HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 53-21-23, 51-42-06, 51-42-21, 51-40-11, 51-21-11, AND 51-25-16.
RIGHT FLOOR SUPPORT BS 280 TO 319.7 IS CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-21-11, 51-25-16, 51-42-06, 51-42-21, 51-42-13, 51-26-00, AND AMM 20-70-00.
LEFT BS 280 BULHEAD WEB IS CORRODED. REMOVED THE CORRODED AREA, FABRICATED AND INSTALLED A REPAIR IAW SRM 51-42-06, 51-42-13, 53-11-10, AND AMM 20-70-00.
BS 280 BULKHEAD STIFFFENER FOUND CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-42-06, AND 51-42-13.
RIGHT BS 280 WEB IS CORRODED. REMOVED CORRODED AREA, FABRICATED AND INSTALLED A REPAIR IAW SRM 51-42-06, 51-42-13, 53-11-10, AND AMM 20-70-00.
LT WING I/B FLAP BOTTOM SURFACE HAS A DENT. REPAIRED DENT ON LT WING IB FLAP BOTTOM SURFACE IAW SRM 57-52-01.
RIGHT SLAT TRACK 1-3 HOUSING BRACKET CRACKED. REPAIRED THE SLAT TRACK HOUSING IAW REO 670-57-42-577, REV.
FWD CARGO DOOR INNER SEAL RETAINER IS DENTED IN 1 PLACE ON THE IB SECTION. REMOVED AND REPLACED FWD CARGO DOOR INNER SEAL RETAINER IAW AMM 52-35-07.
AFT CARGO DOOR UPPER REPAIR DOUBLER GOUGED. REMOVED THE DAMAGED REPAIR DOUBLER, FABRICATED AND INSTALLED A NEW REPAIR DOUBLER IAW REO 670-52-31-076, NDTM PART 1 51-20-006, AND SRM 51-42-21.
WATER LINE BRACKET IN THE AFT EQUIPMENT BAY AT STRINGER 7R, BS 1150 IS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-21.
STRINGER 7R AT BS 1150 IS GOUGED. REPAIRED THE STRINGER IAW REO 670-53-61-292, REV E, NDTM, PART 1, 51-20-006, AND 51-20-008.
LT WING SLAT 1-3 TRACK HOUSING CRACKED. REPAIRED LT WING SLAT 1-3 TRACK HOUSING IAW REO 670-57-42-577 REV 2016-12-02.
LT AND RT CENTER SEAT RAILS FROM FS 485 TO 581 AND FS 581 TO 677 HAVE SIGNS OF CORROSION (4 TRACKS). REMOVED AND REPLACED LT AND RT CENTER SEAT RAILS FROM FS 485 TO 581 AND FS 581 TO 677 IAW REO 670-53-00-343 REV M DATED 2015-10-19 AND AMM 53-00-49.
RT CENTER SEAT RAIL FS 349-485 HAS SIGNS OF CORROSION. REMOVED AND REPLACED RT CENTER SEAT RAIL AT FS 349-485 IAW AMM 53-00-49 AND REO 670-53-00-013 REV J, 2014/10/22.
FLOOR CROSSBEAM AT FS 333 CORRODED JUST RIGHT OF A/C CENTERLINE. REPAIRED CORRODED CROSSBEAM AT FS 333 IAW REO 670-53-21-1503, DATED 2018-03-15.
TWO SIDE SEAT RAILS CORRODED LT AND RT RAILS AT FS 565-669.4. REMOVED AND REPLACED RT AND LT SIDE SEAT RAILS AT FS 565-779 IAW AMM 53-00-49.
EMERGENCY ROPE COVER IS LOOSE. REMOVED AND REPLACED VELCRO TAPE ON ROPE COVER ON EMERGENCY EXIT IAW AMM 51-22-61.
EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW AMM 33-51-17. OPS CHECKED GOOD. NO FUTHER DEFECTS NOTED.
JAMMED PAX DOOR, CLOSED POSITION WITH PAX. PERFORMED GVI OF ACFT & ENSURED PAX DOOR CLOSED & LOCKED. ACFT SAFE FOR A ONE TIME FERRY.
EMERGENCY EXIT LIGHTS INOPERATIVE AFT OF FIRST CLASS. DEFERRED EMER EXIT LIGHTS IAW MEL 33-51-01A CAT A.
PASSENGER DOOR LATCH CAUTION MSG. FOUND DEBRIS ON PROXIMITY SWITCH, CLEANED PROXIMITY SWITCH IAW AMM 52-70-04. OPERATIONS CHECKED GOOD.
FLOOR SUPPORT CORRODED BETWEEN BS 1031-1051, LBL 9, WL 72.5. CORROSION BEYOND ALLOWABLE LIMITS.
LEFT AFT COWLING TIE BAR ATTACH BRACKETS ARE BROKEN. REPLACED LT AFT COWLING TIE BAR BRACKETS 2 IAW SRM 51-42-06 & 51-40-11.
FUSELAGE FRAME BS 333 IS CRACKED, BETWEEN STRINGER 1R & 2R. CUT AWAY DAMAGED FRAME, FABRICATED & INSTALLED NEW REPAIR PARTS IAW REO 670-53-21-1272 REV A. NDT PERFORMED.
PASSENGER DOOR PIANO HINGE LUG IS CRACKED ON FWD END. R & R PAXS DOOR PIANO HINGE IAW SRM 52-11-01, 51-25-16, 51-42-13 & 51-52-06.
FORWARD BAGGAGE BAY FUSELAGE AT FS 565.00 & 16L IS CORRODED. REMOVED DAMAGED AREA OF FRAME & INSTALLED NEW FRAME SECTION, PN SH670-33111-7, IAW REO 670-53-31-361 DATED 29 FEB 2016. NDT PERFORMED DATED 03 MAR 2016.
LEFT MLG INBD DOOR IS CRACKED AT FWD FRAME. R & R LT MLG INBD DOOR, PN KBA670-10500-27, SN 10079, IAW AMM 32-12-01.
