# N998R: 1967 Douglas DC-9-32, registration cancelled 2011-03-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 15, 2011
- Status when cancelled: First renewal notice
- 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: 47030
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: September 30, 1967
- Certificate issued: April 14, 1987
- Last registry action: November 18, 2008
- Mode S code: ADF1D2
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N998R
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=998R
- Page: https://openairdocs.org/deregistered/N998R-2011-03-15

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 (59, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR TWAA0105501](https://openairdocs.org/sdr/TWAA0105501), Mar 26, 2001: BATTERY. DISCHARGED. THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY. CHECK-C 2-4-01 STL.
- [SDR TWAA0101703](https://openairdocs.org/sdr/TWAA0101703), Jan 26, 2001: LONGERON. CRACKED. DURING CHECK-C MAINT LONGERON 6L AT STA 718 WAS FOUND CRACKED AT LOWER FLANGE, .25 INCH CRACK. REMOVED AND REPLACED SECTION OF LONGERON 6L AT STA 699 TO 718 PER
- [SDR TWAA0101507](https://openairdocs.org/sdr/TWAA0101507), Jan 25, 2001: LONGERON. CRACKED. DURING CHECK-C MAINT LONGERON 3R AT STA 658 WAS CRACKED AT LOWER FLANGE .25 INCH LONG. REPAIRED PER SRM 53-02 AND DRAWING SRO 9530128.
- [SDR TWAA0016501](https://openairdocs.org/sdr/TWAA0016501), Oct 22, 2000: SKIN. DAMAGED. THE FUSELAGE SKIN WAS DAMAGED BY GROUND EQUIPMENT AFT OF THE FWD CARGO DOOR, LOWER LT CORNER AT STA 427. REPAIRED PER DOUGLAS DRAWING SRO9530117-7011 AND ARA 16
- [SDR TWAA0014201](https://openairdocs.org/sdr/TWAA0014201), Sep 12, 2000: POWER SUPPLY. INOPERATIVE. THE EGRESS LIGHTS WERE INOPERATIVE FROM ROW 16 TO 21. REPLACED THE POWER SUPPLY. CHECK-C 10-27-99 STL.
- [SDR TWAA0101702](https://openairdocs.org/sdr/TWAA0101702), Jan 27, 2000: LONGERON. CRACKED. DURING CHECK-C MAINT LONGERON 4L WAS FOUND CRACKED IN 2 PLACES AT BELT RING, STA 1087. REMOVED AND REPLACED LONGERON PER SRM 53-02, FIG 18.
- [SDR TWAA9914606](https://openairdocs.org/sdr/TWAA9914606), Oct 29, 1999: CONNECTOR. FAILED. DURING APPROACH, THE LEFT MAIN LANDING GEAR DOWN LOCK LIGHT FLICKERED. REPLACED SWITCH CONNECTOR MFG PN DS07-75295 AND SOCKET MFG PN 800-20-30-1. CC00 10-14-99,
- [SDR TWAA9914803](https://openairdocs.org/sdr/TWAA9914803), Oct 23, 1999: SKIN. CORRODED. DURING CHECK-C MAINT, FOUND SKIN PILLOWED/DENTED AND RIVETS POSSIBLY DISTRESSED ON LT FUSELAGE, NEAR THE PRESSURE DOME, FORWARD AND BELOW THE TR SELECTOR ACCESS
- [SDR TWAA9914802](https://openairdocs.org/sdr/TWAA9914802), Oct 23, 1999: FITTING. CORRODED. DURING CHECK-C MAINT, FOUND AT STA 996 THE END CAP FITTINGS AT LONGERON 23L, 24L, AND 25L WERE FOUND WITH CORROSION. REMOVED AND REPLACED THE FITTINGS PER SRM 5
- [SDR TWAA9914506](https://openairdocs.org/sdr/TWAA9914506), Oct 21, 1999: LONGERON. CRACKED. DURING CHECK-C, MAINT FOUND A 1 INCH CRACK AT STA 1076, LONGERON 2R. SPLICED SECTION PER SRM 53-02, FIG 18.
