# Service difficulty reports: N16301, cancelled Mar 21, 2013

A list on [N16301, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N16301-2013-03-21.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 2 · 89 reports

- [SDR CALA0800546](https://openairdocs.org/sdr/CALA0800546.md): Megaphone · defective · Jun 5, 2008 · N16301 · Boeing 7373T0 · Emergency Equipment
  > A/C MEGAPHONE MISSING VOLUME KNOB AND LOW IN VOLUME. REPLACED MEGAPHONE, OPS CHECK GOOD.
- [SDR CALA0800139](https://openairdocs.org/sdr/CALA0800139.md): Skin · cracked · Feb 14, 2008 · N16301 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > STA 747 ABOVE STRINGER 24 FOUND 1.8" LONG CRACK WHILE PERFORMING C-SCAN INSPECTION. REPAIRED FUSELAGE PER SRM 53-00-01 REPAIR 31 DETAIL X.
- [SDR CALA0700702](https://openairdocs.org/sdr/CALA0700702.md): Skin · cracked · Nov 27, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > FUSE SKIN CRACK INDICATION RT SIDE 39 INCHES AFT OF AFT BIN DOOR FRAME & 30 INCHES ABOVE LAP SEAM. COMPLETED SKIN REPAIR 31 PER SRM 53-00-01 AND REPAIR DEVIATION PER ECRA 5331-01365.
- [SDR CALA0700699](https://openairdocs.org/sdr/CALA0700699.md): Skin · cracked · Nov 25, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > CRACK IN FUSELAGE SKIN 10 INCHES ABOVE LAP JOINT AND 11 INCHES AFT OF AFT UPPER BODY FAIRING RIGHT SIDE AT STATION 727A AND STRINGER S-19R. REPAIRED FUSELAGE SKIN PER SRM 53-00-01.
- [SDR CALA0700564](https://openairdocs.org/sdr/CALA0700564.md): Reflector · contaminated · Oct 4, 2007 · N16301 · Boeing 7373TO · Emergency Lighting
  > THE L-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE EMERGENCY LIGHT REFLECTOR ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-02 AND 33-51-11.
- [SDR CALA0700443](https://openairdocs.org/sdr/CALA0700443.md): Frame · corroded · Aug 18, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FORWARD CORROSION AT ACCESS DOOR AFT FRAME IN BULKHEAD CHORD, BS 227.8 BETWEEN LBL 5.7 AND RBL 5.7. REPAIRED IAW ECRA 5311-01353.
- [SDR CALA0700115](https://openairdocs.org/sdr/CALA0700115.md): Drag Angle · cracked · Mar 2, 2007 · N16301 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > LEFT UPPER WING TO BODY DRAG ANGLE CRACKED FWD OF A/C DOOR 3302L. REPAIRED IAW ECRA 5311-01300.
- [SDR CALA0700114](https://openairdocs.org/sdr/CALA0700114.md): Frame · cracked · Mar 2, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Frame
  > LEFT MAIN FRAME CRACKED AT STA 639. REPAIRED IAW ECRA 5311-01299.
- [SDR CALA0700113](https://openairdocs.org/sdr/CALA0700113.md): Web · cracked · Mar 2, 2007 · N16301 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > CRACKED AT WEB STA 639 ABOVE FLOOR LINE. REPAIRED IAW ECRA 5311-01299.
- [SDR CALA0700116](https://openairdocs.org/sdr/CALA0700116.md): Fitting · cracked · Mar 1, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > INSPECTION FOUND A.5 INCH CRACK IN UPPER RADIUS OF FITTING AFT OF FRAME JUST BELOW STRINGER 17L AND CREASE BEAM AT STA 616. A NEW FITTING WAS INSTALLED IAW SRM 51-10-2 AND 51-40-02.
- [SDR CALA0700103](https://openairdocs.org/sdr/CALA0700103.md): Beam · cracked · Mar 1, 2007 · N16301 · Boeing 7373T0 · Passenger/Crew Doors
  > CRACKED L1 DOOR AFT SIDE OF THE THIRD FROM BOTTOM DOOR STOP CUTOUT. REPAIRED IAW ECRA 5210-01919.
