# Service difficulty reports: N944UP, cancelled Aug 4, 2008

A list on [N944UP, cancelled Aug 4, 2008](https://openairdocs.org/deregistered/N944UP-2008-08-04.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 · 100 reports

- [SDR UPS07250122](https://openairdocs.org/sdr/UPS07250122.md): Slide · out of position · Jul 5, 2007 · N944UP · Boeing 72722C · Escape Slide
  > INSPECTION TYPE:N/A EMERGENCY SLIDE TORN OFF CABIN/COCK PIT ENTRY DOOR, UNABLE TO REINSTALL. DEF YBDER N353884. INSTALLED EVAC SLIDE MAIN CABIN DOOR PER MM CHAP 25-60-14-2.
- [SDR UPS07250083](https://openairdocs.org/sdr/UPS07250083.md): Slide · inoperative · Jun 27, 2007 · N944UP · Boeing 72722C · Escape Slide
  > CREW SLIDE FELL OUT OF CONTAINER WHEN THE ENTRY DOOR WAS OPENED. REINSTALLED EVACUATION SLIDE IN THE CONTAINER IAW MM 52-25-60-14-2.
- [SDR UPS07250056](https://openairdocs.org/sdr/UPS07250056.md): Slide · inoperative · Jun 26, 2007 · N944UP · Boeing 72722C · Escape Slide
  > ESCAPE SLIDE IS OUT OF PACK. REINSTALLED EVACUATION SLIDE IAW AMM 25-60-14-2.
- [SDR UPS06248725](https://openairdocs.org/sdr/UPS06248725.md): Slide · out of position · Nov 30, 2006 · N944UP · Boeing 72722C · Escape Slide
  > INSPECTION TYPE: N/A MAIN ENTRY DOOR ESCAPE SLIDE FALLS OUT OF ITS CONTAINER WHEN DOOR IS MOVED. FOUND COMPARTMENTAL COVER LATCH CABLE DISCONNECTED. REPAIRED IAW 25-60-14-2. OPS CK GOOD.
- [SDR UPS06248335](https://openairdocs.org/sdr/UPS06248335.md): Slide · dislodged · Oct 5, 2006 · N944UP · Boeing 72722C · Escape Slide
  > ESCAPE SLIDE FELL OUT OF STORAGE HOUSING IN FLIGHT. ATTEMPTED TO RESTORE SLIDE. REPACKED SLIDE ASSY AS REQUIRED.
- [SDR UPS06247060](https://openairdocs.org/sdr/UPS06247060.md): Frame · cracked · Jun 1, 2006 · N944UP · Boeing 72722C · Fuselage Main, Frame
  > INSPECTION TYPE:C DURING REMOVAL OF FASTENERS TO FACILITATE THE FLOOR SUPPORT REPAIR FOR NRC 100734 CRACK FOUND ON FRAME FOR INNER RADIUS BS1050 RBL 12. CRACKED FRAME AT ABOVE LOCATION REPAIRED IAW SRM 53-10-02 AND SRM 51-4 0-3
- [SDR UPS06247095](https://openairdocs.org/sdr/UPS06247095.md): Spar · cracked · May 26, 2006 · N944UP · Boeing 72722C · Elevator, Spar/Rib
  > INSPECTION TYPE:C ON INSP CRACK DETECTED ON THE LEFT ELEVATOR REAR SPAR STA 138 APPROX. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACK CONFIRMED, ENDS MARKED. ELEVATOR REMOVED IAW MM 27-30-01. NEW ELEVATOR INSTALLED IAW MM 27-30-01. ELEVATOR FRI
- [SDR UPS06247080](https://openairdocs.org/sdr/UPS06247080.md): Floor Support · cracked · May 26, 2006 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C FLOOR SUPPORT FOUND TO BE CRACKED AT BS 1060 LBL 6. DAMAGE CUT OUT IAW SRM 53-10-05. FASTENERS REMOVED IAW SRM 51-30-02. REPAIR PARTS FABRICATED IAW SRM 53-10-05 AND REPROTECTED IAW SRM 51-10- 02. REPAIR PARTS INSTALLED IAW SRM 51-30-02.
