# Service difficulty reports: N528MC, cancelled Apr 30, 2013

A list on [N528MC, cancelled Apr 30, 2013](https://openairdocs.org/deregistered/N528MC-2013-04-30.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 · 63 reports

- [SDR UIEA200800281](https://openairdocs.org/sdr/UIEA200800281.md): Relief Valve · leaking · Aug 3, 2008 · N528MC · Boeing 7472D7B · Pneumatic Distribution System
  > AT CRUISE NR 4 ENG HAD MULTPLE FIRE WARNINGS ON BOTH A&B. PERFORMED IN FLIGHT SHUT DOWN AND AIR TURNBACK. MAINTENANCE FOUND LEAKING PRESSURE RELIEF VALVE, WHICH WAS BLASTING HOT AIR ON THE DETECTORS. REPLACED OVER PRESSURE RELIEF VALVE PER 36-11-03, OPS CHE
- [SDR UIEA200800169](https://openairdocs.org/sdr/UIEA200800169.md): Shear Pin · broken · May 5, 2008 · N528MC · Boeing 7472D7B · Cargo/Baggage Doors
  > AIR TURN BACK, SIDE CARGO DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL. RETURNED TO BLOCKS PER FHB. FOUND OUTSIDE MASTER LATCH LOCK HANDLE SHEAR PIN BROKEN. REMOVED AND REPLACED SHEAR PIN PER AMM 52-32-06. OPS CHECKED OKAY.
- [SDR UIEA200800163](https://openairdocs.org/sdr/UIEA200800163.md): Regulator Valve · leaking · May 1, 2008 · N528MC · Boeing 7472D7B · Pneumatic Distribution System
  > NR 1 ENGINE FULL POWER TAKEOFF ON CLIMB-OUT BOTH A/B LOOPS REACHED 3.0. AFTER POWER REDUCTION BOTH LOOPS CAME BACK DOWN TO 2.0. REST OF FLIGHT WAS OK. OPENED COWL AND FOUND LEAKING PRV. REPLACED THE PRV IAW AMM 36-11-13. OPS AND LEAK CHECKED OK.
- [SDR UIEA200800114](https://openairdocs.org/sdr/UIEA200800114.md): Skin Panel · corroded · Apr 7, 2008 · N528MC · Boeing 7472D7B · Fuselage Main, Plate/Skin
  > EVIDENCE OF CORROSION UNDER LAP JOINT STRINGER 46 RIGHT, BETWEEN STA 1737-1745. INTERIM REPAIR ACCOMPLISHED IAW SRM 53-30-03 FIG 17 TABLE LLL WITH INITIAL INSPECTION SCHEDULED AT 15000 FLIGHT CYCLES AFTER INTERIM REPAIR AND REPEAT INSPECTION THEREAFTER AT EVE
- [SDR UIEA200800113](https://openairdocs.org/sdr/UIEA200800113.md): Skin · delaminated · Apr 7, 2008 · N528MC · Boeing 7472D7B · Spoilers
  > RIGHT WING INBOARD SPOILER UPPER SURFACE HAS DELAMINATION WBL 235.150. REMOVED NR 7 GROUND SPOILER IAW MM 27-62-01. REPAIRED DELAMINATION IAW SRM 51-40-20. INSTALLED SPOILER AND OPS CHECKED OKAY PER 27-62-01.
- [SDR UIEA200800042](https://openairdocs.org/sdr/UIEA200800042.md): Radome · damaged · Feb 13, 2008 · N528MC · Boeing 7472D7B · Aerodynamic Fairings
  > AIRCRAFT WAS HIT BY LIGHTNING STRIKE. ENTRANCE AT THE RADOME. NO COMMUNICATIONS OR NAV FAILURES REPORTED BY CREW. FOUND RADOME DAMAGED BY LIGHTNING STRIKE. FOUND RIGHT HF ANTENNA DAMAGED BY LIGHTNING STRIKE. LIGHTNING STRIKE INSPECTION ACCOMPLISHED PER 5-
- [SDR UIEA200700352](https://openairdocs.org/sdr/UIEA200700352.md): Web · cracked · Sep 5, 2007 · N528MC · Boeing 7472D7B · Trailing Edge Flaps
  > OLEO 1450 FWD CRACKED JUST FWD OF NR 25 V/C FLAP UPPER FITTING. CARRY OUT REPAIR AS PER SRM 51-40-03.