- [SDR TWAA9914505](https://openairdocs.org/sdr/TWAA9914505), Oct 21, 1999: LONGERON. CRACKED. DURING CHECK-C, MAINT FOUND LONGERON 2L AT STA 1076 HAD A 1 INCH CRACK. SPLICED SECTION PER SRM 53-02, PAGE 18.
- [SDR TWAA9908201](https://openairdocs.org/sdr/TWAA9908201), May 29, 1999: SKIN. SCRATCHED. FOUND THE RT WING T/E FLAP AFT OF MOVAEBLE VANE HAD 2 SCRATCHES .020 TO .050 IN DEEP. REMOVED DAMAGED AREA AND REPAIRED PER SRM 57-01, FIG 5, AND ENGR CONCURREN
- [SDR TWAA9907302](https://openairdocs.org/sdr/TWAA9907302), May 12, 1999: BRACKET. CRACKED. THE CAPTAINS RUDDER PEDAL BRACKET WAS CRACKED AT THE AFT O/B MOUNT LEG, 1.125 INCH LONG. REMOVED AND REPLACED THE RUDDER BRACKET PER MM 27-20-12. CHECK-C 8-7-98
- [SDR TWAA9812511](https://openairdocs.org/sdr/TWAA9812511), Aug 3, 1998: SKIN. DAMAGED. DURING OP 16 MAINT CHECK, FOUND EXTERNAL DOUBLER INSTALLED AT FS 495 TO 505, LONG 19 TO 20R. REPAIRED PER DC9 SRM 53-04, FIG 12B SHEET 6.
- [SDR TWAA9812510](https://openairdocs.org/sdr/TWAA9812510), Aug 3, 1998: SKIN. DAMAGED. DURING OP 16 MAINT CHECK, FOUND EXTERNAL DOUBLER INSTALLED AT FS 800, LONG 16R. INSTALLED CLASS I REPAIR DOUBLER PER SRM 53-04, FIG 12B.
- [SDR TWAA9812509](https://openairdocs.org/sdr/TWAA9812509), Aug 3, 1998: SKIN. DENTED. DURING OP 16 MAINT CHECK, FOUND DENT IN FUSELAGE AT FS 871, BETWEEN LONG 29 AND 30 RT, 4 IN BY 6 IN BY .125 IN. REPAIRED PER SRM 53-04, FIG 12B, PAGE 25.
- [SDR TWAA9812508](https://openairdocs.org/sdr/TWAA9812508), Aug 3, 1998: LONGERON. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION ON TOP OF LONG 30 AT FS 950. REPLACED LONGERON FROM FS 931 TO 955, PER 51-01, PAGE 4. SEALED PER SRM 51-20-0.
- [SDR TWAA9812505](https://openairdocs.org/sdr/TWAA9812505), Aug 3, 1998: DOUBLER. CRACKED. DURING OP 16 MAINT CHECK, FOUND EXTERNAL DOUBLER INSTALLED AT FS 996, LONGERON 28 AND 29R. REPAIRED CRACK AS REQUIRED PER SRM 53-04, FIG 12B, AND ARA 15299.
- [SDR TWAA9812512](https://openairdocs.org/sdr/TWAA9812512), Jul 28, 1998: INTERCOSTAL. CRACKED. DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL CRACKED 3 INCHES FWD OF STA 294, AT ZERO BL. FABRICATED NEW INTERCOSTAL FROM 2024-0 ALUM MATERIAL HEAT TREATED TO 20
- [SDR TWAA9812206](https://openairdocs.org/sdr/TWAA9812206), Jul 22, 1998: LONGERON. CRACKED. DURING OP 16 MAINT CHECK, FOUND LONGERON 17L CRACKED AT STA 965, AFT SIDE OF BULKHEAD. REPLACED CRACKED LONGERON SECTION AND SPLICED PER SRM 53-02, FIG 18.
