N138EV
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.
186 reports on file, 2010-08-07 – 2026-05-05.
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 37,274 hrs · 27,158 cycles
EXTERIOR SERVICE DOOR EMERGENCY LIGHT OUT. R/R EXTERIOR SERVICE DOOR EMERGENCY LIGHT BULB IN REFERENCE TO AMM 33-51-15. PN ON/OFF: 8GH002473-08
Part: FAIRING — CRACKED (THRUST REVERSER) · airframe 37,253 hrs · 27,140 cycles
CRACK ON LINE LOWER FAIRING BTW LOWER TRANSCOWL AND PYLON AT LH ENGINE LINE LOWER FAIRING BTW LOWER TRANSCOWL AND PYLON AT LH ENGINE WAS FABRICATED AND REPLACED PER EA NO. CRJ954-22055 REV.A AND CRJ-900 AMM 54-12-01
Part: LANDING — CRACKED (ZONE 100) · airframe 37,253 hrs · 27,140 cycles
CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCES DOOR 212AR. RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCES DOOR 212AR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01
Part: ANGLE — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
CORROSION ON ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-41-02-001-001-A01
Part: ANGLE — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
CORROSION ON ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-41-02-001-001-A01
Part: ANGLE — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
CORROSION ON ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-41-02-001-001-A01
Part: ANGLE — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
CORROSION ON LOWER SILL ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. CORROSION ON LOWER SILL ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 THEREFORE WAS REPLACED PER CRJ-900 AMM 53-21-27-000-802, SRM 51-42-06-001-001-A01, SRM 51 -42-21-001-001-A01
Part: ANGLE — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
CORROSION ON ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR ANGLE MIC CAP AND ANGLE KICKPLATE AT SURROUND STRUCTURE OF PASSENGER DOOR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-41-02-001-001-A01
Part: ANGLE — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
CORROSION ON LOWER SILL ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR. CORROSION ON LOWER SILL ANGLE AND MOUNTING ANGLE AT SURROUND STRUCTURE OF GALLEY SERVICE DOOR WAS REMOVED PER SRM 51-21-06-001-001-A01 EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02 THEREFORE WAS REPLACED PER CRJ-900 AMM 53-21-27-000-802, SRM 51-42-06-001-001-A01, SRM 51 -42-21-001-001-A01
Part: PLATE — BENT (ZONE 100) · airframe 37,253 hrs · 27,140 cycles
WEAR AND BENT IN LOWER PLATE AND SEAL RETAINER OF FWD/CTR BAGGAGE-BAY CARGO DOOR LOWER PLATE (2 EA) ON FWD/CTR BAGGAGE-BAY CARGO DOOR WERE REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01
Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 37,253 hrs · 27,140 cycles
CRACK ON SUPPORT ANGLE OF COMMUNICATION/SERVICE PANEL BOX AT FWD FUSELAGE SUPPORT ANGLE OF COMMUNICATION/SERVICE PANEL BOX AT FWD FUSELAGE WAS FABRICATED AND INSTALLED PER EA CRJ953-21779 REV. IR AND SRM 51-42-06-001-001-A01
Part: CHANNEL — CORRODED (ZONE 100) · airframe 37,253 hrs · 27,140 cycles
CORROSION ON INTERNAL CHANNEL AT AREA OF AFT DRAIN MAST (FS1031.00 TO FS 1051.30 BTW STGR 27 TO 26RH) INTERNAL CHANNEL AT AREA OF AFT DRAIN MAST (FS1031.00 TO FS 1051.30 BTW STGR 27 TO 26RH) WAS REPAIRED PER EA NO: CRJ953-21943 REV. A
Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
AFTER RH CROSSBEAM REMOVAL, CRACK ON ANGLE RBL26.00 & LBL26.00 FS280.00 WAS FOUND AT FWD FACE OF THE BULKHEAD FS280.00, BELOW FLOOR ANGLE RBL26.00 & LBL26.00 FS280.00 AT FWD FACE OF THE BULKHEAD FS280.00, BELOW FLOOR WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
AFTER RH CROSSBEAM REMOVAL, CRACK ON ANGLE RBL26.00 & LBL26.00 FS280.00 WAS FOUND AT FWD FACE OF THE BULKHEAD FS280.00, BELOW FLOOR ANGLE RBL26.00 & LBL26.00 FS280.00 AT FWD FACE OF THE BULKHEAD FS280.00, BELOW FLOOR WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
Part: CHANNEL — DAMAGED (ZONE 100) · airframe 37,253 hrs · 27,140 cycles
ELONGATED HOLE ON UP CHANNEL AT LH MLG WHEEL WELL UP CHANNEL AT LH MLG WHEEL WELL WAS REPLACED PER CRJ 900 SRM 51-41-21-001-001-A01
Part: FITTING — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
CORROSION ON ATTACHMENT FITTING OF GALLEY 1 WAS FOUND. FITTING OF GALLEY 1 WAS REPLACED PER CRJ/900 SRM 51-42-21-001-001-A01
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
CORROSION ON CROSSBEAM LH AT FS 280.00 CROSSBEAM LH AT FS 280.00 WAS REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01
Part: BRACKET — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
AFTER LOWER SIL REMOVAL, CORROSION ON PROTECTOR WEB FLOOR 4(EAS) WAS FOUND. PROTECTOR WEB FLOOR 1(EA) WAS CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND 3(EAS) WERE EVALUATED DUE TO EXCESIVE CORROSION, THEREFORE MUST BE REPLACE PER CRJ-900 SRM 53-00-00-101-001-A01
Part: BRACKET — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
AFTER LOWER SIL REMOVAL, CORROSION ON PROTECTOR WEB FLOOR 4(EAS) WAS FOUND. PROTECTOR WEB FLOOR 1(EA) WAS CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND 3(EAS) WERE EVALUATED DUE TO EXCESIVE CORROSION, THEREFORE MUST BE REPLACE PER CRJ-900 SRM 53-00-00-101-001-A01
Part: WEB — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
AFTER LOWER SIL REMOVAL, CORROSION ON PROTECTOR WEB FLOOR 4(EAS) WAS FOUND. PROTECTOR WEB FLOOR 1(EA) WAS CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND 3(EAS) WERE EVALUATED DUE TO EXCESIVE CORROSION, THEREFORE MUST BE REPLACE PER CRJ-900 SRM 53-00-00-101-001-A01
Part: FITTING — CORRODED (ZONE 800) · airframe 37,253 hrs · 27,140 cycles
AFTER DISCONNECT FWD HANDRAIL ACTUATOR ROD, CORROSION ON FWD FITTING WAS FOUND AT SURROUND STRUCTURE OF PASSENGER DOOR. FWD FITTING AT SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02, FITTING P/N SH670-31905-5 WAS VERIFIED PER CRJ 900 SRM 53-21-23-001-001-A01 AND MUST BE INSTALLED PER NRC 124
Part: SUPPORT BRACKET — CRACKED · airframe 37,253 hrs · 27,140 cycles
BROKEN SUPPORT BRACKET OF BONDING JUMPER AT FLAP MECHANISM. SUPPORT BRACKET OF BONDING JUMPER AT FLAP MECHANISM WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 & EA CRJ957-22035 REV. IR.
