N909XJ
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
CRACK ON AFT LOW CHANNEL FS 1047.00 ATTACHED TO DOOR SURROUND STRUCTURE OF AFT BAGGAGE BAY COMPARTMENT AFT LOW CHANNEL FS 1047.00 ATTACHED TO DOOR SURROUND STRUCTURE OF AFT BAGGAGE BAY COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL. CORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) ON LH/RH MAIN WHEEL WELL WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED SUPPORT PLATES RH WHEEL WELL WITHIN LIMITS PER CRJ-900 SRM-53-00-00-101-001-A01, SUPPORT PLATES LH WHEEL WELL EVALUATED OUT LIMITS PER CRJ-900 SRM-53-00-00-101-001-A01 THEREFORE CONNECTOR SUPORT PLATE (1 EA L/H) WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
CRACKS ON AFT RT DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR REPLACE PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01
CORROSION ON FLOOR SILL RH BTW FS280 TO FS319.70 AT FLOOR STRUCTURE OF PASSENGER CABIN. CORROSION WAS EVALUATED OUT LIMITS DUE TO EXCESIVE DAMAGE THEREFORE WAS REPLACED PER CRJ-900 SRM 53-00-45-201-001-A01 AND CRJ-900 SRM 51-42-06-001-001-A01 SRM 51-42-13-001-001-A01 AND SRM 51-42-22-001-001-A01
CORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORT PLATE (UPPER AND LOWER) (IN BK, LG EXT, LG RET) (4 EAS) RBL 45/LBL 45 ON WHEEL WELL. SUMMMARY OF NRC 00034: CORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORT PLATE (UPPER AND LOWER) (IN BK, LG EXT, LG RET) (4 EAS) RBL 45/LBL 45 ON WHEEL WELL WAS REMOVED CRJ900 SRM 51-21-06-001-001-A01, MLG SUPPORT PLATE (1EA) L/H LOWER WHEEL WELL, RH/LH MLG HYDRAULIC LINES SUPPORT PLATES (UPPER) (IN BK, LG EXT, LG RET) (2 EAS) RBL 45/LBL 45 ON WHEEL WELL EVALUATED WITHIN LIMITS PER CRJ-900 SRM-53-00-00-101-001-A01, MLG SUPPORT PLATE 1EA R/H LOWER WHEEL WELL OUT LIMITS PER CRJ-900 SRM-53-00-00-101-001-A01 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
CRACK ON ACCESS PANEL 433BT AND 433BB ACCESS PANEL 433BT AND 433BB WERE REPLACE PER SRM 51-42-10-001-001-A01 AND 51-42-06-001-001-A01
CRACK ON ACCESS PANEL 433BT AND 433BB ACCESS PANEL 433BT AND 433BB WERE REPLACE PER SRM 51-42-10-001-001-A01 AND 51-42-06-001-001-A01
CRACK HINGES OTBD EDGES OF ACCESS PANELS NBR 591LB & 691LB AT LH/RH WINGS PERFORM THE REPLACEMENT OF THE HINGE PER SRM 51-42-06-001-001-A01 AND EA CRJ957-22208 REV IR
CRACK HINGES OTBD EDGES OF ACCESS PANELS NBR 591LB & 691LB AT LH/RH WINGS PERFORM THE REPLACEMENT OF THE HINGE PER SRM 51-42-06-001-001-A01 AND EA CRJ957-22208 REV IR
CORROSION ON SEAT RAIL BTW FS 349 TO FS 409 9RBL AND FS 370 TO FS 409 LBL9 AT FLOOR PASSENGER CABIN SEAT RAIL BTW FS 349 TO FS 409 9RBL AND FS 370 TO FS 409 LBL9 AT FLOOR PASSENGER CABIN WERE REPLACED PER CRJ 900 SRM 53-00-49-000-801-A07 AND SRM 53-00-49-400-801-A07
CORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA 337.657 (LUG L2) AND 342.911 (LUG L5) LUG BORE ON AIL STA 337.657 (LUG L2) AND 342.911 (LUG L5) WERE REPAIRED PER REO 690-57-61-521 REV. - - AND REO 670-57-61-237 REV - -
AFTER RH AILERON BUSHINGS REMOVAL, CORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA 336.4015 ( LUG R1), 337.657 (LUG R2), 338.424 (LUG R3), 342.911 (LUG R5) AND 344.1665 (LUG R6) LUG BORE ON AIL STA 336.4015 ( LUG R1), AND 338.424 (LUG R3) WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01, INSPECTED PER CRJ/900 SRM 51-11-00-001-001-A01 AND DAMAGES NOT WERE FOUND. LUG BORE ON AIL STA 337.657 (LUG R2), 342.911 (LUG R5) AND 344.1665 (LUG R6) WERE REPAIRED PER REO 690-57-61-522 REV - -, REO 690-57-61-522 REV -A, AND REO 670-57-61-237 REV - -
CORROSION FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV. 10
CORROSION FLOOR FITTING IN AFT ACCESS 107 OUT SIDE (1EA) ON GALLEY 1 NEW FLOOR FITTING P/N: A661091-1 IN AFT ACCESS 107 OUT SIDE (1EA) ON GALLEY 1. WAS MANUFACTURED PER EA NO: CRJ953-22230 REV IR. AND REPLACED PER SAFRAN CMM 25-33-67 REV NO. 10 DATED JUN 20/22
CORROSION FLOOR FITTING IN AFT AND FWD ACCESS 205 (2EAS) ON GALLEY 2. FLOOR FITTING (PN: A391251-3) IN AFT ACCESS 205 (1 EA) ON GALLEY 2 WAS MANUFACTURED PER EA CRJ953-22214 REV IR AND INSTALLED PER CMM 25-32-84 REV NO. 9 AND FLOOR FITTING ( PN: 9861251-3 IN FWD ACCESS 205 (1 EA) ON GALLEY 2 WAS REPLACED PER CMM 25-32-84 REV NR 9.
CORROSION FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV. 10
CORROSION ON CROSSBEAMS ON FS349 BTW LBL9 TO RBL9 AT FLOOR STRUCTURE PASSENGER. CROSSBEAMS ON FS349 BTW LBL9 TO RBL9 AT FLOOR STRUCTURE PASSENGER WAS REPAIRED PER REO 690-53-21-2136 REV.--
CORROSION ON SUPPORT ANGLES (2EA) ON FUEL PANEL ON ACCESS PANEL 192AR. SUPPORT ANGLES (2EA) ON FUEL PANEL ON ACCESS PANEL 192AR WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01.
CORROSION ON SUPPORT ANGLES (2EA) ON FUEL PANEL ON ACCESS PANEL 192AR. SUPPORT ANGLES (2EA) ON FUEL PANEL ON ACCESS PANEL 192AR WERE REPLACED PER SRM 51-42-10-001-001-A01.
BENT AND WEAR ON INNER AND OUTBOARD (4 EAS) RETAINER SEAL AT FWD AND CTR BAGGAGE BAY DOORS COMPARTMENT SEAL RETAINER (2AE) AT FWD AND CTR BAGGAGE BAY DOORS COMPARTMENT WERE EVALUATED PER CRJ-900 SRM 52-35-07-201-001-A01 OUT LIMITS THEREFORE WERE REPLACED ER CRJ 900 SRM 51-42-06-001-001-A01, LOWER PLATE (1EA) AT CTR BAGGAGE BAY DOORS COMPARTMENT WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 52-35-07-201-001-A01 THEREFORE WAS REPLACED PER CRJ 900 AMM 52-35-07-000-802-A02, AMM 52-35-07-400-802-A02, LOWER PLATE FWD (1EA) WAS CONFORMED PER CRJ 900 SRM 52-35-07-201-001-A01.
BENT AND WEAR ON INNER AND OUTBOARD (4 EAS) RETAINER SEAL AT FWD AND CTR BAGGAGE BAY DOORS COMPARTMENT SEAL RETAINER (2AE) AT FWD AND CTR BAGGAGE BAY DOORS COMPARTMENT WERE EVALUATED PER CRJ-900 SRM 52-35-07-201-001-A01 OUT LIMITS THEREFORE WERE REPLACED ER CRJ 900 SRM 51-42-06-001-001-A01, LOWER PLATE (1EA) AT CTR BAGGAGE BAY DOORS COMPARTMENT WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 52-35-07-201-001-A01 THEREFORE WAS REPLACED PER CRJ 900 AMM 52-35-07-000-802-A02, AMM 52-35-07-400-802-A02, LOWER PLATE FWD (1EA) WAS CONFORMED PER CRJ 900 SRM 52-35-07-201-001-A01.
