# Service difficulty reports: Boeing 737-290C

A list on [Boeing 737-290C](https://openairdocs.org/model/boeing-737-290c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 29 · 1,409 reports

- [SDR TSAA20141128048](https://openairdocs.org/sdr/TSAA20141128048.md): Skin · cracked · Nov 25, 2014 · N842AL · Boeing 737290C · Fuselage Main, Plate/Skin
  > DISCOVERED 1.25 INCH SKIN CRACK APPROX 2 INCHES FWD OF BS 540 BETWEEN STRINGER 1 & 2L. REPAIRED IAW SRM 53-30-3 FIG 48 DETAIL XXIII PROCEDURE III & VII.
- [SDR TSAA20141010009](https://openairdocs.org/sdr/TSAA20141010009.md): Control Unit · faulty · Oct 10, 2014 · N842AL · Boeing 737290C · APU Controls
  > APU AUTO SHUTDOWN DUE TO OVERSPEED DURING FLIGHT, EMER DECLARED. ADJUSTED APU ENG SPEED IAW AMM 49-11-00. R & R APU CONTROL UNIT IAW 49-61-11. R & R ELECTRONIC SPEED SWITCH IAW 49-61-22. R & R APU FUEL CONTROL UNIT IAW 49-31-11.
- [SDR TSAA20140601004](https://openairdocs.org/sdr/TSAA20140601004.md): Skin · cracked · Jun 1, 2014 · N842AL · Boeing 737290C · Fuselage Main, Plate/Skin
  > SKIN HAS A CRACK INDICATION AT BS 312 BELOW STRINGER 19R. REPAIRED FUSELAGE IAW SRM 53-30-3 FIGURE 48.
- [SDR 7AHR20130130001](https://openairdocs.org/sdr/7AHR20130130001.md): Skin · corroded · Jan 30, 2013 · N842AL · Boeing 737290C · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT BS 1121, AT STRINGER 20R HAS FASTENERS PULLING THROUGH SKIN LOCATED ABOVE APU ACCESS DOOR CUT OUT. AFTER REMOVAL OF FASTENERS IT WAS DETERMINED THAT WHITE POWDER AND CORRODED METAL CAME OUT OF THE FASTENER HOLES. AFTER A CUT OUT OF THE CORRO
- [SDR 7AHR20130129014](https://openairdocs.org/sdr/7AHR20130129014.md): Skin · worn · Jan 29, 2013 · N842AL · Boeing 737290C · Nacelle/Pylon, Plate/Skin
  > RT ENGINE COWL WORN. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW REPAIR DOUBLER ON THE RT ENGINE COWL IAW SRM 51-40-3.
- [SDR 7AHR20130129013](https://openairdocs.org/sdr/7AHR20130129013.md): Rib · worn · Jan 29, 2013 · N842AL · Boeing 737290C · Nacelle/Pylon, Frame/Spar/Rib
  > RT ENGINE COWL HAS AN AREA OF DAMAGE AT NR 11 RIB. AREA OF DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 54-10-1. REMOVED DAMAGE AND WORN PARTS (ANGLE) IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW REPAIR ANGLE IAW 200 51-40-3.
- [SDR 7AHR20130129012](https://openairdocs.org/sdr/7AHR20130129012.md): Rib · worn · Jan 29, 2013 · N842AL · Boeing 737290C · Nacelle/Pylon, Frame/Spar/Rib
  > RT ENGINE COWL HAS AN AREA OF DAMAGE AT NR 10 RIB. AREA OF DAMAGE IS FOUND TO BE OUT OF LIMITS IAW SRM 54-10-1. REMOVED DAMAGED PARTS (ANGLES). FABRICATED NEW REPAIR ANGLES IAW SRM 51-40-3. INSTALLED REPAIR ANGLES IAW SRM 51-40-3.
