N532EA
Registered owner: AMERICAN AIRLINES INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| PSA Airlines Inc. | Operator | 2026-02-24 – 2026-02-24 | Operator named in NTSB report |
| PSA AIRLINES, INC. (VNAA) | Operator | 2026-02-24 – 2026-02-24 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
HYD SYSTEM 3 FLUID LOST AS SOON AS WE REACH CRUISE. / REMOVED AND REPLACED HYD SYS 3 PRESSURE MANIFOLD ASSY IAW CRJ 700 AMM 29-12-09-000/400-801-A01, REMOVED AND REPLACED BOTH PUMP PRESSURE SWITCHES HYD SYS 3 IAW AMM 29-34-01-000/400-802-A01, REMOVED AND REPLACED HYD SYS 3 PRESSURE TRANSDUCER IAW AMM 29-31-01-000/400-802-A01, REMOVED AND REPLACED HYD SYS 3 PRESSURE MANIFOLD RELIEF VALVE IAW AMM 29-12-07-000/400-801-A01, FLUSHED HYD SYS 3 A/C ON THE GROUND IAW AMM 29-10-00-616-803-A01, SERVICED AND BLED THE HYD SYS 3 IAW AMM 29-12-29-611-802-A01-PSA/29-10-00-870-802-A01. ALL OPS CHECK GOOD AND NO LEAKS NOTED AT THIS TIME.
ON DRILL UP OF LT PRESSURE BOX, FOUND TWO PILOT HOLES ON LBL 18 TO BE MISALIGNED. OVERSIZED MISALIIGNED HOLES IAW REO 670-53-41-797 REV--.
WHILE PERFORMING SB670BA-53-040 FUSELAGE CENTER FUSELAGE, PRIMARY STRUCTURE BS 280.00 TO 295 INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR FOUND A CRACK EXTENDING FROM BS 280 TO PAST 4TH FASTENER HOLE GOING AFT ON STRINGER 3L REPAIRED THE DAMAGE IAW REO 670-53-21-493, REV D.
L/H WING SLAT TRACK 3-3 ECCENTRIC ROLLERS, FOUND SLAT TRACK TO HAVE GROOVES ON EACH SIDE AND TOP AND BOTTOM OF TRACK. SLAT TRACK 3-3. COMPLIED WITH REO 670-57-42-1680 REV --, REMOVED AND REINSTALLED LH SLAT TRACK 3-3 PER CRJ700 AMM 27-81-41-000-803-A01 AND 27-81-41-400-803-A01.
620FH PERM REPAIR FOR DAMAGED SCREW HOLE TO THE VERTICAL STABILIZER RH SKIN BETWEEN RIB 2 & RIB 3 AND BETWEEN FRONT SPAR & STRG 1. C/W 620FH PERMANENT REPAIR FOR THE DAMAGED HOLE TO V-STAB RH SKIN BTW RIB 2 & RIB 3 AND BTW FRONT SPAR & STRG 1 (PERMANENT REPAIR FOR TEMPORARY REO 670-55-31-169) IAW MHI RJ REO 670-55-31-174 REV. --.
4X DENTS LOCATED ON LOWER SKIN UNDER PANELS 195DL AND 196DR APPROXIMATELY @FS 969 STRINGER 26L - 27. #1: .4 X .4 X .019. #2: .8 X .4 X .011. #3: 1.0 X .7 X .027. #4: 1.1 X 1.1 X .034. DAMAGE IS NOT ALLOWED IN THIS AREA PER CRJ700 SRM 53-51-01-101-003-A01. REPAIRED IN ACCORDANCE WITH DOCUMENT MJI UCL REO 670-53-00-738 REV --.
GOUGE DAMAGE TO LH FIXED LEADING EDGE 621AT, ABOVE LANDING/TAXI LIGHT. SMOOTH AND BLENDED DAMAGED AREA IAW CRJ 900 SRM 57-41-01-201-001-A01, NDT COMPLIED WITH, AREA RE-FINISHED IAW REO 670-57-41-576.
INTERCOSTAL C/T STRINGER 20R, BETWEEN FRAMES AT FS310.00 AND FS319.70, BELOW AND FORWARD OF THE SERVICE DOOR LOWER SILL (WL72.50), HAS LIGHT CORROSION ON THE UPPER FACE. 319.70 HAS ELONGATED HOLE THROUGH INTERCOSTAL AND DRILL START IN STRINGER. HOLE MEASURES: .235 X .160 THROUGH INTERCOSTAL. REPAIR AND INSTALLATION OF INTERCOSTAL AND STRINGER COMPLETED IAW REO 670-53-21-2451. PERFORMED BLEND OUT OF DAMAGE TO SMOOTH CONTOUR IN 2 (EA) AREAS PER SRM 51-12-00 (20:1 TRANSITION) AND NDT PER 51-20-006 AND DETERMINED REWORKED AREAS WERE CRACK FREE PER PARAGON NDT JOB NO. A270824. FINAL REPAIR HOLE SIZE .2750" DIA. PERFORMED REPAIR STEPS 1 THRU 12. INSTALLED THE 2 (EA) MANUFACTURED FREEZE PLUGS 670-53-21-2451-1 AND -2 ON STRINGER AND INTERCOSTAL.