- [SDR CALA0700102](https://openairdocs.org/sdr/CALA0700102.md): Skin · cracked · Feb 28, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > A 2 INCH CRACK IN R1 DOOR AT THE LOWER BOTTOM CORNER. REPAIRED IAW ECRA 5331-01291.
- [SDR CALA0700101](https://openairdocs.org/sdr/CALA0700101.md): Skin · cracked · Feb 28, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > A 3 INCH CRACK LOWER AFT FUSELAGE STA 727D AND 727E. REPAIRED IAW ECRA5331-01292.
- [SDR CALA0700100](https://openairdocs.org/sdr/CALA0700100.md): Frame · cracked · Feb 27, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT CRACKED ON FWD BULKHEAD FRAME. INSTALLED STIFFENER IAW SRM 51-10-02, 51-30-01, AND 51-40-02.
- [SDR CALA0700096](https://openairdocs.org/sdr/CALA0700096.md): Frame · corroded · Feb 25, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Frame
  > AFT CARGO FLOOR FRAME AT STA 747 IS CORRODED FROM STR 26L TO 26R. REPAIRED IAW SRM 53-00-07 DETAIL 2, 51-40-02 & 51-10-02.
- [SDR CALA0700094](https://openairdocs.org/sdr/CALA0700094.md): Keelbeam · damaged · Feb 24, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Keel
  > LOWER FUSE SKIN BULGED BETWEEN RIVETS ALONG STRINGER 28R STA 500C TO 500D. REPAIRED KEEL BEAM IAW SRM 53-60-12.
- [SDR CALA0700093](https://openairdocs.org/sdr/CALA0700093.md): Keelbeam · corroded · Feb 24, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Keel
  > AFT CARGO COMPARTMENT CORRODED AT KEEL BEAM STA 727, LBL 6. REPAIRED IAW ECRA 5311-01293 AND 5311-01296.
- [SDR CALA0700092](https://openairdocs.org/sdr/CALA0700092.md): Pan · cracked · Feb 23, 2007 · N16301 · Boeing 7373T0 · Cargo/Baggage Doors
  > C2 DOOR FWD SIDE PAN CRACKED AT SPLICE POINT. INSTALLED NEW PAN IAW SRM 52-30-02.
- [SDR CALA0700091](https://openairdocs.org/sdr/CALA0700091.md): Pan · cracked · Feb 23, 2007 · N16301 · Boeing 7373T0 · Doors
  > UPPER FWD PAN CRACKED AT FWD SPLICE. INSTALLED SERVICEABLE PAN.
- [SDR CALA0700089](https://openairdocs.org/sdr/CALA0700089.md): Bulkhead · corroded · Feb 23, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > FWD APB LOWER CENTER SECTION WEB CORRODED. REPAIRED IAW ECRA 5311-01298.
- [SDR CALA0700088](https://openairdocs.org/sdr/CALA0700088.md): Structure · bulged · Feb 23, 2007 · N16301 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > FWD BAG BIN BULGED ALONG S28L FROM STA 500D 6 INCHES. REPAIRED IAW SRM 53-30-12.
- [SDR CALA0700090](https://openairdocs.org/sdr/CALA0700090.md): Support Angle · cracked · Feb 22, 2007 · N16301 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > SUPPORT ANGLE CRACKED AT 360 AND STRINGER S11L. REPAIRED IAW ECRA 5311-01297.
- [SDR CALA0700083](https://openairdocs.org/sdr/CALA0700083.md): Frame · corroded · Feb 22, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND AFT CARGO COMPARTMENT FLOOR FRAME CORRODED AT STA 847 BETWEEN STRINGERS 27L AND 27R, LBL 8 TO RBL 8. THE CORRODED SECTION OF FLOOR FRAME WAS REMOVED AT FLOOR FRAME ATTACH AND A SHEAR TIE REPAIR WAS INSTALLED IAW SRM 53-00-07.
- [SDR CALA0700082](https://openairdocs.org/sdr/CALA0700082.md): Stringer · corroded · Feb 21, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LIGHT SURFACE CORROSION DOWN CENTER OF STRINGER 26L IN FORWARD BAGGAGE BIN AT STA 500D-520. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.
