N2823W
Registered owner: SMITH SCOT, NC (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.
81 reports on file, 1995-02-06 – 1995-11-08.
Part: ANTENNA — FAILED (RADAR)
WX RADAR SPOKES AND DISPLAYS TEST PATTERN WHILE IN NORM AND CONTOUR. REPLACED RADAR ANTENNA AND WAVE GUIDE, OPERATION NORMAL.
Part: ANGLE — CRACKED (NR 7 SLAT)
DURING A-1 LETTER CHECK, FOUND .25 INCH CRACK NR 7 L/E SLAT COVE SKIN ATTACH ANGLE AT I/B STOP PAD. REPAIRED PER M/M 57-54-0.
Part: ANGLE — CRACKED (NR 2 LE SLAT)
DURING A-1 LETTER CHECK, FOUND 2 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE AT O/B STOP PAD. REPAIRED PER M/M 57-54-0.
Part: STRINGER — CORRODED (FS 950-1007)
DURING HMV, CORROSION WAS FOUND FROM STA 950F TO 1007, STR 29L AROUND FASTENER LOCATIONS ON THE UPPER SURFACE OF THE O/B SKIN ATTACH FLANGE. REPAIRED PER DL ERA 3012174-14.
Part: STRINGER — CORRODED (STR 25R STA 1148)
AT HMV, FOUND STRINGER 25 CORRODED AT FS 1148. REMOVED DAMAGED SECTION REPAIRED PER SRM53-10-3 FIG 1.
Part: ANGLES — CORRODED (STA 1166)
AT HMV THE FLOOR SUPPORT ANGLES AT STA 1166 WERE FOUND TO BE CORRODED. THE ANGLES WERE REPAIRED PER SRM 53-10-5 FIG 10.
Part: ANGLE — CORRODED (BS 1166)
DURING HMV, THE FLOOR SUPPORT ANGLES AT STA 1166 WERE FOUND TO BE CORRODED. THESE WERE REPAIRED PER SRM 53-10-3 FIG 10.
Part: FRAME — CRACKED (FS 580)
AT HMV, FOUND FUSELAGE FS 580 FRAME CRACKED AT STR 25L. CRACK IS IN DOUBLER ON TOP OF FRAME UPPER FLANGE. REPAIRED PER SRM 53-10-4 PG 106.
Part: FLAP — WORN (NR 4 FORE LE)
AT HMV SHOP INSPECTION NR 4 FOREFLAP WAS FOUND WITH WEAR DAMAGE TO L/E SKIN AT 54 INCHES FROM THE O/B END OF FLAP. REPAIRED PER SRM 57-50-4.
Part: SEAT TRACK — DAMAGED (STA 800)
SEAT TRACK RT I/B HAS TOOLING DAMAGE ON O/B FLANGE STA 800. REPAIRED PER SRM 53-10-5 PG27. FOUND AT HMV.
Part: STRINGER — CORRODED (STA 700 STR 28L)
FWD B/B CORROSION ON STR 28L AT STA 700. REPAIRED PER SRM 53-10-3 FIG 1. FOUND AT HMV.
Part: STRINGER — CORRODED (BS 740)
STRINGER 27R CORRODED INSIDE STRINGER STA 740 AFT OF SPLICE STRINGER SLICE PER SRM 53-10-3 PG 3. FOUND AT HMV.
Part: SUPPORT — CORRODED (BS 720)
AT HMV, FOUND LOWER FUSELAGE SKIN SUPPORT ANGLE AT FS 720 WITH CORROSION DAMAGE. REPLACED ANGLE PER MM 53-11-10 PG 858 TO 859.
Part: SEAT TRACKS — CORRODED (RH STA1010-1050)
RT I/B AND RT O/B SEAT TRACKS CORRODED STA 1010-1050. REPAIRED PER MM 53-20-11 FIG 804. FOUND AT HMV.
Part: FLAP — WORN (NR 3 FLAP)
LEADING EDGE WORN 52 INCHES FROM I/B END OF RT WING NR 3 AFT FLAP. REPAIRED PER SRM 575004 FIG 9.
