N228PQ
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.
200 reports on file, 2010-09-08 – 2025-09-30.
Part: RETAINER — CORRODED (ZONE 100) · airframe 35,388 hrs · 26,027 cycles
AFTER SEAL AFT BAGGAGE-BAY DOOR REMOVAL IN REF NRC 00112, CORROSION ON SEAL RETAINER LOWER WAS FOUND. SEAL RETAINER LOWER WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
Part: SKIN — WORN (ZONE 100) · airframe 35,388 hrs · 26,027 cycles
WEAR ON EXTERNAL FUSELAGE SKIN FS913.00 TP FS 927.00 BTW STGR 26LH TO STGR 26RH EXTERNAL FUSELAGE SKIN FS913.00 TP FS 927.00 BTW STGR 26LH TO STGR 26RH WAS REPAIRED PER REO 670-53-00-290 REV -E
Part: WEB — CRACKED (ZONE 100) · airframe 35,388 hrs · 26,027 cycles
LEFT ELECTRICAL BAY WEB FLOOR FS 193.00 (BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT LH ELECTRICAL BAY WEB FLOOR FS 193.00 (BELOW ACCUMULATOR GAUGE INDICATOR) AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01
Part: FITTING — CORRODED (ZONE 200) · airframe 35,388 hrs · 26,027 cycles
CORROSION ON ATTACHEMENT POINT (2EAS) OF GALLEY 1 LOCATED BTW FS280/FS295 AND RBL 18 AND 38 AT FLOOR STRUCTURE OF CABIN PAX. CORROSION ON ATTACHMENT POINT (2EAS) OF GALLEY 1 LOCATED BTW FS280/FS295 AND RBL 18 AND 38 AT FLOOR STRUCTURE OF CABIN PAX WAS REMOVED IAW CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT OT LIMITS IAW CRJ900 SRM 53-00-00-101-001-A01 THEREFORE ATTACHMENT POINTS (2EAS) WERE REPLACED IAW CRJ900 SRM 51-42-21-001-001-A01
Part: PANEL — CRACKED (ZONE 800) · airframe 35,388 hrs · 26,027 cycles
CRACK ON FWD SIDE PANEL (STEPS) AT L1 DOOR. CRACKED ON FWD SIDE PANEL (STEPS) AT L1 DOOR. WAS REPAIRED IAW SRM 52-11-04-201-004-A01.
Part: SUPPORT FITTING — WORN (ZONE 800) · airframe 35,388 hrs · 26,027 cycles
INITIAL INSPECTION': WEAR AT FWD / AFT HANDRAIL SUPPORT FITTING AT FWD & AFT SIDE PANEL OF PASSENGER DOOR, ALSO MISSING BUMPERS. MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE LH WAS FABRICATED AND INSTALLED AND BIN SUPPORT RH WAS REPLACED PER EA CRJ953-20434 REV. A, SRM 51-41-02-001-001-A01, AND AMM 20-21-00-910-801-A01
Part: DOOR — CRACKED (ZONE 800) · airframe 35,388 hrs · 26,027 cycles
CRACK ON FWD MEMBRANE OF INBD DOOR AT LH MLG INBD DOOR AT LH MLG WAS REPLACED IAW CRJ-900 AMM 32-12-01-400-802-A04
Part: BEAM — WORN (ZONE 800) · airframe 35,388 hrs · 26,027 cycles
OUT OF SCOPE: WEAR ON AFT BEAM AT AFT BAGGAGE-BAY CARGO DOOR STRUCTURE (INTERFERENCE WITH AFT BALANCE SPRING CABLE). WEAR ON AFT BEAM AT AFT BAGGAGE-BAY CARGO DOOR STRUCTURE (INTERFERENCE WITH AFT BALANCE SPRING CABLE) WAS REPAIRED PER EA CRJ953-20392 REV IR.
Part: COVER — CRACKED (ZONE 800) · airframe 35,388 hrs · 26,027 cycles
OUT OF SCOPE: CRACK ON AFT TRACK COVER OF THE AFT BAGGAGE BAY DOOR. AFT TRACK COVER ( ROLLER GUIDE) OF THE AFT BAGGAGE BAY DOOR WAS FABRICATED PER EA CRJ953-20421 REV IR AND REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: PANEL — CRACKED (ZONE 800) · airframe 35,388 hrs · 26,027 cycles
CRACK ON AFT SIDE PANEL (STEPS) AT L1 DOOR. CRACKED ON AFT SIDE PANEL (STEPS) AT L1 DOOR WAS REPAIRED IAW SRM 52-11-04-201-004-A01.
Part: SUPPORT FITTING — WORN (ZONE 800) · airframe 35,388 hrs · 26,027 cycles
WEAR AT FWD / AFT HANDRAIL SUPPORT FITTING AT FWD & AFT SIDE PANEL OF PASSENGER DOOR, ALSO MISSING BUMPERS. WEAR AT FWD / AFT HANDRAIL SUPPORT FITTING AT FWD & AFT SIDE PANEL OF PASSENGER DOOR WERE FOUND OUT LIMITS THEREFORE WERE REPLACED AND BUMPERS WERE INSTALLED PER SRM 53-82-55-101-002-A02 AND SRM 51-42-21-001-001-A01
Part: SUPPORT FITTING — WORN (ZONE 800) · airframe 35,388 hrs · 26,027 cycles
WEAR AT FWD / AFT HANDRAIL SUPPORT FITTING AT FWD & AFT SIDE PANEL OF PASSENGER DOOR, ALSO MISSING BUMPERS. MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE LH WAS FABRICATED AND INSTALLED AND BIN SUPPORT RH WAS REPLACED PER EA CRJ953-20434 REV. A CRJ900 SRM 51-41-02-001-001-A01 AND AMM 20-21-00-910-801-A01
Part: PLATE — WORN (ZONE 500) · airframe 35,388 hrs · 26,027 cycles
"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF FLAP STUB FAIRING 171DL AND 172DR AT RH/LH WING TRAILING EDGE (ROOT WING). WEAR ON FLAP FITTING AND PLATE SUPPORT OF FLAP STUB FAIRING 171DL AND 172DR AT RH/LH WING TRAILING EDGE (ROOT WING) WERE FOUND OUT LIMITS THEREFORE WERE REPLACED PER CRJ900 SRM 53-82-55-101-002-A02, SRM 51-42-21-001-001-A01 AND SRM 51-41-04-01-001-A01"
Part: FITTING — WORN (ZONE 500) · airframe 35,388 hrs · 26,027 cycles
WEAR ON FLAP FITTING AND PLATE SUPPORT OF FLAP STUB FAIRING 171DL AND 172DR AT RH/LH WING TRAILING EDGE (ROOT WING). WEAR ON FLAP FITTING AND PLATE SUPPORT OF FLAP STUB FAIRING 171DL AND 172DR AT RH/LH WING TRAILING EDGE (ROOT WING) WERE FOUND OUT LIMITS THEREFORE WERE REPLACED PER CRJ900 SRM 53-82-55-101-002-A02, SRM 51-42-21-001-001-A01 AND SRM 51-41-04-01-001-A01"
Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 35,388 hrs · 26,027 cycles
CRACK AT LOWER SUPPORT ANGLE OF EXTERNAL SERVICE PANEL. CRACKED LOWER SUPPORT ANGLE OF EXTERNAL SERVICE PANEL WAS REPLACED IAW SRM 51-42-06-001-001-A01
Part: ACCESS PANEL — CORRODED (ZONE 100) · airframe 35,388 hrs · 26,027 cycles
CORROSION ON SETTLEMENT AREA OF HYDRAULIC ACCESS PANEL 195AB. STRAP ON SETTLEMENT AREA ON ACCESS PANEL 195AB WAS FOUND TO EXCESSIVE DAMAGE THEREFORE WAS FABRICATED AND INSTALLED PER CRJ900 SRM 53-82-55-101-002-A02, SRM 51-42-13-001-001-A01 AND EA CRJ953-20441 REV IR
Part: LATCH — OUT OF TOLERANCE (ZONE 800) · airframe 34,916 hrs · 25,603 cycles
ONCE ARRIVE IN ATL PAX DOOR JAMMED AND UNABLE TO OPEN. FOUND DOOR INTERNALLY OUT OF RIG AND AFT SPIGOT OUT OF ADJUSTMENT TOLERANCE. PERFORMED ADJUSTMENT OF THE LATCH MECHANISM IAW CRJ900 AMM 52-11-02. ADJUSTED AFT SPIGOT IAW CRJ900 AMM 52-21-23. FUNCTIONAL OF PAX DOOR LATCH MECHANISM GOOD.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 34,258 hrs · 24,999 cycles
LH FWD OVERWING EMERGENCY EXIT DOOR, VISIBLE CRACK AT BOTTOM OF TOP AFT LUG. REPAIRED L/H FWD OVERWING EMERGENCY EXIT DOOR IAW MHIRJ GREO 670-52-21-103 REV--11/06/2024.
Part: DIAPHRAGM — DAMAGED (ZONE 200) · airframe 34,258 hrs · 24,999 cycles
WHILE PERFORMING SB 670BA-53-036 AND REMOVING THE LH BL36 FLOOR BEAM TWO HOLES WERE ELONGATED IN THE FS 756 DIAPHRAGM. THE DIAPHRAGM REQUIRES REPLACEMENT OR A REPAIR. REPAIRED DIAPHRAGM IAW MHIRJ REO 690-53-41-514 REV -- DATED 2025-02-17
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 34,258 hrs · 24,999 cycles
LH AFT OVERWING EMERGENCY EXIT DOOR, VISIBLE CRACK AT BOTTOM OF TOP AFT LUG. REPAIRED L/H AFT OVERWING EMERGENCY EXIT DOOR IAW MHIRJ GREO 670-52-21-103 REV--11/06/2024.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 34,258 hrs · 24,999 cycles
RH AFT OVERWING EMERGENCY EXIT DOOR, SUSPECT CRACK AT BOTTOM OF TOP AFT LUG. REPAIRED R/H AFT OVERWING EMERGENCY EXIT DOOR IAW MHIRJ GREO 670-52-21-103 REV--11/06/2024.
