# Service difficulty reports: N579PE, cancelled May 19, 2015

A list on [N579PE, cancelled May 19, 2015](https://openairdocs.org/deregistered/N579PE-2015-05-19.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 2 · 73 reports

- [SDR GAIA04054OP](https://openairdocs.org/sdr/GAIA04054OP.md): Switch · inoperative · Mar 17, 2004 · N579PE · Boeing 727243 · Trailing Flap Position Indicating System
  > FLT 753 - CLT-FWA - DURING TAXI, THE FLIGHT CREW NOTICED THAT THE NR 5 LEADING EDGE DEVICE WOULD NOT EXTEND. REMOVED AND REPLACED THE NR 5 LEADING EDGE FLAP POSTION SWITCH. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA04026OP](https://openairdocs.org/sdr/GAIA04026OP.md): Warning Light · illuminated · Feb 5, 2004 · N579PE · Boeing 727243 · Landing Gear System
  > AFTER TAKEOFF, THE TAIL SKID LIGHT REMAINED ILLUMINATED. RECYCLED THE LANDING GEAR AND THE LIGHT WENT OUT. PERFORMED OPERATIONAL CHECK AND TEST OF THE TAIL SKID SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M)
- [SDR GAIA02077OP](https://openairdocs.org/sdr/GAIA02077OP.md): Spoiler · out of rig · Jul 23, 2002 · N579PE · Boeing 727243 · Drag Control System
  > FLT 705 - DFW-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THE AIRCRAFT SHUDDER AT.78 MACH. THE SHUDDER STOPPED WHEN THE AIRCRAFT SLOWED TO KIAS. THE CREW ELECTED TO DIVERT TO MEM. AN UNEVENTFUL LANDING WAS MADE. THE NR 1, NR 5, NR 6, NR 10 AND NR 11 SPOI
- [SDR GAIA02018ST](https://openairdocs.org/sdr/GAIA02018ST.md): Frame · cracked · Feb 8, 2002 · N579PE · Boeing 727243 · Fuselage Main, Frame
  > DURING INSPECTION, IT WAS DISCOVERED THAT A FUSELAGE FRAME WAS CRACKED AT STATION 640. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3. (M)
- [SDR GAIA02017ST](https://openairdocs.org/sdr/GAIA02017ST.md): Frame · cracked · Feb 4, 2002 · N579PE · Boeing 727243 · Fuselage Main, Frame
  > DURING INSPECTION, IT WAS DISCOVERED THAT A FUSELAGE FRAME WAS CRACKED AT STATION 580. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3. (M)
- [SDR GAIA00109](https://openairdocs.org/sdr/GAIA00109.md): Warning Light · illuminated · Mar 17, 2000 · N579PE · Boeing 727243 · Compressor Bleed Control
  > FLT 1844 - FWA-ORF - DURING TAKEOFF, THE NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED. THE CREW DECLARED A EMERGENCY LANDING BACK AT FWA. THE CREW RAN EMERGENCY CHECKLIST AND DISCHARGED FIRE BOTTLE. DURING SHUT DOWN NR 2 ENGINE, THROTTLE DIFF
- [SDR GAIA00047](https://openairdocs.org/sdr/GAIA00047.md): Light · inoperative · Feb 1, 2000 · N579PE · Boeing 727243 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE, FOUND EMERGENCY EXIT LIGHT OVER L-1 DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)
- [SDR GAIA0012](https://openairdocs.org/sdr/GAIA0012.md): Seat Track · damaged · Jan 11, 2000 · N579PE · Boeing 727243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ALONG CABIN SEAT TRACK FROM BS 950 TO 1135 RIGHT BODY LINE 25. REPLACED SECTION OF CABIN SEAT TRACK FROM BS 950 TO 1135, RBL 25. MATERIAL USED, PART NR CAB1520-792, 185 INCH LONG. REPAIR ACCOMPLISHED IAW SRM 53-1
- [SDR GAIA0011](https://openairdocs.org/sdr/GAIA0011.md): Floorbeam · damaged · Jan 11, 2000 · N579PE · Boeing 727243 · Fuselage Main, Floor Beam
  > DURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ALONG CABIN FLOORBEAM SUPPORT BS 400, RIGHT BODY LINE 55. INSTALLED REPAIR AT CABIN FLOORBEAM SUPPORT BS 400, RBL 55. MATERIAL USED, PART NR BAC1505-100617 AND BAC1490-2831, T-ANGLE 15 INCH LONG, SUPPORT ANGLES, 1
