# N29SW: Boeing 737-2H4

- Status: Valid registration
- Airframe: [Boeing 737-2H4](https://openairdocs.org/model/boeing-737-2h4) (registry code 138448C, 124 seats)
- Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (Pratt & Whitney) (OpenAirDocs)
- Serial number: 21340
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 22, 1999
- Certificate issued: April 23, 2018
- Expires: April 30, 2028
- Mode S code: A2F4C6
- Registered owner: [Kansas Aviation Museum](https://openairdocs.org/faa-owner/KANSAS%20AVIATION%20MUSEUM)
- Location: [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- Owner type: Corporation
- Owner's area on the map: 37.6429° N, 97.2101° W: Placed by OpenAirDocs at the center of ZIP code 67210, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=29SW
- Page: https://openairdocs.org/aircraft/N29SW

From the FAA registry file of October 22, 2026. 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. The registry lists only the engine series, so ADs for every Pratt & Whitney JT8D-9 model are included.

## ADs that may apply (OpenAirDocs): 38 in force

### Matched by airframe (Boeing 737-2H4)

None in force.

### Matched by engine (Pratt & Whitney JT8D-9 series)

- [AD 2011-03-01](https://openairdocs.org/ad/2011-03-01): Critical life- limited parts · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 9 more. Effective Mar 4, 2011
- [AD 2010-21-17](https://openairdocs.org/ad/2010-21-17): Fan blade · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-17 and 3 more. Effective Nov 12, 2010
- [AD 2009-24-01](https://openairdocs.org/ad/2009-24-01): Fan blade · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-17 and 5 more. Effective Jan 4, 2010
- [AD 2006-17-07 R1](https://openairdocs.org/ad/2006-17-07-R1): High pressure compressor (HPC) front hubs and HPC disk · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Nov 2, 2006
- [AD 2005-17-16](https://openairdocs.org/ad/2005-17-16): Critical life-limited rotating parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Sep 30, 2005
- [AD 2003-12-07](https://openairdocs.org/ad/2003-12-07): 12th Stage high pressure compressor · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jul 18, 2003
- [AD 2003-05-07](https://openairdocs.org/ad/2003-05-07): Low pressure compressor (LPC) · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Apr 17, 2003
- [AD 2001-15-18](https://openairdocs.org/ad/2001-15-18): Stage Compressor Disks · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Sep 4, 2001
- [AD 2000-22-06](https://openairdocs.org/ad/2000-22-06): Main Fuel Pump · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 8 more. Effective Dec 4, 2000
- [AD 99-01-08](https://openairdocs.org/ad/99-01-08): Stage 7 through Stage 15 High-Pressure Compressor (HPC) Disks · Pratt & Whitney Division JT3D-1, JT3D-1-MC6, JT3D-1-MC7 and 30 more. Effective Jan 5, 1999
- [AD 98-21-24](https://openairdocs.org/ad/98-21-24): Compressor Disks · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Nov 16, 1998
- [AD 98-04-39](https://openairdocs.org/ad/98-04-39): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Feb 25, 1998
- [AD 97-19-12](https://openairdocs.org/ad/97-19-12): Hub Inspection · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 9 more. Effective Nov 18, 1997
- [AD 97-19-14](https://openairdocs.org/ad/97-19-14): Low Pressure Turbine (LPT) Blade Sets · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 9 more. Effective Oct 24, 1997
- [AD 96-23-14](https://openairdocs.org/ad/96-23-14): Combustion Chamber Outer Cases · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jan 2, 1997
