N426AW
Registered owner: SPIRE AVIATION II LLC, NC (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
AFTER TAKEOFF RECEIVED ANTISKID IB AND PAKING BRAKE SOV CAUTION MESSAGES AFTER GEAR SELECTED TO UP POSITION. GEAR INDICATED DOWN 3 GREEN WITH GEAR LEVER IN UP POSITION DID NOT RECEIVE GEAR DISAGREE WARNING. DID NOT EXCEED SPEED LIMITATIONS REMAINED UNDER 250 KTS. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPS CHECK OF ANTI SKID SYSTEM IAW AMM 32-44-00. OPS CHECK GOOD. INTERROGATED PSEU AND RECEIVED CODE DI 11 DWN OFF AND TS PER FIM 32-40-00 FOR PARKING BRAKE SOV MSG AND DID NOT RECIVE 28V AT P1GH PIN 1 AND PIN 2. SUSPECT LANDING GEAR CONTROL HANDLE OR LANDING GEAR CONTROL PANEL. REF FIM 32-60-00. FURTHER TS REQUIRED. INSTALLED LANDING GEAR PINS AND REMOVED FLAGS IAW AWA SUP 11-054A. IN PREPARATION FOR FERRY FLIGHT. REF W/O 339143 WC 4 AND 5 FOR WORK PERFORMED. (REMOVED AND REPLACED GEAR CONTROL HANDLE OPS CHECKED GOOD.
50057 334424 601R-57-21-3821 HRS 24.45 CRACK FOUND ON LOWER WING SKIN LANDING UNDER ACCESS PANEL 601R10213-4. AIRCRAFT REMOVED FROM SERVICE. (RH MLG) REPAIR WAS PERFORMED TO THE RH WING LOWER AFT PLANK BY MHI MRT. REF. MHI RJ REO 601R-57-21-3821 REV. A DATED 2-28-2024. SHOT PEENING HFEC & ROTO HOLE INSPECTIONS COMPLIED WITH RESTORED ALL PROTECTIVE FINISHES REF. MHI RJ REO 601R-57-21-3821 REV. A DATED 2-28-2024. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 004188 CARD NO. 20119. TT: 43, 201:59, TC: 41,865
CORROSION ON STRUCTURE AT FS605 BETWEEN STR 25R AND 26R. AIRCRAFT REMOVED FROM SERVICE. EVALUATED AND REMOVED CORROSION FROM FUSELAGE SKIN AT FS605 TO 621 STR 25R AND 26R REF CRJ200 SRM 53-00-00, AND 53-00-31 REV39, AND REMOVED AND REPLACED INTERNAL DOUBLER AT FS605 TO 621 STR 25R TO 26R REF CRJ200 SRM 51-40-11, REV 39. ACCOMPLISHED HFEC, AND RESTORED ALL PROTECTIVE FINISHES REF CRJ200 SRM 51-12-00, 51-25-06, 51-25-16 REV 39. ALL WORK PERFORMED UNDER WORK ORDER 004188 CARD NO. 20119. TT: 43, 201:59, TC: 41,865
CRACKED BRACKET ON PREVIOUS REPAIR ON AFT PRESSURE BULKHEAD NEAR LINTEL AT FS 629.00 AND LBL36. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CHANNEL AT FS 629.00 AND LBL36 WITH FABRICATED NEW CHANNEL. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-42-20 REV 39, SRM 51-24-21 REV 39, SRM 51-40-11 REV 39, SRM 51-12-00 REV 39, REV 39 AND SRM 51-25-16 REV 39. 51-25-06, REV 39.
RECEIVED GEAR DISAGREE AND NOSE DOOR WARNING MSGS ON TAKEOFF CW QRH MSGS CLEARED. MSGS POSTED ABOUT 6 SECONDS AFTER RETRACTION WAS SELECTED. NO HYD SYSTEM ABNORMALITIES WERE NOTED LANDING WEIGHT WAS 46800 AND LANDING WAS SMOOTH. NO GEAR LIT UP RED ON EICAS. AIRCRAFT REMOVED FROM SERVICE. INSP AND FOUND NOSE LANDING GEAR WEIGHT OFF WHEELS #2 AND CENTERED HARNESS ASSY/ SUPPORT BRACKET DAMAGED FROM TOW STRAP. R&R HARNESS AND BRACKET IAW AMM SUP 12-029E. OPS CHECK GOOD.
STEERING INOP CAUTION CLIMBING THROUGH FL140. C/W QRH MESSAGE PERSISTS. AFTER LANDING WITH NWS ARMED, MESSAGE RETURNED. *****AIRCRAFT REMOVED FROM SERVICE****** R&R NWS ECU IAW AMM 32-51-10. PERFORMED OPS CHECK, OPS CHECK GOOD.PN: 16900-107 S/N OFF: 02-744
TEMPORARY REPAIR TO THE R/H HORIZONTAL STABILIZER CLOSING RIB ******AIRCRAFT REMOVED FROM SERVICE****** REPAIRED CLOSING RIB REF REO 601R-55-11-739 REV A DATED 2023-01-19
R/H SIDEWALL SEAT TRACKS (3 EA) FROM FS 409+111.98 TO FS 549.06 HAVE SEVERAL AREAS SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS 409+111.98 TO FS 549.06 FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 3 EACH R/H SIDEWALL SEAT TRACKS FROM FS 409+111.98 TO FS 549.06 IAW CRJ200 AMM 53-01-11 REV 64. RESTORED PROTECTIVE FINISH TO SEAT TRACKS PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 38, CRJ200 SRM 51-25-06 REV 38, AND CRJ200 SRM 51-25-00 REV 38. WORK COMPLETED ON AERSALE WO #003541 CARD #20172. CRS #4AER685B N426AW TT: 41,140:31 TC: 39,653
RH SIDEWALL SEAT TRACK FROM FS409.00 + 16 TO FS409.00 + 112 HAS SURFACE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED RH SIDEWALL SEAT TRACK PN 20276-144-0-0 FROM FS409.00 + 16 TO FS409.00 + 112. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-40-11 REV 38 AND CRJ200 AMM 53-01-11 REV 64. WORK PERFORMED UNDER AERSALE WORK ORDER 003541, CARD NO. 20171, TT: 41,140:31 TC: 39,653.
CHAFE DAMAGE TO THE LEFT WING INBOARD FLAP AFT HINGE FITTING. ****AIRCRAFT REMOVED FROM SERVICE ****** BLENDED CHAFE DAMAGE TO THE LEFT WING INBOARD FLAP AFT HINGE FITTING PN601R10315. CHAFE DIMENSIONS L = 0.500ÿ½ X W = 1.750ÿ½ X D = 0.020ÿ½. PERFORMED HFEC WITH NO INDICATIONS. . PERFORMED ROTO PEEN TO REWORKED AREAS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01846 REV IR DATED 4/14/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003541, CARD NO. 20220, TT: 41,140:31, TC: 39,653.
DENT ON FORWARD FUSELAGE LOWER SKIN AT FS283 AND STR23R - STR24R. ****AIRCRAFT REMOVED FROM SERVICE **** HAND DRESSED DENT ON AFT FUSELAGE SKIN AT FS283 AND STR23R - STR24R. PN 601R31022-3. DENT DIMENSIONS P1- L = 1.20ÿ½ X W = 1.00ÿ½ X D = 0.023ÿ½. ORIGINAL MATERIAL THICKNESS 0.063ÿ½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01840 REV IR DATED 4/7/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003541, CARD NO. 20117, TT: 41,140:31, TC: 39,653.
DENT ON AFT FUSELAGE SKIN AT FS605.00 ÿ½ FS621.00 AND S25L - S26L. ***AIRCRAFT REMOVED FROM SERVICE **** VERIFIED NO LOOSE OR PULLED FASTENERS AROUND DENT ON AFT FUSELAGE SKIN AT FS605.00 ÿ½ FS621.00 AND S25L - S26L. PN 601R35005-143. DENT DIMENSIONS P1- L = 1.00ÿ½ X W = 0.800ÿ½ X D = 0.022ÿ½. PERFORMED HFEC WITH NO INDICATIONS. PROTECTIVE FINISH NOT DISTURBED OR DAMAGED. APPLIED TEMPORARY YELLOW DOT IAW GMM VOL 1, CHAP 18, SECTION 3.1.1. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01841 REV IR DATED 4/8/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003541, CARD NO. 20111, TT: 41,140:31, TC: 39,653.