PITCH DISCONNECT & ALTERNATE EXTENSION HANDLES MISSING ILLUMINATING PLACARDS. INSTALLED PLACARDS, 604-51878-1, 604-51878-3, & 604-51878-7, ON HANDLES IAW AMM 20-60-04.
FLOORBOARD SUPPORT IN AVIONICS BAT AR FS 280.00 IS CORRODED. R & R FLOORBOARD SUPPORT ANGLE AT FS 280.00 IAW SRM 51-42-06 & 51-25-16.
BURNING WIRE SMELL COMING FROM PAX DOOR AREA. TROUBLE SHOT WIRING & FOUND WIRES TCE4418WB LEADING TO PX27 & TCE4419WB LEADING TO PX EITH BURN MARK. WIRE REPAIR CARRIED OUT IAW ELEC WIRE REPAIR MANUAL 20-30-00. PERFORMED DOOR INDICATION CHECK IAW AMM 52-70-04. NO FURTHER DEFECTS NOTED.
WHILE PERFORMING SB 670BA-53-044, FOUND LT SIDE CAP ANGLE AT FS 202, BETWEEN STR 13L AND 14L TO BE GOUGED ON AFT SIDE NEAR RADIUS .27"L X .070"W X .040"D.
EMERGENCY LIGHT NEAR ROW 1 INOPERATIVE. DEFERRED EMER LIGHT NEAR ROW 1 IAW MEL 33-51-01B.
EMERGENCY LIGHTS STAY ON, TWO IN FIRST CLASS & TWO AT THE OVERWING EXIT.
UNABLE TO OPEN MAIN PAX DOOR. CLEANED & LUBED PAX DOOR AS REQUIRED. PERFORMED OPERATIONS CHECK OF PAX DOOR IAW AM 52-11-00. OPERATIONS CHECKED GOOD.
EMERGENCY COCKPIT HATCH LEAKING WATER. CLEANED & LUBED HATCH SEAL IAW AMM 12-20-52, NO LEAKS.
RIGHT OVERWING EMER EXIT LAMP OUT. RELAMPED RT OVERWING EMER EXIT LIGHT IAW AMM 33-51-05. OPERATIONS CHECKED GOOD.
EMERGENCY EXIT LIGHT BULBS BURNT OUT. R & R PAX & GALLEY DOOR EMER LIGHTS BULBS IAW AMM 33-51-05. OPERATIONS CHECKED GOOD.
SERVICE DOOR DOES NOT CLOSE PROPERLY. REPOSITIONED SERVICE DOOR PIN IAW AMM 52-11-00. OPERATIONS CHECKED GOOD.
PASSENGER DOOR SUPPORT WHEEL FAILED TO DEPLOY WHEN DOOR OPENED & HIT THE GND. PERFORMED INSPECTION & OPERATIONS CHECK OF PAX DOOR SUPPORT WHEEL IAW AMM 52-11-13. PERFORMED EXTERNAL INSPECTION & OPERATIONS CHECK OF PAX DOOR IAW AMM 52-11-00. ALL OPERATIONS CHECKED GOOD AT THIS TIME.
UNABLE TO CLOSE PAX DOOR. CLEANED & LUBED LINKAGE, CYCLED DOOR 5 CYCLES, OPERATIONS CHECKED GOOD IAW AMM 52-11-02.
MAIN CABIN DOOR ASSIST MOTOR STOPS ABOUT 3/4 WAY DOWN. DEFERRED PAX DOOR POWER ASSIST MOTOR IAW MEL 52-11-01A CAT C.
PASSENGER DOOR ASSIST CABLE BROKEN. DIFFERED PAX DOOR ASSIST CABLE IAW MEL 52-11-01A. ON 2/19/15 R & R DOOR ASSIST CABLE IAW AMM 52-11-08.
EMERGENCY LIGHT BULBS INOPERATIVE AT ROW 12A. RELAMPED LOWER EMER LIGHT AT SEAT 12A IAW AMM 33-51-05. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.
CABIN ALTIMETER CAUTION MSG. R & R SAFETY VLV IAW AMM 21-32-03. OPERATIONS CHECKED GOOD.
MAIN PAX DOOR MOTOR INTERMITTENT. PERFORMED OPERATIONS CHECK OF PAX DOOR FOR TROUBLESHOOTING IAW AMM 52-11-00, OPERATIONS CHECKED GOOD AT THIS TIME.
PASSENGER DOOR EMER FLOODLIGHT BULBS INOPERATIVE. R & R BULBS IAW AMM 33-51-05, OPERATIONS CHECKED GOOD AT THIS TIME.
LEFT BLEED DUCT CAUTION MSG. INSPECTED DUCT MON SYS IAW AMM 36-21-00, OPERATIONS CHECK GOOD. INSPECTED BLEED SYS & PERFORMED OPERATIONS CHECK OF THE LT BLEED SYS IAW AMM 36-10-00, OPERATIONS & LEAK CHECK GOOD. FOUND BAD APU BLEED COVER COUPLING. R & R COVER IAW AMM 36-19-01.
SMOKE SMELL IN THE CABIN & COCKPIT. INSPECTED & FOUND RT ACM AS CAUSE OF SMOKE. DEFERRED RT PACK IAW MEL 21-51-01A CAT C.
LEFT BLEED DUCT WARNING IN FLIGHT. INSPECTED & FOUND BLEED LOOP AY MT141B & 142B TO BE TOUCHING. REPOSITIONED LOOPS IAW AMM 36-21-01. RAN EVENT LOCATIONS & FOUND NO DEFECTS AT THIS TIME. OPERATIONS CHECKED GOOD AT THIS TIME.
PASSENGER DOOR CABLE FRAYED. DEFERRED PAX DOOR POWER ASSIST SYS IAW MEL 52-11-01A CAT C.
FORWARD EMERGENCY LIGHTS INOPERATIVE. R & R NR 1, 2 & 3 EMERGENCY LIGHT BATTERIES IAW AMM 33-51-17.
ESCAPE HATCH LEAKS WATER. REMOVED HATCH, CLEANED SEAL IAW CRJ700 AMM 12-20-52. RE-INSTALLED HATCH IAW CRJ700 AMM 12-20-52, NO WATER LEAKS AT THIS TIME, OK FOR SERVICE.