- [AD 95-26-03](https://openairdocs.org/ad/95-26-03): High Pressure Compressor Disks · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jan 11, 1996
- [AD 86-09-02 R2](https://openairdocs.org/ad/86-09-02-R2): Combustion Chamber Liners · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Nov 17, 1995
- [AD 95-16-07](https://openairdocs.org/ad/95-16-07): High Pressure Compressor (HPC) Disks · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 11 more. Effective Sep 11, 1995
- [AD 95-10-10](https://openairdocs.org/ad/95-10-10): Compressor Fan Hub · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Jul 21, 1995
- [AD 94-25-07](https://openairdocs.org/ad/94-25-07): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Mar 30, 1995
- [AD 95-02-16](https://openairdocs.org/ad/95-02-16): Fuel Nozzle and Support Assembly · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Feb 21, 1995
- [AD 91-24-14](https://openairdocs.org/ad/91-24-14): Bearing Seal Spacer · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Jan 21, 1992
- [AD 89-25-11](https://openairdocs.org/ad/89-25-11): Fan Blade Retaining Plates · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Jan 15, 1990
- [AD 86-08-04 R1](https://openairdocs.org/ad/86-08-04-R1): HPC Removable Sleeve Spacers · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Nov 4, 1986
- [AD 86-02-52 R1](https://openairdocs.org/ad/86-02-52-R1): Combustion Chamber · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Apr 14, 1986
- [AD 78-17-02 R3](https://openairdocs.org/ad/78-17-02-R3): Compressor Front Hubs · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Mar 30, 1984
- [AD 80-15-51](https://openairdocs.org/ad/80-15-51): Engine Rear Compressor Front Hubs · Pratt & Whitney Division JT8D-209, JT8D-1, JT8D-11 and 11 more. Effective Aug 21, 1980
- [AD 78-23-12](https://openairdocs.org/ad/78-23-12): Third Stage Turbine Blade Rivet · Pratt & Whitney Division JT8D-1, JT8D-1A, JT8D-1B and 5 more. Effective Dec 20, 1978
- [AD 77-16-12](https://openairdocs.org/ad/77-16-12): Low Turbine Shaft · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 8 more. Effective Aug 31, 1977
- [AD 76-24-01](https://openairdocs.org/ad/76-24-01): Eighth Stage Compressor Disk · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-1A and 6 more. Effective Jun 22, 1977
- [AD 77-07-11](https://openairdocs.org/ad/77-07-11): Fourth Stage Turbine Stator And Rotor · Pratt & Whitney Division JT8D-9 and JT8D-9A. Effective Apr 15, 1977
- [AD 75-05-06](https://openairdocs.org/ad/75-05-06): Fuel Manifold Leakage · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Feb 24, 1977
- [AD 71-25-07](https://openairdocs.org/ad/71-25-07): Fuel Nozzle Support Assemblies · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-1A and 3 more. Effective Dec 14, 1971
- [AD 70-26-05](https://openairdocs.org/ad/70-26-05): First Stage Compressor Rotor Blades · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Dec 29, 1970
- [AD 70-25-08](https://openairdocs.org/ad/70-25-08): Seventh Stage Compressor Rotor Disc · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Dec 15, 1970
- [AD 70-11-03](https://openairdocs.org/ad/70-11-03): Sixth Stage Compressor Discs · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Jun 12, 1970
- [AD 70-02-02](https://openairdocs.org/ad/70-02-02): Sixth Stage Compressor Rotor Disc · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Apr 15, 1970
- [AD 76-12-06](https://openairdocs.org/ad/76-12-06): Second Stage Fan Blades · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-17 and 1 more

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N29SW.