- [SDR UIEA200700349](https://openairdocs.org/sdr/UIEA200700349.md): Nozzle · dented · Sep 5, 2007 · N528MC · Boeing 7472D7B · Engine Collector/Tailpipe/Nozzle
  > NR 1 ENGINE EXHAUST NOZZLE DENTED AT 0300. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMITS AMM 78-11-01 PAGE 601.
- [SDR UIEA200700347](https://openairdocs.org/sdr/UIEA200700347.md): Web · cracked · Sep 5, 2007 · N528MC · Boeing 7472D7B · Trailing Edge Flaps
  > UPON L/E CAP REMOVAL OLES 1522, NR 26VC FLAP UPPER STOP FTG FWD WEB DOUBLER FOUND CRACKED. DOUBLER REPLACED IAW SRM 51-10-01.
- [SDR UIEA200700346](https://openairdocs.org/sdr/UIEA200700346.md): Frame · cracked · Sep 5, 2007 · N528MC · Boeing 7472D7B · Fuselage Main, Frame
  > R1 MED LOWER AFT CORNER FRAME CRACKED AT STA 490 RT S-25R TO S-26R AREA. C/OUT AS PER SRM 52-10-02 FIG 10.
- [SDR UIEA200700345](https://openairdocs.org/sdr/UIEA200700345.md): Door Frame · cracked · Sep 5, 2007 · N528MC · Boeing 7472D7B · Fuselage Main, Structure
  > M/D R4 MED FWD UPPER CORNER FRAME CRACKED AT STA 1670 S-16R TO S-17R AREA. CARRY OUT REPAIR AS PER SRM 52-10-02, FIG 10.
- [SDR UIEA200700344](https://openairdocs.org/sdr/UIEA200700344.md): Door Frame · cracked · Sep 5, 2007 · N528MC · Boeing 7472D7B · Service Doors
  > R3 DOOR FWD UPPER CORNER FRAME FOUND CRACKED. C/OUT AS PER SRM 52-10-02, FIG 10.
- [SDR UIEA200700343](https://openairdocs.org/sdr/UIEA200700343.md): Web · corroded · Sep 5, 2007 · N528MC · Boeing 7472D7B · Fuselage Miscellaneous Structure
  > BULK CARGO BS 1980-2030 DOOR LOWER SILL FLOOR WEB, CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND SRM 51-10-02 WITHIN ALLOWABLE LIMIT AS PER SRM 53-10-01.
- [SDR UIEA200700342](https://openairdocs.org/sdr/UIEA200700342.md): Panel · contaminated · Sep 5, 2007 · N528MC · Boeing 7472D7B · Trailing Edge Flaps
  > RT WING I/B T/E PANEL FOUND WATER. REPLACE RHW I/B T/E PANEL AS PER SRM 51-10-01 AND SRM 51-30-02.
- [SDR UIEA200700348](https://openairdocs.org/sdr/UIEA200700348.md): Frame · cracked · Sep 5, 2007 · N528MC · Boeing 7472D7B · Leading Edge Devices
  > AFT REMOVAL OF L/E NOSE CAP FOUND THAT "D" SECTION CRACKED. CARRY OUT REPAIR AS PER SRM 57-20-03.
- [SDR UIEA200700350](https://openairdocs.org/sdr/UIEA200700350.md): Nozzle · dented · Sep 5, 2007 · N528MC · Boeing 7472D7B · Engine Collector/Tailpipe/Nozzle
  > NR 3 ENGINE EXHAUST NOZZLE EXTERIOR SKIN DENTED AT 0900. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMIT AMM 78-11-01 PAGE 601.
- [SDR UIEA200700351](https://openairdocs.org/sdr/UIEA200700351.md): Nozzle · dented · Sep 5, 2007 · N528MC · Boeing 7472D7B · Engine Collector/Tailpipe/Nozzle
  > NR 4 ENGINE EXHAUST NOZZLE EXTERIOR SKIN DENTED AT 0700 TO 0900. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMIT AMM 78-11-01 PAGE 601.
- [SDR UIEA200700336](https://openairdocs.org/sdr/UIEA200700336.md): Access Panel · elongated · Aug 31, 2007 · N528MC · Boeing 7472D7B · Air Conditioning Doors
  > AIR COND, BAY ACCESS PANEL 192ER EXT SURFACE FOUND SKIN ELONGATION. AIR COND BAY ACCESS PANEL 192ER REPAIRED WITH PRE-PRED FABRIC AS PER MESSAGE NR 1-497468248-2.
