# Service difficulty reports: Boeing 727-2B7

A list on [Boeing 727-2B7](https://openairdocs.org/model/boeing-727-2b7.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 290 reports

- [SDR FDEA201008233107](https://openairdocs.org/sdr/FDEA201008233107.md): Frame · gouged · Aug 23, 2010 · N494FE · Boeing 7272B7 · Fuselage Main, Frame
  > MAIN CARGO DOOR FWD FRAME INNER SKIN IS GOUGED IN NUMEROUS PLACES BS 480. REMOVED DAMAGED FWD INNER SKIN, FABRICATED NEW INNER SKIN & INSTALLED NEW SKIN AT CUTOUT FWD IAW SRM 51-30-5, SRM 51-30-2, & DWG NR 53FX1551.
- [SDR EE4Y10351](https://openairdocs.org/sdr/EE4Y10351.md): Floorbeam · corroded · Aug 18, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, Floor Beam
  > DURING INSP, LOWER FUSELAGE AFT CARGO COMPARTMENT STA 1130 FLOORBEAM UPPER CHORD CORRODED.
- [SDR EE4Y1010347](https://openairdocs.org/sdr/EE4Y1010347.md): Skin · dented · Aug 17, 2010 · N762AT · Boeing 7272B7 · Ailerons
  > RIGHT WING OTBD AILERON, LOWER SURFACE WITH DENT AND BULGED SKIN.
- [SDR EE4Y1010346](https://openairdocs.org/sdr/EE4Y1010346.md): Stringer · cracked · Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > (EE4Y) EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, ST STA 157 STR 7L CRACKED.
- [SDR EE4Y1010345](https://openairdocs.org/sdr/EE4Y1010345.md): Stringer · cracked · Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > EMPENNAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 8R AT STA 180 CRACKED.
- [SDR EE4Y1010344](https://openairdocs.org/sdr/EE4Y1010344.md): Stringer · cracked · Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 6L CRACKED AT STA 180.
- [SDR EE4Y1010343](https://openairdocs.org/sdr/EE4Y1010343.md): Stringer · cracked · Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY,STR 5L AT STA 22.5 AND STA 157 WITH CRACK.
- [SDR EE4Y1010342](https://openairdocs.org/sdr/EE4Y1010342.md): Stringer · cracked · Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > EMPENAGE VERTICAL STABILIZER CAVITY,STR 9L CRACKED AT STA 110.
- [SDR EE4Y1010341](https://openairdocs.org/sdr/EE4Y1010341.md): Stringer · cracked · Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 8L CRACKED AT STA 157, STA 133 AND STA 22.5.
- [SDR EE4Y1010329](https://openairdocs.org/sdr/EE4Y1010329.md): Keelbeam · corroded · Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, Keel
  > LOWER FUSELAGE AFT CARGO COMPARTMENT FROM 950D TO STA 1000, KEEL BEAM LT CORRODED.
- [SDR EE4Y1010328](https://openairdocs.org/sdr/EE4Y1010328.md): Cover · corroded · Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, Structure
  > LOWER FUSELAGE, RAM AIR DOOR INLET AREA, VERTICAL FIXED COVER WITH CORROSION.
- [SDR EE4Y1010327](https://openairdocs.org/sdr/EE4Y1010327.md): Floor Support · corroded · Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous Structure
  > MAIN CARGO CABIN FLOOR SUPPORT CHANNEL CORRODED AT BS 1145, LBL 12.
- [SDR EE4Y1010326](https://openairdocs.org/sdr/EE4Y1010326.md): Keelbeam · corroded · Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, Keel
  > LOWER FUSELAGE AFT CARGO COMPARTMENT FROM BS 950A TO BS 989, KEEL BEAM RT WITH CORROSION.
- [SDR EE4Y1010325](https://openairdocs.org/sdr/EE4Y1010325.md): Skin Panel · cracked · Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN WITH CRACK AT BS 243, WL 178, LT SIDE.
