# Service difficulty reports: N743DH, cancelled Mar 8, 2010

A list on [N743DH, cancelled Mar 8, 2010](https://openairdocs.org/deregistered/N743DH-2010-03-08.md).

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

Page 1 of 6 · 299 reports

- [SDR DHLA2009743DH665](https://openairdocs.org/sdr/DHLA2009743DH665.md): Stringer · corroded · Feb 10, 2009 · N743DH · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > 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.md): Frame · corroded · Jan 19, 2009 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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 B727 SRM 53-10-4 FIG 13 AND REPLACED SHEAR TIE P/N 69-13293-3 IAW B727 SRM 51-10-1 PARA 7A.
- [SDR DHLA2009743543](https://openairdocs.org/sdr/DHLA2009743543.md): Seat Track · corroded · Jan 19, 2009 · N743DH · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Floorbeam · corroded · Jan 18, 2009 · N743DH · Boeing 727225 · Fuselage Main, Floor Beam
  > 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.md): Floorbeam · damaged · Jan 18, 2009 · N743DH · Boeing 727225 · Fuselage Main, Floor Beam
  > 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 12/24/08 AND ASTAR EVA B253-00205 FOR REPAIR APPROVAL.
- [SDR DHLA2009743541](https://openairdocs.org/sdr/DHLA2009743541.md): Angle · cracked · Jan 6, 2009 · N743DH · Boeing 727225 · Trailing Edge Flaps
  > 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.md): Strap · corroded · Jan 6, 2009 · N743DH · Boeing 727225 · Fuselage Miscellaneous Structure
  > 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.md): Frame · damaged · Jan 5, 2009 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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 51-40-3 FIG 1.
- [SDR DHLA2009743535](https://openairdocs.org/sdr/DHLA2009743535.md): Frame · damaged · Dec 29, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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, AND 51-10-1.
- [SDR DHLA2009743533](https://openairdocs.org/sdr/DHLA2009743533.md): Skin · dented · Dec 29, 2008 · N743DH · Boeing 727225 · Fuselage Main, Plate/Skin
  > 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.md): Attach Fitting · cracked · Dec 22, 2008 · N743DH · Boeing 727225 · Wing, Attach Fittings
  > 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 FASTENERS, BOLTS IAW B727 SRM 51-30-2 PARA 4B, PARA 7D AND PARA 9B.
- [SDR DHLA2009743548](https://openairdocs.org/sdr/DHLA2009743548.md): Frame · dented · Dec 22, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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.md): Floorbeam · damaged · Dec 18, 2008 · N743DH · Boeing 727225 · Fuselage Main, Floor Beam
  > 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 COOPESA EO COO-2-53-502-08 DTD 12/24/08 DOCUMENTED ON FAA FORM 8110-3.
- [SDR DHLA2009743DH655](https://openairdocs.org/sdr/DHLA2009743DH655.md): Floorbeam · damaged · Dec 18, 2008 · N743DH · Boeing 727225 · Fuselage Main, Floor Beam
  > 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 COO-2-53-502-08 DTD 12/24/08 DOCUMENTED ON FAA FORM 8110-3.
- [SDR DHLA2009743DH570](https://openairdocs.org/sdr/DHLA2009743DH570.md): Web · corroded · Dec 10, 2008 · N743DH · Boeing 727225 · Fuselage Miscellaneous Structure
  > 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 1154.75 BETWEEN LBL 25 AND LBL 31 AND FROM BS 1154.75 TO BS 1183 BTWN LBL 25 AND LBL 62 FOUND WITH
- [SDR DHLA2009743DH569](https://openairdocs.org/sdr/DHLA2009743DH569.md): Web · corroded · Dec 10, 2008 · N743DH · Boeing 727225 · Fuselage Miscellaneous Structure
  > 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 TO BS 1183 BETWEEN RBL 25 AND RBL 52.5 AND FROM BS 1152.5 TO BS 1183 BETWEEN RBL 52.5 AND RBL62 IA
- [SDR DHLA2009743534](https://openairdocs.org/sdr/DHLA2009743534.md): Web · corroded · Dec 5, 2008 · N743DH · Boeing 727225 · Fuselage Miscellaneous Structure
  > 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.md): Floorbeam · corroded · Dec 5, 2008 · N743DH · Boeing 727225 · Fuselage Main, Floor Beam
  > 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.md): Flap Track · corroded · Dec 3, 2008 · N743DH · Boeing 727225 · Trailing Edge Flaps
  > 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.md): Stiffener · cracked · Dec 2, 2008 · N743DH · Boeing 727225 · Fuselage Miscellaneous Structure
  > 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, DATED 01/25/96.
- [SDR DHLA2008743DH668](https://openairdocs.org/sdr/DHLA2008743DH668.md): Floorbeam · damaged · Nov 29, 2008 · N743DH · Boeing 727225 · Fuselage Main, Floor Beam
  > 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-2-53-477-08 DTD 12/18/08 DOCUMENTED ON FAA FORM 8110-3.
- [SDR DHLA2009743552](https://openairdocs.org/sdr/DHLA2009743552.md): Frame · damaged · Nov 29, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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.md): Floorbeam · damaged · Nov 28, 2008 · N743DH · Boeing 727225 · Fuselage Main, Floor Beam
  > 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 COO-2-53-467-08 DTD 12/17/08 DOCUMENTED ON FAA FORM 8110-3.
- [SDR DHLA2009743554](https://openairdocs.org/sdr/DHLA2009743554.md): Frame · damaged · Nov 27, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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 17L.