Part: BRACKET — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
"STUCK PRESS-TO-TEST INDICATOR LIGHT, CORROSION AT SUPPORT & CLIP OF AFT WASTE TANK (BTW STGR 24RH AND STGR 23RH, FS 959.00). (SM)"" AFT LAV WASTE LEVEL INDICATOR AND NEW BRACKET WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ-900 AMM 38-31-08-960-801-A01 "
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
CRACK RH FS 280.00 BEAM. RH FS 280.00 BEAM WAS REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01
Part: FITTING — CORRODED (ZONE 800) · airframe 37,253 hrs · 27,140 cycles
CORROSION WAS FOUND ON FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS) WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 & SRM 51-41-04-001-001-A01.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
CORROSION ON RH SEAT TRACK RBL9 BTW FS349 TO FS394 AT PAX CABIN FLOOR STRUCTURE RH SEAT RAIL RBL9 BTW FS349 TO FS394 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER CRJ900 AMM 53-00-49
Part: DOOR SILL — CORRODED (ZONE 100) · airframe 37,253 hrs · 27,140 cycles
CORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH. AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1047.00, BTW STGR 17LH AND STGR 18LH WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 & SRM 51-42-10-001-001-A01
Part: SUPPORT — CRACKED (ZONE 100) · airframe 37,253 hrs · 27,140 cycles
CRACK ON BIN SUPPORT MEMBRANES (2E/A) ON LBL34 AND RBL34 AT FWD FACE OF MLG WHEEL WELL. & CRACK ON ANGLE OF FAIRING SUPPORT 194AB ON BL0 AT MMLG WHEEL WELL. (3 EAS TOTAL). BIN SUPPORT MEMBRANES (2E/A) ON LBL34 AND RBL34 AT FWD FACE OF MLG WHEEL WELL. & ANGLE OF FAIRING SUPPORT 194AB ON BL0 AT MMLG WHEEL WELL. (3 EAS TOTAL) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01, SRM 51-42-06-001-001-A01
Part: SUPPORT — CRACKED (ZONE 100) · airframe 37,253 hrs · 27,140 cycles
CRACK ON BIN SUPPORT MEMBRANES (2E/A) ON LBL34 AND RBL34 AT FWD FACE OF MLG WHEEL WELL. & CRACK ON ANGLE OF FAIRING SUPPORT 194AB ON BL0 AT MMLG WHEEL WELL. (3 EAS TOTAL). BIN SUPPORT MEMBRANES (2E/A) ON LBL34 AND RBL34 AT FWD FACE OF MLG WHEEL WELL. & ANGLE OF FAIRING SUPPORT 194AB ON BL0 AT MMLG WHEEL WELL. (3 EAS TOTAL) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01, SRM 51-42-06-001-001-A01
Part: ANGLE — CRACKED (ZONE 100) · airframe 37,253 hrs · 27,140 cycles
CRACK ON BIN SUPPORT MEMBRANES (2E/A) ON LBL34 AND RBL34 AT FWD FACE OF MLG WHEEL WELL. & CRACK ON ANGLE OF FAIRING SUPPORT 194AB ON BL0 AT MMLG WHEEL WELL. (3 EAS TOTAL). BIN SUPPORT MEMBRANES (2E/A) ON LBL34 AND RBL34 AT FWD FACE OF MLG WHEEL WELL. & ANGLE OF FAIRING SUPPORT 194AB ON BL0 AT MMLG WHEEL WELL. (3 EAS TOTAL) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01, SRM 51-42-06-001-001-A01
Part: FITTING — CORRODED (ZONE 800) · airframe 37,253 hrs · 27,140 cycles
CORROSION WAS FOUND ON FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS) WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 & SRM 51-41-04-001-001-A01.
Part: FITTING — CORRODED (ZONE 800) · airframe 37,253 hrs · 27,140 cycles
CORROSION WAS FOUND ON FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS) WERE REPLACED PER SRM 51-42-21-001-001-A01 & SRM 51-41-04-001-001-A01.
Part: SUPPORT — CRACKED (ZONE 100) · airframe 37,253 hrs · 27,140 cycles
CRACK ON ALL CORNERS ON SUPPORT OF JB6 AT FWD ACCESORY COMPARMENT. SUPPORT OF JB6 AT FWD ACCESORY COMPARMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.
Part: FITTING — CORRODED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
CORROSION AT SPLICE DOUBLER, GALLEY SERVICE DOOR SURROUND STRUCTURE FS319.70 STGR 17. SPLICE DOUBLER ON GALLEY SERVICE DOOR SURROUND STRUCTURE FS319.70 STGR 17 WAS REPLACED PER SRM 51-42-21-001-001-A01.
Part: HINGE — CORRODED (ZONE 800) · airframe 37,253 hrs · 27,140 cycles
CORROSION WAS FOUND ON FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). FITTINGS LH/RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS) WERE REPLACED PER SRM 51-42-21-001-001-A01 & SRM 51-41-04-001-001-A01.
Part: RIB — CRACKED (ZONE 600) · airframe 37,253 hrs · 27,140 cycles
CRACK ON RIB LEADING EDGE SS57.16 RIB LEADING EDGE SS57.16 WAS REPAIRED PER REO 690-57-41-240 REV - -
Part: PROTECTOR — CRACKED (ZONE 800) · airframe 37,253 hrs · 27,140 cycles
CRACK ON HARNESS PROTECTOR AT FWD HINGE ARM OF FWD BAGGAGE BAY CARGO DOOR. FORWARD BAGGAGE-BAY DOOR HARNESS PROTECTOR WAS REPAIRED PER EA: CRJ952-21867 REV:IR
Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 37,253 hrs · 27,140 cycles
CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201- 001-A01
Part: DRAG ANGLE — CRACKED (ZONE 200) · airframe 37,253 hrs · 27,140 cycles
CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201- 001-A01
Part: DRAG ANGLE — CRACKED (ZOEN 200) · airframe 37,253 hrs · 27,140 cycles
CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. COMPLETE: LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM WAS REPAIRED PER SRM 55-31-00-201- 001-A01.
Part: BULB — BURNED OUT (ZONE 200) · airframe 36,930 hrs · 26,867 cycles
EMERGENCY FLOOD LIGHT AT PAX DOOR HAS BULB BURNT OUT R/R BULB OPC GOOD IAW CRJ900 AMM 33-51-00
Earlier reports · 2010–2025 · 145 reports
2025
Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 35,162 hrs · 25,452 cycles
ON TAKE OFF, SMOKE/ODOR IN COCKPIT & CABIN, EMERGENCY DECLARED, NO FIRE INDICATIONS, GO AROUND, RETURNED TO RDU. PERFORMED DRYOUT PROCEDURES IAW CRJ-900 AMM 72-00-00. SMELL EVENTUALLY WAS REMOVED FROM AC. NO FURTHER ANOMALIES NOTED.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 34,765 hrs · 25,129 cycles
LH AFT OVERWING EMERGENCY LIGHT OUT. R & R AT OVERWING EMERGENCY LIGHT HOUSING/BULB IAW AMM 33-51-15 OPS CHEC K GOOD. PNON/OFF:2LA006954-00 SNON:PT318617 SNOFF:GLSB364
2024
Part: LUG — CRACKED (ZONE 800) · airframe 34,496 hrs · 24,911 cycles
LH AFT EMERGENCY EXIT AFT LUG CRACKED COMPLIED WITH ENDEAVOR EA CRJ952-17972 REV IR 12/23/24
Part: VENT LINE — CORRODED (ZONE 600) · airframe 34,496 hrs · 24,911 cycles
R/H I/B FWD MAIN FUEL VENT TUBE HAS SPOTS OF CORROSION COMPLIED WITH ENDEAVOR AIR EA CRJ928-17903 REV IR DATED 12/14/2024. DTA FOR 6000FH UNTIL PERMANENT REPAIR.
Part: LUG — CRACKED (ZONE 800) · airframe 34,496 hrs · 24,911 cycles
LH FWD EMERGENCY EXIT AFT LUG CRACKED COMPLIED WITH ENDEAVOR EA CRJ952-17960 REV IR 12/17/2024
Part: LUG — CRACKED (ZONE 800) · airframe 34,496 hrs · 24,911 cycles
RH AFT EMERGENCY EXIT AFT LUG CRACKED COMPLIED WITH ENDEAVOR EA CRJ952-17961 REV IR 12/23/2024.
2022
Part: SEAT TRACK — NONE · airframe 30,028 hrs · 21,068 cycles
SEAT TRACK SCRATCHED AND PITTED FROM APPROX. FS581-693 LBL27 REPLACED.
