N931XJ
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.
138 reports on file, 2010-09-27 – 2024-04-17.
Part: NONE — NONE (NONE) · airframe 35,201 hrs · 24,780 cycles
"THE L/H AILERON HAS PREVIOUSLY O/S LUG BORES LABELED ""C"" & ""F"". FABRICATION OF (QTY. #2) O/S BUSHINGS IS REQUIRED. REPAIRED IAW BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25. "
Part: HANDLE — CRACKED (ESCAPE HATCH) · airframe 35,201 hrs · 24,780 cycles
CREW ESCAPE HATCH HANDLE HOUSING IS CRACKED. REMOVED AND REPLACED CREW ESCAPE HATCH HANDLE HOUSING (P/N: H3419-35) IAW CRJ900 SM 51-42-06-001-001-A01, 51-40-11-001-001-A01. DISPLACED AND REINSTALLED INSULATION FOR ACCESS IAW CRJ900 AMM 25-81-01-000/400-801 (A01).COMPLETED FINISH SURFACE IAW CRJ900 SRM 51-21-16-001-001-A01.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 35,201 hrs · 24,780 cycles
PAX DOOR DD6 MID INTERCOSTAL CORRODED. REMOVED PAX DOOR INTERCOSTAL AT DD6IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01, RECEIVED NEW INTERCOSTAL P/N 601R318057-1 , LOCATED AND DRILLED AND INSTALLED NEW INTERCOSTAL IAW CRJ SRM 900 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: FORMER — CORRODED (ZONE 800) · airframe 35,201 hrs · 24,780 cycles
PAX DOOR FWD FORMER IS CORRODED IN SEVERAL AREAS. REPLACED FWD PAX DOOR FORMER P/N 601R318031-5 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-42-21-001-001-A01
Part: FORMER — CORRODED (ZONE 800) · airframe 35,201 hrs · 24,780 cycles
PAX DOOR FWD FORMER IS CORRODED IN SEVERAL AREAS. REPLACED FWD PAX DOOR FORMER P/N 601R318031-5 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-42-21-001-001-A01
Part: STRINGER — CORRODED (ZONE 100) · airframe 35,201 hrs · 24,780 cycles
STGR 21R FOUND TO BE CORRODED THROUGH BETWEEN F.S. 364 AND F.S. 379. REPAIRED IAW CRJ900 SRM 53-00-03-201-001-A02.
Part: STRINGER — CORRODED (BS 364-379 S21R) · airframe 35,201 hrs · 24,780 cycles
STGR 21R FOUND TO BE CORRODED THROUGH BETWEEN F.S. 364 AND F.S. 379. REPAIRED IAW CRJ900 SRM 53-00-03-201-001-A02.
Part: FRAME — CORRODED (ZONE 100) · airframe 35,201 hrs · 24,780 cycles
FS379 FRAME SEGMENT FROM STR 25R TO STR 21R CORRODED REPLACE FRAME SEGMENT IAW CRJ 900 SRM 51-42-06-001-001-A01.
Part: DIAPHRAGM — CORRODED · airframe 35,201 hrs · 24,780 cycles
STRUCTURE INSIDE FWD TOILET SERVICE DOOR IS CORRODED. REMOVED AND REPLACED DIAPHRAGMS AND BRACKET IAW CRJ 900SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 35,201 hrs · 24,780 cycles
"STGR 19R SPLICE IS CORRODED BETWEEN F.S. 677 TO F.S. 669.40. DISPLACED WIRE HARNESS BETWEEN FS 661+90 - FS 693 REMOVED FASTENERS AT AFFECTED LOCATIONS FOR ACCESS IAW CRJ 900 SRM 51-42-06/21-001-001-A01. REMOVED CORROSION FROM FWD SIDE OF STGR 19R SPLICE (P/N: SH690-39111-1), FWD DIAPHRAGM (P/N: SH 690-39112-1) AND AFT TENSION FITTING (P/N: SH670-39089-1) BETWEEN FS 661.15+90 - FS 677.00 IAW CRJ 900 SRM 51-21-06-001-001-A01. C/W UTT ON STR 19R SPLICE FS 669+90-677 REWORKED AREAS IAW CRJ 900 NDTM PART 01 51-20-004-270-A01. FOUND LOWEST TO BE .050"" OR GREATER AND RECORDED ON PART. EVALUATED UT MEASUREMENTS AND STRINGER 19R SPLICE PN: SH690-39111-1 ORIGINAL THICKNESS IS .063"" AND REMAINING THICKNESS IS .063"", DIAPHRAGM PN: SH690-39112-1 ORIGINAL THICKNESS IS .050"" AND REMAINING THICKNESS IS .050"" AND BOTH PARTS ARE WITHIN LIMITS IAW CRJ 900 SRM 53-00-00-101-001-A01. AFT TENSION FITTING PN: SH670-39089-1 ORIGINAL THICKNESS IS .080"" AND REMAINING THICKNESS IS .063"", DAMAGE IS NOT ALLOWED ON FITTINGS IAW CRJ 900 SRM 53-00-00-101-001-A01. FABRICATED TENSION FITTING (P.N.# SH670-39089-S0101) USING MATERIAL 7475-T7 (P.O. W54674) PER STEP #1 OF MHIRJ SNIEO SH670-39089 IDENTIFIER S01. LOCATED DRILLED AND INSTALLED NEWLY FABRICATED AFT TENSION FITTING P.N. SH670-39089-SO101 LOCATED AT STR19R BETWEEN FS661 AND FS677 IAW ALL STEPS 1 THRU 4 OF MHIRJ SNIEO SH670-39100 IDENTIFIER S01. INSTALLED FASTENERS AT AFFECTED LOCATIONS FOR ACCESS IAW CRJ 900 SRM 51-42-06/21-001-001-A01. APPLIED SURFACE FINISH A023 ON P.N. SH670-39089-S0101 IAW MHIRJ SNIEO SH670-39089 IDENTIFIER S01 STEP 3. APPLIED SURFACE FINISH REWORK AREA IAW CRJ 900 SRM 51-21-16-001-001-A01. RE-PLACED WIRE HARNESS BETWEEN FS 661+90- FS 693 IAW CRJ900 SRM 51-41-04-01-001-A01 "
Part: FLOORBEAM — CORRODED (BS 280) · airframe 35,201 hrs · 24,780 cycles
"FOUND RH FS 280 CROSSBEAM TO HAVE CORROSION. REMOVED AND REPLACED RH FS 280 CROSSBEAM PN: CC670-34094-2 IAW CRJ 900 SRM 51-42-06-001-00-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01, 51-40-11-001-001-A01. PAINTED RH FS 280 CROSSBEAM IAW CRJ 900 SRM 51-25-21-001-001-A01. APPLIED CIC TO AFT SIDE OF FS 280 CROSSBEAM IAW CRJ 900 SRM 51-21-11-001-001-A01. "
Part: FLOORBEAM — CORRODED (BS 280) · airframe 35,201 hrs · 24,780 cycles
FOUND LH FS 280 CROSSBEAM TO HAVE CORROSION. REMOVED AND REPLACED LH FS 280 CROSSBEAM PN: CC670-34094-1 IAW CRJ 900 SRM 51-42-06-001-00-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01, 51-40-11-001-001-A01. PAINTED LH FS 280 CROSSBEAM IAW CRJ 900 SRM 51-25-21-001-001-A01. APPLIED CIC TO AFT SIDE OF FS 280 CROSSBEAM IAW CRJ 900 SRM 51-21-11-001-001-A01.