- [SDR DHLA2009743553](https://openairdocs.org/sdr/DHLA2009743553.md): Frame · damaged · Nov 27, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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.md): Keelbeam · cracked · Nov 26, 2008 · N743DH · Boeing 727225 · Fuselage Main, Keel
  > 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 PARA 7A.
- [SDR DHLA2009743546](https://openairdocs.org/sdr/DHLA2009743546.md): Frame · damaged · Nov 26, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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.md): Frame · damaged · Nov 26, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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.md): Frame · damaged · Nov 26, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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 INSTALLED PER B727 SRM 53-10-2 FIG 2, AND 51-10-1. ALSO, ACCOMPLISHED FRAME REPAIR BETWEEN STR 11R AND 14
- [SDR DHLA2009743555](https://openairdocs.org/sdr/DHLA2009743555.md): Frame · damaged · Nov 25, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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.md): Frame · dented · Nov 25, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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.md): Frame · damaged · Nov 25, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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.md): Frame · damaged · Nov 25, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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.md): Frame · dented · Nov 25, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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.md): Frame · dented · Nov 25, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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.md): Stringer · corroded · Nov 25, 2008 · N743DH · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · corroded · Nov 24, 2008 · N743DH · Boeing 727225 · Fuselage Main, Longeron/Stringer
  > 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 53-10-3 FIG 1.
- [SDR DHLA2009743545](https://openairdocs.org/sdr/DHLA2009743545.md): Stringer · cracked · Nov 24, 2008 · N743DH · Boeing 727225 · Vertical Stabilizer, Spar/Rib
  > 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.md): Frame · damaged · Nov 23, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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.md): Strap · cracked · Nov 23, 2008 · N743DH · Boeing 727225 · Fuselage Miscellaneous Structure
  > 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 B727 SRM 51-10-1 PARA 7A.
- [SDR DHLA2009743DH654](https://openairdocs.org/sdr/DHLA2009743DH654.md): Frame · dented · Nov 20, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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-2-53-430-08 DTD 11/24/08 DOCUMENTED ON FAA FORM 8110-3.
- [SDR DHLA2008743509](https://openairdocs.org/sdr/DHLA2008743509.md): Floorbeam · corroded · Nov 20, 2008 · N743DH · Boeing 727225 · Fuselage Main, Floor Beam
  > 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 TO CORROSION IAW SRM 51-10-1 PARA 7A.
- [SDR DHLA2008743524](https://openairdocs.org/sdr/DHLA2008743524.md): Frame · damaged · Nov 18, 2008 · N743DH · Boeing 727225 · Fuselage Main, Frame
  > 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.md): Skin Panel · damaged · Nov 17, 2008 · N743DH · Boeing 727225 · Fuselage Main, Plate/Skin
  > 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" BTWN S-25L AND S-28L IAW EO COO-2-53-496-08 DTD 12/24/08 DOCUMENTED ON FAA FORM 8110-3.
- [SDR DHLA2008743506](https://openairdocs.org/sdr/DHLA2008743506.md): Floorbeam · corroded · Nov 17, 2008 · N743DH · Boeing 727225 · Fuselage Main, Floor Beam
  > 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 51-10-1 PARA 7.
- [SDR DHLA2009743DH663](https://openairdocs.org/sdr/DHLA2009743DH663.md): Beam · corroded · Nov 15, 2008 · N743DH · Boeing 727225 · Wing, Landing Gear Attach Fittings
  > 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 DUE TO CORROSION IAW EO C00-2-57-436-08 DTD 11/28/08 AND MESSAGE NR 1-1087194336-2 DTD 11/26/08 DOC
- [SDR DHLA2009743DH686](https://openairdocs.org/sdr/DHLA2009743DH686.md): Channel · cracked · Nov 14, 2008 · N743DH · Boeing 727225 · Cargo/Baggage Doors
  > 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 ON MAIN CARGO DOOR DUE TO CRACK IAW B727 SRM 51-10-1 PARA 7A.
- [SDR DHLA2009743DH645](https://openairdocs.org/sdr/DHLA2009743DH645.md): Floorbeam · damaged · Nov 14, 2008 · N743DH · Boeing 727225 · Fuselage Main, Floor Beam
  > 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 12/04/08 DOCUMENTED ON FAA FORM 8110-3.
- [SDR DHLA2009743DH644](https://openairdocs.org/sdr/DHLA2009743DH644.md): Floorbeam · damaged · Nov 14, 2008 · N743DH · Boeing 727225 · Fuselage Main, Floor Beam
  > 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 COOPESA EO COO-2-53-435-08 DTD 12/04/08 DOCUMENTED ON FAA FORM 8110-3.
- [SDR DHLA2009743DH636](https://openairdocs.org/sdr/DHLA2009743DH636.md): Door Frame · cracked · Nov 14, 2008 · N743DH · Boeing 727225 · Cargo/Baggage Doors
  > 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 MAIN CARGO DOOR FRAME SECT AT BS 598 UPPER JAMB HINGE AREA IAW COOPESA EO COO-2-52-424-08 DTD 11/2

Next page: https://openairdocs.org/deregistered/N743DH-2010-03-08/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N743DH' AND deregistration_id = 'N743DH-2010-03-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N743DH-2010-03-08/reports

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