Part: STRINGER — CORRODED (STA 740 27R)
AT HMV, FOUND STRINER 27R, CORRODED AT FS 740. REPAIRED PER SRM 53-10-3 FIG. 1.
Part: LIGHT BOX — CRACKED (CABIN)
DURING HMV FOUND L/W L/E LIGHT BOX, STR 15L IS CRACKED ON FWD AND AFT SIDES OF LIGHT BOX, REPAIRED PER SRM 53-10-1 FIG 1.
Part: TEE — CORRODED (STA 742)
AT HMV, FOUND LOWER FUSELAGE STRUCTURE TEE ANGLE CORRODED AT FORWARD HINGE AREA OF PANEL 3448 AT FS 742. REPAIRED PER MM 53-30-1 FIG 804.
Part: BONDNG WIRE HOLE — ELONGATED (LT AILERON)
DURING HMV, FOUND 727 O/B AILERON BONDING WIRE ATTACH HOLE ELONGATED. REPAIRED PER SRM 57-50-5.
Part: SKIN — PUNCTURE (LT AILERON)
DURING HMV, FOUND HOLE PUNCTURED IN LOWER SKIN, I/B END 727 O/B AILERON. REPAIRED PER SRM 57-50-5.
Part: STRINGER — CRACKED (BS 990-1000)
DURING HMV, FOUND STRINGER CRACKED NR 29L CRACKED IN LOWER RADIUS FROM FS 990 - 1000. REPAIRED PER ERA 301274-14 REV B. FOUND AT HMV.
Part: FLOOR — CORRODED (STA 1167 LBL44-4)
STA 1167 FLOOR AT LBL 44 TO LBL 49 CORRODED. FOUND AT HMV. REPAIRED PER SRM 53-10-8 FIG 10.
Part: STRINGER — CRACKED (STR 1L)
DURING HMV INSPECTION PER EO 4-59253-3AD, FOUR DIFFERENT VERTICAL STABILIZER STRINGERS WERE FOUND CRACKED. THE CRACK LOCATIONS ARE STR8L AT STA 180.6, STR 9L AT STA 133.8, STR 7R AT STA 133.8, AND STR 1L AT STA 39.809. IN ACCORDANCE WITH M/M 55-30-0, PG. 803, AND S/B 727-55-0075, REV 2, THE STRINGERS WERE REPAIRED.
Part: SEAT TRACK — CORRODED (STA 420-380)
AT HMV, FOUND SEAT TRACK CORRODED AT FS 420 - 380 AT RBL 24 SPLICED IN SECTION FROM 400 TO 344 PER MM 53-20-11 FIG 802. SPLICED SEAT TRACK SECTION FROM 400-440 PER MM 53-20-11.
Part: BEAM — CORROSION (STA 1110)
CORROSION FLOOR BEAM STA 1110, TOP OF BEAM ALL THE WAY ACROSS. REPAIRED AT RBL 18 TO RBL 33 PER SRM 53-10-8.
Part: ANGLE — CORROSION (FS312-344)
ANGLE CORRODED FLOOR SUPPORT ANGLES CORRODED FROM FS 312 TO FS 344 LBL28. REPLACED SUPPORT AT FS 312 TO 328 AND CLEANED CORROSION PER SRM 51-10-6.
Part: SEAT TRACK — CORRODED (BS 420-380)
SEAT TRACK CORRODED STA 420 TO 380. REPLACED SECTION OF TRACK PER MM 53-20-11.
Part: SKIN — CRACKED (FS 1052)
AT HMV, FOUND FUSELAGE SKIN CRACKED AT FS 1052 OUTBOARD OF STRINGER 28L. REPAIRED PER SRM 53-30-3.
Part: SUPPORT — CORROSION (BS 1130-1148)
FLOOR SUPPORTS STA 1130 TO 1148 RBL12 AND SMALL CONNECTING STUB SUPPORT WERE FOUND CORRODED. CLEANED CORROSION PER SRM 51-10-6, WITHIN LIMITS 53-20-11 FIG 804, TREATED PER 51-10-2 PG 1. REPLACED STUB SUPPORT.