FOUND SCRATCHES UNDER SEALANT ON RH SLAT #1 ACCESS FLANGE, 4TH OUTBOARD, BETWEEN WS92.20 TO WS102.43. REPAIRED IAW EA-A1-670-57-00046.
650FH PERM REPAIR - TEMPORARY DISPOSITION FOR DENT DAMAGE TO PYLON L/E SKIN, RHS. COMPLIED WITH REO M670-54-52-079 REV-- PERMANENT DISPOSITION FOR DENT & BLENDED DAMAGE TO PYLON L/E SKIN.
FLOOR SEAT TRACK #58, LOCATED AT FS863.00 TO FS977.00, RBL9.00, HAS 6 AREAS OF MILD CORROSION FROM FS874.00 TO FS957.00. REMOVED AND REPLACED SEAT TRACK #58, LOCATED AT FS863.00 TO FS977.00, RBL9.00 WITH FABRICATED SEAT TRACK FROM EXTRUSION PN 20276-288-0-0 IAW CRJ 700 REO 670-53-00-589 REV C AND AMM 53-00-49-000/400-801-A03.
LIGHT SCRATCHES FOUND IN MULTIPLE AREAS ON THE UPPER AND LOWER EDGE FRAME OF THE AFT CARGO BAY DOOR. @ STRINGER 11-STRINGER 20 FS977-FS1051. LH SIDE SKIN PN: MM670-35116-007. SMOOTHED AND BLENDED LIGHT SCRATCHES FOUND IN MULTIPLE AREAS ON THE UPPER AND LOWER EDGE FRAME OF THE AFT CARGO BAY DOOR AT STR11L - STR20L FROM FS977 TO FS105 AND REMOVED AND REPLACED ANY AFFECTED FASTENERS AND RE-APPLIED CHEMICAL CONVERSION COATINGS IAW MHI RJ REO 670-53-61-2347 REV --.
FLOOR SEAT TRACK #54R, LOCATED AT FS677.00 TO FS863.00, RBL9.00, HAS 11 AREAS OF MILD CORROSION FROM FS678.00 TO FS863.00, A GOUGED LUG (I/B SIDE) AT FS812.00, AND GOUGES IN THE BOTTOM OF THE TRACK CHANNEL FROM FS764.00 TO FS775.00. REMOVED AND REPLACED SEAT TRACK #54R, LOCATED AT FS677.00 TO FS863.00, RBL9.00 WITH FABRICATED SEAT TRACK FROM EXTRUSION PN 20276-288-0-0 IAW CRJ 700 REO 670-53-00-589 REV C AND AMM 53-00-49-000/400-801-A03.
CARGO TRACK #1 RBL27.00, LOCATED AT FS977.13 TO FS1005.13, HAS MILD CORROSION AT FS 989.00 AND FROM FS993.00 TO FS1005.13. REMOVED AND REPLACED SEAT TRACK CARGO TRACK #1 RBL27.00, LOCATED AT FS977.13 TO FS1005.13 WITH FABRICATED TRACK FROM EXTRUSION PN 20276-288-0-0 IAW CRJ 700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-000/400-801-A03.
CARGO TRACK #1 RBL9.00, LOCATED AT FS977.13 TO FS1005.13, HAS MILD CORROSION FROM FS994.00 TO FS1000.00 AND UPPER SURFACE CORROSION AT FS994.00. REMOVED AND REPLACED SEAT TRACK CARGO TRACK #1 RBL9.00, LOCATED AT FS977.13 TO FS1005.13 WITH FABRICATED TRACK FROM EXTRUSION PN 20276-288-0-0 IAW CRJ 700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-000/400-801-A03.
CORROSION ON AREAS B, C ARE COMMON TO STRINGER 22R FS333. FRAME CLEAT PN:SH670-31253-3. : FABRICATED FRAME CLEAT C/T STRINGER 22 @FS333 FROM 2024T3-0.050 LOT#446842B7/1.16.1 PER BOMBARDIER DRAWING #:SH670-31253 REV. A, AND INSTALLED IAW CRJ700 SRM TASK 51-42-06-001-A01. APPLIED SURFACE FINISH IAW CRJ 700 SRM 51-25-01-001-001-A01.
FLOOR SEAT TRACK #57, LOCATED AT FS863.00 TO FS988.25, LBL9.00, HAS 5 AREAS OF MILD CORROSION FROM FS875.00 TO FS957.00, ONE GOUGED LUG AT FS956, AND A SECTION WITH GOUGES IN THE TRACK CHANNEL FROM FS926 TO FS936. REMOVED AND REPLACED SEAT TRACK #57, LOCATED AT FS863.00 TO FS988.25, LBL9.00, WITH FABRICATED SEAT TRACK FROM EXTRUSION PN 20276-288-0-0 IAW CRJ 700 REO 670-53-00-589 REV C AND AMM 53-00-49-000/400-801-A03.
FLOOR SEAT RAIL #54L, LOCATED AT FS677.00 TO FS863.00, LBL9.00, HAS 12 AREAS OF MILD CORROSION FROM FS677.00 TO FS862.00.