Part: COVER — CRACKED · airframe 30,028 hrs · 21,068 cycles
PAX DOOR AFT CORNER HAS A CRACK@1 EA FASTENER HOLE REPLACED CORNER COVER
Part: BRACKET — CRACKED · airframe 30,028 hrs · 21,068 cycles
PASSENGER DOOR INTERNAL STRUCTURE AFT GAS SPRING BRACKET TAB CRACKED ORDER AND REPLACE BRACKET-BUMP AS REQUIRE
Part: NONE — CORRODED · airframe 30,028 hrs · 21,068 cycles
PASSENGER DOOR INTERNAL STRUCTURE FWD WEB AT TOP STEP CORRODED. REMOVED AND REPLACED PASSENGER DOOR INTERNAL STRUCTURE FWD WEB AT TOP STGR CORRODED. REF CRJ900 SRM 51-42-06-001-001-A01
Part: STIFFENER — CRACKED · airframe 30,028 hrs · 21,068 cycles
PAX DOOR HAS CRACK ON STIFFENER ATTACHED TO AFT WEB (STIFFENER FOR MOUNTING DOOR ASSIST MOTOR) ORDER AND REPLACE STIFFENER
Part: ANGLE — CRACKED · airframe 30,028 hrs · 21,068 cycles
PAX DOOR AFT DRAG ANGLE IS CRACKED REPLACED ANGLE
Part: NONE — CRACKED · airframe 30,028 hrs · 21,068 cycles
STAIR ASSY PAX DOOR HAS CRACK REPLACED TOP STAIR ASSY
Part: BRACKET — CORRODED · airframe 30,028 hrs · 21,068 cycles
CORROSION ON FWD CARGO MACHINED BRACKET FWD OF FS517.00 BETWEEN STGR 22L-23L REPLACED MACHINED BRACKET.
Part: INTERCOSTAL — CORRODED · airframe 30,028 hrs · 21,068 cycles
PASSENGER DOOR INTERNAL STRUCTURE MID DD6 INTERCOSTAL CORRODED REPLACED INTERCOSTAL PAX DOOR MID DD6
Part: SEAT TRACK — NONE · airframe 30,028 hrs · 21,068 cycles
SEAT TRACK SCRATCHED AND PITTED FROM APPROX. FS485.00 TO FS581.00/LBL9 REMOVED AND INSTALLED NEW SEAT TRACK
Part: SEAT TRACK — CRACKED · airframe 30,028 hrs · 21,068 cycles
SEAT TRACK SCRATCHED AND PITTED FROM APPROX. FS364 TO FS485.00/LBL27 REMOVED AND INSTALLED NEW SEAT TRACK
Part: SEAT TRACK — NONE · airframe 30,028 hrs · 21,068 cycles
SEAT TRACK SCRATCHED AND PITTED FROM APPROX FS581 TO FS693.00/LBL9 REMOVED AND INSTALLED NEW SEAT TRACK
Part: SEAT TRACK — CRACKED · airframe 30,028 hrs · 21,068 cycles
SEAT TRACK SCRATCHED AND PITTED FROM APPROX FS485.00 TO FS581.00/LBL27 REMOVED AND INSTALLED NEW SEAT TRACK
Part: INTERCOSTAL — CORRODED · airframe 30,028 hrs · 21,068 cycles
MAIN AVIONICS DOOR SURROUND STRUCTURE HAS CORROSION ON FWD RIGHT HAND I/B INTERCOSTAL AT FS364 REPLACED INTERCOSTAL
Part: NONE — CORRODED · airframe 30,028 hrs · 21,068 cycles
RH FLOOR SILL CORRODED AT FS319.70 REPLACED FLOOR SILL
Part: SEAT TRACK — NONE · airframe 30,028 hrs · 21,068 cycles
SEAT TRACK SCRATCHED AND PITTED FROM APPROX FS485.00 TO FS581.00/RBL9 REMOVED AND INSTALLED NEW SEAT TRACK
Part: INTERCOSTAL — CRACKED · airframe 30,028 hrs · 21,068 cycles
PAX DOOR INTERCOSTAL DD1 FS338.00-FS347.25 IS CRACKED REPLACED INTERCOSTAL
Part: ANGLE — CORRODED · airframe 30,028 hrs · 21,068 cycles
PAX DOOR ANGLE@DD7A FS327.763-FS338.963 IS CORRODED REPLACED ANGLE
Part: NONE — CORRODED · airframe 30,028 hrs · 21,068 cycles
RH FLOOR CORRODED AT FS 319.70 REPLACED FLOOR SILL
Part: CLEAT — CORRODED · airframe 30,028 hrs · 21,068 cycles
2 EA. CLEATS @DD7A FS327.763 AND FS338.963 ARE CORRODED REPLACE 2 EA CLEATS
Part: FORMER — CORRODED · airframe 30,028 hrs · 21,068 cycles
PASSENGER DOOR INTERNAL STRUCTURE FWD FORMER BETWEEN DD6 AND DD5 IS CORRODED REPLACED FORMER FWD BETWEEN DD6 AND DD5
Part: BRACKET — CORRODED · airframe 30,028 hrs · 21,068 cycles
BRACKET @ INTERCOSTAL DD6 FS311.75 IS CORRODED. REPLACED BRACKET
Part: BRACKET — CORRODED · airframe 30,028 hrs · 21,068 cycles
CORROSION ON CENTER CARGO MACHINED BRACKET AFT OF FS661.00+16 BETWEEN STGR 22L-23L REMOVED AND REPLACED CENTER CARGO MACHINED BRACKET (P/N SH670-33390-2) REF CRJ900 SRM 51-42-06-001-001 AND CRJ SRM 51-42-21-001-001-A01
Part: INTERCOSTAL — CORRODED · airframe 30,028 hrs · 21,068 cycles
MAIN AVIONICS DOOR SURROUND STRUCTURE HAS CORROSION ON FWD LEFT HAND I/B INTERCOSTAL AT FS364 FOUND TO BE OUT OF LIMITS. REPLACED WITH NEW.
Part: NONE — CORRODED · airframe 30,028 hrs · 21,068 cycles
WHILE CONDUCTING INSPECTION IN THE AREA FOUND CORROSION ON RH SIDE SEAT RAIL CHANNEL JUST AFT OF RH AFT OVER-WING EXIT REPLACED SEAT RAIL
Part: SUPPORT — CORRODED · airframe 30,028 hrs · 21,068 cycles
THE FWD JACK FITTING LH SUPPORT HAS CORROSION ON THE OUTBD AFT SIDE REPLACED INTERCOSTAL JACK FITTING SUPPORT PER CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01
Part: ANGLE — CORRODED · airframe 30,028 hrs · 21,068 cycles
LEFT WING INTERNAL REAR SPAR TO AUXILIARY SPAR ACCESS PANEL MOUNT FLANGE BELOW FQGC CONNECTOR IS CORRODED REPLACED PART
2021
Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 27,955 hrs · 19,266 cycles
FOUND LT FWD EMERGENCY OVERWING LIGHT OUT. FOUND LIGHT ASSEMBLY HAD A BROKEN PIN OFF OF WIRE. R & R EMERGGENCY EXT LIGHT ASSEMBLY PN OFF/ON: 2LA006954-00, IAW AMM 33-51-15. OPERATIONS CHECKED GOOD.
2020
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 27,588 hrs · 18,963 cycles
FWD GALLEY EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT LOCATION PS35, IAW CRJ-900 AMM 33-51-17. OPERATIONS CHECK GOOD AT THIS TIME.
Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 27,359 hrs · 18,775 cycles
PS 37 BATTERY CHARGER ASSY NOT CHARGING. R & R PS 37 EPSU BATTERY CHARGER, IAW AMM 33-51-17. OPS CHECKS GOOD, IAW AMM 33-51-19 P/N ON AND OFF 11-0049 S/N ON 22686 S/N OFF 23858.
Part: LIGHT — BURNED OUT (EXTERIOR) · airframe 27,333 hrs · 18,749 cycles
RT EXTERIOR AFT PASSENGER EMERGENCY EXIT LIGHT INOP. REPLACED RT EXTERIOR AFT PASSENGER EMERGENCY EXIT LIGHT BULB, IAW CRJ 900 AMM 33-51-15. OPS CHECK GOOD.
2018
Part: FIRE GLOVES — MISSING (COCKPIT) · airframe 23,613 hrs · 15,905 cycles
COCKPIT FIRE GLOVES NOT IN BAG INSTALLED SERV FIRE GLOVE SAFETY GLOVES/DEVICE IAW CRJ AMM 25-60-00.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,546 hrs · 15,850 cycles
CORROSION ON SIDE SEAT RAILS STA FS669 TO FS977, STR 15L AND STR 15R AT CPAX (CPAX ). TCI (53-20-233). SIDE SEAT RAILS STA FS669 TO FS977, STR 15L AND STR 15R AT CPAX WERE REPLACE PER AMM 53-00-49-400-80 1 PAR 4(A)(B).