Part: FLOOR BEAM — CORRODED (STA 380 RBL 60)
AT HMV, FOUND FS 380 CABIN FLOOR BEAM CORRODED AT RBL 60. REPAIRED PER SRM 53-10-8 FIG 1.
Part: STRINGER — CORRODED (FS 1154)
AT HMV, STRINGER 22L WAS FOUND CORRODED AT FS 1154 ON IB FLANGE AND A SPLICE BELOW LAV DUMP CHUTE. DAMAGED AREA WAS REMOVED AND NEW SECTION WAS MFG PER SRM 53-10-3 AND INSTALLED.
Part: SUPPORT — WORN (AC BAY STA 720D)
SUPPORT WORN AC DISTRIBUTION BAY BULKHEAD SUPPORT WORN AT UPPER ATTACH POINT, FS 720D ABOVE STR26L. REPAIRED PER SRM 53-10-9 FIG 8. FOUND AT HMV.
Part: FLOOR SUPPORT — CORRODED (STA 418)
FLOOR SUPPORT CORRODED AT STA 418 RBL 12 INCHES TO Z ANGLE AT AFT SIDE OF FWD SVC DOOR. REPAIRED PER MM 53-20-11 FIG 804. FOUND AT HMV.
Part: BEAM — WORN (STA 720D)
BEAM WORN C1 AFT BULKHEAD WALL SUPPORT BEAM AT STA 720D, BELOW RT I/B SEAT TRACK IS WORN AT WASHERS. REPAIRED PER SRM 53-10-9 FIG 8. FOUND AT HMV.
Part: CHORD — CORRODED (FS950)
CHORD CORRDED, CORROSION ON CHORD OB OF RT KEEL BEAM EXTENSION FS950, FOUND AT HMV. REPAIRED PER SRM 53-10-9 FIG 11.
Part: FLOOR BEAM — CORRODED (FUS. STA 400)
FLOOR BEAM CORRODED AT FS 400 FROM LBL 12 TO RBL 12. SPLICED IN NEW SECTION OF BEAM PER SRM 53-10-8 FIG 3. FOUND AT HMV.
Part: FLOOR BEAM — CORRODED (STA 420 RBL 56)
FLOOR BEAM CORRODED AT STA 42O, RBL 56 INCHES. O/B SEATTRACK RIGHT SIDE CORRODED SAME LOC AS ITEM 1. REPAIRED PER SRM 53-10-8 FIG 1. FOUND AT HMV.
Part: SEAT TRACK — WORN (BS 1110-1130)
DURING HMV FOUND LT SEAT TRACKS WORN AT SEVERAL SEAT LOCATIONS BETWEEN 950F AND 1138, REPAIRED BY REMOVING CORROSION PER SRM 51-10-6, TREATED AND PAINTED STA 950F THROUGH 1110, SPLICED IN NEW SECTION OF TRACK FROM STA 1110 TO 1130 LT OUTBOARD SPLICED IN NEW SECTION OF TRACK FROM STA 1110 TO 1130 LT INBOARD PER SRM 53-20-11 PG 803.
Part: DOUBLER — REQ REPLACEMENT (STA 1060)
AT HMV FOUND TIME LIMITED REPAIR AT FS1060 BETWEEN STR 21 AND 22L. INSTALLED PERMANENT REPAIR PER SRM 53-30-3 FIG 1.
Part: SKIN — DAMAGED (LT AILERON)
DURING HMV, FOUND L/W OB AILERON HOLE NEXT TO WT AND BALANCE PLACARD ON I/B UNDERSIDE. REPAIRED PER SRM 57-50-5.
Part: FRAME — CRACKED (FS 804.95)
DURING HMV, FOUND FS 804.95 FRAME CRACKED, RT SIDE JUST BELOW WINDOW FRAME. REPAIRED PER SRM 53-10-4 FIG 22.
Part: BONDNG WIRE HOLE — ELONGATED (LT AILERON)
DURING HMV, FOUND O/B LT WG AILERON BONDING WIRE ATTACH HOLE IS ELONGATED AT O/B TAB CUTOUT AREA. RPAIRED PER SRM 57-50-5 FIG 3.