## FAA accident and incident reports (6)

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 19960617029309I](https://openairdocs.org/incident/19960617029309I), Jun 17, 1996: Boeing 7372H4 (N29SW), Wichita Falls, TX. Narrative: emergency landing 6/17/96. Southwest airlines (swaa) N29SW 737-2H4 flt no.273, enroute from lubbock, TX. (Lbb) to dallas, TX (dal). Flight 273,…
- [Incident 19890611032059I](https://openairdocs.org/incident/19890611032059I), Jun 11, 1989: Boeing 7372H4 (N29SW), San Antonio, TX. NR1 engine starter valve open warning after departure. Shut engine down. Returned. Warning due to faulty switch.
- [Incident 19801205085569I](https://openairdocs.org/incident/19801205085569I), Dec 5, 1980: Boeing 737* (N29SW), Corpus Christi, TX. Za flght diverted due to overheated engine. Overheat sensing loop faulty.
- [Incident 19800220026839I](https://openairdocs.org/incident/19800220026839I), Feb 20, 1980: Boeing 737/ (N29SW), San Antonio, TX. Flight taxied out. Had fuel smell in cockpit. Taxied back to gate. Departed 13 minutes later.
- [Incident 19791025054289I](https://openairdocs.org/incident/19791025054289I), Oct 25, 1979: Boeing 737/ (N29SW), Houston, TX, Substantial damage. Engine turbine failed at rotation.
- [Incident 19780525040359I](https://openairdocs.org/incident/19780525040359I), May 25, 1978: Boeing 737/ (N29SW), Austin, TX, Minor damage. Jetway stalled after craft had been cleared by ground crew to taxi. Wingtip struck jetway.

