N904FJ
Registered owner: SKYWEST AIRLINES INC, UT (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.
308 reports on file, 2003-10-04 – 2022-10-27.
Part: BATTERY PACK — DISCHARGED (AFT FLASHLIGHT) · airframe 44,379 hrs · 34,843 cycles
AFT FA FLASH LIGHT IS NOT BLINKING. R/R BATTERY, OPS CHK GOOD.
Part: BATTERY PACK — DISCHARGED (MEGAPHONE) · airframe 44,379 hrs · 34,843 cycles
MEGAPHONE WILL NOT TEST PROPERLY. R/R BATTERY, OPS CHK GOOD.
Part: BULB — INOPERATIVE (ZONE 200) · airframe 44,276 hrs · 34,757 cycles
ROW 14 D/F MID LVL EXIT SIGN (2) BULBS INOP REPLACED BULBS
Part: NONE — NONE · airframe 43,997 hrs · 34,564 cycles
CEILING LEVEL EMERGENCY FLOOD LIGHT AT ROW 18 INOP. PLACED ON MEL.
Part: NONE — NONE · airframe 43,914 hrs · 34,910 cycles
L PACK ODOR - DEFERRED LH PACK
Part: NONE — NONE · airframe 43,659 hrs · 34,320 cycles
PAX ENTRY SIDEWALL EMER EXIT LIGHT INOP (FLOODLIGHT). PLACED ON MEL.
Part: BULB — INOPERATIVE (ZONE 200) · airframe 43,513 hrs · 34,123 cycles
13F LWR LVL EXIT SIGN 2 BULBS INOP REPLACED BULBS
Part: NONE — NONE (BOTTOM STEP/PNL) · airframe 43,484 hrs · 34,205 cycles
THE L 1 DOOR ACCESS PANEL 832AT BOTTOM STEP WAS FOUND WITH WEAR DAMAGE IN THE SETTLEMENT AREA. PERFORMED PERM REPAIR IAW CRJ700/900 STRUCTURAL REPAIR MANUAL (SRM) 52-11-04-001-001-A01 ITEM 30 (REV.38 DATED JUL.25, 2020).
Part: TRANSCOWL — CRACKED (RH UPPR TRANSCOW) · airframe 43,484 hrs · 34,205 cycles
THE RH UPPER TRANSCOWL WAS FOUND TO HAVE CRACK DAMAGE TO THE OUTER SKIN. PERFORMED PERM REPAIR IAW CRJ?00/900 STRUCTURAL REPAIR MANUAL (SRM) 54-21-05, FIGURE 54-21-05-991-801, ITEM 1 (REV.38 DATED JUL. 25, 2020).
Part: NONE — CORRODED (LH WING) · airframe 43,484 hrs · 34,205 cycles
SLAT TRACKS 2-3 (P/N: CC670-12062-7) ON THE LH WING WAS FOUND TO HAVE CORROSION DAMAGE ON THE UPPER FACES. PERFORMED PERM REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIGURE 5, ITEM 105,(REV. 70 DATED, 10 AUG 2021).
Part: NONE — CORRODED (LH WING) · airframe 43,484 hrs · 34,205 cycles
SLAT TRACKS 3-1 (P/N: CC670-12072-7) AND TRACK 3-2 (P/N: CC670-12081-9) ON THE LH WING WAS FOUND TO HAVE CORROSION DAMAGE ON THE UPPER FACES. PERFORMED PERM REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPG) 27-81-41, FIGURE 10, ITEM15,AND 90 (REV. 70 DATED 10 AUG 2021 ).
Part: EXHAUST CONE — DENTED (SKIN/AFT CONE) · airframe 43,484 hrs · 34,205 cycles
MAINTENANCE DISCOVERED TWO DENTS AFFECTING THE SKIN AFT CONE (P/N: WA670-30701-1). PERFORMED PERM REPAIR IAW CRJ700/900 STRUCTURAL REPAIR MANUAL (SRM) 53-85-00-001-002-A01, ITEM 1.
Part: NONE — NONE (LWR RH FAN CWL D) · airframe 43,484 hrs · 34,205 cycles
THE RH LOWER FAN COWL DOOR WAS FOUND TO HAVE 10 EA. ELONGATED COUNTERSINKS AND FASTENER HOLES ALONG THE EDGE OF THE OUTER SKIN PANEL AND AFT EDGE MEMBER. PERFORMED PERM REPAIR IAW CRJ700/900 STRUCTURAL REPAIR MANUAL (SRM) 54-14-01, FIGURE 54-14-01-991-801, ITEMS 1A,7 (REV.38 DATED JUL. 15, 2020).
Part: SKIN — CORRODED (STA.305TO315&STG) · airframe 43,484 hrs · 34,205 cycles
THE FUSELAGE SKIN AT STGR 21R AND BETWEEN STA 305 TO 315 WS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERM REPAIR IAW CRJ900 STRUCTURAL REPAIR MANUAL (SRM) 53-21-01-001-002-A01, FIGURE 53-21.-01-991-802, ITEM 1.
Part: NONE — DENTED (FLS 48.00) · airframe 43,484 hrs · 34,205 cycles
THE INBOARD FLAP LOWER SKIN OF THE RH WING WAS FOUND WITH A DENT AT FLS 48.00. PERFORMED PERM REPAIR IAW CRJ700/900 STRUCTURAL REPAIR MANUAL (SRM) 57-52-01, ITEM 28A, D (REV.38 DATED JULY 9TH, 2021 ).
Part: NONE — CRACKED (AFT SVC DOOR PLU) · airframe 43,484 hrs · 34,205 cycles
THE REPAIR AFT IAW SERVICE CRJ?00/900 DOOR PLUG STRUCTURAL INNER SKIN REPAIR (P/N: MANUAL CC690-38511-1) (SRM) WAS 53-51-01-001-005-A01 FOUND TO HAVE ITEM (2) 2, "SKIN, CRACKS. AFT PERFORMED SERVICE DOOR PERM PLUG-STRUCTURAL IDENTIFICATION" (REV.38 DATED JUL. 25, 2020).
Part: NONE — CORRODED (LH WING) · airframe 43,484 hrs · 34,205 cycles
SLAT TRACKS 1-1 (P/N: CC670-12010-5} AND 1-2 (P/N: CC670-12021-9) AND 1-3 (P/N: CC670-12030-3} ON THE LH WING WERE_ FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND /OR LOWER SURFACES. PERFORMED PERM REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIGURE 1, ITEM 40A, 80, AND 100A (REV. 70 DATED 10 AUG 2021).
Part: NONE — CORRODED (RH WING) · airframe 43,484 hrs · 34,205 cycles
SLAT TRACKS 3-1 (P/N: CC670-12070-3) AND 3-2 (P/N: CC670-12081-7) ON THE RH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND /OR LOWER SURFACES. PERFORMED PERM REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIGURE 10, ITEM 10A AND 85 (REV. 70 DATED 10 AUG 2021 ).
Part: NONE — CORRODED (LH ENG INLET COW) · airframe 43,484 hrs · 34,205 cycles
THE LH INLET COWL LIPSKIN WAS FOUND TO HAVE EROSION DAMAGE AND WAS BLENDED OUT PER SRM 54-11-05-101-001-A01. PERFORM PERM REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUEL (SRM) 54-11-05, FIGURE 54-11-05-991-801, ITEM 1 (REV.37 DATED AUG. 15, 2019).
Part: NONE — NONE (WING AI DUCT &SH) · airframe 43,484 hrs · 34,205 cycles
THE WING ANTI ICE (WAI) RH SUPPLY DUCT SHIELD (PN-9911996-102) EXTERIOR SURFACE. PERFORMED PERM REPAIR IAW_ CRJ900 AIRCRAFT ILLUSTRATED PARTS CATALOG (AIPC) 30-11-04-01, FIGURE 1, ITEM 30 & 33 (REV71 DATED 1/17/2022).
Part: NONE — CORRODED (RH WING) · airframe 43,484 hrs · 34,205 cycles
SLAT TRACKS 2-1 (P/N: CC670-12040-3) AND 2-2 (P/N: CC670-12051-9) ON THE RH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND /OR LOWER SURFACES. PERFORMED PERM REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIGURE 5, ITEM 15 AND 85 (REV. 70 DATED 10 AUG 2021).
Part: NONE — CORRODED (RH WING) · airframe 43,484 hrs · 34,205 cycles
SLAT TRACKS 1-1 (P/N: CC670-12010-5) AND 1-2 (P/N: CC670-12021-9) AND 1-3 (P/N:CC670-12030-3) ON THE RH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND /OR LOWER SURFACES. PERFORMED PERM REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIGURE 10, ITEM 15 AND 90 (REV. 70 DATED 10 AUG 2021).