Part: BRACKET — CRACKED (RT WING) · airframe 23,546 hrs · 15,850 cycles
CRACK ON CANISTER, WELDED NR 3 RT STA WS148 AT MAIN FUEL TANK RT WING. CRACK ON CANISTER, WELDED NR 3 RT STA WS 148 AT MAIN FUEL TANK RT WING WAS REPAIRED PER REO 670-57-42-577 REV-.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,546 hrs · 15,850 cycles
CORROSION ON SEAT RAILS STA FS477 TO FS693 X=9 AND X=-9 (CPAX ).TCI (53-20-245). SEAT RAILS FS477 TO FS693 X=9 AND X=-9 WERE REPLACED PER SRM 51-41-02 AND AMM 53-00-49-400-801 PAR 4 (A) (B).
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,546 hrs · 15,850 cycles
CORROSION ON SEAT RAILS STA FS349 TO FS477 X=9 AND X=-9 AT CPAX (CPAX). TCI (53-20-243). CORROSION LEVEL 2 SEAT RAILS STA FS349 TO FS 477 X=9 AND X=-9 AT CPAX WERE REPLACED PER AMM 53-00-49 AND SRM 51-41-02.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,546 hrs · 15,850 cycles
CORROSION ON SIDE SEAT RAILS STA FS379 TO FS699, STR 15L AND STR 15R AT CPAX (CPAX ). TCI (53-20-217). SEAT RAILS ON STA FS379 TO FS699 , STR 15L AND STR 15R AT CPAX WERE REPLACE PER AMM 53-00-49-400-801 PAR 4(A)(B).
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,918 hrs · 15,391 cycles
LEFT NR 3 EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-15. OPS CHECKED GOOD.
Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 22,070 hrs · 14,785 cycles
DURING WAKE CHECK, NOTED THE AFT LAVATORY SMOKE DETECTOR CONTINUED TO SOUND. CYCLED CIRCUIT BREAKERS P1 & D9, PREFORMED AN OPS CHECK IAW AMM 23-16-00, OPS CHECKED GOOD.
2017
Part: SMOKE DETECTOR — NO TEST (FWD LAVATORY) · airframe 22,047 hrs · 14,768 cycles
FWD LAVATORY SMOKE ALARM WON`T TEST. REPLACED THE FWD LAVATORY SMOKE DETECTOR IAW AMM 26-16-01, OPS TESTED GOOD.
Part: SMOKE DETECTOR — MALFUNCTIONED (FWD LAVATORY) · airframe 22,020 hrs · 14,754 cycles
FWD LAVATORY SMOKE DETECTOR WILL NOT TEST. OPS CHECKED ADJUSTMENT FOR FWD LAVATORY SMOKE DETECTOR COMPLEDTED IAW AMM 26-10-00. OK FOR SERVICE.
Part: OXYGEN MASK — FAILED (COCKPIT) · airframe 24,429 hrs · 15,468 cycles
PILOT SIDE O2 MASK WILL NOT TEST. REMOVED/REPLACED PILOT SIDE O2 MASK IAW AMM 35-11-12. OPS CHECK IS GOOD. A/C OK FOR SVC.
Part: STEP — CRACKED (L1 DOOR) · airframe 21,676 hrs · 14,514 cycles
L1 DOOR, BOTTOM STEP IS CRACKED ON THE FWD EDGE. REMOVED AND REPLACED THE STEP IAW AMM 52-11-04-400-806.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 21,676 hrs · 14,514 cycles
FOUND EMERGENCY LIGHT WIRING AT PANEL 171CL, BELOW AFT LEFT EMERGENCY EXIT, TO BE BROKEN. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-15-000-801, AMM 33-51-15-400-801. OPS CHECKED GOOD IAW AMM 33-51-15-710-801.
Part: FAN — INOPERATIVE (GALLEY) · airframe 20,610 hrs · 13,725 cycles
CREW REPORTED SMELLING SMOKE IN THE GALLEY. MDC REPORTED FWD GALLEY FAN FAILED AT LOW SPEED. R & R GALLEY EXHAUST FAN, OPS CHECKED GOOD.
Part: RELAY — BURNED (EMERGENCY LIGHTS) · airframe 20,585 hrs · 13,701 cycles
PILOT REPORTED STRONG ELECTRICAL ODOR IN COCKPIT AFTER TAKEOFF, STRONGER A F180. .REMOVED AND REPLACED THE EMERGENCY LIGHT RELAY, OPS CHECKED GOO. ACFT WAS RETURNED TO SERVICE.
2016
Part: WIRE — BROKEN (MEGAPHONE) · airframe 18,466 hrs · 12,203 cycles
MEGAPHONE INOPERATIVE, FOUND BROKEN WIRE. R & R MEGAPHONE IAW AMM 25-61-14. REF IPC 25-61-14, FIG 1, ITEM 5.
Part: TERMINAL — DAMAGED (EMERGENCY LIGHT) · airframe 18,202 hrs · 12,014 cycles
CENTER EMERGENCY EXIT LIGHT ON LT SIDE UNDER EMERGENCY EXIT DOOR INOP. EMERGENCY LIGHTS, ALL ACFT NOT OPERATED AT NIGHT. REPAIRED BOTH WIRES BY INSTALLING NEW TERMINALS REF ESPM 20-16-05. OPS CHECK GOOD AT THIS TIME. THIS CLEARS DMIL A656045, 33-51-02.1 CAT C. PLACARD REMOVED.
2015
Part: MEGAPHONE — NOT REPORTED (CABIN) · airframe 17,377 hrs · 11,428 cycles
CABIN MEGAPHONE REQUIRES REPLACEMENT. R & R CABIN MEGAPHONE IAW AMM 25-61-14 AND REF 25-61-14.
Part: ACM — CONTAMINATED (RIGHT) · airframe 17,288 hrs · 11,365 cycles
SMOKE OR HAZE REPORTED IN CABIN BY FAS. COMPLIED WITH QRH. TURNED RT PACK OFF AND SMOKE DISSIPATED. AIR CONDITIONING PACKS, RT PACK. R & R ACM IAW AMM 21-51-08, REF AIPC 21-51-08, ITEM 5. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME.
Part: FRAME — CORRODED (BS 333) · airframe 15,835 hrs · 10,325 cycles
333 CIRCUMFERENTIAL JOINT HAS CORROSION FROM STR 25L TO 27, JUST FWD OF 333 FRAME, FS 333 JOINT OUT OF LIMITS AND STR 26L SPLICE OUT OF LIMITS IAW SRM 53-21-06-101-006-A02. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01 BETWEEN STRS 25LT AND 27 333 CIRCUMFERETIAL JOINT AND STRG SPLICE AT 26L.
Part: CARGO TRACK — CORRODED (BS 565) · airframe 15,835 hrs · 10,325 cycles
FWD BAGGAGE BAY TIE DOWN BRACKET AT FS 565, STR 24L HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 FOUND TO BE OUT OF LIMITS IAW SRM 53-32-58-101-001-A01. COMPLIED WITH STS EA 25-2015-124, BRACKET FWD BAGAGE BAT AT FS 565 AND STR 24L.
Part: SEAT TRACK — CORRODED (BS 477-581) · airframe 15,833 hrs · 10,324 cycles
SEAT TRACK AT RBL9, FS 477.40-581 HAS CORROSION. EVALAUTED SEAT TRACK RBL9, FS477.40, FS581 FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. R & R SEAT TRACK AT RBL9 FS477.40- FS581 IAW AMM 53-00-49-400-801-A11 AND 53-00-49-400-801 A11.
Part: SEAT TRACK — CORRODED (BS 661-847) · airframe 15,833 hrs · 10,324 cycles
SEAT TRACK AT LBL9, FS 661.00+32-FS 847.00+16 HAS CORROSION. EVALUATED SEAT TRACK LBL9 FS 661.00+32-FS 847.00+16, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REMOVED SEAT TRACK LBL9 FS661.00+32-FS847.00+16 IAW CRJ900 AMM 53-00-49-000-801 A11. REPLACED SEAT RAIL CORRODED SEAT RAIL WITH NEW SEAT RAIL AT LBL9 FS661.00+32-FS847.00+16 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. CLASSIFIED AS A MAJOR ALTERATION IAW REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 565-661) · airframe 15,833 hrs · 10,324 cycles
RT SIDE WALL SEAT TRACK AT FS 565- 661+840 HAS CORROSION. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R RT SIDE WALL SEAT TRACK IAW AMM 53-00-49-000-801-A11, AND 53-00-49-400-801-A11. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 690-53-00-343 REV J AS WRITTEN. COMPLIED WITH REO 670-53-00-343, REV L.
Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 15,833 hrs · 10,324 cycles
SEAT TRACK AT LBL9, FS 364-485 HAS CORROSION. EVALUATED SEAT RAIL AT LBL9, FS364-FS485 FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REMOVED AND INSTALLED NEW FABRICATED SEAT TRACK AT LBL9 FS364-FS485 IAW AMM 53-00-49-000-801-A11, 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 847-985) · airframe 15,833 hrs · 10,324 cycles
SEAT TRACK AT RBL9, FS 847+16 - 985 HAS CORROSION. EVALUATED SEAT TRACK AT RBL9, FS 8.00+16-FS985, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REVJ. REMOVED SEAT TRACK RBL9, FS 847.00+16. FS 985 INSTALLED NEW FABRICATED SEAT TRACK AT RBL9, FS 847.00+16-FS 985 IAW AMM 53-00-49-000-801-A11 -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 744-752) · airframe 15,835 hrs · 10,325 cycles
RT SEAT SIDE RAIL SUPPORT BRACKET CORRODED FS744-752. REMOVED CORROSION AT STA 744-752 RT SIDE ON THE SIDE SEAT RAIL SUPPORT BRACKET IAW SRM 51-21-06-001-001-A01. OUT OF LIMITS IAW SRM 53-41-51-101-801-A02. RECEIVED STS EA 32-2015-171 TRIM RETAINER, SEAT TRACK RT FS 744.15 TO FS761.85 DATED 5/4/15. COMPLIED WITH STS EA 32-2015-171 DATED 5/4/2015.
Part: FLOORBEAM — CRACKED (COCKPIT) · airframe 15,835 hrs · 10,325 cycles
LEFT COCKPIT FLOORBEAM IS CRACKED. COMPLIED WTH REO PL 690-53-11-756. FABRICATED -1 AND -7 REPAIR ANGLES REO 690-53-11-756, REV DATED 5-1-15.
Part: SEAT TRACK — CORRODED (BS 469-581) · airframe 15,833 hrs · 10,324 cycles
SEAT TRACK LBL9, BS 469 - 581 HAS CORRROSION. EVALAUTED SEAT TRACK LBL9 FS469-581 FOUND TO BE OUT OF LIMITS IAW REO 67-53-00-013, REV I. R & R SEAT TRACK IAW AMM 53-00-49-400-801-A11.AND 53-00-49-400-801 A11.
Part: SEAT TRACK — CORRODED (BS 661-847) · airframe 15,833 hrs · 10,324 cycles
SEAT TRACK AT RBL 9, FS 661+32-847+16 HAS CORROSION. EVALAUTED SEAT TRACK AT RBL9, FS 5661 NOT FOUND TO BE OUT OF LIMITS IAW REO REV I. R & R WITH SERVICEABLE SEAT RAIL AT RBL 9 FS661.00+32-847.00+16 IAW AMM 53-00-49-000-801-A11 AND 53-00-49-400-801 A11.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 15,833 hrs · 10,324 cycles
SEAT TRACK AT LBL9, FS 581-661+46 HAS CORROSION. EVALAUTED SEAT TRACK LBL9 FS581-FS661+46 FOUND TO BE OUT OF LIMITS IAW REO 67-53-00-013, REV J. R & R SEAT TRACK AT LBL9 FS581-661+46 IAW AMM 53-00-49-400-801-A11 AND 53-00-49-400-801 A11.
Part: SEAT TRACK — CORRODED (BS 649-661) · airframe 15,833 hrs · 10,324 cycles
LT SIDE WALL SEAT TRACK AT FS 649.40-FS 661.00+840 HAS CORROSION. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK FS 649.40-661.00+48 IAW AMM 53-00-49-000-801 A11. INSTALLED NEW SEAT TRACK AT 649.40-661.00+48 IAW AMM 53-00-49-400-801.
Part: FLOOR SUPPORT — CORRODED (BS 752-785) · airframe 15,833 hrs · 10,324 cycles
LT UPPER LONGERON FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION ALONG FS 752-785. REMOVED CORROSION ON LT UPPER LOUNGEMAN FLOOR SILL BETWEEN FS 752-785 IAW SRM 51-26-06-001-001-A01. COMPLIED WITH STS EA 32-2015-173, DATED 5-4-20156 FLOOR ANGLE PRESSURE SILL LG AT FS 767.75 AND 778.25. COMPLIED WITH FOR EA 32-2015-173 AND COMPLIED WITH ECTC EA 32-2015-173 AS REQUIRED.
Part: SEAT TRACK — CORRODED (BS 847-985) · airframe 15,833 hrs · 10,324 cycles
SEAT TRACK AT LBL9, FS 847+16-985 HAS CORROSION. EVALUATED SEAT TRACK AT LBL9 FS 847.00+16-FS985 FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013 REV J. REMOVED SEAT TRACK AT LBL9, FS847.00+16-FS985 IAW AMM 53-00-49-000-801-A11. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801 SEAT TRACK PREVIOUSLY FABRICATED IAW ATTACHED REO 670-53-00-343. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343 REV J AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 761-847) · airframe 15,833 hrs · 10,324 cycles
LT SIDE WALL SEAT TRACK AT FS 847+16 - 761.85 HAS CORROSION. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801-A11. INSTALLED NEW SEAT RAIL IAW AMM 53-00-49-400-801-A11. INSTALLED SCREW IN SEAT RAIL FS 847-FS 761 IAW AMM 53-00-49-400-801-A11 SCREW LOCATION 10AFT.
Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 15,833 hrs · 10,324 cycles
SEAT TRACK AT LBL 9, FS 661.00+32-693 HAS CORROSION. EVALUATED SEAT TRACK LBL9 FS661.00+32-FS693 FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REMOVED SEAT TRACK AT LBL9 FS661.00+32-FS693 IAW AMM 53-00-49-000-801-A11. INSTALLED SEAT TRACK AT LBL9 FS661.00+32-FS693 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: FLOOR SUPPORT — CORRODED (BS 720-785) · airframe 15,835 hrs · 10,325 cycles
RT UPPER LONGERON FLOOR SILL HAS MULTIPLE CORROSION ALONG FS720-785. REMOVED CORROSION ON RT UPPER LONGERON FLOOR SILL BETWEEN FS 720-785 IAW SRM 51-21-06-001-001-A01. COMPLIED WITH STS EA 32-2015-169 FLOOR ANGLE PRESSURE SILL RT AT FS724.08 AND FS735.90 ISSUE DATE 5/4/2015 AND STS EA 32-2015-170 DATED 5/4/2015 AT FS768.75 AND FS778.25. COMPLIED WITH ECTC EA 32-2015-169 AND ECTC EA 32-2015-170.
Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 15,833 hrs · 10,324 cycles
SEAT TRACK AT RBL9, FS 661.00+32-693 HAS CORROSION. EVALUATED SEAT TRACK, RBL9, FS 661.00+32-FS693 FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REMOVED SEAT TRACK RBL9, FS 661.00+32-FS 693 IAW AMM 53-00-49-000-801-A11. REPLACED SEAT RAIL AT RBL9 FS 661.00+32-FS693 IAW AMM 53-00-49-400-801-A11 WITH NEW SEAT RAIL. COMPLIED WITH ECTC REO 670-53-00-343 AND REO 670-53-00-343, REV J AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 744-752) · airframe 15,835 hrs · 10,325 cycles
LT SIDE SEAT RAIL SUPPORT BRACKET CORRODED FS744-752. REMOVED COORROSION AT STA 744-752 LT SIDE ON THE SLAT RAIL SUPPORT BRACKET IAW SRM 51-21-06-001-001-A01. OUT OF LIMITS IAW SRM 53-41-51-101-001-A02. COMPLIED WITH STS EA 32-2015-172 TRIM RETAINER SEAT TRACK LT FS 743.00 TO FS 763.00. VERIFIED ALL STEPS OF EA 32-2015-172 ARE COMPLETE AND COMPLIED WITH ECTC EA 32-2015-172 AS REQUIRED.