Part: FITTING — UNKNOWN · airframe 34,984 hrs · 24,597 cycles
WHILE PERFORMING SB 670BA-53-044 REV G PART B & C - PRIMARY STRUCTURE FS 144 TO FS 280 - REINFORCEMENT OF THE LH & RH SIDES OF THE FS 202.75 BULKHEAD ABOVE THE FLOOR AND NLG BOX WE FOUND THE R/H STRINGER 12A FITTING CC670-33562-001SB WILL ONLY PICK UP TWO FASTENERS ON THE FS 202 BULKHEAD FLANGE IN LIEU OF THREE PER THE SB REQUIREMENTS. ENGINEERING REQUIRED. COMPLIED WITH MHIRJ REO 690-53-11-1684 REV-- DATED 2024-02-09
Part: LUG — CRACKED (RT EMER EXIT) · airframe 34,984 hrs · 24,597 cycles
R/H FWD EMERGENCY EXIT UPPER AFT LUG POSIBLE CRACK, REPAIRED IAW MHIRJ REO 690-52-21-155 REV -- DATED 2024-02-15,
Part: LUG — CRACKED (EMERGENCY EXIT) · airframe 34,984 hrs · 24,597 cycles
L/H AFT EMERGENCY EXIT UPPER AFT LUG POSIBLE CRACK, REPAIRED IAW MHIRJ REO 690-52-21-154 REV -.
Part: WIRE HARNESS — INOPERATIVE (BRAKE OVERHEAT) · airframe 34,983 hrs · 24,596 cycles
AFTER TAKEOFF RECEIVED BRAKE OVHT WARNING INDICATION FOR RIGHT INBOARD BRAKE. RETURNED TO ATL. REMOVED AND REPLACED PROXIMITY SENSOR HARNESS ASSEMBLY IAW AMM 32-61-05. OPS TEST DONE IAW AMM 32-61-00, OPS TEST GOOD. ALSO REMOVED AND REPLACED BRAKE TEMPERATURE SENSOR IAW CRJ 900 AMM 32-46-01. PERFORMED OPS CHECK, OPS CHECK GOOD.
Earlier reports · 2010–2022 · 122 reports
2022
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,523 hrs · 22,538 cycles
FOUND FWD EMERGENCY LIGHTS INOP R&R EPSU BATTERY IAW AMM 33-51-17 OPS CHECK GOOD.
2021
Part: NONE — INOPERATIVE · airframe 30,816 hrs · 21,136 cycles
EPSU BATTERY CHARGER FAILED OPS CHECK WHEN REPLACING EPSU BATTERY PACK @PS37. R&R EPSU BATTERY CHARGER @PS37. OPS CHECK IS GOOD. IAW AMM 33-51-17 PN ON & OFF: 11-0049. SN ON: 27237 SN OFF: 23106
2020
Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 28,576 hrs · 19,184 cycles
EMERGENCY LIGHT ON RT OVERWING PANEL 172CRJ IS INOPERABLE. INVESTIGATED AND FOUND WIRE PULLED OUT OF CONTACT AT LIGHT. INSTALLED SERVICEABLE CONTACT ON WIRE AND CONNECTED TO EMERGENCY LIGHT ON PANEL 172CR, IAW CRJ 900 ESPM 20-26-00. OPERATIONS TEST GOOD, IAW CRJ 900 AMM 33-51-00-710-802-A16.
Part: SKIN — DENTED (RUDDER) · airframe 28,576 hrs · 19,184 cycles
INTERNAL RUDDER BAYS, BELOW PCU ATTACH POINTS PAINT DISBONDED FROM INTERNAL SURFACES DUE TO SKYDROL EXPOSURE. REPAIRED RUDDER, IAW MHIRJ EO NR CC670-22001-SNIEO-S01, ENDEAVOR AIRLINES EA'S NR CRJ955-10925, CRJ955-10926, CRJ955-10927 AND CRJ955-10928 REV IR DATED 10/30/2020.
Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 28,576 hrs · 19,184 cycles
AFT CARGO LT OUTBOARD FLOOR SILL BETWEEN FS 985.00 TO FS 1000 IS CORRODED IN SEVERAL LOCATIONS, LT SIDE. CW ENDEAVOR AIR EA CRJ953-10919 REV IR DATED 10-28-20 FOR AFT CARGO OUTBOARD FLOOR SILL BETWEEN FS 985.00 TO FS 1000.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,576 hrs · 19,184 cycles
FLOOR SEAT RAIL AT RBL 9 BEGINNING AT APPROXIMATLEY FS 661.00+32 CORRODED IN 4 LOCATIONS. REMOVED & INSTALLED NEW SEAT TRACK AT FS 661.00+32 RBL 9, IAW REO 670-53-00-342 CRJ 900 SRM 51-40-11, 57-42-02 TASK 51-41-02-001-A01 &CRJ 900 AMM 53-00-17-400-801-A07.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,576 hrs · 19,184 cycles
FLOOR SEAT RAIL AT LBL 9 BEGINNING AT APPROX FS 693.00 CORRODED IN 3 LOCATIONS. REMOVED, REPLACED AND FABRICATED NEW SEAT TRACK AT LBL 9, FS 693.00-830.40 WITH PART NR 20276-288-0-0A, IAW REO 670-53-00-343 REV N DATED 07/16/19 AND CRJ 900 SRM 51-40-11-001-001-A01.