FLOOR SEAT TRACK #56, LOCATED AT FS923.00 TO FS977.00, LBL27.00, HAS MILD CORROSION FROM FS969.00 TO FS974.00. : REMOVED AND REPLACED SEAT TRACK #56, LOCATED AT 923.00 TO FS977.00, LBL27.00, WITH FABRICATED SEAT TRACK FROM EXTRUSION PN 20276-288-0-0 IAW CRJ 700 REO 670-53-00-589 AND AMM 53-00-49-000/400-801-A03.
CARGO TRACK #2, LOCATED AT FS988.25 TO 1005.13, LBL9.00, HAS MILD CORROSION ON UPPER SURFACE AT FS992.00, MILD CORROSION IN THE TRACK CHANNEL FROM FS992.00 TO 1005.13. REMOVED AND REPLACED CARGO TRACK #2, LOCATED AT FS988.25 TO 1005.13, LBL9.00 WITH FABRICATED TRACK FROM EXTRUSION PN 20276-288-0-0 IAW CRJ 700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-000/400-801-A03.
STRINGER 24R HAS MULTIPLE AREAS OF CORROSION BETWEEN FS310-FS349. REMOVED CORRODED STRINGER 24R FWD (FS280-FS333) AND AFT(FS333-FS349) AND WET INSTALLED NEW STRINGER 24R FWD AND AFT IAW CRJ700 SRM 51-42-06-001-001-A01. PERFORMED STRINGER SPLICE @349-364 IAW CRJ700 SRM TASK 53- 00-03-201-001-A01 REPAIR S6295 TYPE Z10. RESTORED SURFACE FINISH ON INTERIOR AND EXTERIOR OF STRINGERS IAW CRJ700 SRM 51-25-21-001-001-A01.
CORROSION FOUND ON STRINGER 22R PN:SH670-31210-2 AT FS.340-FS349. NO REPAIRS ALLOWED PER CRJ700 SRM TASK 53-00-03-201-001-A01. REMOVED CORRODED STRINGER 22R FWD(280-333) AND AFT(333-349) AND WET INSTALLED NEW STRINGER 22R FWD AND AFT IAW CRJ700 SRM 51-42-06-001-001-A01. PERFORMED STRINGER SPLICE @295-310 IAW CRJ700 SRM TASK 53-00-03-201-001-A01 REPAIR S6295 TYPE Z10. RESTORED SURFACE FINISH ON INTERIOR AND EXTERIOR OF STRINGERS IAW CRJ700 SRM 51-25-21-001-001-A01.
STRINGER 23R HAS SEVERAL AREAS OF CORROSION FROM FS310-FS349. AREAS FROM FS319-FS349 ARE NO REPAIRS ALLOWED PER CRJ700 SRM 53-00-03-201-001-A01. REMOVED AND REPLACED CORRODED STRINGER 23R FWD(FS280-FS333)AND AFT(FS333-FS379) PER CRJ700 SRM 51-42-06-001-001-A01. REMOVED AND REPLACED CORRODED STRINGER JOINT PIECE @FS333 IAW CRJ700 SRM 51-42-06-001-001-A01. APPLIED SURFACE FINISH ON INTERIOR AND EXTERIOR OF SKIN IAW 51-25-21-001-001-A01.
FLOOR SEAT RAIL #48, LOCATED AT FS350.00 TO FS485.00, RBL9.00, HAS 4 AREAS OF MILD CORROSION FROM FS356.00 TO FS469.00 AND GOUGES IN THE BOTTOM OF THE TRACK CHANNEL IN 2 SECTIONS FROM FS419.00 TO FS437.00 AND FS455.00 TO FS473.00. REMOVED AND REPLACED FLOOR SEAT RAIL #48 LOCATED AT FS350.00 TO FS485.00 ON RBL9.00 IAW CRJ 700 AMM 53-00-49-000/400-801-A03.
PERM REPAIR - SKIN, FUSELAGE - BETWEEN FS1031.00 AND FS 1051.30 AND STR 22R AND STR 25R. PERFORMED PERM REPAIR - SKIN, FUSELAGE - BETWEEN FS1031.00 AND FS 1051.30 AND STR 22R AND STR 25R IAW REO-670-53-61-2326 REV--.
PASSENGER DOOR SILL, MIDDLE DRAIN TUBE ASSY IS CORRODED. REMOVED DAMAGED DRAIN TUBE ASSY AND REPLACED WITH A NEW ASSY (SH670-31904-5) WITH PERMANENT FASTENERS IAW CRJ700 SRM TASK 51-42-20-001-001-A01. TOUCH UP PAINT AND FASTENERS IAW CRJ700 SRM TASK 51-25-01-001-001-A01, SEALED WITH PS 870 B2 LOT # 57940114F EXP 8/24 IAW CRJ 700 SRM 51-23-00-001-001-A01.
UPON REMOVING RH WINDSHIELD, SEVERAL GOUGES WERE FOUND IN THE FWD. LOWER SILL PN:CC670-33195-5. BLENDED DAMAGE ON RH LWR FWD SILL, ROTO-PEENED REWORKED AREA IAW CRJ700/900 SRM 51-24-11 PER REO 670-53-11-2000, REV--. USED TUNGSTEN CARBINE 9/16 X 1.25" DOUBLE ROW FLAPPER. ALMEN TYPE "A" GRADE 1 TEST STRIP (LOT 034438-36) USED ON A 3M MAGNETIC BASE WITH 3M CORRECTION AT 300 RPM AND INTENSITY OF 0.008 TO DETERMINE A WORK TIME OF 19 MINUTES AND 52 SECONDS AND ALODINE PB34707129 EXP:11-21-25 AND EPOXY PRIMER BASE BATCH # 8473304075 EXP- :01/31/2026, CURING SOLUTION BATCH #8473319025 EXP:01/31/2026 AT REWORKED AREA IAW CRJ700/- 900 SRM 51-24-11 PER REO 670-53-11-1999, REV--.
