# Service difficulty reports: N17356, cancelled Mar 21, 2013

A list on [N17356, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N17356-2013-03-21.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 · 105 reports

- [SDR CALA2009022300105](https://openairdocs.org/sdr/CALA2009022300105.md): Cable Assy · frayed · Feb 22, 2009 · N17356 · Boeing 7373T0 · Escape Slide
  > L-2 DOOR EMERGENCY ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS. REPLACED L-2 DOOR EMERGENCY ESCAPE SLIDE LATCH CABLE PER MM 25-61-35.
- [SDR CALA0800948](https://openairdocs.org/sdr/CALA0800948.md): Keelbeam · corroded · Oct 6, 2008 · N17356 · Boeing 7373T0 · Fuselage Main, Keel
  > RIGHT KEEL BEAM HAS CORROSION ON OUTBOARD FLANGE AT STATION 500D PLUS 3 - 6. REPAIRED KEEL BEAM RIGHT SIDE PER SRM 53-60-12 PAGE 206 FIGURE 201.
- [SDR CALA0800946](https://openairdocs.org/sdr/CALA0800946.md): Intercostal · cracked · Oct 6, 2008 · N17356 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > WEB CRACKED BODY STATION 294.3 LT INTERCOSTAL 16. REMOVED AND REPLACED CRACKED WEB PER ECRA 5311-01424 REV A.
- [SDR CALA0800945](https://openairdocs.org/sdr/CALA0800945.md): Intercostal · cracked · Oct 6, 2008 · N17356 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > WEB CRACKED BODY STATION 294.3 LT INTERCOSTAL 12. REMOVED AND REPLACED CRACKED WED PER ECRA 5311-01424 REV A.
- [SDR CALA0800942](https://openairdocs.org/sdr/CALA0800942.md): Attach Fitting · cracked · Oct 2, 2008 · N17356 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > ATTACH CLIP STATION 294.5 LT STR 10 CRACKED. INSTALLED REPAIR/MODIFICATION PER ECRA 5311-01423.
- [SDR CALA0800937](https://openairdocs.org/sdr/CALA0800937.md): Skin · cracked · Oct 1, 2008 · N17356 · Boeing 7373T0 · Cargo/Baggage Doors
  > C-2 DOOR EXTERIOR SKIN CRACKED AT HANDLE CUTOUT AFT UPPER CORNER. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 52-00-01 FIG 201.
- [SDR CALA0800930](https://openairdocs.org/sdr/CALA0800930.md): Web · cracked · Oct 1, 2008 · N17356 · Boeing 7373T0 · Cargo/Baggage Doors
  > C2 DOOR WEB CRACKED ON UPPER FORWARD SIDE UNDER PULLEY BRACKET OF COUNTER BALANCE. INSTALLED NEW FRAME PER 51-40-02.
- [SDR CALA0800929](https://openairdocs.org/sdr/CALA0800929.md): Skin · damaged · Oct 1, 2008 · N17356 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CREASED AFT OF PREVIOUS REPAIR, STATION 847 AT S-4L. REPAIRED PER SRM 53-00-01 FIG 201, PAGE 23.
- [SDR CALA0800928](https://openairdocs.org/sdr/CALA0800928.md): Skin · cracked · Sep 29, 2008 · N17356 · Boeing 7373T0 · Passenger/Crew Doors
  > L-1 DOOR SKIN IS CRACKED AT 5TH STOP FROM TOP. TRIMMED OUT CRACK AND INSTALLED REPAIR DOUBLER PER ECRA 5210-02035.
- [SDR CALA0800927](https://openairdocs.org/sdr/CALA0800927.md): Skin · cracked · Sep 29, 2008 · N17356 · Boeing 7373T0 · Passenger/Crew Doors
  > L-1 DOOR SKIN IS CRACKED AT 4TH STOP FROM TOP, AFT SIDE OF DOOR. TRIMMED OUT CRACK AND INSTALLED REPAIR DOUBLER PER ECRA 5210-02035.
- [SDR CALA0800926](https://openairdocs.org/sdr/CALA0800926.md): Frame · corroded · Sep 29, 2008 · N17356 · Boeing 7373T0 · Fuselage Main, Frame
  > B737-53-4-0033 NWW LT TUNNEL LEVELING COMPOUND AT BOTTOM AREA BETWEEN FRAMES 259.5 AND 277 IS BUBBLED UP AND LOOSE CTN 53-310-202 SEQ 309 03-5310-1-2613. REMOVED AND REPLACED LT NWW CHORD REF SRM 51-40-02 AND BOEING DWG 65-45819.