CRACK ON LH & RH CHANNEL LOCATED BTW FS 799.00 AT LBL42.00 AND RBL42.00 ON MLG WHEEL WELL AREA (WHEEL BIN SUPPORT CHANNEL). CHANNEL LH & RH LOCATED BTW FS 799.00 AT LBL42.00 AND RBL42.00 ON MLG WHEEL WELL AREA (WHEEL BIN SUPPORT CHANNEL) WERE REMPLACED PER. CRJ900 SRM 51-41-02-001-001-A01
CRACK ON LH & RH CHANNEL LOCATED BTW FS 799.00 AT LBL42.00 AND RBL42.00 ON MLG WHEEL WELL AREA (WHEEL BIN SUPPORT CHANNEL). CHANNEL LH & RH LOCATED BTW FS 799.00 AT LBL42.00 AND RBL42.00 ON MLG WHEEL WELL AREA (WHEEL BIN SUPPORT CHANNEL) WERE REMPLACED PER. CRJ900 SRM 51-41-02-001-001-A01
BROKEN OUTBOARD CORNER SETTLEMENT AREA OF EQUIPPED LINER AT CTR BAGGAGE BAY DOOR ANGLE (2EAS) UPPER AFT AND UPPER FWD WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-41-02-001-001-A01
CRACK ON UPPER / LOWER SUPPORT BRACKET OF PYLON TIE-BAR, THROUGH PYLON ACCESS PANELS 433BT AND 433BB AT LH ENGINE.. UPPER / LOWER SUPPORT BRACKET OF PYLON TIE-BAR, THROUGH PYLON ACCESS PANELS 433BT AND 433BB AT LH ENGINE WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
WEAR ON EXTERNAL FUSELAGE SKIN LOCATED BTW BS 897 - 913 AND STGR 27. EXTERNAL FUSELAGE SKIN LOCATED BTW FS 897.00 TO FS 913.00 AND STGR 27 WAS REPAIRED PER REO 670-53-00-290 REV. -F, PL 670-53-00-29 0 SHEET #5, REV.-E FIGURE 3.
CRACK ON UPPER / LOWER SUPPORT BRACKET OF PYLON TIE-BAR, THROUGH PYLON ACCESS PANELS 433BT AND 433BB AT LH ENGINE.. UPPER / LOWER SUPPORT BRACKET OF PYLON TIE-BAR, THROUGH PYLON ACCESS PANELS 433BT AND 433BB AT LH ENGINE WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIR PER CRJ900 SRM 55-31-00-201-001-A01
"CORROSION ON ACCESS PANEL 832EL AND CORROSION ON HINGE AT ACCESS DOOR 832ET CORROSION WAS REMOVED OF ACCESS PANEL 832EL PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN LIMITS PER CRJ-900 SRM 52-11-32-101-001-A01, HINGE (P/N: CC670-31981-3) AT ACCESS PANEL ""832ET"" WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-A01."
CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ900 SRM-55-31-00-201-001-A01
"ON FINAL APPROACH, ""GEAR DISAGREE"" WARNING MESSAGE. GEAR DID NOT COME DOWN. RECYCLED LANDING GEAR LEVER 2 TIMES. GEAR STILL DID NOT COME DOWN RAN QRH. PER QRH RELEASED GEAR VIA MANUAL GEAR RELEASE. THEN WE RECEIVED GREEN INDICATIONS ON ALL THREE. AFTER LANDING, USED RUDDERS TO EXIT RUNWAY VIA HIGH SPEED TAXIWAY, BECAUSE OF ""STEER INOP"" CAUTION MESSAGE. WE WERE THEN TAKEN TO GATE VIA TUG. R/R LANDING GEAR SELECTOR VALVE IAW CRJ-900 AMM 32-32-10 LEAK CHECK GOOD. LANDING GEAR EXTENSION AND RETRACTION TEST REQUIRED REFER TO LOGPAGE 4041375-1 "
RIGHT SIDE WINDSHIELD HEAT CONTROLLER POPPED DURING CRUISE. SPARKS SMOKE AND FUMES PRESENT, SIMULTANEOUSLY DISPLAYING RIGHT WINDSHIELD HEAT CAUTION MSG. RAN RIGHT WINDSHIELD HEAT QRH PROCEDURE AND SHUT OFF RIGHT WINDSHIELD HEAT CONTROLLER. THERE WERE NO POPPED CIRCUIT BREAKER OR CRACKS ON RIGHT WINDSHIELD PRESENT. C/W TS 002736-R1 PLACED RH W/S HEAT ON MEL IAW MEL 30-41-1A . PLACARD INSTALLED MOC NOTIFIED 103619 , NO DAMAGE NOTED ON W/S////////REMOVED & REPLACED RH WINDSHIELD IAW JC 900-56-900-901. OPS & LEAK CHECKS GOOD. THIS CLEARS CONTROL #4041353-1. MMO2 UPDATED, PLACARD REMOVED, MOC #7821
GEAR DISAGREE WARNING AFTER GEAR RETRACTION HANDLE SELECTED UP. ALL GEAR REMAINED DOWN AFTER CYCLNG HANDLE. GEAR WAS ABLE TO RETRACT ON THIRD ATTEMPT. R/R LANDING GEAR SELECTOR VALVE IAW AMM 32-32-10 REFER TO NRWC #869574, 869575, AND 869803 FOR WORK PERFORMED REQUIRED OPS TEST FOR LANDING GEAR SELECTOR VAVLE AND LANDING GEAR CONTROL PANEL LEVER REFER TO CONTROL # 4001830-1 . ALL OPS CHECK GOOD.
ON INITIAL CLIMB OUT HEARD VIBRATION FOLLOWED BY A LOUD BANG, SAW OBJECT FLY BY FO WINDOW EMERGENCY DECLARED WITH ATC, RETURNED TO LAND IN ATL, NO ABNORMAL INDICATIONS ON EICAS ON POST FLIGHT WALK AROUND, A PIECE OF HEAD SET JACK WAS DISCOVERED STILL CONNECTED IN SERVICE PANNEL. FOUND LARGE DENT ON RIGHT ENGINE COWL AND DAMAGE TO FAN BLADES. R/R RIGHT ENGINE ASSY IAW JOBCARD 900-72-430-902. ALL OP/C & LEAK CHECKS GOOD.
FWD EMERGENCY FLOOR LIGHT HAS BURNT OUT BULBS R/R BULBS IAW CRJ900 AMM 33-51-11 OPC GOOD P/N OFF/ON 3071BPEGPL
NOTED AFT EMERGENCY LIGHTS OVER WING WENT DIM/OUT R+R BATTERY PACK PS43 PER AMM REF. 33-15-17 PERFORMED OPS TEST PER AMM REF. 33-51-17 OPS TEST GOOD AT THIS TIME P/N OFF/ON 2013-1ASMI S/N OFF 14058 S/N ON 16248
CORROSION FOUND ON PAX DOOR CLIP AT FS 313.56 BETWEEN DD4 AND DD5 INTERCOSTALS REMOVED CLEAT, AND REPLACED WITH NEW CLIP, PART NUMBER: 600-31902-269 WITH NEW FASTENERS. REF. CRJ900 SRM 51-42-06-001-001-A01.
CORROSION FOUND ON PAX DOOR STAIR LOWER ANGLE AT MULTIPLE LOCATIONS INSTALLED NEW REPLACEMENT PAX DOOR STAIR LOWER ANGLE. REF CRJ900 SRM 51-42-13-001-001-A01, SRM 51-45-00-001-001-A01
PAX DOOR STAIR STEP LOWER CUP FEED THROUGH CASTING IS CRACKED REMOVED AND REPLACED PAX DOOR STAIR STEP LOWER CUP FEED THROUGH CASTING P/N 601R317077-3 WITH NEW FASTENERS. REF CRJ 900 SRM 51-42-06-001-001-A01
PAX DOOR FWD FORMER SUPPORT ANGLE AT FS311.75 HAS EXFOLIATED CORROSION. EVALUATED, CORRODED, PAX DOOR, FORWARD FORMER SUPPORT ANGLE AT FS311.75, AS OUT-OF-LIMITS. REMOVED CORRODED FORMER SUPPORT ANGLE AND INSTALLED NEW SUPPORT ANGLE PN: 601R318731-3. REF.CRJ900 SRM 51-42-06-001-001-A01.
CORROSION FOUND ON PAX DOOR FRAME AT FS 313.56 BETWEEN DD4 AND DD5 INTERCOSTALS REMOVED FRAME SECTION AND REPLACED WITH NEW FRAME SECTION PART NUMBER: 601R318086-1 WITH NEW FASTENERS. REF. CRJ900 SRM 51-42-06-001-001-A01.