UPON REMOVING COCKPIT RH SIDE WINDOW, TOOL MARKS/GOUGES WERE FOUND ON RH LOWER AFT SILL PN: CC670-33196-2. BLENDED DAMAGE ON RH LWR AFT SILL, ROTO-PEENED REWORKED AREA IAW CRJ700/900 SRM 51-24-11 PER REO 670-53-11-1999. USED TUNGSTEN CARBINE 9/16 X 1.25" DOUBLE ROW FLAPPER. ALMEN TYPE "A" GRADE 1 TEST STRIP (LOT 034438-36) USED ON A 3M MAGNETIC BASE WITH 3M CORRECTION AT 300 RPM AND INTENSITY OF 0.008 TO DETERMINE A WORK TIME OF 17 MINUTES AND 52 SECONDS AND APPLIED FINAL FINISH IAW REO 670-53-11-1999, REV--.
PASSENGER DOOR SILL, AFT DRAIN TUBE ASSY (P/N SH670-31904-5) IS CORRODED AND HAS A LARGE HOLE ON THE BACKSIDE / RADIUS OF THE TUBE. - REMOVED AND REPLACED DRAIN TUBE ASSY (SH670-31904-5) AND INSTALLED NEW SOLID RIVETS (MS20470AD5-9) IAW CRJ700 SRM TASK 51-42-06-001-001-A01. TOUCH UP PAINT AND FASTENERS IAW CRJ700 SRM TASK 51-25-01-001-001-A01.
FWD, AFT BAGGAGE BAY TRACK P/N CC670-38809-1 ROLLER GUIDE, LOWER, FWD, DOOR SURROUND, HAS TWO GOUGES ON THE I/B SIDE OF THE OPENING ROUGHLY 0.60" LONG AND 0.050" WIDE. BLENDED IAW CRJ 700 SRM 51-12-00 USING A 20:1 RATIO. NOMINAL THICKNESS .080" AND MINIMUM THICKNESS IS .078". EDDY CURRENT FOUND NO INDICATIONS DETECTED. ALODINED WITH BONDERITE M-CR 1132 LOT: PB 34457792 M48241 EXP: 11-02-25 AND PRIMED WITH BATCH: 8473347011 EXP: 02/26 AREAS WORKED IAW CRJ 700 SRM 51-21-11 AND 51-25-06. RESTORED FINISH OF THE RE WORKED AREA A023 PER SRM 51-21-16. ALL COMPLETED IAW MHIRJ REO 670-53-61-2315.
AFT CARGO DOOR SILL IS CORRODED
INTERCOSTAL 27L BETWEEN FS349 AND FS364 IS CORRODED
AFT CARGO DOOR SILL IS CORRODED
AFT BELLY FAIRNING SUPPORT STRUCTURE FROM FS879 TO FS939 STR24R STRAP WITH NUTPLATES ATTACHED HAS SEVERAL AREAS OF CORROSION AROUND NUTPLATES ON BOTTOM SIDES.
INTERCOSTAL 26L CORRODED BETWEEN FS 349 AND FS 364
TAKING OFF OUT OF DCA THE RH ENGINE DID NOT ACHIEVE TAKEOFF POWER SO THE TAKEOFF WAS ABORTED. RH ENG LOW PWR ON TAKE OFF ROLL HIGH SPEED ABORT. REMOVED AND REPLACED FUEL METERING UNIT IAW 73-21-03-000/400-801-A01. OPS AND LEAK CHECK OF THE FMU GOOD AT THIS TIME. ENGINE RUN AND FURTHER OPS CHECK REQUIRED. POWER ASSURANCE AND ACCELERATION TEST NEEDS TO BE C/W. REFER TO LOGPAGE 1989518-4 FOR FURTHER MAINTENANCE. RH ENGINE BORESCOPE COMPLETED. FOUND DAMAGE (FOD) ON STAGE 6 OF COMPRESSOR. SEE WO#4 LOGBOOK 1989522 FOR FURTHER MAINTENANCE IAW CF34-8C LMM 72-00-00 INSPECTION 003.
