N398CA
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
172 reports on file, 1998-09-20 – 2026-04-21.
Part: DOOR — BINDING (ZONE 800) · airframe 46,032 hrs · 35,602 cycles
SERVICE DOOR HARD TO OPEN FROM INSIDE EVEN HARDER FROM OUTSIDE. FOUND CHAFE DAMAGE ON BACKSIDE OF ALIGNMENT MARK HOUSING. COMPLYED WITH EA CRJ752-22072.OPS TEST GOOD SEE NRWC #938126 FOR DETAILS
Part: FITTING — FAULTED (ZONE 800) · airframe 46,032 hrs · 35,602 cycles
PASSENGER DOOR HARD TO OPEN FROM OUTSIDE. ADJUSTED HANDRAILS PER AMM 52-11-05. ADJUSTED AFT SPIGOT PER AMM 53-21-23, REPLACED ROD BEARING PER FIM 52-11-00, ADJUSTED PAX DOOR OUTER HANDLE PER AMM 52-11-03. R/R AFT CAM FITTING PER SRM 51-42-21. ADJUSTED COUNTER BALANCE SYSTEM PER AMM 52-11-17. ALL CKS GOOD. SEE NRWC 938121 + NRCC 147085+147086 FOR DETAILS.
Part: FITTING — DAMAGED (AILERON) · airframe 45,987 hrs · 35,555 cycles
BUSHINGS IN AILERON LH, OVERSIZED WAS FOUND ON INBD LUG BORE TO WING TRAILING EDGE AILERON HINGE FITTING #1 AT WS294.50, LHS FOR OVERSIZED LUG BORE TO WING TRAILING EDGE AILERON HINGE FITTING #1 ASSEMBLY AT WS294.50, LHS WAS REPAIRED PER REO 670-57-51-697 REV --
Part: BEAM — CORRODED (ZONE 200) · airframe 45,987 hrs · 35,555 cycles
SEVERAL CORROSION ON BEAM RBL 9.00 BTW FS477.40 TO FS830.00 WERE FOUND. BEAM RBL 9.00 BTW FS 477.40 TO FS 830.00 WAS REPAIRED PER REP 670-53-41-827 REV --
Part: STRAP — CORRODED (ZONE 100) · airframe 45,987 hrs · 35,555 cycles
SECONDARY NRC FROM NRC:00305: AFTER REMOVAL OF CHANNELS, CORROSION ON STRAP AT PANNEL NRB 195DL. STRAP OF PANEL NR 195DL WAS FABRICATED PER EA NO: CRJ753-21742 REV. IR
Part: FITTING — CORRODED (ZONE 100) · airframe 45,987 hrs · 35,555 cycles
CORROSION ON MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE). MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE) WERE REPAIRED PER REO 670-53-41-834 REV --
Part: FITTING — CORRODED (ZONE 100) · airframe 45,987 hrs · 35,555 cycles
CORROSION ON MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE). MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE) WERE REPAIRED PER REO 670-53-41-834 REV --
Part: BEAM — CORRODED (ZONE 200) · airframe 45,987 hrs · 35,555 cycles
SEVERAL CORROSION ON BEAM LBL 9.00 BTW FS477.40 TO FS830.00 WERE FOUND BEAM LBL 9.00 BTW FS477.40 TO FS 830.00 WAS REPAIRED PER REO 670-53-41-833 REV --, REO 670-55-41-835 REV --,REO 670-53-31-1169 REV -- AND EA CRJ753-21644 REV IR
Part: FITTING — CORRODED (ZONE 100) · airframe 45,987 hrs · 35,555 cycles
CORROSION ON STGR 22L, FROM FS 389 TO FS 409, AT MAIN AVIONICS COMPARTMENT. STGR 22L, FROM FS 389 TO FS 409, AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ-700 SRM 53-00-03-201-001-A01.
Part: FITTING — CORRODED (ZONE 100) · airframe 45,987 hrs · 35,555 cycles
CORROSION ON STGR 22L, FROM FS 389 TO FS 409, AT MAIN AVIONICS COMPARTMENT. STGR 22L, FROM FS 389 TO FS 409, AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ-700 SRM 53-00-03-201-001-A01.
Part: STRAP — CORRODED (ZONE 200) · airframe 45,987 hrs · 35,555 cycles
INITIAL INSPECTION: CORROSION ON JOINT STRAP, SETTLEMENT ÿ½REA OF FAIRING ACCESS PANEL 194AB & 193AB JOINT STRAP (FRAME ASSY) SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB & 193AB WAS REPAIRED PER REO 670-53-82-733. REV. --
Part: RIB — CRACKED (ZONE 600) · airframe 45,987 hrs · 35,555 cycles
CRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT RH WING CRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT RH WING WAS REPAIRED PER REO 670-57-41-681 REV - -.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 45,987 hrs · 35,555 cycles
CRACKED CENTER COCKPIT FLOOR BEAM RBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT CENTER COCKPIT FLOOR BEAM RBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 670-53-11-2278REV. --
Part: HINGE — CORRODED (ZONE 100) · airframe 45,987 hrs · 35,555 cycles
CORROSION ON HINGE FWD/MID/AFT (3EAS), ALSO DEGRADED PAINT OF STEP PLATE AT AFT CARGO COMPARTMENT HINGE MID (P/N: MM670-35623-003) OF STEP PLATE AT AFT CARGO COMPARTMENT WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01, HINGE FWD (P/N: MM670-35622-003) WAS FABRICATED PER EA: CRJ753-21639. REV: IR., HINGE AFT (P/N: MM670-35624-003) WAS FABRICATED PER EA: CRJ753-21638. REV: IR., AND STEP PLATE AT AFT CARGO COMPARTMENT WAS PAINTED PER CRJ-700 SRM 51-25-01-001-001-A01 AND PER CRJ-700 SRM 51-25-01-001-001-A01.
Part: TRACK — CORRODED (ZONE 800) · airframe 45,987 hrs · 35,555 cycles
CORROSION ON RAILS ON FWD CARGO COMPARTMENT 10E/Aÿ½S RAILS (2EAS P/N: DSY7058-5) WERE REPLACED AND VERIFIED PER CRJ-700 IPC: 52-51-02-01 ITEM: 250, RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21615 REV. IR., RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21616 REV. IR., RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21617 REV. IR., AND RAILS (2EAS P/N: DSY7058-1) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21618 REV. IR.
Part: TRACK — CORRODED (ZONE 800) · airframe 45,987 hrs · 35,555 cycles
CORROSION ON RAILS ON FWD CARGO COMPARTMENT 10E/Aÿ½S RAILS (2EAS P/N: DSY7058-5) WERE REPLACED AND VERIFIED PER CRJ-700 IPC: 52-51-02-01 ITEM: 250, RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21615 REV. IR., RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21616 REV. IR., RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21617 REV. IR., AND RAILS (2EAS P/N: DSY7058-1) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21618 REV. IR.
Part: TRACK — CORRODED (ZONE 800) · airframe 45,987 hrs · 35,555 cycles
CORROSION ON RAILS ON FWD CARGO COMPARTMENT 10E/Aÿ½S RAILS (2EAS P/N: DSY7058-5) WERE REPLACED AND VERIFIED PER CRJ-700 IPC: 52-51-02-01 ITEM: 250, RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21615 REV. IR., RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21616 REV. IR., RAILS (2EAS P/N: DSY7058-3) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21617 REV. IR., AND RAILS (2EAS P/N: DSY7058-1) WERE FABRICATED PER CRJ-700 EA NO.CRJ725-21618 REV. IR.
Part: HINGE — CORRODED (ZONE 100) · airframe 45,987 hrs · 35,555 cycles
CORROSION ON HINGE FWD/MID/AFT (3EAS), ALSO DEGRADED PAINT OF STEP PLATE AT AFT CARGO COMPARTMENT HINGE MID (P/N: MM670-35623-003) OF STEP PLATE AT AFT CARGO COMPARTMENT WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01, HINGE FWD (P/N: MM670-35622-003) WAS FABRICATED PER EA: CRJ753-21639. REV: IR., HINGE AFT (P/N: MM670-35624-003) WAS FABRICATED PER EA: CRJ753-21638. REV: IR., AND STEP PLATE AT AFT CARGO COMPARTMENT WAS PAINTED PER CRJ-700 SRM 51-25-01-001-001-A01 AND PER CRJ-700 SRM 51-25-01-001-001-A01.