- [SDR UIEA200700329](https://openairdocs.org/sdr/UIEA200700329.md): Frame · cracked · Aug 31, 2007 · N528MC · Boeing 7472D7B · Fuselage Main, Frame
  > BS 800 S17 LT ONE FASTENER HOLE FOUND CRACK ON FWD INNER CHORD ANGLE. REPLACEMENT PER BOEING CONTROL NO PO24708.
- [SDR UIEA200700337](https://openairdocs.org/sdr/UIEA200700337.md): Access Panel · delaminated · Aug 31, 2007 · N528MC · Boeing 7472D7B · Air Conditioning Doors
  > AIR COND, BAY ACCESS PANEL 192HR EXT SURFACE FOUND SKIN DELAMINATION. AIR COND BAY ACCESS PANEL 192HR REPAIRED WITH PRE-PRED FABRIC AS PER MESSAGE NR 1-497468248-2.
- [SDR UIEA200700335](https://openairdocs.org/sdr/UIEA200700335.md): Access Panel · eroded · Aug 31, 2007 · N528MC · Boeing 7472D7B · Air Conditioning Doors
  > AIR COND, BAY ACCESS PANEL 191HL EXT SURFACE FOUND ERODED. AIR COND BAY ACCESS PANEL 191HL REPAIRED WITH PRE-PRED FABRIC AS PER MESSAGE NR 1-497468248-2.
- [SDR UIEA200700332](https://openairdocs.org/sdr/UIEA200700332.md): Floorbeam · cracked · Aug 31, 2007 · N528MC · Boeing 7472D7B · Fuselage Main, Floor Beam
  > FLOOR STRUCTURE BEAM WEB CRACKED. C/OUT AS PER BOEING MESSAGE NR 1-497681686-1.
- [SDR UIEA200700338](https://openairdocs.org/sdr/UIEA200700338.md): Torque Link · chafed · Aug 31, 2007 · N528MC · Boeing 7472D7B · Nose/Tail Landing Gear
  > NLG LOWER TORSION LINK FOUND CHAFING. BLEND OUT THE CHAFING AREA WITH MIN 20-1 BLEND-RATIO.
- [SDR UIEA200700331](https://openairdocs.org/sdr/UIEA200700331.md): Skin · dented · Aug 31, 2007 · N528MC · Boeing 7472D7B · Elevator, Plate/Skin
  > HORIZONTAL STAB RT I/B ELEVATOR L/E UPPER SKIN DENTED. REPAIRED IAW BOEING MESSAGE SR 1-514407012.
- [SDR UIEA200700333](https://openairdocs.org/sdr/UIEA200700333.md): Floorbeam · cracked · Aug 31, 2007 · N528MC · Boeing 7472D7B · Fuselage Main, Floor Beam
  > FLOOR STRUCTURE BEAM WEB CRACKED. REPAIRED IAW BOEING MESSAGE NR 1-497681686-1.
- [SDR UIEA200700339](https://openairdocs.org/sdr/UIEA200700339.md): Skin · dented · Aug 31, 2007 · N528MC · Boeing 7472D7B · Fuselage Main, Plate/Skin
  > FX EXTERIOR SKIN DENT AS MARKED APPR, 1" SQ IN AT BS 780 S47-R. REINSTALLED A REPAIRED DOUBLER AS PER SRM 53-30-03 DETAILS AS PER SWS SHOWN.
- [SDR UIEA200700334](https://openairdocs.org/sdr/UIEA200700334.md): Pan · cracked · Aug 31, 2007 · N528MC · Boeing 7472D7B · Flight Compartment Equipment
  > COCKPIT 2ND OBSERVER SEAT PAN CRACKED. REPAIRED IAW BOEING MESSAGE NR 1-497681686-1.
- [SDR UIEA200700340](https://openairdocs.org/sdr/UIEA200700340.md): Hinge Fitting · cracked · Aug 31, 2007 · N528MC · Boeing 7472D7B · Horizontal Stabilizer Structure
  > BS 2598 H/S RT RBL 40" REAR SPAR UPPER I/B OF HINGE FITTING OPEN HOLE. OVERSIZE TO 0.403", USED BACB30 US6K21Y BOLT. CARRIED OUT NDT TEST OF THE OPEN OVERSIZE HOLE FOUND SATISFACTORY.
