N912XJ
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
FWD FLIGHT ATTENDANT CALLED REPORTING A STRONG SMELL (A STRONG FUME ODOR) DURING CLIMB OUT. NO EICAS INDICATIONS NO SMOKE OBSERVED IN THE FLIGHT DECK. THE SMELL SEEMED TO BE STRONGEST IN THE GALLEY AREA. R & R GALLEY EXHAUST FAN IAW AMM 21-23-93. OPC NORMAL. R/R GALLEY HEATER IAW AMM 21-23-64, OPC NORMAL. ODORS WENT AWAY. A/C OK FOR SERVICE.
WHEN EMERGENCY LIGHTS SELECTED ON, EXT LIGHTS DO NOT TURN ON AND INT LIGHTS GO FROM DIM TO OFF. R & R PS43 ESPU BATTERY PACK IAW J/C 33-900-701 NO ISSUES NOTED, AIRCRAFT GOOD FOR SVC.
WHILE PERFORMING SB 670BA-53-044 REVISION G DATED JUL05/2022 FOUND LH AND RH DOUBLERS PN CC670-34222-001SB AND CC670-34222-002SB AND LH AND RH STR12A FITTINGS PN CC670-34365-001SB AND CC670-34365-002SB CANNOT BE INSTALLED PER SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING RIVET PATTERN COMPLIED WITH MHIRJ REO 690-53-11-1926 REV -- DATED 2025-01-17.
WHILE PERFORMING R53595-R/R BLIND BLTS ON PRES FLR SIL DECK FS792-801 WE FOUND CORROSION ON THE L/H SIDE SILL DECK AT F.S. 801 AND ONE OVERSIZE FASTENER, FURTHER EVALUATION WILL BE REQUIRED. REPAIRED SILL DECK IAW MHIRJ REO 690-53-41-509 REV-- 1/27/2025.
WHILE PERFORMING R53595-R/R BLIND BLTS ON PRES FLR SIL DECK FS792-801 WE FOUND CORROSION ON THE R/H SIDE SILL DECK AT F.S. 792 AND F.S 801, FURTHER EVALUATION WILL BE REQUIRED. REPAIRED SILL DECK IAW MHIRJ REO 690-53-41-510 REV-- 1/27/2025.
PAX DOOR SILL ANGLE IS CORRODED ON IB & OB SIDE NEAR OR AT SEVERAL FASTENER HOLES AND AT LOWER FORWARD FLANGE. DOOR SILL ANGLE (KICKPLATE ANGLE) P/N SH670-31875-7 ON PAX DOOR SURROUND STRUCTURE, IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
PAX DOOR SILL ANGLE IS CORRODED ON IB & OB SIDE NEAR OR AT SEVERAL FASTENER HOLES AND AT LOWER FORWARD FLANGE. AFTER REMOVED ANGLE, MID CAP FROM PAX DOOR SURROUND STRUCTURE FOUND CORRODED MORE THAN 30% OF A MEMBER, PART IS OUT OF LIMITS, IAW CRJ900 SRM 53-21-23-101-001-A02 NOTE 2, REQUIRE REPLACEMENT ANGLE. CORRECTIVE ACTION: INSTALLED NEW ANGLE, MID CAP P/N SH670-31825-9 ON PAX DOOR SURROUND STRUCTURE, IAW CRJ900 SRM 51-41-02-001-001-A01 & 51-42-06-001-001-A01
LH FLOOR SILL ATTACHMENT ANGLE AT FS 693 IS CORRODED AROUND DRAIN TUBE. INSTALLED NEW ATTACHMENT ANGLE SERVICEABLE AT LH FLOOR SILL DRAIN TUBE FS 693 IAW CRJ900 SRM 51-42-06-001-001-A01.
FLOOR BOARD SUPPORT ANGLE AT F.S.265 AND ATTACH ANGLE TO STGR 27 ARE CORRODED. REMOVED ATTACHMENT ANGLE AT FS.265 STRINGER 27. LOCATED, DRILLED AND INSTALLED ATTACHMENT ANGLE AT FS. 265 STRINGER 27 P/N: CC670-34228-3 IAW CRJ 900 SRM 15-40-11-001-001-A01 & 51-42-21-001-001-A01.
PAX DOOR DD6 FWD INTERCOSTAL AFT CLIP IS CORRODED. REMOVED DAMAGED CLEAT. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE CLIP PN 600-31902-269 IAW CRJ 900 SRM 51-40-11-001-001-A01
PAX DOOR DD1 INTERCOSTAL ATTACH FLANGE BENT AND BULGED WITH CRACK. REMOVE DAMAGE PAX DOOR AFT DD1 INTERCOSTAL IAW CRJ 900 SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL PN 601R31902-318 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
PAX DOOR DD1 FWD INTERCOSTAL ATTACH FLANGE IS BENT AND BULGED. REMOVED DAMAGED INTERCOSTAL. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL PN600-31902-259 IAW CRJ 900 SRM 51-40-11-001-001-A)1 AND 51-42-06-001-001-A01
RH SIDE SEAT TRACKS HAVE SEVERAL AREAS OF CORROSION FS 785-867. THERE IS MISSING METAL AT FS 890 ON EITHER SIDE OF SCALLOP. INSTALLED NEW SIDE SEAT TRACK SH670-36260-5 AND SH670-37543-3 BETWEEN FS785.00 TO FS847.00 IAW CRJ900 AMM 53-00-49-400-801-A07.
STRINGER 19R FROM F.S.597 TO F.S.613 IS CORRODED. REPAIRED IAW CRJ-900 SRM 53-00-03-201-001-A02
STRINGER 19R FROM F.S.597 TO F.S.613 IS CORRODED. REPAIRED IAW CRJ-900 SRM 53-00-03-201-001-A02
RIGHT WING AILERON CABLES ARE CORRODED. (OUTBOARD WING TRAILING EDGE) REMOVED AND REPLACED 2 CORRODED R/H OUTBOARD AILERON WING CIRCUIT CABLES WITH 2 NEW R/H OUTBOARD AILERON WING CIRCUIT CABLES P/N: BA670-93210-31 AND P/N: BA670-93210-29 IAW CRJ-900 AMM 27-11-00-000/400-803-A01.RIG AND OPS CHECKS GOOD.
FOUND 4EA L/H AILERON SIDE BUSHING LUGS LABELED ÿ½Bÿ½, ÿ½Cÿ½, ÿ½Fÿ½, AND ÿ½Gÿ½ TO HAVE PITTING AND CORROSION REPAIRED IAW BOMBARDIER REO 670-57-61-237 REV - DATED 2017-07-25
"FOUND 2EA R/H AILERON BUSHING LUGS LABELED ÿ½Cÿ½ AND ÿ½Fÿ½ TO HAVE PITTING AND CORROSION REAMED 2EA BUSHING LUGS LABELED ""C"" AND ""F"" PER REPAIR F. STEPS 1-4 OF BOMBARDIER REO 670-57-61-237 REV - DATED 2017-07-25. COMPLIED WITH STEP# F (7) OF BOMBARDIER REO 670-57-61-237 REV.- DATED 2017-07-25. FABRICATED 2EA O/S AILERON BUSHINGS (P.N. S10009-225Y) USING MATERIAL AMS5659 15-5 PH H1000 (P.O. W90151). CAD PLATED 2EA R/H AILERON SIDE O/S BUSHINGS IAW CRJ900 SRM 51-21-11-001-001-A01. COMPLIED WITH REO 670-57-61-237 REV - DATED 2017-07-25."
THE LH FS 280 BEAM IS CORRODED IN SEVERAL AREAS ON THE LOWER SURFACE IN THE RADIUS. REMOVED AND REPLACED CROSSBEAM I.A.W. BOMBARDIER CRJ900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-22-001-001-A01, 51-40-11-001-001-A01, 51-21-11-001-001-A01 AND 51-25-16-001-001-A01.