CORROSION FOUND ON PAX DOOR FORMER AT FS 329.41 BETWEEN DD5 AND DD6 INTERCOSTALS REMOVED AND INSTALLED A NEW PAX DOOR FORMER AT FS329.41 BETWEEN DD5-DD6 WITH NEW FASTENERS. REF CRJ 900 SRM 51-42-06-001-001-A01.
THE CABIN FLOOR SEAT TRACK AT RBL9 BETWEEN FS847+62 AND FS977 HAS MULTIPLE SPOTS OF CORROSION AND SCRATCHES. REMOVED AND REPLACED NEW FLOOR SEAT TRACK AT RBL9 BETWEEN FS847+62 AND FS977 REF CRJ900 AMM 53-00-49-000-801-A07 AND CRJ900 AMM 53-00-49-400-801-A07.
THE CABIN FLOOR SEAT TRACK AT LBL9 BETWEEN FS847+62 AND FS977 HAS MULTIPLE SPOTS OF CORROSION AND SCRATCHES EVALUATED CABIN FLOOR SEAT TRACK AT LBL9 BETWEEN FS.847+62 AND FS.977, FOUND TO BE OUT OF LIMITS REF CRJ900 SRM 53-41-49-101-001-A02, AND 53-51-49-101-001-A02. FABRICATED A NEW SEAT TRACK REF CRJ-900 SRM 53-00-49-201-002-A01 REMOVED AND INSTALLED SEAT TRACK NEW SEAT TRACK REF. CRJ-900 AMM 53-00-49-400-801-A07
THE PASSENGER DOOR INTERNAL STRUCTURE'S INTERCOSTAL DD6 BETWEEN FS320.163 AND FS338.963 HAS CORROSION ON ITS FLANGES AND WEB. REMOVED PAX DOOR INTERCOSTAL DD6 BETWEEN FS 320.163 AND FS 338.963, ORDERED AND RECEIVED, LOCATED AND DRILLED, AND INSTALLED NEW INTERCOSTAL PER CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
AFT SIDE OF BULKEAD FS1098.20 AT STRG 24L. CLIP HAS THE APPEARANCE OF A CRACK IN UPPER CORNER. REMOVED AND REPLACED CLIP WITH NEW CLIP P/N: MM670-35192-001. REF CRJ900 SRM 51-42-006-001-001-A01. DWG MM670-35012 REV G
THE AFT BAG BAY DOOR SURROUND LOWER SILL HAS MULTIPLE LOCATION OF CORROSION. REMOVED AND REPLACED AFT CARGO DOOR SILL. ASSY REF DWG MM670-35085 REV L. CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01.
MAIN CABIN FLOOR SEAT TRACK CORRODED AT LBL9 BETWEEN FS.661+32 AND FS.693.00
THE CABIN FLOOR SEAT TRACK AT RBL9 BETWEEN FS847 AND FS847+48 HAS MULTIPLE SPOTS OF CORROSION AND SCRATCHES.
THE PAX DOOR SURROUND AFT ANCHOR FITTING IS CHAFFED. INSTALLED A NEW PAX DOOR SURROUND LOWER AFT ANCHOR FITTING (SWIVEL-LEVER P/N CC670-31982-5) WITH NEW HARDWARE. REF CRJ900 AMM 52-11-17-400-803.
THE PAX DOOR SURROUND LOWER FWD ANCHOR FITTING IS CHAFFED. INSTALLED A NEW PAX DOOR SURROUND LOWER FWD ANCHOR FITTING (SWIVEL-LEVER P/N CC670-31982-6) WITH NEW HARDWARE. REF CRJ900 AMM 52-11-17-400-803-A01
THE PAX DOOR SURROUND LOWER FWD PIN STOP FITTING IS CHAFFED. REPLACED PAX DOOR SURROUND LOWER-FORWARD STOP FITTING WITH NEW PN:601R38388-7. REF. CRJ900 AMM 52-11-02-400-830-A01
THE PAX DOOR SURROUND LOWER AFT PIN STOP FITTING IS CHAFFED. INSTALLED NEW PAX DOOR SURROUND AFT PIN STOP FITTING REF CRJ900 AMM 52-11-02-400-830-A01.
THE PAX DOOR SURROUND AFT LATCH FITTING IS CHAFFED. REMOVED AND INSTALLED NEW SERVICEBLE PAX DOOR AFT UPPER PIN STOP FITTING. REF. CRJ900 AMM 52-11-02-000-830-A01
THE PAX DOOR SURROUND AFT CAM FITTING IS CHAFFED. INSTALLED NEW PAX DOOR SURROUND AFT CAM FITTING REF CRJ900 SRM 51-42-21-001-001-A01
THE PAX DOOR SURROUND FWD CAM FITTING IS CHAFFED. INSTALLED NEW PAX DOOR SURROUND FWD CAM FITTING IAW CRJ900 SRM 51-42-21-001-001-A01.
THE PAX DOOR SURROUND UPPER FWD STOP FITTING IS CHAFED. INSTALLED NEW PAX DOOR SURROUND FWD DROP DOWN STOP ASSY FITTING REF CRJ900 SRM 51-41-02-001-001-A01
PANEL 584ET IS CHAFED. RECEIVED LOCATED AND DRILLED NEW PANEL ASSY, VANE ACCESS, FLAP INBD. PN#CC670-140027-3. REF CRJ900 SRM 51-40-11-001-001-A01.
PASSENGER DOOR SUSPECTED AFT DRAG ANGLE CRACKED BY THE MOTOR ASSIST PULLEY. INSTALLED NEW DRAG ANGLE REPAIR SECTION AND 2 EA SPLICE ANGLES TO PAX DOOR AFT WEB DRAG ANGLE REF CRJ900 SRM 52-11-04-201-001-A01 REPAIR TYPE 1
CORROSION FOUND ON PAX DOOR FWD STAIR WEB AT MULTIPLE LOCATIONS REPLACED PAX DOOR FWD STAIR WEB REF CRJ 900 SRM 51--42-06-001-001-A01
CORROSION FOUND ON PAX DOOR AFT STAIR WEB AT MULTIPLE LOCATIONS REPLACED PAX DOOR AFT STAIR WEB WEB REF CRJ900 SRM 51-40-11-001-001-A01
CORROSION FOUND ON PAX DOOR INNER SKIN AT MULTIPLE LOCATIONS INSTALLED NEW INNER SKIN TO PAX DOOR REF CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01
R/H FORWARD OVER WING EMERGENCY EXIT DOOR HAS A SUSPECTED CRACK IN THE CAST BODY AT THE BASE OF ONE HOOK FITTING, MARKED. COMPLIED WITH FINAL REVISION OF ENDEAVOR EA NO: CRJ952-13562, ISSUE DATE: 5/12/2022,REV -IR. FOR RH FWD OVER WING EMER EXIT DOOR CRACK REPAIR.
L/H FORWARD OVER WING EMERGENCY EXIT DOOR HAS A SUSPECTED CRACK IN THE CAST BODY AT THE BASE OF ONE HOOK FITTING, MARKED. PERFORMED REPAIR AT THE LH OVER WING EMER EXIT DOOR CAST BODY AT HOOK FITTING REF. ENDEAVOR AIR EA NO. CRJ952-13584 REV.IR DATED 5/11/2022
L/H AFT OVER WING EMERGENCY EXIT DOOR HAS A SUSPECTED CRACK IN THE CAST BODY AT THE BASE OF ONE HOOK FITTING, MARKED. CUT AWAY DAMAGED AREA AND INSTALLED REPAIR DOUBLER REF. ENDEAVOR AIR EA CRJ952-13583 DATED 5/11/2022 REV IR STEP 9.
MAIN CABIN FLOOR SEAT TRACK CORRODED AT RBL9 BETWEEN FS.661+32 AND FS.693.00 INSTALLED NEW SEAT TRACK AT RBL9 BETWEEN FS.661+32 AND FS.693.00. REF. CRJ-900 AMM 53-00-49-400-801-A07
LEADING EDGE SKIN ON PANEL 622CB HAS DAMAGE. EVALUATED DAMAGED PANE #622CB. SUBMITTED TO ENGINEERING AND RECEIVED COMPLIED WITH ALL STEPS OF EA CRJ-957-13325 REV A 4-30-2022
DAMAGE PANEL 699AB, CHAFE (IS MARKED). BLENDED CHAFE DAMAGE FROM PANEL 699AB REF CRJ900 SRM 51-12-00-001-001-A01. FOUND TO BE OUT OF LIMITS REF CRJ900 SRM 57-61-01-001-001-A01 AND CRJ900 SRM 57-61-01-101-001-A01. DRILL AND LOCATED NEW 699AB PANEL REF 900 SRM 51-40-11-001-001-A01.