GALLEY SERVICE DOOR MOUNTING ANGLE CORRODED. R & R GALLEY SERVICE DOOR MOUNTING ANGLE PN SH670-31996-3 IAW CRJ700 SRM 51-42-06 & CRJ700 AMM 20-70-00.
PASSENGER DOOR LOWER STAIR PANEL HINGE ASSEMBLY CRACKED. R & R PAX DOOR LOWER STAIR PANEL HINGE ASSEMBLY PN 601R31980-65 IAW CRJ 700 AMM 52-11-04.
SERVICE DOOR CONVOLEX TUBING CHAFFED & TORN. R & R CONVOLEX TUBING PN HCTE-0312-0 & APPLIED NEW HEAT SHRINK, PN RNF100-3-4BLK IAW REO 670-20-12-045.
PASSENGER DOOR LATCH CAUTION MSG. PERFORMED PAX DOOR WARNING SYS OPERATIONS CHECKED IAW CRJ700 AMM 52-70-04, OPERATIONS CHECKED GOOD.
PASSENGER DOOR LATCH CAUTION INTERMITTENT IN FLIGHT. PERFORMED OPERATIONS CHECK OF DOOR IAW CRJ700 AMM 52-70-04, OPERATIONS CHECKED GOOD AT THIS TIME, NO FAULTS DETECTED.
COCKPIT FLOOR PANEL 1/4 TURN ANGLE AT FS 280 BEAM CORRODED. REPLACED 1/4 TURN ANGLE AT FS 280.00 BEAM, PN CL670-33292-13 IAW CRJ700 SRM 51-42-06 & 51-42-13.
GALLEY 1 HAS THREE CORRODED FLOOR FITTINGS. REPLACED THREE CORRODED GALLEY FLOOR FITTINGS PN`S 9331091-3, CDSP 2019-7C760 & A661091-1 IAW C & D ZODIAC CMM 25-33-42.
LEFT OVERWING EMERGENCY EXIT PRESS SEAL IMPROPERLY INSTALLED. R & R LT OVERWING EMERGENCY SEAL WITH NEW IAW CRJ 700 AMM 52-21-07.
FUSELAGE GOUGED AT FS 981.00, STRINGER 27. REMOVED DAMAGED SECTIONS, FABRICATED REPAIR PARTS & INSTALLED IAW REO 670-53-00-290 REV C.
LINTEL AT STRINGER 3 & FS 285 CRACKED. REMOVED DAMAGED PORTION, PERFORMED NDT, FABRICATED NEW ANGLES & INSTALLED NEW PARTS IAW REO 670-53-21-493 REV C.
RIGHT HAND FS 280 - 319.7 SILL CORRODED. REMOVED DAMAGED SILL & ORIGINAL DOUBLER, INSTALLED NEW SILL & ORIGINAL DOUBLER IAW CRJ 700 SRM 51-42-13, 51-21-01, 51-25-16, 51-21-11, 51-40-11 & CRJ 700 AMM 20-70-00.
TRU NR 2 0VERHEATED. R & R NR 2 TRU IAW CRJ 700 AMM 34-31-01, OPERATIONS CHECKED GOOD.
FS 280.00 BEAM CORRODED. R & R FS 280.00 BEAM WITH NEW PN CC670-34175-7S IAW SRM 53-11-41, 51-21-11, 51-21-16, 51-24-36, 51-42-13, 51-42-22, 51-42-02, 51-42-21, 51-42-06 & AMM 20-70-00.
FRAME AT FS 1036.00 AT LBL 26 CORRODED. REMOVED CORRODED SECTION OF BEAM FROM FS 994.00 - 1037.00 AT LBL 27, FABRICATED REPAIR PARTS & INSTALLED IAW REO 670-53-00-029 REV A DATED 2010-08-31.
INTERCOSTAL AT STRINGER 27, NR 3 POSITION CORRODED. R & R INTERCOSTAL AT STRINGER 27, NR 3 POSITION WITH NEW PN SH670-3075-3 IAW SRM 51-42-06, 51-21-11, 51-40-11, 51-23-00, 51-21-16, 51-42-13, 51-42-21 & AMM 20-70-00.
INTERCOSTAL AT STRINGER 27, NR 2 POSITION, AT FS 364.00 CORRODED. R & R INTERCOSTAL AT STRINGER 27, NR 2 POSITION AT FS 364.00 WITH NEW PN SH670-32075-4 CRJ 700 SRM 51-42-06, 51-21-11, 51-40-11, 51-23-00, 51-21-16, 51-42-13, 51-42-21 & CRJ AMM 20-70-00.
RIGHT STATION 280.00 LOWER BULKHEAD WEB CORRODED. REMOVED LOWER WEB, FABRICATED & INSTALLED NEW WEB PN CC670-34170 IAW REO 670-53-11-594 REV 2011 04 27.
LEFT STATION 280.00 LOWER BULKHEAD WEB CORRODED. REMOVED LOWER WEB, FABRICATED & INSTALLED NEW WEB PN CC670-34170 IAW REO 670-53-11-594 REV 2011 04 27.
PASSENGER DOOR FWD CAP ANGLE CORRODED. R & R FWD CAP ANGLE PN SH670-31821-5 IAW CRJ700 SRM 51-42-06, 51-40-11, & AMM 20-70-00.
PASSENGER DOOR FWD CLOSING FITTING CORRODED. R & R CLOSING FITTING PN SH670-31840-3 IAW CRJ700 SRM 51-40-11, 51-45-00, 51-42-21, 51-42-06, & AMM 20-70-00.
AFT QUARTER TURN ANGLE AT FS 280.00 CORRODED. R & R AFT QUARTER TURN ANGLE PN CC670-33292-13S IAW CRJ700 SRM 51-42-06 & 51-42-21.
PASSENGER DOOR MID CAP ANGLE CORRODED. R & R ANGLE IAW SRM 51-41-02, 51-40-11, 51-25-06, 51-45-00, & AMM 51-21-01 20-70-00.