- [SDR TWAA9812203](https://openairdocs.org/sdr/TWAA9812203), Jul 22, 1998: LONGERON. CRACKED. DURING OP 16 MAINT CHECK, FOUND LONGERON 16L CRACKED AT STA 965, AFT SIDE OF BULKHEAD. REPLACED CRACKED LONGERON SECTION AND SPLICED PER SRM 53-02, FIG 18.
- [SDR TWAA9812126](https://openairdocs.org/sdr/TWAA9812126), Jul 20, 1998: SKIN. DENTED. DURING OP 16 MAINT CHECK, FOUND DENT ON NR 1 L/E SLAT, LT WING, EXCEEDING ALLOWABLE LIMITS PER SRM 57-03, PG 20A. DENT IS 2.5 BY 17 IN BY .150 DEEP. CUT OUT DAM
- [SDR TWAA9812009](https://openairdocs.org/sdr/TWAA9812009), Jul 17, 1998: SKIN. WORN. DURING OP 16 MAINT CHECK, FOUND FUSELAGE SKIN WORN AT LONGERON 26L, STA 815, UNDER FUSELAGE FAIRING. TRIMMED DAMAGED AREA WHICH IS FOR A LAP SEAM. INSTALLED REP
- [SDR TWAA9812008](https://openairdocs.org/sdr/TWAA9812008), Jul 17, 1998: INTERCOSTAL. CRACKED. DURING OP 16 MAINT CHECK, FOUND INTERCOASTAL CRACKED AT AFT END OF PULLEY CLUSTER AT STA 1010, RBL 20 INCHES. NEW SUPPORT FABRICATED IN SHOP PER DRAWING 9915540
- [SDR TWAA9812007](https://openairdocs.org/sdr/TWAA9812007), Jul 17, 1998: FRAME. CRACKED. DURING OP 16 MAINT CHECK, FOUND FRAME WITH APPROX 1 IN CRACK AT STA 980, LONGERON 17R. ACCOMPLISHED FRAME REPAIR BY CUTTING DAMAGED SECTION OUT BETWEEN L14R AND
- [SDR TWAA9812006](https://openairdocs.org/sdr/TWAA9812006), Jul 17, 1998: SKIN. DAMAGED. DURING OP 16 MAINT CHECK, FOUND LT HORIZ STAB, LEADING EDGE OF STAB DAMAGED AND FILLET DETERIORATED APPROX 20 IN FROM O/B END. INSTALLED DOUBLER PER SRM 55-03, 
- [SDR TWAA9811506](https://openairdocs.org/sdr/TWAA9811506), Jul 16, 1998: BULKHEAD. CRACKED. DURING OP 16 MAINTENANCE CHECK AT STA 965, THE BULKHEAD WEB HAD 2 EACH CRACKS APPROX 2 INCHES LONG AT WL 200, JUST INBD OF LONGERON 18R. REPLACED FULL BULKHEAD 
- [SDR TWAA9811504](https://openairdocs.org/sdr/TWAA9811504), Jul 15, 1998: SKIN. DEFECTIVE. DURING OP 16 MAINTENANCE CHECK, FOUND FUSELAGE UPPER AND LOWER SKIN THICKNESS MEASURED BY NDT WAS .024 INCH. SKIN THICKNESS IS .063 INCH AT STA 815, L26R. REPAI
- [SDR TWAA9811505](https://openairdocs.org/sdr/TWAA9811505), Jul 13, 1998: LONGERON. CRACKED. DUIRNG OP 16 MAINTENANCE CHECK, FOUND LONGERON 17R AT STA 980 WITH .50 INCH CRACK AT ATTACH HOLE TO FORMER. REPLACED SECTION OF LONGERON FROM STA 956 TO STA 996
- [SDR TWAA9811503](https://openairdocs.org/sdr/TWAA9811503), Jul 9, 1998: ANGLE. CORRODED. DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR ANGLE WITH EXFOLIATION AT FS 914, S29R. REMOVED EXFOLIATED SECTION OF ANGLE AND REPAIRED AREA PER SRM 53-01, FIG 2 S
- [SDR TWAA9811005](https://openairdocs.org/sdr/TWAA9811005), Jul 7, 1998: SKIN. DAMAGED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE WING SKIN WITH HOLE WORN THROUGH SKIN INBD OF NR 1 SLAT TRACK, L.E. OF WING TO END OF WING TO NR 3 SLAT T
- [SDR TWAA9810805](https://openairdocs.org/sdr/TWAA9810805), Jul 2, 1998: WEB. CRACKED. MCI- DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR MEMBRANE CRACKED AT FS 744, RBL 50. REPLACED MEMBRANE WITH NEW PART PER SRM 51-01 PAGE 04. ACFT TT: 77,783 HOUR
