# Service difficulty reports: N511PE, cancelled May 31, 2017

A list on [N511PE, cancelled May 31, 2017](https://openairdocs.org/deregistered/N511PE-2017-05-31.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 3 · 101 reports

- [SDR C7WA200500125](https://openairdocs.org/sdr/C7WA200500125.md): Indicator · intermittent · Dec 21, 2005 · N511PE · Boeing 727232 · Trailing Flap Position Indicating System
  > AIR RETURN. IB FLAP STUCK AT 15 DEGREES, AFTER TAKEOFF. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW MM. FLAP SYS OPERATIONAL CHECKS GOOD. (K)
- [SDR C7W2006F00000](https://openairdocs.org/sdr/C7W2006F00000.md): Indicator · intermittent · Dec 21, 2005 · N511PE · Boeing 727232 · Trailing Flap Position Indicating System
  > AIR RETURN. IB FLAP STUCK AT 15 DEGREES AFTER TAKEOFF. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW MM. FLAP SYS OPERATIONAL CHECKS GOOD.
- [SDR C7WA200400074](https://openairdocs.org/sdr/C7WA200400074.md): Engine · damaged · Jan 11, 2005 · N511PE · Boeing 727232 · Engine (Turbine/Turboprop)
  > NR 3 THROTTLE VIBRATION FELT INFLIGHT ALL OTHER ENGINE INSTRUMENT AND INDICATIONS NORMAL, REF LOGPAGE NR 21307. C1, C2, AND C3 DAMAGE FOUND, NR 3 ENGINE REPLACED, S/N OF INSTALLED ENGINE IS 654920. (M)
- [SDR C7WA200400032](https://openairdocs.org/sdr/C7WA200400032.md): Skin · dented · Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND LEFT FUSELAGE SKIN DENTED FS 380 STRINGER 26 RT. INSTALLED EXTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)
- [SDR C7WA200400019](https://openairdocs.org/sdr/C7WA200400019.md): Skin · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Wing, Plate/Skin
  > FOUND WING CENTER SECTION UPPER SKIN CORRODED RBL 50 BETWEEN STATION 848 AND 870. INSTALLED INTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)
- [SDR C7WA200400020](https://openairdocs.org/sdr/C7WA200400020.md): Skin · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Wing, Plate/Skin
  > FOUND WING CENTER SECTION UPPER SKIN CORRODED LBL 50 BETWEEN STATION 848 AND 870. INSTALLED INTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)
- [SDR C7WA200400017](https://openairdocs.org/sdr/C7WA200400017.md): Hinge · cracked · Jun 9, 2004 · N511PE · Boeing 727232 · Cargo/Baggage Doors
  > FOUND MAIN CARGO DOOR UPPER AFT HINGE SECITON CRACKED. REMOVED AND REPLACED UPPER AFT HINGE SECTION PER AEI SERVICE BULLETIN AE01-01 AND AE MM CHAPTER 52 PAGE 15. (M)
- [SDR C7WA200400018](https://openairdocs.org/sdr/C7WA200400018.md): Stringer · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 28 RIGHT STATION 1050 EVIDENCE OF CORROSION. INSTALLED EXTERNAL SKIN REPAIR IAW 727 SRM 53-30-3 FIGURE 3. (M)
- [SDR C7WA200400021](https://openairdocs.org/sdr/C7WA200400021.md): Frame · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Frame
  > FOUND AFT CARGO COMPARTMENT FUSELAGE FRAME CORRODED STAITON 1148 STRINGER 25 RIGHT. INSTALLED INTERNAL FRAME REPAIR IAW 727 SRM 51-20-1 AND 51-30-2. (M)
- [SDR C7WA200400022](https://openairdocs.org/sdr/C7WA200400022.md): Stringer · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND AFT CARGO COMPARTMENT STRINGER 27 RIGHT STATION 950E HAS LIGHT CORROSION. INSTALLED STRINGER REPAIR IAW 727 SRM 51-40-4 FIGURE 3. (M)
- [SDR C7WA200400023](https://openairdocs.org/sdr/C7WA200400023.md): Stringer · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND FORWARD CARGO COMPARTMENT STRINGER 27 RIGHT STATION 720E CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)
- [SDR C7WA200400024](https://openairdocs.org/sdr/C7WA200400024.md): Stringer · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND FORWARD CARGO COMPARTMENT STRINGER 27 RIGHT STATION 700 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE. (M)