Part: HINGE — CORRODED (ZONE 100) · airframe 45,987 hrs · 35,555 cycles
CORROSION ON HINGE FWD/MID/AFT (3EAS), ALSO DEGRADED PAINT OF STEP PLATE AT AFT CARGO COMPARTMENT HINGE MID (P/N: MM670-35623-003) OF STEP PLATE AT AFT CARGO COMPARTMENT WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01, HINGE FWD (P/N: MM670-35622-003) WAS FABRICATED PER EA: CRJ753-21639. REV: IR., HINGE AFT (P/N: MM670-35624-003) WAS FABRICATED PER EA: CRJ753-21638. REV: IR., AND STEP PLATE AT AFT CARGO COMPARTMENT WAS PAINTED PER CRJ-700 SRM 51-25-01-001-001-A01 AND PER CRJ-700 SRM 51-25-01-001-001-A01.
Part: SEAL REST — CORRODED (ZONE 200) · airframe 45,987 hrs · 35,555 cycles
INITIAL INSPECTION: CORROSION ON AFT BAGGAGE BAY DOOR SEAL REST BTW FS1000.00 TO FS1047.00 AND LBL 43 APROX. CORROSION ON AFT BAGGAGE BAY DOOR SEAL REST BTW FS1000.00 TO FS1047.00 AND LBL 43 APROX WAS EVALUATED OUT LIMITS PER CRJ700 SRM 53-61-23-101-001-A01 THEREFORE WAS REPAIRED AND REPLACED PER EA NO. CRJ953-21743 REV IR AND CRJ700 SRM 51-42-06-001-001-A01 ,CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-13-001-001-A01
Part: PLATE — CRACKED (ZONE 200) · airframe 45,987 hrs · 35,555 cycles
CRACK ON SUPPORT PANEL OF RH SIDE CONSOLE AT FLIGHT COMPARTMENT. SUPPORT PANEL OF RH SIDE CONSOLE AT FLIGHT COMPARTMENT WAS REPAIRED PER EA CRJ725-21690 REV. IR
Part: DRAIN PAN — CRACKED (ZONE 200) · airframe 45,987 hrs · 35,555 cycles
CRACK AND BEND LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT. LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT WERE REPAIRED PER CRJ/700 SRM 51-71-59-001-001-A01 AND CRJ/700 SRM 51-25-16-001-001-A01
Part: STIFFENER — WORN (ZONE 100) · airframe 45,987 hrs · 35,555 cycles
INITIAL INSPECTION: WEAR ON INTERNAL SKIN AND ANGLE ON TAIL BUMPER CUTOUT AREA BTW STGR 26L TO STGR 27R AND VS67.5% APPROX AT AFT EQUIPMENT COMPARTMENT PAINT ON INTERNAL SKIN WAS REMOVED AND NOT DAMAGE WAS FOUND PER CRJ-700 SRM 51-26-01-001-001-A01 AND ANGLE ON TAIL BUMPER CUTOUT AREA BTW STGR 26L TO STGR 27R AND VS67.5% APPROX AT AFT EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01
Part: DRAIN PAN — CRACKED (ZONE 100) · airframe 45,987 hrs · 35,555 cycles
CRACK AND BEND LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT. LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT WERE REPAIRED PER CRJ/700 SRM 51-71-59-001-001-A01 AND CRJ/700 SRM 51-25-16-001-001-A01
Part: ANGLE — CORRODED (ZONE 200) · airframe 45,987 hrs · 35,555 cycles
INITIAL INSPECTION: CORROSION ON MID CAP AT PASSENGER DOOR CUTOUT. CORROSION ON MID CAP AT PASSENGER DOOR CUTOUT WAS EVALUATED OUT LIMITS PER CRJ-700 SRM 51-10-06-001-001-A01 THEREFORE WAS REPLACED PER CRJ700 SRM 51-41-02-001-001-A01
Part: ANGLE — CRACKED (ZONE 300) · airframe 45,987 hrs · 35,555 cycles
CRACK ON LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER WERE REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01
Earlier reports · 1998–2025 · 146 reports
2025
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 45,567 hrs · 35,116 cycles
CENTER AISLE SECOND TO LAST EMERGENCY LIGHT INOPERATIVE. R & R LIGHT BULB IAW CRJ 700 AMM 33-51-09 OPS TEST GOOD PN ON/OFF:1317
2022
Part: SUPPORT ANGLE — CRACKED (AFT CRGO TRACK) · airframe 41,507 hrs · 31,073 cycles
AFT CARGO DOOR FORWARD TRACK LOWER SUPPORT ANGLE CLIP MISSING FABRICATED AND INSTALLED NEW AFT CARGO DOOR FORWARD TRACK LOWER SUPPORT ANGLE CLIP
Part: TORQUE LINK — CORRODED · airframe 41,507 hrs · 31,073 cycles
RIGHT MAIN LANDING GEAR TORQUE LINKS ( UPPER AND LOWER ) HAVE AREAS OF CORROSION AS WELL AS MISSING PROTECTIVE FINISH " REPLACED R/H UPPER MLG TORQUE LINK ASSEMBLY REF CRJ 700 AMM 32-11-37-400-801 CONFIG A01,"
Part: SKIN — WORN (RT WING TE FLAP) · airframe 41,507 hrs · 31,073 cycles
RH WING FLAP SKIN PANEL 684GB CHAFED. REPLACED PANEL 684GB WITH NEW PANEL.
Part: BAFFLE — WORN (THRUST REVERSER) · airframe 41,507 hrs · 31,073 cycles
R/H UPPER TRANSCOWL HAS CHAFED BAFFLE ON FWD COWL EDGE. NO MANUFACTURER DAMAGE LIMITATIONS FOR PART; REPLACE BAFFLE REMOVED DAMAGE BAFFLE AND INSTALLED 1 EA NEW BAFFLE REF CRJ700 SRM 51-42-06-001-001-A01
Part: BAFFLE — CRACKED (THRUST REVERSER) · airframe 41,507 hrs · 31,073 cycles
RH UPPER TRANSCOWL HAS CRACKED BAFFLE ON FWD COWL EDGE. REMOVED DAMAGED BAFFLE AND INSTALLED 1 EA NEW BAFFLE REF CRJ700 SRM 51-42-06-001-001-A01
Part: BAFFLE — CRACKED (THRUST REVERSER) · airframe 41,507 hrs · 31,073 cycles
RH UPPER TRANSCOWL BAFFLE CRACKED AT FWD END OF COWL. REPLACED CRACKED BAFFLE WITH SERVICEABLE PART PER CRJ700 SRM 51-42-06-001-001-A01
2019
Part: FRAME — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 319 BETWEEN STR 26L TO 25R AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI : 53-20-304). SUMMARY NRC S/N 00131: CORROSION LEVEL 2 ON FRAME FS319 BTW STR 25L TO 25R AT MAIN AVIONIC COMPARTMENT WAS REPAIRED PER EA N° CRJ753-08851 REV. "IR".
Part: FRAME — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 310 BETWEEN STR 24L TO 26R AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI : 53-20-304) SUMMARY NRC S/N 00129: CORROSION LEVEL 2 ON FRAME FS310 BTW STR 24L TO 24R AT MAIN AVIONIC COMPARTMENT WAS REPAIRED PER EA N° CRJ753-08803 REV. "IR".
Part: STRIKER — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON LOWER STRIKER IN STA. FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY: CORROSION LEVEL 2. DUE TO NOT DAMAGE ALLOWED ON LOWER STRIKER THIS WAS REPLACED PER SRM 53-21-23-101-002-A01 AND SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON STRINGER 23R / 24R IN STA. FS= 280 TO FS= 333 AT MAIN AVIONICS COMPARTMENT. (E/E)(TCI:53-20-304). CORROSION LEVEL 1: CORROSION ON STRINGER 23R IN STA. FS= 298 TO FS=315 AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER SRM 51-21-06-001-001-A01. REWORKED AREAS ON STRINGER 23R IN STA. FS= 280 TO FS= 333 AT MAIN AVIONICS COMPARTMENT WERE MEASURED AND FOUND WITH THE FOLLOWING MAX. DEPTH DIMENSION: OT=0.063", MRT=0.057", THEREFORE ARE WITHIN LIMITS PER SRM 53-21-03-101-002-A01 AND SRM 53-00-00-101-001-A01. CORROSION LEVEL 2: STRINGER 24RH IN STA. FS= 280 TO FS= 333 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01.