THE CABIN FLOOR SEAT TRACK AT LBL9 BETWEEN FS847 AND FS847+48 HAS MULTIPLE SPOTS OF CORROSION AND SCRATCHES. "BLENDED-OUT DAMAGE ON CABIN FLOOR SEAT TRACK AT FS847.00 AND FS847+48, AND EVALUATED AS OUT-OF-LIMITS. FABRICATED NEW SEAT TRACK. REF. CRJ900 SRM 51-40-11-001-001-A01."
FORWARD BAGGAGE BAY DOOR SURROUND, FORWARD EDGE NUT PLATE BRACKET CORRODED. EVALUATED, CORRODED, FORWARD BAGGAGE BAY DOOR, FORWARD EDGE NUT PLATE BRACKET AS OUT-OF-LIMITS. REMOVED BRACKET, AND REPLACED WITH NEW, FABRICATED BRACKET PN: SH670-33385-9. REF. CRJ900 SRM 51-42-06-001-001-A01
STGR26R CORRODED FS1031.00 â FS1047.00. INSTALLED NEW STRINGER 26R SPLICE AT APPROX. FS1031.00-FS1088.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG MM690-35007 REV-U
THE PASSENGER DOOR INTERNAL STRUCTURE'S FWD FORMER AT FS311.75 HAS CORROSION ON ITS WEB AND FLANGE BEHIND ACCESS PANEL 832FL. REMOVED AND REPLACED WITH NEW PAX DOOR FWD FORMER AT FS311.75 PER CRJ900 SRM 51-42-06-001-001-A01 & BOMBARDIER DRAWING 601R31702 REV-N.
FRAME CORRODED AT FS1031.00 BETWEEN STRG. 26R AND STGR. 25R REPAIRED FRAME SECTION AT FS.1031 STRG 25R AND 26L PER EA NO: CRJ953-13596 DATE 5-16-22 REV IR
CORROSION FOUND ON CLEAT AT JUNCTION OF FS 320 FRAME AND DD4 INTERCOSTAL INSTALLED A NEW CLEAT AT FS320.00 FRAME AND DD4 INTERCOSTAL, P/N 600-31902-269 WITH NEW FASTENERS. REF CRJ 900 SRM 51-42-06-001-001-A01
AFT SIDE OF BULKHEAD FS 1098.20 AT STRG 24L CLIP HAS THE APPEARANCE OF A CRACK. REPLACE CLIP IAW DWG MM670-35012 REV G. LOCATED AND DRILLED NEW CLIP IAW CRJ900 SRM 51-40-11-001-001-A01
FS280 ANGLES AT RBL 7.0 POSSIBLE CRACK LOCATED, DRILLED AND REPLACED 2 EA ANGLES IAW BOMBARDIER DWG #CC670-34010 REV J
THE AFT BAY DOOR SURROUND LOWER SILL HAS MULTIPLE LOCATIONS ON CORROSION REPLACED AFT DOOR SILL IAW DWG MM670-35085 REV L
STRINGER 21R AT APPROX FS969.00 IS CORRODED. REPAIRED STRINGER 21R BETWEEN FS942.00 AND FS927.00 REF CRJ900 ENDEAVOR AIR EA NO. CRJ953-13581 REV A DATED 6/7/22. PRESSURE LEAK CHECK GOOD.
BATTERY CHARGER AND BATTERY PACK #4 FAIL OPERATIONAL TEST OF THE EMERGENCY LIGHTS. REMOVED AND INSTALLED NEW EPSU BATTERY PACK AND BATTERY CHARGER REF CRJ900 AMM 33-51-17-400-801-A02. OP TESTS GOOD.
LH FWD OVERWING PSGR EMERENCY EXIT DOOR HAS A SUSPENDED CRACK IN THE CAST BODY AT THE BASE OF ONE HOOK FITTING. CUT AND REMOVE DAMAGE AND INSTALL REPAIR DOUBLER AND FITTING.
L FWD E LIGHT BULB OUT ON EXTERIOR. DEFERRED L FWD E LIGHT BULB ON EXTERIOR IAW MEL 33-51-2A MOC NOTIFIED 96365 PLACARD INSTALLED MM02 UPDATED///R&R LIGHT BULB IN THE EXTERIOR EMERGENCY LIGHT IAW CRJ 900 AMM 33-51-15 OPS TEST GOOD MM02 UPDATED, PLACARD REMOVED, MOC #95974
PART RACKS: BENT ON METALIC GUIDES AT AFT CORE COWLING OF RT ENGINE. SUMMARY, METALIC GUIDES AT AFT CORE COWLING OF RT ENGINE WERE REPLACED PER SRM 51-41-02-001-001-A01. ADDITIONAL PART NUMBER REPLACED CN625-2379-008.
INITIAL INSPECTION: CORROSION ON LOWER SILL STRIKER OF GALLEY SERVICE DOOR SURROUND STRUCTURE. (PTAS)(TCI: 53-20-219). SUMMARY. CORROSION LEVEL 2, ON LOWER SILL STRIKER OF GALLEY SERVICE DOOR SURROUND STRUCTURE WAS REPLACED PER SRM 51-42-06-001-001-A01.
INITIAL INSPECTION. BROKEN AND BENT ON LOWER PRESSURE SEAL RETAINER IN FWD/AFT CORNER AT CENTRAL BAGGAGE BAY DOOR. (CCD) SUMMARY. LOWER PRESSURE SEAL RETAINER WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR. 6A UPPER PRESSURE RETAINER AND PRESSURE SEAL WILL BE ATTENDED WITH NRC 00161.
INITIAL INSPECTION: DENT ON SCUFF PLATE OF SOURROUND STRUCTURE AT THE FWD BAGGAGE BAY DOORS (CCD). SCUFF PLATE FWD BAGGAGE BAY DOORS WERE REPLACED PER AMM 25-52-01.
INITIAL INSPECTION : CORROSION ON ANGLE SUPPORT CRAWLWAY FLOOR PANELS AT MAIN AVIONICS COMPARTMENT (E/E) (TCI: 53-10-219). SUMMARY. CORROSION LEVEL 2. ANGLE SUPPORT CRAWLWAY FLOOR PANELS AT MAIN AVIONICS COMPARTMENT (E/E) WAS REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01.
INITIAL INSPECTION; WEAR ON PRESSURE BOX SKIN AT LOW PRESSURE GROUND AIR CONECTION. (FUS) SUMMARY: REPAIR PLATE WAS REPLACED PER EA NR CRJ953-09612,REV IR.
INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT STA FS. 280 BTW LBL9 AND RBL9 AT COCKPIT (TCI: 53-10-219). CORROSION LEVEL 2. FLOOR SUPPORT STA FS 280 BTW LBL9 AND RBL9 AT COCKPIT WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6A AND SRM 51-42-20-001-001-A01 PAR 6A.
INITIAL INSPECTION: CORROSION ON SCUFFT PLATE ANGLE SUPPORTS (4EA) AT GALLEY SERVICE DOOR LOWER SURROUND STRUCTURE. (PTAS)(TCI:53-20-19). SUMMARY: ANGLE SUPPORTS (2EA) IN FS:319 AND FS:333 WERE REPLACED PER SRM 51-42-06-001-001-A01 PAR 6A AND CORROSION ON ANGLE SUPPORTS (2EA) FS:310 AND FS:349 WAS REMOVED PER SRM 51-21-06-001-001-A01.
AWR; HIDDEN DAMAGE: CRACK ON CROSSBEAM FS 280 RBL 14 IN REF NRC 252, TCI: 53-10-219 (CPAX). CROSSBEAM FS 280 RT REPLACED PER SRM 51-42-06-001-001-A01 PAR 6A, SRM 51-42-10-001-001-A01 PAR 8A. AND SRM 51-42-20-001-001-A01 PAR 6A.
INITIAL INSPECTION: CORROSION ON MOUNTING ANGLE AT LOWER SERVICE DOOR SURROUND STRUCTURE. (TCI 53-20-219). (PTAS). SUMMARY: MOUNTING ANGLE AT LOWER SERVICE DOOR SURROUND STRUCTURE WAS REPLACED SRM 51-42-06-001-001-A01.
AWR; HIDDEN DAMAGE: CRACK ON CROSSBEAM FS 280 LBL14 IN REF NRC 252, TCI: 53-10-219 (CPAX). CROSSBEAM FS 280 LT WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6A, SRM 51-42-10-001-001-A01 PAR 8A AND SRM 51-42-20-001-001-A01 PAR 6A.