RH SIDEWALL SEAT TRACK FROM FS364 TO FS409.00 + 16 HAS SURFACE CORROSION. ****AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED RH SIDEWALL SEAT TRACK PN 20276-144-0-0 FROM FS364 TO FS409.00 + 16. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-40-11 REV 38 AND CRJ200 AMM 53-01-11 REV 64. WORK PERFORMED UNDER AERSALE WORK ORDER 003541, CARD NO. 20170, TT: 41,140:31 TC: 39,653.
DENT ON AFT FUSELAGE SKIN AT FS654.50 ÿ½ FS672.20 AND S25L - S26L. ****AIRCRAFT REMOVED FROM SERVICE ***** HAND DRESSED DENT ON AFT FUSELAGE SKIN AT FS654.50 ÿ½ FS672.20 AND S25L - S26L. PN 601R35005. DENT DIMENSIONS P1- L = 0.500ÿ½ X W = 0.500ÿ½ X D = 0.008ÿ½. ORIGINAL MATERIAL THICKNESS 0.036ÿ½, REMAINING MATERIAL THICKNESS 0.028ÿ½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01842 REV IR DATED 4/8/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003541, CARD NO. 20097, TT: 41,140:31, TC: 39,653.
PAX DOOR FWD ANCHO FITTING PLATE P/N600-38061-11 WAS FOUND CORRODED. THE EXPANSION CAUSED THE PAX DOOR FWD ANCHOR FITTING TO CRACK. ***AIRCRAFT REMOVED FROM SERVICE*** R&R PAX DOOR FWD ANCHOR PLATE AND ALL ATTACHING HARDWARE, FWD PAX DOOR SWIVEL CABLE END, AMD SWIVEL GUIDESHAFT. IAW AMM 52-11-17 CLEANED PAX DOOR SILL 15075 11/18/2021 AND DRAINS. C/W NDT OF FWD ANCHOR FITTING MATING SURFACE AMD FASTENER HOLES. .
ON FINAL NLG DID NOT SHOW DOWN & GREEN. DID NOT RECEIVE GEAR DISAGREE MESSAGE. NLG INDICATED RED. RAN GEAR DISAGREE QRH. NLG BOX TURNED GREEN AND MESSAGE CLEARED. NO ABNORMAL HYD INDICATIONS. NO OTHER EICAS MESSAGES NOTED. AIRCRAFT REMOVED FROM SERVICE INTERROGATED PSEU & GOT S21 DOWN FAR. INSTALLED NLG & MLG PINS & REMOVED FLAGS IAW AWAC SUPP 11-054A. REF 319305/2 FOR MEL. R&R LH NLG DOWN LOCK HARNESS IAW AWA SUPP 12-029D. PERFORMED GEAR SWINGS, OPS CHECKS GOOD. REMOVED PLACARD AND FROM MEL.
CARGO DOOR SEAL RETAINER CHAFFED IN MULTIPLE SPOTS. AIRCRAFT REMOVED FROM SERVICE REPLACED CARGO DOOR SEAL RETAINER I/A/W CRJ200 SRM 51-42-06 & 51-42-21. CARGO DOOR LEAK CHECK GOOD I/A/W CRJ200 AMM 52-31-07-710-801
PER CUSTOMER REQUEST, APPLY GENERIC REO 601R-53-11-0048 ON LEFT SIDE SKIN RADIUS AT FS 235. AIRCRAFT REMOVED FROM SERVICE REPAIRED NLG CUTOUT, LH SIDE, AT FS235 I/A/W BOMBARDIER REO 601R-53-11-0048 REV. D.
FUSELAGE SKIN AT AFT RIGHT CORNER NEXT TO SPADE DOOR IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REPAIRED FUSELAGE SKIN IAW REO 601R-53-11-3525 REV-- DATED 01-02-2020.
RIGHT HAND VERTICAL STIFFENER ON OUTBOARD SIDE OF NOSE LANDING GEAR WHEEL WELL STRUCTURE IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED RH SIDE VERTICAL STIFFENER ON OUTBOARD SIDE OF NLG WHEEL WELL IAW CRJ200 SRM 51-42-06 AND 51-42-21.
BOTTOM SIDE OF APU ENCLOSURE WELD REPAIR IS CRACKED AIRCRAFT REMOVED FROM SERVICE REPAIRED APU ENCLOSURE IAW AWAC SUP 19-341C
PANEL 446AL HAS PREVIOUS REPAIR DOUBLER CRACKED ON 2ND RIB AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED 2ND RIB ON PANEL 446AL IAW BOMB. CMM 20-42-06
RIGHT FLOOR SILL CORRODED AT NUT PLATE, FS 295.00-319.70, STR17R. AIRCRAFT REMOVED FROM SERVICE REPLACED SILL IAW CRJ200 SRM 51-42-13.
RIGHT LOWER WING TO FUSELAGE FAIRING FITTING CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED FITTING IAW CRJ 200 SRM 51-42-21.
RIGHT WING TO FUSELAGE FAIRING ATTACH BRACKET CRACKED AT FS 449.85, RBL45. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ200 SRM 51-42-06.
LEFT WING TO FUSELAGE FAIRING ATTACH BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.
LEFT WING TO FUSELAGE FAIRING ATTACH BRACKET CRACKED. AT FS461.00,LBL45. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ200 SRM 51-42-06.
LEFT WING TO BODY FAIRING ATTACH BRACKET CRACKED AT FS 449.85, LBL 45. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.
LEFT FUSELAGE TO WING FAIRING BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED BRACKET IAW CRJ 200 SRM 51-42-06.
FAIRING ATTACH BRACKET ON FUSELAGE LONGERON AT RBL 45 AND FS 469.63 IS CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED BRACKET IAW CRJ-200 SRM 51-42-06
LEFT LOWER SIDE WINDOW JOINT TO FUSELAGE ATTACH FITTING IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED ATTACH FITTING IAW CRJ 200 SRM 51-42-21
FS621 APB SUPPORT CRACKED AT LBL45 WL80 AN AFT SIDE OF BULKHEAD AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED STIFFNER IAW CRJ 200 SRM 51-42-06
L/H FLOOR SUPPORT SILL PLATE CRACKED AT FS 605.0 ADJACENT TO FASTENER COMMON TO SILL AND FLOOR SUPPORT BEAM AIRCRAFT REMOVED FROM SERVICE REPAIRED L/H FLOOR SILL PLATE AT FS 605.0 IAW REO 601R-53-61-433
LEFT HAND DOOR 211AL AFT LATCH CUT-OUT IS CRACKED REPAIRED SKIN IAW AWAC SUP. 19-016B
PERFORM MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS 621.0 AIRCRAFT REMOVED FROM SERVICE COMPLETED MODIFICATION OF THE REAR PRESSURE BULKHEAD AT FS 621.0 IAW REO 601R-53-61-1240 REV D
ATTACH ANGLE COMMON TO FS621.0 RPB AND CARGO NET AFT TIE DOWN FITTING SUPPORT STRUCTURE IS CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED ANGLE IAW CRJ -200 SRM 51-42-21
R/H AILERON OUTBOARD LOWER SKIN LEADING EDG IS CHAFFED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED LEADING EDGE IAW CRJ-200 SRM 51-42-21 AND 51-42-06
GEN #1 CAUTION MESSAGE IN CRUISE C/W QRH DID NOT RESET. AIRCRAFT REMOVED FROM SERVICE. #1 IDG TEMP BULB CANNON PLUG FOUND LOOSE RE-SECURED CANNON PLUG REF AMM 24-12 OPS CHECK GOOD.