Part: INTERCOSTAL — CORRODED (E/E BAY) · airframe 28,576 hrs · 19,184 cycles
AVIONICS BAY DOOR SURROUND STRUCTURE, FWD INTERCOSTAL BETWEEN FS 349 AND FS 364 AT STGR 27L CORRODED. REMOVED AND INSTALLED NEW INTERCOSTAL AT FS 349-364 AT STR 27L, IAW CRJ 900 SRM 51-42-21-001-001-A01. OPERATIONS CHECK GOOD.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,576 hrs · 19,184 cycles
FLOOR SEAT TRACK ON LBL 27 BETWEEN FS 409 AND FS 477.40 GOUGED AND CHAFED IN SEVERAL LOCATIONS. DAMAGE EXCEEDS ALLOWABLE LIMITS AT FS 409-FS 477, IAW CRJ 900 SRM 53-21-49-101-001-A01. LOCATED AND DRILLED SEAT TRACK, IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW SEAT TRACK, IAW BOMBARDIER REO 670-53-00-343 REV N DATED 2019-07-16 AND IAW AMM 53-00-49-400-801-A01
Part: BRACKET — CORRODED (RT WING TE FLAP) · airframe 28,576 hrs · 19,184 cycles
RT INBOARD FLAP PANEL 684ET IS CHAFED. REPLACED PANEL 684ET, LOCATED HOLES, PER CRJ 900 SRM 51-40-11-001-001-A01.
Part: BRACKET — CORRODED (FWD CARGO BAY) · airframe 28,576 hrs · 19,184 cycles
FWD BAGGAGE BAY DOOR SURROUND STRUCTURE MACHINED BRACKET CORRODED AT APPROX FS 565.00 AND LBL 24.0. REMOVED MACHINED BRACKET AT FS 565 STR LBL 24, IAW CRJ 900 SRM 51-42-22-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED SERVICEABLE MACHINED BRACKET, IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED AND TOPCOATED SERVICEABLE MACHINED BRACKET, IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-42-22-001-001-A01 AND 51-25-16-001-001-A01.
Part: PLATE — CORRODED (FWD CARGO BAY) · airframe 28,576 hrs · 19,184 cycles
FWD BAGGAGE BAY DOOR PLATE CORRODED AT FS 557 AND LBL 3.4. REPLACED FWD BAGGAGE BAY DOOR PLATE, IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: BRACKET — CORRODED (FWD CARGO BAY) · airframe 28,576 hrs · 19,184 cycles
FWD BAGGAGE BAY STRUCUTRE, MACHINED BRACKET CORRODED AT LBL 2.6 AND APPROXIMATELY FS 565. REMOVED & REPLACED MACHINED BRACKET, IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, & 51-42-22-001-001-A01.
Part: ANGLE — CHAFED (CRGO DOOR TRACK) · airframe 28,576 hrs · 19,184 cycles
TWO BRACKETS ON AFT CARGO DOOR TRACKS AREA CHAFED AND GOUGED AT FS 985 AND FS 1047. REMOVED AND FABRICATED NEW FWD AND AFT CLIPS ON AFT CARGO DOOR TRACKS, IAW DWG MM670-35514 AND MM 670-35518 AND SRM 51J-42-21-001-010-A01.
Part: ANGLE — CHAFED (CRGO DOOR TRACK) · airframe 28,576 hrs · 19,184 cycles
TWO BRACKETS ON AFT CARGO DOOR TRACKS AREA CHAFED AND GOUGED AT FS 985 AND FS 1047. REMOVED AND FABRICATED NEW FWD AND AFT CLIPS ON AFT CARGO DOOR TRACKS, IAW DWG MM670-35514 AND MM 670-35518 AND SRM 51J-42-21-001-010-A01.
Part: INTERCOSTAL — CORRODED (E/E BAY) · airframe 28,576 hrs · 19,184 cycles
AVIONICS BAY DOOR SURROUND STRUCUTRE, AFT INTERCOSTAL BETWEEN FS 379 AND FS 394 AT STGR 27R. DAMAGED INTERCOSTAL BETWEEN FS 394 AND FS 409 STR 27R EXCEEDS ALLOWABLE LIMITS, IAW CRJ 900 SRM 53-21-23-101-003-A02. LOCATED AND DRILLED NEW INTERCOSTAL AT STR 27R BETWEEN FS 394 AND FS 409, IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE INTERCOSTAL AT STGR 27R BETWEEN FS 394 AND FS 409, IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: INTERCOSTAL — CORRODED (E/E BAY) · airframe 28,576 hrs · 19,184 cycles
AVIONICS BAY DOOR SURROUND STRUCTURE, AFT INTERCOSTAL BETWEEN FS 379 AND FS 394 AT STGR 27L CORRODED. DAMAGED INTERCOSTAL BETWEEN FS 394 AND FS 394 STR 27L EXCEEDS ALLOWABLE LIMITS, IAW CRJ 900 SRM 53-21-23-101-003-A02. REMOVED INTERCOSTAL AT STR 27L BETWEEN FS 394 AND FS 409, IAW CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE INTERCOASTAL AT FS 394 AND FS 409 STGR 27L, IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 28,576 hrs · 19,184 cycles
FLOOR SEAT RAIL AT RBL 9 BEGINNING AT APPROXIMATELY FS 581.00 CORRODED IN THREE LOCATIONS. REMOVED SEAT TRACK AT RBL 9 FS 581.00. FABRICATED AND INSTALLED NEW SEAT TRACK, IAW BOMBARDIER REO 670-53-00-343, REV N DATED 7/16/19 AND IAW CRJ 900 AMM 53-00-49-400-801-A17.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,576 hrs · 19,184 cycles
FOUND FWD J ANGLE TO BE CORRODED. FWD J CHANNEL FOUND TO BE HEAVILY PITTED AND CORRODED AND REQUIRED REPLACEMENT. REMOVED FWD J CHANNEL, IAW CRJ 900 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW J CHANNEL, IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE J CHANNEL, IAW CRJ 900 SRM 51-42-06.
Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 28,576 hrs · 19,184 cycles
SERVICE DOOR SEAL ANGLE CORRODED BETWEEN FS 319.70 AND 349 AT WL 72. REPLACED CORRODED SERVICE DOOR SEAL STRIKER, IAW CRJ 900 SRM 51-42-06-001-001-A01.
Part: DOOR SILL — CORRODED (AFT CARGO DOOR) · airframe 28,576 hrs · 19,184 cycles
AFT CARGO DOOR LOWER SILL HAS MULTIPLE AREAS OF CORROSION. REMOVED AND INSTALLED NEW LOWER SILL, IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-41-02-001-001- A01.