- [SDR 7AHR20130129011](https://openairdocs.org/sdr/7AHR20130129011.md): Rib · worn · Jan 29, 2013 · N842AL · Boeing 737290C · Nacelle/Pylon, Main Frame
  > RT ENGINE COWL HAS AREA OF DAMAGE, AREA NR 7 RIB. REMOVED DAMAGE RIB ANGLE IAW SRM 51-40-3. FABRICATED NEW REPAIR ANGLE IAW SRM 51-40-3. INSTALLED NEW REPAIR ANGLE TO NR 7 RIB IAW SRM 51-40-3.
- [SDR 7AHR20130129010](https://openairdocs.org/sdr/7AHR20130129010.md): Intercostal · corroded · Jan 29, 2013 · N842AL · Boeing 737290C · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT BS 727A AND 727B AT STRINGER 27L AND 27R. REMOVED INTERCOSTALS AT STRINGER 27L & 27R SRM 51-30-02, UPON FURTHER EVALUATION BOTH INTERCOSTALS WERE FOUND TO HAVE EXTENSIVE CORROSION. IN ADDITION TO THE INTERCOSTALS A WEB AND 2 ANGLE
- [SDR 7AHR20130129009](https://openairdocs.org/sdr/7AHR20130129009.md): Shear Tie · corroded · Jan 29, 2013 · N842AL · Boeing 737290C · Fuselage Internal Mounting Structure
  > CORROSION IN AFT CARGO BS 767 STRINGER 27L TO 27R AT AFT FRAME, SHEAR TIES. REMOVED FASTENERS FOR ACCESS TO CORROSION IAW SRM 51-30-2. CORROSION AT SHEAR TIE IS FOUND TO BE OUT OF LIMITS. CUT OUT AND REMOVED CORRODED SHEAR TIE ANGLE IAW SRM 53-10-4. FABRICA
- [SDR 7AHR20130129008](https://openairdocs.org/sdr/7AHR20130129008.md): Shear Tie · corroded · Jan 29, 2013 · N842AL · Boeing 737290C · Fuselage Internal Mounting Structure
  > EXTERIOR FUSELAGE BELLY, SKIN BULGE AROUND FASTENERS BETWEEN STRINGER 27L AND 27R. REMOVED FASTENERS AT EXTERIOR FUSELAGE SKIN AT BS 747 BETWEEN STRINGER 27L & 27R IAW SRM 51-30-02. FRAME HAS CORROSION DAMAGE BEYOND LIMITS IAW SRM 53-10-1. FABRICATED REPAIR
- [SDR 7AHR20130129007](https://openairdocs.org/sdr/7AHR20130129007.md): Strap · worn · Jan 29, 2013 · N842AL · Boeing 737290C · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE UPPER FIXED COWL HAS A CHAFED STRAP. RUB STRAP DOUBLER FOUND TO BE WORN BEYOUD LIMITS IAW SRM 54-10-1. FABRICATED REPAIR PARTS IAW SRM 51-20-1. INSTALLED STRAP DOUBLER IAW SRM 51-30-2.
- [SDR 7AHR20130129006](https://openairdocs.org/sdr/7AHR20130129006.md): Skin · corroded · Jan 29, 2013 · N842AL · Boeing 737290C · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE BELLY SKIN, BULGE AROUND FASTENERS AT BS 727B BETWEEN STRINGER 27L AND 27R. REMOVED FASTENERS AT EXT FUSELAGE AT BS 727B, DICOVERED FRAME BETWEEN STR 27L & 27R HAS CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED UNSERVICEABLE PARTS 53-10-4.
- [SDR 7AHR20130129005](https://openairdocs.org/sdr/7AHR20130129005.md): Shear Tie · corroded · Jan 29, 2013 · N842AL · Boeing 737290C · Fuselage Internal Mounting Structure
  > LOWER FUESLAGE E/E BAY CORROSION ON SHEAR TIE ANGLE AT BS 312 AT STRINGER 27L, FORWARD OF ACCESS DOOR. REMOVED CORRODED SHEAR TIE ATTACH ANGLE IAW SRM 51-30-2. FABRICATED NEW ATTACH ANGLE IAW SRM 51-20-1. INSTALLED NEW SHEAR TIE ATTACH ANGLE IAW SRM 51-30-2.