- [SDR C7WA200400025](https://openairdocs.org/sdr/C7WA200400025.md): Stringer · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND E/E COMPARTMENT STRINGER 28 LEFT STATION 720C CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-4 FIGURE 13. (M)
- [SDR C7WA200400026](https://openairdocs.org/sdr/C7WA200400026.md): Stringer · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND E/E COMPARTMENT STRINGER 27 LEFT STATION 450 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)
- [SDR C7WA200400027](https://openairdocs.org/sdr/C7WA200400027.md): Stringer · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND E/E COMPARTMENT STRINGER 20 RIGHT STATION 460 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)
- [SDR C7WA200400028](https://openairdocs.org/sdr/C7WA200400028.md): Skin · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Wing, Center Box
  > FOUND WING CENTER SECTION UPPER SKIN CORRODED FS 825.95 RBL 50. INSTALLED REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)
- [SDR C7WA200400029](https://openairdocs.org/sdr/C7WA200400029.md): Stringer · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND E/E COMPARTMENT STRINGER 28 RIGHT STATION 480 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)
- [SDR C7WA200400030](https://openairdocs.org/sdr/C7WA200400030.md): Frame · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Frame
  > FOUND FUSELAGE FRAME UPPER CHORD CORRODED BS 950E AT STRINGER 27 RT. INSTALLED FRAME REPAIR IAW 727 SRM 53-10-4 FIGURE 2. (M)
- [SDR C7WA200400031](https://openairdocs.org/sdr/C7WA200400031.md): Stringer · corroded · Jun 9, 2004 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > E/E COMPARTMENT STRINGER 26 RIGHT STATION 480 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)
- [SDR C7WA200200034](https://openairdocs.org/sdr/C7WA200200034.md): Oil Cooler · faulty · Oct 22, 2002 · N511PE · Boeing 727232 · Engine Fuel/Oil Cooler
  > AFTER TAEKOFF, NR 1 ENGINE OIL TEMPERATURE WENT INTO YELLOW ARC (APPROX 126) AND STAYED THERE. HIGH OIL TEMP ABNORMAL CHECKLIST ACCOMPLISHED. AFTER 15 MINUTES OF OIL TEMPERATURE IN YELLOW BAND PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED AS PER CHECKLIST. HIG
- [SDR C7WA200200033](https://openairdocs.org/sdr/C7WA200200033.md): Ground Wire · loose · Oct 22, 2002 · N511PE · Boeing 727232 · Air Conditioning System Wiring
  > CLIMBING THROUGH FL195 FOR FL280 CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE WAS AT 10.5. EMERGENCY DESCENT INITIATED AS PRESSURE COULD NOT BE MAINTAINED IN STANDBY, ONLY IN MANUAL DC. CABIN REACHED 12 BEFORE PRESSURE COULD BE CONTROLLED MARGINALLY
- [SDR C7WA200200032](https://openairdocs.org/sdr/C7WA200200032.md): Position Switch · failed · Oct 19, 2002 · N511PE · Boeing 727232 · Leading Edge Slat Position Indicating System
  > FLT 41 - DURING TAKEOFF AT 80 KNOTS, THE FORWARD LEADING EDGE INTRANSIT LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. REMOVED AND REPLACED NR 8 LEADING EDGE SLAT POSITION SWITCH IAW MM 27-81-11. OPS CHECK GOOD. (M)
- [SDR COOSDR020218](https://openairdocs.org/sdr/COOSDR020218.md): Skin · delaminated · Aug 1, 2002 · N511PE · Boeing 727232 · Landing Gear Doors
  > NOSE LANDING GEAR LEFT AFT DOOR DELAMINATED SKIN.
- [SDR COOSDR020217](https://openairdocs.org/sdr/COOSDR020217.md): Skin · delaminated · Aug 1, 2002 · N511PE · Boeing 727232 · Ailerons
  > LEFT WING OUTBOARD AILERON TRAILING EDGE DELAMINATED.
- [SDR COOSDR020216](https://openairdocs.org/sdr/COOSDR020216.md): Bulkhead · cracked · Aug 1, 2002 · N511PE · Boeing 727232 · Fuselage Main, Bulkhead
  > AFT CARGO COMPARTMENT PRESSURE BULKHEAD, CRACKED.
- [SDR COOSDR020221](https://openairdocs.org/sdr/COOSDR020221.md): Flap Track · broken · Aug 1, 2002 · N511PE · Boeing 727232 · Trailing Edge Flaps
  > RT WING, INBOARD FLAP, NR 5 MOVABLE FAIRING INBOARD FAIRING TRACK, BROKEN.
