N98876

No registry detail on file · not in current registry

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.

21 reports on file, 1995-04-06 – 2002-12-17.

OTHER · 2002-12-17 Matched by certificate designator
ATA 5330

Part: SKIN — CRACKED (@MCD) · airframe 45,648 hrs · 23,260 cycles

INSPECTION FOUND A 1" CRACK IN FUSELAGE SKIN AROUND HOLD OPEN HOOK AT MAIN CABIN DOOR. DOUBLERS WERE INSTALLED IAW SRM 53-04, FIGURE 24.

Source: SDR CALA0200589
OTHER · 2002-11-25 Matched by certificate designator
ATA 5350

Part: CABLE — FRAYED (TAILCONE) · airframe 45,648 hrs · 23,260 cycles

THE TAILCONE DROP TEST FAILED AT EACH OF THREE LOCATIONS. MAINTENANCE FOUND THE LEFT UPPER TAILCONE JETTISON CABLE FRAYED IN TWO PLACES. THE CABLE WAS REMOVED AND REPLACED. PERFORMED ADJUSTMENT OF TAILCONE RELEASE SYSTEM IAW MM 53-53-00.

Source: SDR CALA0200564
OTHER · 2002-11-22 Matched by certificate designator
ATA 5311

Part: BELTFRAME — CRACKED (STA 1418) · airframe 45,648 hrs · 23,260 cycles

INSPECTION FOUND A 1" CRACK IN BELTFRAME AT STA 1418, LONGERON 2R. A REPAIR WAS INSTALLED IAW ECRA 5310-04296.

Source: SDR CALA0200559
OTHER · 2002-11-16 Matched by certificate designator
ATA 5311

Part: LONGERON — CORRODED (STA 1287) · airframe 45,648 hrs · 23,260 cycles

INSPECTION FOUND AFT CARGO BELT FRAME CORRODED AT STA 1287, LONGERON 30. THE BELTFRAME WAS REMOVED AND REPLACED IAW SRM 51-30-02.

Source: SDR CALA0200555
OTHER · 2002-11-14 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FUSELAGE) · airframe 45,648 hrs · 23,260 cycles

INSPECTION FOUND CUSP WEB CORRODED IN CABIN AT RT SIDE, STA 513-579. THE CUSP WEB SECTION WAS REPLACED IAW SRM 51-30-2.

Source: SDR CALA0200551
OTHER · 2002-11-11 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,648 hrs · 23,260 cycles

INSPECTION FOUND CENTER FLOOR SUPPORT ANGLE CORRODED AT STA 1174 BETWEEN LEFT AND RIGHT I/B SEAT TRACKS. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5.

Source: SDR CALA0200543
OTHER · 2002-11-11 Matched by certificate designator
ATA 5313

Part: LONGERON — CRACKED (STA 1418) · airframe 45,648 hrs · 23,260 cycles

INSPECTION FOUND A 1" CRACK IN LONGERON 2L AT STA 1418. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 18.

Source: SDR CALA0200545
OTHER · 2002-11-09 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,648 hrs · 23,260 cycles

INSPECTION FOUND FORWARD ENTRY I/B FLOOR SUPPORT FOR PANEL K AND O/B SUPPORT FOR PANEL I AND J CORRODED THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-0.

Source: SDR CALA0200538
OTHER · 2002-11-08 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (STA 218-265) · airframe 45,648 hrs · 23,260 cycles

INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 218-265. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05-4F AND 53-05-4B1.

Source: SDR CALA0200537
OTHER · 2002-11-08 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,648 hrs · 23,260 cycles

INSPECTION FOUND FLOOR SUPPORT BETWEEN PANEL H AND G CORRODED AT STA 148.5 TO 200. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-0.

Source: SDR CALA0200536
OTHER · 2002-11-07 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (STA 1193-1309) · airframe 45,648 hrs · 23,260 cycles

INSPECTION FOUND L/H I/B SEAT TRACK CORRODED AROUND HOLES AT STA 1193-1309. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-5.

Source: SDR CALA0200534
Earlier reports · 1995–2000 · 10 reports

2000

WARNING INDICATION · 2000-07-06 Matched by certificate designator
ATA 3222

Part: STRUT — DISCHARGED (NLG) · airframe 42,314 hrs · 21,309 cycles

WHEN GEAR WAS RETRACTED AFTER TAKEOFF FROM IAH, THE HANDLE CAME UP, BUT THREE RED LIGHTS AND 1 YELLOW WERE ILLUMINATED ACCOMPANIED BY GEAR NOISE. THE HANDLE WAS LOWERED AND THREE GREEN LIGHTS WERE INDICATED WITH GEAR DOOR LIGHT OUT. THE GEAR WAS RECYCLED WITH SAME RESULTS. THE AIRCRAFT WAS RETURNED TO IAH. WHEN SPOILER HANDLE WAS TRIED ON LANDING, THE HANDLE WOULD NOT MOVE. RECYCLED C/B''S L-33 AND K-33, BUT SPOILER HANDLE STILL WOULD NOT MOVE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE LANDING GEAR WAS EXTENDED AND RETRACTED 10 TIMES IAW MM 32-30-00 AND OPERATION AND INDICATIONS CHECKED GOOD. SPOILER OPERATION CHECKED GOOD IAW MM 27-60-00. A FULL NOSE STRUT SERVICING WAS PERFORMED IAW MM 32-21-02.