2018
Part: STOWAGE BOX — BROKEN (COCKPIT) · airframe 23,996 hrs · 15,712 cycles
PILOT OXYGEN MASK QUICK-RELEASE DOOR BROKEN. SWAPPED CA OXYGEN MASK STOWAGE BOX WITH OBSERVER OXYGEN MASK BOX PER A MM 35-11-15. OPS CHECK GOOD. REMOVED AND REPLACED OBSERVERS MASK STOWAGE BOX AND OXYGEN MASK IAW AMM 35-11-15 & 35-11-12. PERFORMED OPERATIONAL TEST OF THE
Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 22,800 hrs · 14,832 cycles
ON APPROACH WITH GEAR DOWN, RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE. AFTER LANDING PERFORMED RESET PROCEDURE AND TAXIED TO THE GATE. MDC CHECKED IAW FIM 32-51-50-810- 802. NO FAULT REPORTED. OPS TESTED IAW AMM 32-51-00. OPS CHECKED GOOD.
Part: OXYGEN BOTTLE — EMPTY (MAIN CABIN) · airframe 22,778 hrs · 14,816 cycles
AFT PORTABLE OXYGEN BOTTLE DEPLETED. REMOVED & REPLACED THE OXYGEN BOTTLE IAW 35-31-61.
2017
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,497 hrs · 14,620 cycles
CAPTAINS SIDE EMERGENCY FLASHLIGHT INOP. REPLACED CAPTAINS SIDE EMER FLASHLIGHT OPS CK GOOD REF AMM 25-61-00.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,492 hrs · 14,614 cycles
LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE AND RT FWD OVERWING EMERGENCY LIGHT INOPERATIVE AND CABIN FWD EMERGENCY DOOR LOWER ON BOTH SIDES AND OVERHEAD OVERWING FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REMOVED THE PS38 BATTERY PACK IAW JC 33-900-701. OPS CHECKED GOOD, NO DEFECT NOTED.
Part: STRAP — BROKEN (FLASHLIGHT) · airframe 22,446 hrs · 14,573 cycles
AFT FA EMER FLASHLIGHT WIRE BROKEN. REPLACED EMERGENCY AFT FLASHLIGHT STRAP IAW AMM 25-61-02. FLASHLIGHT CHECKS GOOD.
Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 22,405 hrs · 14,538 cycles
EMERGENCY LIGHTS FAILED AN OPS CHECK. REPAIRED A WIRE IAW ESPM 20-44-00. OPS TESTED THE ESPU. CHECKED GOOD IAW AMM 33-51-17-710-801. OPS TESTED THE EMERGENCY LIGHT. CHECKED GOOD IAW AMM 33-51-00-710-802.
Part: BEARING — WORN (RUDDER) · airframe 22,405 hrs · 14,538 cycles
RUDDER CENTER LOWER HINGE BEARING HAS EXCESSIVE PLAY. REMOVED AND INSTALLED A NEW BEARING IAW CMM 55-41-27, AND SRM 51-42-21.
Part: SKIN — CHAFED (RUDDER) · airframe 22,405 hrs · 14,538 cycles
LEFT LE OF RUDDER CHAFED ABOVE CENTER HINGE AREA. REMOVED AND REPLACED THE RUDDER SKIN IAW SRM 51-42-06.
Part: FLASHLIGHT — DAMAGED (CABIN) · airframe 22,405 hrs · 14,538 cycles
3RD F/A FLASHLIGHT ASSY ON FWD FACE IS DAMAGED. REMOVED AND REPLACED 3RD F/A FLASHLIGHT ASSY IAW AMM 25-61-02-400-801-A10.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 22,405 hrs · 14,538 cycles
LEFT WING INBD FLAP DENTED ON THE LOWER SURFACE 15 INCHES FROM THE TE EDGE, AND 18 INCHES FROM THE INBD EDGE. REPAIRED THE LEFT FLAP SKIN IAW SRM 57-52-01-201-001-A01, TYPE IV.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 22,405 hrs · 14,538 cycles
LEFT WING, INBD FLAP IS DENTED ON LOWER SURFACE 9 INCHES FROM THE OTBD EDGE AND 11INCHES FROM THE TE. REPAIRED THE FLAP SKIN IAW SRM 57-52-01-200-001-A01 TYPE IV.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 22,405 hrs · 14,538 cycles
LEFT WING INBD FLAP SKIN IS DENTED ON THE LOWER SURFACE 7 INCHES FROM THE TE EDGE, AND 18 INCHES FROM THE INBD EDGE. REPAIRED THE FLAP SKIN IAW SRM 57-52-01-201-001-A01, TYPE IV.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,215 hrs · 14,413 cycles
LIGHT BULBS INOPERATIVE FORWARD EMERGENCY EXIT SIGN. R & R THE BULBS, OPS CHECKED GOOD IAW AMM 33-50-00. OK FOR SERVICE.
Part: LIGHT — DAMAGED (CABIN) · airframe 21,788 hrs · 14,098 cycles
DURING INSPECTION, NOTED THE LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. UPON FURTHER INSPECTION, NOTED LIGHT ASSY PINS WERE FOUND BROKEN OFF. INSTALLED A NEW LIGHT ASSY IAW AMM 33-51-15, OPS CHECKED GOOD.
Part: SMOKE DETECTOR — NO TEST (LAVATORY) · airframe 21,317 hrs · 13,754 cycles
FORWARD LAV SMOKE DETECTOR TEST LIGHT INOPERATIVE. REPOSITIONED FWD LAV SMOKE DETECTOR GREEN LED IAW AMM 26-16-01. CHECKED GOOD.
Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 21,054 hrs · 13,565 cycles
SMOKE AFT LAVATORY WARNING IN FLIGHT. NO SMOKE PRESENT IN AFT LAVATORY. REPLACED LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECKED GOOD
Part: COVER — MISSING (ESCAPE ROPE) · airframe 20,734 hrs · 13,362 cycles
EXIT ROW 12A IS MISSING THE ESCAPE ROPE PANEL COVER. REPLACED EXIT ROW COVER PER AMM 25-63-04. ALL CHECKS GOOD.
2016
Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 20,205 hrs · 12,994 cycles
AFT LAVATORY WARNING, INSPECTED FIRE EXTINGUISHER FOUND NO DEFECTS. REMOVED AND REPLACED AFT LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. AND REMOVED AND REPLACED FIRE CONTROL UNIT IAW AMM 26-10-01. OPS CHECKED PERFORMED IAW AMM 26-10-00. OPS CHECKED NORMAL.
Part: UNKNOWN — ODOR (CABIN) · airframe 20,173 hrs · 12,970 cycles
LOUD SQUEAL FROM LEFT AND BEHIND CAPT LIKE A FAN SEIZING. SLIGHT SMOKE ODOR. COULD NO RECREATE ISSUE DESCRIBED. PERFORMED VISUAL INSPECTION AND OPS CHECK OF THE FOLLOWING SYSTEMS: RECIRCULATION FANS (AMM 21-22-10), TRU (AMM 24-31-01), DISPLAY SUPPLY FAN AND CHECK VALVE (AMM 21-24-12).
Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 19,617 hrs · 12,602 cycles
AFT FA FLASHLIGHT INOPERATIVE. R & R AFT FA FLASHLIGHT IAW AMM 25-61-02. OPS TESTED GOOD.
Part: OXYGEN MASK — LEAKING (FIRST OFFICER) · airframe 19,601 hrs · 12,588 cycles
OXYGEN LOW PRESSURE CAUTION MESSAGE. FOUND THE FIRST OFFICER`S OXYGEN MASK LEAKING. REMOVED AND REPLACED IAW AMM35-11-12. OPS TESTED AND LEAK TESTED GOOD. SERVICED CREW OXYGEN IAW AMM12-16-35. DUST COVER INSTALLED AND SERVICING DOOR SECURED VERIFIED OXYGEN.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 19,539 hrs · 12,552 cycles
INBD FLIGHT SPOILERS AND INBD SPOILERONS CAUTION MSG WHILE DESCENT. PERFORMED SELF-TEST OF THE SPOILER AND STABILIZER CONTROL UNITS IAW AMM TASK 27-61-05-740-801. NO DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.
Part: CONNECTOR — DISCONNECTED (BATTERY CHARGER) · airframe 19,424 hrs · 12,471 cycles
SERVICE DOOR EMERGENCY LIGHT IS INOPERATIVE. FOUND #2 EMERGENCY POWER SUPPLY UNIT BATTERY CHARGER NOT CONNECTED. INSTALLED THE BATTERY CHARGER CONNECTOR P536P1 IAW MM 33-51-17-400-802-A02. SERVICE DOOR EXIT EMERGENCY LIGHTS OPS CHECKED OK IAW MM 33-51-00-710-802-A16. "
Part: DOOR SILL — CORRODED (BS 319-349) · airframe 19,424 hrs · 12,471 cycles
SERVICE DOOR SILL IS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 319 - 349. REMOVED & REPLACED THE DOOR SILL IAW SRM 51-42-06-001-001-A01, AND 51-08-02-001-001-A01.
Part: FRAME — CORRODED (BS 847) · airframe 19,424 hrs · 12,471 cycles
FRAME CORRODED BS 847+32 BETWEEN STRINGERS 26L TO 26R. REPAIRED THE FRAME IAW EA CRJ953-04580.
Part: SEAT TRACK — CORRODED (BS 677-720) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK FROM BS 677 - 720 IS CORRODED AT MULTIPLE AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-11-001-001-A01, AND AMM 53-00-49-000/400-801A07.
Part: FLOOR SUPPORT — CORRODED (BS 280-310) · airframe 19,424 hrs · 12,471 cycles
CABIN FLOOR SUPPORT IS CORRODED AT BS 280 - 310. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-77-00-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 453) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK CORRODED AT BS 453. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A07, SRM 51-40-11-001-001-A01, AND REO 670-53-00-343 REV M.
Part: DOOR SILL — CORRODED (BS 310-349) · airframe 19,424 hrs · 12,471 cycles
PAX DOOR LOWER SILL IS CORRODED BETWEEN BS 310 - 349. REMOVED AND REPLACED THE DOOR SILL. IAW SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01, & AMM 52-11-05-400-801/802 A01.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK FROM BS 744 - 761 IS CORRODED AT MULTIPLE AREAS. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M, AND AMM 53-00-49-400-801-A07.
Part: STIFFENER — CRACKED (NOT REPORTED) · airframe 19,424 hrs · 12,471 cycles
FOUND STIFFENER ANGLE CRACKED. REMOVED & REPLACED THE STIFFENER ANGLE IAW SRM 51-42-06-001-001-A01.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 19,424 hrs · 12,471 cycles
FS 280 BULKHEAD WEB CORRODED. REMOVED AND REPLACED THE BULKHEAD WEB IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-22-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01 AND REO:670-53-11-594 REV.
Part: SEAT TRACK — CORRODED (BS 669-720) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK FROM BS 669 - 720.85 IS CORRODED AT MULTIPLE AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801 A07, SRM 51-40-11-001-001-A01, AND REO 670-53-00-343 REV M.
Part: FRAME — CORRODED (B 265) · airframe 19,424 hrs · 12,471 cycles
BS 265 FRAME LOWER SECTOR IS CORRODED. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED (BS 295-310) · airframe 19,424 hrs · 12,471 cycles
STRINGER 25R BETWEEN BS 295 - 310 IS CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-21-001-001-A01, AND 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK FROM BS 785.15 - 847+16 IS CORRODED AT MULTIPLE AREAS.
Part: INTERCOSTAL — CORRODED · airframe 19,424 hrs · 12,471 cycles
INTERCOSTAL CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW EA 953-04567, SRM 51-42-06-001-001-A01, AND 51-40-11-001-001-A01.
Part: FRAME — CORRODED (BS 295) · airframe 19,424 hrs · 12,471 cycles
BS 295 FRAME LOWER SECTOR IS CORRODED STRINGERS 25L - 25R. REMOVED AND REPLACED IAW REO 670-53-21-799, REV.
Part: SEAT TRACK — CORRODED (BS 847-954) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK AT RBL 9 IS CORRODED BETWEEN BS 847+54 - 954. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A07 AND REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 837-847) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK SEGMENT AT LBL 9 BETWEEN FS 837 TO FS 847+54 HAS AREAS OF CORROSION. FABRICATED, LOCATED, DRILLED, COUNTERSUNK AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M, SRM 51-40-11-01-A01 AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 847-905) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK FROM BS 847 - 905 IS CORRODED AT MULTIPLE AREAS. LOCATED, DRILLED, COUNTERSUNK AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 661-669) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK FROM BS 661+90 - 669 IS CORRODED MULTIPLE AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07, AND REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 693-837) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK AT LBL 9 IS CORRODED BETWEEN BS 693 - 837. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 379-483) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK BS 379 TO 483 HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343 REV M AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 573-661) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK FROM BS 573.10 - 661 IS CORRODED AT MULTIPLE AREAS. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M, SRM 51-40-11-001-001-A01 AND AMM 53-00-49-400-801-A07.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 19,424 hrs · 12,471 cycles
ON REMOVAL OF THE LEFT GUSSET BS 280 J-ANGLE, FOUND THE FLOORBEAM ANGLE CRACKED. REMOVED AND REPLACED FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 905-969) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK FROM BS 905 - 969 IS CORRODED AT MULTIPLE AREAS. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 847-865) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK FROM BS 847+16 - 865 IS CORRODED AT MULTIPLE AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A07, AND REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 661-677) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK FROM BS 661 - 677 IS CORRODED AT MULTPLE AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — DAMAGED (BS 785-847) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK FROM BS 785 - 847 AND IS CORRODED AT MULTIPLE AREAS. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M, AMM 53-00-49-400-801-A07, AND SRM 51-21-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK AT LBL 27 HAS AREAS OF CORROSION BETWEEN BS 485 - 565. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW SRM 51-40-11-001-001-A01, AMM 53-00-49-400-801 AND REO:670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 485-573) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK FROM BS 485 - 573 IS CORRODED AT MULTIPLE AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-11-001-001-A01, AMM 53-00-49-400-801-A01, AND REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (BS 693-837) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK SEGMENT AT RBL 9 IS CORRODED BETWEEN FS 693 TO FS 837. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M, SRM 51-40-11-001-001-A01 AND 53-41-49-101-001-A02.