- [SDR UPS06247004](https://openairdocs.org/sdr/UPS06247004.md): Skin · cracked · May 26, 2006 · N944UP · Boeing 72722C · Passenger/Crew Doors
  > INSPECTION TYPE:C SUSPECT SKIN CRACK IN AFT AIRSTAIRS SKIN AT THE NR 8 STEP FROM THE BOTTOM POSITION. CARRY OUT NDI AND RECTIFY AS NECESSARY. HFEC CARRIED OUT ON SUSPECT CRACK IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACK CONFIRMED, ENDS MARKED. REPAIR CARRIED
- [SDR UPS06247061](https://openairdocs.org/sdr/UPS06247061.md): Floor Support · cracked · May 25, 2006 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C AFT CARGO BAY CRACK ON FLOOR SUPPORT AT BS 1060 RBL 0. DAMAGED AREA CUT OUT IAW SRM 53-10-05. FASTENERS REMOVED IAW SRM 51-30 -02. REPAIR PARTS FABRICATED IAW SRM 53-10-05. REPAIR PARTS REPROTECTED IAW SRM 51-10-02. REPAIR PARTS INSTALLED IA
- [SDR UPS06247055](https://openairdocs.org/sdr/UPS06247055.md): Web · cracked · May 25, 2006 · N944UP · Boeing 72722C · Entrance Stairs
  > INSPECTION TYPE:C AFT AIRSTAIRS RT LIGHTENING HOLE CRACKED. AREA MARKED, PLS REPAIR IAW SRM REPAIR CARRIED OUT IAW SRM 51-40-2, 51-10-2 & 51-30-2.
- [SDR UPS06247054](https://openairdocs.org/sdr/UPS06247054.md): Web · cracked · May 25, 2006 · N944UP · Boeing 72722C · Entrance Stairs
  > INSPECTION TYPE:C CRACK ON THE LEFT WEB IN THE AFT AIRSTAIRS AREA MARKED. REPAIR IAW SRM REPAIR CARRIED OUT IAW SRM 51-40-2, 51-10-2 & 51-30-2.
- [SDR UPS06247045](https://openairdocs.org/sdr/UPS06247045.md): Door Frame · cracked · May 25, 2006 · N944UP · Boeing 72722C · Cargo/Baggage Doors
  > INSPECTION TYPE:C AFT CARGO DOOR SUSPECT CRACK ON FRAME AT UPPER AFT DOOR STOP. AREA CLEANED AND REINSPECTED, CRACK CONFIRMED VISUALLY AT AFT UPPER DOOR STOP CUTOUT. DUE TO EXCESSIVE WORK REQUIRED TO REPAIR, DOOR TO BE REPLACED.
- [SDR UPS06247067](https://openairdocs.org/sdr/UPS06247067.md): Floor Support · corroded · May 24, 2006 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C AFT CARGO BAY BS 1110 RBL20 FLOOR SUPPORT CORRODED AT ANCHOR NUTS LOCATION. TO GAIN ACCESS FLOOR PANEL AND SCUFF PLATE AT CARGO DOOR CUT OUT REMOVED IAW SRM 51-30-02. DAMAGE FOUND TO BE OUTSIDE LIMITS IAW SRM 53-10* 0-01. DAMAGED SECTION RE
- [SDR UPS06247005](https://openairdocs.org/sdr/UPS06247005.md): Angle · corroded · May 24, 2006 · N944UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C DURING RECTIFICATION OF NRC 100332 ADJACENT ANGLE OF FWD CARGO BLKD UP PER SECTION BS 680 RBL 30 TO 40 FOUND TO BE CORRODED AT ANCHOR NUT LOCATIONS. ON CLEAN UP CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AFT BLKD ANGLE IAW SRM 51-30-2. R
- [SDR UPS06247079](https://openairdocs.org/sdr/UPS06247079.md): Support Angle · cracked · May 23, 2006 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C BS660 LT CRACK ON OB SUPPORT ANGLE FOR RAM AIR INTAKE DUCTING AT FASTENER LOCATION. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-30-02. FABRICATED SUPPORT ANGLE AND HEAT TREATED IAW SRM 51-20-1. INSTALLED SUPPORT ANGLE IAW SRM 5 1-30-02.