AT CRUISE FL250 NOTICED RT PACK OFF STATUS MESSAGE AND RT PACK OFF SWITCH LIGHT ILLUMINATED. CYCLED RT PACK SWITCH TWICE. PACK REMAINED OFF. SELECTED ECS PAGE ON EICAS. RT 10TH STAGE BLEED CLOSED. CYCLED R 10TH SWITCH CLOSED THEN OPEN. PRESSURIZATION RESUMED. DISPATCH ADDS THAT THE CREW RECEIVED CABIN ALT. CAUTION MESSAGE, CONSULTED QRH AND REQUESTED A LOWER ALTITUDE FROM ATC. WHILE DESCENDING, CREW RECEIVED CABIN ALT WARNING MESSAGE AND DECLARED AN EMERGENCY WITH ATC. CONTINUED FLIGHT TO IAD. PERFORMED OPS CHECK OF 10TH STAGE BLEED SYSTEM WITH BOTH LEFT AND RIGHT ENGINES RUNNING IAW AMM 36-11-00. OPENED AND CLOSED LEFT AND RIGHT 10TH STAGE VALVES MULTIPLE TIMES. UNABLE TO DUPLICATE ORIGINAL DISCREPANCY. 10TH STAGE BLEED AIR SYSTEM FUNCTIONS NORMALLY. OPS CHECK GOOD AT THIS TIME.
DURING SINGLE PACK OPERATION ON ENGINE BLEED AIR IN CLIMB AT APPROX 92% N1 RECEIVED RIGHT PACK OFF LIGHT AND RIGHT PACK OVERPRESS MESSAGE C/W QRH AND IAC RIGHT PACK OPERATION NORMAL ON APU BLEED R/R ACM IAW 21-51-10. OPS CK GOOD.
FRAME AT BS 605 ATTACHMENT FLANGES CRACKED ABOVE AND BELOW STRINGER 9L. REPAIRED THE FRAME
RIGHT INBD FLAP LOWER SKIN IS DENTED 22 INCHES FROM INBD EDGE AND 16 INCHES FROM T/E.
FRAME BS 333 BETWEEN STRINGER 2 AND 3 LEFT IS CRACKED.
AFT PRESSURE BULKHEAD ABOVE FLOOR HAS SCRATCHES AND BARE METAL. REPAIRED THE BULKHEAD.
LEFT INBD FLAP LOWER SKIN PANEL PITTED WITH BARE METAL AT WS 56.30 TO WS 75.27.
LEFT INBD FLAP VANE CHAFED ON THE LE IN MULTIPLE AREAS. REPLACED THE FLAP VANE.
FLOORBEAM BS 280 IS CRACKED AT THE LOWER ANGLE JUST OB OF THE MLG ALT CABLE PULLEY BRACKET. REPAIRED THE ANGLE.
BS 280, LBL 10 FLOORBEAM ANGLE CRACKED. REPLACED THE ANGLE
BS 280 RBL 10 FLOORBEAM ANGLE CRACKED. REPLACED THE ANGLE
1015090-3000-0014 - L/H UPPER OBLIQUE ANGLE CRACKED AFT PRESSURE BULKHEAD
1015090 6000-0018 - RH WING LEADING EDGE CENTER TO IB LEADING EDGE INNER ATTACH BRACKET OB ATTACH CRACKED. REPLACED
RT MLG BRAKE APPLICATION PRESSURE TRANSDUCER MOUNTING BRACKET CRACKED THE WW. REPLACED THE BRACKET.
1015090 1000-0005 - LH WING BATT RIB DRAG ANGLE IS CRACKED. REPLACED
LT MLG BRAKE APPLICATION PRESSURE TRANSDUCER MOUNTING BRACKET CRACKED IN THE LT MLG WW. REPLACED THE BRACKET
1015090 1000-0048 - HINGE POCKET IS CORRODED AT FS 342 LBL 39. REPLACED
1015090 1000-0064 - LH FLOOR SILL CRACKED AT FS 589. REPAIRED
LOOSE CARGO BAY LINER SCREW GOUGED AN EXISTING REPAIR ON BAGGAGE BAY DOOR. REPLACED PATCH ON BAGGAGE BAY DOOR IAW REO 601R-52-31-250, REV A.
RPB HAS DAMAGED DIAMOND PATCH REPAIRS ON LBL 18.00 & LBL 27.50 BETWEEN WL 73.50 & WL 120.
GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. SELECTING UP. APPROX 6 SECONDS AFTER GEAR HANDLE MOVEMENT ACCOMPANIED WITH STEERING INOP CAUTION. RAN QRH, USED MANUAL RELEASE. NOSE LANDING GEAR DID NOT MOVE. NO ICING, NO TURBULENCE, NO EXCESSIVE MOVEMENT. ALL HYDRAULIC INDICATIONS NORMAL. HYD 2B AND 3B WERE IN ON POSITION, HYD 1 AUTO. EMERGENCY DECLARED. AIRSPEED APPROXIMATELY 170 LANDING WEIGHT 46,600.
EMERGENCY LIGHTS WOULD NOT ILLUMINATE AT ROW 12 AND APPEAR TO BE MISSING ARROWS.
FLIGHT 3969, MAIN ENTRY DOOR EMERGENCY FLOOR FLOOD LIGHT AND ROW 1 EMERGENCY LIGHT INOPERATIVE. FOUND EMERGENCY LIGHTS IN WARDROBE WIRED INCORRECTLY. REWIRED EMRGENCY LIGHTS IAW AMM 33-50-00. OPS CHECKED GOOD.
MAIN ENTRY DOOR EMERGENCY FLOOR FLOOD LIGHT AND ROW 1 EMERGENCY FLOOR PATH LIGHTING INOPERATIVE.
UNCOMMANDED YAW AT FL 190. COMPLIED WITH IAC & QRH. YAW MOTION CONTINUED WITH AUTOPILOT AND YAW DAMP DISCONNECTED. NOTE RUDDER MOVEMENT ON FLIGHT CONTROL SYNOPTIC WITH NO PILOT INPUT. YAW MOVEMENT NOT FELT IN PEDALS.
SERVICE DOOR WOULD NOT OPEN FROM OUTSIDE ACFT. PLUNGER WOULD NOT POP OUT.
UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE.
REQUEST INSPECTION FOR SMOKE COMING FROM BRAKE BTMS READS 8, 7, 5, 6.
REF 299167 3 SERVICE DOOR DIFFICULT TO OPEN REQUIRES RE-RIGGING. FOUND OUTER HANDLE HAS BENT METAL & WONâT EJECT. REPLACED OUTER HANDLE IAW AMM 52-41-03, REBUILT ROLLER END ON INNER HANDLE PLUNGER & ADJUSTED IAW AMM 52-41-00. DOOR OPENED & CLOSED FROM INNER & OUTER HANDLE NORMALLY. OK FOR SERVICE.
ON WALK AROUND NOTICED SMOKE FROM RT OTBD BRAKE & BLACK PUDDLE UNDER WHEEL ASSEMBLY.
ABORTED TAKEOFF FOR IDG2 CAUTION MSG BELOW 80 KNOTS. NORMAL BTMS.
NOTICED PUDDLE TO THE LT OF RT MAIN GEAR & LT NR 3 TIRE SMOKING.
ON POST FLIGHT SMOKE COMING FROM RT MLG TIRE BTMS 4, 4, 5, 5 WAS 4,4,6,6.
DURING FLIGHT CONTROL CHECK A, LOUD CLICKING IS HEARD FROM CAPTAINS RUDDER PEDAL. CLICKING OCCURS NEAR NEUTRAL POSITION, NO NOISE IS HEARD WHEN MOVING FIRST OFFICERS PEDALS.
RIGHT AILERON UPPER LE SKIN CHAFED. REPLACED.
RIGHT WING TO BODY SKIRT CHAFED BY CONTACT WITH STUB FAIRING SEAL.
ANGLE IS CRACKED AT THE OTBD SIDE OF RBL 36 & FS 484 IN THE CABIN. REPAIRED ANGLE IAW REO 601R53-41-059.
PASSENGER DOOR AFT SIDE PANEL CRACKED AT POWER ASSIST MOTOR CABLE CUT OUT. REPAIRED.