Part: ANGLE — CORRODED (BS 280) · airframe 19,424 hrs · 12,471 cycles
FS 280 FWD J-ANGLE IS CORRODED. REMOVED & INSTALLED A NEW J-ANGLE IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: FITTING — CORRODED (BS 349) · airframe 19,424 hrs · 12,471 cycles
FRAME DOUBLER FITTING IS CORRODED BS 349 AT WL 72.5 BELOW PAX DOOR ANCHOR FITTING. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-21-001-001-A01 & SRM 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 681-661) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK AT LBL 9 BETWEEN BS 581 TO 661+32 HAS AREAS OF CORROSION. FABRICATED & INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK AT LBL 9 BETWEEN BS 661+32 - 693 HAS AREAS OF CORROSION. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 681-661) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK AT RBL 9 BETWEEN BS 581 - 661+32 HAS AREAS OF CORROSION. FABRICATED & INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343, & AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 661) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK FROM BS 661.8 - 661+9 IS CORRODED AT MULTIPLE AREAS. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M, SRM 51-40-11-001-001-A01, AND AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 661-693) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK AT RBL 9 BETWEEN BS 661+32 - 693 HAS AREAS OF CORROSION. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343, & AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 847-954) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK AT LBL 9 IS CORRODED BETWEEN BS 847+54 - 954. FABRICATED & INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 & AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 565-661) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK BS 565 - 661+8 IS CORRODED AT MULTIPLE AREAS. FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343 REV M, AND SRM 51-41-02-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 837-847) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK AT RBL 9 BETWEEN BS 837 - 847+54 HAS AREAS OF CORROSION. LOCATED, DRILLED AND INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-400-801-A07, 51-40-11-001-001-A01 AND REO 670-53-00-343 REV M.
Part: SEAT TRACK — CORRODED (BS 379) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK BS 379 IS CORRODED. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A07, & 25-31-01-400-801-A08.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,424 hrs · 12,471 cycles
SEAT TRACK AT RBL 9 BETWEEN BS 485 - 581 HAS AREAS OF CORROSION. FABRICATED & INSTALLED A NEW SEAT TRACK IAW REO 670-53-00-343, & AMM 53-00-49-400-801-A07.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 19,424 hrs · 12,471 cycles
AVIONICS BAY DOOR RT INTERCOSTAL FS 364 TO FS 349 CORRODED. REMOVED AND REPLACED IAW SRM 51-42-21-001-001-A01, 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
Part: LIGHT — UNSECURE (CABIN) · airframe 19,180 hrs · 12,301 cycles
EMERGENCY FLOOR TRACK LIGHTING STRIPS NEED SECURING NEAR FWD LAVATORY & LT SIDE OF GALLEY CARTS NEAR BOARDING DOOR. SECURED LOOSE STRIPS IAW AMM 33-51-01.
Part: LIGHT — MISSING (CABIN) · airframe 18,648 hrs · 11,927 cycles
FLIGHT ATTENDANT REPORTS MISSING STRIP OF EMER LIGHTING ON FLOOR NEXT TO LAVATORY DOOR, APPROX 2 FEET LONG. INSTALLED NEW STRIP OF EMER LIGHTING NEXT TO LAVATORY DOOR IAW AMM 33-51-01.
Part: GLOWSTRIP — LOOSE (CABIN) · airframe 18,347 hrs · 11,734 cycles
PHOTO LUMINESCENT EMER PATH STRIP IN FRONT OF FWD LAVATORY DOOR COMING LOOSE. REATTACHED EMER PATH STRIP IN FRONT OF FWD LAVATORY AS REQUIRED.
2015
Part: DOOR SEAL — MISALIGNED (ESCAPE HATCH) · airframe 17,807 hrs · 11,359 cycles
WATER LEAKING BETWEEN LT SIDE WINDOW & LT FRONT WINDSHIELD, CARPET IS SOAKED, PLANE HAS BEEN SITTING IN RAIN FOR SEVERAL HOURS. FOUND ESCAPE HATCH OUTER SEAL SLIGHTLY MISALIGNED CAUSING MINOR WATER LEAKAGE ONTO COCKPIT SIDE POST. RESEALED ESCAPE HATCH WITH NO FURTHER LEAKAGE NOTED. ALL RESIDUAL WATER REMOVED IAW AMM 52-22-02.
Part: LIGHT — UNSECURE (CABIN) · airframe 17,571 hrs · 11,186 cycles
FLIGHT ATTENDANTS REPORT A SMALL SECTION OF EMER FLOOR TRACK LIGHTING NOT SECURE TO FLOOR IN FRONT OF SEAT 13B. SECURED EMER FLOOR TRACK IAW AMM 33-51-01. CHECKED GOOD. OK FOR SERVICE.
Part: ACM — MALFUNCTIONED (AC BAY) · airframe 17,566 hrs · 11,181 cycles
ON SHORT FINAL, PACK 1 DUCT TEMP WENT TO 44 C IN AUTO MODE WITH FULL COLD SET. NOTICED SULFUR TYPE SMELL IN COCKPIT. WENT TO MANUAL MODE DUCT TEMP SHOT UP TO 87 C, WITH FULL COLD SELECTED. DEFERRED LT PACK IAW MEL 21-51-1B. INSTALLED PLACARD, MM02 UPDATED & MXC 4632 NOTIFIED. R & R LT ACM IAW JC 900-21-310-902. OPERATIONS CHECKED & LEAK CHECK GOOD. DM 3198372-1 CLEARED. PLACARD REMOVED & MOC NOTIFIED 95770.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,371 hrs · 11,042 cycles
MAIN CABIN EMER LIGHTS DON'T ILLUMINATE. CHECKED & RELAMPED AS REQUIRED. OPERATIONS CHECKED GOOD IAW AMM 33-51-15.