- [SDR C7WA200200005](https://openairdocs.org/sdr/C7WA200200005.md): Skin · dented · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE BS 310 BETWEEN STRINGER 23R AND 24R SKIN WITH DENT OUT OF LIMITS. REPAIRED FUSELAGE SKIN SECTION FROM BS 312.5 TO BS 308 BETWEEN STRINGER 23R AND 24R IAW SRM 53-30-3 FIG 13. (M)
- [SDR C7WA200200004](https://openairdocs.org/sdr/C7WA200200004.md): Skin · dented · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE BS 40 BETWEEN STRINGER 19R AND 20R SKIN WITH DENT OUT OF LIMITS. INSTALLED REPAIR IAW SRM 53-30-3 FIG 13. (M)
- [SDR C7WA200200027](https://openairdocs.org/sdr/C7WA200200027.md): Skin Panel · delaminated · Jul 13, 2002 · N511PE · Boeing 727232 · Ailerons
  > DURING C-CHECK INSPECTION, FOUND LT WING OUTBOARD AILERON TRAILING EDGE PANEL DELAMINATED. REPAIRED LEFT WING OUTBOARD AILERON IAW COOPESA EO COO0CMP-2-57-366-02 WITH DER APPROVAL. (M)
- [SDR C7WA200200026](https://openairdocs.org/sdr/C7WA200200026.md): Skin · delaminated · Jul 13, 2002 · N511PE · Boeing 727232 · Landing Gear Doors
  > DURING C-CHECK INSPECTION AT, FOUND NLG LEFT AFT DOOR DELAMINATED. REPAIRED DELAMINATION IAW COOPESA EO COO-CMP-2-52-369-02 WITH DER APPROVAL. (M)
- [SDR C7WA200200025](https://openairdocs.org/sdr/C7WA200200025.md): Skin · cracked · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN CRACK AT BS 196.5 WL 217. REPAIRED FUSELAGE SKIN FROM BS 191.5 TO BS 203.0 BETWEEN WL 212.5 AND WL 222.5 LBL 38.0 IAW S/B 727-53-0183 SECTION III PART I PARA C. (M)
- [SDR C7WA200200024](https://openairdocs.org/sdr/C7WA200200024.md): Skin · cracked · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 203.8 BETWEEN RIGHT WL 219 AND WL 220. REPAIRED FUSELAGE SKIN FROM BS 191.0 TO BS 209.0 BETWEEN WL 214 AND 224.5 RBL 38.0 IAW S/B 727-53-0183 SECTION III PART I PARA C. (M)
- [SDR C7WA200200022](https://openairdocs.org/sdr/C7WA200200022.md): Skin · cracked · Jul 13, 2002 · N511PE · Boeing 727232 · Passenger/Crew Doors
  > DURING C-CHECK INSPECTION, FOUND FORWARD ENTRY DOOR OUTER SKIN UPPER HINGE AREA CRACKED. REPAIRED FORWARD ENTRY DOOR SKIN FROM BS 325 TO BS 316 UPPER HINGE CUTOUT IAW SRM 52-00-3 FIG 4. (M)
- [SDR C7WA200200023](https://openairdocs.org/sdr/C7WA200200023.md): Skin · corroded · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND EXT FUSELAGE SKIN BULGED AT BS 950F PLUS 10.0 AT STRINGER 4R. REPAIRED FUSELAGE SKIN LEVEL 2 CORROSION FROM BS 950F PLUS 8.00 TO BS 950F PLUS 19.5 BETWEEN STRINGER 3R AND STRINGER 5R IAW SRM 53-30-3 FIG 14 DETAIL IV. (M)
- [SDR C7WA200200021](https://openairdocs.org/sdr/C7WA200200021.md): Skin · dented · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENT AT BS 360 BETWEEN STRINGER 16L AND 17L. REPAIRED FUSELAGE SKIN FROM BS 360 TO BS 371.50 BETWEEN STRINGER 16L AND STRINGER 21L IAW SRM 53-30-4 FIG 12. (M)
- [SDR C7WA200200020](https://openairdocs.org/sdr/C7WA200200020.md): Skin · dented · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND DENT AT BS 421 BETWEEN STRINGER 16R AND 17R. REPAIRED FUSELAGE SKIN FROM BS 416.25 TO BS 428 BETWEEN STRINGER 16R AND STRINGER 18R IAW SRM 53-30-3 FIG 3. (M)
- [SDR C7WA200200019](https://openairdocs.org/sdr/C7WA200200019.md): Bulkhead · cracked · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Bulkhead
  > DURING C-CHECK INSPECTION, FOUND FUSELAGE BS 178 BULKHEAD WITH CRACK BETWEEN LBL 4.00 AND LBL 10.00 BETWEEN WL 232.T AND WL 238.5. REPAIRED CRACKED WEB IAW SRM 53-10-9 FIG 4. (M)
- [SDR C7WA200200018](https://openairdocs.org/sdr/C7WA200200018.md): Stringer · corroded · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FS STRINGER 26L BETWEEN BS 480 AND BS 720D. REPAIRED FUSELAGE STRINGER 26L FROM BS 480 TO BS 680 IAW SRM 53-10-3 FIG 1. (M)
- [SDR C7WA200200017](https://openairdocs.org/sdr/C7WA200200017.md): Stringer · corroded · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 25R BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 25R FROM BS 720D PLUS 5.00 TO BS 740 IAW SRM 53-10-3 FIG 3. (M)