NOTED CABIN EMERGENCY LIGHT CEILING LEVEL ROW 1 INOPERATIVE. FOUND CONNECTOR FOR ROW 1 EMERGENCY LIGHT LOOSE. CONNECTED. PERFORMED OPS TEST OF EMERGENCY LIGHTS ALL NORMAL IAW AMM 33-51.
WHILE INCORPORATING SB 670BA-57-020 FOUND 1 FASTENER HOLE IN THE RT MAIN LANDING GEAR AFT DOOR HINGE AFT HOLE TO BE OVERSIZED TO .4355. REPAIRED RT MAIN LANDING GEAR AFT DOOR HINGE AFT FASTENER HOLE IAW REO 690-57-21-307.
FWD FA FLASHLIGHT SEAL BROKEN AND THE FLASHLIGHT NOT CHARGING. REMOVED & REPLACED THE FWD FA FLASHLIGHT & SEAL IAW AMM 25-61-02 OPS CHECKED GOOD.
FWD FA POB MISSING FACE MASKS. REPLACED TWO O2 BOTTLE MASK IAW AMM 35-31-04.
FWD LAVATORY SMOKE ALARM ACTIVATED DURING PREVIOUS FLIGHT, POWERED DOWN AIRCRAFT PERFORMED AN OPS CHECK OF THE FWD LAVATORY SMOKE DETECTOR IAW AMM 26-16-00, NO DEFECTS NOTED. OK FOR SERVICE.
FIRST OFFICER`S OXYGEN MASK FAILED A PRE-FLIGHT CHECK. R & R THE OXYGEN MASK IAW AMM 35-11-12, OPS CHECKED GOOD.
AFT PBE HAS NO VACUUM. REMOVED AND REPLACED THE PBE IAW AMM 35-31-06.
EMERGENCY EXIT LIGHTS IN GALLEY, LT LOWER, RT FWD & RT AFT HAVE BULBS INOPERATIVE. REPLACED THE BULBS IAW AMM 33-51-11.
WEB BS 349 - 364, LBL 3 FOUND CORRODED. REMOVED AND REPLACED THE WEB IAW SRM 51-42-06, AND 51-42-21. AAR SM-33
E & E BAY FRAME BS 295 IS CORRODED BETWEEN STRINGERS 23L - 23R. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-21-1308. REPAIRED IAW REO 670-53-21-799.
E & E BAY FRAME AT BS 310 IS CORRODED BETWEEN STRINGERS 23L - 23R. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, REPAIRED IAW REO 670-53-21-799.
STRINGER SPLICE 26R CORRODED AT BS 333, FOUND TO BE OUT OF LIMITS. INSTALLED A NEW STRINGER SPLICE IAW SRM 51-42-06, AND 51-42-21.
STRINGER SPLICE 26L CORRODED AT BS 333, AND FOUND OUT OF LIMITS. INSTALLED A NEW STRINGER SPLICE IAW SRM 51-42-06, AND 51-42-21.
STRINGER 26L CORRODED, BS 333 - 349, FOUND TO BE OUT OF LIMITS. INSTALLED A NEW STRINGER IAW SRM 51-42-06, AND 51-42-21.
STRINGER SPLICE 24R AT BS 333 IS CORRODED OUT OF LIMITS. INSTALLED A NEW STRINGER SPLICE IAW SRM 51-42-06, AND 51-42-21.
STRINGER 26R FOUND CORRODED, BS 280 - 333 AROUND FASTENERS. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06.
STRINGER 25L CORRODED AROUND FASTENERS, BS 319 - 333, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06.
STRINGER 24R FOUND CORRODED BETWEEN BS 280 - 333, AROUND FASTENERS. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06, AND 51-42-21.
FWD EQUPMENT BAY LT SIDE SHELF CRACKED IN THE CORNER OTBD OF HYDRAULIC GAUGES. REPAIRED THE SHELF IAW REO 670-53-11-509, REV D.
FWD EQUIPMENT BAY, RT SIDE SHELF UNDER HAND PUMP CRACKED IN THE OTBD CORNER. REPAIRED IAW REO 670-53-11-509, REV D.
STRINGER 19R, BS 280 - 319 CORRODED AROUND FASTENERS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06, AND 51-42-21.
WHILE INSTALLING RADIO ALTIMETER ANTENNA FOUND CORROSION ON THE MOUNTING PLATE AT BS 1012. REMOVED THE CORRODED ANTENNA MOUNTING PLATE AND INSTALLED A NEW PLATE IAW SRM 51-42-06, PARA 6.
WHILE INSTALLING RADIO ALTIMETER ANTENNA FOUND CORROSION ON MOUNTING PLATE AT BS 1078. REMOVED CORRODED ANTENNA MOUNTING PLATE AND INSTALLED A NEW PLATE IAW SRM 51-42-06, PARA 6.
WHILE INSTALLING RADIO ALTIMETER ANTENNA FOUND CORROSION ON MOUNTING PLATE AT BS 1033.83. REMOVED THE CORRODED ANTENNA MOUNTING PLATE AND INSTALLED A NEW PLATE IAW SRM 51-42-06, PARA 6.
PAX DOOR POWER ASSIST MOTOR LOWER BRACKET IS CRACKED. REMOVED AND REPLACED THE LOWER BRACKET IAW SRM 51-42-06, AND SRM 51-42-21.
PAX DOOR TOP WEB IS CRACKED ON AFT CORNER. REMOVED THE DAMAGE, CUTOUT AND INSTALLED A REPAIR IAW SRM 52-11-04.
MEGAPHONE FOUND BROKEN DURING EE-900. R & R THE MEGAPHONE IAW AMM 25-60-00. OPS CHECKED GOOD.
MEGAPHONE SIREN FUNCTION INOP. REMOVED MEGAPHONE & INSTALLED SERVICABLE UNIT IAW 25-61-14.
LENS ON FLOOR TRACK LIGHTING AT SEAT 3A BROKEN AND MISSING SECTION. REMOVED & REPLACED FLLOR TRACK LENS AT SEAT 3A IAW AMM 33-51-0. 1 "
AFT CARGO DOOR, FLOOR SILL IS CORRODED BETWEEN FS 1000.00 AND FS 1047.00. CONTINUATION CARD 81514111, OPS 99 & 202. R & R CARGO DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 & 51-42-21-001-001-A01.
STRINGER 21R IS CORRODED BETWEEN BS 969 - 927 IN MULTIPLE LOCATIONS. REPAIRED THE STRINGER IAW SRM 51-21-06-001-001-A01, 53-51-03-101-003-A02, 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01 AND 51-42-06-001-001-A01. "
STRINGER 24R IS CORRODED AT BS 969. REPAIRED THE STRINGER IAW EA CRJ953-04523.
MLG FAIRING 193AB, LT AND RT SUPPORT STRAPS ARE CORRODED. CONTINUATION CARD 81514111, OP 192. REPLACED SUPPORT STRAPS ON MLG FAIRING 193AB IAW SRM 51-42-13-001-001-A01, 51-42-15-001-001-A01, 51-40-11-001-001-A01, 51-25-01-001-001-A01, AMM 51-23-00-390-820-A01 AND DWG NR PL CC670-39004. CURE CHECK GOOD.
FS 280, J-ANGLE CORRODED. R & R FS 280, J-ANGLE, PN:CC670-34905-35 IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
PASSENGER DOOR SILL ANGLE CORRODED BS 310 - 349. REMOVED & REPLACED THE DOOR SILL ANGLE IAW SRM 51-41-02-001-001-A01. "
FS 280.00 LT CROSSBEAM IS CORRODED. CONTINUATION CARD 81514111, OP 169. R & R LT FS 280.00, CROSSBEAM, PN CC670-34094-1 IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 & EO R53117.
FS 280.00, RT CROSSBEAM IS CORRODED. CONTINUATION CARD 81514111, OP 168. R & R RT FS 280.00, CROSSBEAM, PN CC670-34094-2 IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 & EO R53117.
SEAT TRACK SEGMENT AT RBL 9 IS CORRODED BETWEEN FS 349 - 394. REMOVED & REPLACED THE SEAT TRACK SEGMENT IAW AMM 53-00-49-400-801-A07. "
INBD FLAP PANEL 584GB IS CHAFED. REPLACED INBD FLAP PANEL 584GB IAW SRM 51-40-11-001-001-A01 AND 51-25-01-001-001-A01.
RT SIDE SEAT TRACK SEGMENT BETWEEN FS 379.00 AND FS 482.00 IS GOUGED AT FS 469.00. R & R SIDE SEAT TRACK SEGMENT BETWEEN FS 379.00 AND FS 482.00 IAW REO:670-53-00-343 AND AMM 53-00-49-400-801-A07.