- [SDR GAIA0010](https://openairdocs.org/sdr/GAIA0010.md): Gusset · damaged · Jan 11, 2000 · N579PE · Boeing 727243 · Fuselage Miscellaneous Structure
  > DURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ON GUSSET AT STATION 825 LEFT INNER FLANGE, LEFT BODY LINE. REPLACED GUSSET AT STATION 825 LEFT INNER FLANGE JUST ABOVE CENTER SECTION UPPER SKIN, LBL 70. MATERIAL USED, 7075-T6,.090 INCH, 5 INCH BY 3 INCH. REPA
- [SDR GAIA0009](https://openairdocs.org/sdr/GAIA0009.md): Floorbeam · damaged · Jan 11, 2000 · N579PE · Boeing 727243 · Fuselage Main, Floor Beam
  > DURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ALONG FLOORBEAM UPPER T-CAP AT STATION 344 LEFT BODY LINE 62.5 TO RT BODY LINE 62.5. REPLACED FLOORBEAM UPPER T-CAP AT STATION 344, LBL 62.5. MATERIAL USED, PART NR BAC1505-29222. REPAIR ACCOMPLISHED IAW SRM 53-1
- [SDR GAIA0008](https://openairdocs.org/sdr/GAIA0008.md): Seat Track · damaged · Jan 11, 2000 · N579PE · Boeing 727243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ALONG CABIN SEAT TRACK FROM BS 1080 TO 1135, RIGHT BODY LINE 45. REPLACED SECTION OF CABIN SEAT TRACK FROM BS 1080 TO BS 1135, RBL 45 IAW SRM 53-10-5 FIG 7. MATERIAL USED, PART NR BAC1520-792, 55 INCHES LONG. SEE
- [SDR GAIA0007](https://openairdocs.org/sdr/GAIA0007.md): Seat Track · damaged · Jan 11, 2000 · N579PE · Boeing 727243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ALONG SEAT TRACK FROM STATION 344 TO 480 RIGHT BODY LINE 45.5. REPLACED SEAT TRACK FROM STATION 344 TO STATION 480, RBL 45.5. MATERIAL USED, PART NR CAB1520-792. ACCOMPLISHED IAW SUPPLEMENTAL TYPE CERTIFICATE (ST
- [SDR GAIA0006](https://openairdocs.org/sdr/GAIA0006.md): Seat Track · damaged · Jan 11, 2000 · N579PE · Boeing 727243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING PHASE IN INSPECTION, DAMAGE WAS FOUND ALONG SEAT TRACK FROM STATION 344 TO 480, RIGHT BODY LINE 24.75. REPLACED SEAT TRACK FROM STATION 344 TO STATION 480, RBL 24.75. MATERIAL USED, PART NR CAB1520-792. ACCOMPLISHED IAW SUPPLEMENTAL TYPE CERTIFICATE
- [SDR GAIA0005](https://openairdocs.org/sdr/GAIA0005.md): Seat Track · damaged · Jan 11, 2000 · N579PE · Boeing 727243 · Fuselage, Seat/Cargo Attach Fittings
  > DURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ALONG SEAT TRACK FROM STATION 344 TO 480 LEFT BODY LINE 45.5. REPLACED SEAT TRACK FROM STATION 344 TO STATION 480, LBL 45.5. MATERIAL USED, PART NR BAC1520-792. ACCOMPLISHED IAW SUPPLEMENTAL TYPE CERTIFICATE (STC
- [SDR CALA9900928](https://openairdocs.org/sdr/CALA9900928.md): Floorbeam · corroded · Jul 31, 1999 · N579PE · Boeing 727243 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FORWARD LAV FLOORBEAM CORRODED AT STA 327, RBL 44-60. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03889.
- [SDR GAIA0001](https://openairdocs.org/sdr/GAIA0001.md): Bulb · failed · Jan 3, 1999 · N579PE · Boeing 727243 · Emergency Lighting
  > DURING POST FLIGHT, MAINTENANCE DISCOVERED THE EMERGENCY EXIT LIGHT OVER THE COCKPIT DOOR WAS INOPERATIVE. MAINTENANCE RE-LAMPED THE LIGHT ASSEMBLY AND PERFORMED AN SATISFACTORY OPS CHECK IAW BOEING 727 MM 33-50-4. THE AIRCRAFT WAS THEN RELEASED BACK TO SERV
- [SDR CALA9801919](https://openairdocs.org/sdr/CALA9801919.md): Skin · delaminated · Oct 8, 1998 · N579PE · Boeing 727243 · Spoilers
  > INSPECTION FOUND THE RT WING NR 8 SPOILER DELAMINATED. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1, PAGE 401-404.