- [SDR CALA0700081](https://openairdocs.org/sdr/CALA0700081.md): Skin · cracked · Feb 20, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 0.75 INCH CRACK IN FUSELAGE SKIN AT R-2 DOOR FORWARD LOWER RADIUS, STA 947.5, S14R. A DOUBLER WAS INSTALLED IAW SRM 53-60-01, FIGURE 201.
- [SDR CALA0700075](https://openairdocs.org/sdr/CALA0700075.md): Frame · corroded · Feb 20, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT CENTER FLOOR AREA, STA 867, S28L TO S28R. THE CORRODED SECTION OF FRAME WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 201.
- [SDR CALA0700067](https://openairdocs.org/sdr/CALA0700067.md): Stiffener · corroded · Feb 15, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND TWO CHANNEL STIFFENERS CORRODED ON FORWARD FACE OF APB LOWER SECTION. THE STIFFENERS WERE REMOVED AND NEW SECTIONS WERE SPLICED IN IAW BOEING DRAWING 65C28106.
- [SDR CALA0700066](https://openairdocs.org/sdr/CALA0700066.md): Stringer · corroded · Feb 15, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND CENTER OF STRINGER 27L CORRODED AROUND NUT PLATE IN FORWARD BAGGAGE BIN AT STA 500D. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.
- [SDR CALA0700062](https://openairdocs.org/sdr/CALA0700062.md): Floorbeam · corroded · Feb 11, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 947, RBL 6 TO LBL 6. A FLOORBEAM REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 201.
- [SDR CALA0700061](https://openairdocs.org/sdr/CALA0700061.md): Frame · cracked · Feb 11, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN RT MAIN FRAME AT STA 616 BELOW FLOOR LINE. THE CRACKED AREA OF FRAME WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED IAW ECRA 5311-01158.
- [SDR CALA0700060](https://openairdocs.org/sdr/CALA0700060.md): Floorbeam · corroded · Feb 10, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT NUT PLATES ON TOP AND BOTTOM, STA 1016, LBL 6 TO LBL 34. THE FLOORBEAM CHORD WAS REMOVED AND REPLACED IAW ECRA 5310-03851.
- [SDR CALA0700059](https://openairdocs.org/sdr/CALA0700059.md): Frame · cracked · Feb 9, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN LT FRAME AT STA 616, S17L TO S18L BELOW FLOOR LINE. THE CRACKED AREA OF FRAME WAS REMOVED AND A REPAIR ANGLE AND FILLER WAS INSTALLED IAW ECRA 5311-01158.
- [SDR CALA0700054](https://openairdocs.org/sdr/CALA0700054.md): Frame · cracked · Feb 6, 2007 · N16301 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN FRAME AT STA 597, S13L. THE FRAME WAS REPAIRED IAW SRM 53-00-07, PAGE 203, FIGURE 201.
- [SDR CALA0600511](https://openairdocs.org/sdr/CALA0600511.md): Skin · cracked · Dec 11, 2006 · N16301 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 727A-727B, S22R TO S25R. REPAIRED IAW ECRA 5331-01283.
- [SDR CALA0600225](https://openairdocs.org/sdr/CALA0600225.md): Frame · corroded · Jun 26, 2006 · N16301 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR FORWARD FRAME CORRODED. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-80-02.
- [SDR CALA0500132](https://openairdocs.org/sdr/CALA0500132.md): Panel · cracked · Apr 18, 2005 · N16301 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT STA 727D, STRINGER 23R. REPLACED PANEL PER ECRA 5331-01178A.
- [SDR CALA0500076](https://openairdocs.org/sdr/CALA0500076.md): Skin · cracked · Mar 11, 2005 · N16301 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1.7 INCH CRACK IN FUSELAGE SKIN THREE INCHES AFT OF STA 727D JUST BELOW S23R ON BONDED DOUBLER LINE. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5331-01178.
- [SDR CALA0500066](https://openairdocs.org/sdr/CALA0500066.md): Stiffener · cracked · Mar 4, 2005 · N16301 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND 8 INCH CRACK IN STIFFENER FOR NR 3 VHF ANTENNA BETWEEN STA 727D AND 727E. A NEW STIFFENER WAS INSTALLED IAW SRM 51-40-2.