Part: SEAT TRACK — CORRODED (BS 669-720) · airframe 15,833 hrs · 10,324 cycles
LT SIDE WALL SEAT TRACK AT FS 669.40-720.85 HAS CORROSION. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801-A11. INSTALLED NEW SEAT RAIL IAW AMM 53-00-49-400-801-A11. INSTALLED 4 SCREWS AT SEAT RAIL FS 669.40-720.85 IAW AMM 53-00-49-400-801-A11. SDR CLOSED.
Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 15,826 hrs · 10,320 cycles
FLOOR SEAT TRACK AT RBL 9, FS 349-485 IS CORRODED IN MULTIPLE AREAS. FOUND TO BE OUT OF LIMITS IAW REO 67-53-00-013, REV 5. REMOVED AND REPLACED IAW AMM 53-00-49-000-801-A11 AND AMM 53-00-49-400-801-A11.
Part: CARGO TRACK — CORRODED (BS 629) · airframe 15,826 hrs · 10,320 cycles
FWD BAGGAGE BAY TIE DOWN BRACKET FS629, STR 27 HAS CORROSION. REMOVED DAMAGED BRACKET AND REPLACED WITH NEW BRACKET IAW SRM 51-42-26-001-001-A01/ 51-40-11-001-001-A01.
Part: STRINGER — CRACKED (BS 280) · airframe 15,826 hrs · 10,320 cycles
STR 3L HAS POSSIBLE CRACK AFT OF FS 280 NEED NDT TO VERIFY. STR 3L REPAIR PERFORMED DURING THE INCORPATION OF SB 670BA-53-040.
Part: CARGO TRACK — CORRODED (BS 661) · airframe 15,826 hrs · 10,320 cycles
FWD BAGGAGE BAY TIE DOWN BRACKET BS 661, STR 25R HAS CORROISON. REMOVED DAMAGED BRACKET AND REPLACED WITH NEW BRACKET IAW SRM 51-42-26-001-001-A01/ 51-40-11-001-001-A01.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,826 hrs · 10,320 cycles
AFT COCKPIT FLOOR SUPPORT AT FS 280.00 HAS CORROSION. REMOVED AFT FLOOR SUPPORT REF SRM 51-42-26-001-001-A01 AND 51-42-22-001-001-A01. INSTALLED NEW FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001. LOCATED AND DRILLED AND INSTALLED FLOORBOARD NUTPLATES AND INSTALLED 2EA RIVETS IN CORNER GUSSET IAW SRM 51-42-06-001-001.
Part: DOUBLER — CORRODED (BS 295-310) · airframe 15,826 hrs · 10,320 cycles
ANTENNA DOUBLER HAS CORROSION BETWEEN BS 295 - 310 AT STR 27. R & R TCAS DOUBLER BETWEEN FRAME 295-310 AT STR 27 IAW SRM 51-42-06-001-001-A01.
Part: FRAME — CORRODED (BS 333) · airframe 15,826 hrs · 10,320 cycles
BS 333 FRAME JOINT HAS CORROSION FROM STR 26L TO 26R. REMOVED CORROSION ON FRAME AT FS 333 BETWEEN STR 26L AND 27, REF SRM 51-21-06-001-001-A01. COMPLIED WITH EA 25-2015-135.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 15,826 hrs · 10,320 cycles
EMERGENCY LIGHT ON PANEL 172CR, OVERWING, HAS A BROKEN WIRE. FOUND WIRE BROKEN AT CONTACT PIN. INSTALLED SERVICEABLE CONTACT PIN ON TO EMERGENCY LIGHT WIRE AT PANEL 172R IAW ESPM 20-16-00. COMPLETED OPS TEST OF EMERGENCY LIGHT REF AMM TASK 33-51-00-710-802. OPS CHECK GOOD.
2014
Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 14,573 hrs · 9,496 cycles
RT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R RT AFT OVERWING EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-15.
Part: SILL — CORRODED (FUSELAGE) · airframe 12,624 hrs · 8,157 cycles
PAX DOOR ENTRY WAY SILL MID CAP ANGLE, CORRODED. REMOVED PAX DOOR ENTRY WAY SILL MID CAP ANGLE IAW GMM 3-8.6 ELEMENTARY OPERATIONS, 4 SCREWS AND JUMPER. INSTALLED SERVICEABLE PAX DOOR ENTRY WAY SILL MID CAP ANGLE IAW GMM 3-8.6 FOR ELEMENTARY OPERATIONS AND AMM 20-21-00.
Part: SILL — CORRODED (FUSELAGE) · airframe 12,624 hrs · 8,157 cycles
PAX DOOR SILL MID CAP ANGLE, CORRODED.
2013
Part: SIGN — MISINSTALLED (EMERGENCY LIGHT) · airframe 11,991 hrs · 7,752 cycles
EMERGENCY EXIT SIGN AT PASSENGER DOOR HAS THE ARROW POINTING THE WRONG WAY. R & R PASSENGER DOOR EXIT SIGN WITH CORRECT PART IAW AMM 33-51-05. NO FURTHER DEFECTS NOTED. ACFT RETURNED TO SERVICE.
Part: MEGAPHONE — UNSERVICEABLE (CABIN) · airframe 11,197 hrs · 7,270 cycles
MEGAPHONE UNSERVICEAGLE. R & R MEGAPHONE IAW AMM 25-61-14, AIPC 25-61-14, FIG 1K ITEM 5.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 10,898 hrs · 7,078 cycles
LT AFT OVERWING EMERGENCY LIGHT HAS BROKEN WIRES. REMOVED LT AFT OVERWING EMERGENCY LIGHT IAW AMM 33-61-15-000-801. INSTALLED NEW EXTERIOR EMERGENCY LIGHT ON LT SIDE AFT IAW AMM 33-51-15-400-801. OPS TESTED GOOD.
Part: INTERCOSTAL — CORRODED (BS 661) · airframe 10,898 hrs · 7,078 cycles
CORNER OF INTERCOSTAL CORRODED AT FS 661.00 AND STR 25R. REMOVED CORROSION IAW 0.002" SRM 51-21-06-001-001-A01, 53-32-50-101-001-A01 AND REO 690-52-32-011 IAW NDTM PT 1, 51-20-006-250-A01.
Part: SILL — CORRODED (BS 349) · airframe 10,898 hrs · 7,078 cycles
SERVICE DOOR CUTOUT LOWER SILL HAS CORROSION DAMAGE FS 349.70 - FS 349.0. REMOVED SERVICE DOOR SILL IAW SRM 51-42-06 AND 51-42-34. INSTALLED NEW SERVICE DOOR SILL IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED LOWER DOOR SILL IAW SRM 51-40-11-001-001-A01.
Part: BULKHEAD — CORRODED (BS 280) · airframe 10,898 hrs · 7,078 cycles
RT BS 280 BULKHEAD WEB CORRODED AT RBL 12. REMOVED DAMAGED BULKHEAD WEB SECTION AND REPAIR IAW REO 670-53-11-594.
Part: BULKHEAD — CORRODED (BS 280) · airframe 10,898 hrs · 7,078 cycles
LT 280 BULKHEAD WEB CORRODED AT LBL12. REPAIRED IAW REO 670-53-11-594.
Part: SEAT TRACK — CORRODED (BS 669.4-720.85) · airframe 10,990 hrs · 7,136 cycles
LEFT SEAT TRACK SEGMENT FROM BS 669.4 TO 720.85 CORRODED. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-800-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343, REV D.
Part: SEAT TRACK — CORRODED (BS 661-667) · airframe 10,990 hrs · 7,136 cycles
SEAT TRACK SEGMENT AT LBL 9 FROM FS 661 TO 677 CORRODED. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801 (CONFIG A11), REO 670-53-00-343, REV D, AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 347-517) · airframe 10,898 hrs · 7,078 cycles
SEAT TRACK SEGMENT AT RBL9 AND FROM FS 347 TO 517 HAS 1 CORRODED SPOT. REMOVED SEAT TRACK IAW SRM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW SRM 53-00-49-400-801.