- [SDR DHLA2009770AT526](https://openairdocs.org/sdr/DHLA2009770AT526.md): Frame · worn · Jan 6, 2009 · N770AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > EMPENNAGE VERTICAL STABILIZER ACTUATOR RT ACCESS PANEL FRAME "T" SHAPE SUPPORT WORN AND LOOSE. REPAIRED VERTICAL STABILIZER MID SPAR CHORD RIGHT SIDE FROM FIN STA 222 TO FIN STA 235 IAW B727 SRM 55-30-6 FIG 3
- [SDR DHLA2009770AT521](https://openairdocs.org/sdr/DHLA2009770AT521.md): Stringer · corroded · Dec 19, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/Stringer
  > LWR FUSELAGE FWD CARGO COMPARTMENT S-28R WITH CORROSION AT BS 488. REPAIRED S-28R SECTION BETWEEN BS 480 TO BS 516.5 IAW SRM 53-10-3 FIG 1. REPLACED S-28R SECTION FROM BS 450 TO BS 480 IAW SRM 51-10-1 PARA 7A AND 53-10-3 FIG 1.
- [SDR DHLA2009770AT517](https://openairdocs.org/sdr/DHLA2009770AT517.md): Support Channel · corroded · Dec 19, 2008 · N770AT · Boeing 7272B7 · Fuselage Miscellaneous Structure
  > REF N/R 1-306 LOWER FUSELAGE INTERIOR FWD NOSE COMPARTMENT, LOWER CHORD AND SUPPORT CHANNEL WITH CORROSION AT BS 227.8 LBL2. REPAIRED FUSELAGE FWD NOSE COMPT LOWER CHORD SECTION AT BS 227.8 BTWN LBL 5.5 AND RBL 6 IAW SRM 51-40-4 FIG 1.
- [SDR DHLA2009770AT508](https://openairdocs.org/sdr/DHLA2009770AT508.md): Frame · dented · Dec 19, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Frame
  > UPPER FUSELAGE CARGO CABIN FRAME WITH DENT AT BS 580 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION BS 580 BTWN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1.
- [SDR DHLA2009770AT524](https://openairdocs.org/sdr/DHLA2009770AT524.md): Skin Panel · corroded · Dec 18, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE FWD CARGO COMPARTMENT SKIN WITH CORROSION FROM BS 486 TO BS 494 BETWEEN S-27R AND S28R. REPAIRED FUSELAGE SKIN SECTION FROM BS 481 TO BS 496.5 BETWEEN BL 0 AND S27R IAW EO-COO-2-53-500-08 DTD 12/23/08 DOCUMENTED OF FAA FORM 8110-3. DTA WITHIN
- [SDR DHLA2009770AT520](https://openairdocs.org/sdr/DHLA2009770AT520.md): Seat Track · corroded · Dec 18, 2008 · N770AT · Boeing 7272B7 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE MAIN CARGO CABIN SEAT TRACK WITH CORROSION FROM BS 480 TO BS 620 RBL 45.5 OTBD FLANGE. REPLACED SEAT TRACK FROM BS 480 TO BS 690 RBL 45.5 IAW SRM 51-10-1 PARA 7A AND IAW RIGID BARRIER INSTALLATION PARA 5.4.
- [SDR DHLA2009770AT510](https://openairdocs.org/sdr/DHLA2009770AT510.md): Frame · dented · Dec 18, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Frame
  > UPPER FUSELAGE CARGO CABIN FRAME WITH DENT AT BS 640 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION BS 640 BETWEEN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1.
- [SDR DHLA2009770AT504](https://openairdocs.org/sdr/DHLA2009770AT504.md): Frame · dented · Dec 18, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Frame
  > UPPER FUSELAGE CARGO CABIN FRAME WITH DENT AT BS 520 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION AT BS 520 BTWN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1.
- [SDR DHLA2009770503](https://openairdocs.org/sdr/DHLA2009770503.md): Frame · dented · Dec 18, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Frame
  > UPPER FUSELAGE CARGO CABIN FRAME WITH DENT AT BS 540 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION BS 540 BETWEEN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1.
- [SDR DHLA2009770502](https://openairdocs.org/sdr/DHLA2009770502.md): Frame · dented · Dec 18, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Frame
  > UPPER FUSELAGE CARGO CABIN FRAME WITH DENT BS 600 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION BS 600 BETWEEN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1.
- [SDR DHLA2009770AT514](https://openairdocs.org/sdr/DHLA2009770AT514.md): Floorbeam · corroded · Dec 13, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Floor Beam
  > LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 1130 RBL 45 FLOORBEAM LOWER FWD FLANGE WITH CORROSION. REPAIRED FUSELAGE FLOORBEAM LOWER CHORD SECTION BS 1130 BETWEEN RBL 20 AND RBL 56.5 IAW B727 SRM 53-10-8 FIG 10 DETAIL V.
