# N743DH: 1980 Boeing 727-225, registration cancelled 2010-03-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 8, 2010 - Exported to: Brazil - Status when cancelled: Valid registration - Airframe: [Boeing 727-225](https://openairdocs.org/model/boeing-727-225) (registry code 1384077) - Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 22438 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 30, 2000 - Certificate issued: May 24, 1999 - Last registry action: November 19, 2008 - Mode S code: A9FE02 - Owner when cancelled: [Pegasus Aviation II Inc](https://openairdocs.org/faa-owner/PEGASUS%20AVIATION%20II%20INC) - Location: [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco) - Owner type: Corporation - Owner's area on the map: 37.7984° N, 122.3992° W: Placed by OpenAirDocs at the center of ZIP code 94111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N743DH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=743DH - Page: https://openairdocs.org/deregistered/N743DH-2010-03-08 From the FAA registry file of November 5, 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 Boeing 727-225: https://openairdocs.org/model/boeing-727-225.md ## Service difficulty reports (299, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DHLA2009743DH665](https://openairdocs.org/sdr/DHLA2009743DH665), Feb 10, 2009: STRINGER. CORRODED. LOWER FUSELAGE FROM BS 1183 TO BS 1193 S-26L WITH CORROSION. REPLACED S-26L SECTION FROM BS 1185 TO BS 1213.25 IAW SRM 51-10-1 PARA 7A. - [SDR DHLA2009743DH618](https://openairdocs.org/sdr/DHLA2009743DH618), Jan 19, 2009: FRAME. CORRODED. LOWER FUSELAGE E/E COMPARTMENT AT BS 460 BETWEEN S-23L AND S-24L FRAME WITH CORROSION. REPAIRED FRAME SECTION SHEAR TIE AT BS 460 BETWEEN S-23L AND S-24L IAW B7 - [SDR DHLA2009743543](https://openairdocs.org/sdr/DHLA2009743543), Jan 19, 2009: SEAT TRACK. CORRODED. CABIN SEAT TRACK CORRODED, BS 950 +9 INCH TO BS 1135, RBL 45. REMOVED, FABRICATED NEW, AND INSTALLED SEAT TRACK SECTION PER B727 SRM 53-10-5 FIG 7 AND 51-10-1. - [SDR DHLA2009743544](https://openairdocs.org/sdr/DHLA2009743544), Jan 18, 2009: FLOORBEAM. CORRODED. CABIN FLOORBEAM AT BS 950F CORRODED ON UPPER FLANGE AT RBL 11. ACCOMPLISHED FLOORBEAM REPAIR PER SRM 53-10-8 FIG 8. - [SDR DHLA2009743542](https://openairdocs.org/sdr/DHLA2009743542), Jan 18, 2009: FLOORBEAM. DAMAGED. CABIN FLOORBEAM AT BS 660 HAS DOUBLE DRILLED HOLES AT RBL 62.5. REPAIRED FLOORBEAM AS REQUIRED IN EO COO-2-53-470-08 DATED 12/17/08. REF FAA FORM 8110-3 DATED 1 - [SDR DHLA2009743541](https://openairdocs.org/sdr/DHLA2009743541), Jan 6, 2009: ANGLE. CRACKED. LT INBD MID FLAP LOWER T/E PANEL ATTACH ANGLE CRACKED AT WBL 106. REPAIRED ANGLE BY SPLICING IN A NEW SECTION PER SRM 51-40-4 FIG 1. - [SDR