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 34,258 hrs · 24,999 cycles
RH FWD OVERWING EMERGENCY EXIT DOOR, VISIBLE CRACK AT BOTTOM OF TOP AFT LUG. REPAIRED R/H FWD OVERWING EMERGENCY EXIT DOOR IAW MHIRJ GREO 670-52-21-103 REV--11/06/2024.
Part: FITTING — NONE · airframe 34,258 hrs · 24,999 cycles
WHILE PERFORMING SB 670BA-53-044 REVISION G, DATED JUL 05/2022 FOUND LH FITTING PN CC670-33563-001SB AND RH FITTING PN CC670-33562-001SB AT STR12A CANNOT BE INSTALLED IN ACCORDANCE WITH SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING AIRCRAFT RIVET PATTERN. COMPLIED WITH MHIRJ REO 690-53-11-1946 REV-- DATED 2025-02-13.
Part: SENSOR — INOPERATIVE (BRAKE TEMP) · airframe 34,141 hrs · 24,906 cycles
DURING CLIMB AT FL 230, BRAKE OVHT WARNING MESSAGE ANNUNCIATED, FOLLOWED EMERGENCY CHECKLIST AND DESCENDED TO 10,000 AND EXTENDED LANDING GEAR. BTMS ON RHOB BRAKE WERE SPORADIC. FAULTY SENSOR SUSPECTED AND CONTINUE TO DESTINATION AS DIRECTED BY QRH DEFERRING RH EICAS BRAKE TEMPERATURE MONITORING READOUT IAW MEL 32-46-1D. M PROCEDURES C/W, MMO2 UPDATED, PLACARD INSTALLED, MOC NOTIFIED # 103486. R/R RT OTBD THERMOCOUPLE SENSOR IAW AMM 32-46-01. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. MOC #95909 NOTIFIED. PLACARD REMOVED. OSD: 1/21/2025
Earlier reports · 2010–2024 · 176 reports
2024
Part: LATCH — INOPERATIVE (MAIN DOOR) · airframe 32,986 hrs · 23,907 cycles
MAIN CABIN DOOR FAILED TO OPEN AFTER MULTIPLE ATTEMPTS BY FA AND GROUND CREW PERSONNEL. DOOR HANDLE FAILED TO UNLATCH. PERFORMED OPS TEST OF DOOR PER AMM 52-11-00-710-801. CYCLED DOOR 4 TIMES. NO DEFECTS NOTED. A/C OK FOR SVC.
2023
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,610 hrs · 22,755 cycles
GALLEY EMERGENCY FLOOR LIGHT AND RT SIDE FIRST CLASS DIVIDER EMERGENCY LIGHT INOP REMOVED AND REPLACED #1 EMERGENCY BATTERY PACK CHARGER IAWCRJ 900 AMM 33-51-17. OPC GOOD. PN OFF-ON: 11-0049, SN OFF: 23709 SN ON: 22853
Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 31,154 hrs · 22,372 cycles
FLOOR PROXIMITY EXIT SIGN (DS156) HAS BULBS INOP RELAMPED EXIT SIGN (DS156) IAW CRJ 900 AMM 33-51-05. OPC GOOD. P/N OFF/ON: OL-3071BPE/GPL
2022
Part: SILL DRAIN — CORRODED · airframe 28,669 hrs · 20,268 cycles
AFT BAGGAGE BAY DOOR SILL CORRODED BETWEEN FS1000 AND FS1047. - REMOVED CORRODED DOOR SILL BETWEEN F.S.1000 AND F.S.1047 AND INSTALLED NEW SERVICABLE DOOR SILL IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND51-42-21-001-001-A01.
Part: SKIN — CORRODED · airframe 28,669 hrs · 20,268 cycles
PASSENGER DOOR, FWD UPPER SIDE, INNER SKIN, CORROSION AROUND ACCESS 832AL. - REPLACED PAX DOOR INNER SKIN IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, CW EA CRJ952-12954. REPAIRED FASTENER HOLE IAW EA CRJ 952-12954 REV IR.
Part: DOUBLER — CORRODED · airframe 28,669 hrs · 20,268 cycles
ANTENNA DOUBLER AT STGR 27 BETWEEN FS 295 AND FS 310 HAS MULTIPLE SPOTS OF CORROSION. TCI# 53-20-304 - REPLACED ANTENNA DOUBLER IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01. REPLACED & INSTALLED ANTENNA IAW CRJ 900 AMM 34-53-04-000/400-801-A01, 34-53-00-710-801(A01) 34-53-00-720-801(A01)
Part: BRACKET — GOUGED · airframe 28,669 hrs · 20,268 cycles
FWD CARGO DOOR BOTTOM AFT MOUNT BRACKET IS GOUGED AT F.S. 565. - REPLACED FWD CARGO DOOR BOTTOM AFT MOUNT BRACKET AT FS 565 IAW CRJ 900 SRM'S 51-42-06-001-001-A01 51-12-00-001-001-A01, 53-31-23-101-001-A02, AND NDTM 51-20-008-270-A01
Part: FRAME — CORRODED · airframe 28,669 hrs · 20,268 cycles
STGR 24R IS CORRODED BETWEEN F.S. 669.40 TO F.S. 677. TCI 53-20-306 - COMPLIED WITH ACCESS/REINSTALL & STRINGER REPAIR IAW EA CRJ953-13033 REV. IR, SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01, AMM'S 21-24-18-000/400-A01, 21-23-57-000/400-801-A07, 21-23-54-000/400-811-A01, 21-23-54-000/400-810-A01, 21-23-53-000/400-806-A01 & ESPM 20-12-00 LK CKS GOOD IAW AMM 21-23-00-700-801-A01
Part: FRAME — CUT · airframe 28,669 hrs · 20,268 cycles
FRAME AT FS 661.00+74 NEEDS REMOVED FROM STR 20R TO STR 25R FOR STRINGER REPAIR ACCESS. (REF JOB 81522851, OPS 337 & 335) - ACCESSED FRAME IAW AMM 21-23-54-000/400-801-A01, ESPM 20-72-00, SRMS 51-42-21-101-001-A01, 51-42-06-001-001-A01, 53-01-06-201-001-A03, 53-00-06-201-001-A03, LK CK GOOD IAW AMM 21-23-00-700-801-A01
Part: STRINGER — CORRODED · airframe 28,669 hrs · 20,268 cycles
CORROSION FOUND ON STGR 20R BETWEEN FS661+90-177. - COMPLIED WITH EA CRJ953-13031 REV A.
Part: STRINGER — CORRODED · airframe 28,669 hrs · 20,268 cycles
FWD STRINGER 20R IS CORRODED FROM FS 280 TO FS 319. - COMPLIED WITH EA CRJ 953-13053 REV IR
Part: SPLICE — CORRODED · airframe 28,669 hrs · 20,268 cycles
SPLICE AT STRINGER 24R FS 333 IS CORRODED. - REPLACED SPLICE AT STR 24R FS 333 IAW CRJ 900 SRM'S, 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-12-21-001-001-A01, 51-23-001-001-A01 AND 51-21-11-001-001-A01.
Part: FRAME — CORRODED · airframe 28,669 hrs · 20,268 cycles
F.S 280 IS CORRODED BETWEEN STGR 25R TO STGR 25L AROUND NUTPLATES. - REPAIRED IAW EA CRJ953-12961 REV IR & SRM 51-42-10-001-001-A01.
Part: STRINGER — CORRODED · airframe 28,669 hrs · 20,268 cycles
FWD STRINGER 24R IS CORRODED FROM FS 280 TO 333. - RECEIVED & COMPLIED WITH ENDEAVOR AIR EA CRJ 953-13054 REV IR DATED 3/16/22 SECURED WIRE TO STANDOFF IAW ESPM 20-12-00
Part: SEAL PLATE — GOUGED · airframe 28,669 hrs · 20,268 cycles
CENTER CARGO DOOR LOWER SEAL PLATE GOUGED - REMOVED, LOCATED, DRILLED & INSTALLED CENTER CARGO DOOR IAW CRJ900 SRM 52-35-07-000/400/802(A02), SRM 51-40-11-001-001-A01.
Part: SILL DRAIN — CORRODED · airframe 28,669 hrs · 20,268 cycles
R/H FLOOR SEAL AT F.S. 280 IS CORRODED ON THE BOTTOM SIDE WHERE DRAIN TUB MOUNTS. - REMOVED, DRILLED, LOCATED AND INSTALLED SERVICABLE SILL IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01. LOCATED, DRILLED & INSTALLED NUTPLATES IAW CRJ 900 SRM 51-40-11-001-001-A01. REMOVED & INSTALLED SOLID RIVETS & HI-LITE FASTENER, APPLIED CIC IAW CRJ 900 SRM 51-21-11-001-001-A01.
Part: ANGLE — CORRODED · airframe 28,669 hrs · 20,268 cycles
PAX DOOR TOP ANGLE & CLIPS (FWD & AFT) AT INTERCOSTAL DD7A ARE CORRODED. - REPLACED TOP ANGLE & CLIPS (FWD & AFT) AT INTERCOSTAL DD7A W/ NEW, IAW CRJ900 SRM TASK 51-40-11-001-001-A01. ALSO IAW CRJ 900 SRM TASK 51-42-06-001-001-A01. ALSO, IAW CRJ 900 SRM TASK 51-42-21-001-001-A01.