Part: UPLOCK SUPPORT — DAMAGED (WS 913)
AT HMV, LEFT MLG UPLOCK SUPPORT FRAME AT FS 913 WAS FOUND WITH TIME LIMITED REPAIR. INSTALLED PERMANENT REPAIR PER MM 53-11-0 PG 815.
Part: SUPPORT — WORN (NR 2 ENGINE)
THE NR 2 FWD COWL MATING SUPPORT RING FOUND WORN AT HMV. INSTALLED SPLICES AND REPAIR ANGLE PER MM 53-11-0.
Part: SKIN — STOP DRILLED (VERTICAL STAB.)
DURING HMV, FOUND VERTICAL STABILIZER EXTERIOR SKIN HAS A STOP DRILL ON RT SIDE 20 INCHES FWD OF REAR SPAR AT FUSELAGE, REPAIRED PER FABRICATING DOUBLER PER MM 55-30-0 PG 801 CRACK PREVIOUSLY STOP DRILLED, DYE CHECKED CRACK AND NO FURTHER DAMAGE. INSTALLED DOUBLER PER MM 55-30-0 PG 801.
Part: SKIN — CRACKED (STA 1125 STR 27R)
SKIN BULGED AND CRACKED STA 1125 STR 27 RT. FOUND AT HMV. REPAIRED PER SRM 53-30-3 FIG.
Part: WEB — CRACKED (STA 1303)
AT HMV THE WEB INSIDE VERT STAB HAD 2 CRACKS IN RT LOWER CORNER AT STA 1303. STOP DRILLED CRACK AND REPAIRED PER SRM 53-10-4.
Part: WEB — CRACKED (STA 1303)
AT HMV THE WEB INSIDE VERT STAB JUST ABOVE S-DUCT WAS CRACKED AT THE LT LOWER CORNER. STOP DRILLED THE CRACK AND FABRICATED REPAIR PER SRM 53-10-4. INSTALLED REPAIR.
Part: STRINGER — CORROSION (STA 1050 STR 28L)
AFT B/B CORROSION ON O/B SIDE OF STR 28L FS 1050-1070 NEAR JUNCTURE WITH FUS SKIN. FOUND AND REPAIRED AT HMV. REPAIRED PER SRM 53-10-3.
Part: SKIN CLIP — CORRODED (STA 970 IB 29R)
AFT BB SKIN CLIP CORRODED STA 970 LOWER LEG OF FRAME AFT SIDE BETWEEN 30 AND 29R. REPAIRED PER MM 53-11-0 FIG 815.
Part: SKIN — CORRODED (STA 1065 STR 28L)
AT HMV, FOUND AFT B/B FUSELAGE SKIN WITH CORROSION DAMAGE UNDER A PREVIOUS REPAIR AT FS 1065 AT STR 28L. REPAIRED PER SRM 53-30-3.
Part: SKIN — CRACKED (STA 700 STR 26L)
AT HMV, FOUND FUSELAGE SKIN CRACKED AT FS 700 AT STR 26L. REMOVED DAMAGED AREA, REPAIRED PER SRM 53-30-3.
Part: STRINGER — CORRODED (FS 970-990 29L)
AT HMV, FOUND AFT CARGO STRINGER 29L CORRODED BETWEEN STA 970 AND 990. REPAIRED PER DL ERA 301274-14.
Part: STRINGER — CORRODED (STA 1050 STR 28R)
AT HMV, FOUND STR 28R CORRODED AT SPLICE AT FS 1050. REPAIRED PER SRM 53-10-3.
Part: RIB — CRACKED (RT LE SLAT)
DURING HMV, FOUND NR 6 LEADING EDGE SLAT TAI 'T' DUCT HAS EXCESSIVE PLAY AT 'T' JOINT. THE ADJACENT O/B RIB TO ABOVE BAY IS CRACKED AT FWD CLOSURE CHORD. REPAIRED PER MM 57-54-0 PG 806.
