# N929L: 1968 Douglas DC-9-32, registration cancelled 2013-08-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 22, 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: 47174
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 1, 1968
- Last registry action: December 15, 2004
- Mode S code: ACE093
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Individual
- Owner's area on the map: 25.8166° N, 80.3105° W: Placed by OpenAirDocs at the center of ZIP code 33166, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N929L
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=929L
- Page: https://openairdocs.org/deregistered/N929L-2013-08-22

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 TWAA0016004](https://openairdocs.org/sdr/TWAA0016004), Oct 11, 2000: SKIN. CORRODED. DURING CHECK-C MAINT, FOUND SKIN BULGING AND SIGNS OF CORROSION FROM LONGERON 26R TO 26L, STA 996. REPAIRED SKIN PER SRM 53-03, FIG 9.
- [SDR TWAA0015712](https://openairdocs.org/sdr/TWAA0015712), Oct 3, 2000: BULKHEAD. CRACKED. DURING CHECK-C MAINT AN EDDY CURRENT CHECK OF THE BULKHEAD T-CAP SHOWED A CRACK APPROXIMATELY 1 INCH LONG IN RADIUS AT LONGERON 28L. INSTALLED NEW T-CAP PER SRM
- [SDR TWAA0015711](https://openairdocs.org/sdr/TWAA0015711), Oct 3, 2000: BULKHEAD. CORRODED. DURING CHECK-C MAINT, THE AFT PRESSURE BULKHEAD SKIN WAS CORRODED ALONG THE BOTTOM EDGE AT ''T'' CAP, STA 996 FROM LONGERON 27L TO 28R, 23 INCHES LONG BY 2.25 I
- [SDR TWAA0012107](https://openairdocs.org/sdr/TWAA0012107), Jul 31, 2000: LONGERON. CRACKED. FOUND A .5 INCH CRACK ON THE I/B FLANGE OF LONGERON 2R, STA 680. SPLICED LONGERON PER SRM 53-02, FIG 18. CHECK-C 7-20-99 STL.
- [SDR TWAA0012106](https://openairdocs.org/sdr/TWAA0012106), Jul 31, 2000: LONGERON. CRACKED. FOUND A .5 INCH CRACK IN I/B AND O/B FLANGE OF LONGERON 2R AT STA 756. SPLICED NEW LONGERON SECTION PER SRM 53-02, FIG 18. CHECK-C 7-20-99 STL.
- [SDR TWAA9914603](https://openairdocs.org/sdr/TWAA9914603), Oct 27, 1999: FUEL PUMP. FAILED. ABORTED TAKEOFF ROLL, DUE TO RT ENG COMPRESSOR STALL. FOUND RT ENG FUEL PUMP OUT PUT SHAFT SHEARED. REPLACED FUEL PUMP ASSY. CC00 7-20-99 STL.
- [SDR TWAA9809303](https://openairdocs.org/sdr/TWAA9809303), Apr 30, 1998: FITTING. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT PYLON WITH CORROSION ON FRONT SPAR LOWER BEAVER TAIL FITTING. REMOVED CORROSION ON BEAVER TAIL FITTING PER SRM 54
- [SDR TWAA9806512](https://openairdocs.org/sdr/TWAA9806512), Apr 22, 1998: SPAR. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT LT BARREL NUT HOLE IN FRONT SPAR CRACKED BEYOND LIMITS. REPLACED FRONT SPAR PER SRM 
- [SDR TWAA9806511](https://openairdocs.org/sdr/TWAA9806511), Apr 22, 1998: SPAR CAP. RUSTY. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT LT BARREL NUT IN FRONT SPAR FOR STABILIZER ATTACHMENT TO CENTER SECTION WAS VERY RUS
- [SDR TWAA9806510](https://openairdocs.org/sdr/TWAA9806510), Apr 22, 1998: RIB. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING LE WITH CRACK AT AFT FASTENER IN WING LE RIB ABOVE LE LOWER PANEL 1113. REMOVED AND REPLACED WITH NEW RIB AN
- [SDR TWAA9806509](https://openairdocs.org/sdr/TWAA9806509), Apr 22, 1998: RIB. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING LE WITH CRACK AT AFT LOWER FASTENER IN WING LE RIB ABOVE LOWER PANEL NR 1112. INSTALLED NEW RIB PER SRM 51-0
- [SDR TWAA9806508](https://openairdocs.org/sdr/TWAA9806508), Apr 22, 1998: RIB. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING LE WITH CRACK AT AFT LOWER FASTENER IN WING LE RIB ABOVE LE LOWER PANEL NR 1111. INSTALLED NEW RIB PER SRM 5