- [SDR 7AHR20130129004](https://openairdocs.org/sdr/7AHR20130129004.md): Shim · corroded · Jan 29, 2013 · N842AL · Boeing 737290C · Fuselage Miscellaneous Structure
  > EXTERIOR FUSELAGE, EXTERNAL POWER RECEPTACLE ACCESS DOOR HAS CORRODED SHIMS BENEATH LATCHES ALONG WITH CORRODED HARDWARE. REMOVED CORRODED SHIMS AND HARDWARE, FOUND TO BE OUT OF LIMITS. FABRICATED REPLACEMENT SHIMS IAW SRM 51-20-1. INSTALLED REPLACEMENT SHIMS
- [SDR 7AHR20130129003](https://openairdocs.org/sdr/7AHR20130129003.md): Floor Support · corroded · Jan 29, 2013 · N842AL · Boeing 737290C · Fuselage Miscellaneous Structure
  > FORWARD PIT STATION 385 AT RBL 14 CARGO FLOOR SUPPORT IS CORRODED. REMOVED CORROSION ON FLOOR SUPPORT IAW SRM 51-10-1. CORROSION WAS FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS IAW SRM 53-10-5. INSTALLED REPAIR PARTS IAW 51-30-2 AND 53-10-5.
- [SDR 7AHR20130129002](https://openairdocs.org/sdr/7AHR20130129002.md): Attach Angle · cracked · Jan 29, 2013 · N842AL · Boeing 737290C · Fuselage Main, Attach Fittings
  > MAIN CABIN, LT LOWER AFT BULKHEAD SIDE WALL ATTACH ANGLE CRACKED IN 4 PLACES. FABRICATED REPAIR ANGLE FROM MATERIAL 2024 T3 IAW SRM 51-20-1.
- [SDR 7AHR20130129001](https://openairdocs.org/sdr/7AHR20130129001.md): Floorboard · corroded · Jan 29, 2013 · N842AL · Boeing 737290C · Fuselage Floor Panel
  > FORWARD PIT FLOORBOARD SPLICE BETWEEN NR 1 AND NR 2 FLOORBOARD IS CORRODED AND MISSING NUT PLATES. FORWARD PIT FLOORBOARD SPLICE FOUND TO BE OUT OF LIMITS. FABRICATED FLOORBOARD SPLICE IAW SRM 51-30-5. TREATED AND PRIMED SPLICE IAW SRM 51-10-2. INSTALLED 21 NU
- [SDR 7AHR2011030803](https://openairdocs.org/sdr/7AHR2011030803.md): Skin · dented · Mar 8, 2011 · N842AL · Boeing 737290C · Horizontal Stabilizer, Plate/Skin
  > A DENT WAS FOUND ON THE RT HORIZ STABILIZER LOWER SURFACE BETWEEN STABILIZER STA 120.0 AND 129.0 JUST FORWARD OF THE REAR SPAR. A/Y RATIO DETERMINED THE DENT WAS OUT OF LIMITS. THIS AREA WAS THEN REPAIRED IAW SRM REF 55-10-3, FIG 8. NO OTHER DAMAGE WAS NOTED
- [SDR 7AHR2011021802](https://openairdocs.org/sdr/7AHR2011021802.md): Stringer · corroded · Feb 18, 2011 · N842AL · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, A VISUAL INSP REVEALED CORROSION ON STR 19 LT AT BODY STA 294.5. A 16 IN SECTION OF STRINGER WAS REPLACED IAW SRM REF 53-10-3. NO OTHER DAMAGE WAS NOTED AT THIS LOCATION.