Part: SKIN — CORRODED (FUSELAGE) · airframe 43,484 hrs · 34,205 cycles
IN REF NRC S/N 00352, DURING STRINGER 21RH REMOVAL, CORROSION ON INTERNAL FUSELAGE SKIN WAS FOUND BTW FS 305-315 (SETTLEMENT AREA OF STRG 21R). IT WAS REPAIRED PER EA 81-2022-044 REV. IR
Part: STRINGER — CORRODED (E/E) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON STRINGER 21 RH BTW FS295-FS333, AT MAIN E/E COMPARTMENT. STRINGER 21 RH BTW FS280 TO FS333 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01
Part: STRINGER — CORRODED (E/E) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON STRINGER 23 RH BTW FS319.5-FS333, AT MAIN E/E COMPARTMENT. STRINGER 23 RH BTW FS319.5-FS333, AT MAIN E/E COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-00-03-201-001-A02
Part: NONE — CORRODED (E/E COMPARMENT) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON STRINGER 19RH BTW FS295-FS330, AT MAIN E/E COMPARTMENT. CORRECTIVE ACTION: STRINGER 19RH BTW FS295-FS330 WAS REPLACED PER CRJ900 SRM 53-00-03-201-001-A02.
Part: NONE — NONE (RH ENG UPPR TRAN) · airframe 43,484 hrs · 34,205 cycles
THE RH ENGINE UPPER TRANSCOWL LATCH DOOR (PN-CN624-2021-901) WAS FOUND TO HAVE WEAR ON THE SURROUND LANDING AT THE FREE EDGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 (SRM) TASK 54-21-05-003-A01, (REV. 38 DATED 9JUL2021). (SUPPLEMENTAL)
Part: NONE — CORRODED (RH ENG UPPR TRAN) · airframe 43,484 hrs · 34,205 cycles
THE RH ENGINE UPPER TRANSCOWL LATCH DOOR (PN-CN624-2021-901) WAS FOUND TO HAVE CORROSION ON THE SURROUND LANDING AT THE FREE EDGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 (SRM) TASK 54-21-05-003-A01, (REV. 38 DATED 9JUL2021 ).
Part: NONE — NONE (RH AILERON-AS343) · airframe 43,484 hrs · 34,205 cycles
THE RH AILERON CENTER HINGE ASSEMBLY WAS DISCOVERED TO HAVE TOOL MARKS DURING THE REMOVAL OF THE PCU ATTACH LINK BOLT AT AS343.53. PERFORMED PERMANANT REPAIR IAW CRJ700/900 ILLUSTRATED PARTS CATALOG {IPC) 57-60-00, FIGURE 1, ITEM 146 (REV.37 DATED AUG. 15, 2019).
Part: NONE — NONE (AFT SERVICE DOOR) · airframe 43,484 hrs · 34,205 cycles
THE AFT SERVICE DOOR LOWER BEAM WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ700/900 SRM 52-46-06-001-001-A01 ITEM 45 (REV. 38 DATED JUL. 25, 2020).
Part: FLAP — DENTED (LH WING FS235.96) · airframe 43,484 hrs · 34,205 cycles
A DENT WAS FOUND AFFECTING THE SKIN THE LOWER SKIN ON LEFT OUTBOARD FLAP ALONG THE AFT EDGE. .PERFORMED A PERMANENT REPAIR IAW CRJ900 SRM 57-52-01, FIGURE 57-53-01-001-001-A01, ITEM 3. DEFECT LOCATION: LH WING, FS235.96-245.84
Part: NONE — DENTED (INBOARD SKIN PAN) · airframe 43,484 hrs · 34,205 cycles
EIGHT DENTS WERE REPORTED AFFECTING THE LH ENGINE INBOARD INLET COWL AT THE 5 TO 7 O'CLOCK POSITION LOOKING FORWARD ON THE OUTER INBOARD SKIN. PERFORMED A PERMANENT REPAIR IAW CRJ700/900 SRM 54-11-01-001-002-A01 FIGURE 54-11-01-991-802 ITEM (REV. 37 DATED 24 FEB 2021 ).
Part: NONE — CORRODED (RH WING) · airframe 43,484 hrs · 34,205 cycles
PITTING CORROSION ON SLAT TRACKS: 1-1, 1-3, 3-1 AT UPPER SURFACE; SLAT TRACK 1-2 & 2-2 AT LOWER SURFACE; SLAT TRACK 2-1 & 3-2 AT UPPER/LOWER SURFACE FOR RH WING.| CORRECTIVE ACTION: SLAT TRACKS WAS PERFORMED PER EA 81-2022-038 REV IR.EA 81-2022-039 REV IR AND EA 81-2022-037 REV IR
Part: TRIPLER — WORN (REAR FUSELAGE) · airframe 43,484 hrs · 34,205 cycles
WEAR ON TRIPLER SKIN SKIN (PREVIOUS REPAIR) LOCATED BTW FS969-985 FS969 & SGTR 26L-26R, REAR FUSELAGE (4 LOCATIONS). CORRECTIVE ACTION: TRIPLER SKIN SKIN (PREVIOUS REPAIR) LOCATED BTW FS969-985 FS969 & SGTR 26L-26R, REAR FUSELAGE WERE REPAIRED PER REO 690-53-00-313 REV. -
Part: NONE — CRACKED (COCKPIT) · airframe 43,484 hrs · 34,205 cycles
INITIAL INSPECTION: CRACK ON COCKPIT FLOOR LONGITUDINAL BEAMS (LBL 12/RBL 12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT | BEAMS (LBL 12/RBL 12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER CRJ 900 SRM 53-11-43-201-003-A01.
Part: NONE — CORRODED (LH WING) · airframe 43,484 hrs · 34,205 cycles
PITTING CORROSION ON SLAT TRACK: 1-1, 1-2, 1-3 & 2-3 AT UPPER/LOWER SURFACE; SLAT TRACK 2-3, 3-1 & 3-2 AT UPPER SURFACE, FOR LH WING |CORRECTIVE ACTION: SLAT TRACKS WAS PERFORMED PER EA 81-2022-040 REV IR, EA 81-2022-041 REV IR AND EA 81-2022-042 REV IR
Part: NONE — CORRODED (PAX CABN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 483.00 - FS 573.00 | LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 483.00 - FS 573.00 WAS REPLACED PER CRJ-900 AMM 53-00-49
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 379.00 - FS 483.00. | CORRECTIVE ACTION: SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 379.00 - FS 483.00 WAS REPLACED PER CRJ 900 AMM 53-00-49
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 483.00 - FS 573.00. RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 483.00 - FS 573.00 WAS REPLACED PER CRJ900 AMM 53-00-49
Part: NONE — CORRODED (PAX CA BIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 573.00 - FS 661.00+14. RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 573.00 - FS 661.00+14 WAS REPLACED PER CRJ900 AMM 53-00-49
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 573.00 - FS 661.00+14 | LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 573.00 - FS 661.00+14 WAS INSTALLED PER CRJ900-AMM-53-00-49
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 847.00+14 - FS 907.00| H SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 847.00+14 - FS 907.00 WAS REPLACED PER CRJ 900 SRM 53-0044
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON FLOOR SEAT RAIL AT LBL 27.00 BETWEEN FS 349.50 - FS 485.00| FLOOR SEAT RAIL AT LBL 27.00 BETWEEN FS 349.50 - FS 485.00 AS REPLACED PER CRJ900 AMM 53-00-49
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 672.00 - FS 772.00 |LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 672.00 - FS 772.00 WAS REPLACED PER CRJ900 AMM 53-00-49
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 379.00 - FS 483.00 |LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 379.00 - FS 483.00. WAS REPLACED PER CRJ-900 AMM 53-00-49
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 743.00 - FS 763.00. LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 743.00 - FS 763.00 WAS REPLACED PER CRJ900 AMM 53-00-49
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 661.00+90 - FS 672.00 | LH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 661.00+90 - FS 672.00 WAS REPLACED PER CRJ-900 AMM 53-00-49
Part: PLATE — CORRODED (ACCESS PANEL 814) · airframe 43,484 hrs · 34,025 cycles
CORROSION AND GOUGE ON ACCESS PANEL 814FZ (SERVICE DOOR LATCH COVER) ACTION ACCESS PANEL 814FZ WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON FLOOR SEAT RAIL AT LBL 9.00 BETWEEN FS 374.00 - FS 485.00 CORRECTIVE ACTION: FLOOR SEAT RAIL AT LBL 9.00 BETWEEN FS 374.00 - FS 485.00 WAS REPLACED PER CRJ900 AMM 53-00-49
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON FLOOR SEAT RAIL AT LBL 9.00 BETWEEN FS 485.00 - FS 581.00 | CORRECTIVE ACTION: FLOOR SEAT RAIL AT LBL 9.00 BETWEEN FS 485.00- FS 581.00 WAS REPLACED PER CRJ900 AMM 53-00-49
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON FLOOR SEAT RAIL AT LBL 9.00 BETWEEN FS 581.00- FS 683.50 CORRECTIVE ACTION: FLOOR SEAT RAIL AT LBL 9.00 BETWEEN FS 581.00 - FS 683.50 WAS REPLACED PER CRJ900 AMM 53-00-49
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON FLOOR SEAT RAIL AT RBL9 BTW FS 597.00 - FS 661 CORRECTIVE ACTION: FLOOR SEAT RAIL AT RBL9 BTW FS 597.00 - FS 661 WAS REPLACED PER CRJ-900 AMM 53-00-49.