Part: DRAG ANGLE — ELONGATED · airframe 28,669 hrs · 20,268 cycles
FWD DRAG ANGLE (P/N 601R31772-6) ON PAX DOOR HAS OVERSIZED AND ELONGATED FASTENER HOLES. - REMOVED AND REPLACED PAX DOOR FWD DRAG ANGLE P/N 601R31772-6 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: ANGLE — CORRODED · airframe 28,669 hrs · 20,268 cycles
PAX DOOR TOP ANGLE & CLIPS (FWD & AFT) AT INTERCOSTAL DD7A ARE CORRODED. - REPLACED TOP ANGLE & CLIPS (FWD & AFT) AT INTERCOSTAL DD7A W/ NEW, IAW CRJ900 SRM TASK 51-40-11-001-001-A01. ALSO IAW CRJ 900 SRM TASK 51-42-06-001-001-A01. ALSO, IAW CRJ 900 SRM TASK 51-42-21-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 28,669 hrs · 20,268 cycles
PAX DOOR INTERCOSTAL DD6 IS CORRODED. - REPLACED INTERCOSTAL DD6 W/NEW IAW CRJ 900 SRM TASK 51-40-11-001-001-A01. ALSO SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: ANGLE — MISINSTALLED · airframe 28,669 hrs · 20,268 cycles
PAX DOOR AFT WEB FASTENER HOLES COMMON WITH DRAG ANGLE ARE OVERSIZED & FASTENERS ARE PULLING THROUGH. - REMOVED AND REPLACED AFT PAX DOOR WEB P/N 601R317071-11 AND DRAG ANGLE P/N 601R31772-5 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 28,669 hrs · 20,268 cycles
PAX DOOR INTERCOSTAL DD2 (FWD) IS CORRODED. - REPLACED PAX DOOR INTERCOSTAL DD2 W/NEW IAW CRJ 900 SRM TASK 51-40-11-001-001-A01. D.STEPHENS ALSO SRM 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 28,669 hrs · 20,268 cycles
PAX DOOR INTERCOSTAL DD2 (MID) IS CORRODED. - REPLACED PAX DOOR INTERCOSTAL DD2 W/NEW IAW CRJ 900 SRM TASK 51-40-11-001-001-A01. ALSO SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 28,669 hrs · 20,268 cycles
PAX DOOR INTERCOSTAL DD5 (FWD) IS CORRODED. - REPLACED PAX DOOR INTERCOSTAL DD5 IAW CRJ 900 SRM TASK 51-40-1-001-001-A01. ALSO SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001 -A01.
Part: WEB — CORRODED · airframe 28,669 hrs · 20,268 cycles
CORROSION FOUND ON WEB OF PAX DOOR. (P/N 601R317071-12) - REMOVED AND REPLACED PAX DOOR FWD WEB P/N 601R317071-12 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: WEB — MISINSTALLED · airframe 28,669 hrs · 20,268 cycles
PAX DOOR AFT WEB FASTENER HOLES COMMON WITH DRAG ANGLE ARE OVERSIZED & FASTENERS ARE PULLING THROUGH. - REMOVED AND REPLACED AFT PAX DOOR WEB P/N 601R317071-11 AND DRAG ANGLE P/N 601R31772-5 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: YOKE — CHAFED · airframe 28,669 hrs · 20,268 cycles
RH ENG YOKE CHAFFED ON INBD UPPER AND LOWER RADIUS (MARKED WITH ORANGE TAPE) - REMOVED/REINSTALLED RH ENG YOKE AND REPAIRED IAW AMM 71-21-01-000/400-801-A01 AND REO 670-71-21-057 REV-- ,
Part: YOKE — CHAFED · airframe 28,669 hrs · 20,268 cycles
LH ENG YOKE CHAFFED ON INBD RADUIS (UPPER AND LOWER) MARKED WITH ORANGE TAPE. - REMOVED/REINSTALLED AND REPAIRED ENG YOKE IAW AMM 71-21-01-000/400-801-A01 AND REO 690-71-21-057 R-- AND 670-71-21-057 REV
Part: STRINGER — CORRODED · airframe 28,669 hrs · 20,268 cycles
F.S 517 TO F.S 565 FWD CARGO DOOR ENTRY SEAL IS CORRODED AROUND RIVETS. - REPAIRED STR 26R IAW CRJ 900 SRM 53-00-03-201-001-A02.
Part: FRAME — CUT · airframe 28,669 hrs · 20,268 cycles
LOWER FRAME SECTOR AT FS 661 BETWEEN STGR 26L AND STGR 25R REQUIRES REMOVAL FOR STGR 26R REPAIR. - REMOVED & REINSTALLED FS 661 LOWER FRAME SECTOR BRWN STR 26L AND 26R IAW CRJ900 SRM 53-00-06-201-801-A01/A03.
Part: FITTING — CORRODED · airframe 28,669 hrs · 20,268 cycles
R/H WING, AILERON CENTER HINGE FITTINGS GOUGED IN SEVERAL AREAS (MARKED) - REMOVED RH WING AILERON CENTER HINGE FITTING IAW MHIRJ REO 690-57-51-255 REV-- DATED 2022-03-02
Part: INTERCOSTAL — CORRODED · airframe 28,669 hrs · 20,268 cycles
#2 INTERCOSTAL BETWEEN FS349.00 + 364.00 LOCATED BETWEEN STR 26L & 27 IS CORRODED - FOUND NO ALLOWABLE DAMAGE. REMOVED, LOCATED & DRILLED AND INSTALLED INTERCOSTAL IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01. REMOVED & REINSTALLED AVI DOOR PROX SENSOR IAW CRJ 900 AMM 52-70-08-000/400-801(A01) OPS TEST GOOD IAW CRJ 900 AMM 52-42-00-710-801-A01
Part: RETAINER — CORRODED · airframe 28,669 hrs · 20,268 cycles
AVI DOOR L/H & R/H FWD SEAL RETAINERS ARE CORRODED - REMOVED & REPLACED LH & RH FWD & AFT SEAL RETAINERS IAW CRJ 900 SRM 51-42-06-001-001-A01. OPS CHECK OF AVI DOOR GOOD IAW CRJ 900 AMM 52-42-00-710-801(A01) REMOVED & REINSTALLED DOOR IAW CRJ 900 AMM 52-42-00-000/400-801(A01)
Part: FRAME — CUT · airframe 28,669 hrs · 20,268 cycles
LOWER FRAME SECTOR AT FS 645 BETWEEN STGR 26L AND STGR 26R REQUIRES REMOVAL FOR STGR 26R REPAIR. - REMOVED AND REPLACED FS 645 LOWER FROM SECTOR BETWEEN STR 26L AND 26R IAW 53-00-06-201-001-A01 AND 51-42-06-001-001-A01, 51-21-16-001-001-A01 CRJ 900 SRM.
Part: SHIM — CORRODED · airframe 28,669 hrs · 20,268 cycles
2 EA SHIMS COMMON TO FLOORBEAM @ FS 333 & RBL 9 ARE CORRODED - REPAIRED SHIMS I/A/W CRJ 900 SRM 51-21-06-001-001-A01, AND 51-42-06-001-001-A01.
Part: ANGLE — CORRODED · airframe 28,669 hrs · 20,268 cycles
CORROSION FOUND ON UPPER PAX DOOR SILL ANGLE AT FS 319. - REPLACED PAX DOOR SILL ANGLE AT FS319 IAW CRJ 900 SRM 51-41-02-001-001-A01, 51-21-11-001-001-A01, 53-211-23-101-001-A02.
Part: STRINGER — CORRODED · airframe 28,669 hrs · 20,268 cycles
STGR 26R IS CORRODED BETWEEN F.S. 661+74 TO F.S. 669.40. - COMPLIED WITH EA CRJ953-12984 REV IR.
Part: FORMER — CORRODED · airframe 28,669 hrs · 20,268 cycles
PAX DOOR FWD FORMER IS CORRODED. - REMOVED AND REPLACED PAX DOOR FWD FORMER IAW CRJ 900 SRMS 51-26-00-001-001-A01, 51-40-11-001-001-A01, 51-41-02-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01.
Part: STRINGER — CORRODED · airframe 28,669 hrs · 20,268 cycles
FWD STRINGER 22R IS CORRODED FROM FS. 280 TO FS. 333. - REPLACED STR 22R AT FS 280-333 IAW CRJ900 SRM 51-42-06-001-001-A01 51-40-11-001-001-A01
Part: STRINGER — CORRODED · airframe 28,669 hrs · 20,268 cycles
AFT STRINGER 24R AT FS 333-364 IS CORRODED. - REPLACED AFT STR 24R AT FS 333-364 IAW CRJ900 SRM 53-00-03-201-001-A02 51-40-11-001-001-A01 51-42-06-001-001-A01
Part: CROSSBEAM — CORRODED · airframe 28,669 hrs · 20,268 cycles
LH FS 280.00 CROSSBEAM IS CORRODED. - REPLACED LH FS 280 CROSSBEAM IAW CRJ900 SRM'S 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, 51-42-10-001-001-A01 & REMOVED & REINSTALLED DRIP TRAY & SHEAR BOX.
Part: STIFFENER — CRACKED · airframe 28,669 hrs · 20,268 cycles
RH MID STIFFINER AT FS 280 IS CRACKED. - REMOVED AND REPLACED RH MID STIFFENER IAW CRJ 900 SRM 51-40-11, 11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.
Part: SPLICE ANGLE — CORRODED · airframe 28,669 hrs · 20,268 cycles
SPLICE ANGLE AT FS 333 FRAME, STRINGER 22R IS CORRODED. - REPLACED STR 22R SPLICE ANGLE AT FS 333 IAW CRJ900 SRM 51-42-06-001-001-A01
Part: STRINGER — CORRODED · airframe 28,669 hrs · 20,268 cycles
AFT STRINGER 22R IS CORRODED FROM FS. 333 TO FS. 349. - REPLACED STR 22R FS 333-349 IAW CRJ900 SRM 51-40-11-001-001-A01 51-42-06-001-001-A01 51-42-21-001-001-A01
Part: CROSSBEAM — CORRODED · airframe 28,669 hrs · 20,268 cycles
RH FS 280 CROSSBEAM IS CORRODED. - REMOVED AND REPLACED FS 280 CROSSBEAM IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, 51-42-10-001-001-A01 AND 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 28,669 hrs · 20,268 cycles
INTERCOSTAL AT STGR 20R AND BETWEEN FS 319 TO FS 349 BELOW GALLEY SERVICE DOOR IS CORRODED. - REPLACED INTERCOSTAL AT STR20R FS319-349 IAW CRJ 900 SRM 57-42-06-001-001-A01, 57-42-21-001-001-A01, 57-40-11-001-001-A01 & 3 EA CLEATS.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
RH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 744 TO FS 752. - REMOVED AND REPLACED SEAT TRACK IAW CRJ 900 AMM 53-00-49-400-801-A11.