FRAME FS 319 BETWEEN STRINGER 26L-26R IS CORRODED A: REMOVED CORROSION ON FS 319 BETWEEN STGR 26L - STGR 27 IAW CRJ 900 SRM 53-00-06-201-005-A01(STEP 6A1) / 51-21-06-001-001-A01
INTERCOSTAL AT STGR 21L FROM FS 333 - FS 349 CORRODED REMOVED INTERCOSTAL FROM STRG 21L BTWN FS 333 TO FS 349, IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED NEW INTERCOSTAL (BACKUP SILL) P/N SH670-31823-1 ON STRG 21L BTWN FS 333 TO FS 349 IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01
STGR 21R IS CORRODE FROM FS 333 TO FS 364 REMOVED STRINGER 21R BETWEEN FS 333 TO 379 IAW CRJ 900 SRM 51-42-06-001-001-A01. INSTALLED STGR 21R PN: SH670-31383-1S FROM FS 333 TO FS 379 THROUGH SKIN IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
STGR 21R IS CORRODE FROM FS 333 TO FS 364 REMOVED STRINGER 21R BETWEEN FS 333 TO 379 IAW CRJ 900 SRM 51-42-06-001-001-A01. INSTALLED STGR 21R PN: SH670-31383-1S FROM FS 333 TO FS 379 THROUGH SKIN IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
STRINGER 19R IS CORRODED BETWEEN FS 597.00 AND 613.00. REMOVED AND INSTALLED NEW STGR 19L, FWD AND AFT SHIMS, AND FWD AND AFT SPLICE REPAIRS IAW CRJ 900 SRM 53-00-03-201-001-A02
STRINGER 22L IS CORRODED BETWEEN FS 485.00 AND 501.00. COMPLIED WITH EA NO: CRJ953-14082 REV IR DATED 6/25/2023
STRINGER 22R IS CORRODED BETWEEN FS 295 - FS 333 REMOVED STRINGER 21R BETWEEN FS 280 TO 333 IAW CRJ 900 SRM 51-42-06-001-001-A01. INSTALLED STGR 21R PN: SH670-31636-1U FROM FS 280 TO FS 333 THROUGH SKIN IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
STRINGER 22R IS CORRODED BETWEEN FS 295 - FS 333 REMOVED STRINGER 22R BETWEEN FS 280 TO 333 IAW CRJ 900 SRM 51-42-06-001-001-A01. INSTALLED STGR 22R PN: SH670-31210-2U FROM FS 280 TO FS 333 THROUGH SKIN IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
ANTENNA DOUBLER BETWEEN FRAMES FS295-FS310 STRINGER 27 IS CORRODED. REMOVED AND REPLACED DOUBLER I.A.W. BOMBARDIER CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01 AND 51-21-16-001-001-A01.
3 PAX DOOR STRUCTURE INTERCOSTALS BELOW FLOOR AT LONGITUDINAL JOINT FROM FS.310 TO FS.349 ARE CORRODED. UPON INVESTIGATION FOUND 2 EACH STR 21L INTERCOSTALS (P/N'S SH670-31822-1 AND SH670-31823-1) BETWEEN FS310.00 - FS349.00 TO BE HEAVILY CORRODED AND BEYOND ALLOWABLE DAMAGE LIMITS OF CRJ 900 SRM 53-21-23-101-001-A02.REMOVED STGR 21L INTERCOSTAL F.S.310.00 TO F.S.333.00 AND STGR 21L INTERCOSTAL BETWEEN F.S.333 TO F.S.349 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.INSTALLED TWO SERVICEABLE STGR 21L INTERCOSTAL F.S.310.00 TO F.S.333.00 AND STGR 21L INTERCOSTAL BETWEEN F.S.333 TO F.S.349 IAW CRJ-900 SRM 51-42-06-001-001-A01.
RIGHT VERTICAL STAB DRAG ANGLE IS CRACKED AT THE 67.5 REAR SPAR DATUM. REPAIRED R/H FWD VERTICAL STAB DRAG ANGLE IAW CRJ 900 SRM 55-31-00-201-001-A01.
ELONGATED HOLE FOUND ON AFT CHANNEL, EXTERNAL AC POWER AREA. REMOVED AFT CHANNEL IAW CRJ900 SRM 51-42-06-001-001-A01. INSTALLED SERVICEABLE CHANNEL WITH PN: CC670-33402-1 IAW CRJ900 SRM 51-42-06-001-001-A01.
R/H GROUND STUD BRACKET AT F.S. 333.00 STRINGER 21R IS CORRODED. REMOVED AND REPLACED STRINGER SPLICE I.A.W. BOMBARDIER CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-25-00-001-001-A01.
F.S. 280.00 FLOORBOARD SUPPORT ANGLE AFT SIDE OF 280 FRAME IS CORRODED. REMOVED AND REPLACED ANGLE I.AW. BOMBARDIER CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.
RH FWD EMERGENCY EXIT STEP PLATE IS CORRODED. COMPLIED WITH ENDEAVOR EA CRJ 953-1401
RH FWD EMERGENCY EXIT STEP PLATE IS CORRODED. REMOVED CORROSION AT LH AFT EMERGENCY EXIT STEP PLATE IAW. CRJ-900 SRM 51-21-06-001-001-A01
RH AFT EMERGENCY EXIT STEP PLATE IS CORRODED. REMOVED CORROSION AT LH AFT EMERGENCY EXIT STEP PLATE IAW. CRJ-900 SRM 51-21-06-001-001-A01
LH FS 280 WEB IS CORRODED AT LBL 11. REPAIRED IAW CRJ 900 SRM 53-11-10-201-004-A01
FUSELAGE FRAME F.S.250 BETWEEN STGR 26L AND 26R IS CORRODED. REPAIRED IAW ENDEAVOR AIR EA CRJ953-14013
FUSELAGE FRAME F.S.533 BETWEEN STGR 26L TO 26R IS CORRODED REPAIRED IAW ENDEAVOR AIR EA CRJ953-14013
FORWARD JACK PAD INTERCOSTALS ARE CORRODED FROM F.S.280 TO F.S.265 AT STGR 27. REPAIRED FORWARD JACK PAD INTERCOSTALS IAW ENDEAVOR EA CRJ953-15247 AND EA CRJ953-13991
THE RH FS 280 BEAM IS CORRODED IN SEVERAL AREAS ON THE LOWER SURFACE IN THE RADIUS. BETWEEN RBL 9 AND BL 0. REMOVED RH FS 280 CROSSBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-22-001-001-A01. CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE FS 280 R/H CROSSBEAM P/N CC670-34094JP-2S IAW CRJ 900 SRM 51-40-11-001-001-A01. P/N CC670-34094ZJP-2
R/H MLG WHEEL WELL LINE SHROUD PANEL ATTACH ANGLE IS CORRODED. REMOVED AND REPLACED ATTACH ANGLE I.A.W. BOMBARDIER CRJ900 SRM 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.
PAX DOOR TOP FIXED COVER PLATE FASTENER HOLES ARE CORRODED. REMOVED TOP PANEL IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01 LOCATED AND DRILLED NEW SERVICEABLE TOP PANEL P/N:601R317075-3IAW CRJ900 SRM 51-40-11-001-001-A01 INSTALLED NEW SERVICEABLE TOP FIXED COVER PLATE IAW CRJ 900 SRM 51-42-096-001-001-A01
S/N SBO 600 L/H AFT OVERWING EMERGENCY EXIT DOOR TOP FORMER IS CRACKED AT DOOR SWITCH TARGET. REPAIRED DAMAGE I.A.W. ENDEAVOR AIRLINES EA# CRJ952-15190 REV.IR, DATED 05/24/2023.
S/N SBO 601 R/H AFT OVERWING EXIT DOOR TOP FORMER IS CRACKED AT DOOR SWITCH TARGET. REPAIRED DAMAGE I.A.W. MHIRJ REO 690-52-21-134 REV.--, DATED 2023-06-13.
1EA. BRACKET CHAFED ON THE INBOARD SIDE OF OUTBOARD HINGE ARM ON THE RIGHT INBOARD FLAP. REMOVED BRACKET PLATE WITH IS P/N CC670-14146-2 IN INBOARD SIDE OF INBOARD HINGE BEAM OF THE RIGHT INBOARD FLAP IAW CRJ900 SRM 51-42-06-001-001-A01. INSTALLED BRACKET PLATE P/N CC670-14146-2 ON INBOARD SIDE OF INBOARD HINGE BEAM OF THE RIGHT INBOARD FLAP IAW CRJ900 SRM 51-42-06-001-001-A01.