DHLA2009743529](https://openairdocs.org/sdr/DHLA2009743529), Jan 6, 2009: STRAP. CORRODED. FLOORBEAM STABALIZER STRAP CORRODED, BS 1010 TO BS 1130 AT RBL 25. REMOVED, FABRICATED, AND INSTALLED NEW STABALIZER STRAP IAW SRM 51-10-1 AND 51-30-2. - [SDR DHLA2009743DH557](https://openairdocs.org/sdr/DHLA2009743DH557), Jan 5, 2009: FRAME. DAMAGED. UPPER FUSELAGE MAIN CARGO CABIN BS 420 BTWN S-16R AND S-17R FUSELAGE FRAME WITH DOUBLE HOLE. REPAIRED FRAME SECTION AT BS 420 BTWN S-15R AND S-17R IAW B727 SRM - [SDR DHLA2009743535](https://openairdocs.org/sdr/DHLA2009743535), Dec 29, 2008: FRAME. DAMAGED. FUSELAGE FRAME HAS DOUBLE DRILLED HOLES AT BS 560, STR 14R TO 17R. REMOVED FRAME SECTION. FABRICATED, AND INSTALLED FRAME SECTION PER SRM 53-10-2 FIG 2, 51-30-2 - [SDR DHLA2009743533](https://openairdocs.org/sdr/DHLA2009743533), Dec 29, 2008: SKIN. DENTED. FUSELAGE SKIN DENTED AT BS 950F +14 INCH, BETWEEN STR 28R AND 29R. ACCOMPLISHED DOUBLER REPAIR TO FUSE SKIN PER SRM 53-30-3 FIG 1. - [SDR DHLA7432009648](https://openairdocs.org/sdr/DHLA7432009648), Dec 22, 2008: ATTACH FITTING. CRACKED. LT WING NR 7 SPOILER ACTUATOR SUPPORT FITTING CRACKED. REPLACED NR 7 SPOILER ACTUATOR SUPPORT FITTING IAW B727 SRM 51-10-1 PARA 7. INSTALLED RIVETS, LOCK FASTEN - [SDR DHLA2009743548](https://openairdocs.org/sdr/DHLA2009743548), Dec 22, 2008: FRAME. DENTED. BS 1030 FRAME DENTED AT STR 26L. ACCOMPLISHED FRAME REPAIR AS REQUIRED PER B727 SRM 51-40-3 FIG 1. - [SDR DHLA2008743DH669](https://openairdocs.org/sdr/DHLA2008743DH669), Dec 18, 2008: FLOORBEAM. DAMAGED. UPPER FUSELAGE MAIN CARGO CABIN AT BS 1148 LBL 62 FLOORBEAM UPPER FLANGE WITH DOUBLE HOLE. REPAIRED FLOORBEAM SECTION AT BS 1148 BTWN LBL 22 AND LBL 70 IAW COOP - [SDR DHLA2009743DH655](https://openairdocs.org/sdr/DHLA2009743DH655), Dec 18, 2008: FLOORBEAM. DAMAGED. UPPER FUSELAGE MAIN CARGO CABIN AT BS 1148 RBL 62 FLOORBEAM UPPER FLANGE WITH DOUBLE HOLE. REPAIRED FLOORBEAM SECTION AT BS 1148 BTWN RBL 52 AND RBL 62 IAW EO C - [SDR DHLA2009743DH570](https://openairdocs.org/sdr/DHLA2009743DH570), Dec 10, 2008: WEB. CORRODED. UPPER FUSELAGE MAIN CARGO CABIN FROM BS 1130 TO BS 1183 BETWEEN LBL 25 AND LBL62 FLOOR WEB WITH DOUBLE HOLES AND CORROSION. REMOVED CORROSION FROM BS 1130 TO BS - [SDR DHLA2009743DH569](https://openairdocs.org/sdr/DHLA2009743DH569), Dec 10, 2008: WEB. CORRODED. UPPER FUSELAGE MAIN CARGO CABIN FROM BS 1130 TO BS 1183 BETWEEN RBL 25 AND RBL 62 FLOOR WEB WITH CORROSION. REMOVED CORROSION AND FOUND WITHIN LIMITS AT BS 1130 - [SDR DHLA2009743534](https://openairdocs.org/sdr/DHLA2009743534), Dec 5, 2008: WEB. CORRODED. VERTICAL FLOOR WEB IN AFT CARGO COMPT CORRODED, BS 1165 TO 1170, WL 208, RBL 25. ACCOMPLISHED WEB REPAIR PER SRM 51-40-2 FIG 2. - [SDR