Part: STRINGER — CORRODED · airframe 28,669 hrs · 20,268 cycles
STGR 21R IS CORRODED BETWEEN FS 333 AND FS 319.70. - NO DAMAGE ALLOWED ON STR 21R BETWEEN FS 310 TO FS 333 IAW CRJ 900 SRM 53-21-03-101-002-A04 STR 21R BETWEEN FS 280.00 TO FS 333.0 NEED TO BE REPLACED, RECEIVED AND COMPLETED ENDEAVOR AIR EA #CRJ953-13008 REV IR
Part: ANGLE — CORRODED · airframe 28,669 hrs · 20,268 cycles
J ANGLE AT FLOOR LEVEL FS 280, COCKPIT DOOR THRESHOLD IS CORRODED. - REPLACED "J" ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01.
Part: STRINGER SPLICE — CORRODED · airframe 28,669 hrs · 20,268 cycles
STGR SPLICE ON STGR 21R AT FS 333 IS CORRODED. - LOCATED, DRILLED, AND INSTALLED NEW STR SPLICE AT STR 21R AND FS 333 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 P/N:SH670-31197-1.
Part: POST — CORRODED · airframe 28,669 hrs · 20,268 cycles
LBL9 FLIGHT COMPARTMENT POST IS CORRODED AT F.S. 280 - REPAIRED LBL9 POST IAW CRJ 900 SRM 53-11-10-201-006-A01. =
Part: POST — CORRODED · airframe 28,669 hrs · 20,268 cycles
LBL9 FLIGHT COMPARTMENT POST IS CORRODED AT F.S. 280 - REPAIRED LBL9 POST IAW CRJ 900 SRM 53-11-10-201-006-A01.
Part: STRINGER — INCORRECT · airframe 28,669 hrs · 20,268 cycles
UPON REMOVAL OF FS 645, STR 16L CLEAT FOUND THE PRESENCE OF A THIRD HOLE IN STR 16L. - REPAIRED STR 16L AT FS 645 IAW CRJ900 SRM 53-00-03-201-001-A02.
Part: POST — CORRODED · airframe 28,669 hrs · 20,268 cycles
RBL9 FLIGHT COMPARTMENT POST CORRODED AT F.S 280. - REPLACED ATTACH ANGLE CLIP RBL9 FLIGHT COMPARTMENT FS280 IAW CRJ 900 SRM 51-42-10-001-001-A01, 57-11-10-201-006-A01, 51-40-11-001-001-A01.
Part: BRACKET — GOUGED · airframe 28,669 hrs · 20,268 cycles
FWD CARGO DOOR BOTTOM AFT MOUNT BRACKET IS GOUGED AT F.S. 565. - REPLACED FWD CARGO DOOR BOTTOM AFT MOUNT BRACKET AT FS 565 IAW CRJ 900 SRM'S 51-42-06-001-001-A01 51-12-00-001-001-A01, 53-31-23-101-001-A02, AND NDTM 51-20-008-270-A01
Part: FRAME — CORRODED · airframe 28,669 hrs · 20,268 cycles
F.S 581 FRAME IS CORRODED BETWEEN STGR 26R TO STGR 25L. - FOUND FRAME 581 BEYOND LIMITS IAW CRJ 900 SRM 53-31-06-101-003-A04. COMPLIED WITH SPLICE REPAIR IAW CRJ 900 SRM 53-00-06-201-001-A03. INSTALLED STRAP IAW CRJ 900 SRM 51-42-06-001-001-A01. TIGHTENED & HUMISEAL GROUND STUD & APPLIED CIC IAW CRJ 900 SRM 51-21-11-001-001-A01 & ESPM 20-23-01/00
Part: SPLICE ANGLE — CORRODED · airframe 28,669 hrs · 20,268 cycles
SPLICE ANGLE AT FS. 333 R/H IS CORRODED. AT STRINGER 23R - REPLACED SPICE ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 51-40-11-001-001-A01
Part: STRINGER — CORRODED · airframe 28,669 hrs · 20,268 cycles
STG 21R IS CORRODED BETWEEN FS 333 AND FS 349. - REPLACED STR 21R FS 333-349 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-10-001-001-A01, 53-21-03-101-006-A01.
Part: FRAME — CORRODED · airframe 28,669 hrs · 20,268 cycles
F.S 645 FRAME IS CORRODED BETWEEN STGR 17L TO 18L. - REPAIRED FRAME 645 BETWEEN STR 17L-18L IAW CRJ 900 SRM'S 51-21-11-001-001-A01, 51-42-06/21-001-001-A01, 53-00-06-001-001-A01, 51-42-21-001-001-A01.
Part: FITTING — CORRODED · airframe 28,669 hrs · 20,268 cycles
MONUMENT FITTING NEAR FS 280 RBL 18 IS CORRODED. - REPLACED FITTING AT FS280 RBL18 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-77-00-001-001-A01.
Part: ANGLE — CORRODED · airframe 28,669 hrs · 20,268 cycles
STG 23L IS CORRODED BETWEEN F.S. 469 TO 477.40 - COMPLIED WITH EA CRJ953-12910 REV A.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
SEAT TRACK AT FS 847+16 - 979 RBL9 HAS CORROSION - REPLACED SEAT TRACK FS847+16 - 979 RBL9 IAW CRJ900 SRM 53-00-49-201-002-A01, 53-00-49-400-801, 53-00-49-000-801 (A11)
Part: STRINGER — CORRODED · airframe 28,669 hrs · 20,268 cycles
FWD STRINGER 23R IS CORRODED FROM FS 280 TO FS 333. - REPLACED STR 23R FS 280-333 IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, 53-21-03-101-002-A04.
Part: STRINGER — CORRODED · airframe 28,669 hrs · 20,268 cycles
AFT STRINGER 23R IS CORRODED BETWEEN FS 333 AND 364. - WORK SUMMARY STATEMENT REQUIRED. J.HURST 3/8/22 C/A: 4. REPACED STR 23R IAW CRJ900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01.
Part: STRINGER — CORRODED · airframe 28,669 hrs · 20,268 cycles
STG 23L IS CORRODED BETWEEN F.S. 469 TO 477.40 - COMPLIED WITH EA CRJ953-12910 REV A.
Part: THRESHOLD — CORRODED · airframe 28,669 hrs · 20,268 cycles
SERVICE DOOR THRESHOLD IS CORRODED AROUND SCREW HOLES & HAS 1 BROKEN NUTPLATE - REPLACED SERVICE DOOR THRESHOLD I/A/W CRJ-900 SRM 51-40-11-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
LH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 847 TO FS 913. - REMOVED AND REPLACED SEAT RAIL FS 847 - FS 913 LH IAW CRJ 900 AMM 53-00-49-000-801-A11 AND 53-00-49-400-801-A11.
Part: INTERCOSTAL — CORRODED · airframe 28,669 hrs · 20,268 cycles
#3 INTERCOSTAL BETWEEN FS349 & FS364 LOCATED BETWEEN STR 27 & STR 26R IS CORRODED - REMOVED AND REPLACED INTERCOSTAL I/A/W CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
RH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 797 TO FS 847+16 - REMOVED AND REPLACED SEAT RAIL RH FS797-847+16 IAW CRJ 900 AMM 53-00-49-400-801 (CONFIG A11) AND CRJ 900 AMM 53-00-49-000-801 (CONFIG A11)
Part: ANGLE — CORRODED · airframe 28,669 hrs · 20,268 cycles
KICKPLATE ANGLE AT PAX DOOR SURROUND IS CORRODED. - REMOVED AND REPLACED PAX DOOR SURROUND KICKPLATE ANGLE I/A/W CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
RH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 847+16 - REMOVED AND REPLACED RH SIDEWALL SEAT AT FS 847+16 TO FS 865 IAW CRJ 900 AMM 53-31-49-400-801-A11.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
LH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 797 TO FS 847+16. - REMOVED & REPLACED SIDE WALL SEAT TRACK IAW CRJ 900 AMM 53-00-49-000/400-801-A11
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
LH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 897 TO FS 969. - REMOVED AND REPLACED SEAT RAIL I/A/W CRJ 900 AMM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
RH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 661+90 TO FS 720. - INSTALLED NEW RH SIDEWALL SEAT TRACK BTW FS 661+90 TO FS 720 IAW CRJ 900 AMM 53-00-49-000-801-A01 AND CRJ-900 AMM 53-00-49-000-801
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
LH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 379 TO FS 581. - REMOVED AND REPLACED LH SIDEWALL SEAT TRACKS AT FS379 - FS485 IAW CRJ 900 AMM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
LH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 661+90 TO FS 720. - LH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 661+90 TO FS 720.
Part: LUG — GOUGED · airframe 28,669 hrs · 20,268 cycles
RH AILERON LUG MARKED F HAS GOUGE INSIDE BORE. - REPAIRED RH AILERON LUG IAW BOMBARDIER GREO 670-57-61-237 REV. -- DATED 2017-07-25.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
LH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 744 TO FS 752. - REMOVED AND REPLACED LH SIDEWALL SEAT TRACK AT FS744 TO FS752 IAW CRJ 900 AMM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
RH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 661 TO FS 677. - REMOVED & REPLACED SEAT RAIL IAW CRJ 900 AMM 53-00-49-000/400-801 (A11).