- [SDR DHLA2009770AT523](https://openairdocs.org/sdr/DHLA2009770AT523.md): Frame · cracked · Dec 12, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Frame
  > LWR FUSELAGE FWD CARGO COMPARTMENT DOOR CUTOUT BS 560 AT STOP FITTING NR 1 WEB WITH CRACK. REPAIRED FRAME WEB SECTION AT BS 560 BETWEEN S-17R AND S-22R IAW SRM 51-40-2 FIG 1.
- [SDR DHLA2009770AT522](https://openairdocs.org/sdr/DHLA2009770AT522.md): Frame · cracked · Dec 12, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Frame
  > LWR FUSELAGE FWD CARGO COMPARTMENT DOOR CUTOUT BS 620 AT STOP FITTING NR 1 WEB WITH CRACK. REPAIRED FUSELAGE FRAME WEB SECTION AT BS 620 BETWEEN S-18R AND S-22R IAW B727 SRM 51-40-2 FIG 1.
- [SDR DHLA2009770AT516](https://openairdocs.org/sdr/DHLA2009770AT516.md): Stringer · corroded · Dec 12, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/Stringer
  > REF N/R 1-279 LWR FUSELAGE AFT CARGO COMPARTMENT AT BS 1010 S-29R WITH CORROSION. REPAIRED FUSELAGE S-29R SECTION FROM BS 1010 TO BS 1045 IAW SRM 53-10-3 FIG 1 DETAIL 1.
- [SDR DHLA2009770AT507](https://openairdocs.org/sdr/DHLA2009770AT507.md): Stringer · corroded · Dec 12, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/Stringer
  > LOWER FUSELAGE FWD CARGO COMPARTMENT BS 727E STRINGER END S-27R CORRODED. REPAIRED FUSELAGE S-27R SECTION FROM BS 727E TO BS 740 IAW B727 SRM 53-10-3 FIG 1 DETAIL 1.
- [SDR DHLA2009770AT506](https://openairdocs.org/sdr/DHLA2009770AT506.md): Web · dented · Dec 12, 2008 · N770AT · Boeing 7272B7 · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE NOSE W/W WEB DENTED AT BS 323 WL 181 BL 0. REPAIRED NOSE W/W WEB FROM BS 320 TO BS 325.5 BETWEEN LBL4 AND RBL 5 IAW B727 SRM 51-40-2 FIG 1.
- [SDR DHLA2009770AT512](https://openairdocs.org/sdr/DHLA2009770AT512.md): Shear Tie · corroded · Dec 11, 2008 · N770AT · Boeing 7272B7 · Fuselage Internal Mounting Structure
  > LOWER FUSELAGE AFT CARGO COMPARTMENT BS 1050 BETWEEN S-26L AND S-27L SHEARTIE WITH CORROSION. REPLACED FUSELAGE SHEARTIE SECTION AT BS 1050 BETWEEN S-26L AND S-27L.
- [SDR DHLA2009770AT509](https://openairdocs.org/sdr/DHLA2009770AT509.md): Strap · cracked · Dec 11, 2008 · N770AT · Boeing 7272B7 · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE STABILIZER STRAP WITH CRACK AT BS 344 LBL 23 WL 201. REPAIRED STABILIZER STRAP FROM BS 324.5 TO BS 347.5 AT LBL 23 IAW B727 SRM 53-10-8 FIG 6.
- [SDR DHLA2009770AT505](https://openairdocs.org/sdr/DHLA2009770AT505.md): Frame · damaged · Dec 11, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Frame
  > UPPER FUSELAGE CARGO CABIN FRAME WITH DOUBLE HOLE AT BS 1090 BETWEEN S-16L AND S-17L. REPAIRED FUSELAGE FRAME SECTION AT BS 1090 BETWEEN S-16L AND S-17L IAW B727 SRM 51-40-3 FIG 1.
- [SDR DHLA2009770AT501](https://openairdocs.org/sdr/DHLA2009770AT501.md): Failsafe · corroded · Dec 11, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Frame
  > UPPER FUSELAGE CARGO CABIN FRAME FAIL SAFE CHORD WITH CORROSION AT BS 1166 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME FAIL SAFE CHORD SECTION AT BS 1166 BETWEEN S-16R AND S-18R DUE TO CORROSION IAW B727 SRM 51-40-3 FIG 1.