Part: NONE — CORRODED (PAX CABIN) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 847.00+14 - FS 867.00 | RH SIDE SEAT RAIL AT WL 85.25 BETWEEN FS 847.00+14 - FS 867.00 WAS REPLACED PER CRJ 900-53-00-49
Part: NONE — CORRODED (E/E) · airframe 43,484 hrs · 34,205 cycles
CORROSION ON INTERNAL FUSELAGE SKIN WAS FOUND BTW FS 305-315 (SETTLEMENT AREA OF STRG 21R) CORROSION ON INTERNAL FUSELAGE SKIN WAS FOUND BTW FS 305-315 (SETTLEMENT AREA OF STRG 21R) WAS REPAIRED PER EA 81-2022-044 REV. IR
Part: NONE — NONE · airframe 43,480 hrs · 34,202 cycles
14A FLOOR LEVEL EXIT SIGN HAS ONE BULB INOP- RELAMPED
Part: NONE — NONE · airframe 43,289 hrs · 34,068 cycles
LH FWD EXT OVERWING EMER LIGHT LT INOP. PLACED ON MEL
Part: BULB — INOPERATIVE (ZONE 200) · airframe 43,468 hrs · 34,046 cycles
GALLEY EMR LITE INOP PLACED ON MEL
Earlier reports · 2003–2021 · 251 reports
2021
Part: NONE — NONE · airframe 42,746 hrs · 33,684 cycles
ALL BULBS INOP ON 4D EXIT LIGHT. MX CURRENLTY IN WORK T/S.
Part: LIGHT — NO TEST (ROW 18) · airframe 42,409 hrs · 33,441 cycles
ROW 18 CEILING LVL EMER FLOOD LIGHT INOP. PLACED ON MEL.
Part: LIGHT — INOPERATIVE (ROW 11) · airframe 41,623 hrs · 32,870 cycles
ROW 11 CEILING EMERGENCY FLOODLIGHT INOP. PLACED ON MEL.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,279 hrs · 32,627 cycles
EMER EXIT SIGN 14A BULB INOP REPLACED BULB
2020
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,816 hrs · 32,292 cycles
PAX DOOR FLOOR LEVEL EXIT SIGN 1 BULB INOPERABLE, PLACED ON MEL.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 40,437 hrs · 32,014 cycles
AFT EMERGENCY LIGHTS INOPERABLE. CHARGED EPSUS, OPERATIONS NORMAL.
Part: UNKNOWN — VIBRATION (AIRFRAME) · airframe 40,399 hrs · 31,980 cycles
AIRFRAME VIBRATION ABOVE 290 KTS
Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,341 hrs · 31,932 cycles
ROW 18 CEILING FLOOD LIGHT INOP. PLACE ON MEL.
Part: WIRE — BROKEN (CABIN) · airframe 40,333 hrs · 31,922 cycles
ROW 4 F EXIT SIGN INOPERATIVE. REPAIRED BROKEN WIRE.
Part: CONNECTOR — UNSECURE (CABIN) · airframe 40,333 hrs · 31,922 cycles
ROW 14 LOWER EXIT SIGNS INOPERATIVE. RESECURED THE EMERGENCY BATTERY NR 3 CONNECTOR.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,306 hrs · 31,899 cycles
AFT CABIN EMERG LIGHTS INOP - R&R #2/#3 EPSU BATTERY PACKS
2019
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,328 hrs · 31,178 cycles
ROW 14F LOWER EMER EXIT 1 BULB INOP REPLACED BULB
Part: LIGHT — NOT REPORTED (ROW 3) · airframe 39,023 hrs · 30,933 cycles
CEILING EMER LIGHT ROW 3. PLACED ON MEL
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 38,981 hrs · 30,897 cycles
EMER FLOOD LIGHTMROW 9 INOP REPLACED BULB
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 38,852 hrs · 30,793 cycles
AFT FA FLASHLIGHT INOP. REPLACED BATTERY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,460 hrs · 30,489 cycles
ROW 13A LOWER EMER LIGHT INOP. RELAMPED.
Part: DOOR SILL — CORRODED (BS 328-340) · airframe 38,242 hrs · 30,320 cycles
SERVICE DOOR LOWER SILL CORRODED BETWEEN FS 326 AND FS 342.
Part: SEAT TRACK — CORRODED (BS 785-847) · corrosion level 2 · airframe 38,242 hrs · 30,320 cycles
LEFT HAND SIDE SEAT RAIL, FS785.15 - FS847.16, C0ORRODED BEYOND LIMITS. SIDE SEAT RAIL FABRICATED AND REPLACED I.A.W. APPLICABLE BOMBARDIER STRUCTURAL REPAIR MANUALS.
Part: FLOOR SUPPORT — CORRODED (BS 1000-1069.75) · corrosion level 2 · airframe 38,242 hrs · 30,320 cycles
AFT CARGO FLOOR BEAM UPPER SURFACE CORRODED, LBL 9, FS 1000.00 - FS1055.00. REPAIRED FLOOR BEAM I.A.W. BOMBARDIER REO #690-53-61-845,REV --, DATED 2019/05/20.
Part: FRAME — CORRODED (BS 870) · corrosion level 2 · airframe 38,242 hrs · 30,310 cycles
LOWER FRAME SECTOR, @ FS 847.00 & 16, STGR 26L - 26R CORRODED BEYOND ALLOWABLE LIMITS.
Part: FLOOR SUPPORT — CORRODED (BS 992-1055) · corrosion level 2 · airframe 38,242 hrs · 30,320 cycles
PERFORMED A MAJOR REPAIR BY REMOVING THE CORRODED SECTION OF FLOOR BEAM AT FS 1015.00 â 1031.00, LBL 27 AND INSTALLING A NEW BEAM SECTION IAW BOMBARDIER REO 690-53-61-854 REV. â DATED 2019-06-14. REF WVAC JOB 915004101, OP 127.
Part: SEAT TRACK — CORRODED (BS 785-797) · corrosion level 2 · airframe 38,242 hrs · 30,320 cycles
R/H SIDE CABIN SEAT TRACK FS 785.15 TO FS 797 IS CORRODED BEYOND REPAIRABLE LIMITS.
Part: SEAT TRACK — CORRODED (BS 661-677) · corrosion level 2 · airframe 38,242 hrs · 30,320 cycles
R/H SIDE SEAT TRACK FS 661+16 TO FS 677.0 IS CORRODED BEYOND REPAIRABLE LIMITS.
Part: FLOORBEAM — CORRODED (BS 549) · airframe 38,242 hrs · 30,320 cycles
LONGITUDINAL / TRANSVERSE FLOOR BEAMS CORRODED @ FS 549.00 / RBL-9 BEYOND ALLOWABLE LIMITS. REPAIRED BOTH FLOOR BEAMS I.A.W. REO #690-53-31-430, REV --, DATED 2019-06-15.
Part: SEAT TRACK — CORRODED (BS 661-673) · corrosion level 2 · airframe 38,242 hrs · 30,320 cycles
L/H SIDE SEAT TRACK FS 661+16 TO FS 673 CORRODED BEYOND REPAIRABLE LIMITS.
Part: ANGLE — CORRODED (DOOR SILL) · airframe 38,342 hrs · 30,320 cycles
SERVICE DOOR SILL ANGLE CORRODED IN MULTIPLE AREAS FS319 TO FS349
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,242 hrs · 30,320 cycles
SEAT TRACK IS CORRODED AT RBL 9.0 BETWEEN FS 847.00+48 AND FS 977.00.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,242 hrs · 30,320 cycles
SEAT TRACK IS CORRODED AT LBL 9.0 BETWEEN FS 372.00 AND 485.00.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,242 hrs · 30,320 cycles
SEAT TRACK IS CORRODED AT RBL 9.0 BETWEEN FS 693.00 AND 847.00.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,242 hrs · 30,320 cycles
RT SEAT TRACK AT RBL 9.0 IS CORRODED AT FS 661.00+54.
Part: DOOR SILL — CORRODED (BS 319-349) · corrosion level 2 · airframe 38,342 hrs · 30,320 cycles
SERVICE DOOR LOWER SILL ANGLE IS CORRODED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,342 hrs · 30,320 cycles
SEAT TRACK SEGMENT FS693.00 - FS 847.00, LBL-9, CORRODED BEYOND REPAIRABLE LIMITS, MANUFACTURED AND INSTALLED NEW SEAT TRACK.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,242 hrs · 30,320 cycles
2 EACH INTERCOSTALS, FS 349.00 - FS 364.00, STGR27L + STGR27R, FWD OF AVIONICS BAY DOOR, CORRODED BEYOND REPAIRABLE LIMITS. REPLACED BOTH INTERCOSTALS WITH NEW SERVICEABLE INTERCOSTALS IAW APPLICABLE SRM'S.
Part: THRESHOLD — CORRODED (BS 319-349) · corrosion level 2 · airframe 38,342 hrs · 30,320 cycles
OUTBOARD ANGLE AT SERVICE DOOR THRESHOLD IS CORRODED AROUND SCREW HOLES IN 2 LOCATIONS (SEAL STRIKER).
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,242 hrs · 30,320 cycles
SERVICE DOOR SILL ANGLE CORRODED IN MULTIPLE AREAS FS 319.0 TO FS 349.0.
Part: SKIN — CORRODED (BS 265-280) · corrosion level 2 · airframe 38,342 hrs · 30,320 cycles
BELLY SKIN CORRODED BETWEEN F.S 265 TO F.S. 280 STGR 27 TO 26R.