## Service difficulty reports (100, newest 50)

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

- [SDR 2002F00416](https://openairdocs.org/sdr/2002F00416), Mar 15, 2002: CIRCUIT BREAKER. SHORTED. IN FLIGHT, CREW NOTICED CIRCUIT BREAKER POPPED AND ELECTRICAL SMOKE IN COCKPIT. AIRCRAFT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. (M)
- [SDR 2002F00415](https://openairdocs.org/sdr/2002F00415), Mar 7, 2002: BOTTLE. DISCHARGED. IN FLIGHT, GOT APU OVERHEAT INDICATION. DISCHARGED APU FIRE BOTTLE. AIRCRAFT LANDED WITHOUT INCIDENT. NO EVIDENCE OF FIRE FOUND AFTER APU INSPECTION. (M)
- [SDR 2002F00117](https://openairdocs.org/sdr/2002F00117), Dec 30, 2001: FIRE WARNING. MALFUNCTIONED. MASTER FIRE WARNING LIGHT FLICKERED ON AND OFF DURING DESCENT. ON FINAL, LIGHT CAME ON STEADY WITH NO OTHER ASSOCIATED FIRE WARNINGS. LIGHT WAS RESET. (M)
- [SDR COOSDR010073](https://openairdocs.org/sdr/COOSDR010073), Jul 12, 2001: FLOORBEAM. CRACKED. PAX CABIN FROM BS 520 RBL 25 AND WL 208, FLOOR BEAM CRACKED.
- [SDR COOSDR010072](https://openairdocs.org/sdr/COOSDR010072), Jul 12, 2001: FRAME. CRACKED. LOWER FUSELAGE LEFT WHEEL WELL, BS 663.75 LBL 25 AND WL 208 CHORD, CRACKED.
- [SDR COOSDR010071](https://openairdocs.org/sdr/COOSDR010071), Jul 12, 2001: ANGLE. CRACKED. LOWER FUSELAGE RIGHT WHEEL WELL, BULKHEAD BS 727, BL 0 AND WL 208 ANGLE, CRACKED.
- [SDR COOSDR010070](https://openairdocs.org/sdr/COOSDR010070), Jul 12, 2001: SKIN. DELAMINATED. LEFT WING GROUND SPOILER NR 5 WITH UPPER SKIN DELAMINATED.
- [SDR COOSDR010069](https://openairdocs.org/sdr/COOSDR010069), Jul 12, 2001: SKIN. DELAMINATED. RIGHT WING, FLIGHT SPOILER NR 8 UPPER SKIN, DELAMINATED.
- [SDR COOSDR010068](https://openairdocs.org/sdr/COOSDR010068), Jul 12, 2001: SKIN. DELAMINATED. LEFT WING, IB FORE FLAP UPPER SKIN DELAMINATED.
- [SDR COOSDR010067](https://openairdocs.org/sdr/COOSDR010067), Jul 12, 2001: SKIN. DELAMINATED. LEFT WING, GROUND SPOILER NR4 UPPER SKIN DELAMINATED.
- [SDR COOSDR010066](https://openairdocs.org/sdr/COOSDR010066), Jul 12, 2001: SKIN. DELAMINATED. LEFT WING SLAT NR 3 UPPER SKIN DELAMINATED.
- [SDR COOSDR010064](https://openairdocs.org/sdr/COOSDR010064), Jul 12, 2001: STRINGER. CRACKED. FUSELAGE STRINGER SECTION 27L FROM BS 960 TO BS 1016, CRACKED.
- [SDR COOSDR010063](https://openairdocs.org/sdr/COOSDR010063), Jul 12, 2001: FLOORBEAM. CRACKED. FUSELAGE FLOOR BEAM SECTION UPPER CHORD AT BS 328 BETWEEN RBL 24.5 AND RBL40, CRACKED.
- [SDR COOSDR010062](https://openairdocs.org/sdr/COOSDR010062), Jul 12, 2001: FRAME. CRACKED. FUSELAGE FRAME SECTION AT BS 328 BETWEEN STR 1R AND 4R, CRACKED.
- [SDR COOSDR010061](https://openairdocs.org/sdr/COOSDR010061), Jul 12, 2001: STRINGER. CRACKED. FUSELAGE STRINGER SECTION FROM BS 306 TO BS 326 AT STR 4R, CRACKED.
- [SDR COOSDR010060](https://openairdocs.org/sdr/COOSDR010060), Jul 12, 2001: STRINGER. CRACKED. FUSELAGE STRINGER SECTION FROM BS 429 TO BS 450 AT STR 4R, CRACKED.
- [SDR COOSDR010059](https://openairdocs.org/sdr/COOSDR010059), Jul 12, 2001: FRAME. CRACKED. FUSELAGE FRAME SECTION AT BS 344 FROM STR. 4L AND STR 6L, CRACKED.