- [SDR CALA0800921](https://openairdocs.org/sdr/CALA0800921.md): Skin · gouged · Sep 26, 2008 · N17356 · Boeing 7373T0 · Horizontal Stabilizer, Plate/Skin
  > 02/21/2008, LEFT HORIZONTAL STABILIZER STATION 108 16 INCHES AFT OF LEADING EDGE PANEL APPROXIMATELY 8.5" X 2.5" X.300 DEPTH. COMPLETED INTERIM REPAIR OF LEFT HORIZONTAL STABILIZER PER SRM 55-10-01 REPAIR 4, ISSUED DIP TO INSPECT FASTENERS EVERY 3,000 FLT HR
- [SDR CALA0800920](https://openairdocs.org/sdr/CALA0800920.md): Skin · cracked · Sep 25, 2008 · N17356 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > R1 DOOR FUSELAGE SKIN AFT OF LOWER CUTOUT CRACKED. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PLATES AND FILLERS PER SRM 53-10-01 REPAIR 2. RESTORATION OF AIRCRAFT FINISH WILL BE ACCOMPLISHED ON L/P 9698525 SEQ N00667.
- [SDR CALA0800908](https://openairdocs.org/sdr/CALA0800908.md): Floorbeam · corroded · Sep 17, 2008 · N17356 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > STATION 986.5 FLOORBEAM SURFACE CORROSION AT LBL 29 AND LBL 32. INSTALLED REPAIR STRAP PER SRM 53-00-51 FIGURE 201.
- [SDR CALA0800483](https://openairdocs.org/sdr/CALA0800483.md): Skin · cracked · May 21, 2008 · N17356 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > CRACK AT AFT END OF E&E COOLING EXHAUST PORT AT CENTER OF FUSELAGE. INSTALLED REPAIR PER EC/RA 5330-03806, STEPS 1-19. PLACED ON DIP FOR PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 12 MONTHS.
- [SDR CALA0800165](https://openairdocs.org/sdr/CALA0800165.md): Floorbeam · corroded · Feb 21, 2008 · N17356 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON CABIN LATERAL FLOORBEAM UPPER CAP AT BS 344 AND LBL 6.0 AS VIEWED FROM E&E CEILING. INSTALLED REPAIR PER SRM 53-10-51.
- [SDR CALA0800164](https://openairdocs.org/sdr/CALA0800164.md): Floorbeam · corroded · Feb 21, 2008 · N17356 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON FLOORBEAM AT BS 328 AND LBL 30.0 AS SEEN FROM E&E COMPARTMENT CEILING. INSTALLED REPAIR AND REPAIR PARTS PER SRM 53-10-51.
- [SDR CALA0700589](https://openairdocs.org/sdr/CALA0700589.md): Skin · cracked · Oct 16, 2007 · N17356 · Boeing 7373T0 · Cargo/Baggage Doors
  > FWD CARGO DOOR INNER SKIN LIGHTNING HOLE CRACKED, AFT SIDE CENTER ROW. REPAIRED SKIN IAW ECRA 5232-01094.
- [SDR CALA0600529](https://openairdocs.org/sdr/CALA0600529.md): Skin · corroded · Dec 18, 2006 · N17356 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND SURFACE CORROSION ON SKIN UNDER NR 1 DME ANTENNA AT STA 460-480, S29L. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5331-01285.
- [SDR CALA0600528](https://openairdocs.org/sdr/CALA0600528.md): Frame · corroded · Dec 18, 2006 · N17356 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME CORRODED AT STA 227, S28L TO S28R, LBL 4 TO RBL 4. THE FRAME WAS REPAIRED IAW ECRA 5311-01286.
- [SDR CALA0600525](https://openairdocs.org/sdr/CALA0600525.md): Skin · cracked · Dec 16, 2006 · N17356 · Boeing 7373T0 · Spoilers
  > INSPECTION FOUND A 0.125 INCH CRACK IN NR 3 SPOILER UPPER SKIN. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-70-01.
- [SDR CALA0600524](https://openairdocs.org/sdr/CALA0600524.md): Skin · cracked · Dec 16, 2006 · N17356 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A.25 INCH CRACK AT FASTENERS (11 EACH) IN RIGHT WING NR 5 SLAT LOWER SKIN. THE SLAT SKIN WAS REPAIRED IAW SRM 57-43-01.
- [SDR CALA0600523](https://openairdocs.org/sdr/CALA0600523.md): Skin · cracked · Dec 16, 2006 · N17356 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A 5 INCH CRACK AT FASTENER IN RIGHT WING NR 6 SLAT LOWER SKIN. THE CRACKED AREA WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-43-01.