- [SDR 7AHR2011021801](https://openairdocs.org/sdr/7AHR2011021801.md): Stringer · corroded · Feb 18, 2011 · N842AL · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > DURING A C-CHECK, A VISUAL INSP REVEALED CORROSION ON STR 22 LT AT FUSELAGE BODY STA 344. A 20 IN SECTION OF STR WAS REPLACED IAW SRM REF 53-10-3. NO OTHER DAMAGE WAS NOTED AT THIS LOCATION.
- [SDR 2011F00035](https://openairdocs.org/sdr/2011F00035.md): Stringer · corroded · Feb 11, 2011 · N842AL · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > DURING A C-CHECK, A VISUAL INSP REVEALED CORROSION ON STR 22 LT AT FUSELAGE BODY STA 344. A 20 INCH SECTION OF STRINGER WAS REPLACED IAW SRM REF 53-10-3. NO OTHER DAMAGE WAS NOTED AT THIS LOCATION.
- [SDR 2011F00034](https://openairdocs.org/sdr/2011F00034.md): Stringer · corroded · Feb 11, 2011 · N842AL · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > DURING A C-CHECK, A VISUAL INSP REVEALED CORROSION ON STR 19 LT AT FUSELAGE BODY STA 294.5. A 16 INCH SECTION OF STRINGER WAS REPLACED IAW SRM REF 53-10-3. NO OTHER DAMAGE WAS NOTED AT THIS LOCATION.
- [SDR TSAA1031010](https://openairdocs.org/sdr/TSAA1031010.md): Warning Horn · activated · Jun 10, 2010 · N842AL · Boeing 737290C · Central Warning
  > NON-ETOPS CARGO FLIGHT. TAKEOFF WARNING HORN SOUNDED AT THROTTLE UP FOR TAKEOFF. CREW ABORTED TAKEOFF AT 10 KTS. CREW FOUND THE SPEED BRAKE LEVER WAS NOT COMPLETELY IN THE STOWED POSITION. CREW STOWED THE SPEED BRAKE LEVER AND CONTINUED THE FLIGHT WITHOUT F
- [SDR TSAA1077009](https://openairdocs.org/sdr/TSAA1077009.md): Bulkhead · cracked · May 25, 2010 · N842AL · Boeing 737290C · Fuselage Main, Bulkhead
  > A SCHEDULED INSPECTION REVEALED A CRACK AT THE 1ST RIVET AT BS 1016 AFT PRESSURE BULKHEAD AT THE WEB DOME SECTION ALONG STIFFENER/ STR-17L. TRIMMED DOME WEBS ONE FASTENER ROW BELOW EXISTING REPAIR. REMOVED CIRCUMFERENTIAL TEAR STRAP AND DAMAGED WEB DOME SECTI
- [SDR TSAA1077004](https://openairdocs.org/sdr/TSAA1077004.md): Transmitter · inoperative · Feb 17, 2010 · N842AL · Boeing 737290C · Engine Pressure Ratio (EPR)
  > ABORTED TAKEOFF, WHEN ADVANCING POWER FOR TAKEOFF NR 1 EPR MOVED SLOWLY AND ONLY WENT TO 1.50. ON TAXI BACK NR 1 EPR WOULD NOT MOVE. R & R NR1 ENGINE EPR TRANSMITTER IAW MM 77-11-21. GROUND RUN UP OPS & LEAK CK OK. ACFT RETURNED TO SERVICE.
- [SDR TSAA1026003](https://openairdocs.org/sdr/TSAA1026003.md): Bulb · inoperative · Feb 9, 2010 · N842AL · Boeing 737290C · Smoke Detection
  > DURING APPROACH AFT CARGO COMPARTMENT SMOKE LIGHT ILLUMINATED. R & R AFT CARGO SMOKE DETECTOR BULB ASSY. OPS CK OK IAW AMM 26-16-00.