- [SDR UIEA200700330](https://openairdocs.org/sdr/UIEA200700330.md): Panel · contaminated · Aug 31, 2007 · N528MC · Boeing 7472D7B · Trailing Edge Flaps
  > LT WING T/E I/B PANEL FOUND WATER. REPLACE LHW T/E I/B FIXED PAL AS PER SRM 51-10-01 AND SRM 51-30-02, AND PANEL REPAIR IAW BOEING MESSAGE 31-516595696-1 TO 1-516595696-4.
- [SDR UIEA200700260](https://openairdocs.org/sdr/UIEA200700260.md): Unknown · odor · Jul 8, 2007 · N528MC · Boeing 7472D7B · Air Distribution System
  > AT DEPARTURE SMOKE AND BURNING ODOR IN COCKPIT, ELECTRICAL ODOR. PULLED C/BS FOR T/R UNITS, SMOKE AND ODOR STOPPED. WIRE BUNDLES AND AREA BELOW F/E PANEL (4) INSPECTED NO SIGN OF SHORTING OR CHAFING FOUND. PULLED T/R UNITS, PULLED AND INSPECTED FOUND NR 1 T
- [SDR UIEA200700259](https://openairdocs.org/sdr/UIEA200700259.md): Seal · loose · Jul 3, 2007 · N528MC · Boeing 7472D7B · Flight Compartment Windows
  > L-3 WINDOW SEAL LIFTING IN THE WIND WITH EXCESSIVE COCKPIT NOISE. ALSO, DURING LEVEL FLIGHT APPROX TIME 1335Z FL 31.0 TEMP -09 TAT HEARD BANG AIRCRAFT SHOOK, POSSIBLE ENGINE STALL. AUTO THROTTLES TRIPPED OFF SEVERAL TIMES IN FLIGHT. RESECURED WINDOW SEAL I
- [SDR UIEA200700255](https://openairdocs.org/sdr/UIEA200700255.md): Panel · corroded · Jun 21, 2007 · N528MC · Boeing 7472D7B · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE CENTER PANELS 191HH AND 191JJ BETWEEN NR 1 AND NR 3 ACM'S HAVE AREA OF CORROSION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-02 FIG 1. ALSO, REFERENCE ATLAS AIR XEO NR 53-062007.
- [SDR UIEA200700252](https://openairdocs.org/sdr/UIEA200700252.md): Fairing · damaged · Jun 21, 2007 · N528MC · Boeing 7472D7B · Trailing Edge Flaps
  > RT WING, NR 8 FLAPTRACK FORWARD FIXED FAIRING HAS SEVERAL SMALL HOLES AT LEADING EDGE AREA. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 51-40-09, FIG 6, TABLE I AND 747-200 SRM 51-40-12. ALSO, REFERENCE ATLAS AIR XEO NR 57-061907.
- [SDR UIEA200700254](https://openairdocs.org/sdr/UIEA200700254.md): Support · corroded · Jun 21, 2007 · N528MC · Boeing 7472D7B · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE AIR CONDITIONING ACCESS DOOR AREA, BELOW KEEL BEAM BOX, EXTERIOR CENTER PANEL SUPPORT EXTRUSION HAS CORROSION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER 747-200 SRM 51-40-04, FIG 1. ALSO REFERENCE ATLAS AIR XEO NR 53-062007.
- [SDR UIEA200700251](https://openairdocs.org/sdr/UIEA200700251.md): Fairing · cracked · Jun 21, 2007 · N528MC · Boeing 7472D7B · Trailing Edge Flaps
  > RT WING NR 7 FLAP TRACK CANOE FAIRING DAMAGED AT LOWER SIDE, AFT OF ACCESS PANEL 667CB. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 51-40-09, FIG 6 TABLE I AND 747-200 SRM 51-40-12. ALSO REFERENCE ATLAS AIR XEO NR 57-061907.
- [SDR UIEA200700253](https://openairdocs.org/sdr/UIEA200700253.md): Skin · delaminated · Jun 21, 2007 · N528MC · Boeing 7472D7B · Engine Thrust Reverser
  > NR 4 ENGINE RT REVERSER AT NAC STATION 206.10 UPPER SIDEWALL SKIN DELAMINATED. PERMANENT REPAIR WAS ACCOMPLISHED AS PER CF6-50 ENGINE MANUAL 78-32-03, REPAIR NR 13, REF: FIG 1. ALSO, REFERENCE ATLAS AIR XEO NR 78-062007.