- [SDR UPS06247078](https://openairdocs.org/sdr/UPS06247078.md): Support · chafed · May 23, 2006 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C ON REMOVAL OF FLOW VENTURI SENSE LINE CROSS SUPPORT STRUCTURAL MEMBER AT LBL 40 BETWEEN BS 1203 AND 1223 FOUND CHAFFED. CROSS STRUCTURAL MEMBER REMOVED IAW SRM 51-30-02. REPLACEMENT REQUIRED. INSTALLED NEW CROSS STRUCTURAL MEMBER IAW SRM 51
- [SDR UPS06247059](https://openairdocs.org/sdr/UPS06247059.md): Spar · cracked · May 23, 2006 · N944UP · Boeing 72722C · Elevator, Spar/Rib
  > INSPECTION TYPE:C X-RAY INSPECTION HAS DETECTED 2 SUSPECT CRACKS ON INSPAR RIBS LOCATED BETWEEN ELEVATOR STATION 99.50-136.50 DISPLACED UPPER ELEVATOR SKIN FROM BS 99.5 TO BS 136.5 IAW SRM 51-30- 02 AND REMOVED REPAIR DOUBLER FROM LOWER SKIN. HFEC CARRIED
- [SDR UPS06247053](https://openairdocs.org/sdr/UPS06247053.md): Rib · cracked · May 23, 2006 · N944UP · Boeing 72722C · Elevator, Spar/Rib
  > INSPECTION TYPE:C X-RAY INSP DETECTED ONE SUSPECT CRACK ON THE LT ELEVATOR INTERNAL RIB LOCATED BETWEEN ELEV STA 179.50 - 205.50. ELEV BEYOND ECONOMIC REPAIR REF NRC 100783 FOR REPLACEMENT OF LT ELEVATOR.
- [SDR UPS06247056](https://openairdocs.org/sdr/UPS06247056.md): Casting · cracked · May 19, 2006 · N944UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE:C LEFT O/B FOREFLAP I/B SECTION HAS CRACKS FROM FASTENER HOLES. PAINT STRIPPED AREA IAW MM 51-20-01. HFEC INSP CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4. RESULT - CRACK CONFIRMED. FOR FLAP REPLACEMENT REF NRC 100295 DUE TO I/B CASTING N
- [SDR UPS06247046](https://openairdocs.org/sdr/UPS06247046.md): Skin · delaminated · May 18, 2006 · N944UP · Boeing 72722C · Spoilers
  > INSPECTION TYPE:C NR 9 SPOILER DELAM ON LOWER SURFACE AT O/B FWD CORNER. DELAMINATED SKIN REMOVED AT O/B FWD CORNER IAW SRM 51-40-20. DELAM LIMITS FOUND TO BEYOND ECONOMIC REPAIR. SPOILER REPLACED.
- [SDR UPS06246109](https://openairdocs.org/sdr/UPS06246109.md): Light · malfunctioned · Jan 10, 2006 · N944UP · Boeing 72722C · Emergency Lighting
  > DURING WEEKEND CK FOUND MAIN ENTRY EMERGENCY LIGHTS VERY DIM UPON TEST ING. REPLACED LIGHT ASSEMBLY.
- [SDR UPS06245927](https://openairdocs.org/sdr/UPS06245927.md): Light · failed · Jan 10, 2006 · N944UP · Boeing 72722C · Emergency Lighting
  > MAIN ENTRY EMERGENCY LIGHT DIM. REPLACED LIGHT ASSEMBLY. REF 33-50-67.
- [SDR UPS04243613](https://openairdocs.org/sdr/UPS04243613.md): Light · inoperative · Dec 20, 2004 · N944UP · Boeing 72722C · Emergency Lighting
  > FWD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AS PER MM 33-50-01. F/C OK.
- [SDR UPS04243257](https://openairdocs.org/sdr/UPS04243257.md): Floor Panel · cracked · Sep 24, 2004 · N944UP · Boeing 72722C · Fuselage Floor Panel
  > INSPECTION TYPE: C, E/E FLOOR PANEL RIGHT SIDE BS 440 TO 400 HAS ONE CRACK. CRACK STOP DRILLED IAW 51-10-1. HFEC CARRIED OUT IAW NDT MM 51-00-00. RESULT - CRACK CONTAINED. AREA REPAIRED IAW SRM 51-40-2.