- [SDR TSAA0926013](https://openairdocs.org/sdr/TSAA0926013.md): Control Panel · failed · Dec 7, 2009 · N842AL · Boeing 737290C · Fire Detection
  > NON-ETOPS CARGO FLIGHT. AFTER TAKEOFF PWR WAS SELECTED, OVERHEAT/FIRE ANNUNCIATOR LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND THE CREW RETURNED THE ACFT TO FREIGHT RAMP WITHOUT FURTHER INCIDENT. MX FOUND THAT THE CARGO FIRE DETECTION AND SUPPRESSION PANEL MO
- [SDR TSAA0975015](https://openairdocs.org/sdr/TSAA0975015.md): Duct · failed · Dec 6, 2009 · N842AL · Boeing 737290C · Engine Anti-Icing System
  > NON-ETOPS CARGO FLIGHT, DURING CLIMB, THE CREW NOTED THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATE. NR1 ENGINE EGT REMAINED WITHIN LIMITS. THE NR 1 THROTTLE WAS RETARDED TO IDLE AND THE OVERHEAT LIGHT EXTINGUISHED. ENGINE WAS KEPT AT IDLE AND THE CREW RETURNED
- [SDR EE4Y090186](https://openairdocs.org/sdr/EE4Y090186.md): Floor Support · corroded · Jul 7, 2009 · N842AL · Boeing 737290C · Fuselage Miscellaneous Structure
  > UPPER FUSELAGE, CARGO CABIN AT BS 660 RBL 50 FLOOR SUPPORT CORRODED.
- [SDR EE4Y090185](https://openairdocs.org/sdr/EE4Y090185.md): Stringer · cracked · Jul 1, 2009 · N842AL · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > FUSELAGE TAIL CONE BETWEEN BS 1138 AND BS 1142 STR 5A LT, CRACKED.
- [SDR EE4Y090184](https://openairdocs.org/sdr/EE4Y090184.md): Stringer · cracked · Jun 30, 2009 · N842AL · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > UPPER FUSELAGE CARGO CABIN, LAVATORY AREA BS 303 STR 14L, CRACKED.
- [SDR EE4Y090183](https://openairdocs.org/sdr/EE4Y090183.md): Stringer Clip · cracked · Jun 30, 2009 · N842AL · Boeing 737290C · Fuselage Main, Attach Fittings
  > UPPER FUSELAGE CARGO CABIN AT BS 663 STR 10L CLIP CRACKED.
- [SDR EE4Y090181](https://openairdocs.org/sdr/EE4Y090181.md): Frame · damaged · Jun 30, 2009 · N842AL · Boeing 737290C · Fuselage Main, Frame
  > LOWER FUSELAGE AT BS 219.8, RBL 17.5 FRAME OTBD CHORD DRILLED.
- [SDR EE4Y090179](https://openairdocs.org/sdr/EE4Y090179.md): Stringer Clip · cracked · Jun 30, 2009 · N842AL · Boeing 737290C · Fuselage Main, Attach Fittings
  > UPPER FUSELAGE CARGO CABIN AT BS 747 STR 5R CLIP CRACKED.
- [SDR EE4Y090178](https://openairdocs.org/sdr/EE4Y090178.md): Skin · scratched · Jun 30, 2009 · N842AL · Boeing 737290C · Fuselage Main, Plate/Skin
  > LWR FUSELAGE AT BS 227.8, RBL 17.5, SKIN SCRATCHED.
- [SDR EE4Y090163](https://openairdocs.org/sdr/EE4Y090163.md): Stringer · cracked · Jun 30, 2009 · N842AL · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > UPPER FUSELAGE CARGO CABIN AT BS 503, STR 8L, CRACKED.
- [SDR EE4Y090147A](https://openairdocs.org/sdr/EE4Y090147A.md): Stringer Clip · cracked · Jun 30, 2009 · N842AL · Boeing 737290C · Fuselage Main, Attach Fittings
  > UPPER FUSELAGE,CARGO CABIN AT BS 685 STR 6L, STRINGER CLIP CRACKED.