S/N SBO 601 R/H AFT OVERWING EMERGENCY EXIT DOOR HAS CORROSION ON FRAME LEG AT RIVET INSIDE DOOR BELOW THE WINDOW. REPAIRED DAMAGE I.A.W. MHIRJ REO 690-52-21-133 REV.--, DATED 2023-06-13.
WHILE INCORPORATING SB 670BA-57-020, FOUND 4 EA 2ND OVERSIZE FASTENERS IN THE COLD WORK ZONE. (HST254). ON LH WING PLANK STRAP. REPAIRED LH WING PLANK OVERSIZE FASTENERS IAW REO 690-57-21-341 REV--DATED 2020-01-30.
PREVIOUS CREW REPORTED GEAR DISAGREE ON T/O FOR 20 SECONDS. AFTER REVIEWING A/C MAINT LOG THIS IS A REPEAT PROBLEM THAT REQUIRES DOCUMENTATION ON THE GEAR DISAGREE SHEET. UNABLE TO LOCATE THE PREVIOUS CREW FOR WRITE UP. COMPLIED WITH MOTOR GROUP REQUEST TO R&R RT MLG RETRACT ACTUATOR REFER LOG PAGE 3534457-1 FOR DETAILS. A/C OK FOR SERVICE. REPLACED RT MLG RETRACTION ACTUATOR IAW AMM 32-32-05 AND OPS CHECK IS GOOD. A/C OK FOR SERVICE.
LEFT ENGINE FLAME OUT AT TOP OF DECENT. FLAMEOUT WAS PRECEDED BY 2 SEPARATE VIBRATIONS AND THEN ENGINE FLAMEOUT. FOLLOWED QRH GUIDANCE, ENGINE RELIT NORMALLY. AS ENGINE FLAMEOUT ITT WENT INTO RED MOMENTARILY CAUSING LITT EXCEED B STATUS MESSAGE TO POST AFTER ENGINE RELIT ENGINE PERFORMED NORMALLY FOR REMAINDER OF FLIGHT INCLUDING USE OF REVERSE THRUST. COMPLETED WORK SCOPE. LT ENGINE FLAMEOUT DATED 11-02-18. REPLACED LT ENG 6TH STAGE CHECK VALVE IAW AMM 36-44-11. OPS GOOD IAW 72-00-00.
""GEAR DISAGREE"" WARNING AFTER TAKEOFF IN KBUF,AND ""PROX SYS FAULT""STATUS MESSAGE DURING WARNING. WENT AWAY (BOTH MESSAGES) 20 SECONDS LATER W/O RUNNING QRH. PROCEEDED WITH NORMAL OPERATIONS. *NOTE : RIGHT MAIN GEAR "" AS PER MOTR, REMOVE+REPLACED PROX SENSOR PX18. REMOVED +REPLACED RT UPLOCK SENSOR PX18 IAW AMM 32-61-05. OPS CHK GOOD IAW AMM 32-61-00. PERFORMED GEAR SWING IAW AMM 32-30-00. REFER TO LOGPAGE 3485428-1 FOR CAT II RELEASE.
GEAR DISAGREE (UP) WARNING ON CLIMBOUT (RIGHT MAIN GEAR) WHILE PERFORMING T/S FOUND THE RT MLG UPLOCK ASSY PROX SWITCH (PX18) TO BE OUT OF LIMITS (.062) ADJUSTED SWITCH PX18 TO .040 IAW AMM 32-64-05. ADJ TEST OF EXTENSION/ RETRACTION SYS CHECKS GOOD IAW AMM 32-30-00
STR 25R LONGERON FS 349 CORRODED OUT OF LIMTIS. REMOVED AND REPLACED LONGERON IAW SRM 51-42-06
AFT CARGO FLOORBEAM CORROED ON UPPER SURFACE FS 1015-1031 LBL 9. REPAIRED FLOORBEAM IAW REO 670-53-00-029.
AFT CARGO FLOORBEAM CORROED ON UPPER SURFACE FS 1031 LBL 27. REPAIRED FLOORBEAM FS1031 LBL 27 IAW REO 670-53-00-029 REV A R-SM-6
PYLON PANEL 443BB CRACKED AT FASTENER HOLE FWD END. REMOVED/REPLACED PYLON PNL SKIN IAW SRM 51-42-06 AND 51-42-13.
PYLON PANEL 443BT CRACKED AT FASTENER HOLE. REMOVED/REPLACED PYLON PNL SKIN IAW SRM 51-42-06 AND 51-42-13.
LEFT WING NR 1 SLAT, SLAT CAN 1-3 HAS CRACK ON INTERNAL MOUNTING POINT OF THE SLAT CAN. REPAIRED LT WING NR 1 SLAT CAN 1-3 CRACK DAMAGE REO670-37-42-377.
GALLEY SERVICE DOOR SCUFF PLATE CORRODED AT CORNERS ON LOWER. LOCATED AND DRILLED SCUFF PLATE IAW SRM 51-40-11 DOME SEALED NUTPLATES IAW SRM 51-23-00.
LT SIDEWALL SEAT TRACK STICK 3 HAS CORROSION, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK LT SIDEWALL NR 3 IAW AMM 53-00-1. SM-58.
RBL9 SEAT TRACK BETWEEN FS693.0 TO FS830.40 HAS CORROSION REMOVED/REPLACED RBL9 SEAT TRACK BETWEEN FS693.0 TO FS830.40 IAW AMM 53-00-49 SM-58
LT SIDEWALL SEAT TRACK STICK 4 HAS CORROSION, IN THE CABIN. REMOVED/REPLACED LT SIDEWALL SEAT TRACK NR 4 IAW AMM 53-00-49. SM-58.
LT SIDEWALL SEAT TRACK STICK 8 HAS CORROSION, IN THE CABIN. REMOVED CORROSION IAW SRM 51-21-06 FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49 FABRICATED NEW SEAT TRACK ON NR 6573662. REMOVED/REPLACED SEAT TRACK IAW SRM 51-41-04 SM-58
LT SIDEWALL SEAT TRACK STICK 2 HAS CORROSION, IN THE CABIN. REMOVED/REPLACED LT SIDEWALL SEAT RAIL STICK 2 IAW AMM 53-00-49. R SM 4.
LBL9 SEAT TRACK BETWEEN FS847.48 TO FS954.0 HAS CORROSION. REMOVED/REPLACED LBL9 SEAT TRACK BETWEEN FS847.48 TO FS954.0 IAW AMM 53-00-49 R SM 4
ANGLE AT STA 280 AND LBL 9 O/B WL 79 FOUND CRACKED. RECEIVED NEW ANGLE PN: CC670-34-269-4S, TAG# B20860 LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-11 INSTALLATION OF NEW ANGLE TO BE ACCOMPLISHED ON W/O 1016131 ZONE 1000 ITEM 0122 SN 6528544 SM-107
RBL9 SEAT TRACK BETWEEN FS830.40 TO FS847.0+48 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK AT RBL9 BETWEEN FS830.40 TO FS847.0+48 IAW AMM 53-00-49 R SM 4
SPLICE ON STGR 26L HAS CORROSION ON THE FWD SIDE OF FRAME 333, IN THE FWD E & E BAY. REPLACED STRINGER SPLICE ON 26L AT FS 333 IAW CRJ 900 SRM 51-42-06 AND SRM 51-42-21 SM-33
RT AISLE SEAT TRACK STICK 2 HAS CORROSION, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK ON RT AISLE STICK 2 IAW AMM 53-00-49. R SM4.
SEAT TRACK ON LBL 27 STICK 2 HAS CORROSION , IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IN LBL 27 STICK 2 IAW AMM 53-00-49. R SM 4.
PASSENGER ENTRY DOOR AFT DRAG ANGLE IS CRACKED. REMOVED/REPLACED PASSENGER ENTRY DOOR AFT DRAG ANGLE IAW SRM 52-11-04.
STR 25R HAS CORROSION BETWEEN FRAMES 295 AND 280, IN THE FWD E & E BAY. REPLACED STR 25R FROM FRAME 280 TO 333 IAW SRM 51-42-06 AND 51-42-21 SM-33
RT AISLE SEAT TRACK STICK 3 HAS CORROSION, IN THE CABIN. REMOVED CORROSION IAW SRM 51-51-06, FOUND TO BE OUT OF LIMITS IAW AMM 53-00-49. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49 NEW SEAT TRACK FABRICATED ON W/O 6530091. SM-58.