LEFT FUSELAGE SKIN AT BS 559 AT STUB FAIRING ATTACH POINT CHAFED. REPAIRED.
RIGHT INBD GROUND SPOILER HAS ONE EACH SHARP DENT IN LOWER SKIN.
LEFT AISLE SEAT TRACK 3, BETWEEN FS 409+112 - FS 559 CORRODED. REPLACED.
PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED.
FS 621 BULKHEAD FWD FACE HAS 9 GOUGES IN PREVIOUS REPAIRS.
FS 621 BULKHEAD FWD FACE SKIN IS CHAFED BEHIND ISOLATOR MOUNT AT RBL18, APPROX 40" ABOVE FLOOR. REPAIRED IAW REO 601R-53-61-1285 REV A.
STIFFENER AT LBL 27 IS CRACKED AT THE INBD LOWER AFT SIDE CORNER AT FS 409+128, FWD SIDE OF WING BOX IN CABIN. REPAIRED STIFFENER IAW REO 601R-53-41-056.
FRAME 333 HAS CORROSION ON THE FWD & AFT SIDES, BETWEEN STRINGER 25L & 24R IN THE FWD E & E BAY. REPAIRED IAW EA 40-2015-271.
FLOOR STRIP HAS CORROSION AT FS 559.00, BETWEEN RBL 36 & RT FLOOR SILL. REPAIRED FLOOR STRIP AT FS 559.00, BETWEEN RBL 36 & RT SILL BY INSTALLING REPLACEMENT PART IAW SRM 51-42-06.
AFT FUSELAGE COMPARTMENT BULKHEAD 621 RT INTERCOSTAL CLIP, CRACKED AT FUSELAGE SKIN, STRINGER 13R. R & R CLIP ON RT INTERCOSTAL AT STRINGER 13R ON AFT SIDE OF FS 621 BULKHEAD IAW SRM 51-42-06.
AFT FUSELAGE COMPARTMENT BULKHEAD 621, RT INTERCOSTAL CLIP AT FUSELAGE SKIN IS CRACKED, 3:30 O'CLOCK POSITION. R & R CLIP ON INTERCOSTAL AT STRINGER 14R ON AFT SIDE OF 621 BULKHEAD IAW SRM 51-42-06.
FLOOR STRAP HAS CORROSION AT FS 559.00, BETWEEN LBL 36 & THE LT FLOOR SUPPORT. REPAIRED THE STRAP IAW SRM 51-40-02.
SEAT TRACK LBL 27, INBD & OTBD FLANGES, BS 574 - 621, HAVE CORRODED FASTENER HOLES. REMOVED CORROSION IAW AWAC SUPPLEMENT 14-029. R & R IAW SRM 51-24-36, 51-40-11, 51-61-43 & REO 601R-53-61-3778 REV A.
LEFT AISLE SEAT TRACK STICK NR 2 HAS CORROSION, BETWEEN FS 394 & FS 409+112 IN CABIN. REPAIRED AISLE SEAT TRACK STICK NR 2, BETWEEN FS 394 & FS 409+112 IAW REO 601R-53-00-485 & AMM 53-01-11.
LEFT SIDEWALL SEAT TRACK STICK NR 6 HAS CORROSION, BETWEEN FS 544 & FS 559+80 IN CABIN. R & R LT SIDEWALL SEAT TRACK STICK IAW REO 601R-53-00-485 & AMM 53-01-1.
EMERGENCY LIGHT AT ROWS 2 - 5 INOPERATIVE. R & R THE INVERTER.
FLIGHT 3847, EMER FLOOR LIGHTS INOPERATIVE ROWS 2 - 5. SECURED CONNECTOR ON EMER LIGHTS FLOOR LEVEL ROWS 2 - 5. PERFORMED OPERATIONS CHECK IAW AMM 33-51-00-946-001. OPERATIONS CHECKED GOOD.
SMOKE COMING FROM APU INTAKE DOOR, APU IS OFF & DOOR CLOSED. INSPECTED & FOUND SIGNS OF GLYCOL COMING OUT OF APU.
EMERGENCY LIGHTS NEAR ROW 13 NOT SECURE.
PASSENGER DOOR POWER ASSIST MOTOR SUPPORT BRACKET CRACKED, R & R.
CARGO DOOR NET TIE DOWN SUPPORTS HAVE CORROSION & GOUGES ON TOP SURFACE ON ALL THREE. REMOVED THREE EACH CARGO DOOR NET TIE DOWN SUPPORTS & INSTALLED SERVICEABLE TIE DOWN SUPPORTS IAW CRJ 200 SRM 51-42-06 & 51-42-21.
SERVICE DOOR STOPS AT FS 349, STRINGER 11R & 12R ARE CHAFED. BLENDED CHAFES TO ALLOWABLE DAMAGES IAW REO 601R-53-21-2484.
NUMBER 3 HYD RESERVOIR REAR MOUNT IS CRACKED ON LT SIDE. R & R NR 3 HYD RESERVOIR REAR MOUNT BRACKET.
LEFT AILERON UPPER LE SKIN CHAFED. FOUND TO BE OUT OF LIMITS & REPLACED WITH NEW SERVICEABLE PART PN CC670-13052-3 IAW CRJ 200 SRM 51-42-21 & 51-42-06.
LEFT WING UPPER ACCESS PANEL 540AT LANDING HAS FRETTING CORROSION. BLEND TO ALLOWABLE LIMITS IAW REO 601R-57-21-2053.
LEFT WING UPPER ACCESS PANEL 540CT LANDING HAS FRETTING CORROSION. BLEND TO ALLOWABLE LIMITS IAW REO 601R-57-21-2053.
LEFT WING UPPER ACCESS PANEL 540BT LANDING HAS FRETTING CORROSION. BLENDED TO ALLOWABLE LIMITS IAW REO 601R-57-21-2053.
LEFT WING OTBD MOST FWD EDGE OF FLIGHT SPOILER GOUGED FROM BENT UP SPRING SEAL. BLENDED OUT GOUGE & FOUND TO BE WITHIN LIMITS IAW REO 601R-57-73-226.
SERVICE DOOR CUT OUT LOWER STRIKER GOUGED ON TWO LOCATIONS. BLENDED GOUGES TWO LOCATIONS, OUT OF LIMITS IAW CRJ 200 SRM 52-00-00 & 51-12-00 REV D. NEW DEPRESSOR INSTALLED ONE EACH IAW CRJ 200 SRM 51-41-00.
SERVICE DOOR LOWER SILL CORRODED AROUND SPRICOT FITTING. R & R ANGLE IAW CRJ 200 SRM 51-42-01.
LEFT WING FWD EDGE OF FLIGHT SPOILER INBD MOST END HAS GOUGE LOWER SIDE. BLENDED OUT GOUGES & FOUND TO BE WITHIN LIMITS IAW REO 601R-57-73-226.
RUDDER CTR UPPER & LOWER HINGE BORE DIMENSIONS ARE OUT OF TOLERANCES. R & R HINGES.
SPAN WISE FLOOR SUPPORT BEAM AT FS 349 CORRODED AT RBL 27 TO 32 & BEAM HAS ONE DISCREPANT HOLE AT RBL 36. REMOVED CORROSION FOUND TO BE WITHIN SERVICEABLE LIMITS IAW CRJ 200 SRMS 51-21-06 & 53-21-15. REPAIRED DISCREPANT HOLE AT RBL 36 IAW STS EA 12-2013-567.
RIGHT UPPER LE RUDDER SKIN CRACKED. R & R RUDDER SKIN.
PASSENGER DOOR LOWER STEP SUPPORT SKIN FWD & AFT BRACKETS ARE CRACKED. REPAIRED IAW STS EA 15-2013-509, 11-27-2013.
PASSENGER DOOR SEAL STRIKER PLATE HAS A DENT FS 349 LT STRINGER 6. REPAIR IAW REO 601R-53-22-033 REV C.