- [SDR CALA9801920](https://openairdocs.org/sdr/CALA9801920.md): Skin · delaminated · Oct 7, 1998 · N579PE · Boeing 727243 · Ailerons
  > INSPECTION FOUND THE LT OUTBOARD AILERON TRAILING EDGE DELAMINATED SIX INCHES FROM OUTBOARD END. THE PANEL WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2.
- [SDR CALA9801918](https://openairdocs.org/sdr/CALA9801918.md): Tab · bent · Oct 7, 1998 · N579PE · Boeing 727243 · Aileron Tabs
  > INSPECTION FOUND LT OUTBOARD AILERON TAB INBOARD END BENT. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41, PAGE 401-403.
- [SDR CALA9801917](https://openairdocs.org/sdr/CALA9801917.md): Skin · bent · Oct 7, 1998 · N579PE · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND RT INBOARD FOREFLAP BENT AT O/B TRAILING EDGE. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-1.
- [SDR CALA9801910](https://openairdocs.org/sdr/CALA9801910.md): Stringer · corroded · Oct 5, 1998 · N579PE · Boeing 727243 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 29R CORRODED AT STA 1000. THE CORRODED AREA WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 51-40-3, 51-10-2, AND SB 727-53-0179.
- [SDR CALA9801909](https://openairdocs.org/sdr/CALA9801909.md): Rib · cracked · Oct 5, 1998 · N579PE · Boeing 727243 · Leading Edge Devices
  > INSPECTION FOUND A 1.25 INCH CRACK AT AFT LOWER END OF NR 3 SLAT LEADING EDGE RIB AND A 1.25 INCH CRACK WAS FOUND AT FORWARD LOWER END OUTBOARD OF ACTUATOR ROD MOUNT. THE CRACKS WERE STOP DRILLED IAW SRM 51-30-2, A DOUBLER WAS INSTALLED IAW SRM 57-50-3, PAGE
- [SDR CALA9801908](https://openairdocs.org/sdr/CALA9801908.md): Angle · corroded · Oct 5, 1998 · N579PE · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT ANGLE JUST INSIDE R-2 DOOR THRESHOLD AREA CORRODED AROUND SCREW HOLES. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2, PAGE 4.
- [SDR CALA9801907](https://openairdocs.org/sdr/CALA9801907.md): Skin · delaminated · Oct 5, 1998 · N579PE · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND LT WING OUTBOARD AFT FLAP UPPER SURFACE DELAMINATED 9 TO 15 INCHES FROM OUTBOARD EDGE. THE LT OUTBOARD AFT FLAP ASSEMBLY WAS REMOVED AND REPLACED IAW MM 27-51-12, PAGE 401.
- [SDR CALA9801906](https://openairdocs.org/sdr/CALA9801906.md): Skin · delaminated · Oct 5, 1998 · N579PE · Boeing 727243 · Elevator, Tab Structure
  > INSPECTION FOUND RT ELEVATOR CONTROL TAB TRAILING EDGE DELAMINATED. THE RT ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.
- [SDR CALA9801905](https://openairdocs.org/sdr/CALA9801905.md): Beam · cracked · Oct 5, 1998 · N579PE · Boeing 727243 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.375 INCH CRACK IN LT WING J-BEAM ABOVE NR 7 SPOILER ACTUATOR. A REPAIR WAS INSTALLED IAW ECRA 5750-02914.
- [SDR CALA9801899](https://openairdocs.org/sdr/CALA9801899.md): Skin · torn · Sep 30, 1998 · N579PE · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A TEAR IN RT LOWER FUSELAGE SKIN AT STA 1050, STRINGER 28R. THE TORN AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-30-3 AND 51-10-1.
- [SDR CALA9801898](https://openairdocs.org/sdr/CALA9801898.md): Intercostal · corroded · Sep 30, 1998 · N579PE · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL CORRODED AT BS 1050, STRINGER 28R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-1, 51-30-2, AND 51-10-6.