Part: FRAME — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
DUE EXCESSIVE DAMAGE CORROSION, OUT LIMITS DAMAGES ON FRAME FS=364 BTW STR 26L TO 25R AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI : 53-20-304) IN REFERENCE NRC 00132. CORROSION LEVEL 2: FRAME FS=364 BTW STR 26L TO 25R AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER SRM 53-21-23-201-008-A01
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT [ JUMPER/PROX-SENSOR/CONNECTOR-WIRING ANGLE ] IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) CORROSION LEVEL 2: FLOOR SUPPORT IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LOWER SILL, WAS REPLACED PER CRJ-700 SRM 51-41-02-001-001-A01 OPERATIONAL TEST OF THE PASSENGER DOOR WAS PERFORMED PER AMM 52-11-00-710-801 CONF. A02 TEST OK.
Part: CANISTER — CRACKED (LE SLAT) · airframe 36,495 hrs · 26,593 cycles
SUPPLEMENTAL INFORMATION (UPDATNG WING STATION) - INITIAL INSPECTION. CRACK ON SLAT TRACK CANISTER 1-3 AT RT WING MAIN FUEL TANK WS 148. (SM)(AD). SLAT TRACK CANISTER 1-3 AT RT WING MAIN FUEL TANK WS 148 WAS REPAIRED PER REO 670-57-42-577 REV. --. LEAK TEST WAS PERFORMED AND LEAK WAS NOT FOUND PER AMM 28-11-00-790-801-A01.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION : CORROSION ON INTERCOSTAL AND CHANNEL FS=1031 / FS=1051 STRG 27 AT REAR FUSELAGE INTERNAL STRUCTURE (FUS) ( TCI:53-30-310).(C2) INTERCOSTAL WAS CLEANED PER SRM 51-26-00-001-001-A01, AFTER CLEANING ON INTERCOSTAL RE-INSPECTION WAS PERFORMED PER AMM:05-21-00-210-801 AND NOT FOUND CORROSION. CHANNEL BTW FS=1031 / FS=1051 STR 27 WAS REPLACED PER SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
CORROSION ON STRINGER 24L FROM FS 280 TO 333 AT MAIN AVIONICS COMPARTMENT.(SM)(E/E). CORROSION LEVEL 2: STRINGER 24L FROM FS. 280 TO FS. 333 WAS REPLACED PER SRM 51-42-06-001-001-A01
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON SEAT TRACK RAILS BTW FS581 / FS677+3 AND LBL9.00/ RBL9.00 SIDE ABOVE FLOOR (TCI: 53-20-245) CORROSION LEVEL 2: SEAT TRACK RAILS BTW FS581 / FS677+3 AND LBL9.00/ RBL9.00 WERE REPLACED PER AMM 53-00-49-400-801 (CONFIG A03)
Part: FRAME — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 295 BETWEEN STR 26L TO 23R AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI : 53-20-304) SUMMARY: FRAME WAS REPAIR PER EA NO CRJ953-08849 REV.IR.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON INTERCOSTAL 6 LBL / 6RBL 2LBL AND 2RBL BTW FS 364 TO 349. AT E/E COMPARTMENT.(TCI:53-20-313). CORROSION LEVEL 2: DUE TO SEVERE DAMAGE INTERCOSTAL 6 LBL / 6RBL 2LBL AND 2RBL BTW FS 364 TO 349. AT E/E COMPARTMENT WERE REPLACED PER SRM 51-42-20-001-001-A01 PAR. 6.E AND SRM 51-42-06-001-A01 PAR 6A.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON STRINGER 27 IN STA. FS= 280 TO FS= 295 ALSO 25L BTW FS=295 TO FS=310 AT MAIN AVIONICS COMPARTMENT. (E/E)(TCI:53-20-305). CORROSION LEVEL 2. STRINGER 27 IN STA. FS= 280 TO FS= 295 AND 25L FS=280 TO FS=333 WERE REPLACED PER SRM 51-42-06-001-001-A01. P/NS SH670-31642-1 AND SH670-31212-1.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
CORROSION ON STRINGER 25R FROM FS 333 TO 364 AT MAIN AVIONICS COMPARTMENT.(SM)(E/E). CORROSION LEVEL 2: STRINGER 25R FROM FS 333 TO 364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON STRINGER 26R IN STA. FS= 280 TO FS= 295 ALSO 25RH BTW FS=280 TO FS=310 AT MAIN AVIONICS COMPARTMENT. (E/E) (TCI:53-20-304). STRINGER 26R IN STA. FS= 280 TO FS= 333 AND 25R BTW FS=280 TO FS=333 WAS REPLACED PER SRM 51-42-06-001-001-A01. P/NS SH670-31634-2 AND SH670-31212-2.
Part: FRAME — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION:CORROSION ON FRAME AT FS.517, FS.533, FS.549 BTW STR 25L TO 25R. AT THE FORWARD BAGGAGE COMPARMENT. (CAR) (SM) CORROSION ON SECTION FRAME FS 533 AND FS 549 WAS REMOVED PER FRAME FS=533 WAS MEASURED WITH THE FOLLOWING CONDITIONS: ORIGINAL THICKNESS IS= 0.100" AND REMAINING THICKNESS IS= 0.096". THEREFORE ARE WITHIN LIMITS PER SRM 53-31-23-101-001-A01. FRAME FS=549 WAS MEASURED WITH THE FOLLOWING CONDITIONS: ORIGINAL THICKNESS IS= 0.063" AND REMAINING THICKNESS IS= 0.060". THEREFORE ARE WITHIN LIMITS PER SRM 53-31-06-101-003-A01. FRAME FS 517 WAS REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STR 26L TO 26R AT MAIN AVIONICS COMPARTMENT. (E/E)(TCI:53-20-304). INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STR 26L TO 26R WAS REPLACED PER SRM 51-42-06-001-001-A01.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION. CORROSION ON STRINGER SPLICE 25R IN STA. FS= 329 TO FS= 339 AT MAIN AVIONICS COMPARTMENT.(TCI:53-20-305) (E/E). STRINGER SPLICE 25R IN STA. FS= 329 TO FS= 339 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT ANGLE IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) CORROSION LEVEL 2. DUE TO NOT ALLOWED ON PROTECTION PLATE SUPPORT ANGLE THIS WAS REPLACED PER SRM 53-21-23-101-002-A01 AND SRM 51-42-21-001-001-A01.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION : CORROSION ON FLOORBEAM 27LBL BTW FS=1006 TO FS=1041 AT REAR FUSELAGE INTERNAL STRUCTURE (FUS) ( TCI:53-30-310). FLOORBEAM WAS REPAIRED PER SRM 53-00-42-201-001-A01.