LBL9 SEAT TRACK BETWEEN FS693.0 TO FS830.40 HAS CORROSION REMOVED AND REPLACED LBL9 SEAT TRACK BETWEEN FS693.0 TO FS830.40 IAW AMM 53-00-49
RT SIDE WALL SEAT TRACK STICK 5 HAS CORROSION IN THE CABIN REMOVED & REPLACED RT SIDEWALL SEAT TRACK STICK 5 IAW AMM 53-00-49-000-801 & 53-00-49-400-801. SM-58.
LBL9 SEAT TRACK BETWEEN FS830.40 TO 847.0+48 HAS CORROSION. REMOVED AND REPLACED LBL9 SEAT TRACK BETWEEN FS830.40 TO FS847.0+48 IAW AMM 53-00-49 R S/M 4
LBL9 SEAT TRACK BETWEEN FS693.0 TO FS830.40 HAS CORROSION. REMOVED AND REPLACED LBL9 SEAT TRACK BETWEEN FS693.0 TO FS830.40 IAW AMM 53-00-49
LT AISLE SEAT TRACK STICK 4 HAS CORROSION, IN THE CABIN. REMOVED/REPLACED SEAT TRACK IAW AMM 53-00-49. SM-58.
LT AISLE SEAT TRACK STICK 1 HAS CORROSION, IN THE CABIN. REMOVED AND REPLACED LT AISLE SEAT TRACK STICK IAW AMM 53-00-49. R SM 4.
RT AISLE SEAT TRACK STICK 1 HAS CORROSION, IN THE CABIN. REMOVED AND REPLACED RT AISLE SEAT TRACK IAW AMM 53-00-49. R SM 4.
PASSENGER ENTRY DOOR FORWARD WEB IS CRACKED AT MID STEP. REMOVED PASSENGER ENTRY DOOR CRACK AT MID STEP FOUND WITHIN LIMITS IAW CRJ 900 SRM 52-11-04.
FIRST OFFICER`S RED ROUND BUTTON ON THE OXYGEN PANEL WAS MISSING THE CENTER CAP. R & R THE FIRST OFFICER`S OXYGEN MASK IAW AMM 35-11-12. OPS CHECKED GOOD.
RT OW E-LIGHT INOP. R&R RH OW E-LIGHT ASSY IAW AMM 33-51-15 OP/C GOOD.
LEFT MIDDLE OVERWING EMERGENCY EXIT LIGHT LENS WAS CRACKED. REMOVED AND REPLACED THE LENS IAW CMM 33-51-02.
LEFT OVERWING EMERGENCY EXIT LIGHT HAD A DAMAGED LENS. REMOVED AND REPLACED LT AFT EMERGENCY LIGHT LENS IAW CMM 33-52-07.
MEGAPHONE INOPERATIVE. REMOVED AND REPLACED THE MEGAPHONE IAW AMM 25-61-14. ACFT OK FOR SERVICE. C.
YAW DAMPER UNCOMMANDED OCCILATIONS IN FLIGHT AT 26000 FT, QLH COMPLETED. OCCILATIONS STOPPED WHEN YAW DAMPERS WERE DISENGAGED. COULD NOT DUPLICATE, PERFORMED OPS TEST OF NR 1 YAW DAMPER IAW AMM 22-22-04 TESTED GOOD.
SLATS FAIL AFTER TAKEOFF UPON RETRACTION. T/S FLAPS/SLATS SYS IAW FIM 27-81-03, PERFORMED OPS CHECK IAW AMM 27-50-00 AND CLEARD INHIBITS IAW AMM 45-45-00. ALL CHECKS PASSED NO MESSAGES AT THIS TIME A/C OK FOR SVC.
AFT FA OXYGEN MASK HOSE HAS NICKS AND CRIMPS. REMOVED AND REPLACED THE AFT FA OXYGEN MASK IAW AMM 35-21-09. "
MEGAPHONE INOP. REMOVED AND REPLACED AFT MEGAPHONE IAW AMM 25-61-14. OK FOR SVC.
ELT FAILS G SWITCH TEST ON JC-25-220-700. REMOVED & REPLACED ELT IAW AMM 25-62-02. OPS CHECKED OK PER JC-25-220-700.
RIGHT FLOOR SUPPORT BS 280 - 319 IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.
SERVICE DOOR SEAL STRIKER IS CORRODED AROUND SCREW HOLES. REPLACED THE SERVICE DOOR SEAL STRIKER IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
VERTICAL STAB AFT DRAG ANGLE CRACKED ON LEFT SIDE. REPLACED THE DRAG ANGLE IAW SRM 51-42-00-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-40-06-001-001-A01, AND 51-42--22-001-001-A01.
INTERCOSTAL AT STRINGER 20R BELOW SERVICE DOOR SILL IS CORRODED BETWEEN BS 319 AND 333. REPLACED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.
COCKPIT FLOOR SUPPORT BS 280-265 RBL 12 IS CRACKED .5 INCHES LONG, ABOVE REINFORCEMENT ANGLE ATTACH POINT. REPAIRED THE FLOOR SUPPORT IAW EO R53187.
COCKPIT FLOORBEAM BS 280-265 LBL 12 IS CRACKED .5 INCHES LONG ABOVE REINFORCEMENT ANGLE ATTACH POINT. REPAIRED THE FLOORBEAM IAW EO R53187. "
SEAT TRACK CORRODED AT RBL 9, BETWEEN BS 349 AND 364. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A07.
RIGHT VERTICAL STAB AFT DRAG ANGLE CRACKED. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01 & 51-42-00-001-001-A01.
EMERGENCY LIGHT LT SIDE AT BS 762.36 BETWEEN PAX SEATS IS DAMAGED. REMOVED AND REPLACED THE IAW AMM 33-51-01-400-801-A21.
PAX DOOR UPPER STAIR PANEL UPPER HINGE IS CORRODED. REMOVED AND REPLACED THE HINGE IAW SRM 51-40-11-001-001-A01 AND 51-41-02-001-001-A01.
PAX DOOR PANELS 832AL AND 832FL HAVE CORROSION. FOUND TO BE OUT OF LIMITS. BONDED NEW GASKETS TO PANELS IAW AMM 51-22-81-340-802-A01.
SEAT TRACK AT BS 927 RBL 9 IS CORRODED. REMOVED & REPLACED THE SEAT TRACK, RETAINER & MOUNT FITTINGS IAW SRM 51-40-11-001-001-A01, REO 670-53-00-343 REV M, AMM 53-00-49-400-801-A01 & SRM 51-41-02-001-001-A01.
SKIN FOUND CHAFED. REPLACED THE SKIN PANEL IAW SRM 51-40-11-001-001-A01.
BS 280 FLOORBEAM IS CORRODED. REMOVED & REPLACED IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.
LEFT BS 280 BULKHEAD WEB WAS FOUND CORRODED. REMOVED & REPLACED THE BULKHEAD WEB IAW REO 670-53-11-594.
BS 280 FWD J-ANGLE IS CORRODED AROUND CAMLOCK RECEPTACLES. INSTALLED A NEW ANGLE IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
SERVICE DOOR UPPER SILL ANGLE IS CORRODED. REMOVED AND REPLACED THE DOOR SILL ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
BS 280 AFT SIDE FLOORBEAM ANGLE CORRODED AROUND NUTPLATES. REMOVED & REPLACED IAW SRM 521-42-21-001-001-A01 & 51-40-11-001-001-A01.
BS 280 FLOORBEAM IS CORRODED. REMOVED & REPLACED IAW SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.
FLIGHT DECK PBE HAS LOST ITS VACUUM SEAL. ITS IS SOFT TO THE TOUCH. R & R THE PBE IAW AMM 35-32-06. OPS CHECK GOOD. OK FOR SERVICE.
PIECE OF THE EMERGENCY LIGHT FOUND LOOSE. SECURED THE LIGHT.
EMERGENCY LIGHT LOOSE ROW 13 AB. SECURED THE LIGHT IAW AMM 33-51-01.
CAPTAIN`S OXYGEN MASK NET LEAKING, RUPTURED RUBBER TUBING. SWAPPED CAPTAIN`S MASK WITH OBSERVER`S MASK IAW AMM 35-11-12. NO LEAKS NOTED ON CAPTAIN`S MASK. REMOVED AND REPLACED OBSERVER`S OXYGEN MASK IAW AMM TA 001714R1. OPS TESTED GOOD.