AFT CARGO DOOR SILL CORRODED. REPLACED AFT CARGO DOOR SILL WITH NEW PN MM670-35655-003 IAW SRM 51-42-06, 51-42-13, 51-42-21, 51-23-00, 51-21-11, 51-40-11, 51-41-00, 51-25-16 & AMM 20-70-00.
LEFT POST AT FS 279.00 LBL 11 CORRODED. REPAIRED LT POST AT FS 279.00 LBL 11 BY REMOVING CORRODED AREA, FABRICATING REPAIR PARTS & INSTALLING IAW REO 670-53-11-745 DATED 2012-09-08.
SERVICE DOOR SEAL STRIKER CORRODED. R & R SEAL STRIKER WITH NEW PN SH670-31412-7 IAW CRJ700 SRM 51-42-06 & CRJ700 AMM 20-70-00.
PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE BY REMOVING DAMAGED AREA, FABRICATING REPAIR PARTS & INSTALLING IAW REO 670-52-11-072 REV E DATED 2009-10-26.
ATTACHMENT ANGLE AT STRINGER 26R CORRODED. R & R ATTACHMENT ANGLE IAW CRJ 700 SRM 51-42-06 & 51-42-13. AVMAX WORK ORDER 80201 & WORK CARD 1095.
CORROSION FOUND ON MAIN PAX DOOR LOWER PUSH ROD ASSEMBLY. REMOVED LOWER PUSH ROD BOLT. CLEANED AFFECTED AREA IAW AMM 51-26-00, NO FURTHER DAMAGE FOUND. REINSTALLED LOWER PUSH ROD BOLT IAW CRJ 700 AMM 52-11-02.
TWO DAMAGED RIVETS, ONE FWD OF LOWER STEP & ONE AFT OF LOWER STEP ON MAIN PAX DOOR. R & R TWO RIVETS IAW SRM 51-42-10..
EMERGENCY EXIT LIGHT LENS ON RT SIDE IS BROKEN. DEFERRED RT FWD EMERGENCY EXIT LIGHT LENS IAW CRJ700 CDL 33-50.
OTBD SPOILERS & OTBD SPOILERON CAUTION MESSAGE. PILOT PERFORMED SOP RESET PROCEDURE. NO MESSAGES AT THIS TIME.
LEFT ENGINE BLEED MASTER CAUTION LIGHT. R & R NR 1 PACK COMPRESSOR DISCHARGE PIPE ASSEMBLY IAW AMM 21-51-06 AND 21-51-08, OP'S AND LEAK CHECK CHECK GOOD AT THIS TIME.
RT BLEED DUCT WARNING MESSAGE AT 13000 FT. R & R RT 10TH STAGE HIGH PRESSURE SHUTOFF VALVE IAW AMM 36-12-05. OPS AND LEAK CHECK GOOD AT THIS TIME.
PAX DOOR OUTER HANDLE CAUTION.
PAX DOOR OUTER HANDLE CAUTION MESSAGE. PERFORMED OP'S TEST OF DOOR WARNING SYS IAW AMM 52-70-00. OP'S CHECKED GOOD AT THIS TIME.
NOSE DOOR OPEN WARNING MESSAGE AND PROXIMITY SYS NR 1 AFTER TAKEOFF. ADJUSTED PROXIMITY SENSOR TO CORRECT RANGE AND OPS CHECK GOOD IAW AMM 32-61-05.
PAX DOOR OUTER HANDLE CAUTION MESSAGE. PERFORMED OP'S CHECK OF PAX DOOR IAW AMM 52-11-00, OP'S CHECKED GOOD, NO DEFECTS AT THIS TIME.
LEFT BLEED DUCT MASTER WARNING MESSAGE IN FLIGHT. INSPECTED BLEED AIR LOOP, NO DEFECTS NOTED. INSPECTED LT SIDE BLEED AIR DUCT IN SAME AREA, NO DEFECTS NOTED IAW AMM 63-21-00.
GROUNDING CABLE ON PAX DOOR BROKEN. R & R CABLE ASSY IAW AMM 52-11-15, OP'S CHECK GOOD AT THIS TIME.
EMRERGENCY LIGHTS WILL NOT REMAIN ILLUMINATED.
EMERGENCY LIGHTS WILL NOT REMAIN ILLUMINATED.
EMERGENCY LIGHTS WILL NOT REMAIN ON. R & R NR 2 BATTERY CHARGER IAW AMM 33-51-17. OP'S CHECKED GOOD ON GROUND IAW AMM 33-51-00.
EMERGENCY LIGHTS WILL NOT REMAIN ILLUMINATED.
EMERGENCY OVERHEAD LIGHT BURNED OUT AT ROW 9. REPLACED LAMP EMERGENCY LIGHT ROW 9 IAW 33-51-09, OP'S CHECKED GOOD.
PAX DOOR STEP HAS LOOSE HARWARE. TORQUED PAX DOOR STEP HARDWARE IAW AMM 20-21-00.
PAX DOOR BONDING STRAP BROKEN. R & R PAX DOOR BONDING STRAP IAW AMM 51-80-00.
PAX DOOR AFT RAIL PIN IS DAMAGED. R & R PAX DOOR AFT RAIL PIN IAW AMM 52-11-27.
PAX DOOR "OPEN" PLACARD WORN. REMOVED DAMAGED PLACARD, REPLACED WITH SERVICABLE PLACARD IAW AMM 20-60-04.
WATER DRIPPING FROM THE EMERGENCY EXIT HATCH IN THE COCKPIT. REMOVED HATCH, CLEANED DEBRIS FROM SEAL, REINSTALLED HATCH IAW AMM 52-22-00.
PAX DOOR POWER ASSIST CABLE CAME OFF THE PULLEY. FOUND MIDDLE CABLE ON PAX DOOR OFF OF PULLEY, RESECURED CABLE, IAW AMM 52-10-01, OP'S CHECK GOOD AT THIS TIME.
RIGHT FADEC MESSAGE ON TAKE OFF ROLL. REMOVED & REPLACED NR 2 ENGINE FMU PER AMM. OP'S CHECKED GOOD AT THIS TIME.