HYD 1 LO PRESS CAUTION MSG ALONG WITH HYDRAULIC 1 SOV CLSD STATUS MSG AND ENGINE BOTTLE SWITCH LIGHTS ILLUMINATED AND LH ENG BLEED CAUTION MSG SHORTLY AFTER TAKEOFF. QRH WAS RAN AND MESSAGES CLEARED. ON CLIMB OUT HYD 1 LO PRESS CAUTION MSG ALONG WITH HYDRAULIC 1 SOV CLSD STATUS MSG AND ENGINE BOTTLE SWITCH LIGHTS ILLUMINATED. QRH CLEARED. PERFORMED OPS TEST OF HYD SYSTEM NR 1 IAW AMM 29-10-00-710-801, OPS TEST GOOD. PERFORMED OPS TEST OF HYD SYSTEM NR 1 FIREWALL-SHUTOFF-VALVES IAW AMM 29-11-36-710-806, OPS TEST GOOD. PERFORMED FUNCTIONAL TEST OF EDP 1A IAW AMM 29-11-01-720-801, FUNCTIONAL TEST GOOD, NO LEAKS EVIDENT. C/W TAP 0225 TO STEP 7. DIAGNOSED B1-007205 FOR LDU/ NO CHANNEL B OUTPUT, AND FOUND THAT THE LDU HAD AN INTERNAL FAULT PER FIM 31-41-07-810-817. R & R LDU IAW 31-41-07-000/400-801-A01. OPS CHECKED GOOD, NO FURTHER FAULTS FOUND. R & R K137 RELAY BY REQUEST IAW AMM 24-01-05-000/400-801-A01. OPS CHECK GOOD. NO FAULTS FOUND. COMPLETED TAP STEP 7. R & R JB3 PCB 2 IAW AMM 24-02-05-000/400-801. CW OPS CHECK IAW AMM 24-02-05-710-801. OPS CHECK STEPS 8,9,12 STILL NEED CW. COMPLETED OPS TESTS IAW AMM 24-02-05-400-801. STEPS 8 AND 9. OPS TEST GOOD. OPS TEST STEPS 12 (ADG SPIN-UP) STILL NEED C/W. COMPLIED WITH FUNCTIONAL TEST OF THE ADG IAW AMM 24-23-01-720-801 CHECKED GOOD. PERFORMED OPS TEST OF BLEED VALVES IN NORMAL FUNCTION MODE, NO FAULTS NOTED. PERFORMED OPS TEST OF THE BLEED-AIR MANUAL CONTROL MODES IAW AMM 36-10-00-710-801, ALL MODES OPS TEST GOOD. RAN ENGINES AT POWER FOR 50 MINUTES WITH LT BLEED SELECTED MANUAL. NO DEFECTS NOTED. MANUAL BLEED OPS TEST GOOD IAW AMM 36-10-00-710-801. OCF FLIGHT WAS FOUND TO BE SATISFACTORY, NO DEFECTS NOTED DURING THE FLIGHT.
ROW 16 OVERHEAD AND LOWER ROW 16AC EMERGENCY LIGHTS NOT ILLUMINATING. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW 33-51-17-400-801 OPS CHECK GOOD.
STRINGER 27 IS CORRODED JUST AFT OF FRAME FS280. REMOVED AND REPLACED STRINGER 27 JUST AFT OF FS280.00 IAW SRM 51-42-06 AND SRM 51-42-20.
DENTS ON LEFT INBOARD FLAP LOWER SIDE 17 INCHES FROM INBD EDGE 4 INCHES FROM THE TRAILING EDGE. -C/A-REPAIRED LH INBD FLAP LOWER SIDE IAW SRM 57-52-01-991-812.
RT WING INBOARD FLAP UNDER SIDE HAD FOUR DENTS. COMPLIED WITH REPAIR IAW ERS-CR-57MR-1173 01
FRAME AT FS 319.0 IS CORRODED FWD SIDE BETWEEN STR 26L & 26R-C/A-COMPLETED FRAME REPAIR IAW SRM 53-00-06
FRAME AT FS 333.0 IS CORRODED FWD AND AFT SIDES BETWEEN STR 26R AND STR 27-C/A-COMPLETED THE FRAME REPAIR AT FS 333.00 IAW SRM 53-00-06 AND SRM 51-42-21
SERVICE DOOR SILL HAS AREAS OF CORROSSION BETWEEN FS 319.70 ANS 349.00-C/A-REMOVED AND REPLACED SERVIE DOOR SILL ANGLE IAW SRM51-42-21 AND 51-42-06.
STRINGER 26 RT IS CORRODED BETWEEN FS FRAME 280.00 AND FS FRAME 295.00-C/A-RAR STRINGER 26 RT BETWEEN FS280 AND FS333 IAW SRM 51-42-06.
STRINGER 25 RT IS CORRODED BETWEEN FRAME FS280.00 AND FS295.00. C/A-R&R STRINGER 25R BETWEEN FS2800.00 AND FS295.00 IAW SRM 51-42-06.
STRINGER 26 LT WAS CORRODED BETWEEN BS 2800 AND 295. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06 AND 53-21-03.
RIGHT FLOOR BEAM AT FS280.00 HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE THERE IT IS LAYERED BETWEEN DRIP TRAY AND UPPER L ANGLE-C/A-REMOVED AND REPLACED RT FLOOR BEAM AT FS 280 IAW SRM 51-42-06 AND SRM 51-42-13.
LEFT SIDE LOWER BULKHEAD AT FS 280.00 HAS CORROSION. COMPLETED INSTALLATION OF THE LHS LOWER BULKHEAD WEB AND DOUBLER IAW SRM 53-11-10.
LEFT FLOOR BEAM AT FS280.00 HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE WHERE IT IS LAYERED BETWEEN DRIP TRAY AND UPPER L ANGLE.-C/A-REMOVED AND REPLACED LH FS280.00 CROSSBEAM IAW SRM 51-42-06 AND SRM 51-42-13.