Part: INTERCOSTAL — CORRODED (BS 265-280) · corrosion level 2 · airframe 38,342 hrs · 30,320 cycles
NLG JACK FITTING INTERCOSTALS ARE CORRODED.
2018
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,396 hrs · 29,726 cycles
ROW 15 EMERGENCY CEILING LIGHT INOP. RELAMPED
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,304 hrs · 29,652 cycles
ROW 15 OVERHEAD EMERGENCY FLOOD LIGHT INOP. RELAMPED.
Part: LIGHT — INOPERATIVE (ROW 18) · airframe 37,304 hrs · 29,652 cycles
ROW 18 OVERHEAD EMERGENCY FLOOD LIGHT INOP. PLACED ON MEL.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 37,296 hrs · 29,646 cycles
PAX DOOR EMER EXIT LIGHT INOP. PLACED ON MEL.
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 37,198 hrs · 29,576 cycles
CAPT FLASHLIGHT INOP. PLACED ON MEL
Part: LIGHT — INOPERATIVE (SEAT 2DF) · airframe 27,071 hrs · 29,483 cycles
EMERG FLOOR LUMIN STRIP AT 2DF INOP. REPLACED
Part: LIGHT — INOPERATIVE (SEAT 1DF) · airframe 37,071 hrs · 29,483 cycles
EMERG FLOOR LUMIN STRIP AT 1DF INOP. REPLACED
Part: BATTERY — DISCHARGED (CABIN) · airframe 36,869 hrs · 29,325 cycles
ALL EMER LIGHTS INOP. RECHARGED BATTERIES OPS CKS GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,868 hrs · 29,324 cycles
ALL EMER LIGHTS INOP. RECHARGED LIGHTS.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 36,329 hrs · 28,889 cycles
L BLEED CAUTION, EMER DIVERSION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,285 hrs · 28,861 cycles
ROW 6 EMERGENCY FLOOD LIGHT INOP. REPLACED BULB.
Part: SKIN — DAMAGED (RUDDER)
LEFT SIDE OF RUDDER, APPROXIMATELY 18 INCHES FROM BOTTOM EDGE, THREE GOUGES AND DENTS.
Part: SKIN — CORRODED (FUSELAGE)
ALL EXTERIOR EDGE NUTPLATE FOR FORWARD BODY TO WING FAIRINGS, 191BB AND 192BB ARE CORRODED.
Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 36,101 hrs · 28,721 cycles
BS 280 FLOORBEAM FWD J ANGLE HAS CORROSION AROUND RECEPTACLE AND FASTNERS.
Part: SEAT TRACK — CORRODED (BS 349-379) · corrosion level 2 · airframe 36,101 hrs · 28,721 cycles
SEAT TRACK, RBL 9 CORRODED BS 349 - 379.
Part: STRINGER — CORRODED (BS 319-333) · corrosion level 2 · airframe 36,101 hrs · 28,721 cycles
STRINGER 25R IS CORRODED, BS 319 - 333.
Part: FRAME — CORRODED (BS 295) · corrosion level 2 · airframe 36,101 hrs · 28,721 cycles
BS 295 FRAME WAS FOUND CORRODED FROM STRINGERS 24R-26R.
Part: FRAME — CORRODED (BS 310) · corrosion level 2 · airframe 36,101 hrs · 28,721 cycles
BS 310 FRAME WAS FOUND CORRODED FROM STRINGERS 25R - 26R.
Part: INTERCOSTAL — CORRODED (BS 349-364) · corrosion level 2 · airframe 36,101 hrs · 28,721 cycles
INTERCOSTAL AT STRINGER 26R, BETWEEN BS 349 AND 364 WAS FOUND CORRODED.
Part: STRINGER — CORRODED (BS 333-349) · corrosion level 2 · airframe 36,101 hrs · 28,721 cycles
STRINGER 26R IS CORRODED FROM BS 333 - 349.
Part: FRAME — CORRODED (BS 319) · corrosion level 2 · airframe 36,101 hrs · 28,721 cycles
BS 319 FRAME WAS FOUND CORRODED FROM STRINGERS 26R - 26L.
Part: INTERCOSTAL — CRACKED (BS 169-202) · airframe 36,101 hrs · 28,721 cycles
INTERCOSTAL IN 121AL FWD UPPER CRACKED.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 36,101 hrs · 28,721 cycles
RIGHT VERTICAL DRAG ANGLE, FWD, CRACKED. CONFIRMED BY EDDY CURRENT.
Part: RIVET — SHEARED (RT WING TE FLAP) · airframe 36,101 hrs · 28,721 cycles
RIGHT OTBD FLAP, TOP SKIN, APPROX FLS 179.96, FOUR RIVETS WITH SHEARD HEADS.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,532 hrs · 28,321 cycles
ROW 3 EMERGENCY CEILING LIGHT INOPERATIVE. REPLACED THE BULBS
Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,470 hrs · 28,281 cycles
CEILING EMERGENCY FLOOD LIGHT ROW 15 INOPERATIVE. PLACED ON MEL.
2017
Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,437 hrs · 28,259 cycles
AFT CABIN CEILING EMERGENCY FLOOD LIGHT INOP. PLACED ON MEL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,426 hrs · 28,250 cycles
CEILING LEVEL EMER LIGHT INOP. PLACED ON MEL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,193 hrs · 28,071 cycles
CENTER CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE.
Part: LIGHT — INOPERATIVE (ROW 18) · airframe 34,959 hrs · 27,894 cycles
ROW 18 EMERGENCY OVERHEAD FLOODLIGHT INOPERATIVE.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,945 hrs · 27,884 cycles
RIGHT FWD EXTERIOR EMERGENCY LIGHT NEAR THE GALLEY DOOR FOUND INOPERATIVE.
Part: LIGHT — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,945 hrs · 27,884 cycles
LEFT FWD OVERWING EMERGENCY LIGHT INOPERATIVE.
Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 34,945 hrs · 27,884 cycles
RIGHT FWD OVERWING EMERGENCY LIGHT INOPERATIVE.
Part: ENGINE — OVERTEMP (ITT) · airframe 34,599 hrs · 27,603 cycles
RIGHT ENGINE HIGH ITT ON TAKE OFF ROLL, 963 DEGREES FOR 14 SECONDS. COMPLIED WITH HIGH ENERGY STOP INSPECTION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,033 hrs · 27,152 cycles
ROW 18 OVHD EMERGENCY FLOOD LIGHT INOP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,907 hrs · 27,052 cycles
ROW 15 CEILING LVL EMER FLOODLIGHT INOP. REPLACED BULB.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,907 hrs · 27,052 cycles
ROW 18 CEILING LVL EMER FLOODLIGHT INOP. REPLACED BULB.
Part: LIGHT — INOPERATIVE (GALLEY) · airframe 33,681 hrs · 26,869 cycles
GALLEY FLOOR LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 33,668 hrs · 26,859 cycles
BOTTOM RT EXIT SIGN AT GALLEY DOOR INOPERATIVE. CONNECTOR FOUND DISCONNECTED. OPS NORMAL
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,601 hrs · 26,800 cycles
FWD FA FLASHLIGHT INOP. R2 BATTERY.
2016
Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,286 hrs · 26,551 cycles
EMER FLOOD LIGHT LT ROW 11 INOPERATIVE. R & R THE BULB IAW 33-51-09 OPS CHECKED GOOD IAW AMM 33-51-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,143 hrs · 26,442 cycles
EMER LIGHT AFT OVERHEAD LIGHT INOP. REPLACED BULBS.
Part: LIGHT — INOPERATIVE (ROW 15) · airframe 32,823 hrs · 26,197 cycles
ROW 15 CEILING LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,643 hrs · 26,071 cycles
ROW 9 AND 18 CEILING EMERGENCY LIGHTS FOUND INOPERATIVE. REPLACED THE LAMPS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,441 hrs · 25,923 cycles
ALL EMERGENCY LIGHTS INOPERATIVE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,310 hrs · 25,822 cycles
ROW 18 AFT EMERGENCY CEILING FLOOD LIGHT INOPERATIVE. PLACED ON MEL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,998 hrs · 25,585 cycles
EMERGENCY FLOOD LIGHT ROW 22 INOPERATIVE, REPLACED THE LAMP.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,822 hrs · 25,445 cycles
6 OVERHEAD EMERGENCY LIGHTS DIM, GO OUT. R & R EMERGENCY BATTERY PACKS.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,719 hrs · 25,366 cycles
FOUND PEANUT BULB OUT ON FWD LT SIDEWALL EMERGENCY LIGHT OUT. R & R BULB, OPS CHECK GOOD.
Part: BULB — INOPERATIVE (OVERWING) · airframe 31,719 hrs · 25,366 cycles
FOUND PEANUT BULB OUT ON OVERWING LIGHT FIXTURE. R & R BULB, OPS CHECK GOOD.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,600 hrs · 25,276 cycles
ROW 14DF EXIT SIGN, HAD ONE BULB INOPERATIVE.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,527 hrs · 25,220 cycles
PAX DOOR FLOOR LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,527 hrs · 25,220 cycles
14F FLOOR EMERGENCY EXIT HAD ONE BULB INOPERATIVE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,488 hrs · 25,196 cycles
SIDEWALL EMERGENCY EXIT SIGN 13DF, TWO BULBS INOPERATIVE, REPLACED THE LAMP.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,445 hrs · 25,156 cycles
GALLEY FLOOR LEVEL EMERGENCY EXIT SIGN BULB INOPERATIVE.