Part: FITTING — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION. CORROSION ON CLIPS FS 310 AND 349 STRG 20R AT MAIN AVIONICS COMPARTMENT. (E/E)(SM)(TCI :53-20-304). CORROSION ON CLIPS FS 310 AND 349 STR 20R AT MAIN AVIONICS COMPARTMENT. CLIP ON FS 310 WAS CLEANED PER. SRM. 51-26-00-001-001-A01. AND CLIP ON FS 349 WAS REPLACED PER. SRM. 51-42-21-001-001-A01.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON SUPPORT MOUNTING ANGLE IN STA. FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUPPORT MOUNTING ANGLE BTW FS319/349 AND 41RBL AT GALLEY SERVICE DOOR LOWER SILL, WAS REPLACED FOR A NEW ONE (P/N: SH670-31996-3) PER SRM 51-42-06-001-001-A01.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY OF NRC S/N 00296: CORROSION LEVEL 2. DUE TO NOT DAMAGE ALLOWED ON PROTECTION PLATE SUPPORT THIS WAS REPLACED PER SRM 53-21-23-101-002-A01 AND SRM 51-42-21-001-001-A01.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) CORROSION LEVEL 2. DUE TO NOT ALLOWED ON PROTECTION PLATE SUPPORT ANGLE THIS WAS REPLACED PER SRM 53-21-23-101-002-A01 AND SRM 51-42-21-001-001-A01
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,495 hrs · 26,593 cycles
AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT ANGLE IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY OF NRC 00293: CORROSION LEVEL 2. DUE TO NOT ALLOWED ON PROTECTION PLATE SUPPORT ANGLE THIS WAS REPLACED PER SRM 53-21-23-101-002-A01 AND SRM 51-42-21-001-001-A01.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT ANGLE IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY OF NRC 00292: CORROSION LEVEL 2. DUE TO NOT ALLOWED ON PROTECTION PLATE SUPPORT ANGLE THIS WAS REPLACED PER SRM 53-21-23-101-002-A01 AND SRM 51-42-21-001-001-A01.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY OF NRC 00295: CORROSION LEVEL 2. DUE TO NOT DAMAGE ALLOWED ON PROTECTION PLATE SUPPORT THIS WAS REPLACED PER SRM 53-21-23-101-002-A01 AND SRM 51-42-21-001-001-A01.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX)SUMMARY OF NRC 00297: CORROSION LEVEL 2. DUE TO NOT DAMAGE ALLOWED ON PROTECTION PLATE SUPPORT THIS WAS REPLACED PER SRM 53-21-23-101-002-A01 AND SRM 51-42-21-001-001-A01.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
SUPPLEMENTAL INFORMATION (CORRECTING BUTT LINE LOCATION) - (AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) SUMMARY OF NRC 00298: CORROSION LEVEL 2. DUE TO NOT DAMAGE ALLOWED ON PROTECTION PLATE SUPPORT THIS WAS REPLACED PER SRM 53-21-23-101-002-A01 AND SRM 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON SEAT TRACK RAILS BTW FS677+3 / FS830.40+3 AND LBL9.00 SIDE ABOVE FLOOR (TCI: 53-20-245) SEAT TRACK RAILS BTW FS677+3 / FS830.40+3 AND LBL9.00 WAS REPLACED PER AMM 53-00-49-400-801 (CONFIG A03)
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
CORROSION ON SIDE SEAT RAIL STRUCTURE (LT/R) FROM FS953+8 TO FS985+2 AT PAX CABIN (TCI: 53-20-356) NEW SIDE SEAT RAIL STRUCTURE (LT/RT) FROM FS953+8 TO FS985+2 WERE REPLACED PER AMM 53-00-49-400-801 (CONFIG. A17). LEVEL CORROSION 2.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL STRUCTURE (LH/RH) FROM FS379 TO FS485, FS485 TO FS 565+8, FS565 TO FS677 AND FS677 TO FS 708+3 AT PAX CABIN (TCI: 53-20-245) SIDE SEAT RAIL STRUCTURE (LH/RH) FROM FS379 TO FS485, FS485 TO FS 565+8, FS565 TO FS677 AND FS677 TO FS 708+3 AT PAX CABIN WERE REPLACED PER AMM 53-00-49-400-801 (CONFIG A03) LEVEL CORROSION 2.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON SIDE SEAT RAIL STRUCTURE (LH/RH) FROM FS708+4 TO FS761.85, FS785.15 TO FS 847+6, FS847+6 TO FS863+5 AND FS863+5 TO FS 953+8 AT PAX CABIN (TCI: 53-20-318) SIDE SEAT RAIL STRUCTURE (LH/RH) FROM FS708+4 TO FS761.85, FS785.15 TO FS 847+6, FS847+6 TO FS863+5 AND FS863+5 TO FS 953+8 AT PAX CABIN WERE REPLACED PER AMM 53-00-49-400-801 (CONFIG A03) LEVEL CORROSION 2.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON SEAT TRACK RAILS BTW FS485 / FS581 AND RBL9.00 / LBL9.00 SIDE ABOVE FLOOR (TCI: 53-20-245) SEAT TRACK RAILS BTW FS485 / FS581 AND RBL9.00 / LBL9.00 WERE REPLACED PER AMM 53-00-49-400-801 (CONFIG A03)
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON SEAT TRACK RAILS BTW FS349 / FS485 AND RBL9.00 SIDE ABOVE FLOOR (TCI: 53-20-243) SEAT TRACK RAILS BTW FS349 / FS485 AND RBL9.00 WAS REPLACED PER AMM 53-00-49-400-801 (CONFIG A03)
Part: DOUBLER — CHAFED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CHAFING ON PREVIOUS REPAIR DOUBLER, TRIPLER AND TAPER SHIMS IN FS=968 TO FS=985 AT FUSELAGE SKIN.(FUS)(SM)(TCI 53-20-252). REPAIR DOUBLER, TRIPLER AND TAPER SHIMS IN FS=968 TO FS=985 AT FUSELAGE SKIN WERE REPLACED PER REO 670-53-00-290 REV. E AND SRM 51-25-01-001-001-A01.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,495 hrs · 26,593 cycles
INITIAL INSPECTION: CORROSION ON STRINGER 21RH IN STA. FS= 280 TO FS= 364 AT MAIN AVIONICS COMPARTMENT. (E/E)(TCI:53-20-304) STRINGER 21R IN SECTION STA. FS= 280 TO FS=333 WAS CLEANED PER SRM. 51-26-00-001-001-A01 AND DAMAGE NO FOUND, STRINGER 21R AND SPLICE IN SECTION STA. FS= 333 TO FS=364 WAS REPLACED FOR A NEW ONE PER SRM 51-42-06-001-001-A01 AT MAIN AVIONICS COMPARTMENT. (LEVEL CORROSION 2)
2018
Part: OXYGEN BOTTLE — LEAKING (COCKPIT) · airframe 35,194 hrs · 25,688 cycles
CREW O2 SYSTEM LOSING 10PSI PRESURE EVERY 5-10 MINUTES. REMOVE AND REPLACED CREW O2 BOTTLE IAW AMM 35-11-03.
Part: OXYGEN MASK — LEAKING (FIRST OFFICER'S) · airframe 35,091 hrs · 25,613 cycles
FIRST OFFICER`S OXYGEN MASK FOUND TO BE LEAKING AFTER SERVICING. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS TESTED GOOD, NO LEAKS DETECTED, NO DEFECTS DETECTED.
Part: CYLINDER — LOW PRESSURE (PORTABLE OXYGEN) · airframe 35,014 hrs · 25,558 cycles
PORTABLE OXYGEN CYLINDER PRESSURE 1500, REMOVED & REPLACED THE CYLINDER IAW AMM 35-31-01-00-801.
2017
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 32,779 hrs · 23,892 cycles
FS 202.75 FWD SIDE OF BULKHEAD AT RBL 30 HAS INDICATION NOTED AT TOP OF I BEAM INTERSECTION .150" LONG. FAILED NDT INSPECTION. REPAIRED RBL 30 I BEAM IAW SRM 53-11-10-201-005-A01.
Part: FRAME — CRACKED (FUSELAGE) · airframe 32,779 hrs · 23,892 cycles
RT FS 235 FRAME HAS ONE INDICATION NOTED NEAR I/B RADIUS AT STR 13A .300" LONG FAILED NDT. REMOVED UNSERVICEABLE RT FS 235 FRAME P/N CC670-34133-4 AND INSTALLED A SERVICEABLE RT FS 235 FRAME P/N CC670-34133-10 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND SERVICE BULLETIN 670-53-045.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,779 hrs · 23,892 cycles
RT SEAT TRACK AT RBL 9 FS687 TO FS840 IS CORRODED. COMPLIED WITH EC/TC REO 670-53-00-343 REV K AND REO 670-53-00-343 REV K.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,779 hrs · 23,892 cycles
LT SEAT TRACK AT LBL 9 FS687 TO FS840 IS CORRODED. COMPLIED WITH EC/TC REO 670-53-00-343 REV K AND REO 670-53-00-343 REV K.