FLOOR SEAT TRACK ON RBL 9 & LBL 9 CORRODED AT FS 379.00. BOTH FLOOR SEAT TRACKS RBL 9 & LBL 9 WERE 80% OUT OF LIMITS IAW CRJ 1200 SRM 53-21-49 FIG 10. RECEIVED & INSTALLED NEW SEAT TRACKS AT LBL 9 & RBL 9 IAW CRJ 200 AMM 53-01-11 & SRM 51-41-02.
CARGO DOOR FLOOR SILL CORRODED AROUND NUTPLATES ON UPPER & LOWER SURFACE. REMOVED UNSERVICEABLE SECTION OF CARGO DOOR FLOOR SILL BETWEEN FS 580 & 621. FABRICATED & INSTALLED NEW SERVICEABLE SECTION OF CARGO DOOR FLOOR SILL IAW CRJ 200 SRM 51-24-21, 51-40-11, 51-21-11, 51-25-06, 51-42-06, 51-42-06 & 51-42-15 REO 601R-53-61-690 REV D.
RIGHT BRAKE VOLUMETRIC FUSE TRANSDUCER MOUNT BRACKET IS CRACKED & BROKEN. R & R BRACKET IAW CRJ 200 SRM 51-42-06.
FUEL PRESS BOX AFT PROTECTOR PLATE NUT HOLES DO NOT ALIGN. R & R IAW SRM.
CORROSION ON RT WALL SEAT TRACK AT FS 559+116 - 559+32. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW AMM 53-01-11.
AVIONICS BAY DOOR SEAL RETAINER HAS CORROSION. R & R AVIONICS BAY DOOR SEAL RETAINER IAW CRJ 200 SRM 51-42-06.
CORROSION ON LT WALL SEAT TRACK AT FS 424. BLENDED CORROSION FOUND TO BE WITHIN LIMITS WITH MATERIAL LOSS OF .014 MAX ALLOWED IS .020 IAW CRJ 200 SRM 53-21-49.
LEFT WING LE EDGE BRACKET CRACKED OTBD END AT WS 150. R & R DUPLICATED BRACKET.
CARGO DOOR FWD STOP MOUNT LOWER CLIP IS CRACKED UNDER SILL. REMOVED UNSERVICEABLE CLIP, FABRICATED & INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 53-61-23,51-24-21, 51-40-11, 51-42-21.
FUSELAGE STATION 280 CLIP CRACKED AT LT STRINGER 3L. R & R IAW SRM.
CARGO FLOOR TRACK CORRODED ON RBL 9 AT FS 559+112 & FS 559+98. R & R FLOOR TRACK.
EXFOLIATED CARGO TIE DOWN, REMOVED & REPLACED.
CORROSION ON SEAT TRACK RBL 9 AT MULTIPLE AREAS FS 449.85, FS 494, FS 513, FS 529, FS 544, FS 559 & FS 461.
LEFT ENG JET PIPE INBD & OTBD MOUNT NUTPLATE BRACKETS ARE CRACKED. R & R CRACKED NUTPLATE BRACKETS IAW CRJ 200 SRM 51-42-06.
CARGO FLOOR TRACKS CORRODED ON LBL 9 AT FS 559+112 & 559+98. R & R FLOOR TRACK.
FUSELAGE STATION 280 LBL 9 CLIP CRACKED. REMOVED, FABRICATED & INSTALLED NEW CLIP.
FUSELAGE STATION 280 AT RBL 9 CLIP CRACKED. REMOVED, FABRICATED & INSTALLED NEW CLIP.
CLIP AT FS 484 & RBL 27 IS CRACKED. R & R CLIP.
DURING GEAR SWINGS FOR MLG CHANGES GEAR DISAGREE (NLG). REPLACED SPRING UNIT ASSY ON NLG MANUAL RELEASE MECHANISM REF AMM 32-34-15 OPS CHECKED OK
ANTI-ICE DUCT WARNING MESSAGE IN FLT SELECTED WING ANTI-ICE OFF. RT WING ANTI-ICE OFF. RT WING DUCT IND RED IN CRUSE. TROUBLESHOT IAW FIM 36-20-00. VERIFIED NO LEAKS FROM RT PICCALO TUBE COUPLINGS. R & R RT BLEED LEAK CONTROL UNIT IAW AMM 36-21-10. OPS CHECKED GOOD.
O2 MASKS INCLUDING LAV, DID NOT DEPLOY DURING AUTO OR MANUAL DEPLOYMENT TEST. FOUND FIG 3636 AT FS 409, WL 128.05, RBL 40.95 VERY LOOSE, CAUSING INTERMITTENT O2 MASK DEPLOY RETURN. TIGHTENED GS IAW ESPM 20-20-00.
RT BATT RIB CRACKED. COMPLIED WITH REO 601R-57-51-5663 ON RT CRACKED BATT RIB.
SERVICE DOOR INNER HANDLE GOUGED. REPAIRED GOUGE IAW REO 601R-52-41-199.
RT UPPER NOSE COWL T/E STRIP CHAFED. REPAIRED RT UPPER NOSE COWL T/E STRIP IAW CMM 71-14-01.
RT PYLON PANEL 422BT AFT ANGLE CRACKED. REMOVED UNSERVICEABLE RT PYLON PANEL: 422BT AFT ANGLE AND INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06.
FLOORBEAM CAP UNDER FLOORBOARD 281LLF IS CORRODED. REPAIRED FLOORBEAM CAP AT FS 615 & LBL 27.00 IAW REO 601R-53-61-4289.
RT MLG, GEAR DOOR ATTACH LUG CHAFED. BLENDED DAMAGED AREA ON RT MLG DOOR IAW REO 601R-52-92-43.
RT INBD FLAP INBD HINGE BOX TOP INBD LUG CHAFED. REPAIRED RT INBD FLAP INBD HINGE BOX LUG IAW REO 601R-57-21-1554.
LOWER FUSELAGE UNDER EACH OTBD ENDS OF MLG FWD FAIRING HAVE CHAFING DAMAGE. REPAIRED DAMAGE IAW REO 601R-57-21-880.
PAX DOOR OUTER HANDLE CRACKED. R & R WITH NEW HANDLE.
RT LOWER CORE COWL FWD INNER SKIN GOUGED 6 SPOTS. REPAIRED RT LOWER CORE COWL FWD INNER SKIN IAW REO 601R-71-12-4086.
RT SIDE OF 280 BULKHEAD DAMAGED FROM GALLEY DOOR COMPLIED WITH REO 601R-53-11-1727 & 601R-53-11-2237.
INDICATION OF CORROSION INBD END OF C/O 650AB. REPAIRED IAW REO 601R-57-21-030.
RT & LT FS 625.00 OBLIQUE ANGLES CRACKED. REPAIRED L/R 625.00 OBLIQUE ANGLES BY INCORPORATING REO 601R-53-61-100 & 601R-53-61-422.
PAX DOOR FWD & AFT STRIKER PLATES CHAFED. BLENDED FWD & AFT STRIKER PLATES IAW SRM 51-12-00. ORG THICKNESS .187 AFTER BLENDING FWD .155, AFT .163 WITHIN LIMITS IAW REO 601R-52-11-296. ALODINED, PRIMED, TOP COATED IAW SRM 51-21-11, 51-25-06, 51-25-16.
PAX DOOR FWD PULL IN LEVER CHAFED, BLENDED IAW SRM 51-12-00 (TOOL 1671 CAL DUE4/12/12). REMOVED .030, WITHIN LIMITS IAW REO 601R-52-11-524, FIG 1. NDT INSPECTED, ALODINED, PRIMED, TOP COATED.
FOUND LT BATTERY RIB CRACKED. REPAIRED LT BATT RIB IAW REO 601R-57-51-046.
FOUND LT BATT RIB CRACKED. REPAIRED LT BATT RIB IAW REO601R-57-51-046.
LT WING AILERON PANEL 559AB HAS AREAS OF CHAFING. BLENDED DAMAGED AREA IAW SRM 51-12-00. ORG THICKNESS .055 AFTER BLENDING MIN THICKNESS .048 TOOL REF 326 (CAL DUE 6/14/12. WITHIN LIMITS IAW REO 601R-57-60-020. NDT INSPECTION ALODINED, PRIMED, TOP COATED IAW SRM 51-21-11, 51-25-06, 51-25-16.