- [SDR C7WA200200016](https://openairdocs.org/sdr/C7WA200200016.md): Stringer · corroded · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 22R BETWEEN BS 720 AND BS 740. REPAIRED FUSELAGE STRINGER 22R BETWEEN BS 720E PLUS 1.50 TO BS 740 IAW SRM 53-10-3 FIG 1. (M)
- [SDR C7WA200200015](https://openairdocs.org/sdr/C7WA200200015.md): Stringer · corroded · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK INSPECTION AT COOPESA-SJO, FOUND LEVEL 2 CORROSION ON STRINGER 21R BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 21R BETWEEN BS 720E PLUS 4.00 TO BS 740 IAW SRM 53-10-3 FIG 1. (M)
- [SDR C7WA200200014](https://openairdocs.org/sdr/C7WA200200014.md): Stringer · corroded · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FUSELAGE STRINGER 25L BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 25L BETWEEN BS 720E PLUS 5.00 AND BS 740 IAW SRM 53-10-3 FIG 3. (M)
- [SDR C7WA200200013](https://openairdocs.org/sdr/C7WA200200013.md): Stringer · corroded · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 22L BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 22L FROM BS 720E PLUS 4.00 TO BS 740 IAW SRM 53-10-3 FIG 1. (M)
- [SDR C7WA200200012](https://openairdocs.org/sdr/C7WA200200012.md): Stringer · corroded · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION STRINGER 21L BETWEEN BS 720 AND 740. REPAIRED FUSELAGE STRINGER 21L FROM BS 720E PLUS 3 TO BS 740 IAW SRM 53-10-3 FIG 1. (M)
- [SDR C7WA200200011](https://openairdocs.org/sdr/C7WA200200011.md): Stringer · corroded · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 29R FROM BS 480 TO BS 540. REPLACED STRINGER 29R SECTION BETWEEN BS 480 AND BS 545 IAW SRM 51-30-2. (M)
- [SDR C7WA200200010](https://openairdocs.org/sdr/C7WA200200010.md): Frame · corroded · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Frame
  > DURING C-CHECK INSPECTION, FOUND FUSELAGE FRAME AT BS 1110 WITH LEVEL 2 CORROSION AND HOLE DAMAGED IN UPPER SECTION BETWEEN STRINGER 27L AND STRINGER 29L. REPAIRED FUSELAGE FRAME UPPER SECTION AT BS 1110 BETWEEN STRINGER 25L AND 27L IAW SRM 51-40-3. (M)
- [SDR C7WA200200006](https://openairdocs.org/sdr/C7WA200200006.md): Skin · canning · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN BS 469 TO 458 BETWEEN STRINGER 21R AND 23R OIL CANNED. REPAIRED WITH DOUBLER AND FILLER IAW SRM 53-30-4 FIG 4. (M)
- [SDR C7WA200200009](https://openairdocs.org/sdr/C7WA200200009.md): Bulkhead · cracked · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Bulkhead
  > DURING C-CHECK INSPECTION, FOUND AFT AFT PRESSURE BULKHEAD BS 1183 WITH 1.5 INCH CRACK AT WL 188.31 LBL 13. REPAIRED BS 1183 WEB WITH DOUBLERS LBL 9.5 TO LBL 22 BETWEEN WL 181.5 AND WL 193.5 IAW COOPESA EO COO-2-53-345-02. (M)
- [SDR C7WA200200008](https://openairdocs.org/sdr/C7WA200200008.md): Skin · corroded · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN BULGED FROM BS 344 TO BS 360 BETWEEN STRINGER 19R AND 24R. REPAIRED FUSELAGE SKIN FROM BS 337.5 TO BS 360 BETWEEN STRINGER 19R AND 24R IAW SRM 53-30-4 FIG 12 WITH DOUBLER TO REMOVED LEVEL 2 CORROSION. (
- [SDR C7WA200200007](https://openairdocs.org/sdr/C7WA200200007.md): Stringer · corroded · Jul 13, 2002 · N511PE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK INSPECTION, FOUND EXT FUSELAGE BETWEEN BS 440 AND BS 450 AT STRINGER 23R SKIN BULGED. REPAIRED STRINGER 23R FROM BS 440 TO BS 473 DUE TO LEVEL 2 CORROSION IAW SRM 53-10-3 FIG 1. FUSELAGE SKIN FOUND SATISFACTORY. (M)

Next page: https://openairdocs.org/deregistered/N511PE-2017-05-31/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 = 'N511PE' AND deregistration_id = 'N511PE-2017-05-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N511PE-2017-05-31/reports

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