Part: FRAME — CORRODED (BS 1130)
AFT BB FRAME CORRODED, STA 1130 BETWEEN STR 28R AND 29R. REPAIRED PER 53-11-0 PAGE 825. FOUND AT HMV.
Part: RIB — CRACKED (RT LE FLAP)
DURING HMV, FOUND NR 6 LEADING EDGE SLAT RIB MARKED '11' IS CRACKED BEHIND CLOSURE CHORD. REPAIRED PER MM 57-54-0.
Part: RIB — CRACKED (LT LE SLAT)
DURING HMV, FOUND NR 1 LEADING EDGE SLAT RIB MARKED NR 4 HAS CRACKED ATTACH ANGLE. REPAIRED BY REPLACING ANGLE.
Part: STRINGER — CRACKED (LT WING)
AT HMV, AFT SIDE OF FORWARD VENT BOX STRINGER CRACKED AT RIB ATTACH, WS 686.5, LT WING. REPAIRED PER MM 57-13-0 PG 808.
Part: NOSE COWL — WORN (NR 1 ENGINE)
NOSE COWL, FLANGE WORN, NR 1 ENG NOSE COWL AFT FLANGE IS WORN TO RAZOR EDGE AT 7:00 POSITION. INSTALLED DOUBLER PER SRM 54-10-3. NR 290.
Part: STRINGER — CORRODED (BS 1183)
AFT BB STRINGER END IS CORRODED, NR 29R AT STA 1183. REPAIRED PER SRM 53-10-3 FIG 1. FOUND AT HMV.
Part: STRINGER — CRACKED (FS 720)
AT HMV, FOUND STRINGER 15R CRACKED AT ITS ENDS AT WING ICE LIGHT HOUSING FS 720C. REPAIRED PER SRM 53-1-03.
Part: SKIN — CRACKED (NR 6 LE FLAP)
NR 6 LE SLAT INTERIOR SKIN CRACKED, LOCATED IN BAY IB OF ACTUATOR RIBS. REPAIRED PER MM 57-54-0 PG 804. FOUND AT HMV.
Part: STRINGER — CRACKED (CABIN)
DURING HMV FOUND L/W L/E LIGHT BOX, STR 15L IS CRACKED ON FWD AND AFT SIDES OF LIGHT BOX, REPAIRED PER SRM 53-10-3 FIG 1 DETAIL II FOR FWD AND AFT.
Part: RIBS — CRACKED (RT LE SLAT)
DURING HMV FOUND NR 4 SLAT ACTUATOR RIB MARKED NR 12 CRACKED 3 PLACES AND RIB MKD NR 11 CRACKED IN FWD LOWER RADIUS, REPAIRED PER M/M 57-54-0 PG 805.
Part: FRAME — BROKEN (AFT BAG BIN)
DURING HMV, FOUND AFT BAG BIN FRAME BROKEN AT STA 970 ABOVE STRINGER 23 L, REPAIRED BY CUTTING OUT DAMAGE DYE CHECKED PER 900-6-3 NR 1, NO CRACK FOUND. FABRICATED DOUBLER AND FILLER INSTALLED REPAIR PER SRM 53-10-4.
Part: SKIN CLIP — CORRODED (STA 970 IB 28R)
AFT BB SKIN CLIP CORRODED STA 970 AFT SIDE BETWEEN STR 29R AND 28R. FOUND AND REPAIRED AT HMV, PER MM 53-11-0 PG 815.
Part: RIBS — CRACKED (RT LE SLAT)
DURING HMV FOUND NR 4 LEADING EDGE SLAT RIB MARKED NR 21 CRACKED AT FWD CLOSURE CHORD, REPAIRED PER M/M 57-54-0 PG 806.
Part: FLAP — CORROSION (NR 3 MID)
NR 3MID FLAP DURING HMV INSP WAS FOUND TO HAVE CORROSION IN THREE THRUST BEARING RETAINER BOLT HOLES.
Part: DOUBLER — MIS INSTALLED (NR 3 MID FLAP)
NR 3 MID FLAP DURING HMV INSP WAS FOUND TO HAVE IMPROPERLY INSTALLED DOUBLER ON AFT LOWER SPAR AT QUADRANT PUSH ROD CUTOUT I/B END. THIS IS A REWRITE FROM CARD NR 4974.