Part: FITTING — CORRODED · airframe 28,669 hrs · 20,268 cycles
TIE DOWN BLOCK LOCATED @ FS 390 RBL 18 IS CORRODED - BLENDED CORROSION FOUND OUT OF LIMITS IAW CRJ 900 SRM 53-21-43-101-001-A05 & 51-42-21-001-001-A01. REMOVED & REPLACED FITTING IAW CRJ 900 SRM 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
SEAT TRACK FROM FS 677-547+16 LBL 9 IS CORRODED. - REMOVED AND REPLACED SEAT TRACK FROM FS 677-847+16 LBL 9 IAW CRJ 900 AMM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,669 hrs · 20,268 cycles
RH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 379 TO FS 485. - REMOVED AND REPLACED RH SIDEWALL SEAT RAIL FS 379-485 IAW CRJ 900 AMM 53-00-49-000-801-A11 AND AMM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
RH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 469 TO FS 581. - REMOVED AND REPLACED RH SIDEWALL SEAT TRACK FS 469-581 IAW CRJ 900 AMM 53-00-49-000-801-A11 AND AM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
LH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 661+16 TO FS 677. - REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW CRJ 900 AMM 53-00-49-400-801-A11 AND SRM 53-00-49-201-002-A01
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
SEAT TRACK AT F.S 847 + 16 - 985 BLB9 HAS CORROSION. - REMOVED AND INSTALLED SEAT TRACK AT LBL 9 AT FS 847+16 - 985 IAW CRJ 900 AMM 53-00-49-000/400-801-A11 PN SH690-37388-5.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
SEAT TRACK FROM FS 364-485 LBL 28 IS CORRODED. - INSTALLED NEW SEAT TRACK PN SH690-321-27-3 FROM LBL 27 FS 364-485 IAW CRJ 900 AMM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
SEAT TRACK AT FS 927-979 RBL 28 HAS CORROSION. - REMOVED AND INSTALLED SEAT TRACK AT FS 927-979 RBL 28 IAW CRJ 900 AMM 53-00-49-000/400-801-A11 PN SH690-37386-1.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
RH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 565 TO FS 661+16. - REMOVED AND REPLACED RH SIDEWALL SEAT RAIL F/S 565-FS661+16 IAW CRJ900 AMM 53-00-49-000-801-(CONFIG A11) AND AMM 53-00-49-400-801(CONFIG A11)
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
SEAT TRACK AT FS 349-485 RBL 9 IS CORRODED. - REMOVED AND REPLACED SEAT TRACK IAW CRJ 900 AMM 53-00-49-400-801-A11, REPLACED LAV MOUNT FITTINGS IAW CRJ 900 SRM 51-41-02-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
SEAT TRACK AT FS 376-485 LBL 9 IS CORRODED. - INSTALLED NEW SEAT TRACK PN 670-32249-3 FROM LBL 9 FS 376-485 IAW CRJ 900 AMM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED · airframe 28,669 hrs · 20,268 cycles
LH SIDEWALL SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION FROM FS 565 TO FS 661+16. - REMOVED AND RELACED LH SIDEWALL SEAT RAIL FS565-FS661+16 IAW CRJ 900 AMM 53-00-49-000-801 (CONFIG A11) AND AMM 53-00-49-400-801 (CONFIG A11)
2020
Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 27,519 hrs · 19,261 cycles
ARRIVED AT PLANE, FA PANEL EMERGENCY LIGHT WERE ON. REPLACED BATT PACK TM159 (PS35), IAW AMM 33-51-17. OPS CHECK GOOD.
2018
Part: FITTING — CRACKED (FUSELAGE) · airframe 23,114 hrs · 15,916 cycles
LINTEL 3L AT STA 280 CRACKED. PERFORMED CUTOUT TO REMOVED CRACK FABRICATED AND INSTALLED REPAIR PART AT FS 280, STGR 3L LINTEL IAW EO R53568.
Part: SUPPORT STRAP — BROKEN (CABIN) · airframe 23,114 hrs · 15,916 cycles
NR 6 DADO PANEL RT SIDE (272SRW) SUPPORT STRAP BROKEN. REMOVED AND REPLACED WITH NEW SUPPORT STRAP ON DADO PNL 272SRW IAW SRM 51-42-06 AND SRM 51-40-11.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 23,114 hrs · 15,916 cycles
E&E BAY STA. 364 STR 26R CORROSION. REMOVED CORROSION 100% MAT LOSS IAW SRM 53-21-03 REMOVED & REPLACED STR 26R STA 332 TO STA 364 IAW SRM 51-42-06 & SRM 51-42-21.
Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 23,114 hrs · 15,916 cycles
AFT BAGGAGE BAY FLOOR STRUCTURE LBL9 HAS CORROSION AT FS1031.00. REPAIRED LBL9 FLOORBEAM AT STATION 1031.00 IAW REO 670-53-00-029.
Part: PANEL — CHAFED (PYLON) · airframe 23,114 hrs · 15,916 cycles
FAIRING PANEL 433 BB HAS CHAIFING AND CRACKED DOUBLER AT END OF PANEL (PR). REMOVED AND REPLACED FAIRING PANEL IAW SRM 51-42-06 AND 51-42-13.
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 23,114 hrs · 15,916 cycles
AFT BAGGAGE BAY FLOOR STRUCTURE LBL27 HAS CORROSION FROM FS1015.00 TO 1051.30. REPAIRED DAMAGED LBL27 FLOORBEAM IN CARGO HOLD AT FS1000 TO FS1051 (APPROX SIZE) IAW GREO 670-53-00-029 REVA FIG13.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 23,114 hrs · 15,916 cycles
AFT ATG ANTENNA EXTERNAL DOUBLER HAS LIGHT PITTING CORROSION AND TOOL MARKS. REPAIRED AFT ATG ANTENNA EXTERNAL DOUBLER IAW EA DV3689-MSN15228 REV B DATED 25 JUNE 2018. AFT ATG ANTENNA REMOVED/INSTALLED ON WORK ORDER ZONE ITEM 1015804/1000/0056 SN6355066.
Part: RETAINER — CRACKED (PAX DOOR) · airframe 23,114 hrs · 15,916 cycles
UPON REMOVAL OF THE PAX DOOR LOWER STEP FOUND THE SEAL RETAINER CRACKED. RECEIVED NEW SEAL RETAINER LOCATED & DRILLED IAW SRM 51-40-11.
Part: FIRESHIELD — CRACKED (CARGO DOOR) · airframe 23,114 hrs · 15,916 cycles
FWD CARGO DOOR UPPER FIRE SHIELD CRACKED FWD CORNER. REMOVED AND REPLACED FWD CARGO DOOR UPPER FIRE SHIELD FWD CORNER IAW SRM 51-42-06.
Part: SENSOR — OUT OF ADJUST (NLG CENTERING) · airframe 22,763 hrs · 15,656 cycles
GEAR DISAGREE IN THE UP POSTION AFTER TAKE OFF. ADJUSTED THE NLG CENTERING POSITION SENSOR IAW AMM 32-61-05. PERFORMED FUNCTIONAL CHECK OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM IAW AMM 32-30-00. OPS CHECKED GOOD AND NO MESSAGE POSTED.
Part: HARNESS — BROKEN (OXYGEN MASK) · airframe 22,359 hrs · 15,377 cycles
FIRST OFFICER`S EMERGENCY OXYGEN MASK HARNESS IS BROKEN. R & R THE FIRST OFFICER`S OXYGEN MASK AND SERVICED THE CREW OXYGEN BOTTLE IAW AMM 35-11-12. OPS CHECKED GOOD, ACFT OK FOR SERVICE.
2017
Part: POST — CORRODED (FUSELAGE) · airframe 21,620 hrs · 14,852 cycles
VERTICAL POST AT FS280 STRINGER 25R IS CORRODED. REPAIRED CORROSION DAMAGE TO VERTICAL POST FS280 STR25R PER EA CRJ953-06135.
Part: SKIN — CORRODED (FUSELAGE) · airframe 21,620 hrs · 14,852 cycles
FOUND CORROSION ON LOWER FUSELAGE SKIN BETWEEN FS280-FS295 S26R-25R. REPAIRED CORROSION DAMAGE TO FUSE. SKIN FS280-FS295 STR 26R-25R PER EA CRJ953-06132.
Part: POST — CORRODED (FUSELAGE) · airframe 21,620 hrs · 14,852 cycles
VERTICAL POST AT FS280 STRINGER 25R IS CORRODED. REPAIRED CORROSION DAMAGE TO VERTICAL POST FS280 STR25R PER EA CRJ953-06135.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 21,620 hrs · 14,852 cycles
STRINGER 25R IS CORRODED BETWEEN FS 280-295. STRINGER 25R CORRODED OUT OF LIMITS, REMOVED AND REPLACED STRINGER IAW SRM 51-42-06.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 21,620 hrs · 14,852 cycles
STRINGER 26R IS CORRODED BETWEEN FS280-295. REMOVED CORRODED STRINGER AND SPLICE 26R AND INSTALLED NEW STRINGER IAW SRM 51-42-06.
Part: HOOK AND LOOP — WORN (EMERGENCY EXIT) · airframe 21,119 hrs · 14,480 cycles
ALL 4 EMERGENCY EXIT ROW COVERED NEED TO BE SECURED. REPLACED HOOK AND LOOP ON ALL FOUR EMERGENCY EXIT DOOR HANDLE COVERS PER AMM 51-22-61.
2016
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 18,924 hrs · 12,980 cycles
MEGAPHONE INOPERATIVE. REMOVED AND REPLACED THE MEGAPHONE IAW AMM 25-61-14.
Part: SKIN — DENTED (BS 265-280) · airframe 18,164 hrs · 12,438 cycles
DENT ON BOTTOM OF AIRCRAFT, 3 FT BEHIND NOSE GEAR, RT SIDE. STRIPPED PAINT FROM DAMAGE AREA, FOUND DAMAGE TO CONSIST OF DENT IF FUSELAGE SKIN WITH A GOUGE INSIDE THE DENT LOCATED BETWEEN FS 265 AND FS 280 BETWEEN STR 24R AND STR 25R. DENT MEASURES APPROXIMATELY .091" D X 4.2" L X 3.2" W, BLENDED GOUGE MEASURES APPROXIMATELY .005" D X .800" L X 1.3" W. DAMAGE FOUND TO BE OUT OF LIMITS REF SRM 53-11-01. COMPLIED WITH TEMP DISPOSITION EA 32-2016-065. THIS CONDITION IS ACCEPTABLE AS IS FOR 2405 FLT HRS WITH REINSPECT EVERY 200 FLT HRS. THIS IS CLASSIFIED AS A MAJOR REPAIR.