2016
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 31,746 hrs · 23,136 cycles
DURING SCHEDULED MAINTENANCE, THE OVERHEAD ISLE EMERGENCY LIGHT AT ROW 9 WAS FOUND INOPERATIVE. MX SECURED THE CONNECTOR J358 AND PERFORMED OPS CHECK WITH SATISFACTORY RESULTS. ACFT WAS APPROVED FOR RETURN TO SERVICE.
Part: ENGINE — FAILED (RIGHT) · airframe 31,055 hrs · 22,576 cycles
AFTER TAKE OFF, ACFT BEGAN TO SHAKE, RT ENGINE VIBRATION CAUTION UP TO 6.8. AND ITT WENT RED. SHUT RT ENGINE DOWN AND RETURNED TO DEPARTURE. REMOVED AND REPLACED THE RT ENGINE IAW AMM 71-00-00. INSTALLED RT ENGINE IDG IAW AMM 24-11-01.
2015
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,468 hrs · 21,325 cycles
MAIN ENTRANCE LOWER EXIT SIGN HAD TWO LIGHT BULBS BURNED OUT. R & R BURNED OUT BULBS AS REQURIED. OPS CHECK GOOD IAW AMM 33-51-00.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,468 hrs · 21,325 cycles
GALLEY AFT LOWER EXIT SIGN HAVE 1 BULB BURNED OUT. R & R BURNED OUT BULBS AS REQURIED. OPS CHECK GOOD IAW AMM 33-51-00.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,468 hrs · 21,325 cycles
GALLEY FORWARD LOWER EXIT SIGNS HAD ONE BULB BURNED. R & R BURNED BULBS AS REQUIRED. OPS CHECK GOOD IAW AMM 33-51-00.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,468 hrs · 21,325 cycles
12 CD LOWER EXIT SIGN ONE BULB BURNED OUT. R & R BURNED OUT BULBS AS REQURIED. OPS CHECK GOOD IAW AMM 33-51-00.
Part: WARNING LIGHT — ILLUMINATED · airframe 29,440 hrs · 21,305 cycles
ELECTRICAL ODOR NOTED AFTER REV D, A STBY PITOT HEAT CAUTION MESSAGE AND A TAT PROBE CAUTION. ENROUTE, ACFT DIVERTED DUE TO MAINTENANCE. EMERGENCY DECLARED AS A PRECAUTION. R & R ABO ADSHC IAW AMM 30-31-15, IPC 30-31-15, PG 0, FIG 1, ITEM 5. OPS TEST GOOD, ACFT OK FOR SERVICE.
Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 28,966 hrs · 20,913 cycles
PAX DOOR EXIT SIGN LENS DARKENED WHEN RECEIVED. REMOVED AND INSTALLED NEW PAX DOOR EXIT SIGN LENS IAW AMM 33-51-05-000-801-A01 AND 33-51-05-400-801-A01.
Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 28,966 hrs · 20,913 cycles
SERVICE DOOR EMERGENCY LIGHT LENS DAMAGED. REMOVED SERVICE DOOR EMERGENCY LIGHT LENS IAW AMM 33-51-05-000-801A-01. INSTALLED SERVICEBALE EMERGENCY LIGHT LENS IAW AMM 33-51-05-400-801-A01.
Part: INTERCOSTAL — CORRODED (BS 265-280) · airframe 28,966 hrs · 20,913 cycles
DISCOVERED INTERCOSTAL AT STR 27L BETWEN FS 265 TO FS 280 IS CORRODED. EVALUATED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-A01. REMOVED INTERCOSTAL AT LT SIDE OF STR 27 BETWEEN FS 265-280 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED HOLES IN NEW INTERCOASTAL IAW SRM 51-40-11-001-001-A01. INSTALLED LT INTERCOSTAL AT STRINGER 27, FS 265-280 & INSTALLED STANDOFF ATTACHING ANGLES AT FS 280 IAW SRM 51-42-06-001-001-A01 SRM 51-42-21-001-001-A01 & DWG CC670-32179, REV C.
Part: SKIN — CORRODED (FUSELAGE) · airframe 28,966 hrs · 20,913 cycles
FUSELAGE SKIN CORRODED UNDERNEATH THE BOTTOM ADF ANTENNA. NO DAMAGE ALLOWED ON SKIN UNDERNEATH ADR ANTENNA IAW SRM 53-31-01-101-003-A01. COMPLIED WITH EA 32-2015-281, REV A. COMPLIED WITH EA 32-2015-281.
Part: DOUBLER — CORRODED (BS 295-310) · airframe 28,945 hrs · 20,894 cycles
TCAS DOUBLER CORRODED AT FS 295-310 BETWEEN STRINGERS 26L AND 26R. REMOVED TCAS DOUBLER IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW TCAS DOUBLER IAW SRM 51-40-11-001-001-A01. INSTALLED NEW TCAS DOUBLER IAW SRM 51-42-06-001-001-A01 AND FINISHED RIVETS IAW SRM 51-21-16-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 28,945 hrs · 20,894 cycles
RBL 9 SEAT TRACK CORROSION BS 485-581. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801, CONFIG A03. AND INSTALLED A NEW SEAL TRACK IAW AMM 53-00-49-400-801, CONFIG A03.
Part: SHEAR TIE — CORRODED (BS 565)
FS 565 FRAME ATTACH ANGLE BETWEEN STRINGERSS 18 - 19L HAS CORROSION. COMPLIED WITH REO 670-53-31-345 AND ECTC REO 670-53-31-345.
Part: FRAME — CORRODED (BS 549) · airframe 28,945 hrs · 20,894 cycles
BS 549, FRAME HAS CORROSION BETWEEN STRINGERS 18 AND 19L. REMOVED THE CORROSION IAW SRM 51-21-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 28,945 hrs · 20,894 cycles
LBL 9 SEAT TRACK HAS CORROSION ON BS 581- 677, LBL 9, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-13. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 28,945 hrs · 20,894 cycles
LBL 9 SEAT TRACK HAS CORROSION ON BS 485-581 SEGMENT. CORRODED BEYOND LIMITS. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.
Part: FRAME — CORRODED (BS 565) · airframe 28,966 hrs · 20,913 cycles
FS 565, FRAME HAS CORROSION BETWEEN STRINGERS 18 - 19L. EVALUATED FRAME AND FOUND IT TO BE EXTREMELY EXFOILATED, NO ALLOWABLE DAMAGE IS PERMITTED IN THIS AREA. RECEIVED AND COMPLIED WITH REO 670-53-31-345, REV-- (P1), DATED 2015-07-03. RECEIVED AND COMPLIED WITH FINAL REO 670-53-31-345 AND REO 670-53-31-345.
Part: ANGLE — CORRODED (BS 549) · airframe 28,945 hrs · 20,894 cycles
FS 549 FRAME ANGLE CORRODED BETWEEN STR 18-19L . REMOVED CORROSION FROM ANGLE IAW SRM 51-21-06-001-001-A01. BLENDED AREA WAS FOUND TO BE WITHIN LIMITS ON SRM 53-31-23-101-001-A01. UPON FURTHER EVALUATION FOUND ADDITIONAL CORROSION ON ANGLE. REMOVED FASTENERS TO FACILITATE CORROSION REMOVAL. REMOVED CORROSION, REF SRM 51-42-06-001-001-A01, 51-42-22-001-001-A01 AND 51-21-06-001-001-A01. MEASURED MECHANICALLY AND FOUND MINIMUM MATERIAL THICKNESS TO BE .044" IS OUT OF LIMITS IAW 53-00-07. COMPLIED WITH EA 32-2015-277, REV DATED 7/8/15, PERMANENT REPAIR. COMPLIED WITH EA 32-2015-277.
Part: DOOR FRAME — CORRODED · airframe 28,945 hrs · 20,894 cycles
LEFT DOOR POST CORRODED AT BS 280 CROSSBEAM. REMOVED CORROSION ON LT DOOR POST AT 280 CROSSBEAM AREA IAW SRM 51-21-06-001-001-A01. COMPLIED WITH STS EA 25-2015-195. COMPLIED WITH EA 25-2015-197.