2015
Part: UNKNOWN — ODOR (COCKPIT) · airframe 31,215 hrs · 24,980 cycles
STRONG ODOR IN FLIGHT DECK WITH PAC ON. OPS CHECK OF PACKS GOOD, NO ODOR NOTED, NO EICAS MSGS.
Part: SKIN — CHAFED (BS 910-920) · airframe 31,170 hrs · 24,945 cycles
MULTIPLE CHAFES AND DAMAGED RIVETS FROM BS 910 TO 920, ON STR 27.
Part: POST — CORRODED (BS 280 BULKHEAD) · corrosion level 2 · airframe 31,170 hrs · 24,945 cycles
FS 280 BULKHEAD SIDE POST HAS EXFOLIATION CORROSION AT LBL12 AT WL 72.5.
Part: SEAT — CRACKED (CABIN) · airframe 31,170 hrs · 24,945 cycles
PASSENGER SEAT 3D SEAT PAN IS CRACKED.
Part: SEAT — CRACKED (CABIN) · airframe 31,170 hrs · 24,945 cycles
PASSENGER SEAT 1A SEAT PAN IS CRACKED.
Part: SEAT — BROKEN (PAX CABIN) · airframe 31,170 hrs · 24,945 cycles
PASSENGER SEAT PAN IS BROKEN.
Part: SEAT — CRACKED (CABIN) · airframe 31,170 hrs · 24,945 cycles
PASSENGER SEAT 2A SEAT PAN IS CRACKED.
Part: SEAT — CRACKED (CABIN) · airframe 31,170 hrs · 24,945 cycles
PASSENGER SEAT 2F SEATPAN IS CRACKED.
Part: FLOOR SUPPORT — CORRODED (BS 280) · corrosion level 2 · airframe 31,170 hrs · 24,945 cycles
FS 280.00 BULKHEAD SIDE POST HAS CORROSION AROUND FASTENER AT RBL 12, WL72.5. REPLACED COCKPIT CENTER FLOOR ANGLE AT RBL12 IAW REO 670-53-11-745, REV, DATED 2012-09-08.
Part: FLOORBEAM — UNDAMAGED (BS 280) · airframe 31,170 hrs · 24,945 cycles
FS 280.00 TRANSVERSE FLOOR CROSSBEAM PREVIOUSLY TEMPORARILY REPAIRED UNDER REO 670-53-11-579, REV-B AND REO 690-53-11-521. REQUIRED REPLACEMENT AND PERMANENTLY REPAIRED IAW SB 670BA-53-041, REV-D, DATED FEB 28/2014.
Part: HINGE — GOUGED (PAX DOOR) · airframe 31,170 hrs · 24,945 cycles
PASSENGER DOOR PIANO HINGE IS GOUGED ON LUGS 4, 5, 6, & 8.
Part: HINGE — GOUGED (PAX DOOR) · airframe 31,170 hrs · 24,945 cycles
PAX DOOR PIANO HINGE ON FUSELAGE SIDE AFT LANDING GOUGED FROM PAX DOOR ROLL PIN. REPAIRED IAW REO 670-53-21-582.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 31,170 hrs · 24,945 cycles
VERTICAL STABILIZER LT DRAG ANGLE IS CRACKED APPROXIMATELY 2". REPAIRED IAW REO 690-55-31-004, REV-A, DATED 2009-03-04.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,643 hrs · 24,510 cycles
AFT CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.
Part: LIGHT — MISSING (CABIN) · airframe 30,584 hrs · 24,464 cycles
EMERGENCY LIGHT ROW 13AC PARTIAL MISSING, REPOSITIONED.
Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 30,263 hrs · 24,225 cycles
AFT F/A FLASHLIGHT INOPERATIVE.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,186 hrs · 24,179 cycles
LEFT FORWARD EMERGENCY DOOR LOWER EXIT SIGN HAS ONE BULB INOPERATIVE.
Part: SIGN — INOPERATIVE (CABIN) · airframe 29,917 hrs · 23,982 cycles
FLOOR LEVEL EXIT SIGN LIGHT OUT.
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,411 hrs · 23,596 cycles
F/O'S FLASHLIGHT INOPERATIVE. PLACED ON MEL.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,100 hrs · 23,376 cycles
EXIT LIGHT 13A ONE BULB INOPERATIVE. REPLACED BULB.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,011 hrs · 23,322 cycles
EMERGENCY EXIT LIGHTS INOPERATIVE. CHARGED BATTERIES, OPS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (ROW 21) · airframe 28,960 hrs · 23,289 cycles
ROW 21 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.
2014
Part: LIGHT — INOPERATIVE (ROW 18) · airframe 28,426 hrs · 22,866 cycles
ROW 18 EMERGENCY FLOOD LIGHT INOPERATIVE.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,117 hrs · 22,614 cycles
13F FLOOR LEVEL EMERGENCY EXIT LT HAS ONE BULB INOPERATIVE.
Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 27,986 hrs · 22,499 cycles
LEFT AFT OVER THE WING EMERGENCY LIGHT LENS HAZY. REMOVED AND REPLACED THE EMERGENCY LIGHT LENS.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,986 hrs · 22,499 cycles
ENTRY LOWER EMERGENCY LIGHT BULB OUT. R & R ENTRY LOWER EMERGENCY LIGHT BULB.
Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 27,986 hrs · 22,499 cycles
LT FWD OVER THE WING EMERGENCY LIGHT LENS HAZY. REMOVED AND REPLACED THE WING EMERGENCY LIGHT LENS.
Part: LIGHT — INOPERATIVE (ROW 20) · airframe 27,900 hrs · 22,423 cycles
EMERGENCY EXIT CEILING FLOODLIGHT ROW 20 INOPERATIVE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,033 hrs · 21,646 cycles
LEFT EMERGENCY EXIT DOOR LIGHTS OUT, REPLACED LAMP.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,600 hrs · 21,243 cycles
LEFT & RT FLOOR EMERGENCY LIGHTS, ONE BULB OUT.
2013
Part: METERING VALVE — INOPERATIVE (BRAKE SYSTEM) · airframe 25,656 hrs · 20,399 cycles
UNEVEN BRAKE TEMPS & FEELS LESS EFFECTIVE. REPLACED BRAKE METERING VALVE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,372 hrs · 20,124 cycles
FWD CEILING EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. REPLACED LAMP, OPS CHECKED GOOD.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,336 hrs · 20,084 cycles
FORWARD F/A FLASHLIGHT INOPERATIVE.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,137 hrs · 19,899 cycles
FLOOR LEVEL ROW 13 EMERGENCY EXIT SIGN BULB INOPERATIVE. MX REPLACED BULB.
Part: BULB — INOPERATIVE (EMERGENCY LGIHT) · airframe 25,099 hrs · 19,861 cycles
ROW 14F EMERGENCY EXIT SIGN HAS ONE BULB INOPERATIVE. REPLACED BULB.
Part: FITTING — CRACKED (PAX DOOR) · airframe 24,953 hrs · 19,741 cycles
PASSENGER DOOR LINTEL IS CRACKED JUST AFT OF FS 280.00, STRINGER 3L.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 19,741 cycles
FRAME STATION 280.00 WEBS CORRODED AT WL 72.0, LBL 12 AND RBL 12.
Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 19,741 cycles
FRAME STATION 280.00 CROSSBEAM IS CORRODED IN NUMEROUS AREAS ON TOP SURFACE, ALONG WITH FORWARD "J" ANGLE.
2012
Part: LENS — CRACKED (EXTERIOR) · airframe 23,973 hrs · 18,923 cycles
LEFT FWD EXTERNAL EMERGENCY LIGHT LENS CRACKED. REMOVED AND REPLACED LEFT FWD EXTERIOR EMERGENCY LENS.
Part: LENS — CRACKED (EXTERIOR) · airframe 23,973 hrs · 18,923 cycles
LEFT AFT EXTERNAL EMERGENCY LIGHT LENS CRACKED. REMOVED AND REPLACED LEFT AFT EXTERNAL EMERGENCY LIGHT LENS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,947 hrs · 18,903 cycles
ROW 13 OVERHEAD EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS GOOD.
Part: DRAIN — CORRODED (PAX DOOR) · airframe 23,617 hrs · 18,642 cycles
PAX DOOR DRAIN CORRODED. PERFORM EO 9-52-0032.
Part: GLOWSTRIP — MISSING (CABIN) · airframe 23,445 hrs · 18,515 cycles
PHOTO ILLUM STRIP ROW 13 AC MISSING. RE-ATTACHED PHOTO ILLUM STRIP.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,904 hrs · 18,100 cycles
CABIN CEILING LEVEL EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LAMP.
Part: SEAL — DIRTY (EMERGENCY EXIT) · airframe 22,892 hrs · 18,090 cycles
ROW 17 LEFT EMERGENCY DOOR SQUEALS. MAINTENANCE CLEANED AND LUBED DOOR SEAL. OPS GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,540 hrs · 17,814 cycles
ROW 14 LOWER EMERGENCY LIGHT BULBS OUT. RELAMPED EMERGENCY LIGHT.