2015
Part: FLASHLIGHT — FAILED (COCKPIT) · airframe 17,271 hrs · 11,832 cycles
CAPT'S FLASHLIGHT IS INOPERATIVE. R & R CAPT FLASHLIGHT. OPS CHECK GOOD IAW AMM 25-61-00. NO DEFECTS NOTED.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,519 hrs · 10,634 cycles
AFT CABIN EXIT LIGHT INOPERATIVE. REPLACED EPSU BATTERY PACK IAW AM 33-51-17 AND AIPC REF 33-51-17, FIG 1, ITEM 6 NO HELP.[REPAIRS MADE UNDER DEFECT A135265: R & R EMERGENCY POWER SUPPLY AND CHARGER/BATTER IAW AMM 33-51-17. BATTERY PACK AT NR 3 POSITION. IPC REF 33-51-17, ITEM 8 AND 6A. OPS CK CHECK GOOD.
Part: SEAT TRACK — CORRODED (BS 661-667) · airframe 15,481 hrs · 10,611 cycles
RIGHT SIDE SEAT TRACK AT FS 661.00 +16 - 667.40 HAS CORROSION. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. REMOVED SIDE SEAT RAIL AT FS661.00+16 669.40 IAW AMM 53-00-49-00-801-A01. INSTALLED SIDE SEAT RAIL RT AT FS661.00+16-669.40 IAW AMM 53-00-400-801-A01.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 15,481 hrs · 10,611 cycles
LEFT SIDE SEAT TRACK AT FS 785.15-847.00+8.40 HAS CORROSION. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801-A11. INSTALLED SIDE SEAT RAIL AT FS 785.15 TO 847.00+8.40 IAW AMM 53-00-49-400-801 -A11.
Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 15,481 hrs · 10,611 cycles
LEFT SEAT TRACK AT FS 661-693 HAS CORROSION. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-000-343, REV J AS WRITTEN. REMOVED SEAT RAIL AT FS 661-693, LBL9 IAW AMM 53-00-49-000-801, SEAT RAIL EXFOLIATED 100 PERCENT MATERIAL LOSS, OUT OF LIMITS. INSTALLED SERVICEABLE SEAT TRACK OF LBL9 AT FS 661-693 IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 15,481 hrs · 10,611 cycles
RIGHT SEAT TRACK AT FS 661-693 HAS CORROSION. REMOVED 0.012" CORROSION FROM SEAT TRACK AT BS UE. FOUND TO BE OUT OF LIMITS IAW SRM SUPPLEMENT 53-41-49. R & R SEAT RAIL IAW AMM 53-00-49-000-801-A11 & 53-00-49-400-801-A11. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801-A11. INSTALLED SEAT RAIL IAW AMM 53-00-49-400-801-A11. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 477-581) · airframe 15,481 hrs · 10,611 cycles
LEFT SEAT TRACK AT FS 477-581 HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM SUPPLEMENT 53-41-49. FABBED LT SEAT TRACK AT FS 477-581, COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00343, REV J, AS WRITTEN. REMOVED SEAT TRACK FROM LBL 9, FS 477-581 IAW AMM 53-00-49-000-801. INSTALLED SERVICEABLE LT SEAT TRACK AT FS 477-581 IAW AMM 53-00-49-400-801 A11.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 15,481 hrs · 10,611 cycles
RIGHT SEAT TRACK AT FS 581-661 HAS CORROSION. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. REMOVED SEAT RAIL AT FS 581-661 IAW AMM 53-00-49-00-801 A11. INSTALLED SEAT TRACK AT FS 581-661-RBL9 IAW AMM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 15,481 hrs · 10,611 cycles
LEFT SEAT TRACK AT BS 581-661 HAS CORROSION. FABBED LT SEAT TRACK AT FS 581-561. COMPLIED WITH ECTC REO 670-53-000-343 AND GREO 670-53-000-343, REV J AS WRITTEN. REMOVED SEAT TRACK FROM LBL-9 FS 581-661 IAW AMM 53-00-44-000-806 SEAT TRACK EXFOLIATED. FOUND TO BE OUT OF LIMITS. INSTALLED SERVICEABLE SEAT TRACK AT LBL 9, FS 581-661 IAW AMM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED (BS 669-720) · airframe 15,481 hrs · 10,611 cycles
RT SIDE SEAT TRACK AT F/S 669.40-720.85 HAS CORROSION. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. REMOVED RT SIDE SEAT TRACK AT FS 669.40-720-85 IAW TASK 53-00-49-000-801-A11. INSTALLED SIDE SEAT TRACK AT FS 669.40-720.85 IAW TASK 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED (BS 477-581) · airframe 15,479 hrs · 10,610 cycles
RIGHT SEAT TRACK AT BS 477-581 HAS CORROSION. FABRICATED SEAT TRACK AT RBL 9, FS 477-581, COMPLIED WITH EC/TC REO 670-53-000-343, AND GREO 670-53-000-343. REMOVED SEAT TRACK AT RBL9, FS 477-581. INSTALLED SERVICABLE SEAT TRACK AT RBL 9, FS. 477-581 IAW AMM 5300-49-400-201-A01.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 15,481 hrs · 10,611 cycles
RIGHT SIDE SEAT TRACK AT FS 785.15-847.00+8.40 HAS CORROSION. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. REMOVED RT SIDE WALL SEAT TRACK AT FS 785.15-847.00+8.40 IAW AMM 53-00-49-000-801-A11 AND INSTALLED IAW AMM 53-00-49-801.
Part: SEAT TRACK — CORRODED (BS 669-720) · airframe 15,481 hrs · 10,611 cycles
LEFT SIDE SEAT TRACK AT F/S 669.40-720.85 HAS CORROSION. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. REMOVED SIDE SEAT RAIL LT FS 669.40-720.85 IAW AMM 53-00-49-00-801-A11. INSTALLED SIDE SEAT RAIL LT FS 699.40-720.85 IAW AMM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 15,481 hrs · 10,611 cycles
LEFT SIDE SEAT TRACK AT F/S 744.15-761-85 HAS CORROSION. COMPLIED WITH SIGNOFF STATEMENT, COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. REMOVED IAW AMM 53-00-49-000-801, CONFIG A11. INSTALLED NEW SERVICEABLE SEAT RAIL IAW SRM 51-41-02-001-001 DWG SH690-36-285 AND AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 15,481 hrs · 10,611 cycles
RIGHT SIDE SEAT TRACK AT F/S 744.15-761.85 HAS CORROSION. COMPLIED WITH SIGNOFF STATEMENT: COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343 REV J AS WRITTEN. NEW SERVICABLE SEAT RAIL FABRICATED IAW AMM 53-00-49-400-801, CONFIG A11. INSTALLED NEW SERIVCBALE SEAT RAIL AT FS744-761 RT IAW AMM 53-00-49-400-801, CONFIG A11 AND DWG SH690-36285. REMOVED CORRODED SEAT RAIL -SIDE RT FS744.15-761.85 IAW AMM 53-00-49-00-801.
Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 15,479 hrs · 10,610 cycles
SEAT TRACK AT F/S 379-485 LBL 9 HAS CORROSION. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. CORROSION EXCEEDS THE ALLOWABLE DAMAGE LIMITS OF SRM 53-21-49-101-001-A01. REMOVED CORRODED SEAT TRACK REF: AMM 53-00-49-000-803-A11. INSTALLED SERVICEABLE SEAT TRACK AT FS 379-485 LBL9 REF: AMM 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED (BS 847-1000) · airframe 15,479 hrs · 10,610 cycles
FLOOR SEAT RAIL FS 847.0+16-FS 1000.0, RBL 9 HAS CORROSION DAMAGE. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J. REMOVED FLOOR SEAT RAIL FS 847+16, FS 1000 RBL 9 IAW AMM 53-00-49-000-801, A11, DUE TO BEING CORRODED OUT OF LIMITS. INSTALLED NEW SEAT RAIL AT FS 847.0 + 16-FS 1000.0 RBL 9 IAW AMM 53-00-49-400-801. REMOVED CORROSION FROM SEAT RAIL FS 847.0+16 FS 1000 IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. FABRICATED NEW SEAT RAIL FOR FS 847.0+16-FS 1000 RBL9 IAW EC/TC REO 670-53-000-343.
Part: SEAT TRACK — CORRODED (BS 847-1000) · airframe 15,479 hrs · 10,610 cycles
SEAT TRACK BS 847+16- 1000, LBL 9 HAS CORROSION DAMAGE. FABRICATED A NEW SEAT TRACK, COMPLIED WITH EC/TC REO 670-53-00-343- & GREO 670-53-00-343- REV J . REMOVED SEAT TRACK IAS AMM 53-00-49-001-801. INSTALLED SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801-A11.
Part: FLOOR SUPPORT — CORRODED (BS 280-310) · airframe 15,479 hrs · 10,610 cycles
RT FLOOR SILL CORRODED FROM FS280-FS310 IN NUTPLATE AREAS. REMOVED RT FLOOR SILL BS 280-310 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01. DRILLED UP NEW RT FLOOR SILL IAW SRM 51-40-11-001-001-A01 & DWG SH670-32172-11, REV E. STARTED THE INSTALLATION OF RT FLOOR SILL IAW SRM 51-42-06-000-001-A01 & DWG SH670-32172-11, REV E. FINISHED INSTALLING FLOOR SILL RT IAW SRM 51-42-06-0009001-A01 & DWG SH670-32172-11, REV E.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,467 hrs · 10,603 cycles
FS280.00, RT SIDE FLOORBEAM CORRODED. REMOVED RT 280 CROSBEAM IAW SRM 51-42-06-001-001. INSTALLED NEW RT 280 CROSSBEAM IAW SRM 51-42-06-001-001 AND SRM 51-42-13-001-001 IAW DWG CC670-34010.