TWO OF FIVE BULBS INOPERATIVE IN EXIT SIGN, ROW 12 SEATS A & C RT. PERFORMED OPS CHECK OF OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD.
LT OVERWING EXIT PULL HANDLE COVER MISSING THE LENS. DEFERED TO NEF 25-100-6, NEF CONTROL 12587, CAT 5.
RT AFT EXTERIOR EMERGENCY EXIT LENS CRACKED. R & R RT AFT EXTERIOR EMERGENCY EXIT LENS IAW AMM 33-51-15.
PAX DOOR ASSIST CABLE ENDS AT SURROND AREA MISSING RUBBER CAPS. INSTALLED HEAT SHRINK RUBBER CAPS ON DOOR ASSIST CABLE ENDS IAW AMM 52-11-00.
AFT INTERIOR SERVICE DOOR EMERGENCY EXIT LENS CRACKED. R & R INTERIOR SERVICE DOOR EMERGENCY EXIT LENS IAW AMM 33-51-05.
FORWARD INTERIOR SERVICE DOOR EMERGENCY EXIT LENS CRACKED. R & R FORWARD INTERIOR SERVICE DOOR EMERGENCY EXIT LENS IAW IAW AMM 33-51-15.
LEFT FORWARD EXTERIOR EMERGENCY EXIT LENS CRACKED. R & R LT FORWARD EXTERIOR EMERGENCY EXIT LENS IAW AMM 33-51-15.
RIGHT FORWARD EXTERIOR EMERGENCY EXIT LENS NEEDS TO BE INDEXED PROPERLY. INDEXED RT FORWARD EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-15.
RT BS 280 WEB CORRODED JUST ABOVE FLOOR LEVEL. COMPLIED WITH REO 670-53-11-59401 AND REO 670-53-594 REV.
LT 280 CROSSBEAM WEB CORRODED. COMPLY WITH REO 670-53-11-594.
DENTS IN FUSELAGE SKIN FS 193 - 202 S15-16L. REPAIRED IAW REO 670-53-11-671.
FS 280 CROSSBEAM CORRODED. COMPLY WITH REO 670-53-11-047.
STRINGER 7 RT IS CHAFED AT FS 1158. BLENDED DAMAGE. DAMAGE WITHIN LIMITS OF REO 670-53-61-292, REPAIR B, STEP 1.
INTERCOSTAL & STRINGER 9R CHAFED. BLENDED DAMAGE TO SMOOTH CONTOUR IAW REO 670-53-61-292 REPAIR A STEPS 1-3. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PROCEDURE UT-3. MIN MATERIAL REMAINING IS .055", ORIGINAL IS .071" MATERIAL. REMOVED IS .046" WITHIN ALLOWABLE LIMITS IAW REO 670-53-61-292.
AVIONICS BAY FLOOR SUPPORT CHANNEL CORRODED. REMOVED CORRODED FLOOR SUPPORT CHANNEL IAW SRM 51-42-06-001-001. LOCATED AND DRILLED NEW SUPPORT CHANNEL IAW SRM 51-40-11-001-001. INSTALLED NEW FLOOR SUPPORT CHANNEL IAW SRM 51-42-06-001-001. REPAIR CLASSIFIED AS A MINOR.
REMOVED COCKPIT FLOORBEAM IAW SRM 51-42-06-001-001-, 51-42-21-001-001, 51-42-22-001-001. INSTALLED COCKPIT FLOORBEAM ANGLE AT IAW SRM 51-42-06-001-001, 51-42-21-001-001 AND 51-42-22-001-001.
RIGHT NUTPLATE CHANNEL ON AFT CARGO BAY SILL CORRODED AT APPROX FS 1031 TO FS 1088.20. REMOVE CORROSION IAW SRM 51-21-001-001-A01. REPAIR CLASSIFIED AS MINOR.
RT 280 WEB CORRODED JUST ABOVE FLOOR LEVEL. BLENDED CORROSION IAW SRM 51-21-06-001-001 AND 53-11-10-201-003. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRED IAW REO 670-53-11-594.
FS 280 FLOORBEAM CORRODED. R & R FLOORBEAM IAW SRM 51-42-06, 51-42-13, 51-42-21 & REO 670-53-11-047.
AFT CARGO TRACK AT LBL 9.00 HAS CORROSION AROUND SCREW HOLES. REMOVED CARGO TRACK IAW AMM 53-00-49-000-8001. INSTALLED SERVICEABLE CARGO TRACK IAW AMM 53-00-49-400-801.
CARGO TRACK AT RBL 27, FS 1000.00 CORRODED AROUND SCREW HOLES AFT CAGRO BAY. REMOVED CARGO TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICEABLE CARGO TRACK IAW AMM 53-00-49-400-801.
CARGO TRACK AT RBL 9, FS 1000.00 CORRODED AROUND SCREW HOLES AFT CARGO BAY. REMOVED CARGO TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICEABLE CARGO TRACK IAW AMM 53-00-49-400-801.
IN FWD CARGO BAY AT BS 533 LBL 2.5 THE MACHINE BRACKET IS CORRODED. NO CORROSION FOUND ON MACHINE BRACKET AT ST533, LBL2.6.
IN FWD CARGO BAY AT FS 581, LBL 2.6, BRACKET CORRODED. R & R BRACKET IAW SRM 51-40-11-001-001-A01. MINOR REPAIR.
LEFT INBD FLAP OTBD HINGE ARM OTBD NUTPLATE BRACKET CRACKED IN HALF. REMOVED DAMAGED BRACKET IAW SRM 51-42-06-001-001-A01. INSTALLED NEW BRACKET IAW SRM 51-42-06-001-001-A01.
LBL 9 SEAT TRACK FROM FS 581 TO 677 HAS AN AREA OF DEEP CORROSION.
RT SIDEWALL SEAT TRACK CORRODED IN MULTIPLE LOCATIONS. R & R SEAT TRACK IAW AMM 53-00-49-000-801.
SEAT TRACK NR 3 FS 565-677 CORRODED AT MULTIPLE LOCATIONS. REMOVED SEAT TRACK IAW AMM TASK 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW GREO 670-53-00-343 & SRM 51-40-11-001-001-A01. INSTALLED SEAT TRACK IAW AMM TASK 53-00-49-400-801.