- [SDR UPS04243258](https://openairdocs.org/sdr/UPS04243258.md): Pressure Panel · cracked · Sep 21, 2004 · N944UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C, LT NOSE WHEEL WELL HAS CRACKS ON FASTENER ROW, BS 243, 4 INCHES BELOW FWD PRESSURE PANEL OPENING. HFEC CARRIED OUT IAW NDT MM 51-00-00. RESULT - CRACKS CONFIRMED. FILLER AND DOUBLER FABRICATED AND INSTALLED IAW SRM 51-40-02.
- [SDR UPS04243273](https://openairdocs.org/sdr/UPS04243273.md): Fitting · cracked · Sep 20, 2004 · N944UP · Boeing 72722C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C, SUSPECT CRACK FROM LT TERMINAL FITTING FOR STABILIZING LINK LWR IN TAIL SKID COMPARTMENT. INSTALLED NEW TERMINAL FITTING IAW SRM 51-30-02.
- [SDR UPS04243272](https://openairdocs.org/sdr/UPS04243272.md): Fitting · cracked · Sep 20, 2004 · N944UP · Boeing 72722C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C, SUSPECT CRACK FROM RIGHT TERMINAL FITTING FOR STABILIZING LINK LWR IN TA TAIL SKID COMPARTMENT. INSTALLED NEW TERMINAL FITTING IAW SRM 51-30-02.
- [SDR UPS04243259](https://openairdocs.org/sdr/UPS04243259.md): Bolt · damaged · Sep 17, 2004 · N944UP · Boeing 72722C · Fasteners
  > INSPECTION TYPE: C, NR 3 ENGINE FWD AND AFT CRANE BEAMS SHOULDER BOLTS HAVE CAD PLATING DAMAGE. BOLTS REPLACED IAW MM 71-10-32.
- [SDR UPS04243278](https://openairdocs.org/sdr/UPS04243278.md): Skin Panel · corroded · Sep 16, 2004 · N944UP · Boeing 72722C · Elevator Structure
  > INSPECTION TYPE: C, SURFACE CORROSION ON LT ELEVATOR LOWER SKIN AT BUTT JOINT BETWEEN 5TH AND 6TH ACCESS PANELS FROM OUTBOARD. CORROSION REMOVED IAW SRM 51-10-1. BLEND OUT AREA FOUND TO BE WITHIN LIMITS IAW SRM 55-20-1. AREA REPROTECTED IAW SRM 51-10-2.
- [SDR UPS04243251](https://openairdocs.org/sdr/UPS04243251.md): Panel · cracked · Sep 13, 2004 · N944UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C, HULL PRESSURE LEAK IN NLG WHEEL WELL CEILING PANEL (DUE TO CRACKING) AT BS 260 LBL 20. DAMAGED AREA REMOVED AS REQUIRED IAW SRM 51-40-2. HFEC CARRIED OUT - NO DEFECTS FOUND. REPAIR PARTS FABRICATED IAW SRM 51-40-2. REPAIR PARTS INSTALLED
- [SDR UPS04243277](https://openairdocs.org/sdr/UPS04243277.md): Web · cracked · Sep 12, 2004 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, SUSPECT CRACK ON RIGHT 950 FITTING HORIZONTAL WEB WL 202 APPROX. REPAIR CARRIED OUT IAW SRM 51-10-06, 51-10-02 & AAAE EO 2004-085-001. UPS ENGINEERING FILE 727-53-20166.
- [SDR UPS04243275](https://openairdocs.org/sdr/UPS04243275.md): Fitting · cracked · Sep 12, 2004 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, EVIDENCE OF CRACK ANGLE FITTING RIGHT SIDE ON SHELF MID WAY UP 950 AFT RIGHT WALL. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-10-01, 51-10-02, 51-30-2 & SOH M 20-10-03 FIG 9.