- [SDR CALA0500302](https://openairdocs.org/sdr/CALA0500302.md): Charger · inoperative · Sep 5, 2005 · N17356 · Boeing 7373T0 · Emergency Lighting
  > INSPECTION FOUND SEAT 21 ABC EMERGENCY LIGHT INOPERATIVE. THE BATTERY CHARGER ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-81.
- [SDR CALA0400638](https://openairdocs.org/sdr/CALA0400638.md): Skin · cracked · Sep 2, 2004 · N17356 · Boeing 7373T0 · Passenger/Crew Doors
  > INSPECTION FOUND A.5 INCH CRACK IN THE MID INNER SKIN PANEL OF THE FORWARD ENTRY DOOR. THE SKIN WAS REPAIRED IAW ECRA 5211-01072.
- [SDR CALA0400626](https://openairdocs.org/sdr/CALA0400626.md): Skin · cracked · Sep 1, 2004 · N17356 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A 1 INCH CRACK IN NR 3 SLAT LOWER EXTERNAL SKIN AT WS 270. A REPAIR WAS INSTALLED IAW SRM 57-43-01.
- [SDR CALA0400619](https://openairdocs.org/sdr/CALA0400619.md): Skin · loose · Aug 26, 2004 · N17356 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND SMOKING AND LOOSE RIVETS IN FUSELAGE SKIN AT STA 1006-1016, S2L TO S3L. REMOVED AND REPLACED DOUBLER IAW SRM 53-00-01, FIGURE 229, PAGE 332.
- [SDR CALA0400618](https://openairdocs.org/sdr/CALA0400618.md): Floorbeam · corroded · Aug 25, 2004 · N17356 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 21. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-51, FIGURE 205.
- [SDR CALA0400637](https://openairdocs.org/sdr/CALA0400637.md): Floorbeam · cracked · Aug 24, 2004 · N17356 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A CRACK IN THE LONGITUDINAL FLOORBEAM UPPER CHORD AT ITS ATTACHMENT TO THE TRANSVERSE FLOORBEAM AT STA 727B, LBL 45.50. THE CRACK WAS LOCATED ON THE OB SIDE OF THE LONGITUDINAL FLOORBEAM AT THE FIRST HI-LOK FASTENER HOLE FORWARD OF STA 727B.
- [SDR CALA0400614](https://openairdocs.org/sdr/CALA0400614.md): Floorbeam · corroded · Aug 24, 2004 · N17356 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT UPPER FLANGE STA 986.5 FROM BL 0 TO RBL 36. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW ECRA 5310-03851.
- [SDR CALA0400613](https://openairdocs.org/sdr/CALA0400613.md): Angle · corroded · Aug 24, 2004 · N17356 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ZEE ANGLE CORRODED AT R-2 DOOR, STA 967-986.5, RBL 45. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.
- [SDR CALA0400612](https://openairdocs.org/sdr/CALA0400612.md): Seat Track · cracked · Aug 24, 2004 · N17356 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND A 1 INCH CRACK IN LEFT O/B SEAT TRACK AT STA 727B. THE CRACKED AREA WAS CUT OUT AND A REPAIR STRAP WAS INSTALLED IAW ECRA 5321-01200.
- [SDR CALA0400610](https://openairdocs.org/sdr/CALA0400610.md): Stringer · cracked · Aug 23, 2004 · N17356 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT STA 500C. A NEW STRINGER SECTION WAS SPLICED IN IAW SRM 53-00-03.
- [SDR CALA0300306](https://openairdocs.org/sdr/CALA0300306.md): Floor Support · cracked · Jun 11, 2003 · N17356 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK AND UPPER SHIM DAMAGE IN FLOOR PANEL SUPPORT AT STA 540, LBL 10. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0300305](https://openairdocs.org/sdr/CALA0300305.md): Skin · dented · Jun 10, 2003 · N17356 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT BAGGAGE BIN DOOR SKIN DENTED AT CENTER AREA 38 INCHES FROM BOTTOM AND FORWARD 22 INCHES FROM AFT WITH A DEPTH OF 0.128 INCH, 3.5 INCH WIDTH, AND 6 INCHES IN LENGTH. THE DENTED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52
- [SDR CALA0200305](https://openairdocs.org/sdr/CALA0200305.md): Socket · inoperative · May 21, 2002 · N17356 · Boeing 7373T0 · Emergency Lighting
  > EMERGENCY ESCAPE PATH AISLE LIGHT INOP AT SEAT 23 LEFT. REPLACED LIGHT SOCKET ASSEMBLY PER MM 33-51-81.
- [SDR CALA0100211](https://openairdocs.org/sdr/CALA0100211.md): Floorbeam · cracked · Mar 6, 2001 · N17356 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A.25 INCH CRACK IN FLOORBEAM AT STA 520, RBL 45.5. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-04105 AND EA 04-5310-0669.