Part: PLACARD — WORN (PAX DOOR) · airframe 22,238 hrs · 17,591 cycles
PASSENGER DOOR OPEN PLACARD WORN. R2 PLACARD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,227 hrs · 17,580 cycles
LT AFT OVERWING EMER LIGHT INOP. RELAMPED EMERGENCY LIGHT.
Part: SEAL — OBSTRUCTED (EMERGENCY EXIT) · airframe 22,203 hrs · 17,565 cycles
EMERGENCY EXIT 14F MAKE SQUEALING NOISE IN FL. CLEANED DEBRIS FROM SEAL.
Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 21,889 hrs · 17,317 cycles
ROW 21 EMERGENCY CEILING FLOOD LIGHT INOPERATIVE. R & R PINS ON CONNECTOR J360.
2011
Part: HANDSET — NOISY (CABIN) · airframe 21,802 hrs · 17,245 cycles
AFT FA HANDSET SQUEALS. OP CHECK GOOD.
Part: SEAL — DIRTY (OVERWING EXIT) · airframe 21,772 hrs · 17,219 cycles
OVERWING EXIT 14A SQUEALS OVERWING EXIT 14A SQUEALS. CLEANED DEBRIS FROM SEAL / LUBED AND RE-INSTALLED / OPS GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,746 hrs · 17,199 cycles
FLOOD LIGHT 20 DF INOP. RELAMPED, OP GOOD.
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,555 hrs · 17,055 cycles
CAPTS FLASHLIGHT INOP. R2 FLASHLIGHT.
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,555 hrs · 17,055 cycles
CAPTAIN`S FLASHLIGHT INOP. REPLACED FLASHLIGHT.
Part: WIRE — DAMAGED (LANDING GEAR) · airframe 21,545 hrs · 17,045 cycles
PROX FAULT 2. REPAIRED WIRING AT PX28 PROX SENSOR.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,429 hrs · 16,950 cycles
AFT CEILING CABIN FLOOD LIGHT OUT. RELAMPED CEILING FLOOD LIGHT.
Part: GLOWSTRIP — LOOSE (CABIN) · airframe 21,380 hrs · 16,914 cycles
ROW 15 PHOTO ILLUMINATE STRIPS LOOSE. RE-SECURED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,363 hrs · 16,897 cycles
AFT RT EXTTERIOR EMERGENCY LIGHT OUT; RELAMPED EMERGENCY LIGHT.
Part: SEAL — UNSECURE (PAX DOOR) · airframe 21,300 hrs · 16,842 cycles
PAX DOOR LOUD SQUEAL INFLT. RE-SECURED SEAL.
Part: DOOR — NOISY (CABIN) · airframe 21,291 hrs · 16,833 cycles
LOUD SQUEAL FROM PAX DOOR. PRESS CHECK NORM, NO SQUEALS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,285 hrs · 16,827 cycles
ROW 23 EMERGENCY FLOOD INOP. RELAMPED EMERGENCY LIGHT.
Part: ACM — MALFUNCTIONED (AC BAY) · airframe 21,228 hrs · 16,769 cycles
LT PACK CAUSE SMOKE DURING DESCENT. R2 LT ACM.
Part: WARNING SYSTEM — OUT OF ADJUST (PAX DOOR HANDLE) · airframe 21,186 hrs · 16,728 cycles
PAX DOOR LATCH CAUTION INTERMITTENT IN FLT. ADJUSTED.
Part: SNUBBER — OUT OF ADJUST (PAX DOOR) · airframe 21,164 hrs · 16,710 cycles
PAX DOOR FREE FALLING. ADJUSTED FWD SNUBBER.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,081 hrs · 16,641 cycles
AFT F/A FLASHLIGHT LED NOT FLASHING. R2 FLASHLIGHT.
Part: BRAKE — MALFUNCTIONED (NR 2) · airframe 20,846 hrs · 16,442 cycles
LEFT BRAKES GRABBING (NR 1 TEMP 3 & NR 2 9). R2 NR 2 BRAKE, TAXI CHECK GOOD, 3 AT HIGHEST.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,718 hrs · 16,330 cycles
CEILING LVL EMERGENCY FLOOD LIGHT. RELAMPED EMERGENCY LIGHT.
Part: AHRS — MALFUNCTIONED (NR 1) · airframe 20,541 hrs · 16,167 cycles
FOUR UNCOMMANDED RUDDER DEFLECT IN FLT. R2 THE NR 1 AHRS, NR 1 YD ACTUATOR.
Part: CONNECTOR — DIRTY (BTMS) · airframe 20,452 hrs · 16,088 cycles
NR 3 BRAKE HOTTER THAN OTHERS BTMS 7. CLEANED BTMS CONNECTOR AND PERFORMED TAXI CHECK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,445 hrs · 16,080 cycles
NUMBER 4 CEILING EMERGENCY LIGHT OUT. R2 BULB.
Part: BRAKE — OVERTEMP (NR 2) · airframe 20,391 hrs · 16,034 cycles
NR 2 BRAKE TEMP ABNORMALLY HIGH. COOLED BRAKE AND PERFORMED TAXI CHECK.
Part: TRANSDUCER — DIRTY (MLG) · airframe 20,362 hrs · 16,009 cycles
NR 3 BRAKE SMOKING, IND 9 DURING TAXI. BLED BRAKES & CLEANED WHEELSPEED TRANSDUCER.
Part: MARKER — OUT OF POSITION (CABIN) · airframe 20,216 hrs · 15,890 cycles
THE 15-C FLOOR PATH MARKER OUT OF POSITION. REPOSITIONED 15-C FLOOR PATH MARKER IN THE CORRECT POSITION
Part: PROXIMITY SWITCH — OUT OF ADJUST (LT MLG) · airframe 20,210 hrs · 15,885 cycles
GEAR UP DISAGREE LEFT MAIN SHOWS RED. MX ADJUSTED PX18 AND PX 20 PROX SWITCHES.
Part: ROD — DETACHED (PAX DOOR) · airframe 20,197 hrs · 15,873 cycles
PAX DOOR LOWER STEP ROD DETACHED. R2 LOWER STEP ASSY.
Part: WINDOW — CRACKED (COCKPIT) · airframe 20,049 hrs · 15,753 cycles
RT WINDOW CRACKED. FERRY TO PHX, R2 WINDOW.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,959 hrs · 15,674 cycles
FWD F/A FLASHLIGHT INOP. MX R2 FLASHLIGHT BATTERY.
Part: SENSOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 19,896 hrs · 15,612 cycles
RT AFT EMERGENCY DOOR CAUTION IN FLT. MX CLEANED & ADJUSTED SENSOR.
Part: PLACARD — MISSING (CABIN) · airframe 19,875 hrs · 15,593 cycles
SEAT 15A EMERGENCY EXIT DOOR PLACARD MISSING. MX INSTALLED PLACARD.
Part: BONDING STRAP — BROKEN (CABIN DOOR) · airframe 19,707 hrs · 15,453 cycles
FWD ENTRY DOOR TO STEP BONDING WIRE BROKEN. MX INSTALLED BONDING WIRE AT FWD ENTRY DOOR, NO OTHER DEFECTS NOTED.
Part: SEAL — OUT OF POSITION (PAX DOOR) · airframe 19,641 hrs · 15,390 cycles
LIGHT VISIBLE THROUGH PAX DOOR SEAL. MX REPOSITIONED SEAL, OPS GOOD.
Part: BRAKE ASSY — MALFUNCTIONED (MLG) · airframe 19,625 hrs · 15,380 cycles
NR 2 BRAKE OH WARNING AFTER T/O. MX REPLACED NR 2 BRAKE AND MLG WHEEL ASSEMBLIES.
Part: CONNECTOR — DAMAGED (BRAKE SENSOR) · airframe 19,625 hrs · 15,380 cycles
NR 2 BRAKE OVERHEAT WARNING AFTER TAKEOFF, ACFT RETURNED TO FIELD. REPINNED BRAKE 2 TEMP SENSOR PLUG.
Part: WARNING SYSTEM — OUT OF RIG (PAX DOOR) · airframe 19,601 hrs · 15,362 cycles
PAX DOOR CAUTION MESSAGE IN FLIGHT. MX RIGGED PX 46, OPS GOOD.
Part: LENS — MISSING (CABIN) · airframe 19,558 hrs · 15,324 cycles
SERVICE DOOR FLOOR LEVEL EXIT LIGHT COVER MISSING. MX INSTALLED LENS COVER.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,430 hrs · 15,209 cycles
CEILING EMERGENCY FLOOD LIGHT AT ROW 23 INOP. MX RELAMPED EMERGENCY LIGHT.
Part: SENSOR — FAULTY (NR 2 BTMS) · airframe 19,400 hrs · 15,184 cycles
FALSE NR 2 BTMS WARNING IN FLIGHT. MX REPLACED NR 2 BTMS SENSOR, OPS GOOD.
Part: CONNECTOR — DIRTY (BRAKE) · airframe 19,386 hrs · 15,173 cycles
LT INBOARD BRAKE O/H WARNING INTERMITTENT IN FLT. MX CLEANED & RE-SECURED CONNECTOR.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 19,372 hrs · 15,164 cycles
EMERGENCY LIGHTS INOP ROW 15/PAX DOOR/AFT OVERWING. MX R2 NR 4 BATTERY PACK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,331 hrs · 15,134 cycles
CTR CEILING LEVEL EMERGENCY FLOODLIGHT INOP. MX RELAMPED EMERGENCY LIGHT.