Part: DOOR FRAME — CORRODED (BS 280) · airframe 10,898 hrs · 7,078 cycles
LIGHT LOWER DOOR POST AT FS 280 CORRODED. REPAIRED IAW REO 690-53-11-526 IAW NDTM PT.1, 51-20-006-250-A01.
Part: SEAT TRACK — CORRODED (BS 785.15-847) · airframe 10,898 hrs · 7,078 cycles
RIGHT SIDE SEAT TRACK SEGMENT FROM FS 785.15 TO 847+16 CORRODED. R & R RT SIDE SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 785.15-847.16) · airframe 10,898 hrs · 7,078 cycles
LT SIDE SEAT TRACK SEGMENT FROM FS 785.15 TO FS 847.16 CORRODED. R & R LT SIDE SEAT TRACK IAW AMM 53-00-49-400-801+000-801.
Part: SEAT TRACK — CORRODED (BS 744.15-761.85) · airframe 10,898 hrs · 7,078 cycles
LEFT SIDE SEAT TRACK SEGMENT FROM FS 744.15 TO 761.85 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 661-667) · airframe 10,990 hrs · 7,136 cycles
SEAT TRACK SEGMENT AT RBL 9 AND FROM BS 661 TO 677 CORRODED. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801 (CONFIG A11), REO 670-53-00-343, REV D AND 670-53-00-013.
Part: DOOR FRAME — CORRODED (BS 280) · airframe 10,898 hrs · 7,078 cycles
RIGHT LOWER DOOR POST AT FS 280 CORRODED. REPAIRED IAW REO 690-53-11-526.
Part: SEAT TRACK — CORRODED (BS 597-661) · airframe 10,898 hrs · 7,078 cycles
SEAT TRACK SEGMENT AT LBL9 AND FROM FS 597 TO 661 HAS NUMEROUS CORROSION SPOTS. R & R SEAT TRACK IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 588-661) · airframe 10,898 hrs · 7,078 cycles
SEAT TRACK SEGMENT AT RBL9 AND FROM FS 588 TO FS 661 HAS NUMEROUS CORROSION SPOTS. R & R SEAT TRACK IAW AMM 53-00-49-400-801.
Part: BEAM — CORRODED (BS 645) · airframe 10,898 hrs · 7,078 cycles
FS 645.00 BEAM CORRODED BETWEEN STR26L AND 25R. REMOVED LIGHT SURFACE CORROSION BY HAND, NO PITTING FOUND IAW SRM 51-21-06-001-001-A01. BLENDED AREA OUT OF LIMIT IAW SRM 53-31-06-101-003-A02.
Part: SEAT TRACK — CORRODED (BS 744.15-761.85) · airframe 10,898 hrs · 7,078 cycles
RIGHT SIDE SEAT TRACK SEGMENT FROM FS 744.15 TO 761.85 CORRODED. R & R WITH NEW RT SIDE SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
Part: SILL — CORRODED (FUSELAGE) · airframe 10,898 hrs · 7,078 cycles
WHILE WORKING SERVICE DOOR SILL, CORROSION FOUND ON DOOR SILL UPPER ANGLE. REMOVED DOOR SILL ANGLE ON SERVICE DOOR SILL IAW SRM 51-42-06-00. INSTALLED DOOR SILL ANGLE IAW SRM 51-42-06-001-001 AND SRM 51-42-21-001-001. DRILLED UP NEW ANGLE IAW SRM 51-40-11-001-001-A01. MAJOR REPAIR
Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 10,898 hrs · 7,078 cycles
RT SIDE FLOOR SUPPORT CORRODED AT FS 280.00 AND RBL 38. REMOVED RT FLOOR SUPPORT FS 280-310 LOCATED & DRILLED NEW FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 & DWG SH670-32172.
Part: FLOORBEAM — CRACKED (BS 274) · airframe 10,898 hrs · 7,078 cycles
COCKPIT FLOORBEAM AT RBL 12 IS CRACKED AT FS 274.00. REPAIRED IAW REO 690-53-11-522.
Part: SILL — CORRODED (FUSELAGE) · airframe 10,898 hrs · 7,078 cycles
CORROSION DAMAGE ON AFT CARGO DOOR CUTOUT LOWER SILL. REPAIRED IAW REO NR 670-53-61-913.
Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 10,898 hrs · 7,078 cycles
FLOOR SUPPORT ANGLE ON RBL9 AND AT FS 280 IS CRACKED. REPAIRED IAW SRM 51-42-06-001-001 AND 51-42-21-001-001.
Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 10,898 hrs · 7,078 cycles
FLOOR SUPPORT ANGLE ON LBL9 AND AT FS 280 IS CRACKED. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001. DRILLED NEW ANGLE TO FIT AND TRANSFERRED RECEPTACLES IAW SRM 51-42-06-001-001-A01. INSTALLED NEW FLOOR SUPPORT ANGLE AT LBL9 AND FS 280 IAW SRM 51-42-06-001-001.
Part: INTERCOSTAL — CORRODED (BS 364 S26L) · airframe 10,898 hrs · 7,078 cycles
INTERCOSTAL CORRODED AT FS 364 AND STR26L. RESOLUTION DESCRIPTION: REMOVED INTERCOSTAL PER SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,898 hrs · 7,078 cycles
FLOORBEAM CORRODED. REMOVED BS 280 FLOORBEAM IAW SRM 51-42-06-001-001. LOCATED AND DRILLED NEW SERVICABLE FLOORBEAM IAW SRM 51-42-06-001-001. INSTALLED NEW FLOORBEAM IAW SRM 51-42-06-001-001-A01, REF DWG CC670-340-94.
Part: FRAME — CORRODED (BS 333) · airframe 10,990 hrs · 7,136 cycles
FRAME CORRODED AT FS 333 AND BETWEEN STR27 AND 26L. REPAIRED IAW SRM 57-21-06-001-001-A01 AND REO 690-53-21-468. CLASSIFIED AS A MAJOR REPAIR.
Part: FRAME — CORRODED (BS 333) · airframe 10,990 hrs · 7,136 cycles
FRAME CORRODED AT FS 333 AND BETWEEN STR 26 AND 27R. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 690-53-21-468. CLASSIFIED AS A MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 10,898 hrs · 7,078 cycles
BS 280 FLOORBEAM CORRODED. REMOVED BS 280 FLOORBEAM IAW SRM 51-42-06-001-001. LOCATED AND DRILLED NEW SERVICABLE FLOORBEAM IAW SRM 51-42-06-001-001. INSTALLED NEW FLOORBEAM IAW SRM 51-42-06-001-001-A01. REF DWG CC670-340-94.
Part: INTERCOSTAL — CORRODED (BS 364) · airframe 10,898 hrs · 7,078 cycles
INTERCOSTAL CORRODED AT FS 364 AND S27R. CORROSION DAMAGE FOUND TO BE BEYOND LIMITS IAW SRM 53-21-23-101-003-Z01. REMOVED CORRODED INTERCOSTAL IAW SRM 51-26-00-001-001-A01, 51-42-21-001-001-A01. INSTALLED NEW SERVICABLE INTERCOSTAL AT FS364, STGR 27 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: FLOORBEAM — CRACKED (BS 274) · airframe 10,898 hrs · 7,078 cycles
COCKPIT FLOORBEAM AT LBL 12 IS CRACKED AT FS 274. REPAIRED IAW REO 690-53-11-522.
Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 10,898 hrs · 7,078 cycles
FLOOR SUPPORT ANGLE ON RBL9 AND AT FS280 IS CRACKED. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001. INSTALLED FLOORB SUPPORT ANGLE IAW SRM 51-42-06-001-001 AND 51-42-21-001-001.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 10,444 hrs · 6,801 cycles
CREW REPORTS MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
Part: LIGHT — MISSING (CABIN) · airframe 10,418 hrs · 6,784 cycles
EXIT FLOOR LIGHTS MISSING AT GALLEY 3. REPLACED EMERGENCY FLOOR LIGHT IAW AMM 33-51-01.
2012
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 9,467 hrs · 6,207 cycles
PAX DOOR AFT SIDE DRAG ANGLE HALF WAY DOWN THE DOOR, CRACKED. COMPLIED WITH REO 670-52-11-287, REV C.