- [SDR UPS03240690](https://openairdocs.org/sdr/UPS03240690.md): Hinge Fitting · cracked · Apr 30, 2003 · N944UP · Boeing 72722C · Spoilers
  > INSPECTION TYPE: C&SI, SUSPECT CRACK FOUND ON NR 5 SPOILER CENTRE HINGE FITTING HFEC INSP. CARRIED OUT ON NR 5 SPOILER CENTER HINGE FITTING IAW B727 N DTM PT 6 51-00-00 FIG 4 RESULT: CRACK CONFIRMED. CENTER HINGE FITTI NG REPLACED IAW SRM 51-30-02
- [SDR UPS03240664](https://openairdocs.org/sdr/UPS03240664.md): Frame · corroded · Apr 28, 2003 · N944UP · Boeing 72722C · Wing Spar
  > INSPECTION TYPE: C&SI, FRAME ASSY ON LWR SURFACE OF APU EXHAUST PANEL ON RT WING IS CORRODED. FRAME ASSY REPLACED IAW DRAWING 6562837 & SRM 51-30-32
- [SDR UPS03240672](https://openairdocs.org/sdr/UPS03240672.md): Support · cracked · Apr 24, 2003 · N944UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE: C&SI, RT RAM AIR INTAKE DOOR SUPPORT BRACKET FOUND CRACKED AT BS 600 S25R. DOOR SUPPORT BRACKET FABRICATED IAW SRM 51-20-1 FIG 7, NEW BRACKET RE-PROTECTED IAW SRM 51-10-02 NEW DOOR SUPPORT AND FASTENERS RE-INSTALLED IAW SRM 51-30-02
- [SDR UPS03240686](https://openairdocs.org/sdr/UPS03240686.md): Rib · corroded · Apr 23, 2003 · N944UP · Boeing 72722C · Aerodynamic Fairings
  > INSPECTION TYPE: C&SI, FUSELAGE FAIRING NR 3430, FWD FORMED SECTION SUPPORT RIB HAS EVIDENCE OF HEAVY CORROSION UNDER ANCHOR NUT PLATES, JUST FWD OF GRND MOVER DOOR CUT OUT DOOR REMOVED IAW SRM 51-30-02. FRAME REMOVED IAW SRM 51-30-02. CORR OSION REMOVE
- [SDR UPS03240665](https://openairdocs.org/sdr/UPS03240665.md): Skin · cracked · Apr 18, 2003 · N944UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C&SI, RT MLG DOOR, DOOR SKIN ON O/B SECTION OF DOOR ASSY CRACKED BS 910 AREA OF CRACKED SKIN TRIMMED OUT IAW SRM 52-80-02. HFEC INSP. CARRI ED OUT AROUND CUTOUT AT R/H MLG DOOR SKIN ON O/B SECTION OF DOOR ASS Y IAW B727 NDTM PT 6 510000 FIG
- [SDR UPS03240685](https://openairdocs.org/sdr/UPS03240685.md): Door Frame · cracked · Apr 17, 2003 · N944UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE: C&SI, SUSPECT CRACK AT NR 1 STOP FITTING CUT OUT ON FWD FRAME OF AFT CARGO DOOR CUTOUT. REPAIR CARRIED OUT IAW SRM 51-30-02 & SMRO EO 2003-025-021 UPS ENGINEERING FILE NO. B727-5330-18744-A
- [SDR UPS03240641](https://openairdocs.org/sdr/UPS03240641.md): Angle · cracked · Apr 17, 2003 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C&SI, CRACK ON ANGLE, AFT CARGO DOOR INTERIOR, ABOVE AFT DOOR STOP. REMOVED ANGLE FROM DOOR INTERIOR IAW SRM 51-30-2 FABRICATED NEW ANGL E IAW SRM 51-20-1 FIG 7 INSTALLED NEW ANGLE IAW SRM 51-30-2
- [SDR UPS03240640](https://openairdocs.org/sdr/UPS03240640.md): Skin · cracked · Apr 17, 2003 · N944UP · Boeing 72722C · Cargo/Baggage Doors
  > INSPECTION TYPE: C&SI, CRACK ON AFT CARGO DOOR INNER SKIN AT HOLE CUT OUT FOR BALANCE MECHANISM CABLE PULLEY. STOP DRILLED HOLE IAW SRM 51-10-1 REPAIR WAS THEN CARRIED OUT IAW SR M 51-40-2 REPROTECTED IAW SRM 51-10-2
- [SDR UPS03240639](https://openairdocs.org/sdr/UPS03240639.md): Panel · eroded · Apr 17, 2003 · N944UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C&SI, AIRSTAIRS COMPARTMENT, CLOSE OUT PANEL AT STA 1223 LOBE THAT JOINS TO EXTERNAL SKIN IS SHOWING SIGNS OF ERROSION ALONG ITS EDGE ON LT SIDE. AREA REPAIRED IAW SRM 51-40-3 FIG 1