Part: FRAME — CORRODED (BS 295) · airframe 15,471 hrs · 10,605 cycles
CORROSION ON AFT SIDE OF FS295 BETWEEN STR 27-26R. 2 PLACES, BLENDED CORROSION ON AFT SIDE OF FS 295 AT STR 27-26R IAW SRM 51-21-06-001-001-A01. BLEND AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 53-21-06-101-002-A01. REPAIRED FRAME STA 295 IAW REO 670-53-021-799 BY COMPLYING WITH ECTC REO 670-53-21-799. FABRICATION OF FRAME SPLICES/SECTOR AT FS 295.
Part: ANGLE — CORRODED (DOOR SILL) · airframe 15,479 hrs · 10,610 cycles
PASSENGER DOOR SILL ANGLE CORRODED. CAP ANGLE AND LOWER SILL ANGLE CORRODED BEYOND LIMITS IAW SRM 53-21-23-101-001-A02. R & R CAP ANGLE AND LOWER SILL ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. REMOVED CAP ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND INSTALLED CAP ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 DWG 54670-31825. REMOVED LOWER SILL IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND INSTALLED LOWER SILL ANGLE IAW SRM 51-40-11-001-001-A01 AND 57-42-06-001-001-A01 DWG 54670-31875.
Part: ANGLE — CORRODED (DOOR SILL) · airframe 15,479 hrs · 10,610 cycles
SERIVCE DOOR SILL ANGLE CORRODED. CORROISON WAS FOUND OUT OF LIMITS IAW SRM 51-21-23-101-002-A01. REMOVED UPPER AND LOWER SILL ANGLES AND CLIP FROM SERVICE DOOR IAW SRM 51-42-00-001-001-A01. LOCATED, DRILLED AND ASSEMBLIED SERVICE DOOR SILL ANGLES AND CLIP IAW SRM 51-42-06-001-001-A01 AND DWG SH690-319.06 AND SH670-31996. INSTALLED SERIVCE DOOR ANGLES AND CLIP IAW SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01 AND DWG SH690-31986 AMD SH670-31996.
Part: FLOORBEAM — CRACKED (BS 274) · airframe 15,467 hrs · 10,603 cycles
COCKPIT FLOORBEAM CRACKED AT FS 274.00, LBL 12, RECEIVED SRM 51-24-16-001-001-A01. COMPLIED WITH SRM 51-11-11-001-001-A01. RECEIVED AND COMPLIED WITH EC/TC REO 690-53-11-749.
Part: FLOORBEAM — CRACKED (BS 274) · airframe 15,467 hrs · 10,603 cycles
COCKPIT FLOORBEAM CRACKED AT FS 274.00, RBL 12. RECEIVED AND COMPLIED WITH SRM 51-24-16-001-001-A01. RECEIVED AND COMPLIED WITH EC/TC REO 690-53-11-749.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,467 hrs · 10,603 cycles
FS280.00, LT SIDE FLOORBEAM CORRODED. REMOVED LT 280 CROSBEAM IAW SRM 51-42-06-001-001. INSTALLED NEW 280 CROSBEAM LT SIDE IAW SRM 51-42-06-001-001 AND SRM 51-42-13-001-001 IAW DWG CC670-34010.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 15,471 hrs · 10,605 cycles
FS 280.00 BULKHEAD LOWER WEB LT SIDE CORRODED. WEB CORRODED BEYOND LIMITS AT FS280 LBL, WL72.50 IAW SRM 51-21-06-001-001-A01. COMPLIED WITH ECTC REO 670-53-11-594 AND GREO 670-53-11594, REV DATED: 04/27/2011. R & R STIFFERNER ANGLE AT LBL33 IAW SRM 51-42-06-001-001.
Part: STRUCTURE — CORRODED (BS 280-282) · airframe 15,471 hrs · 10,605 cycles
CIRCUMFERENTIAL JOINT FS280-282.86 CORRODED BETWEEN 26L-26R. BLENDED CORROSION AT FS280, STR 26L-26R IAW SRM 51-21-06-001-001-A01. NO DAMAGE LIMITS IN SRM FOR CIRCUMFERENTIAL JOINT AT FS 280.00. FOUND MORE CORROSION WHILE CLEANING, REMOVED 8 EA FASTENERS IAW SRM 51-42-06-001-001-A01. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.
Part: DOOR FRAME — CORRODED (COCKPIT) · airframe 15,467 hrs · 10,603 cycles
COCKPIT DOOR POST CORRODED AT LOWER SECTION FS280.00, LBL 11. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AT FS280/WL72.50/LBL11. RECEIVED STS EA 32-2015-100 AND REQUESTED EC/TC FROM EXPRESS JET. RECEIVED EC/TC EA 32-2015-100 AND COMPLIED WITH ALL STEPS OF EC/TC EA32-2015-100 PERMANENT REPAIR.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,467 hrs · 10,603 cycles
FS 280.00 COCKPIT FLOOR PANEL SUPPORT ANGLE ASSY CORRODED. REMOVED FS280 COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001. INSTALLED NEW FS280 COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001. LOCATED, DRILLED,AND INSTALLED LIGHT BRACKET ASSY IAW SRM 51-42-06-001-001.
Part: SEAT TRACK — CORRODED (BS 349) · airframe 15,479 hrs · 10,610 cycles
SEAT RAIL AT RBL9 FS349 CORRODED. CORRODED BEYOND LIMITS IAW SRM 53-21-49-101-001-A01. R & R SEAT RAIL ON RBL 9 AT FS 349 REF: REO 670-53-00-343, REV J REF: AMM 20-21-00-910-801-A01 53-00-49-000-801-A11 53-00-49-400-801-A11. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV J. R & R WITH NEW GALLEY MOUNT FITTINGS IN SEAT RAIL AT RBL9 FS 349-485 IAW AMM 53-00-49-400-801, CONFIG A11.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 15,471 hrs · 10,605 cycles
FS 280.00 BULKHEAD LOWER WEB RT SIDE CORRODED. WEB CORRODED BEYOND LIMITS AT FS280 RBL 12, WL72.50 IAW SRM 51-21-06-001-001-A01. COMPLIED WITH ECTC REO 670-53-11-594 01 AND GREO 670-53-11-594, REV , DATED: 04-27-2011. R & R 2EA STIFFENER ANGLES AT RBL 17.46 AND RBL 38.5 IAW SRM 51-42-06-001-001.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,471 hrs · 10,605 cycles
CRAWLWAY FLOOR SUPPORT ANGLE AFT SIDE OF FS280 CORRODED. BLENDED CORROSION AT FS 280 ON CRAWLWAY SUPPORT ANGLE IAW SRM 51-21-06-001-001-A01. CRAWLWAY FLOOR SUPPORT AT FS 280 IS CORRODED BEYOND LIMITS IAW SRM 51-21-06-001-001-A01. R & R FLOOR SUPPORT ANGLE AFT SIDE OF FS 280 IAW DWG CC670-34010, REV:J CRJ 900, SRM 51-42-21-001-001-A01 51-42-13-001-001-A01 51-42-06-001-001-A01 51-21-11-001-001-A01.
Part: SKIN — ERODED (UNKNOWN) · airframe 15,467 hrs · 10,603 cycles
PANEL 522 DB HAS SCREW HOLE DAMAGED AND L/E EDGE ERODED. REMOVED DAMAGE AT L/E EDGE AND AROUND SCREW HOLE, REF: SRM 51-12-00-001-001-AS01, TR 51-0050. RECEIVED AND COMPLIED WITH STS EA 32-2015-097. PERMANENT REPAIR. ALL STEPS COMPLETED. RECEIVED AND COMPLIED WITH ECTC EA 32-2015-097, DATED 03/16/15.
Part: SKIN — DAMAGED · airframe 15,467 hrs · 10,603 cycles
FUSELAGE SKIN DAMAGED BY POTABLE SERVICE WATER DOOR FWD SIDE. REMOVED DAMAGE AT FUSELAGE SKIN BY POTABLE SERIVCE WATER DOOR FWD SIDE, REF SRM 51-12-00-001-001-A01 TR 51-0050 BLEND LENGTH 2.00 BY 0.250" WIDE. COMPLIED WITH STS EA 32-2015-098 ALL STEPS COMPLETED-PERMANENT REPAIR. RECEIVED AND COMPLIED WITH ECTC32-2015-087.
Part: SKIN — DAMAGED · airframe 15,467 hrs · 10,603 cycles
FUSELAGE SKIN DAMAGED JUST BELOW POTABLE WATER SERVICE DOOR. REMOVED DAMAGE AT FUSELAGE SKIN JUST BELOW POTABLE WATER SERVICE DOOR REF SRM 51-12-00-001-0001-A01 TR51-0050 BLEND LENGTH 3.300" BY 0.800" WIDE. SUBMITTED TO ENGINEERING FOR PERMANAMENT DISPOSITION. COMPLIED WITH STS EA 32-2015-098 ALL STEPS COMPLETED-PERMANENT REPAIR. RECEIVED AND COMPLIED WITH ECTC EA32-2015-098.
Part: SKIN — DETERIORATED (LAV SERVICE DOOR) · airframe 15,467 hrs · 10,603 cycles
FS DAMAGED BY EWD LAV SERVICE DOOR, FWD. REMOVED DAMAGE AT FS BY FWD LAV SERVICE DOOR 2 EA LOCATIONS, FWD OF DOOR AND JUST BELOW DOOR, REF SRM 51-12-00-001-001-A01 TR 51-0050 BLEND LENGTH 2.200" BY 0.500", FWD OF DOOR, BLEND LENGTH 4.500" BY 0.300", JUST BELOW DOOR. SUBMITTED TO ENGINEERING FOR PERMANENT DISPOSITION. COMPLIED WITH STS EA 32-2015-098 ALL STEPS COMPLETED, PERMANENT REPAIR. RECEIVED AND COMPLIED WITH ECTC EA32-2015-098.