- [SDR UIEA200700148](https://openairdocs.org/sdr/UIEA200700148.md): Skin · cracked · Apr 8, 2007 · N528MC · Boeing 7472D7B · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS 12" CRACK FROM STA 2650 TO 2658 ON RIGHT SIDE OF AIRCRAFT BETWEEN STRINGERS 11R AND 13R. FOUND CRACKED IN A SEMI-CIRCULAR SHAPE. REPAIRED PER SRM 53-30-03 FIG 1 DETAIL L AND XEO 53-04-06-07. (TIME LIMITED REPAIR)
- [SDR UIEA200700068](https://openairdocs.org/sdr/UIEA200700068.md): Altimeter · faulty · Feb 5, 2007 · N528MC · Boeing 7472D7B · Altimeter, Barometric/Encoder
  > CAPT ALT UNRESPONSIVE TO ALL CHANGE BOTH CADC/STBY MODES, PERFORMED CHECK DIFFERENCE BETWEEN ALT INDICATORS (3,34,7), CHANGE ALT LAGS IN DESCENT BY OVER 300' AND DIFFERS BY OVER 180' AT EL 290-310-MACH.84. T/S AND FOUND PIN NR 22 AT PLUG DN 101. CAPT ALT IN
- [SDR UIEA200700066](https://openairdocs.org/sdr/UIEA200700066.md): Cadc · sticking · Feb 4, 2007 · N528MC · Boeing 7472D7B · Altimeter, Barometric/Encoder
  > DURING CLIMB CAPT ALTIMETER NEEDLE WOULD STICK IN POSITION CAUSING PULL-UP TERRAIN WARNINGS, DON’T SINK WARNING AUDIBLES, ALTIMETER READ 37.0, ATC 36.8. PERFORMED STATIC SYSTEM LEAK CHECK NORMAL AS PER MM 34-11-00. FOUND NR 1 CADC DEFECTIVE. REMOVED AND REP
- [SDR UIEA200700065](https://openairdocs.org/sdr/UIEA200700065.md): Altimeter · sticking · Feb 3, 2007 · N528MC · Boeing 7472D7B · Altimeter, Barometric/Encoder
  > DURING CLIMB CAPT'S ALTIMETER NEEDLE WOULD STICK IN POSITION CAUSING PULL-UP TERRAIN WARNING, DON'T SINK WARNING AUDIBLES. CAPT'S ALTIMETER REMOVED AND REPLACED, INDICATION AND LEAK CHECK CARRIED OUT, OK IAW MM 34-13-04.
- [SDR UIEA200700026](https://openairdocs.org/sdr/UIEA200700026.md): Panel · cracked · Jan 27, 2007 · N528MC · Boeing 7472D7B · Wing, Plate/Skin
  > LT WING PYLON GAP PANEL AT ILES 640.47 HAS A 3.0 INCH CRACK. ACCOMPLISHED PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 18 SHEET 5 AND SRM 51-40-12, ALSO REFERENCE ATLAS AIR EO 4757A342.
- [SDR UIEA200700027](https://openairdocs.org/sdr/UIEA200700027.md): Panel · cracked · Jan 27, 2007 · N528MC · Boeing 7472D7B · Wing, Plate/Skin
  > LT WING UPPER FIXED PANEL, 12 INCHES FROM FORWARD EDGE OF NR 5 SPOILER, WBL 421.00 HAS A 6.0 INCH CRACK. ACCOMPLISHED PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 2 SHEET 5 AND SRM 51-40-12 AND ATLAS AIR EO 4757A342.
- [SDR UIEA200600290](https://openairdocs.org/sdr/UIEA200600290.md): Skin · punctured · Nov 15, 2006 · N528MC · Boeing 7472D7B · Leading Edge Devices
  > NR 21 LEADING EDGE DEVICE FOLDING NOSE FOUND DAMAGED ON ARRIVAL. NOSE HINGE ARM FOUND BROKEN AND SKIN PUNCTURED. UNABLE TO CONCLUSIVELY DETERMINE THE REASON FOR THE FAILURE AND SUBSEQUENT DAMAGE. REPLACED NR 21 LEADING EDGE DEVICE ASSY.