- [SDR UPS03240692](https://openairdocs.org/sdr/UPS03240692.md): Carriage · corroded · Apr 16, 2003 · N944UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE: C&SI, NR 6 FLAP CARRIAGE SPINDLE INTERNALLY CORRODED. NR 6 FLAP CARRIAGE REPLACED IAW OHM 57-58-02 & OHM 57-52-01 REF. TC C5 7-581-04-4D FOR INST. & DUAL
- [SDR UPS03240687](https://openairdocs.org/sdr/UPS03240687.md): Panel · contaminated · Apr 15, 2003 · N944UP · Boeing 72722C · Spoilers
  > INSPECTION TYPE: C&SI, AFTER X-RAY INSP. NR 9 SPOILER FOUND TO HAVE WATER INGRESS AND CELL DISTORTATION SPOILER PANEL REPLACED IAW MM 27-61-01 & MM 27-62-01
- [SDR UPS03240670](https://openairdocs.org/sdr/UPS03240670.md): Butt Joint · damaged · Apr 15, 2003 · N944UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C&SI NDT INSP. HAS INDICATION OF MATERIAL LOSS AT BS 1080 BUTT JOINT BETW EEN S2L & 2R. VISUAL INSP. CARRIED OUT CORROSION FOUND TO EXTEND UP TO S3L NEW CUT OUT LINE MADE IAW 69-62161 S3L REPAIR CARRIED OUT IAW DRAWINGS 69-6 2161 & UPS EO B72
- [SDR UPS03240668](https://openairdocs.org/sdr/UPS03240668.md): Frame · cracked · Apr 15, 2003 · N944UP · Boeing 72722C · Fuselage Main, Frame
  > INSPECTION TYPE: C&SI, SUSPECT CRACK ON FRAME ADJACENT TO HINGE STRUCTURE AT FWD END OF FWD CARGO BAY DOOR. ON REMOVAL OF STIFFENER IN PREPARATION FOR REPAIR A NEW CRACK WAS FO UND WHICH WAS OUTSIDE THE PERMITED REPAIR AREA. FRAME WAS REMOVED IAW SRM 51-30-0
- [SDR UPS03240688](https://openairdocs.org/sdr/UPS03240688.md): Frame · corroded · Apr 14, 2003 · N944UP · Boeing 72722C · Fuselage Main, Frame
  > INSPECTION TYPE: C&SI, CORROSION ON FRAME TIE ANGLE BS 351.2 S24L - S25L. DAMAGE REMOVED IAW SRM 51-10-01 FOUND OUTSIDE LIMITS. REPAIR SECTIO N FABRICATED IAW FLAP PATTERN LAYOUT AS PER SRM 51-20-1.
- [SDR UPS03240671](https://openairdocs.org/sdr/UPS03240671.md): Floorbeam · corroded · Apr 14, 2003 · N944UP · Boeing 72722C · Fuselage Main, Floor Beam
  > INSPECTION TYPE: C&SI, CORROSION UNDER ANCHOR CLIP ON LWR SIDE OF FLOORBEAM TOP STRUCTURE BS 344 LBL 12 APPROX. REPAIR CARRIED OUT IAW SRM 53-10-8 FIG 7
- [SDR UPS03240666](https://openairdocs.org/sdr/UPS03240666.md): Attach Fitting · cracked · Apr 14, 2003 · N944UP · Boeing 72722C · Passenger/Crew Doors
  > INSPECTION TYPE: C&SI, RT MLG WING DOOR ACTUATING ROD ATTACH FITTING CRACKED FITTING REPLACED IAW EO B727-3210-2583-G APP. D, E, F & G
- [SDR UPS03240654](https://openairdocs.org/sdr/UPS03240654.md): Web · cracked · Apr 14, 2003 · N944UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C&SI, NOSE WHEEL WELL LT SIDE AT STA 992 WL 140 TWO SMALL CRACKS ON HORIZONTAL WEB. HORIZONTAL WEB REMOVED & REPLACED IAW SRM 51-20-01 & 51-30-02

Next page: https://openairdocs.org/deregistered/N944UP-2008-08-04/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 = 'N944UP' AND deregistration_id = 'N944UP-2008-08-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N944UP-2008-08-04/reports

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