- [SDR TWAA9806616](https://openairdocs.org/sdr/TWAA9806616), Apr 16, 1998: PANEL. TORN. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND TOP TE PANEL ON RUDDER SEPARATED AND TORN AT JOINT SEAMS. REPAIRED PER SRM 51-90-0. (M)
- [SDR TWAA9806601](https://openairdocs.org/sdr/TWAA9806601), Apr 16, 1998: SKIN. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE WITH CRACK AT LOWER AFT FASTENER IN LE ABOVE LE PANEL NR 1211A. INSTALLED NEW RIB PER SRM 51-01 PAGE 1. (
- [SDR TWAA9806515](https://openairdocs.org/sdr/TWAA9806515), Apr 16, 1998: RIB. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT TOP AFT FASTENER IN RT WING LE RIB ABOVE LE PANEL 1213A. REPLACED RIB PER SRM 51-01, PG 1 ITEM C. ACFT TT: 
- [SDR TWAA9806514](https://openairdocs.org/sdr/TWAA9806514), Apr 16, 1998: FLOORBEAM. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT STA 937 TO STA 965, CABIN FLOORBEAM CAP WITH METAL REMOVED BEYOND LIMITS FOR CORROSION REMOVAL. INSTALLED NEW SEC
- [SDR TWAA9806413](https://openairdocs.org/sdr/TWAA9806413), Apr 16, 1998: RIB. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT TOP AFT FASTENER IN RT WING LE RIB ABOVE LE PANEL 1213A. REPLACED PART PER SRM 51-01, PG 1 ITEM C. ACFT TT:
- [SDR TWAA9806412](https://openairdocs.org/sdr/TWAA9806412), Apr 16, 1998: BARREL NUT. RUSTED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT RT BARREL NUT IN FRONT SPAR FOR STABILIZER ATTACH TO CENTER SECTION WAS RUSTY AND EM
- [SDR TWAA9806410](https://openairdocs.org/sdr/TWAA9806410), Apr 16, 1998: SUPPORT. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND METAL REMOVED BEYOND LIMIT FOR CORROSION REMOVAL AT CABIN STA 937 TO STA 965, CENTER FLOOR CAP. INSTALLED NEW SECTIO
- [SDR TWAA9806409](https://openairdocs.org/sdr/TWAA9806409), Apr 16, 1998: RIB. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE HAD CRACK AT LOWER AFT FASTENER IN LE RIB ABOVE LE PANEL NR 1211A. INSTALLED NEW RIB PER SRM 51-01, PAGE 
- [SDR TWAA9809304](https://openairdocs.org/sdr/TWAA9809304), Apr 14, 1998: BULKHEAD. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND 1104 CANTED BULKHEAD AT NR 3 LONGERON RT AND LT SIDE, WITH 2 EACH FASTENERS MISSING. HFEC AREA FOUND 2 INCH CRACK. R
- [SDR TWAA9809301](https://openairdocs.org/sdr/TWAA9809301), Apr 14, 1998: BULKHEAD ANGLE. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT PYLON UPPER AFT BULKHEAD ANGLE CRACKED AT INBOARD AND OUTBOARD ENDS. MADE AND INSTALLED NEW ANGLE PER SRM 51-01, 
- [SDR TWAA9807320](https://openairdocs.org/sdr/TWAA9807320), Apr 14, 1998: FITTING. FLAT SPOT. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZ STABILIZER LEFT PIVOT BEARING LUG, IN LT SIDE OF STAB CENTER SECTION RIB, WITH FLAT SPOT IN BEARING BORE AT AP
- [SDR TWAA9807319](https://openairdocs.org/sdr/TWAA9807319), Apr 13, 1998: BULKHEAD CASTING. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CABIN FOOT CASTING AFT INBOARD SIDE OF 965 BULKHEAD, CRACKED. REMOVED AND REPLACED CASTING PER SRM 51-01 AND STANDAR
- [SDR TWAA9807312](https://openairdocs.org/sdr/TWAA9807312), Apr 13, 1998: BLOCK. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING TE FLAP INSIDE FLAP OUTBOARD FLAP HINGE TO FORWARD MOUNT BOLT, RT AND LT SIDE MOUNT WEBS CRACKED OUT FROM BO
- [SDR TWAA9807306](https://openairdocs.org/sdr/TWAA9807306), Apr 7, 1998: HORIZ STAB. GOUGED. MCI - DURING OP16 MAINTENANCE CHECK, FOUND ON LT HORIZ STAB TOP AFT 2 BARREL NUT HOLES GOUGED. REAMED HOLES AND INSTALLED BUSHING AND REDRILLED .562 IN PER ARA 
