# Service difficulty reports: N553NA, cancelled Feb 28, 2017

A list on [N553NA, cancelled Feb 28, 2017](https://openairdocs.org/deregistered/N553NA-2017-02-28.md).

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

- [SDR 2001F00272](https://openairdocs.org/sdr/2001F00272.md): Control Valve · failed · Jul 23, 2001 · N553NA · Boeing 7272J7 · Compressor Bleed Valve
  > ON FLT 748 - FPO-CVG - TAKEOFF ROLL, NR 2 ENGINE STALLED DURING ACCELERATION THROUGH 70 KTS. PARAMETERS WERE OBSERVED TO RECOVER TO NORMAL. HOWEVER, NR 2 ENGINE ACCESS DOOR LIGHT ILLUMINATED, TAKEOFF ABORTED. REMOVED AND REPLACED NR 2 PRBC VALVE, OPERATION
- [SDR 2001F00271](https://openairdocs.org/sdr/2001F00271.md): Latch · broken · Jul 23, 2001 · N553NA · Boeing 7272J7 · Engine Cowling System
  > FLT 1 - FLL - ON DEPARTURE CLIMB-OUT, NR 2 ENGINE ACCESS DOOR ILLUMINATED. AIRCRAFT RETURNED TO FLL. INSPECTED AND FOUND BROKEN LATCH ON NR 2 ENGINE ACCESS DOOR. REMOVED AND REPLACED LATCH ASSEMBLY PER MM 71-10-00. OPERATION CHECKED NORMAL. AIRCRAFT RETUR
- [SDR 97ZZZX4688](https://openairdocs.org/sdr/97ZZZX4688.md): Coupler · shorted · Nov 1, 1997 · N553NA · Boeing 7272J7 · Autopilot System
  > LOG BOOK ENTRY: EXCESSIVELY HARD LOWER RUDDER INPUTS LEFT AND RIGHT INDEPENDANT OF PILOT ACTION OR INPUT. VISUAL INDICATION OF SAME ON COCKPIT RUDDER INDICATOR. FOUND LOWER YAW DAMPENER RACK CONNECTOR WET WITH WATER. GALLEY FLOOR DRAIN SYSTEM AT FAULT. RE
- [SDR 97ZZZM1117](https://openairdocs.org/sdr/97ZZZM1117.md): Seat Track · corroded · Oct 10, 1997 · N553NA · Boeing 7272J7 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 4 STATION 500-600 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW BOEING SRM 51-10-0, 51-10-2, 51-20-0 AND 51-30-2. (M)
- [SDR 97ZZZM1116](https://openairdocs.org/sdr/97ZZZM1116.md): Seat Track · corroded · Oct 10, 1997 · N553NA · Boeing 7272J7 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED BEYOND LIMITS STATION 1010-1130 NR 4. REMOVED AND REPLACED SEAT TRACK IAW BOEING SRM 51-10-0, 51-10-2, 51-20-0, 51-30-2. (M)
- [SDR 97ZZZM1115](https://openairdocs.org/sdr/97ZZZM1115.md): Floorbeam · corroded · Oct 10, 1997 · N553NA · Boeing 7272J7 · Fuselage Main, Floor Beam
  > FLOORBEAM AT STATION 344 CORRODED BEYOND LIMITS END TO END. REMOVED AND REPLACED FLOORBEAM IAW BOEING SRM 51-10-2, 51-10-6, 51-30-2 AND 51-10-01 AND 53-10-8. (M)
- [SDR 97ZZZM1114](https://openairdocs.org/sdr/97ZZZM1114.md): Seat Track · corroded · Oct 10, 1997 · N553NA · Boeing 7272J7 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 5 CORRODED FROM STATION 344-380 BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW BOEING SRM 51-10-0, 51-10-2, 51-20-0 AND 51-30-2. (M)
- [SDR 97ZZZM1113](https://openairdocs.org/sdr/97ZZZM1113.md): Floorbeam · corroded · Oct 10, 1997 · N553NA · Boeing 7272J7 · Fuselage Main, Floor Beam
  > FLOORBEAM AT STATION 380 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAM IAW BOEING SRM 51-10-2, 51-10-6, 51-30-2, 51-10-01 AND 53-10-8. (M)