FLOOR FRONT EXIT, FLOOR EMER LIGHTING MISSING. TRACK LIGHTING INSTALLED, EMER LIGHTING STRIP AS REQUESTED, OK FOR SERVICE IAW AMM 33-51-01.
GEAR DISAGREE WARNING MSG AFTER TAKEOFF RAN NON-NORMAL CHECKLIST. CHECKED ON ARRIVAL & FOUND NOSE STRUTS COMPLETE FLAT. SERVICED NOSE STRUTS WITH OIL & NITROGEN IAW AMM 12-12-32. ALL GEAR EXTENSION & RETRACTION CHECK PERFORMED IAW AMM 32-30-00. ALL CHECKED GOOD.
EXTRA FLIGHT ATTENDANT JUMP SEATS FLASHLIGHT INOPERATIVE. DEFERRED FLASHLIGHT AT EXTRA FLIGHT ATTENDANTS STATION IAW MEL 25-61-4A. PLACARD INSTALLED, ENTERED INTO MM2. R & R FLIGHT ATTENDANTS EXTRA FLASHLIGHT IAW AMM 25-61-02. OPERATIONS CHECKED GOOD. MM02 UPDATED & PLACARD REMOVED.
EMERGENCY PATH LIGHTING STRIP MISSING IN FRONT OF GALLEY, BEHIND FWD FLIGHT ATTENDANT JUMP SEAT. SECURED BIOLUMINESCENT STRIP AS REQUIRED IAW AMM 33-51-01.
SECTION OF EMER FLOOR TRACK LIGHTING MISSING, RT SIDE JUST FWD OF FWD LAVATORY. INSTALLED EMER FLOOR TRACK IAW 33-51-01.
REFLECTIVE STRIP LEADING TO EMER EXIT, FRONT OF SEATS 12CD, NEED TO BE SECURED. SECURED EMER LIGHT STRIP AT ROW 12CD IAW AMM 33-51-01. SECURITY CHECKED GOOD AT THIS TIME.
ON TAKEOFF, SMELT SMOKE & FIRST OFFICER WAS COVERED IN A WHITE SUBSTANCE. RETURNED TO AIRPORT. DEFERRED LT AIR CONDITIONING PACK IAW MEL 21-51-1B. CAT C PLACARD INSTALLED. R & R LT ACM PN ON & OFF GG670-95009-5, SN OFF 00622 SN. EMER WAS DECLARED.
AFT CABIN EMER FLASHING LIGHT DEAD. R & R AFT CABIN EMER FLASHLIGHT BRACKET IAW AMM 25-61-02. PERFORMED OPERATIONS CHECK IAW AMM 25-61-00. OPERATIONS CHECKED GOOD AT THIS TIME, NO DEFECTS NOTED. ALL MX PROCEDURES COMPLIED WITH.
EMERGENCY LIGHTING STRIP IS NOT GLUED DOWN TO FRONT LT SIDE OF ACFT. SECURED EMER LIGHT STRIP IAW AMM 25-25-00. OK FOR SERVICE.
REFLECTIVE FLOOR PATH STRIP IN GALLEY AHEAD OF CLOSET UNGLUED. SECURED REFLECTIVE FLOOR PATH STRIP IN GALLEY AREA IAW AMM 33-51-01. ALL CHECKED GOOD.
FLOOR STRIP LIGHTING HAS COME OFF AROUND 12C. SECURED EMER FLOOR LIGHT STRIP. PERFORMED OPERATIONS CHECK IAW 33-51-01. OPERATIONS CHECK WAS GOOD.
PASSENGER DOOR OUTER HANDLE CRACKED. R & R PAX DOOR OUTER HANDLE IAW SB 670BA-52-030.
PANEL 443BT IS CRACKED. R & R PANEL 443BT IAW SRM'S 51-42-06 & 51-40-11 TO BE INSTALLED ON PANEL OPENING & CLOSING CARD 8 OF 15. ON OPERATIONS 192.
PANEL 432BT CRACKED & CHAFED. R & R PANEL 432BT IAW SRM 51-42-06 & 51-40-11 TO BE INSTALLED ON PANEL OPENING & CLOSING CARD 19.
LEFT LE OF RUDDER CHAFED AT TOP ON PANEL 327CL. DRILL NEW PANEL FASTENER HOLES IAW 51-40-11. PANEL TO BE INSTALLED ON OPERATION 192. BLENDED CHAFE ON LT LE RUDDER SKIN IAW SRM 55-41-01 BETWEEN STATION 151.51 & 136.90 WITHIN LIMITS. DEPTH .001"-.0085" BLENDS 1) L 3.3" W .45" 2) L3.9" W.9" 3) L3.1"W.2" 4) 1.0"W.2" 5) L1.4"W.2" 5) L1.4"W.18" 6) L1.25"W.28" 7) 1.1"W.5"
TASK CARD 900-53-140-509 COCKPIT FLOOR SILL AT FS 279.00 HAS CORROSION & IS MISSING 2 NUTPLATES. INSTALLED TWO RECEPTACLES IN FLOOR SILL AT FS 279 IAW SRM 51-42-06. BLENDED FLOOR SILL TO REMOVE CORROSION AT FS 279. TOTAL MATERIAL REMOVED .003", MATERIAL REMAINING .060", FLOOR SILL IS WITHIN LIMITS IAW SRM 51-21-00 & 53-00-00. ALODINED & PRIMED AFFECTED AREA ON FLOOR SILL IAW SRM 51-25-06.
TASK CARD 900-52-830-300 PAX DOOR STEP STRUCTURE TOP PANEL APPEARS TO BE CRACKED IN RADIUS ON FWD & AFT SIDES. FWD RADIUS FOUND NOT TO BE CRACKED. SEE PARTIAL WORK ACCOMPLISHED FOR DETAILS. AFT RADIUS WAS FOUND TO BE CRACKED & WAS REQUIRED IAW SRM 52-11-04.
PANEL 584ET CHAFED. OLD PANEL IS OUT OF LIMITS. DRILLED NEW PANEL & TOP COATED IAW SRM 51-40-11, 57-52-01, 51-25-01 TO BE INSTALLED ON PANEL. OPENING & CLOSING CARD 9 OF 15.
PANEL 684ET CHAFED. OLD PANEL IS OUT OF LIMITS. DRILLED UP NEW PANEL 684ET IAW SRM 51-40-11, 57-52-01 & APPLIED TOP COAT SRM 51-25-01 TO BE INSTALLED ON PANEL OPENING AND CLOSING CARD 12 OF 15.
TASK CARD 900-53-900-504 PASSENGER DOOR SILL HAS POSSIBLE CORROSION IN SEVERAL LOCATIONS. CORROSION FOUND TO BE TOO DEEP. R & R CAP ANGLE IAW SRM 51-42-06 & 51-40-11.
TASK CARD 900-57-570-300 AVIONICS BAY DOOR HANDLE HOUSING HAS POSSIBLE CRACK. R & R AVIONICS COMPARTMENT DOOR HANDLE HOUSING ASSEMBLY IAW SRM 51-42-21.
TASK CARD 900-52-830-300 PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW 900 SRM 52-11-04-201-002-A01.
TASK CARD 192 LEFT WING PANEL 584EB HAS CHAFE DAMAGE. BLENDED PANEL 584EB REMOVING .028 MATERIAL, PANEL OUT OF LIMITS. RECEIVED NEW PANEL, MATCH DRILLED IAW SRM 57-52-01-101-001-A01 & 51-40-11-001-001-A01. PANEL TO BE INSTALLED ON OPS 192.
TASK CARD 900-53-900-504 CORROSION ON RT SIDE FLOOR SEAL, RBL36, AFT OF GALLEY DOOR BETWEEN FS 349.00 - 364.00, FS 349.00 - 364.00, BL 36R, WL72. REPAIRED FLOOR SILL IAW EA CRJ953-03422.
TASK CARD 900-53-230-500 SERVICE DOOR SILL HAS POSSIBLE CORROSION ON ALL SCREW HOLES. R & R SERVICE DOOR SILL, SEAL STRIKER, IAW SRM 51-41-00, 51-42-06, AMM 53-21-23 & 53-21-27.