Part: FLAP — DAMAGED (NR 1 FORE LE)
NR 1 FORE FLAP, TWO TEMP REPAIRS ON LEADING EDGE NEAR I/B END ON UPPER SIDE OF FLAP. FOUND DURING HMV, SHOP INSP. REPLACED TEMP REPAIRS WITH PERM REPAIR AS PER 57-50-4, FIG 1.
Part: FLAP — CRACKED (NR 2 MID)
NR 2 MID FLAP, CRACK IN LOWER AFT SPAR CHORD AT 41 INCHES FROM O/B END OF FLAP AND ONE AT 18 INCHES FROM I/B END OF FLAP. REPAIRED PER M/M 575200 PG 807, INSTALLED DOUBLER. FOUND AT HMV SHOP INSPECTION.
Part: FLAP — WORN (NR 1 FORE)
NR 1 FORE FLAP, LEADING EDGE WORN 12 INCHES FROM I/B END LOWERSIDE. FOUND DURING HMV, SHOP INSPECTION. REPAIRED PER SRM 57-50-4, FIG 1.
Part: FLAP — DAMAGED (NR 1 FORE LE)
NR 1 FORE FLAP, TEMP REPAIR INSTALLED ON LEADING EDGE, 48 INCHES FROM O/B END. FOUND AT HMV, SHOP INSPECTION. REPAIRED PER SRM 57-50-4, FIG. 1
Part: FLAP — CORROSION (NR 3 MID)
NR 3 MID FLAP DURING HMV INSP WAS FOUND TO HAVE CORROSION I/B CARRIAGE FITTING IN THE I/B THRUST BEARING RETAINER BOLT HOLE CORROSION WAS REPAIRED PER SRM 57-50-4.
Part: FLAP — CORRODED (RT TE MID FLAP)
THE NR 4 MID FLAP, I/B AND O/B CARRIAGE SUPPORT HOUSING BOTTOM SURFACE EACH HAVE 5 BOLT HOLES CORRODED. REPAIRED PER SRM 57-50-04 REAMED AND BUSHED HOLES. ALSO, I/B HAS 2 DAMAGED SPRING ATTACH BOLT HOLES. REPAIRED PER SRM 57-50-04. REAMED AND BUSHED HOLES. FOUND AT HMV SHOP INSPECTION.
Part: FLAP DOUBLER — MIS INSTALLED (NR 3 MID)
NR 3 MID FLAP DURING HMV INSP WAS FOUND TO HAVE AN IMPROPERLY INSTALLED DOUBLER ON THE AFT LOWER SPAR AT I/B QUADRENT PUSH ROD CUTOUT.
Part: SPAR — CRACK (NR 3 MID FLAP)
NR 3 MID FLAP DURING HMV INSP WAS FOUND TO HAVE A CRACKED AFT LOWER SPAR 55 INCHES FROM I/B END.
Part: FLAP — CORRODED (RT TE MID FLAP)
THE NR 4 MID FLAP, I/B CARRIAGE THRUST BEARING RETAINER UPPER I/B AND O/B BOLT HOLES CORRODED. REPAIRED PER SRM 57-57-04, REAMED AND BUSHED HOLES. FOUND AT HMV SHOP INSPECTION.
Part: NOSE COWL — DAMAGED (NR 1 ENGINE)
TWO TEMP REPAIRS LOCATED AT THE 5:00 AND 6:00 POSITIONS IN THE NOSE COWL LIP SKIN. C/W ERA 258540-14 BY INSTALLING DOUBLER PER SRM 54-30-3 FIGURE 2. N/R'S 202 AND 5.
Part: TEE — CORROSION (PANEL 3348)
AT HMV, FOUND CORROSION AT LOWER FUSELAGE HINGED PANEL 3348 FRAME WHERE HINGES ATTACH, IN THE RADIUS OF FRAME BEAM. REPAIRED ATTACH 'T' PER M/M 53-30-1, REPAIRED FORMED SECTION PER SRM 51-40-3 FIG 1.