- [SDR 97ZZZM1112](https://openairdocs.org/sdr/97ZZZM1112.md): Seat Track · corroded · Oct 10, 1997 · N553NA · Boeing 7272J7 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 3 FROM STATION 344-480 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW BOEING SRM 51-10-0, 51-10-2, 51-10-6, 51-20-0 AND 51-30-2. (M)
- [SDR 97ZZZM1111](https://openairdocs.org/sdr/97ZZZM1111.md): Skin · corroded · Oct 10, 1997 · N553NA · Boeing 7272J7 · Fuselage Main, Plate/Skin
  > LEFT AND RIGHT RAM AIR PLENUM CAVITY SKINS CORRODED BEYOND LIMITS AT STATION 772.45 TO 848.95. REPAIRED IAW BOEING DOC DWG MAJR970919 AND B727 SRM 57-30-3 FIG 9 DETAIL 1 AND 53-30-10 FIG 1. (M)
- [SDR 97ZZZM1110](https://openairdocs.org/sdr/97ZZZM1110.md): Seat Track · corroded · Oct 10, 1997 · N553NA · Boeing 7272J7 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 4 FROM STATION 344-500 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW BOEING SRM 51-10-0, 51-10-2, 51-20-0 AND 51-30-2. (M)
- [SDR 97ZZZM1109](https://openairdocs.org/sdr/97ZZZM1109.md): Seat Track · corroded · Oct 10, 1997 · N553NA · Boeing 7272J7 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 1 FROM STATION 344-480 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW BOEING SRM 51-10-0, 51-10-2, 51-20-0 AND 51-30-2. (M)
- [SDR 97ZZZM1108](https://openairdocs.org/sdr/97ZZZM1108.md): Floorbeam · corroded · Oct 10, 1997 · N553NA · Boeing 7272J7 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED END TO END AT STATION 400 BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAM IAW BOEING SRM 51-10-2, 51-10-0, 51-10-6, 51-30-2 AND 53-10-8. (M)
- [SDR 97ZZZM520](https://openairdocs.org/sdr/97ZZZM520.md): Cowl · corroded · Sep 18, 1996 · N553NA · Boeing 7272J7 · Engine Cowling System
  > EXFOLIATED CORROSION ON NR 1 ENGINE FIXED COWL FORWARD SKIN. CORROSION BETWEEN HEAT SHILL AND SKIN. REMOVED FASTENERS AND SKIN. FABRICATED NEW SKIN FROM 2024-T3.032 INCH 21.75 INCH BY 30.5 INCH. DRILLED, COUNTERSUNK AND DEBURRED. ALODINED AND PRIMED NEW
- [SDR 97ZZZM515](https://openairdocs.org/sdr/97ZZZM515.md): Control Valve · chafed · Sep 17, 1996 · N553NA · Boeing 7272J7 · Engine Start Valves/Controls
  > NR 1 ENGINE STARTER CONTROL VALVE CHAFED AND COVER BROKE AT CORNERS. REMOVED AND REPLACED STARTER CONTROL VALVE IAW B727 80-11-11. LEAK CHECKED OK. LOG PAGE 6465.
- [SDR 97ZZZM519](https://openairdocs.org/sdr/97ZZZM519.md): Rib · cracked · Sep 14, 1996 · N553NA · Boeing 7272J7 · Vertical Stabilizer, Spar/Rib
  > FIN STATION 35, STRINGER NR 4 SECOND BAY UP FROM THE BOTTOM, RIB CRACKED WITH PREVIOUS ANGLE REPAIR, STOP DRILL IS NET.25 INCH AND CRACKED ON FORWARD SIDE OF RIB RUNS TO THE SIDE OF STOP DRILL. CRACK RUNS PAST ANGLE DOUBLER RT SIDE OF VERTICAL STABILIZER. R
- [SDR 97ZZZM523](https://openairdocs.org/sdr/97ZZZM523.md): Spar Cap · corroded · Sep 13, 1996 · N553NA · Boeing 7272J7 · Wing Spar
  > DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RIGHT WING STATION 520 L/E FORWARD LOWER SPAR CAP CORRODED. FOUND TO BE IN LIMITS.
- [SDR 97ZZZM522](https://openairdocs.org/sdr/97ZZZM522.md): Spar Cap · corroded · Sep 13, 1996 · N553NA · Boeing 7272J7 · Wing Spar
  > DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RT WING STATION 420 L/E FORWARD LOWER SPAR CAP CORRODED. FOUND TO BE IN LIMITS.