- [SDR EE4Y090174](https://openairdocs.org/sdr/EE4Y090174.md): Stringer · damaged · Jun 22, 2009 · N842AL · Boeing 737290C · Fuselage Main, Structure
  > LOWER FUSELAGE E&E COMPARTMENT,BETWEEN BS 355 AND BS 365,STR 19R WITH DOUBLE HOLE.
- [SDR EE4Y090177](https://openairdocs.org/sdr/EE4Y090177.md): Web · cracked · Jun 22, 2009 · N842AL · Boeing 737290C · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE, NOSE WHEEL WELL AT BS 250, RBL 2" UPPER WEB CRACKED.
- [SDR EE4Y090175](https://openairdocs.org/sdr/EE4Y090175.md): Shear Tie · cracked · Jun 22, 2009 · N842AL · Boeing 737290C · Fuselage Internal Mounting Structure
  > LOWER FUSELAGE E AND E AT BS 360 BETWEEN STR18R AND 19R, SHEAR TIE CRACKED.
- [SDR EE4Y090173](https://openairdocs.org/sdr/EE4Y090173.md): Angle · cracked · Jun 22, 2009 · N842AL · Boeing 737290C · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE BS 1040 STR 21 ANGLE CRACKED.
- [SDR EE4Y090172](https://openairdocs.org/sdr/EE4Y090172.md): Skin · scratched · Jun 22, 2009 · N842AL · Boeing 737290C · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE AT BS 875.5 STR 17R SKIN WITH SCRATCH.
- [SDR EE4Y090171](https://openairdocs.org/sdr/EE4Y090171.md): Stringer · corroded · Jun 22, 2009 · N842AL · Boeing 737290C · Fuselage Main, Longeron/Stringer
  > LOWER FUSELAGE AT STA 1016 STR 24L END FITTING CORRODED.
- [SDR EE4Y090170](https://openairdocs.org/sdr/EE4Y090170.md): Floor Support · corroded · Jun 22, 2009 · N842AL · Boeing 737290C · Fuselage Miscellaneous Structure
  > UPPER FUSELAGE CARGO CABIN FROM BS 540 TO BS 685, RBL 25 TRANSVERSAL BEAM UPPER FLANGE CORRODED.
- [SDR EE4Y090169](https://openairdocs.org/sdr/EE4Y090169.md): Shear Tie · cracked · Jun 22, 2009 · N842AL · Boeing 737290C · Fuselage Internal Mounting Structure
  > LOWER FUSELAGE FWD CARGO COMPARTMENT BS 380 BETWEEN STR 19 AND MAIN CARGO DOOR CUTOUT, SHEAR TIE CRACKED.
- [SDR EE4Y090168](https://openairdocs.org/sdr/EE4Y090168.md): Skin · corroded · Jun 22, 2009 · N842AL · Boeing 737290C · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE ST BS 500 BETWEEN STR 27R AND 28R,SKIN CORRODED
- [SDR EE4Y090167](https://openairdocs.org/sdr/EE4Y090167.md): Skin · canning · Jun 20, 2009 · N842AL · Boeing 737290C · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE AT BS 973, BETWEEN STR 21L AND 22L, SKIN OIL CANNING.
- [SDR EE4Y090166](https://openairdocs.org/sdr/EE4Y090166.md): Skin · canning · Jun 20, 2009 · N842AL · Boeing 737290C · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE AT BS 963 BETWEEN STR 21L AND 22L, SKIN OIL CANNING.
- [SDR EE4Y090165](https://openairdocs.org/sdr/EE4Y090165.md): Skin · dented · Jun 20, 2009 · N842AL · Boeing 737290C · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE AT BS 950 BETWEEN STR 21L AND 22L, SKIN DENTED.

Next page: https://openairdocs.org/model/boeing-737-290c/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 aircraft_model_key = '737290C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-290c/reports

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