RIGHT SIDE SEAT TRACK SEGMENT IS GOUGED AT BS 661+62. REMOVED AND REPLACED THE SEAT TRACK FROM 661+16 TO 669.4 IAW AMM 53-00-49-400-801-A07 AND REO 670-53-00-343. "
RIGHT SIDE SEAT TRACK HAS A WORN AND DAMAGED LUG AT BS 813.7. REMOVED AND REPLACED THE SEAT TRACK FROM BS 785.15 - 847 IAW AMM 53-00-49-400-801-A07 AND REO 670-53-00-343. "
LEFT SIDE SEAT TRACKS CORROSION AT BS 708. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-400-801-A07, REO 670-53-00-343, AND SRM 51-4 0-11-01-001-001-A01. "
LEFT SIDE SEAT TRACK SEGMENT IS CORRODED FROM BS 629 - 645, 661 TO 661+16, AND 613. FABRICATED A NEW SERVICEABLE SEAT TRACK BETWEEN BS 573 - 661+16 IAW REO 670-53-00-343 REV-M AND INSTALLED IAW AMM 53-00-49-400-801-A01. "
PANEL 642BZ HAS MINOR CORROSION AT MULTIPLE LOCATIONS. LOCATED AND DRILLED NEW PANEL 642BZ IAW SRM 51-40-11-001-001-A01.
LEFT SIDE SEAT TRACK SEGMENT CORRODED AT BS 437 & 477.4. REMOVED AND REPLACED THE SEAT TRACK SEGMENT FROM BS 379 - 485 IAW AMM 53-00-49-400-801-A07 AND REO 670-53-00-343. "
INBOARD FLAP PANEL 684EB IS CHAFED. LOCATED AND DRILLED NEW PANEL 684EB IAW SRM 51-40-11-001-001-A01 AND 57-52-01-101-001-A01. REFER TO WVAC MASTER PANEL BOOK FOR INSTALL.
LEFT SEAT TRACK SEGMENT BETWEEN LEFT OVERWING EMERGENCY EXIT DOOR CUTOUTS HAS CORROSION AT BS 744.15. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, 53-00-49-400-801(A02).
LEFT SIDE SEAT TRACK SEGMENT FOUND CORRODED FROM BS 661+32 TO 661+46, 661+62 TO 661+74.00 AND FS 661+90 TO 669.4. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A07. "
RIGHT SIDE SEAT TRACK SEGMENT IS CORRODED IN SEVERAL AREAS FROM BS 661 - 661+16. REMOVED AND REPLACED THE SEAT TRACK SEGMENT BETWEEN BS 573 AND 661+16 IAW AMM 53-00-49-400-801-A07 AND REO 670-53-00-343.
RIGHT SIDE SEAT TRACK SEGMENT IS CORRODED AT BS 549 AND GOUGED AT BS 565. REMOVED AND REPLACED THE SEAT TRACK BS 482 - 612 IAW AMM 53-00-49-400-801-A07 AND REO 670-53-00-343. "
LEFT SEAT TRACK SEGMENT CORRODED AT BS 509 AND 549. FABRICATED AND REPLACED THE SEAT TRACK BETWEEN BS 482 - 613 IAW REO 670-53-00-343 REV M AND AMM 53-00-49-400-801-A07. "
LEFT SIDE SEAT TRACK HAS TWO LOCATIONS OF CORROSION BS 813.7 AND 847. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, 53-00-49-400-801-A07 AND REO 670-53-00-343.
WINDOW POST MAP LIGHT ON THE F/O'S SIDE STARTED SMOKING, CB POPPED, CBP 2 G7. DEFER F/O'S MAP LIGHT IAW MEL 33-11-1A, CAT "C". R & R F/O'S WINDOW POST MAP READING LIGHT WITH NEW LIGHT AND OP CHECKED GOOD IAW AMM 33-13-03-000/-400-801 AND 33-13-03-710-801-A01.
CAPTAINS O2 MASK LEAKS, WILL NOT STOP FLOWING IN TEST. REPLACED IAW AMM 35-11-12, PN MF10-08-01, SN ON SE 18540I & SN OFF SE14869. OPERATIONS CHECKED GOOD AT THIS TIME. OK FOR SERVICE. REPLACED FIRST OFFICERS STOWAGE BOX ALSO IAW AMM 35-11-15. OPERATIONS CHECKED AT THIS TIME OK FOR SERVICE. BOX PN MXP411-4, SN ON SE27794 & OFF SE30862.
GALLEY FLOOR ESCAPE LIGHTING NEEDS TO BE REATTACHED. SECURED EMER FLOOR PATH MARKER IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED.
EMERGENCY LIGHT THAT ILLUMINATES THE STAIRS IS CRACKED. REMOVE LENS COVER & INSTALLED A SERV UNIT IAW CMM 33-52-07.
AFTER TAKEOFF IN CLIMB, THRUST ACCELERATING FROM 200KTS - 250KTS 6000 FT, RT ENG LOUD NOISE, YAW RT, LOSS OF OIL PRESS, ITT SPIKED, ENG FLAMED OUT N1 & N2 DECELERATION. PERFORMED EAC ENG FIRE OR SEVERE ENG DAMAGE & ALL QRH PROCEDURES. REPLACED RT ENG PN ON & OFF CF34-8C5, SN OFF 194616 & SN ON 194734 IAW JC 900-72-430-906. OPERATIONS & LEAK CHECKS GOOD IAW 409 524919 & JC 900-72-430-902 FOR DETAILS.
FLASHLIGHT NOT WORKING FWD. R & R FWD FLASHLIGHT BATTERY IAW AMM 25-61-02. COMPLETED OPERATIONS TEST IAW 25-61-00. OPERATIONS TESTED GOOD, OK FOR SERVICE.
TASK CARD 900-52-810-305 FWD CARGO DOOR SEAL RETAINER BENT & CRACKED IN VARIOUS AREAS. DISPLACED FWD CARGO DOOR SEAL FOR ACCESS TO AREA IAW AMM 52-35-07-000-802-A02. R & R RETAINER IAW SRM 51-42-06-001-001-A01. REINSTALLED SEAL IAW AMM 52-35-07-400-802-A02. LEAK CHECKED GOOD IAW AMM 52-00-00-790-801A01.
TASK CARD CRJ 900 PANEL 684ET CHAFED. R & R PANEL 684ET IAW AMM 57-51-32-000-804-A01, 57-51-32-400-804-A01 & SRM 51-40-11-001-001-A01. PANEL WAS CHAFED BEYOND LIMITS SRM 57-52-01-101-001-A01.
TASK CARD CR FLIGHT DECK RT EMER FLASHLIGHT RED CHARGED LIGHT NO LONGER FLASHING, BATTERY PN P4-01-0021 EF-1 DME 25-60-02. REPLACED FLIGHT DECK RT EMER FLASHLIGHT BATTERY PACK IAW CMM 25-60-02 PG 6001 3 0 A - F.
TASK CARD 900-54-430-301 LT NACELLE UPPER & LOWER FWD COWL TO CORE, COWL RUB STRIPS CHAFED. REPAIRED LT NACELLE UPPER & LOWER COWL RUB STRIPS IAW SRM 54-23-00-201-007-A01.
TASK CARD 900-54-430-301 LEFT NACELLE LOWER HALF ACOC PAN DAMAGED. REPAIRED ACOC ON LOWER LT NACELLE IAW EO R54090 & ROUTINE 60013.
TASK CARD 900-26-430-100 LEFT AFT CORE COWLING STANDOFF BLOCK TABS WORN. R & R STANDOFF BLOCK ON LT AFT CORE COWLING IAW SRM 54-13-00-201-002-A01 & REO 690-54-13-097.
TASK CARD 900-57-900-300 PANEL 584EB CHAFED. R & R PANEL 584EB IAW AMM 57-51-32-000-801-A01, 57-51-32-400-801-A01 & SRM 51-40-11-001-001-A01.
TASK CARD 900-05-900-901 RIGHT ELEVATOR TE HAS LIGHTNING STRIKE DAMAGE. REPAIRED RT ELEVATOR TE LIGHTNING STRIKE DAMAGE IAW SRM 55-21-01-201-001-A01. APPLIED PAINT TO REPAIRED AREA IAW SRM 51-25-01-001-001-A01.
TASK CARD CRJ-900 PANEL 433BT CHAFED. DAMAGE FOUND TO BE OUT OF LIMITS .070 DEEP. REMOVED & INSTALLED STIFFENERS & SEALS FROM DAMAGED PANEL ON NEW PANEL IAW SRM 51-42-06-001-001-A01 & SRM 51-42-13-001-001-A01. OUT OF LIMITS SRM 54-12-01-101-001-A01.