Part: SIGN — MISSING (CABIN) · airframe 8,969 hrs · 5,912 cycles
FORWARD FACING EXIT SIGN FOR OVER WING EMERGENCY EXITS MISSING. FOUND MISSING COVER AND INSTALLED FWD FACING EXIT SIGN ASSY IAW AMM 33-51-07, OPS CHECKED GOOD, ACFT OK FOR SERVICE. SDR CLOSED.
Part: GLOWSTRIP — BROKEN (CABIN) · airframe 8,744 hrs · 5,783 cycles
PHOTO LUMINESCENT AROUND SERVICE DOOR IS BROKEN OFF. R & R TRIM PANEL ON LT SIDE OF SERVICE DOOR IAW AMM 25-26-07. NO FURTHER DEFECTS NOTED, ACFT OK FOR SERVICE.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 8,294 hrs · 5,488 cycles
BOTH EMERGENCEY EXIT LIGHTS ON LT SIDE OF ACFT BELOW EMERGENCY DOOR ARE INOPERATIVE. FOUND CONNECTOR P5300 DISCONNECTED. SECURED CONNECTOR IAW ESPM 20-26-00. OPS CKS GOOD IAW AMM 33-51-00.
Part: OVERHEAT LOOP — FALSE ACTIVATION (RT BLEED) · airframe 8,278 hrs · 5,479 cycles
IN FLIGHT, CLIMBING THRU 220, RECEIVED RT ENGINE BLEED MESSAGE, COMPLIED WITH QRH. CONTINUED FLT UNPRESSURIZED AT 10,000 FT . EMERGENCY DECLARED. R & R AILC AND BLEED LOOP MT205. OPS CHECKED GOOD IAW 36-21-00.
Part: O-RING — LEAKING (BLEED AIR) · airframe 8,278 hrs · 5,479 cycles
RECIEVED RT BLEED RED WARNING AT 20.000 FT, DECLARED EMERGENCY, LOST ALL PRESSURIZATION, FOLLOWED QRH. REPAIRED BLEED AIR LEAK BY R & R RT CONDENSOR/ REHEATER PIPE O-RING IAW AMM 21-51-14. LEAK CHECKED GOOD. PRESSURIZED THE AIR CON SYS WITH THE ENGINES IAW AMM 21-50-00 AND PERFORMED HIGH POWER RUNS IAW AMM 71-00-00. NO DEFECTS NOTED.
Part: OVERHEAT LOOP — OUT OF POSITION (RIGHT) · airframe 8,255 hrs · 5,462 cycles
RT BLEED DUCT OVERHEAT WARNING. EMERGENCY DECLARED. FOUND BOTH LOOPS PRESSED INTO THW DUCTING COVERS. CORRECTLY POSITIONED BOTH LOOPS IAW AMM 36-21-03. PERFORMED BLEED LEAK DETECTION TEST IAW AMM 36-21-00, LOOPS OPERATE CORRECTLY, PERFORMED EXTENSIVE INSP FOR ANY ACTUAL BLEED LEAKS, NO LEAKS COULD BE FOUND IN THE BLEED SYS IN THE AFT EQUIPMENT AREA.
Part: LIGHT — MISSING (CABIN) · airframe 7,534 hrs · 4,976 cycles
EMERGENCY LIGHT AT FWD LAV & EMERGENCY ROW 12 C&D MISSING. INSTALLED EMERGENCY LIGHT IAW AMM 33-51-01.
Part: CONNECTOR — CONTAMINATED (BRAKE TEMP) · airframe 7,314 hrs · 4,838 cycles
LEFT OTBD BRAKE SHOWED OVERHEAT ON TAKEOFF "BRAKE OVERHEAT WARNING" FOLLOWED QRH AND RETURNED TO DEPARTURE. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. CLEANED LEFT OTBD BRAKE TEMP MONITORING SYSTEM ELECTRICAL CONNECTOR AND REATTACHED IAW AMM 3246-01. OPS CHECKED GOOD.
2011
Part: LIGHT — BROKEN (CABIN) · airframe 7,142 hrs · 4,742 cycles
ABOUT 5 INCHES OF EMERGENCY LIGHT MISSING NEAR SEAT 5C. REPLACED 5 INCHES LIGHT IAW AMM 33-51-01. OK FOR SERVICE.
Part: LIGHT — BROKEN (CABIN) · airframe 7,142 hrs · 4,742 cycles
ABOUT 12 INCHES OF EMERGENCY FLOOR LIGHT, MISSING ACROSS FROM LAVATORY. REPLACED 12 INCHES OF EMERGENCY LIGHT IAW AMM 33--51-01. OK FOR SERVICE.
Part: LIGHT — BROKEN (CABIN) · airframe 7,142 hrs · 4,742 cycles
ABOUT 4 INCHES OF EMERGENCY LIGHTING MISSING TOWARD AFT LAVATORY. REPLACED LIGHT IAW AMM 33-51-01. OK FOR SERVICE.
Part: LIGHT — BROKEN (CABIN) · airframe 7,142 hrs · 4,742 cycles
ABOUT 5 INCHES OF EMERGENCY LIGHT MISSING FROM NEAR SEAT 9B. REPLACED 5 INCHES OF EMERGENCY LIGHT IAW AMM 33-51-01. OK FOR SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,006 hrs · 4,664 cycles
EMERGENCY EXIT LIGHT AT ENTRY DOOR INOPERATIVE. R & R NR 1 EMERGENCY BATTERY PACK, IAW AMM 33-51-17, OPS CHECKED GOOD.
Part: LIGHT — MISSING (CABIN) · airframe 6,800 hrs · 4,537 cycles
EMERGENCY LIGHT MISSING. R & R IAW AMM 33-51-01.
Part: GLOWSTRIP — MISSING (CABIN) · airframe 6,790 hrs · 4,531 cycles
ABOUT 18 INCHES OF FLOOR LIGHTING MISSING IN FRONT OF FWD LAV PHOTOLUMINESCENT STRIP/TAPE R & R EMERGENCY GLOWSTRIP IAW AMM 33-51-01.
Part: SENSOR — MALFUNCTIONED (MLG) · airframe 5,596 hrs · 3,795 cycles
RECEIVED A BRAKE OVERHEAT WARNING MESSAGE ON TAKEOFF ROLL APPROX 90 KNOTS. PERFORMED REJECTED TAKEOFF . R & R NR 3 BTMS THERMOCOUPLE SENSOR IAW AMM 32-46-01. OPS CHECED GOOD.
Part: CABLE — LACK OF LUBE (PAX DOOR) · airframe 5,588 hrs · 3,789 cycles
PAX DOOR IS DIFFERCULT TO OPEN. OPS CHECKED PAX. NO DEFECTS FOUND. LUBRICATED THE PRESSURE VENT FLAP CABLE. OK FOR SERVICE.
Part: SEAT TRACK — CORRODED (BS 349-364) · airframe 5,311 hrs · 3,593 cycles
MINOR CORROSION ON SEAT TRACK, RBL 9 FROM BS 349-364. BLENDED SEAT TRACK ON RBL 9 FROM BS 349 - 364 APPROX FOUND TO BE OUT OF LIMITS ORINIAL THICKNESS IS .370, REMOVED .040, REMAINING MATERIAL .330. ALL WORK DONE IAW SRM 53-21-49-101-001-A01. MINOR REPAIR. REPLACED SEAT TRACK ON RBL9 FROM FS 349 - 364 APPROX EM161737. SEALED NEW TRACK AND INSTALLED ALL ATTACHING BOLTS IAW TASK 20-21-00-910-801.
Part: LIGHT — MISSING (CABIN) · airframe 4,954 hrs · 3,338 cycles
ABOUT 20 INCHES OF FLOOR FLORESCENT EMERGENCY LIGHTING MISSING OF FIRST CLASS FWD OF FIRST CLASS LAV. INSTALLED NEW FLOOR FLORESCENT EMERGENCY LIGHT STRIP & CHECKED GOOD IAW AMM 33-50-01
2010
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 3,397 hrs · 2,336 cycles
MEGAPHONE INOP, R & R MEGAPHONE IAW AMM 25-61-14.OPS CK GOOD.