Part: DOOR FRAME — CORRODED (BS 280) · airframe 28,945 hrs · 20,894 cycles
RIGHT DOOR POST CORRODED AT BS 280 CROSSBEAM. REMOVED CORROSION ON RT DOOR POST AT 280 CROSSBEAM AREA IAW SRM 51-21-06-001-001-A01. COMPLIED WITH STS EA 25-2015-195. COMPLIED WITH EA 25-2015-195.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 28,945 hrs · 20,894 cycles
BS 280 BULKHEAD WEB CORRODED. CORROSION DAMGE FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-006. COMPLIED WITH ECTC REO 670-53-11-59401 AND GREO 670-53-11-594, REV A.
Part: PLATE — CORRODED (RT OVERWING) · airframe 28,945 hrs · 20,894 cycles
RT OVERWING EMERGENCY EXIT STEP PLATE CORRODED. REMOVED RT O/W EXIT STEP PLATE BY REMOVING 8 SCREWS AND LIFTING PLATE. INSTALLED RT EMERGENCY EXIT STEP RATE BY INSTALLING 8 SCREWS IAW SRM 51-41-02-001-001-A01. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREAS ARE OUT OF ALLOWABLE LIMITS IAW SRM 53-41-23-101-001-A01. COMPLIED WITH AND VERIFIED ALL STEPS OF EA 32-2015-276 AND ECTC EA 32-2015-276 HAVE BEEN COMPLETED.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 28,945 hrs · 20,894 cycles
BS 280 BULKHEAD WEB CORRODED. CORROSION DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594, REV A DATED 4/27/2011.
Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 28,945 hrs · 20,894 cycles
SIDE WALL SEAT TRACK HAS CORROSION LT SIDE FS 677-708. SIDE SEAT TRACK LT IS CORRODED BEYOND LIMITS IAW SRM 53-31-49. REMOVED SIDE SEAT TRACK AT FS 677-708 IAW AMM 53-00-49-000-801-A03. REPLACED SIDE SEAT TRACK AT FS 677-708 WITH SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03. SEAT TRACK FABRICATION COMPLIED WITH IAW ECTC REO 670-53-00-343, REV L AND GREO 670-53-00-343, REV L. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV L.
Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 28,945 hrs · 20,894 cycles
SIDE WALL SEAT TRACK HAS CORROSION RT SIDE BS 677-708. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 708-761) · airframe 28,945 hrs · 20,894 cycles
SIDE WALL SEAT TRACK HAS CORROSION RT SIDE BS 708-761. REMOVED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED A NEW SEAT -761 IAW AMM 53-00-49-400-801-A03.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,945 hrs · 20,894 cycles
AVIONICS FLOORBEAM ANGLE CORRODED AT BS 280.00. REMOVED THE ANGLE AND REPLACED WITH NEW IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 & 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 374-485) · airframe 28,945 hrs · 20,894 cycles
SEAT TRACK CORRODED LBL9, BS 374-485. REMOVED SEAT TRACK BS 374-485, LBL9 IAW AMM 53-00-49-000-801, CONFIG A03. INSTALLED NEW SEAL TRACK STA 374-485, LBL9 IAW AMM 53-00-49-400-801, CONFIG A03.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 28,945 hrs · 20,894 cycles
BS 280 CROSSBEAM HAS CORROSION. CROSSBEAM R & R IAW SB670BA-53-041.
Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 28,945 hrs · 20,894 cycles
AFT COCKPIT FLOOR SUPPORT CORRODED. AFT COCKPIT FLOOR SUPPORT R & R IAW SB670BA-53-041.
Part: FAIRING — CRACKED (THRUST REVERSER)
PANEL 433BT HINGELINE FAIRING CRACKED. COMPLIED WITH REO 670-78-33-998. COMPLIED WITH ECTC REO 670-78-33-998 AND REO 670-78-33-998, REV NC DATED 08/26/2014.
Part: SEAL — CORRODED (E/E BAY DOOR) · airframe 28,966 hrs · 20,913 cycles
MAIN AVIONICS DOOR SEAL CONTACT SURFACE IS CORRODED. REMOVED CORROSION FROM MAIN ACCESS DOOR SEAL CONTACT SURFACE IAW AMM. NO ALLOWABLE LIMITS PERMITTED IN AREA IAW SRM 53-00-01-101-001-A01. COMPLIED WITH GREO 670-53-21-0241, REV B ONCE ECTC RECEIVED. BLENDED IS WITHIN ALLOWABLE LIMITS IAW REO 670-53-21-242. COMPLIED WITH ECTC ERO 670-53-21-242 AND MODSUM ECTC IS67053210097. COMPLIED WITH ECTC REO 670-53-21-242 AND REO 670-53-21-242, REV B DATED 07/29/201. COMPLIED WITH MODSUM IS6705-3210097, REV A.
Part: RUB STRIP — DEBONDED (RT AILERON) · airframe 28,945 hrs · 20,894 cycles
RT AILERON RUB STRIP DISBONDED. REPAIRED IAW EC/TC REO 670-57-61-006, REV E.
2013
Part: LIGHT — INOPERATIVE (SIGN) · airframe 24,409 hrs · 17,519 cycles
EMERGENCY SIGN BACK LIGHTING STOPPED WORKING. PERFORMED OPS CK OF EMERGENCY LIGHTS IAW AMM 33-51-00. FAULT NO LONGER EXSISTS. ACFT RETURNED TO SERVICE.
Part: ANGLE — CORRODED (PAX DOORWAY) · airframe 24,009 hrs · 17,231 cycles
PAX DOOR MID CAP ANGLE THAT PROXIMITY SWITCH MOUNTS IN IS CORRODED AT SCREW HOLES. REMOVED CORRODED DOOR MID CAP ANGLE IAW SRM 51-41-02-001-001-A01. INSTALLED REPLACEMENT MID CAP ANGLE THAT THE PROX SWITCH MOUNTS ON THE PAX DOOR IAW SRM 51-41-02-001-A01. LOCATED, DRILLED AND TRANSFERED ALL ATTACHED CLIPS AND NUTPLATES TO THE REPLACMENT MID CAP ANGLE IAW SRMS 51-42-06-001-001-A01, 51-45-00-001-001-A01, AND 51-40-11-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 24,009 hrs · 17,231 cycles
UPON REMOVAL OF SERVICE DOOR SILL PLATE ANGLE FOUND SERVICE DOOR FLOOR SUPPORT ANGLE CORRODED. R & R FLOOR SUPPORT ANGLE AT SERVICE DOOR IAW SRM 51-42-06-001-001 & 51-42-13-001-001.
Part: ANGLE — CORRODED (SERVICE DOORWAY) · airframe 24,009 hrs · 17,231 cycles
SERVICE DOOR SILL PLATE ANGLE IS CORRODED. LOCATED & DRILLED NEW SERVICEABLE MOUNTING ANGLE IAW SRM 51-40-06-001-001-A01. REMOVED & INSTALLED NEW SERVICEABLE MOUNTING ANGLE IAW SRM 51-42-06-001-001 & 51-42-13-001-001.
Part: POST — CORRODED (BS 280 BULKHEAD) · airframe 24,009 hrs · 17,231 cycles
FS 280.00 BULKHEAD POST HAS CORROSION RBL9. REPAIRED IAW SRM 51-21-06-001-001-A01.
Part: POST — CORRODED (BS 280 BULKHEAD) · airframe 24,009 hrs · 17,231 cycles
FS 280 BULKHEAD POST HAS CORROSION LBL9. REPAIRED IAW SRM 51-21-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 581) · airframe 24,009 hrs · 17,231 cycles
LT SIDEWALL SEAT TRACK CORRODED AT FS 581. R & R WITH NEW SERVICEABLE SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 549) · airframe 24,009 hrs · 17,231 cycles
RT CENTER FLOOR SEAT TRACK CORRODED AT FS 549. R & R WITH SERVICEABLE SEAT TRACK ON RBL 9 FROM FS 485 TO 581 IAW AMM 53-00-49-000-801(CONFIG 3) AND 53-00-49-400-801(CONFIG A03).