LEFT SIDEWALL SEAT TRACK NR 5 FS 708-761 CORRODED AT MULTIPLE LOCATION SCREWS, LOWER CHANNEL, OUTER SURFACE AND OUTER SURFACE CHAFED BY SEAT. FABRICATED NEW SEAT TRACK IAW GREO 670-53-00-343 AND SRM 51-40-11-001-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.
COCKPIT FLOOR PANEL 221ALF AFT FLOOR SUPPORT CORRODED. REMOVED FWD FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001, 51-42-22-001-001.
FOWARD EQUIPMENT COMPARTMENT ELECTRIC BAY FLOOR SKIN CRACKED AT W LINE 79.50 UNDER AD6 RESTOW PUMP, RT SIDE. REPAIRED IAW GREO 670-53-11-509.
FWD EQUIPMENT COMPARTMENT ELECTRIC BAY FLOOR SKIN CRACKED AT WL 79.50 UNDER PRESSURE GAGES LT SIDE. REPAIRED IAW GREO 670-53-11-809.
LEFT BS 280 WEB CORRODED IN MULTIPLE LOCATIONS JUST ABOVE FLOOR LEVEL. BLEND CORROSION IAW SRM 51-21-06-001-001 AND 53-11-10-201-803. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REPAIRED IAW REO 670-53-11-594.
RBL 9 SEAT TRACK FROM FS 349 TO 485 HAS ONE AREA OF DEEP CORROSION AT APPROX FS 380. FABRICATED NEW SEAT TRACK IAW GREO 670-53-00-343 AND SRM 51-40-11-001-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.
RBL 9 SEAT TRACK FROM FS 485 TO 581 HAS 3 AREAS OF CORROSION. R & R SEAT TRACK IAW AMM'S 53-00-49-000-801 AND 53-00-49-400-801.
LBL9 SEAT TRACK FROM FS 581 TO 677 HAS AREAS OF DEEP CORROSION. R & R SEAT TRACK IAW AMM 53-00-40-000-801.
RT SIDEWALL SEAT TRACK NR 5 FS 708-761 CORRODED IN MULTIPLE LOCATIONS. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343 & SRM 51-40-11-001-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.
RT SIDEWALL SEAT TRACK NR 6, FS 785-863 CORRODED IN MULTIPLE LOCATIONS AT SCREWS, LOWER CHANNEL, OUTER SURFACE. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801(A02).
LEFT SIDEWALL SEAT TRACK NR 6 FS 785-863 CORRODED AT MULTIPLE LOCATED SCREWS, FOOT SCALLOP HOLES OUTER SURFACES. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343 & SRM 51-40-11-001-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED IAW AMM 53-00-49-400-801-A02.
RBL 9, SEAT TRACK FROM FS 349 TO 485 HAS ONE AREA OF DEEP CORROSION AT FS 380.
RBL 9 SEAT TRACK FROM FS 485 TO 581 HAS 3 AREAS OF CORROSION.
LEFT 2ND SIDEWALL SEAT TRACK CORRODED AT MULTIPLE LOCATIONS FS 485-565. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
LEFT FWD SIDEWALL, SEAT TRACK CORRODED AT MULTIPLE LOCATIONS FS 379-485. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
RT SIDEWALL SEAT TRACK NR 2 FS 485-565 CORRODED ON MULTIPLE LOCATIONS AT SCREWS, LOWER CHANNEL, OUTER SURFACE. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343 AND SRM 51-40-11-001-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.
LEFT SIDEWALL SEAT TRACK NR4 FS 677-708 CORRODED AT MULTIPLE LOCATIONS. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343 AND SRM 51-40-11-001-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.
WITH ICE PROTECTION SYS ON (COWL AND WING) RECEIVED RT WING ANTI-ICE CAUTION MESSAGE. APPLIED QRH PROCEDURES THEN RECEIVED ANTI-ICE DUCT WARNING. APPLIED QRH. PERFORMED AILC TEST AND RESET SYS IAW FIM 30-12-00. FAULT NO LONGER EXISTS. IAW MCC, NO FURTHER ACTION REQUIRED.
MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD.
RUDDER LIMITER CAUTION MESSAGE ILLUMINATED AFTER TAKEOFF, COMPLIED WITH QRH. EMERGENCY DECLARED, RETURNED TO DEPARTURE. COMPLIED WITH INSPECTION OF WATER TRAPS, NO MOISTURE FOUND. COMPLIED WITH SPOST 1 & 2, FAULTS CLEARED. COMPLIED WITH OPS OF SPOILER AND STABILIZER SYS, OPS CHECKED GOOD IAW AMM 27-61-05.
DURING CRUISE, LOST HYD SYS 2 QTY (FIRE EQUIPMENT REQUESTED AS A PRECAUTION) UPON INSP, FOUND NR 2 PRESSURE MANIFOLD DP INDICATIOR O-RING BROKEN. R & R NR 2 PRESSURE MANIFOLD IAW AMM 29-11-05. LEAK CHECK GOOD. (
EMERGENCY LIGHT NR 4 BATTERY PACK NEEDS REPLACING. R & R EMERGENCY LIGHT BATTERY PACKS NR 4 IAW AMM 33-51-17. PERFORMED OPS TEST OF EMERGENCY POWER SUPPLY UNITS IAW AMM 33-51-17-710-801. SYS CHECKS GOOD.
EMERGENCY LIGHTS WOULD NOT COME ON. R & R EMERGENCY LIGHT BATTERY PACKS NR 1, NR 2 AND NR 3 IAW AMM 33-51-17. PERFORMED OPS TEST OF EMERGENCY POWER SUPPLY UNITS IAW AMM 33-51-17-710-801. SYS CHECKS GOOD.
F/A FLASHLIGHT INOP. R & R F/A FLASHLIGHT IAW AMM 25-60-00.
