# N995Z: 1967 Douglas DC-9-32, registration cancelled 2013-03-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 21, 2013 - Status when cancelled: Sale reported, canceled - Airframe: [Douglas DC-9-32](https://openairdocs.org/model/douglas-dc-9-32) (registry code 3022066) - Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47027 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard - Last registry action: March 5, 2010 - Mode S code: ADE775 - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Individual - Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N995Z - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=995Z - Page: https://openairdocs.org/deregistered/N995Z-2013-03-21 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Douglas DC-9-32: https://openairdocs.org/model/douglas-dc-9-32.md ## Service difficulty reports (67, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ZW0A0100901](https://openairdocs.org/sdr/ZW0A0100901), Apr 27, 2001: WHEEL. FAILED. DURING LANDING THE LEFT LANDING GEAR INBD WHEEL RIM FAILED. SOME METAL SEPARATED AND THE TIRE ROLLED OFF THE RIM DAMAGING SOME AREAS OF THE GEAR INCLUDING THE G - [SDR TWAA0101602](https://openairdocs.org/sdr/TWAA0101602), Jan 21, 2001: BATTERY PACK. DISCHARGED. THE EMERGENCY CABIN LIGHTS AT THE LEFT NUMBER 1 CABIN DOOR, RT NUMBER 1, AND COCKPIT DOORS CAME ON WHEN THE SWITCH IS ARMED. REPLACED THE BATTERY PACK. CHECK-C - [SDR TWAA0101301](https://openairdocs.org/sdr/TWAA0101301), Jan 21, 2001: BATTERY PACK. DISCHARGED. THE CABIN EMERGENCY LIGHTS AT THE LEFT SIDE NUMBER 1 DOOR, RT SIDE NUMBER 1 DOOR, AND COCKPIT DOOR WERE ON WITH THE SWITCH IN ARM POSITION. REPLACED THE BATTERY - [SDR TWAA0101017](https://openairdocs.org/sdr/TWAA0101017), Jan 11, 2001: LONGERON. CRACKED. DURING CHECK-C MAINT, LONGERON 2R WAS CRACKED AT FORMER RING AT STA 658. FOUND DURING VISUAL INSPECTION FOR MC8-AD-AM. REPLACED CRACKED SECTION OF LONGERON AND - [SDR TWAA0101016](https://openairdocs.org/sdr/TWAA0101016), Jan 11, 2001: LONGERON. CRACKED. DURING CHECK-C MAINT, LONGERON 5L WAS CRACKED AT FORMER RING AT STA 737. FOUND DURING VISUAL INSPECTION FOR MD8-AD-AM. INSTALLED NEW SECTION OF LONGERON AND MAN - [SDR TWAA0003604](https://openairdocs.org/sdr/TWAA0003604), Mar 4, 2000: DOOR LATCH. UNSECURE. FWD ACC COMPT DOOR LIGHT ILLUMINATED AT LIFT OFF.. FOUND R LATCH LOOSE ON FWD ACC DOOR NEAREST LIGHT SWITCH. SECURED LATCH. CC00 11-11-99 STL. - [SDR TWAA0101020](https://openairdocs.org/sdr/TWAA0101020), Jan 18, 2000: LONGERON. CRACKED. DURING CHECK-C MAINT, LONGERON 3R WAS CRACKED AT FORMER RING STA 639. INSTALLED NEW LONGERON SECTION AND SPLICE PER SRO9530128. - [SDR TWAA9915203](https://openairdocs.org/sdr/TWAA9915203), Nov 8, 1999: SKIN. CRACKED. DURING CHECK-C MAINT, FOUND 2 CRACKS IN SKIN IN FWD UPPER CORNER OF THE RT SIDE FORWARD CABIN SERVICE