- [SDR TWAA9810711](https://openairdocs.org/sdr/TWAA9810711), Jul 1, 1998: RIB. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LOWER SURFACE AT DAMPER CUT OUT LOWER RIB CAP CRACKED ON LT ELEVATOR. REPLACED LOWER RIB CAP PER DAC DWG 9918535. AC
- [SDR TWAA9810808](https://openairdocs.org/sdr/TWAA9810808), Jun 29, 1998: SPAR CAP. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON RT WING UPPER REAR SPAR CAP, AN 'EYE BROW' CRACK ABOVE BOTH THE INBD AND OTBD STUD HOLES. CRACK LENGTH WAS 0.75 I
- [SDR TWAA9810714](https://openairdocs.org/sdr/TWAA9810714), Jun 29, 1998: SPLICE. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON LT WING 10 INCHES OTBD OF INBD END OF NR 3 SLAT, LE OF WING SPLICE PLATE, CRACKED. REMOVED CRACKED SPLICE PLATE A
- [SDR TWAA9810713](https://openairdocs.org/sdr/TWAA9810713), Jun 29, 1998: TIE. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACKED STRINGER TIE AT FS 585, AND STR 26R. REMOVED FORMER RING AT STA 579 FROM S25L TO S25R TO GAIN ACCESS TO STRI
- [SDR TWAA9810710](https://openairdocs.org/sdr/TWAA9810710), Jun 29, 1998: SKIN. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ROUND INTERIM REPAIR AT THE RADIO ALT ANTENNA AT FS 510, L30. REMOVED PREVIOUS REPAIR. INSTALLED REPAIR DO
- [SDR TWAA9810709](https://openairdocs.org/sdr/TWAA9810709), Jun 29, 1998: LONGERON. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, A DYE CHECK SHOWED A ONE INCH CRACK IN LOWER FLANGE OF LONGERON 13R, AT FASTENER AT STA 965 FORMER FRAME. REMOVED CRACKED 
- [SDR TWAA9810715](https://openairdocs.org/sdr/TWAA9810715), Jun 25, 1998: SEAT TRACK. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR TRACK NR 3, FS 937 TO FS 946. REMOVED OLD TRACK FROM STA 929 TO STA 965. INSTALLED NEW TRACK PER 
- [SDR TWAA9810615](https://openairdocs.org/sdr/TWAA9810615), Jun 25, 1998: WEB. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND A .50 INCH CRACK IN MEMBRANE AT LONGERON 18L, STA 234. REMOVED MEMBRANE AT L18L, FS 218 TO FS 237 PER DAC SRM 51-61 
- [SDR TWAA9810614](https://openairdocs.org/sdr/TWAA9810614), Jun 25, 1998: LONGERON. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, ON LOWER FUSELAGE, FOUND LONGERON 25L WITH CRACK AT FASTENER AT STA 256 FORMER FRAME. INSTALLED NEW LONGERON SECTION AND T
- [SDR TWAA9810716](https://openairdocs.org/sdr/TWAA9810716), Jun 24, 1998: SUPPORT. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR PANEL SUPPORT HAT SECTION WITH APPROXIMATELY 1.5 INCH CRACK AT STA 237, RBL 2 INCHES. REPAIRED PER SRM 51-01, 
- [SDR TWAA9810610](https://openairdocs.org/sdr/TWAA9810610), Jun 24, 1998: RIB. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND A CRACK IN AFT FASTENER RIB, 18 IN OUTBOARD OF NR 5 SLAT CENTER TRACK RIB IN LE OF LEFT WING. REPLACED RIB PER SRM 5