- [SDR TWAA9809305](https://openairdocs.org/sdr/TWAA9809305), Apr 3, 1998: FITTING. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON NR 1 PYLON FRONT SPAR LOWER BEAVER TAIL FITTING. REMOVED CORROSION ON BEAVER TAIL FITTING PER SRM 54-04
- [SDR TWAA9809307](https://openairdocs.org/sdr/TWAA9809307), Mar 31, 1998: SKIN. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CLASS III REPAIR INSTALLED ABOVE AND JUST FORWARD OF EXTERNAL POWER RECEPTACLE. INSTALLED CLASS I REPAIR PER SRM 53-
- [SDR TWAA9809302](https://openairdocs.org/sdr/TWAA9809302), Mar 30, 1998: SKIN. DENTED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND DENT IN FUSELAGE SKIN RT SIDE AFT OF AFT CARGO DOOR. FOUND INTERIM REPAIR INSTALLED. INSTALLED CLASS 1 REPAIR PER SR
- [SDR TWAA9809309](https://openairdocs.org/sdr/TWAA9809309), Mar 27, 1998: SPAR. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING HOLE 43 INDICATING CRACK WITH HFEC, RT WING LOWER REAR SPAR STA XRS 154. REPAIRED PER SERVICE REWORK DRAWI
- [SDR TWAA9809308](https://openairdocs.org/sdr/TWAA9809308), Mar 27, 1998: SPAR. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING HOLE 71 INDICATING CRACKED, LOWER REAR SPAR RT XRS 200. REPAIRED PER SERVICE REWORK DRAWING J060173 AND TW
- [SDR TWAA9809306](https://openairdocs.org/sdr/TWAA9809306), Mar 27, 1998: FRAME. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND NR 1 PYLON LOWER END CHORD ANGLE CRACKED, 60 INCHES AFT OF LEADING EDGE, 4 INCHES INBOARD AT OUTBOARD END. INSTALLED
- [SDR TWAA9807315](https://openairdocs.org/sdr/TWAA9807315), Mar 27, 1998: FLOORBEAM. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION BEYOND LIMIT ON FLOORBEAM CAP FROM STATION 196 TO 218 OBL. FABRICATED AND INSTALLED NEW BEAM CAP PER SRM 5
- [SDR TWAA9807311](https://openairdocs.org/sdr/TWAA9807311), Mar 27, 1998: PIVOT ARM. WORN. MCI - DURING OP16 MAINTENANCE CHECK, FOUND LT TE FLAP CENTER HINGE PIVOT BEARING OUTBOARD LUG WORN AND CORRODED INBEARING BORE. INBOARD BEARING BORE WORN OVERSI
- [SDR TWAA9807310](https://openairdocs.org/sdr/TWAA9807310), Mar 27, 1998: PIVOT ARM. WORN. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING FLAP CENTER HINGE PIVOT BEARING INBOARD AND OUTBOARD LUGS WITH WORN GROOVES AND PITTING CONDITION IN BEARING
- [SDR TWAA9807305](https://openairdocs.org/sdr/TWAA9807305), Mar 27, 1998: SPAR. CRACKED. MCI - DURING OP16 MAINTENANCE CHECK, FOUND HOLE 104 INDICATING CRACK RT WING LOWER SPAR STATION XRS 268. REPAIRED PER SERVICE REWORK DRAWING J060173 AND TWA STD
- [SDR TWAA9806502](https://openairdocs.org/sdr/TWAA9806502), Mar 25, 1998: SEAT TRACK. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK FOUND CORROSION BEYOND LIMITS IN CHAIR TRACK AT STA 570 TO STA 617, LBL 45 IN. REMOVED AND REPLACED SEAT TRACK AT STA 570 T
- [SDR TWAA9809310](https://openairdocs.org/sdr/TWAA9809310), Mar 23, 1998: FRAME. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FUSELAGE FRAME STA 89 WITH CRACK IN OUTBOARD RADIUS BETWEEN LONGERONS 18 AND 19. STOP DRILLED CRACK PER SRM 51-10 AN
- [SDR TWAA9807318](https://openairdocs.org/sdr/TWAA9807318), Mar 23, 1998: SPAR CAP. CRACKED. MCI - DURING OP 16 MAINTENANCE CEHCK, FOUND RT WING TE UPPER REAR SPAR CAP CRACKED AT INBOARD FLAP HINGE UPPER ATTACH HOLES. STOP DRILLED CRACK, REPAIRED PER DA
- [SDR TWAA9807317](https://openairdocs.org/sdr/TWAA9807317), Mar 23, 1998: LONGERON. BROKEN. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 4L BROKEN JUST FORWARD OF FORMER 160. REPAIRED PER SRM 53-02, FIG 18 PAGE 48. (M)
- [SDR TWAA9807316](https://openairdocs.org/sdr/TWAA9807316), Mar 23, 1998: LONGERON. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 4L CRACKED AT STATION 200. REPAIRED PER SRM 53-02, FIG 18 PAGE 48. (M)