- [SDR COOSDR010058](https://openairdocs.org/sdr/COOSDR010058), Jul 12, 2001: STRINGER. CRACKED. FUSELAGE STRINGER SECTION 9L FROM BS 727A+7 TO BS 727B+12, CRACKED.
- [SDR COOSDR010057](https://openairdocs.org/sdr/COOSDR010057), Jul 12, 2001: STRINGER. CRACKED. FUSELAGE STRINGER SECTION 9R FROM BS 755 TO BS 780, CRACKED.
- [SDR COOSDR010056](https://openairdocs.org/sdr/COOSDR010056), Jul 12, 2001: STRINGER. CRACKED. UPPER FUSELAGE MAIN CABIN STRINGER 11R AT BS 540, CRACKED.
- [SDR COOSDR010055](https://openairdocs.org/sdr/COOSDR010055), Jul 12, 2001: STRINGER. CRACKED. UPPER FUSELAGE MAIN CABIN STRINGER 11L AT BS 540 CRACKED.
- [SDR COOSDR010054](https://openairdocs.org/sdr/COOSDR010054), Jul 12, 2001: STRINGER. CRACKED. PAX CABIN, BS 727+9INCHES, STRINGER NR 1 CRACKED.
- [SDR COOSDR010053](https://openairdocs.org/sdr/COOSDR010053), Jul 12, 2001: SKIN. CANNING. EXT. FUSELAGE BS 864 BETWEEN STRINGER 16L AND 17L, SKIN WITH OIL CAN.
- [SDR COOSDR010052](https://openairdocs.org/sdr/COOSDR010052), Jul 12, 2001: FLOORBEAM. CRACKED. FORWARD C/C, FLOOR BEAM, LOWER CHORD, RBL 25 INCHES, WL 201 WITH CRACK.
- [SDR COOSDR010051](https://openairdocs.org/sdr/COOSDR010051), Jul 12, 2001: STRINGER. CORRODED. AFT C/C BAY, STA967, STR 27R CORRODED.
- [SDR COOSDR010050](https://openairdocs.org/sdr/COOSDR010050), Jul 12, 2001: SKIN. CRACKED. EXTERNAL FUSELAGE, E & E COMPARTMENT, DOOR AROUND CUT OUT SKIN WITH SHARP EDGES AND CRACKED.
- [SDR COOSDR010049](https://openairdocs.org/sdr/COOSDR010049), Jul 12, 2001: SKIN. DENTED. EXTERNAL FUSELAGE, BETWEEN BS 423 AND BS 435 BETWEEN STR 20R, SKIN DENTED.
- [SDR COOSDR010048](https://openairdocs.org/sdr/COOSDR010048), Jul 12, 2001: SKIN. DENTED. EXTERNAL FUSELAGE BS890 BETWEEN STR 20R AND STR 21R DENTED.
- [SDR COOSDR010044](https://openairdocs.org/sdr/COOSDR010044), Jun 21, 2001: SPAR. CRACKED. WING - CENTER WING BOX - REAR SPAR CRACKED - STA 663.0/ RBL6.150/ WL 170.4
- [SDR COOSDR010043](https://openairdocs.org/sdr/COOSDR010043), Jun 21, 2001: BULKHEAD. CRACKED. AFT PRESSURE BULKHEAD - BS 1016 WEB CRACKED, Y CHORD INSPECTION.
- [SDR COOSDR010039](https://openairdocs.org/sdr/COOSDR010039), Jun 21, 2001: FRAME. CRACKED. PAX CABIN, BS 727, AT STR 14L LEVEL FRAME CRACKED. PROBABLE CAUSE IS FATIGUE.
- [SDR COOSDR010037](https://openairdocs.org/sdr/COOSDR010037), Jun 21, 2001: FLOORBEAM. CORRODED. PAX CABIN, STA 947 FLOOR BEAM UPPER FLANGE CORRODED AT LBL 50.
- [SDR COOSDR010036](https://openairdocs.org/sdr/COOSDR010036), Jun 21, 2001: STRINGER. CRACKED. PAX CABIN, STA 618, STRINGER 17R, HORIZONTAL FLANGE CRACKED.
- [SDR 2001F00180](https://openairdocs.org/sdr/2001F00180), May 27, 2001: FLOORBEAM. CORRODED. FOUND PASSENGER CABIN, STATION 947 FLOORBEAM UPPER FLANGE CORRODED AT LBL 50. THE CORRODED FLOORBEAM SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW EO 
- [SDR 2001F00146](https://openairdocs.org/sdr/2001F00146), May 27, 2001: FLOORBEAM. CORRODED. FOUND PASSENGER CABIN, STATION 947 FLOORBEAM UPPER FLANGE CORRODED AT LBL 50. THE CORRODED FLOORBEAM SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW EO 