- [SDR TWAA9810717](https://openairdocs.org/sdr/TWAA9810717), Jun 23, 1998: LONGERON. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND IN CABIN DYE CHECK SHOWING 2 EACH CACKS IN LOWER FLANGE OF LONGERON 16R, AT STA 965 FORMER FRAME. REMOVED CRACKED SE
- [SDR TWAA9810605](https://openairdocs.org/sdr/TWAA9810605), Jun 17, 1998: FLOORBEAM. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND SURFACE CORROSION TOP SIDE OF FLOORBEAM, STATION 996 RBL 22 IN TO RBL 50 INCH. REPLACED ANGLE PER SRM 51-01 AND STD 
- [SDR TWAA9810604](https://openairdocs.org/sdr/TWAA9810604), Jun 17, 1998: BULKHEAD. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND TIE ANGLE FOR FLOORBEAM, FORMER RING AND PRESSURE BULKHEAD CRACKED AT STATION 996, RBL 58.6 INCHES. VERIFIED BY NDT.
- [SDR TWAA9809810](https://openairdocs.org/sdr/TWAA9809810), Jun 16, 1998: FRAME. BENT. MCI - DURING OP 16 MAINTENANCE CHECK FOUND STA 544 FORMER RING FOOT BENT BEYOND LIMITS, BETWEEN LONGERONS 28R AND 29R. REPLACED FORMER FOOT PER SRM 53-03, FIG 3
- [SDR TWAA9809809](https://openairdocs.org/sdr/TWAA9809809), Jun 16, 1998: SEAT TRACK. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION BLENDED BEYOND LIMITS AT STA 200, RBL 22, FLOOR TRACK. REPLACED CORRODED TRACK SECTION PER SRM 51-01, PG 1
- [SDR TWAA9809705](https://openairdocs.org/sdr/TWAA9809705), Jun 12, 1998: TIE. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND STR 30 CORRODED AT TIE CLIP, FS 167. REMOVED CORROSION IN STRINGER PER SRM 51-10-3, PARA 35, PAGE 21. REMOVED STRING
- [SDR TWAA9809704](https://openairdocs.org/sdr/TWAA9809704), Jun 12, 1998: LONGERON. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND 2 EACH CRACKS AT STA 200, LONGERON 4L. REMOVED AND REPLACED 4L LONGERON FROM STA 128 TO STA 229. INSTALLED LONGERON 

All 59: https://openairdocs.org/deregistered/N998R-2011-03-15/reports.md

## FAA accident and incident reports (3)

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 19990716024339I](https://openairdocs.org/incident/19990716024339I), Jul 16, 1999: Doug DC932 (N998R), Austin, TX, Minor damage. Ground crew marshalled aircraft into baggage cart.
- [Incident 19920115001869I](https://openairdocs.org/incident/19920115001869I), Jan 15, 1992: Doug DC932 (N998R), Cedar Rapids, IA. Left gear down unsafe indication. Visually down. Landed safely. Wire off down lock switch and cannon plug.
- [Incident 19790119003179I](https://openairdocs.org/incident/19790119003179I), Jan 19, 1979: Doug DC9 (N998R), Dallas, TX, Minor damage. Engine shut down due to fire warning light. Anti ice pneumatic duct failed due to 13th stage bleed air lear.

## Other aircraft with N998R

- [Registered now](https://openairdocs.org/aircraft/N998R): Bombardier BD-700-2A12, S/N 70019, built 2020
- [Cancelled 2024-08-20](https://openairdocs.org/deregistered/N998R-2024-08-20): Bombardier BD-700-1A10, S/N 9294, built 2008. Exported to Singapore. Owner: [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake)

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