F/A REPORTS A POPPING SOUND FOLLOWED BY A FAINT ELECTICAL SMELL STRONGEST AT THE TOP OF FIRST CLASS CABIN. R & R DIMMER PS49 IAW AMM 33-21-03. OPS CK GOOD. ACFT OK FOR SERVICE. (CLOSED)
MAIN CABIN EMERGENCY LIGHTING , NR 2 BATTERY PACK INOP. REPLACED EMERGENCY LIGHT BATTERY PACK NR 2, OPS CHECKED IAW MM 33-51-00. OPS CHECK GOOD.
MAIN CABIN PASSENGER CABIN G1 GALLEY EMERGENCY EXIT LIGHT LENS CRACKED. R & R EMERGENCY EXIT SIGN LENS IAW AMM 33-51-10. DEFER CLEARED. PLACARD REMOVED.
SMELL OF SMOKE/ELECTRICAL IN GALLEY. REMOVED AND REPLACED FWD HEATED DRAIN MAST IAW AMM 38-32-11, OPS CHECK GOOD. DMIL CLEARED, PLACARD REMOVED. R & R FWD HEATED DRAIN MAST IAW AMM 38-32-11, OPS CHECK GOOD. DMIL CLEARED, PLACARD REMOVED.
F/A REPORTS WHEN FWD LAVATORY IS USED THERE IS A BURNING ODOR NOTED. OPS CHECKED LAV LIGHTS, FLUSH MOTOR, DOOR SWITCH C/N/D . NO BURNING ODOR DETECTED. OK FOR SERVICE IAW AMM 38-31-00.
F/A FLASHLIGHT BATTERIES INOPERATIVE. R & R F/A FLASHLIGHT BATTERIES AS REQUIRED. OPS CK GOOD IAW AMM 25-61-00-710-801.
EMERGENCY EXTERIOR PLACARD "EMERGENCY EXIT" FADED. INSTALLED EXTERIOR PLACARD "EMERGENCY EXIT" PER AMM 20-60-04.
CORROSION FOUND ON RT AND LT INBD SEAT TRACK FROM FS 340 TO 830. REMOVED SEAT TRACK IAW SRM 51-41-02-001-001-A01. FABRICATED NEW SEAT TRACK. REINSTALLED SEAT TRACK IAW AMM TASK 53-00-49-400-801-A02.
RT SIDE SEAT RAILS HAVE COROSION AT FS 379 TO OVERWING EXIT. REMOVED CORROSION AT RT SIDE SEAT RAILS FROM STR379 TO FS533.00 REF SRM 51-21-06-001-001-A01. MEASURED RT SIDE SEAT RAILS FROM FS 379 TO FS 763 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01 & SRM 53-31-49-101-001-A01 & SRM 53-41-49-101-001-A01. COMPLIED WITH REO 670-53-00-013. COMPLIED WITH ASA ECTC REO 670-53-00-013 DATED 06/18/09 REV B SEE JOB 7105511 OP 200.
LT SIDE SEAT RAILS HAVE CORROSION AT FS 379 TO OVERWING EXIT. MEASURED LT SIDE SEAT RAIL, FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01 & SRM 53-31-49-101-001-A01 & SRM 53-41-49-101-001-A01. COMPLIED WITH REO 670-53-00-013. COMPLIED WITH ASA ECTC REO 670-53-00-013 DATED 06-18-09 REV B.
LT AND RT CTR SEAT RAILS HAVE AREAS OF CORROSION FROM FS 830.00 ALL THE WAY AFT. MEASURED LT & RT CTR SEAT RAILS & FOUND TO BE OUT OF LIMITS REF SRM 53-41-49-101-001-A01. REPLACED LBL9.0 SEAT TRACK IAW SRM 51-41-02-001-001-A01. REPLACED SEAT TRACK HARDWARE USING NAS7503-4 & NAS7503-5 IAW SRM.
LT AND RT OTBD SEAT RAILS FROM 909. TO 977 RT AND FROM 923 TO 977 LT HAVE CORROSION. MEASURED LT SIDE SEAT RAILS FROM FS909 TO FS977 & RT SIDE SEAT RAILS FROM FS 923 TO FS 977 BOTH LT & RT RAILS FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. COMPLIED WITH REO 670-53-00-013. COMPLIED WITH ASA ECTC REO 670-53-00-013 DATED 06/18/09 REV B.
THE SMALL EMERGENCY EXIT SIGN AT ROW 14AB LIGHTS ARE INOP.
DURING 6 YEAR INSPECTION IAW TC 53-900-500, FOUND CORROSION OF LEFT LOWER WEB STRUCTURE AT FS 280.00.
DURING 6 YEAR INSPECTION IAW TC 53-900-500, FOUND CORROSION OF RIGHT LOWER WEB STRUCTURE AT FS 280.00. REMOVED AND REPLACED RT LOWER WEB STRUCTURE AT FS 280 IAW CRJ 700 SRM 53-11-10 TASK 53-11-10-201-003-A01. BLENDED CORROSION IAW SRM 51-12-00 AND FOUND TO BE OUT OF LIMITS REF SRM 53-11-10 REPAIR 003-A01. REMOVED WEB IAW SRM 51-42-06.LOCATED HOLES IN NEW WEB OF BULKHEAD PN 670-53-11-52-2 IAW SRM 51-42-06, 51-42-13 AND 53-11-10 INSTALLED WEB IAW SRM 51-42-06 AND 51-42-11.
DURING 6 YEAR INSPECTION IAW TC 53-900-500, FOUND CORROSION OF FLOORBEAM AT FS 280.00. BLENDED AREA, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FS280 CROSSBEAM AS PER SRM 51-42-21, 51-42-06 SB 670BA-53-026.
COCKPIT CENTER FLOOR AFT ATTACH ANGLE IS CORRODED AT FS 280. FOUND AFT ATTACH ANGLE CORRODED BEYOND LIMITS OF SRM 53-00-00. REMOVED AND REPLACED AFT CENTER FLOOR SUPPORT ANGLE AT FS 280 IAW SRM 51-42-06 AND 51-42-21.
LEFT FWD EXTERIOR EMERGENCY LIGHT NOT ILLUMINATING.