RIGHT SIDE LOWER BULKHEAD AT FS280.00 HAS CORROSION.-C/A-REMOVED AND REPLACED RH SIDE LOWER BULKHEAD AT FS-280.00 IAW SRM 53-11-10.
RH CENTER COCKPIT FLOOR BEAM BL12.00 IS CRACKED JUST FWD OF FLOOR BEAM AT FS 280.00. REPAIRED RH CENTER COCKPIT FLOOR BEAM BL 12.00 IAW SRM 53-11-43.
PAX DOOR STEP SHELL HAS APPROX 1" CRACK BY FWD SIDE JUST BELOW THE BOTTOM STEP (DOOR CLOSED). C/A-REPAIRED IAW SRM 52-11-04.
PAX DOOR STEP SHELL HAS APPROX 1" CRACK BY AFT SIDE JUST BELOW THE BOTTOM STEP (DOOR CLOSED). C/A-REPAIRED IAW SRM 52-11-04.
LH CENTER COCKPIT FLOOR BEAM BL12.00 IS CRACKED JUST FWD OF FLOOR BEAM AT FS 280.00. -C/A-REPAIRED LH CENTER COCKPIT FLOOR BEAM BL 12.00 IAW SRM 53-11-43
LT SIDE OF THE FWD EQUIPMENT COMPARTMENT FLOOR PANEL HAS A 3/8" CRACK AT FS202.75. JUST AFT OF THE DOOR OPENING. C/A-REPAIRED LT SIDE OF THE FWD EQUIPMENT COMPARTMENT FLOOR PANEL IAW ETNCR-53-099R1.
FLASH LIGHT FROM COCK PIT IS INOPT.-C/A-COMPLETE:REMOVED BURNT OUT BULB FROM A COCKPIT FLASHLIGHT AND REPLACED WITH NEW BULB, OPERATIONAL CHECK GOOD. IAW AMM 25-61-00 AND CRJ EEL
LH ENGINE AIR INLET HAS APPROX 3" CRACK IN UPPER PERFORATED LINER AT IB EDGE, APPROX 1" AFT OF FWD EDGE.-C/A-FOUND DAMAGE TO BE OUT OF LIMITS IAW CRJ SRM 54-11-15. COMPLETED REMOVED AND REPLACED OF LH ENGINE AIR INLET IAW CRJ AMM 71-61-01. ENGINE RUNS, OPC, AND LEAK CHECK GOOD.
"SLAT FAIL" MSG (CAUTION) WHEN FLAPS SET 1 RESET SAME RESULT LANDED. C/A-FOUND MDC HISTORICAL MESSAGE SLAT MECHANICAL JAM. INSPECTED ALL SLAT ACTUATOR TRIP-INDICATORS AND FOUND NONE TRIPPED IAW ETN CR-27-084. OPS CHECK GOOD, SLATS SERVICEABLE. SUSPECT IT WAS ICING CONDITIONS ON LANDING.
FUEL CAP CAME OFF INFLIGHT. C/A-INSTALLED FUEL CAP ON RT WING IAW AMM 28-11-16.
STEERING INOP CAUTION IN FLIGHT. REMOVED AND REPLACED STEERING MANIFOLD IAW MM 32-51-50. OPS CK & LEAK CK GOOD.
RT SIDE FUSELAGE TRAILING EMERGENCY LIGHT INOP. REPLACED RT SIDE FUSELAGE TRAILING EMERGENCY LIGHT BULB IAW CMM 33-52-07. OPS TEST OF THE RT TRAILING EXTERIOR LIGHT WAS DONE IAW AMM 33-51-15.
CABIN FLOOR EMERGENCY LIGHTING STRIP DETACHED. SECURED THE RIGHT EMERGENCY LIGHT STRIP IN FRONT OF ROW 1 PAX SEATS.
GROUND DISPLAY FAN VERY LOUD ACCOMPANIED BY A BURNING ELECTRICAL ODOR. AFTER TROUBLESHOOTING, FOUND THE NR 2 FAN OF THE AVIONICS DISPLAY UNIT WAS THE CAUSE THE ODOR & NOISE. REMOVED AND REPLACED NR 2 DISPLAY COOLING FAN AND OP CK GOOD IAW AMM 21-24-12.
LEFT INBD FLAP LOWER SURFACE IS DAMAGED APPROX 17" FROM INBD EDGE. REPAIRED LT INBOARD FLAP LOWER SURFACE IAW ERS-CR-57MR-792.
PASSENGER DOOR FORWARD SIDE SKIN REPAIR DOUBLER CRACKED AT SECOND FROM BOTTOM RADIUS. COMPLETED REPAIR IAW SRM CH 52-11-04 TEMPORARY REVISION 52-0025.
PASSENGER DOOR STEPS AFT SIDE SKIN REPAIR DOUBLER CRACKED, SECOND FROM BOTTOM RADIUS. REPAIRED DAMAGED AREA IAW SRM 52-11-04 TEMP REVISION 52-005.
DURING DESCENT BELOW 20,000, F/A 1 CALLED WITH AN ACCETONE TYPE AROMA IN GALLEY AREA. BOTH F/A 1&2 ADVISED OF AN ELECTRICAL ODOR BEGINNING AROUND ROW 6 AND ALSO IN FRONT OF LAVATORY. COMPLIED WITH CABIN ABNORMAL ODOR FIM TASK 21-22-00-810-806. IN PROCESS, FOUND DEFECT WITH GALLEY HEATER. NO FURTHER DEFECTS NOTED. REMOVED AND REPLACED GALLEY HEATER IAW AMM 21-23-64. NO DEFECTS NOTED.