- [SDR UIEA200600158](https://openairdocs.org/sdr/UIEA200600158.md): Duct · ruptured · Jul 2, 2006 · N528MC · Boeing 7472D7B · Pneumatic Distribution System
  > FOLLOWING TAKEOFF NR 4 ENG FIRE INDICATIONS NACELLE TEMPS A/B HIGH, THEN TO FIRE "F" AND FULL WARNING ENG NR 4 SHUTDOWN AS PER CHECKLIST. NR 4 ENG FIRE BOTTLE "A" DISCHARGED, FIRE WARNING EXTINGUISHED. FOUND 14TH STAGE BLEED AIR DUCT RUPTURE. REMOVED AND RE
- [SDR UIEA200700256](https://openairdocs.org/sdr/UIEA200700256.md): Skin · dented · Jun 21, 2006 · N528MC · Boeing 7472D7B · Engine Thrust Reverser
  > NR 4 ENGINE LT REVERSER HAS DENT ON UPPER SIDE OF TRANSLATING COWL AT NAC STATION 224.6. PERMANENT REPAIR WAS ACCOMPLISHED AS PER CF6-50 ENGINE MANUAL 78-32-01, REPAIR 003. ALSO, REFERENCE ATLAS AIR XEO NR 78-062107.
- [SDR UIEA200600131](https://openairdocs.org/sdr/UIEA200600131.md): Hydraulic Line · cracked · Jun 13, 2006 · N528MC · Boeing 7472D7B · Hydraulic System, Main
  > DURING CLIMB NR 4 HYD SYSTEM STARTED DECREASING AND LOW QUANTITY LIGHT CAME ON. FHB PROCEDURES C/W AND QUANTITY WAS STILL DECREASING. ENG PUMP SWITCH WAS POSITIONED TO "SUPPLY OFF" WITH ENGINE RUNNING. QUANTITY INDICATOR ZERO AT COMPLETION OF CHECKLIST. FO
- [SDR UIEA200600136](https://openairdocs.org/sdr/UIEA200600136.md): Start Valve · damaged · Jun 11, 2006 · N528MC · Boeing 7472D7B · Engine Starter
  > NR4 ENGINE SHUT DOWN AT 1945Z DUE TO NR 4 START VALVE ENGINE LIGHT FLICKERING AND THEN COMING ON. REMOVED AND REPLACED NR 4 START VALVE AS PER AMM 80-11-04. PERFORMED GROUND OPS BY MONITORING SATISFACTORY.
- [SDR UIEA200600121](https://openairdocs.org/sdr/UIEA200600121.md): Seal · damaged · May 26, 2006 · N528MC · Boeing 7472D7B · Turbine Engine Accessory Drive
  > ACCOMPLISHED AIR TURNBACK DUE TO LOSS OF ALL OIL IN ENGINE NR 1, DURING CLIMBOUT. FOLLOWED SHORTLY BY A DROP IN OIL PRESSURE INTO THE MID TO LOWER AMBER BAND. FOUND NR 1 ENGINE HYD PUMP SHAFT SEAL CAVITY LEAKING OIL DURING IDLE RUN. HYD (EDP) PUMP SHAFT SEA
- [SDR UIEA200600127](https://openairdocs.org/sdr/UIEA200600127.md): Relief Valve · leaking · May 24, 2006 · N528MC · Boeing 7472D7B · Engine Emergency Shutdown System
  > AT 3000 FT DURING CLIMBOUT FIRE DETECTION LIGHT ON PILOT'S CENTER ANNUNCIATOR PANEL ILLUMINATED, FOLLOWED SHORTLY BY A FIRE INDICATION ON NR 1 ENGINE. FIRE CAUSED SEVERE DAMAGE OR SEPARATION, CHECKLIST COMPLETE AS PER FHB 3.701. OVERWEIGHT LANDING AT 287.0 K
- [SDR UIEA200600006](https://openairdocs.org/sdr/UIEA200600006.md): Panel · missing · Feb 14, 2006 · N528MC · Boeing 7472D7B · Nacelle/Pylon, Plate/Skin
  > ON WALKAROUND FOUND NR 1 ENGINE LOWER ACCESS PANEL MISSING.

Next page: https://openairdocs.org/deregistered/N528MC-2013-04-30/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 = 'N528MC' AND deregistration_id = 'N528MC-2013-04-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N528MC-2013-04-30/reports

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