LOWER U-BRACKET CRACKED AT FS 574.00, STR 16A, LT AT CARGO DOOR TRACK. REMOVED U-BRACKET AND REPLACED WITH NEW BRACKET IAW SRM 51-42-06.
LEFT THRUST REVERSER BLOCKER DOORS 3-10 CHAFED FROM STOPS. BLENDED DAMAGED AREAS ON RT BLOCKER DOORS IAW CMM 78-30-00.
LT THRUST REVERSER OTBD TRACK ATTACHING LUG CHAFED. BLENDED LT LOWER OTBD TRACK ATTACHING LUG DAMAGE IAW REO 601R-78-34-2435.
LT THRUST REVERSER BLOCKER DOORS 3-10 CHAFED FROM STOPS. AFTER FURTHER INVESTIGATION, FOUND DAMAGE ON ALL 10 BLOCKER DOORS. BLENDED DAMAGED AREAS ON LT T/R BLOCKER DOORS IAW CMM 78-30-00.
PAX DOOR HINGE FUSELAGE SIDE 2ND LUG FWD END IS GOUGED. BLENDED 2ND FWD LUG ON PAX DOOR FUSELAGE SIDE. REMOVED .009 OF MAT REMAINING MAT IS WITHIN SERVICEABLE LIMITS OF .116 MIN REQUIREMENT IS .100 IAW REO 601R-53-21-814.
ABORTED T/O AT 50-55 KNOTS, DUE TO DIRECTIONAL CONTROL PROBLEMS. ACFT PULLS TO RT, FULL LEFT RUDDER COULD NOT BRING IT BACK CENTERED. R & R LEFT AND RIGHT NOSE WHEEL ASSY. AC TAXIED GOOD IAW 32-50-00.
PAX DOOR FLAP VENT DOOR CHAFED FROM ICE BRAKE CABLE BLENDED IAW SRM 51-12-00 USING TOOL 1243, CAL DUE 4/20/12. REMOVED .020 WITHIN LIMITS IAW REO 601R-52-11-1040. NDT INSPECTED, ALODINED, PRIMED, TOP COATED IAW SRM 51-21-11, 51-25-06, 51-25-16.
AT CRUISE, FL190, 310 IAS, OAT -26C, RECEIVED MULTIPLE STAB TRIM AND MACH TRIM CAUSTION MSG`S. SLOWED ACFT, STILL RECEIVED MSG`S. C/W QRH AIR RETURN TO DEPARTURE. INTERROGATED MDC, FOUND CAPT PITCH TRIM DISCONNECT SWITCH FAILED, VERIFIED FAILURE WITH SWITCH SENSITIVITY TEST IAW AMM SUP 05-029A, R & R SWITCH IAW AMM 27-41-30, OPS CHECK GOOD.
INSPECTED RT EMERGENCY ESCAPE ROPE FOR MISSING RED CLASP. INSTALLED RT WING EMERGENCY ESCAPE ROPE "D" RING AND ROPE RETAINING STRAP AS REQUIRED REF AMM 25-63.
RT THRUST REVERSER UNLOCK MESSAGE IN FLIGHT, DURING CLIMBOUT. REMAINED ON TIL LANDING. R & R RT THRUST REVERSER PNEUMATIC DRIVE UNIT IAW AMM 78-32-03, OPS CHECK GOOD.
PAX DOOR WOULD NOT OPEN FROM OUTSIDE. PLACED ON MEL, PHL 2-2. INSPECTED LUBED AND OPS TEST OF DOOR IAW AMM 52-11-00, OPS GOOD. REMOVED FROM MEL.
INTERCOSTAL CLIP FS 621.0 TO 625.0, ADJACENT STR 14R CRACK INTERCOSTAL CLIP FS621.0 TO FS 625.0 ADJACENT TO STR 14R REPLACED IAW.
RT AILERON INBD PCU ATTACHMENT OTBD LUG BUSHING GOUGED. RT AILERON INBD PCU ATTACHMENT OTBD LUG BUSHING REPLACED IAW AMM 20-26-00-910-803 AND REO 601R-57-61-250 REV B.
LT ENG LOWER ACCESS COWL PANEL 432 AC VENT COVER CRACKED LT ENG LOWER ACCESS COWL PANEL 432 AC VENT COVER REPLACED IAW SRM 51-42-13.
CRACK FOUND ON PAX DOOR STAIR AFT SIDE PANEL ZONE 2,3,4. PAX DOOR STAIR AFT SIDE PANEL ZONE 2,3,4. REPAIRED IAW REO 601R-52-11-702, REV A.
CRACK FOUND ON PAX DOOR STAIR FWD SIDE PANEL ZONE 2 PAX DOOR STAIR FWD SIDE PANEL ZONE 2, REPAIRED IAW REO 601R-52-11-702, REV A.
PRESSURE BULKHEAD CAP ANGLE FOUND CRACKED IN THE RADIUS AT FS 559.0, RBL 18.0. PRESSURE BULKHEAD STRUCTURE AT FS 559.0, RBL 18.0. REPAIRED IAW REO 601R-53-41-260, REV D AND 601R-53-41-609, REV A.
RT AILERON OTBD PCU ATTACHMENT INBD LUG BUSHING GOUGED RT AILERON OTBD PCU ATTACHMENT INBD LUG BUSHING REPLACED IAW AMM CRJ 200 20-26-00-910-803 AND REO 601R-57-61-250, REV B. (K)
FWD FUSELAGE RT FLIGHT CONTROLS COMPT (ACCESS BY PANEL 132AL) ANGLE CRACKED ON FLOOR STRUCTURE FS 235.00. FWD FUSELAGE RT FLIGHT CONTROLS COMPT (ACCESS BY PANEL 132 AL) ANGLE REPLACED ON FLOOR STRUCTURE FS 235.00 IAW SRM 51-42-06.
CORROSION FOUND ON FLOOR STRUCTURE FITTING TO FR FS 319.00, WL 79.00, RBL 45.0 FLOOR STRUCTURE FITTING TO FR FS 319.0, WL 79.00, RBL 45.0. REPLACED IAW SRM 51-42-21.
CRACK FOUND ON PAX DOOR AFT DRAG STAIR ANGLE (CRACK LENGTH .500) AT PAX DOOR AFT DRAG STAIR ANGLE REPAIR PERFORMED IAW REO 601R-52-11-513, REV A.
PAX DOOR LOWER LONGERON EXT AND INT SURFACE CORRODED PAX DOOR LOWER LONGERON REPLACED IAW SRM 51-42-06, 51-42-13, 51-42-21.
ON RT COWL TORQUE BOX 2 FWD SEALS (BOTTOM AND OTBD BOTTOM) FOUND CRACKED ON RT COWL TORQUE BOX 2 FWD SEALS REPLACED IAW SRM 51-42-12.
PRESSURE BULKHEAD CAP ANGLE FOUND CRACKED IN THE RADIUS AT FS 559.0, LBL 18.0. PRESSURE BULKHEAD STRUCTURE AT FS 559.00, LBL 18.0 REPAIRED IAW REO 601R-53-41-260 REV D AND REO 601R-53-41-609, REV A, EVIATION C.
AFT ANGLE OF BULKHEAD AT FS 280, WL 73.10, LBL 9.0 CRACKED AFT ANGLE OF BULKHEAD AT FS 280, WL 73.10, LBL 9.0, REPAIRED IAW REO 601R-53-11-138 REV NC.
CRACK FOUND ON CARGO DOOR HANDLE HOUSING (CRACK LENGTH 1.00). REPLACED CARGO DOOR HANDLE HOUSING IAW SRM 51-42-21.
FWD ANGLE OF BULKHEAD, AT FS 280.0, WL 73.10, RBL 9.0 CRACK FWD ANGLE OF BULKHEAD AT FS 280.0, WL 73.10, RBL 9.0, REPLACED IAW SRM 51-42-06.