Part: SEAT TRACK — CORRODED (BS 581-613) · airframe 24,009 hrs · 17,231 cycles
RT SIDEWALL SEAT TRACK CORRODED AT FS 581 APROX AND 613. R & R WITH SERVICEABLE SIDE SEAT TRACK AT FS 581 AND 613 IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 736) · airframe 24,009 hrs · 17,231 cycles
RT SIDEWALL SEAT TRACK CORRODED AT FS 736. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801 (CONFIG A03) AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801 (CONFIG A03).
Part: SEAT TRACK — CORRODED (BS 670) · airframe 24,009 hrs · 17,231 cycles
RT CENTER FLOOR SEAT TRACK CORRODED OF FS 670. R & R WITH SERVICEABLE SEAT TRACK ON RBL 9 FROM FS 571 TO 675 IAW AMM 53-00-49-000-801(CONFIG A03) AND 53-00-49-400-801(CNFIG A03).
Part: SEAT TRACK — CORRODED (BS 706) · airframe 24,009 hrs · 17,231 cycles
LT SIDEWALL SEAT TRACK CORRODED AT FS 706. R & R CORRODED SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
Part: FLOORBEAM — CORRODED (BS 1051) · airframe 24,009 hrs · 17,231 cycles
FLOORBEAM AT FS 1051.3 RT RBL 45 WAS FOUND TO BE CORRODED. REPAIRED IAW 670-53-61-953. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (BS 629-677) · airframe 24,009 hrs · 17,231 cycles
LT CENTER FLOOR SEAT TRACK IS CORRODED AT FS 677 AND 629 MULTIPLE ON ONETRACK. R & R WITH SERVICEABLE SEAT TRACK AT LBL 9 FROM FS 571 TO 675 IAW AMM 53-00-49-000-801 (CONFIG A03) AND 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 813) · airframe 24,009 hrs · 17,231 cycles
RT SIDEWALL SEAT TRACK CORRODED AT FS813 APPROX. R & R RT SIDEWALL SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 459) · airframe 24,009 hrs · 17,231 cycles
RT CENTER FLOOR SEAT TRACK CORRODED AT FS 459. R & R WITH SERVICEABLE SEAT TRACK FS 350 TO FS 485 IAW AMM 53-00-49-000-801 (CONFIG A03), 53-00-49-400-801(CONFIG A03).
Part: SEAT TRACK — CORRODED (BS 708) · airframe 24,009 hrs · 17,231 cycles
RT SIDEWALL SEAT TRACK CORRODED AT FS 708. R & R WITH SERVICEABLE SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (S 736) · airframe 24,009 hrs · 17,231 cycles
LEFT SIDEWALL SEAT TRACK CORRODED AT FS 736. R & R WITH NEW SEAT TRACK LT SIDEWALL FROM FS 713 TO 761 IAW AMM 53-00-49-000-801 (CONFIG A03) AND 53-00-49-801. (CONFIG A03).
Part: SEAT TRACK — CORRODED (BS 785-797) · airframe 24,009 hrs · 17,231 cycles
LT SIDEWALL SEAT TRACK CORRODED AT FS 785 AND AT 797 MULTIPLE ON ONE TRACK. REMOVED LT SIDEWALL SEAT TRACK FROM FS 785 TO 861 IAW AMM 53-00-49-000-801-A03. INSTALLED SERVICEABLE LT SIDEWALL SEAT TRACK IAW AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (BS 540) · airframe 24,009 hrs · 17,231 cycles
LT CENTER FLOOR SEAT TRACK CORRODED AT FS 540 APPROX. R & R WITH NEW SEAT TRACK ON LBL9 FROM FS 485 TO 581 IAW AMM 53-00-49-000-801 (CONFIG A03) AND 53-00-49-400-801 (CONFIG A03).
Part: FLOOR SUPPORT — CORRODED (BS 285) · airframe 24,009 hrs · 17,231 cycles
RT FUSELAGE FLOOR SUPPORT IS CORRODED AT FS 285 APPROX. BLENDED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01. REPAIRED IAW REO 670-53-21-139.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,000 hrs · 17,227 cycles
FS 280 FLOORBEAM HAS CORROSION LBL8 APROX. R & R BS 280 LT FLOORBEAM IAW SRMS 51-42-06-001-001-A01 & 51-42-13-001-001-A01.
Part: BULKHEAD — CORRODED (BS 280) · airframe 24,000 hrs · 17,227 cycles
FS 280, RBL9 HAS CORROSION ON BULKHEAD POST AND WEB. REPAIRED IAW REO 670-53-11-594.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,009 hrs · 17,231 cycles
RT FS 280 FLOORBEAM CORRODED AT RBL 8. REMOVED FLOORBEAM IAW SRM 51-42-01-001-001-A01. INSTALLED FLOORBEAM IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. MAJOR REPAIR.
Part: ATTACH ANGLE — CORRODED (BS 280) · airframe 24,000 hrs · 17,227 cycles
ATTACH ANGLE FOR FLIGHT COMPARTMENT FLOOR PANEL 221ALF IS CORRODED AT FS280. RECEIVED NEW SERVICEABLE PART PN CL670-33292-13S, LOCATED AND DRILLED TO MATCH ACFT IAW SRM 51-40-11-001-001-A01. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED FLOOR SUPPORT ANGLE FOR FLOOR PANEL 221ALF AT FS 280 IAW SRM 51-42-06-001-001-A01.
Part: BULKHEAD — CORRODED (BS 280) · airframe 24,000 hrs · 17,227 cycles
FS 280, LBL9 HAS CORROSION ON BULKHEAD POST AND WEB. REPAIRED IAW REO 670-53-11-594.
Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 24,000 hrs · 17,227 cycles
AFT CARGO FLOOR SUPPORT HAS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REPAIRED IAW EO CL600-2C10-53-I00245.
Part: BRACKET — CORRODED (BS 533) · airframe 24,000 hrs · 17,227 cycles
CORROSION ON TOP OF PLATE ATTACHED TO FS 533 FRAME AND STR 26L. REMOVED BRACKET IAW SRM 51-42-21-001-001 AND 51-42-06-001-001 BY REMOVING RIVETS AND HILITES. INSTALLED BRACKET, PN SH670-33389-1 AT F/S533 STR 26L IAW SRM 51-42-21-001-001-A01 AND 51-42-13-001-001-A01.
Part: FRAME — CORRODED (BS 533) · airframe 24,000 hrs · 17,227 cycles
MINOR CORROSION ON TOP OF FS 533, FRAME AND STR 24L. LOCATED AND DRILLED THE REPLACEMENT STRAP IAW SRM 51-40-11-001-001-A01. INSTALLED THE REPLACEMENT STRAP IAW SRM 51-44-16-001-001-A01 AND DWG SH670-33793. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 24,000 hrs · 17,227 cycles
AFT CARGO FLOOR SUPPORT HAS CORRODED. REPAIRED IAW REO 670-53-61-954.
Part: FLOOR SUPPORT — CORRODED (BS 1000-1047) · airframe 24,000 hrs · 17,227 cycles
AFT CARGO FLOOR SUPPORT HAS CORROSION FROM FS 1000-1047 AT LBL 45. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REPAIRED IAW REO 670-53-61-956.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 24,000 hrs · 17,227 cycles
ANTENNA DOUBLER HAS CORROSION S27 BETWEEN BS 295 & 310. REMOVED CORRODED ANTENNA DOUBLER. INSTALLED NEW ANTENNA DOUBLER.
Part: STRAP — CORRODED (BS 280) · airframe 24,000 hrs · 17,227 cycles
FS 280 STRAP HAS CORROSION FROM S24 - 27R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.
Part: FRAME — CORRODED (BS 310) · airframe 24,000 hrs · 17,227 cycles
FRAME BS 310, CORRODED BETWEEN 26LT - 26RT. REPAIRED IAW REO 670-53-21-799.
Part: STRINGER — CORRODED (BS 364) · airframe 24,000 hrs · 17,227 cycles
STRINGER 27R CORRODED AT FS 364. REMOVED LATCH PIN INTERCOSTAL ZT RT SIDE FS 364 STR27 IAW SRM 51-42-21/06-001-001-A01. INSTALLED NEW LATCH PIN INTERCOSTAL AT FS 364, STR RT 27 IAW SRM 51-42-21/06-001-001-A01.