DHLA2009743532](https://openairdocs.org/sdr/DHLA2009743532), Dec 5, 2008: FLOORBEAM. CORRODED. FLOORBEAM UPPER CHORD CORRODED AT BS 328, WL 208, AT RBL 44. REMOVED, FABRICATED, AND REPLACED FLOORBEAM UPPER CHORD IAW SRM 51-10-1 AND 51-30-2. - [SDR DHLA2009743536](https://openairdocs.org/sdr/DHLA2009743536), Dec 3, 2008: FLAP TRACK. CORRODED. NR 3 FLAP TRACK, FWD AND AFT ATTACH SURFACES CORRODED. ACCOMPLISHED REPAIR TO FLAP TRACK SURFACES IAW OHM 57-40-01 PAGE 403-411. - [SDR DHLA2009743530](https://openairdocs.org/sdr/DHLA2009743530), Dec 2, 2008: STIFFENER. CRACKED. REF NR 1-267: VERTICAL STIFFENER ON BS 1183 BULKHEAD, AT RBL 8, CRACKED. ACCOMPLISHED REPAIR TO STIFFENER IAW SB 727-53-0175 R3, SECT III, PART III, FIG 3, DATE - [SDR DHLA2008743DH668](https://openairdocs.org/sdr/DHLA2008743DH668), Nov 29, 2008: FLOORBEAM. DAMAGED. UPPER FUSELAGE MAIN CARGO CABIN AT BS 720A RBL 62 FLOORBEAM WITH DOUBLE HOLE. REPAIRED FLOORBEAM SECTION AT BS 720A BTWN RBL 27 AND RBL 70 IAW COOPESA EO COO-2- - [SDR DHLA2009743552](https://openairdocs.org/sdr/DHLA2009743552), Nov 29, 2008: FRAME. DAMAGED. BS 825 MAIN FRAME HAS DOUBLE DRILLED HOLES BETWEEN STR 3L AND 5L. ACCOMPLISHED FRAME REPAIR IAW SRM 53-10-4 FIG 1. - [SDR DHLA2009743DH642](https://openairdocs.org/sdr/DHLA2009743DH642), Nov 28, 2008: FLOORBEAM. DAMAGED. UPPER FUSELAGE MAIN CARGO CABIN AT BS 500 LBL 62 FLOORBEAM UPPER CHORD WITH DOUBLE HOLE. REPAIRED FLOORBEAM SECTION AT BS 500 BTWN LBL 56.5 AND LBL 70 IAW EO CO - [SDR DHLA2009743554](https://openairdocs.org/sdr/DHLA2009743554), Nov 27, 2008: FRAME. DAMAGED. BS 700 MAIN FRAME HAS DOUBLE DRILLED HOLES BETWEEN STR 13L AND 17L. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1 AND 53-10-4 FIG 1 BETWEEN STR 11L AND 1 - [SDR DHLA2009743553](https://openairdocs.org/sdr/DHLA2009743553), Nov 27, 2008: FRAME. DAMAGED. BS 783 MAIN FRAME HAS DOUBLE DRILLED HOLES BETWEEN STR 7L AND 8L. ACCOMPLISHED FRAME REPAIR IAW SRM 53-10-4 FIG 1. - [SDR DHLA2009743DH574](https://openairdocs.org/sdr/DHLA2009743DH574), Nov 26, 2008: KEELBEAM. CRACKED. LOWER FUSELAGE BS 740 LBL 8 WL 147 KEEL BEAM AREA CHORD ANGLE WITH CRACK. REPLACED CHORD ANGLE AT BS 740 BETWEEN LBL 8 AND LBL 18.5 WL 147 IAW B727 SRM 51-10-1 - [SDR DHLA2009743546](https://openairdocs.org/sdr/DHLA2009743546), Nov 26, 2008: FRAME. DAMAGED. BS 1110 FRAME HAS DOUBLE DRILLED HOLES BETWEEN STR 4L AND 5L. ACCOMPLISHED FRAME REPAIR AS REQUIRED PER B727 SRM 51-40-3 FIG 1. - [SDR DHLA2009743540](https://openairdocs.org/sdr/DHLA2009743540), Nov 26, 2008: FRAME. DAMAGED. BS 720 FRAME HAS DOUBLE DRILLED HOLES BETWEEN STR 16L AND 17L. ACCOMPLISHED FRAME REPAIR AS REQ PER SRM 51-40-3 FIG 1. - [SDR DHLA2009743538](https://openairdocs.org/sdr/DHLA2009743538), Nov 26, 2008: FRAME. DAMAGED. FUSELAGE FRAME AT BS 600 HAS DOUBLE DRILLED HOLES BETWEEN STR 13R AND 17R. REMOVED FRAME SECTION BETWEEN STR 13R AND 18R. FABRICATED FRAME SECTION, AND INSTALLE - [SDR DHLA2009743555](https://openairdocs.org/sdr/DHLA2009743555), Nov 25, 2008: FRAME. DAMAGED. BS 460 MAIN FRAME INBD FLANGE HAS ELONGATED HOLES BETWEEN STR 6R AND 7R. ACCOMPLISHED FRAME REPAIR IAW SRM 53-10-4 FIG 1. - [SDR DHLA2009743551](https://openairdocs.org/sdr/DHLA2009743551), Nov 25, 2008: FRAME. DENTED. BS 680 MAIN FRAME DENTED/DOUBLE DRILLED HOLES BETWEEN STR 13L AND 17L. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1. - [SDR DHLA2009743549](https://openairdocs.org/sdr/DHLA2009743549), Nov 25, 2008: FRAME. DAMAGED. BS 848 FRAME HAS DOUBLE DRILLED AND ELONGATED HOLES BETWEEN STR 2L AND 5L. ACCOMPLISHED FRAME REPAIR AS REQUIRED PER B727 SRM 53-10-4 FIG 1. - [SDR DHLA2009743547](https://openairdocs.org/sdr/DHLA2009743547), Nov 25, 2008: FRAME. DAMAGED. BS 400 FRAME HAS DOUBLE DRILLED HOLES BETWEEN STR 2L AND 3L. ACCOMPLISHED FRAME REPAIR AS REQUIRED PER B727 SRM 53-10-4 FIG 1. - [SDR DHLA2009743539](https://openairdocs.org/sdr/DHLA2009743539), Nov 25, 2008: FRAME. DENTED. FUSELAGE FRAME AT BS 1070 DENTED BETWEEN STR 25R AND 27R. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1. - [SDR DHLA2009743537](https://openairdocs.org/sdr/DHLA2009743537), Nov 25, 2008: FRAME. DENTED. FUSELAGE FRAME AT BS 1050 DENTED AT STR 26L. REPAIRED FRAME SECTION IAW SRM 51-40-3 FIG 1. - [SDR DHLA2008743511](https://openairdocs.org/sdr/DHLA2008743511), Nov 25, 2008: STRINGER. CORRODED. LOWER FUSELAGE FROM BS 720F TO BS 740 S27L WITH CORROSION. REPAIRED FUSELAGE STRINGER SECTION FROM BS 720F+17.25 INCH TO BS 740 S27L IAW SRM 53-10-3 FIG 1. - [SDR DHLA7432009647](https://openairdocs.org/sdr/DHLA7432009647), Nov 24, 2008: STRINGER. CORRODED. LOWER FUSELAGE FWD CARGO COMPT FROM BS 720 F+15 TO BS 740 STR 27R WITH CORROSION. REPAIRED AT STR 27R FROM BS 720 F+ 15 TO BS 740-2" DUE TO CORROSION IAW SRM 53 - [SDR DHLA2009743545](https://openairdocs.org/sdr/DHLA2009743545), Nov 24, 2008: STRINGER. CRACKED. VERTICAL STABILIZER, LT SIDE, AT FIN STA 133, STR 9 CRACKED AT WL 359. ACCOMPLISHED REPAIR TO STRINGER PER B727 SRM 55-30-3 FIG 2. - [SDR DHLA2009743550](https://openairdocs.org/sdr/DHLA2009743550), Nov 23, 2008: FRAME. DAMAGED. BS 1170 FRAME HAS DOUBLE DRILLED HOLES ON INBD FLANGE BETWEEN STR 16L AND 17L. ACCOMPLISHED FRAME REPAIR AS REQUIRED PER B727 SRM 51-40-3 FIG 1. - [SDR DHLA2008743517](https://openairdocs.org/sdr/DHLA2008743517), Nov 23, 2008: STRAP. CRACKED. LOWER FUSELAGE E/E COMPARTMENT FROM BS 294.5 TO BS 360 WL 199 BL 0 STABILIZER CRACKED. REPLACED STABILIZER STRAP SECTION FROM BS 294.5 TO BS 360 WL 199 BL 0 IAW - [SDR DHLA2009743DH654](https://openairdocs.org/sdr/DHLA2009743DH654), Nov 20, 2008: FRAME. DENTED. UPPER FUSELAGE MAIN CARGO CABIN AT BS 360 BTWN S-4L AND S-5L FRAME INBD FLANGE WITH DENT. REPAIRED FRAME SECTION AT BS 360 BTWN S-4L AND S-6L IAW EO COO-2-53-43 - [SDR DHLA2008743509](https://openairdocs.org/sdr/DHLA2008743509), Nov 20, 2008: FLOORBEAM. CORRODED. UPPER FUSELAGE CARGO CABIN BS 328 BTWN LBL 45 AND RBL 45 FLOORBEAM UPPER CHORD CORRODED. REPLACED FLOORBEAM SECTION AT BS 328 WL 208 BTWN RBL 63 AND LBL 63 DUE - [SDR DHLA2008743524](https://openairdocs.org/sdr/DHLA2008743524), Nov 18, 2008: FRAME. DAMAGED. FUSELAGE FRAME HAS DOUBLE DRILLED HOLES AT BS 680, STR 16R TO 17R. REPAIRED FUSE FRAME SECTION PER SRM 51-40-3 FIG 1. - [SDR DHLA2009743DH682](https://openairdocs.org/sdr/DHLA2009743DH682), Nov 17, 2008: SKIN PANEL. DAMAGED. LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 950D BTWN S-26L AND S-27L FUSELAGE SKIN WITH DOUBLE HOLE. REPAIRED FUSELAGE SKIN PANEL FROM BS 950C+16" TO BS 950D+6" - [SDR DHLA2008743506](https://openairdocs.org/sdr/DHLA2008743506), Nov 17, 2008: FLOORBEAM. CORRODED. LOWER FUSELAGE E/E COMPARTMENT BS 328 WL 208 RBL 44 FLOORBEAM WITH CORROSION. REPLACED FUSELAGE FLOORBEAM SECTION AT BS 328 BETWEEN LBL 63 AND RBL 63 IAW SRM 51 - [SDR DHLA2009743DH663](https://openairdocs.org/sdr/DHLA2009743DH663), Nov 15, 2008: BEAM. CORRODED. RT WING TRAILING EDGE SECTION MAIN LANDING GEAR WALKING BEAM HOLES WITH CORROSION INCLUDING LOWER SURFACE. REPAIRED RT MLG WALKING BEAM HOLES AND LOWER SURFACE - [SDR DHLA2009743DH686](https://openairdocs.org/sdr/DHLA2009743DH686), Nov 14, 2008: CHANNEL. CRACKED. MAIN CARGO DOOR UPPER FORWARD CORNER CHANNEL WITH CRACK FOUND WHEN PERFORM OPEN HOLE INSPECTION PER ASTAR TASK CARD EC-00297-001. REPLACED UPPER FORWARD CHANNEL - [SDR DHLA2009743DH645](https://openairdocs.org/sdr/DHLA2009743DH645), Nov 14, 2008: FLOORBEAM. DAMAGED. UPPER FUSELAGE MAIN CARGO CABIN AT BS 1130 RBL 62 UPPER CHORD WITH DOUBLE HOLE. REPAIRED FLOORBEAM AT BS 1130 BTWN RBL 57 AND RBL 62 IAW EO COO-2-53-435-08 DTD - [SDR DHLA2009743DH644](https://openairdocs.org/sdr/DHLA2009743DH644), Nov 14, 2008: FLOORBEAM. DAMAGED. UPPER FUSELAGE MAIN CARGO CABIN AT BS 1130 LBL 62 FLOORBEAM UPPER CHORD WITH DOUBLE HOLE. REPAIRED FLOORBEAM SECTION AT BS 1130 BTWN LBL 6.5 AND LBL 62 IAW COOP - [SDR DHLA2009743DH636](https://openairdocs.org/sdr/DHLA2009743DH636), Nov 14, 2008: DOOR FRAME. CRACKED. MAIN CARGO DOOR AT BS 597 DOOR FRAME CRACKED AT HINGE LOWER ROW. FOUND WHEN PERFORMING OPEN HOLE INSPECTION PER ASTAR AIRCARGO TASK CARD EC-00297-001. REPAIRED All 299: https://openairdocs.org/deregistered/N743DH-2010-03-08/reports.md --- 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.