2010
Part: SUPPORT — BROKEN (STEP) · airframe 19,306 hrs · 15,113 cycles
AIRSTAIR BOTTOM STEP SUPPORT ROD BROKEN. REPLACED STEP PANEL.
Part: PROXIMITY SENSOR — OUT OF ADJUST (EMERGENCY EXIT)
AFT LT EMER EXIT CAUTION MESSAGE DURING TAXI. ADJUSTED PROX SENSOR.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT)
PAX DOOR HANDLE CAUTION. FAULT CLEARED ITSELF IN FLIGHT, NFAR.
Part: SENSOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 19,184 hrs · 15,007 cycles
RIGHT FWD EMERGENCY DOOR CAUTION INTERMITTENT. MX ADJUSTED SENSOR.
Part: SENSOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 19,184 hrs · 15,007 cycles
INTERMITTENT LEFT EMERGENCY DOOR CAUTION. MX ADJUSTED SENSOR.
Part: WIRE — DAMAGED (DOOR WARNING) · airframe 19,177 hrs · 15,001 cycles
LT FWD EMERGENCY EXIT CAUTION INTERMITTENT. MX REPAIRED WIRING TO PX43.
Part: PIN — BACKED OUT (EMERGENCY LIGHT) · airframe 19,143 hrs · 14,975 cycles
AFT EMERGENCY CEILING LIGHT INOP. MX RE-SEATED PUSHED PIN.
Part: BATTERY — DISCHARGED (CABIN) · airframe 19,143 hrs · 14,975 cycles
ALL EMERGENCY LIGHTS INOP. MX RECHARGED EMERGENCY BATTERIES.
Part: QUICK DISCONNECT — DIRTY (BRAKE SYSTEM) · airframe 19,021 hrs · 14,878 cycles
RTG DUE TO BRAKES STICKING DURING TAXI. MX CLEANED RESEATED ALL 4 QD'S, TAXI CHECK GOOD.
Part: WARNING SYSTEM — ACTIVATED (PAX DOOR) · airframe 19,003 hrs · 14,862 cycles
PAX DOOR OUTER HANDLE CAUTION. MX R2 PX107.
Part: PLACARD — MISSING (CABIN) · airframe 18,957 hrs · 14,818 cycles
OPEN PLACARD MISSING. MX REPLACED PLACARD.
Part: WIRE HARNESS — BROKEN (PAX DOOR) · airframe 18,938 hrs · 14,802 cycles
PAX DOOR OUTER HANDLE CAUTION PROX 2. MX REPAIRED BROKEN WIRE IN HARNESS.
Part: SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 18,522 hrs · 14,508 cycles
LEFT FWD EMERGENCY EXIT CTN ON TAXI. MX ADJUSTED PX SENSOR.
Part: BATTERY — DISCHARGED (CABIN) · airframe 18,433 hrs · 14,455 cycles
AC EMERGENCY LIGHTS NOT ILLUMINATING. MX CHARGED BATTERIES WITH ACFT PWR NFAR.
Part: PROXIMITY SWITCH — OUT OF ADJUST (DOOR) · airframe 18,259 hrs · 14,337 cycles
LEFT AFT EXIT DOOR CAUTION. ADJUSTED PX12 PROX SWITCH.
Part: VALVE — MALFUNCTIONED (BRAKE SYSTEM) · airframe 18,253 hrs · 14,332 cycles
NR 2 BRAKE TEMP INDICATION WARNING IN FLT. NR 2 SENSOR DISCONNECT; R2 PARKING BRAKE SOV & ANTI SKID CONTROL VALVE, OP GOOD.
Part: SENSOR — OUT OF ADJUST (DOOR) · airframe 18,156 hrs · 14,247 cycles
LT WING FWD EXIT DOOR CAUTION. MX ADJUSTED SENSORS.
Part: SENSOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 17,984 hrs · 14,092 cycles
LIGHT FWD EMERGENCY EXIT DOOR CAUTION INTERMITTENT. MX ADJUSTED SENSOR.
Part: TARGET — LOOSE (EXIT) · airframe 17,946 hrs · 14,061 cycles
RT WING AFT EXIT CAUTION. MX SECURED TARGET FOR PX7, OP GOOD.
Part: CONNECTOR — DEFECTIVE (BRAKE SYSTEM) · airframe 17,932 hrs · 14,048 cycles
NR 2 BRAKE OVERHEAT WARNING IN FLT REPEAT. REMOVED AND REPLACED NR 2 BTMS, ASCU, HARNESS PLUG.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,892 hrs · 14,015 cycles
F/O AND AFT F/A EMERGENCY FLASH LIGHTS NO FLASHING CHARGE LIGHT. PLACED ON MEL. REMOVED AND REPLACED FLASHLIGHT BATTERY.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,898 hrs · 14,021 cycles
CAPT EMERGENCY FLASHLIGHT INOP. PLACED ON MEL. REMOVED AND REPLACED FLASHLIGHT BATTERY.
Part: ENGINE — NOISY (LEFT) · airframe 17,747 hrs · 13,892 cycles
DIVERT TO SAV - DECLARED EMERGENCY. LT ENG LOUD NOISE AND INDICATION FLUX. R2 NR 1 ENG.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,698 hrs · 13,851 cycles
ROW 17 EMERGENCY FLOOD LIGHT INOP. PLACED ON MEL 33-51-01-1, THEN RELAMPED.
Part: GUARD — BROKEN (EMERGENCY LIGHTS) · airframe 17,628 hrs · 13,793 cycles
FWD EMERGENCY LIGHT SWITCH GUARD BROKEN. REPLACED GUARD.
Part: LIGHT — MISSING (CABIN) · airframe 17,210 hrs · 13,445 cycles
THE 16-A/C FLOOR LEVEL EMERGENCY STRIP MISSING. INSTALLED EMERGENCY FLOOR LEVEL STRAP, OPS CHECK GOOD.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,863 hrs · 12,297 cycles
ASH FLT 2879 PHX-ELP. LT EXIT ROW FLOOR STRIP LIGHT LOOSE. MX RE-SECURED IT.
2008
Part: CONNECTOR — DIRTY (TEMP SENSOR) · airframe 14,217 hrs · 11,025 cycles
ASH 2889 BUR-PHX. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE DUE TO SMOKE IN THE COCKPIT. MX CLEANED AND TIGHTENED RT INLET TEMP SENSOR CONNECTOR.
Part: LIGHT — INOPERATIVE (ROW 17) · airframe 14,218 hrs · 11,025 cycles
ASH FLT 2709 CLT-DTW - CAPTAIN REPORTS THE OVERHEAD EMERGENCY FLOOD LIGHT AT ROW 17 INOP. MX REMOVED AND REPLACED LIGHT.
Part: WARNING SYSTEM — FALSE ACTIVATION (PAX DOOR)
ASH FLT 2615 - IAD-CLT - ON TAXI IN PAX DOOR OUTER HANDLE CAUTION MESSAGE ILLUMINATED ON EICAS. MAINTENANCE RESET. OPS GOOD. (S)
Part: SEAL — LEAKING (EMERGENCY EXIT)
ASH FLT 2889 PHX-AUS - EMERGENCY EXIT 15F SQUEELS. MAINTENANCE INSPECTED, CLEANED AND LUBED SEAL. (S)
Part: SEAL — LACK OF LUBE (EMERGENCY EXIT) · airframe 13,266 hrs · 10,225 cycles
ASH FLT 2889 PHX-AUS - RT AFT EMERGENCY EXIT DOOR HIGH PITCH NOISE IN FLIGHT. LUBED DOOR SEALS, NO SQUEAK.
Part: PROXIMITY SWITCH — OUT OF ADJUST (EMERGENCY EXIT) · airframe 12,561 hrs · 9,736 cycles
ASH FLT 2627 CLT BHM - LT FORWARD EMERGENCY DOOR CAUTION WHEN AIRCRAFT IS DEPRESSURIZED. MX ADJUSTED PROX SWITCH.
2007
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,574 hrs · 8,891 cycles
ASH FLT 2853 PHX-LAX - EMERGENCY FLOOD LIGHT AISLE 20 INOP. MX RELAMPED THE FLOOD LIGHT, OPS CHECK GOOD.
Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 11,519 hrs · 8,852 cycles
ASH FLT 2785 PHX - EMERGENCY EXIT ROW LIGHTS INOP AT ROWS 17 AND 22. MX REPLACED LIGHTS.
2006
Part: DOOR — NOT CLOSED (CARGO BAY) · airframe 9,626 hrs · 7,572 cycles
ASH 2825 DFW - CABIN ALT CAUTION MESSAGE. ACFT WOULD NOT PRESSURIZE. MX FOUND THE AFT CARGO DOOR NOT PROPERLY SECURED CLOSED. MX CLOSED THE AFT CARGO DOOR AND ACFT PRESSURIZED WITH NO PROBLEMS.
Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 9,533 hrs · 7,263 cycles
ASH 2732 PHX. SPOILER/STAB FAULT STATUS MESSAGE. MX RESET SYSTEM AND PERFORMED S-POST WITH NO DEFECTS NOTED.
Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 9,524 hrs · 7,255 cycles
ASH 2989 LAS. STAB CHANNEL 1 INOP STATUS MESSAGE & WILL NOT ENGAGE. MX RESET SYSTEM OPS CHECKED GOOD.
Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 8,990 hrs · 6,818 cycles
ASH 2612 ATL. SPOILER / STAB AND SSCU 2 FAULT STATUS MESSAGES. MX RESET THE SYSTEM. NO FURTHER DEFECTS NOTED.
Part: SENSOR — FAULTY (L/E SLAT) · airframe 8,896 hrs · 6,737 cycles
ASH 2617 CLT. SLATS FAULT STATUS MESSAGE. MX DEFERRED SLAT SKEW DETECTIONS SYSTEM. MX R2 SLAT DISCONNECT SENSOR.
Part: ODOR — DETECTED (COCKPIT) · airframe 8,490 hrs · 6,411 cycles
ASH 5093 CLT - PILOT REPORTED SMOKY SMELL FROM COCKPIT. MX INSPECTED, RAN ALL ELEC SYSTEM. NO DEFECTS NOTED.
Part: PRECOOLER — UNKNOWN · airframe 8,292 hrs · 6,240 cycles
ASH 6527 PHX - RIGHT BLEED WARNING MESSAGE. MAINTENANCE REMOVED AND REPLACED THE PRE-COOLER.
Part: WARNING SYSTEM — MALFUNCTIONED (RUDDER) · airframe 8,130 hrs · 6,119 cycles
ASH 6119 PHX - RUDDER LIMIT FAULT. MX RESET SYSTEM. OP'S CHECK WAS GOOD. ACFT CONTINUED OPERATIONS.
Part: DOOR — LOOSE (EMERGENCY EXIT) · airframe 8,066 hrs · 6,069 cycles
ASH 6455 AUS - LEFT EMERGENCY EXIT DOOR CAUTION AFTER LANDING. MX RE-SECURED DOOR. ACFT CONTINUED OPERATIONS.
Part: WARNING MESSAGE — ILLUMINATED · airframe 8,034 hrs · 6,041 cycles
ASH 5098 CLT - GLD NOT ARMED EICAS MSG IN FLT. MX PERFORMED SPOST AND SSCU TESTS.
Part: LAMP — INOPERATIVE (CABIN) · airframe 7,816 hrs · 5,860 cycles
ASH 6437 PHX - CABIN EMERGENCY EXIT LIGHT SIGN INOP AT ROW 7F. MAINTENANCE RELAMPED THE SIGN.
Part: STAB SYSTEM — WARNING MESSAGE · airframe 7,669 hrs · 5,746 cycles
ASH 6109 PSP - STAB FAULT STATUS. PERFORMED SPOST 2 W/FLIGHT CREW. NO FURTHER DEFECTS NOTED.
Part: CAUTION MESSAGE — FALSE ACTIVATION (E/E BAY DOOR) · airframe 7,633 hrs · 5,713 cycles
ASH 5022 CLT - AVIONICS BAY DOOR CAUTION MESSAGE. MX INSPECTED AND FOUND DOOR CLOSED AND INDICATIONS NORMAL. ACFT RETURNED TO SERVICE.
Part: LIGHT — LOOSE (CABIN) · airframe 7,467 hrs · 5,589 cycles
EMERGENCY EXIT LIGHT FLOOR PATH LUMINESCENT WAS LOOSE ADJACENT TO LT AFT OVERWING EXIT. MX RESECURED LUMINESCENT. AIRCRAFT RETURNED TO SERVICE.
Part: WARNING MESSAGE — ILLUMINATED · airframe 7,421 hrs · 5,547 cycles
ASH 5045 CLT - STAB FAULT STATUS MESSAGE REPORTED BY THE CREW. CREW PERFORMED THE SPOST PROCEDURE WITH MX CONTROL. OP'S CHECK GOOD.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 7,410 hrs · 5,534 cycles
ALL EMERGENCY EXIT ROW LIGHTS WILL NOT STAY ILLUMINATAED. MX CHARGED EMERGENCY BATTERIES WITH APU. PERFORMED OP'S CHECK OF EMERGENCY LIGHTS. NO FURTHER DEFECTS NOTED.
Part: NONE — NONE (NONE) · airframe 7,344 hrs · 5,188 cycles
ASH 6519 PVR - ABORTED TAKEOFF, FO SUSPECTED THE ELEVATOR WAS STIFF. AFTER REDUCING THRUST, FO DECIDED ELEVATOR WAS FINE, BUT NOT ENOUGH RUN-WAY TO CONTINUE TAKEOFF. FLIGHT CREW DETERMINED ELEVATOR FUNCTIONING PROPERLY. NO FURTHER ACTION REQUIRED.
Part: CONTROL UNIT — MALFUNCTIONED · airframe 7,322 hrs · 5,160 cycles
ASH 5052 CHS - RUDDER LIMIT FAULT, SPOILER STAB FAULT, SLATS HALF SPEED AND PITCH FEEL CAUTION MESSAGE. MAINTENANCE REMOVED AND REPLACED SSCU NR 1.
Part: CAUTION MESSAGE — ACTIVATED (PITCH FEEL) · airframe 7,306 hrs · 5,445 cycles
ASH 5039 GSO - PITCH FEEL CAUTION ON POWER UP. PERFORMED SPOST2 WITH FLIGHT CREW.
Part: CAUTION MESSAGE — FALSE ACTIVATION · airframe 7,302 hrs · 5,438 cycles
ASH 6681 FAT - CAPTAIN REPORTED A GLD CAUTION MESSAGE AT APPROX 150 FEET FROM LANDING. MX PERFORMED SYSTEM OPS CHECK AND COULD NOT DUPLICATE. OPS CHECK GOOD.
Part: YAW DAMPER — WARNING LIGHT (NR 2) · airframe 7,229 hrs · 5,382 cycles
YAW DAMP 2 INOP CAUTION MESSAGE. MX RESET SYSTEM. OPS CHECK GOOD.
Part: NONE — NONE (NONE) · airframe 7,204 hrs · 5,364 cycles
ASH 6486 ELP - CAPTAIN REPORTED THAT THE FWD PBE VSI IS PROTRUDING. MX FOUND PBE TO BE SERVICEABLE PER THE ESSEX PB/E CORP REFERENCE AND PROCEDURES MANUAL.
Part: YAW DAMPER — INOPERATIVE (NR 2) · airframe 7,148 hrs · 5,329 cycles
CAPTAIN REPORTED A YAW DAMP 2 INOP. MAINTENANCE OPS CHECKED, BUT COULD NOT DUPLICATE THIS DISCREPANCY. ACFT CONTINUED OPERATIONS.
Part: CIRCUIT CARD — MALFUNCTIONED (YAW DAMPER) · airframe 7,156 hrs · 5,331 cycles
CREW REPORTED THE YAW DAMPNER 2 WOULD NOT STAY ENGAGED. MAINTENANCE DEFERRED THE YAW DAMPNER. MX R2 FCC.
2005
Part: SENSOR — MALFUNCTIONED (SLATS) · airframe 6,900 hrs · 5,134 cycles
ASH 2618 CLT - SLAT FAULT STATUS MESSAGE. MAINTENANCE REMOVED AND REPLACED THE INBOARD SLAT DISCONNECT SENSOR.
Part: SMOKE GOGGLES — CRACKED (COCKPIT) · airframe 6,263 hrs · 4,697 cycles
ASH 6475 LAX - FO'S SMOKE GOGGLES CRACKED. MX REPLACED SMOKE GOGGLES.
Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 6,229 hrs · 4,674 cycles
ASH 6090 PHX - PILOT RETURNED TO GATE DUE TO A INBOARD SPOILERS AND INBOARD SPOILERONS FAULT. MX R2 PCU.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,867 hrs · 4,410 cycles
ASH 6584 OAK - DURING PRE-FLT, CREW FOUND CEILING EMER FLOODLIGHT INOP. MX RELAMPED.
Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 4,984 hrs · 3,780 cycles
ASH 6588 SAN TO PVR. THE CREW REPORTED FLAPS FAIL IN FLIGHT. MX R2 RIGHT OUTBOARD FLAP OUTBOARD SKEW SENSOR.
2004
Part: MECHANISM — LACK OF LUBE (SERVICE DOOR) · airframe 3,650 hrs · 2,839 cycles
SERVICE DOOR WAS DIFFICULT TO OPEN. MX LUBED SERVICE DOOR, NO FURTHER DISCREPANCIES.
Part: LIGHT — INOPERATIVE (CABIN)
CREW REPORTED EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE TESTED SYSTEM AND COULD NOT DUPLICATE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS USED. (M)
Part: CONTROL VALVE — DEFECTIVE (THRUST REVERSER)
ABORTED TAKEOFF DUE TO LT ENGINE T/R UNLOCK MSG. MAINTENANCE REPLACED THE ISOLATION CONTROL VALVE ON THE LT THRUST REVERSER. ALL LEAK AND OPERATIONAL CHECKS GOOD. (M)
2003
Part: ISOLATION VALVE — MALFUNCTIONED (THRUST REVERSER)
CREW ABORTED TAKEOFF DUE TO RIGHT REVERSER UNSAFE CAUTION MESSAGE. MAINTENANCE TROUBLESHOT AND REPLACED THE NR 2 ENGINE T/R ISOLATION VALVE. (M)