- [SDR 2001F00183](https://openairdocs.org/sdr/2001F00183), May 26, 2001: SKIN. DENTED. THE FUSELAGE SKIN AT BS 890 BETWEEN STRINGER 20R AND 21R WAS FOUND DENTED. THE DAMAGED AREA WAS REPAIRED IAW BOEING FAX COO-SJD-01-003292MM DATED 6/11/2001. (M)
- [SDR 2001F00145](https://openairdocs.org/sdr/2001F00145), May 26, 2001: SKIN. DENTED. THE FUSELAGE SKIN AT BS 890 BETWEEN STRINGER 20R AND 21R WAS FOUND DENTED. THE DAMAGED AREA WAS REPAIRED IAW BOEING FAX COO-SJD-01-00392M DATED 6/11/2001. (M)
- [SDR 2001F00197](https://openairdocs.org/sdr/2001F00197), May 1, 2001: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 440, STRINGER 4 RIGHT. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 3. (M)
- [SDR 2001F00196](https://openairdocs.org/sdr/2001F00196), May 1, 2001: STRINGER. CRACKED. FOUND STRINGER AT STATION BS 727B STRINGER 9 LEFT HAS CRACK. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIG 3. (M)
- [SDR 2001F00195](https://openairdocs.org/sdr/2001F00195), May 1, 2001: FLOORBEAM. CORRODED. THE FLOORBEAM WAS FOUND CORRODED AT BS 328, RBL 32. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-9 FIGURE 6. (M)
- [SDR 2001F00194](https://openairdocs.org/sdr/2001F00194), May 1, 2001: STRINGER. CORRODED. AT STRINGER 27L FROM BS 1006 TO BS 1016, CORROSION WAS FOUND. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 1. (M)
- [SDR 2001F00193](https://openairdocs.org/sdr/2001F00193), May 1, 2001: ANGLE. CRACKED. FOUND LOWER FUSELAGE, BS 727 BULKHEAD, BLO WL 208 ANGLE CRACKED. DAMAGED AREA WAS REPAIRED PER SB 737-53-1053. (M)
- [SDR 2001F00192](https://openairdocs.org/sdr/2001F00192), May 1, 2001: FRAME. CRACKED. FOUND CRACK IN FRAME STATION BS 344 STRINGER 6 LEFT. THE DAMAGED AREA WAS REPAIRED IAW SRM 51-40-3 FIGURE 1. (M)
- [SDR 2001F00191](https://openairdocs.org/sdr/2001F00191), May 1, 2001: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 312, STRINGER 4 RIGHT. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 3. (M)
- [SDR 2001F00190](https://openairdocs.org/sdr/2001F00190), May 1, 2001: SKIN. CANNING. THE FUSELAGE SKIN WAS FOUND WITH OIL CANNING. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-30-3 FIGURE 3. (M)
- [SDR 2001F00189](https://openairdocs.org/sdr/2001F00189), May 1, 2001: FRAME. DAMAGED. THE FRAME WAS FOUND WITH ELONGATED HOLES AT BS 328 BETWEEN STRINGER 2R AND STRINGER 3R. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-4 FIGURE 1. (M)
- [SDR 2001F00188](https://openairdocs.org/sdr/2001F00188), May 1, 2001: FLOORBEAM. CRACKED. FOUND FLOORBEAM FOUND CRACKED AT BS 520 RBL 25 WL 208. THE DAMAGED AREA WAS REPAIRED IAW SB 737-53-1120. (M)
- [SDR 2001F00187](https://openairdocs.org/sdr/2001F00187), May 1, 2001: FLOORBEAM. CRACKED. FOUND FLOORBEAM AT BS 520 RBL 25 INCH LOWER CHORD HAS CRACK. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-9 FIGURE 7. (M)
- [SDR 2001F00186](https://openairdocs.org/sdr/2001F00186), May 1, 2001: SLAT. DELAMINATED. THE NR 3 SLAT WAS FOUND DELAMINATED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-239-01. (M)
- [SDR 2001F00185](https://openairdocs.org/sdr/2001F00185), May 1, 2001: FLAP. WORN. THE UPPER SURFACE OF THE INBOARD FORE FLAP WAS SHOWING WEAR. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-A57-243-01, DATED JUNE 06-01. (M)