DOOR JAM. CRACKS WERE .0625 IN AND .3125 IN LONG COMING OU - [SDR TWAA9915103](https://openairdocs.org/sdr/TWAA9915103), Nov 4, 1999: SKIN. CRACKED. DURING CHECK-C MAINT, TWO SKIN CRACKS WERE FOUND ON THE FORWARD CARGO DOOR, LOWER AFT CORNER, FUSELAGE STA 427 AND LONGERON 27R. CRACKS WERE 13/32 AND 5/32 IN L - [SDR TWAA9915001](https://openairdocs.org/sdr/TWAA9915001), Nov 3, 1999: DOUBLER. CRACKED. DURING CHECK-C MAINT, FOUND 3 CRACKS IN INTERNAL SKIN DOUBLER AT FWD ENTRY DOOR CUTOUT. CRACKS WERE 3 INCHES, 1.75 IN, AND .75 IN. REMOVED DAMAGED MATERIAL AND - [SDR TWAA9914905](https://openairdocs.org/sdr/TWAA9914905), Nov 2, 1999: END CAP. CRACKED. DURING CHECK-C MAINT, FOUND LONGERONS R2 AND L2 WITH THE END CAPS CRACKED AT STA 1076, EACH WITH APPROXIMATELY A 1.5 INCH CRACK. REPLACED EACH LONGERON SECTION - [SDR TWAA9904402](https://openairdocs.org/sdr/TWAA9904402), Mar 23, 1999: BATTERY PACK. DISCHARGED. THE CABIN EGRESS LIGHTS WERE FOUND INOPERATIVE FROM SEAT ROW 16 TO 21. REPLACED BATTERY PACK. CHECK-C 8-31-98 MCI. - [SDR TWAA9813207](https://openairdocs.org/sdr/TWAA9813207), Aug 13, 1998: BULKHEAD JAMB. DAMAGED. DURING CHECK-C MAINT, AN INTERIM REPAIR WAS FOUND ACCOMPLISHED WITH BLIND FASTENERS ON A CRACK AT THE AFT PRESS BLKHD DOOR JAMB, RT SIDE. INSTALLED DOOR JAMB PE - [SDR TWAA9812506](https://openairdocs.org/sdr/TWAA9812506), Aug 3, 1998: DOUBLER. CORRODED. DURING OP 16 MAINT CHECK, FOUND REINFORCING DOUBLER ABOVE JACK PAD ABOVE SKIN WITH CORROSION, FS 996 LONGERON 28L TO L28R. REMOVED DOUBLER FOR REPLACEMENT PER S - [SDR TWAA9812504](https://openairdocs.org/sdr/TWAA9812504), Aug 3, 1998: BULKHEAD ANGLE. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION ON L-ANGLE AT PRESSURE BULKHEAD UNDER REPAIR 6 IN LBL TO 6 IN RBL. REMOVED L-ANGLE DOUBLER NR 9915661-33 FOR REPLACEME - [SDR TWAA9812514](https://openairdocs.org/sdr/TWAA9812514), Jul 29, 1998: SKIN. CORRODED. DURING OP 16 MAINT CHECK, FOUND FUSELAGE CORROSION CLEAN UP BEYOND MANUAL LIMITS, 30 PERCENT REMOVED, AT FS 993, LONGERON 29L ON FUSELAGE SKIN. REPAIRED DAMAGED - [SDR TWAA9812513](https://openairdocs.org/sdr/TWAA9812513), Jul 29, 1998: SKIN. CORRODED. DURING OP 16 MAINT CHECK, FOUND ON LOWER FUSELAGE CORROSION AND FASTENER HEADS MISSING AT LOWER FWD CORNER OF THE AFT LAV DUMP SERVICE DOOR. CUT OUT CORRODED MA - [SDR TWAA9812507](https://openairdocs.org/sdr/TWAA9812507), Jul 26, 1998: SKIN. CRACKED. DURING OP 16 MAINT CHECK, FOUND SKIN CRACKED AT STA 192, STR 22L, .1875 IN LONG AT 10 O'CLOCK. REMOVED CRACK PER SRM 53-04, P33 NOTE NR 1. INSTALLED REPAIR PER - [SDR TWAA9812119](https://openairdocs.org/sdr/TWAA9812119), Jul 23, 1998: SKIN. CRACKED. DURING OP 16 MAINT CHECK, ON RT WING UPPER SURFACE WING SKIN FOUND CRACK AT O/B AFT CORNER OF FUEL TANK ACCESS PLATE NR 1410A. STOP DRILLED CRACK, INSTALLED DOU - [SDR