TASK CARD 900-53-900-514 RIGHT SIDE SEAT RAIL AT FS 863 PREVIOUS BLEND WAS .039, NEW BLEND AT .070, BLEND OUT OF LIMITS IAW REO 670-53-00-013. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REMOVED .70". R & R SEAT TRACK IAW AMM 53-00-49.
TASK CARD 900-53-900-514 RIGHT SEAT RAIL AT FS 693.00 HAS INTERGRANULAR CORROSION. BLENDED CORROSION ON RT SEAT RAIL AT FS 693. REMOVED .062 OF ALLOWABLE .035, FOUND TO BE OUT OF LIMITS IAW REO 670-5.-00-013. R & R SEAT RAILS IAW AMM 53-00-49.
TASK CARD 900-52-830-300 PASSENGER DOOR AFT SIDE STRUCTURE BY BOTTOM STEP IS CRACKED. REMOVED AFT SPRING TO FOM IAW AMM 52-11-17. REMOVED GAS SPRING BEAM IAW SRM 51-42-06. REPAIRED CRACKED STAIR PANEL ON PAX DOOR IAW REO 670-52-11-104. REINSTALLED AFT GAS SPRING & BEAM IAW AMM 52-11-17 & SRM 51-42-06. OPERATIONAL TEST TO BE COMPLETED ON NR 20144.
TASK CARD 900-53-900-514 LEFT SEAT RAIL AT FS 693.00 HAS CORROSION. R & R LT SEAT RAIL AT FS 693 IAW AMM 53-00-49. BLENDED SEAT RAIL AT FS 693. REMOVED .061 OF ALLOWABLE .035, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013.
TASK CARD 900-54-430-300 LEFT AFT CORE COWL HAS CHAFING ON THE RUB STRIP. REMOVED DAMAGE FROM AFT CORE COWL RUB STRIP, LE TEE, IN A 11.5"X1" AREA. REMAINING THICKNESS .0876", MINIMUM ALLOWABLE THICKNESS .100", OUT OF LIMITS IAW SRM 54-13-00-201-005-A01. RECEIVED NEW AFT LT CORE COWL. NEW CORE COWL TO BE INSTALLED.
TASK CARD 900-53-900-504 CORROSION ON RT SIDE FLOOR SEAL, RBL36, FWD OF GALLEY SERVICE DOOR NEAR FS 319.00 & BS 316.00 - 319.00, BL 36R, WL72. REPAIRED RT SIDE FLOOR SILL FWD OF GALLEY SERVICE DOOR AT FS 319.00 IAW EA 953-03419.
TASK CARD 900-53-900-506 RIGHT SEAT RAIL HAS LIGHT SURFACE CORROSION AT FS 645.00. BLENDED CORROSION ON SEAT RAIL. REMOVED .042 OF ALLOWABLE .035, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R SEAT RAIL IAW AMM 53-00-49.
TASK CARD 900-53-900-101 RT SIDE FLOOR SEAT RAIL HAS CORROSION BETWEEN FS 349.00 & 377.00. BLENDED CORROSION ON RT FLOOR SEAT RAIL. REMOVED .062, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R SEAT RAIL IAW AMM 53-00-49.
TASK CARD 900-53-900-506 LEFT SIDE SEAT RAIL AT FS 811 HAS CORROSION. SIDE SEAT TRACK AT FS 811 & FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R SEAT TRACK IAW AMM 53-00-49.
TASK CARD 900-53-900-506 LEFT SEAT RAIL HAS CORROSION AT FS 661 + 62. MECH REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R SEAT TRACK IAW AMM 53-00-49.
TASK CARD 900-53-900-504 CORROSION ON FWD END OF LT SIDE FLOOR SEAT RAIL, LBL9, NEAR FS 374.00, BS 374.00 & WL 72.00. MECH REMOVED DAMAGE FROM LT FLOOR SEAT TRACK NEW FS 374.00 & FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R TRACK IAW AMM 53-00-49.
TASK CARD 900-25-260-100 LT EMER ESCAPE ROPE FRAYED NEAR ATTACH POINT. R & R LT EMER ESCAPE ROPE IAW AMM 25-63-04.
CAPTAINS SIDE EMER LIGHT INOPERATIVE. R &R BATTERY IAW 25-61-00. OPERATIONS CHECKED GOOD.
GEN 1 OFF LINE TURNED MAGENTA IN FLIGHT. R & R 1 GCU IAW AMM 24-11-07. OPERATIONS CHECKED GOOD. OK FOR SERVICE. PN OFF & ON 766283C, SN OFF 1397 & SN ON 2191.
EXIT ROW 13 A - B EMER EXIT ROW LIGHTING STRIP MISSING. ROBBED 10 INCH SECTION FROM 1A LT SIDE. ROBBED 5 INCH SECTION AT RT SIDE 20CD. INSTALLED LIGHTING STRIP AT ROW 13AB. DEFERRED ROBBED SECTIONS IAW MEL 33-51-1G MC 96579 ADVISED. CAT C ENTERED INTO MM02, PLACARD APPLIED. INSTALLED NEW EMER LIGHT FLOOR STRIPS AT 1AB & 20CD IAW AMM.
ROW 13A EMERGENCY LIGHT CAME OFF. SECURED THE EMERGENCY LIGHT IAW AMM 33-51-00.
13B FLOOR EMERGENCY LIGHT IS NOT SECURE. SECURED LIGHT IAW AMM 33-51-01. OK FOR SERVICE.
EMERGENCY FLOOR STRIPES IN EXIT ROW 13 LT & RT SIDE PULLED UP. REINSTALLED EMER FLOOR TRACKS ON ROW 13 SEAT AB IAW AMM 33-51-01.
FIRST OFFICER`S SIDE EMERGENCY FLASHLIGHT NOT CHARGING, RED LIGHT IS NOT FLASHING. INSTALLED NEW BATTERY IAW AMM 25-61-02. OPS CHECKED GOOD.
FLIGHT ATTENDANT`S REPORTS FLASHLIGHT ON GALLEY SERVICE DOOR, RED LIGHT NOT FLASHING. DEFERRED FLASHLIGHT IAW MEL 25-61-4 MX NOTIFIED 53431 ENTERED INTO MM02 & PLACARD PLACED. R & R FLIGHT ATTENDANTâS EMERGENCY FLASHLIGHT ASSEMBLY BY SERVICE DOOR IAW AMM 25-61-02. NOTIFIED MX 53431, PLACARD REMOVED, CLEARED FROM MM02.
THREE INFANT LIFE VEST MISSING FROM WARDROBE CLOSET. INSTALLED THREE VEST PN P0640-101.
FWD CARGO DOOR LOWER OUTER SEAL RETAINER IS DENTED AND GOUGED. REPLACED FWD CARGO DOOR LOWER OUTER SEAL RETAINER IAW SRM 51-42-06, LEAK TEST OF FWD CARGO DOOR GOOD IAW AMM 52-00-00-790-801, REF MM409 282677.
CLUSTER OF GOUGES ON HINGE INBD SEAL AREA OF PAX DOOR. REMOVED GOUGES ON INBD SEALANT PAX DOOR AND IS IN LIMITS IAW EO R53481.
FWD CARGO DOOR INNER LOWER SEAL RETAINER IS BENT. REPLACED FWD CARGO DOOR INNER LOWER SEAL RETAINER WITH NEW IAW AMM 52-35-07 LEAK TEST OF FWD CARGO DOOR GOOD IAW AMM 52-00-00-790-801.
LT BS 280 FLOORBEAM HAS CORROSION AT LBL9, TOP SIDE. REPAIRED CORROSION DAMAGE IAW EO R53482.
LT LWR, LT LOWER TRANSCOWL COAMING DOUBLER L/E CHAFED. REPAIRED LOWER TRANSCOWL COAMING DOUBLER IAW REO 670-54-21-1028 C/W FUNCTIONAL TEST OF THE T/R SYS NO DEFECTS NOTED IAW AMM 78-30-00-720-801, PN CR3522-5-3.
LT UPPER TRANSCOWL COAMING DOUBLER L/E CHAFED. REPAIRED LT UPPER TRANSCOWL COAMING DOUBLE L/E IAW REQ 670-54-21-1028 FUNCTIONAL TEST OF THE T/R SYS GOOD IAW AMM 78-30-00-720-801.