TASK CARD 900-71-430-100 LT FWD COWL LOWER BLOW OUT DOOR HINGE & LATCH PLATE ARE WORN & THE UPPER BLOW OUT DOOR LATCH PLATE IS WORN. REMOVED LT LOWER & UPPER FWD COWL BLOW OUT DOOR LATCH PLATES IAW SRM 51-42-06-001-001-A01 & 51-42-10-001-001-A01. INSTALLED NEW LATCH PLATES IAW SRM 51-42-06-001-001-A01 & 51-42-13-000-001-A01. R & R LT LOWER BLOW OUT DOOR INBD HINGE IAW AMM 71-12-05-000-801-A01, SRM 51-42-21-001-001-A01 & AMM 71-12-05-400-801-A01.
TASK CARD 900-26-440-100 RT AFT CORE COWLING STANDOFF BLOCK TABS WORN. R & R RT AFT CORE COWL STANDOFF BLOCK IAW SRM 54-12-00-201-A01.
TASK CARD 900-54-440-301 RT ENG TR ALIGNMENT PINS DAMAGED. FOUND STRUCTURE UNDER RT ENG ALIGNMENT PINS BENT & CRACKED. REMOVED OTBD EDGE CHANNEL IAW SRM 51-42-06-001-001-A01 & 51-42-10-001-001-A01. INSTALLED NEW CHANNEL IAW SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01.
RIGHT ELEVATOR STRIKE DAMAGE NEAR INBD TE. REPAIRED IAW SRM 55-21-01-201-001-A01.
TSK CARD 900-52-810-306 CTR CARGO DOOR SEAL RETAINER BENT & BROKEN IN VARIOUS AREAS. REMOVED DAMAGED CTR CARGO DOOR SEAL RETAINER. REPAIR WITH NEW SEAL RETAINER IAW SRM 51-42-06-001-001-A01. LEAK CHECK WILL BE PERFORMED ON NR 46111 SEE ATTACHED COPY.
TSK CARD 900-53-900-504 FLOOR SILL CORRODED FROM FS 349 - 364. REPAIRED CORRODED AREA IAW CRJ 953-03362 & SRM 53-00-00-101-001-A01, 53-00-00-101-001-A01, 51-25-06-001-001-A01 & AMM 53-00-47-000-802-A01 & 53-00-47-000-807-A01 DEPTH GAUGE EXQS121 SCREW GUN 306-1.
TASK CARD 900-53-900-504 FLOOR SILL CORRODED FROM FS 280 - 310. REMOVED & REAPPLIED FINISHES. REMOVED CORROSION IAW SRM 51-25-06-001-001-A01, 51-25-16-001-001-A01 & 53-00-00-101-001-A01. REPAIRED THE DAMAGE AT STATION 310 IAW EA CRJ953-03361. COMPLETED EA CRJ953-03361 & ROUTINE CARD 60008 COPY ATTACHED.
EXIT ROW PHOTO LUMINESCENT STRIP NEEDS TO BE ATTACHED. SECURED FLOOR TRACK LIGHTING IAW AMM 33-51-01. OK FOR SERVICE.
DURING FLIGHT NOTICED ROW 12 EMER EXIT REFLECTIVE FLOOR STRIP MISSING. REPLACED MISSING FLOOR STRIP IAW 33-51-01. OPERATIONS CHECKED GOOD. OK FOR SERVICE.
FLOOR TRACK LIGHTING STRIP BY SEAT 13 B IS MISSING. INSTALLED FLOOR TRACK LIGHT IN FRONT OF 13B IAW AMM 33-51-01. ACFT OK FOR SERVICE.
FLIGHT ATTENDANT REPORTED MISSING EMER FLOOR LIGHTING STRIP IN FRONT OF TWO GALLEY CARTS. INSTALLED EMER FLOOR STRIP IAW AMM 33-51-01.
DURING FLIGHT SMOKE AFT LAVATORY WARNING ILLUMINATED FOR 2 SECONDS & EXTINGUISHED. PERFORMED OPERATIONS CHECK OF AFT LAVATORY SMOKE DETECTOR IAW CRJ-900 26-16-00. OPERATIONS CHECKED GOOD NO MSG DISPLAYED, ACFT OK FOR SERVICE.
REAR F/A JUMPSEAT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT. OPS CHECKED GOOD IAW AMM 25-61-00.
CTR AISLE AFT OVERHEAD E LIGHT RED LENS CAP MISSING. RED LENS CAP DEFERRED IAW N33-50-1 CAT E. 90 DAYS TRANSFERRED TO MM02 NOTIFIED.
AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IS NOT FLASHING RED. DEFERRED AFT FLIGHT ATTENDANT FLASHLIGHT IAW CRJ900 MEL 25-61-4A CAT C MXC 821723, ENTERED INTO MMO2, PLACARD PLACED. CREW HAS FLASHLIGHTS AVAILABLE. ACFT OK FOR SERVICE.
MID CABIN EMERGENCY EXIT SIGN FWD SIDE WAS MISSING, F/A EMERGENCY CALL LIGHT. INSTALLED SERVICEABLE LENS COVER IAW AMM 33-51-07.
INBD SPOILERON & INBD FLT SPOILERS CAUTION, 2A PUMP ON HYDRAULIC PAGE INTERMITTENT YELLOW, VIBRATION FELT THROUGHOUT ACFT. HYD 2, LOW PRESSURE. 2A PUMP SHUTDOWN, HYD EDP 2A CAUTION TEMP NORMAL QUANTITY 5 PERCENT, RT ENG SHUTDOWN AND EDP 2A OFF. DEACTIVATED NR 2 EDP IAW AMM 29-11-01. INSTALLED NEW EDP. OPS CHECKED GOOD IAW AMM 29-11-01.
LOWER FUSELAGE SKIN FS 1069.75 TO 1162, S21-22L, HAS MULTIPLE DENTS AT THE VENTRAL FIN FAIRING INTERFACE. RECONTOURED DENTED AREA TO WITHIN LIMITS CONDITION IAW REO 690-53-61-389 AND EO R53458.
LOWER FUSELAGE SKIN PANEL, FS 1069.75 - 1162, S21-22L, HAS MULTIPLE DENTS AT THE VENTRAL FIN FAIRING INTERFACE. RECONTOURED DENTED AREA TO WITHIN LIMITS CONDITION IAW REO 690-53-61-389 AND EO R53458.
UPON REMOVAL OF PAX DOOR LWR FWD PULL IN LEVER FOUND DOOR GOUGED BEHIND LEVER. IAW REO 690-52-11-257, REPAIRED PAX DOOR INNER SKIN & REPLACED PAX DOOR FWD FRAME.
FWD EQUIPMENT BAY SKIN CRACKED UNDER ADG PUMP. REPAIRED FWD EQUIPMENT BAY SKIN CRACK UNDER ADG PUMP IAW EO R53460.
PANEL 684EB IS CHAFED. REPAIRED PANEL IAW REO 690-57-52-153.
FWD CARGO DOOR AFT LOWER HINGE ARM IS GOUGED ON AFT SIDE. REPAIRED FWD CARGO DOOR AFT LOWER HINGE ARM IAW REO 690-52-35-093.
LEFT AILERON LOWER SURFACE L/E OTBD IS CHAFED. REPAIRED AILERON IAW EO R57139.
LOWER FUSELAGE SKIN PANEL, FS 1069.75 - 1162, STRINGER 21-22R HAS MULTIPLE DENTS AT THE VENTRAL FIN FAIRING INTERFACE. RECONTOURED DENTED AREAS TO WITHIN LIMITS CONDITION IAW REO 90-53-61-389 AND EO R53548. SM-74, A-247.
DURING REMOVAL OF CORROSSION ON RT FLOOR SUPPORT FOUND CORRODED BETWEEN FS 310 - 319. R & R CORRODED AREA IAW REO 690-53-21-511 AND EO R53457 S/M-114.
PAX DOOR LOWER SKIN PANEL BENT WITH GOUGE ON EDGE JUST FWD OF DOOR HINGE. REPAIRED PAX DOOR LOWER SKIN PANEL IAW REO 690-52-11-254 AND EO R52085 S/M-114.
LOWER FUSELAGE SKIN PANEL, FS 1162 - 1167.5 STRINGER 21-22R HAS MULTIPLE DENTS AT THE VENTRAL FIN FAIRING INTERFACE. DENTS ON LOWER FUSELAGE SKIN PANEL FOUND TO BE IN LIMITS IAW REO 690-53-71-014 AND EO R53549.
AFTER CLEANING, FOUND LONGERON 25L CORRODED, FS 333 - 364. R & R LONGERON 25L IAW SRM 51-42-06.