LT OVERWING EMERGENCY EXIT LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS
FOUND CRACK IN INNER SKIN BY HANDLE ASSY.
F/A MEGAPHONE NOT WORKING. FLT 4995 DEL 61 MINS.
PAX DOOR DIFFICULT TO CLOSE AND HITS HARD WHEN OPENNING. FLT 4286. REMOVED AND REPLACED FWD AND AFT GAS STRUTS ON ASD OPS CHECK GOOD IAW MM 52-11-17. (B)
AFT MEGAPHONE VOLUME WEAK.
PAX DOOR INNER SKIN CRACKED 8 INCHES AFT OF FWD EDGE 4 INCHES UP FROM BOTTOM ON SKIN. REMOVED INNER SKIN AND INSTALLED NEW INNER SKIN PER CRJ 700 SRM 51-42-06,51-42-13 AND 52-11-01.
LEFT 280 WEB CORRODED BEYOND LIMITS.
PAX DOOR INTERCOSTAL 318 CRACKED. REMOVED AND REPLACED 318 INTERCOSTAL IAW SRM 51-42-06.
FS 280 TRANSVERSE BEAM CORRODED BEYOND LIMITS AND CRACKED. REPAIRS PERFORMED IN ACCORDANCE WITH BOMBARDIER REO 670-53-11-047 & BOMBARDIER SERVICE BULLETIN SB670-BA-53-026. SUPPLEMENTAL SDR CLOSED 3/27/08.
FS 280 TRANSVERSE BEAM CORRODED BEYOND LIMITS AND CRACKED.
LEFT VERTICAL STAB DRAG ANGLE CRACKED AT AFT END (MARKED). PERFORMED EDDY CURRENT INSPECTION OF LT VERTICAL STAB DRAG ANGLE IAW NDTM 51-20-006 TO LOCATE END OF CRACK. END OF CRACK IS MARKED. INSTALLED AND SEALED L/H DRAG ANGLE PER REO 670-55-31-018.
RIGHT VERTICAL STAB DRAG ANGLE CRACKED AT AFT END (MARKED). PERFORMED EDDY CURRENT INSPECTION OF RIGHT HAND VERTICAL STAB DRAG ANGLE IAW NDTM 51-20-006 TO LOCATE END OF CRACK. END OF CRACK IS MARKED. INSTALLED AND SEALED RT DRAG ANGLE PER REO 670-55-31-018.
PAX DOOR OUTER HANDLE CRACKED. REMOVED OUTER HANDLE AND INSTALLED NEW HANDLE PER AMM 52-11-03.
PAX DOOR "EXIT" PLACARD WORN. REPLACED PLACARD PER 11-30-00.
FLOOR SILL CORROSION BEYOND LIMITS APPROXIMATELY 3 INCHES AFT OF FS 280 ON THE RIGHT HAND SIDE. REPAIRS CARRIED OUT IAW BOMBARDIER EO 601R-53-6796.
PASSENGER DOOR SEAL STRICKER IS DENTED. REPAIRS CARRIED OUT IAW BOMBARDIER REO 670-53-22-001 REV E REPAIR TYPE 1.
NLG OUTER CYLINDER P/N 52101-1 S/N BA0025 CORRODED. CORROSION REPAIRED IAW BOMBARDIER REO 670-32-21-0060 AND GOODRICH SCR 0028-05.
TRANSVERSE BEAM AT FS 280 FROM LBL 36 TO RBL 36. CORRODED ALONG UPPER AND LOWER EDGES. REPLACED TRANSVERSE BEAM AT FS 280 IAW BOMBARDIER REO 670-53-11-047 REV C.
FS 280 BULKHEAD LOWER WEBS CORRODED BEYOND LIMITS FROM LBL 36 TO RBL 36. REPLACED FS 280 BULKHEAD LOWER WEBS IAW BOMBARDIER REO 670-53-11-052 REV A REPAIR 2.
LIGHTNING STRIKE EXIT DAMAGE ON LT ELEVATOR TRAILING EDGE. REPAIRED ELEVATOR UPPER SKIN TRAILING EDGE IAW BOMBARDIER EO 601R-55-6779.
FLIGHT 5020 DURING DESCENT INTO CVG WHEN FLIGHT SPOILERS WERE DEPLOYED, RECEIVED SPOILERON AND FLIGHT SPOILER CAUTION MESSAGES, CREW DECLARED AN EMERGENCY, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LT OUTBOARD MULTIFUNCTION SPOILER POWER CONTROL UNIT.
FLIGHT 5020 DURING TPA APPROACH WHEN FLIGHT SPOILERS WERE DEPLOYED, RECEIVED A SPOILERON AND FLIGHT SPOILER CAUTION MESSAGE ON EICAS PRIMARY SCREEN. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED A GROUND FUNCTIONAL CHECK OF SPOILERON. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY.
FLIGHT 5020 DURING DESCENT INTO CVG WHEN FLIGHT SPOILERS WERE DEPLOYED, RECEIVED SPOILERON AND FLIGHT SPOILER CAUTION MESSAGES. CREW DECLARED AN EMERGENCY, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT INBOARD MULTIFUNCTION SPOILER POWER CONTROL UNIT.
FLIGHT 5020 SUSPECTED PITCH TRIM ANOMALY. REPLACED THE FLIGHT CONTROL COMPUTER.
FLIGHT 5077 GEAR DISAGREE WARNING. REPLACED THE SELECTOR VALVE.
FLIGHT 5249 LT ENGINE FAN AT 2.3 VIBES. REPLACED THE LT ENGINE FAN BLADES.
THE RIGHT OUTBOARD MULTI-FUNCTION SPOILER OUTBOARD ATTACH FITTING (WS 216.9) IS CRACKED. REMOVED THE CRACKED ATTACH FITTING AND INSTALLED A NEW ATTACH FITTING P/N CC670-17113-5 IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES EO 601R-57-4790A.
FLIGHT 5043 RT ENGINE FAN VIB CAUTION MESSAGE. REPLACED THE RT ENGINE FAN BLADES.
FLIGHT 454 NOSE WHEEL STEERING FAIL CAUTION MESSAGE. REPLACED THE TILLER.