RIGHT AILERON ACCESS PANEL 699CB IS CHAFED. REPAIRED RT AILERON ACCESS PANEL 699CB IAW REO 690-57-61-093.
LEFT WING NR 1 SLAT IS GOUGED ON T/E AT APPROXIMATELY WS 128. REPAIRED LT WING NR 1 SLAT T/E IAW REO 690-57-42-263.
UPPER FLANGE CRACKED ON LT SHUTOFF VALVE IN AFT CARGO BAY. R & R LT SHUTOFF VALVE IAW AMM 21-55-02. PERFORMED OPS TEST OF SHUTOFF VALVE. OPS TESTED GOOD IAW AMM 21-55-02.
FWD E&E BAY FS 280 CIRCUMFERENTIAL STRAP CORRODED. REPAIRED AND FOUND WITHIN LIMITS IAW SRM 51-21-06.
RT WHEEL WELL OTBD BODY TO WING MOUNT CHAFED. BLENDED CHAFE O/H BODY TO WING MOUNT AND IS IN LIMITS IAW EO R57152.
LT WHEEL WELL OTBD BODY TO WING MOUNT CHAFED. BLENDED CHAFE ON LT BODY TO WING MOUNT AND IS IN LIMITS IAW EO R57152.
PASSENGER DOOR, FWD UPPER CENTERING PLATE IS WORN. REPAIRED WEAR DAMAGE AND FWD UPPER CENTERING PLATE ON PAX DOOR IAW EOR52093 GAGE CHECK GOOD IAW MM 52-11-00, REF MM409 282682. PN MS20426AD6-8.
RT MAIN GEAR DOOR LOWER INNER SKIN PUNCTURED. REPAIRED RT MAIN CARGO DOOR LOWER INNER SKIN IAW REO 690-52-82-086 GAP CHECK GOOD IAW MM 32-12-01.
RT MAIN GEAR DOOR OTBD UPPER AFT EDGE DAMAGED. REPAIRED RT MAIN CARGO DOOR OTBD UPPER AFT EDGE IAW REO 690-52-82-086, GAP CHECKED GOOD IAW MM 32-12-01.
LT WING FUEL PANEL 541CB DAMAGE. REPAIRED LT WING FUEL PANEL 541CB IAW REO 690-57-22-018.
RIGHT AILERON L/E SKIN IS CHAFED AT WS 353 AND 314.50. REPAIRED CHAFED AREAS ON RT AILERON L/E SKIN IAW REO 690-57-61-093.
LEFT INBD FLAP VANE, INBD ACCESS PANEL 584ET IS CHAFED. R & R WITH NEW PANEL 584ET IAW SRM 51-40-11, PN CC670-4027-3.
WHILE INSTALLING RT INBD WING L/E, NUT PLATE CHANNEL FOUND TO BE DAMAGED. R & R NUT PLATE CHANNEL IAW SRM 51-42-06.
RIGHT AILERON L/E SKIN IS CHAFED AT WS 353 AND 314.5. REPAIRED CHAFED AREAS ON RT AILERON L/E SKIN IAW REO 690-57-61-093.
PANEL 622AR HAS CHAFED METAL ALONG L/E. REMOVED CHAFES IAW REO 690-57-41-114 ON PANEL 622AR AND IS WITHIN LIMITS IAW REO 690-57-41-114.
AFT LOWER SKIN CHAFED AT BS 913, REPAIRED SKIN IAW EO R53480.
RIGHT AILERON ACCESS PANEL 699BB IS CHAFED. REPAIRED RT AILERON ACCESS PANEL 699BB IAW REO 690-57-61-093.
THE 11TH HINGE LUG ON THE DOOR HINGE IS GOUGED. REPAIRED 11TH HINGE LUG ON DOOR HINGE IAW EO R52092, MM 409 282683.
SECOND HINGE LUG ON FUSELAGE SIDE OF PAX DOOR IS GOUGED. REPAIRED HINGE LUG ON FUSELAGE SIDE OF PAX DOOR IAW EO R53481.
FWD E & E BAY LT INBD INTERCOSTAL CORRODED AT FS 364, REPAIRED LT INBD INTERCOSTAL & FOUND WITHIN LIMITS IAW SRM 51-21-06.
FWD CARGO DOOR INNER WEB IS GOUGED ON LOWER FWD AND AFT CORNERS. REPAIRED FWD CARGO DOOR INNER WEB LOWER FWD AND AFT CORNERS IAW REO3 690-52-35-107, REF MM409, 282664.
MID CARGO DOOR INNER WEB IS CHAFED ON LOWER FWD AND AFT CORNERS. REPAIRED MID CARGO DOOR INNER WEB LOWER AND FWD AND AFT CORNERS IAW REO 690-52-35-106, REF MM409 282665, PN CR3213-5-3.
FWD E & E BAY INBD INTERCOSTAL CORRODED AT FS 364, REPAIRED RT INBD INTERCOSIAL AND FOUND WITHIN LIMITS IAW SRM 51-21-06.
FWD E & E BAY STRINGER 25L SPLICE CORRODED AT FS 33, REPAIRED & FOUND WITHIN LIMITS IAW SRM 51-21-06.
FWD E & E BAY TCAS DOUBLER CORRODED. REPAIRED TCAS DOUBLER FOUND WITHIN LIMITS IAW SRM 51-21-06.
FWD E&E BAY FS 280 AFT LOWER PANEL LANDING CORRODED. REPAIRED AND FOUND WITHIN LIMITS IAW SRM 51-21-06.
MID CARGO DOOR FWD LOWER HINGE ARM IS GOUGED. COMPLIED WITH REO 690-52-35-105 TO REPAIRED MID CARGO DOOR FWD LOWER HINGE ARM.
FWD CARGO DOOR AFT LOWER HINGE ARM IS GOUGED. COMPLIED WITH REO 690-52-35-104 IN REPAIR OF FWD CARGO DOOR AFT HINGE ARM REF MM.
FWD CARGO DOOR FWD LOWER HINGE ARM IS GOUGED. COMPLIED WITH REO 690-52-35-104 TO REPAIR FWD CARGO DOOR FWD LOWER HINGE ARM.
NLG DOOR HINGE DAMAGED. R & R NLG DOOR HINGE IAW SRM 51-42-02.
RT AFT NLG FITTING IS DAMAGED. R & R FITTING IAW SRM 51-42-21.
FWD E&E BAY S27 CORRODED BETWEEN FS 319.7 & 310. R & R STRINGER 27 IAW SRM 51-42-06.
FWD E & E BAY FS 333 CORRODED BETWEEN S26L & 26R. REPAIRED, FOUND WITHIN LIMITS IAW SRM 51-21-06 AND R53277.
FWD E & E BAY FS 349 CORRODED BETWEEN S26L & 26R. REPAIRED AND FOUND WITHIN LIMITS IAW SRM 51-21-06, EO R53277.
FWD E & E BAY FS 295 CORRODED BETWEEN S26L & 26R. REPAIRED AND FOUND WITHIN LIMITS IAW SRM 51-21-06 AND EO R53277.
FWD E & E BAY FS 310 CORRODED BETWEEN S26L & 26R. REPAIRED AND FOUND WITHIN LIMITS IAW SRM 51-21-06 AND EO R53277.
FWD E & E BAY RT LONGERON CORRODED AT FS 349, R & R RT LONGERON IAW SRM 51-42-06.
AFT ADG ANTENNA INNER DOUBLER IS CORRODED AT FWD COAX HOLE. REPAIRED AFT ADG ANTENNA INNER DOUBLER IAW EA CRJ953-0018893.
FLIGHT DECK FLOORBEAM CORRODED AT FS 280. R & R FLOORBEAM ANGLE IAW SRM 57-47-06.
MID CARGO DOOR AFT LOWER HINGE ARM IS GOUGED. COMPLIED WITH REO 690-52-35-105 TO REPAIR MID CARGO DOOR AFT LOWER HINGE.
RT UPPER RT UPPER TRANSCOWL ACCESS DOOR HINGE WORN. R & R RT UPPER TRANSCOWL ACCESS DOOR HINGE IAW SRM 51-24-18 AND SRM 51-42-21.
RIGHT LOWER TRANSCOWL COAMING AND DOUBLER WORN. REPLACED RT LOWER TRANSCOWL LOAMING AND DOUBLES IAW SRM 51-42-06 AND 51-42-13.