FWD E & E BAY STRINGER SPLICE 26R CORRODED. R & R STRINGER SPLICE IAW SRM 51-42-06, PN
AFTER CLEANING FOUND STRINGER 26R CORRODED, FS 295-333. R & R STRINGER IAW SRM 51-42-06.
FWD E & E BAY, STRINGER 25R CORRODED FS 295 - 333. R & R STRINGER IAW SRM 51-42-06.
STRINGER SPLICE 25R FOUND CORRODED FS 333 TO 364. R & R STRINGER 25R IAW SRM 51-42-06.
PANEL 584GB IS CHAFED. REPAIRED PANEL IAW REO 690-57-52-151 CLEARANCE CHECKED GOOD IAW REO 690-57-52-151.
RIGHT FLAP VANE PANEL 684ET CHAFED. LOCATED AND DRILLED NEW PANEL TO REPLACE PANEL 684ET IAW SRM 51-40-11.
FS 280 CROSSBEAM CENTER FWD ANGLE CORRODED. R & R CROSSBEAM ANGLE IAW SRM 51-42-06.
LEFT FS 280 FLOORBEAM CORRODED. R & R LT FLOORBEAM IAW EO ATR53455.
RT FS 280 BULKHEAD LOWER WEB CORRODED. REPAIRED BULKHEAD IAW EO R53456.
LEFT FS 280, BULKHEAD LOWER WEB CORRODED. REPAIRED BULKHEAD IAW EO R53456.
GALLEY SERVICE DOOR OUTER LOWER SKIN PANEL GOUGED. REMOVED GOUGES FROM GALLEY SERVICE DOOR OUTER LOWER SKIN IAW REO 690-52-41-026 AND EO R52084, S/M-112.
MID CARGO DOOR AFT LOWER HINGE ARM IS GOUGED ON THE AFT SIDE. REMOVED GOUGE ON MID CARGO DOOR AFT LOWER HINGE AND IS IN LIMITS IAW REO 690-52-35-094.
MID CARGO DOOR, FWD LOWER HINGE ARM IS GOUGED ON FWD SIDE. REMOVED GOUGE ON MID CARGO DOOR FWD LOWER HINGE ARM AND IS IN LIMITS IAW REO 690-52-35-094.
RT FS 280 CROSSBEAM CORRODED. R & R RT FS 280 FLOORBEAM IAW EO.
LT WING NR 2 SLAT IS CHAFED OTBD CORNER A250-019. REMOVED CHAFE ON LT WING 2 SLAT OTBD CORNER TO WITHIN LIMITS CONDITION IAW REO 690-57-42-256.
RT AFT OTBD WING TO FUSELAGE MOUNT CHAFED. REPAIRED RT AFT OTBD WING TO FUSELAGE MOUNT IAW REO 690-57-11-026 AND EO R57138.
LT AFT OTBD WING TO FUSELAGE MOUNT CHAFED. REPAIRED LT AFT OTBD WING TO FUSELAGE MOUNT IAW REO 690-57-11-025 AND EO R57137 S/M-114.
FOUND STRINGER SPLICE 25L CORRODED. R & R STRINGER SPLICE IAW SRM 51-42-06 PN SH670-32429-4.
FWD E & E BAY STRINGER SPLICE 25R CORRODED. R & R STRINGER SPLICE IAW SRM 51-42-06 PN SH670-32429-3.
FWD E & E BAY STRINGER 26R CORRODED. FS 333 - 364. R & R STRINGER IAW SRM 51-42-06.
PAX DOOR FWD CORNER COVER DENTED WITH 1EA DAMAGED RIVET. R & R CORNER COVER IAW SRM 51-42-13.
PAX DOOR AFT CORNER COVER DENTED WITH ONE DAMAGED RIVET. R & R CORNER COVER IAW CRM 51-42-13.
MEGAPHONE BATTERIES DEAD. R & R MEGAPHONE BATTERIES IAW ACR/EM 1A PORTABLE SAFETY MEGAPHONE MANUAL Y1-03-001, REV AC.
EMERGENCY FLOOR LIGHTING STRIP MISSING FROM EXIT ROW. REPLACED FLOOR LIGHTING STRIP AS REQUIRED. MXC NOTIFIED.
F/A REPORTS FWD EMERGENCY LIGHT SECURITY STRAP IS BROKEN AND LED LIGHT IS NOT FLASHING. DEFERRED FWD CABIN EMERGENCY FLASHLIGHT PER MEL 25-61-4A. REPLACED FWD F/A FLASHLIGHT WITH SERVICEABLE IAW CRJ-900 MM 25-61.
MULTIPLE INTERIOR AND EXTERIOR EMERGENCY LIGHTS DO NOT PASS OPS CHECK. REMOVED AND REPLACED EPSU BATTERY PACK NR 5 IAW AMM 33-51-17. OPS CHECKED GOOD.
RT FLOOR SUPORT CORRODED. REPAIRED RT FLOOR SUPPORT IAW RE0690-53-21-359 AND EO R53186.
SERVICE DOOR SILL CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL ANGLE IAW AMM 51-42-06 AND 51-42-21.
SERVICE DOOR THRESHOLD CORRODED. BLENDED CORROSION AND FOUND AREA TO BE WITHIN LIMITS WITH .001 MAT. LOSS AND 062 REMAINING IAW CRJ 900 SRM 53-21-23. AAR SM-48.
FLOOR SUPPORT AFT OF SERVICE DOOR CORRODED. BLENDED CORROSION AND FOUND AREA TO BE WITHIN LIMITS WITH .004. REMOVED AND .046 REMAINING IAW SRM 53-00-00. RESTORED FINISH IAW SRM 51-21-11 AND 51-21-16.
PAX DOOR SILL AT FLOOR LANDING CORRODED. REMOVED CORROSION FROM PAX DOOR SILL IAW SRM 51-21-06. FOUND TO BE IN LIMITS IAW SRM 53-00-00.
EMERGENCY STRIP LIGHT COVER MISSING IN GALLEY LEFT. REPLACED GALLEY FLOOR TRACK LIGHTING STRIP P/N 88-901LH00 AS REQ.
EMERGENCY LIGHTS CYCLE ON AND OFF IN THE ARM POSITION. REPLACED RELAY K198. OPS CHECKED GOOD IN ARM MODE AND PER AMM 33-51-00 OPS TEST.
PAX DOOR FIFTH STAIR RISER CRACKED AT NR3 STEP. REPAIRED DOOR AFT STAIR RISER ZONE 3 IAW REO 670-52-11-104 AND EO 52024.
PAX DOOR FWD STEP RISER CRACKED AT 2ND STEP ADJACENT TO RAIL SUPPORT. REPAIRED PAX DOOR FWD STEP RISER IAW EO R52022.
PAX DOOR RETRACT MOTOR MOUNT ANGLES RIVETS SHEARED AND SUPPORT WEB CRACKED. REPAIRED PAX DOOR AFT STAIR RISER ZONE 4 IAW REO 670-52-11-104 AND EO R52024.
RT HORIZONTAL STAB TIP FAIRING SUPPORT ANGLE BENT OTBD OF STAB END RIB UNDER PANEL 343BR/343AR. FABRICATED NEW RT STAB TIP RIB IAW EO AV670-23248 AND INSTALLED IAW SRM 51-42-06.
F/S 280 FLOOR SUPPORT ANGLE IS CORRODED ON UPPER AND LOWER SURFACE (ANGLE IS THE CAMLOCK RECEPTACLE ANGLE). R & R THE FS 280 FLOOR SUPPORT ANGLE IAW SRM 51-42-06 AND 51-42-20.
SEAT TRACK BY FWD LAV IS CORRODED. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801, PN SH670-32159-1.
A FLOOR PHOTO LUMINESCENT STRIP FOR EMERGENCY EXIT ROW 13AB IS MISSING. INSTALLED NEW FLOOR TRACK LIGHTING STRIP AT ROWS 13AB IAW CRJ900 25-10 AND MAL GMM 4.23.
AFTER TAKEOFF FROM KIND, 3596 EXPERIENCED A NOSE GEAR CAUTION EICAS MESSAGE, FOLLOWING THE POM, THE CREW RETURNED TO AND LANDED AT IND. I DID NOT RECEIVE INFORMATION AS TO THE EXACT EICAS MESSAGE, BUT IT WAS A FLASHING AMBER CAUTION MESSAGE. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ900 M/M 32-32-10 PN NR 53340-7/SN NR NGL/1681/08-OFF PN NR 53340-7/SN NR NGL/1558/06. OPS CHECK AND LEAK CHECK GOOD.