Part: STRIP — LOOSE (CABIN) · airframe 17,371 hrs · 11,042 cycles
12 A & B FLOOR STRIP CAME LOOSE. SECURED FLOOR STRAP IAW AMM 33-51-01.
Part: LIGHT — UNSECURE (CABIN) · airframe 17,288 hrs · 10,980 cycles
EMERGENCY LIGHT FLOOR STRIP DEGRADED NEXT TO ROW 12 - 13 AB AS REPORTED BY FLIGHT ATTENDANT. SECURED EMER FLOOR TRACK LIGHT AT ROW 12 - 13 AB IAW AMM 33-51-01.
Part: FIRE LOOP — SHORTED (NOT REPORTED) · airframe 17,114 hrs · 10,852 cycles
FIRE SYS FAULT MESSAGE ILLUMINATED INFLIGHT & REMAINED ON WHEN ON THE GROUND. FOUND LOOP A238 SHORTED TO GROUND. ADJUSTED AS REQUIRED & OPS CHECKED GOOD IAW AMM 26-10-00.
Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 16,980 hrs · 10,752 cycles
FIRE SYS FAULT STATUS MSG DURING TAKEOFF ROLL. COULD NOT DUPLICATE FAULT, NO MSGS IN MDC CURRENT OR HISTORY. OPERATIONS CHECKED FIRE SYS IAW AMM 26-10-00. ALL CHECKED GOOD.
Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 16,086 hrs · 10,133 cycles
SMOKE AFT LAVATORY WARNING ON DESCENT. PULLED CB'S IAW EMER NON-NORMAL CHECKLIST. AFT SMOKE ALARM WAS ON BUT NO SMOKE. WARNING WENT OFF BEFORE LANDING. COMPLETED SMOKE FUMES SMOKE TOILET WORK SCOPE, NO DEFECTS FOUND. PERFORMED OPERATIONS TEST OF AFT LAVATORY SMOKE DETECTION SYS IAW AMM 26-16-00. OPERATIONS TESTED OK. OK FOR SERVICE.
2014
Part: SKIN — DENTED (TE FLAP) · airframe 14,855 hrs · 9,330 cycles
TASK CARD 900-57-680-302 RT WING INBD FLAP LOWER SURFACE HAS 2 DENTS. REPAIRED RT WING INBD FLAP LOWER SURFACE DENT AT FLS 46.5 IAW SRM 57-52-01-201-001-A01. TYPE IV & EOR57184 DENT AT FLS 34, 1.1 INCHES FROM RIB, 11.2 INCHES FROM TE MEASURING 1.12 INCHES X 1.12 INCHES X 0.036 INCHES DIAMETER IS WITHIN SRM 57-52-01-101-001-A01. ENTERED INTO SCRATCH & DENT LOG.
Part: CHANNEL — CRACKED (FUSELAGE) · airframe 14,855 hrs · 9,330 cycles
TASK CARD CRJ900 C1 PANEL SHEET AFT WING TO BODY FAIRING 196DR HAS CRACK IN JOINT STRAP EXTRUSION. REMOVED CHANNEL IAW SRM 51-42-10-001-001-A01. FABRICATED NEW CHANNEL FROM 2024-T3. .63 INCHES IAW SRM 51-24-21-001-001-A01. INSTALLED NEW CHANNEL ON FAIRING 1960R EXTRUSION IAW SRM 51-42-13-001-001-A01.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 14,855 hrs · 9,330 cycles
TASK CARD 900-52-830-300 PAX DOOR AFT DRAG ANGLE POSSIBLE CRACK. REPAIRED PAX DOOR AFT DRAG ANGLE IAW SRM 52-11-04-201-002-A01, SECTION 4 & 51-42-10-001-001-A01.
Part: FIRESHIELD — DAMAGED (NR 2 COWLING) · airframe 14,855 hrs · 9,330 cycles
TASK CARD 90-26-440-100 NR 2 ENG LOWER CORE COWL FIRE SHIELD BETWEEN DRAIN PAN & ACOC VENT. REPAIRED NR 2 ENG LOWER CORE COWL FIRE SHIELD CHAFE IAW EO R54090.
Part: RUB STRIP — CHAFED (NR 1 COWLING) · airframe 14,855 hrs · 9,330 cycles
TASK CARD 900-26-430-100 NR 1 ENG LOWER CORE COWL EXHAUST COWL RUB STRIP CHAFED OTBD END. REPAIRED NR 1 ENG LOWER CORE COWL RUB STRIP IAW SRM 54-23-00-201-007-A01.
Part: SKIN — DENTED (PAX DOOR) · airframe 14,855 hrs · 9,330 cycles
TASK CARD 900-52-830-300 PAX DOOR HAS A DENT ON THE RT SIDE INNER SKIN BY THE TOP STEP. REPAIRED DENT ON PAX DOOR RT SIDE AFT IAW EACRJ952-02735 REV 1R.
Part: RUB STRIP — CHAFED (NR 2 COWLING) · airframe 14,855 hrs · 9,330 cycles
TASK CARD 90-26-440-100 NR 2 ENG LOWER CORE COWL EXHAUST COWL RUB STRIP CHAFED OTBD END. REPAIRED NR 2 ENG LOWER CORE COWL RUB STRIP IAW SRM 54-23-00-201-007-A01.
Part: RUB STRIP — CHAFED (NR 2 COWLING) · airframe 14,855 hrs · 9,330 cycles
TASK CARD 90-26-440-100 NR 2 ENG UPPER CORE COWL EXHAUST COWL RUB STRIP CHAFED OTBD END. REPAIRED NR 2 ENG UPPER CORE COWL RUB STRIP IAW SRM 54-23-00-201-007-A01.
Part: SKIN — DENTED (PAX DOOR) · airframe 14,855 hrs · 9,330 cycles
TASK CARD 900-52-830-300 PAX DOOR HAS A DENT ON THE LT SIDE INNER SKIN BY THE TOP STEP. REPAIRED DENT ON PAX DOOR LT FWD SIDE IAW EA CRJ 952-02734 REV 1R.
Part: RACK — BENT (CARGO BAY) · airframe 14,855 hrs · 9,330 cycles
TASK CARD 900-25-280-101 AFT BAGGAGE COMPARTMENT WIRE RACK OTBD END IS BENT. REPAIRED WI-FI RACK OTBD END IAW EA CRJ946-02733.