- [SDR CALA0100204](https://openairdocs.org/sdr/CALA0100204.md): Floorbeam · corroded · Mar 4, 2001 · N17356 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER FLANGE CORRODED AT STA 294.5, BL 0. THE FLOORBEAM UPPER FLANGE WAS REPAIRED IAW ECRA 5310-04110 AND EA 04-5310-0697.
- [SDR CALA0100203](https://openairdocs.org/sdr/CALA0100203.md): Skin · cracked · Mar 4, 2001 · N17356 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE EXTERNAL SKIN AT R-1 DOOR LOWER HINGE CUTOUT. THE SKIN WAS REPAIRED IAW ECRA 5330-03036 AND EA 04-5311-0688.
- [SDR CALA0100201](https://openairdocs.org/sdr/CALA0100201.md): Skin · gouged · Mar 3, 2001 · N17356 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A VERTICAL GOUGE IN FUSELAGE EXTERNAL SKIN FROM WINDOW EDGE TO LAP SEAM AT STA 877, STRINGER 14L. THE SKIN WAS REPAIRED IAW ECRA 5330-03037.
- [SDR CALA0100197](https://openairdocs.org/sdr/CALA0100197.md): Door Frame · dented · Mar 3, 2001 · N17356 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND FORWARD CARGO DOOR JAMB DENTED AT STA 492, FLOOR LINE. THE DENTED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-70-13.
- [SDR CALA0100196](https://openairdocs.org/sdr/CALA0100196.md): Stringer · cracked · Mar 3, 2001 · N17356 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A CRACK APPROXIMATELY.25 INCH LONG AT HOLE IN STRINGER 21L BETWEEN STA 460 - 480. THE HOLE WAS REAMED TO 0.312 INCH. AN ANGLE REPAIR WAS INSTALLED IAW SRM 53-00-03.
- [SDR CALA0100194](https://openairdocs.org/sdr/CALA0100194.md): Floorbeam · corroded · Mar 2, 2001 · N17356 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES ON TOP SURFACE AT STA 947, RBL 12 TO LBL 25. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5310-03851.
- [SDR CALA0100192](https://openairdocs.org/sdr/CALA0100192.md): Skin · delaminated · Mar 2, 2001 · N17356 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING L/E DELAMINATED AT WBL 254.0. THE LEADING EDGE WAS REPAIRED IAW SRM 57-41-01, FIGURE 2, 51-70-16, PARAGRAPH 3A, ECRA 5720-01838, AND EA 04-5741-0672.
- [SDR CALA0100191](https://openairdocs.org/sdr/CALA0100191.md): Skin · dented · Mar 2, 2001 · N17356 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 344 AND TWO INCHES BELOW S19R. THE DENTED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5330-03035 AND EA 04-5310-0679.
- [SDR CALA0100190](https://openairdocs.org/sdr/CALA0100190.md): Intercostal · cracked · Mar 2, 2001 · N17356 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL CRACKED BETWEEN STA 500D AND 520, RBL 45, WL 208.1. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-2.
- [SDR CALA0100189](https://openairdocs.org/sdr/CALA0100189.md): Door Frame · dented · Mar 2, 2001 · N17356 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND FORWARD CARGO DOOR JAMB DENTED AT STA 440 AT FLOOR LINE. THE DENTED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW DRAWING 69-15224 AND SRM 51-70-13.
- [SDR CALA0100188](https://openairdocs.org/sdr/CALA0100188.md): Web · cracked · Mar 2, 2001 · N17356 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK BETWEEN RIVETS ON FORWARD EDGE OF WEB ON AFT CARGO DOOR CUTOUT AFT SIDE, BS 847 BETWEEN S24R AND S25R. THE CRACKED AREA OF WEB WAS REMOVED AND A REPAIR WEB WAS INSTALLED IAW SRM 53-60-15, 51-20-01, AND 51-40-02.
- [SDR CALA0100185](https://openairdocs.org/sdr/CALA0100185.md): Web · cracked · Mar 1, 2001 · N17356 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.25 INCH CRACK IN WEB AT FRAME OF AFT PIT CUTOUT AREA, FORWARD SIDE, BS 787, S25R. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 53-60-15, FIGURE 1, 51-20-01, AND 51-40-01.
- [SDR CALA0100184](https://openairdocs.org/sdr/CALA0100184.md): Floor Support · corroded · Mar 1, 2001 · N17356 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 967 - 986, LBL 16. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-2.

Next page: https://openairdocs.org/deregistered/N17356-2013-03-21/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 = 'N17356' AND deregistration_id = 'N17356-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17356-2013-03-21/reports

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