INTERCOSTAL FOUND CRACKED BEHIND AFT PRESSURE BULKHEAD AT WL 100.5, LBL 48, FS 621. CRACK LENGTH .500" INTERCOSTAL REPLACED IAW SRM 51-42-06 AND SRM 51-42-21. (K)
CRACK FOUND AT LINTEL FITTING OF THE AFT PRESSURE BULKHEAD. BULKHEAD FS 621 AT LINTEL FITTING REPAIRED IAW REO 601R-53-61-1230, REV D. (K)
CRACK FOUND AT FS 621, LBL 27.50, WL 130.00 AT THE END OF CARGO DOOR TRACK. REPAIR PERFORMED AT FS 621.00, LBL 27.50, WL 130.00 AT THE END OF CARGO DOOR TRACK IAW REO 601R-53-61-1541, REV B. (K)
LOG 189993/2 FLIGHT 3802, 3845, UNCOMMANDED FLAPS EXTENSION OF 8 DEGREES AT FL 31.0 TAT -23, SAT -48, MACH .74, IAS 275, INTERMITTENT INDICATION OF FLAPS EXTENDING TO 2 DEGREES FOLLOWED. DOWNLOADED FDR IAW AMM 31-31-01, CONFIRMED LT FLAP POSITION TRANSMITTER SHOWS ERRATIC FLAP MOVEMENT TO 8 DEGREE DURING FLIGHT. REF W/O 129548 CARD 2 FOR REMOVED AND REPLACEMENT OF LT FLAP TRANSMITTER. REMOVED AND REPLACED FLAP POS TRANSMITTER ASSY IAW AMM 27-55-01. OPS CHECK GOOD AT THIS TIME.
STRONG ELECTRICAL SMELL PRESENT IN CABIN BETWEEN ROWS 4 AND 9 EXCLUSIVE. (DISCOVERED ON GROUND) REMOVED AND REPLACED NR 4 RT SIDEWALL LIGHT BALLAST IAW AMM 33-21-10. CONFIRMED BALLAST WAS CAUSE OF SMELL. (K)
ON TAKEOFF RECEIVED GEN NR 2 OFF AND IDG NR 2 FAIL MESSAGES. ABORTED TAKEOFF AT 80 KNOTS. BTMS READ 7-7-5-5. FOUND NR 2 IDG LOW ON OIL. SERVICED NR 2 IDG IAW AMM 12-13-24. OPS AND LEAK CHECK GOOD. (A)
IB CREW REPORTED HYD NR 2 LEAK ON SHORT FINAL. HYD NR 2 CAUTION MESSAGE RECEIVED. HYD QUANTITY NO READS 25 PERCENT. (K)
AC CONNECTOR LANDING STRUCTURE OF ACCESS DOOR FOUND CRACKED APPROX 2.500 INCH. AC CONNECTOR ACCESS DOOR LANDING REPAIRED IAW REO 601R-53-11-569, REV A. (K)
A/C CONNECTOR BOX STRUCTURE AFT INTERNCOSTAL CRACKED. AC CONNECTOR BOX STRUCTURE AFT INTERCOSTAL REMOVED AND FABRICATED IAW SRM 51-24-16, ALODINE IAW 51-21-11 AND INSTALLED IAW SRM 51-42-06, 51-42-13, 51-42-20. (K)
GENERATOR NR 1 CAUTION RECEIVED AT CRUISE, COMPLIED WITH QRH. FOUND AC GENERATOR BURNED UP AT TERMINALS. REMOVED AND REPLACED GENERATOR NR 1 ASSY IAW AMM 24. (K)
HYDRAULIC SUPPORT BRACKET OF MLG BAY FS 529.50 RT FS 523, RBL 31 IS CRACKED. HYD SUPPORT BRACKET OF MLG BAY FS 529.50 AND FS 523 RBL 31. REPLACED IAW CRJ 200 SRM 51-42-06. (M)
FOUND CORROSION EXIST ON FORWARD DOOR SEAL RETAINER OF MAIN AVIONICS DOOR. FORWARD MAIN AVIONICS DOOR SEAL RETAINER REPLACED IAW CRJ 200 SRM 51-42-06. (M)
FOUND CRACK ON 2 BRACKETS FS 625.0 STRINGER 14R AND STRINGER 14L. BRACKETS REPLACED 2X AT FS 625 STRINGER 14R AND STRINGER 14L IAW SRM 51-42-20. (M)
FOUND CRACK EXIST ON BRACKET ON INTERCOSTAL FS 484 RBL 27. REPLACED IAW REO 601R-53-41-059 REV A. (M)
RIGHT AILERON, UPPER LEADING EDGE SKIN BTW WS 389 TO WS 285, ABRASION EXIST. ABRASION FOUND OUT OF LIMITS IAW REO 601R-57-60-013. LEADING EDGE SKIN ON RIGHT AILERON (UPPER) REPLACED IAW CRJ 200 SRM 51-42-06. (M)
MAIN AVIONICS DOOR HANDLE CRACK MAIN AVIONIC DOOR HANDLE REPLACED IAW CRJ 200 SRM 51-42-06. (M)
CHANNEL SUPPORT CRACK, FRAME FS 574 STRINGER LT. CHANNEL ON FRAME 574 STRINGER 16L. REPLACED IAW CRJ 200 SRM 51-42-06. (M)
FOUND CRACK EXIST ON FORWARD AND AFT EDGE MEMBER OF PAX DOOR. FORWARD AND AFT EDGE MEMBER OF PAX DOOR REPAIRED IAW REO 601R-52-11-279. (M)
FOUND SERVICE DOOR LOWER SILL PROTECTOR PLATE IS CORRODED. FOUND OUT OF LIMITS IAW SRM 53-21-27. SERVICE DOOR LOWER SILL PROTECTIVE PLATE REPLACED IAW CRJ 200 SRM 51-41-04. (M)
FOUND CRACK EXIST ON ANGLE CLIP FS 280 LBL 9 INBOARD CLIP AND RBL 9 INBOARD CLIP. REPLACED IAW CRJ 200 SRM 51-42-06. (M)
HYDRAULIC SUPPORT BRACKET OF MLG BAY FOUND CRACKED. REPLACED HYD SUPPORT BRACKET OF MLG BAY LT FS 529.50 LBL 31 IAW CRJ 200 SRM 51-42-06 ML 1617. (M)
RIGHT SIDE INTERNAL LEADING EDGE WS 163, BAY 630AZ 1 DENT EXIST ON DEICING TUBE (PICCOLO TUBE) DYE PENETRANT PERFORMED ON DENT, ONE CRACK FOUND. PICCOLO TUBE REPLACED IAW CRJ 200 AMM 30-11-41-000-801. (M)
RIGHT ENGINE THRUST REVERSER MAIN TRACK AT 7 OâCLOCK FOUND CRACKED. REPLACED IAW CRJ 200 AMM 78-34-11-801. OP CHECK OF T/R TRANSFERRED TO MWC 115431-208. (M)
BRACKET CRACK AT JUNCTION OF NET POST AND AFT PRESSURE BULKHEAD FORWARD FACE, FS 621, CARGO BAY AREA. BRACKET FABRIATED IAW CRJ SRM 53-61-23 AND SRM 51-24-16, AND INSTALLED IAW CRJ 20 SRM 51-42-20. (M)
FOUND CRACK EXIST ON FLOORBEAM AT FUSELAGE STATION 280 RBL 9. REPAIR PERFORMED IAW REO 601R-53-11-171 REV D. (M)
ENROUTE FROM DCA T 1252Z HYD2 LOW PRESSURE MESSAGE COMPLIED WITH QRH DIVERTED. HYD QTY NR 2 SYSTEM READS ZERO. PRESSED FDR EVENT BUTTON. LANDING WEIGHT 46900, BRAKE TEMP READS 4,5,4,4. REMOVED AND REPLACED ENGINE DRIVEN HYDRAULIC PUMP NR 2. OPERATIONAL AND LEAK CHECKS GOOD. (K)
LEFT THRUST REVERSER UNLOCK MESSAGE DURING CRUISE FLIGHT. CWM ACTION REF 154290/4 FOR MEL. DEACTIVATED TR IAW AMM IAW AMM 78-30-00. REMOVED AND REPLACED LT ENGINE POWER DRIVE UNIT IAW AMM 78-32-03. OPERATIONAL CHECK GOOD. (M)
LEFT THRUST REVERSER UNLOCKED CAUTION MESSAGE. COMPLIED WITH QRH. AIR RETURN BACK TO PHL. LUBED LT T/R TRACKS. CLEANED STOW SWITCH. OPS CHECK GOOD IAW 78-30-00. REMOVED FROM MEL. (M)