TWAA9812118](https://openairdocs.org/sdr/TWAA9812118), Jul 23, 1998: FLOOR. CRACKED. DURING OP 16 MAINT CHECK, FOUND RT CENTER CABIN FLOOR PANEL AT FS 465 TO 579 WITH 5 CRACKS AT U-CHANNELS ON BOTTOM SIDE, NR 39 PANEL. NEW PANEL FABRICATED PER S - [SDR TWAA9812117](https://openairdocs.org/sdr/TWAA9812117), Jul 23, 1998: LONGERON. CRACKED. DURING OP 16 MAINT CHECK LONGERON 23L HAD 1.5 IN CRACK IN O/B FLANGE RUNNING DOWN INTO RADIUS AT FS 200. CONFIRMED BY EDDY CURRENT. REMOVED CRACKED LONG, INSTAL - [SDR TWAA9812116](https://openairdocs.org/sdr/TWAA9812116), Jul 22, 1998: BULKHEAD CHORD. CORRODED. DURING OP 16 MAINT CHECK, FOUND AT FS 604, THE AFT BULKHEAD OF THE FWD CARGO COMPT, THE BOTTOM CHORD AT STA 30 HAD AREA OF CORROSION. REMOVED CORROSION PER SRM - [SDR TWAA9812115](https://openairdocs.org/sdr/TWAA9812115), Jul 22, 1998: TIE. CORRODED. DURING OP 16 MAINT CHECK, FOUND STRINGER END TIE CORRODED AT STA 994, STR 27R AND 28R. REMOVED AND REPLACED 2 (P/N 4912515-1), INSTALLED FASTENERS PER SRM 51-30 - [SDR TWAA9812121](https://openairdocs.org/sdr/TWAA9812121), Jul 21, 1998: SKIN. CORRODED. DURING OP 16 MAINT CHECK, FOUND AT BOTTOM OF FUSELAGE SKIN AT FWD END OF RT WHEEL WELL, CORROSION THRU WHERE HINGE PIN SHIELD COVERS. REMOVED CORROSION PER SRM - [SDR TWAA9812120](https://openairdocs.org/sdr/TWAA9812120), Jul 21, 1998: BULKHEAD. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION AT BOTTOM OF AFT PRESSURE BULKHEAD, 6 IN LBL TO 6 IN RBL. REMOVED CORROSION BY CUTTING OUT CORRODED SECTION PER SRM 53 - [SDR TWAA9812124](https://openairdocs.org/sdr/TWAA9812124), Jul 20, 1998: INTERCOSTAL. CORRODED. DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL AT 29R BADLY CORRODED AT STA 965 TO 980. MADE NEW PER SRM 51-01, FABRICATED INTERCOSTAL FROM 7075-0 AND HEAT TREATED - [SDR TWAA9812123](https://openairdocs.org/sdr/TWAA9812123), Jul 20, 1998: DOUBLER. MISINSTALLED. DURING OP 16 MAINT CHECK, FOUND REPAIR INSTALLED WITH BLIND FASTENERS ON FUSELGE SKIN AND NO DOUBLER AT STA 965 AND 970 BETWEEN LONG 16L AND 17L. REPLACED BLIND - [SDR TWAA9812122](https://openairdocs.org/sdr/TWAA9812122), Jul 20, 1998: LONGERON. CRACKED. DURING OP 16 MAINT CHECK, FOUND LONGERON 17L CRACKED AT STA 965. REPLACED SECTION OF LONGERON FROM FS 955 TO 996, PER SRM 51-10, PG 1 ITEM C, AND INSTALLED LONG - [SDR TWAA9812005](https://openairdocs.org/sdr/TWAA9812005), Jul 20, 1998: BULKHEAD WEB. CRACKED. DURING OP 16 MAINT CHECK, FOUND BULKHEAD 965 RBL 58, APPROX 28 IN ABOVE FLOOR LINE WITH CRACK IN WEB. STOP DRILLED AND INSTALLED DOUBLER. INSTALLED NEW WEB PER - [SDR TWAA9812004](https://openairdocs.org/sdr/TWAA9812004), Jul 20, 1998: BULKHEAD DOUBLER. CORRODED. DURING OP 16 MAINT CHECK, FOUND SPAR WEB DOUBLER ON AFT SIDE OF BULKHEAR WEB, STA 965 RT SIDE, CRACKED. REPAIRED WITH .090 DOUBLER 2024-T3 AND INSTALLED PER MO - [SDR TWAA9812302](https://openairdocs.org/sdr/TWAA9812302), Jul 17, 1998: FORMER. CORRODED. DURING OP 16 MAINT CHECK, FOUND FORMER CORRODED AT INBD ANGLE STA 1038, BETWEEN S15R AND S17R. CORROSION GROUND TO A DEPTH OF .090. REMOVED CORROSION PER SRM 51 - [SDR TWAA9812003](https://openairdocs.org/sdr/TWAA9812003), Jul 15, 1998: FRAME. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION AT STA 965, FORMER S29L TO S29R. SPLICE REPAIRED FORMER PER SRM 53-03, FIG 2A. - [SDR TWAA9812002](https://openairdocs.org/sdr/TWAA9812002), Jul 15, 1998: SKIN. CRACKED. DURING OP 16 MAINT CHECK, FOUND A CRACK IN FUSELAGE SKIN LEFT SIDE JUST BELOW THE LEFT PYLON STA 965. AREA HAD AN INTERIM REPAIR WITH BLIND FASTENERS. ACCOMP ED - [SDR TWAA9811909](https://openairdocs.org/sdr/TWAA9811909), Jul 15, 1998: LONGERON. CORRODED. DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 24L WITH INNER GRANULAR CORROSION ON ATTACH FITTING AT FWD SIDE OF FS 996. REMOVED CORROSION PER SRM 51-10-03, ST - [SDR TWAA9811908](https://openairdocs.org/sdr/TWAA9811908), Jul 13, 1998: BULKHEAD CLIP. CRACKED. DURING OP 16 MAINTENANCE CHECK, FOUND 2 INCH CRACK ON STA 1143 CANTED BULKHEAD WEB CLIP, RT SIDE A RUDDER TRIM CABLE CUT-OUT. REPLACED CRACKED ANGLE PER SRM 51- - [SDR TWAA9811907](https://openairdocs.org/sdr/TWAA9811907), Jul 13, 1998: INTERCOSTAL. CRACKED. DURING OP 16 MAINTENANCE CHECK, FOUND INTERCOSTAL AT STA 513 ABOVE S27R CRACKED. REPAIRED PER SRM 53-01, PG 10. INSTALLED DOUBLER REPAIR. ACFT TT: 77,210 HOURS. - [SDR TWAA9811903](https://openairdocs.org/sdr/TWAA9811903), Jul 13, 1998: LONGERON. CRACKED. DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 29R CRACKED JUST FORWARD ON STATION 587 FRAME. REMOVED AND REPLACED LONGERON END PER DWG INST 592176 PER SRM 51-0 - [SDR TWAA9811906](https://openairdocs.org/sdr/TWAA9811906), Jul 10, 1998: SKIN. CORRODED. DURING OP 16 MAINTENANCE CHECK, FOUND SKIN PILLOWING AT FS 575 TO FS 604, L27R THROUGH LONGERON 27L. REMOVED FRAMES FROM FS 579 TO FS 604. REMOVED LONGERONS 26L - [SDR TWAA9811905](https://openairdocs.org/sdr/TWAA9811905), Jul 10, 1998: LONGERON. CRACKED. DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 30 CRACKED JUST FORWARD OF STA 578 FRAME. INSTALLED NEW LONGERON END PER INSTL DWG 592176 PER SRM 51-01, PG 1 ITE - [SDR TWAA9811904](https://openairdocs.org/sdr/TWAA9811904), Jul 10, 1998: LONGERON. CRACKED. DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 29L CRACKED JUST FORWARD OF STA 578 FRAME. REMOVED AND REPLACED LONGERON END PER INSTL DWG 592176 PER SRM 51-01, - [SDR TWAA9811902](https://openairdocs.org/sdr/TWAA9811902), Jul 8, 1998: FLOOR PANEL. CRACKED. DURING OP 16 MAINTENANCE CHECK, FOUND FORWARD CABIN FLOOR PANEL NR 40 WITH HAT SECTIONS CRACKED IN SEVERAL PLACES. REPLACED CRACKED HAT SECTIONS IN FLOOR PANEL - [SDR TWAA9811003](https://openairdocs.org/sdr/TWAA9811003), Jul 7, 1998: RIB. BENT. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON LT WING FLAP, TWO RIBS INSIDE LOWER INBD ACCESS PLATE WERE BENT. INSTALLED REPAIR DOUBLER PER ARA 15361. ACFT TT: - [SDR TWAA9810712](https://openairdocs.org/sdr/TWAA9810712), Jul 1, 1998: FRAME. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOND FORMER FOOT STA 980 CRCKED BELOW LONGEORN 14R AND ABOVE 16R. REPLACED FORMER PER MO 72J14. ACFT TT: 77,210 HOURS. ACF - [SDR TWAA9810613](https://openairdocs.org/sdr/TWAA9810613), Jun 25, 1998: CASTING. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING, THE CENTER AND INBD FWD FLAP HINGE CASTING HAD BADLY PITTED MOUNT HOLES. INSTALLED NEW FLAP HINGE CASTING - [SDR TWAA9810804](https://openairdocs.org/sdr/TWAA9810804), Jun 24, 1998: SPLICE. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON RT WING A CRACK IN WING L.E. ON SPLICE DOUBLER. LOCATED OTBD END OF NR 1 SLAT. INSTALLED SPLICE PER SRM 51-01, PG - [SDR TWAA9810611](https://openairdocs.org/sdr/TWAA9810611), Jun 22, 1998: SKIN. CRACKED. MCI - DURING OP16 MAINTENANCE CHECK, EDDY CURRENT INDICATED .125 INCH LONG CRACK RUNNING AFT FROM UNDER RIVET RBL 13 IN, STATION 699, TOP FUSELAGE SKIN. ACCOMP - [SDR TWAA9810612](https://openairdocs.org/sdr/TWAA9810612), Jun 19, 1998: LONGERON. CRACKED. MCI - DURING OP16 MAINTENANCE CHECK, FOUND FWD ENTRY DOOR AREA LONGERON CRACKED AT STATION 200, L2L. REMOVED CRACKED LONGERON. INSTALLED NEW LONGERON PER SRM 51 - [SDR TWAA9810806](https://openairdocs.org/sdr/TWAA9810806), Jun 18, 1998: DOUBLER. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND DOUBLER AT RBL 58, FLOOR LINE, CORRODED AT STA 929 TO STA 945. REMOVED CORROSION PER 51-10-03, PARA 30 TO PARA 42. R - [SDR TWAA9810609](https://openairdocs.org/sdr/TWAA9810609), Jun 18, 1998: SKIN. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT SEVENTH FASTENER ABOVE LAP SEAM, LONGERON 14, AT FS 1076 ABOVE RT ENGINE PYLON. CRACK IN BEYOND STOP DRILL, - [SDR TWAA9810608](https://openairdocs.org/sdr/TWAA9810608), Jun 18, 1998: ANGLE. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND SUPPORT ANGLE TO FRONT SPAR CRACKED AT BULKHEAD STATION 604, BETWEEN LONGERON 23R AND 24R. REPLACED CRACKED SUPPORT All 67: https://openairdocs.org/deregistered/N995Z-2013-03-21/reports.md ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19871130074959I](https://openairdocs.org/incident/19871130074959I), Nov 30, 1987: Doug DC932 (N995Z), St Louis, MO. Number 1 engine oil quantity dropped to zero in climb. Indicated 13 quarts on approach. Oil quantity system faulty. - [Incident 19780817037929I](https://openairdocs.org/incident/19780817037929I), Aug 17, 1978: Doug DC9 (N995Z), Moline, IL. Engine shutdown due to loss of oil pressure. Found broken line. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.