- [SDR CALA9701430](https://openairdocs.org/sdr/CALA9701430.md): Duct · broken · Oct 12, 1997 · N579PE · Boeing 727243 · Air Intake Anti/De-Ice System
  > NUMBER 3 ENGINE FIRE WARNING LIGHT BELL ON AFTER TAKEOFF. RETARDED THROTTLE, LIGHT WENT OUT. FOUND NOSE COWL ANTI-ICE DUCT BROKEN. REPLACED DUCT ASSEMBLY.
- [SDR CALA9701141](https://openairdocs.org/sdr/CALA9701141.md): Battery · discharged · Jul 16, 1997 · N579PE · Boeing 727243 · Emergency Lighting
  > MAIN CABIN OVERHEAD AT STATION 520 LEFT SIDE ESCAPE PATH BATTERY PACK DEAD. REPLACED BATTERY PACK PER MM 33-00-00.
- [SDR CALA9701140](https://openairdocs.org/sdr/CALA9701140.md): Battery · discharged · Jul 16, 1997 · N579PE · Boeing 727243 · Emergency Lighting
  > LEFT OVER WING EMERGENCY EXTERIOR LIGHTS ARE INOP. CLEANED AND RECHARGED BATTERY PACK PER MM 33-50-00.
- [SDR CALA9701139](https://openairdocs.org/sdr/CALA9701139.md): Stringer · cracked · Jul 12, 1997 · N579PE · Boeing 727243 · Wing, Longeron/Stringer
  > 2 CRACK ON UPPER WING STRINGER AT W/S 304 IN NR 1 FUEL TANK. CUT OUT DAMAGED AREA AND INSTALLED A 'J' STIFFENER AS PER SRM 57-10-4 FIG 6.
- [SDR CALA9701106](https://openairdocs.org/sdr/CALA9701106.md): Stringer · gouged · Jul 4, 1997 · N579PE · Boeing 727243 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER GOUGED AT LT FUSELAGE STA 1213 ABOVE PANEL NR 3901. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, FIGURE 2.
- [SDR CALA9701099](https://openairdocs.org/sdr/CALA9701099.md): Stringer · corroded · Jul 4, 1997 · N579PE · Boeing 727243 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER SPLICE AND STRINGER 28L CORRODED IN FORWARD CARGO COMPARTMENT AT STA 480. THE CORRODED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3.
- [SDR CALA9701135](https://openairdocs.org/sdr/CALA9701135.md): Angle · cracked · Jul 3, 1997 · N579PE · Boeing 727243 · Fuselage Miscellaneous Structure
  > LEFT AFT LAV FLOOR PANEL TO DITCH PAN ATTACH ANGLE AT LBL 50 HAS 3 FOOT LONG CRACK AT STA 1175. FABRICATED AND INSTALLED NEW ANGLE IN ACCORDANCE WITH SRM 51-30-2.
- [SDR CALA9701105](https://openairdocs.org/sdr/CALA9701105.md): Frame · corroded · Jul 3, 1997 · N579PE · Boeing 727243 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD SIDE OF AFT BAGGAGE BIN DOOR CORRODED AT UPPER STOP. THE CORRODED AREA WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.
- [SDR CALA9701097](https://openairdocs.org/sdr/CALA9701097.md): Frame · cracked · Jul 3, 1997 · N579PE · Boeing 727243 · Fuselage Main, Frame
  > INSPECTION FOUND A 2 INCH CRACK AT LOWER INBOARD FASTENER HOLE OF FRAME AT STA 783.5, RT SIDE. THE CRACK WAS STOP DRILLED, REPAIR PARTS WERE FORMED, HEAT TREATED, AND INSTALLED IAW BOEING DRAWING NR 65C36280.
- [SDR CALA9701116](https://openairdocs.org/sdr/CALA9701116.md): Rib · cracked · Jul 2, 1997 · N579PE · Boeing 727243 · Trailing Edge Flaps
  > INSPECTION FOUND A.5 INCH CRACK IN INBOARD END RIB OF RT OUTBOARD MID FLAP LOWER END AT FAIRING LOWER BOLT. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-40-2.
- [SDR CALA9701108](https://openairdocs.org/sdr/CALA9701108.md): Floorbeam · corroded · Jul 2, 1997 · N579PE · Boeing 727243 · Fuselage Main, Floor Beam
  > INSPECTION FOUND TOP OF FLOORBEAM CORRODED FROM BS 303-344, LBL 30 TO RBL 30. THE CORROSION WAS REMOVED. A T-CAP WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.