FUSELAGE SKIN SUSTAINED LIGHTNING STRIKE DAMAGE AT FS 559, STRINGER 13R AT FASTENER HOLE. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE LIGHTNING STRIKE DAMAGE FUSELAGE SKIN AT RT SIDE FS 559 PLUS 13 BY CUTTING OUT THE DAMAGED SKIN SECTION AND FABRICATING REPAIR PARTS IAW BSC EO 601R-53-9009A. (M)
REQUEST INSPECTION FOR POSSIBLE LIGHTNING STRIKE. ALTITUDE WAS 5000 FEET GEAR RETRACTED, FLAPS UP. ENGINE NR 2 POWER ROLLED BACK TO 29 PERCENT, N1 FOR TWO MINUTES, ENGINE POWER RECOVERED. NO OTHER INSTRUMENTATION MALFUNCTIONS NOTED. COMPLIED WITH INSPECTION OF ENGINES. NO DEFECTS NOTED IAW CRJ AMM 72-00-00-210-006. (M)
UPON POST FLIGHT INOPERATIVE NOTED SMOKE COMING FROM APU INLET DOOR. INSPECTED APU INLET AND COMPARTMENT FOUND NO EVIDENCE OF OIL LEAK OR SMOKE. RAN APU FOR SEVERAL MINUTES, SHUTDOWN OPS CHECK NORMAL AT THIS TIME. (K)
MWC 258 CREW ESCAPE HATCH OUTER HANDLE SHAFT HAS PITTING, CORROSION. REMOVED OUTER HANDLE ASSY AND INSTALLED NEW HANDLE ASSY, PN H341937, IAW AMM. (K)
RT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED. MAINTENANCE PERFORMED REPAIR TO RT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K)
NUMEROUS NICKS IN PAIR AND/OR SKIN ON AFT FUSELAGE RT SIDE FS 589 TO 605 BETWEEN STRINGERS 21R TO 26R. REPAIRED DAMAGED AREA IAW EO BY CUTTING AWAY DAMAGE AND INSTALLING FILLERS AND EXTERNAL DOUBLERS. (K)
THE FUSELAGE 5 KM BETWEEN VS 55.625 PERCENT AND VS 67.5 PERCENT. SPAR DATUM BETWEEN STRINGER 2R AND 4R HAS A DENT 1.5 INCH LONG X 1.875 INCH WIDE X .109 INCH DEEP. REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN VS 55.625 AND VS 67.5 SPAR DATUM BETWEEN STRINGERS 2R AND 4R IAW EO. (K)
LT FS621 FLOOR SUPPORT ANGLE IS CRACKED MAINTENANCE PERFORMED REPAIR TO LT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K)
RT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED. PERFORMED REPAIR TO RT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K)
LT FS640 BONDED SKIN CRACKED. REPAIRED LT BONDED DOUBLER AT FS 640 BY FABRICATING ANGLE AND INSTALLING BETWEEN STR6L AND 14L. (K)
WO 87925, MWC 213, FS484, RBL36 IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCH LONG. REPAIRED CRACKED ANGLE AT FS 484, RBL36 BY REMOVING AND REPLACING ANGLE WITH FABRICATED ANGLE IAW REO. (K)
OB CLIP AT FS 280, LBL 9.0, IS CRACKED IN RADIUS AT TOP OF CLIP CRACK APPROX .5 INCH LONG. REMOVED AND REPLACED FS 280, LBL 9.0 FLOORBEAM TO BULKHEAD ATTACHMENT ANGLE IAW SRM (OB CLIP). (K)
FS 484, LBL 36, IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCH LONG. (K)
FS484, RBL 36 IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCHES LONG. (K)
IB CLIP AT FS280, RBL 9.0, IS CRACKED IN RADIUS AT TOP OF CLIP, APPROX .5 INCH LONG. REMOVED AND REPLACED FS 280, RBL 9.0 FLOORBEAM TO BULKHEAD IB ATTACHMENT ANGLE IAW SRM. (K)
WO 87925, MWC 214, FS484, LBL 36 IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCH LONG. REPAIRED CRACKED ANGLE AT FS 484, LBL 36 BY REMOVING AND REPAIRING ANGLE WITH FABRICATED ANGLE IAW REO. (K)
OB CUP AT FS280, RBL 9.0 IS CRACKED IN RADIUS AT TOP OF CUP, APPROX .50 INCH LONG. REMOVED AND REPLACED FS280, RBL 9.0 FLOORBEAM TO BULKHEAD ATTACHMENT ANGLE IAW SRM (OB CLIP). (K)
OB CLIP AT FS 280, RBL 9.0 IS CRACKED IN RADIUS AT TOP OF CUP, APPROX .50 INCH LONG. REMOVED AND REPLACED FS 280, RBL 9.0 FLOORBEAM TO BULKHEAD ATTACHMENT ANGLE IAW BRAS SRM (OB CLIP). (K)
OB CLIP AT FS 280, LBL 9.0 IS CRACKED IN RADIUS AT TOP CLIP, CRACK APPROX .50 INCH LONG. REMOVED AND REPLACED FS 280, LBL 9.0 FLOORBEAM TO BULKHEAD ANGLE IAW SRM (OB CLIP). (K)
PAX DOOR AFT DRAG ANGLE CRACKED APPROX 1.0 INCH LONG AT DOOR SUPPORT CABLE PULLEY. CUT AWAY DAMAGED SECTION OF DRAG ANGLE AND INSTALLED REPAIR ANGLE AND SPLICES IAW REO. (K)
FS 621 TO FS 625 TOP RT INTERCOSTAL ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. (K)
MWC 22, FS 621 TO FS 625 TOP LT INTERCOSTAL ANGLE CRACKED 1.5 INCH LONG IN AFT RADIUS. C/A IN PROGRESS. (K)
FLAPS FAIL CAS APPROACH, MYR FLAPS SELECTED NOT MOVE QAR C/W FLAPS ZERO LANDING. ACCOMPLISHED -30 DEGREES. REMOVED AND REPLACED LT BPSU IAW AMM. OPS CHECK GOOD. (K)
DURING APPROACH, WHEN SELECTING FLAPS FROM 30 TO 45 AIRCRAFT STARTED ROLLING LT, REQUIRED HALF AVAILABLE AILERON TRIM AND RT CONTROL WHEEL INPUT TO KEEP WINGS LEVEL. FLAP TRAVEL APPEARS UNEVEN. PERFORMED FLAP RIG CHECK, OPS CHECK GOOD. SPOILER SYSTEMS OPS CHECK GOOD. INSPECTED FLAPS RUB STRIP, RUB STRIPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (K)
STANDBY AIRSPEED INOPERATIVE DURING TAKEOFF ROLL AT 80-90 KNOTS. ABORTED TAKEOFF. COMPLIED WITH ABORTED TAKEOFF INSPECTION, NO DEFECTS. PERFORMED P3 CONTAMINATION REMOVAL PER TASK 34-11-00-100-806, AND LEAK TESTED. NO LEAKS DETECTED. (M)
WHILE TAXIING AIRCRAFT LOST NR 3 HYD FLUID LEAKING AROUND NLG. REMOVED AND REPLACD RIGHT INBOARD BRAKE LINE IN NOSE COMPARTMENT. (M)
WHILE TAXIING AIRCRAFT LOST NR 3 HYDRAULIC. FLUID LEAKING AROUND NOSE LANDING GEAR. REMOVED AND REPLACED RIGHT INBOARD LINE IN NOSE COMPARTMENT. (M)