MAIN CABIN DOOR IS HARD TO OPEN. REPORTED BY NR 1 FLT ATTD. CLEANED/LUBRICATED DOOR IAW SMP. AIRCRAFT OK FOR SERVICE.
LT EMERGENCY FLOOR LIGHTING STRIP JUST AFT OF EMERGENCY EXIT ROW HAS CRACKED COVER. R&R LT EMERGENCY FLOOR LIGHTING STRIP COVER JUST AFT OF EMERGENCY EXIT ROW IAW AMM 33-51-01.
CPCP SSI 532047, LEFT BULKHEAD CORNER AT FLIGHT COMPARTMENT THRESHOLD ABOVE FS 280.00 IS SEPARATING DUE TO CORROSION. REPAIRED LT BULKHEAD LOWER WEB IAW SRM 53-11-10.
FLOOR SUPPORT FS 280.00 IS CRACKED ON THE LT SIDE. REPAIRED FLOOR SUPPORT FS 280.00, LT SIDE IAW SRM 53-11-41.
HYD 3 LOW PRESSURE. REMOVED PANEL 293BR AND 1 AFT OF 233BR, AMM 53-52-32. INSPECTED AND FOUND RT PRESSURE TRANSDUCER LEAKING. ITEM 3 OF THIS LOG PAGE. REAPPLIED PANEL 195EV AND 196 EV IAW 53-52-72 AMM. FOUND SIGNIFICANT LEAK FROM NR 3 HYDRAULIC PRESSURE TRANSDUCER. R&R SYS NR 3 PRESSURE MANIFOLD IAW AMM 29-12-09. OPS AND LEAK CHECK GOOD. R&R SYS NR 3 RT PUMP ALTERNATING CURRENT MOTOR (ACMP) IAW AMM 29-12-03. LEAK CHECK GOOD. AND OPS CHECK GOOD. PUMP-AC MOTOR P/N 66195-01 S/N K0715. R&R PUMP LT AC MOTOR IAW AMM 29-12-03. LEAKS CHECK GOOD AND OPS CHECK GOOD PUMP-AC MOTOR P/N 66195 S/N K2430. R&R SYS NR 3 RETURN MANIFOLD FILTER ELEMENT IAW AMM 29-12-36. LEAKS CHECK GOOD. R&R SYS NR 3 CASE DRAIN FILTER ELEMENT IAW AMM 29-12-36. LEAKS CHECK GOOD. R&R SYS NR 3 PRESSURE TRANSDUCER IAW AMM 29-31-01. OPS AND LEAKS CHECK GOOD. PRESSURE TRANDUCER P/N 945173-3 S/N PT2383.
OVERWING EMER LIGHTS WONâT GO OFF. R & R NR 4 EPSU BATTERY PACK IAW AMM 33-51-17. OPERATIONS CHECK IS GOOD. EMER LIGHTING BATTERY PN 2013-1A & SN 108104.
FUMES IN CABIN AT FL 330 EMER DESCENT, GOT WORSE UPON DESCENT. PERFORMED GVI OF COOLING DUCTS & CLAMPS IN AFT EQUIP BAY. OPERATIONS TESTED A/C DISTRIBUTION SYS IAW AMM 21-51-00, NO FUMES OR OTHER DISCREPANCIES NOTED. FCF FOUND SATISFACTORY.
ON TAKEOFF THE TRIM CONTROLS COMPLETELY FAILED ON CAPTAIN`S SIDE & ACFT WOULD NOT AUTO TRIM NOSE UP OR NOSE DOWN ON ITS OWN REGARDLESS OF THE AUTOPILOT BEING ENGAGED OR NOT. FIRST OFFICER`S SIDE TRIM WORKED & WOULD OVERRIDE BUT WHEN YOU LET GO TRIM BEGAN AGAIN. CAPTAIN`S SIDE COULD TRIM NOSE UP ONLY AT FL290 THEN FAILED AGAIN IN DESCENT. NORMAL VISUAL APP & LANDING MADE WITH 400 FPM SINK AT TOUCHDOWN & TRANSFERRED TO NRWC 532-DFW-01155. R & R CAPTAIN`S PITCH TRIM SWITCH IAW AMM 27-41-05. OPERATIONS CHECKED GOOD IAW AMM 27-40-00. OVERWEIGHT LAND WAS WITHIN LIMITS IAW AMM 05-51-01.
ON TAKEOFF, THE TRIM CONTROLS COMPLETELY FAILED ON CAPTAIN`S SIDE & ACFT WOULD NOT AUTO TRIM NOSE UP OR NOSE DOWN ON ITS OWN REGARDLESS OF THE AUTOPILOT BEING ENGAGED OR NOT. FIRST OFFICER`S SIDE TRIM WORKED & WOULD OVERRIDE BUT WHEN YOU LET GO TRIM BEGAN AGAIN. CAPTAIN`S SIDE COULD TRIM NOSE UP ONLY AT FL 290 THEN FAILED AGAIN IN DESCENT. NORMAL VISUAL APP & LANDING MADE WITH 400 FPM SINK AT TOUCHDOWN & TRANSFERRED TO NRWC 532-DFW-01155. R & R CAPTAIN'S PITCH TRIM SWITCH IAW AMM 27-41-05. OPERATIONS CHECKED GOOD IAW AMM 27-40-00. OVERWEIGHT LAND WAS WITHIN LIMITS IAW AMM 05-51-01.