- [SDR 97ZZZM521](https://openairdocs.org/sdr/97ZZZM521.md): Spar Cap · corroded · Sep 13, 1996 · N553NA · Boeing 7272J7 · Wing Spar
  > DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RIGHT WING STATION 410.0 L/E FORWARD LOWER SPAR CAP CORRODED. MECH REMOVED CORROSION BOTTOM OF FORWARD CHORD AT RIGHT WING STATION 410 IAW B727 SRM 51-10-6. CORROSION REMOVAL WENT OUT OF LIMITS
- [SDR 97ZZZM516](https://openairdocs.org/sdr/97ZZZM516.md): Fitting · cracked · Sep 13, 1996 · N553NA · Boeing 7272J7 · Spoilers
  > DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND LT WING NR 5 SPOILER ACTUATOR FITTING IS CRACKED 2 PLACES. REMOVED AND REPLACED FITTING IAW SRM 51-30-2 AND 51-10-1. REMOVED AND REINSTALLED SPOILER PANEL TO FOM IAW MM 27-10-2. OPS CHECKED GO
- [SDR 97ZZZM514](https://openairdocs.org/sdr/97ZZZM514.md): Rib · cracked · Sep 13, 1996 · N553NA · Boeing 7272J7 · Wing, Rib/Bulkhead
  > DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RT WING STATION 738.5 LOWER RIB FLANGE IS CRACKED AT STRINGER NR 8 ATTACH POINT. STOP DRILLED CRACK IAW B 727 SRM 51-10-1. FABRICATED CHANNEL FROM 7075-0.080 4 INCH BY 15 INCH IAW B727 SRM 57-
- [SDR 97ZZZM511](https://openairdocs.org/sdr/97ZZZM511.md): Spar · corroded · Sep 13, 1996 · N553NA · Boeing 7272J7 · Wing Spar
  > DURING SCHEDULED INSPECTION AT AERO COP IN LAKE CITY, FL, FOUND LT WING STATION 491.5 L/E SPAR AFT OF NR 4 SLAT ACTUATOR CORRODED APPROX 6 INCHES IN LENGTH. MECH REMOVED CORROSION AT WS 491.5 L/E SPAR IAW B727-SRM 51-10-6. REMOVED AT.091 METAL 14 INCHES ORI
- [SDR 97ZZZM510](https://openairdocs.org/sdr/97ZZZM510.md): Spar · corroded · Sep 13, 1996 · N553NA · Boeing 7272J7 · Fuselage Main, Frame
  > DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND LT WING STATION 383 L/E SPAR AT NR 4 SLAT FORWARD OF ACTUATOR ROD CORRODED APPROXIMATELY 18 INCHES IN LENGTH. MECH REMOVED CORROSION AT LEFT WING L/E SPAR IAW SRM 51-10-6. REMOVED AT.058 18 INC
- [SDR 97ZZZM508](https://openairdocs.org/sdr/97ZZZM508.md): Spar · corroded · Sep 13, 1996 · N553NA · Boeing 7272J7 · Wing Spar
  > DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING STATION 546.5 L/E SPAR CORRODED FORWARD OF NR 4 SLAT ACTUATOR ARM. FOUND TO BE IN LIMITS.
- [SDR 97ZZZM507](https://openairdocs.org/sdr/97ZZZM507.md): Spar · corroded · Sep 13, 1996 · N553NA · Boeing 7272J7 · Wing Spar
  > DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RT WING STATION 629, L/E SPAR CORRODED AT ACTUATOR ARM NR 7. FOUND TO BE IN LIMITS.
- [SDR 97ZZZM505](https://openairdocs.org/sdr/97ZZZM505.md): Fitting · corroded · Sep 13, 1996 · N553NA · Boeing 7272J7 · Landing Gear Actuator
  > DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND NLG ACTUATOR ATTACH FITTING (AIRFRAME) CORRODED LT SIDE OUTBOARD. REMOVED NLG ATTACH FITTING FROM 2.799 TO 2.845. FABRICATED BUSHINGS TO 2.84700 (.002 INTERFENCE FIT). INSTALLED BUSHING WET WIT
- [SDR 97ZZZM503](https://openairdocs.org/sdr/97ZZZM503.md): Spar Cap · corroded · Sep 13, 1996 · N553NA · Boeing 7272J7 · Wing Spar
  > DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RT WING STATION 738.5 LEFT FORWARD LOWER SPAR CAP CORRODED. FOUND TO BE IN LIMIT.