- [SDR TWAA9807309](https://openairdocs.org/sdr/TWAA9807309), Mar 23, 1998: FLOORBEAM. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND SURFACE CORROSION ON FLOORBEAM CAP AT FS 160 FROM OL-288. REPLACED FLOORBEAM CAP PER SRM 51-01, PAGE 1 ITEM 1C. SEAL
- [SDR TWAA9809108](https://openairdocs.org/sdr/TWAA9809108), Mar 17, 1998: FLOORBEAM. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FLOORBEAM CAP AT FS 160 TO 196, RBL 44, CORRODED BEYOND LIMITS. INSTALLED NEW FLOORBEAM PER SRM 51-01, PAGE 1 ITEM C
- [SDR TWAA9809106](https://openairdocs.org/sdr/TWAA9809106), Mar 17, 1998: ANGLE. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK IN FORWARD FUSELAGE INTERCOSTAL TO FS 69.55 FORMER ATTACH 'T' ANGLE AT LBL 13 INCH. REPLACED 'T' ANGLE PER SRM
- [SDR TWAA9809104](https://openairdocs.org/sdr/TWAA9809104), Mar 17, 1998: SKIN. DENTED. MCI - DURING OP 16 MAINTENANCE CHECK,F OUND DENT ON LEFT SIDE BELOW AFT CORNER OF EXTERNAL POWER RECEPTACLE, 1 INCH BY 1 INCH BY .045 INCH DEEP. INSTALLED DOUBL
- [SDR TWAA9809103](https://openairdocs.org/sdr/TWAA9809103), Mar 17, 1998: SKIN. DENTED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND DENT IN LEFT SIDE BELOW FORWARD CORNER OF EXTERNAL POWER RECEPTACLE, 1 INCH BY 1.25 INCH BY .055. INSTALLED DOUBLER 
- [SDR TWAA9807314](https://openairdocs.org/sdr/TWAA9807314), Mar 12, 1998: FLOORBEAM. WORN. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CABIN FLOORBEAM WITH WEAR AREA AT STATION 237, LBL 4 INCHES. REPAIRED FLOORBEAM PER SRM 53-05 FIG 30. (M)
- [SDR TWAA9807313](https://openairdocs.org/sdr/TWAA9807313), Mar 12, 1998: ANGLE. CRACKED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND BELOW RT AFT LAVATORY FLOOR, ANGLE AT STATION 996 BELOW LONGERON 18R, AT CUST LINE, CRACKED. REPLACED ANGLE PER SRM 
- [SDR TWAA9807308](https://openairdocs.org/sdr/TWAA9807308), Mar 7, 1998: SKIN. DAMAGED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND UNFILLED HOLES IN FUSELAGE SKIN AT STATION 965, BELOW LONGERON 14R. REPAIRED PER ARA 15017A. (M)
- [SDR TWAA9807307](https://openairdocs.org/sdr/TWAA9807307), Mar 7, 1998: SPAR. CRACKED. MCI - DURING OP16 MAINTENANCE CHECK, FOUND HOLE 44 INDICATING CRACK IN RT WING LOWER REAR SPAR STATION XSR 155. REWORKED PER SERVICE REWORK DRAWING JO60173 AND 

All 59: https://openairdocs.org/deregistered/N929L-2013-08-22/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 19940919042779I](https://openairdocs.org/incident/19940919042779I), Sep 19, 1994: Doug DC932 (N929L), Little Rock, AR. Tail compartment warning light. Returned to Little Rock. Two air ducts separated at octopus cluster.
- [Incident 19880320024059I](https://openairdocs.org/incident/19880320024059I), Mar 20, 1988: Doug DC932 (N929L), St Louis, MO. Fuel venting from wing on takeoff. Returned to stl. Replaced wing climb vent float valve. Resealed wing surge box.
- [Incident 19870519019629I](https://openairdocs.org/incident/19870519019629I), May 19, 1987: Doug DC932 (N929L), St Louis, MO. Right engine oil pressure fell on takeoff. Reduced power and returned. Adjusted relief valve.

## Other aircraft with N929L

- [Cancelled 2025-05-23](https://openairdocs.org/deregistered/N929L-2025-05-23): Diamond Aircraft Ind DA 40 NG, S/N 40.NC334, built 2024. Exported to France. Owner: [Diamond Aircraft Sales U S A Inc](https://openairdocs.org/faa-owner/DIAMOND%20AIRCRAFT%20SALES%20U%20S%20A%20INC), London Ontario

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