FORWARD ENTRY & SERVICE DOOR EMER LIGHTS INOPERATIVE. R & R NR 1 BATTERY POWER SUPPLY CHARGER IAW AMM 33-51-17. OPERATIONS CHECKED GOOD.
SMOKE AFT LAVATORY WARNING, EMER DECLARED. FLIGHT ATTENDANT SMELLED FUMES BUT NO SMOKE. PERFORMED AMM TASK 72-00-00-100-801 STEP H. NO FUMES OR SMELL NOTED AT THIS TIME.
DURING PS2 INSPECTION FOUND EMER EXIT SIGN NEAR THE FLOOR FOR THE LT OVERWING DS177 INOPERATIVE. R & R NR 3 EMER EPSU BATTERY PACK IAW WC 33-002. OPERATIONS CHECKED GOOD.
NUMBER 2 FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 33-50-00.
FORWARD FLIGHT ATTENDANT`S FLASHLIGHT NOT CHARGING. R & R FWD FLIGHT ATTENDANT`S FLASHLIGHT ASSEMBLY IAW MM 25-61-02, OPERATIONS CHECKED OK.
ON FLIGHT 3629 CREW REPORTED CAPTAIN`S FLASHLIGHT INOPERABLE. R & R CAPTAIN'S FLASHLIGHT IAW CRJ700 AMM 25-61-02 BRACKETS & FLASHLIGHT MOUNTING. OPERATIONS CHECKED GOOD AT THIS TIME.
AFTER TAKEOFF, PILOTS AND F/A NOTICED STRONG ODOR THROUGHOUT THE CABIN AND COCKPIT. REPAIRED TWO HYD TUBES IN AFT FUSELAGE FS 925.00 - 1162.00 IAW 20-30-00. LEAK CHECKED GOOD. PERFORMED OPS CHECK OF AIR SYSTEM. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.
DURING THE LANDING, A BURN ODOR WAS NOTICED. T NO INDICATION OF ANY ABNORMALITIES. BEFORE TOUCHING DOWN, ODOR HAD DISSIPATED. PROCEEDED TO GATE WITH NO FURTHER ISSUE. THOROUGH POSTFLIGHT INCLUDING THE ENGINES, AND NO ABNORMALITIES WERE NOTED. DURING ENGINES START UP AND TAXI, NO ABNORMALITIES WERE NOTED.
NR 1 F/A FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT HOLDER IAW AMM 25-61-02.
ON FLIGHT 3681 THE CREW REPORTED THAT ON DESCENT THRU FL 180 FLT SPOILER EXTENDED RECEIVED O/B SPOILERONS (LEFT SIDE) REMAINED ON WITH FLT SPOILERS RETRACTED. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OUTBOARD SPOILERON PCU IAW CRJ-MM-26-62-01. ALSO REMOVED AND REPLACED O-RING PART# NAS1612-4, PIN COTTER PART# MS24665-151 & COTTER PIN PART # MS24665-300. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
FLIGHT 4639, CREW REPORTED THE RED LIGHT AT ROW 13 EXIT SIGN REMAINS ON. AIRCRAFT REMOVED FROM SERVICE. RESET LAV/TOILET CIRCUIT BREAKER AS PER STANDARD MAINTENANCE PRACTICES. NO FURTHER DEFECTS NOTED. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
FOR FLIGHT 3756 WHILE AT THE GATE THE O2 MASK INADVERTENLTY DEPLOYED. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESTOWED MASK. NR 2 GENERATORS WERE ACTIVATED. THE AIRCRAFT WAS RETURNED TO SERVICE.
DURING MAINTENANCE BASE VISIT FOUND THE CABIN MEGAPHONE WEAK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN MEGAPHONE IAW CRJ700 STANDARD MAINTENANCE PRACTICES. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3876 THE CREW REPORTED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERIVCE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT IAW AMM 25-61-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
ON FLIGHT 3865 DURING TAKEOFF AT ROTATION THE CREW REPORTED, RECEIVED AN ANTI-SKID CAUTION MESSAGE ON EICAS AND ASSOCIATED GROUND SPOLIER FAULT STATUS. THE CAPTAIN DECLARED AN EMERGENCY INBOUND TO ORD. THE AIRCRAFT LANDED WITHOUT USING BRAKES. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED GENERAL VISUAL INSPECTION OF THE ANTI SKID CONTROL UNIT AND RIB WHEEL SPEED TRANSDUCER CONNECTOR/PINS. COMPLIED WITH CRJ FIM 32-44-01. RE-INITIALIZED POWER TO AIRCRAFT AND COMPLETED THE OPERATIONAL CHECK OF THE ANTI SKID AND CONTROL UNIT IAW CRJ MM 32-44-06. NO CURRENT EICAS OR MDC MESSAGES AT THIS TIME. THE OPERATIONAL CHECK WAS GOOD, SSCU OPERATIONAL CHECK GOOD IAW CRJ MM 27-61-05. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.