- [SDR 97ZZZM504](https://openairdocs.org/sdr/97ZZZM504.md): Cowl · cracked · Sep 6, 1996 · N553NA · Boeing 7272J7 · Engine Cowling System
  > NR 3 ENGINE FIXED COWL FORWARD UPPER OUTER SKIN IS CRACKED 3 INCHES IN LENGTH 3H. REMOVED SECTION OF UPPER FORWARD OUTER SKIN 21 INCHES BY 1.3125 INCHES BY 11.25 INCHES FROM NR 3 ENGINE FIXED COWLING. FABRICATED NEW SECTION OF SKIN OUT OF 2024-T3.032. DRIL
- [SDR 97ZZZM513](https://openairdocs.org/sdr/97ZZZM513.md): Skin · corroded · Sep 4, 1996 · N553NA · Boeing 7272J7 · Leading Edge Devices
  > RIGHT WING LEADING EDGE 5 SLAT HAS CORROSION UNDER PANEL SS128. MECH REMOVED CORROSION AND TR WING LEADING EDGE SPAR IAW SRM 51-10-6. REMOVED AT.088 METAL ORIGINAL THICKNESS.360 MATERIAL ALLOWABLE.012 OUT OF LIMIT IAW SRM 57-10-1. NO CRACKS NOTED BY EDDY
- [SDR 97ZZZM512](https://openairdocs.org/sdr/97ZZZM512.md): Skin · delaminated · Sep 4, 1996 · N553NA · Boeing 7272J7 · Trailing Edge Flaps
  > ON THE UPPER SURFACE T/E OF THE INBD MID-FLAP ON ITS OUTBD T/E THE FLAP HAS BECOME DELAMINATED. ALSO, AT TWO OTHER SMALLER SPOTS ON ITS MIDDLE T/E OF THE SAME FLAP. REMOVED LT INBD FLAP IAW MM 27-51-31. REMOVED DELAMINATED SKIN AND CRUSHED HONEYCOMB IAW SRM
- [SDR 97ZZZM509](https://openairdocs.org/sdr/97ZZZM509.md): Spar · corroded · Sep 4, 1996 · N553NA · Boeing 7272J7 · Wing Spar
  > WING STATION LEADING EDGE SPAR JUST FORWARD OF NR 2 SLAT ACT ROD HAS CORROSION AT 3 INCHES LONGERON. MECH REMOVED CORROSION AT WING STATION 616.5 LE SPAR IAW SRM 51-10-6. REMOVED AT.024 METAL 6 INCHES LONG ORIGINAL THICKNESS.225 MAX OUT ALLOWABLE.012 OUT
- [SDR 97ZZZM506](https://openairdocs.org/sdr/97ZZZM506.md): Skin · corroded · Sep 4, 1996 · N553NA · Boeing 7272J7 · Wing, Plate/Skin
  > RIGHT WING UPPER LEFT END SKIN CORRODED AT MOUNT SCREWS FROM WS 170-760 FORWARD AND AFT CHORD. ACCOMPLISHED CORROSION REMOVAL ON RIGHT WING UPPER LT SPAR IAW SRM 51-10-6. INSTALLED TWO REPAIRS AT W/S NR 3 AND NR 4, 16 AND 18 BETWEEN W/S 190 AND 332. REPAIR
- [SDR 97ZZZM517](https://openairdocs.org/sdr/97ZZZM517.md): Skin · corroded · Sep 3, 1996 · N553NA · Boeing 7272J7 · Trailing Edge Flaps
  > RIGHT WING OUTBOARD FLAP, THE AFT FLAP HAS A CORRODED AREA AT 9 FEET FROM THE OUTBOARD END. REMOVED CORROSION, REVEALED PUNCTURE HOLE IN FLAP FULL OF FILLER. CUT OUT CORRODED AREA. REQUIRES COMPOSITE REPAIR. CLEANED OUT OLD POTTING MATERIAL. PRIMED AREA I
- [SDR 97ZZZM518](https://openairdocs.org/sdr/97ZZZM518.md): Fitting · damaged · Aug 30, 1996 · N553NA · Boeing 7272J7 · Fuselage, Landing Gear Attach Fittings
  > REMOVED AND REPLACED LT NOSE GEAR FITTING PER B727 MM 32 AND S/B 727-53-0119R2 PART 3. REMOVED AND REPLACED LT NOSE GEAR FITTING PER B727 M32 AND SB 727-53. (M)
- [SDR 96ZZZX4865](https://openairdocs.org/sdr/96ZZZX4865.md): Control Valve · cracked · Jun 27, 1996 · N553NA · Boeing 7272J7 · Trailing Edge Flap Control System
  > FLIGHT RETURN. LOST A-SYSTEM HYDRAULICS IN-FLIGHT DUE TO LOSS OF FLUID. FOUND OUTBOARD FLAP CONTROL VALVE LEAKING (DUE TO CRACK IN CASE). THE OUTBOARD FLAP CONTROL VALVE WAS REPLACED TO CORRECT THE PROBLEM.
- [SDR 96ZZZX3666](https://openairdocs.org/sdr/96ZZZX3666.md): Stringer · corroded · Dec 4, 1995 · N553NA · Boeing 7272J7 · Fuselage Main, Longeron/Stringer
  > WHILE PERFORMING CPCP TASK CARD NR C53-113-01.01, FOUND CORROSION BLEEDING FROM FASTENERS ON STR 26L BETWEEN STA 500 - STA 520 IN ZONE 1-13. OPEN AREA FOUND LEVEL 2 CORROSION ON STRINGER. REPLACED SECTION OF STRINGER FROM STA 480 TO STA 515. THE REMAINDER O

## 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 = 'N553NA' AND deregistration_id = 'N553NA-2017-02-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N553NA-2017-02-28/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.