Part: COWLING — DAMAGED (NR 2 ENGINE) · airframe 14,855 hrs · 9,330 cycles
TASK CARD 900-26-440-100 NR 2 ENG AFT CORE COWL SHOWS WEAR DAMAGE AT PYLON INTERFACE AREA. REPAIRED NR ENG AFT CORE COWL IAW THE FOLLOWING SRM'S 54-13-00-201-006-A01, 51-20-006-250-A01, 51-40-91-001-001-A01, 51-24-26-001-001-A01 & 51-42-13-001-A01.
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 14,797 hrs · 9,289 cycles
PREFLIGHT SAFETY EQUIPMENT CHECK FWD FLIGHT ATTENDANT & FIRST OFFICER EMER FLASHLIGHTS NOT FLASHING, DEFERRED IAW MEL 25Â61Â4A. UPDATED & PLACARD INSTALLED. R & R FLIGHT ATTENDANT & FIRST OFFICERS EMER FLASHLIGHT IAW AMM 25-61-02. THIS CLEARS MEL 3079347-1.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 14,757 hrs · 9,267 cycles
AFTER TAKEOFF STEERING INOPERATIVE CAUTION DISPLAYED FOLLOWED NON-NORMAL E AFTER LANDING, DID THE FAULT RESET PROCEDURE & MSG WENT AWAY. 1ST OCCURRENCE PER MX CONT. NO CORRECTIVE ACTION REQUIRED IAW POM SECTION 4-2 01. TROUBLE SHOT SYS BY ACCESSING MDC FAULT HISTORY. WHICH GENERATED A B1 CODE 007464. TROUBLE SHOT IAW FEM TASK 32-51-50-810-801. NO MSGS DISPLAYED. PERFORMED OPERATIONS IAW AMM TASK 32-51-00-710-801. OPERATIONS CHECKED GOOD.
2013
Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 13,536 hrs · 8,467 cycles
DURING MGMT REQUEST FOR ANTI-ICE DUCT WARNING PANEL 171CL WIRE BROKE OFF AFT EMERGENCY LIGHTS. REPAIRED WIRING, REPLACED CONTACTS PN 001104-20002. INSTALLED & SECURED PANEL, OPERATIONS CHECKED GOOD IAW AMM 51-51-00.
Part: SEAL — BROKEN (PBE) · airframe 12,609 hrs · 7,889 cycles
FLIGHT DECK PBE HAS LOST ITS VACUUM SEAL. REPLACED CAPTS PBE IAW JC 900-25-900-902.
Part: WARNING LIGHT — ILLUMINATED (LT A/C PACK) · airframe 12,354 hrs · 7,733 cycles
LT A/C PACK AUTO FAIL CAUTION DISPLAYED. CAPTAIN SAYS THERE WAS A LITTLE SMOKE IN THE CABIN, CAUSED BY THE LT PACK CAUTION.
Part: A/C PACK — OVERHEATED (LEFT)
2500 FT ON APPROACH, BOTH PILOTS SUDDENLY SMELLED AND SAW SMOKE. DECLARED AN EMERGENCY WHILE CONTINUING APPROACH. ON LANDING, THEY EXECUTED EMERGENCY NON-NORMAL AND CHECKED THE ECS SYNOPTIC PAGE. FOUND LT PACK HAD POSTED A FAILED AUTO SHUTDOWN MESSAGE AND PACK WAS SHOWING A TEMP OF 99 DEGREES. ON GROUND SCANNED THE ACFT AND DID NOT FIND ANY HEAT SOURCES. SMOKE STARTED TO DISSIPATE ONCE LEFT PACK WAS SHUTDOWN.
2011
Part: LIGHT — MISSING (CABIN) · airframe 7,727 hrs · 4,841 cycles
GALLEY FLOOR TRACK EMERGENCY LIGHTING STRIP MISSING. PILOT LOCATED ORIGINAL EMERGENCY LIGHTING STRIP AND ORIGINAL STRIP RESECURED.
Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 7,172 hrs · 4,494 cycles
UPON DEPARTURE, RECEIVED A "GEAR DISAGREE" WARNING. RETURNED TO BDL AFTER BURNING FUEL TO PREVENT OVERWEIGHT LANDING. ACCESSED CURRENT FAULTS SHOW 005968 NO GEAR MOVEMENT. DEFERRED LANDING GEAR RETRACTION STS IAW MEL 32-30-1A. MX PROCEDURES C/W. REPLACED LANDING GEAR SELECTOR VALVE IAW AMM 32-32-10 CHECKED GOOD.
2010
Part: LIGHT — DAMAGED (CABIN) · airframe 5,894 hrs · 3,747 cycles
ROUTINE-900, THE LT FLOOR EMERGENCY LIGHTING STRIP IN THE GALLEY AREA IS DAMAGED. INSTALLED SERVICEABLE LIGHT STRIP IN THE GALLEY IAW AMM 33-51-01-400-801.
Part: SKIN — CHAFED (FUSELAGE) · airframe 5,894 hrs · 3,747 cycles
CHAFE ON BELLY SKIN CAUSED BY BELLY FAIRINGS 195DL AND 196DR AT AFT END. REPAIRED SKIN IAW REO670-53-00-014 AND MODSUM NR IS670538200021.
Part: LIGHT — SMOKE (CABIN) · airframe 5,392 hrs · 3,458 cycles
F/A & PASSENGER SAW SMOKE AND FUMES COMING FROM LT SIDE OF CABIN ROW 7A&B. FUMES DISSIPATED ON DESCENT. LANDED ARFF CHECKED OUT. TAXIED TO GATE. FUMES AND SMOKE BECAME NOTICEABLE AROUND 18000 FT & DISSIPATED THROUGH DESCENT. PERFORMED OPS TEST OF ALL CABIN INT LIGHTING IAW AMM 33-21-00. FOUND 1 PAX READ LIGHT INOP REF NR 21. DROPPED ALL PSU'S AND OPS CHECKED AND INSPECTED PCBS. NO DEFECTS. INSPECTED ALL CONNECTORS FROM ROWS 4-11. NO DEFECTS. REMOVED CEILING PANELS & INSPECTED ACCENT AND EMERGENCY AND OVERHEAD LIGHT STRIPS. NO DEFECTS (ROWS 4-11). INSPECTED AND TESTED ALL LAV (FORE AND AFT) AND GALLEY EQUIPMENT. ALL OPS CHECK GOOD. INSPECTED AVIONICS COMPARTMENT. NO DEFECTS NOTED. FOUND ACFT TO BE OK FOR SERVICE.