- [SDR CALA0300165](https://openairdocs.org/sdr/CALA0300165.md): Skin · cracked · Apr 1, 2003 · N16301 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 0.4 INCH CRACK IN SKIN AT UPPER FORWARD CORNER OF PILOT'S WINDOW CD POST AT BS 205, WL 238. REPAIRED IAW SRM 53-10-01, FIGURE 210.
- [SDR CALA0300164](https://openairdocs.org/sdr/CALA0300164.md): Floorbeam · corroded · Apr 1, 2003 · N16301 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND TOP SURFACE OF TOP CAP OF LATERAL FLOORBEAM AT STA 1016 CORRODED AT LT SIDE AREA UNDER LAV TANK. REPAIRED IAW ECRA 5310-03851.
- [SDR CALA0300163](https://openairdocs.org/sdr/CALA0300163.md): Skin · dented · Apr 1, 2003 · N16301 · Boeing 7373T0 · Galley Doors
  > INSPECTION FOUND R-2 DOOR EXTERNAL SKIN DENTED AT FORWARD LOWER CORNER. REPAIRED IAW SRM 52-00-01.
- [SDR CALA0300162](https://openairdocs.org/sdr/CALA0300162.md): Bulkhead · cracked · Apr 1, 2003 · N16301 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND TWO 0.1 INCH CRACKS AT RIVET HOLES IN AFT PRESSURE BULKHEAD BETWEEN S6L AND S7L AT BS 1016. REPAIRED IAW SRM 53-80-08, FIGURE 202 AND 207.
- [SDR CALA0300161](https://openairdocs.org/sdr/CALA0300161.md): Stringer · corroded · Apr 1, 2003 · N16301 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND AFT CARGO COMPARTMENT STRINGER 26R CORRODED AT BS 1010. REPAIRED IAW SRM 51-40-02 AND B737-300 AMM 20-50-11.
- [SDR CALA0300157](https://openairdocs.org/sdr/CALA0300157.md): Frame · corroded · Mar 31, 2003 · N16301 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND AFT CARGO COMPARTMENT LOWER LOBE INTERIOR FRAME CORRODED AT BS 847 BETWEEN S28L AND S28R. REPAIRED IAW SRM 53-00-07, FIGURE 208.
- [SDR CALA0300156](https://openairdocs.org/sdr/CALA0300156.md): Floorbeam · corroded · Mar 31, 2003 · N16301 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 312 AND 320, R-1 DOOR THRESHOLD. REPAIRED WITH REPLACEMENT PART IAW SRM 51-40-02.
- [SDR CALA0300155](https://openairdocs.org/sdr/CALA0300155.md): Skin · torn · Mar 31, 2003 · N16301 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FORWARD CARGO DOOR SKIN CUTOUT TORN AT BS 440, S24R. THE SKIN WAS REPAIRED IAW ECRA 5330-03222.
- [SDR CALA0300154](https://openairdocs.org/sdr/CALA0300154.md): Skin · gouged · Mar 28, 2003 · N16301 · Boeing 7373T0 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND LT HORIZONTAL STABILIZER LEADING EDGE SKIN GOUGED AT STA 176.50. REPAIRED IAW ECRA 5515-01008.
- [SDR CALA0300153](https://openairdocs.org/sdr/CALA0300153.md): Skin · dented · Mar 28, 2003 · N16301 · Boeing 7373T0 · Vertical Stabilizer, Plate/Skin
  > INSPECTION FOUND VERTICAL STABILIZER LEADING EDGE SKIN DENTED AT L/E STA 132.92 + 6 AND AT 226.54 + 1.3. THE DENTED AREAS WERE REPAIRED IAW SRM 55-30-01, FIGURE 203.
- [SDR CALA0300152](https://openairdocs.org/sdr/CALA0300152.md): Stringer · punctured · Mar 28, 2003 · N16301 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 24R PUNCTURED AT BS 363. REPAIRED IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0300151](https://openairdocs.org/sdr/CALA0300151.md): Stringer · corroded · Mar 28, 2003 · N16301 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 25R CORRODED AT BS 364 AND S24R WAS CORRODED AT BS 360. REPAIRED IAW SRM 53-00-03, FIGURE 201.

Next page: https://openairdocs.org/deregistered/N16301-2013-03-21/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 = 'N16301' AND deregistration_id = 'N16301-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N16301-2013-03-21/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.