- [SDR CALA9701107](https://openairdocs.org/sdr/CALA9701107.md): Floorbeam · corroded · Jul 2, 1997 · N579PE · Boeing 727243 · Fuselage Main, Floor Beam
  > INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 1070, RBL 40. THE CORRODED AREA WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-8.
- [SDR CALA9701104](https://openairdocs.org/sdr/CALA9701104.md): Web · corroded · Jul 2, 1997 · N579PE · Boeing 727243 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND DELTA BEAM CENTER BOTTOM WEB CORRODED AT BS 780. THE CORRODED SECTION OF WEB WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-40-2, FIGURE 1.
- [SDR CALA9701098](https://openairdocs.org/sdr/CALA9701098.md): Floorbeam · corroded · Jul 2, 1997 · N579PE · Boeing 727243 · Fuselage Main, Floor Beam
  > INSPECTION FOUNDTOP OF FLOORBEAM CORRODED AT STA 380, RBL 24 TO RBL 45.5. THE FLOORBEAM UPPER CHORD WAS REMOVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.
- [SDR CALA9701134](https://openairdocs.org/sdr/CALA9701134.md): Shear Tie · dented · Jul 1, 1997 · N579PE · Boeing 727243 · Fuselage Miscellaneous Structure
  > FUSELAGE HAS DENT IN SHEAR TIE AT STA 380 STR 18L. CUT OUT, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IN ACCORDANCE WITH SRM 53-30-3 FIG 3.
- [SDR CALA9701138](https://openairdocs.org/sdr/CALA9701138.md): Flap · delaminated · Jun 30, 1997 · N579PE · Boeing 727243 · Trailing Edge Flaps
  > RIGHT INBOARD AFT FLAP IS DELAMINATED 32 THROUGH 54 FROM INBOARD END. REMOVED, REPAIRED AND REINSTALLED IN ACCORDANCE WITH MM 57-53-2.
- [SDR CALA9701137](https://openairdocs.org/sdr/CALA9701137.md): Bracket · cracked · Jun 30, 1997 · N579PE · Boeing 727243 · Leading Edge Slat Actuator
  > LEFT WING NUMBER 1 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED BELOW INBOARD UPPER CORNER AREA INSIDE LEADING EDGE, LENGTH.75 FABRICATED AND INSTALLED NEW BRACKET IN ACCORDANCE WITH MM 27-81-1.
- [SDR CALA9701136](https://openairdocs.org/sdr/CALA9701136.md): Bracket · cracked · Jun 30, 1997 · N579PE · Boeing 727243 · Leading Edge Slat Actuator
  > LEFT WING MOUNT BRACKETS CRACKED AT ALL FOUR CORNER AREAS WHERE NUMBER 2 LEADING EDGE FLAP ACTUATOR MOUNTS, INSIDE LEADING EDGE. LENGTH.75. FABRICATED AND INSTALLED NEW MOUNT BRACKET PER MM 27-91-1.
- [SDR CALA9701109](https://openairdocs.org/sdr/CALA9701109.md): Tab · debonded · Jun 30, 1997 · N579PE · Boeing 727243 · Aileron Tabs
  > INSPECTION FOUND LEFT OUTBOARD AILERON TAB INBOARD END DEBONDED AND END FILLER MISSING. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-0.
- [SDR CALA9701100](https://openairdocs.org/sdr/CALA9701100.md): Skin · dented · Jun 30, 1997 · N579PE · Boeing 727243 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 188. THE DENTED AREA OF SKIN WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.
- [SDR CALA9701096](https://openairdocs.org/sdr/CALA9701096.md): Skin · debonded · Jun 30, 1997 · N579PE · Boeing 727243 · Ailerons
  > INSPECTION FOUND LT OUTBOARD AILERON OUTBOARD MOST TRAILING EDGE SPLIT/DEBONDED. THE AILERON TRAILING EDGE WEDGE WAS REMOVED. REPLACEMENT SKIN PANELS WERE FABRICATED AND INSTALLED IAW SRM 51-40-6 AND 51-30-2. THE AILERON WEDGE WAS REINSTALLED.

Next page: https://openairdocs.org/deregistered/N579PE-2015-05-19/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 = 'N579PE' AND deregistration_id = 'N579PE-2015-05-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N579PE-2015-05-19/reports

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