- [SDR DHLA2009770AT530](https://openairdocs.org/sdr/DHLA2009770AT530.md): Keelbeam · cracked · Dec 10, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Keel
  > LOWER FUSELAGE AIR CONDITIONING BAY AT BS 740 KEEL BEAM LOWER LEFT CHORD WITH CRACK. REPAIRED FUSELAGE LEFT SIDE KEEL BEAM LOWER CHORD AT HORIZONTAL FLANGE SECTION FROM BS 740 TO BS 748 LBL 7 IAW COOPESA EO-COO-2-53-503-08 DTD 12/24/08 AND BOEING MESSAGE 1-11
- [SDR DHLA 2009770AT527](https://openairdocs.org/sdr/DHLA%202009770AT527.md): Skin Panel · cracked · Dec 9, 2008 · N770AT · Boeing 7272B7 · Wing, Plate/Skin
  > RIGHT WING FRONT SPAR SECTION LEADING EDGE SKIN CRACKED AT WS 491. REPAIRED RIGHT WING FIXED LEADING EDGE SKIN SECTION FROM LE STA 151.40 TO LE STA 195.65 IAW COOPESA EO COO-2-57-461-08 DTD 12/19/08.
- [SDR DHLA2009770AT513](https://openairdocs.org/sdr/DHLA2009770AT513.md): Floorbeam · corroded · Dec 9, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Floor Beam
  > UPPER FUSELAGE CARGO CABIN AT BS 1130 BETWEEN RBL 25 AND RBL 45 FLOORBEAM UPPER AND LOWER FACE WITH CORROSION. REPAIRED FUSELAGE FLOORBEAM UPPER CHORD SECTION AT BS 1130 BETWEEN RBL 37 AND RBL 47.5 IAW B727 SRM 53-10-8 FIG 10.
- [SDR DHLA2009770AT529](https://openairdocs.org/sdr/DHLA2009770AT529.md): Frame · corroded · Dec 8, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Frame
  > LOWER FUSELAGE AT BS 740 BTWN S-27L AND S-28L FRAME WITH CORROSION. REPLACED FUSELAGE CHORD SECTION AT BS 740 BTWN S-27L AND S-28L IAW B727 SRM 51-10-1 PARA 7A.
- [SDR DHLA2009770AT528](https://openairdocs.org/sdr/DHLA2009770AT528.md): Frame · worn · Dec 8, 2008 · N770AT · Boeing 7272B7 · Vertical Stabilizer, Spar/Rib
  > EMPENNAGE VERTICAL STABILIZER ACTUATOR LT ACCESS PANEL FRAME "T" SHAPE SUPPORT WORN AND LOOSE. REPAIRED VERTICAL STABILIZER MID SPAR CHORD SECTION FROM FIN STA 222 TO FIN STA 241 IAW COOPESA EO COO-2-55-499-08 DTD 12/22/08 DOCUMENTED ON FAA FORM 8110-3.
- [SDR DHLA2009770AT525](https://openairdocs.org/sdr/DHLA2009770AT525.md): Skin Panel · corroded · Dec 8, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE FWD CARGO COMPARTMENT FROM BS 560 TO BS 570 RBL 11 WL 148 SKIN WITH CORROSION. REPAIRED FUSELAGE SKIN SECTION FROM BS 557 TO BS 579 BTWN S-26R AND S-28L IAW EO COO-2-53-474-08 DTD 12/18/08.
- [SDR DHLA2009770AT518](https://openairdocs.org/sdr/DHLA2009770AT518.md): Skin Panel · dented · Dec 8, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Plate/Skin
  > LWR FUSELAGE AT BS 509.5 BTWN S-20R AND S-21R WITH DENTS. REPAIRED FUSELAGE SKIN FROM BS 501 TO BS 512 BTWN S-19R AND S-21R IAW SRM 53-30-3 FIG 2.
- [SDR DHLA2009770AT515](https://openairdocs.org/sdr/DHLA2009770AT515.md): Skin · dented · Dec 8, 2008 · N770AT · Boeing 7272B7 · Cargo/Baggage Doors
  > LOWER FUSELAGE FWD CARGO COMPARTMENT DOOR OUTER SKIN WITH DENT AT BS 617.5 BETWEEN BEAM 2 AND BEAM 3. REPAIRED FWD CARGO COMPARTMENT DOOR OUTER SKIN SECTION AT BS 615.5 TO620 BETWEEN BEAMS 2 AND 3 IAW B727 SRM 52-00-3 FIG 3.