All 100: https://openairdocs.org/aircraft/N29SW/reports.md

## STCs that may be installed (OpenAirDocs) (19)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (Pratt & Whitney JT8D-9 series)

- [STC SE1622GL](https://openairdocs.org/stc/SE1622GL): Installation of Ametek 8TJ124GGR1 digital mass fuel flow transmitter. ABX Air Incorporated
- [STC SE01588AT](https://openairdocs.org/stc/SE01588AT): Installation of McClain International JT8D first stage turbine airseal as documented. McClain International, Inc
- [STC SE2930SO](https://openairdocs.org/stc/SE2930SO): Installation of an alternate gearbox cover seal utilizing an aluminum retainer .040-inch thick with a molded-in-place elastomeric seal contoured to fit the main housing/cover flange interface. Parker O-Seal Division. Lists JT8D Series
- [STC SE497NE](https://openairdocs.org/stc/SE497NE): Installation of oil tank filler neck check valve assembly. Aviation Components Support
- [STC SE3916NM](https://openairdocs.org/stc/SE3916NM): Installation of CADC bleed valve supports brackets, P/N B10002 or RB10003, as a replacement part for P&W P/N 578273. Aeroparts Mfg & Repair. Lists JT8D Series
- [STC SE79WE](https://openairdocs.org/stc/SE79WE): Installation of CADC bleed valve support brackets, P/N B10001 or RB10006, as a replacement part for P&W P/N 493317 used on JT8D-1, -5, -7, -9, -9A, -15 and -17 engines. Aeroparts Mfg & Repair. Lists JT8D Series
- [STC SE00049AT-D](https://openairdocs.org/stc/SE00049AT-D): Installation of Intermediate Compressor Case (JT8D SERIES). Aero Component Technologies. Lists JT8D Series
- [STC SE2787CE](https://openairdocs.org/stc/SE2787CE): Installation of P/N T92871 first stage turbine vanes. Trans World Airlines Inc
- [STC SE59GL](https://openairdocs.org/stc/SE59GL): Installation of O-ring face seal P/N-s 1-1337-700, -701, 1-1633-700, -701, 1-1738-700, -701; and/or 1-2233-700, 701. Rexnord, Inc
- [STC SE86WE](https://openairdocs.org/stc/SE86WE): Replace the airoils on P&WA P/Ns 495051, 478351, 583751, 653851, 653951, 572451, 583351, 653751, 653151, 676951, 728951, 709951, 710751, 627751, 737271, 578551, 738271, 747171, 792871, 786471, 583751, 777971, 780591, 782571, 793181, 799771, 794481, 794491 , 798781, and 799191. Chromizing Company
- [STC SE557NE](https://openairdocs.org/stc/SE557NE): Installation of oil tank shuttle valve. Stockbridge William D
- [STC SE2666SO](https://openairdocs.org/stc/SE2666SO): Modification of the anti-ice mount bracket. Cook Airtomic
- [STC SE593NE](https://openairdocs.org/stc/SE593NE): Installation of a Select Controls Inc. Engine Oil Shuttle Valve, P/N 2057-1-001. (See Eligibility List). Basken Valve Corporation. Lists JT8D Series
- [STC SE1930SO](https://openairdocs.org/stc/SE1930SO): Installation of power control shaft bushing. Cook Airtomic Division. Lists JT8D Series
- [STC SE83WE](https://openairdocs.org/stc/SE83WE): Installation of heat shield assembly P/N 408-007 as a replacement part for P&W P/N499941 or 749609 used on JT8D-1, -5, -7, -9, -9A, -15 and -17 engines. Hughes Helicopter. Lists JT8D Series
- [STC SE84WE](https://openairdocs.org/stc/SE84WE): Installation of heat shield assembly 408-008 as a replacement part for P&W No. 586918 used on JT8D-1, -5, -7, -9, -9A, -15 and -17 engines. Hughes Helicopter. Lists JT8D Series
- [STC SE67WE](https://openairdocs.org/stc/SE67WE): Installation of fuel control rod end bearings. Triumph Corporation. Lists JT8D Series
- [STC SA2627WE](https://openairdocs.org/stc/SA2627WE): Installation of fuel control rod end bearings. Triumph Corporation. Lists JT8D Series
- [STC SE5058NM](https://openairdocs.org/stc/SE5058NM): Incorporation of feather seals into platforms of the first stage nozzle guide vanes, P&W P/N 653751, 737271, 738271, 747171, 792871, 786471, and 798771. Chromizing Company

## Related

- Other Boeing 737-2H4 aircraft: https://openairdocs.org/model/boeing-737-2h4/aircraft.md
- The Pratt & Whitney JT8D-9 series engine: https://openairdocs.org/engine/pratt-whitney-jt8d-9-series.md

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