# N53SW: Johnson Gary GLASAIR FT SPR II-S

- Status: Valid registration
- Airframe: Johnson Gary GLASAIR FT SPR II-S (registry code 05616MI)
- Serial number: 2382
- Type: Fixed wing single engine
- Certificate issued: December 17, 2003
- Expires: February 28, 2029
- Mode S code: A6AFB9
- Registered owner: Johnson Gary F
- Location: Humboldt, TN
- Owner's area on the map: 35.8270° N, 88.9284° W: Placed by OpenAirDocs at the center of ZIP code 38343, within about 7 miles (OpenAirDocs)
- Page: https://openairdocs.org/aircraft/N53SW

ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs matched by airframe (Johnson Gary GLASAIR FT SPR II-S) (OpenAirDocs)

None matched.

## Earlier aircraft with N53SW

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N53SW before.

- [Cancelled 1999-04-02](https://openairdocs.org/deregistered/N53SW-1999-04-02): Boeing 737-2H4, S/N 21534. Exported to Philippines. Owner: Aar Aircraft & Engine Group Inc, Wood Dale, IL

## Service difficulty reports (34)

- [SDR SWAA982136](https://openairdocs.org/sdr/SWAA982136), Sep 17, 1998: INTERCOSTAL. DURING SCHEDULED C4 CHECK, FOUND INTERCOSTAL CRACKED AT DOOR UPLATCH BRACKET.  REMOVED AND REPLACED PER BOEING SRM.
- [SDR SWAA980403](https://openairdocs.org/sdr/SWAA980403), Mar 26, 1998: SENSOR. DURING FLIGHT, LEFT WING BODY OVERHEAT ILLUMINATED AT APPROXIMATELY 8,000 FT.  LIGHT EXTINGUISHED SHORTLY AFTER CLOSING ISOLATION AND NR 1 ENG BLEED VALVES.  RE
- [SDR SWAA971045](https://openairdocs.org/sdr/SWAA971045), Dec 12, 1997: SKIN. DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN AND DOOR BEAR STRAP, FWD LOWER HINGE CUTOUT,  AT AFT SERVICE DOOR. REPAIRED PER DALFORT AVIATION XEA  X2-53-
- [SDR SWAA971044](https://openairdocs.org/sdr/SWAA971044), Dec 12, 1997: SKIN. DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN AND DOOR BEAR STRAP, FWD LOWER HINGE CUTOUT, AT AFT ENTRY DOOR.  REPAIRED PER DALFORT AVIATION XEA  X2-53-19
- [SDR SWAA971043](https://openairdocs.org/sdr/SWAA971043), Dec 12, 1997: SKIN. DURING SCHEDULED SPECIAL VISIT, FOUND NUMEROUS FASTENER HOLES CRACKED AT THE FOLLOWING LOCATIONS: BS 907-937, S10L.  REPAIRED PER DALFORT AVIATION XEA  X2-53-18
- [SDR SWAA971042](https://openairdocs.org/sdr/SWAA971042), Dec 12, 1997: SKIN. DURING SCHEDULED SPECIAL VISIT, FOUND NUMEROUS FASTENER HOLES CRACKED AT THE FOLLOWING LOCATIONS: BS 907-947, S4R BS 907-937, 14L, BS 907-903, S10R BS 1006-1016
- [SDR SWAA970672](https://openairdocs.org/sdr/SWAA970672), Aug 6, 1997: SKIN. DURING C4 CHECK, FOUND AFT FUSELAGE SKIN CRACKED AT BS 948, AT S24R.  REPAIRED PER BOEING SRM.
- [SDR SWAA970930](https://openairdocs.org/sdr/SWAA970930), Mar 15, 1997: BATTERY. DURING SCHEDULED A1 CHECK, FOUND LT OVERWING  EMERGENCY EXIT LIGHTS INOP.  REPLACED BOTH BATTERY PACKS PER BOEING M/M.
- [SDR SWAA970243](https://openairdocs.org/sdr/SWAA970243), Feb 25, 1997: LIGHT. DURING SCHEDULED C2 CHECK, FOUND SECTION OF FLOOR LIGHTING INOP.  RELAMPED AND OP CHECKED PER BOEING M/M.
- [SDR SWAA961335](https://openairdocs.org/sdr/SWAA961335), Dec 9, 1996: SKIN. DURING SCHEDULED C1 CHECK, FOUND NOSE WHEEL WELL SKIN CRACKED, 4 INCHES BEHIND GEAR MANUAL EXTENSION RETURN SPRING BRACKET.  REPAIRED PER BOEING SRM.

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.