- [SDR DHLA2009770AT519](https://openairdocs.org/sdr/DHLA2009770AT519.md): Skin Panel · cracked · Dec 5, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE AT BS 1218.5 RBL 10.25 SKIN CRACKED. REPLACED SKIN SECTION FROM BS 1204.25 TO BS 1232.25 BTWN BL 0 AND RBL 21 IAW SRM 51-10-01 PAR 7A.
- [SDR DHLA2009770AT511](https://openairdocs.org/sdr/DHLA2009770AT511.md): Skin Panel · dented · Dec 5, 2008 · N770AT · Boeing 7272B7 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE AT BS 316 BETWEEN S-22R AND S-23R SKIN WITH DENT. REPAIRED FUSELAGE SKIN SECTION FROM BS 309.25 TO BS 323 BETWEEN S-21R AND S-24R IAW B727 SRM 53-30-3 FIG 1.
- [SDR DHLA200800132](https://openairdocs.org/sdr/DHLA200800132.md): Oil Filter · bypassing · Nov 19, 2008 · N762AT · Boeing 7272B7 · Turbine Engine Oil System
  > NR 3 OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT PRESS TO TEST CAUSED LIGHT TO BE BRIGHTER SHUT DOWN ENGINE IN ACCORDANCE WITH ABNORMAL PROCEDURES RESOLUTION: REMOVED AND REPLACED NR 3 MAIN OIL FILTER PER MM CH 79-00 OPS CHECK NORMAL. A/C WAS GROUNDED.
- [SDR DHLA200800089](https://openairdocs.org/sdr/DHLA200800089.md): Fire Warning · false activation · Aug 20, 2008 · N770AT · Boeing 7272B7 · Fire Detection
  > FLT 549 - DURING CRUISE FLIGHT AT FL360, WHEEL WELL FIRE RED LIGHT ILLUMINATED FAINTLY FOR 1 SECOND ACCOMPANIED BY 1 DING OF THE FIRE BELL. INSPECTED AND TESTED SYSTEM PER MM CH 26-12-0. NO DEFECTS FOUND. SYSTEM OP CHECKS GOOD. ACFT WAS GROUNDED.
- [SDR DHL2008F00001](https://openairdocs.org/sdr/DHL2008F00001.md): Tab · delaminated · Jun 27, 2008 · N762AT · Boeing 7272B7 · Aileron Tabs
  > A 3 X 1 INCH DELAMINATION ON RT WING O/B AILERON BALANCE TAB AT TRAILING EDGE. AILERON BALANCE TAB WAS REMOVED AND REPLACED IAW BOEING 727 MAINTENANCE MANUAL 27-10-41. OPERATION CHECK NORMAL. (A)
- [SDR DHL2008760002](https://openairdocs.org/sdr/DHL2008760002.md): Angle · corroded · May 22, 2008 · N760AT · Boeing 7272B7 · Fuselage Main, Bulkhead
  > LWR FUSELAGE AFT BULKHEAD IN FWD CARGO PIT AT STA 740 RBL 10-20 LOWER CHORD ANGLE IN BILGE AREA HAS CORROSION. REMOVED AND FAB NEW ANGLE SKIN SUPPORT MATERIAL USED 7075-0.190" PO 7220256 DIM 10.25" X 11.75" IAW B727 DWG 69-64841 IAW EC-00958-001.
- [SDR DHL2008760001](https://openairdocs.org/sdr/DHL2008760001.md): Web · cracked · May 19, 2008 · N760AT · Boeing 7272B7 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS WELL AREA, RT LWR TORQUE BOX AT STA 1223 PREVIOUS REPAIR ON WORK PLATFORM WEB IS CRACKED BEYOND STOP DRILLED HOLES. CUT-OUT DAMAGED AREA APPROX DIM 5 1/2 INCH BY 6 INCH. FAB REPAIR DOUBLER FROM 7075-T6.0.40 INCH PO NR 9006639 APPROX DIM 10 INC
- [SDR DHL2008760531](https://openairdocs.org/sdr/DHL2008760531.md): Hinge · cracked · Apr 30, 2008 · N760AT · Boeing 7272B7 · Fuselage, Door Hinge
  > REMOVED AND REPLACED CRACKED AFT HINGE SECTION, BS 620 TO 640, FOR MCD PER B727-200 FREIGHTER MM FIG 5201B AND CH 52 REV G, STOCK HINGE P/N MS20001-16-7200

Next page: https://openairdocs.org/model/boeing-727-2b7/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 aircraft_model_key = '7272B7'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-2b7/reports

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