FWD E & E BAY FS 319.70 CORRODED BETWEEN S26L & 26R, REPAIRED AND FOUND WITHIN LIMITS IAW SRM 51-21-06 AND EO R53277.
PANEL 684EB HAS BARE METAL SHOWING. REPLACED PANEL 684EB WITH NEW IAW SRM 51-40-11.
LEFT LOWER TRANSCOWL INBD STANDOFF CRACKED. REPLACED LEFT LOWER TRANSCOWL INBD STANDOFF IAW SRM 51-42-14 AND 51-42-13.
RIGHT UPPER TRANSCOWL INBD STANDOFF CRACKED. REPLACED RT UPPER TRANSCOWL INBD STANDOFF IAW SRM 51-42-14 AND 51-42-13.
SERVICE DOOR ANGLE HAS LIGHT CORROSION ON THE FWD AND AFT CORNERS. R & R SERVICE DOOR ANGLE IAW SRM 51-42-21 AND 51-42-06.
LEFT UPPER TRANSCOWL INBD STANDOFF CRACKED. R & R LT UPPER TRANSCOWL INBD STANDOFF WET IAW SRM 51-42-14, 51-42-20 AND 51-23-00.
SKIN PANEL 433BB IS CHAFED. FABRICATED NEW SKIN PANEL AND REPLACED IAW SRM 51-24-21 AND SRM 51-40-11.
COCKPIT EMERGENCY EXIT EXTERNAL HANDLE WILL NOT RELEASE. CLEANED AND LUBRICATED COCKPIT EMERGENCY EXIT EXTERNAL HANDLE IAW AMM 12-20-52-640-803. NO DEFECTS NOTED. PERFORMED OPS/TEST CHECK OF THE CREW SCAPE HATCH LATCH MECHANISM OUTER HANDLE IAW AMM 52-22-02-710-801, OPS CHECKED GOOD.
ONE LAMP INOPERATIVE AT DS155 WHILE DOING JC900-33-900-001. REPLACED LAMPS IAW AMM 33-51-11. OP CHECKED IAW TASK CARD 33-51-00-710-802 AND JC 900-33-900-001.
CORROSION WAS FOUND ON RT 280 FLOORBEAM. REMOVED AND REPLACED RT FS 280 FLOORBEAM IAW EO NR R53188.
FOUND BS 280 FLOORBEAM CORRODED. REMOVED AND REPLACED FLOORBEAM IAW EO NR 53188.
EXTERNAL EMERGENCY LIGHT RT AFT INOPERATIVE. REPAIRED CONNECTOR P876 IAW ESPM 20-11-11. OPS TEST GOOD IAW AMM 33-51-15.
FLOORBEAM LBL12 IN FLT DECK CRACKED. REMOVED DAMAGED SECTION OF LBL 12 FLOORBEAM AND REPLACED WITH NEW SECTION IAW REO 690-53-11-390 AND EO NR R53187.
LT UPPER ENGINE COWL PYLON HINGE PANEL BROKEN. REMOVED AND REPLACED LT UPPER ENGINE COWL PYLON HINGE PANEL SKIN IAW SRM 51-42-06 AND 51-42-13.
FLIGHT DECK FLOORBEAM CORRODED AT FS 280. REMOVED AND REPLACED FLT DECK FLOORBEAM AT FS280 IAW SRM 51-42-06 AND 51-42-21.
LT SIDE SEAT TRACK NR 7 AND HARDWARE CORRODED SEVERAL PLACES. REMOVED AND REPLACED LT SIDE SEAT TRACK NR 7 TRACK AND HARDWARE IAW AMM 53-00-49.
FOUND BS 280 WEB CORRODED. REPAIRED RT FS 280 WEB IAW EO R53190.
FOUND BS 280 WEB CORRODED. REPAIRED LT FS 280 WEB IAW EO R53190.
LEFT WING PANEL NR 599AB CHAFED. LOCATED AND DRILLED NEW LT WING PANEL IAW SRM 51-40-11.
PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED DRAG ANGLE IAW SRM 52-11-04.
PAX DOOR SKIN DAMAGED. REPAIRED PASSENGER DOOR SKIN IAW REO 690-52-11-193 AND EO NR R52044.
HINGE LINE FAIRING 422DB CRACKED. DOT A124-003. REMOVED AND REPLACED HINGE LINE FAIRING 422DB IAW ARM 51-42-06.
HINGE LINE FAIRING 422DB CRACKED. REMOVED AND REPLACED HINGE LINE FAIRING 422DB IAW ARM 51-42-06.
WHEN SELECTING GEAR UP, HANDLE DID NOT MOVE, PUSHED (DOWNLOCK RELEASE) UPON MOVING LEVER TO UP POSITION WARNING MESSAGE DISAGREE APPEARED ALONG WITH WOW INPUT CAUTION A/SKID INBD CAUTION AND PROX SYS T1 STATUS. RETURNED FOR LANDING OVERWEIGHT 2500 LBS OVER. LESS THAN 200 FPM. COMPLETED 409 NR393314. ADJUSTED NLG W OFF W PROX SENSORS IAW 32-61-05. OPS CHECK OF PROX SYS AND GEAR RETRACTION/EXTENSION SYS CHECKS GOOD. NOSE STEERING AND ANTISKID SYS CHECKS GOOD. NO OVERWEIGHT LANDING INSP REQUIRED IAW 05-51-01. ALL GEAR SWINGS AND OPS CHECKS GOOD.
AFT F/A REPORTS FLOOR EMERGENCY LIGHT BETWEEN ROWS 11-12 IS MISSING. INSTALLED EMERGENCY LIGHT AT ROW 11, IAW AMM 33-51-01.
FLOOR TRACK LIGHT MISSING AT EXIT ROW ON RT SIDE. INSTALLED FLOOR TRACK LIGHT AT RT EXIT ROW SIDE AS REQUIRED.
FWD AVIONICS FLOOR PLATE AT FS193.00 CRACKED AT AD6 RESTOW PUMP BD3189099. COMPLIED WITH REO 670-53-11-509.
FOUND LT GALLEY FLOOR PATH LIGHTING CRACKED AND PEELING. R & R LT GALLEY FLOOR PATH LIGHT IAW AMM 35-51, PN ON/OFF PL88-900LH, PL88-930LH05, PL88-910LH00.
AFTER RAISING GEAR "GEAR DISAGREE" MASTER WARNING. RT MAIN GEAR DISAGREE. ABNORMAL CHECKLIST COMPLETE. ALTERNATE RELEASE CABLE MECHANISM WAS FOUND IN WRONG POSITION. DEFERRED LANDING GEAR RETRACTION SYS IAW MEL 32-30-1 A. PERFORMED MX PROC IAW MEL PLACED ON MM02. MX NOTIFIED 0782. PERFORMED OPS TEST OF LANDING GEAR EXTENSION/RETRACTION SYS IAW AMM NR32-30-00. REMOVED FROM DMR. MX NOTIFIED NR22802.
WHILE SITTING AT GATE 20 MIN AFTER AIRCRAFT POWER UP "EMER LTS ON" STATUS MESSAGE ILLUMINATED. SIMILAR DISCREPANCY LOG PAGE 2056476 AND PAGE 2056477. CYCLED EMER LIGHT SWITCHES, THE LIGHTS CAME BACK ON. NOW ARE STUCK IN GRR. AIRCRAFT TO BE FERRIED FROM GRR TO DTW FOR THE PURPOSE OF REPAIR OF EMERGENCY LIGHTING SYSTEM. T/S EMER LTS SYS, DETERMINED THE ESS BUS SENSE RELAY DEFECTIVE. NO OTHER ELECTRICAL PROBLEMS NOTED. INSPECTED AIRCRAFT AND FOUND SAFE FOR FERRY FLIGHT FROM GRR TO DTW FOR THE PURPOSE OF REPAIRS. REMOVED AND REPLACED AC ESS BUS SENSE RELAY K198 PN M8356/17-002L IAW CRJ9000 AMM 20-42-00. PERFORMED OPS CHECK OF EMER LTS, OPS CHECK GOOD AT THIS TIME.
EMERGENCY FLOOR PATH LIGHTING STRIP DAMAGED/DETERIORATED; MOST FWD STRIP, LT/RT SIDES AT GALLEY AREAS. REPLACED LIGHTING STRIP.