Part: FRAME — CORRODED (BS 333) · airframe 24,000 hrs · 17,227 cycles
FRAME BS 333 CORRODED BETWEEN S26 - 27L. REPAIRED FRAME IAW REO 670-53-21-799.
Part: STRINGER — CORRODED (BS 364) · airframe 24,000 hrs · 17,227 cycles
STRINGER 27LT CORRODED AT FS 364. REMOVED LATCH PIN INTERCOSTAL AT LT SIDE FS 364, STR 27L IAW SRM 51-42-21/06-001-001-A01. INSTALLED NEW LATCH PIN INTERCOSTAL AT FS364, STR 27L IAW SRM 51-42-21/06-001-001-A01, DWG SH670-32050. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.
2012
Part: O-RING — FAILED (HYDRAULIC SYS) · airframe 21,565 hrs · 15,453 cycles
ON CLIMBOUT FROM HOU TO CVG, COMPLETE LOSS OF SYSTEM NR 3 HYD FLUID. EMERGENCY DECLARED, A/C DIVERTED TO IAH, LANDED SAFELY. INSPECTED A/C, FOUND LEAKING FITTING ON NR 3 HYD PRESSURE MANIFOLD. REMOVED AND REPLACED O-RING ON PRESSURE MANIFOLD. OPS CHECK GOOD, NO LEAKS NOTED.
2011
Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,376 hrs · 14,582 cycles
LEFT 280 CROSSBEAM IS CORRODED AND REQUIRES REPLACEMENT. REMOVED LEFT FS 280 CROSSBEAM AND INSTALLED SERVICABLE 280 CROSSBEAM IAW CRJ SRM 51-25-06, 51-42-10 AND 51-42-21.
Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,376 hrs · 14,582 cycles
RIGHT 280 CROSSBEAM IS CORRODED AND REQUIRES REPLACEMENT. REMOVED AND REPLACED RIGHT CROSSBEAM IAW CRJ SRM 51-42-06.
2008
Part: WARNING LIGHT — FALSE INDICATION (NLG STEERING) · airframe 14,190 hrs · 10,209 cycles
ON APPROACH INTO CVG, RECEIVED STEERING INOP CAUTION MSG AFTER GEAR WAS SELECTED DOWN. EMERGENCY DECLARED, ACFT LANDED SAFELY. POWERED DOWN ACFT AND BACK UP, PERFORMED NWS SYSTEM OPERATIONAL CHECKS, NO DEFECTS NOTED.
Part: SLAT — MALFUNCTIONED (WING) · airframe 14,090 hrs · 10,136 cycles
AFTER TAKEOFF FROM JFK RECEIVED A SLAT FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND CONTINUED TO BWI, AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED SYSTEM RESET.
Part: WARNING SYSTEM — MALFUNCTIONED (L/E SLAT) · airframe 13,386 hrs · 9,615 cycles
FLIGHT 5622 RECEIVED SLAT FAIL CAUTION MESSAGE. DECLARED EMERGENCY, RETURNED TO ATL, LANDED WITHOUT INCIDENT. PERFORMED RESET AND CLEARED INHIBITS. VISUALLY INSPECTED SLATS AND SLAT DISCONNECT SYSTEM. PERFORMED OPERATIONAL CHECK. NO FURTHER DEFECTS. (S)
Part: FAN BLADE — STUCK (LT ENGINE) · airframe 12,731 hrs · 9,181 cycles
FLIGHT 5311 - EN ROUTE FROM CVG TO COS, N1 VIBE ON NR 1 ENGINE WENT TO 1.9. EMERGENCY DECLARED AND AIRCRAFT DIVERTED TO MCI AND LANDED SAFELY. REMOVED AND REPLACED ALL FAN BLADES ON NR 1 ENGINE.
2007
Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 11,746 hrs · 8,542 cycles
FLIGHT 5250 - NOSE WHEEL STEERING INOP. PERFORMED RESET OF NWS SYSTEM. OPS CHECK GOOD.
Part: WINDOW — CRACKED (COCKPIT) · airframe 11,727 hrs · 8,539 cycles
FLIGHT 5419 - F/O SIDE WINDOW CRACKED IN FLIGHT PASSING 7000FT. NO IMPACT WITH ANY OUTSIDE OBJECT NOTED. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED F/O'S SIDE WINDOW.
Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 11,218 hrs · 8,190 cycles
FS 280.0 CROSSBEAM IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06.
2006
Part: CAUTION MESSAGE — ILLUMINATED (SPOILER) · airframe 7,711 hrs · 5,831 cycles
FLIGHT 5410 - DURING CVG APPROACH RECEIVED AN INBOARD FLIGHT SPOILER AND INBOARD SPOILERON CAUTION MESSAGE. PERFORMED SYSTEM RESET.
2005
Part: SMOKE — DETECTED (COCKPIT) · airframe 6,475 hrs · 5,031 cycles
FLIGHT 5803 - FUMES IN COCKPIT. TURNED OFF LEFT BLEED AIR AND FUMES DISSIPATED. NO FUMES OR SMELL DURING GROUND RUNS.
Part: CONTROL UNIT — MALFUNCTIONED (RUDDER/SPOILERS) · airframe 6,419 hrs · 4,987 cycles
SPOILER, STAB AND RUDDER LIMITER FAULT. RESET THE SSCU. NO DEFECTS NOTED.
2004
Part: PDU — FAILED (L/E SLAT) · airframe 3,934 hrs · 3,065 cycles
FLIGHT 9495 SLAT FAIL MESSAGE. REPLACED THE POWER DRIVE UNIT.
Part: PSEU — MALFUNCTIONED (E/E BAY) · airframe 3,931 hrs · 3,062 cycles
FLIGHT 5071 SLAT FAIL CAUTION. REPLACED THE PSEU.
Part: SLAT — MALFUNCTIONED (WING) · airframe 3,930 hrs · 3,061 cycles
FLIGHT 5454, SLAT FAIL CAUTION MESSAGE. COULD NOT DUPLICATE, FOUND NO DEFECTS. REMOVED AND REPLACED DCU'S AND SLAT ACTUATORS FOR TROUBLESHOOTING.
Part: WINDOW — CRACKED (COCKPIT) · airframe 3,301 hrs · 2,567 cycles
FLIGHT 5249 CO-PILOTS SIDE WINDOW CRACKED. REPLACED WINDOW.
Part: DOOR — OPEN (CARGO BAY) · airframe 2,081 hrs · 1,610 cycles
FLIGHT 5091 CABIN ALTITUDE CAUTION MESSAGE. FOUND AFT CARGO DOOR NOT CLOSED PROPERLY. CLOSED DOOR, NO DEFECTS FOUND.
Part: WARNING LIGHT — MALFUNCTIONED (SLATS) · airframe 1,307 hrs · 1,042 cycles
FLIGHT 5362 SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. NO FAULTS IN COMPUTER, SYSTEM OPERATION NORMAL.
Part: CONTROLLER — MALFUNCTIONED (SPOILER) · airframe 1,148 hrs · 929 cycles
FLIGHT 5585 GROUND LIFT DUMP NOT ARMED MESSAGE. COULD NOT DUPLICATE. NO FAULTS LOGGED IN COMPUTER.
Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 1,068 hrs · 869 cycles
FLIGHT 5079 RIGHT THRUST REVERSER UNSAFE MESSAGE DURING T/O. DEFERRED MAINT PER MEL.
Part: LIGHT — FIRE (COCKPIT) · airframe 1,026 hrs · 840 cycles
COPILOTS FWD FLOOD LIGHT CAUGHT ON FIRE. DEACTIVATED BY PULLING CIRCUIT BREAKER AND DEFERRED MAINT PER MEL.
2003
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 356 hrs · 316 cycles
LEFT FS 1098.20 BULKHEAD BETWEEN STRINGERS 8L AND 9L IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW MFG REO 670-53-61-034 REV B.
1998
Part: VALVE — LEAKING (RT ENGINE)
RIGHT ENGINE B-SUMP REGULATOR VALVE LEAKING. REPLACED VALVE.