Source: SDR CALA0001014

1999

FALSE WARNING · 1999-06-29 Matched by certificate designator
ATA 3260

Part: INDICATION — MALFUNCTIONED (LANDING GEAR)

THREE RED GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING ROC. CYCLING THE GEAR WAS NO HELP. THE AIRCRAFT WAS RETURNED TO ROC WHERE IT LANDED WITHOUT INCIDENT. THE GEAR WAS SWUNG SEVERAL TIMES AND THE PROBLEM COULD NOT BE DUPLICATED. AN ADJUSTMENT/TEST WAS PERFORMED ON THE GEAR INDICATION IAW MM 32-60-00 AND ALL CHECKED GOOD.

Source: SDR CALA9900748

1998

FALSE WARNING · 1998-07-14 Matched by certificate designator
ATA 3260

Part: LAMPS — FAILED (NLG)

THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON APPROAC. ALL OTHER INDICATIONS APPEARED NORMAL AND GEAR WAS MECHANICALLY CONFIRMED DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED ALL FOUR NOSE GEAR INDICATION LAMPS. A GEAR RETRACTION WAS PERFORMED IAW MM 32-60-00, PAGE 201 WITH OPERATION AND INDICATIONS CHECKING GOOD.

Source: SDR CALA9801244
NO TEST · 1998-05-23 Matched by certificate designator
ATA 3350

Part: BATT CHARGER — INOPERATIVE (CABIN)

INSPECTION FOUND AFT SECTION OF SEAT TRACK EMERGENCY LIGHTS INOPERATIVE. THE AFT SEAT TRACK EMERGENCY LIGHT BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATION OF EMERGENCY LIGHTS WAS RESTORED.

Source: SDR CALA9800901

1997

WARNING INDICATION · 1997-08-15 Matched by certificate designator
ATA 3233

Part: ACTUATOR — INOPERATIVE (NLG)

THE AIRCRAFT HAD A BRIEF HISTORY OF THE NLG RED UNSAFE LIGHT REMAINING ILLUMINATED AFTER GEAR RETRACTION. CYCLING THE GEAR CORRECTED THE PROBLEM. MAINTENANCE FOUND THE NLG ACTUATOR AT FAULT. THE NLG ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-32-06. LEAK AND OPERATIONAL CHECKS WERE GOOD.

Source: SDR CALA9701221
OTHER · 1997-04-16 Matched by certificate designator
ATA 5350

Part: CLAMP — BROKEN (TAIL CONE)

DURING 1/4 D-CHECK INSP, FOUND TAIL CONE RELEASE CONDUIT CABLE HAS CLAMP AT LOWER END BROKEN. REMOVED AND REPLACED BROKEN CLAMP WITH NEW CLAMP (P/N AN74206).

Source: SDR CALA9700630
WARNING INDICATION · 1997-03-02 Matched by certificate designator
ATA 3233

Part: ATTACH LINK — BROKEN (LT MLG ACTUATOR)

THE LEFT MLG WOULD NOT INDICATE UP AND LOCKED AND THE RED LT MLG LIGHT REMAINED ON WITH AMBER GEAR DOOR LIGHT ILLUMINATED AFTER TAKEOFF. WHEN GEAR WAS EXTENDED FOR LANDING, CREW RECEIVED THREE GREEN AND DOOR CLOSED LIGHTS WERE NORMAL. MAINTENANCE FOUND THE LT MLG ACTUATOR LOWER ATTACH LINK BROKEN. THE LOWER ATTACH LINK WAS REPLACED IAW MM 32-32-02 AND OVERHAUL MANUAL 32-17-00, PAGE 601. IN ADDITION, THE LT MLG ACTUATOR UPPER ATTACH LINK WAS REPLACED AS A PRECAUTIONARY MEASURE. OPERATIONAL CHECKS WERE GOOD.

Source: SDR CALA9700300

1996

OTHER · 1996-10-05 Matched by certificate designator
ATA 5330

Part: SKIN — TORN (CARGO DR CUTOUT)

INSPECTION FOUND ALL SKIN LAYERS TORN 1.5 INCH DEEP AT MID CARGO DOOR FRAME LOWER AFT CORNER. A DOUBLER AND TRIPLER WERE INSTALLED IAW ECRA 5330-02447.

Source: SDR CALA960147S
OTHER · 1996-07-14 Matched by certificate designator
ATA 5530

Part: ATTACH ANGLE — CRACKED (DORSAL FIN)

INSPECTION FOUND RT DORSAL FIN ATTACH ANGLE CRACKED. THE ANGLE WAS REPAIRED IAW EA 5340-01012.

Source: SDR CALA9601143

1995

FALSE WARNING · 1995-04-06 Matched by certificate designator
ATA 3260

Part: SENSOR — OUT OF ADJUST (NLG)

IAH - FLT 0458 - THE NLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE LIGHT EXTINGUISHED. THE POSITION SENSOR ON THE NOSE GEAR DRAG BRACE WAS ADJUSTED PER MM 32-60-00, PAGE 218. THE AIRCRAFT HAS FLOWN OVER 15 FLIGHTS WITHOUT A REPEAT OF THE PROBLEM SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTED. (X)

Source: SDR CAL950262