Part: SKIN — GOUGED (FUSELAGE) · airframe 15,481 hrs · 10,611 cycles
GOUGE RT SIDE FUSELAGE NEAR LOW PSI AIR CONDITION. COMPLIED WITH PERMANENT REPAIR ON GOUGE RT SIDE FUSELAGE IAW EC/TC EA 30-2014-005. REMOVED FINISH IAW SRM 51-26-00-001-001-A01. RESTORED EXTERNAL SURFACE PAINT, REPAIR AREA, IAW SRM TASK 51-25-01-001-001-A01. COMPLIED WITH EA 30-2014-005, SECTION III, PERMANENT REPAIR. RECEIVED EC/TC EA 30-2014-005 AND VERIFIED ALL STEPS HAVE BEEN COMPLETED.
Part: SKIN — GOUGED (FUSELAGE) · airframe 15,481 hrs · 10,611 cycles
FUSELAGE HAS 18" GOUGE BELOW RT ENGINE. COMPLIED WITH PERMANENT REPAIR OF 18" GOUGE BELOW RT ENGINE IAW EC/TC EA 30-2014-005. COMPLIED WITH EA 30-2014-005, SECTION III, PERMANENT REPAIR. RECEIVED EC/TC EA 30-2014-005 AND VERIFIED ALL STEPS HAVE BEEN COMPLETED.
2014
Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 13,661 hrs · 9,380 cycles
FWD CARGO BAY FWD DOOR SEAL RETAINER BENT AND MISSING MATERIAL AT AFT LWR CORNER. REPAIRED IAW REO 690-52-35-013, REV. A. MAJOR REPAIR IAW GMM 5-3.
Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 13,661 hrs · 9,380 cycles
FWD CARGO BAY FWD DOOR SEAL RETAINER BENT AT FWD LWR CORNER. COMPLIED WITH REO 690-52-35-013, REV A. MAJOR REPAIR IAW GMM 5-3.
Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 13,525 hrs · 9,291 cycles
LEFT FOWARD OVERWING EMERGENCY LIGHT COVER IS CRACKED. REPLACED COVER IAW VCMM 33-51-02. ACFT OK FOR SERVICE.
Part: RETAINER — BENT (CARGO DOOR SEAL) · airframe 13,525 hrs · 9,291 cycles
FWD CARGO BAY AFT DOOR SEAL RETAINER BENT INSIDE AND CRACKED ON THE OUTSIDE AT FWD LOWER CORNER. COMPLIED WITH EC/TC REO 680-52-35-013.
2013
Part: SKIN — BURNED (BS 295) · airframe 11,697 hrs · 8,146 cycles
1 BURN ON FASTENER AT FS 295 AND S25L. INSTALLED SOLID RIVET, SRM 51-42-06 AND REO 670-53-00-045, REV G, SECTION B2.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 11,555 hrs · 8,054 cycles
EMERGENCY BATTERY PACK 4 AND 5 FAILED. R & R EMERGENCY BATTERY PACK IAW AMM 33-51-17.
Part: LIGHT — MISSING (CABIN) · airframe 10,590 hrs · 7,468 cycles
EMERGENCY LIGHT STRIP IN GALLEY AREA MISSING. INSTALLED EMERGENCY LIGHT STRIP IN GALLEY IAW CRJ900 AMM 33-51-01. OK FOR SERVICE.
Part: STRIP — UNSECURE (CABIN) · airframe 10,582 hrs · 7,463 cycles
EMERGENCY FLOOR STRIPPING AT 13A NEEDS TO BE SECURED. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT STRIP PER CRJ900 AMM 33-51-01. OK FOR SERVICE.
Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 10,460 hrs · 7,379 cycles
SEAT 13C LIFE VEST HAS A HOLE IN THE PACKAGE. REMOVED AND REPLACED PASSENGER LIFE VEST AT 13C IAW AMM 25-61-03.
Part: STRIP — MISSING (CABIN) · airframe 10,391 hrs · 7,331 cycles
EMERGENCY FLOOR PATH MARKING IS MISSING AT EXIT ROW 12AB. INSTALLED EMERGENCY FLOOR STRIP AS REQUIRED IAW AMM 33-51-01.
Part: LIFE VEST — TORN (CABIN) · airframe 10,369 hrs · 7,315 cycles
AFT FLIGHT ATTENDANT LIFE VEST BAG TORN. REMOVED AND REPLACED AFT FLIGHT ATTENDANT LIFE VEST BAG IAW AMM 25-61-03.
Part: INDICATOR — TRIPPED (SLAT ACTUATOR) · airframe 9,985 hrs · 7,059 cycles
ON FLIGHT 3604 (ATL TO ALB) RECEIVED SLATS FAIL MESSAGE ON APPROACH INTO ALB. AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY. VERIFIED DISCREPANCY, FOUND RIGHT SLAT 3-1 ACTUATOR TRIP INDICATOR TRIPPED, RESET TRIP INDICATOR IAW CRJ900 AMM 27-81-09. PERFORMED OPS CHECK OF THE SLATS & FLAP SYSTEM IAW CRJ900 AMM 27-50-00. OPS TEST GOOD AT THIS TIME. RIGHT SLAT ACTUATOR AT TRACK 3-1 PER MOC AUTH # 01431 (R.E.). AIRCRAFT OK FOR SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 9,971 hrs · 7,051 cycles
ALL EMERGENCY LIGHTS INOPERABLE. RUN GPU TO CHARGE EMERGENCY BATTERY PACK. OPS CHECK GOOD IAW 33-51-00. AIRCRAFT OK FOR SERVICE.
2012
Part: EPSU — DEFECTIVE (CABIN) · airframe 9,507 hrs · 6,734 cycles
HEAVY CHECK FOUND MULTIPLE FORWARD EMERGENCY LIGHTS ARE WORKING INTERMITTENTLY. REMOVED AND INSTALLED EPSU NR 1 IAW CRJ900 AMM 33-57-17, OPS CHECKS GOOD IAW CRJ 900 AMM 33-51-17. (ORIGINAL CONTROL NUMBER REXA2012111501684 DUP DROPPED THE 4)
Part: STRUCTURE — CHAFED (RT WING) · airframe 9,502 hrs · 6,731 cycles
RIGHT INBOARD IS CHAFED SEVERAL AREAS BETWEEN SLAT TRACK 1-1 AND TRACK 1-3. REPAIRED IAW SRM 57-41-01.
Part: STRUCTURE — CRACKED (LT WING) · airframe 9,502 hrs · 6,731 cycles
LEFT INBOARD IS CHAFED SEVERAL AREAS BETWEEN SLAT TRACK 1-1 AND TRACK 1-3. REPAIRED IAW SRM 57-41-01.
Part: LIFE VEST — MISSING (SEAT 4A) · airframe 9,101 hrs · 6,409 cycles
PASSENGER SEAT LIFE VEST MISSING AT 4A. INSTALLED LIFEVEST.
Part: SKIN — DENTED (BS 897-613) · airframe 8,627 hrs · 6,059 cycles
MAINTENANCE FOUND DAMAGE TO THE FUSELAGE SKIN BETWEEN FS 597 AND 613 AND S-16-17L. DENT MEASURED 2.35 INCH BY 1.25 INCH WITH A GOUGE IN THE CENTER OF THE DENT MEASURING 0.055 INCH DEEP. REPAIRED IAW EA CRJ953-00684.
Part: MANIFOLD — DEFECTIVE (NLG STEERING) · airframe 7,714 hrs · 5,336 cycles
STEERING INOP (ABORTED TAKEOFF 80 KNTS). REMOVED AND REPLACED NOSE STEERING MANIFOLD ASSY IAW AMM 32-51-50. OPS AND LEAK CHECK GOOD. A/C DOES NOT MEET REQUIREMENTS FOR HIGH ENERGY STOP (HES) / REJECTED TAKEOFF (RTO) PER TCI CHAPTER 4 PAGE 6 SECTION M. OK FOR SERVICE.
Part: GLOWSTRIP — BROKEN (CABIN) · airframe 7,712 hrs · 5,334 cycles
GLOW STRIP ON EXIT ROW CA SIDE HAS BROKE OFF FLOORBOARD. REPLACED GLOW STRIPP AT ROW 12 A&B (EXIT ROW) PER AMM 33-51-01. OK FOR SERVICE.
Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 7,696 hrs · 5,324 cycles
ABORTED TAKEOFF FOR STEERING INOPERATIVE CAUTION AT 95 KTS DURING TAKE OFF ROLL. PERFORMED OPS CHECK OF NOSE STEERING SYSTEM ON GROUND AND HIGH SPEED TAXI (100 KTS) WITH CREW. OPS CHECKED GOOD. NO DEFECTS NOTED. OK FOR SERVICE PER AMM 32-51-00.
Part: BLADE — LACK OF LUBE (RT ENGINE) · airframe 7,657 hrs · 5,301 cycles
UNSCHEDULED LANDING FOR R ENGINE FAN VIBE 1.8 IN AMBER CAUTION RANGE AT FL 300. RAN QRH. BROUGHT IT BACK TO NORMAL WITH THRUST MANAGEMENT. PERFORMED FAN BLADE TANG LUBE ON RT ENGING IAW AMM 72-21-02. OP CHECK GOOD.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 7,392 hrs · 5,149 cycles
EXIT SIGN LIGHT IN MIDDLE OF CABIN DOESN'T EXTINGUISH. RESET POWER. OPS CHECK GOOD PER CRJ900 AMM 33-51-09. OK FOR SVC.
2011
Part: COMPUTER — MALFUNCTIONED (FUEL SYSTEM) · airframe 6,605 hrs · 4,589 cycles
XFLOW PUMP CAUTION MESSAGE RESET FQG COMPUTER, OPS CHECK GOOD IAW CRJ 900 AMM 28-13-00. OK FOR SERVICE.
Part: UNKNOWN — SMOKE (CABIN) · airframe 5,618 hrs · 3,949 cycles
SMOKE LAV MSG AFTER BOARDING & SMOKE IN THE CABIN MOC B/B.
2010
Part: UNKNOWN — OUT OF RIG (NLG) · airframe 3,712 hrs · 2,715 cycles
NOSE LANDING GEAR DISAGREE MASTER WARNING MESSAGE AFTER TAKEOFF. FOUND PX 22 OUT OF LIMITS; RE-RIGGED PX 22 IAW 32-61-05 SEE AML 342483 DISC NR 2 FOR OPS CHECK.